Limitations Flashcards
Maximum structural takeoff weight
21,500 lbs
Maximum landing weight
19,200 lbs
MMO/VMO
0.81 Mach / 330 KIAS
Maximum Ramp weight
21,750 lbs
Baggage compartment weight limit
500 lbs
Minimum flight weight
14,000 lbs
Maximum landing gear extended speed (Vle)
260 KIAS
APU generator limit
300 amps continuous
Maximuum landing gear operating speed (Vlo)
200 KIAS
Runway water landing limitation
3/4 in
Landing EICAS page
SUMRY or FLT page
Maximum reverse thrust is available at speeds down to
40 KIAS
What are the thrust reversers limited to when in Manual fuel mode?
idle
Flap/Gear/Maneuvers limit
Flap/gear - do not extend above 18,000 ft
Manuevers - no aerobatics. Intentional stalls prohibited above 18,000 ft
Maximum Flap extended speed (VFE)
8° - 250 KIAS
20° - 200 KIAS
40° - 150 KIAS
Landing pressurization limit
not pressurized
Max fuel imbalance
200 lbs
Fuel Capacity
Total: 6062 lbs
Wings: 500 gal total (1678 L/1676 R)
Fuselage: 404 gal (2708)
“Configuration” before takeoff (7)
-pitch trim bias not at 0
-pitch trim miscompare
-parking brake “ON”
-thrust reversers not stowed
-takeoff trim not set on all 3 axis’
-spoilers extended
-flaps not 8 or 20
Pressurization concerning altitudes
Cabin altitude CAUTION: above 8500’
EMER PRESS auto activation: 9500’
Cabin altitude WARNING: 10000’
Outflow valves close: 13700’
Masks deploy with EMER lights: 14500’
Maximum control speed ground (VMCG)
Rudder boost ON, APR ON - 102 KIAS
Rudder boost ON, APR OFF - 100 KIAS
(Vmcg- the calibrated airspeed during the takeoff run at which, when the critical engine is suddenly made inoperative, it is possible to maintain control of the airplane using the rudder control alone)
what does the ADC provide data to?
-AHRS
-flight director/autopilot
-vertical modes
-xponders
-spoilerons computers
-cabin pressurization
-landing gear warning system
-stall warning system
-DEECs
Oxygen system limitations
O2 masks not approved for use above 40,000’ cabin altitude
Prolonged operation of pax masks above 25,000’ cabin altitude not recommended
Maximum pressure altitude (takeoff and landing)
14,000 ft
When must HI-FLOW be off?
- Takeoff power selected
- Landing
- Anti-ice operations
- Flight above 30,000’
Maximum zero fuel weight
16,500 lb (modified by SB 45-11-5)
16,000 lb (not modified)
Spoilers limitation
do not extend spoilers with flaps extended WHILE AIRBOURNE, except in an emergency
ITT limits
APR/TAKEOFF/MCT/MCR/START
APR - 1013°
T/O - 991°
MCT - 991°
MCR - 974°
START 991°
Cabin pressurization limits
Delta P - +9.9 psid to -0.5 psid
Maximum pressure altitude
51,000 ft
Rudder boost
must be ON for takeoff
Do not use thrust reversers (2)
-For backing up aircraft
-For touch and go landings
Airspeed/Mach limits
(Standby instruments)
Vmo - 325 KIAS
Mmo - 0.75 Mi
When is APU operation prohibited?
-During gravity refueling
-During fluid deicing/anti-icing
**do NOT take off with APU FAIL amber CAS illuminated
Aircraft generator limit
Continuous - 300 amps
Transient - higher transient loads for cross-starts and battery charging are authorized
Tailwind component
10 KTS
Above 12,000’ - 0 KTS
CABIN/COCKPIT FIRE, SMOKE, OR FUMES
- Crew O2 masks ——————— Don & 100%
- Smoke Goggles ——— ————-Don
- EMER DEPRESS ———————- ON
- Pilot and Copilot mic/mask ——-MASK
- Pilot and Copilot INPH ———— INPH
LOSS OF BOTH GENERATORS AND BOTH MAIN BATTERIES
- L & R BATT —————————— On, one at a time
- L & R GEN circuit breakers ——— Set
- Engine N2 ——————————– 80% or Above
- L & R GEN —- One at a time, Depress (approx 1 sec)
EMERGENCY DESCENT
“CABIN ALTITUDE”
(Cabin alt exceeds 10,000 ft)
- Crew O2 masks —————-Don & 100%
- Thrust Levers ——————— IDLE
- Autopilot ———————— Disengage
- SPOILER —————————-EXT
- Descend at Mmo/Vmo, but not below minimum safe altitude
- DEPLOY (PAX OXYGEN) ——-—— ON
- Pilot and Copilot mic/mask ——-MASK
- Pilot and Copilot INPH ———— INPH
EMERGENCY EVACUATION
- EMERGENCY PARKING BRAKE ——- Set
- Thrust Levers ——- ——————CUTOFF
- EMER LIGHTS —————————- ON
- EMER BATT, L & R BATT ———-—- OFF
ENGINE FIRE
“RIGHT ENGINE FIRE”
“LEFT ENGINE FIRE”
- Thrust Lever —————- IDLE
…………….unless a critical thrust situation exists - *if fire continues more than 15 seconds or there are other indications of fire:
—a. Thrust Lever ————————CUTOFF
—b. Applicable FIRE (Engine) —- FIRE PUSH
—c. EXTINGUISHER #1 (Engine) —- ARMED Push
ENGINE FAILURE
During Takeoff: Below V1 speed
- Brakes —————- Apply
- Thrust Levers —— IDLE
ENGINE FAILURE
During takeoff: Above V1 speed
- Rotate at Vr to target takeoff pitch attitude; Climb at V2
- Gear ——— UP
- Climb to 1500 feet AGL or Obstacle Clearance Altitude (as appropriate), accelerate to V2+25, retract flaps, then accelerate to 200 KIAS en route climb speed
ENGINE FAILURE
During Approach
- Control Wheel Master (MSW) —- Depress & Release
- Thrust Lever (operative engine) — Increase as req’d
- Flaps ———— 20°
- Airspeed ——- Vref + 5
IMMEDIATE ENGINE AIRSTART
Affected Engine
- Thrust Lever ——- IDLE
- STBY (FUEL) ——— ON
AILERON CONTROL JAM
