Limitations Flashcards
General
Minimum External Temperature
-54°C
General
Maximum External Temperature
+38°C
With air condition functioning
General
Maximum Operating Altitude
Bleeds OPEN
EEC ON: 32,000 ft
EEC OFF: 25,000 ft
General
Maximum Operating Altitude
Bleeds COSED
EEC ON: 25,000 ft
EEC OFF: 20,000 ft
General
Above what altitude EEC must be OFF for takeoff and landing
8,000 FT
Genaral
What is the maximum takeoff and landing altitude
10,000 ft
Genaral
What is the maximum runway slope
+/- 2°
Genaral
Maximum Ramp Weight
MRW
26,609 lb
Genaral
Maximum Takeoff Weight
MRW
26,433 lb
Genaral
Maximum Landing Weight
MLW
25,794 lb
Genaral
Maximum Zero Fuel Weight
MZFW
24,030 lb
Speed
Maximum DV window seeped
140 KIAS
Autopilot
Minimum speed with autopilot ON
One Engine
120 KIAS
Speed
Maximum turbulence penetration seeped
Vb
175 KIAS
Speed
Maximum tire speed
165 KIAS
Electrical
Starter duty cycle
30s ON: 3min OFF
30s ON: 3min OFF
30s ON: 30min OFF
Pressurization
Maximum Differential Pressure
7.2 PIS
Pressurization
Normal Differential Pressure
7 PSI
Fuel
Total Fuel
5,732 lb
Fuel
Maximum Usable Fuel per wing
2,886 lb
Fuel
Unusable Fuel in each wing
24 lb
Add 76.9 lb when main ejectror pump inop
Fuel
Maximum demonstrated fuel imbalance
600 lb
ICE
When can leading edge deicers be activated during takeoff
At final segament speed
ICE
Atmospheric icing condition exists when
Indicated OAT during ground operations or TAT in flight is 10°C or below and visible moisture in any form is present
ICE
Ground icing condition exists when
Indicated OAT during ground operations is 10°C or below and visible moisture, standing water, slush, ice, snow, is present on ramps, taxiways, or runways
ICE
In icing condition use of flaps is restricted to what flight conditions
Takeoff, approach and landing only
ICE
When flaps have been extended they may not be retracted unless
In flight icing condition
The uppers surface of the wing aft of the protected area is clear of ice, or unless flap retraction is essential for go-arounds
ICE
All wing inspection lights must be operational prior to flight in
Known icing at night
ICE
Both stall warning systems must be operative prior to
Flight into known icing
ICE
When ice protection is detecting ice and/or the deice boots are activated what indication is unreliable
Fast/slow
AUTOPILOT
The Autopilot and Yaw Damper must be off
All flight conditions
Takeoff and landing
AUTOPILOT
Minimum Altitude for Autopilot/Yaw Damper on ILS coupled approaches
200 ft AGL
GENERAL
Required Flight Crew
Pilot and Copilot
GENERAL
Kinds of Opeartions
VFR, IFR, FIKI
GENERAL
Maneuvering Load Factors Limits
Flaps up: +2.8G/-1.0G
Flaps down: +2.0G/-0G
GENERAL
Condition lever position during all ground opeartions
Exept when cleard for takoff or during landing roll
MIN RPM
Genaral
Power Levers must be in what position during all ground operations
Exept for breif excursions as needed to maneuver the airplane
GROUND IDLE
SPEED
Maximum speed for windshield operations
160 KIAS
SPEED
Vmo/Mmo
272 KIAS/0.52 MACH
SPEED
Va
200 KIAS
SPEED
Vle/Vlo
200 KAIS
SPEED
Vfe
200 KAIS
150 KIAS
135 KIAS
GENERAL
Max Demonstrated Crosswind
30 KIAS
GENERAL
Maximum Tailwind Speed Takeoff and Landing
Gear and Flaps Up
10 KIAS
SPEED
Minimum Speed in Icing Conditions
Gear up Flaps 15°
165 KIAS
APU
Operations above what altitude is permitted only with APU bleed extraction set to both air conditioning packs
APU limitation
16,000 ft
APU
APU maximum speed and altitude
For starting
200 KAIS
20,000 ft
Airspeed may vary with altitude
APU
APU maximum operating temperature
APU limitation
Up to 16,000 ft: +38°
Above 16,000 ft: +35°
APU
APU maximum allowable EGT during start
During Start
732°C
EGT above 732°C to a max of 947°C are limited to 10 seconds only
ELECTRICAL
Maximul Load per MAIN genrator
Up to 27,000 ft: 400 AMPS
Above 27,000 ft: 380 AMPS
ELECTRICAL
Maximum Laod per AUX generator
Up to 18,000 ft: 150 AMPS
Above 18,000 ft: 140 AMPS
APU
Maximum Load per APU generator
ISA below 35°C
Up to 16,000 ft: 400 AMPS
Above 16,000 ft: 290 AMPS
ISA above 35°C
Up to 16,000 ft: 400 AMPS
Above 16,000 ft: 280 AMPS
ELECTRICAL
Maximum Battery temperature
70°C
FUEL
Fuel Used
JET A, JET A-1,*JET B
QAV 1, *QAV 4
*JP 4, JP 5, JP 8
* Emergency only
Aviation gasoline may be used in an emergency up to a limit of
150 hours between overhauls
ICE
When ground or athmospheric icing condition exists or at the first sign of ice accretion enywhere on th airplane or ICE DETECTOR ilght is illuminated, turn ON the following ice protection swithces
AOA, TAT, Slip, Engine Air Inlet, Ignition, Propeller, Leading Edge Deicer, Windshield Heat
SPEED
Bird impact speed
250 KIAS below 8,000 ft
GEMERAL
PROP SYNC must be off
Flight condition
For Takeoff and Landing per airworthiness directive
FUEL
When fuel quatity indicator reads what indication in level flight, any fuel ramining in the tank cant be used safetly in flight
Zero
ICE
Continuous ignition must be used during the following conditions
Takeoff and landings on contaminated runways
Takeoffs with inoperative EEC
Flight trough moderate or greater rain
Flight trough known or forecasted icing
GENERAL
Zone Weight Limits
Zone 1-3: 2,600 lb.
Zone 4: 1,213 lb.
FUEL
Minimum oil pressure to ensure intake deicing and to prevent fuel icing
45°C
ICE
Minimum Nh required for operations of the pneumatic deicing system
80%
ICE
The propeller blades may be heated only when the oil pressure is above
40 PSID
GENERAL
Operation id oil pressure is below what PSID is not permitted
40 PSID