Douglas DC-8-73
Service difficulty reports · 821
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 = 'DC873' 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 = 'DC873' 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 DHL2001803549Pressure Panel · crackedNLG NOSE TUNNELS STRUCTURES SHOW 3 INCH CRACK ON FRAME NEAR STA 12 AND LONG 33 RT.SDR DHL2001803548Skin · damagedLT WING L/E SKIN EXHAUST GATE BROKEN APPROX 1.5 INCH. REMOVED DAMAGED SKIN PER SRM 51-1-21 PG 1. FABRICATED SKIN (2024-T3 0.032) PER SRM 57-2-1 FIG 1. CLEANED, TREATED AND PRIMED PER SRM 51-1-8B. INSTALLED NEW SKIN PER SRM 51-1-21 PG 1.SDR DHL2001803503Rib · brokenAT C CK; LH WING-CLOSING RIB BROKEN ON INBOARD AILERON RH LATERAL PART. REMOVED FASTNERS IAW SRM 51-1-21A, PG 1, CLEANED,TREATED AND PRIMED AREA IAW SRM 51-1-8B, FABRICATED AND INSTALLED DOUBLER IAW SRM 57-2-1, PAR. 1, SRM 51-1-21A, PG 1. REF: N/R 0616. SDR CLSDR DHL2001803502Angle · crackedAT C CK; FWD CARGO COMPT.- RH SHROUD ANGLE WITH 1/2" CRACK ON DOOR. REMOVED CRACKED ANGLE IAW SRM 51-1-21 PG 1, CLEANED,TREATED AND PRIMED AREA IAW SRM 51-1-8B, FABRICATED AND INSTALLED NEW ANGLE IAW SRM 51-1-21, PG 1. REF. N/R 1362. SDR CLOSED.SDR DHL2001803546Keelbeam · crackedRT MAIN LANDING GEAR WHEEL WELL KEEL BEAM INNER RIB SHOWS 1 INCH CRACK AT STA 920.SDR DHL2001803509Skin · crackedFUSELAGE EXTERNAL SKIN SHOWS CRACK (0.500 IN LENGTH) AT STA -13.000, L-1DR. CUT OUT DAMAGED SKIN PER SRM 53-2-1 FIG 7 SHEET 4.5. INSTALLED FILLER AND DOUBLER AND NEW FASTENERS PER SRM 51-20-20D PG 9.SDR DHL2001803507Structure · crackedTAIL CONE-RT ELEVATOR BRUSH COVER INNER STRUCTURE CRACKED 1.25. PERFORMED STOP HOLE PER SRM 53-2-0 FIG 1B. FABRICATED DOUBLER WITH ALCLAD (2420T3 0.025) PER SRM 53-2-0 FIG 1B. CLEANED, TREATED AND PRIMED PER SRM 51-1-8, INSTALLED DOUBLER PER SRM 53-20 FIG 1SDR DHL2001803506Cover · crackedAT C CK; RH HORIZONTAL STAB. CLOSING REAR SPAR COVER SHOWS 2", 1 1/2",2" AND 1" CRACKS FROM STA. XRS 179 TO XRS 221. REMOVED DAMAGED COVER IAW SRM 55-2-0 FIG 6, CLEANED,TREATED AND PRIMED AREA IAW SRM 51-1-8B, INSTALLED NEW COVER IAW SRM 55-2-0 FIG 6. REF: N/RSDR DHL2001803504Doubler · corrodedAT C CK; COCKPIT- FINGER DOUBLER SHOWS CORROSION STA. 8.000 THRU STA. 20.000, LBL 60, L-22L. REMOVED FASTNERS IAW SRM 51-1-21, PG 7, REMOVED CORROSION AT FINGER DOUBLER IAW SRM 51-1-8, PG 17-18, FOUND OUT OF LIMITS IAW SRM 53-2-0, PG 2, CLEANED,TREATED AND PRISDR DHL2001803505Door · crackedAT C CK; FWD CARGO COMPT.-AFT DOOR FWD UPPER CORNER CRACKED 1/4" AT STA. 520.000. CUTOUT DAMAGED AREA IAW SRM 53-2-0, FIG 20, CLEANED,TREATED AND PRIMED AREA IAW SRM 51-1-8B, FABRICATED AND INSTALLED FILLER AND DOUBLER IAW SRM 53-2-0, FIG 20, PG 141 & SRM 51-1SDR DHL2001803547Seat Track · wornMAIN CARGO COMPT - LUGS WORN ON CENTRAL TRACK AT STA 163.00 TO STA 62.000.REMOVED DAMAGED CTR TRACK (STA 62-163)PER SRM 51-3-0 PG 1.CLEANED TREATED AND PRIMED AREA PER SRM 51-1-8B.INSTALLED NEW TRACK PER SRM 57-3-0 PG 1 AND 51-3-1 PG 1SDR DHL2001803530Angle · brokenFWD CARGO COMPT- LINING SUPPORT ANGLE BROKEN AT STA 440, L-27L.SDR DHL2001803527Angle · crackedFWD CARGO COMPT - LINING SUPPORT ANGLE CRACKED (.25 INCH) AT STA 600, L-31L.SDR DHL2001803526Angle · crackedFWD CARGO COMPT- LINING SUPPORT ANGLE CRACKED 1 INCH AT STA 620, L-31R.SDR DHL2001803525Floor Support · crackedFWD CARGO COMPT- FLOOR SUPPORT ANGLE CRACKED 1.5 INCH AT STA 580, L-34R.SDR DHL2001803521Angle · crackedFWD CARGO LINING SUPPORT ANGLE SHOWS 2 EA 1.5 IN CRACKS BETWEEN L-33 TO L34 RT STA 480.000.SDR DHL2001803518Angle · crackedFWD CARGO COMPT-LINING SUPPORT ANGLE CRACKED (3/4 IN) AT STA 360.000 L-33L.SDR DHL2001803517Angle · crackedFWD CARGO COMPT LINING SUPPORT ANGLE CRACKED (1/2 IN) AT STA 100.00 L-31L.SDR DHL2001803516Floor Support · crackedFWD CARGO COMPT, FLOOR SUPPORT ANGLE CRACKED (O/B) 1.5 IN AT STA 560.00 L-35L TO L-35R.SDR DHL2001803515Floor Support · crackedFWD CARGO COMPT-FLOOR SUPPORT ANGLE CRACKED 1 IN AT STA 500.000 L-34W.SDR DHL2001803514Angle · crackedFWD CARGO COMPT LINING SUPPORT ANGLE CRACKED .375 IN AT STA 620.000 L-29R.SDR DHL2001803513Floor Support · crackedFWD CARGO COMPT FLOOR SUPPORT ANGLE CRACKED (1/4 IN) AT STA 5000.000.SDR DHL2001803512Angle · crackedFWD CARGO COMPT LINING SUPPORT ANGLE CRACKED .25 IN AT STA 460.000, L31L.SDR DHL2001803511Angle · crackedFWD CARGO COMPT LINING SUPPORT ANGLE CRACKED .25 IN AT STA 460.000, L31L.SDR DHL2001803529Angle · crackedFWD CARGO COMPT- LINING SUPPORT ANGLE CRACKED (.5 INCH) AT STA 460, L-29L.SDR DHL2001803528Angle · crackedFWD CARGO COMPT- LINING SUPPORT ANGLE CRACKED (1.5 INCH) AT STA 460, L-31R.SDR DHL2001803524Angle · crackedFWD CARGO COMPT- LINING SUPPORT ANGLE CRACKED 1.5 IN AT STA 600, L31R.SDR DHL2001803523Seat Track · wornMAIN CARGO COMPT - LUGS WORN ON L/H # 1 TRACK AT STA 1570-1710.CUR OUT DAMAGED TRACK AT MAIN CARGO COMPT, STA 1530.000 - 1710.000 PER SRM 53-2-3 PG 1&2.CLEANED , TREATED AND PRIMED AREA PER SRN 51-1-8B.INSTALLED NEW TRACK PER SRM 53-2-3 PG 1 & 2SDR DHL2001803522Angle · crackedFWD CARGO LINING SUPPORT ANGLE WITH .5 IN CRACK AT L 32 LT AT STA 80.000.SDR DHL2001803510Angle · crackedFWD CARGO LINING SUPPORT ANGLE SHOWS .25 IN CRACK L-31 RT STA 480.000.SDR DHL2001803531Angle · crackedRT FUSELAGE WALL EXT VERTICAL ANGLE SHOWS .5 INCH CRACK AT STA 980.SDR DHL2001803519Fitting · crackedRT MLG TRAPEZOIDAL LWR END, STOP DRILLED CRACK (6.125 IN ) CONTINUES .5 IN BEYOND STOP DRILL AT STA 896.12. STOP DRILLED CRACK (.375 DIA), INSPECTED WITH NDT, CRACK DOES NOT CONTINUE PER SEQ-LIM 0100070H 06-20-01.SDR DHL2001803508Skin · dentedVERTICAL STABILIZER L/E SHOWS 3.52 IN DENT AT ZFS 123.500. CUT OUT DAMAGED AREA PER SRM 55-2-1 PG 17. FABRICATED FILLER (ALCLAD 7075 T6,0.050) PER SRM 55-2-1. FABRICATED DOUBLER (ALCLAD 7075-T6 0.050) PER SRM 55-2-1 PG 17. CLEANED, TREATED AND PRIMED PER SSDR DHL2001803520Angle · crackedFWD CARGO COMPT - LINING SUPPORT ANGLE CRACKED (.25 IN) AT STA 400.00 L-31L.SDR DHL2001802009Spring · lack of lubeCAPT'S SEAT INTERMITTENTLY DOES NOT LOCK INTO POSITION ON TRACKS. LUBED TRACK & SPRING MECHANISM OP CK GOOD IAW 25-11-1SDR DHL2001803536Fairing · crackedAT C-CK, RT WING TO FUSELAGE UPPER FAIRING SHOWS 1 INCH BREAK AT STA 834.SDR DHL2001803535Skin · crackedAT C-CK, NR 2 ENGINE - RT THRUST REVERSER INTERNAL SKIN CRACKED 2 INCHES AT 3 O'CLOCK POSITION.SDR DHL2001803532Skin · crackedAT C-CK, ENGINE NR 3 HAD 1.5 INCH CRACK ON EXTERNAL SKIN OF TRANSLATING COWL LT (UPPER BORDER) AT 11 O'CLOCK.SDR DHL2001803534Angle · crackedAT C CK, RT WING - WING TO FUSELAGE FILLET SUPPORT ANGLE CRACKED (2 INCHES) AT XW 908-XCW 69.5.SDR DHL2001803533Doubler · brokenAT C-CK, RT WING- EXT PATCH ON OUTBOARD FLAP UPPER SKIN NEAR STA XW 219.00 SHOWS .3125 INCH BREAK APPROX.SDR DHL2001803537Radome · crackedAT C-CK, RADOME- 2 (EA) .25 INCH CRACKS ON RADOME LOWER LIP (INNER PART). PERFORMED STOP HOLE IAW SRM 53-2-0 FIG 1B, FABRICATED AND INSTALLED DOUBLER IAW SRM 53-2-0 FIG 1B.SDR DHL2001802008Indicator · defectiveNR 1 MAIN FUEL TANK QUANTITY AT 2000 LBS WITH NO FUEL QUANTITY LOW LIGHT ILLUMINATED. REMOVED AND REPLACED NR 1 MAIN FUEL QTY GAUGE PER MM 28-41-0 AND CALIBRATED GAUGE.SDR DHL2001807019Computer · malfunctionedAUTOPILOT WILL NOT LEVEL OFF FROM CLIMB OR DESCENTS EVEN WITH MIN RATE ON INITIATION LEVEL OFF. CLEANED AND RE-SEATED A/P PITCH COMPUTER IN RACK. PERFORMED TEST OF A/P PITCH CHANNEL PER M/M 22-13-0. ALL TESTS GOOD.SDR DHL2001807016Gyro · faultyAUTOPILOT ELEVATOR CONTROL JERKS ON CLIMBOUT AND IN LEVEL FLIGHT. AUTOPILOT ELEVATOR SERVO INDICATOR SHOWS CORRESPONDING MOVEMENT. THIS IS A REPEAT ITEM. COULD NOT DUPLICATE AUTOPILOT JERKS. SWAPPED TO AUX VERTICAL GYRO FOR TROUBLESHOOTING. CAPTAINS NORMASDR DHL2001807015Servo · defectiveAUTOPILOT ELEVATOR CONTROL JERKS ON CLIMBOUT AND LEVEL FLIGHT. AUTOPILOT ELEVATOR SERVO INDICATOR SHOWS CORRESPONDING MOVEMENT. REMOVED AND REPLACED ELEVATOR SERVO DRIVE IAW DHL DC-8 MM 22-10-4. OPS CK GOOD IAW MM 22-10-4. RII SERVO DRIVE INSTALLATION.SDR DHL2001807018Autopilot Sys · malfunctionedAUTOPILOT WHILE ON FINAL APPROACH BELOW 1000 FT ALT CONTINUED TO DIVERGE BELOW GLIDESLOPE WITHOUT CORRECTION. REPOSITIONED LINKAGE ABOVE SERVO MICROSWITCH, OPS CKD OK IAW MM 22-20-0.SDR DHL2001807017Linkage · out of positionAUTOPILOT EXCEEDED 35 DEG BANK DURING TURNS. REPOSITIONED LINKAGE ABOVE SERVO MICROSWITCH. OPS CK''D OK IAW MM 22-20-0.SDR DHL2001807014Linkage · jammedAUTOPILOT PITCH CONTROL IS ERRATIC IN CLIMB AND TURNS JERKS CONTROL YOKE BACK AND FORTH. FOUND JAMMED LINKAGE ABOVE SERVO MICRO-SWITCH. REMOVED AND PROPERLY REPOSITIONED LINKAGE. CLEANED CONNECTOR TO MICROSWITCH AND SERVO. OPS CK''D OK IAW MM 22-20-0.SDR DHL2001807013Computer · malfunctionedAUTOPILOT PITCH CONTROL IS ERRATIC IN CLIMB AND TURNS (JERKS CENTER YOKE BACK & FORTH). REMOVED AND REPLACED PITCH CHANNEL 2 COMPUTER IAW DC-8 MM CH 22-13-1. AUTOPILOT PITCH CONTROL OPS CK NORMAL.SDR DHL2001807012Control Panel · malfunctionedAUTOPILOT PITCH CONTROL IS ERRATIC IN CLIMB AND TURNS. R&R A/P CONTROL PANEL IAW 22-10-2. A/P CHECKS GOOD.
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