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ICE AND RAIN PROTECTION

Operation

Aircraft Operations Manual

11.2

PAGE

CONDITIONS

NORMAL PROCEDURES

2.2

DEFINITIONS
AND FOD
PREVENTION

DEFINITIONS
Definition of icing conditions for engine anti

−

icing operation

For engine anti

−

ice system operation, icing conditions exist whenever the out-

side air temperature (OAT) or static air temperature (SAT) is + 5 degrees C
(Plus 5

C) (+10 according to FAA AD 96

−

04 R1 and 2008

−

11) or colder

and:

−

There is any type of visible moisture present (such as clouds, fog with visibil-
ity of one mile or less, rain, snow, sleet, ice crystals); or

−

When on the ground, there is standing water, slush, or snow (hard packed
snow excluded) on the ramps, taxiways or runways.

When anticipating engine anti

−

ice operation turn on engine anti

−

ice early. Turn-

ing engine anti

−

ice on well in advance will preheat the surface and thereby pre-

vent ice formation. Turn engine anti

−

ice on if there is any possibility that icing

conditions exist.

Definition of icing conditions for propeller de

−

icing system operation

For propeller de

−

ice system operation, icing conditions exist when the OAT or

SAT is

−

5 degrees C (Minus 5

C) or colder and any ice accretion is observed on

any part of the aircraft.

Definition of icing conditions for operation of wing and stabilizer de

−

ic-

ing boots and for adherence to minimum airspeed and autopilot/flight di-
rector limitations for icing conditions

For operation of wing and stabilizer de

−

icing boots and for adherence to mini-

mum airspeed and autopilot/flight director limitations for icing conditions, icing
conditions exist when:

−

The OAT or SAT is +5 degrees C (Plus 5

C) or colder and there is any type

of visible moisture present (such as clouds, fog with visibility of one mile or
less, rain, snow, sleet, ice crystals); or

−

Any amount of ice is observed on any part of the aircraft; or

−

If it is not certain that there is no ice accumulation on the aircraft.

FOD PREVENTION

Ice must never be allowed to build up on the engine air intake lips or intake. Once
ice formation occurs, turning on anti

−

ice may free the ice build

−

up in chunks that

could be sucked through the engine compressor, possibly causing Foreign Object
Damage (FOD) and a power interruption.

CAUTION

DO NOT RELY ON AIRFRAME VISUAL ICING CUES TO TURN ENGINE
ANTI

−

ICE ON. USE THE TEMPERATURE AND VISUAL MOISTURE CRI-

TERIA SPECIFIED FOR ICING CONDITIONS.

(Cont’d)

Dec 01/20

Содержание 340B

Страница 1: ...y and confidential to Saab AB and may not a be used for any purpose other than those for which it was supplied b be copied or reproduced in whole or in part without the prior written consent of Saab A...

Страница 2: ...THIS PAGE INTENTIONALLY LEFT BLANK...

Страница 3: ...fore inserting this revision ensure that Revision No 58 Jun 01 20 is incorporated Update the manual according to the revised List of Effective Pages R revised to be replaced D deleted to be removed N...

Страница 4: ...Aircraft Operations Manual EXTENDED WINGTIPS PAGE 2 Dec 01 20 THIS PAGE INTENTIONALLY LEFT BLANK...

Страница 5: ...v 06 98 52 Dec 01 16 30 Jun 24 99 53 Jun 01 17 31 Oct 15 99 54 Dec 01 17 32 Feb 02 01 55 Jun 01 18 33 Oct 05 01 56 Jun 01 19 34 Dec 03 01 57 Sep 30 19 35 Sep 06 02 58 Jun 01 20 36 Dec 15 03 59 Dec 01...

Страница 6: ...Aircraft Operations Manual EXTENDED WINGTIPS PAGE 2 Dec 01 20 THIS PAGE INTENTIONALLY LEFT BLANK...

Страница 7: ...ion revision 58 Jun 01 20 8 1 2 Text added to highlight who controls the aircraft after pitch discon nect 3 4 Page shift due to new text on page 2 11 2 2 Text relocated on page 13 1 13 Power lever ang...

Страница 8: ...ery will be removed from the EADI in the event of large difference in source of attitude 24 2 E4 1 00 Text added to highlight who controls the aircraft after pitch discon nect 25 12 7 Text added to in...

Страница 9: ...ASON FOR CHANGE CODE PAGES 32 2 1 19 20 New pages with new tables for all engines climb gradient metric 32 2 2 19 20 New pages with new tables for all engines climb gradient impe rial 37 3 5 E4 1 15 T...

Страница 10: ...Aircraft Operations Manual EXTENDED WINGTIPS PAGE 4 Dec 01 20 THIS PAGE INTENTIONALLY LEFT BLANK...

Страница 11: ...s necessary Flight Ops Action Date Received V To be included in Rev dated V In process V Rejected reason MANUAL USER COMMENTS on omissions procedures etc Aircraft Operations Manual From Date Phone Fax...

Страница 12: ...Aircraft Operations Manual Manual User Comments PAGE 2 Jun 01 17 THIS PAGE INTENTIONALLY LEFT BLANK...

Страница 13: ...h the LFV approved Airplane Flight Manual AFM the AFM shall apply 3 MANUAL LAYOUT The manual is divided into three parts each con tained in a separate binder 3 1 Part 1 The first binder is applicable...

Страница 14: ...es 25 Flight Procedures 26 Power Settings 27 Speeds 28 Takeoff 29 Service Ceiling 30 Landing 31 Range 32 Climb Cruise Descent 33 Special Range 34 Performance Supplements 35 Line Checks 36 Appendices 3...

Страница 15: ...used as the example shows Prefix Explanation S Standard equipment S1 Different standards S2 Different standards O Optional equipment O1 Different options O2 Different options C Collins equipment C I...

Страница 16: ...INTRODUCTION Aircraft Operations Manual INTRO PAGE 4 THIS PAGE INTENTIONALLY LEFT BLANK Dec 01 16...

Страница 17: ...R 19 Dec 01 20 R 20 Dec 01 20 R 21 Dec 01 20 R 22 Dec 01 20 R 23 Dec 01 20 R 24 Dec 01 20 R 25 Dec 01 20 R 26 Dec 01 20 R 27 Dec 01 20 R 28 Dec 01 20 R 29 Dec 01 20 R 30 Dec 01 20 LEP Part 2 R 17 Dec...

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Страница 20: ...un 01 18 KO 3 Jun 01 18 KO 4 Jun 01 18 4 4 1 S1 1 Dec 01 15 S1 2 Dec 01 15 S1 3 Dec 01 15 S1 4 Dec 01 15 S1 5 Dec 01 15 S1 6 Dec 01 15 S1 7 Dec 01 15 S1 8 Dec 01 15 S2 1 Dec 01 15 S2 2 Dec 01 15 S2 3...

Страница 21: ...01 19 36 Jun 01 19 37 Jun 01 19 38 Jun 01 19 39 Jun 01 19 40 Jun 01 19 5 2 1 Apr 01 15 2 Apr 01 15 3 Apr 01 15 4 Apr 01 15 TAB DIV 6 6 1 Apr 01 15 2 Apr 01 15 6 1 1 1 Apr 01 15 2 Apr 01 15 6 2 1 1 Apr...

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Страница 23: ...V 11 11 1 Apr 01 15 2 Apr 01 15 11 1 1 Jun 01 17 2 Jun 01 17 3 Jun 01 17 4 Jun 01 17 5 Jun 01 17 6 Jun 01 17 7 Jun 01 17 8 Jun 01 17 9 Jun 01 17 10 Jun 01 17 S1 11 Jun 01 17 S1 12 Jun 01 17 S2 11 Jun...

Страница 24: ...15 3 Jun 30 15 4 Jun 30 15 5 Jun 30 15 6 Jun 30 15 12 2 1 1 Apr 01 15 2 Apr 01 15 3 Apr 01 15 4 Apr 01 15 12 3 1 S1 1 Apr 01 15 S1 2 Apr 01 15 S2 1 Apr 01 15 S2 2 Apr 01 15 O1 1 Apr 01 15 O1 2 Apr 01...

Страница 25: ...1 15 6 Apr 01 15 14 2 1 1 Jun 30 15 2 Jun 30 15 3 Jun 01 20 4 Jun 30 15 5 Jun 30 15 6 Jun 30 15 7 Jun 30 15 8 Jun 30 15 14 3 1 S 1 Apr 01 15 S 2 Apr 01 15 O 1 Apr 01 15 O 2 Jun 01 20 S1 1 Apr 01 15 S1...

Страница 26: ...O 13 Apr 01 15 O 14 Apr 01 15 O 15 Apr 01 15 O 16 Jun 01 20 O 17 Apr 01 15 O 18 Apr 01 15 15 2 0 1 Jun 01 20 2 Apr 01 15 15 2 1 C 1 Jun 01 17 C 2 Jun 01 17 K 1 Jun 01 17 K 2 Jun 01 17 KO 1 Jun 01 17 K...

Страница 27: ...4 Apr 01 15 K 1 Apr 01 15 K 2 Apr 01 15 K 3 Apr 01 15 K 4 Apr 01 15 KO 1 Apr 01 15 KO 2 Apr 01 15 KO 3 Apr 01 15 KO 4 Apr 01 15 15 5 1 S 1 Apr 01 15 S 2 Apr 01 15 S 3 Apr 01 15 S 4 Apr 01 15 S 5 Apr 0...

Страница 28: ...O2 3 Sep 30 19 CO2 4 Sep 30 19 CO2 5 Sep 30 19 CO2 6 Sep 30 19 K 1 Sep 30 19 K 2 Sep 30 19 K 3 Sep 30 19 K 4 Sep 30 19 KO 1 Sep 30 19 KO 2 Sep 30 19 KO 3 Sep 30 19 KO 4 Sep 30 19 15 6 2 C 1 Sep 30 19...

Страница 29: ...2 9 Dec 01 16 O2 10 Dec 01 16 O3 1 Dec 01 16 O3 2 Dec 01 16 O3 3 Dec 01 16 O3 4 Dec 01 16 O3 5 Dec 01 16 O3 6 Dec 01 16 O3 7 Dec 01 16 O3 8 Dec 01 16 O3 9 Dec 01 16 O3 10 Dec 01 16 15 9 2 O 1 Apr 01 1...

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Страница 31: ...1 Apr 01 15 2 Apr 01 15 3 Apr 01 15 4 Apr 01 15 19 5 1 1 Apr 01 15 2 Apr 01 15 3 Apr 01 15 4 Apr 01 15 5 Apr 01 15 6 Apr 01 15 7 Apr 01 15 8 Apr 01 15 9 Apr 01 15 10 Apr 01 15 11 Apr 01 15 12 Apr 01...

Страница 32: ...01 15 S3 3 Apr 01 15 S3 4 Apr 01 15 S3 5 Apr 01 15 S3 6 Apr 01 15 7 Apr 01 15 8 Apr 01 15 19 7 1 1 Jun30 15 2 Jun30 15 3 Jun30 15 4 Jun30 15 5 Jun30 15 6 Jun30 15 7 Jun30 15 8 Jun30 15 9 Jun30 15 10...

Страница 33: ...30 19 50 N4 Sep 30 19 00 N5 Sep 30 19 10 N5 Jun 01 20 20 N5 Sep 30 19 00 N6 Sep 30 19 00 N7 Sep 30 19 10 N7 Sep 30 19 00 N8 Sep 30 19 22 2 1 Sep 30 19 2 Sep 30 19 3 Sep 30 19 4 Sep 30 19 5 Sep 30 19 6...

Страница 34: ...un 01 19 00 A2 9 Jun 01 19 10 A2 9 exp Jun 01 19 10 A2 9 Jun 01 19 00 A2 10 exp Jun 01 19 00 A2 10 Jun 01 19 10 A2 10 exp Jun 01 19 10 A2 10 Jun 01 19 00 A2 11 exp Jun 01 19 00 A2 11 Jun 01 20 00 A2 1...

Страница 35: ...17 00 A6 12 Dec 01 17 A7 0 Jun 01 16 00 A7 1 exp Jun 01 16 00 A7 1 Jun 01 16 00 A7 2 exp Jun 01 16 00 A7 2 Jun 01 16 00 A7 3 exp Jun 01 16 00 A7 3 Jun 01 16 00 A7 4 exp Jun 01 16 00 A7 4 Jun 01 16 00...

Страница 36: ...5 1 Jun 01 16 10 A15 1 exp Jun 01 16 10 A15 1 Jun 01 16 A16 0 Jun 01 16 00 A16 1 exp Jun 01 16 00 A16 1 Jun 01 16 00 A16 2 exp Jun 01 16 00 A16 2 Jun 01 16 A17 0 Jun 01 16 00 A17 1 exp Jun 01 16 00 A1...

Страница 37: ...8 10 E3 3 Jun 01 18 00 E3 4 exp Jun 01 20 00 E3 4 Jun 01 20 00 E3 5 exp Jun 01 20 00 E3 5 Jun 01 20 10 E3 5 exp Jun 01 20 10 E3 5 Jun 01 20 00 E3 6 exp Jun 01 20 00 E3 6 Jun 01 20 10 E3 6 exp Jun 01 2...

Страница 38: ...5 2 Apr 01 15 TAB DIV 25 25 1 Apr 01 15 2 Jun 01 20 25 1 1 Jun 01 19 2 Jun 01 19 3 Jun 01 19 4 Jun 01 19 5 Jun 01 19 6 Jun 01 19 7 Jun 01 19 8 Jun 01 19 9 Jun 01 19 10 Jun 01 19 11 Jun 01 19 12 Jun 01...

Страница 39: ...01 15 S1 4 Apr 01 15 S1 5 Apr 01 15 S1 6 Apr 01 15 S2 1 Apr 01 15 S2 2 Apr 01 15 S2 3 Apr 01 15 S2 4 Apr 01 15 S2 5 Apr 01 15 S2 6 Apr 01 15 26 4 1 Apr 01 15 2 Apr 01 15 3 Apr 01 15 4 Apr 01 15 5 Apr...

Страница 40: ...Jun 01 17 12 Jun 01 17 13 Jun 01 17 14 Jun 01 17 TAB DIV 28 28 1 Apr 01 15 2 Apr 01 15 28 1 1 Apr 01 15 2 Apr 01 15 3 Apr 01 15 4 Apr 01 15 5 Apr 01 15 6 Apr 01 15 7 Apr 01 15 8 Apr 01 15 9 Apr 01 15...

Страница 41: ...pr 01 15 19 Apr 01 15 20 Apr 01 15 21 Apr 01 15 22 Apr 01 15 23 Apr 01 15 24 Apr 01 15 28 5 1 1 Apr 01 15 2 Apr 01 15 3 Apr 01 15 4 Apr 01 15 5 Apr 01 15 6 Apr 01 15 7 Apr 01 15 8 Apr 01 15 9 Apr 01 1...

Страница 42: ...1 1 Dec 01 15 S1 2 Dec 01 15 S2 1 Dec 01 15 S2 2 Dec 01 15 3 Dec 01 15 4 Dec 01 15 29 4 1 S1 1 Dec 01 15 S1 2 Dec 01 15 S1 3 Dec 01 15 S1 4 Dec 01 15 S2 1 Dec 01 15 S2 2 Dec 01 15 S2 3 Dec 01 15 S2 4...

Страница 43: ...1 31 1 Apr 01 15 2 Apr 01 15 31 1 1 1 Jun 01 20 2 Apr 01 15 3 Apr 01 15 4 Apr 01 15 5 Apr 01 15 6 Apr 01 15 7 Apr 01 15 8 Apr 01 15 9 Apr 01 15 10 Apr 01 15 31 1 2 1 Apr 01 15 2 Apr 01 15 3 Apr 01 15...

Страница 44: ...15 8 Apr 01 15 32 3 2 1 Apr 01 15 2 Apr 01 15 3 Apr 01 15 4 Apr 01 15 5 Apr 01 15 6 Apr 01 15 7 Apr 01 15 8 Apr 01 15 32 4 1 1 Apr 01 15 2 Apr 01 15 3 Apr 01 15 4 Apr 01 15 5 Apr 01 15 6 Apr 01 15 32...

Страница 45: ...15 S1 10 Apr 01 15 S1 11 Apr 01 15 S1 12 Apr 01 15 S1 13 Apr 01 15 S1 14 Apr 01 15 S1 15 Apr 01 15 S1 16 Apr 01 15 S1 17 Apr 01 15 S1 18 Apr 01 15 S1 19 Apr 01 15 S1 20 Apr 01 15 S2 1 Apr 01 15 S2 2...

Страница 46: ...3 4 1 1 Dec 01 17 2 Dec 01 17 33 4 2 1 Dec 01 17 2 Dec 01 17 TAB DIV 34 34 1 Apr 01 15 2 Apr 01 15 TAB DIV 35 35 1 Apr 01 15 2 Apr 01 15 35 1 1 Jun 01 18 2 Jun 01 18 TAB DIV 36 36 1 Apr 01 15 2 Apr 01...

Страница 47: ...01 18 10 Jun 01 18 11 Jun 01 18 12 Jun 01 18 13 Jun 01 18 14 Jun 01 18 15 Jun 01 18 16 Jun 01 18 17 Jun 01 18 18 Jun 01 18 19 Jun 01 18 20 Jun 01 18 21 Jun 01 18 22 Jun 01 18 23 Jun 01 18 24 Jun 01 18...

Страница 48: ...16 25 A6 9 Jun 01 16 15 A6 10 exp Jun 01 16 15 A6 10 Jun 01 16 25 A6 10 exp Jun 01 16 25 A6 10 Jun 01 16 15 A6 11 exp Jun 01 16 15 A6 11 Jun 01 16 15 A6 12 exp Jun 01 16 15 A6 12 Jun 01 16 A8 0 Jun 01...

Страница 49: ...01 15 S1 4 Apr 01 15 S2 3 Apr 01 15 S2 4 Apr 01 15 5 Apr 01 15 6 Apr 01 15 S1 7 Apr 01 15 S1 8 Apr 01 15 S2 7 Apr 01 15 S2 8 Apr 01 15 9 Apr 01 15 10 Apr 01 15 S1 11 Apr 01 15 S1 12 Apr 01 15 S2 11 A...

Страница 50: ...CHAPTER CHAPTER SECT SUB PREFIX PAGE DATE SECT SUB PREFIX PAGE DATE LIST OF EFFECTIVE PAGES Aircraft Operations Manual EXTENDED WINGTIPS LEP PAGE 34 Dec 01 20 THIS PAGE INTENTIONALLY LEFT BLANK...

Страница 51: ...WR 850 1991 21 024 Change of Outflow Valve and installation of Air ventilation tailcone 2024 174 177 180 999 Change of static inverter 2066 61 028 PROP brake slippage due to PGB leakage 2070 33 032 In...

Страница 52: ...DC electronic start system 2650 27 075 Stall warning new stall curves req by Canada push button 2662 30 054 Engine air intake controlled service introduc tion ACT L H side 2664 30 084 Engine air intak...

Страница 53: ...a Flat Bulkhead 3151 34 162 TAWS Additional Altitude Callouts 3167 34 166 TAWS Steep Approach 3168 30 089 Improved Ice Detector 3281 34 200 Installation of UNS 1Lw MMMS 3310 34 204 Flight Management S...

Страница 54: ...ED IN THIS MANUAL Cont d Mod No Item Prod Eff Service Bulletin No 3543 24 052 Installation of Electronic Flight Bag EFB Arm holder knob and USB Power outlets modified charger compared to Mod No 3453 3...

Страница 55: ...Operations Manual 1 CONTENTS PAGE 1 Apr 01 15 CONTENTS Aircraft Data 1 1 0 Highlights not applicable 1 1 1 Description 1 1 2 Operation Cockpit 1 2 0 Highlights not applicable 1 2 1 Description 1 2 2...

Страница 56: ...AIRCRAFT GENERAL Aircraft Operations Manual 1 CONTENTS PAGE 2 Apr 01 15 THIS PAGE INTENTIONALLY LEFT BLANK...

Страница 57: ...cone Accommodation in the cockpit is provided for two operating crew members and one observer The aircraft is certificated to carry up to 37 passengers Passenger seating layout may however be varied...

Страница 58: ...AIRCRAFT GENERAL AIRCRAFT DATA Description Aircraft Operations Manual 1 1 1 PAGE 2 Apr 01 15 2 THREE VIEW DRAWING A9898 Fig 1 Three view drawing without extended wingtips...

Страница 59: ...1 1 1 PAGE 3 Apr 01 15 3 MINIMUM TURNING RADIUS A15474 TURN CENTER MINIMUM PAVEMENT WIDTH TIRE SLIPPAGE IS NOT CONSIDERED 58 ft 18 m WING TIP SWEEP 108 ft 33 3 m WITH EXTENDED WING TIPS WING TIP SWEE...

Страница 60: ...CRAFT DATA Description Aircraft Operations Manual 1 1 1 PAGE 4 Apr 01 15 4 CABIN CROSS SECTION A11574 Ref in m a b c d e f a b c d e f 85 0 2 16 72 0 1 83 16 3 0 41 17 0 0 43 67 0 1 70 91 0 2 31 Fig 3...

Страница 61: ...A C 106 219 5 ANTENNA ARRANGEMENT COLLINS DUAL ADF ANTENNA ADF 1 ADF 2 OPTION ADF 2 KING OPTION VHF COM 1 GLIDE SLOPE HF ANT OPTION VOR LOC ELT VLF OMEGA OPTION ADF 1 KING MARKER BEACON ATC 2 OPTION...

Страница 62: ...AIRCRAFT GENERAL AIRCRAFT DATA Description Aircraft Operations Manual 1 1 1 S1 PAGE 6 Apr 01 15 A C 106 219 THIS PAGE INTENTIONALLY LEFT BLANK...

Страница 63: ...ENT A28642 GLIDE SLOPE option TCAS option RADIO ALT ATC 1 ATC 2 option MARKER BEACON VHF 2 ACARS VHF 3 option DME 1 DME 2 option WEATHER RADAR ELT RNAV VLF OMEGA option VOR LOC HF option option option...

Страница 64: ...AIRCRAFT GENERAL AIRCRAFT DATA Description Aircraft Operations Manual 1 1 1 S2 PAGE 6 Apr 01 15 A C 220 UP or TCAS Mod for a c 160 219 except for MARKER and VHF 2 THIS PAGE INTENTIONALLY LEFT BLANK...

Страница 65: ...AIRCRAFT GENERAL AIRCRAFT DATA Description Aircraft Operations Manual 1 1 1 PAGE 7 Apr 01 15 A9986 0 802 kg L Fig 5 Ground service connections...

Страница 66: ...AIRCRAFT GENERAL AIRCRAFT DATA Description Aircraft Operations Manual 1 1 1 PAGE 8 Apr 01 15 THIS PAGE INTENTIONALLY LEFT BLANK...

Страница 67: ...passenger seats 37 Carriage of cargo The cargo compartment is classified as a class C cargo compartment Operation in day and night Visual Flying Rules VFR Operation in day and night Instrument Flying...

Страница 68: ...dance with the AFM must be met A12127 1 0 1 5 5 8 10 15 20 25 60 50 40 30 20 10 0 10 20 30 40 50 15 47 ISA OAT IN DEGREES CELSIUS PRESSURE ALTITUDE x 1000 FT 55 TAKE OFF LIMITS 1 4 STRUCTURAL WEIGHT L...

Страница 69: ...take off climb to cruise altitude cruise descent and landing A typical flight cycle is assumed to be carried out with duration and at altitudes associated with such operation Significant and recurring...

Страница 70: ...AIRCRAFT GENERAL AIRCRAFT DATA Operation Aircraft Operations Manual 1 1 2 PAGE 4 Apr 01 15 THIS PAGE INTENTIONALLY LEFT BLANK...

Страница 71: ...pit ceiling This hatch can also be used for ventilation on the ground The cockpit is also provided with two adjustable sun visors A sun visor must never be folded in a position blocking the handgrips...

Страница 72: ...tly pulling the lower part of the seat back and then adjusting the height The shoulder harness is of a reel type which can be locked by a handle or by inertia If optional ACARS installed With ACARS in...

Страница 73: ...AIRCRAFT GENERAL COCKPIT Description Aircraft Operations Manual 1 2 1 PAGE 3 Jun 30 15 3 EYE POSITION INDICATOR A11949 Fig 3 Eye position indicator...

Страница 74: ...1 PAGE 4 Jun 30 15 4 PEDALS The rudder pedals can be adjusted in forward aft direction By pulling the lever the pedal lock is re leased and the pedals are free to be repositioned When unlocked the pe...

Страница 75: ...nel Left headset holder Left pilot instrument panel Left circuit breaker panel See AOM 5 1 Left side panel Pedestal Right side panel Right circuit breaker panel See AOM 5 1 Right pilot instrument pane...

Страница 76: ...AIRCRAFT GENERAL COCKPIT Description Aircraft Operations Manual 1 2 1 PAGE 6 Jun 30 15 THIS PAGE INTENTIONALLY LEFT BLANK...

Страница 77: ...t Operations Manual 1 2 1 PAGE 7 Jun 30 15 A30788 Valid for a c with Mod no 3529 for 340 B 3530 for 340 WT Improved stall warning system for icing condition Fig 6 Standard instrument panel King avioni...

Страница 78: ...AIRCRAFT GENERAL COCKPIT Description Aircraft Operations Manual 1 2 1 PAGE 8 Jun 30 15 THIS PAGE INTENTIONALLY LEFT BLANK...

Страница 79: ...Operations Manual 1 2 1 PAGE 9 Jun 30 15 A30789 Valid for a c with Mod no 3529 for 340 B 3530 for 340 WT Improved stall warning system for icing condition Fig 7 Standard instrument panel Collins avion...

Страница 80: ...AIRCRAFT GENERAL COCKPIT Description Aircraft Operations Manual 1 2 1 PAGE 10 Jun 30 15 THIS PAGE INTENTIONALLY LEFT BLANK...

Страница 81: ...AIRCRAFT GENERAL COCKPIT Description Aircraft Operations Manual 1 2 1 PAGE 11 Jun 30 15 A9875 Fig 8 Standard side panels and control wheels Highest modification standard shown...

Страница 82: ...AIRCRAFT GENERAL COCKPIT Description Aircraft Operations Manual 1 2 1 PAGE 12 Jun 30 15 THIS PAGE INTENTIONALLY LEFT BLANK...

Страница 83: ...AIRCRAFT GENERAL COCKPIT Description Aircraft Operations Manual 1 2 1 PAGE 13 Jun 30 15 A9876 Fig 9 Max option side panels and controls wheels Highest modification standard shown...

Страница 84: ...AIRCRAFT GENERAL COCKPIT Description Aircraft Operations Manual 1 2 1 PAGE 14 Jun 30 15 THIS PAGE INTENTIONALLY LEFT BLANK...

Страница 85: ...AIRCRAFT GENERAL COCKPIT Description Aircraft Operations Manual 1 2 1 PAGE 15 Jun 30 15 A10750 Fig 10 Standard overhead panel and pedestal King avionics shown Highest modification standard shown...

Страница 86: ...AIRCRAFT GENERAL COCKPIT Description Aircraft Operations Manual 1 2 1 PAGE 16 Jun 30 15 THIS PAGE INTENTIONALLY LEFT BLANK...

Страница 87: ...AIRCRAFT GENERAL COCKPIT Description Aircraft Operations Manual 1 2 1 PAGE 17 Jun 30 15 A10729 Fig 11 Max option overhead panel and pedestal Collins avionics shown Highest modification standard shown...

Страница 88: ...AIRCRAFT GENERAL COCKPIT Description Aircraft Operations Manual 1 2 1 PAGE 18 Jun 30 15 THIS PAGE INTENTIONALLY LEFT BLANK...

Страница 89: ...toward passenger cabin due to immovable obstruction on cabin side the door may be partially opened into the cockpit as follows a Remove the jumpseat assembly from its frame b Turn the door stop color...

Страница 90: ...engage the pintle latch lever Blowout panel In case of a rapid decompression the door has a pressure equalization panel blowout panel to equalize the pressure between the passenger compartment and the...

Страница 91: ...AIRCRAFT GENERAL COCKPIT Description Aircraft Operations Manual 1 2 1 S1 PAGE 21 Jun 30 15 THIS PAGE INTENTIONALLY LEFT BLANK...

Страница 92: ...AIRCRAFT GENERAL COCKPIT Description Aircraft Operations Manual 1 2 1 S1 PAGE 22 Jun 30 15 THIS PAGE INTENTIONALLY LEFT BLANK...

Страница 93: ...butment The abutment angle is attached to the cockpit side of the door jamb by three clevis pins thus allowing removal of the abut ment angle by aircrew in event door must be opened inward A large cle...

Страница 94: ...jumpseat harness buckle holder etc However slight force should overcome such obstructions NOTE Due to possibility of damage to door assembly hinge etc opening of door inwards is consid ered an abnorma...

Страница 95: ...n band painted above the rounded knob Rounded knob Used to engage the pintle latch lever Nylon lanyard Used to pull the door towards closed position Blowout panel cage assembly The cage assembly built...

Страница 96: ...AIRCRAFT GENERAL COCKPIT Description Aircraft Operations Manual 1 2 1 S2 PAGE 22 Jun 30 15 THIS PAGE INTENTIONALLY LEFT BLANK...

Страница 97: ...quipment The linkage and Electronic Flight Bag EFB attachment plate is a carry on equipment The formal operational approval of the complete EFB installation rests with the operator NOTE 7 2 System des...

Страница 98: ...ations Manual 1 2 1 PAGE 24 Jun 30 15 A A A Left side shown A31199 Fig 13 Typical EFB support by RAM Mounting System Inc A31949 L H side USB connector R H side USB connector Fig 14 Location of electri...

Страница 99: ...AIR CONDITIONING PRESSURIZATION Aircraft Operations Manual 2 CONTENTS PAGE 1 Apr 01 15 CONTENTS Air Conditioning Pressurization 2 0 Highlights not applicable 2 1 Description 2 2 Operation...

Страница 100: ...AIR CONDITIONING PRESSURIZATION Aircraft Operations Manual 2 CONTENTS PAGE 2 Apr 01 15 THIS PAGE INTENTIONALLY LEFT BLANK...

Страница 101: ...ally regulates the electro pneumatic primary outflow valve to maintain the correct pressure The manually controlled system is an all pneumatic system The pilot operates the pneumatic second ary outflo...

Страница 102: ...amount of bleed air is routed from Left and Right Air Conditioning Pack to the Cabin Pressure Air Filter The air is blown over the filter to prevent a moisture build up in the filter With Mod No 1991...

Страница 103: ...eactivated in manual mode extreme care shall be taken not to obtain a temperature below freezing in the distribu tion duct Therefore always keep the recirculating fan ON for that pack which is operate...

Страница 104: ...e electro pneumatic primary outflow valve preventing cabin altitude to exceed 15 000 ft should the pressurization control ler fail For emergency pressure relief the electro pneu matical outflow valve...

Страница 105: ...s 15 000 ft In addi tion the controller will ensure that the differential pressure never exceeds 7 1 psi At takeoff with both BLD VALVES switched off both outflow valves will be closed When switching...

Страница 106: ...tion Rotating the knob clockwise will increase and counterclockwise will decrease the cabin altitude The electro pneumatic outflow valve will remain closed Pressure indication The pressure system has...

Страница 107: ...G AND PRESSURIZATION Description Aircraft Operations Manual 2 1 PAGE 7 Jun 01 18 A12060 For R side temperature signals are received from sensors in cockpit and duct Fig 1 Air conditioning pack schemat...

Страница 108: ...AIR CONDITIONING AND PRESSURIZATION Description Aircraft Operations Manual 2 1 PAGE 8 Jun 01 18 A12061 Fig 2 Flow path through air conditioning pack...

Страница 109: ...NING AND PRESSURIZATION Description Aircraft Operations Manual 2 1 S PAGE 9 Jun 01 18 This page is Applicable to aircraft without Mod no 1991 installed A26903 Fig 3 Air conditioning distribution syste...

Страница 110: ...AIR CONDITIONING AND PRESSURIZATION Description Aircraft Operations Manual 2 1 S PAGE 10 Jun 01 18 This page is Applicable to aircraft without Mod no 1991 installed THIS PAGE INTENTIONALLY LEFT BLANK...

Страница 111: ...ITIONING AND PRESSURIZATION Description Aircraft Operations Manual 2 1 S PAGE 11 Jun 01 18 This page is applicable to aircraft without Mod no 1994 installed A12063 Fig 4 Cabin pressurization system sc...

Страница 112: ...AIR CONDITIONING AND PRESSURIZATION Description Aircraft Operations Manual 2 1 S PAGE 12 Jun 01 18 This page is applicable to aircraft without Mod no 1994 installed THIS PAGE INTENTIONALLY LEFT BLANK...

Страница 113: ...IONING AND PRESSURIZATION Description Aircraft Operations Manual 2 1 O PAGE 9 Jun 01 18 This page is applicable to aircraft with Mod no 1991 installed A26864 Fig 3 Air conditioning distribution system...

Страница 114: ...AIR CONDITIONING AND PRESSURIZATION Description Aircraft Operations Manual 2 1 O PAGE 10 Jun 01 18 This page is applicable to aircraft with Mod no 1991 installed THIS PAGE INTENTIONALLY LEFT BLANK...

Страница 115: ...ING AND PRESSURIZATION Description Aircraft Operations Manual 2 1 O PAGE 11 Jun 01 18 This page is applicable to aircraft with Mod no 1994 installed A26863 BELOW T O PWR Fig 4 Cabin pressurization sys...

Страница 116: ...AIR CONDITIONING AND PRESSURIZATION Description Aircraft Operations Manual 2 1 O PAGE 12 Jun 01 18 This page is applicable to aircraft with Mod no 1994 installed THIS PAGE INTENTIONALLY LEFT BLANK...

Страница 117: ...SELECT switch Used to select automatic or manual control of temperature in the respective compartments AUTO Temperature automatically regu lated at level selected with temper ature selector knob HOT...

Страница 118: ...AIR CONDITIONING AND PRESSURIZATION Description Aircraft Operations Manual 2 1 S1 PAGE 14 Jun 01 18 Applicable to aircraft without Mod No 3121 installed THIS PAGE INTENTIONALLY LEFT BLANK...

Страница 119: ...itions where tem perature control valve moves in desired direction Shall only be used if the automatic temp regula tion fails The temperature switches are guarded in AUTO position to prevent unnecessa...

Страница 120: ...AIR CONDITIONING AND PRESSURIZATION Description Aircraft Operations Manual 2 1 S2 PAGE 14 Jun 01 18 Applicable to aircraft with Mod No 3121 installed THIS PAGE INTENTIONALLY LEFT BLANK...

Страница 121: ...pneumatical outflow valve to fully open position DIFF PRESS indicator Displays cabin differential pressure Shows 8 8 when LAMP TEST switch on test panel is held in LWR position A negative diff pressur...

Страница 122: ...ield altitude Barometric set knob Used to set airfield barometric pressure in inch Hg As an option the BARO scale is available in millibars MODE SELECTOR AUTO Pressure controller operates automaticall...

Страница 123: ...tch Three position Heater control switch Air flow Regulator Controls the amount of air directed to the fwd part of the cockpit floor TEST 2 L R L GEN R OVV RUD LIM CAB PRESS GDN AHRS L R AIR DATA EMER...

Страница 124: ...L R FIRE DET FAIL FUEL ELEC ICE PROT ENGINE FLAPS AIRCOND PARK BRK ON HYDR EMER LTS UN ARMED OXYGEN DOORS AVIONICS VET AVIONICS A SKID INOP L STALL FAIL GUST LOCK PUSHER SYSTEM R STALL FAIL CABIN PRES...

Страница 125: ...ion Aircraft Operations Manual 2 1 PAGE 19 Jun 01 18 A10800 A A A Heater element location COCKPIT FLOOR HEATERS MOD NO 2293 Heater switch Two position heater element ON OFF switch Fig 10 Air condition...

Страница 126: ...ITIONING PANEL CARGO HEATER ON OFF B B CARGO HEATER ON OFF switch Used to control the optional cargo heater TEMP IND switch Used to select either CABIN CARGO or L DUCT temperature to be displayed on t...

Страница 127: ...AIR CONDITIONING AND PRESSURIZATION Description Aircraft Operations Manual 2 1 PAGE 21 A15969 Fig 12 Optional cargo heater installation Dec 01 20...

Страница 128: ...ion L GEN BUS H 17 CABIN RECIRC Overheat detection L MAIN BUS H 20 RECIRC OVHT Cabin temperature indication L ESS BUS H 14 CABIN TEMP IND Avionic rack fan control L MAIN BUS G 10 VENT AVION FAN CONTRO...

Страница 129: ...5 Landing psi 0 2 Negative diff pressure psi 0 5 CABIN PRESS warning psi 7 5 Cabin altitude CABIN PRESS warning ft 10 000 1 2 SYSTEM LIMITS Air conditioning Compartment temperature AUTO mode C 18 29...

Страница 130: ...erature variation from ISA as REFERENCE TEMPERATURE 2 Follow the line for the REFERENCE TEMPERATURE until intersect with the FLYING TIME and find the CARGO COMPARTMENT TEMPERATURE Example Departure Ai...

Страница 131: ...00 120 20 10 0 10 Ex Ex REFERENCE TEMPERATURE ISA 15 C REFERENCE TEMPERATURE ISA 10 C REFERENCE TEMPERATURE ISA 5 C REFERENCE ISA CARGO COMPARTMENT TEMPERATURE C 20 40 60 80 100 120 20 10 0 10 CARGO C...

Страница 132: ...ONDI TIONING NORMAL OPERATION AUTO MODE This procedure assumes that the pneumatic system is checked and set accord ing to AOM 16 2 PNEUMATICS Running a recirculation fan creates heat around the fan it...

Страница 133: ...omfortable level in a heat soaked parked aircraft The procedure will also minimize the amount of moisture and condensation experienced in the air dis tribution ducting during temperature pull down in...

Страница 134: ...closed while the entrance door is open to minimize moisture and condensation in cockpit 11 RECIRC fans OFF With passengers on board and entrance door closed 12 Temperature control knobs COLD Set the k...

Страница 135: ...st temperature as required by momentarily setting the TEMP SELECT switch in either HOT or COLD position 2 5 PRESSURIZA TION CONTROL SYSTEM NORMAL OPERATION Preflight 1 Cabin pressurization control CHK...

Страница 136: ...matic outflow valve while the normal electropneumatical outflow valve is closed 1 Mode selector switch MAN This will disconnect the automatic pressure control system 2 Manual control knob ADJUST AS RE...

Страница 137: ...HT Aircraft Operations Manual 3 CONTENTS PAGE 1 Apr 01 15 CONTENTS Autoflight CAT I STANDARD 3 0 Highlights 3 1 Description 3 2 Operation Autoflight CAT II OPTION 3 0 Highlights 3 1 Description 3 2 Op...

Страница 138: ...AUTOFLIGHT Aircraft Operations Manual 3 CONTENTS PAGE 2 Apr 01 15 THIS PAGE INTENTIONALLY LEFT BLANK...

Страница 139: ...ation standard of the aircraft If a modification is not installed the following applies as a complement to what is stated in this chapter DESCRIPTION OPERATION 0 1 Flight Director comparator caution W...

Страница 140: ...AUTOFLIGHT CAT I Highlights Aircraft Operations Manual 3 0 S PAGE 2 Apr 01 15 THIS PAGE INTENTIONALLY LEFT BLANK...

Страница 141: ...ds pitch and roll indication are selected with the FD operating mode pushbuttons on the MSP Pitch and roll guidance cues as well as mode information from the FD are displayed on the EADI s The FD comm...

Страница 142: ...push will reset the aural warning by moving the AP YD levers to DISENGAGED position by selecting GA L R Power lever button by operating the pitch trim switches AP disengage only The Stall warning com...

Страница 143: ...n ALT mode is in track The computed IAS is a function of altitude at me dium aircraft weight Selectable by ALT mode button Selection of ALT clears any previously selected vertical mode except ALTS and...

Страница 144: ...nges from GA to PTCH It is only the reference data that is changed The respective mode function is retained Pitch trim is not affected AP will remain engaged LATERAL MODES HDG Heading mode The FCC giv...

Страница 145: ...cing the GS CAP indication on the EADI EHSI With the CRS selector set for the normal Localizer inbound course the LOC symbols on the EADI EHSI are not reversed when flying Inbound on the Back course O...

Страница 146: ...2 3 Autopilot Panel APP Located on the pedestal Contains engage disen gage levers for AP and YD and controls for heading and vertical speed changes 2 4 NAV source selection There are two navigation so...

Страница 147: ...D AP flight control computer FCC Including yaw damper YD ALT SEL Nav data DME NO 1 Vert Nav data Air data ATT HDG data Rudder servo Aileron servo Elevator servo Elevator autotrim Rudder autotrim Pitch...

Страница 148: ...s of 50 ft Moving pitch wheel from detent resets vertical mode to VS except in GS CAP and ALTS mode and then slews vertical speed reference at rate proportional to the amount of wheel displacement NAV...

Страница 149: ...s Indicators in mode buttons illuminate to annunciate mode selected Active as well as preselected armed modes are annunciated on EADI In addition to modes selected on MSP GA push buttons in the power...

Страница 150: ...AUTOFLIGHT CAT I Description Aircraft Operations Manual 3 1 S PAGE 10 Jun 01 19 THIS PAGE INTENTIONALLY LEFT BLANK...

Страница 151: ...position Vertical Speed VS bug Indicates selected VS when the AP FD is in the VS mode and initial VS selected with the PUSH TST knob when not in the VS hold A VERTICAL NAVIGATION INDICATOR VNI IF INST...

Страница 152: ...AUTOFLIGHT CAT I Description Aircraft Operations Manual 3 1 S PAGE 12 Jun 01 19 THIS PAGE INTENTIONALLY LEFT BLANK...

Страница 153: ...is rate in ft min VVVV VS Vert speed down VVVV is rate in ft min SSS I CLB CLIMB SSS is speed in knots I is speed mode L M H SSS ALT ALTITUDE SSS is Flight advisory speed in knots for long range crui...

Страница 154: ...AUTOFLIGHT CAT I Description Aircraft Operations Manual 3 1 S PAGE 14 Jun 01 19 THIS PAGE INTENTIONALLY LEFT BLANK...

Страница 155: ...CS DIAGNOSTICS 000000 000000 000000 000000 000000 REPORT MODE REPAIR CODE AP DIS CODE YD DIS CODE AP ENG CODE YD ENG CODE 032000 000000 000000 000000 000000 LEFT RIGHT HDG BANK NAV APPR VS IAS CLIMB V...

Страница 156: ...AUTOFLIGHT CAT I Description Aircraft Operations Manual 3 1 S PAGE 16 Jun 01 19 THIS PAGE INTENTIONALLY LEFT BLANK...

Страница 157: ...ption Aircraft Operations Manual 3 1 S PAGE 17 Jun 01 19 4 ELECTRICAL POWER SUPPLY Flight director L AVIONIC BUS G 13 FD Autopilot L AVIONIC BUS G 12 AP Flight director R AVIONIC BUS N 10 FD Autopilot...

Страница 158: ...AUTOFLIGHT CAT I Description Aircraft Operations Manual 3 1 S PAGE 18 Jun 01 19 THIS PAGE INTENTIONALLY LEFT BLANK...

Страница 159: ...pilot engaged it is re quired to disconnect the AP and re trim the a c before re engagement of the AP kt 1 2 1 2 VMO MMO 1 2 1 2 OPERATION LIMITS Flight Director Use of flight director information in...

Страница 160: ...ES OF CLIMB BUTTON CYCLES H M L SPEED PRO FILES ALT ANY ANY TO ZERO ALT REF SEE SE LECTED LATERAL MODE RETURN TO VS MODE SEE SE LECTED LATERAL MODE ALT REF SYNCS TO EXISTING ALT AT SELEC TION NO BARO...

Страница 161: ...TERAL MODE SEE SE LECTED VERTICAL MODE SEE SE LECTED LATERAL MODE VNAV ARM NOT SELECT ABLE IN ALTS VNAV ARM NOT SELECTABLE UNTIL 3 MIN FROM THE DE SCEND POINT VNAV CAP Op tion ANY ANY FLIES COM MANDS...

Страница 162: ...EADI SELECT ABLE VER TICAL MODES SELECT ABLE LATERAL MODES APPR ARM ANY ANY SEE SE LECTED VERTICAL MODE TO ZERO HDG DIF FERENCE ON EHSI SEE SE LECTED VERTICAL MODE HDG BUG ON EHSI TO SLEW HDG WILL RE...

Страница 163: ...the rudder pedals prepared to disengage the au topilot and take over manual control if necessary NOTE 2 2 FLIGHT DIRECTOR GENERAL The FD V shaped magenta colored command bar shall normally be selecte...

Страница 164: ...n power levers Always confirm with the EADI mode annunciation that selected mode has been armed engaged NOTE A new mode can always be selected by pushing desired button on MSP Exceptions A new vertica...

Страница 165: ...o change selected airspeed Change of selected airspeed is by pressing and releasing the VERT SYNC button or via other modes 2 8 CLIMB MODE 1 CLIMB button PRESS Check EADI to annunciate CLB H M L respe...

Страница 166: ...V NAV Automatic patch capture above or below present altitude using initial vertical speed 1 NAV frequency selector SET VOR DME FREQUENCY 2 Altitude preselect CLEARED TO ALT 3 Aimpoint altitude SET Se...

Страница 167: ...e to the aimpoint When the aircraft reaches the aimpoint which is at the altitude selected on the altitude pre selector automatic level off occurs Automatic path capture above or below presents altitu...

Страница 168: ...Distance display shows distance to path captured point When aircraft reaches path capture point the ANG ARM and TO TRK an nunciators go blank and the AP FD captures the path to the aimpoint Check TO A...

Страница 169: ...ry rotating the function switch to DIR and back to ACT Distance to the aimpoint TO ALT is shown on the DISTANCE display For path tracking information use FD display on EADI or vertical deviation displ...

Страница 170: ...ow B C replacing the GS indication on the EADI EHSI With the CRS selector set for the normal localizer inbound course the LOC sym bols on the EADI EHSI are not reversed when flying Inbound on the back...

Страница 171: ...green and LOC white on EADI 6 At LOC CAP LOC green on EADI CHECK 7 VS or IAS button PRESS Check EADI to annunciate VS or IAS 8 HDG knob SET GA HDG 9 Altitude set knob APA SET GA ALT To be selected be...

Страница 172: ...be selected on both NAV controls 2 CRS selector SET ILS INBOUND COURSE Check course readout on EHSI 3 HDG knob SET LOC INTERCEPT HDG 4 DCP SET HDG 5 MSP APPR button PRESS Do not selected APPR mode un...

Страница 173: ...ing and a fixed pitch attitude HDG indicator remains at preset heading Re engagement of AP Condition for re engagement Radio height equal to or greater than 200 ft 2 AP YD ENGAGE Check EADI to annunci...

Страница 174: ...I and aural AP warning comes on ACTIONS 1 AP disconnect button PUSH This will cancel AP warnings If not effective pull affected side sides FD CB G 13 N 10 2 CB s CHECK RESET CB FD G 13 N 10 and AP G 1...

Страница 175: ...AP does not follow FD commands AP impossible to disengage in one or more channels Elevator trim indicator shows abnormal trim action Single stroke chime Master caution light FD hard over AVIONICS ligh...

Страница 176: ...th close attention to flight path Below 600 feet ARTE Perform immediate go around unless visual contact has been established New approach may be performed to CAT I minima Glideslope and or Localizer r...

Страница 177: ...changing flight director modes Other failure modes can occur which will provide different cues such as aircraft attitude or flight path changes and it is always the pilots responsibility to monitor sy...

Страница 178: ...NAV mode and LOC capture Loss of electrical power to the NAV receiver will cause the following on the EADI LOSS OF 28 VDC The FD AP will revert to basic modes HDG VS changing captured LOC GS annuncia...

Страница 179: ...ation standard of the aircraft If a modification is not installed the following applies as a complement to what is stated in this chapter DESCRIPTION OPERATION 0 1 Flight Director comparator caution W...

Страница 180: ...AUTOFLIGHT CAT II Highlights Aircraft Operations Manual 3 0 O PAGE 2 Apr 01 15 THIS PAGE INTENTIONALLY LEFT BLANK...

Страница 181: ...ode pushbuttons on the MSP Pitch and roll guid ance cues as well as mode information from the FD are displayed on the EADI s The FD command bars on the EADI s direct the pilot to turn climb or descend...

Страница 182: ...trim system should fail The AP YD can be disengaged by pushing the AP disconnect button on the con trol wheel A second push will reset the aural warning by moving the AP YD levers to DISENGAGED positi...

Страница 183: ...mode change Selection of CLIMB mode clears any previously selected vertical mode except GS CAP and ALTS ALT FCC holds the altitude existing at time of mode engagement or if already in ALT at time of...

Страница 184: ...in IAS mode the FCC reference data changes to existing IAS c if in ALT mode the FCC reference data changes to existing ALT d if in GA mode the FCC reference data changes to existing attitude The verti...

Страница 185: ...I lateral mode annunciation changes to LOC CAP GS ARM is displayed for the vertical axis GS shall be captured from below the beam In GS CAP a new vertical mode can only be selected after a new lateral...

Страница 186: ...ated on the pedestal Contains engage discon nect levers for AP and YD a button for AP transfer between the two FCC channels and controls for heading and vertical speed changes 2 4 NAV source selection...

Страница 187: ...FD AP flight control computer FCC Including yaw damper YD ALT SEL Nav data DME NO 1 Vert Nav data Air data ATT HDG data Rudder servo Aileron servo Elevator servo Elevator autotrim Rudder autotrim Pitc...

Страница 188: ...heel from detent resets vertical mode to VS except in GS CAP and ALTS mode and then slews vertical speed reference at rate proportional to the amount of wheel displacement AP XFR button The AP XFR but...

Страница 189: ...AP auto trim or YD auto trim systems AUTO TRIM AUTO COARSEN Mode select panel CONFIG Mode select buttons are integrally lighted momentary push on buttons Indicators in mode buttons illumi nated to an...

Страница 190: ...AUTOFLIGHT CAT II Description Aircraft Operations Manual 3 1 O PAGE 10 Jun 01 19 THIS PAGE INTENTIONALLY LEFT BLANK...

Страница 191: ...Vertical Speed VS bug Indicates selected VS when the AP FD is in the VS mode and initial VS selected with the PUSH TST knob when not in the VS hold A VERTICAL NAVIGATION INDICATOR VNI IF INSTALLED DI...

Страница 192: ...AUTOFLIGHT CAT II Description Aircraft Operations Manual 3 1 O PAGE 12 Jun 01 19 THIS PAGE INTENTIONALLY LEFT BLANK...

Страница 193: ...in knots for long range cruise only displayed when ALT in track mode SSS ALTS ALTITUDE SSS is Flight advisory speed in knots for long range cruise only displayed when ALTS in track mode SSS IAS indica...

Страница 194: ...AUTOFLIGHT CAT II Description Aircraft Operations Manual 3 1 O PAGE 14 Jun 01 19 THIS PAGE INTENTIONALLY LEFT BLANK...

Страница 195: ...D YD AP FCS DIAGNOSTICS 000000 000000 000000 000000 000000 REPORT MODE REPAIR CODE AP DIS CODE YD DIS CODE AP ENG CODE YD ENG CODE 032000 000000 000000 000000 000000 LEFT RIGHT HDG BANK NAV APPR VS IA...

Страница 196: ...AUTOFLIGHT CAT II Description Aircraft Operations Manual 3 1 O PAGE 16 Jun 01 19 THIS PAGE INTENTIONALLY LEFT BLANK...

Страница 197: ...iption Aircraft Operations Manual 3 1 O PAGE 17 Jun 01 19 4 ELECTRICAL POWER SUPPLY Flight director L AVIONIC BUS G 13 FD Autopilot L AVIONIC BUS G 12 AP Flight director R AVIONIC BUS N 10 FD Autopilo...

Страница 198: ...AUTOFLIGHT CAT II Description Aircraft Operations Manual 3 1 O PAGE 18 Jun 01 19 THIS PAGE INTENTIONALLY LEFT BLANK...

Страница 199: ...is re quired to disconnect the AP and re trim the a c before re engagement of the AP kt 1 2 1 2 VMO MMO 1 2 Surface wind component limits during CAT II ap proach Crosswind kt 19 1 2 OPERATION LIMITS F...

Страница 200: ...HES OF CLIMB BUTTON CYCLES H M L SPEED PRO FILES ALT ANY ANY TO ZERO ALT REF SEE SE LECTED LATERAL MODE RETURN TO VS MODE SEE SE LECTED LATERAL MODE ALT REF SYNCS TO EXISTING ALT AT SELEC TION NO BARO...

Страница 201: ...DG GA ENGAGING AP RETURNS SYSTEM TO VS MODE WHEN IN ALTS CAP LAT MODE WILL CHANGE TO GA AND VERT MODE WILL REMAIN ALTS UNTIL A NEW VERT MODE IS MANUALLY SELECTED VNAV ARM Op tion ANY VNAV ARM NOT SELE...

Страница 202: ...RTICAL MODE TO ZERO HDG DIF FERENCE ON EHSI SEE SE LECTED VERTICAL MODE HDG BUG ON EHSI TO SLEW FLIES HDG UN TIL VOR OR LOC CAPTURE NAV CAP ANY ANY SEE SE LECTED VERTICAL MODE TO AC QUIRE AND TRACK ZE...

Страница 203: ...DIRECTOR GENERAL The FD V shaped magenta colored command bar shall normally be selected on both EADIs However the displayed command bars can be deselected by pressing the FD button on the DCP except...

Страница 204: ...apture point for the APA setting Exception ALTS is not armed in GS CAP GA mode can only be engaged by GA switches in power levers Always confirm with the EADI mode annunciation that selected mode has...

Страница 205: ...Change of selected airspeed is by the IAS bug on the airspeed indicator Change of selected airspeed is by pressing and releasing the VERT SYNC button or via other modes 2 8 CLIMB MODE 1 CLIMB button...

Страница 206: ...V NAV Automatic patch capture above or below present altitude using initial vertical speed 1 NAV frequency selector SET VOR DME FREQUENCY 2 Altitude preselect CLEARED TO ALT 3 Aimpoint altitude SET Se...

Страница 207: ...to the aimpoint When the aircraft reaches the aimpoint which is at the altitude selected on the altitude pre selector automatic level off occurs Automatic path capture above or below present altitude...

Страница 208: ...Distance display shows distance to path captured point When aircraft reaches path capture point the ANG ARM and TO TRK an nunciators go blank and the AP FD captures the path to the aimpoint Check TO A...

Страница 209: ...ary rotating the function switch to DIR and back to ACT Distance to the aimpoint TO ALT is shown on the DISTANCE display For path tracking information use FD display on EADI or vertical deviation disp...

Страница 210: ...low B C replacing the GS indication on the EADI EHSI With the CRS selector set for the normal localizer inbound course the LOC sym bols on the EADI EHSI are not reversed when flying Inbound on the bac...

Страница 211: ...green and LOC white on EADI 6 At LOC CAP LOC green on EADI CHECK 7 VS or IAS button PRESS Check EADI to annunciate VS or IAS 8 HDG knob SET GA HDG 9 Altitude set knob APA SET GA ALT To be selected be...

Страница 212: ...DG knob SET LOC INTERCEPT HDG 4 DCP SET HDG 5 Radio altimeter CHECK Radio altimeter test must be performed before APPR mode is selected Tem porary config warning will occur if RA test performed with P...

Страница 213: ...TION Only required for CAT II approach 2 16 GA MODE 1 GA button on power levers PRESS Check EADI to annunciate GA AP YD disengages FD commands existing heading and a fixed pitch attitude HDG indicator...

Страница 214: ...DI and aural AP warning comes on ACTIONS 1 AP disconnect button PUSH This will cancel AP warnings If not effective pull affected side sides FD CB G 13 N 10 2 CB s CHECK RESET CB FD G 13 N 10 and AP G...

Страница 215: ...AP does not follow FD commands AP impossible to disengage in one or more channels Elevator trim indicator shows abnormal trim action Single stroke chime Master caution light FD hard over AVIONICS ligh...

Страница 216: ...been established Autopilot discon nect Above 600 ft ARTE Approach may be continued manually to CAT I minima Below 600 ft ARTE Perform immediate go around unless visual contact has been established Gli...

Страница 217: ...changing flight director modes Other failure modes can occur which will provide different cues such as aircraft attitude or flight path changes and it is always the pilots responsibility to monitor s...

Страница 218: ...ll revert to basic modes HDG VS changing captured LOC GS annunciation to captured HDG VS annunciation LOC and or GS indication disappears The FD AP will maintain HDG and VS mode until other modes are...

Страница 219: ...PTION 4 2 0 Highlights not applicable 4 2 1 Description 4 2 2 Operation VHF COM 4 3 0 Highlights 4 3 1 Description 4 3 2 Operation PA Interphone 4 4 0 Highlights not applicable 4 4 1 Description 4 4 2...

Страница 220: ...COMMUNICATIONS Aircraft Operations Manual 4 CONTENTS PAGE 2 Apr 01 15 THIS PAGE INTENTIONALLY LEFT BLANK...

Страница 221: ...n be bypassed the REU and switched directly to the headsets by the NORM EMER switch on associated ACP VHF COM 1 to the L P ACP and VHF COM 2 to the R P ACP 2 2 Audio Control Panel ACP Two ACP s are in...

Страница 222: ...r With the observer hand microphone selected it is still possible for the pilot to transmit using the PTT button on the ACP or control wheel 2 6 Ground crew jack panel The ground crew jack panel locat...

Страница 223: ...and 2 HF COM L P Observer R P L P R P Cockpit Ground crew REU REMOTE ELECTRONIC UNIT Logic Audio PHONE switch Audio Logic Chime Audio Audio Mic ON OFF switch VOR LOC Marker DME ADF Cockpit speakers Fl...

Страница 224: ...ntercom COLD The microphone is only on in the intercom when the PTT is de pressed for transmission BOOM MASK switch BOOM Headset microphone selected MASK Oxygen mask microphone selected NORM EMER swit...

Страница 225: ...PANEL Ground crew light A white light comes on when ground crew headset is connected in the nose wheel well Connection for oxygen mask microphone Connections for headset Two types of connectors are ac...

Страница 226: ...cts the observer s headset to the left pilot audio R P Connects the observer s headset to the right pilot audio Connections for headsets Two types of connectors are accepted MIC switch HOT Headset mic...

Страница 227: ...on Aircraft Operations Manual 4 1 1 PAGE 7 Apr 01 15 A11579 COCKPIT CALL BUT TON option GROUND CREW JACK PANEL GROUND CREW HEADSET TALK SWITCH schematic Microphoneplug Earphone plug Talk switch Headse...

Страница 228: ...COMMUNICATIONS AUDIO INTEGRATING Description Aircraft Operations Manual 4 1 1 PAGE 8 Apr 01 15 THIS PAGE INTENTIONALLY LEFT BLANK...

Страница 229: ...COMMUNICATIONS AUDIO INTEGRATING Description Aircraft Operations Manual 4 1 1 PAGE 9 Apr 01 15 A C 180 up A11565 OXY MASK MIC Fig 6 Observers oxygen mask microphone jack...

Страница 230: ...COMMUNICATIONS AUDIO INTEGRATING Description Aircraft Operations Manual 4 1 1 PAGE 10 Apr 01 15 A C 180 up THIS PAGE INTENTIONALLY LEFT BLANK...

Страница 231: ...ING Description Aircraft Operations Manual 4 1 1 PAGE 11 Apr 01 15 With Mod No 2600 installed A29408 OXY MASK MIC MIC OBSERVER Connection for observer hand microphone Observer hand microphone Fig 7 Ob...

Страница 232: ...SPKR MKR 1 ADF 2 A MIC OBSERVER SWITCH A Observer Pilot Hand Microphone selector switch guarded This switch selects which hand microphone is active for transmission OBSVR Observer hand microphone sele...

Страница 233: ...iption Aircraft Operations Manual 4 1 1 PAGE 13 Apr 01 15 4 ELECTRICAL POWER SUPPLY Left pilot audio L BAT BUS E 10 AUDIO L Right pilot audio R BAT BUS L 10 AUDIO R Active Noise Reduction Headsets RH...

Страница 234: ...COMMUNICATIONS AUDIO INTEGRATING Description Aircraft Operations Manual 4 1 1 PAGE 14 Apr 01 15 THIS PAGE INTENTIONALLY LEFT BLANK...

Страница 235: ...ver transmit longer than 2 min when transmission will be shut off automatically Communication still lost 3 NORM EMER switch EMER COM 1 L audio control panel COM 2 R audio control panel Communication r...

Страница 236: ...S AUDIO INTEGRATING Operation Aircraft Operations Manual 4 1 2 PAGE 2 Apr 01 15 CONDITIONS ABNORMAL PROCEDURES 3 2 COCKPIT IN TERCOM DEAD ACTIONS 1 CBs E 10 AUDIO L and L 10 AUDIO R CHECK RESET 2 End...

Страница 237: ...also mode and squelch controls The clarifier permits the pitch of the received signal to be varied 100 Hz in all modes except AM 2 2 Transceiver and Power amplifier The transceiver contains the freque...

Страница 238: ...5 COLLINS HF 230 A26866 CONTROL UNIT TRANSCEIVER MODE FREQ SQUELCH CLARIFIER TEST POWER AMPLIFIER ANTENNA COUPLER TUNING TRANSMIT RECEIVE TUNING TRANSMIT RECEIVE TUNING FAULT COCPIT VOICE RECORDER AUD...

Страница 239: ...requency mode of operation Photocell Controls display brightness R Receive T Transmit Right inner No effcect on user channels pushed in or pulled out Knob functions when selecting an ITU telephone cha...

Страница 240: ...COMMUNICATIONS HF COM Description Aircraft Operations Manual 4 2 1 O PAGE 4 Apr 01 15 COLLINS HF 230 THIS PAGE INTENTIONALLY LEFT BLANK...

Страница 241: ...MICROPHONE PTT D I S C A P A CONTROL WHEEL PTT BUTTON C B A B C XMIT SELECT 1 COM 2 COM 3 HF INT COLD BOOM HOT MIC MASK NORM EMER 1 NAV 2 MKR PA 1 ADF 2 SPKR VOICE IDENT PTT C AUDIO CONTROL PANEL ACP...

Страница 242: ...COMMUNICATIONS HF COM Description Aircraft Operations Manual 4 2 1 O PAGE 6 Apr 01 15 4 ELECTRICAL POWER SUPPLY HF L AVIONICS BUS E 14 COM HF...

Страница 243: ...t of detent applies power to the HF Allow 15 minutes warmup before use NOTE 2 2 USER CHANNELS PROGRAMM ING The 40 user programmable channels can be easily programmed on ground or in flight All program...

Страница 244: ...to store the data The display will blank for a short period of time to confirm storage 6 Enter and store the transmit frequency When the display returns it will be blinking faster with the transmit fr...

Страница 245: ...once again to store the data The display will blank for a short period of time to confirm storage 6 Store the transmit frequency When the display returns it will be blinking faster with the simplex t...

Страница 246: ...red operating mode USB LSB AM TEL SUP CAR or TEL PLT CAR by pulling out the PULL MODE knob and rotating it until the appropriate mode appears in the MODE display 5 Store the receive frequency and mode...

Страница 247: ...5 PULL MODE knob SELECT Select mode of operation Successful HF communications depend on compatibility between the airborne and the ground station It is extremely important that the oper ator select t...

Страница 248: ...system is ready for use If the antenna does not tune after approx 35 to 40 seconds the steady 1000 Hz tone will begin to beep indicating a fault has occurred To clear the fault simply rotate one of t...

Страница 249: ...ing on prevailing conditions when it will be necessary to maintain satisfactory reception This is because of conditions relating to propagation and the ionosphere that causes the HF receiver to have t...

Страница 250: ...s away from and then back to the desired frequency or channel and initiate another turning cycle by momentarily pressing the microphone PTT but ton The 1000 Hz tone should again be present and then di...

Страница 251: ...ighlights Aircraft Operations Manual 4 3 0 PAGE 1 Apr 01 15 0 MODIFICATION STANDARD DESCRIPTION OPERATION 0 1 VHF COM frequency range Without mod no 2060 embodied The frequency range of the VHF COM is...

Страница 252: ...COMMUNICATIONS VHF COM Highlights Aircraft Operations Manual 4 3 0 PAGE 2 Apr 01 15 THIS PAGE INTENTIONALLY LEFT BLANK...

Страница 253: ...on may momentarily change less than 1 of full scale indication when transmitting on COM 2 NOTE The transmission PTT button keying is recorded on the Digital Flight Data Recorder DFDR via the Flight Da...

Страница 254: ...equency selector Large knob Controls the three left digits in 1 MHz steps Small knob Controls the two three right digits in 50 kHz steps or 25 8 33 kHz steps for the first two steps after the directio...

Страница 255: ...to fuel tank probe wiring fuel quantity indica tion may momentarily change less than 1 of full scale indication when transmitting on COM 2 NOTE The transmission PTT button keying is recorded on the Di...

Страница 256: ...y When depressed for more than 2 sec Standby frequency display goes off Frequency selectors control active frequency display When pressed again momentarily Standby frequency displayed again and func t...

Страница 257: ...ission PTT button keying is recorded on the Digital Flight Data Recorder DFDR via the Flight Data Acquisition Unit FDAU The commu nication will also be recorded by the Cockpit Voice Recorder via the A...

Страница 258: ...quency selector controls either one of Upper Lo wer display for setup of Memory Frequency display Upper Displays active frequency When transmitting a T is displayed at the right of the active frequenc...

Страница 259: ...Transmit Volume control for COM 1 and COM 2 XMIT SELECT button Momentarily press associated button to select COM for transmitting COM 3 not used ex cept with Mod No 3142 installed NORM EMER switch NO...

Страница 260: ...use The oxygen mask microphone plug is normally connected to the OXY MASK re ceptacle 1 and with the BOOM MASK switch 2 set to MASK when oxygen mask in use If the ACP fails and or NORM EMER switch is...

Страница 261: ...COMMUNICATIONS VHF COM Description Aircraft Operations Manual 4 3 1 PAGE 5 Apr 01 15 4 ELECTRICAL POWER SUPPLY VHF 1 EMER AVIONIC BUS E 13 VHF COM 1 VHF 2 R AVIONIC BUS L 12 VHF COM 2...

Страница 262: ...COMMUNICATIONS VHF COM Description Aircraft Operations Manual 4 3 1 PAGE 6 Apr 01 15 THIS PAGE INTENTIONALLY LEFT BLANK...

Страница 263: ...agnostic Fail Code Two tones will be heard 2 TEST button RELEASE 2 3 PROGRAM MING OF THE FREQUENCY MEMORY The Control unit contains six programmable memorycells 1 XFR MEM switch MEM PRESS Momentarily...

Страница 264: ...microphones and loudspeakers 4 NORM SQ OFF selector CHECK Selector normally in NORM position However it may be necessary to deactivate squelch SQ OFF to receive weak signals Transmitting 3 XMIT SELEC...

Страница 265: ...o control panel COM 2 R audio control panel Communication re established 4 The audio control panel failed Only the COM can be used with switch in EMER All other functions must be controlled by the opp...

Страница 266: ...COMMUNICATIONS VHF COM Operation Aircraft Operations Manual 4 3 2 C PAGE 4 Jun 01 18 COLLINS PRO LINE II THIS PAGE INTENTIONALLY LEFT BLANK...

Страница 267: ...akers 3 PULL TEST knob CHECK Knob normally in pushed position However it may be necessary to deactivate squelch Pull knob to receive weak signals Transmitting 2 XMIT SELECT COM 1 COM 2 SELECT Check bu...

Страница 268: ...l panel COM 2 R audio control panel Communication re established 4 The audio control panel failed Only the COM can be used with switch in EMER All other functions must be controlled by the opposite au...

Страница 269: ...rycells 1 CHAN button PRESS 2 SEC Momentarily press CHAN button for more than 2 seconds to enter program mode 2 Frequency selector SELECT MEMORYCELL 3 Transfer button PRESS When momentarily pressed fi...

Страница 270: ...n PRESS Momentarily press Transfer button to make chosen memory frequency active Or no active for 5 seconds will make chosen memory frequency standy SBY Receiving 4 COM volume lever AS REQUIRED Use he...

Страница 271: ...DITIONS NORMAL PROCEDURES Cont d 5 PTT button PRESS Check a T to appear right of active frequency 6 PTT button RELEASE After message For King VHF COM If transmitting on one COM with a frequency separa...

Страница 272: ...ntrol panel COM 2 R audio control panel Communication re established 4 The audio control panel failed Only the COM can be used with switch in EMER All other functions must be controlled by the opposit...

Страница 273: ...rs for distribution of messages Boarding music entertainment systems 2 MAIN COMPONENTS AND SUBSYSTEMS 2 1 PA AMPLIFIER The PA amplifier basically consists of an amplifier circuit and a chime generator...

Страница 274: ...Remote electric unit REU PA amplifier AUDIO Audio chime Cockpit speakers Audio chime Cabin speakers Cockpit voice recorder PA CALL EMER PA CALL EMER Attendant panel Passenger call buttons COCKPIT INTE...

Страница 275: ...attendant SEAT BELT and NO SMOKING switches CKPT STERILE instead of no smoking if mod no 2070 installed give Hi chime in cabin whenever cabin signs are switched OFF ON or ON OFF Cabin PA volume Only w...

Страница 276: ...mes on without chime when cabin crew gives message to the passengers Selected PA CALL buttonlight illuminates in green EMER in red and flashing Press to talk button Handset release Pull the lever to r...

Страница 277: ...ges No other function can be selected After message release oxygen mask interphone button Calls from cabin Press oxygen mask interphone button to answer message the passengers will also hear the an sw...

Страница 278: ...uttonlights PA Select to give passenger messages CALL Select to call cockpit EMRG Select to emergency call cockpit The selected CALL or EMER buttonlight comes on together with HI LOW chime when cabin...

Страница 279: ...N READ L CABIN READ R Boarding music if installed R ESS BUS L 11 BOARD MUSIC Supplied by the R INV BUS if the boarding music is AC powered IF TAWS INSTALLED PA L BAT BUS E 12 PA L Passenger cabin atte...

Страница 280: ...COMMUNICATIONS PA INTERPHONE Description Aircraft Operations Manual 4 4 1 S1 PAGE 8 Dec 01 15 A C 160 379 THIS PAGE INTENTIONALLY LEFT BLANK...

Страница 281: ...for distribution of messages Boarding music entertainment systems 2 MAIN COMPONENTS AND SUBSYSTEMS 2 1 PA AMPLIFIER The PA amplifier basically consists of an amplifier circuit and a chime generator c...

Страница 282: ...L Digital Remote electric unit REU PA amplifier Audio chime Cockpit speakers Audio chime Cabin speakers Cockpit voice recorder Attendant panel Passenger call buttons COCKPIT INTERPHONE CABIN INTERPHON...

Страница 283: ...attendant Cabin PA volume Only when PA selected in cockpit or cabin Messages given to the passanger from cockpit crew or cabin attendant can be listened to by increasing the PA volume A14872 SEAT BELT...

Страница 284: ...nction button Calls from cabin Press the CAB interphone button to answer message After message release the CAB inter phone button Interphone calls Calls to cabin Lift the handset and select PA CALL or...

Страница 285: ...ges No other function can be selected After message release oxygen mask interphone button Calls from cabin Press oxygen mask interphone button to answer message the passengers will also hear the an sw...

Страница 286: ...tton Only needed for PA calls Call buttons EMG Emergency call to flight deck PA Passenger calls FLT Flight deck call The phone is protected against inadvertent use the handset must be released before...

Страница 287: ...4 A CABIN CALL LIGHTS PA green CALL green EMERGENCY red and flashing The selected CALL or EMER call light comes on together with HI LOW chime when cabin attendant is called by cockpit crew PA call lig...

Страница 288: ...READ L CABIN READ R Boarding music if installed R ESS BUS L 11 BOARD MUSIC Supplied by the R INV BUS if the boarding music is AC powered IF TAWS INSTALLED PA L BAT BUS E 12 PA L Passenger cabin atten...

Страница 289: ...IN Call button lights PA Select to give passenger messages CALL Select to call cabin attendant EMER Select to give emergency call to cabin attendant Via cockpit interphone 1 Button light cockpit inter...

Страница 290: ...LLS FROM CABIN Cabin attendant announcements to the passengers is indicated by the PA button light coming on and can be listened to via the PA volume lever ACP Answer cabin attendant calls Via cockpit...

Страница 291: ...all button lights PA Select to give passenger messages CALL Select to call cockpit crew EMER Select to give emergency call to cockpit crew 1 Handset LIFT The interphone is protected against inadverten...

Страница 292: ...onlight goes off indicating the interphone is reset when the cockpit handset interphone button is replaced reset When calling the cockpit If the pilots are using oxygen masks the answer will come over...

Страница 293: ...l button lights PA Select to give passenger messages CALL Select to call cabin attendant EMER Select to give emergency call to cabin attendant Via cockpit interphone 2 Handset LIFT 3 Button light SELE...

Страница 294: ...button light goes off indicating the interphone is reset when the cabin attendant replaces the cabin handset Via headset with or without oxygen mask 2 CAB LP or RP button PRESS AND HOLD Answer the cal...

Страница 295: ...reset 2 5 CALLS FROM COCKPIT Cockpit announcement to the passengers are indicated by the PA buttonlight comes on 1 Handset cabin interphone LIFT 2 Handset talk switch PRESS AND HOLD Answer the call Af...

Страница 296: ...PAGE 4 Apr 01 15 A C 380 up 3 ABNORMAL OPERATION It is recommended that the individual operator develop alternative procedures for normal operation in case of interphone system failure CONDITIONS ABN...

Страница 297: ...nel VHF com transceiver and a VHF an tenna The ground station network consists of a VHF com ground station controlled by a central pro cessing computer and a switching network con nected to individual...

Страница 298: ...mmuting with the ARINC central computer through the switching network Fig 2 The ARINC Electronics Switching Systems ESS network provides VHF radio coverage to enroute aircraft and terminal coverage at...

Страница 299: ...1 PAGE 3 Apr 01 15 A9870 AIRLINE COMPUTER AIRLINE COMPUTER AIRLINE COMPUTER WIRE LINE GROUN D STATION GROUN D STATION ESS NET WORK VHF COM MANAGEMENT UNIT ARINC VHF RADIO SITE ARINC VHF RADIO SITE ARI...

Страница 300: ...ion Aircraft Operations Manual 4 5 1 PAGE 4 Apr 01 15 3 CONTROLS AND INDICATORS A9866 A Collins D A T A L I N K A ACARS CONTROL DISPLAY PANEL Ambient Light sensor Touch sensitive display Fig 3 ACARS c...

Страница 301: ...ightness control page DIAG Displays MIDU location page which shows pgm pin status Select User Function page keypads 1 2 Label Function Performed MENU Displays MIDU MENU page Up arrow not operational D...

Страница 302: ...ys MIDU MENU page RTN Displays subsystem page CLR Clears last operation Clears last character CLR LINE Clears scratch pad of last message text entry NUM Displays numeric keyboard page Numeric keyboard...

Страница 303: ...paper advance The paper will advance as long as the button is depressed PWR ON light green Indicates when printer is under power 115 VAC ALERT RESET button Press button to reset the PTR BUSY alert PT...

Страница 304: ...COM 3 R MAIN BUS L 14 VHF COM3 ACARS R INV BUS 115 VAC N 18 ACARS PWR Back up power ACARS R HOT BAT BUS N 19 ACARS BACK UP With Mod No 2544 installed the power supply for ACARS COM3 and Inverter is c...

Страница 305: ...that the ACARS can be used on battery power NOTE 2 2 PRINTER SELF TEST 1 SELF TEST button PRESS A test pattern will be printed as long as the button is depressed 2 3 CONTROL DISPLAY PANEL Keep the di...

Страница 306: ...MAL PROCEDURES 3 1 ACARS FAIL URE POWER SUPPLY INDICATIONS ACARS display control panel is black and PWR ON light on the printer is extin guished ACTIONS 1 CB N 18 ACARS PWR CHECK RESET 2 CB N 19 ACARS...

Страница 307: ...recognized 243 000 MHz emergency frequency The transceiver allows conti nuos monitoring of that frequency while simulta neously receiving on the tuneable main receiver The operating frequency may be s...

Страница 308: ...n pressed and held the program ming mode for channels is activated Frequency Channel select Receive Mode select Each momentary press cycles through the following modes MAIN Allows transmitting and rec...

Страница 309: ...MICROPHONE PTT D I S C A P A CONTROL WHEEL PTT BUTTON C B A B C XMIT SELECT 1 COM 2 COM 3 HF INT COLD BOOM HOT MIC MASK NORM EMER 1 NAV 2 MKR PA 1 ADF 2 SPKR VOICE IDENT PTT C AUDIO CONTROL PANEL ACP...

Страница 310: ...COMMUNICATIONS UHF COM Description Aircraft Operations Manual 4 6 1 O PAGE 4 Apr 01 15 4 ELECTRICAL POWER SUPPLY UHF RH AVIONIC BUS L 14 UHF...

Страница 311: ...to decrease the volume 2 2 UHF COM SYSTEM TEST 1 PUSH TONE button COM control unit PRESS AND HOLD Pressing this button modulates the signal with a 1 KHz tone This verifies the operation of the transm...

Страница 312: ...he frequency display begins to flash 4 Frequency selector SET FREQUENCY Rotate the frequency selector knobs to select the desired receive transmit frequency see 2 6 The display now indicates the desir...

Страница 313: ...cy selector knobs to change the MHz portion of the fre quency to 225 or 399 Decrement one step from 225 or increment one step from 399 and the display will show dashes in the frequency display 5 CHAN...

Страница 314: ...nob to change the frequency in 25 KHz steps Rotate the large frequency selector knob to change the frequency in 1 MHz steps 2 9 COMMUNICA TIONS Receiving 1 UHF COM 3 volume lever ACP ADJUST Use headse...

Страница 315: ...active for more than 90 seconds a transmit timeout error occurs This is indicated by the flashing of every illuminated segment of the display The transmitter will go inactive until the fault is found...

Страница 316: ...d 2 Display CHECK The fault display shall be shown on the right side of the bottom row of the display It shall be made up of the alphabetic character F and a number as shown below CODE FAULT 0 None 1...

Страница 317: ...ELECTRICAL Aircraft Operations Manual 5 CONTENTS PAGE 1 Apr 01 15 CONTENTS Electrical 5 0 Highlight not applicable 5 1 Description 5 2 Operation...

Страница 318: ...ELECTRICAL Aircraft Operations Manual 5 CONTENTS PAGE 2 Apr 01 15 THIS PAGE INTENTIONALLY LEFT BLANK...

Страница 319: ...d through the standby inverter from the R MAIN BUS Wild frequency AC used for ice protection only is supplied from two generators driven by the respec tive propeller gearbox to the L and R GEN BUS 115...

Страница 320: ...uld not be used for engine starting A second thermal switch closes at a tem perature of 71 C thereby disconnecting the battery from its GEN BUS and the START BUS indicated by a BAT HOT light on the ov...

Страница 321: ...R BAT switch on overhead panel in ON posi tion EXT PWR switch off Battery temperature below 71 C or Battery switch in OVRD positions for emergency use only The batteries will be charged from respecti...

Страница 322: ...AIN BUS also supplies the UTILITY BUS via a RCCB If the R MAIN BUS is powered the RCCB will close and supply power to the UTILITY BUS provided both generators are on line or exter nal power is switche...

Страница 323: ...battery voltage drop and must be reset after engine start if tripped 2 9 Wild frequency AC system Fig 10 The wild frequency 115V AC system is for ice protection only Wild is because the frequency is...

Страница 324: ...BUS relay L AVION BUS relay RCCB Left power distrubution unit Right power distrubution unit R MAIN BUS relay UTILITY BUS relay START BUS R GEN BUS R HOT BAT BUS Left generator control unit GCU Right g...

Страница 325: ...ION BUS relay RCCB Left power distrubution unit Right power distrubution unit R MAIN BUS relay UTILITY BUS relay START BUS R GEN BUS R HOT BAT BUS Left generator control unit GCU Right generator contr...

Страница 326: ...RCCB Left power distrubution unit Right power distrubution unit R MAIN BUS relay UTILITY BUS relay START BUS R GEN BUS R HOT BAT BUS Left generator control unit GCU Right generator control unit GCU Ge...

Страница 327: ...BUS relay RCCB Left power distrubution unit Right power distrubution unit R MAIN BUS relay UTILITY BUS relay START BUS R GEN BUS R HOT BAT BUS Left generator control unit GCU Right generator control...

Страница 328: ...N BUS relay RCCB Left power distrubution unit Right power distrubution unit R MAIN BUS relay UTILITY BUS relay START BUS R GEN BUS R HOT BAT BUS Left generator control unit GCU Right generator control...

Страница 329: ...ION BUS relay RCCB Left power distrubution unit Right power distrubution unit R MAIN BUS relay UTILITY BUS relay START BUS R GEN BUS R HOT BAT BUS Left generator control unit GCU Right generator contr...

Страница 330: ...RCCB Left power distrubution unit Right power distrubution unit R MAIN BUS relay UTILITY BUS relay START BUS R GEN BUS R HOT BAT BUS Left generator control unit GCU Right generator control unit GCU G...

Страница 331: ...B Left power distrubution unit Right power distrubution unit R MAIN BUS relay UTILITY BUS relay START BUS R GEN BUS R HOT BAT BUS Left generator control unit GCU Right generator control unit GCU Gen r...

Страница 332: ...Inverter 1 L MAIN BUS 2 Inverter R MAIN BUS MAIN AND STANDBY INVETER SYSTEM MAIN INV STBY INV MAIN INV 115V 26V ON OFF L INV BUS 115 VAC R INV BUS 115 VAC L INV BUS 26 VAC R INV BUS 26 VAC INVERTER 1...

Страница 333: ...ELECTRICAL Description Aircraft Operations Manual 5 1 PAGE 15 Jun 01 19 A12678 Fig 10 Wild frequency AC system schematic...

Страница 334: ...ire handle HP Bleed and Gen shut off Dome entrance and cargo lights L battery voltage indication AHRS 1 backup power L Battery control R HOT BAT BUS R engine fire extinguisher R fire handle HP Bleed a...

Страница 335: ...engine temp ITT L engine torque L engine oil temp and press indication L engine fuel flow L engine CTOT L and R engine anti ice control lights Cont d R BAT BUS Fuel used indication if installed Outflo...

Страница 336: ...rol ind Wing and stab de ice air supply control Warning annunciator system channel 2 with mod 2328 and 300 up ACARS VHF COM3 if installed with mod 2544 INVERTER 2 with mod 2544 FI STOP with mod no 225...

Страница 337: ...ic pump AUTO L engine anti ice air valve fails open Anti skid inboard L landing light Navigation lights one bulb each position Cabin window lighting Propeller synchrophazing L HP manual control fails...

Страница 338: ...lost FDAU for a c 160 249 with mod 2245 and or with mod 2948 and for a c 250 UP AHRS 1 main power L AVION BUS voltage indication TAWS power if installed R AVIONIC BUS Flight director and MSP Autopilo...

Страница 339: ...ise Control if installed Tail compartment shutoff valve Cabin Attendant Call Buttons if installed AC Power Inverter if installed 230 V AC Cabin Power Outlets if installed EMERGENCY BUS Audio system ba...

Страница 340: ...PWS power R INV BUS 115 V AC Flight recorder power for a c 160 249 with mod 2245 and or with mod 2948 and for a c 250 UP Weather radar stabilization ACARS if installed WILD FREQUENCY AC POWER L GEN BU...

Страница 341: ...NN The BUS TIE relay is energized with power from the emergency bus and the generator buses are connected AUTO The BUS TIE relay is energized and the generator buses are connected with batteries ON an...

Страница 342: ...ELECTRICAL Description Aircraft Operations Manual 5 1 PAGE 24 Jun 01 19 THIS PAGE INTENTIONALLY LEFT BLANK...

Страница 343: ...drops below 24V ESS AVION switch Connects The ESS AVIONIC BUS to the L ESS BUS The EMER AVIONIC BUS to the EMER BUS L R AVION switch Connects The L R AVIONIC BUS to the respective MAIN BUS The L R AV...

Страница 344: ...ELECTRICAL Description Aircraft Operations Manual 5 1 PAGE 26 Jun 01 19 THIS PAGE INTENTIONALLY LEFT BLANK...

Страница 345: ...or Indicates the voltage for respective selected bus or source If L or R GEN selected the indicator also shows current load in amperes NOTE AMP is only indicated when L or R GEN is selected DC AMP VOL...

Страница 346: ...ELECTRICAL Description Aircraft Operations Manual 5 1 S1 PAGE 28 Jun 01 19 THIS PAGE INTENTIONALLY LEFT BLANK...

Страница 347: ...r Selects bus or source to be displayed on DC AMP VOLT indicator inverter lIGHT AMBER Comes on if the selected inverter fails or the INVERTER switch is in OFF position INVERTER switch In 1 or 2 positi...

Страница 348: ...ELECTRICAL Description Aircraft Operations Manual 5 1 S2 PAGE 28 Jun 01 19 THIS PAGE INTENTIONALLY LEFT BLANK...

Страница 349: ...es for the generator overvoltage circuit L R AC GEN light amber Comes on when the AC generator is not supplying power L R AC GEN switch ON Energizes the AC generator relay and thereby connects the AC...

Страница 350: ...tem comes on ICE PROT light amber The ICE PROT light will come on flashing together with the L R AC GEN light 5 6 7 8 9 10 5 6 7 8 9 10 AUTO COARSEN PITCH TRIM RUDDER LIMIT L FIRE DET FAIL R FIRE DET...

Страница 351: ...ELECTRICAL Description Aircraft Operations Manual 5 1 PAGE 31 Jun 01 19 A11394 STANDARD HIGHEST MODIFICATION STANDARD SHOWN L PL MIN T O Fig 16 Left side pilot circuit breaker panels standard...

Страница 352: ...ELECTRICAL Description Aircraft Operations Manual 5 1 PAGE 32 Jun 01 19 THIS PAGE INTENTIONALLY LEFT BLANK...

Страница 353: ...ECTRICAL Description Aircraft Operations Manual 5 1 PAGE 33 Jun 01 19 A11182 STANDARD HIGHEST MODIFICATION STANDARD SHOWN R PL MIN T O LDG RELAYS Fig 17 Right side pilot circuit breaker panels standar...

Страница 354: ...ELECTRICAL Description Aircraft Operations Manual 5 1 PAGE 34 Jun 01 19 THIS PAGE INTENTIONALLY LEFT BLANK...

Страница 355: ...l 5 1 PAGE 35 Jun 01 19 A24784 MAX OPTION HIGHEST MODIFICATION STANDARD SHOWN L PL MIN T O TOILET DATA AQUIS EXT 1 BUS DATA REC TAWS DATA AQUIS TAWS DATA BAT TAWS Applies to Mod No 3523 AQUIS Fig 18 L...

Страница 356: ...ELECTRICAL Description Aircraft Operations Manual 5 1 PAGE 36 Jun 01 19 THIS PAGE INTENTIONALLY LEFT BLANK...

Страница 357: ...Manual 5 1 PAGE 37 Jun 01 19 A30942 MAX OPTION HIGHEST MODIFICATION STANDARD SHOWN R PL MIN T O EXT 2 RELAYS BOARD MUSIC VSI NOISE CTL PWR ELT IND RECORD SW ICE IND AUDIO TAWS TERR DISP Fig 19 Right s...

Страница 358: ...ELECTRICAL Description Aircraft Operations Manual 5 1 PAGE 38 Jun 01 19 THIS PAGE INTENTIONALLY LEFT BLANK...

Страница 359: ...T Emergency K 4 EMER Utility S 5 UTILITY Overcurrent relay reset Bus tie reset K 1 RESET BUS TIE Batteries L battery vent L MAIN BUS K 2 L BAT VENT L battery control override J 1 CONTROL OVRD L batter...

Страница 360: ...ESS L avionic bus K 11 L AVION R avionic bus S 8 R AVION Emergency bus K 10 EMER AC generator Load transfer left A K 28 LOAD XFR A Load transfer left B K 27 LOAD XFR B Load transfer left C K 26 LOAD...

Страница 361: ...5 minutes A 600 Main batteries Voltage V DC 24 Capacity per battery Ah 43 Temperature C 30 Emergency lighting battery temperature must be warm er than 18 C NOTE Emergency power supply Voltage V DC 24...

Страница 362: ...be guarded in ON position 6 L BAT switch ON 7 R BAT switch ON Check BAT voltage to indicate min 24V for both batteries 8 L and R BAT HOT light CHECK OUT Check lights to be out 9 EMER PWR light CHECK O...

Страница 363: ...and R BAT light to come on indicating that batteries are discon nected from the generator and start busses Check BUS TIE CONN light to remain on If the external power voltage should drop to approximat...

Страница 364: ...ELECTRICAL Operation Aircraft Operations Manual 5 2 PAGE 4 Apr 01 15 3 ABNORMAL OPERATION For Abnormal Operation see section 23 ABNORMAL PROCEDURES and 24 EMERGENCY PROCEDURES...

Страница 365: ...ption 6 4 2 Operations not applicable PBE Smoke goggles 6 5 0 Highlights not applicable 6 5 1 Description 6 5 2 Operations not applicable Flotation equipment 6 6 0 Highlights not applicable 6 6 1 Desc...

Страница 366: ...EMERGENCY EQUIPMENT Aircraft Operations Manual 6 CONTENTS PAGE 2 Apr 01 15 THIS PAGE INTENTIONALLY LEFT BLANK...

Страница 367: ...310 L Fire extinguiser 1 F A life vest Passenger oxygen masks Full face mask PBE 1 when required PBE 1 when required Emergency flash light Main Door Forward right exit Overwing exits First aid kit Lif...

Страница 368: ...EMERGENCY EQUIPMENT Location Aircraft Operations Manual 6 1 1 PAGE 2 Apr 01 15 THIS PAGE INTENTIONALLY LEFT BLANK...

Страница 369: ...h pressure oxygen approx 1 850 psi The oxygen flows through a manually operated shut off valve to a pressure reg ulator which reduces pressure to 70 psi before it is distributed to outlets Each outlet...

Страница 370: ...push pull handle located on the forward right side pan el adjacent to the oxygen pressure gauge The handle has a green mark at the base indicating open position Oxygen to the passenger cabin is contro...

Страница 371: ...DET FAIL FUEL ELEC ICE PROT ENGINE FLAPS AIR COND PARK BRK ON HYDR EMER LTS UN ARMED OXYGEN DOORS AVIONICS VENT AVIONICS A SKID INOP L STALL FAIL GUST LOCK PUSHER SYSTEM R STALL FAIL A OXYGEN PRESSUR...

Страница 372: ...gen valve Observers oxygen outlet Pilot oxygen outlet Passen ger oxygen outlets Supply line Pilot oxygen outlet Charging connect Pressure indicator Regulator and supply valve LP relief HP relief Blow...

Страница 373: ...310 l portable oxygen bottle if desired However they can not be used with the small 120 l bottle which will only accept the first aid mask The quick donning masks are diluter demand type with mask mo...

Страница 374: ...movement The cabin has passenger oxygen outlets lo cated on the overhead passenger service units P S U and connected to the fixed system Num ber of outlets varies with national regulations Passenger...

Страница 375: ...s Minimum duration with 1 800 psi initial pressure One outlet in use 80 min Two outlets in use 50 min With the full face smoke mask in use duration is reduced to 10 20 min depending on inhalation rate...

Страница 376: ...ottle either by hanging it over your shoulder or on the passengers seat back connect mask turn valve fully open check flow put mask on passengers oxygen mask secure with elastic cord and metal strip M...

Страница 377: ...configurations are covered the basic 1 and the optional 3 fixed bottles installa tion Oxygen temperature OXYGEN SUPPLY DURATION charts are pres ented for 20 C 4 F 0 C 32 F 20 C 70 F and 40 C 105 F oxy...

Страница 378: ...ration Fig 11 are based on the descent profile for FAR 121 and the whole system configuration meets the FAR 121 require ment The optional 3 bottles installation with 2 or 3 crew masks in use and 30 pa...

Страница 379: ...GEN SUPPLY DURATION Basic 1 bottle system 2 crew masks in use OXYGEN BOTTLES TEMPERATURE 20 C 70 F 40 C 105 F AOM0009 0 C 32 F 20 C 4 F 60 120 90 30 40 50 70 80 100 110 1850 1800 1700 1600 1500 1400 1...

Страница 380: ...BOTTLES TEMPERATURE 20 C 70 F 40 C 105 F AOM0007 0 C 32 F 20 C 4 F OXYGEN SUPPLY DURATION Optional 3 bottle system 2 crew masks in use 60 120 90 30 40 50 70 80 100 110 1850 1800 1700 1600 1500 1400 1...

Страница 381: ...de a 2 hour oxygen supply to the cockpit crew 2 or 3 MINIMUM DISPATCH PRESSURE Basic 1 bottle system 4 passengers masks installation 2 COCKPIT CREW Minimum Dispatch Pressure PSI Outside Air Temperatur...

Страница 382: ...010 1050 1090 1120 1160 1200 1240 21 25 960 1000 1040 1080 1130 1170 1210 1250 1300 1340 1380 26 30 1050 1100 1150 1200 1240 1290 1340 1380 1430 1480 1530 3 COCKPIT CREW Minimum Dispatch Pressure PSI...

Страница 383: ...30 1170 1210 1250 1300 1340 1380 26 30 1050 1100 1150 1200 1240 1290 1340 1380 1430 1480 1530 31 34 1140 1190 1240 1290 1340 1390 1440 1490 1540 1600 1650 3 COCKPIT CREW Minimum Dispatch Pressure PSI...

Страница 384: ...altitudes When compiling the dispatch pressure it is important to notice that the last 300 psi of indicated oxygen pressure must be treated as unusable since the oxygen regulation function starts to...

Страница 385: ...come on Manually by selecting cockpit switch to ON or pushing F A button to ON provided any Battery Switch is in ON position or R ESS BUS is pow ered The F A button will activate the system also when...

Страница 386: ...in the cabin entrance area close to the F A seat The F A flashlight has a small red light which keeps blinking when the batteries are properly charged In the bottom a carrying loop is attached The fla...

Страница 387: ...button F A button Emergency lights may be selected on and off by pushing the button ARM yellow light comes on when EMER LIGHT cockpit switch is in ARMED position ON red light comes on when emergency l...

Страница 388: ...Lighting Aircraft Operations Manual 6 3 1 PAGE 4 Apr 01 15 A9920 A A CENTRAL WARNING PANEL EMER LTS UNARMED light amber The light will come on when the EMER LIGHT switch is in OFF position Fig 3 Emerg...

Страница 389: ...chemical which when ex pelled from the nozzle contains approx 85 liquid and 15 gas The liquid when hitting the fire forms a cloud The extinguishing effect is obtained through a chemical reaction in th...

Страница 390: ...epress trigger Aim at fire Hold the extinguisher upright It is possible to form water spray by holding a finger on the nozzle A31890 Trigger CO2 Cartridge Handle Standpipe Fig 2 H20 fire extinguisher...

Страница 391: ...es vary For full de scription contact your Flight Operations department 1 1 SMOKE GOGGLES There are two smoke goggles in the cockpit located behind each pilot s seat adjacent to the oxygen mask A thir...

Страница 392: ...EMERGENCY EQUIPMENT PBE Smoke Goggles Aircraft Operations Manual 6 5 1 PAGE 2 Apr 01 15 THIS PAGE INTENTIONALLY LEFT BLANK...

Страница 393: ...peration put the vest over the head tighten the straps around you pull the red inflation tabs after leaving through the exit use mouthpieces if the inflation doesn t work activate the light if needed...

Страница 394: ...EMERGENCY EQUIPMENT Flotation equipment Aircraft Operations Manual 6 6 1 PAGE 2 Jun 01 19 THIS PAGE INTENTIONALLY LEFT BLANK...

Страница 395: ...LT will then activate automatically on impact 3 2 Manual activation The ELT can be purposely activated by setting the ELT switch in cockpit to ON 3 3 Deactivation Should the ELT be inadvertently activ...

Страница 396: ...ency Locator Transmitter Aircraft Operations Manual 6 7 1 S1 PAGE 2 Apr 01 15 A C 160 170 A11112 A A EMERGENCY PANEL ELT switch ON Manual activation of ELT ARMED Automatic activation of ELT by impact...

Страница 397: ...he cargo compartment ELT external antenna Blade antenna for portable operation Pull plastic end to extend the antenna RESET button When pressed the ELT selector in OFF position the ELT is deactivated...

Страница 398: ...EMERGENCY EQUIPMENT Emergency Locator Transmitter Aircraft Operations Manual 6 7 1 S1 PAGE 4 Apr 01 15 A C 160 170 THIS PAGE INTENTIONALLY LEFT BLANK...

Страница 399: ...um capacity of 52 hours of transmission There is one permanent external antenna mounted on the tail cone The ELT is controlled by an internal impact switch and an ELT switch on the transmitter front p...

Страница 400: ...ency Locator Transmitter Aircraft Operations Manual 6 7 1 S2 PAGE 2 Apr 01 15 A C 171 299 A11112 A A EMERGENCY PANEL ELT switch ON Manual activation of ELT ARMED Automatic activation of ELT by impact...

Страница 401: ...pr 01 15 A C 171 299 A11217 A Access panel to the ELT in the cargo compartment ELT external antenna A EMERGENCY LOCATOR TRANSMITTER ELT switch AUTO Normal position Automatic ac tivation by impact swit...

Страница 402: ...EMERGENCY EQUIPMENT Emergency Locator Transmitter Aircraft Operations Manual 6 7 1 S2 PAGE 4 Apr 01 15 A C 171 299 THIS PAGE INTENTIONALLY LEFT BLANK...

Страница 403: ...ERGENCY panel 3 1 Automatic activation For normal operation the ELT switch in cockpit shall be positioned in ARMED position The ELT will then activate automatically on impact 3 2 Manual activation The...

Страница 404: ...installed A11194 A A EMERGENCY PANEL RESET ELT switch ON Manual activation of ELT Transmission starts after 30 seconds ARMED Automatic activation of ELT by impact switch RESET Deactivation of ELT tran...

Страница 405: ...artment ELT external antenna A EMERGENCY LOCATOR TRANSMITTER Locking mechanism for re lease of the clamp Flexible antenna For portable use Safety string The ELT will flash in upside position in water...

Страница 406: ...EMERGENCY EQUIPMENT Emergency Locator Transmitter Aircraft Operations Manual 6 7 1 S3 PAGE 4 Apr 01 15 A C 300 UP or with Mod No 2204 installed THIS PAGE INTENTIONALLY LEFT BLANK...

Страница 407: ...utomatic activation For normal operation the ELT switch in cockpit shall be positioned in ARMED position The ELT will then activate automatically on impact 3 2 Manual activation The ELT can be purpose...

Страница 408: ...recision ELT A11194 A A EMERGENCY PANEL RESET ELT switch ON Manual activation of ELT Transmission starts after 2 seconds ARMED Automatic activation of ELT by impact switch RESET Deactivation of ELT tr...

Страница 409: ...switch or activation by remote switch Portable use MAN RESET ELT is on in MAN RESET position OFF ELT is off in OFF position A ELT EXTERNAL ANTENNA A EMERGENCY LOCATOR TRANSMITTER OFF ANT MAN AUTO RES...

Страница 410: ...EMERGENCY EQUIPMENT Emergency Locator Transmitter Aircraft Operations Manual 6 7 1 S4 PAGE 4 Apr 01 15 With Mod No 3112 installed Air Precision ELT THIS PAGE INTENTIONALLY LEFT BLANK...

Страница 411: ...e EMERGENCY overhead panel in the flight com partment Upon activation the ELT starts to transmit on 121 5 and 243 MHz There is a time delay of 47 seconds before the ELT starts to transmit on 406 25 MH...

Страница 412: ...ion indicated by red flashing light Transmission on 121 5 and 243 MHz starts upon activation and after 47 seconds on 406 25 MHz ELT switch ON Manual activation of ELT Transmission on 121 5 and 243 MHz...

Страница 413: ...to the ELT in the cargo compartment ELT external antenna ELT switch ON Normal position Automatic activation by impact switch or activation by remote switch OFF ELT is off OFF ON A ELT Activation indic...

Страница 414: ...EMERGENCY EQUIPMENT Emergency Locator Transmitter Aircraft Operations Manual 6 7 1 S5 PAGE 4 Apr 01 15 Applicable for A C with mod 3504 Artex ELT C406 1 THIS PAGE INTENTIONALLY LEFT BLANK...

Страница 415: ...1 x3 plastic adhesive bandage 16 per unit 2 PVP iodine swabs 10 per unit 1 Ammonia inhalants 10 per unit 8 4 bandage compress 1 per unit 5 Triangular bandage 1 per unit 1 Calloid 1 8 oz tube 6 per uni...

Страница 416: ...EMERGENCY EQUIPMENT First Aid Kit Aircraft Operations Manual 6 8 1 PAGE 2 Apr 01 15 THIS PAGE INTENTIONALLY LEFT BLANK...

Страница 417: ...t Operations Manual 6 9 1 PAGE 1 Apr 01 15 1 SPARE BULBS AND FUSES Two boxes located in the cockpit L and R lower side panels respectively contain spare bulbs and fuses as well as padlocks for externa...

Страница 418: ...EMERGENCY EQUIPMENT Spare bulbs and fuses Aircraft Operations Manual 6 9 1 PAGE 2 Apr 01 15 THIS PAGE INTENTIONALLY LEFT BLANK...

Страница 419: ...ation NOTE 2 MAIN DOOR If the main door handle has been inadvertently moved to the closed position with the door open a latch in the middle of the door inside has to be pressed before the handle can b...

Страница 420: ...atch Check centered prior flight Shoot bolt index window Shoot bolt tip switch External Door Handle Guidepin Switch Fig 2 Main door operation and indication Opening from inside release flaps move hand...

Страница 421: ...locking mechanisms are found in the up per ends the lower ends have hooks Operation Forward right exit outside handle is located on the bottom of the hatch NOTE A9880 OPEN EMERGENCY EXIT PULL EXIT COV...

Страница 422: ...eration To open hatch from inside turn handle 90 degrees to OPEN remove hatch For ventilation smoke evacuation turn handle 45 degrees to VENTILATION lower hatch to the stop approx 4 inches To open hat...

Страница 423: ...o handle for door inside operation Without Mod No 1819 accomplished The Inside Door Handle can be inserted in the fit ting through a hole in the door linkage cover panel With Mod No 1819 accomplished...

Страница 424: ...ation The reason for this is the possibility of a bent slide hand rail which could render the stair un movable or stuck in a middle position thereby blocking the exit CAUTION Operation To extend from...

Страница 425: ...FIRE PROTECTION Aircraft Operations Manual 7 CONTENTS PAGE 1 Apr 01 15 CONTENTS Fire Protection 7 0 Highlights not applicable 7 1 Description 7 2 Operation...

Страница 426: ...FIRE PROTECTION Aircraft Operations Manual 7 CONTENTS PAGE 2 Apr 01 15 THIS PAGE INTENTIONALLY LEFT BLANK...

Страница 427: ...L R FIRE DET FAIL light on CWP to steady The CWP light remains on as long as the caution condition exists The engine fire warning and detector failure system can be tested with two switches on the TE...

Страница 428: ...s except the respective CWP light which will change from flashing to steady and stay on until the smoke has disappeared In the standard passenger version the smoke de tectors are tested by one single...

Страница 429: ...ndard system may be installed on the left side of the cargo compartment Like the standard system the extinguisher is dis charged in two stages the first with rapid flooding and the second with a slowe...

Страница 430: ...FIRE PROTECTION Description Aircraft Operations Manual 7 1 PAGE 4 Apr 01 15 THIS PAGE INTENTIONALLY LEFT BLANK...

Страница 431: ...ON Description Aircraft Operations Manual 7 1 S1 PAGE 5 Applicable to aircraft without Mod No 3400 3401 installed A11992 Triple chimes Fig 1 Engine fire protection and exhaust duct overtemperature sys...

Страница 432: ...FIRE PROTECTION Description Aircraft Operations Manual 7 1 S1 PAGE 6 Apr 01 15 Applicable to aircraft without Mod No 3400 3401 installed THIS PAGE INTENTIONALLY LEFT BLANK...

Страница 433: ...OT CONTROL UNIT MASTER WARNING MASTER WARNING SENSOR LOOP FIRE LOOP FIRE L R TEST 1 PANEL FIRE SHORT FIRE TEST DETECTOR FAILURE TEST TRIPLE CHIMES SINGLE CHIMES FIRE BELL FLASHING FLASHING CWP FLASHIN...

Страница 434: ...FIRE PROTECTION Description Aircraft Operations Manual 7 1 S2 PAGE 6 Apr 01 15 Applicable to aircraft with Mod No 3400 3401 installed THIS PAGE INTENTIONALLY LEFT BLANK...

Страница 435: ...FIRE PROTECTION Description Aircraft Operations Manual 7 1 PAGE 7 Apr 01 15 A11993 Pressure gauge Fig 2 Engine fire extinguishing system...

Страница 436: ...r Cargo smoke sensor Repetitive chimes MASTER WARNING Flashing AVIONIC SMOKE LAV SMOKE CARGO SMOKE CWP flashing Smoke signal Lavatory smoke sensor Test signals TEST 1 PANEL SMOKE NOTE With Mod No 1819...

Страница 437: ...de of the fire will be discharged through the crossover line into the fire Engine fire handle 2 Will come on red when a fire condition occurs and remain on until the fire is out When the handle is pul...

Страница 438: ...PUSHER SYSTEM R STALL FAIL CENTRAL WARNING PANEL A L R ENG FIRE light red Comes on flashing for an engine fire condition The light will remain on as long as the fire exists AVIONIC LAV CARGO SMOKE li...

Страница 439: ...ture system are checked with a simulated warning condition The engine fire test warnings are MASTER WARNING lights L R ENG FIRE light L R fire handle light Fire bell The additional tail pipe overtempe...

Страница 440: ...FIRE PROTECTION Description Aircraft Operations Manual 7 1 PAGE 12 Apr 01 15 A11994 Fig 7 Fire protection controls and indicators...

Страница 441: ...Lavatory cargo smoke det R BAT BUS L 3 LAV CARGO SMOKE Fire extinguishing L main squib R reserve squib L HOT BAT BUS E 3 L BOTTLE R main squib L reserve squib R HOT BAT BUS L 3 R BOTTLE Left engine sh...

Страница 442: ...FIRE PROTECTION Description Aircraft Operations Manual 7 1 PAGE 14 Apr 01 15 THIS PAGE INTENTIONALLY LEFT BLANK...

Страница 443: ...and check that MASTER WARNING lights come on L ENG FIRE light comes on L TAIL P HOT light comes on L ENG fire handle light comes on Fire bell sounds Repetitive chime sounds Hold switch in R and check...

Страница 444: ...FIRE PROTECTION Operation Aircraft Operations Manual 7 2 PAGE 2 Apr 01 15 3 ABNORMAL OPERATION For Abnormal Operation see section 23 ABNORMAL PROCEDURES and 24 EMERGENCY PROCEDURES...

Страница 445: ...FLIGHT CONTROLS Aircraft Operations Manual 8 CONTENTS PAGE 1 Apr 01 15 CONTENTS Flight Controls 8 0 Highlights not applicable 8 1 Description 8 2 Operation...

Страница 446: ...FLIGHT CONTROLS Aircraft Operations Manual 8 CONTENTS PAGE 2 Apr 01 15 THIS PAGE INTENTIONALLY LEFT BLANK...

Страница 447: ...ly actuated Geared tabs are used with the elevator and aileron systems while a spring tab is used with the rudder system The geared tabs deflect proportionally to control surface movement to assist th...

Страница 448: ...ing the pitch disconnect handle in the cockpit which separates the two channels from each other If the handle is not pulled the dis connect function is automatically reset when the excessive control f...

Страница 449: ...interconnected and are oper ated by hydraulic power and controlled with a han dle on the center pedestal The flaps can also be powered by hydraulic hand pump pressure Ref AOM 10 1 and 10 2 To prevent...

Страница 450: ...e center pedestal These switches actuate the right elevator trim tab only Standby pitch trim also deactivates the synchro nization In this case it can be reset with the PITCH RESET switch on the trim...

Страница 451: ...or Dual pointers L and R indicate position of left and right flaps Flap handle Used to select flap positions as indicated on the handle placard Detents at 7 15 20 and 35 For flaps up selection there a...

Страница 452: ...he movement of the power levers is limited by a stop on the gust lock handle With the gust lock engaged the following is possible Operation of right engine propeller brake Erasing of cockpit voice rec...

Страница 453: ...Standby roll trim switches right set guarded control the right aileron trim tab Yaw trim is accomplished by operating the yaw trim switches simultaneously Standby pitch trim switches guarded control...

Страница 454: ...FLIGHT CONTROLS Description Aircraft Operations Manual 8 1 PAGE 8 Apr 01 15 THIS PAGE INTENTIONALLY LEFT BLANK...

Страница 455: ...H TRIM lights comes on when pitch trim synchronization is deactivated GUST LOCK light amber The GUST LOCK light comes on if gust lock handle is in off position but the rudder gust lock remains engaged...

Страница 456: ...FLIGHT CONTROLS Description Aircraft Operations Manual 8 1 PAGE 10 Apr 01 15 THIS PAGE INTENTIONALLY LEFT BLANK...

Страница 457: ...actuator which permanently separates the interconnection between left and right aileron control channels Pitch disconnect handle Pulling the handle activates an electrical actuator which permanently s...

Страница 458: ...AT BUS N 1 TRIM PITCH ROLL Pitch trim sync R BAT BUS N 6 PITCH TRIM SWITCH Pitch roll disconnect L BAT BUS G 3 PITCH ROLL DISC Rudder limiter L AVIONIC START BUS G 5 RUDDER LIMIT Rudder limiter overri...

Страница 459: ...both MAIN PITCH and STBY PITCH trim indicators to move towards UP and DN positions 2 Check that left pilot s pitch trim switches override right to pilots s switches Check that the MAIN PITCH trim can...

Страница 460: ...ated by just one switch 2 3 FLAP SYSTEM TEST Check flap area to be free from obstructions CAUTION 2 4 FLAP SYSTEM TEST Check and set flaps as follows 1 Flap handle FULL DOWN Check flap indicator point...

Страница 461: ...rspeed According to Table 201 in referenced AMM section Flaps Gear According to Table 201 in referenced AMM section Yaw Damper OFF Autopilot OFF Autopilot OFF The aircraft must be free of ice and the...

Страница 462: ...ORMAL PROCEDURES 3 1 FLIGHT CONTROL MALFUNC TIONS It is of utmost importance that a thorough and professional trouble shooting is per formed whenever an irregular or abnormal function the flight contr...

Страница 463: ...FUEL Aircraft Operations Manual 9 CONTENTS PAGE 1 Apr 01 15 CONTENTS Fuel 9 1 0 Highlights 9 1 1 Description 9 1 2 Operation Fueling instruction 9 2 0 Highlights 9 2 1 Description 9 2 2 Operation...

Страница 464: ...FUEL Aircraft Operations Manual 9 CONTENTS PAGE 2 Apr 01 15 THIS PAGE INTENTIONALLY LEFT BLANK...

Страница 465: ...s chapter assumes a certain modification standard of the aircraft If a modification is not installed the following apply as a complement to what is stated in this chapter DESCRIPTION OPERATION 0 1 FUE...

Страница 466: ...FUEL Highlights Aircraft Operations Manual 9 1 0 PAGE 2 Apr 01 15 THIS PAGE INTENTIONALLY LEFT BLANK...

Страница 467: ...e is one engine driven main fuel boost pump on each engine and an electrically driven standby pump in each tank The standby pump starts auto matically by a pressure switch in case of a main pump failu...

Страница 468: ...noid controlled and actuated by the fueling pressure They are lo cated inside the inboard tank cells The outboard cells are replenished by overflow through the vent line from the inboard cells Optical...

Страница 469: ...ank a float switch in each inboard cell will activate the master caution L R LOW LEVEL light on the overhead panel and FUEL CWP light Mechanical quantity indication There is a magnetic dipstick in eac...

Страница 470: ...index scale If the tank is filled with more fuel than indicated by 10 index the correct fuel quantity can not be measured by the dipstick Reading 10 index means however that there is a minimum of 472...

Страница 471: ...FUEL Description Aircraft Operations Manual 9 1 1 PAGE 5 Apr 01 15 STANDBY PUMP DIFFERENTIAL PRESSURE SWITCH A11644 MAIN PUMP DIFFERENTIAL PRESSURE SWITCH Fig 4 Fuel system schematic...

Страница 472: ...FUEL Description Aircraft Operations Manual 9 1 1 PAGE 6 Apr 01 15 THIS PAGE INTENTIONALLY LEFT BLANK...

Страница 473: ...6 XFEED ON R VALVE CLOSED L VALVE CLOSED L FUEL FILTER L MAIN PUMP L STBY PRESS R FUEL FILTER R MAIN PUMP R STBY PRESS R LOW LEVEL L LOW LEVEL Engine feed Crossfeed Interconnect Refuel defuel Vent Ven...

Страница 474: ...FUEL Description Aircraft Operations Manual 9 1 1 PAGE 8 Apr 01 15 THIS PAGE INTENTIONALLY LEFT BLANK...

Страница 475: ...Fueling light blue Indicates that the fueling panel is operated for fueling or defueling The light comes on either when the FUEL PAN EL switch is on FUEL PANEL position or the defuel valve is open Tem...

Страница 476: ...FUEL Description Aircraft Operations Manual 9 1 1 PAGE 10 Apr 01 15 THIS PAGE INTENTIONALLY LEFT BLANK...

Страница 477: ...35 30kg CONN VALVE OPEN light amber Comes on when the interconnect valve is open CONN VALVE switch When set to OPEN the interconnect valve will open and the CONN VLV OPEN light will come on indicating...

Страница 478: ...FUEL Description Aircraft Operations Manual 9 1 1 PAGE 12 Apr 01 15 THIS PAGE INTENTIONALLY LEFT BLANK...

Страница 479: ...ANEL FUEL light amber Comes on flashing whenever a caution light as sociated with the fuel system comes on except for XFEED ON and CONN VLV OPEN FUEL test switch L Left fuel quantity indicators shows...

Страница 480: ...FUEL Description Aircraft Operations Manual 9 1 1 PAGE 14 Apr 01 15 THIS PAGE INTENTIONALLY LEFT BLANK...

Страница 481: ...PUMP PWR Right standby pump control R BAT BUS R 14 R STBY PUMP CONTROL Right fuel press norm R BAT BUS R 15 R MAIN PRESS Valves Interconnect valve L ESS BUS J 14 CONN VALVE Crossfeed valve R ESS BUS...

Страница 482: ...FUEL Description Aircraft Operations Manual 9 1 1 PAGE 16 Apr 01 15 THIS PAGE INTENTIONALLY LEFT BLANK...

Страница 483: ...JP4 FL 250 Fuel temperature for above specified fuel types Kerosene fuel Jet A Jet A1 JP5 JP8 C 40 43 F 40 110 Wide cut fuel Jet B JP4 C 40 18 F 40 64 1 2 SYSTEM LIMITS LOW LEVEL light lb 230 300 370...

Страница 484: ...ve is fully closed 2 2 FUEL QUAN TITY INDICA TOR AND FUEL FLOW INDICA TOR TEST 1 FUEL test switch HOLD IN L Check left fuel quantity indicator to show without mod 2091 950 50 lb 432 23 kg with mod 209...

Страница 485: ...ure can be used to balance the fuel load in the tanks both on ground and during cruise 1 CONN VALVE switch OPEN Check CONN VLV OPEN light to come on When fuel quantities in both tanks are equal 2 CONN...

Страница 486: ...FUEL Operation Aircraft Operations Manual 9 1 2 PAGE 4 Apr 01 15 3 ABNORMAL OPERATION For Abnormal Operation see section 23 ABNORMAL PROCEDURES...

Страница 487: ...ibed in this chapter assumes a certain modification standard of the aircraft If a modification is not installed the following apply as a complement to what is stated in this chapter DESCRIPTION OPERAT...

Страница 488: ...FUEL FUELING INSTRUCTION Highlights Aircraft Operations Manual 9 2 0 PAGE 2 Apr 01 15 THIS PAGE INTENTIONALLY LEFT BLANK...

Страница 489: ...control switch OFF Refueling valves are closed MID LEVEL Refueling valves will close when tanks are filled to mid level FULL LEVEL Refueling valves will close at maximum tank capacity OVERFULL light r...

Страница 490: ...FUEL FUELING INSTRUCTION Description Aircraft Operations Manual 9 2 1 PAGE 2 Apr 01 15 THIS PAGE INTENTIONALLY LEFT BLANK...

Страница 491: ...ON Description Aircraft Operations Manual 9 2 1 PAGE 3 Apr 01 15 A12401 Fuel additive blender Handle Trigger Hold additive upright during blending Blender tube with nozzle attachment Fuel nozzle Fig 2...

Страница 492: ...FUEL FUELING INSTRUCTION Description Aircraft Operations Manual 9 2 1 PAGE 4 Apr 01 15 THIS PAGE INTENTIONALLY LEFT BLANK...

Страница 493: ...ctric SB 73 0048 Kerosene fuels JET A JET A1 JP5 JP8 Wide cut distillate fuels JET B JP4 In addition to the fuel types listed above all aviation gas turbine fuels not listed above but conforming to th...

Страница 494: ...terial for Aviation Turbine Fuels Addendum 76 1 Equivalent specifications Canada CAN 2 3 22 France AIR 3407 United kingdom DERD 2486 United States ASTM D1655 MIL T 5624 JP4 Mixing of different fuel ty...

Страница 495: ...itted in the fueling area A fire extinguisher shall be at hand during the fueling Do not connect or disconnect electrical power to the aircraft during fueling Do not operate the weather radar during f...

Страница 496: ...T Bonding cable from fuel truck connected to the grounding point beside the fueling panel 7 Fueling access door OPEN Check all switches to be OFF CLOSE Remove cap on receptacle Connect fuel nozzle 8 F...

Страница 497: ...stall cap on receptacle 18 Fuel panel access door CLOSE 19 Ground connection bonding cable REMOVE 2 3 GRAVITY FUELING 1 Check with flight crew or in Aircraft Log for complaints on the fuel systems In...

Страница 498: ...cap before disconnecting nozzle bonding cable 13 FUEL PANEL switch OFF 14 Fueling access door CLOSE 15 Ground connection bonding cable REMOVE 2 4 DEFUELING Pressure defueling is the quickest and most...

Страница 499: ...cap on receptacle Connect fuel nozzle 5 FUEL PANEL switch FUEL PANEL 6 IND TEST button DEPRESS Check quantity indicators to show without mod 2091 950 50 lb 432 23 kg with mod 2091 1000 50 lb 455 23 kg...

Страница 500: ...ON If defueling only bright tank leave switch in OFF Check XFEED ON light to come on 10 CONN VALVE switch CHECK CLOSED Outside the aircraft 11 Order suction defuel to start 12 Monitor defueling on th...

Страница 501: ...t a physician immediately WARNING 1 Perform items 1 to 10 of procedure 2 3 GRAVITY FUELING 2 Connect the additive can to the blender and connect the blender tube to the fuel nozzle See 9 2 1 Fig 2 Add...

Страница 502: ...FUEL FUELING INSTRUCTION Operation Aircraft Operations Manual 9 2 2 PAGE 10 Jun 01 17 THIS PAGE INTENTIONALLY LEFT BLANK...

Страница 503: ...HYDRAULICS Aircraft Operations Manual 10 CONTENTS PAGE 1 Apr 01 15 CONTENTS Hydraulics 10 0 Highlights not applicable 10 1 Description 10 2 Operation...

Страница 504: ...HYDRAULICS Aircraft Operations Manual 10 CONTENTS PAGE 2 Apr 01 15 THIS PAGE INTENTIONALLY LEFT BLANK...

Страница 505: ...p In case of loss of pressurization a spring will ensure a positive fluid supply Hand pump reservoir The hand pump reservoir supplies hydraulic fluid to the hand pump exclusively It has a capacity of...

Страница 506: ...en to 1650 psi Each accumulator has a capacity of 22 cubic inches approx 0 35 liters hydraulic fluid at 2900 psi pres sure It is important to notice that in case of a hydraulic pump failure when press...

Страница 507: ...HYDRAULICS Description Aircraft Operations Manual 10 1 PAGE 3 Apr 01 15 A11221 Return actuator Gear emergency uplock actuator Fig 1 Hydraulic system schematic...

Страница 508: ...HYDRAULICS Description Aircraft Operations Manual 10 1 PAGE 4 Apr 01 15 THIS PAGE INTENTIONALLY LEFT BLANK...

Страница 509: ...pressure falls below 2100 psi and until pressure reaches 2900 psi During landing gear extension or retraction irrespective of pressure When R PROP BRK switch is selected ON OFF No electrical power to...

Страница 510: ...erature of the fluid in the main reservoir Hand pump Provides hydraulic pressure to operate flaps brakes and landing gear Operated by a detachable handle stowed on the right rear cockpit wall Hand pum...

Страница 511: ...e L PDU Hydr pump control AUTO L MAIN BUS F 9 PUMP AUTO Hydr pump control OVRD L ESS BUS F 8 PUMP OVRD without Mod No 2414 Hydr pump control OVRD L BAT BUS F 8 PUMP OVRD with Mod No 2414 Hydr quantity...

Страница 512: ...HYDRAULICS Description Aircraft Operations Manual 10 1 PAGE 8 Apr 01 15 THIS PAGE INTENTIONALLY LEFT BLANK...

Страница 513: ...2100 2900 2950 Electrical pump OVRD psi 3000 Low pressure warning HYDR psi 1800 1850 1900 Temperature High temperature warning HYDR Light on C 116 Light off C 93 Quantity Main reservoir Capacity cu in...

Страница 514: ...power ON or gener ator supplying power NOTE After engine start 2 Hydraulic gauges CHECK Check pressures and quantity to be within green arc During approach 3 Hydraulic pressure CHECK Check all four hy...

Страница 515: ...hydraulic system pressure relief valve will open at 3 750 psi in main sys tem If the hydraulic pump is allowed to operate with relief valve controlling pressure hydraulic overtemperature will result N...

Страница 516: ...HYDRAULICS Operation Aircraft Operations Manual 10 2 PAGE 4 Apr 01 15 THIS PAGE INTENTIONALLY LEFT BLANK...

Страница 517: ...ICE RAIN PROTECTION Aircraft Operations Manual 11 CONTENTS PAGE 1 Apr 01 15 CONTENTS Ice Rain Protection 11 0 Highlights not applicable 11 1 Description 11 2 Operation...

Страница 518: ...ICE RAIN PROTECTION Aircraft Operations Manual 11 CONTENTS PAGE 2 Apr 01 15 THIS PAGE INTENTIONALLY LEFT BLANK...

Страница 519: ...cy system is used for ice and rain protection Bleed air is used for the wing and stabilizer inflatable boots the engine split lip and inlet guide vanes Electrical power is used for the remainder of th...

Страница 520: ...and outboard wing de ice and one in the fin for sta bilizer deice On a c s n 240 up post Mod 2083 the regu lated pressure is directed to a distribution duct supplying all boots through five ejector fl...

Страница 521: ...d to the Splitter Lip the inlet guide vanes and the Inlet Particle Separator Ejector Duct When power is increased the bleed air reduces and at 90 Ng corrected temperature related the sleeve valve is f...

Страница 522: ...s in the upper and lower duct A failure in the inlet ice protection system is indi cated by L or R INTAKE light in the ENGINE anti ice panel coming on The light comes on regardless of if the ENGINE AN...

Страница 523: ...ng Fig 4 The front windshields and the forward part of the side windshields are electrically heated from the 115 VAC wild frequency buses for anti icing L AC BUS supplies heating power for L front and...

Страница 524: ...st be powered for 5 minutes to be pro vide with full anti ice protection 2 7 Ice detector Optional Mod No 1933 The ice detector consists of an ultrasonic axially vibrating tube as sensing element The...

Страница 525: ...s will remain steady i e the flashing is suppressed The ice detector is powered from R AC GEN BUS IT IS VERY IMPORTANT TO UNDERSTAND THAT THE ICE DETECTOR ALERT SHALL NOT BE USED AS THE CUE FOR SWITCH...

Страница 526: ...ICE AND RAIN PROTECTION Description Aircraft Operations Manual 11 1 PAGE 8 Jun 01 17 THIS PAGE INTENTIONALLY LEFT BLANK...

Страница 527: ...jector Pneumatic system Pre cooler Shut off valve Regulator with relief and check valves Distribution duct Overheat sensor 150 C Distribution valve Horizontal stabilizer boots Vertical stabilizer boot...

Страница 528: ...ICE AND RAIN PROTECTION Description Aircraft Operations Manual 11 1 PAGE 10 Jun 01 17 THIS PAGE INTENTIONALLY LEFT BLANK...

Страница 529: ...Switching monitor unit 28 VDC control power Control power Max Norm Off Heating failure signal Power to heating boots on ground resetable circuit breakers L AC GEN R AC GEN ON LOAD XFR OFF R L AC GEN R...

Страница 530: ...OTECTION Description Aircraft Operations Manual 11 1 S1 PAGE 12 Jun 01 17 This page is applicable to aircraft with LUCAS intake Without Mod No 2095 and without Mod No 3529 or 3530 THIS PAGE INTENTIONA...

Страница 531: ...nit 28 VDC control power Control power Max Norm Off Heating failure signal Power to heating boots on ground resetable circuit breakers L AC GEN R AC GEN ON LOAD XFR OFF R L AC GEN R AC GEN AC HEAT Fro...

Страница 532: ...PROTECTION Description Aircraft Operations Manual 11 1 S2 PAGE 12 Jun 01 17 This page is applicable to aircraft with LUCAS intake Without Mod No 2095 and with Mod No 3529 or 3530 THIS PAGE INTENTIONAL...

Страница 533: ...cuit breakers L AC GEN R AC GEN ON LOAD XFR OFF R L AC GEN R AC GEN AC HEAT From R115 VAC GEN Bus GEN CONTROL UNIT GCU To RAC GEN Switch ON LOAD XFR OFF R Heating boot ON OFF signals Failure signals O...

Страница 534: ...PROTECTION Description Aircraft Operations Manual 11 1 O1 PAGE 12 Jun 01 17 This page is applicable to aircraft with COX intake With Mod no 2095 and without Mod No 3529 or 3530 THIS PAGE INTENTIONALL...

Страница 535: ...L UNIT GCU To RAC GEN Switch ON LOAD XFR OFF R Heating boot ON OFF signals Failure signals ON OFF signals ON OFF signals from GCU ON LOAD XFR OFFR signals from AC GEN switch MICRO PROCESSOR LOWER DUCT...

Страница 536: ...N PROTECTION Description Aircraft Operations Manual 11 1 O2 PAGE 12 Jun 01 17 This page is applicable to aircraft with COX intake With Mod no 2095 and with Mod No 3529 or 3530 THIS PAGE INTENTIONALLY...

Страница 537: ...AND RAIN PROTECTION Description Aircraft Operations Manual 11 1 S1 PAGE 13 Jun 01 17 A C 160 299 A9913 L Bat Bus R Bat Bus Gen Bus Gen Bus Gen Bus Gen Bus L Bat Bus R Bat Bus Fig 4 Window heat schema...

Страница 538: ...ICE AND RAIN PROTECTION Description Aircraft Operations Manual 11 1 S1 PAGE 14 Jun 01 17 A C 160 299 THIS PAGE INTENTIONALLY LEFT BLANK...

Страница 539: ...PROTECTION Description Aircraft Operations Manual 11 1 S2 PAGE 13 Jun01 17 A C 300 up A11029 L Bat Bus R Bat Bus Gen Bus Gen Bus Gen Bus Gen Bus L Bat Bus R Bat Bus ON OFF ON OFF ON OFF Fig 4 Window h...

Страница 540: ...ICE AND RAIN PROTECTION Description Aircraft Operations Manual 11 1 S2 PAGE 14 Jun01 17 A C 300 up THIS PAGE INTENTIONALLY LEFT BLANK...

Страница 541: ...OT R PITOT L ALPHA R ALPHA OAT STBY PITOT RW o W Switch NLG up lock switch R 115VAC GEN BUS 28 VDC 28 VDC STBY PITOT ON OFF ICE PROTECTION R INV BUS 28 VDC L 115VAC GEN BUS Right pitot Right angle of...

Страница 542: ...in any boot zone AUTO CYCLING switch in ONE CYCLE or CONT control power to timer is lost depressing any of the Manual push buttons while in CONT or during a one CYCLE sequence will result in the TIME...

Страница 543: ...e heat supplied by own gener ator OFF R Off reset position Power transfer from other side No intake heat L R PROP DE ICE light blue Will come on when the system is working and will go out in case of s...

Страница 544: ...ICE AND RAIN PROTECTION Description Aircraft Operations Manual 11 1 PAGE 18 Jun 01 17 THIS PAGE INTENTIONALLY LEFT BLANK...

Страница 545: ...me on when an overheat or controller fault occurs L R FRONT windshield heating switch Regulated power is applied to front windshield when set to ON L R PROP light ambers Will come on when a fault is d...

Страница 546: ...ICE AND RAIN PROTECTION Description Aircraft Operations Manual 11 1 S1 PAGE 20 Jun01 17 A C 160 299 THIS PAGE INTENTIONALLY LEFT BLANK...

Страница 547: ...d when set to ON L R PROP light ambers Will come on when a fault is detected in an acti vated system L R PROP de ice switch When set to ON a timer monitor initiates heating cycles as below for each pa...

Страница 548: ...ICE AND RAIN PROTECTION Description Aircraft Operations Manual 11 1 S2 PAGE 20 Jun 01 17 A C 300 up THIS PAGE INTENTIONALLY LEFT BLANK...

Страница 549: ...ber Will come on when power is lost to the tempera ture probe when NLG is locked in retracted posi tion L R ALPHA light amber Will come on when power loss is lost to the respec tive angle of attack se...

Страница 550: ...11 1 PAGE 22 Jun01 17 A9920 A ICE PROT light amber The ICE PROT light will come on flashing whenever a caution light associated with the ice protectin system comes on A CENTRAL WARNING PANEL Fig 10 I...

Страница 551: ...tional Mod No 1933 TEST Self test of the ice detector mi cro processor Flashing of the L and R ENG ANTI ICE blue sta tus light within 5 seconds while the switch is hold in TEST posi tion is a confirma...

Страница 552: ...ENG ANTI ICE blue status light within 5 seconds while the switch is hold in TEST position is a con firmation of a successful selftest ON Normal position The ice detection system is ON OFF Guarded OFF...

Страница 553: ...ption Aircraft Operations Manual 11 1 PAGE 25 Jun01 17 A14690 L BETA L PROP DE ICE L ENG ANTI ICE L APR L IGN 6 7 9 1 2 1 2 1 2 ICE SPD ON CENTER INSTRUMENT PANEL ICE SPD ON OFF pushbutton Fig 13 ICE...

Страница 554: ...BAT BUS H 26 L INTAKE Air control L L MAIN BUS H 25 L AIR VALVE Electric control R R BAT BUS R 27 R INTAKE Air control R R MAIN BUS R 28 R AIR VALVE Left intake PWR A L 115 VAC GEN BUS PWR B L 115 VAC...

Страница 555: ...trol R BAT BUS R 23 CONTROL Right side PWR A R 115 VAC GEN BUS R 24 PWR A PWR B R 115 VAC GEN BUS R 25 PWR B Control R BAT BUS R 26 CONTROL Windshield wipers Wiper L L BAT BUS H 28 L WIPER Wiper R R M...

Страница 556: ...erations Manual 11 1 S1 PAGE 28 Jun 01 17 A C 160 299 Cont d Ice detector with Mod No 1933 and 2546 R 115 VAC GEN BUS Ice detector with Mod No 3168 R 115 VAC GEN BUS Not in cockpit Improved S W system...

Страница 557: ...ight side PWR A R 115 VAC GEN BUS J 25 PWR A Control R BAT BUS J 24 CONTROL Windshield wipers Wiper L L BAT BUS H 28 L WIPER Wiper R R MAIN BUS P 28 R WIPER Probe heat Pitot L L 115 VAC GEN BUS J 27 L...

Страница 558: ...CTION Description Aircraft Operations Manual 11 1 S2 PAGE 28 Jun 01 17 A C 300 up Cont d Ice detector with Mod No 3168 R 115 VAC GEN BUS Not in cockpit Improved S W system Mod No 3529 or 3530 R BAT BU...

Страница 559: ...ps in PROP RPM below the preset AC generator trigger level If the drop lasts more than 7 seconds the AC generator will trip and MASTER CAUTION ICE PROT CWP lights will come on together with AC GEN cau...

Страница 560: ...when the OAT or SAT is 5 degrees C Minus 5 C or colder and any ice accretion is observed on any part of the aircraft Definition of icing conditions for operation of wing and stabilizer de ic ing boots...

Страница 561: ...w and then will in crease the possibility of identifying unexpected icing conditions The air inlet can be inspected from the cockpit by use of a flashlight Operation in and after certain icing conditi...

Страница 562: ...Ground Idle 2 HP BLD VALVE switch one only AUTO 3 AIR SUPPLY switch CHECK ON 4 BOOT IND switch ON Set BOOT IND switch to ON for boot indication lights to work during test 5 AUTO CYCLING switch ONE CY...

Страница 563: ...stals is present and three 3 de icing boot cycles 9 minutes in CONT mode have been completed after exiting visible moisture If entering SAT below 40 _C turn boots off before completion of 3 cycles Whe...

Страница 564: ...OTE Except for the first 6 minutes after liftoff make sure to have a speed not less than the published minimum speed with engine Anti ice ON speeds with applicable ice increment before selecting engin...

Страница 565: ...onditions are experienced or expected NOTE If unacceptable propeller vibrations occur in the temperature range 10 C to 12 C SAT due to propeller ice use MAX mode If unacceptable vibrations occur at wa...

Страница 566: ...becomes warmer then 5 C Propeller de ice selected in too warm temperature when in icing conditions may cause per formance degradation up to 30 CAUTION The propeller de ice system can be selected OFF w...

Страница 567: ...d overheat generating smoke in the cockpit If smoke is generated place the rotary switch in OFF position When the tem perature then goes down the smoke will cease NOTE 2 8 PROBE HEAT Probe heat for th...

Страница 568: ...d or ice accumulation on the wing upper surface aft of protected surface NOTE 2 11 VISUAL CUE OF ICE ACCUMU LATION Visual cue of ice accumulation The windshield wiper arms give a visual cue of ice acc...

Страница 569: ...light in the button will then go out After a Touch and Go landing with Engine Anti ice selected ON the light will first go out and after 6 minutes illuminate again when the system be comes active Dea...

Страница 570: ...ration below 50 KIAS will cause a reversion in airflow through the birdcatcher AVOID USE OF REVERSE POWER BELOW 50 KIAS IF OPERATIONALLY FEASIBLE NOTE After encountering icing conditions with a faulty...

Страница 571: ...not applicable 12 1 1 Description 12 1 2 Operation Clocks 12 2 0 Highlights not applicable 12 2 1 Description 12 2 2 Operation not applicable Flight Recorder System 12 3 0 Highlights not applicable 12...

Страница 572: ...INSTRUMENTS AND RECORDERS Aircraft Operations Manual 12 CONTENTS PAGE 2 Apr 01 15 THIS PAGE INTENTIONALLY LEFT BLANK...

Страница 573: ...icing Also see AOM 11 1 ICE AND RAIN PROTECTION Should the heater fail the OAT caution light on the over head panel will come on The OAT probe is located on the upper part of the fwd fuselage 2 3 Air...

Страница 574: ...INSTRUMENTS AND RECORDERS AIR DATA SYSTEM Description Aircraft Operations Manual 12 1 1 PAGE 2 Apr 01 15 C0714 Fig 1 Pitot static systems schematic...

Страница 575: ...INSTRUMENTS AND RECORDERS AIR DATA SYSTEM Description Aircraft Operations Manual 12 1 1 PAGE 3 Apr 01 15 A25727 EFIS MFD if installed Fig 2 ADC inputs outputs...

Страница 576: ...INSTRUMENTS AND RECORDERS AIR DATA SYSTEM Description Aircraft Operations Manual 12 1 1 PAGE 4 Apr 01 15 THIS PAGE INTENTIONALLY LEFT BLANK...

Страница 577: ...he ADC The pneumatic indicator converts change in static pressure into a proportion al vertical speed Vertical navigation indicator Optional This instrument has two functions To serve as an indicator...

Страница 578: ...INSTRUMENTS AND RECORDERS AIR DATA SYSTEM Description Aircraft Operations Manual 12 1 1 PAGE 6 Apr 01 15 THIS PAGE INTENTIONALLY LEFT BLANK...

Страница 579: ...DBY IAS INDICATOR A B Altitude indication Shows aircraft altitude with a smallest scale increment of 20 ft by a digital and an analogue scale Baroset indication Displays set barometric pressure in mil...

Страница 580: ...ning flag red Flag is indicated if The test button is pressed The IAS indicator fails Loss of airspeed data from the ADC VMO pointer IAS pointer TEST button When pressed and held Warning flag comes in...

Страница 581: ...DBY IAS INDICATOR A B Altitude indication Shows aircraft altitude with a smallest scale increment of 20 ft by a digital and an analogue scale Baroset indication Displays set barometric pressure in mil...

Страница 582: ...eed data from the ADC VMO pointer IAS pointer IAS bug knob When IAS mode FD AP is selected then IAS bug will capture the actual IAS Turn the IAS bug knob to change IAS and the FD AP will follow Also s...

Страница 583: ...ND RECORDERS AIR DATA SYSTEM Description Aircraft Operations Manual 12 1 1 PAGE 9 Apr 01 15 C0720 VMO pointer IAS pointer Airspeed reference bug A A RIGHT IAS INDICATOR Fig 5 Right Indicated Airspeed...

Страница 584: ...ta from the ADC Altitude indication Shows aircraft altitude by a digital and an analogue scale with a smallest scale increment of 20 ft Baroset indication Displays set barometric pressure in inch es m...

Страница 585: ...ndication Shows aircraft altitude by a digital and an analogue scale with a smallest scale increment of 20 ft Baroset indication Displays set barometric pressure in milli bars MB and in inches mercury...

Страница 586: ...ATOR A Warning flag red Flag is indicated if The test button is pressed The vertical speed indicator fails Loss of vertical speed data from the ADC Vertical speed pointer Vertical speed scale Scaled i...

Страница 587: ...ARM to black SETUP and DISTANCE annunciators sequentially show SETUP display indicates 888 8 8 DISTANCE display indicates 18 8 VSR display indicates 8 8 Back to normal A26576 A VERTICAL NAVIGATION IND...

Страница 588: ...INSTRUMENTS AND RECORDERS AIR DATA SYSTEM Description Aircraft Operations Manual 12 1 1 O PAGE 14 Apr 01 15 THIS PAGE INTENTIONALLY LEFT BLANK...

Страница 589: ...DATA SYSTEM Description Aircraft Operations Manual 12 1 1 S PAGE 15 Apr 01 15 A26670 A VS A RIGHT VERTICAL SPEED INDICATOR Vertical speed scale Scaled in fpm x 1000 Vertical speed pointer Fig 10 Righ...

Страница 590: ...INSTRUMENTS AND RECORDERS AIR DATA SYSTEM Description Aircraft Operations Manual 12 1 1 S PAGE 16 Apr 01 15 THIS PAGE INTENTIONALLY LEFT BLANK...

Страница 591: ...on Green diamond shaped pointer indi cates the difference between the speed selected with the IAS bug on the IAS indicator and the actual IAS 1 dot 5 knots Fast or Slow index 10 knots faster or slower...

Страница 592: ...INSTRUMENTS AND RECORDERS AIR DATA SYSTEM Description Aircraft Operations Manual 12 1 1 O PAGE 18 Apr 01 15 THIS PAGE INTENTIONALLY LEFT BLANK...

Страница 593: ...7 C TAS indication True airspeed in knots If ADC speed information fails readout turns to red dashes flashes for 10 s then steady SAT indication Static air temperature in degrees centigrade If ADC tem...

Страница 594: ...ENG OVSP A B L R A TEST 2 PANEL A STATIC PRESS VALVE LIFT TO CLOSE B STATIC PRESSURE SHUTOFF VALVE B B AIR DATA Computer test switch for maintenance only When pressed and held on ground The left IAS...

Страница 595: ...knob Turning the knob will change altitude in 100 feet increments ALT ALERT buttonlight amber Illuminates steady when approaching and flashes when deviating from selected alti tude If an alert has bee...

Страница 596: ...ed altitude Altitude alert light illuminates steady No alert light Altitude alert light flashing Aural alert c chord tone Deviation altitude 300 ft deviation altitude alert with Collins PRE 80D P N 01...

Страница 597: ...al 12 1 1 PAGE 23 Apr 01 15 4 ELECTRICAL POWER SUPPLY ADC IAS indicator L AVIONIC START BUS F 15 ADC L ASI ADC altimeter L AVIONIC START BUS F 14 ADC L ALTIM VSI VNI preselect L AVIONIC START BUS F 13...

Страница 598: ...INSTRUMENTS AND RECORDERS AIR DATA SYSTEM Description Aircraft Operations Manual 12 1 1 PAGE 24 Apr 01 15 THIS PAGE INTENTIONALLY LEFT BLANK...

Страница 599: ...LERANCES Deviation from true altitude at ground check and difference between two indicators according to national regulations 1 2 AIRSPEED INDICATOR OPERATIONAL TOLERANCES Difference between two indic...

Страница 600: ...INSTRUMENTS AND RECORDERS AIR DATA SYSTEM Operation Aircraft Operations Manual 12 1 2 PAGE 2 Jun30 15...

Страница 601: ...check that no flag is visible and indication at zero Check difference between left right and standby IAS indicator 3 Vertical speed indicators CHECK On left indicator check that no flag is visible and...

Страница 602: ...ure 3 2 LEFT INSTRU MENTS ERRATIC INDICATIONS Erratic or stuck indication on any of the left instruments Airspeed Altimeter Vertical speed or VNAV if installed ACTIONS Only the Altimeter affected 1 CB...

Страница 603: ...altimeter and or standby altimeter End of procedure 3 4 RIGHT INSTRU MENTS ERRATIC INDICATIONS Erratic or stuck indication on any of the right instruments Airspeed Altimeter Vertical speed ACTIONS 1 C...

Страница 604: ...or altimeter indicators L and R side L and standby R and standby ACTIONS Not valid for leakage in the standby system NOTE If erratic indication on one side On the erratic indication side 1 Static shut...

Страница 605: ...ional chronometer is provided on the right instrument panel From A C 300 and up the chronometer is electrical powered from either RH HOT BAT BUS or if HOT BAT not available by its own internal battery...

Страница 606: ...NDICATORS A11195 12 1 2 3 4 5 6 7 8 9 10 11 A CHRONOMETER A A if installed Chronometer button Momentarily press button to Start Stop Reset Minute hand Elapsed time minutes Elapsed time seconds Spring...

Страница 607: ...INSTRUMENTS AND RECORDERS CLOCKS Description Aircraft Operations Manual 12 2 1 PAGE 3 Apr 01 15 4 ELECTRICAL POWER SUPPLY Chronometer R HOT BAT BUS M 17 CLOCK Both chronometers if option installed...

Страница 608: ...INSTRUMENTS AND RECORDERS CLOCKS Description Aircraft Operations Manual 12 2 1 PAGE 4 Apr 01 15 THIS PAGE INTENTIONALLY LEFT BLANK...

Страница 609: ...r example transcribed into more conveniently readable form altitude in feet etc 2 2 Digital Flight Data Recorder DFDR This is a recorder with a crashproof tape magazine installed in the rear compartme...

Страница 610: ...T RECORDER PANEL FDAU light amber Comes on when the FDAU internal monitoring detects a failure EVENT button Press to mark events on the tape DFDR light amber Light goes out after first engine is start...

Страница 611: ...e form altitude in feet etc 2 2 Digital Flight Data Recorder DFDR This is a recorder with a crashproof tape magazine installed in the rear compartment The recorder uses magnetic tape and is of the con...

Страница 612: ...Comes on when the FDAU internal monitoring detects a failure Thumb wheel switches Used to set operator flight trip number data EVENT button Press to mark events on the tape DFDR light amber Light goes...

Страница 613: ...orm altitude in feet etc 2 2 Digital Flight Data Recorder DFDR This is a recorder with a crashproof tape magazine installed in the rear compartment The recorder uses magnetic tape and is of the contin...

Страница 614: ...st engine is started and one generator on line indicating Flight Recorder is valid Also comes on when the DFDR internal moni toring detects a failure FDAU light amber Comes on when the FDAU internal m...

Страница 615: ...upon as an endless band holding information from the last 25 flight hours To prevent unintentional blanking of recorded data during ground stops or at maintenance a relay controlled by either engine o...

Страница 616: ...es out after first engine is started and one generator on line indicating Flight Recorder is valid Also comes on when the DFDR internal monitoring detects a failure EVENT button Press to mark events o...

Страница 617: ...hout Mod No 2245 and or without Mod No 2948 Flight recorder L INV BUS 115 VAC F 19 RECORD FLIGHT FDAU R AVIONIC BUS M 19 FLIGHT DATA AQUIS Applicable for A C 160 249 with Mod No 2245 and or with Mod N...

Страница 618: ...INSTRUMENTS AND RECORDERS FLIGHT RECORDER SYSTEM Description Aircraft Operations Manual 12 3 1 PAGE 4 Apr 01 15 THIS PAGE INTENTIONALLY LEFT BLANK...

Страница 619: ...controlled by engine oil pressure after engine start Applicable for A C 160 249 with Mod No 2245 and or with Mod No 2948 and for A C 250 UP 1 L AVION and MAIN INV switches ON Power is applied to the...

Страница 620: ...LIGHT CHECK RESET 2 End of procedure Applicable for A C 160 249 with Mod No 2245 and or with Mod No 2948 and for A C 250 UP 1 CB M 19 RECORD FLIGHT CHECK RESET 2 End of procedure 3 2 FDAU LIGHT ON ACT...

Страница 621: ...lay controlled by engine oil pressure after engine start Applicable to A C 160 249 with Mod No 2245 and or with Mod No 2948 and for A C 250 UP 1 L AVION and MAIN INV switches ON Power is applied to th...

Страница 622: ...on Aircraft Operations Manual 12 3 2 O PAGE 2 Apr 01 15 CONDITIONS NORMAL PROCEDURES 2 3 EVENT 1 EVENT button PRESS A mark will be made on the tape The mark will make it easier to find such periods of...

Страница 623: ...FLIGHT CHECK RESET 2 End of procedure Applicable to A C 160 249 with Mod No 2245 and or with Mod No 2948 and for A C 250 UP 1 CB M 19 RECORD FLIGHT CHECK RESET 2 End of procedure 3 2 FDAU LIGHT ON ACT...

Страница 624: ...INSTRUMENTS AND RECORDERS FLIGHT RECORDER SYSTEM Operation Aircraft Operations Manual 12 3 2 O PAGE 4 Apr 01 15 THIS PAGE INTENTIONALLY LEFT BLANK...

Страница 625: ...cation directly from the Remote Electronic Unit REU on three separate channels for pilot copilot and PA Cabin Interphone The fourth channel records sounds picked up with the cockpit area microphone in...

Страница 626: ...L PANEL TEST ERASE HEADSET Monitor meter Cockpit area microphone TEST button When pressed an internal test starts pro ducing A 600 Hz audio tone to headset output A green band indication on the monito...

Страница 627: ...GE 3 Jun 01 19 A C 160 399 4 ELECTRICAL POWER SUPPLY Applicable for A C 160 249 without Mod No 2245 and or without Mod No 2948 Voice recorder L BAT BUS F 18 RECORD VOICE Applicable for A C 160 249 wit...

Страница 628: ...INSTRUMENTS AND RECORDERS COCKPIT VOICE RECORDER Description Aircraft Operations Manual 12 4 1 S1 PAGE 4 Jun 01 19 A C 160 399 THIS PAGE INTENTIONALLY LEFT BLANK...

Страница 629: ...ation directly from the Remote Electronic Unit REU on three separate channels for pilot copilot and PA Cabin Interphone The fourth channel records sounds picked up with the cockpit area microphone in...

Страница 630: ...EST button pressed an internal test starts producing The green TEST light comes on extin guishes when TEST button is released A 600 Hz audio tone to headset output ERASE button When pressed at least 2...

Страница 631: ...INSTRUMENTS AND RECORDERS COCKPIT VOICE RECORDER Description Aircraft Operations Manual 12 4 1 S2 PAGE 3 Jun 01 19 A C 400 up 4 ELECTRICAL POWER SUPPLY Voice recorder L BAT BUS E 15 RECORD VOICE...

Страница 632: ...INSTRUMENTS AND RECORDERS COCKPIT VOICE RECORDER Description Aircraft Operations Manual 12 4 1 S2 PAGE 4 Jun 01 19 A C 400 up THIS PAGE INTENTIONALLY LEFT BLANK...

Страница 633: ...e to operate until a force of more than 2G opens the contacts of the inertia switch or the ESS AVION switch is set to OFF The SSCVR records audio from four communica tion channels the PA system the pi...

Страница 634: ...st 2 seconds with air craft on ground and with gust lock set all data in the solid state flash memories will be erased Headset output Used to monitor present recordings TEST button and TEST light When...

Страница 635: ...o A C with Solid State with 30 minutes recording time 4 ELECTRICAL POWER SUPPLY Applicable for A C 160 249 without Mod No 2245 and or without Mod No 2948 Voice recorder L BAT BUS F 18 RECORD VOICE App...

Страница 636: ...NTS AND RECORDERS COCKPIT VOICE RECORDER Description Aircraft Operations Manual 12 4 1 S3 PAGE 4 Jun 01 19 Applicable to A C with Solid State with 30 minutes recording time THIS PAGE INTENTIONALLY LEF...

Страница 637: ...ch of the four audio inputs in the solid state flash memo ry High quality audio for these four channels are recorded for a period of 30 minutes After this the oldest parts of the data is automatically...

Страница 638: ...2 seconds with air craft on ground and with gust lock set all data in the solid state flash memories will be erased Headset output Used to monitor present recordings TEST button and TEST light When T...

Страница 639: ...e to A C with Solid State with 2 hours recording time 4 ELECTRICAL POWER SUPPLY Applicable to A C 160 249 without Mod No 2245 and or without Mod No 2948 Voice recorder L BAT BUS F 18 RECORD VOICE Appl...

Страница 640: ...MENTS AND RECORDERS COCKPIT VOICE RECORDER Description Aircraft Operations Manual 12 4 1 S4 PAGE 4 Jun 01 19 Applicable to A C with Solid State with 2 hours recording time THIS PAGE INTENTIONALLY LEFT...

Страница 641: ...E button PRESS Press for at least 2 seconds 2 4 SAVING THE RECORDINGS The voice recorder holds only the recording of the last 30 minutes and if these records are to be preserved pull CB RECORD VOICE F...

Страница 642: ...OPERATION CONDITIONS ABNORMAL PROCEDURES 3 1 FAILURE AT TEST ACTION Applicable to A C 160 249 without Mod No 2245 and or without Mod No 2948 1 CB F 18 RECORD VOICE CHECK RESET 2 End of procedure Appl...

Страница 643: ...hall go out 2 3 ERASING Total erasing is possible only on ground and with gust lock set as follows 1 ERASE button PRESS Press for at least 2 seconds 2 4 SAVING THE RECORDINGS The voice recorder holds...

Страница 644: ...CKPIT VOICE RECORDER Operation Aircraft Operations Manual 12 4 2 S2 PAGE 2 Apr 01 15 A C 400 up 3 ABNORMAL OPERATION CONDITIONS ABNORMAL PROCEDURES 3 1 FAILURE AT TEST ACTION 1 CB E 15 RECORD VOICE CH...

Страница 645: ...lock set as follows 1 ERASE button PRESS Press for at least 2 seconds 2 4 SAVING THE RECORDINGS The voice recorder holds only the recording of the last 30 minutes and if these records are to be prese...

Страница 646: ...s recording time 3 ABNORMAL OPERATION CONDITIONS ABNORMAL PROCEDURES 3 1 FAILURE AT TEST ACTION Applicable to A C 160 249 without Mod No 2245 and or without Mod No 2948 1 CB F 18 RECORD VOICE CHECK RE...

Страница 647: ...d and with gust lock set as follows 1 ERASE button PRESS Press for at least 2 seconds 2 4 SAVING THE RECORDINGS The voice recorder holds only the recording of the last 2 hours and if these records are...

Страница 648: ...recording time 3 ABNORMAL OPERATION CONDITIONS ABNORMAL PROCEDURES 3 1 FAILURE AT TEST ACTION Applicable to A C 160 249 without Mod No 2245 and or without Mod No 2948 1 CB F 18 RECORD VOICE CHECK RESE...

Страница 649: ...LANDING GEAR Aircraft Operations Manual 13 CONTENTS PAGE 1 Apr 01 15 CONTENTS Landing Gear 13 0 Highlights not applicable 13 1 Description 13 2 Operation...

Страница 650: ...LANDING GEAR Aircraft Operations Manual 13 CONTENTS PAGE 2 Apr 01 15 THIS PAGE INTENTIONALLY LEFT BLANK...

Страница 651: ...etraction With gear UP selected an electrically operated con trol valve ports hydraulic pressure to release the downlocks and pressurize the hydraulic actuators A mechanical lock on the landing gear c...

Страница 652: ...s Fig 1 The main landing gear wheels are fitted with self adjusting hydraulic disc brakes There are two brake circuits one for the outboard and one for the inboard brakes Each circuit has its own accu...

Страница 653: ...i the valve will auto matically open and relieve remaining pressure to the return line The handle remains in the pulled up position The brake handle can be locked in the pulled position by turning the...

Страница 654: ...ht Idle Stop ATC 1 Transponder Flight Data Recorder TCAS ACAS RIGHT OUTBOARD SWITCH Anti Skid left and right outboard wheels Stall Warning inhibit on ground Cabin pressurization system Air Data System...

Страница 655: ...NFIG light and inter mittent horn are all activated if the gear is up radio altitude less than 500 ft and one power lever re tarded below minimum takeoff power 62 Power Lever Angle The horn may be sil...

Страница 656: ...tboard anti skid valve Left pilot Right pilot Brake pedals Outboard accumulator Inboard accumulator Pressure from electric or hand pump Pressure from electric or hand pump Return Parking brake handle...

Страница 657: ...r Uplock actuator Gnd Air To explosive separation bolts Emergency extension handle Solenoid UP DOWN Landing gear handle Ground mode Flight mode 28 VDC Gear selector Down signal Up signal Main accumula...

Страница 658: ...44 Control valve Steering wheel Solenoid steering brake M L WoW R WoW Air Gnd NLG down and locked Shutoff valve Actuator Return P Main accumulator Hydraulic handpump Solenoid 28 VDC Ground handling Lo...

Страница 659: ...nded position The handle knob contains an integral amber dis agreement light that comes on whenever the position of all gears does not agree with handle position TEST button When pressed With the gear...

Страница 660: ...te the flaps the flap handle must be set to desired flap setting before using the hand pump To extend the landing gear the gear handle must be in down position OUTBD BK ACC The outboard brake accumula...

Страница 661: ...cen tral warning panel illuminated PARKING BRAKE handle To engage parking brake pull the parking brake handle and turn approximately 30 clockwise to lock Apply brake pressure with the brake pedals Che...

Страница 662: ...hen left or right brake pedal is depressed the respective main gear brake is activated The brake pedals are also used in conjunction with the parking brake handle to set parking brakes PARK BRK ON lig...

Страница 663: ...gage and allow pressure to the hydraulic steering ac tuator CONFIG light red Will come on together with the intermittent horn when the aircraft is not in landing configuration Gear not down below 500...

Страница 664: ...n right R BAT BUS L 9 R LDG EMER RELEAS Anti skid inboard L MAIN BUS F 6 A SKID INBD Anti skid outboard R MAIN BUS M 4 A SKID OUTBD Anti skid touch down protection inboard L MAIN BUS J 19 ENG AUTO IGN...

Страница 665: ...r retraction time s 7 9 Nose wheel steering angle Using steering wheel deg 60 Backing with reverse thrust deg 45 The nose steering wheel must be kept depressed during backing with reverse thrust Numbe...

Страница 666: ...ing gear handle UP DETENT 5 Landing gear lights CHECK OFF When gear handle is set to UP detent transit light will come on and green downlock lights go off Check transit light to go off indicating that...

Страница 667: ...nly differential power sufficient to maintain speed in turns is permissible CAUTION Backing Slow backing of the aircraft is permissible start backing by depressing the nose steering wheel and apply re...

Страница 668: ...Turn the braking brake handle approximately 30 counter clockwise and push down Check PARK BRK ON CWP light to be off 5 Brakes CHECK Brake smoothly during initial taxiing to verify brake operation Use...

Страница 669: ...not pump brake pedals For MAXIMUM braking depress brake pedals fully and hold steady until reaching 20 kt Below 20 kt modulate brake pressure to avoid locking wheels Parking 8 Parking brakes SET Set p...

Страница 670: ...LANDING GEAR Operation Aircraft Operations Manual 13 2 PAGE 6 Apr 01 15 3 ABNORMAL OPERATION For Abnormal Operation see section 23 ABNORMAL PROCEDURES...

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Saab 340B, Руководство по эксплуатации

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