# N413US: 1988 Boeing 737-401, registration cancelled 2003-09-18

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: September 18, 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: 23882
- Year built: 1988
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: November 14, 1988
- Certificate issued: April 24, 2003
- Last registry action: April 24, 2003
- Mode S code: A4E118
- 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/N413US
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=413US
- Page: https://openairdocs.org/deregistered/N413US-2003-09-18

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 737-401: https://openairdocs.org/model/boeing-737-401.md

## Service difficulty reports (65, newest 50)

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

- [SDR USAASB02127](https://openairdocs.org/sdr/USAASB02127), Jun 29, 2002: BATTERY PACK. NOT SEATED. IND - MAINTENANCE FOUND THE EMERGENCY LIGHTS AT SEAT ROWS 20 THROUGH 23 AND AT THE AFT LEFT SERVICE DOOR INOPERATIVE. MAINTENANCE RERACKED THE BATTERY PACK. OPE
- [SDR USAASB02077](https://openairdocs.org/sdr/USAASB02077), Apr 22, 2002: CHARGER. INOPERATIVE. PIT - FOUND CIRCUIT INOPERATIVE ON EMERGENCY LIGHT BATTERY CHARGER. MAINTENANCE REPLACED THE BATTERY CHARGER. (M)
- [SDR USAASB02076](https://openairdocs.org/sdr/USAASB02076), Apr 22, 2002: FUSE. BROKEN. PIT - FOUND BROKEN FUSE ON EMERGENCY LIGHT CHARGER. MAINTENANCE REPLACED THE CHARGER. (M)
- [SDR USAASB02028](https://openairdocs.org/sdr/USAASB02028), Feb 5, 2002: SMOKE DETECTOR. MALFUNCTIONED. CLT - FLT 417 - ON CLIMB-OUT FROM CLT, EN ROUTE TO SRQ, THE FLIGHT ATTENDANT REPORTED THE FORWARD LAVATORY SMOKE DETECTOR ALARM SOUNDING. FLIGHT RETURNED TO FIE
- [SDR USAA011387](https://openairdocs.org/sdr/USAA011387), Nov 16, 2001: SKIN. CRACKED. TPA - FOUND SKIN .250 INCH, UPPER HINGE CUTOUT ON MAIN ENTRY DOOR. INSTALLED DOUBLER PER SB 737-52-1096 ALSO EA NR 94248. (M)
- [SDR USAA010958](https://openairdocs.org/sdr/USAA010958), Jul 27, 2001: BULKHEAD. DAMAGED. CLT - FOUND PRESSURE WEB WITH ELONGATED HOLES, .281 INCH TO .321 INCH, BS 178, WL 207. DAMAGE REMOVED, INSTALLED ACCESS HOLE DOUBLER PER EA 85146. (M)
- [SDR USAA010959](https://openairdocs.org/sdr/USAA010959), Jul 27, 2001: BULKHEAD. CRACKED. CLT - FOUND PRESSURE WEB CRACKED .5 INCH, BS 178 WL 217 AT LBL 6. DAMAGE REMOVED, REPAIR DOUBLER INSTALLED PER EO 5300V153. (M)
- [SDR USAA010960](https://openairdocs.org/sdr/USAA010960), Jul 27, 2001: STIFFENER. CRACKED. CLT - FOUND VERTICAL CHORD CRACKED IN TWO PLACES .25 INCH EACH, BS 178, WL 184 AND 195 AT LBL 5.7. DOUBLER INSTALLED PER EO 5300V155. (M)
- [SDR USAA010956](https://openairdocs.org/sdr/USAA010956), Jul 27, 2001: FRAME. CRACKED. CLT - FOUND SIDE CHORDS .5 INCH, BS 178 WL 207 LEFT AND RIGHT SIDE. DAMAGE SECTION REMOVED, INSTALLED CHORD SPLICE REPAIR AND EXT SKIN STRAP PER EO 5300V157. (M
- [SDR USAA010957](https://openairdocs.org/sdr/USAA010957), Jul 27, 2001: STRAP. DAMAGED. CLT - FOUND VERTICAL STRAP .125 INCH, BS 178, WL 208, LBL 25. DAMAGE SECTION REMOVED, REPLACEMENT SECTION SPLICED IN WITH DOUBLER PER EA 85114. (M)
- [SDR USAA010681](https://openairdocs.org/sdr/USAA010681), Jun 14, 2001: SKIN. CRACKED. CLT - FOUND SKIN CRACKED, BS 727D, LEFT SIDE, EMERGENCY LIGHT AFT OF WHEEL WELL. DAMAGE REMOVED, INSTALLED DOUBLER PER SRM 53-00-01, FIG 202. (M)
- [SDR USAA010586](https://openairdocs.org/sdr/USAA010586), May 10, 2001: SKIN. CRACKED. PIT - FOUND SKIN CRACKED 2.5 INCHES, STRINGER 23R STATION 727D. CUT OUT DAMAGE, INSTALLED EXTERNAL DOUBLER PER EA 71032 AND SRM 53-00-01 FIG 202. (M)
- [SDR USAA010277](https://openairdocs.org/sdr/USAA010277), Feb 14, 2001: FRAME. CRACKED. CLT - FOUND FRAME CRACKED .5 INCH, STATION 400 FRAME RIGHT SIDE BETWEEN STRINGER 8R AND 9R. REMOVED DAMAGED, REPAIRED TR 53-10-14. (M)
- [SDR USAASB01038](https://openairdocs.org/sdr/USAASB01038), Feb 5, 2001: BLADE. DAMAGED. BWI - FLT 1882 - EN ROUTE FROM CLT TO PHL, BOTH ENGINE VIBRATION INDICATORS APPROACHED NR 5. FLIGHT DIVERTED TO BWI AND LANDED WITHOUT FURTHER INCIDENT. UPON AR
- [SDR USAASB00327](https://openairdocs.org/sdr/USAASB00327), Nov 24, 2000: TRANSMITTER. FAILED. PHL - FLT 80 - EN ROUTE FROM PIT TO PHL, THE NR 2 ENGINE OIL PRESSURE DROPPED TO 20 PSI, THEN TO RED RADIAL. OIL TEMPERATURE AND OIL QUANTITY WERE BOTH NORMAL. 
- [SDR USAASB00249](https://openairdocs.org/sdr/USAASB00249), Sep 10, 2000: WIRE. BROKEN. CLT - FLT 1620 - ON FINAL APPROACH, AT FL030, A FLAP ASYMMETRY OCCURRED. AS CREW EXTENDED FLAPS FROM 5 TO 10 DEGREES, RIGHT FLAP NEEDLE WENT OT 10 DEGREES AND L
- [SDR USAASB00070](https://openairdocs.org/sdr/USAASB00070), Mar 11, 2000: CONTROLLER. FAILED. BDL - FLT 519 - DURING CLIMB-OUT FROM BDL, AT APPROXIMATELY FL210, THE CABIN WARNING HORN SOUNDED. NO OTHER WARNING INDICATORS ILLUMINATED. CABIN ALTITUDE WAS C
- [SDR USAASB99130](https://openairdocs.org/sdr/USAASB99130), May 17, 1999: CONNECTOR. LOOSE. TPA - MAINTENANCE FOUND THE EMERGENCY AISLE LIGHTING AT SEAT ROW 6A AND THE FIRST CLASS CABINET, LEFT SIDE INOPERATIVE. MAINTENANCE FOUND THE CANNON PLUG AT THE
- [SDR USAA990429](https://openairdocs.org/sdr/USAA990429), May 2, 1999: FRAME. CRACKED. CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .375 INCH CRACK IN FRAME AT BS 400 BETWEEN STRINGER 8L AND STRINGER 9. FABRICATED DOUBLER AND INSTALLED PER EA
- [SDR USAA990428](https://openairdocs.org/sdr/USAA990428), May 2, 1999: ANGLE. CRACKED. CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK IN RADIUS AT STATION 294.5 RBL 54.75 WL 208 ANGLE. INSTALLED DOUBLER ANGLE PER SRM 51-70-11. (M)
- [SDR USAA990427](https://openairdocs.org/sdr/USAA990427), May 2, 1999: FLOORBEAM. CORRODED. CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND CORROSION AT STATION 986.5 ALONG ENTIRE FLOORBEAM CORROSION TASK NR C53-107-02. INSTALLED NEW T-CAP, STRAPS, AND
- [SDR USAA990426](https://openairdocs.org/sdr/USAA990426), May 2, 1999: BEAM. CORRODED. CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 1 INCH SPOT OF SURFACE CORROSION AT FS 328 RBL 40 BEAM, CORROSION TASK NR C53-107-02. SPLICED IN NEW SECTION O
- [SDR USAA990425](https://openairdocs.org/sdr/USAA990425), May 2, 1999: BULKHEAD. CORRODED. CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 5.3 INCH BY 3.5 INCH AREA OF CORROSION AT RBL 3 STATION 1016 PLUS 5 INCHES BL 0 PRESS BULKHEAD. INSTALLED DOUB
- [SDR USAA990424](https://openairdocs.org/sdr/USAA990424), May 2, 1999: STRAP. CORRODED. CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 2 INCH BY 67 INCH AREA OF SPOTTED CORROSION AT RBL 20 STATION 780-847 STRAP. INSTALLED NEW STRAP PER SRM 51-10
- [SDR USAA990419](https://openairdocs.org/sdr/USAA990419), May 2, 1999: FRAME. CRACKED. CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK AT BS 867 BETWEEN STRINGER 8R AND STRINGER 9R FRAME. INSTALLED DOUBLER PER SRM 53-00-07 FIG 202 
- [SDR USAA990418](https://openairdocs.org/sdr/USAA990418), May 2, 1999: FRAME. CRACKED. CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK AT BS 907 BETWEEN STRINGER 8R AND STRINGER 9R FRAME. INSTALLED DOUBLER PER SRM 53-00-07 FIG 202 
- [SDR USAA990417](https://openairdocs.org/sdr/USAA990417), May 2, 1999: FLOOR. CRACKED. CLT - DURING Q-2 CHECK, NDT VISUAL INSPECTION, FOUND A .75 INCH CRACK AT BS 663.75 LBL 32 FLOOR. INSTALLED DOUBLER PER EA 64378. (M)
- [SDR USAA990416](https://openairdocs.org/sdr/USAA990416), May 2, 1999: FRAME. CRACKED. CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK AT BS 787 BETWEEN STRINGER 8R AND STRINGER 9R FRAME. INSTALLED DOUBLER PER SRM 53-00-07 FIG 202 
- [SDR USAA990415](https://openairdocs.org/sdr/USAA990415), May 2, 1999: WEB. CRACKED. CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK AT STATION 178 LBL 4.5 W/L 201 WEB. FABRICATED AND INSTALLED DOUBLER PER EA 6420. (M)
- [SDR USAA990414](https://openairdocs.org/sdr/USAA990414), May 2, 1999: TIE CLIP. CRACKED. CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AT TIE CLIP STATION 767 STRINGER 26L. REMOVED AND REPLACED STRINGER TIE CLIP PER SRM 51-10-2. (
- [SDR USAA990413](https://openairdocs.org/sdr/USAA990413), May 2, 1999: FRAME. CRACKED. CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 9 INCH CRACK IN FRAME AT BS 747 BETWEEN STRINGER 8L AND STRINGER 9L. INSTALLED DOUBLER PER EA 64326. (M)
- [SDR USAA990412](https://openairdocs.org/sdr/USAA990412), May 2, 1999: FLOORBEAM. CORRODED. CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 32 INCH AREA OF CORROSION AT STATION 947.5 LT AND RT OF BL 0 FLOORBEAM. REPAIRED 'T' CAP PER TR 53-60-02. (M)
- [SDR USAA990399](https://openairdocs.org/sdr/USAA990399), May 2, 1999: ANGLE. CORRODED. CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 26 INCH AREA OF CORROSION AT FORWARD ENTRY DOOR THRESHOLD 'Z' ANGLE F/S 270 TO FS 344 LBBL 55. REMOVED AND REP
- [SDR USAA990398](https://openairdocs.org/sdr/USAA990398), May 2, 1999: FLOORBEAM. CORRODED. CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 1 INCH AREA OF SPOTTED CORROSION FROM STATION 787 TO 847 RBL 14 FLOORBEAM. CORROSION TASK NR C53-208-01. REMOV
- [SDR USAA990397](https://openairdocs.org/sdr/USAA990397), May 2, 1999: WEB. CORRODED. CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 14 INCH BY 30 INCH AREA OF SPOTTED CORROSION UNDER AFT CARGO SILL PANEL WEB. CORROSION TASK NR C53-202-07. REM
- [SDR USAA990381](https://openairdocs.org/sdr/USAA990381), May 2, 1999: FRAME. CRACKED. CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK IN FRAME AT BS 727A BETWEEN STRINGER 8R AND STRINGER 9R. REPAIRED DOUBLER PER EA 64326 AND SRM 5
- [SDR USAA990380](https://openairdocs.org/sdr/USAA990380), May 2, 1999: FRAME. CRACKED. CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK IN FRAME AT BS 727D BETWEEN STRINGER 8L AND STRINGER 9L. REPAIRED DOUBLER PER EA 64326 AND SRM 5
- [SDR USAA990379](https://openairdocs.org/sdr/USAA990379), May 2, 1999: FRAME. CRACKED. CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK IN FRAME AT BS 727F BETWEEN STRINGER 8R AND 9R. DOUBLER REPAIRED PER SRM 53-00-07 GIF 202. (M)
- [SDR USAA990378](https://openairdocs.org/sdr/USAA990378), May 2, 1999: FRAME. CRACKED. CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK IN FRAME AT BS 747 BETWEEN STRINGER 8R AND STRINGER 9R. REPAIRED DOUBLER PER EA 64326 AND SRM 53
- [SDR USAA990377](https://openairdocs.org/sdr/USAA990377), May 2, 1999: BEAM. CORRODED. CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND AN AREA OF SURFACE CORROSION SPOTS APPROX 1 INCH AT FS 312, LBBL 24 TO RBBL 12. CORROSION TASK NR C53-107-02. SP
- [SDR USAA990372](https://openairdocs.org/sdr/USAA990372), May 2, 1999: BULKHEAD. CORRODED. CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 6 INCH AREA OF CORROSION AT PRESSURE BULKHEAD RT OF BL 0 JUST AFT STATION 1016. INSTALLED DOUBLER PER SRM 53-8
- [SDR USAA990371](https://openairdocs.org/sdr/USAA990371), May 2, 1999: BULKHEAD WEB. CORRODED. CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND CORROSION AFT PRESSURE BULKHEAD DOME WEB STIFFENER AT BOTTOM OF BL 0 STATION 1016. INSTALLED REPAIR STIFFENER AN
- [SDR USAA990370](https://openairdocs.org/sdr/USAA990370), May 2, 1999: BULKHEAD. CRACKED. CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 1.5 INCH CRACK AT BS 178 RBL .5 WL 188 BULKHEAD WEB. INSTALLED DOUBLER PER SRM 53-10-08. (M)
- [SDR USAA990369](https://openairdocs.org/sdr/USAA990369), May 2, 1999: BEAM. CORRODED. CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND SURFACE CORROSION FS 344 BL 0 TO LBBL 10 BEAM. CORROSION TASK NR C53-107-02. INSTALLED T-CHORD PER EA 64363 AND 
- [SDR USAA990368](https://openairdocs.org/sdr/USAA990368), May 2, 1999: FRAME. CRACKED. CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AT BS 727F BETWEEN STRINGER 8L AND 9L FRAME. INSTALLED DOUBLER PER SRM 53-00-07, SRM 53-30-07, 
- [SDR USAA990367](https://openairdocs.org/sdr/USAA990367), May 2, 1999: FRAME. CRACKED. CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .375 INCH CRACK AT BS 867 BETWEEN STRINGER 8L AND 9L FRAME. INSTALLED DOUBLER PER SRM 53-00-07 AND EA 64326. (
- [SDR USAA990366](https://openairdocs.org/sdr/USAA990366), May 2, 1999: FRAME. CRACKED. CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AT BS 827 BETWEEN STRINGER 8L AND 9L FRAME. INSTALLED FILLER AND DOUBLER PER SRM 53-00-07, 53-3
- [SDR USAA990362](https://openairdocs.org/sdr/USAA990362), May 2, 1999: WEB. CRACKED. CLT - DURNG Q-2 CHECK VISUAL INSPECTION, FOUND A CRACK .5 INCH VERTICAL ON WEB AT STATION 178 RBL 4.5 WL 201 BULKHEAD WEB. INSTALLED DOUBLER AND FILLER PER T/R 
- [SDR USAA990361](https://openairdocs.org/sdr/USAA990361), May 2, 1999: WEB. CRACKED. CLT - DURING Q-2 CHECK VISUAL INSPECTIOIN, FOUND A CRACK .5 INCH VERTICAL ON WEB AT STATION 178 RBL 4.5 WL 198 BULKHEAD WEB. INSTALLED DOUBLER AND FILLER PER T/
- [SDR USAA990510](https://openairdocs.org/sdr/USAA990510), Apr 30, 1999: BULKHEAD ANGLE. DRILL MARKS. CLT - DURING Q-2 CHECK, FOUND 3 PLACES .125 INCH DRILL MARKS AT BS 1030 RBL 23 (UNDER FLOOR ATTACH ANGLE) AT 1016 PRESSURE BULKHEAD. BLENDED AREAS/DRILLED HOLE 

All 65: https://openairdocs.org/deregistered/N413US-2003-09-18/reports.md

## NTSB investigations (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB ATL89IA187](https://openairdocs.org/ntsb/ATL89IA187), Aug 2, 1989: Boeing 737-400 (N413US), Greensboro, NC, incident, minor damage. Probable cause: FAILURE OF THE LINE MECHANIC, A CHECK MECHANIC, AND FIRST OFFICER TO IDENTIFY AND REMOVE THE WHEEL CHOCK FROM THE WHEEL WELL DURING THE REQUIRED INSPECTIONS.

## 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 19890802065989I](https://openairdocs.org/incident/19890802065989I), Aug 2, 1989: Boeing 737401 (N413US), Greensboro, NC, Minor damage. Gear jammed in up position got all but left main down by g force. Landed on 3 gears. Mechanic put chock in gear well

## Other aircraft with N413US

- [Registered now](https://openairdocs.org/aircraft/N413US): Cessna 305A, S/N 23164

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