# N19357: 1988 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: 23841
- Year built: 1988
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: March 15, 1988
- Certificate issued: January 11, 2010
- Last registry action: September 13, 2010
- Mode S code: A17677
- Owner when cancelled: [Continential Airlines Inc](https://openairdocs.org/faa-owner/CONTINENTIAL%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/N19357
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=19357
- Page: https://openairdocs.org/deregistered/N19357-2013-03-21

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 (88, newest 50)

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

- [SDR CALA0700194](https://openairdocs.org/sdr/CALA0700194), Apr 21, 2007: SKIN. CORRODED. FUSELAGE SKIN INSIDE AIR DISTRIBUTION BAY FWD SIDE OF STA 540 STR 28RT KEEL BEAM CORRODED. REPAIRED IAW ECRA 5331-01301.
- [SDR CALA0700193](https://openairdocs.org/sdr/CALA0700193), Apr 21, 2007: FRAME. CRACKED. FUSELAGE FRAME AND WEB CRACKED AT STA 639 AT STRINGER 17L. REPAIRED IAW ECRA 5311-01311.
- [SDR CALA0700192](https://openairdocs.org/sdr/CALA0700192), Apr 21, 2007: FRAME. CRACKED. LEFT FRAME CRACKED AT STA 639 ON O/B CHORD. REPAIRED IAW ECRA 5311-01312.
- [SDR CALA0700191](https://openairdocs.org/sdr/CALA0700191), Apr 21, 2007: FRAME. CRACKED. LEFT FRAME CRACKED AT STA 639 ON OUTBOARD CHORD. REPAIRED IAW ECRA 5311-01312.
- [SDR CALA0700190](https://openairdocs.org/sdr/CALA0700190), Apr 21, 2007: PLATE. CRACKED. NR 1 ENGINE PYLON PANEL OPENING FOR PANEL 5724 CRACKED. REPAIRED IAW ECRA 5431-01034.
- [SDR CALA0700189](https://openairdocs.org/sdr/CALA0700189), Apr 21, 2007: KEELBEAM. DAMAGED. LWR FUSELAGE SKIN BULGING AT STA 540, RBL 4. REPAIRED IAW SRM 51-40-02, AND 53-60-12.
- [SDR CALA0700188](https://openairdocs.org/sdr/CALA0700188), Apr 21, 2007: SHEAR TIE. CRACKED. FWD BAG BIN STA 500D, BL 0, CRACKED SHEAR TIE. REPAIRED IAW SRM 51-40-02, AND DRWG 69-73057-11.
- [SDR CALA0700187](https://openairdocs.org/sdr/CALA0700187), Apr 20, 2007: FRAME. CORRODED. CORROSION INSIDE LWR NOSE COMPARTMENT AFT SIDE OF CUTOUT, STA 227. REPAIRED IAW ECRA 5311-01308.
- [SDR CALA0700178](https://openairdocs.org/sdr/CALA0700178), Apr 16, 2007: ANGLE. CRACKED. CRACKED ANGLE FOR INTERCOSTAL STRINGER 16L AT STA 344. REPAIRED IAW SRM 53-10-04.
- [SDR CALA0700176](https://openairdocs.org/sdr/CALA0700176), Apr 12, 2007: DOOR FRAME. CRACKED. CRACK AROUND LWR STOP PAD FITTING AT THE FWD CARGO DOOR AFT FRAME. REPAIRED IAW SRM 51-40-02.
- [SDR CALA0700172](https://openairdocs.org/sdr/CALA0700172), Apr 10, 2007: DOOR FRAME. CRACKED. FWD CARGO DOOR CUTOUT, FWD FRAME CRACKED AROUND THE LOWER STOP PAD FITTING. REPLACED FRAME IAW SRM 51-40-02, AND DRAWING 65-20722.
- [SDR CALA0600498](https://openairdocs.org/sdr/CALA0600498), Nov 25, 2006: CHARGER. INOPERATIVE. THE AFT CENTER EMERGENCY LIGHT BATTERY PACK AND CHARGER WERE FOUND INOPERATIVE. THE BATTERY AND CHARGER WERE REPLACED IAW MM 33-51-51-201.
- [SDR CALA0600368](https://openairdocs.org/sdr/CALA0600368), Sep 12, 2006: SKIN. CRACKED. INSPECTION FOUND A 2.5 INCH CRACK IN FUSELAGE SKIN AT STA 727D + 9.9, S22L. THE SKIN WAS REPAIRED IAW ECRA 5330-03580 AND A DIP WAS ISSUED TO REINSPECT THE AREA
- [SDR CALA0600268](https://openairdocs.org/sdr/CALA0600268), Jul 12, 2006: SKIN. CORRODED. INSPECTION FOUND INSIDE SURFACE OF FUSELAGE SKIN PANEL CORRODED AT STA 967 BETWEEN S27L AND S27R. THE PANEL WAS REPAIRED IAW ECRA 5331-01246.
- [SDR CALA0400741](https://openairdocs.org/sdr/CALA0400741), Dec 9, 2004: SKIN. CRACKED. INSPECTION FOUND A .5 INCH CRACK AT LIGHTENING HOLE (3RD FROM TOP AND 1 FROM AFT EDGE OF DOOR) IN AFT CARGO DOOR INNER SKIN. A DOUBLER WAS INSTALLED IAW ECRA 52
- [SDR CALA0400740](https://openairdocs.org/sdr/CALA0400740), Dec 9, 2004: SKIN. CRACKED. INSPECTION FOUND A .5 INCH CRACK AT LIGHTENING HOLE (2ND ROW FROM TOP) IN C-1 DOOR INNER SKIN. A DOUBLER WAS INSTALLED IAW ECRA 5232-01053.
- [SDR CALA0400724](https://openairdocs.org/sdr/CALA0400724), Nov 21, 2004: SEAT TRACK. CORRODED. INSPECTION FOUND RIGHT O/B SEAT TRACK CORRODED AT STA 328-360. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-00-52.
- [SDR CALA0400723](https://openairdocs.org/sdr/CALA0400723), Nov 21, 2004: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM UPPER CHORD CORRODED AT STA 328, LBL 29 TO RBL 58. THE FLOORBEAM UPPER CHORD WAS REPLACED IAW SRM 53-10-51.
- [SDR CALA0400722](https://openairdocs.org/sdr/CALA0400722), Nov 20, 2004: ANGLE. CORRODED. INSPECTION FOUND R-2 DOOR ZEE ANGLE CORRODED AT STA 907-1006, RBL 0 TO RBL 45. THE ZEE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-02.
- [SDR CALA0400725](https://openairdocs.org/sdr/CALA0400725), Nov 19, 2004: STRINGER. CRACKED. INSPECTION FOUND MULTIPLE CRACKS IN STRINGER 16L AND 16R AT STA 540. THE CRACKS WERE 0.025 INCH LONG. CHANNELS WERE INSTALLED IAW ECRA 5310-03418.
- [SDR CALA0400720](https://openairdocs.org/sdr/CALA0400720), Nov 19, 2004: FITTING. CORRODED. INSPECTION FOUND LT MLG UPLOCK FORWARD SUPPORT FRAME FITTINGS (2 EACH) CORRODED WITH BUSHINGS WORN AT STA 685, S17L. THE LUG FITTING WAS REWORKED TO REMOVE THE 
- [SDR CALA0400718](https://openairdocs.org/sdr/CALA0400718), Nov 18, 2004: SPLICE. CRACKED. INSPECTION FOUND A 0.65 INCH CRACK IN STRINGER 4R SPLICE AT STA 907. THE STRINGER SPLICE WAS REMOVED AND REPLACED IAW SRM 51-10-02.
- [SDR CALA0400717](https://openairdocs.org/sdr/CALA0400717), Nov 18, 2004: SPLICE. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN STRINGER 4L SPLICE AT STA 907. THE STRINGER SPLICE WAS REMOVED AND REPLACED IAW SRM 51-10-02.
- [SDR CALA0400716](https://openairdocs.org/sdr/CALA0400716), Nov 17, 2004: SEAT TRACK. CORRODED. INSPECTION FOUND G-1 GALLEY HOLD DOWN SEAT TRACK CORRODED AT STA 277-294.5 FROM BL 0 TO RBL 43. THE CORRODED SECTION OF TRACK WAS REMOVED AND A NEW SECTION OF T
- [SDR CALA0400714](https://openairdocs.org/sdr/CALA0400714), Nov 11, 2004: CONNECTOR. SHORTED. THE APU DET INOP LIGHT CAME ON WHILE CLIMBING THROUGH FL 180. THE APU FIRE WARNING LIGHT WITH FIRE BELL ACTIVATED WHILE CLIMBING THROUGH FL 330. THE APU FIRE BO
- [SDR CALA0400592](https://openairdocs.org/sdr/CALA0400592), Jul 29, 2004: SKIN. CRACKED. MAINTENANCE FOUND THE FUSELAGE SKIN DENTED AND CRACKED BETWEEN STA 500D + 10 AND 520, S12L. THE CRACK WAS 1.4 INCHES LONG. AN INTERIM REPAIR WAS INSTALLED IAW E
- [SDR CALA0300539](https://openairdocs.org/sdr/CALA0300539), Sep 19, 2003: SKIN. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN NR 1 ENGINE PYLON ACCESS PANEL NR 5727L CUTOUT. A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5430-01230.
- [SDR CALA0300535](https://openairdocs.org/sdr/CALA0300535), Sep 18, 2003: CARGO TRACK. DAMAGED. INSPECTION FOUND IMPACT DAMAGE TO AFT BAGGAGE BIN LT TIE DOWN RAIL AT BS 787. REPLACED TIE DOWN RAIL IAW SRM 53-00-53.
- [SDR CALA0300534](https://openairdocs.org/sdr/CALA0300534), Sep 17, 2003: ATTACH FITTING. CORRODED. INSPECTION FOUND THE RT HORIZONTAL STABILIZER CENTER SECTION FORWARD UPPER LUG CORRODED AT AFT SIDE AROUND BUSHING. AN OVERSIZED BUSHING WAS INSTALLED IAW CMM 5
- [SDR CALA0100381](https://openairdocs.org/sdr/CALA0100381), Apr 16, 2001: FITTING. GOUGED. INSPECTION FOUND RT WING AFT SPAR SPOILER FITTING GOUGED AT WS 133. THE SPOILER FITTING WAS REPLACED IAW ECRA 5750-03517 AND AMS EA 04-5750-0842.
- [SDR CALA0100380](https://openairdocs.org/sdr/CALA0100380), Apr 16, 2001: STIFFENER. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN VERTICAL STIFFENER 18 INCHES ABOVE RT KEEL BEAM AT MAIN WHEEL WELL FORWARD BULKHEAD, STA 663, RBL 6. THE STIFFENER WAS REMOVE
- [SDR CALA0100367](https://openairdocs.org/sdr/CALA0100367), Apr 15, 2001: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM CORRODED ON UPPER SURFACE AROUND SCREW HOLES AT STA 967, RBL 27, LBL 6, AND LBL 27. REPAIR STRAPS AND SHIMS WERE INSTALLED IAW SRM 53
- [SDR CALA0100360](https://openairdocs.org/sdr/CALA0100360), Apr 13, 2001: ATTACH ANGLE. CORRODED. INSPECTION FOUND FORWARD CARGO COMPARTMENT AFT PRESSURE BULKHEAD RT PANEL LOWER ATTACH ANGLE CORRODED AT STA 500D, S26R. THE ATTACH ANGLE WAS REMOVED AND TWO RE
- [SDR CALA0100359](https://openairdocs.org/sdr/CALA0100359), Apr 13, 2001: DOOR FRAME. CRACKED. INSPECTION FOUND A 2.5 INCH CRACK IN AFT CARGO DOOR FORWARD FRAME SPLICE, THROUGH HOLE FOR TENSION PULLEY FOR COUNTER BALANCE MECHANISM, APPROXIMATELY 3.5 INCH 
- [SDR CALA0100358](https://openairdocs.org/sdr/CALA0100358), Apr 13, 2001: INTERCOSTAL. BENT. INSPECTION FOUND INTERCOSTAL IN FORWARD CARGO COMPARTMENT BENT ON UPPER SURFACE AT STA 440-460, S28R. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-40-02.
- [SDR CALA0100357](https://openairdocs.org/sdr/CALA0100357), Apr 13, 2001: ANGLE. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN FLOOR SUPPORT INTERCOSTAL ANGLE AT STA 927-947, BL 0. REMOVED CRACKED ANGLE ON INTERCOSTAL AND A NEW ANGLE WAS INSTALLED IAW 
- [SDR CALA0100356](https://openairdocs.org/sdr/CALA0100356), Apr 13, 2001: FLOOR SUPPORT. CORRODED. INSPECTION FOUND FLOOR SUPPORTS CORRODED AT STA 967-986.5, LBL 18 AND RBL 18. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-40-02.
- [SDR CALA0100350](https://openairdocs.org/sdr/CALA0100350), Apr 12, 2001: WEB. CORRODED. INSPECTION FOUND FORWARD CARGO COMPARTMENT DOOR OPENING LOWER SUPPORT PANEL (SILL WEB) CORRODED AT STA 440-490, S25R. THE SILL WEB WAS REMOVED AND A NEW SILL WE
- [SDR CALA0100349](https://openairdocs.org/sdr/CALA0100349), Apr 12, 2001: PAN. CORRODED. INSPECTION FOUND FLOOR PAN AT STA 1016 TO AFT PRESSURE BULKHEAD CORRODED AT BL 0 TO LBL 48. THE FLOOR PAN WAS REMOVED AND A NEW FLOOR PAN WAS INSTALLED IAW SRM 
- [SDR CALA0100348](https://openairdocs.org/sdr/CALA0100348), Apr 12, 2001: WEB. CORRODED. INSPECTION FOUND FORWARD END OF FLOOR PAN CORRODED AT STA 986.5-1016, RBL 36-48. THE CORRODED FLOOR PAN WEB WAS REMOVED AND A NEW FLOOR PAN WEB WAS INSTALLED IA
- [SDR CALA0100346](https://openairdocs.org/sdr/CALA0100346), Apr 12, 2001: SEAT TRACK. CORRODED. INSPECTION FOUND RIGHT O/B MAIN CABIN SEAT TRACK CORRODED AT STA 540-727. THE CORRODED SECTION OF SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-00-52.
- [SDR CALA0100343](https://openairdocs.org/sdr/CALA0100343), Apr 12, 2001: CHANNEL. CORRODED. INSPECTION FOUND CHANNEL CORRODED AT L-1 DOOR THRESHOLD CUSP WEB, L18L. THE CHANNEL WAS REMOVED AND REPLACED IAW SRM 51-40-02.
- [SDR CALA0100342](https://openairdocs.org/sdr/CALA0100342), Apr 12, 2001: ANGLE. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN FORWARD ENTRYWAY L-ANGLE AT FLOORBEAM AFT FLANGE ATTACH POINT, STA 344, LBL 10. THE L-ANGLE ON TOP OF INTERCOSTAL WAS REMOVE
- [SDR CALA0100341](https://openairdocs.org/sdr/CALA0100341), Apr 12, 2001: FLOOR SUPPORT. CRACKED. INSPECTION FOUND A 3 INCH CRACK IN FORWARD CARGO COMPARTMENT FLOOR SUPPORT AT STA 500 ABOVE S27R. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INST
- [SDR CALA0100340](https://openairdocs.org/sdr/CALA0100340), Apr 12, 2001: RIB. WORN. INSPECTION FOUND RT ELEVATOR CENTER BALANCE HAD WEAR MARKS ON I/B WALL (HOR STAB RIB) AT STA 66.54. THE WORN AREA WAS REMOVED IAW SRM 57-70-10, PARA 4B. FILLER 
- [SDR CALA0100338](https://openairdocs.org/sdr/CALA0100338), Apr 12, 2001: BEARING. FROZEN. INSPECTION FOUND RT MLG SUPPORT BEAM HAD LOOSE BEARING HOUSING AND FROZEN BEARING AT MOUNT FITTING. REMOVED NR 5 FLAP TRACK WITH TRANSMISSION, REMOVED FITTING A
- [SDR CALA0100337](https://openairdocs.org/sdr/CALA0100337), Apr 11, 2001: ANGLE. CORRODED. INSPECTION FOUND R-1 DOOR I/B CHORD O/B L-ANGLE CORRODED ON TOP AND BOTTOM SURFACES AT STA 312, S18R. THE L-ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-02 AND 
- [SDR CALA0100336](https://openairdocs.org/sdr/CALA0100336), Apr 11, 2001: INTERCOSTAL. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN FORWARD ENTRYWAY INTERCOSTAL AT FLOORBEAM ATTACH AREA, STA 312, BL 0. THE INTERCOSTAL WAS REMOVED AND A NEW INTERCOSTAL WAS I
- [SDR CALA0100335](https://openairdocs.org/sdr/CALA0100335), Apr 11, 2001: FLOORBEAM. CORRODED. INSPECTION FOUND UPPER SURFACE OF FLOORBEAM CORRODED AT STA 986.5. THE CORRODED SECTION OF FLOORBEAM T-CAP WAS REMOVED AND A NEW SECTION WAS INSTALLED USING REP
- [SDR CALA0100334](https://openairdocs.org/sdr/CALA0100334), Apr 11, 2001: FRAME. WORN. INSPECTION FOUND RT ENGINE PYLON FORWARD O/B UPPER CHORD WORN. THE CHORD WAS REPAIRED IAW ECRA 5440-01221 AND EA 04-5440-0836.

All 88: https://openairdocs.org/deregistered/N19357-2013-03-21/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 20000321015989I](https://openairdocs.org/incident/20000321015989I), Mar 21, 2000: Boeing 7373TO (N19357), Houston, TX, Minor damage. (-23)Aircraft blew #2 tire ontakeoff from iah at 155 KTS. After landing the pax were taken by bus to the terminal. Aircraft was towed form the runway to a…

## Other aircraft with N19357

- [Cancelled 1988-06-16](https://openairdocs.org/deregistered/N19357-1988-06-16): Boeing 737-73Q, S/N 23839. N-number assigned, not yet registered
- [Cancelled 1975-11-20](https://openairdocs.org/deregistered/N19357-1975-11-20): Cessna 150L, S/N 15074361, built 1973. Exported to Canada. Owner: [G B Dupont Co Inc](https://openairdocs.org/faa-owner/G%20B%20DUPONT%20CO%20INC), [Pontiac, MI](https://openairdocs.org/faa-place/MI/Pontiac)

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