# N996Z: 1967 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: 47028
- Year built: 1967
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: August 2, 1967
- Certificate issued: February 7, 2005
- Last registry action: February 7, 2005
- Mode S code: ADEB2C
- 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/N996Z
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=996Z
- Page: https://openairdocs.org/deregistered/N996Z-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 (101, newest 50)

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

- [SDR ZW0A0109401](https://openairdocs.org/sdr/ZW0A0109401), Oct 4, 2001: DOOR. OPEN. AFTER GEAR RETRACTION PILOT NOTED A VIBRATION IN THE NOSE GEAR AREA. CREW ACCOMPLISHED FLY BY FOR VISUAL CHECK OF NOSE AREA, THEN RETURNED TO STL. FOUND LEFT NO
- [SDR TWAA0017408](https://openairdocs.org/sdr/TWAA0017408), Oct 30, 2000: SEAT TRACK. CORRODED. DURING OP 15 MAINT CHECK IN THE COCKPIT, CORROSION WAS FOUND IN FASTENER HOLES UNDER FLOOR PANEL NUMBER 3. REMOVED CORRODED TRACK SECTION. INSTALLED NEW SEAT TR
- [SDR TWAA0017407](https://openairdocs.org/sdr/TWAA0017407), Oct 30, 2000: INTERCOSTAL. CORRODED. DURING OP 15 MAINT CHECK IN THE ELECTRONIC COMPT BETWEEN STA 200 AND 218, BL 0, INTERCOSTAL WAS CORRODED AROUND FASTENER HOLES, LEVEL NUMBER 1. SENT TO SHOP FOR
- [SDR TWAA0017406](https://openairdocs.org/sdr/TWAA0017406), Oct 30, 2000: SKIN. CORRODED. DURING OP 15 MAINT CHECK THE LT FUSELAGE SKIN WAS PILLOWING AT STA 935, BETWEEN LONGERON 22 AND 23L. REPLACED FUSELAGE SKIN FROM STA 784 TO 996, LONGERON 18L TO
- [SDR TWAA0017405](https://openairdocs.org/sdr/TWAA0017405), Oct 30, 2000: PAN. CORRODED. DURING OP 15 MAINT CHECK ON THE AFT CARGO COMPT DOOR, THE FWD LOWER DOOR PAN AT STA 889 TO 937, AND RL 24 TO RL 29, HAD CORROSION. AFT CARGO DOOR ALSO HAD CORRO
- [SDR TWAA0017404](https://openairdocs.org/sdr/TWAA0017404), Oct 27, 2000: FLOORBEAM. CORRODED. DURING OP 15 MAINT CHECK IN THE RT AFT LAVATORY, AT STA 996 THE FLOORBEAM WAS CORRODED, 55 INCHES RBL, UNDER TOP FLANGE. FABRICATED AND INSTALLED REPAIR PER SRM
- [SDR TWAA0017215](https://openairdocs.org/sdr/TWAA0017215), Oct 27, 2000: FLOORBEAM. CORRODED. DURING OP 15 MAINT CHECK AT RT AFT LAV AT STA 996, FLOORBEAM 8 PLACES HAD CORROSION ON TOP FLANGE. REMOVED THE CORROSION PER SPM 6-80-01. FABRICATED AND REPAIRE
- [SDR TWAA0017214](https://openairdocs.org/sdr/TWAA0017214), Oct 27, 2000: ANGLE. CRACKED. DURING OP 15 MAINT CHECK THE AFT PRESSURE BULKHEAD ANGLE WAS CRACKED AT FASTENER TO L/E AND FASTENERS HAD TOOLING MARKS ABOVE LT DOOR JAMB FOR AFT AIRSTAIRS. BU
- [SDR TWAA0017213](https://openairdocs.org/sdr/TWAA0017213), Oct 27, 2000: SKIN. DAMAGED. DURING OP 15 MAINT CHECK FOUND FIELD SKIN REPAIR FWD OF STA 313, RL 24 TO 25. REPAIRED PER SRM 53-04, FIG 38.
- [SDR TWAA0017212](https://openairdocs.org/sdr/TWAA0017212), Oct 26, 2000: INTERCOSTAL. CORRODED. DURING OP 15 MAINT CHECK IN AFT CARGO COMPT FOUND CORROSION ON UNDER SIDE OF RL 29, STA 897 TO 917. REPLACED INTERCOSTAL PER DOUGLAS PRINT 5910158.
- [SDR TWAA0017211](https://openairdocs.org/sdr/TWAA0017211), Oct 26, 2000: LONGERON. CRACKED. DURING OP 15 MAINT CHECK, FOUND LONGERON 17L WAS CRACKED AT STA 945. CRACK CONFIRMED BY NDT. REPLACED CRACKED LONGERON 17L AT STA 945 WITH NEW PER SRM 53-11-3, 
- [SDR TWAA0017210](https://openairdocs.org/sdr/TWAA0017210), Oct 26, 2000: SEAT TRACK. CORRODED. DURING OP 15 MAINT CHECK, FOUND CORROSION ON SEAT TRACK AT STA 200, LBL 22. REPAIRED PER 53-05, PAGE 10L, FIG 4F SHEET 6.
- [SDR TWAA0017209](https://openairdocs.org/sdr/TWAA0017209), Oct 26, 2000: WEB. CRACKED. DURING OP 15 MAINT CHECK IN THE AFT CARGO COMPT FOUND AT STA 889, LBL 45, A WEB CRACKED UNDER CABIN FLOOR TRACK FLANGE BETWEEN TIE BOLT AND RIVET. REPAIRED PER 
- [SDR TWAA0017208](https://openairdocs.org/sdr/TWAA0017208), Oct 25, 2000: FLOOR SUPPORT. CORRODED. DURING OP 15 MAINT CHECK FOUND CORROSION ON FLOOR SUPPORT AT STA 160, RBL 0 TO 53. FABRICATED NEW SUPPORT PER SRM 53-10-1 AND SPM 6-70-01 AND REPLACED. INSTALLE
- [SDR WAA0017207](https://openairdocs.org/sdr/WAA0017207), Oct 25, 2000: WEB. CORRODED. DURING OP 15 MAINT CHECK FOUND MEMBRANE CORRODED BETWEEN TRACKS 3 AND 4, STA 200 TO 218. REMOVED OLD MEMBRANE AND INSTALLED PER 53-01, PAGE 18. MANUFACTURED AND
- [SDR TWAA0017206](https://openairdocs.org/sdr/TWAA0017206), Oct 25, 2000: FLOORBEAM. CORRODED. DURING OP 15 MAINT CHECK AT STA 199, BETWEEN RBL 44 AND RBL 53, THE FLOOR WEB WAS CORRODED, JUST AFT OF SERVICE DOOR. REMOVED OLD MEMBRANE AND INSTALLED PER SRM
- [SDR TWAA0017205](https://openairdocs.org/sdr/TWAA0017205), Oct 25, 2000: FLOORBEAM. CORRODED. DURING OP 15 MAINT CHECK AT STA 180 BETWEEN RBL 44 AND 52, LEVEL ONE CORROSION WAS FOUND ON FLOOR WEB IN 2 LOCATIONS, WHERE FLOOR PANEL RUBBED ON WEB. REMOVED O
- [SDR TWAA0017108](https://openairdocs.org/sdr/TWAA0017108), Oct 25, 2000: WEB. DAMAGED. DURING OP 15 MAINT CHECK, FOUND REPAIR TO FLOOR MEMBRANE NEEDED REPLACEMENT AT STA 205, RBL 0 TO 20. REMOVED OLD MEMBRANE. MANUFACTURED NEW PER 6-70-01. INSTALL
- [SDR TWAA0017107](https://openairdocs.org/sdr/TWAA0017107), Oct 25, 2000: FLOOR SUPPORT. CORRODED. DURING OP 15 MAINT CHECK, FOUND 37 INCHES OF FLOOR SUPPORT CORRODED BETWEEN STA 162 AND 200, RBL 43. REPLACED OLD SUPPORT WITH NEW. MADE PER SPM 6-70-1. INSTALL
- [SDR TWAA0017106](https://openairdocs.org/sdr/TWAA0017106), Oct 25, 2000: FLOOR SUPPORT. CORRODED. DURING OP 15 MAINT CHECK, FOUND 11 INCH LONG SECTION OF FLOOR SUPPORT CORRODED AT STA 200 BETWEEN RBL 44 AND RBL 56, JUST AFT OF SERVICE DOOR. REMOVED OLD SUPPO
- [SDR TWAA0017105](https://openairdocs.org/sdr/TWAA0017105), Oct 25, 2000: FLOOR SUPPORT. CORRODED. DURING OP 15 MAINT CHECK, THE FLOOR SUPPORT WAS CORRODED AT RBL 0 TO 58 STA 200, AND AT BL 0 AT STA 160 TO 237. REMOVED OLD SUPPORTS. MADE NEW SUPPORTS PER SPM 
- [SDR TWAA0017104](https://openairdocs.org/sdr/TWAA0017104), Oct 25, 2000: FLOOR PANEL. CRACKED. DURING OP 15 MAINT CHECK, THE AFT CABIN FLOOR PANEL NUMBER 69 HAD AFT RT CORNER CRACKED AND CORRODED. FABRICATED NEW FLOOR PANEL PER SSRM 53-00-104.
- [SDR TWAA0017103](https://openairdocs.org/sdr/TWAA0017103), Oct 25, 2000: FRAME. CORRODED. DURING OP 15 MAINT CHECK, FOUND CORROSION ON FRAME AT STA 503, BETWEEN LONGERONS 28R TO 28L. REMOVED 2 FOOT SECTION OF FRAME AND INSTALLED NEW SECTION PER SRM 5
- [SDR TWAA0016810](https://openairdocs.org/sdr/TWAA0016810), Oct 23, 2000: SPLICE. CRACKED. DURING OP 15 MAINT CHECK AT STA 555, LONGERON 28L, FOUND A CRACK IN LONGERON SPLICES. INSTALLED NEW SPLICE PER SRM 53-02, FIG 18.
- [SDR TWAA0016809](https://openairdocs.org/sdr/TWAA0016809), Oct 22, 2000: SEAT TRACK. WORN. DURING OP 15 MAINT CHECK, NUMBER 3 CHAIR TRACK HAD WORN AREA AT STA 208 AND CORROSION AT STA 214 AND 233. REMOVED OLD TRACK AND FABRICATED NEW PER SRM 53-05, SP
- [SDR TWAA0016808](https://openairdocs.org/sdr/TWAA0016808), Oct 22, 2000: SEAT TRACK. CORRODED. DURING OP 15 MAINT CHECK, FOUND NUMBER 4 CHAIR TRACK CORRODED ON TOP BETWEEN STA 200 AND 218, RBL 44, 18 INCHES LONG. REMOVED OLD TRACK AND FABRICATED NEW TRACK
- [SDR TWAA0016807](https://openairdocs.org/sdr/TWAA0016807), Oct 22, 2000: SKIN. DENTED. DURING OP 15 MAINT CHECK, FOUND 3 DENTS ON FUSELAGE SKIN AT STA 207, BETWEEN LONGERON 16R AND 18R. DENTS 1 INCH BY 1.5 INCH BY 0.090 DEEP. INSTALLED FLUSH REPAI
- [SDR TWAA0016806](https://openairdocs.org/sdr/TWAA0016806), Oct 20, 2000: FRAME. CRACKED. DURING OP 15 MAINT CHECK, FORMER REPAIR WAS CRACKED APPROX 2.5 INCH LONG, APPROX 3 INCHES UNDER RL 14, STA 980. REWORKED WITH MO 72J15. REMOVED CRACKED FORMER R
- [SDR TWAA0017403](https://openairdocs.org/sdr/TWAA0017403), Oct 19, 2000: FLOOR PANEL. CORRODED. DURING OP 15 MAINT CHECK IN THE FWD CABIN, THE FLOOR MEMBRANE HAD CORRODED AND WORN AT STA 160 TO 200, LBL 44 INCHES. REMOVED MEMBRANE AND FABRICATED NEW PART P
- [SDR TWAA0016412](https://openairdocs.org/sdr/TWAA0016412), Oct 19, 2000: WEB. CORRODED. DURING OP 15 MAINT CHECK THE FWD CABIN FLOOR MEMBRANE WAS CORRODED AND WORN AT STA 200 TO STA 160, LBL 44 TO LBL 56. REMOVED MEMBRANE AND FABRICATED NEW PART PE
- [SDR TWAA0016411](https://openairdocs.org/sdr/TWAA0016411), Oct 19, 2000: WEB. CRACKED. DURING OP 15 MAINT CHECK THE FWD CABIN FLOOR MEMBRANE WAS CORRODED THROUGH AND CRACKED AT STA 160, LBL 2. REMOVED AND REPLACED PART PER DRAWING 9910078. INSTALL
- [SDR TWAA0016410](https://openairdocs.org/sdr/TWAA0016410), Oct 19, 2000: FLOOR SUPPORT. CORRODED. DURING OP 15 MAINT CHECK IN THE FWD CABIN CORROSION WAS FOUND ON THE FLOOR SUPPORT AT STA 218, LBL 0 TO LBL 44. REMOVED FLOOR SUPPORT. FABRICATED NEW PART PER D
- [SDR TWAA0016409](https://openairdocs.org/sdr/TWAA0016409), Oct 19, 2000: FLOOR SUPPORT. CORRODED. DURING OP 15 MAINT CHECK IN THE FWD CABIN, THE FLOOR SUPPORT WAS CORRODED AT STA 200 TO 237, LBL 14. REMOVED AND REPLACED FLOOR SUPPORT PER DRAWING 9910078. INS
- [SDR TWAA0016408](https://openairdocs.org/sdr/TWAA0016408), Oct 19, 2000: FLOOR SUPPORT. CORRODED. DURING OP 15 MAINT CHECK IN THE FWD CABIN THE FLOOR SUPPORT AT STA 160 TO 200, AT LBL 56, HAD CORROSION. REMOVED AND REPLACED FLOOR SUPPORT PER DRAWING 9910078.
- [SDR TWAA0016407](https://openairdocs.org/sdr/TWAA0016407), Oct 19, 2000: FLOOR SUPPORT. CORRODED. DURING OP 15 MAINT CHECK IN THE FWD CABIN THE FLOOR SUPPORT AT STA 160 TO 200, LBL 44, WAS CORRODED. REMOVED FLOOR SUPPORT. FABRICATED NEW PART PER DRAWING 9910
- [SDR TWAA0016406](https://openairdocs.org/sdr/TWAA0016406), Oct 19, 2000: FRAME. CORRODED. DURING OP 15 MAINT CHECK, THE FRAME AT THE LAST LT WINDOW, AFT SIDE OF WINDOW CUT AT STA 918 TO 935 HAD CORROSION ON THE FLOOR WEB TO FUSELAGE SKIN. CUT OUT COR
- [SDR TWAA0017402](https://openairdocs.org/sdr/TWAA0017402), Oct 18, 2000: SKIN. CORRODED. DURING OP 15 MAINT CHECK ON THE AFT FUSELAGE, LONGERON 20L TO 21L, STA 965, THE TOP AFT CORNER OF THE PRESSURE OUTFLOW CONTROL VALVE CUTOUT HAD CORROSION, 4 INC
- [SDR TWAA0016405](https://openairdocs.org/sdr/TWAA0016405), Oct 18, 2000: MEMBRANE. CRACKED. DURING OP 15 MAINT CHECK, THE MEMBRANE WAS CRACKED AT STA 892, RT SIDE. INSTALLED NEW MEMBRANE PER SRM 51-01 AND SRM 51-30-02.
- [SDR TWAA0016404](https://openairdocs.org/sdr/TWAA0016404), Oct 17, 2000: SKIN. BROKEN. DURING OP 15 MAINT CHECK, THE TOP AFT CORNER OF THE LEFT LAV CUTOUT WAS FOUND WITH AN EXISTING REPAIR THAT WAS LOOSE AND THE AFT CORNER OF MATERIAL ON THE LIP W
- [SDR TWAA0016205](https://openairdocs.org/sdr/TWAA0016205), Oct 16, 2000: CLIP. BROKEN. DURING OP 15 MAINT CHECK, THE TOP FWD CORNER OF THE LAVATORY SERVICE PORT CUTOUT HAD A CLIP BROKEN OFF APPROXIMATELY .75 INCH LONG. FABRICATED NEW DOUBLER AND I
- [SDR TWAA0016109](https://openairdocs.org/sdr/TWAA0016109), Oct 16, 2000: FINGER DOUBLER. CRACKED. DURING OP 15 MAINT CHECK, THE FINGER DOUBLER WAS CRACKED OUT AT LONGERON 26L, STA 784 TO 813. FABRICATED NEW FINGER DOUBLER FROM STA 784 TO 813, LONGERON 26L PE
- [SDR TWAA0016110](https://openairdocs.org/sdr/TWAA0016110), Oct 16, 2000: DOUBLER. CORRODED. DURING OP 15 MAINT CHECK FOUND INTERNAL DOUBLER DAMAGED AND CORRODED AT STA 870 TO 996, LONGERON 18 TO 23L. FABRICATED NEW DOUBLER AND INSTALLED PER DRAWING 591
- [SDR TWAA0016108](https://openairdocs.org/sdr/TWAA0016108), Oct 16, 2000: SKIN. CORRODED. DURING OP 15 MAINT CHECK, FOUND STA 965 BETWEEN LONGERON 19L AND 20L, THE AFT CORNER OF THE LAV SERVICE PORT HAD 3 IN BY 4 IN AREA OF CORNER BULGING OUT WITH RI
- [SDR TWAA0016107](https://openairdocs.org/sdr/TWAA0016107), Oct 16, 2000: ACCESS PANEL. CORRODED. DURING OP 15 MAINT CHECK, FOUND THE AFT LAVATORY SERVICE PANEL LT FUSELAGE LOWER FWD CORNER OF THE CUT OUT INTERIOR OF EXTERIOR DOOR COVER HAD CORROSION AND MET
- [SDR TWAA0016012](https://openairdocs.org/sdr/TWAA0016012), Oct 11, 2000: ANGLE. CHAFED. DURING OP 15 MAINT CHECK, FWD OF RT WHEEL WELL, FILLET FAIRING ATTACH ANGLE WAS WORN AND CHAFED WITH HEAVY PITTING. INSTALLED ANGLE REPAIR DOUBLERS PER SRM 53-0
- [SDR TWAA0016011](https://openairdocs.org/sdr/TWAA0016011), Oct 10, 2000: SKIN. CORRODED. DURING OP 15 MAINT CHECK, FOUND CORROSION ON SKIN UNDER DOOR PAN AT STA 936, RBL 13 INCHES. REMOVED CORROSION ON SKIN UNDER DOOR PAN AT STA 936, RBL 13 INCHES, 
- [SDR TWAA0016010](https://openairdocs.org/sdr/TWAA0016010), Oct 5, 2000: FINGER DOUBLER. MISINSTALLED. DURING OP 15 MAINT CHECK, FOUND INTERCOSTAL FINGER DOUBLERS NOT PROPERLY INSTALLED AT STA 965, BETWEEN LONGERON 13R AND 14R. INSTALLED NEW FINGER DOUBLER OF 0.0
- [SDR TWAA0016009](https://openairdocs.org/sdr/TWAA0016009), Oct 5, 2000: WEB. CORRODED. DURING OP 15 MAINT CHECK, FOUND FLOOR MEMBRANE CORRODED 8 INCHES INBD OF FWD GALLEY DRAIN PAN STA 152, AS SEEN FROM E AND E COMPT. CUT OUT CORRODED SECTION OF M
- [SDR TWAA0016005](https://openairdocs.org/sdr/TWAA0016005), Oct 5, 2000: LONGERON. CRACKED. DURING OP 15 MAINT CHECK, FOUND LONGERON CRACKED AT STA 586, LONGERON 25R. REPLACED PART AND FASTENERS PER SRM 51-30-01 AND SPM 6-70-01.
- [SDR TWAA0016008](https://openairdocs.org/sdr/TWAA0016008), Oct 4, 2000: FLOOR SUPPORT. CORRODED. DURING OP 15 MAINT CHECK FOUND FLOOR SUPPORT CORRODED AT STA 148 TO 160, RBL 34 INCHES. MADE AND INSTALLED NEW FLOOR SUPPORT PER SPM 6-70-01 PAGE 3. INSTALLED F

All 101: https://openairdocs.org/deregistered/N996Z-2005-10-19/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 19891002055089I](https://openairdocs.org/incident/19891002055089I), Oct 2, 1989: Doug DC932 (N996Z), St Louis, MO. Unsafe light on left gear extension. Appreared down. Landed safely. Down lock switch defective.
- [Incident 19860621034099I](https://openairdocs.org/incident/19860621034099I), Jun 21, 1986: Doug DC932 (N996Z), St Louis, MO. At takeoff,the tail over temperature warning light came on. Returned and found a hole in air conditioning mix line.
- [Incident 19850825045179I](https://openairdocs.org/incident/19850825045179I), Aug 25, 1985: Doug DC931 (N996Z), Des Moines, IA. Engine shutdown and aircraft diverted due to rising oil temperature. Fuel heat valve stuck full open.

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