# N618UA: 1983 Boeing 767-222, registration cancelled 2007-07-13 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: July 13, 2007 - Exported to: South Africa - Status when cancelled: Sale reported - Airframe: [Boeing 767-222](https://openairdocs.org/model/boeing-767-222) (registry code 1385122) - Engine: [Pratt & Whitney JT9D series](https://openairdocs.org/engine/pratt-whitney-jt9d-series) (registry code 52054) - Data sheets: [TCDS A1NM](https://openairdocs.org/tcds/A1NM) (OpenAirDocs) - Serial number: 21878 - Year built: 1983 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: March 30, 1983 - Last registry action: January 11, 2007 - Mode S code: A80E39 - Location: Libreville Gabon, Gabon - Owner type: Individual - The mark today: https://openairdocs.org/aircraft/N618UA - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=618UA - Page: https://openairdocs.org/deregistered/N618UA-2007-07-13 From the FAA registry file of November 7, 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 767-222: https://openairdocs.org/model/boeing-767-222.md ## Service difficulty reports (32) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR 2004UALA00418](https://openairdocs.org/sdr/2004UALA00418), Mar 18, 2004: BOLT. SHEARED. NOSE GEAR LT DOOR LINK ROD HINGE BOLT IS SHEARED. FOUND DURING NR 1 SERVICE. BOLT NOT RECOVERED, CAUSE OF FAILURE UNKNOWN. REPLACED BOLT. - [SDR 2003UALA00618](https://openairdocs.org/sdr/2003UALA00618), Aug 12, 2003: KEELBEAM. CORRODED. KEELBEAM WEB DRAIN HOLE HAS CORROSION AT BS 786, BL0. - [SDR 2003UALA00632](https://openairdocs.org/sdr/2003UALA00632), Aug 4, 2003: WEDGE. DELAMINATED. T/E WEDGE DELAMINATED. T/E WEDGE REPLACED. - [SDR 2003UALA00285](https://openairdocs.org/sdr/2003UALA00285), Mar 16, 2003: SKIN. GOUGED. A/C DAMAGED BY LOADER AFT OF FWD CARGO DOOR. VARIOUS DENTS AND GOUGES MAJOR REPAIR ACCOMPLISHED WITH DOUBLERS IN AREA FWD OF CARGO DOOR BELOW RT WING LITE. - [SDR 2001UALA01977](https://openairdocs.org/sdr/2001UALA01977), Aug 31, 2001: CONTROLLER. FAILED. FWD EQUIPMENT NO COOLING LIGHT ON FOR 3 MINUTES. REPLACED CONTROLLER AND CLEANED EQUIPMENT COOLING AIR CLEANER. - [SDR 2001UALA00886](https://openairdocs.org/sdr/2001UALA00886), May 10, 2001: ENGINE. MALFUNCTIONED. AT LOW POWER SETTING ON CLIMB UNDER 1.20 EPR RT ENG LAGGED LT BY .15 EPR AND 15 PERCENT N1, ABOVE 1.20 EPR AT CRUISE OKAY. ON DESCENT AT LOW ALT RT LAGGED BY .1 - [SDR 2001UALA00156](https://openairdocs.org/sdr/2001UALA00156), Feb 24, 2001: STRINGER. CORRODED. AFT PIT BS 1307 - 1329 STRINGER 35L CORRODED. INSTALLED STRINGER REPAIR REF: SRM 53-00-03 FIG 202. - [SDR 2001UALA00154](https://openairdocs.org/sdr/2001UALA00154), Feb 24, 2001: SHEAR TIE. CORRODED. AFT PIT BS 1153 BETWEEN STRINGERS 38R - 39R SHEAR TIE CORRODED. REPLACED SHEAR TIE REF: BAC DWG 140T2102, SRM 53-00-07, 51-40-02. - [SDR 2001UALA00155](https://openairdocs.org/sdr/2001UALA00155), Feb 23, 2001: SHEAR TIE. CORRODED. AFT PIT BS 1263 BETWEEN STRINGERS 37L - 38L SHEAR TIE CORRODED. REPLACED SHEAR TIE REF: BAC DWG 140T2101, SRM 51-10-00, AND 51-40-02. - [SDR 2001UALA00153](https://openairdocs.org/sdr/2001UALA00153), Feb 23, 2001: RIB. CORRODED. AFT CARGO DOOR BS 1270-1350 RIB NR 3 CORRODED. REPAIRED DOOR BEAM PER TIMCO REO-GO7862 REF: SRM 52-30-02. - [SDR 2001UALA00124](https://openairdocs.org/sdr/2001UALA00124), Feb 15, 2001: SHEAR TIE. CORRODED. AFT CARGO PIT BS 1197 BETWEEN STR 37L AND 38L SHEAR TIE CORRODED. REPLACED SHEAR TIE BY OSV TIMCO, REFERENCE SRM 51-40-02 FOR FASTENER INSTALLATION PROCEDURES. - [SDR 2001UALA00118](https://openairdocs.org/sdr/2001UALA00118), Feb 15, 2001: FRAME. DAMAGED. AFT PIT BS 1153 BETWEEN STRINGER 39L AND 39R FRAME WEB HAS ELONGATED HOLE. *S/D* WEB REPAIR INSTALLED BY OSV TIMCO, REFERENCE SRM 51-40-02 FOR FASTENER INSTALLA - [SDR 2001UALA00189](https://openairdocs.org/sdr/2001UALA00189), Feb 14, 2001: SPLICE. CORRODED. NR 1 PYLON INBOARD SIDE BETWEEN 2 SIDE PANELS, ATTACH SPLICE IS CORRODED. REPLACED SPLICE PER SRM 51-40-02. - [SDR 2001UALA00186](https://openairdocs.org/sdr/2001UALA00186), Feb 14, 2001: SHEAR TIE. CORRODED. AFT PIT SHEAR TIE CORRODED BS 1480. REPLACED SHEAR TIE REF: BAC 140T2102 AND SRM 51-40-02. - [SDR 2001UALA00183](https://openairdocs.org/sdr/2001UALA00183), Feb 14, 2001: SHEAR TIE. CORRODED. AFT PIT SHEAR TIE BETWEEN STR 39L AND 39R CORRODED. INSTALLED NEW SHEAR TIE PER BAC DRAWING 146T1206 AND SRM 51-40-2. - [SDR 2001UALA00182](https://openairdocs.org/sdr/2001UALA00182), Feb 14, 2001: SEAT TRACK. CORRODED. MAIN CABIN SEAT TRACK FITTING CORRODED AT STATION 1421 T0 1471, RBL 90, UNDER FLANGE. REPLACED FITTING PER BAC DWG 146T5204-2 AND INSTALLED FITTING PER SRM 51-4 - [SDR 2001UALA00134](https://openairdocs.org/sdr/2001UALA00134), Feb 14, 2001: STRINGER. CORRODED. AFT CARGO PIT AT BS 1395, STRINGER 39L END FITTING IS CORRODED BOTH SIDES OF STRINGER. REMOVED CORROSION FROM STRINGER PER GN-MM 5-0-6-1. REPLACED STRINGER SPLI - [SDR 2001UALA00111](https://openairdocs.org/sdr/2001UALA00111), Feb 12, 2001: ATTACH ANGLE. CORRODED. AFT CARGO PIT BS 1087 STRINGER 39R FRAME TO STRINGER ATTACH ANGLE CORRODED. *S/D* STRINGER ATTACH ANGLE WAS REPLACED BY OSV TIMCO, REFERENCE SRM 51-40-02 FOR FA - [SDR 2001UALA00107](https://openairdocs.org/sdr/2001UALA00107), Feb 9, 2001: SHEAR TIE. CORRODED. AFT CARGO PIT AT BS 1307 BETWEEN STRINGERS 36L AND 36R SHEAR TIE IS CORRODED. *S/D* SHEAR TIE WAS REPLACED BY OSV TIMCO, REFERENCE SRM 51-40-02 FOR FASTENER INS - [SDR 2001UALA00093](https://openairdocs.org/sdr/2001UALA00093), Feb 8, 2001: FRAME. CORRODED. AFT CARGO PIT AT BS 1197 FROM RBL 13-19, FRAME CAP IS CORRODED. *S/D* FRAME T-CAP WAS REPLACED BY OSV TIMCO, REFRENCE 51-40-02 FOR FASTENER INSTALLATION PROCEDU - [SDR 2001UALA00092](https://openairdocs.org/sdr/2001UALA00092), Feb 7, 2001: SKIN PANEL. CORRODED. EXTERIOR FUSELAGE VHF RIGHT ANTENNA SKIN CUTOUT CORRODED STATION 510 BL 0. *S/D* SKIN REPAIRED PER SRM 53-30-01 AT OSV TIMCO. - [SDR 99UAL900211](https://openairdocs.org/sdr/99UAL900211), Apr 14, 1999: HEAT TAPE. FAILED. FLIGHT ATTENDANT REPORTED SMOKE IN CABIN/COCKPIT AREA, NOTIFIED MAINTENANCE. *S/D* HEATER TAPE B109 FAILED CAUSING INSULATION ON FORWARD GALLEY CHILLER DUCT TO - [SDR 98UAL900545](https://openairdocs.org/sdr/98UAL900545), Nov 15, 1998: BATTERY PACK. DISCHARGED. LEFT EMERGENCY ESCAPE LIGHT DOES NOT COME ON WHEN TEST 1 BUTTON IS PUSHED. BATTERY PACK WAS REPLACED. PROBLEM WAS CORRECTED. - [SDR 98UAL900267](https://openairdocs.org/sdr/98UAL900267), Jun 17, 1998: SEAL. MISINSTALLED. RIGHT OVERWING HATCH MAJOR AIR LEAK. UNABLE TO MAINTAIN CABIN PRESSURIZATION. RETURNED TO SFO. *S/D* FOUND DOOR SEAL AT RIGHT OVERWING EXIT DOOR TO BE INSTALLED - [SDR 98UAL900227](https://openairdocs.org/sdr/98UAL900227), May 31, 1998: SQUIB. FAILED. NR 1 SQUIBB WILL NOT TEST FOR THE LEFT OVERWING EXIT. - [SDR 96UAL900864](https://openairdocs.org/sdr/96UAL900864), Nov 12, 1996: HEATER. MALFUNCTIONED. DIVERTED TO ORD DUE TO AN ELECTRICAL ODOR IN THE COCKPIT. *S/D* THE FIRST OFFICER'S SHOULDER HEATER OVERHEATED. THE HEATER WAS REPLACED, OPERATIONS CHECK NORMAL - [SDR 96UAL900862](https://openairdocs.org/sdr/96UAL900862), Nov 12, 1996: HEATER. MALFUNCTIONED. DIVERTED TO DEN UNDER AMBER ALERT WITH SMOKE IN THE COCKPIT. *S/D* THE FIRST OFFICER'S SHOULDER HEATER OVERHEATED. THE HEATER WAS REPLACED, OPERATIONS CHECK NOR - [SDR 96UAL900658](https://openairdocs.org/sdr/96UAL900658), Aug 27, 1996: COMPRESSOR. STALLED. ON LANDING ROLL-OUT. THE RIGHT ENGINE HAD A COMPRESSOR STALL WHILE COMING OUT OF REVERSE THRUST. ENGINE EXCEEDED EXHAUST GAS TEMPERATURE LIMIT AND WAS IMMEDIATE - [SDR 96UAL900422](https://openairdocs.org/sdr/96UAL900422), Jun 7, 1996: FIRE WARNING. ACTIVATED. CREW REPORTED APU AUTO SHUT DOWN AND FIRE WARNING. FLIGHT CREW DISCHARGED THE FIRE BOTTLE. SUPPLEMENTAL DATA UPDATE: REPLACED APU FIRE BOTTLE AND SQUIBB PER MM - [SDR 96UAL900179](https://openairdocs.org/sdr/96UAL900179), Mar 11, 1996: BATTERY PACK. DISCHARGED. THREE EXTERIOR EMERGENCY LIGHTS ON RIGHT SIDE INOP. TWO OVER THE WING AND ONE BY THE RIGHT FORWARD ENTRY DOOR. REPLACED BATTERY PACK. - [SDR 96UAL900178](https://openairdocs.org/sdr/96UAL900178), Mar 11, 1996: AUTO BUSS. MALFUNCTIONED. RIGHT AC AUTO BUS TIE DID NOT PICK UP LOAD WHEN RIGHT GENERATOR TRIPPED. AT CRUISE TRIED TURNING OFF RIGHT BUS WITH APU GEN ON LINE. RIGHT BUS TIE BREAKER WOULD - [SDR 95UAL900103](https://openairdocs.org/sdr/95UAL900103), Aug 21, 1995: EEL CONNECTOR. INOP. EMERGENCY EEL LIGHT INOP, RIGHT FWD AISLE. REPLACED POWER STRIP CONNECTOR, CHECKS NORMAL. ## FAA accident and incident reports (1) From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [Incident 19841027066599I](https://openairdocs.org/incident/19841027066599I), Oct 27, 1984: Boeing 767222 (N618UA), Chicago, IL. Lost automatic cabin pressure control. Diverted to O'Hare. Out flow valve gearbox replaced. --- 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.