Limits Flashcards
Max engine ground start TGT?
Time limit?
700
Momentary
Max engine air start relighting TGT?
Time limit?
850
Momentary
Max engine takeoff LP
HP
TGT
Time limit
101.1
99.6
900
5 mins. Two engine, 10 mins. Single engine
Max continuous LP
HP
TGT
Time limit
101
98.9
860
Unrestricted
Max engine over speed LP
HP
TGT
TIME LIMIT
101.5
99.8
905
20 seconds
Max reverse thrust LP
TIME LIMIT
70
30 seconds
Max Zero fuel weight
54,500
Max ramp weight
91,400
Max takeoff weight
91,000
Max landing weight
75,300
Fuel imbalance for takeoff
1,000 lbs
Fuel imbalance in-flight
2,000 lbs
Max fuel
41,300 lbs
Aircraft length
96’ 5”
Aircraft wingspan
93’ 6”
Aircraft height
25’ 11”
Aircraft nosewheel to MLG
45’
MLG width
14’ 4”
Elevator width
35’ 2”
When HMG is in operation, speed brakes may be used provided operation is ?
Slow operation, approx 3 seconds for full range movement
Do not operate HMG when normal AC power is available, except?
For L or R ESS DC bus failure
Max cabin diff for taxi/takeoff/landing
0.3 PSID
Max cabin pressure diff
10.48 PSID
When aircraft is static on the ground, stabilized engine operation in the keep out zone of what LP RPM, is prohibited.
Any accel-decel through this band must not exceed 10 seconds.
66 to 80% RPM
Max ZFW
54,500 lbs
Max ramp weight
91,400 lbs
Max takeoff
91,000 lbs
Max landing
75,300
Max fuel imbalance for takeoff
1,000 lbs
Max fuel imbalance in-flight
2,000 lbs
Max fuel load
41,300 lbs
Max TGT prio to ground start
150 deg. C
When the HMG is in operation, speed brakes may be used provided operation is ? (Approx. ? seconds for full range movement
Slow, 3 seconds
Max cabin pressure diff
10.48 PSID
Max cabin press diff taxi/takeoff/land
0.3 PSID
Keep out zone
66-80% while static, on the ground. Any accel/decel must not exceed 10 seconds.
Takeoff in ? Control mode is prohibited
Alt
X-wind above 20 knots, accel to takeoff power, fan speed limited to <?% until a fwd speed of ? Knots
66%
20 knots
Add ? Feet to required field length for slam takeoff
600’
X-wind >20 kts, forward speed >20 kts, a ? Acceleration is required.
Slam
Max x-wind for takeoff & land
28 knots
Once takeoff had commenced, use of tiller >? Knots, is not recommended
60 knots
Max x-wind for engine start
30 knots
Max tailwind for engine start
20 knots
Weather radar, ? Feet from refueling ops
300’
Min crew
2 pilots
Max pax
19
Max occupants
22
Slope
+2% uphill
-2% downhill
Max eng oil temp
160 deg C
Min eng oil temp for start
-30 deg C
Min eng oil temp for takeoff power
20 deg C
Min Eng oil press for T/O (<72.3 HP)
35 PSI <72.3 HP
Min oil press for T/O (>90 Hp)
45 PSI >90 HP
Eng oil press continue flight (<72.3 HP)
25 PSI <72.3 HP
Eng oil press continue flight (>90 HP)
35 psi >90HP
Engine starter duty limits
3, three minute attempts, 15 seconds between each then 15 minutes off
The starter may be reengaged at HP RPM speeds up to starter cut out of
42% HP RPM
All operable fuel boost pumps must be selected “?” for ??? phases of flight unless fuel balancing is in progress
On for all
Engines will suction feed at or below ? feet
20,000’
Use of T/R’s for power back is/is not approved?
Is not
Minimum fuel tank temp
-37 deg C
Max fuel tank temp
+54 deg C
10 deg flaps speed
250 knots/.60 mt
20 deg flaps speed
220kcas/.60mt
39 deg flaps speed
170 kcas/.60 mt
Use of speed brakes is/is not allowed with gear down and/or full flaps?
Is not
Ground spoilers may be inop if ? Is operative! 20 deg flaps are used, and wing anti-ice systems are not used. See MEL
Anti-skid
If a touch-and-go landing is to be performed, the ground spoiler switch must be ? and manual spoiler landing distances must be taken into account.
Off
Max landing gear altitude
20,000 MSL maximum
Normal ops landing gear speed (VLO)
225 kcas/.70 mt
Normal ops landing gear extended speed (VLE)
250 kcas/.70mt
Landing gear blowdown speed?
Once gear extended?
175kcas
250kcas/.70mt
Anti-skid may be inop provided? See MEL
Dry rwy, ground spoilers operative, flaps 20, cowl & wing anti-ice not used.
Airspeed limit FL290-320
0.85
Airspeed limit FL320-440
0.885
Airspeed limit FL440-510
0.86
Vmo above 8,000’
340 kcas
Vmo below 8,000
300kcas
Minimum control airspeed (Vmca)
112kcas
Minimum control speed landing (Vmcl)
110kcas
Minimum control speed ground (Vmcg)
107kcas at sea level
Minimum control speed ground (Vmcg)
.86kcas at 15,000’
Vmcg decreases linearly at approx. ? Knot per ? Ft from sea level to 15,000
1 knot per 1,000’
Maneuvering speed (Va)
206kcas
Turb. Penetration speed (Vb) > 10,000
270kcas/.80mt
Turb. Penetration speed (Vb) <10,000’
240kcas
Holding speed in icing conditions
160kcas
Minimum Mach trim inop.
0.80mt
Tire speed limit
195.5 kts
Yaw damp inop >10,000’ ft max
260kcas/.80
Yaw damp inop. <10,000’ max
250kcas
Yaw damps inop. >20,000 ft. minimum
210kcas
Yaw damp inop. <20,000’
See chart AOM Vol 1
Max airport operating altitude
14,500
Max airport with HLFE system fitted
15,000
Max operating altitude
51,000
Single pack operations
48,000
Internal baggage door open
Above 40,000 ft for 5 mins
Internal baggage door open with one Pack
One ECS PACK, no entry >45,000 ft
Maximum yaw damp inop altitude
45,000
APU max operating altitude
45,000’
APU guaranteed start altitude
39,000
(May start up to 43,000)
APU Electrical load
100% sea level up to 45,000’
APU may be used for starter assisted air starts below ? Feet. However, max altitude for an engine air start is ? Feet.
30,000
25,000
APU max start TGT
1,050
APU max running TGT
732
APU max rotor speed
106%
Continuous operation of the APU starter when powered by airplane batteries:
? consecutive start attempts followed by a ? hour cooldown
3 consecutive start attempts followed by a 1 hour cooldown
Continuous operation of APU starter when powered by external DC cart:
Max of ? start attempts with a ? minute cool down between each attempt. ? hour cool down after 3rd attempt
Successful consecutive starts limited to ? at ? minute intervals per start
Max of 3 start attempts with a 15 minute cool down between each attempt. 1 hour cool down after 3rd attempt.
Successful consecutive starts limited to 6 at 10 minute intervals per start
What conditions do we turn on Cowl anti-ice ?
SAT 10 deg. C or below and visible moisture
When do we turn on wing anti-ice?
Icing conditions are imminent or immediately upon detection
Max engine fuel temp
140 C
Fuel temp up to ? for a max of ? minutes is permissible
165 C , 15 mins
Minimum engine fuel temp
-40 C
Speed brakes are not allowed when landing gear is ? and/or ?
Gear extended and/or full flaps
Flaps 0 flight load
-1 to 2.5
Flaps 10 or 20 flight load
0 to 2.0 up to max takeoff weight
Flaps 39 flight load < 75,300 lbs
0 to 2.0
Flaps 39 flight load > 75,300 lbs
0 to 1.5
Do not operate HMG when normal ? power is available, except as provided for in L or R ? failure.
AC
ESS DC bus failure
With a single nine inop, select ? Only as the TCAS operating
TA only
Mach trim inop
.80 MT maximum
Autopilot minimum engage height on takeoff
200’ AGL
Autopilot minimum disengage height for ILS, MLS, or LPV approach
60’ AGL
Autopilot minimum disengage height for MDA/DA from LNAV approach
50’ below MDA/DA
Autopilot minimum demonstrated altitude loss for coupled go-around
60’
Auto-throttles are available from takeoff to landing except?
Single engine approach
Minimum flight crew
Pilot and copilot
Maximum passengers
19
Max occupants
22
Max slope for takeoff and landing
+2% uphill and -2% downhill
APU ? Ground ops are prohibited
Ground
APU use in flight prohibited except the following
Dual engine failure
Dual generator failure
Single engine failure
Single generator failure
The APU may be operated in-flight for the purpose of “bleeds off” takeoff, up to a max of ? Ft
5,000’ AGL
Dispatch is ? Premiered with any engine generator inop
Not
