N301KH

Service difficulty reports · 210

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 = 'N301KH' 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 TSAA2026081700001Cabin Press Sys · faultedAT 1000 FT ON CLIMB OUT AUTO FAIL LIGHT ILLUMINATE AND STANDBY LIGHT ILLUMINATE CLIMB RATE PASS 3000FT/MIN DRIVE CABIN PRESS BELOW SEA LEVELAug 18, 2026 · N301KH · Boeing 737330 · Cabin Pressure Control SystemSDR TSAA2024112600026Skin · corrodedCORROSION 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 DAMANov 23, 2024 · N301KH · Boeing 737330 · Fuselage Main, Plate/SkinSDR TSAA2024112600025Skin · corrodedCORROSION 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 DNov 23, 2024 · N301KH · Boeing 737330 · Fuselage Main, Plate/SkinSDR TSAA2024112600024Skin · corrodedCORROSION 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 Nov 23, 2024 · N301KH · Boeing 737330 · Fuselage Main, Plate/SkinSDR TSAA2024112600023Floorbeam · crackedCA1579/202 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 PERNov 23, 2024 · N301KH · Boeing 737330 · Fuselage Main, Floor BeamSDR TSAA2024112600022Fuel Tank · corrodedCA1579/20 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" CORROSINov 23, 2024 · N301KH · Boeing 737330 · Fuel StorageSDR TSAA2024112600021Seat Track · corrodedSEAT 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-B737-241101Nov 23, 2024 · N301KH · Boeing 737330 · Fuselage, Seat/Cargo Attach FittingsSDR TSAA2024112600020Spar · corrodedCORROSION (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 LIMITSNov 23, 2024 · N301KH · Boeing 737330 · Horizontal Stabilizer, Spar/RibSDR TSAA2024112600019Frame · corrodedCORROSION (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 SNov 23, 2024 · N301KH · Boeing 737330 · Rudder, Spar/RibSDR TSAA2024112600018Spar · corrodedCORROSION (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"Nov 23, 2024 · N301KH · Boeing 737330 · Horizontal Stabilizer, Spar/RibSDR TSAA2024112600017Spar · corrodedCORROSION (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 2.270Nov 23, 2024 · N301KH · Boeing 737330 · Horizontal Stabilizer, Spar/RibSDR TSAA2024112600016Skin · corrodedSURFACE 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 Nov 23, 2024 · N301KH · Boeing 737330 · Fuselage Main, Plate/SkinSDR TSAA2024112600015Fuel Tank · corrodedSURFACE 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 TONov 23, 2024 · N301KH · Boeing 737330 · Fuel StorageSDR TSAA2024112600014Fuel Tank · corrodedSURFACE 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 WITHINNov 23, 2024 · N301KH · Boeing 737330 · Fuel StorageSDR TSAA2024112600013Fuel Tank · corrodedSURFACE 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-737Nov 23, 2024 · N301KH · Boeing 737330 · Fuel StorageSDR TSAA2024112600012Skin · corrodedCORROSION 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 BOEINNov 23, 2024 · N301KH · Boeing 737330 · Leading Edge DevicesSDR TSAA2024112600011Skin · corrodedSURFACE 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 IDENTIFICATIONov 23, 2024 · N301KH · Boeing 737330 · Fuselage Main, Plate/SkinSDR TSAA2024112600010Skin · corrodedSURFACE 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 IDENTIFNov 23, 2024 · N301KH · Boeing 737330 · Fuselage Main, Plate/SkinSDR TSAA2024112600009Skin · crackedLH 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)Nov 23, 2024 · N301KH · Boeing 737330 · Leading Edge DevicesSDR TSAA2024112600008Skin · crackedLH 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)Nov 23, 2024 · N301KH · Boeing 737330 · Leading Edge DevicesSDR TSAA2024112600007Frame Angle · crackedFUSELAGE 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)Nov 23, 2024 · N301KH · Boeing 737330 · Fuselage Main, FrameSDR TSAA2024112600006Pressure Blkhd · crackedMAIN 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)Nov 23, 2024 · N301KH · Boeing 737330 · Fuselage Main, BulkheadSDR TSAA2024112600004Fuel Tank · corrodedSURFACE 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:CA1Nov 23, 2024 · N301KH · Boeing 737330 · Fuel StorageSDR TSAA2024112600003Fuel Tank · corrodedSURFACE 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 CONov 23, 2024 · N301KH · Boeing 737330 · Fuel StorageSDR TSAA2024112600002Attach Fitting · corrodedCORROSION 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 & 65-46881Nov 23, 2024 · N301KH · Boeing 737330 · Fuselage Main, BulkheadSDR TSAA2024112600001Cover · erodedEROSION (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 SURFACENov 23, 2024 · N301KH · Boeing 737330 · Vertical Stabilizer, Plate/SkinSDR TSAA202311074109Unknown · unknownDURING ECO 3925, DISCOVERED DENT AT BS 440R APPROX 5" FROM FLOOR, 1 1/4" WIDE, AND 0.07" DEEP.Nov 4, 2023 · N301KH · Boeing 737300 · Fuselage Structure (General)SDR TSAA202311074110Unknown · unknownDURING ECO 3925, DISCOVERED 2 RIVETS MISSING AT BS 360R JUST ABOVE FLOOR BOARD.Nov 4, 2023 · N301KH · Boeing 737300 · Fuselage Structure (General)SDR TSAA20230606107Unknown · unknownCA 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.Jun 6, 2023 · N301KH · Boeing 737330 · FastenersSDR TSAA20230606106Unknown · unknownCA 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 LIMIJun 6, 2023 · N301KH · Boeing 737330 · Fuselage Structure (General)SDR TSAA20230606105Unknown · unknownCA 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 CJun 6, 2023 · N301KH · Boeing 737330 · Wing StructureSDR TSAA20230606104Unknown · unknownCA 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 Jun 6, 2023 · N301KH · Boeing 737330 · Wing StructureSDR TSAA20230606103Unknown · unknownCA 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",Jun 6, 2023 · N301KH · Boeing 737330 · Fuselage Structure (General)SDR TSAA20230606102Unknown · unknownCA 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-Jun 6, 2023 · N301KH · Boeing 737330 · Fuselage Structure (General)SDR TSAA20230606101Unknown · unknownCA 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 51-10Jun 6, 2023 · N301KH · Boeing 737330 · Fuselage Structure (General)SDR TSAA20230606100Unknown · unknownCA 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 PJun 6, 2023 · N301KH · Boeing 737330 · Wing StructureSDR TSAA20230606099Unknown · unknownCA 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 Jun 6, 2023 · N301KH · Boeing 737330 · Wing StructureSDR TSAA20230606098Unknown · unknownCA 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 PJun 6, 2023 · N301KH · Boeing 737330 · Wing StructureSDR TSAA20230606097Unknown · unknownCA 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 CJun 6, 2023 · N301KH · Boeing 737330 · Wing StructureSDR TSAA20230606096Unknown · unknownCA 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 CLEAJun 6, 2023 · N301KH · Boeing 737330 · Wing StructureSDR TSAA20230606095Unknown · unknownCA 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 Jun 6, 2023 · N301KH · Boeing 737330 · Wing StructureSDR TSAA20230606094Unknown · unknownCA 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 R23-01849-001Jun 6, 2023 · N301KH · Boeing 737330 · Wing StructureSDR TSAA20230606093Unknown · unknownCA 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 Jun 6, 2023 · N301KH · Boeing 737330 · Wing StructureSDR TSAA20230606092Unknown · unknownCA 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 R23-01849-001RJun 6, 2023 · N301KH · Boeing 737330 · Wing StructureSDR TSAA20230606091Unknown · unknownCA 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 R23-01849-001RJun 6, 2023 · N301KH · Boeing 737330 · Wing StructureSDR TSAA20230606090Unknown · unknownCA 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 PROTJun 6, 2023 · N301KH · Boeing 737330 · Wing StructureSDR TSAA20230606089Unknown · unknownCA 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 / 5Jun 6, 2023 · N301KH · Boeing 737330 · Wing StructureSDR TSAA20230606088Unknown · unknownCA 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 7Jun 6, 2023 · N301KH · Boeing 737330 · Standard Practices/StructuresSDR TSAA20230606087Unknown · unknownCA 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 CLEAJun 6, 2023 · N301KH · Boeing 737330 · Wing StructureSDR TSAA20230606086Unknown · unknownCA 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. Jun 6, 2023 · N301KH · Boeing 737330 · Wing Structure
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