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 UPS97824983Rib · crackedINSPECTION TYPE-C, LT WING L/E RIB UPPER ARM CRACKED BY AFT FSTR AT STA 291.50. REPAIRED IAW SRM 57-2-0.Nov 5, 1997 · N840UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS97824953Doubler · crackedINSPECTION TYPE-C, LT WING L/E INNER DOUBLER CRACKED JUST AFT AND INBD OF O/B SLOT DOOR. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT SPLICE DOUBLER IAW SRM 51-1-20D AND DWG 5769891.Nov 5, 1997 · N840UP · Doug DC873F · Wing Miscellaneous StructureSDR UPS97824952Rib · crackedINSPECTION TYPE-C, LT WING L/E RIB CRACKED STA 778.750. REPAIRED IAW SRM 57-2-0.Nov 5, 1997 · N840UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS97824949Rib · crackedINSPECTION TYPE-C, RT WING L/E AT STA XFS 822.500 THE UPPER L/E RIB IS CRACKED. REPAIRED IAW SRM 57-2-0.Nov 5, 1997 · N840UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS97824948Rib · crackedINSPECTION TYPE-C, RT WING L/E AT STA XFS 828.250 THE UPPER L/E RIB IS CRACKED. REPAIRED IAW SRM 57-2-0.Nov 5, 1997 · N840UP · Doug DC873F · Wing, Rib/BulkheadSDR RRXA97309Harness · failedON CLIMBOUT EGT ON #3 ENG DROPPED 200 THEN FLUCTUATED BETWEEN 535 AND 542. IT IS UNRELIABLE. WE PERFORMED PRECAUTIONARY SHUTDOWN ON #3 ENG. **********CORRECTIVE ACTION**********R&R L/H EGT HARNESS OPS CK OF #3 EGT GOOD THRU ALL RANGES.Nov 5, 1997 · N870TV · Doug DC873F · Engine EGT/TIT Indicating SystemSDR DHL9780259CFitting · crackedAT C-CHECK, ULTRASONIC INSP FOUND LEFT HAND 98 PORKCHOP DRIVE LINK FLAP FITTING HAS CRACK AT ACTUATOR MOUNTING HOLE. REPLACED FITTING PER M/M.Nov 5, 1997 · N802DH · Doug DC873F · Trailing Edge Flap ActuatorSDR DHL9780251CSeat Track · wornAT C-CHECK, COPILOT SEAT TRACK WORN. REMOVED SEAT TRACKS AND FABRICATED PER SRM 53-2-3.Nov 5, 1997 · N802DH · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR DHL9780215CSkin · damagedAT C-CHECK, RIGHT WING OUTBD FLAP UPPER SKIN INBD SIDE OF INBD ICE BREAKER HAS INTERM REPAIR. REMOVED REPAIR, CUT OUT DAMAGED SECTION, FABRICATED NEW PARTS AND INSTALLED PER SRM 53-2-3. REPAIR 25 X 5.Nov 5, 1997 · N802DH · Doug DC873F · Trailing Edge FlapsSDR UPS97825065Rib · crackedINSPECTION TYPE-C, LT WING STA 641.250 L/E RIB (UPPER) CRACKED AND HOLES WITH NO PITCH. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT RIB IAW SRM 51-1-21, AND DWG 5769400.Nov 4, 1997 · N840UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS97825035Rib · crackedINSPECTION TYPE-C, LT WING L/E RIB AT STA XOLDI 6.225 IS CRACKED. REPAIRED IAW SRM 57-2-0.Nov 4, 1997 · N840UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS97824925Floorbeam · corrodedINSPECTION TYPE-C, FLOORBEAM AND WEB CORRODED FS 1700 BL 0. REPAIRED IAW DHC SK-801-128.Nov 4, 1997 · N801UP · Doug DC873F · Fuselage Main, Floor BeamSDR RRXA97307Fitting · damagedDURING A MAINTENANCE VISIT, FOUND FWD FRAME FITTING (P/N 3891767) DAMAGED BEYOND REPAIR IAW DC-8 SRM. PART AND REPAIR MATERAIL WAS NOT AVAILABLE FOR PURCHASE. FABRICATED NEW FITTING BY MATERAIL SUBSTITUTION IAW FAA APPROVED DER ENGINEERING SKETCH REO-03840.Nov 4, 1997 · N791FT · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA97306Bushing · corrosionDURING A MAINTENANCE VISIT, FOUND NLG DRAG BRACE RT UPPER ATTACH LUG BUSHING WAS PITTED. AFTER REMOVAL OF BUSHING, PITTING WAS FOUND ON THE ID OF THE BRACE ATTACH POINT. FINAL ID AFTER CORROSION REMOVAL IS 2.601, MAX. ALLOWABLE IS 2.577. *S/D* FABRICATED ANov 4, 1997 · N791FT · Doug DC873F · Landing Gear Retraction/Extension SystemSDR RRXA97305Doubler · damagedDURING A MAINTENANCE VISIT, FOUND RIGHT WING LOWER MAIN LANDING GEAR SUPPORT DOUBLER (P/N 5753736-1) HAD LARGE COUNTERSUNKS AND 3 KNIFE EDGE HOLES. *S/D* REMOVED DAMAGED SECTION, FABRICATED AND INSTALLED DOUBLER REPAIR IAW FAA DER APPROVED ENGINEERING SKETCHNov 4, 1997 · N791FT · Doug DC873F · Wing Miscellaneous StructureSDR RRXA97304Drain Mast · deletedDURING A MAINTENANCE VISIT, DELETED PART DRAIN MAST (P/N 5756067). DRAIN MAST NO LONGER REQUIRED AFT LWR FUSELAGE AT STA 1726.656. REMOVED DRAIN MAST AND INSTALLED BLANK-OFF PLATE TO COVER REMAINING HOLES IAW FAA DER APPROVED ENGINEERING SKETCH REO-03774.Nov 4, 1997 · N791FT · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA97303Frame · corrodedDURING A MAINTENANCE VISIT, FOUND FRAME INNER FLANGE CORRODED BEYOND LIMITATIONS IAW DC-8 SRM AT STA 1520 AND LONGERON 21R. *S/D* REMOVED AND TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER TO FRAME IAW FAA DER APPROVED TIMCO ENGINNov 4, 1997 · N791FT · Doug DC873F · Fuselage Main, FrameSDR RRXA97302Fitting · damagedDURING A MAINTENANCE VISIT, FOUND MAIN LANDING GEAR FITTING (P/N 5616344) DAMAGED BEYOND REPAIR IAW DC-8 SRM. (P/N 5616344 AND 5616132) ARE FABRICATED FROM 7075 ALUMINUM FORGING BLANK 5616429. FABRICATED BY SUBSTITUTION AND INSTALLED IAW FAA APPROVED DER TIMNov 4, 1997 · N791FT · Doug DC873F · Main Landing Gear Attach SectionSDR RRXA97301Fitting · damagedDURING A MAINTENANCE VISIT, FOUND I/B DOOR JAMB FITTING (P/N 4643861) DAMAGED BEYOND LIMITATIONS IAW DC-8 SRM. (P/N 4643861-1) IS FABRICATED FROM 2014-T6 ALUMINUM FORGING BLANK 4641554-1. THIS FORGING BLANK IS NOT AVAILABLE FOR PURCHASE. FABRICATED BY SUBSNov 4, 1997 · N791FT · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA97300Skin · dingedDURING A MAINTENANCE VISIT, FOUND DING IN SKIN, BLEND-OUT REPAIR WENT BEYOND LIMITATIONS IAW DC-8 SRM AT STA 62.25 AND LONGERON 22L. *S/D* REPAIRED BY FABRICATED AND INSTALLED DOUBLER REPAIR BY WELDED IAW FAA DER APPROVED TIMCO ENGINEERING SKETCH REO-03857 ANov 4, 1997 · N791FT · Doug DC873F · Fuselage Main, Plate/SkinSDR RRXA97299Frame · gougedDURING A MAINTENANCE VISIT, FOUND FRAME GOUGED IN UPPER FLANGE AND WEB AT STA 1260 AND BETWEEN LONGERONS 31R AND 32R. *S/D* REMOVED DAMAGED SECTION, FABRICATED AND INSTALLED DOUBLER REPAIR IAW FAA DER APPROVED TIMCO ENGINEERING SKETCH REO-03756. ALSO, IAW SNov 4, 1997 · N791FT · Doug DC873F · Fuselage Main, FrameSDR RRXA97298Skin · gougedDURING A MAINTENANCE VISIT, FOUND FUSELAGE SKIN HAS NUMEROUS GOUGES AND BLEND-OUTS LOCATED DIRECTLY BELOW MAIN CARGO DOOR CUTOUT. *S/D* BLEND-OUT DAMAGE BEYOND IAW DC-8 SRM 53-2-0 LIMITATIONS. FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW FAA DER ANov 4, 1997 · N791FT · Doug DC873F · Fuselage Main, Plate/SkinSDR RRXA97297Fitting · gougedDURING A MAINTENANCE VISIT, FOUND RIGHT WING AILERON SUPPORT FITTING (P/N 5640622-2) DAMAGED BEYOND LIMITATIONS IAW DC-8 SRM. PART AND FORGING MATERIAL NOT AVAILABLE. SUBSTITUTED MATERIAL IAW FAA APPROVED DER TIMCO ENGINEERING REO-03747 FOR FABRICATION.Nov 4, 1997 · N791FT · Doug DC873F · AileronsSDR RRXA97296Elect Panel · damagedDURING A MAINTENANCE VISIT, AFT ELECTRICAL PANEL LOCATED ABOVE AFT RIGHT OF ENTRY DOOR IS BEING RELOCATED BECAUSE OF CONSTANT DAMAGE BY CARGO CONTAINERS. RELOCATION WILL BE TO THE AFT CEILING AREA ACROSS FROM THE FLIGHT RECORDER, AT STA 1734 IAW FAA APPROVED Nov 4, 1997 · N791FT · Doug DC873F · AC Power Distribution SystemSDR RRXA97295Fitting · corrodedDURING A MAINTENANCE VISIT, FOUND RIGHT WING FLAP CANOE FITTING GOUGED BEYOND LIMITATIONS IAW DC-8 SRM AND DAC DWG 5614372 AT XW 98. *S/D* ALSO, FOUND CORROSION DAMAGE TO WING FLAP CANOE FITTING BEYOND LIMITATIONS IAW DC-8 SRM. REMOVED AND TREATED CORROSIONNov 4, 1997 · N791FT · Doug DC873F · Wing Miscellaneous StructureSDR RRXA97294Fitting · elongatedDURING A MAINTENANCE VISIT, FOUND LT WING FLAP FITTING (P/N 5652807) HAS ELONGATED HOLE AT HINGE END AT XW 4.0. REMOVED BASE FITTING IAW DC-8 SRM 51-3-2. REAMED HOLE TO 0.6735 IAW SRM 51-3-2 AND FAA DER APPROVED TIMCO ENGINEERING SKETCH REO-03724. FABRICATENov 4, 1997 · N791FT · Doug DC873F · Trailing Edge FlapsSDR RRXA97293Fitting · corrodedDURING A MAINTENANCE VISIT, FOUND FITTING (P/N 5711283-514, -515) CORRODED BEYOND LIMITATIONS IAW DC-8 SRM. (P/N 5711283-514, -515) IS MADE FROM 7075 FORGING BLANK, (P/N 4710626). THIS FORGING IS NOT AVAILABLE, MATERAIL SUBSTITUTED IAW FAA APPROVED DER TIMCONov 4, 1997 · N791FT · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA97292Vane · crackedDURING A MAINTENANCE VISIT, FOUND RIGHT WING OTBD L/E VANE ASSY HAS NUMEROUS SMALL CRACKS AT T/E. *S/D* FABRICATED AND INSTALLED REPAIR STRAP IAW FAA DER APPROVED TIMCO ENGINEERING SKETCH REO-03704.Nov 4, 1997 · N791FT · Doug DC873F · Leading Edge DevicesSDR RRXA97291Frame · mis drilledDURING A MAINTENANCE VISIT, FOUND FRAME WITH MIS DRILLED HOLE AT STA 360 AND LO NGERON 34R. *S/D* FABRICATED AND INSTALLED REPAIR STRAP IAW DC-8 SRM 53-2-0 FIGURE 1F, SHEET 3 AND FAA DER APPROVED TIMCO ENGINEERING SKETCH REO-03697.Nov 4, 1997 · N791FT · Doug DC873F · Fuselage Main, FrameSDR RRXA97290Flap Link · gougedDURING A MAINTENANCE VISIT, FOUND LEFT WING FLAP LINK GOUGED (0.060 X 0.50) AFT OF GREASE FITTING. *S/D* REPAIRED PART BY BLEND-OUT AND WITHIN LIMITATIONS IAW FAA DER APPROVED ENGINEERING SKETCH REO-03696 AND SRM 57-2-0 FIGURE 7.Nov 4, 1997 · N791FT · Doug DC873F · Trailing Edge FlapsSDR RRXA97289Skin · corrosionDURING A MAINTENANCE VISIT, FOUND SKIN ON UPPER RIGHT WING CORROSION DAMAGE BEYOND LIMITATIONS IAW DC-8 SRM AT XR 25.7555. REMOVED ALL CORROSION AND DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA DER APPROVED TIMCO ENGINEERING SKETCH REO-03695 REV.A.Nov 4, 1997 · N791FT · Doug DC873F · Wing, Plate/SkinSDR RRXA97288Skin · crackedDURING A MAINTENANCE VISIT, FOUND SKIN PANEL CRACKED UNDER EXISTING DOUBLER BETWEEN STA 220 AND STA 240 AND LONGERONS 24L AND 25L. *S/D* REMOVED DAMAGED SECTION, FABRICATED AND INSTALLED DOUBLER AND SPLICE REPAIR IAW DAC DAW 5641013 AND FAA DER TIMCO ENGINEENov 4, 1997 · N791FT · Doug DC873F · Fuselage Main, Plate/SkinSDR DHL9780229CSeat Track · wornAT C-CHECK, FS 420 LINE NR 3 TRACK CHIPPED. CUT OUT DAMAGED AREA AND FABRICATED REPAIR PLUG PER SRM SRM 53-2-3 PER SRM 51-1-8.Nov 4, 1997 · N802DH · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR UPS97825026Rib · crackedINSPECTION TYPE-C, RT WING L/E AT STA XFS 741.250, THE UPPER L/E RIB IS CRACKED AT THE AFT END. REPAIRED IAW SRM 57-2-0.Nov 3, 1997 · N840UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS97825025Rib · crackedINSPECTION TYPE-C, RT WING L/E AT STA XFS 816.25, THE UPPER L/E RIB IS CRACKED AT THE AFT END. REPAIRED IAW SRM 57-2-0.Nov 3, 1997 · N840UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS97825020Rib · crackedINSPECTION TYPE-C, RT WING L/E AT STA XFS 722.500, THE UPPER L/E RIB IS CRACKED AT THE AFT END. REPAIRED IAW SRM 57-2-0.Nov 3, 1997 · N840UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS97825019Rib · crackedINSPECTION TYPE-C, RT WING L/E AT STA XFS 803.750 UPPER RIB CRACKED. REPAIRED IAW SRM 57-2-0.Nov 3, 1997 · N840UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS97825018Rib · crackedINSPECTION TYPE-C, RT WING L/E AT STA XFS 797.50, THE UPPER L/E RIB IS CRACKED AT THE AFT END. REPAIRED IAW SRM 57-2-0.Nov 3, 1997 · N840UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS97825010Rib · crackedINSPECTION TYPE-C, RT WING L/E AT STA XFS 753.750, THE UPPER L/E RIB IS CRACKED AT THE AFT END. REPAIRED IAW SRM 57-2-0.Nov 3, 1997 · N840UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS97825008Rib · crackedINSPECTION TYPE-C, RT WING L/E AT STA XFS 810.00, THE L/E RIB IS CRACKED AT THE AFT END. REPAIRED IAW SRM 57-2-0.Nov 3, 1997 · N840UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS97825000Rib · crackedINSPECTION TYPE-C, RT WING L/E AT STA XFS 772.00, THE UPPER L/E RIB IS CRACKED AT THE AFT END. REPAIRED IAW SRM 57-2-0.Nov 3, 1997 · N840UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS97824981Skin · corrodedINSPECTION TYPE-C, RT WING L/E O/B OF O/B SECTION O/B END, L/E HAS HEAVY CORROSION UNDER THE SURFACE. REPAIRED IAW UPS EO DC8-5720-4087-B APDX C.Nov 3, 1997 · N840UP · Doug DC873F · Wing, Plate/SkinSDR UPS97824912Seat Track · corrodedINSPECTION TYPE-C, SEAT TRACK CORRODED FS 1695 BL 0. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT SECTION OF TRACK IAW SRM 53-2-3 AND 51-3-0.Nov 3, 1997 · N801UP · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR UPS97825100Rib · crackedINSPECTION TYPE-C, LT WING L/E RIB UPPER ARM CRACKED BY AFT FSTR AT STA 610.00. REPAIRED IAW SRM 57-2-0.Nov 2, 1997 · N840UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS97825063Seat Track · corrodedINSPECTION TYPE-C, SEAT TRACK LBL 45 HAS HEAVY CORROSION FS 1464 TO 1470 AND MODERATE CORROSION FS 1420 TO 1430. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT SECTION OF TRACK IAW SRM 53-2-3.Nov 2, 1997 · N840UP · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR UPS97825059Web · crackedINSPECTION TYPE-C, WEB BETWEEN FRAMES AT FS 65 AND 70 AND BETWEEN LONGERONS 21L AND 13L HAVE NUMEROUS DOUBLE DRILLED HOLES, OPEN HOLES, AND CRACKS. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT WEB IAW SRM 51-1-21 AND DWG 5597645.Nov 2, 1997 · N840UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS97825040Fitting · crackedINSPECTION TYPE-C, LT WING UPPER STRINGER END FITTING CRACKED JUST AFT OF MLG ACTUATOR. REMOVED AND REPLACED FITTING IAW SRM 51-1-21.Nov 2, 1997 · N840UP · Doug DC873F · Wing Miscellaneous StructureSDR UPS97825031Jamb · crackedINSPECTION TYPE-C, EXT FUSELAGE RT FWD SERVICE DOOR UPPER FWD DOOR JAMB HAS CRACK. REPAIRED IAW SRM 53-2-0.Nov 2, 1997 · N840UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS97825021Rib · crackedINSPECTION TYPE-C, RT WING L/E AT STA XFS 716.25, THE UPPER L/E RIB IS CRACKED AT THE AFT END. REPAIRED IAW SRM 57-2-0.Nov 2, 1997 · N840UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS97825006Rib · crackedINSPECTION TYPE-C, RT WING L/E AT STA XFS 791.250, THE UPPER L/E RIB IS CRACKED AT THE AFT END. REPAIRED IAW SRM 57-2-0.Nov 2, 1997 · N840UP · Doug DC873F · Wing, Rib/Bulkhead
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