N936AT

Service difficulty reports · 206

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 = 'N936AT' 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 DALA2019062603857Skin · crackedCRACK AT FUSELAGE SKIN STA 1087 BETWEEN LONGERON 13/14RH (FUS). NRC 597: CRACK AT FUSELAGE SKIN STA 1087 BETWEEN LONGERON 13/14RH WAS REPAIRED PER ETI-17-19-075 REV 5 AND ER/A 579256-14 REV. ORIG.Jun 25, 2019 · N936AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2019062503830Frame Angle · corrodedEXFOLEATED FRAME CLIP ON STA Y=1022 BTW LONG 27 LH AND 27RH AT AFT CARGO COMPARTMENT. NRC 00302: CORROSION LEVEL 2, FRAME CLIP AT STA Y=1022 BTW LONG 27 LH AND 27RH AT AFT CARGO COMPARTMENT WAS REPLACED PER B717-200 SRM 51-41-02-0G AND DWG #9912243 REV. JS. (LJun 24, 2019 · N936AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2019062503828Skin · corrodedCORROSION ON LOWER SKIN OF STA Y=851 AND STRINGER 30. CORROSION ON LOWER SKIN OF STA Y=851 AND STRINGER 30 WAS REPAIRED PER B-717-200 SRM 53-20-70-2R-1 FIG .201.Jun 24, 2019 · N936AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2019062403801Frame · crackedCRACK ON FRAME BS 696 LH SIDE.FRAME REPLACED PER AD 2013-19-22 TASK CARD 5310-01436-03A.Jun 24, 2019 · N936AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2019062403800Frame · crackedAD 2013-19-22 CRACK ON FRAME STA 696 RH SIDE. NRC 00371: FRAME STA 696 RH SIDE WAS REPLACED PER AD 2013-19-22 TASK CARD 5310-01436-03B. (LP #1137896)Jun 24, 2019 · N936AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2019062653856Cargo Track · damagedELONGATED HOLES ON RH TIE TRACK STA 954 AT AFT CARGO COMPARTMENT. NRC 00277: TIE TRACK RH ON STA 895 TO STA 954 AT AFT CARGO COMPARMENT WAS REPLACED PER B717-200 SRM 53-20-51-0I-7 IDENTIFICATION 7, ITEM 8, FIG.2 (SHEET 2), PER B717-200 SRM 51-41-01-0G AND 51-4Jun 23, 2019 · N936AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2019062543825Frame Angle · corrodedCORROSION ON FRAME CLIP STA Y=1002 BTW LONG 26LH-25LH AT AFT CARGO COMPARTMENT (C2). NRC 0711: CORROSION LEVEL 2, FRAME CLIP AT STA Y=1002 BTW LONG 26LH-25LH WAS REPAIRED PER B717-200 SRM 51-41-02-0G, 53-00-06-2R REPAIR 2 PAR. 4. A. FIG. 201, AND DWG #9957739 Jun 23, 2019 · N936AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2019062533820Frame · corrodedCORROSION ON FRAME STA 889 LONG 30 WAS FOUND OUT OF LIMITS PER B717 SRM 53-00-00-1A FIG 103. CORROSION LEVEL 2, FRAME AT STA 889 LONG 30 WAS REPAIRED PER B717-200 SRM 53-20-07-2R PROCEDURE 3 REPAIR 3 FIGURE 201, SHEET 1.Jun 22, 2019 · N936AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2019062533819Barrier · corrodedCORROSION ON VAPOR BARRIER LH SIDE STA X=22 AND STA Y=715 AT PAX CAB (CPAX). NRC 00535: CORROSION LEVEL 2, CORROSION WAS REPAIRED PER ER/A 579113-14 REV. ORIGINAL: SECTION I. ASSOCIATED ER/A 14-579113 ADDED FOR AC 9563. (LP #1136277)Jun 22, 2019 · N936AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2019062533818Barrier · corrodedCORROSION ON VAPOR BARRIER STA X=54 AND STA Y=663 TO STA Y=715 AT PAX CABIN. CORROSION LEVEL 2, CORROSION WAS REPAIRED PER ER/A 579177-14 REV. ORIGINAL: SECTION I.Jun 22, 2019 · N936AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2019062533817Skin · corrodedCORROSION ON UPPER SKIN STA Y=717 X=-19 AND Z-10 AT WING BOX. NRC 00483: CORROSION LEVEL 2, CORROSION WAS REPAIRED PER ER/A 579114-14 REV. ORIGINAL: SECTION I.Jun 22, 2019 · N936AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2019062533816Skin · corrodedCORROSION ON UPPER SKIN STA Y=708 X=-24 AND Z-10 AT WING BOX. NRC 00482: CORROSION LEVEL 2, CORROSION WAS REPAIRED PER ER/A 579114-14 REV. ORIGINAL: SECTION I.Jun 22, 2019 · N936AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2019062533815Frame Angle · corrodedEXFOLATION FRAME CLIP STA Y=927 BTW LONG 24LH TO LONG 26RH AT AFT CARGO COMPARTMENT. NRC 00192: CORROSION LEVEL 2, FRAME CLIP AT STA Y=927 BTW LONG 26LH AND 26RH WAS REPLACED PER B717-200 DWG #9915524 REV. P, PER B717-200 SRM 51-41-02-0G AND 51-41-05-0G.Jun 22, 2019 · N936AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2019062533814Barrier · corrodedCORROSION ON VAPOR BARRIER STA X=22 AND STA Y=715 TO STA Y=737 AT PAX CAB (CPAX). NRC 00534: CORROSION LEVEL 2, CORROSION WAS REPAIRED PER ER/A 579113-14 REV. ORIGINAL: SECTION I.Jun 22, 2019 · N936AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2019062533813Doubler · corrodedCORROSION ON DOUBLER FROM STA Y=737 TO Y=748 BTW X=44 TO X=60 AND Z-10 AT WING BOX. NRC 00486: CORROSION LEVEL 2, CORROSION WAS REPAIRED PER ER/A 579113-14 REV. ORIGINAL.Jun 22, 2019 · N936AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2019062533812Skin · corrodedCORROSION ON UPPER SKIN FROM STA Y=715 TO Y=737 BTW X=44 TO X=60 AND Z=-10 AT WING BOX. NRC 00481: CORROSION LEVEL 2, CORROSION WAS REPAIRED PER ER/A 579113-14 REV. ORIGINAL: SECTION I. ASSOCIATED ER/A 14-579113.Jun 22, 2019 · N936AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2019062523811Longeron · corrodedCORROSION ON SECTION LONG 27LH FROM STA Y=984 TO STA Y=1010 AT AFT CARGO COMPARTMENT IN REFERENCE NRC 00284. (C2). NRC 683: CORROSION LEVEL 2, SECTION LONG 27LH FROM STA Y=984 TO STA Y=1010 AT AFT CARGO COMPARTMENT WAS REPLACED PER B717-200 SRM 51-41-02-0G ANDJun 22, 2019 · N936AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2019062523810Frame · corrodedEXFOLATION ON FRAME STA Y=1037 BTW LONG 25RH TO 25LH AT AFT CARGO COMPARTMENT. NRC 00296: CORROSION LEVEL 2, FRAME STA Y=1037 BTW LONG 25RH TO 25LH AT AFT CARGO COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-20-07-2R.Jun 22, 2019 · N936AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2019062433791Skin · damagedCRACK AT FUSELAGE SKIN STA 1022 BETWEEN LONG. 13/14R. FUSELAGE SKIN STA 1022 BETWEEN LONG. 13/14RH (FUS) WAS REPAIRED PER ERA/A 579005-14 REV. ORIGINAL, SECTION I PERMANENT REPAIR AND ETI-17-19-077 REV. 3.Jun 22, 2019 · N936AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2019062543826Door Frame · crackedCRACKED RH NOSE LANDING GEAR JAMB BEAM AROUND STA Y-47. RT NOSE LANDING GEAR JAMB BEAM AROUND STA Y-47 WAS REPAIRED PER ER/A 495600-14MA REV C.Jun 21, 2019 · N936AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2019062423778Beam · crackedCRACKED LH NOSE LANDING GEAR JAMB BEAM AROUND STA: Y-47 (FYT). NRC 00569: LH NOSE LANDING GEAR JAMB BEAM AROUND STA Y-47 WAS REPAIRED PER B-717-200 SRM 53-10-14-2R FIG. 201 REP. 2.Jun 21, 2019 · N936AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2019062103703Pan · crackedCRACK ON PAN BTW BEAM 1 TO BEAM 2 AND STA 994 AT AFT CARGO DOOR (C2). NRC 00439: AREA WAS REPAIRED PER ER/A 579043-14 REV. ORIG. AND ETI-17-19-074, REV 2. (LP #1133339)Jun 21, 2019 · N936AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2019062603875Doubler · corrodedEXFOLATION DOUBLER ON LOWER CUT OUT DOOR JAMB STA Y=972 AT AFT CARGO COMPARTMENT. NR 00325: CORROSION LEVEL 2, EXFOLATION CORROSION ON DOUBLER AT LOWER CUT OUT DOOR JAMB STA Y=972 AT AFT CARGO COMPARTMENT WAS ATTENDED PER ER/A 578898-14 REV. ORIGINAL. ASSOCIATJun 20, 2019 · N936AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2019062103701Intercostal · corrodedCORROSION ON INTERCOSTAL STA Y=1032 AND LONG 25LH AT AFT CARGO COMPARTMENT. NRC 00317: CORROSION LEVEL 2, INTERCOSTAL STA Y=1032 AND LONG 25LH AT AFT CARGO COMPARTMENT WAS REPLACED PER DWG #5936071 REV. W AND PER B717-200 SRM 51-41-02-0G. (LP #1132805)Jun 20, 2019 · N936AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2019062103700Finger Doubler · corrodedCORROSION ON FINGER DOUBLER FROM STA Y=943 TO 960 AND Y=1005 TO Y=1044 BELOW LH LONGERON AT AFT CARGO COMPARTMENT WAS FOUND OUT OF LIMITS. NRC 00691: CORROSION LEVEL 2, SECTION OF FINGER DOUBLERS STA Y=943 TO Y=960 AND Y=1005 TO Y=1044 BELOW LH LONGERON AT AFTJun 20, 2019 · N936AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2019062103698Frame Angle · corrodedEXFOLATION ON FRAME CLIP STA Y=1037 BTW LONG 25RH TO LONG 25LH AT AFT CARGO COMPARTMENT. NRC 0316: CORROSION LEVEL 2, FRAME CLIP FROM STA Y=1037 BTW LONG 25RH TO LONG 25LH AT AFT CARGO COMPARTMENT WAS REPLACED PER B717-200 SRM 51-41-02-0G AND DWG #9958238-85 RJun 20, 2019 · N936AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2019070304025Splice · corrodedEXFOLATION ON SPLICE CLIP STA Y=898.500 BTW LONG 25L TO LONG 25R AT AFT CARGO COMPARTMENT. NRC 00171: CORROSION LEVEL 2, SPLICE CLIP STA Y= 898.500 BTW LONG 25L TO LONG 25R AT AFT CARGO WAS REPLACED PER SRM 53-20-01-0I AND 51-41-05-0G. (LP #1131371)Jun 19, 2019 · N936AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA201906213697Doubler · corrodedCORROSION ON DOUBLER STA 1053 OVER PROJECTION STG 30 ON LOWER BULHEAD AREA AT AFT CARGO COMPARTMENT. THE DOUBLER WAS REPLACED PER B717-200 SRM 51-41-05-0G AND SRM 53-20-08-0I- 2 FIG. 1.Jun 19, 2019 · N936AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2019062003668Pan · corrodedCORROSION ON FWD CARGO COMPARTMENT LOWER DOOR JAMB PAN, BTW STA Y=370 TO Y=427 REASON FOR RE-WRITE WRONG MEASSUREMENT. (CCD). NRC 00679: CORROSION LEVEL 2, FWD CARGO COMPARTMENT LOWER DOOR JAMB PAN, BTW STA Y=370 TO Y=427 WAS REPLACED PER B717-200 SRM 53-20-15Jun 19, 2019 · N936AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2019062003667Door Frame · corrodedCORROSION ON LOWER DOOR JAMB FROM STA Y=954 TO Y=994 AT AFT CARGO COMPARTMENT. NRC 00324: LOWER DOOR JAMB AND SPLICES WERE REPLACED PER B717-200 SRM 53-20-15-2R REPAIR 7 AND 51-41-02-0G, 51-41-04-0G, AND 51-41-05-0G. (LP #1131248)Jun 19, 2019 · N936AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2019062003666Reinforcement · crackedCRACK ON LH SLINDING WINDOW REINFORCEMENT CUTOUT, AFT UPPER CORNER AT FLIGHT COMPARTMENT (CPIL). NRC 00475: BRACKET LH SLINDING WINDOW REINFORCEMENT CUTOUT, AFT UPPER CORNER WAS REPLACED PER B717-200 SRM 51-41-01-0G, 51-41-02-0G, AND 51-41-05-0G. (LP #1130511)Jun 19, 2019 · N936AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2019061903652Beam · crackedCRACK ON BEAM STA Y=737, X= 54 AND Z=-2 LH SIDE AT WING BOX. NRC 00467: FLOOR BEAM WAS REPLACED PER B717-200 SRM 51-41-02-0G AND SRM 51-41-05-0G .Jun 19, 2019 · N936AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2019061983650Longeron · corrodedCORROSION ON LONGERON END 23RH STA Y=1003 AT AFT CARGO COMPARTMENT. NRC 0304: CORROSION LEVEL 2, DUE TO CORROSION OUT OF LIMITS LONGERON END 23RH STA Y=1003 AT AFT CARGO COMPARTMENT WAS REPLACED PER B717-200 SRM 51-41-05-0G. (LP #1127877)Jun 17, 2019 · N936AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2019061803623Frame Angle · corrodedEXFOLATION ON FRAME CLIP STA Y=908 BTW LONGERON 26LH TO LONGERON 28RH BOTH FACES AT AFT CARGO COMPARTMENT. NRC 0174: CORROSION LEVEL 2, FRAME CLIP STA Y=908 BTW LONG 26LH TO LONG 28RH AT AFT CARGO COMPARTMENT WAS REPLACED PER B-717-200 SRM 51-41-02-0G. (LP #11Jun 17, 2019 · N936AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2019061703620Cusp Web · crackedCRACK ON LH CUSP WEB BETWEEN STA 655/653 IN REF NRC 00647. (CPAX). NRC 00675: LH CUSP WEB BETWEEN STA 655/653 WAS REPLACED PER B717-200 SRM 53-00-55-2R-4, 51-41-02-0G, AND 51-41-05-0G.Jun 16, 2019 · N936AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2019061703619Cusp Web · crackedCRACK ON LH CUSP WEB STA 655 UNDER PRODUCTION DOUBLER. (CPAX). NRC 00647: LH CUSP WEB STA 655 UNDER PRODUCTION DOUBLER WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4 FIG. 211.Jun 16, 2019 · N936AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2019061703618Frame Angle · crackedCRACK ON CLIP FRAME LONG 14RH STA 1022 AT FWD FACE OF BULKHEAD (CPAX). NRC 00401: FRAME CLIP WAS REPLACED PER B717-200 SRM 51-41-05-0G.Jun 16, 2019 · N936AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2019061703617Gusset · crackedCRACK ON GUSSET PROJECTION LONGERON 7RH STA 1022 AT AFT FACE OF BULKHEAD (CPAX). NRC 00397: GUSSET PROJECTION LONG 7RH STA 1022 AT AFT FACE OF BULKHEAD WAS REPAIRED PER ER/A 578999-14 REV.ORIGINAL (SECTION I: PERMANENT REPAIR) AND ETI-17-19-076 REV. 1. ASSOCIAJun 16, 2019 · N936AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2019061763615Gusset · crackedCRACK ON GUSSET PROJECTION LONGERON 7LH STA 1022 (CPAX). NRC 00398: GUSSET PROJECTION LONG 7LH STA 1022 WAS REPAIRED PER ER/A 57899-14 REV. ORIGINAL (SECTION I: PERMANENT REPAIR) AND ETI-17-19-076 REV. 1. ASSOCIATED ER/A 14-578999 ADDED FOR AC 9563. (LP #11249Jun 16, 2019 · N936AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2019061763614Access Panel · corrodedEXCESSIVE CORROSION ON FUEL ACCESS PLATE #520LB.(AI). NRC 00666: CORROSION LEVEL 2, CORROSION ON FUEL TANK ACCESS DOOR #520LB OF LH WING FUEL TANK WAS REMOVED PER B717-200 SRM 51-10-04-0G PAR 26 AND B717-200 SRM 57-10-01- 2R REPAIR 2 PAR. 5.; DIAMETER OF COUNTJun 16, 2019 · N936AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2019061763613Frame · crackedCRACK ON FRAME, LONG 17RH STA 1037 (CPAX). NRC 00404: FRAME, LONG 17RH STA 1037 WAS REPAIRED PER B717-200 SRM 53-20-07-2R-4. (LP #1124857)Jun 16, 2019 · N936AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2019061763591Longeron · crackedCRACK ON LONGERON 6RH STA 1022 AT AFT FACE OF BULKHEAD (CPAX). NRC 00396: SECTION OF LONGERON 6RH BTW STA 996 TO 1053 WAS REPAIRED PER B717-200 SRM 53-00-05-2R. (LP #1124449)Jun 15, 2019 · N936AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2019061763590Cusp Web · canningOIL CANING ON CUSP WEB AT BTW STA 889/908 LH X= 44/60 (FUS). NRC 00361: CUSP WEB DAMAGED BTW STA 889 TO 908 LH, X =-44 TO X=-60, WAS REPLACED PER B-717-200 SRM 51-41-02-0G AND SRM 51-41-05-0G. (LP #1124292)Jun 15, 2019 · N936AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2019061753589Longeron · crackedCRACK ON LONGERON 4LH STA 1022 (CPAX). NRC 00388: SECTION LONGERON 4 LH FROM STA. 1010 TO STA. 1053 WAS REPAIRED PER B-717-200 SRM 53-00-05-2R.Jun 14, 2019 · N936AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2019061303544Seat Track · corrodedCORROSION ON F.O. LOWER OUTBOARD SEAT TRACK. NRC 00559: CORROSION LEVEL 2, SEAT TRACK WAS REPLACED PER B717-200 SRM 51-41-01-0G.Jun 13, 2019 · N936AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2019061303542Frame · crackedCRACK ON FRAME, LONG 17LH STA 1037 (CPAX). NRC 00402: FRAME STA 1037 AT LONG 17LH WAS REPAIRED B717-200 SRM 53-20-07-2R-4. (LP #1120245)Jun 13, 2019 · N936AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2019061303543Frame Angle · crackedCRACK ON CLIP FRAME LONG 16RH STA 1022 AT FWD FACE OF BULKHEAD (CPAX). NRC 00398: FRAME LONG 16RH STA 1022 AT FWD FACE OF BULKHEAD WAS REPLACED PER B717-200 SRM 51-41-05-0G AND DWG #9912243 REV. JS. (LP #1120252)Jun 12, 2019 · N936AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2019061203520Frame · crackedCRACK ON RING PAN UPPER AFT CORNER STA Y:832 RH SIDE AT PASSENGER CABIN (CPAX). NRC 00242: CRACK ON RING PAN UPPER AFT CORNER STA Y:832 RH SIDE AT PASSENGER CABIN WAS REPAIRED PER B717-200 SRM 56-20-02 REPAIR 1. (LP #1118572)Jun 11, 2019 · N936AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2019061203519Floor Support · corrodedCORROSION ON FLOOR SUPPORT AT STA 200 FROM X=7 (CPAX). NRC 00432: CORROSION LEVEL 2, CORROSION ON FLOOR SUPPORT AT STA 200 FROM X=7 WAS REMOVED PER B717-200 SRM 51-10- 04 PAR 26. REMAINING THICKNESS OF 0.003" IS OUT OF LIMITS PER B-717-200 SRM 53-00-00-1A FIG.Jun 11, 2019 · N936AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2019061203518Access Panel · corrodedEXCESSIVE CORROSION ON FUEL ACCESS PLATES #520PB AND #520DT.(AI). NRC 00667: CORROSION ON FUEL TANK ACCESS DOORS #520DT AND 520PB OF LH WING WAS REMOVED PER B717-200 SRM 51-10-04-0G PAR 26 AND 57-10-01-2R REPAIR 2 PAR. 5. REMAINING THICKNESS WAS OUT OF LIMITS Jun 11, 2019 · N936AT · Boeing 717200 · Wing, Plate/Skin
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