# N370UA: 1989 Boeing 737-322, registration cancelled 2011-01-11

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: January 11, 2011
- Status when cancelled: Sale reported
- 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: 24539
- Year built: 1989
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: October 2, 1989
- Last registry action: December 15, 2010
- Mode S code: A4358E
- Location: [Miami, FL](https://openairdocs.org/faa-place/FL/Miami)
- Owner type: Individual
- Owner's area on the map: 25.7655° N, 80.1843° W: Placed by OpenAirDocs at the center of ZIP code 33131, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N370UA
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=370UA
- Page: https://openairdocs.org/deregistered/N370UA-2011-01-11

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 737-322: https://openairdocs.org/model/boeing-737-322.md

## Service difficulty reports (64, newest 50)

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR UALA2009031000717](https://openairdocs.org/sdr/UALA2009031000717), Mar 4, 2009: LIGHT. INOPERATIVE. DOOR 1L EXTERIOR EMERGENCY LIGHT INOP. RELAMPED EMERGENCY LIGHT. OP CHECK NORMAL.
- [SDR UALA2009030501396](https://openairdocs.org/sdr/UALA2009030501396), Mar 4, 2009: LIGHT. INOPERATIVE. DOOR 1L EXTERIOR EMERGENCY LIGHT INOP. RELAMPED EMERGENCY LIGHT, OP CHECK NORMAL.
- [SDR 2008UALA06478](https://openairdocs.org/sdr/2008UALA06478), Nov 10, 2008: FLASHLIGHT. INOPERATIVE. FWD F/A FLASHLIGHT NOT BLINKING. REPLACED FLASHLIGHT.
- [SDR 2008UALA03526](https://openairdocs.org/sdr/2008UALA03526), Jun 20, 2008: LAMP. INOPERATIVE. LEFT EMERGENCY EXIT WING LIGHT IS INOP. FOUND BURNED OUT LAMP. REPLACED LAMP OP CHECKED GOOD. AC OK FOR SERVICE.
- [SDR 2008UALA02547](https://openairdocs.org/sdr/2008UALA02547), May 1, 2008: UNKNOWN. UNKNOWN. VERTICAL FLUTTER IN INTERVALS OF THREE DURING ALL PHASES OF FLIGHT.
- [SDR 2008UALA01954](https://openairdocs.org/sdr/2008UALA01954), Apr 4, 2008: CABLE. FAULTY. CREW REPORT, FO O2 MASK MIC INOP. REPLACED OXYGEN MASK. SHOP FOUND MIC CABLE BAD AND RUBBER BANDS DETERIORATED. REPLACED CHORD AND RUBBER BANDS.
- [SDR 2007UALA04957](https://openairdocs.org/sdr/2007UALA04957), Dec 4, 2007: RIB. CRACKED. NR 2 MAIN FUEL TANK LT RIB LOWER CHORD CRACKED WBL 135.5 BETWEEN WING STRINGERS S2 AND S3. CRACK IS APPROXIMATELY 2.5 INCH LONG & ORIGINATES IN THE CUTOUT RADIU
- [SDR 2007UALA04956](https://openairdocs.org/sdr/2007UALA04956), Dec 4, 2007: RIB. CRACKED. NR 1 MAIN FUEL TANK LT RIB LOWER CHORD CRACKED WBL135.5 BETWEEN WING STRINGERS S2 AND S3. CRACK IS APPROXIMATELY 1 INCH LONG & ORIGINATES IN THE CUTOUT RADIUS O
- [SDR 2007UALA04955](https://openairdocs.org/sdr/2007UALA04955), Dec 4, 2007: ATTACH BRACKET. CRACKED. INNER FUSELAGE STRUCTURE AFT OF DOOR CUTOUT FOR 1-L, INTERCOSTAL WEB ATTACH BRACKET IS CRACKED, FWD SIDE OF STA 360, STR 11-L. MAJOR REPAIR ACCOMPLISHED: REMOVE
- [SDR 2007UALA04954](https://openairdocs.org/sdr/2007UALA04954), Dec 4, 2007: STRINGER SPLICE. CRACKED. FWD ENTRY DOOR CUTOUT STRINGER SPLICE CHANNEL CRACKED AT BS 360 AND STRINGER 16L. MAJOR REPAIR ACCOMPLISHED: REPLACED STRINGER SPLICE CHANNEL AT BS 360 STR 16L.
- [SDR 2007UALA04953](https://openairdocs.org/sdr/2007UALA04953), Dec 4, 2007: ATTACH BRACKET. CRACKED. INNER FUSELAGE STRUCTURE AT FWD ENTRY DOOR CUTOUT INTERCOSTAL ATTACH BRACKET CRACKED AFT SIDE OF BS 294.5 AT STRINGER 11L. MAJOR REPAIR ACCOMPLISHED: REPAIRED I
- [SDR 2007UALA04952](https://openairdocs.org/sdr/2007UALA04952), Dec 4, 2007: BEAR STRAP. CRACKED. FUSELAGE FORWARD ENTRY DOOR (1L) CUTOUT UPPER HINGE CUTOUT BEAR STRAP IS CRACKED OUT OF FASTENER HOLE BELOW LOWER GUIDE PLATE. MAJOR REPAIR ACCOMPLISHED: CUT OU
- [SDR 2007UALA04951](https://openairdocs.org/sdr/2007UALA04951), Dec 4, 2007: ATTACH ANGLE. CRACKED. MED 1L, BS 294 UPPER HINGE BOX LOWER AUX INTERCOSTAL ATTACH ANGLE CRACKED DURING FASTENER REMOVAL. MAJOR REPAIR ACCOMPLISHED: FABRICATED & INSTALLED UPPER HINGE
- [SDR 2007UALA04950](https://openairdocs.org/sdr/2007UALA04950), Dec 4, 2007: INTERCOSTAL. CRACKED. INNER FUSELAGE STRUCTURE AT ENTRY DOOR CUTOUT FOR 1-L. INTERCOSTAL HAS CRACK, AFT SIDE OF STA 294.5, STR 12-L. MAJOR REPAIR ACCOMPLISHED: REPLACED INTERCOSTAL W
- [SDR 2007UALA04949](https://openairdocs.org/sdr/2007UALA04949), Dec 4, 2007: ANGLE. CRACKED. INNER FUSELAGE STRUCTURE AT DOOR CUTOUT 1L, L-ANGLE UNDER INTERCOSTAL WEB IS CRACKED STA 294.5+7 INCHES AT STR 13-L. MAJOR REPAIR ACCOMPLISHED: FABRICATED & INS
- [SDR 2007UALA04909](https://openairdocs.org/sdr/2007UALA04909), Dec 2, 2007: STRINGER. CORRODED. FUSELAGE STRINGER CORRODED JUST BELOW FWD LAV SERVICE PANEL - RT NOSE TUNNEL STR 21R. MAJOR REPAIR: REMOVED DAMAGED PART OF STRINGER. REMOVED CORROSION FROM SKI
- [SDR 2007UALA04908](https://openairdocs.org/sdr/2007UALA04908), Dec 1, 2007: SKIN. CRACKED. FWD GALLEY DOOR CUTOUT, LWR AFT CORNER IS CRACKED. MAJOR REPAIR; REMOVED DAMAGE, FABRICATED AND INSTALLED EXTERNAL FUSELAGE SKIN DOUBLER-TRIPLER REPAIR.
- [SDR 2007UALA04906](https://openairdocs.org/sdr/2007UALA04906), Dec 1, 2007: BEAR STRAP. CRACKED. FUSELAGE FORWARD ENTRY DOOR CUTOUT LOWER HINGE CUTOUT BEAR STRAP HAS CRACK OUT OF FASTENER HOLES ABOVE & BELOW GUIDE PLATES. MAJOR REPAIR: REMOVED DAMAGE. FABRI
- [SDR 2007UALA04905](https://openairdocs.org/sdr/2007UALA04905), Dec 1, 2007: SKIN. CRACKED. BS 517 TO 519 AT STRINGER 12L, FUSELAGE INTERIOR SKIN CRACKED AT CHEM MILLED STEP BELOW STRINGER. MAJOR REPAIR: REMOVED DAMAGE. FABRICATED AND INSTALLED EXTERNA
- [SDR 2007UALA04904](https://openairdocs.org/sdr/2007UALA04904), Dec 1, 2007: STRUCTURE. CRACKED. AFT ENTRY DOOR LOWER HINGE CUTOUT IN FUSELAGE CRACKED AT THE LOWER FORWARD CORNER. MAJOR REPAIR: REMOVED DAMAGE. FABRICATED AND INSTALLED EXTERNAL SKIN DOUBLER.
- [SDR 2007UALA04884](https://openairdocs.org/sdr/2007UALA04884), Nov 29, 2007: SKIN. DENTED. FUSELAGE CROWN DENT AT BS 360 BETWEEN STR 2R & 3R AND HAS A CRACK AT STR 2 AT RIVET, DENT IS IN COMMON TO BUTT JOINT. MAJOR REPAIR: DENT ALLEVIATED WHEN STRINGE
- [SDR 2007UALA04883](https://openairdocs.org/sdr/2007UALA04883), Nov 29, 2007: FRAME. CORRODED. FRAME CORRODED ON FWD AND AFT SIDE OF BS 380 AND ON SKIN ADJACENT TO FWD SIDE OF FRAME, IN FWD PIT BILGE RBL 2"- LBL 2". MAJOR REPAIR: REMOVED CORROSION AND ACC
- [SDR 2007UALA04882](https://openairdocs.org/sdr/2007UALA04882), Nov 29, 2007: SKIN. DAMAGED. AFT CARGO DOOR CUTOUT, BEAR STRAP REPAIR BS 847 STR 22R NEEDS TO BE REINSTALLED AFTER SKIN REPLACEMENT. MAJOR REPAIR: REPAIRED AFT PIT DOOR CUTOUT BEAR STRAP.
- [SDR 2007UALA04856](https://openairdocs.org/sdr/2007UALA04856), Nov 28, 2007: SKIN. CRACKED. RIGHT HORZ STAB LOWER SKIN IS CRACKED, JUST FWD OF FIRST BALANCE PANEL BAY. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGED SECTION OF LWR SKIN. INSTALLED A SINGLE .
- [SDR 2007UALA04794](https://openairdocs.org/sdr/2007UALA04794), Nov 24, 2007: SKIN. DENTED. LOWER FUSELAGE HAS A DENT ALONG FRAME SHEAR TIE BETWEEN STR 26L-27L BS 807. MAJOR REPAIR: FABRICATED AND INSTALLED EXTERNAL FUSELAGE SKIN DOUBLER. 
- [SDR 2007UALA04793](https://openairdocs.org/sdr/2007UALA04793), Nov 24, 2007: STRINGER SPLICE. CRACKED. STR 15R SPLICE IS CRACKED BS 360. MAJOR REPAIR: REPLACED STRINGER SPLICE.
- [SDR 2007UALA04789](https://openairdocs.org/sdr/2007UALA04789), Nov 21, 2007: SKIN. WORN. EXTERNAL FUSELAGE SKIN HAS SEVERAL AREAS OF WEAR UNDER DORSAL FIN LANDING FROM BS 860-908. BLENDED WORN AREAS. FABRICATED AND INSTALLED EXTERNAL DOUBLER, INTERN
- [SDR 2007UALA04776](https://openairdocs.org/sdr/2007UALA04776), Nov 20, 2007: CREASE BEAM. CORRODED. CABIN FLOOR CREASE BEAM HAS SPOTS OF CORROSION AT BS 294-360, RBL 49". REMOVED AND REPLACED CREASE BEAM.
- [SDR 2007UALA04775](https://openairdocs.org/sdr/2007UALA04775), Nov 20, 2007: FRAME. CRACKED. FWD ENTRY DOOR LOWER FWD CORNER HAS CRACK IN FRAME. REPLACED LOWER FORWARD FRAME.
- [SDR 2007UALA04748](https://openairdocs.org/sdr/2007UALA04748), Nov 19, 2007: DOOR FRAME. CRACKED. FWD GALLEY DOOR, NR 4 STOP FITTING FROM TOP CRACKED IN CUTOUT, CRACK PREVIOUSLY STOP DRILLED.
- [SDR 2007UALA04747](https://openairdocs.org/sdr/2007UALA04747), Nov 19, 2007: DOOR FRAME. CRACKED. FWD GALLEY DOOR AFT FRAME WEB HAS 4 EA CRACKS AT OUTBOARD FASTENER HOLES FOR LOWER STOP FITTING.
- [SDR 2007UALA04746](https://openairdocs.org/sdr/2007UALA04746), Nov 19, 2007: DOOR FRAME. CRACKED. FWD GALLEY DOOR, LOWER AFT CORNER FRAME CRACKED. 
- [SDR 2007UALA04727](https://openairdocs.org/sdr/2007UALA04727), Nov 17, 2007: PRESSURE PANEL. CRACKED. LEFT MAIN WHEEL WELL CEILING CRACKED AT BS 665 LBL 32. MAJOR REPAIR ACCOMPLISHED: FABRICATED & INSTALLED MID CABIN PRESS DECK REPAIR DOUBLER.
- [SDR 2007UALA04726](https://openairdocs.org/sdr/2007UALA04726), Nov 17, 2007: SHEAR TIE. CRACKED. FRAME SHEAR TIE IS CRACKED BS 360 BETWEEN STRINGERS 14R-15R. MAJOR REPAIR ACCOMPLISHED: FABRICATED & INSTALLED SHEAR TIE DOUBLER REPAIR.
- [SDR 2007UALA04725](https://openairdocs.org/sdr/2007UALA04725), Nov 17, 2007: STRINGER SPLICE. DAMAGED. FUSELAGE STRINGER END SPLICE DAMAGED, BS 907 STR 24R. MAJOR REPAIR ACCOMPLISHED: REMOVED & INSTALLED NEW STRINGER END SPLICE.
- [SDR 2007UALA04719](https://openairdocs.org/sdr/2007UALA04719), Nov 16, 2007: ATTACH ANGLE. CRACKED. FUSELAGE INTERCOSTAL WEB ATTACH ANGLE CRACKED BELOW STR 12R FWD OF DOOR 1R AT APPROX BS 291.5. MAJOR REPAIR ACCOMPLISHED: INSTALLED NEW ATTACH ANGLE.
- [SDR 2007UALA04702](https://openairdocs.org/sdr/2007UALA04702), Nov 15, 2007: ATTACH ANGLE. CRACKED. INTERCOSTAL WEB ATTACH ANGLE CRACKED BELOW STRINGER 13R FORWARD OF DOOR 1R CUTOUT APPROX BS 291.5. REMOVED AND REPLACED CRACKED ANGLE.
- [SDR 2007UALA04701](https://openairdocs.org/sdr/2007UALA04701), Nov 15, 2007: INTERCOSTAL. CRACKED. CABIN BS 360 INTERCOSTAL AT RBL 1 FLOOR LEVEL CRACKED AT WL 208. REMOVED AND REPLACED CRACKED INTERCOSTAL WITH NEW UNIT. 
- [SDR 2007UALA04700](https://openairdocs.org/sdr/2007UALA04700), Nov 15, 2007: CREASE BEAM. CORRODED. RIGHT CABIN CREASE BEAM WEB ADJACENT TO STRINGER 17L IS CORRODED ON UPPER SURFACE BETWEEN BS 727D & S 727E WL 208. BLENDED OUT CORROSION. FABRICATED AND INSTALL
- [SDR 2007UALA04699](https://openairdocs.org/sdr/2007UALA04699), Nov 15, 2007: CREASE BEAM. CORRODED. LEFT CABIN CREASE BEAM WEB ADJACENT TO STRINGER 17L IS CORRODED ON UPPER SURFACE BETWEEN BS 500B & S 500C WL 208. BLENDED OUT CORROSION. FABRICATED AND INSTALLE
- [SDR 2007UALA03050](https://openairdocs.org/sdr/2007UALA03050), Aug 7, 2007: UNKNOWN. SMOKE. AFTER LANDING SMOKE REPORTED COMING FROM RT OUTBD MLG BRAKE AREA.
- [SDR 2007UALA02882](https://openairdocs.org/sdr/2007UALA02882), Jul 29, 2007: SLIDE. UNSECURE. DOOR 1L SLIDE PACK HAS 5 INCHES OF EXTRA SLIDE HANGING DOWN BELOW PACK. REINSTALLED SLIDE PACK IN CONTAINER. NO REPEATS.
- [SDR 2007UALA02361](https://openairdocs.org/sdr/2007UALA02361), Jul 2, 2007: MODULE. BROKEN. A-C FAILS STANDBY POWER TEST WHEN SWITCH PLACED FROM OFF TO AUTO POSITION. REPLACED P5-5 MODULE, GEN DRIVE AND STBY PWR MODULE.
- [SDR 2007UALA02131](https://openairdocs.org/sdr/2007UALA02131), Jun 19, 2007: LIGHT. UNSECURE. EMERGENCY EXIT LIGHT STRIP COMING UP OFF FLOOR AT 7C. SECURED STRIP.
- [SDR 2007UALA02054](https://openairdocs.org/sdr/2007UALA02054), Jun 17, 2007: OXYGEN SYSTEM. READS LOW. CREW REPORT: CREW O2 LOW. [07-06-07] SERVICED O2 TO FULL.
- [SDR 2007UALA01917](https://openairdocs.org/sdr/2007UALA01917), Jun 9, 2007: SKIN. DAMAGED. FUSELAGE SKIN AFT OF AFT CARGO DOOR IS DAMAGED. FRAME STA 927 BENT, STA 947.5 CRACKED. STRINGERS 22R AND 23R BENT AND SHEAR TIE STA 927 BENT. [07-03-07] ACCOMPL
- [SDR 2007UALA01838](https://openairdocs.org/sdr/2007UALA01838), Jun 6, 2007: ACTUATOR. MALFUNCTIONED. AUTO SPEED BRAKE DID NOT DEPLOY ON LANDING. REPLACED ACTUATOR.
- [SDR 2007UALA01046](https://openairdocs.org/sdr/2007UALA01046), Apr 6, 2007: SEAL. DAMAGED. NOTICEABLE HI FREQUENCY LO AMPLITUDE VIBRATION DURING CLIMB. REPLACED BLADE SEAL AND RESEALED BODY WING FAIRING.
- [SDR 2007UALA00908](https://openairdocs.org/sdr/2007UALA00908), Mar 25, 2007: ENGINE. ODOR. OIL ODOR IN CABIN WITH RIGHT PACK ON. OIL ODOR WITH NR 2 ENG BLEED. NR 2 ENGINE REPLACED 
- [SDR 2006UALA02317](https://openairdocs.org/sdr/2006UALA02317), Dec 5, 2006: DOOR FRAME. CRACKED. FWD CARGO DOOR CUT-OUT FWD FRAME IS CRACKED AT LOWER DOOR STOP, BS 440 STRINGER S-24R. MAJOR REPAIR: REMOVED DAMAGE. FABRICATED AND INSTALLED TWO NESTED ANGLE R

All 64: https://openairdocs.org/deregistered/N370UA-2011-01-11/reports.md

## 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 19971018035109I](https://openairdocs.org/incident/19971018035109I), Oct 18, 1997: Boeing 737* (N370UA), Buffalo, NY. Narrative: on Saturday, October 18, 1997, at 1311 EDT, a Boeing 737, N370UA, flight 1085, operated by united airlines, on a flight from boston, Massachusetts…

---
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.