# N803AT: 1968 Douglas DC-9-32, registration cancelled 2003-08-18

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: August 18, 2003
- Status when cancelled: Sale reported
- 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: 47261
- Year built: 1968
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: November 12, 1968
- Last registry action: February 3, 2003
- Mode S code: AAED14
- Location: [Hampton, VA](https://openairdocs.org/faa-place/VA/Hampton)
- Owner type: Individual
- Owner's area on the map: 37.0507° N, 76.3393° W: Placed by OpenAirDocs at the center of ZIP code 23669, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N803AT
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=803AT
- Page: https://openairdocs.org/deregistered/N803AT-2003-08-18

From the FAA registry file of October 28, 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 (46)

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

- [SDR AT0100158](https://openairdocs.org/sdr/AT0100158), Apr 21, 2001: THRESHOLD. CORRODED. FOUND AFT ENTRANCE THRESHOLD CORRODED BEYOND LIMITS. FABRICATED AND INSTALLED REPAIR IAW DC9 SRM 51-10-02, 51-10-03, 51-10-04, 51-30, 51-30-02, 51-30-05, AND 51
- [SDR AT0100157](https://openairdocs.org/sdr/AT0100157), Apr 20, 2001: FLOORBEAM. CORRODED. FOUND AFT CARGO COMPARTMENT BS 965 RBL 12 FLOORBEAM ATTACH ANGLE TO HAVE EXFOLIATED CORROSION. REPLACED FLOORBEAM IAW REO L00433 REV A, DC9 SRM 53-04 FIG 12C, 5
- [SDR AT0100156](https://openairdocs.org/sdr/AT0100156), Apr 19, 2001: CONTROL COLUMN. CRACKED. FOUND CAPTAINS CONTROL COLUMN CRACKED BEYOND LIMITS. REPLACED CONTROL COLUMN IAW EO 12-2730-29-B1063.
- [SDR AT0100172](https://openairdocs.org/sdr/AT0100172), Apr 16, 2001: FRAME. CRACKED. FOUND FRAME AT BS 598 LONGERON 11 CRACKED. FABRICATED AND INSTALLED REPAIR IAW REO-L00432.
- [SDR AT0100160](https://openairdocs.org/sdr/AT0100160), Apr 16, 2001: LONGERON. CRACKED. FOUND LONGERON 11 FRAME AT BS 598 CRACKED. INSTALLED REPAIR IAW REO L00432.
- [SDR AT0100159](https://openairdocs.org/sdr/AT0100159), Apr 15, 2001: ATTACH ANGLE. CRACKED. FOUND DORSAL FIN ATTACH ANGLES CRACKED BEYOND LIMITS. REPLACED ATTACH ANGLES IAW EO 09-5350-29-E1645.
- [SDR AT0100162](https://openairdocs.org/sdr/AT0100162), Apr 8, 2001: DOOR FRAME. CORRODED. FOUND AFT STAIRWAY DOOR FRAME CORRODED BEYOND LIMITS. FABRICATED AND INSTALLED ATTACH ANGLE REPAIR IAW DC9 SRM 53-01 FIG 1, 51-30, 51-10-03, 51-10-02, 51-10-04 
- [SDR AT0000114](https://openairdocs.org/sdr/AT0000114), Mar 8, 2000: FUSE. FAILED. FOUND CENTER SECTION OF EMERGENCY PATH LIGHTING INOPERATIVE.. REPLACED BLOWN FUSE AT AFT BATTERY CHARGER.
- [SDR AT0000080](https://openairdocs.org/sdr/AT0000080), Feb 9, 2000: STRINGER. CORRODED. FOUND LEFT HAND WING STRINGER 15 CORRODED. INSTALLED STRAP REPAIR IAW DC9 SRM 51-30-5, 51-10-4, 57-08 FIGURE 2 METHOD 2, 51-22-1 TO -3.
- [SDR AT0000079](https://openairdocs.org/sdr/AT0000079), Feb 9, 2000: STRINGER. CORRODED. FOUND LEFT HAND WING STRINGER 17 CORRODED. CUT AND SPLICED LEFT HAND WING STRINGER 17 IAW DC9 SRM 51-30-5, 51-10-4, 51-22-1, 51-10-3, 57-08 FIGURE 2.
- [SDR AT0000078](https://openairdocs.org/sdr/AT0000078), Feb 9, 2000: STRINGER. CORRODED. FOUND LEFT HAND WING STRINGER 20 CORRODED. CUT AND SPLICED LEFT HAND WING STRINGER 20 IAW DC9 SRM 51-30-5, 51-10-4, 51-22-1, 51-10-3, 57-08 FIGURE 2.
- [SDR AT0000077](https://openairdocs.org/sdr/AT0000077), Feb 9, 2000: STRINGER. CORRODED. FOUND LEFT HAND STRINGER 23 CORRODED. REMOVED AND REPLACED LEFT HAND STRINGER 23 IAW DC9 SRM 51-30-5, 51-10-4, 51-22-1, 51-30-1, 57-08.
- [SDR AT0000072](https://openairdocs.org/sdr/AT0000072), Feb 7, 2000: STRINGER. GOUGED. FOUND AFT CARGO DOOR AT BS 937, LONGERON 23R - 25R WAS BENT AND GOUGED. FABRICATED, DRILLED AND INSTALLED REPAIR IAW TIMCO EO L00036.
- [SDR AT0000075](https://openairdocs.org/sdr/AT0000075), Feb 5, 2000: DOOR PAN. CORRODED. FOUND CORROSION AT LOWER DOOR STOP AT AFT CARGO DOOR FRAME AT BS 917. REMOVED AND REPLACED AFT CARGO DOOR JAMB PAN SECTION IAW DC9 SRM 53-10-01 FIGURE 1, 51-10-
- [SDR AT0000074](https://openairdocs.org/sdr/AT0000074), Feb 3, 2000: DOOR PAN. CORRODED. FOUND C1 CARGO DOOR CUTOUT PAN HAD SEVERAL AREAS OF CORROSION. REMOVED AND REPLACED CARGO DOOR PAN, FABRICATED AND INSTALLED PAN SPLICES IAW DC9 SRM 53-05 FIGUR
- [SDR AT0000076](https://openairdocs.org/sdr/AT0000076), Feb 2, 2000: FRAME. CORRODED. FOUND CORROSION ON FORWARD SIDE FRAME AT BS 980, LONGERON 26R -24R. REMOVED CORROSION, BEYOND LIMITS. REMOVED FRAME SECTION AT BS 980, LONGERON 26R - 24R, INSTA
- [SDR AT0000070](https://openairdocs.org/sdr/AT0000070), Feb 2, 2000: SKIN. CRACKED. FOUND CRACK AT FORWARD ENTRY DOOR JAMB, FORWARD UPPER CORNER ON OUTER SKIN. CUT OUT CRACKED SKIN, FABRICATED DOUBLERS, AND INSTALLED IAW SRD 9530252.
- [SDR AT0000073](https://openairdocs.org/sdr/AT0000073), Feb 1, 2000: BULKHEAD. CORRODED. FOUND CANTED BULKHEAD AT BS 1143, LEFT HAND UNDER THE END OF LEFT HAND PYLON SKIN WAS CORRODED. REMOVED CORROSION, REPLACED SKIN AND DOUBLERS IAW DC9 SRM 53-01 
- [SDR AT0000069](https://openairdocs.org/sdr/AT0000069), Feb 1, 2000: SKIN. CRACKED. FOUND CARGO COMPARTMENT DOOR JAMB FORWARD LOWER CORNER HAS A .375 CRACK ON OUTER SKIN. CUT OUT CRACK, FABRICATED 2 REPAIR DOUBLERS. TREATED PRIMED AND INSTALLED
- [SDR AT0000062](https://openairdocs.org/sdr/AT0000062), Jan 28, 2000: FRAME. CRACKED. FOUND FRAME CRACKED AT RIGHT HAND SIDE NEAR THE ACTUATOR LOWER MOUNT (AIRSTAIRS) AT BS 1143. CUT OUT CRACKED FRAME SECTION FABRICATED L & Z DOUBLERS, HEAT TREAT
- [SDR AT0000071](https://openairdocs.org/sdr/AT0000071), Jan 26, 2000: SKIN. CORRODED. FOUND RIGHT HAND AFT VANITY CLOSE TO ANGLE SKIN WAS CORRODED OUT OF LIMITS. FABRICATED UPPER SKIN, FILLERS, HEAT TREATED AND INSTALLED IAW DC9 SRM 51-30-1, 51-1
- [SDR AT0000059](https://openairdocs.org/sdr/AT0000059), Jan 26, 2000: LONGERON. CORRODED. FOUND LONGERON 24R HAD CORROSION AT BS 935 FROM END CAP ALONG UPPER CHANNEL TO BS 945. REMOVED LONGERON 24R, END CLIP, END FITTING. INSTALLED NEW SKIN PATCH AT 
- [SDR AT0000046](https://openairdocs.org/sdr/AT0000046), Jan 23, 2000: FRAME. CORRODED. FOUND AFT PIT LONGERON CORRODED AT BS 832 ALONG FRAME. REMOVED CORROSION, TREATED, ALODINED AND PRIMED IAW DC9 SRM 53-01 FIGURE 1, TABLE 2, 51-10-3.
- [SDR AT0000044](https://openairdocs.org/sdr/AT0000044), Jan 19, 2000: WEB. CORRODED. FOUND ELECTRICAL COMPARTMENT COCKPIT SUBFLOOR CORRODED AT BS 150-160. CUT OUT CORRODED AREA OF SUBFLOOR, FABRICATED FILLER/DOUBLER AND INSTALLED IAW DC9 SRM 51-
- [SDR AT0000043](https://openairdocs.org/sdr/AT0000043), Jan 19, 2000: FLOORBEAM. CORRODED. FOUND AFT PIT CABIN FLOORBEAM HAS EXFOLIATED CORROSION AT BS 996. REMOVED FLOORBEAM UPPER CAP, FABRICATED NEW CAP ANGLE, TREATED, PRIMED AND INSTALLED NEW CAP A
- [SDR AT0000045](https://openairdocs.org/sdr/AT0000045), Jan 18, 2000: FITTING. CORRODED. FOUND DURING REMOVAL OF WEB, FITTING WAS EXFOLIATED WITH CORROSION AT BS 996. REMOVED AND REPLACED FITTING IAW DC9 SRM 51-01 FIGURE 1, 51-10-4, 51-30-5.
- [SDR AT0000047](https://openairdocs.org/sdr/AT0000047), Jan 17, 2000: DOUBLER. CORRODED. FOUND CORROSION OUT OF LIMITS ON G-4 LEFT HAND GALLEY SIDEWALL. CUT OUT CORRODED AREA, FABRICATED FILLER/DOUBLER, AND INSTALLED IAW DC9 SRM 51-10-3, 51-10-4, 51
- [SDR AT0000039](https://openairdocs.org/sdr/AT0000039), Jan 13, 2000: ANGLE. CORRODED. FOUND ELECTRICAL EQUIPMENT COMPARTMENT SUPPORT BETWEEN BS 110-120 IS CORRODED FROM LONGERON 25R TO 26R. CORROSION FOUND TO BE OUT OF LIMITS. REMOVED CORROSION F
- [SDR AT9900894](https://openairdocs.org/sdr/AT9900894), Dec 19, 1999: LIGHT. INOPERATIVE. DURING SERVICE CHECK, LEFT AFT OVERWING EMERGENCY EXIT IDENTIFIER LIGHT AT BS 669 WAS INOPERATIVE. TIGHTENED NUT ON GROUND TERMINAL OF LIGHT FIXTURE L2-245 AT B
- [SDR AT9900606](https://openairdocs.org/sdr/AT9900606), Aug 14, 1999: FLOOR. WEAK. SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, UPON INSTALLATION FOUND CABIN FLOORBOARD NR 97 WEAK. FABRICATED A REPLACEMENT FLOORBOARD PANEL IAW DC9 SRM 53-21-0,
- [SDR AT9900604](https://openairdocs.org/sdr/AT9900604), Aug 9, 1999: BRACKET. CORRODED. SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, FOUND CORROSION ON TOP OF CONTROL CABLE AILERON PULLEY TOWER IN FORWARD OUTBOARD OF LEFT WHEEL WELL. REMOVED AND RE
- [SDR AT9900775](https://openairdocs.org/sdr/AT9900775), Aug 6, 1999: WEB. CORRODED. FOUND 4 CRACK AT BS 955-960, LBL 48-52 IN CUSP WEB AND CORROSION OUT OF LIMITS. FABRICATED REPAIR IAW DC9 SRM 53-05 FIGURE 97, 51-10-3, 51-30-1, 51-30-2, AND DC
- [SDR AT9900605](https://openairdocs.org/sdr/AT9900605), Aug 4, 1999: SKIN. CHAFED. SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, FOUND THE LEFT LOWER AFT BANANA FAIRING ON THE VERTICAL STABILIZER AND SKIN CHAFFED AT YV 227-247. BLEND CHAFFED AR
- [SDR AT9900776](https://openairdocs.org/sdr/AT9900776), Jul 29, 1999: WEB. CORRODED. FOUND CUSP WEB AT BS 945-965 WITH EXFOLIATED CORROSION. FABRICATED REPAIR WEB IAW DC9 SRM 53-05 FIGURE 97, 51-10-3, 51-30-1, 51-30-2, AND DC9 MM 53-20-1.
- [SDR AT9900603](https://openairdocs.org/sdr/AT9900603), Jul 29, 1999: SKIN. CRACKED. SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, FOUND THE AFT CARGO DOOR OUTER SKIN CRACK AT FASTENERS ON THE LOWER SIDE. REMOVED LOWER HALF OF PRESSURE SEAL FOR A
- [SDR AT9900805](https://openairdocs.org/sdr/AT9900805), Jul 25, 1999: LONGERON. CORRODED. FOUND AFT PIT LONGERON AT BS 870-965 CORRODED. INSTALLED LONGERON REPAIR BETWEEN BS 870-955 IAW DC9 SRM 53-03 FIGURE 2A, 51-10-2, 51-10-4, 51-30-2, 51-70-2, 53-
- [SDR AT9900777](https://openairdocs.org/sdr/AT9900777), Jul 24, 1999: SKIN&LONGERON. CORRODED. LOWER KEEL BEAM SKIN AT BS 658-756 HAS A BULDGING AREA OF CORROSION THAT HAS PUSHED OUT AND CRACKED THE SKIN. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. R
- [SDR AT9900615](https://openairdocs.org/sdr/AT9900615), Jul 22, 1999: CUSP WEB. CORRODED. DURING SCHEDULED INSPECTION AT TIMCO LAKE CITY FLORIDA, FOUND RT CUSP WEB CORRODED AT BS 945-965. REMOVED CUSP WEB. FABRICATED, ALODINED, PRIMED AND INSTALLED R
- [SDR AT9900614](https://openairdocs.org/sdr/AT9900614), Jul 22, 1999: FLOOR. CRACKED. DURING SCHEDULED INSPECTION AT TIMCO LAKE CITY FLORIDA, FOUND CUSP WEB CRACKED AT BS 955-960 LBL 48-52. REMOVED CUSP FOUND CORROSION. FORMED, DRILLED AND DEBURR
- [SDR AT9900610](https://openairdocs.org/sdr/AT9900610), Jul 19, 1999: SEAT TRACK. CORRODED. SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL. FOUND THE LEFT OUTBOARD SEAT TRACK AT BS 570 - 590 WITH NICKS, SCRATCHES AND CORROSION. CUT OUT SECTION OF SEAT TRA
- [SDR AT9900804](https://openairdocs.org/sdr/AT9900804), Jul 18, 1999: SEAT TRACK. CORRODED. FOUND RIGHT INBOARD SEAT TRACK AT BS 218-965 WITH NICKS, SCRATCHES AND CORROSION. REPLACED SEAT TRACK IAW DC9 SRM 53-05 FIGURE 4, 51-30-2, 51-10-3.
- [SDR AT9900618](https://openairdocs.org/sdr/AT9900618), Jul 14, 1999: LONGERON. CORRODED. DURING SCHEDULED INSPECTION AT TIMCO LAKE CITY FLORIDA, FOUND AFT PIT LONGERON 30 CORRODED AT BS 870-965. CUT LONGERON FROM BS 870-955. REMOVED SHEAR TIES, FLOO
- [SDR AT9900619](https://openairdocs.org/sdr/AT9900619), Jul 8, 1999: ADF PANEL. CORRODED. DURING SCHEDULED INSPECTION AT TIMCO LAKE CITY FLORIDA, FOUND FLAKING PAINT AND FLARE SPRAY ON LEFT FORWARD ADF PANEL. REMOVED CORROSION AND PEELING FLARE SPRAY
- [SDR AT9900617](https://openairdocs.org/sdr/AT9900617), Jul 8, 1999: SEAT TRACK. CORRODED. DURING SCHEDULED INSPECTION AT TIMCO LAKE CITY FLORIDA, FOUND RT INBOARD SEAT TRACK SCRATCHED AND CORRODED AT BS 218 TO 965. REMOVED SECTION OF SEAT TRACK FROM 
- [SDR AT9900616](https://openairdocs.org/sdr/AT9900616), Jul 6, 1999: SKIN. CORRODED. DURING SCHEDULED INSPECTION AT TIMCO LAKE CITY FLORIDA, FOUND LOWER KEEL BEAM SKIN AT BS 770 HAS AN AREA OF BULGING CORROSION THAT HAS PUSHED OUT AND CRACKED TH
- [SDR AT9900620](https://openairdocs.org/sdr/AT9900620), Jun 27, 1999: SKIN. MISREPAIRED. DURING SCHEDULED INSPECTION AT TIMCO LAKE CITY FLORIDA, FOUND CLASS III TEMPORARY REPAIR ON FUSELAGE FORWARD OF RIGHT WING ROOT PER DC9 SRM 53-40 FIG 12B SHT 15

## 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 20010224002649I](https://openairdocs.org/incident/20010224002649I), Feb 24, 2001: Doug DC932 (N803AT), Newport News, VA. (-23)Returned to land after takeoff, smoke smell in rear cabin. Log page #F210671, disc. #18: "acrid smoke smell in aft cabin. No smoke visible." Corrective…

## Other aircraft with N803AT

- [Registered now](https://openairdocs.org/aircraft/N803AT): Piper PA-44-180, S/N 4496332, built 2013

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