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 = '72725' 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 = '72725' 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 95FDEA01442Spar · corrodedWHILE WORKING CUST ID NR0443, FOUND CORROSION EVIDENCE ON LT WING FRONT UPPER SPAR CHORD UPPER SURFACE AT SIX FASTENER HOLES, LES 331.7 - LES 339.7. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PARTS IAW FEDEX SRM 57-30-4 AND EA NR 7-5710-25816. AT SDR 95FDEA01441Frame · corrodedCORROSION ON INSIDE SKIN AND NOSE DOOR CUT OUT FRAME AT BS 211, LBL 19, WL 172. FOUND ADDITIONAL CORROSION ON WEB BETWEEN BS 203-219, LBL 15, ON L-ANGLE FOR SAME WEB, ON WEB FOR FRAME AT BS 211, LBL 16. FABRICATED NEW WEB AND L-ANGLE FOR BS 203-219, LBL 15, SDR 95FDEA01440Frame · corrodedCORROSION ON UPPER CHORD BS 950, WL 208, RBL 12, 45 AND LBL 25. FOUND ADDITIONAL CORROSION AT LBL 11. REMOVED CORROSION FROM ALL AREAS. FOUND AREAS AT LBL 11, 25 TO BE WITHIN LIMITS. AREA AT RBL 12, 48 WERE FOUND OUT OF LIMITS. REPAIRED AREAS AT RBL 12 ANSDR 95FDEA01439Frame · corrodedCORROSION FOUND ON FRAME AT STA 580, WL 156-172, LBL 26-45 AROUND NUT PLATES (MARKED). REMOVED CORROSION ON FRAME BS 580, STR 24 LT. FABRICATED NEW SPLICE PLATE. TREATED REWORKED AREA AND INSTALLED REPAIR PARTS IAW FEDEX EA 7-5310-25825.SDR 95FDEA01438Frame · crackedPOSSIBLE CRACK FOUND IN FRAME AT STA 620, RBL 60, WL 190. CONFIRMED CRACK. CUT OUT DAMAGE, FABRICATED REPAIR PARTS AND INSTALLED PER FEDEX EA NR 7-5310-25817.SDR EISA95417Sensing Tube · bentSMOKE DETECTOR SENSING TUBE BENT LT SIDE COMP 1. REMOVED DAMAGE PER MM 20-10-5. FABRICATED NEW TUBE PER MM 26-17-0 AND BPS 5001. INSTALLED AND SECURED PER MM 26-17-0 AND SRM 51-30-2. (X)SDR EISA95415Sensing Tube · bentSMOKE DETECTION SENSING TUBE BEN RIGHT SIDE COMP 2. REMOVED DAMAGES SECTION OF TUBING PER MM 20-10-5 REPOSITIONED PER ANI CARGO DOOR MANUAL PG 17 FIG 6. (M)SDR EISA95414Skin · open holesBS 560 STRINGER 21L UPPER AND LOWER FLANGES, HAVE OPEN HOLES ADJACENT TO FASTENER HOLES. REPAIRED IAW SRM 53-10-3 FIG 2. (M)SDR 95FDEA01427Frame · corrodedCORROSION FOUND ON FRAME, STA 660 WL 156 LBL 26 AROUND NUTPLATE. FOUND CORROSION OUT OF LIMITS, CUT OUT DAMAGE AND REPAIRED PER FEDEX EA NR 7-5310-25826.SDR 95FDEA01405Fail-Safe · crackedCRACKED FAIL-SAFE ON BS 337 FRAME WL 171 LBL 50. REMOVED CRACKED FAIL-SAFE ON BS 337 FRAME, FABRICATED NEW FAIL-SAFE, TRIMMED, BACK DRILLED, ALODINED, PRIMERED, AND PAINTED IAW FEDEX SRM 53-10-2, 51-30-2 AND MM 51-20-2, INSTALLED WET WITH SEALANT.SDR 95FDEA01403Frame · crackedCRACK IN FRAME EMANATING FROM TOOLING HOLE AT BS 312 LBL 47 WL 175. REMOVED CRACKED FRAME AT BS 312 LBL 47 WL 175. RELEVELED NEW FRAME, DRILLED, ALODINED, PRIMED AND INSTALLED PER FEDEX SRM 51-20-1, 51-10-02, 51-30-02.SDR 95FDEA01402Skin · damagedLIGHTNING STRIKE STA 910 BETWEEN STR 1 TO 2L. SKIN AND TEAR STRAP DAMAGE WAS BEYOND REPAIRABLE LIMITS PER FEDEX SRM 53-30-1. INSTALLED SKIN AND TEAR STRAP REPAIR IAW FEDEX SRM 53-30-3 AND 53-30-4 BS 910 BETWEEN STR 1 TO 2L.SDR 95FDEA01404Clip · crackedWHILE PERFORMING INSPECTION PER EO 7-5310-7-2354, NOTED CRACK INDICATION IN LOWER HOLE STR 28L BS 1166. FURTHER INSPECTION REVEALED CRACK WAS LIMITED TO STR CLIP ONLY. REMOVED AND REPLACED STR CLIP REF SRM 51-30-2.SDR EISA95409Skin · corrosionFUSE EXT BS 360-380 STRINGERS 17L-19L SKIN HAS PILLOWING. REMOVED CORROSION IAW 51-10-6. INSTALLED DOUBLER IAW SRM 51-30-2. (M)SDR 95FDEA01362Rib · crackedRT HORIZONTAL STAB NR 5 HINGE SUPPORT FITTING CRACKED AT LOWER TRAILING EDGE BEAM ATTACH POINT. REMOVED WIPER PLATES TO GAIN ACCESS TO RT HORIZONTAL STAB HINGE SUPPORT RIB. REPAIRED RIB IAW FEDEX SRM 55-10-4 AND REINSTALLED WIPER PLATES IAW FEDEX SRM 51-30-2SDR 95FDEA01361Floorbeam · corrodedCORROSION (72C235-02), ON BEAM BS 480 LBL 12 TO 36 WL 208. REPAIRED UPPER CHORD OF FLOORBEAM BS 480 RBL 15 LBL 36 PER FEDEX SRM 53-10-8, ALODINED, PRIMERED AND PAINTED. FOUND CORROSION OUT OF LIMITS PER FEDEX SRM 53-10-1.SDR 95FDEA01360Seat Track · corrodedCORROSION (72C235-02), ON SEAT TRACK BS 380 TO 420 LBL 24 WL 208. REMOVED CORROSION ON SEAT TRACK, OUT OF LIMITS IAW FEDEX 53-10-1. REMOVED AND REPLACED DAMAGED SEAT TRACK FROM BS 380 TO 420 LBL 24 WL 208 IAW PER FEDEX SRM 53-10-5.SDR 95FDEA01359Skin · corrodedCORROSION ON INTERIOR SKIN, BS 847 WL 214 BETWEEN STR 16 TO 17R. REMOVED STR SPLICE FOR ACCESS STR 16R BS 825 TO 850, BLENDED CORROSION ON INTERIOR SKIN BS 847 WL 214 RT IN 1 INCH BY 1 INCH AREA. ORIG THICKNESS .200, REMOVED .018, REMOVAL IS WITHIN LIMITS IASDR 95FDEA01358Skin · disbondLT WING I/B MIDFLAP T/E LWR SURFACE, 6 FEET FROM I/B END HAS DISBOND. REPLACED DELAMINATION 6 FEET FROM I/B AND ON THE LT WING I/B MIDFLAP T/E LOWER SURFACE IAW FEDEX SRM 51-40-6.SDR 95FDEA01357Skin · lightning strikeLIGHTNING STRIKE BS 860 STR 1L. DAMAGE FOUND TO BE OUT OF LIMITS PER FEDEX SRM 53-30-1. REPAIRED PER FEDEX SRM 53-30-3.SDR 95FDEA01356Skin · lightning strikeLIGHTNING STRIKE BS 848.95 LBL 1, CROW DOUBLE STRIKE. DAMAGED WAS FOUND TO BE OUT OF LIMITS PER FEDEX SRM 53-30-1. REPAIRED PER FEDEX SRM 53-30-3.SDR EISA95408Panel · crackedRIGHT WING LOWER ACCESS PANEL JUST FORWARD AND INBOARD OF VENT SCOOP HAS A 4 INCH CRACK. FABRICATED NEW PANEL IAW SRM 51-30-8 AND 51-10-1 INSTALLED PANEL IAW SRM 51-30-2. (M)SDR EISA95395Skin · tornUPON SCHEDULED INSPECTION, FOUND HOLE AND TEAR IN SKIN UNDER THRESHOLD OF THE AFT CARGO BIN CUTOUT. REPAIRED DISCREPANCY IAW EO 1280-003. (M)SDR 95FDEA01337Hyd Line · chafedBOTH SYS-A HYD LOW PRESS LIGHTS CAME ON WITH AUDIBLE PRESS SURGES. A-SYS PRESS IND ZERO, FULL QTY IND AND OPERATED 3 MIN WITH LIGHTS ON. FOUND NR 2 ENG PUMP PRESS LINE CHAFED THROUGH BECAUSE OF MISROUTING. REMOVED AND REPLACED NR 2 HYD PUMP PRESS LINE AND RSDR EISA95405Skin · corrodedFUSELAGE LAP JOINT AT STRINGER 4R HAS MATERIAL LOSS IN EXCESS OF 10 PERCENT FROM BS 482-740 IN AREAS THAT WERE NOT PREVIOUSLY TERMINATED WITH REPAIRS. REPAIRED AND INSTALLED DOUBLER IAW SRM 53-30-3. (M)SDR EISA95402Bob Weights · crackedLEFT ELEVATOR TAB HAS 3 BOB WEIGHTS CRACKED. REMOVED AND REPLACED BOB WEIGHTS AND BALANCED TAB IAW SRM 51-80-9 INSTALLED LEFT ELEVATOR TAB IAW MM 27-30-11, RIG AND OPS CHECK IAW 27-30-0. (M)SDR EISA95400Bob Weights · crackedRIGHT ELEVATOR TAB HAS 3 BOB WEIGHTS CRACKED. REPLACED 3 BOB WEIGHTS AND BALANCED TAB IAW SRM 51-00-09. INSTALLED RIGHT ELEVATOR TAB IAW MM 27-30-11, RIG AND OPS CHECK IAW MM 27-30-0. (M)SDR EISA95394Te Skin · disbondedLEFT ELEVATOR TAB TRAILING EDGE HAS DISBONDED AT THE INBOARD END. REPAIRED AND REBALANCED IAW SRM 51-40-10 FIG 2 DETAIL 2 AND INSTALLED IAW 27-30-11. (M)SDR EISA95399Bottle Pin · corrodedLEFT FORWARD WING TERMINAL FITTING BOTTLE PIN IS PITTED AND CHROME IS FLAKING OFF. REMOVED AND REPLACED BOTTLE PIN WITH SEREVICEABLE UNIT IAW BOEING MAINTENANCE MANUAL CHAPTER 57. (M)SDR 95FDEA01324Rub Strip · disbondLT WING O/B MIDFLAP UPPER I/B RUB STRIP DISBONDED. LT WING O/B MIDFLAP UPPER I/B RUB STRIP WAS REPAIRED PER FEDEX MM 51-51-11.SDR 95FDEA01323Skin · disbondedNR 12 SPOILER HAS LARGE DISBONDED AREA OF LOWER SKIN. REPAIRED NR 12 SPOILER LOWER SKIN IAW FEDEX SRM 51-40-6.SDR 95FDEA01322Skin · disbondedNR 11 SPOILER HAS DISBONDED AREA OF LOWER SKIN AT HINGE DOUBLER. REPAIRED NR 11 SPOILER LOWER SKIN IAW FEDEX SRM 51-40-6.SDR 95FDEA01321Skin · disbondLT WING O/B AFT FLAP 2 INCHES FROM O/B END HAS DISBOND, LOWER SURFACE. REPAIRED LT WING O/B AFT FLAP 2 INCHES FROM O/B END IAW FEDEX SRM 51-40-6.SDR 95FDEA01320Skin · disbondRT WING O/B MIDFLAP HAS DISBOND AT O/B CORNER ON UPPER SURFACE. REPAIRED RT WING O/B MIDFLAP O/B CORNER UPPER SURFACE IAW FEDEX SRM 57-50-01, 51-40-06.SDR 95FDEA01319Skin · disbondRT WING O/B MIDFLAP HAS DISBOND, 70 INCHES FROM O/B END UPPER SURFACE. REPAIRED RT WING O/B MIDFLAP, 70 INCHES FROM O/B END UPPER SURFACE IAW FEDEX SRM 57-50-01, 51-40-06.SDR 95FDEA01318Skin · disbondRT WING O/B MIDFLAP HAS DISBOND, 28 INCHES FROM I/B UPPER SURFACE. REPAIRED RT WING O/B MIDFLAP, 28 INCHES FROM I/B END UPPER SURFACE IAW FEDEX SRM 57-50-01, 51-40-06.SDR 95FDEA01317Skin · disbondRT WING O/B MIDFLAP HAS DISBOND AT I/B CORNER UPPER SURFACE. REPAIRED RT WING O/B MIDFLAP I/B CORNER UPPER SURFACE, IAW FEDEX SRM 57-50-01 AND 51-40-06.SDR EISA95398Bottle Pin · corrodedLEFT AFT WING TERMINAL FITTING IS PITTED AND CHROME IS FLAKING. REMOVED AND REPLACED WITH SERVICEABLE UNIT, P/N 69-13901-5, IAW BOEING MM 57-00-00. (M)SDR EISA95397Bottle Pin · corrodedRIGHT AFT WING FITTING TERMINAL BOTTLE PIN IS PITTED AND CHROME IS FLAKING OFF. REMOVED AND REPLACED RIGHT AFT WING BOTTLE PIN, P/N 69-13901-5, IAW MM 57-00-00. (M)SDR EISA95396Bottle Pin · corrodedRIGHT FORWARD WING TERMINAL FITTING BOTTLE PIN IS PITTED AND CHROME IS FLAKING OFF. REMOVED AND REPLACED RIGHT FORWARD BOTTLE PIN WITH SERVICEABLE UNIT IAW BOEING MM CH 57-00-00. (M)SDR EISA95420Blkhd Skin · crackLOWER LOBE INTERIOR 1.5 INCH CRACK IN VERTICAL STRAP AT RBL 46, BULKHEAD 1183 OUTBOARD SIDE. FABRICATED ANGLE AND FILLER IAW SRM 51-40-4 FIG 1 AND SRM 51-30-2. (M)SDR EISA95416Skin · dentedFUSELAGE SKIN, AT STATION 380 STRINGER 18LT, HAS DENTS OUT OF LIMITS. FABRICATED AND INSTALLED DOUBLERS IAW SRM 53-30-3 FIG 3. (M)SDR 95FDEA01201Floorbeam · corrodedCORROSION (72C235-02), ON FLOORBEAM UPPER FLANGE BS 620 RBL 8 TO 17 WL 208. REMOVED AND REPLACED UPPER FLOORBEAM T-CHORD BS 620 LBL 15 RBL 34 PER FEDEX SRM 53-10-8.SDR 95FDEA01177Rib · crackedPOSSIBLE CRACK ON THE NR 6 ELEVATOR HINGE RIB UPPER SURFACE BETWEEN THE 2ND AND 3RD RIVET FORWARD FROM THE T/E BEAM. NDI VERIFIED CRACK, REMOVED AND REPLACED NR 6 ELEVATOR HINGE RIB PER FEDEX MM 27-30-21, SRM 51-30-02, EA 7-5510-25592A.SDR 95FDEA01176Spar · corrodedCORROSION ON LOWER WING SPAR CHORD AT STA 740, LBL 16, WL 168. ACCOMPLISHED REPAIR OF LOWER 740 CHORD AND SKIN IAW FEDEX EA 7-5710-25579.SDR 95FDEA01175Skin · dentedDENT IN FUSELAGE SKIN BS 1135 BETWEEN 2R - 3R. REMOVED DAMAGED SKIN AND REPAIRED PER FEDEX SRM 53-30-3.SDR 95FDEA01174Shear Tie · crackedSHEAR TIE CRACKED AT BS 1203, WL 249, RBL 66. REPAIRED SHEAR TIE PER EWO 95-2953, BS 1203, RBL 66, WL 249.SDR 95FDEA01173Keel Beam · corrodedCORROSION AROUND FASTENER ON KEEL BEAM AT BS 990-1010 AND BS 1030-1050, S29R. CORROSION REMOVAL WAS OUT OF LIMITS, OVERSIZED FASTENER HOLES TO REMOVE CORROSION, FABRICATED FREEZE PLUGS AND REPAIR ANGLES, INSTALLED ALL WORK DONE PER TRAMCO EWO NR 95-2968, EA 7SDR 95FDEA01172Bullnose · corrodedCORROSION ON NR 6 K-FLAP O/B BULLNOSE ACTUATING ROD LOWER ATTACH POINT AT BULLNOSE. REMOVED AND REPLACED NR 6 K-FLAP PER FEDEX MM 27-81-01.SDR 95FDEA01171Skin · crackedLIGHTNING STRIKE BS 444 BETWEEN FASTENER ON STR 4L. FOUND LIGHTNING STRIKE DAMAGE TO BE OUT OF LIMITS. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PARTS PER FEDEX SRM 53-30-3.
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