# N352UA: 1989 Boeing 737-322, registration cancelled 2005-05-16 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: May 16, 2005 - Exported to: Germany - Status when cancelled: Triennial form not returned - 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: 24320 - Year built: 1989 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: February 9, 1989 - Certificate issued: April 7, 1989 - Last registry action: September 21, 2004 - Mode S code: A3EDFE - Owner when cancelled: [Wilmington Trust Co Trustee](https://openairdocs.org/faa-owner/WILMINGTON%20TRUST%20CO%20TRUSTEE) - 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/N352UA - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=352UA - Page: https://openairdocs.org/deregistered/N352UA-2005-05-16 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 (48) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR 2004UALA00781](https://openairdocs.org/sdr/2004UALA00781), Aug 21, 2004: ELEVATOR. MALFUNCTIONED. RETURNED TO DEN WITH ELEVATOR PROBLEM. NO FAULT HAS BEEN IDENTIFIED WITHIN THE ELEVATOR SYSTEM. THE FOLLOWING ACTIONS WERE TAKEN IN THE COURSE OF TROUBLESHOOTIN - [SDR 2004UALA00733](https://openairdocs.org/sdr/2004UALA00733), Aug 7, 2004: CSD. FAILED. RETURNED TO ORD DUE TO A NR 1 ENGINE GENERATOR DRIVE LIGHT. NR 1 CSD FAILED. OIL LOSS EVIDENT ON COWL, CSD EXTREMELY HOT ON ARRIVAL, SUSPECT INTERNAL FAILURE. R - [SDR 2002UALA01603](https://openairdocs.org/sdr/2002UALA01603), Oct 18, 2002: DOOR FRAME. CORRODED. AFT CARGO COMPARTMENT DOOR CUTOUT FRAME AT BODY STATION 794 S23R TO S24R AFT SIDE HAS EXCESSIVE MATERIAL REMOVED TO CLEAN CORROSION. MAJOR REPAIR ACCOMPLISHED. - [SDR 2002UALA01602](https://openairdocs.org/sdr/2002UALA01602), Oct 18, 2002: SKIN. CRACKED. CRACK IN FUSELAGE SKIN DOUBLER AT FORWARD EDGE OF FORWARD PIT DOOR CUTOUT 13 INCHES ABOVE LOWER EDGE. MAJOR REPAIR ACCOMPLISHED. TRIPLER REPAIR. - [SDR 2002UALA01596](https://openairdocs.org/sdr/2002UALA01596), Oct 16, 2002: INTERCOSTAL. CRACKED. CABIN FLOOR INTERCOSTAL UPPER FLANGE CRACKED AT BODY STATION 933 BL 0. MAJOR REPAIR ACCOMPLISHED. REPLACED UPPER FLANGE. - [SDR 2002UALA01587](https://openairdocs.org/sdr/2002UALA01587), Oct 14, 2002: TEE FITTING. CORRODED. AFT PIT DOOR OPENING FORWARD FRAME TEE FITTING FOR BOTTOM STOP PAD FITTING IS CORRODED BEYOND LIMITS. MAJOR REPAIR ACCOMPLISHED. REPLACED SUPPORT TEE FITTING. - [SDR 2002UALA01577](https://openairdocs.org/sdr/2002UALA01577), Oct 13, 2002: DOOR FRAME. CRACKED. FORWARD GALLEY DOOR CUTOUT FORWARD FRAME AT STOP PAD FITTING IS CRACKED (UPPER FITTING). MAJOR REPAIR ACCOMPLISHED. INSTALLED REPAIR ANGLE. INSTALLED FRAME. - [SDR 2002UALA01575](https://openairdocs.org/sdr/2002UALA01575), Oct 12, 2002: SKIN. DAMAGED. AFT EDGE OF AFT CARGO DOOR CUTOUT SKIN BLENDED WORN. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. - [SDR 2002UALA01574](https://openairdocs.org/sdr/2002UALA01574), Oct 12, 2002: FRAME. CRACKED. LEFT HAND BODY STATION 188 FRAME CRACKED AT STRINGER 17 LEFT HAND. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. - [SDR 2002UALA01573](https://openairdocs.org/sdr/2002UALA01573), Oct 12, 2002: BULKHEAD. CRACKED. LEFT HAND BODY STATION 178 FUSELAGE CHORD CRACKED AT WL207. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW WEB REPAIR. - [SDR 2002UALA01572](https://openairdocs.org/sdr/2002UALA01572), Oct 12, 2002: FRAME. CRACKED. RIGHT HAND BODY STATION 188 FRAME CRACKED AT STRINGER 17 RIGHT HAND. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. - [SDR 2002UALA01571](https://openairdocs.org/sdr/2002UALA01571), Oct 12, 2002: BULKHEAD. CRACKED. RIGHT HAND BODY STATION 178 FUSELAGE CHORD CRACKED AT WL207. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW WEB SECTION REPAIR. - [SDR 2002UALA01546](https://openairdocs.org/sdr/2002UALA01546), Oct 7, 2002: CREASE BEAM. CORRODED. LEFT HAND CREASE BEAM WEB CORRODED BETWEEN BODY STATION 639 AND BODY STATION 663. MAJOR REPAIR ACCOMPLISHED. REPLACED WEB. - [SDR 2002UALA01540](https://openairdocs.org/sdr/2002UALA01540), Oct 6, 2002: INTERCOSTAL. CRACKED. CABIN INTERCOSTAL, OUTBOARD ANGLE CRACKED FORWARD OF BODY STATION 291.5 FRAME AND BELOW STRINGER 11 RIGHT HAND. MAJOR REPAIR ACCOMPLISHED. REPLACED ANGLE. - [SDR 2002UALA01539](https://openairdocs.org/sdr/2002UALA01539), Oct 6, 2002: CREASE BEAM. CORRODED. RIGHT HAND CREASE BEAM WEB CORRODED BETWEEN BODY STATION 616 AND 639. MAJOR REPAIR ACCOMPLISHED. NEW WEB INSTALLED. - [SDR 2002UALA01538](https://openairdocs.org/sdr/2002UALA01538), Oct 6, 2002: CREASE BEAM. CORRODED. RIGHT HAND CREASE BEAM WEB CORRODED BETWEEN BODY STATION 578 AND 597. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW WEB. - [SDR 2002UALA01535](https://openairdocs.org/sdr/2002UALA01535), Oct 4, 2002: FLOORBEAM. CORRODED. FORWARD CABIN STATION 360 RBL 12 FLOORBEAM HAS SURFACE CORROSION. MAJOR REPAIR ACCOMPLISHED, INSTALLED STRAP REPAIR. - [SDR 2002UALA01556](https://openairdocs.org/sdr/2002UALA01556), Oct 3, 2002: SHEAR TIE. CRACKED. CABIN STATION 787 FRAME WEB JUST ABOVE STRINGER 9R SHEAR TIE IS CRACKED. MAJOR REPAIR ACCOMPLISHED. J ANGLE REPAIR. - [SDR 2002UALA01531](https://openairdocs.org/sdr/2002UALA01531), Oct 3, 2002: FRAME. CRACKED. CABIN STATION 787 FRAME WEB JUST ABOVE STRINGER 9R SHEAR TIE IS CRACKED. MAJOR REPAIR ACCOMPLISHED. REPAIR ANGLE INSTALLED ON FRAME. - [SDR 2002UALA01528](https://openairdocs.org/sdr/2002UALA01528), Oct 2, 2002: FRAME. CRACKED. CABIN STATION 400 FRAME IS CRACKED AT STATION 9L PASSENGER SERVICE UNIT - VENT SUPPORT INBOARD FASTENER. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. - [SDR 2002UALA01525](https://openairdocs.org/sdr/2002UALA01525), Oct 1, 2002: SPLICE. CRACKED. CABIN 907 STRINGER 4L STRINGER SPLICE IS CRACKED AT TWO FASTENERS. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW SPLICE. - [SDR 2002UALA01524](https://openairdocs.org/sdr/2002UALA01524), Oct 1, 2002: FRAME. CRACKED. CABIN STATION 807 FRAME WEB ABOVE STRINGER 9R SHEAR TIE IS CRACKED. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. - [SDR 2002UALA01523](https://openairdocs.org/sdr/2002UALA01523), Oct 1, 2002: FRAME. CRACKED. CABIN STATION 480 FRAME IS CRACKED AT STRINGER 9L PASSENGER SERVICE UNIT VENT SUPPORT INBOARD FASTENER. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. - [SDR 2002UALA01522](https://openairdocs.org/sdr/2002UALA01522), Oct 1, 2002: FRAME. CRACKED. CABIN STATION 827 FRAME WEB ABOVE STRINGER 9L SHEAR TIE IS CRACKED. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. - [SDR 2002UALA01521](https://openairdocs.org/sdr/2002UALA01521), Oct 1, 2002: CREASE BEAM. CORRODED. AFT CABIN RIGHT HAND SIDE FLOOR CREASE BEAM CORRODED BETWEEN STA 947-990 JUST INBOARD OF DOOR 2 RIGHT HAND BELOW DRAIN GUTTER. MAJOR REPAIR ACCOMPLISHED. REPLAC - [SDR 2002UALA01517](https://openairdocs.org/sdr/2002UALA01517), Sep 30, 2002: SPLICE. CRACKED. CABIN STATION 907 STRINGER 4R STRINGER SPLICE IS CRACKED AT 2 FASTENERS. MAJOR REPAIR ACCOMPLISHED. REPLACE STRINGER SPLICE. - [SDR 2002UALA01510](https://openairdocs.org/sdr/2002UALA01510), Sep 29, 2002: FRAME. CRACKED. CABIN STATION 440 FRAME IS CRACKED AT STRINGER 10L IN RADIUS JUST INBOARD OF STRINGER CLIP. MAJOR REPAIR ACCOMPLISHED. FUSELAGE FRAME REPAIR INSTALLED. - [SDR 2002UALA01509](https://openairdocs.org/sdr/2002UALA01509), Sep 28, 2002: FRAME. CRACKED. CABIN STATION 887 FRAME WEB ABOVE STRINGER 9R SHEAR TIE IS CRACKED. REPAIR ANGLE INSTALLED ON FRAME. - [SDR 2002UALA01508](https://openairdocs.org/sdr/2002UALA01508), Sep 28, 2002: FLOORBEAM. CRACKED. CABIN FLOOR BEAM INTERCOSTAL UPPER FLANGE IS CRACKED BODY STATION 500D-520, BL0, WL208. MAJOR REPAIR ACCOMPLISHED. REPLACED INTERCOSTAL UPPER FLANGE . - [SDR 2002UALA01507](https://openairdocs.org/sdr/2002UALA01507), Sep 28, 2002: FRAME. CRACKED. CABIN STATION 480 FRAME IS CRACKED AT STRINGER 9R AT PASSENGER SERVICE UNIT-VENT SUPPORT INBOARD FASTENER. MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR. - [SDR 2002UALA01505](https://openairdocs.org/sdr/2002UALA01505), Sep 28, 2002: STRINGER CLIP. CRACKED. STATION 727A STRINGER CLIP CRACKED STRINGER 6R. MAJOR REPAIR ACCOMPLISHED. REPLACED CLIP. - [SDR 2002UALA01504](https://openairdocs.org/sdr/2002UALA01504), Sep 28, 2002: STRINGER CLIP. CRACKED. STATION BODY STATION 616 STRINGER CLIP CRACKED 4L STRINGER. MAJOR REPAIR ACCOMPLISHED. REPLACED CLIP. - [SDR 2002UALA01503](https://openairdocs.org/sdr/2002UALA01503), Sep 28, 2002: FRAME. CRACKED. CABIN STATION 887 FRAME WEB ABOVE STRINGER 9L SHEAR TIE, IS CRACKED. REPAIR ANGLE INSTALLED ON FRAME. - [SDR 2002UALA01502](https://openairdocs.org/sdr/2002UALA01502), Sep 28, 2002: FRAME. CRACKED. CABIN STATION 827 FRAME WEB ABOVE STRINGER 9R SHEAR TIE IS CRACKED. MAJOR REPAIR ACCOMPLISHED. REPAIR ANGLE INSTALLED ON FRAME. - [SDR 2002UALA01495](https://openairdocs.org/sdr/2002UALA01495), Sep 26, 2002: FRAME. CRACKED. CABIN FRAME WEB CRACKED BODY STATION 807 STRINGER 9L WL 258. MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR ON FRAME. - [SDR 2002UALA01558](https://openairdocs.org/sdr/2002UALA01558), Sep 21, 2002: FLOORBEAM. CORRODED. AFT CABIN STATION 1016 FLOORBEAM UPPER CHORD LBL 7 TO 11 HAS EXCESSIVE MATERIAL LOSS DUE TO BLEND REMOVAL OF CORROSION. MAJOR REPAIR ACCOMPLISHED. REPAIR STRAP - [SDR 2001UALA02347](https://openairdocs.org/sdr/2001UALA02347), Nov 28, 2001: BULKHEAD. CRACKED. STATION 178 BULKHEAD RBL 5.7 AT WL 210 HAS CRACK INDICATION. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. FABRICATED FILLER AND DOUBLER AND INSTALLED. - [SDR 2001UALA02346](https://openairdocs.org/sdr/2001UALA02346), Nov 28, 2001: BULKHEAD. CRACKED. STATION 178 BULKHEAD LBL 5.7 AT WL 210 HAS CRACK INDICATION. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. FABRICATED FILLER AND DOUBLER AND INSTALLED. - [SDR 2001UALA02345](https://openairdocs.org/sdr/2001UALA02345), Nov 27, 2001: BULKHEAD. CRACKED. STATION 178 BULKHEAD RBL 5.7 WL 200 HAS 2 EA CRACKS. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER AND FILLER. - [SDR 2001UALA02331](https://openairdocs.org/sdr/2001UALA02331), Nov 27, 2001: BULKHEAD. CRACKED. STATION 178 BULKHEAD RBL 5.7 WL 200 HAS 2 CRACK INDICATIONS FOUND BY NONDESTRUCTIVE TESTING. MAJOR REPAIR ACCOMPLISHED, FABRICATED AND INSTALLED DOUBLER AND FIL - [SDR 2000UALA00416](https://openairdocs.org/sdr/2000UALA00416), Jul 13, 2000: SENSOR. FAILED. NORMAL AND ALTERNATE EQUIPMENT COOLING WARNING LIGHTS ILLUMINATED. *S/D* M100 LOW FLOW INSTRUMENT COOLING SENSOR FAILED. REPLACED M100 LOW FLOW INSTRUMENT COOLI - [SDR 98UAL900520](https://openairdocs.org/sdr/98UAL900520), Oct 30, 1998: ELEMENT. FAILED. APU FIRE LIGHT CAME ON. NO EXTERIOR INDICATIONS. REPLACED APU TAIL PIPE OVER HEAT SENSING ELEMENT AND WIRE HARNESS FOR OVER HEAT ELEMENT, REF MM 26-15-14. TESTE - [SDR 98UAL900421](https://openairdocs.org/sdr/98UAL900421), Aug 31, 1998: SENSOR. OUT OF ADJUST. CARGO DOOR WARNING LIGHT ILLUMINATED. *S/D* ADJUSTED SENSOR TARGET. - [SDR 98UAL900251](https://openairdocs.org/sdr/98UAL900251), Jun 10, 1998: TRIM. FAILED. CREW DIVERTED TO BNA DUE TO INOPERATIVE HORIZONTAL STABILIZER TRIM. - [SDR 97UAL900793](https://openairdocs.org/sdr/97UAL900793), Oct 24, 1997: CONTROLLER. FAILED. UNABLE TO PRESSURIZE AIRCRAFT AFTER TAKEOFF. AIRCRAFT WAS OPERATING IN AUTO MODE, SWITCHED TO STANDBY AND CABIN STILL CONTINUED TO CLIMB 500 FPM. OUTFLOW VALVE - [SDR 97UAL900556](https://openairdocs.org/sdr/97UAL900556), Jul 16, 1997: TIRE. FAILED. TIRE TREAD LOSS ON TAKEOFF. SURROUNDING GEAR DOORS WERE DAMAGED. *S/D* REPLACED NR 3 AND NR 4 MLG TIRES DUE TO NR 4 TIRE THROWING TREAD. DAMAGE INCURRED TO RT M - [SDR 96UAL900763](https://openairdocs.org/sdr/96UAL900763), Sep 30, 1996: LIGHT. FAILED. ONE SECTION OF EMERGENCY EGRESS LIGHTING INOP ROW 12. INSTALLED NEW LIGHT SECTION, OPERATION CHECKS NORMAL. - [SDR 95UAL900209](https://openairdocs.org/sdr/95UAL900209), Oct 17, 1995: VALVE. STICKING. ABORTED TAKEOFF AT LGA AT 75 KNOTS DUE TO NR 2 ENGINE BLEED PROBLEM. REPLACED NR TWO ENGINE HIGH-STAGE VALVE. ALSO, REPLACED NR ONE ENGINE HIGH-STAGE VALVE AND ## 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 19981226044699I](https://openairdocs.org/incident/19981226044699I), Dec 26, 1998: Boeing 737300 (N352UA), Jackson, WY. This is a report concerning the united air lines B-737-300 that went off the runway at Jackson Hole, Wyoming on 12/26/98. Ual flight 1956 lax/jac was under the… - [Incident 19980610024089I](https://openairdocs.org/incident/19980610024089I), Jun 10, 1998: Boeing 737322 (N352UA), Nashville, TN. Diverted to bna due to inoperative horizontal stabilizer trim system. ## Other aircraft with N352UA - [Registered now](https://openairdocs.org/aircraft/N352UA): Hybrid Project SUPERVOLO GEN 4, S/N SV4-00-036 --- 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.