# N367UA: 1989 Boeing 737-322, registration cancelled 2018-02-08

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: February 8, 2018
- Status when cancelled: Registration expired, pending cancellation
- 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: 24536
- Year built: 1989
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: September 6, 1989
- Certificate issued: September 28, 1989
- Last registry action: April 11, 2012
- Mode S code: A42810
- Owner when cancelled: [Wilmington Trust Company-Trustee](https://openairdocs.org/faa-owner/WILMINGTON%20TRUST%20COMPANY-TRUSTEE)
- Location: [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington)
- Owner type: Corporation
- Owner's area on the map: 39.7357° N, 75.5321° W: Placed by OpenAirDocs: center of Wilmington, DE, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N367UA
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=367UA
- Page: https://openairdocs.org/deregistered/N367UA-2018-02-08

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 (57, newest 50)

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

- [SDR UALA2009070701952](https://openairdocs.org/sdr/UALA2009070701952), Jul 5, 2009: CONTROL PANEL. FALSE INDICATION. CARGO SMOKE DETECTOR CONTROL PANEL GIVES FALSE FAILURES FOR ALL DETECTORS. REPLACED CARGO SMOKE DETECTOR CONTROL PANEL, TESTS GOOD.
- [SDR UALA2009070101889](https://openairdocs.org/sdr/UALA2009070101889), Jun 30, 2009: STRUCTURE. CRACKED. FOUND CRACK ON E/E COOLING DUCT CUTOUT. LOWER FUSELAGE BS BETWEEN 360-380 AND 28L/R. ACP HFEC OF SUSPECT CRACK IN SKIN AFT OF EQUIP COOLING EXHAUST OPENING. ARE
- [SDR UALA2009012900310](https://openairdocs.org/sdr/UALA2009012900310), Jan 28, 2009: POWER SUPPLY. INOPERATIVE. FWD ENTRY DOOR (1L) EMERGENCY EXIT LIGHTS IN THE INTERIOR DOOR SURROUND AREA INOP. REPLACED BATTERY POWER SUPPLY M1133.
- [SDR UALA2009012200240](https://openairdocs.org/sdr/UALA2009012200240), Jan 18, 2009: SKIN. CRACKED. DOOR 1R LWR AFT CORNER CRACK IN SKIN. MAJOR REPAIR ACCOMPLISHED. HFEC INSPECTION OF SUSPECTED SURFACE AREA, SHOWS INDICATION OF DEFECT OR CRACK. ACCOMPLISHED TE
- [SDR 2008UALA04045](https://openairdocs.org/sdr/2008UALA04045), Jul 30, 2008: SQUAT SWITCH. FAILED. TAKEOFF WARNING HORN SOUNDED. RTFL. REPLACED M991 AIR SENSING SQUAT SWITCH. PERFORMED TAKEOFF AURAL WARNING TEST. CHECKED OKAY.
- [SDR 2008UALA03709](https://openairdocs.org/sdr/2008UALA03709), Jul 6, 2008: WARNING SWITCH. MALFUNCTIONED. ORAL WARNING HORN PROBLEM CAUSED DIVERSION. FOUND FAULTY CABIN ALTITUDE WARNING SWITCH. REPLACED CABIN ALTITUDE WARNING SWITCH.
- [SDR UALA2008111302602](https://openairdocs.org/sdr/UALA2008111302602), May 4, 2008: WIRE. BURNED. FOUND GENERATOR LEAD WIRES BURNT AND ARCING ON OIL PUMP, NEEDS REPLACEMENT. UNDER INVESTIGATION 5/19/08. REPLACED APU FEEDER CABLES. REMOVED AND REPLACED OIL PU
- [SDR 2008UALA02602](https://openairdocs.org/sdr/2008UALA02602), May 4, 2008: WIRE. BURNED. FOUND GENERATOR LEAD WIRES BURNT AND ARCING ON OIL PUMP, NEED REPLACEMENT.
- [SDR 2008UALA02619](https://openairdocs.org/sdr/2008UALA02619), May 2, 2008: MODULE. FAULTY. FIRE WARNING BELL FAILS TO RING. REPLACED WARNING BELL MODULE, OP CHECKED GOOD. AC OK FOR SERVICE.
- [SDR 2008UALA02254](https://openairdocs.org/sdr/2008UALA02254), Apr 14, 2008: HARNESS. LEAKING. CREW OXYGEN SYSTEM-LOW. RECORD PRESSURE PRIOR TO SERVICING. FOUND FIRST OBSERVERS O2 MASK INFLATABLE HARNESS HAS HOLE AND WON`T INFLATE. SERVICED SYSTEM. AND RE
- [SDR 2008UALA01105](https://openairdocs.org/sdr/2008UALA01105), Feb 28, 2008: RIB. CRACKED. RT WING RIB AT WBL 135.5 IS CRACKED AT AFT LOWER RIB CLIP NR 13349-6000-0033. ACP'D PER EVA 080161. MAJOR REPAIR: REPAIR ACCOMPLISHED.
- [SDR UALA2008111305073](https://openairdocs.org/sdr/UALA2008111305073), Dec 12, 2007: SENSOR. FAULTY. NOSE LANDING GEAR RED LIGHT WAS ILLUMINATED AFTER TAKEOFF, AND CONTINUED TO BE ILLUMINATED. CREW VERIFIED NOSE GEAR WAS UP. S845 HAS DAMAGED WIRES IN NOSE WHEEL
- [SDR 2007UALA05073](https://openairdocs.org/sdr/2007UALA05073), Dec 12, 2007: WARNING LIGHT. FALSE ACTIVATION. NOSE LANDING GEAR RED LIGHT WAS ILLUMINATED AFTER TAKEOFF, AND CONTINUED TO BE ILLUMINATED. CREW VERIFIED NOSE GEAR WAS UP.
- [SDR 2007UALA04851](https://openairdocs.org/sdr/2007UALA04851), Nov 27, 2007: LIGHT. INOPERATIVE. EEL LIGHTS INOP ROWS 11-16. FOUND POWER LEAD DAMAGE. REPLACED POWER LEAD AT ROW 12. EEL LIGHTS OPERATE CORRECTLY.
- [SDR 2007UALA03538](https://openairdocs.org/sdr/2007UALA03538), Sep 4, 2007: WARNING SYSTEM. ACTIVATED. CREW REPORT: PASSING 7000 FT AT CLIMB THRUST T/O WARNING HORN SOUNDED FOR 20 SECONDS. CABIN CLIMBING NORMAL, LANDING GEAR HANDLE OFF POSITION.
- [SDR 2007UALA02812](https://openairdocs.org/sdr/2007UALA02812), Jul 24, 2007: OXYGEN MASK. FAULTY. CAPT OXYGEN MASK LEAKING. MASK DOES NOT LEAK WHEN STOWED, ONLY LEAKS WHEN HOSE PRESSURIZED. REPLACED OXYGEN MASK AND SERVICED OXYGEN SYSTEM TO FULL.
- [SDR 2007UALA02311](https://openairdocs.org/sdr/2007UALA02311), Jun 29, 2007: FIRE DETECTOR. NO TEST. FWD CARGO PIT FIRE DETECTOR LIGHT NO TEST, A AND B CHANNELS NO TEST. REPLACED B LOOP DETECTORS. INSTALLED 2 A LOOP DETECTORS IN FORWARD PIT. REPLACED 3 EACH A L
- [SDR 2007UALA01366](https://openairdocs.org/sdr/2007UALA01366), Apr 30, 2007: BEAR STRAP. CRACKED. FWD ENTRY DOOR (1L) LOWER HINGE CUTOUT HAS 1 EACH FASTENER HOLE CRACKED. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGE FROM HOLE & BEAR STRAP. NDT FOR CRACK CONTAIN
- [SDR 2007UALA01365](https://openairdocs.org/sdr/2007UALA01365), Apr 30, 2007: SKIN. CRACKED. FUSELAGE SKIN CRACKED AT STA 516-518 AT CHEM MILLED STEP .5 INCH BELOW STR 12L. MAJOR REPAIR ACCOMPLISHED: TRIMMED OUT DAMAGE & NDT FOR CRACK CONTAINMENT. FABRI
- [SDR 2007UALA01338](https://openairdocs.org/sdr/2007UALA01338), Apr 29, 2007: SHEAR TIE. CRACKED. BS 294 SHEAR TIE CRACKED AT STRINGER 11L. [SUP 05-16-07] MAJOR REPAIR ACCOMPLISHED: REMOVED CRACKED SHEAR TIE. FABRICATED & INSTALLED NEW SHEAR TIE.
- [SDR 2007UALA01337](https://openairdocs.org/sdr/2007UALA01337), Apr 29, 2007: STRUCTURE. CRACKED. LEFT UPPER FUSELAGE FWD ENTRY DOOR UPPER HINGE CUTOUT HAS 3 EA EXISTING FASTENER HOLES CRACKED. [SUP 05-16-07] MAJOR REPAIR ACCOMPLISHED: ENLARGED HOLES & SPOT 
- [SDR 2007UALA01336](https://openairdocs.org/sdr/2007UALA01336), Apr 29, 2007: SKIN. CRACKED. EXTERNAL FUSELAGE SKIN HAS A 4 INCH CRACK 13 INCHES AFT OF BS 927 JUST ABOVE STR 24L. [SUP 05-16-07] MAJOR REPAIR ACCOMPLISHED: CUT OUT DAMAGED AREA. FABRICATED
- [SDR 2007UALA01335](https://openairdocs.org/sdr/2007UALA01335), Apr 29, 2007: STRINGER SPLICE. CRACKED. CABIN INTERIOR AT BS 348 AND STRINGER S-15L SPLICE CHANNEL LOWER FLANGE CRACKED. [SUP 05-16-07] MAJOR REPAIR ACCOMPLISHED: REMOVED & REPLACED CRACKED SPLICE CHA
- [SDR 2007UALA01334](https://openairdocs.org/sdr/2007UALA01334), Apr 29, 2007: FITTING. CORRODED. VERTICAL STAB FUSELAGE FITTING AT BS 1088 RIGHT AFT PRIMARY FITTING FORWARD FACE CORRODED. [SUP 05-16-07] MAJOR REPAIR: REMOVED CORROSION AND SPOT FACED FORWARD
- [SDR 2007UALA01333](https://openairdocs.org/sdr/2007UALA01333), Apr 29, 2007: PRESSURE PANEL. WORN. RIGHT WHEEL WELL ABOVE SPOILER MIXER RATIO CHANGER PRESSURE DECK SKIN WORN IN 2 AREAS. [SUP 05-16-07] MAJOR REPAIR ACCOMPLISHED: BLENDED OUT DAMAGE. FABRICATED 
- [SDR 2007UALA01332](https://openairdocs.org/sdr/2007UALA01332), Apr 29, 2007: SKIN. DAMAGED. FIN STA 145, BETWEEN FWD AND AFT SPAR HAS DAMAGE. [SUP 05-16-07] MAJOR REPAIR ACCOMPLISHED: REMOVED EXISTING REPAIRS & DAMAGED SKIN SECTION. FABRICATED & INSTAL
- [SDR 2007UALA01300](https://openairdocs.org/sdr/2007UALA01300), Apr 25, 2007: DOOR FRAME. CRACKED. AFT CARGO DOOR FWD LOWER FRAME CRACKED. MAJOR REPAIR ACCOMPLISHED: REMOVED & REPLACED FRAME SECTION.
- [SDR 2007UALA01299](https://openairdocs.org/sdr/2007UALA01299), Apr 25, 2007: TEE FITTING. CRACKED. AFT CARGO DOOR LOWER "T" CHORD CRACKED AT LOWER AFT CORNER. MAJOR REPAIR ACCOMPLISHED: REMOVED & REPLACED LOWER "T" CHORD ASSY.
- [SDR 2007UALA01298](https://openairdocs.org/sdr/2007UALA01298), Apr 25, 2007: FLOORBEAM. CORRODED. AFT CABIN FLOOR STRUCTURE, UPPER "T" CAP CORRODED ON UPPER SURFACE AT BS 1016 LBL5 TO 39 WL 208. MAJOR REPAIR ACCOMPLISHED: REMOVED CORROSION. FABRICATED & INST
- [SDR 2007UALA01297](https://openairdocs.org/sdr/2007UALA01297), Apr 25, 2007: FLOORBEAM. CORRODED. AFT CABIN FLOOR STRUCTURE, FLOORBEAM UPPER "T" CAP UPPER SURFACE HAS 2 SPOTS OF CORROSION. BS 1016 RBL 5 TO 14.5 AT WL 208. MAJOR REPAIR ACCOMPLISHED: REMOVED C
- [SDR 2007UALA01264](https://openairdocs.org/sdr/2007UALA01264), Apr 23, 2007: SKIN. DENTED. FWD CARGO DOOR HAS A 8" LONG .312" WIDE .062" DEPTH DENT, 3" FWD OF AFT DOOR EDGE AND 20" UP FROM BOTTOM OF DOOR. MAJOR REPAIR ACCOMPLISHED: FABRICATED & INSTAL
- [SDR 2007UALA01263](https://openairdocs.org/sdr/2007UALA01263), Apr 23, 2007: ANGLE. CRACKED. RIGHT HAND WHEEL WELL BS 695 FRAME INNER CHORD ANGLE CRACKED, LOWER INNER RADIUS. MAJOR REPAIR ACCOMPLISHED: REMOVED & REPLACED CRACKED CHORD ANGLE.
- [SDR 2007UALA01219](https://openairdocs.org/sdr/2007UALA01219), Apr 18, 2007: CREASE BEAM. CORRODED. FWD CABIN FLOOR STRUCTURE CREASE BEAM Z-ANGLE HAS CORROSION ON UPPER SURFACE AT BS 294 TO 360 RBL 55 TO 63 AT WL 208. [SUP 05-01-07] MAJOR REPAIR ACCOMPLISHED: 
- [SDR 2007UALA01153](https://openairdocs.org/sdr/2007UALA01153), Apr 15, 2007: CREASE BEAM. CORRODED. AFT CABIN FLOOR STRUCTURE CREASE BEAM HAS CORROSION ON UPPER SURFACE BS 960-996 RBL 46-57 AT 208. [SUP 05-01-07] MAJOR REPAIR: INSTALLED NEW CREASE BEAM. REFERE
- [SDR 2007UALA01152](https://openairdocs.org/sdr/2007UALA01152), Apr 15, 2007: CREASE BEAM. CORRODED. FWD CABIN FLOOR STRUCTURE CREASE BEAM Z-ANGLE HAS CORROSION ON UPPER SURFACE THROUGHOUT LENGTH BS 312 TO 360 LBL 55-60 WL 208. [SUP 05-01-07] MAJOR REPAIR: INST
- [SDR 2007UALA01150](https://openairdocs.org/sdr/2007UALA01150), Apr 14, 2007: FRAME. CRACKED. LEFT WHEEL WELL BS 695 FRAME CHORD ANGLE CRACKED INNER RADIUS AREA. [SUP 05-01-07] MAJOR REPAIR: REPLACED INNER FRAME CHORD PER MM 53-10-98 PG601.
- [SDR 2007UALA01149](https://openairdocs.org/sdr/2007UALA01149), Apr 14, 2007: SKIN. GOUGED. UPPER EXTERNAL FUSELAGE SKIN GOUGED FROM APPARENT JET WAY CONTACT BS 278-279 STR 3L. [SUP 05-01-07] MAJOR REPAIR: INSTALLED EXTERNAL DOULBER-TRIPLER REPAIR PER 
- [SDR 2007UALA01148](https://openairdocs.org/sdr/2007UALA01148), Apr 14, 2007: SKIN. CRACKED. INNER SURFACE OF FUSELAGE SKIN CRACKED ON EDGE OF BONDED DOUBLER AFT OF STA 927 FRAME BTWN STR 22R AND 23R. [SUP 05-01-07] MAJOR REPAIR: INSTALLED EXTERNAL SKIN
- [SDR 2007UALA01147](https://openairdocs.org/sdr/2007UALA01147), Apr 14, 2007: SKIN. DENTED. DENT IN RT HORIZONTAL STABILIZER LEADING EDGE APPROX SIX RIVET ROWS FROM FUSELAGE. [SUP 5-10-07] MAJOR REPAIR: INSTALLED DOUBLER REPAIR PER SRM 55-10-01 PG 201-
- [SDR 2007UALA01146](https://openairdocs.org/sdr/2007UALA01146), Apr 14, 2007: CREASE BEAM. CORRODED. AFT CABIN FLOOR STRUCTURE AT DOOR CUT-OUT 2L, INNER CREASE BEAM ANGLE HAS CORROSION IN SPOTS ON UPPER SURFACE AT BS 960-987 LBL50 40-50 WL 209. [SUP 5-1-07] MAJ
- [SDR 2007UALA01168](https://openairdocs.org/sdr/2007UALA01168), Apr 13, 2007: FRAME. CRACKED. FWD GALLEY DOOR FWD LOWER FRAME IS CRACKED AT 2 FASTENER HOLES. [SUP 05-01-07] MAJOR REPAIR: INSTALLED NEW FRAME SPLICE SECTION KIT 69-69430-9. REFERENCE SRM 51
- [SDR 2007UALA00615](https://openairdocs.org/sdr/2007UALA00615), Feb 26, 2007: O-RING. LEAKING. LOW BOTTLE PRESSURE. CAUSED BY GAUGE ADAPTER FITTING O-RING LEAKING. REPLACED O-RING.
- [SDR 2007UALA00007](https://openairdocs.org/sdr/2007UALA00007), Dec 31, 2006: SIGN. INOPERATIVE. EMERGENCY EXIT LOCATOR SIGN INOP FORWARD OF RT OVERWING EXIT ON LOWER SIDEWALL. REPLACED INVERTER.
- [SDR 2007UALA00006](https://openairdocs.org/sdr/2007UALA00006), Dec 31, 2006: LIGHT. INOPERATIVE. RT EEL LIGHT IN ICE DETECTION PANEL IS INOPERATIVE. RELAMPED.
- [SDR 2007UALA00005](https://openairdocs.org/sdr/2007UALA00005), Dec 31, 2006: LIGHT. INOPERATIVE. EMERGENCY LIGHT INOP, LT EXTERIOR, LIGHT ON LOWER FUSELAGE AFT OF THE WING. REPLACED POWER SUPPLY AND BATTERY AT M1136.
- [SDR 2006UALA02036](https://openairdocs.org/sdr/2006UALA02036), Oct 21, 2006: LIGHT. INOPERATIVE. EMERGENCY EXIT LIGHTS AT CEILING FWD CABIN AND BY DOOR 1L INOP. REPLACED BATTERY
- [SDR 2006UALA01982](https://openairdocs.org/sdr/2006UALA01982), Oct 14, 2006: LAP JOINT. DENTED. FOUND DENT ON LAP JOINT APPROX 13.5" AFT OF DR 2L, 22" UP FROM DOOR THRESHOLD. MAJOR REPAIR: REPAIRED FUSELAGE PER SRM 53-00-01 AND EVA 60626.
- [SDR 2006UALA01820](https://openairdocs.org/sdr/2006UALA01820), Sep 19, 2006: BOTTLE. LOW. LOW BOTTLE PRESSURE CAUSE: UNDETERMINED, FOUND NO DEFECTS DURING TROUBLESHOOTING. REPLACED THE SLIDE ON A/C. SLIDE VALVE OVERHAULED AS PRECAUTION.
- [SDR 2006UALA01062](https://openairdocs.org/sdr/2006UALA01062), May 31, 2006: ODOR. DETECTED. BURNING ODOR PRESENT IN CABIN.
- [SDR 2004UALA00694](https://openairdocs.org/sdr/2004UALA00694), Jul 18, 2004: SKIN. DAMAGED. ON SKIN DAMAGE AT STA 360, A DENT IN STRINGER 20R SKIN FLANGE. MAJOR REPAIR ACCOMPLISHED. SKIN REPAIRED. REPLACED STRINGER SPLICE FITTING.

All 57: https://openairdocs.org/deregistered/N367UA-2018-02-08/reports.md

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