Douglas DC-8-73F
Service difficulty reports · 15,471
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 = 'DC873F' 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 = 'DC873F' 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 UPS01836240Longeron · crackedINSPECTION TYPE:C2 AFT PIT LONGERON 34L CRACKED FS 1482-1487. REMOVED DAMAGED PART OF LONGERON, INSTALLED NEW PART OF LONGERON AND NEW SPLICE.SDR RRXA11323Frame · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO FRAME AT STA.55 AND L24R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-20D, 51-1-11, 53-SDR UPS01836350Longeron · crackedINSPECTION TYPE:C2 STA 1773 LONG 17R IS CRACKED. REPAIRED LONGERON IAW SRM 53-2-3 FIG 5.SDR RRXA11379Fitting · crackedDURING A MAINTENANCE VISIT FOUND R/H WING CTR L/E STA XFS 404-400 FITTING CRACKED. *** CORRECTIVE ACTION *** REMOVED AND REPLACED FITTING IAW DWG # 5770409, SRM 51-1-20, 51-1-21 AND 51-1-21ASDR RRXA11378Fitting · crackedDURING A MAINTENANCE VISIT FOUND CPIT L31L SPLICE FITTING CRACKED. *** CORRECTIVE ACTION *** REMOVED AND REPLACED FITTING IAW SRM 51-1-20DSDR RRXA11377Frame · crackedDURING A MAINTENANCE VISIT FOUND FRAME STA 55 L24L CRACKED. *** CORRECTIVE ACTION *** REMOVED DAMAGED AREA IAW SRM 53-3-3, FABRICATED AND INSTALLED REPLACEMENT PARTS IAW SRM 53-3-3 FIG 3, 51-1-21 AND 51-1-20D.SDR RRXA010056Pad · failedON DEPARTURE GEAR HANDLE UP NOSE GEAR HAD EXTREME NO ISE AS IF NOSE WHEELS WERE SPINNING AND RUBBING. ALSO HAD EXTREME VIBRATION, GEAR HANDLE PUT BACK DOWN, VIBRATION CONTINUED WITH GEAR DOWN, WHEN ACFT BANKED IN FLT NOSE GEAR HAD LOUD BANG. BOTH GEAR UP INDISDR UPS01836355Spar Cap · crackedINSPECTION TYPE:C2 RIGHT HORIZONTAL STAB UPPER FORMER/CAP IS CRACKED AT XFS 47.5. REMOVED AND REPLACED CAP IAW DWG 5654549 AND SRM 55-1-0, 51-1-20D, 51-1-21, 51-3-0.SDR UPS01836323Doubler · crackedINSPECTION TYPE:C2 RIGHT WING INTERNAL DOUBLER IS CRACKED AT XFS 597.5. REMOVED, FABRICATED AND REPLACED DOUBLER IAW DWG 5769600 AND SRM 51-1-20D, 51-1-21.SDR UPS01836238Fitting · crackedINSPECTION TYPE:C2 AFT PIT STA 1240 BETWEEN L35R-L34R FITTING CRACKED. REMOVED CRACKED FITTING IAW DC8 SRM 51-1-20D, REC'D LOCATED AND DRILLED NEW FITTING IAW DC8 SRM 51-1-24 AND INSTALLED IAW DC8 SRM 51-1-20D.SDR DHL2001801008Flow Valve · failedAT CRUISE ALTITUDE IN BOTH AUTO AND MANUAL PRESSURIZATION AT ALL FLOW SETTINGS, CABIN CLIMBS AND DESCENDS UP TO 700 FPM AND WILL NOT STABILIZE AT CONSTANT PRESSURE LT MANIFOLD PRESSURE FLUCTUATES 3 PSI IN CRU.FOUND LT FLOW CONTROL VALVE TO INTERMITTENT/INOP INSDR RRXA11376Fitting · corrodedDURING A MAINTENANCE VISIT FOUND C PI BATH TUB FITTING STA 1180 L33R - L34R HAS LITE CORROSION. REMOVED BATH TUB IAW SRM 51-1-20D. REMOVED CORROSION, TREATED AND PRIMED IAW SRM 51-1-8 AND 53-2-0 FIG 1F. INSTALLED REPLACEMENT PARTS IAW SRM51-1-20 AND DWG 375SDR RRXA11373Rib · crackedDURING A MAINTENANCE VISIT FOUND R/H CTR L/E XFS 329.0 LWR WAS CRACKED. *** CORRECTIVE ACTION *** REMOVED AND REPLACED RIB AND REINSTALLED IAW SRM 51-1-20D AND DWG 5769530-54.SDR RRXA11322Wedge · dentedDURING A MAINTENANCE VISIT FOUND DENTED DAMAGE TO L/H O/B FLAP T/E WEDGE AT STA.340-410, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21.SDR UPS01836378Fitting · crackedINSPECTION TYPE:C2 STA 1690 LONG 33R END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4641326 AND SRM 51-3-1, 51-1-21.SDR UPS01836377Floorbeam · corrodedINSPECTION TYPE:C2 STA 1580 LBL 24 FLOORBEAM IS CORRODED BEYOND LIMITS. REPAIRED FLOORBEAM IAW 8110-3 APPROVED DH SK 807-644.SDR UPS01836362Skin · crackedINSPECTION TYPE:C2 RIGHT WING UPPER SKIN IS CRACKED AT XRS 79 AT STRINGER 15. REPAIRED SKIN IAW SRM 57-2-1 FIG 10.SDR UPS01836361Skin · crackedINSPECTION TYPE:C2 RIGHT WING UPPER SKIN IS CRACKED AT XRS 79 AT STRINGER 9. REPAIRED SKIN IAW SRM 57-2-1 FIG 10.SDR UPS01836360Skin · crackedINSPECTION TYPE:C2 RIGHT WING UPPER SKIN IS CRACKED AT XRS 74 STRINGER 10. REPAIRED SKIN IAW SRM 57-2-1 FIG 10.SDR UPS01836359Skin · crackedINSPECTION TYPE:C2 RIGHT WING UPPER SKIN IS CRACKED AT STA XRS 79. REPAIRED SKIN IAW SRM 57-2-1 FIG 10.SDR UPS01836354Seat Track · corrodedINSPECTION TYPE:C2 STA 1620 - 1660 SEAT TRACK IS CORRODED BEYOND LIMITS AT BL 0. REPAIRED SEAT TRACK IAW SRM 53-2-3 FIG 8A.SDR UPS01836352Rib · crackedINSPECTION TYPE:C2 LEFT WING L/E UPPER RIB IS CRACKED AT XFS 678.75. REPAIRED RIB IAW SRM 57-2-0 FIG 2.SDR UPS01836336Skin · corrodedINSPECTION TYPE:C2 RIGHT WING LOWER L/E SKIN IS CORRODED BEYOND LIMITS AT XFS 722. REPAIRED SKIN IAW SRM 57-2-0 FIG 2A.SDR UPS01836335Skin · crackedINSPECTION TYPE:C2 RIGHT WING UPPER SKIN IS CRACKED AT XRS 105 AT STRINGER 14. REPAIRED SKIN IAW SRM 57-2-1 FIG 10.SDR UPS01836331Frame · crackedINSPECTION TYPE:C2 STA 1680 FRAME IS CRACKED AT LONG 21R. REPAIRED FRAME IAW SRM 53-2-0 FIG 2.SDR UPS01836330Doubler · brokenINSPECTION TYPE:C2 LEFT WING LOWER FRONT SPAR STRAP AND DOUBLER ARE BROKEN AT XS 520. REMOVED, FABRICATED AND REPLACED DOUBLER AND STRAP IAW SRM 57-2-1 FIG 14A.SDR UPS01836328Fitting · crackedINSPECTION TYPE:C2 STA 1690 LONG 35R END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4641326 AND SRM 51-1-20D.SDR UPS01836327Skin · crackedINSPECTION TYPE:C2 LEFT WING L/E LOWER SKIN IS CRACKED AT XFS 597.5. REPAIRED SKIN IAW EO DC8-5720-4087.SDR UPS01836326Fitting · crackedINSPECTION TYPE:C2 STA 320 BANANA FITTING IS CRACKED AT 27L. REMOVED AND REPLACED FITTING IAW DWG 3754041 AND SRM 51-1-20D, 51-1-21.SDR UPS01836324Fitting · crackedINSPECTION TYPE:C2 STA 1690 LONG 22L END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4641326 AND SRM 51-1-20D, 51-1-21.SDR UPS01836321Gusset · crackedINSPECTION TYPE:C2 STA 1240 UPPER GUSSET IS CRACKED AT LONG 34R. REMOVED, FABRICATED AND REPLACED GUSSET IAW DWG 9758507 AND SRM 53-1-0, 51-1-20D.SDR RRXA11375Skin · crackedDURING A MAINTENANCE VISIT FOUND R/H WING L/E STA XFS 300 LWR SKIN CRACKED AT FASTENER HOLE. *** CORRECTIVE ACTION *** REPAIRED SKIN IAW 8110-3 APPROVED DH SK 873-883SDR RRXA11374Doubler · corrodedDURING A MAINTENANCE VISIT FOUND FUSELAGE BULGED, POSSIBLE INTERNAL CORROSION @ L21R STA 25 - 8. *** CORRECTIVE ACTION *** REMOVED FASTENER, REMOVED CORRODED DOUBLER. FABRICATED AND INSTALLED REPLACEMENT PART IAW DWG 561386-5613861 AND SRM 51-1-21-1 AND 51-SDR UPS01836379Spar Cap · crackedINSPECTION TYPE:C2 STA 855 LT WING REAR SPAR LOWER CAP IS CRACKED FROM XCW 0 TO XCW 10. REPAIRED SPAR IAW 8110-3 APPROVED DH SK 807-357.SDR UPS01836358Longeron · crackedINSPECTION TYPE:C2 STA 940 - 960 LONG 24L IS CRACKED. REPAIRED LONGERON IAW SRM 53-2-2 FIG 5.SDR UPS01836357Skin · crackedINSPECTION TYPE:C2 STA 1600 AT LONG 20L FWD LOWER CORNER OF L-2 DOOR FUSELAGE SKIN IS CRACKED. REPAIRED SKIN IAW SRM 53-2-0 FIG 18.SDR UPS01836356Skin · crackedINSPECTION TYPE:C2 STA 160 LONG 10R FUSELAGE SKIN IS CRACKED AT FWD UPPER CORNER OF R-1 DOOR OPENING. REPAIRED SKIN IAW SRM 53-2-0 FIG 14.SDR UPS01836351Rib · crackedINSPECTION TYPE:C2 LEFT WING L/E LOWER RIB IS CRACKED AT XFS 397.75. REPAIRED RIB IAW SRM 57-2-0 FIG 2.SDR UPS01836334Skin · crackedINSPECTION TYPE:C2 STA 1620 LONG 20R LOWER FWD CORNER SKIN IS CRACKED AT R-2 DOOR. REPAIRED SKIN IAW SRM 53-2-0 FIG 17.SDR UPS01836333Skin · crackedINSPECTION TYPE:C2 RIGHT WING L/E UPPER SKIN IS CRACKED AT XFS 572.5. REPAIRED SKIN IAW SRM 57-2-1 FIG 38.SDR UPS01836332Web · crackedINSPECTION TYPE:C2 STA 354 CUSP MEMBRANE IS CRACKED AT LONG 21L. REPAIRED MEMBRANE IAW SRM 53-2-0 FIG 1B.SDR UPS01836329Skin · crackedINSPECTION TYPE:C2 RIGHT WING L/E UPPER SKIN IS CRACKED AT XFS 200. REPAIRED SKIN IAW SRM 57-2-0 FIG 2.SDR UPS01836322Rib · crackedINSPECTION TYPE:C2 LEFT WING L/E LOWER RIB IS CRACKED AT XFS 341. REPAIRED RIB IAW SRM 57-2-0 FIG 2.SDR UPS01836319Skin · crackedINSPECTION TYPE:C2 COMPLY WITH EO DC8-5330-12073-A, STA 25 LONG 10L FOUND TWO SKIN CRACKS AFTER DOUBLER WAS REMOVED. REPAIRED SKIN IAW SRM 53-2-0 FIG 15.SDR RRXA11321Intercostal · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO INTERCOSTAL AT STA.355, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21, 57-3-3, 51-1-20D.SDR RRXA11320Angle · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO ANGLE AT D-PIT DOOR JAMB LOWER SEAL DEPRESSOR, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 5SDR UPS01836353Skin · crackedINSPECTION TYPE:C2 FUSELAGE SKIN IS CRACKED AT STA 1766 AT LONG 15R. REPAIRED SKIN IAW SRM 53-2-1 FIG 7.SDR RRXA11372Seat Track · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION ON SEAT TRACK MAIN CABIN STA 550-590 LBL48 - LBL63. *** CORRECTIVE ACTION *** REMOVED AND REPLACED CORRODED FASTENER IAW SRM51-3-0. SPLICED CORRODED SEAT TRACK IAW SRM 53-2-3 FIG 8A AND 51-3-0.SDR RRXA11371Rib · crackedDURING A MAINTENANCE VISIT FOUND L/H CENTER L/E @ XS461 RIB IS CRACKED AT UPPER SKIN END. *** CORRECTIVE ACTION *** STOP DRILLED CRACK PER SRM 57-2-0 FIG 2. NDT CRACK TERMINATED PER SPM 06-10-01.001. FABRICATED AND INSTALLED REPAIR PARTS PER SRM 57-2-0 FIGSDR RRXA11370Fitting · corrodedDURING A MAINTENANCE VISIT FOUND C PIT BATH TUB FITTING AT STA 1160 L33R I/B TO 33R O/B HAS HEAVY CORROSION. REMOVED BATH TUB FITTING PER SRM 51-1-20D, REMOVED CORROSION ON BATH TUB FITTING MOUNT POINT. THICKNESS PER NDI SPM 04.00.06 FOUND TO BE WITHIN LIMIT
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