# N12235: Boeing 737-222, registration cancelled 2000-01-06 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: January 6, 2000 - Status when cancelled: Valid registration - Airframe: [Boeing 737-222](https://openairdocs.org/model/boeing-737-222) (registry code 1384473) - Data sheets: [TCDS A16WE](https://openairdocs.org/tcds/A16WE) (OpenAirDocs) - Serial number: 19758 - Type of aircraft: Fixed wing multi engine - Certificate issued: August 26, 1998 - Last registry action: August 27, 1998 - Mode S code: A05DFF - 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/N12235 - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=12235 - Page: https://openairdocs.org/deregistered/N12235-2000-01-06 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 737-222: https://openairdocs.org/model/boeing-737-222.md ## Service difficulty reports (42) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR CALA9801116](https://openairdocs.org/sdr/CALA9801116), Jun 18, 1998: LIGHT. LOOSE. WHEN GEAR WAS EXTENDED ON APPROACH TO EWR, NEITHER A RED OR GREEN INDICATION WAS RECEIVED FOR RT MLG. THE APPROACH WAS ABORTED, AND WHEN GEAR WAS CYCLED, THE GR - [SDR CALA9701232](https://openairdocs.org/sdr/CALA9701232), Aug 24, 1997: CONNECTOR. SHORTED. THE AIRCRAFT HAD A BRIEF HISTORY OF THE APU FIRE WARNING ACTIVATING DURING FLIGHT. NO EVIDENCE OF FIRE WAS FOUND. TROUBLESHOOTING FOUND APU TAILPIPE DETECTOR CO - [SDR CALA9700705](https://openairdocs.org/sdr/CALA9700705), Apr 23, 1997: ANGLE. CORRODED. INSPECTION FOUND RT WING TO BODY ATTACH ANGLE AT STA 727 TO 727B CORRODED. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 53-50-1 AN - [SDR CALA9700693](https://openairdocs.org/sdr/CALA9700693), Apr 19, 1997: SKIN. CORRODED. INSPECTION FOUND FUSELAGE SKIN CORRODED AT STA 925, STRINGER 26L. THE CORRODED SECTION OF SKIN WAS REMOVED, A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-30-3 AND 5 - [SDR CALA9700691](https://openairdocs.org/sdr/CALA9700691), Apr 16, 1997: FRAME. CRACKED. INSPECTION FOUND A .125 INCH CRACK IN FRAME AT STA 500A, STRINGER 20L AND 21L. THE CRACKED AREA WAS REMOVED, A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10 - [SDR CALA9700679](https://openairdocs.org/sdr/CALA9700679), Apr 15, 1997: SUPPORT. CORRODED. INSPECTION FOUND CABIN FLOOR SUPPORT CORRODED AT STA 986 TO 1016, RBL 4 TO RBL 20. A FLOOR SUPPORT ANGLE WAS FABRICATED AND INSTALLED IAW SRM 53-10-2, FIGURE 7 - [SDR CALA9700676](https://openairdocs.org/sdr/CALA9700676), Apr 15, 1997: DOUBLER. CORRODED. INSPECTION FOUND DOUBLER CORRODED AT FS 837, STRINGER 24L. THE DOUBLER WAS REMOVED AND A REPLACEMENT DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-2, 51-30 - [SDR CALA9700701](https://openairdocs.org/sdr/CALA9700701), Apr 14, 1997: SUPPORT. CORRODED. INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 277 TO 294, LBL 50. THE SUPPORT WAS REMOVED, A REPLACEMENT SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 53-10-9 A - [SDR CALA9700689](https://openairdocs.org/sdr/CALA9700689), Apr 14, 1997: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM CORRODED AT STA 1016. THE CORRODED AREA WAS REMOVED, A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-30-2 AND 51-30-1. - [SDR CALA9700680](https://openairdocs.org/sdr/CALA9700680), Apr 14, 1997: ANGLE. CORRODED. INSPECTION FOUND SUPPORT ANGLE CORRODED AT STA 270 TO 360, RBL 52. THE CORRODED AREA WAS REMOVED, A SUPPORT ANGLE WAS FABRICATED AND INSTALLED IAW SRM 53-10-2, - [SDR CALA9700677](https://openairdocs.org/sdr/CALA9700677), Apr 14, 1997: FRAME. CORRODED. INSPECTION FOUND FRAME CORRODED AT FS 480, STRINGER 25L TO 22L. THE CORRODED SECTION OF FRAME WAS REMOVED, A NEW SECTION WAS FABRICATED AND INSTALLED IAW SRM 51 - [SDR CALA9700688](https://openairdocs.org/sdr/CALA9700688), Apr 13, 1997: CHANNEL. CORRODED. INSPECTION FOUND AFT CABIN CLOSET TO FLOOR ATTACH CHANNEL CORRODED AT STA 1016 TO AFT PRESSURE BULKHEAD, RBL 2. THE CORRODED AREA WAS REMOVED, A REPAIR WAS FABR - [SDR CALA9700678](https://openairdocs.org/sdr/CALA9700678), Apr 13, 1997: FLOOR. CORRODED. INSPECTION FOUND AFT LAV FLOOR WEB CORRODED AT STA 994 TO 1016, LBL 37 TO LBL 46. THE CORRODED AREA WAS REMOVED, A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 5 - [SDR CALA9700703](https://openairdocs.org/sdr/CALA9700703), Apr 12, 1997: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM CORRODED AT STA 986.5, LBL 24 TO RBL 24. THE FLOORBEAM WAS REPAIRED IAW SRM 53-10-9. - [SDR CALA9700699](https://openairdocs.org/sdr/CALA9700699), Apr 12, 1997: FRAME. CRACKED. INSPECTION FOUND A 2 INCH CRACK IN FORWARD FRAME OF R-1 DOOR AT STA 294, STRINGER 17R. THE CRACKED AREA WAS CUT OUT, A REPAIR WAS INSTALLED IAW SRM 51-40-3, 51- - [SDR CALA9700687](https://openairdocs.org/sdr/CALA9700687), Apr 10, 1997: ANGLE. CORRODED. INSPECTION FOUND SUPPORT ANGLES ATTACHED TO FLOORBEAM AT STA 994, LBL 17 TO LBL 44 AND RBL 17 TO RBL 44 CORRODED. THE SUPPORT ANGLES WERE REMOVED AND REPLACED I - [SDR CALA9700686](https://openairdocs.org/sdr/CALA9700686), Apr 10, 1997: ANGLE. CORRODED. INSPECTION FOUND TIE ANGLE CORRODED AT STA 360, STRINGER 28R. THE TIE ANGLE WAS REMOVED AND A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 53-10-2, 51-10-6, A - [SDR CALA9700685](https://openairdocs.org/sdr/CALA9700685), Apr 9, 1997: INTERCOSTAL. CRACKED. INSPECTION FOUND A 2 INCH CRACK IN INTERCOSTAL IN FORWARD CARGO PIT AT STA 500A TO 500B, STRINGER 26R. THE CRACK WAS STOP DRILLED, A DOUBLER WAS FABRICATED AND - [SDR CALA9700695](https://openairdocs.org/sdr/CALA9700695), Apr 7, 1997: ANGLE. CORRODED. INSPECTION FOUND L-ANGLE CORRODED AT STA 267 TO 277, LBL 12 TO RBL 12. A REPLACEMENT ANGLE WAS FABRICATED AND INSTALLED IAW SRM 53-10-2 AND 51-30-2. - [SDR CALA9700683](https://openairdocs.org/sdr/CALA9700683), Apr 7, 1997: FLOORBEAM. CRACKED. INSPECTION FOUND A 1.5 INCH CRACK IN FLOORBEAM CHANNEL AT STA 807. THE CRACKED AREA WAS REMOVED, A NEW PART WAS FABRICATED AND INSTALLED IAW SRM 51-10-2, 53-10- - [SDR CALA9700684](https://openairdocs.org/sdr/CALA9700684), Apr 6, 1997: SUPPORT. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN SUPPORT AT FS 770 LT. THE CRACKED AREA WAS REMOVED AND A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-2, FIGURE 7. - [SDR CALA9700696](https://openairdocs.org/sdr/CALA9700696), Apr 5, 1997: CHANNEL. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN SUPPORT CHANNEL AT BASE OF VERTICAL FIN. A REPAIR ANGLE WAS FABRICATED AND INSTALLED IAW SRM 53-10-2 AND 51-30-2. - [SDR CALA9700694](https://openairdocs.org/sdr/CALA9700694), Apr 4, 1997: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM UPPER CHORD CORRODED AT STA 312, LBL 20 TO RBL 20. THE CORRODED SECTION OF FLOORBEAM WAS REMOVED, A REPLACEMENT PART WAS FABRICATED A - [SDR CALA9700692](https://openairdocs.org/sdr/CALA9700692), Apr 4, 1997: FRAME. CRACKED. INSPECTION FOUND A .125 INCH CRACK IN FRAME UPPER FLANGE IN FORWARD CARGO PIT AT FS 500A, STRINGER 23L. THE CRACKED AREA WAS REMOVED IAW SRM 53-10-4. FILLER AND - [SDR CALA9700690](https://openairdocs.org/sdr/CALA9700690), Apr 4, 1997: FLOOR. CRACKED. INSPECTION FOUND A 1.5 INCH CRACK IN FLOOR WEB AT STA 986 TO 995, RBL 43. THE CRACKED AREA WAS REMOVED IAW SRM 51-40-2, A REPAIR DOUBLER WAS FABRICATED AND INST - [SDR CALA9700682](https://openairdocs.org/sdr/CALA9700682), Apr 4, 1997: SKIN. CRACKED. INSPECTION FOUND A .5 INCH CRACK AT LOWER FORWARD CORNER OF R-2 DOOR SKIN. THE CRACK WAS STOP DRILLED, A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-10-1 AN - [SDR CALA9700681](https://openairdocs.org/sdr/CALA9700681), Apr 4, 1997: INTERCOSTAL. CORRODED. INSPECTION FOUND FLOOR INTERCOSTAL CORRODED AT STA 1006 TO 1016. THE CORRODED AREA WAS REMOVED, A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-2 AND 51-30- - [SDR CALA9700675](https://openairdocs.org/sdr/CALA9700675), Apr 4, 1997: SKIN. CRACKED. INSPECTION FOUND A 0.4 CRACK IN NR 2 ENGINE FORWARD PYLON FAIRING SKIN. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 54-10-2 AND 51-30-2. - [SDR CALA9700674](https://openairdocs.org/sdr/CALA9700674), Apr 4, 1997: PANEL. CRACKED. INSPECTION FOUND A 1 CRACK IN NR 2 ENGINE TO PYLON UPPER AFT PANEL. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 54-10-2, 51-40-2, AND 51-30-2. - [SDR CALA9700704](https://openairdocs.org/sdr/CALA9700704), Apr 2, 1997: FRAME. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN BELTFRAME AT STA 767, STRINGER 13 AND 14R. THE CRACK WAS STOP DRILLED, A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-4 - [SDR CALA9700700](https://openairdocs.org/sdr/CALA9700700), Apr 2, 1997: FLOORBEAM. CORRODED. INSPECTION FOUND UPPER CAP CORRODED AT STA 344, LBL 40 TO RBL 17. THE FLOORBEAM UPPER CAP WAS REMOVED IAW SRM 53-10-9, FIGURE 5. REPAIR ANGLES, SHIM, AND CHORD - [SDR CALA9700698](https://openairdocs.org/sdr/CALA9700698), Apr 2, 1997: TEE. CRACKED. INSPECTION FOUND A 1.5 INCH CRACK IN FORMED TEE AT BS 342, LBL 12. THE CRACKED TEE WAS REMOVED AND A NEW TEE WAS FABRICATED AND INSTALLED IAW SRM 53-10-2 AND 51 - [SDR CALA9700697](https://openairdocs.org/sdr/CALA9700697), Apr 2, 1997: FLOORBEAM. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN FLOORBEAM SUPPORT TEE AT STA 328, LBL 48. THE TEE WAS REMOVED AND A NEW TEE WAS FABRICATED AND INSTALLED IAW SRM 51-30-2 AND - [SDR CALA9601732](https://openairdocs.org/sdr/CALA9601732), Dec 5, 1996: HYD LINE. RUPTURED. THE A-SYSTEM HYDRAULIC QUANTITY WAS LOST APPROXIMATELY 15 MINUTES INTO FLIGHT. THE LOSS WAS ACCOMPANIED BY ILLUMINATION OF THE NR 1 AND NR 2 PUMP LOW PRESSURE L - [SDR CALA9601513](https://openairdocs.org/sdr/CALA9601513), Oct 26, 1996: OIL PRESS SW. CRACKED. THE NR 2 ENGINE LOW OIL PRESSURE LIGHT ILLUMINATED AND THE ENGINE OIL QUANTITY DROPPED WHILE ON APPROACH. THE 2 ENGINE WAS SHUT DOWN AND THE AIRCRAFT LANDED WIT - [SDR CALA9601037](https://openairdocs.org/sdr/CALA9601037), Jul 11, 1996: FRAME. CRACKED. INSPECTION FOUND A 3.75 INCH CRACK BELOW UPPER STOP FITTING OF FORWARD CARGO DOOR AFT FRAME. THE CRACKED SECTION OF FRAME WAS CUT OUT, A FRAME SPLICE REPAIR WAS - [SDR CALA9600773](https://openairdocs.org/sdr/CALA9600773), Jun 10, 1996: ADC. INOPERATIVE. THE CAPTAIN'S ALTIMETER, COMPASS FLAG IN HSI, OFF FLAG IN ALT SELECT WINDOW, AUTO PILOT, MACH TRIM, GPWS, MODE-C AND CAPTAIN'S DME INSTRUMENTATION ALL WENT INOP - [SDR CALA9600820](https://openairdocs.org/sdr/CALA9600820), Jun 2, 1996: SKIN. CRACKED. INSPECTION FOUND A .75 INCH CRACK IN EXTERNAL SKIN AT FORWARD LOWER CORNER OF L-2 DOOR CUTOUT. THE CRACKED AREA WAS CUT OUT, REPAIR DOUBLERS WERE FABRICATED AND - [SDR CALA9600822](https://openairdocs.org/sdr/CALA9600822), May 31, 1996: DOUBLER. CRACKED. INSPECTION FOUND THREE EACH CRACKS IN T-CHORD AND WEB DOUBLER AT STA 675, RBL 24.8. THE CRACKS WERE .25 INCH OR SMALLER. THE DOUBLER WAS REMOVED AND A NEW DOUBL - [SDR CALA9600821](https://openairdocs.org/sdr/CALA9600821), May 29, 1996: FLOORBEAM. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN FLOORBEAM WEB AT STA 665, BBL 0. THE AREA WAS REPAIRED IAW EA 5710-01322, SRM 51-30-09 AND SRM 51-30-02. - [SDR CAL950292](https://openairdocs.org/sdr/CAL950292), Apr 18, 1995: SKIN. CRACKED. GSO - INSPECTION FOUND A 1 INCH CRACK EXTENDING BEYOND STOP HOLE IN RT WING UPPER SURFACE FIXED LEADING EDGE. THE ADJACENT SKIN AT O/B TRACK FOR NR 5 SLAT WAS W - [SDR CAL950291](https://openairdocs.org/sdr/CAL950291), Apr 16, 1995: SKIN. CRACKED. GSO - INSPECTION FOUND SEVERAL FASTENER HOLES CRACKED IN RT FUSELAGE SKIN AT BS 188 TO 251 BETWEEN WL 207 AND WL 234. THE CRACKS WERE ALL APPROXIMATELY .1 INCH ## 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 FTW92IA184](https://openairdocs.org/ntsb/FTW92IA184), Jul 15, 1992: Boeing 737-222 (N12235), Oklahoma City, OK, incident, no damage. Probable cause: HYDRAULIC FLUID EXHAUSTION DUE TO THE CHAFED 'A' SYSTEM HYDRAULIC LINE AND THE IMPROPER INSTALLATION BY UNKNOWN MAINTENANCE PERSONNEL OF THE 'B' SYSTEM LINE. ## Other aircraft with N12235 - [Cancelled 1968-01-10](https://openairdocs.org/deregistered/N12235-1968-01-10): Pilatus PC-6/A-H2, S/N 556. Owner: [Air America Inc](https://openairdocs.org/faa-owner/AIR%20AMERICA%20INC), [Washington, DC](https://openairdocs.org/faa-place/DC/Washington) - [Cancelled 1948-04-09](https://openairdocs.org/deregistered/N12235-1948-04-09): Kinner SPORTSTER K, S/N 1. Owner: [State Department Of Vocational Education](https://openairdocs.org/faa-owner/STATE%20DEPARTMENT%20OF%20VOCATIONAL%20EDUCATION), [Phoenix, AZ](https://openairdocs.org/faa-place/AZ/Phoenix) --- 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.