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 TSAA20230606085Unknown · unknownCA 1464/244 THE DENTS WERE FOUND AT LH WING O/B AFT FLAP LOWER SKIN, BETWEEN WBL 342.64 AND WBL 344.9 (WBL 342.9, L:0.8", W:0.6", D:0.008"),(WBL 343.9, L:0.8", W:0.4", D:0.002"). REMOVED SURFACE FINISH OF DENTS AND DID SURFACE PREPARATION AT LH WING O/B AFT FJun 6, 2023 · N301KH · Boeing 737330 · Wing StructureSDR TSAA20230606084Unknown · unknownCA 1464/243 THE DENT WAS FOUND AT LH WING O/B AFT FLAP LOWER SKIN, WBL 335.4, L:1.2 INCH, W:0.9 INCH, D:0.007 INCH. DENT AT LH WING O/B AFT FLAP LOWER SKIN WBL 335.4, L:1.2", W:0.9", D:0.007" CHECK WITHIN ALLOWABLE LIMIT. I.A.W. B737-300 SRM 57-53-01 ALLOWABJun 6, 2023 · N301KH · Boeing 737330 · Wing StructureSDR TSAA20230606083Unknown · unknownCA 1464/242 THE DENT WAS FOUND AT LH WING O/B AFT FLAP LOWER SKIN, WBL 287.05, L:2.8 INCH, W:2.7 INCH, D:0.070 INCH. REMOVED THE DAMAGE AREA AT LH WING O/B AFT FLAP LOWER SKIN WBL 287.05. MADE THE REPAIR SKIN AND DOUBLER. INSTALLED THE REPAIR PARTS AND PERFJun 6, 2023 · N301KH · Boeing 737330 · Wing StructureSDR TSAA20230606082Unknown · unknownCA 1464/241 THE DENTS WERE FOUND AT LH WING O/B AFT FLAP LOWER SKIN, BETWEEN WBL 276.55 AND WBL 281.05. (WBL 277.55, L:0.9", W:0.8", D:0.018"),(WBL 279.05, L:0.7", W:0.6", D:0.005"),(WBL 280.5, L:1.1", W:0.9", D:0.014"),(WBL 280.8, L:0.7", W:0.4" , D:0.003"). Jun 6, 2023 · N301KH · Boeing 737330 · Wing StructureSDR TSAA20230606081Unknown · unknownCA 1464/233 LIGHT CORROSION AT RUDDER LEADING EDGE RIB AT RUDDER STA 90 NEARBY RUDDER HINGE 4. ALL CORROSION REMOVED AT RUDDER LEADING EDGE RIB AT RUDDER STA 90 NEARBY RUDDER HINGE 4. REMOVED 0.002" MATERIAL & REMAINING 0.038" IS WITHIN ALLOWABLE LIMIT. AREJun 6, 2023 · N301KH · Boeing 737330 · Empennage StructureSDR TSAA20230606080Unknown · unknownCA 1464/232 LIGHT CORROSION AT LH SIDE VERTICAL STABILIZER EXTERNAL SKIN AT REAR SPAR AREA AT FIN STA 247. ALL CORROSION REMOVED AT LH SIDE VERTICAL STABILIZER EXTERNAL SKIN AT REAR SPAR AREA AT FIN STA 247. REMOVED 0.002" MATERIAL & REMAINING 0.097" IS WITHJun 6, 2023 · N301KH · Boeing 737330 · Empennage StructureSDR TSAA20230606079Unknown · unknownCA 1464/231 LIGHT CORROSION AT RH SIDE VERTICAL STABILIZER EXTERNAL SKIN AT REAR SPAR AREA AT FIN STA 79~93. ALL CORROSION REMOVED AT RH SIDE VERTICAL STABILIZER EXTERNAL SKIN AT REAR SPAR AREA AT FIN STA 79 ~ 93. REMOVED 0.002" MATERIAL & REMAINING 0.097" IJun 6, 2023 · N301KH · Boeing 737330 · Empennage StructureSDR TSAA20230606078Unknown · unknownCA 1464/230 CORROSION AT RH REAR FUSELAGE SKIN AT STA 1016, S-4R~S-9R. ALL CORROSION REMOVED AT RH REAR FUSELAGE SKIN AT STA 1016, S-4R ~ S-9R. REMOVED 0.003" MATERIAL & REMAINING 0.059" IS WITHIN ALLOWABLE LIMIT. AREA CLEAN & PROTECTIVE I.A.W. B737-300 SRMJun 6, 2023 · N301KH · Boeing 737330 · Fuselage Structure (General)SDR TSAA20230606077Unknown · unknownCA 1464/229 CORROSION AT RH REAR FUSELAGE SKIN AT STA 1088, S-3R~S-5R. ALL CORROSION REMOVED AT RH REAR FUSELAGE SKIN AT STA 1088, S-3R ~ S-5R. REMOVED 0.003" MATERIAL & REMAINING 0.060" WITHIN ALLOWABLE LIMIT. AREA CLEAN & PROTECTIVE I.AW. B737-300 SRM 51-Jun 6, 2023 · N301KH · Boeing 737330 · Fuselage Structure (General)SDR TSAA20230606076Unknown · unknownCA1464/199 SURFACE CORROSION ON CENTER WING EXTERIOR LOWER SKIN BS570 FORM RBL 44 TO RBL 50. CORROSION ON CENTER WING LOWER EXTERIOR SKIN BS570 FORM RBL 44 TO RBL 50, REPAIRED IAW AIR ASIA EL-737-230501. (V1 AEROSPACE, LLC REPAIR INSTRUCTION R23-01840-001)Jun 6, 2023 · N301KH · Boeing 737330 · Wing StructureSDR TSAA20230606075Unknown · unknownCA 1464/198 SURFACE CORROSION ON CENTER WING EXTERIOR LOWER SKIN BS645 LBL 47. CORROSION ON CENTER WING LOWER EXTERIOR SKIN BS600, BS640 AND BS645, REPAIRED IAW AIR ASIA EL-737-230502. (V1 AEROSPACE, LLC REPAIR INSTRUCTION R23-01839-003)Jun 6, 2023 · N301KH · Boeing 737330 · Wing StructureSDR TSAA20230606074Unknown · unknownCA 1464/197 SURFACE CORROSION ON CENTER WING EXTERIOR LOWER SKIN BS640 LBL44. CORROSION ON CENTER WING LOWER EXTERIOR SKIN BS600, BS640 AND BS645, REPAIRED IAW AIR ASIA EL-737-230502. (V1 AEROSPACE, LLC REPAIR INSTRUCTION R23-01839-002)Jun 6, 2023 · N301KH · Boeing 737330 · Wing StructureSDR TSAA20230606073Unknown · unknownCA 1464/196 SURFACE CORROSION ON CENTER WING LOWER EXTERIOR SKIN BS600 LBL 50. CORROSION ON CENTER WING LOWER EXTERIOR SKIN BS600, BS640 AND BS645. REPAIRED IAW AIR ASIA EL-737-230502. (V1 AEROSPACE, LLC REPAIR INSTRUCTION R23-01839-001)Jun 6, 2023 · N301KH · Boeing 737330 · Wing StructureSDR TSAA20230606072Unknown · unknownCA 1464/193 CORROSION AT R/H SIDE HORIZONTAL STABILIZER REAR SPAR UPPER SURFACE AT STAB STA 143 (1.0" X 0.4" IN AREA). ALL CORROSION REMOVED AT RH HORIZONTAL STABILIZER REAR SPAR UPPER SURFACE AT STAB STA 143 (1.0" X 0.4" IN AREA). REMOVED 0.020" AND REMAINIJun 6, 2023 · N301KH · Boeing 737330 · Empennage StructureSDR TSAA20230606071Unknown · unknownCA 1464/192 CORROSION AT R/H SIDE HORIZONTAL STABILIZER REAR SAPR UPPER SURFACE AT STAB STA 116 (0.5" X 0.2" IN AREA). ALL CORROSION REMOVED AT RH HORIZONTAL STABILIZER REAR SPAR UPPER SURFACE AT STAB STA 116 (0.5" X 0.2" IN AREA). REMOVED 0.015" AND REMAINIJun 6, 2023 · N301KH · Boeing 737330 · Empennage StructureSDR TSAA20230606070Unknown · unknownCA 1464/191 CORROSION AT L/H SIDE HORIZONTAL STABILIZER REAR SPAR UPPER SURFACE AT STAB STA 153 (1.2" X 0.3" IN AREA). ALL CORROSION REMOVED AT LH HORIZONTAL STABILIZER REAR SPAR UPPER SURFACE AT STAB STA 153 (1.2" X 0.3" IN AREA). REMOVED 0.040" AND REMAINIJun 6, 2023 · N301KH · Boeing 737330 · Empennage StructureSDR TSAA20230606069Unknown · unknownCA 1464/190 CORROSION AT L/H SIDE HORIZONTAL STABILIZER REAR SPAR UPPER SURFACE AT STAB STA 116. (1.0" X 0.3" IN AREA). ALL CORROSION REMOVED AT LH HORIZONTAL STABILIZER REAR SPAR UPPER SURFACE AT STAB STA 116 (1.0" X 0.3" IN AREA). REMOVED 0.002" AND REMAINJun 6, 2023 · N301KH · Boeing 737330 · Empennage StructureSDR TSAA20230606068Unknown · unknownCA 1464/186 CORROSION AT FUSELAGE CROWN DOUBLER BETWEEN STA 500 AND STA 540, S-1R AND S-2R, 14 AREA (L:3.1",W:2.2")(L:1.4",W:1.4")(L:0.9",W:0.5")(L:0.5",W:0.4") (L:1.9",W:0.7")(L:2.3",W:1.4")(L:1.7",W:1")(L:1.3",W:0.6")(L:1.1",W:0.6")(L:0.4",W:0.3)(L:0.8",W:0.Jun 6, 2023 · N301KH · Boeing 737330 · Fuselage Structure (General)SDR TSAA20230606067Unknown · unknownCA 1464/185 CORROSION AT FUSELAGE CROWN SKIN STA727, BETWEEN S-3L AND S-3R, 5 AREA (L:0.7",W:0.5")(L:1.5",W:0.6")(L:5.7"W:0.8)(L:1",W:0.5")(L:0.8",W:0.7"). ALL CORROSION REMOVED AT FUSELAGE CROWN SKIN AT STA 727, BETWEEN S-3L AND S-3R (L:0.7", W:0.5") (L:1.5"Jun 6, 2023 · N301KH · Boeing 737330 · Fuselage Structure (General)SDR TSAA20230606066Unknown · unknownCA 1464/184 CORROSION AT FUSELAGE SKIN STA 947.5, BETWEEN S-2R AND S-3R (L:5.6",W:1.4"). ALL CORROSION REMOVED AT FUSELAGE SKIN AT STA 947.5, BETWEEN S-2R AND S-3R (L:5.6", W:1.4"). REMOVED MATERIAL 0.003" AND REMAINING 0.037" IS WITHIN ALLOWABLE LIMIT. AREJun 6, 2023 · N301KH · Boeing 737330 · Fuselage Structure (General)SDR TSAA20230606065Unknown · unknownCA 1464/173 CORROSION AT LH WING I/B AFT FLAP UPPER SKIN BETWEEN WBL 88.5 AND WBL 90.5. ALL CORROSION REMOVED AT LH WING I/B AFT FLAP UPPER SKIN BETWEEN WBL 88.5 AND WBL 90.5. REMOVED MATERIAL 0.001" AND REMAINING 0.015" IS WITHIN ALLOWABLE LIMIT. AREA CLEAJun 6, 2023 · N301KH · Boeing 737330 · Wing StructureSDR TSAA20230606064Unknown · unknownCA1464/172 CORROSION AT LH WING I/B AFT FLAP UPPER SKIN BETWEEN WBL 84.0 AND WBL 85.5. ALL CORROSION REMOVED AT LH WING I/B AFT FLAP UPPER SKIN BETWEEN WBL 84.0 AND 85.5. REMOVED MATERIAL 0.001" AND REMAINING 0.015" IS WITHIN ALLOWABLE LIMIT. AREA CLEAN ANDJun 6, 2023 · N301KH · Boeing 737330 · Wing StructureSDR TSAA20230606063Unknown · unknownCA 1464/167 CORROSION AT LH WING I/B AFT FLAP LOWER SKIN BETWEEN WBL 116.0 AND WBL 118.0. ALL CORROSION REMOVED AT LH WING I/B AFT FLAP LOWER SKIN BETWEEN WBL 116.0 AND WBL 118.0. REMOVED MATERIAL 0.003" AND REMAINING 0.013" IS WITHIN ALLOWABLE LIMIT. AREA Jun 6, 2023 · N301KH · Boeing 737330 · Wing StructureSDR TSAA20230606062Unknown · unknownCA 1464/165 CORROSION AT LH WING I/B AFT FLAP LOWER SKIN BETWEEN WBL 92.75 AND WBL 94.05. ALL CORROSION REMOVED AT LH WING I/B AFT FLAP LOWER SKIN BETWEEN WBL 92.75 AND 94.05. REMOVED MATERIAL 0.003" AND REMAINING 0.013" IS WITHIN ALLOWABLE LIMIT. AREA CLEAJun 6, 2023 · N301KH · Boeing 737330 · Wing StructureSDR TSAA20230606061Unknown · unknownCA 1464/164 CORROSION AT LH WING I/B AFT FLAP LOWER SKIN BETWEEN WBL 87.25 AND WBL 91.25. ALL CORROSION REMOVED AT LH WING I/B AFT FLAP LOWER SKIN BETWEEN WBL 87.25 AND 91.25. REMOVED MATERIAL 0.001" AND REMAINING 0.015" IS WITHIN ALLOWABLE LIMIT. AREA CLEAJun 6, 2023 · N301KH · Boeing 737330 · Wing StructureSDR TSAA20230606060Unknown · unknownCA 1464/163 CORROSION AT LH WING I/B AFT FLAP LOWER SKIN BETWEEN WBL 86.25 AND WBL 87.25. ALL CORROSION REMOVED AT LH WING I/B AFT FLAP LOWER SKIN BETWEEN WBL 86.25 AND 87.25. REMOVED MATERIAL 0.001" AND REMAINING 0.015" IS WITHIN ALLOWABLE LIMIT. AREA CLEAJun 6, 2023 · N301KH · Boeing 737330 · Wing StructureSDR TSAA20230606059Unknown · unknownCA 1464/162 CORROSION AT LH WING I/B EXHAUST GATE LOWER SKIN WBL 183. ALL CORROSION REMOVED AT LH WING I/B EXHAUST GATE LOWER SKIN BETWEEN WBL 183. REMOVED MATERIAL 0.002" AND REMAINING 0.078" IS WITHIN ALLOWABLE LIMIT. AREA CLEAN AND PROTECTIVE IAW B737-30Jun 6, 2023 · N301KH · Boeing 737330 · Wing StructureSDR TSAA20230606058Unknown · unknownCA 1464/161 CORROSION AT LH WING I/B EXHAUST GATE LOWER SKIN WBL 169. ALL CORROSION REMOVED AT LH WING I/B EXHAUST GATE LOWER SKIN BETWEEN WBL 169. REMOVED MATERIAL 0.002" AND REMAINING 0.078" IS WITHIN ALLOWABLE LIMIT. AREA CLEAN AND PROTECTIVE IAW B737-30Jun 6, 2023 · N301KH · Boeing 737330 · Wing StructureSDR TSAA20230606057Unknown · unknownCA 1464/160 LH WING I/B FORE FLAP LOWER SKIN DELAMINATION BETWEEN WBL REPAIR IAW AIR ASIA EL-737-230504. (V1 AEROSPACE, LLC REPAIR INSTRUCTION R23-01844-001)Jun 6, 2023 · N301KH · Boeing 737330 · Wing StructureSDR TSAA20230606056Unknown · unknownCA 1464/140 CORROSION AT RH WINDOWS CUTOUT EDGE, BETWEEN STA 887 AND STA 907, (L:0.7",W:0.3"). ALL CORROSION REMOVED AT RH WINDOWS CUTOUT EDGE BETWEEN STA 887 AND STA 907 (L: 0.7", W:0.3"). REMOVED 0.003" IS WITHIN ALLOWABLE LIMIT. AREA CLEAN AND PROTECTIVEJun 6, 2023 · N301KH · Boeing 737330 · Window/Windshield SystemSDR TSAA20230606055Unknown · unknownCA 1464/139 CORROSION AT RH WINDOWS CUTOUT EDGE, BETWEEN STA 867 AND STA 887, (L:0.7",W:0.3"). ALL CORROSION REMOVED AT RH WINDOWS CUTOUT EDGE BETWEEN STA 867 AND STA 887. REMOVED 0.006" IS WITHIN ALLOWABLE LIMIT. AREA CLEAN AND PROTECTIVE IAW B737-300 SRM Jun 6, 2023 · N301KH · Boeing 737330 · Window/Windshield SystemSDR TSAA20230606054Unknown · unknownCA 1464/135 T-BRACKET LOWER SKIN CORROSION AT BS 508 /S26R. DAMAGE T-BRACKET REMOVED AT BS 508, S-26R. INSTALL NEW PARTS I.A.W. B737-300 SRM 51-40-2 PARA 4. P2 (R130).Jun 6, 2023 · N301KH · Boeing 737330 · Standard Practices/StructuresSDR TSAA20230606053Unknown · unknownCA 1464/129 SURFACE CORROSION ON FUSELAGE EXTERIOR SKIN BS500B/S24R+2". ALL CORROSION REMOVED AT FUSELAGE EXTERIOR SKIN BS5008, S-24R+2". REMOVED 0.001" AND REMAINING 0.070" IS WITHIN ALLOWABLE LIMIT. AREA CLEAN AND PROTECTIVE IAW B737-300 SRM 51-10-2, 51-2Jun 6, 2023 · N301KH · Boeing 737330 · Fuselage Structure (General)SDR TSAA20230606052Unknown · unknownCA 1464/123 CORROSION AT APU INLET DOOR AT STA 1064, S-15R. CORROSION AT APU INLET DOOR AT STA 1064, S-15R, REPAIRED IAW AIR ASIA EL-737-230506. (ASAP INC. EO 5323-075)Jun 6, 2023 · N301KH · Boeing 737330 · Fuselage Structure (General)SDR TSAA20230606051Unknown · unknownCA 1464/122 CORROSION AT RH SIDE FUSELAGE AT STA 1071, S-20R. ALL CORROSION REMOVED AT RH FUSELAGE AT STA 1071, S-20R.. REMOVED 0.002" MATERIAL AND REMAINING 0.073" IS WITHIN ALLOWABLE LIMIT. AREA CLEAN AND PROTECTIVE IAW B737-300 SRM 51-10-2, 51-20-01 AND Jun 6, 2023 · N301KH · Boeing 737330 · Fuselage Structure (General)SDR TSAA20230606050Unknown · unknownCA 1464/121 CORROSION AT REPAIRED DOUBLER SKIN AT STA 1076, S-17AR. ALL CORROSION REMOVED AT REPAIRED DOUBLER SKIN AT STA 1076.5, S-17AR. REMOVED 0.003" MATERIAL AND REMAINING 0.053" IS WITHIN ALLOWABLE LIMIT. AREA CLEAN AND PROTECTIVE IAW 8737-300 SRM 51-1Jun 6, 2023 · N301KH · Boeing 737330 · Fuselage Structure (General)SDR TSAA20230606049Unknown · unknownCA 1464/119 CORROSION AT RH SIDE FUSELAGE AT STA 1115-1128, S-20R. ALL CORROSION REMOVED AT RH FUSELAGE AT STA 1115-1128, S-20R. REMOVED 0.004" MATERIAL AND REMAINING 0.067" IS WITHIN ALLOWABLE LIMIT. AREA CLEAN AND PROTECTIVE IAW B737-300 SRM 51-10-2, 51Jun 6, 2023 · N301KH · Boeing 737330 · Fuselage Structure (General)SDR TSAA20230606048Unknown · unknownCA 1464/118 CORROSION AT RH SIDE FUSELAGE AT STA 1156, S-20R. CORROSION ON FUSELAGE SECTION 48 STRAP 65-45688-172 AT STA 1156, REPAIR IAW AIR ASIA EL-737-230507. (V1 AEROSPACE, LLC REPAIR INSTRUCTION R23-01859-001 R01)Jun 6, 2023 · N301KH · Boeing 737330 · Fuselage Structure (General)SDR TSAA20230606047Unknown · unknownCA 1464/117 LIGHT CORROSION AT RIVET AREA OF STRINGER AT STA 1040~1060, S-24L. ALL CORROSION REMOVED AT RIVET AREA OF STRINGER AT STA 1040~1060 S-24L. REMOVED 0.005" AND REMAINING 0.040" IS WITHIN ALLOWABLE LIMIT. AREA CLEAN AND PROTECTIVE IAW B737-300 SRM Jun 6, 2023 · N301KH · Boeing 737330 · Fuselage Structure (General)SDR TSAA20230606046Unknown · unknownCA 1464/116 LIGHT CORROSION AT ACCESS AND BLOWOUT DOOR CUTOUT AREA AT STA 1058, S-20L. ALL CORROSION REMOVED AT ACCESS AND BLOWOUT DOOR CUTOUT AREA AT STA 1058, S-20L. REMOVED 0.002" MATERIAL AND REMAINING 0.054" IS WITHIN ALLOWABLE LIMIT. AREA CLEAN AND PRJun 6, 2023 · N301KH · Boeing 737330 · Fuselage Structure (General)SDR TSAA20230606045Unknown · unknownCA 1464/115 LIGHT CORROSION AT ACCESS AND BLOWOUT DOOR CUTOUT AREA AT STA 1064, S-23L. ALL CORROSION REMOVED AT ACCESS AND BLOWOUT DOOR CUTOUT AREA AT STA 1064,S-23L. REMOVED 0.002" MATERIAL AND REMAINING 0.054" IS WITHIN ALLOWABLE LIMIT. AREA CLEAN AND PROJun 6, 2023 · N301KH · Boeing 737330 · Fuselage Structure (General)SDR TSAA20230606044Unknown · unknownCA 1464/114 DENT (1.0" X 0.5" IN AREA, MAX DEPTH=0.015") AT LH SIDE FUSELAGE EXTERNAL SKIN AT STA 1072, IN ABOVE S-22L 0.5" DENT (1.0" X 0.5" IN AREA, MAX DEPTH=0.015") AT LH FUSELAGE EXTERNAL SKIN AT STA 1072. ABOVE TO S-22L 0.5". CHECK WITHIN ALLOWABLE LIMJun 6, 2023 · N301KH · Boeing 737330 · Fuselage Structure (General)SDR TSAA20230606043Unknown · unknownCA 1464/99 CORROSION AT RH WINDOWS CUTOUT EDGE, BETWEEN STA 685 AND STA 706, 2 AREA (L:3.2",W:0.2")(L:0.5",W:0.3"). ALL CORROSION REMOVED AT RH WINDOWS CUTOUT EDGE BETWEEN STA 685 AND STA 706 (L:3.2", W:0.2") (L:0.5", W:0.3"). REMOVED 0.003", 0.004" IS WITHIJun 6, 2023 · N301KH · Boeing 737330 · Window/Windshield SystemSDR TSAA20230606042Unknown · unknownCA 1464/98 CORROSION AT RH WINDOWS CUTOUT EDGE, BETWEEN STA 663.75 AND STA 685 (L:4",W:0.3"). ALL CORROSION REMOVED AT RH WINDOWS CUTOUT EDGE BETWEEN STA 663.75 AND STA 685 (L:4", W:0.3"). REMOVED 0.003" IS WITHIN ALLOWABLE LIMIT. AREA CLEAN AND PROTECTIVE Jun 6, 2023 · N301KH · Boeing 737330 · Window/Windshield SystemSDR TSAA20230606041Unknown · unknownCA 1464/97 CORROSION AT RH WINDOWS CUTOUT EDGE, BETWEEN STA 597 AND STA 616 (L:0.4",W:0.4"). ALL CORROSION REMOVED AT RH WINDOWS CUTOUT EDGE BETWEEN STA 597 AND STA 616 (L:0.4", W:0.4"). REMOVED 0.009" IS WITHIN ALLOWABLE LIMIT. AREA CLEAN AND PROTECTIVE IAJun 6, 2023 · N301KH · Boeing 737330 · Window/Windshield SystemSDR TSAA20230606040Unknown · unknownCA 1464/96 CORROSION AT RH WINDOWS CUTOUT EDGE, BETWEEN STA 559 AND STA 578 (L:0.4",W:0.4"). ALL CORROSION REMOVED AT RH WINDOWS CUTOUT EDGE BETWEEN STA 559 AND STA 578 (L:0.4", W:0.4"). REMOVED 0.009" IS WITHIN ALLOWABLE LIMIT. AREA CLEAN AND PROTECTIVE IAJun 6, 2023 · N301KH · Boeing 737330 · Window/Windshield SystemSDR TSAA20230606039Unknown · unknownCA 1464/95 CORROSION AT RH WINDOWS CUTOUT EDGE, BETWEEN STA 540 AND STA 559, 2 AREA (L:0.7",W:0.5")(L:0.6",W:0.2"). ALL CORROSION REMOVED AT RH WINDOWS CUTOUT EDGE BETWEEN STA 540 AND STA 559 (L:0.7", W:0.5") (L:0.6", W:0.2"). REMOVED 0.006", 0.005" IS WITHIJun 6, 2023 · N301KH · Boeing 737330 · Window/Windshield SystemSDR TSAA20230606038Unknown · unknownCA 1464/94 CORROSION AT RH WINDOWS CUTOUT EDGE, BETWEEN STA 520 AND STA 540, 3 AREA (L:2",W:0.5")(L:0.5",W:0.5)(L:0.5",W:0.5"). ALL CORROSION REMOVED AT RH WINDOWS CUTOUT EDGE BETWEEN STA 520 AND STA E540 (L:2",W:0.5") (L:0.5",W:0.5") (L:0.5",W:0.5"). REMOJun 6, 2023 · N301KH · Boeing 737330 · Window/Windshield SystemSDR TSAA20230606037Unknown · unknownCA 1464/93 CORROSION AT RH WINDOWS CUTOUT EDGE, BETWEEN STA 500B AND STA 500C (L:0.6",W:0.5"). ALL CORROSION REMOVED AT RH WINDOWS CUTOUT EDGE BETWEEN STA 500B AND STA 500C. REMOVED 0.006" IS WITHIN ALLOWABLE LIMIT. AREA CLEAN AND PROTECTIVE IAW B737-300 SRJun 6, 2023 · N301KH · Boeing 737330 · Window/Windshield SystemSDR TSAA20230606036Unknown · unknownCA 1464/92 CORROSION AT RH WINDOWS CUTOUT EDGE, BETWEEN STA 500A AND STA 500B (L:0.5",W:0.4"). ALL CORROSION REMOVED AT RH WINDOWS CUTOUT EDGE BETWEEN STA 500A AND STA 500B (L:0.5",W:0.4"). REMOVED 0.004" IS WITHIN ALLOWABLE LIMIT. AREA CLEAN AND PROTECTIVEJun 6, 2023 · N301KH · Boeing 737330 · Window/Windshield System
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