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 DHL2003802013Fire Loop · shortedNR 2 ENGINE SHORT CIRCUIT LIGHT ILLUMINATED ON LOOP (A). LOOP (B) OPS CHECKED NORMAL. CLEANED CONNECTOR ON NR 2 ENGINE SYSTEM OPS CHECK GOOD IAW DC8 M/M 26-10-0.SDR UPS03841220Wire · looseINSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS NOT PERATING PROPERLY. RESET CONNECTOR ON EMERGENCY LIGHT BATTERY PACK, OPS CK NORMAL.SDR DHL2003802012Door · crackedRT MAIN GEAR DOOR HAS .2500 INCH CRACK PROPAGATING FROM RIVET B.S. 875.125 20 INCH OUT FROM INBOARD HINGE. STOPPED DRILLED CRACK, INSTALLED A DOUBLER REPAIR IAW SRM 52-2-3.SDR DHL2003802011Door · crackedRIGHT MAIN GEAR DOOR HAS CRACK PROPAGATING FROM RIVET B.S. 860 12 INCHES FROM OUTBOARD RADIUS. CRACK .5 INCHES LONG. STOPPED DRILLED CRACK. INSTALLED A DOUBLER REPAIR IAW SRM 52-2-3.SDR DHL2003803015Battery · inoperativeEMERGENCY LIGHTS BATTERY CHARGER CIRCUIT BREAKER WILL NOT RESET. REMOVED AND REPLACED EMERGENCY BATTERY LIGHT BATTERY AND RELAY UNIT IAW M/M 33-50-1 OPS CHECKED SERVICEABLE.SDR DHL2003803014Battery · dischargedEMERGENCY LIGHT BATTERY DRAINED. REPLACED IAW M/M 33-50-1. OPS CHECKED SERVICEABLE.SDR DHL2003803013Escape Rope · out of adjustCAPTAIN'S ESCAPE ROPE ACCESS DOOR WILL NOT REMAIN SECURED AND OPENED FREQUENTLY. RE-POSITIONED AND SECURED AS REQUIRED. CAPTAIN'S ESCAPE ROPE ACCESS DOOR OK, REF M/M 25-60-2.SDR DHL2003803012Lamp · inoperativeDURING PREFLIGHT, DISCOVERED NR 14 SMOKE DETECTOR INOPERATIVE. MAYBE DEFERRED IAW MEL 26-6 DMI 13597 PLACARD INSTALLED. REF DMI 13597. DURING PREFLIGHT DISCOVERED NR 14 SMOKE DETECTOR INOPERATIVE. REMOVED AND REPLACED BOTH BEACON AND TEST LAMP ON NR 14 SMOSDR DHL2003803010Seat · inoperativeF/O SEAT DOES NOT ADJUST VERTICALLY WITH LEVER. REPLACED F/O SEAT ASSY IAW MM 25-11-0. OPS CHECK GOOD.SDR DHL2003803009Seat · brokenSO'S SEAT LATERAL ADJUST HANDLE BROKE. REMOVED AND REPLACED SO'S SEAT IAW M/M 25-11-3. OPS CK NORMAL.SDR DHL2003803008Seat · inoperativeF/O SEAT SLIDES FORE AND AFT EASILY BUT DIFFICULT TO LOCK IN PLACE. REPLACED F/O SEAT ASSY IAW MM 25-11-1. OPS CHKS GOODSDR DHL2003803007Seat · inoperativeSECOND OFFICER'S SEAT WILL NOT LOCK UP OR DOWN. LUBED SECOND OFFICER'S SEAT VERTICAL ADJUSTMENT IAW 25-11-6. OPS CHECK WAS GOOD.SDR DHL2003802010Lamp · burned outNR 5 SMOKE DETECTOR WILL NOT TEST. RELAMPED NR 5 SMOKE DETECTOR. OPS NORMAL PER M/M 26-10-0.SDR DHL2003802009Seat · bindingCAPTAIN'S SEAT BINDS DURING FORE AND AFT ADJUSTMENT. ADJUSTED CAPTAIN'S FORE AND AFT SEAT LEVER. SEAT OPS GOOD IAW 25-11-1.SDR DHL2003802008Engine · leakingLOSS OF OIL QUANTITY NR 3 ENGINE. PERFORMED ABNORMAL PROCEDURE, RESULTED IN IN-FLIGHT ENGINE SHUTDOWN AT 0620Z. OIL PRESS 6 PSI. OIL QUANTITY -0-. OIL TEMP 75 CELSIUS. REMOVED STARTER ON NR 3 ENGINE. FOUND SHAFT SHEARED AND DAMAGE TO TRANSFER GEARBOX (TGSDR DHL2003802007Connector · defectiveNR 3 FIRE DETECTOR LOOP-B SYSTEM FAILED TO TEST. TRANSFERRED TO DMI 12964 CAT-C IAW MEL 26-2-3, PLACARDS INSTALLED. REF DMI 12964 NR 3 FIRE DETECTOR LOOP-B SYSTEM FAILED TO TEST. REPLACED DEFECTIVE CONNECTOR AT FAN CASE RT PER DACO M/M 20-504. OPS CHECKED SDR DHL2003802006Connector · damagedNR 2 ENGINE FIRE DETECTOR SHORT CIRCUIT LIGHT CAME ON (LOOP "A") DURING TAXI, OK ON LOOP "B". DEFERRED PER MEL 26-2-3, CONTROL 12777. REF. DMI 12777 - NR 2 ENGINE FIRE DEFECT SHORT CIRCUIT LIGHT CAME ON (LOOP "A") DURING TAXI. OK ON LOOP "B". TROUBLESHOSDR DHL2003802005Connector · dirtyNR 2 ENGINE FIRE SHORT CIRCUIT LIGHT FLASHED ON LOOP-A, LOOP-B OK. INSPECTED ALL LOOPS AND CLEANED CONNECTOR. OPS CHECKED GOOD IAW M/M 26-10-0.SDR DHL2003802004Seat Track · lack of lubeS/O SEAT VERY HARD TO MOVE WHEN USING FORWARD SEAT EDGE RELEASE HANDLE. LUBRICATED GUIDE RAILS, OPS CHECKED GOOD PER M/M 25-11-2.SDR DHL2003802003Fire Loop · shortedNR 2 ENGINE FIRE LOOP "A" INDICATES A SHORT. "B" LOOP OK. ENTERED ON DMI 12760 IAW MEL 26-2-3 CAT. "C". REF. DMI 12760 NR 2 ENGINE FIRE LOOP "A" INDICATES A SHORT. "B" LOOP OK. NR 2 ENGINE COWL OPEN TO FACILITATE MAINTENANCE. INSPECTED ALL LOOPS AND RE-SDR DHL2003803006Seat Track · dirtyF/E'S SEAT DIFFICULT TO SLIDE FORE AND AFT. LOCKING MECHANISM DOES NOT SEEM TO BE DISENGAGING FULLY. CLEANED SEAT TRACK, LUBED TRACK AND MECHANICAL HANDLE SEAT, OPS OK M/M 25-11-6.SDR DHL2003803005Smoke Detector · will not testNR 4 SMOKE DETECTOR WILL NOT TEST. DEFERRED PER MEL 26-6-1. CAT. "C". THIS IS DMI 12416. NR 4 SMOKE DETECTOR WILL NOT TEST REF. DMI 12416. REMOVED AND REPLACED NR 4 SMOKE DETECTOR BULBS PER M/M 26-10-5. SYSTEM OPS CHECKED GOOD. THIS CLEARED DMI 12416.SDR DHL2003803004Seat Track · lack of lubeS/O'S SEAT DIFFICULT TO MOVE FORE AND AFT. LUBED F/O'S AND S/O'S SEAT TRACKS AND CHECKED MOVEMENT. OK PER M/M 25-11-1.SDR DHL2003802002Lamp1) #3, #8, AND #9 MAIN CARGO SMOKE DETECTOR WILL NOT TEST.2) RELAMPED SMOKE DETECTOR #3 AND #8 - OPS CHECKED GOOD. DEFERRED #9 SMOKE DETECTOR PER DC8 MEL 26-6-1. CONTROL #12224 CAT. "C".3) REF. DMI #12224 #9 SMOKE DETECTOR INOPERATIVE.4) REPLACED LAMP ON SDR DHL2003803003Smoke Detector · malfunctionedSMOKE DETECTOR NR 13 TEST IMPROPERLY LIGHT STAY'S ON. RELAMPED NR 13 SMOKE DETECTOR, NO HELP. DEFERRED IAW MEL 26-6-1 DMI 11984.SDR DHL2003803002Lamp1) DURING PREFLIGHT #7 SMOKE DETECTOR WOULD NOT TEST.2) RELAMPED SMOKE DECTETOR OPS CK GOOD PER MM 26-10-0.SDR DHL2003803001B-Nut · crackedNR 4 ENGINE LOST 4 QUARTS OF OIL IN FLIGHT FROM MEX APPROXIMATELY 1/2 QUART EVERY HALF HOUR. FOUND OIL TUBE SUPPLY TGB CRACKED AT B-NUT. REMOVED FOR FABRICATION. NR 4 ENGINE QUIT ON DESCENT. OIL PRESSURE AND TEMPERATURE NORMAL. ENGINE CONTINUED WINDMILLINSDR DHL2003802001Lamp1) #4 SMOKE DETECTOR WILL NOT TEST.2) PLACED #4 SMOKE DETECTOR ON DMI #11684 MEL 26-6-1.3) REF. DMI #11684, #4 SMOKE DETECTOR WILL NOT TEST.4) RELAMPED SMOKE DETECTOR. OPS CHECKED GOOD PER M/M 26-10-1. THIS CLEARS DMI #11684. PLACARD REMOVED.SDR DHL2002803013Warning Light · false indicationNR 3 FUEL BYPASS LIGHT KEEPS ILLUMINATING IN FLIGHT. RESETS OK, BUT RE-ILLUMINATES WITHIN ONE MINUTE. DEFERRED NR 3 FUEL BYPASS LIGHT PER MEL 73-2-2. REMOVED AND REPLACED NR 3 FUEL FILTER. NO CONTAMINATION PRESENT. DMI 11188 ASSIGNED. SPECIAL PROCEDURE COMPLSDR DHL2002803012Fuel Filter1) #3 FUEL BYPASS LIGHT ILLUMINATED IN FLIGHT. PERFORMED ABNORMAL PROCEEDURE AND LIGHT EXTINGUISHED. BYPASS LIGHT ILLUMINATED A SECOND TIME AND WOULD NOT EXTINGUISH. FUEL FILTER BYPASS RESET LIGHT INOPERATIVE.2) FOUND #3 ENGINE FUEL FILTER CONTAMINATED. REMOSDR DHL2002803011Lamp1) #13 SMOKE DETECTOR WILL NOT TEST.2) DEFERRED PER MEL 26-6-1 DMI #11131.3) RE: DMI #11131 - #13 SMOKE DETECTOR WILL NOT TEST.4) REMOVED AND REPLACED BOTH LAMPS IN #13 SMOKE DETECTOR. SYSTEM CHECKED GOOD PER 26-10-0. CLEARED DMI #11131. PLACARD REMOVED.SDR DHL2002803010Seat · damagedFIRST OFFICER'S SEAT UNABLE TO MOVE FORE AND AFT. REPLACED COTTER PIN TO FORE AND AFT ADJUSTMENT ON RT SIDE. OPS CHECKED NORMAL PER M/M 25-11-1.SDR DHL2002803539Panel · delaminatedITEM REF. N/R 0409 : LOWER FUS.- #715 LH LOWER ACCESS PANEL INNER SKIN FLANGE UNBONDEDCORR: R/R #715 LH LOWER ACCESS PANEL ON LOWER FUS. , CTR. WING IAW 51-3-0 PG. 1SDR DHL2002803535Panel · delaminatedIITEM REF N/R: 0108 : RH WING LOWER SURFACE T/E LOWER PANEL EXTERNAL SLIN DELAMINATED XRS 162.000 TO XF 219.000 CORR: removed and replaced panel iaw srm 51-1-3SDR DHL2002802011Smoke Detector · will not testNR 5 MAIN CABIN SMOKE DETECTOR FAILED TO TEST. RELAMPED NR 5 MAIN CABIN SMOKE DETECTOR OPS CHECKED OK IAW M/M 26-10-0.SDR DHL2002803541Longeron · crackedAFT OF PRESSURE DOME AREA, INTERIOR LONGERON 17 LT AT FS 1766.000 WITH 2 INCH CRACK IN IT PERFORMED MAJOR REPAIR IAW SRM53-1-10. REMOVED DAMAGED LONGERON IAW SRM 51-1-21. CLEANED, TREATED AND PRIMED AREA IAW SRM51-1-8B. INSTALLED NEW LONGERON IAW SRM51-1-21 SDR DHL2002803540Longeron · crackedITEM REF. N/R: 1842: FUS. AFT OF PRESSURE DOME AREA- INTERIOR-LONGERON 17R@FUS.STA. 1766.000 WITH 1" CRACK IN IT. (MAJOR REPAIR)SDR DHL2002803536Fitting · crackedITEM REF N/R: 0470 MAIN CARGO COMPT. - SPLICE FITTING CRACKED .500 @ STA. 759.000 RBL 23 ( MAJOR REPAIR)CORR:PERFORMED MAJOR REPAIR IAW ATM# po111892 , drawing 5750549.REMOVED SPLICE FITTING CRACKED IAW SRM 51-1-20D PG. 21. CLEANED , TREATED , AND PRIMED AREA SDR DHL2002803543Skin · corrodedFUSELAGE SKIN CORRODED BETWEEN STA 78.000 AND STA 82.000 , L32 LT TO L33 LT. PERFORMED MAJOR REPAIR IAW EO DHL021002 , ED-3136 , REMOVED FASTNERS IAW SRM51-1-21. REMOVED CORROSION IAW SRM51-1-8, OUT OF LIMITS IAW SRM53-2-0. TRIMMED OUT DAMAGED AREA SKIN SEGMSDR DHL2002803547Plate · crackedRT INBD SLOT LE INTERNAL PLATE WITH 2 INCH CRACK IN IT STA XFS 218.000. REMOVED DAMAGED PLATE IAW SRM 57-2-0 FIG 2 FABRICATED NEW PLATE IAW SRM57-2-0 FIG. 2. CLEANED ,TREATED AND PRIMED AREA IAW SRM 51-1-8B INSTALLED NEW PLATE IAW SRM 57-2-0 FIG. 2SDR DHL2002803542Former · crackedITEM REF. LH WING FORMER CENTRAL LEADING EDGE CRACKED 3" @ STA. XFS347.000 (MAJOR REPAIR).PERFORMED MAJOR REPAIR IAW SRM57-2-20 D PG. 21 STOP DRILLED CRACK IAW SRM 57-2-0 PG. 1-10 FABRICATED DOUBLERS (02EA.)(7075T6AL .071) IAW SRM 57-2-0 PG 9-10 CLEANED , TRESDR DHL2002803537Skin · dentedITEM REF. N/R: 0179: FUS. EXT. EXTERNAL SKIN DENTED 30.0000 " LONG NEAR L14R STA. 35.000 - STA. -12.000 ( MAJOR REPAIR) CORR: PERFORMED MAJOR REPAIR IAW FAX BOEING DHL-CVG-02-00057H; ED-3135 & ED-3142. REMOVED FASTNERSIAW SRM 51-1-21 PG. 1 , CLEANED , TREATED SDR DHL2002803546Fitting · crackedITEM REF. N/R 0819: AFT ACCY COMPT. - FITTING 2" CRACKED, STA. 1766.000 L28L (MAJOR REPAIR)CORR: PERFORMED MAJOR REPAIR IAW SRM53-1-0 PG. 1 REMOVED DAMAGED FITTING IAW SRM51-1-20D PG. 21CLEANED , TREATED , AND AREA IAW SRM51-1-8B. INSTALLED NEW FITTING IAW SRMSDR DHL2002803545Rib · crackedLT WING OUTBD LE FORMER AT STA XRS 597.000 WITH 1/2 INCH CRACK IN IT. STOP DRILLED CRACK IAW SRM 57-2-0 PG. 9-10 FABRICATED RE-INFORCING ANGLE IAW SRM 57-2-0 PG 9-10 CLEANED , TREATED AND PRIMED IAW SRM 51-1-8B INSTALLED REINFORCING ANGLE IAW SRM 57-2-0 PG. 9SDR DHL2002803525Frame · crackedRT WING L/E FRAME UPPER PART AT STA 680.000 WITH 1/2 INCH CRACK IN IT. REMOVED FASTENERS PER SRM 51-1-21 PG 1. STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10. FABRICATED REINFORCING ANGLE (2024.T3 AL0.032) PER SRM 57-2-0 PG9-10. CLEANED TREATED AND PRIMED PER SSDR DHL2002803505Frame · crackedRT WING L/E UPPER PART FRAME CRACKED 1/2 IN AT STA 649.000. REMOVED FASTNERS PER SRM 51-121 PG 1.STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10. FABRICATED REINFORCING ANGLE (2024.T3 AL 0.32) PER SRM 57-2-0 PG 9-10,51-1-21 PG 1. CLEANED TREATED AND PRIMED PER SRM SDR DHL2002803531Frame · crackedLT WING CENTRAL L/E FRAME CRACKED 1 INCH AT STA XFS 422.000. REMOVED FASTNERS PER SRM 51-1-20D PG 21. STOP DRILLED 1 INCH CRACK PER SRM 57-20 PG 9-10.FABRICATED A DOUBLER ANGLE (2024T3AL0.032) PER SRM 57-2-0 PG 9-10. CLEANED TREATED AND PRIMED PER SRM 51-1-SDR DHL2002803530Frame · crackedLT WING CENTRAL L/E FRAME CRACKED AT STA XFS 471.000. REMOVED FASTNERS PER SRM 51-1-20 PG 21. STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10. FABRICATED DOUBLER ANGLE (2024 T3 AL 0.032) PER SRM 57-2-0 PG 9-10. CLEANED TREATED AND PRIMED PER SRM 51-1-8B. INSTALLEDSDR DHL2002803526Frame · crackedRT WING L/E FRAME LOWER PART AT STA 643.000 WITH 1/2 INCH CRACK IN IT. REMOVED FASTNERS PER SRM 51-1-21 PG 1. STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10. FABRICATED REINFOCING ANGLE (2024.T3 AL0.032) PER SRM 57-2-0 PG9-10. CLEANED TREATED AND PRIMED PER SRSDR DHL2002803524Frame · crackedRT WING L/E FRAME UPPER PART AT STA 649.000 WITH 1/2 INCH CRACK IN IT. REMOVED FASTNESS PER SRM 51-1-21 PG 1. STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10. FABRICATED REINFORCING ANGLE (2024.T3 AL0.032) PER SRM 57-2-0 PG9-10. CLEANED TREATED AND PRIMED PER SRM
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