Ops Limits Flashcards
Airplane / power plant maximum operating ambient temperature:
+50C or ISA +35C, whichever is lower
Airplane / power plant minimum operating temperature:
-54C
APU maximum operating ambient temperature:
+50C or ISA +35C, whichever is lower
APU minimum operating temperature:
-54C
Maximum operating altitude:
25,000 ASL
Maximum operating altitude for takeoff:
10,000 ASL
Max crosswind for takeoff and landing:
32 knots
Max ramp weight:
65,400 lbs
Max takeoff weight:
65,200 lbs
Max landing weight:
62,000 lbs
Severe turbulence speed:
210 Knots
Maneuvering Speed (vA): (Maximum speed with full application of rudder and aileron controls and maneuvers that involve angles of attack near the stall.)
204 Knots
Max Gear Extended Speed (vLE):
The maximum speed with landing gear extended.
215 Knots
Landing Gear Operating Speed (vLO):
The maximum speed it is safe to extend or retract landing gear.
195 Knots
Max Fuel Capacity:
11,724 lbs
Fuel: Max Imbalance (Inflight Only)
600 lbs
Fuel: Tank 1 and 2 Auxiliary Pumps
On for takeoff and landing
Engine Starter Cranking Limit:
70 seconds followed by 2 minutes off
APU Starter Cranking Limit:
- 60 seconds followed by 5 minutes off.
- Second attempt 60 seconds followed by 30 minutes off (MX Req’d after 2nd attempt).
Battery Load Prior to Takeoff (Main, Aux, Standby):
0.1
Min Battery Temperature Prior to Takeoff:
-20C
Max Altitude Gear and Flaps Extended:
15,000
Max Cabin Differential:
5.95 psi
Max Cabin Differential - Takeoff and Landing:
.5 psi
Bleed Air Must Be Off For Takeoff or Landing Whenever: (WTTL)
- Wind shear is suspected
- Tailwind exceeds 10 knots
- Takeoff with MTOP power selected
- Landing only when OAT exceeds 39C (100F)
AHRS: Takeoff is prohibited in
BASIC mode
DG mode
Baggage Compartment Fire Extinguishing:
Unless the fwd and aft baggage compartments are empty, the airplane shall not be operated farther than one hour flying time from a suitable airport for landing.
Conditions Requiring a Takeoff Abort: (WHEETTFM)
- Windshear encounter
- HGS failure, “TO WARN”, or loss of HGS symbology during takeoff below 500 RVR when runway CL is not in sight
- Engine fire or failure
- Exceeding engine limitations
- Takeoff warning horn
- Takeoff torque not obtained on either engine
- Failure of the A/F ARM message to illuminate on ED
- MASTER WARNING
First Officer’s Briefing:
Call out 80, V1 and rotate. Call any malfunctions, if before V1 it will be your decision to abort. After V1 I will continue the takeoff.
Flight Compartment Communication:
HOT MIC select switches on the Captain and FO ARCDU shall be OFF and the INT/RAD switch on the observer’s audio control panel shall be centered when using the flight deck speakers.
APU Limitations:
- APU is approved for GROUND OPERATION ONLY
- APU shall be shutdown prior to takeoff
- APU shall not be operated unattended with passengers on board
- APU shall not be operated during gravity refueling
- (QX) To maintain steady electrical state, the APU shall not be started during refueling
- (QX) The APU bleed air shall be selected OFF when the aircraft is being deices/anti-iced
Engine Limitations (3):
- Setting power for takeoff prior to brake release with winds over 8 knots more than 45 degrees off the nose is prohibited
- Inflight operation of the POWER levers aft of the FLIGHT IDLE gate is prohibited
- Engine Intake Bypass Doors must be open for operation in icing conditions
The use of VOR without associated DME is prohibited in _____ mode:
APP
Definition of icing conditions (Inflight):
SAT is 5 degrees or below and visible moisture is present in any form. Ice accretion on aerodynamic surfaces is not considered to exist at temperatures of -40dC or below.
