CHAPTER 32 LANDING GEAR. Section Title Page
|
|
|
- Austin Booker
- 5 years ago
- Views:
Transcription
1 CHAPTER 32 LANDING GEAR Section Title Page Description Landing Gear Assembly Cross Tubes Skid Tubes Skid Shoes Skid Extension Replacement Ground Handling Wheel Support Replacement Fairing Assemblies Maintenance OCT 2010 R66 Maintenance Manual Chapter 32 Landing Gear Page 32.i
2 Intentionally Blank Page 32.ii Chapter 32 Landing Gear R66 Maintenance Manual 25 OCT 2010
3 CHAPTER 32 LANDING GEAR Description R66 Turbine standard landing gear includes two aluminum skid tubes, two aluminum cross tubes, and four steel strut assemblies. Aerodynamic fairings fasten to each strut assembly. R66 spring and yield, skid-type landing gear is designed to absorb normal and hard landings. The landing gear attaches to the fuselage at each strut assembly collar and gusset. Left side attachments connect to the fuselage via pivoting shackles. Normal landings are absorbed elastically. In an extremely hard landing, left side strut assemblies hinge up and out as the cross tube yields (takes permanent set), absorbing impact. Slight yielding of the aft cross tube is acceptable. For tail skid height limitation, see Section For hard landing inspection, see Section Five hardened steel skid shoes attach to the bottom of each skid tube. Inspect skid tubes and skid shoes per Section 32-30, especially following touch-down autorotations or running takeoffs or landings Landing Gear Assembly A. Removal 1. Open cabin aft doors and baggage compartment door. Remove engine cowling per Section Refer to Section 6-70; remove G308-2 and two F475-6 cross tube covers. Remove fairing assemblies per Section Refer to Figure Remove hardware securing A936-3 (ground) wire assembly to aft, right landing gear attachment. 4. Using putty knife or plastic scraper, cut sealant securing four cross tube rain caps to landing gear assembly and remove caps. Remove sealant residue from caps, cross tubes, and strut assemblies. Clean surfaces with solvent. 5. Hoist helicopter per Section Raise skids above ground approximately 4 inches. CAUTION Support landing gear assembly as mounting bolts are removed. Do not damage forward cross tube hinged inspection cover. 6. Remove hardware securing forward, right strut assembly & forward cross tube to fuselage support. Mounting bolt access hole is located on aft, right seat box forward wall. 7. Remove hardware securing aft, right strut assembly & aft cross tube to fuselage support. Mounting bolt access hole is located on baggage compartment aft wall. 8. Rotate forward, left shackle to align mounting bolt with access hole on aft, left seat box forward wall. Remove hardware securing landing gear to shackle. 9. Rotate aft, left shackle to align mounting bolt with access hole on baggage compartment aft wall. Remove hardware securing landing gear to shackle. 25 OCT 2010 R66 Maintenance Manual Chapter 32 Landing Gear Page 32.1
4 FIGURE 32-1 LANDING GEAR ATTACHMENT Page 32.2 Chapter 32 Landing Gear R66 Maintenance Manual 25 OCT 2010
5 32-10 Landing Gear Assembly (continued) B. Installation Refer to R66 Illustrated Parts Catalog (IPC) Figure WARNING Landing gear mounting bolts are critical fasteners. See Section for torque requirements. CAUTION Support landing gear assembly as mounting bolts are installed. Do not damage forward cross tube hinged inspection cover. 1. Hoist helicopter per Section 7-20 to required height. 2. Refer to Figure Insert hardware thru left side access hole on baggage compartment aft wall, and thru shackle. Align mounting bolt with aft, left landing gear attachment. Install hardware, special torque bolt per Section 20-33, & torque stripe per Figure Insert hardware thru access hole on aft, left seat box forward wall, and thru shackle. Align mounting bolt with forward, left landing gear attachment. Install hardware, special torque bolt per Section 20-33, & torque stripe per Figure Insert hardware thru right side access hole on baggage compartment aft wall and aft, right landing gear attachment. Install hardware, special torque bolt per Section 20-33, & torque stripe per Figure Insert hardware thru access hole on aft, right seat box forward wall and forward, right landing gear attachment. Install hardware, special torque bolt per Section 20-33, & torque stripe per Figure Lower helicopter per Section Close cabin aft doors and baggage compartment door. 7. Verify surface under terminal is clean and dry and install hardware securing A936-3 (ground) wire assembly to aft, right landing gear attachment. Standard torque screw per Section and torque stripe per Figure Verify rain caps and bonding surfaces are clean and dry. Bond caps to landing gear assembly using B270-1 sealant. Mix sealant according to manufacturer's instructions. 9. Refinish landing gear as required per Chapter When surfaces are dry, install engine cowling per Section Refer to Section 6-70; install G308-2 and two F475-6 cross tube covers. Install fairing assemblies per Section OCT 2010 R66 Maintenance Manual Chapter 32 Landing Gear Page 32.3
6 FIGURE 32-2 CROSS TUBE REMOVAL Page 32.4 Chapter 32 Landing Gear R66 Maintenance Manual 25 OCT 2010
7 32-20 Cross Tubes A. Inspection Replace aft cross tube if tail skid height is less than 38 inches from ground when aircraft is minimally loaded on level pavement. For hard landing inspection, see Section B. Removal 1. Remove landing gear per Section Refer to Figure Remove hardware securing one skid tube (left or right) to same side strut assemblies. 3. Remove hardware securing cross tube (to be replaced) to strut assemblies. Using brass drift, tap on strut assembly collars to separate struts from cross tube. Do not tap on jack tabs. C. Installation Refer to R66 Illustrated Parts Catalog (IPC) Figure NOTE When installing A936-3 (ground) wire assembly, verify finish is removed from surface under wire terminal. 1. Refer to Figure Lightly coat mating surfaces of cross tube with zinc-chromate or epoxy primer using approved materials per Section While primer is wet, install cross tube into strut assemblies and align fastener holes. 2. Install hardware securing cross tube to strut assemblies, standard torque screws per Section 20-32, and torque stripe per Figure Install hardware securing left or right skid tube to strut assemblies, standard torque bolts per Section 20-32, and torque stripe per Figure Install landing gear per Section OCT 2010 R66 Maintenance Manual Chapter 32 Landing Gear Page 32.5
8 FIGURE 32-3 SKID TUBES AND FAIRINGS (Strut and skid tube angles exaggerated for clarity) Page 32.6 Chapter 32 Landing Gear R66 Maintenance Manual 25 OCT 2010
9 32-30 Skid Tubes Refer to R66 Illustrated Parts Catalog (IPC) Figure A. Inspection CAUTION Minimize personnel movement around raised helicopter. Use caution when working under raised skid tubes. 1. Install ground handling wheels per Section Pull down on tail rotor gearbox and place blocks under skid tubes, forward of forward strut assemblies. Skids should be approximately parallel with the ground. 3. Measure damage on left or right skid tube. Replace skid tube if damage exceeds the following limits: a inch maximum depth longitudinal scratch (no length limit). b inch maximum depth and 0.50 inch maximum length circumference scratch. c inch maximum width flat spot. 4. Measure the thickness of skid tube's skid shoes (five per skid). Replace a skid shoe per Section if damage exceeds inch minimum thickness. Repeat steps on opposite skid tube. B. Removal 1. Jack or hoist helicopter per Sections 7-10 or Raise skids above ground approximately 4 inches. 2. Refer to Figure Remove hardware securing left or right skid tube to same side strut assemblies. C. Installation 1. Jack or hoist helicopter per Sections 7-10 or 7-20 to required height. 2. Refer to Figure Install hardware securing skid tube to strut assemblies. Standard torque bolts per Section and torque stripe per Figure Lower helicopter per Sections 7-10 or OCT 2010 R66 Maintenance Manual Chapter 32 Landing Gear Page 32.7
10 32-31 Skid Shoes Refer to R66 Illustrated Parts Catalog (IPC) Figure A. Inspection Inspect skid tubes and skid shoes per Section B. Replacement 1. Refer to Figure Remove and discard hardware securing skid shoe to skid tube. Discard a shoe damaged beyond limits in Section Install new A142-1 screws to secure skid shoe to skid tube. Standard torque screws per Section Skid Extension Replacement Refer to R66 Illustrated Parts Catalog (IPC) Figure Remove skid tube per Section Refer to Figure Remove and discard hardware securing aft skid shoe to skid tube. Remove skid extension. 3. Clean interior of skid tube as practical. Install new skid extension and align fastener holes. 4. Install new A142-1 screws to secure aft skid shoe to skid tube. Standard torque screws per Section Install skid tube per Section Fill gap in side of skid extension using B270-1 sealant. Mix sealant according to manufacturer's instructions Ground Handling Wheel Support Replacement Refer to R66 Illustrated Parts Catalog (IPC) Refer to Figure Remove hardware securing support weldment to skid tube and remove support. 2. Install hardware securing new support weldment to skid tube. Verify correct support orientation. Special torque hardware per Section and torque stripe per Figure 5-1. Page 32.8 Chapter 32 Landing Gear R66 Maintenance Manual 25 OCT 2010
11 32-40 Fairing Assemblies Refer to R66 Illustrated Parts Catalog (IPC) Figure A. Removal 1. Refer to Figure Remove screws securing fairing assembly together at trailing edge. 2. Remove screws securing fairing assembly to strut assembly. Unscrew clamp through fairing inboard access hole and remove fairing. B. Installation 1. Refer to Figure Verify fairing assembly clip nuts are installed. Verify clamp threads through fairing clips, with hex facing inboard access hole. 2. Position fairing assembly on strut assembly and install screws securing fairing to strut. 3. Tighten clamp, and special torque hex through fairing assembly inboard access hole per Section Install screws securing fairing assembly together at trailing edge. 5. Verify inch clearance between fairing assembly edge and fuselage. Remove and trim fairing as required; reinstall per preceding steps Maintenance 1. Refer to Figure Verify drain holes in bottom of skid tubes are free of obstructions (two per skid, between two forward skid shoes and aft of skid shoe at forward strut assembly). 2. Refinish landing gear to prevent corrosion per Chapter Inspect skid tubes and skid shoes per Section 32-30, especially following touch-down autorotations or running take-offs or landings. 4. Verify skid tube and strut assembly rain caps are properly sealed. Replace or re-seal rain caps per the following: a. Using putty knife or plastic scraper, cut sealant securing rain cap to landing gear assembly and remove cap. Remove sealant residue from caps, cross tubes, and/or strut assemblies. Clean surfaces with solvent. b. Verify rain caps and bonding surfaces are clean and dry. Bond caps to landing gear assembly using B270-1 sealant. Mix sealant according to manufacturer's instructions. 25 OCT 2010 R66 Maintenance Manual Chapter 32 Landing Gear Page 32.9
12 Intentionally Blank Page Chapter 32 Landing Gear R66 Maintenance Manual 25 OCT 2010
CHAPTER 8 WEIGHT AND BALANCE. Section Title Page
CHAPTER 8 WEIGHT AND BALANCE Section Title Page 8-10 Leveling.......................................... 8.1 8-11 Leveling for Weight and Balance................. 8.1 8-12 Leveling for Rigging..........................
CHAPTER 18 WEIGHT AND BALANCE
CHAPTER 18 WEIGHT AND BALANCE Section Title 18-10 Leveling................................................. 18.1 18-11 Leveling at Lower Right Side Frame Tube & Aft Landing Gear Cross Tube.. 18.1 18-12
CHAPTER 64 TAIL ROTOR. Section Title Page
CHAPTER 64 TAIL ROTOR Section Title Page 64-00 Description........................................ 64.1 64-10 Tail Rotor Assembly.................................. 64.1 64-11 Static Balance..............................
CHAPTER 63 MAIN ROTOR DRIVE SYSTEM
Section Title CHAPTER 63 MAIN ROTOR DRIVE SYSTEM 63-00 Description............................................... 63.1 63-10 Engine Shaft Weldment...................................... 63.1 63-11 (Engine
CHAPTER 79 ENGINE OIL SYSTEM
Section Title CHAPTER 79 ENGINE OIL SYSTEM 79-00 Description............................................... 79.1 79-10 Scroll and Fanwheel Assemblies................................ 79.3 79-11 Fanwheel-to-Inlet
CHAPTER 9 GROUND HANDLING. Section Title Page
CHAPTER 9 GROUND HANDLING Section Title Page 9-10 Ground Handling.................................... 9.1 9-11 Ground Handling Wheels...................... 9.1 9-12 Moving Helicopter on Ground Handling
CHAPTER 65 TAIL ROTOR DRIVE SYSTEM. Section Title Page
CHAPTER 65 TAIL ROTOR DRIVE SYSTEM Section Title Page 65-00 Description........................................ 65.1 65-10 Tail Rotor Drive Fan Shaft.............................. 65.1 65-20 Tail Rotor
CHAPTER 21 ENVIRONMENT CONTROL. Section Title Page
CHAPTER 21 ENVIRONMENT CONTROL Section Title Page 21-00 Description........................................ 21.1 21-10 Ventilation........................................ 21.3 21-11 Nose Vent................................
CHAPTER 76 ENGINE CONTROLS. Section Title Page
CHAPTER 76 ENGINE CONTROLS Section Title Page 76-00 Description........................................ 76.1 76-10 Fuel Control Unit (FCU)............................... 76.1 76-11 FCU Throttle Control
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.........................................
CHAPTER 15 FURNISHINGS. Section Title Page
CHAPTER 15 FURNISHINGS Section Title Page 15.000 Description..................................... 15.1 15.100 Seat Harnesses................................... 15.3 15.110 Four-Point Harness Assembly.................
Chapter 52 DOORS -Title
Chapter 52 DOORS 52-Title Page 1 January 23, 2012 INTENTIONALLY LEFT BLANK 52-Title Page 2 January 23, 2012 LIST OF EFFECTIVE PAGES Chapter Section Page No. Date 52 52-Title 1 January 23, 2012 2 January
CHAPTER 9 ROTOR SYSTEMS. Section Title Page
CHAPTER 9 ROTOR SYSTEMS Section Title Page 9.000 Rotor Systems........................................... 9.1 9.100 Main Rotor............................................. 9.1 9.110 Main Rotor Blades....................................
CHAPTER 12 SERVICING. Section Title Page
CHAPTER 12 SERVICING Section Title Page 12-10 Main Rotor Gearbox.................................. 12.1 12-11 Servicing................................. 12.1 12-12 Filter Replacement...........................
CHAPTER 13 INSTRUMENTS
CHAPTER 13 INSTRUMENTS Section Title Page 13.000 Description.............................................. 13.1 13.100 Pitot-Static System......................................... 13.3 13.200 Primary Instruments........................................
Chapter 14 SERVICING TABLE OF CONTENTS ILLUSTRATIONS
Chapter 14 SERVICING TABLE OF CONTENTS INTRODUCTION -------------------------------------------------------------------------- 3 General ----------------------------------------------------------------------------------
SECTION 35iS/U: LANDING GEAR & ENGINE MOUNT
WD-1221 ENGINE MOUNT STANDOFF SECTION 35iS/U: LANDING GEAR & ENGINE MOUNT U-01203E-1 INBOARD DOUBLER PLATE U-01203B-1 INBOARD WEAR PLATE U-01203C-1 BEARING PLATE U-01203-2 (U-01203-1 SHOWN) INBOARD MAIN
CHAPTER 36 SPECIAL TOOLS Special Tools Illustrations and Tasks
CHAPTER 36 SPECIAL TOOLS Section Title 36-10 Special Tools............................................. 36.1 36-20 Illustrations and Tasks....................................... 36.2 Page OCT 2018 Chapter
Service Bulletin. ATA 52-10: Passenger and Crew Doors Door Latching Assembly Upgrade
Service Bulletin Issued: 5 Oct 00 Models SR0 and SR ATA 5-10: Passenger and Crew Doors Door Latching Assembly Upgrade COMPLIANCE Optional: Accomplishment of this Service Bulletin is at the owner s option.
53-40 ATTACH FITTINGS
ATTACH FITTINGS. DESCRIPTION Attach fittings are provided for attachment of the seats (Refer to -0), baggage straps (Refer to -0), rear seat harnesses (Refer to -0), cargo net straps (Refer to -0), cabin
11 - Fairings. Fairings. February XLF Page 11-1
11 - Fairings Fairings February 2003 11-XLF Page 11-1 11 - Fairings This Page Intentionally Left Blank Page 11-2 11-XLF February 2003 11 - Fairings Contents 11.0 - Chapter Preface... 11-4 11.0.1 - Parts
CHAPTER 9 ROTOR SYSTEMS
Section Title CHAPTER 9 ROTOR SYSTEMS 9.000 Description............................................... 9.1 9.100 Main Rotor............................................... 9.1 9.200 Tail Rotor................................................
CHAPTER 1 GENERAL. Section Title
Section Title CHAPTER 1 GENERAL 1-00 Introduction.............................................. 1.1 1-10 R66 Maintenance Manual Revisions.............................. 1.1 1-20 R66 Maintenance Authorization.................................
CHAPTER 13 INSTRUMENT SYSTEM
CHAPTER 13 INSTRUMENT SYSTEM Section Title 13-00 Description............................................... 13.1 13-10 Pitot-Static System......................................... 13.3 13-20 Primary Instruments.........................................
NOTE ITEM PART NUMBER KIT CONTENTS QTY
R44 II Aux Fuel Pump Assembly Upgrade Installation Kit Instructions Applicable to helicopter S/N 13158 and prior equipped with D743-1, D743-2, or D743-4 Aux Fuel Pump. D743-1, D743-2, and D743-4 pumps
SUBJECT: TRANSMISSION FAIRING INSTALLATION, IMPROVEMENT OF. HELICOPTERS AFFECTED: Serial numbers through
TECHNICAL BULLETIN 505-18-04 16 January 2018 MODEL AFFECTED: 505 SUBJECT: TRANSMISSION FAIRING INSTALLATION, IMPROVEMENT OF HELICOPTERS AFFECTED: Serial numbers 65011 through 65056. [Serial number 65057
INSTALLATION INSTRUCTIONS SKID STEP and Utility Handles FOR MDHI 369D, 369E, 369FF, & 500N
INSTALLATION INSTRUCTIONS SKID STEP and Utility Handles FOR MDHI 369D, 369E, 369FF, & 500N AEROCRAFT INC. 4420 COMMODITY WAY, UNIT B SHINGLE SPRINGS, CA 95682 LOG OF REVISIONS REVISION DATE PAGES EFFECTED
REVISION DESCRIPTION:
REVISION DESCRIPTION: 14401 Keil Road NE, Aurora, Oregon, USA 97002 PHONE 503-678-6545 FAX 503-678-6560 www.vansaircraft.com info@vansaircraft.com Service Letters and Bulletins: www.vansaircraft.com/public/service.htm
CIRRUS AIRPLANE MAINTENANCE MANUAL
MODEL SR PASSENGER AND CREW DOORS. DESCRIPTION AND OPERATION Serials 000 thru 00: The two crew/passenger doors incorporate a flush-mount outside door handle, key-operated door lock, and a conventional
COMPOSITE INLET COWLING, RETROFIT OF. HELICOPTERS AFFECTED: Serial numbers through 45790, through and through
TECHNICAL BULLETIN 206L-18-255 28 June 2018 MODEL AFFECTED: 206L-1, 206L-3, and 206L-4 SUBJECT: COMPOSITE INLET COWLING, RETROFIT OF HELICOPTERS AFFECTED: Serial numbers 45154 through 45790, 51001 through
C I R R U S COWLING DESCRIPTION
COWLING 1. DESCRIPTION Serials 22-0002 thru 22-019, 22-0821 thru 22-711: The engine cowling, fabricated from fiberglass and epoxy, consists of one upper and two lower halves. A one-piece (22-0002 thru
CHAPTER 22 SERVICING
CHAPTER 22 SERVICING Section Title 22-10 Main Rotor Gearbox......................................... 22.1 22-11 Cleaning Chip Detector..................................... 22.3 22-12 Cleaning Sight Gage.......................................
CIRRUS AIRPLANE MAINTENANCE MANUAL
JACKING 1. DESCRIPTION Three jack points, located at each wing tiedown and tail tiedown, are provided to perform maintenance operations. Tie-down rings must be removed and replaced with jack points prior
CIRRUS AIRPLANE MAINTENANCE MANUAL
AERODYNAMIC FAIRINGS 1. DESCRIPTION This section describes those components which make up the aerodynamic fairings. A fixed, composite wing root fairing is installed around the wing root, enclosing the
1) Page: REV 5: Changed depiction to show added hardware and T-01220
REVISION DESCRIPTION: 1) Page: 37-01 REV 5: Changed depiction to show added hardware and T-01220 Page: 37-02 REV 4: Added Figure 3 depicting Separating the T-01220 Doublers. Figure 4 was Figure 3. Added
Flight Compartment. 1. General
CIRRUS AIRPLANE MAINTENANCE MANUAL Flight Compartment CHAPTER 56-10: FLIGHT COMPARTMENT GENERAL 56-10: FLIGHT COMPARTMENT 1. General The windshield is manufactured of acrylic and is adhesive bonded to
CHAPTER 6 POWERPLANT
Section Title CHAPTER 6 POWERPLANT 6.000 Powerplant And Related Systems................................ 6.1 6.001 Introduction............................................ 6.1 6.002 Description.............................................
SECTION 3 EMERGENCY PROCEDURES CONTENTS
CONTENTS Page Definitions.................................. 3-1 Power Failure - General......................... 3-1 Power Failure Above 500 feet AGL................ 3-2 Power Failure Between 8 and 500
Page: REV 1: In Step 4 "a minimum of 1/16 [1.6 mm] gap" was "an approximately 1/16 [1.6 mm] gap."
![Page: REV 1: In Step 4 a minimum of 1/16 [1.6 mm] gap was an approximately 1/16 [1.6 mm] gap.](/thumbs/72/66557156.jpg "Page: REV 1: In Step 4 a minimum of 1/16 [1.6 mm] gap was an approximately 1/16 [1.6 mm] gap.")
14401 Keil Road NE, Aurora, Oregon, USA 97002 PHONE 503-678-6545 FAX 503-678-6560 www.vansaircraft.com info@vansaircraft.com Service Letters and Bulletins: www.vansaircraft.com/public/service.htm REVISION
PARAVION TECHNOLOGY, INC AIRWAY AVENUE FT. COLLINS, COLORADO 80524
PARAVION TECHNOLOGY, INC. 2001 AIRWAY AVENUE FT. COLLINS, COLORADO 80524 DOCUMENT NO. INSTALLATION INSTRUCTIONS BELL 206A/B/L/L1/L3/L4 HELICOPTER MODELS Page i Rev. H, 02/06/06 REVISIONS REV. DATE DESCRIPTION
REVISION DESCRIPTION:
REVISION DESCRIPTION: 1) Page: 12-03 REV 1: Step 1: and Figure 1: Final-Drill s.b. Match-Drill. Step 4: Updated flox mixture description to match later description (removed "peanut butter-like" description).
CIRRUS AIRPLANE MAINTENANCE MANUAL
UNSCHEDULED MAINTENANCE CHECKS 1. DESCRIPTION The following describes those maintenance checks and inspections on the aircraft which are dictated by special or unusual conditions which are not related
Pitch Control and Trim
Pitch Control and Trim GENERAL 27-30: PITCH CONTROL AND TRIM. General This section describes that portion of the flight control system which controls the position and movement of the elevator. This includes
Utah Soaring Association Rigging and De-Rigging. USA G-103 Twin II. Procedures for safe assembly and dis-assembly of the glider. (Trailers 1, 2 and 3)
USA G-103 Procedures for safe assembly and dis-assembly of the glider (Trailers 1, 2 and 3) Grob Glider Rigging Tools Required: Large blade standard screwdriver #2 (medium blade) Phillips screwdriver (if
Seabee Annual/100-Hour Inspection
Date Completed Seabee Annual/100-Hour Inspection ENGINE Mechanic s Initials 1 Drain engine oil and check for foreign material 2 Check oil screen for proper rotation or looseness 3 Safety Oil Plug 4 Refill
RPM Rollbar Installation Instructions Ford Mustang 05-11
RPM Rollbar Installation Instructions Ford Mustang 05-11 IMPORTANT READ BEFORE STARTING INSTALLATION Check for backing plate clearance between the undercarriage and fuel lines directly below area where
SERVICE INFORMATION LETTER
SERVICE INFORMATION LETTER DATE: August 19, 2015 SERVICE INFORMATION LETTER NO. 0183 Page 1 of 18 1. SUBJECT: Collective Stick Socket Replacement 2. MODEL: F28A, 280, F28C, 280C, F28F, 280F, and 280FX
F-1202D-L PANEL ATTACH STRIP F L UPPER FWD FUSELAGE SKIN RIB F CABIN EGRESS HANDLE F-1240B COVER PLATE
SECTION 29iS/U: F-1202D-L PANEL ATTACH STRIP F-01240-1 UPPER FORWARD FUSELAGE SKIN (SHOWN TRANSPARENT) VAN'S AIRCRAFT, INC. FWD UPPER FUSELAGE F-00078 CABIN EGRESS HANDLE F-00077-L UPPER FWD FUSELAGE SKIN
SECTION 4 NORMAL PROCEDURES CONTENTS
CONTENTS Page Recommended Airspeeds....................... 4-1 Daily or Preflight Checks........................ 4-1 Before Starting Engine.......................... 4-6 Starting Engine and Run-Up......................
Unscheduled Maintenance Checks
CIRRUS AIRPLANE MAINTENANCE MANUAL CHAPTER 5-50: UNSCHEDULED MAINTENANCE CHECKS GENERAL Unscheduled Maintenance Checks 5-50: UNSCHEDULED MAINTENANCE CHECKS 1. General The following describes those maintenance
Assembly Instructions
Assembly Instructions Part Number Description Model Approx. Assembly Time 99994-0903 Windshield Wiper Kit Mule SX 1 Hour WARNING Improper installation of this accessory could result in an accident causing
Seabee Annual Inspection Procedures
Procedures Due to the wide variety of Seabee s flying out there, these procedures should be modified to fit YOUR Seabee. Make sure that all AD s are complied with as well as any required Service Bulletins
Page: REV 3: Add drill and tap information to Figure 4 DRILL #3, TAP 1/4-28 BOTH ENDS.
REVISION DESCRIPTION: 1) Page: 32-03 MEMO: Step 4 should not be bold. Fix WD-1213 callout in Figure 3. Page: 32-04 REV 3: Add drill and tap information to Figure 4 DRILL #3, TAP 1/4-28 BOTH ENDS. Add make
nd STREET, MENOMINEE, MICHIGAN 49858
2209 22 nd STREET, MENOMINEE, MICHIGAN 49858 DATE: July 7, 2011 1. SUBJECT: Special Inspections for Agricultural Aircraft 2. MODEL: 480 and 480B Helicopters 3. EFFECTIVITY: Helicopters Equipped with Ag
PARAVION TECHNOLOGY, INC AIRWAY AVENUE FORT COLLINS, COLORADO 80524
Revision F PARAVION TECHNOLOGY, INC. 2001 AIRWAY AVENUE FORT COLLINS, COLORADO 80524 REPORT NO. INSTALLATION INSTRUCTIONS BELL MODEL 407 SERIES BLEED-AIR CABIN HEATER Page i Rev. F, 04/06/09 REVISIONS
C I R R U S HOISTING DESCRIPTION
HOISTING 1. DESCRIPTION This chapter describes those instructions necessary to support the airplane during maintenance and repair. In some instances (i.e. off-runway landing, collapsed gear, etc.) it may
CHAPTER 4 AIRWORTHINESS LIMITATIONS
Section Title CHAPTER 4 AIRWORTHINESS LIMITATIONS 4-10 Airworthiness Limitations..................................... 4.1 4-20 Additional Limitations....................................... 4.3 4-21 Parts
Subject: Align-Trac Procedures. Lit No: LIT1004 Date: 05/30/2015 Revision: A
Watson & Chalin recently announced the addition of the new Align-Trac trailing arm-to-hanger pivot connection for trailer air suspensions. This Technical Bulletin outlines the procedure to align the axle
SECTION 6 WEIGHT & BALANCE/EQUIPMENT LIST
SECTION 6 WEIGHT AND BALANCE / EQUIPMENT LIST TABLE OF CONTENTS Page Introduction... 6-3 Airplane Weighing Procedures... 6-4 Airplane Weighing Form... 6-5 Sample Weight and Balance Record... 6-8 Loading
RIM Hood For Aeromaster Bodies
RIM Hood For Aeromaster Bodies Service Guide WARNING: Hood should be opened by releasing the hold-down straps, lifting the hood, and engaging the prop rod. Be sure prop rod is properly engaged before working
FUSELAGE ASSEMBLY SECOND SECTION (of three)
FUSELAGE ASSEMBLY SECOND SECTION (of three) 1 FRONT FLOOR ASSEMBLY The front floor assembly is fabricated from three pieces of the two ply pre-pregnated panel material supplied. The basic floor panel and
R44-series Ground Handling Wheel (Pop-Out Floats) Installation Kit Instructions ( upgrade to lever-style ground handling wheel assembly) NOTE
R44-series Ground Handling Wheel (Pop-Out Floats) Installation Kit Instructions ( upgrade to lever-style ground handling wheel assembly) NOTE Visit www.robinsonheli.com to verify kit instructions are current
Service Bulletin. ATA 27-00: Flight Controls Rudder-Aileron Interconnect Modification
Service Bulletin Issued: 09 May 2007 Models SR20 and SR22 ATA 27-00: Flight Controls Rudder-Aileron Interconnect Modification COMPLIANCE Mandatory: Accomplish this Service Bulletin within 25 Flight Hours
57-50 FLIGHT SURFACES
FLIGHT SURFACES 1. DESCRIPTION The flaps are mounted to the trailing edge of each wing between the inboard end of the ailerons and the fuselage. The ailerons are located near the wing tips and hinge to
RIGGING THE FLIGHT CONTROLS
RIGGING THE FLIGHT CONTROLS Rigging refers to the installation and adjustment of the rods that move flight surfaces in response to inputs from the controls of the helicopter. These rods are cut to length,
Service Bulletin No: Ref No: 170 Modification No: EC ATA Chapter: 53
PILATUS AIRCRAFT LTD. STANS, SWITZERLAND Service Bulletin No: 53-014 Ref No: 170 Modification No: EC-15-0854 ATA Chapter: 53 FUSELAGE - MAIN FRAMES REPLACE THE LEFT AND / OR RIGHT FRAME 11 FITTINGS 1.
36-01 REV 1: Updated figure to depict current F Bellcrank configuration.
REVISION DESCRIPTION: 36-01 REV 1: Updated figure to depict current F-00067 Bellcrank configuration. 36-06 REV 1: Updated Figure 1 and Figure 2 to depict current F-00067 Bellcrank configuration. 36-07
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
Single Engine MODIFICATION KIT
Single Engine MODIFICATION KIT TITLE SECURITY LOCK INSTALLATION EFFECTIVITY Model Serial Numbers 172R 17280001 and On 172S 172S8001 and On 182S 18280001 thru 18280944 182T 18280945 and On T182T T18208001
Intentionally left blank
Supplement D42L AFM Intentionally left blank Page 9-S3-2 DOT Approved D42L AFM Supplement LIST OF EFFECTIVE PAGES Chapter Page Date 0 DOT-approved 9-S3-1 9-S3-2 LOEP 9-S3-3 9-S3-4 TOC 9-S3-5 9-S3-6 1 9-S3-7
Page REV 1: Added "Step 4: Bend the tabs on the wiring channel to match the slant of the F L & -R Tunnel Sides."
14401 Keil Road NE, Aurora, Oregon, USA 97002 PHONE 503-678-6545 FAX 503-678-6560 www.vansaircraft.com info@vansaircraft.com Service Letters and Bulletins: www.vansaircraft.com/public/service.htm REVISION
Waco Regional Airport P.O. Box 5500 Waco, Texas Beechcraft King Air 200 & 300 Series Airplanes INSTRUCTIONS FOR CONTINUED AIRWORTHINESS
Waco Regional Airport P.O. Box 5500 Waco, Texas 76708 Beechcraft King Air 200 & 300 Series Airplanes INSTRUCTIONS FOR CONTINUED AIRWORTHINESS ICA Manual No. 26012-30 Revision 1 DEC. 2015 RECORD OF REVISIONS
USA G-103 Twin Astir
USA G-103 Procedures for safe assembly and dis-assembly of the glider (Trailers 2 and 3) Grob Glider Rigging Tools Required: Needle nosed pliers Wire cutters (side cut) Very large crescent wrench (for
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
Installation Instructions - D-Series Warming Cabinet Instruction Door for Hinge UseReversal (Glass and Stainless Steel Doors)
Header Cam Lock Reversal... pg 1-4 Glass Door hinge reversal..... pg 5-9 Steel Door hinge reversal..... pg 10-13 Remove Panels Before reversing door hinges, the Header Cam Lock assembly must be reversed.
Falcon 5250 complete repair kit
Towing and Suspension Solutions 855010-02 08-14 Falcon 5250 complete repair kit part number 910003-55 This kit contains the components to replace the Falcon 5250 Autowlok button assemblies, collar shoulder
Belt Conveyor Systems
Belt Conveyor Systems Product & Installation Manual 24-in, 36-in, and 48-in Widths Manual #: IM-704-01 i 11/14 ii Table of Contents SECTION 1 OVERVIEW 1-1 System Length 1-1 Component Dimensions 1-2 Drive
MD - RA. Minister s Delegates - Recreational Aviation Représentants du Ministre - Aviation de Loisir Service d Inspection
Think Safety Inspection Service MD - RA Pensons Sécurité Minister s Delegates - Recreational Aviation Représentants du Ministre - Aviation de Loisir Service d Inspection 51% Amateur Determination Checklist
Service Bulletin. SB-GA Issue 1. Subject: Horizontal Stabiliser Attachment Area Inspection and Reinforcement. Applicability: Amendments:
PO Box 881, Morwell, Victoria 3840, Australia Ph + 61 (0) 3 5172 1200 Fax + 61 (0) 3 5172 1201 www.mahindraaerospace.com Service Bulletin SB-GA8-2016-163 Issue 1 OPTIONAL Subject: Horizontal Stabiliser
SECTION 4 NORMAL PROCEDURES CONTENTS
CONTENTS Page Recommended Airspeeds....................... 4-1 Daily or Preflight Checks........................ 4-1 Before Starting Engine.......................... 4-6 Engine Starting Tips...........................
TL REPAIR MANUAL. Telma model FV61-00 (FU831310) replacement on Dana 19060S axle. Page 1 of 8 30jun10
TL103035 REPAIR MANUAL Telma model FV61-00 (FU831310) replacement on Dana 19060S axle Page 1 of 8 30jun10 Exploded view TL103035 Stator carrier Telma Unit Flange Yoke Page 2 of 8 30jun10 Disassembly 1.
Ground Effects, P/N: (V6), (V8)
, P/N: 92248596 (V6), 92248560 (V8) 3. Open trunk and remove 3 scrivets per side. Retain. Remove LH and RH tail lamp access cover. Retain. Refer to Figure 1. NOTE: Installation is made easier with the
Copyright 1999 Inter-Industry Conference On Auto Collision Repair v.4.0
Uniform Procedures For Collision Repair DO31P Skin Copyright 1999 Inter-Industry Conference On Auto Collision Repair v.4.0 1. Description This procedure describes the complete or partial replacement of
SECTION 4 NORMAL PROCEDURES CONTENTS
CONTENTS Page Recommended Airspeeds....................... 4-1 Daily or Preflight Checks........................ 4-1 Before Starting Engine.......................... 4-6 Starting Engine and Run-Up......................
CIRRUS AIRPLANE MAINTENANCE MANUAL
FLIGHT SURFACES. DESCRIPTION The flaps are mounted to the trailing edge of each wing between the inboard end of the ailerons and the fuselage. The ailerons are located near the wing tips and hinge to the
NOTE. KI & KI Revision H
KI-179-5 & KI-179-7 R22-series Kannad AF Integra ELT Installation Kit Instructions For R22 helicopters without ELTs or if replacing previously installed Pointer 3000-10 or 4000-10 ELT (RHC Inst l) NOTE
FIGURE 2: ADDING FITTINGS TO BRAKE ASSEMBLY (RIGHT SHOWN) FIGURE 1: ATTACHING AND ALIGNING THE MAIN GEAR AXLES
VAN'S AIRCRAFT, INC. Step 2: Apply pipe thread sealant and attach the fluid fittings to the brake as shown in Figure 2. Note that the brakes should mirror each other when installed. Step 1: Bolt the main
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,
SECTION 4 NORMAL PROCEDURES CONTENTS
CONTENTS Page Recommended Airspeeds....................... 4-1 Daily or Preflight Checks........................ 4-1 Cold Weather Operation........................ 4-5 Before Starting Engine..........................
Accident Prevention Program
Accident Prevention Program Maintenance Aspects of Owning Your Own Airplane Introduction As an owner-pilot, FAR Part 43 allows you to perform certain types of inspections and maintenance on your airplane.
Chapter 73. Engine Fuel and Control
Chapter 73 Engine Fuel and Control PAGE 1 Table of Contents Chapter Title 73-20-00 CONTROLLING............................. 3 73-20-10 Throttle..................................... 3 73-20-11 Throttle
TECHNICAL MANUAL AVIATION UNIT AND INTERMEDIATE MAINTENANCE INSTRUCTIONS ARMY MODEL UH-1H/V/EH-1H/X HELICOPTERS
TECHNICAL MANUAL AVIATION UNIT AND INTERMEDIATE MAINTENANCE INSTRUCTIONS ARMY MODEL UH-1H/V/EH-1H/X HELICOPTERS This manual supersedes TM 55-1520-210-23-2, 20 February 1979, including all changes. HEADQUARTERS,
AFT MOUNTED OXYGEN SYSTEM INSTALLATION BEECHCRAFT 33, 35, 36, 55, AND 58
ENGINE TECHNOLOGIES INC. REPORT 35-4960004, REV. A, JULY 12, 2013 INSTALLATION INSTRUCTIONS FOR OXYGEN SYSTEM ON HAWKER BEECHCRAFT S35, V35, V35A, V35B, 35-C33A, E33A, 36, A36, F33A, G33, 95-55, 95-A55,
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
THE SERIES-E POWR Slider
C.R. LAURENCE CO., INC. PATENT NO. 4,920,698 THE SERIES-E POWR Slider MODEL: EPC814S 2014+ CHEVY/GMC SILVERADO/SIERRA 1500 NAGS: DY90122PK5 ELECTRIC SLIDING REAR WINDOW 2014 + CHEVY/GMC SILVERADO/SIERRA
Service Bulletin No: Ref No: 121 Modification No: INSPECTION ATA Chapter: 53
PILATUS AIRCRAFT LTD. STANS, SWITZERLAND Service Bulletin No: 53-014 Ref No: 121 Modification No: INSPECTION ATA Chapter: 53 FUSELAGE - GENERAL INSPECTION FOR CORROSION ON THE UPPER LEFT AND RIGHT LONGERONS
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
HARTZELL PROPELLER INC.
HARTZELL PROPELLER INC. One Propeller Place Piqua, Ohio 45356-2634 U.S.A. Telephone: 937.778.4200 Fax: 937.778.4391 MANUAL REVISION TRANSMITTAL Manual (61-00-11) Propeller Owner's Manual and Logbook REVISION
Service Bulletin No: Ref No: 331 Modification No: EC , EC ATA Chapter: 27
PILATUS AIRCRAFT LTD, STANS, SWITZERLAND Service Bulletin No: 27-021 Ref No: 331 Modification No: EC-14-0549, EC-14-0714 ATA Chapter: 27 FLIGHT CONTROLS - AILERON CONTROL SYSTEM AILERON TAB COUNTER BALANCE
»Product» Safety Warning
D1401 Installation Instructions 2013 Ram 3500, 2014 Ram 2500 4.5" Radius Arm Suspension Lift Read and understand all instructions and warnings prior to installation of product and operation of vehicle.