PARKING - MAINTENANCE PRACTICES
|
|
- Bennett Melton
- 5 years ago
- Views:
Transcription
1 PARKING - MAINTENANCE PRACTICES TASK Removal of the Nose Landing Gear (NLG) Lockpin A. Reference Information TASK TASK Open the Nose Landing Gear (NLG) Forward Doors Close the Nose Landing Gear (NLG) Forward Doors B. Tools and Equipment GSE Tag, Circuit Breaker NOTE: Refer to the Illustrated Tool and Equipment Manual to make sure that you use the correct equipment configuration. C. Job Set Up (1) Open the NLG forward doors (TASK ). (2) Open and tag the circuit breaker that follows: LOCATION CB NUMBER CB NAME ZONE CBP 1 F2 WOW/GEAR/SPLR NO D. Procedure Refer to Figure 201. WARNING: KEEP THE LOCKPIN IN POSITION IF IT IS NOT EASY TO REMOVE. IF YOU REMOVE THE LOCKPIN, THE LANDING GEAR IS NOT SAFE, AND CAN ACCIDENTALLY RETRACT. THIS CAN CAUSE INJURIES TO PERSONS AND DAMAGE TO THE AIRCRAFT. (1) Remove the lockpin (1) by hand, from the hole (2) in the upper link of the NLG drag brace. NOTE: If the lockpin is not easy to remove, there may be a problem with the landing gear and you must correct the problem. Page 201
2 E. Close Out (1) Remove the tag and close the circuit breaker that follows: LOCATION CB NUMBER CB NAME ZONE CBP 1 F2 WOW/GEAR/SPLR NO (2) Close the NLG forward doors (TASK ). (3) Remove all tools, equipment, and unwanted materials from the work area. Page 202
3 2 1 LMM _001 Nose Landing Gear (NLG) Lockpin Removal/Installation Figure 201 Page 203
4 TASK Installation of the Nose Landing Gear (NLG) Lockpin A. Reference Information CL 605 AIRCRAFT MAINTENANCE MANUAL PART II TASK TASK Open the Nose Landing Gear (NLG) Forward Doors Close the Nose Landing Gear (NLG) Forward Doors B. Tools and Equipment GSE GSE Lockpin, NLG Tag, Circuit Breaker NOTE: Refer to the Illustrated Tool and Equipment Manual to make sure that you use the correct equipment configuration. C. Job Set Up (1) Open the NLG forward doors (TASK ) (2) Open and tag the circuit breaker that follows: LOCATION CB NUMBER CB NAME ZONE CBP 1 F2 WOW/GEAR/SPLR NO D. Procedure Refer to Figure 201. (1) Put the lockpin (1) fully into the hole (2) in the upper link of the NLG drag brace. NOTE: If the lockpin is not easy to install, there may be a problem with the landing gear and you must correct the problem. Page 204
5 E. Close Out (1) Remove the tag and close the circuit breaker that follows: LOCATION CB NUMBER CB NAME ZONE CBP 1 F2 WOW/GEAR/SPLR NO (2) Close the NLG forward doors (TASK ). (3) Remove all tools, equipment, and unwanted materials from the work area. Page 205
6 TASK Removal of the Main Landing Gear (MLG) Lockpins A. Procedure Refer to Figure 202. CL 605 AIRCRAFT MAINTENANCE MANUAL PART II WARNING: KEEP THE LOCKPIN IN POSITION IF IT IS NOT EASY TO REMOVE. IF YOU REMOVE THE LOCKPIN, THE LANDING GEAR IS NOT SAFE, AND CAN ACCIDENTALLY RETRACT. THIS CAN CAUSE INJURIES TO PERSONS AND DAMAGE TO THE AIRCRAFT. (1) Remove the lockpin (3) by hand, from the hole (2) in the retraction actuator. NOTE: If the lockpin is not easy to remove, there may be a problem with the landing gear and you must correct the problem. (2) Move the spring clip (1) to the holes on the retraction actuator. B. Close Out (1) Remove all tools, equipment, and unwanted materials from the work area. Page 206
7 SHOCK STRUT ACTUATOR 1 A 2 3 A LMM _011 Main Landing Gear (MLG) Lockpin Removal/Installation Figure 202 Page 207
8 TASK Installation of the Main Landing Gear (MLG) Lockpins A. Tools and Equipment CL 605 AIRCRAFT MAINTENANCE MANUAL PART II GSE Lockpin, MLG NOTE: Refer to the Illustrated Tool and Equipment Manual to make sure that you use the correct equipment configuration. B. Procedure Refer to Figure 202. WARNING: DO NOT STAY BELOW THE AIRCRAFT IF YOU CANNOT EASILY INSTALL THE LOCKPIN. IF YOU CANNOT EASILY INSTALL THE LOCKPIN, THE LANDING GEAR IS NOT SAFE, AND CAN ACCIDENTALLY RETRACT. THIS CAN CAUSE INJURIES TO PERSONS AND DAMAGE TO THE AIRCRAFT. (1) Move the spring clip (1) at the outboard end of the retraction actuator to one side to open the lockpin holes (2). (2) Put the lockpin (3) by hand, fully into one of the holes (2) in the retraction actuator. NOTE: If the lockpin is not easy to install there may be a problem with the landing gear and you must correct the problem. C. Close Out (1) Remove all tools, equipment, and unwanted materials from the work area. Page 208
9 TASK Removal of the Air Driven Generator (ADG) Lockpin A. Reference Information CL 605 AIRCRAFT MAINTENANCE MANUAL PART II TASK TASK Open the Nose Landing Gear (NLG) Forward Doors Close the Nose Landing Gear (NLG) Forward Doors B. Tools and Equipment GSE Tag, Circuit Breaker NOTE: Refer to the Illustrated Tool and Equipment Manual to make sure that you use the correct equipment configuration. C. Job Set Up (1) Open the nose landing gear (NLG) forward doors (TASK ) (2) Open and tag the circuit breaker that follows: LOCATION CB NUMBER CB NAME ZONE CBP 1 F2 WOW/GEAR/SPLR NO D. Procedure Refer to Figure 203. WARNING: KEEP THE LOCKPIN IN POSITION IF IT IS NOT EASY TO REMOVE. IF YOU MUST USE FORCE TO REMOVE THE LOCKPIN, THE ADG UPLOCK IS NOT SAFE, AND THE ADG CAN ACCIDENTALLY EXTEND. THIS CAN CAUSE INJURIES TO PERSONS AND DAMAGE TO THE AIRCRAFT. IF THE LOCKPIN IS NOT EASY REMOVE. YOU MUST CORRECT THE PROBLEM. (1) Remove the lockpin by hand from the hole on the right side of the nose gear well. Page 209
10 E. Close Out (1) Remove the tag and close the circuit breaker that follows: LOCATION CB NUMBER CB NAME ZONE CBP 1 F2 WOW/GEAR/SPLR NO (2) Remove all tools, equipment, and unwanted materials from the work area. (3) Close the nose landing gear NLG forward doors (TASK ). Page 210
11 A GROUND SAFETY PIN B ADG UPLOCK A GROUND SAFETY PIN B LMM _021 Air Driven Generator (ADG) Lockpin Removal/Installation Figure 203 Page 211
12 TASK Installation of the Air Driven Generator (ADG) Lockpin A. Reference Information CL 605 AIRCRAFT MAINTENANCE MANUAL PART II TASK TASK Open the Nose Landing Gear (NLG) Forward Doors Close the Nose Landing Gear (NLG) Forward Doors B. Tools and Equipment GSE GSE Lockpin, ADG Tag, Circuit Breaker NOTE: Refer to the Illustrated Tool and Equipment Manual to make sure that you use the correct equipment configuration. C. Job Set Up (1) Open the nose landing gear (NLG) forward doors (TASK ). (2) Open and tag the circuit breaker that follows: LOCATION CB NUMBER CB NAME ZONE CBP 1 F2 WOW/GEAR/SPLR NO D. Procedure Refer to Figure 203. (1) Put the lockpin by hand, fully into the hole on the right side of the nose gear well. E. Close Out (1) Remove the tag and close the circuit breaker that follows: LOCATION CB NUMBER CB NAME ZONE CBP 1 F2 WOW/GEAR/SPLR NO Page 212
13 (2) Remove all tools, equipment, and unwanted materials from the work area. (3) Close the nose landing gear NLG forward doors (TASK ). Page 213
14 TASK Short Term Parking A. Reference Information CL 605 AIRCRAFT MAINTENANCE MANUAL PART II TASK TASK TASK TASK TASK TASK TASK TASK TASK Towing of the Aircraft Installation of the Nose Landing Gear (NLG) Lockpin Installation of the Main Landing Gear (MLG) Lockpins Installation of the Air Driven Generator (ADG) Lockpin Grounding of the Aircraft Set the Parking Brake Release the Parking Brake Installation of the Covers and Plugs Aircraft Mooring B. Tools and Equipment GSE Chocks, Rubber NOTE: Refer to the Illustrated Tool and Equipment Manual to make sure that you use the correct equipment configuration. C. Procedure (1) If the aircraft is going to be parked for more than 48 hours, gain access to CBP 6 by opening the right forward equipment bay door (212AR) and pull the circuit breaker that follows: LOCATION CB NUMBER CB NAME ZONE CBP 6 B3 CLOCK STANDBY 212 Page 214
15 (2) If the aircraft is parked in a closed hanger, do the steps that follow: (a) (b) (c) (d) (e) (f) (g) Set the parking brake (TASK ). Install the wheel chocks at the nose landing gear (NLG) and main landing gear (MLG). Release the parking brake (TASK ). Install the NLG lockpin (TASK ). Install the MLG lockpins (TASK ). Install the air driven generator (ADG) lockpin (TASK ). Install the grounding wire (TASK ). (3) If the aircraft is parked in an open area, do the steps that follow: (a) (b) (c) (d) (e) (f) (g) (h) (i) (j) Park the aircraft in the correct position to point in the direction of the wind. Set the parking brake (TASK ). Install the wheel chocks at the nose landing gear (NLG) and main landing gear (MLG). Release the parking brake (TASK ). Install the NLG lockpin (TASK ). Install the MLG lockpins (TASK ). Install the (ADG) lockpin (TASK ). Install the grounding wire (TASK ). Install all applicable covers and plugs (TASK ). Do a regular inspection of the local weather conditions and do the steps that follow: 1 If the direction of the wind changes, move the aircraft to point in the direction of the wind, as necessary. 2 If high winds are possible, and a closed hangar is available, immediately tow the aircraft into the hangar until the wind is not a problem (TASK ). Page 215 May 29/2009
16 CAUTION: DO NOT PARK OR MOOR THE AIRCRAFT IN AN OPEN AREA WHEN WINDS OF 52 KNOTS (27 M/SEC) OR MORE ARE POSSIBLE. DURING THESE CONDITIONS, YOU MUST MOVE THE AIRCRAFT INTO A CLOSED HANGAR. IF YOU DO NOT DO THIS, YOU CAN CAUSE DAMAGE TO THE AIRCRAFT. D. Close Out 3 Moor the aircraft if high winds less than 52 kt (27 m/sec) are possible, and the aircraft is kept in an open area (TASK ). (1) Remove all tools, equipment, and unwanted materials from the work area. Page 216
17 TASK Long Term Parking A. Reference Information CL 605 AIRCRAFT MAINTENANCE MANUAL PART II TASK TASK TASK TASK TASK TASK TASK TASK TASK TASK TASK TASK Towing of the Aircraft Installation of the Nose Landing Gear (NLG) Lockpin Installation of the Main Landing Gear (MLG) Lockpins Installation of the Air Driven Generator (ADG) Lockpin Grounding of the Aircraft Set the Parking Brake Release the Parking Brake Installation of the Covers and Plugs Aircraft Storage Aircraft Mooring Disconnect the Main Battery Disconnect the Auxiliary Power Unit (APU) Battery B. Tools and Equipment GSE Chocks, Rubber NOTE: Refer to the Illustrated Tool and Equipment Manual to make sure that you use the correct equipment configuration. Page 217
18 C. Consumable Materials CL 605 AIRCRAFT MAINTENANCE MANUAL PART II MANUFACTURERS AND/OR SPECIFICATION Desiccant, Silica Gel MIL D 3464 D. Procedure (1) If the aircraft is parked in a closed hangar, do the steps that follow: (a) (b) (c) (d) (e) (f) (g) (h) (i) Set the parking brake (TASK ). Install the wheel chocks at the nose landing gear (NLG) and main landing gear (MLG). Release the parking brake (TASK ). Install the NLG lockpin (TASK ). Install the MLG lockpin (TASK ). Install the air driven generator (ADG) lockpin (TASK ). Install the grounding wire (TASK ). Disconnect the main battery (TASK ) Disconnect auxiliary power unit (APU) battery (TASK ) (2) If the aircraft is parked in an open area, do the steps that follow: (a) (b) (c) (d) (e) (f) (g) (h) (i) Park the aircraft in the correct position to point in the direction of the wind. Set the parking brake (TASK ). Install the wheel chocks at the nose landing gear (NLG) and main landing gear (MLG). Release the parking brake (TASK ). Install the NLG lockpin (TASK ). Install the MLG lockpins (TASK ). Install the ADG lockpin (TASK ). Install the grounding wire (TASK ) Disconnect the main battery (TASK ). Page 218 May 29/2009
19 (j) (k) (l) Disconnect auxiliary power unit (APU) battery (TASK ). Install all applicable covers and plugs and install desiccant where necessary to prevent contamination (TASK ). Do a regular inspection of the local weather conditions and do the steps that follow: 1 If the direction of the wind changes, move the aircraft to point in the direction of the wind, as necessary. 2 If high winds are possible, and a closed hangar is available immediately tow the aircraft into the hangar until the wind is not a problem (TASK ). CAUTION: DO NOT PARK OR MOOR THE AIRCRAFT IN AN OPEN AREA WHEN WINDS OF 52 KNOTS (27 M/SEC) OR MORE ARE POSSIBLE. DURING THESE CONDITIONS, YOU MUST MOVE THE AIRCRAFT INTO A CLOSED HANGAR. IF YOU DO NOT DO THIS, YOU CAN CAUSE DAMAGE TO THE AIRCRAFT. 3 Moor the aircraft if high winds are less than 52 kt (27 m/sec) are possible, and the aircraft is kept in an open area (TASK ). (3) If the aircraft storage is necessary, do the aircraft storage procedure (TASK ). E. Close Out (1) Remove all tools, equipment, and unwanted materials from the work area. Page 219 May 29/2009
20 TASK Grounding of the Aircraft A. Reference Information CL 605 AIRCRAFT MAINTENANCE MANUAL PART II TASK TASK TASK Electrical/Electronic Safety Precautions Open the Nose Landing Gear (NLG) Forward Doors Close the Nose Landing Gear (NLG) Forward Doors B. Tools and Equipment GSE Tag, Circuit Breaker NOTE: Refer to the Illustrated Tool and Equipment Manual to make sure that you use the correct equipment configuration. C. Job Set Up (1) Obey the electrical/electronic safety precautions (TASK ). (2) Open the NLG forward doors (TASK ) (3) Open and tag the circuit breaker that follows: LOCATION CB NUMBER CB NAME ZONE CBP 1 F2 WOW/GEAR/SPLR NO D. Procedure Refer to Figure 204. (1) If the grounding wire has an alligator clip, attach the clamp to the grounding lug (1) on the right side wall of the nose gear compartment. (2) If the grounding wire has a ground stud, put the stud in the nearest ground stud receptacle (2) on the wing leading edge. Page 220
21 E. Close Out (1) Remove the tag and close the circuit breaker that follows: LOCATION CB NUMBER CB NAME ZONE CBP 1 F2 WOW/GEAR/SPLR NO (2) Remove all tools, equipment, and unwanted materials from the work area. (3) Close the NLG forward doors (TASK ). Page 221
22 B 1 2 B A LMM _031 Grounding of the Aircraft Maintenance Practices Figure 204 Page 222
23 TASK Set the Parking Brake A. Reference Information CL 605 AIRCRAFT MAINTENANCE MANUAL PART II TASK Pressurize Hydraulic System No. 3 TASK Release Hydraulic Pressure System No. 3 B. Job Set Up (1) In the flight compartment, make sure that the brake systems have sufficient hydraulic pressure as follows: (a) (b) (c) (d) Push the HYD pushbutton on the engine indication and crew alerting system (EICAS) control panel to get the hydraulic page. Examine the hydraulic pressure for system No. 3. Make sure that the pressure indication shows 0 psi. On the HYDRAULIC control panel, set the 3A switch to ON. Examine the HYDRAULIC synoptic page on EICAS. Make sure that the conditions that follow: C. Procedure 1 The input/output flow indication for system No. 3A changes to green 2 The system No. 3A shows a minimum pressure of 1500 psi (10342 kpa). If the pressure is less than the necessary minimum, then pressurize system No. 3A to a minimum of 1500 psi (10342 kpa) (TASK ). (1) With your foot. push down and hold the brake pedals. (2) Fully release the parking brake handle. (3) Turn the parking brake handle 90 degrees clockwise. Make sure that the parking brake handle is locked in position. (4) Release the parking brake handle. (5) Release the brake pedals. Page 223
24 D. Close Out (1) If necessary, release hydraulic pressure from system No. 3A (TASK ) (2) Remove all tools, equipment, and unwanted materials from the work area. Page 224
25 TASK Release the Parking Brake A. Procedure (1) With your foot, push down and hold the brake pedals. (2) Fully release the parking brake handle. (3) Turn the parking brake handle 90 degrees counterclockwise. (4) Fully push in the parking brake handle and release it. (5) Release the brake pedals. CL 605 AIRCRAFT MAINTENANCE MANUAL PART II Page 225
26
PARKING - MAINTENANCE PRACTICES
PARKING - MAINTENANCE PRACTICES TASK 000 801 1. Removal of the Nose Landing Gear (NLG) Lockpin A. Reference Information TASK 32 22 00 010 801 TASK 32 22 00 410 801 Open the Nose Landing Gear (NLG) Forward
More informationELECTRICAL POWER, EXTERNAL - SERVICING
ELECTRICAL POWER, EXTERNAL - SERVICING TASK 861 801 1. Connect and Energize External AC Power A. Reference Information TASK 10 10 01 867 801 TASK 861 802 TASK 24 00 00 861 801 Grounding of the Aircraft
More informationTOWING - MAINTENANCE PRACTICES
TOWING - MAINTENANCE PRACTICES TASK 584 801 1. Towing of the Aircraft A. Personnel In open areas, a minimum of two persons are necessary to do this task. In small or confined areas, a minimum of five persons
More informationTOWING - MAINTENANCE PRACTICES. Lockpins. Installation of the Air Driven Generator (ADG) Lockpin
TOWING - MAINTENANCE PRACTICES TASK 584 801 1. Towing of the Aircraft A. Reference Information REFERENCE TASK 10 10 01 400 801 TASK 10 10 01 400 802 TASK 10 10 01 400 803 TASK 10 10 01 587 801 TASK 10
More informationTOWING MAINTENANCE PRACTICES. A. Towing Aircraft (Figure 201 and Figure 202) Cord, headset extension GSE Ref. No
TOWING MAINTENANCE PRACTICES 1. General All possible precautions must be taken to ensure the safety of personnel and the security of aircraft and equipment when moving aircraft. A. Towing Aircraft (Figure
More informationCHAPTER 09 TOWING AND TAXIING LIST OF EFFECTIVE PAGES
09 - Effective Pages AIRCRAFT MAINTENANCE MANUAL - PART I CHAPTER 09 TOWING AND TAXIING LIST OF EFFECTIVE PAGES Ch-Se-Su Effectivity Page Date Ch-Se-Su Effectivity Page Date ALL 1 09 - Contents ALL 1 ALL
More informationBD 700 AIRCRAFT MAINTENANCE MANUAL PART II GRAVITY REFUELING - SERVICING
GRAVITY REFUELING - SERVICING TASK 620 801 1. Use of Fuel Biocide Additive When Gravity Refueling A. Tools and Equipment REFERENCE Pneumatic Injector Shop Air, 90 ±10 psi (620.53 ±68.95 kpa) Test Panel,
More informationFalcon 50 AIRCRAFT MAINTENANCE MANUAL
TASK SPECIFIC MAINTENANCE FOR A/C OPERATING IN CORROSIVE AMBIENT CONDITIONS 1. 2. OVERVIEW OF THE JOB Operation codes: -01 Inspections and anti-corrosion treatments at short time intervals -02 Inspections
More informationPRESSURE REFUELING - SERVICING
PRESSURE REFUELING - SERVICING TASK 620 801 1. Use of Fuel Biocide Additive When Pressure Refueling A. Reference Information REFERENCE DESIGNATION TASK 650 801 TASK 28 00 00 910 801 Pressure Refueling
More informationE4610 (2 8160) Wing Landing Gear Retract Actuator Assy E4620 (2 8189) Wing Landing Gear Unlock Actuator Assy
32 30 29 17008 MLG Side Stay Actuator Assembly CL601 RJ 12 9/30/2016 32 30 30 19011 CL 604 Side Stay Actuator 8 8/11/2014 32 30 23 21501 Side Brace Actuator Assembly 16 12/22/2016 32 30 43 40310 MLG Side
More informationCHAPTER HYDRAULIC POWER LIST OF ILLUSTRATIONS
Vol. 1 14--00--1 HYDRAULIC POWER Table of Contents REV 3, May 03/05 CHAPTER 14 --- HYDRAULIC POWER Page TABLE OF CONTENT 14-00 Table of Contents 14--00--1 INTRODUCTION 14-10 Introduction 14--10--1 YTEM
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 information- (Ref , P. Block 001) - (Ref , P. Block 301) - (Ref , P. Block 301)
ENGINE PUMP PRESSURE SWITCH 113GK (112GK) REMOVAL/INSTALLATION WARNING: 1. Equipment and Materials CHECK THAT THE LANDING GEAR GROUND SAFETIES INCLUDING WHEEL CHOCKS ARE IN POSITION. BEFORE APPLING OR
More informationFokker 50 - Landing Gear
LANDING GEAR OPERATION Features General The Landing Gear (LG) consists of a forward retracting nose gear and two rearward retracting main gears. Doors enclose the landing gear bays. The LG is retracted
More informationEMERGENCY GEAR DOWN HANDLE CHECK VALVE GEAR DROP TO EXTEND POSITION DOOR SELECTOR DOOR SELECTOR VALVE UPLOCK RELEASE CYLINDER DOOR CYLINDER
WARN HORN CUT BEECHJET Landing Gear System LEGEND VENT LINE PRESSURE LINE RETURN LINE NITROGEN ELECTRICAL CIRCUIT CABLE LINE PACKAGE DUMP LANDING SELECTOR CHECK SELECTOR EMERGENCY DOWN HANDLE DROP TO EXTEND
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 informationA AMM - KRUEGER FLAP ACTUATOR - REMOVAL/INSTALLATION
FED ALL WARNING : 1. Equipment and Materials KRUEGER FLAP ACTUATOR - LANDING GEAR - MAKE SURE THAT THE GROUND SAFETIES AND CHOCKS ARE IN POSITION. FLIGHT CONTROLS - MAKE SURE THAT THE GROUND SAFETIES AND
More informationSERVICE BULLETIN REVISION
Revision 7 REVISION TRANSMITTAL SHEET This sheet transmits Revision 7 to Service Bulletin. A. Replaces the AN960PD10L Washers with NAS1149D0316K Washers. B. Removes the optional Aviation Brake System antiskid
More informationBombardier Challenger Hydraulic System
GENERAL The Challenger 605 is equipped with three independent hydraulic systems, designated as 1, 2, and 3. All systems operate at a nominal pressure of 3,000 psi to power the primary and secondary flight
More informationSeal Dynamics McCormick Drive Tampa, Florida Installation Instructions
Installation Instructions NLG Steering Actuator Bushing Replacement Bombardier Model CL-600-2B19 Report Number: SD3122015INSTL, Dated 09/14/2015 Page 1 of 50 Log of Revisions Revision Description Date
More informationcanadair chsfflencjibr
canadair chsfflencjibr HYDRAULICS TABLE OF CONTENTS Page GENERAL 1 HYDRAULIC SYSTEM COMPONENTS 1 A. Engine Pumps (2) 1 B. Electric Pumps (4) 1 C. Reservoirs (3) 2 D. Accumulators (3) 2 E. Heat Exchanger
More informationLanding Gear & Brakes
EMBRAER 135/145 Landing Gear & Brakes GENERAL The EMB-145 landing gear incorporates braking and steering capabilities. The extension/retraction, steering and braking functions are hydraulically assisted,
More informationMODEL 510 MAINTENANCE MANUAL
1. Scope TOWING AND TAXIING - GENERAL A. This chapter gives the procedures used to tow and taxi the airplane. Obey the local tow and taxi procedures. Examples are the use of the correct ramp and the correct
More informationSECTION II AIRPLANE AND SYSTEMS MODEL 750 HYDRAULIC
HYDRAULIC The main hydraulic system is comprised of two independent systems; system A and system B. Hydraulic power is used to power the primary flight controls (rudder, elevators, ailerons, and roll spoilers),
More informationAircraft Handling Ground Connections
Aircraft Handling Ground Connections Contents Ground Connections... 2 Electrical Power Connection... 3 Pneumatic Power Connection... 6 Conditioned Air Connection... 8 External Hydraulic Source Connection...
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 informationAVANTI P180. Ground Handling
AVANTI P180 Ground Handling Towing The airplane should be moved on the ground with the aid of the nosewheel towing bar provided with the airplane. The tow bar is designed to attach to the nose wheel axle.
More informationLEAR Description
LEAR 45 TOWING DESCRIPTION AND OPERATION 1. Description A. Towing and taxiing procedures are basically the same as those used for other aircraft equipped with tricycle landing gear. B. The aircraft can
More informationGeneral. Gear Retraction and Extension
Land.10 Landing Gear and Brakes-Description and Operation General The aircraft has a tricycle landing gear consisting of four-wheel trucks on each main gear, dual wheels on the nose gear, and a dual wheel
More informationGRAVITY REFUELING - SERVICING
GRAVITY REFUELING - SERVICING TASK 620 801 1. Use of Fuel Biocide Additive When Gravity Refueling A. Reference Information REFERENCE DESIGNATION TASK 650 801 TASK 28 00 00 910 801 Gravity Refueling Fuel
More informationLANDING GEAR. Table of Contents. Sep 13/2004 Flight Crew Operating Manual Volume 2 REV 1 CSP REV 1
Table of Contents Introduction... 15-01-01 Proximity Sensing System...15-01-02 Description... 15-01-02 Components and Operation... 15-01-02 Landing Gear Position and Warning System... 15-01-02 Landing
More informationRAYTHEON PREMIER I. TOWING Information This section of this sub-chapter provides information on towing procedures for the Model 390 airplane.
RAYTHEON PREMIER I TOWING Information This section of this sub-chapter provides information on towing procedures for the Model 390 airplane. Towing involves ground movement of the airplane without engine
More informationDESIGNATION. (1) Access Platform, 3.0 m (10 ft.) (2) 98A Guard - Safety, Flap/Slat Ctl Lever. (6) Circuit Breaker Safety Clips and Tags
KRUEGER FLAP HYDRAULIC ACTUATION - ADJUSTMENT/TEST CHECK THAT THE LANDING GEAR GROUND SAFETIES INCLUDING WHEEL CHOCKS ARE IN POSITION. BEFORE APPLYING OR RELIEVING HYDRAULIC SYSTEM PRESSURE, MAKE CERTAIN
More informationFALCON SERVICE ADVISORY
Cold Weather Operations Jan 10, 11 Origin: Field Status: Closed Classification: Maint & Ops REASON At the approach of winter, we would like to offer some additional guidance for operating your aircraft
More informationSD3-60 AIRCRAFT MAINTENANCE MANUAL. These procedures will be required by personnel engaged in manoeuvring the aircraft on the ground.
AMM 9-00-00 1.0.0.0TOWING AND TAXIING 1. General This chapter deals with aspects of: - Towing. Refer to 9-10-00, pb201. - Taxiing. Refer to 9-20-00, pb201. These procedures will be required by personnel
More informationService Bulletin No: Ref No: 105 Modification No: INSPECTION ATA Chapter: 32
PILATUS AIRCRAFT LTD. STANS, SWITZERLAND Service Bulletin No: 32-010 Ref No: 105 Modification No: INSPECTION ATA Chapter: 32 LANDING GEAR - MAIN GEAR AND DOORS INSPECTION OF THE MAIN-GEAR SUPPORT STRUT
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 informationSurface and Brakes Anti-Ice Systems
Surface and Brakes Anti-Ice Systems WING DEICE DISTRIBUTOR VALVE TAIL DEICE R BLEED FAIL VDC FROM RIGHT ENGINE P3 PNEUMATIC AIR SHUTOFF VALVE N.O. R BK DEICE ON Ice and Rain Protection N.C. TO DOOR SEAL
More informationCHAPTER ICE AND RAIN PROTECTION SYSTEM
15--00--1 ICE AND RAIN PROTECTION SYSTEM Table of Contents REV 3, May 03/05 CHAPTER 15 --- ICE AND RAIN PROTECTION SYSTEM Page TABLE OF CONTENTS 15-00 Table of Contents 15--00--1 INTRODUCTION 15-10 Introduction
More informationCHAPTER 10 PARKING AND MOORING
CHAPTER 10 PARKING AND MOORING P/N 135A-970-100 Chapter 10 REVISION ~ Page 1 of 12 Copyright 2009 All rights reserved. The information contained herein is proprietary to Liberty Aerospace, Incorporated.
More informationBEECHJET 400A TOWING AND TAXIING
TOWING AND TAXIING DESCRIPTION AND OPERATION Towing involves ground movement of the airplane without engine operation and is the preferred method of airplane positioning since it provides more safety and
More informationTHS ACTUATOR VALVE BLOCKS - ADJUSMENT/TEST
1. Reason for the Job WARNING: THS ACTUATOR VALVE BLOCKS - ADJUSMENT/TEST CHECK THAT LANDING GEAR GROUND SAFETIES, INCLUDING WHEEL CHOCKS ARE IN POSITION. BEFORE APPLYING OR RELIEVING HYDRAULIC SYSTEM
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 informationB757 AMM - DC GENERATION - ADJUSTMENT/TEST
1. General DC GENERATION - ADJUSTMENT/TEST A. This procedure has these tasks: (1) An Operational Test of the DC Generation System and Battery Charger Failure Detection Circuit. (2) An Operational Test
More informationSECTION III HYDRAULICS & LANDING GEAR
TABLE OF CONTENTS Pilot s Manual SECTION III HYDRAULICS & LANDING GEAR Hydraulic System... 3-1 Firewall Shutoff Valves... 3-2 Source Selector Valve... 3-2 AUX HYD Pump Control... 3-2 Main/Auxiliary System
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 informationCHAPTER FUEL SYSTEM
Vol. 1 13--00--1 FUEL SYSTEM Table of Contents REV 3, May 03/05 CHAPTER 13 --- FUEL SYSTEM Page TABLE OF CTENTS 13-00 Table of Contents 13--00--1 INTRODUCTI 13-10 Introduction 13--10--1 FUEL STORAGE 13-20
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 informationRotary Speed Brake Actuation System ICA Supplement
CESSNA AIRCRAFT COMPANY AIRCRAFT DIVISION WICHITA, KANSAS 67277 Rotary Speed Brake Actuation System ICA Supplement MODEL NO: 510 SUPPLEMENT NO: ICA-510-27-00001 SUPPLEMENT DATE: 04/28/2009 PREPARED BY:
More informationDOORS Table of Contents REV 3, May 03/05 CHAPTER DOORS. INTRODUCTION Introduction System Circuit Breakers
Vol. 1 06--00--1 DOOR Table of Contents REV 3, May 03/05 CHAPTER 6 --- DOOR Page TABLE OF CONTENT 06-00 -1 Table of Contents 06--00--1 INTRODUCTION 06-10 -1 Introduction 06--10--1 ystem Circuit Breakers
More informationPILATUS AIRCRAFT LTD. CH-6371 STANS, SWITZERLAND SERVICE BULLETIN SERVICE BULLETIN NO: REF NO: 184 MODIFICATION NO: ATA CHAPTER: 32
PILATUS AIRCRAFT LTD. CH-6371 STANS, SWITZERLAND NO: 32-016 REF NO: 184 MODIFICATION NO: ATA CHAPTER: 32 LANDING GEAR LANDING GEAR - INSPECTION AND REPLACEMENT OF COMPONENTS 1. Planning Information A.
More informationLANDING GEAR TABLE OF CONTENTS CHAPTER 15
TABLE OF CONTENTS CHAPTER 15 Page TABLE OF CONTENTS DESCRIPTION General Main Landing Gear Assembly Main Landing Gear Schematic Wheel Assemblies Main Gear/Door Downlock Safety Pins Main Landing Gear Overheat
More informationDornier 328Jet - Pneumatic
ECS Control Panel Page 1 MESSAGE (SYNOPTIC) WARN INHIBIT CONDITION Location (COLOR) TONE 1 2 3 APU BLEED LEAK CAS Field (AMBER) X X LEAK (APU BLEED) Bleed air leak in APU bleed air duct. ECS Page (AMBER)
More informationCanadair Regional Jet 100/200 - Fuel System
1. INTRODUCTION The fuel system consists of three integral tanks within the wing box structure. Ejector pumps and electrical boost pumps supply fuel to each engine. The fuel system also provides facilities
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 informationB737 NG APU REMOVAL / INSTALLATION
Form No: ENG/5806 A/C Reg: Issue: 02 Check: Date: JULY 2018 Date: Compiled From: 737 NG AMM CHAPTER Station: 49-11-00 S/No Off: A/C Type Boeing 737 NG S/No On: EQUIPMENT AND MATERIALS: APU CRADLE, FISHPOLE
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 informationПриложение 1 ТЕХНИЧЕСКО ЗАДАНИЕ
Приложение 1 ТЕХНИЧЕСКО ЗАДАНИЕ A319-112, MSN 3188, LZ-AOB AIRCRAFT LIST OF MAINTENANCE INSPECTIONS, OPERATIONS AND WORKS TO BE PERFORMED DURING INCOMMING OVERHAUL OF MLG, NLG AND RELATED RETRACTING ACTUATORS
More informationEmbraer Systems Summary [Landing Gear & Brakes]
GENERAL DESCRIPTION The airplane has two main landing gears and a single nose gear. Each main gear is a conventional two-wheeled landing gear. The nose gear is a conventional steerable two-wheeled unit.
More informationINTRODUCTION TO THE COMPANY
INTRODUCTION TO THE COMPANY Pacific Support Equipment Ltd. (PSE) established in 1987 specializes in the manufacture of high quality Aero Engine Tooling, Industrial Gas Turbine Tooling, and Aircraft Ground
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 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 informationFUEL SYSTEM REPLENISHING. NOTE: For calculation of fuel weights refer to Chapter 28. British Canadian American Specific Gravity
FUEL SYSTEM REPLENISHING 1. General Pressure refueling facilities are provided by a single point adapter located at the right wing leading edge fillet. Provision is also made for gravity refueling through
More informationAirworthiness Directive Schedule
Airworthiness Directive Schedule Aeroplanes 27 July 2006 The date above indicates the amendment date of this schedule. New or amended ADs are shown with an asterisk * Contents DCA/B99/1 Wing Attachment
More informationOPERATIONS MANUAL SECTION 6-2
SECTION 6-2 Index Page Pilot's Seats... 6-2-2 Pilot's Seats Adjustment... 6-2-4 Pedals Adjustment... 6-2-5 Direct Vision Windows... 6-2-6 Observer's Seat... 6-2-7 Attendant's Furnishings Typical (Version
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 informationCHAPTER 14 LANDING GEAR
CHAPTER 14 LANDING GEAR Page TABLE OF CONTENTS 14-00-01/02 DESCRIPTION General 14-10-01 Description 14-10-01 Controls and Indicators 14-10-04 COMPONENTS Nose Gear 14-20-01 Main and Center Gear 14-20-02
More informationDUCHESS BE-76 AND COMMERCIAL MULTI ADD-ON ORAL REVIEW FOR CHECKRIDE
DUCHESS BE-76 AND COMMERCIAL MULTI ADD-ON ORAL REVIEW FOR CHECKRIDE The Critical Engine The critical engine is the engine whose failure would most adversely affect the airplane s performance or handling
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 informationA AMM - MAIN GEAR SPHERICAL BEARING - REMOVAL/INSTALLATION
MAIN GEAR SPHERICAL BEARING - 1. Equipment and Materials CHECK THAT THE LANDING GEAR GROUND SAFETIES INCLUDING WHEEL CHOCKS ARE IN POSITION. BEFORE APPLYING OR RELIEVING HYDRAULIC SYSTEM PRESSURE, MAKE
More informationPNEUMATICS CONTENTS HST-TAMPER
CONTENTS Tamper Pneumatic Component Locations...2 Manually Releasing Air Brakes... 3 Releasing Air Pressure... 4 Removing Water from Air Tanks... 4 Adjusting Air Compressor Governor... 4 Check/Replace
More informationSR22 Airplane Flight Manual (AFM) Temporary Change
Cirrus Design TPOH AFM Temporary Change Airplane Flight Manual (AFM) Temporary Change Information in this Temporary Change adds to, supersedes, or deletes information in the basic Pilot s Operating Handbook.
More informationCAL Ramp Operations Safety Notes
CAL Ramp Operations Safety Notes Ramp Security & Safety 1. Persons who need to access the aircraft SHALL hold a valid identification badge on the front of the outer garment above the waist. 2. Smoking
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 informationColumbusJACK/Regent. The Strength of Experience. Bead Breakers
ColumbusJACK/Regent The Strength of Experience Bead Breakers Bead Breakers Six models provide breaking capability for all aircraft models, both fixed and rotary wing. Breaking capacities from 2,000 lb
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 informationSD3-60 AIRCRAFT MAINTENANCE MANUAL PROTECTION DESCRIPTION & OPERATION
SD3-60 AIRCRAFT MAINTENANCE MANUAL z AMM 31.0.0.0COLD WEATHER PROTECTION DESCRIPTION & OPERATION 1. General This section details precautions necessary to protect the aircraft on the ground during cold
More informationSR22T Airplane Flight Manual (AFM) Temporary Change
Cirrus Design TPOH Airplane Flight Manual (AFM) Temporary Change Information in this Temporary Change adds to, supersedes, or deletes information in the basic Pilot s Operating Handbook. Affected Publications:
More informationFLIGHT CONTROLS SYSTEM
FLIGHT CONTROLS SYSTEM DESCRIPTION Primary flight control of the aircraft is provided by aileron, elevator and rudder control surfaces. The elevator and rudder control surfaces are mechanically operated.
More informationPreservation. A.1. Preservation for a Period of up to 30 Days. Pág. 2. Memoria ** ON A/C , , TASK
Annex Pág. 2 Memoria A Preservation A.1. Preservation for a Period of up to 30 Days ** ON A/C 001-010, 012-099, 201-299 TASK 72-00-00-600-001 Preservation for a Period of up to 30 Days 1. Reason for the
More informationMain Landing Gear Torque Links - Remove procedures
Main Landing Gear Torque Links - Remove procedures DMC: Title: Issue no: Main Landing Gear Torque Links - Remove procedures 003 new Issue Date: 2015-01-21 Language: Security classification : Responsible
More informationSD3-60 AIRCRAFT MAINTENANCE MANUAL - DESCRIPTION & OPERATION
SD3-60 AIRCRAFT MAINTENANCE MANUAL z PAMM 54.0.0.0STEERING - DESCRIPTION & OPERATION 1. Description The nosewheel is operationally steerable through a radius of 55 degrees on either side of the aircraft
More informationAIRCRAFT EXPOSURE TO VOLCANIC ASH PROPRIETARY NOTICE
Gulfstream. DOCUMENT NO: ~S~G~E~R~-3~8~7 FAAPROJECTNO:~N~~~ CURRENT REVISION:...,:.A..::s:...:.,N.:..::o:.:::te:.::,d INITIAL DATE: May 06,2010 GAC CAGE CODE: 59734 MODEL: G-1159, G-1159A, G-1159B, G100,
More informationHYDRAULICS & LANDING GEAR
IC~--u U ; ~~^U ul'h HYDRAULICS & LANDING GEAR TABLE OF CONTENTS Hydraulic System.....................................................................................3-1 HYD PUMP Switch................................................................................3-2
More informationBombardier Q300 nose landing gear incidents
Bombardier Q300 nose landing gear incidents Peter R. Williams Transport Accident Investigation Commission ANZSASI Regional Air Safety Seminar Christchurch, June 2013 September 2010 Flight WLG NSN, wx divert
More informationCIRRUS AIRPLANE MAINTENANCE MANUAL
JACKING 1. DESCRIPTION Three jack points, located at each wing tiedown and tail tiedown, are provided to perform maintenance operations. Tie-down rings must be removed and replaced with jack points prior
More informationInstallation Work for Alpha Systems Angle of Attack System DSTR-AOA-9600K 05/28/2015
Installation Work for Alpha Systems Angle of Attack System DSTR-AOA-9600K 05/28/2015 Aircraft Information: Piper Arrow 200 PA-28R-200 Overall Description: A model DSTR-AOA-9600K Angle of Attack System
More informationAIRCRAFT INFORMATION MSN: 4066
AIRCRAFT INFORMATION MSN: 4066 This report contains the following: Section 1 - Aircraft Status Section 2 - Engines Status (Owned Engines) Section 3 Propeller Status Section 4 - APU Status Section 5 - Landing
More informationChapter Four CASTER POWER-BACK AND INDICATION SYSTEM
Chapter Four CASTER POWER-BACK AND INDICATION SYSTEM The Caster Power-Back System provides the capability of free-castering the Aft MLGs. Castering the Aft MLGs with the forward MLGs locked, facilitates
More informationWorld Leaders in Engineered Performance. Regional and Business Aircraft
World Leaders in Engineered Performance Regional and Business Aircraft From Commercial to Combat, This is Where Innovation Is Born Operational Excellence On Two Continents Feet-On-The-Ground Around The
More informationDASSAULT AVIATION Proprietary Data
F900EX EASY 02-27-00 CODDE 1 PAGE 1 / 2 TABLE OF CONTENTS 02-27 02-27-00 TABLE OF CONTENTS 02-27-05 GENERAL Introduction Flight control sources Primary and secondary flight controls 02-27-10 DESCRIPTION
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 informationModels Affected: Certain 2013 Model Year Propane Vision Buses Equipped with Ford 6.8L Engines CORRECTIVE ACTION ---- PROCEDURE
Models Affected: Certain 2013 Model Year Propane Vision Buses Equipped with Ford 6.8L Engines ISSUE Certain 2013 model year propane Vision buses equipped with Ford 6.8L engines may not have the service
More informationTRANSPORT WINGS 1:72 Mixed-media kit of the DC Second generation jet airliner History, Notes and Instructions
TRANSPORT WINGS 1:72 Mixed-media kit of the DC-10-30 Second generation jet airliner History, Notes and Instructions Introduction TRANSPORT WINGS kits are model kits of large aircraft. They are suitable
More informationLucinda Handwriting & Arial Black 11, 16, 18 34
Access and inspection holes are provided in the cabin floor for servicing cables, hydraulic lines, landing gear and gasoline tank. Additional access holes are provided on the exterior at the boom for servicing
More informationCHAPTER 6 ELECTRICAL SYSTEMS
CHAPTER 6 ELECTRICAL SYSTEMS Page TABLE OF CONTENTS 06-00-01/02 DESCRIPTION General 06-10-01 Description 06-10-01 Controls and Indicators 06-10-02 COMPONENTS Circuit Breaker Panel Locations 06-20-01/02
More informationPrevent corrosion that can decrease the aircraft structure life. Do a thorough inspection for corrosion and other types of damage.
TASK -100-801-A EFFECTIVITY: ALL 1. External Aircraft - Cleaning A. General (1) This task gives the procedures to remove light and heavy dirt from the ACFT external surfaces to: Prevent corrosion that
More informationReport RL 2004:21e. Accident involving aircraft LN-ALK at Malmö Sturup Airport, M county, Sweden, on 14 April 2004
ISSN 1400-5719 Report RL 2004:21e Accident involving aircraft LN-ALK at Malmö Sturup Airport, M county, Sweden, on 14 April 2004 Case L-07/04 SHK investigates accidents and incidents with regard to safety.
More informationThe 747 s body gear Project Report
Hogeschool van Amsterdam, Technology, Aviation The 747 s body gear Project Report Projectgroup 2A2R Projectleader Ivar van Cuyk Kevin van der Plas Sander van der Pijl Jos Frijmann Roy van Schagen Wytze
More information