# N12230: Boeing 737-217, registration cancelled 1999-07-22 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: July 22, 1999 - Status when cancelled: Valid registration - Airframe: [Boeing 737-217](https://openairdocs.org/model/boeing-737-217) (registry code 1384464) - Data sheets: [TCDS A16WE](https://openairdocs.org/tcds/A16WE) (OpenAirDocs) - Serial number: 19884 - Type of aircraft: Fixed wing multi engine - Certificate issued: November 10, 1998 - Last registry action: December 30, 1998 - Mode S code: A05DFA - 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/N12230 - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=12230 - Page: https://openairdocs.org/deregistered/N12230-1999-07-22 From the FAA registry file of October 31, 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 737-217: https://openairdocs.org/model/boeing-737-217.md ## Service difficulty reports (53, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR CALA9801229](https://openairdocs.org/sdr/CALA9801229), Jul 8, 1998: ANGLE. CRACKED. INSPECTION FOUND A 5 INCH CRACK IN FLOOR SUPPORT ANGLE AT STA 648-767, RBL 45. THE CRACKED AREA WAS CUT OUT. A REPAIR ANGLE WAS FABRICATED AND INSTALLED IAW SRM - [SDR CALA9800854](https://openairdocs.org/sdr/CALA9800854), May 13, 1998: WIRE. BROKEN. ESCAPE PATH LIGHT INOP AT ROW 24. BROKEN WIRE AND MISSING LENS. REPAIRED LIGHT SOCKET WIRE AND REPLACED LENS SET PER MM 33-51-5. - [SDR CALA9601704](https://openairdocs.org/sdr/CALA9601704), Nov 23, 1996: FUEL PUMP. INOPERATIVE. THE NR 2 ENGINE FLAMED OUT DURING CLIMB AT 900 FEET AGL. THE AIRCRAFT WAS RETURNED TO CHS WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 2 ENGINE FU - [SDR CALA9601382](https://openairdocs.org/sdr/CALA9601382), Oct 5, 1996: HYD LINE. CRACKED. THE A-HYDRAULIC SYSTEM QUANTITY WAS LOST WHILE ON APPROACH. THE A-SYSTEM HYDRAULIC QUANTITY LOSS CHECKLIST WAS COMPLIED WITH AND THE AIRCRAFT LANDED WITHOUT INC - [SDR CALA9601320](https://openairdocs.org/sdr/CALA9601320), Sep 21, 1996: HYD LINE. CRACKED. THE AIRCRAFT LOST A-SYSTEM HYDRAULIC PRESSURE AND QUANTITY UPON LANDING. THE AIRCRAFT STOPPED SAFELY AND WAS TOWED TO THE GATE. MAINTENANCE FOUND HYDRAULIC LINE - [SDR CALA9600806](https://openairdocs.org/sdr/CALA9600806), Jun 12, 1996: FIRE LOOP. BURNED. THE APU FIRE WARNING LIGHT BEGAN TO FLASH INTERMITTENTLY APPROXIMATELY FIVE MINUTES INTO THE FLIGHT WITH THE APU SHUT DOWN. THE APU FIRE HANDLE WAS PULLED AND T - [SDR CALA9600689](https://openairdocs.org/sdr/CALA9600689), May 15, 1996: FRAME. CRACKED. INSPECTION FOUND A 1 INCH AND 1.5 INCH CRACK IN FRAME AT STA 480 BETWEEN STRINGER 22L AND 23L. THE CRACKED FRAME SECTION WAS REMOVED, A NEW FRAME SECTION WAS FA - [SDR CALA9600721](https://openairdocs.org/sdr/CALA9600721), May 7, 1996: FRAME. CRACKED. INSPECTION FOUND TWO, .5 INCH CRACKS IN FRAME AT BS 328 BETWEEN STRINGER 2OR AND 21R. THE CRACKED AREAS WERE REMOVED, FILLER AND REPAIR PLATES WERE FABRICATED A - [SDR CALA9600720](https://openairdocs.org/sdr/CALA9600720), May 7, 1996: FRAME. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN FRAME AT STA 328, STRINGER 26L. THE CRACKED AREA WAS REMOVED AND A DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-40- - [SDR CALA9600719](https://openairdocs.org/sdr/CALA9600719), May 7, 1996: FRAME. CRACKED. INSPECTION FOUND TWO 1 INCH CRACKS AT NUTPLATE HOLES OF FRAME AT BS 440, LT SIDE. THE FRAME WAS REMOVED AND REPLACED IAW BOEING DRAWING 65C25113. - [SDR CALA9600718](https://openairdocs.org/sdr/CALA9600718), May 7, 1996: FRAME. CRACKED. INSPECTION FOUND A 2 INCH CRACK AT NUTPLATE HOLE OF FRAME, BS 420, STRINGER 22L. THE FRAME SEGMENT WAS REMOVED AND REPLACED IAW BOEING DRAWING 65C25113. - [SDR CALA9600706](https://openairdocs.org/sdr/CALA9600706), May 7, 1996: FRAME. CRACKED. INSPECTION FOUND A 1.5 CRACK AT NUTPLATE HOLE OF FRAME, BS 500A, RT SIDE. THE FRAME SEGMENT WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW BOEING DRAWING 65C25 - [SDR CALA9600704](https://openairdocs.org/sdr/CALA9600704), May 7, 1996: FLOORBEAM. CRACKED. INSPECTION FOUND A .75 CRACK IN FLOORBEAM AT STA 676, RBL 24. THE BEAM WAS REPAIRED IAW EA 5710-01638. - [SDR CALA9600700](https://openairdocs.org/sdr/CALA9600700), May 7, 1996: FRAME. CRACKED. INSPECTION FOUND A 1 INCH CRACK AT TWO NUTPLATE LOCATIONS ON FRAME AT BS 500, RT SIDE. THE CRACKED FRAME SEGMENT WAS REMOVED AND REPLACED IAW BOEING DRAWING 65C - [SDR CALA9600698](https://openairdocs.org/sdr/CALA9600698), May 7, 1996: SPLICE. CRACKED. INSPECTION FOUND A 1.5 INCH CRACK IN STRINGER SPLICE AT STA 360, STRINGER 21R. THE SPLICE WAS REMOVED AND A NEW SPLICE WAS FABRICATED AND INSTALLED IAW SRM 53-1 - [SDR CALA9600695](https://openairdocs.org/sdr/CALA9600695), May 7, 1996: SKIN. CRACKED. INSPECTION FOUND SEVERAL CRACKS IN SECTION 41 FUSELAGE SKIN ON LT SIDE, BS 188 TO 251, WL 207 TO 234. THE CRACKS RANGED FROM .125 INCH TO .25 INCH IN LENGTH. TH - [SDR CALA9600694](https://openairdocs.org/sdr/CALA9600694), May 7, 1996: STRINGER. CRACKED. INSPECTION FOUND A .5 INCH CRACK AND CORROSION AT FASTENER HOLE OF STRINGER 26L, BS 323. THE CRACKED STRINGER WAS REMOVED AND A NEW PART WAS INSTALLED IAW SRM 5 - [SDR CALA9600688](https://openairdocs.org/sdr/CALA9600688), May 7, 1996: STRINGER. CORRODED. INSPECTION FOUND STRINGER 22L CORRODED AT STA 727. THE CORRODED SECTION OF STRINGER WAS REMOVED. A NEW STRINGER AND SPLICE ANGLES WERE FABRICATED AND INSTALLED - [SDR CALA9600693](https://openairdocs.org/sdr/CALA9600693), May 6, 1996: ANGLE. CORRODED. INSPECTION FOUND FRAME UPPER L-ANGLE AND WEB CORRODED AT BS 259, RT SIDE. THE L-ANGLE AND WEB WERE REMOVED AND REPLACED IAW SRM 51-40-2, 51-40-4, 51-30-2, 51-10 - [SDR CALA9600723](https://openairdocs.org/sdr/CALA9600723), May 5, 1996: FRAME. CRACKED. INSPECTION FOUND TWO, .75 INCH CRACKS IN FRAME AT BS 500B BETWEEN STRINGERS 22R AND 24R. THE FRAME WAS REMOVED AND A NEW FRAME WAS INSTALLED IAW BOEING DRAWING - [SDR CALA9600715](https://openairdocs.org/sdr/CALA9600715), May 5, 1996: SKIN. DELAMINATED. INSPECTION FOUND THE LT WING AILERON TAB SKIN DELAMINATING. THE DELAMINATED AREA WAS REMOVED AND A FIBERGLASS OVERLAY REPAIR WAS INSTALLED IAW SRM 51-40-9. - [SDR CALA9600714](https://openairdocs.org/sdr/CALA9600714), May 5, 1996: SKIN. DAMAGED. INSPECTION FOUND IMPACT DAMAGE TO FORWARD CARGO DOOR OUTER SKIN. THE DAMAGED AREA WAS REMOVED AND A FILLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW S - [SDR CALA9600717](https://openairdocs.org/sdr/CALA9600717), May 4, 1996: STRINGER. CORRODED. INSPECTION FOUND CHORD CORRODED AT STA 294 TO 335, STRINGER 26R. THE CHORD SECTION WAS REMOVED AND REPLACED IAW SRM 51-10-1 AND 51-30-0. - [SDR CALA9600705](https://openairdocs.org/sdr/CALA9600705), May 2, 1996: FLOORBEAM. CRACKED. INSPECTION FOUND A 1 INCH CRACK EXTENDING FROM RIVET OF FLOORBEAM AT STA 707, BBL 0. A REPAIR WAS INSTALLED IAW EA 5710-01322. - [SDR CALA9600709](https://openairdocs.org/sdr/CALA9600709), Apr 29, 1996: SKIN. DENTED. INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 887, STRINGER 25R. THE DENTED AREA OF SKIN WAS CUT OUT, A SKIN SECTION AND SPLICE DOUBLER WERE FABRICATED AND INSTA - [SDR CALA9600708](https://openairdocs.org/sdr/CALA9600708), Apr 29, 1996: SKIN. PUNCTURED. INSPECTION FOUND A HOLE IN FUSELAGE SKIN AFT OF AFT CARGO DOOR. A FILLER AND DOUBLER SMALL FLUSH REPAIR WAS INSTALLED IAW SRM 53-30-3. - [SDR CALA9600707](https://openairdocs.org/sdr/CALA9600707), Apr 29, 1996: SKIN. DENTED. INSPECTION FOUND A DENT IN RT WING LEADING EDGE SKIN JUST OUTBOARD OF LANDING LIGHT. THE DENTED AREA WAS CUT OUT. A FILLER AND DOUBLER REPAIR WAS FABRICATED AND - [SDR CALA9600701](https://openairdocs.org/sdr/CALA9600701), Apr 29, 1996: FRAME. CRACKED. INSPECTION FOUND A .75 CRACK IN FRAME AT RT SIDE OF E AND E DOOR CUTOUT. THE CRACK WAS STOP DRILLED. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-10-2 AND - [SDR CALA9600697](https://openairdocs.org/sdr/CALA9600697), Apr 29, 1996: BEAM. CRACKED. INSPECTION FOUND VERTICAL BEAM CRACKED IN HALF AT BS 540, RBL 24.8. THE BEAM WAS REMOVED AND A NEW BEAM WAS FABRICATED AND INSTALLED IAW SRM 51-30-2 AND 57-10-2 - [SDR CALA9600722](https://openairdocs.org/sdr/CALA9600722), Apr 26, 1996: BULKHEAD WEB. CRACKED. INSPECTION FOUND A 7 INCH CRACK IN BULKHEAD PRESSURE WEB AT STA 664, RBL 30. THE WEB WAS REMOVED AND REPLACED IAW SRM 51-30-2. - [SDR CALA9600713](https://openairdocs.org/sdr/CALA9600713), Apr 26, 1996: STRINGER. CORRODED. INSPECTION FOUND STRINGER 23R CORRODED AT STA 355. THE STRINGER WAS REMOVED AND A NEW STRINGER WAS INSTALLED IAW SRM 53-10-3. - [SDR CALA9600712](https://openairdocs.org/sdr/CALA9600712), Apr 26, 1996: FRAME. CRACKED. INSPECTION FOUND A 1.5 INCH CRACK AT FASTENER HOLE OF FRAME AT STA 400 LOWER LOBE. THE CRACKED AREA WAS REMOVED, A FILLER AND DOUBLER REPAIR WAS FABRICATED AND - [SDR CALA9600711](https://openairdocs.org/sdr/CALA9600711), Apr 26, 1996: STRINGER. CORRODED. INSPECTION FOUND STRINGER 26R CORRODED AT STA 360 TO 420. THE STRINGER WAS REMOVED AND A NEW STRINGER WAS FABRICATED AND INSTALLED IAW SRM 53-10-2 AND 51-30-5. - [SDR CALA9600710](https://openairdocs.org/sdr/CALA9600710), Apr 26, 1996: STRINGER. CORRODED. INSPECTION FOUND STRINGER 20R CORRODED AT STA 383. THE STRINGER WAS REMOVED AND A NEW STRINGER WAS FABRICATED AND INSTALLED IAW SRM 51-30-2 AND 51-10-2. - [SDR CALA9600702](https://openairdocs.org/sdr/CALA9600702), Apr 26, 1996: SKIN. CRACKED. INSPECTION FOUND A 1.33 CRACK AT FASTENER HOLE IN AFT CARGO DOOR FRAME AFT SKIN. THE CRACKED AREA WAS CUT OUT, A FILLER AND DOUBLER REPAIR WAS FABRICATED AND IN - [SDR CALA9600699](https://openairdocs.org/sdr/CALA9600699), Apr 26, 1996: FRAME. CRACKED. INSPECTION FOUND A 3 INCH CRACK AT NUTPLATE HOLE OF FRAME AT BS 500, LT SIDE. THE CRACKED FRAME SECTION WAS REMOVED AND A NEW FRAME SEGMENT WAS SPLICED IN IAW B - [SDR CALA9600696](https://openairdocs.org/sdr/CALA9600696), Apr 24, 1996: INTERCOSTAL. CRACKED. INSPECTION FOUND A 2 INCH CRACK IN INTERCOSTAL BETWEEN STA 500 AND 500A, STRINGER 26L. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW BOEING DRAWING 69-41473. - [SDR CALA9600691](https://openairdocs.org/sdr/CALA9600691), Apr 24, 1996: SKIN. DENTED. INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 500A BELOW WINDOW BELT ON BOTH LEFT AND RIGHT HAND SIDE OF FUSELAGE. BOTH AREAS WERE REPAIRED IAW SRM 53-30-3. - [SDR CALA9600690](https://openairdocs.org/sdr/CALA9600690), Apr 23, 1996: SKIN. CORRODED. INSPECTION FOUND FUSELAGE SKIN AND FRAME SHEAR TIES CORRODED AT STA 328, STRINGER 18R. THE CORRODED AREAS OF SKIN AND SHEAR TIES WERE CUT OUT. FILLER AND DOUBLE - [SDR CALA9600716](https://openairdocs.org/sdr/CALA9600716), Apr 22, 1996: SKIN. DENTED. INSPECTION FOUND RT FUSELAGE SKIN DENTED AT STA 1040. THE DENTED AREA WAS CUT OUT, A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-30-3, FIGURE 1. - [SDR CALA9600703](https://openairdocs.org/sdr/CALA9600703), Apr 22, 1996: SKIN. DENTED. INSPECTION FOUND A DENT IN RT FUSELAGE AT STA 1040. THE DENTED AREA WAS CUT OUT. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-30-3, FIGURE 1. - [SDR CALA9600692](https://openairdocs.org/sdr/CALA9600692), Apr 22, 1996: SKIN. CRACKED. INSPECTION FOUND A 1.5 INCH CRACK AT FASTENER HOLE OF L-1 DOOR LOWER SKIN. THE CRACKED SKIN WAS REMOVED, A FILLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLE - [SDR CALA9600687](https://openairdocs.org/sdr/CALA9600687), Apr 18, 1996: SKIN. DENTED. INSPECTION FOUND SKIN DENTED FROM STA 360 TO 447 RT SIDE, STRINGER 19R TO 25R. THE SKIN WAS REMOVED AND REPLACED IAW SRM 51-30-2. - [SDR CALA9600686](https://openairdocs.org/sdr/CALA9600686), Apr 18, 1996: SKIN. DENTED. INSPECTION FOUND FUSELAGE SKIN DENTED FROM STA 259 TO 360, STRINGER 19R TO 24R. THE SKIN WAS REMOVED AND REPLACED IAW SRM 51-30-2. - [SDR CAL960453](https://openairdocs.org/sdr/CAL960453), Apr 10, 1996: CONNECTOR. SHORTED. CAE - FLT 1598 - THE NR 1 ENGINE FIRE LIGHT FLICKERED OFF AND ON AND THEN THE FIRE LIGHT AND BELL CAME ON STEADY WHILE EN ROUTE FROM TPA TO GSO. THE NR 1 ENGINE - [SDR CAL960309](https://openairdocs.org/sdr/CAL960309), Mar 13, 1996: WIRE. SHORTED. FLT NR 1087 - EWR - THE CREW NOTICED APPROXIMATELY ONE THIRD OF THE EMERGENCY PATH LIGHTING SYSTEM WAS INOPERATIVE AFTER LOSING GROUND POWER. MAINTENANCE FOUND - [SDR CAL960280](https://openairdocs.org/sdr/CAL960280), Mar 5, 1996: HYD LINE. LEAKING. FLT NR 512 - EWR - THE 'B' HYD SYSTEM WAS LOST AFTER TAKEOFF FROM EWR. THE LOSS WAS ACCOMPANIED BY ILLUMINATION OF SYSTEM 'B' LOW PRESSURE LIGHTS. THE 'B' SYSTE - [SDR CAL950944](https://openairdocs.org/sdr/CAL950944), Oct 21, 1995: OVERHEAT LIGHT. ILLUMINATED. FLT NR 1444 - EWR - AIRCRAFT INBOUND, NR 1 ENGINE OVERHEAT LIGHT ILLUMINATES WITH THROTTLE ADVANCE. RETURNED TO BASE. MAINTENANCE REPLACED CONNECTOR AND ELEMENT - [SDR CAL950765](https://openairdocs.org/sdr/CAL950765), Aug 28, 1995: PROX SENSOR. INOPERATIVE. FLT NR 1580 - GSO - THE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF FROM GSO. THE AIRCRAFT WAS RETURNED TO GSO WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FO - [SDR CAL950749](https://openairdocs.org/sdr/CAL950749), Aug 18, 1995: STRINGER. CORRODED. MIA - INSPECTION FOUND CORROSION ON STRINGER 27L FROM STATION 947.5 TO 967. A STRINGER SPLICE REPAIR WAS INSTALLED IAW SRM 53-10-3. (M) All 53: https://openairdocs.org/deregistered/N12230-1999-07-22/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 19940210029569I](https://openairdocs.org/incident/19940210029569I), Feb 10, 1994: Boeing 737217 (N12230), Lorian, OH. Narrative: on 2-10-94 at 1958 LCL EST., a Boeing 737-200 aircraft N12230, owned /operated by Continental airlines inc., houston, TX and piloted by russell a.… ## Other aircraft with N12230 - [Cancelled 1932-02-11](https://openairdocs.org/deregistered/N12230-1932-02-11): Lockheed ALTAIR, S/N 188. Exported to Japan. Owner: [Lockheed Aircraft Co](https://openairdocs.org/faa-owner/LOCKHEED%20AIRCRAFT%20CO), [Burbank, CA](https://openairdocs.org/faa-place/CA/Burbank) --- 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.