Mirage AVS-500 Manuel de service

MALIBU MIRAGEPA-46-350PSN 4636196 AND UPPILOT’SOPERATINGHANDBOOKANDFAA APPROVEDAIRPLANE FLIGHT MANUALAIRPLANE AIRPLANESERIAL NO. ____________________

Revision FAA ApprovedNumber and Revised Description of Revisions SignatureCode Pages and DatePA-46-350P, MALIBUPILOT'S OPERATING HANDBOOK LOG OF

SECTION 4NORMAL PROCEDURES PA-46-350P, MALIBUSECTION 4NORMAL PROCEDURES PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19994-16REPORT: VB-1710

4.5m Approach And Landing Checklist (4.31) (Continued)SHORT FIELD TECHNIQUE (4.31b)Flaps...

SECTION 4NORMAL PROCEDURES PA-46-350P, MALIBUSECTION 4NORMAL PROCEDURES PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19994-18REPORT: VB-1710

4.7 AMPLIFIED NORMAL PROCEDURES (GENERAL)The following paragraphs are provided to supply detailed informationand the explanation of the normal proced

SECTION 4NORMAL PROCEDURES PA-46-350P, MALIBUSECTION 4NORMAL PROCEDURES PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19994-20REPORT: VB-1710

4.9 PREFLIGHT CHECK (4.5a) (Continued)4.9d Nose Section (4.5a)Check the general condition of the nose section; look for oil or fluidleakage and that t

SECTION 4NORMAL PROCEDURES PA-46-350P, MALIBUSECTION 4NORMAL PROCEDURES PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19994-22REPORT: VB-1710

4.11 BEFORE STARTING ENGINE (4.5b) (Continued)If the flight is to be made unpressurized, the cabin pressurization controlshould be pulled out to dump

SECTION 4NORMAL PROCEDURES PA-46-350P, MALIBUSECTION 4NORMAL PROCEDURES PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19994-24REPORT: VB-1710

4.13 ENGINE START (4.5c) (Continued)4.13e Engine Start With External Power Source (4.5c)An optional feature allows the operator to use an external p

TABLE OF CONTENTSSECTION 1 GENERALSECTION 2 LIMITATIONSSECTION 3 EMERGENCY PROCEDURESSECTION 4 NORMAL PROCEDURESSECTION 5 PERFORMANCESECTION 6 WEIGHT

SECTION 4NORMAL PROCEDURES PA-46-350P, MALIBUSECTION 4NORMAL PROCEDURES PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19994-26REPORT: VB-1710

4.19 GROUND CHECK (4.5f)CAUTIONAlternate air is unfiltered. Use of alternate airduring ground or flight operations when dustor other contaminants are

SECTION 4NORMAL PROCEDURES PA-46-350P, MALIBUSECTION 4NORMAL PROCEDURES PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19994-28REPORT: VB-1710

4.23 TAKEOFF (4.5h) (Continued)4.23a Normal Technique (4.5h)When the available runway length is well in excess of that required andobstacle clearance

SECTION 4NORMAL PROCEDURES PA-46-350P, MALIBUSECTION 4NORMAL PROCEDURES PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19994-30REPORT: VB-1710

4.27 CRUISE (4.5J) (CONTINUED)The cruising speed is determined by many factors, including power setting,altitude, temperature, loading, and equipment

SECTION 4NORMAL PROCEDURES PA-46-350P, MALIBUSECTION 4NORMAL PROCEDURES PA-46-350P, MALIBUREPORT: VB-1710 ISSUED:FEBRUARY 23, 19994-32REPORT: VB-1710

4.29 DESCENT (4.5k)The recommended procedure for descent is to leave the engine controlsat the cruise settings and increase the airspeed to give the d

SECTION 4NORMAL PROCEDURES PA-46-350P, MALIBUSECTION 4NORMAL PROCEDURES PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19994-34REPORT: VB-1710

4.33 GO-AROUND (4.5n)To initiate a go-around from a landing approach, the mixture should beset to full RICH, the propeller control should be at full

TABLE OF CONTENTSSECTION 1 GENERALParagraph PageNo. No.1.1 Introduction ...

SECTION 4NORMAL PROCEDURES PA-46-350P, MALIBUSECTION 4NORMAL PROCEDURES PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19994-36REPORT: VB-1710

4.45 CABIN PRESSURIZATION SYSTEMCabin pressurization system controls, gauges and switches are located tothe right of the pilots control wheel shaft. (

SECTION 4NORMAL PROCEDURES PA-46-350P, MALIBUSECTION 4NORMAL PROCEDURES PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19994-38REPORT: VB-1710

4.47 SUPPLEMENTAL ELECTRIC HEATERAFTER ENGINE STARTBATT MASTER Switch ...

SECTION 4NORMAL PROCEDURES PA-46-350P, MALIBUSECTION 4NORMAL PROCEDURES PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19994-40REPORT: VB-1710

SECTION 4 PA-46-350P, MALIBU NORMAL PROCEDURES4.50 ICING INFORMATION"THE FOLLOWING WEATHER CONDITIONS MAY BECONDUCIVE TO SEVERE IN-FLIGHT ICING&

TABLE OF CONTENTSSECTION 5PERFORMANCEParagraph PageNo. No.5.1 General ...

SECTION 5PERFORMANCE5.1 GENERALAll of the required (FAA regulations) and complementary performanceinformation is provided by this section.Performance

SECTION 5PERFORMANCE PA-46-350P, MALIBUSECTION 5PERFORMANCE PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19995-2REPORT: VB-1710 ISSUED: FEBR

5.5 FLIGHT PLANNING EXAMPLE(a) Aircraft LoadingThe first step in planning the flight is to calculate the airplaneweight and center of gravity by utili

SECTION 1GENERAL1.1 INTRODUCTIONThis Pilot’s Operating Handbook is designed for maximum utilizationas an operating guide for the pilot. It includes th

SECTION 5PERFORMANCE PA-46-350P, MALIBUSECTION 5PERFORMANCE PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19995-4 REVISED: SEPTEMBER 20, 1999

5.5 FLIGHT PLANNING EXAMPLE (CONT)NOTEThe remainder of the performance charts usedin this flight plan example assume a no windcondition. The effect of

SECTION 5PERFORMANCE PA-46-350P, MALIBUSECTION 5PERFORMANCE PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19995-6REPORT: VB-1710 ISSUED: FEBR

SECTION 5PA-46-350P, MALIBU PERFORMANCESECTION 5PA-46-350P, MALIBU PERFORMANCEISSUED: FEBRUARY 23, 1999 REPORT: VB-1710REVISED: SEPTEMBER 20, 1999 5-

SECTION 5PERFORMANCE PA-46-350P, MALIBUSECTION 5PERFORMANCE PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19995-8 REVISED: SEPTEMBER 20, 1999

SECTION 5PA-46-350P, MALIBU PERFORMANCESECTION 5PA-46-350P, MALIBU PERFORMANCEISSUED: FEBRUARY 23, 1999 REPORT: VB-1710REVISED: SEPTEMBER 20, 1999 5-9

SECTION 5PA-46-350P, MALIBU PERFORMANCESECTION 5PA-46-350P, MALIBU PERFORMANCEISSUED: FEBRUARY 23, 1999 REPORT: VB-17105-11ISSUED: FEBRUARY 23, 1999 R

SECTION 5PERFORMANCE PA-46-350P, MALIBUSECTION 5PERFORMANCE PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19995-12REPORT: VB-1710 ISSUED: FEB

SECTION 5PA-46-350P, MALIBU PERFORMANCESECTION 5PA-46-350P, MALIBU PERFORMANCEISSUED: FEBRUARY 23, 1999 REPORT: VB-17105-13ISSUED: FEBRUARY 23, 1999

SECTION 5PERFORMANCE PA-46-350P, MALIBUSECTION 5PERFORMANCE PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19995-14REPORT: VB-1710 ISSUED: FEB

SECTION 1GENERAL PA-46-350P, MALIBUSECTION 1GENERAL PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19991-2REPORT: VB-1710 ISSUED: FEBRUARY 23,

SECTION 5PA-46-350P, MALIBU PERFORMANCESECTION 5PA-46-350P, MALIBU PERFORMANCEISSUED: FEBRUARY 23, 1999 REPORT: VB-17105-15ISSUED: FEBRUARY 23, 1999 R

SECTION 5PERFORMANCE PA-46-350P, MALIBUSECTION 5PERFORMANCE PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19995-16REPORT: VB-1710 ISSUED: FEB

SECTION 5PA-46-350P, MALIBU PERFORMANCESECTION 5PA-46-350P, MALIBU PERFORMANCEISSUED: FEBRUARY 23, 1999 REPORT: VB-17105-17ISSUED: FEBRUARY 23, 1999 R

SECTION 5PERFORMANCE PA-46-350P, MALIBUSECTION 5PERFORMANCE PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19995-18REPORT: VB-1710 ISSUED: FEB

SECTION 5PA-46-350P, MALIBU PERFORMANCESECTION 5PA-46-350P, MALIBU PERFORMANCEISSUED: FEBRUARY 23, 1999 REPORT: VB-17105-19ISSUED: FEBRUARY 23, 1999 R

SECTION 5PERFORMANCE PA-46-350P, MALIBUSECTION 5PERFORMANCE PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19995-20REPORT: VB-1710 ISSUED: FEB

SECTION 5PA-46-350P, MALIBU PERFORMANCESECTION 5PA-46-350P, MALIBU PERFORMANCEISSUED: FEBRUARY 23, 1999 REPORT: VB-17105-21ISSUED: FEBRUARY 23, 1999 R

SECTION 5PERFORMANCE PA-46-350P, MALIBUSECTION 5PERFORMANCE PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19995-22 REVISED: SEPTEMBER 20, 199

SECTION 5PA-46-350P, MALIBU PERFORMANCESECTION 5PA-46-350P, MALIBU PERFORMANCEISSUED: FEBRUARY 23, 1999 REPORT: VB-1710REVISED: SEPTEMBER 20, 1999 5-2

SECTION 5PERFORMANCE PA-46-350P, MALIBUSECTION 5PERFORMANCE PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19995-24 REVISED: SEPTEMBER 20, 199

1.3 ENGINE(a)Number of Engines 1(b) Engine Manufacturer Textron Lycoming(c) Engine Model Number TIO-540-AE2A(d) Rated Horsepower 350(e) Rated Speed (r

SECTION 5PA-46-350P, MALIBU PERFORMANCESECTION 5PA-46-350P, MALIBU PERFORMANCEISSUED: FEBRUARY 23, 1999 REPORT: VB-17105-25ISSUED: FEBRUARY 23, 1999 R

SECTION 5PERFORMANCE PA-46-350P, MALIBUSECTION 5PERFORMANCE PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19995-26REPORT: VB-1710 ISSUED: FEB

SECTION 5PA-46-350P, MALIBU PERFORMANCESECTION 5PA-46-350P, MALIBU PERFORMANCEISSUED: FEBRUARY 23, 1999 REPORT: VB-17105-27ISSUED: FEBRUARY 23, 1999 R

SECTION 5PERFORMANCE PA-46-350P, MALIBUSECTION 5PERFORMANCE PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19995-28 REVISED: SEPTEMBER 20, 199

SECTION 5PA-46-350P, MALIBU PERFORMANCESECTION 5PA-46-350P, MALIBU PERFORMANCEISSUED: FEBRUARY 23, 1999 REPORT: VB-17105-29ISSUED: FEBRUARY 23, 1999 R

SECTION 5PERFORMANCE PA-46-350P, MALIBUSECTION 5PERFORMANCE PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19995-30REPORT: VB-1710 ISSUED: FEB

SECTION 5PA-46-350P, MALIBU PERFORMANCESECTION 5PA-46-350P, MALIBU PERFORMANCEISSUED: FEBRUARY 23, 1999 REPORT: VB-17105-31ISSUED: FEBRUARY 23, 1999 R

SECTION 5PERFORMANCE PA-46-350P, MALIBUSECTION 5PERFORMANCE PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19995-32REPORT: VB-1710 ISSUED: FEB

SECTION 5PA-46-350P, MALIBU PERFORMANCESECTION 5PA-46-350P, MALIBU PERFORMANCEISSUED: FEBRUARY 23, 1999 REPORT: VB-1710REVISED: SEPTEMBER 20, 1999 5-

SECTION 5PERFORMANCE PA-46-350P, MALIBUSECTION 5PERFORMANCE PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19995-34 REVISED: SEPTEMBER 20, 199

SECTION 1GENERAL PA-46-350P, MALIBUSECTION 1GENERAL PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19991-4REPORT: VB-1710 ISSUED: FEBRUARY 23,

TABLE OF CONTENTSSECTION 6 WEIGHT AND BALANCEParagraph PageNo. No.6.1 General ...

SECTION 6WEIGHT AND BALANCE6.1 GENERALIn order to achieve the performance and flying characteristics which aredesigned into the airplane, it must be f

SECTION 6WEIGHT AND BALANCE PA-46-350P, MALIBUSECTION 6WEIGHT AND BALANCE PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19996-2REPORT: VB-171

SECTION 6 PA-46-350P, MALIBU WEIGHT AND BALANCE6.3 AIRPLANE WEIGHING PROCEDURE (Continued)CAUTIONWhenever the fuel system is completely drainedand fue

SECTION 6WEIGHT AND BALANCE PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19996-4 REVISED: SEPTEMBER 10, 20016.3 AIRPLANE WEIGHING PROCEDURE

6.3 AIRPLANE WEIGHING PROCEDURE (Continued)(2) The basic empty weight center of gravity (as weighedincluding optional equipment, full oil and unusable

SECTION 6WEIGHT AND BALANCE PA-46-350P, MALIBUSECTION 6WEIGHT AND BALANCE PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19996-6REPORT: VB-171

SECTION 6PA-46-350P, MALIBU WEIGHT AND BALANCESECTION 6PA-46-350P, MALIBU WEIGHT AND BALANCEISSUED: FEBRUARY 23, 1999 REPORT: VB-17106-7ISSUED: FEBRUA

SECTION 6WEIGHT AND BALANCE PA-46-350P, MALIBUSECTION 6WEIGHT AND BALANCE PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19996-8REPORT: VB-171

6.7 GENERAL LOADING RECOMMENDATIONSFor all airplane configurations, it is the responsibility of the pilot incommand to make sure that the airplane alw

1.11 MAXIMUM WEIGHTS(a) Maximum Ramp Weight (lb) 4358(b) Maximum Takeoff Weight (lb) 4340(c) Maximum Landing Weight (lb) 4123(d) Maximum Zero Fuel Wei

SECTION 6WEIGHT AND BALANCE PA-46-350P, MALIBUSECTION 6WEIGHT AND BALANCE PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19996-10REPORT: VB-17

SECTION 6PA-46-350P, MALIBU WEIGHT AND BALANCESECTION 6PA-46-350P, MALIBU WEIGHT AND BALANCEISSUED: FEBRUARY 23, 1999 REPORT: VB-1710REVISED: SEPTEMBE

SECTION 6WEIGHT AND BALANCE PA-46-350P, MALIBUSECTION 6WEIGHT AND BALANCE PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19996-12 REVISED: SEP

SECTION 6PA-46-350P, MALIBU WEIGHT AND BALANCESECTION 6PA-46-350P, MALIBU WEIGHT AND BALANCEISSUED: FEBRUARY 23, 1999 REPORT: VB-17106-13ISSUED: FEBRU

SECTION 6WEIGHT AND BALANCE PA-46-350P, MALIBUSECTION 6WEIGHT AND BALANCE PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19996-14 REVISED: SEP

TABLE OF CONTENTSSECTION 7DESCRIPTION AND OPERATIONOF THE AIRPLANE AND ITS SYSTEMSParagraphPageNo. No.7.1 The Airplane...

SECTION 7DESCRIPTION AND OPERATIONOF THE AIRPLANE AND ITS SYSTEMS7.1 THE AIRPLANEThe PA-46-350P Malibu is a single engine, all metal, retractable land

SECTION 7DESCR/OPERATION PA-46-350P, MALIBUSECTION 7DESCR/OPERATION PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19997-2REPORT: VB-1710 ISSU

7.5 ENGINE AND PROPELLER (Continued)manifold pressure. Accessories include a starter, two magnetos, a propellergovernor, two belt driven alternators,

SECTION 7DESCR/OPERATION PA-46-350P, MALIBUSECTION 7DESCR/OPERATION PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19997-4REPORT: VB-1710 ISSU

1.21 SYMBOLS, ABBREVIATIONS AND TERMINOLOGYThe following definitions are of symbols, abbreviations and terminologyused throughout the handbook and tho

7.5 ENGINE AND PROPELLER (continued)from overboost damage by limiting manifold pressure to 42.0 in. Hg. In theevent of a controller malfunction, there

SECTION 7DESCR/OPERATION PA-46-350P, MALIBUSECTION 7DESCR/OPERATION PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19997-6 REPORT: VB-1710 ISS

SECTION 7PA-46-350P, MALIBU DESCR/OPERATIONSECTION 7PA-46-350P, MALIBU DESCR/OPERATIONISSUED: FEBRUARY 23, 1999 REPORT: VB-17107-7ISSUED: FEBRUARY 2

SECTION 7DESCR/OPERATION PA-46-350P, MALIBUSECTION 7DESCR/OPERATION PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19997-8REPORT: VB-1710 ISSU

SECTION 7PA-46-350P, MALIBU DESCR/OPERATIONSECTION 7PA-46-350P, MALIBU DESCR/OPERATIONISSUED: FEBRUARY 23, 1999 REPORT: VB-17107-9ISSUED: FEBRUARY 23,

SECTION 7DESCR/OPERATION PA-46-350P, MALIBUSECTION 7DESCR/OPERATION PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19997-10REPORT: VB-1710 ISS

SECTION 7 PA-46-350P, MALIBU DESCR/OPERATIONSECTION 7 PA-46-350P, MALIBU DESCR/OPERATIONISSUED: FEBRUARY 23, 1999 REPORT: VB-17107-11ISSUED: FEBRUAR

SECTION 7DESCR/OPERATION PA-46-350P, MALIBUSECTION 7DESCR/OPERATION PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19997-12REPORT: VB-1710 ISS

SECTION 7 PA-46-350P, MALIBU DESCR/OPERATIONISSUED: FEBRUARY 23, 1999 REPORT: VB-17107-13SECTION 7 PA-46-350P, MALIBU DESCR/OPERATIONFIGURE 7-7Trans

SECTION 7DESCR/OPERATION PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19997-14 REVISED: SEPTEMBER 10, 20017.8 TRANSICOIL ELECTRONIC MODULE

SECTION 1GENERAL PA-46-350P, MALIBUSECTION 1GENERAL PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19991-8REPORT: VB-1710 ISSUED: FEBRUARY 23,

SECTION 7 PA-46-350P, MALIBU DESCR/OPERATIONAs percent power is changed, a suggested approximate value for manifoldpressure and fuel flow will be disp

SECTION 7DESCR/OPERATION PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19997-167.8 TRANSICOIL ELECTRONIC MODULE INSTRUMENT SYSTEM(EMIS) (CON

The push button functions used to review the limitation exceedance eventsin the exceedance review mode "PEAK DISPLAY" are"1. Down Arro

SECTION 7DESCR/OPERATION PA-46-350P, MALIBUSECTION 7DESCR/OPERATION PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19997-18REPORT: VB-1710 ISS

SECTION 7PA-46-350P, MALIBU DESCR/OPERATIONSECTION 7PA-46-350P, MALIBU DESCR/OPERATIONISSUED: FEBRUARY 23, 1999 REPORT: VB-17107-19ISSUED: FEBRUARY 23

SECTION 7DESCR/OPERATION PA-46-350P, MALIBUSECTION 7DESCR/OPERATION PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19997-20REPORT: VB-1710 ISS

SECTION 7PA-46-350P, MALIBU DESCR/OPERATIONSECTION 7PA-46-350P, MALIBU DESCR/OPERATIONISSUED: FEBRUARY 23, 1999 REPORT: VB-17107-21ISSUED: FEBRUARY 23

SECTION 7DESCR/OPERATION PA-46-350P, MALIBUSECTION 7DESCR/OPERATION PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19997-22REPORT: VB-1710 ISS

SECTION 7DESCR/OPERATION PA-46-350P, MALIBUSECTION 7DESCR/OPERATION PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19997-24REPORT: VB-1710 ISS

SECTION 7PA-46-350P, MALIBU DESCR/OPERATIONSECTION 7PA-46-350P, MALIBU DESCR/OPERATIONISSUED: FEBRUARY 23, 1999 REPORT: VB-17107-25ISSUED: FEBRUARY 23

REPORT: VB-1710 ISSUED: FEBRUARY 23, 1999iiREPORT: VB-1710 ISSUED: FEBRUARY 23, 1999iiWARNINGEXTREME CARE MUST BE EXERCISED TO LIMIT THEUSE OF THIS HA

1.21 SYMBOLS, ABBREVIATIONS AND TERMINOLOGY (Continued)(b) Meteorological TerminologyISA International Standard Atmosphere inwhich:(1) The air is a dr

SECTION 7DESCR/OPERATION PA-46-350P, MALIBUSECTION 7DESCR/OPERATION PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19997-26REPORT: VB-1710 ISS

7.11 LANDING GEAR (continued)The landing gear is held in the DOWN position by spring loadedmechanical locking mechanisms built into each of the three

SECTION 7DESCR/OPERATION PA-46-350P, MALIBUSECTION 7DESCR/OPERATION PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19997-28REPORT: VB-1710 ISS

SECTION 7 PA-46-350P, MALIBU DESCR/OPERATION7.11 LANDING GEAR (Continued)CAUTION:When flying in extreme cold where the aircraft has been coldsoaked fo

SECTION 7DESCR/OPERATION PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19997-307.13 BRAKE SYSTEM (Continued)The parking brake knob is locate

7.17 FUEL SYSTEMFuel is stored in two main integral wing tanks (see Figure 7-27), locatedoutboard of the mid-wing splice. Fuel quantity held by each w

SECTION 7DESCR/OPERATION PA-46-350P, MALIBUSECTION 7DESCR/OPERATION PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19997-32REPORT: VB-1710 ISS

SECTION 7PA-46-350P, MALIBU DESCR/OPERATIONSECTION 7PA-46-350P, MALIBU DESCR/OPERATIONISSUED: FEBRUARY 23, 1999 REPORT: VB-17107-33ISSUED: FEBRUARY 23

SECTION 7DESCR/OPERATION PA-46-350P, MALIBUSECTION 7DESCR/OPERATION PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19997-34 REVISED: SEPTEMBER

7.17 FUEL SYSTEM (Continued)When beginning flight operations with an equal amount of fuel in eachtank, start, taxi, takeoff, and climb on the left ta

SECTION 1GENERAL PA-46-350P, MALIBUSECTION 1GENERAL PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19991-10REPORT: VB-1710 ISSUED: FEBRUARY 23

SECTION 7DESCR/OPERATION PA-46-350P, MALIBUSECTION 7DESCR/OPERATION PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19997-36REPORT: VB-1710 ISS

7.19 ELECTRICAL SYSTEM (Continued)When the Battery Master switch, located on the main switch panel, isturned ON, the battery solenoid contactor close

SECTION 7DESCR/OPERATION PA-46-350P, MALIBUSECTION 7DESCR/OPERATION PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19997-38 REVISED: SEPTEMBER

SECTION 7PA-46-350P, MALIBU DESCR/OPERATIONSECTION 7PA-46-350P, MALIBU DESCR/OPERATIONISSUED: FEBRUARY 23, 1999 REPORT: VB-17107-39ISSUED: FEBRUARY 23

SECTION 7DESCR/OPERATION PA-46-350P, MALIBUSECTION 7DESCR/OPERATION PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19997-40REPORT: VB-1710 ISS

SECTION 7PA-46-350P, MALIBU DESCR/OPERATIONSECTION 7PA-46-350P, MALIBU DESCR/OPERATIONISSUED: FEBRUARY 23, 1999 REPORT: VB-17107-41ISSUED: FEBRUARY 23

SECTION 7DESCR/OPERATION PA-46-350P, MALIBUSECTION 7DESCR/OPERATION PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19997-42REPORT: VB-1710 ISS

7.21 INSTRUMENT PANEL (Continued)An annunciator panel, located at the top of the left radio stack. Monitoredsystem includes:VACUUM NO. 1 INOP, VACUUM

SECTION 7DESCR/OPERATION PA-46-350P, MALIBUSECTION 7DESCR/OPERATION PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19997-44REPORT: VB-1710 ISS

SECTION 7PA-46-350P, MALIBU DESCR/OPERATIONSECTION 7PA-46-350P, MALIBU DESCR/OPERATIONISSUED: FEBRUARY 23, 1999 REPORT: VB-17107-45ISSUED: FEBRUARY 23

1.21 SYMBOLS, ABBREVIATIONS AND TERMINOLOGY (Continued)(f) Weight and Balance TerminologyReference Datum An imaginary vertical plane from which allhor

SECTION 7DESCR/OPERATION PA-46-350P, MALIBUSECTION 7DESCR/OPERATION PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19997-46REPORT: VB-1710 ISS

SECTION 7PA-46-350P, MALIBU DESCR/OPERATIONSECTION 7PA-46-350P, MALIBU DESCR/OPERATIONISSUED: FEBRUARY 23, 1999 REPORT: VB-17107-47ISSUED: FEBRUARY 23

SECTION 7DESCR/OPERATION PA-46-350P, MALIBUSECTION 7DESCR/OPERATION PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19997-48 REVISED: SEPTEMBER

The supplemental electric heater consists of a resistance type heatelement, a dual hermetically sealed bimetallic type overtemperatureprotection, a po

SECTION 7DESCR/OPERATION PA-46-350P, MALIBUSECTION 7DESCR/OPERATION PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19997-50 REVISED: SEPTEMBER

SECTION 7PA-46-350P, MALIBU DESCR/OPERATIONSECTION 7PA-46-350P, MALIBU DESCR/OPERATIONISSUED: FEBRUARY 23, 1999 REPORT: VB-17107-51ISSUED: FEBRUARY 23

SECTION 7DESCR/OPERATION PA-46-350P, MALIBUSECTION 7DESCR/OPERATION PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19997-52REPORT: VB-1710 ISS

SECTION 7PA-46-350P, MALIBU DESCR/OPERATIONSECTION 7PA-46-350P, MALIBU DESCR/OPERATIONISSUED: FEBRUARY 23, 1999 REPORT: VB-17107-53ISSUED: FEBRUARY 23

SECTION 7DESCR/OPERATION PA-46-350P, MALIBUSECTION 7DESCR/OPERATION PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19997-54REPORT: VB-1710 ISS

7.27 BLEED AIR, CONDITIONING AND PRESSURIZATION SYSTEM(Continued)For unpressurized flight the CABIN PRESS control should be pulledfully out. Setting t

SECTION 1GENERAL PA-46-350P, MALIBUSECTION 1GENERAL PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19991-12REPORT: VB-1710 ISSUED: FEBRUARY 23

SECTION 7DESCR/OPERATION PA-46-350P, MALIBUSECTION 7DESCR/OPERATION PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19997-56REPORT: VB-1710 ISS

SECTION 7PA-46-350P, MALIBU DESCR/OPERATIONSECTION 7PA-46-350P, MALIBU DESCR/OPERATIONISSUED: FEBRUARY 23, 1999 REPORT: VB-17107-57ISSUED: FEBRUARY 23

SECTION 7DESCR/OPERATION PA-46-350P, MALIBUSECTION 7DESCR/OPERATION PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19997-58REPORT: VB-1710 ISS

SECTION 7PA-46-350P, MALIBU DESCR/OPERATIONSECTION 7PA-46-350P, MALIBU DESCR/OPERATIONISSUED: FEBRUARY 23, 1999 REPORT: VB-17107-59ISSUED: FEBRUARY 23

SECTION 7DESCR/OPERATION PA-46-350P, MALIBUSECTION 7DESCR/OPERATION PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19997-60REPORT: VB-1710 ISS

7.39 EMERGENCY LOCATOR TRANSMITTERThe Emergency Locator Transmitter (ELT) meets the requirements ofFAR 91.52. It operates on self-contained batteries

SECTION 7DESCR/OPERATION PA-46-350P, MALIBUSECTION 7DESCR/OPERATION PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19997-62REPORT: VB-1710 ISS

7.43 RADAR*A weather radar system can be installed in the airplane. The basiccomponents of this installation are a Receiver-Transmitter Antenna and a

TABLE OF CONTENTSSECTION 8AIRPLANE HANDLING, SERVICING, AND MAINTNEANCEParagraph PageNo. No.8.1 General ...

SECTION 8AIRPLANE HANDLING, SERVICING, AND MAINTENANCE8.1 GENERALThis section provides guidelines relating to the handling, servicing, andmaintenance

TABLE OF CONTENTSSECTION 2 LIMITATIONSParagraph PageNo. No.2.1 General ...

SECTION 8HAND/SERV/MAINT PA-46-350P, MALIBUSECTION 8HAND/SERV/MAINT PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19998-1A REVISED: OCTOBER 1

8.1 GENERAL (CONTINUED)Every owner should stay in close contact with an authorized Piper ServiceCenter or Piper’s Customer Services Department to obta

SECTION 8HAND/SERV/MAINT PA-46-350P, MALIBUSECTION 8HAND/SERV/MAINT PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19998-2 REVISED: OCTOBER 14

8.3 AIRPLANE INSPECTION PERIODS (CONTINUED)A spectrographic analysis of the engine oil is available from severalsources. This inspection, if performe

SECTION 8HAND/SERV/MAINT PA-46-350P, MALIBUSECTION 8HAND/SERV/MAINT PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19998-4REPORT: VB-1710 ISSU

8.9 GROUND HANDLING (CONTINUED)by not less than fifteen feet, and a qualified person should ride in thepilot’s seat to maintain control by use of the

SECTION 8HAND/SERV/MAINT PA-46-350P, MALIBUSECTION 8HAND/SERV/MAINT PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19998-6REPORT: VB-1710 ISSU

8.9 GROUND HANDLING (CONTINUED)(6) Install a pitot head cover if available. Be sure to remove thepitot head cover before flight.(7) Cabin and baggage

SECTION 8HAND/SERV/MAINT PA-46-350P, MALIBUSECTION 8HAND/SERV/MAINT PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19998-8REPORT: VB-1710 ISSU

8.13 BRAKE SERVICE (CONTINUED)located behind the aft access panel in the forward baggage compartment. Ifthe entire system must be refilled, fill with

SECTION 2LIMITATIONS2.1 GENERALThis section provides the FAA Approved operating limitations,instrument markings, color coding and basic placards neces

SECTION 8HAND/SERV/MAINT PA-46-350P, MALIBUSECTION 8HAND/SERV/MAINT PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19998-10REPORT: VB-1710 ISS

SECTION 8PA-46-350P, MALIBU HAND/SERV/MAINTSECTION 8PA-46-350P, MALIBU HAND/SERV/MAINTISSUED: FEBRUARY 23, 1999 REPORT: VB-17108-11ISSUED: FEBRUARY 23

SECTION 8HAND/SERV/MAINT PA-46-350P, MALIBUSECTION 8HAND/SERV/MAINT PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19998-12REPORT: VB-1710 ISS

8.23 FUEL SYSTEM (CONTINUED)The operation of the aircraft is approved with an anti-icingadditive in the fuel. When an anti-icing additive is used it m

SECTION 8HAND/SERV/MAINT PA-46-350P, MALIBUSECTION 8HAND/SERV/MAINT PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19998-14REPORT: VB-1710 ISS

8.23 FUEL SYSTEM (CONTINUED)FUEL TANK DRAINFigure 8-3(e) Emptying Fuel SystemDrain the bulk of fuel at sump tanks. Set fuel selector on left orright t

SECTION 8HAND/SERV/MAINT PA-46-350P, MALIBUSECTION 8HAND/SERV/MAINT PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19998-16REPORT: VB-1710 ISS

8.33 LUBRICATIONFor lubricating instructions, a chart showing lubrication points and types oflubricants to be used, and lubrication methods, refer to

SECTION 8HAND/SERV/MAINT PA-46-350P, MALIBUSECTION 8HAND/SERV/MAINT PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19998-18REPORT: VB-1710 ISS

8.35 CLEANING (CONTINUED)(d) Cleaning Windshield and WindowsCAUTIONUse only mild soap and water when cleaning theheated windshield. Use of ANY other c

SECTION 2LIMITATIONS PA-46-350P, MALIBUSECTION 2LIMITATIONS PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19992-2REPORT: VB-1710 ISSUED: FEBR

SECTION 8HAND/SERV/MAINT PA-46-350P, MALIBUSECTION 8HAND/SERV/MAINT PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19998-20REPORT: VB-1710 ISS

8.35 CLEANING (CONTINUED)airplane. If difficulty is encountered with the water freezing onboots, direct a blast of warm air along the region being cle

SECTION 8HAND/SERV/MAINT PA-46-350P, MALIBUSECTION 8HAND/SERV/MAINT PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19998-22REPORT: VB-1710 ISS

(b) ExteriorExterior bottom painted surfaces of the aircraft must be cleanedfrom the firewall to the tip of the tail including the bottom of the tails

SECTION 9 PA-46-350P, MALIBU SUPPLEMENTSTABLE OF CONTENTSSECTION 9SUPPLEMENTSParagraph/Supplement PageNo. No.9.1 General ...

SECTION 9SUPPLEMENTS PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19999-ii REVISED: JANUARY 20, 2004SECTION 9SUPPLEMENTS PA-46-350P, MALIBUR

SECTION 9SUPPLEMENTS9.1 GENERALThis section provides information in the form of supplements which arenecessary for efficient operation of the airplane

PILOT’S OPERATING HANDBOOKANDFAA APPROVED AIRPLANE FLIGHT MANUALSUPPLEMENT NO. 1FOREMERGENCY OXYGEN SYSTEMThis supplement must be attached to the Pilo

SECTION 9SUPPLEMENT 1 PA-46-350P, MALIBUSECTION 9SUPPLEMENT 1 PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19999-4, 2 of 6REPORT: VB-1710

SECTION 3 - EMERGENCY PROCEDURESIn the event that the emergency oxygen system is needed, proceed asfollows:Mask compartment(s)...

2.7 POWER PLANT LIMITATIONS(a) Number of Engines 1(b) Engine Manufacturer Textron Lycoming(c) Engine Model No. TIO-540-AE2A(d) Engine Operating Limits

SECTION 9SUPPLEMENT 1 PA-46-350, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19999-6, 4 of 6SECTION 4 - NORMAL PROCEDURESPrior to each flight, turn

The crew assembly is located under the copilot’s seat and contains onetwo-man oxygen generator and two masks mounted on a sliding tray. Thetray is acc

SECTION 9SUPPLEMENT 1 PA-46-350P, MALIBUSECTION 9SUPPLEMENT 1 PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19999-8, 6 of 6REPORT: VB-1710

PILOT’S OPERATING HANDBOOKANDFAA APPROVED AIRPLANE FLIGHT MANUALSUPPLEMENT NO. 2FORPROPELLER HEAT, HEATED WINDSHIELD ANDWING ICE DETECTION LIGHTThis s

SECTION 9SUPPLEMENT 2 PA-46-350P, MALIBUSECTION 9SUPPLEMENT 2 PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19999-10, 2 of 6 REVISED: SEPT

When in visible moisture at temperatures at or below +5°C and icingconditions are anticipated, turn on the windshield heat LO switch. If lowwindshield

SECTION 9SUPPLEMENT 2 PA-46-350P, MALIBUSECTION 9SUPPLEMENT 2 PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19999-12, 4 of 6REPORT: VB-171

ELECTRIC HEATED WINDSHIELDWARNINGFlight into known or forecast icing is notapproved. If icing is encountered, take avoidanceaction immediately.The ele

PILOT’S OPERATING HANDBOOKANDFAA APPROVED AIRPLANE FLIGHT MANUALSUPPLEMENT NO. 3FORICE PROTECTION SYSTEM(APPROVED FOR FLIGHT INTO KNOWN ICING CONDITIO

SECTION 9SUPPLEMENT 3 PA-46-350P, MALIBUSECTION 9SUPPLEMENT 3 PA-46-350P, MALIBUREPORT:-1710 ISSUED: FEBRUARY 23, 19999-16, 2 of 16REPORT:-1710 ISS

SECTION 2LIMITATIONS PA-46-350P, MALIBUSECTION 2LIMITATIONS PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19992-4REPORT: VB-1710 ISSUED: FEBR

SECTION 3 - EMERGENCY PROCEDURESWARNINGThe malfunction of any required deice equipmentrequires immediate action to exit icing conditions.Depending on

SECTION 9SUPPLEMENT 3 PA-46-350P, MALIBUSECTION 9SUPPLEMENT 3 PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19999-18, 4 of 16REPORT: VB-17

SURFACE DEICE MALFUNCTIONIf SURFACE DE-ICE annunciator light remains illuminated more than 30seconds, pull the surface deice circuit breaker. Immediat

SECTION 9SUPPLEMENT 3 PA-46-350P, MALIBUSECTION 9SUPPLEMENT 3 PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19999-20, 6 of 16REPORT: VB-17

IN FLIGHTIcing conditions of any kind should be avoided whenever possible, sinceany minor malfunction which may occur is potentially more serious in i

SECTION 9SUPPLEMENT 3 PA-46-350P, MALIBUSECTION 9SUPPLEMENT 3 PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19999-22, 8 of 16REPORT: VB-17

SECTION 5 - PERFORMANCEClimb speed should be increased to 130 knots when icing conditions areencountered during climb.Cruise speeds are reduced approx

SECTION 9SUPPLEMENT 3 PA-46-350P, MALIBUSECTION 9SUPPLEMENT 3 PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19999-24, 10 of 16 REVISED: SE

deice flow valves for approximately six seconds. The boot solenoid valves areactivated and air pressure is released to the boots, sequentially inflati

SECTION 9SUPPLEMENT 3 PA-46-350P, MALIBUSECTION 9SUPPLEMENT 3 PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19999-26, 12 of 16REPORT: VB-1

2.13 WEIGHT LIMITS(a) Maximum Ramp Weight 4358 LB(b) Maximum Takeoff Weight 4340 LB(c) Maximum Landing Weight 4123 LB(d) Maximum Zero Fuel Weight 4123

HEATED PITOT HEADA heated AN type head is installed under the the wing. It is controlled byan ON-OFF type PITOT HEAT switch located on the switch pane

SECTION 9SUPPLEMENT 3 PA-46-350P, MALIBUSECTION 9SUPPLEMENT 3 PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19999-28, 14 of 16REPORT: VB-1

SECTION 9PA-46-350P, MALIBU SUPPLEMENT 3SECTION 9PA-46-350P, MALIBU SUPPLEMENT 3ISSUED: FEBRUARY 23, 1999 REPORT: VB-171015 of 16, 9-29ISSUED: FE

SECTION 9PA-46-350P, MALIBU SUPPLEMENT 4PILOT’S OPERATING HANDBOOKANDFAA APPROVED AIRPLANE FLIGHT MANUALSUPPLEMENT NO. 4FORB.F. GOODRICH INTEGRATED IC

SECTION 9SUPPLEMENT 4 PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19999-32, 2 of 4 REVISED: SEPTEMBER 10, 2001SECTION 1 - GENERALThis su

IN FLIGHT (Cont’d)If the ice is removed from the empennage following inflation, the “deice”annunciator will extinguish. If less than 90% of the ice c

SECTION 9SUPPLEMENT 4 PA-46-350P, MALIBUSECTION 9SUPPLEMENT 4 PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19999-34, 4 of 4REPORT: VB-1710

PILOT’S OPERATING HANDBOOKSUPPLEMENT NO. 5FORKING 150 SERIES FLIGHT CONTROL SYSTEMThis supplement has been DELETED as the FAA Approved OperationalSupp

PILOT’S OPERATING HANDBOOKANDFAA APPROVED AIRPLANE FLIGHT MANUALSUPPLEMENT NO. 6FORKING KAS 297B VERTICAL SPEED AND ALTITUDE SELECTORThis supplement h

PILOT’S OPERATING HANDBOOKANDFAA APPROVED AIRPLANE FLIGHT MANUALSUPPLEMENT 7FOR3M (SERIES II) STORMSCOPE, WX-1000/WX-1000+This supplement must be atta

PA-46-350P, MALIBUAPPLICABILITYApplication of this handbook is limited to the specific Piper PA-46-350Pmodel airplane designated by serial number and

SECTION 2LIMITATIONS PA-46-350P, MALIBUSECTION 2LIMITATIONS PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19992-6REPORT: VB-1710 ISSUED: FEBR

SECTION 9SUPPLEMENT 7 PA-46-350P, MALIBUSECTION 9SUPPLEMENT 7 PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19999-40, 2 of 4REPORT: VB-171

SECTION 5 - PERFORMANCENo change.SECTION 6 - WEIGHT AND BALANCEFactory installed optional equipment is included in the licensed weightand balance data

SECTION 9SUPPLEMENT 7 PA-46-350P, MALIBUSECTION 9SUPPLEMENT 7 PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19999-42, 4 of 4REPORT: VB-171

PILOT’S OPERATING HANDBOOKANDFAA APPROVED AIRPLANE FLIGHT MANUALSUPPLEMENT NO. 8FORBENDIX/KING EHI 40This supplement must be attached to the Pilot’s O

SECTION 9SUPPLEMENT 8 PA-46-350P, MALIBUSECTION 9SUPPLEMENT 8 PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19999-44 2 of 26REPORT: VB-17

SECTION 1 - GENERAL (Continued)NAV NavigationNM Nautical MilesRNAV Area NavigationSTBY StandbyTST TestVAR VariationVOR Very High Frequency Omni RangeS

SECTION 9SUPPLEMENT 8 PA-46-350P, MALIBUSECTION 9SUPPLEMENT 8 PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19999-46 4 of 26REPORT: VB-171

SECTION 3 - EMERGENCY PROCEDURES (continued)RED HDG ANNUNCIATIONRed HDG annunciation indicates a failure in the compass system byremoving the lubber l

SECTION 9SUPPLEMENTM 8 PA-46-350P, MALIBUSECTION 9SUPPLEMENT 8 PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19999-48, 6 of 26REPORT: VB-1

SECTION 3 - EMERGENCY PROCEDURES (continued)YELLOW DU ANNUNCIATIONYellow DU annunciation indicates a failure of the EHSI cooling fan. If afan failure

SECTION 2PA-46-350P, MALIBU LIMITATIONSSECTION 2PA-46-350P, MALIBU LIMITATIONSISSUED: FEBRUARY 23, 1999 REPORT: VB-17102-7ISSUED: FEBRUARY 23, 1999

SECTION 9SUPPLEMENT 8 PA-46-350P, MALIBUSECTION 9SUPPLEMENT 8 PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19999-50, 8 of 26REPORT: VB-17

SECTION 5 - PERFORMANCENo changes.SECTION 6 - WEIGHT AND BALANCEFactory installed optional equipment is included in the licensed weight andbalance dat

SECTION 9SUPPLEMENT 8 PA-46-350P, MALIBUSECTION 9SUPPLEMENT 8 PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19999-52 10 of 26REPORT: VB-17

SECTION 7 - DESCRIPTION AND OPERATION (Continued)3. NUMBER 1 SYSTEM BEARING POINTER SELECT - The bearingpointer select button works similar to the NAV

SECTION 9SUPPLEMENT 8 PA-46-350P, MALIBUSECTION 9SUPPLEMENT 8 PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19999-54 12 of 26REPORT: VB-17

SECTION 7 - DESCRIPTION AND OPERATION (Continued)7. RANGE SELECTIONRANGE DOWN - A press of the RANGE DOWN button selects thenext lower range to be dis

SECTION 9SUPPLEMENT 8 PA-46-350P, MALIBUSECTION 9SUPPLEMENT 8 PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19999-56 14 of 26REPORT: VB-17

SECTION 9PA-46-350P, MALIBU SUPPLEMENT 8SECTION 9PA-46-350P, MALIBU SUPPLEMENT 8ISSUED: FEBRUARY 23, 1999 REPORT: VB-171015 of 26 9-57ISSUED: FEBRU

SECTION 9SUPPLEMENT 8 PA-46-350P, MALIBUSECTION 9SUPPLEMENT 8 PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19999-58 16 of 26REPORT: VB-17

SECTION 7 - DESCRIPTION AND OPERATION (Continued)4. Heading Select BugA notched orange heading bug is manually rotated around thecompass scale by the

SECTION 2LIMITATIONS PA-46-350P, MALIBUSECTION 2LIMITATIONS PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19992-8REPORT: VB-1710 ISSUED: FEBR

SECTION 9SUPPLEMENT 8 PA-46-350P, MALIBUSECTION 9SUPPLEMENT 8 PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19999-60 18 of 26 REPORT: VB

SECTION 7 - DESCRIPTION AND OPERATION (Continued)9. Distance and Ground Speed Display (continued)When the selected bearing pointer source has DME data

SECTION 9SUPPLEMENT 8 PA-46-350P, MALIBUSECTION 9SUPPLEMENT 8 PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19999-62 20 of 26REPORT: VB-171

SECTION 9PA-46-350P, MALIBU SUPPLEMENT 8SECTION 9PA-46-350P, MALIBU SUPPLEMENT 8ISSUED: FEBRUARY 23, 1999 REPORT: VB-171021 of 26 9-63ISSUED: FEBRU

SECTION 9SUPPLEMENT 8 PA-46-350P, MALIBUSECTION 9SUPPLEMENT 8 PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19999-64 22 of 26REPORT: VB-171

SECTION 7 - DESCRIPTION AND OPERATION (Continued)MAP DISPLAY (refer to figure 7-7)The EHI 40 provides two basic types of map; a 360 degree map display

SECTION 9SUPPLEMENT 8 PA-46-350P, MALIBUSECTION 9SUPPLEMENT 8 PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19999-66 24 of 26REPORT: VB-17

SECTION 7 - DESCRIPTION AND OPERATION (Continued)9. MAP Weather Radar Information - Four data lines are reserved belowthe primary NAV sensor source an

SECTION 9SUPPLEMENT 8 PA-46-350P, MALIBUSECTION 9SUPPLEMENT 8 PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19999-68 26 of 26REPORT: VB-17

PILOT’S OPERATING HANDBOOKANDFAA APPROVED AIRPLANE FLIGHT MANUALSUPPLEMENT NO. 9FORBENDIX/KING RDR 2000 VERTICAL PROFILEWEATHER RADAR SYSTEMThis suppl

SECTION 2PA-46-350P, MALIBU LIMITATIONSSECTION 2PA-46-350P, MALIBU LIMITATIONSISSUED: FEBRUARY 23, 1999 REPORT: VB-17102-9ISSUED: FEBRUARY 23, 1999 RE

SECTION 9SUPPLEMENT 9 PA-46-350P, MALIBUSECTION 9SUPPLEMENT 9 PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19999-70 2 of 10 REPORT: VB-1

SECTION 5 - PERFORMANCEWhen the radar pod is installed:a. The rate of climb is decreased approximately 50 fpm.b. The cruise speed is decreased approxi

SECTION 9SUPPLEMENT 9 PA-46-350P, MALIBUSECTION 9SUPPLEMENT 9 PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19999-72 4 of 10 REPORT: VB-17

SECTION 9PA-46-350P, MALIBU SUPPLEMENT 9SECTION 9PA-46-350P, MALIBU SUPPLEMENT 9ISSUED: FEBRUARY 23, 1999 REPORT: VB-17105 of 10 9-73ISSUED: FEBRUARY

SECTION 9SUPPLEMENT 9 PA-46-350P, MALIBUSECTION 9SUPPLEMENT 9 PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19999-74 6 of 10 REPORT: VB-1

SECTION 9PA-46-350P, MALIBU SUPPLEMENT 9SECTION 9PA-46-350P, MALIBU SUPPLEMENT 9ISSUED: FEBRUARY 23, 1999 REPORT: VB-17107 of 10 9-75ISSUED: FEBRUARY

SECTION 9SUPPLEMENT 9 PA-46-350P, MALIBUSECTION 9SUPPLEMENT 9 PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19999-76 8 of 10 REPORT: VB-1

SECTION 9PA-46-350P, MALIBU SUPPLEMENT 9SECTION 9PA-46-350P, MALIBU SUPPLEMENT 9ISSUED: FEBRUARY 23, 1999 REPORT: VB-17109 of 10, 9-77ISSUED: FEBR

SECTION 9SUPPLEMENT 9 PA-46-350P, MALIBUSECTION 9SUPPLEMENT 9 PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19999-78, 10 of 10REPORT: VB-

PILOT'S OPERATING HANDBOOKANDFAA APPROVED AIRPLANE FLIGHT MANUALSUPPLEMENT 10FORARGUS 7000CE MOVING MAP DISPLAYThis supplement must be attached t

SECTION 2LIMITATIONS PA-46-350P, MALIBUSECTION 2LIMITATIONS PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19992-10REPORT: VB-1710 ISSUED: FEB

SECTION 9SUPPLEMENT 10 PA-46-350P, MALIBUSECTION 9SUPPLEMENT 10 PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19999-80, 2 of 8REPORT: VB-

conducting a precision approach to, or departure from, a landingfacility.f. When using the ADF bearing pointer for navigation in the map andplan submo

SECTION 9SUPPLEMENT 10 PA-46-350P, MALIBUSECTION 9SUPPLEMENT 10 PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19999-82, 4 of 8REPORT: VB-

SECTION 7 - DESCRIPTION AND OPERATION (Continued)(2) In addition, the Software Program VERsion will appear on theDisclaimer Page, which will remain in

SECTION 9SUPPLEMENT 10 PA-46-350P, MALIBUSECTION 9SUPPLEMENT 10 PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19999-84, 6 of 8REPORT: VB-

SECTION 7 - DESCRIPTION AND OPERATION (Continued)d. ADF Bearing Pointer and Digital ADF Bearing Procedures.(1) In the DEParture or ENRoute modes, when

PILOT’S OPERATING HANDBOOKANDFAA APPROVED AIRPLANE FLIGHT MANUALSUPPLEMENT NO. 11FORBENDIX/KING KLN 90B GPSNAVIGATION SYSTEM WITH KAP/KFC 150 or 225 A

SECTION 9SUPPLEMENT 11 PA-46-350P, MALIBUSECTION 9SUPPLEMENT 11 PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19999-88, 2 of 12,REPORT

SECTION 2 - LIMITATIONSA. The KLN 90B GPS Pilot’s Guide, P/N 006-08773-0000, datedDecember, 1994 (or later applicable revision) must be immediatelyava

SECTION 9SUPPLEMENT 11 PA-46-350P, MALIBUSECTION 9SUPPLEMENT 11 PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19999-90, 4 of 12,REPORT

SECTION 2PA-46-350P, MALIBU LIMITATIONSSECTION 2PA-46-350P, MALIBU LIMITATIONSISSUED: FEBRUARY 23, 1999 REPORT: VB-17102-11ISSUED: FEBRUARY 23, 1999 R

SECTION 4 - NORMAL PROCEDURES (CONT'D)3. Waypoint (WPT) annunciator - Prior to reaching a waypoint in the active flight plan, the KLN 90B GPS wil

SECTION 9SUPPLEMENT 11 PA-46-350P, MALIBUSECTION 9SUPPLEMENT 11 PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19999-92, 6 of 12,REPORT

SECTION 4 - NORMAL PROCEDURES (CONT'D)E. APPROACH MODE SEQUENCING AND RAIM PREDICTIONNOTEThe special use airspace alert willautomatically be disa

SECTION 9SUPPLEMENT 11 PA-46-350P, MALIBUSECTION 9SUPPLEMENT 11 PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19999-94, 8 of 12REPORT:

SECTION 9PA-46-350P, MALIBU SUPPLEMENT 11SECTION 9PA-46-350P, MALIBU SUPPLEMENT 11ISSUED: FEBRUARY 23, 1999 REPORT: VB-17109 of 12, 9-95ISSUED: FEB

SECTION 9SUPPLEMENT 11 PA-46-350P, MALIBUSECTION 9SUPPLEMENT 11 PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19999-96, 10 of 12REPORT: VB

SECTION 4 - NORMAL PROCEDURES (CONT'D• APR ARM to APR ACTV is automaticprovided: a. You are in APR ARM (normallyautomatic).b. You are in LEG mo

PILOT'S OPERATING HANDBOOKANDFAA APPROVED AIRPLANE FLIGHT MANUALSUPPLEMENT NO. 12FORBENDIX/KING KX 155A COMM/NAV SYSTEMThis supplement must be at

SECTION 9SUPPLEMENT 12 PA-46-350P, MALIBUSECTION 9SUPPLEMENT 12 PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19999-100, 2 of 12REPORT: V

SECTION 7 DESCRIPTION & OPERATIONGENERALAll controls required to operate the KX 155A/165A are located on the unit front panel. (See Figure 3-1.)

SECTION 2LIMITATIONS PA-46-350P, MALIBUSECTION 2LIMITATIONS PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19992-12REPORT: VB-1710 ISSUED: FEB

SECTION 9SUPPLEMENT 12 PA-46-350P, MALIBUSECTION 9SUPPLEMENT 12 PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19999-102, 4 of 12REPORT: V

The KX 155A also has provision to program 32 channels. Pressing the CHANbutton for 2 or more seconds will cause the unit to enter the channel programm

SECTION 9SUPPLEMENT 12 PA-46-350P, MALIBUSECTION 9SUPPLEMENT 12 PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19999-104, 6 of 12REPORT: V

FIGURE 3-3 NAV DISPLAY; ACTIVE LOCALIZER FREQUENCY/CDI FORMATWhen the received signal is too weak to ensure accuracy the display will“flag”. See Figur

SECTION 9SUPPLEMENT 12 PA-46-350P, MALIBUSECTION 9SUPPLEMENT 12 PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19999-106, 8 of 12REPORT: V

Another push of the mode button will cause the NAV display to go from theACTIVE/BEARING format to the ACTIVE/RADIAL format as shown inFigure 3-7. In t

SECTION 9SUPPLEMENT 12 PA-46-350P, MALIBUSECTION 9SUPPLEMENT 12 PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19999-108, 10 of 12REPORT:

PILOT CONFIGURATIONThis mode can be accessed by pressing and holding the Nav Mode Button formore than 2 seconds and then pressing the Nav Frequency Tr

PILOT’S OPERATING HANDBOOKSUPPLEMENT NO. 13FORPRECISE FLIGHT SPEEDBRAKE 2000This supplement has been DELETED as the FAA Approved OperationalSupplement

PILOT’S OPERATING HANDBOOKSUPPLEMENT NO. 14FORBENDIX/KING KFC 225 FLIGHT CONTROL SYSTEMThis supplement has been DELETED as the FAA Approved Operationa

2.33 MAXIMUM SEATING CONFIGURATIONThe maximum seating capacity is 6 (six) persons.2.34 ICING INFORMATION"WARNING"Severe icing may result fr

SECTION 9PA-46-350P, MALIBU SUPPLEMENT 15PILOT’S OPERATING HANDBOOKANDFAA APPROVED AIRPLANE FLIGHT MANUALSUPPLEMENT NO. 15FORGARMIN GNS 430 VHF COMMUN

SECTION 9SUPPLEMENT 15 PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19999-116 2 of 8 REVISED: DECEMBER 20, 2001SECTION 1 - GENERALThe

SECTION 9PA-46-350P, MALIBU SUPPLEMENT 15SECTION 2 - LIMITATIONSA. The GARMIN GNS 430 Pilot’s Guide, p/n 190-00140-00, Rev. A, datedOctober 1998, or l

SECTION 9SUPPLEMENT 15 PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19999-118 4 of 8 REVISED: SEPTEMBER 10, 2001SECTION 2 - LIMITATIO

SECTION 3 - EMERGENCY PROCEDURESABNORMAL PROCEDURESA. If GARMIN GNS 430 navigation information is not available or invalid,utilize remaining operation

SECTION 9SUPPLEMENT 15 PA-46-350P, MALIBUSECTION 9SUPPLEMENT 15 PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19999-120 6 of 8 REVISED

SECTION 5 - PERFORMANCENo change.SECTION 6 - WEIGHT AND BALANCEFactory installed optional equipment is included in the licensed weight andbalance data

PILOT'S OPERATING HANDBOOKANDFAA APPROVED AIRPLANE FLIGHT MANUALSUPPLEMENT NO. 16FORS-TEC SYSTEM 55 TWO AXISAUTOMATIC FLIGHT GUIDANCE SYSTEMWITH

SECTION 9PA-46-350P, MALIBU SUPPLEMENT 17PILOT’S OPERATING HANDBOOKANDFAA APPROVED AIRPLANE FLIGHT MANUALSUPPLEMENT NO. 17FORGARMIN GNS 530 VHF COMMUN

SECTION 9SUPPLEMENT 17 PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19999-126 2 of 8 REVISED: SEPTEMBER 10, 2001SECTION 1 - GENERALTh

SECTION 2LIMITATIONS PA-46-350P, MALIBUSECTION 2LIMITATIONS PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19992-14 REVISED: NOVEMBER 12, 1999

SECTION 9PA-46-350P, MALIBU SUPPLEMENT 17ISSUED: FEBRUARY 23, 1999 REPORT: VB-1710REVISED: SEPTEMBER 10, 2001 3 of 8, 9-127SECTION 9PA-46-350P, MA

SECTION 9SUPPLEMENT 17 PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19999-128 4 of 8 REVISED: SEPTEMBER 10, 2001SECTION 2 - LIMITATIO

SECTION 9PA-46-350P, MALIBU SUPPLEMENT 17SECTION 3 - EMERGENCY PROCEDURESABNORMAL PROCEDURESA. If GARMIN GNS 530 navigation information is not availab

SECTION 9SUPPLEMENT 17 PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19999-130 6 of 8 REVISED: SEPTEMBER 10, 2001SECTION 4 - NORMAL PR

SECTION 9PA-46-350P, MALIBU SUPPLEMENT 17SECTION 4 - NORMAL PROCEDURES (continued)E. AUTOMATIC LOCALIZER COURSE CAPTUREBy default, the GNS 530 autom

SECTION 9PA-46-350P, MALIBU SUPPLEMENT 18PILOT’S OPERATING HANDBOOKANDFAA APPROVED AIRPLANE FLIGHT MANUALSUPPLEMENT NO. 18FORGARMIN GTX 327 TRANSPONDE

SECTION 9SUPPLEMENT 18 PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19999-134 2 of 10 REVISED: SEPTEMBER 10, 2001SECTION 1 - GENERALT

SECTION 9PA-46-350P, MALIBU SUPPLEMENT 18ISSUED: FEBRUARY 23, 1999 REPORT: VB-1710REVISED: SEPTEMBER 10, 2001 3 of 10, 9-135SECTION 9PA-46-350P, M

SECTION 9SUPPLEMENT 18 PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19999-136 4 of 10 REVISED: SEPTEMBER 10, 2001SECTION 9SUPPLEMENT

SECTION 9PA-46-350P, MALIBU SUPPLEMENT 18ISSUED: FEBRUARY 23, 1999 REPORT: VB-1710REVISED: SEPTEMBER 10, 2001 5 of 10, 9-137SECTION 9PA-46-350P, M

SECTION 2PA-46-350P, MALIBU LIMITATIONS2.35 PLACARDS (CONTINUED)Near the magnetic compass:CAUTION - COMPASS CAL. MAY BE INERROR WITH ELECT. EQUIPMENTO

SECTION 9SUPPLEMENT 18 PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19999-138 6 of 10 REVISED: SEPTEMBER 10, 2001SECTION 9SUPPLEMENT

SECTION 9PA-46-350P, MALIBU SUPPLEMENT 18ISSUED: FEBRUARY 23, 1999 REPORT: VB-1710REVISED: SEPTEMBER 10, 2001 7 of 10, 9-139SECTION 9PA-46-350P, M

SECTION 9SUPPLEMENT 18 PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19999-140 8 of 10 REVISED: SEPTEMBER 10, 2001SECTION 7 - DESCRIPT

SECTION 9PA-46-350P, MALIBU SUPPLEMENT 18SECTION 7 - DESCRIPTION AND OPERATION (continued)Automatic ALT/STBY Mode SwitchingIf the GTX 327 is configure

PILOT’S OPERATING HANDBOOKANDFAA APPROVED AIRPLANE FLIGHT MANUALSUPPLEMENT NO. 19FORAVIDYNE 5RR-MFC-SERIESFLIGHTMAX FLIGHT SITUATION DISPLAYThis suppl

SECTION 1 - GENERALNOTEFlightMax 700 FSD is a radar indicator only and does nothave functionality for Navigator, Lightning, Charts, orTraffic. The Fli

SECTION 3 - EMERGENCY PROCEDURESThere is no change to the aircraft emergency procedures with this equipmentinstalled.SECTION 4 - NORMAL PROCEDURESNorm

SECTION 7 - DESCRIPTION AND OPERATION (CONTINUED)AVIDYNE NAVIGATOR (FlightMax 750 FSD only) (continued)Navigator displays real-time navigation data s

SECTION 7 - DESCRIPTION AND OPERATION (CONTINUED)AVIDYNE LIGHTNING (FlightMax 750 FSD only)Avidyne Lightning displays weather avoidance data gathered

SECTION 7 - DESCRIPTION AND OPERATION (CONTINUED)AVIDYNE CHARTS (FlightMax 750 FSD only)Avidyne Charts is a moving map display. Interfacing with an o

PA-46-350P, MALIBUREVISIONSThe information compiled in the Pilot’s Operating Handbook, with theexception of the equipment list, will be kept current b

SECTION 2LIMITATIONS PA-46-350P, MALIBU2.35 PLACARDS (CONTINUED)Over emergency exit handle:EMERGENCY EXITREMOVE GLASSPULL DOOR IN - LIFT UPOn aft bagg

SECTION 7 - DESCRIPTION AND OPERATION (CONTINUED)DATABASE UPDATESAvidyne Navigator is intended for use as an enhanced human interface to avariety of

PILOT’S OPERATING HANDBOOKANDFAA APPROVED AIRPLANE FLIGHT MANUALSUPPLEMENT NO. 20FORB.F. GOODRICHSKYWATCH TRAFFIC ADVISORY SYSTEMMODEL SKY497This supp

SECTION 1 - GENERALThe SKYWATCH system is an on-board traffic advisory system whichmonitors a radius of nominally 6 nautical miles about the aircraft

SECTION 2 - LIMITATIONSInformation shown on the display is provided to the pilot as an aid tovisually acquiring traffic. Pilot’s should maneuver their

SECTION 4 - NORMAL PROCEDURES (continued)SELF TEST (continued)If “TRAFFIC ADVISORY SYSTEM TEST FAILED” is heard or theSKY497 FAILED screen appears,

SECTION 4 - NORMAL PROCEDURES (continued)ABNORMAL PROCEDURESIf “TRAFFIC ADVISORY SYSTEM TEST FAILED” is heard or theSKY497 FAILED screen appears, the

PILOT’S OPERATING HANDBOOKANDFAA APPROVED AIRPLANE FLIGHT MANUALSUPPLEMENT NO. 21FORBF GOODRICH AEROSPACEWX-500 STORMSCOPE - SERIES II WEATHER MAPPING

SECTION 1 - GENERALThis supplement provides information necessary for the operation of theaircraft with the BF Goodrich WX-500 Stormscope.WARNINGNever

SECTION 4 - NORMAL PROCEDURESNormal operating procedures are described in the BF Goodrich AerospaceWX-500 Stormscope Users Guide, p/n 009-11501-001, R

SECTION 9PA-46-350P, MALIBU SUPPLEMENT 22PILOT'S OPERATING HANDBOOKANDFAA APPROVED AIRPLANE FLIGHT MANUALSUPPLEMENT NO. 22FORMEGGITT ELECTRONIC F

TABLE OF CONTENTSSECTION 3EMERGENCY PROCEDURESParagraph PageNo. No.3.1 General ...

SECTION 9PA-46-350P, MALIBU SUPPLEMENT 23PILOT’S OPERATING HANDBOOKANDFAA APPROVED AIRPLANE FLIGHT MANUALSUPPLEMENT NO. 23FORBENDIX/KING KMH 880MULTI-

SECTION 9 PA-46-350P, MALIBU SUPPLEMENT 24 ISSUED: FEBRUARY 23, 1999 REPORT: VB-1710REVISED: JANUARY 20, 2004 1 of 4, 9-165PILOT’S OPERATING HANDBOOKA

SECTION 9SUPPLEMENT 24 PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19999-166, 2 of 4 REVISED: JANUARY 20, 2004SECTION 1 - GENERALThis suppl

SECTION 9 PA-46-350P, MALIBU SUPPLEMENT 24 ISSUED: FEBRUARY 23, 1999 REPORT: VB-1710REVISED: JANUARY 20, 2004 3 of 4, 9-167SECTION 4 - NORMAL PROCEDUR

SECTION 9SUPPLEMENT 24 PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19999-168, 4 of 4 REVISED: JANUARY 20, 2004SECTION 5 - PERFORMANCENo cha

TABLE OF CONTENTSSECTION 10 OPERATING TIPSParagraph PageNo. No.10.1 General ...

SECTION 10OPERATING TIPS10.1 GENERALThis section provides operating tips of particular value in the operationof the Malibu.10.3 OPERATING TIPS(a) Lear

SECTION 10OPERATING TIPS PA-46-350P, MALIBUSECTION 10OPERATING TIPS PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 199910-2REPORT: VB-1710 ISS

REPORT: VB-1710 ISSUED: FEBRUARY 23, 19993-iiREPORT: VB-1710 ISSUED: FEBRUARY 23, 19993-iiTABLE OF CONTENTSSECTION 3 (cont)EMERGENCY PROCEDURESParagra

TABLE OF CONTENTSSECTION 3 (cont)EMERGENCY PROCEDURESParagraph PageNo. No.3.45 Inadvertent Icing Encounter (3.3v) ...

SECTION 3EMERGENCY PROCEDURES3.1 GENERALThis section provides the recommended procedures for coping withvarious emergency or critical situations. All

SECTION 3EMERG PROCEDURES PA-46-350P, MALIBUSECTION 3EMERG PROCEDURES PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19993-2REPORT: VB-1710 IS

3.3b TURBOCHARGER FAILURE (3.8) (Cont’d)PARTIAL LOSS OF ENGINE POWERIf the turbocharger wastegate fails in the OPEN position, a partial loss ofengine

SECTION 3EMERG PROCEDURES PA-46-350P, MALIBUSECTION 3EMERG PROCEDURES PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19993-4REPORT: VB-1710 IS

SECTION 3PA-46-350P, MALIBU EMERG PROCEDURESSECTION 3PA-46-350P, MALIBU EMERG PROCEDURESISSUED: FEBRUARY 23, 1999 REPORT: VB-17103-5ISSUED: FEBRUARY 2

SECTION 3EMERG PROCEDURES PA-46-350P, MALIBUSECTION 3EMERG PROCEDURES PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19993-6REPORT: VB-1710 IS

PA-46-350P, MALIBUPILOT'S OPERATING HANDBOOK LOG OF REVISIONSPA-46-350P, MALIBUPILOT'S OPERATING HANDBOOK LOG OF REVISIONSISSUED: FEBRUARY 2

SECTION 3PA-46-350P, MALIBU EMERG PROCEDURESSECTION 3PA-46-350P, MALIBU EMERG PROCEDURESISSUED: FEBRUARY 23, 1999 REPORT: VB-17103-7ISSUED: FEBRUARY 2

SECTION 3EMERG PROCEDURES PA-46-350P, MALIBUSECTION 3EMERG PROCEDURES PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19993-8REPORT: VB-1710 IS

SECTION 3PA-46-350P, MALIBU EMERG PROCEDURES3.3k TURBINE INLET TEMPERATURE (TIT) INDICATOR FAILURE(3.24)If failure occurs during takeoff, climb, or la

SECTION 3EMERG PROCEDURES PA-46-350P, MALIBU3.3l HIGH CYLINDER HEAD TEMPERATURE (3.25)If indicated cylinder head temperature reaches 480°F:CHT Cycle P

3.3m ELECTRICAL FAILURES (3.27) (Continued)Dual Alternator Failure (Zero amps both ammeters or ALTERNATOR #land #2 INOP lights illuminated - annunciat

SECTION 3EMERG PROCEDURES PA-46-350P, MALIBUSECTION 3EMERG PROCEDURES PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19993-12 REVISED: SEPTEMB

3.3p SPIN RECOVERY (3.33)Rudder ...FULL OPPOSITE toDIRECTION of ROTATION

SECTION 3EMERG PROCEDURES PA-46-350P, MALIBUSECTION 3EMERG PROCEDURES PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19993-14REPORT: VB-1710 I

3.3t CABIN AIR CONTAMINATION/SMOKE EVACUATION (3.41)(Pressurized)NOTEIf pressurized, the following procedure will resultin an immediate loss of pressu

SECTION 3EMERG PROCEDURES PA-46-350P, MALIBUSECTION 3EMERG PROCEDURES PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19993-16REPORT: VB-1710 I

Revision FAA ApprovedNumber and Revised Description of Revisions SignatureCode Pages and DateRev. 1(continued)9-115 Added Section 9 thru Supplement 15

3.3v INADVERTENT ICING ENCOUNTER (3.45) (Continued)Vent/Defog Fan...

SECTION 3EMERG PROCEDURES PA-46-350P, MALIBUSECTION 3EMERG PROCEDURES PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19993-18REPORT: VB-1710 I

3.3aa ANNUNCIATOR LIGHT PANEL FAILURE (ANNUNCIATORINOP light illuminated - annunciator panel) (3.57) (Continued)If annunciator lights illuminate, annu

3.5 AMPLIFIED EMERGENCY PROCEDURES (GENERAL)The following paragraphs are presented to supply additional informationfor the purpose of providing the pi

SECTION 3EMERG PROCEDURES PA-46-350P, MALIBUSECTION 3EMERG PROCEDURES PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19993-22REPORT: VB-1710 I

3.9 ENGINE POWER LOSS DURING TAKEOFF (3.3c)The proper action to be taken if loss of power occurs during takeoff willdepend on the circumstances of the

SECTION 3EMERG PROCEDURES PA-46-350P, MALIBUSECTION 3EMERG PROCEDURES PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19993-24REPORT: VB-1710 I

3.13 POWER OFF LANDING (3.3e)If loss of power occurs at altitude, trim the aircraft for best gliding angle,(90 KIAS) and look for a suitable field. If

SECTION 3EMERG PROCEDURES PA-46-350P, MALIBUSECTION 3EMERG PROCEDURES PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19993-26REPORT: VB-1710 I

SECTION 3PA-46-350P, MALIBU EMERG PROCEDURES3.15 FIRE IN FLIGHT (3.3f) (Continued)all cases, the heater and defroster should be OFF. If radio communic

PA-46-350P, MALIBUPILOT'S OPERATING HANDBOOK LOG OF REVISIONS (cont)Revision FAA ApprovedNumber and Revised Description of Revisions SignatureCod

SECTION 3EMERG PROCEDURES PA-46-350P, MALIBU3.19 LOSS OF FUEL FLOW (3.3h) (Continued)If power is restored, turn OFF the emergency (EMERG) fuel pump (e

3.24 TURBINE INLET TEMP (TIT) INDICATOR FAILURE (3.3k)(CONT’D)If TIT failure occurs prior to setting cruise power, set power per the POHSection 5 powe

SECTION 3EMERG PROCEDURES PA-46-350P, MALIBUSECTION 3EMERG PROCEDURES PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19993-30REPORT: VB-1710 I

3.27 ELECTRICAL FAILURES (3.3m) (Continued)DUAL ALTERNATOR FAILURE (Zero amps both ammeters orALTERNATOR #1 and #2 INOP light illuminated - annunciato

SECTION 3EMERG PROCEDURES PA-46-350P, MALIBUSECTION 3EMERG PROCEDURES PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19993-32 REVISED: SEPTEMB

3.35 ENGINE ROUGHNESS (3.3q)Engine roughness may be caused by dirt in the injector nozzles,induction filter icing, ignition problems, or other causes.

SECTION 3EMERG PROCEDURES PA-46-350P, MALIBUSECTION 3EMERG PROCEDURES PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19993-34REPORT: VB-1710 I

3.43 VACUUM SYSTEM FAILURE (3.3u)A failure of either vacuum pump is indicated by the illumination of avacuum failure annunciator, “VACUUM NO. 1 INOP”.

SECTION 3EMERG PROCEDURES PA-46-350P, MALIBUSECTION 3EMERG PROCEDURES PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19993-36REPORT: VB-1710 I

3.53 FUEL TANK SUBMERGED PUMP FAILURE (BOOST PUMPlight illuminated - annunciator panel) (3.3y)Illumination of the BOOST PUMP annunciator light indicat

Revision FAA ApprovedNumber and Revised Description of Revisions SignatureCode Pages and DateRev. 7 iii Added Warning and moved(PR021014) info. to pag

SECTION 3EMERG PROCEDURES PA-46-350P, MALIBUSECTION 3EMERG PROCEDURES PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19993-38REPORT: VB-1710 I

SECTION 4 PA-46-350P, MALIBU NORMAL PROCEDURESTABLE OF CONTENTSSECTION 4NORMAL PROCEDURESParagraph PageNo. No.4.1 GENERAL ...

SECTION 4NORMAL PROCEDURES PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19994-ii REVISED: JANUARY 20, 2004TABLE OF CONTENTSSECTION 4 (cont)N

SECTION 4 PA-46-350P, MALIBU NORMAL PROCEDURESTABLE OF CONTENTSSECTION 4 (cont)NORMAL PROCEDURESParagraph PageNo. No.4.11 BEFORE STARTING ENGINE (4.5b

SECTION 4NORMAL PROCEDURES PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19994-iv REVISED: JANUARY 20, 2004TABLE OF CONTENTSSECTION 4 (cont)N

SECTION 4 PA-46-350P, MALIBU NORMAL PROCEDURESSECTION 4NORMAL PROCEDURES4.1 GENERALThis section provides the normal operating procedures for the PA-4

SECTION 4NORMAL PROCEDURES PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19994-2 REVISED: JANUARY 20, 20044.3 AIRSPEEDS FOR SAFE OPERATIONSTh

SECTION 4 PA-46-350P, MALIBU NORMAL PROCEDURESWALK-AROUNDFigure 4-14.5 NORMAL PROCEDURES CHECKLIST4.5a Preflight Checklists (4.9)COCKPIT (4.9a)Control

SECTION 4NORMAL PROCEDURES PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19994-4 REVISED: JANUARY 20, 20044.5a Preflight Checklist (Continued

SECTION 4 PA-46-350P, MALIBU NORMAL PROCEDURES4.5a Preflight Checklist (4.9) (Continued)RIGHT WING (4.9C) (CONTINUED)Fuel Tank Vent ...

PA-46-350P, MALIBUPILOT'S OPERATING HANDBOOK LOG OF REVISIONS (cont)Revision FAA ApprovedNumber and Revised Description of Revisions SignatureCod

SECTION 4NORMAL PROCEDURES PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19994-6 REVISED: JANUARY 20, 20044.5a Preflight Checklist (4.9) (Con

SECTION 4 PA-46-350P, MALIBU NORMAL PROCEDURES4.5a Preflight Checklist (4.9) (Continued)MISCELLANEOUS (4.9f) (Continued)Exterior Lighting Switches ..

SECTION 4NORMAL PROCEDURES PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19994-8 REVISED: JANUARY 20, 20044.5c Engine Start Checklist (4.13)E

SECTION 4 PA-46-350P, MALIBU NORMAL PROCEDURES4.5c Engine Start Checklist (4.13) (Continued)NORMAL START - COLD ENGINE (4.13b) (Continued)NOTEThe amou

SECTION 4NORMAL PROCEDURES PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19994-10 REVISED: JANUARY 20, 20044.5c Engine Start Checklist (4.13)

SECTION 4 PA-46-350P, MALIBU NORMAL PROCEDURES4.5d Before Taxiing Checklist (4.15)BEFORE TAXIING (4.15)CAUTIONDo not operate engine above 1200 RPM wit

SECTION 4NORMAL PROCEDURES PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19994-12 REVISED: JANUARY 20, 20044.5f Ground Check Checklist (4.19)

SECTION 4 PA-46-350P, MALIBU NORMAL PROCEDURES4.5g Before Takeoff Checklist (4.21) (Continued)BEFORE TAKEOFF (4.21) (Continued)Seat Backs ...

SECTION 4NORMAL PROCEDURES PA-46-350P, MALIBUREPORT: VB-1710 ISSUED: FEBRUARY 23, 19994-14 REVISED: JANUARY 20, 20044.5h Takeoff Checklist (4.23) (Con

4.5i Climb Checklist (Continued)CRUISE CLIMB (4.25b)Manifold Pressure ..................35 IN. HGPro