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 engine_model_key = 'CF66D' 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 engine_model_key = 'CF66D' 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 FDEA201007122486Skin · misrepairedEXISTING REPAIR AT FUSELAGE SKIN, STA 1069 TO STA 1099, LONGERON 38R. EXISTING REPAIR AT FUSELAGE SKIN STA 1069 TO STA 1099 LONGERON 38R EVALUATED AND FOUND NOT IN ACCORDANCE WITH ANY SRM REPAIR SCHEME. EXISTING REPAIR DOUBLER REMOVED IAW SRM 51-31-01 VOL II SDR FDEA201007122489Skin · misrepairedEXISTING REPAIR FOUND AT FUSELAGE SKIN RT STA 1199 TO STA 1219 BETWEEN LONGERON 51R AND LONGERON 52. EXISTING REPAIR EVALUATED AND FOUND NOT IAW ANY SRM REPAIR SCHEME. EXISTING REPAIR DOUBLER REMOVED IAW SRM 51-31-01 VO. II, REV. 96 AND REPAIR CARRIED OUT ISDR FDEA201007092437Skin · crackedLT WING FIXED L/E STA XOS 774 SLAT TRACK NR 12 CUT OUT LOWER OTBD CORNER FOUND CRACKED. REPAIRED IAW SRM 57-10-00 FIG 68, VOLUME I, REV 96. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 110.SDR FDEA201007092438Skin · crackedRT WING FIXED L/E STA XOS 774 SLAT TRACK NR 12 CUT OUT LOWER OTBD CORNER FOUND CRACKED. TRIMMED OUT AND REPAIRED IAW SRM 57-10-00, FIG 68, VOL I, REV 96. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100 REV 110.SDR FDEA201007092439Skin · crackedRT WING OTBD FLAP ASSY UPPER SURFACE FOUND CRACKED. REPAIRED IAW SRM 57-10-00 FIG 85, VOL I, REV 96. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 110.SDR FDEA201007082408Skin · dentedLT WING TIP UPPER SURFACE AT FWD SIDE FOUND DENTED. REPAIR CARRIED OUT IAW SRM 57-00-01, FIG 4, VOL I REV 96. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 110.SDR FDEA201007082410Skin · crackedRT OTBD T/E FLAP UPPER SURFACE 01 EACH FOUND CRACKED. ON SKIN LOCATION 12 INCH FROM INBD EDGE, 6 INCH FROM T/E. REPAIR CARRIED OUT IAW SRM 57-10-00, FIG 7, VOL I REV 96. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 110.SDR FDEA201007082411Seat Track · damagedCABIN RT STA 1015 X=-8.5 SEAT TRACK FOUND DAMAGED. CARRIED OUT REPAIR AND SECTION SEAT TRACK REPLACED AT STA 989 TO STA 1029 IAW SRM 53-70-00 FIG 1, REV 96. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 110.SDR FDEA201007082427Skin · crackedRT WING FIXED L/E TELESCOPIC DUCT CUTOUT FOUND CRACKED. REPAIR CARRIED OUT IAW EA NR8-5710-140426, REPAIR IS CLASSIFIED MAJOR IAW GMM 6-2-100, REV 110.SDR FDEA201007082428Access Door · crackedRT WING - WING TIP LOWER SURFACE AFT OF STROBE LIGHT ACCESS DOOR FOUND CRACKED. REPAIR CARRIED OUT IAW EA NR8-5720-138577, REPAIR IS CLASSIFIED MAJOR IAW GMM 6-2-100, REV 110.SDR FDEA201007082429Skin · dentedRT WING - NR 6 SLAT, ENTIRE FWD EXTERIOR SURFACE SKIN FOUND WITH DENTS. NR 6 SLAT ASSY R & R IAW AMM 27-80-01, REV 10. REPAIR CLASSIFIED MINOR IAW GMM 6-2-100, REV 110.SDR FDEA201007082430Skin · dentedRT WING - NR 7 SLAT ENTIRE FWD EXTERIOR SURFACE SKIN FOUND WITH DENTS. SLAT ASSY R & R IAW AMM 27-80-01, REV 10. REPAIR CLASSIFIED MINOR IAW GMM 6-2-100, REV 110.SDR FDEA201007082431Skin · dentedLT WING - NR 6 SLAT, APPROX STA XOS 789 EXTERIOR FWD SKIN FOUND WITH DENT. REPAIRED IAW SRM 57-10-00, FIG 11, VOL I REV 96. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REV 110.SDR FDEA201007082432Skin · dentedLT WING - NR 3 SLAT, APPROX STA XOS 390 TO XOS 440 EXTERIOR FWD SKIN FOUND WITH DENTS. R & R IAW AMM 27-80-01, REV 10. REPAIR CLASSIFIED MINOR IAW GMM 6-2-100, REV 110.SDR FDEA201007082433Skin · dentedLT WING INBD FLAP ASSY LOWER SURFACE, INBD LOWER SEGMENT FOUND WITH DENTS. TRIMMED OFF AND REPAIRED IAW SRM 57-10-00, FIG 3, VOL I, REV 96. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100 REV 110.SDR FDEA201007082434Skin · dentedLT WING INBD FLAP ASSY LOWER SURFACE, OTBD LOWER SEGMENT FOUND WITH DENTS. REPAIRED IAW SRM 57-10-00, FIG 3, VOLUME I, REV 96. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 110.SDR FDEA201007082465Fitting · crackedNR 6 SPOOL FITTING LOCATION HAS CRACK INDICATIONS AT HOLES "A", "B", "C" AND "D". R & R NR 6 SPOOL FITTING IAW SRM 51-31-01, VOL I, SRM 53-50-00, FIG 17, VOL I AND EA 8-5310-123543 "FUSELAGE -JAMB LOWER SILL OVERSIZE HOLES AT NR 1 -NR 7 SPOOL FITTING LOCATIOSDR FDEA201007062350Skin · corrodedCABIN RT STA 1189 XCW=-100 - XCW=-117 CTR WING UPPER PANEL FOUND CORRODED. CORROSION REMOVED IAW SRM 51-21-01 VOL II, REV 96. ORIGINAL THICKNESS = 0.139", REMAINING THICKNESS = 0.107", MATERIAL REMOVED = 0.032" FOUND EXCEEDED LIMIT IAW SRM 57-20-00, FIG 8A SDR FDEA201007062351Skin · corrodedCABIN RT STATION 1195 XCW=-100 - XCW=-117 CTR WING UPPER PANEL FOUND CORRODED. CORROSION REMOVED IAW SRM 51-21-01, VOL II, REV. 96. FOUND EXCEED LIMIT IAW SRM 57-20-00 FIG 8A, VOL I, REV 96.ORIGINAL THICKNESS: 0.143", REMAINING THICKNESS: 0.106", MATERIAL SDR FDEA201007062352Skin · corrodedCABIN RT STATION 1205 XCW=-100 - XCW=-117 CTR WING UPPER PANEL FOUND CORRODED. CORROSION REMOVED IAW SRM 51-21-01, VOL II, REV I 96. ORIGINAL THICKNESS = 0.142", REMAINING THICKNESS = 0.110", MATERIAL REMOVED = 0.032" FOUND EXCEEDED LIMIT IAW SRM 57-20-00SDR FDEA201007062353Skin · corrodedCABIN RT STATION 1212 XCW=-100 - XCW=-117 CTR WING UPPER PANEL FOUND CORRODED. CORROSION REMOVED IAW SRM 51-21-01 VOL II REV 96. ORIGINAL THICKNESS:0.149", MATERIAL REMOVED: 0.040", REMAINING THICKNESS: 0.109" FOUND EXCEED LIMIT IAW SRM 57-20-00, FIG 8A, SDR FDEA201007062354Skin · corrodedCABIN RT STATION 1219 XCW=-100 - XCW=-117 CTR WING UPPER PANEL FOUND CORRODED. CORROSION REMOVED IAW SRM 51-21-01, VOL II REV 96. ORIGINAL THICKNESS = 0.147", REMAINING THICKNESS = 0.113", MATERIAL REMOVED = 0.034" FOUND EXCEEDED LIMIT IAW SRM 57-20-00, FIG SDR FDEA201007062355Skin · corrodedCABIN RT STA 1229 XCW=-97 - XCW=-105 CTR WING UPPER PANEL FOUND CORRODED. CORROSION REMOVED IAW SRM 51-21-01, VOL II, REV 96. ORIGINAL THICKNESS = 0.147", REMAINING THICKNESS = 0.125", MATERIAL REMOVED = 0.022" FOUND EXCEEDED LI REPAIR IS CLASSIFIED AS MISDR FDEA201007062357Skin · corrodedCABIN LT STATION 1181 XCW=109 - XCW=111 CTR WING UPPER PANEL FOUND CORROSION. CORROSION REMOVED IAW SRM 51-21-01, VOL II, REV 96. ORIGINAL THICKNESS = 0.133", REMAINING THICKNESS = 0.098", MATERIAL REMOVED = 0.035" FOUND EXCEEDED LIMIT IAW SRM 57-20-00, FIGSDR FDEA201007062358Skin · corrodedCABIN LT STA 1189 XCW=108 - XCW=111 CTR WING UPPER PANEL FOUND CORROSION. CORROSION REMOVED IAW SRM 51-21-01, VOL II, REV 96. ORIGINAL THICKNESS = 0.132", REMAINING THICKNESS = 0.105", MATERIAL REMOVED = 0.027" FOUND EXCEEDED LIMIT IAW SRM 57-20-00, FIG 8A,SDR FDEA201007062359Skin · corrodedCABIN LT STA 1195 XCW=108 - XCW=114 CTR WING UPPER PANEL FOUND CORROSION. CORROSION REMOVED IAW SRM 51-21-01, VOL II REV 96. ORIGINAL THICKNESS = 0.133", REMAINING THICKNESS = 0.112", MATERIAL REMOVED = 0.021" FOUND EXCEEDED LIMIT IAW SRM 57-20-00, FIG 8A, SDR FDEA201007062360Skin · corrodedCABIN LT STATION 1205 XCW=108 - XCW=117 CTR WING UPPER PANEL FOUND CORRODED. CORROSION REMOVED IAW SRM 51-21-01, VOL II, REV 96. ORIGINAL THICKNESS = 0.132", REMAINING THICKNESS = 0.106", MATERIAL REMOVED = 0.032" FOUND EXCEEDED LIMIT IAW SRM 57-20-00, FIG SDR FDEA201007062361Skin · corrodedCABIN LT STATION 1212 XCW=105 - XCW=117 CTR WING UPPER PANEL FOUND CORRODED. CORROSION REMOVED IAW SRM 51-21-01, VOL II, REV 96. ORIGINAL THICKNESS = 0.143", REMAINING THICKNESS = 0.102", MATERIAL REMOVED = 0.041" FOUND EXCEEDED LIMIT IAW SRM 57-20-00, FSDR FDEA201007062362Skin · corrodedCABIN LT STATION 1219 XCW=105 - XCW=117 CTR WING UPPER PANEL FOUND CORRODED. CORROSION REMOVED IAW SRM 51-21-01 VOL II REV 96. ORIGINAL THICKNESS = 0.148", REMAINING THICKNESS = 0.121", MATERIAL REMOVED = 0.027" FOUND EXCEEDED LIMIT IAW SRM 57-20-00, FIG SDR FDEA201007062363Skin · corrodedCABIN LT STATION 1229 XCW=105 - XCW=117 CTR WING UPPER PANEL FOUND CORRODED. CORROSION REMOVED IAW SRM 51-21-01 VOL II, REV 96. ORIGINAL THICKNESS = 0.151", REMAINING THICKNESS = 0.120", MATERIAL REMOVED = 0.031" FOUND EXCEEDED LIMIT IAW SRM 57-20-00, FIG 8SDR FDEA201007062364Skin · corrodedCABIN LT STATION 1236 XCW=104 - XCW=117 CTR WING UPPER PANEL FOUND CORRODED. CORROSION REMOVED IAW SRM 51-21-01 VOL II, REV 96. ORIGINAL THICKNESS = 0.155", REMAINING THICKNESS = 0.121", MATERIAL REMOVED = 0.034" FOUND EXCEEDED LIMIT IAW SRM 57-20-00, FIG 8SDR FDEA201007062365Skin · corrodedCABIN LT STATION 1229 XCW=105 - XCW=117 CTR WING UPPER AFT PANEL FOUND CORRODED. CORROSION REMOVED IAW SRM 51-21-01 VOL II REV 96. ORIGINAL THICKNESS = 0.150", REMAINING THICKNESS = 0.131", MATERIAL REMOVED = 0.019" FOUND EXCEEDED LIMIT IAW SRM 57-20-00, FIGSDR FDEA201007062374Longeron · corrodedCABIN - LONGERON 19 LT FROM STA 1381 TO STA 1401 CORRODED. R & R IAW SRM 51-31-01 VOLUME II, REVISION 96. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 110.SDR FDEA201007062376Longeron · corrodedCABIN - LONGERON 17 LT FROM STA 1421 TO STA 1441 CORRODED. R & R IAW SRM 51-31-01 VOLUME II, REVISION 96. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 110.SDR FDEA201007022314Skin · crackedRT WING ANTI ICE TELESCOPIC DUCT DOOR CUT OUT SKIN FOUND CRACKED. RT WING ANTI ICE TELESCOPIC DUCT DOOR CUT OUT SKIN REPAIRED IAW EA NR 8-5710-132442, TITLE: WINGS - RT WING ANTI-ICING TELESCOPIC DUCT DOOR CUTOUT - REPAIR. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-SDR FDEA201007022315Skin · deformedRT WING OTBD T/E FLAP INBD LOWER EDGE FOUND DEFORMED. RT WING OTBD T/E FLAP INBD LOWER EDGE REPAIRED IAW SRM 57-10-00, FIG 7, VOLUME I, REVISION 96. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 110 SKIN.SDR FDEA201007022316Slat Track · chafedLT WING NR 6 SLAT TRACK CHAFING WITH OTBD ATTACHED RIB FITTING. R & R IAW SRM 51-31-01 VOLUME I, REV 96. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 110.SDR FDEA201007012307Floor Panel · delaminatedFWD CARGO PIT FLOOR PANEL 123 TF IS DELAMINATED. FABRICATED NEW FWD CARGO PIT FLOOR PANEL 123 TF IAW FEDEX DWG SRZ 25-005, REV "H".SDR FDEA201007012297Skin · damagedFUSELAGE - FD CARGO DOOR CUT-OUT AFT LOWER MID AREA EXTERIOR SKIN FOUND DAMAGED. FWD CARGO DOOR CUTOUT AFT LOWER MID DAMAGED AREA TRIMMED OUT AS PER SRM 53-50-00 FIG 26 VOL 1 REV. 96. TRIMMED OUT AREA IS 1" X 9.5". REPAIR DOUBLER AND FILLER FABRICATED AND INSSDR FDEA201006292221Skin · bentLOWER EXTERNAL FUSELAGE; FWD CARGO DOOR; FWD EDGE OF DOOR CUTOUT IS BENT AT FS 879 BETWEEN LONGERONS 42R & 43R.SDR FDEA201006282213Stringer · corrodedFWS CARGO BILGE AREA AT FR 899 AND STR 52. STRINGER HAS EXFOLIATION CORROSION. REMOVED SPLICE IAW SRM 51-21-01. REMOVED COROOSION IAW SRM 51-21-10. FABRICATED PARTS LONGERON REPAIR AND SPLICE REPAIR ON TRAVELER T10/838926 AND T10/838928. LOCATED AND DRILLESDR FDEA201006282214Skin · gougedFWD CARGO AT AFT FUSELAGE CUT OUT LOWER CORNER DOUBLER INSTALLED HAS GOUGE. REPAIRED CORNER IAW SRM 53-50-00. DOUBLER AND TRIPLER, DOUBLER FROM 2024-T3 .071 BATCH 182963, TRIPLER FROM 2024 T3 .080 BATCH 1747937.SDR FDEA201006262191Stiffener · crackedSTIFFENER CRACKED, NR 3 AC BAY AFT PRESSURE BULKHEAD FS 595.0. REPAIRED STIFFENER IAW SRM 53-00-01 FIG 7 CLASSIFIED AS A MAJOR REPAIR.SDR FDEA201006252171Floor Panel · puncturedMAIN CARGO COMPARTMENT FLOOR PANEL IS PUNCTURED AT STA 1521; 15 INCHES RT OF C/L. FABRICATED NEW MAIN CARGO COMPARTMENT FLOOR PANEL STA.1521, 15" RH OF C/L IAW SRZ25-005 REV.H. INSTALLED NEW FLOORBOARD IAW MM 53-21-08-2. APPLIED HOT MELT IAW MM 53-21-08-2SDR FDEA201006232117Skin · dentedRT WING INBD FLAP LOWER SKIN IS DENTED. CHECKED ALL DENTS IAW MD/DC10 SRM 57-10-00, FIG 48, PG 162A, VOL I. ALL DENTS BETWEEN XIFH 192 TO XIFH 199 AND YIFH 39 TO YIFH 51 ARE WITHIN LIMITS. DENT AT XIFH 201 AND YIFH 72 IS CREASED OUT OF LIMITS. BLENDED OUSDR FDEA201006222104Skin · crackedLT WING FIXED L/E NR 3 SLAT TELESCOPIC UPPER DOOR CUTOUT OTBD AREA FOUND CRACKED. REPAIR CARRIED OUT IAW EA NR 8-5710-132424, REPAIR IS CLASSIFIED MAJOR IAW GMM 6-2-100, REV 110.SDR FDEA201006222105Skin · crackedRT FIXED L/E NR 3 SLAT TELESCOPIC DUCT UPPER DOOR CUTOUT FOUND CRACKED. REPAIR CARRIED OUT IAW EA 8-5710-132425. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-110, REV 110.SDR FDEA201006222115Seat Track · damagedCABIN LT STATION 1119 X=47.5 SEAT TRACK FOUND DAMAGED. DAMAGED SEAT TRACK AT CABIN STATION 1119 X=47.5 LT AREA CARRIED OUT REPAIR AND SECTION SEAT TRACK REPLACED AT STATION 1109 TO STATION 1129 X=47.5 IAW SRM 53-70-00, FIG 1, VOL I, REV 96. REPAIR CLASSIFIEDSDR FDEA201006212094Latch · wornNR 2 ENGINE PYLON ACCESS PANEL, 457 CL ON LT SIDE HAS WORN LATCHES. LATCH LANDS FOUND TO BE OUT OF LIMITS IAW SRM 54-00-01, VOL I. FABRICATED NEW DOUBLER AND INSTALLED IAW DAC DWG AVB7332 AND SRM 51-33-01, VOL II.SDR FDEA201006182060Hinge Fitting · corrodedLT OTBD FLAP; OTBD HINGE FITTING LOCATION NR3 OTBD BORE IS CORRODED. REPAIRED FLAP HINGE FITTING NR 3 OTBD BORE IAW EA NR 8-5740-136666.
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