# N339US: 1986 Boeing 737-301, registration cancelled 2003-11-19 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: November 19, 2003 - Exported to: Malaysia - Status when cancelled: Valid registration - Airframe: [Boeing 737-301](https://openairdocs.org/model/boeing-737-301) (registry code 138447R) - Engine: [Amateur-built UNKNOWN ENG](https://openairdocs.org/engine/amateur-built-unknown-eng) (registry code 99999) - Data sheets: [TCDS A16WE](https://openairdocs.org/tcds/A16WE) (OpenAirDocs) - Serial number: 23236 - Year built: 1986 - Type of aircraft: Fixed wing multi engine - Airworthiness: Standard, transport - Airworthiness date: May 1, 1986 - Certificate issued: April 25, 2003 - Last registry action: April 25, 2003 - Mode S code: A3B911 - Owner when cancelled: [Afs Investments Xliii LLC](https://openairdocs.org/faa-owner/AFS%20INVESTMENTS%20XLIII%20LLC) - Location: [Stamford, CT](https://openairdocs.org/faa-place/CT/Stamford) - Owner type: Corporation - Owner's area on the map: 41.0534° N, 73.5387° W: Placed by OpenAirDocs: center of Stamford, CT, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N339US - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=339US - Page: https://openairdocs.org/deregistered/N339US-2003-11-19 From the FAA registry file of October 29, 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 737-301: https://openairdocs.org/model/boeing-737-301.md ## Service difficulty reports (38) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR USAASB02192](https://openairdocs.org/sdr/USAASB02192), Oct 23, 2002: SAFETY SWITCH. FAILED. PIT - FLT 1591 - EN ROUTE, SEVERAL DISCREPANCIES THAT INDICATE THE A/C LOGIC WAS IN GROUND MODE. CB`S WERE NORMAL. AIRCRAFT STARTED TO DEPRESSURIZE AT FL280. NO - [SDR USAA011052](https://openairdocs.org/sdr/USAA011052), Aug 9, 2001: SKIN. CLT - FOUND SKIN DAMAGED 1 INCH, BETWEEN BS 28L AND BS 28R BS 380. INSTALLED .100 INCH THICK 2024 T3 DOUBLER PER TR 53-30-07, SB 737-53-1117 REV 1. (M) - [SDR USAA011066](https://openairdocs.org/sdr/USAA011066), Aug 6, 2001: SKIN. CRACKED. TPA - FOUND 1 INCH CRACK IN SKIN AFT OF EQUIPMENT COOLING EXH, LOWER LOBE SKIN BETWEEN S28L AND 28R STATION 380. INSTALLED DOUBLER PER TYPICAL REPAIR 53-30-07, - [SDR USAA010418](https://openairdocs.org/sdr/USAA010418), Mar 31, 2001: DOOR FRAME. CRACKED. PIT - FOUND FORWARD CORNER FRAME CRACKED 1 INCH AND .25 INCH, FORWARD CARGO DOOR LOWER FWD CORNER TOP FLANGE. DEFECTIVE PART REPLACED WITH IDENTICAL PART NR PER - [SDR USAASB01014](https://openairdocs.org/sdr/USAASB01014), Jan 21, 2001: REGULATOR. FAILED. BWI - FLT 1801 - EN ROUTE FROM BOS-ATL, THE CREW HAD TROUBLE MAINTAINING CABIN PRESSURIZATION. AT FL230, THE RIGHT BLEED PRESSURE WENT TO 30 PSI WHILE THE LEFT - [SDR USAA001392](https://openairdocs.org/sdr/USAA001392), Aug 29, 2000: SKIN. CRACKED. TPA - FOUND SKIN CRACKED .800 INCH, AFT SERVICE LOWER HINGE CUTOUT STATION 947.5 STRINGER 10R. INSTALLED DOUBLER PER SRM 53-60-01 FIG 207. (M) - [SDR USAASB99238](https://openairdocs.org/sdr/USAASB99238), Sep 27, 1999: FAIRING. MISSING. BOS - FLT 8053 - FLIGHT RETURNED TO FIELD AT BOS DUE TO A LOUD HIGH PITCH HUMMING NOISE AND VIBRATION AROUND CABIN WINDOW AT SEAT ROW 9ABC. VIBRATION AND HUMMIN - [SDR USAA990926](https://openairdocs.org/sdr/USAA990926), Sep 3, 1999: ANGLE. CORRODED. CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH FORWARD OF STATION 251 FRAME, RBL 16, WL 157 ALONG INBOARD ROW OF FASTENERS RIGHT LOWER CHORD A - [SDR USAA990910](https://openairdocs.org/sdr/USAA990910), Sep 3, 1999: CHORD. CORRODED. CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND CORROSION AT STATION 270, RBL 2.5 - LBL 2.5 Z-CHORD. CORROSION LEVEL 1. REPAIRED REPLACEMENT 'Z' CHORD PER EA 65 - [SDR USAA990882](https://openairdocs.org/sdr/USAA990882), Sep 3, 1999: WEB. CRACKED. CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK SHEAR BEAM WEB SHELF 18A AFT WW BULKHEAD. INSTALLED DOUBLER PER EA 65323. (M) - [SDR USAA990877](https://openairdocs.org/sdr/USAA990877), Sep 3, 1999: SKIN. CRACKED. CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK AFT SERVICE DOOR FORWARD EDGE 30 INCH BELOW TOP SKIN. INSTALLED DOUBLER PER SRM 52-10-01. (M) - [SDR USAA990876](https://openairdocs.org/sdr/USAA990876), Sep 3, 1999: FLOORBEAM. CORRODED. CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .25 INCH BY .25 INCH AREA OF CORROSION STATIO N1006, LBL 26 FLOORBEAM. CORROSION LEVEL 1. INSTALLED REPAIR STR - [SDR USAA990875](https://openairdocs.org/sdr/USAA990875), Sep 3, 1999: FLOORBEAM. CORRODED. CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A 1 INCH BY 1 INCH AREA OF CORROSION LBL 21, 28, 35, 42 AND 45, BS 344, WL 208.1 FLOORBEAM. CORROSION LEVEL 1. I - [SDR USAA990855](https://openairdocs.org/sdr/USAA990855), Sep 3, 1999: ANGLE. CRACKED. CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A CRACK AT BS 289.5 STRINGER 10R WEB ANGLE. INSTALLED NEW WEB ANGLE PER SRM 51-10-02. (M) - [SDR USAA990843](https://openairdocs.org/sdr/USAA990843), Sep 3, 1999: TIE CLIP. CRACKED. CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK STATION 616, STRINGER 8L TIE CLIP. REPLACED CLIP PER SRM 51-40-02. (M) - [SDR USAA990842](https://openairdocs.org/sdr/USAA990842), Sep 3, 1999: TIE CLIP. CRACKED. CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK STATION 616, STRINGER 4R TIE CLIP. REPLACED CLIP PER SRM 51-40-02. (M) - [SDR USAA990841](https://openairdocs.org/sdr/USAA990841), Sep 3, 1999: CLIP. CRACKED. CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A CRACKED CLIP STATION 663.75 AT STRINGER 10R. REPLACED CLP PER SRM 51-10-02. (M) - [SDR USAA990840](https://openairdocs.org/sdr/USAA990840), Sep 3, 1999: CLIP. CRACKED. CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A CRACKED CLIP STATION 727D STRINGER 4R. REPLACED CLIP PER SRM 51-10-02. (M) - [SDR USAA990839](https://openairdocs.org/sdr/USAA990839), Sep 3, 1999: FRAME. CRACKED. CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AT STATION 887, STRINGER 9L FRAME. INSTALLED DOUBLER PER SRM 53-00-07 FIG 202. (M) - [SDR USAA990838](https://openairdocs.org/sdr/USAA990838), Sep 3, 1999: SPLICE. CRACKED. CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AT STATION 907, STRINGER 5R SPLICE. REPLACED SPLICE PER SRM 51-00-02. (M) - [SDR USAA990837](https://openairdocs.org/sdr/USAA990837), Sep 3, 1999: SPLICE. CRACKED. CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AT STATION 907, STRINGER 4L SPLICE. REPLACED SPLICE PER SRM 51-00-02. (M) - [SDR USAA990824](https://openairdocs.org/sdr/USAA990824), Sep 3, 1999: SHEAR TIE. CRACKED. CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK IN SHEAR TIE STATION 639 STRINGER 7R AND 8R. REPAIRED PER SRM 51-40-02. (M) - [SDR USAA990823](https://openairdocs.org/sdr/USAA990823), Sep 3, 1999: FRAME. CRACKED. CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STATION 727D STRINGER 7R FRAME AND TIE CLIP. INSTALLED NEW TIE CLIP PER SRM 51-10-02. (M) - [SDR USAA990822](https://openairdocs.org/sdr/USAA990822), Sep 3, 1999: FRAME. CRACKED. CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STATION 727A STRINGER 3R FRAME AND TIE CLIP. INSTALLED NEW TIE CLIP PER SRM 51-10-02. (M) - [SDR USAA990821](https://openairdocs.org/sdr/USAA990821), Sep 3, 1999: TIE CLIP. CRACKED. CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STATION 639 STRINGER 5L TIE CLIP. INSTALLED NEW TIE CLIP PER SRM 51-40-02. (M) - [SDR USAASB99164](https://openairdocs.org/sdr/USAASB99164), Jul 6, 1999: ENGINE. FATIGUED. BOS - FLT 221 - JUST AFTER TAKEOFF, CREW ENCOUNTERED A WINDSHEAR ON DEPARTURE AND APPLIED FIREWALL POWER FOR A PERIOD APPROXIMATELY 10 SECONDS. CAPTAIN FELT HE - [SDR USAA990221](https://openairdocs.org/sdr/USAA990221), Mar 2, 1999: SKIN. CRACKED. CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK EXTERNAL SKIN FORWARD SERVICE DOOR LOWER HINGE CUTOUT. INSTALLED DOUBLER PER EA 64060 AND SB 52 - [SDR USAA980344](https://openairdocs.org/sdr/USAA980344), Aug 17, 1998: SKIN. CRACKED. CLT - DURING DAILY CHECK VISUAL INSPECTION, FOUND A 5 INCH CRACK BL 0 BETWEEN STATION 727D AND 727E ON FUSELAGE SKIN. INSTALLED DOUBLER PER SRM 53-00-01. (M) - [SDR USAASB97266](https://openairdocs.org/sdr/USAASB97266), Sep 25, 1997: LIGHT. INOPERATIVE. CLT - EXIT LIGHT INOPERATIVE AT SEAT 10 A,B,C. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD. (X) - [SDR USAASB97235](https://openairdocs.org/sdr/USAASB97235), Aug 28, 1997: BATTERY PACK. DISCHARGED. DCA - FIRST CLASS LOW LEVEL LIGHTING FOUND INOP DURING RON MAINTENANCE. REPLACED BATTERY PACK. SYSTEM OPERATIONALLY CHECKED OK. (M) - [SDR USAA951010](https://openairdocs.org/sdr/USAA951010), Sep 21, 1995: FLOOR BEAM. CORROSION. INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION EXCEEDING LIMITS AROUND HOLE, BS 958 RBL 7.5. FABRICATED NEW INTERCOSTAL FROM BAC1506-437075-T6 AND IN - [SDR USAA951013](https://openairdocs.org/sdr/USAA951013), Sep 19, 1995: ANGLE. CORROSION. INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 20 INCHES AT BS 947.5 TO BS 992.5 LBL 53 AFT ENTRY DOOR. REPAIRED PER BOEING DRAWING 65-5287 - [SDR USAA951011](https://openairdocs.org/sdr/USAA951011), Sep 13, 1995: ANGLE. CORROSION. INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 5 INCHES AT STATION 370 AT FORWARD ENTRY THRESHOLD. REPLACED Z-ANGLE. REPAIRED PER BOEING DR - [SDR USAA951009](https://openairdocs.org/sdr/USAA951009), Sep 13, 1995: FLOOR BEAM. CORROSION. INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 2 INCHES AT STATION 294.5 LBL 20 INCHES. CUT OUT CORROSION AND INSTALLED DOUBLER AND FILLER. - [SDR USAA951012](https://openairdocs.org/sdr/USAA951012), Sep 12, 1995: ANGLE. CORROSION. INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 24 INCHES AT FORWARD SERVICE DOOR THRESHOLD. REPLACED Z-ANGLE. REPAIRED PER BOEING DRAWING N - [SDR USAA951007](https://openairdocs.org/sdr/USAA951007), Sep 8, 1995: FLOOR BEAM. CORROSION. INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 18 INCHES STATION 986.5 BL ZERO TO LBL 24 INCHES. REPLACED UPPER T-CAP. REPAIRED PER SRM 53- - [SDR USAA951008](https://openairdocs.org/sdr/USAA951008), Sep 6, 1995: FLOOR BEAM. CORROSION. INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 36 INCHES STATION 344 LBL 24 INCHES TO RBL 12 INCHES. REPLACED UPPER T-CAP OF BEAM. REPAIRED - [SDR USAA950384](https://openairdocs.org/sdr/USAA950384), Apr 19, 1995: EEL ASSY. INOPERATIVE. PIT - EMERGENCY EXIT LIGHT AT EXIT ROW INOPERATIVE. MAINTENANCE REPLACED EMERGENCY EXIT LIGHT AT EXIT ROW. OPS CHECKS NORMAL. (W) ## FAA accident and incident reports (3) 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 19920223015669I](https://openairdocs.org/incident/19920223015669I), Feb 23, 1992: Boeing 737301 (N339US), Los Angeles, CA. Cleared and landed on runway 24R. Another aircraft made a go around as it also assigned 24R sidestep to 24L. - [Incident 19890826058269I](https://openairdocs.org/incident/19890826058269I), Aug 26, 1989: Boeing 737301 (N339US), Dayton, OH, Minor damage. Stabilizer struck jetway while taxiing out of gate area. Marshal giving instructions. Jetway out of position. - [Incident 19890110008739I](https://openairdocs.org/incident/19890110008739I), Jan 10, 1989: Boeing 737301 (N339US), West Palm Beach, FL. Smoke from cabin and cockpit ducting. Nose wheel APU warning. Passengers evacuated. Suspect oil seal leak. ## Other aircraft with N339US - [Cancelled 2011-02-08](https://openairdocs.org/deregistered/N339US-2011-02-08): North American F-51D, S/N 45-11464. Assigned, pending cancellation --- 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.