# N925L: 1969 Douglas DC-9-32, registration cancelled 2005-10-19 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: October 19, 2005 - Exported to: Venezuela - Status when cancelled: Valid registration - Airframe: [Douglas DC-9-32](https://openairdocs.org/model/douglas-dc-9-32) (registry code 3022066) - Engine: [Pratt & Whitney JT8D-1](https://openairdocs.org/engine/pratt-whitney-jt8d-1) (registry code 52044) - Data sheets: [TCDS A6WE](https://openairdocs.org/tcds/A6WE), [TCDS E2EA](https://openairdocs.org/tcds/E2EA) (OpenAirDocs) - Serial number: 47357 - Year built: 1969 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard - Certificate issued: September 21, 2004 - Last registry action: September 21, 2004 - Mode S code: ACD1B7 - Owner when cancelled: [Alameda Corp Trustee](https://openairdocs.org/faa-owner/ALAMEDA%20CORP%20TRUSTEE) - Location: [San Antonio, TX](https://openairdocs.org/faa-place/TX/San%20Antonio) - Owner type: Corporation - Owner's area on the map: 29.5387° N, 98.4913° W: Placed by OpenAirDocs at the center of ZIP code 78216, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N925L - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=925L - Page: https://openairdocs.org/deregistered/N925L-2005-10-19 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 Douglas DC-9-32: https://openairdocs.org/model/douglas-dc-9-32.md ## Service difficulty reports (121, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR TWAA0018301](https://openairdocs.org/sdr/TWAA0018301), Nov 22, 2000: SOCKET. CRACKED. AIRCRAFT RETURNED FROM TAXI DUE TO ELECTRICAL SMELL IN AREA OF CABIN ROW 20 AND 21, LEFT SIDE. REPLACED BURNED LIGHT BULB SOCKET AT ROW 20ABC FOR LOWER SIDEWALL - [SDR TWAA0010401](https://openairdocs.org/sdr/TWAA0010401), Jul 3, 2000: BULB. FAILED. THE EMERGENCY LIGHT ABOVE THE AFT FLIGHT ATTENDANT SEAT WAS INOPERATIVE. REPLACED THE BULB. CHECK-C 3-29-00 MCI. ---CLOSED--- - [SDR TWAA0004903](https://openairdocs.org/sdr/TWAA0004903), Mar 22, 2000: FLOOR SUPPORT. CRACKED. DURING OP 16 MAINT CHECK, THE SUPPORT RIBS FOR FLOOR PANEL NUMBER 40 WERE CRACKED. MADE NEW PANEL PER STA SSRM 53-00-104 PAGE 201. - [SDR TWAA0004302](https://openairdocs.org/sdr/TWAA0004302), Mar 14, 2000: FRAME. CRACKED. DURING OP 16 MAINT CHECK, THE VENTRAL STAIRWAY DOOR, LT FRAME O/B OF THE INNER DOOR HANDLE BAR HAD AN 11 INCH CRACK IN THE RADIUS. REMOVED CRACKED FRAME AND FAB - [SDR TWAA0003812](https://openairdocs.org/sdr/TWAA0003812), Mar 1, 2000: BRACKET. CRACKED. DURING OP 16 MAINT CHECK, ON LT WING THE INBD BUTE DOOR ATTACH BRACKET AND REPAIR DOUBLER WERE CRACKED AT AFT END, APPROX 21 INCHES INBD OF INBD FLAP HINGE CAST - [SDR TWAA0003202](https://openairdocs.org/sdr/TWAA0003202), Feb 22, 2000: FLANGE. CRACKED. DURING OP 16 MAINT CHECK, FOUND IN LT WHEEL WELL THE UPPER FLANGE OF THE TRAPEZONDAL PANEL HAD A CRACK BETWEEN NUMBER 6 AND 9 BOLT HOLES. COMPLIED WITH SERVICE - [SDR TWAA0003201](https://openairdocs.org/sdr/TWAA0003201), Feb 22, 2000: FLANGE. CRACKED. DURING OP 16 MAINT CHECK, IN RT WHEEL WELL FOUND UPPER FLANGE OF TRAPEZONDAL PANEL HAD A CRACK BETWEEN NUMBER 7 AND 8 HOLES. COMPLIED WITH SERVICE BULLETIN 53-1 - [SDR TWAA0003014](https://openairdocs.org/sdr/TWAA0003014), Feb 15, 2000: SPAR. CRACKED. DURING OP 16 MAINT CHECK, RT WING HAD APPROX .375 IN CRACK AT LOWER INBD HOLE ON SURFACE OF REAR SPAR AT INBD FLAP HINGE, STA XRS 164. STOP DRILLED CRACKS PER D - [SDR TWAA0003013](https://openairdocs.org/sdr/TWAA0003013), Feb 14, 2000: STRUCTURE. DAMAGED. DURING OP 16 MAINT CHECK, NECESSARY TO REPAIR HOLE DAMAGE IN FUSELAGE AT APPORX STA 608 TO 612, LONGERON 28L TO 28R. COMPLIED WITH ARA 16532. - [SDR TWAA0003012](https://openairdocs.org/sdr/TWAA0003012), Feb 14, 2000: SKIN. CORRODED. DURING OP 16 MAINT CHECK, LOWER FUSELAGE EXISTING REPAIR HAD CORROSION ON FUSELAGE SKIN AFT OF STA 604. REMOVED VISIBLE SURFACE CORROSION PER TWA STD PROCESSES - [SDR TWAA0005810](https://openairdocs.org/sdr/TWAA0005810), Feb 11, 2000: ANGLE. CRACKED. DURING OP 16 MAINT CHECK, THE LT WING FLAP WAS CRACKED IN UPPER SUPPORT ANGLE ON I/B SIDE OF O/B FLAP HINGE CASTING IN FLANGE. CRACKED ANGLE (P/N 9957600-7) WAS - [SDR TWAA0003011](https://openairdocs.org/sdr/TWAA0003011), Feb 11, 2000: LONGERON. CRACKED. DURING OP 16 MAINT CHECK, FUSELAGE STA 579 TO 604 AREA HAD A CRACK IN LONGERON 24L. REPLACED LONGERON 24L PER DAC PRINT 5910068. - [SDR TWAA0002708](https://openairdocs.org/sdr/TWAA0002708), Feb 11, 2000: LONGERON. BROKEN. DURING OP 16 MAINT CHECK, LONGERON 25 LT& RT, LONGERON 29 LT STA 579 TO 604 WAS BROKEN OFF AT THE FWD END. REPLACED LONGERON AT EACH AREA AND INSTALLED PER PRIN - [SDR TWAA0002707](https://openairdocs.org/sdr/TWAA0002707), Feb 10, 2000: SKIN. CORRODED. DURING OP 16 MAINT CHECK, THE LOWER FUSELAGE HAD CORROSION COMING FROM MATING SURFACE OF FUSELAGE SKIN AND LONGERONS AT STA 604 TO 617, AND STRINGER 28L TO 29R. - [SDR TWAA0002613](https://openairdocs.org/sdr/TWAA0002613), Feb 9, 2000: LONGERON. CRACKED. DURING OP 16 MAINT CHECK, THE LOWER FUSELAGE, LONGERON 27L, AT STA 566 TO 585, WAS FOUND CRACKED AT THE FWD END. REPLACED CRACKED FITTING WITH (P/N 3920595-501) - [SDR TWAA0002612](https://openairdocs.org/sdr/TWAA0002612), Feb 9, 2000: CASTING. CRACKED. DURING OP 16 MAINT CHECK, THE RT WING TRAILING EDGE FLAP O/B HINGE CASTING ATTACH FRAME WAS CRACKED AT I/B AND O/B SIDES. REPLACED CRACKED FRAME PER SRM 51-10-0 - [SDR TWAA0002611](https://openairdocs.org/sdr/TWAA0002611), Feb 9, 2000: SKIN. DAMAGED. DURING OP 16 MAINT CHECK, FOUND STATIC BURN ON FUSELAGE SKIN AT STA 294, BETWEEN LONGERON 18L AND 19L. NO CRACK PER NDT HFEC PER 51-00-03 PART 6. BLENDED STATIC - [SDR TWAA0002610](https://openairdocs.org/sdr/TWAA0002610), Feb 9, 2000: SKIN. DAMAGED. DURING OP 16 MAINT CHECK, FOUND STATIC BURN ON FUSELAGE SKIN AT STA 164, LONGERON 25L. NO CRACK PER PART 6, 51-00-03. REPLACED RIVET PER SPM 6-70-01 PAGE 3, AND - [SDR TWAA0002609](https://openairdocs.org/sdr/TWAA0002609), Feb 9, 2000: RIVET. DAMAGED. DURING OP 16 MAINT CHECK, ON RT FWD FUSELAGE FOUND RIVET BURN AT APPROX STA 446, 3.5 IN BELOW LONGERON 18R. NO CRACK PER PART 6, 51-00-03. REPLACED RIVET PER SP - [SDR TWAA0002608](https://openairdocs.org/sdr/TWAA0002608), Feb 9, 2000: RIVET. DAMAGED. DURING OP 16 MAINT CHECK, THE RT FWD FUSELAGE APPROX STA 469 HAD A RIVET BURN 2.75 IN BELOW LONGERON 18R. REPLACED RIVET PER SPM 6-70-01, PAGE 3, SRM 51-30 AND - [SDR TWAA0002406](https://openairdocs.org/sdr/TWAA0002406), Feb 4, 2000: CHANNEL. DAMAGED. DURING OP 16 MAINT CHECK FOUND CABIN AFT VAULT DOOR, WITH TORN METAL U CHANNEL BY RT SIDE OF DOOR JAMB. REPAIRED PER ARA 16326 AND INSTALLED. - [SDR TWAA0002405](https://openairdocs.org/sdr/TWAA0002405), Feb 4, 2000: ANGLE. CRACKED. DURING OP 16 MAINT CHECK FOUND CABIN AFT PRESSURE BULKHEAD DOOR INTERNAL CENTER SUPPORT, FWD T ANGLE CRACKED LT END. REMOVED OLD T ANGLE, MADE NEW ONE AND INSTA - [SDR TWAA0002404](https://openairdocs.org/sdr/TWAA0002404), Feb 4, 2000: SUPPORT. CRACKED. DURING OP 16 MAINT CHECK FOUND AFT CABIN PRESSURE BULKHEAD DOOR INTERNAL CENTER SUPPORT WEB CRACKED, LT END WITH END SECTION MISSING. INSTALLED NEW SUPPORT WEB - [SDR TWAA0002403](https://openairdocs.org/sdr/TWAA0002403), Feb 4, 2000: CASTING. CRACKED. DURING OP 16 MAINT CHECK FOUND AFT CABIN PRESSURE BULKHEAD DOOR INTERNAL LT LOWER TOP CASTING CRACKED AT LOWER LEG. REPLACED WITH NEW CASTING PER SERVICE REWORK - [SDR TWAA0002402](https://openairdocs.org/sdr/TWAA0002402), Feb 3, 2000: FASTENER. LOOSE. DURING OP 16 MAINT CHECK FOUND NUMBER 1 PYLON TOP AFT SKIN HAD 4 ROWS OF BLIND FASTENERS LOOSE AND WORKING. REPLACED UPPER SKIN AND FASTENERS PER DAC DRAWING 99 - [SDR TWAA0002316](https://openairdocs.org/sdr/TWAA0002316), Feb 3, 2000: FASTENER. MISINSTALLED. DURING OP 16 MAINT CHECK ON NUMBER 2 PYLON, TOP OF PYLON SKIN INBD OF AFT ENGINE MOUNT HAD ROW OF SCREWS WITH SKIN WASHERS LOOSE AND IMPROPERLY INSTALLED. REPLA - [SDR TWAA0002315](https://openairdocs.org/sdr/TWAA0002315), Feb 2, 2000: STRUCTURE. CORRODED. DURING OP 16 MAINTENANCE CHECK, ON NUMBER 1 PYLON TOP AND BOTTOM OF PYLON FOR ENG MOUNT YOKE STRUCTURE HAD RUSTY SURFACES AT LE ATTACH. CHECKED MATERIAL THICKNE - [SDR TWAA0002313](https://openairdocs.org/sdr/TWAA0002313), Feb 2, 2000: SKIN. DAMAGED. DURING OP 16 MAINTENANCE, CHECK NECESSARY TO INSTALL UPPER WINDOW BELT STRIP FROM STA 699 TO 756 ON LT SIDE. REINSTALLED WINDOW BELT DOUBLER PER MO 71K21 AND EM - [SDR TWAA0002013](https://openairdocs.org/sdr/TWAA0002013), Jan 31, 2000: FINGER DOUBLER. CORRODED. DURING OP 16 MAINT CHECK, FOUND FUSELAGE CORROSION ON THE LOWER PRESSURE BULKHEAD FINGER DOUBLERS FROM LONGERON 24L TO L24R, STA 604. REPLACED WITH NEW FINGER D - [SDR TWAA0002012](https://openairdocs.org/sdr/TWAA0002012), Jan 31, 2000: TEE. DAMAGED. DURING OP 16 MAINT CHECK, THE LOWER FUSELAGE LOWER BULKHEAD TEE AT STA 604 REQUIRED REPLACEMENT. CLEANED LOWER BULKHEAD TEE AREA STA 604. REPLACED WITH NEW TEE - [SDR TWAA0002011](https://openairdocs.org/sdr/TWAA0002011), Jan 31, 2000: RIB. CRACKED. DURING OP 16 MAINT CHECK THE NUMBER 2 ENG PYLON, OTBD SUPPORT RIB WAS CRACKED AT THE FWD END. REPLACED PART PER DAC INSTALLATION PRINT 9915502 AND INSTALLED RIB - [SDR TWAA0002010](https://openairdocs.org/sdr/TWAA0002010), Jan 31, 2000: WEB. CRACKED. DURING OP 16 MAINT CHECK, NR 2 PYLON HAD A CRACK IN THE WEB 9.5 INCHES OTBD OF THE FUSELAGE SKIN, TOP OF PYLON AT STA 1038. REPLACED PART PER DAC PRINT INSTALLA - [SDR TWAA0002009](https://openairdocs.org/sdr/TWAA0002009), Jan 31, 2000: RIB. CRACKED. DURING OP 16 MAINT CHECK, FOUND NR 2 ENGINE PYLON, INBD RIB WAS CRACKED AT THE FWD END. REPLACED PART PER DAC INSTALLATION PRINT 9915503 AND INSTALLED RIB 99155 - [SDR TWAA0002008](https://openairdocs.org/sdr/TWAA0002008), Jan 26, 2000: KEEL BEAM. CORRODED. DURING OP 16 MAINT CHECK, FOUND FUSELAGE STA 607 TO 667 HAD CORROSION ON THE KEEL BEAM. REMOVED CORROSION PER SRM 6-80-01, PAGE 1. - [SDR TWAA0002312](https://openairdocs.org/sdr/TWAA0002312), Jan 25, 2000: FASTENER. WRONG PART. DURING OP 16 MAINTENANCE CHECK, FOUND SEVERAL CHERRY FASTENERS IN UPSIDE DOWN HAT SECTION FROM STA 606 TO 659 AND BETWEEN KEEL AND STRINGER 29R. RE-INSTALLED MS - [SDR TWAA0002007](https://openairdocs.org/sdr/TWAA0002007), Jan 21, 2000: PANEL. CRACKED. DURING OP 16 MAINT CHECK, FOUND LT MLG WHEEL WELL LT TRAP PANEL AREA, A CRACK HAD MIGRATED BEYOND STOP DRILL AND WAS IN MOUNT BOLT HOLE. CONFIRMED BY HIGH FREQ - [SDR TWAA0001406](https://openairdocs.org/sdr/TWAA0001406), Jan 19, 2000: FLOOR PANEL. CORRODED. DURING OP 16 MAINT CHECK, FOUND CABIN FLOOR PANEL 23 HAD CORROSION. FABRICATED NEW FLOOR PANEL PER SRRM 53-00-104, PAGE 201. - [SDR TWAA0001414](https://openairdocs.org/sdr/TWAA0001414), Jan 18, 2000: SUPPORT. CRACKED. DURING OP 16 MAINT CHECK, FOUND CABIN FLOOR PANEL NUMBER 26, HAD SUPPORT RIB CRACKED. FABRICATED PANEL PER SSRM 53-00-104, PAGE 102. - [SDR TWAA0001413](https://openairdocs.org/sdr/TWAA0001413), Jan 17, 2000: FLOOR PANEL. CORRODED. DURING OP 16 MAINT CHECK, FOUND CABIN FLOOR PANEL MEMBER NUMBER 12 HAD CORROSION ON IT. REF CPCP TASK C46-53306 FWD GALLEY AREA. REMOVED CORROSION PER SPM 51-10 - [SDR TWAA0001412](https://openairdocs.org/sdr/TWAA0001412), Jan 14, 2000: SUPPORT. CRACKED. DURING OP 16 MAINT CHECK, FOUND CABIN FLOOR PANEL 25 SUPPORT RIBS CRACKED. FABRICATED NEW FLOOR PANEL WITH NEW RIBS PER SPM 6-70-01, PAGES 2 AND 3, AND SSRM 53- - [SDR TWAA0001411](https://openairdocs.org/sdr/TWAA0001411), Jan 14, 2000: FLOOR PANEL. CORRODED. DURING OP 16 MAINT CHECK, FOUND CABIN FLOOR PANEL 35 HAD CORROSION. FABRICATED NEW FLOOR PANEL PER SSRM 53-00-104, PAGE 201. - [SDR TWAA0001410](https://openairdocs.org/sdr/TWAA0001410), Jan 14, 2000: SUPPORT. DAMAGED. DURING OP 16 MAINT CHECK, FOUND CABIN FLOOR PANEL 40C SUPPORT RIBS DAMAGED. FABRICATED NEW PANEL PER SSRM 53-00-104, PAGE 201. - [SDR TWAA0001409](https://openairdocs.org/sdr/TWAA0001409), Jan 14, 2000: FLOOR PANEL. CRACKED. DURING OP 16 MAINT CHECK, FOUND CABIN FLOOR PANEL SCREW HOLES CRACKED IN SEVERAL PLACES, PANEL 48. FABRICATED NEW PANEL PER SSRM 53-00-104, PAGE 201. - [SDR TWAA0001408](https://openairdocs.org/sdr/TWAA0001408), Jan 14, 2000: FLOOR PANEL. DAMAGED. DURING OP 16 MAINT CHECK, FOUND CABIN FLOOR PANEL 77, HAD THE END OF THE PANEL BROKEN OUT. FABRICATED NEW PANEL PER SSRM 53-00-104, PAGE 201. - [SDR TWAA0001407](https://openairdocs.org/sdr/TWAA0001407), Jan 14, 2000: FLOOR PANEL. DAMAGED. DURING OP 16 MAINT CHECK, FOUND CABIN FLOOR PANEL 42 HAD BOTTOMSIDE IN CHANNEL. FABRICATED NEW PANEL PER SSRM 53-00-104, PAGE 201.. - [SDR TWAA0001405](https://openairdocs.org/sdr/TWAA0001405), Jan 14, 2000: SUPPORT. CRACKED. DURING OP 16 MAINT CHECK, FOUND FLOOR PANEL 40A SUPPORT RIBS CRACKED. REPLACED SUPPORT RIBS WHILE FABRICATING NEW FLOOR PANEL PER SSRM 53-00-104, PAGE 201. PICK - [SDR TWAA0001009](https://openairdocs.org/sdr/TWAA0001009), Jan 7, 2000: FLOOR PANEL. DAMAGED. DURING OP 16 MAINT CHECK, FOUND CABIN FLOOR PANEL NUMBER 40B WITH FIELD REPAIR. MADE NEW FLOOR PANEL PER TWA SSRM 53-00-104, PAGE 201. - [SDR TWAA0001008](https://openairdocs.org/sdr/TWAA0001008), Jan 6, 2000: FLOOR PANEL. CORRODED. DURING OP 16 MAINT CHECK, PANEL NUMBER 44 HAD GOUGES AT END OF TOP HATS AND CORROSION AT OPPOSITE END. FABRICATED NEW FLOOR PANEL PER SSRM 53-00-104, PAGE 201. - [SDR TWAA0001007](https://openairdocs.org/sdr/TWAA0001007), Jan 6, 2000: FLOOR PANEL. BROKEN. DURING OP 16 MAINT CHECK, NUMBER 21 FLOOR PANEL CORNER WAS BROKEN. FABRICATED NEW PANEL PER SSRM 53-00-14, PAGE 201. - [SDR TWAA0001006](https://openairdocs.org/sdr/TWAA0001006), Jan 6, 2000: FLOOR PANEL. CRACKED. DURING OP 16 MAINT CHECK, FOUND FLOOR PANEL 19 SUPPORT RIBS WERE CRACKED. FABRICATED NEW FLOOR PANEL PER SSRM 53-00-104, PAGE 201.. All 121: https://openairdocs.org/deregistered/N925L-2005-10-19/reports.md ## NTSB investigations (1) From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [NTSB CHI96IA059](https://openairdocs.org/ntsb/CHI96IA059), Dec 19, 1995: Douglas DC-9-32 (N925L), Saint Louis, MO, incident, no damage. Probable cause: loss of induction air into the engine inlets resulting in simultaneous loss of power on both engines. Factors relating to this incident were: disconnection of the airplane's hydraulic pumps and… ## FAA accident and incident reports (2) 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 19951219045689I](https://openairdocs.org/incident/19951219045689I), Dec 19, 1995: Doug DC932 (N925L), St Louis, MO. Narrative: upon landing at stl runway 30L, during thrust reversal the flight crew experienced a power loss to both engines (engines quit). The aircraft came to… - [Incident 19901015053589I](https://openairdocs.org/incident/19901015053589I), Oct 15, 1990: Doug DC932 (N925L), St Louis, MO, Minor damage. Tail compartment high temperature light on. Returned. Had failed v clamp on left augmentation valve bleed air line ## Other aircraft with N925L - [Registered now](https://openairdocs.org/aircraft/N925L): Diamond Aircraft Ind DA 40 NG, S/N 40.NC294, built 2024 --- 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.