N403YK

Service difficulty reports · 53

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 = 'N403YK' 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.

SDR NACA2024082700001Skin · crackedWHILE PERFORMING A DVI FOR AN UNRELATED EO, FOUND A 7/8 INCH FUSELAGE SKIN CRACK BELOW STR 22L AND BS 7278+2 3/8, CONFIRMED WITH EDDY CURRENT. ACCOMPLISHED EO 737-53-0360, REFERENCE ATTACHED PROJECT WORKSHEET.Aug 27, 2024 · N403YK · Boeing 737436 · Fuselage Main, Plate/SkinSDR NACA2024022100005Seat Track · crackedPILOT SEAT TRACK CRACK ON  FWD INBORD, LOCATED END OF TRACK AROUND FWD STOP SCREW HOLE. 1. REMOVE PILOT SEAT CRACK TRACK 2. INSTALL PILOT SEAT NEW TRACK COMPLETED REF: AMM 53-42-00 P1. 20-50-11 PAGE 201 R98 PME: 006162 DUE DATE: JUL 06 2024Feb 21, 2024 · N403YK · Boeing 737436 · Fuselage, Seat/Cargo Attach FittingsSDR NACA2024022100004Battery · dischargedRECHARGE EMERGENCY LIGHTS BATTERY PACKS , FOUND EMERGENCY LIGHTS BATTERY PACK MALFUNCTION , PACK:M01133. REPLACE THE EMER BATTERY PACK AND TEST NORMAL REF AMM 33-51-51-962-015 REV98Feb 21, 2024 · N403YK · Boeing 737436 · Emergency LightingSDR NACA2024022100003Battery Pack · dischargedRECHARGE EMERGENCY LIGHTS BATTERY PACKS , FOUND EMERGENCY LIGHTS BATTERY PACK MALFUNCTION , PACK:M01132. REPLACE THE EMER BATTERY PACK AND TEST NORMAL REF AMM 33-51-51-962-015 REV98Feb 21, 2024 · N403YK · Boeing 737436 · Emergency LightingSDR NACA2024020600002Skin · crackedTHE CRACK WAS FOUND AT #3 SLAT OUTER SKIN SS.S. 88.4 AND S.S. 94.4 AREA. PERFORMED REPAIR AT #3 SLAT OUTER SKIN 55.88.4 & 94.4 AREA. I.A.W. B737-400 SSRM 57-43-01 REPAIR 6 PAGE 201-205 (REV.115) & DMG 65C26603Feb 6, 2024 · N403YK · Boeing 737436 · Leading Edge DevicesSDR NACA2024020200002Skin · crackedACCORDING TO AD 2019-08-03 INTERNAL OPEN HOLE HFEC INSPECTION , 2 EA FASTENERS HOLE SKIN CRACKED(UP L: 0.4" LOWER L:0.35") AT BS380 IB CHORD BETWEEN S20L AND S21L. REPAIRED DAMAGED CHORD AT BS 380L BETWEEN STRANGER S21 & S22 AS PER NAC EO 737-53-3507 REV. IRFeb 2, 2024 · N403YK · Boeing 737436 · Fuselage Main, Plate/SkinSDR NACA2024020100005Web · crackedA CRACK AT WEB FASTERNER HOLE, STA 710 LBL 0.07, LENTH:0.250". 1. REMOVE THE STIFFENER & FILLER 2. CUT-OUT THE WEB FROM DAMAGED AREA 3. INSTALL REPAIR KIT (NEW, DOACER & WEB) 4. ALL ASSY REINSTALL WITH SEALANT PER: SB 737-57-1210 FIG 5 PAGE 86, PEMCO EA PD 37-Feb 1, 2024 · N403YK · Boeing 737436 · Fuselage Miscellaneous StructureSDR NACA2024020100004Skin · dentedDENT (3.2" X 2.0" IN AREA, MAX. DEPTH= 0.080") AT BS STA 1148, RBL+4". PERFORM PERMANENT REPAIR AT BS STA 1148 RBL+4" PER NAC EO737-53-0336Feb 1, 2024 · N403YK · Boeing 737436 · Fuselage Main, Plate/SkinSDR NACA2024013000002Skin · corrodedDURING NRC:CA1528/152 , CORROSION WAS FOUND AT LH WING UPPER SURFACE , WBL79 , S-11 AREA. REMOVED CORROSION LEVEL 2 AT LH WING UPPER SURFACE WBL 83,S11 AREA FROM P/N 65C25204-15 ORIGINAL THICKNESS 0.160" REMOVES 0.028"AND REMAINING THICKNESS IS 0.132" IS OVER Jan 30, 2024 · N403YK · Boeing 737436 · Wing, Plate/SkinSDR NACA2024012900004Skin · dentedDENT ( 7.0" X 2.0" IN AREA, MAX DEPTH =0.120") AT RH HROIZONTAL STABILIZER LEADING EDGE AT STAB STA 186~193. PERFORMED PERMANENT REPAIR AT RH HORIZONTAL STABILIZER LEADING EDGE AT STAB STA 186~190 CATEGORY A PER: 737-400 SRM 55-70-01 REPAIR 3 (R115)Jan 29, 2024 · N403YK · Boeing 737436 · Horizontal Stabilizer, Plate/SkinSDR NACA2024012900003Torque Box · corrodedCORROSION AT APU RH SIDE LOWER TORQUE BOX AT STA 1126. TEE ANGLE REPLACED AT APU RH SIDE LOWER TORQUE BOX AT STA 1126 PER: DRAWING 65-46579 SHEET 4 #531, SRM 51-40-02 PARA 4 R115Jan 29, 2024 · N403YK · Boeing 737436 · APU Cowling/ContainmentSDR NACA2024012900002Skin · dentedTHE DENT WAS FOUND AT #3 SLAT OUTER SKIN S.S.55 AREA , L:2.6 INCH , W:1.3 INCH , Y (DEPTH OF DENT) :0.076 INCH . PER SRM 57-43-01 ALLOWABLE DAMAGE 1 , A/Y: 1.3/0.076=17.1 , OVER LIMIT. PERFORMED REPAIR AT #3 SLAT OUTER SKIN 5.5.55 AREA, 2:2.6", W:1.3". I.A.WJan 29, 2024 · N403YK · Boeing 737436 · Leading Edge DevicesSDR NACA2024012900001Skin · crackedTHE CRACK WAS FOUND AT #1 SLAT OUTER SKIN S.S.299.53 ,L:0.1 INCH. PERFORMED REPAIR AT #1 SLAT OUTER SKIN 5.5.299.53, L: 0.1INCH. I.A.W.B737-400 SRM 57-43-01 REPAIR 6 PAGE 201-205 (REV.115) & DWG 65C26601Jan 29, 2024 · N403YK · Boeing 737436 · Leading Edge DevicesSDR NACA2024012600005Retainer · corrodedOVERWING ENERGENCY HATCH SEAL RETAINER HAS BEEN CORRODED AROUND LOWER PORTION OF THE DOOR. RH FWD(2415R). 1. CORROSION REMOVED. THE SEAL RETAINER AND LOWER PORTION WERE OVER LIMIT 2. CUT-OUT THE DAMAGED AREA AND MADE REPAIR PARTS AND INSTALL WITH SEALANT. 3. Jan 26, 2024 · N403YK · Boeing 737436 · Fuselage Main, StructureSDR NACA2024012600004Retainer · corrodedOVERWING ENERGENCY HATCH SEAL RETAINER HAS BEEN CORRODED AROUND LOWER PORTION OF THE DOOR. LH FWD(2414L). 1. CORROSION REMOVED. THE DOOR LOWER PORTION & SEAL RETAINER WERE OVER LIMIT. 2. CUT OUT THE DAMAGED AREA & MADE REPAIR PARTS AND INSTALL WITH SEALANT. PJan 26, 2024 · N403YK · Boeing 737436 · Fuselage Main, StructureSDR NACA2024012600003Retainer · corrodedOVERWING ENERGENCY HATCH SEAL RETAINER HAS BEEN CORRODED AROUND LOWER PORTION OF THE DOOR. LH AFT(2403L). OVERWING EMERGENCY HATCH SEAL RETAINER HAS BEEN CORRODED AROUND LOWER PORTION OF THE DOOR, RH AFT (2404R). 1. CORROSION REMOVED. THE DOOR LOWER PORTION Jan 26, 2024 · N403YK · Boeing 737436 · Fuselage Main, StructureSDR NACA2024012400002Skin · debondedRH WING O/B AFT FLAP DISBOND BETWEEN WBL.230.68 ~ WBL.234.68 .(L:4 INCH , W:0.3 INCH). PERFORMED CATEGORY A REPAIR OF A DISBOND AT THE EDGE OF ALUM HONEYCOMB STRUCTURE, RH WING O/B AFT FLAP BETWEEN WBL 230.68~WBL 234.68 I.A.W. B737-400 SRM 57-53-02-2R-2 & SRJan 24, 2024 · N403YK · Boeing 737436 · Trailing Edge FlapsSDR NACA2023120700006Unknown · unknownIN FLIGHT 2020Z AT FL360 SMOKE IN CABIN. DECLARED EMERGENCY WITH ATC ASK FOR DIRECT KRFD. LF RECIRC FAN FOUND SHORTING AND POPPING CIRCUIT BREAKER. DEFERRED LH RECIRC FAN PER MEL 21-31-05.Dec 7, 2023 · N403YK · Boeing 737436 · Air Distribution SystemSDR NACA202304070001Unknown · unknown1.5 INCH CRACK FOUND IN FUSELAGE SKIN @ STR 23L EIGHT INCHES FORWARD OF BS 727E. INSTALLED REPAIR IN LOCATION GIVEN IAW BOEING SRM 53-00-01 REPAIR 31. SEE PROJECT WORKSHEET FOR DETAILS.Apr 7, 2023 · N403YK · Boeing 737 · Fuselage Structure (General)SDR NACA2022082200002None · intermittentAUTO FAIL LIGHT ILLUMINATED AND CABIN ALT EXCEEDED 10000 FT. REPLACED CABIN PRESSURE MAIN OUTFLOW VALVE REF BOEING 737-400 AMM 21-31-11. FINAL FIX: REPLACED CABIN PRESSURE CONTROLLER REF B737-400 AMM 21-31-21Aug 22, 2022 · N403YK · Boeing 737 · Cabin Pressure ControllerSDR DU4R2020061800049Frame · crackedAD 2019-08-02(H): TABLE 2 / PART 2 AND BOEING SB 737-53A1360,IR,PART 2 INSPECTION FIGURE 7,8,13 AND 14, FORWARD SIDE OF FRAME WEB HAS A CRACK RUNNING OUTBOARD FROM FASTENER HOLE 1/4" LONG BS 500E JUST BELOW STR10LJun 18, 2020 · N403YK · Boeing 737436 · Fuselage Main, FrameSDR DU4R2020061600047Skin · crackedAIR STAIR DOOR CUTOUT AROUND FWD UPPER HOLE NR 8 WAS CRACKED.Jun 16, 2020 · N403YK · Boeing 737436 · Fuselage Main, Plate/SkinSDR DU4R2020061500046Frame · crackedBS360 BETWEEN STR25L AND STR27 6 EACH FASTENER HOLES PRODUCED REJECTABLE INDICATIONS DURING ABHEC INSPECTION. ALL APPLICABLE DISCREPANT HOLES MARKEDJun 15, 2020 · N403YK · Boeing 737436 · Fuselage Main, FrameSDR DU4R2020061500045Attach Fitting · crackedLEFT MLG BEAM FORWARD SUPPORT FITTING FASTENER HOLE MARKED AS #16 CRACKED AT 1:00. THOUGHT TO BE IN THE WEB LAYER. BOEING SERVICE BULLETIN 737-57A1334,IR, PARAGRAPH 3.B PART 2Jun 15, 2020 · N403YK · Boeing 737436 · Wing, Landing Gear Attach FittingsSDR DU4R20200615045Floor Support · corrodedFORWARD LOWER CARGO COMPARTMENT R/H SIDE STR 26R FLOOR SUPPORT PROFILE HAS CORROSION BETWEEN BS 520-540Jun 15, 2020 · N403YK · Boeing 737436 · Fuselage Miscellaneous StructureSDR DU4R2020061500044Floor Support · corrodedFORWARD LOWER CARGO COMPARTMENT LT SIDE STR 26L FLOOR SUPPORT PROFILE HAS CORROSION BETWEEN BS 500D-520.Jun 15, 2020 · N403YK · Boeing 737436 · Fuselage Miscellaneous StructureSDR DU4R2020061500043Support · corrodedFORWARD LOWER CARGO COMPARTMENT LH SIDE SIDEWALL SUPPORT HAS CORROSION AT BS 500CJun 15, 2020 · N403YK · Boeing 737436 · Fuselage Miscellaneous StructureSDR DU4R2020061400042Structure · crackedAD2016-13-11 RELATED, UPON FASTENER REMOVAL TO ACCOMPLISH PREVENTIVE MOD AT BS727 FOUND CRACKS GOUGES AND OUT OF ROUND HOLES AT LBL 24.82, LBL 45.57,RBL 24.82 AND RBL 45.57 TOTALING 10 EA HOLESJun 14, 2020 · N403YK · Boeing 737436 · Fuselage Main, StructureSDR DU4R2020061000041Fitting · crackedAD 2018-09-13(H): TABLE 8/OPTION 1: SERVICE BULLETIN 737-57A1318, R1, PARA 3B PART 3A1, LEFT MLG FORWARD SUPPORT FITTING, AFT SUPPORT FITTING, REAR SPAR UPPER CHORD AND REAR SPAR WEB HOLE 5 IS CRACKED IN THE AFT FITTING AT 600 AND IN THE WEN AT 1:00.Jun 10, 2020 · N403YK · Boeing 737436 · Wing, Landing Gear Attach FittingsSDR DU4R2020061000040Attach Fitting · crackedAD 2018-09-13(H): TABLE 8 / OPTION 1: RT MLG FORWARD FITTING, AFT SUPPORT FITTING, REAR SPAR UPPER CHORD AND REAR WEB, IAW SB 737-57A1318,R1 PARA 3B PART 3 STEP 3A1, HOLE 4 AND 5 ARE CRACKED IN THE AFT FTG AND IN THE UPPER SPAR CHORD.Jun 10, 2020 · N403YK · Boeing 737436 · Wing, Landing Gear Attach FittingsSDR DU4R2020061000039Skin · crackedAFT GALLEY DOOR, FWD LWR CORNER HAS CRACK, EMANATES FROM EDGE, TRAVELS DOWN TO 5TH FASTENER HOLE IN NDT INSPECTION AREA ( SEE SB 737-53A1350 FIG 8) THEN COMES OUT OF THAT HOLE AND TRAVELS DOWN/FWD S INSIDE HOLE,AS MARKED IN BLACKJun 10, 2020 · N403YK · Boeing 737436 · Galley DoorsSDR DU4R2020052800038Frame · crackedMAIN CARGO, RT FR360 FOUND CRACK AT STR 13R.May 28, 2020 · N403YK · Boeing 737436 · Fuselage Main, FrameSDR DU4R2020052800037Shear Tie · crackedAD 2019-08-02(H): TABLE 3/:PART 3: SB 737-53A1360, IR, PART 3, CABIN BS 360 FRAME TO BODY SHEAR TIE OUTBOARD FLANGE IS CRACKED AT STRINGER 15.May 28, 2020 · N403YK · Boeing 737436 · Fuselage Internal Mounting StructureSDR DU4R2020052000035Frame Angle · corrodedAD 2019-15-07 AFT CARGO COMPARTMENT L/H FRAME AT BS727D UPPER SURFACE ON ANGLE ASSY CORRODED AT SEVERAL LOCATIONS FROMMay 20, 2020 · N403YK · Boeing 737436 · Fuselage Main, FrameSDR DU4R2020052000033Floorbeam · corrodedFORWARD LOWER CARGO COMPARTMENT FLOOR BEAM BETWEEN STR 26L-27L HAS CORROSION JUST FWD OF AFT BULKHEADMay 20, 2020 · N403YK · Boeing 737436 · Fuselage Main, Floor BeamSDR DU4R2020051900032Baffle · crackedLH BAFFLE BETWEEN 400D AND 500E CRACKED AT STRINGER 26LMay 19, 2020 · N403YK · Boeing 737436 · Fuselage Miscellaneous StructureSDR DU4R2020051900031Support Web · crackedLH TRANSITION PANEL SUPPORT WEB AT STR 26L BETWEEN BS 400-420 CRACKEDMay 19, 2020 · N403YK · Boeing 737436 · Fuselage Miscellaneous StructureSDR DU4R2020051900030Baffle · crackedBAFFLE CRACKED BETWEEN FR STATION 500E AND 500F AT STRINGER 26L FWD CARGO PITMay 19, 2020 · N403YK · Boeing 737436 · Fuselage Miscellaneous StructureSDR DU4R2020051900029Stringer Clip · crackedAD 2019-08-02(H): TABLE 2/PART 2 AND BOEING SB 737-53A1360,IR PART 2 INSPECTION FIGURE 7,8,13 AND 14. STRINGER CLIP IS CRACKED AFT SIDE OF FRAME BS727B S10LMay 19, 2020 · N403YK · Boeing 737436 · Fuselage Main, Attach FittingsSDR DU4R2020051900028Stringer Clip · crackedAD 2019-08-02(H):TABLE 2 /PART 2 AND BOEING SB 737-53A1360,IR, PART 2 INSPECTION FIGURE 7,8,13 AND 14, STRINGER CLIP IS CRACKED UPPER AND LOWER FLANGES AFT SIDE OF FRAME BS 500D S10LMay 19, 2020 · N403YK · Boeing 737436 · Fuselage Main, Attach FittingsSDR DU4R2020051900027Channel · corrodedFORWARD LOWER CARGO COMPARTMENT L/H SIDE STR 26L FLOOR SUPPORT SIDE PLATE HAS CORROSION BETWEEN B.S 500B-500CMay 19, 2020 · N403YK · Boeing 737436 · Fuselage Miscellaneous StructureSDR DU4R2020051900026Baffle · crackedCRACKED BAFFLE IN FWD PIT COMP BETWEEN BS 460-480 STR 26LMay 19, 2020 · N403YK · Boeing 737436 · Fuselage Miscellaneous StructureSDR DU4R2020051900025Intercostal · crackedFUSELAGE FWD OF R1 DOOR AT STR 14R ADJACENT TO FRAME BS 277 HAS CRACK IN ITS FWD RADIUS TRIM OUT. REPAIR IN CONJUNCTION WITH SB 737-53A1241.May 19, 2020 · N403YK · Boeing 737436 · Fuselage Miscellaneous StructureSDR DU4R2020051900024Gusset · gougedAPU DOOR INNER SURFACE GUSSET AND CENTER HINGE SUPPORT GOUGEDMay 19, 2020 · N403YK · Boeing 737436 · Auxiliary Power Unit (APU) DoorsSDR DU4R2020051900023Stringer Clip · crackedAD 2019-08-02(H): TABLE 3 /PART3: BOEING SB 737-53A1360,IR, PART 3. CABIN B>S. 420 FORWARD SIDE OF FRAME STRINGER CLIP UPR HORIZ FLANGE AFT FASTENER HOLE IS CRACKED AT STRINGER 16RMay 19, 2020 · N403YK · Boeing 737436 · Fuselage Main, Attach FittingsSDR DU4R2020051900022Stringer Clip · crackedAD 2019-08-02(H): TABLE 3/ PART 3: BOEING SB 737-53A1360,IR,PART 3. CABIN B.S 380 FORWARD SIDE OF FRAME STRINGER CLIP UPR HORIZ. FLANGE AFT FASTENER HOLE IS CRACKED AT STRINGER 15RMay 19, 2020 · N403YK · Boeing 737436 · Fuselage Main, Attach FittingsSDR DU4R2020051900021Stringer Clip · crackedAD 2019-08-02(H)TABLE 3/PART 3: SB 737-53A1360 IR PART 3. CABIN BS 440 FORWARD SIDE OF FRAME STRINGER CLIP LWR HORIZ FLANGE AFT FASTENER HOLE IS CRACKED AT STRINGER 16R.May 19, 2020 · N403YK · Boeing 737436 · Fuselage Main, Attach FittingsSDR DU4R202005190020Stringer Clip · crackedAD 2019-08-02(H): TABLE 2 / PART 2 AND SB 737-53A1360 IR PART 2 INSPECTION FIGURE 7,8,13 AND 14. STRINGER CLIP IS CRACKED HORIZONTAL FLANGE AFT HOLE S16L FORWARD SIDE OF FRAME BS767.May 19, 2020 · N403YK · Boeing 737436 · Fuselage Main, Attach FittingsSDR DU4R2020051900019Stringer Clip · crackedFUSELAGE FWD OF R1 DOOR, STRINGER CLIP AT STR 10R, FWD SIDE OF FRAME BS 277 HAS CRACK REPAIR IN CONJUNCTION WITH SB 737-53A1241.May 19, 2020 · N403YK · Boeing 737436 · Fuselage Main, Attach FittingsSDR DU4R2020051900018Support Plate · corrodedFORWARD LOWER CARGO COMPARTMENT RT SIDE STR26R FLOOR SIDE PLATE HAS CORROSION APPROX 6" FWD BS 500D.May 19, 2020 · N403YK · Boeing 737436 · Fuselage Miscellaneous Structure
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