# N12349: 1987 Boeing 737-3TO, registration cancelled 2008-12-31 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: December 31, 2008 - Status when cancelled: Valid registration - Airframe: [Boeing 737-3TO](https://openairdocs.org/model/boeing-737-3to) (registry code 138447G) - Engine: [GE CFM56 series](https://openairdocs.org/engine/ge-cfm56-series) (registry code 30016) - Serial number: 23587 - Year built: 1987 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: July 17, 1987 - Certificate issued: October 4, 2006 - Last registry action: December 1, 2008 - Mode S code: A061DD - Owner when cancelled: [Bank Of New York Mellon Trustee](https://openairdocs.org/faa-owner/BANK%20OF%20NEW%20YORK%20MELLON%20%20TRUSTEE) - Location: [Los Angeles, CA](https://openairdocs.org/faa-place/CA/Los%20Angeles) - Owner type: Corporation - Owner's area on the map: 34.0531° N, 118.2645° W: Placed by OpenAirDocs at the center of ZIP code 90017, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N12349 - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=12349 - Page: https://openairdocs.org/deregistered/N12349-2008-12-31 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 737-3TO: https://openairdocs.org/model/boeing-737-3to.md ## Service difficulty reports (46) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR CALA0800636](https://openairdocs.org/sdr/CALA0800636), Jun 25, 2008: CHARGER. FAULTY. ROWS 12 - 20 EMERGENCY SEAT LIGHTS INOPERATIVE. FOUND CHARGER PART NUMBER RPS1-B AT FAULT, LOCATED IN CEILING CENTER AREA BETWEEN AFT GALLEYS. REMOVED AND REPLA - [SDR CALA0600182](https://openairdocs.org/sdr/CALA0600182), May 22, 2006: SKIN. CRACKED. INSPECTION FOUND A 0.58 INCH CRACK IN FORWARD CARGO DOOR INNER SKIN AROUND FORWARD LIGHTENING CUTOUTS SPRING COMPARTMENT. A REPAIR WAS INSTALLED IAW ECRA 5232-0 - [SDR CALA0600181](https://openairdocs.org/sdr/CALA0600181), May 22, 2006: INTERCOSTAL. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN INTERCOSTAL AT STA 294, S12L FORWARD OF L-1 DOOR. A REPAIR WAS INSTALLED IAW ECRA 5310-04535. - [SDR CALA0600180](https://openairdocs.org/sdr/CALA0600180), May 22, 2006: STRINGER SPLICE. CRACKED. INSPECTION FOUND A .75 INCH CRACK IN STRINGER SPLICE CHANNEL AT STA 360, S14L AFT OF L-1 DOOR. A REPAIR WAS INSTALLED IAW ECRA 5310-04535. - [SDR CALA0600179](https://openairdocs.org/sdr/CALA0600179), May 21, 2006: PAN. CRACKED. INSPECTION FOUND A 0.8 INCH CRACK IN C-2 DOOR PAN AT FORWARD MID SECTION. THE DOOR PAN WAS REPAIRED IAW SRM 51-40-02. - [SDR CALA0600176](https://openairdocs.org/sdr/CALA0600176), May 21, 2006: FITTING. CRACKED. INSPECTION FOUND A 5 INCH CRACK IN HORIZONTAL STABILIZER CENTER SECTION -X- BRACE RT FORWARD LOWER CORNER FITTING. THE FITTING WAS REPLACED IAW SRM 51-40-02. - [SDR CALA0600172](https://openairdocs.org/sdr/CALA0600172), May 20, 2006: BELTFRAME. CORRODED. AFT CARGO COMPARTMENT BELT FRAME STA 794, S25R - S22R, LOWER SIDE AT C-2 DOOR CUTOUT, STRAP AND REPAIR DOUBLER HAVE SOME CORROSION BY NUT PLATES. REPAIRED BELT - [SDR CALA0600171](https://openairdocs.org/sdr/CALA0600171), May 20, 2006: PAN. CRACKED. INSPECTION FOUND A .75 INCH CRACK IN C-1 DOOR PAN LOWER FORWARD CORNER NEXT TO UPLATCH HOOK, STA 440-500, S17R TO S27R. THE PAN WAS REMOVED AND A NEW PAN WAS IN - [SDR CALA0600168](https://openairdocs.org/sdr/CALA0600168), May 17, 2006: KEELBEAM. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN LT KEEL BEAM AT STA 540, S29L. THE KEEL BEAM WAS REPAIRED IAW SRM 53-60-12, FIGURE 201, PAGE 205. - [SDR CALA0600165](https://openairdocs.org/sdr/CALA0600165), May 10, 2006: STIFFENER. CORRODED. INSPECTION FOUND RT CHANNEL STIFFENER CORRODED AT LOWER APB STA 1016, RBL 1. THE CORROSION WAS REMOVED AND A DOUBLER WAS INSTALLED IAW BOEING DRAWING 65C28106 A - [SDR CALA0600161](https://openairdocs.org/sdr/CALA0600161), May 9, 2006: BULKHEAD. CORRODED. INSPECTION FOUND FORWARD SIDE OF AFT PRESSURE BULKHEAD CORRODED AT STA 1014 BETWEEN S27R AND S27L. THE AREA WAS REPAIRED IAW SRM 51-40-02. - [SDR CALA0600160](https://openairdocs.org/sdr/CALA0600160), May 9, 2006: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM CORRODED AT STA 967, LBL 4 TO LBL 36. THE CORRODED FLOORBEAM SECTION WAS REMOVED AND REPLACED IAW SRM 53-00-51. - [SDR CALA0600156](https://openairdocs.org/sdr/CALA0600156), May 8, 2006: SEAT TRACK. CORRODED. INSPECTION FOUND THE LEFT I/B SEAT TRACK CORRODED AT STA 907 TO 947.5, LBL 25. THE SEAT TRACK SECTION WAS REMOVED AND REPLACED IAW SRM 51-40-02. - [SDR CALA0600155](https://openairdocs.org/sdr/CALA0600155), May 8, 2006: FRAME. CRACKED. INSPECTION FOUND A .25 INCH CRACK IN LEFT MAIN FRAME BELOW MAIN DECK AT STA 616, LBL 60 TO LBL 61. THE MAIN FRAME WAS REPAIRED IAW ECRA 5311-01158. - [SDR CALA00128](https://openairdocs.org/sdr/CALA00128), Apr 25, 2005: SENSOR. INTERMITTENT. LANDING GEAR UNSAFE LIGHT CAME ON THEN INTERMITTENT AFTER LEVEL AT FL35. REPLACED NLG SENSOR PER AMM 32-61-51. - [SDR CALA0400640](https://openairdocs.org/sdr/CALA0400640), Sep 17, 2004: ACCESS PANEL. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN NR 1 ENGINE PYLON ACCESS PANEL NR 5724 CUTOUT. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS INSTALLED IAW ECRA 5430-01204. - [SDR CALA0400636](https://openairdocs.org/sdr/CALA0400636), Sep 14, 2004: SEAT TRACK. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN LT OB SEAT TRACK, OB FLANGE AT STA 727B. A REPAIR WAS INSTALLED IAW ECRA 5321-01202. - [SDR CALA0400552](https://openairdocs.org/sdr/CALA0400552), Jun 26, 2004: CHARGER. INOPERATIVE. THE EMERGENCY EXIT SIGN AT L-2 DOOR WAS FOUND FLICKERING ON AND OFF. THE BATTERY CHARGER AND BATTERY PACK AT L-2 DOOR WERE REMOVED AND REPLACED IAW MM 33-51-51, - [SDR CALA2000266](https://openairdocs.org/sdr/CALA2000266), May 7, 2002: SPOILER. #3 SPOILER DENTED AND CRACKED .75X.75 INCHES JUST FWD AND OB OF ACTUATOR ATTACH POINT. INSTALLED DOUBLER PER SRM 57-70-01, FIG 204. - [SDR CALA0200242](https://openairdocs.org/sdr/CALA0200242), Apr 25, 2002: WEB. CORRODED. INSPECTION FOUND AFT CARGO DOOR CUTOUT THRESHOLD WEB CORRODED AT STA 793-847. THE WEB WAS REMOVED AND REPLACED IAW SRM 51-10-2. - [SDR CALA0200239](https://openairdocs.org/sdr/CALA0200239), Apr 25, 2002: WEB. CORRODED. INSPECTION FOUND CORROSION UNDER FLANGE OF VERTICAL THRESHOLD WEB AT AFT BAGGAGE BIN DOORWAY FROM STA 767-847. THE WEB WAS REMOVED AND REPLACED IAW SRM 51-10-2. - [SDR CALA0200232](https://openairdocs.org/sdr/CALA0200232), Apr 21, 2002: CHANNEL. CORRODED. INSPECTION FOUND AFT BAGGAGE BIN FLOOR SUPPORT CHANNELS CORRODED AT STA 794, LBL 3 AND RBL 3. CHANNEL BEAM REPAIRS WERE INSTALLED AT EACH LOCATION IAW SRM 53-00 - [SDR CALA0200231](https://openairdocs.org/sdr/CALA0200231), Apr 21, 2002: CHANNEL. CORRODED. INSPECTION FOUND CHANNEL CORRODED IN AFT BAGGAGE BIN AT STA 794, RBL 8. REPAIRED IAW SRM 53-00-53. - [SDR CALA0200230](https://openairdocs.org/sdr/CALA0200230), Apr 21, 2002: CHANNEL. CORRODED. INSPECTION FOUND AFT BAGGAGE BIN FLOOR SUPPORT CHANNEL CORRODED AT STA 727D+5" RBL 3. A REPAIR ANGLE WAS INSTALLED IAW ECRA 5320-01603. - [SDR CALA0200229](https://openairdocs.org/sdr/CALA0200229), Apr 21, 2002: CHANNEL. CORRODED. INSPECTION FOUND AFT BAGGAGE BIN FLOOR SUPPORT CHANNELS CORRODED AT STA 727D+5", RBL 8 AND LBL 8. REPAIR ANGLES WERE INSTALLED AT EACH LOCATION IAW ECRA 5320-01 - [SDR CALA0200228](https://openairdocs.org/sdr/CALA0200228), Apr 21, 2002: FLOOR SUPPORT. CORRODED. INSPECTION FOUND AFT BAGGAGE BIN FLOOR SUPPORT CHANNEL CORRODED AT STA 727D+5, LBL 12. A REPAIR ANGLE WAS INSTALLED IAW ECRA 5320-01603. - [SDR CALA0200224](https://openairdocs.org/sdr/CALA0200224), Apr 20, 2002: FLOOR SUPPORT. CORRODED. INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 294-312, RBL 15. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-02. - [SDR CALA0200223](https://openairdocs.org/sdr/CALA0200223), Apr 20, 2002: FLOORBEAM. CORRODED. INSPECTION FOUND CABIN FLOORBEAM UPPER CAP CORRODED AT STA 312. A SPLICE REPAIR WAS INSTALLED IAW SRM 53-10-51. - [SDR CALA0200219](https://openairdocs.org/sdr/CALA0200219), Apr 19, 2002: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM UPPER T CAP CORRODED AT FASTENER HOLES, STA 294.5, LBL 20 TO RBL 58. REPAIRED IAW SRM 53-10-51. - [SDR CALA0200217](https://openairdocs.org/sdr/CALA0200217), Apr 18, 2002: WEB. CRACKED. INSPECTION FOUND A 3" CRACK IN WEB AT R/H SIDEWALL FLOOR BETWEEN STA 559 AND 578. THE WEB WAS REMOVED AND A NEW WEB WAS INSTALLED IAW SRM 51-10-02. - [SDR CALA0200216](https://openairdocs.org/sdr/CALA0200216), Apr 18, 2002: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM T-CAP CORRODED AT FASTENER HOLES, STA 344. REPAIRED IAW SRM 51-10-51. - [SDR CALA0200212](https://openairdocs.org/sdr/CALA0200212), Apr 17, 2002: STRINGER. CRACKED. INSPECTION FOUND A 1/2" CRACK IN STRINGER 16L JUST FORWARD OF WING ILLUMINATION LIGHT HOUSING AT STA 500C. A NEW STRINGER WAS INSTALLED IAW SRM 53-30-03 AND 53- - [SDR CALA0200211](https://openairdocs.org/sdr/CALA0200211), Apr 16, 2002: MOUNT. CORRODED. INSPECTION FOUND AFT O/B LAV MOUNT CORRODED AT STA 1012, LBL 38. THE LAV MOUNT WAS REMOVED AND REPLACED IAW SRM 51-40-02. - [SDR CALA0200210](https://openairdocs.org/sdr/CALA0200210), Apr 16, 2002: CHANNEL. CORRODED. INSPECTION FOUND AFT O/B CHANNEL OF WEB CORRODED AT STA 986.5-1006, LBL 38. THE CHANNEL WAS REMOVED AND REPLACED IAW SRM 51-40-02. - [SDR CALA0200206](https://openairdocs.org/sdr/CALA0200206), Apr 15, 2002: STRINGER. CORRODED. INSPECTION FOUND STRINGER 26R CORRODED BETWEEN STA 1006 AND 1016. THE STRINGER WAS REMOVED AND REPLACED IAW SRM 51-10-02. - [SDR CALA0001321](https://openairdocs.org/sdr/CALA0001321), Aug 25, 2000: SKIN. CRACKED. INSPECTION FOUND A 0.4 INCH CRACK IN ABB DOOR INTERIOR SKIN AT LIGHTENING HOLE EDGE. THE EXISTING REPAIR DOUBLERS WERE REMOVED AND A NEW SINGLE DOUBLER REPAIR W - [SDR CALA0001320](https://openairdocs.org/sdr/CALA0001320), Aug 25, 2000: SKIN. GOUGED. INSPECTION FOUND AFT BAGGAGE BIN DOOR EXTERIOR SKIN GOUGED. THE SKIN WAS REMOVED AND NEW SKIN WAS INSTALLED IAW SRM 51-40-02. - [SDR CALA9801163](https://openairdocs.org/sdr/CALA9801163), Jun 24, 1998: CHANNEL. CORRODED. INSPECTION FOUND R-1 DOOR Z-CHANNEL CORRODED AT STA 294-328. THE Z-CHANNEL WAS REMOVED AND REPLACED IAW SRM 51-10-02. - [SDR CALA9801161](https://openairdocs.org/sdr/CALA9801161), Jun 24, 1998: PANEL. CORRODED. INSPECTION FOUND RT TRANSITION PANEL CORRODED AT STA 847-867. THE TRANSITION PANEL WAS REMOVED AND REPLACED IAW SRM 51-10-2. - [SDR CALA9801158](https://openairdocs.org/sdr/CALA9801158), Jun 23, 1998: SEAT TRACK. CORRODED. INSPECTION FOUND SEAT TRACK CORRODED AT FS 328-344. THE CORRODED SEAT TRACK SECTION WAS REMOVED AND REPLACED IAW SRM 53-00-52. - [SDR CALA9801147](https://openairdocs.org/sdr/CALA9801147), Jun 21, 1998: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM CAP IN FORWARD GALLEY AREA CORRODED AT FS 294.5, RBL 8. THE FLOORBEAM CAP WAS REPAIRED IAW SRM 53-10-51. - [SDR CALA9801146](https://openairdocs.org/sdr/CALA9801146), Jun 20, 1998: FLOOR TRACK. CORRODED. INSPECTION FOUND FORWARD GALLEY FLOOR TRACK CORRODED AT STA 294.5. THE FLOOR TRACK WAS REMOVED AND A NEW ONE WAS FABRICATED AND INSTALLED IAW SRM 53-00-52. - [SDR CALA9701804](https://openairdocs.org/sdr/CALA9701804), Dec 30, 1997: CORRODED. CORRODED. INSPECTION FOUND CORROSION ON FLOORBEAM/TRACK TIEDOWN IN AFT PIT AT STA 947, LBBL 17.2. A NEW TRACK TIEDOWN WAS SPLICED IN IAW SRM 53-00-53, FIGURE 202. - [SDR CALA9600794](https://openairdocs.org/sdr/CALA9600794), Jun 8, 1996: LIGHT. INOPERATIVE. THE L-2 DOOR EMERGENCY SLIDE EXIT LIGHT WAS FOUND INOPERATIVE. THE EXIT LIGHT WAS REMOVED AND REPLACED. - [SDR CAL960385](https://openairdocs.org/sdr/CAL960385), Mar 23, 1996: NOSE LINK. BROKEN. EWR - FLT 0725 - THE NR 2 LEADING EDGE FLAP TRANSIT LIGHT ON OVERHEAD PANEL AND FORWARD PANEL LEADING EDGE FLAP TRANSIT LIGHT ILLUMINATED WITH THE FLAPS RETRACT - [SDR CAL950948](https://openairdocs.org/sdr/CAL950948), Oct 23, 1995: O-RINGS. CUT. GSO - FLT 0171 - THE NR 2 ENGINE LOW OIL PRESSURE LIGHT ILLUMINATED WHILE ON FINAL APPROACH TO GSO. THE NR 2 ENGINE WAS SHUT DOWN AS A PRECAUTIONARY MEASURE. TH ## Other aircraft with N12349 - [Cancelled 2025-04-18](https://openairdocs.org/deregistered/N12349-2025-04-18): Gordon Miller SUPER BEE, S/N 001. Owner: [Miller Gordon N](https://openairdocs.org/faa-owner/MILLER%20GORDON%20N), [Greenville, OH](https://openairdocs.org/faa-place/OH/Greenville) --- 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.