Douglas DC-8-71F
Service difficulty reports · 8,938
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 = 'DC871F' 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 = 'DC871F' 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 UPS04843300Beam · crackedINSPECTION TYPE:C3 AFT SIDE OF AFT PRESSURE BULKHEAD 4TH J-BEAM UP FROM BOTTOM HAS LOWER EXISTING DOUBLER CRACKED AT CENTERLINE. NDT VERIFIED CRACK IN LOWER EXISTING DOUBLER IS 2 INCHES IN LENGTH. REMOVED EXISTING REPAIR DOUBLERS. NDT VERIFIED 2 INCH CRACK SDR UPS04843299Beam · crackedINSPECTION TYPE:C3 AFT PRESSURE BULKHEAD AFT SIDE 3RD J-BEAM UP FROM BOTTOM CRACKED AT BO BOTH UPPER & LOWER EXISTING DOUBLERS AT CENTERLINE WITH UPPER FLANGE HANS SHEARED & LOOSE FASTENERS. NDT VERIFIED CRACK IN BOTH UPPER & LOWER J-BEAM DOUBLERS IS 2 INCHESSDR UPS04843306Finger Doubler · corrodedINSPECTION TYPE-C3 SHEARED FASTENERS AND CORROSION UNDER FINGER DOUBLER STA 880-900 BL 0. CUT OUT DAMAGE TO WEB AND FINGER DOUBLER. FABRICATED FILLER, FINGER DO DOUBLER, AND DOUBLER IAW SRO DWG 5645332. INSTALLED ALL REPAIR PARTS IAW SAA SK772-069.SDR UPS04843303Fitting · corrodedINSPECTION TYPE: C3, LOWER CARGO COMPARTMENT C-PIT DOOR (JAMB) FRAME AT APPROX STA 1165 LW LOWER LATCH BACK-UP FITTING HAS SEVER CORROSION ON FITTING & FASTENERS. REMOVED AND REPLACED FITTING IAW DC-8 SRM 53-2-0 FIG 2D.SDR UPS04843264Longeron · crackedINSPECTION TYPE: C3, LONGERON 14L CRACKED AT CANTED FRAME STA 1740. CUT OUT DAMAGED AREA. NDT VERIFIED NO CRACKS NOTED AT CUT OUT. FABRICATED REPAIR ANGLE & FILLER AND INSTALLED IAW DC-8 SRM 53-2-2 FIG 11.SDR IXXA060588SSkin · gougedDURING ROUTINE C CHECK, FOUND LEFT INBOARD FLAP TOP SKIN GOUGED AT STATION XF 90. REMOVED DAMAGED AREA. FABRICATED DOUBLER, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED FILLER AND DOUBLER IAW DC8 SRM 57-2-0, 51-1-8, AND 51-1-21.SDR UPS04843088Slide · deployedINSPECTION TYPE:N/A ESCAPE SLIDE DEPLOYED WHILE ATTEMPTING TO CLOSE MAIN ENTRY DOOR. REF M287491. REPLACED SLIDE AS PER MM 25-60-02-2, S/N INSTALLED 36-22 THIS CLEARS M287491.SDR UPS04843301Rib · crackedINSPECTION TYPE:C3 LEFT O/B SLOT UPPER DOOR CLOSE-OUT RIB AT I/B END BROKEN IN LOWER RADIUS. REMOVED AND REPLACED LEFT O/B SLOT CLOSE OUT RIB (PAN) IAW DC-8 SRM 51-1-21. REPAIRED LEFT O/B SLOT O/B END IAW SAA SK772-387.SDR UPS04843265Door Frame · crackedINSPECTION TYPE: C3, L1 DOOR HAS A CRACK ON THE LOWER FWD DOOR JAMB STARTING FROM THE EDGE AND TERMINATES AT THE FASTENER HOLE. CUT OUT CRACK ON FWD LOWER CORNER OF L1 DOOR JAMB OUTER SKIN AND INTERNAL DOUBLER. NDT VERIFIED NO CRACKS NOTED AT CUT OUTS. FABRSDR UPS04843262Pan · crackedINSPECTION TYPE: C3, RADIOGRAPHIC (X-RAY) INSP DETECTED A CRACK ON THE FWD LEFT EMERGENCY OV OVERWING EXIT ON THE UPPER AFT JAMB CORNER APPROX .562 INCH IN LENGTH. NDT VERIFIED CRACK EXISTS IN INTERNAL DOOR PAN. TRIMMED EDGE OF INTERNAL DOOR PAN TO REMOVE CRSDR UPS04843252Rib · chafedINSPECTION TYPE: C3, RT WING I/B STUB WING RIB XILD 42 HAS A DEEP CHAFF. REMOVED DAMAGED AREA. NDT VERIFIED NO CRACKS NOTED AROUND CUTOUT. FABRICATED REPAIR ANGLES (2 EA) & FILLER AND INSTALLED IAW DC-8 SRM 57-2- 0.SDR UPS04843229Rib · crackedINSPECTION TYPE: C3, WING LT LEADING EDGE AT STA XFS 672.500 RIB IS CRACKED. STOP DRILLED CRACK. NDT VERIFIED STOP DRILL TERMINATES CRACK. FABRICATED SHIM & REPAIR ANGLE AND INSTALLED IAW DC-8 SRM 57-2-0 FIG 2.SDR UPS04843227Rib · crackedINSPECTION TYPE:C3 WING LEFT L/E RIB IS CRACKED AT STA 785. STOP DRILLED CRACK. NDT VERIFIED STOP DRILL TERMINATES CRACK. FABRICATED REPAIR ANGLE AND INSTALLED IAW DC-8 SRM 57-2-0 FIG 2.SDR UPS04843225Rib · crackedINSPECTION TYPE:C3, WING LT OUTBOARD LEADING EDGE AT STA 778.250 APROX RIB CRACKED. STOP DRILLED CRACK. NDT VERIFIED STOP DRILL TERMINATES CRACK. FABRICATED REPAIR ANGLE AND INSTALLED IAW DC-8 SRM 57-2-0 FIG 2.SDR UPS04843224Rib · crackedINSPECTION TYPE:C3 WING LT LEADING EDGE AT STA 735 RIB IS CRACKED. STOP DRILLED CRACK. NDT VERIFIED STOP DRILL TERMINATES CRACK. FABRICATED SHIM & REPAIR DOUBLER AND INSTALLED IAW DC-8 SRM 57-2-0 FIG 2.SDR UPS04843223Rib · crackedINSPECTION TYPE:C3 UPPER RIB CRACKED IN LT CENTER L/E ABOVE OPENING FOR PANEL 520B. STOP DRILLED CRACK. NDT VERIFIED STOP DRILL TERMINATES CRACK. FABRICATED TWO REPAIR DOUBLERS AND INSTALLED IAW DC-8 SRM 57-2-0 FIG 2.SDR UPS04843148Rib · crackedC3 RT WING NR 4 STUB WING HAS TWO RIBS CRACKED ABOVE NR 4 PYLON FOOT STOOL. STOP DRILLED ONE CRACK AND CUT OUT ONE CRACK. NDT VERIFIED STOP DRILL TERMINATES CRACK AND NO CRACKS NOTED AT CUT OUT. FABRICATED REPAIR ANGLES AND INSTALLED IAW SRM 57-2-0 FIG 2SDR UPS04843147Rib · crackedC3 WING RT L/E AT STA XFS 335.250 DRAIN HOLE DOUBLER IS CRACKED. NDT VERIFIED CRACK IS APPROX. .3750 INCH LONG. REMOVED INTERNAL DOUBLER ON RT WING L/E, FABRICATED REPLACEMENT DOUBLER IAW DWG 5769589-27. INSTALLED REPLACEMENT DOUBLER ON RT L/E AT STA XFS 335.SDR UPS04843145Rib · crackedC3 WING RT L/E AT APPROX. STA XFS 465 HAS CRACKED RIB. STOP DRILLED CRACK. NDT VERIFIED STOP DRILL TERMINATES CRACK. FABRICATED REPAIR ANGLE DOUBLER AND INSTALLED IAW SRM 57-2-0 FIG 2.SDR UPS04843144Rib · crackedC3 LT WING L/E AT STA. XFS 716.250 RIB IS CRACKED. STOP DRILLED CRACK. NDT VERIFIED STOP DRILL TERMINATES CRACK. FABRICATED REPAIR ANGLE AND INSTALLED IAW SRM 57-2-0 FIG 2.SDR UPS04843143Rib · crackedC3 WING LT L/E RIB IS CRACKED AT STA XFS 816.250. STOP DRILLED CRACK. NDT VERIFIED STOP DRILL TERMINATES CRACK. FABRICATED REPAIR ANGLE AND SHIM AND INSTALLED IAW SRM 57-2-0 FIG 2SDR UPS04843142Rib · crackedINSPECTION TYPE: C3, WING LT L/E AT STA XFS 578 RIB IS CRACKED. NDT VERIFIED CRACK .5 INCH LONG. STOP DRILLED CRACK. NDT VERIFIED CRACK TERMINATES AT STOP DRILL. FABRICATED REPAIR ANGLE AND SHIM AND INSTALLED IAW SRM 57-2-0 FIG 2.SDR UPS04843139Rib · crackedC3 WING LT L/E AT STA. XFS 591.250 RIB IS CRACKED. REPAIRED LT WING L/E RIB AT STA. XFS 591.250 IAW SRM 57-2-0 FIG 2.SDR UPS04843255Pressure Blkhd · crackedINSPECTION TYPE: C3, F/S 1766 FWD SIDE OF AFT PRESSURE BULKHEAD IS CRACKED 65 INCHES ABOVE FLOOR AND LBL 35. REMOVED EXISTING REPAIR AND CUT OUT CRACKED AREA. NDT VERIFIED NO CRACKS NOTED AT CUT OUT. FABRICATED FILLER, FINGER DOUBLER, & DOUBLER INSTALLED IASDR UPS04843254Pressure Blkhd · crackedINSPECTION TYPE:C3 F/S 1766 FWD SIDE OF AFT PRESSURE BULKHEAD IS CRACKED 65 INCHES ABOVE FLOOR AND RBL 35. REMOVED EXISTING REPAIR DOUBLERS AND CUT OUT CRACKED AREA. NDT VERIFIED NO CRACKS NOTED AT CUTOUT. FABRICATED REPAIR DOUBLERS & FILLER AND INSTALLED ISDR UPS04843228Rib · crackedINSPECTION TYPE:C3 CRACKED RIB AT APPROX STA XFS 728 RIGHT WING LEADING EDGE. REMOVED PREVIOUS REPAIR AND TRIMMED OUT CRACK. NDT VERIFIED NO CRACKS NOTED AT TRIM OUT. REINSTALLED REPAIR PARTS IAW DC-8 SRM 51-1-21 AND 51-1-20D.SDR UPS04843146Rib · crackedC3 RT WING MID L/E XFS 335 UPPER RIB IS CRACKED AT AFT END. STOP DRILLED CRACK. NDT VERIFIED STOP DRILL TERMINATES CRACK. FABRICATED REPAIR ANGLE DOUBLERS AND INSTALLED IAW SRM 57-2-0 FIG 2.SDR UPS04843130Battery Pack · inoperativeEMERGENCY LIGHTS FADED DURING EMERGENCY LIGHTS TEST. REMOVED AND INSTALLED A SERVICEABLE LIGHTING BATTERY AND RELAY UNIT REF DC8 MM 30-50-01-2. TEST GOOD.SDR UPS04843307Cusp Web · corrodedINSPECTION TYPE: C3, HEAVY CORROSION ON CUSP, LT SIDE MAIN CABIN, STA 1153. REMOVED TEE ANGLE AND L-ANGLE. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW DC-8 SRM 53-2-0 FIG 1F. FABRICATED FILLER IAW SAA SK772-604. INSTALLED FILLER AND REINSTALLED T-ANGLE &SDR UPS04843253Door Frame · crackedINSPECTION TYPE: C3, LEFT FWD EMERGENCY EXIT DOOR IS CRACKED AT UPPER FWD CORNER OF FRAME. TWO CRACKS VISIBLE .5 INCH AND 1.5 INCH IN LENGTH. STOP DRILLED 2 EA CRACKS. NDT VERIFIED STOP DRILLS TERMINATES CRACKS. FABRICATED REPAIR DOUBLER AND INSTALLED IAW SDR UPS04843266Web · crackedINSPECTION TYPE: C3, CENTER WING FS 700 LEFT CRACK IN WEB EXTENDED PAST REPAIR. REMOVED EXISTING REPAIR. CUT OUT DAMAGED WEB. FABRICATED WEB & SPLICE DOUBLER AND INSTALLED IAW DC-8 SRM 53-2-0.SDR UPS04843308Bulkhead · corrodedINSPECTION TYPE: C3, FWD SIDE OF FS 70 BULKHEAD LOWER CHORD HAS INTERGRANULAR CORROSION AT LONGERON 32R. FOUND INTERGRANULAR CORROSION OUT OF LIMITS IAW DC-8 SRM 53-2-0 FIG 1F. REMOVED STA 70 LOWER FWD CHORD BETWEEN LONGERONS 32R & 33R. FABRICATE AND ONE -9SDR UPS04843263Skin · crackedINSPECTION TYPE: C3, POSSIBLE CRACK IN UPPER WING SKIN (LT) AT FASTENER ON AFT SIDE OF STRINGER 15, JUST O/B OF RIB AT XRS 74. NDT VERIFIED CRACK 1 INCH IN LENGTH. CUT OUT DAMAGED AREA 1.375 INCH DIAMETER. NDT VERIFIED NO CRACKS NOTED AT CUT OUT. FABRICATESDR UPS04843167Attach Angle · crackedINSPECTION TYPE: C2, LEFT HORIZONTAL STAB L/E ATTACH ANGLE CRACKED AT LOWER I/B CORNER. REMOVED HORIZONTAL STAB SIDE ROLLER BEARING, TRACK, AND ANGLE FITTING PER SRM 51-3-0, 51-1-20D, 51-1-21 AND MM 55-10-00-2. INSTALLED NEW ANGLE FITTING PER SRM 51-3-0, 51-SDR UPS04843164Fitting · crackedINSPECTION TYPE: C2, LONGERON 32R SPLICE FITTING CRACKED FROM STA 620 TO STA 640. REMOVED AND REPLACED SPLICE FITTING PER SRM 51-1-20D.SDR UPS04843166Fitting · crackedINSPECTION TYPE: C2, BATHTUB FITTING CRACKED AT STA 280 L27L. REMOVED CRACKED FITTING. FABBED REPAIR PARTS FROM BAC1503-100163 PER SRM 53-2-0 FIG 2D. INSTALLED NEW FITTING AND REPAIR PARTS PER SRM 53-2-0 FIG 2D, 51-1-8, 51-1-20D, 51-3-0, 51-1-15.SDR UPS04843165Fitting · crackedINSPECTION TYPE:C2 LONGERON 36 END FITTING CRACKED AT STA 203. REMOVED AND REPLACED END FITTING REF DC8 SRM 51-1-20D.SDR UPS04843168Skin · lightning strikeINSPECTION TYPE:C2 LIGHTNING STRIKES ON FUSE EXTERIOR STA 415 BETWEEN L5R & L6R. BURNISHED DAMAGE AREA PER SRM 53-2-0 FIG 1F. NDT VERIFIED MATERIAL THICKNESS OUT OF LIMITS, .020' TO .053, PER NDT SPM 04-00-06. CUT OUT DAMAGED AREA PER 53-2-1 FIG 7. FABBED SDR UPS04843035Light · inoperativeEMERGENCY EXIT LIGHTS DID NOT ILLUMINATE ON PREFLIGHT TEST. REMOVED AND REPLACED BATTERY PACK, OPS CHECK NORMAL.SDR UPS04843100Attach Angle · crackedINSPECTION TYPE:C2 VERT STAB LOWER FRONT SPAR EXTERNAL DRAG ANGLE CRACKED AT STA 1756. REMOVED DOUBLER PER SRM 51-3-0, 51-1-21. STOP DRILLED CRACK PER SRM 53-2-0, NDT VERIFIED STOP DRILL PER SPM 06-10-01.001. FABBED REPAIR ANGLE FROM S25043-17-7PH .080. HESDR IXXA0400106OEngine · failedDURING TAKE OFF NR 1 GEN HAD NO FREQ AND LOW VOLT ON ENGINE DISCONNECTED GENERATOR. ON TAKE OFF TOWER WAS TOLD THAT NR 1 ENGINE HAD A TAIL PIPE FIRE. ENGINE SHUT DOWN, AIRCRAFT RETURNED TO BLOCKS AND TRIED TO ROTATE N1 FAN NO ROTATION, TRIED TO MOTOR ENGINE N2SDR UPS04843128Bulkhead · crackedINSPECTION TYPE: C2, THE AFT PRESSURE BULKHEAD WEB APPROXIMATE 2 INCH CRACK AT RBL 3 STA.1766 FROM INSIDE 60 H0LE. REPAIRED AFT PRESSURE BULKHEAD WEB 2 INCH CRACK AT STA.1766 RBL 3 IAW SAA SK708-993 DATED 8/26/04, UPS EO DC8-5320-20956 DATED 09/08/04 & 8110-3SDR UPS04843101Fitting · corrodedINSPECTION TYPE: C2, BATHTUB FITTING CORRODED AT STA 340 BETWEEN L35R & L34R. REMOVED BATHTUB FITTING PER SRM 51-1-20D. FABBED REPAIR ANGLES PER SRM 53-2-0 FIG 2D. INSTALLED NEW FITTING & REPAIR ANGLES PER SRM 51-1-20D, 53-2-0 FIG 2D.SDR UPS04843099Fitting · corrodedINSPECTION TYPE:C2 A-PIT FS 300 BATHTUB FITTING BETWEEN L34L & L33L HAS HEAVY CORROSION. REMOVED BATHTUB FITTING. FABBED REPAIR ANGLES PER SRM 53-2-0 FIG 2B. INSTALLED NEW FITTING AND REPAIR ANGLES PER SRM 53-2-0 FIG 2B, 51-1-20D.SDR UPS04843098Fitting · crackedINSPECTION TYPE: C2, FS 450 L31L SPLICE FITTING CRACKED. REMOVED AND REPLACED SPLICE FITTING AT FS 450 L31L.SDR UPS04843027Fitting · crackedINSPECTION TYPE: C, STATION 1776 LONG 10L END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4772397 AND SRM 51-1-20D.SDR UPS04842978Rib · crackedINSPECTION TYPE: C, LEFT HORIZONTAL STAB L/E UPPER RIB CRACKED AT XFS 47.5. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR ANGLES PER SRM 55-2-0 FIG 2.SDR UPS04843120Fitting · crackedINSPECTION TYPE: C1, RT FLAP HINGE 3 FITTING HAS APPROX 6-8 IN LONG CRACK BETWEEN TRACK LANDS. REMOVED FLAP HINGE 3 FITTING. IAW SRM 51-1-20D, 51-1-21 AND 51-3-0. FABED IAW SAA SK 708-840-2 FITTING SAME MFG P/N 5642342-2, FLAP LINK SUPPORT FITTING FROM 70SDR UPS04843016Longeron · corrodedINSPECTION TYPE: C2, STATION 70 LONGERON 35R AND END FITTING ARE CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND REPLACED LONGERON SECTION BETWEEN STATION 70 AND 90, INSTALLED SPLICE AND REPLACED END FITTING IAW SRM 53-2-2 FIG 10.SDR UPS04842977Skin · damagedINSPECTION TYPE: C, EXTERNAL FUSELAGE EXISTING REPAIR DOUBLER AT STA 70 L36 REQUIRES REMOVAL, ASSESSMENT, AND REPAIR IAW SRM 53-2-1 FIG 7 REF EO DC8-5330-12800 REPAIR 708-2R-01. REMOVED EXISTING DOUBLER, CUT OUT DAMAGE, FABRICATED AND INSTALLED FILLER, EXT DO
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