SERVICE BULLETIN SB
|
|
- Charla Harrison
- 6 years ago
- Views:
Transcription
1 TITLE NAVIGATION - RADIO ALTIMETER CONVERTER UPGRADE EFFECTIVITY MODEL SERIAL NUMBERS thru The equivalent of this service bulletin has been incorporated on production airplanes and On. NOTE: If this service bulletin is to be accomplished near a Collins Repair Facility, the Radio Altimeter Converter may be taken to a Collins Repair Facility to accomplish Service Bulletin 501, Reduce Nuisance Radio Altimeter Flags. Service Bulletin 501, Reduce Nuisance Radio Altimeter Flags, will convert the Radio Altimeter Converter to a Otherwise order an exchange Radio Altimeter Converter from Cessna. REASON To correct the radio altimeter (RA) flash on the primary flight display (PFD). DESCRIPTION This service bulletin provides parts and instructions to replace the radio altimeter converter. COMPLIANCE DISCRETIONARY. This service bulletin may be accomplished at the discretion of the owner, if the RA flashes on the PFD. FLIGHT CREW OPERATIONS No Change. APPROVAL FAA approval has been obtained on technical data in this publication that affects airplane type design. This information shall be considered an amendment to the Cessna Manufacturer s Maintenance Manual and should be accomplished within the specified time requirement. Page 1 of 5 To obtain satisfactory results, procedures specified in this publication must be accomplished in accordance with accepted industry maintenance practices and prevailing government regulations. Cessna Aircraft Company is not responsible for the quality of work performed in complying with the requirements herein if the work is accomplished at other than a Cessna-owned Citation Service Center. Cessna Aircraft Company, Citation Marketing Division, P.O. Box 7706, Wichita, Kansas 67277, U.S.A , Telefax COPYRIGHT 2003
2 MANPOWER WORK PHASE MAN-HOURS Modification * MATERIAL - Cost and Availability PART NUMBER AVAILABILITY COST * * * Refer to the attached Service Bulletin Supplemental Data sheet for man-hours, material cost and availability, and warranty information. CHANGE IN WEIGHT AND BALANCE None REFERENCES Cessna Model 525 Maintenance Manual PUBLICATIONS AFFECTED Cessna Model 525 Illustrated Parts Catalog ACCOMPLISHMENT INSTRUCTIONS 1. Prepare the airplane for maintenance. A. Make sure that all switches are in the OFF/NORM position. B. Disconnect electrical power from the airplane. (1) Disconnect the airplane battery. (2) Disconnect external electrical power. C. Attach maintenance warning tags to the battery and external power receptacle that have "DO NOT CONNECT ELECTRICAL POWER - MAINTENANCE IN PROGRESS" written on them. 2. Remove the nose radome. (Refer to the Maintenance Manual, Chapter 53, Nose Radome - Maintenance Practices.) 3. (Refer to Figure 1, Sheet 1, Detail A.) Remove the Radio Altimeter Converter. (Refer to the Maintenance Manual, Chapter 34, Collins Pro Line 21 Radio Sensor System - Removal/Installation.) NOTE: If this service bulletin is to be accomplished near a Collins Repair Facility, the Radio Altimeter Converter may be taken to a Collins Repair Facility to accomplish Service Bulletin 501, Reduce Nuisance Radio Altimeter Flags. Service Bulletin 501, Reduce Nuisance Radio Altimeter Flags, will convert the Radio Altimeter Converter to a Otherwise order the Radio Altimeter Convert from Cessna. 4. (Refer to Figure 1, Sheet 1, Detail A.) Install the Radio Altimeter Converter. (Refer to the Maintenance Manual, Chapter 34, Collins Pro Line 21 Radio Sensor System - Removal/Installation.) 5. Remove the maintenance warning tags and connect external power to the airplane. Page 2
3 6. Do a test of radio altimeter. A. Set the minimum altitude to 200 feet on the pilot s PFD. B. Press the MENU SET button in the middle of the PUSH MENU ADVANCE knob until the cursor box is over the minimum altitude numbers. C. Set the minimum safe altitude to 200 feet. D. Push the R LSK 1 button on the PFD to turn on the radio altimeter. E. Cover the receiving (aft) radio altimeter antenna with a piece of aluminum. NOTE: Covering the receiving (aft) radio altimeter antenna will simulate that the airplane is above 2500 feet altitude. NOTE: The operational check will require two technicians to complete. One must observe the PFD display and the other will cover and remove the aluminum sheet from the receiving (aft) radio altimeter antenna. F. Remove the aluminum sheet from the radio altimeter antenna. G. Monitor the PFD display. H. The radio altimeter should count down from 2500 feet past the 200 feet minimum to zero feet. I. Make sure that the aural alert sounds and the visual alert appears on the PFD. 7. Remove external power from the airplane. 8. Install the nose radome. (Refer to the Maintenance Manual, Chapter 53, Nose Radome - Maintenance Practices.) 9. Record that this service bulletin has been completed. A. Complete a Maintenance Transaction Report. B. Put a copy of the completed Maintenance Transaction Report in the airplane logbook. C. Send a copy of the completed Maintenance Transaction Report to: CESCOM, PO Box 7706, Wichita, KS Page 3
4 MATERIAL INFORMATION NOTE: The parts included in this service bulletin cover installation for one airplane. NEW P/N QUAN- TITY 1 Kit, consisting of the following parts: 1 Instructions KEY WORD OLD P/N INSTRUCTIONS/ DISPOSITION NOTE: In addition to the above kit the following part may be required. Airplanes that are in close proximity to a Collins Repair Facility may take the Radio Altimeter Converter to Collins to have Service Bulletin 501, Reduce Nuisance Radio Altimeter Flags, incorporated to make the Radio Altimeter Converter. NEW P/N QUAN- TITY KEY WORD OLD P/N INSTRUCTIONS/ DISPOSITION Radio Altimeter Converter Return to the nearest Collins Repair Facility or to Cessna to exchange for upgraded units NOTE: International Owner/Operators: The existing Radio Altimeter Converter may be returned to Cessna Aircraft Company, Citation Parts Distribution, 7121 Southwest Boulevard, Wichita, Kansas 67215, USA, and exchanged for upgraded units. Due to limited availability, please expedite the return of the removed part. NOTE: Domestic Owner/Operators: The existing Radio Altimeter Converter is to be returned to Cessna Aircraft Company, Citation Parts Distribution, 7121 Southwest Boulevard, Wichita, Kansas 67215, USA, upgraded to the current mod level and returned to the owner/operator for installation. This option will require advance scheduling with Citation Parts Distribution, Telephone number (Domestic) or (International) or Telefax We estimate a turn around time of approximately 7 days. Page 4
5 Figure 1. Radio Altimeter Converter Upgrade (Sheet 1) Page 5
6
7 TITLE SUPPLEMENTAL DATA NAVIGATION - RADIO ALTIMETER CONVERTER UPGRADE EFFECTIVITY MODEL SERIAL NUMBERS thru The equivalent of this service bulletin has been incorporated on production airplanes and On. NOTE: If this service bulletin is to be accomplished near a Collins Repair Facility the Radio Altimeter Converter may be taken to a Collins Repair Facility to accomplish Service Bulletin 501, Reduce Nuisance Radio Altimeter Flags. Service Bulletin 501, Reduce Nuisance Radio Altimeter Flags, will convert the Radio Altimeter Converter to a Otherwise order an exchange Radio Altimeter Converter from Cessna. MANPOWER WORK PHASE MAN-HOURS Modification 2.0 MATERIAL - Cost and Availability PART NUMBER AVAILABILITY COST * * * Please contact Citation Parts Distribution for current cost and availability of parts listed in this service bulletin. Phone at (Domestic) or (International). Send to: citationparts@cessna.textron.com or telefax at Based on availability and lead times, parts may require advanced scheduling. In cases where the required part(s) are available as exchange, order the exchange part and, upon completion, expedite the return of the removed core to avoid return penalties. Contact the Citation Parts Distribution Sales Desk for availability of exchange parts. Page 1 of 2 To obtain satisfactory results, procedures specified in this publication must be accomplished in accordance with accepted industry maintenance practices and prevailing government regulations. Cessna Aircraft Company is not responsible for the quality of work performed in complying with the requirements herein if the work is accomplished at other than a Cessna-owned Citation Service Center. Cessna Aircraft Company, Citation Marketing Division, P.O. Box 7706, Wichita, Kansas 67277, U.S.A , Telefax COPYRIGHT 2003
8 SUPPLEMENTAL DATA WARRANTY CREDIT PROGRAM Eligible Citations exhibiting conditions described in this service bulletin may demonstrate improved operation by incorporation of the work described herein. This bulletin is to be accomplished at the discretion of the owner. Eligible airplanes may qualify for parts and labor coverage, as described below. Eligibility: Parts Coverage: Labor Coverage: Credit Application: Expiration: Jul 31/2005 Citations identified within the serial number effectivity of this service bulletin which are within the five year warranty period on the original issue date of this bulletin. Authorized Citation Service Facilities, operators, or other maintenance facilities may submit a Citation Credit Claim Form for the parts required to accomplish this bulletin. Authorized Citation Service Facilities may submit a Citation Credit Claim Form for the labor necessary to accomplish this service bulletin. Please note Manpower Requirements for coverage guidelines. If actual labor differs from coverage guidelines, claim actual labor and detail all discrepancies. All work must be completed and the Citation Credit Claim Form submitted before the date shown below. Send the Citation Credit Claim, along with any required parts (see Material Information), to the point of purchase. Parts to be returned to Citation Parts Distribution should be forwarded to: Citation Warranty Administration 7121 Southwest Boulevard Wichita, KS USA Page 2
SERVICE LETTER SERIAL NUMBERS thru with Hydraulic Pump
TITLE HYDRAULIC POWER - ENGINE DRIVEN HYDRAULIC PUMP VERIFICATION EFFECTIVITY REASON MODEL 525B (CJ3) 525B (CJ3+) SERIAL NUMBERS -0001 thru -0415 with 9912062-8 Hydraulic Pump Installed -0451 thru -0485
More informationSERVICE BULLETIN TITLE ELECTRICAL POWER - RIGHT HAND ENGINE WIRE BUNDLE ROUTING IMPROVEMENT
TITLE ELECTRICAL POWER - RIGHT HAND ENGINE WIRE BUNDLE ROUTING IMPROVEMENT EFFECTIVITY REASON MODEL SERIAL NUMBERS 560XL (Citation XLS+) -6001 thru -6232 The equivalent of this service bulletin has been
More informationSERVICE BULLETIN TITLE EQUIPMENT/FURNISHINGS - SEAT CONTROL CABLE ROUTING IMPROVEMENT
TITLE EQUIPMENT/FURNISHINGS - SEAT CONTROL CABLE ROUTING IMPROVEMENT EFFECTIVITY REASON MODEL SERIAL NUMBERS 525B (CJ3) -0451 thru -0504 The equivalent of this service bulletin has been incorporated on
More informationSERVICE BULLETIN TITLE FLIGHT CONTROLS - RUDDER AND ELEVATOR AUTOPILOT SERVO CABLE REPLACEMENT
TITLE FLIGHT CONTROLS - RUDDER AND ELEVATOR AUTOPILOT SERVO CABLE REPLACEMENT EFFECTIVITY REASON MODEL SERIAL NUMBERS 525 (M2) -0685, -0800 thru -0870 The equivalent of this service bulletin has been incorporated
More informationSERVICE LETTER. EFFECTIVITY Model 206H airplanes that have replaced the 10880A Oil Cooler after May SERIAL NUMBERS 206H thru
MANDATORY SERVICE LETTER TITLE OIL - OIL COOLER REPLACEMENT EFFECTIVITY Model 206H airplanes that have replaced the 10880A Oil Cooler after May 2014 MODEL SERIAL NUMBERS 206H 20608001 thru 20608353 REASON
More informationSERVICE BULLETIN. SERIAL NUMBERS thru
TITLE WINGS - ACCESS PANEL INSTALLATION FOR FORWARD SPAR EFFECTIVITY REASON MODEL SERIAL NUMBERS 425 425-0001 thru 425-0236 Customers have requested an access panel to gain easy access to the forward spar
More informationSERVICE BULLETIN REVISION
Revision 3 REVISION TRANSMITTAL SHEET This sheet transmits Revision 3 to, which: A. Removes the 453-5000-999 ELT from the kits and makes it a stand alone part. B. Changes part numbers within the kits.
More informationSERVICE BULLETIN. SERIAL NUMBERS thru A0001 thru 402A B0001 thru 401B thru
TITLE WINGS - ACCESS PANEL INSTALLATION FOR FORWARD SPAR EFFECTIVITY REASON MODEL SERIAL NUMBERS 401 401-0001 thru 401-0322 401A 401B 401A0001 thru 401A0132 401B0001 thru 401B0221 402 402-0001 thru 402-0322
More informationSERVICE LETTER. EFFECTIVITY The Model T206H airplanes were delivered from Textron Aviation with a suspect 10865B Oil Cooler.
MANDATORY SERVICE LETTER TITLE OIL - OIL COOLER REPLACEMENT EFFECTIVITY The Model T206H airplanes were delivered from Textron Aviation with a suspect 10865B Oil Cooler. MODEL SERIAL NUMBERS T206H T20609001
More informationMandatory: shall be accomplished at the next scheduled 100 hour or annual/12 month type inspection, not to exceed 12 months, whichever occurs first.
Single Engine Service Bulletin February 26, 2007 TITLE WING STRUT TO FUSELAGE CUFF MODIFICATION EFFECTIVITY Model Serial Numbers 206H 20608001 thru 20608289 T206H T20608001 thru T20608734 REASON It has
More informationSERVICE BULLETIN REVISION
Revision 2 REVISION TRANSMITTAL SHEET This sheet transmits Revision 2 to. A. Revised Figure 2, View B-B to show the dimensions to locate the cutout for the Mark V EGPWS test switch. B. Removed the note
More informationSERVICE BULLETIN REVISION TRANSMITTAL
REVISION TRANSMITTAL TO: Cessna Distributors, Multi-Engine Authorized Service Facilities, and CPC's SUBJECT: Multi-Engine Service Bulletin Revision 1: Control Column Internal Glide Attach Screw Installation
More informationSERVICE BULLETIN REVISION
Revision 1 REVISION TRANSMITTAL SHEET This sheet transmits Revision 1 to. A. Removed the 4890307-2 Carpet from the -2 Kit and added the requirement to order it separately based on airplane color scheme.
More informationSERVICE BULLETIN TITLE NAVIGATION - CI COMM/GPS/XM ANTENNA REPLACEMENT (NON-WAAS ONLY)
TITLE NAVIGATION - CI2480-400 COMM/GPS/XM ANTENNA REPLACEMENT (NON-WAAS ONLY) EFFECTIVITY REASON The airplanes that follow equipped with the Garmin G1000 Nav III System: MODEL SERIAL NUMBERS 172R 17281241
More informationTo give parts and instructions to replace the wing root canted rib upper cap with a new strengthened replacement cap.
Conquest SERVICE KIT TITLE CANTED RIB CAP MODIFICATION EFFECTIVITY MODEL SERIAL NUMBERS 441 441-0001 thru 441-0362 441 698 DESCRIPTION To give parts and instructions to replace the wing root canted rib
More informationRADAR ALTIMETER CABLES, REPLACEMENT OF. HELICOPTERS AFFECTED: Serial numbers through
TECHNICAL BULLETIN 42-7-24 23 October 207 MODEL AFFECTED: SUBJECT: 42EP RADAR ALTIMETER CABLES, REPLACEMENT OF. HELICOPTERS AFFECTED: Serial numbers 37002 through 3703. [Serial number 3704 and subsequent
More informationSERVICE KIT. March 22, 2011 Original Issue: January 22, 2001 Page 1 of 7
Single Engine SERVICE KIT TITLE RUDDER STOP MODIFICATION - SHEET METAL BULKHEAD EFFECTIVITY NOTE: Some airplanes in this serial range may have a forged bulkhead installed after leaving the factory. Service
More informationSUPPLEMENT REVISION CESSNA MODEL 182T
SUPPLEMENT REVISION CESSNA MODEL 182T NAV III AVIONICS OPTION - Serials 18281228 and 18281318 thru 18281868 and 18281870 thru 18281875 PILOTS OPERATING HANDBOOK AND AIRPLANE FLIGHT MANUAL REVISION 1 1
More informationSERVICE BULLETIN REVISION
Revision 1 REVISION TRANSMITTAL SHEET This sheet transmits Revision 1 to. A. Changed the drawing number in the REFERENCES table from C190629 to CI90629. B. Changed the drawing number in the REFERENCES
More informationService Bulletin. Fuel Systems. Bulletin No.: PRS-103. Date: 05/12/98. SUBJECT: RSA-10 Fuel Diaphragm Assembly, Part Number
3220 100TH ST. SW BLDG E EVERETT, WASHINGTON 98204 FAA-PMA FACILITY #PQ111NM Service Bulletin Fuel Systems Bulletin No.: PRS-103 SUBJECT: RSA-10 Fuel Diaphragm Assembly, Part Number 2541803. A. EFFECTIVITY:
More informationSERVICE BULLETIN. NO.: 0713 Revision D. All Garmin Aviation Service Centers and Aircraft OEM Service Centers DATE: 13 June 2007
SERVICE BULLETIN NO.: 0713 TO: All Garmin Aviation Service Centers and Aircraft OEM Service Centers DATE: 13 June 2007 SUBJECT: GSM 85 Inspection Procedure REVISION D: corrects LRU Part Numbers listed
More informationDEPARTMENT OF TRANSPORTATION
DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [61 FR 625 No. 6; 01/09/96][SN] [Docket No. 94-ANE-63; Amendment 39-9458; AD 95-03-10] Textron Lycoming AD 95-03-10 Amendment
More informationSERVICE BULLETIN TRANSMITTAL SHEET HC-SB Propeller - Blade Seal Replacement
TRANSMITTAL SHEET January 08, 2019 This page transmits a revision to Service Bulletin. Original Issue, dated Revision 1, dated Jan 08/19 Propeller assemblies that have previously complied with the terminating
More informationSERVICE BULLETIN N F
SERVICE BULLETIN N F406-104 MANUFACTURER REFERENCE: N F406-104 N ATA: 27 Date: TITLE: Inspection of rudder control pedal torque tube EFFECTIVITY Model Serial Number F406 0001 to 0098 PURPOSE A pilot rudder
More informationField Hub Installation Guide. P/N Rev. C 05/15
Field Hub Installation Guide P/N016-0171-380 Rev. C 05/15 E21714 Copyright 2015 Disclaimer While every effort has been made to ensure the accuracy of this document, Raven Industries assumes no responsibility
More informationAirworthiness Directive
Airworthiness Directive Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [61 FR 29271 NO. 112 06/10/96] [Docket No. 93-ANE-48;
More informationSERVICE BULLETIN TRANSMITTAL SHEET HC-SB De-ice - Wire Harness Replacement
TRANSMITTAL SHEET May 18, 2016 This page transmits a revision to Service Bulletin. Original Issue, dated Revision 1, dated Apr 18/16 Revision 2, dated May 18/16 Propeller assemblies that have previously
More informationP/N CABLE ASSEMBLY, ONE TIME INSPECTION FOR DEFECTIVE BODY, P/N PART I (Inspection): Within the next 25 flight hours
ALERT SERVICE BULLETIN 204B-12-68 10 October 2012 MODEL AFFECTED: SUBJECT: HELICOPTERS AFFECTED: 204B P/N 205-001-720-001 CABLE ASSEMBLY, ONE TIME INSPECTION FOR DEFECTIVE BODY, P/N 205-001-742-001 ALL
More informationInstructions for Continued Airworthiness Supplement
CESSNA AIRCRAFT COMPANY AIRCRAFT DIVISION WICHITA, KANSAS 67277 Instructions for Continued Airworthiness Supplement MODEL NO: 510 REPORT NO: ICA-510-34-00001 REPORT: GA36 & GA37 GPS ANTENNAS REPORT DATE:
More informationP.O. BOX 3090 ALBANY, GEORGIA PHONE 229/ FAX 229/ NIGHT LIGHTING SYSTEM AND VOLTAGE REGULATOR CIRCUIT INTERACTION
Rockwell service letter No. SL-AG-66 International P.O. BOX 3090 ALBANY, GEORGIA 31706-3090 PHONE 229/883-1440 FAX 229/439-9790 Service Letter No. SL-AG-66 NIGHT LIGHTING SYSTEM AND VOLTAGE REGULATOR CIRCUIT
More informationNomad CONTROL SYSTEM IMPROVED PULLEY MOUNTING AT STATION (MOD N137) Page No Rev No
CONTROL SYSTEM IMPROVED PULLEY MOUNTING AT STATION 67.95 (MOD N137) 1. PLANNING INFORMATION A. Effectivity (1) Aircraft Affected All Nomad N22 Series and N24 Series aircraft whose log books do not already
More informationSERVICE BULLETIN HC-SB De-ice - Wire Harness Replacement
1. Planning Information A. Effectivity (1) Hartzell Propeller Inc. lightweight turbine propellers models listed below that have any of the affected de-ice wire harnesses listed in section 1.A.(1)(a) installed
More informationSD3-60 AIRCRAFT MAINTENANCE MANUAL
AMM 46.0.0.0RADAR ALTIMETER SYSTEM - DESCRIPTION & OPERATION 1. Description A. General Refer to Figure 1. The Honeywell radar altimeter system is installed to indicate heights between 0 and 2500 ft above
More informationSERVICE BULLETIN. No. SB-AG-45 Rev. B JUNE 1, 2007 FIN SPAR & ATTACH FITTINGS INSPECTION AND UPGRADE IMPORTANT:
THRUSH AIRCRAFT, INC. P.O. Box 3149 300 Old Pretoria Rd. Albany, GA 31706-3149 Product Support 229-883-1440 ext. 341 FAX 229-436-4856 jbays@thrushaircraft.com SERVICE BULLETIN No. SB-AG-45 Rev. B JUNE
More informationSERVICE BULLETIN TRANSMITTAL SHEET HC-SB De-ice - Wire Harness Replacement
TRANSMITTAL SHEET April 27, 2017 This page transmits a revision to Service Bulletin. Original Issue, dated Revision 1, dated Apr 27/17 Propeller assemblies that have previously complied with the terminating
More information400/500 Series GTS 8XX Interface. Pilot s Guide Addendum
400/500 Series GTS 8XX Interface Pilot s Guide Addendum Copyright 2010 Garmin Ltd. or its subsidiaries. All rights reserved. This manual reflects the operation of Software version 5.03 or later for 4XX
More informationSTC GROUP LLC 480 RUDDIMAN DRIVE MUSKEGON, MICHIGAN REPORT NO: REV - TRIO AUTO PILOT INSTALLATION INSTRUCTIONS CESSNA MODEL 182
STC GROUP LLC 480 RUDDIMAN DRIVE MUSKEGON, MICHIGAN 49445 REPORT NO: 1006003 REV - TRIO AUTO PILOT INSTALLATION INSTRUCTIONS CESSNA MODEL 182 DATE: Original Issue 10 July, 2017 WRITTEN BY: Paul Odum APPROVED
More informationC I R R U S EMERGENCY DESCRIPTION A. Emergency Locator Transmitter (ELT)
EMERGENCY 1. DESCRIPTION A. Emergency Locator Transmitter (ELT) This airplane is equipped with a self-contained ELT. The ELT transmitter is installed immediately behind the aft cabin bulkhead. The ELT
More information*MANDATORY SERVICE BULLETIN*
NUMBER: SB-004 DATE: 1/26/2009 SUBJECT: ELECTRICAL; Potentiometer Replacement KODIAK MANDATORY SERVICE BULLETIN SUMMARY RECURRENT REQUIREMENTS No recurrent requirements associated with this Mandatory Service
More informationRadio Control Installation and Operating Instructions System 4
Radio Control Installation and Operating Instructions System 4 P.O. Box 403, One Cedar Parkway, Jackson, WI 53037 Phone: 800-628-1909 Fax: 262-677-2058 Revision: April 19, 2012 Contents Introduction 3
More informationWILLIAM P WITZIG Date: :55:37-04'00'
FAA Approved Airplane Flight Manual Supplement For Airplanes listed in AML with Avidyne AXP340 Transponder p/n 200-00247-XXX or Avidyne AXP322 Transponder p/n 200-00269-XXX in Make and Model Airplane Registration
More informationCIRRUS SR22 SB 2X R3. Service Bulletin. Issued: Revised: October 13, 2009 May 18, 2010
CIRRUS SR22 Service Bulletin Number: Issued: Revised: October 13, 2009 SNS SUBJECT: 30-10 ICE PROTECTION - AIRFOIL - Porous Panel Vent Inspection 1. COMPLIANCE Recommended: Accomplish this Service Bulletin
More informationKMD 550/850. Traffic Avoidance Function (TCAS/TAS/TIS) Pilot s Guide Addendum. Multi-Function Display. For Software Version 01/13 or later
N B KMD 550/850 Multi-Function Display Traffic Avoidance Function (TCAS/TAS/TIS) Pilot s Guide Addendum For Software Version 01/13 or later Revision 3 Jun/2004 006-18238-0000 The information contained
More informationIndependent Position Determining
GENERAL Independent Position Determining 34-40: INDEPENDENT POSITION DETERMINING 1. General This section covers that portion of the system which provides information to determine position from sources
More informationALERT SERVICE BULLETIN
January 28, 2010 TITLE INSPECTION OF MODEL 1A103/TCM PROPELLER HUB FOR CRACKING AND REWORK PROCEDURES TO: FAA-Approved Propeller Repair Stations, Cessna Aircraft Company, Aircraft Owners, and Operators
More informationRADIO SYSTEM DESCRIPTION The radio system consists of the following equipment:
COMMUNICATION SYSTEM RADIO SYSTEM DESCRIPTION The radio system consists of the following equipment: Radio tuning function located in MFD s Dual CDU s (for tuning - shared with FMS) Two VHF communication
More informationKGX 150/130 ADS -B Certified Transceivers & Receivers
BendixKing By Honeywell 9201 -B San Mateo Blvd. NE Albuquerque, NM 87113 U.S.A. CAGE: 6PC31 Telephone: 1-505 -903-6148 Telephone: 1-855 -250-7027 (Toll Free in U.S.A.) Web site: http://www.bendixking.com
More informationHARTZELL PROPELLER INC. SERVICE BULLETIN
1. Planning Information A. Effectivity Hartzell propeller models HC-B(3,4,5)( )(P,N)-( )( ) that were installed on an aircraft, or that have had B-3339 mounting bolts replaced, between January 30, 2001
More informationAEROPRAKT SAFETY ALERT. No. SA A32-03 REPLACEMENT OF DOOR LATCHES
Aeroprakt Ltd AEROPRAKT SAFETY ALERT No. SA A32-03 REPLACEMENT OF DOOR LATCHES Repeating symbols: Please, pay attention to the following symbols throughout this document marking important information.
More informationService Bulletin No: Ref No: 136 Modification No: INSPECTION ATA Chapter: 57
PILATUS AIRCRAFT LTD. STANS, SWITZERLAND Service Bulletin No: 57-015 Ref No: 136 Modification No: INSPECTION ATA Chapter: 57 WING - AILERON INSTALLATION INSPECTION OF THE AILERON OUTBOARD-BEARING SUPPORT
More informationUniversal ADS-B Receiver. Equipment Supplement
Universal ADS-B Receiver Equipment Supplement Revision A 17-Mar-2016 Revision Notes Revision Date Change Description A 05/03/17 Initial Release ADS-B Receiver Supplement 2 Table of Contents Section 1:
More informationGTS 8XX Traffic System Instructions for Continued Airworthiness as installed in
GTS 8XX Traffic System Instructions for Continued Airworthiness as installed in (Make and Model Airplane) Reg. No. S/N Dwg. Number: 190-00993-01 Rev. 1 Garmin Ltd. Or its subsidiaries c/o Garmin International,
More informationCopyright Information
PILOT S GUIDE Copyright Information Stratus 3 Pilot s Guide, 2018 Appareo Systems, LLC. All Rights Reserved. All content within is copyrighted by Appareo Systems, LLC and may not be reprinted without permission.
More informationSERVICE BULLETIN EQUIPMENT / FURNISHING PASSENGER COMPARTMENT INSPECTION / REPLACEMENT OF EJECTOR BASE SERVICE BULLETIN NUMBER ISSUE 10
EQUIPMENT / FURNISHING PASSENGER COMPARTMENT INSPECTION / REPLACEMENT OF EJECTOR BASE SERVICE BULLETIN NUMBER ISSUE 10 ISSUED BY: AMSAFE INC. 1043 N. 47 th AVENUE PHOENIX, AZ USA 85043 TEL: (602) 850 2850
More informationINSTALLATION AND MAINTENANCE MANUAL FOR P/N: D564-XXX-001 L864 RED MEDIUM INTENSITY BEACON
INSTALLATION AND MAINTENANCE MANUAL FOR P/N: D564-XXX-001 L864 RED MEDIUM INTENSITY BEACON Page 1 of 8 Contents Page List of Figures and Tables... 2 Reference Drawings... 2 Section 1: Overview... 3 Section
More informationEXP5000. Software Release 8. Primary Flight Display Pilot s Guide Addendum Rev: 02
EXP5000 Primary Flight Display Pilot s Guide Addendum Software Release 8 600-00259-000 Rev: 02 THIS PAGE INTENTIONALLY LEFT BLANK Document Revision History Date Revision Description April 27, 2010 00 Initial
More informationPARAVION TECHNOLOGY, INC AIRWAY AVENUE FT. COLLINS, COLORADO
PARAVION TECHNOLOGY, INC. 2001 AIRWAY AVENUE FT. COLLINS, COLORADO 80524 PR C208WS 900M For Workstation/Equipment Cabinet Cessna Model 208, 208B Airplanes Page ii of v REVISION HISTORY Revision Date Detail
More informationSeychelles Civil Aviation Authority SAFETY NOTICE. Coding and registration of Seychelles 406 Mhz Emergency Locator Transmitters (ELTs)
Seychelles Civil Aviation Authority Safety Notice SAFETY NOTICE Number: Issued: 25 April 2018 Coding and registration of Seychelles 406 Mhz Emergency Locator Transmitters (ELTs) This Safety Notice contains
More informationDEPARTMENT OF TRANSPORTATION
DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 Textron Lycoming AD 92-12-05 Amendment 39-8265 Effective July 10, 1992 Recurring: No [Docket No. 91-ANE-48; Amendment 39-8265;
More informationFlight Data Systems Pathfinder Remote ADS-B Receiver Equipment Supplement
Flight Data Systems Pathfinder Remote ADS-B Receiver Equipment Supplement Revision A1 10-Nov-2014 Revision Notes Revision Date Change Description A 9-Jul-2014 Initial Release A1 10-Nov-2014 Section 2.1-
More informationKeychain Radio Remote Control System
Innovation in Mobility Keychain Radio Remote Control System Operator Manual 04/23/02 95-2002 RICON CORPORATION All Rights Reserved U.S. and foreign patents pending Printed in the United States of America
More informationAIRWORTHINESS DIRECTIVE
EASA AIRWORTHINESS DIRECTIVE AD No.: 2013-0288 Date: 06 December 2013 Note: This Airworthiness Directive (AD) is issued by EASA, acting in accordance with Regulation (EC) No 216/2008 on behalf of the European
More informationGTX 320A. Mode A/C Transponder. pilot s guide
GTX 320A Mode A/C Transponder pilot s guide 2000 GARMIN Corporation GARMIN International, Inc. 1200 East 151 st Street, Olathe, Kansas 66062, U.S.A. Tel. 913/397.8200 or 800/800.1020 Fax 913/397.8282 GARMIN
More informationProfessional UHF Rechargeable Wireless Microphone System POWER ON/OFF BATTERY CHARGE. Green Light (Full) Better Music Builder DOWN VOLUME
Green Light (Full) KARAOKE Professional UHF Rechargeable Wireless Microphone System VM-93C Operating Instructions UHF Frequency 64 Selectable POWER ON/OFF CHARGE Better Music Builder VM-93C CHARGER UHF
More informationGTS 8XX Series. Pilot s Guide Traffic Advisory System
GTS 8XX Series Pilot s Guide Traffic Advisory System 2009 Garmin Ltd. or its subsidiaries. All rights reserved. Garmin International, Inc., 1200 East 151st Street, Olathe, KS 66062, U.S.A. Tel: 913/397.8200
More informationGTS 825 TAS/ADS-B OUT AND PHASE 14 SOFTWARE UPDATE ICA Supplement
AIRCRAFT DIVISION WICHITA, KANSAS 67277 GTS 825 TAS/ADS-B OUT AND PHASE 14 SOFTWARE UPDATE ICA Supplement MODEL NO: 208 SUPPLEMENT NO: ICA-208-34-00001 SUPPLEMENT DATE: 2/18/2016 Cessna Aircraft Company
More informationWalkie-Talkie. User Manual and Instruction. Getting Started
Walkie-Talkie User Manual and Instruction Getting Started Installing the AA Batteries Your radio uses 3 AA Alkaline batteries. 1. With the back of the radio facing you, lift the battery latch up to release
More informationDistribution Amplifiers 1
Distribution Amplifiers 1-30dB PUT 49-750 MHz 43 db GA POWER DOUBLED P/N: 1002705 REVERSE GA M MAX DESCRIPTION The R.L. DRAKE models DA8642, DA8632,, and DA7533, are broadband distribution amplifiers designed
More informationAP OL LO SL 60 VHF Communications Transceiver and GNSS (GPS) Navigation Receiver
SkyRentals INFO FOR VH-VMA Insert to SECTION 9 MODEL 182Q (1977) VHF Com1 & GNSS Nav Receiver AP OL LO SL 60 VHF Communications Transceiver and GNSS (GPS) Navigation Receiver VHF Com1 & GNSS Nav components
More informationMANUFACTURER S DATA SECTION ROTORCRAFT FLIGHT MANUAL SUPPLEMENT
MANUFACTURER S DATA SECTION OF ROTORCRAFT FLIGHT MANUAL SUPPLEMENT TO THE SIKORSKY S-76A ROTORCRAFT FLIGHT MANUAL Aircraft Serial Number: Aircraft Registration Number: This supplement must be attached
More informationAT01 AIRPLANE FLIGHT MANUAL
Table of Contents Supplement AVE12 1. Section 1 General AVE12 3 2. Section 2 Operating Limitations AVE12 3 3. Section 3 Emergency Procedures AVE12 3 4. Section 4 Normal Procedures AVE12 4 5. Section 5
More informationINSTALLATION AND MAINTENANCE MANUAL FOR P/N: D564-A /240VAC, 50/60 Hz, L864 RED MEDIUM INTENSITY BEACON
INSTALLATION AND MAINTENANCE MANUAL FOR P/N: D564-A13-001 120/240VAC, 50/60 Hz, L864 RED MEDIUM INTENSITY BEACON 1 of 14 Contents Page List of Figures and Tables...2 Reference Drawings...2 Section 1: Overview...3
More informationP/N 135A FAA Approved: 7/26/2005 Section 9 Initial Release Page 1 of 10
FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT FOR GARMIN GNS 430 - VHF COMM/NAV/GPS Serial No: Registration No: When installing the Garmin GNS 430 - VHF COMM/NAV/GPS in the Liberty Aerospace XL2, this
More informationSERVICE LETTER. FAA-Approved Propeller Repair Stations, Aircraft Manufacturers, Owners and Operators.
December 15, 2008 TITLE MODEL D3A34C447 PROPELLER SERVICE INFORMATION UPDATE TO: FAA-Approved Propeller Repair Stations, Aircraft Manufacturers, Owners and Operators. EFFECTIVITY Model D3A34C447 Propeller,
More information32 CHANNEL SELECTABLE CH MHZ DOWN VOLUME
KARAOKE Professional UHF Wireless Microphone System VM-92U Operating Instructions UHF Frequency 64 Selectable Better Music Builder UHF MIC WIRELESS SYSTEM VM-92U 32 CHANNEL SELECTABLE 248 13.10 CH MHZ
More informationWelcome to the World of Einstein E-Collar ET-800A Owner's Manual
Welcome to the World of Einstein E-Collar ET-800A Owner's Manual Remote Education Collar Thank you for purchasing the Einstein Remote Education Collar from E-Collar Technologies, Inc. We have made every
More informationGMINI 300PE AM/FM/Shortwave Radio OWNER S MANUAL
GMINI 300PE AM/FM/Shortwave Radio OWNER S MANUAL Grundig Radio Line By www.etoncorp.com Grundig Radio Line By DO YOU NEED HELP? Contact Us Etón Corporation 1015 Corporation Way Palo Alto, CA 94303, USA.
More informationAIS 300 Installation Instructions
Use these instructions to install the Garmin AIS 300 Automatic Identification System (AIS) Class B receiver device. Compare the contents of this package with the packing list on the box. If any pieces
More informationWelcome to or ecolar
800 802 Welcome to Thank you for purchasing the Einstein Remote Education Collar from E-Collar Technologies, Inc. We have made every attempt to provide you with the most technologically advanced product
More informationCopyrighted Material - Taylor & Francis
22 Traffic Alert and Collision Avoidance System II (TCAS II) Steve Henely Rockwell Collins 22. Introduction...22-22.2 Components...22-2 22.3 Surveillance...22-3 22. Protected Airspace...22-3 22. Collision
More informationSwiftBroadbandWi-FiAntennas ICASupplement
AIRCRAFTDIVISION WICHITA,KANSAS67277 SwiftBroadbandWi-FiAntennas ICASupplement MODELNO:750 SUPPLEMENTNO: SUPPLEMENTDATE:9/22/2014 CessnaAircraftCompany AIRCRAFTDIVISION WICHITA,KANSAS67277 REVISIONS Rev:
More informationFOUND FBA-2C1/2C2 BUSH HAWK EQUIPPED WITH SINGLE GARMIN GNS-430 # 1 VHF-AM COMM / VOR-ILS / GPS RECEIVER
FOUND SUPPLEMENT M400-S11 Transport Canada Approved Flight Manual Supplement For FOUND BUSH HAWK EQUIPPED WITH SINGLE # 1 VHF-AM COMM / VOR-ILS / GPS RECEIVER Section 1 General is Unapproved and provided
More informationGTS Traffic Systems. Pilot s Guide
GTS Traffic Systems Pilot s Guide 2014 Garmin Ltd. or its subsidiaries. All rights reserved. Garmin International, Inc., 1200 East 151st Street, Olathe, KS 66062, U.S.A. Tel: 913/397.8200 Fax: 913/397.8282
More informationCONTACT INFORMATION. Welcome to the World of Einstein E-Collars ET-1200 Owner's Manual
Contact Information CONTACT INFORMATION Welcome to the World of Einstein E-Collars ET-1200 Owner's Manual E-Collar Technologies, Inc. 2120 Forrest Park Drive Garrett, IN 46738 Toll-Free 1-855-326-5527
More informationEQUIPMENT INSTALLATION MANUAL. for the GDC62 RADIO ALTIMETER INTERFACE UNIT P/N
EQUIPMENT INSTALLATION MANUAL for the GDC62 RADIO ALTIMETER INTERFACE UNIT P/N 1102-4000-01 DAC International 6702 McNeil Drive Austin, TX 78729 Copyright 2013, DAC International. All rights reserved.
More informationDisclaimers. Important Notice
Disclaimers Disclaimers Important Notice Copyright SolarEdge Inc. All rights reserved. No part of this document may be reproduced, stored in a retrieval system, or transmitted, in any form or by any means,
More information500S Smart Antenna Installation and Operation Manual. P/N Rev. A 09/17 E29808
500S Smart Antenna Installation and Operation Manual P/N 016-0171-668 Rev. A 09/17 E29808 Copyright 2017 1 Disclaimer While every effort has been made to ensure the accuracy of this document, Raven Industries
More informationIDENTIFICATION AND RECOVERY SYSTEM FOR SUBMARINE FLEETS S-10 SUBMARINE BEACON. ORCA S10 User Manual
IDENTIFICATION AND RECOVERY SYSTEM FOR SUBMARINE FLEETS SUBMARINE BEACON S-10 ORCA S10 User Manual BriarTek, Inc. Technical Support: 703.548.7892 Email: support@briartek.com Web: www.briartek.com 2018
More informationAIRCRAFT OPERATING INSTRUCTIONS Doc. No. S2006AOIUSS17 SUPPLEMENT EMERGENCY LOCATOR TRANSMITTER MODEL AK
AIRCRAFT OPERATING INSTRUCTIONS Section 9 SUPPLEMENT EMERGENCY LOCATOR TRANSMITTER MODEL AK --- 450 AMERI --- KING CORPORATION Registration mark: Serial number: This Supplement must be contained in the
More informationHAZARD AVOIDANCE. Displaying traffic on the Navigation Map. Displaying traffic information (PFD Inset Map):
HAZARD AVOIDANCE Displaying traffic on the Navigation Map 1) Ensure that the TAS system is operating. With the Navigation Map displayed, select the MAP Softkey. 2) Select the TRAFFIC Softkey. Traffic is
More informationAIRPLANE FLIGHT MANUAL AQUILA AT01. Date of Issue A.01 Initial Issue (minor change MB-AT ) all March
0.1 LIST OF REVISIONS AND AMENDMENTS Revision Reason for Amendment/Revision Affected Pages Date of Issue A.01 Initial Issue (minor change MB-AT01-00297) all 2009 19. March 0.2 LIST OF EFFECTIVE PAGES Page
More informationInstructions for Continued
+ LORD BULLETIN NO. SM-6553 BELL 206 Instructions for Continued Airworthiness INSTRUCTIONS FOR CONTINUED AIRWORTHINESS FOR LORD P/N LORD206-310-004101 AND P/N LORD206-310-004103 INSTALLED ON BELL 206A,
More information11 Traffic-alert and Collision Avoidance System (TCAS)
11 Traffic-alert and Collision Avoidance System (TCAS) INSTRUMENTATION 11.1 Introduction In the early nineties the American FAA stated that civil aircraft flying in US airspace were equipped with a Traffic-alert
More informationFokker 50 - Automatic Flight Control System
GENERAL The Automatic Flight Control System (AFCS) controls the aircraft around the pitch, roll, and yaw axes. The system consists of: Two Flight Directors (FD). Autopilot (AP). Flight Augmentation System
More informationSD3-60 AIRCRAFT MAINTENANCE MANUAL - DESCRIPTION & OPERATION (PRE-MOD A8062) (1) Transceiver, Collins type DME40, (Part No.
AMM 53.0.0.0DME SYSTEM - DESCRIPTION & OPERATION (PRE-MOD A8062) 1. Description A. General Two identical D.M.E. systems are installed, one for each pilot. Frequency selection is made via each respective
More informationEBC-502H INSTRUCTION AND MAINTENANCE MANUAL
EBC-502H INSTRUCTION AND MAINTENANCE MANUAL EMERGENCY BEACON CORPORATION 15 RIVER STREET NEW ROCHELLE, NY 10801 PHONE (914) 235-9400 PHONE 1 800-382-0079 FAX (914) 576-7075 MADE IN THE U.S.A. September
More informationOberebenestrasse Bremgarten Switzerland Tel Fax
Oberebenestrasse 11 5620 Bremgarten Switzerland Tel. +41 56 640 06 70 Fax. +41 56 640 06 74 Single Phase - Battery Operated Automatic Transformer Turns Ratiometer Test System Model: TR-1 Model: TR-1P Instruction
More informationAmendments to the Wichita-Sedgwick County of the Unified Zoning Code Required by K.S.A & FCC Declaratory Ruling
Amendments to the Wichita-Sedgwick County of the Unified Zoning Code Required by K.S.A. 66-2019 & FCC Declaratory Ruling Section II-B.14.p. and Section II-B.14.q. p. Wireless Communication means wireless
More informationTable of Contents. Introduction 3. Pictorials of the 40 and 50 Systems 4. List of Applicable Acronyms 6
Table of Contents Introduction 3 Pictorials of the 40 and 50 Systems 4 List of Applicable Acronyms 6 System 40 Modes of Operation 7 System 40 Functional Preflight Procedures 10 System 40 In Flight Procedures
More informationInstallation Instructions Dual battery Tray Wrangler & Unlimited Part # 2799
Please read instructions entirely before installing this product. Wiring is not included with this part and should be done by an experienced technician. This part is designed to work with Optima Class
More information