Nabtesco Aerospace Inc. Product Capability list AIRCRAFT PART NAME NABTESCO P/N CUSTOMER P/N
|
|
|
- Noah Copeland
- 6 years ago
- Views:
Transcription
1 B767(-200) Yaw Damper Servo S252T S252T S252T704-3 B757 Yaw Damper Servo S251N313-1 B757 Yaw Damper Servo S252T B S252T (-300) * Changed to , S252T S252T B757 / B767 Yaw Damper Servo S252T S252T ,-9 S252T ,-11 S252T B747 Outboard Aileron ,-1MOD.A 60B Lockout Act. Assembly , , B767 Outboard Aileron ,-7 60B Lockout Act. Assembly ,-13,-15 60B B767 / B ,-17D 60B B B757 Aileron S251N114-2 Power Control Unit Assembly S251N114-3 * Changed to B757 Aileron S251N114-4 Power Control Unit Assembly S251N114-5 B767/B Outboard Aileron B Lockout Act. Assembly B A,B Aileron S251W B Power Control Unit Assembly S251W B7-300ER B /400/500 Valve B /200 Pressure Reducer Bypass B /400/500 Valve B /200 Pressure Reducer Bypass B A,B Elevator S251W B Power Control Unit Assembly 1 of 6
2 B737, B Elevator Feel Shift Module S251A225-1 B ER MD-11 Inboard Elevator Actuator Assy ,-51,-503 BLG ,-71,-703 BLG MD-11 Outboard Elevator Actuator Assy ,-51 BLG ,-71 BLG B747 Flap Load Relief ,-1MOD.A 60B Linear Act. Assembly , , B ,-303 B747 Flap Load Relief ,-1MOD.A 60B Linear Act. Assembly , , B747 Flap Load Relief B Servo Act. Assembly (B767) Flap Load Relief ( ) (60B ) (B767 / B ) Linear Act. Assembly ( ) B B C550 Actuator Assy Flap, Hydraulic C525 Actuator Assy C525A Flap, Hydraulic B A,B Flaperon S251W B Power Control Unit Assembly S251W S251W B777 Flaperon S251W Power Control Unit Assembly B767 Inboard Spoiler Power (Built-to-Print) 252T Control Actuator Assy 252T (Boeing) 252T C650 Actuator Assy Spoiler, Hydraulic of 6
3 B767 Power Control ,-3 S252T303-1, -2 Actuator Assembly ,-3 S252T303-1, -2 Inboard Spoiler , -7 S252T303-1, ,-11 S252T303-1, ,-15 S252T303-1, -2 DHC8 Actuator Assy, EPS 8/9-1 Spoiler Sovereign Power Control Unit Assy, (C680) Spoiler / Speed Brake, Hyd B767 Outboard Spoiler Power 252T Control Actuator Assy (Built-to-Print) 252T (Boeing) 252T B767 Power Control ,-3 S252T304-1, -2 Actuator Assembly ,-3 S252T304-1, -2 Outboard Spoiler ,-7 S252T304-1, ,-11,-13,-15 S252T304-1, ,-19 S252T304-1, -2 C525 Actuator Assy Speed Brake, Hydraulic (C525A)CJ C550 Actuator Assy Speed Brake, Hydraulic ERJ Actuator Assy SCD Spoiler, Multi-Function MD-11 Leading Edge BRG Slat Actuator Assy B757, B767, B777 Valve Assy S271T463-1 Selector, Reservoir Fill B ,-200 Main Gear Actuator Assy (Built-to-Print) thru -9 (Boeing) -11,-12,-13,-27 thru thru -9-11,-12,-15,-16,-21, thru 31,-33,-34,-36, thru -14, -17 thru -23, -26 thru -30 B ,-400,-500 Main Gear Actuator Assy (Built-to-Print) 65C ,-3,-4,-6 (Boeing) ,-32,-35,-42 3 of 6
4 B ,-200 Main Gear Damper Assy (Built-to-Print) ,-2,-3,-5 (Boeing) ,-3, ,-3,-5,-7,-8 B737 MLG Shimmy Damper (Built-to-Print) 273A3610-1,-2,-4,-5 (Boeing) C400 Actuator Assy Nose Landing Gear, Hydraulic, A Locking A C550 Actuator Assy Nose Landing Gear, Hydraulic Ultra (C550) Actuator Assy C560 Nose Landing Gear, Hydraulic , ,-4 BRAVO (C550) Actuator Assy Encore (C560 BPC) Nose Landing Gear, Hydraulic , ,-4 EXCEL (C560) Actuator Assy Nose Landing Gear, Hydraulic , ,-5 C650 Actuator Assy Nose Landing Gear, Hydraulic C525 Actuator Assy Nose Landing Gear, Hydraulic CJ2 (C525A) C400 Actuator Assy Main Landing Gear, Hydraulic, Locking C500 Actuator Assy Main Landing Gear, Hydraulic of 6
5 C560 Actuator Assy Main Landing Gear, Hydraulic BRAVO (C550) Actuator Assy Main Landing Gear, Hydraulic EXCEL (C560) Actuator Assy ,-5A Main Landing Gear, Hydraulic ,-6A , , Encore (C560BPC) Actuator Assy , , -2 Main Landing Gear, Hydraulic , , -2 C650 Actuator Assy Main Landing Gear, Hydraulic C525 Actuator Assy A Main Landing Gear, Hydraulic B , , -8 CJ2 (C525A) Actuator Assy Main Landing Gear, Hydraulic B ER Safety Valve Assy S257T440-2 Main Gear Door BA609 Door Actuator , / -102 Main Landing Gear B ER MLG Door Actuator (Built-to-Print) 273T (Boeing) B ,-400,-500 Valve Assembly Brake Metering S92 Parking Brake Valve, Main Landing Gear S92 Master Brake Cylinder Main Landing Gear 5 of 6
6 B747 Nose Gear Rudder ,-1MOD.A 60B Pedal Steering ,-5 60B B Interconnect ,-901 Linear Act. Assembly C650 Locking Side Brace Mechanism, Main Landing Gear, Hydraulic, Unlock B747 Snubber Assy, B Bulk Cargo Door MH2000 Servo Assy AS Main Rotor Head AS (MHI) AS MH2000 Servo Assy AS Tail Rotor Head AS (MHI) V2500-A1 Fuel Diverter & Return Valve 13289G10 5L0004 (IHI) 13289G11 5L G12 5L G13 5L G14 5L G15 5L G16 5L0075 V2500-A5 / D5 Fuel Diverter & Return Valve 17300G04 5L0054 (IHI) 17300G05 5L G06 5L G07 5L G08 5L G09 5L0076 B747,B757,B767 Valve, Isolation ,-3,-5 S271T528-1,-2,-3 6 of 6
C A P A B I L I T Y M A N U A L
C A P A B I L I T Y M A N U A L REVISION Rev. BI REVISION DATE 15 December 2015 ISSUE Second TABLE OF CONTENTS INTRODUCTION... 2 Company... 2 Capability Manual... 2 Record of Revision... 3 List of Effective
PUBLICATIONS INDEX TITLE/ ACFT/ PART NUMBER DATE
Phone: (35) 552223 24233 9//982 HP 38200 Valve, Emergency Generator Control Bae 46 RJ 27200 9/5/2009 9253 Actuator, Rudder Spring (RSA) EMB505 Phenom 300 2720 6 2/29/202 40C4062A3 (S253W933) Damper, Primary
PUBLICATIONS INDEX TITLE/ ACFT/ PART NUMBER DATE
Phone: (35) 552223 24233 9//982 HP 38200 Valve, Emergency Generator Control Bae 46 RJ 27200 9/5/2009 9253 Actuator, Rudder Spring (RSA) EMB505 Phenom 300 2720 6 2/29/202 40C4062A3 (S253W933) Damper, Primary
E4610 (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
BALLAST 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
System 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
LISTA DE PEÇAS CONTROLADAS - LEARJET 35A S/N 479
1 BENDIX GENERATOR - OVERHAUL - P/N 6608201 - LH 30B107-11-A 2 BENDIX GENERATOR - OVERHAUL- P/N 6608201 - RH 30B107-11-A 3 FIRE EXTINGUISH HAND HELD - HYD TST 344T 4 5 NOSE WHEEL STEERING ACTUATOR P/N
EMERGENCY 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
SD3-60 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,
FLIGHT 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.
CHAPTER 27 - FLIGHT CONTROLS TABLE OF CONTENTS
FLIGHT CONTROLS 27-00 General 1 Troubleshooting 2 AILERON AND ROLL TRIM SYSTEM 27-10 Aileron System Cables 2 Removal - Aileron System Cables 2 Installation - Aileron System Cables 2 Adjustment/Test - Aileron
ARIANA 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
Bombardier 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
DASSAULT 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
Fokker 50 - Landing Gear & Flaps
FLIGHT CONTROLS The flight controls can be operated manually and automatically. From the flight deck, all control surfaces are mechanically operated via rod-and-cable systems, except the electrically operated
FLIGHT CONTROLS TABLE OF CONTENTS CHAPTER 10
TABLE OF CONTENTS CHAPTER 10 Page TABLE OF CONTENTS DESCRIPTION Primary Flight Controls Secondary Flight Controls Spoiler System Trim Control High Lift Devices Stall Protection Hydraulic Power Distribution
SUPER 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 - - - - -
Chapter Thirteen. Nose Wheel Steering Systems. A. Small Aircraft. B. Large Aircraft. C. Shimmy Dampers
Chapter Thirteen Nose Wheel Steering Systems A. Small Aircraft Almost all airplanes with tricycle landing gear have some provisions for steering on the ground by controlling the nose wheel. Some of the
DASSAULT AVIATION Proprietary Data
F2000EX 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
CHAPTER9 FLIGHT CONTROLS
CHAPTER9 FLIGHT CONTROLS Page TABLE OF CONTENTS 09-00-01 DESCRIPTION General. 09-10-01 Description 09-10-01 Controls and Indicators 09-10-05/06 COMPONENTS Major Components 09-20-01/02 CONTROLS AND INDICATORS
Radian Pro DX6i Setup
Radian Pro DX6i Setup With the DX6i you can use flaps and CROW on the Radian Pro. This setup allows you to use basic flaps or engage CROW with the DX6i. There are not enough mixes available on the DX6i
CHAPTER 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
Part 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
Rotables Available CRJ Classic
0059-0008-3 CHECK VALVE 2 009519-05 SWITCH, AIRFLOW SENSOR 2 009519-06 SWITCH, AIR FLOW SENSOR 1 009519-08 SWITCH, AIR FLOW 1 0108084-05 SYSTEM PILOT RESTRAINT 5 0108084-101 SYSTEM PILOT RESTRAINT 1 016498-03
,00 X X X. Aircraft Jacking Set for Narrow Body (incl. axle jacks (3each), control desk and cable car)
OPP.ENG@s7.ru REV. 20.06.2018 1 950,00 X X X 2 950,00 X X X 3 950,00 X X X 4 950,00 X X X 5 1 200,00 X X X 6 1 200,00 X X X 7 1 200,00 X X X 8 1 200,00 X X X 9 1 200,00 X X X 10 5 000,00 X X X 11 12 OPTIMUM
Mooney Mite M-18X Plans and Drawings Index Arranged by Group Miscellaneous Group
Miscellaneous Group 110470 Bushings - Special 314410 Airspeed & Altimeter Installation 110190 Arm - Landing Warning 110070 Button - Static Airspeed 213260 Cone - Wing Fillet 110120 Control - Placard 616100
General. 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
CHAPTER 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
TABLE OF CONTENTS FLIGHT CONTROLS. Page. 10-i
Chapter 10: Flight Controls TABLE OF CONTENTS Page Introduction...10-1 Description...10-2 Primary Flight Controls...10-2 Secondary Flight Controls...10-4 Spoiler System...10-4 Trim Control...10-4 High
General. Lateral Control System. Longitudinal Control System
Flt.0 Flight Controls-Description and Operation General All primary and secondary flight controls are hydraulically powered, each by at least two, and in some cases, by all three airplane hydraulic systems.
Chapter 27 FLIGHT CONTROLS
Chapter 27 FLIGHT CONTROLS 27-Title Page 1 January 23, 2012 INTENTIONALLY LEFT BLANK 27-Title Page 2 January 23, 2012 LIST OF EFFECTIVE PAGES Chapter Section Page No. Date 27 27-Title 1 January 23, 2012
11/15/ Right S/N FWA-3829 TSN TSO TIME/CALENDAR LIMIT HOURS HOURS HOURS HOURS HOURS HOURS
Engine Model AIRCRAFT STATUS REPORT A/C Reg# B A/C S/N FL-8. TSO. Right S/N FWA-8 TSN. TSO.. TSO. TSHSI.8 CSN, CSO, Right S/N PCE-PK TSN. TSO. TSHSI.8 CSN,8 CSO,8 LINE PHASE and INSPECTION --.. Prop Model
SECTION 2-13 FLIGHT CONTROLS
SECTION 2-13 TABLE OF CONTENTS Block General... 2-13-05..01 Pitch Control... 2-13-10..01 General... 2-13-10..01 Elevator... 2-13-10..02 General... 2-13-10..02 Jammed Elevator... 2-13-10..02 Jammed Elevator
Presenting the HYD-LDG-BRK
Page 1 Presenting the HYD-LDG-BRK Global Aerospace Training Systems 7955 Calle De Gato Redding, CA. 96001 Toll Free 877-688-6753 / International call 530-244-3373 / Fax 530-244-7245 www.gats.net or email
SECTION 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),
A 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
(Attachment) Docket Number
(Attachment) Docket Number 155181227 June 2018 Ministry of Land, Infrastructure, Transport and Tourism Japan Civil Aviation Bureau Aviation Safety and Security Department Air Transport Safety Unit Subject:
BOOTSTRAP PRESSURE 2,400 PSI NOSEWHEEL STEERING LNDG GEAR AILERONS SPEEDBRAKES GROUND SPOILERS HYD FAN 1 THRUST REVERSERS
Hydraulic System LEFT FEED BUS LEFT CB ANEL 2 RESSURE- OERATED RESERVOIR FIREWALL SHUTOFF LH ENGINE FIRE USH 150 IN 3 LOW FLUID LEVEL SHUTOFF VALVE 150 IN 3 2 RH ENGINE FIRE USH XOVR RIGHT FEED BUS LEFT
TORNADO II, S, & SS FUSELAGE TRACKING
TORNADO II, S, & SS FUSELAGE TRACKING 92-INS-0176-C Nose Fork Assembly Instructions Approved 92-INS-0178-D Spindle and Brake Assembly Approved 92-INS-0181-F Anti Servo Control Assembly Approved 92-INS-0182-C
Dimensions And Areas. 1. General. A. Airplane Dimensions and Areas
Dimensions And Areas 600: DIMENSIONS AND AREAS 1. General This section describes those diagrams and text which shows the area, dimensions, stations, access doors, and physical locations of the structural
L 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
Cause of AA587 A R
Another Possible Cause of AA587 A300-605R Accident July 18, 2005 This brief report is prepared to explain the possibility that the inertial forces on the control linkages moved control surfaces, or at
The tie to tube front windshield was rounded to avoid a distorted by this point.
CHANGES IN AIRFRAME IBIS MAGIC GS-700 (2.008) Drilling of plastic polycarbonate drill with 9/64 so that it is an amplitude when riveting. The tie to tube front windshield was rounded to avoid a distorted
Push-Pull Controls and Accessories
Solid metal construction Pilot friendly knobs Lifetime lubrication Superior low friction conduit Custom controls available Metal Construction Unlike the controls of our competitors that use plastic, McFarlane
TECHNICAL MANUAL. Approved for public released; distribution is unlimited. I. This copy is a reprint which includes current pages from Change 1 and 2.
TM 55-1520-210-23P-3 TECHNICAL MANUAL AVIATION UNIT AND INTERMEDIATE MAINTENANCE REPAIR PARTS AND SPECIAL TOOLS LIST (INCLUDING DEPOT MAINTENANCE REPAIR PARTS AND SPECIAL TOOLS) FOR HELICOPTER, UTILITY
Embraer Systems Summary [Landing Gear & Brakes]
![Embraer Systems Summary [Landing Gear & Brakes]](/thumbs/87/96901154.jpg "Embraer 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.
CHAPTER 29 HYDRAULICS Description Hydraulic Pump Hydraulic Reservoir Hydraulic Servos
Section Title CHAPTER 29 HYDRAULICS 29-00 Description............................................... 29.1 29-10 Hydraulic Pump............................................ 29.1 29-20 Hydraulic Reservoir.........................................
A Simplified Index of Mooney M-18 Drawings at the NASM
A Simplified Index of Mooney M-18 Drawings at the NASM Dwg. No. Dwg. date Title Models Remarks IDnum Price 0000 23-Aug-54 M-18 Aileron Crank Mooney M-18 17 x 22 DD-0029487 $2.10 0000 [Lower Pick-Up Strap
Inventory 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
Examen 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:
JAS ENGINEERED SOLUTIONS SM FAA-PMA PARTS
1 59943 PDM59943 Commutator Brush DHC-6 2 255649 PDM255649 Yellow Burst Disc DHC-6 3 396626 PDM396626 Wire Clamp DHC-6 4 398602 PDM398602 Fuel Tank Gasket DHC-6* 5 700246 PDM700246 Check Valve DHC-6* 6
ATR72 DGCANO SUBJECT REFERENCE COMPLIANCE APPLICABILITY
DGCA/ATR 72/1 DGCA/ATR 72/2 TO ENSURE THAT FLIGHT CREWS ACTIVATE THE WING & TAIL PNEUMATIC DEICING BOOTS TO PREVENT FATIGUE CRACKING OF THE FUSELAGE & THE PAX. & SERVICE DOORS FAA AD 99-19-10 FAA AD 2000-04-13
OVERHEAD 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
SECTION 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
Yaw Control and Trim. 1. General. A. Yaw Control System. B. Yaw Trim System
CIRRUS AIRPLANE MAINTENANCE MANUAL MODELS SR AND SRT Yaw Control and Trim CHAPTER 7-0: YAW CONTROL AND TRIM GENERAL 7-0: YAW CONTROL AND TRIM. General This section describes that portion of the flight
CIRRUS AIRPLANE MAINTENANCE MANUAL
ELEVATOR AND PITCH TRIM SYSTEM 1. DESCRIPTION This section describes that portion of the flight control system which controls the position and movement of the elevator. Included are; elevator system torque
77777 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
MOONEY MITE AIRCRAFT DRAWINGS NASM Archives Accession No HOW TO ORDER COPIES OF DRAWINGS
SI-382712 BLUEPRINT MOONEY MITE AIRCRAFT DRAWINGS NASM Archives Accession No.1989-0028 HOW TO ORDER COPIES OF DRAWINGS NASM s collection of Mooney M-18 Mite drawings is available to restorers, researchers,
#1 ENG. 6/4/ apu APU HOURS HOBBS
APU 2145.3 HOBBS airframe inspections 30 DAY INSPT PREFLIGHT DETAL 2/4/2016 30 DAY 3/5/2016 12 MONTH 8/1/2015 8968.2 12 MONTH 8/1/2016 24 MONTH 7/1/2014 24 MONTH 7/1/2016 48 MONTH 7/1/2014 48 MONTH 7/1/2018
Chapter 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
SNOW ENGINEERING CO. ENGINEERING NUMBER 02 Wichita Falls, Texas REPORT ORDER MODEL All
LETTER INDE DATE *6/21/17 PAGE 1 OF *5 * 401/402 SERVICE INFORMATION LETTERS 0001 Flap Actuator Travel Limit Mircro Switches 0002 Hopper Rinse Spray Ball 0003 Converting to Argentine Configuration 0004
canadair 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
REDELIVERY C- CHECK PACKAGE TASK OF B ER AIRCRAFT S2-AHL (MSN 32630) (PHASE#14 INCLUDING ALL LESSER CHECKS) THRES. REPEAT ZONE ACCESS
REDELIVERY C- CHECK PACKAGE OF B777-200ER AIRCRAFT S2-AHL (MSN 32630) AMP 1 05-001-BG-01 DEMO REDELIVERY REDELIVERY 12 2 08-12-CAAB-01 08-12-00-580 MSR 05 YR 05 YR 4 3 12-001-BG-01 12-25-01 CLN 1000 FH
Landing 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,
Revision Status AMM C3 2/1/2009 C OF A 7/15/2002 Revision Status AFM C6 12/1/ INSPECTION REQUIREMENT
Date: 4.29.10 AFTT: 2353.7 Reg# N427JS AFTC: 3100 Ser# BB-1801 HOBBS: 2353.7 #1 Eng PT6A-42 TSN: 2353.7 TSO: N/A TSHSI: 588.1 Ser# PCE-PJ0630 CSN: 3100 CSO: N/A CSHSI: 978 #2 Eng PT6A-42 TSN: 2353.7 TSO:
~eechcraft. Twin-Bonanza TABLE OF CONTENTS
~eechcraft Twin-Bonanza TABLE OF CONTENTS A Absorber Main Landing Shock Nose Gear Shock Accessories & Loose Tools Accumulator Propeller Unfeathering. Valve, Propeller Actuator Aileron Tab Bracket, Rudder
Aeroplane 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
DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT SPECIFICATION NO. 1A Piper Drive Vero Beach, Florida 32960
DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION 1A6 Revision 33 PIPER PA-22 PA-22-108 PA-22-135 PA-22S-135 PA-22-150 PA-22S-150 PA-22-160 PA-22S-160 February 12, 1999 AIRCRAFT SPECIFICATION
CHAPTER 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
Caution Notes. Features. Specifications. Installation. A3 3-axis Gyro & Stabilizer User Manual V1.0
Caution Notes Thank you for choosing our products. If any difficulties are encountered while setting up or operating it, please consult this manual first. For further help, please don t hesitate to contact
The Airplane That Could!
The Airplane That Could! Critical Design Review December 6 th, 2008 Haoyun Fu Suzanne Lessack Andrew McArthur Nicholas Rooney Jin Yan Yang Yang Agenda Criteria Preliminary Designs Down Selection Features
Lot No. 05: List of the Special Tools (U/S) used in DC A/C
Re-RFP No. DACPP/RFP//DC10/F28 SPARES/26-17 Date: 21.09.26 Lot No. 05: List of the Special Tools (U/S) used in DC-10-30 A/C Sl. No. Part No Nomenclature Qty. Remarks. DZZ 7160-1, DZZ7160-2 Torque adapter
CIRRUS AIRPLANE MAINTENANCE MANUAL
DIMENSIONS AND AREAS 1. GENERAL This section describes those diagrams and text which shows the area, dimensions, stations, access doors, and physical locations of the structural members of the airplane.
Instruction Manual book
book ITEM CODE:BH 145 SPECIFICATION Wingspan: 6,000mm 236.22 in. Length : 2,800 mm 110.24 in. Weight : 18.5 kg 40.7 Lbs. Parts listing required (not included). Radio : 07-08 channels. Servo : 09-10 standard
CIRRUS AIRPLANE MAINTENANCE MANUAL
MODEL SR0 YAW CONTROL AND TRIM. GENERAL This section describes that portion of the flight control system which controls the position and movement of the rudder. Included are; rudder system rigging, rudder
Trainer Assembly Manual
Trainer Assembly Manual www.pilot-rc.com -Pilot Trainer- 1 -Pilot Trainer- 2 -Pilot Trainer- 3 -Preliminary i wing & stab assembly- 1-) Locate both Plywood wing joiners (Large and small one) 2-) Insert
SD3-60 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
A.M.M. Revision Status AMM B30 May-14 C OF A 23-May-03 A.L.M. Revision Status ALM B Mar-14 AFM Revision Status AFM B3 Jul-05
Date: 6/17/2015 AFTT: 2724.5 Reg# N629JG AFTC: 2617 Ser# LJ-1688 HOBBS: 2724.5 #1 Eng PT6A-21 TSN: 2724.5 TSO: TSHSI: 930.8 Ser# PCE-PE0515 CSN: 2617 CSO: CSHSI: 744 #2 Eng PT6A-21 TSN: 2724.5 TSO: TSHSI:
INTRODUCTION. This Catalog:
Editor s Note: This Parts Catalog has been reproduced from the original Republic Parts Catalog. Obviously, most of the information is obsolete; the pictures are accurate and up-to-date. If nothing else,
SUPER KING AIR 200 SERIES MAINTENANCE MANUAL SCHEDULED INSPECTION PROGRAM (PHASE 1)-MAINTENANCE PRACTICES A. NOSE SECTION ATA/GAMA REFERENCE
200200200 SCHEDULED ECTION PROGRAM (PHASE 1)-MAINTENANCE PRACTICES Owner W /O Num ber Date In Date Out SerialNo. Reg.No. LastInspection Phase LastInspection Date LastInspection Hours Hourm eter TotalTim
MODEL 95 PARTS CATALOG ALPHABETICAL INDEX , 21, 21A 31 3, 4, 4A , 58A 60 61A, 61B, 61C
A MODEL 5 PARTS CATALOG FIGURE A FIGURE Access Doors, Wing Accessories 7 Accumulatn~.' Propeller Governor Unfeathering. 56 Actuator Aileron T"JJ. Cover, Fl2v Cowl Flap Elevator Tab. Flap. Landing Gear
TRAINING NEEDS ANALYSIS COURSE SYLLABUS & CONTENT
TRAINING NEEDS ANALYSIS COURSE SYLLABUS & CONTENT Course Title: BOEING 787 GENERAL FAMILIARISATION FOUNDATION Mechanical (Electrical Power / Airframe / Powerplant / Avionics) General Standard This syllabus
HYDRAULICS & LANDING GEAR
IC~--u U ; ~~^U ul'h HYDRAULICS & LANDING GEAR TABLE OF CONTENTS Hydraulic System.....................................................................................3-1 HYD PUMP Switch................................................................................3-2
LAD 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
TYPE CERTIFICATE DATA SHEET NO. 2H2. Wilbarger County Airport Airport Drive Vernon, Texas 76384
DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION 2H2 Revision 23 BRANTLY (YHO 3BR) B-2 B-2A B-2B August 14, 2002 TYPE CERTIFICATE DATA SHEET NO. 2H2 This data sheet which is part of type certificate
HELIWORK SERVICES UK APPROVED CAPABILITY MANUAL. Ref: HW/ENG/145/3. Issue 6
HELIWORK SERVICES Ref: HW/ENG/145/3 Issue 6 Dated: 16 October 2013 General INTRODUCTION Section: 0.1 Issue: 6 Rev: 1 Date: 01/06/2016 This Approved Capability Manual Ref HW/ENG/145/3 contains a detailed
Aircraft Hydraulic Systems Design and Performance
Unit T25: Aircraft Hydraulic Systems Design and Performance Unit code: T/504/0126 QCF level: 6 Credit value: 15 Aim The aim of this unit is to give learners an understanding of the principles that underpin
IHI Sustainability Report 2016
IHI Sustainability Report 2016 IHI SUSTAINABILITY REPORT2016 1 IHI SUSTAINABILITY REPORT2016 2 IHI SUSTAINABILITY REPORT2016 3 IHI SUSTAINABILITY REPORT2016 4 IHI SUSTAINABILITY REPORT2016 5 IHI SUSTAINABILITY
IDEA INTERNATIONAL HELICOPTER ACCESSORY SERVICE, INC. (HAS) PARTS
IDEA INTERNATIONAL HELICOPTER ACCESSORY SERVICE, INC. (HAS) PARTS Please read the information below for a list of the parts we currently have for our clients:! #34 54 #34 54!!! 6 70 8! " ' ( ",., 9: 4
AEROPRO Checklist B Service/Maintenance
AEROPRO Checklist B Service/Maintenance 2 Periodic maintenance AIRFRAME Maintenance Interval Time Limitation - after first 25 2 hours when reached - after first 50 3 hours when reached - after 100 5 hours
DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT SPECIFICATION NO. 1A9. 4 Baltimore Avenue Georgetown, DE 19947
DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT SPECIFICATION NO. 1A9 1A9 Revision 18 Taylorcraft 2000, LLC 19 F19 F21 F21A F21B F22 F22A F22B F22C August 8, 2000 Type Certificate
Instruction Manual EXTRA 260-EP. 1075mm (42.32 in) 1000mm (39.37 in) 1100gr gr. 4 channel - 4 mini servo. Axi motor 2820
1075mm (42.32 in) 1000mm (39.37 in) 1100gr - 1400gr 4 channel - 4 mini servo Axi motor 2820 KIT CONTENTS: We have organized the parts as they come out of the box for better identification during assembly.
Instruction Manual MUSTANG P51 - EP. Wingspan : 1377mm (54.21in) : 1180mm (46.46 in) : 2200gr gr. : AXI motor 2826 or 4120
Instruction Manual MUSTANG P51 - EP Wingspan : 1377mm (54.21in) g Length : 1180mm (46.46 in) Weight : 2200gr - 2600gr Engine : AXI motor 2826 or 4120 Radio : 4 channel / 4 servos standard KIT CONTENTS:
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
DASSAULT 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
Airworthiness Directive Schedule
Airworthiness Directive Schedule Aeroplanes 30 July 2015 Notes 1. This AD schedule is applicable to De Havilland Canada DHC-2 Beaver MK I aircraft manufactured under Transport Canada Type Certificate Number:
N416WM. 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
/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.
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
Instruction Manual book
Instruction Manual book ITEM CODE:BH135 SPECIFICATION Wingspan : 4,200mm. 163.35 in. Length : 2,100 mm. 82.68 in. Weight : 7,6 kg. 16.72lbs Radio : 07 channels. Servo : 05 06 standard high torque servos,