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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR 20000615SH024Web · crackedDURING C-CHECK, FOUND ELONGATED HOLES AND CRACKS IN CUSP WEB BS 756 TO BS 775, LBL 44.5. CAUSE UNKNOWN. (X)SDR 20000615SH023Web · crackedDURING C-CHECK, FOUND ELONGATED HOLES, CORROSION, AND CRACKS IN CUSP WEB AT BS 756 TO BS 775, RBL 44.5. CAUSE UNKNOWN. (X)SDR ABXA000191Rheostat · shortedDURING DESCENT INTO BOS, ACRID FUMES EMITTED FROM THE FIRST OFFICER'S INSTRUMENT PANEL. REPLACED FIRST OFFICER'S BRIEFCASE LIGHT RHEOSTAT.SDR 20000615SH022Web · damagedDURING C-CHECK, FOUND ELONGATED HOLES IN CUSP WEB AT BS 503 TO BS 598,RBL 44.5. CAUSE UNKNOWN. (X)SDR 20000615SH021Floorbeam · corrodedDURING C-CHECK, FOUND CORROSION ON FLOORBEAM, PN 9958212-25 AT BS 756, APPROXIMATELY LBL 14.5. CAUSE UNKNOWN. (X)SDR 20000615SH020Web · damagedDURING C-CHECK, FOUND ELONGATED HOLES IN CUSP WEB AT BS 313 TO BS 389, RBL 44.5. CAUSE UNKNOWN. (X)SDR 20000615SH019Web · damagedDURING C-CHECK, FOUND ELONGATED HOLES IN CUSP WEB AT BS 389 TO BS 503, RBL 44.5. CAUSE UNKNOWN. (X)SDR 20000615SH018Web · crackedDURING C-CHECK, FOUND ELONGATED HOLES AND CRACKS IN CUSP WEB BS 218 TO BS 237, RBL 44.5. CAUSE UNKNOWN. (X)SDR 20000615SH017Web · crackedDURING C-CHECK, FOUND ELONGATED HOLES AND CRACKS IN CUSP WEB AT BS 237 TO BS 313, RBL 44.5. CAUSE UNKNOWN. (X)SDR 20000615SH016Floorbeam · gougedDURING C-CHECK, FOUND GOUGE IN FLOORBEAM WEB BS 100, RBL 10. CAUSE UNKNOWN. (X)SDR 20000615SH015Door Frame · damagedDURING C-CHECK, FOUND OVERSIZED HOLE IN AFT CARGO DOOR JAMB AT BS 937. CAUSE UNKNOWN. (X)SDR 20000615SH014Frame · tool damageDURING C-CHECK, FOUND HOLE AND DRILL MARKS IN FRAME BS 294 BETWEEN LONGERON L16 AND L18.SDR ABXA000152Battery · dischargedCOCKPIT EMERGENCY LIGHTS WERE INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT BATTERY POWER SUPPLY.SDR ABXA000173Intercostal · corrodedDURING C-CHECK, FOUND INTERCOSTAL CORRODED IN FORWARD LOWER CARGO COMPARTMENT BETWEEN STATION 484 AND 503 AT BL 0.0. REPLACED INTERCOSTAL IAW DC9 MM 51-30-02.SDR ABXA000172Intercostal · corrodedDURING C-CHECK, FOUND INTERCOSTAL CORRODED AT BL 0.0 BETWEEN STATION 503 AND 522. REPAIRED IAW DC9 SRM 51-30-02.SDR ABXA000167Floorbeam · corrodedDURING C-CHECK, FOUND FLOOR SUPPORT CORRODED AT STATION 1002 AND RBL 30. REPLACED FLOOR SUPPORT IAW DC9 SRM 51-30-2.SDR ABXA000170Hinge · crackedDURING C-CHECK, FOUND RIGHT FLAP OUTBOARD HINGE FITTING CRACKED. REPLACED FITTING IAW DC9 SRM 51-30-02.SDR ABXA000169Skin · delaminatedDURING C-CHECK, FOUND LEFT OUTBOARD SPOILER BOARD DELAMINATED INTERNALLY. REPLACED PANEL IAW DC9 MM 27-61-01.SDR ABXA000168Fitting · crackedDURING C-CHECK, FOUND VERTICAL SUPPORT FITTING CRACKED AT STATION 680 AT LBL 44. REPLACED VERTICAL SUPPORT FITTING IAW DC9 SRM 51-30-02.SDR ABXA000166Panel · corrodedDURING C-CHECK, FOUND THE OVER WHEEL WELL PRESSURE PANEL CORRODED AT STATION 718 AND BL 0.0. REPLACED PRESSURE PANEL IAW DC9 SRM 51-30-2 AND ABX REA D953-35901MR.SDR ABXA000165Floorbeam · crackedDURING C-CHECK, FOUND VERTICAL SUPPORT FITTING CRACKED AT STATION 680 FLOORBEAMAND RBL 44. REPLACED FITTING IAW DC9 SRM 51-30-2.SDR ABXA000164Pan · crackedDURING C-CHECK, FOUND MAIN ENTRY DOOR PAN CRACKED. REPAIRED IAW DC9 SRM 51-30-2.SDR ABXA000133Battery · dischargedDURING COCKPIT CHECK, EMERGENCY EVAC LIGHT FOUND NOT WORKING WHEN SWITCH WAS IN THE ON POSITION. REPLACED EMERGENCY LIGHT BATTERY SUPPLY IAW DC9 SMM 33-53-00. OPS CHECKED GOOD.SDR ABXA000131Frame · crackedRIGHT MAIN FRAME AT STATION 699 WAS CRACKED AT THE UPPER INBOARD, FORWARD FLANGE (PT.K - PT.J, REF: SERVICE SKETCH 2765B, SHEET 7). REPAIRED FRAME IAW ABX REA D953-35455MR.SDR ABXA000130Plate · crackedRIGHT HORIZONTAL STAB PLANK WAS CRACKED AT STRINGER NR 1 XHS 204 AND STRINGER NR 2 STATION FHS 244. REPAIRED PLANK IAW DC9 SRM 55-02, FIGURE 16.SDR ABXA000129Plate · crackedRIGHT HORIZONTAL STAB PLANK WAS CRACKED AT STRINGER NR 2 AND NR 3 STATION XFS 40.7 UPPER PLANK. REPAIRED PLANK IAW DC9 SRM 55-02, FIGURE 16.SDR ABXA000128Fitting · crackedRIGHT WHEEL WELL BULKHEAD TO KEEL VERTICAL FITTING AT STATION 718 WAS CRACKED. REPLACED FITTING IAW ABX REA D953-35458MR.SDR ABXA000127Yoke · corrodedNR 2 ENGINE FORWARD MOUNT YOKE ASSEMBLY WAS CORRODED. REPLACED YOKE ASSEMBY IAW DC9 MM 71-20-3.SDR ABXA000126Fitting · crackedAFT LOWER CARGO COMPARTMENT DOOR UPPER BEAM FORWARD END FITTING WAS CRACKED. REPLACED END FITTING IAW DC9 SRM 51-30-1 AND 51-30-5.SDR ABXA000125Tab · delaminatedRUDDER TAB HAD AREAS OF DELAMINATION AND SURFACE CORROSION. REPLACED RUDDER TAB IAW DC9 MM 27-20-2.SDR ABXA000124Fitting · crackedRIGHT HORIZONTAL STAB OUTBOARD END FITTING WAS CRACKED AT THE UPPER FORWARD FLANGE. REPLACED FITTING IAW DC9 SRM 51-30-1, 51-30-2, 51-30-5.SDR ABXA000123Frame · crackedLEFT MAIN FRAME STATION 718 WAS CRACKED AT THE FORWARD AND AFT UPPER INBOARD FLANGES EXTENDING INBOARD UNDER THE FLOORBEAM SPLICE ANGLES BETWEEN PT K - PT J AND RUNNING PAST PT 5, REF: SERVICE SKETCH 2765B, SHEET 7. REPLACED FRAME IAW ABX REA D953-35438MR.SDR ABXA000122Frame · crackedRIGHT MAIN FRAME STATION 737 WAS CRACKED BETWEEN SEAT TRACK SUPPORT BOLTS UPPER AFT INBOARD FLANGE (BETWEEN PT G AND PT J, REF: SERVICE SKETCH 2765B, SHEET 7). REPAIRED FRAME IAW ABX REA D953-35470MR.SDR ABXA000121Skin · corrodedFUSELAGE SKIN UNDER LEFT STATIC PORT PLATE WAS CORRODED. REPAIRED SKIN IAW DC9 SRM 53-04, FIGURE 3.SDR 2000ZZZX362Doubler · temporaryREMOVED THE EXISTING CLASS 2 REPAIR AND INSTALLED A CLASS 1 REPAIR AT LT STA 376.00 BETWEEN L22L AND L24L. REMOVED CLASS 2 REPAIRS AND INSTALLED CLASS 1 REPAIRS FROM LT STA 376.00 TO STA 395.00 BETWEEN L22L TO L24L PER EIA ECRA 941-53-090-2.SDR 2000ZZZX331Floorbeam · chafedAFT CARGO PIT STA 917 BL ZERO FLOORBEAM CHAFED. REPAIRED PER ECRA NR 941-53-094-2.SDR 2000ZZZX330Skin · gougedFORWARD PIT DOOR, DOOR EDGE, LOWER AFT, AND UPPER END FORWARD, HAS A GOUGE. INSTALLED REPAIR PER SRM 52-01 FIG 01 AND ECRA 941-52-091-2.SDR 2000ZZZX329Door Jamb · crackedCRACK FOUND ON AFT LOWER CORNER OF THE FORWARD SERVICE DOOR. DOOR JAMB CRACK COMING OUT OF AFT UPPER SCREW HOLE FOR SCUFF PLATE AND CORROSION UNDER SCUFF PLATE. REPAIRED PER ECRA 941-53-098-2 REV A.SDR 2000ZZZX328Skin · damagedREMOVED EXISTING REPAIR DOUBLER AT STA 737 BETWEEN L17-L18 RT SIDE FOR INSPECTION AND MEASURING BLENDED AREA PER ENGINEERING. REPAIRED PER ECRA 941-53-061-2.SDR 2000ZZZX327Frame · gougedINSIDE L-2 DOOR STA 185.0 LBL 44.5, TEE CHORD HAS .50 INCH LONG DEEP GOUGE ON TOP SIDE. REPAIR PER ECRA 941-53-088-2.SDR 2000ZZZX326Frame · crackedFRAME 718 RIGHT CRACKED ON FORWARD SIDE OF INTERMEDIATE POCKET, LOWER AFT RADIUS FROM FASTENER HOLE TO FASTENER HOLE UNDER CABIN FLOOR. REPLACED FRAME 718 RIGHT SIDE PER SB 53-131 AND ECRA 941-53-067-2.SDR 2000ZZZX325Skin · damagedRIGHT ELEVATOR LOWER SURFACE OUTBOARD END HAS A HOLE. REPLACED SKIN PER DOUGLAS DRAWING ECRA 942-55-083-2 REV A AND DC9 SRM.SDR 2000ZZZX324Frame · crackedFUSELAGE STATION 699 RIGHT AFT SIDE OF FRAME IN MID-POCKET. FRAME HAS THREE CRACKS LOCATED BENEATH FLOOR. REPLACED FRAME PER SB 53-131 REV 4.SDR 2000ZZZX323Splice · corrodedFUSELAGE STA 715 RIGHT BUTT LINE 58. CORROSION ON WEB. CORROSION ON FORWARD, LOWER SURFACE OF FRAME 718, SPLICE UNDER CABIN FLOOR. REPLACED FRAME STA 781, REPLACED WEB PER SB 53-131 REV 4 AND SRM 53-2, 51-30-5.SDR 2000ZZZX322Skin · misdrilledRIGHT SKIN AT STA 229 - STA 588 HAS A LOT OF DAMAGE AND INTERNAL DOUBLER HAS A HOLE FROM PREVIOUS REPAIR. REMOVED AND REPLACED SKINS AND INTERNAL DOUBLER PER ECRA 94-53-0003-3.SDR 2000ZZZX321Skin · misrepairedFUSELAGE SKIN REPAIR ON RIGHT OF FUSELAGE AT FS 168.750 OVERLAPPING SKIN PANEL BUTT JOINT ON LONGERON 26 NEEDS TO BE CHANGED FROM A CLASS 2 REPAIR TO A CLASS 1 REPAIR. REPAIRED PER ECRA 941-53-081-2.SDR 2000ZZZX320Skin · misrepairedCLASS 2 SKIN REPAIR AT RT STA 996, L28R AND L29R. REPAIRED EXISTING CLASS 2 SKIN REPAIR AT RIGHT STA 996, L28R AND L29R TO A CLASS 1 REPAIR PER EIA ECRA 941-53-051-2.SDR 2000ZZZX319Web · damagedDAMAGE ON THE CUSP WEB BETWEEN RT STA 313 AND STA 323 AT RBL 54. REPAIRED DAMAGED CUSP WEB BETWEEN RT STA 313 TO STA 323 AT RBL 54 PER EIA ECRA 941-53-087-2.SDR 2000ZZZX318Chord · gougedTEE CHORD AT STA 319, L19L HAS A GOUGE AND DENT DAMAGE. REPAIRED GOUGED TEE CHORD AT STA 319, L19L PER EIA ECRA 941-53-093-2.SDR 2000ZZZX317Door · damagedEXISTING EXTRA JOINT IN THE RIGHT WING BUTTE DOOR AT XRS 294. REPAIRED RT WING BUTTE DOOR HINGE AT XRS 294 PER EIA ECRA 941-57-082-2.
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