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 DHL9980203CFitting · crackedAT C-CHECK, CENTER TANK AREA UPPER FUSELAGE STA 760 O/B RT OF SET TRACK NR 6 FITTING CRACKED BETWEEN FASTENERS. REMOVED CRACKED FITTING FROM CENTER TANK AREA UPPER FUSELAGE. DRILLED NEW FITTING PER SRM. CLEANED FITTING AREA PER SRM. OK TO TREAT, PRIME AREASDR UPS99829653Longeron · crackedINSPECTION TYPE:C2, LONGERON 36 IS CRACKED BETWEEN FS 1350 AND 1347. REPAIRED LONGERON IAW DH SK880-592.SDR UPS99829585Splice · crackedINSPECTION TYPE:C2 LONGERON 35L SPLICE AT FS 1490 IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D AND 51-1-21.SDR UPS99829574Frame · corrodedINSPECTION TYPE:C2 FS 1000 FRAME UPPER FLANGE, LWR SURFACE AT LONGERON 36, IS CORRODED BEYOND LIMITS. REPAIRED FRAME IAW SRM 53-2-0 FIG 2.SDR UPS99829476Battery Pack · dischargedEMERGENCY EXIT LIGHTS INOPERATIVE ON BATTERY POWER. REMOVED AND REPLACED EMERGENCY LIGHT BATT PACK. OPS CHECK GOOD P/N ON 60-1223-5, S/N 356, P/N OFF 5708458-503, S/N 488.SDR RRXA991346Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, SKIN FORWARD OF TAIL SKID AT STA 1746, LONGERON 36. 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 51-1-21 AND 51-1-2SDR RRXA991328Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, RIGHT WING, SKIN EDGE AND SCREW HOLES AT WING O/B LEADING EDGE I/B SECTION OF STA XS 540 BETWEEN + 38 AND +45 FORWARD OF FRONT SPAR. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM SDR DHL9980269CSkin · crackedC-CHECK, RT WING T/E LOWER PANEL HAS CRACK STA XRS 240 IS ABOUT 4 LONG DOT 64109. CUT OUT CRACKED AREA AT RT WING T/E LWR PANEL ST XRS 240 IAW DC-8 SRM 51-1-9A PG 1 THRU 69, FABRICATED FILLER FROM 2024-T3 0.020 (3 X 6) & DOUBLER REPAIR FROM 2024-T3 0.020 (7 XSDR DHL9980268CRib · crackedC-CHECK, RT WING O/B L/E INT THRU ACCES PANEL 517B RIB CRACK AT UPPER END XFS 848 DOT 64118. STOP DRILLED END CRACK AT RT WING O/B L/E RIBS STA XFS 848 & IAW DC-8 SRM 57-2-0 PG 9 FIG 2. FABRICATED ANGLE REPAIR 2024 T3 050 .75 X 1.25 X 5 IAW DC-8 SRM 57-2-0 PSDR DHL9980267CRib · crackedC-CHECK, RT WING O/B L/E INT THRU ACCESS PANEL 517B RIB CRACK AT UPPER END XFS 828 DOT 64119. STOP DRILLED END CRACK AT RT WING O/B L/E RIBS STA XFS 828 IAW DC-8 SRM 57-2-0 PG 9 FIG 2. FABRICATED ANGLE REPAIR 2024 T3 050 .75 X 1.25 X 4 IAW DC8 SRM 57-2-0 PG SDR DHL9980266CRib · crackedC-CHECK, RT WING O/B L/E INT THRU ACCESS PANEL 518A RIBS CRACKED AT UPPER END 3 XFS 822; XFS 815 & XFS 809 DOT 64120-64122-64121. STOP DRILLED END CRACK AT RT WING O/B L/E RIBS STA XFS 822 XFS 815 XFS 809 IAW DC-8 SRM 57-2-0 PG 9 FIG 2. STOP DRILLED END CRACSDR DHL9980265CRib · crackedC-CHECK, RT WING O/B L/E INT THRU ACCESS PANEL 518A RIB CRACK AT UPPER END XFS 797 DOT 64123. STOP DRILLED END CRACK AT RT WING O/B L/E RIB STA XFS 797.000 IAW DC-8 SRM 57-2-0 PG 9 FIG 2. FABRICATED ANGLE REPAIR 2024 T3 .050 .75 X 1.25 X 5 IAW DC-8 SRM 57-2-SDR DHL9980264CRib · crackedC-CHECK, RT WING O/B L/E INT THRU ACCES PANEL 518B CRACKED RIBS AT THE UPPER END XFS 772; XFS 779 & XFS 785 DOT 64124-64125-64126. STOP DRILLED END CRACK AT RT WING O/B L/E RIBS STA XFS 772, XFS 779 & XFS 785 IAW DC-8 SRM 51-3-2 PG 1 PAR 1 & SRM 57-2-0 PG 9/1SDR DHL9980257CSeat Track · crackedC-CHECK, SEAT TRACK NR 2 BETWEEN STA 240-260 PLUG NO GOOD. REMOVED (1) DAMAGED (4) FOUR HOLES CARGO TRACK REPAIR FROM NR 2 SEAT TRACK STA 240-260 IAW DC-8 SRM 51-3-0 PAR 1 & 2 FIG. CLEANED REPAIRED AREA PER SRM 51-1-8 PAR 6A. TREATED & PRIMED AREA IAW DC-8 SDR DHL9980256CRib · crackedC-CHECK, RT WING OUTB L/E INT THRU ACCESS PANEL 518B CRACKED RIBS AT UPPER END XFS 766.25 & XFS 760 DOT 64127-64128. STOPPED DRILLED END CRACK AT RT WING O/B L/E RIB STA XFS 766.250 & 760 IAW DC-8 SRM 57-2-0 PG 10 FIG 2. TREATED & PRIMED PER DC-8 SRM 51-1-8 SDR DHL9980255CRib · crackedC-CHECK, RT WING O/B L/E INTO THRU ACCESS PANEL 519C CRACKED RIBS TO UPPER END XFS 622 AND XFS 644 DOT 64131-64132. STOP DRILLED END CRACK AT RT WING O/B L/E RIBS STA XFS 641 & 622 IAW DC-8 SRM 57-2-0 PG 9 FIG 2. FABRICATED ANGLE REPAIR 2024 T3 050 .75 X 1.2SDR DHL9980254CRib · crackedC-CHECK, RT WING O/B L/E INT THRU ACCESS PANEL S/B CRACKED RIBS AT UPPER END XFS 728 & XFS 747 DOT 64129-64130. STOP DRILLED END CRACK AT RT WING O/B L/E RIBS STA XFS 728 &747 IAW DC-8 SRM 57-2-0 PG 9 FIG 2. FABRICATED ANGLE REPAIR 2024T3 050 .75 X 1.25 X 5 SDR DHL9980252CSeat Track · wornC-CHECK, SEAT TRACK NR 2 BETWEEN STA 1560-1610 TRACK WORN/CHIPPED. CUT OUT DAMAGED SECTION OF SEAT TRACK NR 2 BETWEEN STA 1560 TO 1650 & PREPARED NEW SECTION FROM: APPROPPIATE MATCHING SECTION OF TRACK & FABRICATED SPLICES FROM:7075-T6 0.100 (1 X 13) 0.125 (1SDR DHL9980237CSeat Track · crackedC-CHECK, SEAT TRACK NR 1 BETWEEN STA 480-580 TRACK HAS CORRODED SPOTS. CUT OUT DAMAGED SECTIONS OF TRACK NR 1 STA 520 IAW DC-8 SRM 53-2-3 FIG 6D SHEET 1-3. CLEANED REWORKED AREA PER SRM 51-1-8 PAR 6. TREATED & PRIMED REWORKED AREA IAW DC-8 SRM 51-1-8 PG 13 SDR DHL9980236CSeat Track · crackedC-CHECK, SEAT TRACK NR 1 BETWEEN STA 329 TO 380 TRACK HAS CORROSION. CUT OUT DAMAGED SECTION OF TRACK NR 1 AT STA 329 & CLEANED AREA OF SEAT TRACK BETWEEN STA 329 TO 380 IAW DC-8 SRM 53-2-3 FIG 6D SHEET 1 & 51-1-8 PAR 6A. FOUR HOLES CARGO TRACK REPAIR INSTALSDR DHL9980235CSpar · crackedC-CHECK, RT WING AT REAR SPAR AREA XW 5 WEB PANEL IS CRACK 3 LONG DOT 64101. STOP DRILLED END CRACK AT RT WING, REAR SPAR ARA XW5 WEB PANEL IAW DC-8 SRM 51-3-2. FABRICATED DOUBLER REPAIR AS PER SRM 57-2-0 PAR 2 E 6 X 6 .090-2024T3. TREATED & PRIMED AS PER SSDR DHL9980234CFitting · crackedC-CHECK, LT STA 97 FLAP HINGE SUPPORT FITTING HAS TWO CRACK INDICATION, ONE IN LT SIDE NR 2 HOLE & ONE IN RT SIDE NR 1 HOLE MARKED. ENLARGED CRACKED HOLES TO THE LIMITATIONS CONTAINED ON SR DRAWING 5894377 & CRACK WAS NOT REMOVED. REMOVED O/B FITTING STA 97 SDR DHL9980209CSeat Track · corrodedC-CHECK, SEAT TRACK NR 1 STA 980-1080 TRACK IS CORRODED. CUT OUT DAMAGED SECTIONS OF TRACK NR 1 STA 1100 IAW DC-8 SRM 53-2-3 FIG 6D SHEET 1-3. CLEANED REWORKED AREA PER SRM 51-1-8 PAR 6A. TREATED & PRIMED REWORKED AREA IAW DC-8 SRM 51-1-8 PG 13 & 16. INSTASDR DHL9980208CSeat Track · corrodedC-CHECK, SEAT TRACK NR 1 BETWEEN STA 880-980 TRACK WAS CORRODED. CUT OUT DAMAGED SECTION OF TRACK NR 1 AT STA 920 AND CLEANED AREA OF TRACK BETWEEN STA 880-980 IAW DC-8 SRM 53-2-3 FIG 6D SHEET 1 & 51-1-8 PARA 6A. OK TO TREAT AND PRIME REWORKED AREA IAW DC-8 SDR DHL9980205CSkin · crackedC CHECK, NONROUTE ENG #4 INSIDE CENTER PYLON SECTION GENERATOR FEEDER CABLE SUPPORT HAD CRACK DAMAGE ON SURFACE. REMOVED GENERATOR FEEDER CABLE SUPPORT AS PER DC8 MM 20-50-1. CUT OUT CRACKED AREAS FROM PANEL AT NR 4 PYLON CENTER AREA IAW DC8 SRM 3-2-0 FIG 23SDR DHL9980263CSeat Track · wornC-CHECK, SEAT TRACK NR 3 BETWEEN STA 400-440 TRACK WORN. REMOVED (2) DAMAGED, FOUR HOLES CARGO TRACK REPAIR FROM NR 3 SEAT TRACK STA 400-440 IAW DC-8 SRM 51-3-0 PAR 1 & 2. CLEANED REPAIRED AREA PER SRM 51-1-8 PAR 6A. TREATED & PRIMED AREA IAW DC8 SRM 51-1-8SDR DHL9980262CSeat Track · wornC-CHECK, SEAT TRACK NR 3 BETWEEN STA 320-340 TRACK WORN. CUT OUT DAMAGED SECTION OF SEAT TRACK NR 3 BETWEEN STA 310 TO 370 & PREPARED NEW SECTION FROM APPROPIATED MATCHING SECTION OF TRACK & FABRICATED SPLICE FROM 7075-T6 0.100 (1 X 13) 0.125 (1 X 7) 0.160 (1SDR DHL9980261CSeat Track · wornC-CHECK, SEAT TRACK NR 4 BETWEEN STA 1300-1320 TRACK WORN. CUT OUT DAMAGED SECTION OF SEAT TRACK NUMBER 4 BETWEEN STA 1290-1350 & PREPARED NEW SECTION FROM APPROPRIATED MATCHING SECTION OF TRACK & FABRICATED SPLICES FROM: 7075-T6 0.100 (1 X 7) 0.160 (1 X 8) ISDR DHL9980260CSeat Track · wornC-CHECK, SEAT TRACK NR 4 BETWEEN STA 221-260 TRACK WORN. CUT OUT DAMAGED SECTION OF SEAT TRACK NR 4 BETWEEN STA 210-250 & PREPARED NEW SECTION FROM APROPRIATE MATCHING SECTION OF TRACK & FABRICATED SPLICES FROM 7075-T6 1000 (1 X 13) 0.125 (1 X 7) 0.160 (1 X 8SDR DHL9980259CSeat Track · wornC-CHECK, SEAT TRACK NR 4 BETWEEN STA 270-290 TRACK WORN. CUT OUT DAMAGED SECTIONS OF TRACK NR 4 STA 280-290 IAW DC-8 SRM 53-2-3 FIG 6D SHEET 1-3. CLEANED REWORKED AREA PER SRM 51-1-8 PAR 6A. TREATED & PRIMED REWORKED AREA IAW DC-8 SRM 51-1-8 PG 13 & 16. INSDR DHL9980258CSeat Track · wornC-CHECK, SEAT TRACK NR 4 BETWEEN STA 300-340 TRACK WORN. CUT OUT DAMAGED SECTION OF SEAT TRACK NR 4 BETWEEN STA 310-370 & PREPARED NEW SECTION FROM APPROPIATED MATCHING SECTION OF TRACK & FABRICATED SPLICES FROM 7075-T6 0.100 (1 X 13), 0.125 (1 X 7) 0.160 (1 SDR DHL9980253CSkin · delaminatedC-CHECK, LT WING NR 1 FLAP VANE HAS DELAMINATED AREA DOT 53901. REMOVED NR 1 FLAP VANE FROM I/H WING IAW DC-8 MM 27-51-14. SENT TO STOCKROOM. INSTALLED NR 1 FLAP VANE I/H WING IAW DC-8 M/M 27-51-14 PG 201, 203 PAR 2B. PENDING OPS CHK PERFORMED, OPS CHK NORSDR DHL9980250CPanel · delaminatedC-CHECK, LT WING I/B AREA PANEL BELOW NR 2 SPOILER IS DELAMINATED. REMOVED DELAMINATED PANEL AT LT WING 8/B AREA LOWER SURFACE BELOW SPOILER NR 2 IAW DC-8 SRM 51-1-21 PG F1 P1. SEND DELAMINATED PANEL OUT TO BE REPAIR DRILLED SERVICEABLE PANEL PER DC-8 SRM 51SDR DHL9980249CPanel · crackedC-CHECK, LT WING ABOUT STA 162.263 T/E PANEL BEHIND REAR SPAR HAS A CRACK DOT 382618. STOP DRILLED END CRACK .25 DIAMETER IAW DER NR MHA-312A. FABRICATED DOUBLER REPAIR 7.5 X 9.5 2024T3 .050IAW DER NR MHA 3124. TREATED & PRIMED PER DC-8 SRM 51-1-8 PG 16 & 1SDR DHL9980248CAngle · crackedC-CHECK, ABOUT XCW 46.00 BELOW LT WING IS CRACKED DOT 382627. REMOVED DAMAGED ANGLE AT LT WING XW 46.00 IAW DC-8 SRM 51-1-21 PG 1 PAR 1. FABRICATED NEW ANGLE .071 2024T3 12 X 6 IAW DC-8 SRM 51-1-4 PG 1 PAR 1. TREATED & PRIMED PER DC-8.SDR DHL9980246CAngle · crackedC-CHECK, ABOUT XTS 6.000 BELOW LT WING IS A CRACK SEE MARK DOT 38262. REMOVED CRACKED ANGLE FROM WING ABOUT STA XRS 6.000 IAW DC-8 SRM 51-1-21 PAR 1 FIG 32. FABRICATED NEW ANGLE SAME MATERIAL & THICKNESS 2024-T3 0.050 (20 X 11) IAW DC-8 SRM 57-3-1 FIG 25. SDR DHL9980245CSeat Track · corrodedC-CHECK, SEAT TRACK NR 7 BETWEEN STA 299.200 CORROSION SPUTS ON TRACK. CUT OUT DAMAGED SECTION OF TRACK NR 7 AT STA 273 & CLEANED AREA OF TRACK BETWEEN STA 299-200 IAW DC-8 SRM 53-2-3 FIG 6D SHEET 1 THRU 3, 51-1-8 PAR 6A. TREATED & PRIMED REWORKED AREAS IAW SDR DHL9980244CCowl · crackedC-CHECK, NR 1 ENGINE NOSE COWL L/E INTERIOR AT 10 O'CLOCK POSITION INTERNAL LIP FLANGE IS CRACKED D20EN4. ACCOMPLISHED ENG NR 1 NOSE COWL ANTI-ICE DEFLECTOR REPAIR BY TRIMMING CRACKED SECTION IAW SB 71-105 FIG 2. TREATED AREA OF TRIMMED DEFECTOR PER DC-8 SRMSDR DHL9980243CSeat Track · wornC-CHECK, NONROUTINE SEAT TRACK NR 6 BTWN STA 220-260 TRACK HOLES WORN & SOME ELONGATED. CUT OUT DAMAGED SECTION OF TRACK NR 6 BETWEEN STA 170 TO 310 & PREPARED NEW SECTION FROM APPROPRIATE MATCHING SECTION OF TRACK & FABRICATED SPLICES FROM 7075-T6 0.100 (1 XSDR DHL9980242CSeat Track · wornC-CHECK, BETWEEN STA 1560-1600 SEAT TRACK NR 5 IS WORN. CUT OUT DAMAGES SECTION OF NR 5 SEAT TRACK AT STA 1563 IAW DC-8 SRM 53-2-3 FIG 6D SHEET 1 THRU 3. CLEANED REWORKED AREA PER SRM 51-1-8 PAR 6A. TREATED & PRIMED REWORKED AREA IAW DC-8 SRM 51-1-8 PG 13, SDR DHL9980241CFrame · crackedC-CHECK, UPPER CARGO COMPT AT STA 1600 CIRCUMFERENTIAL FRAME AT CUSP LINE IS CRACKED RT SIDE. CUT OUT CRACKED SECTION OF FRAME AT FS 1580 RT CARGO CABIN IAW DC-8 SRM 53-2-0 FIG 2. FABRICATED NEW SECTION OF FRAME: 7075-0 0.080' (6 X 2.5) & SPLICE FROM 7075.0 SDR DHL9980240CSeat Track · wornC-CHECK, SEAT TRACK NR 6 BTWN STA 415 - 420 TRACK HOLES WORN. REMOVED (2) DAMAGED, FOUR HOLES CARGO TRACK REPAIR FROM NR 6 SEAT TRACK STA 415-420 IAW DC-8 SRM 51-3-0 PAR 1 & 2. CLEANED REPAIR AREA PER SRM 51-1-8 PAR 6A. TREATED & PRIMED AREA IAW DC-8 SRM 51SDR DHL9980239CFairing · crackedC-CHECK, RT WING FLAP HINGE FAIRING AT STA 340 CRACKED IN 2 PLACES, DOT 450 ON RACK E4. STOP DRILLED END CRACK AT RT WING FLAP HINGE FAIRING IAW DC-8 SRM 51-3-2 PG 1 PAR 1. FABRICATED DOUBLER REPAIR 2024 T3.063 4 X 2.5 IAW DC-8 SR 51-1-4 PG 1 PAR 1. TREATEDSDR DHL9980238CSeat Track · crackedC-CHECK, SEAT TRACK NR 1 BETWEEN STA 1280-1380 TRACK CORRODED. CUT OUT DAMAGED SECTION OF TRACK NR 1 BETWEEN STA 1350 TO 1370 & PREPARED NEW SECTION FROM APPROPRIATED MATCHING SECTION OF TRACK & FABRICATED SPLICES FROM 7075-T6 0.100 (1 X 13), 0.125 (1 X 7), 0SDR DHL9980213CBracket · crackedC-CHECK, BELOW LT WING ABOUT X 46.000 STA 880 BRACKET CRACKED. REMOVED CRACKED BRACKET FROM LT WING AT STA 880 IAW DC-8 SRM 51-1-20D & 51-1-21 PAR 1. FABRICATED NEW BRACKET SAME MATERIAL & THICKNESS 2024-T3 0.0063 DC-8 SRM 53-8-3 FIG 2. CLEANED BRACKET ARESDR DHL9980212CTr Cowl · crackedC-CHECK, NR 1 ENGINE PYLON LT AFT REVERSER COWL UPPER AFT AREA FOUND CRACK ON U-CHANNEL ANGLE. REMOVED CRACKED U-CHANNEL ANGLE AT ENG NR 1 LT AFT REVERSER COWL IAW DC-8 SRM 51-1-21A PG 1 PARA 1. FABRICATED NEW U ANGLE 5.5 X 1.375. 301 STAINLESS .25 HARD 0.20SDR DHL9980210CSpar · crackedC-CHECK, PYLON FAIRED AREA INBOARD NR 1 PYLON FWD SPAR CAP HAD TWO INCHES & PROGRESSING PREVIOIUSLY STOP HOLE. DOT 382844. REMOVED 2 FASTENERS FOR ACCESS TO NDT AT PYLON NR 1 FWD SPAR CAP IAW DC-8 SRM 51-3-0 FIG 52A. REMOVED NR 1 DC-8 SRM 51-1-20 PAR 8 MM 2SDR DHL9980207CFitting · crackedC-CHECK, RUDDER I/E INTERIOR, FITTING CRACKED. MARKED STA ZR 105 DOT 327. STOP DRILLED END CRACK 1/4 PR DC-8 SRM 55-2-0 PAGE 7 FIG 2. FABRICATED ANGLE REPAIR 063 2024T3 7 X 1 1/2 X 1/2 IAW DC-8 SRM 55-2-0. TREATED & PRIMED PER DC8 SRM 51-1-8 PAGE 16 AND 13 SDR DHL9980206CStiffener · crackedC-CHECK, RUDDER L/E INTERTIOR STIFFENER CRACKED, MARKED STA ZR DOT 3211. REMOVED STIFFENER FROM RUDDER L/E INTERIOR AT STA ZR 105 IAW. CLEANED DAMAGED AREA, NO CRACKS FOUND AFTER DYE PENETRANT TEST IAW NDT SPM PART 8. TREATED & PRIMED STIFFENER. OK TO INSTSDR UPS99829572Longeron · corrodedINSPECTION TYPE:C2 LONG 36 FLANGE AT FS 1360 IS CORRODED BEYOND LIMITS. REPAIRED LONGERON 36 IAW DHC SK880-514.
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