TRAINING NEEDS ANALYSIS COURSE SYLLABUS & CONTENT
|
|
- Melinda Smith
- 6 years ago
- Views:
Transcription
1 TRAINING NEEDS ANALYSIS COURSE SYLLABUS & CONTENT Course Title: BOEING 787 GENERAL FAMILIARISATION FOUNDATION Mechanical (Electrical Power / Airframe / Powerplant / Avionics) General Standard This syllabus has been compiled in the sequence, which will normally be used for instruction. However, it may be necessary to vary this sequence from time to time in order to suit particular course planning requirements. Aircraft visits will occur during the course ideally at the times stated but more reasonably as aircraft are available. All visits are recorded on MON/PROC/138 Form 11. The course is designed for aircraft maintenance engineers to meet the standard of knowledge required for approval and licensing purposes. The course is based on the Boeing technical training requirement for entry on to a Boeing 787 B1/B2 line and base maintenance course, that the students are given a Foundation in B787 systems. The initial entry standard for training is normally holders of the appropriate PART 66 B1/2 or BCAR Section L Aircraft Maintenance Licences. In any case the student should be capable of full comprehension of the technical content. The course content and levels are to Part-66 Appendix II. Course Objective To provide a General Foundation and understanding with an introduction to the new technology of the B787 aircraft and its systems. On completion of the course the student will have sufficient knowledge to enable him/her to satisfactorily gain entry to the Boeing 787 B1/B2 Part 147 type approval course, subject to all other EASA / UK CAA conditions and company requirements being satisfied. Course Duration 30 hrs (5 6hrs per day) Reference Material Manufacturers training material, maintenance, overhaul and repair manuals relevant to type. Service Bulletins, modification and newsletters. Examinations Certification There are no examination requirements for this course. A certificate will be issued at the end of each course to each student who has satisfactorily completed the course. Monarch Aircraft Engineering Ltd. Page 1 of 15 FOUNDATION GEN FAM TNA 14/10/2011
2 Hours of Tuition Monday To Friday, Six Hours Instruction Per Day. 08:30 10:00 Period 1 10:00 10:15 Morning Break 10:15 11:45 Period 2 11:45 12:30 Lunch 12:30 14:00 Period 3 14:00 14:15 Afternoon Break 14:15 15:45 Period 4 Monarch Aircraft Engineering Ltd. Page 2 of 15 FOUNDATION GEN FAM TNA 14/10/2011
3 BOEING 787 FOUNDATION AND GENERAL FAMILIARISATION COURSE (Electrical Power / Airframe / Powerplant/ Avionics ) Weekly Programme Week One Day Period 1 Subject Period 2 Subject Period 3 Subject Period 4 Subject 1 Introduction & Aircraft General Structures Common Core Systems Crew Alerting & Displays Doors Windows Core Information System Central Maintenance Computing Function 2 Electrical Systems Crew Information CIS Maintenance Laptop Data Management Indicating and Recording Oxygen Ice and Rain 3 Hydraulics Landing Gear & Brakes Flight Controls Fire Protection 4 Auto Flight Communication Navigation Lights Cabin Core Systems Water Waste 5 Air Conditioning Fuel Nitrogen Generation system APU Engine (GENX) Monarch Aircraft Engineering Ltd. Page 3 of 15 FOUNDATION GEN FAM TNA 14/10/2011
4 BOEING 787 FOUNDATION AND GENERAL FAMILIARISATION COURSE (Electrical Power / Airframe / Powerplant/ Avionics) SYLLABUS DAY ONE General Introduction & Manuals Introduction to the B787 including the following sub topics: INTRODUCTION & MANUALS a) Training Philosophy b) Boeing Learning Management System c) Electronic Notes and Classroom d) Introduction to CBT e) The Maintenance Toolbox f) Desk Top Simulation ATA 07 and 09 Ground Handling a) Structural Philosophy b) Dimensions and Areas c) Equipment Bays d) Flight Deck and Flight Deck Panels e) Aircraft Jacking Points and Procedures f) Towing and Taxiing ATA 12 Servicing a) Ground Servicing ATA 50 SERIES LEVEL 1 General description of the Airframe Structure including, construction and maintenance practices. To include the following sub topics: Structure 50 Series a) General Structure b) Composite Material Usage c) Fuselage Construction and Station Numbering d) Wing Structure and Station Numbering e) Pylons/Nacelles and Attachments f) Wing Control Surfaces g) Horizontal Stabiliser h) Elevators i) Vertical Stabiliser j) Rudder k) Composite repair l) Current Return Network (CRN) ATA LEVEL 1 General description of the Common Core System To include the following sub topics: Common Core Systems (CCS) Time 1:00 hrs a) Introduction b) System Architecture Description c) System Components d) Common Computing Resource (CCR) e) Common Data Network (CDN) ATA LEVEL 1 General description of the Caution and Warning Systems including, the following sub topics: Master Warn and Caution a) Introduction b) System Architecture Description Time 0:15 hrs Monarch Aircraft Engineering Ltd. Page 4 of 15 FOUNDATION GEN FAM TNA 14/10/2011
5 ATA LEVEL 1 General description of the Display and Crew alerting systems including, maintenance practices and trouble-shooting. To include the following sub topics: Primary Display System (PDS) a) Introduction b) System Architecture Description c) System Components d) Head Down displays e) Head Up Displays f) Maintenance pages ATA 52 LEVEL 1 Detailed description of the Doors including, the following sub topics: Doors a) Doors Introduction b) General Location and Identification c) Passenger / Crew Entry Doors d) Fwd & Aft Cargo Doors e) Miscellaneous Service Doors f) Flight Compartment Door ATA 56 LEVEL 1 General description of the Windows, to include the following sub topics: Windows Time 0:15 hrs a) Flight Compartment Windows b) Passenger Compartment Windows c) Electrically Dimmable windows control d) Door-Mounted Windows ATA LEVEL 1 General Introduction and description of the Core Network System including, the following sub topics: Core Network System a) Introduction b) System Architecture Description c) System Components Time 0:45 hrs ATA LEVEL 1 General introduction and description of the Computer Maintenance system to include the following sub topics: Central Maintenance Computing Function (CMCF) Time 0:45 hrs a) Introduction b) System Architecture Description c) Electronic Flight Bag d) Maintenance laptop Monarch Aircraft Engineering Ltd. Page 5 of 15 FOUNDATION GEN FAM TNA 14/10/2011
6 DAY TWO ATA 24 LEVEL 3 Detailed description of the Electrical Power Systems including, maintenance practices and operation including trouble-shooting. To include the following sub topics: Electrical Power a) Electrical Power Introduction b) Electrical Power And Control c) Distribution General Description d) Electrical Component Locations e) Electrical Power - Operation f) Variable Frequency Starter Gen (VFSG) g) Generator Drive - Servicing h) APU Starter Generator i) 235 V AC Generation Introduction j) Generator Control Unit (GCU) k) Electrical Load Control Units ELCU l) APU Generator Control Unit (AGCU) m) AGCU APB Control n) Hi Voltage DC System General Description o) Common Motor Start Control Unit (CMSC) p) Electric Brake Power Supply Units (EBPSU) q) Auto Transformer Rectifier Unit (ATRU) r) Bus Power Control Unit (BPCU) s) External Power Introduction t) Ram Air Turbine (RAT) u) Main Battery v) APU Battery w) External Power Supply Indication x) Circuit Breaker Indication and Control (CBIC) y) Electronic Systems Indication and Control (ESIC) z) Towing Power Time 1:30 hrs ATA LEVEL 1 General introduction and description of the Computer Maintenance Crew Information Systems to include the following sub topics: Crew Information System (CIS) a) Introduction b) System Architecture Description c) Terminal Wireless d) Data Networks e) Wired Connection f) Electronic Flight Bag g) MCDF functions h) Maintenance laptop i) Airplane Fault Isolation Time 0:45 hrs ATA 45 LEVEL 1 General introduction and description of the Data Management system to include the following sub topics: Data Management e) Introduction f) System Architecture Description g) Onboard Data Load Function (ODLF) h) Aircraft Condition Monitoring (ACMF) i) Electronic Flight Bag Time 0:45 hrs Monarch Aircraft Engineering Ltd. Page 6 of 15 FOUNDATION GEN FAM TNA 14/10/2011
7 ATA 31 LEVEL 1 General description of the Indicating and Recording Systems. To include the following sub topics: Indicating and Recording Systems Recorders a) DFDR/ACMS flight Data Recorder System b) FDRS - General Description c) Flight Deck Printer d) Video Surveillance Time 1:00 hours ATA 35 LEVEL 1 Detailed description of the Oxygen Systems including, maintenance practices, operation and trouble-shooting. To include the following sub topics: Oxygen a) General Description b) Control Panels c) Crew System Presentation d) Crew System Control and Indication e) Crew System Components f) Passenger System - General g) Passenger System Control and Indication h) Passenger System Components i) Portable Oxygen Equipment ATA 30 LEVEL 1 Detailed description of the Ice and Rain Protection Systems including, maintenance practices, operation and trouble-shooting. To include the following sub topics: Ice & Rain Protection Time 1:30 hrs a) Ice and Rain Protection Introduction b) Primary Ice detection system (PIDS) c) Engine Anti Ice Protection (EAI) d) Wing Ice Protection System (WIPS) e) Cabin Air Compressor Inlet Ice Protection (CIPS) f) Window heat g) Washer wiper system DAY THREE ATA 29 LEVEL 1 General description of the Hydraulic Power Systems including, maintenance practices, operation and trouble-shooting. To include the following sub topics: Hydraulic Power a) Hydraulic Schematic System diagram symbols b) Hydraulic Power c) Hydraulic Power Distribution d) Controls and Indications e) Panel Description f) Hydraulic Component Locations g) Engine-Driven Pump Hydraulic Control h) Engine-Driven Pump Electrical Control i) Electric Motor-Driven Pump (EMDP) j) Ram Air Turbine (RAT) Time 1:30 hrs Monarch Aircraft Engineering Ltd. Page 7 of 15 FOUNDATION GEN FAM TNA 14/10/2011
8 ATA 32 LEVEL 1 General description of the Landing Gear Systems. To include the following sub topics: Landing Gear Time 1:30 hrs a) Landing Gear -- General Description a) Proximity Sensor Electronic b) Main Landing Gear c) Landing Gear - Downlock Pins d) Main Landing Gear and Doors e) Nose Landing Gear f) Nose Landing Gear and Doors g) Landing Gear - Components h) Landing Gear - Controls and Indications i) MLG alternate Extension System - Control Mechanism Braking Systems a) Electric Brake System Description b) Brake System Components c) Controls and Indications d) Antiskid/Autobrake System e) Parking Brake System f) Brake system sensing g) Towing Power Nose wheel Steering a) Nose wheel steering. b) Electronic control. ATA 27 LEVEL 1 General description of the Flight Controls Systems including, operation. To include the following sub topics: Flight Controls a) Flight Controls - General Description. b) Flight Control Electronics (FCE) c) Primary Flight Control Function (PFCF) d) Flight Controls Hydraulic e) Controls and Indications f) Maintenance pages g) Rigging Ailerons a) Aileron and Aileron Trim Control System b) Flaperons Spoiler Systems a) Flight Spoiler Control System - General Description b) Speedbrake Operation c) Ground Spoiler d) Auto Speedbrake Rudder a) Rudder and Rudder Trim Control System b) Rudder Pressure Reducer c) Gust suppression system Elevator a) Elevator and Tab Control System Introduction b) Elevator System Components Overview a) Stall Warning System c) Elevator Feel Computer d) Elevator Feel and Centring system e) Elevator backdrive Horizontal Stabiliser a) Horizontal Stabilizer Trim Control System Introduction Time 2:00 hrs Monarch Aircraft Engineering Ltd. Page 8 of 15 FOUNDATION GEN FAM TNA 14/10/2011
9 b) Electric Motor EMCU c) Nose gear pressure transducers d) Stab Trim Stall Warning System b) SWS -- Control Column Shaker c) SWS -- Stall Warning Test Panel d) SWS - SMYD - Stall Management Yaw Damper e) Sws - Stall Management Yaw Damper f) CPC g) SWS - SMYD - Analog Interfaces - SMYD 1 h) SWS - SMYD - Digital Interface i) SWS - SMYD - BITE j) SWS - WSMYD BITE - Ground Tests High Lift Function a) High Lift Function (HLF) b) HLF modes c) TE Flap System - Controls and Indications d) TE Flap System Component Location e) Variable Camber trim Unit (VCTU) f) Alternate Flap Operation Leading Edge Flap Lift Augmentation a) LE Flap and Slat Control System Controls b) LE Flap and Slat Control System -- Indications c) LE Flap and Slat Control System -- Component Location ATA 26 LEVEL 1 General description of the Fire Protection Systems including the following sub topics: Fire Protection Time 1:00 hours a) Fire Protection - Fire Detection - Fire Alarms Engine Fire Protection a) Engine Fire Detectors b) Fire Protection -- Fire Extinguishing c) Engine Fire Extinguishing APU Fire Protection a) APU Fire Detection b) Overheat/Fire Test c) APU Ground Control Panel P40 Cargo Fire Protection a) Cargo Compartment Smoke Detection Lower b) Cargo Compartment Fire Extinguishing DAY FOUR ATA 22 LEVEL 1 General Description and operation of Automatic Flight Control System, Displays.To include the following sub topics: Automatic Pilot Flight Director System Time 1:30 hours General a) Control systems backdrive b) ATC uplink c) Autopilot Indications d) Flight Director Indications Thrust Management a) Locations b) Interface schematic c) Autothrottle Monarch Aircraft Engineering Ltd. Page 9 of 15 FOUNDATION GEN FAM TNA 14/10/2011
10 d) TMF input e) MCP operation f) PFD and EICAS Displays ATA 23 LEVEL 1 Description and Operation of Communications System including Trouble-shooting limited to the use of BITE systems. To include the following sub topics: Communications Emergency Locator Transmitter a) ELT - Component Location b) ELT - Interface c) ELT - Control Panel d) ELT - Transmitter e) ELT - Antenna f) ELT - Functional Description Data Comm Management Function (DCMF) a) General Description b) Operation Flight Interphone a) General b) Operation c) Audio Control Panel d) Interfaces e) Funct. Description Service Interphone a) Ground Crew Call System Introduction b) Ext. Comp. Location c) Flight Comp. Locations d) Interfaces Audio Gateway Unit (AGU) e) Flight Crew Call / Cabin Interphone VHF Communication a) Very High Frequency System b) VHF- Antenna Component Locations c) VHF - VHF 1 / 2 Transceiver Interfaces d) VHF-Tuning Control Panel (TCP) e) Audio Gateway Unit (AGU) f) VHF Communication System - Vhf Antenna g) VHF Communication System - Operation Selcal a) General SELCAL - Functional Description b) Selective Calling System - Introduction c) SELCAL - Flight Comp. Location HF Communication General a) High Frequency Communication b) HF - General Description c) HF - Flight Compartment Locations d) HF - Transceiver Location e) HF - Antenna Component Location f) HF - Interfaces g) HF - Control Panel Satcom a) General Functional description b) Sattellite High Gain antenna c) Diplex Module d) Operation Ground Crew Call a) General Functional description b) Crew Call Horn c) Operation Manual d) Operation Automatic. Time 1:30 hours Monarch Aircraft Engineering Ltd. Page 10 of 15 FOUNDATION GEN FAM TNA 14/10/2011
11 ATA 34 LEVEL 1 General Description and operation of Navigation system and Displays including Trouble- Shooting limited to the use of BITE systems. To include the following sub topics: Navigation Integrated Surveillance System a) General Description b) TCAS c) Weather radar Air Data Reference System a) Standby Indicators b) Description c) Air Data System Components d) Description e) Air Data SystemTest Earth Reference System a) Purpose b) General Description c) Attitude Heading Reference Units (AHRU) d) Inertial reference Unit (IRUS) e) ERS alignment f) Indications on PFD and ND Integrated Navigation Radio a) General b) GNSS c) ILS d) VOR e) GLS f) Components Locations g) Operation Integrated Standby Flight Display a) Purpose b) General Description Low Range Radio Altimeter a) General Description b) RA / DH - Control and Indication c) Operation d) Bite DME a) General Description b) Control and Indication c) Component Description d) DME Operation, Description ADF a) Control and Indication b) Components c) ADF Operation Flight Management Function (FMF) a) General b) FMS Components c) FMS Schematic d) LNAV e) VNAV Time 2:00 hours ATA 33 LEVEL 1 General description of the Lighting System including,, operation. To include the following sub topics: Lights a) Lights General Description b) Flight Compartment Lighting Time 1:00 hrs Monarch Aircraft Engineering Ltd. Page 11 of 15 FOUNDATION GEN FAM TNA 14/10/2011
12 c) Passenger Compartment Lighting d) Cargo and Service Compartment Lighting e) Exterior Lighting f) HID Lighting g) Emergency Lighting Power Supplies h) Anti Collision lights i) Runway Turnoff and landing j) Position lights ATA LEVEL 1 General description of the Cabin Core system including, operation to include the following sub topics: Cabin Core Systems a) General Introduction b) Cabin Services Systems Controllers (CSSC) c) Cabin Zone Units d) Cabin attendants Panel e) Operation Time 1:00 hrs ATA 38 LEVEL 1 General description of the Water and Waste Systems including, maintenance practices, operation and trouble-shooting. To include the following sub topics: Water & Waste a) Potable Water b) Passenger Water System c) Water Service Panel d) Servicing Procedure e) Ultra Violet water treatment system f) Water Tank Air Pressurization g) Potable Water Tank - Pressurization Components h) Water Pressurisation - Electrical i) Water/Waste -- Toilet System j) Vacuum Toilet System k) Toilet System - Toilet Service Panel l) Toilet Flush Motor/Pump-Filter Assembly Function m) Vacuum Blowers DAY FIVE ATA 21 LEVEL 3 General description of the Air Conditioning and Pressurisation Systems including, maintenance practices, operation and trouble-shooting. To include the following sub topics: Air Conditioning / Pressurisation a) Cabin Air Compressors (CACs) b) Pack Valve Operation Operational Logic c) Pack Flow Operation d) Cooling e) Lower recirculation f) Air Cycle Machine g) Temperature Control Operation and Logic h) Pack/Zone Temperature Control i) Supplemental heating j) Fluid Cooling Systems (PECS) k) Equipment Cooling Systems l) Integrated Cooling system (ICS) Time 2:00 hrs Monarch Aircraft Engineering Ltd. Page 12 of 15 FOUNDATION GEN FAM TNA 14/10/2011
13 Pressurisation Digital System a) Digital Pressure Control b) Automatic Pressurization Control c) Manual Pressurization Control d) Data Input Interface e) Outflow Valve Interface f) Fwd and Aft Outflow Valve Assembly g) Positive Pressure Relief Valve h) Negative Pressure Relief Valve ATA 28 LEVEL 3 Detailed description of the Airframe Fuel Systems including, maintenance practices, operation and trouble-shooting. To include the following sub topics: Airframe Fuel System a) Introduction into System b) Fuel General Description and Operation c) Fuel - Storage - Integral Fuel Tanks d) Fuel -- Storage - Wing Fuel Tank Access Panels e) Fuel Tank Vent Operation f) Pressure Fuelling System g) Fuelling Operation h) Engine Fuel Feed System i) APU DC Boost Pump j) Main and Centre Tank Boost Pump Power Control k) Defueling l) Fuel Tank Scavenge System m) Fuel Quantity Indicating System - Operation n) Fuel Indication - Tank and Compensator Units o) Fuel Balance System Time 1:00 hrs ATA 49 LEVEL 3 Detailed description of the Auxiliary Power Unit(s) used on this aircraft including, construction, maintenance practices, operation and trouble-shooting. To include the following sub topics. Auxiliary Power Unit (APU) a) Introduction b) Auxiliary Power Unit General Description c) Auxiliary Power Unit (Allied Signal / GTCP) d) Airborne Auxiliary Power Controls e) APU Indications f) APU Engine g) Fuel Control Unit h) APU Fuel System i) Auxiliary Power Unit -- Ignition And Start System j) APU Ignition And Start System - SPU And SCU k) APU Starter-Generator l) Ignition System - General Description m) APU Controls - Electronic Control Unit - Inputs n) APU Indicating System o) APU Indicating System - Data Memory Module (DMM) p) APU Exhaust System - Exhaust Duct q) APU Exhaust System - Aft Fairing r) APU Lubrication System - Lube Module - Functional Description Monarch Aircraft Engineering Ltd. Page 13 of 15 FOUNDATION GEN FAM TNA 14/10/2011
14 ATA 71 LEVEL 3 General description of the Power Plant, To include the following sub topics: Power Plant & Installation a) General Introduction & Description of Engine b) Engine Station Numbering c) Airflow Paths & Stations d) Engine Cowlings & Opening/Closing Procedures e) Cowling Specific Features ATA 72 LEVEL 3 General description of the Engine including, construction,. To include the following sub topics: Engine Construction a) Engine -- General Description b) Engine Specification and Characteristics c) Engine -- General Dimensions d) Engine -- Accessory Drive Gearbox ATA 77 LEVEL 3 General description of the Engine Indicating Systems. To include the following sub topics: Engine Indicating a) Engine Indicating b) Fan Trim Balance ATA 76 LEVEL 3 General description of the Engine Controls. To include the following sub topics: Engine Controls and Power Management a) Engine Control System b) Forward Thrust Control System c) Reverse Thrust Control System d) Start Control System e) Engine Control Components ATA 73 LEVEL 3 Detailed description of the Engine Fuel and Control Systems,. To include the following sub topics: Engine Fuel & Control a) Engine Fuel And Control - b) Engine Fuel And Control - Distribution - Component Location c) Fuel Manifolds And Fuel Nozzles d) Engine Fuel And Control - Engine Control e) Engine Control - Interfaces f) EEC Modes g) Fuel Indicating - Introduction ATA 74 LEVEL 3 Detailed description of the Start and Ignition Systems including, maintenance practices, operation and trouble-shooting. Ignition System a) Engine Ignition -- Introduction b) Ignition System Monarch Aircraft Engineering Ltd. Page 14 of 15 FOUNDATION GEN FAM TNA 14/10/2011
15 ATA 80 LEVEL 3 General description of the Start and Ignition Systems including, maintenance practices, operation and trouble-shooting. Start a) Introduction into System b) Flight Deck Controls & Indications c) Electric Start ATA 75 LEVEL 3 General description of the Air Systems, To include the following sub topics. Air System a) Engine Air Systems Introduction b) Compressor Control c) Forward and Aft Bearing Sump Pressurizing d) Turbine Clearance Control e) Compressor Control ATA 79 LEVEL 3 General description of the Oil Systems including, To include the following sub topics: Oil System a) Introduction to System b) Oil Tank Mounting & Other Features c) Lube & Scavenge Pump d) Pressure Filter e) DMS f) Fuel/Oil Heat Exchanger ATA 78 LEVEL 3 Detailed description of the Exhaust Systems. To include the following sub topics: Exhaust & Thrust Reverser a) Introduction into Thrust Reverser System b) Thrust Reverser System Description c) Thrust Reverser Construction & Component Location d) Directional Control e) Drive System Installation & Maintenance Practices f) Deploy and Stow Operation & Control g) Cowl Opening & Systems Monarch Aircraft Engineering Ltd. Page 15 of 15 FOUNDATION GEN FAM TNA 14/10/2011
Cessna 550/551/560 (PWC JT15D) Initial Aircraft Type Training Course MAINTENANCE INITIAL
Cessna 550/551/560 (PWC JT15D) Initial Aircraft Type Training Course CONTENTS INTRODUCTION 5 COURSE DESCRIPTION 6 COURSE OBJECTIVES 7 COURSE MATERIAL 8 TIMETABLE WEEK ONE 9 TIMETABLE WEEK TWO 10 LEVEL
More informationLAD Inc. Beechcraft King Air 200 Series Technical Ground School Syllabus Material Covered
Topic Introduction Description Structures ATA 05 Technical Publications ATA 05 Aircraft Handling ATA 12 LAD Inc. Beechcraft King Air 200 Series Technical Ground School Syllabus Material Covered Course
More informationAIRPLANE GENERAL Exterior REV 3, May 03/05
Vol. 1 01--20--1 AIRPLANE GENERAL Exterior REV 3, May 03/05 24 ft 1 in (7.34 m) 5ft1in(1.55m) 10 ft 7 in (3.23 m) 6ft4in (1.93 m) 81 ft 6 in (24.85 m) 9ft6in(2.89m) 8ft10in (2.69 m) 36 ft 4 in (11.07 m)
More informationOVERHEAD PANEL PROCEDURES FLASH CARDS
OVERHEAD PANEL PROCEDURES FLASH CARDS Boeing 737-800 A supplement to the procedures and checklists publication, Flying the Boeing 737-800 NG Greg Whiley Aussie Star Flight Simulation ELECTRICAL POWER UP
More informationAeroplane Aerodynamics and Flight Controls 1 2
11.1 Theory of Flight 11.1.1. Aeroplane Aerodynamics and Flight Controls 1 2 Operation and effect of: roll control: ailerons and spoilers, pitch control: elevators, stabilators, variable incidence stabilisers
More informationOfficial Journal of the European Union L 298/53
16.11.2011 Official Journal of the European Union L 298/53 A B1 B2 B3 10.6 Continuing airworthiness 2 2 2 2 Detailed understanding of Part-21 provisions related to continuing airworthiness. Detailed understanding
More informationMaintenance Practice Training Manual DC9/MD80 PWJT8 DC9/MD80 PWJT8 MAINTENANCE PRACTICE TRAINING MANUAL B1 or B1/B2 LEVEL
aintenance Practice Training anual DC9/D80 PWJT8 DC9/D80 PWJT8 AINTENANCE PRACTICE TRAINING ANUAL B1 or B1/B2 LEVEL DOC.FOR.06 Ed 3 1/32 aintenance Practice Training anual DC9/D80 PWJT8 TRAINEE SURNAE:
More information1. Aircraft General (0 Hours 39 minutes) 2. Doors (0 Hours 33 minutes) 3. EFIS (2 Hours 55 minutes) 4. Exterior Lighting (0 Hours 24 minutes)
Course: CRJ900 (Pilot) Delivery Formats: Web Based or Portable Classroom Number of modules: 26 Estimated Course Time: 36 Hours 16 minutes The following topics are included in this CRJ900 (Pilot) CBT/WBT
More informationPractical experience Group 2 and Group 3 Aircraft, cat. B2: Avionics and Electrical systems.
Practical experience Group 2 and Group 3 Aircraft, cat. B2: Avionics and Electrical systems. This logbook is to be used to record details of B2 experience on Group 2 and Group 3 Aircraft type rating(individual
More informationPOWER ON CHECK LIST COCKPIT PREPARATION
Normal Check List DASH 8-402 1 POWER ON CHECK LIST CIRCUIT BREAKERS... CHECKED BATTERY MASTER... ON BATTERIES... ON MAIN BUS TIE... TIED EXTERNAL POWER... AS REQUIRED APU... AS REQUIRED BATTERIES & BATTERY
More informationCessna Citation XLS - Electrical
GENERAL Electrical power for the Citation XLS comes primarily from DC sources originating with the starter/ generators, the Auxiliary Power Unit (APU) or the battery. A receptacle below the left engine
More informationSUPER KING AIR B200C Registration : PK - YGT Total Time : 9116
CHAPTER 21 1 210101 21,010 AMM 21-10-00 L/H Flow Control Unit 101-380025-21 UNK O/C 9112 2-Oct-14 7333 0 0 0 - - - - - - 2 210106 21,050 L/H Flow Control Pneumostat 101-380013-3 UNK O/C 0 0 0 - - - - -
More informationL 298/70 Official Journal of the European Union
L 298/70 Official Journal of the European Union 16.11.2011 MODULE 12. HELICOPTER AERODYNAMICS, STRUCTURES AND SYSTEMS 12.1 Theory of Flight Rotary Wing Aerodynamics 1 2 Terminology; Effects of gyroscopic
More informationN416WM. Maintenance Due List Sort By Earliest Due Date Include only mandatory service information not yet accomplished. Projected Through:
Phone: FAX: Aircraft Make Gulfstream Aircraft Model GIII Aircraft Serial No. 487 Airworthiness Date 9 Jul 1986 Regulation 91-3 Sort By Earliest Due Date Include only mandatory service information not yet
More information2006 Embraer Legacy 600
PRESENTS 2006 Embraer Legacy 600 Serial Number 14500948 HIGHLIGHTS EASA Certified Engines Covered Under RR Corporate Care Enrolled in Embraer Executive Care Standard Programme Fresh 12 Year Inspection
More informationDoors Four outward-opening cabin doors are provided, two on each side of the fuselage. For use and operation see subsection DOORS.
AIRFRAME AND SYSTEMS Introduction The Fokker 50 is a twin-engined, pressurized, high-wing aircraft, designed for short or medium-haul operations. Principal dimensions and limitations are given in the applicable
More informationAirworthiness Physical Survey Report
M.A Subpart G Approval No: Airworthiness Physical Survey Report UK.MG.0035 Aircraft Type: Registration: MSN: Hours at Survey: Survey Date: Location: Audit Ref: Cycles at Survey: Documentation Review (M.A.710(c)
More informationBALLAST UNIT Ea 5 New REPAIRABLE INDICATOR FLAP POSITION Ea 1 Overhauled ROTABLE
Part Number Description UoM Qty Condition Aircraft type Aircraft type Part Class 05939-108 BALLAST UNIT Ea 5 New REPAIRABLE 07311P000-02 BALLSCREW Ea 1 Overhauled B737-; B737-800 10-60791-13 INDICATOR
More informationARIANA AFGHAN AIRLINES MPD Tally Sheet - Routine Jobs
B737-400 YA-PID 26085 Kabul AFG-PID-26085-1217 MPD (C2-CHECK) 1 of 15 1. 20-020-31-01 B20-20-31-6C 203 204 INSPECT THE CONTROL CABLES FOR BROKEN WIRES AND WEAR IN THE NLG WHEEL WELL. DI 2. 20-020-32-01
More information/200/300/400/500 SERIES FLAMMABLE MATERIAL LOCATIONS
73737-100/200/300/400/500 SERIES FLAMMABLE MATERIAL LOCATIONS (tab) 1 390/492/984 GAL - 1476/1862/3725 L WINGLETS OPTIONAL AUXILIARY FUEL TANK IN LWR AFT CARGO COMPARTMENT VENT SURGE TANK FUEL TANK No.
More informationBombardier Global Express - Hydraulics
INTRODUCTION Hydraulic power is provided by three independent and isolated systems designated 1, 2 and 3 and operate at a nominal pressure of psi. SYSTEM 1 AND 2 Systems 1 and 2 are each powered by an
More information12.1 Theory of Flight Rotary Wing Aerodynamics 1 2
12.1 Theory of Flight Rotary Wing Aerodynamics 1 2 Terminology; Effects of gyroscopic precession; Torque reaction and directional control; Dissymmetry of lift, Blade tip stall; Translating tendency and
More informationPart Number Description QTY UM COND COMPUTER, VHF COMM 1 EA SV DME 1 EA AR NAV/ILS RECEIVER 3 EA AR
064-1005-14 COMPUTER, VHF COMM 1 EA SV 066-1019-01 DME 1 EA AR 066-1149-48 NAV/ILS RECEIVER 3 EA AR 066-50003-0101 TRAFFIC DISPLAY 2 EA AR 071-50001-8102 TCAS ANTENNA 2 EA SV 0856CC-10 PITOT TUBE 2 EA
More information2007 A119 Koala Price: Make an Offer
2007 A119 Koala Price: Make an Offer Aircraft Details Manufacture Date: 2007 Hours: 87hrs Airframe: Aluminium alloy & bonded panel fuselage Semimonocoque aluminium alloy tail boom Skid type landing gear
More informationPreflight Inspection. Table of Contents. Left Main Landing Gear... 2A-15 Left Fuselage... 2A-16. Left Wing Trailing Edge... 2A-13
Preflight Inspection Table of Contents Preflight Inspection Walkaround Path........ 2A-2 Exterior Walkaround Inspection............ 2A-2 Left Forward Fuselage.................. 2A-2 Nose............................
More informationB777. Electrical DO NOT USE FOR FLIGHT
B777 Electrical DO NOT USE FOR FLIGHT 6.10 Electrical-Controls and Indicators Electrical Panel [IFE/PASS SEATS and CABIN/UTILITY switches basic with C/L 350] 1 2 IFE/PASS CABIN/ SEATS UTILITY 3 11 APU
More informationSECTION 2-05 ELECTRICAL
SECTION 2-05 TABLE OF CONTENTS Block General...2-05-05...01 DC System...2-05-05...02 DC System Protection...2-05-05...04 External Power Source...2-05-05...05 Batteries...2-05-05...06 Backup Battery...2-05-05...07
More informationIntroduction. I. Introduction Abbreviations Icon Legend Resources
Introduction Management Reference Guide I. Introduction Abbreviations Icon Legend Resources II. Takeoff Performance Computation Limitation Legend Corrections Maximum Takeoff Performance (Full Thrust Method)
More informationBombardier Challenger Auxiliary Power Unit
GENERAL A Honeywell 36 150(CL) constant-speed gas turbine auxiliary power unit (APU) is installed within a fire-resistant compartment in the aft equipment bay. The APU drives a generator, providing AC
More informationATR OVERHAUL/REPAIR CAPABILITY LIST
OVERHAUL/REPAIR CAPABILITY LIST Effective: 5/2/2018 repairs@usaerospacecorp.com Page 1 of 8 011232 Fan, Recirculation 011232-100 Fan, Recirculation 011232-500 Fan, Recirculation 011260 Fan, Air Extraction
More informationInventory Majestic Jet
Inventory Majestic Jet TO BE SOLD IN BULK Description Transceiver-VHF Comm P/N:822-1114-001 Transceiver-VHF Comm P/N:822-1114-001 Coupler-Mode P/N:792-6255-001 Coupler-Mode P/N:792-6255-001 Computer-Flight
More informationVH-DBT. Maintenance Due List Sort By Earliest Due Date Include only mandatory service information not yet accomplished. Projected Through: 5746.
Phone: FAX: Aircraft Make Gulfstream Aircraft Model GIV-MSG3 Aircraft Serial No. 1363 Airworthiness Date 15 Feb 1999 Regulation 91-4 Sort By Earliest Due Date Include only mandatory service information
More informationAW 169 Commercial in Confidence AW 169 VIP CONFIGURATION Airframe Transmission Drive System and Hydraulic System Electrical Systems
AW 169 VIP Year of Manufacture 2017 Airframe Total Time Brand new Configuration VIP Engines PW210A Availability July 2017 LHD Warranty 3 years / 2000 hours CONFIGURATION Airframe Airframe structure including
More informationP68 Observer 2 STANDARD EQUIPMENT LIST V
P68 Observer 2 STANDARD EQUIPMENT LIST V9.03.12 P68 OBSERVER 2 IMPORTANT NOTE: this document is a general description of the aircraft equipment only. It is not a technical document and is to be used only
More informationCHAPTER 1 AIRCRAFT GENERAL
CHAPTER 1 AIRCRAFT GENERAL INTRODUCTION This manual provides a description of the major airframe and engine systems in the Cessna Citation Mustang (Figure 1-1). This material does not supersede, nor is
More informationATA 49 AUXILIARY POWER UNIT
F900EX EASY 02-49-00 CODDE 1 PAGE 1 / 2 TABLE OF CONTENTS 02-49 02-49-00 TABLE OF CONTENTS 02-49-05 GENERAL Introduction Sources APU location 02-49-10 DESCRIPTION Introduction Description Operating principle
More informationOffers for Sale Q Series: Q400 Aircraft MSN 4064
Offers for Sale Q Series: Q400 Aircraft MSN 4064 TTSN: 25,213 Flight Hours TCSN: 32,085 Flight Cycles Data Date: 20 th May 2018 Expected Availability: October 2018 Page 1 of 11 Date of Manufacture: March
More informationHAB. B-777 AIRPLANE GENERAL, EMER EQUIP, DOORS, WINDOWS
HAB. B-777 AIRPLANE GENERAL, EMER EQUIP, DOORS, WINDOWS 1 What must the aircrew do if using the portable halon fire extinguishers on the flight deck? A) All flight crew members must wear oxygen masks and
More informationENGINE GROUND RUNNING
B737 600/700/800/900 (CFM 56) ENGINE GROUND RUNNING Guide and Reference Sheets This publication is for TRAINING PURPOSES ONLY. This information is accurate at the time of completion. No update service
More informationDavid s Flight Simulator Operations Manual
DPW Solutions David s Flight Simulator Operations Manual Draft 0.2 David Woolterton Update 10/5/2016 Table of Contents Pre-Start Checklist... 2 Startup Checklist... 3 Before Taxi Checklist... 3 Taxi Checklist...
More informationTakeoff Flaps UP 2000
Takeoff Flaps UP 2000 30 60 75 80 85 V1 Gear UP Flap Position Indicator blanked 10 seconds after flaps UP Asymmetry Protection Near Zero Yaw Automatic unlock all surfaces (maintenance) Speedbrakes auto
More informationVr V STANDARD EQUIPMENT LIST
Vr V5.02.09 STANDARD EQUIPMENT LIST IMPORTANT NOTE: this document is a general description of the aircraft equipment only. It is not a technical document and is to be used only for the purpose of generally
More informationDASSAULT FALCON 7X SYSTEMS SUMMARY
DASSAULT FALCON 7X SYSTEMS SUMMARY Airframe & Doors This material is to be used for training purpose only Do not use it for flight! Please note that this document is not affiliated in any way with any
More information2012 Gulfstream G650 s/n 60XX
2012 Gulfstream G650 s/n 60XX Airframe: Total Time: 2456.7 Engines: Rolls Royce BR725A1-12 (G650) 1 Engine Landings: 1190 Serial Number: 251XX EIS: March 2013 Total Time: 2456.7 Cycles: 1190 APU: Honeywell
More informationAIRPLANE FLIGHT MANUAL AQUILA AT01 AIRPLANE FLIGHT MANUAL - SUPPLEMENT AVE28 GLASS COCKPIT. equipped with ASPEN EFD1000 PFD
SECTION 9 AIRPLANE FLIGHT MANUAL - SUPPLEMENT AVE28 GLASS COCKPIT equipped with ASPEN EFD1000 PFD This AFM supplement is applicable and must be inserted into Section 9 of the Airplane Flight Manual when
More informationGENERAL TECHNICAL SPECIFICAITON
GENERAL TECHNICAL SPECIFICAITON AIRCRAFT TYPE Bombardier CL-600-2B19 RJ Series 200-LR SERIAL NUMBER 7457 COUNTRY OF REGISTRATION REGISTRATION NUMBER United States N655BR DATE OF MANUFACTURE December 9,
More informationExamen Teórico sobre Habilitación de Tipo B (Última actualización: Septiembre 2016)
DIRECCIÓN GENERAL DE AERONÁUTICA CIVIL DEPARTAMENTO SEGURIDAD OPERACIONAL SUBDEPARTAMENTO LICENCIAS Examen Teórico sobre Habilitación de Tipo B-737-300 (Última actualización: Septiembre 2016) Materia:
More informationPROSIM 737 Overhead Panel Switchmap (July 2012)
PROSIM 737 Overhead Panel Switchmap (July 2012) This Is How I Have Wired Up My Overhead To Work With Prosim. I have used 3 x BU0836X Boards for the inputs Why? Not because I think they are better than
More informationVr (P68R) STANDARD EQUIPMENT LIST V
Vr (P68R) STANDARD EQUIPMENT LIST V15.04.16 IMPORTANT NOTE: this document is a general description of the aircraft equipment only. It is not a technical document and is to be used only for the purpose
More informationMAJESTIC Q400 SHARED COCKPIT FLOWS CHECKLISTS MULTIPLAYER OPERATIONS.
PRE LOAD IN Agree on Ports, Share IP and select who will be doing W&B. INITIAL LOAD IN On 1 System transfer Weight and Balance to Simulator Pause Simulation Save Flight as normal FSX Flight Transfer Save
More informationSD3-60 AIRCRAFT MAINTENANCE MANUAL. This chapter includes information on dimensions, areas, zoning, etc. and is presented as follows:
AMM 6-00-00 1.0.0.0GENERAL 1. General This chapter includes information on dimensions, areas, oning, etc. and is presented as follows: Measurements and Figures which show the stations of fuselage frames,
More informationLANCAIR LEGACY PRE-TEST FLIGHT INSPECTION (8-04)
LANCAIR LEGACY PRE-TEST FLIGHT INSPECTION (8-04) OWNER PHONE # ADDRESS N SERIAL # AIRCRAFT TYPE DATE / / TACH TIME hrs. TOTAL TIME hrs. EMPTY WEIGHT CG. PAINT & INTERIOR? YES NO ENGINE TYPE PROPELLER ALL
More informationSystem Normal Secondary Direct. All 3 PFC work in parallel. available. Pitch Normal Secondary Direct. Pitch maneuver command.
Flight s System Normal Secondary Direct Primary Flight Computers (PFC) Three Primary Flight Computers use control wheel and pedal inputs from the pilot to electronically the primary flight control surfaces
More information77777 SERIES FLAMMABLE MATERIAL LOCATIONS
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATI 77 FLAMMABLE MATERIAL LOCATIS (tab) CAUTI: Rescue crews wearing full PPE to include SCBA s must use caution when moving across sections of aircraft that have
More informationDash8 - Q400 - Pneumatics
12.19.1 Introduction The Auxiliary Power Unit (APU) replaces the standard composite tailcone with a titanium tailcone and firewall. The APU is accessed by two clamshell type doors on the bottom of the
More informationEXAMEN POR MATERIAS PARA USO DE LOS POSTULANTES A LA HABILITACIÓN DE TIPO EN MATERIAL B733. ENERO 2018
DEPARTAMENTO SEGURIDAD OPERACIONAL SUBDEPARTAMENTO LICENCIAS SECCIÓN EVALUACIONES EXAMEN POR MATERIAS PARA USO DE LOS POSTULANTES A LA HABILITACIÓN DE TIPO EN MATERIAL B733. ENERO 2018 Cantidad de Preguntas
More informationATA 36 PNEUMATIC TABLE OF CONTENTS DGT ATA 36 PNEUMATIC TABLE OF CONTENTS GENERAL Introduction Sources
F900EX EASY 02-36-00 CODDE 1 PAGE 1 / 2 TABLE OF CONTENTS 02-36 02-36-00 TABLE OF CONTENTS 02-36-05 GENERAL Introduction Sources 02-36-10 DESCRIPTION Introduction Main sub-systems Distribution 02-36-15
More informationAIRCRAFT GENERAL KNOWLEDGE (1) AIRFRAME/SYSTEMS/POWERPLANT
1 In flight, a cantilever wing of an airplane containing fuel undergoes vertical loads which produce a bending moment: A highest at the wing root B equal to the zero -fuel weight multiplied by the span
More informationLOG OF REVISIONS. Model G58 Baron (Serials TH-2125 and After) Pilot s Operating Handbook and FAA Approved Airplane Flight Manual
LOG OF REVISIONS Model G58 Baron (Serials TH-2125 and After) Pilot s Operating Handbook and FAA Approved Airplane Flight Manual Revision A12 - May, 2015 Title Page LOEP LOR Section 1 All Reformatted to
More informationDASSAULT AVIATION Proprietary Data
F2000EX EASY 02-49-00 CODDE 1 PAGE 1 / 2 TABLE OF CONTENTS 02-49 02-49-00 TABLE OF CONTENTS 02-49-05 GENERAL Introduction Sources Equipment location 02-49-10 DESCRIPTION Introduction Description Operating
More informationPractical experience Group 2a Aircraft, single turboprop aeroplanes, cat. B1.1.
Practical experience Group 2a, single turboprop aeroplanes, cat. B1.1. This logbook is to be used to record details of experience on Group 2a type rating(individual or subgroup). This logbook is based
More informationA310 MEMORY ITEMS Last Updated: 20th th October 2011
A310 MEMORY ITEMS Last Updated: 20th th October 2011 1. Emergency Descent: Crew Oxygen Mask ON Crew Communication (Headsets) Establish Turn Initiate Descent Initiate o It is recommended to descend with
More informationNORMAL CHECKLIST ATTENTION!
Avion Training CHECKLIST Normal Checklist CESSNA 172R / TC-STS Cessna 172 R TC-STS NORMAL CHECKLIST ATTENTION! DO NOT STOW THIS CHECKLIST IN DIRECT SUNLIGHT Avion Training - Doc.nr. 212 Revision 1 / 02022018
More informationSURVEILLANCE CHECK LIST RENEWAL OF CERTIFICATE OF AIRWORTHINESS S/N ITEMS OF INSPECTION REMARKS SIGNATURE AIRCRAFT RELATED DOCUMENTS
Registration No.: Type of Aircraft: Type of Engine fitted: No. of Engine: Type of Propeller (if applicable): Name of owner/ operator: C of A valid till: Place of Inspection: Name & Designation of Officer:
More informationPA GURW (December 30, 2000) PRE-START. Langley Flying School. Airspeeds (MPH) for Safe Operation. Cockpit Checks
Langley Flying School PA-34-200 GURW (December 30, 2000) Airspeeds (MPH) for Safe Operation V y (all weights) 105 V x (all weights) 90 En Route Climb 120 V mc 80 V yse 105 V xse 93 V r 80 V r (25 Flaps)
More informationBOMBARDIER CHALLENGER 601-3A/ER SERIAL NUMBER 5120 EQUUS GLOBAL AVIATION +1 (954)
BOMBARDIER CHALLENGER 601-3A/ER 11,785 HOURS 5,785 CYCLES ENGINES: ENGINE TYPE: GE CF34-3A2 ( 3R ON CONDITION ENGINES Enrolled on GE On Point) POS. 1: POS. 2: SERIAL NUMBER: 350497 350490 TOTAL HOURS:
More informationPREFLIGHT CHECKLIST PA28R-200
PREFLIGHT CHECKLIST PA28R-200 COCKPIT AND CABIN MAINTENANCE STATUS VERIFIED / CLEARED HOBBS / TACH METERS VERIFIED / RECORDED POH / AIRCRAFT DOCUMENTS AVAILABLE / PARKING BRAKE SET FLIGHT CONTROLS FREE
More informationby Greg Whiley Aussie Star Flight Simulation
Flying the BAe 146 200/300 Version 2 by Greg Whiley Aussie Star Flight Simulation INTENTIALLY LEFT BLANK Greg Whiley Aussie Star Flight Simulation 2 Version Date Revision Version 1.0 25 June 2014 Original
More informationH130 to H125 Course Syllabus
HELICOPTERS Training Services H130 to H125 Course Syllabus T1 Airframe Type Rating Difference Part 147 Technician training 1 Contents #01 General Information p. 03 Course objective Prerequisites Registration
More informationDCS L-39 ALBATROS REAL PILOT START-UP, TAXI AND TAKEOFF CHECKLISTS V 1.0 PREPARED BY LINO_GERMANY
DCS L-39 ALBATROS REAL PILOT START-UP, TAXI AND TAKEOFF CHECKLISTS V 1.0 PREPARED BY LINO_GERMANY T.O. 1T-L39C-1.0 P1 INTRODUCTIONS A. CHECKLISTS This compilation contains amplified normal and (hopefully
More information@AIRBUS A318 AIRCRAFT CHARACTERISTICS AIRPORT AND MAINTENANCE PLANNING
@AIRBUS A318 AIRCRAFT CHARACTERISTICS AIRPORT AND MAINTENANCE PLANNING AC The content of this document is the property of Airbus. It is supplied in confidence and commercial security on its contents must
More informationAVIATION UNIT AND AVIATION INTERMEDIATE TROUBLESHOOTING MANUAL CH-47D HELICOPTER
TECHNICAL MANUAL AVIATION UNIT AND AVIATION INTERMEDIATE TROUBLESHOOTING MANUAL CH-47D HELICOPTER This copy is a reprint which includes current pages from Changes 1 through 10. HEADQUARTERS, DEPARTMENT
More informationECCAIRS Data Definition Standard. Descriptive Factors
ECCAIRS 4.2.8 Data Definition Standard Descriptive Factors The ECCAIRS 4 descriptive factors are based on ICAO's ADREP 2000 taxonomy. They have been organised at five hierarchical levels. An event can
More informationRegistration: N328DP Serial Number: 3169 Delivery Date: 14 December 2000 Operated By: Ultimate JetCharters, Inc.
Dornier 328Jet-310 Registration: N328DP Serial Number: 3169 Delivery Date: 14 December 2000 Operated By: Ultimate JetCharters, Inc. Contents Chapter Title Page 1. Certification 3 2. Power Plant / APU 3
More informationDifferences Training
Differences Training 747-400 Preamble The purpose of this presentation is to familiarize the crew with the various differences in procedures and systems among the 747-400 Fleet. The presentation highlights
More informationDASSAULT AVIATION Proprietary Data
F2000EX EASY 02-24-00 CODDE 1 PAGE 1 / 2 TABLE OF CONTENTS 02-24 02-24-00 TABLE OF CONTENTS 02-24-05 GENERAL Introduction Sources Equipment location 02-24-10 DESCRIPTION Generation Distribution Operation
More informationJump to Table of Contents
Jump to Table of Contents PIPER AIRCRAFT CORPORATION PA-28R-201, CHEROKEE ARROW III SECTION 3 EMERGENCY PROCEDURES 3.3 EMERGENCY PROCEDURES CHECK LIST ENGINE FIRE DURING
More informationCESCOM 20 - Projected Maintenance Due
Date Average Projected Days Months Overdue Maintenance Tasks Position Description Drawing # / Task # City 51211 PHASE 11 051211 051208 : L RIGHT 051208 : R Scheduled Maintenance Tasks Mod Lvl Part Number
More informationMAINTENANCE RECORD (THIS FORM IS TO BE RETAINED IN THE AIRCRAFT LOG)
(THIS FORM IS TO BE RETAINED IN THE AIRCRAFT LOG) AIRCRAFT MAKE / MODEL: Hawker 800A AIRCRAFT TIME IN SERVICE: 6484.0 AIRCRAFT REGISTRATION NUMBER: N803CE AIRCRAFT LANDINGS: 5457 AIRCRAFT SERIAL NUMBER:
More information2004 Challenger 604 S/N Reg# N110BP Presented by: JetLease Office: Fax:
2004 Challenger 604 S/N 5579 - Reg# N110BP Presented by: JetLease Office: 561.242.4393 Fax: 561.242.4394 www.jetlease.com AIRFRAME STATUS: (As of December 4, 2008) Total Time: 2,027.5 Hours Landings: 697
More informationCanadair Regional Jet 100/200 - Auxiliary Power Unit
1. INTRODUCTION The auxiliary power unit (APU) is installed within a fireproof titanium enclosure in the aft equipment compartment. The APU is a fully automated gas turbine power plant which drives an
More informationAVIATION UNIT AND AVIATION INTERMEDIATE TROUBLESHOOTING MANUAL CH-47D HELICOPTER
TECHNICAL MANUAL AVIATION UNIT AND AVIATION INTERMEDIATE TROUBLESHOOTING MANUAL CH-47D HELICOPTER This copy is a reprint which includes current pages from Changes 1 through 17. HEADQUARTERS, DEPARTMENT
More informationREFERENCE: 2861 wings 2044 trunk 4904 total BEW 10,655 BOW 11,185 Max Useful load 5115 MLanding ZFW FUEL BURNS 11min min min
REFERENCE: 2861 wings 2044 trunk 4904 total BEW 10,655 BOW 11,185 Max Useful load 5115 MLanding 15700 ZFW 13000 FUEL BURNS 11min 357 27min 730 36 min 940 58min 1453 1:17 1800 2:20 2933 2:46 3283 3:00 3600
More informationAircraft Design: A Systems Engineering Approach, M. Sadraey, Wiley, 2012 Chapter 11 Aircraft Weight Distribution Tables
Aircraft Design: A Systems Engineering Approach, M. Sadraey, Wiley, 01 Chapter 11 Aircraft Weight Distribution Tables No Component group Elements Weight X cg Y cg Z cg 1 Wing 1.1. Wing main structure 1..
More informationV - Speeds. RV-10 V fe Flaps Speeds Trail (0 deg) Half (15 deg) Full (30 deg) 122 kias 96 kias. 80 kias
RV-10 Check List V - Speeds RV-10 V fe Flaps Speeds Trail (0 deg) Half (15 deg) Full (30 deg) 122 kias 96 kias 87 kias V s1 Stall (Flap Up) 60 kias V s0 Stall (Flap 40 deg) 55 kias Best Glide 80 kias V
More informationService Training. Audi A5 - Networking. Self-Study Programme 395
Service Training Audi A5 - Networking Self-Study Programme 395 Innovations in the electrical system and electronics on the Audi A5 The number of s in motor vehicles continues to increase, and the Audi
More informationCFM56-7B POWER PLANT REMOVAL & INSTALLATION
Task No: 737-71-00-00 NG Maint Prog Ref: BAL/BOE/11 Station: A/C Reg: Issue: 5 Date: NOV 2017 A.M.M. Ref: 71-00-02 Check: Aircraft Type CAA App Ref. UK.145.00112 Scheduled / Unscheduled Delete as applicable
More informationPilot's Operating Handbook Supplement AS-03
POH / AFM SECTION 9 Pilot's Operating Handbook Supplement ASPEN EFD1000 PFD This supplement is applicable and must be inserted into Section 9 of the POH when the Aspen Avionics Evolution Flight Display
More informationDassault Falcon 50 Microsoft Flight Simulator 2004
Dassault Falcon 50 Microsoft Flight Simulator 2004 Model and bitmaps Yannick Lavigne Custom gauge programming Fred Banting Flight dynamics Rob Young and Eric Dantes. Foto: Gerry Stegmeier Foto: Dassault
More informationDASSAULT AVIATION Proprietary Data
F2000EX EASY 02-33-00 CODDE 1 PAGE 1 / 2 TABLE OF CONTENTS 02-33 02-33-00 TABLE OF CONTENTS 02-33-05 GENERAL Introduction Sources 02-33-10 DESCRIPTION General Cockpit lights Cabin lights Servicing lights
More informationFactory Fresh NEW A WITH CFM-56 5B4/P ENGINES
Factory Fresh NEW A320-24 WITH CFM-5 5B4/P ENGINES Engines: 2x CFM5 5B4/P Engines times max. Ferry Hours Year of Manufacture: 200 Aircraft Cycles max. 0 cycles Aux. Power Unit: Honeywell 3-9A Cabin layout
More informationSECTION 2 LIMITATIONS
SECTION 2 TABLE OF CONTENTS PARAGRAPH PAGE 2.1 INTRODUCTION 2-1 2.2 KINDS OF OPERATIONS LIMITS 2-1 2.3 AIRSPEED 2-3 2.4 AIRSPEED INDICATOR MARKINGS 2-3 2.5 POWER PLANT 2-4 2.6 POWER PLANT INSTRUMENT MARKINGS
More informationGeneral Information. Sikorsky Executive S-76C+ Helicopter Serial Number January 2010
Sikorsky Executive S-76C+ Helicopter Serial Number 760479 January 2010 Sikorsky Aircraft Corporation 6900 Main Street, P.O. Box 9729 Stratford, CT 06615-9129 (203) 386-4000 Sikorsky Aircraft Corporation
More informationAIR TRANSPORT INTERNATIONAL
16.04 B757 SERVICE CHECK (FORM 757-16.04-1) B757 SERVICE CHECK SIGNATURE RECORD (FORM 757-16.04-1) NOTE: The Sign-Off Section of the Service Check (Form 757-16.04-1) is a signature record and contains
More informationB737 NG Anti Ice & Rain
B737 NG Anti Ice & Rain Introduction Thermal anti-icing (TAI), electrical anti-icing, and windshield wipers are the systems provided for ice and rain protection. The anti-ice and rain systems include:
More informationMINIMUM EQUIPMENT LIST
CDL 1 of 18 GENERAL LIMITATIONS This Configuration Deviation List contains additional certificate limitations for operation of the Fokker F27 MK050, MK0502 and MK0604 Airplane without certain secondary
More informationAccident Prevention Program
Accident Prevention Program Maintenance Aspects of Owning Your Own Airplane Introduction As an owner-pilot, FAR Part 43 allows you to perform certain types of inspections and maintenance on your airplane.
More informationTECNAM P2004 BRAVO N128LS
TECNAM P2004 BRAVO N128LS GENERAL INFORMATION NORMAL PROCEDURES TIME SENSITIVE EMERGENCY TECNAM P2004 BRAVO CHECKLIST [FLIGHT PLAN DESIGNATION IS BRAV ] EMERGENCY CONTACT The following are First Landings'
More informationHawker 800XP Ground Handling Checklist. Procedures
Hawker 800XP Ground Handling Checklist Procedures A. Introduction This part of the Ground Handling Checklist gives the approved procedures, from the Aircraft Maintenance Manual, to accomplish the Pre-Flight
More informationList of Effective Pages
List of Effective Pages Page No. Revision No. Revision Date Page No. Revision No. Revision Date IV-1 0 08/01/2016 IV-2 0 08/01/2016 IV-3 0 08/01/2016 IV-4 0 08/01/2016 IV-5 0 08/01/2016 IV-6 0 08/01/2016
More information