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 UPS04842788Doubler · crackedINSPECTION TYPE:N/A, NR 3 PIT DOOR CUTOUT AT LWR AFT CORNER HAS CRACK AT DOUBLER. REMOVED CRACKED FITTING & ATTACHING FITTINGS. DRILLED UP NEW FITTINGS, OK TO INSTALL. INSTALLED 80 PERCENT OF FASTENERS IN NEW FITTING. COMPLETED NEW INSTALLATION OF NEW FITTSDR UPS04842787Door Frame · corrodedINSPECTION TYPE:N/A CIRCUMFERENTIAL TIE STRAP BELOW AFT DOOR FRAME AT LOWER DOOR CUTOUT HAS EXFOLIATION CORROSION. ACCOMPLISHED EO DC8-5310-20796 BLENDED OUT CORROSION. REPEAT INSP'S AT EVERY C-CHECK PERFORMED VLT THICKNESS CK & HFEC PER UPS EO DC8-5310-2079SDR UPS04842914Spar Cap · crackedINSPECTION TYPE:C1 WING CENTER SPAR LOWER CAP AT WING STATION XCW 36 IS CRACKED. STOP DRILLED CRACK NDT VERIFIED STOPDRILLS TERMINATED CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER, TRIPLER AND REPAIR ANGLE IAW SAA SK 802-190 AND UPS EO DC8-5710-20888-A.SDR DHL2004804527Skin · wornRIGHT WING OUTBOARD FLAP L/E UPPER SKIN WORN, XF 226.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW ED-EDW27.5, DWG W27-R05 REV 1R. REMOVED FASTENERS IAW SRM 51-1-21 PG 1, SRM 51-3-0 PG 1. TRIMMED OUT DAMAGED PLATING IAW ED-EDW 27.5, DWG W27-R05. FABRICATESDR DHL2004804528Doubler · brokenRT WING OB AILERON LWR. SKIN DOUBLER BROKEN 0.250, XA 615.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW ED EDW 27.2, DWG W27-R02, REV 1R. REMOVED DAMAGED DOUBLER IAW DWG W27-R02, ED EDW 27.2. TRIMMED OUT PLATING SEGMENT(DAMAGED) IAW DWG W27-R02, ED EDW 27.2.SDR DHL2004804530Skin · corrodedLT OUTER WING OB STUB WING SKIN CORRODED (UPPER PART) XOLDO 67.000. PERFORMED MAJOR REPAIR IAW EDEDW 27.3, DWG W27 R03 REV. IR. REMOVED FASTENERS IAW SRM 51-3-0 PG.1, SRM 51-1-21 PG.1. REMOVED CORROSION IAW SRM 51-1-8 PG. 17-18. FOUND OUT OF LIMITS IAW SRM 57SDR DHL2004804529Skin · crackedITEM REF. NR. 0848: REPAIR OF DENT AND BROKEN CRACK TO RT WING IB AILERON UPPER PLATING AT XW 563.000 PERFORMED MAJOR REPAIR IAW ED-EDW 27-1, DWG W27-R01 REV IR. REMOVED EXISTING FASTENERS ON AREA IAW SRM 51-1-21 PG. 1, SRM 51-1-20D PG. 21. TRIMMED OUT DAMAGEDSDR DHL2004804531Skin · wornLT WING IB FLAP UPPER SKIN WORN XW 91.000 (MAJOR REPAIR). CORR.: PERFORMED MAJOR REPAIR IAW ED EDW 27-4, DWG W27-R04 REV. IR. REMOVED FASTENERS IAW SRM 51-1-21 PG.1. TRIMMED OUT DAMAGED PLATING SEGMENT IAW ED EDW 27-4, DWG W27-R04. FABRICATED NEW PLATING SEGMESDR DHL2004804526Clip · crackedITEM REF. NR. 0910: AFT. ACCY. COMPT. CLIP CRACKED 1.500 AT STA. 660.000 L-22L. REMOVED CRACKED CLIP IAW SRM 53-1-0 PG.1, SRM 51-1-20D PG.21. FABRICATED NEW CLIP (STEEL AISI 4130 0.050) IAW SRM 53-4-1 PG. 140, EA5310-032, DWG 3646688. PERFORMED HEAT TREATMENT SDR UPS04842901Fitting · crackedINSPECTION TYPE: C1, NR 4 ALT BOOST PUMP BRACKET AND STRINGER 59 END FITTING AT XW 408 ARE CRACKED. REMOVED, FABRICATED AND REPLACED FITTING AND REPLACED BRACKET IAW DWG 3645611 AND 5644972 AND SRM 51-1-20D.SDR UPS04842848Fitting · crackedINSPECTION TYPE: C1, STATION 1220 AFT SIDE BATHTUB FITTING IS CRACKED BETWEEN LONG 33R AND 32.5R IN TORQUE BOX. REMOVED AND REPLACED FITTING IAW SRM 53-2-0 FIG 2D.SDR DHL2004804525Fitting · crackedMAIN CARGO COMPT FITTING CRACKED 1.000, STA. 702.000, RBL 25. REMOVED CRACKED FITTING AT STA 702.000 RBL 25 IAW DC8 SRM 53-1-0 PG 1, SRM 51-1-20D PG 21. FABRICATED NEW FITTING IAW EA5320-029, DWG 4751820. PERFORMED NDT INSPECTION IAW NDT SPM PART 08-00-02/0SDR UPS04842804Doubler · corrodedINSPECTION TYPE: C1, RT WING INTERIOR DOUBLER CORRODED AT STALL WARNING VANE, STA XFS371- 376. REMOVED CORRODED INTERNAL DOUBLERS SRM51-1-21. FABRICATED AND INSTALLED REPLACEMENT DOUBLER IAW DWG5769589, AND SRM 51-1-21, & 51-1-8.SDR UPS04842795Fitting · crackedINSPECTION TYPE: C1, HFEC INSPECTION DETECTED A CRACK IN FITTING AT STA 1150, FWD SIDE AT LONGERON 33 RT. REMOVED AND REPLACED FITTING AT STA 1150, LONGERON 33 RT IAW SRM 51-3-2, 51-1-8, 51-1-21, 51-1-20D.SDR UPS04842849Fitting · corrodedINSPECTION TYPE:C1 STATION 1170 BACKUP FITTING FWD SIDE IS CORRODED FOR FWD LOWER T-BOLT FITTING AT LONG 33R. REMOVED AND REPLACED FITTING IAW DWG 5894282 AND SRM 53-2-0 FIG 2D.SDR UPS04842847Fitting · crackedINSPECTION TYPE:C1 STATION 990 LONGERON 23R END FITTING IS CRACKED. REMOVED, FABRICATED AND REPLACED FITTING IAW DWG 3753306 AND SRM 51-1-20D.SDR UPS04842805Longeron · crackedINSPECTION TYPE: C1, LONGERON 28L CRACKED AT FRAME INTERSECTION STA 1400, CUT OUT DAMAGED LONGERON SECTION FROM 1390 TO 1410. FABRICATED REPLACEMENT LONGERON. SECTION SRM53-2-2 FIG10 AND SRO853009 AND 53-4-1 FIG44. INSTALLED 2 SPLICE FITTINGS AND LONGERON SSDR UPS04842801Intercostal · crackedINSPECTION TYPE: C1, INTERCOSTAL CRACKED IN MAIN CABIN SUBFLOOR, STA 1726, LBL 35. REMOVED, FABBED, AND REPLACED INTERCOSTAL IAW DWG 5755032, SRM 51-1-21, 51-1-8, 51-1-20D.SDR UPS04842797Fitting · crackedINSPECTION TYPE: C1, INTERCOSTAL ATTACH FITTING CRACKED AT STA 1240 LONG 35R REMOVED AND REPLACED FITTING IAW SRM 51-3-2, 51-1-20D.SDR UPS04842846Longeron · crackedINSPECTION TYPE:C1 STATION 1735 LONG 15R IS CRACKED. REMOVED, FABRICATED AND REPLACED LONGERON SECTION AND INSTALLED SPLICE FITTING AND STRAPS IAW SRM 53-2-2 FIG 10 BETWEEN STATION 1720 TO 1766.SDR UPS04842796Finger Doubler · corrodedINSPECTION TYPE:C1 CORROSION ON/AROUND MAIN CABIN SUBFLOOR FINGER DOUBLER STA 880 TO 900 RBL60-64 FINGER DOUBLER CORRODED BEYOND LIMITS. UNDERLYING STRUCTURE OK. FABBED AND INSTALLED REPLACEMENT FINGER DOUBLER IAW DWG 5645332, SRM 53-2-0 FIG1F, 51-1-8, 51SDR UPS04842794Web · corrodedINSPECTION TYPE: C1, CORROSION ON SUBFLOOR BETWEEN WEB AND CHANNEL, MAIN CABIN STA 857 AT FUEL DUMP TORQUE TUBE. REMOVED UPPER CHANNEL IAW SRM 51-1-21. CUT OUT DAMAGED AREA. FABBED AND INSTALLED REPAIR DOUBLER AND FILLER IAW SRM53-2-0 FIG23, DWG 5645332, 51SDR UPS04842798Fitting · crackedINSPECTION TYPE: C1, LONGERON 31 LT SPLICE FITTING CRACKED AT STA 450. REMOVED AND REPLACED SPLICE FITTING IAW SRM 51-1-11, 51-1-20D.SDR UPS04842800Finger Doubler · corrodedINSPECTION TYPE: C1, FINGER DOUBLER CORRODED IN COCKPIT SUBFLOOR. STA.-75 AT LT CUSP REMOVED, FABRICATED, AND REPLACED CORRODED EDGE DOUBLER IAW SRM 53-3-3 FIG.6, 51-1-8, 51-1-21, AND DWG5612298.SDR UPS04842902Fitting · crackedINSPECTION TYPE: C1, LEFT WING FLAP HINGE STATION 3 FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 5642342 AND SRM 51-1-20D.SDR UPS04842888Longeron · crackedINSPECTION TYPE: C1, STATION 1770 LONG. 17L IS CRACKED REMOVED,FABRICATED AND REPLACED LONGERON IAW DWG. 5649327,AND SRM. 51-1-20D,51-1-21SDR UPS04842865Skin · crackedINSPECTION TYPE: C, FUSELAGE EXTERIOR SKIN IS CRACKED AT STATION 1745 AT LONGERON 15R. CUTOUT DAMAGED AREA, NDT VERIFIED NO CRACKS AT CUTOUT. FABRICATED AND INSTALLED FILLER, DOUBLER, FINGER DOUBLER IAW SRM 53-2-1 FIG 7.SDR UPS04842863Skin · damagedINSPECTION TYPE: C1, RT HORIZONTAL STAB L/E HAS SCREWS PULLED THROUGH SKIN AT XFS 178.750. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 55-2-1 FIG 4.SDR UPS04842845Longeron · crackedINSPECTION TYPE:C1 STATION 1770 LONG 17R IS CRACKED. REMOVED, FABRICATED AND REPLACED LONGERON SECTION IAW DWG 5649327 AND SRM 51-1-20D, 51-1-21.SDR DHL2004804513Fitting · crackedAFT FUSELAGE AFT LONGERON SPLICE FITTING CRACKED 1.000 AT STA 1690.000, L30R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1. REMOVED CRACKED FITTING IAW SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 581-1-8B. INSTALLED NEW FITTINSDR DHL2004804520Fitting · crackedAFT FUSELAGE AFT LONGERON SPLICE FITTING CRACKED 1.000 AT STA 1690.000, L-26R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1. REMOVED CRACKED FITTING IAW SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTINSDR UPS04842793Attach Angle · crackedINSPECTION TYPE: C1, VERTICAL FIN TO FUSELAGE ATTACH ANGLE HAS POPPED RIVET, LT SIDE, STA 1766. REMOVED PAINT IAW SRM 51-20-00. FOUND CRACK, NDT VERIFIED. FABBED REPAIR ANGLE IAW SRM 53-2-5 FIG16A. REMOVED AND REPLACED ANGLE IAW SRM 51-1-20D, 51-1-26, 51-1SDR UPS04842792Attach Angle · crackedINSPECTION TYPE: C1, VERTICAL FIN TO FUSELAGE ATTACH ANGLE CRACKED AT STA 1750 RT SIDE. STRIPPED PAINT IAW MM51-20-00. NDT VERIFIED CRACK. FABBED REPAIR ANGLE IAW SRM 53-2-5 FIG.16A. REMOVED AND REPLACED ANGLE IAW SRM 51-1-20D, 51-1-11, 51-1-26.SDR IXXA060138SSkin · corrodedDURING ROUTINE C-CHECK FOUND INTERNAL SKIN CORROSION AT STATION 610 BETWEEN LONGERON 33 RIGHT AND 34 RIGHT. REMOVED FASTENERS AS NEEDED TO REMOVE DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, DEBURRED, TREATED, PRIMED, INSTALLED REPAIR PARTS, ASDR IXXA060133SAngle · gougedDURING ROUTINE C CHECK, FOUND RIGHT WING JOINT AREA BETWEEN INBOARD AND OUTBOARD FLAPS, AREA ON UPPER OUTBOARD FLAP ANGLE GOUGED. REMOVED DAMAGE. FABRICATED REPAIR PART. LOCATED, DRILLED TRIMMED, DEBURRED, TREATED, PRIMED, INSTALLED REPAIR PART AND NEW FASSDR DHL2004804511Skin · crackedLEFT MLG INBOARD DOOR INTERNAL SKIN CRACKED 0.500 AT STA 912.000 (LWR PART). REMOVED FASTENERS IAW SRM 51-1-21 PG 1. PERFORMED STOP HOLE ON CRACK END AND FABRICATED DOUBLER (AL 7075-T6 0.050) IAW SRM 52-2-0 PG 1-2. CLEANED, TREATED AND PRIMED AREA AND DOUBLSDR DHL2004804521Fitting · corrodedAFT FUSELAGE AFT LONGERON SPLICE FITTING CORRODED AT STA 1690.000, L-26L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1. REMOVED CORRODED FITTING IAW SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IASDR UPS04842864Rib · crackedINSPECTION TYPE: C1, RIGHT WING LEADING EDGE LOWER RIB IS CRACKED AT FASTENER HOLE AT XFS 601. STOPDRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR ANGLES IAW SRM 57-2-0 FIG 2.SDR DHL2004804519Angle · crackedLEFT WING INBOARD SLOT SUPPORT ANGLE CRACKED 1.000, XILD 7095.000. REMOVED CRACKED SUPPORT ANGLE IAW SRM 51-1-21 PG 1. FABRICATED NEW ANGLE (AL 7075-0 0.063) IAWJ SRM 57-2-0 PG 1. PERFORMED HEAT TREATMENT TO NEW ANGLE IAW SRM 51-1-1 PG 1, 13, 17. PERFORMEDSDR DHL2004805007Warning Light · illuminatedWHILE EN ROUTE NR 1 ENGINE FIRE DETECTION SYSTEM ACTIVATED.SDR DHL2004804532Skin · crackedNR. 1072: EXTERNAL FUSELAGE-D BELLY DOOR AFT UPPER JAMB CORNER CRACKED 1.000, STA. 1440.000, L-26 TO L-27R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW AD 2004-06-06, SB DC8 53-0-78 R1, DWG SR08530019 CONFIGURATION H, DWG 5750776. REMOVED FASTENERS IAW SRM 51-1-SDR IXXA060121SSeat Track · wornDURING ROUTINE C-CHECK FOUND CAPTAIN'S OUTBOARD SEAT TRACK HAS EXCESSIVE WEAR AROUND LOCKPIN HOLES. REMOVED FASTENERS AS NEEDED TO REMOVE DAMAGED SEAT TRACK SECTION. FABRICATED REPAIR PARTS, LOCATED, DRILLED, DEBURRED, TREATED, PRIMED, INSTALLED REPAIR PARTSSDR DHL2004807013Bulb · burned outEMERGENCY LIGHTS DISARMED, LIGHT BULB BURNED OUT. RELAMPED EMERGENCY LIGHTS DISARMED. OPS CHECKED IAW MM CH 33-50-2,CHECKED GOOD.(P/N CM1864)SDR UPS04842913Support · crackedINSPECTION TYPE:C1 RIGHT WING FLAP HINGE 3 SUPPORT FITTING IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FITTING IAW DWG 5642342 AND SRM 51-1-20D, 51-1-21.SDR DHL2004804518Fitting · crackedITEM REF. NR.2095: LT IB STUB WING ZEE PAN FITTING CRACK 4.000, STA XILD 43.188. REMOVED AND REPLACED CRACKED ZEE PAN FITTING, STA XILD 43.188 (LT IB STUB WING) IAW SRM 51-1-20D PG. 21, SRM 51-1-21 PG.1.SDR DHL2004804524Floorbeam · crackedMAIN CARGO COMPT BEAM WEB CRACK 2.500, STA 960.000 RBL 59 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DC8 SRM 53-7-3 PG 17-18, DC8 SRM 51-2-0 PG 78, DC8 SRM 51-2-1 (TR 51-130) JAN 26-04 FIG 1. REMOVED FASTENERS IAW DC8 SRM 51-1-20D PG 21. PERFORMED STOP HOLESDR DHL2004804516Bracket · crackedNR 1 ALT TANK AFT BOOSTER PUMP BRACKET CRACKED. REMOVED AND REPLACED CRACKED BRACKET ON NR 1 ALT TANK AFT BOOSTER PUMP IAW SRM 51-3-0 PG 1.SDR DHL2004804517Bracket · crackedITEM REF. NR. 0519: NR 1 ALT TANK FWD BOOSTER PUMP BRACKET CRACKED. REMOVED AND REPLACED CRACKED BRACKET ON NR 1 ALT. TANK FWD BOOSTER PUMP IAW SRM 51-3-0 PG.1SDR DHL2004804512Bracket · crackedRIGHT OUTBOARD AILERON LWR SECTION HINGE BRACKET 1.000 CRACKED, STA XA 752.000. REMOVED CRACKED BRACKET IAW DC8 SRM 51-1-21 PG 1, DC8 SRM 51-3-0 PG 1. CLEANED, TREATED AND PRIMED AREA IAW DC8 SRM 51-1-8B. INSTALLED NEW BRACKET IAW DC8 SRM 51-1-21 PG 1, DC8 SDR IXXA060166SFrame · corrodedDURING ROUTINE C-CHECK, FOUND CORRODED FRAME AT STATION 70 BETWEEN LONGERON 31 RIGHT AND 32 RIGHT. REMOVED FASTENERS AS NEEDED TO REMOVE ATTACHING FRAME STRUCTURE. REMOVED FASTENERS AS NEEDED TO REMOVE DAMAGED FRAME. RECEIVED NEW FRAME, FABRICATED FRAME SPL
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