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INTERNSHIP REPORT 2014 
Pakistan International Airlines 
From 1st of July 2014 to 15th of July 2014 
MUHAMMAD DILDAR AHMED 
IQRA UNIVERSITY 
TELECOMMUNICATION ENGINEERING 
Muhammad Dildar Ahmed 
IQRA University
INTERNSHIP REPORT 2014 
Muhammad Dildar Ahmed 
IQRA University 
Introduction 
The purpose of the internship was to introduce the 
telecommunication systems that are used in aircrafts. These 
systems include HF and VHF communication Systems, GPWS, ADF 
(automatic direction finder), CVR (cockpit voice recorder), Weather 
radar, ATC (air traffic controller), LRRA (low arrange radio 
Altimeter), DME (distance measurement equipment), TCAS (traffic 
collision avoidance system), IFE (interactive flight equipment), VOR 
(VHF Omni Range), ILS (Information Landing System), Marker 
Beacon System. We have also learned the working of Air Craft’s i.e. 
about Rudders, Elevator, Wing, Spoilers. This Internship was 
basically study of PIA aircrafts specially Boeing-777, Boeing-747 
and Boeing-310.
INTERNSHIP REPORT 2014 
Muhammad Dildar Ahmed 
IQRA University
INTERNSHIP REPORT 2014 
HF Communication: 
It is used for long distant communication. It uses sky wave propagation. The power 
requirement of HF transceivers is (100-200) but 120 is recommended. In PIA aircrafts 2 
HF transceivers are used. At a time 1 will work because of Single HF Antenna. 
VHF Communication: 
It is used for communication up to 150 miles. It is mostly used at the time of Take-off 
and landing. The power requirement of VHF transceivers is (18-28) but 22 watt is 
recommended. In PIA aircrafts 3 VHF transceivers are used. 3 can be Used 
Simultaneously 
Muhammad Dildar Ahmed 
IQRA University
INTERNSHIP REPORT 2014 
Automatic Direction Finder (ADF) 
An automatic direction finder (ADF) is an aircraft radio-navigation instrument which 
automatically and continuously displays the relative bearing from the ship or aircraft to 
a suitable radio station. ADF receivers are normally tuned to aviation operating in the 
LW band between 190 – 535 kHz. Like RDF units, most ADF receivers can also receive 
medium wave (AM) broadcast stations, though as mentioned, these are less reliable for 
navigational purposes. 
The operator tunes the ADF receiver to the correct frequency and verifies the identity 
of the beacon by listening to the Morse code signal transmitted. On aviation ADFs, the 
unit automatically moves a compass-like pointer (RMI) to show the direction of the 
beacon. The pilot may use this pointer to home directly towards the beacon, or may 
also use the magnetic compass and calculate the direction from the beacon (the radial) 
at which their aircraft is located. 
Unlike the RDF, the ADF operates without direct intervention, and continuously 
displays the direction of the tuned beacon. Initially, all ADF receivers, both marine and 
aircraft versions, contained a rotating loop or ferrite loop stick aerial driven by a motor 
which was controlled by the receiver. Like the RDF, a sense antenna verified the correct 
direction from its 180-degree opposite. 
More modern aviation ADFs contain a small array of fixed aerials and use electronic 
sensors to deduce the direction using the strength and phase of the signals from each aerial. 
The electronic sensors listen for the trough that occurs when the antenna is at right angles to 
the signal, and provide the heading to the station using a direction indicator. In flight, the 
ADF's RMI or direction indicator will always point to the broadcast station, regardless of the 
aircraft's attitude or heading. Such receivers can be used to determine current position, track 
inbound and outbound flight path, and intercept a desired bearing. These procedures are also 
used to execute holding patterns and non-precision instrument approaches. 
Muhammad Dildar Ahmed 
IQRA University
INTERNSHIP REPORT 2014 
Cockpit Voice Recorder (CVR) 
A cockpit voice recorder (CVR), often referred to as a "black box, is a flight recorder 
used to record the audio environment in the flight deck of an aircraft for the purpose of 
investigation of accidents and incidents. This is typically achieved by recording the 
signals of the microphones and earphones of the pilots’ headsets and of an area 
microphone in the roof of the cockpit. 
Where an aircraft is required to carry a CVR and utilizes digital communications the CVR 
is required to record such communications with air traffic control unless this is 
recorded elsewhere. As of 2005 it is an FAA requirement that the recording duration is 
a minimum of thirty minutes, but the NTSB has long recommended that it should be at 
least two hours. 
Muhammad Dildar Ahmed 
IQRA University
INTERNSHIP REPORT 2014 
Low Range Radio Altimeter 
Low range radio altimeter (LRRA) or simply RA measures altitude above the terrain presently beneath an 
aircraft or spacecraft. 
This type of altimeter provides the distance between the plane and the ground directly 
below it, opposed to a barometric altimeter which provides the distance above a pre-determined datum, 
usually sea level Radar altimeters are frequently used by commercial aircraft for approach and landing, 
especially in low-visibility conditions (see instrument flight rules) and also automatic landing, allowing the 
autopilot to know when to begin the flare manoeuvre. 
In civil aviation applications, radio altimeters generally only give readings up to 2,500 feet (760 m) above 
ground level (AGL) Radio altimeters are an essential part in ground proximity warning systems (GPWS), 
warning the pilot if the aircraft is flying too low or descending too quickly. 
However, radar altimeters cannot see terrain directly ahead of the aircraft, only that directly below it 
functionality requires either knowledge of position and the terrain at radar which uses technology similar 
to a radio altimeter. 
Muhammad Dildar Ahmed 
IQRA University
INTERNSHIP REPORT 2014 
Distance Measurement Equipment DME 
Distance measuring equipment (DME) is a transponder-based radio navigation technology 
that measures distance by timing the propagation delay of VHF or UHF radio signals. Aircraft 
use DME to determine their distance from a land-based transponder by sending and receiving 
pulse pairs - two pulses of fixed duration and separation. The ground stations are typically co-located 
with VORs. A typical DME ground transponder system for en-route or terminal 
navigation will have a 1 kW peak pulse output on the assigned UHF channel. A low-power DME 
can also be co-located with an ILS GLIDE SLOPE where it provides an accurate distance 
function, similar to that otherwise provided by ILS Marker Beacons. 
Muhammad Dildar Ahmed 
IQRA University
INTERNSHIP REPORT 2014 
Traffic Collision Avoidance System (TCAS) 
A traffic collision avoidance system or traffic alert and collision avoidance system 
(both abbreviated as TCAS) is an aircraft collision avoidance system designed to 
reduce the incidence of mid-air collisions between aircraft. It monitors the airspace 
around an aircraft for other aircraft equipped with a corresponding active 
transponder, independent of air traffic control, and warns pilots of the presence of 
other transponder-equipped aircraft which may present a threat of mid-air collision 
(MAC). It is a type of airborne collision avoidance system mandated by the 
International Civil Aviation Organization to be fitted to all aircraft with a maximum 
take-off mass (MTOM) of over 5700 kg (12,586 lbs) or authorized to carry more than 
19 passengers. 
Official definition from PANS-ATM (Nov 2007): ACAS / TCAS is an aircraft system 
based on secondary surveillance radar (SSR) transponder signals which operates 
independently of ground-based equipment to provide advice to the pilot on 
potential conflicting aircraft that are equipped with SSR transponders. 
In modern glass cockpit aircraft, the TCAS display may be integrated in the 
Navigation Display (ND); in older glass cockpit aircraft and those with mechanical 
instrumentation, such an integrated TCAS display may replace the mechanical 
Vertical Speed Indicator (which indicates the rate with which the aircraft is 
descending or climbing). 
Muhammad Dildar Ahmed 
IQRA University
INTERNSHIP REPORT 2014 
In-Flight Entertainment (IFE) 
In-flight entertainment (IFE) refers to the entertainment available to aircraft 
passengers during a flight. At first, IFE consisted of looking out the window. (Zeppelin 
sightseeing flights were available in Europe before the First World War.) In 1936, the 
airship Hindenburg offered passengers a piano, lounge, dining room, smoking room, 
and bar during the 2-1/2 day flight between Europe and America. ) After the Second 
World War, IFE was delivered in the form of food and drink services, along with an 
occasional projector movie during lengthy flights. In 1985 the first personal audio 
player was offered to passengers, along with noise cancelling headphones in 1989. 
During the 1990s the demand for better IFE was a major factor in the design of 
aircraft cabins. Before then, the most a passenger could expect was a movie 
projected on a screen at the front of a cabin, which could be heard via a headphone 
socket at seat. 
The largest manufacturers of IFE systems are Panasonic Avionics Corporation, Thales 
Group, Rockwell Collins and Live TV. Design issues for IFE include system safety, cost 
efficiency, software reliability, hardware maintenance, and user compatibility 
VHF Omni Range (VOR) 
VOR, short for VHF Omni directional radio range, is a type of radio navigation 
system for aircraft. A VOR ground station broadcasts a VHF radio composite signal 
including the station's identifier, voice (if equipped), and navigation signal. The 
identifier Morse code. The voice signal is usually station name, in-flight recorded 
advisories, or live flight service broadcasts. The navigation signal allows the airborne 
receiving equipment to determine a magnetic bearing from the station to the aircraft 
(direction from the VOR station in relation to the Earth's magnetic North at the time 
of installation). VOR stations in areas of magnetic compass unreliability are oriented 
with respect to True North. This line of position is called the "radial" from the VOR. 
The "intersection" of two radials from different VOR stations on a chart provides an 
approximate position of the aircraft. 
Muhammad Dildar Ahmed 
IQRA University
INTERNSHIP REPORT 2014 
Information Landing System (ILS) 
An Optical Landing System (OLS) is used to give glide path information to pilots in 
the terminal phase of landing on an aircraft carrier from the beginning of aircraft 
landing on ships in the 1920s to the introduction of OLSs, pilots relied solely on their 
visual perception of the landing area and the aid of the Landing Signal Officer (LSO in 
the US Navy, or "batsman" in the Commonwealth navies). LSOs used colored flags, 
cloth paddles and lighted wands. 
Muhammad Dildar Ahmed 
IQRA University
INTERNSHIP REPORT 2014 
What is battery? 
An electric battery is a device consisting of one or more electrochemical cells that convert 
stored chemical energy into electrical energy. Each cell contains a positive terminal, or 
cathode, and a negative terminal, or anode. Electrolytes allow ions to move between the 
electrodes and terminals, which allows current to flow out of the battery to perform work. 
Lead–acid battery: 
Lead acid batteries used in the RV and Marine Industries usually consist of two 6-volt 
batteries in series, or a single 12-volt battery. These batteries are constructed of several 
single cells connected in series each cell produces approximately 2.1 volts. A six-volt battery 
has three single cells, which when fully charged produce an output voltage of 6.3 volts. A 
twelve-volt battery has six single cells in series producing a fully charged output voltage of 
12.6 volts. 
A battery cell consists of two lead plates a positive plate covered with a paste of lead 
dioxide and a negative made of sponge lead, with an insulating material (separator) in 
between. The plates are enclosed in a plastic battery case and then submersed in an 
electrolyte consisting of water and sulfuric acid. Each cell is capable of storing 2.1 volts. 
Alkaline battery: 
Alkaline batteries are a type of primary batteries dependent upon the reaction between zinc 
and manganese dioxide (Zn/MnO2). A rechargeable alkaline battery allows reuse of specially 
designed cells. The alkaline battery gets its name becaus e it has an alkaline electrolyte of 
potassium hydroxide, instead of the acidic ammonium chloride or zinc chloride electrolyte 
of the zinc-carbon batteries. Other battery systems also use alkaline electrolytes, but they 
use different active materials for the electrodes. 
The capacity of an alkaline battery is strongly dependent on the load. The nominal voltage 
of a fresh alkaline cell is 1.5 V. Multiple voltages may be achieved with series of cells . The 
effective zero-load voltage of a non discharged alkaline battery varies from 1.50 to 1.65 V, 
Muhammad Dildar Ahmed 
IQRA University
INTERNSHIP REPORT 2014 
depending on the purity of the manganese dioxide used and the contents of zinc oxide in 
the electrolyte. The average voltage under load depends on level of discharge and the 
amount of current being drawn, varying from 1.1 to 1.3 V. The fully discharged cell has a 
remaining voltage in the range of 0.8 to 1.0 V. 
Alkaline batteries are manufactured in standardized cylindrical forms interchangeable with 
zinc-carbon batteries, and in button forms. Several individual cells may be interconnected to 
form a true "battery", such as those sold for use with flashlights and the 9 volt transistor-radio 
battery. 
Navigation: 
Navigation is a field of study that focuses on the process of monitoring and controlling the 
movement of a craft or vehicle from one place to another. The field of navigation includes 
four general categories: land navigation, marine navigation, aeronautic navigation, and 
space navigation. 
All navigational techniques involve locating the navigator's position compared to known 
locations or patterns. 
Muhammad Dildar Ahmed 
IQRA University
INTERNSHIP REPORT 2014 
Muhammad Dildar Ahmed 
IQRA University

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PIA internship report

  • 1. INTERNSHIP REPORT 2014 Pakistan International Airlines From 1st of July 2014 to 15th of July 2014 MUHAMMAD DILDAR AHMED IQRA UNIVERSITY TELECOMMUNICATION ENGINEERING Muhammad Dildar Ahmed IQRA University
  • 2. INTERNSHIP REPORT 2014 Muhammad Dildar Ahmed IQRA University Introduction The purpose of the internship was to introduce the telecommunication systems that are used in aircrafts. These systems include HF and VHF communication Systems, GPWS, ADF (automatic direction finder), CVR (cockpit voice recorder), Weather radar, ATC (air traffic controller), LRRA (low arrange radio Altimeter), DME (distance measurement equipment), TCAS (traffic collision avoidance system), IFE (interactive flight equipment), VOR (VHF Omni Range), ILS (Information Landing System), Marker Beacon System. We have also learned the working of Air Craft’s i.e. about Rudders, Elevator, Wing, Spoilers. This Internship was basically study of PIA aircrafts specially Boeing-777, Boeing-747 and Boeing-310.
  • 3. INTERNSHIP REPORT 2014 Muhammad Dildar Ahmed IQRA University
  • 4. INTERNSHIP REPORT 2014 HF Communication: It is used for long distant communication. It uses sky wave propagation. The power requirement of HF transceivers is (100-200) but 120 is recommended. In PIA aircrafts 2 HF transceivers are used. At a time 1 will work because of Single HF Antenna. VHF Communication: It is used for communication up to 150 miles. It is mostly used at the time of Take-off and landing. The power requirement of VHF transceivers is (18-28) but 22 watt is recommended. In PIA aircrafts 3 VHF transceivers are used. 3 can be Used Simultaneously Muhammad Dildar Ahmed IQRA University
  • 5. INTERNSHIP REPORT 2014 Automatic Direction Finder (ADF) An automatic direction finder (ADF) is an aircraft radio-navigation instrument which automatically and continuously displays the relative bearing from the ship or aircraft to a suitable radio station. ADF receivers are normally tuned to aviation operating in the LW band between 190 – 535 kHz. Like RDF units, most ADF receivers can also receive medium wave (AM) broadcast stations, though as mentioned, these are less reliable for navigational purposes. The operator tunes the ADF receiver to the correct frequency and verifies the identity of the beacon by listening to the Morse code signal transmitted. On aviation ADFs, the unit automatically moves a compass-like pointer (RMI) to show the direction of the beacon. The pilot may use this pointer to home directly towards the beacon, or may also use the magnetic compass and calculate the direction from the beacon (the radial) at which their aircraft is located. Unlike the RDF, the ADF operates without direct intervention, and continuously displays the direction of the tuned beacon. Initially, all ADF receivers, both marine and aircraft versions, contained a rotating loop or ferrite loop stick aerial driven by a motor which was controlled by the receiver. Like the RDF, a sense antenna verified the correct direction from its 180-degree opposite. More modern aviation ADFs contain a small array of fixed aerials and use electronic sensors to deduce the direction using the strength and phase of the signals from each aerial. The electronic sensors listen for the trough that occurs when the antenna is at right angles to the signal, and provide the heading to the station using a direction indicator. In flight, the ADF's RMI or direction indicator will always point to the broadcast station, regardless of the aircraft's attitude or heading. Such receivers can be used to determine current position, track inbound and outbound flight path, and intercept a desired bearing. These procedures are also used to execute holding patterns and non-precision instrument approaches. Muhammad Dildar Ahmed IQRA University
  • 6. INTERNSHIP REPORT 2014 Cockpit Voice Recorder (CVR) A cockpit voice recorder (CVR), often referred to as a "black box, is a flight recorder used to record the audio environment in the flight deck of an aircraft for the purpose of investigation of accidents and incidents. This is typically achieved by recording the signals of the microphones and earphones of the pilots’ headsets and of an area microphone in the roof of the cockpit. Where an aircraft is required to carry a CVR and utilizes digital communications the CVR is required to record such communications with air traffic control unless this is recorded elsewhere. As of 2005 it is an FAA requirement that the recording duration is a minimum of thirty minutes, but the NTSB has long recommended that it should be at least two hours. Muhammad Dildar Ahmed IQRA University
  • 7. INTERNSHIP REPORT 2014 Low Range Radio Altimeter Low range radio altimeter (LRRA) or simply RA measures altitude above the terrain presently beneath an aircraft or spacecraft. This type of altimeter provides the distance between the plane and the ground directly below it, opposed to a barometric altimeter which provides the distance above a pre-determined datum, usually sea level Radar altimeters are frequently used by commercial aircraft for approach and landing, especially in low-visibility conditions (see instrument flight rules) and also automatic landing, allowing the autopilot to know when to begin the flare manoeuvre. In civil aviation applications, radio altimeters generally only give readings up to 2,500 feet (760 m) above ground level (AGL) Radio altimeters are an essential part in ground proximity warning systems (GPWS), warning the pilot if the aircraft is flying too low or descending too quickly. However, radar altimeters cannot see terrain directly ahead of the aircraft, only that directly below it functionality requires either knowledge of position and the terrain at radar which uses technology similar to a radio altimeter. Muhammad Dildar Ahmed IQRA University
  • 8. INTERNSHIP REPORT 2014 Distance Measurement Equipment DME Distance measuring equipment (DME) is a transponder-based radio navigation technology that measures distance by timing the propagation delay of VHF or UHF radio signals. Aircraft use DME to determine their distance from a land-based transponder by sending and receiving pulse pairs - two pulses of fixed duration and separation. The ground stations are typically co-located with VORs. A typical DME ground transponder system for en-route or terminal navigation will have a 1 kW peak pulse output on the assigned UHF channel. A low-power DME can also be co-located with an ILS GLIDE SLOPE where it provides an accurate distance function, similar to that otherwise provided by ILS Marker Beacons. Muhammad Dildar Ahmed IQRA University
  • 9. INTERNSHIP REPORT 2014 Traffic Collision Avoidance System (TCAS) A traffic collision avoidance system or traffic alert and collision avoidance system (both abbreviated as TCAS) is an aircraft collision avoidance system designed to reduce the incidence of mid-air collisions between aircraft. It monitors the airspace around an aircraft for other aircraft equipped with a corresponding active transponder, independent of air traffic control, and warns pilots of the presence of other transponder-equipped aircraft which may present a threat of mid-air collision (MAC). It is a type of airborne collision avoidance system mandated by the International Civil Aviation Organization to be fitted to all aircraft with a maximum take-off mass (MTOM) of over 5700 kg (12,586 lbs) or authorized to carry more than 19 passengers. Official definition from PANS-ATM (Nov 2007): ACAS / TCAS is an aircraft system based on secondary surveillance radar (SSR) transponder signals which operates independently of ground-based equipment to provide advice to the pilot on potential conflicting aircraft that are equipped with SSR transponders. In modern glass cockpit aircraft, the TCAS display may be integrated in the Navigation Display (ND); in older glass cockpit aircraft and those with mechanical instrumentation, such an integrated TCAS display may replace the mechanical Vertical Speed Indicator (which indicates the rate with which the aircraft is descending or climbing). Muhammad Dildar Ahmed IQRA University
  • 10. INTERNSHIP REPORT 2014 In-Flight Entertainment (IFE) In-flight entertainment (IFE) refers to the entertainment available to aircraft passengers during a flight. At first, IFE consisted of looking out the window. (Zeppelin sightseeing flights were available in Europe before the First World War.) In 1936, the airship Hindenburg offered passengers a piano, lounge, dining room, smoking room, and bar during the 2-1/2 day flight between Europe and America. ) After the Second World War, IFE was delivered in the form of food and drink services, along with an occasional projector movie during lengthy flights. In 1985 the first personal audio player was offered to passengers, along with noise cancelling headphones in 1989. During the 1990s the demand for better IFE was a major factor in the design of aircraft cabins. Before then, the most a passenger could expect was a movie projected on a screen at the front of a cabin, which could be heard via a headphone socket at seat. The largest manufacturers of IFE systems are Panasonic Avionics Corporation, Thales Group, Rockwell Collins and Live TV. Design issues for IFE include system safety, cost efficiency, software reliability, hardware maintenance, and user compatibility VHF Omni Range (VOR) VOR, short for VHF Omni directional radio range, is a type of radio navigation system for aircraft. A VOR ground station broadcasts a VHF radio composite signal including the station's identifier, voice (if equipped), and navigation signal. The identifier Morse code. The voice signal is usually station name, in-flight recorded advisories, or live flight service broadcasts. The navigation signal allows the airborne receiving equipment to determine a magnetic bearing from the station to the aircraft (direction from the VOR station in relation to the Earth's magnetic North at the time of installation). VOR stations in areas of magnetic compass unreliability are oriented with respect to True North. This line of position is called the "radial" from the VOR. The "intersection" of two radials from different VOR stations on a chart provides an approximate position of the aircraft. Muhammad Dildar Ahmed IQRA University
  • 11. INTERNSHIP REPORT 2014 Information Landing System (ILS) An Optical Landing System (OLS) is used to give glide path information to pilots in the terminal phase of landing on an aircraft carrier from the beginning of aircraft landing on ships in the 1920s to the introduction of OLSs, pilots relied solely on their visual perception of the landing area and the aid of the Landing Signal Officer (LSO in the US Navy, or "batsman" in the Commonwealth navies). LSOs used colored flags, cloth paddles and lighted wands. Muhammad Dildar Ahmed IQRA University
  • 12. INTERNSHIP REPORT 2014 What is battery? An electric battery is a device consisting of one or more electrochemical cells that convert stored chemical energy into electrical energy. Each cell contains a positive terminal, or cathode, and a negative terminal, or anode. Electrolytes allow ions to move between the electrodes and terminals, which allows current to flow out of the battery to perform work. Lead–acid battery: Lead acid batteries used in the RV and Marine Industries usually consist of two 6-volt batteries in series, or a single 12-volt battery. These batteries are constructed of several single cells connected in series each cell produces approximately 2.1 volts. A six-volt battery has three single cells, which when fully charged produce an output voltage of 6.3 volts. A twelve-volt battery has six single cells in series producing a fully charged output voltage of 12.6 volts. A battery cell consists of two lead plates a positive plate covered with a paste of lead dioxide and a negative made of sponge lead, with an insulating material (separator) in between. The plates are enclosed in a plastic battery case and then submersed in an electrolyte consisting of water and sulfuric acid. Each cell is capable of storing 2.1 volts. Alkaline battery: Alkaline batteries are a type of primary batteries dependent upon the reaction between zinc and manganese dioxide (Zn/MnO2). A rechargeable alkaline battery allows reuse of specially designed cells. The alkaline battery gets its name becaus e it has an alkaline electrolyte of potassium hydroxide, instead of the acidic ammonium chloride or zinc chloride electrolyte of the zinc-carbon batteries. Other battery systems also use alkaline electrolytes, but they use different active materials for the electrodes. The capacity of an alkaline battery is strongly dependent on the load. The nominal voltage of a fresh alkaline cell is 1.5 V. Multiple voltages may be achieved with series of cells . The effective zero-load voltage of a non discharged alkaline battery varies from 1.50 to 1.65 V, Muhammad Dildar Ahmed IQRA University
  • 13. INTERNSHIP REPORT 2014 depending on the purity of the manganese dioxide used and the contents of zinc oxide in the electrolyte. The average voltage under load depends on level of discharge and the amount of current being drawn, varying from 1.1 to 1.3 V. The fully discharged cell has a remaining voltage in the range of 0.8 to 1.0 V. Alkaline batteries are manufactured in standardized cylindrical forms interchangeable with zinc-carbon batteries, and in button forms. Several individual cells may be interconnected to form a true "battery", such as those sold for use with flashlights and the 9 volt transistor-radio battery. Navigation: Navigation is a field of study that focuses on the process of monitoring and controlling the movement of a craft or vehicle from one place to another. The field of navigation includes four general categories: land navigation, marine navigation, aeronautic navigation, and space navigation. All navigational techniques involve locating the navigator's position compared to known locations or patterns. Muhammad Dildar Ahmed IQRA University
  • 14. INTERNSHIP REPORT 2014 Muhammad Dildar Ahmed IQRA University