AFM LIMITATIONS Flashcards
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)
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
Fuel imbalance
Ground
Flight
On the ground / take off / landing
600 LBS
Flight 1.100 LBS
Min Fuel for GO-AROUND
750 LBS / each Wing
Min Fuel for Wing to Wing transfer
2500 LBS / each Wing
Fuel crossfeed …. TO & Landing
Bellow 10.000 ft dual engine ops?
Must be OFF for Take Off & Landing
Must be off below 10.000 ft
OIL Temp
Min for START
Min before selecting TO power
Maxim for Cont Ops
Transient Ops
-40°C
+43°C
+160°C
+160°C - +165°C
Max Oil consumption
0.31 Q/Hour
Operation of the oil replenish syst
Prohibited with OAT -12 or colder
The Oil replenish syst must contain for take off at least
2.5 Q
APU
Type
SPU 300
APU
MAX RPM
105%
APU
MAX EGT
Start
Normal OPS
1032°C
718°C
APU
Max Ops altitude
51000 ft
APU
Min ambient temp for start a cold soak on the ground
-40°C
APU
Max number of start / hour
3
APU
Max starting Altitude
45000 ft
APU
Bleed Air Extraction Limit
Altitude
Temp on ground
25000 ft
+48°C OAT
What is the maximum speed for flap 4 extension?
A. 200KIAS
B. 185KIAS
C. 210KIAS
D. 220KIAS
B
The airplane has a maximum zero fuel weight of:
A. 67,500 lb (30,617 kg).
B. 76,000 lb (34,473 kg).
C. 78,600 lb (35,655 kg).
D. 65,000 lb (29,483 kg).
A
The airplane has a maximum takeoff weight of:
A. 114,950lb (52,140 kg).
B. 115,100 lb (52,209 kg).
C. 114,850lb (52,095 kg).
D. 114,650 lb (52,001 kg).
C
Minimum oil temperature for starting an engine is beforetakeoff power can be applied
A. -30°C, +33°C
B. -30°C, +43°C
C. -40°C, +33°C
D. -40°C, +43°C
D
Maximum speed for turbulence penetration is:
A. 265 KIAS from sea level to 8000 ft, linearly increasing to 285 KIAS at 10.000 ft
B. 285 KIAS from sea level to 8000 ft, linearly increasing to 300 KIAS at 10.000 ft.
C. 300 KIAS from sea level to 8000 ft, linearly increasing to 335 KIAS at 10,000 ft.
D. 265 KIAS from 10,000 ft and above or 0.80 Mach, whichever is lower.
A
Maximum speed for gear manoeuvre is …… and to operate with gear extended is …….
A. 200, 250
B. 200,225
C. 250, 185
D. 250, 210
A
The minimum ambient air temperature approved for takeoff is:
A. -45°C
B. -40°C
C. -35°C
D. -30°C
B
Auxiliary pressurization (AUX PRESS) system operations are prohibited at altitudes greater than:
A. 30,000 ft
B. 37,000 ft
C. 41,000 ft
D. 45,000 ft
C
APU bleed air extraction is limited to:
A. 45,000 ft
B. 25,000 ft
C. 51,000 ft
D. 23,000 ft
B
APU bleed air extraction on the ground for ECS operation is limited to what OAT?
A 50°C
B. 40°C
C. 43°C
D. 48°C
D
Engine START inflight limitations
Via APU speed below 250 kts up to FL 230
CrossBLEED below 250 kts up to FL300
Windmill assist speed above 250 kts N2 greater 7.5% up to FL 300
Flying an approach with a glide path greater than ….. degrees is prohibited
More then 5.5 degrees is prohibited
Between 3.5 and 4.5 could be flown with Supp. 8
Between 4.5 to 5.5 degrees with Supp 20
