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Engine 1 and 2 %RPM (Np)
- 12 Sec Transient 106-121
- Max 105
- Transient 102-105
- Continuous 96-101
- Transient 92-95
- Min (except idle & trans) 91
-
Engine TGT Temp
- 12 Sec Transient 920-965
- 2.5 Min OEI Transient 884-919
- 10 Min Limit 870-883
- Max Start 869
- 30 Min Limit 829-869
- Normal 0-828
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Engine Ng Speed 1 & 2
- Max 105.0
- 12 Sec Limit 102.1-105.0
- 30 Min Limit 99.1-102.0
- Continuous 0-99.0
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Engine TRQ
- DUAL ENGINE
- Max 150
- 10 Sec Limit 121-150
- Continuous 0-120
- SINGLE ENGINE
- Max 150
- 10 Sec Limit 135-150
- Continuous 0-134
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Engine Oil Temp
- Max 150
- 30 Min Limit 136-150
- Continuous -50-135
-
Engine Oil Pressure
- Maximum 120
- Precautionary 101-120
- Continuous >90%Ng 35-100
- <90%Ng 22-100
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XMSN Temp
- Maximum 120
- 30 Min Limit 106-120
- Continuous -50 - 105
-
XMSN Pressure
- Maximum 130
- Precautionary 66-130
- Continuous 31-65
- Idle/Transient 20-30
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Fuel Qty
- Normal 201-1600
- Precautionary 0-200
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Main Rotor Limits
- POWER ON
- Transient 101-107
- Continuous 95-101
- Transient 91-95
- POWER OFF
- Max 110 (120 MTF)
- Transient 105-110
- Normail 90-105
- Rotor Start/Stop 45Kts
- Rotor Brake Max RPM Norm 40%, Max 76%
- Min Px for start 450 psi
-
Prohibited Manoeuvres
- Hovering turns greater than 30 deg/sec
- Aerobatic manoeuvres (rolls,loops etc)
- Flight beyond 90 deg AOB
- Simultaneous movement of PCLs to IDLE or OFF for other than emg
- Practive touchdown autos
- Manoeuvring flight that results in heavy stall
-
Manoeuvres to be avoided
- No intentional out of balance flight above 45KIAS
- Rapid turns using more than 60 deg AOB
- Any manoeuvring resulting in onset of 4:1 vibes
- Any manoeuvre likely to result in droop stop pounding
- Abrupt manoeuvre and large control reversals
- Practice autos except as req for pilot training, MTF and cat events
-
Downwind Hovering
- Prolonged rearward flight and downwind hovering to be avoided to prevent accumulation of exhaust fumes in helicopter and heat
- damage to open cargo doors
-
Stabilator
Manual op of stab in flt is prohibited except as required by formal trg or to overcome an auto mode failure
-
Airspeed Limits
- Max 193
- Sideward/rearward 35
- Max 20250-22000 125 up to 3000ft
- OEI 130 Max
- Auto (16825lbs or less) 150
- Auto (16825-20250) 130
- Auto (above 20250) 125
- One SAS out 170
- Two SAS out 150
- Two SAS out IMC 140
- One HYD SYS out 170
- Two HYD SYS out 150
- Two HYD SYS out IMC 140
- Landing Light 180, extended by 130
- Search Light 180, extended by 100
- Gunners Window Fully open to 170
- Cabin doors open 145
- Open/Close cabin door 80
- Max with ext load 140
AOB limited to 30 deg when a PRI SERVO light illuminated
-
Engine Starter Limits
- 16 deg FAT and below
- 2 Consecutive start cycles followed by 3min rest the 2 additional start cycles followed by 30 min rest
- 17-52 deg FAT
- 2 Consecutive start cycles followed by a 30min rest before additional starts
- 60 sec between each start cycle
- Cycle = starter initiation to starter dropout
- X-Bleed start = 90%Ng, 100% RPMR and Anti-ice light off
-
Pneumatic Source Inlet Limits
- Minimum = 40PSIG @ 30 PPM and 149 deg
- Maximum = 50 PSIG @ 249 deg
(measured @ external air connector on fuselage)
-
Landing Gear Limits
- Up to 16825 lbs
- = 540 fpm ROD on level terrain
- = 360 fpm ROD on slopes
- Above 16825 lbs
- = 300 fpm ROD on level terrain
- = 180 fpm ROD on slopes
Max landing Speed = 60 Kts
-
Slope Landing Limits
- Nose up, right wheel or left wheel up - slope:
- 15 deg (reduce by 4 deg for every 10kts downslope wind)
- Nose down slope:
- 6 deg (tailwind no greater than 15kts)
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Weight Limits
- Max (clean) 22,000
- Ferry (ESSS) 24,500
- Cargo hook 8,000
- Rescue hoist 600
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Backup Hyd Pump (Rotor Sys. Static)
- FAT Operating time (mins) Cool down time (mins)
- -54 to 32 Unlimited n/a
- 33 to 38 24 72
- 39 to 52 16 48
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APU Operating Limits
43 deg and above with eng and rotor operating = 30 mins
With eng and rotor not operating = Continuous up to 51 deg
-
Turb and TS limits
Intentional flt into severe or extreme turb is prohibited
Intentional flt into TS is prohibited
Mod turb. penetration speed is Vlrc - 10kts or Vne - 15kts, whichever is less
-
Rescue hoist duty cycle
- Operated without limit unless HYD OVERHEAT light
- comes on. In that case, hoist ops stop at earliest opportunity.
- May resume when light goes out.
-
Windscreen wiper
Do not operate on dry screen
Do not allow a notable reduction of wiper speed
-
Flight in Icing
With all anti-ice and de-ice equip functioning are permitted flt into known or forecast moderate icing conditions
With only blade de-ice inoperative are permitted flight in known trace icing conditions
With blade de-ice and other anti-ice equip inoperative should not be flown into known or forecast icing conditions
-
ESSS Jettison Envelope
- Level flight : 0 to Vh
- Descent: 0 to 1000 ft/min (up to 60KIAS)
- 0 to 500 ft/min (up to 120KIAS)
- Sideslip: One ball width up to 120KIAS
-
S.O. Approach Limits
- Pitch: 30 deg or less
- Roll: 30 deg or less
- Yaw: Balanced above 45KIAS
- TQ during Flare entry: >0%
- TQ prior to Final Gate: at least 15%
- Into Wind: Cat 4 + 5% (HOGE +10)
- Tail Wind: Cat 4 + 15% (HOGE +20)
- Max Tail wind: 15KTS
-
S.O. Approach
- FLARE POINT
- 0.9 HUD
- >50ft AHO
- Max 100kts G/S
- INTERMEDIATE GATE
- 0.4 HUD (470m vis)
- Max 80kts G/S or
- Max 100KIAS
- FINAL GATE
- TQ - not less than 15% and increasing; and
- PITCH - reducing from 30 deg; and
- ROLL - 10 deg or less; and
- ROC - no greater than fast walking pace
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