eliasafr

Is there any indication in the flight deck for pressurization failure in C-130H or C-130E aircraft?

Can anyone provide me the service bulletin on this?

Can anyone please help me by giving the allowable EBH of c-130j aircraft..........

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?

Its on the rudder booster panel both side ........

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?

We recover the problem by replacing the anti skid valve....it was found faulty during before taxi check

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....?

We solve the prob by replacing the screws by high lock pin.....a.c. Is waiting for fcf

thanks a lot....can u provide me the manual reference...... please

What are the part no of bolts to be installed after removal of A/ A32H-4A cargo handling system of c-130 ac......

Can anybody help me by providing the TO for suction booster pump please?

ok. but will you provide any reference on this.....

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?

no prob sir.........its ok ....and thank you for suggestion......

C-130B........modified with the wing of c-130h and upgrade cockpit instruments

Thanks....we find it..the edp no-1 not produsing sufficient pressure...

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....

thanks a lot. yes just the same happened...I will be very pleased to get further information about this.....

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.....?

After what interval should the turbine cooler oil is to be changed for c-130 ac.....

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 ...

Can anybody help me by giving me the IPC/TO of Pump, Suction Booster Part no 411000-2/ 411000-4 please....

Only one........even some time if the aux pump switch on the gen out light comes on......

thanks for it sir...........it will solve my requirement........