# N337US: 1986 Boeing 737-301, registration cancelled 2003-12-04

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: December 4, 2003
- Exported to: Malaysia
- Status when cancelled: Valid registration
- Airframe: [Boeing 737-301](https://openairdocs.org/model/boeing-737-301) (registry code 138447R)
- 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: 23235
- Year built: 1986
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: April 3, 1986
- Certificate issued: April 25, 2003
- Last registry action: April 25, 2003
- Mode S code: A3B1A3
- 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/N337US
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=337US
- Page: https://openairdocs.org/deregistered/N337US-2003-12-04

From the FAA registry file of October 28, 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 (57, newest 50)

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

- [SDR USAA020359](https://openairdocs.org/sdr/USAA020359), Sep 4, 2002: SKIN. CRACKED. CLT - FOUND SKIN CRACKED 2.1 INCH, S23R AT STATION 727D PLUS 4. INSTALLED DOUBLER AND TRIPLER PER EA 74734. (M)
- [SDR USAA020358](https://openairdocs.org/sdr/USAA020358), Aug 31, 2002: SKIN. CRACKED. CLT - FOUND SKIN CRACKED 1 INCH, S22L AT STATION 727D PLUS 13. INSTALLED DOUBLER PER SRM 53-00-01 FIG 201. (M)
- [SDR USAASB02135](https://openairdocs.org/sdr/USAASB02135), Jul 17, 2002: BATTERY PACK. INOPERATIVE. PHL - MAINTENANCE FOUND THE EMERGENCY EXIT LIGHT ABOVE THE AFT LEFT ENTRY DOOR INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK
- [SDR USA2002F00044](https://openairdocs.org/sdr/USA2002F00044), Jun 1, 2002: LANDING GEAR. OUT OF RIG. IN PREPARATION FOR LANDING, CREW EXPERIENCED A LANDING GEAR INDICATION PROBLEM. GREW RECEIVED 3 GREEN AND 3 RED LANDING GEAR LIGHTS WHEN SELECTING GEAR DOWN. CR
- [SDR USAASB02084](https://openairdocs.org/sdr/USAASB02084), Apr 27, 2002: CONTROL HANDLE. LACK OF LUBE. PHL - FLT 577 - ON GEAR EXTENSION FOR LANDING, CREW RECEIVED THREE GREEN LIGHTS AND THEN THREE RED LIGHTS. CREW EXECUTED A MISSED APPROACH AND CYCLED THE GEAR. 
- [SDR USAASB01351](https://openairdocs.org/sdr/USAASB01351), Dec 26, 2001: BATTERY PACK. DISCHARGED. GSO - MAINTENANCE FOUND THE EMERGENCY LIGHTS IN FIRST CLASS EXTINGUISH AFTER A SHORT PERIOD OF OPERATION. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPE
- [SDR USAASB01336](https://openairdocs.org/sdr/USAASB01336), Dec 4, 2001: DOWNLOCK SENSOR. INTERMITTENT. CLT - FLT 841 - ON APPROACH TO CLT, WHEN THE GEAR WAS EXTENDED, THE CREW RECEIVED GREEN INDICATIONS FOR THE MAIN GEAR AND RED FOR THE NOSE GEAR. ON THE GO-AROUN
- [SDR USAA011296](https://openairdocs.org/sdr/USAA011296), Sep 10, 2001: FRAME. CRACKED. CLT - FOUND CHORD CRACKED .25 INCH, BS 178 WL 207 LBL 26 AND RBL 26. DAMAGE AREAS WERE CUTOUT, SIDE CHORD SPLICE REPAIRS INSTALLED PER EO 5300V157. (M)
- [SDR USAA011297](https://openairdocs.org/sdr/USAA011297), Sep 10, 2001: WEB. CRACKED. CLT - FOUND WEB CRACKED .5 INCH, BS 178 WL 213 RBL 6 AND WL 207 LBL 1. INSTALLED REPAIR DOUBLER PER EO 5300V153. (M)
- [SDR USAA010760](https://openairdocs.org/sdr/USAA010760), Jun 30, 2001: SKIN. CRACKED. CLT - FOUND SKIN CRACKED 2 INCHES, BS 727E, STRINGER 22R AND 23R. DAMAGE REMOVED, REPAIR DOUBLER AND TRIPLER INSTALLED PER EA 71604. (M)
- [SDR USAASB01010](https://openairdocs.org/sdr/USAASB01010), Jan 18, 2001: WIRE. DISCONNECTED. PIT - FLT 276 - AFTER TAKEOFF FROM AVP, EN ROUTE TO PIT, THE LANDING GEAR HANDLE WOULD NOT MOVE BEYOND THE OFF POSITION. CREW FOLLOWED QUICK REFERENCE HANDBOOK 
- [SDR USAASB00147](https://openairdocs.org/sdr/USAASB00147), May 22, 2000: UNKNOWN. ODOR. CLT - FLT 2151 - AFTER TAKEOFF, CREW NOTED A RUBBER LIKE SMELL IN THE CABIN. FLIGHT RETURNED TO CLT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED T
- [SDR USAASB00138](https://openairdocs.org/sdr/USAASB00138), May 8, 2000: FIRE LOOP. FAILED. PIT - FLT 2004 - ON CLIMB-OUT FROM PIT, EN ROUTE TO LGA, THE CREW NOTED AN ENGINE OVERHEAT WARNING ON THE NR 2 ENGINE. THE A LOOP FOR THE NR 2 ENGINE WAS ON MEL
- [SDR USAASB99296](https://openairdocs.org/sdr/USAASB99296), Dec 17, 1999: MEC. FAULTY. CLT - FLT 299 - ON CLIMB-OUT FROM CLT, AT FL210, THE NR 1 ENGINE N1 INDICATOR BEGAN FLUCTUATING IN ALL PARAMETERS OF FLIGHT. THE N1 WOULD SURGE PLUS OR MINUS 7 
- [SDR USAASB99194](https://openairdocs.org/sdr/USAASB99194), Aug 7, 1999: FUSE. BLOWN. PHL - DURING OPERATIONAL TEST OF EMERGENCY LIGHT SYSTEM ON OVERNIGHT CHECK, MAINTENANCE FOUND THE FIRST CLASS SEAT EMERGENCY LIGHTS FAILED TO FULLY ILLUMINATE. 
- [SDR USAA990484](https://openairdocs.org/sdr/USAA990484), Jun 21, 1999: WEB. CRACKED. CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .300 INCH CRACK AT STATION 727 STRINGER 18A LEFT MAIN WHEEL WELL SHEAR WEB. INSTALLED DEFECTIVE PART WITH IDEN
- [SDR USAA990565](https://openairdocs.org/sdr/USAA990565), Jun 21, 1999: BULKHEAD. CRACKED. CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .5 INCH, 1 INCH AND .75 INCH CRACK AT STATION 178 RIGHT SIDE PLUS 6 INCHES WL 200 AT 4.75 AND 6.75 BULKHEAD. I
- [SDR USAA990573](https://openairdocs.org/sdr/USAA990573), Jun 21, 1999: SKIN. CORRODED. CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 12 INCH AREA OF FUSELAGE OF CORROSION BETWEEN NR 3 VHF ANTENNA MOUNT STATION 727D PLUS 3 TO 727D PLUS 15 AND I
- [SDR USAA990574](https://openairdocs.org/sdr/USAA990574), Jun 21, 1999: FLOORBEAM. CORRODED. CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 20 INCH AREA OF CORROSION BS 270, LBL 10 - RBL 10 FLOOR SUPPORT. INSTALLED NEW Z-ANGLE PER TR 53-20-04 AND EA 
- [SDR USAA990575](https://openairdocs.org/sdr/USAA990575), Jun 21, 1999: FLOORBEAM. CORRODED. CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 2 INCH BY 3 INCH AREA OF CORROSION ON T-CAP AND AROUND NUT PLATE HOLES AT BS 294.5 FROM LBL 12 TO RBL 7. CORRO
- [SDR USAA990576](https://openairdocs.org/sdr/USAA990576), Jun 21, 1999: CHANNEL. CORRODED. CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 1 INCH AREA OF CORROSION AT BS 986.5 RBL 24 HOT CHANNEL. CORROSION LEVEL 2. INSTALLED FABRICATED PART PER SRM 
- [SDR USAA990578](https://openairdocs.org/sdr/USAA990578), Jun 21, 1999: FLOORBEAM. CORRODED. CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 6 INCH AREA OF CORROSION AT STATION 986.5 LBL 24 FLOORBEAM, CORROSION LEVEL 2. FABRICATED NEW PART PER SRM 51-
- [SDR USAA990579](https://openairdocs.org/sdr/USAA990579), Jun 21, 1999: FRAME. CORRODED. CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 6 INCH AREA OF CORROSION ON INBOARD J CHANNEL BS 993.5 FRAME AT WL 208.1, CORROSION LEVEL 2. INSTALLED DOUBLER
- [SDR USAA990580](https://openairdocs.org/sdr/USAA990580), Jun 21, 1999: WEB. CORRODED. CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 2 INCH AREA OF CORROSION AFT RIGHT LAV FILL CONN ON FLOOR WEB, CORROSION LEVEL 2. NEW WEB INSTALLED PER SRM 51
- [SDR USAA990581](https://openairdocs.org/sdr/USAA990581), Jun 21, 1999: FLOORBEAM. CORRODED. CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND 60 INCH AREA OF CORROSION AT STATION 986.5 FLOORBEAM. INSTALLED UPPER T-CAP PER SRM 53-00-51. (M)
- [SDR USAA990582](https://openairdocs.org/sdr/USAA990582), Jun 21, 1999: FLOORBEAM. CORRODED. CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND 1 INCH AREA OF CORROSION AT BS 312, LBL 12 T-CAP. CORROSION LEVEL 2, CORROSION TASK NR C53-107-02. FABRICATED T-
- [SDR USAA990583](https://openairdocs.org/sdr/USAA990583), Jun 21, 1999: FLOORBEAM. CORRODED. CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND 1 INCH AREA OF CORROSION AT BS 312, LBL1 AND LBL 11 FLOORBEAM. CORROSION LEVEL 2, CORROSION TASK NR C53-107-02. 
- [SDR USAA990584](https://openairdocs.org/sdr/USAA990584), Jun 21, 1999: FLOORBEAM. CORRODED. CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND 1 INCH AREA OF CORROSION AT BS 312, BL 0 LBL 7 AND RBL 8 FLOORBEAM, CORROSION LEVEL 2, CORROSION TASK NR C53-107
- [SDR USAA990617](https://openairdocs.org/sdr/USAA990617), Jun 21, 1999: SKIN. CRACKED. CLT - DURING Q-1 CHECK, FOUND .75 INCH CRACK ON SKIN AT PILOTS NR 1 WINDOW CUTOUT UPPER OUTBOARD CORNER. FABRICATED DOUBLER PER EA 64783A. (M)
- [SDR USAA990606](https://openairdocs.org/sdr/USAA990606), Jun 21, 1999: SKIN. CRACKED. CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A SMALL SKIN CRACK AT CARGO DOOR HANDLE CUTOUT AFT CARGO DOOR, AFT RADIUS OF HANDLE ACCESS CUTOUT EXTERIOR SKIN.
- [SDR USAA990586](https://openairdocs.org/sdr/USAA990586), Jun 21, 1999: FRAME. CRACKED. CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK AT STATION 727D AT LBL 02 AND RBL 02 FRAME. INSTALLED DOUBLER AND FILLERS PER SRM 53-60-07 AND EA 
- [SDR USAA990585](https://openairdocs.org/sdr/USAA990585), Jun 21, 1999: FRAME. CRACKED. CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND 1.5 INCH CRACK ON FRAME AT STATION 727D AT LBL 2 INCH AT VERTICAL ANGLES FOR ANTENNA MOUNT. CUTOUT CRACK AND INS
- [SDR USAA990564](https://openairdocs.org/sdr/USAA990564), Jun 21, 1999: BULKHEAD. CRACKED. CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK AT STATION 178 BULKHEAD RBL 314 WL 187. INSTALLED DOUBLER PER SRM 53-10-08 FIG 203. (M)
- [SDR USAA990563](https://openairdocs.org/sdr/USAA990563), Jun 10, 1999: FLOORBEAM. CRACKED. CLT - DURING Q-1 CHECK, FOUND 1 INCH CRACK IN LONGITUDINAL FLOORBEAM AT BS 708.5 AND BS 709.5. INSTALLED DOUBLER AND FILLER PER SRM 511-70-13. (M)
- [SDR USAA990561](https://openairdocs.org/sdr/USAA990561), Jun 10, 1999: FLOOR. CRACKED. CLT - DURING Q-1 CHECK, FOUND 1.5 INCH CRACK AND .400 INCH CRACK JUST AFT OF STATION 663.75 BL 32 IN PRESSURE FLOOR PANEL. INSTALLED DOUBLER, FILLER AND ANGLE S
- [SDR USAA990560](https://openairdocs.org/sdr/USAA990560), Jun 10, 1999: FLOORBEAM. CORRODED. CLT - DURING Q-1 CHECK, FOUND 6 CORROSION AT SCREW HOLE IN FLOORBEAM JOGGLE AT BS 860 RBL 8. INSTALLED REPAIR ANGLE PER TYPICAL REPAIR 53-10-06. (M)
- [SDR USAA990559](https://openairdocs.org/sdr/USAA990559), Jun 10, 1999: CLIP. CRACKED. CLT - DURING Q-1 CHECK, FOUND .5 INCH CRACK IN TIE CLIP AT STATION 727A FRAME TO STRINGER 6R. DEFECTIVE PART REPLACED WITH IDENTICAL PART NUMBER PER SRM 51-10-0
- [SDR USAA990558](https://openairdocs.org/sdr/USAA990558), Jun 10, 1999: CLIP. CRACKED. CLT - DURING Q-1 CHECK, FOUND .12 5INCH CRACK IN TIE CLIP AT STATION 727C STRINGER 6L. DEFECTIVE PART REPLACED WITH IDENTICAL PART NR PER SRM 51-10-02. (M)
- [SDR USAA990557](https://openairdocs.org/sdr/USAA990557), Jun 10, 1999: CLIP. CRACKED. CLT - DURING Q-1 CHECK, FOUND .125 INCH CRACKED TIE CLIP AT BS 727A STRINGER 5 RT. DEFECTIVE PART REPLACED WITH IDENTICAL PART NR PER SRM 51-10-02. (M)
- [SDR USAA990556](https://openairdocs.org/sdr/USAA990556), Jun 10, 1999: GUSSET. CRACKED. CLT - DURING Q-1 CHECK, FOUND 3 INCH CRACK IN NOSE GEAR ACT FORWARD ATTACH FITTING GUSSET. REPLACED GUSSET WITH IDENTICAL PART NUMBER. (M)
- [SDR USAA990555](https://openairdocs.org/sdr/USAA990555), Jun 10, 1999: CLIP. CRACKED. CLT - DURING Q-1 CHECK, FOUND .125 INCH CRACK IN TIE CLIP AT STATION 616 STRINGER 4L. DEFECTIVE PART REPLACED WITH IDENTICAL PART NR PER SRM 51-10-02. (M)
- [SDR USAA990554](https://openairdocs.org/sdr/USAA990554), Jun 10, 1999: CLIP. CRACKED. CLT - DURING Q-1 CHECK, FOUND .125 INCH CRACK IN TIE CLIP AT STATION 616 STRINGER 8L. DEFECTIVE PART REPLACED WITH IDENTICAL PART NR PER SRM 51-10-02. (M)
- [SDR USAA990553](https://openairdocs.org/sdr/USAA990553), Jun 10, 1999: CLIP. CRACKED. CLT - DURING Q-1 CHECK, FOUND CRACKED TIE CLIP .125 INCH CRACK AT BS 706 STRINGER 2L. DEFECTIVE PART REPLACED WITH IDENTICAL PART NR PER SRM 51-10-02. (M)
- [SDR USAA990551](https://openairdocs.org/sdr/USAA990551), Jun 10, 1999: CLIP. CRACKED. CLT - DURING Q-1 CHECK, FOUND CRACKED TIE CLIP .125 INCH AT BS 663 STRINGER 10 RIGHT. DEFECTIVE PART REPLACED WITH IDENTICAL PART NR PER SRM 51-10-02. (M)
- [SDR USAA990550](https://openairdocs.org/sdr/USAA990550), Jun 10, 1999: CLIP. CRACKED. CLT - DURING Q-1 CHECK, FOUND TWO .5 INCH CRACKS IN TIE CLIP AT BS 663 FRAME TO S-10L TIE CLIP. DEFECTIVE PART REPLACED WITH IDENTICAL PART NR PER SRM 51-10-02.
- [SDR USAA990549](https://openairdocs.org/sdr/USAA990549), Jun 10, 1999: STRINGER. CRACKED. CLT - DURING Q-1 CHECK, FOUND 2 INCH CRACK IN STRINGER 4L AT STATION 907 ABOVE TIE CLIP AT STRINGER 4L. INSTALLED SPLICE ANGLE PER EA 64679 AND SRM 51-10-02. (M
- [SDR USAA990514](https://openairdocs.org/sdr/USAA990514), Jun 10, 1999: CLIP. CRACKED. CLT - DURING Q-1 CHECK, FOUND .250 INCH CRACK IN TIE CLIP AT BS 727D STRINGER 5 LEFT. DEFECTIVE PART REPLACED WITH IDENTICAL PART NUMBER PER SRM PARA 4. (M)
- [SDR USAA980660](https://openairdocs.org/sdr/USAA980660), Dec 23, 1998: SKIN. CRACKED. TPA - DURING A CX-2 CHECK VISUAL INSPECTION, FOUND A .3125 INCH CRACK IN SKIN AT BS 375 AND BL 0. INSTALLED DOUBLER PER TR 53-30-07. (M)
- [SDR USAASB98196](https://openairdocs.org/sdr/USAASB98196), Jul 24, 1998: BATTERY PACK. DISCHARGED. IAH - MAINTENANCE FOUND THE EMERGENCY EXIT LIGHT AT THE AFT RIGHT SERVICE DOOR INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. 
- [SDR USAASB97205](https://openairdocs.org/sdr/USAASB97205), Jul 20, 1997: LIGHT. INOPERATIVE. PHL - MAINTENANCE FOUND THE EMERGENCY SEAT LIGHTING AT SEAT ROW 10 ABC INTERMITTENT/INOP. MAINTENANCE FOUND A LOOSE WIRE/BAD CONNECTION AT LIGHT ASSEMBLY. REPLA

All 57: https://openairdocs.org/deregistered/N337US-2003-12-04/reports.md

## 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 20021013032329I](https://openairdocs.org/incident/20021013032329I), Oct 13, 2002: Boeing 737301 (N337US), Greensboro, NC. (-23) On very short final, just after flare the aircraft struck a flock of geese. The aircraft landed safely and taxied to the gate. Crew walk around found…
- [Incident 19921130050599I](https://openairdocs.org/incident/19921130050599I), Nov 30, 1992: Boeing 737301 (N337US), San Francisco, CA. After takeoff pilot was unable to pressurize cabin. Returned. Found out flow valve stuck open.

## Other aircraft with N337US

- [Registered now](https://openairdocs.org/aircraft/N337US): Smith Mark R MINI MAX 1500R, S/N JDT-177, built 2014

---
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.