Limitations Flashcards
max ramp weight
85800
Max takeoff weight
85500
Max Landing weight
74900
max zero fuel
69,800
fwd cargo weight
3306
aft cargo weight
2535
max headwind cat II
25 knots
max crosswind dry
35 (Mark said 38)
max crosswind less than 4000 and 3/4
15 (e)
max crosswind takeoff (wet)
30 (e)
max runway slope
+/- 2°
max maneuvering load limits flaps up
-1.0 to +2.5
Max maneuvering load limit flaps down
-0 to +2.0
maximum operating altitude
41,000’
Max T/O and LDG alt
8000
MAX SAT FOR T/O LDG/ GND START
52C
max alt with flaps extended
20,000
max operating latitude
78N (E)
78S (E)
Min SAT for T/O LDG and GND Start
-40C
Max Crosswind Code 6 breaking action (-)
38 knots
Max Crosswind Code 5 breaking action (good)
31
Max Crosswind Code 4 breaking action (good to medium)
20
Max Crosswind Code 3 breaking action (Medium)
15
Max Crosswind Code 2 breaking action (medium to poor))
12
Max Crosswind Code 1 breaking action (Poor)
8
What are all winds based limits based on
Peak Gust Value
Min operating speed limit
Intentional operation below onset of stall warning (stick shaker) is prohibited unless specifically authorized for flight test.
Max Opp Airspeed
320
Max Mach
.82
Max RAT airspeed
Vmo Mmo
Turbulent Airspeed below 10,000
250
Turbulent Airspeed above 10,000
270/.76M
Tire Limit Groundspeed
195 knots
Max speed windshield wiper operation
“Hi”
-Jason Vandergriff (hahaha)
(250 knots)
Max speed windshield wiper failed not in non-parked position
320KIAS
MAX SPEED FLIGHT DECK WINDOW OPEN
160 KIAS
MAX GEAR (Retraction, extension, extended)
250 KIAS
Flaps 1 MAX SPEED
230
Flaps 2 MAX SPEED
215
Flaps 3 MAX SPEED
200
Flaps 4 MAX SPEED
180
Flaps 5 MAX SPEED
180
Flaps FULL MAX SPEED
165
Min Controllable Speed
Vapp +10, refer to QRH
Design Maneuvering Speed
Full application of rudder and aileron controls, as well as maneuvers that involve angles of attach near stall must be confined to speeds at or below 240 KIAS
Definition of Ice
OAT or TAT (in flight) of 10C or below AND:
- Visible moisture (precipitation or visibility of less than 1 mile)
- operating on surfaces covered in snow, ice, slush, or standing water
Engine and Wind Anti-Ice temp limit in Auto
There is no temperature limit in the AUTO position
Engine and Wing Anti-ice operations
must be set to “ALL” when 10C or below and icing conditions exist
Approved Fuels
Jet-A and A-1
JP-8
QAV-1
When using JET-A with a temp below -30C, the fuel temp prior to flight must be verified to be above -29C
Fuel density
6.77 lbs/gal
Max fuel Capacity
10,392lbs per tank (20,734 total usable)
75lbs unusable fuel per tank
Min Fuel Temp
-37C
Max Fuel Imbalance
800lbs
Crossfeed Operation for Takeoff and Landing
Crossfeed OFF for Takeoff and Landing
APU Start Limit 1st/2nd cycle
60 seconds off per start
APU Start Limit 3rd cycle
5 minutes off
APU MIN/MAX temp for operation
-54C to ISA+35C
MAX APU START ALT
30,000
MAX APU OPERATION (ELECTRICAL)
33000
MAX APU OPERATION (BLEED)
15,000
MAX APU OPERATION (ENGINE START)
21,000
MAX APU ROTOR SPEED
108%
MAX APU EGT START
1032C
MAX APU EGT CONTINUOUS OPERATION
717
MAX SINGLE PACK ALT
31,000
MAX DIFF PRESSURE (UP TO 37,000)
7.8
MAX DIFF PRESSURE (ABOVE 37,000)
8.3
MAX DIFF OVERPRESSURE
8.7
MAX NEG DIFF PRESSURE
-0.5
MAX DIFF PRESSURE FOR T/O AND LDG
.2
OZONE CONCENTRATION LIMITS
REFER TO TABLE IN LIMITATIONS SECTION OF AOM 1
BRAKE TEMP limit for Takeoff
DO NOT TAKE OFF WITH BRAKE TEMPS IN THE AMBER.
FLAPS ENROUTE
ENROUTE USE OF FLAPS/SLATS IS PROHIBITED
MAX ALTITUDE WITH FLAPS/SLATS EXTENDED
20,000
AUTOPILOT MIN ALT
TAKEOFF- 400’
LANDING- 50’
TCAS DEVIATIONS
DEVIATIONS FROM ATC CLEARANCES ARE AUTHORIZED TO COMPLY WITH TCAS RA
TCAS DEVIATIONS BASED SOLELY ON NAV DISPLAY
MANEUVERS MUST NOT BE BASED SOLELY ON INFORMATION PRESENTED ON NAV DISPLAY
IS COMPLIANCE WITH A TCAS RA REQUIRED
YES, UNLESS PIC DETERMINES DOING SO WOULD JEOPARDIZE SAFE OPERATION OF FLIGHT
CAN YOU NAVIGATE WITH EGPWS DISPLAY
NO, NAV MUST NOT BE PREDICATED ON EGPWS DISPLAY
ARE DEVIATIONS FROM ATC CLEARANCES PERMITTED TO COMPLY WITH EGPWS WARNINGS?
YES
WHEN SHOULD THE PILOT MANUALLY INHIBIT TERRAIN/OBSTACLE AWARENESS ALERTING?
WITHIN 15 MILES ON APPROACH TO AN AIRPORT NOT IN THE EGPWS AIRPORT DATABASE
HOW WILL CREWS KNOW AN AIRPORT IN NOT IN THE EGPWS DATABASE
IT WILL BE NOTED IN THE F4 MESSAGES OF THE RELEASE
BANK ANGLES ON FMS LNAV
THERE IS NOT AUTOMATIC BANK ANGLE PROTECTION FOR SINGLE ENGINE OPERATIONS WHEN IN FMS LNAV
TAS TAT AND SAT ARE ONLY VALID ABOVE WHAT AIRSPEED?
60 KNOTS
WHAT TYPE OF ENGINE DO WE HAVE
GE CF34-8E5
WHAT INFORMATION IS USED TO DETERMINE WHETHER WE ARE WITHIN ENGINE LIMITATIONS
THE MARKINGS ON THE EICAS
MAX AND MIN ENGINE LIMITATIONS ARE DEPICTED ON THE EICAS HOW?
IN RED
ENGINE CAUTION RANGE IS DEPICTED ON THE EICAS HOW?
AMBER
ENGINE NORMAL OPERATING RANGE IS DEPICTED ON THE EICAS HOW?
GREEN
NORMAL AND MAXIMUM TAKEOFF AND GO AROUND TEMPERATURES ARE LIMITED TO _____MINUTES DURING A ____ MINUTE PERIOD
5, 10
NORMAL TAKEOFF AND GO AROUND TEMP/TIME LIMIT
965 (2 MIN)
949 (3MIN)
MAX TAKEOFF AND GO AROUND TEMP/TIME LIMIT DURING WINDSHEAR OR OEI WITH THRUST LEVERS IN TOGA
1006 (2 MIN)
990 (3 MIN)
MAX CONTINUOUS ENGINE TEMP LIMIT
960
ENGINE START TEMP LIMIT
815
ENGINE N1 MAX RPM
100% N1
ENGINE N2 MAX RPM
100% N2
MAX ENGINE OIL TEMP (TIME)
163C FOR 15 MINUTES
MAX ENGINE OIL PRESSURE (TIME)
95PSI FOR 25 MIN
ENGINE START CYCLE LIMIT GROUND (1ST AND SECOND)
90 SEC ON, 10 SECONDS OFF
ENGINE START CYCLE LIMIT GROUND (3RD-5TH)
90 SEC ON, 5 MIN OFF
ENGINE START CYCLE LIMIT FLIGHT (1ST AND 2ND)
120 SEC ON ON, 10 SEC OFF
ENGINE START CYCLE LIMIT FLIGHT (3RD-5TH))
120 SEC ON, 5 MIN OFF
ENGINE MOTORING LIMIT (AIR AND GND) (1ST)
90 SEC ON, 5 MIN OFF
ENGINE MOTORING LIMIT (AIR AND GND) (2ND-5TH)
30 SEC ON, 5 MIN OFF
AFTER 5 MOTORINGS, HOW MUCH TIME BEFORE CYCLE CAN BE REPEATED
15 MIN
CAN WE GO AROUND AFTER DEPLOYING REVERSER
NO
CAN WE BACK UP WITH REVERSE THRUST
NO
CAN WE USE REVERSE THRUST IN THE AIR
NO
MIN SPEED FOR FULL REVERSE THRUST
60 KIAS
FUEL CIRCUIT BREAKER RESET (EVER?)
NO: “RESETTING A FUEL BOOST PUMP, OR FUEL INDICATING SYSTEM CIRCUIT BREAKER IS PROHIBITED.”
“THERE IS NO OPERATIONAL SITUATION IN WHICH IT WOULD BE NECESSARY TO RESET A TRIPPED FUEL BOOST PUMP OR FUEL INDICATING SYSTEM CIRCUIT BREAKER”
MIN BATTERY TEMP FOR APU STARTING
-20C, THIS DOES NOT PROHIBIT STARTING THE APU VIA DC POWER IF A DC GPU IS AVAILABLE AND UTILIZED
WHEN MUST THE FLIGHT DECK DOOR ACCESS SYSTEM BE TESTED
PRIOR TO THE FIRST FLIGHT OF THE DAY
WHEN MUST THE ESCAPE SLIDES BE ARMED?
WHENEVER OCCUPANTS ARE IN THE CABIN, THE ESCAPE SLIDE MUST BE ARMED FOR TAXI, TAKEOFF, AND LANDING.
FOR DOOR ARMING REQUIREMENTS ON FERRY, TRAINING, AND CHARTER FLIGHTS, REFER TO FM-1 (E)
ALTIMETER TOLERANCES (STBY ALT)
STBY ALTIMETERS DO NOT MEET ACCURACY REQUIREMENTS OF RVSM
MAX ALLOWABLE IN FLIGHT DIFFERENCE BETWEEN CAPT AND FO ALTITUDE DISPLAY FOR RVSM?
200 FEET
length
width
height
104
94
32
certified operations
day/night VFR/IFR ICING CAT I CAT II RVSM
