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 UPS02837850Fitting · crackedINSPECTION TYPE:C RT AFT OVERWING EMERGENCY DOOR AFT FRAME ATTACH ANGLE CRACKED. REMOVED DAMAGED FITTING PER SRM 51-1-20D. INSTALLED PER SRM 51-1-20D.SDR UPS02837734Attach Angle · crackedINSPECTION TYPE:C INTERCOSTAL ATTACH ANGLE CRACKED AT STA 600 RBL 12. REMOVED ANGLE, FABRICATED REPLACEMENT PER DAC DWG 5610326, INSTALLED PER SRM 51-1-21.SDR UPS02837886Fitting · crackedINSPECTION TYPE:C23 AFT PIT BILGE Z-FITTING CRACKED O/B OF L34R AT STA 1180. REMOVED CRACK Z-FITTING, LOCATED AND DRILLED NEW FITTING AND SPLICES IAW DC8 SRM 51-1-8. INSTALLED NEW FITTING IAW DC8 SRM 53-2-0 AND 51-120D.SDR UPS02837885Floorbeam · corrodedINSPECTION TYPE:C23 AFT PIT LT TUNNEL CORR ON BOTTOM OF CABIN FLOORBEAM UPPER FWD FLANGE AT STA 1240 LBL 62. REMOVED CORROSION IAW DC8 SRM 51-1-8, OUT OF LIMITS IAW DC8 SRM 53-2-0. FABBED AND INSTALLED IAW DC8 SRM.SDR UPS02837774Fitting · crackedINSPECTION TYPE:C23 AFT PIT BILGE Z-FITTING CRACKED O/B OF L35R STA 1180. REMOVED CRACKED FITTING, FABBED SPLICES FOR FITTING REPAIR AND INSTALLED NEW FITTING IAW DC8 SRM 51-1-21, 53-2-0 NOTE 17.SDR UPS02837751Fitting · crackedINSPECTION TYPE:C23 AFT PIT BILGE Z-FITTING CRACKED O/B AT L28L STA 1180. REMOVED CRACKED Z-FITTING. INSTALLED FITTING AND SPLICES IAW DC8 SRM 53-2-0.SDR UPS02837745Skin · crackedINSPECTION TYPE:C STEEL DOUBLER AT UPPER FWD CORNER OF R1 DOOR DOES NOT CONFORM TO SRM. CUT OUT CRACKED AREA. FABRICATED AND INSTALLED REPAIR PARTS PER SRM 53-2-0 FIG 14.SDR UPS02837739Intercostal · crackedINSPECTION TYPE:C INTERCOSTAL CRACKED AT STA 1520 L33R. REMOVED CRACKED INTERCOSTAL IAW SRM 51-1-20D. FOUND ATTACH ANGLE AND CLIP DAMAGED BEYOND LIMITS. INSTALLED PARTS PER SRM 51-1-20D.SDR UPS02837919Skin · crackedINSPECTION TYPE:C1 FWD AND AFT LOWER CORNERS OF L-1 DOOR JAMB SKIN, INTERNAL DOUBLER, AND FRAME TO CUSP FITTING ARE CRACKED AT STA 25 AND 70 BETWEEN LONG 20L TO 21L. CUT OUT CRACKED SKIN, INTERNAL DOUBLER SEGMENT, FABRICATED AND INSTALLED SKIN SEGMENT, INTERNSDR UPS02837892Skin · damagedINSPECTION TYPE:C REMOVE STEEL DOUBLER AT L2 DOOR, LWR FWD CORNER & INSTALL APPROVED REPAIR PER SRM. REPAIRED PER UPS EO DC8-5330-16382-A.SDR UPS02837883Door Frame · crackedINSPECTION TYPE:C23 L1 DOOR CORNER UPPER FWD DOUBLER CONDUCTIVITY TEST SHOWS NOT TO BE ALUMINUM. REMOVED EXISTING DOUBLER, ROUTED OUT DAMAGED AREA, FABRICATED AND INSTALLED DOUBLERS IAW DC8 SRM 53-2-0 FIG 15.SDR IXXA0200005OCowling · departedEN ROUTE, SHORTLY AFTER TAKEOFF THE FLIGHT CREW HEARD AN ABNORMAL NOISE IN THE COCKPIT. THE FLIGHT CREW CYCLED THE LANDING GEAR BUT THE NOISE WAS STILL PRESENT. THE FLIGHT RETURNED TO MCO FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE AIRCRAFT WHICH RSDR UPS02837713Finger Doubler · corrodedINSPECTION TYPE:SP STA 1510 FINGER DOUBLER IS CORRODED BEYOND LIMITS BETWEEN LONG 22L TO 30L. REMOVED, FABRICATED AND REPLACED DOUBLER IAW DWG 5615372 AND SRM 51-1-21.SDR UPS02837657Battery Pack · dischargedINSPECTION TYPE:N/A EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER M/M 33-50-01.SDR UPS02837709Web · crackedINSPECTION TYPE:C2 TRAILING EDGE RIB ON O/B END IS CRACKED BY CUT OUT FOR BOLT ACCESS. REMOVED CRACKED WEB IAW DC8 SRM 51-1-20D & 51-1-21. LOCATED AND DRILLED NEW WEB IAW DC8 SRM 51-1-24. REMOVED SPOILER ATTACH FITTING IAW DC8 SRM 51-1-20D, 51-1-21. LOCATESDR UPS02837623Rib · crackedINSPECTION TYPE:C2 TRAILING EDGE RIB ON O/B END IS CRACKED BY CUT-OUT FOR BOLT ACCESS. REMOVED CRACKED WEB IAW DC8 SRM 51-1-24 & REMOVED SPOILER ATTACH IAW DC8 SRM 51-1-20 D & 51-1-21 LOCATED & DRILLED NEW SPOILER ATTACH FITTING IAW DC8 SRM 51-1-24 INSTALLED SDR IXXA0200017SSpar · crackedDURING ROUTINE C-CHECK INSPECTION, A CRACK WAS DETECTED ON THE RIGHT WING LOWER SPAR INBOARD OF THE #4 ENGINE PYLON FORWARD SECTION. FABRICATED AND INSTALLED REPAIR DOUBLER IN ACCORDANCE WITH DOUGLAS STRUCTURAL REPAIR MANUAL AND ENGINEERING ORDER 57-DC8-1837.SDR UPS02837720Clip · crackedINSPECTION TYPE:C2 LEFT WING NR 1 ALT TANK HAS 2 ATTACH CLIPS CRACKED AT O/B SKATE ANGLE AT XW485 BETWEEN STRINGER 62 & 63. REMOVED, FABRICATED ONE CLIP, REPLACED OTHER CLIP AND INSTALLED BOTH CLIPS IAW DWG 5804006 AND 5804007 AND SRM 51-1-20D.SDR UPS02837652Clip · crackedINSPECTION TYPE:C2 RT WING CLIP CRACKED AT XW467 BETWEEN S62 AND S63. REMOVED AND REPLACED CLIP IAW SRM 51-1-20D AND DAC DWG 5804006.SDR IXXA0200004OStrut · crackedEN ROUTE FROM TOL TO BDL, THE LANDING GEAR AND DOOR UNSAFE WARNING LIGHTS REMAINED ILLUMINATED AFTER GEAR RETRACTION. THE FLIGHT CREW CYCLED THE LANDING GEAR BUT THE UNSAFE WARNING INDICATION REMAINED THE SAME. THE FLIGHT RETURNED TO TOL FOR AND UNEVENTFUL LSDR UPS02837580Battery Pack · dischargedINSPECTION TYPE:IN EMERGENCY LIGHTS FAILED PREFLIGHT CHECK. REPLACED LIGHT BATTERY PACK, OPS CHECK NORMAL.SDR UPS02837723Fitting · crackedINSPECTION TYPE:C2 STRINGER FITTING CRACKED BETWEEN XRS 50 AND XRS 74 AT STRINGER 51 IN LEFT WING TANK. REMOVED AND REPLACED FITTING IAW DWG 3704841 AND SRM 51-1-20D, 51-1-20D, 51-1-23.SDR UPS02837656Longeron · crackedINSPECTION TYPE:C2 LOWER FLANGE CRACKED ON LONG 15R, STA 1753. REMOVED CRACKED LONGERON SECTION. FABRICATED SPLICE AND INSTALLED REPLACEMENT LONGERON SECTION PER 53-2-2 FIG 10.SDR UPS02837602Longeron · crackedINSPECTION TYPE:C2 STA 1753 CANTED FRAME HAS LONGERON 15L CRACKED. CUT OUT DAMAGED SECTION OF LONGERON, FABRICATED AND INSTALLED LONGERON REPAIR IAW SRM 53-2-2 FIG 10.SDR UPS02837701Pan · crackedINSPECTION TYPE:C2 STA 200 LONG 20R WEB AND DOOR PAN ARE CRACKED AT R-1 DOOR AFT LOWER CORNER. CUT OUT DAMAGE, NDT VERIFIED NO CRACKS. FABRICATED AND INSTALLED REPAIR DOUBLERS ON PAN AND WEB IAW SRM 53-2-0 FIG 23 AND DWG 5615700.SDR UPS02837653Doubler · brokenINSPECTION TYPE:C2 LT WING LOWER SPAR CAP DOUBLER BROKEN, PIECE MISSING AT XS520. REMOVED, FABRICATED AND REPLACED DOUBLER IAW SRM 57-2-1 FIG 14 A.SDR UPS02837651Longeron · crackedINSPECTION TYPE:C2 LONGERON 11R CRACKED AT R2 DOOR UPPER AFT CORNER. REMOVED CRACKED LONGERON SECTION FROM 1570 TO 1690. INSTALLED REPLACEMENT SECTION IAW SRM 53-1-0, 51-1-21, 51-1-20D.SDR UPS02837606Attach Angle · crackedINSPECTION TYPE:C2 LEFT WING CENTER L/E VERTICAL ATTACH ANGLE IS CRACKED AT LOWER END AT XS 520. REMOVED, FABRICATED AND INSTALLED REPLACEMENT ANGLE IAW DWG 9753297 AND SRM 51-1-20D.SDR UPS02837604Rib · crackedINSPECTION TYPE:C2 LEFT WING L/E LOWER RIB IS CRACKED AT XFS 341.5. STOP DRILLED CRACK, NDT VERIFIED CRACK IS TERMINATED, FABRICATED AND INSTALLED REPAIR DOUBLERS IAW SRM 57-2-0 FIG 2.SDR UPS02837565Battery Pack · dischargedINSPECTION TYPE:N/A EMERGENCY LIGHT DIM. REMOVED AND REPLACED EMERGENCY EXIT BATTERY PACK IAW MM 33-50-01.SDR UPS02837699Fitting · crackedINSPECTION TYPE:C2 STA 388 LONG 31L SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3754473 AND SRM 53-1-0, 51-1-20D.SDR UPS02837721Fitting · crackedINSPECTION TYPE:C2 FRAME FITTING IS CRACKED AT STA 781 ON FWD SIDE ABOVE WING CENTER SECTION LBL 59. REMOVED, FABRICATED AND REPLACED FITTING IAW DWG 5641007, 8110-3 APPROVED DH SK 703-641 AND DC8-53-20143A.SDR UPS02837697Longeron · corrodedINSPECTION TYPE:C2 STA 118 LONG 36 IS CORRODED BEYOND LIMITS. REMOVED CORRODED LONGERON SECTION STA 100-130, FABRICATED AND INSTALLED LONGERON REPAIR IAW SRM 53-2-2 FIG 10.SDR UPS02837655Door Frame · crackedINSPECTION TYPE:C2 L2 LOWER AFT FRAME CRACKED AT STA 1660 NEAR 19L. REMOVED DAMAGED FRAME SECTION. FAB AND INSTALLED FRAME SECTION, FILLER AND DOUBLER PER DAC DWG 5751040, DC8-5310-11728 AND DC8-53A-011.SDR UPS02837654Skin · crackedINSPECTION TYPE:C2 X-RAY REVEALED ONE INCH CRACK AT R2 DOOR UPPER AFT DOUBLER STA 1660 LONG 11R. CUT OUT DAMAGE. NDT VERIFIED ALL DAMAGE REMOVED. FABRICATED AND INSTALLED FILLER AND DOUBLERS PER SRM 53-1-0 FIG 16.SDR UPS02837603Stiffener · crackedINSPECTION TYPE:C2 LEFT HORIZONTAL STAB L/E STIFFENER IS CRACKED AT XAR 0. REMOVED AND REPLACED STIFFENER IAW DWG 5654501 AND SRM 51-1-20D.SDR UPS02837722Web · corrodedINSPECTION TYPE:C2 STATION 1322 LONG 21L AT LBL 67 CUSP IS CORRODED BEYOND LIMITS. CUT OUT CUSP SECTION BETWEEN STA 1250-1390, FABRICATED AND INSTALLED REPAIR SECTION OD CUSP IAW DWG J060296 AND SRM 53-2-5 FIG 15.SDR UPS02837696Skin · crackedINSPECTION TYPE:C2 LEFT WING CENTER L/E UPPER SKIN IS CRACKED AND HAS INTERGRANULAR CORROSION BETWEEN XFS 341 TO XFS 366.5. CUT OUT CRACKED AND CORRODED AREAS, NDT VERIFIED NO CRACKS. FABRICATED AND INSTALLED DOUBLER AND FILLERS IAW SRM 57-2-1 FIG 38 AND UPSSDR UPS02837650Longeron · corrodedINSPECTION TYPE:C2 L35L HEAVILY CORRODED AT SPILCE FITTING, STA 1690. CUT OUT CORRODED SECTION OF LONG, FABRICATED AND INSTALLED LONGERON REPAIR IAW SRM 53-2-2 FIG 10.SDR UPS02837605Frame · crackedINSPECTION TYPE:C2 STA 1580 FUSELAGE FRAME IS CRACKED AT LOWER END AT LONG 21L. REMOVED DAMAGED AREA, NDT VERIFIED NO CRACKS AROUND CUTOUT, FABRICATED AND INSTALLED REPAIR DOUBLER IAW EO DC8-53A-011.SDR UPS02837569Skin · crackedINSPECTION TYPE:C2 LEFT WING L/E LOWER SKIN IS CRACKED AT DRAIN HOLE AT XFS 597.5. STOP DRILLED CRACK, NDT VERIFIED CRACK IS TERMINATED, FABRICATED AND INSTALLED DOUBLER IAW EO DC8-5780-4087-B APPX C.SDR UPS02837567Skin · corrodedINSPECTION TYPE:C2 LEFT WING CENTER L/E UPPER SKIN HAS INTERGRANULAR CORROSION AT XFS 329. CUT OUT CORRODED AREA. FABRICATED AND INSTALLED FILLER AND DOUBLER IAW SRM 57-2-1 FIG 38.SDR UPS02837549Container · damagedINSPECTION TYPE:PFLT REF M231085 SLIDE ASSY OUT OF DOOR, BAR HOLDER BROKEN OFF OF CONTAINER. REMOVED AND REPLACED SLIDE EVAC CONTAINER. REINSTALLED SAME SLIDE ASSY INTO CONTAINER PER MM 25-60-01 3B, P/N ON & OFF-5750113-505, S/N ON-TAG645594A. OK FOR SERVICSDR UPS02837698Skin · crackedINSPECTION TYPE:C2 FUSELAGE SKIN IS CRACKED BEYOND PREVIOUS REPAIR CUTOUT, AT STATION 25 BETWEEN LONG 10L TO 11L AT L-1 DOOR FWD UPPER CORNER OPENING. CUT OUT DAMAGE, NDT VERIFIED NO CRACKS, FABRICATED AND INSTALLED FILLER AND DOUBLERS IAW SRM 53-2-0 FIG 15.SDR UPS02837620Door Frame · crackedINSPECTION TYPE:C2 L2 UPPER FWD DOOR JAMB CORNER CRACKED AT FASTENER HOLE. REPAIRED AREA IAW DC8 SRM 53-2-0 FIG 18.SDR UPS02837613Doubler · crackedINSPECTION TYPE:C2 REMOVED STEEL DOUBLER FROM L2 DOOR JAMB EXTERIOR UPPER L2 UPPER AFT CORNER. REPAIRED AREA IAW DC8 SRM 53-2-0 FIG 18.SDR UPS02837612Pan · crackedINSPECTION TYPE:C2 C PIT DOOR PAN CRACKED AT UPPER FWD CORNER NEAR GRAB HANDLE. REMOVED DOOR PAN SECTION P/N 57542060 -17 & REPLACED IT WITH NEW DOOR PAN SECTION IAW 51-1-8, 51-3-0, 51-1-21, 51-1-20D.SDR UPS02837621Fitting · corrodedINSPECTION TYPE:C2 AFT PIT FS 1220 C3 DOOR JAMB SHROUD SUPPORT FITTING IS CORRODED. LOCATED AND DRILLED NEW FITTING IAW DC8 SRM 51-1-24, INSTALLED FITTING IAW DC8 SRM 51-3-0.SDR UPS02837619Longeron · corrodedINSPECTION TYPE:C2 AFT ACCY COMPARTMENT FS 1660 LONG 32R IS CORRODED.SDR UPS02837618Fitting · corrodedINSPECTION TYPE:C2 AFT ACCY COMPARTMENT FS 1660 LONG 32R END FITTING IS CORRODED. RECD LOCATED DRILLER FITTING IAW DC8 SRM 51-1-24 AND INSTALLED IAW DC8 SRM 51-1-21 & 51-1-20D.
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