Limitations, Memory Items, and Extra Flashcards
Maximum Ramp Weight
85,800 lbs
Maximum Takeoff Weight (MTOW)
85,500 lbs
Maximum Landing Weight (MLW)
74,900 lbs
Maximum Zero Fuel Weight (MZFW)
69,800 lbs
Maximum Forward Cargo Compartment Loading Weight
3,307 lbs
Maximum Aft Cargo Compartment Loading Weight
2,535 lbs
Aircraft Height
32’ 4” (33’)
Aircraft Width
93’ 11” (94’)
Aircraft Length
103’ 11” (104’)
Maximum Headwind for CAT II Approaches
25 knots
Maximum Crosswind for Landing (vis < 4000 or 3/4)
15 knots (E)
Maximum Takeoff and Landing Tailwind Component
10 knots
Maximum Operating Altitude
41,000
Maximum Altitude with Flaps Extended
20,000
Passenger Carrying Capacity
76 (12 First Class and 64 Coach)
Minimum Number of Crew
2 Pilots
Authorized Aircraft Operating Conditions
Day and Night
VFR and IFR
Icing Conditions
CAT I and CAT II
RVSM
Maximum Cabin Differential Overpressure
8.8 psi
Maximum Cabin Differential Pressure Above FL370
8.4 psi
Maximum Cabin Differential Pressure During Takeoff and Landing
0.2 psi
Maximum Negative Cabin Differential Pressure
-0.5 psi
Maximum Operating Altitude While Depressurized
10,000 or MEA, whichever is higher
Maximum Operating Altitude for Single Pack Operation
31,000
MMO Above FL280
0.82 M
VMO Between 10,000 and FL280
320 knots
VMO Below 10,000
300 (structural)
250 (FAA speed limit)
VA
240
VLE
250
VLO
250
VLR
250
VFE1
230
VFE2
215
VFE3
200
VFE4
180
VFE5
180
VFEFULL
165
Maximum Turbulent Airspeed Below 10,000
250
Maximum Turbulent Airspeed 10,000 and Above
270 or .76M, whichever is lower
Maximum Crosswind for Takeoff (DRY)
35 knots
Maximum Crosswind for Takeoff (WET)
30 knots
Maximum Tailwind
10 knots
Maximum Direct View Window Operation
160
Maximum Tire Speed
195
Maximum Speed for Windshield Wiper Operation
250
Aircraft Maximum Operating Altitude
41,000
Maximum Takeoff and Landing Altitude
10,000
Minimum Takeoff and Landing Altitude
-1,000
Min/Max Takeoff and Landing Temperature (SAT)
-40°C | 54°C
note: In the event of a landing below -40°C, takeoff not authorized without further maintenance inspection
Maximum Altitude Display Difference in Flight for RVSM
180 ft
APU Make and Model
Sundstrand APS 2300
APU Starting Time Limits
1st and 2nd Attempt: 60 secs off
3rd Attempt: 5 mins off
APU Minimum Starting Temperature
-54°C
APU Maximum Operating Temperature
ISA + 39°C
note: Supplemental restrictions applicable > ISA + 35°C
APU Maximum EGT (Start)
1032°C
APU Maximum EGT (Continuous)
717°C
note: No time limit for amber indications on ground or inflight between 662°C - 717°C
APU Maximum Operating Altitude
33,000
APU Maximum Altitude for Electrical Demand
33,000
APU Maximum Starting Altitude
30,000
APU Maximum Altitude for Engine Start Bleed
21,000
APU Maximum Altitude for ECS (Pack) Bleed Demand
15,000
Minimum Battery Temperature for APU Start
-20°C (Battery #2)
note: This does not prevent starting the APU via DC power if a DC GPU is available and utilized
Minimum Autopilot Engagement Altitude on Takeoff and Go Around
Above 400’
Minimum Altitude for Autopilot Disconnect During Landing
50’
Engine Make and Model
GE CF34-8E5
N1 Maximum RPM
99.5%
N2 Maximum RPM
99.4%
Engine Maximum Takeoff and Go Around ITT (Dual Engine)
965°C (2 mins)
949°C (3 mins)
note: Total of 5 mins
Engine Maximum Takeoff and Go Around ITT (Single Engine)
1006°C (2 min)
990°C (3 min)
note: Total of 5 mins
Engine Maximum Continuous ITT
960°C
Min/Max Engine Oil Pressure
25 psi | 95 psi
Engine Continuous Oil Temperature
155°C
Engine Transient Oil Temperature
163°C
note: 15 min time limit
Engine Thrust T/O-1
13,000 lbs
ATTCS = 14,200 lbs
Engine Thrust T/O-2
11,800 lbs
ATTCS = 13,000 lbs
Maximum Fuel Capacity
10,467 lbs per tank (20,934 total)
Maximum Usable Fuel Capacity
10,392 lbs per tank (20,784 total)
Unusable Fuel Amount
75 lbs per tank (150 total)
Maximum Fuel Tank Imbalance
794 lbs
Fuel Pounds to Gallon Conversion Ratio
6.767 lbs / US Gallon
Minimum Fuel Tank Temperature
-37°C
Engine Starting Time Limits
1st and 2nd Attempt:
GND: 90 sec START / 10 sec Cool-down
FLT: 120 sec START / 10 sec Cool-down
3rd - 5th Attempt:
GND: 90 sec START / 5 min Cool-down
FLT: 120 sec START / 5 min Cool-down
Engine Dry Motoring Time Limits
1st Attempt: 90 sec maximum / 5 min Cool-down
2nd - 5th Attempt: 30 sec maximum / 5 min Cool-down
note: After 5 sequential dry motoring attempts, the sequence may be repeated following a 15 min cool-down period
Cabin Altitude HI / Rapid Depressurization
- Oxygen Masks …… CR ….. ON, 100%
Jammed Control Column - Pitch
Elevator Disconnect ……………….. CR ……………….. PRESS and PULL
Jammed Control Wheel - Roll
Aileron Disconnect ……………….. CR ……………….. PRESS and PULL
Pitch Trim Runaway
- AP/TRIM Disconnect ………………………………… PRESS and HOLD
- TRIM PITCH SYS 1 & 2 CUTOUT ………………… Push IN
(Roll or Yaw) Trim Runaway
AP/TRIM Disconnect …………………………………….. PRESS and HOLD
Nosewheel Steering Runaway
STEER DISC ……………. PRESS and HOLD
Aborted Engine Start
- Associated Thrust Lever …………………………. IDLE
- Associated START/STOP …………………………. STOP
Minimum Airspeed for Maximum Reverse Thrust
60 KIAS
note: Below 60 KIAS reduce reverse thrust to idle
Definition of Icing Conditions
10°C or below (OAT on ground or TAT in flight) AND at least one of:
- Visible moisture in any form including clouds or fog (one mile or less visibility).
- When operating on ramps, taxiways, or runways with snow, ice, or standing water contamination.
Before Start, REF A/I on the MCDU must be set to:
“ENG” when the OAT is between 5°C and 10°C or “ALL” when OAT is below 5°C
and icing conditions exist or are anticipated prior to reaching 1,700 ft above field elevation
All landings on runways with an RCC less than 5/5/5 must be at what flap setting?
Flaps FULL
note: Unless otherwise required by operational restrictions such as CAT II, MEL status, or Emergency/Abnormal procedures
The green towing light illuminates when:
Steering is disengaged.
Parking brake is not on.
Main brakes are not applied.
A rejected takeoff should only be initiated between 80 knots and V1 for the following:
- Fire or fire warning
- Engine failure
- Stagnant airspeed or sudden negative wind change
- If the airplane is unsafe or unable to fly
The T/O Config button checks what items?
Flaps (not in takeoff position or disagrees with FMS takeoff page 2/2)
Parking Brake (brakes are on)
Pitch Trim (outside of green range)
Spoilers (any panel is deployed)
What happens when an Engine Fire Handle is pulled?
- Fuel shutoff valve closes
- Hydraulic shutoff valve closes
- Engine bleed air valve closes
Items in the accessory gearbox
Integrated Drive Generator (IDG)
Hydraulic Pump
Permanent Magnet Alternator (PMA)
Air Turbine Starter (ATS)
note: Radial drive shaft connects to the N2 rotor
Maximum Crosswind for Landing
38 knots
Engine Start Maximum ITT
815°C
