N452WN
Service difficulty reports · 321
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 = 'N452WN' 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 = 'N452WN' 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 SWAA2022020360697Skin · crackedCRACK FOUND AT LT HORIZONTAL STABILIZER LOWER SKIN STAB STA 193.9 24' AFT OF FWD EDGE I/B OF I/B FASTENER ROW CRACK LENGHT 107' ; CORRECTION: CRACK FOUND AT LT HORIZONTAL STABILIZER LOWER SKIN STAB STA 193.9 24' AFT OF FWD EDGE IB OF IB FASTENER ROW CRACK LENGSDR SWAA2022020359596Web · corrodedSUPPLEMENTAL INFORMATION: AFT CARGO DOOR CUT OUT LOWER WEB HAS NUMEROUS SPOTS OF CORROSION ; AFT CARGO DOOR CT OT LOWER WE HAS NMEROS SPOTS OF CORROSION / [01] LOCATED AND DRILLED NEW PART AT AFT CARGO DOOR CUT OUT LOWER WEB REF B-737-700-SRM 51-40-05-0G-0; [0SDR SWAA2022020361594Seal · damagedL/H HORIZONTAL STAB. UPPER T/E PANEL # 333AT HAS METAL SLIDING SEAL WORN ; / [01] REMOVED AND REPLACED METAL SLIDING SEAL AT PANEL 333AT IAW B737-700 SRM 51-40-02-0G-0; [02] VERIFIED STEP 1SDR SWAA2022020458992Support · corrodedSUPPLEMENTAL INFORMATION: AFT CARGO COMPARTMENT R/H SIDE PLATE SUPPORT ZEE; HAS MANY SPOTS OF CORROSION FROM STA 767 TO 727. ; / [01] REMOVED CORROSION AT AFT CARGO R/H Z CHANNEL FROM 727-767 AS PER B737-700 SRM 51-10-02-0G-0; [02] VERIFIED 1; [03] PERFORMED USDR SWAA2022020458236Fitting · corrodedAFT CARGO FLOOR AREA BS 767 - 787, RT RAIL AT CARGO NET ATTACH FITTING HAD CORROSION. REMOVED CORROSION IAW SRM 51-10-02-0G-0. PERFORMED UT THICKNESS INSP ON REWORKED AREA IAW NDT P4 51-00-00 PROC.3, ORIGINAL MATERIAL 0.070', MATERIAL REMAINING 0.068', FOUSDR SWAA2022020458246Rail · corrodedAFT CARGO FLOOR AREA AT STA 927 L/H RAIL TOP AREA HAS CORROSION. REMOVED CORROSION AT AFT CARGO FLOOR AREA IAW SRM 51-10-02-0G-0. PERFORMED UT THICKNESS INSP ON REWORKED AREA IAW NDT P4 51-00-00 PROC.3. MATERIAL 0.086' AFTER REMAINING 0.077' MATERIAL LOST 0SDR SWAA2022020458244Rail · corrodedAFT CARGO FLOOR AREA BETWEEN BS 927 - 947.5 RT RAIL CORRODED. REMOVED CORROSION IAW SRM 51-10-02-0G-0. PERFORMED UT THICKNESS INSP ON REWORKED AREA IAW NDT P4 51-00-00 PROC.3. ORIGINAL MATERIAL THICKNESS 0.070'; MATERIAL LOSS 0.011'; REMAINING MATERIAL 0.059SDR SWAA2022020458243Attach Fitting · corrodedAFT CARGO FLOOR AREA BS 907 RT RAIL HAS CORROSION AT NET ATTACH FITTING. REMOVED CORROSION IAW SRM 51-10-02-0G-0. PERFORMED UT THICKNESS INSP ON REWORKED AREA IAW NDT P4 51-00-00 PROC.3, PERFORMED EVALUATION WITH UT THICKNESS AT REWORKED AREA AND ADJACENT SDR SWAA2022020457914Floorbeam · corrodedCORROSION AROUND FASTENER HOLES ON FLOORBEAM UPPER FLANGE BS 986.5, RBL 28'-46'. EVALUATED REWORKED AREA ORG. MAT.0.150' MAT REMAINING 0.100' MAT REMOVED 0.050' FOUND TO BE OUT OF LIMITS IAW SRM=53-70-51-11A-1. LOCATED AND DRILLED HOLES IAW B737 SRM 53-70-51SDR SWAA2022020457910Floorbeam · corrodedCORROSION SPOT ON AFT CABIN WET AREA FLOOR BEAM UPPER FLANGE AROUND FASTENER HOLE B.S.986.5 L.BL. 43'. REMOVED CORROSION IAW B 737-7 SRM 53-70-51-1A-1-A00108. EVALUATED REWORKED AREA ORG. MAT.0.150' MAT REMAINING 0.102' MAT REMOVED 0.048' FOUND TO BE OUT OF SDR SWAA2022020457912Floorbeam · corrodedCORROSION SPOT ON AFT CABIN WET AREA FLOORBEAM UPPER FLANGE AT BS 986.5 R.BL. 5'. REMOVED CORROSION IAW SRM 53-70-51-1A-1-A00108. PERFORMED UT THICKNESS INSP. IAW NDT PART 4; 51-00-00; PROCEDURE 3. MIN. THICKNESS 0.137'. FOUND TO BE OUT OF LIMITS IAW SRM=53SDR SWAA2022020457913Door · crackedRT GEAR FIXED DOOR CRACKED. REMOVED DOOR ASSY IAW AMM 32-13-11-000-803. INSTALLED A NEW MLG DOOR ASSY IAW AMM 32-13-11-420-803 FROM STEP 7.0 UP TO AND INCLUDING STEP 7.H.(3)(D)1)A).SDR SWAA2022010657909None · corrodedCORROSION SPOTS ON CABIN FLOOR WEB AFT WET AREA B.S. 1006+9 L.BL. 40'. (51-002). REMOVED CORROSION AT AFT CABIN FLOOR WEB AT STA 1006+9 AND LBL 40' IAW SRM 53-70-51-1A-1-A00108. REMOVED SHEAR WEB CORROSION WAS EXFOLIATING WEB IS OUT OF LIMITS IAW 51-40-02-0GSDR SWAA2022020356643Floor Panel · deterioratedAFT CARGO FLOOR PNL 140AF DETERIORATED ; / [01] REPLACED AFT CARGO FLOOR PANEL 140AF IN REF B-737 700 AMM 25-52-01-201-801-NG.; [02] CORRECTION FOR STEP #1 TO READ FABRICATED NEW AFT CARGO FLOOR PANEL 140AF IN REF B-737 700 AMM 25-52-01-201-801-NG; [03] VERIFISDR SWAA2022020356644Floor Panel · deterioratedAFT CARGO FLOOR PNL 140 BF DETERIORATED ; / [01] REPLACED AFT CARGO FLOOR PANEL 140BF IN REF B-737 700 AMM 25-52-01-201-801-NG.; [02] VERIFIED STEP 1SDR SWAA2022020356645Floor Panel · deterioratedAFT CARGO FLOOR PNL 140 DF DETERIORATED ; / [01] FABRICATED AFT CARGO FLOOR PANEL 140 DF AS PER B737-700 AMM 25-52-01-201-801; [02] VERIFIED STEP 1..SDR SWAA2022020456551Skin · crackedTWO CRACKS FOUND AT LT HORIZONTAL STABILIZER LOWER SKIN STAB STA193.90:(1) 16' AFT OF FWD EDGE;I/B OF I/B FASTENER ROW.CRACK LENGTH1'(2) 24'AFT OF FWD EDGE I/B OF I/B FASTENER ROW.CRACK LENGTH 1.7' ; TWO CRACKS FOND AT LT HORIZONTAL STAILIZER LOWER SKIN STAB SSDR SWAA2022020456550Skin · crackedCRACK FOUND AT RT HORIZONTAL STABILIZER LOWER SKIN STAB STA 193.90; 17' AFT OF FWD EDGE;I/B OF I/B FASTENER ROW. CRACK LENGTH 1'. ; CRACK FOND AT RT HORIZONTAL STAILIZER LOWER SKIN STAB STA 193.90; 17' AFT OF FWD EDGE;IB OF IB FASTENER ROW. CRACK LENGTH 1'. / SDR SWAA2022020456549Rib · crackedABOVE FWD ENTRY DOOR FWD CORNER AT BS 312 THERE`S A CRACKED RIB. FABRICATED UPPER CHORD REPAIR IAW SRM 53-10-07-2R-1 REPAIR 1, TRIMMED OUT CRACK AREA IAW SRM 53-10-07-2R-1 REPAIR 1. PERFORMED HFEC AT CUT OUT IAW NDTM PART 6; 51-00-00 PROCEDURE 23. NO CRACKSSDR SWAA2022020356642Intercostal · crackedFWD WET AREA STATION 312 - 328 INTERCOSTAL CRACKED RBL 30 ; / [01] PERFORMED HFEC AND CONFIRMED CRACK ON UPPER SECTION OF INTERCOSTAL AT FWD WET AREA BETWEEN STA 312 AND STA 328 AT RBL 30 IAW NDTM PART 6;51-00-00 PROCEDURE 23. CRACK LENGTH : 0.787' ( AT 12 ANDSDR SWAA2022020356153Floor Panel · distortedFWD CARGO FLOOR PANEL 120CF IS WORN AND DISTORTED ; / [01] FABRICATED FLOOR CARGO PANEL#120CF AT FWD CARGO COMPARTMENT IN REF B737-700 AMM25-52-01-201-801.SDR SWAA2021112947682Slide · failedSUPPLEMENTAL INFORMATION: R1 DOOR SLIDE FALLING OUT OF COVER. ; / [01] REINSTALLED SLIDE PER AMM 25-66-01.SDR SWAA2021112245643Support · crackedLH WING FIXED TRAILING EDGE BULKHEAD SUPPORT IS CRACKED AT LOWER RADIUS THROUGH BOLT HOLE. ; / [01] COMPLETED SRM REPAIR STEPS UP TO AND INCLUDING 57-51-02 4. N.; [02] REMOVED AND REPLACED LH WING FIXED TRAILING EDGE BULKHEAD SUPPORT PER AMM 70-20-02; [03] ENTSDR SWAA2021040558897Attach Angle · crackedL/H A/C BAY; AFT UPPER CORNER OF BAY; BS 662; LBL40.0'; CRACK IN WING CENTER SECTION LOWER SKIN TO BS 663 BULKHEAD ATTACH ANGLE; MARKED IN BLACK / REMOVED CRACKED ATTACH ANGLE STA 663 L/H LBL 65 TO LBL 35 AND REPAIRED IAW SRM 57-10-10-2R-5 APPLIED CIC IAW AMM SDR SWAA2021040658183Attach Angle · crackedEVIDENCE OF CRACK FOUND AT CENTER WING BOX STA 663 RBL 8.5. CTR WING LWR EXT SURFACE. / REPAIRED CENTER WING LOWER EXTERNAL SURFACE VAPOR BARRIER ATTACH ANGLE AT STA 663 RBL 8.5 IAW SRM 57-10-10-2R-5. ACCOMPLISHED LEAK CHECK IAW AMM 28-11-00-400-801. LEAK CHECSDR SWAA2021040558182Bulkhead · crackedBS 663; RBL 45; IN CABIN; CRACK NOTED VISUALY AT HORIZONTAL FLANGE OF CENTER WING TANK UPPER SKIN LOWER CHORD REPAIRED CENTER WING TANK UPPER SKIN LOWER CHORD AT BS 663 RBL 45 IAW AAR EA 210069 IR AND SWA EA 2115700758 REV IRSDR SWAA2021033058308Floorboard · damagedCABIN FLOOR BOARD 241AF FACE SHEET PLY PULLED OFF / REPAIRED CABIN FLOORBOARD 241AF UPPER FACE SHEET PLIES MISSING IAW SRM 53-00-50-2R-1 AND SRM 53-00-50-2R-0 REPAIR GENERALSDR SWAA2021033058307Panel · pulledCABIN FLOOR BOARD 231XF FACE SHEET PLY PULLED OFF / REPAIRED FWD RIGHT CORNER CORE ON PANEL 231XF. IAW B737-700 SRM 53-00-50-2R-10; SRM 53-00-50-2R-0SDR SWAA2021032958309Floorboard · pulledCABIN FLOOR BOARD 232SF FACE SHEET PLY PULLED OFF / REPAIRED DAMAGE TO UPPER SURFACE SHEET ON FLOOR BOARD 232 SF 737-700 SRM 53-00-50-2R-0 REV 72 REPAIR AND SRM 53-00-50-2R-1 REV REPAIR 1. TAP TEST GOODSDR SWAA2021032958303Floorboard · pulledCABIN FLOOR BOARD 241CF FACE SHEET PLY PULLED OFF / REPAIRED CABIN FLOOR BOARD 241CF UPPER FACE SHEET IAW B737 SRM 53-00-50-2R-1SDR SWAA2021032958302Floorboard · pulledCABIN FLOOR BOARD 232RF FACE SHEET PLY PULLED OFF / REPAIRED DAMAGE TO UPPER SURFACE FACE SHEET ON FLOOR BOARD 232 RF 737-700 SRM 53-00-50-2R-0 REV 72 REPAIR GENERAL AND SRM 53-00-50-2R-1 REV 72 REPAIR 1. TAP TEST GOODSDR SWAA2021032558306Floorboard · damagedCABIN FLOOR BOARD 231ZF FACE SHEET PLY PULLED OFF / REPAIRED CABIN BOARD 2312F SHEET PLY PULLED OFF ON UPPER SURFACE IAW SRM 53-00-50-2R11 AND SRM 53-00-50-2R-0 REPAIR GENERALSDR SWAA2021032957300Skin · crackedRH FUSELAGE EXTERNAL POWER RECEPTACAL LOWER CUTOUT AT STA 235.8 ABOVE STR 24R CRACKED AT FASTENER / CUT AND REMOVED DAMAGED PORTION OF ELECTRICAL GROUND POWER RECEPTACLE R/H FUSELAGE LOWER CUTOUT AT STA 235.8 ABOVE STR 24R FABRICATED & INSTALLED REPAIR PARTS ISDR SWAA2020090111980Girt Bar · displacedFORWARD SERVICE DOOR EMERGENCY SLIDE GIRT TO LONG / ATTACHED GRIT PER MT 725-61-06SDR SWAA2020062593570Battery Pack · inoperativeLEFT AFT EMERGENCY EXIT IDENTIFIER LIGHT & CENTER AFT OVER HEAD EMERGENCY LIGHT INOP / R&R BATTERY PACK OPS CK OK REF AMM 33-51-06SDR SWAA2020012940854Motor · inoperativeDECLARED EMERGENCY------------------------------------------------AFTER DEPARTURE OUT OF HRL FIRST OFFICER NOTICED STABILIZER TRIM SWITCH WOULD NOT WORK. CAPTAIN SWITCHES INOPERATIVE. AS WELL. AUTOPILOT TRIM INOPERATIVE. MANUAL TRIM WAS OPERATIVE. COMPLIED WISDR SWAA2020010940295Actuator · failedCROSS FEED FUEL VALVE FAILED OPEN. / R&R FUEL TANK CROSS-FEED VALVE ACTUATOR PER MM.SDR SWAA2020010740240Power Supply · inoperativeR/H AFTER WING EMERGENCY ESCAPE LIGHT INOP. / R&R POWER SUPPLY PER AMM.SDR SWAA2020010740239Power Supply · inoperativeL/H AFTER WING EMERGENCY ESCAPE LIGHT INOP. / R&R POWER SUPPLY PER AMM.SDR SWAA2020010740238Battery Pack · dischargedR/H AFTER WING EMERGENCY ESCAPE LIGHT INOP. / R&R BATTERY PACK PER AMM.SDR SWAA2020010740237Light · inoperativeL2 DOOR EXTERIOR EMERGENCY ESCAPE SLIDE LIGHT INOP. / RELAMPED LIGHT IAW AMM.SDR SWAA2020010740201Battery Pack · dischargedL/H AFTER WING EMERGENCY ESCAPE LIGHT INOP. / R&R BATTERY PACK PER AMM.SDR SWAA2020010740200Light · inoperativeL1 DOOR EXTERIOR EMERGENCY ESCAPE SLIDE LIGHT INOP. / RELAMPED LIGHT IAW AMM.SDR SWAA2020010340160Band · missingAFT FLIGHT ATTENDANT STATION EMERGENCY FLASHLIGHT SECURITY BAND MISSING. / INSTALLED BAND (SHIELD) PER DWG AND SRM.SDR SWAA2022032851232Bracket · crackedFWD CARGO COMPARTMENT L/H FWD OF STA 500A; BETWEEN S-24L AND S-25L BRACKET NOTED CRACKED / REMOVED AND REPLACED BRACKET (CUP) PNO 7531258 AT FWD CARGO L/H FWD STA 500A BETWEEN STR 25L AND STR 24L IRW B737 SRM 51-40-02-0G-0 AND DWD 143A7505SDR SWAA2022032551230Support · crackedAFT CARGO COMPARTMENT AFT OF STA 947.5 BL+10' ABOVE LBL 26L FLOOR ANGLE SUPPORT CRACKED NOTED. / REMOVED AND REPLACED FLOOR ANGLE SUPPORT AT AFT CARGO COMPR. AFT OF STA 947 BT 10' ABOVE LBL 26L PER REF: SRM 51-40-02-0G-0 B737-700.SDR SWAA2022041251226Floorbeam · corroded**CORROSION** FLOOR BEAM STA 328; RBL 44; WL 208.1 / THIS ITEM WAS ACCOMPLISHED ON N/R; S/N W.135684 THIS ITEM NOW CLOSED.SDR SWAA2022041251224Support · corroded***CORROSION*** NOTED ON TEE SUPPORTSURFACE AT AFT CARGO COMPARTMENT STA 772 / REMOVED CORROSION AT AFT CARGO TEE SUPPORT STA 772. MEASURES: ORIGINIAL THICKNESS .070';MINIMUM THICKNESS FOUND .031'. MATERIAL LOST .039' FOUND OUT OF LIMITS.REPLACED TEE SUPPORT PSDR SWAA2022040551217Floor Panel · corrodedCORROSION--AFT CARGO STA 887 FLOOR PANELS SPLICER HAS EVIDENCE OF CORROSION AT SEVERAL ATTACH HOLES / ACCOMPLISHED INSPECTION AT AFT CARGO FLOOR PANEL SPLICER STA 887; FOUND DEEP CORROSION OUT OF LIMITS. REMOVED AND REPLACED FLOOR PANEL TEE SPLICER AS PER REF SDR SWAA2019123040016Floorbeam · corrodedFLOOR BEAM AREA CORRODED AT BS. 328, BETWEEN RBL 43 TO RBL 47. REPAIRED THE FLOORBEAM TEE CAP IAW SRM.
Back to N452WN