# N208US: 1968 Mcdonnell Douglas DC-9-32F, registration cancelled 2023-06-21 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: June 21, 2023 - Exported to: Mexico - Status when cancelled: Sale reported - Airframe: [Mcdonnell Douglas DC-9-32F](https://openairdocs.org/model/mcdonnell-douglas-dc-9-32f) (registry code 302206E) - Engine: [Amateur-built UNKNOWN ENG](https://openairdocs.org/engine/amateur-built-unknown-eng) (registry code 99999) - Data sheets: [TCDS A6WE](https://openairdocs.org/tcds/A6WE) (OpenAirDocs) - Serial number: 47220 - Year built: 1968 - Type of aircraft: Fixed wing multi engine - Airworthiness: Standard, transport - Airworthiness date: October 23, 1981 - Last registry action: June 20, 2023 - Mode S code: A1B18E - Location: [Xxx, OK](https://openairdocs.org/faa-place/OK/Xxx) - Owner type: Individual - Owner's area on the map: 35.3806° N, 97.6484° W: Placed by OpenAirDocs at the center of ZIP code 73169, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N208US - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=208US - Page: https://openairdocs.org/deregistered/N208US-2023-06-21 From the FAA registry file of November 4, 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 Mcdonnell Douglas DC-9-32F: https://openairdocs.org/model/mcdonnell-douglas-dc-9-32f.md ## Service difficulty reports (41) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR Y2PA201809250032](https://openairdocs.org/sdr/Y2PA201809250032), Sep 25, 2018: SKIN PANEL. CORRODED. DURING C-CHECK AT KSFB, CORROSION WAS DISCOVERED ON SKIN AT STA 1114, LONGERON 18R. MAINTENANCE AT KSFB. REMOVED AND REPLACED LOWER SKIN FROM STA 1087-1121, LON - [SDR Y2PA2016022800004](https://openairdocs.org/sdr/Y2PA2016022800004), Feb 25, 2016: LANDING GEAR. MALFUNCTIONED. DURING APPROACH, GEAR HANDLE PLACED IN DOWN POSITION. NOSE LANDING GEAR LIGHT DID NOT ILLUMINATE GREEN. CYCLED GEAR, NOSE GEAR LIGHT STILL DID NOT ILLUMINATE GR - [SDR Y2PA20130511039](https://openairdocs.org/sdr/Y2PA20130511039), May 11, 2013: LINE. FAILED. CREW REPORTED POST V1 & JUST INTO ROTATION, MASTER CAUTION ILLUMINATED FOR LT OIL PRESSURE LOW. DECISION MADE TO LEAVE MLG DOWN. OIL PRESSURE LOW & QTY DECREASI - [SDR Y2PA20130507036](https://openairdocs.org/sdr/Y2PA20130507036), May 6, 2013: SKIN. CRACKED. DURING C-CHECK INSPECTION AT YIP, MX DISCOVERED THE LT FLAP LOWER SKIN CRACKED. MX AT REPAIRED IAW SRM 57-01, FIGURE 3, SHEET 2 AND EA 96-51-02 R1. - [SDR Y2PA20130507035](https://openairdocs.org/sdr/Y2PA20130507035), May 6, 2013: HINGE. CRACKED. DURING C-CHECK INSPECTION, MX DISCOVERED THE LT WING CENTER AFT FLAP HINGE CRACKED. MX R & R HINGE IAW AMM 27-51-1 AND OHM 27-50-1. - [SDR Y2PA20130507034](https://openairdocs.org/sdr/Y2PA20130507034), May 6, 2013: BRACKET. CORRODED. DURING C-CHECK INSPECTION, MX DISCOVERED THE MAIN UPPER CARGO DOOR LOWER SILL BRACKET CORRODED. MX R & R BRACKET IAW SRM 51-30-5. - [SDR Y2PA20130507033](https://openairdocs.org/sdr/Y2PA20130507033), May 6, 2013: PANEL. DELAMINATED. DURING C-CHECK INSPECTION, MX DISCOVERED THE INBD LT T/E WING PANEL DELAMINATED. MX R & R PANEL WITH SERVICEABLE IAW SRM 51-30-2. - [SDR Y2PA20130507032](https://openairdocs.org/sdr/Y2PA20130507032), May 6, 2013: PANEL. DELAMINATED. DURING C-CHECK INSPECTION, MX DISCOVERED THE SECOND FROM OTBD LT T/E WING PANEL DELAMINATED. MX R & R PANEL WITH SERVICEABLE IAW SRM 51-30-2. - [SDR Y2PA20130507031](https://openairdocs.org/sdr/Y2PA20130507031), May 6, 2013: TEE FITTING. CORRODED. DURING C-CHECK INSPECTION, MX DISCOVERED A TEE FITTING CORRODED AT BS 160 ON THE RT CUSP LINE. MX R & R TEE FITTING IAW SRM 51-30-2 AND 51-30-5. - [SDR Y2PA20130507029](https://openairdocs.org/sdr/Y2PA20130507029), May 6, 2013: LONGERON. CORRODED. DURING C-CHECK INSPECTION, MX DISCOVERED LONGERON END SHOVEL CORRODED IN THE LOWER AFT CARGO BAY AT BS 996 ON LONGERONS 29L. MX R & R SHOVELS IAW SRM 51-30-5. - [SDR Y2PA20130507028](https://openairdocs.org/sdr/Y2PA20130507028), May 6, 2013: SLEEVE. CRACKED. DURING C-CHECK INSPECTION, MX DISCOVERED BOTH LT AND RT HORIZONTAL STABILIZER HINGE BOLT SLEEVES CRACKED. MX R & R SLEEVES IAW AMM 55-10-0. - [SDR Y2PA20130507027](https://openairdocs.org/sdr/Y2PA20130507027), May 6, 2013: SKIN. CORRODED. DURING C-CHECK INSPECTION, MX DISCOVERED THE LOWER AFT CARGO BAY SKIN CORRODED AT BS 756, LONGERON 27L 29R. MX REPAIRED IAW EA 13-53-321 AND DER DWG 53-13118-1, - [SDR Y2PA20130507026](https://openairdocs.org/sdr/Y2PA20130507026), May 6, 2013: WEB. CORRODED. DURING C-CHECK INSPECTION, MX DISCOVERED THE LOWER AFT CARGO BAY CENTERLINE WEB CORRODED AT BS 996. MX REPAIRED IAW SRM 53-01, FIG 2 SHEET 3 AND EA 96-51-02 R3. - [SDR Y2PA20130507025](https://openairdocs.org/sdr/Y2PA20130507025), May 6, 2013: WINDOW FRAME. CRACKED. DURING INSPECTION IAW AD 2002-21-09, 2 EACH .5" CRACKS WERE DISCOVERED IN THE CENTER FRAME OF THE COCKPIT WINDOW SILL. MX R & R THE COCKPIT WINDOW SILL CENTER F - [SDR Y2PA20130507024](https://openairdocs.org/sdr/Y2PA20130507024), May 6, 2013: SPAR. CRACKED. DURING C-CHECK X-RAY INSPECTION, MX DISCOVERED THE LT ELEVATOR FRONT SPAR CRACKED OUT OF LIMITS. MX AT YIP R & R THE LT ELEVATOR WITH A SERVICEABLE PART IAW MM - [SDR Y2PA2011092000024](https://openairdocs.org/sdr/Y2PA2011092000024), Sep 16, 2011: BATTERY PACK. DISCHARGED. EMERGENCY LIGHTS INOPERATIVE DURING INSP. MX R & R BATTERY POWER SUPPLY IAW AMM 33-50-0. OPS CHECKS GOOD, NO OTHER DEFECTS NOTED. - [SDR Y2PA2010111500028](https://openairdocs.org/sdr/Y2PA2010111500028), Nov 10, 2010: DOWNLOCK SWITCH. MALFUNCTIONED. UPON APPROACH, THE RT MLG DID NOT DISPLAY GREEN INDICATION, ONLY RED. CREW EXECUTED MISSED APPROACH AND REVIEWED COM PROCEDURES. CREW DIVERTED AND DECLARED AN E - [SDR ABXR080086](https://openairdocs.org/sdr/ABXR080086), Feb 14, 2008: RIB. CRACKED. RIB CRACKED AT FASTENERS LEFT AND RIGHT SIDES OF VERT STAB LEADING EDGE ZFS 18. REPAIRED IAW DC9 SSRM DWG K05159. - [SDR ABXR080085](https://openairdocs.org/sdr/ABXR080085), Feb 14, 2008: RIB. CRACKED. RIB CRACKED AT FASTENERS LEFT AND RIGHT SIDES OF VERT STAB LEADING EDGE ZFS 50. REPAIRED IAW DC9 SSRM DWG K05159. - [SDR ABXR080082](https://openairdocs.org/sdr/ABXR080082), Feb 14, 2008: RIB. CRACKED. RIB CRACKED AT FASTENER LEFT SIDE VERT STABILIZER LEADING EDGE ZFS 93. REPAIRED RIB IAW DC9 SRM D05159. - [SDR ABXR080084](https://openairdocs.org/sdr/ABXR080084), Feb 14, 2008: RIB. CRACKED. RIB CRACKED AT FASTENERS LEFT AND RIGHT VERT STAB LEADING EDGE ZFS 43. REPAIRED IAW DC9 SSRM DWG K05159. - [SDR ABXR080081](https://openairdocs.org/sdr/ABXR080081), Feb 14, 2008: RIB. CRACKED. RIB CRACKED AT FASTENER LEFT SIDE OF VERTICAL STAB LEADING EDGE XFS 148. REPAIRED IAW DC9 SSRM DWG K05159. - [SDR ABXR080078](https://openairdocs.org/sdr/ABXR080078), Feb 14, 2008: RIB. CRACKED. RIB CRACKED AT FASTENERS LEFT AND RIGHT SIDES OF VERTICAL STAB LEADING EDGE ZFS 50. REPAIRED IAW DC9 SSRM DWG K05159. - [SDR ABXR080077](https://openairdocs.org/sdr/ABXR080077), Feb 14, 2008: RIB. CRACKED. RIB CRACKED AT FASTENERS LEFT AND RIGHT SIDE OF VERTICAL STAB LEADING EDGE ZFS 43. REPAIRED IAW DC9 SSRM DWG K05159. - [SDR ABXR080076](https://openairdocs.org/sdr/ABXR080076), Feb 14, 2008: RIB. CRACKED. RIB CRACKED AT FASTENERS LEFT AND RIGHT SIDES OF VERTICAL STAB LEADING EDGE ZFS 18. REPAIRED IAW DC9 SSRM DWG K05159. - [SDR ABXR080075](https://openairdocs.org/sdr/ABXR080075), Feb 14, 2008: RIB. CRACKED. RIB CRACKED AT FASTENER RIGHT SIDE OF VERTICAL STAB LEADING EDGE ZFS 23. REPAIRED IAW DC9 SSRM DWG K05159. - [SDR ABXR080083](https://openairdocs.org/sdr/ABXR080083), Feb 14, 2008: RIB. CRACKED. RIB CRACKED AT FASTENERS LEFT AND RIGHT SIDES OF VERT STAB LEADING EDGE ZFS 18. REPAIRED IAW DC9 SSRM DWG K05159. - [SDR ABXR080080](https://openairdocs.org/sdr/ABXR080080), Feb 14, 2008: RIB. CRACKED. RIB CRACKED AT FASTENERS LEFT AND RIGHT SIDES OF VERTICAL STAB LEADING EDGE ZFS 74. REPAIRED LEFT AND RIGHT RIBS IAW DC9 SSRM K05159. - [SDR ABXR080079](https://openairdocs.org/sdr/ABXR080079), Feb 14, 2008: RIB. CRACKED. RIB CRACKED AT FASTENER RIGHT SIDE OF VERTICAL STAB LEADING EDGE ZFS 80. REPAIRED RIB IAW DC9 SSRM K05159. - [SDR ABXR080074](https://openairdocs.org/sdr/ABXR080074), Feb 7, 2008: FRAME. CRACKED. FRAME AT STA 1168 AT APPROX 3 O'CLOCK POSITION WAS CRACKED. REPAIRED AREA IAW DC9 SRM 53-01, FIG 2. - [SDR ABXR080073](https://openairdocs.org/sdr/ABXR080073), Feb 7, 2008: DOUBLER. CRACKED. DOUBLER SKIN BETWEEN STA 1132 AND 1143 WAS CRACKED AT BOTH CORNERS TO FASTENER HOLES. INSTALLED TWO DOUBLERS AT EACH CRACK LOCATION IAW DC9 SRM 53-01 FIG 2, SHE - [SDR ABXR080072](https://openairdocs.org/sdr/ABXR080072), Feb 6, 2008: FRAME. CRACKED. FRAME CRACKED STA 1076, LONGERON 14 RIGHT. REPAIRED FRAME IAW DC9 SRM 53-03, FIG 32, SHEET 4. - [SDR ABXR080071](https://openairdocs.org/sdr/ABXR080071), Feb 6, 2008: REPAIR. DAMAGED. AFT LOWER CARGO DOOR INNER PAN REPAIR AT THE AFT LOCK REQUIRED EVAL IAW AD 2006-10-14. REMOVED AND REPAIRED AREA IAW DC9 SRM 52-05, FIG 26B, 51-30-5, 51-30-2, A - [SDR ABXR080070](https://openairdocs.org/sdr/ABXR080070), Feb 5, 2008: DOOR. CRACKED. RIGHT MAIN LANDING GEAR INBOARD DOOR CRACKED, UPPER AFT CORNER. REPAIRED CRACKED AREA IAW DC9 REA D952-57026. - [SDR ABXR080069](https://openairdocs.org/sdr/ABXR080069), Feb 5, 2008: RIB. CRACKED. LEFT HORIZONTAL STAB LEADING EDGE NR 3 FROM INBOARD RIB CRACKED. INSTALLED SINGLE STACK REPAIR IAW DC9 ABX DWG K05159. - [SDR ABXR080068](https://openairdocs.org/sdr/ABXR080068), Feb 5, 2008: STRUCTURE. CRACKED. STRUCTURE UNDER FORWARD LOWER CARGO DOOR AFT ATTACH POINT AS SEEN THROUGH LIGHTENING HOLE WAS CRACKED. REPAIRED IAW REA D953-57015-MR. - [SDR ABXR080067](https://openairdocs.org/sdr/ABXR080067), Feb 5, 2008: FRAME. CORRODED. FRAME CORRODED ON AFT SIDE AT STA 350, LONGERON 30. REPAIRED CRACKED FRAME IAW DC9 SRM 53-03. - [SDR ABXR080066](https://openairdocs.org/sdr/ABXR080066), Feb 4, 2008: SUPPORT. CRACKED. RIGHT INBOARD SPOILER TORQUE TUBE INBOARD VERTICAL SUPPORT CRACKED AT UPPER END. REMOVED AND REPLACED SUPPORT IAW DC9 SRM 51-30-1, 51-30-2 AND 51-30-5. - [SDR ABXR080065](https://openairdocs.org/sdr/ABXR080065), Feb 2, 2008: SKIN. CORRODED. LEFT WING UPPER TRAILING EDGE SKIN BULGED, RIVETS CUPPED FORWARD OF SPOILER BOARDS (CENTER). CUT OUT DAMAGE. INSTALLED NEW SECTION OF SKIN AND -9 DOUBLER IAW DC - [SDR Y2PA200700026](https://openairdocs.org/sdr/Y2PA200700026), Nov 2, 2007: CSD. FAILED. CREW REPORTED ENGINE VIBRATION THEN FAILURE ON NR 2 ENGINE. IRREGULARITY FILLED OUT BY CREW REPORTED AS FOLLOWS. AFTER DEPARTURE IN CLIMB, VIBRATION FOLLOWED BY - [SDR Y2PA03025](https://openairdocs.org/sdr/Y2PA03025), Dec 9, 2003: RELAY. FAILED. CREW WORKING ELECTRICAL PROBLEM ON LT BUSS USING COM W/APU STARTED & RUNNING. APU LOW OIL PRESSURE LIGHT & OIL TEMP HIGH LIGHT ILLUM. APU SHUTDOWN. A/C OPS ON N ## 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 20021113034649I](https://openairdocs.org/incident/20021113034649I), Nov 13, 2002: Doug DC932F (N208US), Kansas City, MO. (-23) As jet usa flight 208 entered Kansas City airspace, enroute to Kansas City international airport, chicago center passed the flight over to Kansas City… --- 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.