Malibu Boats PA-46-310P Pilot Operating Handbook Download

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SECTION 5

PIPER AIRCRAFT CORPORA

TION

PERFORMANCE

A-46-310P

, MALIB

REPOR

: VB-1300

ISSUED: JUL

Y 1, 1986

5-18

REVISED: NO

VEMBER 22, 1989

AKEOFF DIST

ANCE O

VER 50 FT

. OBST

CLE, 20° FLAPS

Figure 5-15

SECTION 5

PIPER AIRCRAFT CORPORA

TION

PERFORMANCE

A-46-310P

, MALIB

REPOR

: VB-1300

ISSUED: JUL

Y 1, 1986

5-18

REVISED: NO

VEMBER 22, 1989

AKEOFF DIST

ANCE O

VER 50 FT

. OBST

CLE, 20° FLAPS

Figure 5-15

FOR REFERENCE ONLY

NOT FOR FLIGHT

Summary of Contents for PA-46-310P

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

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Page 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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Page 17: ...300 vii ...

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Page 19: ...N 1 AL 00 1 i ...

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

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

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

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Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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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Page 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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Page 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...

Page 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...

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

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

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

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Page 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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Page 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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Page 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 ...

Page 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...

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

Page 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...

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

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

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

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Page 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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Page 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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Page 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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Page 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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Page 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...

Page 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 ...

Page 117: ...N 5 CE e 00 5 i ...

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Page 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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Page 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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Page 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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Page 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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Page 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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Page 129: ...N 5 CE 00 11 ...

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Page 131: ...N 5 CE 00 13 ...

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Page 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 ...

Page 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 ...

Page 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 ...

Page 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 ...

Page 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 ...

Page 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 ...

Page 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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Page 141: ...N 5 CE 00 23 ...

Page 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 ...

Page 143: ...N 5 CE 00 25 ...

Page 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 ...

Page 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 ...

Page 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 ...

Page 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 ...

Page 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 ...

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

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

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

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Page 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 ...

Page 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...

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

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

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Page 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 ...

Page 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 ...

Page 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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Page 166: ...N 6 CE 00 17 ...

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Page 168: ...N 6 CE 00 19 ...

Page 169: ...7 N 0 i ...

Page 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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Page 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 ...

Page 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 ...

Page 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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Page 176: ...N 7 ON 00 7 7 ...

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Page 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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Page 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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Page 182: ...N 7 ON 00 13 ...

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Page 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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Page 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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Page 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 ...

Page 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 ...

Page 190: ...N 7 ON 00 21 ...

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Page 192: ...N 7 ON 300 23 ...

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Page 194: ...N 7 ON 00 25 ...

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Page 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 ...

Page 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 ...

Page 198: ...N 7 ON 00 29 ...

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Page 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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Page 202: ...N 7 ON 00 33 ...

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

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Page 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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Page 208: ...N 7 ON 00 39 ...

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

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

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

Page 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 ...

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

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

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

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

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

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

Page 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...

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

Page 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...

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

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

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

Page 256: ......

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

Page 258: ......

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

Page 260: ......

Page 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 ...

Page 262: ......

Page 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 ...

Page 264: ......

Page 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 ...

Page 266: ......

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

Page 268: ......

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

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

Page 271: ......

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

Page 273: ......

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

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

Page 276: ......

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

Page 278: ......

Page 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 ...

Page 280: ......

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

Page 282: ......

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

Page 284: ......

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

Page 286: ......

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

Page 288: ......

Page 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 ...

Page 290: ......

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

Page 292: ......

Page 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 ...

Page 294: ......

Page 295: ...N 9 T 8 00 89 ...

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

Page 297: ......

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

Page 299: ......

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

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

Page 302: ......

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

Page 304: ......

Page 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 ...

Page 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...

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

Page 308: ......

Page 309: ...N 9 10 ght 00 05 ...

Page 310: ......

Page 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 ...

Page 312: ......

Page 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 ...

Page 314: ......

Page 315: ...N 9 10 00 11 ...

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

Page 317: ......

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

Page 319: ......

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

Page 321: ......

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

Page 323: ......

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

Page 325: ......

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

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

Page 328: ......

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

Page 330: ......

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

Page 332: ......

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

Page 334: ......

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

Page 336: ......

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

Page 338: ......

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

Page 340: ......

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

Page 342: ......

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

Page 344: ......

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

Page 346: ......

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

Page 348: ......

Page 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 ...

Page 350: ......

Page 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 ...

Page 352: ......

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

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

Page 355: ......

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Malibu Boats PA-46-310P, Pilot Operating Handbook

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