# N61304: 1985 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: 23355
- Year built: 1985
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: July 30, 1985
- Certificate issued: April 4, 2006
- Last registry action: January 18, 2011
- Mode S code: A7FC58
- 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/N61304
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=61304
- Page: https://openairdocs.org/deregistered/N61304-2013-03-21

From the FAA registry file of November 5, 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 (56, newest 50)

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR CALA0700531](https://openairdocs.org/sdr/CALA0700531), Sep 23, 2007: SKIN. CRACKED. INSPECTION FOUND A 2.5 INCH CRACK IN SKIN AT STA 727E, S24L. REPAIRED IAW SRM 53-00-01, REPAIR 31.
- [SDR CALA0600340](https://openairdocs.org/sdr/CALA0600340), Sep 14, 2006: SKIN. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN FORWARD CARGO DOOR INNER SKIN AT THE CENTER INTERCOSTAL ON THE BOTTOM. A DOUBLER WAS INSTALLED IAW ECRA 5232-01081.
- [SDR CALA0600336](https://openairdocs.org/sdr/CALA0600336), Sep 13, 2006: STRINGER SPLICE. CRACKED. INSPECTION FOUND A 1/2" CRACK IN THE L-1 DOOR AFT NR 14 INTERCOSTAL STRINGER SPLICE AT STA 344-360, S14L. THE STRINGER SPLICE WAS REPLACED IAW ECRA 5311-01271 A
- [SDR CALA0600335](https://openairdocs.org/sdr/CALA0600335), Sep 13, 2006: INTERCOSTAL. CRACKED. INSPECTION FOUND A 1/2" CRACK IN L-1 DOOR FORWARD SIDE UPPER HINGE INTERCOSTAL LOWER WEB AT STA 294.5-312, S10L. THE INTERCOSTAL WEB WAS REPAIRED IAW ECRA 5311-
- [SDR CALA0600334](https://openairdocs.org/sdr/CALA0600334), Sep 13, 2006: STRINGER SPLICE. CRACKED. INSPECTION FOUND A 1/2" CRACK IN L-1 DOOR AFT NR 15 INTERCOSTAL STRINGER SPLICE AT STA 344-360, S15L. A NEW STRINGER SPLICE CHANNEL WAS INSTALLED IAW ECRA 5311-
- [SDR CALA0600339](https://openairdocs.org/sdr/CALA0600339), Sep 12, 2006: FITTING. CRACKED. INSPECTION FOUND A 1/4" CRACK IN A FRAME FITTING ON RT SIDE OF FUSELAGE JUST AFT OF STA 639, S15L, FRAME IS JUST BELOW THE CREASE BEAM IN THE MAIN CABIN. REPAIR
- [SDR CALA0600333](https://openairdocs.org/sdr/CALA0600333), Sep 12, 2006: FRAME. CORRODED. INSPECTION FOUND LOWER O/B CHORD OF BULKHEAD CORRODED AT STA 227.8, LBL 5 TO RBL 10, S29L TO 29R. A REPAIR WAS INSTALLED IAW ECRA 5311-01268.
- [SDR CALA0600332](https://openairdocs.org/sdr/CALA0600332), Sep 10, 2006: SLAT TRACK. CRACKED. INSPECTION FOUND A 1 INCH CRACK AROUND RIVET HOLES IN RT WING NR 6 SLAT I/B AUX TRACK LOWER AREA. THE AREA WAS REPAIRED IAW SRM 57-43-01.
- [SDR CALA0600331](https://openairdocs.org/sdr/CALA0600331), Sep 5, 2006: FRAME. CORRODED. INSPECTION FOUND UPPER SURFACE OF FRAME CORRODED AT STA 727B BETWEEN S26L AND S27L. THE CORRODED SECTION OF FRAME WAS TRIMMED OFF AND A REPAIR DOUBLER WAS INSTA
- [SDR CALA0600330](https://openairdocs.org/sdr/CALA0600330), Sep 3, 2006: FITTING. CORRODED. INSPECTION FOUND LEFT AFT FWD, RIGHT AFT FWD, AND RIGHT AFT O/B VERTICAL STABILIZER DRAG ANGLE FITTINGS CORRODED AT STA 1088, S2L AND S2R. THE FITTINGS WERE REM
- [SDR CALA0600329](https://openairdocs.org/sdr/CALA0600329), Sep 2, 2006: FITTING. CORRODED. INSPECTION FOUND NR 1 FLAP TRACK AFT SPAR FITTING CORRODED AT MOUNT BOLT. THE SPAR FITTING WAS REMOVED AND REPLACED IAW SRM 51-40-02 AND BOEING DRAWING 65-46429
- [SDR CALA0600328](https://openairdocs.org/sdr/CALA0600328), Sep 2, 2006: SHEAR TIE. CORRODED. INSPECTION FOUND LOWER CENTER SHEAR CLIP ON FRAME IN FORWARD CARGO COMPARTMENT AT STA 500, S28L TO 28R CORRODED. THE CORRODED AREA WAS REMOVED AND FILLER AND DO
- [SDR CALA0600327](https://openairdocs.org/sdr/CALA0600327), Sep 1, 2006: STRINGER. CORRODED. INSPECTION FOUND STRINGER 25L CORRODED AT STA 344-360. THE CORRODED SECTION OF STRINGER WAS CUT OUT AND A STRINGER REPAIR WAS INSTALLED IAW SRM 53-00-03, REPAIR
- [SDR CALA0600324](https://openairdocs.org/sdr/CALA0600324), Sep 1, 2006: STRINGER. CORRODED. INSPECTION FOUND STRINGER 25L CORRODED AT STA 967. A NEW STRINGER SECTION WAS SPLICED IN IAW SRM 53-00-03.
- [SDR CALA0600338](https://openairdocs.org/sdr/CALA0600338), Aug 31, 2006: INTERCOSTAL. CRACKED. INSPECTION FOUND A 1" CRACK IN L-1 DOOR AFT INTERCOSTAL INNER STRAP AT STA 360, S16L. THE INTERCOSTAL INNER STRAP WAS REPAIRED IAW SRM 53-10-04.
- [SDR CALA0600337](https://openairdocs.org/sdr/CALA0600337), Aug 31, 2006: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM CORRODED AT STA 1016, RBL 4 TO RBL 36. THE FLOORBEAM UPPER CHORD WAS REMOVED AND REPLACED IAW ECRA 5310-03851.
- [SDR CALA0600323](https://openairdocs.org/sdr/CALA0600323), Aug 31, 2006: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM CORRODED AT STA 1016, RBL 4 TO RBL 36. THE FLOORBEAM UPPER CHORD WAS REMOVED AND REPLACED IAW ECRA 5310-03851.
- [SDR CALA0600322](https://openairdocs.org/sdr/CALA0600322), Aug 31, 2006: STRINGER. CORRODED. INSPECTION FOUND STRINGER 24L CORRODED AT STA 1016, LBL 20. THE STRINGER WAS REPAIRED IAW SRM 53-00-03.
- [SDR CALA0600320](https://openairdocs.org/sdr/CALA0600320), Aug 31, 2006: CREASE BEAM. CRACKED. INSPECTION FOUND A 1.5 INCH CRACK IN RIGHT SIDE CREASE BEAM WEB JUST AFT OF STA 616, RBL 45. THE WEB WAS REMOVED AND A NEW WEB WAS INSTALLED IAW SRM 51-40-02.
- [SDR CALA0600321](https://openairdocs.org/sdr/CALA0600321), Aug 30, 2006: PRESSURE PANEL. CRACKED. INSPECTION FOUND A 1.5 INCH CRACK IN MAIN CABIN LOWER PRESSURE DECK AT STA 663.75, LBL 30. A REPAIR WAS INSTALLED IAW SRM 53-60-51, FIGURE 201.
- [SDR CALA0600315](https://openairdocs.org/sdr/CALA0600315), Aug 27, 2006: FRAME. CORRODED. INSPECTION FOUND HEAVY INTERGRANULAR CORROSION ON FORWARD SIDE OF FRAME AT STA 219.8, S27R, RBL 17, O/B LOWER CHORD. A NEW CHORD WAS INSTALLED IAW SRM 51-2-02 A
- [SDR CALA0600311](https://openairdocs.org/sdr/CALA0600311), Aug 24, 2006: STRINGER. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN STRINGER 16L BETWEEN STA 500C AND 500D. THE STRINGER WAS REMOVED AND REPLACED IAW SRM 53-30-03.
- [SDR CALA0600309](https://openairdocs.org/sdr/CALA0600309), Aug 24, 2006: SEAT TRACK. CORRODED. INSPECTION FOUND RT OB SEAT TRACK CORRODED AT STA 540-727, RBL 24. THE SEAT TRACK WAS REPLACED IAW SRM 53-00-52, REPAIR 2, FIGURE 201.
- [SDR CALA0600308](https://openairdocs.org/sdr/CALA0600308), Aug 23, 2006: FRAME. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN LT MAIN FRAME AT STA 616 JUST BELOW FLOOR, S17L. A REPAIR ANGLE AND FILLER WERE INSTALLED IAW ECRA 5311-01158.
- [SDR CALA0600306](https://openairdocs.org/sdr/CALA0600306), Aug 23, 2006: FITTING. CORRODED. INSPECTION FOUND RT HORIZONTAL STABILIZER AFT AIRFRAME MOUNT LUG AT LOWER AND UPPER FORWARD POSITIONS CORRODED. THE AREA WAS REPAIRED AND NEW BUSHINGS WERE INST
- [SDR CALA0600305](https://openairdocs.org/sdr/CALA0600305), Aug 23, 2006: FITTING. CORRODED. INSPECTION FOUND RT HORIZONTAL STABILIZER FORWARD AIRFRAME MOUNT LUG AT LOWER AFT AND FORWARD POSITIONS AND AT UPPER FORWARD AND AFT POSITIONS CORRODED. THE ARE
- [SDR CALA0600301](https://openairdocs.org/sdr/CALA0600301), Aug 20, 2006: SEAT TRACK. CORRODED. INSPECTION FOUND SEAT TRACK CORRODED AT STA 270-294.5, RBL 42. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-40-02.
- [SDR CALA0600300](https://openairdocs.org/sdr/CALA0600300), Aug 20, 2006: SEAT TRACK. CORRODED. INSPECTION FOUND RIGHT O/B SEAT TRACK CORRODED AT STA 328. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-40-02.
- [SDR CALA0600299](https://openairdocs.org/sdr/CALA0600299), Aug 19, 2006: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM CORRODED AT STA 328, RBL 32-50. THE CORRODED AREA WAS BLENDED OUT AND A STRAP DOUBLER WAS INSTALLED IAW SRM 53-00-51 FIGURE 201.
- [SDR CALA0600028](https://openairdocs.org/sdr/CALA0600028), Jan 24, 2006: BEAM. CRACKED. THE LT AILERON BEAM WAS FOUND CRACKED AT WS 538, THE CRACK WAS STOP DRILLED PER ECRA 5752-01230. A DIP WAS ISSUED TO REINSPECT THE AREA AT 50 FLIGHT HOUR INTERV
- [SDR CALA0400749](https://openairdocs.org/sdr/CALA0400749), Dec 18, 2004: PANEL. CRACKED. INSPECTION FOUND TWO 1 INCH CRACKS IN NR 2 PYLON PANEL CUTOUT 5824R. THE CRACKS WERE LOCATED AT UPPER FORWARD CORNER OF PANEL. ONE CRACK ORIGINATED FROM RIVET H
- [SDR CALA0400748](https://openairdocs.org/sdr/CALA0400748), Dec 18, 2004: KEELBEAM. CORRODED. INSPECTION FOUND LT SIDE KEELBEAM CORRODED BETWEEN STA 520 AND 540, LBL 10. A KEEL BEAM SPLICE REPAIR WAS INSTALLED IAW SRM 53-60-12, FIGURE 203.
- [SDR CALA0500029](https://openairdocs.org/sdr/CALA0500029), Dec 17, 2004: STRINGER. CORRODED. INSPECTION FOUND STRINGER 26L CORRODED BETWEEN STA 440 AND 500D. THE STRINGER WAS REPAIRED USING A SPLICE IAW ECRA 5311-01215.
- [SDR CALA0400608](https://openairdocs.org/sdr/CALA0400608), Aug 23, 2004: SKIN. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN EXTERNAL SKIN BETWEEN STA 947.5 AND 967, S10L TO S11L (L-2 DOOR UPPER HINGE CUTOUT FORWARD CORNER RADIUS JUST BELOW THE RAIN 
- [SDR CALA0300650](https://openairdocs.org/sdr/CALA0300650), Nov 18, 2003: SKIN. CRACKED. INSPECTION FOUND A 5 INCH CRACK IN FUSELAGE BELLY SKIN AFT OF E&E COOLING DUCT AT BS 380, S28L. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS INSTALLED IAW ECRA 
- [SDR CALA0200465](https://openairdocs.org/sdr/CALA0200465), Sep 16, 2002: ANGLE. CRACKED. INSPECTION FOUND A 3" CRACK IN L/H WING LOWER/AFT O/B SUPPORT ANGLE. THE SUPPORT ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-2.
- [SDR CALA0200463](https://openairdocs.org/sdr/CALA0200463), Sep 16, 2002: DOUBLER. CRACKED. INSPECTION FOUND A 2" CRACK IN R/H WING UPPER I/B T/E PANEL DOUBLER, WBL 80. THE DOUBLER WAS REMOVED AND REPLACED IAW SRM 51-70-11.
- [SDR CALA0200461](https://openairdocs.org/sdr/CALA0200461), Sep 13, 2002: STIFFENER. CORRODED. INSPECTION FOUND CENTER STIFFENER ON AFT PRESSURE BULKHEAD FORWARD FACE CORRODED ON R/H SIDE, IN BILGE, BS 1016-1022. REPAIRED STIFFENER IAW SRM 51-70-11 AND 53
- [SDR CALA0200460](https://openairdocs.org/sdr/CALA0200460), Sep 11, 2002: WEB. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN CABIN FLOOR VERTICAL WEB AT STA 1016, LBL 26 BELOW STRAP. A REPAIR WAS INSTALLED IAW SRM 51-40-00.
- [SDR CALA0200459](https://openairdocs.org/sdr/CALA0200459), Sep 11, 2002: STIFFENER. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN STIFFENER ACROSS BOTTOM OF FLOORBEAMS AT STA 312, RBL 36, WL 201. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS INSTALLED IAW
- [SDR CALA0200458](https://openairdocs.org/sdr/CALA0200458), Sep 11, 2002: STIFFENER. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN STIFFENER ACROSS BOTTOM OF FLOORBEAMS AT STA 328, RBL 45, WL 201. A DOUBLER WAS INSTALLED IAW SRM 53-10-51.
- [SDR CALA0200455](https://openairdocs.org/sdr/CALA0200455), Sep 9, 2002: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM CORRODED AT STA 328, LBL 34. THE CORRODED AREA OF FLOORBEAM WAS CUT OUT. A CHORD AND SPLICE ANGLE REPAIR WAS INSTALLED IAW SRM 53-10-
- [SDR CALA0200129](https://openairdocs.org/sdr/CALA0200129), Mar 13, 2002: GROUND WIRE. UNSECURE. THE RIGHT WING EMERGENCY EXIT SIGN WOULD NOT TEST. MAINTENANCE FOUND LIGHT ASSEMBLY GROUND WIRE NOT SECURED TO GROUND STUD. TIGHTENED LOCKING NUT AND OPERATION 
- [SDR CALA0100402](https://openairdocs.org/sdr/CALA0100402), Apr 23, 2001: ACCESS PANEL. CRACKED. LEFT ENGINE PYLON UPPER OUTBOARD ACCESS PANEL CRACKED AT CUTOUT (.75 INCH). STOP DRILLED CRACK AND INSTALLED A REPAIR DOUBLER PER EC/RA 5430C01230.
- [SDR CALA0100401](https://openairdocs.org/sdr/CALA0100401), Apr 21, 2001: SKIN. CRACKED. PILOTS OUTBOARD WINDOW POST CRACKED AT TOP OUTBOARD CORNER (.75 INCH). INSTALLED REPAIR DOUBLER ON PST PER SRM 53-10-01 FIG 210.
- [SDR CALA0100110](https://openairdocs.org/sdr/CALA0100110), Jan 29, 2001: BULKHEAD. CRACKED. INSPECTION FOUND TWO 1 INCH CRACKS IN BULKHEAD WITH A STIFFENER BROKEN IN HALF AT STA 178. THE BULKHEAD WAS REMOVED AND REPLACED IAW EA 5310-03040.
- [SDR CALA0000991](https://openairdocs.org/sdr/CALA0000991), Jun 27, 2000: SKIN. CORRODED. INSPECTION FOUND SKIN CORRODED AND RIVET HEADS PULLED THROUGH SKIN AT STA 530-538, RBL 6.25. THE SKIN, KEEL BEAM LOWER CHORD, AND WING CENTER SECTION FRONT SPAR
- [SDR CALA9901440](https://openairdocs.org/sdr/CALA9901440), Oct 27, 1999: FRAME/BEAM. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN LOWER AFT FRAME AND A 2 INCH CRACK IN T-BEAM OF FORWARD CARGO DOOR LOWER FORWARD CORNER. THE FRAME WAS REPLACED IAW SRM 51-10
- [SDR CALA9801982](https://openairdocs.org/sdr/CALA9801982), Oct 21, 1998: FLOORBEAM. CORRODED. INSPECTION FOUND LT AFT LAV FLOORBEAM CORRODED AT STA 1006, LBL 16 TO LBL 28. REPAIRED IAW SRM 53-00-51.
- [SDR CALA9801978](https://openairdocs.org/sdr/CALA9801978), Oct 19, 1998: FLOORBEAM. CORRODED. INSPECTION FOUND LT AFT LAV FLOORBEAM CORRODED AT FASTENER HOLE, STA 1016, WL 208, LBL 5 TO LBL 38. THE FLOORBEAM WAS REPAIRED IAW ECRA 5310-03450.

All 56: https://openairdocs.org/deregistered/N61304-2013-03-21/reports.md

## FAA accident and incident reports (3)

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 20081125854669I](https://openairdocs.org/incident/20081125854669I), Nov 25, 2008: Boeing 7373TO (N61304), Cleveland, OH, Minor damage. (-23) Aircraft was at deicing pad when a deicing truck struck the tip of the left horizontal stabilizer. The aircraft taxied back to the gate and was deplaned.…
- [Incident 19930202003449I](https://openairdocs.org/incident/19930202003449I), Feb 2, 1993: Boeing 737300 (N61304), Washington, DC. NR2 engine oil quanity pressure went to zero. Precautionary landing. Found oil leak on oil cooler line.
- [Incident 19910308012039I](https://openairdocs.org/incident/19910308012039I), Mar 8, 1991: Boeing 7373T0 (N61304), Atlanta, GA. Odor of smoke in cockpit. Returned. Turned off ac packs. Found fork assembly of ac accessory unit missing.

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