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Super Tucano was in Pakistan sometime before, I don't remember hearing anything about it

Came for demo. Happens all the time
 
J20 with DSI. 7th prototype
 

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By looking at the pictures and it looks like a big number is in China c-130 il-78 f-7 mirages and thunder and may be KE(AWACS) that is alot
 
Air-Launched Weapons

Chief designer reveals data on China's new Luoyang PL-10 AAM

Richard D Fisher Jr, London - IHS Jane's Defence Weekly

17 September 2015


The Luoyang Electro-Optical Research Institute (LEOC) has largely competed development of its fifth-generation PL-10 short-range air-to-air missile (AAM), according to comments by the missile's designer on a Chinese TV show broadcast in late August.

The PL-10 AAM was first seen on Chinese websites in 2013 being carried on a retractable/covered pylon on the Chengdu Aircraft Corporation (CAC) J-20 fifth-generation fighter. More recently it has been seen on the wingtip pylon of the Shenyang Aircraft Corporation J-11 fighter.

The TV report featured an interview with the PL-10's chief designer, Liang Xiaogeng. According to Mark Stokes of the Project 2049 research institute, Liang also served as the deputy chief designer of LEOC's PL-9C infrared/helmet-sighted AAM and as chief designer of the PL-12 self-guided medium-range AAM.

The report was unusual in that it provided significant historic and performance data about a new weapon before its unveiling at a major arms show or exhibition. For example, the report noted that the PL-10 weighs 89 kg, has a length of 3 m, and a range of 20 km. It has been in development for seven years, a prototype was completed in 2013, and since then has been test-fired 30 times.

The report also noted that the PL-10 has "world class" capabilities that include a "multi-element imaging infrared seeker with anti-jamming capabilities" and indicated that it is capable of high off-boresight attacks and has super manoeuvrability.

Images from 2013 and more recently confirm that the PL-10 uses thrust vectoring vanes in its motor exhaust. These, plus unique large aft fins with a slight forward sweep, likely confer super manoeuvrability.

Like comparable AAMs, the PL-10 probably also uses a new helmet-mounted display (HMD) sighting system.

Is this China's version of the AIM 9x
 
Hi Gentlemens:)

How can Pakistan Air Force trust Russian aircraft engines? A lot of people says : Russian RD33 engine had 500 hours lifetime. After you have to change???
Why you dont buy another F-16s? Usa dont sell?
Fighter Jet Engine Life — Military Forum | Airliners.net
Sovietjet ,

The Initial RD 33 without turbine modifications had a ridiculously low engine life of 350-400 hours before overhaul. In most of the engines which came with the initial batch of fulcrums for the Indian air force , the engine TBO was kept at 200 hrs to reduce a whole bunch of accidents.Most of the contry's operating the MiG 29 (Atleast India and Germany) made modifications to the turbine section to increase this. Currently the overhaul times for the engine is about 650-700 hours , rarely reaches 700 hours though. The problem with the RD 33 was that while it gave enormous power it always used to overheat. That caused turbine failures. The engines manufactured by HAL under license all have the improved turbine section incorporated in them.
 
Hi Gentlemens:)

How can Pakistan Air Force trust Russian aircraft engines? A lot of people says : Russian RD33 engine had 500 hours lifetime. After you have to change???
Why you dont buy another F-16s? Usa dont sell?
Fighter Jet Engine Life — Military Forum | Airliners.net
Sovietjet ,

The Initial RD 33 without turbine modifications had a ridiculously low engine life of 350-400 hours before overhaul. In most of the engines which came with the initial batch of fulcrums for the Indian air force , the engine TBO was kept at 200 hrs to reduce a whole bunch of accidents.Most of the contry's operating the MiG 29 (Atleast India and Germany) made modifications to the turbine section to increase this. Currently the overhaul times for the engine is about 650-700 hours , rarely reaches 700 hours though. The problem with the RD 33 was that while it gave enormous power it always used to overheat. That caused turbine failures. The engines manufactured by HAL under license all have the improved turbine section incorporated in them.
AL 31 used on SU 35 claims a life of 4000 hours.
 
AL 31 used on SU 35 claims a life of 4000 hours.
Interesting. Another peoples says :al31 maximum 900 hours but russian enginers working for the 1500hours.
Who is right?:) How and where can i get a information in the internet?
 
The version of AL-31 on the Su-35S (the production version of Su-35BM) is also referred to as the Saturn 117S or AL-41F1S
 

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