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PIPER AIRCRAFT CORPORATION

SECTION 1

PA-46-310P, MALIBU

GENERAL

TABLE OF CONTENTS

SECTION 1

GENERAL

Paragraph

Page

No.

1.1

Introduction ..............................................................................

1-1

1.3

Engine.......................................................................................

1-3

1.5

Propeller ...................................................................................

1-3

1.7

Fuel...........................................................................................

1-3

1.9

Oil.............................................................................................

1-4

1.11

Maximum Weights ...................................................................

1-4

1.13

Standard Airplane Weights.......................................................

1-4

1.15

Cabin and Entry Dimensions....................................................

1-5

1.17

Baggage Space and Entry Dimensions.....................................

1-5

1.19

Specific Loading.......................................................................

1-5

1.21

Symbols, Abbreviations and Terminology ...............................

1-7

ISSUED: JULY 1, 1986

REPORT: VB-1300

1-i

PIPER AIRCRAFT CORPORATION

SECTION 1

PA-46-310P, MALIBU

GENERAL

TABLE OF CONTENTS

SECTION 1

GENERAL

Paragraph

Page

No.

1.1

Introduction ..............................................................................

1-1

1.3

Engine.......................................................................................

1-3

1.5

Propeller ...................................................................................

1-3

1.7

Fuel...........................................................................................

1-3

1.9

Oil.............................................................................................

1-4

1.11

Maximum Weights ...................................................................

1-4

1.13

Standard Airplane Weights.......................................................

1-4

1.15

Cabin and Entry Dimensions....................................................

1-5

1.17

Baggage Space and Entry Dimensions.....................................

1-5

1.19

Specific Loading.......................................................................

1-5

1.21

Symbols, Abbreviations and Terminology ...............................

1-7

ISSUED: JULY 1, 1986

REPORT: VB-1300

1-i

FOR REFERENCE ONLY

NOT FOR FLIGHT

Содержание PA-46-310P

Страница 1: ...U P 08 40 S G K ED AL ___ THE ION VED ANE ...

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Страница 15: ...Relocated info from page 2 9 2 11 Relocated info from page 2 10 2 12 Added page relocated info from page 2 11 3 i Revised T of C 3 ii Revised T of C 3 5 Relocated info from page 3 6 3 6 Added TIT info relocated info to pages 3 5 3 6 3 7 Relocated info from page 3 6 3 21 Added TIT info relocated info to page 3 22 3 22 Relocated info from page 3 21 to page 3 23 3 23 Relocated info from page 3 22 4 i...

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Страница 19: ...N 1 AL 00 1 i ...

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Страница 21: ...N 1 AL tion be onal AA and ves d to t be the for ible ment its ting self ing ach ons mal s to ures tant ave gure nk 300 1 1 ...

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Страница 23: ...N 1 AL 1 ntal BE 310 600 38 0 5 25 4 00 520 5 1 ive sed ged cted 1 zell 2 2 1BF 78 80 eed ated 0LL ade n of etin des 300 1 3 ...

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Страница 25: ...N 1 AL 49 5 148 47 24 46 14 20 x 23 x 46 23 4 13 2 300 1 5 ...

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Страница 27: ...N 1 AL and e of ated tion eed ard ane air ator IAS ume eed ane CAS and eed ble the the s in 300 1 7 ...

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Страница 29: ...N 1 AL in 5 hes ea he is nd air om nd in an has 3 2 vel or ed nd ok ed eld les be nd 00 1 9 ...

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Страница 31: ...N 1 AL all or ge the nce an em by ce of ld the he he e s um ns ted een n ng ull 00 11 ...

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Страница 33: ...vity Limits 2 5 2 17 Maneuver Limits 2 5 2 19 Flight Load Factors 2 5 2 21 Kinds of Operation Equipment List 2 6 2 23 Fuel Limitations 2 7 2 25 Operating Altitude Limitations 2 8 2 27 Cabin Pressurization Limits 2 8 2 29 Noise Level 2 8 2 31 Maximum Seating Configuration 2 8 2 32 Icing Information 2 9 2 33 Placards 2 10 PIPER AIRCRAFT CORPORATION SECTION 2 PA 46 310P MALIBU LIMITATIONS ISSUED JULY...

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Страница 35: ...N 2 NS ns or ent 9 AS 00 70 33 02 00 2 1 ...

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Страница 37: ...N 2 NS 1 tal BE PM F F F F Hg Hg PSI PSI hr LL ade 1 ell 78 80 2 1 hes 00 2 3 ...

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Страница 39: ...N 2 NS m G G ted ved 00 2 5 ...

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Страница 41: ...2 NS L L 0 L in 00 7 ...

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Страница 43: ...dling from Air Traffic Control to facilitate a route or an altitude change to exit the icing conditions Unusually extensive ice accumulation on the airframe and windshield in areas not normally observed to collect ice Accumulation of ice on the upper surface of the wing aft of the protected area Accumulation of ice on the engine cowling and propeller spinner farther aft than normally observed Sinc...

Страница 44: ...ding spins approved This aircraft approved for V F R I F R day and night icing flight when equipped in accordance with the Airplane Flight Manual In full view of the pilot the following takeoff and landing checklists will be installed TAKEOFF CHECKLIST Fuel on Proper Tank Flaps Set Engine Gauges Checked Trim Set Induction Air Primary Controls Free Seat Backs Erect Door Secured Mixture Set Air Cond...

Страница 45: ...F M BEFORE RE ENGAGEMENT On the face of the turbine inlet temperature gauge CRUISE MIXTURE SETTING IS 50 LEAN OF PEAK T I T See A F M In full view of the pilot WARNING TURN OFF STROBE LIGHTS WHEN IN CLOSE PROXIMITY TO GROUND OR DURING FLIGHT THROUGH CLOUD FOG OR HAZE Near the magnetic compass CAUTION COMPASS CALIBRATION MAY BE IN ERROR WITH ELECTRICAL EQUIPMENT OTHER THAN AVIONICS ON ISSUED JULY 1...

Страница 46: ...ST BE OFF TO INSURE NORMAL TAKEOFF CLIMB PERFORMANCE On the inside of the forward baggage door MAXIMUM BAGGAGE THIS COMPART MENT 100 LBS On aft baggage closeout MAXIMUM BAGGAGE THIS COMPART MENT 100 LBS In full view of the pilot PRESSURIZED LANDING NOT APPROVED Adjacent to fuel tank filler caps Over emergency exit handle EMERGENCY EXIT REMOVE GLASS PULL DOOR IN LIFT UP SEC LIM REP 2 12 FOR REFEREN...

Страница 47: ...et Temperature TIT Indicator Failure 3 6 Electrical Failures 3 6 Electrical Overload 3 7 Propeller Overspeed 3 9 Emergency Landing Gear Extension 3 9 Spin Recovery 3 10 Engine Roughness 3 10 Emergency Descent 3 10 Pressurization System Malfunction 3 11 Cabin Air Contamination Smoke Evacuation Pressurized 3 12 Gyro Suction Failure 3 12 Inadvertent Icing Encounter or Flight in Snow 3 13 Hydraulic Sy...

Страница 48: ...3 25 High Cylinder Head Temperature 3 21 3 26 Turbine Inlet Temperature TIT Indicator Failure 3 21 3 27 Electrical Failures 3 21 3 29 Electrical Overload 3 22 3 31 Propeller Overspeed 3 24 3 33 Emergency Landing Gear Extension 3 24 3 35 Spin Recovery 3 24 3 37 Engine Roughness 3 25 3 39 Emergency Descent 3 25 3 41 Pressurization System Malfunction 3 26 3 43 Cabin Air Contamination Smoke Evacuation...

Страница 49: ...N 3 ES of he for res nd n 9 cy tle cy h a he ent res an e a ed to on he ain 00 3 1 ...

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Страница 51: ...N 3 ES OW TE on oss RY FF GH CH wer SE ch aps red ED off FF 00 3 3 ...

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Страница 53: ...red Aux fuel pump OFF Mixture as required If power not restored within ten seconds Aux fuel pump HIGH Mixture FULL RICH Throttle approx 75 power ENGINE DRIVEN FUEL PUMP FAILURE Throttle retard Aux fuel pump HIGH Throttle reset as required Mixture reset as required CAUTION If normal engine operation and fuel flow is not immediately re established the auxiliary fuel pumpshouldbeturnedOFF Thelackofaf...

Страница 54: ... FULL RICH If failure occurs after setting cruise power Mixture 6 GPH fuel flow above value in section 5 Power Setting Table Cylinder Head and Oil Temperatures MONITOR NOTE Repair TIT indicator as soon as possible ELECTRICAL FAILURES CAUTION The alternator output circuit breakers should never be opened manually when the alternators are functioning properly as voltage regulator damage may occur ALT...

Страница 55: ... not restored dual alternator system ALTR switch affected alternator OFF Electrical loads reduce Ammeter operating alternator monitor ELECTRICAL OVERLOAD alternator more than 20 amps above known electrical load AIRCRAFT EQUIPPED WITH SINGLE ALTERNATOR Electrical load reduce ALTR No 1 switch ON Battery switch OFF If alternator loads are reduced Electrical load reduce to minimum Land as soon as prac...

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Страница 57: ...N 3 ES FF FF FF ON ard eck m ny ble uce ain pm the ON eck me AS LL WN LL ne 00 3 9 ...

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Страница 59: ...N 3 ES AS AS AS ral MP ize eet FF IN eet 00 11 ...

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Страница 61: ...N 3 ES ON ON ON ON or red nd ull set ull 00 13 ...

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Страница 63: ...N 3 ES ly he not be his ure on is of ng as ne 00 15 ...

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Страница 65: ...N 3 ES le wer he ent ng vel ify If nd to ow be of ny to or will ed a e ed as ut to es 00 17 ...

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Страница 67: ...N 3 RES s of ing the n or rest ure ntil wer off ons oil ure the fuel fuel the 300 19 ...

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Страница 69: ... indication fails after cruise power has been set maintain cruise power setting and lean to 6 GPH fuel flow above that specified in the Power Setting Table in Section 5 of this handbook Continually monitor engine cylinder head and oil temperatures to avoid exceeding limits The TIT indicating system must be repaired as soon as possible after failure has occurred Continued operation with failed TIT ...

Страница 70: ...F the ALTR switch of the affected alternator insure electrical loads are below 60 amps and continue the flight Monitor the ammeter of the operating alternator since the ALTERNATOR annunciator light will remain on The ammeter is the only indication of the condition of the remaining alternator 3 29 ELECTRICAL OVERLOAD Alternator more than 20 amps above known electrical load If abnormally high altern...

Страница 71: ...the ALTR No 1 switch OFF and the battery switch OFF and turn the EMER BUS switch ON Activation of the emergency bus switch will allow the use of the minimum equipment necessary to operate the aircraft and will provide maximum flight time prior to battery depletion Refer to the Electrical Schematics in Section 7 for a list of equipment supplied by the emergency bus All electrical loads are being su...

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Страница 73: ...N 3 ES es un uel uel ngs en to ble t s nd to he ue in 00 25 ...

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Страница 75: ...N 3 ES an he of ng as he aft on ed on ng tot he as or ect 00 27 ...

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Страница 77: ...4 ES 0 0 1 2 2 2 3 3 4 4 4 5 5 8 9 00 4 i ...

Страница 78: ...4 23 Takeoff 4 24 4 25 Climb 4 26 4 27 Cruising 4 26 4 29 Descent 4 29 4 31 Approach and Landing 4 29 4 33 Go Around 4 30 4 35 Stopping Engine 4 31 4 37 Parking 4 31 4 39 Stalls 4 31 4 41 Turbulent Air Operation 4 32 4 43 Landing Gear 4 32 4 45 Cabin Pressurization System 4 33 4 47 Weight and Balance 4 34 4 49 Icing Information 4 35 SEC NO REP 4 ii Para No 4 15 4 17 4 19 4 21 4 23 4 25 4 27 4 29 4...

Страница 79: ...N 4 ES of ns ed nd n 9 nd for in he ch he res nd an ist afe at 00 4 1 ...

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Страница 81: ...N 4 ES nts set WN FF FF off ON ity eck eck nd FF on 00 4 3 ...

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Страница 83: ...N 4 ES eck eck ent uel ure ean eck ear eck ove per n eck eck ted ure ure ure ow eck ent uel ove per n eck eck ear ply cap ear 00 4 5 ...

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Страница 85: ...N 4 ES set ASE ank OFF ON set set set set eck CH RD ASE ON ON OFF ON 300 4 7 ...

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Страница 87: ...N 4 ES PM cle ure ON ter eck PM ved sed ear SE wly eck eck 00 4 9 ...

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Страница 89: ...N 4 ES FF ck RY ED ED ED ED ect on CH SE ed ed set set ee ed FF ed set set wer to de 00 11 ...

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Страница 91: ...N 4 ES CH PM Hg 0 ft 0 ft red set 5 ble I T FF eck 00 13 ...

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Страница 93: ...N 4 ES WN AS ed CH SE wer to de AS UP wly ed act FF FF SE ED off FF FF FF set lts up ce ure 00 4a ...

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Страница 95: ...N 4 ES on he ck us ht ght ore rol ke ure all he uel nel un is urn or to he or ny he he es he 00 15 ...

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Страница 97: ...N 4 ES tal ns on tic ne gin nd is ous ght per mal he uld ap nd are m is ior are xt tot 00 17 ...

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Страница 99: ...N 4 ES ock bin to op he FF ard ith on be not en mer W ree ow he 00 19 ...

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Страница 101: ...N 4 ES If and get to ger at 300 21 ...

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Страница 103: ...N 4 ES at hat mp to AC ice s for to for In at has he PM tal he 00 23 ...

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Страница 105: ...4 ES he et S er to S 90 le 00 25 ...

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Страница 107: ...N 4 ES wer he uel res ent uel an ure ure le to in ce en ure of if his g a ns 00 27 ...

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Страница 109: ...N 4 ES ols of ise ent he be to ase mal be At ne to ate ng ate be ith lly ed is he at 00 29 ...

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Страница 111: ...N 4 ES be he sed ear he cle t a cal he ure oid ery of or by he he nd An ed nd AS ng 00 31 ...

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Страница 113: ...N 4 ES in as mb ion the ove air led be not uld the the the at aft et 00 33 ...

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Страница 115: ...y request priority handling from Air Traffic Control to facilitate a route or an altitude change to exit the severe icing conditions in order to avoid extended exposure to flight conditions more severe than those for which the airplane has been certificated Avoid abrupt and excessive maneuvering that may exacerbate control difficulties Do not engage the autopilot If the autopilot is engaged hold t...

Страница 116: ...PIPER AIRCRAFT CORPORATION NORMAL PROCEDURES PA 46 310P MALIBU REPORT VB 1300 ISSUED JULY 1 1986 4 36 REVISED FEBRUARY 25 1999 THIS PAGE INTENTIONALLY LEFT BLANK SEC NO REP 4 36 FOR REFERENCE ONLY NOT FOR FLIGHT ...

Страница 117: ...N 5 CE e 00 5 i ...

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Страница 119: ...N 5 CE nce nd n 9 G on ons de nce he he by nd ge ng 00 5 1 ...

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Страница 121: ...N 5 CE ne ed he he to 7 he 6 to ity he he of bs bs bs bs bs bs he G 00 5 3 ...

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Страница 123: ...N 5 CE ary ise be me el air ng w of me for ve ft C n es l 00 5 5 ...

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Страница 125: ...N 5 CE wer ntal 5 the ise the iles iles wer AS H in gal mb me and 300 5 7 ...

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Страница 127: ...N 5 CE age No 1 2 3 4 5 6 7 8 9 0 1 3 4 5 6 7 8 9 0 00 5 9 ...

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Страница 129: ...N 5 CE 00 11 ...

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Страница 133: ... 46 310P MALIBU PERFORMANCE TAKEOFF GROUND ROLL 0 FLAPS Figure 5 9 ISSUED JULY 1 1986 REPORT VB 1300 5 15 PIPER AIRCRAFT CORPORATIO PA 46 310P MALIBU TAKEOFF GROU Fig ISSUED JULY 1 1986 F O R R E F E R E N C E O N L Y N O T F O R F L I G H T ...

Страница 134: ...ERFORMANCE PA 46 310P MALIBU REPORT VB 1300 ISSUED JULY 1 1986 5 16 TAKEOFF GROUND ROLL 20 FLAPS Figure 5 11 SECTION 5 PIPE PERFORMANCE REPORT VB 1300 5 16 TAKEOFF GROUND R Figure 5 1 F O R R E F E R E N C E O N L Y N O T F O R F L I G H T ...

Страница 135: ...U PERFORMANCE TAKEOFF DISTANCE OVER 50 FT OBSTACLE 0 FLAPS Figure 5 13 ISSUED JULY 1 1986 REPORT VB 1300 5 17 PIPER AIRCRAFT CORPORATIO PA 46 310P MALIBU TAKEOFF DISTANCE OVE Figu ISSUED JULY 1 1986 F O R R E F E R E N C E O N L Y N O T F O R F L I G H T ...

Страница 136: ...U REPORT VB 1300 ISSUED JULY 1 1986 5 18 REVISED NOVEMBER 22 1989 TAKEOFF DISTANCE OVER 50 FT OBSTACLE 20 FLAPS Figure 5 15 SECTION 5 PIPE PERFORMANCE REPORT VB 1300 5 18 R TAKEOFF DISTANCE OVER 50 F Figure 5 1 F O R R E F E R E N C E O N L Y N O T F O R F L I G H T ...

Страница 137: ...ECTION 5 PA 46 310P MALIBU PERFORMANCE RATE OF CLIMB Figure 5 17 ISSUED JULY 1 1986 REPORT VB 1300 5 19 PIPER AIRCRAFT CORPORATI PA 46 310P MALIBU RATE Fig ISSUED JULY 1 1986 F O R R E F E R E N C E O N L Y N O T F O R F L I G H T ...

Страница 138: ... 46 310P MALIBU REPORT VB 1300 ISSUED JULY 1 1986 5 20 REVISED APRIL 10 1987 TIME DISTANCE AND FUEL TO CLIMB Figure 5 19 SECTION 5 PIPE PERFORMANCE REPORT VB 1300 5 20 TIME DISTANCE AND Figure 5 1 F O R R E F E R E N C E O N L Y N O T F O R F L I G H T ...

Страница 139: ... CLIMB TIME DISTANCE AND FUEL TO CLIMB Figure 5 20 ISSUED JULY 1 1986 REPORT VB 1300 REVISED APRIL 10 1987 5 21 PIPER AIRCRAFT CORPORATI PA 46 310P MALIBU CRUI TIME DISTANCE Fig ISSUED JULY 1 1986 REVISED APRIL 10 1987 F O R R E F E R E N C E O N L Y N O T F O R F L I G H T ...

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Страница 141: ...N 5 CE 00 23 ...

Страница 142: ...AFT CORPORATION PERFORMANCE PA 46 310P MALIBU REPORT VB 1300 ISSUED JULY 1 1986 5 24 RANGE Figure 5 23 SECTION 5 PIPE PERFORMANCE REPORT VB 1300 5 24 RANGE Figure 5 2 F O R R E F E R E N C E O N L Y N O T F O R F L I G H T ...

Страница 143: ...N 5 CE 00 25 ...

Страница 144: ...RMANCE PA 46 310P MALIBU REPORT VB 1300 ISSUED JULY 1 1986 5 26 TIME DISTANCE AND FUEL TO DESCEND Figure 5 27 SECTION 5 PIPE PERFORMANCE REPORT VB 1300 5 26 TIME DISTANCE AND FU Figure 5 2 F O R R E F E R E N C E O N L Y N O T F O R F L I G H T ...

Страница 145: ...PA 46 310P MALIBU PERFORMANCE GLIDE TIME AND DISTANCE Figure 5 29 ISSUED JULY 1 1986 REPORT VB 1300 5 27 PIPER AIRCRAFT CORPORATIO PA 46 310P MALIBU GLIDE TIME Figu ISSUED JULY 1 1986 F O R R E F E R E N C E O N L Y N O T F O R F L I G H T ...

Страница 146: ...TION PERFORMANCE PA 46 310P MALIBU REPORT VB 1300 ISSUED JULY 1 1986 5 28 BALKED LANDING CLIMB Figure 5 31 SECTION 5 PIPE PERFORMANCE REPORT VB 1300 5 28 BALKED LANDIN Figure 5 3 F O R R E F E R E N C E O N L Y N O T F O R F L I G H T ...

Страница 147: ...NDING DISTANCE OVER 50 FT OBSTACLE Figure 5 33 ISSUED JULY 1 1986 REPORT VB 1300 REVISED APRIL 27 1990 5 29 PIPER AIRCRAFT CORPORATIO PA 46 310P MALIBU LANDING DISTANCE Figu ISSUED JULY 1 1986 REVISED APRIL 27 1990 F O R R E F E R E N C E O N L Y N O T F O R F L I G H T ...

Страница 148: ...ATION PERFORMANCE PA 46 310P MALIBU REPORT VB 1300 ISSUED JULY 1 1986 5 30 LANDING GROUND ROLL Figure 5 35 SECTION 5 PIPE PERFORMANCE REPORT VB 1300 5 30 LANDING GROU Figure 5 3 F O R R E F E R E N C E O N L Y N O T F O R F L I G H T ...

Страница 149: ...N 6 CE ge No 1 2 5 9 10 15 ith aft ork 300 6 i ...

Страница 150: ...N 6 CE are of e ith um ure s a ed ne he for ate nal ns aft ore ed ne G ed ng 00 6 1 ...

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Страница 152: ...N 6 CE of on bar nd ent ach ose ng he om 00 6 3 ...

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Страница 154: ...N 6 CE ed el ad ese on has is nd he or 00 6 5 ...

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Страница 156: ...Number Registration Number Page Number Date Item No Added Weight Change Running Basic Empty Weight Moment 100 Description of Article or Modification Wt Lb Remove d Moment 100 Arm In Wt Lb PA 46 310P Serial Number Registration Number Page Number Date Item No Added Weight Change Running Basic Empty Weight Moment 100 Description of Article or Modification Wt Lb Remove d Moment 100 Arm In Wt Lb F O R ...

Страница 157: ...Serial Number Registration Number Page Number Date Item No Added Weight Change Running Basic Empty Weight Moment 100 Description of Article or Modification Wt Lb Remove d Moment 100 Arm In Wt Lb PA 46 310P Serial Number Registration Number Page Number Date Item No Added Weight Change Running Basic Empty Weight Moment 100 Description of Article or Modification Wt Lb Remove d Moment 100 Arm In Wt Lb...

Страница 158: ...N 6 CE in w s a to ity uel of pe in ble 00 6 9 ...

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Страница 160: ...N 6 CE t ng 43 th nce nd G ER LL 00 11 ...

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Страница 162: ...N 6 PA 46 310P MALIBU WEIGHT AND BALANCE ISSUED JULY 1 1986 REPORT VB 1300 6 13 PIPER AIRCRAFT CORPORATIO PA 46 310P MALIBU ISSUED JULY 1 1986 LOADING GRAPH Figure 6 13 LOADI Fig F O R R E F E R E N C E O N L Y N O T F O R F L I G H T ...

Страница 163: ...AND BALANCE PA 46 310P MALIBU REPORT VB 1300 ISSUED JULY 1 1986 6 14 C G RANGE AND WEIGHT GRAPH Figure 6 15 SECTION 6 PIPE WEIGHT AND BALANCE REPORT VB 1300 6 14 C G RANGE AND WE Figure 6 1 F O R R E F E R E N C E O N L Y N O T F O R F L I G H T ...

Страница 164: ...N 6 CE CE the ent om ord ng an ed t a be ne ng ght of he ave he is el get 00 15 ...

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Страница 166: ...N 6 CE 00 17 ...

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Страница 168: ...N 6 CE 00 19 ...

Страница 169: ...7 N 0 i ...

Страница 170: ...N 7 ON ng ith eel nd sh at ns ne ger ve ed aft eps pe ent a ch 00 7 1 ...

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Страница 172: ...N 7 ON en oil ies mp o act ess at he air ng of on for air ity ke is er ke ve ed he nd he as en ate old er ive nd old ne 00 7 3 ...

Страница 173: ...N DESCR OPERATION PA 46 310P MALIBU REPORT VB 1300 ISSUED JULY 1 1986 7 4 TURBO INDUCTION SYSTEM Figure 7 1 SECTION 7 PIPE DESCR OPERATION REPORT VB 1300 7 4 TURBO INDUCTIO Figure 7 F O R R E F E R E N C E O N L Y N O T F O R F L I G H T ...

Страница 174: ...N 7 ON vent tion tion era tain ors om dual low ally ven and the low usly gine han the mer into wn ghts h a l is lve oil ven ers rear ion Oil 300 7 5 ...

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Страница 176: ...N 7 ON 00 7 7 ...

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Страница 178: ...N 7 ON he is is nd he wn rol he act he ge ral bly ief ed nd by he is ne ply ed ent ear ese 00 7 9 ...

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Страница 180: ...N 7 ON le tor ed ear lly lly is he are WN ear he s a UP ear he tor ch ly ck he ed he WN ed ng lly he lso not he 00 11 ...

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Страница 182: ...N 7 ON 00 13 ...

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Страница 184: ...N 7 ON are ed he im of ose ual on he aps ch lly ap 20 20 tor he in he ker nd em d ted 60 The eds nks ght 00 15 ...

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Страница 186: ...N 7 ON tor nd lly ht ng uel ent be ht of be is to ne is or is 00 17 ...

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Страница 188: ...N 7 ON tor n a ed nd to om ow HT nk FF nst ow on ush will he he mp ed he urn A he 00 19 ...

Страница 189: ...ON BU 986 ine by be most ron uld fuel first the igh Fuel C ery eath tem ting mum C ator mes ons ...

Страница 190: ...N 7 ON 00 21 ...

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Страница 192: ...N 7 ON 300 23 ...

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Страница 194: ...N 7 ON 00 25 ...

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Страница 196: ...N 7 ON ed AR MP E ect ery ent to or of lly ve is he ne ure nd ure is r a ed he 00 27 ...

Страница 197: ...ION DESCR OPERATION PA 46 310P MALIBU REPORT VB 1300 ISSUED JULY 1 1986 7 28 INSTRUMENT PANEL Figure 7 21 SECTION 7 PIPE DESCR OPERATION REPORT VB 1300 7 28 INSTRUMENT Figure 7 2 F O R R E F E R E N C E O N L Y N O T F O R F L I G H T ...

Страница 198: ...N 7 ON 00 29 ...

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Страница 200: ...CR OPERATION PITOT STATIC SYSTEM Figure 7 23 ISSUED JULY 1 1986 REPORT VB 1300 REVISED MARCH 18 1991 7 31 PIPER AIRCRAFT CORPORATI PA 46 310P MALIBU PITOT STA Fig ISSUED JULY 1 1986 REVISED MARCH 18 1991 F O R R E F E R E N C E O N L Y N O T F O R F L I G H T ...

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Страница 202: ...N 7 ON 00 33 ...

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Страница 204: ...N 7 ON es in bin ns is al ill ar ng on ng in 00 35 ...

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Страница 206: ...N 7 ON ed ow he to air ng nd bin ent he has rty ero mp ge em of ad of ies ies to um of ure he be 00 37 ...

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Страница 208: ...N 7 ON 00 39 ...

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Страница 210: ...N 7 ON ng all ng ap om as he an ap he ed bin are eat s is eaf ed ght ins six per are 00 41 ...

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Страница 212: ...N 7 ON nd of he he oor OR To ble is me he f a ng rn nd of 00 43 ...

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Страница 214: ...N 7 ON is he nd he will he ch en an ay res he to be to o a nt be of sic d a ect ous he on 00 45 ...

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Страница 216: ...N 8 NT e 0 1 2 6 6 6 6 7 7 2 00 8 i ...

Страница 217: ...nd to N 8 NT 00 1 ...

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Страница 219: ...ce on ort get cal ce rs rs in on his es if ve al est ce ble ee r s ble ne N 8 NT 00 1B ...

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Страница 221: ...al he be at ns he ot ial or A he AA ce ay me pe N 8 NT 00 3 ...

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Страница 223: ...N 8 NT the nel on wn is ar ng to ess or ver up or he tly no gth eft nd ake ake 00 8 5 ...

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Страница 225: ...N 8 NT ove ir of air 50 sty ept use ket of rs ge nel lic our is 00 8 7 ...

Страница 226: ...PORATION HAND SERV MAINT PA 46 310P MALIBU BRAKE SYSTEM Figure 8 1 REPORT VB 1300 ISSUED JULY 1 1986 8 8 SECTION 8 PIPE HAND SERV MAINT BRAKE SYS Figure 8 REPORT VB 1300 8 8 F O R R E F E R E N C E O N L Y N O T F O R F L I G H T ...

Страница 227: ...N 8 NT If he ed ith ric ge aft uid nd up els s a x 5 nd for ee on ntil uld to eo in he ow lve 00 8 9 ...

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Страница 229: ...N 8 NT 300 11 an um t is t is or ers ntal oil red ...

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Страница 231: ...N 8 NT ng ust ed of be uid der for ng 00 13 ...

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Страница 233: ...N 8 NT or en mp 00 15 ...

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Страница 235: ...N 8 NT nd 46 he er se ere en nal in ble are ust er 00 17 ...

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Страница 237: ...N 8 NT ior aft ght ith ard e a by oth to lds at ry rit he art oil 00 19 ...

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Страница 239: ...N 8 NT on ed ed ly oes as ed ter ice ne ch ed 00 21 ...

Страница 240: ......

Страница 241: ...N 8 NT ned ail be ce ter nd to hly ed as 00 23 ...

Страница 242: ...6 Pages 9 85 9 TI 9000 Loran C Navigator With KAP KFC 150 Autopilot System 6 Pages 9 91 10 Ice Protection System 16 Pages 9 97 11 3M Ryan Stormscope WX 11 6 Pages 9 113 12 ARNAV R 30 Loran C Navigator and RS08 Series Remote Switch with KAP KFC 150 Autopilot System 6 Pages 9 119 13 Northstar M1 Loran C Navigator with KAP KFC 150 Autopilot System 4 Pages 9 125 14 Supplemental Electric Heater 6 Pages...

Страница 243: ...N 9 TS are ne ith nd he ed 00 9 1 ...

Страница 244: ...proved Operational Supplement to the Bendix King 150 Series Flight Control System as installed per STC SA1778CE D Effective this revision Bendix King will be responsible to supply and revise the operational supplement It is permitted to include the Bendix King supplement in this location of the Pilots Operating Handbook unless otherwise stated by Bendix King pages 9 4 through 9 36 DELETED ISSUED J...

Страница 245: ...N 9 T 2 ok rea he in ght nd he ght 00 37 ...

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Страница 247: ...N 9 T 2 SP he ce for SE ols ler he he in on ear he he he git in TA in nce he NM NM be 00 39 ...

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Страница 249: ...N 9 T 2 and by osi mute ng pear use nt 2 DSP data ace nt 2 TAC M CDI ying rom nce d of ion 300 41 ...

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Страница 251: ...N 9 T 2 and the as ects way ows note 300 43 ...

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Страница 253: ...N 9 T 2 of a lide CDI two usly ime nce th a hile OR the the hen e in hen wer to ory oint eak Hz lay ory wing 300 45 ...

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Страница 255: ...N 9 T 2 ted ree nd nd is 00 47 ...

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Страница 257: ...N 9 T 2 go ST ay 00 49 ...

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Страница 259: ...N 9 T 3 ok rea or he ght nd sic 00 51 ...

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Страница 261: ...N 9 T 3 00 53 int he he nt ble ce ob on ect TA ect ow um on a ts he nd OR me int me me AV ...

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Страница 263: ...N 9 T 3 tor ME ce on ay 10 he he om be to will but GS nly ay ng NV ay All 00 55 ...

Страница 264: ......

Страница 265: ...N 9 T 3 nel tal R ME R DE ed VE ge nd nd ant ch ace nd ch he ges nd he or TA ma for ed by he PT me ng ile was h a int 00 57 ...

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Страница 267: ...N 9 T 3 00 59 nd nd on re he re nd nd AD ME ...

Страница 268: ......

Страница 269: ...N 9 T 3 00 61 ies may UT he ith he ur he on ver ob po ...

Страница 270: ...N 9 T 4 ok lis per or nd For his AA 00 63 ...

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Страница 272: ...N 9 T 4 00 65 mup Y ght nate h a ning tion ness ...

Страница 273: ......

Страница 274: ...N 9 T 4 nd of of is is ght 00 67 ...

Страница 275: ...N 9 T 5 ok en on t s in ce t s 00 69 ...

Страница 276: ......

Страница 277: ...N 9 T 5 as EN ard ate on s om ES ow 00 ute ed 00 71 ...

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Страница 279: ...N 9 T 5 ne he is is be he en ent ery oth ng se wo sks ny me sk eat en ew he tor he 00 73 ...

Страница 280: ......

Страница 281: ...N 9 T 6 ok ner on t s in ce t s 00 75 ...

Страница 282: ......

Страница 283: ...N 9 T 6 ise or air ght ile ght 00 77 ...

Страница 284: ......

Страница 285: ...N 9 T 7 ok 0A on sic ual nce t s 00 79 ...

Страница 286: ......

Страница 287: ...N 9 T 7 ad ret em the NM be ew ols 00 81 ...

Страница 288: ......

Страница 289: ...N 9 T 7 he ted of will ow he he he om he tic als ate ant er per ght ng 00 83 ...

Страница 290: ......

Страница 291: ...N 9 T 8 ok ng wg ce he ed ns nt ne 00 85 ...

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Страница 293: ...N 9 T 8 ght AT CE ply ded to rol an ght ice ker he N ch em en he eat 00 87 ...

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Страница 295: ...N 9 T 8 00 89 ...

Страница 296: ...N 9 T 9 ok 00 on ng eas not ok 00 91 ...

Страница 297: ......

Страница 298: ...N 9 T 9 on of C 81 her V ce es ght or he rse des 00 93 ...

Страница 299: ......

Страница 300: ...N 9 T 9 on yed he sic ng 00 95 ...

Страница 301: ...N 9 10 ok per ein ng eas not ok 00 97 ...

Страница 302: ......

Страница 303: ...N 9 10 OR for ors mps ng ine tor eck d ON FF ce ase be ed ng 00 99 ...

Страница 304: ......

Страница 305: ...N 9 10 ons in as no ht d ow ure ve ed in ht or on m not ed he ds 00 01 ...

Страница 306: ...activated again A green SURFACE DEICE annunciator light will remain on for approximately eighteen seconds 2 Visually check to insure that the boots have fully deflated to indicate proper operation of the vacuum portion of the pneumatic boot pump system e The dual alternators should be checked by cycling the A V volt ammeter switch and observing for indication of output from both alternators on the...

Страница 307: ...N 9 10 al TE ON ON ON ON UT nal red 1 2 on ler ent ich ery ect 00 03 ...

Страница 308: ......

Страница 309: ...N 9 10 ght 00 05 ...

Страница 310: ......

Страница 311: ...N 9 10 RF an ght ice ker he N ch cal el mer he ute to he or ove AT of he he am 00 07 ...

Страница 312: ......

Страница 313: ...N 9 10 00 09 ete ng TR uit he be he he ge he lly AC ng by ice the uld of red ent wn he cal aft ay he en ur ...

Страница 314: ......

Страница 315: ...N 9 10 00 11 ...

Страница 316: ...N 9 11 ok 11 on sic ual nd sic 00 13 ...

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Страница 318: ...N 9 11 ad ret em on 00 lly ew ols ure dot urn ain be LR or LR 00 15 ...

Страница 319: ......

Страница 320: ...N 9 11 he ted of will ow he he he om he tic als ate ant er ify ght 00 17 ...

Страница 321: ......

Страница 322: ...N 9 12 ok R on ng eas not ok 00 19 ...

Страница 323: ......

Страница 324: ...N 9 12 00 21 her V on ese ual ng he rse des R R R R he n ...

Страница 325: ......

Страница 326: ...N 9 12 he ail by ay ely ht will he air on ed ve LS vi ies ed ght 00 23 ...

Страница 327: ...N 9 13 00 25 ok M1 on ng eas not ok ...

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Страница 329: ...N 9 13 00 27 her V on se ual ng he se des d e s ...

Страница 330: ......

Страница 331: ...N 9 14 ok tal 65 he ed ns nt ne 00 29 ...

Страница 332: ......

Страница 333: ...N 9 14 ON FF ON CK Vdc as ge ED FF FF ON ON ON FF UT AR IN 00 31 ...

Страница 334: ......

Страница 335: ...9 14 00 33 he to or ...

Страница 336: ......

Страница 337: ...N 9 15 00 35 ook ow he or ved ns nt ane ...

Страница 338: ......

Страница 339: ...N 9 15 00 37 II ag di on FR ck cal ed he be on nd nel on of ...

Страница 340: ......

Страница 341: ...N 9 15 00 39 lly is nly ff or rse or ng ed hat lly T ht or vi ht or ...

Страница 342: ......

Страница 343: ...N 9 16 ok nal he or nd in ed nd __ 00 41 ...

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Страница 345: ...N 9 16 ase nd na he na he of he ted 00 43 ...

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Страница 347: ...N 9 T 16 300 145 ying Wx the n 2 enta her the s of ...

Страница 348: ......

Страница 349: ...N 9 T 16 300 147 nly is her wer sor wn the and 30 up No nna Y is ay ern no will of her on ON the ted AV ies to dar ...

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Страница 351: ...ON 9 T 16 300 149 iate the e to l be ine cted tem aken the tton wo lt to r to The ight the ead Tilt FF the ...

Страница 352: ......

Страница 353: ...10 PS e 1 1 00 0 i ...

Страница 354: ...10 PS on on mal an of ull is the ive ght to gh ial ity 00 0 1 ...

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Malibu Boats PA-46-310P, Руководство по эксплуатации для пилотов

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Содержание PA-46-310P

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