CV ADEEL JUNAID HAIDER 1). Name Adeel Junaid Haider2). Father’s Name Ghulam Haider

3). Religion Islam

4). Nationality Pakistani

5) Work Permit Eligible Malaysian Work

Permit

6). Date of Birth 18-01-1991

7). Residential Address No. 18-3 Block D Jalan PJS 3/46

Taman Sri Manja 46000 Petaling Jaya Selangor MALAYSIA

8). Mobie No. 0060163757040

9). E-mail chadeelhaider@gmail.com

1O). Academic Qualification

Degree Subject University/Board Year Marks obtained

Percentage Division

Matric Science Rawalpindi 2006 636/1050 60.57 First

11). Professional Qualification

Degree Discipline University/Board Year Marks obtained

Percentage Division

3 years Mech. DAE

Mechanical PBTE, Lahore 2007-09 2536/3350 75.70 First

B. Tech Pass.

Mechanical Preston University, Isb

2010-12 2.7/4.0 CGPA

2.7 CGPA First

B. Tech Hons.

Mechanical Preston University, Isb

2012-14 3.0/4.0 CGPA

3. 0CGPA First

12).Experience: Pakistan Aeronautical complex kamra JF-17 Thunder

Aircraft / F-16 Aircraft Seven years experience as Charge Hand (Aero Technician) JF-17 Thunder Aircraft/F-16

FTS (Flight Test station) I already worked in hydraulic system, fuel system, pneumatic system, ECS system,

Flight control system and Landing Gear system.

FUEL SYSTEM: Fuel cleaning, fuel feeding transfer sequence check and fuel system indication check,

fuel Air tightness checks, pressure refueling gravity refueling and defueling drop tank removal and

installation.

HYDRAULIC SYSTEM: Hydraulic system1&2 tightness check, Hydraulic pumps pressure check and

removal & Installion, EMG Hydraulic pump pressure check, Hydraulic break pressure(Auto break parking

break normal break anti skidding break) adjustment and removal& installation resiviour charging,

accumulator charging

FLIGHT CONTROL SYS:( aileron, trailing edge flaps, horizontal tail and rudder) adjustment and

degree checks and extension & retraction timing check

PNEUMATIC SYS: Main & EMG sys tightness check, canopy tightness, sys charging, accumulator

charging, emergency landing gear lowering, emergency break check canopy sealing check and drag chute

check

LANDING GEAR SYS: landing gear extension& retraction timing check, landing gear leg charging

tyre charging and nose wheel steering degree check and speed break check, wheel removal & installion

ECS SYS: ECS compensator water separator turbo cooler oil charging |& removal & installion, canopy

safety vale check

We done schedule unshedule aircraft maintenance work, AO(Assembly order) , aircraft maintenance work

card, preparation for ground run, preparation for flight card, post flight card.aircraft refuelling/defuelling

hydraulic charging, pneumatic charging, landing gears leg charging, wheel removal/installation, tyre

charging, accumulator charging, hydraulic pumps removal/installation

FTS(Flight test station) process include Aos Flight test work card and special maintenance works card.FTS

related schedule/unshedule maintenance. schedule/unschedule maintenance of FTS related tester/ground

equipment special tools and towing.

I can operat tester such as HTS, Vehical HTS, Habit/GPU(Ground power supply), Hydraulic charging cart

nitrogen charging trolly, fuel cleaning truck, fuel seauence track, fuel pressurization tester, jacks, ground

supports, fuel tanks pressure mearsurement unit and cockpit air tightness tester.