This presentation covers the overall structure of an organization along with an overview of all the factories at Pakistan Aeronautical Complex, Kamra.

1. Internship at PAKISTAN
AERONAUTICAL COMPLEX
Author: -
Muhammad Usman
0335-4770766
muhammadusmankambo@gmail.com
Mechanical Engineer
UET, Lahore

2. Learning objectives
 What is an organization and how it works?
 Overall structure of the organization.
 Fields of work being done over there.
 Details of work.

3. Organization
 PAC (Pakistan Aeronautical Complex) is situated in KAMRA, Attock.
 One of the most developed and advanced working Industry of Pakistan
 Manufacturing, maintenance and rebuilding of Aircrafts is being done over here.

4. Structure
 The overall structure can be depicted through this diagram: -
PACKAMRA
ARF
APF
AMF
MRF
BASEComesunder Ministryof defence
PAF

5. ARF (AIRCRAFT REBILD FACTORY)
 The working sequence is as given below:-
Acceptance Disassemble Depainting
Structurerepair
Assembly
Final Assembly
Flight TestPaint
Ferryout

7. APF (Avionic Production Factory)
 Electronics used in the aircrafts
Three main features are: -
1. GPL (Generic Production Line)
2. GTL (Generic Testing Line)
3. ESS (Environment Stress Screening)

9. AMF (Aircraft Manufacturing Factory)
 AMF Light MISHAK
 AMF Heavy JF-Thunder
 Control system includes
Up-down, right left & rolling / inversion
 Final Assembly and FTS includes: -
 Fuel, pneumatic and hydraulic system
 A.C system
 Electric Power “ON” check
 Flight control test + Landing gear
 Avionic Test
 Flight Test (by electric signal)

11. MRF (Mirage Rebuilt Factory)
 Originated in France in 1953. Pakistan made an agreement in 1962.
 Mirage Single Seater Jet Fighter
 Mirage Double Seater Training Purposes
 Pakistan made a renovation in Mirage by up introducing Radar systems & Steering
systems etc. and named them as Mirage PA 3 & Mirage PA 5.
 Specifications: -
Length = 51.05 ft.
Span = 26.97 ft.
Height = 14.76 ft.
Weight = 14990 lb (without fuel)
Take off Weight = 21150-29707 lb

13.  It is composed of 38 frames connected together by Ribs & Spars and material of
which body is made of is A24G Aluminium.
 System in Mirage includes: -
Hydraulic System, A.C System, Fuel System, Hydromechanics + Hydroelectric System,
Control System, Gear System & Cooling System.
 Operating Detail: -
Operate on Brayton Cycle.
Compressor Combustion Chamber Turbine
 Fuel: - JP 4
 Inspection: -
1. Pre-flight Inspection
2. Through Flight Inspection
3. Post Flight Inspection

14. Overall Structure of MRF
MRF
Aircraft Wing EngineWing
QualityShop
Production&
PlanningShop
Repait &
Fabrication
Shop
AccessoryShop
EngineShop

15. Repair & Fabrication Wing
R&FWing
SurfaceTreatment
Shop Metal Shop MachineShop WeldingShop Plasma Shop Heat Treatment
Shop
Plating
Anti-corrosive
ProtectingCoating
Painting
CompressiveStress
Marking
Cutiing
Grinding
Flusing
Patchrepair
Drilling
Reaming
Riveting
Reshaping
Fitting
DI
Blending
Turning
Grinding
Tigboring
Milling
Fitting&Drilling
E-Beam
R-Welsing
TigWelding
Oxyacetylene
Induction
ElectricArc
Vacuum

16. Flow Chart of ERP
Cleaning
NDT/ Insp
Pre-Machining Metal work
Q
Plating Plasma Welding
Q
Post. Machinhg
Cleaning
NDT/ Insp
Post / Insp
PASS
PASS
FAIL
FAIL

17. Flow Chart of Crack/ Scratch Repair
Cleaning
NDT/ Insp
Heat Treatment
Cleaning Q Metal Work
Welding
Machining Q Metal Work
NDT
Q
HT
Cleaning
NDT
Final Insp
Fail
Fail
Pass
Pass
Pass

18. NDT and Cleaning Facility
NDT Facility Cleaning Facility
Visual/ Optical Testing Chemical Mechanical
Penetrant Testing Chemical removal Dry blasting
Magnetic Testing Oxidation removal Wet blasting
Eddy Current Testing Paint striping Stream blasting
Radiographic Testing Vapour degreasing Ultrasonic blasting
Ultrasonic Testing

19. Quality Assurance
 AS (Aerospace Standard)certified
 PDCA cycle i.e. Planning, Do, Check, Act
 4 main Terminologies are Shall, Should, May, Can
Quality Management Principles
 Customer Focus
 Leadership
 Engagement of people
 Process approach
 Improvement
 Evidence
 Relationship Management.
ISO-9000 (International Organization for Standardization)

20. Quality Management Principles
Clauses: -
1. Context of Organization
2. Leadership
3. Quality Shop
4. Planning
5. Support
6. Environment
7. Monitoring Measurement
Deign and Development
Design _____ Prototype ______ CMM Production

21. Quality Engine Shop
Testing
Destructivetesting Non-dest. Testing
Penetrant Testing
Magnetic par. insp.
Radiographic
Ultrasonic
Eddy current
Fluorescent Penetrant
DyePenetrant
Dual
Steps:-
Part Cleaning
Penetrant application
Penetrant Removal
Drying
Developer isapplied
Inspection
Post Cleaning
Steps:-
Cleaning
Cureent applied
Inspection
De-magnetization
Preservation

22. Quality Policy
“Our Aim is to Overhaul Mirage, Aircraft, Aero Engines, Components/
Accessories and manufacturing of commercial desirable products as per laid
down procedures and regulations to meet all the requirement with
endeavour to continually improve the quality management system by setting
and resetting the quality objectives with employ participation”.
ISO 9001:2015, AS 9100D, ISO 17025 Certified

23. THANKS