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 UPS07849367Skin · corrodedINSPECTION TYPE:C3 LEFT WING UPPER SKIN AT XW 408 TP CANT 508 BETWEEN STR 6 AND REAR SPAR REQUIRES REPAIR. REPAIR WING UPPER SKIN IAW SAA EA 008-5730-01-A0660 AND UPS EO DC8-5 730-26300-A.SDR UPS07849366Skin · corrodedINSPECTION TYPE:C3 LEFT WING UPPER SKIN AT XRS650 TO XRS659 OVER STR 7 REQUIRES REPAIR. REPAIR WING UPPER SKIN IAW SAA EA3 008-5730-01-A0655 AND UPS EO DC8-57 30-26300-A.SDR UPS07849365Skin · corrodedINSPECTION TYPE:C3 LEFT WING UPPER SKIN AT CANT 495 TO XW408 OVER CENTER SPAR REQUIRES REPAIR. REPAIRED WING UPPER SKIN IAW SAA EA 008-5730-01-A0659 AND UPS EO DC8-5730-26300-A.SDR UPS07849364Skin · corrodedINSPECTION TYPE:C3 LEFT UPPER WING SKIN AT CANT 495 TO XRS 554 BETWEEN STR 5 AND 8 REQUIRES REPAIR. REPAIRED UPPER WING SKIN IAW SAA EA 008-5730-01-A0658 AND UPS EO DC8-5730-26300-A.SDR UPS07849363Skin · corrodedINSPECTION TYPE:C3 LEFT UPPER WING SKIN AT XRS 589 BETWEEN STR 1 TO REAR SPAR REQUIRES REPAIR. REPAIRED WING UPPER SKIN IAW SAA EA 008-5730-01-A0656 AND UPS EO DC8-5730-26300-A.SDR UPS07849233Bracket · crackedINSPECTION TYPE:C3 LEFT WING FLAP WELL FUEL DUMP CHUTE HORSE SHOE BRACKET CRACKED. REMOVED CRACKED HORSE SHOE BRACKET FROM LEFT WING DUMP CHUTE IAW SRM 51-1-20D. FABRICATED AND INSTALLED HORSE SHOE BRACKET AT LEFT WING FUEL DUMP CHUTE IAW DWG 5649654, AND SRSDR UPS07849210Doubler · crackedINSPECTION TYPE:C3 LEFT WING CENTER L/E UPPER INNER DOUBLER CRACKED AT STA XOLDI 6.2246. REMOVED CRACKED DOUBLER AT LEFT WING CENTER L/E STA XOLDI 6.2246 IAW SRM 51-1-21. FABRICATED AND INSTALLED REPLACEMENT DOUBLER AT LEFT WING CENTER UPPER L/E STA XOLDI 6.SDR UPS07849209Rib · crackedINSPECTION TYPE:C3 LT WING CENTER LEADING EDGE UPPER RIB CRACKED AT XFS 366. STOP DRILLED CRACK AT LEFT WING L/E AT STA XFS 366 IAW SRM 57-02-00 FIG 2. FABRICATED AND INSTALLED REPAIR DOUBLER ON LEFT CENTER L/E AT STA XFS 366 IAW SRM 57-02-00 AND SRM 51-01-2SDR IXXA070006SSkin · misrepairedLOWER D PIT DOOR HAS NON-STANDARD REPAIR PER AD2005-18-07 AND SB DC8-53-078. REMOVED EXISTING SKIN PANEL. LOCATED, DRILLED, TRIMMED, TREATED AND PRIMED NEW SKIN PANEL, APPLIED SEALANT TO FAYING SURFACES. INSTALLED NEW SKIN PANEL AT LOWER D PIT DOOR FROM STATSDR UPS07849344Skin · crackedINSPECTION TYPE:C3 LEFT WING UPPER SKIN 1 INCH CRACK AT XRS 107.000 UPPER FRONT SPAR SKIN. REPAIRED UPPER WING SKIN AT XRS 107.000 FRONT SPAR IAW SAA EA 008-5710-01-A0685 AND UPS RAA DC8-57-20211.SDR UPS07849224Longeron · corrodedINSPECTION TYPE:C3 CORROSION UNDER SPLICE FITTING AND LONGERON 33L IN AFT ACCESSORY COMPT AT STA 1550. REMOVED SPLICE FITTING AND CUT OUT CORRODED SECTION OF L33L FROM STA 1530-1550 IAW SRM 51-1-21. LOCATED, DRILLED UP, AND INSTALLED NEW SPLICE FITTING AND LSDR UPS07849211Bulkhead · crackedINSPECTION TYPE:C3 AFT PRESSURE BULKHEAD CRACKED AT STA 1766 LBL 24 L10L AREA. CUT OUT DAMAGED AREA AT AFT PRESSURE BULKHEAD STA 1766 LBL 24 L10L IAW SRM 53-2-5 FIG 14A. FABRICATED AND INSTALLED FINGER DOUBLER, FILLER AND REPAIR DOUBLER AT AFT PRESSURE BULKSDR UPS07849242Longeron · corrodedINSPECTION TYPE:C3 HEAVILY CORRODED LONGERON IN AFT ACC COMPT STA 1570 L34L. REMOVED CORRODED LONGERON SECTION L34L STA 1560-1570 IAW SRM 51-01- 20D, AND SRM 51-01-21-0. FABRICATED AND INSTALLED LONGERON SPLICE SECTION AND NEW END FITTING AT STA 1560-1570 L3SDR UPS07849223Skin · dentedINSPECTION TYPE:C3 RUDDER RT SIDE LEADING EDGE STA ZR 140 SKIN HAS DENT. FOUND DENT OUT OF LIMITS AT RUDDER STA ZR 140 IAW SRM 55-02-00-0 FIG 001. REMOVED AND REPLACED SKIN AT RUDDER BAY NR 2 STA ZR 140 IAW SRM 51-3-0, 51-1-21, AND SRM 55-06-01-0. NO WEIGHTSDR UPS07849241Skin · dentedINSPECTION TYPE:C3 LEFT FUSELAGE STA 1580 BETWEEN L24L & L25L EXT SKIN HAS DENT WITH GOUGE 6 INCHES LONG 1.5 INCH WIDE AND APPROX. .100 INCH DEEP. CUT OUT DAMAGED AREA AT STA 1580 BETWEEN L24L & L25L EXTERIOR SKIN IAW SRM 53-2-1 FIG 7. FABRICATED AND INSTALLSDR IXXA070007OSwitch · contaminatedDURING TAKEOFF FROM KTOL, THE DOORS NOT LATCHED LIGHT REMAINED ON AFTER GEAR WAS RETRACTED. THE CREW ACCOMPLISHED THE UNSATISFACTORY UP-LATCH PROCEDURE AND THE DOORS NOT LATCHED LIGHT REMAINED ON. THE CREW CONTINUED THE FLIGHT TO KLAX AND LANDED WITHOUT INCISDR UPS07849135Battery · no testINSPECTION TYPE:N/A ON PREFLIGHT A/C FAILED EMERGENCY EXIT LIGHT PREFLIGHT TEST. REPLACED EMERGENCY LIGHTING BATTERY AND RELAY UNIT IAW DC-8 AMM 33-50-01-2. OPS TEST GOOD.SDR UPS07849115Battery Pack · inoperativeINSPECTION TYPE:N/A EMERGENCY LIGHT WILL NOT TURN ON PREFLIGHT CHECK. EMERGENCY LIGHT BATTERY PACK REPLACED IAW AMM 33-50-01-2 AND SYSTEM CHECK SERVICEABLE.SDR IXXA07SMN087SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING OUTBOARD FLAP UPPER SKIN PANEL HAS A NON STANDARD REPAIR FROM STATION XF169.000 TO STATION XF172.000. REMOVED EXISTING SKIN PANEL WITH NON STANDARD REPAIR. FABRICATED NEW SKIN PANEL AND REPAIR PARTS. BONDESDR IXXA07SMN086SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING LEADING EDGE HAS A NON STANDARD REPAIR FROM STATION XFS422.000 TO STATION XOLDI6.220. REMOVED EXISTING NON STANDARD REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACKS OR CORROSION FOUND, AFTSDR IXXA07SMN085SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING LEADING EDGE HAS A NON STANDARD REPAIR FROM STATION XFS416.000 TO STATION XOLDI6.220. REMOVED EXISTING NON STANDARD REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACKS OR CORROSION FOUND AFTESDR IXXA07SMN084SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING LEADING EDGE HAS A NON STANDARD REPAIR FROM STATION XFS304.000 TO STATION XFS310.000. REMOVED EXISTING NON STANDARD REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACKS OR CORROSION FOUND, AFTSDR IXXA07SMN081SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING LOWER CENTRAL LEADING EDGE HAS A NON STANDARD REPAIR FROM STATION XFS304.000 TO XFS316.000. REMOVED EXISTING NON STANDARD REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK OR CORROSION FOUNDSDR IXXA07SMN080SLongeron · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND LONGERON 25 RIGHT CORRODED AT STATION 1620.000. REMOVED FASTENERS. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED CORRODED LONGERON SECTION AND FABRICATED NEW LONGERON SECTION. PERFORMED HEAT TREATMENT. PERFORMEDSDR IXXA07SMN079SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND A CRACKED FITTING AT STATION FS 702.000, LONGERON 19 RIGHT. REMOVED CRACKED FITTING. CLEANED, TREATED AND PRIMED AREA. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D DC8 SRM 51-3-1 AND DC8 SRM 51-1-8B.SDR IXXA07SMN078SFastener · wrong partDURING ROUTINE C CHECK INSPECTION, FOUND LEFT ELEVATOR LOWER SKIN PANEL HAS IMPROPER FASTENERS FROM STATION XE306.062 TO STATION XE273.875. REMOVED EXISTING SKIN PANEL WITH IMPROPER FASTENERS. FABRICATED NEW SKIN PANEL AND FINGER DOUBLER. BONDED PARTS AS NESDR IXXA07SMN077SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT ELEVATOR LOWER SKIN PANEL HAS A NON STANDARD REPAIR FROM STATION XE79.531 TO STATION XE89.718. REMOVED EXISTING SKIN PANEL WITH NON STANDARD REPAIR. FABRICATED NEW SKIN PANEL AND FINGER DOUBLER. BONDED PARTS ASSDR IXXA07SMN075SSkin Panel · delaminatedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT ELEVATOR UPPER SKIN PANEL IS DELAMINATED AT STATION XE50.000. REMOVED DAMAGED SKIN PANEL. FABRICATED NEW SKIN PANEL AND REPAIR PARTS. BONDED REPAIR PARTS AS NEEDED WITH HYSOL. CLEANED, TREATED AND PRIMED AREA SDR IXXA07SMN074SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT ELEVATOR LOWER PANEL HAS A NON STANDARD REPAIR FROM STATION XE55.062 TO STATION XE65.156. REMOVED SKIN PANEL WITH EXISTING NON STANDARD REPAIR. FABRICATED NEW SKIN PANEL AND REPAIR PARTS. BONDED PARTS AS NEEDEDSDR IXXA07SMN072SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND A CRACKED FITTING AT STATION FS680.000, LONGERON 2 LEFT. REMOVED CRACKED FITTING CLEANED, TREATED AND PRIMED AREA. INSTALLED NEW FITTING IAW DC8 SRM 51-1-21 SRM 51-1-20D, DC8 SRM 51-3-1 PAGE 2A AND DC8 SRM 51-1-8B.SDR IXXA07SMN069SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND A CRACKED FITTING AT STATION FS 1690.000, LONGERON 24 LEFT. REMOVED CRACKED FITTING. CLEANED, TREATED AND PRIMED AREA. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D, DC8 SRM 51-3-1 AND DC8 SRM 51-1-8B.SDR IXXA07SMN067SDoubler · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND EXISTING INTERNAL DOUBLER CORRODED FROM STATION FS 1640.000 TO STATION FS 1660.000 AND FROM LONGERON 29 RIGHT TO LONGERON 33 RIGHT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CORROSION. FOUND OUT OF LIMITSDR IXXA07SMN065SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT OUTBOARD FLAP HAS A NON STANDARD REPAIR AT STATION XF240.000. REMOVED EXISTING REPAIR. REMOVED DAMAGED SKIN. PERFORMED NDT INSPECTION. NO CRACKS OR CORROSION FOUND AFTER DAMAGE REMOVED. FABRICATED NEW SKIN ANSDR IXXA07SMN062SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND A CRACKED FITTING AT STATION FS 980.000 LONGERON 22 RIGHT. REMOVED CRACKED FITTING. CLEANED, TREATED AND PRIMED AREA. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D, DC8 SRM 51-3-1 AND DC8 SRM 51-1-8B.SDR IXXA07SMN061SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND A CRACKED FITTING AT STATION FS702.000 LONGERON 14 RIGHT. REMOVED CRACKED FITTING. FABRICATED FITTING. PERFORMED NDT INSPECTION. CLEANED, TREATED AND PRIMED AREA AND FITTING. INSTALLED FITTING IAW DC8 SRM 51-1-20D,SDR IXXA07SMN060SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND A CRACKED FITTING AT STATION FS824.000 LONGERON 19 LEFT. REPLACED CRACKED FITTING IAW DC8 SRM 51-1-20D AND DC8 SRM 51-3-1.SDR IXXA07SMN059SFitting · crackedDURING ROUTINE C CHECK INSPECTION FOUND A CRACKED FITTING AT STATION FS 824.000 LONGERON 14 RIGHT. REMOVED CRACKED FITTING. FABRICATED FITTING. PERFORMED NDT INSPECTION, NO CRACKS OR CORROSION FOUND. CLEANED, TREATED AND PRIMED AREA AND FITTING. INSTALLEDSDR IXXA07SMN057SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND A CRACKED FITTING AT STATION FS 240.000, LONGERON 33 RIGHT. REPLACED CRACKED FITTING IAW DC8 SRM 51-1-20D AND DC8 SRM 51-3-1.SDR IXXA07SMN056SFitting · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND A CORRODED FITTING AT STATION FS450.000, LONGERON 26 LEFT. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED CORRODED FITTING. CLEANED, TREATED AND PRIMED AREA. INSTALLED NEW FITTING IAW DC8 SRM 51-1-8 PAGE 17-18, DC8SDR IXXA07SMN055SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND A NON STANDARD REPAIR AT STATION FS12.000 LONGERON 27 RIGHT. REMOVED EXISTING NON STANDARD REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK OR CORROSION FOUND. AFTER DAMAGE REMOVED. FABRICATED REPAISDR IXXA07SMN054SSkin · crackedDURING ROUTINE C CHECK INSPECTION, FOUND EXTERNAL FUSELAGE SKIN CRACKED AT STATION FS1400.00 LONGERON 33 RIGHT. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACKS OR CORROSION FOUND, AFTER DAMAGE REMOVED. FABRICATED REPAIR PARTS. CLEANED, TREATED ASDR IXXA07SMN053SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING UPPER LEADING EDGE CORRODED, BETWEEN STATIONS XFS341.500 AND XFS304.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. FABRICATED REPAIR PARSDR IXXA07SMN052SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION FOUND A IMPROPER REPAIR AT STATION FS1762, LONGERON 34 LEFT. REMOVED DAMAGED SKIN PANEL CLEANED TREATED AND PRIMED AREA AND NEW SKIN PANEL. APPLIED SEALANT TO FAYING SURFACES. INSTALLED NEW SKIN PANEL FROM STATION 1696 TO SSDR IXXA07SMN050SSkin · damagedDURING ROUTINE C CHECK INSPECTION, FOUND LOWER FUSELAGE SKIN HAS SCRATCHES AND SMALL DENT AT STATION FS1870 LONGERON 36. REMOVED DAMAGED SKIN PANEL. CLEANED TREATED AND PRIMED AREA AND NEW SKIN PANEL. APPLIED SEALANT TO FAYING SURFACES INSTALLED NEW SKIN PASDR IXXA07SMN051SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND AN IMPROPER REPAIR AT STATION FS367, LONGERON 20 LEFT. REMOVED EXISTING REPAIR DOUBLER. REMOVED DAMAGED AREA. FABRICATED REPAIR PARTS. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. APPLIED SEALANT TO FAYING SUSDR IXXA07SMN076SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT ELEVATOR.-LOWER SKIN HAS A NON STANDARD REPAIR FROM STATION XE55.062 TO STATION XE65.156. REMOVED SKIN WITH EXISTING NON STANDARD REPAIR. FABRICATED NEW SKIN AND REPAIR PARTS. BONDED REPAIR PARTS WITH HYSOL AS NSDR IXXA07SMN083SVane · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING LEADING EDGE SLOT VANE HAS A NON STANDARD REPAIR FROM STATION XFS521.000 TO STATION XFS527.000. REMOVED EXISTING NON STANDARD REPAIRS. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACKS OR CORROSIONSDR IXXA07SMN064SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION FOUND RIGHT HAND UPPER OUTBOARD FLAP HAS A NON STANDARD REPAIR AT STATION XF210.000. REMOVED SKIN WITH EXISTING NON STANDARD REPAIR. FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AREA AND NEW SKIN AS NEEDED. APPLIED SEALANTSDR IXXA07SMN082SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING UPPER FORWARD SKIN CORRODED AT STATION XFS410.250. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CORROSION. FOUND DAMAGE OUT OF LIMITS. REMOVED DAMAGED AREA. FABRICATED REPAIR DOUBLER AND FILLERSDR IXXA07SMN073SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING FLAP UPPER SKIN HAS A NON STANDARD REPAIR BETWEEN STATIONS XF415.000 AND XF420.000. REMOVED SKIN WITH EXISTING NON STANDARD REPAIR. FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AREA AND NEW SKIN INTERNA
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