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SECTION 2

LIMITATIONS

SOCATA
MODEL TB 20

The content of this document is the property of

socata

. It is supplied in

confidence and commercial security of its contents must be maintained.

It must not be used for any purpose other than that for which it is supplied, nor

may information contained in it be disclosed to unauthorized persons. It must not

be reproduced nor transmitted in any form in whole or in part without permission

in writing from the owners of the Copyright.

Information in this document is subject to change without notice.

socata

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Contents

June 30, 1988

Revision 6

2.7

POWER PLANT INSTRUMENT MARKINGS

Power plant instrument markings and their color code significance are shown
in Figure 2.3.

INSTRUMENT

Red

Line or arc

---------

Minimum

Limit

Yellow Arc

------------

Caution

Range

Green Arc

-----------

Normal

Operating

Red Line

--------

Maximum

Limit

Tachometer

–––

750 to

2575 RPM

Oil Temperature

–––

below 104

(40

104 to 244

(40 to 118

244

(118

Fuel Pressure

Fuel flow

0.1 psi

2 Gal / hr

–––

0.1 to 8 psi

2 to 25 Gal / hr

8 psi

25 Gal / hr

Oil Pressure

(1)

25 psi

25 to 60 psi

and

90 to 100 psi

60 to 90 psi

100 psi

Oil Pressure

(2)

25 psi

25 to 55 psi

and

95 to 115 psi

55 to 95 psi

115 psi

Cylinder Head

Temperature

(3)

–––

435 to 500

(224 to 260

(4)

200 to 435

(93 to 224

(4)

500

(260

(1) Alternative No. 1

(2) Alternative No. 2

(3) If installed on airplane

(4) Optional marking (according to instrument model)

Figure 2.3 – POWER PLANT INSTRUMENT MARKINGS

Содержание TB20GT

Страница 1: ...nd commercial security of its contents must be maintained It must not be used for any purpose other than that for which it is supplied nor may information contained in it be disclosed to unauthorized...

Страница 2: ...thorized persons It must not be reproduced nor transmitted in any form in whole or in part without permission in writing from the owners of the Copyright Information in this document is subject to cha...

Страница 3: ...994 to 1996 1997 2000 socata All rights reserved Back to Contents June 30 1988 Revision 8 1 1 SECTION 1 GENERAL TABLE OF CONTENTS Page THREE VIEW DRAWING 1 2 GENERAL 1 3 DESCRIPTIVE DATA 1 3 ENGINE 1...

Страница 4: ...it is supplied nor may information contained in it be disclosed to unauthorized persons It must not be reproduced nor transmitted in any form in whole or in part without permission in writing from the...

Страница 5: ...t is supplied nor may information contained in it be disclosed to unauthorized persons It must not be reproduced nor transmitted in any form in whole or in part without permission in writing from the...

Страница 6: ...r which it is supplied nor may information contained in it be disclosed to unauthorized persons It must not be reproduced nor transmitted in any form in whole or in part without permission in writing...

Страница 7: ...Part 23 to be furnished to the pilot for operation of SOCATA Model TB 20 airplane It also contains supplemental data supplied by SOCATA This section provides basic data and information of general int...

Страница 8: ...8 U S Gallons 336 Litres Total capacity each tank 44 4 U S Gallons 168 Litres Total usable 86 2 U S Gallons 326 Litres NOTE Isopropyl alcohol or ethylene glycol monomethyl ether may be added to the f...

Страница 9: ...tandard Empty Weight 1764 lbs 800 kg 1814 lbs 823 kg Maximum Useful Load 1323 lbs 600 kg 1272 lbs 577 kg CABIN AND ENTRY DIMENSIONS Pre MOD 151 Post MOD 151 Maximum Cabin Width 4 20 ft 1 28 m 4 20 ft...

Страница 10: ...Miles per Hour Calibrated Airspeed KIAS Knots Indicated Airspeed is the speed shown on the airspeed indicator and expressed in knots MPH IAS Miles per Hour Indicated Airspeed KTAS Knots True Airspeed...

Страница 11: ...r each 1000 ft of altitude OAT Outside Air Temperature is the free air static temperature It is expressed in either degrees Celsius or degrees Fahrenheit QNH Setting at the pressure corresponding to t...

Страница 12: ...LANCE TERMINOLOGY Reference Datum Is an imaginary vertical plane from which all horizontal distances are measured for balance purpose Arm Is the horizontal distance from the reference datum to the cen...

Страница 13: ...tents June 30 1988 Revision 8 1 9 Maximum Take off Weight Is the maximum weight approved for the start of the take off run Maximum Weight at Landing Is the maximum weight approved for landing touch do...

Страница 14: ...served Back to Contents June 30 1988 Revision 8 1 10 GENERAL ABBREVIATIONS Cont d qt Quart SM Statute Mile S N Serial Number sq ft Square foot Std Standard U S Gal U S Gallon V Volt RADIO ABBREVIATION...

Страница 15: ...without notice 1988 1991 1992 1994 to 1996 1997 2000 socata All rights reserved Back to Contents January 31 1988 1 11 CONVERSION FACTORS IMPERIAL AND U S UNITS TO METRIC UNITS METRIC UNITS TO IMPERIA...

Страница 16: ...956 28 23 957 28 26 958 28 29 959 28 32 960 28 35 961 28 38 962 28 41 963 28 44 964 28 47 965 28 50 966 28 53 967 28 56 968 28 58 969 28 61 970 28 64 971 28 67 972 28 70 973 28 73 974 28 76 975 28 79...

Страница 17: ...wners of the Copyright Information in this document is subject to change without notice 1988 1991 1992 1994 to 1996 1997 2000 socata All rights reserved Back to Contents June 30 1988 Revision 6 2 1 SE...

Страница 18: ...that for which it is supplied nor may information contained in it be disclosed to unauthorized persons It must not be reproduced nor transmitted in any form in whole or in part without permission in w...

Страница 19: ...is Basic general technical conditions FAR 23 Regulations amendments 1 to 16 Complementary general technical conditions Paragraph 23 1581 amendment 21 Special technical condition The landing gear being...

Страница 20: ...d Back to Contents January 31 1988 2 4 AIRSPEED LIMITATIONS Airspeed limitations and their operational significance are shown in Figure 2 1 SPEED KCAS KIAS REMARKS VNE Never Exceed Speed 189 187 Do no...

Страница 21: ...cata All rights reserved Back to Contents January 31 1988 2 5 AIRSPEED INDICATOR OR TRUE AIRSPEED INDICATOR MARKINGS Airspeed indicator or true airspeed indicator markings and their color code signifi...

Страница 22: ...d Back to Contents June 30 1988 Revision 8 2 6 POWER PLANT LIMITATIONS Number of engines 1 Engine Manufacturer AVCO LYCOMING Engine Model Number IO 540 C4 D5D or IO 540 C4 B5D Engine Operating Limits...

Страница 23: ...on 6 2 7 POWER PLANT INSTRUMENT MARKINGS Power plant instrument markings and their color code significance are shown in Figure 2 3 INSTRUMENT Red Line or arc Minimum Limit Yellow Arc Caution Range Gre...

Страница 24: ...65 kg refer to Section 6 for cargo loading CENTER OF GRAVITY LIMITS Center of gravity range with landing gear extended Forward 42 2 inches 1 071 m aft of datum at 3086 lbs 1400 kg 37 4 inches 0 949 m...

Страница 25: ...VFR operations and may be equipped for night VFR and day night IFR operations See Supplements Section of this Manual Flight into known icing conditions is prohibited FUEL LIMITATIONS 2 Tanks 44 4 U S...

Страница 26: ...n it be disclosed to unauthorized persons It must not be reproduced nor transmitted in any form in whole or in part without permission in writing from the owners of the Copyright Information in this d...

Страница 27: ...ARDS NOTE The placards described in the Section 9 Supplements replace or supplement those described in this paragraph 1 In full view of the pilot forward of overhead lights THIS AIRPLANE MUST BE OPERA...

Страница 28: ...ermission in writing from the owners of the Copyright Information in this document is subject to change without notice 1988 1991 1992 1994 to 1996 1997 2000 socata All rights reserved Back to Contents...

Страница 29: ...must not be reproduced nor transmitted in any form in whole or in part without permission in writing from the owners of the Copyright Information in this document is subject to change without notice...

Страница 30: ...in it be disclosed to unauthorized persons It must not be reproduced nor transmitted in any form in whole or in part without permission in writing from the owners of the Copyright Information in this...

Страница 31: ...ay information contained in it be disclosed to unauthorized persons It must not be reproduced nor transmitted in any form in whole or in part without permission in writing from the owners of the Copyr...

Страница 32: ...for which it is supplied nor may information contained in it be disclosed to unauthorized persons It must not be reproduced nor transmitted in any form in whole or in part without permission in writin...

Страница 33: ...ange without notice 1988 1991 1992 1994 to 1996 1997 2000 socata All rights reserved Back to Contents June 30 1988 Revision 2 3 1 SECTION 3 EMERGENCY PROCEDURES TABLE OF CONTENTS Page GENERAL 3 3 AIRS...

Страница 34: ...8 Revision 7 3 2 TABLE OF CONTENTS Continued Page ICING 3 10 LANDING GEAR MALFUNCTIONS 3 10 LANDING GEAR FAILS TO RETRACT 3 10 LANDING GEAR FAILS TO EXTEND ONE OR SEVERAL GREEN GEAR DOWNLIGHTS FAIL TO...

Страница 35: ...e encountered in operating the SOCATA Model TB 20 airplane If proper preflight inspections operating procedures and maintenance practices are used emergencies due to airplane or engine malfunction sho...

Страница 36: ...to Contents June 30 1988 Revision 7 3 4 Fuel pump OFF Landing gear lever AS REQUIRED Land STRAIGHT AHEAD Magneto selector OFF Main switch OFF WARNING LANDING STRAIGHT AHEAD IS USUALLY ADVISABLE ENGIN...

Страница 37: ...ts June 30 1988 Revision 2 3 5 LOW OIL PRESSURE Oil warning light ON Pressure indicator IN RED LOW SECTOR Throttle REDUCE AS FAR AS POSSIBLE Oil temperature CHECKED If oil temperature in red sector RE...

Страница 38: ...D LANDINGS NOTE It is recommended that the wheels be up if landing on an unprepared surface EMERGENCY LANDING WITHOUT ENGINE POWER Glide speed 92 KIAS Radio TRANSMIT MAYDAY on 121 5 MHz or on the appr...

Страница 39: ...97 2000 socata All rights reserved Back to Contents June 30 1988 Revision 5 3 7 DITCHING Radio TRANSMIT MAYDAY on 121 5 MHz or on the appropriate frequency giving location and intentions Landing gear...

Страница 40: ...1996 1997 2000 socata All rights reserved Back to Contents June 30 1988 Revision 8 3 8 If fire goes on Main switch OFF Magneto selector OFF Evacuate passengers and extinguish fire using all available...

Страница 41: ...RE is in CABIN Main switch OFF ALTr FLD switch breaker OFF All electrical switches except magnetos OFF Cabin air cooling demisting FIRE CUT OFF Fire extinguisher if installed ACTIVATE If FIRE APPEARS...

Страница 42: ...WN ICING CONDITIONS IS PROHIBITED Cabin temperature FULL HOT Pitot heating if installed ON Demisting OPEN Alternate Air FULLY PULLED Engine INCREASE POWER without exceeding red line and periodically c...

Страница 43: ...Continue flight with landing gear down up to destination or toward an appropriate alternate airfield Maximum airspeed 139 KIAS THE RED LIGHT REMAINS ON WITH OR WITHOUT GREEN LIGHT ON LDG GEAR circuit...

Страница 44: ...hat for which it is supplied nor may information contained in it be disclosed to unauthorized persons It must not be reproduced nor transmitted in any form in whole or in part without permission in wr...

Страница 45: ...ATE Main switch ON Landing gear lever DOWN LDG GEAR circuit breaker CHECK CLOSED Landing gear lights ILLUMINATE DURING TEST Flaps TAKE OFF Airspeed 97 KIAS The landing gear should extend and lock norm...

Страница 46: ...ce 1988 1991 1992 1994 to 1996 1997 2000 socata All rights reserved Back to Contents June 30 1988 Revision 8 3 12 LANDING WITH A LANDING GEAR NOT LOCKED Landing gear position CHECK POSITION WITH THE T...

Страница 47: ...s reserved Back to Contents June 30 1988 Revision 8 3 13 Main gear not locked NOTE In case only one main gear extends minimum airplane damage will result if a gear up landing is made Retract the landi...

Страница 48: ...in whole or in part without permission in writing from the owners of the Copyright Information in this document is subject to change without notice 1988 1991 1992 1994 to 1996 1997 2000 socata All ri...

Страница 49: ...ICAL EQUIPMENT FAILURE Check the circuit breakers panel If the circuit breaker is open close it once only If it opens again do not try to close the circuit breaker the equipment has failed ALTERNATOR...

Страница 50: ...wners of the Copyright Information in this document is subject to change without notice 1988 1991 1992 1994 to 1996 1997 2000 socata All rights reserved Back to Contents June 30 1988 Revision 8 3 16 E...

Страница 51: ...FAILURE DIAGRAM NOTE WHEN BUS 3 PULL OFF TYPE CIRCUIT BREAKER IS OPEN LANDING GEAR ELECTRICAL CONTROL BECOMES INOPERATIVE AND THE LANDING GEAR MUST BE EXTENDED USING EMERGENCY SYSTEM KEY CB Circuit br...

Страница 52: ...1994 to 1996 1997 2000 socata All rights reserved Back to Contents June 30 1988 Revision 8 3 18 Figure 3 2 BATTERY FAILURE DIAGRAM Voltmeter KEY PCB Pull off type circuit breaker SB Switch breaker LEA...

Страница 53: ...NOTE If closing of Bus 2 or Bus 3 PCB makes ALTr PCB or ALTr FLD SB open pull faulty Bus PCB and close ALTr FLD SB CONTINUE FLIGHT CAREFULLY BATTERY FAILURE SEE FIGURE 3 2 LEAVE IMC CONDITIONS IF POSS...

Страница 54: ...to Contents June 30 1988 Revision 8 3 20 AIRSPEED INDICATING SYSTEM FAILURE In case of erroneous indications in flight Pitot heating if installed ON Alternate static source if installed PULL For IAS...

Страница 55: ...bject to change without notice 1988 1991 1992 1994 to 1996 1997 2000 socata All rights reserved Back to Contents June 30 1988 Revision 8 3 21 INVOLUNTARY SPIN INTENTIONAL SPINS ARE PROHIBITED However...

Страница 56: ...ight Information in this document is subject to change without notice 1988 1991 1992 1994 to 1996 1997 2000 socata All rights reserved Back to Contents June 30 1988 Revision 2 3 22 OPTIMUM GLIDE WITHO...

Страница 57: ...without permission in writing from the owners of the Copyright Information in this document is subject to change without notice 1988 1991 1992 1994 to 1996 1997 2000 socata All rights reserved Back to...

Страница 58: ...closed to unauthorized persons It must not be reproduced nor transmitted in any form in whole or in part without permission in writing from the owners of the Copyright Information in this document is...

Страница 59: ...RAL This section provides procedures for the conduct of normal operation of the SOCATA Model TB 20 airplane The normal procedures for optional systems are given in Section Supplements of this Manual A...

Страница 60: ...tion contained in it be disclosed to unauthorized persons It must not be reproduced nor transmitted in any form in whole or in part without permission in writing from the owners of the Copyright Infor...

Страница 61: ...evision 8 4 5 PREFLIGHT INSPECTIONS See Figure 4 1 AIRFRAME 1 Cabin Pilot door OPEN Control lock REMOVED Magneto selector OFF Landing gear lever DOWN Mixture IDLE CUT OFF Main switch ON Flaps LANDING...

Страница 62: ...k CLOSED 5 L H main landing gear Chocks REMOVE Tire Check condition Shock absorber Normal position Door Check play and cleanliness Microswitches Clean Landing gear well No foreign body 6 Forward fusel...

Страница 63: ...erved Back to Contents June 30 1988 Revision 8 4 7 9 R H wing leading edge Fuel tank draining Fuel free from water and sediment Fuel tank drain Check CLOSED Fuel tank Check level Fuel tank cap SECURED...

Страница 64: ...el pump OFF Main switch ON Advisory panel Tested Landing gear indicator lights Tested Fuel gages Check Flaps RETRACT Instrument lights ON Navigation lights ON Anticollision lights if installed ON Stro...

Страница 65: ...robe light if installed Flashing Anticollision light if installed Flashing e Cabin Navigation lights OFF Strobe lights if installed OFF Anticollision lights if installed OFF Recognition lights if inst...

Страница 66: ...reserved Back to Contents June 30 1988 Revision 8 4 10 ENGINE STARTING Anticollision lights if installed ON COLD ENGINE Main switch ON Propeller FULL FORWARD Throttle 1 4 OPEN Mixture IDLE CUT OFF Fu...

Страница 67: ...R STARTING ENGINE ELECTRICAL POWER CHECK ALTr FLD switch breaker OFF ALTr warning light ON Voltmeter Yellow sector ALTr FLD switch breaker ON ALTr warning light OFF Voltmeter Green sector Turn and ban...

Страница 68: ...dder pedals only is generally sufficient The combined use of the rudder pedals and the brakes permits if necessary tight turns Check operation of gyroscopic instruments horizontal attitude heading and...

Страница 69: ...eats seat belts shoulder harnesses Check Doors LOCKED Controls Free Pitch trim TAKE OFF Rudder trim TAKE OFF Flaps TAKE OFF Magneto selector BOTH Alternate Air Pushed Propeller FULL FORWARD Mixture FU...

Страница 70: ...ntents June 30 1988 Revision 6 4 14 WHEN SAFELY AIRBORNE Brakes Apply Landing gear RETRACT AT 300 ft Flaps RETRACT AT 1000 ft Fuel pump OFF External lights As required Air conditioning switch if insta...

Страница 71: ...icing conditions as soon as possible Remember to push in the Alternate Air control after leaving the icing area and when you are sure there is no ice on the airframe DESCENT Power setting as required...

Страница 72: ...June 30 1988 Revision 8 4 16 When climb rate is positive Landing gear lever UP Flaps TAKE OFF Airspeed 90 KIAS Flaps RETRACTED Climb at 95 KIAS AFTER LANDING Fuel pump OFF Flaps RETRACTED Landing lig...

Страница 73: ...D switch breaker OFF Main switch OFF Fuel selector OFF Control lock Installed Chocks Tie downs Installed Depending on the kind of operation it is not necessary to perform this test more than once a da...

Страница 74: ...All rights reserved Back to Contents June 30 1988 Revision 5 4 18 FLIGHT WITH CROSSWIND TAKE OFF Apply full power before brake release Aileron control moved into wind Keep the airplane on runway cent...

Страница 75: ...reproduced nor transmitted in any form in whole or in part without permission in writing from the owners of the Copyright Information in this document is subject to change without notice 1988 1991 199...

Страница 76: ...n that for which it is supplied nor may information contained in it be disclosed to unauthorized persons It must not be reproduced nor transmitted in any form in whole or in part without permission in...

Страница 77: ...wners of the Copyright Information in this document is subject to change without notice 1988 1991 1992 1994 to 1996 1997 2000 socata All rights reserved Back to Contents June 30 1988 Revision 8 5 1 SE...

Страница 78: ...t Information in this document is subject to change without notice 1988 1991 1992 1994 to 1996 1997 2000 socata All rights reserved Back to Contents January 31 1988 5 2 ACOUSTIC LIMITATION In complian...

Страница 79: ...AIRSPEED CALIBRATION NOTE The indicated airspeeds IAS suppose instrument error to be null FLAPS RETRACTED L Gear UP FLAPS TAKE OFF L Gear UP OR DOWN FLAPS LANDING L Gear DOWN KIAS KCAS KIAS KCAS KIAS...

Страница 80: ...he Copyright Information in this document is subject to change without notice 1988 1991 1992 1994 to 1996 1997 2000 socata All rights reserved Back to Contents June 30 1988 Revision 7 5 4 ALTITUDE COM...

Страница 81: ...part without permission in writing from the owners of the Copyright Information in this document is subject to change without notice 1988 1991 1992 1994 to 1996 1997 2000 socata All rights reserved Ba...

Страница 82: ...n part without permission in writing from the owners of the Copyright Information in this document is subject to change without notice 1988 1991 1992 1994 to 1996 1997 2000 socata All rights reserved...

Страница 83: ...ure Performance values given do not take into account factors such as pilot technique or degraded airplane condition Take off and landing performance figures are based on a dry hard surface runway The...

Страница 84: ...to 1996 1997 2000 socata All rights reserved Back to Contents June 30 1988 Revision 7 5 8 TAKE OFF PERFORMANCE CONDITIONS IAS Lift off 63 KIAS 73 MPH IAS Clear 50 ft 69 KIAS 79 MPH IAS Weight 2370 lbs...

Страница 85: ...1996 1997 2000 socata All rights reserved Back to Contents June 30 1988 Revision 7 5 9 TAKE OFF PERFORMANCE CONDITIONS IAS Lift off 71 KIAS 82 MPH IAS Clear 50 ft 78 KIAS 90 MPH IAS Weight 3086 lbs 14...

Страница 86: ...document is subject to change without notice 1988 1991 1992 1994 to 1996 1997 2000 socata All rights reserved Back to Contents June 30 1988 Revision 7 5 10 CLIMB PERFORMANCE CONDITIONS Landing gear U...

Страница 87: ...this document is subject to change without notice 1988 1991 1992 1994 to 1996 1997 2000 socata All rights reserved Back to Contents June 30 1988 Revision 7 5 11 CLIMB PERFORMANCE CONDITIONS Landing ge...

Страница 88: ...o 1996 1997 2000 socata All rights reserved Back to Contents June 30 1988 Revision 7 5 12 CLIMB PERFORMANCE CONDITIONS Landing gear UP Weight 2370 lbs 1075 kg Indicated speed 86 KIAS 99 MPH IAS Mixtur...

Страница 89: ...996 1997 2000 socata All rights reserved Back to Contents June 30 1988 Revision 7 5 13 CLIMB PERFORMANCE CONDITIONS Landing gear UP Weight 3086 lbs 1400 kg Indicated speed 95 KIAS 109 MPH IAS Mixture...

Страница 90: ...ct to change without notice 1988 1991 1992 1994 to 1996 1997 2000 socata All rights reserved Back to Contents June 30 1988 Revision 8 5 14 MAXIMUM PERFORMANCE ALTITUDE Maximum performance altitude in...

Страница 91: ...s of the Copyright Information in this document is subject to change without notice 1988 1991 1992 1994 to 1996 1997 2000 socata All rights reserved Back to Contents June 30 1988 Revision 8 5 14A Post...

Страница 92: ...for which it is supplied nor may information contained in it be disclosed to unauthorized persons It must not be reproduced nor transmitted in any form in whole or in part without permission in writin...

Страница 93: ...served Back to Contents June 30 1988 Revision 8 5 15 LEVEL FLIGHT PERFORMANCE Level flight performance are given for a weight of 2943 lbs 1335 kg and for setting Best Power or Best Economy obtained wi...

Страница 94: ...Bold faced types represent recommended power N PA CAS TAS MIXTURE ADJUSTING SPECIFIC CONSUMPTION BHP RPM in Hg MPH kt MPH kt l h U S Gal hr l 100 NM U S Gal 100 NM 2500 23 6 61 3 16 2 40 6 10 7 2400...

Страница 95: ...E Bold faced types represent recommended power N PA CAS TAS MIXTURE ADJUSTING SPECIFIC CONSUMPTION BHP RPM in Hg MPH kt MPH kt l h U S Gal hr l 100 NM U S Gal 100 NM 2500 23 0 61 3 16 2 39 9 10 5 2400...

Страница 96: ...lbs 1335 kg NOTE Bold faced types represent recommended power N PA CAS TAS MIXTURE ADJUSTING SPECIFIC CONSUMPTION BHP RPM in Hg MPH kt MPH kt l h U S Gal hr l 100 NM U S Gal 100 NM 2500 22 5 61 3 16...

Страница 97: ...thout antennas nor external lights Weight 2943 lbs 1335 kg NOTE Bold faced types represent recommended power N PA CAS TAS MIXTURE ADJUSTING SPECIFIC CONSUMPTION BHP RPM in Hg MPH kt MPH kt l h U S Gal...

Страница 98: ...evision 6 5 20 LEVEL FLIGHT PERFORMANCE PRESSURE ALTITUDE 8500 ft ISA 28 4 F 2 C CONDITIONS Mixture adjusted to the BEST POWER Speed without antennas nor external lights Weight 2943 lbs 1335 kg NOTE B...

Страница 99: ...997 2000 socata All rights reserved Back to Contents June 30 1988 Revision 6 5 21 LEVEL FLIGHT PERFORMANCE PRESSURE ALTITUDE 10500 ft ISA 49 6 F 6 C CONDITIONS Mixture adjusted to the BEST POWER Speed...

Страница 100: ...o change without notice 1988 1991 1992 1994 to 1996 1997 2000 socata All rights reserved Back to Contents June 30 1988 Revision 6 5 22 LEVEL FLIGHT PERFORMANCE PRESSURE ALTITUDE 12500 ft ISA 14 F 10 C...

Страница 101: ...kg NOTE Bold faced types represent recommended power N PA CAS TAS MIXTURE ADJUSTING SPECIFIC CONSUMPTION BHP RPM in Hg MPH kt MPH kt l h U S Gal hr l 100 NM U S Gal 100 NM 2500 23 6 52 8 14 0 35 6 9 4...

Страница 102: ...g NOTE Bold faced types represent recommended power N PA CAS TAS MIXTURE ADJUSTING SPECIFIC CONSUMPTION BHP RPM in Hg MPH kt MPH kt l h U S Gal hr l 100 NM U S Gal 100 NM 2500 23 0 52 8 13 9 35 0 9 2...

Страница 103: ...2943 lbs 1335 kg NOTE Bold faced types represent recommended power N PA CAS TAS MIXTURE ADJUSTING SPECIFIC CONSUMPTION BHP RPM in Hg MPH kt MPH kt l h U S Gal hr l 100 NM U S Gal 100 NM 2500 22 5 52 8...

Страница 104: ...ithout antennas nor external lights Weight 2943 lbs 1335 kg NOTE Bold faced types represent recommended power N PA CAS TAS MIXTURE ADJUSTING SPECIFIC CONSUMPTION BHP RPM in Hg MPH kt MPH kt l h U S Ga...

Страница 105: ...vision 6 5 27 LEVEL FLIGHT PERFORMANCE PRESSURE ALTITUDE 8500 ft ISA 28 4 F 2 C CONDITIONS Mixture adjusted to the BEST ECONOMY Speed without antennas nor external lights Weight 2943 lbs 1335 kg NOTE...

Страница 106: ...97 2000 socata All rights reserved Back to Contents June 30 1988 Revision 6 5 28 LEVEL FLIGHT PERFORMANCE PRESSURE ALTITUDE 10500 ft ISA 49 6 F 6 C CONDITIONS Mixture adjusted to the BEST ECONOMY Spee...

Страница 107: ...2000 socata All rights reserved Back to Contents June 30 1988 Revision 6 5 29 LEVEL FLIGHT PERFORMANCE PRESSURE ALTITUDE 12500 ft ISA 14 F 10 C CONDITIONS Mixture adjusted to the BEST ECONOMY Speed w...

Страница 108: ...change without notice 1988 1991 1992 1994 to 1996 1997 2000 socata All rights reserved Back to Contents June 30 1988 Revision 7 5 30 LANDING PERFORMANCE WEIGHT 2370 lbs 1075kg CONDITIONS Clear 50 ft...

Страница 109: ...nge without notice 1988 1991 1992 1994 to 1996 1997 2000 socata All rights reserved Back to Contents September 30 1994 Revision 7 5 31 LANDING PERFORMANCE WEIGHT 3086 lbs 1400kg CONDITIONS Clear 50 ft...

Страница 110: ...for which it is supplied nor may information contained in it be disclosed to unauthorized persons It must not be reproduced nor transmitted in any form in whole or in part without permission in writin...

Страница 111: ...transmitted in any form in whole or in part without permission in writing from the owners of the Copyright Information in this document is subject to change without notice 1988 1991 1992 1994 to 1996...

Страница 112: ...this airplane is included at the back of this section It should be noted that the list of specific optional equipment installed on your airplane as delivered from the factory can be found in the recor...

Страница 113: ...em 6 of rear bench or Post MOD 151 of rear seats and remove arm rest kept in position with Velcro straps If you want to free the back from its support plate lift it up about 1 5 inch 3 cm at both ends...

Страница 114: ...ontained in it be disclosed to unauthorized persons It must not be reproduced nor transmitted in any form in whole or in part without permission in writing from the owners of the Copyright Information...

Страница 115: ...sidered is the one noted on the last weighing form The data concerning loading are given on following graphs Loading graph see Figure 6 4 Weight Moment envelope see Figure 6 5 To determine airplane lo...

Страница 116: ...draw the rear passengers straight line to get point B 1 related to rear seat loading Our sample loading 2 persons 340 lb 154 kg Superpose point B 1 and point B of graph 2 draw the fuel straight line t...

Страница 117: ...QUIPMENT AFFECTING WEIGHT AND BALANCE AIRPLANE MODEL SERIAL NUMBER PAGE NUMBER WEIGHT CHANGE RUNNING DATE ITEM No DESCRIPTION OF EQUIPEMENT OR MODIFICATION ADDED REMOVED BASIC EMPTYWEIGHT IN OUT OR MO...

Страница 118: ...rd empty weight 1764 37 06 65 37 Optional equipment 102 51 66 5 27 Basic empty weight 1866 70 64 A 1 Pilot without Opt 0800 170 45 38 7 71 Pilot with Opt 0800 47 44 Front passenger without Opt 0800 17...

Страница 119: ...n writing from the owners of the Copyright Information in this document is subject to change without notice 1988 1991 1992 1994 to 1996 1997 2000 socata All rights reserved Back to Contents June 30 19...

Страница 120: ...an that for which it is supplied nor may information contained in it be disclosed to unauthorized persons It must not be reproduced nor transmitted in any form in whole or in part without permission i...

Страница 121: ...authorized persons It must not be reproduced nor transmitted in any form in whole or in part without permission in writing from the owners of the Copyright Information in this document is subject to c...

Страница 122: ...ized persons It must not be reproduced nor transmitted in any form in whole or in part without permission in writing from the owners of the Copyright Information in this document is subject to change...

Страница 123: ...in your airplane file Columns showing weight in pounds and arm in inches provide the weight and center of gravity location for the equipment The equipment list provides the following information a Re...

Страница 124: ...of the Copyright Information in this document is subject to change without notice 1988 1991 1992 1994 to 1996 1997 2000 socata All rights reserved Back to Contents June 30 1988 Revision 5 7 1 SECTION...

Страница 125: ...t notice 1988 1991 1992 1994 to 1996 1997 2000 socata All rights reserved Back to Contents June 30 1988 Revision 8 7 2 TABLE OF CONTENTS Continued BAGGAGE COMPARTMENT 7 23 CARGO CONFIGURATION 7 23 SEA...

Страница 126: ...ata All rights reserved Back to Contents June 30 1988 Revision 8 7 3 TABLE OF CONTENTS Continued STANDARD ELECTRICAL SYSTEM 7 40 ALTERNATOR CONTROL UNIT 7 40 MAIN SWITCH 7 42 ALTERNATOR CONTROL 7 42 A...

Страница 127: ...ission in writing from the owners of the Copyright Information in this document is subject to change without notice 1988 1991 1992 1994 to 1996 1997 2000 socata All rights reserved Back to Contents Ju...

Страница 128: ...low wing single engine airplane equipped with retractable tricycle landing gear and is designed to be used in normal category The fuselage consists of an all metal aluminium alloy structure of semimo...

Страница 129: ...erodynamic chord 4 002 ft 1 220 m True chord 4 085 ft 1 245 m Wing area 128 091 sq ft 11 90 m2 Wing setting 3 Ailerons Unit area 4 897 sq ft 0 46 m2 Mean span 4 081 ft 1 244 m Recoil and slotted type...

Страница 130: ...g of aileron stabilator and rudder surfaces Each front seat is provided with a control wheel which actuates ailerons and stabilator through rods and bellcranks The control wheel being actuated fully a...

Страница 131: ...LE OF INSTRUMENT PANEL AND L H SUBPANEL HANDLE MAP READING LIGHT SWITCH If installed EMERGENCY LIGHTING CONTROL EMERGENCY GEAR CONTROL AND CIRCUIT BREAKERS PANEL LIGHTING VOR ILS INDICATOR If installe...

Страница 132: ...tion will trim nose up Stabilator tab deflection with stabilator in maximum nose up attitude must be nose up 0 0 5 nose down 15 1 5 Rudder trimming is accomplished by rotating a control knob rudder tr...

Страница 133: ...rights reserved Back to Contents June 30 1988 Revision 6 7 10 Figure 7 2 EXAMPLE OF CONSOLE AND PEDESTAL RADIONAVIGATION EQUIPMENT If installed WING FLAP INDICATOR WING FLAP CONTROL MIXTURE CONTROL E...

Страница 134: ...alternate static source valve and vacuum gage if installed complete the L H panel strip The central console see Figure 7 2 contains in the upper edge the engine monitoring cluster then radio navigati...

Страница 135: ...not be reproduced nor transmitted in any form in whole or in part without permission in writing from the owners of the Copyright Information in this document is subject to change without notice 1988...

Страница 136: ...whole or in part without permission in writing from the owners of the Copyright Information in this document is subject to change without notice 1988 1991 1992 1994 to 1996 1997 2000 socata All right...

Страница 137: ...the top edge of the L H instrument panel directly in front of the pilot The panel contains separate indicator lights which illuminate green amber or red when a specific condition occurs in the associ...

Страница 138: ...t permission in writing from the owners of the Copyright Information in this document is subject to change without notice 1988 1991 1992 1994 to 1996 1997 2000 socata All rights reserved Back to Conte...

Страница 139: ...he owners of the Copyright Information in this document is subject to change without notice 1988 1991 1992 1994 to 1996 1997 2000 socata All rights reserved Back to Contents June 30 1988 Revision 8 7...

Страница 140: ...ed in it be disclosed to unauthorized persons It must not be reproduced nor transmitted in any form in whole or in part without permission in writing from the owners of the Copyright Information in th...

Страница 141: ...m the owners of the Copyright Information in this document is subject to change without notice 1988 1991 1992 1994 to 1996 1997 2000 socata All rights reserved Back to Contents June 30 1988 Revision 8...

Страница 142: ...the owners of the Copyright Information in this document is subject to change without notice 1988 1991 1992 1994 to 1996 1997 2000 socata All rights reserved Back to Contents June 30 1988 Revision 8 7...

Страница 143: ...for which it is supplied nor may information contained in it be disclosed to unauthorized persons It must not be reproduced nor transmitted in any form in whole or in part without permission in writin...

Страница 144: ...to Contents January 31 1988 7 17 GROUND CONTROL Effective ground control while taxiing is accomplished through nose wheel steering by using the rudder pedals connected to nose wheel through rods When...

Страница 145: ...pplied nor may information contained in it be disclosed to unauthorized persons It must not be reproduced nor transmitted in any form in whole or in part without permission in writing from the owners...

Страница 146: ...ous flaps positions The wing flaps system is protected by a 10 amp circuit breaker labeled FLAPS located on L H circuit breakers side panel see Figure 7 6 LANDING GEAR The landing gear system is a ret...

Страница 147: ...LANDING GEAR CONTROL The landing gear lever is located on the R H side of the L H panel strip The lever has two positions up and down which give a mechanical indication of the gear position selected...

Страница 148: ...ny gear is not fully retracted or locked down the red gear unlocked light will illuminate The electric pump will continue to run during landing gear extension until the green indicator lights illumina...

Страница 149: ...ency landing gear control under the L H panel strip to extend the gear For this push on central knob before pulling the lever rearward For complete procedures refer to Section 3 Emergency procedures T...

Страница 150: ...ts June 30 1988 Revision 1 7 23 BAGGAGE COMPARTMENT The baggage compartment extends from the rear seat to the rear bulkhead of the cabin former n 6 The access is possible either through a lockable doo...

Страница 151: ...osed to unauthorized persons It must not be reproduced nor transmitted in any form in whole or in part without permission in writing from the owners of the Copyright Information in this document is su...

Страница 152: ...Use the lever located on the outboard side of the seat To change the seat back angle if installed Use the knurled knob located at the bottom part on the inboard side of the seat back To adjust the ba...

Страница 153: ...for which it is supplied nor may information contained in it be disclosed to unauthorized persons It must not be reproduced nor transmitted in any form in whole or in part without permission in writi...

Страница 154: ...seat belt shall not be twisted In any case and for all types of belts check that they are not impeded in their operation Further to a severe accident replace the belts which were installed when the a...

Страница 155: ...losed to unauthorized persons It must not be reproduced nor transmitted in any form in whole or in part without permission in writing from the owners of the Copyright Information in this document is s...

Страница 156: ...le to Closed position WARNING PRIOR TO EACH FLIGHT CHECK THAT BOTH CABIN ACCESS DOORS ARE NOT KEY LOCKED CHECK THAT BOTH LOCKING HOOKS ARE PROPERLY NOTCHED EXITS Pre MOD 151 In case of L H and R H doo...

Страница 157: ...upper cowl is fitted with an inspection door provided to check oil level it can also be fitted with an access door to the propeller deicing fluid tank The lower cowl is fitted with incorporated air i...

Страница 158: ...mum engine performance and T B O the pilot should apply the procedures recommended by Lycoming Operator s Manual concerning the engine ENGINE CONTROLS Engine manifold pressure is controlled by the thr...

Страница 159: ...RUMENTS Indicators enable the pilot to assure a permanent check of oil pressure oil temperature tachometer manifold pressure flowmeter and if installed EGT and CHT IGNITION STARTER SYSTEM Engine ignit...

Страница 160: ...ny form in whole or in part without permission in writing from the owners of the Copyright Information in this document is subject to change without notice 1988 1991 1992 1994 to 1996 1997 2000 socata...

Страница 161: ...t must not be reproduced nor transmitted in any form in whole or in part without permission in writing from the owners of the Copyright Information in this document is subject to change without notice...

Страница 162: ...Use dispersant oil in compliance with Specification MIL L 22851 only after the first 50 hours ENGINE LUBRICATION SYSTEM See Figures 7 12 and 7 12A The engine is lubricated by an oil system powered by...

Страница 163: ...termines propeller rotation speed and thus the engine speed to be maintained The governor controls flow of engine oil boosted to high pressure by the governing pump on a piston located in propeller hu...

Страница 164: ...Information in this document is subject to change without notice 1988 1991 1992 1994 to 1996 1997 2000 socata All rights reserved Back to Contents June 30 1988 Revision 3 7 35 Figure 7 13 FUEL SYSTEM...

Страница 165: ...n any form in whole or in part without permission in writing from the owners of the Copyright Information in this document is subject to change without notice 1988 1991 1992 1994 to 1996 1997 2000 soc...

Страница 166: ...ld a vent become blocked the fuel flow from the tank concerned is reduced and the engine may cut out The ventilation is ensured by ducts which run to the lower surface of each wing The quantity of fue...

Страница 167: ...e fuel sampler provided to drain fuel from the wing tank sump drain and the fuel strainers drains The fuel tank sump drains are located just outboard of each main landing gear well and the fuel strain...

Страница 168: ...thorized persons It must not be reproduced nor transmitted in any form in whole or in part without permission in writing from the owners of the Copyright Information in this document is subject to cha...

Страница 169: ...d persons It must not be reproduced nor transmitted in any form in whole or in part without permission in writing from the owners of the Copyright Information in this document is subject to change wit...

Страница 170: ...ight Information in this document is subject to change without notice 1988 1991 1992 1994 to 1996 1997 2000 socata All rights reserved Back to Contents June 30 1988 Revision 6 7 39B PARKING BRAKE Park...

Страница 171: ...alternator installed on the engine and in standard version a battery located in a compartment under the baggage compartment floor supply the system In optional version the battery is located in a com...

Страница 172: ...for which it is supplied nor may information contained in it be disclosed to unauthorized persons It must not be reproduced nor transmitted in any form in whole or in part without permission in writin...

Страница 173: ...ch it is supplied nor may information contained in it be disclosed to unauthorized persons It must not be reproduced nor transmitted in any form in whole or in part without permission in writing from...

Страница 174: ...ch it is supplied nor may information contained in it be disclosed to unauthorized persons It must not be reproduced nor transmitted in any form in whole or in part without permission in writing from...

Страница 175: ...the alternator through the regulator In the event of an alternator disconnection should the flight be continued only the necessary electrical equipment will be used The opening of BAT and ALTr FLD pul...

Страница 176: ...oltmeter is incorporated to the engine control instruments module located on the upper part of the console to monitor electric generation system efficiency With the alternator operating the indication...

Страница 177: ...be closed again pressed down Avionics equipment are protected by circuit breakers grouped in the lower part of the L H side circuit breakers panel In addition to protection of the alternator supply wi...

Страница 178: ...UND POWER RECEPTACLE if installed A ground power receptacle permits the use of an external power source for cold weather starting and during maintenance work on the airplane electrical system Details...

Страница 179: ...en the airplane is equipped with the tail cone strobe light A switch located on the circuit breaker panel see Figure 7 6 controls the strobe light illumination This circuit is protected by a circuit b...

Страница 180: ...n OFF turn clockwise for FULL INTENSITY OPERATION then still clockwise modulate towards MINIMUM INTENSITY turn back to OFF position turning counterclockwise Emergency control Pre MOD 151 modulates lig...

Страница 181: ...ut off by a fire cut off shutter and allows hot air distribution on both sides of the windshield Hot airflow is regulated from the control panel located on R H side of instrument panel strip AIR REGUL...

Страница 182: ...subject to change without notice 1988 1991 1992 1994 to 1996 1997 2000 socata All rights reserved Back to Contents June 30 1988 Revision 7 7 49 Figure 7 18 DEMISTING AIR REGULATION VENTILATION CUT OFF...

Страница 183: ...airflow may be regulated located on both parts of the instrument panel strip The upper control of cabin air selector allows adjustment of NACA opening NOTE To get air from the air outlets combine thei...

Страница 184: ...ed indicator the vertical speed indicator and the altimeter The system consists of a pitot which can be heated located on the lower surface of the L H wing two static ports located on L H and R H side...

Страница 185: ...persons It must not be reproduced nor transmitted in any form in whole or in part without permission in writing from the owners of the Copyright Information in this document is subject to change with...

Страница 186: ...rt without permission in writing from the owners of the Copyright Information in this document is subject to change without notice 1988 1991 1992 1994 to 1996 1997 2000 socata All rights reserved Back...

Страница 187: ...ERTICAL SPEED INDICATOR The vertical speed indicator depicts airplane rate of climb or descent in feet per minute The pointer is actuated by atmospheric pressure changes resulting from changes of alti...

Страница 188: ...zed persons It must not be reproduced nor transmitted in any form in whole or in part without permission in writing from the owners of the Copyright Information in this document is subject to change w...

Страница 189: ...uthorized persons It must not be reproduced nor transmitted in any form in whole or in part without permission in writing from the owners of the Copyright Information in this document is subject to ch...

Страница 190: ...for which it is supplied nor may information contained in it be disclosed to unauthorized persons It must not be reproduced nor transmitted in any form in whole or in part without permission in writin...

Страница 191: ...nter mark Pitch and roll attitudes are presented by a miniature airplane superimposed over a symbolic horizon area divided into two sections by a white horizon bar The upper sky blue area and the lowe...

Страница 192: ...knots above the stall in all configurations The stall warning system should be checked during the preflight inspection by momentarily turning on the battery switch and actuating the vane in the wing...

Страница 193: ...stalled The bank indicator located under the airspeed indicator or the true airspeed indicator may be replaced by a turn and bank indicator it is controlled by a switch breaker located in front of the...

Страница 194: ...ERGENCY LOCATOR TRANSMITTER if installed The airplane may be equipped with an emergency locator transmitter which enables to locate it in case of distress It is located in the baggage compartment The...

Страница 195: ...eset after an inadvertent activation ELT 90 EUROCAE ELT 91 TSO 1 Set ELT switch to MAN RESET or remote control switch to MAN a The ELT keeps on transmitting emergency signal b On remote control the XM...

Страница 196: ...thout permission in writing from the owners of the Copyright Information in this document is subject to change without notice 1988 1991 1992 1994 to 1996 1997 2000 socata All rights reserved Back to C...

Страница 197: ...unauthorized persons It must not be reproduced nor transmitted in any form in whole or in part without permission in writing from the owners of the Copyright Information in this document is subject t...

Страница 198: ...AL This section contains the procedures recommended by SOCATA for the proper ground handling and routine care and servicing of your SOCATA Model TB 20 airplane Also included in this section are the in...

Страница 199: ...it is supplied with a Pilot s Operating Handbook and supplemental data covering optional equipment installed in the airplane In addition the owner may purchase the following Maintenance Manual Illustr...

Страница 200: ...TION USING THE PROPELLER FOR GROUND HANDLING COULD RESULT IN SERIOUS DAMAGE ESPECIALLY IF PRESSURE OR PULL IS EXERTED ON BLADE TIPS The airplane should be moved on the ground with the aid of nose gear...

Страница 201: ...r which it is supplied nor may information contained in it be disclosed to unauthorized persons It must not be reproduced nor transmitted in any form in whole or in part without permission in writing...

Страница 202: ...paragraph TIE DOWN Proper tie down procedure is the best protection against damage to the parked airplane by gusty or strong winds To tie down the airplane securely proceed as follows Install control...

Страница 203: ...TAND WITHIN THE ARC OF THE PROPELLER BLADES WHILE TURNING THE PROPELLER After 30 days in storage the airplane should be flown for at least 30 minutes or a ground runup should be made just long enough...

Страница 204: ...rades 50 first hours MIL L 22851 Spec Dispersant Grades after 50 hours All temperatures SAE 15W50 or 20W50 Above 80 F 27 C SAE 60 SAE 60 Above 60 F 15 C SAE 50 SAE 40 or SAE 50 30 F 1 C to 90 F 32 C S...

Страница 205: ...nder unfavourable conditions Engine oil is changed with the filter Drain the engine oil sump and replace the filter at least every 4 months even though less than the recommended hours have accumulated...

Страница 206: ...ion Fuel Formerly 100 130 Green CAUTION NEVER FLY THE AIRPLANE WITH CONTAMINATED WATER SAND RUST DUST OR UNAPPROVED FUEL NOTE Isopropyl alcohol or ethylene glycol monomethyl ether may be added to the...

Страница 207: ...g under the combined effect of use of certain fuels with high humidity conditions on the ground followed by flight at high altitude and low temperature Under these unusual conditions small amounts of...

Страница 208: ...2 8 13 To ensure proper mixing the following is recommended For best results the alcohol should be added during the fueling operation by pouring the alcohol directly on the fuel stream issuing from t...

Страница 209: ...G OF THE EGME COMPOUND WITH THE FUEL IS EXTREMELY IMPORTANT A CONCENTRATION IN EXCESS OF THAT RECOMMENDED 0 15 BY VOLUME MAXIMUM WILL RESULT IN DETRIMENTAL EFFECTS TO THE FUEL TANKS DETERIORATION OF P...

Страница 210: ...r than that for which it is supplied nor may information contained in it be disclosed to unauthorized persons It must not be reproduced nor transmitted in any form in whole or in part without permissi...

Страница 211: ...ack to Contents June 30 1988 Revision 7 8 16 LANDING GEAR Nose gear tire 5 00 5 6 PRTT Inflating pressure 56 5 psi 3 9 bars Main gear tires 15 6 00 6 6 PRTT Inflating pressure 63 9 psi 4 4 bars Nose g...

Страница 212: ...aner sparingly with soft cloths and rub with moderate pressure until all dirt oil scum and bug stains are removed Allow the cleaner to dry then wipe it off with soft flannel cloths CAUTION NEVER USE G...

Страница 213: ...lly with an oily cloth to clean off grass and bug stains will assure long blade life Small nicks on the propeller particularly near the tips and on the leading edges should be dressed out as soon as p...

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