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eliasafr

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Everything posted by eliasafr

  1. eliasafr
    Is there any indication in the flight deck for pressurization failure in C-130H or C-130E aircraft?
  2. eliasafr
    Can anyone provide me the service bulletin on this?
  3. eliasafr
    Can anyone please help me by giving the allowable EBH of c-130j aircraft..........
  4. eliasafr
    During performance check of AE2100D3 turboprop engine, why the MGT may be less then zero? How it is being calculated? Can anybody give me some idea about MGT margin?
  5. eliasafr
    Its on the rudder booster panel both side ........
  6. eliasafr
    In C-130B aircraft tail no 58-0754 Lockheed no 3553 right rear mlg vertical beam got cracked. According to ipc 130B-4 the part no is 373014-1 L/R we tried to replace it by 373014-3 L/R as previous part no not available.but it is found not matched with the existing one.Now can we replace it with 388482-32?
  7. eliasafr
    We recover the problem by replacing the anti skid valve....it was found faulty during before taxi check
  8. eliasafr
    Lt rear tyre of c-130b a.c. Ser no 61-2640 brust during landing. It seems it skid through runway....but on ground check brake seems ok....and it was found free. What might be the cause....?
  9. eliasafr
    We solve the prob by replacing the screws by high lock pin.....a.c. Is waiting for fcf
  10. eliasafr
    thanks a lot....can u provide me the manual reference...... please
  11. eliasafr
    What are the part no of bolts to be installed after removal of A/ A32H-4A cargo handling system of c-130 ac......
  12. eliasafr
    Can anybody help me by providing the TO for suction booster pump please?
  13. eliasafr
    ok. but will you provide any reference on this.....
  14. eliasafr
    How will I calculate the TBO life of mlg motor, antiskid control valve? according to SMP515C-122 it is 6300 hrs.....is it the airframe hrs?
  15. eliasafr
    no prob sir.........its ok ....and thank you for suggestion......
  16. eliasafr
    C-130B........modified with the wing of c-130h and upgrade cockpit instruments
  17. eliasafr
    Thanks....we find it..the edp no-1 not produsing sufficient pressure...
  18. eliasafr
    While #1,and#2 eng running utility sys press, Brake press, and rudder booster pressure is 2800 psi but when the control stick moves extreme forward perss drops to 2000 psi and remain same but when control stick puts back it is normal.....when elevator booster shutoff switch puts off the press indicated normal....no hydraulic leakage found from the system. we alrady cleaned and replace the hyd filters. please give me some suggestions on this regurd....
  19. eliasafr
    thanks a lot. yes just the same happened...I will be very pleased to get further information about this.....
  20. eliasafr
    the screw of elevator tube found loose, it can't be tighten.....now is there any restriction of flying the aircraft in this condition, and how the problem can be solve.....?
  21. eliasafr
    After what interval should the turbine cooler oil is to be changed for c-130 ac.....
  22. eliasafr
    But can i got the ipc of that bcz i need to replace some gasket/ o ring to recover the leaking problem but we dont have the part no ...
  23. eliasafr
    Can anybody help me by giving me the IPC/TO of Pump, Suction Booster Part no 411000-2/ 411000-4 please....
  24. eliasafr

    atm gen

    eliasafr replied to eliasafr's topic in C-130 Technical

    Only one........even some time if the aux pump switch on the gen out light comes on......
  25. eliasafr
    thanks for it sir...........it will solve my requirement........
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