Douglas DC-9-33F

Service difficulty reports · 1,681

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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 ABXA9900655Skin · crackedDURING C-CHECK, FOUND FUSELAGE EXTERIOR SKIN PANEL CRACKED IN TWO LOCATIONS, STATION 1121 AND 1132, AT 9 O'CLOCK POSITION. REPLACED SKIN IAW DC9 SRM 51-30-02.Aug 13, 1999 · N932AX · Doug DC933F · Fuselage Main, Plate/SkinSDR ABXA9900654Shear Tie · crackedDURING C-CHECK, FOUND SHEAR-TIIE CRACKED AT STATION 980 AND LONGERON 14 LEFT. REPLACED SHEAR-TIE IAW DC9 SRM 51-30-2, 51-30-5 AND ABX REA 953-32623.Aug 13, 1999 · N932AX · Doug DC933F · Fuselage Miscellaneous StructureSDR ABXA9900653Shear Tie · crackedDURING C-CHECK, FOUND SHEAR-TIE CRACKED AT STATION 1087 AND LONGERON LEFT. REPLACED SHEAR-TIE IAW DC9 SRM 51-10-2 AND 51-30-1.Aug 13, 1999 · N932AX · Doug DC933F · Fuselage Miscellaneous StructureSDR ABXA9900652Frame · crackedDURING C-CHECK, FOUND RIGHT MAIN FRAME CRACKED AT STATION 718. REPLACED MAIN FRAME IAW DC9 SERVICE BULLETIN 53-131 AND 53-182.Aug 13, 1999 · N932AX · Doug DC933F · Fuselage Main, FrameSDR ABXA9900651Angle · crackedDURING C-CHECK, FOUND FORWARD FACE OF AFT PRESSURE BULKHEAD, OUTBOARD LEFT ATTACH ANGLE, CRACKED AT LONGERON 15 LEFT. REPLACED ANGLE IAW DC9 SRM 51-30-1 AND 51-30-5.Aug 13, 1999 · N932AX · Doug DC933F · Fuselage Main, BulkheadSDR ABXA9900631Web · crackedDURING C-CHECK, FOUND RIGHT CUSP WEB CRACKED AT STATION 313 RBL 49. REPAIRED IAW DC9 SRM 53-01-00.Aug 3, 1999 · N932AX · Doug DC933F · Fuselage Miscellaneous StructureSDR ABXA9900630Bracket · crackedDURING C-CHECK, FOUND MAIN CARGO DOOR LOWER JAMB BRACKET CORRODED. REPLACED BRACKET IAW DC9 SRM 51-10-04.Aug 3, 1999 · N932AX · Doug DC933F · Fuselage Miscellaneous StructureSDR EIA990272Skin · crackedMZJ - DURING C-CHECK, CRACKS WERE FOUND ON THE RIGHT INBOARD MLG DOOR INNER SKIN PANEL. REPAIRED BY CUTTING AWAY INNER SKIN SECTION FORWARD OF STATION 746.027 AND SPLICING IN A NEW SECTION PER ECRA 942-52-005-2. (M)Aug 2, 1999 · N942F · Doug DC933F · Door Warning SystemSDR EIA990267Angle · damagedMZJ - DURING C-CHECK, OVERSIZE FASTENER HOLES WERE FOUND AT STATION 756 TO 832, STRINGER 18R TO 26R. FOUND AFTER REMOVAL OF JATO MOUNT BRACKETS. REMOVED DAMAGED RIB ANGLES, FABRICATED AND INSTALLED RIB ANGLES, DOUBLERS AND STRAPS PER ECRA 942-53-097-2. (M)Jul 29, 1999 · N942F · Doug DC933F · Fuselage Miscellaneous StructureSDR EIA990266Angle · damagedMZJ - DURING C-CHECK, OVERSIZE FASTENER HOLES WERE FOUND AT STATION 756 TO 832, STRINGER 18L TO 26L. FOUND AFTER REMOVAL OF JATO MOUNT BRACKETS. REMOVED DAMAGED RIB ANGLES, FABRICATED AND INSTALLED RIB ANGLES, DOUBLERS AND STRAPS PER ECRA 942-53-100-2. (M)Jul 29, 1999 · N942F · Doug DC933F · Fuselage Miscellaneous StructureSDR EIA990188Pedal · bindingKSEA - ON FLIGHT 823, CRWE REPORTED THAT ON TAKEOFF ROLL AT ABOUT 100 KTS AIRCRAFT BEGAN PULLING TO THE RIGHT. CAPTAIN APPLIED HEAVY LEFT FOOT PRESSURE ON THE LEFT RUDDER AND HEARD AN AUDIBLE SNAP. CAPTAIN THEN RELEASED PRESSURE ON PEDAL AND AIRCRAFT IMMEDIAJul 26, 1999 · N945F · Doug DC933F · Rudder Control SystemSDR EIA990271Panel · crackedMZJ - DURING C-CHECK, THE NR 1 ENGINE THRUST REVERSER INBOARD ACTUATOR PANEL WAS FOUND CRACKED. REPAIRED BY INSTALLING REPAIR DOUBLER PER DOUGLAS INSTRUCTION AND ECRA 942-78-098-2. (M)Jul 23, 1999 · N942F · Doug DC933F · Engine Thrust ReverserSDR EIAA990186Seat · misinstalledMMV - DURING EVALUATION, FOUND COURIER SEAT INSTALLED PER STC SA2398S0 DID NOT C/W THE 9G FORWARD REQUIREMENT OF FAR 25.561. COURIER SEAT DEACTIVATED PER EO 25-DC9-955-99. SEAT INSTALLATION WILL BE MODIFIED PER EIA EO 25-DC9-805-91. REV C. EO APPROVED BY 811Jul 22, 1999 · N945F · Doug DC933F · Flight Compartment EquipmentSDR EIAA990185Seat · misinstalledMMV - DURING EVALUATION, FOUND THAT COURIER SEAT INSTALLED PER STC SA 2398S0 DID NOT C/W THE 9G FORWARD REQUIREMENT OF FAR 25.561. COURIER SEAT IS DEACTIVATED PER EIA EO 25-DC9-955-99. SEAT INSTALLATION WILL BE MODIFIED PER EIA EO 25-DC9-805-91, REV C. EO APJul 22, 1999 · N944F · Doug DC933F · Flight Compartment EquipmentSDR EIAA990184Seat · misinstalledMMV - DURING EVALUATION, FOUND THAT COURIER SEAT INSTALLED PER STC SA2398S0 DID NOT C/W THE 9G FORWARD REQUIREMENT OF FAR 25.561. COURIER SEAT IS DEACTIVATED PER EIA EO 25-DC9-955-99. SEAT INSTALLATION WILL BE MODIFIED PER EIA EO 25-DC9-805-91, REV C. EO APJul 22, 1999 · N940F · Doug DC933F · Flight Compartment EquipmentSDR EIAA990183Seat · misinstalledDURING EVALUATION, FOUND THAT COURIER SEAT INSTALLED PER STC SA 2398S0 DID NOT C/W THE 9G FORWARD REQUIREMENT OF FAR 25.561. COURIER SEAT IS DEACTIVATED PER EIA EO 25-DC9-955-99. SEAT INSTALLATION WILL BE MODIFIED PER EIA EO-25-DC9-805-91, REV C. EO APPROVEDJul 22, 1999 · N933F · Doug DC933F · Flight Compartment EquipmentSDR EIA990187Drive Link · brokenAFTER LANDING AT PAJN, RIGHT ENGINE THRUST REVERSER WOULD NOT STOW. THRUST REVERSER DRIVE LINK P/N 5958782-503 FOUND BROKEN. (M)Jul 22, 1999 · N945F · Doug DC933F · Engine Thrust ReverserSDR EIA990274Skin · holeMZJ - DURING C-CHECK, A HOLE WAS FOUND IN THE RIGHT ELEVATOR LOWER SURFACE OUTBOARD END. REPAIRED BY REPLACING RIGHT ELEVATOR OUTBOARD LOWER SKIN PER DOUGLAS DRAWING NR 9918480 AND ECRA 942-55-083-2 AND SRM 51-30-2. (M)Jul 20, 1999 · N942F · Doug DC933F · Elevator, Plate/SkinSDR EIA990268Spar · bentDURING C-CHECK, THE LOWER HORIZONTAL FLANGE OF THE LEFT LOWER REAR SPAR CHORD AT XRS 169 WAS FOUND BENT. REPAIRED BY INSTALLING FILLER PER ECRA 942-57-073-2. (M)Jul 3, 1999 · N942F · Doug DC933F · Wing SparSDR EIAA990179Tire · failedON TAKEOFF ROLL AT APPROXIMATELY 60 - 80 KNOTS, AIRCRAFT EXPERIENCED SEVERE VIBRATION. APPEARED TO BE COMING FROM NOSE WHEEL. TAKEOFF ABORTED AND VIBRATIONS TOPPED AT APPROXIMATELY 25 KNOTS. (X)Jun 30, 1999 · N944F · Doug DC933F · TireSDR EIA990179Wheel · out of balanceSYR - ON TAKEOFF ROLL AT APPROX 60-80 KNOTS, AIRCRAFT EXPERIENCED SEVERE VIBRATION APPEARED TO BE COMING FROM NOSEWHEEL. TAKEOFF WAS ABORTED AND VIBRATION STOPPED AT APPROX 25 KNOTS. REPLACED NOSEWHEEL TIRES AFTER INSPECTION OF NOSE GEAR PER MM 32-40-2. (M)Jun 30, 1999 · N944F · Doug DC933F · Wheel/Ski/FloatSDR EIA990265Web · damagedMZJ - DURING C-CHECK, THE LEFT ELEVATOR REAR SPAR WEB WAS FOUND TO HAVE ELONGATED FASTENER HOLES. REPAIRED BY CUTTING OUT DAMAGE AND INSTALLING REPAIR SPLICE AND CHANNEL PER ECRA 942-55-072-2. (M)Jun 11, 1999 · N942F · Doug DC933F · Elevator StructureSDR EIA990264Longeron · damagedMZJ - DURING C-CHECK, DURING SKIN REPLACEMENT, NUMEROUS HOLES IN THE UPPER SKIN AND LONGERON AT STATION 1095, LONGERON 25R, WERE FOUND ELONGATED. REPAIRED BY TRIMMING THE ELONGATED HOLES AND INSTALLING REPAIR FILLERS AND DOUBLERS. (M)Jun 11, 1999 · N942F · Doug DC933F · Fuselage Main, Plate/SkinSDR EIA990263Rib · crackedMZJ - DURING C-CHECK, A 6 INCH CRACK WAS FOUND ON THE RIGHT TRAILING EDGE PYLON 2ND RIB INBOARD. REPAIRED BY TRIMMING RIB AND INSTALLING NEW SPLICE AND REPAIR DOUBLERS PER ECRA 942-55-020-2. (M)May 30, 1999 · N942F · Doug DC933F · Nacelle/Pylon, Frame/Spar/RibSDR EIAA990177Sill · chafedEAC - DURING C-CHECK, THE R5 DOOR CUT-OUT, UPPER INTERNAL SILL CONTACT AREA WAS FOUND TO HAVE CHAFE MARKS. BLENDED AREA PER SPM 53-30-01 FIG 1. FABRICATED NEW SHIM AND ALODINED PER SRM 31-10-02 PAGE 1. PRIMED NEW SHIM IAW SRM 30-40-05 PAGES 1-4. INSTALLED May 28, 1999 · N942F · Doug DC933F · Fuselage Miscellaneous StructureSDR EIA990262Press Panel · corrodedMZJ - DURING C-CHECK, A PRESSURE PANEL AT STATION 699 WAS FOUND TO HAVE EXFOLIATION CORROSION. REPAIRED BY TRIMMING PRESSURE PANEL AND NDT'ING AREA PER ECRA 942-53-049-2. (M)May 7, 1999 · N942F · Doug DC933F · Fuselage Miscellaneous StructureSDR EIA990261Doubler · crackedMZJ - DURING C-CHECK, A CRACK WAS FOUND IN THE FORWARD LOWER CARGO DOOR CUTOUT DOUBLER. CRACKED DOUBLER REPAIRED, ONE DOUBLER AND 2 FILLERS WERE INSTALLED PER ECRA 942-53-016-2. (M)May 7, 1999 · N942F · Doug DC933F · Fuselage Miscellaneous StructureSDR EIA990260Skin · misrepairedMZJ - DURING C-CHECK, SKIN REPAIRS BETWEEN STATION 332 TO 370, LONGERON 21R TO 26R, WERE FOUND TO BE UNACCEPTABLE. REMOVED AND RE-REPAIRED SKIN SECTION PER ECRA 942-53-008-2. (M)May 7, 1999 · N942F · Doug DC933F · Fuselage Main, Plate/SkinSDR EIA990270Frame · crackedMZJ - DURING C-CHECK, A 1 INCH CRACK WAS FOUND AT THE NR 5 TAILCONE RECEPTICLE SHEAR PIN ON THE LEFT SIDE OF THE STATION 1066 CANTED FRAME. REPAIRED BY INSTALLING REPAIR SPLICES PER ECRA 942-53-085-2. (M)May 6, 1999 · N942F · Doug DC933F · Fuselage Main, FrameSDR EIA990259Tail Pipe · crackedMZJ - DURING C-CHECK, THE APU TAIL TO EMPENNAGE WELD WAS FOUND CRACKED. PART WAS NDT'D AND STOP DRILLED PER DOUGLAS SRM 08-00-07. WELD WAS REPAIRED BY REPAIR STATION NR J3WR275J. ALL WORK ACCOMPLISHED WITH INSTRUCTIONS FROM ECRA942-49-006-2 AND BOEING ENGINMay 6, 1999 · N942F · Doug DC933F · APU Exhaust SystemSDR EIA990255Web · crackedMZJ - DURING C-CHECK, THE MAIN CABIN CUSP WEB, LOCATED AT STATION 420R, WAS FOUND CRACKED. REPAIRED CUSP WEB BY FABRICATING AND INSTALLING A REPAIR DOUBLER PER SRM 53-01 AND 51-30-1. (M)May 6, 1999 · N942F · Doug DC933F · Fuselage Miscellaneous StructureSDR EIAA990124Fitting · corrodedMZJ - DURING C-CHECK, THE RIGHT MLG FITTING BRACE ATTACH LUG FACE WAS FOUND CORRODED. REPAIRED PER ECRA NR 942-57-003-2. (X)May 5, 1999 · N942F · Doug DC933F · Wing Miscellaneous StructureSDR EIA990258Fitting · corrodedMZJ - DURING C-CHECK, THE LEFT MAIN LANDING GEAR FITTING SIDE BRACE ATTACH LUG WAS FOUND CORRODED ON AFT FACE. REMOVED CORROSION AND REPAIRED PER ECRA 942-57-003-2. (M)May 5, 1999 · N942F · Doug DC933F · Wing, Landing Gear Attach FittingsSDR EIA990257Skin · misrepairedMZJ - DURING C-CHECK, A FUSELAGE SKIN REPAIR BETWEEN STATION 446 TO 465, LONGERON 23L TO 26L, WAS EVALUATED AND FOUND TO BE AN UNACCEPTABLE REPAIR. REMOVED EFFECTED SECTION OF SKIN, COMPLETED REWORK OF SKIN REPAIR PER ECRA 942 53-1-0211 AND REINSTALLED. (M)May 5, 1999 · N942F · Doug DC933F · Fuselage Main, Plate/SkinSDR EIA990256Skin · misrepairedMZJ - DURING C-CHECK, A FUSELAGE SKIN REPAI AT STATION 737 TO 756, LONGERON 19R, WAS EVALUATED AND FOUND TO BE AN UNACCEPTABLE REPAIR. REMOVED EXISTING REPAIR, NDT'D AREA AND INSTALLED NEW FABRICATED DOUBLER PER ECRA 942-53-0111-2. (M)May 4, 1999 · N942F · Doug DC933F · Fuselage Main, Plate/SkinSDR EIAA990138Pan · crackedMZJ - DURING C-CHECK, A CRACK WAS FOUND IN THE WINDOW RING PAN, LOWER FORWARD CORNER, AT STA 579-L14R. FABRICATED REPAIR ANGLE AND INSTALLED PER ECRA 942-53-026-2. (X)May 2, 1999 · N942F · Doug DC933F · Fuselage Miscellaneous StructureSDR ABXA9900324Window · bindingFIRST OFFICER'S CLEARVIEW WINDOW (EMERG EXIT) WOULD NOT OPEN. LUBRICATED FIRST OFFICER'S CLEARVIEW WINDOW MECHANISM, OPERATED NORMAL IAW DC9 MM.Apr 27, 1999 · N931AX · Doug DC933F · Flight Compartment WindowsSDR EIAA990143Frame · misdrilledMZJ - DURING C-CHECK, THE SUPPORT FITTING AT STA 351, LONGERON 23R WAS FOUND TO HAVE A HOLE DRILLED IN RADIUS. ALSO, HOLE DRILLED IN FRAME RADIUS AT SAME LOCATION. REMOVED AND REPLACED NEW FITTING PER SRM 51-10-1 PAGES 4-6. FABRICATED DOUBLER AND SHIMS PER Apr 22, 1999 · N942F · Doug DC933F · Fuselage Main, FrameSDR EIAA990142Skin · corrodedDURING C-CHECK, THE RIGHT AND LEFT WING LEADING EDGE SKIN WAS FOUND TO HAVE CORROSION AT STA 515.156 (LT), STA 526.718 (RT), AND STA 464.750 (RT). REPAIRED PER ECRA NR 942-57-015-2. (X)Apr 21, 1999 · N942F · Doug DC933F · Wing, Plate/SkinSDR EIAA990174Skin · damagedMZJ - DURING C-CHECK, SKIN DAMAGE WAS FOUND ON THE RT FUSELAGE AT STA 446 BETWEEN L24 AND L25. HFEC INSPECTED THE TRIM-OUT IN THE SKIN FOR CRACKS AND CORROSION PER DOUGLAS NDT SPM, PART 6, 06-00-07, FIG 1. FABRICATED A REPAIR FILLER FROM 2014-T6 OR 2024-T3, Apr 14, 1999 · N942F · Doug DC933F · Fuselage Main, Plate/SkinSDR EIAA990175Fairing · crackedMZJ - DURING -CHECK, CRACKS WERE FOUND ON THE NR 2 ENGINE INBD AFT FAIRING AND DOUBLER. REPAIRED PER ECRA 942-78-004-2. REF: OPER CONTROL NR 99ZZZX4019. (X)Apr 13, 1999 · N942F · Doug DC933F · Nacelle/Pylon StructureSDR 99ZZZX4019Doubler · crackedMZJ - DURING -CHECK, CRACKS WERE FOUND ON THE NR 2 ENGINE INBD AFT FAIRING AND DOUBLER. REPAIRED PER ECRA 942-78-004-2. REF: OPER CONTROL NR EIAA990175.Apr 13, 1999 · N942F · Doug DC933F · Nacelle/Pylon StructureSDR EIAA990176Skin · crackedMZJ - DURING C-CHECK, A SMALL CRACK WAS FOUND ON THE INNER SKIN OF THE RT MAIN LANDING GEAR DOOR. CUT OUT CRACKED AREA OF DOOR INNER SKIN, NDT INSPECTED FORMER AND SKIN, NO CRACKS FOUND. FABRICATED FILLER AND DOUBLER, ALODINED, PRIMED AND INSTALLED WET WITH Apr 1, 1999 · N942F · Doug DC933F · Landing Gear DoorsSDR ABXA9900273Switch · intermittentRIGHT MAIN LANDING GEAR FAILED UPLATCH CHECK ON INITIAL TRY. RECYCLED GEAR, OPS CHECKED GOOD. REPLACED RIGHT MAIN LANDING GEAR UP LIMIT SWITCH.Mar 29, 1999 · N931AX · Doug DC933F · Landing Gear Retraction/Extension SystemSDR ABXA9900268Support · crackedDURING C-CHECK, FOUND RIGHT FLAP CARRIAGE OSCILLATING ROLLER SUPPORT CRACKED. REPLACED SUPPORT IAW DC9 OHM 27-50-7.Mar 22, 1999 · N931AX · Doug DC933F · Trailing Edge Flap Control SystemSDR ABXA9900267Bracket · crackedDURING C-CHECK, FOUND BRACKET CRACKED IN UPPER FORWARD CORNER OF MAIN CARGO DOOR. REPLACED BRACKET IAW DC9 SRM 51-30-1 AND 51-30-2.Mar 22, 1999 · N931AX · Doug DC933F · Passenger/Crew DoorsSDR ABXA9900266Fitting · crackedDURING C-CHECK, FOUND RIGHT WING INBOARD SLAT PULLEY ATTACH BRACKET CRACKED. REPLACED SUPPORT FITTING IAW DC9 SRM 51-10-4 AND 51-30-5.Mar 22, 1999 · N931AX · Doug DC933F · Leading Edge Slat Control SystemSDR ABXA9900265Splice · corrodedDURING C-CHECK, FOUND OUTBOARD FLOORBEAM TO FRAME SPLICE CORRODED AT STATION 965 LEFT. REPLACED SPLICE FITTING IAW DC9 SRM 51-30-5 AND 51-30-1.Mar 22, 1999 · N931AX · Doug DC933F · Fuselage Miscellaneous StructureSDR ABXA9900264Floorbeam · corrodedDURING C-CHECK, FOUND FLOORBEAM AT STATION 313 EXFOLIATED FROM BL 0 TO LBL 14. REPAIRED IAW REA D953-27121MR.Mar 22, 1999 · N931AX · Doug DC933F · Fuselage Main, Floor BeamSDR ABXA9900263Vane · delaminatedDURING C-CHECK, FOUND LEFT INBOARD FIXED VANE DELAMINATED. REPLACED LEFT INBOARD FIXED VANE IAW DC9 MM 27-51-3.Mar 22, 1999 · N931AX · Doug DC933F · Trailing Edge Flaps
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