N455WN
Service difficulty reports · 354
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 = 'N455WN' 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 = 'N455WN' 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 SWAA2021122747996None · corrodedWEB TENSION STRAP BS 1016+2 +12, RBL 18 CORRODED. FOUND TO BE OUT OF LIMIT DUE TO NO LIMITS ON SRM. REMOVED THE WEB TENSION STRAP IAW SRM 51-40-02-0G-0. FABRICATED, LOCATED, AND DRILLED A NEW WEB TENSION STRAP IAW DWG 147A5744, AND SRM 51-40-02. APPLIED SDR SWAA2021122747988Channel · corrodedCORROSION PASSENGER CABIN AED MOPSIL BS947.5-BS986.5+9 LBL51 WL208.1 ; / [01] VERIFY APPLICABILITY ON SRM 53-70-15-0I-1 FOR IDENTIFICATION AND SRM 53-70-15-1A-1 FOR ALLOWABLE DAMAGE; [02] REMOVED CORROSION ON PASSENGER CABIN AED MOPSIL BS947.5-BS986.5-9'' LBL5SDR SWAA2021122747987None · corrodedCORROSION PASSENGER CABIN ASD MOPSIL BS927+3-BS986.5+10 RBL51 WL208.1 ; / [01] REMOVED CORROSION FROM AFT SERVICE DOOR MOPSIL IN AREA OF 1'X1' ORIGINAL MATERIAL THICKNESS 0.080' REMAINING MATERIAL THICKNESS 0.055' FOUND TO BE OUT OF LIMIT IAW SRM 53-70-15-1A-1SDR SWAA2021122747992Floorbeam · corrodedCORROSION PASSENGER CABIN FLOOR BEAM BS986.5 RBL28;32;40;44 WL208.1 ; / [01] REMOVED CORROSION FROM PASSENGER CABIN FLOOR BEAM BS 986.5 RBL 44 WL 208.1 IN AREA OF 2'X 1' X 0.038' DEEP ORIGINAL MATERIAL THICKNESS 0.150' FOUND TO BE OUT OF LIMIT IAW SRM 53-70-51SDR SWAA2021122747990Web · corrodedCORROSION PASSENGER CABIN WEB BS1006+6; +9 RBL39 WL208.1 ; / [01] CORROSION FOUND AT PASSENGER CABIN AFT WEB BS 1006+6 TO BS 1006+9; RBL 39; WL 208.1 FOUND TO BE OUT OF LIMIT DUE TO NO LIMIT ON SRM PARTS WILL BE REPAIRED BY REPLACEMENT IAW SRM 51-10-02-0G-0 PASDR SWAA2021122747989Web · corrodedCORROSION PASSENGER CABIN WEB BS986.5-BS986.5+4 RBL40; BS986.5+8 RBL38 WL208.1 ; / [01] CORROSION FOUND AT PASSENGER CABIN AFT WEB BS 986.5 TO BS 986.5+4; RBL 40; WL 208.1 FOUND TO BE OUT OF LIMIT DUE TO NO LIMIT ON SRM PARTS WILL BE REPAIRED BY REPLACEMENT IASDR SWAA2021122747997None · corrodedWEB TENSION STRAP BS 1016, RBL 3, WL 208.1 CORRODED. FOUND TO BE OUT OF LIMIT DUE TO NO LIMITS ON SRM. REMOVED THE WEB TENSION STRAP IAW SRM 51-40-02-0G-0, LOCATED, AND DRILLED A NEW WEB TENSION STRAP IAW SRM 51-40-05-0G-0, AND DWG 147A5730. INSTALLED TSDR SWAA2021122747995Web · corrodedCORROSION PASSENGER CABIN 1016 WEB BS1016+4 LBL4 WL208.1 ; DAMAGE FOND ON PASSENGER CABIN 1016WEB BS 1016+4'' RBL4 WL208.1 / [01] CORROSION FOUND ON PASSENGER CABIN 1016WEB BS 1016+4'' LBL4 WL208.1 FOUND TO BE OUT OF LIMIT DUE TO NO LIMITS ON SRM PART WILL BE SDR SWAA2021122747511Seat Track · corrodedCORROSION ON PASSENGER CABIN SEAT TRACK RBL25 WL208.1 BS663+12; BS706; BS727; BS727+14; BS727A+5-BS727B ; / [01] ACCOMPLISHED STEPS 1-5; [02] UPDATED TABLE; [03] VERIFIED PARTIALS FOR STEPS 1-5; [04] STEP 6 COMPLETE.; [05] COMPLETED STEPS 1-6SDR SWAA2021112947386Seat Track · corrodedCORROSION ON PASSENGER CABIN SEAT TRACK AT B.S. 663+17-685+7 AND 727+5; R.B.L. 45.5. / COMPLETED ALL STEPS VERIFIED CORROSION REMOVAL IN STEPS 1 AND 2 FOUND TO BE IN LIMITS PER SRM 53-00-52-1A-1; OK TO TREAT AND PRIME APPLIED A CHEMICAL CONVERSION COATING AND SDR SWAA2021112947391Seat Track · corrodedCORROSION ON PASSENGER CABIN SEAT TRACK AT B.S. 380+5; R.B.L. 45.5. REMOVED CORROSION ON CABIN SEAT TRACK AT BS380+1 - BS380+13 RBL45.5 L=12' W=0.8' MAX. MATERIAL LOSS=0.015' WAS FOUND WITHIN LIMIT IAW SRM 53-00-52-1A-1 ITEM 4.A(2)A FIG. 103 DETAIL A. VERIFISDR SWAA2021122747221Bracket · crackedFWD FLASHLIGHT BRACKET IS CRACKED MULTIPLE AREAS. ; / [01] REMOVED AND REPLACED FWD FLASHLIGHT BRACKET IAW CMM 25-60-02 STEP INSTALLATION.; [02] VERIFIED REPLACEMENT OF FWD FLASHLIGHT BRACKET PER CMM 25-60-02SDR SWAA2021122746820Skin · crackedCORROSION ON CROWN SKIN UNDER VERTICAL STABILIZER STA 1012 TO STA 1044; RBL 8 TO RBL 13. ; / [01] REMOVED CORROSION ON CROWN SKIN UNDER VERTICAL STABILIZER STA 1016 TO 1040 RBL 8 TO RBL 13 REWORKED AREAS A= L: 15.6' W: 1.2' B= L: 9.7' W: 2.2' C= L: 4' W: 3.8' SDR SWAA2021122746805Panel · pulledR/W L/E PANEL 621LB HAS SEVERAL PULLED FASTENER HOLES. DAMAGE AT SEVERAL FASTENER HOLES EXCEED ALLOWABLE DAMAGE LIMITS IAW SRM 57-41-01-1A-1 PARAGRAPH 4.A(5). DAMAGE IS PER SRM 51-70-05-2R-6 AS DIRECTED BY SRM 57-41-01-2R-1. REMOVED 2 EACH BACKPLATES TO FACSDR SWAA2021122446168Vapor Barrier · crackedL/H B/S 663 MAIN WHEEL WELL VAPOR BARRIER BULKHEAD PRESSURE DECK WEB IS CRACKED AT LBL 36. (MARKED) ; / [01] REMOVED L/H B/S 663 MAIN WHEEL WELL VAPOR BARRIER BULKHEAD PRESSURE DECK WEB BTW LBL 6.13 TO LBL 72 IAW SRM 51-40-02; [14] INSTALLED NEW LH BS 663 MAINSDR SWAA2021122746151Support Bracket · crackedFWD ENTRY DOOR FWD LOWER LINING SUPPORT BRACKET IS CRACKED ; / [01] INSTALLED NEW FED FWD LOWER LINING SUPPORT BRACKET IAW AMM 25-21-31-420-802 STEP 3. B. (3); [02] VERIFIED COMPLETESDR SWAA2021061582441Retainer · crackedLEFT WING REAR SPAR BEHIND THE #1 ENGINE STRUT TE SHELF VERTICAL SEAL RETAINER IS CRACKED ; / R&R'D LEFT WING REAR SPAR BEHIND THE #1 ENGINE STRUT TE SHELF VERTICAL SEAL RETAINER PER SRM 51-10-02.SDR SWAA2021060299390Bulkhead Web · crackedTRANSFERRED FROM NRC D434429; LEFT ECS BAY AFT BULKHEAD (VAPOR WEB) CRACKED ABOVE BULKHEAD HYDRAULIC FITTINGS. PREVIOUS/EXISTING CRACK REPAIR LOCATED BELOW HYDRAULIC FITTINGS / FOUND NEW CRACK TO BE 6 1/2' LONG. ACCOMPLISHED INTERM REPAIR PER SRM 57-10-10-2R-2SDR SWAA2020020641103Light · brokenAFT GALLEY EXIT SIGN OVER R2 DOOR BROKEN. / R&R LIGHT ASSEMBLY PER MM.SDR SWAA2020010840242Fitting · looseR1 DOOR GIRT BAR CLIP UNSECURE. / SECURED GIRT BAR CLIP PER SIP.SDR SWAA2022022452361Flap · delaminatedL/H O/B AFT FLAP I/B CORNER T/E SEPARATED / REPAIRED FLAP IB T/E PER SRM 51-70-10-2R-1.SDR SWAA2022032452360Track · crackedL/H UPPER AFT HORIZONTAL STABILIZER WARP AROUND PANEL SHARK FIN SEAL RECEIVER TRACK CRACKED UPPER FWD SIDE. / REMOVED AND REPLACED L/H UPPER AFT HORIZONTAL STABILIZER WARP AROUND PANEL SHARK FIN SEAL RECEIVER TRACK PER SOPM 20-50-01SDR SWAA2022032452359Panel · corrodedPANEL 192F HAS CORROSION UNDER ALL 3 ANTENNAS. / REMOVED AND REPLACED PANEL 192F P/N 149A7755-1 PER AMM.53-51-21 MARKER BEACON ANTENNA AND DME ANTENNAS WERE REPLACED ON N/R G697619SDR SWAA2019112539078Escape Rope · looseR/H OVERWING EXIT HATCH ESCAPE ROPE NOT STOWED CORRECTLY AND ROPE RESTRAINT STRAP LOOSE. / SECURED ROPE AND RESTRAINT STRAP IAW AMM.SDR SWAA2022040552275Panel · delaminatedTAIL CONE HAS AREA OF DELAMINATION ON R/H SIDE AT LOWER FWD. CORNER OF CUT OUT FOR ACCESS PANEL / REPAIRED PER SRM 51-70-04-2R-2. SEE SUBTASKS FOR INDIVIDUAL SIGNOFFS.SDR SWAA2019112539079Rib · crackedR/H HORIZONTAL STABILIZER STA. 120.30 RIB CRACKED AT LOWER INBOARD AFT ATTACH FASTENER AT REAR SPAR. / REPAIRED RIB IAW EA AND SRM.SDR SWAA2022041952269Support · crackedAFT E/E E2-2 RACK MID OBD SUPPORT CRACKED. / REMOVED P91 PANEL PER AMM 24-21-21. REMOVED AND INSTALLED NEW SUPPORT BRACKET (143A9173U35) IAW SRM 51-40-02. REINSTALLED ORIGINAL P91 PANEL PER AMM 24-21-21. OPS CHECKS COMPLETED ON SUBTASKS STEPS 4-10. SEE BELOW SSDR SWAA2019112539080Skin · delaminatedL/H WING OUTBOARD AFT FLAP UPPER SURFACE INBOARD CORNER DELAMINATED. / R&R AFT FLAP IAW SRM AND AMM.SDR SWAA2019112539076Skin · crackedR/H WING #5 SLAT LOWER SURFACE OF THE LEADING EDGE NOSE SKIN CRACKED IN THE COUNTERSINK AT THE ACTUATOR FITTING INBOARD MIDDLE 2 HOLES. / INSTALLED #5 SLAT ASSEMBLY PER SRM AND AMM.SDR SWAA2022040552247Splice · corrodedAFT CARGO FLOOR PANEL SPLICE STRIP HAS SURFACE CORROSION AT STA 887. / REMOVED & REPLACED AFT CARGO FLOOR PANEL SPLICE STRIP @ STA 887 AS PER SRM 51-40-02.SDR SWAA2019111138762Attach Angle · corrodedAFT CARGO AFT BULKHEAD LOWER ATTACH ANGLE AT BS. 947 CORRODED ON VERTICAL SURFACE, RBL 17. / R&R ANGLE PER SRM.SDR SWAA2022040652202Support Fitting · crackedAFT CARGO STA 947 LBL 10 BULKHEAD SUPPORT FITTING CRACKED / REMOVED AND INSTALLED REPLACEMENT BULKHEAD FITTING AT STA. 947 LBL 10 PER SRM 51-40-02SDR SWAA2022040652195Strap · corrodedAFT CARGO FLOOR STRAP AT STA. 777 HAS SURFACE CORROSION / REMOVED AND REPLACED AFT CARGO FLOOR STRAP PART #146A9401-4 ; PER SRM. 51-10-02SDR SWAA2022040552194Bracket · crackedAFT CARGO STA 727 FWD BULKHEAD PANEL SUPPORT BRACKET CRACKED 10' ABOVE FLOOR RBL 4' / REMOVED AND REPLACED AFT CARGO BULKHEAD PANEL SUPPORT BRACKET (P/N 144A9401-21) AT STA.727; RBL 4' IAW SRM 51-40-02.SDR SWAA2022040652193Angle · corrodedAFT CARGO L/H TRANSITION ANGLE HAS SEVERAL AREAS OF CORROSION ON AND AROUND SCREW HOLES FROM STA. 727-847 / REMOVED & REPLACED AFT CARGO L/H TRANSITION ANGLE FROM STA. 727-847 AS PER SRM 51-40-02.SDR SWAA2022040652192Angle · corrodedAFT CARGO R/H TRANSITION ANGLE HAS SEVERAL AREAS OF CORROSION ON AND AROUND SCREW HOLES FROM STA. 727-787 / TRANSITION ANGLE REMOVED AND REPLACED PER SRM 51-40-02.SDR SWAA2022040152068Scuff Plate · crackedAFT CARGO AFT CORNER SCUFF PLATE CRACKED ON LOWER SIDE. / REMOVED AND REPLACED AFT CARGO AFT SCUFF PLATE PER AMM 53-11-02 .SDR SWAA2019082036026Trunnion · corrodedL/H GEAR FORWARD TRUNNION FITTING INBOARD LUG, UPPER OUTBOARD FACE CORRODED. / REPAIRED LUG PER EA.SDR SWAA2019081936027Trunnion · corrodedL/H GEAR FORWARD TRUNNION FITTING INBOARD LUG, LOWER OUTBOARD FACE CORRODED. REPAIRED LUG PER EA.SDR SWAA2022031552051Bracket · crackedRIGHT WING TO BODY FAIRING PNL 191AR AFT SIDE VERTICAL SUPPORT BRACKET AT LEADING EDGE SKIN CRACKED. / REMOVED AND REPLACED RIGHT WING TO BODY VERTICAL SUPPORT BRACKET AT LEADING EDGE SKIN PER SRM 51-40-02.SDR SWAA2019073035407Sign · brokenCEILING EMERGENCY EXIT SIGN OVERWING CENTER AISLE BROKEN. R&R SIGN ASSEMBLY IAW AMM.SDR SWAA2019051732798Sensor · faultyAIR TURNBACK, ON DEPARTURE RECEIVED A LEADING EDGE FLAP TRANSIT LIGHT AND #2 LEADING EDGE FLAP INDICATOR LIGHT. R&R SENSOR IAW AMM.SDR SWAA2022030351775Stiffener · crackedL/H WHEEL WELL 1 EACH L SHIFFENER AT 663 LRL HAS A 1 INCH CRACK / REMOVED & REPLACED CRACK SHIFFENER WITH NEW ONE PER SRM 51-40-02SDR SWAA2019021129482Girt Bar · unsecureR1 DOOR SLIDE GIRT BAR CAME OFF. SECURED GIRT BAR IAW MM.SDR SWAA2019010727833Vapor Barrier · crackedCENTER WING SECTION VAPOR BARRIER CRACKED OUTBOARD OF 'A' HYD RETURN FILTER HOUSING. REPAIRED BARRIER PER SRM.SDR SWAA2019010327837Battery · failedEMERGENCY LIGHT BATTERY M1675 FAILED CAPACITY TEST. R&R BATTERY PER MM.SDR SWAA2019010228148Battery · failedEMERGENCY EXIT LIGHT BATTERY PACK M1672 FAILED TEST. R&R BATTERY PER MM.SDR SWAA2019010227834Battery · failedEMERGENCY EXIT LIGHT BATTERY PACK M1673 FAILED TEST. R&R BATTERY PER MM.SDR SWAA2019010327831Light · inoperativeRT OVERWING EXTERIOR EXIT LIGHT INOP. RELAMPED PER MM.SDR SWAA2018082924670Cover · missingR1 DOOR EMERGENCY EXIT LIGHT LOWER LENS COVER MISSING DIRECTIONAL ARROW. R&R COVER PER AMM.
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