# Service difficulty reports: N301KH

A list on [N301KH](https://openairdocs.org/aircraft/N301KH.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 5 · 210 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 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 TSAA202311074109](https://openairdocs.org/sdr/TSAA202311074109.md): Unknown · unknown · Nov 4, 2023 · N301KH · Boeing 737300 · Fuselage Structure (General)
  > DURING ECO 3925, DISCOVERED DENT AT BS 440R APPROX 5" FROM FLOOR, 1 1/4" WIDE, AND 0.07" DEEP.
- [SDR TSAA202311074110](https://openairdocs.org/sdr/TSAA202311074110.md): Unknown · unknown · Nov 4, 2023 · N301KH · Boeing 737300 · Fuselage Structure (General)
  > DURING ECO 3925, DISCOVERED 2 RIVETS MISSING AT BS 360R JUST ABOVE FLOOR BOARD.
- [SDR TSAA20230606107](https://openairdocs.org/sdr/TSAA20230606107.md): Unknown · unknown · Jun 6, 2023 · N301KH · Boeing 737330 · Fasteners
  > CA 1464/361 WHILE PERFORM CUSTOMER PROVIDE TASK CARD ECO 3531-R10 WHICH INDICATED IN SB 737-53A1240, FOUND FASTENER HAD BEEN UPSIDE. PERFORM TASK CARD ECO 3531-R10 INSP FOUND FASTENER WRONG. PERFORM PER AIRASIA EL-737-230508.
- [SDR TSAA20230606106](https://openairdocs.org/sdr/TSAA20230606106.md): Unknown · unknown · Jun 6, 2023 · N301KH · Boeing 737330 · Fuselage Structure (General)
  > CA 1464/100 CORROSION AT FUSELAGE SKIN BETWEEN STA579 AND STA616, S-14R AND S-15R ( L:4.5" W:1"). ALL CORROSION REMOVED AT FUSELAGE SKIN BETWEEN STA 579 AND STA 616, S-14R AND S-15R (L:4.5", W:1"). REMOVED 0.004" AND REMAINING 0.114" IS WITHIN ALLOWABLE LIMI
- [SDR TSAA20230606105](https://openairdocs.org/sdr/TSAA20230606105.md): Unknown · unknown · Jun 6, 2023 · N301KH · Boeing 737330 · Wing Structure
  > CA 1464/166 CORROSION AT LH WING I/B AFT FLAP LOWER SKIN BETWEEN WBL 100.0 AND WBL 102.5. ALL CORROSION REMOVED AT LH WING I/B AFT FLAP LOWER SKIN BETWEEN WBL 100.0 & WBL 102.5. REMOVED 0.001" MATERIAL AND REMAINING 0.015" IS WITHIN ALLOWABLE LIMITS. AREA C
- [SDR TSAA20230606104](https://openairdocs.org/sdr/TSAA20230606104.md): Unknown · unknown · Jun 6, 2023 · N301KH · Boeing 737330 · Wing Structure
  > CA 1464/82 RH WING O/B AFT FLAP LOWER SKIN DELAMINATION BETWEEN WBL 245-WBL 249.5. TRIMMED AND REMOVED THE DAMAGE AREA ON RH WING O/B AFT FLAP LOWER SKIN BETWEEN WBL 245 ~ WBL 247.5. MADE THE REPAIR SKIN AND DOUBLER AND CORE. INSTALLED THE REPAIR PARTS AND
- [SDR TSAA20230606103](https://openairdocs.org/sdr/TSAA20230606103.md): Unknown · unknown · Jun 6, 2023 · N301KH · Boeing 737330 · Fuselage Structure (General)
  > CA 1464/9 FILIFORM CORROSION WERE FOUND ON FUSELAGE EXTERNAL SKIN RH SIDE STRINGER 20 STATION 767 TO 787, 867 TO 897, 927 TO 929. ALL CORROSION REMOVED AT STA500 & STA500E, S-1R & S-2R (L:3.1", W:2.2") (L:14", W:1.4") (L:0.9", W:0.5") L:0.5", W:0.4") (L:1.9",
- [SDR TSAA20230606102](https://openairdocs.org/sdr/TSAA20230606102.md): Unknown · unknown · Jun 6, 2023 · N301KH · Boeing 737330 · Fuselage Structure (General)
  > CA 1464/303 LIGHT CORROSION AT RH SIDE EXTERNAL SKIN AT STA 1088, S-16R. ALL CORROSION REMOVED AT RH SIDE EXTERNAL SKIN AT STA 1088, S-16R. REMOVED 0.004" MATERIAL & REMAINING 0.049" IS WITHIN ALLOWABLE LIMIT. AREA CLEAN & PROTECTIVE I.A.W. B737-300 SRM 51-
- [SDR TSAA20230606101](https://openairdocs.org/sdr/TSAA20230606101.md): Unknown · unknown · Jun 6, 2023 · N301KH · Boeing 737330 · Fuselage Structure (General)
  > CA 1464/302 LIGHT CORROSION AT LH SIDE EXTERNAL SKIN AT STA 1073 S-20L. ALL CORROSION REMOVED AT LH SIDE EXTERNAL SKIN AT STA 1073 S-20L. REMOVED 0.004" MATERIAL & REMAINING 0.049" IS WITHIN ALLOWABLE LIMIT. AREA CLEAN & PROTECTIVE I.A.W. B737-300 SRM 51-10
- [SDR TSAA20230606100](https://openairdocs.org/sdr/TSAA20230606100.md): Unknown · unknown · Jun 6, 2023 · N301KH · Boeing 737330 · Wing Structure
  > CA 1464/298 THE CORROSION WAS FOUND AT LH WING I/B FLAP LOWER PNL 8407, AROUND FASTENER (6EA). ALL CORROSION REMOVED AT LH WING I/B FLAP LOWER PANEL 8407 AROUND FASTENER. REMOVED 0.004" MATERIAL & REMAINING 0.121" IS WITHIN ALLOWABLE LIMIT. AREA CLEAN AND P
- [SDR TSAA20230606099](https://openairdocs.org/sdr/TSAA20230606099.md): Unknown · unknown · Jun 6, 2023 · N301KH · Boeing 737330 · Wing Structure
  > CA 1464/297 THE CORROSION WAS FOUND AT LH WING I/B FLAP LOWER PNL 8406, AROUND FASTENER (10EA). ALL CORROSION REMOVED AT LH WING I/B FLAP LOWER PANEL 8406 AROUND FASTENER. REMOVED 0.004" MATERIAL & REMAINING 0.121" IS WITHIN ALLOWABLE LIMIT. AREA CLEAN AND
- [SDR TSAA20230606098](https://openairdocs.org/sdr/TSAA20230606098.md): Unknown · unknown · Jun 6, 2023 · N301KH · Boeing 737330 · Wing Structure
  > CA 1464/296 THE CORROSION WAS FOUND AT LH WING I/B FLAP LOWER PNL 8404, AROUND FASTENER (9EA). ALL CORROSION REMOVED AT LH WING I/B FLAP LOWER PANEL 8404 AROUND FASTENER. REMOVED 0.005" MATERIAL & REMAINING 0.120" IS WITHIN ALLOWABLE LIMIT. AREA CLEAN AND P
- [SDR TSAA20230606097](https://openairdocs.org/sdr/TSAA20230606097.md): Unknown · unknown · Jun 6, 2023 · N301KH · Boeing 737330 · Wing Structure
  > CA 1464/293 THE CORROSION WAS FOUND AT LH WING LOWER SURFACE, BETWEEN WBL 266.25 AND WBL 266.75. ALL CORROSION REMOVED AT LH WING LOWER SURFACE BETWEEN WBL 266.25 AND WBL 266.75. REMOVED 0.028" MATERIAL AND REMAINING 0.283" IS WITHIN ALLOWABLE LIMIT. AREA C
- [SDR TSAA20230606096](https://openairdocs.org/sdr/TSAA20230606096.md): Unknown · unknown · Jun 6, 2023 · N301KH · Boeing 737330 · Wing Structure
  > CA 1464/292 THE CORROSION WAS FOUND AT LH WING LOWER SURFACE, BETWEEN W STA 468.2 AND W STA 469.0. ALL CORROSION REMOVED AT LH WING LOWER SURFACE BETWEEN WSTA 468.2 AND WSTA 469.0. REMOVED 0.023" MATERIAL & REMAIN 0.149" IS WITHIN ALLOWABLE LIMIT. AREA CLEA
- [SDR TSAA20230606095](https://openairdocs.org/sdr/TSAA20230606095.md): Unknown · unknown · Jun 6, 2023 · N301KH · Boeing 737330 · Wing Structure
  > CA 1464/291 THE CORROSION WAS FOUND AT LH WING LOWER SURFACE, BETWEEN W STA 475.0 AND W STA 477.0. CORROSION AT LH WING LOWER SURFACE, BETWEEN W STA 475.0 AND W STA 477.0, REPAIR IAW AIR ASIA EL-737-230503. (V1 AEROSPACE, LLC REPAIR INSTRUCTION R23-01849-001
- [SDR TSAA20230606094](https://openairdocs.org/sdr/TSAA20230606094.md): Unknown · unknown · Jun 6, 2023 · N301KH · Boeing 737330 · Wing Structure
  > CA 1464/290 THE CORROSION WAS FOUND AT LH WING LOWER SURFACE, BETWEEN W STA 581.3 AND W STA 582.1. CORROSION AT LH WING LOWER SURFACE, BETWEEN W STA 581.3 AND W STA 582.1, REPAIR IAW AIR ASIA EL-737-230503. (V1 AEROSPACE, LLC REPAIR INSTRUCTION R23-01849-001
- [SDR TSAA20230606093](https://openairdocs.org/sdr/TSAA20230606093.md): Unknown · unknown · Jun 6, 2023 · N301KH · Boeing 737330 · Wing Structure
  > CA 1464/289 THE CORROSION WAS FOUND AT LH WING LOWER SURFACE, BETWEEN W STA 477.75 AND W STA 478.25. ALL CORROSION REMOVED AT LH WING LOWER SURFACE BETWEEN WSTA 477.75 AND WSTA 478.25. REMOVED 0.011" MATERIAL & REMAIN 0.139" IS WITHIN ALLOWABLE LIMIT. AREA
- [SDR TSAA20230606092](https://openairdocs.org/sdr/TSAA20230606092.md): Unknown · unknown · Jun 6, 2023 · N301KH · Boeing 737330 · Wing Structure
  > CA 1464/288 THE CORROSION WAS FOUND AT LH WING LOWER SURFACE, BETWEEN W STA 627.5 AND W STA 629.7. CORROSION AT LH WING LOWER SURFACE, BETWEEN W STA 627.5 AND W STA 629.7, REPAIR IAW AIR ASIA EL-737-230503. (V1 AEROSPACE, LLC REPAIR INSTRUCTION R23-01849-001R
- [SDR TSAA20230606091](https://openairdocs.org/sdr/TSAA20230606091.md): Unknown · unknown · Jun 6, 2023 · N301KH · Boeing 737330 · Wing Structure
  > CA 1464/287 THE CORROSION WAS FOUND AT LH WING LOWER SURFACE, BETWEEN W STA 614.0 AND W STA 617.7. CORROSION AT LH WING LOWER SURFACE, BETWEEN W STA 614.0 AND W STA 617.7, REPAIR IAW AIR ASIA EL-737-230503. (V1 AEROSPACE, LLC REPAIR INSTRUCTION R23-01849-001R
- [SDR TSAA20230606090](https://openairdocs.org/sdr/TSAA20230606090.md): Unknown · unknown · Jun 6, 2023 · N301KH · Boeing 737330 · Wing Structure
  > CA 1464/284 THE CORROSION WAS FOUND AT LH WING LOWER SURFACE, BETWEEN WBL 559 AND WBL 560.9. ALL CORROSION REMOVED AT LH WING LOWER SURFACE BETWEEN WBL 559 AND WBL 560.9. REMOVED 0.002" MATERIAL & REMAIN 0.048" IS WITHIN ALLOWABLE LIMIT. AREA CLEAN AND PROT
- [SDR TSAA20230606089](https://openairdocs.org/sdr/TSAA20230606089.md): Unknown · unknown · Jun 6, 2023 · N301KH · Boeing 737330 · Wing Structure
  > CA 1464/269 THE CORROSION WAS FOUND AT #1 SPOILER LOWER SURFACE, RSS 412. ALL CORROSION REMOVED AT #1 SPOILER LOWER SURFACE, RSS412. REMOVED 0.001" MATERIAL & REMAIN 0.019" IS WITHIN ALLOWABLE LIMIT. AREA CLEAN AND PROTECTIVE I.A.W. B737-300 SRM 51-10-2 / 5
- [SDR TSAA20230606088](https://openairdocs.org/sdr/TSAA20230606088.md): Unknown · unknown · Jun 6, 2023 · N301KH · Boeing 737330 · Standard Practices/Structures
  > CA 1464/264 DRILL OFF HI-LOCK FASTENER ON FWD ENTRY DOOR LOWER HINGE EXTERNAL DOUBLER, STA 303.9 S-13L AND S-14L. FASTENER REMOVED AT FWD ENTRY DOOR LOWER HINGE EXTERNAL DOUBLER STA 303.9, S-13L & S14L. REINSTALL FASTENER I.A.W. B737-300 SRM 51-40-2 PARA 7
- [SDR TSAA20230606087](https://openairdocs.org/sdr/TSAA20230606087.md): Unknown · unknown · Jun 6, 2023 · N301KH · Boeing 737330 · Wing Structure
  > CA 1464/256 CORROSION AT RH WING I/B MID FLAP UPPER SKIN BETWEEN WBL 83, WBL 111 AND WBL 138. ALL CORROSION REMOVED AT RH WING I/B FLAP UPPER SKIN BETWEEN WBL83, WBL111 AND WBL138. REMOVED 0.001" MATERIAL & REMAIN 0.019" IS WITHIN ALLOWABLE LIMIT. AREA CLEA
- [SDR TSAA20230606086](https://openairdocs.org/sdr/TSAA20230606086.md): Unknown · unknown · Jun 6, 2023 · N301KH · Boeing 737330 · Wing Structure
  > CA 1464/255 SKIN GOUGE AT RH WING I/B FORE FLAP LOWER SURFACE WBL 99. REMOVED SURFACE FINISH OF GOUGE AREA AT RH WING I/B FORE FLAP LOWER SURFACE WBL 99. FILLED THE DAMAGE WITH FILM ADHESIVE. MADE REPAIR DOUBLER. INSTALLED REPAIR PARTS AND CURED THE BOND.

Next page: https://openairdocs.org/aircraft/N301KH/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 = 'N301KH' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N301KH/reports

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