Limitations Flashcards
Single Point Usable Fuel
14150 Total
L/R 7075
Gravity Usable Fuel
13000 Total
6500 L/R
Min fuel for GA
500 lbs per side
Fuel Transfer Limitations
Power and gravity shut off valves OFF for takeout
Single Point fueling
55 psig
-8 psig
Approved fuels
Jet A
Jet A1
JP 5
JP 8
Jet B & JP 4 approved up to 16000ft
Landing gear altitude
Not extend above 18000ft
Spoilers
- Not extended in flight at airspeeds below approach speed +8 knots.
- Not extended in flight below 500AGL
Flaps
Not too be used above 18000ft.
Flaps 10 - 210kts
Flaps 20 - 210kts
Flaps 30 - 175kts
Electrical (Generators/Batteries)
Continuous:
2 or 3 Generators - 400A
1 Generator on Ground - 400A
1 Generator in Flight - 500A
Transient:
5 minutes - limit 600A
Prohibited to takeoff in Battery Temps are below -20°c.
Compass
Left and Right windshield must be temporarily off while the standby compass is being read.
Standby Instrument
Localizer deviation is prohibited during back course approaches.
GPS T-transition Speed
210kts out less
VNAV
- VFLC is prohibited during climb when airspeed is displayed as Mach.
- VNAV for VMDA approaches is prohibited between final approach fix and MAP.
Autopilot Engagement Heights
Climb, Enroute, Descent - 700 AGL
Precision with GP 3.5 or less - 80 AGL
Precision with GP 3.5 to 4.5 - 160 AGL
Visual and non-precision - 200 AGL
Pressurization
Max Diff on ground - -0.1 psid
Max Diff on landing - 1 psid
Max positive diff - 9.4 psid
Max negative diff - -0.5 psid
Oxygen masks
Crew and Pax Oxygen Masks not approved above 40000ft.
Prolonged operation of Pax masks above 25000ft is not recommended.
Air Conditioning
Do not select air source to TRIM AIR ONLY in the ground.
Pack must be operating when electrical power is on for more than 30 minutes and OAT is greater than 40°c.
Maneuvering Load Limits
Flaps Up +2.6G -1.0G
Flaps Extended +2.0G -0.0G
Max altitude
45000ft
Takeoff and Landing Limitations
Max takeoff and landing altitude 10000ft.
Max tailwind component - 10kts
Max runway slopes +/- 2°
Tire Speed
182kts
Other Airspeeds: Vra Vlo retract Vlo extend Vle Vfe
Vra - 265/.75M Vlo retract - 200kts Vlo extend - 250kts Vle - 250kts Vfe 10, 20, 30 - 210, 210, 175
Max Operating Speeds
Vmo
Mmo
Vmo (up to 8000) - 300kts
Vmo (8001 to 29475) - 320kts
Mmo (above 29475) - 0.83M
Wing Anti-ice
On ground below 5°c + visible moisture
In flight below 10°c + visible moisture except when SAT is below -40°c.
Must be in when ICE DETECTED CAS is on or in icing and below 210kts.
Engine Anti-ice
On ground below 10°c + visible moisture
In flight below 10°c + visible moisture
Must be on when ICE DETECTED CAS is on or in icing conditions.
Stabilized Approach Criteria
ABCD 1PF
- Airspeed Vref -0 to +10
- Briefed
- Configured
- 1 Dot lateral and vertical CDI deflection
- 1000ft/minute or less VSI
- On Profile
- No Flags
Icing limits
Do not hold on icing with flaps extended.
When side window icing is observed - wing and engine Anti-ice must be on, leave icing ASAP.
Dimensions
Wingspan
300 - 63’ 10”
350 - 69’
Length - 68’ 8”
Height - 20’
Minimum pavement for 180° turn - 58’
Wingtip clearance for 180° turn 300 - 95’ 5”, 350 - 101’
Weights Ramp Takeoff Zero Fuel Landing Flight
Max Ramp - 40750 Max Takeoff - 40600 Max ZeroFuel - 28200 Max Landing - 34150 Flight - 24800
Crosswind
Max takeoff - 28kts
Max landing - 24kts
APU RPM / EGT
Max RPM - 108%
Max EGT - 973°c starting, 718°c normal
APU and altitude
APU operation - 37000ft
APU generator - 30000ft
Bleed air for engine start - 20000ft
Bleed air for ECS - 20000ft
Do not use APU to start L engine on ground above 9000ft.
APU ops during de-icing prohibited.
Thrust reversers
- on paved surfaces only
- not in flight
- not for backing up
- not for touch and go’s
- reverse thrust above idle prohibited below 40kts
APU starting
On ground-
3 attempts with 1 minute cooling, after 3rd attempt 20 minutes cooking.
2 more attempts may be made then no further attempts for 40 minutes.
In flight-
Below 285kts, 1 attempt.
Engine start limits
3 consecutive start cycles may be made followed by 15 minutes cooling before more start attempts.
Engines must be motored for 30 seconds after aborted start.
Engine can be motored for 5 minutes followed by 15 minutes cooling.
Engine Type
HTF 7350 / AS907-2-1A
7323lbs thrust
Flat rated ISA +15 TO
Flat rated ISA +20 APR
Engine Oil Temps
Normal range 27 - 138°C
-40°C minimum for Engine Start.
(Below -30°c minimum, oil temp limit is 15°c provided fuel system icing inhibitor is used)
Oil temp of minimum 5°c to operate engines above ground idle.
Oil temp between 5°c - 14°c, engines may be operated up to but not including CLB.
27°C is a Green Indication.
Fuel Temps
Fuel system icing inhibitor must be used when fuel is below -20°c for takeoff.
Takeoff with bulk fuel temp above 50°c is prohibited.
With wing bulk fuel 45°c and above:
- min fuel for takeoff is 2800lbs
- less than 1000lbs per side, do not operate engines for more than 30 minutes.
Fuel Temps:
Jet A - -30°c
Jet A1 - -35°c
Jet B - -40°c
