F100 Flashcards
Max operating altitude
35000ft
Max take off and landing altitude
8000ft
Max operating temperature
ISA + 35˚
Max temperature on the ground with avionics cooling inop
44˚
Max ramp weight F100
44680kg
(230kg above MTOW)
UQD - 46040kg (extra 1360kg)
Max take off weight F100
44450kg
UQD - 45810kg (extra 1360kg)
Max landing weight F100
39915kg
Max zero fuel weight F100
36740kg
UQW - 37420kg (extra 680kg payload)
Max flap extension altitude
FL200
Max gear extension altitude
FL250
Vmo/Mmo
320/.77
Vra
250/.65
Vfe8
250kt
Vfe15
220kt
Vfe25
220kt
Vfe42
180kt
Vlo/Vle
200kt
Max lift dumper extend speed
170kt
Max speed for side window operation (demonstrated)
160kt
Max XWC
35kt
Max XWC wet
30kt
Max TWC
10kt
Max TGT - start
F100 - 740˚ (2 seconds)
F70 - 700˚ (2 seconds)
Max TGT - takeoff
F100 - 850˚ (5 minutes, 10 minutes OEI)
F70 - 800˚ (5 minutes, 10 minutes OEI)
Max TGT - continuous
F100 - 795˚
F70 - 735˚
Minimum idle (N2 should not fall below)
47.9%
Max fuel asymmetry in flight
1000kg
If >350kg, max XWC 20kt
Minimum height for autopilot use - takeoff
35ft AGL
Minimum height for autopilot use - level flight/cruise
700ft AGL
Minimum height for autopilot use - NPA
250ft
Max XWC ILS Cat II
25kt
Max XWC AUTOLAND Flap42
25kt
Max XWC AUTOLAND Flap25
15kt
Max TWC ILS Cat II
10kt
Max TWC AUTOLAND
10kt
Max total wind ILS Cat II
30kt
Max wind AUTOLAND Flap42
25kt
Max wind AUTOLAND Flap25
15kt
ENGINE START FAULT
START PB … OFF
If alert persists:
- BLEED … ALL OFF
- FUEL LEVER … SHUT
EMERGENCY DESCENT
ATS … DISCONNECT
THRUST LEVERS … IDLE
SPEED BRAKE … OUT
FLIGHT MODE PANEL … 10,000FT(/MEA) + LVLCH + MMO/VMO
ON GROUND EMERGENCY EVACUATION
PARK BRAKE ... SET FLAPS ... FULLY DOWN REVERSE THRUST LEVERS ... FULLY DOWN LIFT DUMPERS ... DISARM BOTH FUEL LEVERS ... SHUT
BOTH ENGINES FLAME OUT
IGNITION … RELIGHT
JET-PIPE FIRE
FUEL LEVER ... SHUT BLEED AIR PRESS ... ESTABLISH START PB ... ON ENGINE SELECTOR ... AS REQD Motor engine until fire extinguished or TGT decreases START PB ... OFF
HOT START
If it is anticipated that the TGT start limit (740c) will be exceeded:
- FUEL LEVER … SHUT
After approx. 30 sec:
- START PB … OFF
N2 STAGNATION
If during or after starting, N2 stagnates in combination with a rising TGT:
- FUEL LEVER … SHUT
- START PB … CHECK OFF
LOW IDLING N2
If N2 RPM stabilises below minimum idling (47.9%) advance the thrust lever slowly until minimum idling RPM is reached.
Monitor TGT.
INTERRUPTED START
If a start is interrupted before the fuel lever is selected to OPEN:
- START PB … OFF
NO LIGHT UP
If an engine fails to light up within approx. 20 sec from selecting the fuel lever to OPEN:
- FUEL LEVER … SHUT
After approx. 30 sec:
- START PB … OFF
When shall you not use Flex for take-off?
Contaminated runway Icing conditions (TAT +6˚-25˚ + visible moisture) Windshear Lift dumpers/anti-skid INOP Wind/tail icing ON
Best angle of climb speed
Green dot
Best rate of climb speed
250/.65
Max FOB
10256kg
UQD & F70 - 10692 (extra 430kg fuel)
Max ramp weight F70
41955kg
Max take off weight F70
41730kg
Max landing weight F70
36740kg (same as F100 MZFW)
Max zero fuel weight F70
33565kg
Max TGT - relight
780˚
Max TGT - reverse thrust
F100 - 850˚
F70 - 800˚
Max fuel asymmetry on the ground
500kg for manoeuvring if >39000kg
1000kg for manoeuvring if <39000kg
Minimum height for autopilot use - GS/LOC (no autoland)
80ft
RVSM - notify ATC if:
A primary altimetry system fails
Crosscheck between primary altimetry systems >200ft
Failure of AP alt hold function
Loss of thrust necessitating descent
Any equipment failure resulting in an inability to maintain altitude