Douglas DC-8-73
Service difficulty reports · 821
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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 DHLA200800040Connector · contaminatedFLIGHT 445, NR 2 FIRE LIGHT ILLUMINATED ADHERED TO THE ENGINE FIRE EMERGENCY PROCEDURE FIRE LIGHT STILL REMAIN ILLUMINATED. FOUND OIL IN CONNECTOR FIRELOOP AT FAN SECTION RT. CLEANED LA 26195. FOUND INDICATION ONLY NO OTHER CAUSE, FIRELOOP SYSTEM CKD NORMALSDR DHLA200800043Light · odorFLT NR 160 WITH COMP LIGHT SWITCH ON LIGHT OVER GALLEY ON A PHOSPHOROUS ODOR WAS DETECTED WITH GALLEY POWER OFF TURNED OFF COMP LIGHT SWITCH AND ODOR DISSIPATED, NO SMOKE DETECTED. TURNED ON COMP LIGHTS INSPECTED CARGO COMP LIGHTS, NO ODOR NOTED. OPS CK GOODSDR DHLA200800026Line · looseFLT NR 9994, NR 4 ENGINE ROLLBACK AT FL280 DESCENDED TO FL 200 ENGINE RESTARED NORMAL AND RAN NORMAL THE REST OF THE TRIP WITH NORMAL INDICATIONS. INSPECTED NR 4 ENGINE INTAKE AND EXHAUST NO DEFECTS NOTED. FOUND CDP LINE LOOSE RESECURED LINE IAW CFM 56 MM 71SDR DHLA200800006Connector · looseFLT 631, NR 1 ENGINE FIRE WARN COMES ON INTERMITTENTLY AT CRUISE FLIGHT FL 350 3 TIMES AND BOTH FIRE LOOPS CHECKED OK AND IN DESCENT FIRE LIGHT CAME ON STEADY. COMPLETED ENG FIRE CHECKLIST (CONT) LIGHT REMAINED ON, BOTH BOTTLES DISCHARGED IN A LOOP. FOUND LSDR DHLA200700092Pump · malfunctionedAFTER LDG NR 2 ENG FLAMED OUT WHILE TAXIING IN. REMOVED AND REPLACED NR 2 ENG DRIVEN FUEL BOOST PUMP IAW MM 37-10-1. OPS AND LEAK CHECK GOOD.SDR DHLA200700070Engine · shutdownIN CRUISE FL 360 FELT A/C SHUDDER AND VIBRATION FOUND NR 3 ENGINE SPOOLING DOWN ATTEMPTED RELIGHT EGT 565 ENGINE N1 WOULD NOT ACCELERATE N2 MAX 70. VIBRATION NOTED DURING DECELERATION AND ADVANCE OF THRUST LEVER PRECAUTIONARY SHUTDOWN ACCOMPLISHED A WINDMILLISDR DHLA200700058Engine · shutdownWHILE FOR PARKING, NR 2 ENG FAILED, RESTARTED ENGINE AND TAXIED TO GATE NR 2. INSPECTED NR 2 ENG INLET AND EXHAUST, NO DEFECT NOTED. RUN ENG IAW JRH CAP 12.6., WORKING NORMAL.SDR DHL2007803545Skin · delaminatedLT AFT ADF SENSE ANTENNA SKIN DELAMINATED. REMOVED AND REPLACED LT AFT ADF SENSE ANTENNA IAW SRM 51-3-0.SDR DHL2007803537Skin · delaminatedRT WING T/E UPPER PANEL SKIN DELAMINATED (STA XW 0.000 - 47.000). REMOVED DELAMINATED PANEL IAW SRM 51-3-0. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW PANEL IAW SRM 51-3-0, SRM 51-3-1 PG 2A (TORQUE).SDR DHL2007803542None · noneREMOVE REPAIR BELOW CARGO DOOR AT STA 176 AND INSPECT AREA. INSTALL A NEW REPAIR IAW SRM (PERMANENT) OR APPROVED DATA. ENTER INFORMATION ON 337 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 06-06-07, DWG NR AD42-53-11 REV IR DATED 06-01-0SDR DHL2007803543Frame · wornNR 3 ENG T/R FIXED STRUCTURE AND FWD FRAME WORN STA YN 202.000 AT 5 O'CLOCK POS (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3- DATED 06-08-07, DWG NR AD42-78-110 REV IR DATED 05-30-07. REMOVED FASTENERS IAW SRM 51-1-21. CUT OUT DAMAGED SECTION SDR DHL2007803539Skin · wornNR 2 ENG NACELLE INLET COWL UPPER SIDE WORN, STA YN 147.534 AT 12 O'CLOCK POS. PERFORMED MAJOR REPAIR IAW SRM 71-5-2 FIG 2. REMOVED FASTENERS IAW SRM 51-1-21A. CUT OUT DAMAGED SECTION AND FABRICATED NEW SKIN SEGMENT (AL2024T3 0.080") AND STEEL SPLICE 17.7 PSDR DHL2007803541Skin · wornNR 1 ENG NACELLE INLET COWL UPPER SIDE WORN, STA YN 147.534 AT 12 O'CLOCK POS. PERFORMED MAJOR REPAIR IAW SRM 71-5-2 FIG 2. REMOVED FASTENERS IAW SRM 51-1-21A. CUT OUT DAMAGED AREA AND FABRICATED NEW SKIN SEGMENT (AL2024T3 0.080") AND STEEL SPLICE 17-7PH 0.SDR DHL2007803540Skin · wornNR 4 ENG NOSE COWL EXT SKIN WORN (STA YN 147.000 - 157.000 AT 12 O'CLOCK POS LT/RT) MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW SRM 71-5-2 FIG 2. REMOVED FASTENERS IAW SRM 51-1-21A. CUT OUT DAMAGED SECTION AND FABRICATED NEW SKIN SEGMENT (AL2024T3 0.080") AND SDR DHL2007803538Skin · wornNR 3 ENG NOSE COWL EXTERNAL SKIN WORN (STA YN 147.534, AT 12 O'CLOCK POS) MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW SRM 71-5-2 FIG 2. REMOVED FASTENERS IAW SRM 51-1-21A. CUT OUT DAMAGED SECTION AND FABRICATED NEW SKIN SEGMENT (AL2024T3 0.080") AND STEEL SPLISDR DHL2007803536None · noneREMOVE REPAIR BELOW MAIN CARGO DOOR AT STA 226 AND INSPECT AREA. INSTALL NEW REPAIR IAW SRM (PERMANENT) AND APPROVED DATA. ENTER INFORMATION ON 337 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 06-08-07, DWG NR AD42-53-112 REV IR DATED 06-SDR DHL2007803535Channel · wornRT MLG INBD DOOR ZEE CHANNEL WORN STA 870.000 RBL 50" (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 06-06-07, DWG NR AD42-52-0108 REV IR DATED 05-22-07. REMOVED EXISTING REPAIR DOUBLER IAW SRM 51-1-21. CUT OUT DAMAGED SECTION AND FABRICATSDR DHL2007803534Skin · wornRT OUTBD FLAP UPPER SKIN WORN, STA XF 224.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 06-06-07, DWG NR AD42-57-106 REV IR DATED 05-21-07. REMOVED EXISTING REPAIR PLATING AND INNER DOUBLER IAW SRM 51-1-21. FABRICATED NEW PLATING SEGMSDR DHL2007803533None · noneRT INBD VANE SLOT HAS AN INTERIM REPAIR AT STA XILD 42 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 06-06-2007, DWG NR AD42-57-107 REV IR DATED 05-21-07. REMOVED EXISTING INTERIM REPAIR IAW SRM 51-1-21, SRM 51-3-0. CUT OUT DAMAGED SECTIOSDR DHL2007803531Longeron · damagedFUS NOSE SECTION LONGERON HAS A MISDRILLED HOLE AT STA -32.000 L-17R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 06-04-07, DWG NR AD42-53-109 REV IR DATED 05-25-07. REMOVED FASTENERS IAW SRM 51-1-21. FABRICATED REINFORCEMENT (AL7075T6 5SDR DHL2007803532Access Door · crackedLT FUS NOSE SECTION ACS MODIFICATION DOUBLER AT UPPER AFT JAMB CORNER OF HEAT EXCHANGER ACCESS DOOR, CRACKED 0.250" STA -12.000 L-24L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 06-04-07, DWG NR AD42-53-103 REV IR DATED 05-16-07. REMOVEDSDR DHL2007803544None · nonePERFORM MODIFICATION REPAIR TO THE L2 DOOR, FWD, LOWER CORNER IAW AD2000-20-08, S/B 53-075 AND SR08530021. MAKE ENTRY IN AIRCRAFT LOGBOOK AND PERMANENT RECORD (337 FORM) MAJOR REPAIR (AMOC). PERFORMED MAJOR REPAIR IAW FAA FORM 8100-9 DATED 05-22-07, BOEING MSDR DHL2007803526Doubler · crackedRT WING CTR L/E UPPER ANGLE DOUBLER CRACKED STA XFS 428.000. REMOVED CRACKED ANGLE DOUBLER IAW SRM 51-1-21, SRM 51-1-20D. FABRICATED ANGLE DOUBLER (AL7075"0" 0.080") IAW SRM 57-2-0 PG 9-10, SRM 57-3-3. HEAT TREATED ANGLE DOUBLER FROM 7075"0" TO 7075T6 IAW SSDR DHL2007803523Vane · unknownLT OUTBD VANE SLOT HAS AN INTERIM REPAIR AT STA XOLDO 67 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 06-01-07, DWG NR AD42-57-105, REV IR DATED 05-17-07. REMOVED EXISTING INTERIM REPAIR IAW SRM 51-1-21, SRM 51-3-0. CUT OUT DAMAGED SECTISDR DHL2007807524Vane · unknownRT OUTBD VANE SLOT HAS AN INTERIM REPAIR AT SOLDI 6.224 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 06-01-07, DWG NR AD42-57-101 REV IR DATED 05-16-07. REMOVED EXISTING INTERIM REPAIR IAW SRM 51-1-21, SRM 51-3-0. CUT OUT DAMAGED SECTIONSDR DHL2007803529Vane · unknownRT OUTBD VANE SLOT HAS AN INTERIM REPAIR AT STA XOLDO 67 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3- DATED 06-01-07, DWG NR AD42-57-102 REV IR DATED 05-16-07. REMOVED EXISTING INTERIM REPAIR IAW SRM 51-1-21, SRM 51-3-0. CUT OUT DAMAGED SECTISDR DHL2007803527Fitting · crackedNR 4 ALT TANK INTERIOR FITTING CRACKED 1" STA XW 408.000 S-58 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW JC EC-00363-001, DOUGLAS DWG NR 5644972. REMOVED CRACKED FITTING IAW SRM 57-1-0 PG 1, SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. ISDR DHL2007803528Rib · crackedNR 4 STUB WING RIB CRACKED STA XOLDO 67.750 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW JC EC-00364-001, DOUGLAS DWG NR 9753297. REMOVED CRACKED RIB IAW SRM 57-1-0 PG 1, SRM 51-1-21, SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED SDR DHL2007803530Vane · unknownLT OUTBD VANE SLOT HAS AN INTERIM REPAIR AT STA XOLDI 6.224 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 06-01-07, DWG NR AD42-57-104 REV IR DATED 05-16-07. REMOVED EXISTING INTERIM REPAIR IAW SRM 51-1-21, SRM 51-3-0. CUT OUT DAMAGED SECSDR DHL2007803519Channel · crackedRT WING LWR FAIRING ZEE CHANNEL CRACKED 1" STA XW -3.125. REMOVED CRACKED ZEE CHANNEL IAW SRM 51-1-21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW CHANNEL IAW SRM 51-1-21. REFER TO JC EC-00360-00 (WO 1028) FOR ZEE FABRICATION.SDR DHL2007803521Panel · crackedLT WING LWR PANEL CRACKED 1" STA XW -3.125. REMOVED PANEL IAW SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW PANEL IAW SRM 51-1-20D, SRM 51-3-1 (TORQUE). REFER TO JC EC-00359-001 (WO 1028) FOR PANEL FABRICATION.SDR DHL2007803520Channel · crackedLT WING LWR FAIRING ZEE CHANNEL CRACKED 0.750" STA XW -3.125. REMOVED ZEE CHANNEL IAW SRM 51-1-21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW CHANNEL IAW SRM 51-1-21. REFER TO JC EC-00361-001 (WO 1028) FOR ZEE FABRICATION.SDR DHL2007803522Fitting · crackedRT WING T/E UPPER FITTING 0.250" CRACK STA XRS 421.000. REMOVED CRACKED FITTING IAW SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D. TORQUED IAW SRM 51-3-1 PG 2A.SDR DHL2007803525Attach Angle · crackedRT WING CTR L/E OUTBD VANE SLOT ATTACH ANGLE CRACKED 1/2" STA XOLDI 6.225. REMOVED CRACKED ANGLE IAW SRM 51-1-21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW ANGLE IAW SRM 51-1-21. REFER TO JC EC-00372-001 (WO 1028) FOR ANGLE FABRICATIOSDR DHL2007803515Skin · delaminatedLT WING T/E LWR PANEL SKIN DELAMINATED (STA XF 339.000 - 409.000). REMOVED AND REPLACED DELAMINATED LT WING T/E LWR PANEL IAW SRM 51-3-0, SRM 51-3-1 (TORQUE).SDR DHL2007803516Cargo Track · wornUPPER CARGO COMPT NR 6 TRACK LUGS WORN (STA 135.000 - 270.000). CUT OUT DAMAGED SEGMENT OF TRACK NR 6 AND FABRICATED SPLICES (AL7075T6 0.100"/ 0.125"/ 0.160") IAW SRM 53-2-3 PG 49-50. CLEANED, TREATED AND PRIMED AREA AND SPLICES IAW SRM 51-1-8B. INSTALLED NSDR DHL2007803514Angle · crackedRT MLG W/W ANGLE CRACKED 1" STA 950.000. REMOVED CRACKED ANGLE IAW SRM 51-1-20D. FABRICATED NEW ANGLE (EXTRUSION 2616279) IAW SRM 53-2-0 PG 1, SRM 51-2-0 FIG 50. CLEANED, TREATED AND PRIMED AREA AND ANGLE IAW SRM 51-1-8B. INSTALLED NEW ANGLE IAW SRM 51-1-2SDR DHL2007803513Angle · crackedLT MLG W/W UPPER ANGLE CRACKED STA XFS 920.000 LBL 44". REMOVED CRACKED ANGLE IAW SRM 51-1-21. FABRICATED NEW ANGLE (AL2024T3 0.050") IAW SRM 53-2-0 PG 1. CLEANED, TREATED AND PRIMED AREA AND NEW ANGLE IAW SRM 51-1-8B. INSTALLED NEW ANGLE IAW SRM 51-1-21SDR DHL2007803512Angle · crackedRT MLG W/W ANGLE CRACKED 1" STA 940.000. REMOVED CRACKED ANGLE IAW SRM 51-1-20D. FABRICATED NEW ANGLE (EXTRUSION 2616279) IAW SRM 53-2-0 PG 1, SRM 51-2-0 FIG 50. CLEANED, TREATED AND PRIMED AREA AND NEW ANGLE IAW SRM 51-1-8B. INSTALLED NEW ANGLE IAW SRM 51SDR DHL2007803518Skin · misrepaired"B" CARGO DOOR SKIN REPAIR RIVETS EDGE DISTANCE NOT IN ACCORDANCE WITH SRM (UPPER PORTION) MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW SRM 52-2-0 FIG 4 SHEET 3. REMOVED EXISTING REPAIR IAW SRM 51-1-21. FABRICATED REPAIR DOUBLER AND FILLER (AL7075T6 0.063")IAW SDR DHL2007803508Frame · crackedRT WING OUTBD L/E INNER SECTION FORMER CRACKED 0.250", STA XFS 635.000. REMOVED FASTENERS IAW SRM 51-1-21. FABRICATED (2EA) ANGLE DOUBLERS AL7075T6 0.032" IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED AREA AND ANGLE DOUBLERS IAW SRM 51-1-8B. INSTALLESDR DHL2007803505Frame · crackedRT WING CTR L/E LWR FORMER CRACKED 0.250" STA XFS 466.615. REMOVED FASTENERS IAW SRM 51-1-21. FABRICATED (2EA) DOUBLER (AL7075T6 0.040") IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED AREA AND DOUBLER IAW SRM 51-1-8B. INSTALLED DOUBLER IAW SRM 51-1-21SDR DHL2007803507Frame · crackedRT WING CTR L/E UPPER FORMER CRACKED, STA XFS 397.750. REMOVED FASTENERS IAW SRM 51-1-21, SRM 51-1-20D. PERFORMED STOP HOLE AND FABRICATED (2EA) DOUBLERS (AL7075T6 0.032" / 0.040") IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED AREA AND DOUBLERS IAW SRSDR DHL2007803509Skin · crackedUPPER FUSELAGE EXT SKIN CRACKED 0.500" APPROX, STA 580.000 L-4R TO L-5R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-2-1 FIG 7 SHEET 1, 3. REMOVED FASTENERS IAW SRM 51-1-21. CUT OUT DAMAGED AREA AND FABRICATED REPAIR DOUBLER (AL7075T6 0.100") (2EA) INTSDR DHL2007803501Frame · crackedRT WING OUTBD L/E INNER SECTION LWR FORMER CRACKED 0.500" AT STA XFS 653.750. REMOVED FASTENERS IAW SRM 51-1-21. FABRICATED 2EA ANGLES DOUBLERS (AL7075T6 0.032") IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED AREA AND ANGLES IAW SRM 51-1-8B. INSTALLEDSDR DHL2007803503Frame · crackedRT WING OUTBD L/E INNER SECTION LWR FORMER CRACKED 0.500" AT STA XFS 616.250. REMOVED FASTENERS IAW SRM 51-1-21. FABRICATED 2 ANGLE DOUBLERS AL7075T6 0.032" IAW SRM 57-2-0 PG 9-10. CLEANED,TREATED AND PRIMED AREA AND ANGLE DOUBLERS IAW SRM 51-1-8B. INSTALLSDR DHL2007803500Frame · crackedRT WING OUTBD L/E INNER SECTION LWR FORMER CRACKED 0.500" AT STA XFS 660.000. REMOVED FASTENERS IAW SRM 51-1-21. FABRICATED ANGLES (2EA) DOUBLERS AL7075T6 0.032" IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED AREA AND ANGLE DOUBLERS IAW SRM 51-1-8B. ISDR DHL2007803506Doubler · crackedRT WING CTR L/E LWR SKIN INTERNAL DOUBLER CRACKED 0.500" STA XFS 428.000. REMOVED CRACKED INTERNAL DOUBLER IAW SRM 51-1-21, SRM 51-1-20D. FABRICATED NEW INTERNAL DOUBLER (AL7075T6 0.090") IAW SRM 57-2-0 PG 1 AND CLEANED, TREATED AND PRIMED AREA AND INTERNAL SDR DHL2007803504Skin · wornRT OUTBD FLAP UPPER SKIN WORN STA XF 207.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-7-1 FIG 4, TR NR 57-94 DATED 10-01-02. REMOVED DAMAGED PLATING IAW SRM 57-1-0 PG 1, SRM 51-1-21. FABRICATED NEW PLATING (AL2024T3 0.040") IAW SRM 57-7-1 FIG 4, TRSDR DHL2007803510Skin · crackedUPPER FUSELAGE SKIN CRACKED 0.500" STA 510.000 L-5R TO L-6R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-2-1 FIG 7 SHEET 1-3. REMOVED FASTENERS IAW SRM 51-1-21, SRM 51-1-20D. CUT OUT DAMAGED SECTION AND FABRICATED REPAIR DOUBLER (AL7075T6 0.090") (2EA)
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