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 2000ZZZX316Web · dentedTRIMMED OUT DENT ON FORWARD CARGO COMPARTMENT WEB AT STA 427.00 BETWEEN L24R TO L26R. REPAIRED FORWARD CARGO COMPARTMENT WEB AT STA 427 BETWEEN L24R TO L26R PER EIA ECRA 941-53-080-2.Feb 8, 2000 · N941F · Doug DC933F · Fuselage Miscellaneous StructureSDR 2000ZZZX315Skin · gougedGOUGES ON THE FUSELAGE SKIN BELOW THE AIRSTAIR DOOR. REPAIRED LEFT FUSELAGE EXTERNAL SKIN AT STA 160 TO STA 200 UNDER THE AIRSTAIR DOOR PER EIA ECRA 941-53-078-2.Feb 8, 2000 · N941F · Doug DC933F · Fuselage Main, Plate/SkinSDR 2000ZZZX314Intercostal · gougedGOUGE IN INTERCOSTAL AT STA 180.00, RBL 21. REPAIRED INTERCOSTAL GOUGE AT STA 180, RBL 21 PER EIA ECRA 941-53-079-2.Feb 8, 2000 · N941F · Doug DC933F · Fuselage Miscellaneous StructureSDR 2000ZZZX313Skin · crackedCRACKED AREA OF FUSELAGE SKIN NEAR STA 1810, L23L. REPAIRED FUSELAGE SKIN DOUBLER AT STA 1018, L23L PER EIA ECRA 941-53-062-2 REV A.Feb 8, 2000 · N941F · Doug DC933F · Fuselage Main, Plate/SkinSDR 2000ZZZX312Frame · crackedCRACK IN THE LEFT FRAME AT STA 1037. REPAIRED FUSELGE FRAME AT STA 1037 BETWEEN L12L TO L13L PER EIA ECRA 941-53-053-2.Feb 8, 2000 · N941F · Doug DC933F · Fuselage Main, FrameSDR 2000ZZZX311Fitting · damagedTHREE OVERSIZED HOLES IN THE RT MAIN LANDING GEAR FITTING. REPAIRED RIGHT MAIN LANDING GEAR FITTING OVERSIZED HOLES PER EIA ECRA 941-57-055-2.Feb 8, 2000 · N941F · Doug DC933F · Main Landing GearSDR 2000ZZZX310Frame · misdrilledDOUBLE-DRILLED HOLE TO THE VERTICAL STABILIZER FRAME AT STA YV 247.750, ZV 140.825. REPAIRED DOUBLE-DRILLED HOLE ON VERTICAL STABILIZER FRAME AT STA YV 247.750, ZV 140.825 PER EIA ECRA 941-52-053-2 REV A.Feb 8, 2000 · N941F · Doug DC933F · Vertical StabilizerSDR 2000ZZZX309Web · crackedCRACK DAMAGE ON THE CUSP WEB AT LEFT AFT STA 579, LBL 54.00. REPAIRED LEFT AFT CUSP WEB AT STA 579, LBL 54, PER EIA ECRA 941-53-052-2 REV A.Feb 8, 2000 · N941F · Doug DC933F · Fuselage Miscellaneous StructureSDR 2000ZZZX308Intercostal · corrodedFORWARD ENTRY DOOR LOWER SILL 9957838-3 INTERCOSTAL FOUND CORRODED AT THE NUTPLATE LOCATIONS. WHILE GAINING ACCESS THROUGH THE UPPER CUSP ANGLE, THE LOWER CUSP ANGLE WAS DAMAGED. REPAIRED FORWARD ENTRY DOOR LOWER SILL UPPER AND LOWER CUSP ANGLES PER EIA ECRFeb 8, 2000 · N941F · Doug DC933F · Fuselage Miscellaneous StructureSDR 2000ZZZX307Stringer · misrepairedTWO EXISTING UNAPPROVED REPAIR CHANNELS ON THE LT HORIZONTAL STABILIZER UPPER PANEL AT STR 6 AT XHS 25 AND XHS 37. REPAIRED LT HORIZONTAL STABILIZER UPPER PANEL STRINGER AT XHS 25 AND XHS 37, L6 PER EIA ECRA 941-55-059-2.Feb 8, 2000 · N941F · Doug DC933F · Horizontal Stabilizer, Spar/RibSDR 2000ZZZX306Skin · misrepairedNON-DOCUMENTED DOUBLERS AT FUSELAGE RIGHT STA 927 AND STA 936. REPAIRED RT FUSELAGE SKIN AT STA 927 AND STA 936, BETWEEN L14R AND L15R PER EIA ECRA 941-53-083-2 REV B.Feb 8, 2000 · N941F · Doug DC933F · Fuselage Main, Plate/SkinSDR 2000ZZZX305Rib · crackedDAMAGE TO THE XHS 86.00 RIB IN THE RT HORIZONTAL STABILIZER FORWARD UPPER END WHILE GAINING ACCESS TO AN UNCONFIRMED CRACK. CRACK WAS LATER FOUND TO BE AN ANOMALIE ONLY. REPAIRED RT HORIZONTAL STABILIZER RIB DAMAGE AT XHS 86 PER EIA ECRA 941-55-013-2 REV A.Feb 8, 2000 · N941F · Doug DC933F · Horizontal Stabilizer, Spar/RibSDR 2000ZZZX304Fitting · corrodedCORROSION DAMAGE FOUND IN 5 BOLT HOLES COMMON TO THE LT AND RT MAIN LANDING GEAR FITTINGS. REPAIRED LT AND RT MAIN LANDING GEAR FITTINGS PER EIA ECRA 941-57-065-2 REV A.Feb 8, 2000 · N941F · Doug DC933F · Main Landing GearSDR 2000ZZZX303Frame · misdrilledMISDRILLED HOLE AT LEFT FRAME STA 870.00 L6L. REPAIRED MISDRILLED HOLE AT LEFT FRAME STA 870, L6L PER EIA ECRA 941-53-020-2.Feb 8, 2000 · N941F · Doug DC933F · Fuselage Main, FrameSDR 2000ZZZX302Frame · misdrilledMISDRILLED HOLE AT RT FRAME STA 870.00 L6R. REPAIRED MISDRILLED HOLE AT RIGHT FRAME STA 870 L6R PER EIA ECRA 941-53-019-2.Feb 8, 2000 · N941F · Doug DC933F · Fuselage Main, FrameSDR 2000ZZZX301Bulkhead · crackedELONGATED FASTENER HOLES, GOUGE AND CRACK DAMAGE ASSOCIATED WITH THE AFT PRESSURE BULKHEAD TEE CHORD SPLICE AT L6L TO L8L. REQUIRED AFT PRESSURE BULKHEAD TEE CHORD AT STA 996 BETWEEN L6L TO L8L PER EIA ECRA 941-53-077-2 REV A.Feb 8, 2000 · N941F · Doug DC933F · Fuselage Main, BulkheadSDR 2000ZZZX300Door Frame · crackedA 0.5 INCH CRACK WAS FOUND IN THE RADIUS OF THE SERVICE DOOR FRAME. DURING REPAIR, A FASTENER WAS FOUND WITH A 0.15 INCH EDGE MARGIN MEASURED FROM THE CENTER OF THE FASTENER HOLE TO THE EDGE OF THE FITTING. REPAIRED FORWARD GALLEY SERVICE DOOR NR 2 HORIZONTAFeb 8, 2000 · N941F · Doug DC933F · Fuselage Main, FrameSDR 2000ZZZX299Web · crackedCRACK IN THE FASTENER HOLE ON THE CUSP WEB AT RIGHT STA 343.60, RBL 42. REPAIRED FASTENER HOLE ON CUSP WEB AT RIGHT STA 343.60, RBL 42 PER ECRA 941-53-057-2.Feb 8, 2000 · N941F · Doug DC933F · Fuselage Miscellaneous StructureSDR 2000ZZZX298Cargo Rack · puncturedPUNCTURE IN THE DUAL CARGO TRACK AT LEFT STA 522.00, LBL 24.00. REPAIRED A PUNCTURE IN THE DUAL CARGO TRACK AT STA 522, LBL 24 PER EIA ECRA 941-53-048-2.Feb 8, 2000 · N941F · Doug DC933F · Fuselage, Seat/Cargo Attach FittingsSDR 2000ZZZX297Frame · misdrilledMISDRILLED HOLE AT RIGHT FRAME STA 718, L6R. REPAIRED MISDRILLED HOLE AT RIGHT FRAME STA 718, L6R PER EIA ECRA 941-53-023-2.Feb 8, 2000 · N941F · Doug DC933F · Fuselage Main, FrameSDR 2000ZZZX296Frame · misdrilledMISDRILLED HOLE AT RIGHT FRAME STA 332.00 L6R. REPAIRED MISDRILLED HOLE AT RT FRAME STA 332 L6R PER EIA ECRA 941-53-064-2.Feb 7, 2000 · N941F · Doug DC933F · Fuselage Main, FrameSDR 2000ZZZX295Frame · misdrilledMISDRILLED HOLE AT RT FRAME STA 908.00 L6R. REPAIRED MISDRILLED HOLE AT RT FRAME STA 908 L6R PER EIA ECRA 941-53-039-2.Feb 7, 2000 · N941F · Doug DC933F · Fuselage Main, FrameSDR 2000ZZZX294Rivets · misinstalledOVERLAPPING RIVETS ON THE INTERCOSTALS AT VARIOUS LOCATIONS. REPAIRED OVERLAPPING RIVETS ON THE INTERCOSTALS AT LT STA'S 617, 465, 945, 927, 908, 889, 851, 832, 813, 794 775, 756, 737, 718, 699, 639, 560, 541, AND 256 L6L. RT STA'S 639, 617, 313, 699, 484, 4Feb 7, 2000 · N941F · Doug DC933F · Fuselage Miscellaneous StructureSDR 2000ZZZX293Structure · damagedPREVIOUSLY PLUGGED HOLE WITH SHORT EDGE DISTANCE AND GOUGE ON THE RT FORWARD EMERGENCY EXIT DOOR. REPAIRED PREVIOUSLY PLUGGED HOLE WITH SHORT EDGE DISTANCE AND GOUGE ON THE RT FORWARD EMERGENCY EXIT DOOR PER EIA ECRA 941-52-058-2.Feb 7, 2000 · N941F · Doug DC933F · Emergency ExitsSDR 2000ZZZX292Skin · damagedREPAIRED THE PREVIOUS REPAIR ON THE LT WING LEADING EDGE AT XFS 575.5. REPAIRED PREVIOUS FLUSH REPAIR ON THE LT WING LEADING EDGE AT XFS 575.5 PER EIA ECRA 941-57-009-2 REV A.Feb 7, 2000 · N941F · Doug DC933F · Wing, Plate/SkinSDR 2000ZZZX291Door · damagedDAMAGE ON THE RIGHT WING NR 4 LEADING EDGE SLAT DOOR AT WS X0S 240.081. REPAIRED DAMAGE ON THE RT WING NR 4 L/E SLAT DOOR AT WS X05 240.081 PER DIA ECRA 941-57-089-2.Feb 7, 2000 · N941F · Doug DC933F · Accessory Compartment DoorsSDR 2000ZZZX290Fitting · damagedELONGATED HOLE IN MAIN DECK CARGO DOOR TORQUE TUBE FITTING. REPAIRED UPPER CARGO DOOR TORQUE TUBE AT STA 380 BETWEEN L4L TO L5L PER EIA ECRA 941-53-072-2.Feb 7, 2000 · N941F · Doug DC933F · Cargo/Baggage DoorsSDR 2000ZZZX289Web · puncturedPUNCTURE DAMAGE COMMON TO THE CUSP MEMBRANE BETWEEN STA 452 TO ST 455. REPAIRED RT FUSELAGE CUSP MEMBRANE/WEB PUNTURE BETWEEN STA 452 TO STA 456 PER EIA ECRA 541-53-012-2.Feb 7, 2000 · N941F · Doug DC933F · Fuselage Miscellaneous StructureSDR 2000ZZZX288Skin · dentedDENT DAMAGE FOUND BELOW THE MAIN DECK CARGO DOOR, FORWARD AND ABOVE THE PRESSURE RELIEF VALVES. REPAIRED FUSELAGE SKIN DENT AT STA 320 BETWEEN L18L TO L19L PER EIA ECRA 941-53-014-2 REV A.Feb 7, 2000 · N941F · Doug DC933F · Fuselage Main, Plate/SkinSDR 2000ZZZX287Skin · damagedAPPROVAL FOR AN EXISTING REPAIR ON THE FUSELAGE SKIN AT STA 58.750 L19L. REPAIR REMOVED A CRACK COMMON TO THE SKIN AT THE STA 58.750 FRAME. REPAIRED FUSELAGE SKIN EXTERNAL DOUBLER AT STA 58.750 L18L TO L19L PER EIA ECRA 941-53-005-2.Feb 7, 2000 · N941F · Doug DC933F · Fuselage Main, Plate/SkinSDR 2000ZZZX286Pan · crackedCRACK DAMAGE ON THE LOWER AFT CARGO DOOR INNER AND OUTER PAN. REPAIRED LOWER AFT CARGO DOOR INNER AND OUTER PAN PER EIA ECRA 941-52-102-2.Feb 7, 2000 · N941F · Doug DC933F · Cargo/Baggage DoorsSDR 2000ZZZX284Spar · corrodedRIGHT WING REAR SPAR VERTICAL LEG AT STA 267.0 HAS HEAVY CORROSION. REPAIRED BY TRIMMING UPPER CAP BETWEEN XRS 180.1 AND XRS 319.5. NEW SECTION SPLICED IN PER SB 57-179 AND ECRA 941-57-015-2.Feb 7, 2000 · N941F · Doug DC933F · Wing SparSDR EIA2000012Trim Motor · noisyLCK - PILOT REPORTS STAB TRIM MAKES A GRINDING NOISE WHEN TRIMMING AIRCRAFT TO NOSE DOWN POSITION. (M)Feb 6, 2000 · N941F · Doug DC933F · Elevator Tab Control SystemSDR 20000503SH046Bulkhead · dentedREPAIRS TO FORWARD, LEFT COCKPIT PRESSURE WEB PANEL FROM BS 69 TO BS 83.5 BY REMOVAL OF DAMAGED AREA AND INSTALLATION OF FILLER, DOUBLERS, AND TRIPLER. (EIA ECRA 940-53-042-2).Feb 4, 2000 · N940F · Doug DC933F · Fuselage Main, BulkheadSDR 20000503SH045Skin · crackedCRACK REPAIR AT RT WING LEADING EDGE, STA XIS 188 BY REMOVAL OF DAMAGE AND INSTALLATION OF FILLER, INTERNAL DOUBLER AND EXTERNAL DOUBLER (EIA ECRA 940-57 (044-2). (X)Feb 4, 2000 · N940F · Doug DC933F · Wing, Plate/SkinSDR 20000503SH044Rib · corrodedCORROSION REPAIRS TO FORWARD, LT COCKPIT PRESSURE FLOOR RIB BY REPLACEMENT (EIA ECRA 940-53-045-2). (X)Feb 4, 2000 · N940F · Doug DC933F · Fuselage Miscellaneous StructureSDR 20000503SH042Web · crackedREPAIR FOR CRACKS IN CUSP WEB AT BS 598 TO BS 658, RBL 44.5 BY REPLACEMENT (EIA ECRA 940-53-036-2). (X)Feb 4, 2000 · N940F · Doug DC933F · Fuselage Miscellaneous StructureSDR 20000503SH041Web · crackedREPAIRS TO CUSP WEB FOR CACKS AT BS 438, RBL 45 BY REPLACEMENT (EIA ECRA 940-53-037-2). (X)Feb 4, 2000 · N940F · Doug DC933F · Fuselage Miscellaneous StructureSDR 20000503SH040Web · crackedREPAIRS FOR CRACKS AND ELONGATED HOLES IN CUSP WEB FROM BS 294 TO BS 313, RBL 45 BY REPLACEMENT (EIA ECRA 940-53-039-2). (X)Feb 4, 2000 · N940F · Doug DC933F · Fuselage Miscellaneous StructureSDR 20000503SH039Web · crackedREPAIR FOR CRACKS IN CUSP WEBS AT BS 389, RBL 45 BY REPLACEMENT OF 2 EACH (-11 AND -13) CUSP WEBS. (EIA ECRA 940-53-038-2). (X)Feb 4, 2000 · N940F · Doug DC933F · Fuselage Miscellaneous StructureSDR 20000503SH038Web · crackedREPAIR FOR CRACKS IN CUSP WEBS AT BS 389, RBL 45, BY REPLACEMENT OF 2 EACH (-11 AND -13) CUSP WEBS. (EIA ECRA 940-53-038-2). (X)Feb 4, 2000 · N940F · Doug DC933F · Fuselage Miscellaneous StructureSDR 20000503SH037Web · crackedCRACKS AND ELONGATED HOLES IN BS 503 TO BS 580, LBL 54 CUSP WEB. REPLACED PANEL. (EIA ECRA 940-53-031-2). (X)Feb 4, 2000 · N940F · Doug DC933F · Fuselage Miscellaneous StructureSDR 20000503SH036Web · crackedREPAIRS FOR CRACKS AND ELONGATED HOLES IN CUSP WEB FROM BS 218 TO BS 237, LBL 45.5 BY REPLACEMENT. (EIA ECRA 940-53-040-2). (X)Feb 4, 2000 · N940F · Doug DC933F · Fuselage Miscellaneous StructureSDR 20000503SH035Web · damagedREPAIR OF ELONGATED HOLES IN CUSP WEB FROM BS 237 TO BS 313, LBL 50 BY REPLACEMENT OF WEB. (EIA ECRA 940-53-032-2). (X)Feb 4, 2000 · N940F · Doug DC933F · Fuselage Miscellaneous StructureSDR 20000503SH033Bulkhead · crackedREPAIR OF GOUGES IN AFT PRESSURE BULKHEAD AT BS 1017 (CAUSED BY CONTROL CABLES CHAFING STRUCTURE). (EIA ECRA 940-53-027-2). (X)Feb 4, 2000 · N940F · Doug DC933F · Fuselage Main, BulkheadSDR 20000503SH032Floorboard · crackedREPAIR OF CRACK IN CABIN FLOOR BOARD AT BS 237 TO BS 503, LBL 39 (EIA ECRA 940-53-028-2). (X)Feb 4, 2000 · N940F · Doug DC933F · Fuselage Floor PanelSDR 20000503SH031Floorboard · crackedREPAIRS TO FLOOR PANEL FOR DENTS AND CRACKS FROM BS 237 TO BS 484, BL ZERO TO RBL 14 PER EIA ECRA 940-53-049-2. (X)Feb 4, 2000 · N940F · Doug DC933F · Fuselage Floor PanelSDR 20000503SH030Skin · corrodedREPAIRS FOR CORROSION TO LT COCKPIT SKIN FROM BS 69 TO BS 94, BETWEEN LONGERONS L17 AND L18 BY REMOVAL OF DAMAGE AND INSTALLATION OF FILLER AND INTERNAL AND EXTERNAL DOUBLERS (EIA ECRA 940-53-050-2). (X)Feb 4, 2000 · N940F · Doug DC933F · Fuselage Main, Plate/SkinSDR 20000503SH029Doubler · crackedCRACK IN 501 DOUBLER REPAIRED BY SPLICE OF NEW SECTION (EIA ECRA 940-53-026-2). (X)Feb 4, 2000 · N940F · Doug DC933F · Fuselage Main, Plate/SkinSDR 20000503SH028Skin · dentedREPAIR FOR DENTS AND GOUGES IN ACFT SKIN BY INSTALLATION OF DOUBLERS AND TRIPLERS IN LARGER AREA THAN REQUIRED PER DOUGLAS SB DC9-53-276 IAW EIA ECRA 940-53-024-2. (X)Feb 4, 2000 · N940F · Doug DC933F · Fuselage Main, Plate/Skin
Back to Douglas DC-9-33F