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 TSAA20211117044Skin Panel · crackedCRACKED PANEL ON UPPER SURFACE OF L/H PYLON @ WBL 180, 60" AFT OF LIE SPAR REPLACED WITH NEW PART IAW B737-300 SRM REV 125 51-40-02 PAR 9.SDR TSAA20211117045Fastener · corrodedREMOVED & REINSTALLED FASTENER IN L/H WING UPPER SKIN @ WBL 522-560 30" FWD OFT/E I.A.W. B737-300 SRM REV 126 CH 51-40-02 PAR 7, RE-PROTECTED I.A.W. B737-300 AMM REV 94 CH 51-21-99. INSPECTED WITH 1OX MAG GLASS, CONFIRMED THERE WAS NO CORROSION LIMITED TO PAINSDR TSAA20211117029Stringer Clip · cracked1000605593 - REPLACED STRINGER CLIP@ STA 685, STR 7L IAW ALOHA AIR CARGO ECO 3759 REV 2, DATE 3/20/17, PARA 8.0 PART ILL FIG16. + IAW B737-300 SRM CH 51-40-02 REV 125.SDR TSAA20211117028Stringer · cracked1000605592 - REPLACED STRINGER CLIP@ STA639 STR. 2R IAW ECO NO.3759R2 DATED 3/20/17. FASTENERS INSTALLED IAW B737-300 SRM 51-40-02 REV. 125.SDR TSAA20211117046Skin Panel · crackedREPAIRED CRACKED FIXED LEADING EDGE SKIN ON RIGHT WING STA 196, JUST I/B OF PYLON I.A.W. B737-300 SRM 57-41-01 REPAIR 9 REV. 125.SDR TSAA20211117027Stringer Clip · cracked1000605591 - REPLACED STRINGER CLIP@ STA 597 STR 7L IAW ECO. NO. 3759R2 DATED 3/20/17. FASTENERS INSTALLED IAW B737-300 SRM 51-40-02 REV.125SDR TSAA20211117047Intercostal · corrodedCORROSION ON INTERCOSTAL UNDER ANCHOR NUT @ STA 500A+18" BETWEEN STR 25L-26L REMOVED I.A.W. SRM REV 125 CH 51-10-02. NOMINAL THICKNESS: 0.020", REMAINING THICKNESS: 0.011". MATERIAL REMOVAL OF 0.009" IS NOT WITHIN ALLOWABLE LIMITS OF 0.002" I.A.W. B.737-300 SRSDR TSAA20211117026Flange · corroded1000582166 - REPAIRED FWD FLANGE ON O/B CHORD@ B.S 727 R/H STR 18R I.AW KF AEROSPACE DWG #R27904.1-053-017-001 REV NC AND BOEING PREVENTATIVE MOD SB 737-53A1166 REV 2 DATED JUNE 30, 1994SDR TSAA20211117048Intercostal · corrodedCORROSION ON INTERCOSTAL UNDER ANCHOR NUT @ STA 5008+2" BETWEEN STR 25L-26L REMOVED I.A.W. B.737-300 SRM REV 125 CH 51-10-02. NOMINAL THICKNESS:0.020", REMAINING THICKNESS:0.008". MATERIAL REMOVAL OF 0.012" IS NOT WITHIN ALLOWABLE LIMIT OF 0.002" I.A.W. B.737-SDR TSAA20211117025Skin · cracked1000582164 - REPAIRED CRACKS ON SKIN AT O/B CHORD@ B.S 727 LH STR 18L I.AW KF AEROSPACE DWG NO R27904.1-053-020-001 REV:NC AND BOEING PREVENTATIVE MOD SB 737-531166 REV 2 DATED JUNE
30,1994. AMOC ATTACHED.SDR TSAA20211117049Beltframe · gougedPERFORMED HFEC SURFACE INSPECTION ON BLENDED AREAS ON BELTFRAME STA 727B STR 20R-23R. NO CRACKS FOUND. SEE EXECAIRE WO #498478. REMOVED GOUGES ON I/B FLANGE OF BELTFRAME, STA 727B STR 20R-23R IAW B737-300 SRM REV 125 51-10-02 PARA 5. NOM THICK .063", REMOVED .SDR TSAA20211117024Hinge Fitting · cracked1000582023 - CRACKED INDICATION@ MAIN CARGO DOOR AFT MOST OUTER HINGE PLATE {HINGE ON DOOR)@ STA 500A-500B REPAIRED IAW AEI EO15562 REV IR.SDR TSAA20211117050Fill Port · corrodedCORROSION ON FILL PORT L/H WING PORT OPENING CORRODED BEYOND LIMITS. REPLACED FILL PORT WITH MADE REPAIR PART I.A.W. B737-300 SRM REV 125 CH 51-40-02, REF BOEING DOC #65-45461 REV:M.SDR TSAA20211117051Stringer Clip · crackedREPLACED STRINGER CLIP STA 685 STR 10L IAW ALOHA AIR CARGO ECO 3759 REV 2 3/20/17 PARA 8.0 PART III FIGURE 16.SDR TSAA20211117023Intercostal · cracked1000582022 - REPLACED INTERCOSTAL AT STA 328, LBL 47 FWD GALLEY FLOOR STRUCTURE IAW BOEING DRAWING NUMBER 65-45834 REV HD, FASTENERS INSTALLED IAW B737-300 SRM 51-40-02 PG 2 REV 125.SDR TSAA20211117052None · 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 TSAA20211117053Beltframe · crackedREPLACED BELTFRAME @ FS 440 R/H SIDE BETWEEN ST 17R-16R WITH MADE REPAIR PART IAW B737-300 SRM REV 125 51-10-02 PARA 8. INSTALLED BELTFRAME IAW BOEING DWG 65-20722 REV: AH AND
B737-300 SRM REV 125 51-40-02.SDR TSAA20211117022Bulkhead Web · cracked1000581539 - REPAIRED CRACK EMANATING FROM FASTENER ON STA 1016 BULKHEAD AT CABIN FLOOR LEVEL AT LBL9 AFT FACE OF BULKHEAD IAW KF AEROSPACE DRAWING #R27904.1-53-018-001 REV NC.SDR TSAA20211117021Antenna · cracked1000580928 - CRACKS FOUND (X4) COMMON TO THE FOOTPRINT OF THE #3 VHF ANTENNA REPAIR REMOVED IAW SB737-53-1287 REV 1 NOVE 15, 2010 AND REPAIRED IAW DWG NO.R27904.1-053-021-001 REV NC.SDR TSAA20211117055Pitot System · noneCOMPLIED WITH AD 2019-09-01. PERFORMED PITOT-STATIC MOD, TEMPERATURE PROBE AND ALPHA VANE ANTI-ICING SYSTEM TEST SERVICEABLE I.A.W. ALOHA AIR CARGO ECO 4233 PT.II, REV.1
DATE: 9/17/2021.SDR TSAA20211117056Stringer Splice · crackedCOMPLIED WITH AD 2014-01-05, PERFORMED INSPECTION OF STRINGER SPLICES AND BUTT STRAPS AND REPLACEMENT IAW ALOHA AIR CARGO ECO 3866, PT. II, REVISION 1, DATE: 8/17/17, CRACKS FOUND. SEE NDT REPORT NDT21-1540 ON STRINGER SPLICE AT STA 908 AT STR 4R & 4L CRACKS SDR TSAA20211117020Beltframe · dented1000578902 - DENT ON BELT FRAME STA 727B STR24R ASSESSED IAW B737-300 SRM REV 125 CH 53-00-07 FIG 101 SHEET 2 NOTE E AND FOUND TO BE BEYOND ALLOWABLE LIMITS. DENT IS ON THE FREE FLANGE AND NOTE
E STATES, "DENTS ALLOWED IN FRAME WEBS ONLY" REPLACED DENTED BELTSDR TSAA20211117019Beltframe · dented1000578901 - DENTS (X2) ON BELT FRAME STA 727C STR 23L-25L ASSESSED IAW B737-300 SRM REV 125 CH 53-00-07 FIG 101 SHEET 2 NOTE E AND FOUND TO BE BEYOND ALLOWABLE LIMITS. DENTS ARE ON THE FREE FLANGE. NOTE ESTATES "DENTS ARE ALLOWED, IN FRAME WEB ONLY". DENTED BSDR TSAA20211117057Anti-Ice System · failed inspCOMPLIED WITH AD 2019-09-01, INSTALL NEW J18 JUNCTION BOX TO CHANGE ANTI-ICING SYSTEM MOD, AND WIRING PROVISIONS TO ANTI-ICING SYSTEM IAW ALOHA AIR CARGO ECO 4233 PART 3, REV 1.SDR TSAA20211117018Beltframe · gouged1000575816 - DENT/ GOUGE ON BELT FRAME REPAIR MEMBER INNER FLANGE@ F.S. 500 RH SIDE BETWEEN STR 17R-16R BEYOND LIMITS AND REPLACED WITH NEW FABRICATED REPAIR MEMBER IAWAEI ENGINEERING ORDER # EO9520 REV IRSDR TSAA20211117017Angle · cracked1000575571 - CRACKED L-ANGLE ON FLOOR STRUCTURE AT FWD WET AREA STA 328, RBL 32, WL 200 REPLACED WITH MADE REPAIR PART FABRICATED AND INSTALLED I.AW B.737-300 SRM REV 125 CH 51-30-01 AND
51-40-02. REFERENCE BOEING DWG 65-45812 ID:0003 REV: LAND PL REV: CR FORSDR TSAA20211117016Anchor Fitting · cracked1000575570 - X2 CRACKED L-ANGLES FROM FRAMES TO WEB IN E&E BAY STA'S 320 AND 328 BETWEEN STR 20L AND 21L WERE REPLACED WITH MADE REPAIR PARTS FABRICATED AND INSTALLED I.AW B.737-300 SRM
REV 125 CH 51-30-01 AND 51-40-02. REFERENCE BOEING DWG 65-54892 ID:0002 RSDR TSAA20211117015Scuff Plate · corroded1000573102 - BLENDED CORROSION ON R1 DOOR ATTACH ANGLE FOR LOWER SCUFF PLATE RBL 57 STA 294.5+4 TO STA 328. IAW B737-300 SRM 53-10-15 PG 113 DETAIL IX REV 125. FOUND TO BE BEYOND LIMITS NOM THICKNESS .090", .040" REMOVED, .050 REMAINING IAW B737-300 SRM 53-60-SDR TSAA20211117014Failsafe · broken1000573101- REPLACED FAIL SAFE ANGLE AT STA 420 STR 26L IAW REFERENCE BOEING DRAWING #65-46527 ID:0011 REV A & B737-300 SRM REV 125 CHAPTER 51-40-02 WITH MADE REPAIR PART.SDR TSAA20211117013Floorbeam · corroded1000573059 - CORROSION ON FLOORBEAM TOP CAP@ STA1006, RBL20 REPAIRED IAW AEI EO15495 REV IRSDR TSAA20211117012Floorbeam · corroded1000573058 - CORROSION ON FLOORBEAM TOP CAP@ STA 887 RBL 47 BLENDED I.AW B.737-300 SRM REV 125 CH
51-10-02 PARA 14 AND WAS FOUND TO BE BEYOND ALLOWABLE LIMITS. ORIGINAL THICKNESS .153, MAX REMOVAL ALLOWED.015 (.138), REMAINING THICKNESS .079 I.AW B.737-300 SRSDR TSAA20211117011Anchor Fitting · corroded1000570383 - CORROSION UNDER ANCHOR NUT ON SUPPORT STRUCTURE FOR R/H AIR CON ACCESS PANEL @STA 566 RBL 42 WL 149, BEYOND LIMITS IAW B737-300 SRM REV 125 CH.57-10-13 FIG 101. SUPPORT BEAM LWR
CHORD REPLACED WITH MADE REPAIR PART FABRICATED AND INSTALLED IAW B7SDR TSAA20211117010Cargo Fitting · corroded1000570361 - CORROSION ON FWD CARGO PIT DUSTSILL WEB@ STA 420-STA 440 STR 26R REMOVED AND INSPECTED WITH A 10X MAGNIFYING GLASS I.AW B737-300 SRM REV. 125 51-10-02 PAR.14 NOMINAL THICKNESS:0.040", REMAINING THICKNESS: 0.033". MATERIAL REMOVAL OF 0.007" IS BEYOSDR TSAA20211117009Crease Beam · corroded1000570357 - CORROSION ON LOWER SURFACE ON CREASE BEAM WEB, STA 798 RBL 65 REMOVED AND INSPECTED USING A 10X MAGNIFYING GLASS IAW B737-300 SRM REV 125 51-10-02 PAR.14 NOMINAL THICKNESS
.032" REMAINING THICKNESS .024" MATERIAL REMOVED .008" IS BEYOND ALLOWABLESDR TSAA20211117008Channel · corroded1000570352 - CORROSION UNDER A/NON FLOOR SUPPORT CHANNEL, AFT CARGO PIT STA 773 LBL 3 REMOVED IAW B737-300 SRM REV 125 51-10-02 PARA 14A. NOMINAL THICKNESS .063", REMAINING THICKNESS .020".
MATERIAL REMOVAL OF .043" IS BEYOND THE ALLOWABLE LIMIT OF .0063" IAWSDR TSAA20211117007Keelbeam · corroded1000570259 - REPAIRED R/H KEEL BEAM LWR SURFACE@ STA 663.75-727, RBL 7, WL 148.5 IAW KF AEROSPACE DWG #R27904.1-053-023-001 REV:NC.SDR TSAA20211117006Beam · abnormal1000570256- REPAIRED L/H KEEL BEAM @STA 663.75-707, LBL 7, WL 148.5 IAW KF AEROSPACE DWG R27904.1-
053-022-001 REV:NC.SDR TSAA20211117005Intercostal · gouged1000567496- REMOVED GOUGES ON INTERCOSTAL ATTACH CLIPS X3@ STA 847 STR 20L, 21L, 19L IAW 8737-300 SRM REV 125 CH 53-00-04 FIG 101, MAXIMUM ALLOWABLE EDGE MATERIAL LOSS 0.100" EDGE MATERIAL REMOVED 0.089" IS WITHIN ALLOWABLE LIMITS IAW 8737-300 SRM REV 125 CH 5SDR TSAA20211117004Stringer Clip · broken1000565725 - REPLACED STRINGER CLIP@ STA 616 AT STR 9L IAW 8737-300 SRM REV 125 51-10-02 PARA 8 AND
INSTALLED IAW 8737-300 SRM REV 125 51-40-02 AND BOEING DOCUMENT #65-46539 REV:AV.SDR TSAA20211117003None · noneREPLACED STRINGER CLIP@ STA 727C STR 9L IAW B737-300 SRM REV 125 51-10-02 PARA 8 AND INSTALLED IAW 8737-300 SRM REV 125 51-40-02. AND BOEING DOCUMENTS #65C25228 REV:BK, AND
#65-73746 REV:CK.SDR TSAA20211117002None · noneBLENDED AND ASSESSED CORROSION ON BROWNLINE STA907-STA 1006 BL0 AND FOUND BEYOND ALLOWABLE LIMITS. NOMINAL THICK 0.280" REMOVED 0.034" REMAIN 0.246" IAW B737-300 SRM 53-00-52 FIG 101 DETAIL IX SECTION C-C REV 125. REPLACED BROWNLINE WITH MADE REPAIR PART IAW BSDR TSAA20211117001Structure · corrodedCORROSION ON FUSELAGE BELLY SKIN AT STA 727B, STR 26R FOUND TO BE BEYOND LIMITS IAW B737-300 REV 125 SMR 53-00-01, NOM THICKNESS OF 0.063", ALOWABLE REMOVEL 0.0063", REAMING THICKNESS 0.053", REPAIRED FUSELAGE BELLY SKIN AT STA 727B STR 26R IAW B737-300 REV 12SDR TSAA20191003045Floorbeam · not reportedREPAIRED FLOOR BEAM UPPER CHORD AT STA 986.5 RBL 40-45. REPLACED UPPER CAP FROM LBL 50 TO RBL 50 AS PER AEI EO 9563 REV IR AND FAA FORM 8110-3.SDR TSAA20191003055Skin · damagedREPAIRED RH WING ROOT TO W STA 270, UPPER WING SKIN IN MULTIPLE LOCATIONS AS PER BOEING SR# 4-45466890303 DATED SEPT 23, 2019 AND FAA 8100-9.SDR TSAA20191003056Structure · crackedREPAIRED CRACKED FASTENER HOLE ON RH WING T/E WBL 136 IAW BOEING SR# 4-4546890303 DATED SEP 23, 2019.SDR TSAA20191003013Strap · crackedREPAIRED CRACKED STRAPS AT STA 312 BL 0 AND LBL 14 IAW BOEING 737-300 SRM 53-10-51 REPAIR 4 REV 119.SDR TSAA20191003007Frame · dentedREPAIRED DENT DAMAGE ON INNER FLANGE OF STA 500 FRAME AT STR 16R+4" IAW KF DWG# R27904.1-053-099-001 REV A AND AEI EO 09520 REV IR. SEE FORM 8110-3 FOR FAA APPROVAL.SDR TSAA20191003005Skin · dentedREPAIRED DENT DAMAGE ON FUSELAGE BELLY SKIN AT STA 1016-1088 STR 25L-25R IAW KF DRAWING NO. R27904.1-053-011-001 REV NC, SEE FAA FORM 8110-3 FOR APPROVAL.SDR TSAA20181104024Stringer Clip · not reportedSTRINGER CLIP AT STA 639 STR 4L, STA 597 STR 3L AND STA 616 STR 4R REPLACED WITH OEM PART. FASTENERS INSTALLED IAW SRM 51-40-02 REV 117.SDR TSAA20171017034Frame · crackedCRACKED FRAME, BS 420 STRINGER 26L. REPAIRED IAW EO 5363 REV IR.
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