Douglas DC-8-73F

Service difficulty reports · 15,471

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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 UPS99829618Angle · corrodedINSPECTION TYPE:C2, NUT PLATE ANGLE HAS HEAVY CORROSION ON THE UNDERSIDE, FS 280 LONG 34L TO 34R. REMOVED, FABRICATED AND REPLACED NUT PLATE ANGLE IAW DHC SK880-410 AND SRM 51-1-21.Apr 27, 1999 · N880UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS99829603Longeron · corrodedINSPECTION TYPE:C3, LONG 23L AT FS 1665 HAS HEAVY CORROSION. CUT OUT DAMAGED SECTION FABRICATED AND REPLACED LONGERON IAW DWG 5646666 AND SRM 51-1-20D.Apr 27, 1999 · N840UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS99829593Skin · corrodedINSPECTION TYPE:C3, FUSELAGE SKIN AND DOUBLER AT FS 1654 AND LONG 31L ARE CORRODED BEYOND LIMITS. REPAIRED SKIN AND INTERNAL DOUBLER IAW DHC SK840-923.Apr 27, 1999 · N840UP · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS99829591Skin · damagedINSPECTION TYPE:C3, FUSELAGE SKIN AT FS 1280 TO 1300 LONG 25R TO 27R REQUIRES REPAIR. REPAIRED FUSELAGE SKIN IAW DHC SK840-064.Apr 27, 1999 · N840UP · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS99829587Fitting · corrodedINSPECTION TYPE:C2 FS 340 BETWEEN LONGERON 36 AND 34L, THE FRAME FITTING IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED, AND REPLACED FITTING IAW DHC SK880-410 AND SRM 51-1-20D AND 51-3-0.Apr 27, 1999 · N880UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS99829582Seat Track · corrodedINSPECTION TYPE:C2 SEAT TRACK FLANGE AT RBL 48, FS 55 TO 80 IS CORRODED BEYOND LIMITS. REMOVED DAMAGED SEAT TRACK FS 55 TO 110, FABRICATED AND REPLACED IAW SRM 53-2-3.Apr 27, 1999 · N880UP · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR UPS99829545Rib · crackedINSPECTION TYPE:C2, RT WING L/E RIBS AT XS 461.372 AND XS 484.895 ARE CRACKED AAND& REPAIRED IAW SRM 57-2-0.Apr 27, 1999 · N880UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS99829539Skin · crackedINSPECTION TYPE:C2 RT WING L/E LWR SKIN AT XFS 710 IS CRACKED BETWEEN SCREW HOLES. STOP DRILLED CRACK AND REPAIRED IAW EO DC8-5720-4087B.Apr 27, 1999 · N880UP · Doug DC873F · Wing, Plate/SkinSDR UPS99829538Skin · corrodedINSPECTION TYPE:C2 RT WING L/E LWR SURFACE BETWEEN XFS 38.75 AND 45.00 IS CORRODED BEYOND LIMITS. REPAIRED IAW DHC SK880-933. CPCPApr 27, 1999 · N880UP · Doug DC873F · Wing, Plate/SkinSDR UPS99829514Longeron · drilledINSPECTION TYPE:SV, LONGERON AT STATION 1660 L34R HAS DOUBLE DRILLED HOLE. REPAIRED PER REO 06451.Apr 27, 1999 · N801UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS99829490Rib · crackedINSPECTION TYPE:C2, RT WING L/E RIB AT XS 467.323 IS CRACKED AT THE AFT LWR END. STOP DRILLED, AND REPAIRED RIB IAW SRM 57-2-0 FIG 2.Apr 27, 1999 · N880UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS99829526Fitting · corrodedINSPECTION TYPE:C3 FS 1220 FRAME, FWD FLANGE AT LONGERON 33R IS CORRODED OUT OF LIMITS. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D.Apr 26, 1999 · N840UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS99829511Frame · crackedINSPECTION TYPE:SV, FUSELAGE STATION 1660 L34L FRAME SPLICE CRACKED. REPAIRED IAW REO 06455 REPLACED DAMAGED FRAME SEGMENT AT FUSELAGE STATION 1660 BETWEEN L27L AND RIGHT PER DAC 564024209 FIG 1 AND REPLACED CLIP 5640242-65 PER DWG AND 5615374DW USING 7075T6 Apr 26, 1999 · N801UP · Doug DC873F · Fuselage Main, FrameSDR UPS99829485Rib · crackedINSPECTION TYPE:C2, RT WING L/E RIBS AT XFS 566.25, 855.0, 885.0, 878.75, 829.75, 816.25 803.75, 785.0, 766.25, 747.5, 728.75, 722.5, AND 716.25 ARE CRACKED. STOP DRILLED CRACKS AND REPAIRED IAW SRM 57-2-0 FIG 2.Apr 26, 1999 · N880UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS99829472Shear Tie · crackedINSPECTION TYPE:C2 SHEAR TIE AT FS 1360, BETWEEN LONGERON 31R AND 33R IS CRACKED. REMOVED, FABRICATED, AND INSTALLED SHEAR TIE IAW DWG 9755821-507 AND SRM 51-1-20D AND 51-1-21.Apr 26, 1999 · N880UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS99829470Doubler · corrodedINSPECTION TYPE:C2 FINGER DOUBLER, FS 1350, LONGERON 35L TO 35R IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED, AND INSTALLED FINGER DOUBLER IAW DWG 5750322 AND SRM 51-1-20D AND 51-1-21.Apr 26, 1999 · N880UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS99829425Stringer · corrodedINSPECTION TYPE-A, STRINGER 24L HAS EXTENSIVE CORROSION FROM STA 1660 TO STA 1667. ITEM ACCOMPLISHED ON N/R CARD 544808.Apr 26, 1999 · N814UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS99829424Frame · corrodedINSPECTION TYPE:A L/H CIRCUMFERENTIAL FRAME @ STA 1667 FROM STR 21 TO STR 23 HAS SEVER AL POPPED FASTENERS AND EXTENSIVE CORROSION. REMOVED LOWER SECTION OF CIR FRAME. THIS ITEM ACCOMPLISHED ON N/R CARD 544806.Apr 26, 1999 · N814UP · Doug DC873F · Fuselage Main, FrameSDR UPS99829422Floorbeam · damagedINSPECTION TYPE-A, FLOORBEAM MOUNT HOLES ELONGATED AT STA 1680 AT LT O/B SEAT TRACK. THIS ITEM ACCOMPLISHED ON N/R CARD 544810.Apr 26, 1999 · N814UP · Doug DC873F · Fuselage Main, Floor BeamSDR RRXA991341Web · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, RIGHT ELEVATOR INBOARD LIGHTNING HOLES AT STA XE 32.9. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAW DC8 SRM 55-2-1. REPAIR INDEX 2E Apr 26, 1999 · N606AL · Doug DC873F · Elevator, Plate/SkinSDR UPS99829488Frame · crackedINSPECTION TYPE:C2, FS 1446 FRAME AT LONG 34R IS CRACKED. REMOVED DAMAGED AREA AND REPAIRED IAW SRM 53-2-0 FIG 13.Apr 25, 1999 · N880UP · Doug DC873F · Fuselage Main, FrameSDR UPS99829513Floorbeam · corrodedINSPECTION TYPE:SV, FLOORBEAM STATION 1600 AFT FACE 36 FROM LEFT CUSP HAS CORROSION. REPAIRED IAW REO 06439 REV A PER TIMCO DWG DC08-53-0351 REV A -501 INSTALLATION AND UPS REPAIR AUTHORIZATION DC8-53-2583.Apr 24, 1999 · N801UP · Doug DC873F · Fuselage Main, Floor BeamSDR UPS99829512Cusp · corrodedINSPECTION TYPE:SV, FLOORBEAM STATION 1580 LEFT CUSP HAS CORROSION. REPAIRED IAW REO 06440 REV A TIMCO DWG DC08-53-0351 REV A-501 INSTALLATION AND UPS REPAIR AUTHORIZATION DC8-53-2588.Apr 24, 1999 · N801UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS99829410Battery Pack · dischargedWHILE PERFORMING EMERGENCY EXIT LIGHT TEST FOUND LIGHTS VERY DIM. REMOVED AND REPLACED BATT PACK. SYSTEM OPS CHECK GOOD PER MM 35-52-0.Apr 24, 1999 · N894UP · Doug DC873F · Emergency LightingSDR RRXA991357Shim · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, LT UPPER CUSP AT STA 380 FROM FRAME ATTACH ANGLE SHIM, LONGERON 21 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED SHIM IAW DC8 SRM Apr 24, 1999 · N606AL · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS99829602Fitting · damagedINSPECTION TYPE:C3, FS 55, LBL 54 TO RBL 54, THE FLOOR SUPPORT FITTINGS REQUIRE REPAIR. REPAIRED DAMAGED FLOOR SUPPORT FITTINGS IAW DHC SK840-196 AND DHC SK840-172.Apr 23, 1999 · N840UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS99829541Web · corrodedINSPECTION TYPE:C2 VERT STAB BASE, FS 1781 THROUGH 1818, RT WEB BETWEEN THE CENTER AND REAR SPARS HAS HEAVY EXFOLIATION CORROSION. CUT OUT DAMAGED AREA AND REPAIRED IAW SRM 51-1-9A. CPCPApr 23, 1999 · N880UP · Doug DC873F · Vertical StabilizerSDR UPS99829536Skin · crackedINSPECTION TYPE:C2 FUSELAGE SKIN AT FS 1240 TO 1280, APPROX LONG 33R, AT THE D-PIT DOOR CUT OUT IS CRACKED AND HAS HEAVY CORROSION. REMOVED AND REPLACED THE SKIN IAW SRM 51-1-20D AND 51-3-0. CPCPApr 23, 1999 · N880UP · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS99829505Fitting · crackedINSPECTION TYPE:C3 SUPPORT FITTING AT FS 55, LBL 48 IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D AND 51-1-21.Apr 23, 1999 · N840UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS99829503Longeron · crackedINSPECTION TYPE:C3, LONG 18L AT FS 540 IS CRACKED. REMOVED DAMAGED SECTION, FABRICATED, AND REPLACED LONGERON IAW SRM 53-2-2.Apr 23, 1999 · N840UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR RRXA991363Floorbeam · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, FLOOR SUPPORT UNDER CLIP NUTS AT STA 1746, BETWEEN BL 7-1/2 RIGHT AND BL 23 1/2 RIGHT AT LONGERON 21 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICAApr 23, 1999 · N606AL · Doug DC873F · Fuselage Main, Floor BeamSDR RRXA991361Floorbeam · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, FLOOR SUPPORT UNDER CLIP NUTS, AT STA 1746, BETWEEN BL 1.5 LEFT AND BL 20.5 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FLOORBEAApr 23, 1999 · N606AL · Doug DC873F · Fuselage Main, Floor BeamSDR RRXA991331Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, LEFT WING, AROUND SCREW HOLES, L/E CENTER SECTION UPPER SURFACE BETWEEN STA XFS 304 AND STA XFS 397.750. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALApr 23, 1999 · N606AL · Doug DC873F · Wing, Plate/SkinSDR UPS99829661Floorbeam · damagedINSPECTION TYPE:N/A, FLOORBEAM AT FS 1680 HAS ELONGATED HOLES FOR CENTER FASTENER OF SEAT TRACK AFT END. CLEANED UP HOLES TO .5 PER EO DC8-5310-11039-A.Apr 22, 1999 · N814UP · Doug DC873F · Fuselage Main, Floor BeamSDR UPS99829656Angle · corrodedINSPECTION TYPE:C2, FS -62, LBL 60, THE CUSP TEE ANGLE IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND REPLACED THE TEE ANGLE IAW DWG 5613857 AND SRM 51-1-20D.Apr 22, 1999 · N880UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS99829617Skin · corrodedINSPECTION TYPE:C2, FUSELAGE EXTERNAL SKIN AT FS 1620, LONG 20L IS CORRODED BEYOND LIMITS. CUT OUT DAMAGED AREA AND REPAIRED IAW DHC SK880-113.Apr 22, 1999 · N880UP · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS99829586Fitting · crackedINSPECTION TYPE:C2 FITTING TOP OF CENTER WING BOX AT FS 680 AND LONGERON 22R IS CRACKED. REMOVED, FABRICATED, AND REPLACED FITTING IAW DWG 3642974 AND SRM 51-1-20D.Apr 22, 1999 · N880UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS99829575Fitting · crackedINSPECTION TYPE:C2 RT HORIZ STAB L/E AT XFS 47, THE UPPER BATHTUB FITTING IS CRACKED. REMOVED, FABRICATED, AND INSTALLED FITTING IAW DWG 4653888 AND SRM 51-1-20D.Apr 22, 1999 · N880UP · Doug DC873F · Horizontal Stabilizer StructureSDR UPS99829573Fitting · crackedINSPECTION TYPE:C2 LT HORIZ STAB LWR BATHTUB FITTINGS (3 EA.) AT XFS 47 IS CRACKED. REMOVED, FABRICATED, AND INSTALLED 3 EA FITTINGS IAW DWG 4653888, 4653760; AND SRM 51-1-20D.Apr 22, 1999 · N880UP · Doug DC873F · Horizontal Stabilizer StructureSDR UPS99829540Splice · crackedINSPECTION TYPE:C2 LONGERNON 31L SPLICE AT FS 450 IS CRACKED. REMOVED AND REPLACED SPLICE IAW SRM 51-1-20D.Apr 22, 1999 · N880UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS99829469Skin · corrodedINSPECTION TYPE:C2 LT WING UPPER L/E SKIN AT XFS 347.75 TO 370 IS CORRODED BEYOND LIMITS, AT THE T/E. CUT OUT DAMAGED AREA AND REPAIRED IAW SRM 57-2-1.Apr 22, 1999 · N880UP · Doug DC873F · Wing, Plate/SkinSDR RRXA991337Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, RIGHT WING, L/E TANK UPPER SURFACE AT SCREW HOLES BETWEEN STA XFS 95.000 AND STA XFS 101.250. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLEApr 22, 1999 · N606AL · Doug DC873F · Wing, Plate/SkinSDR UPS99829601Frame · corrodedINSPECTION TYPE:C3, FS 1000 FRAME AT LBL 32 IS CORRODED BEYOND LIMITS. CUT OUT DAMAGED SECTION AND REPAIRED IAW SRM 53-2-0 FIG 2.Apr 21, 1999 · N840UP · Doug DC873F · Fuselage Main, FrameSDR UPS99829583Shear Tie · crackedINSPECTION TYPE:C2 FS 1834 SHEAR TIE CRACKED AT LONGERON 3L. REMOVED DAMAGED SHEAR TIE, FABRICATED, AND REPLACED IAW SRM 53-2-0.Apr 21, 1999 · N880UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS99829579Fitting · crackedINSPECTION TYPE:C2 FS 1150 TORQUE BOX BATHTUB FITTING BETWEEN LONGERON 35R AND 34R IS CRACKED. REMOVED AND REPLACED THE FITTING IAW SRM 53-2-0.Apr 21, 1999 · N880UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS99829547Skin · corrodedINSPECTION TYPE:C2, RT WING L/E LWR SURFACE BETWEEN FS 38.75 AND 45.00 IS CORRODED BEYOND LIMITS. REPAIRED IAW DHC SK880-933.Apr 21, 1999 · N880UP · Doug DC873F · Wing, Plate/SkinSDR UPS99829537Doubler · crackedINSPECTION TYPE:C2 LT HORIZ STAB INBD SIDE OF THE STA XE 221.0 FRAME IS CRACKED AND TORN. REMOVED, FABRICATED, AND INSTALLED FINGER DOUBLER IAW DWG 5644310 AND SRM 51-1-21.Apr 21, 1999 · N880UP · Doug DC873F · Horizontal Stabilizer StructureSDR UPS99829509DOUBlER · crackedINSPECTION TYPE:C3, FS 1360 TO 1390, LT CUSP, THE FINGER DOUBLER IS CRACKED IN 2 PLACES. REMOVED, FABRICATED AND INSTALLED FINGER DOUBLER IAW DWG 5779936 AND SRM 51-1-21.Apr 21, 1999 · N840UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS99829492Skin · corrodedINSPECTION TYPE:C2, RT HORIZ STAB OTBD L/E, INBD FWD SECTION, STA. XFS 210, HAS BULGING CORROSION. CUT OUT DAMAGED AREA AND REPAIRED IAW SRM 55-2-1, FIG 4.Apr 21, 1999 · N880UP · Doug DC873F · Horizontal Stabilizer StructureSDR UPS99829489Fitting · crackedINSPECTION TYPE:C2, FS 1180, THE 'C' PIT DOOR FRAME FWD STOP FITTING IS CRACKED AT LONG 26L. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D.Apr 21, 1999 · N880UP · Doug DC873F · Fuselage Miscellaneous Structure
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