1H-60(H)G-1 Section 5 Flashcards
On any VID strip ___ consecutive lights must not be out and NO lights may be out at a transition point.
Two
The maximum allowable Nr for normal flight operations and emergency procedure training is ___%.
The maximum allowable Nr for Functional Check Flights is ___%.
110%
120%
Maximum wind velocity for rotor start or stop is ___ knots from any direction.
45
Maximum Nr for rotor brake application is ___%
Routine rotor stops shall be done between ___ - ___%.
- 76%
- 30 to 50%. Limit rotor brake stops to 180 psi. Application below 30% Nr should not regularly occur or damage to rotor head may occur.
At 100% Nr on the ground and during level flight, the XMSN oil pressure should remain steady in the ___ - ___ psi range. If pressure should not remain steady or is below 45 psi, make an entry in AFTO Form ____.
50 to 55 psi
781A
Engine ____ check in flight is prohibited.
Overspeed
The rappelling attaching points have a load limit of ___lbs each. Maximum of __ gunners belts may be attached to a single repelling ring.
4,000 lbs.
2 gunners belts
The maximum weight that may be suspended from the cargo hook is ___lbs.
8,000 Lbs.
The maximum weight that can be suspended from the rescue hoist is ___ lbs.
600 Lbs.
Engine starter limits when OAT is ≤ 16°C
1st attempt - 1 minute rest
2nd attempt - 3 minute rest
3rd attempt - 1 minute rest
4th attempt - 30 minute rest
Engine starter limits when OAT is 16-52°C
1st attempt - 1 minute rest
2nd attempt - 30 minute rest
The minimum ground air source required to start the engines is ___ psi and ___ ppm at +___degrees C
The maximum ground air source to be applied to the helicopter is ___ psi at +___degrees C
Min - 40 psi / 30ppm / +149deg C
Max - 50psi / +249deg C
Cross bleed starts will not be attempted unless the source engine’s Ng is above ___%, Nr is ___%, and what advisory light light is OFF?
Ng source engine 90%
Nr 100%
ENG ANTI-ICE ON advisory light - off
The maximum weight that may be suspended from the FRIES release arm is ___ lbs per side when fully extended and ___ lbs when in the intermediate position.
1,300 lbs
1,800 lbs
The CORS is limited to ___ lbs on each cable.
1,560 lbs
The MARS is limited to ___.
5,000 lbs
Both the pilot and copilot airspeed indicators may fluctuate ___ KIAS when firing the GAU 18/A in fixed forward fire mode.
± 10 KIAS
Maximum airspeed for one engine inoperative is ___.
130 KIAS
Maximum airspeed for an autorotation at a GW ≤ 16,825 lbs is ___.
150 KIAS
Maximum airspeed for an autorotation at a GW ≥ 16,825 lbs is ___.
130 KIAS
