5 & 9 Flashcards
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Nr %
106.5 Maximum
99-100 Continuous
86 Minimum
<40 Rotor Brake
N2 %
107-119 15 sec Transient (max)
90-107 Continuous
70-90 15 sec Transient (min)
0-70 Continuous (for idle)
N1 %
106 Maximum 105-106 10 sec Transient 65-105 Continuous 61 idle speed, autorotation 61 idle speed, powered rotor
TOT Normal operation
905 Maximum
801-905 12 sec transient
716-801 30 minutes
360-716 Continuous
TOT Start
927 maximum
843-927 10 seconds
0-843 Normal
TRQ (psi)
>108 Land as soon as possible 99-108 1 sec 95-99 3 sec 84-95 30 sec 81-84 30 minutes 0-81 Continuous
Engine Oil Temp
107 Maximum
0-107 Continuous
0 Minimum
VIDS will not read below 23
Engine Oil PSI
115-130 above 94 N1
90-130 79-94 N1
50-130 below 79 N1
130-200 idle only 61 N1
Fuel
Main
Aux Goliath
Auc ICE
- 8 gal / 407 lbs main (useable)
- 5 gal / 412 lbs aux Goliath (useable)
200 aux ice (useable)
AMP
175 Maximum
140-175 10 Min cautionary
0-140 Normal
ENG out light
55% N1 or less
Fuel low light
14 +/- 0.5 gallons
Fuel Filter Light
Impending bypass
XMSN Oil press light
On below 15 PSI
XMSN hot light
On above 115 degrees C
Airspeed Limit
125 KIAS (130 KCAS)
Wind limits for starting
40 knots max or a 20-knot gust spread with aircraft into the wind
Starter Limits
30 sec on - 2 Min off
30 sec on - 2 Min off
30 sec on - 30 Min off
Max GWT
4700 Max combat/conting ops
4500 Max GWT
4100 Max safe autorotation
3600 Mac practice touchdown autorotations
Max autorotation airspeed
125 KIAS (130 KCAS)
123 KIAS (dual pitot systems)
Extraction Operations
60 Knots W/ max 40 deg bank
90 Knots W/ max 30 deg bank (Emer only)
In flight restart (airspeed)
Recommended airspeed is 60 KIAS
Structural VNE
125 KIAS (130 KCAS) 123 KIAS ( dual pitot system)
Low fuel airspeed
125 KIAS (130 KCAS) 123 KIAS ( dual pitot systems)
Flight into icing
Intentional flight into known or forecast icing conditions is prohibited.
Flight into turbulence
Intentional flight during known or forecast severe turbulence is prohibited without MACOM approval.
Flight under IMC
This aircraft is restricted to visual flight conditions
Altitude limitations
14,000 feet density altitude
Max wind W/ cyclic trim failure
Maximum wind when hovering downwind with a full forward cyclic trim failure is 15 knots.
Slope Limitations
10 deg up
7 deg down
12 deg roll
Land as soon as possible
Execute a landing to the nearest suitable landing area (e.g., open field, etc..). The primary consideration is to ensure the survival of the occupants.
Land as soon as practicable
Execute a landing to the nearest suitable airfield/heliport. The primary consideration is the urgency of the emergency.
Autorotation
- COLLECTIVE -ADJUST as req’d to maintain rotor rpm
- PEDALS -ADJUST, crab or slip as req’d
- AIRSPEED -ADJUST as req’d
- THROTTLE -OFF
- STORES-JETTISON as req’d
Emergency shutdown
- THROTTLE -OFF
- FUEL VALVE HANDLE - CLOSED (UP) only as req’d
- BATTERY SWITCH - OFF