# N407US: 1988 Boeing 737-401, registration cancelled 2003-09-09

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: September 9, 2003
- 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: 23877
- Year built: 1988
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: September 21, 1988
- Certificate issued: April 24, 2003
- Last registry action: April 24, 2003
- Mode S code: A4C875
- Owner when cancelled: [Linc 737 LLC](https://openairdocs.org/faa-owner/LINC%20737%20LLC)
- Location: [Aurora, CO](https://openairdocs.org/faa-place/CO/Aurora)
- Owner type: Corporation
- Owner's area on the map: 39.6636° N, 104.8378° W: Placed by OpenAirDocs at the center of ZIP code 80014, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N407US
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=407US
- Page: https://openairdocs.org/deregistered/N407US-2003-09-09

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 (61, newest 50)

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

- [SDR USAASB02152](https://openairdocs.org/sdr/USAASB02152), Aug 13, 2002: ACTUATOR. FAILED. ON CLIMB OUT, ENROUTE, CREW REPORTED THE LEFT MAIN LANDING GEAR WOULD NOT RETRACT AFTER PLACING GEAR LEVER TO THE UP POSITION. THE LEFT MAIN LANDING GEAR UNSAFE
- [SDR USA2002F00081](https://openairdocs.org/sdr/USA2002F00081), Aug 8, 2002: CIRCUIT CARD. FAULTY. ON CLIMB OUT, CREW REPORTED THE LT MAIN LANDING GEAR RED AND GREEN LIGHTS ILLUMINATED WHEN GEAR WAS RETRACTED, CYCLED GEAR WITH SAME RESULTS. WHEN GEAR WAS EXTE
- [SDR USA2002F00079](https://openairdocs.org/sdr/USA2002F00079), Aug 8, 2002: CARD. FAULTY. ON CLIMB OUT FROM PIT, CREW REPORTED THE LEFT MAIN LANDING GEAR RED AND GREEN LIGHTS ILLUMINATED WHEN THE GEAR WAS RETRACTED. CREW CYCLED GEAR WITH SAME RESULTS
- [SDR USAASB02074](https://openairdocs.org/sdr/USAASB02074), Apr 18, 2002: BATTERY PACK. DISCHARGED. TPA - FOUND CENTER AISLE AND RIGHT OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. MAINTENANCE REPLACED TWO BATTERY PACKS. (M)
- [SDR USAASB02047](https://openairdocs.org/sdr/USAASB02047), Mar 10, 2002: INDICATOR. FAULTY. BDL - FLT 482 - ON SHORT FINAL TO ALB, WHEN FLAPS WERE SELECTED TO 10 UNITS, CAPTAIN RECEIVED A FLAP INDICATOR NEEDLE SPLIT AND ASSOCIATED LEADING EDGE DEVICE A
- [SDR USAASB01310](https://openairdocs.org/sdr/USAASB01310), Nov 12, 2001: CHARGER. FAILED. TPA - MAINTENANCE FOUND THE BULLNOSE EMERGENCY LIGHT AT ROW 9, RIGHT SIDE, INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY CHARGER ASSEMBLY. OPS CHECK
- [SDR USAASB01187](https://openairdocs.org/sdr/USAASB01187), Jun 28, 2001: TRANSMITTER. FAULTY. CLT - FLT 1157 - IN PREPARATION FOR LANDING AT CLT, FROM ORD, CREW REPORTED A SPLIT FLAP INDICATION AS FLAPS WERE STUCK AT 7 DEGREES. FLIGHT LANDED WITHOUT FURT
- [SDR USAA010567](https://openairdocs.org/sdr/USAA010567), May 25, 2001: BULKHEAD. CRACKED. CLT - FOUND PRESSURE WEB .5 INCH, .75 INCH AND 1.5 INCH, BS 178 WL 199 AND 201, LBL 6.5 TO RBL 6.5. REMOVED DAMAGED, INSTALLED REPAIR FILLERS AND DOUBLER PER EO
- [SDR USAA010568](https://openairdocs.org/sdr/USAA010568), May 25, 2001: DOUBLER. CRACKED. CLT - FOUND REPAIR DOUBLER CRACKED .5 INCH, NR 2 SLAT, OUTBOARD OF ACTUATOR ATTACH. REMOVED CRACKED DOUBLER, INSTALLED NEW DOUBLER PER SRM 57-43-01. (M)
- [SDR USAASB00304](https://openairdocs.org/sdr/USAASB00304), Oct 26, 2000: BYPASS VALVE. FAULTY. BTV - FLT 1567 - ON APPROACH INTO BTV, THE FLAPS TO EXTEND AS THEY WOULD NOT MOVE FROM 5 DEGREES. MOVING FLAP LEVER UP OR DOWN WOULD NOT MOVE FLAPS. CREW WAS AB
- [SDR USAA000232](https://openairdocs.org/sdr/USAA000232), Feb 22, 2000: SKIN. CRACKED. TPA - FOUND DOOR SKIN CRACKED .25 INCH, LOWER HINGE CUTOUT FORWARD SERVICE DOOR. INSTALLED DOUBLER PER SRM AND TR 52-40-03A. (M)
- [SDR USAA991163](https://openairdocs.org/sdr/USAA991163), Oct 23, 1999: SKIN. CRACKED. CLT - DURING RON VISUAL INSPECTION, FOUND A 1.250 INCH SKIN CRACK JUST BELOW STRINGER 23L AND 3 INCH AFT OF STATION 727D. INSTALLED REPAIR DOUBLER PER EA 65983 
- [SDR USAASB99158](https://openairdocs.org/sdr/USAASB99158), Jun 29, 1999: EGT LIGHT. ILLUMINATED. CLT - FLT 932 - UPON CLIMB-OUT FROM CLT, AP APPROX 18,000 FT, THE NR 1 ENGINE EGT LIGHT ILLUMINATED AS THE NR 1 ENGINE EXCEEDED LIMITS. CAPTAIN PULLED THE THROT
- [SDR USAA990376](https://openairdocs.org/sdr/USAA990376), May 19, 1999: SUPPORT. CORRODED. CLT - DURING SHOP VISIT, FOUND CORROSION ON CARRIAGES SUPPORT ARM INBOARD MID FLAP, INBOARD CARRIAGE, OUTBOARD ARM AT BEARING MOUNT HOLE FOR ECCENTRIC BUSHING. 
- [SDR USAA990375](https://openairdocs.org/sdr/USAA990375), May 19, 1999: SUPPORT. CORRODED. CLT - DURING SHOP VISIT, FOUND CORROSION IN BEARING RETAINER BORE AT INBOARD MID FLAP OUTBOARD CARRIAGE, INBOARD SUPPORT ARM AT ECCENTRIC BEARING BORE. CORROSIO
- [SDR USAA990374](https://openairdocs.org/sdr/USAA990374), May 19, 1999: SUPPORT. CORRODED. CLT - DURING SHOP VISIT, FOUND CORROSION IN BEARING RETAINER BORE AT INBOARD MID FLAP INBOARD CARRIAGE, INBOARD SUPPORT ARM, AT ECCENTIC BEARING BORE. CORROSION
- [SDR USAA990373](https://openairdocs.org/sdr/USAA990373), May 19, 1999: SUPPORT. CORRODED. CLT - DURING SHOP VISIT, FOUND CORROSION IN BEARING RETAINER BORE AT INBOARD MID FLAP OUTBOARD CARRIAGE, OUTBOARD SUPPORT ARM AT ECCENTRIC BEARING BORE. CORROSI
- [SDR USAASB99108](https://openairdocs.org/sdr/USAASB99108), Apr 23, 1999: EGT INDICATION. MALFUNCTIONED. SDF - FLT 1266 - EN ROUTE FROM MCI-DCA, AT FL330, THE NR 1 ENGINE EGT WAS ON THE RISE AND WENT TO FULL SCALE WITH RED EGT OVERTEMP LIGHT ILLUMINATING. FUEL FLOW
- [SDR USAA99293](https://openairdocs.org/sdr/USAA99293), Mar 8, 1999: FLOORBEAM. CORRODED. CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND CORROSION AT STATION 773 RBL 3, 1 INCH BY 1 INCH AT NUTPLATE HOLES OF FLOOR SUPPORT. REPAIRED PER TR 53-10-06. (
- [SDR USAA990295](https://openairdocs.org/sdr/USAA990295), Mar 8, 1999: FLOORBEAM. CORRODED. CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A 1 INCH BY 8 INCH AREA OF CORROSION AT BS 747 RBBL 13.8 FLOORBEAM. INSTALLED TIE DOWN TRACK PER SRM 53-00-53 FI
- [SDR USAA990294](https://openairdocs.org/sdr/USAA990294), Mar 8, 1999: FLOORBEAM. CORRODED. CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND CORROSION AT BSL 859 LBL 3 FLOORBEAM. INSTALLED DOUBLER PER TR 53-10-06. (M)
- [SDR USAA990292](https://openairdocs.org/sdr/USAA990292), Mar 8, 1999: FLOORBEAM. CORRODED. CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND CORROSION AT STATION 312 AND 328 LBL 11 FLOOR SUPPORT. REPAIRED PER SRM 51-10-2. (M)
- [SDR USAA990178](https://openairdocs.org/sdr/USAA990178), Mar 8, 1999: SKIN. DISTORTED. CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND SKIN DISTORTED ON FUSELAGE BETWEEN STATION 867 TO 887 BETWEEN STRINGER 22R TO 23R. INSTALLED DOUBLER PER SRM 53-
- [SDR USAA990177](https://openairdocs.org/sdr/USAA990177), Mar 8, 1999: FRAME. CRACKED. CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK STATION 787 BETWEEN S8L AND 9L FRAME. INSTALLED DOUBLER PER EA 63838A AND SRM 53-00-07. (M)
- [SDR USAA990176](https://openairdocs.org/sdr/USAA990176), Mar 8, 1999: FRAME. CRACKED. CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK STATION 867 BETWEEN S8L AND 9L FRAME. INSTALLED DOUBLER PER EA 63838A AND SRM 53-00-07. (M)
- [SDR USAA990175](https://openairdocs.org/sdr/USAA990175), Mar 8, 1999: FRAME. CRACKED. CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STATION 867L BETWEEN S8L AND 9L FRAME. INSTALLED DOUBLER PER EA 63838A AND SRM 53-00-07 FIG 202
- [SDR USAA990174](https://openairdocs.org/sdr/USAA990174), Mar 8, 1999: FRAME. CRACKED. CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK STATION 827 BETWEEN S8L AND 9L FRAME. INSTALLED DOUBLER PER EA 63838A AND SRM 53-00-07. (M)
- [SDR USAA990173](https://openairdocs.org/sdr/USAA990173), Mar 8, 1999: FRAME. CRACKED. CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK STATION 747 BETWEEN S8L AND 9L FRAME. INSTALLED DOUBLER PER EA 63838A AND SRM 53-00-07. (M)
- [SDR USAA990172](https://openairdocs.org/sdr/USAA990172), Mar 8, 1999: FRAME. CRACKED. CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STATION 747L BETWEEN S8L AND 9L FRAME. INSTALLED DOUBLER PER EA 63838A AND SRM 53-00-07. (M)
- [SDR USAA990171](https://openairdocs.org/sdr/USAA990171), Mar 8, 1999: FRAME. CRACKED. CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK STATION 727F BETWEEN S8R AND 9R FRAME. INSTALLED DOUBLER PER EA 63838A AND SRM 53-00-07. (M)
- [SDR USAA990170](https://openairdocs.org/sdr/USAA990170), Mar 8, 1999: FRAME. CRACKED. CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK STATION 727B BETWEEN S8L AND 9L FRAME. INSTALLED DOUBLER PER EA 63838A AND SRM 53-00-07 FIG 202.
- [SDR USAA990169](https://openairdocs.org/sdr/USAA990169), Mar 8, 1999: FRAME. CRACKED. CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK STATION 500D BETWEEN S8R AND 9R FRAME. INSTALLED DOUBLER PER EA 63838A AND SRM 53-00-07. (M)
- [SDR USAA990168](https://openairdocs.org/sdr/USAA990168), Mar 8, 1999: FRAME. CRACKED. CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK STATION 500A BETWEEN S8R AND 9R FRAME. INSTALLED DOUBLER PER EA 63838A AND SRM 53-00-07. (M)
- [SDR USAA990167](https://openairdocs.org/sdr/USAA990167), Mar 8, 1999: FRAME. CRACKED. CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK STATION 500A BETWEEN S8L AND 9L. INSTALLED DOUBLER PER EA 63838A AND SRM 53-00-07. (M)
- [SDR USAA990166](https://openairdocs.org/sdr/USAA990166), Mar 8, 1999: FRAME. CRACKED. CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK STATION 480 BETWEEN S8L AND 9L FRAME. INSTALLED DOUBLER PER EA 63838A AND SRM 53-00-07 FIG 202. 
- [SDR USAA990165](https://openairdocs.org/sdr/USAA990165), Mar 8, 1999: FRAME. CRACKED. CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK STATION 440 BETWEEN S8R AND 9R FRAME. INSTALLED DOUBLER PER EA 63838A AND SRM 53-00-07 FIG 202. 
- [SDR USAA990164](https://openairdocs.org/sdr/USAA990164), Mar 8, 1999: FRAME. CRACKED. CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK STATION 400 BETWEEN S8L AND 9L FRAME. INSTALLED DOUBLER PER EA 63838A AND SRM 53-00-07 FIG 202. 
- [SDR USAA990143](https://openairdocs.org/sdr/USAA990143), Mar 8, 1999: FRAME. CRACKED. CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK STATION 380 BETWEEN S8R AND 9R. INSTALLED DOUBLER PER EA 63838A AND SRM 53-00-07. (M)
- [SDR USAA990142](https://openairdocs.org/sdr/USAA990142), Mar 8, 1999: FRAME. CRACKED. CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK STATION 380 BETWEEN S8L AND 9L. INSTALLED DOUBLER PER EA 63838A AND SRM 53-00-07 FIG 202. (M)
- [SDR USAA990138](https://openairdocs.org/sdr/USAA990138), Mar 8, 1999: FLOORBEAM. CORRODED. CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND CORROSION .5 BY .5 INCH AT BS 967 RBL 18 FLOORBEAM, CORROSION TASK NR C53-107-02. INSTALLED 'T' CAP WITH REPAIR 
- [SDR USAA990137](https://openairdocs.org/sdr/USAA990137), Mar 8, 1999: FLOORBEAM. CORRODED. CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND CORROSION .5 BY .5 INCH AT BS 947 LBL 15 RBL 15 AROUND NUT PLATE HOLES FLOORBEAM. CORROSION TASK NR C53-107-02. 
- [SDR USAA990136](https://openairdocs.org/sdr/USAA990136), Mar 8, 1999: BEAM. CORRODED. CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 2 INCH STATION 312 LBL 11 BEAM. REPAIRED PER SRM 53-10-51. (M)
- [SDR USAASB98291](https://openairdocs.org/sdr/USAASB98291), Oct 31, 1998: ACM. FAILED. TPA - FLT 1425 - AFTER TAKEOFF FROM TPA, CREW COULD NOT GET THE AIRCRAFT TO PRESSURIZE. CREW WENT THROUGH ALL PROCEDURES BUT AIRCRAFT FAILED TO PRESSURIZE. DIFF
- [SDR USAASB98253](https://openairdocs.org/sdr/USAASB98253), Sep 24, 1998: OVERHEAT LOOP. FAILED. CLT - FLT 835 - DURING CLIMB-OUT FROM CLT, THE NR 1 ENGINE OVERHEAT LIGHT ILLUMINATED. AFTER ACCOMPLISHING APPROPRIATE CHECKLIST, LIGHT EXTINGUISHED. FLIGHT RET
- [SDR USAASB96089](https://openairdocs.org/sdr/USAASB96089), May 17, 1996: FUSE. FAILED. LGA - MAINTENANCE FOUND THE EMERGENCY EXIT AISLE LIGHTS, IN ROW 24 AND 25, WON'T ILLUMINATE. MAINTENANCE REPLACED FUSE IN BATTERY PACK. (M)
- [SDR USAASB96027](https://openairdocs.org/sdr/USAASB96027), Feb 9, 1996: WINDSHIELD. SHATTERED. TPA - FL 1798 - EN ROUTE CLT-SRQ - THE CAPTAINS OUTER WINDOW PANE SHATTERED. THE FLIGHT DIVERTED TO TPA AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACE
- [SDR USAA951045](https://openairdocs.org/sdr/USAA951045), Sep 26, 1995: AIR DATA COMP. FAILED. PIT - FLT NR 0497 - AFTER TAKEOFF FROM PIT, FLIGHT OFFICERS AIRSPEED, ALTIMETER, AND RATE OF CLIMB INDICATORS FAILED. FLIGHT RETURNED TO PIT AND LANDED WITHOUT 
- [SDR USAA950489](https://openairdocs.org/sdr/USAA950489), Apr 20, 1995: INTERCOSTAL. CORRODED. INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND CORROSION 2 INCH BY 2 INCH BS 747 TO BSL 767 LBL 24 INCHES. REPAIRED PER SRM 51-10-2. CORROSION TASK NR C53-107-
- [SDR USAA950497](https://openairdocs.org/sdr/USAA950497), Apr 4, 1995: ANGLE. CORRODED. INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORRODED AREA (SIZE UNKNOWN) BS 967-986.5 AT AFT SERVICE DOOR. REPAIRED PER SRM 51-10-2. CORROSION TASK NR C53-1
- [SDR USAA950496](https://openairdocs.org/sdr/USAA950496), Apr 4, 1995: ANGLE. CORRODED. INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORRODED AREA (SIZE UNKNOWN) BS 927 TO BS 1006 AT AFT ENTRY DOOR. REPAIRED PER SRM 51-10-2. CORROSION TASK NR C5

All 61: https://openairdocs.org/deregistered/N407US-2003-09-09/reports.md

## FAA accident and incident reports (1)

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 19910113001649I](https://openairdocs.org/incident/19910113001649I), Jan 13, 1991: Boeing 737401 (N407US), Charlotte, NC. Electrical fumes in cabin on climb. Declared emergency and returned. Upper mid strobe failed and breakers popped.

## Other aircraft with N407US

- [Registered now](https://openairdocs.org/aircraft/N407US): Bell Helicopter Textron Canada 407, S/N 53057, built 1996

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