Use LEFT and RIGHT arrow keys to navigate between flashcards;
Use UP and DOWN arrow keys to flip the card;
H to show hint;
A reads text to speech;
43 Cards in this Set
- Front
- Back
TGT |
|
|
Np |
|
|
Nr |
|
|
Dual Engine Torque < 80 KIAS |
|
|
Dual Engine Torque > 80 KIAS |
|
|
Single Engine Torque |
|
|
Ng |
|
|
Transmission Temp |
|
|
Transmission Pressure |
|
|
Engine Oil Temp |
|
|
Eng Oil Pressure |
|
|
Starter Limits |
|
|
Minimum Planned Fuel on Landing |
Minimum planned fuel on landing shall be no less than 600 pounds |
|
APU Limits |
|
|
Transmission Limits |
|
|
Rotor Engagement and Disengagement |
Maximum wind velocity for rotor engagement or disengagement is 45 knots from any direction. |
|
Max Speed |
180 KIAS |
|
Max Sideward/Rearward Speed |
35 KNOTS |
|
Max Auto Speed |
100 KIAS |
|
Max Boost Off Airspeed |
140 KIAS |
|
Two SAS inoperative in IMC speed |
125 KIAS |
|
Either PRI SERVO PRESS caution speed |
125KIAS |
|
Searchlight in fixed position other than stowed airspeed |
160KIAS |
|
Searchlight in transition airspeed |
100KIAS |
|
Dome at trail limits (cable 10ft, dome approx 6ft below aircraft) |
70KIAS, 45 AOB |
|
Dome below trail limits |
70 KIAS, 15 AOB |
|
Cabin door opening/closing airspeed |
60KIAS
|
|
Hovering Limitations |
|
|
Angle of Bank Limits |
|
|
Altitude Limits |
Maximum operating DA is 13,000 ft |
|
Prohibited Maneuvers |
|
|
Rotor Brake Operating Limits |
|
|
Blade, Pylon, and Stabilator Fold and Spread Limits |
|
|
Landing Limits |
|
|
Windows |
Windows shall not be installed or removed in flight, except during actual aircraft emergencies |
|
Aircraft Operating Gross Weight Limits |
Max - 23,500 lbs Aviation Ships - 23,500 lbs Air Capable / Amphibious Assault - 22,500 lbs |
|
Internal Load Weight Limits |
300 pounds per square foot |
|
External Load Weight Limits |
Cargo Hook - 6,000 lbs Rescue Hoist - 600 lbs |
|
Minimum Aircraft Equipment for Night Flight Over Water |
1. LAWS 2. Altitude Hold (RADALT or BARALT) |
|
Emergency Egress Lighting |
Except in emergency situations, helicopter emergency egress lighting (ADHEELS or IHEELS) shall be operational for all overwater flights requiring passengers/non-aircrew in the cabin. |
|
Temperature Limits |
-40 C (-40 F) - 60 C (140 F) |
|
APU Operating Limits |
To prevent overheating, APU operation at ambient temperature of 43C and above with engine and rotor operating is 30 minutes. With engine and rotor not operating, the APU may be operated continuously up to an ambient temperature of 51C. |
|
Backup Hydraulic Pump Limits |
|