# Service difficulty reports: N208US, cancelled Jun 21, 2023 A list on [N208US, cancelled Jun 21, 2023](https://openairdocs.org/deregistered/N208US-2023-06-21.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR Y2PA201809250032](https://openairdocs.org/sdr/Y2PA201809250032.md): Skin Panel · corroded · Sep 25, 2018 · N208US · Doug DC932F · Fuselage Main, Plate/Skin > 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, LONGERON 18R-23R. REMOVED AND REINSTALLED MIDDLE SKIN FROM LONGERON 15R-18R. REMOVED AND REINSTALLED UP - [SDR Y2PA2016022800004](https://openairdocs.org/sdr/Y2PA2016022800004.md): Landing Gear · malfunctioned · Feb 25, 2016 · N208US · Doug DC932F · Landing Gear Position and Warning > 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 GREEN. DECLARED EMERGENCY AND RAN COM EMERGENCY GEAR EXTENSION PROCEDURE. NOSE GEAR LIGHT STILL DID - [SDR Y2PA20130511039](https://openairdocs.org/sdr/Y2PA20130511039.md): Line · failed · May 11, 2013 · N208US · Doug DC932F · Engine Oil Distribution (Airframe Furnished) > 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 DECREASING, NORMAL CHECKLIST COMPLETED & ABNORMAL CHECKLIST LEADING TO A PRECAUTIONARY SHUTDOWN. CREW - [SDR Y2PA20130507036](https://openairdocs.org/sdr/Y2PA20130507036.md): Skin · cracked · May 6, 2013 · N208US · Doug DC932F · Trailing Edge Flaps > 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.md): Hinge · cracked · May 6, 2013 · N208US · Doug DC932F · Trailing Edge Flaps > 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.md): Bracket · corroded · May 6, 2013 · N208US · Doug DC932F · Fuselage Miscellaneous Structure > 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.md): Panel · delaminated · May 6, 2013 · N208US · Doug DC932F · Wing, Plate/Skin > 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.md): Panel · delaminated · May 6, 2013 · N208US · Doug DC932F · Wing, Plate/Skin > 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.md): Tee Fitting · corroded · May 6, 2013 · N208US · Doug DC932F · Fuselage Main, Attach Fittings > 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.md): Longeron · corroded · May 6, 2013 · N208US · Doug DC932F · Fuselage Main, Longeron/Stringer > 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.md): Sleeve · cracked · May 6, 2013 · N208US · Doug DC932F · Horizontal Stabilizer Structure > 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.md): Skin · corroded · May 6, 2013 · N208US · Doug DC932F · Fuselage Main, Plate/Skin > 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, 8110-3, DATED 3/19/13. - [SDR Y2PA20130507026](https://openairdocs.org/sdr/Y2PA20130507026.md): Web · corroded · May 6, 2013 · N208US · Doug DC932F · Fuselage Miscellaneous Structure > 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.md): Window Frame · cracked · May 6, 2013 · N208US · Doug DC932F · Fuselage Main, Structure > 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 FRAME WITH NEW IAW SB 53-290 R3, DWG SR09530268, SRM 51-30-2 AND 51-30-5. - [SDR Y2PA20130507024](https://openairdocs.org/sdr/Y2PA20130507024.md): Spar · cracked · May 6, 2013 · N208US · Doug DC932F · Elevator, Spar/Rib > 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 27-30-2. - [SDR Y2PA2011092000024](https://openairdocs.org/sdr/Y2PA2011092000024.md): Battery Pack · discharged · Sep 16, 2011 · N208US · Doug DC932F · Emergency Lighting > 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.md): Downlock Switch · malfunctioned · Nov 10, 2010 · N208US · Doug DC932F · Landing Gear Position and Warning > 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 EMERGENCY INBOUND. CREW FOLLOWED COM PROCEDURES FOR MANUAL EXTENSION OF GEAR AND SECONDARY SYS SHO - [SDR ABXR080086](https://openairdocs.org/sdr/ABXR080086.md): Rib · cracked · Feb 14, 2008 · N208US · Doug DC933F · Vertical Stabilizer, Spar/Rib > 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.md): Rib · cracked · Feb 14, 2008 · N208US · Doug DC933F · Vertical Stabilizer, Spar/Rib > 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.md): Rib · cracked · Feb 14, 2008 · N208US · Doug DC933F · Vertical Stabilizer, Spar/Rib > 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.md): Rib · cracked · Feb 14, 2008 · N208US · Doug DC933F · Vertical Stabilizer, Spar/Rib > 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.md): Rib · cracked · Feb 14, 2008 · N208US · Doug DC933F · Vertical Stabilizer, Spar/Rib > 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.md): Rib · cracked · Feb 14, 2008 · N208US · Doug DC933F · Vertical Stabilizer, Spar/Rib > 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.md): Rib · cracked · Feb 14, 2008 · N208US · Doug DC933F · Vertical Stabilizer, Spar/Rib > 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.md): Rib · cracked · Feb 14, 2008 · N208US · Doug DC933F · Vertical Stabilizer, Spar/Rib > 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.md): Rib · cracked · Feb 14, 2008 · N208US · Doug DC933F · Vertical Stabilizer, Spar/Rib > 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.md): Rib · cracked · Feb 14, 2008 · N208US · Doug DC933F · Vertical Stabilizer, Spar/Rib > 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.md): Rib · cracked · Feb 14, 2008 · N208US · Doug DC933F · Vertical Stabilizer, Spar/Rib > 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.md): Rib · cracked · Feb 14, 2008 · N208US · Doug DC933F · Vertical Stabilizer, Spar/Rib > 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.md): Frame · cracked · Feb 7, 2008 · N208US · Doug DC933F · Fuselage Main, Frame > 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.md): Doubler · cracked · Feb 7, 2008 · N208US · Doug DC933F · Fuselage Main, Plate/Skin > 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, SHEET 3. - [SDR ABXR080072](https://openairdocs.org/sdr/ABXR080072.md): Frame · cracked · Feb 6, 2008 · N208US · Doug DC933F · Fuselage Main, Frame > 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.md): Repair · damaged · Feb 6, 2008 · N208US · Doug DC933F · Cargo/Baggage Doors > 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, AND ST-6244-03. - [SDR ABXR080070](https://openairdocs.org/sdr/ABXR080070.md): Door · cracked · Feb 5, 2008 · N208US · Doug DC933F · Landing Gear Doors > 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.md): Rib · cracked · Feb 5, 2008 · N208US · Doug DC933F · Horizontal Stabilizer, Spar/Rib > 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.md): Structure · cracked · Feb 5, 2008 · N208US · Doug DC933F · Fuselage Miscellaneous Structure > 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.md): Frame · corroded · Feb 5, 2008 · N208US · Doug DC933F · Fuselage Main, Frame > 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.md): Support · cracked · Feb 4, 2008 · N208US · Doug DC933F · Spoilers > 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.md): Skin · corroded · Feb 2, 2008 · N208US · Doug DC933F · Wing, Plate/Skin > 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 DC9 SRM 57-30-3, 57-01, FIG 3, 51-30-2 AND 51-30-5. - [SDR Y2PA200700026](https://openairdocs.org/sdr/Y2PA200700026.md): Csd · failed · Nov 2, 2007 · N208US · Doug DC932F · Engine (Turbine/Turboprop) > 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 NR 2 ENGINE FLAME OUT AT FL190 FOLLOWED BY AIRCRAFT CROSSTIE LOCKOUT. CREW DECLARED AN EMERGENCY - [SDR Y2PA03025](https://openairdocs.org/sdr/Y2PA03025.md): Relay · failed · Dec 9, 2003 · N208US · Doug DC932F · Airborne Auxiliary Power Unit (APU) System > 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 NR 2 GEN & BATTERIES. AN EMERGENCY DECLARED, A/C GIVEN DIRECT TO SDF & VECTORED FOR APPROACH. AI ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE n_number = 'N208US' AND deregistration_id = 'N208US-2023-06-21' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N208US-2023-06-21/reports --- 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.