# N14209: Boeing 737-130, registration cancelled 1999-03-11

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: March 11, 1999
- Status when cancelled: Triennial form not returned
- Airframe: [Boeing 737-130](https://openairdocs.org/model/boeing-737-130) (registry code 1384435)
- Data sheets: [TCDS A16WE](https://openairdocs.org/tcds/A16WE) (OpenAirDocs)
- Serial number: 19026
- Type of aircraft: Fixed wing multi engine
- Certificate issued: August 8, 1989
- Last registry action: July 17, 1996
- Mode S code: A0AC98
- 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: 29.7533° N, 95.4129° W: Placed by OpenAirDocs at the center of ZIP code 77019, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N14209
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=14209
- Page: https://openairdocs.org/deregistered/N14209-1999-03-11

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 737-130: https://openairdocs.org/model/boeing-737-130.md

## Service difficulty reports (45)

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

- [SDR CALA9801171](https://openairdocs.org/sdr/CALA9801171), Jun 25, 1998: ENGINE. MALFUNCTIONED. THE NR 1 ENGINE LOST POWER DURING CLIMB-OUT OF EWR AT 1800 FEET. THE ENGINE WENT TO IDLE POWER. THE NR 1 ENGINE WAS SHUT DOWN PER FLIGHT MANUAL AND THE AIRCRAFT
- [SDR CALA9800660](https://openairdocs.org/sdr/CALA9800660), Mar 4, 1998: SKIN. CRACKED. INSPECTION FOUND AN 8 INCH CRACK IN LT FUSELAGE SKIN AT STA 262-274, STRINGER 9L. THE CRACKED AREA OF SKIN WAS CUT OUT. REPAIR DOUBLERS AND FILLERS WERE FABRICA
- [SDR CALA9700648](https://openairdocs.org/sdr/CALA9700648), Apr 22, 1997: SKIN. DENTED. INSPECTION FOUND FUSELAGE SKIN DENTED AT UPPER EDGE OF BULKHEAD STA 178. THE DENTED AREA WAS REMOVED, A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-1
- [SDR CALA9700647](https://openairdocs.org/sdr/CALA9700647), Apr 22, 1997: SKIN. LIGHTNING STRIKE. INSPECTION FOUND A LIGHTNING BURN AT FASTENER HEAD FOURTEEN INCHES AFT OF R-1 DOOR, STRINGER 9L. THE DAMAGED AREA WAS CUT OUT, A REPAIR WAS FABRICATED AND INSTA
- [SDR CALA9700646](https://openairdocs.org/sdr/CALA9700646), Apr 21, 1997: SKIN. CRACK. INSPECTION FOUND A .0937 INCH CRACK AND CORROSION IN FUSELAGE SKIN AT STA 312, STRINGER 26L. THE CORRODED AREA WAS CUT OUT, A DOUBLER REPAIR WAS FABRICATED AND 
- [SDR CALA9700644](https://openairdocs.org/sdr/CALA9700644), Apr 20, 1997: SKIN. CRACKED. INSPECTION FOUND A .125 INCH CRACK IN LT WING LEADING EDGE SKIN AT LE STA 219.67. THE CRACKED AREA WAS CUT OUT, A DOUBLER WAS FABRICATED AND INSTALLED IAW ECRA 
- [SDR CALA9700645](https://openairdocs.org/sdr/CALA9700645), Apr 18, 1997: BRACKET. CRACKED. INSPECTION FOUND A 1 INCH CRACK AT UPPER ATTACH BRACKET OF R-1 DOOR WEB. THE BRACKET WAS REMOVED AND A NEW BRACKET WAS FABRICATED AND INSTALLED IAW SRM 51-40-3.
- [SDR CALA9700651](https://openairdocs.org/sdr/CALA9700651), Apr 17, 1997: CLIP. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN FUSELAGE CLIP TIE AT STA 300, STRINGER 29L. THE CLIP WAS REMOVED, A NEW CLIP WAS FABRICATED AND INSTALLED IAW SRM 51-10-1.
- [SDR CALA9700649](https://openairdocs.org/sdr/CALA9700649), Apr 16, 1997: STRINGER. CRACKED. INSPECTION FOUND A 1 INCH CRACK AT FORWARD FASTENER HOLE OF STRINGER 23L AND FAIL SAFE CHORD WAS BULGED AT BS 727. A STRINGER CLIP WAS FABRICATED AND INSTALLED 
- [SDR CALA9700650](https://openairdocs.org/sdr/CALA9700650), Apr 15, 1997: HINGE. CRACKED. INSPECTION FOUND A 1.5 INCH CRACK IN LT WING NR 3 SPOILER INBOARD HINGE. THE HINGE WAS REMOVED, A NEW HINGE WAS FABRICATED AND INSTALLED IAW SRM 51-30-2.
- [SDR CAL960370](https://openairdocs.org/sdr/CAL960370), Mar 15, 1996: LIGHT. INOPERATIVE. GSO - INSPECTION FOUND LT OVERWING EMERGENCY LIGHT INOPERATIVE. THE LT OVERWING EMERGENCY LIGHT ASSY REMOVED AND REPLACED. (X)
- [SDR CAL960368](https://openairdocs.org/sdr/CAL960368), Mar 13, 1996: ANGLE. CORRODED. GSO - INSPECTION FOUND SUPPORT ANGLE CORRODED AT LT SLIDING WINDOW, STA 248.7. THE CORRODED SECTION OF ANGLE WAS CUT OUT IAW SRM 51-40-4. REPAIR ANGLES WERE FAB
- [SDR CAL960353](https://openairdocs.org/sdr/CAL960353), Mar 13, 1996: TAB HINGE FTG. CRACKED. GSO - INSPECTION FOUND LT WING NR 3 AILERON HINGE FITTING CRACKED AT TAB ATTACH POINT. THE CRACK LENGTH WAS NOT IDENTIFIED. THE HINGE ASSY WAS REMOVED AND REPLA
- [SDR CAL960351](https://openairdocs.org/sdr/CAL960351), Mar 12, 1996: SKIN. BUCKLED. GSO - INSPECTION FOUND FUSELAGE SKIN LAP BUCKLED AND A .25 INCH CRACK IN STR 20L, STA 767 TO STA 804. THE EFFECTED SECTION OF SKIN AND STRINGER WERE REMOVED. A 
- [SDR CAL960350](https://openairdocs.org/sdr/CAL960350), Mar 12, 1996: SLAT. DELAMINATED. GSO - INSPECTION FOUND THE OUTBOARD END OF NR 5 SLAT TOP SURFACE DELAMINATED IN AN AREA APPROXIMATELY 10 INCHES SQUARE. THE DELAMINATED SKIN AND CORE WERE REMOV
- [SDR CAL960366](https://openairdocs.org/sdr/CAL960366), Mar 8, 1996: SKIN. CORRODED. GSO - INSPECTION FOUND SKIN AND CHORD CORROSION AT FORWARD RT CORNER OF E AND E BAY DOORWAY CUT-OUT. THE CORRODED SECTION OF SKIN AND CHORD WERE REMOVED IAW SRM
- [SDR CAL960359](https://openairdocs.org/sdr/CAL960359), Mar 8, 1996: DOOR FRAME. CRACKED. GSO - INSPECTION FOUND A 1.25 INCH CRACK IN UPPER SECTION OF FORWARD R-2 DOORWAY FRAME AT STR 10R. THE FRAME SEGMENT WAS REMOVED AND REPLACED IAW SRM 51-30-2 AN
- [SDR CAL960358](https://openairdocs.org/sdr/CAL960358), Mar 8, 1996: SKIN. CRACKED. GSO - INSPECTION FOUND A 1 INCH CRACK IN SKIN AT FORWARD LOWER CORNER OF R-2 DOORWAY CUT-OUT. THE CRACK WAS CUT OUT. A DOUBLER, TRIPLER, AND FILLER REPAIR WAS F
- [SDR CAL960356](https://openairdocs.org/sdr/CAL960356), Mar 8, 1996: WEB. CRACKED. GSO - INSPECTION FOUND A 1 INCH CRACK IN WEB SECTION AT FORWARD R-2 TORQUE BOX UPPER HINGE ARM. THE CRACK WAS CUT OUT IAW SRM 51-40-2. A NEW WEB WAS FABRICATED 
- [SDR CAL960342](https://openairdocs.org/sdr/CAL960342), Mar 8, 1996: SPOILER. BULGED. GSO - INSPECTION FOUND THE NR 3 SPOILER UPPER SURFACE BULGED. THE SPOILER SKIN WAS RETURNED TO ORIGINAL CONTOUR BY FORMING IAW SRM 51-40-1. (X)
- [SDR CAL960339](https://openairdocs.org/sdr/CAL960339), Mar 8, 1996: SKIN. DENTED. GSO - THE FORWARD LOWER CORNER OF FORWARD CARGO DOOR SKIN FOUND DENTED AND SCRATCHED. THE DAMAGED SKIN REMOVED OVER AN AREA OF APPROXIMATELY 6 INCHES IN DIAMETE
- [SDR CAL960355](https://openairdocs.org/sdr/CAL960355), Mar 6, 1996: SKIN. DELAMINATED. GSO - INSPECTION FOUND NR 2 SPOILER SKIN INBOARD LOWER SURFACE DELAMINATED OVER AN AREA OF APPROXIMATELY 10 INCHES BY 8 INCHES. THE DELAMINATED AREA WAS REMOVED
- [SDR CAL960354](https://openairdocs.org/sdr/CAL960354), Mar 6, 1996: SKIN. GOUGED. GSO - INSPECTION FOUND A GOUGE APPROXIMATELY 10 INCHES SQUARE IN TOP SURFACE OF LT WING INBOARD FOREFLAP. REMOVED GOUGED AREA AND POTTED CORE. REPAIRED WITH FIB
- [SDR CAL960367](https://openairdocs.org/sdr/CAL960367), Mar 5, 1996: SKIN. CORRODED. GSO - INSPECTION FOUND SKIN CORROSION AT FORWARD LT CORNER OF E AND E BAY DOORWAY CUT-OUT. THE CORROSION WAS REMOVED AND A T-CHORD SECTION WAS CUT OUT IAW SRM 5
- [SDR CAL960362](https://openairdocs.org/sdr/CAL960362), Mar 5, 1996: WEB. GOUGED. GSO - INSPECTION FOUND A 1 INCH LONG GOUGE IN WEB OF E AND E COMPARTMENT AT LT SIDE OF DOORWAY CUT-OUT. THE WEB WAS REMOVED. A NEW WEB WAS FABRICATED AND INSTAL
- [SDR CAL960348](https://openairdocs.org/sdr/CAL960348), Mar 5, 1996: FRAME. CRACKED. GSO - INSPECTION FOUND A 1 INCH CRACK IN FRAME AT STA 440 ABOVE STR 21L. A NEW FRAME AND CLIP WERE FABRICATED AND INSTALLED IAW BOEING DRAWING 65C25113 AND SRM 
- [SDR CAL960347](https://openairdocs.org/sdr/CAL960347), Mar 5, 1996: SHEAR TIE. CRACKED. GSO - INSPECTION FOUND A .50 INCH CRACK IN SHEAR TIE AT STA 440, BL ZERO. THE CRACKED SECTION SHEAR TIE WAS CUT OFF IAW SRM 53-10-4. AN ANGLE AND FILLER REPAIR 
- [SDR CAL960346](https://openairdocs.org/sdr/CAL960346), Mar 5, 1996: DOUBLER. CRACKED. GSO - INSPECTION FOUND .25 INCH CRACKS IN SEVERAL AREAS OF DOUBLER FOR EXTERNAL POWER RECEPTACLE. THE DOUBLER WAS REMOVED IAW SRM 51-30-2. THE CORROSION WAS REM
- [SDR CAL960345](https://openairdocs.org/sdr/CAL960345), Mar 5, 1996: FLOOR BEAM. CORRODED. GSO - INSPECTION FOUND FLOOR BEAM UPPER CAP CORRODED AT STA 328, RBL 45 TO RBL 65. THE FLOOR BEAM UPPER CAP WAS REMOVED IAW SRM 53-10-9. A NEW CAP AND SPLICE AN
- [SDR CAL960340](https://openairdocs.org/sdr/CAL960340), Mar 5, 1996: INTERCOSTAL. CORRODED. GSO - INSPECTION FOUND INTERCOSTAL CORRODED IN AFT CARGO COMPARTMENT AT FS 870 - FS 887, STR 20R TO STR 21R. THE INTERCOSTAL WAS REMOVED IAW SRM 51-30-2, A NEW 
- [SDR CAL960341](https://openairdocs.org/sdr/CAL960341), Mar 1, 1996: PANEL. CORRODED. GSO - INSPECTION FOUND NOSE WHEELWELL UPPER FORWARD PANEL CORRODED. THE PANEL WAS REPAIRED IAW E.A. 5310-02452. (X)
- [SDR CAL960365](https://openairdocs.org/sdr/CAL960365), Feb 29, 1996: FRAME. CRACKED. GSO - INSPECTION FOUND THE LT LOWER FRAME IN FORWARD PIT STA 480 CRACKED TWO PLACES AT NUTPLATE LOCATIONS FOR CARGO LINER. THE CRACK LENGTHS WERE NOT IDENTIFIED
- [SDR CAL960364](https://openairdocs.org/sdr/CAL960364), Feb 29, 1996: FLOOR BEAM. CORRODED. GSO - INSPECTION FOUND FLOOR BEAM AND WEB CORRODED IN COCKPIT UNDER CAPTAIN'S SEAT. THE AREA WAS REPAIRED IAW SRM 51-40-2 AND ECRA 5310-03239. (X)
- [SDR CAL960357](https://openairdocs.org/sdr/CAL960357), Feb 29, 1996: STRINGER. CRACKED. GSO - INSPECTION FOUND TWO EACH .25 INCH CRACKS AT FASTENER HOLES OF STR 23R, STA 360 TO STA 440. THE STRINGER WAS REMOVED AND REPLACED IAW SRM 51-30-2. (X)
- [SDR CAL960349](https://openairdocs.org/sdr/CAL960349), Feb 29, 1996: FRAME. CRACKED. GSO - INSPECTION FOUND LEFT LOWER FRAME IN FORWARD PIT, STA 460, CRACKED AT NUTPLATES FOR CARGO LINER. THE CRACK LENGTHS WERE NOT IDENTIFIED. THE FRAME WAS REPA
- [SDR CAL960361](https://openairdocs.org/sdr/CAL960361), Feb 26, 1996: STRINGER. CORRODED. GSO - INSPECTION FOUND STR 24R IN FORWARD PIT CORRODED AT STA 478. THE STRINGER WAS REMOVED AND REPLACED IAW SRM 51-30-2 AND BOEING DRAWING 65-45768. (X)
- [SDR CAL960352](https://openairdocs.org/sdr/CAL960352), Feb 26, 1996: ACT FITTING. CRACKED. GSO - INSPECTION FOUND A 1 INCH CRACK AT ROD ATTACH POINT OF NR 5 SPOILER INBOARD ACTUATOR FITTING. THE FITTING WAS REMOVED AND REPLACED IAW SRM 51-30-2. (X)
- [SDR CAL960343](https://openairdocs.org/sdr/CAL960343), Feb 21, 1996: SKIN. CRACKED. GSO - INSPECTION FOUND CRACKS AROUND FASTENERS IN LT EXTERNAL SKIN AT BS 188 TO BS 251, WL 207 THROUGH WL 234. THE CRACK LENGTHS WERE NOT IDENTIFIED, BUT THE RE
- [SDR CAL960344](https://openairdocs.org/sdr/CAL960344), Feb 18, 1996: FRAME. CRACKED. GSO - INSPECTION FOUND A DENT AND .50 INCH CRACK IN FORWARD PIT BELT FRAME AT STA 400, STR 23L TO STR 25L. THE FRAME WAS REPAIRED BY FABRICATING AND INSTALLING 
- [SDR CAL960363](https://openairdocs.org/sdr/CAL960363), Feb 17, 1996: SKIN. CORRODED. GSO - INSPECTION FOUND SKIN CORRODED AT STA 295 TO STA 340, STR 18R TO STR 19R. THE CORRODED SKIN WAS REMOVED. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53
- [SDR CAL960360](https://openairdocs.org/sdr/CAL960360), Feb 17, 1996: STRINGER. CRACKED. GSO - INSPECTION FOUND A .50 INCH CRACK IN RT WING STR 13 AT WBL 92.5. REPAIR ANGLES AND SPLICES WERE FABRICATED AND INSTALLED IAW BOEING DRAWING 65C34533 AFTER
- [SDR CAL960369](https://openairdocs.org/sdr/CAL960369), Feb 16, 1996: BEAR STRAP. CRACKED. GSO - INSPECTION FOUND A .3750 INCH CRACK IN BEAR STRAP AT C-1 DOOR CUT-OUT, LOWER AFT CORNER. THE SKIN WAS REPLACED AND A DOUBLER INSTALLED IAW ECRA 5330-02366
- [SDR CAL950537](https://openairdocs.org/sdr/CAL950537), Jun 13, 1995: CHORD. CRACKED. STA 31J - INSPECTION FOUND A 14 INCH CRACK IN THE LEFT MLG WHEEL WELL AFT BULKHEAD LOWER CIRCUMFERENTIAL ANGLE (PREVIOUSLY STOP DRILLED). THE CHORD WAS REPLACED
- [SDR CAL950423](https://openairdocs.org/sdr/CAL950423), May 21, 1995: CARRIAGE SPINDLE. SHEARED. IAH - INSPECTION FOUND THE RIGHT OUTBOARD FLAP OUTBOARD CARRIAGE SPINDLE SHEARED AT FORWARD RETAINING NUT. THE CARRIAGE ASSEMBLY WAS REMOVED AND REPLACED AND OP
- [SDR CAL950137](https://openairdocs.org/sdr/CAL950137), Feb 18, 1995: HYD LINE. LEAKING. CLE - FLT 1475 - THE A-SYSTEM HYDRAULIC FLUID QUANTITY BEGAN TO DECREASE AFTER TAKEOFF FROM CLE. THE AIRCRAFT WAS RETURNED TO CLE WHERE IT LANDED WITHOUT INCIDE

## 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 19980625023199I](https://openairdocs.org/incident/19980625023199I), Jun 25, 1998: Boeing 737130 (N14209), Newark, NJ. Loss of powr and subsequent engine shutdown due to contained turbine blade failure.

## Other aircraft with N14209

- [Cancelled 1972-04-03](https://openairdocs.org/deregistered/N14209-1972-04-03): Piper PA-23-250, S/N 27-4769, built 1971. Exported to South Africa. Owner: [Floair Inc](https://openairdocs.org/faa-owner/FLOAIR%20INC), [Wichita, KS](https://openairdocs.org/faa-place/KS/Wichita)
- [Cancelled 1948-04-12](https://openairdocs.org/deregistered/N14209-1948-04-12): Robertson ROBERTSON 1A GLIDER, S/N PS-4, built 1934. Owner: [Kuster Victor](https://openairdocs.org/faa-owner/KUSTER%20VICTOR), [Corona, CA](https://openairdocs.org/faa-place/CA/Corona)

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