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 UPS07849828Skin · gougedINSPECTION TYPE:C3 FUSELAGE EXTERIOR SKIN GOUGED AT STA 140 L22L. REPAIRED FUSELAGE SKIN AT STA 140 L22L IAW SAA EA 008-5330-01-A0849 UPS EO DC8-5330-26786-A, DOUGLAS DWG SRO8530027.SDR UPS07849808Skin · corrodedINSPECTION TYPE:C3 FUSELAGE EXTERIOR SKIN CORRODED AT FS 310 L2R. CUT OUT DAMAGED AREA AT STA 310 L2R IAW SRM 53-02-01 FIG 7. FABRICATED AND INSTALLED REPAIR DOUBLER, FINGER DOUBLER, AND FILLER AT STA 310 L2R IAW SRM 53-02-01 FIG 7.SDR UPS07849809Skin · gougedINSPECTION TYPE:C3 FUSELAGE EXTERIOR EXISTING REPAIR DOUBLER HAS DEEP GOUGE AND FASTENER HEADS MISSING AT STA 520 L31R. REMOVED DAMAGED DOUBLER AND CUT OUT AREA AT STA 520 L31R IAW SRM 51-1-20D. FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLERS AT STA 520 SDR UPS07849803Skin · crackedINSPECTION TYPE:C1 HFEC & VISUAL INSPECTION DETECTED A CRACK ON THE C-4 (D-PIT) UPPER FWD DOOR JAMB CORNER. CRACK RUNS FROM FASTENER HOLE TO EDGE OF CUTOUT. REMOVED EXISTING DOUBLER. CUT OUT DAMAGE. FABRICATED AND INSTALLED DOUBLER, TRIPLER AND FILLER. RESDR UPS07849781Skin · misrepairedINSPECTION TYPE:C3 REMOVE STEEL DOUBLER FROM THE C-4 (D-PIT) UPPER FWD CORNER AND REPAIR PER SRM 53-2-0 FIG 21. REMOVED AND REPLACED DOUBLER AT C-4 (D-PIT) UPPER FWD CORNER IAW SRM 53-02-00 FIG 21, AND SRM TR 53-140, & 53-188, THIS REPAIR REQUIRES AN MPI WITHSDR DHL2007806591Angle · crackedRT INBD FLAP LWR "T" ANGLE CRACKED 1 1/2" STA XW 91.000. REMOVED CRACKED "T" ANGLE IAW SRM 51-1-21. FABRICATED NEW "T' ANGLE (EXTRUSION S2701008) IAW SRM 57-7-1 PG 4. CLEANED, TREATED AND PRIMED AREA AND "T" ANGLE IAW SRM 51-1-8B. INSTALLED "T" ANGLE IAW SSDR DHL2007806599Channel · wornLT MLG LT DOOR ZEE CHANNEL EDGE WORN (MAJOR REPAIR) STA 865.000 RBL 45. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 03-30-07, ENGINEERING VARIATION AUTHORIZATION NR D852-00002 DATED 03-17-07 REV IR. REMOVED FASTENERS IAW SRM 51-1-21. CUT OUT DAMAGED SESDR UPS07849672Socket · inoperativeINSPECTION TYPE:N/A EMERGENCY ELECTRIC CONTROL PANEL HAS INOP LIGHT SOCKETS. DEFERRED EMERGENCY ELEC CONTROL PANEL LIGHTS PER MEL 33-1. [SUP 4-25-07] REMOVED AND REPLACED LIGHT PANEL PER DC8 MM 33, SYSTEM CHECKED OK. CLEARED DMI 348799 AND REMOVED PLACARD.SDR DHL2007806589Fitting · crackedFOUND FWD CARGO COMPT FITTING 3" CRACK STA 340.000 L-26R. 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, SRM 51-3-1 (TORQUE) REFER TO JC EC-00247-001 (WO 470) FOR FITTING FSDR DHL2007806598Fitting · crackedNR 4 MAIN TANK FITTING CRACKED STA XRS -255.000 S-51. 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, SRM 51-3-1 (TORQUE). FOR FITTING FABRICATION SEE JC EC-00293-001 (WO 4SDR DHL2007806590Fitting · crackedAFT CARGO COMPT FITTING 3 INCH CRACKED STA 1220.000 L-26R. 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, SRM 51-3-1 (TORQUE). REFER TO JC EC-00247-001 FOR FITTING FABRICASDR DHL2007806592Fitting · crackedMAIN CARGO COMPT FITTING 1" CRACK STA 902.125 L-18R. 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, SRM 51-3-1 (TORQUE) REFER TO JC EC-00276-001 (WO 470) FOR FITTING FABRICSDR DHL2007806596Doubler · crackedRT WING ACCESS DOOR NR 505E INTERNAL DOUBLER CRACKED 0.250" STA XRS 128.000 S-5 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8100-9 DATED 04-18-07, BOEING MESSAGE NR 1-306853011-4 DATED 04-17-07, NR 1-306853011-2 DATED 03-27-07. REMOVED FASTENERS IAW SDR DHL2007806595Doubler · crackedLT WING ACCESS DOOR NR 505F INTERNAL DOUBLER CRACKED 0.250" STA XRS 135.000 X-5 TO S-6 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8100-9 DATED 04-18-07, BOEING MESSAGE NR 1-306853011 DATED 04-18-07, NR 1-306853011-2 DATED 03-27-07. REMOVED FASTENERSSDR DHL2007806594Door · misrepairedREPAIR ON FWD LWR CORNER OF "D" CARGO DOOR (STA 1400.000 - 1420.000 L-31R TO L-35R) IS NOT IN ACCORDANCE WITH DWG NR SR08530019 (SHOWS CORROSION TOO) MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW DOUGLAS DWG NR 5779936. REMOVED NON STANDARD REPAIR IAW SRM 51-1-21SDR UPS07849763Bracket · crackedINSPECTION TYPE:C1 LOWER FRONT SPAR CAP BRACKET IS CRACKED IN 2 PLACES BETWEEN XRS 463-428 NR 1 ALT. REMOVED, FABRICATED AND INSTALLED BRACKET IN NR 1 ALT TANK IAW SRM 51-01-20D, 51-03-02, AND DWG 76335150001.SDR DHL2007806588Skin · damagedRT ELEVATOR LWR SKIN DEFLECTED (STA XE 222.875 - 228.031) DAMAGED (MAJOR REPAIR) DAMAGED BY SEMAN (SEE ACCIDENT REPORT). PERFORMED MAJOR REPAIR IAW SRM 55-4-1 FIG 1 SHEET 1, 2 PG 2, 3. REMOVED DAMAGED PANEL PLATING IAW SRM 55-1-0 PG 1, SRM 51-1-21. FABRICATSDR DHL2007806578Angle · corrodedRT MLG W/W REAR SPAR WEB ANGLE CORRODED AT STA 857.125 RBL 45". REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. REMOVED CORRODED ANGLE IAW SRM 51-1-21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW ANSDR DHL2007806579Fitting · damagedMAIN CARGO COMPT FRAME FITTING HAS A MISDRILLED HOLE STA 1040.000 L-20L TO L-21L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1. REMOVED DAMAGED FITTING IAW SRM 53-1-0. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. APPLIED SEALANT TO FAYINGSDR DHL2007806602Longeron · crackedAFT CARGO COMPT L-24R CRACKED 1" (STA 1490.000 - 1520.000) MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW FAA FORM 8100-9 DATED 04-17-07, BOEING MESSAGE3 1-299391776-2 DATED 03-14-07 AND NR 1-316315027-2 DATED 04-17-07. REMOVED FASTENERS IAW SRM 51-1-21. CUT OUT SDR DHL2007806601Channel · wornRT MLG INBD DOOR FLANGE ZEE CHANNEL AFT PART WORN STA 980.000 RBL 45" (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 04-09-07, ENGINEERING VARIATION AUTHORIZATION NR D85200005 REV IR DATED 03-27-07. REMOVED FASTENERS IAW SRM 51-1-21. CUT OSDR DHL2007806577Floorbeam · corrodedITEM REF. NR. 049960: AFT CARGO COMPT FLOORBEAM SUPPORT FITTING CORRODED, STA 1220.000 RBL 50". REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. REMOVED CORRODED FITTING IAW SRM 51-1-20D. FABRICATED NEW FITTING (AL7075"0SDR DHL2007806586Frame · crackedRT WING INBD L/E FORMER WITH CRACKS 1" AND 1.500" (MAJOR REPAIR) STA XCW 69.000. PERFORMED MAJOR REPAIR IAW SRM 57-3-3 FIG 1. REMOVED CRACKED FORMER IAW SRM 57-1-0 PG 1, SRM 51-1-21. FABRICATED FORMER (AL7075"0" 0.090") IAW SRM 57-3-3 FIG 1, SRM 51-1-4. HESDR DHL2007806593Door Frame · wornRT MLG INBD DOOR JAMB FLANGE WORN STA 865 RBL 45 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 04-09-07, ENGINEERING VARIATION AUTHORIZATION NR D852-00001 REV IR DATED 03-14-07. REMOVED FASTENERS IAW SRM 51-1-21. CUT OUT DAMAGED SECTION ASDR UPS07849636Battery Pack · malfunctionedINSPECTION TYPE:N/A BTB - EMERGENCY LIGHTS ILLUMINATED IN THE ARMED POSITION WITH A/C POWER ON. MAINTENANCE WILL REPLACE THE BATTERY/RELAY PACK ASSY AS A PRECAUTIONARY. ORDERED ON REQ A927417. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK PER MM 33-00-0SDR DHL2007806587Nose Cowl · wornNR 2 ENG RT NOSE COWL UPPER PORTION WORN (STA YN 147.534 - 163.000, AT 12 O'CLOCK POS) MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW SRM 71-5-2 FIG 2 SHEET 1, 2, 3. REMOVED FASTENERS IAW SRM 51-1-21A. CUT OUT DAMAGED SECTION AND FABRICATED SKIN (AL2024T3 0.080")SDR DHL2007806585Nose Cowl · wornNR 1 ENGINE NOSE COWLING RT UPPER PART WORN AT 12 O'CLOCK POS STA YN 163.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 71-5-2 FIG 2 SHEET 1, 2, 3. REMOVED FASTENERS IAW SRM 51-1-21A. CUT OUT DAMAGED SECTION AND FABRICATED SKIN (AL2024T3 0.080") AND SPLSDR DHL2007806581Frame · damagedMAIN CARGO COMPT FRAME FITTING HAS A MISDRILLED HOLE STA 1420.000 L-20R TO L-21R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1. REMOVED DAMAGED FITTING IAW SRM 53-1-0 PG 1, SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. APPLIESDR DHL2007806573Skin · damagedLT WING CTR L/E LWR SKIN HAS ELONGATED HOLES STA XFS 526.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 04-05-07, ENGINEERING VARIATION AUTHORIZATION NR D857-00004 DATED 03-27-07 REV IR. FABRICATED REPAIR DOUBLER (AL7075T6 0.071") IAW ASDR DHL2007806584Door · wornNR 4 ENG LT/RT NACELLE INLET COWL WORN, STA YN 157.000 AT 12 O'CLOCK POS (EXTERIOR) MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW SRM 71-5-2 FIG 2 SHEET 1, 2, 3. REMOVED FASTENERS IAW SRM 51-1-21A. CUT OUT DAMAGED SECTION AND FABRICATED NEW SKIN (AL2024T3 0.080"SDR DHL2007806583Frame · corrodedAFT CARGO COMPT FRAME CORRODED, STA 1320.000 L-24L TO L-25L. PERFORMED MAJOR REPAIR IAW SRM 53-2-0 FIG 2. REMOVED FASTENERS IAW SRM 51-1-20D. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. CUT OUT CORRODED FRAME SEGMESDR DHL2007806582Inlet · wornNR 3 ENG LT/RT NACELLE INLET COWL WORN STA YN 157.000 AT 12 O'CLOCK POS (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 71-5-2 FIG 2 SHEET 1, 2, 3. REMOVED FASTENERS IAW SRM 51-1-21A. CUT OUT DAMAGED SECTION AND FABRICATED NEW SKIN (AL2024T3 0.080") AND SPLISDR DHL2007806600Floorbeam · corrodedMAIN CARGO COMPT FLOORBEAM CORRODED STA 55.000 RBL 54 (FLOORBEAM SEGMENT) MAJOR REPAIR. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. REMOVED CORRODED FLOORBEAM IAW SRM 51-1-20D. FABRICATED NEW FLOOR (EXTRUSION P/N S2SDR DHL2007806570Fitting · crackedFOUND MAIN CARGO COMPT FITTING CRACKED 0.750" STA 759.000 L-18R. 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, SRM 51-3-1 PG 2A (TORQUE). REFER TO JC EC-00246-001 (WO 470SDR DHL2007806580Skin · crackedRT WING UPPER EXT SKIN CRACKED 0.250" STA XRS 74.000 S-11 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-2-1 FIG 10 SHEET 1, PG 59-60. CUT OUT DAMAGED SECTION AND FABRICATED DOUBLER (AL7075T6 0.125") AND FILLER PLUG (AL7075T6 0.280") IAW SRM 57-2-1 FIG 10SDR DHL2007806571Fitting · crackedFOUND MAIN CARGO COMPT FITTING CRACKED 1.500" STA 702.875 L-18L. REMOVED CRACKED FITTING IAW SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-120D, SRM 51-3-1 PG 2A (TORQUE). REFER TO JC EC-00246-001 (WO 47SDR DHL2007806575Fitting · crackedMAIN CARGO COMPT FITTING CRACKED 1.500" STA 5.000 RBL 46". REMOVED CRACKED FITTING IAW SRM 51-1-120D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D, SRM 51-3-1 (TORQUE).SDR UPS07849683Finger Doubler · corrodedINSPECTION TYPE:C1 CORROSION AND POSSIBLE STRESS CRACK ON FINGER DOUBLER COCKPIT SUB FLOOR FS -25 TO 8 RBL 22. REMOVED FINGER DOUBLER AT STA -25 TO 8 RBL 22 IAW SRM 51-1-21. FABRICATED AND INSTALLED FINGER DOUBLER AT STA -25 TO 8 RBL 22 IAW DWG5612298, AND SSDR UPS07849681Finger Doubler · corrodedINSPECTION TYPE:C1 SEVERAL AREAS OF CORROSION AND POSSIBLE CRACK IN FINGER DOUBLER COCKPIT SUBFLOOR FS -60, RBL 22. REMOVED CORRODED FINGER DOUBLER AT STA -60 RBL 22 IAW SRM 51-1-21. FABRICATED AND INSTALLED FINGER DOUBLER AT STA -60 RBL22 IAW DWG 5612298, ASDR UPS07849761Fitting · crackedINSPECTION TYPE:C1 LONGERON END FITTING CRACKED AT STA 855 L10R. REMOVED AND REPLACED LONGERON END FITTING IAW SRM 51-1-20D, 51-1-21, AND 51-3-0.SDR UPS07849729Attach Fitting · crackedINSPECTION TYPE:C1 ATTACH FITTING CRACKED AT STA 756 L13L. REMOVED END FITTING AT STA 756 L13L IAW SRM 51-1-20D. LOCATED, DRILLED UP AND INSTALLED REPLACEMENT FITTING AT STA 756 L13L IAW SRM 51-3-2, AND SRM 51-1-20D.SDR UPS07849728Attach Fitting · crackedINSPECTION TYPE:C1 ATTACH FITTING CRACKED AT STA 697 L18L. REMOVED CRACKED END FITTING AT STA 697 L18L IAW SRM 51-1-20D. LOCATED, DRILLED UP, AND INSTALLED END FITTING AT STA 697 L18L IAW SRM 51-3-1, AND SRM 51-1-20D.SDR UPS07849727Attach Fitting · crackedINSPECTION TYPE:C1 ATTACH FITTING CRACKED AT STA 901 L19R. REMOVED CRACKED FITTING AT STA 901 L19R IAW SRM 51-1-20D. LOCATED DRILLED UP, AND INSTALLED REPLACEMENT FITTING AT STA 901 L19R IAW SRM 51-3-2, AND SRM 51-1-20D.SDR UPS07849713Fitting · corrodedINSPECTION TYPE:C1 BOOT FITTING CORRODED AT STA 759 L22R. REMOVED CORRODED BOOT FITTING AT STA 759 L22R IAW SRM 51-1-20D. PROCURED, LOCATED, DRILLED UP, AND INSTALLED BOOT FITTING AT STA 759 L22R IAW SRM 51-1-21, AND SRM 51-1-20D.SDR UPS07849685Fitting · crackedINSPECTION TYPE:C1 T-BOLT BACKUP FITTING CRACKED IN C-PIT TORQUE BOX, STA 1177 L33R UPPER AND LWR FLANGES. REMOVED DAMAGED FITTING AT STA 1177 L33R IAW SRM 51-1-20D. LOCATED DRILLED UP AND INSTALLED FITTING AT STA 1177 L33R IAW SRM 51-3-2 AND SRM 51-01-20D.SDR UPS07849671Fitting · crackedINSPECTION TYPE:C1 ATTACH FITTING CRACKED AT STA 822 L22L. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.SDR UPS07849670Fitting · gougedINSPECTION TYPE:C1 LOWER FWD T-BOLT FITTING GOUGED AT C-PIT DOOR JAM. REMOVED AND REPLACED LWR FWD T-BOLT FITTING IAW SRM 51-3-2.SDR UPS07849630Light · malfunctionedINSPECTION TYPE:N/A BTB - AFTER TAXI, DIMMING LIGHTS NOTICED THAT EMERGENCY EXIT LIGHTING WAS ILLUMINATED IN THE ARMED POSITION WITH A/C POWER ON AIRCRAFT. RESET C/B. OPS CHECK NORMAL PER AMM 33-50-01-2.SDR UPS07849623Light · malfunctionedINSPECTION TYPE:N/A BTB - AFTER TAXI DIMMING LIGHTS NOTICED THAT EMERGENCY EXIT LIGHTING WAS ILLUMINATED IN THE ARMED POSITION WITH A/C POWER ON AIRCRAFT. RESET C/B. OPS CHECK NORMAL PER AMM 33-50-01-2.SDR IXXA070022OConnector · looseDURING FLIGHT FROM KTOL NUMBER 3 FIRE WARNING LIGHT AND FIRE WARNING BELL CAME ON. THE CREW ACCOMPLISHED ALL NECESSARY PROCEDURES AND LANDED WITHOUT INCIDENT IN KLAS. MAINTENANCE PERFORMED VISUAL INSPECTION ON THE NUMBER 3 ENGINE FOR FIRE, NO INDICATION OF F
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