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Prime Minister Narendra Modi on Sunday said that he would inaugurate the first airport in Sikkim at Pakyong on Monday. The airport will improve connectivity, benefitting the people of the state. PM Modi left for the Himalayan state after launching the Centre's flagship Ayushman Bharat-National Health Protection Mission (AB-NHPM) from Jharkhand capital Ranchi on Sunday. "After the programme in Jharkhand I will leave for Sikkim. In Sikkim, I will be inaugurating the Pakyong Airport tomorrow, which will improve connectivity and benefit the people of Sikkim," Modi tweeted.
- Flight details: The first commercial flight from Pakyong would begin from October 4. SpiceJet will operate 78-seater Bombardier Q400 flights to and fro Delhi, Kolkata and Guwahati everyday under the Civil Aviation Ministry's Ude Desh Ka Aam Nagrik (UDAN) scheme. Initially the airport would only cater to domestic flights, but later it will also provide international flight services connecting Sikkim with other countries like Paro in Bhutan, Kathmandu in Nepal and Dhaka in Bangladesh.
- IAF's Dornier-228 aircraft was tested from Pakyong on March 5. SpiceJet followed it by conducting test runs of the 78-seater Bombardier Q400 from Kolkata to Pakyong on March 10. This led to security clearances for commercial operations.
Sikkim's dream of having an airport is set to come true after nine years. The foundation stone of the greenfield airport was laid, around 33 km from Gangtok, in 2009.
- The Pakyong airport of Sikkim is spread over 201 acres and is located on top of a hill about two km above Pakyong village at 4,500 feet above sea level, according to Sikkim Chief Secretary A K Srivastava.
- Sikkim's first airport has been was constructed by the Airports Authority of India. At present, the nearest airport from Sikkim is located 124 km away in Bagdogra in West Bengal.
- Engineering marvel! Sikkim airport has been constructed at an estimated cost of Rs 605 crore. It is an "engineering marvel" for its soil reinforcement and slope stabilisation techniques keeping in view the altitude it was built at, Srivastava told news agency PTI. According to Pakyong Airport Director R Manjunatha, the land for the airport was carved from the mountainside using massive geotechnical 'cut and fill' engineering works.
- World record! The reinforcement wall of the project is 80-metre-high, which is one of the tallest in the world, said Srivastava.
- Features: Integrated structures comprising an ATC tower-cum-fire station, two sophisticated CFT, one terminal building for passengers, high-intensity runway lights, parking for over 50 vehicles are some of the features of the airport.
- Location: The Pakyong airport is located around 60 km from the Indo-China border.
- Benefit to IAF: The Indian Air Force (IAF) would be able to land various types of aircraft on the airport's runway with the construction of another 75-metre stretch adjacent to the main runway in the coming days.
- Runway, terminal: The airport has a 1.75 km runway with a width of 30 metre. It has a 116-metre-long taxiway connecting it to an apron measuring 106 metre by 76 metre that can simultaneously accommodate two ATR-72 aircraft. The airport has 3,000 sq metre terminal building, which can handle 50 in-bound and as many out-bound passengers.
Security: Sikkim Police has been entrusted with the security of the Pakyong airport, the officials said.
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Sandeep kumar
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List of Modules- AME License Examination
List of Modules- AME License Examination
List of Modules for AME License Examination Revised Scheme by DGCA
Module 1 – Mathematics
Arithmetic
Algebra
Geometry
Module 2- Physics
Matter
Mechanics
Thermodynamics
Optics
Wave Motion and Sound
Module 3 – Electrical Fundamentals
Electron Theory
Static Electricity and Conduction
Electrical Terminology
Generation of Electricity
DC Sources of Electricity
DC Circuits
Resistance/Resistor
Power
Capacitance/Capacitor
Magnetism
Inductance/Inductor
DC Motor/Generator Theory
AC Theory
Resistive (R), Capacitive (C) and Inductive (L) Circuits
Transformers
Filters
AC Generators
AC Motors
Module 4- Electronic Fundamentals
Semiconductors
Printed Circuit Boards
Servomechanisms
Module 5- Digital Techniques Electronic Instrument System
Electronic Instrument Systems
Numbering Systems
Data Conversion
Data Buses
Logic Circuits
Basic Computer Structure
Microprocessors
Integrated Circuits
Multiplexing
Fibre Optics
Electronic Displays
Electrostatic Sensitive Devices
Software Management Control
Electromagnetic Environment
Typical Electronic/Digital Aircraft Systems
Module 6-Materials and Hardware
Aircraft Materials — Ferrous
Aircraft Materials — Non-Ferrous
Aircraft Materials – Composite and Non- Metallic
Corrosion
Fasteners
Pipes and Unions
Springs
Bearings
Transmissions
Control Cables
Electrical Cables and Connectors
Module 7- Maintenance Practices
Safety Precautions-Aircraft and Workshop
Workshop Practices
Tools
Avionic General Test Equipment
Engineering Drawings, Diagrams and Standards
Fits and Clearances
Electrical Wiring Interconnection System (EWIS)
Riveting
Pipes and Hoses
Springs
Bearings
Transmissions
Control Cables
Material handling
Welding, Brazing, Soldering and Bonding
Aircraft Weight and Balance
Aircraft Handling and Storage
Disassembly, Inspection, Repair and Assembly Techniques
Abnormal Events
Maintenance Procedures
Module 8-Basic Aerodynamics
Physics of the Atmosphere
Aerodynamics
Theory of Flight
Flight Stability and Dynamics
Module 9- Human Factors
General
Human Performance and Limitations
Social Psychology
Factors Affecting Performance
Physical Environment
Tasks
Communication
Human Error
Hazards in the Workplace
Module 10- Aviation Legislation
Regulatory Framework
CAR-66 Certifying Staff – Maintenance
CAR-145 — Approved Maintenance Organisations
Aircraft Operations
Aircraft Certification
CAR-M
Applicable National and International Requirements
Safety Management System
Fuel Tank Safety
Module 11A- Turbine Aeroplane Aerodynamics, Structures and Systems
Theory of Flight
Airframe Structures — General Concepts
Airframe Structures — Aeroplanes
Air Conditioning and Cabin Pressurisation (ATA 21)
Instruments/Avionic Systems
Electrical Power (ATA 24)
Equipment and Furnishings (ATA 25)
Fire Protection (ATA 26)
Flight Controls (ATA 27)
Fuel Systems (ATA 28)
Hydraulic Power (ATA 29)
Ice and Rain Protection (ATA 30)
Landing Gear (ATA 32)
Lights (ATA 33)
Oxygen (ATA 35)
Pneumatic/Vacuum (ATA 36)
Water/Waste (ATA 38)
On Board Maintenance Systems (ATA 45)
Integrated Modular Avionics (ATA42 )
Cabin Systems (ATA44)
Module 11B-Piston Aeroplane Aerodynamics, Structures and Systems
Theory of Flight
Airframe Structures — General Concepts
Airframe Structures — Aeroplanes
Air Conditioning and Cabin Pressurisation (ATA 21)
Instruments/Avionic Systems
Electrical Power (ATA 24)
Equipment and Furnishings (ATA 25)
Fire Protection (ATA 26)
Flight Controls (ATA 27)
Fuel Systems (ATA 28)
Hydraulic Power (ATA 29)
Ice and Rain Protection (ATA 30)
Landing Gear (ATA 32)
Lights (ATA 33)
Oxygen (ATA 35)
Pneumatic/Vacuum (ATA 36)
Water/Waste (ATA 38)
Module 12- Helicopter Aerodynamics, Structures and System
Theory of Flight — Rotary Wing Aerodynamics
Flight Control Systems
Blade Tracking and Vibration Analysis
Transmissions
Airframe Structures
Air Conditioning (ATA 21)
Instruments/Avionic Systems
Electrical Power (ATA 24)
Equipment and Furnishings (ATA 25)
Fire Protection (ATA 26)
Fuel Systems (ATA 28)
Hydraulic Power (ATA 29)
Ice and Rain Protection (ATA 30)
Landing Gear (ATA 32)
Lights (ATA 33)
Pneumatic/Vacuum (ATA 36)
Integrated Modular Avionics (ATA42)
On Board Maintenance Systems (ATA45)
Information Systems (ATA46)
Module 13-Aircraft Aerodynamics , Structures and System
Theory of Flight
Structures — General Concepts
Autoflight (ATA 22)
Communication/Navigation (ATA 23/34)
Electrical Power (ATA 24)
Equipment and Furnishings (ATA 25)
Flight Controls (ATA 27)
Instrument Systems (ATA 31)
Lights (ATA 33)
On board Maintenance Systems (ATA 45)
Air Conditioning and Cabin Pressurisation (ATA21)
Pressurisation
Fire Protection (ATA 26)
Fuel Systems (ATA 28)
Hydraulic Power (ATA 29 )
Ice and Rain Protection (ATA 30)
Landing Gear (ATA 32)
Oxygen (ATA 35)
Pneumatic/Vacuum (ATA 36)
Water/Waste (ATA 38)
Integrated Modular Avionics (ATA42)
Cabin Systems (ATA44)
Information Systems (ATA46)
Module 14- Propulsion
Turbine Engines
Engine Indicating Systems
Starting and Ignition Systems
Module 15- Gas Turbine Engine
Fundamentals
Engine Performance
Inlet
Compressors
Combustion Section
Turbine Section
Exhaust
Bearings and Seals
Lubricants and Fuels
Lubrication Systems
Fuel Systems
Air Systems
Starting and Ignition Systems
Engine Indication Systems
Power Augmentation Systems
Turbo-prop Engines
Turbo-shaft engines
Auxiliary Power Units (APUs)
Powerplant Installation
Fire Protection Systems
Engine Monitoring and Ground Operation
Engine Storage and Preservation
Module 16- Piston Engine
Fundamentals
Engine Performance
Engine Construction
Engine Fuel Systems
Carburetors
Fuel injection systems
Electronic engine control
Starting and Ignition Systems
Induction, Exhaust and Cooling Systems
Supercharging/Turbocharging
Lubricants and Fuels
Lubrication Systems
Engine Indication Systems
Powerplant Installation
Engine Monitoring and Ground Operation
Engine Storage and Preservation
Module 17-Propeller
Fundamentals
Propeller Construction
Propeller Pitch Control
Propeller Synchronising
Propeller Ice Protection
Propeller Maintenance
Propeller Storage and Preservation
Sandeep kumar
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Revised Part-66 AME License Examination Policy by DGCA, India (Viman)
Revised Part-66 AME License Examination Policy by DGCA, India (Viman)
AME License Examination Guide 1 :
ONLINE registration for AME License Examination
The Directorate General of Civil Aviation (DGCA) has been conducting examinations for issue/ extension of Aircraft Maintenance Engineer (AME) License, in accordance with Rule 61 of Indian Aircraft Rules 1937. The Central Examination Organization (CEO) of DGCA, located at R. K. Puram, New Delhi is responsible for conducting these examinations. So far these examinations were conducted as per the requirements laid down in Civil Aviation Requirements, Section 2, Series L, however, with the implementation of CAR-66, henceforth the examinations will be conducted based on modular system. In this system, the existing papers have been bifurcated in more than 40 papers (QPREF) of varied complexity and knowledge levels to cater for all modules as per CAR-66.
These examinations will generally be conducted on-line, at the designated centers, in line with prevailing international standards, wherein the candidate appears in the exam through a computer and gets the score on the spot. Initially, some of the papers may be conducted OMR based also. In order to maintain the examination schedule, the October 2016 session has been merged with the first session of February 2017.
The information regarding the schedule of examinations and centers etc. will be published on the DGCA web-site: “http://www.dgca.nic.in”. The examination portal for the registration of both, existing and new AME applicants, desirous to appear for AME examinations is “http://www.viman.gov.in”. Candidates are advised to carefully read the instructions and login to the login to the web site www.viman.gov.in and then read the “User Manual” before filling up the applications.
“USER MANUAL” IS AVAILABLE BELOW , DOWNLOAD TO UNDERSTAND THE VIMAN PORTAL FEATURES.
The fee for appearing in the exam has been revised as per Rule 62 of Indian Aircraft Rule 1937 and accordingly, an additional amount of Rs 2000/- per paper shall be payable by the candidate for appearing in on-line exam. The fee shall be payable in on-line mode only, through „Bharatkosh‟ payment gateway. Back In case of any query with respect to online application, the applicants may contact the helpline at +91 11 26106011. This helpline is available for the above said purpose, on working days between 10:30-12:30 Hrs. and 14:30-16:30 Hrs. The candidate may also e-mail their query on [email protected].
AME License Examination Guide 2 :
Registration and Computer Number Allotment
All these guidance are as per AME Online Examination-VIMAN INSTRUCTION NO.: 01 of 2016
AME License Examination system has been brought ONLINE with effect from NOV’2016. The applicants / candidates are required to interact with the online system of examination through the DGCA AME examination portal www.viman.gov.in.
Henceforth, all the examination with respect to all the categories of AMEs License Examination will be held ONLINE and/or OMR based through this portal only. This portal is to be used by the candidates [New & OLD*] for login, registration , uploading of photo , signature and mandatory documents, allotment of Computer Number (for new candidates only), applying for examination, printing of admit cards, profile update etc. (*All candidates who have been allotted computer number till July2016).
Yes !!! Old Candidates Means All candidates who have been allotted computer number till July2016).
Detailed step by step procedures to be followed by the candidates are available on the examination portal „VIMAN‟.
Candidates are advised to carefully read the instructions and login to the web site www.viman.gov.in and then read the “User Manual” before filling up the applications. Given below are instructions with respect to
Given below are instructions with respect to login and registration for computer number allotment, for applicants‟ strict compliance:
1. The minimum system requirement to access this website is Google chrome or Internet Explorer 11.0.
2. All “Old & New” AME Candidate required to visit www.viman.gov.in and use the respective tab for “Old & New” AME Candidate, under “Registration Area” tab to fill up the required details and “Submit”.
3. Individual Email ID of the candidate is an important component of the System. All important information such as Computer Number, Roll Number, Examination Schedules, and Application Status etc. will be communicated to the candidate on this email ID only.
4. Check your registered e-mail box for the e-mail with a temporary link for activating the account within a period of 24 hours.
5. While generating password, ensure password length should be 8 characters. It must contain at least one upper case letter (A-Z), one lower case letter (a-z), one special character ([email protected]#$%) and one numeric value one numeric value (0– 9).
6. Now to proceed further for Registration, candidates can refer the guideline by referring the “User Manual” tab after login to the system with credentials.
7. The “Old AME Candidate Registration” is a ONE TIME exercise and not required for each session of examination. “OLD Candidate Registration” process will be open for 3 months only, within which all OLD candidates are required to re-register in the new VIMAN online portal. Without registering in the new online portal candidates will not be able to appear in any examination/ access his/ her record in future.
8. All OLD Candidates while registering MUST CHECK their particular (e.g Name /D.O.B / Father‟s Name etc.) displayed in the system including the PASSED Papers. (if any). Any ambiguity / mismatch observed must immediately be brought to the notice of CEO on e-mail [email protected] within 07 days from the date of registration with all relevant supporting documents to CEO by e-mail followed by hard copy by speed post under the subject line “MISMATCH in saved profile. Comp No E-XXXXXXX”.
9. The allotment of Computer Number does not automatically enroll the applicant for the examination. Applicant will have to fill up examination form separately to get Roll Number for appearing in the examination in the same portal, after opening of the portal.
10. The successfully registered OLD and NEW candidates with computer number, can fill online application for examination only after the examination portal is declared open, which will be notified through a Public Notice on DGCA web-site as well as in the „Notice-Board‟ of the home page of examination portal „VIMAN‟.
11. All NEW candidates desiring to appear in the 1 st session of 2017 ONLINE examination must apply for allotment of Computer Number latest by 15th December’2016.
12. A telephone helpline for AME 011-26106011 will be available during (1030-1230 hrs.) and (1430- 1630 hrs.) on all working days for the benefit of the candidates.
13. Candidates are advised to forward all queries, request etc. to the dedicated e-mail address for AME i.e. [email protected] under the specific subject line, for prompt action.
STEP BY STEP SCREENSHOTS FOR YOUR REFERENCE
Old Candidates Registration
New Candidates Registration
Login Page for Old and New Candidates
After Login Page
Check out your Examination History !! If there is any mismatch, Contact the helpline number 011-26106011
Sandeep kumar
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DGCA CAR-66 AME License Examination Guide
DGCA CAR-66 AME License Examination Guide
CAR-66 AME License Examination by DGCA
Highlights of CAR-66
DGCA CAR-66 harmonise the aircraft maintenance personnel licensing system with EASA Part 66.
CAR-66 eliminates the system of obtaining Airframe, Engine, Electrical, Instrument and Radio System Licences separately.
CAR-66 redefines the syllabus for basic knowledge examination in modular pattern
AME Examination Guide
Category of CAR-66 AME License: Aircraft maintenance licences include the following categories:
Category A- A category A aircraft maintenance engineer’s licence permits the holder to issue certificates of release to service following minor scheduled line maintenance and simple defect rectification within the limits of tasks specifically endorsed on the authorization issued by an organization approved under rule 133B for the type of aircraft endorsed on the licence
Category B1– A category B1 aircraft maintenance engineer’s licence shall permit the holder to issue certificates of release to service following maintenance including aircraft structure, power plant and mechanical and electrical systems in respect of an air-craft type endorsed on license. Replacement of avionic line replaceable units, re-quiring simple tests to prove their serviceability shall also be included in the priv-ileges. Category B1 shall automatically include the appropriate A subcate-gory.
Category B2-A category B2 aircraft maintenance engineer’s licence shall permit the holder to issue certificates of release to service following maintenance on avionic and electrical systems of an aircraft type endorsed on the licence .
Category C -A category C aircraft maintenance engineer’s licence shall permit the holder to issue certificates of release to service following base maintenance on aircraft type en-dorsed on the licence.
Categories A and B1 are subdivided into subcategories relative to combinations of aeroplanes, helicopters, turbine and piston engines. The subcategories are:
A1 and B1.1 Aeroplanes Turbine
A2 and B1.2 Aeroplanes Piston
A3 and B1.3 Helicopters Turbine
A4 and B1.4 Helicopters Piston
Understand the knowledge level in CAR-66 AME License Examination
Basic knowledge for categories A, B1 and B2 are indicated by the knowledge levels (1, 2 or 3) against each applicable subject. Category C applicant shall meet either category B1 or B2 basic knowledge level.
DOWNLOAD
Modularisation in CAR-66
DOWNLOAD
CAR-66 AME License Examination Modules Syllabus-
(Download in PDF)
Subject – Syllabus (download PDF)
Module 1- Mathematics
Module 2- Physics
Module 3 – Electrical Fundamentals
Module 4- Electronic Fundamentals
Module 5- Digital Techniques Electronic Instrument System
Module 6-Materials and Hardware
Module 7- Maintenance Practices
Module 8-Basic Aerodynamics
Module 9- Human Factors
Module 10- Aviation Legislation
Module 11A- Turbine Aeroplane Aerodynamics, Structures and Systems
Module 11B-Piston Aeroplane Aerodynamics, Structures and Systems
Module 12- Helicopter Aerodynamics, Structures and System
Module 13-Aircraft Aerodynamics , Structures and System
Module 14- Propulsion
Module 15- Gas Turbine Engine
Module 16- Piston Engine
Module 17-Propeller
Register your profile for AME License Examination
The Directorate General of Civil Aviation (DGCA) has been conducting examinations for issue of Aircraft Maintenance Engineers (AME) License, in accordance with Rule 61 of Indian Aircraft Rules 1937. The Central Examination Organisation(CEO) of DGCA, located at R. K. Puram, New Delhi is responsible for conducting these examinations, in accordance with CAR -66 on modular system. These examinations will generally be conducted on-line, at the designated centers. The information regarding the schedule of examinations and centers etc. will be published on the DGCA web-site: www.dgca.nic.in. “VIMAN” is the official web-site of DGCA for the registration of both existing and new AMEs/ applicants, desirous to appear for AME examinations.
Sandeep kumar
posted a thread.
AME Online Examination- VIMAN
AME Online Examination- VIMAN
The Directorate General of Civil Aviation (DGCA) has been conducting examinations for issue of Aircraft Maintenance Engineers (AME) License, in accordance with Rule 61 of Indian Aircraft Rules 1937. The Central Examination Organisation(CEO) of DGCA, located at R. K. Puram, New Delhi is responsible for conducting these examinations, in accordance with CAR -66 on modular system. These examinations will generally be conducted on-line, at the designated centers. The information regarding the schedule of examinations and centers etc. will be published on the DGCA web-site: www.dgca.nic.in. “VIMAN” is the official web-site of DGCA for the registration of both existing and new AMEs/ applicants, desirous to appear for AME examinations.
Important Instruction:
(1) All AMEs candidates (existing / new) are required to register their profile on VIMAN portal.
(2) VIMAN is recently propelled stage, so there might be odds of web server usefulness. So friends, kindly don’t stress over this. Have patients.
NOTE: FOR ANY QUERIES Do not hesitate to comment here.
Visit :https://viman.gov.in/DGCA_AME/
Contact – DGCA for AME Examination
Address : Central Examination Organisation,
Directorate General of Civil Aviation,
East Block III, Level III, RK Puram,
New Delhi-110066
Phone : 01126193706
Email Address : [email protected]
Sandeep kumar
posted a thread.
FREE BOOKS FOR AIRCRAFT MAINTENANCE ENGINEERING
DOWNLOAD FREE BOOKS FOR AIRCRAFT MAINTENANCE ENGINEERING
Here you will find the most popular , best and recommended books for Aircraft Maintenance Engineering in PDF format. You can click on the title and download it on any device without any login or registration. We recommend you to please subscribe us to get more information on Aviation Engineering.
Here you can find the best popular and recommended books for Aircraft Maintenance Engineering License examination conducted by Director General of Civil Aviation (DGCA), India.
Paper I
1. Aircraft Manual
2. Civil Aviation Requirements (Section 2- Airworthiness)
3. Aeronautical Information Circulars (relating to Airworthiness)
4. Airworthiness Advisory Circulars
5. Human Factor Guidelines Doc 9806
Paper II
1. Civil Aircraft Inspection Procedures (CAP 459-Part I, Basic)
2. Airframe & Powerplant Mechanics (General Handbook EA-AC 65-9A) FAA
3. Shop Theory by James Anderson Earl E. Tatro
4. Electrical Technology by B L Threja
5. Aircraft Materials & Processes by Titterton
6. Machine Drawing by AC Parkinsons
7. Advanced Composites (EA-358) by Cindy Foreman
8. Digital Fundamentals by Malvino and Leech
9. Mechanics of Flight by A C Karmode
10. Standard Aircraft Handbook -Larry Reithmaier
11. Basic electricity for A & P Mechanic by Dale Crane
12. Basic Electronics-Bemard Grob
13. Basic Electronics and radio Installation by Dale crane
14. Electronics and communication System by George kennedy
15. Principles of Electronics by V K Mehta
16. Integrated Electronics by Millman and Halkias
17. Aviation Electronics by Keith W Bose
18. Aviation Maintenance Technician Hand book by FAA
PAPER III – AIRFRAME : (LIGHT AEROPLANES)
1. Airframe and Powerplant Mechanics (AC 65-15A)-Airframe Hand Book FAA
2. Aircraft Materials and Processes by George F.Titterton.
3. Mechanics of Flight By -A.C.Kermode
4. Civil Aircraft Inspection Procedure (CAP 459) Part II Aircraft
5. Aircraft Maintenance and Repair By Kroes, Watkin and Delp
6. Acceptable Methods, Techniques and practices (FAA)-EA-AC 43.13-1 A&2A
7. Aircraft Construction Repair and Inspection by Joe Christy
8. Light Aircraft Maintenance-byJ.E.Heywood
9. Light Aircraft Inspection-by J.E.Heywood
10. Aircraft Electrical Systems-by E.H.J.Pallet
11. Aircraft Instruments-by E.H.J.Pallet
12. Automatic Flight Controls-by E.H.J. Pallet
13. Advanced Composites (EA-358) -by Cindy Foreman
14. Airframe and Powerplant Mechanics (EA-AC 65-9A)-General Hand Book
15. Aircraft repair Manual by Larry Reithmaier
16. Aviation Maintenance Technician Hand book by FAA
PAPER III – AIRFRAME : (HELICOPTERS)
1. The helicopter and How to Fly-by John Fay
2. Basic helicopter maintenance-by Joseph Schafer
3. Basic Helicopter Hand Book-by FAA EA AC 61-13B
4. Helicopter Aerodynamics-by R.W.Prouty
5. Aircraft Materials and Processes by George F. Titterton
6. Advanced Composites(EA-358)-by Cindy Foreman
7. Civil Aircraft Inspection Procedure (CAP 459) Part II Aircraft.
8. Rotary Wing Aerodynamics-by W.Z.Stepniewski
9. Basic Helicopter Aerodynamics by J.Seddon
10. Aircraft Electrical System-by E.H.J.Pallett
11. Aircraft Instruments-by E.H.J.Pallett
12. Automatic Flight Control-by E.H.J.Pallett
PAPER III – AIRFRAME : (HEAVY AEROPLANE)
1. Airframe and Powerplant Mechanics (AC 65-15A) -Airframe Hand Book FAA
2. Civil Aircraft Inspection Procedure (CAP 459) Part II Aircraft
3. Advanced Composites(EA-358)-By Cindy Foreman
4. A & P technician Air Frame Text Book by Jeppesen
5. Aircraft Repair Manual (FAA-AC-43.13)-By Larry Reithmaier
6. Aerodynamics-By Clancey
7. Aircraft Construction Repair and Inspection-By Joe Christy
8 Aviation Maintenance Technician Hand book by FAA
9. Aircraft Materials and Processes-by George F.Titterton
10. Mechanics of Flight-by A.C.Kermode
11. Hydaulic Servo Systems by M. GUILLON:
12. Aircraft Instruments-by E.H.J.Pallett
PAPER III – POWER PLANT : (PISTON ENGINES)
1. Airframe and Powerplant Mechanics (EA-AC 65-12A) -Power Plant Hand FAA
2. Power Plant-By Bent and Mckinley
3. Civil Aircraft Inspection Procedure (CAP 459) Part II Aircraft
4. Aircraft Propeller and Controls-by Frank Delp
5. Powerplant Section Text book- (EA-ITP-P)
6. Aircraft Piston Engines-By Herschel Smith
7. Aviation Maintenance Technician Series by Dale Crane
.
PAPER III – POWER PLANT (TURBINE ENGINES)
1. Aircraft Gas Turbine Tecnology by IRWINE TREAGER
2. The Jet Engine’ by ROLLS ROYCE
3. Power plant Section Text book- (EA-ITP-P)
4. Aviation Maintenance Technician Series by Dale Crane
5. ‘Jet Aircraft power Systems’ by JACK V. CASAMASSA and RALPH D.BENT
6. ‘Gas Turbine Engines’ by Turbomeca, Bordes,France.
7. ‘Encyclopaedia for Aviation Tecnologies’ by DALE CRANE & NEAR CARLSON :
8. ‘Hydaulic Servo Systems’ by M.GUILLON
9. ‘Introduction to Flight by JOHN ANDERSON:
10. ‘Civil Aircraft Inspection Procedure (CAP459) Part- II Aircraft
11. ‘Aircraft Power Plants by M.J.KROES, T.W.Wild, R.D.Bent and J.L.McKINLEY;
12. ‘Aircraft Propellers and Controls’ by FRANK DELP :
PAPER III – ELECTRICAL SYSTEM
1. Electrical Technology-by B.L.Theraja
2. Aircraft Electrical System-by E.H.J.Pallett
3. Basic Electronics-Bemard Grob
4. Digital Computer Fundamentals-by Malvino
5. Micro Electronics Aircraft System- by E.H.J.Pallett
6. Basic Electricity-by Dale Crane
7. Avionics Systems operation & Maintenance by James W Wasson
8. Principles of Servo mechanism-by A Typers & R.B.Miles
9. Aircraft Electricity and electronics-by Bent Mekinley and also by
Eismin/Bent Mekinley
10. Civil Aircraft Inspection Procedure( CAP 459) -Part II Aircraft
11. Integrated Electronics-Millman and Halkias
12. Principles of Electronics by V K Mehta
13. Electrical & Electronics Technology by Edward Hughes
14. Manual of Avionics by Brain Kendel
15. Aircraft Repair Manual (FAA-AC-43.13)-By Larry Reithmaier
16. Aircraft Electrical Systems by J E Bygate
PAPER III INSTRUMENT SYSTEM
1. Aircraft Instruments-by E.H.J.Pallett
2. Automatic Flight Control-by E.H.J.Pallett
3. Digital Principles and Applications- by Malvino and Leech
4. Basic Electronic -by Bemard Grob
5. Aircraft Instruments-by C.A.Williams
6. Integrated Electronic-Millman and Halkias
7. Aircraft Engineers hand Book No. 4 Instruments -by R.W.Sloley and W.H.Coulthard
8. Civil Aircraft Inspection Procedure(CAP 459)-Part II Aircraft
9. Electrical Technology-by B.L.Theraja
10. The Mechanism of Inertial Position and Heading Indication by Winston
Merkey John Hovorka
11. Principles of Servomechanism-by A Typers and R.B.Miles
12.AircraftOxygenSystem byRobert Scheppler and Dale Crane
13. Aircraft Repair Manual (FAA-AC-43.13)-By Larry Reithmaier
14. Manual of Avionics by Brain Kendel
15. Avionics Fundamental by Jeppesen
16 Aircraft Electricity & Electronics By Eismin
17 Avionics Systems operation & Maintenance by James W Wassen
18. Principles of Electronics by V K Mehta
PAPER III – RADIO COMMUNICATION AND NAVIGATION SYSTEMS
1. Aircraft Radio System-by J.Powell
2. Electronic Communication System by George Kennedy
3. Integrated Electronics-Millman and Halkias
4. Digital Fundamentals-By Malvino and Leech
5. Avionics navigation systems By kayton & Fried
6. Manual of Avionics -by Brian Kendal
7. Microelectronics in Aircraft Systems-by E.H.J.Pallett
8. Radio navigation system by Borje forssell
9. Basic electronics and radio Installation By Dale Crane
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Sandeep kumar
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January 16, 2017
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B737NG operating temperatures
Question again out of the field of operation:
An aircraft requested a descent due to low SAT/OAT of – 70°C, is there such a limit on the B737NG?
It looks that we know the answer related to the minimum FUEL temperature in the tank (#1). For takeoff and in flight this is the highest of -43°C, or 3°C above the freezing level of the fuel in the tanks.
Fuel freezing level temperature specifications are:
– JET A1 (JP1) _ freezing point – 47°C
– JET A _ freezing point – 40°C
– JP-5 _ freezing point – 46°C
– JP-8 _ freezing point – 47°C
Any fuel ice preventing additive does not change the minimum fuel tank temperature limit and (just as a guideline), fuel cools depending on fuel quantity and OAT about 3°C/hr.
The actual answer to the question relates to the aircrafts operating OAT’s which can be found on the ENVIRONMENTAL ENVELOPE diagram in the B737NG AFM.
I’ve highlighted the in flight minimum and maximum OAT limits, and also the takeoff and landing OAT limits can be determined to the current PA, and ISA deviations.
Takeoff and landing limits are bounded at sea level and with standard day conditions from:
– Lower OAT limit at – 54°C
– Upper OAT limit to + 54°C until + 39,4°C at 8.400 feet PA. (maximum T/O and LND field elevation)
In flight the lower limit at standard day conditions depends on PA, and varies from:
– Lower OAT limit at 0 ft PA, – 62°C
– Lower OAT limit at FL 410, – 73,2°C
(mind ISA adjustments)
What is a DRY BAY area in A320??
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the dry bay on any acft is an area above the wing mounted engine that doesn't have fuel.
Sandeep kumar
posted a blog.
November 3, 2016
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Fuel boost pumps
Fuel boost pumps are designed as a dual pump unit that scavenges fuel by use of an inducer, and pressurizes fuel by an impeller type pump. During operation the pump units are self cooled and lubricated by fuel flowing through the assembly.
Each main tank (#1/Left and #2/Right) has a FWD and AFT fuel boost pump supplying pressurized fuel to its respective engine, or to the fuel supply manifold for APU and/or X-feeding. These 115 VAC electrical fuel boost pumps produce a flow of ± 9.000 kg/h with a pressure of more than 10 PSI. The boost pumps LOW PRESSURE light illuminates when pump pressure drops below 6 PSI. A LOW PRESSURE light on one side will not straight away trigger the MASTER CAUTION circuit as there is an electrical redundancy on that side. Of course it does illuminate on RECALL, or when both boost pumps on one side produce low or no pressure.
A discharge check valve prevents fuel flow from the engine feed manifold through the pump preventing fuel transfer into that respective tank. A bypass valve allows a secondary fuel flow path to the engine when the boost pump is inoperative, providing a suction fuel feed capability by negative fuel pressure created by operation of the engine fuel pump.
The center tank has two fuel boost pumps which are connecting to the left-, and right side of the fuel supply manifold . These 115 VAC fuel boost pumps produce a flow of ± 12.700 kg/h with a pressure of 23 psi and higher.
A LOW PRESSURE light illuminates when the center tank boost pump switch is ON, and that boost pump output pressure drops below 22 PSI. The latest modification also triggers the MASTER CAUTION light with the respective annunciator on a single center tank boost pump LOW PRESSURE indication. Most of the current used center tank boost pumps are provided with an automatic shut-off when low pressure is sensed for 15 seconds. After an auto shut-off, it is possible to reset the circuit by selecting the respective switch to OFF and back to ON. When the fuel LOW PRESSURE light illuminates, there is a 10 second delay before the MASTER CAUTION is triggered.
Important to know that the center tank boost pump is NOT equipped with a bypass valve so it is not possible to suction feed from the center tank. When both pumps fail and there is fuel in the center tank you have to consider this as unusable fuel that needs to be added up to the ZFW.
The FCOM requires that the flight deck needs to be occupied when a center tank boost pump is operating related to the worst case, that a non modified center tank boost pump is installed without the auto-shutdown feature.
Due to the position of the center boost pumps scavenge pickup, it is possible that the LOW PRESSURE light flickers in a nose up attitude when there is low quantity in the center tank after takeoff. The FCOM states that if the quantity is below 453 Kgs, to switch OFF the center boost pumps until level flight.
When the center tank is empty and the LOW PRESSURE light flickers with intermittent fuel pick-up by the pump, it may take up to 5 minutes to illuminate the associated MASTER CAUTION annunciator.
Electrical power for the boost pumps comes from:
115 VAC XFR bus 1
– 1 FWD boost pump
– 2 AFT boost pump
– Left Center boost pump
115 VAC XFR bus 2
– 1 AFT boost pump
– 2 FWD boost pump
– Right Center boost pump
The circuit breakers for the pumps are not accessible as they are located on the Power Distribution Panel (P-92) in the E & E bay. (see Electrical Supplement)
this is the 737 system.... the larger boeing acft use an override boost pump for the center wing tanks. these are higher volume pumps that will overtake the pressure of the main tank boost pumps. you want to burn the center tank first. almost all acft also have a scavenge pump in the center ta... View More
Sandeep kumar
posted a thread.
Airbus Sharklet - EIS check list presentation
Airbus Sharklet - EIS check list presentation
Airbus Sharklet - EIS check list presentation -Customers - v6 - ref doc _ME1271940_v1.pdf
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