N208US, cancelled Jun 21, 2023

Service difficulty reports · 41

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

Query with SQL
duckdb -csv -c "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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR Y2PA201809250032Skin Panel · corrodedDURING 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 UPSep 25, 2018 · N208US · Doug DC932F · Fuselage Main, Plate/SkinSDR Y2PA2016022800004Landing Gear · malfunctionedDURING 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 DIDFeb 25, 2016 · N208US · Doug DC932F · Landing Gear Position and WarningSDR Y2PA20130511039Line · failedCREW 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 May 11, 2013 · N208US · Doug DC932F · Engine Oil Distribution (Airframe Furnished)SDR Y2PA20130507036Skin · crackedDURING 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.May 6, 2013 · N208US · Doug DC932F · Trailing Edge FlapsSDR Y2PA20130507035Hinge · crackedDURING 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.May 6, 2013 · N208US · Doug DC932F · Trailing Edge FlapsSDR Y2PA20130507034Bracket · corrodedDURING C-CHECK INSPECTION, MX DISCOVERED THE MAIN UPPER CARGO DOOR LOWER SILL BRACKET CORRODED. MX R & R BRACKET IAW SRM 51-30-5.May 6, 2013 · N208US · Doug DC932F · Fuselage Miscellaneous StructureSDR Y2PA20130507033Panel · delaminatedDURING C-CHECK INSPECTION, MX DISCOVERED THE INBD LT T/E WING PANEL DELAMINATED. MX R & R PANEL WITH SERVICEABLE IAW SRM 51-30-2.May 6, 2013 · N208US · Doug DC932F · Wing, Plate/SkinSDR Y2PA20130507032Panel · delaminatedDURING 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.May 6, 2013 · N208US · Doug DC932F · Wing, Plate/SkinSDR Y2PA20130507031Tee Fitting · corrodedDURING 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.May 6, 2013 · N208US · Doug DC932F · Fuselage Main, Attach FittingsSDR Y2PA20130507029Longeron · corrodedDURING 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.May 6, 2013 · N208US · Doug DC932F · Fuselage Main, Longeron/StringerSDR Y2PA20130507028Sleeve · crackedDURING C-CHECK INSPECTION, MX DISCOVERED BOTH LT AND RT HORIZONTAL STABILIZER HINGE BOLT SLEEVES CRACKED. MX R & R SLEEVES IAW AMM 55-10-0.May 6, 2013 · N208US · Doug DC932F · Horizontal Stabilizer StructureSDR Y2PA20130507027Skin · corrodedDURING 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.May 6, 2013 · N208US · Doug DC932F · Fuselage Main, Plate/SkinSDR Y2PA20130507026Web · corrodedDURING 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.May 6, 2013 · N208US · Doug DC932F · Fuselage Miscellaneous StructureSDR Y2PA20130507025Window Frame · crackedDURING 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.May 6, 2013 · N208US · Doug DC932F · Fuselage Main, StructureSDR Y2PA20130507024Spar · crackedDURING 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.May 6, 2013 · N208US · Doug DC932F · Elevator, Spar/RibSDR Y2PA2011092000024Battery Pack · dischargedEMERGENCY LIGHTS INOPERATIVE DURING INSP. MX R & R BATTERY POWER SUPPLY IAW AMM 33-50-0. OPS CHECKS GOOD, NO OTHER DEFECTS NOTED.Sep 16, 2011 · N208US · Doug DC932F · Emergency LightingSDR Y2PA2010111500028Downlock Switch · malfunctionedUPON 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 SHONov 10, 2010 · N208US · Doug DC932F · Landing Gear Position and WarningSDR ABXR080086Rib · crackedRIB CRACKED AT FASTENERS LEFT AND RIGHT SIDES OF VERT STAB LEADING EDGE ZFS 18. REPAIRED IAW DC9 SSRM DWG K05159.Feb 14, 2008 · N208US · Doug DC933F · Vertical Stabilizer, Spar/RibSDR ABXR080085Rib · crackedRIB CRACKED AT FASTENERS LEFT AND RIGHT SIDES OF VERT STAB LEADING EDGE ZFS 50. REPAIRED IAW DC9 SSRM DWG K05159.Feb 14, 2008 · N208US · Doug DC933F · Vertical Stabilizer, Spar/RibSDR ABXR080082Rib · crackedRIB CRACKED AT FASTENER LEFT SIDE VERT STABILIZER LEADING EDGE ZFS 93. REPAIRED RIB IAW DC9 SRM D05159.Feb 14, 2008 · N208US · Doug DC933F · Vertical Stabilizer, Spar/RibSDR ABXR080084Rib · crackedRIB CRACKED AT FASTENERS LEFT AND RIGHT VERT STAB LEADING EDGE ZFS 43. REPAIRED IAW DC9 SSRM DWG K05159.Feb 14, 2008 · N208US · Doug DC933F · Vertical Stabilizer, Spar/RibSDR ABXR080081Rib · crackedRIB CRACKED AT FASTENER LEFT SIDE OF VERTICAL STAB LEADING EDGE XFS 148. REPAIRED IAW DC9 SSRM DWG K05159.Feb 14, 2008 · N208US · Doug DC933F · Vertical Stabilizer, Spar/RibSDR ABXR080078Rib · crackedRIB CRACKED AT FASTENERS LEFT AND RIGHT SIDES OF VERTICAL STAB LEADING EDGE ZFS 50. REPAIRED IAW DC9 SSRM DWG K05159.Feb 14, 2008 · N208US · Doug DC933F · Vertical Stabilizer, Spar/RibSDR ABXR080077Rib · crackedRIB CRACKED AT FASTENERS LEFT AND RIGHT SIDE OF VERTICAL STAB LEADING EDGE ZFS 43. REPAIRED IAW DC9 SSRM DWG K05159.Feb 14, 2008 · N208US · Doug DC933F · Vertical Stabilizer, Spar/RibSDR ABXR080076Rib · crackedRIB CRACKED AT FASTENERS LEFT AND RIGHT SIDES OF VERTICAL STAB LEADING EDGE ZFS 18. REPAIRED IAW DC9 SSRM DWG K05159.Feb 14, 2008 · N208US · Doug DC933F · Vertical Stabilizer, Spar/RibSDR ABXR080075Rib · crackedRIB CRACKED AT FASTENER RIGHT SIDE OF VERTICAL STAB LEADING EDGE ZFS 23. REPAIRED IAW DC9 SSRM DWG K05159.Feb 14, 2008 · N208US · Doug DC933F · Vertical Stabilizer, Spar/RibSDR ABXR080083Rib · crackedRIB CRACKED AT FASTENERS LEFT AND RIGHT SIDES OF VERT STAB LEADING EDGE ZFS 18. REPAIRED IAW DC9 SSRM DWG K05159.Feb 14, 2008 · N208US · Doug DC933F · Vertical Stabilizer, Spar/RibSDR ABXR080080Rib · crackedRIB CRACKED AT FASTENERS LEFT AND RIGHT SIDES OF VERTICAL STAB LEADING EDGE ZFS 74. REPAIRED LEFT AND RIGHT RIBS IAW DC9 SSRM K05159.Feb 14, 2008 · N208US · Doug DC933F · Vertical Stabilizer, Spar/RibSDR ABXR080079Rib · crackedRIB CRACKED AT FASTENER RIGHT SIDE OF VERTICAL STAB LEADING EDGE ZFS 80. REPAIRED RIB IAW DC9 SSRM K05159.Feb 14, 2008 · N208US · Doug DC933F · Vertical Stabilizer, Spar/RibSDR ABXR080074Frame · crackedFRAME AT STA 1168 AT APPROX 3 O'CLOCK POSITION WAS CRACKED. REPAIRED AREA IAW DC9 SRM 53-01, FIG 2.Feb 7, 2008 · N208US · Doug DC933F · Fuselage Main, FrameSDR ABXR080073Doubler · crackedDOUBLER 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.Feb 7, 2008 · N208US · Doug DC933F · Fuselage Main, Plate/SkinSDR ABXR080072Frame · crackedFRAME CRACKED STA 1076, LONGERON 14 RIGHT. REPAIRED FRAME IAW DC9 SRM 53-03, FIG 32, SHEET 4.Feb 6, 2008 · N208US · Doug DC933F · Fuselage Main, FrameSDR ABXR080071Repair · damagedAFT 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.Feb 6, 2008 · N208US · Doug DC933F · Cargo/Baggage DoorsSDR ABXR080070Door · crackedRIGHT MAIN LANDING GEAR INBOARD DOOR CRACKED, UPPER AFT CORNER. REPAIRED CRACKED AREA IAW DC9 REA D952-57026.Feb 5, 2008 · N208US · Doug DC933F · Landing Gear DoorsSDR ABXR080069Rib · crackedLEFT HORIZONTAL STAB LEADING EDGE NR 3 FROM INBOARD RIB CRACKED. INSTALLED SINGLE STACK REPAIR IAW DC9 ABX DWG K05159.Feb 5, 2008 · N208US · Doug DC933F · Horizontal Stabilizer, Spar/RibSDR ABXR080068Structure · crackedSTRUCTURE UNDER FORWARD LOWER CARGO DOOR AFT ATTACH POINT AS SEEN THROUGH LIGHTENING HOLE WAS CRACKED. REPAIRED IAW REA D953-57015-MR.Feb 5, 2008 · N208US · Doug DC933F · Fuselage Miscellaneous StructureSDR ABXR080067Frame · corrodedFRAME CORRODED ON AFT SIDE AT STA 350, LONGERON 30. REPAIRED CRACKED FRAME IAW DC9 SRM 53-03.Feb 5, 2008 · N208US · Doug DC933F · Fuselage Main, FrameSDR ABXR080066Support · crackedRIGHT 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.Feb 4, 2008 · N208US · Doug DC933F · SpoilersSDR ABXR080065Skin · corrodedLEFT 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.Feb 2, 2008 · N208US · Doug DC933F · Wing, Plate/SkinSDR Y2PA200700026Csd · failedCREW 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 EMERGENCYNov 2, 2007 · N208US · Doug DC932F · Engine (Turbine/Turboprop)SDR Y2PA03025Relay · failedCREW 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. AIDec 9, 2003 · N208US · Doug DC932F · Airborne Auxiliary Power Unit (APU) System
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