N610AW
Service difficulty reports not matched to an aircraft · 118
They name N610AW, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. Newest first.
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 = 'N610AW' AND registry_match IS NULL 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 = 'N610AW' AND registry_match IS NULL 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 A6WA200560017Apu · bird ingestionSMOKE IN CABIN WHEN TURNING ON PACKS. MAINTNANCE C/W EO, BOTH AC PACKS. FOUND BIRD AND OIL IN APU INTAKE. REMOVED AND REPLACED APU, BOTH AC PACKS, JET PUMPS AND WATER INJECTOS IAW EO, SYSTEM OPS CHECK GOOD. (K)SDR A6WA20046002Ecu · malfunctionedWHEN FLAPS SELECTED FOR 24-33 DEGREES ON TO ASE, FLAP FAULTS AND INOPERATIVE LIGHTS ILLUMINATED FLAPS STUCK AT 24 DEGREES AIRCRAFT RETURNED TO DEN. MAINTENANCE FOUND CODE 4 ON FLAP ECU, RESET ECU, NO FAULTS. NOTED. (M)SDR A6WA200360058Wire · looseDURING SLIDE DEPLOYMENT FOR FUNCTION TEST LIGHTS CAME ON AND THEN OFF AFTER FULL DEPLOYMENT, INSPECTION FOUND WIRES PULLED OUT OF BATTERY CONNECTORS. MAINTENANCE REMOVED AND REPLACED EVACUATION SLIDE AND DISCREPANCY FORWARDED TO SLIDE SHOP. (M)SDR A6WA200360016Panel · chafedNR 4 PYLON PANEL 481 AT LOWER FORWARD RIGHT ATTACH HOLE CHAFED BADLY FROM LOOSE AND VIBRATING SCREW. HOLE WORN EXCESSIVELY. REPAIRED PANEL IAW BARA/AVR/6361/03-D. (M)SDR A6WA200360015Skin · crackedCRACKED IN HALF ABOVE PYLON NR 2 LEADING EDGE FIXED STRUCTURE. REMOVED AND REPLACED DOUBLER, P/N HC572H1080-001. 2 INCH CRACK TO NUTPLATE. PIECE INTACT, BUT CRACKED ALL THE WAY THROUGH. CAUSE OF DAMAGE, NORMAL FATIGUE. (M)SDR A6WA200360018Skin · damagedLEFT WING INBOARD LEADING EDGE HAS 1 HOLE ENLARGED IN TOP SKIN ABOVE NR 2 PYLON. REPAIRED IAW RIL HC572H9066 AND FAX BARA/AVR/6362/03-DC. (M)SDR A6WA200360017Panel · damagedLT WING LEADING EDGE PANEL 464AT HAS SEVERAL ELONGATED HOLES. REPAIRED IAW RIL HC5459009 AND FAX BARA/AVR/6365/03-DC.SDR 99ZZZX2702Bracket · crackedLEFT WING TE HYDRAULIC LINE CLAMP BRACKET CRACKED AT RIB 5. REPLACED BRACKET.SDR 99ZZZX2688Stiffener · crackedLEFT WING TOP SKIN STIFFENER AFT OF REAR SPAR BETWEEN RIBS 5 AND 6 IS CRACKED AT FORWARD END. REPAIRED IAW BAE RDO DJR/RJ0630-98. REF: W/C 5035 FOR ALODINE PRIME AND PAINT.SDR 99ZZZM560Bracket · crackedLEFT WING TE HYD LINE CLAMP BRACKET CRACKED AT RIB 5. REPLACED BRACKET. (M)SDR 99ZZZM480Screw · damagedRIGHT WING SHORT STALL BAR PULLING OVER CORNER MOUNT SCREWS. REPAIRED SCREWS AS REQ'D IAW AVRO FAX DJR/RJO638-98, GCB/RJ1344-94, JEN/RJ1331-94. OK FOR SERVICE IAW BAE 146 MM. (M)SDR 99ZZZX2689Stiffener · crackedLEFT WING TOP WING STIFFENER AFT OF REAR SPAR BETWEEN RIBS 8 AND 9 IS CRACKED AT FORWARD ENG. REPAIRED IAW BAE RDO EJR/RJ0630-98. REF: W/C 5035 FOR ALODINE, PRIME AND PAINT.SDR 99ZZZX2685Bearing · wornRIGHT WING INNER FLAP TAB NR 1 HINGE BEARING IS WORN. REMOVED AND REPLACED RIGHT NR 1 FLAP TAB HINGE BEARING.SDR 99ZZZX2675Angle · crackedLEFT WING T/E, LOWER SHROUD STIFFENER, AND AFT TAG ANGLE CRACKED BETWEEN RIBS 7 AND 8. REPLACED LEFT WING T/R LOWER SHROUD STIFFENER AND AFT TAG ANGLE BETWEEN RIBS 7 AND 8.SDR 99ZZZX2674Skin · dentedDENT LEFT FUSELAGE AT FRAME 47 BETWEEN STRINGERS 14 AND 16. REPAIRED DENT IAW BAE FAX REF DJR/RJ0620-98.SDR 99ZZZX2696Floor · brokenNR 9 RIGHT BIN FLOOR NEEDS OVERLAY. REPAIRED COMPOSITE STRUCTURE IAW DRAWING AW-25-20-9804-06 OF PS-1. ACFT TT: 19,327 HOURS. ACFT TC: 22,789.SDR 99ZZZX2695Floor · brokenNR 8 RIGHT BIN FLOOR SOFT. REPAIRED COMPOSITE STRUCTURE IAW DRAWING AW-25-30-9804-06 OF PS-1.SDR 99ZZZX2693Floor · brokenNR 9 LEFT BIN FLOOR NEEDS OVERLAY. REPAIRED COMPOSITE STRUCTURE IAW DRAWING AW-25-20-9804-06 OF PS-1.SDR 99ZZZX2692Floor · brokenNR 7 RT BIN FLOOR NEEDS OVERLAY. REPAIRED COMPOSITE STRUCTURE IAW DRAWING AW 25-20-9804-06 OF PS-1.SDR 99ZZZX2691Floor · brokenNR 6 RIGHT BIN FLOOR SOFT. REPAIRED COMPOSITE STRUCTURE IAW DRAWING AW-25-20-9084-06 OF PS-I.SDR 99ZZZX2690Floor · brokenNR 8 LEFT BIN FLOOR SOFT. REPAIRED COMPOSITE STRUCTURE IAW DRAWING AW-25-20-9804-96 (PART OF PS-1).SDR 99ZZZX2687Skin · dentedDENT AT BOXING JT RT FUSELAGE FORWARD OF REAR CARGO DOOR DUE REPAIR IN 3,000 CYCLES. CURRENT CYCLES: 29,794. REPAIR DUE BY 32,794 CYCLES. REPAIRED DENT IAW BAE FAX REF DJR/RJ0610-98. REF: W/C 1049 NDT.SDR 99ZZZX2684Floor · brokenNR 5 LEFT BIN FLOOR SOFT. REPAIRED COMPOSITE STRUCTURE IAW DRAWING AW-25-20-9804-06 OF PS-1.SDR 99ZZZX2673Floor · brokenNR 1 LEFT BIN FLOOR SOFT. REPAIRED COMPOSITE STRUCTURE IAW DRAWING AW-25-20-9804-6 OF PS-1.SDR 99ZZZX2672Floor · brokenNR 5 RIGHT BIN FLOOR NEEDS OVERLAY. REPAIRED COMPOSITE STRUCTURE IAW DRAWING AW-25-20-9804-6 OF PS-1.SDR 99ZZZX2671Floor · brokenNR 1 RT BIN FLOOR SOFT. REPAIRED COMPOSITE STRUCTURE IAW DRAWING AW-25-20-9804-06 OF PS-1.SDR 99ZZZX2670Floor · brokenNR 3 LEFT BIN FLOOR NEEDS OVERLAY. REPAIRED COMPOSITE STRUCTURE IAW DRAWING AW-25-20-9804-06 OF PS-1.SDR 99ZZZX2669Floor · brokenNR 7 LEFT BIN FLOOR SOFT. REPAIRED COMPOSITE STRUCTURE IAW DRAWING AW-25-20-9804-06 OF PS-1.SDR 99ZZZX2668Floor · brokenNR 6 LEFT BIN FLOOR SOFT. REPAIRED COMPOSITE IAW DRAWING AW-25-20-9084-06 OF PSI-1.SDR 99ZZZX2667Floor · brokenNR 2 LEFT BIN FLOOR NEEDS OVERLAY. REPAIRED COMPOSITE STRUCTURE IAW DRAWING AW-25-20-9804-06 OF PS-1.SDR 99ZZZX2666Floor · brokenNR 3 RIGHT BIN FLOOR SOFT. REPAIRED COMPOSITE STRUCTURE IAW AW-25-20-9804-06 OF PS-1.SDR 99ZZZX2665Floor · brokenNR 2 RIGHT BIN FLOOR SOFT. REPAIRED COMPOSITE STRUCTURE IAW DRAWING AW-25-20-9804-06 OF PS-1.SDR 99ZZZX2664Floor · brokenNR 4 RIGHT BIN FLOOR NEEDS OVERLAY. REPAIRED COMPOSITE STRUCTURE IAW DRAWING AW-25-20-9804.SDR 99ZZZM486Floor · brokenNR 4 LEFT BIN FLOOR NEEDS OVERLAY. REPAIRED COMPOSITE STRUCTURE IAW DRAWING AW-25-20-9804-06 OF PS-1, COMPLETED WEIGHT CHANGE NOTIFICATION FORM (ATTACHED) AND TRANSFERRED TESTING STEPS 1-4 FROM ABOVE DRAWING TO ANOTHER WORK CARD. (M)SDR 99ZZZX2686Stiffener · crackedRT WING T/E SHROUD TOP STIFFENER CRACKED AT FORWARD END BETWEEN RIBS 9 AND 10. REPAIRED PER BAE FAX JM/RJ0317/97 USING 2024T3 .040 INCH AND AW FAX HC/142-97 AND DJR/RJ0630-98.SDR 99ZZZM484Bracket · crackedRIGHT WING TE TOP HYDRAULIC LINE CLAMP BRACKET CRACKED RIB NR 6. REMOVED AND REPLACED BRACKET. (M)SDR 99ZZZM478Stiffener · crackedRIGHT WING TE SHROUD TOP STIFFENER CRACKED AT FORWARD END BETWEEN RIBS 5/6. REMOVED AND REPLACED RIGHT WING TE SHROUD TOP STIFFENER. (M)SDR 99ZZZM477Mount · crackedRIGHT LIFT SPOILER VALVE MOUNT PLATE CRACKED. REPLACED MOUNT PLATE. (M)SDR 99ZZZM476Rivet · looseRIGHT WING TE SHROUD TOP STIFFENER BETWEEN RIB 4/5 HAS LOOSE RIVET, AFT END. REMOVED AND REPLACED LOOSE RIVET. (M)SDR 99ZZZM475Bracket · crackedRIGHT WING TE LOWER HYDRAULIC LINE BRACKET CRACKED AT RIB NR 5. REMOVED BRACKET AND FABRICATED NEW BRACKET PER DRAWING HC9 32H0211. INSTALLED BRACKET AND ATTACHED LINES TO BRACKET. (M)SDR 99ZZZM481Bearing · wornRIGHT AILERON OUTBOARD HINGE 'A' FRAME BEARINGS WORN. REMOVED AND REPLACED RIGHT AILERON OUTBOARD 'A' FRAME. W/C GEN FOR FUNCTIONAL CHECK. (M)SDR 99ZZZM482Stiffener · crackedRIGHT WING TE SHROUD TOP STIFFENER CRACKED AT FORWARD END AND RIVET POPPED (AFT END) BETWEEN RIBS 3/4. REPLACED RIGHT WING TRAILING EDGE SHROUD TOP STIFFENER BETWEEN RIBS 3/4. (M)SDR 99ZZZM479Stiffener · crackedTE RIGHT WING TOP SHROUD STIFFENER OUTBOARD CRACKED AT FORWARD END BETWEEN RIB 8/9. REPLACED RIGHT WING TRAILING EDGE SHROUD TO STIFFENER BETWEEN RIBS 8/9. (M)SDR 99ZZZX2694Skin · dentedREPAIR DENT ON LEFT SIDE OF FUSELAGE AT FRAME 9, 3.25 INCHES BELOW SKIN LAP B AND 4.00 INCHES FORWARD OF FRAME 9 IN 3,000 CYCLES. CURRENT TCA 29,540 DUE AT 32,540 TAC.SDR 99ZZZX2683Sub Frame · crackedSUB-FRAME AFT OF FRAME 50 CRACKED AT LOWER LT CORNER. REPAIRED SUB-FRAME AFT OF FRAME 50 AT LOWER LT CORNER IAW BAE FAX DJR/RJ0602-98.SDR 99ZZZX2676Rivet · looseNUMEROUS LOOSE RIVETS AT LT WING T/E LOWER SKIN, AFT OF REAR SPAR. REMOVED AND REPLACED NUMEROUS LOOSE RIVETS ON LT WING T/E LOWER SKIN AFT OF REAR SPAR.SDR 99ZZZM485Skin · dentedCOMPLIED WITH REPAIR OF 2 DENTS AT FRAME 20, STRINGER 20, PORT SIDE IAW SRM 53-00-12 FIG 202 WITHIN 3000 CYCLES, CURRENT CYCLES 29320, DUE BY 32320 CYCLES. REPAIRED DENTS IAW BAE FAX REF DJR/RJO595-98. (M)SDR 99ZZZX2682Longeron · crackedATTACHMENT ANGLE/GUSSET AT THE AFT END OF THE UPPER MOST LEFT AIRBRAKE HINGE LONGERON IS CRACKED. FABRICATED LEFT GUSSET PLATE PER BAE DRAWING HC539H0229. REPLACED LEFT GUSSET PLATE AT UPPER MOST LEFT AIRBRAKE HINGE LONGERON.SDR 99ZZZM483Stiffener · crackedLEFT WING TOP SKIN STIFFENER AFT OF REAR SPAR BETWEEN RIBS 7/8 IS CRACKED AT FORWARD END. REMOVED AND REPLACED TOP SKIN STIFFENER AFT OF REAR SPAR BETWEEN RIBS 7/8. (M)SDR 99ZZZX2679Frame · chafedNR 1 ENGINE FORWARD LEFT COWL DOOR LOWER AFT FRAME CHAFED NEAR LATCH. REPAIRED NR 1 ENGINE LEFT FORWARD COWL DOOR LOWER AFT FRAME IAW SRM 54-10-11.
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