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 97FDEA00270Intercostal · corrodedNR 0507 002, CORROSION (C53-221-01) ON INTERCOSTAL BETWEEN BS 268 AND 274.SDR 97FDEA00269Intercostal · corrosionNR 0506 001, CORROSION (C53-221-01) ON INTERCOSTAL BETWEEN BS 280 TO 294, RBL 15, WL 208. *S/D* REMOVED AND REPLACED INTERCOSTAL/FLOOR SUPPORT AT BS 277 TO 294, RBL 15, WL 208, DUE TO CORROSION BEING OUT OF LIMITS. WORK PERFORMED IAW FED-EX SRM 53-30-2 AND SDR 97FDEA00322Beam · corrosionNR 0542 026, CORROSION (C55-391-20, 2) RT HORIZONTAL STAB UPPER TIE BEAM HAS AN AREA OF CORROSION 138 FROM INBOARD END LWR FWD SIDE. * S/D* REMOVED AND REPLACED RT HORIZONTAL STAB UPPER TRAILING EDGE BEAM IAW FED-EX SRM 51-30-5.SDR 97FDEA00275Beam · corrodedNR 0446 006, CORROSION ON LONGITUDINAL BEAM BS 740 TO 848, LBL 45, WL 208.1. *S/D* REMOVED AND REPLACED LONGITUDINAL BEAM BS 740 TO 848, LBL 45, WL 208.1 IAW FED-EX SRM 51-30-2.SDR EISA97081Fire Warning · illuminatedWHEEL WELL FIRE LIGHT CAME ON WHILE RETURNING TO DAL, PERFORMED EMERGENCY ITEMS, LIGHT WENT OUT. PERFORMED INSPECTION OF WHEEL WELL AND FIRE DETECTOR LOOPS. FOUND NO EVIDENCE OF FIRE, PERFORMED OPERATIONAL CHECK OF FIRE WARNING SYSTEM PER MM 26-10-0. OPS CSDR EISA97080Lights · malfunctionedEMERGENCY EXIT LIGHTS ILLUMINATED IN FLIGHT. RECYCLED EMERGENCY LIGHTS 'DIM' C/B, OPS CHECK OK. (M)SDR CA970314002Bulb · burnt(CAN) ON APPROACH SELECTED GEAR DOWN, RH GEAR DOWN GREEN LIGHT DID NOT ILLUMINATE. MISSED APPROACH CARRIED OUT. ANNUNCIATOR LIGHT CHECKED. BULBS REPLACED.SDR 97FDEA00097Stringer · corrodedNR 0190 009 CORROSION (C53-224-03) ON STR 19 RT BS 313. *S/D* FABRICATED AND INSTALLED FASTENERS TO LOWER FLANGE DOUBLER AT STR 19 RT BS 313. ALODINED AND PRIMED, SEALED PER FED-EX SRM 53-10-3 FIG NR 1.SDR 97FDEA00087Bulkhead · crackedNR 0172 005. BS 950 BULKHEAD IS CRACKED LBL 31, WL 183. REPAIRED CRACK AT LBL 31, WL 183 ON BS 950 BULKHEAD I.A.W. FED-EX SRM 53-10-9.SDR 97FDEA00086Frame · corrodedNR 0405 006. CORROSION (C53-224-03) ON FRAME STA 423, BL ZERO, WL 152. REMOVED FRAME AT STA 423, BL ZERO, WL 152 (E-BAY) ORDERED AND INSTALLED NEW FRAME PER FED-EX SRM 51-30-2.SDR 97FDEA00084Stiffener · corrodedNR 0401 08. CORROSION (C53-224-03) ON VERTICAL STIFFENER STA 344, LBL 13, WL 180. REMOVED CORROSION ON STIFFENER. FOUND TO BE OUT OF LIMITS PER FED-EX SRM 53-10-1. DRILLED UP AND INSTALLED NEW STIFFENER PER FED-EX SRM 51-30-2.SDR 97FDEA00078Bulkhead · crackedNR 0170 04. 950 BULKHEAD IS CRACKED AT RBL 4.5 AND LBL 4.5 WL 176. REPAIRED CRACKS AT 950 BULKHEAD, RBL 4.5 AND LBL 4.5, WL 176 PER FED-EX SRM 53-10-9.SDR 97FDEA00085Stiffener · corrodedNR 0402 07. CORROSION (C53-224-03) ON HORIZONTAL STIFFENER STA 344, LBL 8, WL 180. REMOVED AND REPLACED STIFFENER PER FED-EX SRM 51-30-2.SDR 97FDEA00076Nose Chord · corrodedNR 0406 002. CORROSION (C53-224-03-1/2) ON RT MID-NOSE CHORD BS 312-344, RBL 13, WL 167. REMOVED AND REPLACED RT MID-CHORD AT BS 294 TO 351, WL 169, RBL 13 I.A.W. BAC DRW. 65-18415.SDR 97FDEA00075Web · corrodedNR 0337 003. CORROSION (C53-100-01(1) ON WEB OF FRAME AND BONDED DOUBLER AT BS 211.8, LBL 19, WL 152. CORROSION FOUND TO BE OUT OF LIMITS. REPAIRED WEB AND REPLACED BONDED DOUBLER I.A.W. FED-EX SRM 53-10-01, 51-40-2.SDR 97FDEA00071Floorbeam · corrodedNR 0140 001. CORROSION (C53-224-06) AROUND FASTENER HOLE ON FLOORBEAM AT BS 344, LBL 34 TO LBL 57, WL 208. REMOVED CORRODED UPPER CHORD AT BS 344, RBL 62 - LBL 62, WL 208. INSTALLED NEW UPPER CHORD I.A.W. FED-EX REPAIR DWG SR 27-53-007.SDR EISA97001Actuator · inoperativeAFTER TAKEOFF WITH FLAPS RETRACTED NR 2 SLAT UNSAFE LIGHT REMAINED ILLUMINATED. REMOVED AND REPLACED SLAT ACTUATOR, OPS CHECK GOOD. (M)SDR 96FDEA01707Fire Light · illuminatedWHEEL WELL FIRE LIGHT CAME ON INTERMITTENTLY DURING TAKEOFF. GROUND RACK HOLD DOWN BROKEN. REMOVED AND REPLACED HOLD DOWN. OPERATIONAL CHECK GOOD.SDR 97FDEA00009Fitting · corrodedFUSE STA 740 LT WING ATTACH FWD FITTING CORRODED, FOR LT FWD BOTTLE BOLT. REMOVED CORROSION BY REAMING BORE PER BOEING SRM 57-10-7 FIG 2, SHEET 1. FABRICATED AND INSTALLED SLEEVE PER SRM 57-10-7, FIG 2 SHEET 5.SDR 97FDEA00003Skin · corrodedCORROSION ON INNER FUSE SKIN STR 10 L STA 863 TO 875, FOUND DURING REPLACEMENT OF 870 CASTING. REMOVED CORROSION AND INST DOUBLER AND FILLER ON OUTSIDE OF FUSE PER EA 7-5330-28946 DOUBLER 2024 T 3.071.SDR 97FDEA00002Bulkhead Forging · crackedLT FUSE 870 BULKHEAD FORGING. CRACKED BEYOND LIMITS OF SB 727-53-116, REF NR S001. INSTALLED NEW LT 870 FORGING PER FED EX EA 7-5310-28935, SB 727-53-116, SRM 51-30-2.SDR DHL96708007Yaw Damper · malfunctionedAT FL 310 AND MACH .80, RECEIVED SUDDEN UNCOMMANDED RUDDER INPUTS FROM LOWER YAW DAMPER. WHEN YAW DAMPER SWITCH TURNED OFF, THE UNCOMMANDED RUDDER INPUTS CEASED. CLEANED LOWER YAW DAMPER CONNECTOR AND RERACKED COUPLER, CYCLED RUDDER TO FULL TRAVEL LEFT AND SDR 96FDEA01615Bulkhead · crackedNR 0509 024, CRACK ON THE AFT SIDE OF THE 870 BULKHEAD AT RBL 9.5 AND WL 157.SDR 96FDEA01614Bulkhead · crackedNR 0507 023, POSSIBLE CRACK ON AFT SIDE OF BS 950 BULKHEAD AT LBL 4 WL 176 AND AT LBL 11, WL 181 TO 184.SDR DHL96708006Outflow Valve · failedON DEPARTURE OUT OF 11,000 FT, HEARD LOUD BUMP FROM REAR OF AIRCRAFT. IMMEDIATELY THE AIRCRAFT BEGAN TO DEPRESSURIZE AND CABIN ALTITUDE COULD NOT BE CONTROLLED BY ANY MEANS. REMOVED AND DEFERRED OUTFLOW VALVE.SDR 96FDEA01583Floorbeam · corrodedNR 0437 AND 022, CORROSION (C53-111-01, -3) IN THE AFT CARGO BAY AT BS 1148 LBL 11 TO 23 WL 199 ON FLOORBEAM AT NUTPLATE HOLES. *S/D* CORROSION FOUND TO BE OUT OF LIMITS. REPAIRED FLOORBEAM AT BS 1148 LBL 11 TO 23 WL 199 IAW FEDEX EA 7-5310-31191.SDR 96FDEA01582Floorbeam · corrodedNR 0609 AND 021, CORROSION (C53-224-01, -3) ON STA 1110 RBL 23 WL 208 UNDER TOP FLANGE OF FLOORBEAM. *S/D* FOUND CORROSION TO BE OUT OF LIMITS. CUT OUT DAMAGED SECTION, FABRICATED AND INSTALLED REPAIR IAW FEDEX EA 7-5310-31193.SDR 96FDEA01577S-Duct Skin · corrodedNR0496 AND 019, CORROSION (C54-451-02) ON INTERIOR SKIN OF S-DUCT AT BS 1201 AT CENTER LINE, MIDDLE OF S-DUCT. *S/D* REMOVED DAMAGED SKIN OF INTERIOR OF S-DUCT AT BS 1201. INSTALLED REPAIR DOUBLER IAW FEDEX 727 SRM 54-10-03.SDR EISA96194Gasper Fan · inoperativeWHEN GASPER FAN WAS TURNED ON, A SMOKEY SMELL ENTERED THE COCKPIT. PLACARDED GASPER FAN PER MEL 21-24. REMOVED AND REPLACED GASPER FAN, OPS TEST OK. (M)SDR 96FDEA01571Skin · creasedNR0145 AND 018, CREASE ON SKIN AT BS 254 STR 20 TO 21R. *S/D* REMOVED DAMAGE FROM SKIN AT BS 254 BETWEEN STR 20 TO 21R, FABRICATED AND INSTALLED REPAIR PER FEDEX SRM 53-30-03.SDR 96FDEA01567Stiffener · crackedNR0510 AND 017, TOP OF THE VERTICAL STIFFENER IS CRACKED IN THE WING CENTER SECTION AT BS 740 RBL 45. *S/D* REMOVED AND REPLACED VERTICAL STIFFENER IN THE WING CENTER SECTION AT BS 740 RBL 45 IAW FEDEX SRM 51-30-2.SDR 96FDEA01566Floor Beam · corrodedNR0438 AND 016, CORROSION (C53-111-01, -3) IN THE AFT CARGO BAY AT BS 1130 LBL 11 TO 13 WL 199 ON FLOORBEAM AT NUTPLATE HOLES. *S/D* CORROSION FOUND TO BE OUT OF LIMITS. REMOVED DAMGE, FABRICATED REPAIR FILLERS AND ANGLES, INSTALLED IAW FEDEX EA 7-5310-311SDR 96FDEA01563Floor Beam · corrosionNR0594 AND 015, CORROSION (C53-224-01, -3) AT BS 1110 RBL 43 WL 207 EMITTING FROM UNDER SIDE OF TOP FLANGE OF FLOOR BEAM AT FASTENER HOLE. *S/D* REPAIRED CORROSION DAMAGE ON FLOOR BEAM AT BS 1110 RBL 43 WL 207 PER FEDEX SRM 53-10-8 FIG 8.SDR 96FDEA01557Floorbeam · corrodedNR0440 AND 012, CORROSION (C53-111-01,-3) IN AFT CARGO BAY AT BS1050 LBL TO RBL 20 WL 199 ON FLOOR BEAM AT NUTPLATE HOLES. *S/D* REMOVED CORRODED SECTION OF BS 1050 FLOORBEAM FROM LBL TO RBL 25 LOWER FLANGE. REPAIRED LOWER FLANGE PER FEDEX SRM 53-10-8 FIG 3SDR 96FDEA01553Bonding Jumper · corrodedNR0589 AND 010, WHILE WORKING NR0218 FOUND NR 2 K-FLAP I/B BULLNOSE BONDING JUMPER UPPER ATTACH POINT CORRODED. *S/D* REPAIRED PER FEDEX SRM 57-50-3.SDR 96FDEA01552Floorbeam · corrosionNR0434 AND 009, CORROSION (C53-224-01, -1, -100) AT STA 620 RBL 3 WL 208 ON FRAME FILLER. *S/D* REPAIRED FLOORBEAM AT BS 620 WL 208 RBL 35 TO LBL 24 IAW FEDEX SRM 53-10-8 FIG 3.SDR 96FDEA01551Skin · delaminationNR0579 AND 008, WHILE WORKING NR0576 FOUND THREE AREAS OF DELAMINATION ON LOWER SURFACE. *S/D* REPAIRED DAMAGED SKIN TO RIGHT I/B FORE FLAP LOWER SURFACE PER FEDEX SRM 51-40-6.SDR 96FDEA01556Frame · corrodedNR0541 AND 011, FOUND CORROSION (C53-221-01) ON FRAME WEB AND TWO STIFFENERS AFT SIDE OF BS 251.6 RBL 51 WL 215 TO 221. *S/D* REMOVED CORRODED WEB AND STIFFENERS AT BS 251.6 RBL 51 WL 215 TO 221. FABRICATED AND INSTALLED WEB AND STIFFENERS IAW FEDEX SRM 51SDR 96FDEA01538Chord · corrodedNR0705 AND 041, WHILE WORKING NR0689 FOUND LOWER LT NOSE CHORD AT 320 LBL 19 TO BE CORRODED OUT OF LIMITS. *S/D* REMOVED CORRODED LOWER LT LOWER NOSE CHORD, NEW LOWER LT NOSE CHORD TO BE REINSTALLED ON NR0689 PER BAC DRW NR 65C15724.SDR 96FDEA01537Chord · crackedNR0702 AND 040, WHILE WORKING NR0689 FOUND RT LOWER NOSE CHORD CRACKED AT BS 293 RBL 15 WL 140. *S/D* REMOVED CRACKED RT LOWER NOSE CHORD. NEW RT LOWER NOSE CHORD TO BE REINSTALLED ON NR0689 IAW BAC DRW NR 65C15724.SDR 96FDEA01584Skin · crackedNR 0580 AND 020, CRACK IN L/W O/B AILERON I/B AFT TRAILING EDGE CHORD. *S/D* STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER PER FEDEX SRM 51-40-3.SDR 96FDEA01536Skin · corrodedNR0039 AND 039, BULGE IN SKIN ABOVE AFT LT SERVICE DOOR STA 1170 TO 118 STR 18L. *S/D* REPLACED SECTION OF SKIN AND REPAIRED REF FEDEX EA 7-5330-31176.SDR 96FDEA01535Skin · delaminatedNR0576 AND 007, RT WING I/B FORE FLAP IS DELAMINATED AT I/B END UPPER SURFACE. *S/D* REPAIRED DAMAGED AREA TO RT WING I/B FORE FLAP PER SRM 51-40-6.SDR 96FDEA01534Act Mount · crackedNR 0219 AND 006. NR 3 SLAT ACTUATOR ROD END MOUNT I/B AND O/B RIBS ARE CRACKED. ***S/D***** REMOVED AND REPLACED NR 3 SLAT ACTUATOR ROD AND MOUNT I/B AND O/B RIBS ON SLAT.SDR 96FDEA01525Stringer · corrodedNR0673 AND 038, WHILE WORKING ON NR0039 FOUND CORROSION ON STRINGER 20L AT BS 1163.SDR 96FDEA01524Beam · corrodedNR0697 AND 037, WHILE WORKING NR0642 FOUND CORROSION UNDER INTERCOSTAL ON TOP FLANGE OF TRACK BEAM STA 266 WL 208 LBL 10 TO 8. *S/D* REMOVED AND REPLACED WL 208 PER FEDEX SRM 51-10-1 AND 51-30-2.SDR 96FDEA01520Frame · crackedNR0055 (004) AFT ENTRY DOOR LT SIDE FRAME IS CRACKED AT 41 INCHES FROM BOTTOM OF DOOR. *S/D* REMOVED DAMAGE AFT ENTRY DOOR LT SIDE FRAME 41 FROM BOTTOM OF DOOR. FABRICATED AND INSTALLED REPAIR PER FEDEX SRM 52-10-1 AND 51-40-03.SDR 96FDEA01519Door Frame · crackedNR0055, 004, AFT ENTRY DOOR LT SIDE FRAME IS CRACKED AT 41 INCHES FROM BOTTOM OF DOOR.SDR 96FDEA01518Switch · inoperativeWHEN PUTTING GEAR DOWN, NOSE GEAR DOOR LIGHT INOPERATIVE. REMOVED AND REPLACED NOSE LANDING GEAR LOCK SWITCH IN ACCORDANCE WITH MAINTENANCE MANUAL 32-61-21 PAGE 404, TESTED GOOD PER 32-61-21 PAGE 502.SDR 96FDEA01587Floorbeam · corrodedCORROSION (C53-111-01, -3) IN AFT CARGO BAY AT BS 1050 LBL 20 TO RBL 20 WL 199 ON FLOORBEAM AT NUTPLATES HOLES. REMOVED CORRODED SECTION OF BS 1050 FLOORBEAM FROM LBL 25 TO RBL 25 WL 199 LOWER FLANGE. REPAIRED LOWER FLANGE PER FEDEX SRM 53-10-8 FIG 3 EA NR 7
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