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Revision A5: Feb, 2012
Original Issue: Feb, 2002
PILO
T’S OPERA
TING MANU
AL
P/N 140-590032-0007
fo
r
Applicable to Airplane Seri
als 258541, 258556, 258567 and After
Equipped with Collins Pr
o Line 21 A
vionics
that ha
ve not installed Hawker Beec
hcraft Winglet Kits.
Copyright
©
2012 Hawker Beechcraft Corporation. All rights reserved.
Hawker and Beechcraft are trademarks of
Hawker Beech
craft Corporation.
2
Table of Contents
01 140-590032-0007_Title Page
1
HAWKER 800XP PILOT'S OPERATING MANUAL P/N 140-590032-0007
1
TITLE PAGE
1
INTRODUCTION
2
EXPORT STATEMENT
2
02 140-590032-0007_LOEP
3
LIST OF EFFECTIVE PAGES
3
03 140-590032-0007_LOTC
19
LOG OF TEMPORARY CHANGES
19
140-590032-0007TC1 - CANCELLED
19
140-590032-0007TC2 - CANCELLED
19
140-590032-0007TC3 - CANCELLED
19
140-590032-0007TC4 - CANCELLED
19
04 140-590032-0007_LOR
21
LOG OF REVISIONS
21
REVISION A5: FEBRUARY, 2012
21
REVISION A4: SEPTEMBER 2010
23
REVISION A3: APRIL 2008
27
REVISION A2: NOVEMBER 2004
28
REVISION A1: NOVEMBER 2002
38
ORIGINAL ISSUE: FEBRUARY 2002
47
05 140-590032-0007_Section1
48
SECTION I - GENERAL
48
TABLE OF CONTENTS
48
MANUAL INTRODUCTION
50
REVISIONS AND TEMPORARY CHANGES
50
SUPPLEMENTS
50
CONTENTS
51
AIRPLANE GENERAL
51
FIGURE 1 - GENERAL DIMENSIONS
53
DIMENSIONAL DATA
54
TERMS AND DEFINITIONS
56
FIGURE 2 - DEFINITION OF AREAS
57
06 140-590032-0007_Section2
58
SECTION II - OPERATING LIMITATIONS
58
TABLE OF CONTENTS
58
GENERAL
60
07 140-590032-0007_Section3
62
SECTION III - SYSTEMS DESCRIPTION
62
TABLE OF CONTENTS
62
SUB-SECTION 1 - MASTER WARNING SYSTEM
64
TABLE OF CONTENTS
64
GENERAL
66
ANNUNCIATOR TYPES
66
MWS ARRANGEMENT
66
REPEATER ANNUNCIATORS
66
FIGURE 1 - MASTER WARNING ANNUNCIATIONS AND CONTROLS
67
SYSTEM OPERATION
68
ACKNOWLEDGEMENT
68
ANNUNCIATION SEQUENCE
69
TABLE 1: ANNUNCIATION SEQUENCE
69
TESTING
70
DIM CONTROL FAILURE
70
MWS MASTER WARNING LAMP FAILURE
70
POWER SUPPLIES
70
ANNUNCIATORS WITH ASSOCIATED MWS REPEATERS
71
ELECTRICAL
71
ICE PROTECTION
72
FUEL
73
ENGINE FIRE WARNING
74
DUCT OVHT REPEATER ANNUNCIATOR
74
MWS ANNUNCIATORS - WITHOUT A REPEATER
75
TABLE 2: MWS ANNUNCIATORS - WITHOUT A REPEATER
75
SUB-SECTION 2 - ENGINES
78
TABLE OF CONTENTS
78
DESCRIPTION
83
FIGURE 1 - ENGINE CUTAWAY VIEW
83
FAN
83
COMPRESSOR SECTION
83
LOW PRESSURE SPOOL N1
84
HIGH PRESSURE SPOOL N2
84
COMBUSTION CHAMBER
84
TURBINE SECTION
84
ACCESSORY DRIVE
84
OPERATION
85
FIGURE 2 - GAS FLOW DURING ENGINE OPERATION
85
ENGINE INDICATING SYSTEM (EIS)
86
N1 RPM DISPLAYS
87
N1 REFERENCE DISPLAYS
88
ITT DISPLAYS
89
N2 RPM DISPLAYS
90
FUEL FLOW DISPLAYS
91
OIL PRESSURE DISPLAYS
91
OIL TEMPERATURE DISPLAYS
92
ENGINE FIRE WARNING ANNUNCIATIONS
92
CLIMB ANNUNCIATION
92
AUTOMATIC POWER RESERVE (APR) DISPLAYS
92
ENGINE SYSTEMS AND COMPONENTS
93
ENGINE OIL
93
OIL PUMP ASSEMBLY
93
FIGURE 3 - ENGINE LUBRICATION SYSTEM
94
OIL FILTER
95
OIL TANK
95
FUEL HEATER
95
AIR/OIL COOLER
95
FIGURE 4 - ENGINE VIEWS
96
FUEL/OIL COOLER
98
OIL VENTING
98
LOW OIL PRESSURE ANNUNCIATORS
98
IGNITION
99
IGNITION UNIT
99
IGNITER PLUGS AND LEADS
99
IGNITION SWITCHES
99
FUEL CONTROL
100
FUEL PUMP
100
ANTI-ICE VALVE
100
FILTER BYPASS
100
FIGURE 5 - ENGINE-DRIVEN FUEL PUMP ASSEMBLY
101
FILTER CLOGGED
102
FUEL CONTROL UNIT
102
INLET PRESSURE AND TEMPERATURE SENSOR
102
DIGITAL ELECTRONIC ENGINE CONTROL (FUEL COMPUTER)
103
FIGURE 6 - DEEC ENGINE INTERFACE
104
SURGE BLEED VALVE
105
FUEL FLOW DIVIDER ASSEMBLY
105
FUEL NOZZLES
105
FUEL HEATING
105
FUEL FLOW INDICATING
106
ADDITIONAL FUEL SYSTEM COMPONENTS
106
POWER CONTROLS
107
ENGINE THRUST LEVERS
107
AUDIBLE WARNINGS AND INTERLOCKS
107
HIGH PRESSURE (HP) FUEL COCK LEVERS
107
FIGURE 7 - FUEL CONTROLS
108
ENGINE SYNCHRONIZER
109
POWER SUPPLY
109
BLEED AIR AND VENTILATION
110
FIGURE 8 - ENGINE BLEED AIR AND VENTILATION
110
ANTI-ICING
110
FIGURE 9 - ENGINE ANTI-ICING SYSTEM
111
POWER SUPPLIES
112
AIRPLANE SERVICES
113
AUTOMATIC PERFORMANCE RESERVE (APR)
113
CONTROLS
113
FIGURE 10 - APR SYSTEM
114
OPERATION
115
AUTOMATIC MODE
115
MANUAL MODE
115
FAILURE MODES
115
THRUST REVERSERS
116
DESCRIPTION
116
CONTROLS AND INDICATORS
116
ARM
116
OFF
117
UNLCK
117
REVRS
117
REVERSER ASSEMBLY AND OPERATION
117
INITIATE
117
DEPLOY
118
STOW
118
AUTOSTOW
119
AUTOMATIC THRUST LEVER RETARD/AUTOSTOW SYSTEM
119
SYSTEM SAFETY
119
FIGURE 11 - THRUST REVERSER OPERATING MODE - OVERSTOW AND LATCH
119
FIGURE 12 - THRUST REVERSER OPERATING MODE - DEPLOY
120
SUB-SECTION 3 - FUEL SYSTEM
122
TABLE OF CONTENTS
122
GENERAL
124
WING TANKS
124
FIGURE 1 - WING TANK CROSSFEED AND TRANSFER
125
REFUEL/DEFUEL FILLER POINTS
125
FIGURE 2 - FUEL FEED SYSTEM
126
FIGURE 3 - REFUEL/DEFUEL SYSTEM
127
GRAVITY FILLER
128
TABLE 1: PRESSURE REFULEING QUANTITIES
128
FUEL QUANTITY INDICATIONS
129
REFUEL/DEFUEL CONTROL AND INDICATIONS
129
ENGINE FUEL FEED SYSTEM
130
AUXILIARY TANK TRANSFER
132
WING TANK CROSSFEED AND TRANSFER
132
FUEL FLOW INDICATIONS
133
FUEL TEMPERATURE INDICATOR
133
SUB-SECTION 4 - FIRE PROTECTION
134
TABLE OF CONTENTS
134
GENERAL
136
FIGURE 1 - ENGINE FIRE DETECTION AND WARNING SYSTEM COMPONENT LOCATIONS
136
CONTROLS AND INDICATIONS
137
ENGINE FIRE DETECTION SYSTEM
137
OVERHEAT
137
WARNINGS
138
TESTING
138
ENGINE FIRE EXTINGUISHING SYSTEM
139
OPERATION
139
REAR EQUIPMENT BAY OVERHEAT
139
BAGGAGE BAY AND TOILET SMOKE (IF INSTALLED)
139
FIGURE 2 - ENGINE FIRE EXTINGUISHER SYSTEM
140
BCF PORTABLE FIRE EXTINGUISHER
141
FIGURE 3 - BCF PORTABLE FIRE EXTINGUISHER
141
SUB-SECTION 5 - HYDRAULICS
142
TABLE OF CONTENTS
142
GENERAL
144
MAIN HYDRAULIC SYSTEM
144
AUXILIARY HYDRAULIC SYSTEM
144
MAIN SYSTEM
145
TABLE 1: INDICATORS AND ANNUNCIATORS
145
FLUID STORAGE
145
POWER GENERATION
146
HIGH PRESSURE RELIEF
146
LOW PRESSURE INDICATION
146
HAND PUMP
146
MAINTAINED PRESSURE PATHS
146
THRUST REVERSERS
146
WHEEL BRAKES EMERGENCY PATH
147
ACCUMULATORS
147
NON-MAINTAINED PRESSURE PATHS
147
FIGURE 1 - MAIN HYDRAULIC SYSTEM COMPONENTS
148
KEY TO FIGURE 2
149
FIGURE 2 - MAIN HYDRAULIC SYSTEM
150
AUXILIARY SYSTEM
151
FIGURE 3 - AUXILIARY HYDRAULIC SYSTEM COMPONENTS
151
FIGURE 4 - AUXILIARY HYDRAULIC SYSTEM
152
CONTROLS AND INDICATIONS
153
FLUID STORAGE
153
OPERATION
153
FIGURE 5 - OPERATION OF AUXILIARY HYDRAULIC SYSTEM SELECTOR HANDLE
154
RESETTING THE MAIN SYSTEM
155
SUB-SECTION 6 - FLIGHT CONTROLS
156
TABLE OF CONTENTS
156
GENERAL
158
PRIMARY CONTROLS
158
AILERON CONTROL SYSTEM
158
FIGURE 1 - AILERON CONTROL SYSTEM
159
AILERON TRIM TABS
160
AILERON OUT-OF-TRIM WARNING
160
RUDDER CONTROL SYSTEM
161
FIGURE 2 - RUDDER CONTROL SYSTEM
161
RUDDER TRIM TABS
162
FIGURE 3 - RUDDER TRIM SYSTEM
162
RUDDER BIAS SYSTEM
163
ELECTRIC HEATING
164
FIGURE 4 - RUDDER BIAS SYSTEM
165
ELEVATOR CONTROL SYSTEM
166
FIGURE 5 - ELEVATOR CONTROL SYSTEM
166
ELEVATOR TRIM SYSTEM
167
ELEVATOR OUT-OF-TRIM WARNING
167
FIGURE 6 - ELEVATOR TRIM SYSTEM
168
MACH TRIM
169
SECONDARY CONTROLS
170
FLAP SYSTEM
170
FLAP CONTROL SYSTEM
170
FIGURE 7 - FLAP CONTROL SYSTEM
171
INDICATIONS AND WARNINGS
172
POWER SUPPLIES
173
EMERGENCY OPERATION
173
AIRBRAKE CONTROL SYSTEM (FIGURE 8)
173
FIGURE 8 - AIRBRAKE CONTROL SYSTEM
174
LIFT DUMP
175
ANNUNCIATIONS AND WARNINGS
175
POWER SUPPLIES
175
SUB-SECTION 7 - STALL WARNING/IDENTIFICATION
176
TABLE OF CONTENTS
176
GENERAL
178
CONTROLS AND ANNUNCIATIONS
178
OPERATION
179
STALL IDENTIFICATION SYSTEM
179
FIGURE 1 - STALL VALVE ANNUNCIATORS
179
FIGURE 2 - VARIATION OF STALL IDENTIFICATION ANGLE WITH RATE OF INCREASE OF VANE ANGLE
180
THIRD STALL IDENTIFICATION CHANNEL
181
FIGURE 3 - STALL WARNING AND IDENTIFICATION
181
FIGURE 4 - STALL SYSTEM PITOT STATIC BLOCK DIAGRAM
182
SYSTEM FAULTS AND ANNUNCIATIONS
183
FIGURE 5 - SYSTEM FAULT ANNUNCIATORS
183
FLAP ASYMMETRY
184
WEIGHT-ON-WHEELS ASYMMETRY
184
SSU SELF TEST
184
SYSTEM ANNUNCIATORS
185
TABLE 1: SUMMARY OF ANNUNCIATORS
185
SYSTEM POWER SUPPLIES
185
TABLE 2: POWER SUPPLIES
185
STALL WARNING AND IDENTIFICATION LOGIC
186
FIGURE 6 - STALL SYSTEM FLOW LOGIC
186
SUB-SECTION 8 - LANDING GEAR
188
TABLE OF CONTENTS
188
GENERAL
190
LANDING GEAR SELECTOR AND BAULK OVERRIDE
193
FIGURE 1 - LANDING GEAR SELECTOR AND BAULK OVERRIDE
193
RETRACTION AND EXTENSION
194
FIGURE 2 - LANDING GEAR HYDRAULIC SYSTEM
195
NOSE GEAR
196
NOSE GEAR BAY DOORS
196
FIGURE 3 - MAIN LANDING GEAR
197
FIGURE 4 - NOSE LANDING GEAR
198
FIGURE 5 - NOSE GEAR DOORS RELEASE STRUT
199
AUXILIARY HYDRAULIC SYSTEM
200
LOWERING SEQUENCE
200
FIGURE 6 - AUXILIARY HYDRAULIC SYSTEM
201
WHEELS AND BRAKES
202
WHEEL BRAKES
202
FIGURE 7 - WHEEL BRAKE LEVER
203
FIGURE 8 - COMBINED HYDRAULIC PRESSURE INDICATOR AND EMERGENCY WHEEL BRAKE ANNUNCIATORS
204
POWER SUPPLIES
205
NOSE WHEEL STEERING
205
OPERATION
205
FIGURE 9 - NOSE GEAR STEERING SYSTEM
206
SUB-SECTION 9 - ELECTRICAL POWER
208
TABLE OF CONTENTS
208
CONTROLS AND INDICATIONS
210
AMMETERS
211
FIGURE 1 - DC ELECTRICAL SYSTEM DE-ENERGIZED
212
EXT BATT CHG ON/OFF SWITCH
213
FIGURE 2 - GROUND POWER CONNECTED WITH EXTERNAL BATTERY CHARGE SWITCH ON
214
BATT ISOLATE BATT 1-NORM-BATT 2 SWITCH
216
FIGURE 3 - BATTERY SWITCH ON
217
GEN 1 AND GEN 2 CLOSE-TRIP SWITCHES
218
FIGURE 4 - NORMAL FLIGHT CONDITIONS
219
ENGINE START USING EXTERNAL POWER
220
ABORT START
220
FIGURE 5 - INTERNAL START WITH NO. 2 ENGINE SELECTED
221
ENGINE START USING BATTERY POWER
222
DOUBLE GENERATOR FAILURE (FIGURE 7)
223
FIGURE 6 - SINGLE GENERATOR FAILURE
224
FIGURE 7 - DOUBLE GENERATOR FAILURE
225
APU GENERATOR (IF APU INSTALLED)
226
OVERVOLTAGE PROTECTION
226
FIGURE 8 - APU (IF INSTALLED) GENERATOR ON-LINE
226
AC POWER
227
AC POWER DISTRIBUTION
229
FIGURE 8 - INVERTER SYSTEM BUSBARS - SIMPLIFIED
229
SUB-SECTION 10 - ENVIRONMENTAL
232
TABLE OF CONTENTS
232
AIR CYCLE MACHINE
235
FIGURE 1 - AIR SUPPLY AND DISTRIBUTION
236
PRESSURIZATION CONTROL SYSTEM
244
AUTOMATIC CONTROL
245
PNEUMATIC RELAY
246
ABSOLUTE PRESSURE REGULATORS
246
CABIN DEPRESSURIZATION WARNING
247
FIGURE 2 - PRESSURIZATION SYSTEM
248
SUB-SECTION 11 - ICE PROTECTION
250
TABLE OF CONTENTS
250
SYSTEM OPERATION
252
WING SPOTLIGHTS
253
FIGURE 1 - ICE DETECTION COMPONENTS
254
FLUID STORAGE
255
WARNING ANNUNCIATORS
255
POWER SUPPLIES
255
FIGURE 2 - AIRFRAME ICE PROTECTION SYSTEM
256
ENGINE BLEED AIR ANTI-ICING
257
WARNING ANNUNCIATORS
257
FIGURE 3 - ENGINE ANTI-ICING SYSTEM
258
ICE PROTECTION - WINDSCREENS
259
ELECTRICAL HEATING SYSTEM
259
FIGURE 4 - WINDSCREEN ELECTRICAL HEATING
260
SUB-SECTION 12 - OXYGEN SYSTEM
264
TABLE OF CONTENTS
264
GENERAL
266
FIGURE 1 - OXYGEN CYLINDER ASSEMBLY
266
FIGURE 2 - OXYGEN SYSTEM
267
SERVICING
268
FIGURE 3 - OXYGEN BOX ASSEMBLY
268
OPERATION
269
FIGURE 4 - FLIGHT COMPARTMENT OXYGEN PANEL ON LEFT CONSOLE
269
PORTABLE OXYGEN SMOKE SET
270
FIGURE 5 - PORTABLE OXYGEN SMOKE SET
270
FLIGHT CREW SUPPLY
271
MASK-REGULATOR
271
FIGURE 6 - OXYGEN MASK AND REGULATOR (MOD. NO. 25A025A)
271
GOGGLES
272
FIGURE 7 - SMOKE GOGGLES AND MASK-REGULATOR
272
THERAPEUTIC SUPPLY
272
PASSENGER SUPPLY
273
FIGURE 8 - PASSENGER OXYGEN BOX LOCATIONS AND MASK STOWAGE
273
FIGURE 9 - OXYGEN MASK FOLDING AND STOWAGE
274
SUB-SECTION 13 - LIGHTING SYSTEMS
276
TABLE OF CONTENTS
276
ENTRANCE LIGHTING
278
FIGURE 1 - MAIN ENTRY DOORWAY LIGHTING AND CONTROLS
278
FLIGHT COMPARTMENT LIGHTING
279
INSTRUMENT AND PANEL LIGHTING (FIGURE 2)
279
FIGURE 2 - FLIGHT COMPARTMENT LIGHTING
280
FIGURE 3 - FLIGHT COMPARTMENT BULKHEAD LIGHTING
281
FLIGHT COMPARTMENT LIGHTING POWER SOURCES
282
TABLE 1
282
PRINCIPAL DIMMER CONTROLS
283
TABLE 2
283
GALLEY LIGHTING (FIGURE 4)
285
FIGURE 4 - TYPICAL GALLEY
285
PASSENGER CABIN LIGHTING
286
CABIN LIGHTING POWER SOURCES
287
TABLE 3
287
TOILET COMPARTMENT LIGHTING (FIGURE 5)
289
FIGURE 5 - TOILET COMPARTMENT
289
MISCELLANEOUS INTERIOR LIGHTING AND CONTROLS
290
FIGURE 6 - INTERIOR LIGHTING CONTROL PANEL
290
EXTERIOR LIGHTING
291
WING ICE-INSPECTION SPOTLIGHTS (FIGURES 7 AND 8)
291
FIGURE 7 - EXTERIOR LIGHTING CONTROL PANEL
291
FIGURE 8 - EXTERIOR LIGHTING
292
EXTERIOR LIGHTING POWER SOURCES
294
TABLE 4
294
SUB-SECTION 14 - EQUIPMENT AND FURNISHINGS
296
TABLE OF CONTENTS
296
FLIGHT COMPARTMENT
298
CREW SEATS
298
FIGURE 1 - CREW SEAT
299
3RD CREW MEMBER SEAT
300
FIGURE 2 - 3RD CREW MEMBER SEAT
300
CREW CABINET AREA
300
FIGURE 3 - FLIGHT COMPARTMENT
301
FIGURE 4 - FLIGHT COMPARTMENT MAIN INSTRUMENT PANELS
302
FIGURE 5 - FLIGHT COMPARTMENT OVERHEAD ROOF PANELS
303
FIGURE 6 - FLIGHT COMPARTMENT (LOOKING AFT)
304
FIGURE 7 - FLIGHT COMPARTMENT SIDE CONSOLES
305
FIGURE 8 - FLIGHT COMPARTMENT CENTER PEDESTAL
306
GALLEY
307
FIGURE 9 - TYPICAL GALLEY
307
PASSENGER CABIN
308
FIGURE 10 - TYPICAL INTERIOR LAYOUT
308
SEATING ARRANGEMENTS
309
FIGURE 11 - PASSENGER RIGHT SIDE CONSOLE CONTROL
309
FIGURE 12 - TYPICAL 3 SEAT DIVAN
309
CARGO AND ACCESSORY COMPARTMENTS
310
MAIN RADIO/AVIONICS COMPARTMENTS
310
FIGURE 13 - CARGO AND ACCESSORY COMPARTMENTS
311
TOILET COMPARTMENT
312
FIGURE 14 - TYPICAL TOILET COMPARTMENT
312
SUB-SECTION 15 - EMERGENCY EQUIPMENT
314
TABLE OF CONTENTS
314
PROTECTIVE BREATHING EQUIPMENT (PBE)
318
FIGURE 1 - PROTECTIVE BREATHING EQUIPMENT
318
SUB-SECTION 16 - WATER AND WASTE
320
TABLE OF CONTENTS
320
WATER SYSTEM
322
GALLEY WATER (FIGURE 1)
323
FIGURE 1 - GALLEY MASTER SWITCH AND TYPICAL GALLEY
323
WASTE SYSTEM
324
TOILET (FIGURES 2 AND 3)
324
FIGURE 2 - TYPICAL TOILET COMPARTMENT
324
FIGURE 3 - TYPICAL TOILET WITH EXTERNAL SERVICING FACILITY
325
FIGURE 4 - TOILET GROUND SERVICING
326
SUB-SECTION 17 - AVIONICS
328
TABLE OF CONTENTS
328
GENERAL
330
SYSTEMS AND CONTROLS
330
FIGURE 1 - PUSH-TO-TEST PANEL
330
DISPLAY CONTROL PANELS (DCP) FIGURE 3
331
FLIGHT GUIDANCE PANEL (FGP) FIGURE 3
331
CONTROL DISPLAY UNITS (CDU) FIGURE 2
331
FIGURE 2 - MAIN INSTRUMENT PANELS
332
FIGURE 3 - GLARESHIELD CONTROL PANELS
333
COMPONENT LOCATIONS
336
FIGURE 4 - COMPONENT LOCATIONS
336
RADIO SENSOR SYSTEM (RSS)
337
AUDIO INTEGRATING SYSTEM
337
AUDIO CONTROL PANEL (ACP)
337
HF RADIO TRANSMISSIONS
337
FIGURE 5 - AUDIO CONTROL PANEL (ACP)
338
ACP OPERATION
339
MICROPHONE JACKS
340
FLIGHT COMPARTMENT SPEAKERS
340
OXYGEN MASK ASSEMBLIES
340
ENHANCED GROUND PROXIMITY WARNING SYSTEM (EGPWS) WITH WINDSHEAR
341
EGPWS FEATURES
341
FIGURE 6 - TERRAIN CLEARANCE FLOOR ALERT ENVELOPE
342
FIGURE 7 - IMPROVED TERRAIN CLEARANCE FLOOR ENVELOPE
342
SELF TEST
343
SWITCHES/ANNUNCIATORS
343
FIGURE 8 - RUNWAY FIELD CLEARANCE FLOOR ENVELOPE
344
EGPWS OPERATING MODES
345
MODE 1
345
MODE 2
345
MODE 3
346
MODE 4
346
MODE 5
347
MODE 6
348
MODE 7
349
SUB-SECTION 18 - PITOT-STATIC SYSTEM
350
TABLE OF CONTENTS
350
GENERAL
352
PITOT HEADS
352
STATIC VENT PLATES
352
EQUIPMENT ISOLATION
353
STALL VENTS
353
FIGURE 1 - PITOT-STATIC SYSTEM BLOCK DIAGRAM
354
08 140-590032-0007_Section4
356
SECTION IV - FLIGHT PLANNING DATA
356
TABLE OF CONTENTS
356
SUB-SECTION 1 - GENERAL
358
TABLE OF CONTENTS
358
SPEED AND TEMPERATURE RELATIONSHIPS
361
DETERMINATION OF TEMPERATURES RELATIVE TO ISA
361
FIGURE 1 - ISA TEMPERATURES
361
DETERMINATION OF SPEED AND TEMPERATURE CORRECTION
362
FIGURE 2 - SPEED AND TEMPERATURE CORRECTION
363
CEILING DATA
364
TABLE 1: MAXIMUM CRUISE ALTITUDE
364
TABLE 2: MAXIMUM CRUISE WEIGHT
364
TABLE 3: MAXIMUM TAKEOFF WEIGHT FOR CRUISE ALTITUDE
365
SUB-SECTION 2 - PREFLIGHT
366
TABLE OF CONTENTS
366
INTRODUCTION
368
FIGURE 1 - DEFINITIONS AND TERMS FOR VARIOUS PHASES OF FLIGHT
370
FUEL LOADING PLAN AND WORKED EXAMPLE
371
FUEL LOADING PLAN
372
WORKED EXAMPLE
374
EQUIVALENT STILL AIR DISTANCE TABULATED DATA
387
HOLDING FUEL FLOW
564
SUB-SECTION 3 - CLIMB
568
TABLE OF CONTENTS
568
INTRODUCTION
570
NORMAL CLIMB
571
ISA -15°C
571
ISA -10°C
573
ISA
575
ISA +5°C
577
ISA +10°C
579
ISA +15°C
581
ISA +20°C
583
OPTIMUM TIME-TO-HEIGHT CLIMB
585
ISA -15°C
585
ISA -10°C
587
ISA
589
ISA +10°C
591
ISA +15°C
593
ISA +20°C
595
PRESSURE RATE OF CLIMB
597
FIGURE 1 - NORMAL PROCEDURE PRESSURE RATE OF CLIMB - ANTICE OFF
597
SUB-SECTION 4 - CRUISE EN-ROUTE
598
TABLE OF CONTENTS
598
HIGH SPEED CRUISE
602
5000 FT
602
7000 FT
603
9000 FT
604
11,000 FT
605
13,000 FT
606
15,000 FT
607
17,000 FT
608
19,000 FT
609
21,000 FT
610
23,000 FT
611
25,000 FT
612
27,000 FT
613
29,000 FT
614
31,000 FT
615
33,000 FT
616
35,000 FT
617
37,000 FT
618
39,000 FT
619
41,000 FT
620
INTERMEDIATE CRUISE
622
9000 FT
622
11,000 FT
623
13,000 FT
624
15,000 FT
625
17,000 FT
626
19,000 FT
627
21,000 FT
628
23,000 FT
629
25,000 FT
630
27,000 FT
631
29,000 FT
632
31,000 FT
633
33,000 FT
634
35,000 FT
635
37,000 FT
636
39,000 FT
637
41,000 FT
638
LONG RANGE CRUISE
640
230 KIAS
640
33,000 FT
642
35,000 FT
643
37,000 FT
644
39,000 FT
645
41,000 FT
646
CRUISE AIR MILES PER LB OF FUEL
648
FIGURE 1 - CRUISE AIR MILES PER LB OF FUEL - 20,000 FT ISA
648
FIGURE 2 - CRUISE AIR MILES PER LB OF FUEL - 25,000 FT ISA
649
FIGURE 3 - CRUISE AIR MILES PER LB OF FUEL - 31,000 FT ISA
650
FIGURE 4 - CRUISE AIR MILES PER LB OF FUEL - 33,000 FT ISA
651
FIGURE 5 - CRUISE AIR MILES PER LB OF FUEL - 35,000 FT ISA
652
FIGURE 6 - CRUISE AIR MILES PER LB OF FUEL - 37,000 FT ISA
653
FIGURE 7 - CRUISE AIR MILES PER LB OF FUEL - 39,000 FT ISA
654
FIGURE 8 - CRUISE AIR MILES PER LB OF FUEL - 41,000 FT ISA
655
EN-ROUTE FUEL CHECK
656
INSTRUCTIONS FOR USE OF TABLE
656
SUB-SECTION 5 - NORMAL DESCENT
658
TABLE OF CONTENTS
658
INTRODUCTION
660
NORMAL DESCENT ISA
661
SUB-SECTION 6 - SINGLE ENGINE
664
TABLE OF CONTENTS
664
INTRODUCTION
666
SINGLE ENGINE CEILING
666
SINGLE ENGINE DRIFT DOWN
666
SINGLE ENGINE CRUISE
667
SINGLE ENGINE MAXIMUM CONTINUOUS THRUST FOR DESCENT AND CRUISE
667
SINGLE ENGINE
668
SINGLE ENGINE MINIMUM CRUISE SPEED AND MAXIMUM CRUISE ALTITUDE
668
SINGLE ENGINE MAXIMUM CRUISE WEIGHT
669
SINGLE ENGINE LONG RANGE CRUISE SPEED
669
SUMMARY OF SINGLE ENGINE CEILINGS
670
OBSTACLE CLEARANCE
671
RANGE AFTER ENGINE FAILURE
672
SINGLE ENGINE DRIFT DOWN
673
ISA -15°C
673
ISA -10°C
675
ISA
677
ISA +10°C
679
ISA +20°C
681
SINGLE ENGINE LONG RANGE CRUISE
683
11,000 FT
683
13,000 FT
684
15,000 FT
685
17,000 FT
686
19,000 FT
687
21,000 FT
688
23,000 FT
689
25,000 FT
690
27,000 FT
691
SINGLE ENGINE HOLDING - FUEL FLOW ENGINE ANTICE OFF
692
SINGLE ENGINE HIGH SPEED DESCENT
693
SINGLE ENGINE MAXIMUM CONTINUOUS THRUST CRUISE
695
10,000 FT
695
11,000 FT
696
13,000 FT
697
15,000 FT
698
17,000 FT
699
19,000 FT
700
21,000 FT
701
23,000 FT
702
25,000 FT
703
27,000 FT
704
SUB-SECTION 7 - UNFACTORED LANDING
706
TABLE OF CONTENTS
706
INTRODUCTION
708
INSTRUCTIONS FOR USE OF THE CHART
709
FIGURE 1 - UNFACTORED LANDING DISTANCE REQUIRED
710
SUB-SECTION 8 - GEAR DOWN PERFORMANCE
712
TABLE OF CONTENTS
712
INTRODUCTION
714
GEAR DOWN CLIMB
715
160 KIAS/210 KIAS
715
ISA -15°C
715
ISA -10°C
716
ISA -5°C
717
ISA
718
ISA +5°C
719
ISA +10°C
720
ISA +15°C
721
ISA +20°C
722
GEAR DOWN CRUISE
723
1,000 FT
723
3,000 FT
724
5,000 FT
725
7,000 FT
726
9,000 FT
727
11,000 FT
728
13,000 FT
729
15,000 FT
730
17,000 FT
731
19,000 FT
732
20,000 FT
733
GEAR DOWN DESCENT
734
210 KIAS
734
ISA
734
SUB-SECTION 9 - EXTENDED RANG OPERATIONS (NON-ETOPS)
736
TABLE OF CONTENTS
736
INTRODUCTION
738
EXTENDED RANGE OPERATIONS (NON-ETOPS)
738
09 140-590032-0007_Section5
740
SECTION V - FLIGHT HANDLING
740
TABLE OF CONTENTS
740
SUB-SECTION 1 - NORMAL HANDLING
742
TABLE OF CONTENTS
742
TAKEOFF AND DEPARTURE
744
TAXI
744
THRUST REVERSERS (T/Rs)
744
ENGINE COMPUTER, RUDDER BIAS AND T/R CHECKS
744
ENGINE COMPUTERS
744
RUDDER BIAS
744
T/Rs
745
TYPE OF RUNWAY SURFACE
745
WET RUNWAY
745
SLIPPERY RUNWAY
745
OPERATION ON UNPAVED SURFACES
746
MINIMUM RUNWAY WIDTH
746
FIGURE 1 - MINIMUM TURN RADII
747
WHEEL BRAKES
748
REPEATED WHEEL BRAKE USAGE
748
TAKEOFF
748
ICE PROTECTION - BEFORE TAKEOFF
748
TAKEOFF PROCEDURES
749
TAKEOFF THRUST
750
NOISE ABATEMENT PROCEDURES
750
TAKEOFF THRUST PROCEDURES
750
BEFORE TAKEOFF
750
TAKEOFF
750
UP TO 80 KIAS
750
ABOVE 80 KIAS AND BELOW V1
750
WIND COMPONENT AND CRITICAL ENGINE
750
FIGURE 2 - FLIGHT PROFILE - NORMAL TAKEOFF
751
CLIMB
752
TABLE 1: N1 REFERENCE VALUES FOR MAXIMUM CLIMB - ENGINE ANTI-ICING OFF - SYNC ON
753
TABLE 2: N1 REFERENCE VALUES FOR MAXIMUM CLIMB - ENGINE ANTI-ICING ON - SYNC ON
753
FIGURE 3 - FLIGHT PROFILE - CLIMB, CRUISE AND DESCENT
754
CRUISE
755
MANEUVERING AT HIGH ALTITUDES
755
STABILITY AND TRIM CHANGE
755
RUDDER CONTROL FORCE
756
AIRBRAKES
756
POSITION ERROR CORRECTIONS
756
STALLS
756
CONDITIONS FOR STALLS
756
TECHNIQUE FOR STALLS
757
STALL CHARACTERISTICS
757
AVIONICS AND NAVIGATION
758
FLIGHT MANAGEMENT SYSTEM (FMS)
758
DURATION OF OXYGEN SUPPLY FOR PRIVATE CATEGORY AIRPLANES
759
TABLE 3: DURATION OF OXYGEN SUPPLY - PRIVATE CATEGORY
759
DURATION OF OXYGEN SUPPLY FOR COMPLIANCE WITH 14 CFR 91.211
760
TABLE 4: DURATION OF OXYGEN SUPPLY - 14 CFR 91.211
760
DURATION OF OXYGEN SUPPLY FOR COMPLIANCE WITH 14 CFR 135.157
761
TABLE 5: DURATION OF OXYGEN SUPPLY - 14 CFR 135.157
761
DESCENT AND HOLDING
762
DESCENT
762
TABLE 6: TIME OF DESCENT
762
HOLDING
763
FIGURE 4 - FLIGHT PROFILE - ILS
763
FIGURE 5 - FLIGHT PROFILE - NON-PRECISION APPROACH
764
APPROACH AND LANDING
765
APPROACH
765
NORMAL LANDING
765
TWO ENGINE GO-AROUND
765
FIGURE 6 - FLIGHT PROFILE - VFR APPROACH NORMAL
766
SUB-SECTION 2 - ABNORMAL HANDLING
768
TABLE OF CONTENTS
768
CONTINUED TAKEOFF (ENGINE FAILURE AFTER V1)
771
ENGINE FAILURE AFTER LIFT-OFF
771
FIGURE 1 - FLIGHT PROFILE TAKEOFF: ENGINE FAILURE AFTER V1 WITH APR-HIGH AND LOW PERFORMANCE PROFILES
772
CRUISE WITH ONE ENGINE INOPERATIVE
773
ICING GENERAL
774
WING/TAIL ANTICE FLUIDS
774
BEFORE TAKEOFF
775
CLIMB
776
CRUISE
776
HOLDING
776
DESCENT
776
FIGURE 2 - SPEED FOR USE IN ICING CONDITIONS
777
LEAVING ICING CONDITIONS
778
SEVERE ICING CONDITIONS
778
FLIGHT IN TURBULENT AIR
779
CLEAR AIR AND NON-STORM TURBULENCE
780
STORM TURBULENCE
780
FIGURE 3 - MAXIMUM ALTITUDE FOR FLIGHT WHEN STORM OR SEVERE TURBULENCE MAY BE EXPECTED
780
OPERATION IN WINDSHEAR AND MICROBURST CONDITIONS
781
WINDSHEAR
781
FIGURE 4 - SYMMETRIC MICROBURST
782
FIGURE 5 - ASYMMETRIC MICROBURST
782
FIGURE 6 - DRY MICROBURST
782
DIAGRAM OF FLIGHT CREW ACTION
783
LESSONS LEARNED FROM WINDSHEAR ENCOUNTERS
783
STANDARD OPERATING TECHNIQUES
784
FIGURE 7 - WINDSHEAR EFFECTS ON ROTATION DECISION
788
FIGURE 8 - WINDSHEAR EFFECTS ON FLIGHT PATH DURING APPROACH
789
AIRPLANES WITH WINDSHEAR ALERTING SYSTEMS INSTALLED
793
SUMMARY
793
OPERATION IN AREAS CONTAMINATED BY VOLCANIC ASH
794
GROUND OPERATION
794
PRE-START
794
TAXI
794
TAKEOFF
794
CRUISE
794
LANDING
794
APPROACH AND LANDING (ONE ENGINE INOPERATIVE)
795
GO-AROUND (ONE ENGINE INOPERATIVE)
795
EMERGENCY OVERWEIGHT LANDING
795
LANDING ABOVE WAT LIMIT WITH ONE OR BOTH ENGINES OPERATING
796
LANDING WITH ENGINE FUEL COMPUTER INOPERATIVE
796
NO FLAP LANDING
796
LANDING WITH ASYMMETRIC AIR BRAKE
796
LANDING BY USE OF TRIM SYSTEM
797
LANDING AFTER GEAR FAILS TO FULLY LOCK DOWN
797
FIGURE 9 - FLIGHT PROFILE - NON-PRECISION APPROACH - SINGLE ENGINE
798
FIGURE 10 - FLIGHT PROFILE - ILS APPROACH-SINGLE ENGINE
799
FIGURE 11 - FLIGHT PROFILE - VFR APPROACH - SINGLE ENGINE
800
FIGURE 12 - FLIGHT PROFILE - VFR - NO FLAP APPROACH
801
FIGURE 13 - FLIGHT PROFILE - ILS APPROACH - LANDING ABOVE WAT LIMIT
802
DITCHING
803
DIRECTION OF DITCHING
803
ACTION
803
10 140-590032-0007_Section6
806
SECTION VI - GROUND OPERATIONS
806
TABLE OF CONTENTS
806
SUB-SECTION 1 - GROUND HANDLING
808
TABLE OF CONTENTS
808
INTRODUCTION
810
AIRPLANE DE-ICING
810
REMOVAL OF SLEET AND FREEZING RAIN
813
COLD WEATHER PROCEDURES (SNOW, SLUSH AND ICE)
815
SHUTDOWN AND SECURING
816
COLD SOAK CONDITIONS
817
ENGINE START
819
GROUND MANEUVERING
820
TOWING
820
TOWING PROCEDURE
820
FIGURE 1 - TOWBAR INSTALLATION
821
PARKING AND MOORING
822
PARKING
822
PARKING PROCEDURE
822
FIGURE 2 - LANDING GEAR LOCKING PINS LOCATION
822
FIGURE 3 - THRUST REVERSER LOCKING PINS
823
COVERS AND BLANKS
824
INSTALLATION OF ENGINE COVERS
824
FIGURE 4 - COVERS AND BLANKS
824
MOORING
825
MOORING PROCEDURE
825
FIGURE 5 - AIRPLANE MOORING
825
FIGURE 6 - MAIN AND NOSE LANDING GEAR MOORING
826
GUST LOCKS
827
REMOVAL OF AILERONS AND ELEVATOR GUST LOCK
827
FIGURE 7 - GUST LOCK - AILERONS AND ELEVATORS
827
REMOVAL OF RUDDER GUST LOCK
828
FIGURE 8 - GUST LOCK - RUDDER
828
SUB-SECTION 2 - GROUND SERVICING
830
TABLE OF CONTENTS
830
INTRODUCTION
832
ENGINE GROUND RUNNING
832
ENGINE START
832
FIGURE 1 - ENGINE DANGER ZONES
833
ENGINE OIL SERVICING
834
TABLE 1: ENGINE OIL CAPACITIES
834
TABLE 2: ENGINE OIL CONSUMPTION
834
FIGURE 2 - ENGINE OIL CONTENTS VIEWING POINTS
836
FIGURE 3 - ENGINE OIL SYSTEM REPLENISHMENT DETAILS
837
THRUST REVERSERS
838
FIGURE 4 - THRUST REVERSER PINS
838
FUEL SYSTEM
839
GENERAL
839
FIGURE 5 - FUEL TANKS AND COMPARTMENTS
839
FUEL CAPACITIES
839
TABLE 3: FUEL CAPACITIES
839
APPROVED FUEL SPECIFICATIONS
840
FUEL LOADING (FIGURE 6)
840
FIGURE 6 - FUEL SYSTEM SERVICING POINTS
841
OPERATION OF THE PRESSURE REFUELING COUPLING (FIGURE 7)
842
FIGURE 7 - PRESSURE REFUELING COUPLING
843
PRESSURE AND GRAVITY FUELING
844
FIGURE 8 - WATER DRAIN TOOL
845
POWER SUPPLIES
845
GRAVITY REFUELING AND DEFUELING
856
FIGURE 9 - WING TANK FILLER CAP
864
FIGURE 10 - VENTRAL TANK FILLER CAP
865
FIGURE 11 - GRAVITY DEFUELING DRAIN ADAPTOR
866
ELECTRICAL SYSTEM
867
GENERAL
867
ENERGIZE DC BUSBARS
867
FIGURE 12 - ENERGIZING DC BUSBARS
868
FIGURE 13 - EXTERNAL GROUND POWER RECEPTACLE
869
HYDRAULIC SYSTEM
870
TANK CAPACITIES
870
TABLE 4: CAPACITIES OF RESERVOIRS
870
CHECK HYDRAULIC PRESSURE
870
RELEASE HYDRAULIC PRESSURE
870
CHECK MAIN HYDRAULIC SYSTEM RESERVOIR
870
TABLE 5: EQUIPMENT AND MATERIALS
870
REPLENISH MAIN RESERVOIR (FIGURE 15 AND 16)
871
REPLENISH AUXILIARY RESERVOIR (FIGURE 15)
871
CHARGE ACCUMULATORS (FIGURE 15)
871
FIGURE 14 - HYDRAULIC INDICATIONS
872
FIGURE 15 - HYDRAULIC SERVICING POINTS
873
FIGURE 16 - MAIN HYDRAULIC RESERVOIR
874
LANDING GEAR
875
TIRE PRESSURES
875
FIGURE 17 - VARIATION OF MINIMUM NOSEWHEEL TIRE PRESSURE WITH TAKEOFF AND LANDING WEIGHTS
876
FIGURE 18 - VARIATION OF MINIMUM MAINWHEEL TIRE PRESSURE WITH TAKEOFF AND LANDING WEIGHTS
877
WHEEL REMOVAL
878
TREAD WEAR CHECK
878
TIRE INSPECTION
878
FIGURE 19 - CONSTRUCTION OF A TYPICAL TIRE
879
PERMISSIBLE DAMAGE FOR TIRES (FIGURES 20 AND 20A)
880
TABLE 6: MAXIMUM PERMISSIBLE DAMAGE PENETRATION
880
FIGURE 20 - PERMISSIBLE TIRE DAMAGE
881
FIGURE 20A - PERMISSIBLE TIRE DAMAGE (CONTINUED)
882
WORN TIRES AND NON-PERMISSIBLE TIRE DAMAGE (FIGURE 21)
883
FIGURE 21 - NON-PERMISSIBLE TIRE DAMAGE
884
GEAR ASSEMBLIES
885
NITROGEN INFLATION
885
TABLE 7: MATERIAL REQUIRED
885
FIGURE 22 - GEAR CHARGING VALVES
886
FIGURE 23 - MAIN GEAR - PRESSURE/EXTENSION GRAPH
887
FIGURE 24 - NOSE GEAR - PRESSURE/EXTENSION GRAPH
888
OXYGEN SYSTEM
889
CHECK OXYGEN CONTENTS (FIGURE 25)
889
FIGURE 25 - FLIGHT COMPARTMENT OXYGEN SERVICES PANEL
889
REPLENISH OXYGEN SYSTEM (FIGURE 26)
890
FIGURE 26 - OXYGEN CHARGING POINT (RIGHT SIDE OF REAR FUSELAGE)
890
AIRFRAME ICE PROTECTION SYSTEM (FIGURE 27)
892
REPLENISH SYSTEM TANK
892
PRIME SYSTEM
892
PURGE SYSTEM
892
FIGURE 27 - ICE PROTECTION SERVICING POINTS
893
11 140-590032-0007_Section7
894
SECTION VII - SAFETY INFORMATION
894
TABLE OF CONTENTS
894
GENERAL
896
FAA APPROVED AIRPLANE FLIGHT MANUAL AND PILOT’S OPERATING MANUAL
896
AIRWORTHINESS DIRECTIVES
898
AERONAUTICAL INFORMATION MANUAL
898
GENERAL INFORMATION ON SPECIFIC TOPICS
902
HAZARDS OF UNAPPROVED MODIFICATIONS
903
FLIGHT OPERATIONS
904
GENERAL
904
PREFLIGHT INSPECTION
904
WEIGHT AND BALANCE
904
AUTOPILOT
905
FLUTTER
905
TURBULENT WEATHER
906
WINDSHEAR
907
FLIGHT IN ICING CONDITIONS
908
WEATHER RADAR
910
MOUNTAIN FLYING
911
VFR AT NIGHT
912
VERTIGO - DISORIENTATION
912
FLIGHT WITH ONE ENGINE INOPERATIVE
913
AIR MINIMUM CONTROL SPEED VMCA
913
BASIC SINGLE ENGINE PROCEDURES
914
ENGINE FAILURE DURING TAKEOFF
914
STALLS, SLOW FLIGHT AND TRAINING
914
SPINS
914
VORTICES - WAKE TURBULENCE
916
TAKEOFF AND LANDING CONDITIONS
916
MEDICAL FACTS FOR PILOTS
917
GENERAL
917
FATIGUE
917
HYPOXIA
917
HYPERVENTILATION
918
ALCOHOL
919
ALCOHOL OR DRUGS
919
DRUGS
920
SCUBA DIVING
920
CARBON MONOXIDE AND NIGHT VISION
920
DECOMPRESSION SICKNESS
920
A FINAL WORD
921
12 140-590032-0007_supp_pack
922
Hawker 800XP Pilot's Operating Manual P/N 140-590032-0007 Supplement Pack
922
Section VIII - Supplements
923
Log of Supplements - August 2, 2006
923
4
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Hawker Beechcraft Hawker 800XP Specifications
General
Brand
Hawker Beechcraft
Model
Hawker 800XP
Category
Aircrafts
Language
English
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