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 IPXA09855673Skin · misrepairedINSPECTION TYPE:SV SURVEY SEQ 852-F1-36, FUSE PLUG REPAIR ATTACH FASTENERS SPACING LESS THAN 4D STA 1364 BETWEEN L22R-L23R. REPAIR ACCOMPLISHED PER DC8 SRM 53-2-1 FIG 7 SHT 11 AND T/R53-203.SDR IPXA09855672Structure · misrepairedINSPECTION TYPE:SV SURVEY SEQ 852-S1-04, LT HORIZ STAB L/E, DOES NOT CORRELATE TO SRM, DOUBLER GAGE THICKER THAN SRM CALLOUT. REPAIR ACCOMPLISHED PER DC8 SRM 55-2-1 FIG 4.SDR IPXA09855610Skin · damagedINSPECTION TYPE:SV SURVEY SEQ 852-W4-15 REPAIR DOUBLER HAS FASTENERS WITH SHORT EDGE DISTANCE, RT OTBD L/E LOWER SKIN XFS 712. REPAIR ACCOMPLISHED PER REO-G12675 REV A AND EO DC8-5720-33123-A.SDR IPXA09855608Access Panel · damagedINSPECTION TYPE:SV SURVEY SEQ 852-WS-35 LT WING L/E LOWER SURFACE ACCESS PANEL XFS 502 RE PAIR DOUBLER IS .071 BASE STRUCTURE IS .100. INSTALLED REPAIR PER DAC DWG 5761041-3.SDR IPXA09855607Access Panel · damagedINSPECTION TYPE:SV SURVEY SEQ 852-W3-34-LT WING L/E LOWER SURFACE ACCESS PANEL, XFS 476 EX EXISTING REPAIR DOUBLER IS .071 AND BASE MATERIAL IS .100. INSTALLED REPAIR PER DAC DWG 5761041.SDR IPXA09855654Skin · misrepairedINSPECTION TYPE:SV 852-W4-13 REPAIR DOUBLER CRACKED. RIGHT L/E LOWER SKIN ABOVE NR 4 PYLON XFS 530 35 INCHES FWD OF WING FRONT SPAR. REPAIRED PER DC8 SRM 57-2-01A FIG 2.SDR IPXA09855638Skin · misrepairedINSPECTION TYPE:SV SSN 852-F1-03 REPAIR CONFIGURATION DOES NOT CORRELATE TO A SRM REPAIR. REPAIR ACCOMPLISHED IAW SRM 53-2-0 FIG 1D SHT 3.SDR IPXA09855637Skin · crackedINSPECTION TYPE:SV SSN 852-W4-13 REPAIR DOUBLER CRACKED RT LEAD EDGE LWR SKIN ABOVE NR 4 PYLON XFS 530 35 INCH FWD OF WING FWD SPAR. REPAIR ACCOMPLISHED IAW DC8 SRM 57-02-01A FIG 2 SHT 1.SDR IPXA09855640Cusp Web · crackedINSPECTION TYPE:SV MAIN CABIN CUSP MEMBRANE CRACKED AT FS 1613 RBL57. REPAIR ACCOMPLISHED IAW DC8 SRM 53-2-0 FIG 25 SHT 4 AND TR53-166.SDR IPXA09855635Web · crackedINSPECTION TYPE:SV EFN 85220011042 C PIT RT TUNNEL SUBFLOOR MEMBRANE IS EXFOLIATED AND CRACKED AT RBL 60 BETWEEN FS 1100 AND FS 1120. REMOVED DAMAGE AND FABRICATED DOUBLER PER EO DC8-5330-2159-B. REPAIR ACCOMPLISHED IAW DC8 SRM 53-2-0 FIG 25 SHEETS 4 AND 5 ASDR IPXA09855634Cusp Web · crackedINSPECTION TYPE:SV EFN 85220011031 RT UPPER CUSP MEMBRANE CRACKED BETWEEN FS 1600 TO FS 1620. REPAIRED CRACK IN CUSP MEMBRANE PER EO DC8-5330-2159 -B. REPAIR ACCOMPLISHED IAW DC8 SRM 53-2-0 FIG 25 SHT 4 TR53-166.SDR IPXA09855633Web · puncturedINSPECTION TYPE:SV EFN 85219971087 MAIN CABIN .75 IN PUNCTURED IN MEMBRANE FS 132 RBL65. FABBED AND INSTALLED REPAIR DOUBLER AT CUSP MEMBRANE PER DC8 -5332-2159. REPAIR ACCOMPLISHED IAW SRM 53-2-0 FIG 25 SHT 4 TR53-166.SDR IPXA09855632Cusp Web · damagedINSPECTION TYPE:SV EFN 85219971055 LT CUSP FROM FS 120 TO FS 130 DAMAGED. REPAIRED DAMAGED CUSP PER UPS EO DC8-5330-2159-B. REPAIR ACCOMPLISHED IAW DC8 SRM 53-2-0 FIG 25 SHT 4 TR53-166.SDR IPXA09855631Web · crackedINSPECTION TYPE:SV EFN 85219971054 HEAVY CORROSION AND CRACK IN FLOOR WEB LT CUSP AREA EXTENDING UNDER FLOOR SUPPORT FITTING FROM FS 260 TO FS 280. REPAIR ACCOMPLISHED IAW SRM 53-2-0 FIG 25 SHT 4 TR53-166.SDR IPXA09855630Cusp Web · crackedINSPECTION TYPE:SV EFN 852 19971053 CUSP IS CRACKED FROM LT FS 80 TO FS 100 IN FWD PIT. REPAIRED DAMAGE TO CUSP MEMBRANE PER UPS EO DC8-5330-2159 -B. REPAIR ACCOMPLISHED IAW DC8 SRM 53-20-0 FIG 25 SHT 4 TR53-166.SDR IPXA09855645Skin · misrepairedINSPECTION TYPE:SV SEQ NR 852-F1-33 DOES NOT CORRELATE TO SRM REPAIR. REPAIRED PER DC8 SRM 53-2-1 FIG 7 SHEETS 13 AND 14, TR 53-203.SDR IPXA09855644Skin · misrepairedINSPECTION TYPE:SV SURVEY SEQUENCE 852-F1-25, REPAIR DOUBLER AT STA 1749 BETWEEN L19L AND L20L, DOES NOT CORRELATE TO SRM REPAIR. REPAIRED PER DC8 SRM 53-2-1 FIG 7 SHEETS 11 AND 13 + TR 53-203.SDR IPXA09855643Skin · misrepairedINSPECTION TYPE:SV SURVEY SEQUENCE 852-F1-24, VENT REPAIR DOUBLER, STA 1718.5 BETWEEN L18 L AND L19L DOES NOT CORRELATE TO SRM REPAIR. REPAIRED PER DC8 SRM 53-2-1 FIG 7 SHEET 11 AND 13 + TR 53-203.SDR IPXA09855655Doubler · damagedINSPECTION TYPE:SV 852-W4-10 REPAIR DOUBLER CHAFED/GOUGED AND HAS FASTENERS WITH SHORT E D RT WING LEADING EDGE LOWER SKIN XFS 257, 47 INCHES FWD OF WING FRONT SPAR (ABOVE NR 3 PYLON). REPAIRED PER DC8 SRM 57-2-1A FIG 2.SDR IPXA09855653Skin · misrepairedINSPECTION TYPE:SV SURVEY SEQUENCE 852-W3-20, REPAIR DOUBLER AT LEFT I/B FLAP UPPER SKIN DOES NOT CORRELATE TO SRM. REPAIRED PER DC8 SRM 57-02-01 FIG 002Q SHT 1.SDR IPXA09855641Skin · misrepairedINSPECTION TYPE:SV SURVEY SEQ 852-W3-20 REPAIR DOUBLER AT LT INBD FLAP UPPER SKIN DOES NOT CORRELATE TO SRM. REPAIR ACCOMPLISHED IAW DC8 SRM 57-2-1 FIG 2Q SHT 1.SDR IPXA09855639Skin · misrepairedINSPECTION TYPE:SV SSN 852-F1-01 REPAIR DOES NOT CORRELATE WITH SRM REFERENCES. REPAIR ACCOMPLISHED IAW DC8 SRM 53-2-0 FIG 1D SHT 3.SDR IPXA09855636Skin · damagedINSPECTION TYPE:SV SSN 852-W4-10 REPAIR DOUBLER CHAFED/GOUGED AND HAS FASTENERS WITH SHORT ED RT WING LEAD, EDGE LWR SKIN XFS 257 47 INCH, FWD OF WING FWD SPAR ABOVE NR 3 PYLON. REPAIR ACCOMPLISHED IAW DC8 SRM 57-2-1A FIG 2.SDR DHLA2009801006Angle · corrodedLT MLG WW ANGLE CORRODED, STA XCW 46.000 (NEAR REAR SPAR UPPER PART) PERFORMED MAJOR REPAIR IAW BOEING MSG NR SEU XXX-09-0024-02B DATED 04-20-09, SRM 57-1-0 PG.1. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-0 PG.16. REMOVED CSDR IPXA09855642Skin · misrepairedINSPECTION TYPE:SV SEQ NR 852-F1-05, FLUSH REPAIR, FASTENERS 2 IN FILLER COUNTERSINKS DEEP. REPAIRED PER DC8 SRM 53-2-1 FIG 7 SHT 15 (TR 53-203) ESTABLISH REPETITIVE INSPECTIVE PER SRM 53-2-1 FIG 5 (TR 53-190) 53-2-1 PF 35 AND 51-5-5 PG 1 PAR 2A(1).SDR DHLA2009801008Skin · corrodedNR 4 STUB WING UPPER EXTERNAL SKIN CORRODED, STA.XFS 530.000. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3,09191 DATED 04-30-09, EVA DB57-00258 REV IR DATED 04-22-09, DWG ED9935 DATED 04-16-09. REMOVED FASTENERS IAW SRM 51-3-0, SRM 51-1-21, SRM 51-1-700. REMOSDR IPXA09855536Shear Tie · damagedINSPECTION TYPE:SV SHEAR TIE AT STA 480 L20R-L19R FOUND TO HAVE A DENT AND CRACKED. REPAIR SHEAR TIE PER DAC DWG 3779767.SDR IPXA09855531Skin Panel · misrepairedINSPECTION TYPE:SV SURVEY SEQ 814-F1-18 EXT FUSELAGE DOUBLER AT BS 165 TO BS 143 L13R HAS 6EA FASTENERS EDGE DISTANCE LESS THAN 1.5 FASTENER DIAMETER. REPAIR ACCOMPLISHED PER RE0-G12670 REV A AND UPS EO DC8-5320-32844-A.SDR IXXA09SMN066SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR AT STATION 220.000-240.000 LONGERON 28-31 LEFT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN, INTERNAL, AND EXTERNAL DOUBLERS. CLEANED, TREATED, PRIMED SDR IXXA09SMN065SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR AT STATION 480.000 LONGERON 23-24 RIGHT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN, INTERNAL, AND EXTERNAL DOUBLERS. CLEANED, TREATED, PRIMED AREA, ASDR DHLA2009801010Skin · damagedRT WING CTR L/E REPAIR DOUBLER HOLES ELONGATED, STA X0LDO 67.000. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 09175 DATED 04-28-09, EVA DE53-00257 REV IR DATED 04-21-09, DWG ED 4934 DATED 04-15-09. REMOVED DAMAGED REPAIR DOUBLER IAW SRM 51-1-21, SRM 51-1-2SDR DHLA2009801005Spar Cap · crackedLT LWR WING FRONT SPAR CAP AT L/E ATTACH HOLE SHOWS A 0.500 INCH LENGTH CRACK, STA XFE 523.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8100-9 DATED 05-7-09, EVA D857-00261 REV IA DATED 04-27-09, REPAIR SKETCH 200904200125 DWG J060232, JCT04316 REMSDR IPXA09855795Rib · crackedINSPECTION TYPE:SV LT WING L/E (XFS 309) SUPPORT RIB CRACKED AND REPAIR DOUBLER IS CRACKED. REMOVED AND REPLACED REPAIR PER DC8 SRM 57-2-0 FIG 2 SHT 2.SDR IXXA09SMN059SLongeron Splice · crackedDURING ROUTINE C CHECK INSPECTION, FOUND AFT FUSELAGE SPLICE FITTING CRACKED AT STATION 1770.000 LONGERON 17 RIGHT. REMOVED CRACKED FITTING. INSTALLED NEW SPLICE FITTING IAW SRM 51-1-20D, SRM 51-1-21, AND SRM 51-3-1.SDR IXXA090015OFan · defectiveDURING CRUISE FROM KPHL, THE CREW DETECTED SMOKE FROM THE RECIRCULATION FAN AND NOISY. THE CREW TURNED OFF RECIRCULATION FAN SMOKE ODOR DISSIPATED. THE CREW LANDED IN KEWR WITHOUT FURTHER INCIDENT. MAINTENANCE IN KEWR REPLACED THE RECIRCULATION FAN. OPERATSDR DHLA2009801003Heat Exchanger · crackedLT PRIMARY HEAT EXCHANGER AFT LWR CORNER CRACKED 3/7 INCH STA-12.000 L-27L TO 28L. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 09181 DATED 04-29-09 EVD DB53-00256 REV IR DATED 04-21-09 SEMAN DWG NR ED-4933 DATED 04-13-09. REMOVED FASTENERS IAW SRM 51-1-21SDR DHLA200900024Flashlight · inoperativeEMERGENCY FLASHLIGHT IN LAV INOP. REMOVED AND REPLACED FLASHLIGHT IAW DC-8 MMS 25-60-62, OPS CHECKS GOOD P/N 3800.SDR IXXA09SMN64SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND FORWARD ACCESSORY COMPARTMENT FITTING CRACKED AT STATION 55.000 RIGHT BOTTOM LINE 45. REMOVED CRACKED FITTING. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D, SRM 51-3-1, ATI REPAIR SPECIFICATION 2003-5, AND SEMAN FORM-07SDR DHLA2009801012Skin · delaminatedNR 3 RT SPOILER PANEL EXTERNAL SKIN DELAMINATED (STA XRS 162.000 - 230.000). CUT OUT DELAMINATED AREA IAW SRM 57-2-3 PG 33 FIG 4D PAR 23. FABRICATED REPAIR PLUG AND CORE IAW SRM 57-1-1 PG 15,SRM 57-2-3 PAR.23.6,SRM 57-2-0 PAR. 4. PERFORMED CLEANING IAW SRMSDR DHLA2009801011Cargo Track · wornUPPER CARGO COMPARTMENT NR 5 TRACK SEGMENT LUGS WORN STA 1680.000-1700.000. MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW SRM 53-2-3 FIG. 14 SHEET 1 PG. 49-50. REMOVED WORN TRACK SEGMENT AND EXISTING SPLICES IAW SRM 53-1-0 PG. 1, SRM 51-3-0. FABRICATED NEW TRASDR DHLA2009801009Vane · delaminatedNR 3 LT FLAP VANE INTERNAL SKIN DELAMINATED (STA XF 160.000 - 213.000). REMOVED AND REPLACED NR 3 FLAP VANE IAW MM 27-51-14 PG 201-203.SDR DHLA2009801002Skin · delaminatedRT WING, PANEL NR 577A EXTERNAL SKIN DELAMINATED. REMOVED AND REPLACED WING PANEL NR 577A IAW SRM 51-3-0, SRM 51-3-1.SDR DHLA2009801001Skin · delaminatedLT WING PANEL EXT SKIN DELAMINATED (STA XW 0 - XW 37.000). REMOVED AND REPLACED DELAMINATED LT WING PANEL IAW SRM 51-3-0 SRM 51-3-1.SDR IXXA09SMN058SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND FORWARD ACCESSORY COMPARTMENT FITTING CRACKED AT STATION 55.000 RIGHT BUTTOCKS LINE 45. REMOVED CRACKED FITTING. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D, SRM 51-3-1, ATI REPAIR SPECIFICATION 2003-5, AND SMN-FORM-0SDR DHLA2009801007Doubler · brokenFUSELAGE NOSE SECTION, INTERNAL DOUBLER BROKEN AT STA 156.00, L-36 (REF ACCESS NR 2). MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 09218 DATED 05-11-09, EVA DB53-00259 REV IR DATED 04-22-09, SEMAN DWG ED 4932 DATED 04-14-09. CUT DAMAGED SECTISDR IXXA09SMN055SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND AFT CARGO COMPARTMENT FITTING CRACKED AT STATION 1280.000 LONGERON 35LEFT. REMOVED CRACKED FITTING. CLEANED, TREATED, AND PRIMED AREA. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D, SRM 51-3-4, AND DC8 SRM 51-1-8B.SDR IXXA09SMN054SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND AFT CARGO COMPARTMENT FITTING CRACKED AT STATION 1280.000 LONGERON 35 RT. REMOVED CRACKED FITTING. CLEANED, TREATED, AND PRIMED AREA. INSTALLED NEW FITTING IAW SRM 51-1-20D, SRM 51-3-4, AND SRM 51-1-8B.SDR IXXA09SMN057SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND FORWARD ACCESSORY COMPARTMENT FITTING CRACKED AT STATION 65.000 LONGERON 21 RIGHT. REMOVED CRACKED FITTING. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D, SRM 51-3-1, ATI REPAIR SPECIFICATION 2003-5, AND SMN-FORM-07 IPI SDR IXXA09SMN056SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND FORWARD ACCESSORY COMPARTMENT FITTING CRACKED AT STATION 70.000 LONGERON 21 RIGHT- RIGHT BOTTOM LONE 50. REMOVED CRACKED FITTING. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D, SRM 51-3-1, ATI REPAIR SPECIFICATION 2003-5SDR IXXA09SMN062SStructure · crackedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT HORIZONTAL STABILIZER CAP CRACKED STATION XE 29.812. REMOVED CRACKED CAP. INSTALLED NEW CAP IAW SRM 51-1-20D, SRM 51-3-1, ATI REPAIR SPECIFICATION NUMBER 2003-05, AND SMN-FORM-07 IPI NUMBER 2009420.
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