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 = '72723' 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 = '72723' 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 DHL9871723CSkin · dentedAT C CHECK, FUSELAGE EXT SKIN DENTED AT STA 312 S-23R. CUT OUT DAMAGED AREA, REPAIRED PER SRM 513-30-3, 10 BY 8, N/R 3080.SDR DHL9871751CSkin · damagedAT C CHECK, AFFECT PERMANENT REPAIR TO WING AT STA 410. CUT OUT DAMAGED AREA AND INSTALLED REPAIR PER SRM 57-30-4, 13 BY 8, N/R 2006.SDR 97ZZZX4646Spar · crackedDURING ROUTINE INSPECTION OF AIRCRAFT, TWO CRACKS WERE FOUND ON THE LT HORIZONTAL STABILIZER'S AFT SPAR LOWER CHORD. EACH CRACK WAS APPROXIMATELY 1.5 INCH LONG. ONE CRACK WAS AT STABILIZER STA 169 AND THE OTHER WAS AT STABILIZER STA 179.SDR DHL9771705Tab · delaminatedDURING A CHECK, UPPER RUDDER TAB WAS FOUND DELAMINATED AT UPPER END. REMOVED UPPER RUDDER TAB AND INSTALLED BONDING REPAIR PER BOEING SRM 51-4-06, SIZE OF REPAIR 4 BY 20. UPPER RUDDER TAB WAS REINSTALLED PER M/M 27-20-11.SDR DHL9771704Angle · crackedDURING CORROSION INSPECTION, ANGLE WAS FOUND CRACKED AT LOWER END, STA 1183 NEXT TO LOWER LEFT CORNER OF AFT ENTRY DOOR. REMOVED AND REPLACED ANGLE IAW SRM 51-30-2.SDR 97ZZZX3523Actuator · inaccurateANC - FLT 74 - RETURNED TO ANC AT 0235Z DUE TO NR 7 LEADING EDGE SLAT INDICATING IN-TRANSIT. MAINTENANCE REPLACED NR 7 LEADING EDGE SLAT ACTUATOR DUE TO FAULTY INDICATION AND RETURNED AIRCRAFT TO SERVICE. (X)SDR 97ZZZX3517Slat Actuator · leakingON TAKEOFF ROLL, A-SYSTEM LOW LEVEL LIGHT CAME ON, TAXIED OFF AT BRAVO TO COMPANY RAMP. MAINTENANCE REPLACED NR 5 LEADING EDGE SLAT ACTUATOR AND RETURNED AIRCRAFT TO SERVICE. (X)SDR DHL97717003Seat Track · wornPALLET LOCK IS LOOSE AND WILL NOT STAY IN SEAT TRACK, DEFERRED POSITION. REMOVED SECTION OF SEAT TRACK AND REPLACED PER SRM 53-10-5, REINSTALLED PALLET LOCK, SECTION 6 FT 8.SDR DHL97717002Connector · dirtyNR 2 EPR GAUGE STUCK AT 1.3 EPR. CLEANED CANNON PLUG AT TRANSMITTER. GROUND RAN AIRCRAFT, SYSTEM OPS CHECK NORMAL.SDR DHL97717001Bushing Insert · strippedPRECAUTIONARY SHUTDOWN ENGINE NR 1 DUE TO LOW OIL PRESSURE AND QUANTITIY. REPLACED LP6 FITTING (BUSHING INSERT) IN GEAR BOX. WORK ACCOMPLISHED PER MM 72-61-01. TEST RAN ENGINE, NO LEAKS NOTED.SDR 97ZZZX760Rod Attach · nut missingDURING C-CHECK INSPECTION OF THE LEFT OUTBOARD AILERON CONTROL ROD TO AILERON, INSPECTION REVEALED THE ATTACH BOLT'S NUT, WASHER, AND COTTER PIN WERE NOT INSTALLED (MISSING). THE BOLT MIGRATED APPROX .125 INCH OUTBOARD. SUSPECT DURING AILERON INSTALLATION, TSDR DHL9871786CFitting · crackedAT C CHECK, LOWER AFT CARGO COMP DOOR CUT-OUT LOWER AFT STOP FITTING DAMAGED, CRACKED ON AFT FLANGE EDGE. REPLACED FITTING PER SRM 51-10-1 N/R 3192.SDR 96ZZZM1437Bearing Seal · looseAIRCRAFT DEPARTED MEXICO CITY, CANCUN, EN ROUTE NR 2 ENGINE OIL BYPASS LIGHT CAME ON AND ENGINE TEMPERATURE STARTED TO RISE. NR 2 ENGINE SHUT DOWN, PROCEED TO CANCUN AND LANDED COMPLETE. INVESTIGATION REVEALED OIL SEAL LOOSE IN THE NR 6 BEARING SCAVANGE PUMPSDR 96ZZZX4248Structure · hail damageAIRCRAFT DESCENDING TO MCO AT 13,000 FEET AND 250 KNOTS. ENTERED SCATTERED HAIL. NO FLAPS DOWN, NO LANDING GEAR DOWN. DAMAGE TO NR 2 ENGINE RING COWL, UPPER 180, LEADING EDGE DAMAGE AND ALL OLD REPAIRS TURN LOOSE, WINDOW SEAL TORN BACK, UPPER BEACON BROKE, SDR 96ZZZX2928Cowl · damagedAIRCRAFT DESCENDING TO MCO AT 13,000 FEET AND 250 KNOTS. ENTERED SCATTERED HAIL. NO FLAPS DOWN, NO LANDING GEAR DOWN. DAMAGE TO NR 2 ENGINE RING COWL, UPPER 180, LEADING EDGE DAMAGE AND ALL OLD REPAIRS TORN LOOSE, WINDOW SEAL TORN BACK, UPPER BEACON BROKE, SDR DHL96717005Ballast · failedMEDIUM AMOUNT OF SMOKE IN COCKPIT FROM UNDER FRONT PANEL RIGHT SIDE. FOUND BALLAST FOR PANEL FLUORESCENT LIGHTS CAUSING SMOKE. DEACTIVATED SYSTEM, DEFERRED PER MEL 33-1.SDR DP2R5836Airframe Crown · delaminatedAD 90-20-18. AIRFRAME CROWN DELAMINATION NOTED AS FOLLOWS: BS 950, STR 1. BS 950, STR 2R. BS 950, STR 3R. BS 751, STR 8-10 LT AND RT. BS 775, STR 8-10 LT AND RT. BS 825, STR 8-10 LT AND RT. BS 850, STR 8-10, LT AND RT. (X)SDR 96ZZZX1245Web · crackedDURING C-CHECK, NOSE WHEELWELL, RT SIDE PRESSURE WEB, FOUND CRACKED BELOW ACCESS PANEL, STA 241. CUT OUT DAMAGED AREA AND INSTALLED EXTERNAL DOUBLER 17 INCHES BY 21 INCHES AT STA 241 PER BOEING SRM 51-40-2. TAT: 59,690.0 HRS. TAC: 43,708.SDR 96ZZZM520Skin · corrodedDURING C-CHECK, FOUND FUSELAGE SKIN ABOVE AFT LAV SERVICE DOOR BULGED. INSTALLED PLUB AND DOUBLER 22.25 INCH BY 22.25 INCH PER AERONAUTICAL ENGINE DRAWING AE5093.SDR 96ZZZM515Elev Tip · loose rivetsDURING C-CHECK, RIGHT ELEVATOR OUTBOARD TE TIP REPAIR HAS LOOSE RIVETS UPPER AND LOWER SIDES. REMOVED FASTENERS PER SRM 51-30-2. CUT OUT 9 INCH BY 10 INCH AREA OUTBOARD TE TIP REPAIR, MADE TOP AND LOWER DOUBLER AND FILLER 2024-T3 .032 FILLER .063 PER SRM 55-SDR 96ZZZM514Gusset · crackedDURING C-CHECK, FOUND LEFT SIDE GUSSET CRACKED AT FWD SIDE OF FUSELAGE FRAME 825.95 SUB FLOOR. REMOVED CRACKED GUSSET AS REQUIRED PER SRM 51-10-1. FABRICATED NEW GUSSET 2024-T3 .090 5 INCH BY 4 INCH LOT NR 483-871 PO NR 93110393 AND SHIM 2024-T3 .125 2.5 INCSDR 96ZZZM513Skin · crackedDURING C-CHECK, FOUND FWD ENTRY DOOR EXTERIOR SKIN CRACKED AND BENT AT UPPER HINGE CUTOUT. REMOVED INNER SKIN PANEL AS PER SRM 52-40-2. ROUTED OUT CRACKS FWD ENTRY DOOR EXTERIOR SKIN UPPER HINGE AS PER SRM 51-10-1. FABRICATED DOUBLER .063 2024-T3 9 INCH BY SDR 96ZZZM512Web · crackedDURING C-CHECK, FOUND NOSE W/W LEFT SIDE PRESSURE WEB CRACKED AT STATION 247 4 INCHES ABOVE GEAR DOOR. REMOVED FASTENERS PER SRM 51-30-2. CUT OUT DAMAGED AREA 2 INCH BY 1 INCH AT LEFT SIDE NOSE W/W STATION 247 PER SRM 51-10-1. FABRICATED EXTERNAL DOUBLER 20SDR 96ZZZM511Floor Support · corrosionDURING C-CHECK, FOUND WING SECTION HAS CORROSION ON FLOOR SUPPORT ANGLE BOTTOM SIDE AT STATION 764 RBL 65 INCHES. REMOVED FASTENERS PER SRM 51-30-2. CUT OUT DAMAGED AREA IN LOWER WEB 1.5 INCH DIAMETER APPROX CLEANED AREA, ALODINED AND PRIMED PER SRM 51-10-2.SDR 96ZZZM510Skin · crackedDURING C-CHECK, FOUND EXTERIOR SKIN AROUND 2 FASTENERS CRACKED AT LEFT SIDE BS 203.8 WL 219.5. REMOVED PANELS IN THE COCKPIT TO GET ACCESS TO THE AREA PER SRM 51-30-2. CUT OUT THE DAMAGE AREA PER SRM 53-30-3 FIG 3. FABRICATED EXTERNAL DOUBLER 2024-T3 .063 1SDR 96ZZZM509Angle · corrodedDURING C-CHECK, FOUND REINFORCEMENT CHORD ANGLE AT BS 1176.5 CORROSION NOTED LBL 7 INCH BY RBL 7 INCH. REPLACED CHORD AT BS 1176.5 AS PER SRM 51-10-1 PAR 4 AND SRM 51-30-2.SDR 96ZZZM508Skin · dentedDURING C-CHECK, FOUND MSI 727-0710-1001 RIGHT INBOARD AILERON HAS DENT BEYOND UNFILLED LIMITS AND SPEED TAPED PER BOEING 727 SRM 57-50-1 PAGE 13. CUT OUT DAMAGE AREA AT UPPER SKIN RIGHT OUTBOARD AILERON IAW SRM 57-50-5. FABRICATED AND INSTALLED DOUBLER AND FSDR 96ZZZM507Blkhd Beam · crackedDURING C-CHECK, FOUND CABIN AFT BULKHEAD STATION 1183 WL 283 VERTICAL BEAM CRACKED RBL 3683. REMOVED FASTENERS, STOP DRILLED CRACK AND ALODINED STOP DRILLED HOLES PER SRM 51-30-2, 51-10-1, AND 51-10-2. VERTICAL BEAM REPAIR INSTALLED AT RBL 3683 STATION 1183 SDR 96ZZZM506Door Frame · crackedDURING C-CHECK, FOUND AFT CARGO FRAME 1050 CRACKED, STRINGER 27L. REMOVED SEAT TRACK FOR ACCESS PER SRM 51-30-2. CRACK TERMINATES AT FAST, HOLE PER SRM 51-10-1. INSTALL FRAME REPAIR PER SRM 53-10-4 LOT NR 670917 PO NR 93110262 SIZE 7075-T6 .080. REINSTALL SDR 96ZZZM505Blkhd Beam · crackedDURING C-CHECK, FOUND AFT BULKHEAD STATION 1183 WL 283 LBL 26 VERTICAL BEAM CRACKED. REMOVED AND REPLACED VERTICAL BEAM PER BOEING SB 727-53-182 TYPE IV.SDR 96ZZZM504Skin · crackedDURING C-CHECK, FOUND LEFT ELEVATOR LOWER SKIN CRACKED APPROX STA ELEV 100 2 INCH FROM TRAILING EDGE. ROUTED OUT CRACK AT LEFT ELEV LOWER SKIN APPROX STATION ELEV 100 2 INCH FROM T/E IAW SRM 55-20-3. INSTALLED REPAIR 3 INCH BY 7.75 INCH OF 2024-T3 .032 PO NRSDR 96ZZZM503Skin · crackedDURING C-CHECK, LEFT ELEVATOR LOWER SKIN CRACKED TWO PLACES APPROX STA ELEVATOR 130 JUST AFT OF ACCESS PNL 9312. STOP DRILLED CRACKS AS PER SRM 51-10-1 AT TWO PLACES. INSTALLED REPAIR 9 INCH BY 11.5 INCH 2024-T3 .032 PO NR 93110887 LOT NR 275-611 IAW SRM 55-SDR 96ZZZX1465Windshield · crackedANC - FLT 105 - RETURNED TO ANC DUE TO FAILURE OF CAPTAIN'S WINDSHIELD OUTER PANEL. MAINTENANCE REPLACED L1 WINDOW. REPLACED WINDSHIELD HEAT CONTROLLER AS A PRECAUTIONARY MEASURE. ACFT RETURNED TO SERVICE.SDR 96ZZZM300Floor · corrodedLEVEL 2 EXFOLIATING CORROSION UNDER STAINLESS STEEL PLATE AT STA 1130-1148, RBL 26 AT RIGHT AFT LAV. FABRICATED DOUBLER AND FILLER, LOCATED AND DRILLED AND INSTALLED COMPLETE PER SRM 51-10-6, 51-40-2 AND TREATED. (M)SDR 96ZZZM302Floor Beam · corrodedLEVEL 2 EXFOLIATING CORROSION, STATION 640 RBL 12-64, UPPER SURFACE, FORWARD HORIZONTAL. FLANGE OF FLOOR BEAM, AROUND CLIP NUT HOLES. REMOVED CORROSION TREATED, PRIMED PER SRM 51-10-6, 51-10-2. (M)SDR 96ZZZM301Floor Stabilizer · corrodedLEVEL 2 EXFOLIATING CORROSION, STATION 600-640 RBL 12, UPPER AND LOWER SURFACES OF FLOOR STABILIZER GROUND NUTPLATE HOLES. REMOVED CORROSION, TREATED, PRIMED PER SRM 51-10-6 AND 51-10-2. (M)SDR 96ZZZM304Floor · corrosionLEVEL 2 EXFOLIATING CORROSION, STATION 600-640 RBL 64, UPPER HORIZONTAL SURFACE, OUTBOARD FLOOR STABILIZER. REMOVED CORROSION AND TREATED AND PRIMED PER SRM 51-10-6, 51-10-2. (M)SDR 95ZZZX7070Rib · crackedWHILE INSPECTING AIRCRAFT PER AD 94-07-08 (SB 727-57-127), THE HYDROPRESSED WING RIB AT RT WS 546.5 WAS FOUND CRACKED ON LOWER FLANGE ADJACENT TO THE SECOND FASTENER HOLE FROM FORWARD END OF RIB. SUSPECT CAUSE: FATIGUE.SDR 95ZZZX7069Skin · corrodedWHILE INSPECTING AIRCRAFT PER AD 91-06-06 (SB 727-53-0072), THE FUSELAGE SKINS AT THE LAP JOINT AT STR 19R, BS 360 WERE FOUND CORRODED INSIDE THE LAP JOINT. SUSPECT CAUSE: DELAMINATION OF COLD BOND LAP JOINT.SDR 95ZZZX7068Rib · crackedDURING INSPECTION OF AIRCRAFT PER AD 94-07-08 (SB 727-57-127), THE HYDROPRESSED WING RIB AT LT WS 601.5 WAS FOUND CRACKED IN 4 PLACES. THE UPPER FLANGE WAS CRACKED AT THE 2ND FASTENER HOLE FORWARD OF THE AFT END. THE LOWER FLANGE WAS CRACKED AT THE 3RD, 4TH,SDR 95ZZZX7067Stringer · corrodedDURING THE COURSE OF ROUTINE MAINTENANCE, FUSELAGE STR 21R WAS FOUND EXFOLIATED, REQUIRING SRM REPAIR. SUSPECT CAUSE: AREA IS DIRECTLY BELOW GALLEY, ALTHOUGH NO DIRECT EVIDENCE OF LEAKAGE WAS FOUND.SDR 95ZZZX7066Rib · crackedDURING INSPECTION OF AIRCRAFT PER AD 94-07-08 (SB 727-57-127), THE HYDROPRESSED WING RIB AT LT WS 686.5 WAS FOUND CRACKED IN 2 PLACES AT THE LOWER FLANGE. ONE CRACK WAS AT THE AFTMOST FASTENER HOLE, THE OTHER WAS AT THE THIRD FASTENER HOLE FORWARD FROM THE AFSDR 95ZZZX7065Closure Rib · corrodedWHILE PERFORMING CPC TASK CARD C55-391-30, THE VERTICAL STABILATOR'S UPPER RT CLOSURE RIB WAS FOUND EXFOLIATED ON ITS OUTBOARD SIDE JUST FORWARD OF THE FORKED END OF THE AFT HINGE POINT FITTING FOR THE HORIZONTAL STABILIZER. CORROSION WAS REMOVED AND FOUND TOSDR 95ZZZX7064Rib · crackedWHILE INSPECTING AIRCRAFT PER AD 94-07-08 (SB 727-57-127), THE HYDROPRESSED WING RIB AT LT WS 546.5 WAS FOUND CRACKED ON ITS LOWER FLANGE ADJACENT TO THIRD FASTENER HOLE FORWARD OF THE AFT END OF RIB. SUSPECT CAUSE: FATIGUE.SDR 95ZZZX7063Shear Web · corrodedDURING INSPECTION OF AIRCRAFT PER CPC TASK CARD C53-224-04, THE FLOOR STRUCTURE SHEAR WEB WAS FOUND CORRODED BEYOND SRM LIMITS BETWEEN BS 1168 -BS 1178 AND LBL 30-LBL 36 (UNDER LT AFT LAVATORY).SDR 95ZZZX7062Rib · crackedDURING INSPECTION OF AIRCRAFT PER AD 94-07-08 (SB 727-57-127), THE HYDROPRESSED RIB AT RT WS 601.5 WAS FOUND CRACKED IN 2 PLACES ON THE LOWER FLANGE. ONE CRACK WAS AT THE AFT END FASTENER HOLE AND THE OTHER WAS AT THE THIRD FASTENER HOLE FORWARD OF THE AFT ENSDR 95ZZZX7061Skin · corrodedWHILE PERFORMING INSPECTION OF THE BONDED CIRCUMFERENTIAL DOUBLER AT BS 481 PER AD 90-26-09 (SB 727-53-0084), MATERIAL LOSS RANGING FROM 10-30 PERCENT WAS DETECTED IN THE AREA BOUNDED BY STR 4L TO STR 4R. UPON OPENING UP OF AREA FOR REPAIR, PHYSICAL MEASUREMESDR 95FDEA01479Blkhd Web · corrodedAFT CARGO COMP FS 950 BLKD UPPER FLANGE AND WEB CORRODED BETWEEN RBL 24 - 54. REMOVED CORROSION AND INSTALLED DOUBLER PER SRM 53-10-9 FIG 2, SRM 51-10-9.SDR 95FDEA01478Floor Beam · corrodedUPPER LOBE FLOOR STA 480 LT CORROSION ON UNDERSIDE OF FLOOR BEAM BETWEEN LBL 24 AND LBL 45 AROUND FASTENER HOLES. REMOVED CORROSION NR 7 ABOVE LOCATION PER SRM 51-10-06. CORROSION REMOVED BEYOND LIMITS, REPAIRED CORRODED FLOOR BEAM PER 53-10-8 FIG 5.SDR 95FDEA01430Floor Beam · corrodedHEAVY CORROSION AT F/B SCREW HOLES STA 400, LBL 35 ON FLOOR BEAM TOP SIDE. REMOVED CORROSION BY CUTTING OUT DAMAGED AREA PER SRM 53-10-8. INSTALLED FLOOR BEAM REPAIR PER SRM 53-10-8, PG 45 - 48.
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