N640RW
Service difficulty reports · 132
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. 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 = 'N640RW' AND registry_match = 'registration' 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 = 'N640RW' AND registry_match = 'registration' 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 R61A2026090400248Skin · corrodedAFT CARGO SKIN BETWEEN FR 83 AND FR 84 BETWEEN STR 26R AND 27R CORRODED.SDR R61A2026090400246Skin · crackedLH WING INTERNAL PLANK RIB 17 STRG 19 TERMINUS HAS CRACK FROM INTERNAL SIDE AS SEEN THROUGH PANEL 531DBSDR R61A20260829485Skin · crackedFOUND IN HEAVY CHECK-CRACK DAMAGE AFFECTING THE LH WING MAIN BOX LOWER SKIN, LOCATED IN THE END POINT OF STGR 19, BETWEEN RIBS 16-17.SDR R61A2026062300169Bleed Air Sys · failedBLEED 1 AND BLEED 2 FAIL MSG IN THE AIR. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. COMPLIED WITH PNEUMATIC BLEED SYSTEM TEST FOR BOTH ENGINES, OPS CHECKED GOOD.SDR R61A2024030500099Slide · partial deployR2 DOOR SLIDE DEPLOYED WITHOUT WARNING. R&R R2 DOOR SLIDE AND FLEXBALL CABLESDR R61A2023121500734Doubler · unknownEXTERNAL SIDE REPAIR DOUBLER FR 23-24 STRG 16L-17L HAS 2 GOUGED. PERFORMED EXTERNAL DOUBLER REPAIR ON CF I SKIN AT FR 23-24 STGR 16L-17L. REF EMB SRM 53-21-01 /REPAIR 10P.SDR R61A2023121500733Stringer · corrodedCORROSION ON STRINGER 23R, AT 2 EACH RIVETS, BETWEEN FRAMES 16 AND 17. REMOVED AND REPLACED STRINGER 23R FR 12-20. REF EMB SRM 51-40-08.SDR R61A2023121500730Support Angle · corrodedFUSELAGE FR16 HAS CORRODED ANGLE SUPPORT AT STR 27L-26L. REMOVED AND REPLACED SHEAR CLIP AT FUSELAGE FR16 STR 27L-26L. REF EMB SRM 51--
40-08.SDR R61A2023121500729Shear Tie · corrodedFUSELAGE FR16 HAS CORRODED ANGLE SUPPORT AT STR 28L-27L. REMOVED AND REPLACED SHEAR CLIP AT FUSELAGE FR16 STR 28L-27L. REF EMB SRM 51-
40-08.SDR R61A2023121500728Support Angle · corrodedFUSELAGE FR16 HAS CORRODED ANGLE SUPPORT AT STR 27R-26R. REMOVED AND REPLACED SHEAR CLIP AT FUSELAGE FR16 STR 27R-26R. REF EMB SRM 51--
40-08.SDR R61A2023121500727Support Angle · corrodedFUSELAGE FR16 HAS CORRODED ANGLE SUPPORT AT STR 26R-25R. REMOVED AND REPLACED SHEAR CLIP AT FUSELAGE FR16 STR 26R-25R. REF EMB SRM 51-40-08.SDR R61A2023121500726Support Angle · corrodedFUSELAGE FR16 HAS CORRODED ANGLE SUPPORT AT STR 23R-22R. REMOVED AND REPLACED FWD FUSELAGE ANGLE SUPPORT AT FR16 BETWEEN STGR 23R-22R REFER
SRM 51-40-08.SDR R61A2023121500725Support Angle · corrodedFUSELAGE FR17 HAS CORRODED ANGLE SUPPORT AT STR 23R-22R. REMOVED AND REPLACED ANGLE SUPPORT AT FUSELAGE FR17 STR 23R-22R. REF EMB SRM
51-40-08.SDR R61A2023121500724Shear Tie · corrodedFUSELAGE FR17 HAS CORRODED SHEAR CLIP STR 23R-22R. REMOVED AND REPLACED SHEAR CLIP AT FUSELAGE FR17 STGR 23R-22R REF SRM EMB 51-40-08.SDR R61A2023121500723Shear Tie · corrodedFUSELAGE FR17 HAS CORRODED SHEAR CLIP STR 25R-24R. REMOVED AND REPLACED SHEAR CLIP AT FUSELAGEFR17 STR 25R-24R. REF EMB SRM 51-40-08.SDR R61A2023121500722Shear Tie · corrodedFUSELAGE FR17 HAS CORRODED SHEAR CLIP STR 26R-25R. REMOVED AND REPLACED SHEAR CLIP AT FUSELAGE FR17 STR 26R-25R. REF EMB SRM 51-40-08.SDR R61A2023121500721Shear Tie · corrodedFUSELAGE FR17 HAS CORRODED SHEAR CLIP STR 27R-26R. REMOVED AND REPLACED SHEAR CLIP AT FUSELAGE FR17 STR 27R-26R. REF EMB SRM 51-40-08.SDR R61A2023121500720Shear Tie · corrodedFUSELAGE FR17 HAS CORRODED SHEAR CLIP STR 26L-25L. REMOVED AND REPLACED SHEAR CLIP AT FUSELAGE FR17 STR 26L-25L. REF EMB SRM 51-40-08.SDR R61A2023121500719Shear Tie · corrodedFUSELAGE FR17 HAS CORRODED SHEAR CLIP STR 27L-26L. REMOVED AND REPLACED SHEAR CLIP AT FUSELAGE FR17 STR 27L-26L, REF EMB SRM 51-40-08.SDR R61A2023121500718Shear Tie · corrodedFUSELAGE FR17 HAS CORRODED SHEAR CLIP STR 28L-27L. REMOVED AND REPLACED SHEAR CLIP AT FUSELAGE FR17 STR 28L-27L. REF EMB SRM 51-40-08.SDR R61A2023121500717Shear Tie · corrodedFUSELAGE FR17 HAS CORRODED SHEAR CLIP STR 28L-28R. REMOVED FASTENERS AND FOUND NOT TO BE CORRODED. EMB 51-20-08.SDR R61A2023121500732Fastener · corrodedPER ETD 2020-170-024582 REV.A; STEP B. PERMANENT REPAIR, 2. PREMANENT REPAIR PROCEDURE,8 EACH FASTENERS REQUIRE REPLACEMENT. REMOVED AND REPLACED 8EA FASTENERS ON RH WING MAIN BOX UPPER SKIN AT RIB 10A PER ETD2020-170-024582 REV A.SDR R61A2023121500731Angle · crackedCRACK IN "L" ANGLE L/H FR. 52.REMOVED AND REPLACED LH FR 52 L-ANGLE REF SRM 51-40-08SDR R61A2022071500439Power Unit · inoperativeEMERGENCY LIGHT BATTERY FAULT WHEN DISARMING EMERGENCY LIGHTS. R&R EMERGENCY LIGHT POWER UNIT AFT GALLEY UPPER.SDR R61A2022061700397Bleed Air Sys · false indicationBLEED 2 FAIL, PERFORMED QRH PROCEDURE, MESSAGE EXTINGUISHED. BLEED 2 FAIL CAME ON AGAIN, CABIN ALTITUDE CONTINUED CLIMBING EVEN THOUGH WE WERE AT LEVEL FLIGHT. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. INSPECTED LEFT AND RIGHT PACK OUTLET DUCTS, NO DEFECTS SDR R61A2020090411615Shear Tie · corrodedDURING HEAVY CHECK MAINTENANCE FOUND LEVEL 2 CORROSION FOUND ON SHEAR CLIP AT FR17 BETWEEN STR 27-28 RT. SHEAR CLIP WAS REMOVED AND REPLACED IAW SRM 51-41-01.SDR R61A2020090411614Seat Track · corrodedDURING HEAVY CHECK MAINTENANCE FOUND LEVEL 2 CORROSION FOUND ON CENTER FUSELAGE 3 SEAT TRACK BEAM. BEAM WAS REMOVED AND REPLACED IAW SRM 51-41-01.SDR R61A2020090416617Shear Tie · corrodedWHILE AIRCRAFT WAS OUT OF SERVICE FOR HEAVY CHECK LEVEL 2 CORROSION WAS FOUND IN AFT CARG SHEAR CLIP AT FR82 BETWEEN STR 27-28 RT. SHEAR CLIP WAS REMOVED AND REPLACED IAW SRM 51-41-01.SDR R61A2020009041662Shear Web · corrodedWHILE AIRCRAFT WAS OUT OF SERVICE, LEVEL 2 CORROSION WAS FOUND AT AFT CARGO SHEAR CLIP AT FR86 BETWEEN STR 29L-29R. SHEAR CLIP WAS REMOVED AND REPLACED IAW ETD 2020-170-025195 REV 1.SDR R61A2020090415623Doubler · corrodedWHILE AIRCRAFT WAS OUT OF SERVICE FOR HEAVY CHECK, LEVEL 2 CORROSION WAS FOUND ON FWD FUSELAGE, FLOOR SUPPORT DOUBLER UPPER SURFACE AT FR13, RT SIDE. FWD FUSELAGE FLOOR SUPPORT DOUBLER AT FR13, RT SIDE REPLACED IAW E170 SRM 51-41-02 AND 51-43-02.SDR R61A2020090415621Seat Track · corrodedWHILE AIRCRAFT WAS OUT OF SERVICE FOR HEAVY CHECK, LEVEL 2 CORROSION WAS FOUND ON FWD FUSELAGE FLOOR STRUCTURE INBOARD LT SEAT TRACK BEAM AT FR 17. SEAT BEAM WAS REMOVED AND REPLACED IAW SRM 51-41-02.SDR R61A2020090411611Rib · crackedDURING HEAVY CHECK MAINTENANCE FOUND VERTICAL STABILIZER TRAILING EDGE RIB 10 CRACKED. REPAIRED VERTICAL STAB TRAILING EDGE RIB 9/10 IAW ETD2020-170-05653.SDR R61A2020090415620Seat Track · corrodedWHILE AIRCRAFT WAS OUT OF SERVICE FOR HEAVY CHECK, LEVEL 2 CORROSION WAS FOUND ON FWD FUSELAGE FLOOR STRUCTURE RT INBOARD SEAT TRACK BEAM AT FR17. SEAT TRACK BEAM WAS REMOVED AND REPLACED IAW SRM 51-43-03.SDR R61A2020090415819Doubler · corrodedWHILE AIRCRAFT WAS OUT OF SERVICE FOR HEAVY CHECK, LEVEL 2 CORROSION WAS FOUND ON FORWARD FUSELAGE FLOOR SUPPORT DOUBLER PLATE SURFACE AT FR19 LT SIDE. DOUBLER PLATE WAS REMOVED AND REPLACED IAW 51-41-02.SDR R61A2020090415818Support Fitting · corrodedWHILE AIRCRAFT WAS OUT OF SERVICE FOR HEAVY CHECK LEVEL 2 CORROSION WAS FOUND ON FWD FUSELAGE FLOOR STRUCTURE LAV FITTING AT FR 16 RT. FITTING WAS REMOVED AND REPLACED IAW SRM 51-43-03.SDR R61A2020090411613Rib · crackedDURING HEAVY CHECK MAINTENANCE FOUND RT HORIZ STAB RIB 11A CRACKED. RT HORIZ STAB RIB 11A REPLACED, IAW REPUBLIC EO 170-EO-55-10-0004. REF AAR NRWC 4500769-3000-0082.SDR R61A2020090430607Stiffener · crackedDURING HEAVY CHECK MAINTENANCE FOUND CRACK ON FWD EBAY AVIONICS RACK, FWD LT VERTICAL STIFFENER. REPAIRED IAW JC 170-EO-53-12-0000.SDR R61A2020090411612Rib · crackedDURING HEAVY CHECK MAINTENANCE FOUND LT HORIZ STAB RIBS 10A, 11A AND 12A CRACKED. HORIZ STAB RIBS 10A, 11A AND 12A REPLACED IAW REPUBLIC EO 170EO-55-10-0004. REF AAR NRWC 4500769-3000-0082.SDR R61A2020090411610Bracket · corrodedDURING HEAVY CHECK MAINTENANCE FOUND FWD LAV, AFT LT ATTACHMENT BRACKET CORRODED. FWD LAV, AFT LT ATTACHMENT BRACKET REPLACED IAW CMM 25-41-05.SDR R61A2020090411609Shield · burnedDURING HEAVY CHECK MAINTENANCE FOUND AFT GALLEY SMOKE SHIELD HAS DAMAGE, BURNED, DISCOLORED NEAR COMPARTMENT LIGHT. AFT GALLEY SMOKE SHIELD REPLACED.SDR R61A2020090300606Skin · crackedDURING HEAVY CHECK MAINTENANCE FOUND RT WING UPPER SKIN T/E CRACK FOUND NEAR RIB 10A AND SPOILER 3 HINGE WITH 2 RIVETS MISSING. RT WING UPPER SKIN T/E NEAR RIB 10A REPAIRED IAW ETD 2020-170-024582.SDR R61A201905240554Rod · not reportedFLAP FAIL MESSAGE DURING TAKEOFF. SETTING 1 TO 2. C/W FLAP/SLAT OVERSPEED INSPECTION. R&R LTIB AFT FLAP RODS IAW AMM 57-54-30.SDR R61A2018091320956Web · corrodedDURING HEAVY CHECK MAINTENANCE TECHNICIANS FOUND CABIN WEB CORRODED AFT OF FRAME 13, RBL 36". FOUND TO BE OUT OF LIMITS IAW SRM 53-10-10. REMOVED AND REPLACED WEB IAW SRM 51-40-08. A/C REMAINS IN HEAVY CHECK.SDR R61A2018091320958Floor Support · corrodedDURING HEAVY MAINTENANCE TECHNICIANS FOUND CABIN FLOOR SUPPORT STRUCTURE CORRODED AT FRAME 90, RBL 26 FASTENER HOLE. FOUND OUT OF LIMITS IAW SRM 51-40-08. REMOVED AND REPLACED SUPPORT IAW SRM 51-40-08 AND DRAWING 170-65660-431.SDR R61A2018092200975Support Plate · corrodedWHILE IN HEAVY CHECK MAINTENANCE FOUND CABIN FLOOR STRUCTURE FR90 WITH CORROSION AROUND FASTENER HOLE RBL 26. MAINTENANCE REMOVED CORROSION AND FOUND THE REMAINING THICKNESS TO BE OUT OF LIMITS IAW SRM 51-75-16. REMOVED AND REPLACED FLOOR STRUCTURE PLATE PN-17SDR R61A2018091320957Panel Support · corrodedDURING HEAVY MAINTENANCE TECHNICIANS FOUND CABIN FLOOR STRUCTURE FRAME 89 WITH CORROSION AROUND A FASTENER HOLE RBL 38". FOUND TO BE OUT OF LIMITS IAW SRM 51-75-16. REMOVED AND REPLACED PANEL SUPPORT IAW SRM 51-40-08, 51-75-16 AND 53-23-10. A/C REMAINS IN HEAVSDR R61A2018091320955Floorbeam · corrodedWHILE PERFORMING HEAVY MAINTENANCE TECHNICIANS FOUND CABIN FLOOR STRUCTURE AT FR 87-88 WEB WITH CORROSION AROUND FASTENER HOLES RBL 24-38". FOUND TO BE OUT OF LIMITS PER SRM 53-23-10. REMOVED AND REPLACED WEB IAW SRM 51-40-08 AND ETD 2011-190/01333 REV C. A/C SDR R61A201701160049Step · out of adjustCREW RECEIVED AN L1 DOOR OPEN INDICATION. AN EMERGENCY WAS NOT DECLARED AND LANDED WITHOUT INCIDENT. MAINTENANCE ADJUSTED L1 EXTERIOR STEP GAP IAW AMM AND OPS CHECKED GOOD.SDR R61A201701140045Proximity Sensor · malfunctionedCREW RECEIVED A FORWARD PASSENGER DOOR OPEN MESSAGE. AN EMERGENCY WAS NOT DECLARED AND CREW LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED FORWARD PASSENGER DOOR VENT FLAP PROXIMITY SENSOR IAW AMM AND OPS CHECKED GOOD.SDR R61A201701140044Proximity Sensor · out of adjustMAINTENANCE RECEIVED AN L1 DOOR OPEN MESSAGE. MAINTENANCE ADJUSTED FORWARD DOOR CLOSED PROXIMITY SENSOR IAW AMM AND OPS CHECKED GOOD.
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