MD 500E Flashcards
(32 cards)
Approved as a______ place (maximum) helicopter.
five
Aerobatic flight is __________.
prohibited
Hovering downwind with a cyclic trim failure (full forward) when wind is above ______ knots is prohibited.
15
VNE with doors removed: _______ KIAS or less
130
This rotorcraft is certified in the__________ helicopter category for day and night VFR operation when the appropriate instruments and equipment required
by the airworthiness and/or operating rules are approved, installed and are in operable condition.
normal
Maximum operating _______ altitude is 16,000 feet.
density
Maximum operating density altitude is _______ feet.
16,000
The rotor brake must be in the ________ position prior to engine starting.
stowed
The rotor brake may be applied after engine shutdown with the rotor at or be· low ________ RPM.
205
Normal Operating Range: _____ RPM to_____ RPM (102 - 103 percent N2 )
487 RPM to 492 RPM
Normal Operating Range: 487 RPM to 492 RPM (____ - ____percent N2 )
102 - 103 percent N2
VNE is _______ KIAS or less
152
Maximum gross weight: _________ lbs.
3,000
Minimum flying gross weight: _______ lbs.
1,538
Engine torque limits: Maximum takeoff (5 minute):\_\_\_\_\_\_ psi torque.
87.2
Turbine outlet temperature limits: Maximum takeoff (5 minute): \_\_\_\_\_\_\_\_\_°C
810
Do not attempt engine start with cyclic stick In positions other than________. Damage to rotor head and controls will result.
neutral
Starter time limits are: __ minute ON, __ minute OFF; ___minute ON, and ___ minutes OFF.
1 minute on, one minute off, one minute on, 23 minutes off.
ABORT START IF:
- An immediate temperature rise is not observed on the _____ indicator.
- No Indication of _______ oil pressure is observed.
- Main rotor is not rotating by ___ percent _____.
- A zero or positive indication is observed on__________.
- TOT (Turbine Outlet Temperature).
- Engine
- 25 percent N1
- ammeter.
“Superimposed” means within _____ a needle width.
1/2
The type of helicopter flown is the _____________.
MD 500 E
The type of engine used in the helicopters are ________.
C20
Maximum utility stowage compartment weight is:
50 lbs.
Cargo Deck Capacity is ___________ lbs.
1300 (115 lbs per square foot).