Term
Reduced Vertical Separation Minimum
RVSM requirements |
|
Definition
Auto pilot must be operational
Altitude Alerting System must be operational
Altitude reporting transponder 1 must be operational
Air Data computers (2) Both must be operational |
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Term
Altitudes
Manufacture max
Air Wisconsin max
Max takeoff and landing
minimum takeoff and landing |
|
Definition
41,000 Man. Max
37,000 AWAC Max
10,000 Max takeoff and landing
-1,000 Minimum takeoff and landing |
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Term
Maneuvering Load Limits (G's)
Flaps retracted
Flaps extended |
|
Definition
retracted= -1g to +2.5g
Extended= 0g to +2.0g |
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Term
| AWAC policy on side slip maneuvering |
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Definition
| Avoid unnecessary and large side-slip maneuvers during low speed operations. |
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Term
Temperature
Takeoff minimum (ambient)
Takeoff maximum (-1,000ft to sea level)
Takeoff maximum (sea level to 10,000ft)
Enroute maximum (sea level to 10,000ft)
Enroute maximum (above 10,000ft) |
|
Definition
Takeoff minimum (ambient) -40*c
Takeoff maximum (-1,000ft to sea level) +50*c
Takeoff maximum (sea level to 10,000ft) ISA+35*c
Enroute maximum (sea level to 10,000ft) ISA+35*c
Enroute maximum (above 10,000ft)
ISA+30*c |
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|
Term
Flap Operating / Extended Speeds
Flaps
8
20
30
45 |
|
Definition
Max operating speeds
8= 200 Kias Awac (230 manufacture)
20= 200 Kias Awac (230 manufacture)
30= 185 Kias
45= 170 Kias |
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|
Term
Landing gear max operating speeds
landing gear extension (Vloe)
Landing gear retraction (Vlor)
Max extension speed |
|
Definition
landing gear extension (Vloe) 250kias
Landing gear retraction (Vlor) 200kias
Landing gear extended 250kias |
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|
Term
| Turbulence Penetration Speeds |
|
Definition
Turbulence Penetration Speeds
280 kias or .75 Mach |
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|
Term
Maximum Airspeed operating Limitations
Flight test and pilot training deployment
Following automatic or manual deployment
operationally necessary (windmill airstarts)
Operational necessary |
|
Definition
Maximum Airspeed operating Limitations
Flight test and pilot training deployment: 215kias
Following automatic or manual deployment
:250Kias
operationally necessary (windmill airstarts):251 to 330 up to 12 min.
Operational necessary: 331 o 335 up to 4 min. |
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|
Term
| which A/C do not have ADG speed limits? |
|
Definition
| A/C 405-430, 434 and subsequent |
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|
Term
|
Definition
|
|
Term
Windshield wiper operation
Vwipe |
|
Definition
|
|
Term
Structural Weight Limitations
Max weights
Ramp
Takeoff (MTOW)
Landing (MLW)
Zero Fuel (MZFW)
Minimum Flight Weight |
|
Definition
Ramp: 53,250
Takeoff (MTOW): 53,000
Landing (MLW): 47,000
Zero Fuel (MZFW): 44,000
Minimum Flight Weight: 30,000 |
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|
Term
| Max persons allowed on cl-65 |
|
Definition
57
50 seats
3 lap children
1 flight attendant
2 pilots
1 jumpseater |
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|
Term
Cargo Compartment Loading Limitations
Max weight in cargo bin |
|
Definition
manufacture is 3,500lbs
AWAC installed 100 lb ballast
AWAC limit is 3,400lbs |
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|
Term
Runway slope limitations
minimum slope
maximum slope |
|
Definition
|
|
Term
Crosswind / Tailwind Limits
Dry Runway
Wet Runway
Snow/Ice covered
Max tailwind for takeoff or landing |
|
Definition
Dry Runway: 27knots
Wet Runway: 24knots
Snow/Ice covered: 15knots
Max tailwind for takeoff or landing: 10knots |
|
|
Term
Contaminated Runway Operations
Maximum Depths for takeoff and landing.
Standing water
Slush
Wet Snow
Dry Snow |
|
Definition
Standing water: .50"takeoff .75"landing
Slush: .50" takeoff .88"landing
Wet Snow: 1.00"takeoff 1.5" landing
Dry Snow: 3.0" takeoff 3.75" landing |
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|
Term
| Rotation Rate and pitch attitude |
|
Definition
set bug for 10* pitch up
no more than 3* per second pitch to 10* pitch climb |
|
|
Term
| If cargo is being hauled how close to an airport must we be? |
|
Definition
|
|
Term
| When must crew headsets be worn? |
|
Definition
|
|
Term
Cold weather operations
When must a tactile check of the wing during preflight be accomplished? |
|
Definition
The OAT is 5*c or less; or
The wing fuel temperature is 0*C or less; or
The atmospheric conditions have been conducive to frost formation. |
|
|
Term
Air Conditioning / Pressurization
Max differential pressures:
Positive
Negative
During taxi, takeoff, and landing |
|
Definition
Positive: 8.7psi
Negative: -.05psi
During taxi, takeoff, and landing: .1psi |
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|
Term
Auto-Flight
Restricted Modes |
|
Definition
Restricted Modes
PITCH for climbs (except takeoff)
DES mode during an approach is prohibited |
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|
Term
Auto-Flight
Minimum altitudes for use |
|
Definition
can not use below 600ft AGL except when:
visual and non-precision approaches can go to 400ft AGL
For precision approaches, the minimum autopilot use is 80 ft AGL
at 50ft below the approved minimum descent altitude or DH
In RVSM the auto pilot must be coupled to the appropriate transponder. |
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|
Term
| What type of APU is in the crj-200 |
|
Definition
|
|
Term
APU Limitations
Max operating altitude
Max APU start altitude
Max altitude for extracting APU bleed air
Max altitude for engine starts using APU bleed air |
|
Definition
Max operating altitude: 37,000ft
Max APU start altitude: 30,000ft
Max altitude for extracting APU bleed air: 15,000ft
Max altitude for engine starts using APU bleed air: 13,000ft |
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|
Term
| At what Altitude can APU oil foaming occur? |
|
Definition
|
|
Term
|
Definition
|
|
Term
|
Definition
|
|
Term
|
Definition
| 974*c then no higher than 743*c |
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|
Term
| Air Conditioning in flight from APU bleed air is not permitted above...? |
|
Definition
|
|
Term
| Engine Start during ground operations |
|
Definition
No bleed air extraction limitation.
Each engine ,ay be started using the APU as a bleed air source.
If both engines are to be started using the APU bleed air, then the operating engine's thrust must not exceed 70% N2 |
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|
Term
| Engine start during flight |
|
Definition
During single engine operations, APU bleed air extraction for an engine start is not permitted.
During double engine failure conditions, APU bleed air extraction for engine starts is permitted; however APU bleed air extraction is limited to 13,000ft and below. |
|
|
Term
| What is the Max permissible load on the APU generator in flight is ___kVA |
|
Definition
|
|
Term
| Minimum ambient temp. for starting a cold-soaked APU on the ground? |
|
Definition
|
|
Term
APU start cycles
start 1,2,3,4 |
|
Definition
1: 15sec(GPU) 30sec(Batt.) then 2 min off
2: 15sec(GPU) 30sec(Batt.) then 20 min off
3: 15sec(GPU) 30sec(Batt.) then 2 min off
4: 15sec(GPU) 30sec(Batt.) no further start attempts for at least 40 minutes |
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|
Term
|
Definition
| 10th stage valves must be closed for takeoff and landing if the engine cowl and / or wing anti-ice systems have been selected ON. |
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|
Term
ELECTRICAL
AC system loads must not exceed
0 to FL350
Above FL350 to FL370
Above FL370 |
|
Definition
AC system loads must not exceed
0 to FL350:
Main generators 30kVA APU gen 30kVA
Above FL350 to FL370
main GEN 25kVA APU GEN 30kVa
Above FL370
main GEN 25kVA APU gen 0kVA |
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|
Term
DC system load must not exceed...
In Flight:
Ground Operations: |
|
Definition
In Flight: max of 100amp per TRU
Ground Operations: To protect the CRT displays DC power only for 5 mins. or less while on ground |
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|
Term
| Flaps are prohibited when? |
|
Definition
| Enroute and or above 15,000ft |
|
|
Term
Flight Spoilers Limitations
AWAC:
Manufacture: |
|
Definition
AWAC: Flight spoilers must not be extended in flight below an altitude of 1,000AGL.
Must not be extended in flight at airspeeds below the recommended approach (Vref+5) or maneuvering (Vref+10) speeds plus 17kias
Manufacture: bellow 300ft AGL |
|
|
Term
|
Definition
the stall test must be accomplished before the first flight of the day.
Both stall protection system switches must remain on for all phases of flight. |
|
|
Term
| Integrated Standby Instrument and a back course approach.... |
|
Definition
| it is prohibited to use the ISI because it will only reverse sense. |
|
|
Term
| when setting DH/ MDA altitude if the altitude is 185 and the knob sets only 10 increments, what MDA do you set? |
|
Definition
| 190. You set the next highest 10ft if it is not on an even 10ft. |
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|
Term
Operational Fuel Limitations
takeoff with a fuel load of 500lbs in the center tank is prohibited unless there is a total off _______ in each wing tank |
|
Definition
|
|
Term
| Minimum fuel for a go-around |
|
Definition
| 450lbs per side (900lbs) with a pitch of 10* nose up. |
|
|
Term
| Maximum Permissible Fuel Imbalance |
|
Definition
| 800lbs between the wing tanks |
|
|
Term
| pressure fueling will give us a total of _______lbs of fuel |
|
Definition
|
|
Term
| Lowest engine fuel temperature for takeoff |
|
Definition
|
|
Term
Crossflow Restrictions
powered (auto) crossflow and gravity crossflow must be turned ____ for takeoff |
|
Definition
|
|
Term
| Lowest engine fuel temperature for takeoff |
|
Definition
|
|
Term
Icing condition Definition
Visible Moisture Definition |
|
Definition
In flight at a TAT of 10*c or below, and visible moisture in any form is encountered (such as clouds, rain, snow, sleet, or ice) except when SAT is -40*c or below.
Visible moisture includes, clouds, fog with visibility of 1 mile or less, rain, snow, sleet or ice. |
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|
Term
| When must wing and cowl be on during flight |
|
Definition
When ICE light is on or when in icing conditions and speed below 230kias.
cowl must be on when temp is below 10*c and in icing conditions.
when on ground wing must be on when temp is below 5*c
On ground cowl is on when temp is 10*c or below and visible moisture is present |
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|
Term
| Red Strobe Lights are used for |
|
Definition
| used for ground recognition purposes only and must not be used as anti-collision lights |
|
|
Term
| taxi lights must be off when |
|
Definition
| whenever the aircraft is stationary in excess of 10 minutes. light may burn through the plastic if not complied with. |
|
|
Term
|
Definition
| 2, General Electric CF34-3B1 |
|
|
Term
Maximum Continuous Thrust limits
RED
Amber
Green |
|
Definition
RED 900*c; 874-900*c after 30 seconds
Amber 874-900*c 0 to 30 seconds
Green 0 to 874*c |
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|
Term
| Maximum Transient oil PSI after a cold start |
|
Definition
156psi
130psi at idle for 10 minutes max
Engine must remain at idle until it reaches normal range |
|
|
Term
|
Definition
2% max split between engine.
if N2 is 57% or less with an OAT of -20*c or greater, DO NOT ACCELERATE ABOVE IDLE. |
|
|
Term
| Engine warm up and cool down |
|
Definition
| Engines must run at idle for 2 minutes before takeoff thrust and 2 minutes before shutdown |
|
|
Term
| define cold soaked aircraft |
|
Definition
first flight of the delay when plane sat in temp of -30*c or below for more than 8 hours:
N1 fan rotation must be verified before introducing fuel for engine start.
Thrust reverses must be actuated and stowed in a 5 second cycle |
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|
Term
Continuous Engine Ignition
Requirements for use |
|
Definition
takeoff and landings on contaminated runways
takeoffs with high crosswind components (15+)
Flight through mod or heavier intensity, Rain, Turbulence
Flight in the vicinity of thunderstorms |
|
|
Term
| when must thrust reverser be used |
|
Definition
when LAHSO operations or when landing on runways less than 6,500ft.
when landing on a contaminated runway.
Abnormal or emergency procedures
When the crew feels the need to |
|
|
Term
Starter cranking Limits
Start 1,2,3,4 |
|
Definition
1: 1 min on 10 seconds off
2: 1 min on 10 seconds off
3: 1 min on 5 min off
4: 1 min on 5 min off |
|
|
Term
| when must the starter not be used? |
|
Definition
| when indicated N2 RPM exceeds 55% |
|
|
Term
When can thrust levers be moved from off to IDLE?
On ground
In flight |
|
Definition
On ground when ITT is below 120*
In flight when ITT is below 90* |
|
|
Term
|
Definition
| When the thrust levers are off (no fuel flow) and the starter button is on |
|
|
Term
Dry motoring limitations start cycles
start 1,2 |
|
Definition
1: 90 seconds ON 5 min off
2: 30 seconds ON 5 min off |
|
|
Term
Flexible Thrust Operation
When can we NOT FLEX |
|
Definition
if the normal takeoff fan speed is less than 85% N1.
If wing and or cowl anti-icing bleeds are in use
On contaminated runways
when warnings of wind shear or downdrafts have been forecast |
|
|
Term
|
Definition
| the hyd 3b pump switch must be selected On instead of Auto for all phases of flight |
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