# N737DX: 1990 Boeing 737-408, registration cancelled 2013-07-29

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: July 29, 2013
- Exported to: Canada
- Status when cancelled: Valid registration
- Airframe: [Boeing 737-408](https://openairdocs.org/model/boeing-737-408) (registry code 13844BT)
- 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: 24804
- Year built: 1990
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: December 31, 1998
- Certificate issued: January 12, 2012
- Last registry action: January 12, 2012
- Mode S code: A9E56D
- Owner when cancelled: [International Trading Company Of Yukon Inc](https://openairdocs.org/faa-owner/INTERNATIONAL%20TRADING%20COMPANY%20OF%20YUKON%20INC)
- Location: [Oklahoma City, OK](https://openairdocs.org/faa-place/OK/Oklahoma%20City)
- Owner type: Corporation
- Owner's area on the map: 35.5813° N, 97.5737° W: Placed by OpenAirDocs at the center of ZIP code 73120, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N737DX
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=737DX
- Page: https://openairdocs.org/deregistered/N737DX-2013-07-29

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 737-408: https://openairdocs.org/model/boeing-737-408.md

## Service difficulty reports (17)

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

- [SDR I5EA2012030102](https://openairdocs.org/sdr/I5EA2012030102), Mar 1, 2012: LIGHT. INOPERATIVE. EMERGENCY EXIT LIGHT INOP AT R2 DOOR.
- [SDR I5EA2012030101](https://openairdocs.org/sdr/I5EA2012030101), Mar 1, 2012: LIGHT. INOPERATIVE. EMERGENCY EXIT LIGHT INOP AT L1 DOOR.
- [SDR I5EA20111106](https://openairdocs.org/sdr/I5EA20111106), Nov 15, 2011: STRUCTURE. CRACKED. FOUND CRACK AT THE FRONT OF THE RUDDER BETWEEN RUD STA 116.14 AND 115.40. AWT ENGINEERING RESPONSE FROM BOEING FOR REPAIR.
- [SDR I5EA20110902](https://openairdocs.org/sdr/I5EA20110902), Jul 11, 2011: BATTERY PACK. DISCHARGED. RIGHT OVERWING EXIT, LEFT OVERWING EXIT AND AISLE 6 EMERGENCY LIGHTS INOP.
- [SDR I5EA20110701](https://openairdocs.org/sdr/I5EA20110701), Jul 8, 2011: BATTERY PACK. FAILED. EMERGENCY LIGHTS ON POWER PACK M1133 SLIGHTLY DIMMER THAN OTHER ZONES.
- [SDR PIDA06128](https://openairdocs.org/sdr/PIDA06128), Dec 20, 2006: BUSHING. MIGRATED. REPLACED THE FUSE PIN BUSHING IN THE LEFT ENGINE STRUT MID-SPAR ATTACH FITTING PER BOEING SB 737-54-1037 DUE TO BUSHING MIGRATION.
- [SDR PIDA06121](https://openairdocs.org/sdr/PIDA06121), Dec 19, 2006: SKIN. DAMAGED. THE EXTERIOR SKIN OF THE AFT CARGO DOOR WAS REPLACED PER SRM 52-30-01 DUE TO MULTIPLE AREAS OF DAMAGE.
- [SDR PIDA06123](https://openairdocs.org/sdr/PIDA06123), Dec 15, 2006: SKIN. CORRODED. CORROSION ON THE INNER SKIN OF THE RIGHT ENGINE I/B THRUST REVERSER WAS REPAIRED PER EA 71-349.
- [SDR PIDA06122](https://openairdocs.org/sdr/PIDA06122), Dec 14, 2006: STRIP. WORN. A WEAR STRIP WAS INSTALLED ON THE I/B SIDE OF THE LEFT ENGINE PYLON PER BOEING SB 737-54-1031 DUE TO WEAR MARKS JUST ABOVE THE THRUST REVERSER SLIDER.
- [SDR PIDA06127](https://openairdocs.org/sdr/PIDA06127), Dec 13, 2006: SKIN. DENTED. DENT IN FUSELAGE SKIN AT BS 867+4 JUST BELOW STR 17 LT WAS REPAIRED PER SRM 53-00-01 REPAIR 31.
- [SDR PIDA06107](https://openairdocs.org/sdr/PIDA06107), Dec 8, 2006: TEE FITTING. CRACKED. AFT CARGO DOOR T-CHORD CRACKED AT FASTENER HOLE ON NR 4 FRAME. REPAIRED T-CHORD PER BOEING DWG 65-47952 AND SRM 51-70-12.
- [SDR PIDA2005006](https://openairdocs.org/sdr/PIDA2005006), Apr 16, 2005: COMPUTER. FAILED. AUTO FLIGHT CONTROL SYSTEM A FCC DC CIRCUIT BREAKER TRIPPED IN FLIGHT. WILL NOT RESET. RESULTING FLIGHT DIRECTOR FLAG IN VIEW. REPLACED FLIGHT CONTROL COMPUTER.
- [SDR 737DX0004](https://openairdocs.org/sdr/737DX0004), Jul 22, 2004: SEAT TRACK. CORRODED. SEAT TRACK CORRODED FROM BS 328 TO BS 345 RBL 22. REPLACED SECTION OF SEAT TRACK INTERCOSTAL PER BOEING DRAWING 65C34624 AND SRM 53-20-01.
- [SDR 737DX0005](https://openairdocs.org/sdr/737DX0005), Jul 20, 2004: INTERCOSTAL. CORRODED. INTERCOSTAL AT BS 336.5 RBL 34 IS CORRODED. REPLACED INTERCOSTAL PER BOEING DRAWING 65C34625 AND SRM 51-10-2.
- [SDR 737DX0003](https://openairdocs.org/sdr/737DX0003), Feb 20, 2004: LIMITER. MALFUNCTIONED. AILERON FORCE LIMITER FAILED LRU INTERFACE TEST 50 PERCENT OF THE TIME. REPLACED AILERON FORCE LIMITER PER MM 22-11-13. OPS CHECKS GOOD PER MM 22-11-13.
- [SDR 737DX0002](https://openairdocs.org/sdr/737DX0002), Nov 10, 2003: STRINGER CLIP. DAMAGED. STRINGER TO FRAME TIE DAMAGED, FORWARD SIDE OF BS 400 FRAME AT STR 28 LT. REPLACED STRINGER TO FRAME TIE PER SRM 51-40-02.
- [SDR 737DX0001](https://openairdocs.org/sdr/737DX0001), Nov 3, 2003: BATTERY PACK. INOPERATIVE. NEXT TO AFT RT BULLNOSE EMERGENCY EXIT LIGHT, RT AFT EXTERIOR DOOR EMERGENCY LIGHT, AND AFT RT GALLEY EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY PACK. OPS CHEC

## Other aircraft with N737DX

- [Cancelled 1990-09-07](https://openairdocs.org/deregistered/N737DX-1990-09-07): Cessna 172N, S/N 17269348. N-number assigned, not yet registered

---
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.