ENGINE GROUND RUNNING
|
|
- Aubrey Logan
- 5 years ago
- Views:
Transcription
1 B /700/800/900 (CFM 56) ENGINE GROUND RUNNING Guide and Reference Sheets This publication is for TRAINING PURPOSES ONLY. This information is accurate at the time of completion. No update service will be furnished to maintain the accuracy of this publication. For authorised maintenance practices and specifications, consult chapter 71 of the pertinent maintenance publication
2 For training purposes only Preparation and Cockpit Management Standardisation of Engineers Simulator Training Briefing to students Ground run preparation using aircraft type check sheets, ramp stability, C of G understanding Cockpit set-up fire testing and APU starting Normal starting and precautions during start. Cross bleed starting Demonstration of abnormal situations during starts Hot start Hung start Starter Cut-out defect Start valve defect Failed ignition on start and switching ignition during starting. N1, N2, N3 fail Spar valve and engine solenoid fail Failed EICAS/CDS screens and standby indications Carry out several starts to see corrective action Fire Drill Engine fire APU fire Cargo bay, Wheel Well Overheat High power operation De-brief Engine runaway Compressor stall, hard and core stall Turbine fail Vibration - Fan and Core Brake system failure during high power Aircraft taxiing and use of thrust reverser to give the student a better understanding of the operation and limitations. The above programme is based on a two hour detail with a change of seats at the half way point for each student to experience the command seat, as the person in charge of the run. The training will be tailored to suit the experience levels of the delegates with first-time delegates getting more in depth instruction to prepare for initial approval application. Revision 1 March
3 For training purposes only Hazard Areas Idle Power B737 Revision 1 March
4 For training purposes only Hazard Areas Take Off Power B737 Revision 1 March
5 For training purposes only Hazard Areas Reverse Idle B737 Full Reverse B737 Revision 1 March
6 Preferred Wind Directions and Speed B737 Revision 1 March
7 Entry Corridors B737 WARNING: Entry/Exit corridors must only be used under the following conditions: Engine at idle or shut down Positive communication between Flt Compartment and external ground staff Use of a safety lanyard is recommended If surface wind is greater than 25 knots increase the distance of the inlet boundary by 20%. If the ramp surface is slippery or contaminated additional precautions may be necessary. Revision 1 March
8 GROUND AND FLT DECK RESPONSIBILITIES B /700/800/900 (CFM56) ENGINE GROUND RUN PROCEDURES GUIDE The Engineer operating (EO Left Hand seat) is responsible for the ground run operation. GROUND PREPARATION All staff involved have been fully briefed on the type of ground run to be carried out and what is expected of them. Emergency evacuation procedures will be established and briefed depending upon local requirements such as pax steps/jetway or escape slide deployment. Engineer operating ensures that: All ground crew have been trained on how to use the fire appliances, and that fire equipment is in position for the intended run He/she nominates an Engineer to be on the head set for ground to Flt Deck communications All staff have appropriate PPE Ground staff have the appropriate training to enable them to safely carry out their duties and are aware of the safety precautions and dangers of operation All participants know what to do in the event of an Aircraft, Engine or APU Fire All participants are aware of the danger zones, entry corridors and approach procedures Non-essential ground equipment is well clear of the aircraft If any maintenance has just been completed on the aircraft, the EO must establish that the aircraft has been returned to a condition appropriate for the ground run and that all engine accessories have been replenished and/or serviced as required The Engineer responsible will ensure an external FOD check is carried out around the aircraft, the intake area and behind the aircraft, allowing 1,900ft for the jet stream created by the engines at Take-Off power to ensure no damage to other aircraft or equipment. He/she must be satisfied that the ground run area and apron condition is satisfactory and no loose debris, the aircraft is in an appropriate condition and the Centre of Gravity is within the limitations of ramp stability requirements WARNING: FAILURE TO ESTABLISH THAT THE GROUND RUN AREA IS IN A SATISFACTORY CONDITION FOR THE INTENDED RUN AT HIGH POWER COULD RESULT IN INJURY TO PERSONNEL AND/OR DAMAGE TO EQUIPMENT Revision 1 March
9 The Engineer not operating (Instructed by engineer operating / Right Hand Seat): Will monitor the secondary parameters Will advise the ground crew of any changes through the nominated Engineer on the head set May communicate with the control tower, and in the event of an emergency assist with the correct fire procedure Will monitor the wind direction and outside awareness during the run Will take control in the event of the Engineer Operating being in any way incapacitated and is able to shut down the operating power plants Will carry out instructions given by the Engineer Operating and assist with any monitoring and recording as required Revision 1 March
10 GROUND/FLT DECK PREPARATION B /700/800/900 (CFM56) ENGINE GROUND RUN PROCEDURES GUIDE 1 SURFACE-DOORS-GROUND LOCKS-CHOCKS CHECK 2 AIRSTAIRS (IF APPLICABLE) STOWED, DOORS CLOSED 3 BRAKES CHECK SET - W/L ON NOTE: PRESSURE-CONTENTS SATISFACTORY 4 CIRCUIT BREAKERS CHECK IN REQUIRED SETTINGS FLIGHT RECORDER CIRCUIT BREAKERS P18-3 C9 P18-3 C10 WEATHER RADAR P6-1 D13 PULLED/TRIPPED 5 DISPLAY UNITS L AND R NORMAL (SELECT ENG & SYS ON M.F.D. SWITCH) 6 THRUST LEVERS IDLE POSITION 7 THRUST REVERSER LEVERS STOWED 8 BATTERY SWITCH ON 9 STANDBY POWER SWITCH AUTO 10 P5-13 PANEL DC ROTARY SELECT SWITCH BAT (MONITOR VOLTS DROP IF STARTING OFF BATTERY) 11 GALLEY POWER SWITCH OFF 12 LANDING GEAR LEVER DOWN - 3 GREENS 13 FLT CONTROLS MATCH SELECTED POSITIONS 14 FLAPS/STANDBY SYSTEM ALTERNATE ARM SWITCH OFF 15 FIRE AND OVERHEAT SYSTEMS CHECK/TEST 16 FUEL STATUS - REQUIREMENT FOR RUN CHECK QUANTITY LOW POWER KGS HIGH POWER FULL WINGS Revision 1 March
11 17 APU SWITCH START 18 ELECTRICAL SYSTEMS/COMMON DISPLAY SYSTEM SET 19 AIR CONDITIONING SYSTEM SET (PACKS OFF) 20 ANTI-ICE SWITCHES ALL OFF 21 IGNITION SELECT SWITCH IGN L OR IGN R 22 APU BLEED SWITCH ON (> 30PSI AVAILABLE) 23 AUTOTHROTTLE ARM SWITCH OFF 24 EEC SWITCHES ON 25 DOOR ANNUNICATOR PANEL LIGHTS EXTINGUISHED 26 COMMUNICATIONS CHECK CHECK FREQUENCY DEPENDING ON LOCATION LTN GRD LTN TWR BAL/OPS/MAINTROL PRESSURISATION SYSTEM SELECT MANUAL 28 OUTFLOW VALVE TOGGLE FULLY OPEN Revision 1 March
12 PRIOR TO START 1 ENGINE OIL CHECK CONTENTS 2 PARKING BRAKE SET (ON) ENSURE ANTI-SKID SELECTED TO OFF 3 START LEVERS CUTOFF 4 FUEL QUANTITY CHECK STATUS 5 HYDRAULIC SYSTEMS SET (ALL PUMPS ON) 6 FUEL PUMPS ON (LOW PRESSURE LIGHTS OUT) WARNING: DO NOT OPERATE ANY FUEL PUMP IF THE LOW PRESSURE LIGHT COMES ON AND STAYS ON - RUNNING THE FUEL PUMP WITH NO FUEL IN THE TANK WILL CAUSE OVER HEATING OF THE PUMP AS THE FUEL ACTS AS A COOLING AND LUBRICATING AGENT. THIS MAY CAUSE FUEL VAPOURS IN THE TANK TO IGNITE AND CAUSE A FIRE OR EXPLOSION. 7 ANTI-ICE SWITCHES ALL OFF 8 EITHER ANTI-ICE PROBE SWITCH A or B ON (EEC WILL GO INTO THE ALTERNATE MODE IF NOT SELECTED) 9 AIR CONDITIONING PACK SWITCHES OFF 10 ENGINE BLEEDS ON 11 NOTE WIND DIRECTION AND SPEED AIRPORT ATIS INFO 12 ANTI-COLLISION LIGHTS ON 13 RE-CHECK APU AIR SUPPLY > 30 PSI AVAILABLE Revision 1 March
13 STARTING MAIN ENGINE START USING APU 1 ENGINE START SWITCH GRD 2 ENGINE START VALVE LIGHT ON CDU MONITOR 3 APU DUCT PRESSURE RESPONDS - INCREASES 4 WATCH FOR N1 ROTATION N2 25% OR MAX MOTORING POSITIVE ENGINE SPEED OIL PRESSURE INDICATION 5 START LEVER LIFT TO IDLE DETENT MONITOR START SEQUENCE IF AT ANY STAGE THE EGT DISPLAYS AN IMMINENT OVER-TEMP CONDITION, RETURN START LEVER TO CUT OFF POSITION 6 WATCH FOR STABLE IDLE GENERAL STANDARD DAY FIGURES N1 ROTATION N2 56% STARTER CUTOUT E.G.T. NORMAL START E.G.T RED LINE OIL PRESSURE STABILISED IDLE FUEL FLOW APPROX 20% 59% 410 C 725 C > 35psi 60% N2 20% N1 600pph -272 KG NOTE: ALL ENGINES HAVE DIFFERENT EGT MARGINS DUE TO TIME THE EGT WILL INCREASE, THIS CONDITION CAN CAUSE DIFFERENCES BETWEEN ENGINES. IF THE N1 &N2 AND FUEL FLOW ARE SATISFACTORY AT MINIMUM IDLE YOU CAN HAVE EGT DIFFERENCES OF 60 DEGREES C OR GREATER. STARTER LIMITATIONS NORMAL 1 MIN ON EXTENDED CYCLE 2 MINS ON I MIN COOLING 5 MIN COOLING OBSERVE THE STARTER LIMITATIONS AS DAMAGE TO EQUIPMENT MAY RESULT 7 IDG ON LINE SELECT L AND R Revision 1 March
14 CROSS BLEED START 1 ENGINE OPERATING IDLE 2 SELECT ISOLATION VALVE OPEN 3 APU BLEED SWITCH OFF 4 IGNITION SELECTOR BOTH NOTE: ADVISE THE GROUND CREW THAT AN ENGINE WILL BE OPERATED ABOVE IDLE POWER 5 CHECK DUCT PRESSURE FROM OPERATING ENGINE psi ADVANCE THRUST LEVER OF DELIVERING ENGINE APPROXIMATELY ONE KNOB 6 ENGINE START SWITCH GRD 7 ENGINE START VALVE LIGHT ON CDU MONITOR 8 BLEED DUCT PRESSURE RESPONDS - INCREASES 9 WATCH FOR N1 ROTATION N2 25% OR MAX MOTORING POSITIVE ENGINE SPEED OIL PRESSURE INDICATION 10 START LEVER LIFT TO IDLE DETENT 11 MONITOR START SEQUENCE IF AT ANY STAGE THE EGT DISPLAYS AN IMINENT OVER-TEMP CONDITION-RETURN START LEVER TO CUT OFF POSITION 12 WATCH FOR STABLE IDLE GENERAL STANDARD DAY FIGURES 13 N1 ROTATION N2 56% STARTER CUTOUT E.G.T. NORMAL START E.G.T RED LINE OIL PRESSURE STABILISED IDLE FUEL FLOW N1 APPROX 20% N2 59% 410 C 725 C 60% N2 20% N1 600pph -272 KG. NOTE: ALL ENGINES HAVE DIFFERENT EGT MARGINS - DUE TO TIME, THE EGT WILL INCREASE. THIS CONDITION CAN CAUSE DIFFERENCES BETWEEN ENGINES. IF THE N1, N2 AND FUEL FLOW ARE SATISFACTORY AT MINIMUM IDLE YOU MAY SEE EGT DIFFERENCES OF 60 C OR GREATER. 14 ENGINE DELIVERING BLEED AIR RETARD THROTTLE TO IDLE ISOLATION VALVE RESELECT AUTO Revision 1 March
15 TO START AN ENGINE USING BATTERY POWER ONLY 1 ENSURE THAT THE EXTERNAL CHECK HAS BEEN CARRIED OUT 2 BATTERY SWITCH ON 3 ENSURE THAT BRAKE PRESSURE ADEQUATE & PARKING BRAKE IS ON DEPENDING ON THE BATTERY STATUS YOU MAY ONLY GET ONE START 4 FIRE AND OVERHEAT SYSTEM CHECK/TEST 5 STANDBY POWER SWITCH AUTO 6 GROUND AIR SOURCE PRESSURE SUFFICIENT NOTE: DUCT PRESSURE INDICATOR WILL NOT INDICATE UNTIL AC ELECTRICAL POWER IS APPLIED TO AIRCRAFT 7 EITHER ANTI-ICE PROBE SWITCH A or B ON ABOVE 70% N1 EEC WILL GO INTO SOFT ALTERNATE MODE IF NOT SELECTED (POSSIBLE N1 OVERSPEED) 8 IGNITION SELECTOR RIGHT 9 ENGINE START SWITCH GRD HOLD IN GRD POSITION - MAY NOT LATCH IN UNTIL 15% N2 10 START LEVER LIFT TO IDLE DETENT 11 MONITOR STARTER CUTOUT AND START VALVE 56% 12 CHECK ENGINE ACCELERATION WITH BASIC PARAMETERS CHECK AT 12-15% N2, DEDICATED GENERATOR WILL GIVE POWER TO OTHER INDICATIONS 13 N1 & N2 ROTATION & OIL PRESSURE CHECK 14 ENGINE AT STABILISED IDLE, SELECT GENERATOR SELECT ON CHECK POWER ON BUS AND COMMON DISPLAY SATISFACTORY CAUTION: IF YOU DO AN ENGINE START WITH BATTERY POWER ONLY AND GROUND AIR CART, THE ENGINE WILL START AND RUN TO HIGH IDLE AND WILL GO TO NORMAL (GROUND) IDLE ONLY WHEN AC ELECTRICAL POWER IS ESTABLISHED Revision 1 March
16 PRECAUTIONS AND CONSIDERATIONS WHEN ADVANCING THE THRUST LEVERS TO HIGH POWER ALL MOVEMENTS MUST BE SMOOTH AND CONTROLLED IN OPERATION AND MONITORED ENSURE ALL PERSONNEL ARE AWARE OF THE INTENDED RUN AIRCRAFT FUEL WEIGHT 12,000 KILOS IMPROVES TYRE FRICTION REDUCES UNCOMMANDED MOVEMENT CENTRE OF GRAVITY CONSIDERATIONS PROVIDES THE REQUIRED BALLAST FOR THE RUN TAKE-OFF POWER ENSURE THAT ALL HYDRAULIC SYSTEMS ARE LIVE, THE NOSE WHEELS ARE ALIGNED FORE AND AFT & STEERING BYPASS PIN REMOVED. THIS WILL ENSURE STEERING CONTROL IN THE EVENT ANY UNCOMMANDED AIRCRAFT MOVEMENT ENSURE ENGINE NOT BEING TESTED HAS THE RECOMMENDED POWER TO COUNTER BALANCE THE AIRCRAFT WITH THE OTHER ENGINE AT TAKE-OFF POWER ENSURE AIRCRAFT INTO WIND AND INTAKE WIND SPEED NOT ABOVE THE RECOMMENDED SPEED THAT MAY AFFECT THE TRIM FIGURES TAIL AND CROSSWINDS WILL CREATE FAN TIP STALLS N1 FLUCTUATIONS RAPID AIRFLOW CHANGES UNSTABLE CONDITIONS OF OPERATION AIRCRAFT VIBRATION A LOUD FREQUENT SOUND SIMILAR TO BLOW TORCH RETARD THE THRUST LEVERS TO IDLE 1-2 SECS ALLOW ENGINE TEMPERATURE AND COMPONENTS TO STABILISE BEFORE SHUTTING DOWN THE ENGINE Revision 1 March
17 EXHAUST VELOCITY CFM56-7B IDLE POWER 510 FT TAKE-OFF POWER 1,900 FT THRUST REVERSER 130 FT RADIUS FROM INTAKE COMPRESSOR STALL AND HARD STALL INDICATIONS RUMBLING/LOUD BANGS POSSIBLE FLAME EMISSIONS FROM TAILPIPE FLUCTUATING ENGINE PARAMETERS HIGH EGT SLUGGISH OR NO RESPONSE TO THRUST LEVER MOVEMENT RETARD THRUST LEVER TO IDLE AND CARRY OUT COMPRESSOR STALL INSPECTION REQUIREMENTS RAPID SHUT DOWN RAPID ENGINE SHUT DOWN WITH NO FIRE WARNING INDICATION (3-5 MINUTE COOLING TIME NOT ACCOMPLISHED) WITH SUDDEN LOSS OF COOLING AIR MAY RESULT IN TURBINE BLADE TO SHROUD RUBBING AND SEIZURE OF THE LOW PRESSURE TURBINE (LPT) POSSIBLE REASONS FOR RAPID ACTION OVER SPEED OF ROTOR EEC NO CONTROL HIGH EGT EXCEEDENCE COMPRESSOR CORE STALL VIBRATION EXCEEDENCE Revision 1 March
18 ENGINE SHUT DOWN 1 ALLOW ENGINES TO COOL AT IDLE POWER 3 TO 5 MINUTES 2 CIRCUIT BREAKERS RESET ALL THAT WERE PULLED FOR EGR PURPOSES 3 SWITCH TO APU GENERATOR IF ON IDG SUPPLY SELECT APU GEN 4 START SELECT LEVERS CUT-OFF CHECK ENGINE RUN DOWN TIME 5 FUEL BOOSTER PUMPS OFF 6 FLAPS/FLT CONTROLS CHECK POSITION 7 AIR CONDITIONING PACKS OFF 8 HYDRAULIC SYSTEM EMDPs OFF NOTE: ENSURE ENGINE DRIVEN HYDRAULIC PUMP SWITCHES REMAIN SELECTED ON OTHERWISE SOLENOID LIFE MAY BE REDUCED 9 ANTI-SKID ON 10 PRESSURISATION SELECTOR AUTO WARNING: FAILURE TO RETURN THE PRESSURISATION CONTROL TO AUTO MAY RESULT IN THE AIRCRAFT FAILING TO PRESSURISE DURING NEXT FLIGHT CYCLE 11 CALL GROUND/TWR RUN COMPLETE NOTIFICATION 12 EXTERNAL LIGHTS OFF CARRYOUT A CHECK TO ENSURE THAT NO EXCEEDENCES EXIST - THIS CHECK SHOULD BE CARRIED OUT BEFORE POWER IS REMOVED 13 APU SELECTOR OFF 14 APU INLET DOOR CLOSED 15 STANDBY POWER SWITCH AUTO 16 BATTERY SWITCH OFF 17 FLT DECK AND AIRCRAFT SECURE Revision 1 March
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 informationCFM REGULATION THE POWER OF FLIGHT
CFM56-3 3 REGULATION 1 CFM56-3 2 Speed Governing System Fuel Limiting System VBV VSV N1 Vs P Idling System HPTCCV N1 Vs Z N1 Vs T Main Tasks Additional Tasks Corrections MEC PMC CFM 56-3 ENGINE OPERATIONAL
More informationDASSAULT AVIATION Proprietary Data
F2000EX EASY 02-49-00 CODDE 1 PAGE 1 / 2 TABLE OF CONTENTS 02-49 02-49-00 TABLE OF CONTENTS 02-49-05 GENERAL Introduction Sources Equipment location 02-49-10 DESCRIPTION Introduction Description Operating
More informationGeneral. 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 informationGENERAL The Honeywell model TFE731-40AR turbofan engine is a lightweight, two-spool, geared-stage, front-fan, jet engine.
ENGINE GENERAL The Honeywell model TFE731-40AR turbofan engine is a lightweight, two-spool, geared-stage, front-fan, jet engine. The cross section of the engine is shown in Figure 7-71-1, page VII-71-3.
More informationBombardier Challenger Auxiliary Power Unit
GENERAL A Honeywell 36 150(CL) constant-speed gas turbine auxiliary power unit (APU) is installed within a fire-resistant compartment in the aft equipment bay. The APU drives a generator, providing AC
More 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 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 informationOVERHEAD PANEL PROCEDURES FLASH CARDS
OVERHEAD PANEL PROCEDURES FLASH CARDS Boeing 737-800 A supplement to the procedures and checklists publication, Flying the Boeing 737-800 NG Greg Whiley Aussie Star Flight Simulation ELECTRICAL POWER UP
More informationDavid s Flight Simulator Operations Manual
DPW Solutions David s Flight Simulator Operations Manual Draft 0.2 David Woolterton Update 10/5/2016 Table of Contents Pre-Start Checklist... 2 Startup Checklist... 3 Before Taxi Checklist... 3 Taxi Checklist...
More informationDASSAULT 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 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 informationcanaaair chaiiencjer
canaaair chaiiencjer AUXILIARY POWER UNIT (APU) TABLE OF CONTENTS Subject Page GENERAL APU CONTROL START SYSTEM SHUTDOWN I BLEED AIR SYSTEM OIL SYSTEM 1 1 3 5 5 7 Figure Number LIST OF ILLUSTRATIONS Title
More informationCessna Citation XLS - Electrical
GENERAL Electrical power for the Citation XLS comes primarily from DC sources originating with the starter/ generators, the Auxiliary Power Unit (APU) or the battery. A receptacle below the left engine
More informationIntroduction. APU Location
B737 NG APU Introduction The auxiliary power unit (APU) is a self contained gas turbine engine installed within a fireproof compartment located in the tail of the airplane. The APU supplies bleed air for
More informationcanadair chzflleriqer OPERATING MANUAL PSP 601A-6 SECTION 5 AUXILIARY POWER UNIT (APU)
OPERATING MANUAL. AUXILIARY POWER UNIT (APU) 1.. 3. 4. 5. 6. GENERAL APU CONTROL START SYSTEM SHUTDOWN BLEED AIR SYSTEM OIL SYSTEM TABLE OF CONTENTS Page 1 3 3 Figure Number LIST OF ILLUSTRATIONS Title
More informationPOWER ON CHECK LIST COCKPIT PREPARATION
Normal Check List DASH 8-402 1 POWER ON CHECK LIST CIRCUIT BREAKERS... CHECKED BATTERY MASTER... ON BATTERIES... ON MAIN BUS TIE... TIED EXTERNAL POWER... AS REQUIRED APU... AS REQUIRED BATTERIES & BATTERY
More 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 informationUnited 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 informationDash8 - Q400 - Pneumatics
12.19.1 Introduction The Auxiliary Power Unit (APU) replaces the standard composite tailcone with a titanium tailcone and firewall. The APU is accessed by two clamshell type doors on the bottom of the
More informationB777. Electrical DO NOT USE FOR FLIGHT
B777 Electrical DO NOT USE FOR FLIGHT 6.10 Electrical-Controls and Indicators Electrical Panel [IFE/PASS SEATS and CABIN/UTILITY switches basic with C/L 350] 1 2 IFE/PASS CABIN/ SEATS UTILITY 3 11 APU
More informationPneumatic 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 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 informationATA 36 PNEUMATIC TABLE OF CONTENTS DGT ATA 36 PNEUMATIC TABLE OF CONTENTS GENERAL Introduction Sources
F900EX EASY 02-36-00 CODDE 1 PAGE 1 / 2 TABLE OF CONTENTS 02-36 02-36-00 TABLE OF CONTENTS 02-36-05 GENERAL Introduction Sources 02-36-10 DESCRIPTION Introduction Main sub-systems Distribution 02-36-15
More 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 informationifly Jets: The 737NG Quick Reference Handbook Revision Number: 3 Revision Date: July 26, 2010
ifly Jets: The 737NG ifly Jets: The 737NG Revision Number: 3 Revision Date: July 26, 2010 http://www.iflysimsoft.com/ The ifly Developer Team WARNING This manual is only used for understanding the functionalities
More informationAIRPLANE OPERATIONS MANUAL SECTION 2-15
SECTION 2-15 TABLE OF CONTENTS Block General... 2-15-05..01 Bleed Air Thermal Anti-Icing System... 2-15-10..01 Wing, Stabilizer and Engine Anti-icing Valves Operational Logic... 2-15-10..04 EICAS Messages...
More informationChapter 11 Safety, Ground Ops, Servicing
Chapter 11 Safety, Ground Ops, Servicing Chapter 11 Section A Study Aid Questions 1. Keeping hangars, shop, and the flight line and is essential to safety and efficient maintenance. 2. and should watch
More information1. Aircraft General (0 Hours 39 minutes) 2. Doors (0 Hours 33 minutes) 3. EFIS (2 Hours 55 minutes) 4. Exterior Lighting (0 Hours 24 minutes)
Course: CRJ900 (Pilot) Delivery Formats: Web Based or Portable Classroom Number of modules: 26 Estimated Course Time: 36 Hours 16 minutes The following topics are included in this CRJ900 (Pilot) CBT/WBT
More informationby Greg Whiley Aussie Star Flight Simulation
Flying the BAe 146 200/300 Version 2 by Greg Whiley Aussie Star Flight Simulation INTENTIALLY LEFT BLANK Greg Whiley Aussie Star Flight Simulation 2 Version Date Revision Version 1.0 25 June 2014 Original
More informationDASSAULT 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 informationCOMPONENT IDENTIFICATION
This CFMI publication is for Training Purpose Only. The information is accurate at the time of compilation; however, no update service will be furnished to maintain accuracy. For authorized maintenance
More informationPROSIM 737 Overhead Panel Switchmap (July 2012)
PROSIM 737 Overhead Panel Switchmap (July 2012) This Is How I Have Wired Up My Overhead To Work With Prosim. I have used 3 x BU0836X Boards for the inputs Why? Not because I think they are better than
More informationAIRCRAFT GENERAL KNOWLEDGE (1) AIRFRAME/SYSTEMS/POWERPLANT
1 In flight, a cantilever wing of an airplane containing fuel undergoes vertical loads which produce a bending moment: A highest at the wing root B equal to the zero -fuel weight multiplied by the span
More informationINDEX. 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 informationKing 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 informationSECTION 5 AUXILIARY POWER UNIT (APU) TABLE OF CONTENTS LIST OF ILLUSTRATIONS. Title
BOMBARDIER AUXILIARY POWER UNIT (APU) TABLE OF CONTENTS Subject GENERAL APU CONTROL START SYSTEM SHUTDOWN BLEED AIR SYSTEM OIL SYSTEM Page 1 1 4 6 8 8 LIST OF ILLUSTRATIONS Figure Number 1 APU Control
More informationT-6B EMERGENCY PROCEDURE CRITICAL ACTION MEMORY ITEMS & OPERATING LIMITATIONS EMERGENCY PROCEDURE CRITICAL ACTION MEMORY ITEMS
T-6B EMERGENCY PROCEDURE CRITICAL ACTION MEMORY ITEMS & OPERATING LIMITATIONS EMERGENCY PROCEDURE CRITICAL ACTION MEMORY ITEMS ABORT START PROCEDURE or STARTER switch AUTO/RESET EMERGENCY ENGINE SHUTDOWN
More informationThe 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 informationSECTION 2-14 PNEUMATICS, AIR CONDITIONING AND PRESSURIZATION
AIRPLANE PNEUMATICS SECTION 2-14 PNEUMATICS, TABLE OF CONTENTS Block General... 2-14-05..01 Pneumatic System... 2-14-05..02 Pneumatic System Function Logic... 2-14-05..06 Cross Bleed Valve Operational
More informationMAJESTIC Q400 SHARED COCKPIT FLOWS CHECKLISTS MULTIPLAYER OPERATIONS.
PRE LOAD IN Agree on Ports, Share IP and select who will be doing W&B. INITIAL LOAD IN On 1 System transfer Weight and Balance to Simulator Pause Simulation Save Flight as normal FSX Flight Transfer Save
More informationEMBRAER 190. Powerplant DO NOT USE FOR FLIGHT
EMBRAER 190 Powerplant DO NOT USE FOR FLIGHT Embraer 190 - Systems Summary [Powerplant] Two wing-mounted General Electric CF34-10E engines produce power to the EMBRAER 190. The General Electric CF34-10E
More informationPA GURW (December 30, 2000) PRE-START. Langley Flying School. Airspeeds (MPH) for Safe Operation. Cockpit Checks
Langley Flying School PA-34-200 GURW (December 30, 2000) Airspeeds (MPH) for Safe Operation V y (all weights) 105 V x (all weights) 90 En Route Climb 120 V mc 80 V yse 105 V xse 93 V r 80 V r (25 Flaps)
More informationDash8-200/300 - 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 informationJODEL D.112 INFORMATION MANUAL C-FVOF
JODEL D.112 INFORMATION MANUAL C-FVOF Table of Contents I General Description...4 Dimensions:...4 Powertrain:...4 Landing gear:...4 Control travel:...4 II Limitations...5 Speed limits:...5 Airpeed indicator
More informationCHECKLIST FOR NORMAL OPERATION PIPER P32R
FLUGSCHULE GRENCHEN CHECKLIST Piper Saratoga SP 1 CHECKLIST FOR NORMAL OPERATION PIPER P32R Parameters, restrictions, procedures and emergency procedures see AFM BEFORE FIRST FLIGHT 1. Aircraft & Cockpit
More informationFlight checklist for normal operations Massgebend ist das AFM (parameters, restrictions, emergency, etc.)
JAN13 1 Flight checklist for normal operations Massgebend ist das AFM (parameters, restrictions, emergency, etc.) Cockpit preparation before starting engine 1 Aircraft + Cockpit inspection completed (according
More informationFokker 50 - Limitations GENERAL LIMITATIONS MASS LIMITATIONS. Page 1. Minimum crew. Maximum number of passenger seats.
GENERAL LIMITATIONS Minimum crew Cockpit: Two pilots Maximum number of passenger seats Sixty-two (62) Maximum operating altitudes Maximum operating pressure altitude: Maximum take-off and landing pressure
More informationIntroduction. I. Introduction Abbreviations Icon Legend Resources
Introduction Management Reference Guide I. Introduction Abbreviations Icon Legend Resources II. Takeoff Performance Computation Limitation Legend Corrections Maximum Takeoff Performance (Full Thrust Method)
More informationUnited States Army Warfighting Center Fort Rucker, Alabama OCTOBER 2005
United States Army Warfighting Center Fort Rucker, Alabama OCTOBER 2005 STUDENT HANDOUT TITLE: CH-47D POWER PLANTS FILE NUMBER: 011-2107-5 PROPONENT FOR THIS STUDENT HANDOUT IS: 110 th Aviation Brigade
More informationCHAPTER 4 ---AUXILIARY POWER UNIT
Table of Contents Vol. 1 04--00--1 CHAPTER 4 ---AUXILIARY POWER UNIT Page TABLE OF CONTENT 04-00 Table of Contents 04--00--1 INTRODUCTION 04-10 Introduction 04--10--1 POWER PLANT 04-20 APU Power Plant
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 informationFull Authority Digital Electronic Control (FADEC)
Eng.10 Engines-Description and Operation General The aircraft is equipped with three GE CF6-80C2 engines or three P&W PW4460 or PW4462 engines. Each engine has dual rotors, a Low Pressure Compressor (LPC)
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 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 informationDASSAULT 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 informationOPERATIONS MANUAL FTO SECTION : 06.04
06.04.08. OO-WIK SECTION : 06.04 PARTENAVIA OO-WIK PAGE : 1 PRE ENTRY PITOT COVER - REMOVE SNOW / ICE CHECK AIRCRAFT NOSE INTO WIND AIRCRAFT WEIGHT & BALANCE WITHIN LIMITS EXTERNAL (COCKPIT FIRST) PARK
More informationIN-FLIGHT CHECK LIST B-17 Technical Session for Flight Engineers 11/18/2017 (with REVISION)
IN-FLIGHT CHECK LIST B-17 Technical Session for Flight Engineers 11/18/2017 (with REVISION) Check Lists became an integral part of aviation following the tragic loss of Boeing 299 the prototype for the
More informationEXAMEN POR MATERIAS PARA USO DE LOS POSTULANTES A LA HABILITACIÓN DE TIPO EN MATERIAL B733. ENERO 2018
DEPARTAMENTO SEGURIDAD OPERACIONAL SUBDEPARTAMENTO LICENCIAS SECCIÓN EVALUACIONES EXAMEN POR MATERIAS PARA USO DE LOS POSTULANTES A LA HABILITACIÓN DE TIPO EN MATERIAL B733. ENERO 2018 Cantidad de Preguntas
More informationCHAPTER 4 ---AUXILIARY POWER UNIT
Vol. 1 04--00--1 AUXILIARY POWER UNIT Table of Contents REV 3, May 03/05 CHAPTER 4 ---AUXILIARY POWER UNIT Page TABLE OF CONTENT 04-00 Table of Contents 04--00--1 INTRODUCTION 04-10 Introduction 04--10--1
More informationCESSNA 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 informationFlight Checklist for Normal Operations Massgebend ist das AFM (Parameters, Restrictions, Emergency, etc.)
Flight Checklist for Normal Operations Massgebend ist das AFM (Parameters, Restrictions, Emergency, etc.) Jan18 1 COCKPIT PREPARATION BEFORE STARTING ENGINE 1 Aircraft + Cockpit Inspection COMPLETED 1
More informationREFERENCE: 2861 wings 2044 trunk 4904 total BEW 10,655 BOW 11,185 Max Useful load 5115 MLanding ZFW FUEL BURNS 11min min min
REFERENCE: 2861 wings 2044 trunk 4904 total BEW 10,655 BOW 11,185 Max Useful load 5115 MLanding 15700 ZFW 13000 FUEL BURNS 11min 357 27min 730 36 min 940 58min 1453 1:17 1800 2:20 2933 2:46 3283 3:00 3600
More informationTest Flying should only be performed by a pilot who is licensed, rated and experienced on the aircraft type.
Test Flying Procedure: Test Flying should only be performed by a pilot who is licensed, rated and experienced on the aircraft type. In particular, the test pilot should have recently demonstrated an ability
More informationEuropean Aviation Safety Agency
European Aviation Safety Agency EASA TYPE CERTIFICATE DATA SHEET Number: IM.E.021 Issue: 05 Date: 03 January 2013 Type: General Electric Company CF34-10E Series Engines Variants CF34-10E2A1 CF34-10E5 CF34-10E5A1
More informationN123AX Piper Saratoga II HP (PA-32R-301) Checklist (v23 - Revision 3 April 2011) AIRSPEEDS FOR SAFE OPERATIONS. Best Rate of Climb (gear up, flaps up)
N123AX Piper Saratoga II HP (PA-32R-301) Checklist (v23 - Revision 3 April 2011) AIRSPEEDS FOR SAFE OPERATIS Best Rate of Climb (gear down, flaps up) Best Rate of Climb (gear up, flaps up) Turbulent Air
More informationAIRCRAFT SYSTEMS PNEUMATIC
Intentionally left blank PRELIMINARY PAGES - TABLE OF CONTENTS DSC-36-10 Description DSC-36-10-10 General GENERAL... A DSC-36-10-20 Engine Bleed System GENERAL... A Architecture... B Air Bleed Selection...C
More informationExamen Teórico sobre Habilitación de Tipo B (Última actualización: Septiembre 2016)
DIRECCIÓN GENERAL DE AERONÁUTICA CIVIL DEPARTAMENTO SEGURIDAD OPERACIONAL SUBDEPARTAMENTO LICENCIAS Examen Teórico sobre Habilitación de Tipo B-737-300 (Última actualización: Septiembre 2016) Materia:
More 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 informationDESCRIPTION AND OPERATION ICE DETECTION SYSTEM
ICE DETECTION SYSTEM 2.23. ICE DETECTION SYSTEM The ice detection system consists of an ice detector located on the right side of the airplane nose and two ICE amber caution lighted pushbuttons on both
More informationCARENADO COPYRIGHTS. Normal & Emergency Checklist
NORMAL PROCEDURES CHECKLIST PREFLIGHT CHECK Control wheel -- RELEASE BELTS Avionics -- OFF Master Switch -- ON Fuel quantity gauges -- CHECK Master switch -- OFF Ignition -- OFF Exterior -- CHECK FOR DAMAGE
More informationExpanded Flight Checklist Cessna 152
OUTSIDE CHECK INSIDE CABIN 1 Magnetos... OFF 2 Mixture... IDLE CUT OFF 3 Master switch... ON 4 Fuel quantity... CHECKED 5 Master switch... OFF OUTSIDE CABIN 1 Left wing... CHECKED Surface condition Flap
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 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 informationDASSAULT AVIATION Proprietary Data
F2000EX EASY 02-28-00 CODDE 1 PAGE 1 / 2 TABLE OF CONTENTS 02-28 ATA 28 - FUEL SYSTEM 02-28-00 TABLE OF CONTENTS 02-28-05 GENERAL Introduction Sources Fuel tank location 02-28-10 DESCRIPTION Sub-systems
More informationA310 AIRCRAFT PREPARATION FOR COLD WEATHER OPERATION FCOM>>Procedure and Techniques >>Inclement Weather Operation
A310 AIRCRAFT PREPARATION FOR COLD WEATHER OPERATION FCOM>>Procedure and Techniques >>Inclement Weather Operation General: - Cold weather operation covers the following operating conditions: a) Cold soaked
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 informationVso 61. Vs1 63. Vr 70. Vx 76. Vxse 78. Vy 89. Vyse. 89 (blue line) Vmc. 61 (radial redline) Vsse 76. Va 134) Vno 163
PA34-200T Piper Seneca II Normal procedures V-speeds Knots Vso 6 Vs 63 Vr 70 Vx 76 Vxse 78 Vy 89 Vyse Vmc 89 (blue line) 6 (radial redline) Vsse 76 Va 2-36(@4507lbs 34) Vno 63 Vfe 38 (0*)/2(25*)/07(40*)
More informationCessna 550/551/560 (PWC JT15D) Initial Aircraft Type Training Course MAINTENANCE INITIAL
Cessna 550/551/560 (PWC JT15D) Initial Aircraft Type Training Course CONTENTS INTRODUCTION 5 COURSE DESCRIPTION 6 COURSE OBJECTIVES 7 COURSE MATERIAL 8 TIMETABLE WEEK ONE 9 TIMETABLE WEEK TWO 10 LEVEL
More informationChecklist Robin DR40
Flight Checklist for Normal Operations Massgebend ist das AFM (Parameters, Restrictions, Emergency, etc.) Jan 18 1 COCKPIT PREPARATION BEFORE STARTING ENGINE 1 Aircraft + Cockpit Inspection COMPLETED 1
More informationNORMAL PROCEDURES. TABLE OF CONTENTS Page
CESSNA SECTION 4 MODEL 208B 867 SHP NORMAL PROCEDURES NORMAL PROCEDURES TABLE OF CONTENTS Page Introduction............................................4-3 Airspeeds for Normal Operation............................4-4
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 informationDifferences Training
Differences Training 747-400 Preamble The purpose of this presentation is to familiarize the crew with the various differences in procedures and systems among the 747-400 Fleet. The presentation highlights
More informationPA34-220T Piper Seneca III
PREFLIGHT PA34-220T Piper Seneca III Weight and Balance Documents -Airworthiness Certificate -Registration -Airplane Flight Manual -Weight & Balance Hobbs/Time Landing Gear Avionics and Fan(s) Cowl Fuel
More informationV - Speeds. RV-10 V fe Flaps Speeds Trail (0 deg) Half (15 deg) Full (30 deg) 122 kias 96 kias. 80 kias
RV-10 Check List V - Speeds RV-10 V fe Flaps Speeds Trail (0 deg) Half (15 deg) Full (30 deg) 122 kias 96 kias 87 kias V s1 Stall (Flap Up) 60 kias V s0 Stall (Flap 40 deg) 55 kias Best Glide 80 kias V
More 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 informationOwners Manual. Table of Contents 3.1. INTRODUCTION AIRSPEEDS FOR EMERGENCY OPERATION OPERATIONAL CHECKLISTS 3
EMERGENCY PROCEDURES Table of Contents 3.1. INTRODUCTION 2 3.2. AIRSPEEDS FOR EMERGENCY OPERATION 2 3.3. OPERATIONAL CHECKLISTS 3 3.3.1. ENGINE FAILURES 3. ENGINE FAILURE DURING TAKEOFF RUN 3. ENGINE FAILURE
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 informationB737 NG Anti Ice & Rain
B737 NG Anti Ice & Rain Introduction Thermal anti-icing (TAI), electrical anti-icing, and windshield wipers are the systems provided for ice and rain protection. The anti-ice and rain systems include:
More informationCessna Citation XLS - Environmental & Temperature Control
GENERAL Environmental and temperature control on the Citation XLS is provided by pre-cooled engine and/or APU bleed air. The conditioned bleed air is distributed in a series of ducts and vents. The primary
More informationPilot's Operating Handbook Supplement AS-03
POH / AFM SECTION 9 Pilot's Operating Handbook Supplement ASPEN EFD1000 PFD This supplement is applicable and must be inserted into Section 9 of the POH when the Aspen Avionics Evolution Flight Display
More 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 informationEMERGENCY 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 informationPA32-RT LANCE II CHECKLIST
PA32-RT LANCE II CHECKLIST 6815.10.1112 1 Normal Procedures PREFLIGHT CHECK Control Wheel... RELEASE BELTS Parking brake... Set Master Switch... ON Fuel Quantity Gauges... check Master Switch... OFF Ignition...
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 informationHAZARDS TO FIREFIGHTERS
HAZARDS TO FIREFIGHTERS Introduction The Airport environment and aircraft add even more unique hazards and safety considerations for Firefighters. Video Intro Ready plane for catapult shot Wedged into
More informationSECTION 6-3 POWER PLANT
SECTION 6-3 SYSTEMS DESCRIPTION Index Page General Description... 6-3-3 Engine Features... 6-3-4 Engine Indication System... 6-3-6 Power Plant Control... 6-3-10 Power Plant System Control... 6-3-12 Power
More informationAircraft Checklist Commander 114
Aircraft Checklist Commander 114 This is an abbreviated checklist. Most explanatory items, notes cautions and warnings have been omitted for brevity. Procedures in red/bold text in this checklist should
More information24 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 informationDEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET NO. 1E8
DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION 1E8 Revision 18 PRATT & WHITNEY AIRCRAFT TURBO WASP JT3D-1 JT3D-3 JT3D-1A JT3D-3B JT3D-1-MC6 JT3D-3C JT3D-1A-MC6 JT3D-7 JT3D-1-MC7 JT3D-7A JT3D-1A-MC7
More information