# N422US: 1987 Boeing 737-401, registration cancelled 2014-04-09 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: April 9, 2014 - Exported to: Venezuela - Status when cancelled: Valid registration - Airframe: [Boeing 737-401](https://openairdocs.org/model/boeing-737-401) (registry code 138449B) - 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: 23989 - Year built: 1987 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Special flight permit - Airworthiness date: November 11, 2013 - Certificate issued: April 9, 2014 - Last registry action: April 9, 2014 - Mode S code: A504E0 - Owner when cancelled: [Shell Aerospace Supplies Inc](https://openairdocs.org/faa-owner/SHELL%20AEROSPACE%20SUPPLIES%20INC) - Location: [Miami, FL](https://openairdocs.org/faa-place/FL/Miami) - Owner type: Corporation - Owner's area on the map: 25.8050° N, 80.3151° W: Placed by OpenAirDocs at the center of ZIP code 33122, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N422US - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=422US - Page: https://openairdocs.org/deregistered/N422US-2014-04-09 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 737-401: https://openairdocs.org/model/boeing-737-401.md ## Service difficulty reports (176, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR USAA2012081600008](https://openairdocs.org/sdr/USAA2012081600008), Aug 15, 2012: POWER SUPPLY. FAULTY. C1 CHECK - EMERGENCY LIGHTS POWER SUPPLY M1137 AT STA 960R HAS TOO HIGH CHARGING VOLTAGE. REPLACED EMERGENCY LIGHTS POWER SUPPLY M1137 IAW B737-400 AMM 33-51-51 - [SDR USAA2012062900019](https://openairdocs.org/sdr/USAA2012062900019), Jun 28, 2012: TRANSFORMER. FAULTY. EN ROUTE TPA TO CLT, THE RIGHT GENERATOR BUS OFF LIGHT ILLUMINATED IN DESCENT - RESET WAS SUCCESSFUL. THE APU WAS ON MEL49-01A AT THE TIME. FLIGHT LANDED WITHOU - [SDR USAA2012012000001](https://openairdocs.org/sdr/USAA2012012000001), Jan 17, 2012: WINDSHIELD. CRACKED. DURING CRUISE, EN ROUTE FROM ORD TO CLT, CREW REPORTED THE R1 WINDOW PANE CRACKED AND SPREAD RAPIDLY. AFTER REFERRING TO QRH PROCEDURES, IT WAS DETERMINED TO PR - [SDR USAA2011112500004](https://openairdocs.org/sdr/USAA2011112500004), Nov 24, 2011: BATTERY. DISCHARGED. MAINTENANCE REPORTED THE AFT FLIGHT ATTENDANT LEFT STATION EMERGENCY FLASHLIGHT DISCHARGED. MAINTENANCE REPLACED THE BATTERIES FOR EMERGENCY FLASHLIGHT AT AFT F - [SDR USAA2011110400009](https://openairdocs.org/sdr/USAA2011110400009), Nov 3, 2011: MECHANISM. LACK OF LUBE. CREW REPORTED THE CAPTAIN'S SEAT WAS DIFFICULT TO MOVE FORE AND AFT. MAINTENANCE LUBRICATED THE CAPTAIN'S SEAT TRACK MECHANISM. OPS CHECKED GOOD. - [SDR USAA2011102100011](https://openairdocs.org/sdr/USAA2011102100011), Oct 20, 2011: SKIN. CRACKED. RON - FUSELAGE SKIN CRACK AT BS 897, S25R. REPAIRED FUSELAGE SKIN CRACK AT BS 897, S25R IAW B737-400 SRM 53-00-01 REPAIR 31 DETAIL XI AND XIX. - [SDR USAA2011080300005](https://openairdocs.org/sdr/USAA2011080300005), Aug 2, 2011: WIRE. DAMAGED. MAINTENANCE REPORTED THE PATHWAY LIGHT AT ROW 6D INOPERATIVE. MAINTENANCE REPAIRED WIRE. ALSO, REPLACED BOTH CONNECTORS. SYSTEM CHECKS OK. - [SDR USAA20110622SB107](https://openairdocs.org/sdr/USAA20110622SB107), Jun 18, 2011: ENGINE. BIRD INGESTION. MCO - CREW REPORTED A STRONG SMELL AFTER ROTATION. THE NR 1 ENGINE EGT MAXED OUT WITH RED LIGHT ILLUMINATING. PULLED THROTTLES BACK AND LIGHT WENT OUT. NO EGT I - [SDR USAA2011022390855](https://openairdocs.org/sdr/USAA2011022390855), Feb 23, 2011: PLATE. CRACKED. CLT - Q1 - MAJOR REPAIR - CRACK ON RUDDER LIGHTNING DIVERTER PLATE ON LEFT SIDE OF RUDDER 15 INCHES FROM THE TOP OF RUDDER. REPLACED RUDDER IAW JOB CARD 03C7082 - [SDR USAA2011021890790](https://openairdocs.org/sdr/USAA2011021890790), Feb 16, 2011: THRESHOLD. CORRODED. CLT - MAJOR REPAIR - Q1 CHECK - LEVEL 2 EXFOLIATION CORROSION ON AFT CARGO DOOR CUTOUT THRESHOLD WEB AT BS 797, RBL 30. REPLACED AFT CARGO DOOR CUTOUT THRESHOLD - [SDR USAA2011022190841](https://openairdocs.org/sdr/USAA2011022190841), Feb 14, 2011: FRAME. CRACKED. CLT - MAJOR REPAIR - Q1 CHECK - CRACKED FRAME AT BS 559, S10L - S14L. REPAIRED FRAME AT BS 559, S10L - S14L IAW EA 102700 AND B737 SRM 53-00-07. - [SDR USAA2011021890789](https://openairdocs.org/sdr/USAA2011021890789), Feb 14, 2011: STRINGER. CORRODED. CLT - MAJOR REPAIR - Q1 CHECK - LEVEL 2 EXFOLIATION CORROSION ON STRINGER AT BS 500 - BS 500B, S27L. REPAIRED STRINGER AT BS 500 - BS 500B, S27L IAW B737 SRM 53 - [SDR USAA2011021490712](https://openairdocs.org/sdr/USAA2011021490712), Feb 7, 2011: STRUCTURE. CRACKED. CLT - MAJOR REPAIR - Q1 CHECK - CRACKS ON FORWARD SERVICE DOOR AT NR 3 AND NR 4 STOP FITTINGS. REPAIRED FORWARD SERVICE DOOR AT NR 3 AND NR 4 STOP FITTINGS IAW - [SDR USAA2011022190839](https://openairdocs.org/sdr/USAA2011022190839), Feb 4, 2011: KEELBEAM. CRACKED. CLT - MAJOR REPAIR - Q1 CHECK - CRACKED KEEL BEAM, UPPER DECK AT BS 705, LBL 4. REPAIRED KEEL BEAM, UPPER DECK AT BS 705, LBL 4 IAW EA 102649. - [SDR USAA2011021890791](https://openairdocs.org/sdr/USAA2011021890791), Feb 4, 2011: ACCESS PANEL. CRACKED. CLT - MAJOR REPAIR - Q1 CHECK - LEFT PYLON ACCESS PANEL 5724L CUTOUT IS CRACKED. REPAIRED LEFT PYLON ACCESS PANEL 5724L CUTOUT IAW EA 102587 REV A. - [SDR USAA2011021890793](https://openairdocs.org/sdr/USAA2011021890793), Feb 3, 2011: FRAME. CRACKED. CLT - MAJOR REPAIR - Q1 CHECK - CRACKED FRAME AT BS 500B, S20L - S21L. REPAIRED FRAME AT BS 500B, S20L - S21L IAW EA 102621. - [SDR USAA2011022190840](https://openairdocs.org/sdr/USAA2011022190840), Feb 2, 2011: FRAME. CRACKED. CLT - MAJOR REPAIR - Q1 CHECK - CRACKED FRAME AT BS 500F, S19R. REPAIRED FRAME AT BS 500F, S19R IAW B737 SRM 53-00-07 REPAIR 13. - [SDR USAA2011020990667](https://openairdocs.org/sdr/USAA2011020990667), Feb 2, 2011: FRAME. CRACKED. CLT - MAJOR REPAIR - Q1 CHECK - CRACK ON PREVIOUS FRAME REPAIR BETWEEN BS 288 TO BS 294, S17R. REPAIRED FRAME BETWEEN BS 288 TO BS 294, S17R IAW B737 SRM 51-70- - [SDR USAA2011020990666](https://openairdocs.org/sdr/USAA2011020990666), Feb 2, 2011: FRAME. CRACKED. CLT - MAJOR REPAIR - Q1 CHECK - CRACK ON FRAME AT BS 500E, BETWEEN S20L TO S21L. REPAIRED FRAME AT BS 500E, BETWEEN S20L TO S21L IAW B737 SRM 53-00-07. - [SDR USAA2011022190842](https://openairdocs.org/sdr/USAA2011022190842), Feb 1, 2011: FRAME. CRACKED. CLT - MAJOR REPAIR - Q1 CHECK - CRACKED FRAME AT BS 500C, S2R - S21R. REPAIRED FRAME AT BS 500C, S2R - S21R IAW B737 SRM 53-00-07 REPAIR 13. - [SDR USAA2011020990668](https://openairdocs.org/sdr/USAA2011020990668), Feb 1, 2011: FITTING. CRACKED. CLT - MAJOR REPAIR - Q1 CHECK - CRACK ON CLIP AT BS 294.5, WL 253. REPLACED CLIP AT BS 294.5, WL 253 IAW B737 SRM 51-40-02 , DRAWING 66-14210. - [SDR USAA2011020990664](https://openairdocs.org/sdr/USAA2011020990664), Feb 1, 2011: INTERCOSTAL. CRACKED. CLT - MAJOR REPAIR - Q1 CHECK - CRACK ON INTERCOSTAL AT BS 294.5, WL 244. REPLACED INTERCOSTAL AT BS 294.5, WL 244 IAW B737 SRM 51-10-02. - [SDR USAA2011020990659](https://openairdocs.org/sdr/USAA2011020990659), Feb 1, 2011: STRINGER. CRACKED. CLT - MAJOR REPAIR - Q1 CHECK - CRACK ON PREVIOUS STRINGER DOUBLER REPAIR AT BS 303.9, S16L. REPAIRED STRINGER AT BS 303.9, S16L IAW BOEING DRAWING 65-17684. - [SDR USAA2011020990658](https://openairdocs.org/sdr/USAA2011020990658), Feb 1, 2011: SUPPORT ANGLE. CRACKED. CLT - MAJOR REPAIR - Q1 CHECK - CRACKED SUPPORT ANGLE AT BS 301, WL 258. REPLACED SUPPORT ANGLE AT BS 301, WL 258 IAW B737 SRM 51-10-02. - [SDR USAA2011020990654](https://openairdocs.org/sdr/USAA2011020990654), Feb 1, 2011: FLAP. DEBONDED. CLT - MAJOR REPAIR - Q1 CHECK - DISBONDED AREA 2.5 INCHES BY 3.5 INCHES ON THE RIGHT INBOARD AFT FLAP INBOARD END OF TRAILING EDGE WEDGE. REPAIRED THE RIGHT INB - [SDR USAA2011020990660](https://openairdocs.org/sdr/USAA2011020990660), Jan 31, 2011: SKIN. CRACKED. CLT - MAJOR REPAIR - Q1 CHECK - CRACK ON FORWARD ENTRY DOOR INNER SKIN AFT EDGE BETWEEN NR 5 AND NR 7 STOP FITTING ACCESS HOLES. REPAIRED FORWARD ENTRY DOOR INN - [SDR USAA2011021890794](https://openairdocs.org/sdr/USAA2011021890794), Jan 30, 2011: STRINGER. CORRODED. CLT - MAJOR REPAIR - Q1 CHECK - CORROSION ON STRINGER AT BS 907, S22L. REPAIRED STRINGER AT BS 907, S22L IAW EA 102661. - [SDR USAA2011020990661](https://openairdocs.org/sdr/USAA2011020990661), Jan 28, 2011: SKIN. CRACKED. CLT - MAJOR REPAIR - Q1 CHECK - CRACK ON FUSELAGE SKIN AT BS 955, S11R. REPAIRED FUSELAGE SKIN AT BS 955, S11R IAW B737 SRM 53-60-001, FIGURE 201, REPAIR 5. - [SDR USAA2011020990655](https://openairdocs.org/sdr/USAA2011020990655), Jan 28, 2011: SHEAR TIE. CRACKED. CLT - MAJOR REPAIR - Q1 CHECK - CRACKED SHEAR TIE AT BS 727F, S24L. REPLACED SHEAR TIE AT BS 727F, S24L IAW B737 SRM 51-40-02. - [SDR USAA2011020990662](https://openairdocs.org/sdr/USAA2011020990662), Jan 27, 2011: SKIN. CRACKED. CLT - MAJOR REPAIR - Q1 CHECK - CRACK ON FUSELAGE SKIN AT BS 860, JUST ABOVE S23L. REPAIRED FUSELAGE SKIN AT BS 860, JUST ABOVE S23L IAW B737 SRM 53-00-01, FIGU - [SDR USAA2011020990657](https://openairdocs.org/sdr/USAA2011020990657), Jan 24, 2011: ANGLE. CORRODED. CLT - MAJOR REPAIR - Q1 CHECK - CORROSION ON Z-ANGLE BETWEEN BS 907 AND BS 1006, LBL 54. REPLACED Z-ANGLE BETWEEN BS 907 AND BS 1006, LBL 54 IAW B737 SRM 53-60- - [SDR USAA2011021490714](https://openairdocs.org/sdr/USAA2011021490714), Jan 19, 2011: TIE CLIP. CORRODED. CLT - MAJOR REPAIR - Q1 CHECK - CRACK ON TIE CLIP AT BS 727, S25L. REPLACED TIE CLIP AT BS 727, S25L IAW B737 SRM 51-10-02, 51-40-02 DRAWING 65-46550. - [SDR USAA2011021490713](https://openairdocs.org/sdr/USAA2011021490713), Jan 19, 2011: SHEAR TIE. CORRODED. CLT - MAJOR REPAIR - Q1 CHECK - LEVEL 2 EXFOLIATION CORROSION ON SHEAR TIE LEG AT BS 747, BETWEEN S26R AND S27R. REPAIRED SHEAR TIE LEG AT BS 747, BETWEEN S26R - [SDR USAA2011020990653](https://openairdocs.org/sdr/USAA2011020990653), Jan 18, 2011: SKIN. DEBONDED. CLT - MAJOR REPAIR - Q1 CHECK - DISBONDED AREA 5 INCHES BY 3 INCHES ON THE RIGHT HAND INBOARD FORE FLAP UPPER SURFACE 34.5 INCHES FROM OUTBOARD END AND 6 INCHES - [SDR USAA2011020990663](https://openairdocs.org/sdr/USAA2011020990663), Jan 16, 2011: FLOORBEAM. CORRODED. CLT - MAJOR REPAIR - Q1 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM AT BS 328, RBL 26. REPAIRED FLOORBEAM AT BS 328, RBL 26 IAW B737 SRM 53-00-51. - [SDR USAA2011020990656](https://openairdocs.org/sdr/USAA2011020990656), Jan 13, 2011: SHEAR TIE. CORRODED. CLT - MAJOR REPAIR - Q1 CHECK - LEVEL 2 EXFOLIATION CORROSION ON SHEAR TIE AT BS794.3, S27R. REPLACED SHEAR TIE AT BS 794, S27R IAW B737 SRM 51-00-07, REPAIR 5. - [SDR USAA2011022190844](https://openairdocs.org/sdr/USAA2011022190844), Jan 11, 2011: FRAME. CRACKED. CLT - MAJOR REPAIR - Q1 CHECK - CRACKED FRAME AT BS 727B, S8R - S9R. REPAIRED FRAME AT BS 727B, S8R-S9R IAW EA 102559. - [SDR USAA2011022190843](https://openairdocs.org/sdr/USAA2011022190843), Jan 11, 2011: FRAME. CRACKED. CLT - MAJOR REPAIR - Q1 CHECK - CRACKED FRAME AT BS 787, S8L - S9L. REPAIRED FRAME AT BS 787, S8L-S9L IAW EA 102559. - [SDR USAA2011020990665](https://openairdocs.org/sdr/USAA2011020990665), Jan 11, 2011: FRAME. CRACKED. CLT - MAJOR REPAIR - Q1 CHECK - CRACK ON FRAME AT BS 727F, BETWEEN S8R TO S9R. REPAIRED FRAME AT BS 727F, BETWEEN S8R TO S9R IAW ENGINEERING AUTHORIZATION 10255 - [SDR USAA2011012890406](https://openairdocs.org/sdr/USAA2011012890406), Jan 11, 2011: FRAME. CRACKED. CLT - Q1 - MAJOR REPAIR - CRACK IN FUSELAGE FRAME AT BS 867 BETWEEN S8L TO S9L. REPAIRED FUSELAGE FRAME AT BS 867 BETWEEN S8L TO S9L IAW EA 102559. - [SDR USAA2011012890405](https://openairdocs.org/sdr/USAA2011012890405), Jan 11, 2011: FRAME. CRACKED. CLT - Q1 - MAJOR REPAIR - CRACK IN FUSELAGE FRAME AT BS 480 BETWEEN S8R TO S9R. REPAIRED FUSELAGE FRAME AT BS 480 BETWEEN S8R TO S9R IAW EA 102559. - [SDR USAA2011021890792](https://openairdocs.org/sdr/USAA2011021890792), Jan 10, 2011: BEAR STRAP. CRACKED. CLT - MAJOR REPAIR - Q1 CHECK - CRACKED BEAR STRAP AT BS 304.5, WL 258. REPAIRED BEAR STRAP AT BS 304.5, WL 258 IAW EA 102576. - [SDR USAA20110104SB004](https://openairdocs.org/sdr/USAA20110104SB004), Jan 3, 2011: BATTERY PACK. DISCHARGED. CLT - MAINTENANCE REPORTED THE LEFT SIDE FORWARD GALLEY EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK IN FORWARD GALLEY. OPERATIONAL CHECK - [SDR USAA20110104SB002](https://openairdocs.org/sdr/USAA20110104SB002), Jan 2, 2011: FILTER. DIRTY. CLT - ON DESCENT INTO CLT AND TOWARDS END OF FLIGHT, AFT FLIGHT ATTENDANT NOTICED A STRONG DIRTY SOCK ODOR THROUGHOUT THE CABIN, ESPECIALLY IN THE AFT CABIN. TH - [SDR USAA20101021SB173](https://openairdocs.org/sdr/USAA20101021SB173), Oct 21, 2010: BATTERY PACK. DISCHARGED. CLT - MAINTENANCE REPORTED THE AFT RIGHT EMERGENCY LIGHTS WILL NOT STAY ILLUMINATED FOR MORE THAN THREE SECONDS. MAINTENANCE REMOVED AND REPLACED THE AFT RIGHT - [SDR USAA2010092892134](https://openairdocs.org/sdr/USAA2010092892134), Sep 26, 2010: FUSE PIN. CORRODED. CLT - PYLON INSPECTION - MAJOR REPAIR - CORROSION ON LEFT OUTBOARD MID SPAR FUSE PIN. REPLACED LEFT OUTBOARD MID SPAR FUSE PIN IAW B737 AMM 54-10-01. - [SDR USAA2010092992139](https://openairdocs.org/sdr/USAA2010092992139), Sep 25, 2010: SKIN. CRACKED. CLT - DROP-IN - MAJOR REPAIR - CRACK IN FUSELAGE SKIN AT BS 943, S25R. REPAIRED FUSELAGE SKIN AT BS 943, S25R IAW B737 SRM 53-00-01 REPAIR 31. - [SDR USAA2010092792108](https://openairdocs.org/sdr/USAA2010092792108), Sep 25, 2010: FUSE PIN. CORRODED. CLT - PYLON INSPECTION - MAJOR REPAIR - CORROSION ON HEAD OF LEFT INBOARD MIDSPAR FUSE PIN. REPLACED LEFT INBOARD MIDSPAR FUSE PIN IAW B737 AMM 54-10-01. - [SDR USAA2010010790046](https://openairdocs.org/sdr/USAA2010010790046), Jan 7, 2010: SKIN. DELAMINATED. CLT - C4 - MAJOR REPAIR - DELAMINATION ON NR 9 SPOILER UPPER SKIN BETWEEN WS 447 TO WS 499. REPLACED NR 9 SPOILER IAW B737 AMM 27-62-91. - [SDR USAA2010010790045](https://openairdocs.org/sdr/USAA2010010790045), Jan 7, 2010: SHEAR TIE. CORRODED. CLT - C4 - MAJOR REPAIR - CORROSION ON SHEAR TIE AT BS 867 BETWEEN S26L TO S26R. REPLACED SHEAR TIE AT BS 867 BETWEEN S26L TO S26R IAW B737 SRM 53-00-01, 53-00- All 176: https://openairdocs.org/deregistered/N422US-2014-04-09/reports.md ## Other aircraft with N422US - [Registered now](https://openairdocs.org/aircraft/N422US): Piper PA-28-181, S/N 28020125, built 2023 --- 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.