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 UPS05845340Skin · crackedRT WING LE UPPER SKIN IS CRACKED AT XFS 580.000. CUT OUT DAMAGE, FABRICATED, AND INSTALLED REPAIR IAW DC-8 SRM 57-2-1 FIG 33.SDR UPS05845339Skin · corrodedLT WING LE UPPER SKIN IS CRACKED IB OF XFS 710.000. NO CRACK NOTED, FOUND TO BE CORROSION, CUT OUT DAMAGE, FABRICATED, AND INSTALLED REPAIR IAW DC-8 SRM 57-2-1 FIG 38.SDR UPS05845335Skin · corrodedRT WING LE UPPER SKIN HAS INTERGRANULAR CORROSION AT XFS 766.250. CUT OUT DAMAGE, FABRICATED, AND INSTALLED REPAIR IAW DC-8 SRM 57-2-1 FIG 38.SDR UPS05845334Skin · crackedRT WING LE SKIN IS CRACKED AT FASTENER HOLE XFS 666.250. CUT OUT DAMAGE, FABRICATED, AND INSTALLED REPAIR IAW DC-8 SRM 57-2-1.SDR UPS05845333Rib · crackedRT WING LE UPPER RIB IS CRACKED AT XFS 753.750. STOP DRILLED CRACK, FABRICATED, AND INSTALLED REPAIR IAW DC-8 SRM 57-2 -0 FIG 2.SDR UPS05845332Rib · crackedRT WING LE UPPER RIB IS CRACKED AT XFS 635.000. STOP DRILLED CRACK, FABRICATED, AND INSTALLED REPAIR IAW DC-8 SRM 57-2 -0 FIG 2.SDR UPS05845331Rib · crackedRT WING LE UPPER RIB IS CRACKED AT XFS 622.500. STOP DRILLED CRACK, FABRICATED, AND INSTALLED REPAIR IAW DC-8 SRM 57-2 -0 FIG 2.SDR UPS05845330Rib · crackedRT WING LE UPPER RIB IS CRACKED AT XFS 566.250. STOP DRILLED CRACK, FABRICATED, AND INSTALLED REPAIR IAW DC-8 SRM 57-2 -0 FIG 2.SDR UPS05845329Rib · crackedLT WING LE LOWER RIB IS CRACKED AT XFS 622.500. STOP DRILLED CRACK, FABRICATED, AND INSTALLED REPAIR IAW DC-8 SRM 57-2 -0 FIG 2.SDR UPS05845328Rib · crackedLEFT WING LE LOWER RIB IS CRACKED AT XFS 735.000. STOP DRILLED CRACKED, FABRICATED, AND INSTALLED REPAIR IAW DC-8 SRM 57 -2-0 FIG 2.SDR UPS05845327Rib · crackedLT WING L/E LOWER RIB IS CRACKED AT XFS 772.500. CRACK EXTENDS FROM EDGE TO FASTENER HOLE, FABRICATED, AND INSTALLED REPAIR IAW DC-8 SRM 57-2-0 FIG 2.SDR UPS05845326Rib · crackedLEFT WING L/E LOWER RIB IS CRACKED AT XFS 785.000. STOP DRILLED CRACK, FABRICATED, AND INSTALLED REPAIR IAW DC-8 SRM 57-2 -0 FIG 2.SDR UPS05845325Rib · crackedC3 LT WING L/E LOWER RIB CRACKED AT XFS 822.500. STOP DRILLED CRACK, FABRICATED, AND INSTALLED REPAIR IAW DC-8 SRM 57-2 -0 FIG 2.SDR UPS05845324Doubler · crackedC3 RT LE LWR INNER DOUBLER CRACKED AROUND DRAIN HOLE (2 EA CRACKS). REMOVED, FABRICATED, AND INSTALLED INNER DOUBLER IAW DC-8 SRM 51-1-21 AND DWG 5769600.SDR DHL2005806513Web · crackedRUDDER WEB LWR PART CRACKED .5 INCH STA ZR. 61.156. PERFORMED MAJOR REPAIR. REMOVED CRACKED RIB WEB IAW SRM 51-1-21 PG 1. FABRICATED NEW RIB WEB, 2EA DOUBLERS AND 2EA COVERS. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. APPLIED SEALANT TO FAYING SURFSDR UPS05845542Skin · crackedINSPECTION TYPE: C3, LT WING UPPER SURFACE CRACKED AT XRS 22.750. CUT OUT DAMAGE, FABRICATED, AND INSTALLED REPAIR IAW SAA SK 801-804078 A.SDR UPS05845493Door Frame · crackedINSPECTION TYPE: C3, D-PIT DOOR FWD UPPER CORNER CRACKED 1/2" LONG. CUT OUT DAMAGE, FABRICATED, AND INSTALLED REPAIR IAW DC-8 SRM 53-2-0 FIG 21.SDR UPS05845492Doubler · crackedRT WING LWR SURFACE DOUBLER CORRODED AND POSSIBLE CRACK AT XW 408.343 AFT SIDE AROUND FASTENER HOLE. NDT DETECTED A 1/2" CRACK EXTENDING FROM FASTENER HOLE TO EDGE OF PART. CUT OUT DAMAGE, TREAT, AND PRIMED IAW SAA SK 801-804073.SDR UPS05845391Skin · crackedINSPECTION TYPE: C3, FUSELAGE SKIN CRACKED .5 INCH LONG AT FS 1746 L15L. REMOVED DAMAGED AREA, FABRICATED, AND INSTALLED REPAIR IAW DC-8 SRM 53 -2-1.SDR DHL2005806509Skin · damagedLT WING O/B AILERON LWR SKIN RIVETS SHEARED, XA 722 - XA 752 (PLATING DAMAGED). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1, SRM 57-8-1 FIG 4, DOUGLAS DWG 5763133. REMOVED DAMAGED PANEL PLATING IAW SRM 57-1-0 PG 1, SRM 51-1-21. FABRICATED NEW PANEL AND BONDESDR UPS05845260Mechanism · stuckF/O'S EMERG (CLEAR VIEW, DV WINDOW) WILL NOT OPEN. CLEANED AND LUBED F/O'S WINDOW SLIDE MECH. OPS CK NORMAL.SDR DHL2005806505Splice · crackedLT INNER WING OB EXTENDED L/E SLOT SPLICE CRACKED 10 IN STA XFS 207.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG. 1, SRM 57-3-3 FIG. 3 SHEET 1. REMOVED CRACKED SPLICE IAW SRM 57-1-0 PG. 1, SRM 51-1-21, SRM 51-1-20D. FABRICATED NEW SPLICE IAW SRSDR DHL2005806511Floorbeam · corrodedAFT CARGO COMPT FLOORBEAM LWR FLANGE CORRODED, STA 1240.000 RBL 30" (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 51-2-1 FIG 1 SHEET 9, TR 51-130. REMOVED FASTENERS IAW SRM 51-1-20D. REMOVED CORROSION FROM FLOORBEAM LWR FLANGE, STA 1240.000 RBL 30" IAW SRMSDR DHL2005806533Access Door · corrodedRT OUTBOARD AILERON COUNTERWEIGHTS ACCESS DOOR INTERIOR CORRODED STA XA 615.000 - 630.000. REMOVED CORROSION FROM ACCESS DOOR IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-0 PG 16. REMOVED ACCESS DOOR IAW SRM 57-1-0, 51-3-0. FABRICATED NEW ACCESDR DHL2005806506Angle · crackedLEFT MLG W/W REINFORCING ANGLE CRACKED 1 INCH (STA 946.000 - XCW 69.500). REMOVED CRACKED REINFORCING ANGLE IAW SRM 51-1-21, SRM 51-3-0, SRM 57-1-0. FABRICATED NEW REINFORCING ANGLE (AL2024T3 0.040") IAW SRM 57-2-0 PG 1, SRM 51-1-4 PG 1. CLEANED, TREATED ANSDR DHL2005806504Stiffener · crackedREF. NR. 041519) FWD ACCY COMPT RT PRESSURE BULKHEAD STIFFENER CRACKED 1 AT STA 8.000. REMOVED CRACKED STIFFENER IAW SRM 51-1-21, SRM 51-1-20D. FABRICATED NEW STIFFENER (AL7075 INCH 0 INCH 0.071INCH) IAW SRM 53-3-3 FIG. 3. HEAT TREATED IAW SRM 51-1-1 PG. 1,SDR DHL2005806507Strap · crackedRIGHT WING CTR L/E INTERNAL SPLICE STRAP CRACKED 12 INCHES XW 257.500 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1, SRM 57-3-3 FIG 3 SHEET 3. REMOVED SPLICE STRAP DAMAGED IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 21. FABRICATED NEW SPLICE STRAP (ASDR DHL05805002Fan · failedLT PACK TRIP LIGHT COME ON ON THE GROUND AND LIGHT SMOKE IN COCKPIT, DEFERRED LT AC PACK PER MEL 21-38 CAT C SPECIAL PROCEDURE 21-38 CW A/C RESTRICTED TO FL 250 PLACARD INST DMI 22107. LT PACK TRIP LIGHT CAME ON ON THE GROUND & LIGHT SMOKE IN COCKPIT. R&R LTSDR DHL2005806502Frame · crackedRT WING CTR L/E FORMER UPPER PART CRACKED 0.250 INCH, STA XFS 416.500. PERFORMED STOP HOLE AND FABRICATED 2 THIN FORMED ANGLE DOUBLERS (AL7075T6 0.032 INCH) IAW SRM 57-2-0 PG. 9-10. CLEANED, TREATED AND PRIMED AREA AND 2 THIN FORMED ANGLE DOUBLERS IAW SRM 51-1SDR DHL2005806503Doubler · damagedINTERIM REPAIR ON RT OB FLAP UPPER PLATING (STA XF 208.000-213.000) (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG. 1, SRM 57-7-1 FIG. 4, TR NR 57-94. REMOVED PLATING WITH INTERIM REPAIR ON IT IAW SRM 51-1-21 PG. 1, SRM 51-3-0 PG. 1. FABRICATED NEW PSDR IXXA05SMN181SFrame · corrodedDURING ROUTINE C-CHECK INSPECTION, FWD CARGO CMPT FRAME CORRODED, STA 80.000, L-26L. PERFORMED MAJOR REPAIR. REMOVED FASTENERS. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED FRAME SEGMENT (CORRODED). PERFORMED NDT INSPECTION. NO CRACK, CORROSION FOUNDSDR IXXA05SMN180SFrame · crackedDURING ROUTINE C-CHECK INSPECTION, FWD ACCY CMPT- FRAME CRACKED, STA 55, L-24R. PERFORMED MAJOR REPAIR. REMOVED FASTENERS. TRIMMED OUT DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK CORROSION FOUND AROUND TRIMMED AREA. FABRICATED NEW SEGMENT FRAME (EXTSDR DHL2005806501Finger Doubler · corrodedCOCKPIT SUBFLOOR PRESSURE PANEL FINGER DOUBLER CORRODED (STA -67.000 TO -80.000). REMOVED CORROSION FROM FINGER DOUBLER IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. REMOVED CORRODED FINGER DOUBLER IAW SRM 51-1-21 PG 1. FABRICATED FINGSDR IXXA0500093OIndicator · reads highDURING CLIMB-OUT FROM KLRD TO KMEM, NR 1 EGT INDICATED TO 912 DEGREES. TEMP DECREASED AS THROTTLE WAS PULLED BACK. TEMP WAS AT 912 FOR APPROX 5 SECONDS, OAT WAS 34 DEGREES C, N1 SETTING 91.3% AND THE INDICATOR WAS FLASHING 912 DEGREES. THE CREW DIVERTED A/CSDR IXXA05SMN178SFitting · crackedDURING ROUTINE C-CHECK INSPECTION, AFT CARGO COMPT SPLICE FITTING CRACKED 6, STA 1260.000 STA 1280.000 L-34L. REMOVED CRACKED SPLICE FITTING IAW DC8 SRM 51.1.20D PAGE 21. CLEANED, TRETAED AREA IAW DC8 SRM 51-1-8B. INSTALLED NEW SPLICE FITTING IAW DC8 SRM 51SDR IXXA05SMN177SAccess Door · crackedDURING ROUTINE C-CHECK INSPECTION, RIGHT WING SLOT DOOR CRACKED 1, STA XILD 7095 XS 250.089. REMOVED AND REPLACED INBOARD SLOT UPPER DOOR (NEW CONDITION) ON RIGHT WING IAW DC-8 MM 27-80-02 PAGES 201-204.SDR IXXA05SMN176SSkin · crackedDURING ROUTINE C-CHECK INSPECTION, RIGHT WING UPPER SKIN CRACKED 1, STA XW 74 STR 9. PERFORMED MAJOR REPAIR. REMOVED FASTENERS IAW DC-8 SRM 51-1-20D PAGE 21. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION IAW DC-8 NDT SPM PART 06-10-01-001. FABRICATED REPSDR IXXA05SMN175SBeam · corrodedDURING ROUTINE C-CHECK INSPECTION, FWD ACCY CMPT BEAM CORRODED AT STA 50, RBL 4. PERFORMED MAJOR REPAIR. REMOVED FASTENERS. REMOVED CORROSION, FOUND OUT OF LIMITS. REMOVED CORRODED AREA. PERFORMED NDT INSPECTION IAW DC-8 NDT SPM, PART 06-10-01-001. NO CRSDR IXXA05SMN172SSkin · out of limitsDURING C-CHECK INSPECT, DOUBLER BEHIND D-PIT DOOR OPENING ON SKIN SPLICE, SIDES 2 AND 3 EXCEED MAX RIVET SPACING, ALUMINUM & JO-BOLTS IN LONGERONS. ADD ADDITIONAL RIVETS TO BRING UNDER MAX SPACING OF 1.400, STA FS 1520 L-29R. PERFORMED REPAIR IAW FAA FORM 81SDR IXXA05SMN170SSkin · damagedDURING C-CHECK INSPECT, RT FWD FUSELAGE BELOW FWD STATIC PORT, DOUBLER THICKNESS RATIO EXCEEDED MAX ALLOWED, ALUMINUM RIVETS USED IN LONGERONS. REWORK REPAIR IAW TO BRING INTO CONFORMANCE, STA FS 195, L-35R. PERFORMED MAJOR REPAIR IAW FAA 8110-3 NR 05367 DASDR IXXA05SMN179SFitting · crackedDURING ROUTINE C CHECK INSPECTION, AFT ACCY CMPT BATHTUB FITTING CRACKED 1, STA 1690.000, L-28R. REMOVED CRACKED FITTING IAW DC8 SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW DC8 SRM 51-1-8B. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D PG 9 AND DCSDR IXXA05SMN169SSkin · damagedDURING C-CHECK INSPECT, RT FWD FUSELAGE JUST FWD OF A-PIT DOOR OPENING DOUBLER THICKNESS RATIO EXCEEDED MAX ALLOWED. DOUBLER THICKNESS 0.135", SKIN 0.071". REWORK REPAIR TO BRING INTO SRM LIMITATIONS WITH LOCK FASTENERS IN LONGERONS, STA FS 255 L-36. PERFORMEDSDR IXXA05SMN168SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, FWD CARGO COMPT INTERNAL SKIN CORRODED, STA 80.000, L-31R. DURING ROUTINE C CHECK INSPECTION, FWD CARGO COMPT INTERNAL SKIN CORRODED, STA 80.000 , L-31R. REMOVED SKIN IAW DC-8 SRM 51-1-21 PAGE 1. REMOVED LEVEL I CORROSION SDR IXXA05SMN167SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FWD CARGO COMPT FITTING CRACKED .500 INCHES, STA 300.000 , L-32R L-33R. REMOVED CRACKED FITTING IAW DC-8 SRM 51-1-21 PAGE 1. CLEANED, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8B. INSTALLED NEW FITTING WITH FASTENERS (HILOSDR IXXA05SMN166SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FWD CARGO COMPT FITTING CRACKED .5 INCHES STA 340.000 , L-32R L-33R. REMOVED AND REPLACED CRACKED FITTING ON FWD CARGO CMPT, STA 340.000, L32R-L33R IAW DC8 SRM 51.1.20D PAGES 9, 21. TORQUED IAW DC8 SRM 51-3-1.SDR IXXA05SMN165SSkin · crackedDURING ROUTINE C CHECK INSPECTION, EXTERNAL FUSELAGE AFT HEAT EXCHANGER RT LWR CORNER CRACKED 1, STA 10.000, L-27L. PERFORMED MAJOR REPAIR IAW FAA 8110.3 NR 05367 DATED 08-19-05, SEMAN DWG ED 4055 DATED 08-14-03 AND EO SEMAN NR 20051140 DATED 08-19-05. REMOVSDR IXXA05SMN164SVane · damagedDURING C-CHECK INSPECT, LT WING, VANE SLOT L/E HAS INTERIM REPAIR, XOLDI 6.225. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 05368 DATED 08-19-05, DWG SEMAN ED-4054 DATED 08-15-05 AND EO SEMAN NR 20051136 DATED 08-19-05. REMOVED NON STANDARD REPAIR IAW DC8 SDR IXXA0500091OFiber Optic Gyro · inoperativeDURING CLIMB-OUT FROM KTOL PILOTS HSI/ADHI WAS INOP, INFORMATION WAS LOST. AFTER CREW RESET CIRCUIT BREAKERS ADHI RETURNED THEN WENT BLANK. CREW RETURNED AIRCRAFT TO KTOL AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 1 FOG. PERFORMEDSDR DHL2005801013Engine · failedENGINE FAILURE NR 1. R&R NR 1 ENGINE DRIVEN FUEL PUMP IAW DC8 MM 73-10-1. NO LEAKS NOTED. OPS CKS GOOD ON ENGINE RUN IAW MM 71-00 & ASTAR JRH. PARTS INFO ON LP 056593. EVIDENCE OF CORROSION REPORTED IN AREA OF 3 REMOVED FASTENERS L WING STATION 519.00. REF. ISDR IXXA0500090OIndicator · inoperativeDURING CLIMB-OUT FROM KTOL, PILOT'S HSI/ADHI WAS INOP. LOST ATTITUDE AND HEADING INFORMATION. CREW RETURNED AIRCRAFT TO KTOL AND LANDED WITHOUT INCIDENT. MAINTENANCE RESET EADI AND EHSI CIRCUIT BREAKERS. THE SYSTEM RETURNED TO NORMAL AND THE OPERATIONAL CH
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