# N69333: 1986 Boeing 737-3TO, registration cancelled 2013-03-21

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: March 21, 2013
- Status when cancelled: Third renewal notice
- 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: 23571
- Year built: 1986
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: October 3, 1986
- Certificate issued: April 9, 2009
- Last registry action: April 9, 2009
- Mode S code: A938B8
- 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/N69333
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=69333
- Page: https://openairdocs.org/deregistered/N69333-2013-03-21

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 (55, newest 50)

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

- [SDR CALA0800197](https://openairdocs.org/sdr/CALA0800197), Mar 5, 2008: ATTACH FITTING. CRACKED. STA 384.2 LEFT SIDE S-15 ATTACH CLIP CRACKED. REMOVED AND REPLACED CRACKED CLIP AT BS 348.2 STRINGER 15 LT PER ECRA 5310-04726.
- [SDR CALA08](https://openairdocs.org/sdr/CALA08), Mar 5, 2008: ATTACH FITTING. CRACKED. STA 384.2 LEFT SIDE S-15 ATTACH FITTING CRACKED. REMOVED AND REPLACED CRACKED ATTACH FITTING AT BS 348.2 STRINGER 15 LT PER ECRA 5310-04726.
- [SDR CALA0500422](https://openairdocs.org/sdr/CALA0500422), Nov 29, 2005: SPRING. BROKEN. THE R-2 DOOR AND L-2 DOOR ESCAPE SLIDE AFT GIRT BAR FLOOR BRACKETS WERE FOUND WITH SPRINGS BROKEN. NEW GIRT BAR FLOOR BRACKETS WERE INSTALLED AT BOTH AFT DOORS 
- [SDR CALA0500343](https://openairdocs.org/sdr/CALA0500343), Oct 9, 2005: SKIN. CRACKED. AFT BAG BIN CARGO DOOR SKIN CRACKED AROUND HANDLE. INSTALLED DOUBLER PER SRM 52-00-01, 51-40-02, 51-20-05, 51-20-01.
- [SDR CALA0500342](https://openairdocs.org/sdr/CALA0500342), Oct 9, 2005: FRAME. CORRODED. AFT BAG BIN FLOOR FRAME STA 847 CORRODED AT SHEAR CLIPS. REPLACE FRAME SECTION PER SRM 51-10-02.
- [SDR CALA0500398](https://openairdocs.org/sdr/CALA0500398), Oct 7, 2005: FLOORBEAM. CORRODED. INSPECTION FOUND THE RT SIDE OF UPPER CHORD OF FLOORBEAM CORRODED AT STA 1016, RBL 16 TO RBL 35. THE FLOORBEAM WAS REPAIRED BY SPLICING IN A NEW SECTION OF UPPE
- [SDR CALA0500340](https://openairdocs.org/sdr/CALA0500340), Oct 7, 2005: BULKHEAD. CORRODED. CORROSION AT STA 1016, BL 0, FWD LWR PRESSURE BULKHEAD. REPAIRED PER DRAWING 65C28106.
- [SDR CALA0500339](https://openairdocs.org/sdr/CALA0500339), Oct 7, 2005: KEELBEAM. CORRODED. LEFT KEELBEAM CORRODED FWD OF STA 500D. INSTALLED NEW SECTION OF KEEL BEAM PER SRM 53-60-12.
- [SDR CALA0500338](https://openairdocs.org/sdr/CALA0500338), Oct 7, 2005: WEB. CORRODED. AFT LEFT LAV PAN CORRODED. REPLACED LAV PAN PER SRM 51-40-01.
- [SDR CALA0500337](https://openairdocs.org/sdr/CALA0500337), Oct 7, 2005: WEB. CORRODED. AFT RIGHT LAV PAN CORRODED. REPLACED LAV PAN PER SRM 51-40-01.
- [SDR CALA0500329](https://openairdocs.org/sdr/CALA0500329), Oct 4, 2005: SKIN. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN FUSELAGE SKIN BONDED DOUBLER LINE STA 767 BETWEEN S21R AND S22R. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-00-01, FIGURE 201.
- [SDR CALA0500328](https://openairdocs.org/sdr/CALA0500328), Oct 4, 2005: SKIN. CRACKED. INSPECTION FOUND A 1.5 INCH CRACK IN FUSELAGE SKIN ON BONDED DOUBLER LINE STA 767 BETWEEN S22R AND S23R. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-00-01, FIGURE
- [SDR CALA050341](https://openairdocs.org/sdr/CALA050341), Sep 30, 2005: BULKHEAD. DAMAGED. RIVET HOLE ELONGATED AT AFT PRESSURE BULKHEAD WEB, STA 1016, BL 0. INSTALLED SKIN PER DRAWING 65C28106.
- [SDR CALA0500322](https://openairdocs.org/sdr/CALA0500322), Sep 29, 2005: FLOORBEAM. CORRODED. INSPECTION FOUND MAIN DECK FLOORBEAM CORRODED AT STA 344, LBL 16 TO RBL 9. THE SECTION OF FLOORBEAM WAS REPLACED IAW SRM 53-10-51.
- [SDR CALA0500323](https://openairdocs.org/sdr/CALA0500323), Sep 28, 2005: FLOORBEAM. CORRODED. INSPECTION FOUND MAIN DECK FLOORBEAM CORRODED AT STA 328, RBL 42 TO LBL 35. THE FLOORBEAM SECTION WAS REMOVED AND REPLACED IAW SRM 51-10-02 AND 51-40-02.
- [SDR CALA0500376](https://openairdocs.org/sdr/CALA0500376), Sep 21, 2005: WIRE HARNESS. BURNED. FUEL SHUT-OFF VALVE WIRES & O/B LANDING LIGHT WIRES FOUND BURNED IN JUNCTION BOX NEAR D5164J (LANDING LIGHT DISCONNECT) AT RT SIDE AFT WHEEL WELL. SMOKE & COKIN
- [SDR CALA0400234](https://openairdocs.org/sdr/CALA0400234), Mar 10, 2004: SKIN. DENTED. INSPECTION FOUND A DENT IN AFT CARGO DOOR OUTER SKIN. THE DENTED AREA WAS CUT OUT. A REPAIR DOUBLER WAS INSTALLED IAW SRM 52-00-01, FIGURE 203.
- [SDR CALA0400181](https://openairdocs.org/sdr/CALA0400181), Feb 28, 2004: STRAP. CORRODED. INSPECTION FOUND FLOOR STRAP CORRODED ALONG FASTENER HOLES AT BS 727D. THE STRAP WAS REMOVED AND REPLACED IAW SRM 51-10-02.
- [SDR CALA0400178](https://openairdocs.org/sdr/CALA0400178), Feb 27, 2004: ANGLE. CRACKED. INSPECTION FOUND A 2 INCH CRACK IN MAIN CABIN FLOOR SHEAR WEB ANGLE AT STA 384, BL 0. THE SHEAR WEB ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-02.
- [SDR CALA0400175](https://openairdocs.org/sdr/CALA0400175), Feb 26, 2004: INTERCOSTAL. CRACKED. INSPECTION FOUND A 2 INCH CRACK IN INTERCOSTAL AT STA 344, BL 0. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-10-02.
- [SDR CALA0400163](https://openairdocs.org/sdr/CALA0400163), Feb 25, 2004: FLAP. DELAMINATED. INSPECTION FOUND LEFT WING NR 1 AFT FLAP INBOARD T/E DELAMINATED. REPAIRED IAW SRM 51-70-10.
- [SDR CALA0300571](https://openairdocs.org/sdr/CALA0300571), Oct 2, 2003: GEARBOX. FAILED. THE NR 2 ENGINE SUDDENLY AUTO SHUTDOWN WHILE CLIMBING THROUGH 19K AFTER TAKEOFF FROM EWR. THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAI
- [SDR CALA0300024](https://openairdocs.org/sdr/CALA0300024), Jan 22, 2003: PRESSURE PANEL. CRACKED. INSPECTION FOUND A CRACK IN THE PRESSURE DECK WEB AT STA 663, LBL 32. THE CRACK WAS ESTIMATED AT BEING .5 - .75 INCH LONG. A REPAIR WAS PERFORMED IAW SRM 53-60-
- [SDR CALA0200451](https://openairdocs.org/sdr/CALA0200451), Sep 6, 2002: PUMP. FAILED. THE NR 2 ENGINE FLAMED OUT WHILE ON DESCENT AT 10,000 FEET. AN ENGINE RESTART WAS ATTEMPTED, BUT WAS UNSUCCESSFUL. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTEN
- [SDR CALA0100989](https://openairdocs.org/sdr/CALA0100989), Oct 30, 2001: SKIN. CRACKED. INSPECTION FOUND CRACKS COMING FROM THREE RIVETS ON LOWER SIDE OF #6 SLAT SKIN BELOW I/B AUX TRACK. REPAIRED SLAT IAW SRM 57-43-01.
- [SDR CALA0100982](https://openairdocs.org/sdr/CALA0100982), Oct 28, 2001: SKIN. CRACKED. INSPECTION FOUND #1 SLAT SKIN CRACKED AT AFT ROW OF RIVETS APPROXIMATELY 1/8" ON EITHER SIDE OF RIVET, 43" O/B OF I/B END. A REPAIR WAS INSTALLED IAW SRM 57-43-
- [SDR CALA0100981](https://openairdocs.org/sdr/CALA0100981), Oct 26, 2001: CARGO TRACK. CORRODED. INSPECTION FOUND TIE DOWN RAIL CORRODED AROUND FASTENER HOLES AT STA 727-945.5, RBL 26. THE CORRODED SECTIONS OF TIE DOWN RAIL WERE REMOVED AND REPLACED IAW SRM
- [SDR CALA0100978](https://openairdocs.org/sdr/CALA0100978), Oct 25, 2001: BRACKET. CRACKED. LEFT ELEVATOR #4 HINGE UPPER ACCESS COVER OUTBOARD ATTACH BRACKET CRACKED. FABRICATED AND INSTALLED NEW BRACKET ON ELEVATOR PER SRM 51-40-01.
- [SDR CALA0100971](https://openairdocs.org/sdr/CALA0100971), Oct 24, 2001: SKIN. DENTED. DENT IN LEADING EDGE OF RIGHT HORIZONTAL STABILIZER AT STATION 263. PERFORMED INTERIM REPAIR PER SRM 55-10-01. PERMANENT REPAIR REQUIRED IN 18 MONTHS.
- [SDR CALA0100970](https://openairdocs.org/sdr/CALA0100970), Oct 24, 2001: FRAME. DENTED. FRAME 727B UPPER CAP DENTED AT S-21LT. FABRICATED AND INSTALLED REPAIR PER SRM 51-70-11.
- [SDR CALA0100969](https://openairdocs.org/sdr/CALA0100969), Oct 24, 2001: KEEL. WORN. STRUCTURE AROUND HOLES FOR ATTACHMENT OF WHEEL WELL FAIRING WORN IN LEFT MLG. REPAIRED AREA ON KEEL REQUIRED BY EC/RA 5310-03740.
- [SDR CALA0100968](https://openairdocs.org/sdr/CALA0100968), Oct 24, 2001: ANGLE. WORN. T ANGLE ON FUSELAGE FORWARD END AT FILLET FAIRING SUPPORT ANGLE THAT ATTACHES TO UPPER WING TRAILING EDGE WORN. REMOVED AND REPLACED ANGLE PER SRM 51-10-2 AND 5
- [SDR CALA0100966](https://openairdocs.org/sdr/CALA0100966), Oct 22, 2001: FLOORBEAM. CORRODED. FLOORBEAM STATION 986.5 HAS SEVERAL CORRODED HOLES AT UPPER FLANGE (TOP AND BOTTOM). REPAIRED FLOORBEAM PER EC/RA 5310-03851.
- [SDR CALA0100965](https://openairdocs.org/sdr/CALA0100965), Oct 22, 2001: SKIN. CRACKED. L2 DOOR SKIN CRACKED AT UPPER HINGE CUT OUT (5/16"). REPAIRED PER SRM 52-00-01.
- [SDR CALA0100964](https://openairdocs.org/sdr/CALA0100964), Oct 22, 2001: PANEL. CORRODED. TRANSITION PANEL CORRODED AT BS 420 - 440 RIGHT. FABRICATED AND INSTALLED TRANSITION PANEL PER SRM 51-40-02.
- [SDR CALA0100963](https://openairdocs.org/sdr/CALA0100963), Oct 22, 2001: SEAT TRACK. CORRODED. CABIN RIGHT SIDE INBOARD SEAT TRACK CORRODED FROM STATION 727E TO STATION 767. REMOVED AND REPLACED SEAT TRACK PER SRM 53-00-52, SOPM 20-41-04 AND AMM 51-21-00.
- [SDR CALA0100962](https://openairdocs.org/sdr/CALA0100962), Oct 18, 2001: WEB. CRACKED. AFT LEFT AREA STATION 996 FLOOR WEB CRACKED (1 INCH) UNDER L2 Z-ANGLE. INSTALLED SERVICEABLE WEB WITH FASTENERS PER SRM 51-10-02.
- [SDR CALA0100960](https://openairdocs.org/sdr/CALA0100960), Oct 17, 2001: SEAT TRACK. CRACKED. SEAT TRACK RBL 44 BS 328 - 380 CORRODED. CRACK (1/2") AT BS 380. REPAIRED PER SRM 53-00-02 AND 51-30-02.
- [SDR CALA0100956](https://openairdocs.org/sdr/CALA0100956), Oct 16, 2001: ANGLE. CORRODED. CORROSION ON Z1 ANGLE AND ON L ANGLES BENEATH THE Z (BS 312-328 AND 328-344). REMOVED AND REPLACED ZEE ANGLES AND L-ANGLES PER SRM 51-10-02.
- [SDR CALA0100950](https://openairdocs.org/sdr/CALA0100950), Oct 15, 2001: FLOOR SUPPORT. CRACKED. FLOOR SUPPORT CRACKED AT SCREW HOLES BETWEEN STATIONS 927 AND 947.5 AT BL 0.0. FABRICATED AND INSTALLED SUPPORT ASSEMBLY PER SRM 51-10-2.
- [SDR CALA0100947](https://openairdocs.org/sdr/CALA0100947), Oct 12, 2001: FLOORBEAM. CORRODED. FLOORBEAM BS 360, RBL 0-60, CORROSION UNDER G-2 GALLEY. REPAIRED FLOORBEAM IN REF TO SRM 53-00-51.
- [SDR CALA0100944](https://openairdocs.org/sdr/CALA0100944), Oct 12, 2001: ANGLE. CRACKED. BS 294 BOX ANGLE CRACKED AT R1 DOOR CUT OUT JUST ABOVE FLOOR BEAM. TRIMMED CRACKED FLANGE. APPLIED ALODINE ADN PRIMER AND INSTALLED .050 FILLER PER EC/RA 5310-0
- [SDR CALA0100942](https://openairdocs.org/sdr/CALA0100942), Oct 11, 2001: SKIN. CRACKED. INSPECTION FOUND A 1/2" CRACK IN L-1 WINDOW POST SKIN. THE CRACKED AREA OF SKIN WAS REMOVED AND FILLER AND DOUBLER WERE INSTALLED IAW SRM 53-10-01.
- [SDR CALA9801336](https://openairdocs.org/sdr/CALA9801336), Jul 24, 1998: CIRCUIT BREAKER. POPPED. THE GEAR HANDLE WOULD NOT MOVE PAST OFF POSITION AFTER TAKEOFF. THE AIRCRAFT WAS RETURNED TO ORD WHERE IT LANDED WITHOUT INCIDENT. TROUBLESHOOTING BY MAINTENANC
- [SDR CALA9800877](https://openairdocs.org/sdr/CALA9800877), May 19, 1998: CIRCUIT BREAKER. TRIPPED. THE GEAR LEVER WOULD NOT MOVE FROM THE OFF TO THE UP POSITION UPON GEAR RETRACTION AFTER TAKEOFF FROM IAH. CHECKLIST PROCEDURES WERE ACCOMPLISHED AND THE LOCK O
- [SDR CALA9800724](https://openairdocs.org/sdr/CALA9800724), Apr 29, 1998: WIRE. BROKEN. THE EMERGENCY TRACK LIGHTS AT LAST FIVE ROWS OF AIRCRAFT WERE FOUND INOPERATIVE DURING A PREFLIGHT CHECK. MAINTENANCE FOUND A WIRE BROKEN AT SEAT 21. THE WIRE W
- [SDR CALA971402](https://openairdocs.org/sdr/CALA971402), Oct 2, 1997: CHORD. CRACKED. INSPECTION FOUND A 3 CRACK IN LOWER T-CHORD AT NR 5 SLAT. THE T-CHORD WAS REMOVED AND REPLACED IAW SRM 51-10-02.
- [SDR CALA9701390](https://openairdocs.org/sdr/CALA9701390), Sep 26, 1997: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM CORRODED AT STA 294, RBL 10. THE FLOORBEAM WAS REPAIRED IAW SRM 53-10-51.
- [SDR CALA9700342](https://openairdocs.org/sdr/CALA9700342), Mar 13, 1997: WIRE. SHORTED. INSPECTION FOUND EMERGENCY EXIT FLOOR TRACK LIGHTING INOPERATIVE FROM ROWS 1 TO 7. A BLOWN FUSE WAS FOUND IN FORWARD BATTERY CHARGER. THE FUSE WAS REMOVED AND R
- [SDR CALA9601135](https://openairdocs.org/sdr/CALA9601135), Aug 6, 1996: FUEL CONTROL. INOPERATIVE. THE NR 1 ENGINE FLAMED OUT ON APPROACH TO IAH. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE FUEL CONTROL UNIT. THE FUE

All 55: https://openairdocs.org/deregistered/N69333-2013-03-21/reports.md

## Other aircraft with N69333

- [Cancelled 1973-10-11](https://openairdocs.org/deregistered/N69333-1973-10-11): Cessna 402B, S/N 402B0443. Exported to South Africa. Owner: [Floair Inc](https://openairdocs.org/faa-owner/FLOAIR%20INC), [Wichita, KS](https://openairdocs.org/faa-place/KS/Wichita)
- [Cancelled 1949-04-26](https://openairdocs.org/deregistered/N69333-1949-04-26): Douglas UC-67, S/N 2744. Owner: [Fenwick Hugh Mcl](https://openairdocs.org/faa-owner/FENWICK%20HUGH%20MCL), [New York, NY](https://openairdocs.org/faa-place/NY/New%20York)

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