Alex's Study Guide Flashcards
- What is VMO?
340 KCAS
- What is maximum MMO?
0.88 MT
- What is VA?
S/N 1000-1213 without ASC 190: 170 KCAS
S/N 1214 & subsequent, A/C with ASC190: 206 KCAS
- What is VMC?
VMCA – 104 KCAS, VMCG – 111 KCAS
- What is turbulence penetration speed?
270 KCAS/0.75 MT
- What is maximum ramp weight?
S/N 1000-1213 without ASC 190: 73,600 lbs.
S/N 1214 & subsequent, A/C with ASC190: 75,000 lbs.
- What is maximum takeoff weight?
S/N 1000-1213 without ASC 190: 73,200 lbs.
S/N 1214 & subsequent, A/C with ASC190: 74,600 lbs.
- What is maximum landing weight?
S/N 1000-1213 without ASC 190: 58,500 lbs.
S/N 1214 & subsequent, A/C with ASC190: 66,000 lbs.
- What is maximum zero fuel weight?
S/N 1000-1213 without ASC 190: 46,500 lbs.
S/N 1214 & subsequent, A/C with ASC190: 49,000 lbs.
- What is the maximum approved altitude for takeoff and landing?
15,000 feet
- What is the maximum approved slope for takeoff and landing?
+/- 2%
- What is the maximum approved tailwind (component) for takeoff and landing?
10 knots
- What is the maximum approved operating altitude?
45,000 feet
- What limitation is there on the use of landing lights?
Ground operation is limited to 5 minutes
- Other than the AFM, what 4 publications are required to be immediately available to the flight crew according to Section 1 of the AFM?
Honeywell SPZ-8000 (or SPZ-8400) DIFCS Manual, Honeywell FMS Manual, TCAS manual (if installed), (E)GPWS manual (if installed)
- What is the minimum altitude for autopilot engagement?
200’ AGL
- What is the minimum altitude for autopilot operation on approach?
50’ AGL (Unless VNAV is used then the minimum altitude for autopilot coupled IFR VNAV operations is 300’ AGL or 50’ below minimum descent altitude, whichever is higher.)
- What is the minimum altitude for autothrottle operation on approach?
50’ AGL
- When is the autothrottle not authorized for use during takeoff or go-around?
When wing anti-ice is used.
- What is the engine starter duty cycle?
30 secs. ON, 3 mins. OFF, 30 secs. ON, 3 mins. OFF, 30 secs. ON, 15 mins. OFF
- What is the duty cycle for airstart ignition?
S/N 1000-1249 without ASC 304: 30 secs. ON, 30 secs. OFF; or, 5 mins. ON, 30 mins. OFF
S/N 1250 & subsequent, A/C with ASC 304: Continuous operation
- What is the maximum engine fuel temperature?
90° C indefinitely, or 120° C for 15 minutes
- What is the minimum engine fuel temperature?
-40° C/F
- What is the maximum oil temperature?
105° C indefinitely, or 120° C for 15 minutes
- What is the minimum oil temperature for starting?
-40° C/F
- What is the minimum oil temperature for opening the power lever?
-30° C
- What is the limitation regarding the use of the engine synchronizer system?
The synch must be off for takeoff and landing.
- When do you need to cancel reverse thrust during landing?
Initiate cancellation of reverse thrust by 70 KCAS to achieve idle reverse thrust by normal taxi speed.
- What is the maximum APU EGT?
Start 0-60%: 988° C; 60%-100%: 821° C – 732° C; With bleed air selected: 680° C
- What is the maximum APU RPM?
110.0%
- What are the APU starter duty limits if starting on the airplane batteries?
3 – 30 second attempts, followed by 20 minutes off, followed by 3 more 30 second attempts, followed by 1 hour off.
- What are the APU starter duty limits if starting on an external power unit?
2 – 15 second attempts, followed by 20 minutes off, followed by 2 more 15 second attempts, followed by 1 hour off.
- What is the APU starter duty cycle if the starts are successful?
Successful consecutive starts are limited to 6 starts with 10 minute intervals between starts, then 1 hour off.
- What is the APU starting envelope?
From sea level to 15,000’ at airspeeds below 250 KCAS, the start is guaranteed.
From 15,000’ to 20,000’, start is possible.
- What limitation must be considered if the APU is operated above 30,000 feet?
An inspection is required if the APU is operated above 30,000 feet for more than one hour or more than 5 times.
- What is the allowable electrical load on the APU airborne?
S/N 1000-1155 without ASC 96: APU alternator can deliver 100% power from sea level to 22,000’. From 22,000’ to 30,000’ the limit decreases linearly to 50% power.
S/N 1156 and subsequent, aircraft with ASC 96: The APU alternator can deliver 100% power from sea level to 30,000’. From 30,000’ to 41,000’ the load decreases in steps to 50%.
Note: Do not operate these APU’s above 35,000’
- What limitations apply to the standby electrical system (ABEX)?
Minimum HP RPM is 67.0%
Speedbrakes may be used; however, operation should be slow (approx. 5 seconds for full range movement.)
Landing is approved if auto ground spoilers and thrust reversers are not used for landing.
- What limitation must be observed before pulling the flight power shutoff handle?
Speedbrakes must be retracted.
- What is VLE?
250 KCAS / 0.70 MT
- What is VLO?
Normal – 225 KCAS / 0.70 MT
Alternate – 175 KCAS
- What is maximum tire speed?
S/N 1000-1213 without ASC 190: 182 knots
S/N 1214 & subsequent, A/C with ASC190: 195 knots
- What is the maximum altitude with the landing gear extended?
20,000 feet
- When are speedbrakes not authorized?
When the flaps are at 39° or landing gear is extended.
- If a takeoff is made with ground spoilers inoperative what configuration must be used?
The anti-skid must be operative and flaps 20° must be used.
- If a takeoff is made with anti-skid inoperative what configuration must be used?
Ground spoilers must be operational and flaps 20° must be used.
- What two (2) CAS messages must be cleared before takeoff?
BRAKE FAIL (and BRAKE PEDAL - BBW only)
- What are the VFE speeds?
Flaps 10° – 250 KCAS / 0.60MT
Flaps 20° – 220 KCAS / 0.60MT
Flaps 39° – 170 KCAS / 0.60MT (S/N 1000-1213 without ASC 190)
Flaps 39° – 180 KCAS / 0.60MT (S/N 1214 & subsequent, A/C with ASC190)
- What is the maximum speed with both mach trim compensators inoperative or electric trim inoperative?
0.75 MT
- What speed considerations must be observed if the yaw damper fails in flight?
Above FL180 – 220 KCAS minimum
Below FL180 – See chart in AFM (Speed vs. Fuel Load)
- What limitations apply if both mach trim compensators and the yaw damper are inoperative?
Maximum altitude is 41,000 feet; speed limits for both apply.
- Are the mach trim compensators required to be on during flight?
YES
- Are the stall barrier computers required to be on during flight?
YES
- What is the maximum altitude at which you can operate with flaps 39?
20,000 feet
- What limitation applies if a takeoff is made with the yaw damper inoperative?
Maximum fuel load is 9,000 lbs.
- What bleed consideration must be observed above 41,000 feet?
Both engine bleeds must be on and each engine must be bled by either the air-conditioning system or engine cowl anti-ice.
- What is the maximum cabin differential?
9.8 PSID
- What is the maximum cabin differential permitted during taxi, takeoff and landing?
0.3 PSID
- What is the maximum windshield wiper speed?
200 KCAS
- When is cowl anti-ice required on the ground?
When the static air temp (SAT) is below 8° C and visible moisture, precipitation, or wet runway are present. Engine operation of 85% LP RPM for one minute is recommended just prior to takeoff and at intervals of not more than 60 minutes under these temperature and moisture conditions.
- When is wing anti-ice required?
When icing conditions are imminent or immediately upon detection of ice formation on wings, winglets, or windshield edges.
- What conditions must be met in order to turn off one boost pump while at cruise?
Fuel contains anti-icing additive, or, fuel tank temperature is above 0° C.
- What is the total usable fuel?
29,500 lbs.
- What is the maximum permissible fuel imbalance?
It increases linearly from 400 lbs. at a gross weight of 60,500 lbs. to 2,000 lbs. at a gross weight of 55,000 lbs.
- If a thrust reverser deploys accidentally, what would happen to engine thrust?
Power on that engine is reduced to idle by a cable that automatically retards the respective power lever.
- What EVM indications are considered normal in icing conditions and otherwise?
In icing – 1.25; other times – 0.60
- When checking the engine oil, what precaution must be observed when reading the sight gage?
There are two tapes on either side of the sight gage, a red one for the left engine and a green one for the right engine.
- What 4 indications should be observed prior to opening the HP fuel cock during engine start?
Start Valve Open (SVO) light, ignition light (IGN), positive LP rotation, minimum of 15% HP RPM
- Which hydraulic systems power the thrust reversers?
Left – combined hydraulic system; Right – flight hydraulic system.
- During preflight what should you look for on the thrust reversers?
General condition, doors fully stowed, hydraulic leaks.
- If a flameout occurred and you are unable to close the HP fuel cock what would you suspect has happened?
Shaft separation
- Where do we tap customer bleed?
7th and 12th stages.
- Will the oil filter bypass?
YES
- Will the fuel filter bypass?
NO
- What is the minimum engine idle on the ground / airborne with flaps less than 22° / airborne with flaps at or greater than 22°? (Assuming no malfunctions.)
46.6% HP RPM / 46.6% HP RPM / 67.0 % HP RPM
- What do the colors on the engine instruments indicate?
Red – maximum and/or minimum; Amber – takeoff and caution; White – normal
- When do the standby engine instruments come on?
In auto, if a primary engine instrument fails; in manual, all the time.
- What engine parameters are displayed on the standby engine instruments?
All of the primary engine instruments. (Left side of DU3)
- What would you suspect if the APU master switch is turned on and the low oil pressure light did not come on?
The APU inlet door did not open.
- What is the APU used for on the ground? In the air?
Ground – electricity & air; Air – electricity only
- When shutting down the APU by using the overspeed/test switch, when should you turn off the APU master switch?
When the APU RPM is below 10%
- If an automatic shutdown of the APU occurs, where would you look to determine what caused the shutdown?
On the APU fault indicator panel in the tail compartment
- If a flag is in view on the APU fault panel what should be done before starting the APU?
Actuate the reset switch, and make a note of which flag was in view.
- From where does the APU receive it’s fuel?
From the left fuel ejector line.
- If the APU is started and for some reason it shuts down, and the decision is made to restart, what must be done with the APU cockpit controls prior to the restart?
The APU master switch must be turned off then back on.
- Once the APU is operating, how long should you wait before placing electrical loads on the APU? Pneumatic loads?
Electricity is available immediately; the APU should be operated for 1 minute before air is extracted.
- What is the correct configuration for APU shutdown?
Alternator – OFF, air – UNCHANGED, below 10% RPM – MASTER OFF
- When we shutdown the APU we press the overspeed/test switch. What does this actually do?
It simulates and overspeed of 114%,which causes the ECU to close the APU fuel valve.
- After the APU is operating, how would you turn on the alternator?
By selecting AUX PWR on.
- If the APU is operating and the AUX PWR switch is on, when both engine driven alternators are operating, will the APU OFF light be on?
NO