UH-60M LIMITS EXAM QUESTIONS
WITH ALL CORRECT ANSWERS
SAS inoperative airspeed limits: - Answer-1 SAS inoperative - 170 KIAS.
2 SAS inoperative - 150 KIAS.
2 SAS inoperative in IMC - 140 KIAS.
Hydraulic system inoperative limits: - Answer-1 Hydraulic system inoperative - 170
KIAS.
2 Hydraulic systems inoperative - 150 KIAS.
2 Hydraulic systems inoperative in IMC - 140 KIAS.
Landing light. If use is required, the landing light must be extended prior to reaching a
maximum forward airspeed of ___ KIAS. With landing light extended, airspeed is limited
to ___ KIAS. - Answer-130 KIAS
Searchlight. If use is required, the searchlight must be extended prior to reaching a
maximum forward airspeed of ___ KIAS. With searchlight extended, airspeed is limited
to ___ KIAS . - Answer-100 KIAS (Extending)
180 KIAS (Extended)
Cabin door(s) may be fully open up to ___ KIAS. - Answer-145 KIAS
The door(s) will not be intentionally moved from the fully open or closed position in
flight. The cabin door(s) may be opened or closed during _____ flight. - Answer-
Hovering
Gunner window(s) may be fully open up to ___ KIAS. - Answer-170 KIAS
Stabilator Failure Note: Vne becomes variable to indicate the airspeed limit applicable
for the current stabilator position, except in no case shall the autorotation limit exceed
___ KIAS. - Answer-120 KIAS
The stabilator shall be set _____ at speeds below __ KIAS. - Answer-full down below 40
KIAS
The stabilator shall be set at __ at speeds above __ KIAS. - Answer-0° above 40 KIAS
PROHIBITED MANEUVERS. - Answer-a. Hovering turns greater than 30°per second
are prohibited. Intentional maneuvers beyond attitudes of +/-30°pitch or over 60°roll are
prohibited.
, b. Simultaneous moving of both ENG POWER CONT levers to IDLE or OFF (throttle
chop) in flight is prohibited.
c. Rearward ground taxi is prohibited.
Prolonged ______ and _____ are to be avoided to prevent accumulation of _____ in the
helicopter and heat damage to ______ - Answer-Rearward flight and Downwind
hovering
Exhaust Fumes
Windows on open cargo doors
Maneuvers entered from a low power setting may result in transient droop of ___ NR or
greater. - Answer-5% NR
Above ___ KIAS avoid abrupt, _____ to prevent excess tail rotor system loading. -
Answer-80 KIAS
full pedal inputs
Bank angles shall be limited to ___ when a PRI SERVO FAIL caution appears. -
Answer-30 degrees
Do not exceed a touchdown sink rate of ___ feet-per- minute on level terrain and ___
feet-per-minute on slopes with gross weights of up to 16,825 pounds; above 16,825
pounds gross weight do not exceed ___ feet-per-minute on level terrain and ___ feet-
per-minute on slopes. - Answer-540 , 360
300 , 180
Maximum forward touchdown speed is limited to ___ knots ground speed on level
terrain. - Answer-60 KGS
___ noseup, right wheel up or left wheel upslope. The slope limitations shall be further
reduced by __ for every __knots of wind. - Answer-15 degree
2 degrees
5 knots
___ nose downslope. Landing in downslope conditions with tail winds greater than ___
knots shall not be conducted. A low-frequency oscillation may occur when landing nose-
down on a slope with the cyclic near the aft stop. - Answer-6 degree
15 knots
At slope angle of 10° an indicated oil pressure of ___ to ___ psi is normal; and at 15°
slope angle, a pressure in the range of ___ to ___ is normal due to pitching of the
helicopter. - Answer-30, 35
10, 15
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