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 UPS05845587Fitting · corrodedINSPECTION TYPE:SP, STA 70 L35R END FITTING HAS EXFOLIATION CORROSION AFT CHORD SIDE. REMOVED AND REPLACED END FITTING IAW SRM 51-1-20D AND 51-1-21.SDR IXXA05SMN222SSkin · crackedDURING C CHECK INSPECTION, NR 3 RT STUB WING LWR SKIN CRACK 2 AT STA XW 255.000. PERFORMED MAJOR REPAIR IAW DC8 SRM 57-2-1 FIG 37, EO SEMAN NR 20051284 DATED 09-27-05. REMOVED FASTENERS IAW DC8 SRM 51-1-20D. REMOVED CORROSION IAW DC8 SRM 51-1-8 PG 17-18. FSDR IXXA05SMN221SSkin · crackedDURING C CHECK INSPECT, LT WING LWR SKIN CRACK AT STA XRS 172.000 BETWEEN S-56 AND S-57. PERFORMED MAJOR REPAIR IAW DC8 SRM 57-2-1 FIG 1, EO SEMAN # 20051287 DATED 09-29-05. REMOVED FASTENERS IAW DC8 SRM 51-1-21, DC8 SRM 51-1-20D. STOP DRILLED CRACK END IAW SDR IXXA05SMN220SSkin · scratchedDURING ROUTINE C CHECK INSPECTION, EXTERNAL FUS. (C) BELLY PIT DOOR SKIN SCRATCHES OUT OF LIMITS. PERFORMED MAJOR REPAIR, REMOVED FASTENERS IAW SRM 51-1-20D. REMOVED DAMAGED SECTION IAW DWG NR ED-4075. NDT INSPECTED IAW NDT SPM PART 06-10-01-001. NEITHERSDR IXXA05SMN219SFitting · corrodedDURING ROUTINE C CHECK INSPECTION, FWD ACCY COMPT, FITTING CORRODED, STA 60.000, 70.000 L-34R. PERFORMED MAJOR REPAIR IAW MSG NR 1-126059161-2 DATED 09-26-05, SRM 52-1-0 PG 1. REMOVED DAMAGED SKIN IAW SRM 51-1-21. FABRICATED NEW SKIN (AL7075T6 0.050) IAW MSSDR IXXA05SMN218SFitting · corrodedDURING ROUTINE C CHECK INSPECTION, FWD ACCY COMPT FITTING CORRODED, STA 60.000, 70.000 L-34R. REMOVED CORROSION FROM FITTING IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. REMOVED CORRODED FITTING IAW SRM 51-1-21, SRM 51-1-20D. CLEANED,SDR IXXA05SMN217SLongeron · crackedDURING ROUTINE C-CHECK INSPECTION, AFT FUSELAGE LONGERON 17L CRACKED 1, STA 1786.000PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1, EO SEMAN NR 20051285 DATED 09-27-05. REMOVED CRACKED LONGERON IAW SRM 51-1-20D. FABRICATED NEW LONGERON (EXTRUSION P/N S1616757) ISDR IXXA05SMN216SLongeron · crackedDURING ROUTINE C CHECK INSPECTION, AFT FUSELAGE LONGERON 17R CRACKED 1, STA 1786.000. PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1, EO SEMAN NR 20051286 DATED 09-27-05. REMOVED CRACKED LONGERON IAW SRM 53-5-1 FIG 7 (SHEET 1) ITEM B SRM 51-2-0 FIG 5 (SHEET 37).SDR IXXA05SMN215SFitting · crackedDURING ROUTINE C CHECK INSPECTION, AFT FUSELAGE SPLICE FITTING CRACKED 2, STA 1770.000 RT, L-17R. REMOVED CRACKED FITTING IAW SRM 51-3-0, SRM 51-21-1. FABRICATED NEW FITTING (AL7075T651) IAW ATI REPAIR SPECIFICATION NR 2003-05, EA SEMAN NR 20051318. HEAT TRSDR IXXA05SMN214SSkin · crackedDURING ROUTINE C CHECK INSPECTION, RT IB AIL L/E UPPER PLATING CRACK .2500 AT STA XA 470.000. PERFORMED MAJOR REPAIR IAW SRM 57-8-1 FIG 1, EO SEMAN NR 20051280 DATED 09-26-05. REMOVED DAMAGED PLATING IAW SRM 51-1-21. FABRICATED NEW PLATING (AL2024T3 0.040) SDR IXXA05SMN213SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FWD LOWER FUSELAGE SPLICE FITTING CRACKED 8, STA 445, STA 455.000 L-31L. REMOVED CRACKED FITTING IAW SRM 51-1-20D, SRM 51-3-0. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D, SRM 5SDR IXXA05SMN212SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FWD LOWER FUSELAGE. SPLICE FITTING CRACKED 2 , STA 445.000, STA 455.000 L-31R. REMOVED CRACKED SPLICE FITTING IAW SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D AND SDR IXXA05SMN211SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FWD CARGO COMPT RT TUNNEL SPLICE FITTING CRACKED 2, STA 445.000 L-27R REMOVED CRACKED SPLICE FITTING IAW SRM 51-1-20D PAGE 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW SPLICE FITTING IAW SRM 51-1-20DSDR IXXA05SMN210SSkin · corrodedDURING C CHECK INSPECTION, RT OUTER WING INBD L/E UPPER SKIN CORRODED, STA XFS 710.000. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 05461 DATED 10-10-05, SEMAN DWG # ED-4070 DATED 10-07-05, EO SEMAN # 20051276 DATED 10-10-05. REMOVED FASTENERS IAW DC8 SRM SDR IXXA05SMN209SSkin · crackedDURING ROUTINE C CHECK INSPECTION, RT OUTER WING IB L/E LOWER SKIN, .2500 IN CRACK, STA XFS 597.500. PERFORMED MAJOR REPAIR DATED 10-07-05, DWG NR ED-4069 DATED 10-06-05, EO NR 20051275 DATED 10-07-05. REMOVED FASTENERS IAW SRM 51-1-21, SRM 51-3-0. PERFORMESDR IXXA05SMN207SFitting · crackedDURING ROUTINE C CHECK INSPECTION, AFT LWR CARGO BILGE INTERIOR, FITTING CRACKED 2, STA 1215.000 L-29R. REMOVED CRACKED FITTING IAW SRM 51-3-0 PG 1. CLEANED, TREATED, PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-3-0, SRM 51-1-20D, SRM 51-3-SDR IXXA05SMN206SSkin · corrodedDURING C CHECK INSPECT, LT WING CTR UPPER L/E CORRODED, STA XFS 304 310.000. PERFORMED MAJOR REPAIR IAW DC8 SRM 57-2-1 FIG 44, EO SEMAN # 20051213 DATED 09-22-05. REMOVED FASTENERS IAW DC8 SRM 51-1-21. REMOVED CORROSION IAW DC8 SRM 51-1-8 PG 17-18. FOUND OSDR IXXA05SMN205SSkin · crackedDURING C CHECK INSPECT, LT WING CTR L/E SKIN CRACKED ½, STA XFS 285.250. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 # 05451 DATED 10-07-05, SEMAN DWG # ED-4066 DATED 10-03-05, EO SEMAN # 20051212 DATED 10-07-05. REMOVED FASTENERS IAW DC8 SRM 51-1-21, DC8 SRMSDR IXXA05SMN204SFitting · crackedDURING ROUTINE C CHECK INSPECTION, MAIN CARGO COMPT FITTING CRACKED 1.5, STA 902.000 L-19L. REMOVED CRACKED FITTING IAW SRM 51-1-20D. FABRICATED NEW FITTING (AL7075T651) IAW MFG DWG NR 3779498, EA NR 20051314. PERFORMED NDT INSPECTION IAW NDT SPM PART 08-00SDR IXXA05SMN203SFitting · crackedDURING ROUTINE C CHECK INSPECTION, MAIN CARGO COMPT. AFT FITTING CRACKED 1, STA 857.000 L-19LREMOVED CRACKED FITTING IAW SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D, SRM 51-3-1. (TORQUE)SDR IXXA05SMN202SFitting · crackedDURING ROUTINE C CHECK INSPECTION, MAIN CARGO COMPT. AFT FITTING CRACKED 3, STA 834.5 L-14RREMOVED CRACKED FITTING IAW SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D PG 9, SRM 51-3-1 (TORQUE).SDR IXXA05SMN201SFitting · crackedDURING ROUTINE C CHECK INSPECTION, MAIN CARGO COMPT FWD FITTING CRACKED 2, STA 781.000 L-19L. REMOVED CRACKED FITTING IAW SRM 51-1-20D. FABRICATED NEW FITTING (AL7075T651) IAW MFG DWG NR 3779978, EA NR 20051313. PERFORMED NDT INSPECTION IAW NDT SPM PART 08-SDR IXXA05SMN200SVane · elongatedDURING C CHECK INSPECT, LT WING OTBD SLOT VANE HOLES ELONGATED, STA XS 520.168. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 05447 DATED 10-05-05, SEMAN DWG # ED-4064 DATED 09-30-05, EO SEMAN # 20051206. REMOVED FASTENERS IAW DC8 SRM 51-1-21, DC8 SRM 51-3-0SDR UPS05845520Indicator · inoperativeALL 3 (CAPT'S, FO'S & ALTERANTE) AIRSPEED INDICATIONS ARE UNRELIABLE. AIR TURN BACK - EMERGENCY DECLARED. REPLACED STANDBY ALT/AIRSPEED INDICATOR PER MM 34-11-02-4. R&R AUXILIARY PITOT STATIC DRAIN. SYSTEM OPS CKS NORMAL IAW AMM 34-12-00-5.SDR IXXA05SMN199SSkin · crackedDURING C CHECK INSPECTION, RT WING OTBD L/E LOWER SKIN CRACKED 1” APPROX, BETWEEN STA XFS 710.000 AND XFS 716.250. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 # 05461 DATED 10-05-05, SEMAN DWG # ED-4071 DATED 10-06-05, EO SEMAN # 20051277 DATED 10-05-05. REMOSDR IXXA05SMN198SSkin · crackedDURING C CHECK INSPECT, RT WING CTR L/E LOWER SKIN CRACKED 1” APPROX, BETWEEN STA XFS 335.250 AND XFS 340.000. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 05463 DATED 10-11-05, SEMAN DWG NR ED-4067 DATED 10-11-05, EO SEMAN NR 20051227 DATED 10-11-05. REMOVSDR IXXA05SMN197SSkin · crackedDURING C CHECK INSPECTION, RT WING OTBD L/E LOWER SKIN CRACKED 1” APPROX, BETWEEN STA XFS 566.250 AND XFS 572.500. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 # 05446 DATED 10-05-05, SEMAN DWG # ED-4068 DATED 09-27-05, EO SEMAN # 20051231 DATED 10-05-05. REMOSDR UPS05845484Regulator · inoperativeCREW OXYGEN REGULATOR INOP. REPLACED CAPTAIN'S 02 REGULATOR PER 35-10-07. OPS CHECK NORMAL.SDR IXXA05SMN196SFrame · crackedDURING ROUTINE C CHECK INSPECTION, NR 2 ENGINE, T/R LT INTERNAL PART FRAME CRACKED 2 AT 10 O’CLOCK POSITION, YN 208.000. REMOVED DEFLECTION FAIRING SEAL, PERFORMED STOP HOLE OF 0.06 IAW CFM 56-2 MM 78-31-41 REP. 016 PAGE 2. FAB`D STIFFENER (STEEL SHEET 0.080SDR IXXA05SMN194SCap · crackedDURING ROUTINE C CHECK INSPECTION, MID ACCY CMPT. CAP CRACKED 1, STA 680.000 BETWEEN L 27 AND L 28LPERFORMED MAJOR REPAIR IAW SRM 53-2-5 FIG 14, EO SEMAN NR 20051313 DATED 09-30-05. REMOVED FASTENERS IAW SRM 51-1-20D PG 1. STOP DRILLED ON CRACK END IAW SRMSDR IXXA05SMN193SSkin · crackedDURING ROUTINE C CHECK INSPECTION, LT WING. UPPER SKIN AROUND HILOK CRACKED, XRS 72.000 S.9PERFORMED MAJOR REPAIR IAW SRM 57-2-1 FIG 17, EO SEMAN NR 20051211 DATED 09-21-05. REMOVED FASTENERS IAW SRM . REMOVED DAMAGED SECTION IAW SRM 57-2-1 FIG 17. PERFORMSDR IXXA05SMN192SDoor · crackedDURING ROUTINE C CHECK INSPECTION, LT WING NR 2 ALT TANK 506B ACCESS DOOR CRACKED. REMOVED AND REPLACED CRACKED ACCESS DOOR NR 506 B (NR 2 ALT TANK) IAW SRM 51-3-0, SRM 51-3-1 (TORQUE) REFER TO JC 99116 FOR LEAK CHECK.SDR IXXA05SMN191SSkin · delaminatedDURING ROUTINE C CHECK INSPECTION, VERT STAB DELAMINATED SKIN ON RUDDER TAB. REMOVED DAMAGED SECTION PLUS FABRICATED DOUBLER (AL2024T3 0.012) IAW SRM 55-2-2 PARA 2. BONDED CORE PLUS DOUBLER WITH HYSOL IAW SRM 51-1-9. REFER TO NR 2801 FOR WEIGHT.SDR IXXA05SMN190SRivet · improperDURING C CHECK INSPECTION, FWD LWR FUSELAGE BELLY, STA FS 545.000 L-35.75R, UPGRADE REPAIR DOUBLER TO INCORPORATE A MIN OF 3 ROWS OF RIVETS. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 # 05447 DATED 10-05-05, SEMAN DWG # ED-4061 DATED 09-27-05, EO SEMAN # 2005SDR IXXA05SMN189SRivet · improperDURING C CHECK INSPECT, AFT LWR FUSELAGE BELLY, STA FS 1683.000 L-35.5R, UPGRADE REPAIR DOUBLER TO INCORPORATE A MIN OF 3 ROWS OF RIVETS. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 05448 DATED 10-05-05, SEMAN DWG NR ED-4063 DATED 10-03-05, EO SEMAN NR 2005SDR IXXA05SMN188SRivet · improperDURING C CHECK INSPECT, AFT LWR FUSELAGE BELLY, STA FS 1143 L-35.5L, UPGRADE REPAIR DOUBLER TO INCORPORATE A MIN OF 3 ROWS OF RIVETS. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 05463 DATED 10-11-05, SEMAN DWG NR ED-4062 DATED 10-10-05, EO SEMAN NR 20051197SDR IXXA05SMN187SRivet · improperDURING C CHECK INSPECT, FWD LWR FUSELAGE BELLY, STA FS 399.000 L-35.75R UPGRADE REPAIR DOUBLER TO INCORPORATE A MINIMUM OF 3 ROWS OF RIVETS. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 05448 DATED 10-05-05, SEMAN DWG NR ED-4060 DATED 10-03-05, EO SEMAN NR 2SDR IXXA05SMN186SRivet · improperDURING ROUTINE C CHECK INSPECTION, FWD LOWER FUSELAGE BELLY, STA FS 173.000 L-35.5R. UPGRADE EXTERNAL REPAIR DOUBLER TO INCORPORATE A MINIMUM OF 3 ROWS OF RIVETS. PERFORMED MAJOR REPAIR, REMOVED EXISTING REPAIR DOUBLER IAW SRM 51-1-21. REMOVED DAMAGED SECTIOSDR IXXA05SMN185SRivet · incorrectDURING ROUTINE C CHECK INSP, FUSELAGE BELLY, STA FS 76.000 L-35. 75R. UPGRADE REPAIR DOUBLER TO INCORP A MINIMUM OF 3 ROWS OF RIVETS. PERFORMED REPAIR IAW NR 05446 DATED 10-05-05, DWG NR ED-4058 DATED 09-27-05, EO NR 20051191 DATED 10-05-05. REMOVED EXISTINGSDR UPS05845577Fitting · crackedINSPECTION TYPE:SP L33R END FITTING CRACKED AT STA 12. REMOVED AND REPLACED END FITTING AT STA 12 L33R IAW SRM 51-3-0 AND SRM 51-1-20D.SDR UPS05845570Longeron · corrodedINSPECTION TYPE:SP L33R FS 70 TO FS 8.0 HAS EXFOLIATION CORROSION. REMOVED AND REPLACED LONGERON 33R IAW DWG 3642838 AND SRM 51-1-20D.SDR UPS05845567Shear Tie · corrodedINSPECTION TYPE: SP, SHEAR TIE AT FS 35 L34R TO L34L HAS EXFOLIATION CORROSION. REMOVED SHEAR TIE AT FS 35 L34R - L34L IAW SRM 53-2-0 FIG 1F FABRICATED AND INSTALLED SHEAR TIE AT FS 35 L34R - L34L IAW DWG 5613836, AND SRM 51-1-21, 51-1-20D.SDR UPS05845563Shear Tie · corrodedINSPECTION TYPE:SP SHEAR TIE AT STA 55 L34R TO L34L HAS EXFOLIATION CORROSION. REMOVED SHEAR TIE AT STA 55 L34R - L34L IAW SRM 51-1-21 FABRICATED AND INSTALLED SHEAR TIE AT STA 55 L34R -L34L IAW DWG 5613836, SRM 51-1-21 AND SRM 51-1-20D.SDR UPS05845584Structure · corrodedINSPECTION TYPE:SP, STA 70 LOWER AFT CHORD HAS EXFOLIATION CORROSION AT APPROX L28R-L33L. CUT OUT CORRODED CHORD, FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 51-1-21, 51-1-20D, 53-2-5 FIG 8C.SDR IXXA05SMN184SDoor · crackedDURING ROUTINE C CHECK INSP, EXTERNAL FUS. FREON SYS EXHAUST DOOR AFT UPPER CORNER CRACKED .5, STA 54.000 L-2/8L L29L. PERFORMED MAJOR REPAIR IAW SRM 53-2-0 FIG 13 (SHEET 1, 5), TR NR 53-169, EO SEMAN NR 20051190 DATED 09-20-05. REMOVED EXISTING REPAIR DOUBLSDR IXXA05SMN183SSkin · crackedDURING ROUTINE C CHECK INSPECTION, NOSE SECTION. RT PRIMARY HEAT EXCHANGER AFT LWR CORNER HAS STRUCTURAL MODIFICATION CRACKED .7500 ON DOUBLER STA 12.000 L-27R. PERFORMED MAJOR REPAIR IAW MM 53-30-09, EO SEMAN NR 20051205 DATED 09-21-05. REMOVED FASTENERS IAWSDR IXXA05SMN182SDoor · crackedDURING ROUTINE C CHECK INSP, FWD ENTRANCE DOOR.- JAMB FWD LWR CORNER CRACKED, STA 130.000 L-21L.PERFORMED MAJOR REPAIR IAW AD 2000-20-08, S/B 53-075, SRM 53-2-0 FIG 15 SHEET 2, SRM 53-2-0, TR NR 53-196, MFG DWG NR SRD8530021, EO NR 20051204 DATED 09-21-05, DSDR UPS05845571Longeron · corrodedINSPECTION TYPE:SP L30R FS 70 TO FS 8, LONGERON 30R HAS EXFOLIATION CORROSION. REMOVED AND REPLACED LONGERON 30R AT FS 70 - FS 8 IAW SRM 51-1-20 AND 51-20D.SDR UPS05845569Doubler · corrodedINSPECTION TYPE:SP INTERNAL DOUBLER HAS EXFOLIATION CORROSION AT FS 8 - FS 70 L29R L31R. REMOVED DOUBLER AT FS 8 TO FS 70 L29R TO 31R IAW SRM 51-1-21. FABRICATED AND INSTALLED INTERNAL DOUBLER IAW DWG 5649028 AND SRM 51-1-21.SDR UPS05845568Finger Doubler · corrodedINSPECTION TYPE:SP FINGER DOUBLER AT FS 8 TO FS 70 L31R HAS EXFOLIATION CORROSION. REMOVED FINGER DOUBLER AT FS 8 - FS 70 L31R IAW SRM 51-1-20D FABRICATED AND INSTALLED FINGER DOUBLER AT FS 8 TO FS 70 IAW DWG 5649028 AND SRM 51-1-21.
Back to Douglas DC-8-71F