N468WN
Service difficulty reports · 309
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 = 'N468WN' 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 = 'N468WN' 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 SWAA2024042665548Support Angle · crackedCRACK ANGLE - SUPPORT LOCATED BS 947.5 AND S-26L AFT CARGO COMPARTMENT 2024-195835<[01] REPLACED SUPPORT ANGLE LOCATED BS 947.5 AND S-26L AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9. AND DRAWING # 149A8103 REV: -. SEE INDIVIDUAL SIGN OFF BELOW.;[02]SDR SWAA2024042665552Floorbeam · crackedCRACK ANGLE - SUPPORT LOCATED BS 727 BETWEEN S-27R TO S-27L AFT CARGO COMPARTMENT 2024-195840<[01] REPLACE ANGLE - SUPPORT LOCATED BS 727 BETWEEN S-27R TO S-27L AFT CARGO COMPARTMENT IAW. B737-700 SRM 51-40-02-0G-0 AND DRAWING 144A2600 REV B;[02] CORRECTE STEPSDR SWAA2024042665549Intercostal · corrodedCORROSION WEB - INTERCOSTAL LOCATED BS 767 TO BS787 ND S-25R WL 156 AFT CARGO COMPARTMENT 2024-195841<[01] REPLACE WEB-INTERCOSTAL LOCATED : BS 767 TO BS787 ND S-25R WL 156 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02-0G-0 AND DRAWING #146A0081 REV A.;[02] SDR SWAA2024042665026Pressure Deck · crackedCRACK INDICATION FOUND ON HORIZONTAL PRESSURE DECK WEB LBL 30 AT MAIN WHEEL WELL COMPARTMENT. CRACK LENGTH:0.328 INCH APPROX. 2024-195800 EXACTLY LOCATION OF DAMAGE: HORIZONTAL PRESSURE DECK BS-663 TO BS-675 WEB LBL 30 AT MAIN WHEEL WELL COMPARTMENT. CRACK LENSDR SWAA2024042665161Frame · crackedCRACK FRAME LOCATED STA747 BETWEEN STR8R TO STR9R AT PASSENGER CABIN 2024-195816<[01] REPAIRED FRAME LOC. STA747 BTW S-8R TO -9R AT PASSENGER COMPARTMENT I.A.W EA 1-A53-12114.SE INDIVIDUAL SIGN OFFS BEOW;[02] CORRECTED STEP 1 <BR>PERFORMED PERMANENT REPAIR ON SDR SWAA2024042665164Frame · crackedCRACK FRAME LOCATED STA827 BETWEEN STR8R TO STR9R AT PASSENGER CABIN 2024-195818<[01] PERFORMED PERMANENT REPAIR ON FRAME LOC. STA827 BETWEEN STR8R TO STR9R AT PASSENGER CABIN I.A.W EA 1-A53-12114. SEE INDIVIDUAL SIGN OFF BELOW;[02] PERFORMED PERMANENT REPAIR SDR SWAA2024042665029Web · crackedCRACK WEB FLOOR STRUCTURE LOCATED BETWEEN STA500D TO STA520 AT LEVEL STR28R AT FWD CARGO COMPARTMENT 2024-195808<[01] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 112031023; DUE DATE: 22-JAN-25; TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: SDR SWAA2024042665027Stringer · crackedCRACK STRINGER 23R LOCATED BS 540 FWD CARGO COMPARTMENT 2024-195759<[01] ULTRASONIC EQUIPMENT USED P/N: 45MG; S/N: 232017609 AND DUE DATE: 22-SEP-24.;[02] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES500000; S/N: 142811020; DUE DATE: 23-JAN-25 AND TEMPERATSDR SWAA2024042665028Stringer · crackedCRACK STRINGER 26L LOCATED STA540 FWD CARGO COMPARTMENT 2024-195762<[01] ULTRASONIC EQUIPMENT USED P/N: 45MG; S/N: 232017609 AND DUE DATE: 22-SEP-24.;[02] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES500000; S/N: 142811020; DUE DATE: 23-JAN-25 AND TEMPERATSDR SWAA2024042665030Stringer · crackedCRACK STRINGER 25L LOCATED STA 540 FWD CARGO COMPARTMENT 2024-195806<[01] ULTRASONIC EQUIPMENT USED P/N: 45MG; S/N: 232017609 AND DUE DATE: 22-SEP-24.;[02] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES500000; S/N: 142811020; DUE DATE: 23-JAN-25 AND TEMPERASDR SWAA2024042665160Frame · crackedCRACK FRAME LOCATED STA 747 BETWEEN STR 8L TO STR 9L AT PASSENGER CABIN 2024-195817<[01] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N: 200053402; DUE DATE: 24-AUG-24.;[02] PERFORMED HFEC INSPECTION ON AREA AFTER REMOVED BRACKET AND NOT FOUND DSDR SWAA2024042964847Crease Beam · corrodedCORROSION CREASE BEAM LOCATED STA639 RBL 64.5 WL 208.1 CENTER SECTION 2024-195751<[01] REPLACED CREASE BEAM LOCATED STA616 PLUS 10 IN TO STA639 PLUS 10IN RBL 64.5 WL 208.1 CENTER SECTION IAW B737-700 SRM 53-40-02. AND DWG-144A5901 REV: - SEE INDIVIDUAL SIGN OFSDR SWAA2024042664841Stringer · crackedCRACK ON STRINGER 15L LOCATED BETWEEN STA294.5 TO STA303.9 AT FWD GALLEY AREA 2024-195741<[01] TOOL USED PN. 45MG; SN. 130061901 ; DUE DATE. 09-JUN-24;[02] TOOL USED STEP 7: EDDY CURRENT EQUIPMENT; P/N: NORTEC 500D; S/N: N500X12101U102020; DUE DATE: 07 SEP 24.SDR SWAA2024042664842Tie Clip · crackedCRACK TIE CLIP LOCATED STA277 AND STR10R AT PASSENGER CABIN 2024-195743<[01] INSTALLED TIE CLIP LOCATED STA277 AND STR10R AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND DWG 141A1110 SHEET 18 REV -;[02] REPLECED TIE CLIP LOCATED STA277 AND STR10R AT PASSENGERSDR SWAA2024042664840Crease Beam · corrodedCORROSION CREASE BEAM LOCATED STA639 AND LBL64.5 WL208.1 CENTER SECTION 2024-195750<[01] REPLACED CREASE BEAM LOCATED STA616 PLUS 10 IN TO STA639 PLUS 10IN AND LBL64.5 WL208.1 CENTER SECTION IAW B737-700 SRM 51-40-02 AND DWG 144A5901 REV:- SEE INDIVIDUAL SIGN SDR SWAA2024042664844Floorbeam · crackedCRACK ANGLE FLOOR STRUCTURE LOCATED BS 540 LBL 1 CENTER SECTION 2024-195748<[01] REPLACE ANGLE FLOOR STRUCTURE LOCATED BS 540 LBL 1 CENTER SECTION IAW. B737-700 SRM 51-40-02-0G-0 AND DRAWING 143A0060;[02] INSTALLED NEW ANGLE FLOOR STRUCTURE; PERFORMED VISUAL ISDR SWAA2024042664706Angle · crackedCRACK ANGLE LOCATED BS 695 RBL 24.75 AT CENTER WING BOX. REPLACED ANGLE LOC. BS 695 RBL 24.75 AT CENTER WING BOX IAW B737-700 SRM 51-40-02-0G-0 AND DWG #111A6000 AND DWG #273A9110.;[03] REPLACED ANGLE LOC. BS 695 RBL 24.75 AT CENTER WING BOX IAW B737-700 SRM SDR SWAA2024042664843Floorbeam · crackedCRACK ANGLE FLOOR STRUCTURE LOCATED BS540 RBL 24.75 CENTER SECTION 2024-195746<[01] REPLACED ANGLE FLOOR STRUCTURE LOCATION BS540 RBL 24.75 CENTER SECTION IAW B737-700 SRM 51-40-02-0G-0 AND DRAWING #143A0060 REV: A.;[02] REPLACED ANGLE FLOOR STRUCTURE LOCATIONSDR SWAA2024042664846Floorbeam · crackedCRACK ANGLE FLOOR STRUCTURE LOCATED STA540 BETWEEN RBL24.75 TO RBL45.5 CENTER SECTION 2024-195747<[01] REPLACE ANGLE FLOOR STRUCTURE LOCATED STA540 BETWEEN RBL24.75 TO RBL45.5 CENTER SECTION IAW. B737-700 SRM 51-40-02-0G-0 AND DRAWING 143A0060;[02] INSTALLED NSDR SWAA2024042664845Floorbeam · crackedCRACK ANGLE FLOOR STRUCTURE LOCATED STA540 BETWEEN LBL24.75 TO LBL45.5 CENTER SECTION 2024-195749<[01] REPLACE ANGLE FLOOR STRUCTURE LOCATED STA 540 BETWEEN LBL24.75 TO LBL45.5 CENTER SECTION IAW B737-700 SRM 51-40-02-0G-0 AND DRAWING 143A0060;[02] INSTALLED NSDR SWAA2024042664037Support Angle · crackedCRACK ANGLE - SUPPORT LOCATED BS 727D CEILING AREA AFT CARGO COMPARTMENT 2024-195702 CRACK ANGLE - SUPPORT LOCATED BS727A TO BS747 CEILING AREA AFT CARGO COMPARTMENT<[01] PERFORMED DETAILED VISUAL INSPECTION ON ANGLE - SUPPORT LOC. AT BS727A TO BS747 CEILING ASDR SWAA2024042663458Frame · crackedCRACK ON FRAME LOCATED BS 259.5 AT LEVEL STR 9L AT PASSENGER CABIN 2024-195616<[01] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N: 60007161486; DUE DATE: 28-JUL-24.;[02] PERFORMED PERMANENT REPAIR LOCATED ON FRAME LOCATED BS 259.5 AT LEVEL STR SDR SWAA2024042663456Rib · crackedCRACK INSPAR RIB 120.30 AT 36 INCHES OF FRONT SPAR AT RT HORIZONTAL STABILIZER 2024-195612<[01] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N: 60009161631; DUE DATE: 11-MAR-25.;[02] TOOL UED: EDDY CUREENT EQUIPMENT; PN: NORTEC 600D; SN: 6000716SDR SWAA2023101209759Sign · out of adjustAFT GALLEY AREA O/H EXIT SIGN IS LOSE AND HANGING DOWN<[01] REMOVE AND REPLACED AFT CABIN O/H EMER EXIT SIGN ASSY PER M/M 33-51-01; OPS CHK GOOD.SDR SWAA2023072882896Cover · looseFO SIDE OVER WING EXIT DOOR HANDLE COVER LOOSE<[01] REESE URGED COVER IAW M/M 52-22-51SDR SWAA2023041024041Seal · cracked-LEFT HORIZONTAL STAB FWD UPPER SLIDING SEAL CRACKED.<[01] R&R LEFT HORIZONTAL STAB FWD UPPER SLIDING SEAL REF AMM 53-31-31.;[02] R&R LEFT HORIZONTAL STAB FWD UPPER SLIDING SEAL REF AMM 53-31-31.SDR SWAA2023041024042Seal · cracked-RIGHT HORIZONTAL STAB FWD UPPER SLIDING SEAL CRACKED.<[01] R&R RIGHT HORIZONTAL STAB FWD UPPER SLIDING SEAL. IAW AMM 53-31-31SDR SWAA2023040724044Battery Pack · failed5 EMERGENCY BATTERY PACKS FAILED CAPACITY CHECK<[01] REMOVED AND REPLACED BATTERY PACKS AT LOCATIONS: M1668; M1672; M1673; M1669; M1675 PER AMM 33-51-06. OPS CHECK GOOD.SDR SWAA2022121380961Light · inoperativeLEFT OVERWING EMERGENCY EXIT LIGHT (EXTERIOR) INOPERATIVE. REPLACED THE LAMPS IAW AMM 33-51-04, OPS CHECKED GOOD.SDR SWAA2022090750921None · missingEMERGENCY EXIT SIGN MISSING AT FWD ENTRY LEFT SIDE / [01] INSTALLED NEW LENS IAW AMM 33-51-01 OPS CHECK GOODSDR SWAA2022081842449Panel · elongatedPANEL 193B HAS NUMEROUS ELONGATED FASTENER HOLES AND COUNTERSINKS. / [01] R&R PANEL 193B PER SRM 51-40-02SDR SWAA2022080839181Bracket · brokenLT MLG AREA; LANDING GEAR ELECTRICAL BUNDLE GUIDE; LOWER BRACKET BROKEN LT MLG AREA LANDING GEAR ELECTRICAL BUNDLE GUIDE LOWER BRACKET BROKEN / [01] REMOVED AND REPLACED BRACKET PER. SRM REF. 51-40-02.SDR SWAA2022041191003Light · inoperativeEMERGENCY EXIT SIGN FWD OF L/H OWE HATCH INOP. / [01] CONNECTED CONNECTORS D3670 AND 3672 AND PERFORMED GOOD OPS TEST OF EMERGENCY EXIT SIGN FWD OF L/H OWE HATCH PER AMM 33-51-01-960-801 STEP 2.C.(2).;[02] VERIFIED CORRECTIVE ACTIONS STEP 1.SDR SWAA2022040790169Floor Panel · damagedCABIN FLOOR PANEL 231DF POPS WHEN WALKED ON. / [01] REMOVED FLOOR PANEL 231DF IAW AMM 53-21-00-000-801<BR>REMOVED AND REPLACED FOAM TAPE PER AMM 53-21-00-400-801 OK TO CLOSE FLOOR PANEL;[02] VERIFIED CORRECTIVE ACTION STEP 1.;[03] OK TO CLOSE GIVEN PANEL 231DFSDR SWAA2022040888503Seal Depressor · crackedUPON REMOVING SEAL DEPRESSOR FROM FSD SURROUND STUB FRAME; NOTICED SEAL DEPRESSOR IS CRACKED AT BS294 RBL55 WL255. UPON REMOVING SEAL DEPRESSOR FROM FSD SURROUND STUB FRAME NOTICED SEAL DEPRESSOR IS CRACKED AT BS294 RBL55 WL255. / [01] UPON INVESTIGATION; THERSDR SWAA2022040886965Stub Frame · crackedUPON REMOVING FSD UPPER HINGE FITTING; FSD SURROUND STUB FRAME IS CRACKED AT BS294 RBL55 WL255. / [01] LOCATED AND DRILLED NEW FSD SURROUND STUB FRAME AT BS 294 RBL 55 WL 255 IAW SRM 51-40-05-0G-0 AND DWG 141A8370;[02] VERIFIED CORRECTIVE ACTION 1;[03] OK TO ISDR SWAA2022040886047Floor Support · crackedCRACKED FLOOR SUPPORT BS 312-344 LBL 46 WL 208. / [01] UPON FURTHER INVESTIGATION FOUND CRACKED FLOOR SUPPORT TO BE LOCATED AT BS 312-328; LBL46 WL 208. REMOVED CRACKED FLOOR SUPPORT BS 312-328 LBL 46 WL 208 IAW SRM 51-40-02 0G-0.;[02] LOCATED AND DRILLED NEW SDR SWAA2022040786048Lens · crackedAFT SERVICE DOOR EMERGENCY LIGHT LENS IS CRACKED. / [01] FAULT TO BE CORRECTED ON TTG8Q00BFOV2.;[02] REMOVED & REPLACED AFT SERVICE DOOR (ASD) EMERGENCY LIGHT LENS IAW AMM 33-51-01-960-802;[03] INSPECTED & VERIFIED CORRECTIVE ACTION ITEM 2.SDR SWAA2022041183741Web · corrodedCORROSION ON BS 348 FRAME CLOSE OUT WEB LBL 62 WL 209. / [01] REMOVED CORROSION ON 348 FRAME CLOSEOUT WEB; LBL 62; WL 209. MAX MATERIAL REMOVED WAS .019' 1' BY 2' FROM .071'. OUT OF LIMITS PER SRM 53-10-15-1A-1; SRM 51-10-02-0G-0.;[02] VERIFIED CORRECTIVE ACTISDR SWAA2022041183070Panel · debondedPANEL 193CR HAS SMALL DISBOND ON INNER SURFACE OVER CORE; MARKED / [01] IDENTIFIED PANEL MATERIAL IAW SRM 53-40-70-0I-1; TABLE 2; FIG. 2; ITEM 9. <BR><BR>FOUND DAMAGE TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-40-70-1A-1; PARA. 4.B.(5). <BR><BR>AREA IS TO BE REPSDR SWAA2022041183073Panel · debondedPANEL 193CL HAS SMALL DISBOND ON INNER SURFACE OVER CORE; MARKED / [01] IDENTIFIED MATERIAL OF PANEL 193CL IAW SRM 53-40-70-0I-1 FIGURE 1-2; ITEM 9; TABLE 2<BR><BR>DAMAGE IS OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 53-40-70-1A-1 TABLE 101; PARA 4.A(5)<BR><BR>REPSDR SWAA2022040883069Skin · debondedPANEL 193AL HAS DISBOND ON INNER SURFACE CORE AREA; MARKED / [01] IDENTIFIED PANEL IAW SRM 53-40-70-0I-1 FIG 2 TABLE 2 ITEM 7. <BR><BR>DAMAGE TO INNER SURFACE CORE AREA IS BEYOND ALLOWABLE DAMAGE LIMITS IAW SRM 53-40-70-1A-1 PARA 4.A (6). <BR><BR>DAMAGE TO (1ESDR SWAA2022040883068Panel · debondedPANEL 193AR HAS SEVERAL DISBONDS TO INNER SURFACE OF PANEL CORE AREA; MARKED / [01] IDENTIFIED PART AND MATERIALS IAW SRM 53-40-70-0I-1 FIGURES 1-2; TABLE 2; ITEM[16] APPLIED BMS10-103 PRIMER & BMS10-60 ENAMEL IAW SRM 51-70-05-2R-2 PARA 4 STEP K.<BR>RE INSTALLSDR SWAA2022041182636Stiffener · crackedRT HORIZ STAB RIB AT STAB STA 129.50 #3 VERT STIFFENER IS CRACKED. / [01] APPLICABLE REPAIR FOR THIS CRACKED HORIZONTAL STAB RIB STIFFENER LOWER END IS SRM 55-10-09-2R-4.05] ACCOMPLISHED HFEC INSPECTION OF DAMAGE CUTOUT AND HOLES IN REPAIR AREA NO CRACK NOTED SDR SWAA2022041182375Strap · corrodedCORROSION ON STRAP STA 1018; LBL 3; WL 208. / [01] STRAP STA 1018; LBL 3; WL 208 IS OUT OF LIMITS DUE TO NO ALLOWABLE LIMITS; SRM 51-10-02-0G-0; REPLACEMENT OF PART IS APPLICABLE;[02] VERIFIED CORRECTIVE ACTION STEP 1.;[03] REMOVED STRAP STA 1018; LBL3; WL 208SDR SWAA2022041182376Strap · corrodedCORROSION ON STRAP STA 1016-1029; RBL 3; WL 208. / [01] STRAP STA 1016-1029; RBL 3; WL 208 IS OUT OF LIMITS DUE TO NO ALLOWABLE LIMITS; SRM 51-10-02-0G-0; REPLACEMENT OF PART IS APPLICABLE.;[02] VERIFIED CORRECTIVE ACTION STEP 1.;[03] REMOVED STRAP STA 1016-10SDR SWAA2022041182377Channel · corrodedCORROSION ON AFT SERVICE MOPSILL STA 927-1006; R/H; WL 208. / [01] EVALUATED CORROSION ON ASD MOPSILL STA 927-1006; R/H; WL 208. FOUND TO HAVE 100 PERCENT MATERIAL LOSS. OUT OF LIMITS PER SRM 53-53-70-15-01-1;[02] VERIFIED CORRECTIVE ACTION STEP 1.;[03] REMOVESDR SWAA2022041182383Support · corrodedCORROSION ON FLOOR SUPPORT STA 954; RBL 8; WL 208. / [01] REMOVED CORROSION ON FLOOR SUPPORT STA 954; RBL 8; WL 208. MAX MATERIAL REMOVED WAS .018' 1' BY .5' FROM .075. OUT OF LIMITS PER SRM 53-70-51-1A-1.MEASURED DEPTH WITH SPHERICAL MICROMETER ID# IS000459; SDR SWAA2022041182384Floorbeam · corrodedCORROSION ON 986 FLOORBEAM UPPER FLANGE LBL 2-LBL 45; WL 208. / [01] VERIFY APPLICABILITY PER SRM 53-70-51-1A-1 ALLOWABLE DAMAGE 1;[02] EVALUATED DAMAGE ON BS986 FLOOR BEAM AND FOUND TO BE OUT LIMITS AT LBL2 WL208 1.5'X1.5' ORIG. MAT. THICKNESS IS 0.150' REMAISDR SWAA2022041182378Floorbeam · corrodedCORROSION ON 986 FLOORBEAM UPPER FLANGE RBL 4-RBL 45; WL 208. / [01] VERIFY APPLICABILITY PER SRM 53-70-51-1A-1 ALLOWABLE DAMAGE 1;[02] EVALUATED DAMAGE ON BS986 FLOOR BEAM AND FOUND TO BE OUT LIMITS AT RBL4 WL208 1.5'X1.5' ORIG. MAT. THICKNESS IS 0.150' REMAI
Back to N468WN