# Service difficulty reports: N403YK

A list on [N403YK](https://openairdocs.org/aircraft/N403YK.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 2 · 53 reports

- [SDR NACA2024082700001](https://openairdocs.org/sdr/NACA2024082700001.md): Skin · cracked · Aug 27, 2024 · N403YK · Boeing 737436 · Fuselage Main, Plate/Skin
  > WHILE 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.
- [SDR NACA2024022100005](https://openairdocs.org/sdr/NACA2024022100005.md): Seat Track · cracked · Feb 21, 2024 · N403YK · Boeing 737436 · Fuselage, Seat/Cargo Attach Fittings
  > PILOT 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 2024
- [SDR NACA2024022100004](https://openairdocs.org/sdr/NACA2024022100004.md): Battery · discharged · Feb 21, 2024 · N403YK · Boeing 737436 · Emergency Lighting
  > RECHARGE 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 REV98
- [SDR NACA2024022100003](https://openairdocs.org/sdr/NACA2024022100003.md): Battery Pack · discharged · Feb 21, 2024 · N403YK · Boeing 737436 · Emergency Lighting
  > RECHARGE 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 REV98
- [SDR NACA2024020600002](https://openairdocs.org/sdr/NACA2024020600002.md): Skin · cracked · Feb 6, 2024 · N403YK · Boeing 737436 · Leading Edge Devices
  > THE 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 65C26603
- [SDR NACA2024020200002](https://openairdocs.org/sdr/NACA2024020200002.md): Skin · cracked · Feb 2, 2024 · N403YK · Boeing 737436 · Fuselage Main, Plate/Skin
  > ACCORDING 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. IR
- [SDR NACA2024020100005](https://openairdocs.org/sdr/NACA2024020100005.md): Web · cracked · Feb 1, 2024 · N403YK · Boeing 737436 · Fuselage Miscellaneous Structure
  > A 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-
- [SDR NACA2024020100004](https://openairdocs.org/sdr/NACA2024020100004.md): Skin · dented · Feb 1, 2024 · N403YK · Boeing 737436 · Fuselage Main, Plate/Skin
  > DENT (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 EO737-53-0336
- [SDR NACA2024013000002](https://openairdocs.org/sdr/NACA2024013000002.md): Skin · corroded · Jan 30, 2024 · N403YK · Boeing 737436 · Wing, Plate/Skin
  > DURING 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
- [SDR NACA2024012900004](https://openairdocs.org/sdr/NACA2024012900004.md): Skin · dented · Jan 29, 2024 · N403YK · Boeing 737436 · Horizontal Stabilizer, Plate/Skin
  > DENT ( 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)
- [SDR NACA2024012900003](https://openairdocs.org/sdr/NACA2024012900003.md): Torque Box · corroded · Jan 29, 2024 · N403YK · Boeing 737436 · APU Cowling/Containment
  > CORROSION 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 R115
- [SDR NACA2024012900002](https://openairdocs.org/sdr/NACA2024012900002.md): Skin · dented · Jan 29, 2024 · N403YK · Boeing 737436 · Leading Edge Devices
  > THE 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.W
- [SDR NACA2024012900001](https://openairdocs.org/sdr/NACA2024012900001.md): Skin · cracked · Jan 29, 2024 · N403YK · Boeing 737436 · Leading Edge Devices
  > THE 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 65C26601
- [SDR NACA2024012600005](https://openairdocs.org/sdr/NACA2024012600005.md): Retainer · corroded · Jan 26, 2024 · N403YK · Boeing 737436 · Fuselage Main, Structure
  > OVERWING 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.
- [SDR NACA2024012600004](https://openairdocs.org/sdr/NACA2024012600004.md): Retainer · corroded · Jan 26, 2024 · N403YK · Boeing 737436 · Fuselage Main, Structure
  > OVERWING 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. P
- [SDR NACA2024012600003](https://openairdocs.org/sdr/NACA2024012600003.md): Retainer · corroded · Jan 26, 2024 · N403YK · Boeing 737436 · Fuselage Main, Structure
  > OVERWING 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
- [SDR NACA2024012400002](https://openairdocs.org/sdr/NACA2024012400002.md): Skin · debonded · Jan 24, 2024 · N403YK · Boeing 737436 · Trailing Edge Flaps
  > RH 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 & SR
- [SDR NACA2023120700006](https://openairdocs.org/sdr/NACA2023120700006.md): Unknown · unknown · Dec 7, 2023 · N403YK · Boeing 737436 · Air Distribution System
  > IN 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.
- [SDR NACA202304070001](https://openairdocs.org/sdr/NACA202304070001.md): Unknown · unknown · Apr 7, 2023 · N403YK · Boeing 737 · Fuselage Structure (General)
  > 1.5 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.
- [SDR NACA2022082200002](https://openairdocs.org/sdr/NACA2022082200002.md): None · intermittent · Aug 22, 2022 · N403YK · Boeing 737 · Cabin Pressure Controller
  > AUTO 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 21-31-21
- [SDR DU4R2020061800049](https://openairdocs.org/sdr/DU4R2020061800049.md): Frame · cracked · Jun 18, 2020 · N403YK · Boeing 737436 · Fuselage Main, Frame
  > AD 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 STR10L
- [SDR DU4R2020061600047](https://openairdocs.org/sdr/DU4R2020061600047.md): Skin · cracked · Jun 16, 2020 · N403YK · Boeing 737436 · Fuselage Main, Plate/Skin
  > AIR STAIR DOOR CUTOUT AROUND FWD UPPER HOLE NR 8 WAS CRACKED.
- [SDR DU4R2020061500046](https://openairdocs.org/sdr/DU4R2020061500046.md): Frame · cracked · Jun 15, 2020 · N403YK · Boeing 737436 · Fuselage Main, Frame
  > BS360 BETWEEN STR25L AND STR27 6 EACH FASTENER HOLES PRODUCED REJECTABLE INDICATIONS DURING ABHEC INSPECTION. ALL APPLICABLE DISCREPANT HOLES MARKED
- [SDR DU4R2020061500045](https://openairdocs.org/sdr/DU4R2020061500045.md): Attach Fitting · cracked · Jun 15, 2020 · N403YK · Boeing 737436 · Wing, Landing Gear Attach Fittings
  > LEFT 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 2
- [SDR DU4R20200615045](https://openairdocs.org/sdr/DU4R20200615045.md): Floor Support · corroded · Jun 15, 2020 · N403YK · Boeing 737436 · Fuselage Miscellaneous Structure
  > FORWARD LOWER CARGO COMPARTMENT R/H SIDE STR 26R FLOOR SUPPORT PROFILE HAS CORROSION BETWEEN BS 520-540
- [SDR DU4R2020061500044](https://openairdocs.org/sdr/DU4R2020061500044.md): Floor Support · corroded · Jun 15, 2020 · N403YK · Boeing 737436 · Fuselage Miscellaneous Structure
  > FORWARD LOWER CARGO COMPARTMENT LT SIDE STR 26L FLOOR SUPPORT PROFILE HAS CORROSION BETWEEN BS 500D-520.
- [SDR DU4R2020061500043](https://openairdocs.org/sdr/DU4R2020061500043.md): Support · corroded · Jun 15, 2020 · N403YK · Boeing 737436 · Fuselage Miscellaneous Structure
  > FORWARD LOWER CARGO COMPARTMENT LH SIDE SIDEWALL SUPPORT HAS CORROSION AT BS 500C
- [SDR DU4R2020061400042](https://openairdocs.org/sdr/DU4R2020061400042.md): Structure · cracked · Jun 14, 2020 · N403YK · Boeing 737436 · Fuselage Main, Structure
  > AD2016-13-11 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 HOLES
- [SDR DU4R2020061000041](https://openairdocs.org/sdr/DU4R2020061000041.md): Fitting · cracked · Jun 10, 2020 · N403YK · Boeing 737436 · Wing, Landing Gear Attach Fittings
  > AD 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.
- [SDR DU4R2020061000040](https://openairdocs.org/sdr/DU4R2020061000040.md): Attach Fitting · cracked · Jun 10, 2020 · N403YK · Boeing 737436 · Wing, Landing Gear Attach Fittings
  > AD 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.
- [SDR DU4R2020061000039](https://openairdocs.org/sdr/DU4R2020061000039.md): Skin · cracked · Jun 10, 2020 · N403YK · Boeing 737436 · Galley Doors
  > AFT 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 BLACK
- [SDR DU4R2020052800038](https://openairdocs.org/sdr/DU4R2020052800038.md): Frame · cracked · May 28, 2020 · N403YK · Boeing 737436 · Fuselage Main, Frame
  > MAIN CARGO, RT FR360 FOUND CRACK AT STR 13R.
- [SDR DU4R2020052800037](https://openairdocs.org/sdr/DU4R2020052800037.md): Shear Tie · cracked · May 28, 2020 · N403YK · Boeing 737436 · Fuselage Internal Mounting Structure
  > AD 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.
- [SDR DU4R2020052000035](https://openairdocs.org/sdr/DU4R2020052000035.md): Frame Angle · corroded · May 20, 2020 · N403YK · Boeing 737436 · Fuselage Main, Frame
  > AD 2019-15-07 AFT CARGO COMPARTMENT L/H FRAME AT BS727D UPPER SURFACE ON ANGLE ASSY CORRODED AT SEVERAL LOCATIONS FROM
- [SDR DU4R2020052000033](https://openairdocs.org/sdr/DU4R2020052000033.md): Floorbeam · corroded · May 20, 2020 · N403YK · Boeing 737436 · Fuselage Main, Floor Beam
  > FORWARD LOWER CARGO COMPARTMENT FLOOR BEAM BETWEEN STR 26L-27L HAS CORROSION JUST FWD OF AFT BULKHEAD
- [SDR DU4R2020051900032](https://openairdocs.org/sdr/DU4R2020051900032.md): Baffle · cracked · May 19, 2020 · N403YK · Boeing 737436 · Fuselage Miscellaneous Structure
  > LH BAFFLE BETWEEN 400D AND 500E CRACKED AT STRINGER 26L
- [SDR DU4R2020051900031](https://openairdocs.org/sdr/DU4R2020051900031.md): Support Web · cracked · May 19, 2020 · N403YK · Boeing 737436 · Fuselage Miscellaneous Structure
  > LH TRANSITION PANEL SUPPORT WEB AT STR 26L BETWEEN BS 400-420 CRACKED
- [SDR DU4R2020051900030](https://openairdocs.org/sdr/DU4R2020051900030.md): Baffle · cracked · May 19, 2020 · N403YK · Boeing 737436 · Fuselage Miscellaneous Structure
  > BAFFLE CRACKED BETWEEN FR STATION 500E AND 500F AT STRINGER 26L FWD CARGO PIT
- [SDR DU4R2020051900029](https://openairdocs.org/sdr/DU4R2020051900029.md): Stringer Clip · cracked · May 19, 2020 · N403YK · Boeing 737436 · Fuselage Main, Attach Fittings
  > AD 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 S10L
- [SDR DU4R2020051900028](https://openairdocs.org/sdr/DU4R2020051900028.md): Stringer Clip · cracked · May 19, 2020 · N403YK · Boeing 737436 · Fuselage Main, Attach Fittings
  > AD 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 S10L
- [SDR DU4R2020051900027](https://openairdocs.org/sdr/DU4R2020051900027.md): Channel · corroded · May 19, 2020 · N403YK · Boeing 737436 · Fuselage Miscellaneous Structure
  > FORWARD LOWER CARGO COMPARTMENT L/H SIDE STR 26L FLOOR SUPPORT SIDE PLATE HAS CORROSION BETWEEN B.S 500B-500C
- [SDR DU4R2020051900026](https://openairdocs.org/sdr/DU4R2020051900026.md): Baffle · cracked · May 19, 2020 · N403YK · Boeing 737436 · Fuselage Miscellaneous Structure
  > CRACKED BAFFLE IN FWD PIT COMP BETWEEN BS 460-480 STR 26L
- [SDR DU4R2020051900025](https://openairdocs.org/sdr/DU4R2020051900025.md): Intercostal · cracked · May 19, 2020 · N403YK · Boeing 737436 · Fuselage Miscellaneous Structure
  > FUSELAGE 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.
- [SDR DU4R2020051900024](https://openairdocs.org/sdr/DU4R2020051900024.md): Gusset · gouged · May 19, 2020 · N403YK · Boeing 737436 · Auxiliary Power Unit (APU) Doors
  > APU DOOR INNER SURFACE GUSSET AND CENTER HINGE SUPPORT GOUGED
- [SDR DU4R2020051900023](https://openairdocs.org/sdr/DU4R2020051900023.md): Stringer Clip · cracked · May 19, 2020 · N403YK · Boeing 737436 · Fuselage Main, Attach Fittings
  > AD 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 16R
- [SDR DU4R2020051900022](https://openairdocs.org/sdr/DU4R2020051900022.md): Stringer Clip · cracked · May 19, 2020 · N403YK · Boeing 737436 · Fuselage Main, Attach Fittings
  > AD 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 15R
- [SDR DU4R2020051900021](https://openairdocs.org/sdr/DU4R2020051900021.md): Stringer Clip · cracked · May 19, 2020 · N403YK · Boeing 737436 · Fuselage Main, Attach Fittings
  > AD 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.
- [SDR DU4R202005190020](https://openairdocs.org/sdr/DU4R202005190020.md): Stringer Clip · cracked · May 19, 2020 · N403YK · Boeing 737436 · Fuselage Main, Attach Fittings
  > AD 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.
- [SDR DU4R2020051900019](https://openairdocs.org/sdr/DU4R2020051900019.md): Stringer Clip · cracked · May 19, 2020 · N403YK · Boeing 737436 · Fuselage Main, Attach Fittings
  > FUSELAGE FWD OF R1 DOOR, STRINGER CLIP AT STR 10R, FWD SIDE OF FRAME BS 277 HAS CRACK REPAIR IN CONJUNCTION WITH SB 737-53A1241.
- [SDR DU4R2020051900018](https://openairdocs.org/sdr/DU4R2020051900018.md): Support Plate · corroded · May 19, 2020 · N403YK · Boeing 737436 · Fuselage Miscellaneous Structure
  > FORWARD LOWER CARGO COMPARTMENT RT SIDE STR26R FLOOR SIDE PLATE HAS CORROSION APPROX 6" FWD BS 500D.

Next page: https://openairdocs.org/aircraft/N403YK/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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
```

This list as a web page: https://openairdocs.org/aircraft/N403YK/reports

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