# N338US: 1986 Boeing 737-301, registration cancelled 2004-01-09

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: January 9, 2004
- 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: 23234
- Year built: 1986
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: April 24, 1986
- Certificate issued: April 25, 2003
- Last registry action: April 25, 2003
- Mode S code: A3B55A
- 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/N338US
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=338US
- Page: https://openairdocs.org/deregistered/N338US-2004-01-09

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 (60, newest 50)

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

- [SDR USAA020383](https://openairdocs.org/sdr/USAA020383), Oct 3, 2002: ANGLE. CRACKED. PIT - FOUND Z-ANGLE CRACKED 2 INCHES, W/W FORWARD BULKHEAD LEFT CENTER VERTICAL Z-ANGLE. MANUFACTURED IAW EA 75003. (M)
- [SDR USAA020159](https://openairdocs.org/sdr/USAA020159), Mar 28, 2002: SKIN. CRACKED. CLT - FOUND SKIN CRACKED TWO PLACES 2.25 INCH AND 1.25 INCH, STATION 730 STRINGER 23R AND 24R. INSTALLED DOUBLER PER SRM 53-00-01 FIG 202. (M)
- [SDR USAASB01197](https://openairdocs.org/sdr/USAASB01197), Jul 8, 2001: BATTERY. DISCHARGED. DCA - FOUND MID-CABIN EMERGENCY EXIT LIGHTS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. (M)
- [SDR USAA001762](https://openairdocs.org/sdr/USAA001762), Oct 16, 2000: GUSSET. CRACKED. CLT - GUSSET CRACKED 1 INCH AT BS 259, BBL ZERO TOP OF N/G WELL. INSTALLED NEW GUSSET PER DWG 65 45819. (X)
- [SDR USAA001761](https://openairdocs.org/sdr/USAA001761), Oct 16, 2000: FRAME. CRACKED. CLT - CHORD CRACKED 1.5 INCHES AT BS 178, WL 207, LBL 26. FABRICATED NEW WEB PER SRM 51-10-02. (X)
- [SDR UAAA001709](https://openairdocs.org/sdr/UAAA001709), Oct 10, 2000: BULKHEAD. CRACKED. CLT - WEB CRACKED, .50 INCH, BS 178, WL 207, LBL 26. FABRICATED AND INSTALLED NEW WEB PER SRM 51-10-02. (X)
- [SDR USAA001708](https://openairdocs.org/sdr/USAA001708), Oct 10, 2000: INTERCOSTAL. CRACKED. CLT - DROP IN INTERCOSTAL CRACKED, 2 INCHES, BS 178, WL 195, LBL 24. REPAIRED PER SRM 53-10-08 FIG 207. (X)
- [SDR USAASB00269](https://openairdocs.org/sdr/USAASB00269), Sep 22, 2000: LEVER. JAMMED. PHL - FLT 1820 - EN ROUTE FROM JAX TO PHL, CAPTAIN REPORTED THAT THE NR 1 ENGINE THRUST LEVER WAS JAMMED. THRUST LEVER COULD MOVE FORWARD BUT WOULD NOT RETARD T
- [SDR USAASB00084](https://openairdocs.org/sdr/USAASB00084), Mar 24, 2000: VALVE. FAILED. CLT - FLT 1403 - EN ROUTE FROM TPA-LGA, THE ANTI-SKID INOPERATIVE LIGHT ILLUMINATED. FLIGHT DIVERTED TO CLT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOU
- [SDR USAA990791](https://openairdocs.org/sdr/USAA990791), Jul 29, 1999: STRINGER. CRACKED. CLT - DURING Q3 CHECK, FOUND .75 INCH CRACK AT BS 727 STRINGER 18A WEB S18AL. REPAIRED WITH REPLACEMENT REF SB 737-53-1170. (M)
- [SDR USAA990790](https://openairdocs.org/sdr/USAA990790), Jul 29, 1999: FRAME. CRACKED. CLT - DURING Q3 CHECK, FOUND VARIOUS 1 INCH AREAS OF CORROSION AT NUTPLATE HOLES IN FRAME/WEB AT BS 605 TO 845 STRINGER 25R TOP FLANGE. REPLACED WITH IDENTICAL 
- [SDR USAA990789](https://openairdocs.org/sdr/USAA990789), Jul 29, 1999: INTERCOSTAL. CRACKED. CLT - DURING Q3 CHECK, FOUND 1 INCH CRACK AT STATION 178, 195 INTERCOSTAL RT SIDE. REPLACED WITH IDENTICAL PART NUMBER. (M)
- [SDR USAA990788](https://openairdocs.org/sdr/USAA990788), Jul 29, 1999: POST. CRACKED. CLT - DURING Q3 CHECK, FOUND 1 INCH CRACK AT CAPTAINS UPPER O/B CORNER OF EXTERIOR WINDSHIELD (POST). INSTALLED EXTERNAL DOUBLER PER EA 64979. (M)
- [SDR USAA990787](https://openairdocs.org/sdr/USAA990787), Jul 29, 1999: SKIN. CRACKED. CLT - DURING Q3 CHECK, FOUND 3 CRACKS ONE 1.375 INCH, TWO .5 INCH ON SKIN AT NR 1 L/E SLAT. INSTALLED REPAIR DOUBLER PER TYPICAL REPAIR 57-50-01 REV 'H'. (M)
- [SDR USAA990786](https://openairdocs.org/sdr/USAA990786), Jul 29, 1999: CLIP. CRACKED. CLT - DURING Q3 CHECK, FOUND .25 INCH CRACK AT TIE CLIP AT STATION 663 S10L. REPLACED WITH IDENTICAL PART PER SRM 51-10-2. (M)
- [SDR USAA990785](https://openairdocs.org/sdr/USAA990785), Jul 29, 1999: SKIN. CRACKED. CLT - DURING Q-3 CHECK, FOUND .5 INCH CRACK E/E COOLING DUCT OUTLET INNER FUSELAGE FUSELAGE SKIN AT BS 380 BL 0. INSTALLED EXTERNAL FUSELAGE SKIN DOUBLER 23 INC
- [SDR USAA990784](https://openairdocs.org/sdr/USAA990784), Jul 29, 1999: ANGLE. CRACKED. CLT - DURING Q3 CHECK, FOUND 1 INCH CRACK AT CREASE BEAM INNER CHORD ANGLE BS 294.5 RBL 45 WL 208. INSTALLED CHORD ANGLE PER SRM 51-10-02. (M)
- [SDR USAA990783](https://openairdocs.org/sdr/USAA990783), Jul 29, 1999: SPLICE. CRACKED. CLT - DURING Q3 CHECK, FOUND .250 INCH CRACK AT BS 908 STRINGER SPLICE STRINGER 4LT. REPLACED STRINGER SPLICE WITH IDENTICAL PART. (M)
- [SDR USAA990782](https://openairdocs.org/sdr/USAA990782), Jul 29, 1999: SPLICE. CRACKED. CLT - DURING Q-3 CHECK, FOUND .250 INCH CRACK AT BS 908 STRINGER SPLICE STRINGER 4RT. REPLACED STRINGER SPLICE WITH IDENTICAL PART. (M)
- [SDR USAA990781](https://openairdocs.org/sdr/USAA990781), Jul 29, 1999: FRAME. CRACKED. CLT - DURING Q3 CHECK, FOUND .125 INCH CRACK IN FRAME AT STATION 616 RBL 64 WL 201 INBOARD CHORD ANGLE. INSTALLED REPAIR FILLER AND STIFFENING ANGLE PER EA 6500
- [SDR USAA990780](https://openairdocs.org/sdr/USAA990780), Jul 29, 1999: FRAME. CRACKED. CLT - DUIRNG Q-3 CHECK, FOUND .25 INCH CRACK IN FRAME AT BS 480 S9R. INSTALLED DOUBLER PER EA 65009. (M)
- [SDR USAA990779](https://openairdocs.org/sdr/USAA990779), Jul 29, 1999: TIE CLIP. CRACKED. CLT - DURING Q3 CHECK, FOUND TIE CLIP CRACKED IN HALF. ALSO, FOUND STRINGER CRACKED BELOW CLIP LOCATION, STATION 616, S-4L. INSTALLED STRINGER DOUBLER PER SRM 5
- [SDR USAA990772](https://openairdocs.org/sdr/USAA990772), Jul 29, 1999: STRINGER. CORRODED. CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 4 INCH AREA OF CORROSION AT STATION 727A PLUS 14 INCHES, STRINGER 26L. CORROSION TASK NR C53-202-01, CORROSION L
- [SDR USAA990771](https://openairdocs.org/sdr/USAA990771), Jul 29, 1999: ANGLE. CORRODED. CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 6 SQUARE INCH OF CORROSION MED Z-ANGLE UPPER SURFACE. CORROSION LEVEL 2. REPLACED Z-ANGLE PER SRM 51-10-02. (M)
- [SDR USAA990770](https://openairdocs.org/sdr/USAA990770), Jul 29, 1999: STABILIZER LINK. CORRODED. CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND CORROSION RIGHT GEAR STABILIZER LINK ATTACH POINTS. CORROSION LEVEL 2. REMOVED AND REPLACED STABILIZER LINK PER 
- [SDR USAA990769](https://openairdocs.org/sdr/USAA990769), Jul 29, 1999: ANGLE. CORRODED. CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND CORROSION AT BS 957 AND 987, LBL 45, WL 208 CREASEBEAM INNER CHORD ANGLE. CORROSION LEVEL 2, CORROSION TASK NR C
- [SDR USAA990768](https://openairdocs.org/sdr/USAA990768), Jul 29, 1999: TIE CLIP. CRACKED. CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STATION 616 STRINGER 6L TIE CLIP. INSTALLED NEW TIE CLIP PER SRM 51-40-02. (M)
- [SDR USAA990729](https://openairdocs.org/sdr/USAA990729), Jul 29, 1999: FRAME. CRACKED. CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A .50 INCH CRACK FRAME 312 AT STR 5L. CRACK TRIMMED OUT AND DOUBLER INSTALLED PER SRM 53-00-07 FIG 202 AND EA 65
- [SDR USAA990728](https://openairdocs.org/sdr/USAA990728), Jul 29, 1999: FRAME. CRACKED. CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A .500 INCH CRACK MAIN ENTRY DOORWAY UPPER HINGE H-STRAP DOORWAY FRAME. FABRICATED AND INSTALLED NEW H-STRAP PER
- [SDR USAA990727](https://openairdocs.org/sdr/USAA990727), Jul 29, 1999: ANGLE. CRACKED. CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A .75 INCH CRACK AT AFT END STA 360 STR 14L SHEARBEAM OUTBOARD CHORD ANGLE. REPAIRED PER BOEING DWG NR 69-48985/
- [SDR USAA990726](https://openairdocs.org/sdr/USAA990726), Jul 29, 1999: FRAME. CRACKED. CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK AFT ENTRY DOOR CUT-OUT FRAME UPPER FORWARD SECTION AT BOTTOM HOLE FORWARD EDGE FRAME. INSTALLED D
- [SDR USAA990725](https://openairdocs.org/sdr/USAA990725), Jul 29, 1999: TIE CLIP. CRACKED. CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A CRACK AT STA 639 STR 4L TIE CLIP. INSTALLED NEW TIE CLIP PER SRM 51-40-02. (X)
- [SDR USAA990724](https://openairdocs.org/sdr/USAA990724), Jul 29, 1999: TIE CLIP. CRACKED. CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A CRACK AT STATION 639 STRINGER 4R TIE CLIP. INSTALLED NEW TIE CLIP PER SRM 51-40-02. (M)
- [SDR USAA990723](https://openairdocs.org/sdr/USAA990723), Jul 29, 1999: TIE CLIP. CRACKED. CLT - DURIGN Q-3 CHECK VISUAL INSPECTION, FOUND A CRACK AT STATION 616 STRINGER 4R TIE CLIP. INSTALLED NEW TIE CLIP PER SRM 51-40-02. (M)
- [SDR USAA990722](https://openairdocs.org/sdr/USAA990722), Jul 29, 1999: SKIN. CRACKED. CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A .75 INCH CRACK AT NR 1 ENGINE PYLON SKIN AT ACCESS PANEL NR 5727 CUTOUT LOWER AFT CORNER. INSTALLED DOUBLER PE
- [SDR USAA990721](https://openairdocs.org/sdr/USAA990721), Jul 29, 1999: TIE CLIP. CRACKED. CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AT STATION 520 STRINGER 7R TIE CLIP. INSTALLED NEW TIE CLIP PER SRM 51-40-02. (M)
- [SDR USAA990719](https://openairdocs.org/sdr/USAA990719), Jul 29, 1999: TIE CLIP. CRACKED. CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AT STA 500C STR 7R TIE CLIP. INSTALLED NEW TIE CLIP PER SRM 51-40-02. (X)
- [SDR USAA990718](https://openairdocs.org/sdr/USAA990718), Jul 29, 1999: TIE CLIP. CRACKED. CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AT STA 600 STR 8L TIE CLIP. INSTALLED NEW TIE CLIP PER SRM 51-40-02. (X)
- [SDR USAA990717](https://openairdocs.org/sdr/USAA990717), Jul 29, 1999: LONGERON. CRACKED. CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A .75 INCH LONGERON CRACK AT FORWARD L/B CORNER STATION 277 STRINGER 14R. FABRICATED NEW LONGERON WEB AND INSTAL
- [SDR USAA990716](https://openairdocs.org/sdr/USAA990716), Jul 29, 1999: STRINGER. CRACKED. CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A .50 INCH CRACK IN STRINGER AT STA 306 STR 4L. FABRICATED NEW WEB AND INSTALLED PER SRM 53-10-15. (X)
- [SDR USAA990715](https://openairdocs.org/sdr/USAA990715), Jul 29, 1999: FRAME. CRACKED. CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A .50 INCH CRACK IN FRAME AT STA 727D, RBL 2. INSTALLED REPAIR DOUBLER AND FILLER PER SRM 53-00-07 AND EA 65131 
- [SDR USAA990685](https://openairdocs.org/sdr/USAA990685), Jul 29, 1999: ANGLE. CRACKED. CLT - DURING A Q-3 CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK AT BS 480 STRINGER 9L BAG BIN ATTACH ANGLE. FABRICATED NEW REPAIR DOUBLER PER SRM 53-00-07 AND
- [SDR USAA990684](https://openairdocs.org/sdr/USAA990684), Jul 29, 1999: BULKHEAD. CRACKED. CLT - DURING A Q-3 CHECK VISUAL INSPECTION, FOUND .50 INCH CRACK AT STA 178 BULKHEAD LBL 5 W/L 195 SKIN. INSTALLED DOUBLER PER TR 53-10-07. (X)
- [SDR USAA990683](https://openairdocs.org/sdr/USAA990683), Jul 29, 1999: BULKHEAD. CRACKED. CLT - DURING A Q-3 CHECK VISUAL INSPECTION, FOUND 1 INCH CRACK AT STA 178 BULKHEAD LBL 5 W/L 188 SKIN. INSTALLED REPAIR DOUBLER PER TR 53-10-07. (X)
- [SDR USAA990682](https://openairdocs.org/sdr/USAA990682), Jul 29, 1999: BULKHEAD. CRACKED. CLT - DURING A Q-3 CHECK VISUAL INSPECTION, FOUND .50 INCH CRACK AT STA 178 BULKHEAD RBL1 W/L 188 SKIN. INSTALLED REPAIR DOUBLER PER SRM 53-10-08 FIG 203. (X)
- [SDR USAA990681](https://openairdocs.org/sdr/USAA990681), Jul 29, 1999: BULKHEAD. CRACKED. CLT - DURING A Q-3 CHECK VISUAL INSPECTION FOUND .50 INCH CRACK AT STA 178 BULKHEAD LBL1 W/L 188 SKIN. INSTALLED REPAIR DOUBLER PER SRM 53-10-08 FIG 203. (X)
- [SDR USAA990680](https://openairdocs.org/sdr/USAA990680), Jul 29, 1999: ANGLE. CORRODED. CLT - DURING A Q-3 CHECK VISUAL INSPECTION, FOUND A 1 INCH BY 1 INCH AREA OF CORROSION AFT RT Z-ANGLE AT AFT SERV DOOR. CORROSION LEVEL 2. REPLACED PER SRM 51-1
- [SDR USAASB99015](https://openairdocs.org/sdr/USAASB99015), Jan 20, 1999: BATTERY CHARGER. FAILED. LGA - PILOT REPORTED THAT THE INTERIOR EMERGNECY FLOOR LIGHTING FROM SEAT ROWS 5 THROUGH 10 AND THE LEFT EMERGENCY EXIT LIGHT ASSEMBLY AT SEAT ROW 10ABC WERE IN
- [SDR 99ZZZM158](https://openairdocs.org/sdr/99ZZZM158), Jan 20, 1999: LIGHT. INOPERATIVE. LGA - PILOT REPORTED THAT THE INTERIOR EMERGNECY FLOOR LIGHTING FROM SEAT ROWS 5 THROUGH 10 AND THE LEFT EMERGENCY EXIT LIGHT ASSEMBLY AT SEAT ROW 10ABC WERE IN
- [SDR USAASB98278](https://openairdocs.org/sdr/USAASB98278), Oct 21, 1998: SWITCH. CONTAMINATED. PIT - FLT 345 - DURING LANDING GEAR EXTENSION, GEAR CAME DOWN WITH 3 GREEN AND 3 RED LIGHTS. HYDRAULIC PRESSURE WAS NORMAL. CREW RECYCLED GEAR AND RECEIVED 3 GR

All 60: https://openairdocs.org/deregistered/N338US-2004-01-09/reports.md

## Other aircraft with N338US

- [Registered now](https://openairdocs.org/aircraft/N338US): DJI AGRAS T40, S/N 1581F574B235W00100JR

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