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.

SDR UPS99829334Bulb · failedINSPECTION TYPE:N/A, CAPT'S EMERGENCY INSTRUMENT LIGHT OUT. RELAMPED CAPT'S EMERGENCY INSTRUMENT LIGHT, OPS CHECK GOOD.Apr 17, 1999 · N867UP · Doug DC873F · Emergency LightingSDR RRXA991351Angle · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, ATTACH ANGLE, LOWER AFT CARGO COMPARTMENT AT STA 1320, LONGERON 21 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER AND SUPPApr 17, 1999 · N606AL · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA991340Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, LT ELEVATOR, AREA UNDER PANEL 69 BETWEEN STA XE 32.937 AND STA XE 50.00. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPRApr 17, 1999 · N606AL · Doug DC873F · Elevator, Plate/SkinSDR RRXA991339Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, LT ELEVATOR, 3 SPOTS BETWEEN STA XE259 AND STA XE 269. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FINGER DOUBLERS TO TRAILING EDGE IAW DC8 SRM Apr 17, 1999 · N606AL · Doug DC873F · Elevator, Plate/SkinSDR RRXA991338Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, RIGHT WING, I/B L/E UPPER SURFACE AT SCREW HOLES BETWEEN STA XFS 7.50 AND XFS 26.25. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAW DC8Apr 17, 1999 · N606AL · Doug DC873F · Wing, Plate/SkinSDR RRXA991336Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, LEFT WING, I/B L/E UPPER SURFACE AT SCREW HOLES BETWEEN STA XFS 7.50 AND STA XFS 26.250. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBApr 17, 1999 · N606AL · Doug DC873F · Wing, Plate/SkinSDR RRXA991335Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, RIGHT WING, I/B L/E TANK UPPER SURFACE AROUND SCREW HOLES BETWEEN STA XFS 151.250 AND XFS 157.500. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FApr 17, 1999 · N606AL · Doug DC873F · Wing, Plate/SkinSDR RRXA991334Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, RIGHT WING, I/B L/E UPPER SURFACEO/B END AT STA XFS 191.625. 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 51-1-21 AND Apr 17, 1999 · N606AL · Doug DC873F · Wing, Plate/SkinSDR RRXA991332Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, RIGHT WING, O/B SLOT UPPER I/B PANEL AT L/E, STA XFS.Apr 17, 1999 · N606AL · Doug DC873F · Wing, Plate/SkinSDR RRXA991330Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, RIGHT WING, IN SCREW HOLES O/B LEADING EDGE, I/B SEGMENT UPPER SURFACE AT FRONT SPAR BETWEEN STA XFS 566.250 AND STA XFS 603.750. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1Apr 17, 1999 · N606AL · Doug DC873F · Wing, Plate/SkinSDR RRXA991329Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, RIGHT WING, O/B LEADING EDGE I/B SEGMENT O/B EDGE AT STA XFS 710. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW DC8 Apr 17, 1999 · N606AL · Doug DC873F · Wing, Plate/SkinSDR RRXA991327Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, RIGHT WING, IN SCREW HOLES O/B LEADING EDGE OUTBOARD SEGMENT INBOARD EDGE AT STA XFS 710. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOApr 17, 1999 · N606AL · Doug DC873F · Wing, Plate/SkinSDR RRXA991326Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, RIGHT WING, O/B L/E O/B SEGMENT O/B END LWR SURFACE 22 FWD OF FRONT SPAR AT STA XFS 878.750. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR Apr 17, 1999 · N606AL · Doug DC873F · Wing, Plate/SkinSDR UPS99829534Longeron · crackedINSPECTION TYPE:C RT WHEEL WELL LONG 24R CRACKED AT STA 940 DOT M-944. REMOVED CRACKED LONGERON, REPLACED LONGERON 24R AS PER JOB CARD NR 904 53100.Apr 16, 1999 · N819UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS99829532Fitting · crackedINSPECTION TYPE:C RT WHEEL WELL TRAP FITTING CRACKED IN AFT WEB DOT M942. REMOVED CRACKED TRAP FITTING, REPLACED TRAP FITTING AS PER JOB CARD NR 90432100 (UPS NR 929640).Apr 16, 1999 · N819UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS99829531Fitting · corrodedINSPECTION TYPE:C LEFT WHEEL WELL FITTING AT STA 880, LONG 24R CORRODED DOT M940. REMOVED CORRODED FITTING FABRICATED REPAIR ANGLES IAW DC-8 SRM 53-2- 0, ALODINED AND PRIMED REPAIRED PARTS IAW DC-8 SRM 51-1-8. CUT NEW FITTING IAW DC-8 SRM 53-2-0 AND INSTALLEApr 16, 1999 · N819UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS99829506Skin · damagedINSPECTION TYPE:C3, REPAIR FUSELAGE SKIN AT LONG 31R BETWEEN FS 1260 AND 1280 IAW DH SK 840-431. COMPLIED WITH DH SK 840-431.Apr 16, 1999 · N840UP · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS99829390Skin · corrodedINSPECTION TYPE:C3 VERTICAL STAB L/E SKIN AT ZFS 30.5 IS CORRODED BEYOND LIMITS. CUT OUT DAMAGED AREA AND REPAIRED IAW SRM 55-2-1 FIG 4.Apr 16, 1999 · N840UP · Doug DC873F · Vertical Stabilizer, Plate/SkinSDR RRXA99661Bleed Duct · blownREDUCED EPR TO AT 3000 FT, ALT NR 4 ENG FIRE WARNING WHEN THROTTLE WAS PULLED TO IDLE LT AND BFW WENT OUT RTB TO KGSO. FOUND BLOWN DUCT REMOVED AND REPLACED DUCT IAW MM CHAPTER 75 ENGINE OPS CK GOOD ON ENGINE RUN, NO DEFECTS NOTED ON NR 4 ENGINE.Apr 16, 1999 · N2674U · Doug DC873F · Pneumatic Distribution SystemSDR UPS99829568Fitting · misdrilledINSPECTION TYPE:C2, MAIN CABIN C-3 TORQUE BOX HAS MISDRILLED HOLES L-20R. REMOVED FORWARD SECTION, REMOVED FITTINGS, LOCATED DRILLED FITTINGS, INSTALLED FITTINGS, FABBED INNER AND OUTER IAW DC8 SRM 51-1-20D AND 5 1-3-0.Apr 15, 1999 · N819UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS99829418Rib · crackedINSPECTION TYPE:C3 RT WING L/E RIB AT XFS 847.5 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.Apr 15, 1999 · N840UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS99829400Frame · damagedINSPECTION TYPE:C3 FS 100 FRAME AT LONG 20R HAS A HOLE DRILLED IN THE RADIUS. REPAIRED FRAME IAW DH SK840-071.Apr 15, 1999 · N840UP · Doug DC873F · Fuselage Main, FrameSDR UPS99829398Floorbeam · corrodedINSPECTION TYPE:C3 FS 180 FLOORBEAM AT RBL 24 IS CORRODED OUT OF LIMITS. REPAIRED FLOORBEAM IAW DH SK840-665.Apr 15, 1999 · N840UP · Doug DC873F · Fuselage Main, Floor BeamSDR RRXA991353Channel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, FLOOR ATTACH CHANNEL BETWEEN STA 980 AND STA 1140 AT LONGERON 33 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FLOOR CHANNEL IAW Apr 15, 1999 · N606AL · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA991352Channel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, FLOOR ATTACH CHANNEL BETWEEN STA 980 AND STA 1140 AT LONGERON 33 LEFT.. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FLOOR CHANNEL IAW Apr 15, 1999 · N606AL · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS99829597Frame · corrodedINSPECTION TYPE:C3, FUSELAGE FRAME AT FS 1020 AND LONG 34L HAS HEAVY CORROSION. CUT OUT DAMAGED SECTION AND REPAIRED IAW SRM 53-2-0.Apr 14, 1999 · N840UP · Doug DC873F · Fuselage Main, FrameSDR UPS99829566Bracket · crackedINSPECTION TYPE:C, NR 4 ENGINE OUTBOARD T/R FWD LOWER CORNER BRACKET CRACKED. DYE PEN AREA IAW MIL-27IF, NO CRACKS NOTED.Apr 14, 1999 · N819UP · Doug DC873F · Engine Thrust ReverserSDR UPS99829535Longeron · misdrilledINSPECTION TYPE:C GILINER NUT PLATES INSTALLED INCORRECTLY AT STA 1080 LONG 34-35 1100, LONG 32-33R. REMOVED DAMAGE, AND FABBED DOUBLER, STRAP AND FILLER IAW REO-06431 A ND DWG NR DC-8-53-229, LOCATED DRILLED PARTS PER DC-8 SRM 51-3-2. REPA IRS IAW DC-8 SRM 5Apr 14, 1999 · N819UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR RRXA991343Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, LAV SERVICE DOOR PANEL BETWEEN STA 100 AND STA 120 RIGHT AND BETWEEN LONGERONS 24 RIGHT AND LONGERON 28 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRApr 14, 1999 · N606AL · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS99829452Frame · damagedINSPECTION TYPE:C3, FS 1240 FRAME ABOVE LONGERON 21L HAS A HOLE DRILLED THRU THE RADIUS. REPAIRED FRAME IAW DH SK840-049.Apr 13, 1999 · N840UP · Doug DC873F · Fuselage Main, FrameSDR UPS99829256Battery Pack · dischargedINSPECTION TYPE-N/A, EMERGENCY LIGHTING INOP. REMOVED AND REPLACED EMERGENCY LIGHTING BATT PACK, OPS CHECK GOOD. P/N OFF 5708458-503,P/N ON 60-1223-5, S/N ON 335, OFF 3310Apr 13, 1999 · N867UP · Doug DC873F · Emergency LightingSDR RRXA991360Fitting · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, ATTACH FITTING AT STA 460, LONGERON 21 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPLACEMENT ATTACH FITTING IAW DC8 SRM 51-3-Apr 13, 1999 · N606AL · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA991354Floorbeam · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, FLOORBEAM UNDER SEAT TRACK 3 ABOVE LONGERON 32 LEFT AT STA 1700. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR STRAP IAW FAA APPROApr 13, 1999 · N606AL · Doug DC873F · Fuselage Main, Floor BeamSDR RRXA991350Angle · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, ATTACH ANGLE, FRAME AT STA 360, AFT SIDE ABOVE BETWEEN LONGERONS 31 RIGHT AND LONGERON 29 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSApr 13, 1999 · N606AL · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA991348Angle · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, ATTACH ANGLE AT NUT PLATES STA 640 BETWEEN LONGERONS 27 LEFT AND LONGERON 27 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FILLERApr 13, 1999 · N606AL · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA991345Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, BOTTOM SKIN AT STA 702 BETWEEN LONGERONS 34 LEFT AND LONGERON 34 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAW FAA AApr 13, 1999 · N606AL · Doug DC873F · Fuselage Main, Plate/SkinSDR RRXA991344Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, BOTTOM SKIN AT STA 717 AND LONGERON 36. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLERS IAW FAA APPROVED TENNESSEE TECHNICAL SERVApr 13, 1999 · N606AL · Doug DC873F · Fuselage Main, Plate/SkinSDR RRXA991325Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, LEFT WING, O/B L/E O/B SEGMENT LWR SURFACE AT STA XFS 878.750. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW DC8 SRApr 13, 1999 · N606AL · Doug DC873F · Wing, Plate/SkinSDR UPS99829638Splice · corrodedINSPECTION TYPE:C3, FS 1100 FRAME UPPER LIP AT LONG 27R HAS HEAVY CORROSION. REMOVED DAMAGED SPLICE, FABRICATED AND REPLACED IAW DWG 3773159 AND SRM 51-1-20D.Apr 12, 1999 · N840UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS99829255Battery Pack · dischargedINSPECTION TYPE-N/A, EMERGENCY EXIT LIGHTS DO NOT ILLUMINATE WHEN ARMED. REPLACED BATT PACK, OPS CHECK GOOD.Apr 12, 1999 · N866UP · Doug DC873F · Emergency LightingSDR UPS99829594Fitting · corrodedINSPECTION TYPE:C3, BATHTUB FITTING AT FS 1150 AND LONG 35R IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.Apr 11, 1999 · N840UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS99829588Cusp · corrodedINSPECTION TYPE:C3, RT CUSP FS 1320 TO 1330 & 1340 TO 1365 IS CORRODED BEYOND LIMITS. CUT OUT DAMAGED SECTION, FABRICATED AND REPLACED CUSP IAW SRM 53-2-5.Apr 11, 1999 · N840UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS99829524Cusp · corrodedINSPECTION TYPE:C3 LT CUSP AT FS 390 TO 400, THE UPPER SURFACE IS CORRODED BEYOND LIMITS. REMOVED CUSP BEAM FROM FS 370 TO 470. FABRICATED CUSP AND REPAIR ANGLES IAW SRM 53-2-5 FIG 15A. CPCPApr 11, 1999 · N840UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS99829408Intercostal · corrodedINSPECTION TYPE:C3 FS 120-140 AT LONG 14R, THE INTERCOSTAL UPPER FLANGE IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED, AND INSTALLED INTERCOSTAL IAW DWG 5615614 AND SRM 51-1-21.Apr 11, 1999 · N840UP · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL9980763CTab · delaminatedAT C CHECK, LEFT ELEVATOR GEAR TAB IS DELAMINATED. REPAIRED AND INSTALLED PER MM 27-30-3. N/R 38.Apr 11, 1999 · N807DH · Doug DC873F · Elevator, Tab StructureSDR UPS99829637Longeron · crackedINSPECTION TYPE:C3, LONG 35L IS CRACKED AT FS 1270. REMOVED AND REPLACED SECTION OF LONGERON IAW SRM 51-1-20D.Apr 9, 1999 · N840UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS99829525Fitting · crackedINSPECTION TYPE:C3 INBD SIDE OF THE XRS 74.5 BULKHEAD, THE STR 51 FWD END FITTING IS CRACKED. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20 AND 51-1-23.Apr 9, 1999 · N840UP · Doug DC873F · Wing Miscellaneous StructureSDR UPS99829454Fitting · crackedINSPECTION TYPE:C3, RT WING O/B OF THE XRS 74.5 BULKHEAD, BOTH STRINGER 51 END FITTINGS ARE CRACKED. REMOVED AND REPLACED FITTINGS IAW SRM 51-1-20D AND 51-3-0.Apr 9, 1999 · N840UP · Doug DC873F · Wing Miscellaneous StructureSDR UPS99829397Fitting · crackedINSPECTION TYPE:C3 INBD SIDE OF THE STA XRS 74 BULKHEAD, THE STRINGER 51 AFT END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D AND 51-3-0.Apr 9, 1999 · N840UP · Doug DC873F · Wing Miscellaneous StructureSDR UPS99829307Fitting · corrodedINSPECTION TYPE:C123, STA 1180, THE LONGERON END FITTING IS CORRODED (STR 35R). REMOVED AND REPLACED FITTING IAW DWG 3753845-1.Apr 9, 1999 · N840UP · Doug DC873F · Fuselage Miscellaneous Structure
Back to Douglas DC-8-73F