# N14239: Boeing 737-214, registration cancelled 2000-05-02 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: May 2, 2000 - Status when cancelled: Valid registration - Airframe: [Boeing 737-214](https://openairdocs.org/model/boeing-737-214) (registry code 138446R) - Data sheets: [TCDS A16WE](https://openairdocs.org/tcds/A16WE) (OpenAirDocs) - Serial number: 19920 - Type of aircraft: Fixed wing multi engine - Certificate issued: January 29, 1999 - Last registry action: January 29, 1999 - Mode S code: A0AD01 - Owner when cancelled: [Rfc 737/23 Inc](https://openairdocs.org/faa-owner/RFC%20737%2F23%20INC) - 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/N14239 - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=14239 - Page: https://openairdocs.org/deregistered/N14239-2000-05-02 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 737-214: https://openairdocs.org/model/boeing-737-214.md ## Service difficulty reports (33) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR CALA9801831](https://openairdocs.org/sdr/CALA9801831), Sep 21, 1998: LINE. LEAKING. THE A-SYSTEM HYDRAULIC QUANTITY AND PRESSURE WAS LOST AFTER TAKEOFF. A MANUAL GEAR EXTENSION WAS ATTEMPTED. THE NOSE GEAR DID NOT EXTEND ON FIRST PULL OF HANDLE - [SDR CALA9700350](https://openairdocs.org/sdr/CALA9700350), Mar 17, 1997: HYD LINE. LEAKING. THE COCKPIT AND CABIN FILLED WITH SMOKE AFTER TAKEOFF FROM EWR. THE AIR CONDITIONING SMOKE CHECKLIST WAS ACCOMPLISHED AND A RETURN TO EWR WAS BEGUN. THE CREW NO - [SDR CALA9601368](https://openairdocs.org/sdr/CALA9601368), Sep 18, 1996: FLOORBEAM. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN MAIN CABIN FLOORBEAM AT STA 724, BL 0. THE WEB AND STIFFENER WERE REMOVED IAW SRM 51-30-2. A WEB AND DOUBLER WERE FABRICATED - [SDR CALA9601367](https://openairdocs.org/sdr/CALA9601367), Sep 18, 1996: FITTING. GOUGED. INSPECTION FOUND THE RT HORIZONTAL STABILIZER UPPER AFT SPAR INBOARD ATTACH FITTING GOUGED. THE ATTACH FITTING WAS REPAIRED IAW ECRA 5510-01338. - [SDR CALA9601366](https://openairdocs.org/sdr/CALA9601366), Sep 18, 1996: FLOORBEAM. CRACKED. INSPECTION FOUND A 1.5 INCH CRACK IN FLOORBEAM AT STA 684, LBL 24.8. THE FLOORBEAM WAS REPAIRED IAW EA 5710-01638 AND SRM 51-40-4. - [SDR CALA9601365](https://openairdocs.org/sdr/CALA9601365), Sep 18, 1996: SKIN. CRACKED. INSPECTION FOUND FOUR .125 INCH CRACKS IN SECTION 41, LT FORWARD FUSELAGE EXTERNAL SKIN PANEL. THE CRACKED AREA WAS CUT OUT, FILLERS AND DOUBLERS WERE FABRICATE - [SDR CALA9601364](https://openairdocs.org/sdr/CALA9601364), Sep 18, 1996: SKIN. CRACKED. INSPECTION FOUND THREE .125 INCH CRACKS IN SECTION 41R, RT FORWARD FUSELAGE EXTERNAL SKIN PANEL. THE CRACKED AREA WAS CUT OUT, FILLERS AND DOUBLERS WERE FABRICA - [SDR CALA9601363](https://openairdocs.org/sdr/CALA9601363), Sep 18, 1996: KEEL BEAM. GALLED. INSPECTION FOUND LT KEEL BEAM FAYING FLANGE FROM BS 663 TO 727 GALLED ON LOWER SURFACE AND WORN AROUND FASTENER HOLES ON UPPER SURFACE. EXISTING HOLES WERE OVER - [SDR CALA9601362](https://openairdocs.org/sdr/CALA9601362), Sep 18, 1996: FLANGE. GALLED. INSPECTION FOUND RT KEEL BEAM FAYING FLANGE FROM BS 663 TO BS 727 GALLED ON LOWER SURFACE AND WORN AROUND FASTENER HOLES ON UPPER SURFACE. A REPAIR STRAP WAS FA - [SDR CALA9601361](https://openairdocs.org/sdr/CALA9601361), Sep 18, 1996: FRAME. CRACKED. INSPECTION FOUND A 2.5 INCH CRACK IN FRAME AT STA 947, STRINGER 18R. THE FRAME WAS REPAIRED IAWS SRM 53-10-2, 53-10-4, 51-10-7, 51-10-2 AND 51-30-2. - [SDR CALA9601360](https://openairdocs.org/sdr/CALA9601360), Sep 18, 1996: FLOORBEAM. CRACKED. INSPECTION FOUND A 2 INCH CRACK IN FLOORBEAM AT STA 684, RBL 24.8. THE FLOORBEAM WAS REPAIRED IAW EA 5710-01638 AND SRM 51-40-4. - [SDR CALA9601359](https://openairdocs.org/sdr/CALA9601359), Sep 18, 1996: CHORD ANGLE. CRACKED. INSPECTION FOUND A 3.25 INCH CRACK IN MAIN CABIN FLOORBEAM LOWER CHORD ANGLE AT STA 673, BL 0. THE AREA WAS REPAIRED IAW BOEING DRAWING 65-45410, CAL ENGINEERIN - [SDR CALA9601358](https://openairdocs.org/sdr/CALA9601358), Sep 18, 1996: ANGLE. CRACKED. INSPECTION FOUND A .5 INCH CRACK THROUGH RADIUS OF RT WING ROOT FORWARD FILLET PANEL SUPPORT ANGLE. THE CRACK WAS LOCATED AT STA 540, 10 INCHES BELOW LOWER CAP - [SDR CALA9601357](https://openairdocs.org/sdr/CALA9601357), Sep 18, 1996: STIFFENER. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN STIFFENER BETWEEN STRINGER 10L AND 11L AT FS 295. THE CRACKED SECTION OF STIFFENER WAS REMOVED AND A NEW SECTION WAS FABRICA - [SDR CALA9601356](https://openairdocs.org/sdr/CALA9601356), Sep 18, 1996: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM AND SUPPORT CORRODED AT AFT CABIN L-2 DOOR THRESHOLD, STA 986. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-9, 51-10-2 AND 51- - [SDR CALA9601355](https://openairdocs.org/sdr/CALA9601355), Sep 18, 1996: SKIN. CORRODED. INSPECTION FOUND SKIN BULGED/CORRODED WITH POPPED FASTENERS AT FORWARD INBOARD CORNER OF AFT LAV DUMP CHUTE DOOR CUTOUT. THE CORRODED AREA OF SKIN WAS REMOVED I - [SDR CALA9601354](https://openairdocs.org/sdr/CALA9601354), Sep 18, 1996: STRINGER. CRACKED. INSPECTION FOUND A 1.25 INCH CRACK IN WING SUPPORT STRINGER AT RIGHT WBL 70.85, WS 6. THE CRACKED SECTION OF STRINGER WAS CUT OUT, A REPAIR WAS FABRICATED AND I - [SDR CALA9601353](https://openairdocs.org/sdr/CALA9601353), Sep 18, 1996: SKIN. DENTED. INSPECTION FOUND A 3 BY 5 INCH AREA OF FUSELAGE SKIN DENTED AT BS 890, LT SIDE, TOP OF WINDOW BELT. THE DENTED AREA WAS CUT OUT, DOUBLER AND FILLER WERE FABRICA - [SDR CALA9601352](https://openairdocs.org/sdr/CALA9601352), Sep 18, 1996: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM CORRODED BETWEEN SEAT TRACK ROW D AND CUSP LINE AT STA 360. A NEW FLOORBEAM WAS FABRICATED AND INSTALLED IAW SRM 53-10-9, 51-10-2 AND - [SDR CALA9601351](https://openairdocs.org/sdr/CALA9601351), Sep 18, 1996: BULKHEAD. CRACKED. INSPECTION FOUND A 3.25 CRACK IN R/H SIDE OF PRESSURE BULKHEAD AT STA 178. THE BULKHEAD WAS REPAIRED IAW SRM 53-10-11 AND 53-10-2. - [SDR CALA9601350](https://openairdocs.org/sdr/CALA9601350), Sep 18, 1996: BEAM. CRACKED. INSPECTION FOUND A 3 INCH CRACK IN RADIUS OF TRANSVERSE BEAM AT STA 685. THE CRACK WAS STOP DRILLED, REPAIR ANGLES AND RADIUS FILLERS WERE FABRICATED AND INSTAL - [SDR CALA9601349](https://openairdocs.org/sdr/CALA9601349), Sep 18, 1996: STRINGER. CRACKED. INSPECTION FOUND A 1.125 INCH CRACK IN STRINGER 17R BELOW CABIN FLOOR AT FS 837. REPAIR DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 51-40-4, 51-10-2 AND 51-3 - [SDR CALA9601348](https://openairdocs.org/sdr/CALA9601348), Sep 18, 1996: STRINGER. CRACKED. INSPECTION FOUND A .75 INCH CRACK AT RT OUTBOARD END OF CENTER WING BOX UPPER STRINGER NR 3. THE CRACKED SECTION OF STRINGER WAS CUT OUT, A REPAIR WAS FABRICATE - [SDR CALA9601347](https://openairdocs.org/sdr/CALA9601347), Sep 18, 1996: STRINGER. CRACKED. INSPECTION FOUND A .75 INCH CRACK IN STRINGER 12L AT STA 295. THE STRINGER WAS REPAIRED IAW SRM 53-10-2. - [SDR CALA9601149](https://openairdocs.org/sdr/CALA9601149), Aug 11, 1996: GCU. INOPERATIVE. THE LEFT BUS OFF LIGHT COME ON SHORTLY AFTER TAKEOFF. THE LIGHT WAS ACCOMPANIED BY AN ELECTRICAL ODOR OR AIR CONDITIONING PACK SMELL AND A CLICKING SOUND, LIKE - [SDR CALA9601042](https://openairdocs.org/sdr/CALA9601042), Jul 21, 1996: HYD LINE. LEAKING. THE A-SYSTEM HYDRAULIC QUANTITY BEGAN TO DROP SHORTLY AFTER TAKEOFF. THE AIRCRAFT WAS RETURNED TO CLE WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NO - [SDR CAL951064](https://openairdocs.org/sdr/CAL951064), Nov 21, 1995: DNLOCK ACTUATOR. BROKEN. FLT NR 1249 - EWR - THE RIGHT MLG WOULD NOT RETRACT AFTER DEPARTING BDL FOR CLE. THE GEAR WAS VISUALLY CONFIRMED DOWN AND LOCKED AND THE AIRCRAFT WAS DIVERTED T - [SDR CAL950661](https://openairdocs.org/sdr/CAL950661), Aug 5, 1995: FRAME. CRACKED. GSO - INSPECTION FOUND A .5 INCH CRACK IN FRAME AT STATION 440L BETWEEN STRINGERS 19L-20L. THE CRACKED FRAME SECTION WAS CUT OUT. A NEW FRAME AND CHORD SPLICES - [SDR CAL950659](https://openairdocs.org/sdr/CAL950659), Aug 5, 1995: FRAME. CRACKED. GSO - INSPECTION FOUND A .5 INCH CRACK IN FRAME AT BS 639R, STRINGER 16. REMOVED CRACKED UPPER CHORD AND FRAME WEB AND INSTALLED REPAIR PARTS IAW BOEING DRAWING - [SDR CAL950658](https://openairdocs.org/sdr/CAL950658), Aug 5, 1995: FLOOR BEAM. CORRODED. GSO - INSPECTION FOUND CORROSION ON FLOOR BEAM UNDER COCKPIT FLOOR PANEL AT STATION 250, BBL 0. A WEB AND FILLER REPAIR WERE FABRICATED AND INSTALLED IAW SRM 51 - [SDR CAL950657](https://openairdocs.org/sdr/CAL950657), Aug 5, 1995: FRAME. CRACKED. GSO - INSPECTION FOUND A .75 INCH CRACK IN FORWARD GALLEY DOOR LOWER SIDE OF FRAME AT LOWER FORWARD STOP FITTING. THE CRACKED SEGMENT OF FRAME WAS REMOVED. A NE - [SDR CAL950656](https://openairdocs.org/sdr/CAL950656), Aug 5, 1995: FRAME. CRACKED. GSO - INSPECTION FOUND A .5 INCH CRACK IN FRAME AT STATION 420L BETWEEN STRINGERS 20L-21L. THE DAMAGE WAS CUT OUT AND A NEW FRAME, CHORD, AND SPLICES WERE INSTA - [SDR CAL950654](https://openairdocs.org/sdr/CAL950654), Aug 5, 1995: FRAME. CRACKED. GSO - INSPECTION FOUND A .75 INCH CRACK IN FRAME AT STATION 460L AND STRINGERS 21L-22L. CUT OUT DAMAGE AND INSTALLED A NEW FRAME, CHORD AND SPLICES IAW SRM 51-3 --- 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.