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 n_number = 'N970FD' 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 n_number = 'N970FD' 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 FDEA202605050561Module · faultedAFTER TAKEOFF, GEAR DISAGREE AND GEAR DOORS EICAS MESSAGES APPEARED ACCOMPANIED BY AN AUDIBLE AND TACTILE INDICATION THAT THE GEAR AND/OR GEAR DOORS WERE NOT RETRACTED. APPROXIMATELY 3 MINUTES LATER ALL EICAS MESSAGES AND ACCOMPANYING INDICATORS CEASED. ASDR FDEA202506030833Skin · crackedL/T WING # 2 SLAT POSSIBLE CRACK ON SKIN AT BACK SIDE ON LOWER AREA OF O/B MAIN TRACK TRIMMED DAMAGE AREA, LH WING # 2 SLAT O/B MAIN TRACK IAW B757 SRM 57-43-01-2R FIG 201 REP 4, FORMED, TRIMMED, LOCATE, DRILLED AND INSTALLED REPAIR PARTS IAW B757 SRM 57-4SDR FDEA202506030832Skin · crackedLE SLAT NO 9 INTERNAL SKIN WITH CRACK REMOVED L/E SLAT NO 9 INTERNAL SKIN PANEL IAW B757 SRM 51-40-02-0G, FORMED TRIMMED, LOCATED, DRILLED AND INSTALLED NEW SKIN PANEL IAW B757 SRM 51-40-02-0G AND BOEING DWG # 114N4076 REV C.SDR FDEA202506030831Skin · crackedL/T WING # 1 SLAT POSSIBLE CRACK ON SKIN AT BACK SIDE ON LOWER AREA OF I/B MAIN TRACK TRIMMED OUT DAMAGE AREA L/T WING # 1 SLAT ON SKIN AT I/B MAIN TRACK IAW B757 SRM 57-43- 01-2R FIG 201 REP 4, FORMED, TRIMMED, LOCATED, DRILLED AND INSTALLED REPAIR PARTS IAWSDR FDEA202506030830Skin · crackedLE SLAT NO 8 INTERNAL SKIN WITH CRACK REMOVED SKIN PANEL L/E SLAT NO 8 IAW B757 SRM 51-40-02-0G FORMED, TRIMMED, LOCATED DRILLED AND INSTALL NEW SKIN PANEL IAW BOEING DWG # 114N4077 REV D AND B757 SRM 51-40- 02-0G.SDR FDEA202307281329Unknown · unknownR-3 DOOR, STRINGER CLIP DEFORMED AT STRINGER S-13R BETWEEN BS 1340 AND BS 1360. REMOVED AND REPLACED DEFORMED STRINGER CLIP IAW B757 SRM 51-40-02 AND BACDWG 146N6313 REV. C FABRICATION ON NR N00269SDR FDEA202307261306Retainer · crackedR/H MLG TRUNNION DOOR SEAL RETAINER IS CRACKED.. REMOVED SEAL AND RETAINER, FABRICATED NEW RETAINER PER BAC DWG 113N8200 AND FEDEX EA # F-3210- T0375397 TITLE : LANDING GEAR - MAIN GEAR AND DOORS - RH MLG TRUNNION FAIRING DOOR, SEAL RETAINER, ALTERNATE FINISDR FDEA202307251292Slat · delaminated#3 SLAT UPPER SURFACE TRAILING EDGE WEDGE HAS AN AREA OF DISBOND LOCATED 52" FROM THE OUTBOARD EDGE AND 4" FROM THE TRAILING EDGE. APPROX 2.5" IN DIAMETER. REPAIRED #3 SLAT SURFACE TRAILING EDGE WEDGE 2 EA DAMAGED AREAS IAW B757 SRM 51-10- 02, 57-43-02-0I,5SDR FDEA202307201254Unknown · unknownMAIN CABIN - FLOOR PANEL AT STA 440 TO STA 560 , LBL24 TO LBL 45 IS SATURATED IN HYDRAULIC FLUID REMOVED, FABRICATED AND REPLACED FLOOR PANEL IAW B757 AMM 53-01-01-4 AND DWG SRZ- 25-005 REV RSDR FDEA202211012702Skin · damagedWHILE WORKING #1 O/B T/R C DUCT CHANGE FOUND DAMAGE ON UPPER PORTION OF INBOARD #1 ENG FAN COWL REPAIRED IAW EA F-7110-T0371402 THIS IS A MAJOR REPAIRSDR FDEA202204191001Collar · crackedL1 DOOR HOLD OPEN LOCK COLLAR BROKEN. REMOVED AND REPLACED L1 DOOR OPEN LOCK REF AMM 52-11-08-4. OPS CHECK GOOD.SDR FDEA202204191000Gust Lock · failedMDIS 970 52-10 7067 19APR22 DAY OPEN U R1 DOOR HOLD OPEN LOCK COLLAR BROKEN FACT 21APR22 18:02 MEM R1 DOOR HOLD OPEN LOCK (MPN: 654N0244-8) REPLACED SDR FDEA202203300780Valve · noneL-ENG ANT-ICE EICAS MESSAGE DISPLAYED ALONG WITH VALVE LIGHT ON L ENGINE ANTI ICE SWITCH DISPLAYED DURING DESCENT WHEN SELECTED ON AND STAYED ON FOR REMAINDER OF FLIGHT. REMOVED AND REPLACED L ENGINE ANTI-ICE VALVE M/M 30SDR FDEA202101160132Valve · inoperativeNR 5 BRAKE INOPERABLE FUNCTIONS NORMALLY IN ALTERNATE (LT HYD SYS). REPLACED LEFT ANTISKID SHUTTLE VALVE MODULE, IAW 757 MM 32-42-07-4. OPERATIONS AND LEAK CHECK GOOD.SDR FDEA202010230330Case · corroded#1 ENG AT 9 O`CLOCK LP COMPRESSOR CASE OUTER SURFACE HAS CORROSION IN EXCESS OF 10 AROUND (FWD) MATING FLANGE TO INLET (UNDER KEVLAR WRAP). REMOVED AND REPLACED #1 ENGINE.SDR FDEA202007081461Gust Lock · malfunctionedL ENTRY DOOR GUST LOCK DOES NOT LATCH IN THE RELEASE POSITION.SDR FDEA201907091515Bracket · damagedWIC 5782600-00-01 AGING AIRCRAFT INSPECTION- LT I/B MAIN FLAP O/B SIDE OF #3 FLAP TRACK FWD BRACKET HAS ELONGATED HOLES. REMOVED ,FABRICATED AND INSTALLED NEW BRACKET AT LT I/B MAIN FLAP O/B SIDE OF #3 FLAP TRACK IAW DWG 113N1767 REV.A & E.SDR FDEA201907011451Floor Support · corrodedMAIN CABIN BETWEEN STA.1680-1720, BL.0 - RBL.54 FLOOR SUPPORT WEB CORRODED. REMOVED CORROSION FROM M/C AFT DECK WEB STA.1680 - 1720 , BL.0 - RBL.54, MAX MATERIAL LOSS AT RBL.46 STA.1680, ORIGINAL THICK. .071, MATERIAL LOSS .015, REMAIN. MATERIAL RBL.46 .056, ASDR FDEA201907011449Skin · corrodedCORROSION, APU LT ACCESS DOOR FUSELAGE CUTOUT STRUCTURE FWD END, APPROX. BS.1887.5, INNER SURFACE, JUST AFT OF THE APU FIREWALL. COMPLIED WITH EA#F-5330-T0347755 P1. FUSELAGE-PLATES & SKINS- CORROSION AT STA.1885, S-17L.SDR FDEA201907011442Floorbeam · corrodedCOCKPIT STA.345 BETWEEN LBL5-LBL 24 FLOORBEAM CORRODED. CORROSION ON EXISTING FLOORBEAM "T "CAP REPAIR OUT OF LIMITS, REMOVED EXISTING "T" CHORD ANGLE & REPAIR SPLICES, CUT OUT FLOORBEAM FROM RBL.12 TO RBL.53,FABRICATED NEW "T" CHORD & REPAIR PARTS & INSTALLEDSDR FDEA201907011450Skin · corrodedCORROSION APU RT ACCESS DOOR FUSELAGE CUTOUT STRUCTURE FWD END, APPROX. BS.1887.5, INNER SURFACE, JUST AFT OF THE APU FIREWALL. EVAL. CORROSION DAMAGE WITH 100% MATERIAL LOSS OUT OF LIMITS, FABRICATED AND INSTALLED REPAIR DOUBLER AND TRIPLER IAW SRM 53-80-01-2SDR FDEA201907011448Frame · gougedINSIDE FWD ACC. COMPARTMENT, FRAME AT STA. 231.25 HAS A GOUGE IN UPPER RADIUS AT BL.0. CUT OUT DAMAGE & FABRICATED AND INSTALLED FRAME REPAIR AT STA. 231.25 BL.0 LOWER FRAME SECTION INSIDE FWD ACC. COMPARTMENT IAW SRM 53-00-07-2R, REPAIR 7 FIG 202.SDR FDEA2019021430395Handle · obstructedCOULD NOT ARM SLIDE ON RIGHT HAND ENTRY DOOR. RELOCATED CORD DIDN'T LET CLOSE PROPERLY, OPERATE DOOR SEVERAL TIMES , OPS CKS NORMAL REF AMM 52-11-01-6.SDR FDEA201806071418Static Line · tangledRIGHT FORWARD ENTRY DOOR WILL NOT FULLY DISARM. SLIDE ARM LIGHT WILL EXTINGUISH, BUT EVACUATION SLIDE LEVER WILL NOT MOVE FULLY TO THE DISARM POSITION. FOUND STATIC LINE TANGLED ON THE FORWARD PART OF THE GIRT BAR, RESTOWED STATIC LINE. PERFORMED OPS CHECSDR FDEA201709222674Plunger · damagedRAMP REPORTED THE MAIN CARGO DOOR WILL NOT CLOSE. FOUND THE TIP MISSING FROM PLUNGER ON MAIN CARGO DOOR SEQUENCE VALVE. REPLACED THE TIP IAW SRM 51-40-02. MAIN CARGO DOOR CHECKED GOOD IAW 52-32-00-2. ACFT OK FOR SERVICE.SDR FDEA201705241502Bottle · emptyL1 DOOR WAS ARMED, CREW ATTEMPTED TO OPEN DOOR, L1 EMERGENCY ASSIST BOTTLE DEPLETED SLIDE DID NOT DEPLOY.SDR FDEA201612114381Warning Light · false activationAT LEVEL OFF, RECEIVED A CTR L FUEL PUMP ALERT WITH 5.1 OF FUEL IN CENTER TANK. REACTIVATED LT CTR OVERRIDE FUEL PUMP. AUDIBLE CHECKED THE LT CTR OVERRIDE PUMP FOR OPERATION, PUMP IS RUNNING. TRANSFERRED 22 KLBS INTO CENTER FUEL TANK. LT CTR OVERRIDE PUMSDR FDEA201609213326Window · failedAT CRUISE FL290, A LOUD BANG WAS HEARD THEN ARCING & SHATTERING OF FO'S FORWARD WINDOW. REPLACED RT FWD WINDOW. OK FOR SERVICE.SDR FDEA201507212287Fseu · inoperativeON DEPARTURE, WHEN SELECTING FLAPS UP, HAD A LE DISAGREE EICAS. FLAP INDICATOR SHOWED STUCK BETWEEN 1 DEGREE & UP. PERFORMED CHECKLIST & RETURNED TO DEPARTURE. R & R FSEU IN NR 1 POSITION. OPS CHECKED IAW AMM 27-51-01-2 PAGE 1-16. FLAPS & SLATS OPERATED NSDR FDEA201506201930Skin · dentedPROTRUDING DENT STATION 523 AT STRINGER 26L. COMPLIED WITH EA F-5330-TO318148 PART 1 FUSELAGE PLATES & SKIN. REPAIR AT STATION 523 BETWEEN STRINGERS 26L - 27L.SDR FDEA201506201929Skin · dentedTWO EACH DENTS STATION 490 BELOW 27L. COMPLIED WITH EA F-5330-TO318149 PART 1 FUSELAGE PLATES & SKINS. REPAIR AT STATION 490 BETWEEN STRINGERS 27L - 28L.SDR FDEA201506161821Skin · dentedLEFT AILERON UNDER SIDE HAS SMALL DENT. BONDED REPAIRED IAW SRM 51-70-17 PG 14/15 PARA 4, 57-60-01-212. OPS CHECKED GOOD IAW AMM 27-11-00-0.SDR FDEA201312203031Bolt · out of positionAFTER LANDING GOT FLAP LE SLAT AYSYM EICAS MESSAGE BETWEEN UP & 1 POSITION. NR 1 FLAP, SLAT ELEX UNIT BITE SHOWS RT SLAT DRIVE. NR 2 UNIT SHOWS RT SLAT XMITTER. TROUBLESHOT IAW FIM 27-51. FAULT TREE 805, FOUND NR 6 LE SLAT CTR OTBD TORQUE TUBE DRIVE SPLINESDR FDEA201308081809Wire · looseEMERGENCY EXIT SIGN ABOVE R1 DOOR INOPERATIVE. FOUND R1 DOOR EMERGENCY EXIT LIGHT WIRE NR 1 NOT PROPERLY SEATED AT QUICK DISCONNECT, RESEATED WIRE IAW SMP. R1 DOOR EMERGENCY EXIT LIGHT OPS CHECKED GOOD IAW MM 33-51-01-2. ACFT OK FOR SERVICE.SDR FDEA201307231638Battery Pack · inoperativeSLIDE ILLUMINATION LIGHT AND CENTER EMERGENCY EXIT SIGN INOPERATIVE. R & R EMERGENCY LIGHT POWER SUPPLY ASSY IAW AMM 33-51-07-2. OPS CHECKED GOOD.SDR FDEA201306251413Skin · crackedLT WING NR 3 SLAT, AT INBD TRACK, JUST OUTBOARD, COVE SKIN CRACKED, COVE SKIN FOUND TO BE OUT OF LIMITS IAW-SRM-57-43-01, FIG 101, SHEET (2 OF 4) NOTE B, NO CRACKS ALLOWED. REMOVED COVE SKIN AT LT WING NR 3 SLAT OSS 471.30-483.30. FABRICATED NEW COVE SKIN OSDR FDEA201306131370Crease Beam · crackedCREASE BEAM OTBD ANGLE CRACKED AT BS 1641, S17L. REPAIRED CREASE BEAM IAW EA 757-5361-16-F4175. MAJOR REPAIR.SDR FDEA201306131271Skin · debondedLEFT WING INBD FLAP, TOP OTBD PANEL LOWER SURFACE, DISBONDED. REPAIRED SKIN IAW SRM 51-70-10. REPAIR 4. MAJOR REPAIRSDR FDEA201305311154Skin · misrepairedFUSELAGE SKIN BS 395-418 BETWEEN S2-4L MISREPAIRED. REPAIRED IAW EA F-5330-T0300578. MAJOR REPAIRSDR FDEA201305311153Stringer Fitting · corrodedLOWER LOBE STR 26L AFT END ATTACHMENT FITTING HAS CORROSION BS 1720. REMOVED CORROSION ON STRINGER 26L END FITTING IAW SRM 51-10-02, ORIGINAL THICKNESS .090, REMAINING THICKNESS .066, NO SRM ALLOWABLE LIMITS. R & R END FITTING IAW DWG 146N8849, SH 1 REV- ANDSDR FDEA201305221068Skin · damagedRT WING INBD FLAP, TOP OTBD PANEL, LOWER SURFACE HONEYCOMB EDGE VOID. REPAIRED IAW SRM 51-70-10. REPAIR 4. CAT "A" MAJOR REPAIR.SDR FDEA201305211057Fitting · wornBS 935, BL 0, FITTING HAS ONE OVERSIZED HOLE OF 0.352 IN DIAMETER. THE MATING FLOOR STRUCTURE HAS SAME HOLE SIZE AT SAME LOCATION AT STA 935, BL0. REPAIR WAS ACCOMPLISHED, DUE TO DISCREPANCY EFFECTING THE PTF CONVERSION, ON STAM W/C 49925760001 AND (STAM) EASDR FDEA201305161011Skin · dentedEXTERNAL FUSELAGE SKIN BS 1600-1620 BETWEEN S25-26R HAS TWO DENTS. . BS 1613 BETWEEN S26-25R A=0.6 Y=.045 A/Y= 13.33 OUT OF LIMITS. REPAIRED IAW SRM-53-00-01, FIG 201, REPAIR NR 7. MAJOR REPAIR.SDR FDEA201305151005Skin · corrodedNR 1 SLAT COVE SKIN LWR EDGE CORRODED. REMOVED CORROSION IAW-SRM-51-10-02 ON NR 1 SLAT COVE SKIN LWR EDGE, CHECKED LIMIT .050 MAT. LOSS .009, FOUND OUT OF LIMITS, IAW- SRM-57-43-01, FIG 101, SHEET 4, DET IV, R & R COVE SKIN IAW-SRM-51-40-02 AND DWG 114N4075SDR FDEA201305140982Fitting · crackedNR 2 PYLON STRUT TO DIAGONAL BRACE FITTING RT SIDE AFT INBD HOLE SHOWS CRACK INDICATION AT THE 4:30 POS IN THE ALUMINUM BULKHEAD ONLY. COMPLIED WITH EA F-5450-T0300259THIS IS A MAJOR REPAIR AND IS CONSIDERED CATAGORY "A".SDR FDEA201305100969Skin · misrepairedSKIN MISREPAIRED BS 1700 -1720 S15-16L. REPAIRED IAW EA F-5330-T0300418, CAT "B" MAJOR REPAIR.SDR FDEA201305070932Skin · gougedLEFT FUSELAGE EXTERNAL SKIN HAS GOUGES AT STA. 1862 , S9L.SDR FDEA201304270871Frame · crackedMAIN CABIN BS 760 BETWEEN S8- 9R FRAME IS CRACKED. FOUND CRACKED AT FAST HOLE , CRACKED IS NOT ALLOWED IAW SRM 53- 00-07, REPAIRED FRAME IAW SRM 53-00-07, REPAIR 3. MAJOR REPAIR.SDR FDEA201304240849Skin · crackedNR 2 SLAT COVE SKIN, OSS 677.5 CRACKED AT FASTENER. REMOVED CRACKED NR 2 SLAT COVE SKIN IAW-SRM-51-40-02, REPLACED CRACKED COVE SKIN WITH NEW COVE SKIN IAW-SRM-51-40-02 AND DWG 114N4076, CAT"A" MAJOR REPAIR.SDR FDEA201304230834Skin · crackedNR 1 SLAT COVE SKIN , OSS 736.7, CRACKED AT FASTENER. REMOVED CRACKED NR 1 SLAT COVE SKIN, IAW-SRM-51-40-02, FOUND OUT OF LIMITS, IAW-53-00-71. REPLACED CRACKED COVE SKIN WITH NEW COVE SKIN, IAW-SRM-51-40-02 AND 757 DWG 114N4075, NR 1 SLAT- O.S.S. -736.7 TO
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