# N89427: 1977 Boeing 727-227, registration cancelled 2011-09-20 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: September 20, 2011 - Status when cancelled: Valid registration - Airframe: [Boeing 727-227](https://openairdocs.org/model/boeing-727-227) (registry code 1384078) - Engine: [Pratt & Whitney JT8D-9 series](https://openairdocs.org/engine/pratt-whitney-jt8d-9-series) (registry code 52048) - Data sheets: [TCDS A3WE](https://openairdocs.org/tcds/A3WE), [TCDS E2EA](https://openairdocs.org/tcds/E2EA) (OpenAirDocs) - Serial number: 21365 - Year built: 1977 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: July 5, 1977 - Certificate issued: January 13, 2010 - Last registry action: January 13, 2010 - Mode S code: AC56EE - Owner when cancelled: [Cargo Aircraft Management Inc](https://openairdocs.org/faa-owner/CARGO%20AIRCRAFT%20MANAGEMENT%20INC) - Location: [Orlando, FL](https://openairdocs.org/faa-place/FL/Orlando) - Owner type: Corporation - Owner's area on the map: 28.4899° N, 81.2902° W: Placed by OpenAirDocs at the center of ZIP code 32822, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N89427 - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=89427 - Page: https://openairdocs.org/deregistered/N89427-2011-09-20 From the FAA registry file of October 29, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe. ADs and bulletins for the Boeing 727-227: https://openairdocs.org/model/boeing-727-227.md ## Service difficulty reports (161, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR C8GA2010000056](https://openairdocs.org/sdr/C8GA2010000056), Oct 5, 2010: SWITCH. INOPERATIVE. DURING TAKEOFF ROLL AT 80 KNOTS. THE AMBER AFT AIR-STAIR LIGHT ILLUMINATED. ACFT ABORTED TAKEOFF WHERE IT PRECEDED WITH OUT INCIDENT. POST FLIGHT INSP WAS PERFO - [SDR C8GA201000013](https://openairdocs.org/sdr/C8GA201000013), Jul 30, 2010: SWITCH. FAULTED. DURING TAKEOFF ROLL WITH THE ACFT BELOW 60 KNOTS THE TAKEOFF WARNING HORN SOUNDED. TAKEOFF WAS ABORTED WITHOUT INCIDENT AND RETURNED TO THE BLOCKS. POST FLIGHT - [SDR C8GA201000008](https://openairdocs.org/sdr/C8GA201000008), Apr 16, 2010: DOOR. OUT OF ADJUST. FLT 735 FROM MMY TO TOL ON VISUAL APPROACH INTO TOLEDO UPON SELECTING GEAR DOWN THE LEFT AND RIGHT MAIN GEAR CAME DOWN NORMALLY, BUT THE NOSE GEAR REMAINED IN T - [SDR C8GA201000002](https://openairdocs.org/sdr/C8GA201000002), Jan 20, 2010: DUCT. CRACKED. DURING CLIMB OPERATION THE LOWER AFT BODY OVERHEAT ILLUMINATED IN FLIGHT. CREW PERFORMED APPROPRIATE CHECKLIST AND DIVERTED, WHERE IT LANDED WITHOUT INCIDENT. P - [SDR C8GA20090295](https://openairdocs.org/sdr/C8GA20090295), Jul 31, 2009: SPAR. CORRODED. REMOVED AND REPLACED RT ELEVATOR SPAR AND SUPPORT FITTINGS. ACFT WAS RETURNED TO SERVICE. - [SDR C8GA20090294](https://openairdocs.org/sdr/C8GA20090294), Jul 31, 2009: STRINGER SPLICE. CORRODED. WHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT BS 1010 28L SKIN IS CORRODED. REMOVED SPLICE, FABRICATED NEW SPLICE FROM BAC 1498-131 DIM 12.25" X 4.25" INS - [SDR C8GA20090293](https://openairdocs.org/sdr/C8GA20090293), Jul 31, 2009: STRINGER. CORRODED. WHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT BS 1050-1030 STR 30 IS CORRODED. REMOVED DAMAGED AREA DIM 19". FABRICATED NEW STR FROM BAC 1449146 7075 T62 - [SDR C8GA20090292](https://openairdocs.org/sdr/C8GA20090292), Jul 31, 2009: FRAME. CORRODED. WHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT FRAME AT BS 1010 IS CORRODED AT STR 29L. REMOVED DAMAGED AREA DIM 2" X 5.5". FABRICATED NEW SHEAR TIE FROM 7 - [SDR C8GA20090291](https://openairdocs.org/sdr/C8GA20090291), Jul 31, 2009: STRINGER. CORRODED. WHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT FRAME AT BS 1010 IS CORRODED AT STR 29R. REMOVED PREVIOUS REPAIR. FABRICATED NEW STRINGER FROM BAC1498-147 , - [SDR C8GA20090290](https://openairdocs.org/sdr/C8GA20090290), Jul 31, 2009: FRAME. DENTED. WHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT FRAME AT BS 1030 IS DENTED. BETWEEN STR 27R AND 26R. REMOVED DAMAGED AREA, FABRICATED REPAIR DOUBLER, HEAT T - [SDR C8GA20090289](https://openairdocs.org/sdr/C8GA20090289), Jul 31, 2009: FRAME. CORRODED. WHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT FRAME AT BS 1010 IS CRACKED BETWEEN STR 27R AND 26R. REMOVED DAMAGED AREA DIM 2.5" X 1.5" AND 1.5" X 1.5", F - [SDR C8GA20090288A](https://openairdocs.org/sdr/C8GA20090288A), Jul 31, 2009: SHEAR TIE. CORRODED. WHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT FRAME AT BS 1110 BETWEEN STR 27R AND 30 IS CORRODED. REMOVED DAMAGED AREA DIM 3.75" X .875", FABRICATED SHEA - [SDR C8GA20090288](https://openairdocs.org/sdr/C8GA20090288), Jul 31, 2009: STRINGER. CORRODED. WHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT BS 1080-1130 27 HAS CORRODED IN CHANNEL. REMOVED DAMAGED AREA, FABRICATED NEW STR, & SPLICES. INSTALLED REPA - [SDR C8GA20090287](https://openairdocs.org/sdr/C8GA20090287), Jul 31, 2009: FITTING. CORRODED. WHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT BS 1054-1057 27R HAS CORRODED TIE FITTING. REMOVED DAMAGED AREA, FABRICATED NEW FITTING FROM 7075 T6511DIM 8 - [SDR C8GA20090286](https://openairdocs.org/sdr/C8GA20090286), Jul 31, 2009: STRINGER. CORRODED. WHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT BS 1050-1130 STR 27R HAS CORROSION. REMOVED DAMAGED AREA, FABRICATED NEW STR FROM BAC1498-146 7075 T62 DIM 2 - [SDR C8GA20090285](https://openairdocs.org/sdr/C8GA20090285), Jul 31, 2009: ANGLE. CORRODED. WHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT BS 1130 TIE CLIP IS CORRODED. FABRICATED NEW CLIP FROM 7075 T6 .040" X 4" X 3.5". INSTALLED CLIP, NO OTHER D - [SDR C8GA20090284](https://openairdocs.org/sdr/C8GA20090284), Jul 31, 2009: SHEAR TIE. CORRODED. WHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT FRAME AT BS 1130 SHEAR TIE IS CORRODED BETWEEN STR 26R-29R. REMOVED DAMAGED SECTION, FABRICATED NEW SHEAR TI - [SDR C8GA20090283](https://openairdocs.org/sdr/C8GA20090283), Jul 31, 2009: FRAME. GOUGED. WHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT FRAME AT BS 1090 STR 27L IS GOUGED. REMOVED DAMAGED SECTION, FABRICATED NEW FRAME FROM 7075-0 DIM .071" X 20 - [SDR C8GA20090282](https://openairdocs.org/sdr/C8GA20090282), Jul 31, 2009: FRAME. GOUGED. WHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT FRAME AT BS 1110 STR 27L IS GOUGED. REMOVED DAMAGED SECTION, FABRICATED REPAIR DOUBLER FROM 7075-0 DIM .071" - [SDR C8GA20090281](https://openairdocs.org/sdr/C8GA20090281), Jul 31, 2009: FRAME. GOUGED. WHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT FAME AT BS 1130 STR 27L IS GOUGED. REMOVED DAMAGED SECTION, FABRICATED REPAIR DOUBLER FROM 7075-0 DIM .071" - [SDR C8GA20090280](https://openairdocs.org/sdr/C8GA20090280), Jul 31, 2009: FRAME. CORRODED. WHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT FAME AT BS 1110 STR 26R IS DENTED. REMOVED DAMAGED SECTION, FABRICATED REPAIR DOUBLER FROM 7075-0 DIM .071" - [SDR C8GA20090279](https://openairdocs.org/sdr/C8GA20090279), Jul 31, 2009: FRAME. CORRODED. WHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT FAME AT BS 1110 STR 27R HAS PUNCTURE. REMOVED DAMAGED SECTION, FABRICATED REPAIR DOUBLER FROM 7075-0 DIM .07 - [SDR C8GA20090278](https://openairdocs.org/sdr/C8GA20090278), Jul 31, 2009: REPAIR. CORRODED. WHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT BS 1130-1148 STR 30 PREVIOUS REPAIR IS CORRODED. REMOVED EXISTING REPAIR, FABRICATED NEW REPAIR FROM BAC 149 - [SDR C8GA20090277](https://openairdocs.org/sdr/C8GA20090277), Jul 31, 2009: STRINGER. CORRODED. WHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT BS 1148-1166 STR 30 PREVIOUS REPAIR IS CORRODED. REMOVED EXISTING REPAIR, FABRICATED NEW REPAIR FROM BAC 149 - [SDR C8GA20090276](https://openairdocs.org/sdr/C8GA20090276), Jul 31, 2009: REPAIR. PUNCTURED. WHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT BS 1130 PREVIOUS REPAIR AT 27 R HAS A PUNCTURE. REMOVED PREVIOUS REPAIR AND FABRICATED NEW FROM FROM 7075-0 - [SDR C8GA20090275](https://openairdocs.org/sdr/C8GA20090275), Jul 31, 2009: STRUCTURE. CRACKED. WHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT THE L1 DOOR HAD AN OVER-SIZED FASTENER HOLE. REMOVED FASTENER AND EXISTING DOUBLER. TRIMMED OUT DAMAGE DIM 1 - [SDR C8GA20090274](https://openairdocs.org/sdr/C8GA20090274), Jul 31, 2009: STRINGER. CRACKED. WHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED AT STA 620 STR 27R IS CORRODED. REMOVED DAMAGED SECTION DIM 18" FABRICATED NEW STR FROM BAC1498-147 7075 T62 DIM - [SDR C8GA20090273](https://openairdocs.org/sdr/C8GA20090273), Jul 31, 2009: INTERCOSTAL. CRACKED. WHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED AT STA 620 STR 24R WEB IS CRACKED. REMOVED AND FABRICATED NEW INTERCOSTAL FROM 7075-0 .063" DIM 19.250" X 6" HEAT - [SDR C8GA20090272](https://openairdocs.org/sdr/C8GA20090272), Jul 31, 2009: INTERCOSTAL. CRACKED. WHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED AT STA 620 STR 22R WEB IS CRACKED. REMOVED AND FABRICATED NEW INTERCOSTAL FROM 7075-0 .063" DIM 19.250" X 5.750" - [SDR C8GA20090271](https://openairdocs.org/sdr/C8GA20090271), Jul 31, 2009: INTERCOSTAL. CRACKED. WHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED AT STA 560, STR 23R WEB IS CRACKED. REMOVED AND FABRICATED NEW INTERCOSTAL FROM 7075-0 .063" DIM 19.250" X 7" HEA - [SDR C8GA20090270](https://openairdocs.org/sdr/C8GA20090270), Jul 31, 2009: INTERCOSTAL. CRACKED. WHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED AT STA 560, STR 19R WEB IS CRACKED. REMOVED AND FABRICATED NEW INTERCOSTAL FROM 7075-0 .063" DIM 19" X 7" HEAT TR - [SDR C8GA20090269](https://openairdocs.org/sdr/C8GA20090269), Jul 31, 2009: WEB. CORRODED. WHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT THE WEB AT BS 990 STR 27R-26R IS CORRODED. REMOVED DAMAGED SECTION DIM 1.750" X 2.5". FABRICATED FILLER FROM - [SDR C8GA20090268](https://openairdocs.org/sdr/C8GA20090268), Jul 31, 2009: STRINGER. CORRODED. WHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT STR 27R HAS CORROSION BETWEEN BS 990-1010. FABRICATED DOUBLER FROM 7075 T6 .071" 5.25" X 12.5, SHIM 7075 T6 - [SDR C8GA20090267](https://openairdocs.org/sdr/C8GA20090267), Jul 31, 2009: SHEAR TIE. CORRODED. WHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT THE SHEAR TIE AT 970 STR 29R IS CORRODED. REMOVED DAMAGED AREA DIM 1" X 4.25". FABRICATED REPAIR DOUBLER FRO - [SDR C8GA20090266](https://openairdocs.org/sdr/C8GA20090266), Jul 31, 2009: INTERCOSTAL. CORRODED. WHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT THE INTERCOSTAL AT STA 950A IS CORRODED AT STRINGER 28L. REMOVED INTERCOSTAL AND FABRICATED NEW FROM 7075 T6 - [SDR C8GA20090265](https://openairdocs.org/sdr/C8GA20090265), Jul 31, 2009: BRACKET. CORRODED. WHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT STR 27L BRACKET CORRODED AT BS 950C. REMOVED BRACKET, FABRICATED NEW FROM 7075 T6 .040" DIM 3.25" X 3". INST - [SDR C8GA20090264](https://openairdocs.org/sdr/C8GA20090264), Jul 31, 2009: INTERCOSTAL. CORRODED. WHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT AT STA 950A, STR 29L THE INTERCOSTAL IS CORRODED. REMOVED DAMAGED INTERCOSTAL AND FABRICATED NEW FROM 7075 T - [SDR C8GA20090263](https://openairdocs.org/sdr/C8GA20090263), Jul 31, 2009: WEB. CORRODED. WHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT AT STA 560 STR 25R WEB IS CRACKED. CUT OUT DAMAGED WEB AND FABRICATED NEW FROM 7075 T6 .063" DIM 29.5" X 4.5 - [SDR C8GA20090262](https://openairdocs.org/sdr/C8GA20090262), Jul 31, 2009: SHEAR TIE. CORRODED. WHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT AT STA 970 RBL 15 TO RBL 20 LOWER FLANGE ON THE FRAME IS CORRODED. FABRICATED SHEAR TIE REPAIR FROM 7075-0 . - [SDR C8GA20090261](https://openairdocs.org/sdr/C8GA20090261), Jul 31, 2009: SKIN. CORRODED. WHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT AT STA 720 BL 0 SKIN IS CORRODED. REMOVED PREVIOUS REPAIR, CUT OUT DAMAGE DIM 8.5" X 9.5. FABRICATED REPAIR - [SDR C8GA20090260](https://openairdocs.org/sdr/C8GA20090260), Jul 31, 2009: STRINGER. CORRODED. WHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT STR 27R STA 710 IS CORRODED. REMOVED DAMAGED SECTION OF STR AND FABRICATED NEW FROM BAC1498-144 7075 T6 DIM - [SDR C8GA200900259](https://openairdocs.org/sdr/C8GA200900259), Jul 31, 2009: STRINGER. CORRODED. WHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT STA 560-570, STR 27L IS CORRODED. FLOORBEAM SPLICE PLATE IS CRACKED. REMOVED DAMAGED SECTION OF STR DIM 18.2 - [SDR C8GA200900258](https://openairdocs.org/sdr/C8GA200900258), Jul 31, 2009: FLOORBEAM. CRACKED. WHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT STA 660, STR 17L FLOORBEAM SPLICE PLATE IS CRACKED. REMOVED CRACKED SPLICE PLATE AND FABRICATED NEW FROM 202 - [SDR C8GA200900257](https://openairdocs.org/sdr/C8GA200900257), Jul 31, 2009: FLOORBEAM. CRACKED. WHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT STA 680, STR 17L FLOORBEAM IS CRACKED. REMOVED DAMAGED SECTION . HFEC FORT CONTAINMENT, FABRICATED FILLER FR - [SDR C8GA200900256](https://openairdocs.org/sdr/C8GA200900256), Jul 31, 2009: FAILSAFE. GOUGED. WHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT THE FAIL SAFE IS GOUGED AT STA 540, STR 25L. FABRICATED NEW FAIL SAFE CHORD FROM BAC 1490-2763 .090" DIM 8.7 - [SDR C8GA20090255](https://openairdocs.org/sdr/C8GA20090255), Jul 31, 2009: WEB. CRACKED. WHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT THE WEB IS CRACKED AT STA 500, STR 27L. REMOVED AND REPLACE WEB, FABRICATED FROM 7075 T6 .050" DIM 5.875" X - [SDR C8GA20090254](https://openairdocs.org/sdr/C8GA20090254), Jul 31, 2009: STRINGER. MISREPAIRED. WHILE IN HEAVY MX PERFORMING INSP STR SPLICE WAS FOUND TO BE NO-COMPLIANT AT BS 950E +5 - 969 STR 28R. REMOVED REPAIR AND FABRICATED NEW STR FROM 65-58387-2 DIM - [SDR C8GA20090253](https://openairdocs.org/sdr/C8GA20090253), Jul 31, 2009: SKIN. DAMAGED. WHILE IN HEAVY MX PERFORMING DENT AND REPAIR MAPPING EXISTING EXTERNAL FUSELAGE REPAIR AT BS 1180 BETWEEN STR 19L- 20L IS NON COMPLIANT. REMOVED REPAIR AND FABR - [SDR C8GA20090252](https://openairdocs.org/sdr/C8GA20090252), Jul 31, 2009: SKIN. DAMAGED. WHILE IN HEAVY MX PERFORMING DENT AND REPAIR MAPPING EXISTING EXTERNAL FUSELAGE REPAIR AT BS 1151 BETWEEN STR 18L- 20L IS NON COMPLIANT. REMOVED REPAIR AND FABR - [SDR C8GA20090251](https://openairdocs.org/sdr/C8GA20090251), Jul 31, 2009: STRINGER. CORRODED. WHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT STA 740 STR 24R HAS CORROSION. REMOVED DAMAGED SECTION DIM 11", FABRICATED NEW STR FROM BAC 1498-142 DIM 11" All 161: https://openairdocs.org/deregistered/N89427-2011-09-20/reports.md ## Other aircraft with N89427 - [Cancelled 1980-06-25](https://openairdocs.org/deregistered/N89427-1980-06-25): Cessna 152, S/N 152-82740. Exported to Canada. Owner: [Aer Aisling Ltd](https://openairdocs.org/faa-owner/AER%20AISLING%20LTD), [Flushing, NY](https://openairdocs.org/faa-place/NY/Flushing) - [Cancelled 1955-10-24](https://openairdocs.org/deregistered/N89427-1955-10-24): Cessna 140, S/N 8459. Owner: [Freehold Flying Club Inc](https://openairdocs.org/faa-owner/FREEHOLD%20FLYING%20CLUB%20INC) --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.