5 Flashcards
Any time an operational limit is exceeded, an appropriate entry shall be made on DA Form __________. Entry shall state what limit or limits were____________, ____________, ________________________, and any additional data that would aid maintenance personnel in the maintenance action that may be required. The helicopter shall not be _____________ until corrective action is taken.
Any time an operational limit is exceeded, an appropriate entry shall be made on DA Form 2408-13-1. Entry shall state what limit or limits were exceeded, range, time beyond limits, and any additional data that would aid maintenance personnel in the maintenance action that may be required. The helicopter shall not be flown until corrective action is taken.
ENGINE INSTRUMENT CREW ALERTING SYSTEM (EICAS) AND PFD POWER POD COLOR CODES.
Red and Yellow striped tapes and red readouts indicate the limit _____________.
Yellow tapes and readouts indicate ______________.
Green tapes and readouts indicate the_______________.
Red and Yellow striped tapes and red readouts indicate the limit above or below which continued operation is likely to cause damage or shorten component life.
Yellow tapes and readouts indicate the range when special attention should be given to the parameter the instrument represents.
Green tapes and readouts indicate the normal operating range of the parameter the instrument represents.
Operating an engine against the gust lock is _____________ .
Operating an engine against the gust lock is prohibited .
Rotor brake shall not be applied with engine(s) operating and rotor turning except during an emergency stop. Maximum rotor speed for emergency rotor brake applications is ________%NR.
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Routine stops will be with engine(s) off, NR below ______% and with ______–______ psi applied to stop the rotor in not less than ______seconds.
Routine stops will be with engine(s) off, NR below 40 % and with 150 - 180 psi applied to stop the rotor in not less than 12 seconds.
Minimum rotor brake pressure for engine start is ________ psi. Maximum rotor brake pressure for engine start is ________ psi.
Use of the rotor brake with engine(s) operating is restricted to __________ and __________ engine starts and operations at ___________ only.
Minimum rotor brake pressure for engine start is 450 psi. Maximum rotor brake pressure for engine start is 690 psi.
Use of the rotor brake with engine(s) operating is restricted to single and dual engine starts and operations at idle only.
Single and dual engine starts and operation at __________ with rotor brake on are not time limited.
Single and dual engine starts and operation at idle with rotor brake on are not time limited.
If oil pressure is not steady during steady state forward flight or in a level hover, or if oil pressure is steady but under ______ psi, make an entry on the appropriate maintenance form. Sudden pressure drop (more than ______ psi) without fluctuation requires an entry on the appropriate maintenance form.
If oil pressure is not steady during steady state forward flight or in a level hover, or if oil pressure is steady but under 45 psi, make an entry on the appropriate maintenance form. Sudden pressure drop (more than 10 psi) without fluctuation requires an entry on the appropriate maintenance form.
TORQUE-Q
10 SECOND TRANSIENT
Dual-Engine
Above 80 KIAS ____________%
80 KIAS or below____________%
Single-Engine ______________%
TORQUE-Q
10 SECOND TRANSIENT
Dual-Engine
Above 80 KIAS 100 - 144 %
80 KIAS or below 120 - 144 %
Single-Engine 135 - 144 %
Torque-Q
CONTINUOUS
Dual-Engine
Above 80 KIAS ___________%
80 KIAS or below__________%
Single-Engine ____________%
Torque-Q
CONTINUOUS
Dual-Engine
Above 80 KIAS 0 - 100 %
80 KIAS or below 0 - 120 %
Single-Engine 0 - 135 %
