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 RRXA97062Frame · misdrilledDURING A MAINTENANCE VISIT, FOUND MISDRILLED HOLE IN FRAME AT Y=1480 AND X=0. REMOVED FASTENERS, CLEANED AND TREATED AREA IAW DAC DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER REPAIR IAW DER APPROVED COTNEY ENGINEERING SKETCH C07-R16 AND DAC DC-8 SRM 51-SDR RRXA97061ASkin · looseDURING A MAINTENANCE VISIT, FOUND FIBERGLASS REPAIR PEELING LOOSE ON LEFT WING SKIN AT XRS=155, UPPER SURFACE. AWAITING ON ZANTOP AND COTNEY ENGINEERING TO DETERMINE REPAIR PROCEDURE.SDR RRXA97060ASkin · corrodedDURING A MAINTENANCE VISIT, FOUND INNER SKIN CORROSION AT Y=53 AND LONGERON 34R. AWAITING ON ZANTOP AND COTNEY ENGINEERING TO DETERMINE REPAIR PROCEDURE.SDR RRXA97059ASkin · corrodedDURING A MAINTENANCE VISIT, FOUND SKIN CORROSION ON TOP OF CENTER WING TANK AT Y=780 AND X=+8. AWITING ON ZANTOP AND COTNEY ENGINEERING TO DETERMINE REPAIR PROCEDURE.SDR RRXA97058ASkin · corrodedDURING A MAINTENANCE VISIT, FOUND SKIN CORROSION AT Y=53 AND LONGERON 34L. AWAITING ON ZANTOP AND COTNEY ENGINEERING TO DETERMINE REPAIR PROCEDURE.SDR RRXA97057AAttach Angle · wornDURING A MAINTENANCE VISIT, FOUND RIGHT SIDE WING FLAP EXHAUST GATE HAD EXCESSIVE PLAY. AFTER REMOVAL, FOUND FWD UPPER ATTACHMENT BOLT HOLE FOR INBD ATTACHMENT POINT WORN BEYOND LIMITS AND INBD WEB AND UPPER ATTACHMENT ANGLE WORN. AWAITING ON ZANTOP AND COTNSDR RRXA97056Skin · crackedDURING A MAINTENANCE VISIT, FOUND SKIN CRACKED ON RIGHT WING FLAP AT XCW=64. REMOVED DAMAGE, FABRICATED AND INSTALLED FILLER AND DOUBLER REPAIR, IAW DER APPROVED COTNEY ENGINEERING SKETCH CO7-R10 AND DACO DC-8 SRM 51-1-16.SDR RRXA97055ASkin · crackedDURING A MAINTENANCE VISIT, FOUND OUTER SKIN CRACKED, VERIFIED BY DYE PENE. INSPECTION AT Y=130, RIGHT SIDE AND MAIN CARGO DOOR UPPER FWD CORNER. AWAITING ON ZANTOP AND COTNEY ENGINEERING TO DETERMINE REPAIR PROCEDURE.SDR RRXA97054ASupport · misdrilledDURING MAINTENANCE VISIT, FOUND MISDRILLED HOLE IN FLOOR SUPPORT, AT Y=560 AND X=-46. AWAITING ON ZANTOP AND COTNEY ENGINEERING TO DETERMINE REPAIR PROCEDURE.SDR RRXA97053Hyd Line · failedLOST HYDRAULIC PRESSURE AND QUANTITY UPON LANDING. REMOVED AND REPLACED FLEX LINE HOSE AT LEFT BOGIE TRIM CYLINDER, OPS AND LEAK CHECK GOOD.SDR UPS97822073Floorbeam · corrodedINSPECTION TYPE-C, FLOORBEAM UPPER CAP CORRODED FS 640 RBL 34. CUT OUT DAMAGED AREA, FABRICATED REPAIR ANGLE AND INSTALLED PER DHC SRM 51-1-20, AND DHC SK-806-215A REF ENRG FILE NR DC8-53-1739.SDR UPS97822071Fitting · crackedINSPECTION TYPE-C, C-1 CARGO COMPARTMENT FITTING CRACKED AT FS 280 BETWEEN LONG 27R AND 26R. REMOVED CRACKED FITTING, FABRICATED REPLACEMENT FITTING IAW DWG 3754025, INSTALLED REPLACEMENT FITTING IAW DWG 3754025 AND SRM 51-1-20.SDR DHL9780447CTrim Cylinder · leakingAT C-CHECK, LEFT HAND MLG BOOGIE TRIM CYLINDER LEAKING THROUGH SHAFT. REMOVED AND REPLACED CYLINDER PER MM 32-33-1.SDR UPS97822059Skin · corrodedINSPECTION TYPE-C, SKIN CORRODED BELOW C2 DOOR, STA 520 TO 540, LONGERON 33R. CUT OUT DAMAGE AREA, INSTALLED REPAIR DOUBLER AT STA 520 TO 540, LONGERON 31R TO 35R, IAW SRM 51-1-20, 51-1-21 AND DHC SK-806-705 REF UPS E0 DC8-5330-9022-A.SDR UPS97822056Rib · crackedINSPECTION TYPE-C, LT WING L/E RIB HAS CRACK IN UPPER AFT END AT XW257. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 57-2-0, 57-3-3 AND 51-1-21.SDR RRXA97034Skin · corrosionDURING A MAINTENANCE VISIT, FOUND CORROSION TO INNER SKIN AT Y=1610 TO 1680 BETWEEN LONGERONS 31R AND 31L. DAMAGE PAST LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGED SECTION AND FABRICATED DOUBLERS, FILLERS AND INSTALLED IAW FAA DER APPROVED ENGINEERING SKETCH B0SDR RRXA97033Jamb · dentedDURING A MAINTENANCE VISIT, FOUND DENT TO SERVICE DOOR JAMB LOWER CORNER, PAST LIMITATION IAW DC-8 SRM. FABRICATED REPAIR DOUBLER AND INSTALLED IAW FAA DER APPROVED ENGINEERING SKETCHES B90-R22 AND B90-R23.SDR DHL9780444CFail Monitor · inoperativeAT C-CHECK, NAV MONITOR FAIL SYSTEM SHOWS GREEN ARROW POINTING TO CAPTAINS SIDE ALL TIME. REPLACED FAIL MONITOR PER MM 34-0-4.SDR DHL9780440CFuel Quanity Ind · inoperativeAT C-CHECK, NR 3 MAIN FUEL QUANTITY INDICATOR WILL NOT ADJUST. REMOVED AND REPLACED INDICATOR.SDR UPS97822061Floorbeam · crackedINSPECTION TYPE-C, FLOORBEAM CRACKED AT FASTENER HOLE FS 1580 LBL 36. CUT OUT DAMAGED AREA AND REPAIRED IAW DHC SK-806-586 REV C REF ENRG FILE NR DC8-53-1741.SDR UPS97822058Skin · corrodedINSPECTION TYPE-C, RT FUSELAGE SKIN HAS CORROSION BETWEEN LONGERON 22R AND 23R AT FS 1224. REPAIRED IAW DHC SK-806-392 REV IR REF UPS ENRG FILE NR DC8-53-1738.SDR DHL9780446CFuel Quanity Ind · inoperativeAT C-CHECK, FUEL QUANTITY CENTER AUX WILL NOT CALIBRATE. REMOVED AND REPLACED FUEL PROBES AND INDICATOR PER M/M 28-41-0.SDR DHL9780417CCowling · damagedAT C-CHECK, NR 1 ENGINE OUTBD COWLING HAS 2, 10 INCH TEMPORARY REPAIRS. REMOVED AND REPAIRED COWLING, REINSTALLED COWLING PER M/M 71-20-1.SDR DHL9780415CSeat Track · wornAT C-CHECK, NR 4 FLOOR TRACK FROM BS 300 TO 420 WORN. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED SEAT TRACK PER SRM 53-2-3.SDR RRXA97036Skin · damagedDURING A MAINTENANCE VISIT, FOUND SKIN DAMAGE TO LEFT SIDE HORIZONAL STABILZER AT, XFS=185 AND XE=149. FABRICATED REPAIR AND INSTALLED IAW FAA DER APPROVED ENGINEERING SKETCH B90-R17.SDR RRXA97035Skin · damagedDURING A MAINTENANCE VISIT, FOUND HOLE IN SKIN AT Y=660 TO 702 LEFT SIDE OF OMEGA ANTENNA. DAMAGE PAST LIMITATIONS IAW DC-8 SRM. FABRICATED AND INSTALLED DOUBLER REPAIR IAW FAA DER APPROVED ENGINEERING SKETCH B90-R18.SDR RRXA97031Longeron · corrosionDURING A MAINTENANCE VISIT, FOUND CORROSION TO LEFT LONGERON 29 AND FITTING AT Y=298, DAMAGES PAST LIMITIONS IAW DC-8 SRM. REMOVED AND REPLACED FITTING WITH NEW AND FABRICATED REPAIR ANGLE AND INSTALLED IAW FAA DER APPROVED ENGINEERING SKETCHES B90-R19 AND B1SDR DHL9780445CBolt · brokenAT C-CHECK, 31 PYLON O/B ATTACHMENT RAIL BOLT BROKEN. REMOVED AND REPLACED PER M/M 20-19-0.SDR DHL9780406CSeat Track · wornAT C-CHECK, CARGO FLOOR TRACK, NR 3 FROM STA 150 TO 300 WORN OUT. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED SPLICES PER SRM 53-2-3.SDR DHL9880636CBracket · crackedAT C-CHECK, AFT BAGGAGE COMPARTMENT AFT CARGO DOOR STA 1420 CEILING AREA JUST BEHIND DOOR HINGE AREA BRACKET IS CRACKED. REMOVED AND REPLACED DAMAGED BRACKET PER SRM 51-1-21.SDR DHL9780443CSupport Link · crackedAT C-CHECK, LEFT MLG FLYING DOOR AFT DOOR SUPPORT LINK, FOUND CRACKED. REMOVED AND REPLACED LINK PER M/M 32-12-1.SDR DHL9780442CFillet Bracket · crackedAT C-CHECK, UPPER LEFT WING TO FUSELAGE FILLET PANEL BRACKET HAS CRACKED 24 INCHES FROM L/E. STOP DRILLED CRACK AND REPLACED BRACKET PER SRM 53-2-0.SDR DHL9780441CFitting · crackedAT C-CHECK, C-1 CARGO DOOR SHOWS A 2.5 INCH CRACKED FITTING ON TOP REAR AREA. REMOVED AND REPLACED FITTING PER SRM 51-3-2.SDR DHL9780437CSupport · damagedAT C-CHECK, FWD CARGO COMPT, FWD FUS FWD FRAME SIDEWALL SUPPORT DAMAGED. REPAIRED SIDEWALL SUPPORT PER SRM 53-2-8.SDR DHL9780401CSkin · crackedAT C-CHECK, FUSELAGE SKIN CUT OUT AT NOSE WHEEL WELL IS CRACKED. FABRICATED REPAIR DOUBLER AND INSTALLED PER DRAWING DHL D85330-7251 AND SRM 51-1-21.SDR DHL9780439CAngle · crackedAT C-CHECK, AT STA 620, ANGLE CRACKED BELOW FLOOR PANEL CENTER SECTION. REMOVED CRACKED ANGLE, FABRICATED NEW ANGLE AND INSTALLED PER SRM 51-1-21, 20 IN LENGTH.SDR RRXA97044Web · crackedDURING A MAINTENANCE VISIT, FOUND CRACK IN LEFT FLAP WEB PAST LIMITATIONS IAW DC-8 SRM. FABRICATED DOUBLER REPAIR AND INSTALLED IAW DER APPROVED ENGINEERING SKETCH B90-R13.SDR RRXA97043Web · crackedDURING A MAINTENANCE VISIT, FOUND 2 CRACKS IN RT FLAP WEB PAST LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, FABRICATED DOUBLER REPAIR IAW FAA DER APPROVED ENGINEERING SKETCH B90-R13.SDR RRXA97041Skin · dentedDURING A MAINTENANCE VISIT, FOUND EXTERIOR SKIN DENTED PAST LIMITATIONS IAW DC-8 SRM AT, Y=1385 AND BETWEEN RIGHT LONGERONS 28R AND 29R. REMOVED DAMAGE AREA, FABRICATED DOUBLER REPAIR AND INSTALLED IAW FAA DER APPROVED ENGINEERING SKETCH B90-R3.SDR RRXA97040Skin · crackedDURING A MAINTENANCE VISIT, FOUND RIGHT SIDE AILERON EXTERIOR SKIN WITH CRACKS IN 2 PLACES, AT XW=698. FABRICATED DOUBLER, FILLER AND INSTALLED IAW FAA DER APPROVED ENGINEERING SKETCH B90-R04 AND DC-8 SRM 51-1-21.SDR RRXA97038Skin · corrosionDURING A MAINTENANCE VISIT, FOUND CORROSION TO EXTERIOR SKIN AT, Y=85 TO 95 AND RIGHT LONGERON 27. FABRICATED DOUBLER, FILLER AND INSTALLED IAW FAA DER APPROVED ENGINEERING SKETCH B90-R15.SDR RRXA97037Skin · gougedDURING A MAINTENANCE VISIT, FOUND SKIN GOUGED ON LEFT FLAP, UPPER INBOARD SIDE. DYE PENETRANT AND INSPECTED, NO CRACKS NOTED. TRIMMED LEADING EDGE IAW FAA DER ENGINEERING SKETCH B90-R16.SDR RRXA97032Longeron · corrosionDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO RIGHT LONGERON 31 PAST LIMITATIONS IAW DC-8 SRM AT, Y=1540 TO 1558 AND Z-41 TO X-25. REMOVED DAMAGED SECTION AND FABRICATED NEW SECTION AND INSTALLED TO LONGERON 31R IAW FAA DER APPROVED ENGINEERING SKETCHSDR RRXA97030Floorbeam · corrosionDURING A MAINTENANCE VISIT, FOUND CORROSION ON FLOORBEAM AT, Y=100 AND X-45. REMOVED CORROSION IAW DC-8 SRM 53-2-0 FIGURE 1F AND 51-1-8. FABRICATED REPAIR ANGLE AND INSTALLED IAW FAA DER APPROVED ENGINEERING SKETCH B90-R14.SDR RRXA97042Skin · crackedDURING A MAINTENANCE VISIT, FOUND CRACK IN EXTERIOR SKIN AT Y=40. FABRICATED DOUBLER REPAIR AND INSTALLED IAW FAA DER APPROVED ENGINEERING SKETCH B90-R01.SDR RRXA97039Skin · corrosionDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO EXTERIOR SKIN AT, Y=344 AND RIGHT LONGERON 28. FABRICATED DOUBLER AND FILLER AND INSTALLED IAW FAA DER APPROVED ENGINEERING SKETCH B90-R08.SDR RRXA97029Frame · misdrilledDURING A MAINTENANCE VISIT, FOUND MISDRILLED HOLE IN FRAME AT, Y=702 AND LEFT LONGERON 21. FABRICATED DOUBLER REPAIR AND INSTALLED IAW FAA DER APPROVED ENGINEERING SKETCH B90-R03.SDR RRXA97028Frame · gougedDURING A MAINTENANCE VISIT, FOUND DEEP DRILL START IN FRAME AT, Y=879 AND RIGHT LONGERON 21. FABRICATED DOUBLER AND INSTALLED IAW FAA DER APPROVED ENGINEERING SKETCH B90-R06.SDR RRXA97027Frame · misdrilledDURING A MAINTENANCE VISIT, FOUND MISDRILLED HOLE IN FRAME AT, Y= 759 AND LEFT LONGERON 21. FABRICATED DOUBLER REPAIR AND INSTALLED IAW FAA DER APPROVED ENGINEERING SKETCH B90-R07.SDR RRXA97019Air Distr · odorSTRONG SMELL OF ELECTRICAL SMOKE ON DESCENT, CREW WAS UABLE TO LOCATE SOURCE. ALL COCKPIT LIGHTING BALLAST OPS CHECK GOOD, RAN ALL ENGINES/GENERATORS. ALL OPS CHECK GOOD, COULD NOT DUPLICATE ELECTRICAL SMELL.
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