AFM LIMITATIONS Flashcards
(52 cards)
RVSM equipment on G7500
1 Autopilot 1 Altitude alert 1 Altitude reporting Transponder 2 X Air Data Syst 2 X Pitot tube heater
Structural operational Weights
MRW MTW MLW MZFW Min Flight W
MRW 52.208 kg - 115.100 lbs MTW 52.095 kg - 114.850 lbs MLW 39.735 kg - 87.600 lbs MZFW 30.617 kg - 67.500 lbs MFW 27.216 kg - 60.000 lbs
Procedure for takeoffs and landings above MLW near body’s of water
Outflow valve no2 close and one of the packs off
Maximum altitude for takeoff and landing
10 000 ft
Max Outside Temp for takeoff and landing
55C (131F)
ISA +40
Minimum Outside Temp approved for takeoff
-40°C
Maximum Operating Altitude
51 000 ft
Cowl Anti-ice must be ON
OAT is 10°C (50°F) or less and visible moisture in any form present, visibility 1500 m (1 mile) or less, rain, snow, slush or any form of precipitation present
Ice shedding engine procedure
When vibrations are detected
Increase engine thrust to 50% N1 for 5 sec minimum until engine vibrations return to normal
Perform this procedure every 18 min prior to takeoff
If takeoff is imminent, do not reduce the power but rather increase to takeoff settings
In flight Cowl Anti-Ice conditions
In flight cowl Anti-ice conditions 10C (50F) or bellow with visible moisture
Except when SAT is -40C (-40F)
Wing Anti-Ice
OAT is 5°C (41°F) or less and visible moisture or
TAT 10°C (50°F) or less - flying
NO Anti-Ice at or below -40°C (-40°F) or above TAT +10°C
Super-cooled Large Droplets SLD
Flight into know SLD IS PROHIBITED
SLD is indicated by accumulation of ice on the cockpit windows
Wing and Cowl Anti-Ice must by ON
Max runway slop for Takeoff and Landing
+/- 2%
Tailwind for Takeoff and Landing
10 kts
Cold Weather
If airplane is exposed at temps…….
-20°C the airplane should be operated according to FCOM VOL1 capt10 Adverse weather / Cold Weather Ops
Operation of avionics displays is prohibited in hot temp
Excess of 40°C for 30 min
North Pole OPS
Operations North of 89.5 and South of 89.5 are PROHIBITED
ENGINE
GE PASSPORT 20 19BB1A
What is the maximum landing mass for the airplane? A. 95,000 lb (43,091 kg) B. 78,600 lb (35,652 kg) C. 87,600 lb (39,735 kg) D. 93,750 lb (42,524 kg)
C
What is the maximum airspeed at which it is safe to extend/retract the landing gear? A. 190 KIAS B. 200 KIAS C. 250 KIAS D. 300 KIAS
B
Engine operating limits
ITT START
IDLE
TAKEOFF
MAX CONT
START on ground 750°C
in flight 875°C
IDLE. 65.9% minimum 995°C
TAKEOFF. 1035°C @ 103.7% N1 & 114.9% N2
MAX CONT 995°C @103.7% N1 & 114.9% N2
T/O 5 min all engines 10 min one engine out
1077°C for 15 sec in case of Go- Around
975°C for high power fuel cut or quick windmill relight
Engines STARTS are not permitted with tailwinds more then …..
20 KTS
The starter MUST NOT be used if RPM exceeds
56% N2
Normal Engine start tries?
2 consecutive cycles of 5 min each with 5 min cool down after each one
After the 3 one up to the 10 trial a 15 min cool down in between cycles