# N615UA: 1983 Boeing 767-222, registration cancelled 2018-05-30 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: May 30, 2018 - Status when cancelled: Sale reported, canceled - 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: 21876 - Year built: 1983 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: March 9, 1983 - Last registry action: June 19, 2017 - Mode S code: A80314 - Location: Ealing London, United Kingdom - Owner type: Individual - The mark today: https://openairdocs.org/aircraft/N615UA - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=615UA - Page: https://openairdocs.org/deregistered/N615UA-2018-05-30 From the FAA registry file of November 12, 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 (43) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR 2003UALA00708](https://openairdocs.org/sdr/2003UALA00708), Sep 21, 2003: OIL COOLER. FAILED. DIVERTED TO SYR DUE TO NR 1 ENGINE OIL PRESSURE INDICATION. REPLACED OIL COOLER. SHOP TEST CONFIRMED OIL COOLER MATRIX LEAKING INTERNALLY, ALLOWING FUEL TO CONT - [SDR 2003UALA00398](https://openairdocs.org/sdr/2003UALA00398), May 21, 2003: WIRE. LOOSE. EMERGENCY EXIT LIGHTS FROM SEAT 26F AFT TO AFT GALLEY INOP. SUPPLEMENTAL DATA UPDATE SECURED LOOSE LEAD WIRE CONNECTORS AT EEL. - [SDR 2003UALA00416](https://openairdocs.org/sdr/2003UALA00416), May 6, 2003: WARNING LIGHT. ILLUMINATED. A/C RECEIVED LEFT GENERATOR DRIVE LIGHT INDICATION. DISCONNECTED IDG AND FELT VIBRATION. REMOVED AND REPLACE THE LEFT IDG. SHOP FINDINGS SHOW THAT THE UNIT HAD - [SDR 2003UALA00027](https://openairdocs.org/sdr/2003UALA00027), Jan 6, 2003: BEARING. FAILED. AIRCRAFT LOST NR 4 RIGHT AFT MLG WHEEL. RETURNED TO FIELD. WHEEL LOSS BELIEVED DUE TO BEARING FAILURE. INSPECTION OF RECOVERED PARTS REFLECT LACK OF LUBRICATION - [SDR 2002UALA01842](https://openairdocs.org/sdr/2002UALA01842), Dec 9, 2002: FUEL CONTROL. FAILED. LOSS OF POWER TO NR 2 ENGINE. ENGINE RESTARTED. ENGINE WOULD NOT GO ABOVE IDLE. FCU CHANGED. BENCH CHECK SHOWED ACCEL & DECEL SCHEDULE UNDER LOW LIMITS, PROBABL - [SDR 2002UALA01629](https://openairdocs.org/sdr/2002UALA01629), Oct 24, 2002: PUMP. FLUCTUATES. FROM TAKE OFF TO ABOUT 6000 FT AT REDUCED CLIMB THRUST, NR 1 ENGINE FLUCTUATED ABOUT 4 PERCENT (N1). STABILIZED AFTER THAT. SUPPLEMENTAL DATA UPDATE FUEL CONTRO - [SDR 2002UALA01300](https://openairdocs.org/sdr/2002UALA01300), Aug 12, 2002: BEARING. FAILED. RIGHT ENGINE OIL FILTER MESSAGE DISPLAYED. RIGHT ENGINE SHUTDOWN BEFORE LANDING. FAILURE OF THE NUMBER THREE BEARING. ENGINE WAS 85 HOURS TSO. FAILURE BEING INV - [SDR 2001UALA02287](https://openairdocs.org/sdr/2001UALA02287), Nov 14, 2001: ACTUATOR. FAILED. CAPTAIN CONTACTED DISPATCH ON APPROACH TO SFO WITH A LEFT MAIN GEAR UNSAFE INDICATION. FLIGHT LANDED SAFELY. LEFT MLG RETRACT ACTUATOR PISTON HAD TENSILE FAILUR - [SDR 2001UALA01976](https://openairdocs.org/sdr/2001UALA01976), Aug 31, 2001: CONTROL UNIT. FAULTY. RETURNED TO SFO DUE RUDDER TRIM ANOMALY. REPLACED AILERON AND RUDDER TRIM CONTROL. OPERATIONALLY CHECKED RUDDER SYSTEM PER APPLICABLE MAINTENANCE MANUAL. ALL OP - [SDR 2001UALA01723](https://openairdocs.org/sdr/2001UALA01723), Aug 15, 2001: BEARING. SEIZED. RUDDER PEDALS EXTREMELY STIFF DURING APPROACH AND LANDING AFTER FIVE AND A HALF HOUR FLIGHT. SUPPLEMENTAL DATA UPDATE CAUSE: A SEIZED CAM BEARING IN THE RUDDER - [SDR 2001UALA00992](https://openairdocs.org/sdr/2001UALA00992), Jun 23, 2001: CHARGER. FAILED. ALL EEL AND EMERGENCY LIGHTS ILLUMINATED AFT OF ROW 27 WITH EMERGENCY LIGHT SWITCH IN AUTO. UNABLE TO EXTINGUISH LIGHTS EXCEPT BY PLACING EMERGENCY LIGHT SWITCH - [SDR 2001UALA01074](https://openairdocs.org/sdr/2001UALA01074), Jun 15, 2001: FLOORBEAM. CORRODED. AFT CARGO PIT BS 1175 UNDER T-CAP FROM LBL 30-RBL 45, BOTH SIDES OF WEB CORRODED UNDER NUT PLATES. MAJOR REPAIR ACCOMPLISHED. REPLACED T-CAP PER SRM 53-00-51, B - [SDR 2001UALA01073](https://openairdocs.org/sdr/2001UALA01073), Jun 15, 2001: STRINGER. CORRODED. AFT BULK PIT AT BS 1540 - 1562, STRINGER 39L IS CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED STRINGER SECTION AND SPLICE PER SRM 53-00-03 AND INSTALLED PER S - [SDR 2001UALA01072](https://openairdocs.org/sdr/2001UALA01072), Jun 15, 2001: SPLICE. CORRODED. FWD CARGO PIT AT BS 434 STRINGER 32L, SPLICE FITTING IS CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED NEW SPLICE PER BAC DRAWING 140T0115 AND INSTALLED PER SR - [SDR 2001UALA01071](https://openairdocs.org/sdr/2001UALA01071), Jun 15, 2001: FRAME. CORRODED. AFT CARGO PIT AT BS 1263 AT RBL 20-35, FRAME T-CAP IS CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED NEW T-CAP SECTION PER BAC DRAWING 146T1060 AND INSTALLED P - [SDR 2001UALA01070](https://openairdocs.org/sdr/2001UALA01070), Jun 15, 2001: STRINGER CLIP. DAMAGED. STA 434 STR 39L ELONGATED HOLE IN STRINGER CLIP. MAJOR REPAIR ACCOMPLISHED. REPLACED STRINGER CLIP PER BAC DRAWING 140T2101 AND INSTALLED PER SRM 51-40-2. - [SDR 2001UALA01069](https://openairdocs.org/sdr/2001UALA01069), Jun 15, 2001: ATTACH ANGLE. CORRODED. CABIN BS 1263, STR 12R STRINGER ATTACH ANGLE HAS CORROSION. MAJOR REPAIR ACCOMPLISHED. FABRICATED NEW CLIP PER BAC DRAWING 140T2101 AND INSTALLED PER SRM 51-40- - [SDR 2001UALA01068](https://openairdocs.org/sdr/2001UALA01068), Jun 15, 2001: FRAME. CORRODED. AFT CARGO PIT AT BS 1263 AT RBL 20-35, FRAME T-CAP IS CORRODED. MAJOR REPAIR ACCOMPLISHED. REPLACED T-CAP SECTION PER BAC DRAWING 146T1060 AND INSTALLED PER SRM - [SDR 2001UALA01067](https://openairdocs.org/sdr/2001UALA01067), Jun 15, 2001: FLOORBEAM. CORRODED. FWD PIT STA 544, LBL 20, T-CAP CORRODED. MAJOR REPAIR ACCOMPLISHED. REPAIRED T-CAP PER SRM 53-30-07, FIG 1. - [SDR 2001UALA01066](https://openairdocs.org/sdr/2001UALA01066), Jun 15, 2001: FLOORBEAM. CORRODED. AFT CARGO PIT BS 1175 UNDER T-CAP FROM LBL 30 TO RBL 45, BOTH SIDES OF BS 1175 WEB CORRODED. MAJOR REPAIR ACCOMPLISHED. REPLACED T-CAP PER SRM 53-00-51 AND 51-4 - [SDR 2001UALA01014](https://openairdocs.org/sdr/2001UALA01014), Jun 11, 2001: FLOORBEAM. CORRODED. AFT CARGO PIT AT BS 1285, LBL 45-RBL 45, FRAME T-CAP IS CORRODED. - [SDR 2001UALA00996](https://openairdocs.org/sdr/2001UALA00996), Jun 11, 2001: FRAME. CORRODED. AFT CARGO PIT AT BS 1285, LBL 45-RBL 45, FRAME T-CAP IS CORRODED. - [SDR 2001UALA01013](https://openairdocs.org/sdr/2001UALA01013), Jun 8, 2001: FLOORBEAM. CORRODED. PIT FLOOR T CAP CORRODED BS 1153 RBL 45-LBL 45. - [SDR 2001UALA01007](https://openairdocs.org/sdr/2001UALA01007), Jun 8, 2001: SPLICE. CORRODED. FWD PIT STR SPLICE CORRODED BS 434 STR 39R. - [SDR 2001UALA01006](https://openairdocs.org/sdr/2001UALA01006), Jun 8, 2001: STRINGER. GOUGED. PIT STRINGER GAUGED BS 434-456 STR 39L. - [SDR 2001UALA01005](https://openairdocs.org/sdr/2001UALA01005), Jun 8, 2001: STRINGER. CORRODED. STR CORRODED BS 1540-1562 STR 39R. - [SDR 2001UALA01004](https://openairdocs.org/sdr/2001UALA01004), Jun 8, 2001: SPLICE. CORRODED. STR SPLICE FITTING CORRODED BS 434 STR 35L. - [SDR 2001UALA01003](https://openairdocs.org/sdr/2001UALA01003), Jun 8, 2001: STRINGER. CRACKED. STR CRACKED BS 434 STR 39R. - [SDR 2001UALA01002](https://openairdocs.org/sdr/2001UALA01002), Jun 8, 2001: SPLICE. CORRODED. STRINGER SPLICE FITTING CORRODED BS 434 STR 39L. - [SDR 2001UALA01001](https://openairdocs.org/sdr/2001UALA01001), Jun 8, 2001: SHEAR TIE. CORRODED. SHEARTIE CORRODED BS 368 STR 38R-39R. - [SDR 2001UALA00995](https://openairdocs.org/sdr/2001UALA00995), Jun 8, 2001: STRINGER. CRACKED. STR CRACKED BS 434 STR 39R. - [SDR 2001UALA00994](https://openairdocs.org/sdr/2001UALA00994), Jun 8, 2001: SPLICE. CORRODED. STR SPLICE FITTING CORRODED BS 434 STR 35L. - [SDR 2001UALA01039](https://openairdocs.org/sdr/2001UALA01039), Jun 6, 2001: STRINGER. CORRODED. BS 355 STR 39L CORRODED. - [SDR 2001UALA00818](https://openairdocs.org/sdr/2001UALA00818), May 24, 2001: SHEAR TIE. CORRODED. BS 434 STRINGER 37L - 38L SHEAR TIE CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH BAC DRAWINGS 140T2102 AND 143T1001. - [SDR 2001UALA00817](https://openairdocs.org/sdr/2001UALA00817), May 24, 2001: FRAME. CORRODED. BS 1241 LBL 45 - RBL 45 FRAME T-CAP CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH SRM 51-40-02 AND BAC DRAWINGS 141T10 - [SDR 2001UALA00091](https://openairdocs.org/sdr/2001UALA00091), Feb 7, 2001: BATTERY PACK. DISCHARGED. RIGHT SIDE EEL LIGHTS ON WITH OVERHEAD SWITCH IN THE ARM POSITION. *S/D* ADJUSTED EMERGENCY LIGHT MICROSWITCH ON OVERHEAD PANEL. CHECKED 28VDC CHARGING VOLTAGE - [SDR 2001UALA00089](https://openairdocs.org/sdr/2001UALA00089), Feb 6, 2001: SWITCH. STUCK. ON CLIMBOUT OF JFK, EMERGENCY SIGN LIGHTS ON, ON RIGHT SIDE OF FIRST AND BUSINESS CLASS. *S/D* FOUND FLIGHT ATTENDANT EMERGENCY LIGHT TEST SWITCH STUCK. CYCLED - [SDR 2001UALA00087](https://openairdocs.org/sdr/2001UALA00087), Feb 6, 2001: LIGHT. INTERMITTENT. RIGHT HAND FORWARD CABIN EEL LIGHTS COMES ON INTERMITTENTLY WITH SWITCH IN ARM POSITION. - [SDR 2000UALA00718](https://openairdocs.org/sdr/2000UALA00718), Nov 28, 2000: GEAR. WORN. L/E SLAT ASYM DURING FLAP EXTENTION ON APPROACH. *S/D* THE RIGHT WING SLATS DID NOT MOVE TO THE COMMANDED POSITION DUE TO A SEVERELY WORN OUTBOARD LEADING EDGE - [SDR 99UAL900490](https://openairdocs.org/sdr/99UAL900490), Sep 23, 1999: ENERTAINMENT SYS. FAILED. ELECTRICAL SMELL IN MID CABIN ROW 10-11 READING LIGHTS AND ENTERTAINMENT SYSTEM NOT ACCEPTING COMMANDS NORMALLY. *S/D* FOUND SEAT ELECTRONIC BOX AT SEAT 9 E, F - [SDR 99UAL900321](https://openairdocs.org/sdr/99UAL900321), Jun 13, 1999: BLEED CONTROL. MALFUNCTIONED. ON TAKEOFF, NR 2 ENGINE SUSTAINED TWO SHORT COMPRESSOR STALLS. SURGE CHECKS WERE ACCOMPLISHED REFERENCE MAINTENANCE MANUAL. THE ENGINE VANE BLEED CONTROL WOULD - [SDR 97UAL900058](https://openairdocs.org/sdr/97UAL900058), Jan 11, 1997: CONNECTOR. FAILED. AILERON LOCKOUT LIGHT APPEARED DURING CLIMB AT APPROXIMATELY 300 KNOTS. THE AIRCRAFT CONTINUED TO JFK. FOUND SHORT AT LEFT AILERON ACTUATOR CONNECTOR. REPLACED - [SDR 95UAL900111](https://openairdocs.org/sdr/95UAL900111), Aug 28, 1995: HYD PUMP. FAILED. RETURNED TO FIELD UNDER AMBER ALERT WITH NR TWO SYSTEM HYDRAULIC FAILURE. FOUND ENGINE DRIVEN PUMP FAILED. REPLACED PUMP. CHECKS O.K. ## FAA accident and incident reports (2) 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 20030921031749I](https://openairdocs.org/incident/20030921031749I), Sep 21, 2003: Boeing 767222 (N615UA), Syracuse, NY. (-23) On 9/21/03 at 1438 eastern standard time, united flight #4, a B767-222, N615UA, serial #21876, enroute from lax to jfk diverted to syr (Syracuse, NY) due… - [Incident 19860203003509I](https://openairdocs.org/incident/19860203003509I), Feb 3, 1986: Boeing 767222 (N615UA), Las Vegas, NV, Substantial damage. Oil filter light, fire warning left engine, bottles discharged. Safe diversion. Fire damage, angle gear box failed. --- 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, except the copies of manufacturers’ service documents, which belong to their rights holders.