*C208ELP-100-1, REV. B ITEM # P/N DESCRIPTION QTY TYP 0 *C208ELP-100-1, REV. B EXTERNAL LOAD PROVISIONS CONFIGURATION 1 KIT
|
|
|
- Cameron Strickland
- 5 years ago
- Views:
Transcription
1 Bill of Materials *C208ELP-100-1, REV. B ITEM # P/N DESCRIPTION QTY TYP 0 *C208ELP-100-1, REV. B EXTERNAL LOAD PROVISIONS CONFIGURATION 1 KIT 1 C208ELP FWD EXTERNAL LOAD PROVISIONS INST'N 1 EA 2 C208ELP AFT EXTERNAL LOAD PROVISIONS INST'N 1 EA 3 C208ELP LOAD BEAM INST'N (ALT: C208ELP-112-2) 1 EA Page 1 of 1
2 Bill of Materials *C208ELP-100-2, REV. B ITEM # P/N DESCRIPTION QTY TYP 0 *C208ELP-100-2, REV. B EXTERNAL LOAD PROVISIONS CONFIGURATION 1 KIT 2 C208ELP AFT EXTERNAL LOAD PROVISIONS INST'N 1 EA 3 C208ELP LOAD BEAM INST'N (ALT: C208ELP-112-2) 1 EA 4 C208ELP FWD EXTERNAL LOAD PROVISIONS INST'N 1 EA Page 1 of 1
3
4 FUSELAGE STATION (in) Y max (in) MAX FRONT 3.0 SQ FT (SYMMETRIC INST'N SHOWN) 65.0 in (max) MAX FRONT 3.0 SQ FT Y (SEE TABLE)
5 SINGLE COMPONENT WEIGHT LIMITATIONS in LATERAL LOCATION (+ ) 9.0 in 11.1 in 13.2 in 15.4 in 17.5 in 19.6 in 21.7 in FS 142 & FWD FS 143 & AFT FS 142 & FWD FS 143 & AFT FS 142 & FWD FS 143 & AFT FS 142 & FWD FS 143 & AFT FS 142 & FWD FS 143 & AFT = 1.0 sq ft = 1.5 sq ft = 2.0 sq ft = 2.5 sq ft = 3.0 sq ft ALLOWABLE COMPONENT WEIGHT (lbs) 2-ITEM SYMMETRIC COMPONENT WEIGHT LIMITATIONS 2.1 in LATERAL LOCATION (+ ) 9.0 in 11.1 in 13.2 in 15.4 in 17.5 in 19.6 in 21.7 in ALLOWABLE COMPONENT WEIGHT (lbs, EA.) = 1.0 sq ft = 1.5 sq ft = 2.0 sq ft = 2.5 sq ft = 3.0 sq ft FS 142 & FWD FS 143 & AFT FS 142 & FWD FS 143 & AFT
6 Bill of Materials *C208ELP-110-1, REV. D ITEM # P/N DESCRIPTION QTY TYP 0 *C208ELP-110-1, REV. D FWD EXTERNAL LOAD PROVISIONS 1 KIT 1 C208ELP CHANNEL 2 EA 2 C208ELP CHANNEL 2 EA 3 C208ELP CHANNEL 2 EA 5 C208ELP ANGLE 12 EA 6 C208ELP ANGLE 8 EA 9 AN970-6 WASHER 8 EA 10 C208ELP LOAD RAIL 2 EA 13 AN6-7A BOLT (Alt: AN6H-7A) 12 EA 14 MS21042L6 NUT 12 EA 17 NAS1149D0663J WASHER 20 EA 19 C208ELP DOUBLER 2 EA 20 C208ELP DOUBLER 1 EA 21 C208ELP SHIM 2 EA 22 MS20470AD4-4.5 RIVET 30 EA 23 C208ELP CHANNEL 4 EA 27 NAS1580C3T8 SCREW 28 EA 28 NAS1580C3T10 SCREW 40 EA 29 MS21042L3 NUT 68 EA 30 NAS1149D0332J WASHER 68 EA 31 NAS1149D0363J WASHER 68 EA Page 1 of 1
7 Bill of Materials *C208ELP-110-2, REV. D ITEM # P/N DESCRIPTION QTY TYP 0 *C208ELP-110-2, REV. D AFT EXTERNAL LOAD PROVISIONS 1 KIT 3 C208ELP CHANNEL 4 EA 4 C208ELP CHANNEL 12 EA 5 C208ELP ANGLE 10 EA 6 C208ELP ANGLE 6 EA 7 C208ELP ANGLE 8 EA 8 C208ELP ANGLE 8 EA 9 AN970-6 WASHER 8 EA 11 C208ELP LOAD RAIL 2 EA 12 C208ELP LOAD RAIL 2 EA 13 AN6-7A BOLT (Alt: AN6H-7A) 18 EA 14 MS21042L6 NUT 18 EA 17 NAS1149D0663J WASHER 32 EA 19 C208ELP DOUBLER 1 EA 21 C208ELP SHIM 2 EA 22 MS20470AD4-4.5 RIVET 11 EA 24 C208ELP-T RAIL ASSY TEMPLATE 1 EA 27 NAS1580C3T8 SCREW 44 EA 28 NAS1580C3T10 SCREW 64 EA 29 MS21042L3 NUT 108 EA 30 NAS1149D0332J WASHER 108 EA 31 NAS1149D0363J WASHER 108 EA Page 1 of 1
8 Bill of Materials *C208ELP-110-3, REV. D ITEM # P/N DESCRIPTION QTY TYP 0 *C208ELP-110-3, REV. D FWD EXTERNAL LOAD PROVISIONS 1 KIT 1 C208ELP CHANNEL 2 EA 2 C208ELP CHANNEL 2 EA 3 C208ELP CHANNEL 2 EA 5 C208ELP ANGLE 10 EA 6 C208ELP ANGLE 6 EA 9 AN970-6 WASHER 8 EA 13 AN6-7A BOLT (Alt: AN6H-7A) 10 EA 14 MS21042L6 NUT 10 EA 17 NAS1149D0663J WASHER 16 EA 19 C208ELP DOUBLER 1 EA 20 C208ELP DOUBLER 1 EA 21 C208ELP SHIM 2 EA 22 MS20470AD4-4.5 RIVET 19 EA 23 C208ELP CHANNEL (Replaces C208ELP ) 2 EA 25 C208ELP LOAD RAIL 2 EA 27 NAS1580C3T8 SCREW 20 EA 28 NAS1580C3T10 SCREW 32 EA 29 MS21042L3 NUT 52 EA 30 NAS1149D0332J WASHER 52 EA 31 NAS1149D0363J WASHER 52 EA Page 1 of 1
9
10
11
12 DETAIL C DETAIL G DETAIL B SECTION E-E' SUB-DETAIL J DETAIL F DETAIL D DETAIL A
13
14
15 Bill of Materials *C208ELP-112-1, REV. C ITEM # P/N DESCRIPTION QTY TYP 0 *C208ELP-112-1, REV. C LOAD BEAM INST'N 1 KIT 1 C208ELP DOVETAIL RAIL ASSY 1 EA 2 C208ELP THREADED ROD 2 EA 3 C208ELP MOUNT BLOCK ASSY 1 EA 4 C208ELP SUPPORT BRACKET ASSY 2 EA 5 407BF SUPPORT 2 EA 6 ES TRACK TIE-DOWN FITTING 4 EA 7 ES RF ROD END 4 EA 8 MS21042L6 NUT 4 EA 9 MS21042L4 NUT 2 EA 10 MS SCREW 4 EA 11 AN4-10A BOLT 4 EA 12 AN316C4R JAM NUT (OR EQUIV.) 4 EA 13 NAS1149F0332P WASHER 4 EA 14 NAS1149F0363P WASHER 4 EA 15 NAS1149D0432J WASHER (ALT: NAS1149D0432K) 2 EA 16 NAS1149D0463J WASHER (ALT: NAS1149D0463K) 5 EA 17 NAS1149F0632P WASHER 4 EA 18 MS SOCKET HEAD CAP SCREW (ALT: NAS P) 2 EA 19 ES WASHER 2 EA 21 C208ELP GROUND STRAP 1 EA 22 AN4-4A BOLT 1 EA Page 1 of 1
16 Bill of Materials *C208ELP-112-2, REV. C ITEM # P/N DESCRIPTION QTY TYP 0 *C208ELP-112-2, REV. C LOAD BEAM INST'N 1 KIT 3 C208ELP MOUNT BLOCK ASSY 1 EA 6 ES TRACK TIE-DOWN FITTING 4 EA 8 MS21042L6 NUT 4 EA 17 NAS1149F0632P WASHER 4 EA 20 C208ELP DOVETAIL RAIL ASSY 1 EA 21 C208ELP GROUND STRAP 1 EA 22 AN4-4A BOLT 1 EA Page 1 of 1
17
18
Bill of Materials *206EC-500-1, REV. M ITEM # P/N DESCRIPTION QTY TYP 0 *206EC-500-1, REV. M 206A/B BLEED AIR PLUMBING INST'N 1 KIT 1 NAS1149F1290P WA
Bill of Materials *206EC-500-1, REV. M ITEM # P/N DESCRIPTION QTY TYP 0 *206EC-500-1, REV. M 206A/B BLEED AIR PLUMBING INST'N 1 KIT 1 NAS1149F1290P WASHER 2 EA 2 ES00140-3 RUBBER EXTRUSION 12 IN 3 NAS43DD3-23FC
*407AC-110-3, REV. D ITEM # P/N DESCRIPTION QTY TYP 0 *407AC-110-3, REV. D AIR CONDITIONER INSTALLATION 1 KIT
Bill of Materials *407AC-110-3, REV. D ITEM # P/N DESCRIPTION QTY TYP 0 *407AC-110-3, REV. D AIR CONDITIONER INSTALLATION 1 KIT 2 407AC-210-1 CONDENSER INSTALLATION 1 KIT 3 407AC-310-3 COMPRESSOR INSTALLATION
PARAVION TECHNOLOGY, INC AIRWAY AVENUE FT. COLLINS, COLORADO 80524
[Rev. 5, 11/07/07] PARAVION TECHNOLOGY, INC. 2001 AIRWAY AVENUE FT. COLLINS, COLORADO 80524 INSTRUCTIONS FOR CONTINUED AIRWORTHINESS 407H-120M BLEED-AIR CABIN HEATER INSTALLATION BELL MODEL 407 HELICOPTERS
SERVICE INSTRUCTION SI Revision 1
SERVICE INSTRUCTION SI-25-02 Revision 1 TITLE: Aft Seats Inertia Reel Harness Installation (Mod 1229) SUBJECT / REASON / DESCRIPTION: The FBA-2C1 and FBA-2C2 aircraft are equipped with three individual
PARAVION TECHNOLOGY, INC AIRWAY AVENUE FT. COLLINS, COLORADO 80524
PARAVION TECHNOLOGY, INC. 2001 AIRWAY AVENUE FT. COLLINS, COLORADO 80524 INSTRUCTIONS FOR CONTINUED AIRWORTHINESS DZUS SNOW DEFLECTOR INSTALLATION BELL 206L-1/L-3/L-4 AND 407 MODELS Cover Rev. 3, 12/12/05
PARTS MANUAL FOR WIPLINE MODEL 6100 AMPHIBIAN & SEAPLANE FLOATS PILATUS PC-6/B2-H4
WIPLINE FLOATS SKIS MODIFICATIONS AIRCRAFT SALES AVIONICS INTERIOR MAINTENANCE PAINT REFINISHING PARTS MANUAL FOR WIPLINE MODEL 6100 AMPHIBIAN & SEAPLANE FLOATS PILATUS PC-6/B2-H4 1700 Henry Ave Fleming
ILLUSTRATED PARTS CATALOG STC SR01616SE
ILLUSTRATED PARTS CATALOG STC SR066SE ENGINE INLET BARRIER FILTER SYSTEM Sikorsky S-76A+/A++/C/C+ This document provides information to assist with the identification of parts and assemblies for the 076T-
SERVICE KIT thru , 631, 634, 675 R thru R F thru F FR thru FR
TITLE SEAT BELT AND SHOULDER HARNESS KIT INSTALLATION EFFECTIVITY MODEL SERIES SERIAL NUMBERS 182 33000 thru 18268368 182 613, 631, 634, 675 R182 R18200001 thru R18201973 F182 F18200001 thru F18200169
CHAPTER 63 MAIN ROTOR DRIVE SYSTEM. Figure Title Page 63-1 Main Rotor Gearbox and Mast Assembly Main Rotor Gearbox Installation
CHAPTER 63 MAIN ROTOR DRIVE SYSTEM Figure Title Page 63-1 Main Rotor Gearbox and Mast Assembly...................... 63.0 63-5 Main Rotor Gearbox Installation............................. 63.4 63-7 Rotor
TECHNICAL BULLETIN May 2013 SUBJECT: TAIL ROTOR GEARBOX 3 PIECE FAIRING, MODIFICATION OF
TECHNICAL BULLETIN 206-13-205 24 May 2013 MODEL AFFECTED: 206A/B SUBJECT: TAIL ROTOR GEARBOX 3 PIECE FAIRING, MODIFICATION OF HELICOPTERS AFFECTED: Serial number 004 through 1251. COMPLIANCE: At customer
Page: MEMO: In NOTE before Step 5, "Whenever possible, ream using a drill press..." was "Always ream using a drill press...".
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
TECHNICAL BULLETIN May 2013 Revision A, 11 July 2013 SUBJECT: TAIL ROTOR GEARBOX 3 PIECE FAIRING, MODIFICATION OF
TECHNICAL BULLETIN 206-13-205 24 May 2013 Revision A, 11 July 2013 MODEL AFFECTED: 206A/B SUBJECT: TAIL ROTOR GEARBOX 3 PIECE FAIRING, MODIFICATION OF HELICOPTERS AFFECTED: Serial number 004 through 1251.
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
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
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
PARAVION TECHNOLOGY, INC AIRWAY AVENUE FT. COLLINS, COLORADO 80524
Rev. 2, 01/31/00 PARAVION TECHNOLOGY, INC. 2001 AIRWAY AVENUE FT. COLLINS, COLORADO 80524 INSTRUCTIONS FOR CONTINUED AIRWORTHINESS 206ER-100 ENGINE RELIGHT SYSTEM INSTALLATION BELL MODEL 206A/B AND 206L
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
P68 SERIES. SERVICE BULLETIN No. 115
vulcanair spa via g. pascoli, 7 80026 casoria (na) italia Tel +39 081 5918111 Fax +39 081 5918172 info@vulcanair.com www.vulcanair.com P68 SERIES ENAC approval of Service Bulletins is limited to technical
ROLL BAR FRAME 2 PLACES F-1231A-FL ROLL BAR FRAME F-1231C INBOARD F-1231B OUTBOARD ROLL BAR STRAP BAGGAGE BULKHEAD
SECTION 24iS/U: ROLLOVER F-1231A-FR ROLL BAR FRAME VAN'S AIRCRAFT, INC. F-1231A-AR ROLL BAR FRAME STRUCTURE F-1231E ROLL BAR SPLICE PLATE 2 PLACES F-1232A ROLL BAR BRACE F-01254-R-1 SUPPORT FRAME & F-01207
Nomad RE -ALIGNMENT HORIZONTAL STABILISER CONTROL PULLEY (MOD N63) Page No Rev No
RE -ALIGNMENT HORIZONTAL STABILISER CONTROL PULLEY (MOD N63) 1. PLANNING INFORMATION A. Effectivity: (1) Aircraft Affected: All Nomad N22-Series and N24-Series aircraft whose log books do not already record
PARTS MANUAL CHRISTEN HUSKY A-1, A-1A, A-1B, A-1C
WIPLINE FLOATS SKIS MODIFICATIONS AIRCRAFT SALES AVIONICS INTERIOR MAINTENANCE PAINT REFINISHING WIPLINE FLOATS MODEL 2100 PARTS MANUAL CHRISTEN HUSKY A-1, A-1A, A-1B, A-1C 1700 Henry Ave Fleming Field
SERVICE BULLETIN REVISION TRANSMITTAL
REVISION TRANSMITTAL REASON This sheet transmits Revision 1 to, which: A. Adds instructions and parts to change the Pulselite controller for airplanes with the Pulselite feature. NOTE: This revision replaces
SERVICE BULLETIN. Citation SB TITLE DOORS - WIDE DOOR INSTALLATION MODIFICATION
TITLE DOORS - WIDE DOOR INSTALLATION MODIFICATION EFFECTIVITY MODEL SERIAL NUMBERS 560 (Citation Encore) -0539 thru -0707 560 (Citation Encore+) -0751 thru -0815 NOTE: This modification may only be accomplished
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
SERVICE BULLETIN TITLE AIR CONDITIONING - R134A AIR CONDITIONER SYSTEM INSTALLATION FOR AIRPLANES EQUIPPED WITH G1000 AND 867 SHP ENGINE
TITLE AIR CONDITIONING - R134A AIR CONDITIONER SYSTEM INSTALLATION FOR AIRPLANES EQUIPPED WITH G1000 AND 867 SHP ENGINE EFFECTIVITY DESCRIPTION MODEL 208B SERIAL NUMBERS 208B5000 and On To provide parts
PARTS MANUAL FOR WIPLINE MODEL 4000 AMPHIBIOUS AND SEAPLANE FLOATS CESSNA 185, 206
WIPLINE FLOATS SKIS MODIFICATIONS AIRCRAFT SALES AVIONICS INTERIOR MAINTENANCE PAINT REFINISHING PARTS MANUAL FOR WIPLINE MODEL 4000 AMPHIBIOUS AND SEAPLANE FLOATS CESSNA 185, 206 1700 Henry Ave Fleming
Ignitor supplied with Engine. Power Plant Group - Page 1 (AT-502B) Date: 1/18
4 9 8 9 48 0 4 4 0 0 4 4 Ignitor supplied with Engine 8 4 4 4 Power Plant Group - Page (AT-0B) Date: / POWER PLANT GROUP - Figure. Power Plant, Engine Mount, Oil Cooler and Ejector Installations 04-8 Engine
Appendix D. Vizion PMA Autopilot Piper PA-28/32 Installation
Appendix D Vizion PMA Autopilot Piper PA-28/32 Installation RESTRICTION ON USE, DUPLICATION, OR DISCLOSURE OF PROPRIETARY INFORMATION THIS DOCUMENT CONTAINS PROPRIETARY INFORMATION OF TRUTRAK FLIGHT SYSTEMS,
WIPLINE FLOATS MODEL 2100 PARTS MANUAL
WIPLINE FLOATS SKIS MODIFICATIONS AIRCRAFT SALES AVIONICS INTERIOR MAINTENANCE PAINT REFINISHING WIPLINE FLOATS MODEL 2100 PARTS MANUAL CESSNA 170 1700 Henry Ave Fleming Field (KSGS), South St. Paul, MN
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
HYDRAULIC SYSTEM #1 AND #2 ACCUMULATOR P/N , REMOVAL OF
TECHNICAL BULLETIN 212-17-216 24 May 2017 MODEL AFFECTED: 212 SUBJECT: HYDRAULIC SYSTEM #1 AND #2 ACCUMULATOR P/N 212-076-007-003, REMOVAL OF HELICOPTERS AFFECTED: Serial numbers 30502 through 30603, 30611
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
OFFICE HOURS TECHNICAL SUPPORT SPARES ORDERS CORRESPONDENCE REGARDING ORDERS
Robinson Helicopter Company Phone: (310) 539-0508 2901 Airport Drive Fax: (310) 539-5198 Torrance, California 90505-6115 Web: www.robinsonheli.com UNITED STATES Email: customerservice@robinsonheli.com
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 REVISION
Service Bulletin No.: DAC Rev 3 Date Issued: October 27, 1999 Title: 2-Speed Electric Prime Fuel Pump Page: 1 of 8
Title: 2-Speed Electric Prime Fuel Pump Page: 1 of 8 1. ATA Code: 2820 2. Effectivity: DA20-C1 Aircraft from S/N C0001 up to and including S/N C0089 3. General: This service bulletin addresses the installation
SERVICE BULLETIN THIS BULLETIN IS FAA APPROVED FOR ENGINEERING DESIGN
M20-327 SUBJECT: Mooney wing to fuselage attach fitting plates part number 340035-50 and 340035-502 MODELS/ SN M20R - 29-0523 thru 29-0525 AFFECTED: M20TN - 3-042, 3-043 TIME OF COMPLIANCE: INTRODUCTION:
SERVICE BULLETIN THIS BULLETIN IS FAA APPROVED FOR ENGINEERING DESIGN
MOONEY INTERNATIONAL CORPORATION SERVICE BULLETIN 165 Al Mooney Road North Kerrville, Texas 78028 THIS BULLETIN IS FAA APPROVED FOR ENGINEERING DESIGN SERVICE BULLETIN M20-318 Date: June 2, 2014 SUBJECT:
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 REVISION
P68 VARIANTS SERVICE INSTRUCTION. No. 82. SUBJECT: INCREMENT OF MAXIMUM TAKE-OFF WEIGHT FROM 1990 Kg TO 2084 Kg.
vulcanair spa via g. pascoli, 7 80026 casoria (na) italia Tel +39 081 5918111 Fax +39 081 5918172 info@vulcanair.com www.vulcanair.com P68 VARIANTS SERVICE INSTRUCTION No. 82 SUBJECT: INCREMENT OF MAXIMUM
A bar next to the text in the right hand margin indicates that the text has been changed as a result of the most recent document revision.
Cessna Aircraft Company Page 1 REVISIONS Rev Date By Approved By - 30 November 2009 Jay York A 18 March 2010 Jay York B 30 March 2010 Jay York ECR 067497 Section ALL Description Initial Release NOTE: A
SAMPLE BLUE STAR CONVERSION INSTALLATION OF CONTINENTAL IO-470-N IN H35 BONANZA SERIAL NUMBER D-4866 THROUGH D-5330 LWS 470-H35 STC # SA2660SW
BLUE STAR CONVERSION INSTALLATION OF CONTINENTAL IO-470-N IN H35 BONANZA SERIAL NUMBER D-4866 THROUGH D-5330 LWS 470-H35 STC # SA2660SW SAMPLE BLUE STAR CONVERSION TABLE OF CONTENTS PAGE DESCRIPTION PAGE
INSTRUCTIONS FOR CONTINUED AIRWORTHINESS AND EQUIPMENT MAINTENANCE MANUAL FOR Bell 212/ 412 CARGO NET/TROOP SEAT
INSTRUCTIONS FOR CONTINUED AIRWORTHINESS FOR STC No. SR09485RC ON BELL 212/412 REPORT NUMBER HF-412-ICA-CARGO NET-01 HELIFAB 1318 SMEDE HWY. BROUSSARD, LA 70518 THIS MANUAL IS PREPARED TO PROVIDE INFORMATION,
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,
ROBINSON HELICOPTER COMPANY. R66 Spare Parts Price List
ROBINSON HELICOPTER COMPANY R66 Spare Parts Price List A022-4 Compass Assy., 28V 313.00 A039-19 Position Light Assy., LED, LH, 28V 388.00 A039-20 Position Light Assy., LED, RH, 28V 388.00 A041-10 Pin.85
SERVICE KIT. February 8, 1980 Revision C - April 16, 1999 Page 1 of 24
, TITLE WING FRONT SPAR LOWER CAP MODIFICATION EFFECTIVITY MODEL YEAR SERIAL NUMBERS 401 1967/1968 401-0001 thru 401-0322 401A 1969 401A0001 thru 401A0132 401B 1970/1971 401B0001 thru 401B0121 401B 1972
SECTION 26iS/U: FUEL TANK VAN'S AIRCRAFT, INC. T R OUTBOARD RIB IE-00001X MECHANICAL FUEL GAUGE T R INBOARD RIB T R
VAN'S AIRCRAFT, INC. SECTION 26iS/U: IE-00001X MECHANICAL FUEL GAUGE T-01222-R OUTBOARD RIB FUEL TANK T-01223-R INBOARD RIB T-01228 RETURN LINE BRACKET T-01224-R INBOARD RIB T-01229 INLET ASSEMBLY T-01223-L
SD3-60 STRUCTURAL REPAIR MANUAL STABILIZER (FIN) - STRUCTURAL IDENTIFICATION
SRM 12.0.0.0VERTICAL STABILIZER (FIN) STRUCTURAL IDENTIFICATION 1. General This section identifies the skin panels and structural components of the vertical stabilier. Details are given of specific location;
The engine cowling installation and firewall should be inspected and modified as specified in this Service Bulletin.
Single Engine Service Bulletin August 25, 2008 TITLE ENGINE COWLING ALIGNMENT INSPECTION AND MODIFICATION EFFECTIVITY Model Serial Numbers 172R 17280001 thru 17280724 172S 172S8001 thru 172S8201 REASON
Page REV 1: Added 'Step 2: See the "REMOVE THIS TAB, BOTH SIDES" callout near Detail A. Modify four SB375-4 Snap Bushings as shown.
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
X Jeep / Eagle Model 44 /216 Front Axles for. 4 x 2, Military, J10, J20, Cherokee, Honcho, Wagoneer, Grand Wagoneer
X510-9 Jeep / Eagle 1978-1992 Model 44 /216 Front Axles for 4 x 2, Military, J10, J20, Cherokee, Honcho, Wagoneer, Grand Wagoneer 329 Exploded View X510-9 330 X510-9 Parts Listing ITEM NO. PART NUMBER
X Dodge / Chrysler /2. Model 44 /216 Disconnect Front Axles for. W1500 and W2500 Ram
Dodge / Chrysler 1994-1998 1 /2 Model 44 /216 Disconnect Front Axles for W1500 and W2500 Ram 15 Exploded View 16 Parts Listing ITEM NO. PART NUMBER DESCRIPTION 1 (3) Housing Axle Service 2 (1) Drive Pinion
Ayres service bulletin Corporation
Ayres service bulletin Corporation No. SB-AG-37 P.O. BOX 3090 ONE AYRES WAY ALBANY, GEORGIA 31706-3090 PHONE 229/883-1440 FAX 229/439-9790 Service Bulletin No. SB-AG-37 Page 1 of 12 Approval: FAA Approved
Autodesk VEX Robotics Curriculum
Page 1 of 22 Autodesk VEX Robotics Curriculum Activity In this activity, you build a complete robot called Tumbler. You start by building the right-side drive train. 1. To complete the first step: Locate
INSTALLATION INSTRUCTIONS EXTERNAL AUXILIARY FUEL SYSTEM P/N
INSTALLATION INSTRUCTIONS EXTERNAL AUXILIARY FUEL SYSTEM P/N 41228-000-002-007 Page 1 of 45 List of Revisions Rev. Date Pages Description Approved IR 09/12/05 All Initial Release N/C All Updated to Apical
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
STOL CH F8-2 Front Floor Stiffener. Cut and position the Front Floor Stiffener to the Floor 7F8-7. Back drill through the Floor 7F8-7.
Wait to drill the ends of the Seat Front 7F11-1 to the L angle on the cabin side at location A-A Ref 7-F-9 until after the Cabin Frame is installed. Ref Fuselage Cabin Frame, Section 10, page 11. NOTE:
GENUINE PARTS INSTALLATION INSTRUCTIONS
GENUINE PARTS INSTALLATION INSTRUCTIONS 1. 2. 3. 4. DESCRIPTION: APPLICATION: PART NUMBER: KIT CONTENTS: Fog Lamp Kit Versa Note (SV Only) 999L1 4Z000 - Fog Lamp Kit Item QTY Description Service Part Number
LSM Rev P
Installation Instructions Cessna Citation CJ Series Landing Lights Models 525, 525A, 525B (S/N 525-0001 thru 525-0679, 525A-0001 thru 525A-0416, 525B-0001 thru 525B-0262, 525B-0264 thru 525B-0293) Cessna
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
39 - EFFECTIVE PAGES. Beechcraft Corporation PAGE 1 AUG 01/17 99 ILLUSTRATED PARTS CATALOG DATE CH-SECT-FIG
CH-SECT-FIG PAGE NO. DATE CH-SECT-FIG PAGE NO. DATE 39 - CONTENTS 1 39-10-10 0 39-10-10 1 39-10-10 2 39-10-20 0 39-10-20 1 39-10-20 2 39-10-20 3 39-10-20 4 39-10-20 5 39-10-20 6 39-10-30 0 39-10-30 0A
FAA approval has been obtained on technical data in this publication that affects airplane type design.
Single Engine Service Bulletin January 28, 2008 TITLE ENGINE COWLING ALIGNMENT INSPECTION AND MODIFICATION EFFECTIVITY Model Serial Numbers 172R 17280725 thru 17281262 172S 172S8202 thru 172S10006 REASON
REVISION LIST CHAPTER 21: FLAP SYSTEM COMPLETION
REVISION LIST CHAPTER 21: The following list of revisions will allow you to update the Legacy construction manual chapter listed above. Under the Action column, R&R directs you to remove and replace the
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 Weight and Balance... 6-7 Sample Weight and Balance
FOR REFERENCE ONLY 9
2 4 3 5 16 6 1 15 12 11 FOR REFERENCE ONLY 18 19 20 9 17 8 7 10 21 22 Applicability: BEECHCRAFT Drawing: AFC-W300 Debonair 35-33, 35-A33, 35-B33, 35-C33 Date: 06/01/05 Airwolf Parts List No. AFC-W300 Index
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 REVISION
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
A Product Line of Sonex Aircraft LLC 511 Aviation Road Oshkosh, WI Tel. (920) Fax. (920)
A Product Line of Sonex Aircraft LLC 511 Aviation Road Oshkosh, WI 54902 Tel. (920)-231-8297 Fax. (920)-426-8333 www.aeroconversions.com Rev C, 03/01/2013 (7 pages) The AeroConversion's Pitch Trim unit
ZENITH 601, VLS INSTALLATION
ZENITH 601, VLS INSTALLATION 09/99 DRWG. 6500-A READ INSTRUCTIONS COMPLETELY BEFORE BEGINNING INSTALLATION! The BRS installation for your Zenith 601 was designed to provide a high probability of the aircraft
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
PARAVION TECHNOLOGY, INC AIRWAY AVENUE FT. COLLINS, COLORADO 80524
PARAVION TECHNOLOGY, INC. 2001 AIRWAY AVENUE FT. COLLINS, COLORADO 80524 REPORT NO. PR-369DA-900M PNEUMATIC DOOR OPENER INSTALLATION INSTRUCTIONS FOR 369PDO-100 369, 500N & 600N HELICOPTERS Page i REVISIONS
INSTRUCTIONS, C2 TORSION SPRING REPLACEMENT
LIFT CORPORATION Sht. 1 of 9 DSG# M-14-47 Rev. - Date: 05/31/16 INSTRUCTIONS, C2 TORSION SPRING REPLACEMENT C2 (27 ) TORSION SPRING PIN KIT, P/N 295446-01 (1220) C2-92 TORSION SPRING KIT, P/N 295487-01
PITNEY BOWES FLEXIBLE INK JET TRANSPORT 56 FIT BASE: FIT-56. Parts Manual. (BOM: FIT-56revA) FIT-56parts_rev0 1
FLEXIBLE INK JET TRANSPORT 56 FIT BASE: FIT-56 Parts Manual (BOM: FIT-56revA) FIT-56parts_rev0 1 VERSION HISTORY The table below summarizes the history of this document as it is published onto the company
SECTION 46: ENGINE INSTALLATION VAN'S AIRCRAFT, INC VA-216 FUEL RETURN ASSY FF-1222 MANIFOLD PRESSURE HOSE IGNITION MODULES CLAMP BLOCK
SECTION 46: ENGINE VA-216 FUEL RETURN ASSY VAN'S AIRCRAFT, INC. FF-1222 MANIFOLD PRESSURE HOSE INSTALLATION IGNITION MODULES CLAMP BLOCK GASCOLATOR TO FUEL PUMP HOSE FUEL PRESSURE SENSOR F 4 DTX-S ELBOW
"Figure 2: Trim Washer" was "Figure 1: Trim Washers". Page: 40A-06 REV 1: In Step 6, added "Fully torque the nut."
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
SECTION 4: RV-12 PARTS INDEX
SECTION 4: RV-12 PARTS INDEX PART NUMBER NOMENCLATURE SUB-KIT SECT# PAGE# PART TYPE: MAKE FROM MATERIAL: PART NUMBER NOMENCLATURE SUB-KIT SECT# PAGE# PART TYPE: MAKE FROM MATERIAL: A-1201A-L INBD NOSE
Owner s Manual Dual Cargo Hook System. MD Helicopters 369 Series and 500N
of 49 Dual Cargo Hook System for the MD Helicopters 369 Series and 500N Onboard Systems International 395 NW 3rd Court Vancouver, WA 98685 United States of America Cage Code: Y92 Toll Free Phone: (800)
SERVICE BULLETIN SB
TITLE LIGHTS - LED TAIL POSITION LIGHT INSTALLATION EFFECTIVITY MODEL UNIT NUMBERS 500 (Citation) -0001 thru -0349 with SB500-33-07 incorporated 500 (Citation I) -0350 thru -0528 with SB500-33-07 incorporated,
FKL (25, 75, 150, 205, 250 & 400) Exploded View
3 FKL (5, 75, 50, 05, 50 & 400) Exploded View 3 4 5 6 7 8 9a0 a 3 4 5 6 7 34 35 8 9 0 40 4 4 43 36 37 38 39 44 45 46 65000005 Rev A 4 5 6 Fristam FKL Series Pumps 33 3 7 8 48 47 3 49 9 30 3 b 3 49 33 50
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
INSTRUCTION, GPTLR POWER DOWN HAND PUMP KIT
LIFT CORPORATION Sht. 1 of 29 DSG# M-09-18 Rev. ~ Date: 03/05/14 INSTRUCTION, GPTLR POWER DOWN HAND PUMP KIT GPTLR KIT P/N 283332-01 HAND PUMP MOUNT BRACKET P/N 282381-01 QTY. 1 HAND PUMP HANDLE MOUNT
73 - EFFECTIVE PAGES. Beechcraft Corporation PAGE 1 MODEL 1900D AIRLINER ILLUSTRATED PARTS CATALOG DATE CH-SECT-UNIT-FIG
CH-SECT-UNIT-FIG PAGE NO. DATE CH-SECT-UNIT-FIG PAGE NO. DATE 73 - CONTENTS 1 0 1 2 3 4 5 6 73-10-00-05 0 73-10-00-05 1 73-10-00-05 2 73-10-00-05 3 73-30-00-03 0 73-30-00-03 1 73-30-00-03 2 73-30-00-03
PARTS MANUAL 80D-MQ. Four Stage Full Freeli Mast. Manual Number: Li Technologies, Inc D-MQ
PARTS MANUAL Four Stage Full Freeli Mast Manual Number: 275170 Li Technologies, Inc. 215170 Parts and Service Tel : (864) 647-6320 Fax : (864) 647-7302 Toll Free : (877) 430-6302 Email : parts@lift-tek.com
SUBJECT: FUEL SYSTEM FLOW SWITCHES, P/N , , -003, -101 AND -103, REPLACEMENT OF
ALERT SERVICE BULLETIN 206L-88-52 10 June 1988 Revision A, 26 March 2013 MODEL AFFECTED: 206L and 206L-1 SUBJECT: FUEL SYSTEM FLOW SWITCHES, P/N 206-063- 635-001, 206-064-601-001, -003, -101 AND -103,
PARTS MANUAL. ECN-M0XXX Rev. 2.0, Date Part #
ILM plus,0,,0 PARTS MANUAL ECN-M0XXX Rev..0, Date 0--0 Part #90-07-000 99 Piuma Ave., Cerritos, CA 9070 Tel (888)-77-8 Fax ()-9-88 7 Whitehead Road, Trenton, NJ 089 Tel (09)-87-00 Fax (09)-87-0 Visit our
Page: 42H-03 REV 1: In Figure 1, replace AN507-6R6 with AN507-6R8
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
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
SD3-60 STRUCTURAL REPAIR MANUAL - STRUCTURAL IDENTIFICATION
SD3-60 STRUCTURAL REPAIR MANUAL z SRM 1.0.0.0FUSELAGE - STRUCTURAL IDENTIFICATION 1. Introduction This chapter indicates the location of the strcu tural members of the fuselage and shows methods for repairing
Airglas, Inc. Installation Instructions. MANUAL NO. LH MODEL LH4000 Ski Kit For Cessna 180 and 185 Aircraft.
Airglas, Inc. Installation Instructions MANUAL NO. LH4000-105 MODEL LH4000 Ski Kit For Cessna 180 and 185 Aircraft Cage Code 17564 This Page Intentionally Left Blank 2 P a g e REV LEVEL Initial Release
56 - EFFECTIVE PAGES. Beechcraft Corporation PAGE 1 SUPER KING AIR B200GT SERIES ILLUSTRATED PARTS CATALOG DATE CH-SECT-UNIT-FIG
CH-SECT-UNIT-FIG PAGE NO. DATE CH-SECT-UNIT-FIG PAGE NO. DATE 56 - CONTENTS 1 56-10-00-04 0 56-10-00-04 1 56-10-00-05 0 56-10-00-05 1 56-10-00-05 2 56-20-00-07 0 56-20-00-07 0A 56-20-00-07 1 56-20-00-07
REVISION LIST CHAPTER 24: MISCELLANEOUS SYSTEMS
REVISION LIST CHAPTER 24: The following list of revisions will allow you to update the Legacy construction manual chapter listed above. Under the Action column, R&R directs you to remove and replace the
AIRWOLF FILTER CORP Madison Rd. Middlefield, Ohio U.S.A. (440) / (440) Fax
AIRWOLF FILTER CORP. 15369 Madison Rd. Middlefield, Ohio 44062-8404 U.S.A. (440) 632-5136 / (440) 632-1685 Fax TO THE MECHANIC: This P/N AFC-K010 remote mount oil filter kit incorporates our generic STC
Aero Union Inventory Held by IMP Aerospace as of 16 October 2012
Part Number Description Lot Serial I Location UM Quantity Branch '69494R258 PACKING '177519 '7D1C10E EA 1 '748166-1/2 PACKING WITH RETAINER '495073 '7D1C03D EA 33 '800922-1 01 SEAL, WING SUFACE, ACCESS
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
X Jeep / Eagle Model 30 /181 Disconnect Front Axles for. XJ (Cherokee /Comanche) YJ /TJ (Wrangler)
Jeep / Eagle 1984-1996 Model 30 /181 Disconnect Front Axles for XJ (Cherokee /Comanche) YJ /TJ (Wrangler) 309 Exploded View 310 X510-3 Parts Listing ITEM NO. PART NUMBER DESCRIPTION 1 (3) Housing Axle
FOR REFERENCE ONLY. 310, A, B, C, D, E, F, G, H, E310H, I, J, K, L, N, P, Q Date: 06/01/05 WITH TCM O/IO-470 ENGINES
FOR REFERENCE ONLY Applicability: CESSNA 310, A, B, C, D, E, F, G, H, E310H, I, J, K, L, N, P, Q Date: 06/01/05 WITH TCM O/IO-470 ENGINES Airwolf Parts List No. AFC-W329-A Index Part Number Description
INSTRUCTION BULLETIN
INSTRUCTION BULLETIN No. 9013158 Machine: T12 Published: 08-2016 Rev. 00 NOTE: DO NOT DISCARD the Parts List from the Instruction Bulletin. Place the Parts List in the appropriate place in the machine
RV-14 QBF-02 REV 1: In Step 7 (QB), "5-9" was "5-8", and "12-13" was "11-12"
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
Hustler Mini Z Bac Vac Parts Manual
Hustler Mini Z Bac Vac Parts Manual Hustler Turf Equipment P.O. Box 7000 Hesston, Kansas 67062-2097 379263 Rev. 6/06 Table of Contents Chapter General Information.................................... Chapter
ZODIAC 601 XL. Trim the outboard corner of the front flange of the center spar 6W4-1. Corner should not touch the side of the cabin floor skin 6B10-1.
Trim the outboard corner of the front flange of the center spar 6W4-1. Corner should not touch the side of the cabin floor skin 6B10-1. Tape the side skins to the cabin floor skin (area in front of the
Mallet Nut driver Pop rivet gun Protractor level
RotorWay International Page A Rev. 2 12/99 Airframe and Landing Gear Procedures covered in this section: Drill airframe bushings; mount front and rear landing gear; install skid tubes; tap body support