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Princess' MH-60R HAC Tutorial (MAY20) COPY > NATOPS Ch4 Limits > Flashcards

NATOPS Ch4 Limits Flashcards

1
Q

Whats required if you exceed a limit?

A

Appropriate entry shall be made on MAF–include what limit(s) were exceeded and include range, duration and any additional info that would aid mx personnel.

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2
Q

What should you do if you exceed a limit that XXX is indicated?

A

NOTE

If a limited is exceeded to the extent that a red “XXX” is indicated, the crew SHALL LAND AS SOON AS PRACTICABLE

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3
Q

What is the Engine limited by?

A

Ng, Np, TGT, Oil Press, Oil Temp

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4
Q

Whats a start cycle and whats required between start attempts?

A

A start cycle defined as starter initiation, acceleration of output drive and starter dropout requires a 60 sec delay between start attempts any time a start is aborted except during emergencies

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5
Q

Engine Start Limitations

A
  1. Crossbleed starts: receiving eng shall be at or above 24% Ng prior to advancing PCL to IDLE.
  2. Engine start with main rotor blades or tail rotor pylong folded is prohibited.
  3. Start TGT limit is 851°C until idle speed attained.
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6
Q

Turbine Gas Temp (TGT)

A

0°-810° - Continuous

810°-851° - 30 Min

851°-878° - 10 Min (as required; for Max Power and limiter checks only)

878°-903° - 2.5 min

903°-949° - 12 sec

949° - Max

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7
Q

Power Turbine Speed (Np)

Engagement Caution

A

<96% - Avoid

96-105% - Continuous (yellow above 101%)

105-117% - 20 sec

117-120% - 12 sec

120% - Max

CAUTION

During engagement, extended operations in the 20-40% and 60-75% ranges may cause engine damage

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8
Q

Main Rotor Speed (Nr)

A

<96% - Avoid

96-101% - Continuous

101-120% - Precautionary

120% - Max

>120% - 123%, Max for FCF only

127% - Overspeed Latch

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9
Q

Dual-Eng Torque (TRQ) below 80 KIAS

A

0-120% - Continuous

120-144% - 10 sec

144% - Max

NOTE

Dual Engine Torque Limits apply when both engines are above 65% torque

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10
Q

Dual-Eng Torque (TRQ) above 80 KIAS

A

0-106% - Continuous

106-127% - 10 Sec

127% - Max

NOTE

Dual Engine Torque Limits apply when both engines are above 65% torque

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11
Q

Single-Eng Torque (TRQ)

A

0-135% - Continuous

135-144% - 10 sec

144% - Max

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12
Q

Gas Generator Speed (Ng) SysConfig 16

A

0-102.2% - Continuous

>102.2-106% - 2.5 min

106-107% - 12 sec

107% - Max

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13
Q

What is the Transmission limted by?

What if it’s in a precautionary range?

A

Nr, torque, oil press and oil temp

If oil press and/or temp are in precautionary range, the helo SHALL NOT be scheduled for additional flights until maintenance action is performed

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14
Q

Transmision Temp (XMSN T)

A

-50°-105°C - Continuous

105°-120°C - Precautionary

120°C - Max

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15
Q

Transmission Press (XMSN P)

A

20psi - Min

20-30psi - Idle and transient

30-65psi - Continuous

(45-60psi in level flight)

65-130psi - Precautionary

130psi - Max

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16
Q

What are the notes regarding oil temperature limits?

A

During any operating condition no maintenance is required if transmission oil temp is the precautionary range for 5 min or less

Prolonged hovering in hot weather, 30°C (86°F) , may cause transmission oil temp to raise into the precautionary range. Operation in the precautionary range for less than 30 min during any one flight under this condition is acceptable and no maintenance is required

17
Q

What are the notes regarding oil Pressure limits?

A

Following conditions do not constitute an emergency situation, but may be indicative of a degraded lubrication system. Any discrepancy SHALL be documented on a MAF.

  1. Steady press outside 45-60psi, but within normal limits of 30-65psi
  2. Fluctuations not to exceed a range of 10psi, within the normal limits 30-65psi

During transient pitch or steady-state nose-high pitch attitudes (autos, downwind hovering, rearward flight, slope-up landings, etc) xmsn oil press fluctuations (including momentary fluctuations below 30psi and transient drops below 20psi for up to one sec) are acceptable. Operating with press fluctuations below 30psi shall be limited to 30 min

18
Q

Engine Oil Temp (ENG OIL T)

A

-50°-135°C - Continuous

135°-150°C - 30 min

150°C - Max

19
Q

Engine Oil Press (ENG OIL P)

A

22psi - Min

22-26psi - Precautionary

26-100psi - Continuous

100-120psi - Precautionary

120psi - Max

NOTE

Normal idle range is 22-55psi

20
Q

What are the Starter limits for engine start?

What if you are motoring?

A

Start Cycles

<16°C

Cycle 1 - 60 sec

Cycle 2 - 60 sec

Cycle 3 - 60 sec

Cycle 4 - 30 min

16°-52°C

Cycle 1 - 60 sec

Cycle 2 - 30 min

Engine Motor (Ignition - OFF)

2 min - 5 min

2 min - 30 min

NOTE

Times for motoring are cumulative within a 5-min period.

21
Q

Min Fuel

A

On deck with no less than 600lbs

22
Q

When is the APU allowed in flight?

A

APU is not intended for routine in-flight use. Operation of the APU shall be limited to essential operations only.

Acceptable in-flight use include emergency procedures, single-eng training, practice autos, and powering the ECS during extreme temps.

23
Q

APU Operating Limitations

A

>43°C with eng and rotors operating - 30 min

<51°C with eng and rotors not operating - Continuous

24
Q

Rotor Engagement/Disengagement

A

45 knots from any direction

25
Q
  1. Max (Vne)
  2. Sideward/Rearward Flight
  3. Auto
  4. Boost Off
  5. 2 SAS Inop in IMC
  6. Either PRI SERVO PRESS caution
  7. Searchlight in fixed position other than stowed
  8. Searchlight in transition
  9. Dome at or above trail
  10. Dome below trail
  11. Cabin door opening/closing
A
  1. Max: 180 KIAS
  2. Side/Rear: 35 KIAS
  3. Auto: 100 KIAS
  4. Boost Off: 140 KIAS
  5. 2 SAS Inop IMC: 125 KIAS
  6. PRI SERVO PRESS: 125 KIAS
  7. Searchlight Fixed: 160 KIAS
  8. Searchlight Transition: 100 KIAS
  9. At or Above: 70 KIAS, 45° AOB
  10. Below: 70 KIAS, 15° AOB
  11. Cabin Door Moving: 60 KIAS

NOTE

With FLIR installed, failure to maintain balanced flight below 90 KIAS in descents over 1000fpm will result in inaccurate and erratic airspeed indications.

26
Q

Rates of descent with a Rescue Hoist Load

A

Rate of descent limited to 1000fpm

27
Q

Hovering Limitations

A
  1. Prolonged rearward flight and downwind hovering should be avoided to prevent accumulation of exhaust fumes in the helo and heat damage to the window of an open cabin door.
  2. Hovering turns at a rate in excess of 30° per second.
  3. Dipping operations at altitudes other than 70ft.
  4. Do not tow the transducer in the water above 8KGS with array folded and 4KGS with array unfolded

NOTE

Towing is defined as the cable contacting the funnel. Aircraft ground speed may be greater than 8KGS (folded) or 4KGS (unfolded) if cable is not in contact with the funnel.

28
Q

Angle of Bank Limitations

A
  1. Normal ops: 45°
  2. Operations above 10,000ft DA: 30°
  3. Either PRI SERVO PRESS caution: 30°
  4. Boost off flight: 30°
29
Q

Max Operating Altitude

A

Max operating DA is 13,000ft

30
Q

Prohibited Maneuvers

A
  1. Aerobatic flight
  2. Practice full-autos landings
  3. Intentional approaches into or inducement of retreating blade stall.
31
Q

Rotor Brake Limitations

A

Max rotor speed for application - 76%Nr

Routine stops SHALL be made between - 30-50%

SHOULD be limited to 180psi

32
Q

Blade, Pylon, Stab Fold/Spread wind speed limits

What if you do a full cycle?

A

Max wind velocity 45 knots

Following a complete blade fold and spread cycle, allow 10-min cooling period

33
Q

Landing Limitations

  1. Level terrain
  2. Sloped terrain
  3. Touchdown Speed
  4. Taxi Speed
  5. Slope
  6. Downwind
A
  1. <19,500lbs - 720fpm; >19,500lbs - 480fpm
  2. 360fpm
  3. 75KGS (lock) 20KGS (unlock)
  4. 40KGS (shimmy damper), 20KGS (without)
  5. 6° nose-down; 9° nose-up; 12° cross-slope
  6. SHOULD be avoided
34
Q
  1. Gross Weight
  2. Aviaton Ships
  3. Air Capable/Amphibious Assault Aviation Ships
A
  1. 23,500lbs
  2. 23,500lbs
  3. 22,500lbs
35
Q

Internal Load Limitations

A

300lbs per square ft

36
Q

External Load Limitations

A
  1. 6000lbs on the cargo hook
  2. 600lbs on the rescue hoist. Limited by the RH Brake
37
Q

Egress Lighting

A

Except in emergencies, ADHEELS and IHEELS SHALL be operational for all overwater flights requiring pax/non-aircrew in cabin

38
Q

Temperature Limitations

A

Below -40°C (-40°F) or above 60°C (140°F) are PROHIBITED.

39
Q

Backup Hydraulic Pump Limitations

A

33-38°C : 24 min - 72 min

39-60°C : 16 min - 48 min

Princess' MH-60R HAC Tutorial (MAY20) COPY (26 decks)

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