Single Engine. Service Bulletin TITLE PILOT AND COPILOT SECONDARY SEAT STOP INSTALLATION
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1 Single Engine Service Bulletin May 14, 2007 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 Page 1 of 17 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
2 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 May 14, 2007
3 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 May 14, 2007 Page 3
4 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 May 14, 2007
5 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 May 14, 2007 Page 5
6 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 Page 6 May 14, 2007
7 A thru thru A 1970 thru thru A188A 1970 thru thru B 1972 thru thru A188B 1972 thru thru A188B 1972 thru T thru T A188B 678, 678T T188C T T T188C 1979 thru 1983 T T, T T T188C 1979 thru 1983 T T thru T T thru thru thru thru 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 May 14, 2007 Page 7
8 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 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 Page 8 May 14, 2007
9 210G 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 M/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 May 14, 2007 Page 9
10 A-A188B 1972 thru 1976 A-A thru A-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 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 Page 10 May 14, 2007
11 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 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: 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). APPROVAL FAA approval has been obtained on technical data in this publication that affects airplane type design. May 14, 2007 Page 11
12 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 : 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 May 14, 2007
13 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 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 188/190/195) 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 : 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 May 14, 2007 Page 13
14 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 : 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. OWNER NOTIFICATION Domestic...May14,2009 International...May14,2009 On May 14, 2007 the following Owner Advisory message will be sent to applicable owners of record in A. Dear Cessna Owner: This Owner Advisory is to inform you that : 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, 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 accomplished on your airplane. * * * * * * * Page 14 May 14, 2007
15 Figure 1. Identification of Secondary Seat Stop Installation Configurations (Sheet 1) May 14, 2007 Page 15
16 Figure 1. Identification of Secondary Seat Stop Installation Configurations (Sheet 2) Page 16 May 14, 2007
17 Figure 1. Identification of Secondary Seat Stop Installation Configurations (Sheet 3) May 14, 2007 Page 17
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The parts that follow are available from Cessna Parts Distribution through an appropriate Cessna Service Station.
Service Newsletter June 15, 2010 TITLE MECHANICAL AIR CONDITIONER COMPRESSOR DRIVER SHEAVE / PULLEY ALIGNMENT TO Cessna Distributors and Single Engine Service Stations MODELS AFFECTED The following airplanes
41001 thru incorporating a retrofitted LA nose strut,
Service Newsletter SNL08-15 TITLE LA71325000 NOSE STRUT ASSEMBLY SEALS REPLACEMENT TO Cessna Distributors, Service Stations MODELS AFFECTED Model 300/LC40-550FG Serial Numbers 41001 thru 40079 incorporating
Service Bulletin. ATA 27-00: Flight Controls Rudder-Aileron Interconnect Modification
Service Bulletin Issued: 09 May 2007 Models SR20 and SR22 ATA 27-00: Flight Controls Rudder-Aileron Interconnect Modification COMPLIANCE Mandatory: Accomplish this Service Bulletin within 25 Flight Hours
CIRRUS SR2X SB 2X R2. Service Bulletin. Issued: Revised: June 26, 2012 July 31, 2012
CIRRUS SR2X Service Bulletin Number: Issued: Revised: June 26, 2012 SNS SUBJECT: 57-40 ATTACH FITTINGS - Lower Landing Gear Attach Bracket Torque 1. COMPLIANCE Mandatory: Cirrus Design considers this Service
Certification Basis For Alteration. Original Type Certificate Number
FAA Model List () No. SA02987CH Electroair of Electroair Electronic Issue : July 5, 2011 Revised: July 15, 2016 Page 1 of 11 Electroair IC IC IC IC Aermacchi Model S.205-18/F, S.205-18/R, S.205-20/F, S.205-20/R
MODIFICATION KIT. Serial Numbers 300 (LC40-550FG) thru (LC42-550FG) thru (LC41-550FG) thru
Single Engine MODIFICATION KIT MK400-71-01 TITLE ENGINE OIL COOLER WINTERIZATION MODIFICATION EFFECTIVITY Model Serial Numbers 300 (LC40-550FG) 40004 thru 40079 350 (LC42-550FG) 42001 thru 421018 400 (LC41-550FG)
Page No. 1 of 6 Date: April 29, 2011 Installation Eligibility: Model. PMA NUMBER PQ2724CE Part No. Model No.
PMA NUMBER No. FAA Approval Basis and Approved Design Data Eligibility: Make Page No. 1 of 6 Propeller ATG210760 Woodward G210760 P210452( ), 210685, Test Report and Alexandria 17-30, 17-30A (IO-520 only)
(b) This AD supersedes AD R1, Amendment
2011-06-10 Piper Aircraft, Inc. (Type Certificate Previously Held by The New Piper Aircraft, Inc.):. Amendment 39-16635; Docket No. FAA-2010-1295; Directorate Identifier 2010-CE-060-AD. Effective Date
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
SERVICE BULLETIN CERTIFICATION REQUIREMENTS - FOREIGN CERTIFICATION PLACARD INSTALLATION
TITLE CERTIFICATION REQUIREMENTS - FOREIGN CERTIFICATION PLACARD INSTALLATION EFFECTIVITY MODEL UNIT NUMBERS 550-1040 NOTE: This Service Bulletin may only be accomplished at a Cessna-owned or an authorized
SERVICE FUEL WARNING PLACARD AND POH INSPECTION
Piper Aircraft, Inc. 2926 Piper Drive Vero Beach, Florida, U.S.A. 32960 SERVICE NO. 1266 BULLETIN PIPER CONSIDERS COMPLIANCE MANDATORY Date: December 16, 2014 (S) (M) Service Bulletin (SB) 1266 supersedes
Notification of a Proposal to issue an Airworthiness Directive
Notification of a Proposal to issue an Airworthiness Directive PAD No.: 18-143 Issued: 24 October 2018 Note: This Proposed Airworthiness Directive (PAD) is issued by EASA, acting in accordance with Regulation
Revision Transmittal Sheet
b 2 APPROVED WHITE IN LEARJET 23/24/25, 28/29, 35/36 RT 0980 Revision Transmittal Sheet This page transmits Revision 1 to, Replacement of Air Conditioning Evaporator Assembly. Rework: No rework is required
September 8, Cessna Distributors, Authorized Service Facilities, CPC's, CSTARS, ASR's, and affected Owners of Record
Service Newsletter September 8, 2011 SNL11-23 TITLE P&WC PROPELLER-SHAFT OIL SEAL MODIFICATION TO Cessna Distributors, Authorized Service Facilities, CPC's, CSTARS, ASR's, and affected Owners of Record
SERVICE BULLETIN SERIAL NUMBERS. The equivalent of this service bulletin has been incorporated on production airplanes and On.
TITLE FUSELAGE - TAILCONE GROUND RECEPTACLE INSTALLATION EFFECTIVITY MODEL SERIAL NUMBERS 560-0539 thru -0649 REASON The equivalent of this service bulletin has been incorporated on production airplanes
SERVICE BULLETIN REVISION TRANSMITTAL
REVISION TRANSMITTAL This sheet transmits Revision 2 to, which: A. Adds the CI401-460 GPS Antenna to Step 10A and Step 10B. B. Adds the CI401-460 GPS Antenna to Figure 5. C. Adds the CI401-460 GPS Antenna
SERVICE BULLETIN FLIGHT CONTROLS - RUDDERVATOR DIFFERENTIAL TAIL CONTROL ROD ASSEMBLY INSPECTION/MODIFICATION
Beech ATA Code 27-20 TITLE: FLIGHT CONTROLS - RUDDERVATOR DIFFERENTIAL TAIL CONTROL ROD ASSEMBLY INSPECTION/MODIFICATION SYNOPSIS OF CHANGE This Service Bulletin has been revised and is produced in the
SERVICE BULLETIN TITLE ENGINE CONTROLS - FULL AUTHORITY DIGITAL ENGINE CONTROL (FADEC) SOFTWARE UPGRADE VERSION C10
Citation SB750-76-12 TITLE ENGINE CONTROLS - FULL AUTHORITY DIGITAL ENGINE CONTROL (FADEC) SOFTWARE UPGRADE VERSION C10 EFFECTIVITY REASON MODEL SERIAL NUMBERS 750 (Citation X) -0001 thru -0313 NOTE: Airplanes
Service Bulletin. ATA 52-10: Passenger and Crew Doors Door Latching Assembly Upgrade
Service Bulletin Issued: 5 Oct 00 Models SR0 and SR ATA 5-10: Passenger and Crew Doors Door Latching Assembly Upgrade COMPLIANCE Optional: Accomplishment of this Service Bulletin is at the owner s option.
Cessna Aircraft Company: Amendment ; Docket No. FAA ; Directorate Identifier 2012-NM-020-AD.
2013-09-11 Cessna Aircraft Company: Amendment 39-17453; Docket No. FAA-2012-1001; Directorate Identifier 2012-NM-020-AD. (a) Effective Date. This AD is effective July 5, 2013. (b) Affected ADs None. (c)
SERVICE BULLETIN. The equivalent of this service bulletin has been incorporated on production airplanes and On. REASON
Citation TITLE SERVICE BULLETIN SB560XL-73-02 ENGINE FUEL AND CONTROL - TRANSMITTAL OF PRATT & WHITNEY CANADA SERVICE BULLETIN PW500-72-30290 TURBOFAN ENGINE HYDROMECHANICAL FUEL CONTROL - REPLACEMENT/MODIFICATION
SERVICE LETTER. COMPLIANCE DISCRETIONARY. This service letter should be accomplished at a scheduled Check 1, Check 2, or HSI. LABOR HOURS KEY WORD
Citation SERVICE LETTER SL525C-71-01 TITLE POWER PLANT - TRANSMITTAL OF WILLIAMS INTERNATIONAL SERVICE BULLETIN ENGINE OIL BREATHER TUBE ASSEMBLY & FRONT BYPASS DUCT RH BOSS ASSEMBLY INSTALL EFFECTIVITY
PA Archer 28-E13; thru PA Archer II thru ; ; ; thru
Piper Aircraft, Inc. 2926 Piper Drive Vero Beach, Florida, U.S.A. 32960 SERVICE NO. 1244A BULLETIN PIPER CONSIDERS COMPLIANCE MANDATORY Date: April 1, 2013 (S) (M) Service Bulletin (SB) 1244A supersedes
Cessna Main Gear Fairings
Cessna Main Gear Fairings Original Issue Date 2-6-85 APPLICABLE MODELS 150 Series, 170 Series, 172 Series, 175 Series, 177 Series, 180 Series, 182 Series, 185 Series, 205 Series, 206 Series, 207 Series.
SERVICE BULLETIN REVISION
Revision 7 REVISION TRANSMITTAL SHEET This sheet transmits Revision 7 to Service Bulletin. A. Replaces the AN960PD10L Washers with NAS1149D0316K Washers. B. Removes the optional Aviation Brake System antiskid
1139A. The New Piper Aircraft, Inc Piper Drive Vero Beach, Florida, U.S.A Date: April 9, 2004 (S)(M)
TM 1139A The New Piper Aircraft, Inc. 2926 Piper Drive Vero Beach, Florida, U.S.A. 32960 Date: April 9, 2004 (S)(M) SB1139A supersedes SB 1139. This revision adds a screw retaining clip to the control
MANDATORY SERVICE BULLETIN NO. MSB
Page 1 of 4 MANDATORY SERVICE BULLETIN NO. MSB-40-064 I TECHNICAL DETAILS I.1 Category Mandatory I.2 Airplanes affected Type: DA 40 Serial Numbers: 40.934, 40.942 40.950 through 40.972 40.974, 40.984,
KELLY AEROSPACE POWER SYSTEMS
Page 1 2008-08-17 KELLY AEROSPACE POWER SYSTEMS Amendment 39-15471 Docket No. FAA-2008-0314; Directorate Identifier 2008-NE-09-AD PREAMBLE Effective Date (a) This airworthiness directive (AD) becomes effective
SERVICE BULLETIN SB
TITLE LIGHTS - LED POSITION, TAIL POSITION, AND ANTI-COLLISION (PTA) LIGHT INSTALLATION EFFECTIVITY MODEL SERIAL NUMBERS 560 (Citation Encore) -0539 thru -0707 560 (Citation Encore+) -0751 thru -0802 NOTE:
SERVICE BULLETIN REVISION TRANSMITTAL
REVISION TRANSMITTAL This sheet transmits Revision 2 to, which: A. Adds the reference to Figure 7, Sheet 1 and Sheet 2 to Step 10D. B. Adds Step 10D(7). C. Removes the After Modification view for PN343
[Docket No. FAA ; Directorate Identifier 2008-NE-09-AD; Amendment ; AD ]
![[Docket No. FAA ; Directorate Identifier 2008-NE-09-AD; Amendment ; AD ]](/thumbs/90/103888893.jpg "[Docket No. FAA ; Directorate Identifier 2008-NE-09-AD; Amendment ; AD ]")
[Federal Register: April 21, 2008 (Volume 73, Number 77)] [Rules and Regulations] [Page 21222-21225] From the Federal Register Online via GPO Access [wais.access.gpo.gov] [DOCID:fr21ap08-3] DEPARTMENT
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,
DEPARTMENT OF TRANSPORTATION
DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [62 FR 40262 No. 144; 07/28/97][SN] [Docket No. 97-ANE-26-AD; Amendment 39-10085; AD 97-15-11] RIN 2120-AA64 Avco Lycoming /
SERVICE BULLETIN FUEL - MODIFICATION OF THE ENGINE DRIVEN FUEL PUMP SYSTEM
Beech TITLE: FUEL - MODIFICATION OF THE ENGINE DRIVEN FUEL PUMP SYSTEM 1. Planning Information A. Effectivity (1) Airplanes Beechcraft Bonanza Model A36, Serials E-1946, E-2104, and E-2111 through E-3144;
AIRWORTHINESS DIRECTIVE
AIRWORTHINESS DIRECTIVE REGULATORY SUPPORT DIVISION P.O. BOX 26460 OKLAHOMA CITY, OKLAHOMA 73125-0460 U.S. Department of Transportation Federal Aviation Administration The following Airworthiness Directive
ROTORCRAFT FLIGHT MANUAL TEMPORARY REVISION FOR 4 AXIS AUTOPILOT OPERATIONS, INTRODUCTION OF.
ALERT SERVICE BULLETIN 412-17-175 02 February 2018 MODEL AFFECTED: SUBJECT: 412EP ROTORCRAFT FLIGHT MANUAL TEMPORARY REVISION FOR 4 AXIS AUTOPILOT OPERATIONS, INTRODUCTION OF. HELICOPTERS AFFECTED: Serial
ALERT SERVICE BULLETIN
2900 Selma Highway Montgomery, AL 36108 USA Tel: 334-386-5400 Fax: 334-386-5450 ALERT SERVICE BULLETIN Alert Service Bulletin No. 074 1. Planning Information A. Effectivity (1) Aeroforce turbocharger center
BULLETIN. Piper Aircraft, Inc Piper Drive Vero Beach, FL, U.S.A Date: October 29, 2015 (S) (M)
Piper Aircraft, Inc. 2926 Piper Drive Vero Beach, FL, U.S.A. 32960 SERVICE NO. 1244B BULLETIN PIPER CONSIDERS COMPLIANCE MANDATORY Date: October 29, 2015 (S) (M) Service Bulletin (SB) 1244B supersedes
Airworthiness Directive
Airworthiness Directive Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [62 FR 40262 NO. 144 07/28/97] [Docket No. 97-ANE-26-AD;
PILATUS AIRCRAFT LTD. CH-6371 STANS, SWITZERLAND SERVICE BULLETIN SERVICE BULLETIN NO: REF NO: 106 MODIFICATION NO: ATA CHAPTER: 28
PILATUS AIRCRAFT LTD. CH-6371 STANS, SWITZERLAND NO: 28-009 REF NO: 106 MODIFICATION NO: 03 0178 ATA CHAPTER: 28 FUEL - DISTRIBUTION FUEL BOOSTER PUMP - DAMAGE TO WIRES DURING INSTALLATION 1. Planning
PRATT AND WHITNEY CANADA CORP.
Page 1 2010-17-06 PRATT AND WHITNEY CANADA CORP. (FORMERLY PRATT & WHITNEY CANADA, INC.) Amendment 39-16398 Docket No. FAA-2010-0245; DIRECTORATE IDENTIFIER 2010-NE-15-AD. PREAMBLE Effective Date (a) This
Service Bulletin No: Ref No: 121 Modification No: INSPECTION ATA Chapter: 53
PILATUS AIRCRAFT LTD. STANS, SWITZERLAND Service Bulletin No: 53-014 Ref No: 121 Modification No: INSPECTION ATA Chapter: 53 FUSELAGE - GENERAL INSPECTION FOR CORROSION ON THE UPPER LEFT AND RIGHT LONGERONS
SERVICE BULLETIN REVISION
Revision 1 REVISION TRANSMITTAL SHEET This sheet transmits Revision 1 to. A. Adds Sheet 4 to Figure 1. B. Adds instructions to make the cutouts in the stiffener on the upper engine cowl larger. NOTE: This
SERVICE INSTRUCTION.
652 Oliver Street Williamsport, PA. 17701 U.S.A. Telephone +1 (800) 258-3279 U.S. and Canada (Toll Free) Telephone +1 (570) 323-6181 (Direct) Facsimile +1 (570) 327-7101 Email Technicalsupport@lycoming.com
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 No: Ref No: 165 Modification No: EC ATA Chapter: 21
PILATUS AIRCRAFT LTD. STANS, SWITZERLAND Service Bulletin No: 21-012 Ref No: 165 Modification No: EC-14-0359 ATA Chapter: 21 AIR CONDITIONING - COOLING INSTALL A COVER ASSEMBLY TO THE COMPRESSOR TO PROTECT
Cal Pacific Airmotive, Inc.
Cal Pacific Airmotive, Inc. Title: Inspection of Flight Control System Mandatory Service Bulletin North American Aviation P-51B, P-51C, P-51D, P-51K, F-51D, F-51K S.B. No. P51-001 Revision: 0 Issue Date
Service Bulletin SB 07-03
Service Bulletin SB 07-03 BRS-600 Pick-up Collar Support Replacement Compliance Mandatory: BRS considers this service bulletin to be mandatory. Accomplish this service bulletin within the next 25 flight
201F Fuel Pump Valve Housing Cap Screw Replacement
Service Bulletin 2900 Selma Highway Montgomery, AL 36108 USA Tel: 334-386-5400 Fax: 334-386-5450 http://www.hartzell.aero 201F Fuel Pump Valve Housing Cap Screw Replacement 1. Planning Information A. Effectivity