Piper Malibu PA-46-310P Owner's manual

1
N890PM POH: Table of Contents
Beginning
Section 1- General 21
Section 1 Table of Contents 21
1.1 Introduction 22
1.3 Engine 24
1.5 Propeller 24
1.7 Fuel 24
1.9 Oil 25
1.11 Maximum Weights 25
1.13 Standard Airplane Weights 25
1.15 Cabin and Entry Dimensions 26
1.17 Baggage Space and Entry Dimensions 26
1.19 Specific Loading 26
1.21 Symbols, Abbreviations and Terminology 28
Section 2- Limitations 34
TIT Inlet Supplement 36
Severe Icing Supplement 37
AD 91-07-08 R1 Supplement 39
Section 2 Table of Contents 43
2.1 General 45
2.3 Airspeed Limitations 45
2.5 Airspeed Indicator Markings 46
2.7 Power Plant Limitations 47
2.9 Leaning Limitations 47
2.11 Power Plant Instrument Markings 48
2.13 Weight Limits 48
2.15 Center of Gravity Limits 49
2.17 Maneuver Limits 49
2.19 Flight Load Factors 49
2.21 Kinds of Operation Equipment List 50
2.23 Fuel Limitations 51
2.25 Operating Altitude Limitations 52
2.27 Cabin Pressurization Limits 52
2.29 Noise Level 52
2.31 Maximum Seating Configuration 52
2.32 Icing Information 53
2.33 Placards 53

AD 98-04-26 Icing 57
Section 3- Emergency Procedures 59
Section 3 Table of Contents 59
3.1 General 61
3.3 Emergency Procedures Checklist 62
3.5 Amplified Emergency Procedures (General) 74
3.7 Engine Fire During Start 74
3.9 Engine Power Loss During Takeoff 74
3.11 Engine Power Loss In Flight 77
3.13 Power Off Landing 79
3.15 Fire In Flight 80
3.17 Loss of Oil Pressure 81
3.19 Loss of Fuel Flow 81
3.21 Engine Driven Fuel Pump Failure 82
3.23 High Oil Temperature 82
3.25 High Cylinder Head Temperature 83
3.26 Turbine Inlet Temperature (TIT) Indicator Failure 83
3.27 Electrical Failures 83
3.29 Electrical Overload (Alternator more than 20 amps above known electrical load) 84
3.31 Propeller Overspeed 86
3.33 Emergency Landing Gear Extension 86
3.35 Spin Recovery 86
3.37 Engine Roughness 87
3.39 Emergency Descent 87
3.41 Pressurization System Malfunction 88
3.43 Cabin Air Contamination/Smoke Evacuation 88
3.45 Gyro Suction Failure (Suction below 4.8 in. Hg.) (Aircraft not equipped with stand-by vacuum
pump) 89
3.47 Inadvertant Icing Encounter or Flight In Snow 89
3.48 Hydraulic System Malfunction (serial numbers 46-8508048 through 46-8608046, unless Piper
Kit No. 765 197 is installed) 90
3.49 Flap System Malfunction (serial numbers 46-8608001 and up) 90
Section 4- Normal Procedures 93
Section 4 Table of Contents 93
4.1 General 95
4.3 Airspeeds for Safe Operations 95
4.5 Normal Procedures Checklist 97
4.7 Amplified Normal Procedures (General) 111
4.9 Preflight Check 111

4.11 Before Starting Engine 114
4.13 Starting Engine 115
4.15 Warm-Up 117
4.17 Taxiing 118
4.19 Ground Check 118
4.23 Takeoff 120
4.25 Climb 123
4.27 Cruising 123
4.29 Descent 126
4.31 Approach and Landing 126
4.33 Go-Around 128
4.35 Stopping Engine 128
4.37 Parking 128
4.39 Stalls 128
4.41 Turbulent Air Operation 129
4.43 Landing Gear 129
4.45 Cabin Pressurization System 130
4.47 Weight and Balance 131
4.49 Icing Information 132
Section 5- Performance 133
Section 5 Table of Contents 133
5.1 General 135
5.3 Introduction- Performance and Flight Planning 135
5.5 Flight Planning Example 137
5.7 Performance Graphs 143
Airspeed Calibration 145
Angle of Bank vs. Stall Speed 146
Wind Components 148
Takeoff Ground Roll 0 Flaps 149
Takeoff Ground Roll 20 Flaps 150
Takeoff Distance Over 50ft Obstacle 0 Flaps 151
Takeoff Distance Over 50ft Obstacle 20 Flaps 152
Rate of Climb 153
Maximum Continuous Power Time Distance and Fuel to Climb 154
Cruise Climb Time, Distance, and Fuel to Climb 155
Power Setting Table 156
Cruise Speed vs Altitude 157
Range 158
Endurance 159

Time Distance and Fuel to Descend 160
Glide Time and Distance 161
Balked Landing Climb 162
Landing Distance Over 50ft Obstacle 163
Landing Ground Roll 164
Section 6- Weight and Balance 165
Section 6 Table of Contents 165
6.1 General 167
6.3 Airplane Weighing Procedure 168
6.5 Weight & Balance Data and Record 171
Current Weight and Balance 175
337 Files 181
Engine Mount 337- 1/11/2010 181
Engine Mount Modified 337- 12/15/2009 (Since Removed?) 185
TSIO550 Engine Install 337- 1/11/2010 187
JVC CD Player Install 377- 08/27/2004 190
3 Blade Prop. Install 337- 10/31/2007 192
Continuous Duty Vacuum Pump Install 337- 08/27/2004 196
JPI EDM 700 Install 337- 08/04/2003 198
Suspa Door Struts Install 337- 04/07/1997 209
Gas Cylinder Install 337- 06/15/1995 211
Gas Cylinder Install 337- 07/24/1995 213
Loran Install/Removal 337- 10/31/1993 217
Loran Install 337- 10/24/1984 225
6.7 General Loading Recomendations 229
6.9 Weight & Balance Determination for Flight 230
Loading Graph 233
CG Range & Weight Graph 234
6.11 Instructions For Using The Weight and Balance Plotter 235
Section 7- Description and Operation of the Airplane and its Systems 240
Section 7 Table of Contents 240
7.1 The Airplane 242
7.3 The Airframe 242
7.5 Engine and Propeller 243
7.6 Air Induction System 247
7.7 Engine Controls 249
7.9 Hydraulic System 250
7.13 Brake System 257
7.15 Flight Control System 257

7.17 Fuel System 258
7.19 Electrical System 263
7.21 Instrument Panel 269
7.25 Environmental System 275
7.27 Bleed Air, Conditioning, & Pressurization System 277
Cabin Altitude vs Airplane Altitude Graph 279
7.29 Vacuum System (Standard) 280
7.31 Cabin Features 284
7.33 Baggage Area 286
7.35 Finish 286
7.37 Stall Warning 286
7.39 Emergency Locator Transmitter 287
7.41 External Power 288
7.43 Radar 288
Section 8- Airplane Handling, Servicing, and Maintenance 290
Section 8 Table of Contents 290
8.1 General 292
8.3 Airplane Inspection Periods 295
8.5 Preventive Maintenance 296
8.7 Airplane Alterations 296
8.9 Ground Handling 297
8.11 Engine Induction Air Filter 299
8.13 Brake Service 300
8.15 Hydraulic System Service 302
8.17 Landing Gear Service 302
8.19 Propeller Service 303
8.21 Oil Requirements 304
8.23 Fuel System 305
8.25 Tire Inflation 309
8.27 Battery Service 309
8.29 Emergency Oxygen System (Optional) 309
8.31 Pressurization System 309
8.33 Lubrication 310
8.35 Cleaning 310
8.36 Cleaning and Maintenance of Relief Tube System 315
Section 9- Supplements 318
Section 9 Table of Contents 318
King 150 Series Flight Control System and King KAS 297B Vertical Speed and Altitude Selector
Supplement 319

King KNS-80 Area Navigation System Supplement 362
King KNS-81 Area Navigation System Supplement 378
Honeywell Weatherscout Radar System Supplement 390
Emergency Oxygen System Supplement 396
Air Conditioning System Supplement 402
3M Ryan Stormscope Supplement 406
Prop Heat, Heated Windshield Panel and Wing Ice Detection Light Supplement 412
TI 9100 Loran C Navigator Supplement 418
King KAS 297B Vertical Speed Supplement 424
Ice Protection System Supplement 436
Hydraulic Pump Annunciator Light and Motor Control Supplement 452
3M Ryan Stormscope WX-11 Supplement 456
Supplemental Electric Heater Supplement 462
Bendix/King RDS Digital Weather Radar Supplement 470
Digital Fuel Management System Operating Manual 472
Hartzell Propeller Supplement 483
Piper SB 1258 496
Section 10- Operating Tips 504
Section 10 Table of Contents 504
10.1 General 505
10.3 Operating Tips 505
Original Equipment List 507
Other 517
KY 196 VHF Communications Transceiver Instructions 517
QFRXCc Users Guide 521
Warranty Registration 521
PM3000 Pilots Guide 524
JVC CD Receiver Operating Guide 529

Malibu
Pilot's ·
Operating
Handbook
PIPER

..
MALIBU
PA-46-31 OP
SN 8408001
THRU 4608007
PILOT'S
OPERATING
HANDBOOK
AND
FAA APPROVED
AIRPLANE FLIGHT
MANUAL
AIRPLANE AIRPLANE
SERIAL NO. REGIST. NO. __
PA-46-310P I '\ n .J:'
REPORT: VB-1200FAAAPPROVED BY: WOAcl.. WDM,4 ...
DATE OF APPROVAL :
JANUARY 11, 1984
WARD EVANS
D.O .A. NO. S0 -1
PIPER
AIRCRAFT CORPORATION
VERO BEACH, FLORIDA
THIS HANDBOOK IN CLUD ES THE MATERIAL REQUIRED TO BE FURNISHED TO THE
PILOT
BY THE FEDERAL AVIATION REGULATIONS AND ADDITIONAL INFORMATION
PROVIDED
BY THE MANUFACTURER AND CONSTITUTES THE FAA APPROVED
AIRPLANE FLIGHT
MANUAL THIS HANDBOOK MUST BE CARRIED IN THE AIRPLANE
AT ALL TIMES.
REVISED: APRIL 1, 1987
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WARNING
EXTREME CARE MUST BE EXERCISED TO LIMITTHE USE OF
THIS HANDBOOK TO APPLICABLE AIRCRAFT. THIS HAND-
BOOK IS VALID FOR USE WITH THE AIRPLANE IDENTIFIED
ON THE FACE OF THE TITLE PAGE. SUBSEQUENT REVISIONS
SUPPLIED BY PIPER AIRCRAFT CORPORATION MUST BE
PROPERLY INSERTED.
Published by
PU BU CATIONS DEPARTMENT
Piper Aircraft Corporation
Issued: January 11. 1984
REPORT: VB-1200
ii

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