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 UPS03840726Floorbeam · damagedINSPECTION TYPE: C-2, MAIN CABIN FLOORBEAM T-CAP FOUND BLENDED ON FROM AN EXISTING REPAIR STA 1620 LBL 48. FABBED REPAIR ANGLE IAW DC8 SRM 53-2-0 FIG 1B. ALODINED & PRIMED ANGLES IAW DC8 SRM 51-1-8. INSTALLED REPAIR ANGLES IAW DC8 SRM 51-1-20D.SDR DHL2003604561Frame · crackedLT WING CENTER L/E FORMER CRACKED 0.500 AT XFS 366.500. STOP DRILLED CRACK AT XFS 366.500 AND FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED ANGLE DOUBLER AND AREA IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER WITH NEW FASTENERS IAWSDR DHL2003604551Frame · crackedLT WING CENTER L/E FORMER CRACKED 0.500 AT XFS 354.000. STOP DRILLED CRACK AND FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED AREA AND ANGLE DOUBLER IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER WITH NEW FASTENERS IAW SRM 51-1-20D PSDR DHL2003604572Frame · crackedRT OUTER WING INBD L/E FORMER CRACKED 0.250 AT XFS 597.500. STOP DRILLED CRACK AT XFS 597.500 AND FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9, 10. CLEANED, TREATED AND PRIMED AREA AND ANGLE DOUBLER IAW SRM 51-1-20D PG 9, SRM 51-1-21 PG 1.SDR DHL2003604566Frame · crackedLT WING CENTER L/E FORMER CRACKED 0.500 AT XFS 304.000. REMOVED FASTENERS IAW SRM 51-1-21 PG 1 AND FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9,10. CLEANED,TREATED AND PRIMED AREA AND ANGLE DOUBLER IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER WITH NEW FASTENERS IASDR UPS03840744Cap · crackedINSPECTION TYPE: C-2, RT HORZ STAB INBOARD BOX LOWER CAP CRACKED. REMOVED RT HORZ LEADING EDGE CAP LOCATED & DRILLED NEW FITTING IAW DC8 SRM 51-1-21 & 51-1-20D.SDR UPS03840691Battery Pack · dischargedEMERGENCY EXIT LIGHTS INOPERATIVE, FOUND ON PREDEPARTURE CHECK. REMOVED AND REPLACED EMERGENCY LIGHTS PER M/M 33-50-01. OPS CKS GOOD.SDR UPS03840689Battery Pack · dischargedON DEPARTURE THE EMERGENCY EXIT LIGHTS WERE DEAD, FOUND BATTERY PACK POWER LOW AFTER TIME OF CHARGER. NEED BATTERY PACK REPLACED. REMOVED & REPLACED EMERGENCY LIGHT BATTERY PACK IAW 33-60-00. LIGHT OPS CK GOOD.SDR DHL2003604644Skin · damagedRT WING OUTBOARD FLAP UPPER FWD PLATING HAS AN INTERIM REPAIR, AT STA XF 345.000 - XF 350.000 (MAJOR REPAIR). REMOVED FASTENERS, TRIMMED OUT THE DAMAGED SKIN SEGMENT IAW EODHL-030508, ED-3282. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED A NSDR DHL2003801071Fillet · delaminatedLT LWR FILLET 724 AT STA 779.000 INTERNAL SKIN DELAMINATED. REMOVED AND REPLACED LT LWR FILLET 724 AT STA 779.000 IAW SRM 51-3-0 PG 1.SDR DHL2003801070Panel · delaminatedLT LWR PANEL NR 723 AT STA 750.000 SHOWS DELAMINATED INTERNAL/EXTERNAL SKIN. REMOVED AND REPLACED LT LWR PANEL 723 AT STA 750.000 IAW SRM 51-3-0 PG 1.SDR DHL2003604652Skin · damagedLT WING OUTBOARD FLAP LOWER SKIN SHOWS INTERIM REPAIR BETWEEN STA XF 415.000 AND XW 408.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW EODHL-030502, ED-3379. REMOVED FASTENERS IAW SRM 51-1-21 PG 1, SRM 51-1-21A PG 4. REMOVED DAMAGED SKIN PANEL IAW EODHL-030SDR DHL2003604615Skin · corrodedLT OUTER WING IB L/E CORRODED AT STA. XFS.710.000. PERFORMED MAJOR REPAIR IAW EODHL-030509, ED-3314. REMOVED FASTENERS. REMOVED CORROSION IAW SRM 51-1-8 PG.17-18. FOUND OUT OF LIMITS IAW SRM 57-2-1 PG.11-12. TRIMMED OUT CORRODED SKIN AREA IAW EODHL-030509, EDSDR DHL2003604655Plate · dentedRT OTBD FLAP LOWER PLATING HAS SEVERAL DENTS BETWEEN, STA. XF 415.000 AND XW 408.000. PERFORMED MAJOR REPAIR IAW EODHL 030512, ED-3382. REMOVED FASTENERS IAW SRM 51-1-21 PAGE1, SRM 51-1-21A PAGE4. REMVOED DAMAGED SKIN PANEL IAW EODHL 030512, ED-3382. CLEANED SDR DHL2003604665Skin · damagedLT WING INBD FLAP UPPER PLATING SHOWS INTERIM REPAIR BETWEEN STA XW 91.000 AND XW 75.500. PERFORMED MAJOR REPAIR IAW EO DHL 030506, ED 3280. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. TRIMMED OUT THE DAMAGED SKIN SEGMENT IAW EO DHL 030506, ED 3280. CLEANED, TSDR DHL2003604708Fitting · crackedMAIN CARGO COMPT BATHTUB FITTING AT STA 680.000 L-6R WITH 1.500 CRACK IN IT. PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1, SRM 51-1-20D PG 9, 21, SRM 51-1-21 PG 1. REMOVED CRACKED BATHTUB FITTING IAW SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW SRSDR DHL2003604605Skin · corrodedLT WING CTR L/E UPPER SKIN SHOWS INTERIM REPAIR & CORROSION BETWEEN STA XFS 360.250 AND XFS 379.000. REMOVED FASTENERS AND INTERIM REPAIR. REMOVED CORROSION, FOUND OUT OF LIMITS. TRIMMED OUT DAMAGED AREA. PERFORMED EDDY CURRENT INSPECTION. CLEANED, TREATESDR DHL2003604646Skin · damagedRT HORIZONTAL STAB INTERIM REPAIR ON INBD L/E XFS 178.750. PERFORMED MAJOR REPAIR IAW EODHL-030504, ED-3275. REMOVED FASTENERS, EXISTING INTERIM REPAIR AND FILLER IAW SRM 51-1-21 PG 1. TRIMMED OUT DAMAGED AREA IAW EODHL-030504, ED-3275. CLEANED, TREATED ANSDR DHL2003604593Plate · wornRT WING OTBD FLAP FWD UPPER PLATING WORN ON TWO AREAS BETWEEN STA XF 213.000 TO XF 201.500 (MAJOR REPAIR). REMOVED FASTENERS. TRIMMED OUT THE DAMAGED SKIN SEGMENT IAW EODHL-030507, ED-3281. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED A NEWSDR DHL2003604579Intercostal · crackedLT WING T/E INTERCOSTAL WITH 2.000 CRACK IN IT AT STA. XRS.74.000. STOP DRILLED CRACK AND FABRICATED DOUBLER (2024-T3 0.040) IAW SRM 57-2-0 FIG.2. CLEANED, TREATED AND PRIMED AREA AND DOUBLER IAW SRM 51-1-8B. INSTALLED DOUBLER IAW SRM 51-1-21 PG.1.SDR DHL2003801074Landing Gear · hung upWHEN SELECTING EMERGENCY, LT GEAR HANGS UP FOR 3 SECONDS AND DOES NOT RELEASE PROPERLY. PERFORMED ADJUSTMENT AND TEST OF LT MLG MECH CONTROL SYSTEM IAW MM 32-31-0 PG 201. OPS CHECKED LANDING GEAR IN NORMAL AND EMERGENCY GOOD IAW MM 32-30-0 PG 201.SDR DHL2003604550Skin · damagedINTERIM REPAIR ON LOWER SURFACE OF LT OUTBOARD FLAP BETWEEN XF 309.000 AND XF 333.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1, SRM 57-7-1 FIG 4. REMOVED LOWER SKIN OF LT OUTBOARD FLAP WITH INTERIM REPAIR (XF 309.000 - XF 333.000) IAW SRM 5SDR DHL2003604530Frame · crackedUPPER CARGO DOOR FORMER INNER SKIN CRACKED 1.000 AT STA 220.000, L-6,L-7L. REMOVED DAMAGED AREA FROM MAIN CARGO DOOR FORMER INNER SKIN AND FABRICATED FILLER AND DOUBLER IAW SRM 53-2-0 FIG 1D. CLEANED, TREATED AND FABRICATED AREA IAW SRM 51-1-8B. INSTALLED FILLSDR DHL2003604531Frame · crackedRT WING CTR L/E FORMER LOWER PORTION CRACKED 1.000, STA XS.466.651. STOP DRILLED CRACK AND FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED AREA AND ANGLE DOUBLER IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER ON RT WING CTR L/E FORMER LWSDR UPS03840742Longeron · crackedINSPECTION TYPE: C-2, AFT FUSELAGE EMPENNAGE AREA FS 1766-1806 LONG 17L IS CRACKED. REMOVED CRACKED LONG 17L AND END FITTING AND REPLACED WITH NEW LONG 17L AND END FITTING IAW DC8 SRM 51-1-20D & 51-1-21. FABBED AND INSTALLED REPAIR ANGLE AND FILLER IAW DC8 SDR UPS03840741Longeron · crackedINSPECTION TYPE: C-2, AFT FUSELAGE EMPENNAGE AREA FS 1766 - 1806 LONG 17R IS CRACKED. REMOVED L17R AND END FITTING TO FOM. ALODINED & PRIMED IAW DC8 SRM 51-1-8. INSTALLED L17R & END FITTING IAW DC8 SRM 51-1-21/51-1-20D.SDR DHL2003801072Pin · brokenUPPER CARGO DOOR NR 4 LOCKPIN CRANK ASSY BROKEN. REMOVED CRANK ASSY ON NR 4 LOCKPIN (UPPER CARGO DOOR) IAW OHM 52-3-10 PG 1, 2, 8, 11, 17 AND 18.SDR UPS03840659Skin · crackedRT INBD FLAP INBD WEB CRACKED. REMOVED ONE AREA OF CRACKED SKIN. D. RIEKE. 75838 5-8-03. REMOVED WEB. FABRICATED NEW WEB FROM 2024-T3 .040" PER SAMPLE. STARTED DRILLING NEW WEB. J. DUNLAP 26402 05-09-03. INSTALLED NEW WEB AND STIFFNERS IAW EO DC-8 5750-18733SDR DHL2003604684Door Frame · crackedAFT UPPER CORNER OF RT AFT SERVICE DOOR JAMB WITH 2 CRACKS 1.000 APPROX IN IT. PERFORMED MAJOR REPAIR IAW SRM 53-2-0 FIG 16 SHEET 4, TR 53-131, DWG 5750776, DWG SR08530021. CUT OUT DAMAGED AREA AND FABRICATED, FILLER (7075-T6 AL0.032) (7075-T6 AL0.080) AND (SDR DHL2003604565Skin · damagedRT WING INBD FLAP UPPER PLATING HAS INTERIM REPAIR FROM XW 104.000 TO XW 115.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1, SRM 57-7-1 FIG 1. REMOVED PLATING WITH INTERIM REPAIR IAW SRM 51-1-21 PG 1, SRM 51-3-0 PG 1. FABRICATED NEW PLATING SDR DHL2003801017Panel · delaminatedLT WING UPPER SURFACE- LT NR 2 SPOILER UPPER AND LWR SKIN DELAMINATED. REMOVED DELAMINATED LT NR 2 SPOILER IAW MM 27-61-1 PG 201-206. CLEANED AFFECTED AREA IAW SRM 51-1-9 PG 1. FABRICATED PLUG AND DOUBLER (ALUMINUM SPLICE CORE) (7075-T6 AL0.016) IAW SRM 57-SDR DHL2003604683Door Frame · crackedA 1.000 CRACK IN FWD UPPER CORNER OF FWD SERVICE DOOR JAMB. PERFORMED MAJOR REPAIR IAW SRM 53-2-0 FIG 14 SHEET 3, TR 53-127, DWG 5750776, DWG SR08530021. CUT OUT DAMAGED AREA; FABRICATED (2) FILLERS (7075-T6 AL0.050) (7075-T6 AL0.063) AND (2) DOUBLER (7075-TSDR DHL2003604577Skin · delaminatedRT WING NR 4 SPOILER EXTERNAL SKIN DELAMINATED. CUT OUT DAMAGED AREA IAW SRM 57-2-3 PG 14 PARAGRAPH 6B. FABRICATED PLUG AND DOUBLER IAW SRM 51-1-9 PG 4 PARAGRAPH 4. CLEANED IAW SRM 51-1-9 PG 1, PARAGRAPH 1. BONDED AND CURED IAW SRM 51-1-9 PG 2, PARAGRAPH 2. FOSDR UPS03840740Fitting · crackedINSPECTION TYPE: C-2, NR 56 STRINGER HAS AFT STRINGER END FITTING CRACKED, NR 4 ALT. REC'D NEW FABBED FITTING, ALODINED AND PRIMED IAW DC8 SRM 51-1-8. DRILLED, LOCATED AND DEBURRED NEW FITTING IAW DC8 SRM 51-1-24. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20DSDR DHL2003801068Panel · delaminatedLT WING TO FUSELAGE UPPER FILLET NR 706 INTERNAL SKIN DELAMINATED (STA 912.000-980.000). REMOVED AND REPLACED LT WING TO FUSELAGE UPPER FILLET NR 706 (STA 912.000-980.000) IAW SRM 51-1-21 PG 1.SDR DHL2003604539Doubler · crackedLT OUTER WING IB L/E LWR DOUBLER CRACKED 2.000, XFS.597.500. REMOVED DAMAGED DOUBLER IAW SRM 51-1-21 PG.1. FABRICATED NEW DOUBLER (7075-T6 AL 0.080) IAW SRM 57-1-0 PG.1, SRM 57-3-3 PG.16. CLEANED, TREATED AND PRIMED AREA AND DOUBLER IAW SRM 51-1-8B. INSTALLED SDR UPS03840739Cap · crackedINSPECTION TYPE: C-2, LT HORZ STAB INBOARD BOX INSTALLATION FWD LOWER TEE CAP CRACKED AT OUTBOARD END STA XFS 47. REMOVED LT HORZ STAB INBOARD BOX T-CAP, REC'D NEW FITTING LOCATED, DRILLED NEW FITTING IAW DC8 SRM 51-1-24. INSTALLED NEW FITTING IAW DC8 SRM 5SDR UPS03840738Cap · crackedINSPECTION TYPE: C-2, RT HORIZONTAL STAB INBD BOX INSTALLATION FWD LOWER TEE CAP CRACKED AT OUTBOARD END STA XFS 47. PERFORMED E/C INSP OF LOWER TEE CAP IAW NDT SPM 06-10-01.001 CRACKED AT RADIUS. REMOVED ANGLE LOCATED AND DRILLED NEW ANGLE IAW DC8 SRM 5 1-SDR UPS03840725Attach Fitting · corrodedINSPECTION TYPE: C-2, MAIN CABIN CORRODED FITTING CENTER WING BOX TO SHEAR WEB ATTACH FITTING STA 920 RBL 66 APX. REMOVED AND REPLACED FITTING AND INSTALLED IAW DC8 SRM 51-3-2 AND 51-1-20D.SDR UPS03840724Fitting · corrodedINSPECTION TYPE: C-2, MAIN CABIN CORRODED FITTING CENTER WING BOX TO SHEAR WEB ATTACH FITTING STA 920 RBL 66 APX. REMOVED AND REPLACED FITTING AND INSTALLED IAW DC8 SRM 51-3-2 AND 51-1-20D.SDR UPS03840722Fitting · corrodedINSPECTION TYPE: C-2, MAIN CABIN - FLOORBEAM TO FUSE ATTACHMENT FRAME STA 915 RBL 66 APX CORRODED. REMOVED CORROSION ON FRAME FITTING, OUT OF LIMITS IAW DC8 SRM 53-2-0 FIG 1F. REMOVED FITTING, LOCATED, DRILLED, AND DEBURRED FITTING IAW DAC DWG 5643483. INSDR DHL2003801073Beam · crackedUPPER CARGO DOOR LOCK PINS MECH BEAM CRACKED 1.000 INCH AT STA 230.000. REMOVED AND REPLACED DAMAGED BEAM AT STA 230.000 AND SECURED WITH BOLTS AND RIVETS IAW SRM 51-1-21 PG 1, SRM 51-3-1 PG 2A.SDR DHL2003604502Panel · delaminatedRT WING UPPER SURFACE - NR 708 FILLET OUTER SKIN DELAMINATED STA 980.000 - 1040.000. REMOVED AND REPLACED NR 708 FILLET ON RT WING UPPER SURFACE, STA 980.000 - STA 1040.000 IAW SRM 51-3-0 PG 1.SDR DHL2003604501Panel · delaminatedLT WING LWR SURFACE- LT NR 540 LWR ACCESS DOOR OUTER SKIN DELAMINATED FROM XS 475.000 - XS 507.000. REMOVED AND REPLACED LT LWR ACCESS DOOR NR 540 (STA 475.000 - 507.000) IAW SRM 51-3-0 PG 1.SDR UPS03840737Latch · crackedINSPECTION TYPE: C-2, C-PIT CROSS SLIDE DOOR LOWER JUST AFT OF CENTER LATCH HOOK CRACKED. REMOVED FASTENERS IN WEB IAW DC8 SRM 51-1-21 & 51-3-0 FOR ACCESS. REMOVED CRACKED LATCH HOOK IAW DC8 SRM 51-1-21. INSTALLED LATCH HOOK AND WEB IAW DC8 SRM 51-1-21, 51SDR DHL2003604559Attach Angle · crackedLT WING OUTBOARD STUB WING ATTACHING ANGLE CRACKED 1.000 AT XS 520.168. REMOVED CRACKED ATTACHING ANGLE ON LT WING OUTBOARD STUB WING AT XS 520.168 IAW SRM 51-1-21 PG 1. FABRICATED NEW ANGLE IAW SRM 57-2-0 PG 1. CLEANED, TREATED AND PRIMED NEW ANGLE AND ARESDR UPS03840736Door Frame · crackedINSPECTION TYPE: C-2, L2 LWR FWD DOOR JAMB CORNER, DOOR PAN AND DOOR SEAL CRACKED. REMOVED SEAL DEPRESSOR, DOOR PAN. FABBED REPAIR DOUBLER FOR DRAINPAN AND FABBED NEW SEAL DEPRESSOR. INSTALLED IAW DC8 SRM 51-1-21 AND 51-1-20D.SDR UPS03840735Door Frame · crackedINSPECTION TYPE: C-2, BS 50 - 54 S-21L CUSP FRAME CRACKED APPROX 4.5 INCH LONG. FABBED -31 FRAME IAW DAC DWG 5597646. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED -31 FRAME IAW DC8 SRM 51-1-21 & 51-1-20D.SDR UPS03840734Seat Track · wornINSPECTION TYPE: C-2, FWD PIT STA 320 LBL 27 FLOORBOARD, TRACK CORRODED. REMOVED CORROSION, WITHIN LIMITS IAW DC8 SRM 53-2-3. FOUND SCALLOP ON UPPER SURFACE WORN BEYOND LIMITS IAW DC8 SRM 53-2-3. REMOVED AND REPLACED TRACK SECTION IAW DC8 SRM 51-3-0, 53-2-SDR UPS03840733Skin · crackedINSPECTION TYPE: C-2, L2 DOOR JAMB UPPER AFT CORNER CRACKED 1 EA MARKED FOUND WITH NDT. FAB AND INSTALLED -11, -13 DOUBLERS AND -23 FILLER IAW DC8 SRM 53-2- 0 FIG 18. ALSO, INSTALLED INTERCOSTAL TO SKIN ATTACH ANGLE WEB AND 2 END FITTINGS AT APPROX L10L-L11
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