# N805AT: 1969 Douglas DC-9-32, registration cancelled 2003-05-02 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: May 2, 2003 - 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: 47378 - Year built: 1969 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: June 19, 1969 - Certificate issued: January 12, 2000 - Last registry action: November 13, 2002 - Mode S code: AAF482 - Owner when cancelled: [Wells Fargo Bank Northwest Na Trustee](https://openairdocs.org/faa-owner/WELLS%20FARGO%20BANK%20NORTHWEST%20NA%20TRUSTEE) - Location: [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City) - Owner type: Corporation - Owner's area on the map: 40.7558° N, 111.8843° W: Placed by OpenAirDocs at the center of ZIP code 84111, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N805AT - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=805AT - Page: https://openairdocs.org/deregistered/N805AT-2003-05-02 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 (34) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR AT0100216](https://openairdocs.org/sdr/AT0100216), Jul 20, 2001: BATTERY PACK. INOPERATIVE. FOUND EMERGENCY LIGHTS AT ROWS 18 AND 22 FAILED TEST. CORRECTIVE ACTION: REPLACED BATTERIES IN BATTERY PACK B5-26. IAW DC9 MM 33-50 - [SDR AT0000431](https://openairdocs.org/sdr/AT0000431), Sep 6, 2000: SKIN. DENTED. FOUND DENT AT BS 484. CUT OUT DENTED AREA, FABRICATED REPAIR FILLER, INTERNAL DOUBLER, AND INSTALLED IAW DC9 SRM 53-04 FIGURE 12C. - [SDR AT0000494](https://openairdocs.org/sdr/AT0000494), Aug 30, 2000: SKIN. CRACKED. FOUND 2 EA CRACKS IN FUSELAGE UPPER NOSE SKIN. CUT OUT CRACKED AREA AND INSTALLED REPAIR DOUBLERS. IAW EO 12-5330-29-B1048, AD 96-11-11, SB 53-262AND DC9 SRM 53 - [SDR AT0000434](https://openairdocs.org/sdr/AT0000434), Aug 30, 2000: ANGLE. CORRODED. FOUND CORROSION AT BS 120 ON LONGERON 28R AND BS 130 LONGERON 28 AT BAY DOOR LOCKING INDICATOR. REMOVED 1 T-ANGLE, 1 SUPPORT, FABRICATED NEW SUPPORT AND INSTALL - [SDR AT0000426](https://openairdocs.org/sdr/AT0000426), Aug 29, 2000: SKIN. CRACKED. FOUND FORWARD ENTRY DOOR JAMB AFT SIDE AT THE DOOR STOP IS CRACKED. INSTALLED REPAIR IAW EO 09-5310-29-E1475 AND SRO 9530252. - [SDR AT0000430](https://openairdocs.org/sdr/AT0000430), Aug 27, 2000: FLOORBEAM. CORRODED. FOUND CORROSION ON EPC PANEL FRAME AT FLOOR SUPPORT. REMOVED FRAME AND FLOOR SUPPORT, FABRICATED NEW REPAIR AND INSTALLED IAW DC9 SRM 51-10-2, 51-30-1, 52-61-0. - [SDR AT0000429](https://openairdocs.org/sdr/AT0000429), Aug 25, 2000: FLOOR PANEL. CORRODED. FOUND AFT ENTRY AREA FLOOR BOARD WAS CORRODED. BLENDED OUT CORROSION, FABRICATED NEW HAT CHANNELS AND PANEL. INSTALLED REPAIRS IAW DC9 SRM 51-10-3, 51-10-4, 51- - [SDR AT0000428](https://openairdocs.org/sdr/AT0000428), Aug 25, 2000: SKIN. CRACKED. FOUND A CRACK IN FUSELAGE UPPER NOSE SKIN AT LBL 17 BS 69.5. REMOVED CRACKED FILLER, PERFORMED HFEC, INSTALLED DOUBLER AND FILLER IAW TIMCO SERVICE ORDER 151080 - [SDR AT0000433](https://openairdocs.org/sdr/AT0000433), Aug 24, 2000: FRAME. CRACKED. FOUND FRAME AT BS 737 WAS CRACKED. REPAIRED FRAME AT BS 737 IAW SERVICE BULLETIN 53-131 DRAWING 5935650. - [SDR AT0000436](https://openairdocs.org/sdr/AT0000436), Aug 23, 2000: FRAME. LIGHTNING STRIKE. FOUND LIGHTNING STRIKE ON WINDOW NR 50 LOWER AFT CORNER ON FRAME. BLENDED OUT LIGHTNING STRIKE, FABRICATED AND INSTALLED REPAIR IAW SRO 9530053 AND REO L-00265. - [SDR AT0000435](https://openairdocs.org/sdr/AT0000435), Aug 23, 2000: FITTING. CORRODED. FOUND STRINGER 30 END CAP FITTING AT WING SPAR HAS CORROSION. REMOVED AND REPLACED STRINGER END CAP FITTING AT BS 540 - 580 IAW DC9 SRM 51-01 FIGURE 1, 51-30-0, - [SDR AT0000432](https://openairdocs.org/sdr/AT0000432), Aug 23, 2000: SKIN. DENTED. FOUND DENT AT BS 350, LONGERON 26R, 27L. DENT OUT OF LIMITS. PERFORMED HFEC INSPECTION, FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC9 SRM 53-04 FIGURE 3B. - [SDR AT0000427](https://openairdocs.org/sdr/AT0000427), Aug 23, 2000: BRACKET. CRACKED. FOUND CRACKED SUPPORT BRACKETS FOR CABIN FLOOR PANEL AT BS 725 - 832. REMOVED AND REPLACED SUPPORT BRACKETS IAW TIMCO SERVICE ORDER 151080-20463. - [SDR AT0000425](https://openairdocs.org/sdr/AT0000425), Aug 21, 2000: LANYARD. FRAYED. FOUND FORWARD AND AFT ESCAPE LINE OVER RIGHT WING WERE FRAYED. REMOVED AND REPLACED FORWARD AND AFT EMERGENCY ESCAPE LINES IAW DC9 MM 25-61-0. - [SDR AT0000263](https://openairdocs.org/sdr/AT0000263), May 18, 2000: UNKNOWN. ODOR. DURING CLIMB, FLIGHT ATTENDANTS SMELLED SMOKE IN CABIN. INSPECTED ALL COMPARTMENTS FOR SMOKE OR ODOR, RAN ENGINES, PACKS, AND PRESSURIZED AIRCRAFT WITH NO SMOKE - [SDR AT0000035](https://openairdocs.org/sdr/AT0000035), Jan 22, 2000: WARNING LIGHT. ILLUMINATED. FOUND DURING LANDING GEAR EXTENTION, GEAR DOOR OPEN AMBER LIGHT STAYED ON. RECYCLED GEAR BY EMERGENCY EXTENTION METHOD. LIGHT REMAINED ON. LANDED WITH ABNORMAL - [SDR AT0000035R1](https://openairdocs.org/sdr/AT0000035R1), Jan 18, 2000: BRACKET. LOOSE. FOUND DURING LANDING GEAR EXTENTION, GEAR DOOR OPEN AMBER LIGHT STAYED ON. RECYCLED GEAR BY EMERGENCY EXTENTION METHOD. LIGHT REMAINED ON. LANDED WITH ABNORMAL - [SDR AT0000005](https://openairdocs.org/sdr/AT0000005), Jan 1, 2000: WIRE. BROKEN. EMERGENCY TRACK LIGHT INOPERATIVE. REPAIRED BROKEN WIRE ON FORWARD EMERGENCY TRACK LIGHT IAW MM 33-53. - [SDR AT9900531](https://openairdocs.org/sdr/AT9900531), Jul 4, 1999: PANEL. DELAMINATED. DURING A SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, FOUND DELAMINATION AND CORROSION DAMAGE ON THE LT WING UPPER T/E PANEL P/N 5912737-1. REPAIRED PANEL IAW T - [SDR AT9900525](https://openairdocs.org/sdr/AT9900525), Jun 30, 1999: SKIN. CRACKED. DURING A SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, FOUND FIRST FASTENER ON RIGHT SHEAR TIE CRACKED AT BS 680 AND LONGERON 1 R. CUT OUT CRACKED AREAS. FABRICA - [SDR AT9900526](https://openairdocs.org/sdr/AT9900526), Jun 29, 1999: SKIN. CREASED. DURING A SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, FOUND FUSELAGE SKIN CREASE 60.0 BY 1.5 BY .030 AT BS 290 - 350 BETWEEN L-22L AND L-23L. REMOVED AND REPLAC - [SDR AT9900527](https://openairdocs.org/sdr/AT9900527), Jun 22, 1999: SKIN. DENTED. DURING A SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, FOUND FUSELAGE SKIN DENT 16 BY .5 BY .03. AT BS 300 BETWEEN L-18R AND L-19R DENT EXCEEDS LIMITS PER DC9 SR - [SDR AT9900523](https://openairdocs.org/sdr/AT9900523), Jun 20, 1999: TRIM STRIP. CORRODED. DURING A SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, FOUND AFT PIT CENTER CEILING PANEL ATTACH STRAPS CORRODED AT BS 965-996. DRILLED 5 EACH CEILING PANEL CLOS - [SDR AT9900528](https://openairdocs.org/sdr/AT9900528), Jun 19, 1999: FITTING. CORRODED. DURING A SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, FOUND AFT AIRSTAIRS FWD SKIN AT BS 1090 AND L-30R MISSING INTERNAL SHIMS. AFTER OPEN UP FOUND WEB CRACKED - [SDR AT9900463](https://openairdocs.org/sdr/AT9900463), Jun 16, 1999: FRAME. CORRODED. SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, FOUND FRAME IN THE FORWARD PIT AT BS 541 L-29L-29R CORRODED. REMOVED CORROSION, FABRICATED REPAIR PARTS, HEAT TREAT - [SDR AT9900529](https://openairdocs.org/sdr/AT9900529), Jun 10, 1999: SKIN. DENTED. DURING A SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, FOUND FUSELAGE SKIN CREASE 6 INCHES BELOW CUSP LINE ON LEFT SIDE AT BS 99. DRILLED .025 HOLE, INSTALLED RI - [SDR AT9900441](https://openairdocs.org/sdr/AT9900441), May 30, 1999: WEB. CORRODED. SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL. FOUND ON THE LEFT MAIN CABIN AT BS 928 LONGERON NR 18 ATTACHED WEB CORRODED. MECHANICALLY REMOVED CORROSION, FABRIC - [SDR AT9900434](https://openairdocs.org/sdr/AT9900434), May 30, 1999: WEB. CORRODED. SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL. FOUND CORROSION ON THE MAIN CABIN ATTACHED WEB AT BS 917 L-18L. REMOVED CORROSION, FABRICATED REPAIR DOUBLER AND IN - [SDR AT9900435](https://openairdocs.org/sdr/AT9900435), May 25, 1999: WEB. CORRODED. SHEDULED INSPECTION AT TIMCO LAKE CITY, FL. FOUND THE MAIN CABIN LEFT LONGERON NR 18 AT BS 823 ATTACHED WEB CORRODED. REMOVED CORROSION, FABRICATED REPAIR DOUBL - [SDR AT9900572](https://openairdocs.org/sdr/AT9900572), May 24, 1999: FRAME. CRACKED. DURING SCHEDULED INSPECTION AT TIMCO, FOUND FWD CARGO COMPARTMENT HAS BENT AND CRACKED FRAME AT BS 408 L24L. REMOVED CARGO FRAME FLOOR SUPPORT, FABRICATED REPAI - [SDR AT9900530](https://openairdocs.org/sdr/AT9900530), May 21, 1999: JAMB. GOUGED. DURING A SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, FOUND MAIN RE-FUELING POINT AT LOWER WING SKIN WORN THROUGH WHERE LATCH FOR FUEL DOOR MATES TO LOWER SKIN. - [SDR AT9900571](https://openairdocs.org/sdr/AT9900571), May 20, 1999: BULKHEAD PANEL. CORRODED. DURING SCHEDULED INSPECTION AT TIMCO, FOUND AFT PIT FWD LT BULKHEAD PANEL HAD SEVERAL SPOTS OF SURFACE CORROSION. MECHANICALLY CLEANED AREAS, FABRICATED NEW PAN - [SDR AT9900524](https://openairdocs.org/sdr/AT9900524), May 20, 1999: STRAP. CORRODED. DURING A SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, FOUND FWD PIT CENTER CEILING PANEL FASTENER STRIPS CORRODED AT BS 218. MATERIAL LOSS 100 PERCENT, OUT OF L - [SDR AT9900142](https://openairdocs.org/sdr/AT9900142), Feb 24, 1999: COVER. LOOSE. FOUND THE R-1 DOOR SLIDE COVER NEEDS TO BE SECURED AND INSPECTED FOR PROPER INSTALLATION. SECURED SLIDE COVER PER MM 25-60. ## Other aircraft with N805AT - [Registered now](https://openairdocs.org/aircraft/N805AT): Piper PA-44-180, S/N 4496334, built 2013 --- 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.