# N387UA: 1990 Boeing 737-322, registration cancelled 2005-07-28 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: July 28, 2005 - Exported to: Jordan - Status when cancelled: Valid registration - Airframe: [Boeing 737-322](https://openairdocs.org/model/boeing-737-322) (registry code 138447Y) - Engine: [CFM International CFM56 series](https://openairdocs.org/engine/cfm-international-cfm56-series) (registry code 13802) - Data sheets: [TCDS A16WE](https://openairdocs.org/tcds/A16WE) (OpenAirDocs) - Serial number: 24662 - Year built: 1990 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: May 22, 1990 - Certificate issued: July 22, 2005 - Last registry action: July 22, 2005 - Mode S code: A4770E - Owner when cancelled: [C I T Leasing Corp](https://openairdocs.org/faa-owner/C%20I%20T%20LEASING%20CORP) - Location: [New York, NY](https://openairdocs.org/faa-place/NY/New%20York) - Owner type: Corporation - Owner's area on the map: 40.7598° N, 73.9907° W: Placed by OpenAirDocs at the center of ZIP code 10036, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N387UA - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=387UA - Page: https://openairdocs.org/deregistered/N387UA-2005-07-28 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 737-322: https://openairdocs.org/model/boeing-737-322.md ## Service difficulty reports (28) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR DU4R0507132](https://openairdocs.org/sdr/DU4R0507132), Jun 30, 2005: SKIN. DENTED. BS 1024, S-6L-S-7L HAS A DENT WIDTH 1.5 INCH X .070 DEPTH. - [SDR DU4R0507131](https://openairdocs.org/sdr/DU4R0507131), Jun 30, 2005: SKIN. MISREPAIRED. FUSELAGE RT SIDE BS 927-945.5 S-21R-22R HAS PREVIOUS REPAIR THAT ENDS ON A STRINGER. - [SDR DU4R0507130](https://openairdocs.org/sdr/DU4R0507130), Jun 30, 2005: SKIN. MISREPAIRED. FUSELAGE LT SIDE BS 927-945.5 S-19L- 20L HAS PREVIOUS REPAIR THAT ENDS ON A LAP SEAM. - [SDR DU4R0507128](https://openairdocs.org/sdr/DU4R0507128), Jun 30, 2005: SKIN. CRACKED. DL/H UPPER FUSELAGE SKIN S-7L HAS 1 EA. CHERRY MAX RIVET FS 420. S/O NR 134005, OPS NR 20347. - [SDR DU4R0507003](https://openairdocs.org/sdr/DU4R0507003), Jun 30, 2005: SKIN. DENTED. DENT AND CREASE IN LOWER FUSELAGE SKIN AT BS 907 BETWEEN S-25R - S-26R. - [SDR DU4R0507126](https://openairdocs.org/sdr/DU4R0507126), Jun 30, 2005: STRINGER. CRACKED. CABIN S-15L CRACKED, ALSO END FITTING. - [SDR 20050622A](https://openairdocs.org/sdr/20050622A), Jun 2, 2005: SKIN. DENTED. DENT IN THE LT FUSELAGE SKIN IN AREA OF S20L AT BS 465. - [SDR 2004UALA00405](https://openairdocs.org/sdr/2004UALA00405), Apr 26, 2004: BEAR STRAP. CORRODED. AFT CARGO DOOR CUT OUT AFT SIDE BEAR STRAP HAD CORROSION AND GOUGES. DOUBLER/TRIPLER INSTALLED. - [SDR 2004UALA00404](https://openairdocs.org/sdr/2004UALA00404), Apr 26, 2004: SKIN. DENTED. L/E HORIZ STAB LE IS DENTED AT LE STA 115. TRIMED OUT DAMAGE, INSTALLED INTERNAL DOUBLER AND FILLER. - [SDR 2004UALA00407](https://openairdocs.org/sdr/2004UALA00407), Apr 23, 2004: FITTING. CRACKED. THE LT MLG BEAM O/B FITTING WAS FOUND CRACKED BEYOND LIMITS. FITTING WAS REPLACED. - [SDR 2004UALA00384](https://openairdocs.org/sdr/2004UALA00384), Apr 20, 2004: INTERCOSTAL. CRACKED. CABIN L1 DOOR SURROUND STRUCTURE INTERCOSTAL WEB CRACKED AT BS 294.5 STR 7L. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED NEW INTERCOSTAL. - [SDR 2004UALA00383](https://openairdocs.org/sdr/2004UALA00383), Apr 20, 2004: INTERCOSTAL. CRACKED. CABIN R1 DOOR SURROUND STRUCTURE INTERCOSTAL ANGLE HAS A CRACK AT BS 291 BETWEEN STR 9R AND 10R. MAJOR REPAIR ACCOMPLISHED. INSTALLED REPAIR ANGLE. - [SDR 2004UALA00382](https://openairdocs.org/sdr/2004UALA00382), Apr 20, 2004: INTERCOSTAL. CRACKED. CABIN R1 DOOR SURROUND STRUCTURE INTERCOSTAL ANGLE HAS A CRACK AT BS 291 BETWEEN STR 13R AND 14R. MAJOR REPAIR ACCOMPLISHED. INSTALLED REPAIR ANGLE. - [SDR 2004UALA00381](https://openairdocs.org/sdr/2004UALA00381), Apr 20, 2004: STRINGER CLIP. CRACKED. CABIN FUSELAGE FRAME CLIP CRACKED AT BS 400 STRINGER 4L. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED STRINGER CLIP. - [SDR 2004UALA00380](https://openairdocs.org/sdr/2004UALA00380), Apr 20, 2004: STRINGER CLIP. CRACKED. LT SIDE CABIN STRINGER TIE BRACKET CRACKED AT BS616 STR 4L. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED STRINGER CLIP. - [SDR 2004UALA00379](https://openairdocs.org/sdr/2004UALA00379), Apr 20, 2004: STRINGER CLIP. CRACKED. LT SIDE CABIN STRINGER TIE BRACKET CRACKED AT BS639 AND STRINGER 4L MAJOR REPAIR ACCOMPLISHED. FABRICATED NEW CLIP. - [SDR 2004UALA00347](https://openairdocs.org/sdr/2004UALA00347), Apr 13, 2004: FRAME. CRACKED. FUSELAGE FRAME IS CRACKED AT STA 616 BELOW STR 17L. MAJOR REPAIR ACCOMPLISHED. INSTALLED ANGLE DOUBLER REPAIR. - [SDR 2004UALA00344](https://openairdocs.org/sdr/2004UALA00344), Apr 13, 2004: STRINGER. CRACKED. STR 15L IS CRACKED AT STA 380. MAJOR REPAIR ACCOMPLISHED. SPLICE REPAIR. - [SDR 2004UALA00316](https://openairdocs.org/sdr/2004UALA00316), Apr 7, 2004: PRESSURE PANEL. CRACKED. WHEEL WELL PRESSURE DECK IS CRACKED AT STA 664 AND LBL 32. MAJOR REPAIR ACCOMPLISHED. INSTALLED REPAIR DOUBLER AND FILLER. - [SDR 2000UALA00355](https://openairdocs.org/sdr/2000UALA00355), Jun 24, 2000: INDICATOR. FAILED. FLAPS LOCKED UP AT POSITION ONE. *S/D* THE TRAILING EDGE FLAPS POSITION INDICATOR WAS REPLACED. THE AIRCRAFT HAS NOT HAD ANY FLAP PROBLEMS SINCE THE REPLACEMENT - [SDR 2000UALA00737](https://openairdocs.org/sdr/2000UALA00737), Apr 5, 2000: BULKHEAD. CRACKED. CRACK FOUND ON THE BODY STATION 178 BULKHEAD WEB. SUPPLEMENTAL DATA UPDATE CRACKS REPAIRED PER BOEING SRM 53-10-08. - [SDR 99UAL900475](https://openairdocs.org/sdr/99UAL900475), Sep 13, 1999: STRUCTURE. DAMAGED. THE FUSELAGE SKIN AND TWO FRAMES WERE DAMAGED AFTER CONTACT WITH A SERVICE TRUCK. THE SKIN WAS DAMAGED FROM STATIONS 866 TO 904 BETWEEN STRINGERS 26 AND 27 LT A - [SDR 99UAL900202](https://openairdocs.org/sdr/99UAL900202), Apr 10, 1999: COUPLER. FAILED. UNEXPLAINED YAW FELT BY CREW ON FLIGHT DECK. YAW DAMPER COUPLER BITE TEST WAS PERFORMED BUT NO FAILURES WERE FOUND. REPLACED THE YAW DAMPER COUPLER PER MM 22-12 - [SDR 97UAL900477](https://openairdocs.org/sdr/97UAL900477), Jun 18, 1997: CONTROL MODULE. MISRIGGED. NO GREEN LIGHT ON LEFT MAIN LANDING GEAR WHEN GEAR HANDLE PUT IN DOWN POSITION. GEAR DID NOT EXTEND AND WAS EXTENDED MANUALLY. - [SDR 97UAL900472](https://openairdocs.org/sdr/97UAL900472), Jun 17, 1997: TIRE. FAILED. AMBER LIGHT DUE TO NR 2 MAIN TIRE TREAD SEPARATION AND THE LOSS OF THE 'A' HYDRAULIC SYSTEM. *S/D* FOUND LT LANDING GEAR TRANSFER CYLINDER HAS THREE DAMAGED HYD - [SDR 97UAL900190](https://openairdocs.org/sdr/97UAL900190), Mar 10, 1997: RATE GYRO. OUT OF ADJUST. YAW DAMPER WILL NOT ENGAGE. THE YAW DAMPER COUPLER WAS REPLACED, AFTER WHICH, THE SYSTEM TESTED NORMAL. UPON BENCH TESTING, IT WAS DISCOVERED THAT THE RATE GYRO - [SDR 96UAL900991](https://openairdocs.org/sdr/96UAL900991), Dec 27, 1996: LIGHT. INOPERATIVE. EMERGENCY LIGHT IS INOPERATIVE ABOVE ROW 9C. - [SDR 96UAL900241](https://openairdocs.org/sdr/96UAL900241), Apr 8, 1996: FMC. MALFUNCTIONED. FMC FAILS DURING TAKEOFF AT APPROXIMATELY 80 TO 100 KTS. FLAGS ARE DISPLAYED AND AUTO THROTTLES DISENGAGE. *S/D* NAVIGATION DATA BASE WAS RELOADED AND NO FURTHE ## 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 19990410043409I](https://openairdocs.org/incident/19990410043409I), Apr 10, 1999: Boeing 737322 (N387UA), Las Vegas, NV. (-23)On April 10, 1999, at 1317 hour PDT, a Boeing 737-300, N387UA, aborted the takeoff roll on runway 25R at mccarren international airport, Las Vegas,… ## Other aircraft with N387UA - [Cancelled 2022-07-02](https://openairdocs.org/deregistered/N387UA-2022-07-02): DJI PHANTOM 3 PROFESSION, S/N P78DCF11032485. Registration expired, pending cancellation. Owner: [Shore Kent H](https://openairdocs.org/faa-owner/SHORE%20KENT%20H), [Sarasota, FL](https://openairdocs.org/faa-place/FL/Sarasota) --- 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.