Hawker 800/900XP Flashcards
ABORTED TAKE OFF Memory items
THRUST LEVERS - CLOSE
BRAKES - APPLY
AIR BRAKES - DEPLOY
THRUST REVERSERS - DEPLOY
ENGINE FAILURE ABOVE V1 Memory items
LANDING GEAR - UP
MAIN AIR VALVES - CLOSE
F/DK VALVE - CLOSE
DOUBLE ENGINE FAILURE Memory item
ENG IGNITION 1 & 2 - ON
THRUST LEVERS - CLOSE
CREW OXYGEN - DON MASKS, IF ABOVE 15000 ft
MIC SELECTOR - MASK/OXY MIC, IF ABOVE 15000 ft
ENGINE INDICATIONS - MONITOR
OIL LOW PRESSURE Memory items
OIL PRESSURE - CHECK GAUGE READING
If below:
Hawker 800 XP: 25 PSI
Hawker 900 XP: 49 PSI
HP cock - CLOSE
ENGINE FIRE ON GROUND Memory items
START POWER (starting only) - PUSH FOR ABORT
HP COCK (affected engine) - CLOSE
LP COCK (affected engine) - CLOSE
ENGINE EXT (affected engine) - SHOT 1
ENGINE FIRE BELOW V1 Memory items
THRUST LEVERS - CLOSE
BRAKES - APPLY
AIR BRAKES - OPEN
THRUST REVERSERS - DEPLOY
ENGINE FIRE ABOVE V1 Memory items
LANDING GEAR - UP
MAIN AIR VALVES 1 & 2 - CLOSE BOTH
F/DK VALVE - CLOSE
ENGINE FIRE IN FLIGHT Memory items
THRUST LEVERS (affected engine) - CLOSE
If warning persists:
HP COCK (affected engine) - CLOSE
LP COCK (affected engine) - CLOSE
ENGINE EXT (affected engine) - SHOT 1
If engine shutdown occurs during initial climb:
MAIN AIR VALVES 1 & 2 - CLOSE BOTH
F/DK VALVE - CLOSE
APU FIRE Memory items
STOP SWITCH - PUSH
MASTER SWITCH - OFF
FIRE EXTINGUISHER SWITCH - LIFT GUARD / SELECT ON
If warning persists:
APU FIRE WARNING CB - PULL (DA-D N6)
INADVERTENT THRUST REVERSER DEPLOYMENT DURING TAKE OFF Memory items
Below V1 - take off aborted:
THRUST LEVERS - CLOSE
BRAKES - APPLY
AIR BRAKES - OPEN
THRUST REVERSERS - DEPLOY
Above V1 - take off continued:
LANDING GEAR - UP
MAIN AIR VALVES 1 & 2 - CLOSE BOTH
F/DK VALVE - CLOSE
INADVERTENT THRUST REVERSER DEPLOYMENT IN FLIGHT Memory items
HP COCK (affected engine) - CLOSE
DEPRESSURIZATION Memory items
<ul><li>CREW OXYGEN- DON MASKS</li><li>MIC SELECTOR - MASK / OXY MIC</li></ul>
EMERGENCY DESCENT Memory items
<strong>PF:</strong><ul><li><strong>“EMERGENCY DESCENT”</strong></li><li>ATTITUDE - ROLL into moderate bank (if able) & PITCH nose down</li><li>THRUST LEVERS - CLOSE</li><li>SPEED - MMO / VMO UNLESS STRUCTURAL DAMAGE</li><li>AIR BRAKE - OPEN</li><li>MANUAL PAX MASKS - DROP (if needed)</li></ul><br></br><strong>PM:</strong><ul><li>CABIN NOTICES - ON</li><li>TAXI LIGHTS - ON</li><li>ATC - CALL MAYDAY</li><li>TRANSPONDER - 7700</li><li>PASSENGER - CHECK FOR O2 SUPPLY</li></ul>
FUSELAGE FIRE OR SMOKE Memory items
<ul><li>CREW OXYGEN - DON MASKS (100% EMERG)</li><li>MIC SELECTOR - MASK / OXY MIC</li><li>SMOKE GOOGLES - DON AND VENT</li><li>CABIN NOTICES - ON</li></ul>
SMOKE FROM AIR CONDITIONING DUCTS Memory items
<ul><li>CREW OXYGEN - DON MASKS (100% EMERG)</li><li>MIC SELECTOR - MASK / OXY MIC</li><li>SMOKE GOOGLES - DON AND VENT</li><li>CABIN NOTICES - ON</li></ul>
ELECTRICAL FIRE OR SMOKE Memory items
<ul><li>CREW OXYGEN - DON MASKS (100% EMERG)</li><li>MIC SELECTOR - MASK / OXY MIC</li><li>SMOKE GOOGLES - DON AND VENT</li><li>CABIN NOTICES - ON</li></ul>
REAR EQUIPMENT BAY OVERHEAT Memory items
<ul><li>MAIN AIR VALVES 1 & 2 - CLOSE</li><li>F/DK VALVE - OPEN FULLY</li></ul>
HIGH PRESSURE AIR OVERHEAT Memory items
<ul><li>MAIN AIR VALVE (affected engine) - CLOSE</li><li>F/DK VALVE - CLOSE</li></ul>
BRAKE FAILURE Memory items
<strong>PF:</strong><ul><li>APPLY REVERSE</li><li>BRAKE PEDALS - RELEASE</li><li>WHEEL BRAKE LEVER - EMERGENCY</li><li>BRAKE PEDALS - APPLY GENTLY (one continuous application)</li></ul><br></br><strong>PM:</strong><ul><li>CHECK BRAKE PRESSURE</li><li>ADVISE PF IF FULL REVERSE IS NEEDED</li></ul>
EVACUATION Memory items
<strong>LP:</strong><ul><li>PARK BRAKE - PARK</li><li>HP & LP COCKS - CLOSE</li><li>PAX & ATC - “EVACUATE”</li><li>BATTERY - OFF</li></ul><br></br><strong>RP</strong> (when evacuation is ordered from commander):<ul><li>EMERGENCY LIGHTS - MAN</li><li>DUMP VALVE - OPEN</li><li>HP & LP COCKS - CHECK OFF</li><li>PAX - “EVACUATE”</li></ul>
UNRELIABLE AIRSPEED, ALTITUDE OR PITCH Memory items
<ol><li>Both crew must verify all three ATTITUDE INDICATORS to confirm aircraft state.</li><li>If the aircraft state is uncertain, crew must <strong>fly pitch and thrust</strong> to recover a safe flight phase. Display GPS altitude on <strong>FMS PROG PAGE 3/3 - AIR DATA</strong> to confirm a state of CLIMB, DESCENT OR CRUISE. Use the table attached as guidance.</li><li>Check probe, vane or pitot/static <strong>heat ON. </strong>When memory items are completed push the relevant ADC transfer switch to REV.</li></ol>
STALL Memory items
<strong>PF:</strong><ul><li><strong>”STALL - FULL THRUST”</strong></li><li>A/P - OFF</li><li>NOSE DOWN PITCH CONTROL - AS NEEDED</li><li>BANK - WINGS LEVEL</li><li>AIR BRAKES - RETRACT</li><li>WHEN OUT OF STALL - RETURN TO DESIRED FLIGHT PATH</li></ul><p><br></br></p><p><strong>PM:</strong></p><ul><li>Monitor flight instruments, guide if needed.</li><li>execute commands from PF</li></ul>
NOSE HIGH Memory items
<strong>PF:</strong><ul><li>”<strong>NOSE HIGH - FULL THRUST”</strong></li><li>APPLY FULL THRUST while</li><li>REDUCE PITCH TO ZERO and</li><li>ROLL TO NEAREST HORIZON</li></ul><p><br></br></p><p><strong>PM:</strong></p><ul><li><strong>”NOSE HIGH”</strong></li><li>Monitor flight instruments</li><li>Guide PF as needed</li></ul>
UNUSUAL ATTITUDES - NOSE HIGH Memory items
PF:
- “NOSE HIGH - FULL THRUST”
- APPLY FULL THRUST while;
- REDUCE PITCH TO ZERO and
- ROLL TO NEAREST HORIZON
PM:
- “NOSE HIGH”
- Monitor flight instruments
- Guide PF as needed
UNUSUAL ATTITUDES - NOSE LOW Memory items
PF:
- “NOSE LOW - IDLE THRUST”
- REDUCE THRUST TO IDLE while;
- USE AIR BRAKES IF NEEDED
- ROLL TO NEAREST HORIZON (WINGS LEVEL)
- RAISE NOSE/PITCH TO ZERO
PM:
- “NOSE LOW”
- Monitor flight instruments
- Guide PF as needed
CREW INCAPACITATION Memory items
If the other crew member does not respond on a challenge call the 2:nd time or if incapacitation is suspected:
- Call “I HAVE CONTROLS” and put a hand on the other crew member’s shoulder to trigger a response. If no response (pilot incapacitated):
- Remove crew member from controls
- give oxygen
- call MAYDAY and land at nearest suitable airport
EGPWS (“TERRAIN”, “PULL UP” AUDIO ALERT) Memory items
PF:
- “TERRAIN - FULL THRUST”
- Put hand on yoke and throttles
- Disconnect A/P and climb to safe altitude
PM:
- Push APR Override
- Monitor TAWS display, give guidance to PF
- Advise the best escape route to PF (LEFT or RIGHT)
TCAS TA Memory items
PF:
- “TCAS, I HAVE CONTROL”
- Be prepared to disconnect the A/P and put hands on the controls and thrust levers
PM:
- Monitor TCAS display, zoom in if needed
TCAS RA Memory items
PF:
- “AUTOPILOT OFF”
- Disconnect A/P and follow TCAS green fly-to commands
- Reduce or increase thrust accordingly
- Ask PM to remove flight director (FD) if needed
PM:
- Call ATC “TCAS RA”
- Deselect lateral & vertical guidance (FD’s OFF)
SEVERE WINDSHEAR WARNING Memory items
PF:
- “WINDSHEAR - FULL THRUST”
- Apply full thrust
- Pitch up 15 degrees initially, allowing airspeed to decrease if necessary, then up to stick shaker as pitch limit, if required
- Do not change configuration (flaps & gear) until out of windshear
PM:
- Select APR Override
- Monitor flight instruments, and give guidance to PF until out of windshear
- Call ATC for a revised clearance if needed
VOLCANIC ASH Memory items
PF:
- “VOLCANIC ASH”
- REDUCE THRUST
- 180° TURN
PM:
- CALL ATC
- Monitor flight instruments, read checklist for volcanic ash
SEVERE ICING ENCOUNTER Memory items
PF:
- “SEVERE ICING”
- DISCONNECT AUTOPILOT
- LEAVE SEVERE ICING CONDITIONS
- The quickest way of exit icing conditions is to climb or descent a few thousand feet.
PM:
- CALL ATC and REQUEST CLEARANCE
PED SMOKE or FIRE RESPONSE Memory items
PF:
- “I HAVE ATC”
- CALL MAYDAY
- LAND AS SOON AS POSSIBLE
PM:
- FIRE GLOVES - ON
- Put device in fire proof bag or metal waste bin, soak with large amount of water (no alcohol)
Vmo ventral tank not empty
280 KIAS
Air Brakes speed limit (flaps 0 only)
No limit
Maximum tailwind (takeoff and landing)
10 kt
Maximum tailwind (takeoff and landing)
13000 ft
Maximum field pressure altitude for takeoff and landing (aircraft equipped with high datum)
13000 ft
Maximum altitude flaps 15 (descent and holding)
15000 ft
Maximum transient engine oil temperature
149˚C (2 min)
Maximum slope for takeoff
2 % uphill/downhill
Maximum load factor flaps extended
2.0 g
Single rejected takeoff < 90 KIAS waiting period
25 min
Two or more rejected takeoff < 90 KIAS waiting period
45 min
Rejected takeoff > 90 KIAS requirement
Brake inspection
Maximum demonstrated crosswind
30 kt
Minimum wing fuel required with fuel in the ventral tank
3450 lb/side
APU Maximum operating EGT
1350 ˚F
APU Maximum operating altitude
0 - 30000 ft pressure altitude
APU Maximum starting altitude
0 - 20000 ft pressure altitude
APU Maximum transient EGT
1400 to 1500 ˚F for 15 seconds maximum
APU Maximum generator electrical load
0.8 maximum continuous
1.2 maximum 10 seconds
Maximum forward baggage compartment weight
250 lbs
Maximum continuous N1
100 %
Maximum N2 takeoff
Hawker 800 XP: 100.8%
Hawker 900 XP: 101%
Maximum N2 takeoff (APR Operating)
Hawker 800 XP: 100,8%
Hawker 900 XP: 101%
Maximum continuous ITT
Hawker 800 XP: 968 ˚C
Hawker 900 XP: 991 ˚C
Maximum cruise ITT
932 ˚C
Maximum ITT starting and relighting (unlimited time)
Hawker 800 XP: 978 ˚C
Hawker 900 XP: 994 ˚C
Engine oil pressure limit (minimum idle)
Hawker 800 XP: 25 psi
Hawker 900 XP: 49 psi
Engine oil pressure limit (takeoff, maximum continuous and climb)
Hawker 800 XP: 38-46 psi
Hawker 900 XP: 65-80 psi
Engine oil pressure limit (maximum transient)
Hawker 800 XP: 55 psi (3 minutes)
Hawker 900 XP: 100 psi (3 minutes)
Va
196 kts
Fuel capacity wing tanks
8500 lbs
Engine model
Hawker 800 XP: TFE731-5BR-1H
Hawker 900 XP: TFE731-50R
Vfe flaps 45˚
165 kts
Maximum permissible operating altitude
41000 ft
Minimum ZFM
14120 lbs
Maximum ZFM
18450 lbs
Maximum ramp mass
28120 lbs
Fuel capacity ventral tank
1500 lbs
Mach trim fail speed limit
Mach 0.73 unless autopilot is ON
Maximum cabin press differential
8.55 psi
Minimum fuel temp inflight (JET A)
-38˚C
Max continues engine oil temp
127˚C up to 30,000’
140˚C 30,000 feet and above
Minimum engine oil temperature for starting
-40˚C
Bird strike speed up to 8000ft (window heat on for required time)
280 kts
Fuel carried in the ventral tank shall be transferred into the wing tank when the fuel level in each wing tank reduces to ____ pounds
3300 lbs
TKS fluid has a total quantity of _____ US gal
10 US gal
Maximum temperature for flight
ISA +35˚C
Anti ice low quantity remaining fluid (in minutes)
30 min
Maximum fuel temperature
57˚C
Minimum air temperature for enroute
-75˚C
Auxiliary hydraulic system reservoir quantity
6 U.S pints
MTOM
28000 lbs
Minimum temperature for take-off and landing
-40˚C
Maximum negative differential pressure
-0.5 psi
Ventral tank fuel restriction before flight
Completely full or empty
Maximum fuel imbalance main tanks
500 lbs
Minimum oil temperature for take off
+30˚C
Main hydraulic system pressure
3000 psi
What is the main hydraulic system pressure?
3000 psi
What are the APU starter cranking limits?
30 seconds ON/ 3 minutes OFF, after third attempt 30 minutes OFF
What is the minimum fuel temperature for takeoff (JET A)?
-35˚C
What is Vlo / Vle?
220 KIAS
What is the maximum altitude for gear or flaps extended?
20000 ft
What is the maximum landing mass?
23350 lbs
What is Vmo with the ventral tank empty?
335 KIAS up to 12000 ft reducing by 1 knot per 680 ft to 310 knots at 29000 ft
What is Vfe at 15˚?
220 KIAS
What is Vfe at 25˚?
175 KIAS
What is Vfe at 45˚?
165 KIAS
What is the maximum load with flaps retracted?
2.73 g
What are the engine starter cranking limits?
30 seconds ON/1 minute OFF, after third attempt 30 minutes OFF
What is the maximum continuous engine generator load?
300 amps
What is the maximum transient engine generator load?
400 amps (2 minutes)
What speed must thrust in excess of reverse idle not be selected below?
50 KIAS, except in an emergency.
When should the inlet anti-icing not be used above 50° F (10° C)?
For more than 10 seconds
What is the aircraft length?
51 ft (15.59 m)
What is the aircraft height?
17 ft 5 inches (5.31 m)
What are the lengths of the 800 XP and 900 XP aircraft?
800 XP: 15.66 m, 900 XP: 16.56 m
Wingspan of Hawker 800 XP
15.66 m
Wingspan of Hawker 900 XP
16.56 m
Aircraft wheel track width
9 ft 2 inches (2.79 m)
Maximum nose wheel angle (using cockpit control)
45° each side
Minimum turning radius using nose wheel steering (outside wingtip)
14.8 m
Minimum turning radius using nose wheel steering (inside wheel)
4.8 m
For a TKS tank indicating full, priming and protection for at least ___ minutes is provided
85 minutes
