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 RRXA10902Support Bracket · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE MCD SUPPORT BRACKET FWD NR 7 LATCH SPOOL, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 51-3-0.SDR DHL2001806611Spoiler · delaminatedC-CHECK - RT WING REMOVAL AND INSTALLATION OF NR 1 GROUND SPOILER DUE TO UPPER SKIN DELAMINATED BETWEEN XW 5.000 AND XW 47.000. REMOVED NR 1 GROUND SPOILER (DELAMINATED) IAW MM 27-61-1 PAGE 201 TO 204. INSTALLED NR 1 GROUND SPOILER AFTER ITS REPAIR MADE IN USDR DHL2001806602Fitting · crackedC-CHECK - FWD CARGO COMPART FITTING CRACKED 1/2 INCH, STA 300 L-27 LT. REMOVED CRACKED FITTING (STA 300 L-27L) IAW SRM 51-1-20D PAGE 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D PAGE 9. STATUS-CLOSED.SDR DHL2001806591Rib · crackedC-CHECK - LT WING AILERON INTERIOR LATERAL RIB ACCESS DOOR FRAME CRACKED 4 INCHES, STA XA 425. REMOVED LATERAL RIB ACCESS DOOR FRAME IAW SRM 51-1-21 PAGE 1. CLEANED, TREATED AND PRIMED AILERON INTERIOR LATERAL RIB ACCESS DOOR FRAME AT STA XA 425 IAW SRM 51-1SDR RRXA010030Indicator · faultyIN FLIGHT, SAI SHOWS A 20 DEG RIGHT BANK AND 5 DEG TO 6 DEG NOSE UP IN LEVEL FLIGHT. SAI WILL THEN RETURN TO A 3 DEG RIGHT BANK AND 5 DEG''''S TO 6 DEG''''S NOSE UP. REMOVED AND REPLACED STANDBY ATTITUDE INDICATOR. OPS CHECKS NORMAL IAW MM CH 34-00-00.SDR RRXA11032Skin · damagedDURING A MAINTENANCE VISIT FOUND SCREWS PULLING THROUGH SKIN AT STA XFS 710 ON LT WING OB LE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 57-2-1 FIG2H.SDR DHL2001806529Floor Support · crackedC-CHECK - MAIN CARGO COMPARTMENT. FLOOR SUPPORT U ANGLE CRACKED 1 INCH BL 0 STA 1734-1760. REMOVED CRACKED U ANGLE IAW SRM 51-1-20 PAGE 21. FABRICATED ANGLE IAW SRM 53-2-0 FIG 1B. CLEANED, TREATED, AND PRIMED IAW SRM 51-1-8B. INSTALLED ANGLE IAW SRM 53-2-SDR UPS01835457Coalescer Bag · contaminatedAFTER TAKEOFF AND LEFT PACK TURNED ON, CAUSTIC FUMES FILLED COCKPIT. DECLARED EMERGENCY. RAN FUMES EVAC CHECKLIST WHILE RETURNING TO LAND . AIR TURN BACK. R & R LEFT WATER SEPARATOR SOCK, INSPECTED R-SOCK FOUND NO DEFECTS. LEFT SOCK FUEL FUME SOAKED.SDR UPS01835458Line · blownATB FOR HYD LOST IN FLT, FOUND NR 2 EDP FLEX LINE BLOWN. REMOVED AND REPLACED NR 2 ENGINE HYDRAULIC PRESSURE LINE. RAN ENGINES, LEAK CHECKED. OPS CHECK GOOD.SDR DHL2001806601Skin · misrepairedC-CHECK - RT WING O/B FLAP T/E AT STA XW 454.000 SHOWS REPAIR IMPROPER. REMOVED T/E WITH REPAIR IMPROPER IAW SRM 51-1-21 PAGE 1. FABRICATED NEW T/E IAW SRM 52-2-0 FIG 2D. TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED NEW T/E IAW SRM 51-1-21 PAGE 1. STATUSSDR DHL2001806588Angle · crackedC-CHECK - LT OUTBD FLAP SLIDING COVER HOUSING ANGLE CRACKED AT STA XRS 247.REMOVED ANGLE CRACKED IAW SRM 51-1-21 PAGE 1. FABRICATED NEW ANGLE WITH EXTRUSION 7075 T6 IAW SRM 57-2-0 FIG 2. TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED NEW ANGLE IAW SRM 51-1-2SDR RRXA10896Fitting · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE BATHTUB FITTING AT STA 1160 L29L TO L30L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 51-1-20D, 53-1-SDR RRXA10895Seat Track · wornDURING A MAINTENANCE VISIT FOUND THE SEAT TRACK WORN BEYOND LIMITS AT STA 590 TO 980 LBL 48, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// RECEIVED PART AND INSTALLED IAW DC-8 SRM 53-2-3, FIG 8A AND 53-7-1, FIG 4.SDR RRXA10894Fitting · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE TORQUE BOX BANANA FITTING AT STA 1150 L31R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. RECEIVED PART AND INSTALLED IAW DC-8 SRM 51-1-20D AND 53-1-0.SDR RRXA10890Fitting · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE SPLICE FITTING AT LONGERON 35R AT STA 1050, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. RECEIVED PART AND INSTALLED IAW DC-8 SRM 51-1-20D, 51-3-0, 53-1-0 AND DWG 370545.SDR RRXA010891Fitting · misdrilledDURING A MAINTENANCE VISIT FOUND A DRILLED END FITTING AT RADIUS AT STA 1687 L21R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. RECEIVED PART AND INSTALLED IAW DC-8 SRM 51-1-21, 51-1-20D AND DWG 4773155.SDR DHL2001806619Fitting · crackedC-CHECK - AFT FUSELAGE INTERIOR RT UPPER PART FITTING CRACKED 1-1/2 INCH AT STA 1766 L-9R. REMOVED CRACKED FITTING FROM AFT FUSELAGE INTERIOR RT UPPER PART IAW SRM 51-1-20D PAGE 21. CLEANED, TREATED & PRIMED AREA IAW SRM 51-1-88. INSTALLED NEW FITTING (P/NSDR RRXA10889Doubler · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE LH AUX TANK UPPER SPAR CAP BETWEEN STA XFS 1.25 TO XFS 113.750, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IASDR RRXA10887Fitting · crackedDURING A MAINTENANCE VISIT FOUND A LARGE GAP BETWEEN O/B END FITTING AND BATHTUB FITTING AT FS 1220 AND L33L TO L34L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// RECEIVED PART AND INSTALLED IAW DC-8 SRM 51-1-20D, 53-1-0 AND DWG 3755SDR RRXA10886Fitting · tool damageDURING A MAINTENANCE VISIT FOUND A DRILL START TO THE BATHTUB FITTING AT STA 1228 AND L35L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. RECEIVED PART AND INSTALLED IAW DC-8 SRM 51-1-20D, 53-1-0 AND DWG 3755845.SDR RRXA10885Rib · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE L/H CENTER L/E AT STA XFS 291-500 AND 304.000, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// FABRICATED PART AND INSTALLED IAW DC-8 SRM 57-2-0, FIG 2, 51-1-21 AND 51-1-20D.SDR DHL2001806604Fitting · crackedC-CHECK - FWD CARGO COMPT. FITTING CRACKED 1 INCH AT STA 200 L-25 RT. REMOVED CRACKED FITTING AT STA 200 L-25 RT (FWD CARGO COMPT) IAW SRM 51-3-0 PAGE 1, 2. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-3-0 PAGE 1, 2. STATUSSDR DHL2001806528Support · crackedC-CHECK - RH WING OUTBOARD FLAP. SUPPORT ARM PROTECTOR SHOWS 1 INCH CRACK AT STA XRS 230. REMOVED PROTECTOR FROM SUPPORT ARM IAW SRM 51-1-21 PAGE 1. FABRICATED NEW PROTECTOR IAW SRM 53-2-0 FIG 2. TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED NEW PROTECTOSDR RRXA11029Longeron · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LONGERON AT L33L AND STA 1168-1270, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 51-1-2SDR DHL2001806594Fitting · crackedC-CHECK - AFT CARGO COMPARTMENT. FITTING CRACKED 1 INCH BETWEEN L-25L AND L-23L. STA 1180.000. REMOVED FITTING CRACKED FROM AFT CARGO COMPARTMENT BETWEEN L-25L AND L-27L IAW SRM 51-1-21 PAGE 21. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSPECTED NEW SDR UPS01835539Web · corrodedINSPECTION TYPE:C2 AT STA -67 SUB FLOOR RT SIDE CORROSION AT CUSP IN FLT DECK REPAIRED SUBFLOOR AT STA -67 AT CUSP AREA DAC DWG SRO 8530026SDR UPS01835448Stop Fitting · missingINSPECTION TYPE:PFLT BOTH OVERWING EXIT DOORS MISSING STOP FITTING ASSY/WILL NOT LATCH RESEATED IN SILL AND LATCHED INTO PLACE. M/M 52-20-00SDR RRXA10901Fitting · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE BATHTUB FITTING AT STA 1220 BETWEEN L34R TO L35R AND L35R TO L36R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAWSDR RRXA10900Rib · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE RIGHT WING L/E RIB (UPPER) AT STA XFS 816.250, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. RECEIVED REPAIR AND INSTALLED IAW DC-8 SRM 57-2-0, FIG 2.SDR RRXA10899Doubler · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE FINGER DOUBLER AT FS 1350 L32R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-20D, 51-1-21 AND DWG 5779915.SDR RRXA10898Rib · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE RIB TIP ON THE LT CENTER L/E AT STA XFS 341.500, 354.800 & 360.250, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. RECEIVED REPAIR AND INSTALLED IAW DC-8 SRM 57-2-0, FIG 2.SDR RRXA10897Rib · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE RIB TIP LT WING L/E AT STA XFS 385-250, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. RECEIVED REPAIR AND INSTALLED IAW DC-8 SRM 57-2-0, FIG 2.SDR RRXA10892Rib · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE RIB TIP ON THE L/H L/E WING CENTER AT STA XFS 422.750, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// FABRICATED PART AND INSTALLED IAAW DC-8 SRM 57-2-0, FIG AND 51-1-20D.SDR RRXA10884Skin · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE FWD DRAIN HOLE ON THE LT WING O/B L/E LWR SKIN AT STA XFS 597.5, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21, 51-1-21D AND SH SK 602-627.SDR RRXA10883Fitting · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE C-PIT DOOR FRAME NR 2 LATCH BACKUP FITTING, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 51-1-20D, 53-1SDR RRXA10882Fitting · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE C-PIT DOOR FRAME NR 5 LATCH BACKUP, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 51-1-20D, 53-1-0 AND SDR RRXA10881Fitting · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE C-PIT DOOR FRAME LOWER NR 4 LATCH BACKUP FITTING , DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 53-1-0SDR RRXA10880Longeron · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LONGERON 36 AT STA 140-160, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 53-4-1, FIG 28 AND DWG 5758874SDR RRXA10879Rib · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE RIB ON THE LEFT WING L/E AT STA XFS 641.25, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. RECEIVED REPAIR AND INSTALLED IAW DC-8 SRM 57-2-0, FIG 2.SDR RRXA10878Rib · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE RIB LEFT WING L/E AT STA XFS 616.25 AND 622.5, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. RECEIVED REPAIR AND INSTALLED IAW DC-8 SRM 57-2-0, FIG 2.SDR RRXA10877Rib · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE RIB ON THE LEFT WING L/E AT STA XF 5660, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. RECEIVED REPAIR AND INSTALLED IAW DC-8 SRM 57-2-0, FIG 2.SDR RRXA10876Rib · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE RIB ON THE LEFT WING L/E AT STA XFS 578375, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. RECEIVED REPAIR AND INSTALLED IAW DC-8 SRM 57-2-0, FIG 2.SDR RRXA10875Rib · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE LEFT WING L/E UPPER RIB AT STA X5497-401, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. RECEIVED REPAIR AND INSTALLED IAW DC-8 SRM 57-2-0, FIG 2.SDR DHL2001806634Channel · crackedC-CHECK - MAIN CARGO JOINT ANGLE FROM CROSSBEAM - INTERCOSTAL AT STA 680.000 LBL 46.5 CRACKED 2 INCHES. REMOVED CRACKED ANGLE (CHANNEL) IAW SRM 51-3-0 PAGE 1, 2. FABRICATED NEW ANGLE (CHANNEL) IAW ATM 044340A, EA 2001131, DWG 573275. CLEANED, TREATED, AND PSDR DHL2001802003Switch · faultyUNABLE TO MAINTAIN CABIN PRESS WITH FLOWS AT MAX MANUAL CONTROL FULL CLOSED. FOUND FAULTY SCOOP ANTI-ICE SWITCH CAUSING LT SCOOP VALVE TO INTERMITTINGLY STICK IN THE OPEN POSITION. REPLACED SWITCH PER MM 20-50-1. ALSO REPLACED LT SCOOP VALVE AS PRECAUTION PSDR RRXA10893Skin · crackedDURING A MAINTENANCE VISIT FOUND DAMAGE TO THE LEFT I/B FLAP T/E OTBD END, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21 AND DWG 3652279.SDR DHL2001806606Fitting · corrodedC-CHECK - FWD CARGO COMPARTMENT - FITTING BETWEEN FRAME AND BEAM SHOWS CORROSION AT STA 822.000, L-21R. R/R FITTING CORRODED IAW SRM 51-1-20D PAGE 21. CLEANED, TREATED AND PRIMED MAIN CARGO COMPARTMENT FITTING BETWEEN FRAME AND BEAM AT STA 827.000 L-21R IAWSDR DHL2001806605Fitting · crackedC-CHECK - FWD CARGO COMPARTMENT FITTING CRACKED 4 INCH BETWEEN STA 600.000 AND STA 620.000 L-32R. R/R FITTING CRACKED IAW SRM 51-1-200 PAGE 21. CLEANED TREATED AND PRIMED FWD CARGO COMPT FITTING BETWEEN STA 600.000 AND STA 620.000 L-32R IAW SRM 51-1-8B. ISDR DHL2001805004Connector · dirtyCOMPASS SYSTEM NR 1 AND NR 2 ARE NOT SLAVING TO MAGNETIC HEADING, DG FUNCTION APPEARS NORMAL. CLEANED CONNECTOR AT COMPASS COMPARATOR SYSTEM SLAVING NORMAL, SWUNG TO KNOWN HEADING, SYSTEM CHECKED OK IAW MM 34-24-0.SDR RRXA11046Longeron · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LONGERON AT STA1050-1270 AND L36, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-20D,
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