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 jasc_code = '5711' 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 jasc_code = '5711' 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 ABXA20120405335Fitting · gougedLW KICK FITTING HAS A GOUGE (UPPER AFT SPAR A 5 OB). REPAIRED IAW REA B657-59799-MR, AIRCRAFT WAS GROUNDED. BS 955, WBL 97.95, LEFT WING.SDR FDEA201203291195Spar Cap · crackedLEFT WING REAR SPAR LOWER CAP AT WING STA XORS 347.750, THREE FASTENER HOLES FOUND CRACKED IAW NDT SPM PART 06. COMPLIED REPAIR IAW EA 8-5710-156957, REPAIR CLASSIFIED AS MAJOR.SDR COEA2012032609911Spar · erodedHEAVY CHECK / MAJOR REPAIR: RT WING FRONT SPAR LOWER CHORD BETWEEN RIBS 4 & 5 (BL 1210R TO 1625R) HAS FRETTING INBOARD OF HINGED LEADING EDGE. SUBMITTED TO ATR, REPAIR PER STRUCTURAL REPAIR INSTRUCTIONS AND SRAS FROM ATR.SDR COEA2012032608911Spar · erodedHEAVY CK / MAJOR REPAIR: LT WING FRONT SPAR LOWER CHORD BETWEEN RIBS 4 & 5 (BL 1210L TO BL 1625L) HAS FRETTING INBOARD OF HINGED LEADING EDGE. SUBMIT TO ATR AND REPAIR PER STRUCTURAL REPAIR INSTRUCTIONS AND SRAS FROM ATR.SDR SWAA2012041303109Fitting · corrodedRT WING OUTER WING REAR SPAR FITTING CORRODED. REMOVED AND REPLACED FITTING PER SRM AND DWG.SDR FDEA201203201034Spar · corrodedREAR SPAR AT LT AFT BOOST PUMP UPPER BONDING POINT CORRODED. REWORKED IAW ATTACHED EA F5700-157909. MINOR REPAIR.SDR UALA2012031901767Spar · corrodedLT WING REAR SPAR WEB CORROSION AROUND FASTENERS BETWEEN IRSS 340 AND IRSS 350 WHERE FUEL BOOST PUMP IS INSTALLED. REF 777EN-57-0300. BLEND OUT REPAIR ACP IAW ECRA 5720-02267.SDR UALA2012031901766Spar · corrodedRT WING REAR SPAR WEB CORROSION AROUND FASTENERS BETWEEN IRSS 340 AND IRSS 350 WHERE FUEL BOOST PUMP IS INSTALLED. REF 777EN-57-0299. BLEND OUT REPAIR ACP IAW ECRA 5720-02266.SDR UHLA2012031900120Spar · crackedLEFT WING SPAR 2 RIB 10 EXTENSION CRACKED AT 3RD HI-LOK FROM BACK. REMOVED AND REPLACED LT WING SPAR 2 RIB 10 IAW EMB 170 SRM 51-43-03 AND 51-43-04. MAJOR REPAIRSDR SROM201203200014Spar · corrodedCORROSION FOUND ON LOWER SPAR CHORD.SDR DALA1510789255Spar · crackedWING REAR SPAR CRACKED. REPAIRED IAW AA 5710-01119.SDR 2012FA0000229Spar · damagedTHIS REPORT IS BEING SUBMITTED IAW AD 200-25-02 R1. LT AND RT WING TIPS WERE DAMAGED DUE TO LOOSE TIE DOWN ROPES. OTBD MOST RIBS WERE REPLACED AND RT AFT SPAR WAS REPAIRED AT STA 195.SDR WX0A071128Spar Cap · corrodedRIGHT WING FWD SPAR STA 533, LOWER CAP FLANGE CORRODED, REMOVED CORROSION, REMAINING THICKNESS .124, 1.0" IN LENGTH, HFEC INSPECTED AREA. NO CRACKS NOTED PER NDT SPM PART 06-10-01-063, PROCEDURE 3. INSTALLED FILLER AND REPAIR STRAP IAW STS ENGINEERING 10-201SDR GLBA2012031401Spar Cap · damagedMAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTED, FOUND THE RT WING MAIN WING LWR SPAR CAP BETWEEN RIBS 17 & 18 IS NOT CRACKED BUT FOUND THAT THE MINIMUM INTER-RIVET PITCH IS 12-15MM WHILE PERFORMING SB 120-57-0036 AND PT I/FCD 120-57-036. REPAIRED IAW EOSDR KC8A20120309001Spar Cap · crackedAIRCRAFT WAS LEAKING FUEL FROM AFT LT SIDE OF CENTER FUEL TANK AREA. FURTHER EXAMINATION REVEALED CRACK IN AFT LOWER CENTER WING SPAR CAP LEFT SIDE. DASSAULT FALCON JET HAS BEEN CONTACTED AND THEY HAVE PROVIDED A REPAIR.SDR FDEA201203050785Spar · corrodedLEFT WING REAR SPAR HAS CORROSION. BLEND LIMIT TOLERENCES HAVE BEEN EXCEEDED IAW EA F-2822-7-5009, PT3, STEP B1 ACCOMPLISHED EA F-5710-156998 STEPS 1 THRU 5.SDR GLBA2012030101Spar Cap · chafedMAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION, FOUND A CHAFE ON THE LT WING FWD LOWER SPAR CAP AT BL 29.5, APPROX 1" BY .312" AT WIDEST POINT, .125" TO .187" DEEP AT DEEPEST POINT. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONSSDR MASA2012030134506Spar · gougedRT WING AT WS 158.00 HAS GOUGE FROM TOOLING ON FWD FACE MEASURES .085"L X .085"W X .035" DEEP. REPAIRED AREA IN ACCORDANCE WITH BOMBARDIER REO 690-57-21-038.SDR CA120321011Spar · chafed(CAN) LT WING FRONT SPAR UPPER FLANGE AT RIB 4 AREA HAS CHAFE DAMAGE UNDERSIDE AT FAIRING ATTACH POINT. DAMAGE IS COMMON DUE TO FAIRING CLIP MOVEMENT.SDR AALA20120223034Spar · corrodedCORROSION ON REAR SPAR AT DEFUEL VALVE IRSS 206.75. REMOVED CORROSION PER SRM 51-10-02. REPAIRED PER EA B757-57-021959.SDR FY4Y201202226Spar · corrodedDURING PERFORMED 6C CHECK, CORROSION WAS FOUND ON FUSELAGE WING CENTER SECTION REAR SPAR WEB BS 870 LBL 25 AND 35 TO 39 WL 184. AFTER CORROSION REMOVED, CLEAN UP DEPTH WAS OVER LIMITS PER SRM 57-10-1 PAGE 12.SDR FY4Y201202225Spar · corrodedDURING PERFORMED 6C CHECK, CORROSION WAS FOUND ON FUSELAGE WING CENTER SECTION REAR SPAR WEB BS 870 RBL 35 TO 43 WL 184. AFTER CORROSION REMOVED, THE CLEAN UP DEPTH WAS OVER LIMIT PER SRM 57-10-1 PAGE 12.SDR DXTA2012062805020Spar Cap · damagedON DISASSEMBLY UPPER SPAR CAP PANEL, DOUBLE DRILLED HOLE IN INBD SIDE OF EHS 66.5 HINGES SUPPORT ASSY .SDR UALA2012022101050Spar · corrodedLEFT WING REAR SPAR CORROSION AT AFT FUEL PUMP. CATEGORY 'A' REPAIR ACCOMPLISHED IAW ECRA 5720-02245 AND AMECO 777EN-57-0289-01.SDR AALA20120224006Spar · corrodedCORROSION FOUND ON FASTENER HOLES ON UPPER FORWARD SPAR AFTER REMOVAL OF LEADING EDGE SKIN AT LOCATION 32 INCHES, 37.5 INCHES AND 41 INCHES FROM INBOARD END. ACCOMPLISHED NESTED ANGLE REPAIR SRM 51-70--12-0G AND EA COMP-57-022040.SDR UALA2012022101049Spar · corrodedRIGHT WING REAR SPAR WEB CORROSION AT IRSS 340. BLEND OUT REPAIR ACP IAW ECRA 5720-02244, AMECO 777EN-57-0288-01. CATEGORY A REPAIR.SDR R61A201202190149Spar · crackedWHILE COMPLYING WITH A INSPECTION OF THE RIGHT WING, AFT SPAR, RIB 10 AREA FOR ANY CRACK LIKE VISUAL AND EDDY CURRENT INDICATIONS, PER EMBRAER INSTRUCTIONS. INSPECTION NOTED A CRACK INDICATION IN A FASTNER HOLE ON HORIZONTAL AREA, AFT SPAR AT RIB 10, VERIFIEDSDR DALA1504149263Spar · crackedWING REAR SPAR CRACKING REPAIRED IAW AA 5710-01119.SDR DALA1400810965Spar Cap · crackedA CRACK LESS THAN 2 INCHES ON LOWER SPAR CAP RADIUS. REPAIRED IAW ERA 500101-14.SDR DALA1209070965Spar Cap · crackedRIGHT WING LOWER SPAR CAP AT ATTACH POINT FOR INBD HINGE FITTING AT STA 164 HAS A 1.6" CRACK AT INBD HOLE. INSTALLED TEMP REPAIR PER EA 09-471576-12AD ME06 OPN 0601 AND DRAWING J060271-510.SDR IPXA12M72036Spar · corrodedINSPECTION TYPE: 2C, LEFT WING UPPER REAR SPAR SURFACE HAS CORROSION AND PANEL LIFTING, LWS 608.25 TO 638.25. ACCOMPLISHED STA-SA EA 011-5720-01-A3705 I/R AND EO MD11-5720-46237-A.SDR AALA20120214TUL04Spar · corrodedFORWARD SPAR CORRODED UNDER BOOST PUMP UPPER BONDING STRAP, INSIDE NUMBER 2 KRUGER FLAP WELL. REPLACED FORWARD SPAR SUPPORT BRACKET PER EA B737-57-021843.SDR SWAA2012021501487Stiffener · crackedWING CENTER SECTION REAR SPAR VERTICAL STIFFENER CRACKED AT BS 663.75, LBL 6.15. REPAIRED STIFFENER PER EA.SDR R61A201202060083Spar · crackedWHILE PERFORMING AILERON CABLE REPLACEMENT, A FUEL LEAK WAS NOTED ON THE LEFT WING AROUND RIB 10, AFT SPAR. MAINTENANCE PERFORMED A LEAK CHECK TO SEE WHERE THE FUEL WAS COMING FROM PER EMB 170 AMM. AFTER THE OPENING OF THE FUEL TANK PANEL THEY DISCOVERED A 4SDR CA120202006Spar · cracked(CAN) VISUAL INSPECTION WITH LIGHT AND MIRROR THRU END, RIB BS 24 INDICATED LINES. CLOSER INSPECTION WITH VIDEO CAMARA FOUND THE CRACKS.SDR SWAA2012021701518Structure · crackedRT WING CRACKED ON UPPER CHORD LOCATED AT WBL 114, STR 2. REPAIRED CHORD IAW EO AND EA.SDR SWAA2012021701517Structure · crackedLEFT WING CRACKED ON UPPER CHORD LOCATED AT WBL 114, STR 2. REPAIRED CHORD IAW EO AND EA.SDR FDEA201201280364Spar Cap · crackedDURING ACCOMPLISHMENT OF EO 8-5710-7-5007, P2 RT WING REAR SPAR LOWER CAP OTBD FASTENER HOLES , NR 4 AFT AND NR 6 FWD, INDICATED CRACKS IAW NDT INSPECTION COMPLIED WITH EA 8-5710-156937, REV B. 2 HOLE WERE OPENED TO 0.370 AND 0.510" AFTER COLD WORKING AND SDR NI6R20120131002Spar · brokenAT WING STATION 40, LT SIDE, A CRACK JUST OTBD OF THE FUSELAGE SKIN APPROX 20-24 INCHES LONG WAS DISCOVERED DURING PSE EDDY CURRENT INSPECTION. THE BREAK STARTS AT THE FRONT SPAR NR 22 RUNNING AFT ALONG WITH THE NEXT STRINGER NR 21 AFT OF THE SPAR, WHICH HAD SDR R61A20120062Spar · crackedWHILE PERFORMING FUEL LEAK INSPECTION IN PIT ON LEFT WING, MAINTENANCE DISCOVERED A FIVE INCH CRACK IN THE AFT SPAR LOCATED BETWEEN RIB 10 AND RIB 11. MAINTENANCE IS PERFORMING WING REPAIR PER ETD 2012-170-01018.SDR UALA2012012400490Spar · corrodedRT WING REAR SPAR WEB CORROSION AT IRSS 340.00. MAJOR REPAIR ACCOMPLISHED: BLEND OUT REPAIR ACP IAW ECRA 5720-02228 AND 777EN-57-0274-01. PER EN, THIS REPAIR IS CLASSIFIED AS CATEGORY A AND NO SUPPLEMENTAL INSP REQUIRED. TEXT INCOMPLETE, SEE ECRA.SDR ABXR2012012300015Spar · corrodedDURING INSPECTION, FOUND REAR SPAR WEB CORRODED UNDER RT FORK. REPAIRED IAW SRM AND REA 46963REA10.SDR ABXR2012012300012Spar · corrodedDURING INSPECTION FOUND CENTER WING REAR SPAR CORRODED AT STA 955 INBD OF PICKLE FORK. REPAIRED IAW SRM AND REA 46963REA12.SDR FDEA201201120106Spar · crackedCRACK INDICATION FOUND ON 4TH LAYER FROM BELOW OF HOLE 'S' DURING HFEC OPEN HOLE INSPECTION ON RT SIDE CENTER WING BOX REAR SPAR BOTTOM PANEL AT FRAME 47. REPAIR CARRIED OUT AT RT SIDE CENTER WING BOX FRAME 47 HOLE 'S' IAW EA 6-5710-155862 PART 1. REPAIR CLSDR SWAA2012021001330Stiffener · crackedMAIN WHEEL WELL REAR SPAR STIFFENER CRACKED AT LBL 6.15. REPAIRED STIFFENER IAW EO & EA.SDR DALA1517969236Spar · crackedWING REAR SPAR CRACKED. REPAIRED IAW AA5710-01119.SDR DALA1500589234Spar · crackedWING REAR SPAR CRACKED. REPAIRED IAW AA 5710-01119.SDR CA111228007Spar · buckled(CAN) DURING ROUTINE INSPECTION, WITH ACFT ON JACKS, FOUND RT UPPER WING SKIN BUCKLING BETWEEN WS 30.0 & WS 49.0, BOTH FWD & AFT SKINS. ALSO FOUND, AFT RT WING UPPER SKIN SLIGHTLY BUCKLED AND LIFTING AT FWD. MAIN SPAR JOINT AT WS49.0 & FUSELAGE BS 137.0 JOINSDR CALA2011122200817Spar · corrodedRIGHT WING L/E FRONT SPAR WEB FOUND CORRODED AT OFSS 550. SPAR WEB CORROSION REMOVED. BLEND OUT DEPTH:0.042" ORG:0.162" WIDTH:1" LENGTH:3" OUT OF SRM 57-20-10 ALLOWABLE DMG 1 FIG 103 LIMITS. WORK ACCOMPLISHED AS PER EC5721-01328, SRM 51-10-02, 51-20-01.SDR UALA2011122107028Spar · corrodedRIGHT WING TE IRSS 350 REAR SPAR WEB AFT CORRODED. BLENDED OUT CORRODED AREA, SPOT FACED FASTENER HOLE, FLAP PEENED AREA, ALODINED AND PRIMED PER ECRA 5720-02217.
Back to JASC 5711