# Service difficulty reports: Boeing 737-330

A list on [Boeing 737-330](https://openairdocs.org/model/boeing-737-330.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 9 · 430 reports

- [SDR TSAA2026081700001](https://openairdocs.org/sdr/TSAA2026081700001.md): Cabin Press Sys · faulted · Aug 18, 2026 · N301KH · Boeing 737330 · Cabin Pressure Control System
  > AT 1000 FT ON CLIMB OUT AUTO FAIL LIGHT ILLUMINATE AND STANDBY LIGHT ILLUMINATE CLIMB RATE PASS 3000FT/MIN DRIVE CABIN PRESS BELOW SEA LEVEL
- [SDR NACA2025031300002](https://openairdocs.org/sdr/NACA2025031300002.md): Inlet · corroded · Mar 13, 2025 · N304KH · Boeing 737330 · Nacelle/Pylon, Main Frame
  > CORROSION WAS FOUND AT #1 ENG INLET COWL FACE SHEET- INNER SKIN BETWEEN 5 O'CLOCK AND 6 O'CLOCK AREA, L:1.4 INCH, W:3.0 INCH. REPLACED NO. 1 ENG INLET CPWL REF B737 AMM 71-11-01-004-001-C00, REV 100 PME:005115 DATE DUE:MAR.26.2025 200~1000 IN-1BF
- [SDR TSAA2024112600026](https://openairdocs.org/sdr/TSAA2024112600026.md): Skin · corroded · Nov 23, 2024 · N301KH · Boeing 737330 · Fuselage Main, Plate/Skin
  > CORROSION AT LH SIDE FUSELAGE EXTERNAL SKIN AT STA 1088, S-5L~S-6L. CORROSION REMOVED LEVEL 1 AT 1088, S-5L~S-6L FROM PN 65-46882-1 ORIGINAL THICKNESS 0.064" REMOVED 0.002" AND REMAINING THICKNESS IS 0.062 AND IS WITHIN LIMITS PER SRM 53-00-01 ALLOWABLE DAMA
- [SDR TSAA2024112600025](https://openairdocs.org/sdr/TSAA2024112600025.md): Skin · corroded · Nov 23, 2024 · N301KH · Boeing 737330 · Fuselage Main, Plate/Skin
  > CORROSION AT LH SIDE FUSELAGE EXTERNAL SKIN AT STA 1088, S-2L~S-4L. CORROSION REMOVED LEVEL 1 AT STA 1088, S-2L~S-4L FROM PN 65-46882-1 ORIGINAL THICKNESS 0.071" REMOVED 0.001" AND REMAINING THICKNESS IS 0.070 AND IS WITHIN LIMITS PER SRM 53-00-01 ALLOWABLE D
- [SDR TSAA2024112600024](https://openairdocs.org/sdr/TSAA2024112600024.md): Skin · corroded · Nov 23, 2024 · N301KH · Boeing 737330 · Fuselage Main, Plate/Skin
  > CORROSION AT RH SIDE FUSELAGE EXTERNAL SKIN AT STA 1028~1042, S-9R. CORROSION REMOVED LEVEL 1 AT STA 1028-1042, S-9R FROM PN 65-46882-1 ORIGINAL THICKNESS 0.0064" REMOVED 0.002" AND REMAINING THICKNESS IS 0.062 AND IS WITHIN LIMITS PER SRM 53-00-01 ALLOWABLE
- [SDR TSAA2024112600023](https://openairdocs.org/sdr/TSAA2024112600023.md): Floorbeam · cracked · Nov 23, 2024 · N301KH · Boeing 737330 · Fuselage Main, Floor Beam
  > CA1579/202 REF ECO 3845 PART X PAGE 37 OF 98 REPAIR 2: TWO FANTENERS HOLE CRACK WERE FOUND AT BL 45.5 LONGITUDINAL FLOOR BEAM WEB AT BS 639 STUB RH BEAM. CORRECTIVE ACTION:WEB WITH HOLE CRACKS FOUND AT BL 45.5 LONGITUDINAL FLOOR BEAMWEB AT BS 639 REPLACED PER
- [SDR TSAA2024112600022](https://openairdocs.org/sdr/TSAA2024112600022.md): Fuel Tank · corroded · Nov 23, 2024 · N301KH · Boeing 737330 · Fuel Storage
  > CA1579/20 SURFACE CORROSION ON RH SIDE CENTER WING TANK LOWER SKIN BETWEEN STRINGERS S11C AND S12C,AT RBL 40.875+5.7" AND RBL 45.72+9.5" CORRECTIVE ACTION:1.THE R/H CENTER TANK LOWER SKIN BETWEEN S-11C AND S-12C,AT RBL 40.875+5.7" AND RBL 45.72+9.5" CORROSI
- [SDR TSAA2024112600021](https://openairdocs.org/sdr/TSAA2024112600021.md): Seat Track · corroded · Nov 23, 2024 · N301KH · Boeing 737330 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK CORRODED ABOUT 1.0 INCH, STA: BS887 BL0. CORROSION REMOVED LEVEL 2 THE BLEND OUT DEPTH IS 0.059" AND IS OVER LIMITS PER SRM 53-00-52 ALLOWABLE DAMAGE 1, PERFORMED REPAIR AS PER AIR ASIA WPS CODE: EI-B737-241101
- [SDR TSAA2024112600020](https://openairdocs.org/sdr/TSAA2024112600020.md): Spar · corroded · Nov 23, 2024 · N301KH · Boeing 737330 · Horizontal Stabilizer, Spar/Rib
  > CORROSION (2.0" X 0.4") AT LH SIDE HORI.STAB. REAR SPAR UPPER CHORD. CORROSION REMOVED LEVEL 1 AT HOR1 STAB REAR SPAR UPPER CHORD STAB STA116 FROM PN 65-50581-525 ORIGINAL THICKNESS 1.790" REMOVED 0.036" AND REMAINING THICKNESS IS 1.754" AND IS WITHIN LIMITS
- [SDR TSAA2024112600019](https://openairdocs.org/sdr/TSAA2024112600019.md): Frame · corroded · Nov 23, 2024 · N301KH · Boeing 737330 · Rudder, Spar/Rib
  > CORROSION (19.0" X 1.0") RH SIDE CONDUCTIVE FRAME TRAILING EDGE AT RUD STA 233~252. CORROSION REMOVED LEVEL 1 AT RH SIDE CONDUCTIVE FRAME TRAILING EDGE AT RUD STA 233~252 FROM PN 65C31496-4 AFTER REMOVED SKIN THROUGH REPLACED CONDUCTIVE FRAME I.A.W B737-300 S
- [SDR TSAA2024112600018](https://openairdocs.org/sdr/TSAA2024112600018.md): Spar · corroded · Nov 23, 2024 · N301KH · Boeing 737330 · Horizontal Stabilizer, Spar/Rib
  > CORROSION (3.0" X 0.8") AT RH SIDE HORIZONTAL STABILIZER REAR SPAR UPPER CHORD AT STA 143. CORROSION REMOVED LEVEL 1 AT HOR1 STAB REAR SPAR UPPER CHORD STAB STA116 FROM PN 65-50581-526 ORIGINAL THICKNESS 1.790" REMOVED 0.095" AND REMAINING THICKNESS IS 1.695"
- [SDR TSAA2024112600017](https://openairdocs.org/sdr/TSAA2024112600017.md): Spar · corroded · Nov 23, 2024 · N301KH · Boeing 737330 · Horizontal Stabilizer, Spar/Rib
  > CORROSION (2.0" X 0.5") AT RH SIDE HORIZONTAL STABILIZER REAR SPAR UPPER CHORD AT STA 116. CORROSION REMOVED LEVEL 1 AT HOR1 STAB REAR SPAR UPPER CHORD STAB STA116 FROM PN 65-50581-526 ORIGINAL THICKNESS 2.320" REMOVED 0.050" AND REMAINING THICKNESS IS 2.270
- [SDR TSAA2024112600016](https://openairdocs.org/sdr/TSAA2024112600016.md): Skin · corroded · Nov 23, 2024 · N301KH · Boeing 737330 · Fuselage Main, Plate/Skin
  > SURFACE CORROSION ON FUSELAGE EXTERIOR SKIN AT BS947+6" S25L+3". SURFACE CORROSION ON FUSELAGE EXTERIOR SKIN AT BS947+6" S25L+3" WAS REMOVED LEVEL 1, P/N 65-45776-11 ORIGINAL THICKNESS WAS 0.063" AND AFTER REMOVING 0.003" REMAINED 0.06" AND IS WITHIN LIMIT
- [SDR TSAA2024112600015](https://openairdocs.org/sdr/TSAA2024112600015.md): Fuel Tank · corroded · Nov 23, 2024 · N301KH · Boeing 737330 · Fuel Storage
  > SURFACE CORROSION ON RH SIDE CENTER WING TANK LOWER SKIN BETWEEN STRINGERS S5C RBL40.875+13"&2.5" AND 4.5". THE R/H CENTER TANK LOWER SKIN BETWEEN S-5C -RBL40.875+13"&2.5" AND 4.5" CORROSION REMOVED & NDT CHECK 2. FLAP PEEN REMVED AREA & PRIMER APPLY REFER TO
- [SDR TSAA2024112600014](https://openairdocs.org/sdr/TSAA2024112600014.md): Fuel Tank · corroded · Nov 23, 2024 · N301KH · Boeing 737330 · Fuel Storage
  > SURFACE CORROSION ON LH SIDE CENTER WING TANK LOWER SKIN BETWEEN STRINGERS S5C AND S6C AT LBL40.875+5.5" & S5C AT LBL 40.875+1.0";LBL40.875+3.5",LBL40.875+5.5" & BETWEEN STRINGERS S4C AND S5C AT LBL40.875+2.0". CORROSION REMOVED AND CONDITION CHECK OK WITHIN
- [SDR TSAA2024112600013](https://openairdocs.org/sdr/TSAA2024112600013.md): Fuel Tank · corroded · Nov 23, 2024 · N301KH · Boeing 737330 · Fuel Storage
  > SURFACE CORROSION ON LH SIDE CENTER WING TANK LOWER SKIN BETWEEN STRINGERS S6C LBL40.875+4". CORROSION REMOVED AND CONDITION CHECK OK WITHIN LIMIT ON LH SIDE CENTER WING TANK LOWER SKIN BETWEEN STRINGERS S6C AND LBL 40.874+4" PER REF CA1579/28 WPS CODE:EI-737
- [SDR TSAA2024112600012](https://openairdocs.org/sdr/TSAA2024112600012.md): Skin · corroded · Nov 23, 2024 · N301KH · Boeing 737330 · Leading Edge Devices
  > CORROSION FOUND AT RH WING NO.4 SLAT SLAT STA.13, BETWEEN OUTER SKIN AND TEE CHORD. CUT & REMOVED THE DAMAGED AREA FROM RH WING NO.4 SLAT STA13 2.MADE REPAIR DOUBLER & FILL TO INSTALL WITH SEALANT I.A.W B737-300 SRM 57-43-01 REPAIR 6 FIG201(REV134) REF BOEIN
- [SDR TSAA2024112600011](https://openairdocs.org/sdr/TSAA2024112600011.md): Skin · corroded · Nov 23, 2024 · N301KH · Boeing 737330 · Fuselage Main, Plate/Skin
  > SURFACE CORROSION ON FUSELAGE EXTERIOR SKIN AT BS907 S23R. CORROSION REMOVE LEVEL 1 AT BS907 S23R, FROM PN 65C35778-21, ORIGINAL THICRNESS 0.071" REMOVED 0.007" AND REMAINING THICRNESS IS 0.064" AND IS WITHIN LIMITS PER IAW B737-300 SRM 52-30-01 IDENTIFICATIO
- [SDR TSAA2024112600010](https://openairdocs.org/sdr/TSAA2024112600010.md): Skin · corroded · Nov 23, 2024 · N301KH · Boeing 737330 · Fuselage Main, Plate/Skin
  > SURFACE CORROSION ON FUSELAGE EXTERIOR SKIN AT BS907 S17R+4". CORROSION REMOVE LEVEL 1 AT BS907 S17R+4", FROM PN 65C35768-21, ORIGINAL THICRNESS 0.071" REMOVED 0.007" AND REMAINING THICRNESS IS 0.064" AND IS WITHIN LIMITS PER IAW B737-300 SRM 52-30-01 IDENTIF
- [SDR TSAA2024112600009](https://openairdocs.org/sdr/TSAA2024112600009.md): Skin · cracked · Nov 23, 2024 · N301KH · Boeing 737330 · Leading Edge Devices
  > LH WING NO.2 SLAT OUTER SKIN BULGE AROUND FASTENER HOLE BETWEEN SLAT STA 183 AND SLAT STA 196. LH WING NO.2 SLAT OUTER SKIN REPAIRED BETWEEN SLAT STA 183 AND SLAT STA 196 I.A.W SRM 57-43-01 REPAIR 6 (R134)
- [SDR TSAA2024112600008](https://openairdocs.org/sdr/TSAA2024112600008.md): Skin · cracked · Nov 23, 2024 · N301KH · Boeing 737330 · Leading Edge Devices
  > LH WING NO.1 SLAT OUTER SKIN CRACKED AROUND FASTENER HOLE BETWEEN SLAT STA 294.03 AND SLAT STA 302.03. LH WING NO.1 SLAT OUTER SKIN REPAIRED BETWEEN SLAT STA 294.03 AND SLAT STA 302.03 I.A.W SRM 57-43-01 REPAIR 6 (R134)
- [SDR TSAA2024112600007](https://openairdocs.org/sdr/TSAA2024112600007.md): Frame Angle · cracked · Nov 23, 2024 · N301KH · Boeing 737330 · Fuselage Main, Frame
  > FUSELAGE FRAME CLIP CRACK, STA 360, S-11L. CLIP REPLACED AT FUSELAGE FRAME STA360, S-11L PER:B737-300 DRAWING:65-58280 SHEET2, SRM 51-40-02 PARA.4&7 (REV.134)
- [SDR TSAA2024112600006](https://openairdocs.org/sdr/TSAA2024112600006.md): Pressure Blkhd · cracked · Nov 23, 2024 · N301KH · Boeing 737330 · Fuselage Main, Bulkhead
  > MAIN GEAR WHEEL WELL PRESSURE BLUCKHEAD CRACKS ABOUT 1", STA 663.75 LBL24.75+6". PERFORMED REPAIR AT STA663.75, LBL24.75+6" AS PER B737-300 SRM 53-60-51 REPAIR 4 (R134)
- [SDR TSAA2024112600004](https://openairdocs.org/sdr/TSAA2024112600004.md): Fuel Tank · corroded · Nov 23, 2024 · N301KH · Boeing 737330 · Fuel Storage
  > SURFACE CORROSION ON RH SIDE CENTER WING TANK LOWER SKIN BETWEEN STRINGERS S9C & RBL 40.875+13"-15". THE R/H CENTER TANK LOWER SKIN BETWEEN S-9C & RBL 40.875+13"-15" CORROSION REMOVED & NDT CHECK NORMAL 2. FLAP PEEN REMVED AREA & PRIMER APPLY REFER TO NRC:CA1
- [SDR TSAA2024112600003](https://openairdocs.org/sdr/TSAA2024112600003.md): Fuel Tank · corroded · Nov 23, 2024 · N301KH · Boeing 737330 · Fuel Storage
  > SURFACE CORROSION ON LH SIDE CENTER WING TANK LOWER SKIN BETWEEN STRINGERS S9C AND S10C LBL40.875+13". CORROSION REMOVED AND CONDITION CHECK OK WITHIN LIMIT ON LH SIDE CENTER WING TANK LOWER SKIN BETWEEN STRINGERS S9C AND SPC LBL 40.875+13" PER AIRASIA WPS CO
- [SDR TSAA2024112600002](https://openairdocs.org/sdr/TSAA2024112600002.md): Attach Fitting · corroded · Nov 23, 2024 · N301KH · Boeing 737330 · Fuselage Main, Bulkhead
  > CORROSION AT ATTACH FITTING AT AFT PRESSURE BULKHEAD AFT SIDE AT STA 1016, S-21L. REPLACED FITTING AT AFT PRESSURE BULKHEAD AFT SIDE STA1016, S-21L REMOVED AND REINSTALLED S-21L/ I.A.W. B737-300 SRM 51-40-02 PARA 4 (R134) & DWG 65-46568 & 65-46881
- [SDR TSAA2024112600001](https://openairdocs.org/sdr/TSAA2024112600001.md): Cover · eroded · Nov 23, 2024 · N301KH · Boeing 737330 · Vertical Stabilizer, Plate/Skin
  > EROSION (1.0" X 1.0") AT HF ANTENNA COVER OF VERTICAL STABILIZER LEADING EDGE AT LE STA 90. PERFORMED THE EROSION AREA AT HF ANTENNA COVER OF VERTICAL STABILIZER LEADING EDGE AT LE STA 90. APPLIED THE REPAIR PLIES WITH RESIN AND CURED. MADE THE REPAIR SURFACE
- [SDR NACA2024050300005](https://openairdocs.org/sdr/NACA2024050300005.md): Outflow Valve · failed · May 3, 2024 · N304KH · Boeing 737330 · Pressure Regulator/Outflow Valve
  > ENROUTE TO PANC @ FL350 CABIN ALT WARNING WENT OFF. SELECTED MANUAL AC ON PRESS CONTROLLER PER QRX, COULD NOT RECOVER THE CABIN PRESSURE. PRESS WAS AT 60 WITH 10000 FT CABIN ALTITUDE WHEN WARNING WENT OFF. REMOVED AND REPLACED OUTFLOW VALVE ASSY REF B737-300 A
- [SDR NACA2024041600001](https://openairdocs.org/sdr/NACA2024041600001.md): Skin · cracked · Apr 16, 2024 · N360WA · Boeing 737330 · Fuselage Main, Plate/Skin
  > FOUND CRACK INDICATION BELOW STRINGER 2R @ BS 400 + 1/38. FOUND INTERNAL NICK ON SKIN. REPAIRED NICK @ BS400 + 1 3/8 STR 2R PER NAC EO 737-53-0341-01 AEI EO 233-49
- [SDR NACA2024031200001](https://openairdocs.org/sdr/NACA2024031200001.md): Unknown · cracked · Mar 12, 2024 · N360WA · Boeing 737330 · Fuselage Structure (General)
  > MECHANIC FOUND CRACK DURING SERVICE CHECK AT BS 727E, STR 22L APPROX 2 1/8" LONG. CRACK CONFIRMED BY EDDY CURRENT, COMPLETED REPAIR OF CRACK FOUND ON BS 727E STR 22L IAW SRM 52-31-00 REPAIR 31 & NAC PROJECT WORKSHEET ON 3/20/2024 & WITH REF TO EO 737-53-0339.
- [SDR NACA2024020300001](https://openairdocs.org/sdr/NACA2024020300001.md): Warning Message · false indication · Feb 3, 2024 · N321CM · Boeing 737330 · Engine Bleed Air System
  > R ENG HPSOV EICAS MESSAGE. PERFORMED AIR SUPPLY BITE PROCEDURE 56-20 FAULT TREE 804 FOR R ENG HPSOV STATUS MESSAGE, NO FAULTS FOUND. RESET MSG OK FOR CONT SERVICE
- [SDR NACA2024020200001](https://openairdocs.org/sdr/NACA2024020200001.md): Skin · cracked · Feb 2, 2024 · N304KH · Boeing 737330 · Wing, Plate/Skin
  > 4.5 INCH CRACK FOUND AT #3 SLAT ACTUATOR CUTOUT. WORK IN PROGRESS.
- [SDR NACA202401300001](https://openairdocs.org/sdr/NACA202401300001.md): Seal · fod · Jan 30, 2024 · N360WA · Boeing 737330 · Flight Compartment Windows
  > AUTOFAIL LIGHT WITH CABIN ALT WARNING ACCOMPANIED BY HISSING NOISE FROM CAPT SIDE WINDOW, COULD NOT PRESSURIZE. PERFORMED OPS TEST OF PRESSURIZATION CONTROLLER IAW AMM 21-31-00 OPS CHECK OK. CHECKED AND CLEANED CAPT'S SLIDING WINDOW SEAL. NO DEFECTS NOTED.
- [SDR NACA2024013170001](https://openairdocs.org/sdr/NACA2024013170001.md): Skin · cracked · Jan 27, 2024 · N303KH · Boeing 737330 · Fuselage Main, Plate/Skin
  > CRACK INDICATIONS AT STR 10R BS 827+6 5/8 INCHES LONG, AND BS 827+10 11/16, 1/2 INCHES LONG. REPAIRED PER BOEING SB 737-53A-1234
- [SDR NACA2024010600003](https://openairdocs.org/sdr/NACA2024010600003.md): Unknown · unknown · Jan 6, 2024 · N303KH · Boeing 737330 · Fuselage, Seat/Cargo Attach Fittings
  > CAPTAIN'S RH FORWARD SEAT TRACK CRACKED. REMOVED AND REPLACED CAPT FWD RH SEAT TRACK IAWM AMM 25-11-11
- [SDR NACA2023081100006](https://openairdocs.org/sdr/NACA2023081100006.md): Unknown · unknown · Aug 11, 2023 · N303KH · Boeing 737330 · Wing Structure
  > RH WING NO.5 SLAT T/E WEDGE DELAMINATION AT SS.248~SS.254. REMOVED THE DELAMINATION SKIN AT RH WING NO5 SLAT T/E WEDGE SS248~SS254 MADE THE SKIN FILLER AND DOUBLER INSTALLED THE REPAIR PARTS AND PERFORMED 250°F METAL BOND REPAIR I.A.W B737-00 SRM 51-70-10 REPA
- [SDR NACA2023081100005](https://openairdocs.org/sdr/NACA2023081100005.md): Unknown · unknown · Aug 11, 2023 · N303KH · Boeing 737330 · Wing Structure
  > RH WING NO.4 SLAT T/E WEDGE EDGE DEFORM AT SS.12.25. REMOVE THE INITIAL REPAIR DOUBLER AND DAMAGED CORE AT RH WING NO.4 SLAT T/E WEDGE EDGE SS12.25 MADE THE REPAIR CORE AND DOUBLER AND INSTALLED PERFORMED PERMANENT 250°F METEL METAL BOND REPAIR I.A.W B737-300
- [SDR NACA2023081100004](https://openairdocs.org/sdr/NACA2023081100004.md): Unknown · unknown · Aug 11, 2023 · N303KH · Boeing 737330 · Fuselage, Door Hinge
  > MAIN ENTRY DOOR LOWER HINGE HOUSING CRACK. REPLACED HINGE FITTER AT MAIN ENTRY DOOR LOWER HINGER HOUSING I.A.W B737-300 SRM 51-40-2 PAGE 2~3 PAGE 6~7 (REV 130).
- [SDR NACA2023081100003](https://openairdocs.org/sdr/NACA2023081100003.md): Unknown · unknown · Aug 11, 2023 · N303KH · Boeing 737330 · Fuselage Main, Plate/Skin
  > CORROSION ON FUSELAGE EXTERNAL SKIN AT BS727D S21R+4" REMOVED CORROSION LEVEL 2 AT FUSELAGE EXTERNAL SKIN AT BS727DS21R+4'' FROM P/N 65C38588 ORIGINAL THICKNESS 0.063'' REMOVED 0.063'' AND REMAINING THICKNESS IS 0'' AND IS OVER LIMITS PERFORM REPAIR PER SRM 53
- [SDR NACA2023081100002](https://openairdocs.org/sdr/NACA2023081100002.md): Unknown · unknown · Aug 11, 2023 · N303KH · Boeing 737330 · Fuselage Structure (General)
  > STRINGER TIE CLIP CRACKS WAS FOUND AT STA 727A S-7R. RESOLVED ON W/O: 121696 TASKCARD: N/R-00262) DAMAGE PARTS REPLACED AT STA 727AS-7R PN:69-35352U14.I.A.W B737-300 SRM 51-40-02 PARA 4 PAGE 2.3 (REV30).
- [SDR NACA2023081000005](https://openairdocs.org/sdr/NACA2023081000005.md): Unknown · unknown · Aug 10, 2023 · N303KH · Boeing 737330 · Emergency Lighting
  > INTERIOR EMERGENCY EXIT SIGN COVER CRACK, FWD GALLEY SERVICE DOOR. 1. REPLACE FWD ENTRY DOOR EXIT SIGN ASSEMBLY RE AMM 33-51-11 PAGE 203 REV 097 2. DD EXIT SIGN TEST NORMAL REF AMM 33-51-11 P[AGE 204 STEP D REV 097.
- [SDR NACA2023081000004](https://openairdocs.org/sdr/NACA2023081000004.md): Unknown · unknown · Aug 10, 2023 · N303KH · Boeing 737330 · Fuselage Structure (General)
  > 2 EA SURFACE CORROSION ON CENTER WING EXTERIOR LOWER SKIN BWTWEEN S-11C AND S-12C LBL41-53. PERFORM AIR ASIA WPS CODE EI-737-230801 COMPLETED.
- [SDR NACA2023081000003](https://openairdocs.org/sdr/NACA2023081000003.md): Unknown · unknown · Aug 10, 2023 · N303KH · Boeing 737330 · Flight Control System
  > RH WING UPPER T/E PANEL WBL.214 SUPPORT ROD CRACKED. SUPPORT ROD REPCACED REF: AMM 20-50-11 PAGE 201.R97.
- [SDR NACA2023081000002](https://openairdocs.org/sdr/NACA2023081000002.md): Unknown · unknown · Aug 10, 2023 · N303KH · Boeing 737330 · Wing Structure
  > LH WING L/E PNL SUPPORT WAS CORRODED AT FSS 339. REPLACED PNL SUPPORT AT LH WING L/E FSS 339 FROM PN 69-76227-1 I.A.W B737-300 SRM 51-40-2 PAGE 10~PAGE 12(REV 130)
- [SDR NACA2023080900004](https://openairdocs.org/sdr/NACA2023080900004.md): Unknown · unknown · Aug 9, 2023 · N303KH · Boeing 737330 · Fuselage Main, Longeron/Stringer
  > STRINGER TIE CLIP CRACKS WAS FOUND AT STA 727A S-5R. DAMAGED PARTS REPLACED AT STA 727A-5R PN# 69-35352U14 IAW B737 SRM 51-40-02
- [SDR NACA2023080900003](https://openairdocs.org/sdr/NACA2023080900003.md): Unknown · unknown · Aug 9, 2023 · N303KH · Boeing 737330 · Wing, Attach Fittings
  > LH WING #2 SLAT DEICING DUCT SUPPORT BRACKET CORRODED AT FSS419. REPLACED DAMAGED PARTS AT LH WING #2 SLAT FSS 419 PN# 652627C5U89 IAW B737 SRM 51-40-02
- [SDR NACA2023080800002](https://openairdocs.org/sdr/NACA2023080800002.md): Unknown · unknown · Aug 8, 2023 · N303KH · Boeing 737330 · Fuselage Main, Plate/Skin
  > CORROSION ON FUSELAGE EXTERNAL SKIN AT BS796 S20R~S21R. 1. REMOVED DAMAGE PARTS 2. PERFORMED AIR ASIA WPS CODE LM BACF3TOIE30G65 FOR REPAIR PARTS 3. IA,AW B737-300 SRM 51-40-2 PAGE 6~7 (REV 130) INSTALLED REPAIR PARTS.
- [SDR NACA2023080100001](https://openairdocs.org/sdr/NACA2023080100001.md): Unknown · unknown · Aug 1, 2023 · N303KH · Boeing 737330 · Fuselage Main, Plate/Skin
  > CORROSION AT APU INLET DOOR EXTERNAL SKIN AT STA 1022~1205, S-13R~S-14R. PERFORMED AIR ASIA WPS CODE LM-65-50976-273 REMOVED INSTALLED REPAIR PARTS AND FASTENERS IAW B737 SRM 51-40-2
- [SDR NACA2023073150003](https://openairdocs.org/sdr/NACA2023073150003.md): Unknown · unknown · Jul 25, 2023 · N302KH · Boeing 737330 · Wing Structure
  > DAMAGE NOTED ON UPPER WING SURFACE AFT OF SLAT #3. REPAIRED DAMAGE TO THE #3 SLAT REF SRM 51-70-01 REPAIR 4
- [SDR NACA20230705001](https://openairdocs.org/sdr/NACA20230705001.md): Unknown · unknown · Jun 28, 2023 · N303KH · Boeing 737330 · Ailerons
  > #4 FLAP FAIRING DAMAGED. REPAIRED FAIRING DAMAGE REF SRM 51-70-6 INLET LAYUP REPAIR

Next page: https://openairdocs.org/model/boeing-737-330/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 aircraft_model_key = '737330'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/boeing-737-330/reports

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