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 UPS05845787Fitting · crackedINSPECTION TYPE:C1 "A" PTI ZEE FITTING CRACKED AT STA. 270 L33R. REMOVED AND REPLACED ZEE FITTING IAW SRM 51-1-20D.SDR UPS05845756Shear Tie · corrodedFOUND SHEAR TIE CORRODED AT STA 1240 L35L. REMOVED FAB`D AND INSTALLED REPLACMENT SHEAR TIE IAW SRM 53-04-01-0 FIG 051, 51-01-04-0,53-2-0 AND 51-1-20D.SDR UPS05845711Doubler · corrodedFOUND COCKPIT SUBFLOOR FINGER DOUBLER HAS SEVERAL SHEARED HEAD FASTENERS AT STA -55 RBL 24. REMOVED FINGER DOUBLER, FOUND CORROSION OUT OF LIMITS, FABBED, AND INSTALLED REPLACEMENT DOUBLER IAW DC-8 SRM 53-3-1 AND 51-1-21.SDR UPS05845796Longeron · corrodedINSPECTION TYPE:C1 WHILE WORKING N/R 822550 FOUND PITTING CORROSION ON STEEL LONGERON 35L I/B SIDE BETWEEN FS 1240-1260. REPAIRED LONGERON 35L IAW SAA SK 813-823057 AND UPS EO DC8-53-20522.SDR UPS05845769Spar · crackedINSPECTION TYPE:C1 MLG WW FWD LWR SPAR CHORD CRACKED BETWEEN FASTENERS ON STA 857 (1.5 INCH LONG) XCW 53.500. REPAIRED SPAR CHORD IAW SRO 8570009.SDR UPS05845764Doubler · corrodedINSPECTION TYPE:C1 WHILE WORKING N/R 822550 FOUND INTERNAL EXFOLIATED BETWEEN STA 1240 AND 1260 L35L. CUT OUT DAMAGED AREA AND REPAIRED IAW SAA SK 813-823058, AND UPS EO DC8-53-20520.SDR UPS05845792Skin · corrodedINSPECTION TYPE:C1 INTERGRANULAR CORROSION ON RT HORIZ STAB L/E UPPER SURFACE AT SEGMENT JOINT. CUT OUT DAMAGED AREA AND FABRICATED AND INSTALLED REPAIR IAW SAA SK 81 3-822948 AND UPS EO DC8-55-20022.SDR UPS05845788Skin · corrodedINSPECTION TYPE:C1 INTERGRANULAR CORROSION ON LT HORIZ STAB L/E UPPER SKIN AT SEGMENT JOINT. CUT OUT DAMAGED AREA AND INSTALLED REPAIR DOUBLER AND 2 EA. FILLERS IAW SRM 55-02-01 FIG 004.SDR UPS05845786Fitting · crackedINSPECTION TYPE:C1 LONGERON END FITTING POSSIBLE CRACK AT STA 900 L4L. REMOVED AND REPLACED LONGERON END FITTING IAW SRM 51-1-21 AND 51-1-20D.SDR UPS05845727Fitting · crackedINSPECTION TYPE:C1 MAIN CABIN FITTING CRACKED AT STA 798 L19L. REMOVED, FABRICATED, AND INSTALLED FITTING IAW DWG 4751639 AND DC-8 SRM 51-1-20D.SDR UPS05845724Fitting · crackedINSPECTION TYPE:C1 LONGERON END FITTING CRACKED STA 860 L10R. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-20D.SDR UPS05845642Flap System · splitRIGHT HAND INBD FLAP OUTBD HINGE BRACKET COVER FWD PANEL CRACKED. INSTALLED INTERIM AIRWORTHY PANEL IAW EO DC8-5720-23117-A. DEFERRAL D312507 PER EO. REPLACED PANEL IAW MM 57-30. THIS CLEARS D312507.SDR UPS05845800Web · corrodedINSPECTION TYPE:C1 MAIN CABIN CENTER WING BOX AT STA 857 RBL 5 HAS HEAVY CORROSION ON THE UPPER REAR SPAR CAP. REPAIRED WING REAR SPAR TO FUSELAGE SHEAR WEB ATTACH ANGLE AND WING SKIN SPLICE DOUBLER IAW SAA SK 813-822678 AND UPS EO DC8-57-20145.SDR UPS05845790Pressure Panel · corrodedINSPECTION TYPE:C1 MAIN CABIN SUB FLOOR, FUEL DUMP CHUTE BRACKET UNDER THE PLATE HAS HEAVY CORROSION AT 857 RBL 40. REMOVED DAMAGED AREA AND REPAIRED IAW SAA SK 813-822556 AND UPS EO DC8- 5310-23251-A.SDR UPS05845773Door Frame · crackedINSPECTION TYPE:C1 C-PIT X-SLIDE DOOR FWD LOWER INTERIOR HAS 3.00 INCH LONG CRACK ON FRAME AS SEEM WITH MIRROR THROUGH 3RD LIGHTENING HOLE AFT. STOP DRILLED CRACK, FABRICATED AND INSTALLED DOUBLER IAW SRM 52-2-0, 51-1-21 AND 51-1-20D.SDR UPS05845726Finger Doubler · corrodedINSPECTION TYPE:C1 MAIN CABIN SUB FLOOR FINGER DOUBLER CORRODED AND HAS SHEARED HEAD FASTENERS AT STA 960 TO 940 RBL 65. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT FINGER DOUBLER IAW DC-8 SRM 53-07-03 FIG 4 AND 51-1-21.SDR UPS05845725Longeron · corrodedINSPECTION TYPE:C1 STA 8-25 LONGERON 19R IS CORRODED (EXFOLIATING). REMOVED LONGERON END FITTING, REMOVED CORROSION, AND REINSTALLED LONG END FITTING IAW SAA SK 813-822730.SDR UPS05845719Finger Doubler · crackedFOUND FINGER DOUBLER AT FS 207 HAS TWO CRACKS 3" AND 2" BELOW L21L. REMOVED FINGER DOUBLER AT FS 207 L21L IAW SRM 51-1-20D. FABRICATED AND INSTALLED FINGER DOUBLER AT FS 207 L21L IAW SRM 53-4-1 FIG 4, AND SRM 51-1-21.SDR UPS05845708Fitting · crackedFOUND C-PIT INTERCOSTAL END FITTING AT FS 1140 AT LONGERON 35L CRACKED AT UP PER FASTENER ATTACH POINT. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT FITTING IAW DWG 3758496 9 AND DC-8 SRM 51-1-21.SDR UPS05845707Shear Tie · crackedFOUND LARGE SHEAR TIE CRACKED AT BOTH ENDS AROUND FASTENERS IN 60 COMP'T CEILING BETWEEN L3L AND L3R. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT SHEAR TIE AND REPAIR PARTS IAW DWG 5612148 AND DC-8 SRM 51-1-20D.SDR UPS05845648Fitting · crackedNA FRAME SUPPORT ATTACH FITTING BELOW L21L AT FS 216 IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D, AND SRM 51-3-2 AT FS 216 L21L.SDR UPS05845625Control Valve · bypassingFLT CREW REPORTED SMOKE IN COCKPIT AND PERFORMED AN EMERGENCY EVACUATION VIA ESCAPE SLIDE. SLIDE DEPLOYED NORMALLY. CREW REPORTED LEFT PACK TRIP PRIOR TO SMOKE IN C/P. LEFT PACK TRIP LIGHT ILLUMINATED. FOUND LEFT PACK S/O AND FLOW CNTRL VLV BYPASSING WHEN SDR UPS05845798Frame · corrodedINSPECTION TYPE:C1 FRAME HEAVY CORRODED AT STA 1240 L35L. REPAIRED FUSELAGE FRAME IAW SAA SK813-822550 REV A AND UPS EO DC8-53-20516 A.SDR UPS05845791Bulkhead · crackedINSPECTION TYPE:C1 MAIN CABIN AFT PRESSURE BULKHEAD CRACKED L11R RBL 48. CUT OUT DAMAGED AREA 2 AND FABRICATED AND INSTALLED FINGER DOUBLER, DOUBLER AND 2 FILLER IAW SRM 51-1-20D, 51-3-0, 51-1-21 AND TR- 53-194.SDR UPS05845784Door Frame · misrepairedINSPECTION TYPE:C2 AFTER REMOVAL OF MCD AFT LWR JAMB FOUND ADDITIONAL CUT OUTS NOT PER SRM OR SRO 8530027. FABRICATED AND INSTALLED -1, -3,DOUBLERS AND -5, -7 TRIPPLER AND -11, AND -13 FILLERS IAW UPS EO DC8-5330-23194-A, SAA SK 866-833270, BOEING MESSAGES 1-SDR UPS05845704Fitting · crackedFOUND STA 450 L14L SPLICE FITTING IS CRACKED. REMOVED, FABRICATED, AND INSTALLED FITTING IAW DWG 3887799 AND DC-8 SRM 51-1-20D.SDR UPS05845703Fitting · crackedFOUND "C" PIT LONGERON END FITTING CRACKED STA 1230 L31R. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-20D.SDR UPS05845702Fitting · crackedFOUND FITTING CRACKED 1" LONG AT STA 1280 L33R. REMOVED, FABRICATED, AND INSTALLED FITTING IAW DWG 4758514 AND DC-8 SRM 51-1-20D.SDR UPS05845771Doubler · crackedINSPECTION TYPE:C1 MAIN CARGO COMP L11L STA 260 CARGO DOOR ANGLE CHAFED MARK. UPON REMOVAL OF REPAIR ANGLE, FOUND DOUBLER CRACKED. REMOVED DOUBLER, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW DWG 5772787, SRM 53-2-0 FIG 1F AND 51-1-21.SDR UPS05845763Skin · crackedINSPECTION TYPE:C1 R1 DOOR UPPER FWD CORNER OF CUT OUT IS A .5 INCH CRACK FROM FASTENER TO EDGE OF SKIN. FABRICATED AND INSTALLED DOUBLER, TRIPLER AND FILLER AT FWD UPPER CORNER OF R1 DOOR IAW SRM 53-2-0 FIG 14, 51-1-21 AND 51-3-0.SDR UPS05845751Fitting · crackedFOUND MAIN CARGO COMPARTMENT L2R FITTING CRACKED STA 860. REMOVED AND REPLACED FITTING IAW SRM 51-1-21,51-3-0 AND 51-1-20D.SDR UPS05845749Fitting · chafedFOUND CANOE FITTING CHAFFED IB AND OB AT STA 219 LT OB FLAP. BLENDED OUT CHAFED AREA, SHOT PEENED IAW SRM 51-1-8, DPS 4.999-2 AND SAA SK 813-822426.SDR UPS05845723Fitting · crackedINSPECTION TYPE:C1 MAIN CARGO COMPARTMENT RIGHT BETWEEN STA 440-460 SPLICE FITTING CRACKED L14R. REMOVED, FABRICATED AND INSTALLED REPLACEMENT FITTING IAW DWG 3887799 AND DC-8 SRM 51-1-20D.SDR UPS05845722Fitting · crackedINSPECTION TYPE:C1 MAIN CARGO COMPARTMENT RT STA 840 L12R INTERCOSTAL FITTING CRACKED. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT FITTING IAW DWG 3779874 AND DC-8 SRM 51-1-20D.SDR UPS05845721Fitting · crackedINSPECTION TYPE:C1 MAIN CARGO COMPARTMENT LEFT STA 798 LONGERON 19L BOOT FITTING CRACKED IN RADIUS 4 INCHES LONG. REMOVED AND REPLACED BOOT FITTING IAW DC-8 SRM 51-1-20D.SDR UPS05845706Fitting · crackedFOUND MAIN CARGO COMPARTMENT L1 AFT OF STA 900 FITTING CRACKED. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-20D AND 51-3-0.SDR UPS05845705Fitting · crackedFOUND MAIN CARGO COMPARTMENT L7R FITTING CRACKED STA 860. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-20D.SDR UPS05845701Longeron · crackedRT AFT INTERIOR FS 1756 L14R CRACKED AT UPPER CANTED FRAME INTERSECTION. CUT OUT DAMAGED SECTION OF LONGERON, FABRICATED, AND INSTALLED REPLACEMENT SECTION OF LONGERON IAW DC-8 SRM 53-2-2 FIG 10.SDR UPS05845700Fitting · crackedFOUND RT AFT FUSELAGE INTERIOR FS 1760 L17R END FITTING HAS POSSIBLE CRACK AT UPPER FLANGE. NDT VERIFIED 1.5" CRACK. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51- 1-20D.SDR UPS05845699Fitting · crackedFOUND STA 1690 L3L AFT PROD SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-20D.SDR UPS05845698Longeron · crackedFOUND STA 1716 L18L IS CRACKED AT INTERSECTION OF CANTED FRAME UPPER ATTACH FASTENER. CUT OUT DAMAGED SECTION OF LONGERON, FABRICATED, AND INSTALLED REPLACEMENT SECTION OF LONGERON IAW DC-8 SRM 53-2-2 FIG 10.SDR DHLA102005AASkin · crackedLEFT WING SKIN CRACKED AT STRINGER 64 LT. APPROX XRS 450 AT FASTENER HOLE FOUND WHILE ACCOMPLISHING S/B 57-100 INSPECTIONSDR UPS05845615Windshield · crackedINSPECTION TYPE:N/A, F/O'S WINDSHIELD TOP EDGE GLOWING. WINDSHIELD CRACKED AT 17K FT. REMOVED AND REPLACED F/O WINDSHIELD W/REF TO MM 56-10-02-2.SDR UPS05845695Stringer · crackedNR 4 ALT HAS CRACK ON STRINGER 64 NEAR FRONT SPAR. REMOVED, FAB`D AND INSTALLED STRINGER SPLICE IAW SRM 51-1-21, 51-1-20D.SDR UPS05845656Stiffener · corrodedC2 A-PIT STA 283 AT LWR FWD DOOR CUTOUT, EXTRUDED STIFFNER IS CORRODED OUT OF LIMITS. REMOVED A-PIT LWR FWD DOOR CUTOUT STIFFNER IAW SRM 51-1-24 FABRICATED AND HEAT TREATED STIFFNER IAW DWG 5733892 AND INSTALLED STIFFNER AT STA 283 LWR FWD DOOR CUTOUT IAW DWGSDR DHL2005801014Plate · unknownNR 4 ALT TANK PLATE 505A REMOVED FOR ACCESS. FOUND CRACK FOUND ON VISUAL INSPECTION R/WING WND OF STRINGER 64 APPROX 1" LONG FRONT TO REAR O/B FASTENER AND BY HIGH FREQ EDDY CURRENT. ACP HIGH FREQ EDDY CURRENT INSP. OF LOWER WING SKIN LT SIDE OF LWR WING. OSDR UPS05845621Finger Doubler · crackedFINGER DOUBLER CRACKED AND CORRODED AT STA 1350-1490 L31L. REMOVED FINGER DOUBLER AT STA 1350-1490 L31L IAW SRM 51-1-21. FABRICATED AND INSTALLED FINGER DOUBLER AT STA 1350-1490 L31L IAW SRM 51-3-2, AND SRM 51-1-8, AND 51-1-21.SDR UPS05845620Fitting · crackedFOUND CRACKED LONGERON END FITTING AT STA 1490 L33R. REMOVED LONGERON AND END FITTING IAW SRM 51-1-20D. INSTALLED LONG TRAVERSE SKIN SPLICE FITTING IAW SRM 51-1-20D AT STA 1490 L33R.SDR UPS05845605Shear Tie · crackedINSPECTION TYPE:C2 CRACKED SHEAR TIE AT STA 1395 BETWEEN L35 AND L36 RT. REMOVED SHEAR TIE IAW SRM 53-2-0 FIG 2B, FABRICATED AND INSTALLED SHEAR TIE AND SPLICE REPAIR IAW SRM 53-2-0 FIG 2D AND SRM 51-1-20D.SDR UPS05845658Shear Tie · crackedINSPECTION TYPE: C2 SHEAR TIE AT STA 710 L35L IS CRACKED. REMOVED SHEAR TIE AT STA 710 L35L IAW SRM 51-1-20D, FABRICATED AND INSTALLED SHEAR TIE AT STA 710 L35L IAW DWG 5750365, AND SRM 51-1-21D.
Back to Douglas DC-8-73F