Term
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Definition
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Term
| What is the length of the airplane? |
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Definition
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Term
| What is the height of the tail? |
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Definition
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Term
| What is the turning radius? |
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Definition
| 47' 6" which includes the distance from the outer main gear to the outside tire of the nose gear. |
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Term
| What is the minimum clearance wingtip to wingtip required for a 180 degree turn? |
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Definition
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Term
| What is the capacity of the wash basin reservoir and where does it drain to? |
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Definition
| 2.6 gallons which drains from the basin into the toilet's waste tank. |
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Term
| What is the capacity of the toilet waste tank? |
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Definition
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Term
| What are the standard weight limits for the two baggage compartment sections? |
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Definition
Section 1 (forward) is 882 lbs.
Section 2 (aft) is 771 lbs.
Total capacity of 1653 lbs. |
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Term
| What is the maximum floor loading of the cargo area? |
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Definition
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Term
| What items are on PSEU Subsystem "A"? |
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Definition
9 Door switches
3 Weight on wheels
3 LG downlocks (1 per wheel)
2 Outboard ground spoilers
1 Hyd. A reservoir low quantity sensor |
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Term
| What items are on PSEU subsystem "B"? |
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Definition
3 Weight on wheels
6 LG positions (1 downlock and 1 uplock
per wheel)
1 Nose wheel steering bypass valve
position
2 Inboard ground spoilers
1 Hyd. B reservoir low quantity
sensor |
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Term
| Which doors are annunciated on the doors system page? |
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Definition
PAX door
Galley service door
Baggage door
Emergency Exits
- 2 plug type exits in cabin
- cockpit hatch
External air door (high pressure)
Ground air door (low pressure) |
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Term
| What kinds of operations is the airplane approved for? |
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Definition
Day and night
VFR and IFR
Icing conditions |
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Term
| What is maximum number of occupants? |
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Definition
37 to include:
- 2 pilots
- 1 cockpit jumpseater
- 1 flight attendant
- 30 passengers
- 3 infants |
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Term
| What are the maneuvering load limit factors? |
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Definition
Flaps retracted: -1.0g to +2.7g
Flaps extended: 0.0g to +2.0 g |
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Term
| What is the maximum taxi and ramp weight (MRW)? |
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Definition
33,841 lbs. (Mod 00)
34,789 lbs. (Mod 10) |
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Term
| What is the maximum takeoff weight (MTOW)? |
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Definition
33,510 lbs. (Mod 00)
34,514 lbs. (Mod 10) |
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Term
| What is the maximum landing weight (MLW)? |
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Definition
31,063 lbs. (Mod 00)
31,724 lbs. (Mod 10) |
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Term
| What is the maximum zero fuel weight (ZFW)? |
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Definition
27,800 lbs. (Mod 00)
28,814 lbs. (Mod 10) |
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Term
| What is the minimum flight weight? |
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Definition
| 21,164 lbs. (Mod 00 and Mod 10) |
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Term
| What is the maximum operating altitude? |
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Definition
31,000 ft. or 35,000 ft. depending on model.
Flight above 27,000 ft. are limited to less than 3 hrs. |
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Term
| What is the maximum pressure altitude for takeoff and landing? |
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Definition
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Term
| What is the maximum tailwind component for takeoff and landing? |
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Definition
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Term
| What is the maximum demonstrated crosswind component for takeoff and landing? |
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Definition
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Term
| What is the maximum runway gradient for takeoff and landing? |
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Definition
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Term
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Definition
300 kias. / .66M
Vmo below 8000' is 270 kias. |
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Term
| What is maneuvering speed (Va)? |
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Definition
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Term
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Definition
205 kias (Mod 10)
200 kias (Mod 00) |
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Term
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Definition
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Term
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Definition
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Term
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Definition
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Term
| What is Vtire (max. tire speed)? |
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Definition
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Term
| What is Vwipe (max. wiper speed)? |
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Definition
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Term
| What are the Max ITT, N1, N2, Oil press.range, and Oil temp. range at Max Takeoff thrust setting? |
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Definition
ITT = 920 c
N1 = 105 %
N2 = 105 %
Oil press = 36 to 110 psi.
Oil temp = 21 to 135 c
All of these for a time limit of 5 minutes |
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Term
| What are the Max ITT, N1, N2, Oil press. range, and Oil temp. range at Max continuous thrust setting (MCT)? |
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Definition
ITT = 920 c
N1 = 105 %
N2 = 105 %
Oil press = 36 to 110 psi.
Oil temp = 21 to 135 c
No time limitation. |
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Term
| What is max N2, oil press. range, and oil temp. range at Flight Idle? |
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Definition
N2 = 65%
Oil press = 20 to 110 psi.
Oil temp = -40 to 135 c |
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Term
| What are the oil press. and oil temp. ranges at ground idle? |
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Definition
Oil press = 20 to 110 psi.
Oil temp = -40 to 135 c |
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Term
| What are the Max ITT, oil press. range and minimum oil temp. during starting? |
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Definition
ITT = 950 c
Oil press. = 0 to 220 psi. with a steady increse within 20 seconds of start of N2 rotation.
Oil temp. = -40 c |
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Term
| What are the transient Max. ITT, N1, N2, Oil press., and oil temp. limitations? |
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Definition
ITT = 950 c (for 20 secs.)
N1 = 106% (for 20 secs.)
N2 = 106% (for 20 secs.)
Oil press for 20 secs. = 0 to 20 psi.
Oil press for 90 secs. = 110 to 220 psi
Oil temp for 20 and 90 secs. = 143 c |
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Term
| What are the air turbine starter (ATS) limits? |
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Definition
Two starting cycles, each cycle not longer than 45 secs., are permitted in a 10 min. period with a minimum 10 min. cooling time after.
OR
A maximum of 2 mins. accumulated motoring time is permitted with a minimum cooling time of 20 mins. |
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Term
| What are the maximum and minimum tank fuel temps. for Jet A? |
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Definition
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Term
| What fuel additives are approved for UJC airplanes? |
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Definition
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Term
| What is the max. allowable fuel imbalance? |
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Definition
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Term
What are the max. fueling pressures in automatic mode and manual modes?
What is the max. defueling pressure? |
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Definition
Auto = 50 psi
Manual = 30 psi
Defuel = -10 psi |
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Term
| What are the total fuel capacities for automatic pressure refueling, manual pressure refueling, and gravity refueling? (in lbs.) |
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Definition
Auto = 7800 lbs.
Manual and Gravity = 7970 lbs. |
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Term
| What is the total oil tank capacity and the minimum capacity? (in gallons) |
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Definition
Total = 2.11 gallons
Minimum = 1.32 gallons |
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Term
| What is the max. pressure altitude for engine starting on the ground using the APU? |
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Definition
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Term
| What is the max. pressure altitude for APU operation and engine starting using the APU while airborne? |
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Definition
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Term
| What is the max. pressure altitude for APU start in flight? |
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Definition
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Term
| What are the APU starter limits? |
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Definition
| Three start attempts, with 1 min. 30 sec. total starter running time, followed by a 10 min. cool down. |
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Term
| Unless absolutely essential to the safety of a flight, when must the APU NOT be started in flight? |
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Definition
- after an unsuccessful abnormal APU restart following automatic shutdown without any failure messages
- after an unsuccessful abnormal APU restart following a manual shutdown due to a preceding hot start
-after an automatic shutdown with an amber failure message displayed on the APU page
-after the APU was shut down via the fire protection system |
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Term
| What is the max. continuous load on the APU generator? |
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Definition
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Term
| What are the 4 main electrical system sources (DC and AC) not including the APU? What is the max load for each? |
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Definition
DC GEN 1 = 400A / 28V DC
DC GEN 2 = 400A / 28V DC
AC Alternator 1 = 90A / 115V AC / 30kVA
AC Alternator 2 = 90A / 115V AC / 30kVA |
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Term
| What type of hydraulic fluid does the D328J use? |
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Definition
| mil-spec MIL-H-5606 (orange in color) |
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Term
| What is the max. altitude for landing gear operation? |
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Definition
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Term
| In relation to brake temerature, when is takeoff prohibited? |
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Definition
1) if BRK TEMP HIGH is displayed on EICAS
2) when the BTMS is inoperative unless brakes are cool enough to touch |
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Term
| What is the max. altitude with flaps extended? |
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Definition
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Term
| What is the max. altitude for single pack operation? |
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Definition
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Term
| What is the max. cabin pressure differential? |
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Definition
| 6.9 psi (7.6 psi for FL350 mod) |
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Term
| What is the max. cabin pressure differential for landing? |
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Definition
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Term
| When should the ECS FLOW mode be switched to the HIGH setting? |
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Definition
-with 24 or more pax onboard
-above FL310 with 22 or more pax onboard |
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Term
| When is it ok to take off with the combined use of APU bleed and either engine bleed running the ECS? |
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Definition
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Term
| Takeoff is not permitted when the attitude difference displayed on both PFDs and the standby attitude indicator is ______? |
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Definition
| 3 degrees or more for both bank and pitch |
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Term
| What is the minimum altitude for autopilot use when on (1) a coupled ILS approach, (2) a non-precision approach, and (3) for climb, cruise and descent? |
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Definition
(1) 100 ft. AGL
(2) 200 ft. AGL
(3) 500 ft. AGL |
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Term
| What two EICAS cautions, when they are displayed, prohibit the autopilot from being used? |
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Definition
1) RUDDER NOT LIMITED
2) RUDDER LIMIT FAIL |
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Term
| What atmospheric conditions constitute icing conditions both on the ground and in flight? |
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Definition
9 c or below and visible moisture present
(clouds, fog with viz.1 sm or less, rain, snow, sleet and ice crystals) |
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Term
| When is the airplane certified to fly into known severe icing conditions? |
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Definition
| Never...it is prohibited! |
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Term
| When should the engine intake anti-ice NOT be used on the ground? |
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Definition
| While stationary at temps. above 5 c OAT. |
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Term
| When should the de-ice boots not be used in flight? |
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Definition
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Term
| When should the elevator/rudder horn anti-icing system be activiated? |
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Definition
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Term
| When must the wing inspection lights be operative? |
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Definition
| Prior to flight into icing conditions at night. This supersedes any relief given by the MEL. |
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Term
| What special considerations need to be taken into account while flying an ILS as written in FAA AD 2006-22-05? |
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Definition
1) When corssing the OM on Gld. Slope, altitude must be checked against the published altitude.
2) With one Gld. Slope receiever, fly no lower than published LOC. ONLY MDA.
3) With two Gld. Slope receievers, both RMU's must be tuned in to the LOC frequency and both pilots monitoring the apporach using independent displays |
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