# N70330: 1986 Boeing 737-3TO, registration cancelled 2013-03-21 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: March 21, 2013 - Status when cancelled: Valid registration - Airframe: [Boeing 737-3TO](https://openairdocs.org/model/boeing-737-3to) (registry code 138447G) - Engine: [CFM International CFM56 series](https://openairdocs.org/engine/cfm-international-cfm56-series) (registry code 13802) - Serial number: 23460 - Year built: 1986 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: July 25, 1986 - Certificate issued: August 28, 2008 - Last registry action: January 30, 2012 - Mode S code: A9628D - Owner when cancelled: [Continental Airlines Inc](https://openairdocs.org/faa-owner/CONTINENTAL%20AIRLINES%20INC) - Location: [Houston, TX](https://openairdocs.org/faa-place/TX/Houston) - Owner type: Corporation - Owner's area on the map: 29.7568° N, 95.3657° W: Placed by OpenAirDocs at the center of ZIP code 77002, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N70330 - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=70330 - Page: https://openairdocs.org/deregistered/N70330-2013-03-21 From the FAA registry file of November 4, 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 (59, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR CALA0800268](https://openairdocs.org/sdr/CALA0800268), Mar 27, 2008: CHANNEL. CORRODED. FOUND CORROSION ON Z-CHANNEL UNDER L2 DOOR SILL PLATE. REMOVED AND REPLACED Z-ANGLE PER SRM 51-40-02. - [SDR CALA0700543](https://openairdocs.org/sdr/CALA0700543), Sep 27, 2007: SKIN. CRACKED. INSPECTION FOUND A .75 INCH CRACK IN RIGHT WING LEADING EDGE SKIN AT NR 5 SLAT ACTUATOR. THE SKIN WAS REPAIRED IAW SRM 57-41-01, PAGE 202, FIGURE 201. - [SDR CALA0700536](https://openairdocs.org/sdr/CALA0700536), Sep 24, 2007: BRACKET. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN FORWARD BAGGAGE BIN STA 500A VHF ANTENNA MOUNTING BRACKET. A NEW ANTENNA MOUNTING BRACKET WAS INSTALLED IAW SRM 51-40-02. - [SDR CALA0700535](https://openairdocs.org/sdr/CALA0700535), Sep 24, 2007: STRINGER CLIP. CORRODED. INSPECTION FOUND STRINGER TIE IN FORWARD BAGGAGE BIN CORRODED AT STA 540, S26L. THE STRINGER TIE WAS REPAIRED IAW SRM 51-40-02 AND GMM 10-900-01. - [SDR CALA0700534](https://openairdocs.org/sdr/CALA0700534), Sep 24, 2007: STRINGER. CORRODED. INSPECTION FOUND STRINGER 26L CORRODED AT STA 540. A REPAIR WAS INSTALLED IAW SRM 53-00-03. - [SDR CALA0700533](https://openairdocs.org/sdr/CALA0700533), Sep 23, 2007: DOOR FRAME. CRACKED. INSPECTION FOUND A .5 INCH CRACK AT LOWER STOP PAD HOLES OF FORWARD BAG BIN DOOR CUTOUT AFT FRAME. THE FRAME WAS REMOVED AND REPLACED IAW SRM 51-40-02 AND BOEIN - [SDR CALA0700530](https://openairdocs.org/sdr/CALA0700530), Sep 23, 2007: FRAME. CRACKED. INSPECTION FOUND A .25 INCH CRACK IN FORWARD BAGGAGE BIN FRAME WEB AT STA 500, BL 0. THE CRACKED AREA WAS REMOVED AND A REPAIR DOUBLER AND FILLER WERE INSTALLED - [SDR CALA0700529](https://openairdocs.org/sdr/CALA0700529), Sep 22, 2007: SKIN. CRACKED. INSPECTION FOUND A 1.5 INCH CRACK IN RIGHT FUSELAGE SKIN LAP AT STA 880, S25R. THE SKIN WAS REPAIRED IAW SRM 53-00-01, REPAIR 31. - [SDR CALA0700527](https://openairdocs.org/sdr/CALA0700527), Sep 21, 2007: SKIN. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN LEFT FUSELAGE SKIN AT STA 727E, S22L. THE SKIN WAS REPAIRED IAW SRM 53-00-01, FIGURE 201. - [SDR CALA0600384](https://openairdocs.org/sdr/CALA0600384), Oct 10, 2006: SKIN. CRACKED. FUSELAGE CRACK R/S AFT OF WING, 12 INCHES AFT OF EMERGENCY LIGHT. REPAIRED IAW SRM 53-00-01, REPAIR 31, FIG 201. - [SDR CALA0600377](https://openairdocs.org/sdr/CALA0600377), Oct 8, 2006: SKIN. CRACKED. FUSELAGE CRACK RT SIDE AFT OF WING, 12 INCHES AFT OF EMERGENCY LIGHT. REPAIRED IAW SRM 53-00-01, REPAIR 31, FIG 201. - [SDR CALA0600208](https://openairdocs.org/sdr/CALA0600208), Jun 12, 2006: BATTERY PACK. DISCHARGED. THE EMERGENCY EXIT LIGHTS AT AFT DOORS WERE FOUND INOPERATIVE. THE BATTERY PACK WAS REPLACED. - [SDR CALA0600007](https://openairdocs.org/sdr/CALA0600007), Jan 13, 2006: STIFFENER. CRACKED. INSPECTION FOUND A TWO INCH CRACK IN WING CENTER SECTION VERTICAL STIFFENER AT STA 663.75, RBL 6.15. THE STIFFENER WAS REPAIRED IAW EA 5714-01002. A DIP WAS ISS - [SDR CALA0600033](https://openairdocs.org/sdr/CALA0600033), May 8, 2005: SKIN. CRACKED. MAINTENANCE FOUND A CRACK AT LIGHTENING HOLE IN THE LOWER INNER SKIN OF THE FORWARD CARGO DOOR WHILE THE DOOR WAS IN SHOP FOR MAINTENANCE. THE DOOR HAD BEEN REM - [SDR CALA0500135](https://openairdocs.org/sdr/CALA0500135), Apr 28, 2005: FRAME. CRACKED. MAIN CABIN STA 616L FRAME INNER CHORD CRACKED. INSTALLED FRAME PER ECRA 5311-01158. - [SDR CALA0500127](https://openairdocs.org/sdr/CALA0500127), Apr 26, 2005: FLOORBEAM. CORRODED. CABIN FLOORBEAM CORRODED AT STA 328, LBL 29. INSTALLED NEW ANGLE PER SRM 53-10-51. - [SDR CALA0500126](https://openairdocs.org/sdr/CALA0500126), Apr 26, 2005: FLOORBEAM. CORRODED. CABIN FLOORBEAM CORRODED AT STA 328, LBL 29. INSTALLED NEW ANGLE PER SRM 53-10-51. - [SDR CALA0300471](https://openairdocs.org/sdr/CALA0300471), Aug 14, 2003: SKIN. CRACKED. MAINTENANCE FOUND A SMALL CRACK IN THE LT HORIZONTAL STABILIZER LOWER SKIN JUST FORWARD OF THE REAR SPAR FORWARD FLANGE, STAB STA 152. AN INTERIM REPAIR WAS PER - [SDR CALA0300467](https://openairdocs.org/sdr/CALA0300467), Aug 14, 2003: PANEL. DELAMINATED. INSPECTION FOUND RT WING PANEL UPPER SURFACE DELAMINATED O/B OF MLG. THE PANEL WAS REPAIRED IAW BOEING DRAWING 65-50820-188. - [SDR CALA0300466](https://openairdocs.org/sdr/CALA0300466), Aug 13, 2003: SKIN. CRACKED. INSPECTION FOUND NR 1 SLAT LOWER L/E SKIN CRACKED AT O/B TRACK. THERE WERE FOUR CRACKS MEASURING FROM .125 TO .25 INCH IN LENGTH. A REPAIR DOUBLER WAS INSTALLED - [SDR CALA0300465](https://openairdocs.org/sdr/CALA0300465), Aug 13, 2003: PANEL. GOUGED. INSPECTION FOUND RUDDER HINGE COVER PANELS NR 9559 AND 9555 GOUGED. NEW PANELS WERE INSTALLED IAW SRM 51-10-02 AND BOEING DRAWING 65C25973. - [SDR CALA0300464](https://openairdocs.org/sdr/CALA0300464), Aug 11, 2003: SKIN. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN RT WING LEADING EDGE SKIN AT NR 4 SLAT ACTUATOR. A REPAIR DOUBLER WAS INSTALLED IAW SRM 57-41-01. - [SDR CALA0300463](https://openairdocs.org/sdr/CALA0300463), Aug 11, 2003: CHANNEL. CORRODED. INSPECTION FOUND LT CHANNEL CORRODED ON FORWARD SIDE OF AFT PRESSURE BULKHEAD AT LOWER END, STA 1016, BL 0. THE CHANNEL WAS REPAIRED IAW EA 5310-04045 AND DRAWI - [SDR CALA0300462](https://openairdocs.org/sdr/CALA0300462), Aug 10, 2003: SKIN. CRACKED. INSPECTION FOUND A 0.40 INCH CRACK IN PYLON CUTOUT FOR PANEL NR 5727, NR 1 ENGINE. THE CRACK WAS STOP DRILLED AND A REPAIR WAS INSTALLED IAW ECRA 5430-01230. - [SDR CALA0300461](https://openairdocs.org/sdr/CALA0300461), Aug 10, 2003: FLOOR PANEL. CRACKED. INSPECTION FOUND A 4 INCH CRACK IN PILOT'S LT SIDE FLOOR PANEL. THE FLOOR PANEL WAS REMOVED AND A NEW PANEL WAS INSTALLED IAW SRM 51-10-02. - [SDR CALA0300459](https://openairdocs.org/sdr/CALA0300459), Aug 10, 2003: ATTACH ANGLE. CRACKED. INSPECTION FOUND A 6 INCH CRACK IN ATTACH ANGLE ON HORIZONTAL STABILIZER CENTER SECTION AT UPPER BEAM. THE ATTACH ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-0 - [SDR CALA0300456](https://openairdocs.org/sdr/CALA0300456), Aug 9, 2003: FLOOR SUPPORT. CRACKED. INSPECTION FOUND A .5000 INCH CRACK IN CABIN FLOOR SUPPORT BETWEEN BS 380-400, BL 0. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-40-02. - [SDR CALA0300088](https://openairdocs.org/sdr/CALA0300088), Mar 3, 2003: SKIN. NICKED. INSPECTION FOUND A NICK IN L/H FUSELAGE SKIN AT STA 235.8, 17.7 INCHES BELOW WL 207.5. A REPAIR DOUBLER AND FILLER WERE INSTALLED IAW ECRA 5330-03218. - [SDR CALA0100535](https://openairdocs.org/sdr/CALA0100535), May 25, 2001: KEELBEAM. CRACKED. INSPECTION FOUND A 0.045 INCH CRACK AT HOLE OF KEEL BEAM RT LOWER CHORD, STA 682, RBL 8 (WHEEL WELL AREA). THE CRACKED AREA WAS REMOVED, A FREEZE PLUG AND REPAI - [SDR CALA0100485](https://openairdocs.org/sdr/CALA0100485), May 20, 2001: WEB. CRACKED. INSPECTION FOUND A 0.3 INCH CRACK IN C-2 DOOR AT LIGHTENING HOLE LOCATED AT ACCESS TO SPRING SUPPORT FITTING. THE CRACKED AREA WAS TRIMMED AND DRESSED UP AND A - [SDR CALA0100461](https://openairdocs.org/sdr/CALA0100461), May 16, 2001: SKIN. CRACKED. INSPECTION FOUND A 2 INCH CRACK IN FUSELAGE SKIN AND INTERIOR SUPPORT FOR NR 3 VHF ANTENNA BETWEEN STA 727D AND 727E, BL 0. REPAIRED IAW SRM 53-00-01. - [SDR CALA0100460](https://openairdocs.org/sdr/CALA0100460), May 16, 2001: SKIN. DAMAGED. INSPECTION FOUND A SMALL CREASE IN FUSELAGE SKIN AT STA 1042, S13L. A DOUBLER WAS INSTALLED IAW SRM 53-00-01, FIGURE 202 AND 51-70. - [SDR CALA0100459](https://openairdocs.org/sdr/CALA0100459), May 16, 2001: SKIN. DENTED. INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 1008, S16L. THE DENTED AREA WAS CUT OUT AND A DOUBLER WAS INSTALLED IAW SRM 53-00-01, FIGURE 202. - [SDR CALA0100458](https://openairdocs.org/sdr/CALA0100458), May 15, 2001: SPAR. CRACKED. INSPECTION FOUND A 0.1 INCH CRACK IN RT REAR SPAR UPPER CHORD AT RT MLG BEAM O/B END AFT SPAR FITTING ATTACH AREA. THE CRACK WAS REPAIRED IAW ECRA 5743-01033. A - [SDR CALA0100455](https://openairdocs.org/sdr/CALA0100455), May 12, 2001: STRINGER. GOUGED. INSPECTION FOUND STRINGER 14R GOUGED AT STA 600. A NEW STRINGER SECTION WAS INSTALLED IAW SRM 53-00-03, PAGE 201. - [SDR CALA0100449](https://openairdocs.org/sdr/CALA0100449), May 7, 2001: SEAT TRACK. CORRODED. INSPECTION FOUND LEFT O/B SEAT TRACK CORRODED AT STA 887-947.5. A SEAT TRACK REPAIR WAS INSTALLED IAW SRM 53-00-52, FIGURE 204. - [SDR CALA0100448](https://openairdocs.org/sdr/CALA0100448), May 7, 2001: ANGLE. CORRODED. INSPECTION FOUND R-1 DOOR ENTRYWAY Z-ANGLE CORRODED. THE Z-ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-2. - [SDR CALA0100443](https://openairdocs.org/sdr/CALA0100443), May 4, 2001: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM CORRODED AROUND FASTENER HOLES AT STA 312, LBL 12-RBL 12. THE MAJORITY OF CORROSION WAS BURNISHED OUT. A REPAIR STRAP WAS INSTALLED I - [SDR CALA0100121](https://openairdocs.org/sdr/CALA0100121), Feb 15, 2001: BULKHEAD. CRACKED. INSPECTION FOUND TWO CRACKS ON FLOOR STRUCTURE WEB AT LT AND RT W/L 195, ONE CRACK ON CENTER WEB AT W/L 200, LBL 5.7 AND ONE CRACK ON CENTER WEB AT W/L 201, RBL - [SDR CALA0100114](https://openairdocs.org/sdr/CALA0100114), Feb 10, 2001: SKIN. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN AFT SKIN CUTOUT FOR THE E&E COMPARTMENT COOLING EXHAUST. A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5330-02894. - [SDR CALA9900555](https://openairdocs.org/sdr/CALA9900555), May 17, 1999: SKIN. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN NR 2 ENGINE PYLON SKIN AT PANEL NR 5824 AND A .5 INCH CRACK WAS FOUND IN PANEL NR 5828. REPAIRS WERE INSTALLED IAW ECRA 5430 - [SDR CALA9700776](https://openairdocs.org/sdr/CALA9700776), May 16, 1997: FLOORBEAM. CORRODED. INSPECTION FOUND CORROSION ON TOP OF FLOORBEAM AT STA 986.5. THE CORRODED AREA WAS CUT OUT AND A T-SECTION WAS INSTALLED IAW ECRA 5310-03450. - [SDR CALA9700786](https://openairdocs.org/sdr/CALA9700786), May 14, 1997: ANGLE. CRACKED. INSPECTION FOUND A .75 INCH CRACK IN NR 3 FLAP FAIRING WING TRAILING EDGE ATTACH ANGLE. THE ANGLE WAS REPLACED IAW SRM 51-10-02. - [SDR CALA9700784](https://openairdocs.org/sdr/CALA9700784), May 9, 1997: SUPPORT. CORRODED. INSPECTION FOUND FLOOR SUPPORT CORRODED AT BS 950, LBL 11. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-02. - [SDR CALA9700775](https://openairdocs.org/sdr/CALA9700775), May 9, 1997: STRAP. CORRODED. INSPECTION FOUND LT AFT LAV STRAP CORRODED AT BS 1006 TO 1016, LBL 3. A NEW STRAP WAS FABRICATED AND INSTALLED IAW SRM 51-10-2. - [SDR CALA9700783](https://openairdocs.org/sdr/CALA9700783), May 8, 1997: SUPPORT. CORRODED. INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 299, RBL 20. A REPAIR WAS INSTALLED IAW ECRA 5310-03477. - [SDR CALA9700781](https://openairdocs.org/sdr/CALA9700781), May 8, 1997: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM CORRODED AT STA 344 LBL 31.6 TO L-1 DOOR AND RBL 30 TO LBL 10. THE CORRODED AREAS WERE REMOVED, REPAIRS WERE INSTALLED IAW SRM 53-10- - [SDR CALA9700780](https://openairdocs.org/sdr/CALA9700780), May 8, 1997: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM CORRODED AT STA 294.5, RBL 0. A NEW FLOORBEAM SECTION WAS INSTALLED IAW SRM 53-10-51. - [SDR CALA9700779](https://openairdocs.org/sdr/CALA9700779), May 8, 1997: SUPPORT. CORRODED. INSPECTION FOUND FLOOR SUPPORTS CORRODED BETWEEN STA 294.5 AND 312, RBL 15 AND RBL 30. THE FLOOR SUPPORTS WERE REMOVED AND REPLACED IAW ECRA 5310-03477 AND SRM - [SDR CALA9700785](https://openairdocs.org/sdr/CALA9700785), May 7, 1997: SUPPORT. CORRODED. INSPECTION FOUND RT AFT LAV FLOOR SUPPORT CORRODED AT BS 986 TO 990, RBL 10. THE FLOOR SUPPORT WAS REPAIRED IAW SRM 51-10-00. All 59: https://openairdocs.org/deregistered/N70330-2013-03-21/reports.md ## Other aircraft with N70330 - [Cancelled 1971-11-24](https://openairdocs.org/deregistered/N70330-1971-11-24): Piper J3C-65, S/N 17310. Owner: [Frances Mae Tennille](https://openairdocs.org/faa-owner/FRANCES%20MAE%20TENNILLE), [Milledgeville, GA](https://openairdocs.org/faa-place/GA/Milledgeville) --- 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.