eliasafr

On 10/24/2007 at 12:31 AM, Guest said:

That was before the \"DADTA\" (Damage and Deterioration Tolerance Assessment) studies and calculations. Several studies have been done, and the numbers seem to get worse each time.

 

The calculation provides a factor to de-rate (multiply) the hours logged on the airplane, based on the mission type, ie, low-level, heavyweight, etc, and the environmental conditions (corrosive atmosphere) where the airplane has been operated/assigned.

 

Some airplanes now can only fly one-fourth their original projected life. For people, early retirement sounds good; but for airplanes, it doesn\'t seem right.

What is the service life you use for your C-130J

On 9/30/2023 at 5:59 PM, superbigbig said:

Thank you for your reply. I also found it on our 1C-130H-2-10 PAGE3-3, but there is still no way to use it. I heard our senior maintenance staff said that it does not use any engine or APU. In this case, use a cabin pressure truck to test the fuselage pressure.

On 9/27/2023 at 8:07 PM, superbigbig said:

 

 Does anyone know the use of this device in C-130H?

I asked a senior before that this is the position where the fuselage is pressurized when the aircraft leaves the original factory. Is this correct?

Its a port for pressurize the ac on ground by ground tester. We still use it in C-130B.

Can anyone please say, why the maximum EH of C-130J is 19000 and EBH of C-130B/H is 45000.

BAF C-130B aircraft ser no 58-0754 took his final destination at BAF Museum, Dhaka after 20 years of memorable  service to BD. "Rest in peace, big bird"

Bangladesh Air Force Lockheed C-130B (L-282-1B) ser no 58-0754 LM NO 3553 registration no S3-AGA going for his last ever flight onward retiring from service. Before that he served 21 years in BAF since 2000. Good bye BIG BIRD.....

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....

9 hours ago, Ramrod said:

You have to refer to the 1C-130A-3 for guidance. If you find nothing there, you must request technical assistance from Lockheed. It is known that those screws strip out and the elevator torque tube collar bolt holes get elongated. The only repair for the torque tube collar issue is replacement. I do not think using oversized bolts were authorized, but I am not 100% sure on this.

 

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.....?