# N614UA: 1983 Boeing 767-222, registration cancelled 2018-01-05 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: January 5, 2018 - Status when cancelled: Registration expired, pending cancellation - 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: 21875 - Year built: 1983 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: March 1, 1983 - Certificate issued: September 26, 2011 - Last registry action: September 26, 2011 - Mode S code: A7FF5D - Owner when cancelled: [Boeing Co](https://openairdocs.org/faa-owner/BOEING%20CO) - Location: [Wichita, KS](https://openairdocs.org/faa-place/KS/Wichita) - Owner type: Corporation - Owner's area on the map: 37.6429° N, 97.2101° W: Placed by OpenAirDocs at the center of ZIP code 67210, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N614UA - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=614UA - Page: https://openairdocs.org/deregistered/N614UA-2018-01-05 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 (65, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR USAA050729](https://openairdocs.org/sdr/USAA050729), May 21, 2005: INTERCOSTAL. CORRODED. BFM - C4- INTERCOSTAL UPPER CHORD, 20 INCHES L X 1 INCH W X .008 INCH D, CORROSION; LEVEL 1; TASK C53-252-03; CABIN FLOOR BS 1661-1680, RBL 10. FAB NEW INTERCOS - [SDR 2002UALA00131](https://openairdocs.org/sdr/2002UALA00131), Jan 20, 2002: WARNING SYSTEM. MALFUNCTIONED. CREW HEARD LOUD THUMPING ON LEFT SIDE OF AIRCRAFT, AND HAD L/E SLAT DISAGREE LIGHT ILLUMINATE. DIVERTED TO SLC. NUISANCE EICAS MESSAGE GENERATED BY PROXIMITY SW - [SDR 2002UALA00138](https://openairdocs.org/sdr/2002UALA00138), Jan 20, 2002: WARNING SYSTEM. ACTIVATED. EICAS MESSAGE LEADING EDGE SLAT DISAGREE DISPLAYED INTERMITTANTLY ALONG WITH CAUTION LIGHT ILLUMINATED. FLIGHT DIVERTED TO SLC. - [SDR 2001UALA01454](https://openairdocs.org/sdr/2001UALA01454), Jul 19, 2001: ENGINE. MALFUNCTIONED. WHILE CRUISE FL 410 FOR WEATHER, AVOIDING EXPECTED LIGHT-MOD CHOP. LIGHT PRECIP W-IGNITION CON. LT ENG LOSS THRUST . ENGINE RELIT DURING DESCENT TO FL 310 ON IT - [SDR 2001UALA00929](https://openairdocs.org/sdr/2001UALA00929), May 28, 2001: CONTROL CABLE. OUT OF RIG. ENG LOW THRUST OTHER THAN TAKEOFF. FAULT CODED. L ENG EPR.04. (MCT-CLB FROM FL350 TO FL390 WITH THRUST LEVER FIREWALL. REPLACED TRANSDUCER AND RIGGED THRUST CON - [SDR 2001UALA00812](https://openairdocs.org/sdr/2001UALA00812), May 22, 2001: SMOKE. MALFUNCTIONED. OVEN SMOKING. - [SDR 2001UALA00993](https://openairdocs.org/sdr/2001UALA00993), May 8, 2001: BATTERY PACK. FAULTY. EMERGENCY LIGHTS COMING ON IN AFT PART OF CABIN AFTER LANDING DURING TAXI IN. *S/D* BATTERY PACK ON ORDER FROM CHICAGO OSTF NR A1551 FLT 121 AT 1039. PACK LOCAT - [SDR 2001UALA00537](https://openairdocs.org/sdr/2001UALA00537), Apr 17, 2001: STRINGER. CRACKED. BS 1065 TO 1087 STRINGER CRACKED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH SRM 51-40-02 AND 53-00-03. - [SDR 2001UALA00536](https://openairdocs.org/sdr/2001UALA00536), Apr 17, 2001: SHEAR TIE. CORRODED. BS 368 STRINGERS 37L TO 38L SHEAR TIE CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH BAC DRAWING 141T1221. - [SDR 2001UALA00535](https://openairdocs.org/sdr/2001UALA00535), Apr 17, 2001: FRAME. DAMAGED. BS 390 FRAME T-CAP HAS DOUBLE DRILLED HOLE AT LBL 29. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH 53-00-07 FIGURE 204. - [SDR 2001UALA00534](https://openairdocs.org/sdr/2001UALA00534), Apr 17, 2001: STRINGER CLIP. CORRODED. STATION 355 STRINGER 38L STRINGER CLIP CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH SRM 51-40-02 AND GN/MM 1-0-0-23. - [SDR 2001UALA00533](https://openairdocs.org/sdr/2001UALA00533), Apr 17, 2001: STRINGER CLIP. CORRODED. STATION 355 STRINGER 37L STRINGER CLIP IS CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH SRM 51-40-02 AND GN/MM 1-0-0-2 - [SDR 2001UALA00532](https://openairdocs.org/sdr/2001UALA00532), Apr 17, 2001: SHEAR TIE. CORRODED. BS STRINGER 35L TO 37L SHEAR TIE CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH BAC DRAWING 146T8511 AND SRM 51-40-02. - [SDR 2001UALA00531](https://openairdocs.org/sdr/2001UALA00531), Apr 17, 2001: SHEAR TIE. CORRODED. STATION 355 STRINGERS 35L TO 34L SHEAR TIE CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH BAC DRAWING 141T1221 AND SRM - [SDR 2001UALA00530](https://openairdocs.org/sdr/2001UALA00530), Apr 17, 2001: FLOORBEAM. CORRODED. FLOORBEAM CORRODED UNDER MID GALLEY STATION 824 RBL 8. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH SRM 53-00-51. - [SDR 2001UALA00529](https://openairdocs.org/sdr/2001UALA00529), Apr 17, 2001: DOOR FRAME. CORRODED. BULK PIT DOOR SILL UPPER CHORD CORRODED ON INBOARD LEG STATION 1417 TO 1424 ABOVE STRINGERS 32L TO 33L. MAJOR REPAIR ACCOMPLISHEDFABRICATED AND INSTALLED REPAIR - [SDR 2001UALA00528](https://openairdocs.org/sdr/2001UALA00528), Apr 17, 2001: STRAP. CORRODED. FAIL SAFE STRAP BS 1270 TO 1370 RBL 90.5 CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH BAC DRAWING 146T8511 AND SRM 51 - [SDR 2001UALA00526](https://openairdocs.org/sdr/2001UALA00526), Apr 16, 2001: STRINGER CLIP. DAMAGED. FORWARD PIT STATION 478, STRINGER CLIP HAS OBLONG HOLES. MAJOR REPAIR ACCOMPLISHED. REPLACED CLIP PER BOEING DRAWING 140T2101. - [SDR 2001UALA00514](https://openairdocs.org/sdr/2001UALA00514), Apr 6, 2001: FRAME. CORRODED. AFT PIT FRAME STATION 1351 T-CAP CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH SRM 53-11-99 AND 51-40-01. - [SDR 2001UALA00448](https://openairdocs.org/sdr/2001UALA00448), Apr 6, 2001: FRAME. CORRODED. AFT PIT BS 1285 FRAME T-CAP AT LBL 12-33 T-CAP IS CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH SRM 51-40-02 AND BAC D - [SDR 2001UALA00449](https://openairdocs.org/sdr/2001UALA00449), Apr 5, 2001: FRAME. CORRODED. AFT PIT AT BS 1175 BODY LINE 0 RBL 25 FRAME T-CAP HAS AREAS OF CORROSION. MAJOR REPAIR ACCOMPLISHED.FABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH SRM 51-40 - [SDR 2001UALA00409](https://openairdocs.org/sdr/2001UALA00409), Mar 31, 2001: SPLICE. CORRODED. FORWARD PIT STA. 434 STRINGER 35R SPLICE HAS CORROSION. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW SPLICE PER SRM 51-40-02 AND BOEING DWG 140T0115. - [SDR 2001UALA00408](https://openairdocs.org/sdr/2001UALA00408), Mar 31, 2001: STRINGER. CORRODED. FORWARD PIT STRINGER 37R BETWEEN STA. 412 AND 434 HAS CORROSION. MAJOR REPAIR ACCOMPLISHED. INSTALLED STRINGER SPLICE SRM 53-10-03 FIGURE 201, BOEING DWG 140T01 - [SDR 2001UALA00407](https://openairdocs.org/sdr/2001UALA00407), Mar 31, 2001: STRINGER. CRACKED. AFT CARGO PIT AT STA. 1065 - 1087 STRINGER 33L IS CRACKED UNDER END FITTING RADIUS. MAJOR REPAIR ACCOMPLISHED. SPLICED IN NEW SECTION OF STRINGER PER SRM 51-20- - [SDR 2001UALA00406](https://openairdocs.org/sdr/2001UALA00406), Mar 31, 2001: FLOORBEAM. CORRODED. AFT PIT STA. 1219 FLOOR FRAME T-CAP HAS AREAS OF CORROSION FROM BL0 - LBL 46 ON UPPER AND LOWER FLANGES. MAJOR REPAIR ACCOMPLISHED. REPLACED UPPER T-CAP PER BOE - [SDR 2001UALA00405](https://openairdocs.org/sdr/2001UALA00405), Mar 31, 2001: SHEAR TIE. CORRODED. AFT PIT AT STA. 1395 STRINGERS 38L & 39L SHEAR TIE IS CORRODED. MAJOR REPAIR ACCOMPLISHED. REPLACED SHEAR TIE PER BOEING DWG 140T2102 AND SRM 51-40-02. - [SDR 2001UALA00404](https://openairdocs.org/sdr/2001UALA00404), Mar 31, 2001: SHEAR TIE. CORRODED. AFT BULKPIT AT STA. 1417 BETWEEN STRINGERS 37L AND 38L SHEAR TIE IS CORRODED. MAJOR REPAIR ACCOMPLISHEDFABRICATED NEW SHEAR TIE PER BOEING DWG 140T2102. INSTALL - [SDR 2001UALA00355](https://openairdocs.org/sdr/2001UALA00355), Mar 28, 2001: FRAME. CORRODED. AFT CARGO PIT AT BS 1197 FRAME T-CAP HAS AREAS OF CORROSION FROM BL0 TO RBL 46. MAJOR REPAIR ACCOMPLISHEDREPLACED T-CAP DUE TO CORROSION REMOVAL OUT OF LIMITS P - [SDR 2001UALA00354](https://openairdocs.org/sdr/2001UALA00354), Mar 28, 2001: STRINGER. CRACKED. AFT CARGO PIT AT BS 1065 TO 1087, STRINGER 30R IS CRACKED UNDER END FITTING. MAJOR REPAIR ACCOMPLISHEDREPAIRED STRINGER PER SRM 53-00-03, FIG 202 AND INSTALLED - [SDR 2001UALA00353](https://openairdocs.org/sdr/2001UALA00353), Mar 28, 2001: SHEAR TIE. CORRODED. AFT CARGO PIT AT BS 1329 BETWEEN STRINGERS 38L AND 39L, SHEAR TIE IS CORRODED. MAJOR REPAIR ACCOMPLISHEDREPLACED SHEAR TIE PER SRM 51-40-02 AND BAC DWG 140T2102 - [SDR 2001UALA00351](https://openairdocs.org/sdr/2001UALA00351), Mar 28, 2001: SPLICE. CORRODED. FORWARD CARGO PIT AT BS 434, STRINGER 38L SPLICE FITTING IS CORRODED. MAJOR REPAIR ACCOMPLISHED REPLACED SPLICE AT STRINGER 38L PER SRM 51-40-02 AND BAC DWG 140 - [SDR 2001UALA00350](https://openairdocs.org/sdr/2001UALA00350), Mar 28, 2001: SHEAR TIE. CORRODED. AFT CARGO PIT AT BS 1263 BETWEEN STRINGERS 39L AND 39R, SHEAR TIE IS CORRODED. MAJOR REPAIR ACCOMPLISHEDREPLACED SHEAR TIE PER SRM 51-40-02 AND BAC DWG 140T1209 - [SDR 2001UALA00349](https://openairdocs.org/sdr/2001UALA00349), Mar 28, 2001: SHEAR TIE. CORRODED. AFT CARGO PIT AT BS 1241 BETWEEN STRINGERS 39L AND 39R, SHEAR TIE IS CORRODED. MAJOR REPAIR ACCOMPLISHEDREPLACED SHEAR TIE PER SRM 51-40-02 AND BAC DWG 140T2102 - [SDR 2001UALA00345](https://openairdocs.org/sdr/2001UALA00345), Mar 24, 2001: SHEAR TIE. CORRODED. FORWARD PIT BS 742 STRINGERS 37L - 38L SHEAR TIE CORRODED. MAJOR REPAIR ACCOMPLISHED REPLACED SHEAR TIE REF: BAC143T1214 AND SRM 51-40-02. - [SDR 2001UALA00344](https://openairdocs.org/sdr/2001UALA00344), Mar 24, 2001: FLOORBEAM. CORRODED. FORWARD PIT BS 368 RBL 35 FLOORBEAM T-CAP CORRODED. MAJOR REPAIR ACCOMPLISHED INSTALLED T-CAP REPAIR REF: SRM 53-30-07 FIGURE 201. - [SDR 2001UALA00343](https://openairdocs.org/sdr/2001UALA00343), Mar 22, 2001: SHEAR TIE. CORRODED. AFT PIT SHEAR TIE AT BS 1351 STRINGER 38L CORRODED. MAJOR REPAIR ACCOMPLISHED FABRICATED AND INSTALLED SHEAR TIE IN ACCORDANCE WITH SRM 51-20-02 AND SRM 51-40-0 - [SDR 2001UALA00342](https://openairdocs.org/sdr/2001UALA00342), Mar 22, 2001: FLOORBEAM. CORRODED. CABIN TRANSVERSE FLOORBEAM CORRODED BS 824 LBL 11. MAJOR REPAIR ACCOMPLISHED INSTALLED FLOORBEAM REPAIR REF: SRM 53-00-51. - [SDR 2001UALA00341](https://openairdocs.org/sdr/2001UALA00341), Mar 22, 2001: SHEAR TIE. CORRODED. AFT PIT BS 1329 STRINGERS 37L - 38L SHEARTIE CORRODED. MAJOR REPAIR ACCOMPLISHED REPLACED SHEARTIE REF: BAC140T2102 AND SRM 51-40-02. - [SDR 2001UALA00340](https://openairdocs.org/sdr/2001UALA00340), Mar 22, 2001: SHEAR TIE. CORRODED. AFT PIT BS 1329 STRINGERS 39L - 39R SHEARTIE CORRODED. MAJOR REPAIR ACCOMPLISHED REPLACED SHEARTIE REF: BAC146T1212 AND SRM 51-40-02. - [SDR 2001UALA00338](https://openairdocs.org/sdr/2001UALA00338), Mar 22, 2001: STIFFENER. CRACKED. CABIN FLOORBEAM BS 246 LBL 27 VERTICAL STIFFENER CRACKED. MAJOR REPAIR ACCOMPLISHED REPLACED STIFFENER REF: BAC141T5814 AND SRM 51-40-02. - [SDR 2001UALA00334](https://openairdocs.org/sdr/2001UALA00334), Mar 22, 2001: SHEAR TIE. CORRODED. AFT PIT BS 1329 STRINGERS 36L - 37L SHEAR TIE CORRODED. MAJOR REPAIR ACCOMPLISHED REPLACED SHEAR TIE REF: BAC140T2102 AND SRM 51-40-02. - [SDR 2001UALA00332](https://openairdocs.org/sdr/2001UALA00332), Mar 22, 2001: STIFFENER. CRACKED. CABIN FLOOR BEAM BS 246, RBL 66 VERTICAL STIFFINER CRACKED. MAJOR REPAIR ACCOMPLISHED REPLACED STIFFINER REF: BAC141T5814. - [SDR 2001UALA00329](https://openairdocs.org/sdr/2001UALA00329), Mar 22, 2001: ANGLE. GOUGED. AFT PIT BS 1087 STRINGER 39L FORWARD OF BULKHEAD ANGLE GOUGED. MAJOR REPAIR ACCOMPLISHED REPLACED ANGLE REF: BAC146T1074 AND SRM 51-40-02. - [SDR 2001UALA00326](https://openairdocs.org/sdr/2001UALA00326), Mar 22, 2001: SHEAR TIE. CORRODED. AFT PIT BS 1351 STRINGERS 38L - 39L SHEAR TIE CORRODED. MAJOR REPAIR ACCOMPLISHED. REPLACED SHEAR TIE REF: BAC140T2101 AND SRM 51-40-02. - [SDR 2001UALA00593](https://openairdocs.org/sdr/2001UALA00593), Mar 21, 2001: FRAME. CORRODED. AFT PIT BS 1329 LBL 8-25 FRAME T-CAP CORRODED. MAJOR REPAIR ACCOMPLISHED REPLACED T-CAP REF: BAC 146T1210 AND SRM 51-40-02. - [SDR 2001UALA00236](https://openairdocs.org/sdr/2001UALA00236), Mar 12, 2001: SHEAR TIE. CORRODED. AFT PIT BS 1285 STRI8NGERS 39L - 39R SHEAR TIE CORRODED. REPLACED SHEAR TIE PER SRM 51-40-02. - [SDR 2001UALA00235](https://openairdocs.org/sdr/2001UALA00235), Mar 12, 2001: SHEAR TIE. CORRODED. AFT PIT BS 1285 STRINGERS 36L - 37L SHEAR TIE CORRODED. REPLACED SHEAR TIE PER SRM 51-40-02. - [SDR 2001UALA00234](https://openairdocs.org/sdr/2001UALA00234), Mar 12, 2001: SHEAR TIE. CORRODED. AFT PIT BS 1307 STRINGERS 37L - 38L SHEAR TIE CORRODED. REPLACED SHEAR TIE PER SRM 51-40-02. - [SDR 2001UALA00233](https://openairdocs.org/sdr/2001UALA00233), Mar 12, 2001: SHEAR TIE. CORRODED. AFT PIT BS 1285 STRINGERS 37L - 38L SHEAR TIE CORRODED. REPLACED SHEAR TIE PER SRM 51-40-02. - [SDR 2001UALA00081](https://openairdocs.org/sdr/2001UALA00081), Feb 3, 2001: CART. SHORTED. ENTRY CART 300 IN MID-GALLEY SPARKED WHEN PLUGGED IN AND THE 60 AMP AC CB POPPED. OK AT FIRST SERVICE OF FLIGHT. LEFT UNPLUGGED AND DID NOT RESET. *S/D* CART CO All 65: https://openairdocs.org/deregistered/N614UA-2018-01-05/reports.md ## FAA accident and incident reports (4) 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 19850228017859I](https://openairdocs.org/incident/19850228017859I), Feb 28, 1985: Boeing 767222 (N614UA), Salt Lake City, UT. Smoke from coffee maker, halon used. Found coffee maker overheated due to lack of water, bypass valve found open. - [Incident 19841101066569I](https://openairdocs.org/incident/19841101066569I), Nov 1, 1984: Boeing 767222 (N614UA), Los Angeles, CA, Minor damage. While being towed aircraft was struck by N93106. Damage to aileron, wingtip and leading edge. - [Incident 19840430022689I](https://openairdocs.org/incident/19840430022689I), Apr 30, 1984: Boeing 767 (N614UA), Chicago, IL. Encountered severe turbulence on climbout. Returned. Checked for damage. No reported injuries. - [Incident 19830325020099I](https://openairdocs.org/incident/19830325020099I), Mar 25, 1983: Boeing 767222 (N614UA), San Diego, CA. On rollout forward entrance door started to open. Escape slide deployed. Door handles out of riggings and sequence. --- 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.