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 RRXA991462Skin · crackedDURING A MAINTENANCE VISIT FOUND CRACK, RT WING L/E UPPER SKIN AT STA XFS 423.25 AT 2 RIVET HOLES, ALSO HAS 12 RIVET HEAT CRACKED. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW FASDR RRXA991439Frame · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, LT WING, L/E AUX TANK UPPER AFT MOUNTING CHORD BETWEEN STA XFS 7.50 AND XFS 20.0. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED THE CHORD IAW DC8 SDR RRXA991436Web · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, NLG UPPER PRESSURE PANEL JUST AFT OF AIR CONDITIONING UNIT BETWEEN STA -32 AND STA -12, AND BETWEEN BL 5 RIGHT AND BL 10 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SSDR RRXA991637Web · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, WEB, BETWEEN STA 920 AND STA 940, AT LONGERON 22 RIGHT AND RIGHT BL 60. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR WEB IAW FAASDR RRXA991633Floorbeam · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, FLOOR SUPPORT AT STA 600, BETWEEN LONGERON 33 RIGHT AND LONGERON 36. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FLOOR SUPPORT IAW DACSDR RRXA991438Web · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, WEB, BETWEEN STA Y920 AND SAT Y940, AT LONGERON 22 RIGHT, BL 60 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED WEB IAW FAA APPROVED DER ENGISDR RRXA991431Support · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION, FUSELAGE, FLOOR SUPPORT, AT LOCATION Y600, BETWEEN LONGERONS 33 RIGHT AND LONGERON 36. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FLOOR SUPPOSDR UPS99830464Landing Gear · collapsedINSPECTION TYPE:N/A, AFTER LANDING AND COMING TO A STOP ON RUNWAY 32R, THE NOSE GEAR COLLAPSED INTO THE WHEEL WELL. *S/D* ALL REQUIRED EO'S IE DC8-5300-11498A HAVE BEEN C/W BY TIMCO. PER FERRY FLIGHT PERMIT NR 9086 ALL FERRY FLIGHT PROCEDURES HAVE BEEN ACCOSDR UPS99830353Girt Bar · failedINSPECTION TYPE:N/A, ESCAPE SLIDE GIRT BAR RETAINER FAILED UPON EGRESS OF A/C, SLIDE SEPARATED FROM A/C. STILL I/W ON LOG PAGE 208929/2. FOLLOW UP ACTION SCHEDULED FOR REMAINDER OF DC-8 FLEET. *S/D* INSTALLED HARDWARE IAW EO DC-8-2560-11700, OPS CK NORMAL SDR RRXA991666Fitting · crackedDURING A MAINTENANCE VISIT FOUND CRACK, FLOORBEAM SUPPORT STRUT LOWER FITTING CRACKED AT AFT SIDE OF TEE AT STA 1160, TOP OF LONGERON 29 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED SDR RRXA991665Fitting · crackedDURING A MAINTENANCE VISIT FOUND CRACK, LONGERON SPLICE FITTING CRACKED AT LONGERON 31 LEFT, AT STA 1260. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FITTING IAW MFG DWG 4753059 AND DCSDR RRXA991654Intercostal · crackedDURING A MAINTENANCE VISIT FOUND CRACK, INTERCOSTAL BETWEEN STA 580 AND STA 600 AT LONGERON 33 LEFT, 2 CRACKS FWD OF STA 600. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED INTERCOSTAL IAW MFSDR RRXA991632Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, INTERNAL DOUBLER AND INNER SUFRACE OF OUTER SKIN BETWEEN LONGERONS 31 LEFT AND LONGERON 31 RIGHT AND BETWEEN STA 350 AND STA 370. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-SDR RRXA991631Finger Doubler · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, FINGER DOUBLER AT LONGERON 31 RIGHT, AT STA 100. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FINGER DOUBLER IAW DAC DWG 5779917 AND DCSDR RRXA991519Fitting · crackedDURING A MAINTENANCE VISIT FOUND CRACK, FLOOR BEAM SUPPORT STRUT LOWER FITTING, CRACKED AT AFT SIDE OF TEE, AT STA 1160, TOP OF LONGERON 29 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLSDR RRXA991517Fitting · crackedDURING A MAINTENANCE VISIT FOUND CRACK, LONGERON SPLICE FITTING CRACKED AT LONGERON 31 LEFT, STA 1260. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FITTING IAW DAC DWG NR 470359 AND DC8SDR RRXA991455Intercostal · crackedDURING A MAINTENANCE VISIT FOUND CRACK, INTERCOSTAL BETWEEN STA FS 580 AND FS 600 AT LONGERON 33 LEFT, FWD OF STA FS 600. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED INTERCOSTAL PER DAC DWSDR RRXA991434Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, INTERNAL DOUBLER AND INNER SURFACE OF OUTER SKIN, BETWEEN LONGERONS 31 LEFT AND LONGERON 31 RIGHT, AND BETWEEN STATIONS Y350 AND STA Y370. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED ARESDR RRXA991433Finger Doubler · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, FINGER DOUBLER, AT STA Y100, LONGERON 31 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FINGER DOUBLER IAW DAC DWG NR 5779917 AND SDR UPS99830349Doubler · corrodedINSPECTION TYPE:SV, CORROSION BETWEEN SKIN AND DOUBLER FS 1620 L26R DOT E253. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR IAW UPS DC8 SRM 53-4 -1, 53-2-1 FIG 7, 51-120D.SDR RRXA991664Rib · crackedDURING A MAINTENANCE VISIT FOUND CRACK, RIGHT WING, L/E RIB AT STA XFS 163.75, CRACKED AT THE AFT LWR END. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC8 SRM 57-2-0 FIGSDR RRXA991657Angle · crackedDURING A MAINTENANCE VISIT FOUND CRACK, RIGHT WING, L/E AT STA XW 0.00, THE UPPER AFT L/E ATTACH ANGLE CRACKED. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED ANGLE IAW MFG DWG 5613646 AND DCSDR RRXA991656Skin · crackedDURING A MAINTENANCE VISIT FOUND CRACK, RIGHT WING, L/E LWR SKIN INTERNAL TRIPLER AT STA XFS 430 AT THE SPAR, CRACKED IN TWO. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. F8 REPAIR IAW MFG DWG 5769891 AND DC8 SRM 5SDR RRXA991647Rib · crackedDURING A MAINTENANCE VISIT FOUND CRACK, RT WING, L/E RIB AT STA XFS 385.25, 17 FWD OF THE SPAR. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED CRACK AND REPAIRED IAW DC8 SRM 57-2-0 FIG 2.SDR RRXA991644Rib · crackedDURING A MAINTENANCE VISIT FOUND CRACK, RT WING, L/E RIB AT STA XFS 354, CRACKED AT THE AFT UPPER END. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED CRACK AND REPAIRED IAW DC8 SRM 57-2-0 FIG 2.SDR RRXA991643Intercostal · crackedDURING A MAINTENANCE VISIT FOUND CRACK, WING, RIGHT, L/E RIB AT STA XFS 335.25, 17 FWD OF THE SPAR, AT THE INTERCOSTAL GUSSET AFT FASTENERS IS CRACKED. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED CRACSDR RRXA991642Skin · crackedDURING A MAINTENANCE VISIT FOUND CRACK, RT WING, L/E LWR SKIN AT STA XFS 301.25, 14 FWD OF THE SPAR IS CRACKED AT A RIVET HOLE. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED CRACK AND REPAIRED IAW DC8 SSDR RRXA991641Rib · crackedDURING A MAINTENANCE VISIT FOUND CRACK, WING, RIGHT L/E RIB AT STA XFS 163.75, CRACKED AT THE AFT LOWER END. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED CRACK AND REPAIRED IAW DC8 SRM 57-2-0 FIG 2.SDR RRXA991640Skin · crackedDURING A MAINTENANCE VISIT FOUND CRACK, WING, RIGHT, L/E, LWR SKIN AT STA XS 208, 31 FWD OF THE SPAR. THE CRACK IS APPROX 2 INCHES LONG. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED CRACK AND REPAIREDSDR RRXA991470Rib · crackedDURING A MAINTENANCE VISIT FOUND CRACK, RT WING L/E EDGE RIB AT STA XFS 163.75 AT THE AFT LOWER END. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED CRACKED, FABRICATED AND INSTALLED REPAIR DOUBLER IAW DCSDR RRXA991466Rib · crackedDURING A MAINTENANCE VISIT FOUND CRACK, RIGHT WING, L/E RIB, AT STA XFS 163.75, AT THE AFT LOWER END. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED CRACK AND REPAIRED IAW DC8 SRM 57-2-0, FIG 2.SDR RRXA991458Angle · crackedDURING A MAINTENANCE VISIT FOUND CRACK, RT WING L/E AT STA XW 0.00, THE UPPER AFT L/E ATTACH ANGLE. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR ANGLE IAW DAC DWG NR 5613646 AND DC8 SDR RRXA991457Skin · crackedDURING A MAINTENANCE VISIT FOUND CRACK, RT WING, L/E LWR SKIN INTERNAL TRIPLER AT STA XFS 430 AT THE SPAR, CRACKED IN TWO. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DAC DWG NRSDR RRXA991448Rib · crackedDURING A MAINTENANCE VISIT FOUND CRACK, RT WING L/E RIB AT STA XFS 385.25, 17 FWD OF THE SPAR. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC8 SRM 57SDR RRXA991447Rib · crackedDURING A MAINTENANCE VISIT FOUND CRACK, RT WING LE RIB AT STA XFS 354 AT THE AFT UPPER END. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER PER DC8 SRM 57-2-SDR RRXA991446Intercostal · crackedDURING A MAINTENANCE VISIT FOUND CRACK, RT WING L/E RIB AT STA XFS 335.25, 17 FWD OF THE SPAR, AT THE INTERCOSTAL GUSSET AFT FASTENERS. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED CRACK, FABRICATED ANSDR RRXA991445Skin · crackedDURING A MAINTENANCE VISIT FOUND CRACKED RT WING L/E LWR SKIN AT STA XFS 301.25, 14 FWD OF THE SPAR AT A RIVET HOLE. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR SDR RRXA991444Skin · crackedDURING A MAINTENANCE VISIT FOUND CRACK, RT WING L/E LWR SKIN AT STA XS 208, 31 FWD OF THE SPAR. THE CRACK IS APPROXIMATELY 2 INCHES LONG. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED CRACK, FABRICATEDSDR RRXA991669Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, LEFT WING, LEADING EDGE, EXTERNAL SKIN BETWEEN XFS 7.5 AND XFS 20. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC8 SRM 57-2-1SDR RRXA991668Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, LEFT WING, LEADING EDGE SKIN BETWEEN XFS 250 AND XFS 250.89. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC8 SRM 57-2-0 FIG 2SDR RRXA991667Skin · crackedDURING A MAINTENANCE VISIT FOUND CRACK, FUSELAGE, EXTERIOR FUSELAGE SKIN CRACKED AND CORROSION AT STA 1755, LONGERON 31 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED SKIN AREA IAW DC8SDR RRXA991663Skin · crackedDURING A MAINTENANCE VISIT FOUND CRACK, LEFT WING, CENTER L/E UPPER SKIN CRACKED AT STA XFS 316.5 AT FRONT SPAR. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC8 SRM 57-2-1.SDR RRXA991660Skin · crackedDURING A MAINTENANCE VISIT FOUND CRACK, RIGHT WING, L/E LWR SKIN AT STA XFS 630, 3 FWD OF THE SPAR, CRACKED AT A RIVET HEAD. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED CRACK AND REPAIRED IAW DC8 SRM SDR RRXA991659Rib · crackedDURING A MAINTENANCE VISIT FOUND CRACK, LT L/E LOWER RIB CRACKED AT FASTENER END AT STA XFS 622.5 AND STA XFS 628.750 FWD OF ACCESS PANEL 519C OPENING. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED CRACSDR RRXA991658Rib · crackedDURING A MAINTENANCE VISIT FOUND CRACK, RIGHT WING L/E UPPER RIB AT STA XFS 521.168, CRACKED 6 FWD OF THE SPAR. THE CRACK IS APPROX 2.5 INCHES LONG. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED RIB ANSDR RRXA991655Rib · crackedDURING A MAINTENANCE VISIT FOUND CRACK, LT O/B L/E UPPER RIB CRACKED AT FASTNER END OF STA XFS 585. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED CRACK AND REPAIRED IAW DC8 SRM 57-2-0 FIG 2.SDR RRXA991653Rib · crackedDURING A MAINTENANCE VISIT FOUND CRACK, WING, LEFT, LOWER L/E RIB, CRACKED AT FASTENER END AT STA XFS 653.75 FWD OF ACCESS PANEL 519C OPENING. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED CRACK AND RESDR RRXA991652Rib · crackedDURING A MAINTENANCE VISIT FOUND CRACK, RIGHT WING, L/E RIB AT STA XFS 616.25, CRACKED AT THE LWR FASTENER. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED CRACK AND REPAIRED IAW DC8 SRM 57-2-0 FIB 2.SDR RRXA991651Skin · crackedDURING A MAINTENANCE VISIT FOUND CRACK, RIGHT WING, L/E LWR SKIN INTERNAL DOUBLER AT STA XFS 597.5, CRACKED AT THE DRAIN HOLE, CRACK RUNS AFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DSDR RRXA991650Rib · crackedDURING A MAINTENANCE VISIT FOUND CRACK, RIGHT WING, L/E RIB AT STA XFS 735.00, CRACKED AT THE AFT LOWER END. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED CRACK AND REPAIRED IAW DC8 SRM 57-2-0 FIG 2.
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