Limitations Flashcards
1
Q
APU starter limitations
A
- Between 3 attempts - 1 min off
- Between 2 series of 3 attempts - 30 min off
2
Q
Autopilot SE go-around & approach mode selection
A
- -SE go-around w AP engaged is prohibited.
- -App mode selection during loc capture is allowed only when aircraft is inbound.
3
Q
Minimum/maximum temperature for manual anti-icing operations
A
- -40C-+10C SAT (ground/takeoff)/TAT (flight)
- -No temp limit for auto AI sys operation.
4
Q
Maximum Airpseed After Takeoff/During Climb Without Retrimming
A
160
5
Q
Yaw damper minimum altitudes (not authorized)
A
- -Takeoff to 500’ AFL
- -Landing
6
Q
Vmo
A
- <= 8,000 250
- > 8,000-10,000 250-320 [Red Line]
7
Q
CON
A
901/100/57.0-102.4
8
Q
Vmo/Mmo
A
320/.78
9
Q
Vb/Mb
A
- <= 10,000 200
- > 10,000 250/.63 (lower)
10
Q
T/O-1 (A1)
A
948/100/57.0-102.4
5 minutes
11
Q
Contaminated runway
A
- >25% of RFL within width to be used
- >1/8 inch standing water/slush/wet snow
- >3/4 inchES dry snow
- compacted snow
- ice
12
Q
T/O RSV (A1/3)
A
948/100/57.0-102.4
5 minutes
13
Q
Minimum Temperature for TOL
A
- -40C
- In the event of a landing below -40C, the aircraft may not TO w/o further mx insp.
14
Q
Max ITT for Engine Start
A
800
15
Q
Demonstrated Crosswind for TOL
A
30
16
Q
ALT T/O-1
A
917/100/57.0-102.4
5 minutes
17
Q
Engine Cool Down
A
- Run each engine for a minimum of 1 minute at idle/taxi thrust before shutdown
- (After landing or high power runs)
18
Q
AHRS alignment
A
The aircraft must not be moved when the AHRS is in the initialization mode until all attitude & heading information presented on the PFD is displayed.
19
Q
Icing conditions
A
- Ground: Icing conditions exist when the OAT is 10C or below and visible moisture in any form is present (such as clouds/IC/rain/snow/sleet/fog with vs 1SM or less) [6] OR
- Icing conditions also exist when operating on ramps/taxiways/runways where surface snow/ice/standing water/slush [4] may be ingested by engines/freeze on engines/nacelles/sensor probes [3].
- On the ground, do not rely on visual icing evidence or ice detector actuation to turn on AI system. Use the temp and vis moist criteria as spec above. Delaying use of AI until buildup is visible from cockpit may result in ice ingestion and possible engine damage/flameout.
- Flight: Icing conditions may exist whenever the TAT is 10C or below and visible moisture (above).
- Notwithstanding ID monitoring, crew remains responsible for monitoring potential icing condix for man activation of the IPS if icing condix are present (known icing) and the IDS is not activating the IPS.
20
Q
Autopilot minimum altitudes
A
- -Takeoff: 500’ AFL
- -Landing: MDA/DH/DA/TPA
21
Q
TAT in cruise flight
A
-45C above 25,000
22
Q
Thrust Reverser Use
A
- TR are Intended for use during RTO and landing only.
- After initiating RT, full stop MUST be made.
- Maximum RT MUST be used
- Whenever stopping distance deemed to be critical & use will prevent rwy excursion
- When landing on rwys with M or P BRA unless landing distance penalty (flip cards) applied
- Idle REV MAY be used
- Dry <= 7,000 LDA
- Non-dry & BRAG
- TR use is PROHIBITED for
- Power-back ops
- Taxi ops
- TLs stablized in any intermidate posn between IDLE reverse and MAX reverse
23
Q
Oil Pressure Transient
A
- Amber range up to 115 for 5 minutes in all thrust modes.
- Amber range above 115 up to 155 up to 2 minutes.
- Total time in amber range not to exceed 5 minutes.
- Operation in red range NA.
- Any exceedence must be monitored and logged in the AML by the crew.
24
Q
Minimum/Maximum altitudes
A
- -1,000-37,000
- TOL 8,000
25
Maximum altitude after in flight depressurization
* 10,000' MSL,
* unless MEA or other constraints req a higher alt
26
Engine Oil Level
* Minimum dispatch oil quantity is 8 quarts before engine start
* Or 7 quarts after engine start
27
Va
200
28
Vloe/Vlor/Vle
250/200/250
29
Vfe 9/18/22/45 (plus transient)
250/200/200/145 Momentary AS excursions that are due to wind gusts or turbulence are **allowed** up to 155 with no crew or maintenance action required.
Steady state operation over 145 is not **allowed** and must be entered **into** the AML.
30
T/O (A1/3)
929/100/57.0-102.4
5 minutes
31
Rudder deflection below Va
Full or nearly full rudder deflection in one direction followed by a full or nearly full rudder deflection in the other direction, even at speeds below Va, can dramatically increase the risk of structural failure of the v-stab or the rudder.
32
Engine Warm Up
Minimum Oil Temperature
Engine Warm Up Procedure
* The engines must be allowed to run at low thrust to _stabilize engine temperatures before takeoff thrust_ is selected.
* Run the engine at idle/taxi thrust a minimum for _4 minutes for cold_ engines
* and _2 minutes for warm_ engines.
* An engine is considered cold if it has been shut down for _more than 90 minutes_.
* Prior to increasing _N2 above 83%_, the engine oil temperature must be a _minimum of 40C_.
* In lieu of this minimum oil temp limit, it is acceptable to run the engine for at least _8 minutes_ and ensure the oil temperature is in the _green range_ prior to advancing the TLs for takeoff.
33
Maximum Altitude for Flap Extension
20,000' MSL
34
Engine Starter Limitations
Dry Motoring
* Cycles 1-4: 1 on, 1 off
* Cycle 5 and up: 1 on, 5 off
* Dry motor: Up to 5 on, 5 off
35
Minimum Oil Temperature for Engine Start
-40C
36
Maximum Tailwind Comp TOL
10
37
T/O-1 (A1/3)
929/100/57.0-102.4
5 minutes
38
Holding Configuration
* Landing Gear - UP
* Flaps - UP
* Airspeed/Icing Condix - 200 MINIMUM
39
Minimum Oil Temperature for Takeoff
* 40C
* Or perform Engine Warm Up procedure
