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 = 'N403AS' 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 = 'N403AS' 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 ASAA2026051466099Support Beam · damagedCENTER SECTION LOWER SUPPORT BEAM LOWER CHORD CHAFED THROUGH GROUNDED - YES. CAT A REPAIR REF SRM 57-10-13-2R-3SDR ASAA2026040665352Door · stuckAIRCRAFT RIGHT AFT SERVICE DOOR STUCK. GROUNDED - YES. FREED RIGHT AFT SERVICE DOOR, REF FIM 52-10 TASK 811. DOOR OP CHECK GOOD FROM BOTH INSIDE AND OUTSIDE.SDR ASAA2025092061008Door · out of limitsF/A REPORT R1 DOOR DIFFICULT TO CLOSE. GROUNDED - YES. PERFORMED GALLEY SERVICE DOOR SYSTEM TEST. R1 DOOR CLOSE FORCE IS WELL ABOVE 600 IN-LBS AND IS OUT OF LIMITS. REF AMM 52-41-00. FOUND R1 DOOR OUT OF RIG, ADJUSTED R1 DOOR REF AMM 52-41-00, AND PERFORMED DOSDR ASAA2025092261022Sign · detachedMID-CABIN EXIT SIGN FALLING DOWN. GROUNDED - YES. MID CABIN EXIT SIGN FOR OWE REPOSITIONED & FASTENERS TIGHTENED REF AMM 33-51-01-960-802. OPS CHECKS OF LIGHTING FUNCTION GOOD.SDR ASAA2025081960250Handle · unsecureFLIGHT ATTENDANT REPORTS THAT DOOR L-2 SECURING LEVER WAS MOVING IN FLIGHT UPWARDS BETWEEN 1 TO 2 INCH AND SHE WOULD APPLY DOWNWARD PRESSURE TO THE LEVER BUT IT WOULD NOT STAY SECURED AT ITS BOTTOM RETENT. ADDITIONALLY SHE MENTIONED THAT THE CATERS HAD DIFFICUSDR ASAA2025081360078Lens · missingR1 DOOR EXIT SIGN COVER MISSING. GROUNDED - YES. INSTALLED NEW R1 DOOR EXIT LENS. PER AMM 33-51-01 OPS CHECK GOOD. NO DISCREPANCIES NOTED.SDR ASAA2025042857637Guide Arm · out of adjustF.A REPORTS R2 DOOR NOT CLOSING PROPERLY. GROUNDED - YES. UNSTUCK R2 DOOR, ADJUSTED R2 DOOR GUIDE ARM REF AMM 52-13-00-820-016. R2 DOOR OPENING & CLOSING OP CKS GOOD. PRESSURIZED AIRCRAFT TO 4 PSID, LK CKS GOOD.SDR ASAA2025031956731Lamp · inoperativeWHILE PERFORMING T/C 78233001 R/H SLIDE LT AFT OF WING DID NOT ILLUMINATE. GROUNDED - YES. RELAMPED R/H SLIDE LT AFT OF WING AMM 33-51-04 OP CK GOOD.SDR ASAA2025031956730Lamp · inoperativeWHILE PERFORMING T/C 78233001 R2 DOOR SLIDE LT DID NOT ILLUMINATE. GROUNDED - YES. RELAMPED R2 DOOR SLIDE LT AMM 33-51-04 OP CK GOOD.SDR ASAA2025021155954Door · bindingFA REPORTS R2 DOOR JAMMED UPON CLOSING TSAR174M. GROUNDED - YES. OPENED R2 DOOR AND C/W AFT ENTRY DOOR INSPECTION/CHECKPER AMM 52-3-00 NO DEFECTS NOTED. CLOSED R2 DOORAND FOUND OPS NORMAL PER AMM 52-13-00.SDR ASAA2024121454587Door · no discrepancyAFT SERVICE DOOR R2 NOT CLOSING. GROUNDED - YES. PERFORMED A G.V.I OF R2 DOOR, NO DAMAGE NOTED. PERFORMED A OPEN/CLOSE R2 DOOR OP TEST REF AMM 52-13-00, OPS TEST NORMAL. PERFORMED A PRESSURIZATION CHK, NO DEFECTS NOTED REF AMM 21-00-05.SDR ASAA2024112154058Sign · inoperativeTHE "EXIT" SIGN NEAR THE L2 DOOR NEEDS REPAIR. GROUNDED - YES. REMOVED & REPLACED EXIT SIGN AT L2 DOOR. IAW 33-51-01-960-802. OPS CK NORMAL . THIS CLEARS PLT/ EA 900ER-33EA-27892SDR ASAA2024090252245Lens · detachedAFT EXIT SIGN AIRCRAFT LEFT ABOVE FLIGHT ATTENDANTS SEAT CAME OFF. GROUNDED - YES. INSTLD NEW EXIT SIGN LENS COVER REF AMM 33-51-00.SDR ASAA2024061750360Battery Pack · dischargedWHILE PERFORMING T/C 78233008 FOUND FWD GALLEY EMERGENCY AISLE LIGHT INOP. GROUNDED - YES. REMOVED AND REPLACED BATTERY PACK M1675 REF WDM 33-51-11, EAL LIGHT OPS CHECKS GOOD AFTER REMAINING ON CHARGE, REF AMM 33-51-06-610-802.SDR ASAA2024031848538Power Supply · inoperativeEMERGENCY LIGHTS ASSOCIATED WITH EMERGENCY POWER SUPPY M1694 INOP. GROUNDED - YES. REMOVED AND REPLACED EMER LIGHT PWR SUPPLY AT M1694 IAW B737NG AMM 33-51-06-960-806. EMER LIGHT OPS CK GOOD. (S/N 100929)SDR ASAA2024031848537Power Supply · inoperativeEMERGENCY LIGHTS ASSOCIATED WITH EMERGENCY POWER SUPPLY M2626. GROUNDED - YES. REMOVED AND REPLACED EMER LIGHT PWR SUPPLY AT M2626 IAW B737NG AMM 33-51-06-960-806. EMER LIGHT CK GOOD. (S/N 100038)SDR ASAA2024031848536Power Supply · inoperativeEMERGENCY LIGHTS ASSOCIATED WITH EMERGENCY POWER SUPPLY M1670 INOP. GROUNDED - YES. REMOVED AND REPLACED EMER LIGHT PWR SUPPLY AT M1670 IAW B737NG AMM 33-51-06-960-806. EMER LIGHT OPS CK GOOD. (S/N 100925)SDR ASAA2024031848535Power Supply · inoperativeEMERGENCY LIGHTS ASSOCIATED WITH EMERGENCY POWER SUPPLY M1676 INOP. GROUNDED - YES. REMOVED AND REPLACED EMER LIGHT PWR SUPPLY AT M1676 IAW B737NG AMM 33-51-06-960-806, EMER LIGHT OPS CK GOOD. (S/N 100933)SDR ASAA2024031848534Power Supply · inoperativeEMERGENCY LIGHTS ASSOCIATED WITH EMERGENCY POWER SUPPLY M2335 INOP. GROUNDED - YES. REMOVED AND REPLACED EMER LIGHT PWR SUPPLY AT M2335 IAW B737NG AMM 33-51-06-960-806, EMER LIGHT OPS CK GOOD. (S/N 101616)SDR ASAA2024030548227Mount · corrodedAFT RH LAV AFT OYBD MOUNT FITTING HAS CORROSION AT FLOORBEAM. GROUNDED - YES. BLENDED OUT CORROSION. ORIGINAL THICKNESS 0.180 IAW B737-900ER SRM 53-70-51-0I-1 AND BAC DWG 1518-1212 REMAIN THICKNESS 0.110, REMOVED 0.070OUT OF LIMITS IAW B737-900ER SRM 53-70-51-SDR ASAA2024022848406Seat Track · corrodedR/H MAIN CABIN SEAT TRACKS HAVE WEAR MARKS AND CORROSION THROUGHOUT. GROUNDED - YES. REMOVED DAMAGE AND CORROSION AS READ. ORIG MAT THICKNESS IS .230" REMOVED .027" AT DEEPEST POINT WITH .203" REMAINING FOUND WITHIN ALLOWABLE LIMITS IAW B737-900ER SRM 53-00-52SDR ASAA2024022848403Seat Track · corrodedL/H MAIN CABIN SEAT TRACKS HAVE WEAR MARKS AND CORROSION THROUGHOUT. GROUNDED - YES. REMOVED DAMAGE AND CORROSION AS REQD. ORIG MAT. THICKNESS IS .230", REMOVED .031" AT DEEPEST POINT WITH 0.199" REMAINING. FOUND WITHIN ALLOWABLE LIMITS IAW B737-900ER SRM 53-0SDR ASAA2024022348064Transition Panel · corrodedFWD CARGO COMPARTMENT AT LEFT TRANSITION PANEL HAS SURFACE CORROSION AT 500H +13. GROUNDED - YES. REMOVED CORROSION FROM THE FWD PIT L/H TRANSITION PANEL STA 500H+13 IAW B737-900ER SRM 53-00-53-1A-2.2.D. ORIG THICKNESS IS .040" IAW B737-900ER SRM 53-30-53-01-2SDR ASAA2024022148121Bracket · corrodedDURING REMOVAL OF STRUCTURE FOR REPAIR ON CUSTOMER CARD G1923940, FLOOR SUPPORT BRACKET 147A5676-1 FOUND CORRODED. GROUNDED - YES. REMOVED CORROSION, MEASURED ORIG THICKNESS 0.080, REMAINING THICKNESS 0.025 REMOVED 0.055 OUT OF LIMITS IAW B737-900ER SRM 53-70-SDR ASAA2024021948118Floor Support · corrodedMAIN CABIN FLOOR SUPPORTS STA 947-967 LBL 50 CORRODEDPART RACK. GROUNDED - YES. REMOVED CORROSION, MEASURED ORIG THICKNESS 0.150, REMAINING THICKNESS 0.050 OUT OF LIMITS IAW B737-900ER SRM 53-70-51-1A-1. DRILLED TO FIT NEW INTERCOSTAL STA 947-967 LBL 50 IAW BASDR ASAA2024021948117Floor Support · corrodedMAIN CABIN FLOOR SUPPORT STA 947-967 RBL 25 CORRODED PARTS RACK. GROUNDED - YES. REMOVED CORROSION, MEASURED ORIG. THICKNESS 0.080, REMAINING THCKNESS 0.040, REMOVED 0.040 OUT OF LIMITS IAW B737-900ER SRM 53-70-51-1A-1. DRILLED TO FIT NEW INTERCOSTAL STA 947-9SDR ASAA2024021548226Skin · corrodedN8252008; R-1 DOOR, EXTERNAL HANDLE PAN HAS SURFACE CORROSIONDOT: Z393. GROUNDED - YES. REMOVED WORN HANDLEPAN & INSTALLED NEW HANDLEPAN, REFERENCE B737-900ER SRM 51-40-02 & BAC DWG # 141A6516SDR ASAA2024021548225Skin · corroded8252007; L-2 DOOR, EXTERNAL HANDLE PAN HAS SURFACE CORROSION. GROUNDED - YES. REMOVED DAMAGED HANDLEPAN & INSTALLED NEW HANDLEPAN, REFERENCE B737-900ER SRM 51-40-02 & BAC DWG # 147A6116 REV B.SDR ASAA2024021548220Floor Panel · delaminatedMAIN CABIN AFT WET AREA BOARD DELAME P/N 147A5810-444. GROUNDED - YES. COMPLETED WET LAY UP REPAIR AND REMOVE / REPLACE INSERTS ON MAIN CABIN AFT WET AREA FLOOR BOARD PN: 147A5810-444 IAW B737-900ER SRM 53-0-50-2R-7 REPAIR 7 AND 53-00-50-2R-0.SDR ASAA2024022958120Skin · corrodedN8252009; R-2 DOOR, EXTERNAL HANDLE PAN HAS SURFACE CORROSION. GROUNDED - YES. REMOVED AND REPLACED HANDLE PAN IAW BAC DWG 147A6502 REV A.SDR ASAA2024021548067Floor Panel · delaminatedMAIN CABIN AFT WET AREA BOARD DELAME P/N 147A5810-108. GROUNDED - YES. COMPLETED WET LAY UP REPAIR, REMOVED AND REPLACED 17 INSERTS ON MAIN CABIN AFT WET AREA BOARD PN: 147A5810-108 IAW B737-900ER SRM 53-00-50-2R-7AND 53-00-50-2R-0.SDR ASAA2024021548066Floor Panel · delaminatedMAIN CABIN AFT WET AREA BOARD DELAME P/N 147A5810-445. GROUNDED - YES. COMPLETED WET LAY UP REPAIR AND REMOVE AND REPLLACE INSERTS ON MAIN CABIN AFT WET AREA FLOOR BOARD PN:147A5810-45 IAW B737-900ER SRM 53-00-50-2R-7 REPAIR 7 AND 53-00-50-2R-0.SDR ASAA2024021448533Floor Support · corrodedAFT PIT FLOOR SUPPORT STA 794 TO 827 BL 13.84 HAS CORROSION. GROUNDED - YES. REMOVED DAMAGE FROM AFT PIT FLOOR SUPPORT @ STA 794 TO 827 IAW B737-900ER SRM 53-00-53-1A-2.2.D. ORIG THICKNESS IS .070" IAW B737-900ER SRM 53-60-53-01-2. REMOVED .029", REMAINING .04SDR ASAA2024021448407Pressure Web · corrodedMAIN CABIN AFT PRESSURE WEB UPPER SURFACE HAS SEVERAL AREAS OF CORROSION. GROUNDED - YES. REMOVED CORROSION IAW B737-900ER SRM 51-10-02. NO LIMITS STATED, ACCOMPLISHED ALL STEPS PER EA# 900ER-53EA-26684 REV: P00.SDR ASAA2024021448405Channel · corrodedRH (R2 DOOR AREA) MOP SEAL HAS CORROSION. GROUNDED - YES. REMOVED AND REPLACED MOP SEAL AT STA 887 TO 986.50 RBL 56 I.A.W B737-900ER SRM 51-40-02 AND DWG NO 147A8501 REV.- MATERIAL USED P/N: 147A8540.30, PO: 1083141.2.SDR ASAA2024021448404Web · corrodedLH FLOOR STRUCTURE HAS 4EA AREAS WITH CORROSION. GROUNDED - YES. REMOVED CORROSION IAW B737-900ER SRM 51-10-02. NO LIMITS STATED. FABRICATED NEW WEB P/N 147A5116-19 IAW BAC DWG 147A5116 REV-. ALODINED IAW B737-900 AMM 51-21-41. PRIMED IAW B737-900 AMM 51-21-72SDR ASAA2024021448224Floor Panel · delaminatedMAIN CABIN FWD WET AREA FLOOR BOARD DELAME P/N 141A5810-763. GROUNDED - YES. REPAIRED MAIN CABIN FWD WET AREA FLOOR BOARD P/N 141A5810-763 BY PREFORMING PERMANENT WET LAYUP REPAIR IAW B737-900 SRM 53-00-50-2R-0, 53-00-50-2R-7.SDR ASAA2024021448223Floor Panel · delaminatedMAIN CABN FWD WET AREA FLOOR BOARD DELAME P/N 141A5810-766. GROUNDED - YES. REPAIRED MAIN CABIN FWD WET AREA FLOOR BOARD P/N 141A5810-766 BY PREFORMING PERMANENT WET LAYUP REPAIR IAW B737-900ER SRM 53-00-50-2R-7, 53-00-50-2R-0.SDR ASAA2024021448222Floor Panel · delaminatedMAIN CABIN FWD WET AREA FLOOR BOARD DELAME P/N 141A5810-155. GROUNDED - YES. REPAIRED MAIN CABIN FWD WET AREA FLOOR BOARD P/N 141A5810-155 BY PREFORMING PERMANENT WET LAYUP REPAIR IAW B737-900ER 53-00-50-2R-7, 53-00-50-2R-0.SDR ASAA2024021448221Floor Support · crackedMAIN CABIN FLOOR SUPPORT STRUCTURE IS CRACKED AT STA 540 APPROX LBL2 (MARKED IN RED). GROUNDED - YES. REMOVED AND RELACED MAIN CABIN FLOOR SUPPORT STRUCTURE AT STA 540 IAW B737-900ER SRM 51-40-02 & IAW REF'S AIPC 53-42-11SDR ASAA2024021448098Mount · corrodedLH AFT LAV AFT OTBD MOUNT FITTING HAS CORROSION AT FLOOR BEAM PARTS RACK. GROUNDED - YES. REMOVED DAMAGE IAW B737-900ER SRM 51-10-02. AFTER EVAL REMOVED MORE THAN 50% OF MAT, FOUND TO BE OUT OF LIMITS B737-900ER SRM 53-70-51-1A-1. DRILLED TO FIT NEW INTERCOSTESDR ASAA2024021448065Support · corrodedFWD PIT, AFT BULKHEAD IS CORRODED. GROUNDED - YES. REMOVED DAMAGE FROM FWD PIT AFT BULKHEAD R/H SUPPORT IAW B737-900ER SRM 53-30-08-1A-1.2.C.1. REMAINING THICKNESS: .054" MINIMUM ALLOWABLE REMAINING THICKNESS: .056" AND IS FOUND TO BE OUT OF LIMITS IAW B737-90SDR ASAA2024021448063Floorboard · delaminatedMAIN CABIN FWD WET AREA FLOOR BOARD DELAME P/N 141A5810-183. GROUNDED - YES. REPAIRED MAIN CABIN FWD WET AREA FLOOR BOARD P/N 141A5810-183 NOTED DAMAGE BY PREFORMING PERMANENT WET LAYUP REPAIR TO FACESHEET IAW B737-900ER SRM 53-00-50-WR-7, 53-00-50-2R-O.SDR ASAA2024021448062Floor Support · crackedMAIN CABIN FLOOR SUPPORT STRUCTURE IS CRACKED AT STA 540 APPROX RBL2 (MARKED IN RED). GROUNDED - YES. REMOVE BACK ASSEMBLY IAW B737-900ER SRM 51-40-02. RECEIVED NEW PART #143A5240. PO#1082816.1. LOCATED AND DRILLED NEW PART IAW B737-900ER 51-40-05. INSTALLED FSDR ASAA2024021348401Frame Splice · corrodedAFT CARGO COMPARTMENT, RIGHT HAND FRAME SPLICE CORRODED AT STA 727L (AREA MARKED IN RED). GROUNDED - YES. EVALUATED THE CORRODED AFT PIT R/H FRAME SPLICE AT STA 727L. CORROSION IS LOCATED ON THE INNER CHORD. DAMAGE IS NOT PERMITTED ON THIS LOCATION PER B737-90SDR ASAA2024021348097Frame Splice · corrodedAFT CARGO COMPATMENT, RIGHT FRAME SPLICE CORRODED AT STA 727I (AREA MARKED IN RED). GROUNDED - YES. EVAL'S CORRODED AFT PIT R/H FRAME SPLICE AT STA 727I. CORROSION IS LOCATED ON THE INNER CHORD. DAMAGE IS NOT PERMITED ON THIS LOCATION IAW B77-900ER SRM 53-00-0SDR ASAA2024021248402Web · corrodedMAIN CABIN, AFT CABIN AT STA996(R) HAS CORROSION FOUND. DOT #T834 STREAMER IS ATTACHED. GROUNDED - YES. REMOVED AND REPLACED WEB IAW B737-900ER SRM 51-40-02 & IAW BAC DWG 147A5701 REV: -.SDR ASAA2024021248119Web · corrodedAFT CARGO THRESHOLD SILL HAS CORROSION. GROUNDED - YES. EVALUATED DAMAGE AND REMOVED CORROSION IAW B737-900ER SRM 53-00-53-1A-2 ORIGINAL MAT'L THKS .045 PER B737-900ER SRM 53-60-53-01-2 TABLE 2 REMOVED .022 MAT AND HAD .023 MAT'L, FOUND TO BE OUT OF LIMITS IAWSDR ASAA2024021248096Transition Panel · corrodedAFT CARGO L/H TRANSITION PANEL STA 727-727F HAS 29 PLACES WITH CORROSION. (MARKED IN RED). GROUNDED - YES. REMOVED CORROSION FROM AFT CARGO L/H TRANSITION PANEL STA 727 TO 727F IAW B737-900ER SRM 53-00-53-1A-2. ORIG. THICKNESS IS .040" IAW B737-900ER SRM 53-60SDR ASAA2024021248095Doubler · corrodedLOWER FUSELAGE STA727 CENTER DRAIN DOUBLER HAS CORROSION AROUND FASTNERS GROUNDED - YES. REMOVED AND REPLACED CENTER DRAIN DOUBLER AT LOWER FUSELAGE STA 727 IAW B737-900ER SRM 51-40-02 AND DWG NO. 146A0070 REV A. DWG 146A3239 REV -, BOEING CONTROL # 270917615
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