1H-60(H)G-1 Section 5

Question 1

On any VID strip ___ consecutive lights must not be out and NO lights may be out at a transition point.

Answer 1

Two

Question 2

The maximum allowable Nr for normal flight operations and emergency procedure training is ___%.

The maximum allowable Nr for Functional Check Flights is ___%.

Answer 2

110%

120%

Question 3

Maximum wind velocity for rotor start or stop is ___ knots from any direction.

Answer 3

45

Question 4

Maximum Nr for rotor brake application is ___%

Routine rotor stops shall be done between ___ - ___%.

Answer 4

• 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.

Question 5

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 ____.

Answer 5

50 to 55 psi

781A

Question 6

Engine ____ check in flight is prohibited.

Answer 6

Overspeed

Question 7

The rappelling attaching points have a load limit of ___lbs each. Maximum of __ gunners belts may be attached to a single repelling ring.

Answer 7

4,000 lbs.

2 gunners belts

Question 8

The maximum weight that may be suspended from the cargo hook is ___lbs.

Answer 8

8,000 Lbs.

Question 9

The maximum weight that can be suspended from the rescue hoist is ___ lbs.

Answer 9

600 Lbs.

Question 10

Engine starter limits when OAT is ≤ 16°C

Answer 10

1st attempt - 1 minute rest
2nd attempt - 3 minute rest
3rd attempt - 1 minute rest
4th attempt - 30 minute rest

Question 11

Engine starter limits when OAT is 16-52°C

Answer 11

1st attempt - 1 minute rest
2nd attempt - 30 minute rest

Question 12

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

Answer 12

Min - 40 psi / 30ppm / +149deg C

Max - 50psi / +249deg C

Question 13

Cross bleed starts will not be attempted unless the source engine’s Ng is above ___%, Nr is ___%, and what advisory light light is OFF?

Answer 13

Ng source engine 90%

Nr 100%

ENG ANTI-ICE ON advisory light - off

Question 14

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.

Answer 14

1,300 lbs

1,800 lbs

Question 15

The CORS is limited to ___ lbs on each cable.

Answer 15

1,560 lbs

Question 16

The MARS is limited to ___.

Answer 16

5,000 lbs

Question 17

Both the pilot and copilot airspeed indicators may fluctuate ___ KIAS when firing the GAU 18/A in fixed forward fire mode.

Answer 17

± 10 KIAS

Question 18

Maximum airspeed for one engine inoperative is ___.

Answer 18

130 KIAS

Question 19

Maximum airspeed for an autorotation at a GW ≤ 16,825 lbs is ___.

Answer 19

150 KIAS

Question 20

Maximum airspeed for an autorotation at a GW ≥ 16,825 lbs is ___.

Answer 20

130 KIAS

Question 21

Sideward/Rearward Flight Limits

Answer 21

Hovering in winds greater than 45 knots from the sides or rear is prohibited.

Sideward/rearward flight into the wind, when combined with windspeed, shall not exceed 45 knots.

Question 22

Hydraulic/SAS System Airspeed Limits

Answer 22

1 Hyd/SAS - 170 KIAS

2 Hyd/SAS - 150 KIAS

2 Hyd/SAS in IMC - 140 KIAS

Question 23

Landing/Search Light Airspeed Limits

Answer 23

Maximum to extend the landing light is 130 KIAS, while extended 180 KIAS.

Maximum to extend the search light is 100 KIAS, while extended 180 KIAS.

Question 24

Flight with cabin doors open is authorized up to ___ with sound proofing installed aft of station 379. Without sound proofing installed aft of station 379, flight is authorized up to ___.

Answer 24

100 KIAS

145 KIAS

Question 25

Movement of cabin doors will be accomplished at the lowest possible airspeed, not to exceed ___.

Answer 25

130 KIAS

Question 26

Maximum airspeed to open/close the gunner's window is ___. They must be secured closed for flight above that airspeed.

Answer 26

170 KIAS

Question 27

Routine flight with cockpit doors removed is ___.

Answer 27

Prohibited.

Question 28

Prohibited Maneuvers

Answer 28

1. Hovering turns greater than 30° per second. 2. Simultaneous moving of both throttles to IDLE or OFF (throttle chop) in flight. 3. Practice touchdown autorotations. 4. Aerobatic maneuvers and flight beyond 90° angle of bank. 5. Aerodynamic breaking with collective full down is prohibited once the landing gear touches down.

Question 29

Bank angles shall be limited to ___ when a PRI SERVO PRESS caution light is illuminated.

Answer 29

30°

Question 30

To prevent excess tail rotor system landing, avoid abrupt, full pedal input above ___.

Answer 30

80 KIAS

Question 31

Maximum Touchdown Sink Rates

Answer 31

≥ 16,825 lbs - 540 fpm over level terrain and 360 fpm over slopes ≤ 16,825 lbs - 300 fpm over level terrain and 18- fpm over slopes

Question 32

Slope Landing Limits All slope limits shall be reduced by ___ for every ___ knots of wind. At a slope angle of ___, an indicated oil pressure of ___ is normal, and at an angle of ___ slope, a pressure in the range of ___ is normal due to pitching of the helicopter.

Answer 32

15° nose, right/left wheel upslope (10° for ski equipped aircraft). 6° nose downslope. 2°, 5 knots 10°/30-35 psi, 15°/10-15 psi

Question 33

Backup Hydraulic Pump Limits

Answer 33

< 33°C - unlimited operation/no cooldown 33°-38°C - 24 minutes/72 minutes > 38°C - 16 minutes/48 minutes

Question 34

APU Operational Limits

Answer 34

Engine & Rotors operating: 30 minutes up to 43°C Engine & Rotors not operating: unlimited up to 51°C

Question 35

IR Searchlight Limits

Answer 35

With IR filter installed, do not operate the searchlight with lamp rated greater than 250 watts. Do not operate controllable searchlight with IR filter installed for more than 5 minutes on the ground without the rotor blades turning.

Question 36

Blade De-Ice/Windshield Anti-Ice

Answer 36

Shall not be operated above 21°C

Question 37

Turbulence and Thunderstorm Limits

Answer 37

1. Intentional flight into known severe turbulence is prohibited. 2. Intentional flight into thunderstorms is prohibited. 3. Intentional flight into turbulence with a sling load attached and an inoperative collective pitch friction grip is prohibited.

Question 38

Icing Limits

Answer 38

1. Helicopters not equipped with operating windshield anti-ice, pitot heat, engine anti-ice, and engine inlet anti-ice are prohibited from flying into icing conditions (≤ 4°C with visible moisture) 2. Helicopters not equipped with blade de-ice are permitted to fly in trace conditions. Flight in light conditions is not recommend and flight into moderate conditions is prohibited. 3. Helicopters equipped with operational blade de-ice are permitted flight into moderate conditions.

Question 39

Hoist OAT Limit

Answer 39

-40° to +60°C

Question 40

Main Rotor Overspeed Latch Lights

Answer 40

★ 127% Nr ★★ 137% Nr ★★★ 142%. Nr

Question 41

Nf Bands

Answer 41

12 Second Transient: 105-107 Maximum: 105 Transient: 101-105 Continuous: 95-101 Transient: 91-95 Minimum: 91 Avoid Range: 20-40/60-90

Question 42

Nr Bands (Power On)

Answer 42

Transient: 101-107 Continuous: 95-101 Transient: 91-95 Minimum: 91 Transient Only: 0-91

Question 43

Nr Bands (Power Off)

Answer 43

Normal: 90-105 Transient: 105-110 Maximum: 110 (120 for FCF)

Question 44

Engine % TRQ

Answer 44

12 Second Transient ≥ 80 KIAS: 100-144% ≤ 80 KIAS: 120-144% Single Engine: 135-144% Continuous Single Engine: 0-135% ≥ 80 KIAS: 0-100% ≤ 80 KIAS: 0-120%

Question 45

Velocity Not to Exceed (VNE)

Answer 45

193 KIAS

Question 46

TGT Bands

Answer 46

12 Second Transient: 903°-949°C 2.5 Minute: 878°-903°C (881°-901°C) Start Abort: 851°C 10 Minute: 851°- 878°C (857°-875°C) 30 Minute: 810°-851°C Normal: 0°-810°C

Question 47

Ng Bands

Answer 47

12 Second Transient: 102-105% Maximum: 102% 30 Minute Limit: 99-102% Continuous: 0-99%

Question 48

Engine Oil Temperature Bands

Answer 48

Maximum: 150°C 30 Minute Limit: 135°-150°C Continuous: -50° to 135°C

Question 49

Engine Oil Pressure Bands

Answer 49

Maximum: 120 psi 5 Minute Limit: 100-120 psi Normal: 26-100 psi Idle: 22-26 psi Minimum: 22 psi

Question 50

Main Transmission Oil Temperature Bands

Answer 50

Maximum: 140°C Precautionary: 105°-140°C Continuous: -50° to 105°C

Question 51

Main Transmission Oil Pressure Bands

Answer 51

Maximum: 130 psi Precautionary: 65-130 psi Continuous: 30-65 psi Idle and Transient: 20-30 psi Minimum: 20 psi