N454WN
Service difficulty reports · 342
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 = 'N454WN' 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 = 'N454WN' 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 SWAA2026020566652Handle · brokenL1 DOOR HANDLE BROKEN. REMOVED THE DOOR ASSIST HANDLE FROM FWD LAV AND REPLACED ASSIST HANDLE WITH NO DEFECTS NOTED. ACFT OK FOR SERVICE IAW AMM 52-11-31.SDR SWAA2026010557819Sign · brokenL1 DOOR EMERGENCY EXIT SIGN COVER BROKEN. PERFORMED EA M-21-133-00720 OK TO CONTINUE ON TLD SECURED L1 LOWER EMER EXIT SIGN.SDR SWAA2025111735016Sign · brokenRIGHT OVERWING EXIT FWD LOWER EXIT DOOR LIGHT HAS 2EA BULBS INOPERATIVE. FOUND SIGN BROKEN AND MISSING LENS MOUNTING SCREW; REPLACED RH OVERWING EXIT. FORWARD LOWER EMERGENCY EXIT SIGN AND TESTED PER AMM 33-51-01-960-802, NO DEFECTS NOTED.SDR SWAA2025111734265Battery Pack · inoperativeEMERGENCY EXIT LIGHTS ASSOCIATED WITH BATTERY PACK M1669, DID NOT ILLUMINATE. REPLACED POWER SUPPLY BATTERY PACK M1669 ASSOCIATED WITH EMERGENCY LIGHTS AND PERFORMED GOOD TEST PER AMM 33-51-06-960-805. MAINTENANCE COMPLETED.SDR SWAA2025111731793Attach Angle · crackedCRACKED ATTACH ANGLE AT MID CABIN BS 690, LBL 1, WL 204. REMOVED FABRICATED AND REPLACED ATTACH ANGLE IAW SRM 51-40-02-0G-0, DWGS 273A9112, REV B, DWG 273A9110, REV A.SDR SWAA2025111730206Skin · crackedCRACK ON LH LOWER HORIZONTAL STABILIZER SKIN. AT STAB STA 193.90; 26' FROM FWD EDGE; .4' LENGTH. REPAIRED LT LOWER HORIZONTAL STABILIZER SKIN. AT STAB STA 193.90 PER REF SRM 55-10-01-2R-11. VERIFIED COMPLETED RII STEPS IN CORRECTIVE ACTION 1.SDR SWAA2025111730043Panel · damagedPANEL 661CB HAS SEVERAL ELONGATED FASTENER HOLES. PANEL 661CB WITH SEVERAL ELONGATED FASTENER HOLES WAS REPAIRED PER. SRM 51-70-04-2R-9.SDR SWAA2025111730034Plate · crackedLEFT WING T/E WIGGLE PLATE COMMON TO PANEL 551EB ON THE I/B SIDE IS CRACKED. REMOVED AND REPLACED LEFT WING T/E WIGGLE PLATE COMMON TO PANEL 551EB ON THE I/B SIDE IAW SRM 51-40-02-0G-0, RESTORED EXTERNAL FINISH ON LOWER SURFACE OF LT WING, AROUND THE FASTENESDR SWAA2025111730036Support Beam · crackedLEFT WING T/E AFT PANEL SUPPORT BEAM COMMON TO PANEL 561AB IS CRACKED. REMOVED AND REPLACED LEFT WING T/E AFT PANEL SUPPORT BEAM COMMON TO PANEL 561AB IAW SRM 51-40-02-0G-0 AND AMM 20-50-11-910-801.SDR SWAA2025111730037Plate · crackedRIGHT WING T/E WIGGLE PLATE COMMON TO PANEL 651GB ON THE INBD SIDE IS CRACKED. REMOVED AND REPLACED RIGHT WING T/E WIGGLE PLATE COMMON TO PANEL 651GB ON THE I/B SIDE. IAW SRM-51-40-02-0G-0.SDR SWAA2025111730038Plate · crackedRIGHT WING T/E WIGGLE PLATE COMMON TO PANEL 651EB ON THE I/B SIDE IS CRACKED. REMOVED AND REPLACED RIGHT-WING T/E WIGGLE PLATE P/N 115A2781-4 COMMON TO PANEL 651EB; IAW SRM 51-40-02 AND DWG#115A2781 REV B.SDR SWAA2025111730033Support Angle · crackedLEFT WING FIXED T/E PANEL JUST O/B OF THE NR 6 SPOILER LOWER SUPPORT ANGLE CRACKED. REMOVED AND REPLACED LEFT WING FIXED T/E PANEL JUST O/B OF THE #6 SPOILER LOWER SUPPORT ANGLE.<BR>IAW SRM 51-40-02-0G-0.SDR SWAA2025111729432Attach Angle · crackedB.S. 663 LOWER COMPOSITE BULKHEAD UPPER ATTACH ANGLE IS CRACKED AT LBL 45, WL 167. REMOVED, REPLACED, AND INSTALLED A NEW 663 LT UPPER ATTACH ANGLE LBL 4- TO LBL 65 IAW SRM 51-40-02-0G-0, AND DWG 111A1000, REV -.SDR SWAA2025111729691Attach Angle · crackedCRACKED ATTACH ANGLE AT MID CABIN BS 690, RBL 1, WL 206. REMOVED FABRICATED AND REPLACED ATTACH ANGLE AT PASSENGER COMPARTMENT BS 690, RBL 1, WL 206 IAW SRM 51-10-02-0G-0, SRM 51-40-02-0G-0 AND DWGS 273A9112, REV H, 273A9112, REV-, 273A9110, REV A.SDR SWAA2025111729694Tab · crackedRIGHT WING T/E DEFLECTION CONTROL RIB UPPER TAB CRACKED. REPAIRED RIGHT WING T/E DEFLECTION CONTROL RIB UPPER TAB IAW SRM 57-51-02-1A-1, SRM 57-51-02-2R-3, AND AMM 57-50-01-820-801.SDR SWAA2025111729690Strap · corrodedCORROSION ON STRAP AT MID CABIN BS 709, RBL 63, WL 204. REMOVED, FABRICATED, AND REPACED STRAP AT MID CABIN BS 709, RBL 63, WL 204 IAW EA 25-153-03005.SDR SWAA2025111728485Pressure Deck · crackedSUSPECTED OF CRACK AT HORIZONTAL PRESSURE DECK WEB BS 663, LBL 31, REMOVED AND REPAIRED HORIZONTAL PRESSURE DECK BS 663 - 675, LBL 25 - LBL 60 IAW SRM 53-40-51-2R-2, REPAIR 2.SDR SWAA2025111728307Floor Panel · delaminatedFLOOR PANEL 231XF IS DELAMINATED. FLOOR PANEL 231XF; WITH DELAMINATION; WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0.SDR SWAA2025111728272Slide · out of adjustFWD ENTRY DOOR SLIDE REQUIRES REPOSITIONING. ADJUSTED FWD ENTERY DOOR SLIDE IAW AMM 25-66-01-400-803.SDR SWAA2025100320435Handle · looseFWD GALLEY SERVICE DOOR ASSIST HANDLE LOOSE. RESECURED FWD GALLEY SERVICE DOOR ASSIST HANDLE REF AMM 20-50-11.SDR SWAA2025080196015Slide · looseFWD SERVICE DOOR SLIDE SCREW CAME LOOSE. SECURED LOOSE SCREW IAW MT 725-61-06. SECURED LOOSE SCREW IAW MT 725-61-06 AND SIP.SDR SWAA2024090332086Plate · pulledL/H WING LWR T/E PANEL I/B OF #1 PYLON WIGGLE PLATE FASTENERS PULLED.<[01] R&R L/H WING LWR T/E PANEL OF #1PYLON WIGGLE PLATE PER SRM 51-40-02;[02] R&R L/H WING LWR T/E PANEL I/B OF #1PYLON WIGGLE PLATE PER SRM 51-40-02SDR SWAA2024090332087Support Bracket · separatedL/H WING LWR T/E PANEL I/B OF #1 PYLON I/B SUPPORT BRACKET; FWD SUPPORT ROD SEPARATED/DAMAGED.<[01] REMOVED AND REPLACED L/H LWR WING T/E #1 PYLON I/B SUPPORT BRACKET ROD I.A.W AMM 57-50-02SDR SWAA2024082729482Frame · damagedRH PYLON FWD FRAME 313A2710-1 AND STIFFENER 313A2300-3 HAVE 2 EA ELONGATED HOLES ON THE I/B SIDE<[01] SRM 51-40-02-0G-0-A00729 (GENERAL - FASTENER INSTALLATION AND REMOVAL - AIRFRAME - PERMANENT)SEE FAULT TTG8Q00VEVDL FOR FINAL DEPOSITION.;[02] C/WSDR SWAA2024082731187Stiffener · damagedRH PYLON FWD FRAME 313A2710-1 AND STIFFENER 313A2300-3 HAVE 2 EA ELONGATED HOLES ON THE I/B SIDE<[01] SRM 51-40-02-0G-0-A00729 (GENERAL - FASTENER INSTALLATION AND REMOVAL - AIRFRAME - PERMANENT)SEE FAULT TTG8Q00VEVDL FOR FINAL DEPOSITION.;[02] C/WSDR SWAA2024041172829Lens · misinstalledL2 DOOR EMERGENCY LIGHT COVER ARROW POINTS IN THE WRONG DIRECTION<[01] REPLACED BOTH THE LIGHT ASSY AND THE DIRECTIONAL LENS AT THE L2 DOOR. REF. AMM 33-51-01.SDR SWAA2024010337456Sign · damagedAFT GALLEY EMERGENCY EXIT SIGN DAMAGED<[01] REMOVED AND REPLACED EMERGENCY EXIT SIGN AS PER AMM 33-51-01; OPS CKS GOODSDR SWAA2023121431083Pump · faultyAT CRUISE #1 ENG A HYD PUMP LOW PSI LIGHT ILLUMINATED<[01] REMOVED AND REPLACED #1 ENGINE DRIVEN PUMP;'A' SYSTEM; (EDP) ; PER. AMM REF. 29-11-11. OPS. AND LEAK CHECKED GOOD PER. AMM REF. 29-11-11.SDR SWAA2023121329463Seat · incorrectSEAT BACKS RECLINE ON SEATS 11BC (EMERGENCY EXIT SEATS) 2023-689434<[01] CORRECTED INSTALLED SEAT BACKS ON SEATS 11BC (EMERGENCY EXIT SEATS) IAW CMM B/E AEROSPACE 25-21-42 STEP (G) ITEM (1);[02] CORRECTED STEP 1<BR><BR>CORRECTED INSTALLED SEAT BACKS ON SEATS 1SDR SWAA2023121324852Access Panel · crackedCRACK ON ACCESS PANEL 193AL ON INTERNAL AREA AT LOWER FUSELAGE 2023-689400<[01] TOOL USED: CALIPER P/N: 500-197-30 S/N:15120589 DUE DATE: 13-FEB-24;[02] TOOL USED: HOT BONDER PN: HCS9200B SN: 18165044 DUE DATE: 26/MAR/24;[03] TOOL USED: SCALE PN: SPX621 SN: 83SDR SWAA2023121322877Stringer · crackedCRACK ON STRINGER 24L LOC BS 500D ON FWD CARGO COMP 2023-689381<[01] TOOL USED: DIGITAL CALIPER P/N: 500-193-30; S/N: 0036B49 AND DUE DATE: 31-DEC-23.;[02] TOOL USED: ULTRASONIC EQUIPMENT; P/N: 45 MG; S/N: 232017609; DUE DATE: 22-SEP-24.;[03] TOOL USED: ULTRASSDR SWAA2023121320883Angle · crackedCRACK ON ANGLE AUXILIARY TRACK LOCATED SLAT 8 RT WING 2023-689361<[01] REPLACED ANGLE LOCATED INBOARD AUXILIARY SLAT TRACK SLAT 8 AT RT WING IAW B737-700 SRM 51-40-02 AND DWG 114A5010 SHEET:8 REV:D AND TOOK MEASURE OF CRACK; MEASURE IS L= 1.931 '; TOOL USED: DSDR SWAA2023121320884Rail · crackedCRACK LEADING EDGE RAIL NUTPLATES LOCATED OFSS 574 AT LT WING 2023-689362<[01] REPLACED RAIL NUT PLATES LOCATED OFSS 574 AT LT WING IAW B737-700 SRM 51-40-02 AND TOOK MESURE OF CRACK; MEASURE IS L= 0.418' TOOL USED; DIGITAL CALIPER P/N:500-197-30; S/N:A2114776SDR SWAA2023121320514Bracket · crackedCRACK SUPPORT BRACKET BODY STATION 540 LH SIDE KEEL BEAM 2023-689356<[01] REPLACED SUPPORT BRACKET AND FASTENERS BODY STATION 540 LH SIDE KEEL BEAM IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9. MEASURE CRACK IS: L: 0.900?; TOOL USED. DIGITAL CALIPER P/N: SDR SWAA2023121320076Angle · crackedCRACK ANGLE BTW BS 907 TO BS 927 RBL 13.I FWD POSITION AT AFT CARGO COMPARTMENT 2023-689324 CRACK ANGLE BTW BS 907 TO BS 927 RBL 13.1 FWD POSITION AT AFT CARGO COMPARTMENT<[01] REPLACED ANGLE AND FASTENER I.A.W SRM B737-700 51-40-02 AND DRAWING 147A7221 REV:D SDR SWAA2023121331102Angle · crackedCRACK ANGLE BTW BS 907 TO BS 927 RBL 13.I FWD POSITION AT AFT CARGO COMPARTMENT 2023-689324 CRACK ANGLE BTW BS 907 TO BS 927 RBL 13.1 FWD POSITION AT AFT CARGO COMPARTMENT<[01] REPLACED ANGLE AND FASTENER I.A.W SRM B737-700 51-40-02 AND DRAWING 147A7221 REV:D SDR SWAA2023121331101Angle · crackedCRACK ANGLE BTW BS 907 TO BS 927 RBL 13.8 AFT POSITION AT AFT CARGO COMPARTMENT 2023-689326<[01] REPLACED ANGLE AND FASTENER I.A.W SRM B737-700 51-40-02 AND DRAWING 147A7221 REV:D; SEE INDIVIDUAL STEP SIGN OFFS BELOW;[02] CORRECTED STEP 1.<BR>REPLACED ANGLE ANSDR SWAA2023121320077Angle · crackedCRACK ANGLE BTW BS 907 TO BS 927 RBL 13.8 AFT POSITION AT AFT CARGO COMPARTMENT 2023-689326<[01] REPLACED ANGLE AND FASTENER I.A.W SRM B737-700 51-40-02 AND DRAWING 147A7221 REV:D; SEE INDIVIDUAL STEP SIGN OFFS BELOW;[02] CORRECTED STEP 1.<BR>REPLACED ANGLE ANSDR SWAA2023121319325Girt Bar · wornWEAR HARDWARE ON GIRT BAR FITTING ON ENTRY AND SERVICE DOOR AT FWD GALLEY AREA 2023-689300<[01] REPLACED HARDWARE ON GIRT BAR FITTING ON ENTRY AND SERVICE DOOR AT FWD GALLEY AREA I.A.W B737-700 AMM 25-66-02-400-801;[02] CERTIFIED WORK PERFORMED.SDR SWAA2023121319324Girt Bar · wornWEAR HARDWARE ON GIRT BAR FITTING ON ENTRY AND SERVICE DOOR AT AFT GALLEY AREA 2023-689295<[01] REPLACED HARDWARE ON GIRT BAR FITTING ON ENTRY AND SERVICE DOOR AT AFT GALLEY AREA IAW B737-700 AMM-25-66-02-400-801;[02] REPLACED HARDWARE ON GIRT BAR FITTING ON ESDR SWAA2023121319518Rib · crackedCRACK ON RIB LOCATED ON LE STA 105.26 AT LEADING EDGE AT RT HORIZONTAL STABILIZER 2023-689305<[01] REPLACEED RIB AND NEW FASTENERS LOCATED ON LE STA 105.26 AT LEADING EDGE AT RT HORIZONTAL STABILIZER IAW B737-700 SRM 51-40-02 AND DWG 186A1001 SHEET 10 REV:A ANSDR SWAA2023121319515Rib · crackedCRACK ON RIB LOCATED ON LE STA 95.96 AT LEADING EDGE AT RT HORIZONTAL STABILIZER 2023-689306<[01] REPLACED RIB LOCATED ON LE STA 95.96 AT LEADING EDGE AT RT HORIZONTAL STABILIZER IAW B737-700 SRM 51-40-02 AND DWG 186A1001 SHEET 10 REV A SEE INDIVIDUAL SIGN OFFSDR SWAA2023121319323Battery Pack · inoperativeINOP LOWERED CEILING PANEL BATTERY PACK EMERGENCY LIGHT AT AFT GALLEY AREA (2EA) 2023-689288<[01] REPLACED LOWERED CEILING PANEL BATTERY PACK EMERGENCY LIGHT AT AFT GALLEY AREA (2EA) I.A.W B737-700 AMM 33-51-06-960-805. TEST IS OK. <BR>SEE INDIVIDUAL SIGN OFF SDR SWAA2023121319322Battery Pack · inoperativeINOP LOWERED CEILING PANEL BATTERY PACK EMERGENCY LIGHT AT FWD GALLEY AREA (2EA) 2023-689287<[01] REPLACED CEILING PANEL BATTERY PACK EMERGENCY LIGHT AT FWD GALLEY AREA (2EA) I.A.W B737-700 AMM 33-51-06-960-805; TEST IS OK. <BR>SEE INDIVIDUAL SIGN OFF BELOW.;[SDR SWAA2023121331103Angle · crackedCRACK ON ANGLE LOCATED BS 294.5 BTW STR 12L TO STR 14L AT FWD GALLEY AREA 2023-689277<[01] REPLACED ANGLE AND FASTENERS LOCATED ON BS 294.5 BTW STR 12L TO STR 14L AT FWD GALLEY AREA IAW B737 SRM 51-40-02 AND DWG 141A1311; SHEET 1 AND REV: C.;[02] CORRECTED STESDR SWAA2023121319112Angle · crackedCRACK ON ANGLE LOCATED BS 294.5 BTW STR 12L TO STR 14L AT FWD GALLEY AREA 2023-689277<[01] REPLACED ANGLE AND FASTENERS LOCATED ON BS 294.5 BTW STR 12L TO STR 14L AT FWD GALLEY AREA IAW B737 SRM 51-40-02 AND DWG 141A1311; SHEET 1 AND REV: C.;[02] CORRECTED STESDR SWAA2023121319113Rib · crackedCRACK ON RIB LOCATED LE STA 86.66 AT LT HORIZONTAL STABILIZER 2023-689279<[01] REPLACED RIB AND FASTENERS LOCATED LE STA 86.66 AT LT HORIZONTAL STABILIZER I.A.W. B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9 AND DRAWING #186A1001; SHEET 10; REV A.<BR>SEE INDIVSDR SWAA2023121319114Rib · crackedCRACK ON RIB LOCATED LE STA 105.26 AT LT HORIZONTAL STABILIZER 2023-689280<[01] REPLACED RIB AND FASTENERS LOCATED LE STA 105.26 AT LT HORIZONTAL STABILIZER I.A.W. B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9 AND DRAWING #186A1001; SHEET 10; REV A.<BR>SEE INDSDR SWAA2023121318711Frame · crackedCRACK ON STUD FRAME LOCATED BS 294.5 AT LEVEL STR 17R AT FWD GALLEY AREA 2023-689248<[01] TOOL USED ET EQUIPMENT: P/N: NORTEC 600D; S/N: 210138203; CAL DUE DATE: 09-JUN-24;[02] PERFORMED PERMANENT REPAIR LOCATED BS 291.5 TO BS294.5 AT LEVEL STR 17R AT FWD GALLSDR SWAA2023121318890Frame · crackedCRACK ON FRAME LOCATED BS 747 BTW STR 8L TO STR 9L AT PASSENGER CABIN 2023-689259<[01] TOOL USED P/N: NORTEC 500D; S/N: N500X1693P030456; CAL DUE: 12-MAR-24.;[02] VERIFIED CRACK ON FRAME BS 747 BTW STR 8L TO STR 9L BY HFEC INSPECTION IAW NDT PART 6; 51-00-00 P
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