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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR TSAA20230606035Unknown · unknownCA 1464/91 CORROSION AT RH WINDOWS CUTOUT EDGE, BETWEEN STA 400 AND STA 420 (L:0.5",W:0.3"). ALL CORROSION REMOVED AT RH WINDOWS CUTOUT EDGE BETWEEN STA 400 AND STA 420 (L:0.5",W:0.3"). REMOVED 0.005" IS WITHIN ALLOWABLE LIMIT. AREA CLEAN AND PROTECTIVE IAWSDR TSAA20230606033Unknown · unknownCA 1464/101 CORROSION AT FUSELAGE SKIN BETWEEN STA 685 AND STA 706, S-11R AND S-12R (L:3.5", W:1"). ALL CORROSION REMOVED AT FUSELAGE SKIN BETWEEN STA 685 AND STA 706, S-11R AND S-12R (L:3.5", W:1"). REMOVED 0.004" AND REMAINING 0.114" IS WITHIN ALLOWABLE LISDR TSAA20230606032Unknown · unknownCA 1464/83 CORROSION AT RH WING O/B T/E EXHAUST GATE TRAILING EDGE WEDGE BETWEEN WBL 202.5 AND WBL 224. ALL CORROSION REMOVED AT RH WING I/B EXHAUST GATE LOWER SKIN BETWEEN WBL 202.5 AND WBL 224. REMOVED MATERIAL 0.002" AND REMAINING 0.018" IS WITHIN ALLOWABSDR TSAA20230606031Unknown · unknownCA 1464/77 CORROSION AT RH WING I/B MIDDLE FLAP LOWER SKIN BETWEEN WBL 74 AND WBL 114.5. ALL CORROSION REMOVED AT RH WING I/B MIDDLE FLAP LOWER SKIN BETWEEN WBL 74 AND WBL 114.5. REMOVED MATERIAL 0.009" AND REMAINING 0.116" IS WITHIN ALLOWABLE LIMIT. AREA CSDR TSAA20230606030Unknown · unknownCA 1464/76 CORROSION AT RH WING I/B EXHAUST GATE LOWER SKIN BETWEEN WBL 169 AND WBL 183. ALL CORROSION REMOVED AT RH WING I/B EXHAUST GATE LOWER SKIN BETWEEN WBL 169 AND WBL 183. REMOVED MATERIAL 0.002" AND REMAINING 0.018" IS WITHIN ALLOWABLE LIMIT. AREA CSDR TSAA20230606029Unknown · unknownCA 1464/75 CORROSION AT RH WING I/B AFT FLAP LOWER NOSE SKIN BETWEEN WBL 120 AND WBL 146. ALL CORROSION REMOVED AT RH WING I/B AFT FLAP LOWER NOSE SKIN BETWEEN WBL 120 & WBL 146. REMOVED 0.007" MATERIAL AND REMAINING 0.009" OVER LIMIT. PERFORM REPAIR I.A.W. SDR TSAA20230606028Unknown · unknownCA 1464/61 CORROSION AT LH WINDOWS CUTOUT EDGE, BETWEEN STA 907 AND STA 927, 6 AREA (L:1.3",W:0.5")(L:0.7",W:0.5")(L:0.8",W:0.5")(L:1",W:0.5")(L:0.3",W:0.3")(L:0.6",W:0.2"). ALL CORROSION REMOVED AT LH WINDOWS CUTOUT EDGE BETWEEN STA 907 AND STA 927 (L:1.3",WSDR TSAA20230606027Unknown · unknownCA 1464/60 CORROSION AT LH WINDOWS CUTOUT EDGE, BETWEEN STA 887 AND STA 907, 3 AREA (L:0.8", W:0.4")(L:0.3", W:0.3")(L:7.5", W:0.6"). ALL CORROSION REMOVED AT LH WINDOWS CUTOUT EDGE BETWEEN STA 887 AND STA 907 (L:0.8, W:0.4")(L:0.3", W:0.3")(L:7.5", W:0.6"). SDR TSAA20230606026Unknown · unknownCA 1464/59 CORROSION AT LH WINDOWS CUTOUT EDGE, BETWEEN STA 867 AND STA 887, 8 AREA (L:1.9", W:0.4")(L:1.6", W:0.5")(L:1.7", W:0.5")(L:1.9", W:0.5")(L:2.9", W:0.5")(L:0.4", W:0.3")(L:0.5, W:0.3")(L:0.5", W:0.4"). ALL CORROSION REMOVED AT LH WINDOWS CUTOUT EDGSDR TSAA20230606025Unknown · unknownCA 1464/58 CORROSION AT LH WINDOWS CUTOUT EDGE, BETWEEN STA 847 AND STA 867, 8 AREA (L:5.5", W:0.5")(L:1.7", W:0.5")(L:0.6", W:0.3")(L:0.5", W:0.3")(L:1.1", W:0.6")(L:0.5", W:0.4")(L:0.9", W:0.5")(L:1.6", W:0.5"). ALL CORROSION REMOVED LH WINDOWS CUTOUT EDGE,SDR TSAA20230606024Unknown · unknownCA 1464/57 CORROSION AT LH WINDOWS CUTOUT EDGE, BETWEEN STA 827 AND STA 847, 3 AREA (L:1", W:0,3")(L:2,7", W:0.5")(L:1.4", W:0.5"). ALL CORROSION REMOVED AT LH WINDOWS CUTOUT EDGE, BETWEEN STA 827 AND STA 847 (L:1", W:0.3")(L:2.7", W:0.5")(L:1.4", W:0.5"). RSDR TSAA20230606023Unknown · unknownCA 1464/56 CORROSION AT LH WINDOWS CUTOUT EDGE, BETWEEN STA 807 AND STA 827, 5 AREA (L:1", W:0.5")(L:0.4", W:0.3")(L:0.5", W:0.5")(L:0.6", W:0.4")(L:0.5", W:0.4"). ALL CORROSION REMOVED AT LH WINDOWS CUTOUT EDGE BETWEEN STA 807 AND STA 827 (L:1", W:0.5")(L:0.SDR TSAA20230606022Unknown · unknownCA 1464/55 CORROSION AT LH WINDOWS CUTOUT EDGE, BETWEEN STA 787 AND STA 807, 2 AREA (L:0.4", W:0.2")(L:1.1", W:0.5"). ALL CORROSION REMOVED AT LH WINDOWS CUTOUT EDGE, BETWEEN STA 787 AND STA 807 (L:0.4", W:0.2")(L:1.1", W:0.5"). REMOVED 0.002", 0.004" MATERISDR TSAA20230606021Unknown · unknownCA 1464/54 CORROSION AT LH WINDOWS CUTOUT EDGE, BETWEEN STA 767 AND STA 787, 2 AREA (L:0.9",W:0.3")(L:1.2", W:0.3"). ALL CORROSION REMOVED AT LH WINDOWS CUTOUT EDGE, BETWEEN STA 767 & STA 787, 2 AREA (L:0.9",W:0.3")(L:1.2", W:0.3"). REMOVED 0.003" MATERIAL ISDR TSAA20230606020Unknown · unknownCA 1464/53 CORROSION AT LH WINDOWS CUTOUT EDGE, BETWEEN STA 747 AND STA 767 (L:4.6", W:0.5"). ALL CORROSION REMOVED AT LH WINDOWS CUTOUT EDGE BETWEEN STA 747 & STA 767 (L:4.6", W:0.5"). REMOVED 0.006" MATERIAL IS WITHIN ALLOWABLE LIMIT. AREA CLEAN AND PROTESDR TSAA20230606019Unknown · unknownCA 1464/52 CORROSION AT LH WINDOWS CUTOUT EDGE, BETWEEN STA 727E AND STA 747 (L:0.7", W:0.5"). ALL CORROSION REMOVED AT LH WINDOWS CUTOUT EDGE BETWEEN STA 727E AND STA 747 (L:0.7", W:0.5"). REMOVED 0.0078" MATERIAL IS WITHIN ALLOWABLE LIMIT. AREA CLEAN AND SDR TSAA20230606018Unknown · unknownCA 1464/50 CORROSION AT FUSELAGE SKIN STA 907, BETWEEN S-15L AND S-16L (L:10", W:0.5"). ALL CORROSION REMOVED AT FUSELAGE SKIN STA 907, BETWEEN S-15L & S-16L (L:10", W:0.5"). REMOVED 0.004" MATERIAL AND REMAINING 0.061" IS WITHIN ALLOWABLE LIMIT. AREA CLEANSDR TSAA20230606017Unknown · unknownCA 1464/49 CORROSION AT FUSELAGE SKIN STA 947.5, BETWEEN S-13L AND S-16L, 2 AREA (L:11", W:0.7")(L:5", W:1"). REMOVED MATERIAL AND REMAINING IS WITHIN ALLOWABLE LIMIT. AREA CLEAN AND PROTECTIVE IAW B737-300 SRM 51-10-2, 51-20-01 AND 53-00-01 ALLOWABLE DAMAGESDR TSAA20230606016Unknown · unknownCA 1464/37 MAIN DECK CARGO DOOR SEAL RETAINER CRACK ON FWD LOW CORNER. DAMAGE SEAL RETAINER REMOVED AT FWD LOWER CORNER MAIN DECK CARGO DOOR. INSTALL NEW PARTS IAW B737-300 SRM 51-40-2 PARA 4 P2 (R130).SDR TSAA20230606015Unknown · unknownCA 1464/31 FILIFORM CORROSION WERE FOUND ON THE AFT CARGO DOOR EXTERNAL SKIN EDGE AND HANDLE CUTOUT COVER AS MARK. ALL CORROSION REMOVED AT AFT CARGO DOOR EXTERNAL SKIN EDGE AND HANDLE CUTOUT COVER. REMOVED 0.001" MATERIAL AND REMAINING 0.035" IS WITHIN ALLOSDR TSAA20230606014Unknown · unknownCA 1464/22 FILIFORM CORROSION WERE FOUND ON FUSELAGE EXTERNAL SKIN AFT CARGO CUTOUT FWD EDGE AS MARK. ALL CORROSION REMOVED AT FUSELAGE EXTERNAL SKIN AFT CARGO CUTOUT FWD EDGE. REMOVED 0.001" MATERIAL AND REMAINING 0.035" IS WITHIN ALLOWABLE LIMIT. AREA CLESDR TSAA20230606013Unknown · unknownCA 1464/21 FILIFORM CORROSION WERE FOUND ON FUSELAGE EXTERNAL SKIN LH SIDE STRINGER 27 STATION 987, 900 TO 903. ALL CORROSION REMOVED AT FUSELAGE EXTERNAL SKIN S-27L STA 987, STA 900 TO STA 903. REMOVED MATERIAL AND REMAINING IS WITHIN ALLOWABLE LIMIT. AREASDR TSAA20230606012Unknown · unknownCA 1464/20 FILIFORM CORROSION WERE FOUND ON FUSELAGE EXTERNAL SKIN LH SIDE STRINGER 26 STATION 900 TO 905. ALL CORROSION REMOVED AT FUSELAGE EXTERNAL SKIN S-26L, STA 900 TO 905. REMOVED 0.002" MATERIAL AND REMAINING 0.061" IS WITHIN ALLOWABLE LIMIT. AREA CLSDR TSAA20230606011Unknown · unknownCA 1464/19 FILIFORM CORROSION WERE FOUND ON FUSELAGE EXTERNAL SKIN RH SIDE STRINGER 27 STATION 938 TO 951, 903 TO 907.
ALL CORROSION REMOVED AT FUSELAGE EXTERNAL SKIN AT S-27R STA 938 TO STA 951, STA 903 TO STA 907. REMOVED MATERIAL AND REMAINING IS WITHINSDR TSAA20230606010Unknown · unknownCA 1464/18 FILIFORM CORROSION WERE FOUND ON FUSELAGE EXTERNAL SKIN RH SIDE STRINGER 26 STATION 922, 926 TO 928, 938 TO 942, 954 TO 957, 982 TO 990. ALL CORROSION REMOVED AT FUSELAGE EXTERNAL SKIN AT S-26R STA 922, STA 926 TO STA 928, STA 938 TO STA 942, STA 9SDR TSAA20230606009Unknown · unknownCA 1464/17 FILIFORM CORROSION WERE FOUND ON FUSELAGE EXTERNAL SKIN LH SIDE STA 986 BETWEEN STRINGER 18 AND 19. ALL CORROSION REMOVED AT FUSELAGE EXTERNAL SKIN AT STA 986 BETWEEN S-18L AND S-19L. REMOVED MATERIAL 0.002" AND REMAINING 0.069" IS WITHIN ALLOWABLSDR TSAA20230606008Unknown · unknownCA 1464/16 FILIFORM CORROSION WERE FOUND ON FUSELAGE EXTERNAL SKIN LH SIDE STRINGER 25 STATION 827 TO 847, 881 TO 901. ALL CORROSION REMOVED AT FUSELAGE EXTERNAL SKIN AT S-25L STA 827 TO STA 847, STA 881 TO STA 901. REMOVED MATERIAL AND REMAINING IS WITHIN ASDR TSAA20230606007Unknown · unknownCA 1464/14 FILIFORM CORROSION WERE FOUND ON FUSELAGE EXTERNAL SKIN LH SIDE STRINGER 20 STATION 727D TO 727D+3, 747 TO 787, 825 TO 827, 868 TO 897 AND 986 TO 990. ALL CORROSION REMOVED AT FUSELAGE EXTERNAL SKIN AT S-20L STA 727D TO STA 727+3, STA 747 TO STA 78SDR TSAA20230606006Unknown · unknownCA 1464/12 LIGHT CORROSION ON R/H OVERWING EMERGENCY EXIT HATCH AT LOW PORTION. ALL CORROSION REMOVED AT R/H OVERWING EMERGENCY EXIT HATCH AT LOW PORTION. REMOVED 0.002" MATERIAL AND REMAINING 0.061" IS WITHIN ALLOWABLE LIMIT. AREA CLEAN AND PROTECTIVE IAW SDR TSAA20230606005Unknown · unknownCA 1464/10 FILIFORM CORROSION WERE FOUND ON FUSELAGE EXTERNAL SKIN RH SIDE STRINGER 17 STATION 747 TO 767, STRINGER 24 STATION 847 TO 854. ALL CORROSION REMOVED AT FUSELAGE EXTERNAL SKIN AT S-17R STA 747 TO STA 767, S-24R STA 847 TO STA 854. REMOVED MATERIALSDR TSAA20230606004Unknown · unknownCA 1464/8 FILIFORM CORROSION WERE FOUND ON FUSELAGE EXTERNAL SKIN RH SIDE STRINGER 25 STATION 868 TO 907, 947 TO 957, 990 TO 1006. ALL CORROSION REMOVED AT FUSELAGE EXTERNAL SKIN AT S-25R STA 868 TO STA 907, STA 947 TO STA 957, STA 990 TO 1006. REMOVED MATERSDR TSAA20230606003Unknown · unknownCA 1464/7 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 FUSELAGE EXTERNAL SKIN AT S-20R STA 767 TO STA 787, STA 867 TO STA 897, STA 927 TO STA 929. REMOVED MATSDR TSAA20230606002Unknown · unknownCA 1464/6 FILIFORM CORROSION WERE FOUND ON FUSELAGE EXTERNAL SKIN STATION 1016 BETWEEN LH SIDE STRINGER 17 TO 20 AND RH SIDE STRINGER 17-25. ALL CORROSION REMOVED AT FUSELAGE EXTERNAL SKIN AT STA 1016 BETWEEN S-17L TO S-20L AND S-17R TO S-25R. REMOVED 0.002" SDR TSAA20230606001Unknown · unknownCA 1464/5 FILIFORM CORROSION WERE FOUND ON FUSELAGE EXTERNAL SKIN STATION 907 BETWEEN LH SIDE STRINGER 17 AND RH SIDE STRINGER 17. ALL CORROSION REMOVED AT FUSELAGE EXTERNAL SKIN AT STA 907 BETWEEN LH SIDE S-17 AND RH SIDE S-17. REMOVED 0.001" MATERIAL AND RESDR TSAA20220927001None · noneFLIGHT CREW REPORTED INSOLATION COMING THROUGH RH NOSE WHEEL WELL. SUSPECT CRACK APPROXIMATELY 4 INCHES LONG.SDR TSAA20211117054None · noneCOMPLIED WITH AD 2013-04-05, PERFORMED EXTERNAL HFEC & INTERNAL HFEC INSPECTION FOR ANY CRACKS & CORROSION IAW ALOHA AIR CARGO ECO 3849 PART III REV 2 PARAGRAPH D&H. 3 CRACKS FOUND. REF NOT REPORT #'S NDT21-1508 & NDT21-1529. SEE W/O# 1000580928 FOR RECTIFICATSDR TSAA20211117030None · noneREPLACED CRACKED STRINGER CLIP STA 727A STR 4R IAW ALOHA AIR CARGO ECO 3759 REV 2 DATE 3/20/17. IAW B737-300 SRM REV 125 51-40-02.SDR TSAA20211117031Stringer Clip · crackedREPLACED STRINGER CLIP STA 727L STR 5R IAW ALOHA AIR CARGO ECO 3759 REV 2 DATE 3/20/17. FASTENERS INSTALLED IAW B737-300 SRM 51-40-02 PG 2 REV 125.SDR TSAA20211117032Stringer Clip · crackedREPLACED STRINGER CLIP @ STA 727C STR 7L IAW ALOHA AIR CARGO ECO 3759, REV 2, 3/20/17 PARA 8.0 PART III FIG 16 + IAW B737-300 SRM CH 51-40-02 REV 125.SDR TSAA20211117033Stringer Clip · crackedREPLACED STRINGER CLIP STA 727D STR 1 IAW ALOHA AIR CARGO ECO 3759 REV 2 DATE 3/20/17. FASTENERS INSTALLED IAW B737-300 SRM 51-40-02 PG 2 REV 125.SDR TSAA20211117034Stringer Clip · crackedREPLACED CRACKED STRINGER CLIP STA 727D STR 2R IAW ALOHA AIR CARGO ECO 3759 REV 2 DATE 3/20/17 IAW B737-300 SRM REV 125 51-40-02.SDR TSAA20211117035Stringer Clip · crackedREPLACED STRINGER CLIP @ STA. 727D STR. 5R IAW ECO NO.3759R2 DATED 3/20/17. FASTENERS INSTALLED IAW B737-300 SRM 51-40-02 REV.125.SDR TSAA20211117036Stringer Clip · crackedREPLACED CRACKED STRINGER CLIP @ STA 727E, STR 1 IAW ALOHA AIR CARGO ECO 3759 REV 2, DATE 3/20/17, PARA 8.0, PART III, FIG 16. FASTENERS INSTALLED IAW 8737-300 SRM CH 51-40-02, REV 125.SDR TSAA20211117037Stringer Clip · crackedREPLACED CRACKED STRINGER CLIP STA 727E STR 5L IAW ALOHA AIR CARGO ECO 3759 REV 2 DATE 3/20/17, IAW 8737-300 SRM REV 125 51-40-02.SDR TSAA20211117038Stringer Clip · crackedREPLACED STRINGER CLIP STA 887 STR 4R IAW ALOHA AIR CARGO ECO 3759 REV 2 DATE 3/20/17. FASTENERS INSTALLED IAW 8737-300 SRM 51-40-02 PG 2 REV 125.SDR TSAA20211117039Stringer Clip · crackedREPLACED STRINGER CLIP STA 685 STR10L IAW ALOHA AIR CARGO ECO 3759 REV 2 3/20/17 PARA 8.0 PART III FIGURE 16.SDR TSAA20211117040Doubler · corrodedCORROSION ON VHF ANTENNA DOUBLER HAT SECTION STA 727D-727E,LBL 2 TO RBL 2 INSPECTION CARRIED OUT, NO CORROSION PERMITTED IAW BOEING SB 737-53-1287 REV 1. DATED NOV 15 2010 REPLACED VHF ANTENNA HAT SECTION STA 727D-727E, LBL 2 TO RBL 2 IAW BOEING SB 737-53-1287SDR TSAA20211117041None · noneREPLACED AUXILIARY CHORD AT STA 727 LH BETWEEN STR 17L & STR 22L. I.A.W. B737-300 SRM REV 126 CH 51-40-02 REF BOEING DOC #65-46547 REV:DK.SDR TSAA20211117042Wire · damagedINSPECTED FIRE DETECTION WIRES, FOUND TO BE WITHIN REPAIRABLE LIMITS, REQUIRED WIRES AND APPLIED CHAF PROTECTION NEAR CONNECTOR D3304 O/B #2 ENGINE UPPER CORE SECTION. IAW B737-300 WDM 26-11-21 REV 56 AND BSWPM 20-10-13 REV 78 SERVICEABLE.SDR TSAA20211117043Fork · abnormalREPLACED CONDUCTIVE FRAME FROM UPPER CORNER L/H SIDE OF RUDDER STA 237.64 - FWL 230.25 WITH MADE REPAIR PART I.A.W. B737-300 SRM REV 126 CHP. 55-40-01 AND CHP 51-40-02-0G-O PARA 9,10,11 AND BOEING DWG 65C25841 REV C.
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