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Fighter Jets above Islamabad

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Albeit, the main function has always being held in capital, but i understand bases in other cities also have their own activities specially those in Karachi, Lahore and Peshawar. I remember once an F-16 took off from Sargodha, performed over Rawalpindi, Peshawar and Lahore before returning to it's base.

sir can you confirm of masroor open house on 6th?
 
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It's a common problem with Russian engines.

OB-RW169_smokey_G_20120216233054.jpg
CAn we replace RD 93 with much superior engine?
 
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Itna kharcha mat kar diyo ki 7th September ko IMF jaana par jaaye maangne waste rupaiiah
Kyonki desh to wahi chala rahe hai naa tumhara IMF waale
AAp kia kiya jata hai.
You better take control of poverty and hunger in your country before pointing us.
BTW i am not against regarding your National day parade celebrations.
 
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AAp kia kiya jata hai.
You better take control of poverty and hunger in your country before pointing us.
BTW i am not against regarding your National day parade celebrations.

ignore kia kro... shyad usko toilet ni milta to PDF pe bharas nikal rha hai apni....
 
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sir ru from airforce? and if it is open to civilians, than what sort of pass?
My brother in law is in the Airforce. He's at masoor.i talked to him few days ago when he was busy with Dunya news in making some flying videos, so he mentioned it briefly. Give me some time I ll ask him.
 
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ignore kia kro... shyad usko toilet ni milta to PDF pe bharas nikal rha hai apni....
:sarcastic:

so jf-17 consumes too much fuel?
How would i know.
:hitwall:

I am not sure but I read the replacement somewhere, PAC is surely going to replace these RD-93 with some good Chinese machinery.
well JF-17 engines will be replaced by Chinese WS-13... which is not ready yet so Russians RD-93 MA upgraded version of RD-93
SO guys what will be the benefits of WS 13?
 
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SO guys what will be the benefits of WS 13?


WS-13 vs RD-93.


Length (m)
WS-13-->4.15
RD-93-->4.25
%Diff-->-2.35%


Diameter (m)
WS-13-->1.02
RD-93-->1.04
%Diff-->-1.92%


Weight (Kg)
WS-13-->1135
RD-93-->1055
%Diff-->7.58



Thrust (Full After-Burning, kN)
WS-13-->86.37
RD-93-->81.3
%Diff-->6.24%



Thrust (Dry, kN)
WS-13-->56.75
RD-93-->50.0
%Diff-->13.50%




Bypass ratio
WS-13-->0.57
RD-93-->0.49
%Diff-->16.33%

in short.. with WS-13 Integrated in J-17 will give well up to 100KN thrust some said it'll be 89.74KN thrust
 
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