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Aero Precision provides military aviation aftermarket solutions for c-130

Ahmer

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Ahmer last won the day on October 22 2018

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  1. Ahmer

    Brake Selector Relief valve

    The dual brake control valve have a metering valve piston is hollow with series of radial at return port end.An over pressure condition in the brake assembly ,caused by thermal expansion ,is automatically relieved by metering valve piston. Regard
  2. Ahmer

    NTS Failure

    Yes if NTS system fail prop RPM will be more then power section at that time propeller RPM cross the limit 103.5 . it should be pitch locked and aircraft will yaw opposite direction. If Negative torque increases limit -6000 torque RGB Decoupled from power section. Definitely if outer engine is pitch lock and pilot not confirmed the torque should be more when throttle retarted & aircraft will be yawning opposite direction.we experienced of Pitch lock during NTS system failure during decsanding,Fault is with NTS bracket which not properly actuate NTS system.
  3. Ahmer

    NTS Failure

    NTS system works above flight idle, NTS system work when prop try to rotate engine (during descending,gust load,interruption in TD system,and improper governing) when propeller try to rotate engine (negative torque ) produce this system increase the blade angle when blade angle increase prop RPM decease become in governing range RPM. If ur NTS system fail during descending & NTS system not increasing blade angle through feathering valve and propeller RPM increases obve the pich lock RPM limit ( above 103.5) then propeller should be pitch lock. U can observed pich lock propeller by moving the throttle forward engine RPM follow the throttle movement & torque will be same its indication of pitch lock. REGARDS
  4. It is installed on deverter panel at devert valve on both side utility & booster .regards
  5. Ahmer

    NESA WINDOW HINGE INOPERATIVE

    INOPERATIVE WINDSHIELD ANTI−ICING Operation with inoperative windshield anti−icing is permissible provided. 1. The airplane is not flown in known icing. 2. The maximum speed limit below 10,000 feet is 185 KIAS due to possible bird strikes. Descent from high altitude into warm moist air with an inoperative nesa windshield anti−icing system will cause fogging and possible icing of the windshield. To minimize this, increase cabin air temperature and open the pilot’s and copilot’s windshield defogging valves. It is recommended that a gradual descent be made to allow the windshield, which has been cold−soaked at altitude, to warm with ambient cabin air.
  6. Ahmer

    NESA WINDOW HINGE INOPERATIVE

    Plz check service news for NESA windows. Tnx regards
  7. Hello T56 Expertise plz any body describe about T56-a-15 signature check on c130 aircraft. Why we done on t56-a-15 engine and wt is purpose of this check. Tnx
  8. Ahmer

    Throttle Quadrant

    Hello tiny in 1c-130A-3 tech order not having throttle & condition lever quardadart inspection and removal installtion of inner side.
  9. Ahmer

    Throttle Quadrant

    Dear moeed u r absolutely right , this jg only deal wuth for O level maintenance but not mention any regarding removal, installtion and inspection inside quardarnt area.
  10. Ahmer

    Allison 501-D22A Engine

    Can we use Allison 501-D22A commercial engine on military aircraft in place of T56-A-15 engine officially or by permission of civil aviation authority/ FAA.
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