Thrust Reverser System

Size: px
Start display at page:

Download "Thrust Reverser System"

Transcription

1 Thrust Reverser System LEFT FEED BUS LEFT CB PANEL LH T/R 3,000 PSI ISOLATION VALVE SPRING 200 PSI PRESSURE SITCH SOLENOID CONTROL VALVE ( POSITION SHON) Thrust Reverser System 7.5A XOVER RIGHT FEED BUS LEFT CB PANEL RH T/R RETURN 5A ARN LITE 1 SOLENOID 7.5A RESTRICTOR ARM UNLOCK S T O S EMER NORM BOTTLE 1 ARMED LH ENG FIRE RH ENG FIRE BOTTLE 2 ARMED EMER S T O NORM S ARM UNLOCK AIR GND SQUAT SITCH TO LH RIGHT THROTTLE / SITCH TO LH T/R ED ED POSITION SHON UNLOCK LIMIT S ED HYDRAULIC PRESSURE HYDRAULIC RETURN STATIC PRESSURE THROTTLE LOCK SOLENOID ED OR TRANSIT LIMIT SITCH RIGHT THRUST REVERSER Citation III/VI For training only 4L-1

2 4L-2 For training only Citation III/VI

3 Thrust Reversers hen deployed, the hydraulically operated and electrically controlled thrust reversers deflect engine thrust forward to decrease landing roll and brake wear. Deploy Before thrust reverser deployment can begin, the throttle levers must be in the idle position and the squat switches must be in the ground-on-ground mode (main landing gear struts compressed). Pulling the thrust reverse levers up begins the deploy sequence by moving the throttle stow/deploy switches to the deploy position. DC power from the Left Feed bus and Crossover Right Feed bus energizes the left and right isolation and control valves. The isolation valves shifts to the open position and the control valves shift to the deploy position. Hydraulic fluid at 3,000 PSI flowing through the isolation valves close pressure switches that illuminate the ARM lights. Hydraulic fluid then continues through the control valves to the deploy side of the four thrust reverser actuators (two per side). The actuators retract to pull the thrust reverser carriage forward along the support assembly guide rods. Carriage movement unlocks the overcenter links that, in turn, exert force on the driver links that extend the thrust reverser doors into the engine exhaust path. Movement of carriage also actuates stow limit switches that illuminate the UNLOCKED lights. hen the thrust reverser doors reach the fully deployed position, deploy limit switches actuate to illuminate the lights and release the thrust reverser interlock solenoid. Pulling back on the thrust reverser levers after the lights illuminate, increases reverse thrust. Citation III/VI For training only 4L-3

4 Stow Moving the thrust reverser levers forward and down begins the stow sequence by moving the throttle stow/deploy switches to the stow position. DC power flows to the control valves stow solenoid; the control valves shift to the stow position. Hydraulic fluid under pressure then flows to the stow side of the actuators, and the thrust reversers begin stowing. As they begin stowing, the deploy limit switch de-actuates to extinguish the lights. hen the reverser mechanism stows and locks, the stow limit switch de-actuates and the UNLOCKED lights extinguish. The ARM lights remain illuminated until the isolation valve shifts to cut hydraulic pressure to the thrust reverser system. Emergency Stow If a thrust reverser unlocks or begins deploying in flight, a feedback mechanism between the thrust reverser operating mechanism and the throttle levers forces the affected throttle lever to the idle thrust position. Placing the S in the EMER position supplies 28V DC to energize the isolation valve and the control valve s stow solenoid. Hydraulic pressure then flows through the isolation valve and control valve to the stow side of the thrust reverser actuator. the thrust reverser stows and locks. The ARM light remains illuminated as long as the isolation valve is open and hydraulic pressure exists in the thrust reverser system. 4L-4 For training only Citation III/VI

5 Thrust Reversers Thrust Reverser System Power Source Control Monitor Protection Left Feed bus Crossover Right Feed bus Hydraulic system Thrust reverser levers S (NORM/EMER) ARM/UNLOCK/ annunciators MASTER ARNING lights LH/RH TR circuit breakers Squat switches Citation III/VI For training only 4L-5

6 4L-6 For training only Citation III/VI

BOOTSTRAP PRESSURE 2,400 PSI NOSEWHEEL STEERING LNDG GEAR AILERONS SPEEDBRAKES GROUND SPOILERS HYD FAN 1 THRUST REVERSERS

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

More information

EMERGENCY GEAR DOWN HANDLE CHECK VALVE GEAR DROP TO EXTEND POSITION DOOR SELECTOR DOOR SELECTOR VALVE UPLOCK RELEASE CYLINDER DOOR CYLINDER

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

More information

Bombardier Global Express - Hydraulics

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

More information

Pneumatic Air Conditioning System Citation, Citation I

Pneumatic Air Conditioning System Citation, Citation I Pneumatic Air Conditioning System Citation, Citation I COCKPIT VENT FOOT WARMER OVERHEAD COCKPIT WINDSHIELD WEMAC OPTIMAL VENT OVERHEAD CONDITIONED AIR DUCTS BLOWER SIDE WINDOW UNDER FLOOR CONDITIONED

More information

Cessna Citation XLS - Electrical

Cessna 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 information

CHAPTER 14 LANDING GEAR

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

More information

CHAPTER 6 ELECTRICAL SYSTEMS

CHAPTER 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 information

Chapter Four CASTER POWER-BACK AND INDICATION SYSTEM

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

More information

HYDRAULICS & LANDING GEAR

HYDRAULICS & LANDING GEAR IC~--u U ; ~~^U ul'h HYDRAULICS & LANDING GEAR TABLE OF CONTENTS Hydraulic System.....................................................................................3-1 HYD PUMP Switch................................................................................3-2

More information

SECTION III HYDRAULICS & LANDING GEAR

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

More information

King Air B90. Speeds (KIAS)

King Air B90. Speeds (KIAS) King Air B90 Speeds (KIAS) V MCA 92 V SSE (101) Derived from C90 V X 101 V Y 114 Down to 103 @ 30 000 V XSE 101 V YSE 110 Down to 101 @ 24 000 V A 169 V R 92 V 1 101 V MO 208 V FE 174 35% 130 100% V LE

More information

canadair chsfflencjibr

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

More information

SECTION II AIRPLANE AND SYSTEMS MODEL 750 HYDRAULIC

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),

More information

CESSNA CITATION C750 (CITATION X) PUNTA BRAVA S.A. (Rev Abril 2012)

CESSNA CITATION C750 (CITATION X) PUNTA BRAVA S.A. (Rev Abril 2012) DEPARTAMENTO SEGURIDAD OPERACIONAL SUBDEPARTAMENTO LICENCIAS SECCIÓN EVALUACIONES CESSNA CITATION C750 (CITATION X) PUNTA BRAVA S.A. (Rev. 2-10 Abril 2012) A.- LIMITATIONS: 1.- Limitations ( KIAS) V (Turbulence

More information

/200/300/400/500 SERIES FLAMMABLE MATERIAL LOCATIONS

/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 information

Throttle Quadrant Operating Manual English Version

Throttle Quadrant Operating Manual English Version Throttle Quadrant Operating Manual English Version Cockpitsonicversion1 Page1 Contents 1. Introduction... 3 2. Installation... 3 3. Calibration... 5 4. Using Your Throttle Quadrant... 9 5. Contact Details...

More information

. OPERATING INSTRUCTION MANUAL NO. 548-A

. OPERATING INSTRUCTION MANUAL NO. 548-A WABCO ~. OPERATING INSTRUCTION MANUAL NO. 548-A SATELLITE LOCOMOTIVE REMOTE CONTROL SYSTEM. I,t UNION SWITCH & SIGNAL DIVISION Westinghouse Air Brake Company PITTSBURGH.PA. 15218 SepteITiber, 1963 Al.63-250-848.2

More information

CHAPTER 12. Page TABLE OF CONTENTS /02 DESCRIPTION. General Description Controls and Indicators COMPONENTS

CHAPTER 12. Page TABLE OF CONTENTS /02 DESCRIPTION. General Description Controls and Indicators COMPONENTS CHAPTER 12 HYDRAULIC POWER Page TABLE OF CONTENTS 12-00-01/02 DESCRIPTION General 12-10-01 Description 12-10-01 Controls and Indicators 12-10-02 COMPONENTS Hydraulic System Block Diagram 12-20-01/02 CONTROLS

More information

REFERENCE: 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 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 information

E4610 (2 8160) Wing Landing Gear Retract Actuator Assy E4620 (2 8189) Wing Landing Gear Unlock Actuator Assy

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

More information

DASSAULT AVIATION Proprietary Data

DASSAULT AVIATION Proprietary Data F2000EX EASY 02-70-00 CODDE 1 PAGE 1 / 2 TABLE OF CONTENTS 02-70 02-70-00 TABLE OF CONTENTS 02-70-05 GENERAL Introduction Sources Engine location 02-70-10 DESCRIPTION Introduction Major components Operating

More information

United States Army Warfighting Center Fort Rucker, Alabama NOVEMBER 2006

United States Army Warfighting Center Fort Rucker, Alabama NOVEMBER 2006 United States Army Warfighting Center Fort Rucker, Alabama NOVEMBER 2006 STUDENT HANDOUT TITLE: CH-47D ENGINE CONTROL SYSTEM FILE NUMBER: 011-2109-3 PROPONENT FOR THIS STUDENT HANDOUT IS: 110 th Aviation

More information

ATA 49 AUXILIARY POWER UNIT

ATA 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 information

General. Gear Retraction and Extension

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

More information

FUEL MODEL 750 BAGGAGE COMPARTMENT SMOKE DETECTION

FUEL MODEL 750 BAGGAGE COMPARTMENT SMOKE DETECTION MODEL 750 SECTION II AIRPLANE AND SYSTEMS System test is accomplished by turning the cockpit rotary test switch to FIRE WARN. Proper system operation is indicated by illumination of the APU FIRE indicating

More information

Landing Gear & Brakes

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,

More information

LANDING GEAR. Table of Contents. Sep 13/2004 Flight Crew Operating Manual Volume 2 REV 1 CSP REV 1

LANDING 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 information

EMERGENCY PROCEDURES ENGINE FIRE DURING START/GROUND OPERATIONS STARTER ENERGIZED ANNUNCIATOR ILLUMINATED. Memory items are printed in red.

EMERGENCY PROCEDURES ENGINE FIRE DURING START/GROUND OPERATIONS STARTER ENERGIZED ANNUNCIATOR ILLUMINATED. Memory items are printed in red. ENG FIRE-GRND, STARTER ENERGIZED EMERGENCY PROCEDURES Memory items are printed in red. ENGINE FIRE DURING START/GROUND OPERATIONS 1. Mixture...IDLE CUTOFF 2. Fuel Selector Valve... OFF 3. Battery, Alternator,

More information

Surface and Brakes Anti-Ice Systems

Surface 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 information

General. APU Control System. APU Door System

General. APU Control System. APU Door System .10 -Description and Operation General The Auxiliary Power Unit () provides electrical and pneumatic power for engine start and air conditioning, and supplies ground and in-flight electrical power. Pneumatic

More information

FLIGHT SIMULATOR SYSTEMS

FLIGHT SIMULATOR SYSTEMS FLIGHT SIMULATOR SYSTEMS 1. GENERAL This section describes systems required for simulator operation. This equipment includes the Cirrus Landing Gear Simulator (CLGS). 2. DESCRIPTION The intent of the CLGS

More information

OVERHEAD PANEL PROCEDURES FLASH CARDS

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

More information

GIV MEMORY FLASH CARDS OCT09

GIV MEMORY FLASH CARDS OCT09 OCT09 GIV MEMORY FLASH CARDS Copyright 2009, FlightSafety International, Inc. Unauthorized reproduction or distribution is prohibited. All rights reserved. INSERT LATEST REVISED CARDS, DESTROY SUPERSEDED

More information

FLIGHT CONTROLS SYSTEM

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.

More information

B737 NG Anti Ice & Rain

B737 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 information

AIRCRAFT SYSTEMS HYDRAULIC

AIRCRAFT SYSTEMS HYDRAULIC Intentionally left blank PRELIMINARY PAGES - TABLE OF CONTENTS DSC-29-10 Description DSC-29-10-10 General GENERAL... A DSC-29-10-20 Generation GREEN SYSTEM PUMP...A BLUE SYSTEM PUMPS...B YELLOW SYSTEM

More information

The Straight Word. Beechcraft 90 King Air B90 Series. Condition Lever. Set for Takeoff Cabin Altitude Controller Set Cruise Level + 1

The Straight Word. Beechcraft 90 King Air B90 Series. Condition Lever. Set for Takeoff Cabin Altitude Controller Set Cruise Level + 1 The Straight Word Beechcraft 90 King Air B90 Series I. FLIGHT PROCEDURES: COCKPIT PREPARATION Heading Bug Set QFU HSI Course Indicator Set Course Altimeters Set QNH Power Levers Idle Propeller Levers Max

More information

OUTLINE. Commercial Requirements Insurance Mins Basic Info Systems Limitations Performance Charts Questions

OUTLINE. Commercial Requirements Insurance Mins Basic Info Systems Limitations Performance Charts Questions T-34B GROUND SCHOOL OUTLINE Commercial Requirements Insurance Mins Basic Info Systems Limitations Performance Charts Questions COMMERCIAL REQUIREMENTS 61.129 Aeronautical experience. (a) For an airplane

More information

Canadair Regional Jet 100/200 - Auxiliary Power Unit

Canadair 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 information

POWER SOURCE (Current Flow Chart)

POWER SOURCE (Current Flow Chart) POWER SOURCE (Current Flow Chart) The chart below shows the route by which current flows from the battery to each electrical source (Fusible Link, Circuit Breaker, Fuse, etc.) and other parts. The next

More information

Examen Teórico sobre Habilitación de Tipo B (Última actualización: Septiembre 2016)

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:

More information

LANDING GEAR TABLE OF CONTENTS CHAPTER 15

LANDING 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 information

G ELECTRICAL WIRING ROUTING

G ELECTRICAL WIRING ROUTING G ELECTRICAL WIRING ROUTING Position of Parts in Engine Compartment A 1 A/C Condenser Fan Motor A 2 A/C Magnetic Clutch and Lock Sensor A 3 A/C Triple Pressure SW (A/C Dual and Signal Pressure SW) A 4

More information

Dornier 328Jet - Pneumatic

Dornier 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 information

DASSAULT AVIATION Proprietary Data

DASSAULT AVIATION Proprietary Data FALCON 7X 02-70-05 CODDE 1 PAGE 1 / 6 GENERAL ACRONYMS LIST ACOC AGB APU A/T ATSV BOV CAS CB CL CMC CR DC DCU ECS EEC FADEC FBW FCU FF FOHE FSOV HP HPC HPT IGV ITT LP LPC LPT LRU MV N1 N2 PDU PLA PMA PMU

More information

Position of Parts in Engine Compartment

Position of Parts in Engine Compartment ELECTRICAL WIRING ROUTING [3S GTE] Position of Parts in Engine Compartment A 1 A/C Ambient Temp. Sensor D 1 Date Link Connector 1 (Check Connector) A 2 A/C Condenser Fan Motor D 2 Distributor A 4 A/C Magnetic

More information

Flaps System. 1. General

Flaps System. 1. General CIRRUS AIRPLANE MAINTENANCE MANUAL Flaps System CHAPTER 27-50: FLAPS SYSTEM GENERAL 27-50: FLAPS SYSTEM 1. General This section describes that portion of the flight control system which controls the position

More information

Briefings & Checks. Robinson RH44 Raven II. Briefings & Checks Robinson RH44 Raven II. Helicopter Data (Meteo / NOTAM / DABS / W&B)

Briefings & Checks. Robinson RH44 Raven II. Briefings & Checks Robinson RH44 Raven II. Helicopter Data (Meteo / NOTAM / DABS / W&B) Briefings & Checks Helicopter Data (Meteo / NOTAM / DABS / W&B) 1. Immatriculation: HB- 2. Empty weight: lbs 3. Main fuel: (USG x 6= lbs) lbs 5. Pilot / Pax / Baggage: lbs 6. actual TOM / HOGE: lbs / HOGE

More information

Pilot's Manual Wcyflom v# ANTI-ICE & ENVIRONMENTAL. Learjet 31A

Pilot's Manual Wcyflom v# ANTI-ICE & ENVIRONMENTAL. Learjet 31A Pilot's Manual Wcyflom v# ANTI-ICE & ENVIRONMENTAL TABLE OF CONTENTS Anti-ice Systems........................................................................................ 6-1 Ice Detect Lights.....................................................................................6-1

More information

BEFORE START AFTER START

BEFORE START AFTER START BEFORE START ENGINE START AFTER START - Version 03 1.a. BEFORE START LOADSHEET...CHECK TAKEOFF DATA..... ENTER/REVISE TAKEOFF DATA... XCHECK COCKPIT DOOR...CLOSED SEAT BELTS ADJUST MCDU...PERF TO SEAT

More information

Bombardier Challenger Auxiliary Power Unit

Bombardier 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 information

PREFLIGHT cont. PREFLIGHT A/C documents. RH fuel drain. RH wing+aileron+flap. Pitot and static system. Master switch BEFORE STARTING ENGINE

PREFLIGHT cont. PREFLIGHT A/C documents. RH fuel drain. RH wing+aileron+flap. Pitot and static system. Master switch BEFORE STARTING ENGINE PREFLIGHT A/C documents Landing gear ctrol All Aviics All Electric ctrol Flight ctrols Pitot and static system Landing gear lights Fuel indicati Pitot tube External lights Stall warning All electric down

More information

C I R R U S DISTRIBUTION DESCRIPTION

C I R R U S DISTRIBUTION DESCRIPTION MODELS SR AND SRT DISTRIBUTION. DESCRIPTION This section contains information on the distribution system. The fuel distribution system consists of electric and mechanical (engine-driven) fuel pumps, fuel

More information

DASSAULT AVIATION Proprietary Data

DASSAULT 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 information

ABS and Tire Pressure Warning System

ABS and Tire Pressure Warning System S and Tire Pressure arning System D Data Link 3 * : utomatic /C * : Except * SIL TC TS 7 3 8 K 9 L P- 4 K 0 L 7 S Speed Sensor Rear LH 8 S Speed Sensor Rear RH 3 0 7 3 I 5 I IL IL - R - R P- R G LG L -

More information

INDEX. Preflight Inspection Pages 2-4. Start Up.. Page 5. Take Off. Page 6. Approach to Landing. Pages 7-8. Emergency Procedures..

INDEX. Preflight Inspection Pages 2-4. Start Up.. Page 5. Take Off. Page 6. Approach to Landing. Pages 7-8. Emergency Procedures.. INDEX Preflight Inspection Pages 2-4 Start Up.. Page 5 Take Off. Page 6 Approach to Landing. Pages 7-8 Emergency Procedures.. Page 9 Engine Failure Pages 10-13 Propeller Governor Failure Page 14 Fire.

More information

Ground Circuit. (TURBO AND STi MODEL) B 3 B 4 REARVIEW MIRROR LH (WITH MIRROR HEATER) F17 CRUISE CONTROL MODULE F101 B94 POWER WINDOW RELAY F22 B225

Ground Circuit. (TURBO AND STi MODEL) B 3 B 4 REARVIEW MIRROR LH (WITH MIRROR HEATER) F17 CRUISE CONTROL MODULE F101 B94 POWER WINDOW RELAY F22 B225 . A: IRING DIAGRAM IRING SYSTEM GND-0 SU FAN MOTOR (TURO AND STi MODEL) F MAIN FAN MOTOR (NON-TURO MODEL) MAIN FAN MOTOR (TURO AND STi MODEL) HEADLIGHT LH LO-EAM (HID MODEL) HEADLIGHT RH LO-EAM (HID MODEL)

More information

The parking brake is an electrically actuated system that operates drum brakes integrated into the rear brake discs. The

The parking brake is an electrically actuated system that operates drum brakes integrated into the rear brake discs. The Page 1 of 15 Published: Oct 22, 2004 Parking Brake COMPONENT LOCATIONS Item Part Number Description 1 Clutch pedal position sensor (manual transmission models only) 2 Parking brake indicators (all except

More information

The Straight Word. Cessna 337 Skymaster 337C Series. The front engine should always be started first as the battery-to-starter cable is shorter.

The Straight Word. Cessna 337 Skymaster 337C Series. The front engine should always be started first as the battery-to-starter cable is shorter. The Straight Word Cessna 337 Skymaster 337C Series I. FLIGHT PROCEDURES: COCKPIT PREPARATION Heading Bug OBS Indicator Altimeters Trims Parking Brake Set QFU Set Course Set QNH Set for Takeoff Apply ENGINE

More information

Service Bulletin No. 2905

Service Bulletin No. 2905 MODEL TYPE SECTION/GROUP DATE E4500 / J4500 Series Coaches Service Information 22-Wheelchair Lift May 4, 2005 SUBJECT R ICON W HE E L CHAIR L IF T OPE R AT ION CONDITIONS Service Information Only Description:

More information

SD3-60 AIRCRAFT MAINTENANCE MANUAL

SD3-60 AIRCRAFT MAINTENANCE MANUAL AMM 11.0.0.0AUTO-FEATHERING SYSTEM - DESCRIPTION & OPERATION 1. Description A. General This system is employed to speedily reduce propeller drag by automatically feathering the propeller on an engine which

More information

NORMAL CHECKLIST ATTENTION!

NORMAL 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 information

INSTRUCTION MANUAL MODEL # YEAR WARRANTY KUSSMAUL ELECTRONICS CO., INC.

INSTRUCTION MANUAL MODEL # YEAR WARRANTY KUSSMAUL ELECTRONICS CO., INC. FILE: 091-84.pmd DATE: 9-21-07 INSTRUCTION MANUAL AUTO THROTTLE 1 MODEL #091-84 AN AUTOMATIC HIGH IDLE CONTROLLER 3 YEAR WARRANTY KUSSMAUL ELECTRONICS CO., INC. 170 CHERRY AVE., WEST SAYVILLE, N.Y. 11796

More information

DOORS Table of Contents REV 3, May 03/05 CHAPTER DOORS. INTRODUCTION Introduction System Circuit Breakers

DOORS 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 information

The Straight Word. Cessna 337 Super Skymaster 337G & T337G Series, and corresponding Reims Aviation models

The Straight Word. Cessna 337 Super Skymaster 337G & T337G Series, and corresponding Reims Aviation models The Straight Word Cessna 337 Super Skymaster 337G & T337G Series, and corresponding Reims Aviation models I. FLIGHT PROCEDURES: COCKPIT PREPARATION Heading Bug OBS Indicator Altimeters Trims Parking Brake

More information

DASSAULT AVIATION Proprietary Data

DASSAULT AVIATION Proprietary Data F900EX EASY 02-30-00 CODDE 1 PAGE 1 / 2 TABLE OF CONTENTS 02-30 02-30-00 TABLE OF CONTENTS 02-30-05 GENERAL Introduction Anti-icing protection sources Anti-ice system location overview 02-30-10 DESCRIPTION

More information

BALLAST UNIT Ea 5 New REPAIRABLE INDICATOR FLAP POSITION Ea 1 Overhauled ROTABLE

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

More information

CHAPTER FUEL SYSTEM

CHAPTER 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 information

Bombardier Challenger Hydraulic System

Bombardier 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 information

PA28R ARROW CHECKLIST

PA28R ARROW CHECKLIST PA28R ARROW CHECKLIST 2300.11.0112 1 Normal Procedures Initial PREFLIGHT CHECK General Appearance... CHECKED Position & Taxi Path... CHECKED Tie Downs, Locks, Chocks & Covers... REMOVED Cockpit Controls...UNLOCKED

More information

Position of Parts in Engine Compartment

Position of Parts in Engine Compartment ELECTRICAL WIRING ROUTING [5S FE] Position of Parts in Engine Compartment A 1 A/C Condenser Fan Motor E 4 Engine Coolant Temp. Sensor (EFI Water Temp. A 2 A/C Magnetic Clutch and Lock Sensor Sensor) A

More information

DASSAULT AVIATION Proprietary Data

DASSAULT 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 information

EXAMEN POR MATERIAS PARA USO DE LOS POSTULANTES A LA HABILITACIÓN DE TIPO EN MATERIAL B733. ENERO 2018

EXAMEN 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 information

TRAINEE T-39 NATOPS WORKBOOK

TRAINEE T-39 NATOPS WORKBOOK NAVAL AIR TRAINING COMMAND NAS CORPUS CHRISTI, TEXAS CNATRA P-857 (REV. 10-02) PAT TRAINEE T-39 NATOPS WORKBOOK FLIGHT TRAINING INSTRUCTION INTERMEIDATE PHASE BASIC SNFO 2002 STUDENT GUIDE T-39N/G NATOPS

More information

CIRRUS AIRPLANE MAINTENANCE MANUAL

CIRRUS AIRPLANE MAINTENANCE MANUAL MODEL SR0 INSTRUMENT AND CONTROL PANEL. DESCRIPTION Serials 00 thru 336, 337 thru w/o PFD: The airplane uses standard flight instruments arranged in the basic-six pattern. The airspeed indicator, attitude

More information

G ELECTRICAL WIRING ROUTING [1MZ-FE] Position of Parts in Engine Compartment

G ELECTRICAL WIRING ROUTING [1MZ-FE] Position of Parts in Engine Compartment G ELECTRICAL WIRING ROUTING [1MZ-FE] Position of Parts in Engine Compartment A 1 A/C Ambient Temp. Sensor A 2 A/C Condenser Fan Motor A 3 A/C Magnetic Clutch and Lock Sensor A 4 A/C Triple Pressure SW

More information

A AMM - KRUEGER FLAP ACTUATOR - REMOVAL/INSTALLATION

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

More information

* Transit flight deck preparation

* Transit flight deck preparation Page 1 Explanations * Transit flight deck preparation Procedures By heart items FFD OUTSIDE CHECK INSIDE CABIN First flight a day 1 Crossfeed drain... DRAINED - Drain crossfeed left hand of left forward

More information

Jump to Table of Contents

Jump 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 information

LH POWER LOCK SYSTEMS 8P - 1 POWER LOCK SYSTEMS TABLE OF CONTENTS POWER DOOR LOCKS... 1 REMOTE KEYLESS ENTRY... 4 POWER DOOR LOCKS TABLE OF CONTENTS

LH POWER LOCK SYSTEMS 8P - 1 POWER LOCK SYSTEMS TABLE OF CONTENTS POWER DOOR LOCKS... 1 REMOTE KEYLESS ENTRY... 4 POWER DOOR LOCKS TABLE OF CONTENTS LH POWER LOCK SYSTEMS 8P - 1 POWER LOCK SYSTEMS TABLE OF CONTENTS POWER DOOR LOCKS... 1 REMOTE KEYLESS ENTRY... 4 POWER DOOR LOCKS TABLE OF CONTENTS AND POWER DOOR LOCK SYSTEM...1 CENTRAL LOCKING SYSTEM...2

More information

G ELECTRICAL WIRING ROUTING [2ZZ GE] Position of Parts in Engine Compartment

G ELECTRICAL WIRING ROUTING [2ZZ GE] Position of Parts in Engine Compartment G ELECTRICAL WIRING ROUTING [2ZZ GE] Position of Parts in Engine Compartment A 1 A/C Magnetic Clutch A 2 ABS Speed Sensor Front LH A 3 ABS Speed Sensor Front RH A 4 Airbag Sensor Front LH A 5 Airbag Sensor

More information

DCS 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 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

BEFORE START AFTER START

BEFORE START AFTER START BEFORE START ENGINE START AFTER START A340 - Version 03b 1.a. BEFORE START LOADSHEET...CHECK TAKEOFF DATA..... ENTER/REVISE TAKEOFF DATA... XCHECK COCKPIT DOOR...CLOSED SEAT BELTS ADJUST MCDU...PERF TO

More information

Presenting the HYD-LDG-BRK

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

More information

System Normal Secondary Direct. All 3 PFC work in parallel. available. Pitch Normal Secondary Direct. Pitch maneuver command.

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

More information

Embraer Systems Summary [Landing Gear & Brakes]

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.

More information

Position of Parts in Engine Compartment

Position of Parts in Engine Compartment ELECTRICAL WIRING ROUTING [5S FE] Position of Parts in Engine Compartment A 1 A/C Ambient Temp. Sensor D 1 Distributor A 2 A/C Condenser Fan Motor A 3 A/C Idle Up VSV E 1 ECT Solenoid A 4 A/C Magnet Clutch

More information

Canadair Regional Jet 100/200 - Fuel System

Canadair 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 information

T his chapter contains instructions for installing the RICON S-Series (ADA) Transit Use Wheelchair and Standee Lift

T his chapter contains instructions for installing the RICON S-Series (ADA) Transit Use Wheelchair and Standee Lift II. INSTALLATION T his chapter contains instructions for installing the RICON S-Series (ADA) Transit Use Wheelchair and Standee Lift with Manual Rollstop into most vans and buses, although custom installations

More information

Chapter 24. Electrical Power

Chapter 24. Electrical Power Chapter 24 Electrical Power PAGE 1 TABLE OF CONTENTS Chapter Title 24-00-00 GENERAL................................................................................................................ 3 24-30-00

More information

The Straight Word. Cessna 208 Caravan 208 Caravan I & 208B Grand Caravan Series

The Straight Word. Cessna 208 Caravan 208 Caravan I & 208B Grand Caravan Series The Straight Word Cessna 208 Caravan 208 Caravan I & 208B Grand Caravan Series I. FLIGHT PROCEDURES: COCKPIT PREPARATION Fuel Tank Selectors Ignition Switch Heading Bug HSI Course Indicator Altimeters

More information

OPERATIONS MANUAL SECTION 6-2

OPERATIONS 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 information

24 ELECTRICAL DC ELECTRICAL SYSTEM DESCRIPTION

24 ELECTRICAL DC ELECTRICAL SYSTEM DESCRIPTION 24 ELECTRICAL DC ELECTRICAL SYSTEM DESCRIPTION The Direct Current electrical system provides power to most equipment through an electrical bus system. The power may be supplied from one of three sources:

More information

SD3-60 AIRCRAFT MAINTENANCE MANUAL & RETRACTION - DESCRIPTION & OPERATION

SD3-60 AIRCRAFT MAINTENANCE MANUAL & RETRACTION - DESCRIPTION & OPERATION AMM 17.0.0.0EXTENSION & RETRACTION - DESCRIPTION & OPERATION 1. Description A. General The landing gear is extended and retracted by the operation of a hydraulic actuator at each of the main and nose gear

More information

DASSAULT AVIATION Proprietary Data

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

More information

LISTA DE PEÇAS CONTROLADAS - LEARJET 35A S/N 479

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

More information

SECTION II ENGINES & FUEL

SECTION II ENGINES & FUEL SECTION II ENGINES & FUEL TABLE OF CONTENTS Engines...2-1 Fuel Control Logic Diagram (Figure 2-1)... 2-2 Engine Fuel and Control System... 2-3 Thrust Levers... 2-3 Engine-Driven Fuel Pump... 2-4 Hydromechanical

More information

FINAL EXAM. 3. Name the items on the control shift in the unmodified aircraft (non ASC-36).

FINAL EXAM. 3. Name the items on the control shift in the unmodified aircraft (non ASC-36). FINAL EXAM Name 1. Total usable fuel is 177 gallons 2. Proper fuel(s) specification for the T-28 is (are): XX (a) 100/130 alternate 100LL (b) 115/145 and 100/130 alternate (c) 115/145 and 100/130 emergency

More information

Dash8-200/300 - Auxiliary Power Unit APU CONTROLS AND INDICATORS. Page 1

Dash8-200/300 - Auxiliary Power Unit APU CONTROLS AND INDICATORS. Page 1 APU CONTROLS AND INDICATORS Page 1 APU control and indicators Page 2 closed APU controls and indicators Page 3 SYSTEM DESCRIPTION General The auxiliary power unit (APU) is a gas turbine engine, located

More information

Cessna 172S Skyhawk. AFTER LANDING CHECK RPM CHECK 2. Flaps UP 3. Transponder STANDBY 4. Strobes OFF 5. Contact Ground as Required. 121.

Cessna 172S Skyhawk. AFTER LANDING CHECK RPM CHECK 2. Flaps UP 3. Transponder STANDBY 4. Strobes OFF 5. Contact Ground as Required. 121. PRE-LANDING CHECK 1. ATIS/AWOS/ASOS OBTAIN 2. Seat Belts CHECK 3. Autopilot OFF 4. Master Switch ON 5. Ignition BOTH 6. Circuit Breakers ALL IN 7. Landing Light AS REQ. 8. Mixture (Push) RICH 9. Fuel Selector

More information