N417WN, cancelled Sep 29, 2025
Service difficulty reports · 318
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 = 'N417WN' AND deregistration_id = 'N417WN-2025-09-29' 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 = 'N417WN' AND deregistration_id = 'N417WN-2025-09-29' 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 SWAA2025050566699Inlet · pulled#2 ENGINE INLET HAS 17 FASTENERS PULLED THRU ON OUTBOARD SIDE 3OCLOCK POSITION.<[01] REMOVED #2 ENGINE INLET REF AMM 71-11-01;[02] 01 - REMOVED AND REPLACED PER [AMM 71-11-01-401-NG (INLET COWL - REMOVAL/INSTALLATION - PERMANENT)]SDR SWAA2025041524243Skin · debondedLEFT OUTBOARD TRAILING EDGE FLAP UPPER SKIN HAS MISSING AND DISBONDED/DEFORMED MATERIAL ON THE INBD EDGE AND 10IN FROM THE TRAILING EDGE<[01] REMOVED LH OTBD TRAILING EDGE FLAP PER M/M 27-51-22;[02] INSTALLED LH OB TRAILING EDGE FLAP REF MM 27-51-22SDR SWAA2025041424037Slide · looseFWD SERVICE DOOR SLIDE LOOSE<[01] FOUND GIRT ASSY UNFOLDED. C/W ESCAPE SLIDE PACK CHECK AND FOLDED GIRT ASSY IAW AMM 25-66-01SDR SWAA2025041423226Skin · debondedLEFT OUTBOARD TRAILING EDGE FLAP UPPER SKIN HAS MISSING AND DISBONDED/DEFORMED MATERIAL ON THE INBD EDGE AND 10IN FROM THE TRAILING EDGE.<[01] PERFORMED EA- 25-157-00935;[02] VERIFIED THAT MAINTENANCE ACTIONS HAVE BEEN COMPLIED WITH IAW EA 25-157-00935;[03] VESDR SWAA2024112060963Lens · out of adjustFWD ENTRY EMERY LIGHT LENS<[01] REINSTALLED FWD ENTRY EMERG LIGHT LENS PER AMM 33-51-00SDR SWAA2024111358293Battery Pack · inoperativeFWD GALLEY EMERGENCY EXIT SIGNS LIGHTS INOP.<[01] REMOVED AND REPLACED FWD GALLEY EMERGENCY EXIT LIGHTS BATTERY PACKS PER AMM 33-51-06.SDR SWAA2024091236152Slide · bulgedFWD ENTRY DOOR SLIDE BULGING OUT ON AFT LOWER SIDE<[01] REMOVED AND REPLACED FWD ENTRY DOOR SLIDE REF AMM 25-66-01 AND TASK CARD 25-66-01. REFERENCE TTG8Q00VSP6G FOR TASK CARD AND SIDE PARTS INFORMATION.SDR SWAA2024083032419Slide · out of adjustF/A REPORTS RT FORWARD SERVICE DOOR SLIDE EXTENDS FROM BOTTOM FURTHER THEN NORMAL<[01] RESCURED SLIDE PER AMM 25-66-00SDR SWAA2024061400443Skin · pulled#2 ENGINE INLET COWL HAS MULTIPLE RIVETS PULLED THROUGH INLET SKIN. FWD AND AFT EDGES<[01] REMOVED AND REPLACED #2 ENGINE INLET COWL IAW AMM 71-11-01. OPS CHECK GOODSDR SWAA2024052288194Slide · dislodgedR1 DOOR SLIDE PARTIALLY DISLODGED<[01] SECURED SLIDE PER MT 725-61-06SDR SWAA2024031462578Seal · crackedLH HORIZONTAL STABILIZER FWD LOWER SLIDING SEAL CRACKED.<[01] 01 - REMOVED AND REPLACED PER [AMM 53-31-31-000-803-NG (STABILIZER-TO-BODY LOWER FRONT SPAR SLIDING SEAL REMOVAL - PERMANENT)] AT LH HORIZONTAL STAB;[02] C/W INSPECTIONSDR SWAA2024031362566Battery Pack · no testEMX LIGHT BATT PACK M01674 FAILS CAPACITANCE CHECK<[01] 01 - REMOVED AND REPLACED EMX BATTERY PACK M01674 PER [AMM 33-51-06-960-805-NG (POWER SUPPLY - BATTERY PACK REPLACEMENT - PERMANENT)]SDR SWAA2024031362565Battery Pack · no testEMX LIGHT BATT PACK M01668 FAILS CAPACITANCE CHECK<[01] 01 - REMOVED AND REPLACED EMX BATTERY PACK M01668 PER [AMM 33-51-06-960-805-NG (POWER SUPPLY - BATTERY PACK REPLACEMENT - PERMANENT)]SDR SWAA2024022053492Slide · low pressureFWD SERVICE DOOR SLIDE PRESSURE OUT OF RANGE<[01] R/R FWD SERVICE DOOR SLIDE PER MT 725-61-06FSSDR SWAA2023112223910Light · damagedROW 1ABC PHOTOLUMINESENT STRIP HAS MOISTURE IN IT.<[01] R/R ROW 1ABC PHOTOLUMINESCENT STRIP IAW AMM 33-51-15SDR SWAA2023103015501Lamp · inoperativeRIGHT OVERWING EXIT WINDOW LIGHT INOP. RELAMPED IAW AMM 33-51-01. OPS CHECK GOOD.SDR SWAA2023082391898Lens · brokenCREW REPORTS; L1 DOOR ON FWD LAV AFT WALL EMERGENCY EXIT SIGN LENS FELL OFF / BROKEN<[01] R&R?D L1 DOOR ON FWD LAV AFT WALL EMERGENCY EXIT SIGN LENS IN REF. TO AMM 33-51-01. LIGHT OPS CHECK GOOD @ THIS TIME.SDR SWAA2023072080367Slide · out of positionAFT SERVICE DOOR SLIDE INSPECTION STICKER BLOCKS NEEDLE HARD TO READ<[01] FOUND AFT ENTRY DOOR SLIDE INSPECTION DECAL MISPOSITIONED ; REPLACED DOOR SLIDE DECAL PER SIP. C/W M/T 725-61-06SDR SWAA2023071174613Battery Pack · inoperativeEMERGENCY LIGHTS ASSOCIATED WITH BATTERY PACK M1670 ARE INOP<[01] COMPLETED STEP 1.;[02] REPLACED M1670 EMERGENCY LIGHTS BATTERY AND TESTED PER AMM 33-51-06-960-805; NO DEFECTS NOTED.;[03] VERIFIED CORRECTIVE ACTION 2; AND STEP 1.;[04] MAINTENANCE COMPLETE; DESDR SWAA2023071761688Stiffener · crackedLEFT HORIZONTAL STABILIZER RIB 2ND STIFFENER IS CRACKED AT STAB STA 129.50<[01] REMOVED THE DAMAGED PART AT LH HORIZONTAL STABILIZER STA 129.50 RIB 2ND VERTICAL STIFFENER IAW SRM 55-10-09-2R-4;[02] HFEC REQUEST ON THE CUT OUT EDGES; WEB AND EXISTING FASTENERS SDR SWAA2023071761681Stringer · crackedCRACKED STRINGER END AT AREA AFT OF FWD CARGO BAY BS540 STR 23R<[01] REMOVED EXISTING REPAIR AT FCB STA-500D TO STA-540 STR-23R IAW SRM 51-40-02-0G-0;[02] UPDATE PARTIAL STEP 1-2;[03] REQUEST FOR NDI HFEC INSPECTION ON TRIM-OUT AND EXISTING OPEN HOLE FASTENERSSDR SWAA2023071761683Stringer · crackedCRACKED STRINGER END AT AREA AFT OF FWD CARGO BAY BS540 STR 26R<[01] CUT AND REMOVED DAMAGED STRINGER FCB STR-26R STA-500D+10'' IAW SRM 51-10-02-0G-0;[02] PARTIAL UPDATE STEP 1;[03] REQUEST FOR NDI HFEC INSPECTION ON TRIM-OUT AND EXISTING OPEN HOLE FASTENERS;[SDR SWAA2023071761684Stringer · crackedCRACKED STRINGER END AT AREA AFT OF FWD CARGO BAY BS540 STR 23L<[01] PARTIALLY COMPLETED STEPS 1-2;[02] REMOVED DAMAGED STRINGER SECTION FROM BS 500D+7 TO BS 538 STR 23L IAW SRM 51-10-02-0G-0;[03] REQUEST FOR NDI HFEC INSPECTION ON TRIM-OUT AND EXISTING OPEN HSDR SWAA2023071761685Stringer · crackedCRACKED STRINGER END AT AREA AFT OF FWD CARGO BAY BS540 STR 26R BS 540 STR 26L<[01] PARTIALLY COMPLETED STEPS 1-2;[02] REMOVED DAMAGED STRINGER SECTION FROM BS 500D+7 TO BS 538 STR 26L IAW SRM 51-10-02-0G-0;[03] REQUEST FOR NDI HFEC INSPECTION ON TRIM-OUT AND SDR SWAA2023071261682Stringer · crackedCRACKED STRINGER END AT AREA AFT OF FWD CARGO BAY BS540 STR 25R<[01] CUT AND REMOVED DAMAGED STRINGER FCB STR-25R STA-500D+10'' IAW SRM 51-10-02-0G-0;[02] UPDATE PARTIAL STEPS 1-5;[03] REQUEST FOR NDI HFEC INSPECTION ON TRIM-OUT AND EXISTING OPEN HOLE FASTENERSDR SWAA2023071161686Threshold · corrodedAFT CARGO BAY SUBTHRESHOLD IS CORRODED. CORROSION IS MEASURED FROM FWD EDGE OF PART AND IS MARKED ACCORDINGLY. (+8 TO+14); (+14 TO +16); (+17 TO+19); (+23 TO +25); (29 TO +32); (+33 TO +35)<[01] PARTIALLY STEPS 1;2;3.;[02] AFT CARGO BAY SUB THRESHOLD MUST BE RSDR SWAA2023071161703Threshold · corrodedAFT CARGO BAY SUB THRESHOLD CORRODED. CORROSION MEASURED FROMFWD EDGE AND IS MARKED ACCORDINGLY. (+36 TO +37); (+39); (+41 TO +42); (+44)<[01] REMOVED CORROSION ON AFT CARGO BAY SUBTHRESHOLD BETWEEN BS 827+12' RBL 28; WL.156 IAW SRM 51-10-02.<BR> MEASURE MAX. SDR SWAA2023071760761Panel · crackedVERTICAL FIN PANEL 324AL LOWER CLIP IS CRACKED<[01] CRACKED ON VERTICAL FIN PANEL 324AL LOWER CLIP WITH NEXT DIMENSION L=3.220 TOOL USED CALIPER 2738; DUE:04/2024; DATE:04/2023 FOUND TO BE OUT LIMITS I.A.W SRM 55-30-01-0L-3 FOR IDENTIFICATION AND DUE TO NO ALLSDR SWAA2023071760757Skin · corrodedSPOTTY SKIN CORROSION; BS1050 -1088; BETWEEN SKATE ANGLE AND AFT LEFT VERTICAL FIN FWD SUPPORT ANGLE<[01] SEVERAL AREAS OF CORROSION ON THE ANGLE AT BS 1036 FROM STR2R-STR2L FOUND TO BE OUT OF LIMITS DUE TO NO SRM ALLOWABLE DAMAGE IAW SRM 51-10-02 PAR 9C;[02] SDR SWAA2023071760668Plate · crackedLEFT WING LOWER T/E WIGGLE PLATE IS CRACKED AND LOOSE JUST I/B OF #1 PYLON<[01] REMOVED AND REPLACED LEFT WING LOWER T/E WIGGLE PLATE I/B OF #1 PYLON<BR>IAW SRM 51-40-02-0G-0;[02] UPDATED PARTS;[03] VERIFIED CORRECTION ACTION ITEM 1;2; CARD COMPLETE.SDR SWAA2023071260663Floor Panel · pulledCENTER CABIN FLOOR PANEL 242CF HAS A PULLED THROUGH INSERT<[01] IDENTIFIED FLOOR PANEL 242CF MATERIAL IAW SRM 53-00-50-0I-1 FIGURE 4 TABLE 4 AND BWG DWG 144A5810 ID: 0006.<BR><BR>DAMAGE EXCEEDS ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-50-1A-1 PARAGRAPH 4.F. <BR><SDR SWAA2023071159999Scuff Plate · crackedAFT CARGO BAY FWD CORNER SCUFF PLATE IS CRACKED; INCLUDNG ACROSS PREVIOUS WELD REPAIR<[01] VERIFIED APPLICABILITY PER SRM NOT ALLOWABLE DAMAGE PARTS DO NOT HAVE ENTRIES ARE CALLED REPAIRABLE BY REPLACEMENT;[02] RECEIVED NEW SCUFF PLATE P/N654A0004-97 LOT#14934SDR SWAA2023071759983Stiffener · crackedLEFT HORIZONTAL STABILIZER RIB 3RD STIFFENER IS CRACKED AT STAB STA 129.50<[01] REMOVED THE DAMAGED PART AT LH HORIZONTAL STABILIZER STA 129.50 RIB 3RD VERTICAL STIFFENER IAW SRM 55-10-09-2R-4;[10] FABRICATED REPAIR PARTS (1) T-SECTION FROM 60-5872 7075 T76511SDR SWAA2023071759980Web · crackedBS 663 LH SIDE VAPOR BARRIER WEB HAS CRACKS AND A TEMPORARY REPAIR; LBL 6 TO LBL 15.<[01] IDENTIFIED IAW SRM 57-10-10-0I-2 FIGURE 2 TABLE 2 ITEM 4<BR><BR>DAMAGE EXCEEDS ALLOWABLE DAMAGE LIMITS IAW SRM 57-10-10-1A-2 PAR.4 D(1)<BR><BR>DAMAGE TO BE REPAIRED IAW SSDR SWAA2023071759572Panel · pulledR/W L/E PANEL 621PB HAS PULLED FASTENER HOLE (MARKED)<[01] IDENTIFIED PART AND MATERIAL IAW SRM 57-41-01-0I-4 FIGURES 1+3; TABLE 3; ITEM [1].<BR>FOUND DAMAGE TO BE OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 57-41-01-1A-1 PAR 4.A (5).<BR>A PERMANENT REPAIR WILL BE SDR SWAA2023071759574Panel · pulledL/W L/E PANEL 621HB HAS PULLED FASTENER HOLES (MARKED)<[01] IDENTIFIED PANEL 621HB MATERIAL IAW SRM 57-41-01-0I-4; FIGURE 4; SHEET1; TABLE 4; ITEM [1]. <BR><BR>CLEANED PANEL AND REMOVED FINISH AS NEEDED TO EVALUATE DAMAGE IAW AMM 51-21-11-150-815 PARA. 17. C. SDR SWAA2023071759577Panel · pulledR/W L/E PANEL 621SB HAS PULLED FASTENER HOLES (MARKED)<[01] IDENTIFIED PANEL 621SB MATERIAL IAW SRM 57-41-01-0I-4 TABLE 3 FIGURE 3 ITEM 1. DAMAGE AT DISCREPANT LOCATION EXCEEDS ALLOWABLE DAMAGE LIMITS IAW SRM 57-41-01-1A-1 PARAGRAPH 4.A(5). DAMAGE IS REPAIRABLSDR SWAA2023071759970Panel · pulledL/W L/E PANEL 521TB HAS PULLED FASTENER HOLES (MARKED)<[01] IDENTIFIED 521TB PANEL IAW SRM 57-41-01-0I-4 FIGURE 3; ITEM 1; TABLE 3<BR>FOUND DAMAGE TO BE OUT OF ALLOWABLE LIMITS IAW SRM 57-41-01-1A-1 PARA 4.A.(2).<BR>DAMAGE WILL BE REPAIRED IAW SRM 51-70-04-2R-SDR SWAA2023071759974Panel · pulledL/W L/E PANEL 521JB HAS PULLED FASTENER HOLES (MARKED)<[01] IDENTIFIED PANEL MATERIAL IAW SRM 57-41-01-0I-4 FIG 4 TABLE 4 ITEM 1.<BR>FOUND DAMAGE TO 3EA FASTENER HOLES TO BE OUT OF ALLOWABLE LIMITS IAW SRM 57-41-01-1A-1 PARA 4.A(5).<BR>DAMAGE WILL BE REPAIRED SDR SWAA2023071759973Panel · pulledL/W L/E PANEL 521MB HAS PULLED FASTENER HOLES (MARKED)<[01] IDENTIFIED PANEL 521MB IAW SRM 57-41-01-0I-4 FIGURE 4 ITEM [1]; DAMAGE TO THE PANEL IS BEYOND THE ALLOWABLE LIMITS IAW SRM 57-41-01-1A-1 PARAGRAPH 4.A.(4).(C) AND WILL BE REPAIRED IAW SRM 51-70-04-2R-SDR SWAA2023071759972Panel · pulledL/W L/E PANEL 521QB HAS PULLED FASTENER HOLES (MARKED)<[01] IDENTIFIED 521QB PANEL IAW SRM 57-41-01-0I-4 FIGURE 3; ITEM 1; TABLE 3<BR>FOUND DAMAGE TO BE OUT OF ALLOWABLE LIMITS IAW SRM 57-41-01-1A-1 PARA 4.A.(2).<BR>DAMAGE WILL BE REPAIRED IAW SRM 51-70-04-2R-SDR SWAA2023071759971Panel · pulledL/W L/E PANEL 521WB HAS PULLED FASTENER HOLES (MARKED)<[01] IDENTIFIED 521WB PANEL IAW SRM 57-41-01-0I-4 FIGURE 2; ITEM 1; TABLE 2<BR>FOUND DAMAGE TO BE OUT OF ALLOWABLE LIMITS IAW SRM 57-41-01-1A-1 PARA 4.A.(2).<BR>DAMAGE WILL BE REPAIRED IAW SRM 51-70-04-2R-SDR SWAA2023071759976Panel · pulledL/W L/E PANEL 521CB HAS PULLED FASTENER HOLES (MARKED)<[01] IDENTIFIED PANEL MATERIAL IAW SRM 57-41-01-0I-4 FIG 5 TABLE 5 ITEM 3.<BR>FOUND DAMAGE TO 3EA FASTENER HOLES TO BE OUT OF ALLOWABLE LIMITS IAW SRM 57-41-01-1A-1 PARA 4.A(5).<BR>DAMAGE WILL BE REPAIRED SDR SWAA2023061659140Spar Cap · corrodedRT WING LOWER FWD SPAR CAP SHOWS EVIDENCE OF CORROSION UNDER PANEL 621DB APPROX WS 293.0. EVALUATED EXFOLIATION CORROSION ON LOWER CHORD RT WING LOWER FWD SPAR CAP, FOUND OUT OF LIMITS 100% EXFOLIATION LOWER CHORD IAW SRM 57-20-10-1A-1 4.A. TRIMED OUT DAMAGSDR SWAA2023030611235Handle · looseFLIGHT ATTENDANT REPORTS AFT ENTRY DOOR HANDLE IS LOOSE<[01] SECURED AFT ENTRY DOOR HANDLE IAW M/M 52-13-31SDR SWAA2023030110978Slide · missingFORWARD SERVICE DOOR SLIDE IS MISSING VELCRO MANUAL HANDLE COVER<[01] REMOVED AND REPLACED FWD SERVICE DOOR SLIDE PER MT 725-61-06SDR SWAA2023020800065Slide · out of positionL2 SLIDE APPEARS DISLODGED<[01] REPOSITIONED L2 SLIDE IN CASE IAW AMM 25-66-01 OK FOR SERVICESDR SWAA2023011791756Lamp · inoperativeLEFT AFT EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMPS IAW AMM 33-51-04.SDR SWAA2022113076657Battery Pack · no testFORWARD RT EMERGENCY LIGHT BATTERY PACK FAILED A CAPACITY TEST. REMOVED AND REPLACED THE BATTERY PACK IAW MM 33-51-06.SDR SWAA2022111170118Gauge · obstructedAFT ENTRY DOOR SLIDE PRESSURE GAUGE NEEDLE COVERED BY INSPECTION STICKER. REMOVED SLIDE AND UNCOVERED NEEDLE AND REINSTALLED SLIDE PER MT 725-61-06.
Back to N417WN, cancelled Sep 29, 2025