Douglas DC-9-33F

Service difficulty reports · 1,681

Newest first. General aviation reporting is voluntary.

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 aircraft_model_key = 'DC933F'
  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 20001103SH015Web · crackedDURING C-CHECK, FOUND WEB, CUSP CRACKED. (X)Sep 18, 2000 · N944F · Doug DC933F · Fuselage Miscellaneous StructureSDR 20001103SH014Web · corrodedDURING C-CHECK, FOUND CORROSION. (X)Sep 18, 2000 · N944F · Doug DC933F · Fuselage Miscellaneous StructureSDR 20001103SH012Web · crackedDURING C-CHECK, FOUND CRACK IN CUSP WEB. (X)Sep 18, 2000 · N944F · Doug DC933F · Fuselage Miscellaneous StructureSDR 20001103SH011Web · corrodedCORROSION FOUND DURING C-CHECK. (X)Sep 18, 2000 · N944F · Doug DC933F · Fuselage Miscellaneous StructureSDR ABXA000461Longeron · crackedLONGERON END CAP AT STATION 579 LONGERON 24 LEFT CRACKED. REPLACED END CAP IAW DC9 SRM 51-30-5 AND 51-30-2.Sep 14, 2000 · N931AX · Doug DC933F · Fuselage Main, Longeron/StringerSDR ABXA000418Light · inoperativeDURING PREFLIGHT INSPECTION, FOUND THE EMERGENCY LIGHTS INOPERATIVE. RESECURED WIRING TO OVERHEAD LIGHT SOCKET.Sep 14, 2000 · N934AX · Doug DC933F · Emergency LightingSDR ABXA000460Structure · corrodedSUBFLOOR UNDER PANEL 4431 CORRODED. REPAIRED SUBFLOOR IAW DC9 SRM 53-01.Sep 12, 2000 · N931AX · Doug DC933F · Fuselage Miscellaneous StructureSDR ABXA000459Doubler · crackedDOUBLER CRACKED AT LEADING EDGE LOWER SIDE BETWEEN NR 3 AND NR 4 SLAT TRACKS. REPLACED DOUBLER IAW DC9 SRM 51-30-2.Sep 12, 2000 · N931AX · Doug DC933F · Leading Edge DevicesSDR ABXA000458Skin · crackedBULGE WITH FOUR CRACKS AT STATION 579 LONGERON 25 LEFT. REPAIRED AREA IAW DC9 SRM 53-04.Sep 11, 2000 · N931AX · Doug DC933F · Fuselage Main, Plate/SkinSDR ABXA000457Pressure Panel · corrodedFLOOR SKIN UNDER COCKPIT PANEL 4431 HAD CORROSION THROUGHOUT. REPLACED PANEL IAW DC9 SRM 51-30-2 & 51-30-1.Sep 11, 2000 · N931AX · Doug DC933F · Fuselage Floor PanelSDR ABXA000456Longeron · corrodedEXTERNAL LONGERON 25 RIGHT AFT OF MAIN LANDING GEAR DOOR CUTOUT CORRODED. REPLACED LONGERON IAW DC9 SRM 51-30-2.Sep 11, 2000 · N931AX · Doug DC933F · Fuselage Main, Longeron/StringerSDR ABXA000455Angle · crackedINTERNAL DOUBLER CRACKED AT LEFT WING STATION 267 LEADING EDGE. REPLACED ANGLE IAW DC9 SRM 51-30-25, 51-10-4, 51-10-3, 51-30-2, AND DWG 9919326.Sep 8, 2000 · N931AX · Doug DC933F · Wing Miscellaneous StructureSDR ABXA000453Attach Fitting · crackedLEFT WING UPPER INBOARD TRAILING EDGE SEGMENT LOWER CENTER ATTACH FITTING CRACKED. REPLACED ATTACH FITTING IAW DC9 SRM 51-30-1.Sep 8, 2000 · N931AX · Doug DC933F · Wing, Attach FittingsSDR ABXA000452Spar · crackedLEFT WING SPAR WEB DOUBLER CRACKED AT STATION XRS 146. REPAIRED LEFT WING SPAR DOUBLER IAW DC9 SRM.Sep 8, 2000 · N931AX · Doug DC933F · Wing SparSDR ABXA000451Angle · corrodedUPPER CARGO T-ANGLE CORRODED AT STA 756, BUTT LINE 0 ON PRESSURE FLOOR. REPAIRED UPPER CARGO T-ANGLE IAW DC9 REA D953-38491-MR.Sep 8, 2000 · N931AX · Doug DC933F · Fuselage Miscellaneous StructureSDR EIA2000044Pump · inoperativeKSEA - FLT U823 - WITH RIGHT ENGINE THRUST LEVER AT FORWARD MECHANICAL STOP, EPR=1.80+- .04. RT N1 RPM INITIALLY AT 100 PERCENT, THEN DROPPED TO 94 PERCENT WHILE THRUST LEVER STILL AT STOP. POWER REDUCED FOR REJECTED TAKEOFF. REPLACED FUEL PUMP PER 73-11-1.Aug 31, 2000 · N941F · Doug DC933F · Engine Fuel PumpSDR EIA2000039Rod End · wornKSEA - ON CLIMB-OUT FROM PASI, PASSING 7,000 FT, AIRCRAFT YAWED TO RT WITH NO CHANGE IN POWER. AIRCRAFT REQUIRED 3 UNITS RT RUDDER TRIM TO LEVEL. UNPOWERED AND REPOWERED RUDDER WITH NO CHANGE. TURNED YAW DAMPER OFF THEN BACK ON. NO CHANGE. AIRCRAFT HANDLEAug 14, 2000 · N941F · Doug DC933F · Rudder Control SystemSDR ABXA000364Battery · dischargedEMERGENCY LIGHTS WOULD NOT TEST. REPLACED EMERGENCY LIGHT BATTERY POWER SUPPLY.Aug 7, 2000 · N935AX · Doug DC933F · Emergency LightingSDR 20000731SH031Frame · crackedSTA 1168 UPPER RIGHT SIDE, CANTED FRAME IS CRACKED. REPAIRED PER ECRA 940-53-52-2, CAUSE MAY BE DUE TO THE RUDDER PCU ACTUATOR FITTING ATTACHED TO THE FRAME IN THE SAME AREA. MAYBE SPECIAL INSPECTION CARD FOR THAT AREA. (X)Jul 31, 2000 · N940F · Doug DC933F · Fuselage Main, FrameSDR 20001106SH040Web · mismanufacturedDEVIATION FROM ENGINEERING DRAWING CONFIGURATION OF LIGHTENING HOLES IN FORWARD, LOWER CARGO DOOR CLOSE-OUT WEB (SINGLE FLANGE INSTEAD OF DOUBLE). (X)Jul 20, 2000 · N944F · Doug DC933F · Fuselage Miscellaneous StructureSDR EIA2000026Latch · out of adjKSEA - AFTER TAKEOFF, DURING UPLATCH CHECK, RIGHT MAIN GEAR EXTENDED. WITH GEAR HANDLE IN UP POSITION, RIGHT GEAR UNSAFE LIGHT WAS ON. LUBED AND RETORQUED CLEVIS AND LINK ASSY AT TORQUE TUBE. ADJUSTED LATCH ASSY PER MM 32-31-4. PERFORMED ADJUSTMENT/TEST PEJul 2, 2000 · N941F · Doug DC933F · Landing Gear Retraction/Extension SystemSDR 20000620SH020Web · corrodedDURING C-CHECK FOUND CORROSION ON CUSP WEB BS 937 TO BS 965, RBL 44.5. CAUSE UNKNOWN. (X)Jun 20, 2000 · N945F · Doug DC933F · Fuselage Miscellaneous StructureSDR 20000619SH016Web · crackedDURING C-CHECK, FOUND CRACKS AND CORROSION ON CUSP WEB BS 775 TO BS 897, RBL 44.5. CAUSE UNKNOWN. (X)Jun 19, 2000 · N945F · Doug DC933F · Fuselage Miscellaneous StructureSDR 20000619SH015Floorbeam · misdrilledDURING MAINTENANCE, THE FLOORBEAM AT BS 756, RBL 45, AND BS 737, RBL 45, WERE FOUND MISDRILLED. (X)Jun 19, 2000 · N945F · Doug DC933F · Fuselage Main, Floor BeamSDR 20000619SH013Bulkhead · crackedDURING C-CHECK, FOUND CRACK IN DOUBLER ON THE AFT PRESSURE BULKHEAD BS 996. CAUSE UNKNOWN. (X)Jun 19, 2000 · N945F · Doug DC933F · Fuselage Main, BulkheadSDR 20000619SH012Skin · dentedDURING C-CHECK, FOUND MULTIPLE DENTS IN FUSELAGE SKIN BS 351 TO BS 362, LONGERON 23R TO LONGERON 26R. CAUSE UNKNOWN. (X)Jun 19, 2000 · N945F · Doug DC933F · Fuselage Main, Plate/SkinSDR 20000619SH011Web · crackedDURING C-CHECK, TWO CRACKS WERE FOUND IN RHS CUSP WEB A BS 605 TO BS 617, RBL 44.5 TO RBL 60. CAUSE UNKNOWN. (INT)Jun 19, 2000 · N945F · Doug DC933F · Fuselage Miscellaneous StructureSDR 20000619SH009Web · crackedDURING C-CHECK, FOUND ELONGATED HOLES, CRACKS, AND CORROSION ON CUSP WEB AT BS 737 TO BS 756, RBL 44.5 AND RBL 60. (X)Jun 19, 2000 · N945F · Doug DC933F · Fuselage Miscellaneous StructureSDR 20000619SH010Web · corrodedDURING C-CHECK, FOUND ELONGATED HOLES, CRACKS, AND CORROSION ON CUSP WEB AT BS 737 TO BS 756, RBL 44.5 AND RBL 60. (X)Jun 18, 2000 · N945F · Doug DC933F · Fuselage Miscellaneous StructureSDR 20000615SH013Web · crackedDURING C-CHECK, FOUND CRACK IN CUSP WEB, BS 598, LBL 44.5. CAUSE UNKNOWN. (X)Jun 15, 2000 · N945F · Doug DC933F · Fuselage Miscellaneous StructureSDR EIA2000017Control Cable · dislodgedLCK - DURING TAXI, AILERON CONTROL BEGAN BINDING WITH RIGHT DEFLECTION. INSPECTED SYSTEM, FOUND LEFT SPOILER CONTROL CABLES RIDING ON TOP OF LEFT INBOARD SPOILER HYDRAULIC LINE. REMOVED CONTROL CABLES TO ORIGINAL POSITION. LUBED SPOILER SYSTEM IAW DC9 MM 12May 5, 2000 · N942F · Doug DC933F · Drag Control SystemSDR 20000619SH017Beam · crackedDURING C-CHECK, FOUND CRACK IN FORWARD CARGO DOOR HORIZONTAL BEAM, PN 9957663-13. CAUSED BY FASTENER TOOL. (X)Apr 18, 2000 · N945F · Doug DC933F · Fuselage Miscellaneous StructureSDR 20000619SH014Seat Track · crackedDURING C-CHECK, FOUND CRACK ON THE HORIZONTAL FLANGE OF SEAT TRACK, MAIN CABIN FLOOR. CAUSE UNKNOWN. (X)Apr 18, 2000 · N945F · Doug DC933F · Fuselage, Seat/Cargo Attach FittingsSDR 20000619SH008Structure · misdrilledDURING C-CHECK, FOUND MISLOCATED HOLES COMMON TO CUSP TEE AT BS 775, LBL 60. CAUSE UNKNOWN. (X)Apr 18, 2000 · N945F · Doug DC933F · Fuselage Miscellaneous StructureSDR 20000615SH040Floorboard · crackedDURING C-CHECK, FOUND FLOOR PANEL DENTED AND CRACKED IN TWO PLACES FROM BS 447 TO BS 452.5, BL ZERO. CAUSE UNKNOWN. (X)Apr 18, 2000 · N945F · Doug DC933F · Fuselage Floor PanelSDR 20000615SH039Structure · misdrilledDURING C-CHECK, FOUND MISLOCATED HOLES COMMON TO CUSP TEE AT BS 794, LBL 60. CAUSE UNKNOWN. (X)Apr 18, 2000 · N945F · Doug DC933F · Fuselage Miscellaneous StructureSDR 20000615SH038Floorboard · puncturedDURING C-CHECK, FOUND PUNCTURE IN FLOOR PANEL AT RT BS 516.5, RBL 10-26. CAUSE UNKNOWN. (X)Apr 18, 2000 · N945F · Doug DC933F · Fuselage Floor PanelSDR 20000615SH037Pan · damagedDURING C-CHECK, FOUND OVERSIZED FASTENER HOLE IN THE FORWARD ENTRANCE DOOR PAN AT LEFT BS 197.75 NEAR BEAM NR 1. CAUSE UNKNOWN. (X)Apr 18, 2000 · N945F · Doug DC933F · Passenger/Crew DoorsSDR 20000615SH036Longeron · misdrilledDURING C-CHECK, FOUND DOUBLE DRILLED HOLES ON FLANGE OF LONGERON L30 AT BS 340. CAUSE UNKNOWN. (X)Apr 18, 2000 · N945F · Doug DC933F · Fuselage Main, Longeron/StringerSDR 20000615SH035Skin · misdrilledDURING C-CHECK,, FOUND MISLOCATED HOLES IN FUSELAGE SKIN AT BS 951.8 TO BS 959.6, LONGERON L24. CAUSE UNKNOWN. (X)Apr 18, 2000 · N945F · Doug DC933F · Fuselage Main, Plate/SkinSDR 20000615SH034Web · crackedDURING C-CHECK, FOUND ELONGATED HOLES, CRACKS AND CORROSION ON CUSP WEB AT BS 775 TO BS 832, LBL 44.5. CAUSE UNKNOWN. (X)Apr 18, 2000 · N945F · Doug DC933F · Fuselage Miscellaneous StructureSDR 20000615SH033Bulkhead · misdrilledDURING C-CHECK, FOUND NUMEROUS HOLES MISLOCATED IN THE WEB AT RT BS 965 BETWEEN L7 AND L15. CAUSE UNKNOWN. (X)Apr 18, 2000 · N945F · Doug DC933F · Fuselage Main, BulkheadSDR 20000615SH032Web · crackedDURING C-CHECK, FOUND ELONGATED HOLES, CRACKS, AND CORROSION ON CUSP WEB AT BS 832 TO BS 897, LBL 44.5. CAUSE UNKNOWN. (X)Apr 18, 2000 · N945F · Doug DC933F · Fuselage Miscellaneous StructureSDR 20000615SH031Longeron · corrodedDURING C-CHECK, CORROSION DAMAGE WAS FOUND ON L29L AND L30. CAUSE UNKNOWN.Apr 18, 2000 · N945F · Doug DC933F · Fuselage Main, Longeron/StringerSDR 20000615SH030Web · crackedDURING C-CHECK, FOUND NUMEROUS CRACKS AND ELONGATED HOLES IN CUSP WEB AT BS 218 TO BS 237, LBL 44.5. CAUSE UNKNOWN. (X)Apr 18, 2000 · N945F · Doug DC933F · Fuselage Miscellaneous StructureSDR 20000615SH029Web · crackedDURING C-CHECK, FOUND NUMEROUS CRACKS AND ELONGATED HOLES IN CUSP WEB AT BS 237 TO BS 313. CAUSE UNKNOWN. (X)Apr 18, 2000 · N945F · Doug DC933F · Fuselage Miscellaneous StructureSDR 20000615SH028Seat Track · misdrilledDURING C-CHECK, FOUND MISLOCATED HOLES IN SEAT TRACK AT BS 266 TO BS 455, LBL 54.0. CAUSE UNKNOWN. (X)Apr 18, 2000 · N945F · Doug DC933F · Fuselage, Seat/Cargo Attach FittingsSDR 20000615SH027Floorboard · damagedDURING C-CHECK, FOUND ELONGATED HOLES IN CABIN FLOOR PANEL NR 14, PN 5922429-37. CAUSE UNKNOWN. (X)Apr 18, 2000 · N945F · Doug DC933F · Fuselage Floor PanelSDR 20000615SH026Floorbeam · misdrilledDURING C-CHECK, FOUND MIS-DRILLED HOLE IN UPPER CAP OF FUSELAGE FLOORBEAM AT BS 427, LBL 37. (X)Apr 18, 2000 · N945F · Doug DC933F · Fuselage Main, Floor BeamSDR 20000615SH025Floorboard · crackedDURING C-CHECK, FOUND ELONGATED FASTENER HOLES AND CRACKS IN CAPTAIN''S FLOOR PANEL, PN 9910078-3. CAUSE UNKNOWN. (X)Apr 18, 2000 · N945F · Doug DC933F · Fuselage Floor Panel
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