Single Engine Service Bulletin SEB07-5 Revision 1, Pilot and Copilot Secondary Seat Stop Installation.
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1 Revision Transmittal December 17, 2007 TO: Cessna Distributors and Single Engine Service Stations and CPC's SUBJECT: Single Engine Service Bulletin, Pilot and Copilot Secondary Seat Stop Installation. REASON FOR REVISION To remove all 188 model airplanes from the Effectivity section. To revise the time of compliance from 200 hours of operation or 12 months to 400 hours of operation or 24 months, whichever occurs first. To revise the copilot seat secondary stop installation compliance from mandatory to recommended. To extend the credit expiration dates. Miscellaneous changes as necessary. REQUIRED ACTION Please replace any copy of SEB07-5 with the attached copy of which is printed in its entirety. NOTE: Compliance with Revision 1 is not required if in compliance with the Original Issue. LOG OF EFFECTIVE PAGES Page No. Date Page No. Date 1 December 17, December 17, December 17, December 17, December 17, December 17, December 17, December 17, December 17, December 17, December 17, December 17, December 17, December 17, December 17, December 17, December 17, December 17, 2007 * * * * * * * Page 1 of 1 To obtain satisfactory results, procedures specified in this publication must be accomplished in accordance with accepted methods and prevailing government regulations. Cessna Aircraft Company cannot be responsible for the quality of work performed in accomplishing the requirements of this publication. Cessna Aircraft Company, Product Support, P.O. Box 7706, Wichita, Kansas 67277, U.S.A. (316) , Facsimile (316) COPYRIGHT 2007
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3 Single Engine Service Bulletin December 17, 2007 SEB07-5 Revision 1 TITLE PILOT AND COPILOT SECONDARY SEAT STOP INSTALLATION EFFECTIVITY Model Year Serial Numbers thru A 1949 thru thru A 1949 thru thru B 1952 thru thru B 1952 thru thru B 609, thru thru thru thru thru thru , 612, A thru A 622, B thru B C thru D thru E thru E F thru G thru H thru H thru H I thru J K thru Original Issue: May 14, 2007 Page 1 of 18 To obtain satisfactory results, procedures specified in this publication must be accomplished in accordance with accepted methods and prevailing government regulations. Cessna Aircraft Company cannot be responsible for the quality of work performed in accomplishing the requirements of this publication. Cessna Aircraft Company, Product Support, P.O. Box 7706, Wichita, Kansas 67277, U.S.A. (316) , Facsimile (316) COPYRIGHT 2007
4 172K thru L thru L thru M thru M thru M thru M M thru M thru M thru N thru N N thru N thru N N thru N thru N P thru P thru P thru P thru P thru P thru Q Q thru Q , , Q , , Q , , Q , , Q , , Q , , Q , , Q , , Q , , F172H 1968 F thru F thru thru A, 626, A thru A B thru Page 2 December 17, 2007
5 175C thru P172D 1963 P thru P R172E (T41) 1967 thru 1968 R thru R R172F (T41) 1969 R thru R R172G (T41) 1969 thru 1970 R thru R R172H (T41) 1971 R thru R R172H (T41) 1972 R thru R R172H (T41) 1973 thru 1976 R thru R R172J 1974 P R172K 1977 R thru R R172K 1978 R thru R R172K 1979 R thru R R172K 680 R172K 1980 R thru R R172K 1981 R thru R RG RG0001 thru 172RG RG RG0571 thru172rg RG RG RG0891 thru 172RG RG RG1100 thru 172RG RG RG1145 thru 172RG RG RG1178 thru 172RG thru A thru B thru B thru B thru B B thru B thru B thru B thru B B thru B thru B thru RG RG0001 thru 177RG RG RG0213 thru 177RG RG RG0283 thru 177RG0418 December 17, 2007 Page 3
6 177RG RG0420 thru 177RG RG RG0433 thru 177RG RG RG0593 thru 177RG RG RG0788 thru 177RG RG RG1052 thru 177RG RG RG1267 thru 177RG RG 177RG thru thru , A thru A 1957 thru thru B thru C thru C D thru E thru F thru G thru H 1965 thru thru H J 1973 thru thru J 1973 thru thru K thru K thru K thru K K thru K thru thru A thru A thru A thru B thru B thru B C thru C D thru D E thru Page 4 December 17, 2007
7 182F thru G thru H thru H J thru A182J 1966 A thru A A182K 1967 A thru A A182L 1968 A thru A A182N 1972 thru 1976 A thru A K thru K thru K L thru M M thru M N thru N thru P thru P thru P thru P thru P thru P P thru Q thru Q thru Q Q thru Q Q thru R/T thru R/T R/T thru R/T thru R/T thru R/T thru R thru R R R thru R R182/TR R thru R December 17, 2007 Page 5
8 R182/TR182 R R182/TR R R182/TR R thru R R182/TR R thru R R182/TR R thru R R182/TR R thru R R182/TR R thru R R182/TR R thru R R182/TR182 R R182/TR R thru R thru A thru B thru C thru D thru E thru A185E thru A185E thru A185E thru A185E thru A185E 1970/ thru A185E thru A185F thru A185F thru A185F 652 A185F thru A185F thru A185F thru A185F thru A185F thru A185F thru A185F A185F thru A185F thru A185F thru A185F thru A185F thru A185F thru thru thru thru thru Page 6 December 17, 2007
9 thru thru thru thru A 1948 thru thru A 1948 thru thru B 1948 thru thru B 1948 thru thru (205) thru (205) 641, (205A) thru thru U U thru U U206A 1966 U thru U TU206A 1966 U thru U U206B/TU206B 1967 U thru U U206C/TU206C 1968 U thru U U206D/TU206D 1969 U thru U U206D/TU206D 1970 U thru U U206E/TU206E 1971 U thru U U206F/TU206F 1972 U thru U U206F/TU206F 1973 U thru U U206F/TU206F 1974 U thru U U206F/TU206F 1975 U thru U U206F/TU206F 1975 U thru U U206F/TU206F 1976 U thru U U206G/TU206G 1977 U thru U U206G/TU206G 676 U206G/TU206G 1978 U thru U U206G/TU206G 1979 U thru U U206G/TU206G U U206G/TU206G 1980 U thru U U206G/TU206G 1981 U thru U U206G/TU206G 1982 U thru U U206G/TU206G 1983 U thru U U206G/TU206G 1984 U thru U U206G/TU206G 1985 U thru U U206G/TU206G 1986 U thru U P P thru P P206A 1966 P thru P TP206A 1966 P thru P P206B/TP206B 1967 P thru P P206C/TP206C 1968 P thru P December 17, 2007 Page 7
10 P206D/TP206D 1969 P thru P P206E/TP206E 1970 P thru P P206E/TP206E P /T thru /T thru /T thru /T thru /T thru /T thru /T thru /T thru A/T207A thru A/T207A thru A/T207A thru A/T207A thru A/T207A thru A/T207A thru A/T207A thru A/T207A thru thru A thru A B thru C thru C thru D thru E thru F thru G thru H thru J thru K/T210K thru K/T210K thru L/T210L thru L/T210L thru L/T210L thru L/T210L thru L/T210L thru L/T210L thru M/T210M thru Page 8 December 17, 2007
11 210M/T210M thru M/T210M N/T210N thru N/T210N thru N/T210N thru N/T210N thru N/T210N thru N/T210N thru R/T210R thru R/T210R thru T210F 1966 T thru T T210G 1967 T thru T T210H 1968 T thru T T210J 1969 T thru T T210J P210N 1978 P thru P P210N 1979 P thru P P210N 1980 P thru P P210N 1981 P thru P P210N 1982 P thru P P210N 1983 P thru P P210R 1985 P thru P P210R 1986 P thru P A182J 1966 A thru A A182K 1967 A thru A A182L 1968 A thru A A182N 1972 A thru A A182N 1974 A thru A A182N 1976 A thru A FP FP thru FP F172D 1963 F thru F F172E 1964 F thru F F172F 1965 F thru F F172G 1966 F thru F F172H 1967 F thru F F172H 1967 F thru F F172H 1967 F thru F F172H 1968 F thru F F172H 1968 F F172H 1968 F thru F F172H 1969 F thru F December 17, 2007 Page 9
12 F172H 1970 F thru F F172K 1971 F thru F F172L 1972 F thru F F172M 1973 F thru F F172M 1974 F thru F F172M 1975 F thru F F172M 1976 F thru F F172N 1977 F thru F F172N 1978 F thru F F172N 1979 F thru F F172N 1980 F thru F F172P 1981 F thru F F172P 1982 F thru F F172P 1983 F thru F F172P 1984 F thru F F172P 1985 F thru F F172P 1986 F thru F FR172E 1968 FR thru FR FR172F 1969 FR thru FR FR172G 1970 FR thru FR FR172H 1971 FR thru FR FR172H 1972 FR thru FR FR172J 1973 FR thru FR FR172J 1974 FR thru FR FR172J 1975 FR thru FR FR172J 1976 FR thru FR FR172K 1977 FR thru FR FR172K 1978 FR thru FR FR172K 1979 FR thru FR FR172K 1980 FR thru FR FR172K 1981 FR thru FR F177RG 1971 F177RG0001 thru F177RG0042 F177RG 1972 F177RG0043 thru F177RG0062 F177RG 1973 F177RG0063 thru F177RG0092 F177RG 1974 F177RG0093 thru F177RG0122 F177RG 1975 F177RG0123 thru F177RG0138 F177RG 1976 F177RG0139 thru F177RG0160 F177RG 1977 F177RG0161 thru F177RG0177 F182P 1976 F thru F F182Q 1977 F thru F F182Q 1978 F thru F Page 10 December 17, 2007
13 F182Q 1979 F thru F F182Q 1980 F thru F FR FR thru FR FR FR thru FR FR FR thru FR PURPOSE To provide a modification for installing a new design secondary seat stop for the pilot and copilot seats. The secondary seat stop is designed to assist in providing an additional margin of safety by limiting the aft travel of the seat in the event the primary latch pin is not properly engaged in the seat rail/track. In certain instances, seat slippage could result in some pilots not being able to reach all the controls and/or subsequently losing control of the airplane. COMPLIANCE Mandatory: Pilot seat secondary stop installation shall be accomplished within the next 400 hours of operation or 24 months, whichever occurs first. Recommended: Copilot seat secondary stop installation should be accomplished within the next 400 hours of operation or 24 months, whichever occurs first. NOTE: This Service Bulletin supersedes Service Bulletin SEB89-2: Pilot Seat Secondary Stop Installation (all revisions). Compliance with Revision 1 is not required if in compliance with the Original Issue. APPROVAL FAA approval has been obtained on technical data in this publication that affects airplane type design. December 17, 2007 Page 11
14 MAN-HOURS The man-hours listed below are based on the work being accomplished during a scheduled 100 hour/annual type inspection. SK195-11: Pilot Secondary Seat Stop Installation 6.7 man-hours per airplane SK195-12: Copilot Secondary Seat Stop Installation Approximately 6.2 man-hours per airplane SK A: Pilot Secondary Seat Stop Installation Installation "A": 3.5 man-hours per airplane Installation "B": 3.4 man-hours per airplane Installation "C": 1.5 man-hours per airplane Installation "D": 2.9 man-hours per airplane Installation "E": 2.2 man-hours per airplane Installation "F": 2.0 man-hours per airplane Installation "G": 2.4 man-hours per airplane Installation "H": 2.4 man-hours per airplane Installation "J": 5.4 man-hours per airplane Installation "K": 3.6 man-hours per airplane SK : Copilot Secondary Seat Stop Installation Installation "A": Approximately 3.0 man-hours per airplane Installation "B": Approximately 2.9 man-hours per airplane Installation "C": Approximately 1.0 man-hour per airplane Installation "D": Approximately 2.4 man-hours per airplane Installation "E": Approximately 1.7 man-hours per airplane Installation "F": Approximately 1.5 man-hours per airplane Installation "G": Approximately 1.9 man-hours per airplane Installation "H": Approximately 1.9 man-hours per airplane Installation "J": Approximately 4.9 man-hours per airplane Installation "K": Approximately 3.1 man-hours per airplane Page 12 December 17, 2007
15 MATERIAL The parts below are available from Cessna Parts Distribution through an appropriate Cessna Service Station for the suggested list price shown. NOTE: The airplane serial number must be provided when ordering the seat stop service kits. Part Number Description Qty/Airplane Price SK Pilot Secondary Seat Stop Installation Kit (Models 190/195) 1 $ (N) ea SK SK A SK U000787S Copilot Secondary Seat Stop Installation Kit (Models 190/195) Pilot Secondary Seat Stop Installation Kit (Models 170-P210 except Models 190/195) Copilot Secondary Seat Stop Installation Kit (Models 170-P210 except Models 190/195) EC1300LP Adhesive (1 Pint) 1 $ (N) ea 1 $ (N) ea 1 $ (N) ea (as required) $ (VR) ea ALL PRICES SUBJECT TO CHANGE WITHOUT NOTICE ACCOMPLISHMENT INSTRUCTIONS Service Kit installation instructions are included in the following Service Kits when the kits are shipped from Cessna Parts Distribution. SK and SK A: Pilot Secondary Seat Stop Installation; SK and SK : Copilot Secondary Seat Stop Installation. For your convenience the typical installation of the secondary seat stop installation configurations are shown in Figure 1. NOTE: This information shall be considered an amendment to the Cessna Manufacturer's Service/Maintenance Manual or Instructions for continued airworthiness and must be accomplished for ongoing airworthiness compliance as required per 14 CFR Part December 17, 2007 Page 13
16 CREDIT Applicable Service Kit parts credit and applicable labor allowance credit, as listed in the Man-Hours section of this Service Bulletin, will be provided per airplane to install Service Kits SK and SK A: Pilot Secondary Seat Stop Installation. When applicable, freight will be credited at the most economical method unless pre-approved by Cessna. For pre-approval contact Cessna Parts Distribution Warranty Administration at Telephone: , Fax: or To receive credit, the work must be completed and a Warranty Claim submitted by a Cessna Single Engine Service Station within 30 calendar days of Service Bulletin compliance before the credit expiration dates shown below. NOTE: A copy of the logbook entries and applicable FAA Form , Airworthiness Approval Tag that was shipped with the Service Kit will be required that shows installation of the applicable Service Kit and shall be included with the Warranty Claim. Domestic... December17,2009 International... December17,2009 OWNER NOTIFICATION A. On May 14, 2007 the following Owner Advisory message was sent to applicable owners of record in SEB07-5A. Dear Cessna Owner: This Owner Advisory is to inform you that SEB07-5: Pilot and Copilot Secondary Seat Stop Installation has been issued to announce that Service Kits are available to install a new design secondary seat stop for the pilot and copilot seats. The secondary seat stop is designed to assist in providing an additional margin of safety by limiting the aft travel of the seat in the event the primary latch pin is not properly engaged in the seat rail/track. In certain instances, seat slippage could result in some pilots not being able to reach all the controls and/or subsequently losing control of the airplane. Compliance is mandatory: shall be accomplished within the next 200 hours of operation or 12 months, whichever occurs first. NOTE: This Service Bulletin supersedes Service Bulletin SEB89-2: Pilot Seat Secondary Stop Installation (all revisions). The information contained in the referenced Cessna Service Bulletin shall be considered an amendment to the Cessna Manufacturer's Service/Maintenance Manual or Instructions for continued airworthiness, and must be accomplished for ongoing airworthiness compliance in accordance with 14 CFR Part Applicable Service Kit parts credit and applicable labor allowance credit, as listed in the Man-Hours section of Service Bulletin SEB07-5, will be provided per airplane to install Service Kits SK and SK : Pilot Secondary Seat Stop Installation. To receive credit, the work must be completed and a Warranty Claim submitted by a Cessna Single Engine Service Station within 30 calendar days of Service Bulletin compliance before the credit expiration dates shown below. Domestic...May14,2009 International...May14,2009 Please contact a Cessna Single Engine Service Station for detailed information and arrange to have Cessna Service Bulletin SEB07-5 accomplished on your airplane. Page 14 December 17, 2007
17 B. On December 17, 2007 the following Owner Advisory message will be sent to applicable owners of record in SEB07-5R1A. Dear Cessna Owner: This Owner Advisory is to inform you that Service Bulletin : Pilot and Copilot Secondary Seat Stop Installation has been issued to announce that Service Kits are available to install a new design secondary seat stop for the pilot and copilot seats. The secondary seat stop is designed to assist in providing an additional margin of safety by limiting the aft travel of the seat in the event the primary latch pin is not properly engaged in the seat rail/track. In certain instances, seat slippage could result in some pilots not being able to reach all the controls and/or subsequently losing control of the airplane. Compliance is mandatory for the pilot seat: the secondary seat stop installation shall be accomplished within the next 400 hours of operation or 24 months, whichever occurs first. Compliance is recommended for the copilot seat: the secondary seat stop installation should be accomplished within the next 400 hours of operation or 24 months, whichever occurs first. NOTE: This Service Bulletin supersedes Service Bulletin SEB89-2: Pilot Seat Secondary Stop Installation (all revisions). Compliance with is not required if in compliance with the Original Issue of SEB07-5. The information contained in the referenced Cessna Service Bulletin shall be considered an amendment to the Cessna Manufacturer's Service/Maintenance Manual or Instructions for continued airworthiness, and must be accomplished for ongoing airworthiness compliance in accordance with 14 CFR Part Applicable Service Kit parts credit and applicable labor allowance credit, as listed in the Man-Hours section of Service Bulletin SEB07-5, will be provided per airplane to install Service Kits SK and SK A: Pilot Secondary Seat Stop Installation. To receive credit, the work must be completed and a Warranty Claim submitted by a Cessna Multi-engine Service Station within 30 calendar days of Service Bulletin compliance before the credit expiration dates shown below. Domestic... December17,2009 International... December17,2009 Please contact a Cessna Single Engine Service Station for detailed information and arrange to have Cessna Service Bulletin accomplished on your airplane. * * * * * * * December 17, 2007 Page 15
18 Figure 1. Identification of Secondary Seat Stop Installation Configurations (Sheet 1) Page 16 December 17, 2007
19 Figure 1. Identification of Secondary Seat Stop Installation Configurations (Sheet 2) December 17, 2007 Page 17
20 Figure 1. Identification of Secondary Seat Stop Installation Configurations (Sheet 3) Page 18 December 17, 2007
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FAA Approved Model List () S SA01899WI Amendment Log 3/15/2019 Original Description Issued: March 15, 2019 Page 2 of 8 Aermacchi S.p.A (Aermacchi S.p.A) [Siai Marchetti] Aermacchi S.p.A (Aermacchi S.p.A)
2. CANCELLATION. AC 39-7B, Airworthiness Directives, dated April 8, 1987, is canceled.
U.S. Department of Transportation Federal Aviation Administration Advisory Circular Subject: AIRWORTHINESS DIRECTIVES Date: 11/16/95 AC No: 39-7C Initiated by: AFS-340 Change: 1. PURPOSE. This advisory
SERVICE LETTER. This service letter applies to the models and serials that have 12,000 or more flight hours as follows
TITLE WINGS - FORWARD LOWER SPAR CAP INSPECTION EFFECTIVITY REASON This service letter applies to the models and serials that have 15,000 or more flight hours as follows MODEL SERIAL NUMBERS 401 401-0001
SERVICE INFORMATION LETTER Page: 1 of 2
SERVICE INFORMATION LETTER Page: 1 of 2 SERVICE INFORMATION LETTER NO. SILD42L-007 13 Sep 12 NOTE: NOTE: NOTE: Service Information Letters (SIL) are used only: 1. To distribute information from Diamond
[Docket No. FAA ; Directorate Identifier 2016-CE-021-AD; Amendment ; AD ]
![[Docket No. FAA ; Directorate Identifier 2016-CE-021-AD; Amendment ; AD ]](/thumbs/85/91862129.jpg "[Docket No. FAA ; Directorate Identifier 2016-CE-021-AD; Amendment ; AD ]")
[Federal Register Volume 81, Number 166 (Friday, August 26, 2016)] [Rules and Regulations] [Pages 58813-58816] From the Federal Register Online via the Government Publishing Office [www.gpo.gov] [FR Doc
TRANSMITTAL SHEET. Concurrent Requirement Added G450 Customer Bulletin Number 141 (aircraft that have previously incorporated ASC 016)
TRANSMITTAL SHEET This sheet transmits Revision A, dated, to Gulfstream G450 Aircraft Service Change 016, dated August 18, 2005, titled Aircraft General (ATA 00) Maximum Takeoff Gross Weight (MTOGW) Increase.
SERVICE BULLETIN MANDATORY SB Planning Information TITLE:
SERVICE BULLETIN TITLE: LANDING GEAR - NOSE LANDING GEAR FORWARD RETRACT PLUNGER ROD INSPECTION / REPLACEMENT 1. Planning Information A. Effectivity (1) Airplanes (a) Civil Model G36 Bonanza, Serials E-3979
AIRCRAFT SERVICE CHANGE
AIRCRAFT SERVICE CHANGE NUMBER 077 SUBJECT NAVIGATION (ATA 34) TCAS 7.1 INSTALLATION JUNE 12, 2012 PILOTS INFORMATION SHEET TCAS 7.1 INSTALLATION This service change upgrades TCAS 2000 or 3000SP systems
SERVICE LETTER. Conquest. WARNING: Further flight with a cracked carry through spar cap is prohibited. The carry
TITLE WINGS - FORWARD LOWER SPAR CAP INSPECTION EFFECTIVITY REASON This service letter applies to the models and serials that have 11,000 or more flight hours as follows MODEL SERIAL NUMBERS 425 425-0001
[Docket No. FAA ; Product Identifier 2018-CE-012-AD; Amendment. AGENCY: Federal Aviation Administration (FAA), DOT.
This document is scheduled to be published in the Federal Register on 04/05/2018 and available online at https://federalregister.gov/d/2018-06336, and on FDsys.gov [4910-13-P] DEPARTMENT OF TRANSPORTATION
SERVICE ADVISORY. NO.: 0608 Revision A. All Garmin Aviation Service Centers
SERVICE ADVISORY NO.: 0608 Revision A TO: All Garmin Aviation Service Centers DATE: 9 May 2006 SUBJECT: Applicability of Service Bulletins 0530 and 0532 appropriate to TERRAIN functionality of Garmin 400
[Docket No. FAA ; Product Identifier 2018-NM-075-AD; Amendment ; AD ]
![[Docket No. FAA ; Product Identifier 2018-NM-075-AD; Amendment ; AD ]](/thumbs/83/87655701.jpg "[Docket No. FAA ; Product Identifier 2018-NM-075-AD; Amendment ; AD ]")
[Federal Register Volume 83, Number 153 (Wednesday, August 8, 2018)] [Rules and Regulations] [Pages 38953-38957] From the Federal Register Online via the Government Publishing Office [www.gpo.gov] [FR
S-TEC System 55X Autopilot
TM 1083 B The New Piper Aircraft, Inc. 2926 Piper Drive Vero Beach, Florida, U.S.A. 32960 Date: January 11, 2002 (S,M) This Service Bulletin SB 1083B supersedes SB 1083A in it s entirety. Replace Service
Airworthiness Directive
Airworthiness Directive AD No.: 2018-0262 Issued: 06 December 2018 EASA AD No.: 2018-0262 Note: This Airworthiness Directive (AD) is issued by EASA, acting in accordance with Regulation (EU) 2018/1139
[Docket No. FAA ; Product Identifier 2017-NM-122-AD; Amendment ; AD ]
![[Docket No. FAA ; Product Identifier 2017-NM-122-AD; Amendment ; AD ]](/thumbs/83/87655659.jpg "[Docket No. FAA ; Product Identifier 2017-NM-122-AD; Amendment ; AD ]")
[Federal Register Volume 83, Number 154 (Thursday, August 9, 2018)] [Rules and Regulations] [Pages 39326-39331] From the Federal Register Online via the Government Publishing Office [www.gpo.gov] [FR Doc
[Docket No. FAA ; Product Identifier 2018-CE-006-AD] AGENCY: Federal Aviation Administration (FAA), Department of Transportation
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This document is scheduled to be published in the Federal Register on 05/09/2018 and available online at https://federalregister.gov/d/2018-09602, and on FDsys.gov [4910-13-P] DEPARTMENT OF TRANSPORTATION
[Docket No. FAA ; Directorate Identifier 2015-CE-018-AD] Airworthiness Directives; PIAGGIO AERO INDUSTRIES S.p.
![[Docket No. FAA ; Directorate Identifier 2015-CE-018-AD] Airworthiness Directives; PIAGGIO AERO INDUSTRIES S.p.](/thumbs/95/123560779.jpg "[Docket No. FAA ; Directorate Identifier 2015-CE-018-AD] Airworthiness Directives; PIAGGIO AERO INDUSTRIES S.p.")
This document is scheduled to be published in the Federal Register on 07/06/2015 and available online at http://federalregister.gov/a/2015-16293, and on FDsys.gov [4910-13-P] DEPARTMENT OF TRANSPORTATION
FLIGHT CONTROLS - FLAP FLEX SHAFT (CABLE) ASSEMBLY INSPECTION/ REPLACEMENT
Beech SERVICE BULLETIN TITLE: FLIGHT CONTROLS - FLAP FLEX SHAFT (CABLE) ASSEMBLY INSPECTION/ REPLACEMENT 1. Planning Information A. Effectivity (1) Airplanes (a) Civil All airplanes that have complied
[Docket No. FAA ; Directorate Identifier 2012-CE-014-AD; Amendment ; AD ]
![[Docket No. FAA ; Directorate Identifier 2012-CE-014-AD; Amendment ; AD ]](/thumbs/90/102877349.jpg "[Docket No. FAA ; Directorate Identifier 2012-CE-014-AD; Amendment ; AD ]")
[Federal Register Volume 78, Number 124 (Thursday, June 27, 2013)] [Rules and Regulations] [Pages 38552-38553] From the Federal Register Online via the Government Printing Office [www.gpo.gov] [FR Doc
Amendment Docket No. FAA ; Directorate Identifier 2010-CE-041-AD
Page 1 2011-02-02 SOCATA Amendment 9-16575 Docket No. FAA-2010-0948; Directorate Identifier 2010-CE-041-AD PREAMBLE Effective Date (a) This airworthiness directive (AD) becomes effective March 1, 2011.
SERVICE BULLETIN REVISION
Revision 2 REVISION TRANSMITTAL SHEET This sheet transmits Revision 2 to, which: A. Removes JAA and replaces it with EASA. B. Adds the EASA Approval statement. NOTE: This revision replaces the original
[Docket No. FAA ; Product Identifier 2018-CE-012-AD; Amendment ; AD ]
![[Docket No. FAA ; Product Identifier 2018-CE-012-AD; Amendment ; AD ]](/thumbs/82/86252562.jpg "[Docket No. FAA ; Product Identifier 2018-CE-012-AD; Amendment ; AD ]")
[Federal Register Volume 83, Number 66 (Thursday, April 5, 2018)] [Rules and Regulations] [Pages 14568-14574] From the Federal Register Online via the Government Publishing Office [www.gpo.gov] [FR Doc
PILATUS AIRCRAFT LTD.
Page 1 2010-17-09 PILATUS AIRCRAFT LTD. Amendment 39-16401 Docket No. FAA-2010-0583; Directorate Identifier 2010-CE-028-AD PREAMBLE Effective Date (a) This airworthiness directive (AD) becomes effective
REIMS AVIATION S.A.
Page 1 2011-07-03 REIMS AVIATION S.A. Amendment 39-16640 Docket No. FAA-2011-0058; Directorate Identifier 2010-CE-071-AD PREAMBLE Effective Date (a) This airworthiness directive (AD) becomes effective
[Docket No. FAA ; Directorate Identifier 2005-CE-25-AD; Amendment ; AD ]
![[Docket No. FAA ; Directorate Identifier 2005-CE-25-AD; Amendment ; AD ]](/thumbs/90/101225728.jpg "[Docket No. FAA ; Directorate Identifier 2005-CE-25-AD; Amendment ; AD ]")
[Federal Register: June 14, 2005 (Volume 70, Number 113)] [Rules and Regulations] [Page 34329-34334] From the Federal Register Online via GPO Access [wais.access.gpo.gov] [DOCID:fr14jn05-8] DEPARTMENT
Applicable to the following airplanes equipped with a Cessna Factory Installed Honeywell KT 76C Transponder.
Single Engine Service Bulletin February 27, 2006 TITLE HONEYWELL KT 73 MODE S TRANSPONDER INSTALLATION EFFECTIVITY Applicable to the following airplanes equipped with a Cessna Factory Installed Honeywell
HAWKER BEECHCRAFT CORPORATION MODELS B300 AND B300C (C-12W) AIRPLANES
Page 1 2011-15-05 HAWKER BEECHCRAFT CORPORATION MODELS B300 AND B300C (C-12W) AIRPLANES Amendment 39-16752 Docket No. FAA-2011-0436; Directorate Identifier 2011-CE-009-AD PREAMBLE (a) Effective Date This
[Docket No. FAA ; Product Identifier 2018-CE-006-AD; Amendment. AGENCY: Federal Aviation Administration (FAA), Department of Transportation
This document is scheduled to be published in the Federal Register on 11/05/2018 and available online at https://federalregister.gov/d/2018-24007, and on govinfo.gov [4910-13-P] DEPARTMENT OF TRANSPORTATION
SAAB AB, SAAB AEROSYSTEMS
Page 1 2012-24-06 SAAB AB, SAAB AEROSYSTEMS Amendment 39-17276 Docket No. FAA-2012-0672; Directorate Identifier 2011-NM-261-AD PREAMBLE (a) Effective Date This airworthiness directive (AD) becomes effective
[Docket No SW-25-AD; Amendment ; AD R1]
![[Docket No SW-25-AD; Amendment ; AD R1]](/thumbs/94/120860064.jpg "[Docket No SW-25-AD; Amendment ; AD R1]")
[Federal Register: July 6, 2004 (Volume 69, Number 128)] [Rules and Regulations] [Page 40539-40541] From the Federal Register Online via GPO Access [wais.access.gpo.gov] [DOCID:fr06jy04-4] DEPARTMENT OF
Revo, Incorporated: Amendment ; Docket No. FAA ; Directorate Identifier 2012-CE-013-AD.
2013-08-14 Revo, Incorporated: Amendment 39-17431; Docket No. FAA-2012-0845; Directorate Identifier 2012-CE-013-AD. (a) Effective. Date This airworthiness directive (AD) is effective June 13, 2013. (b)
[Docket No. FAA ; Product Identifier 2017-CE-049-AD; Amendment ; AD ]
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[Federal Register Volume 83, Number 30 (Tuesday, February 13, 2018)] [Rules and Regulations] [Pages 6114-6118] From the Federal Register Online via the Government Publishing Office [www.gpo.gov] [FR Doc
SERVICE BULLETIN TIME LIMITS/MAINTENANCE CHECKS - AIRBORNE INSTRUMENT AIR SYSTEM COMPONENT REPLACEMENT SCHEDULE
Beech TITLE: TIME LIMITS/MAINTENANCE CHECKS - AIRBORNE INSTRUMENT AIR SYSTEM COMPONENT REPLACEMENT SCHEDULE SYNOPSIS OF CHANGE This Service Bulletin has been revised at the request of the Federal Aviation
SERVICE LETTER REVISION
Revision 13 REVISION TRANSMITTAL SHEET This sheet transmits Revision 13 to, which: A. Updates the Accomplishment Instructions and the list of training agencies. B. Revises the expiration date to March
NUMBER 008 PLACARDS AND MARKINGS (ATA 11) MAXIMUM ZERO FUEL GROSS WEIGHT - 48,000 POUNDS PLACARD INSTALLATION
NUMBER 008 PLACARDS AND MARKINGS (ATA 11) MAXIMUM ZERO FUEL GROSS WEIGHT - 48,000 POUNDS PLACARD INSTALLATION December 15, 2004 PILOTS INFORMATION SHEET MAXIMUM ZERO FUEL GROSS WEIGHT - 48,000 POUNDS PLACARD
[Docket No. FAA ; Product Identifier 2017-CE-042-AD] Airworthiness Directives; GA 8 Airvan (Pty) Ltd Airplanes
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This document is scheduled to be published in the Federal Register on 12/19/2017 and available online at https://federalregister.gov/d/2017-27167, and on FDsys.gov [4910-13-P] DEPARTMENT OF TRANSPORTATION
SERVICE BULLETIN REVISION
Revision 3 REVISION TRANSMITTAL SHEET This sheet transmits Revision 3 to which: A. Removes the NOTE from the Effectivity section. B. Adds a NOTE to the Reason section. C. Changes SB750-76-06 to SB750-76-07
SERVICE BULLETIN FLIGHT CONTROLS - CONTROL COLUMN HARDWARE REPLACEMENT
SERVICE BULLETIN TITLE: FLIGHT CONTROLS - CONTROL COLUMN HARDWARE REPLACEMENT 1. Planning Information A. Effectivity (1) Airplanes Model A36 Bonanza, Serials E-2104, E-2111 through E-3629, and E-3631 through
PIPER AIRCRAFT, INC.
Page 1 2010-15-10 PIPER AIRCRAFT, INC. Amendment 39-16376 Docket No. FAA-2009-1015; Directorate Identifier 2009-CE-039-AD PREAMBLE Effective Date (a) This AD becomes effective on August 31, 2010. Affected
THE CESSNA AIRCRAFT COMPANY
Page 1 2010-20-10 THE CESSNA AIRCRAFT COMPANY Amendment 39-16444 Docket No. FAA-2010-0380; Directorate Identifier 2009-NM-009-AD PREAMBLE Effective Date (a) This AD becomes effective November 1, 2010.
BOMBARDIER, INC
Page 1 2010-18-08 BOMBARDIER, INC Amendment 39-16421 Docket No. FAA-2009-1110; Directorate Identifier 2009-NM-116-AD PREAMBLE Effective Date (a) This airworthiness directive (AD) becomes effective October
[Docket No. FAA ; Directorate Identifier 2016-NM-155-AD; Amendment. AGENCY: Federal Aviation Administration (FAA), DOT.
This document is scheduled to be published in the Federal Register on 04/17/2017 and available online at https://federalregister.gov/d/2017-07551, and on FDsys.gov [4910-13-P] DEPARTMENT OF TRANSPORTATION
[Docket No. FAA ; Product Identifier 2017-CE-049-AD; Amendment ; AD R1]
![[Docket No. FAA ; Product Identifier 2017-CE-049-AD; Amendment ; AD R1]](/thumbs/93/111165002.jpg "[Docket No. FAA ; Product Identifier 2017-CE-049-AD; Amendment ; AD R1]")
[Federal Register Volume 83, Number 89 (Tuesday, May 8, 2018)] [Rules and Regulations] [Pages 20719-20725] From the Federal Register Online via the Government Publishing Office [www.gpo.gov] [FR Doc No:
[Docket No. FAA ; Directorate Identifier 2017-CE-004-AD] Airworthiness Directives; Aerospace Welding Minneapolis, Inc.
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This document is scheduled to be published in the Federal Register on 04/18/2017 and available online at https://federalregister.gov/d/2017-07775, and on FDsys.gov [4910-13-P] DEPARTMENT OF TRANSPORTATION
[Docket No. FAA ; Directorate Identifier 2012-CE-013-AD] Airworthiness Directives; Revo, Incorporated Airplanes
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This document is scheduled to be published in the Federal Register on 08/16/2012 and available online at http://federalregister.gov/a/2012-20107, and on FDsys.gov [4910-13-P] DEPARTMENT OF TRANSPORTATION
[Docket No. FAA ; Directorate Identifier 2014-NM-041-AD; Amendment
This document is scheduled to be published in the Federal Register on 12/16/2014 and available online at http://federalregister.gov/a/2014-29225, and on FDsys.gov [4910-13-P] DEPARTMENT OF TRANSPORTATION
[Docket No. FAA ; Directorate Identifier 2012-NM-002-AD; Amendment ; AD ]
![[Docket No. FAA ; Directorate Identifier 2012-NM-002-AD; Amendment ; AD ]](/thumbs/89/99631284.jpg "[Docket No. FAA ; Directorate Identifier 2012-NM-002-AD; Amendment ; AD ]")
[Federal Register Volume 78, Number 104 (Thursday, May 30, 2013)] [Rules and Regulations] [Pages 32347-32349] From the Federal Register Online via the Government Printing Office [www.gpo.gov] [FR Doc No:
[Docket No. FAA ; Product Identifier 2017-NM-086-AD; AGENCY: Federal Aviation Administration (FAA), Department of Transportation
This document is scheduled to be published in the Federal Register on 06/05/2018 and available online at https://federalregister.gov/d/2018-11414, and on FDsys.gov [4910-13-P] DEPARTMENT OF TRANSPORTATION
Avidyne Corporation: Amendment ; Docket No. FAA ; Directorate Identifier 2008-CE-047-AD.
2009-05-05 Avidyne Corporation: Amendment 39-15829; Docket No. FAA- 2008-1210; Directorate Identifier 2008-CE-047-AD. Effective. Date (a) This AD becomes effective on April 3, 2009. Affected ADs (b) This
SERVICE BULLETIN. NOTE: SL should be accomplished in conjunction with this service bulletin.
SERVICE BULLETIN TITLE NAVIGATION - TDR-94D TRANSPONDER UPGRADE EFFECTIVITY MODEL SERIAL NUMBERS 560 ( Encore+) -0751thru-0802 with diversity enhanced surveillance transponders The equivalent of this service
[Docket No. FAA ; Product Identifier 2017-NM-072-AD; Amendment 39-
This document is scheduled to be published in the Federal Register on 03/26/2018 and available online at https://federalregister.gov/d/2018-05013, and on FDsys.gov [4910-13-P] DEPARTMENT OF TRANSPORTATION
SERVICE BULLETIN FLIGHT CONTROLS - FLIGHT CONTROL (GUST) LOCK INSPECTION / REPLACEMENT SYNOPSIS OF CHANGE
SERVICE BULLETIN TITLE: FLIGHT CONTROLS - FLIGHT CONTROL (GUST) LOCK INSPECTION / REPLACEMENT SYNOPSIS OF CHANGE This Service Bulletin has been revised to add ending serial effectivity. The first paragraph
[Docket No. FAA ; Directorate Identifier 2015-CE-017-AD] SUMMARY: The FAA is correcting a notice of proposed rulemaking (NPRM) that
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This document is scheduled to be published in the Federal Register on 09/04/2015 and available online at http://federalregister.gov/a/2015-21934, and on FDsys.gov [4910-13-P] DEPARTMENT OF TRANSPORTATION
[Docket No. FAA ; Directorate Identifier 2012-NM-218-AD] AGENCY: Federal Aviation Administration (FAA), DOT.
![[Docket No. FAA ; Directorate Identifier 2012-NM-218-AD] AGENCY: Federal Aviation Administration (FAA), DOT.](/thumbs/94/120859820.jpg "[Docket No. FAA ; Directorate Identifier 2012-NM-218-AD] AGENCY: Federal Aviation Administration (FAA), DOT.")
This document is scheduled to be published in the Federal Register on 02/10/2014 and available online at http://federalregister.gov/a/2014-02715, and on FDsys.gov [4910-13-P] DEPARTMENT OF TRANSPORTATION
[Docket No. FAA ; Directorate Identifier 2013-CE-028-AD] Airworthiness Directives; DORNIER LUFTFAHRT GmbH Airplanes
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This document is scheduled to be published in the Federal Register on 11/19/2013 and available online at http://federalregister.gov/a/2013-27665, and on FDsys.gov [4910-13-P] DEPARTMENT OF TRANSPORTATION
SUPPORT SERVICES GMBH
Page 1 2011-18-13 328 SUPPORT SERVICES GMBH (TYPE CERTIFICATE PREVIOUSLY HELD BY AVCRAFT AEROSPACE GMBH; FAIRCHILD DORNIER GMBH; DORNIER LUFTFAHRT GMBH) Amendment 39-16795 Docket No. FAA-2010-1163; Directorate
AIRWORTHINESS DIRECTIVE
EASA AIRWORTHINESS DIRECTIVE AD No : 2007-0272 Date: 16 October 2007 No person may operate an aircraft to which an Airworthiness Directive applies, except in accordance with the requirements of that Airworthiness
[Docket No. FAA ; Product Identifier 2018-NM-096-AD; Amendment ; AD ]
![[Docket No. FAA ; Product Identifier 2018-NM-096-AD; Amendment ; AD ]](/thumbs/91/107339271.jpg "[Docket No. FAA ; Product Identifier 2018-NM-096-AD; Amendment ; AD ]")
[Federal Register Volume 83, Number 236 (Monday, December 10, 2018)] [Rules and Regulations] [Pages 63394-63396] From the Federal Register Online via the Government Publishing Office [www.gpo.gov] [FR
[Docket No. FAA ; Product Identifier 2017-CE-022-AD] AGENCY: Federal Aviation Administration (FAA), Department of Transportation
![[Docket No. FAA ; Product Identifier 2017-CE-022-AD] AGENCY: Federal Aviation Administration (FAA), Department of Transportation](/thumbs/88/116055228.jpg "[Docket No. FAA ; Product Identifier 2017-CE-022-AD] AGENCY: Federal Aviation Administration (FAA), Department of Transportation")
This document is scheduled to be published in the Federal Register on 03/13/2018 and available online at https://federalregister.gov/d/2018-05012, and on FDsys.gov [4910-13-P] DEPARTMENT OF TRANSPORTATION
EMBRAER-EMPRESA BRASILEIRA DE AERONAUTICA S.A.
Page 1 2011-17-15 EMBRAER-EMPRESA BRASILEIRA DE AERONAUTICA S.A. Amendment 39-16779 Docket No. FAA-2011-0088; Directorate Identifier 2010-CE-072-AD PREAMBLE Effective Date (a) This airworthiness directive
[Docket No. FAA ; Directorate Identifier 2007-CE-004-AD; Amendment ; AD ]
![[Docket No. FAA ; Directorate Identifier 2007-CE-004-AD; Amendment ; AD ]](/thumbs/94/119658205.jpg "[Docket No. FAA ; Directorate Identifier 2007-CE-004-AD; Amendment ; AD ]")
[Federal Register: June 11, 2007 (Volume 72, Number 111)] [Rules and Regulations] [Page 31988-31990] From the Federal Register Online via GPO Access [wais.access.gpo.gov] [DOCID:fr11jn07-8] DEPARTMENT
[Docket No. FAA ; Product Identifier 2017-NM-111-AD; Amendment ; AD ]
![[Docket No. FAA ; Product Identifier 2017-NM-111-AD; Amendment ; AD ]](/thumbs/89/98947347.jpg "[Docket No. FAA ; Product Identifier 2017-NM-111-AD; Amendment ; AD ]")
[Federal Register Volume 83, Number 178 (Thursday, September 13, 2018)] [Rules and Regulations] [Pages 46377-46380] From the Federal Register Online via the Government Publishing Office [www.gpo.gov] [FR