N937AT

Service difficulty reports · 240

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 = 'N937AT' 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 DALA2022042903016None · noneCRACK ON BEAM #1 STA Y=200 ON THE EDGE AT L1 DOOR. SUMMARY OF NRC 00159: BEAM #1 STA Y=200 ON THE EDGE AT L1 DOOR WAS REPAIRED PER B-717 SRM 52-10-02-2R-7 FIGURE 201. (LP #2214723)Apr 28, 2022 · N937AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2022042702958Flap · dentedDENTS ON AFT MOVABLE VANE, LOWER SKIN LH FLAP. SUMMARY OF NRC 00044: MOVABLE VANE LOWER SKIN LH FLAP WAS REPAIRED PER B 717 SRM 57-53-01-2R PROCEDURE 1. (LP #2212347)Apr 26, 2022 · N937AT · Boeing 717200 · Trailing Edge FlapsSDR DALA2022042702957Vane · dentedDENTS #2, #3, AND #11 WERE IDENTIFIED AND EVALUATED PER B717 SRM 57-53-01-1A PROCEDURE 1 ALLOWABLE DAMAGE 1 PAR 3. AT AFT MOVABLE VANE RH WING, TO ACCOMPLISH MON/ 9586/1712741, REF NRC S/N 00256 (AD). SUMMARY OF NRC 00259: MOVABLE VANE RH WING WAS REPAIRED PERApr 26, 2022 · N937AT · Boeing 717200 · Trailing Edge FlapsSDR DALA2022042702956Stay · corrodedCORROSION ON FRAME CLIP STA Y=927 BTW LONG 28 LH TO LONG 30 AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00123: CORROSION LEVEL 2, FRAME CLIP STA Y=927 BTW LONG 28 LH TO LONG 30 WAS REPLACED PER B717 SRM 51-41-02 PAR 4 AND 51-41-05 PAR 8 AND DWG 9915524 REV P. (LPApr 26, 2022 · N937AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2022042602927Frame · corrodedCORROSION ON FRAME CLIP STA Y=974 BTW LONG 28 LH TO 28 RH AFT CARGO COMPARTMENT. SUMMARY OF NRC 00145: CORROSION LEVEL 2, FRAME CLIP STA Y=974 BTW LONG 28 LH TO 28 RH AFT CARGO COMPARTMENT WAS REPAIRED PER B717 SRM 53-00-06-2R FIG. 201. (LP #2211458)Apr 25, 2022 · N937AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2022042402852Stay · corrodedCORROSION ON FRAME CLIP STA Y=954 BTW LONG 28 LH TO 28 RH AFT CARGO COMPARTMENT. SUMMARY OF NRC 00144: CORROSION LEVEL 2, FRAME CLIP STA Y=954 BTW LONG 28 LH TO 28 RH AFT CARGO COMPARTMENT WAS REPAIRED PER B717 SRM 53-00-06-2R FIG. 201. (LP #2208838)Apr 24, 2022 · N937AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2022042402851Stay · corrodedCORROSION ON FRAME CLIP STA Y=946 BTW LOGS 29 LH - 29 RH, AT AFT CARGO COMPARTMENT (C2). SUMMARY OF NRC 00255: CORROSION LEVEL 2, FRAME CLIP STA Y=946 BTW LOGS 29 LH - 29 RH, AT AFT CARGO COMPARTMENT WAS REPAIRED PER B717 SRM 53-00-06-2R. (LP #2208952)Apr 24, 2022 · N937AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2022042402850Doubler · corrodedCORROSION ON DOUBLER STA APROX 974 AFTER REMOTION OF LOWER PAN OF AFTER CARGO DOOR JAMB STA 954 TO 990 IN ORDER TO PERFORM NRC 052 (C2). SUMMARY OF NRC 00242: CORROSION LEVEL 2, DOUBLER STA APROX 974 WAS REPAIRED PER ER/A 598922-14 REV ORIGINAL/PRI 598922-14 RApr 24, 2022 · N937AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2022042402849Door Sill · corrodedCORROSION ON AFT CARGO COMPARTMENT LOWER DOOR JAMB (C2). SUMMARY OF NRC 0052: CORROSION LEVEL 2, PREVIOUS REPAIR AND LOWER DOOR JAMB ON AFT CARGO COMPARTMENT WAS REPLACED PER B717 SRM 53-20-15-2R PROCEDURE 7. (LP #2208730)Apr 23, 2022 · N937AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2022042402848Stay · corrodedCORROSION ON FRAME CLIP STA Y=908 BTW LONG 28 LH TO LONG 30 AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00122: CORROSION LEVEL 2, FRAME CLIP STA Y=908 BTW LONG 26 LH TO LONG 26 RH AT AFT CARGO COMPARTMENT WAS REPLACED PER B717 SRM 51-41-02-0G AND DWG 9915524 REV Apr 23, 2022 · N937AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2022042202828Longeron · crackedCRACK LONG 2LH STA 1133 AT AFT ACCESORIES COMPARTMENT. SUMMARY 0F NRC 00204: LONG 2LH AT STA 1133 AT AFT ACCESORIES COMPARTMENT WAS REPAIRED PER B717 SRM 53-00-05-2R-2. (LP #2205975)Apr 21, 2022 · N937AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2022042202827Longeron · crackedCRACK LONG 2RH AT STA 1133 AT AFT ACCESORIES COMPARTMENT. SUMMARY 0F NRC 00203: LONG 2RH AT STA 1133 AT AFT ACCESORIES COMPARTMENT.WAS REPAIRED PER B717 SRM 53-00-05-2R-2. (LP #2205959)Apr 21, 2022 · N937AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2022042202826Doubler · corrodedCORROSION ON DOUBLER ATTACH AFT PRESSURE BULKHEAD STA Y=1053 AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00161: LEVEL CORROSION 2, DOUBLER ATTACH AFT PRESSURE BULKHEAD STA Y=1053 AT AFT CARGO COMPARTMENT WAS REPLACED PER B717 SRM 51-41-05-0G PAR. 8.B. (LP #220590Apr 21, 2022 · N937AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2022042202825Longeron · corrodedCORROSION ON LONGERON 29 LH FROM STA 928 TO 931 AFT CARGO COMPARTIMENT IN ORDER TO PERFORM NRC 139. SUMMARY OF NRC 00251: CORROSION LEVEL 2, LONGERON 29 LH FROM STA 928 TO 931 AFT CARGO COMPARTIMENT IN ORDER TO PERFORM NRC 139 WAS REPAIRED PER B-717 SRM 53-00-Apr 21, 2022 · N937AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2023102508762Unknown · unknownMAIN ENTRANCE DOOR, (L-1), HOLD OPEN HOOK CAVITY IS GOUGED ON THE AFT SIDE. REPAIRED FUSELAGE SKIN AT L-1 DOOR HOLD OPEN HOOK CAVITY IAW B717 SRM 53-10-01-2R-7. INSPECTION REQ AT 8000 F.C. FROM DATE OF REPAIR INSTALL & REPEAT EVERY 8000 F.C. THERE AFTER INSP ROct 19, 2019 · N937AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2019032501895Light · inoperativeCOCKPIT EMERGENCY FLOODLIGHT INOP. RELAMPED PER AMM 33-51 NO HELP. R&R EMERGENCY BATTERY PACK B5-123 PER AMM 33-51 OPS CHECK NORMAL OK FOR SERVICE. (LP5528324)Mar 25, 2019 · N937AT · Boeing 717200 · Emergency LightingSDR DALA2018102306239Floor Panel · damagedLEFT OUTBOARD MAIN CABIN METAL FLOOR PANEL AT STA 720 HAS A SMALL HOLE IN CENTER OF PANEL. CUT OUT DAMAGED AREA DIM 700"X700" AT LEFT O/B MAIN CABIN METAL FLOOR PANEL AT STA 720 IAW B717 SRM 51-70-10. FABRICATED AND INSTALLED DOUBLER FROM 7075 T6 .032 DIM 4 1/Oct 22, 2018 · N937AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2023083007070Unknown · unknownPUSHBACK TOWBAR BROKE, AIRCRAFT MADE CONTACT WITH TUG. FOUND 3 DENTS AND 3 GOUGES AFT OF STA 37 12.5 INCHES BELOW THE PRESSURE BOUNDRY. LIGHTLY BLENDED GOUGE AREA & ACCOMPLISHED UT THICKNESS MEASUREMENT, REF B717 NDT SPM 04-00-03, MIN REMAINING THICKNESS IS .0Oct 3, 2018 · N937AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2018071604487Power Supply · inoperativeTHE AFT DOOR EXIT SIGN IS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY POWER SUPPLY IAW AMM 33-51-03. OPERATIONAL CHECK WAS GOOD.Jul 15, 2018 · N937AT · Boeing 717200 · Emergency LightingSDR DALA2017071705456Power Supply · malfunctionedAFT EMERGENCY EXIT LIGHT FLICKERING / INTERMITTENT. REPLACED AFT OVERHEAD POWER SUPPLY AND BATTERY PACKS. OPS CHECKED GOOD IAW AMM 33-54.Jul 16, 2017 · N937AT · Boeing 717200 · Emergency LightingSDR DALA2016120909741Pan · crackedCRACKED RT RING PAN UPPER AFT CORNER BS 832. REPAIRED THE RING PAN IAW SRM 56-20-02 FIG. 202.Dec 8, 2016 · N937AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2016112609262Skin · crackedCRACK ON EXTERNAL FUSELAGE SKIN BS 1076 LONGERON 14L REPAIRED IAW ETI-17-16-154 REV.4 AND ER/A 551747-14 REV. A .Nov 25, 2016 · N937AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2016112409261Skin · crackedCRACKED INBD BUTTE DOOR INBD SKIN AT RT WING. REPAIRED IAW ETI-17-16-171 REV. 1 AND ER/A 551772-14 REV. ORIG.Nov 23, 2016 · N937AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2016112008948Access Panel · crackedCRACK ON FUEL ACCESS PLATE 620MB. ACCESS PLATE 620MB WAS REPLACED PER AMM 28-00-00 AND IPC 57-23-01-01.Nov 19, 2016 · N937AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2016112008947Doubler · corrodedCORROSION ON DOUBLER, STA Y=954 AND PROTECTION BTW LONG 26R TO 27R DOOR JAMB, AT AFTER CARGO COMPARTMENT. DOUBLER WAS REMOVED PER SRM 51-41-05 PAR 10 AND 51-41-07 PAR 10, DOUBLERS WERE MANUFACTURED PER SRM 51-20-09 AND 53-20-15 REPAIR 7 AND DOUBLER WAS INSTALLNov 19, 2016 · N937AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016112109065Cargo Track · corrodedCORRODED LT CARGO TRACK BETWEEN BS 813 - 1022. THE CORROSION WAS REMOVED IAW SRM 51-10-04 PAR 26. UT WAS ACCOMPLISHED IAW NDT SPM 04-00-07 PAR 5 FIG 3 (SHEET 1 AND 2) AND FOUND WITHIN LIMITS AT BS 813 TO 896 IAW SRM 53-20-52. FIG 101 (SHEET 1 OF 3). THE CANov 18, 2016 · N937AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2016111908941Skin · crackedCRACK ON INTERNAL FUSELAGE SKIN STA Y=1021 BTW LONG 13L-14L AT PAX CABIN. CRACKS ON FUSELAGE/SKIN AND DOUBLER/STA 1022 & L-13-L14 WERE REPAIRED WITH ETI-17-16-149 REV 3 AND ER/A 551741-14 REV ORIGINAL. PERFORM GVI ON EXTERNAL SURFACE, EVERY 3000 FLIGHT CYCLES Nov 18, 2016 · N937AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2016111808914Hinge · corrodedCORROSION AT HORIZONTAL STABILIZER CENTER SECTION HINGE BORE AT STRINGER 7 RT SIDE. THE REPAIR WAS ACCOMPLISHED PER ETI-17-16-155 REV 2 AND ER/A 551748-14 REV ORIG.Nov 17, 2016 · N937AT · Boeing 717200 · Horizontal Stabilizer StructureSDR DALA2016111808939Panel · corrodedCORROSION AND DISBONDED VOR ANTENNA PANELS UPPER AND LOWER (4EA). VOR ANTENNA PANELS UPPER AND LOWER (4EA) WERE REMOVED PER AMM 34-32-03. VOR ANTENNAS (4 EA) WERE REPLACED PER AMM 34-32-03. FUNCTIONAL TEST WAS PERFORMED PER AMM 34-51-00. TEST OK.Nov 16, 2016 · N937AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2016111708912Pan · damagedELONGATED HOLE ON INNER PAN AT AFT SIDE BELOW HINGE ON AFT CARGO DOOR (C2) (S/N 00554). REPAIR ON INNER PAN AT AFT SIDE BELOW HINGE ON AFT CARGO DOOR (C2) WAS PERFORMED PER ETI-17-16-166 REV 1 AND ER/A 551752-14 REV ORIGINAL, AMM 52-31-03-000 802 AND SRM 51-41Nov 16, 2016 · N937AT · Boeing 717200 · Cargo/Baggage DoorsSDR DALA2016111608813Retainer · wornWORN LOWER RETAINER AT FWD DOOR BARRIER. LOWER RETAINER WAS REPAIRED IAW ETI -17-16-168 REV. ORG. AND ER/A 551759-14 REV ORG.Nov 15, 2016 · N937AT · Boeing 717200 · Cargo/Baggage DoorsSDR DALA2016111608811Beam · crackedCRACKED LT NLG DOOR FRAME BEAM BS 48. AREA DAMAGE WAS REPAIRED IAW SRM 53-10-14 FIG. 201 REP. 2, ETI-17-16-158 REV. 1 AND ER/A 551751-14 REV. ORIG.Nov 15, 2016 · N937AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2016111508810Access Panel · corrodedCORROSION ON FUEL ACCESS PANEL COUNTERSINK ON THE RT WING. THE ACCESS PANEL WAS REPLACED IAW SRM 57-10-01.Nov 14, 2016 · N937AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2016111508809Access Panel · corrodedCORROSION ON FUEL ACCESS PANEL ON COUNTERSINK 520DT ON LT WING. THE ACCESS PANEL WAS REPLACED IAW SRM 57-10-01.Nov 14, 2016 · N937AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2016111508808Access Panel · corrodedCORROSION ON FUEL ACCESS PANEL ON SETTLEMENT AREA AND COUNTERSINK 520 CT AT RT WING. THE ACCESS PANEL REPLACED IAW SRM 57-10-01.Nov 14, 2016 · N937AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2016111408743Cusp Web · crackedCRACKED CUSP WEB BETWEEN BS 1002 AND 1020, RBL 54 TO 60. THE CUSP WEB WAS REPAIRED IAW SRM 53-00-55 REPAIR 4 FIG. 216. AND 51-41-05.Nov 13, 2016 · N937AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016111408793Beam · crackedCRACK AT BEAM NR 6 ON FWD PASSENGER DOOR L1. BEAM NR 6 ON FWD PASSENGER DOOR WAS REPAIRED PER ER/A 551749-14 REV ORIGINAL AND ETI-17-16-156 REV ORIGINAL.Nov 12, 2016 · N937AT · Boeing 717200 · Passenger/Crew DoorsSDR DALA2016111208740Channel · crackedCRACKED FWD CHANNEL OF THE LT MLG DOOR CUTOUT BS 764 AT LT WW AREA. THE CHANNEL WAS REMOVED PER B-717 SRM 51-41-02. A NEW CHANNEL WAS DRILLING IAW SRM 51-40-08. THE CHANNEL WAS TREATED AND PAINTED IAW SRM B717 51-10-04 PART 15 & 21. THE CHANNEL WAS INSTALLNov 11, 2016 · N937AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016111108713Channel · crackedCRACKED CHANNEL ON FLOOR PANEL 222AFF AND 222AF, ALSO CRACKED WEB ON FLOOR PANEL 222XF AND CRACK ON STRAP ON FLOOR PANEL 223EF (S/N 00242). CRACKS ON FLOOR PANELS 222AFF, 222AF, 222XF AND 223EF WERE REPAIRED PER SRM 53-20-50 REPAIR 5, 53-00-00 REPAIR 1, AND 51Nov 10, 2016 · N937AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2016111108712Cusp Web · crackedDURING CORROSION REMOVAL CRACK WAS FOUND AT CUSP WEB STA Y=660 X=60. IN REF CARD 00278. (S/N 00525). CUSP WEB WAS REPAIRED PER SRM 53-00-55 FIG 126 HFEC WAS ACCOMPLISHED AND NO CRACKS WAS FOUND AFTER CUT OUT PER NDT SPM 06-10-01.001.Nov 10, 2016 · N937AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016111108711Angle · crackedCRACK ON ANGLES 2EAS AT AFT PASSENGER EMERGENCY EXIT DOOR JAMB LT SIDE LOWER AND MIDDLE STOP AREA. (S/N 00506) FITTINGS WERE REPLACED PER SRM 51-41-02 AND 51-41-01.Nov 10, 2016 · N937AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016111108710Fitting · crackedCRACKED TEE AND CLIP AT FWD CARGO DOOR LOWER ANGLE BEAM INTERNAL STRUCTURE STA Y=410 APPROX. TEE AND CLIP WERE REPLACED PER SRM 51-41-01, 51-41-02, 51-41-05, AND DPS 4.710-3.Nov 10, 2016 · N937AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016111108705Fitting · crackedCRACKED FITTING AT LT AFT OVERWING EMERGENCY EXIT DOOR BEAM 1 FWD EDGE. CLIP WAS REPLACED AND INSTALLED PER SRM 51-41-02, 51-41-05, AND DRAWING 9957735 REV G.Nov 10, 2016 · N937AT · Boeing 717200 · Emergency ExitsSDR DALA2016111108704Fitting · crackedCRACKED CLIPS AT Z=41.375 STA 196.8 AND STA 172.5 ON FWD GALLEY DOOR. CLIPS WERE REPLACED PER SRM 51-41-02, 51-41-05, AND DRAWING 9911581 REV U.Nov 10, 2016 · N937AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016111108703Frame · crackedCRACKED FRAMES STA 680, 696, 715 BTW LONG 28/25 LT AT KEEL BEAM AREA. FRAMES WERE REPAIRED PER SRM 51-70-11 REPAIR 1, 51-41-05, 51-41-02, AND 51-10-04 PAR 37. HFEC INSPECTION WAS ACCOMPLISHED AND NO CRACKS WERE FOUND AFTER THE REMOVED DAMAGE FRAME Y=696 LT PERNov 10, 2016 · N937AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2016111008440Pan · crackedCRACK ON PAN AT BS 170 AND Z 11.063 ON FWD R1 SERVICE DOOR. HFEC INSPECTION WAS ACCOMPLISHED AND A CRACK OF 0.312" WAS FOUND IAW NDTSPM 06-10-01. THE CRACK WAS STOP DRILL IAW SRM 52-00-00 FIG. 202. NO CRACKS FOUND AFTER STOP DRILL, IAW NDTSPM 06-10-01 .001Nov 9, 2016 · N937AT · Boeing 717200 · Service DoorsSDR DALA2016111008438Frame · crackedCRACKED FRAMES BS 680 BETWEEN LONGERON 25-28R. THE FRAME WAS REPAIRED IAW SRM 51-70-11 REPAIR 1, 51-41-05, 51-41-02, AND 51-10-04 PAR 37.Nov 9, 2016 · N937AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2016110908363Floor Panel · damagedDAMAGED FLOOR PANEL. FLOOR PANEL REPLACED IAW DWG 9936639 REV: P.Nov 8, 2016 · N937AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2016110708316Floor Support · corrodedCORROSION ON FLOOR SUPPORT X=0 STA AND Y= 218 AT W1 AREA (S/N 00489). NEW SUPPORT FLOOR PANEL WAS INSTALLED PER SRM 51-41-02.Nov 6, 2016 · N937AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016110708315Window · crackedCRACKED UPPER FWD CORNER WINDOW BETWEEN BS 427 AND 446. REPAIRED IAW SRM 56-20-02 REPAIR 1 TYPE C FIG 203. HFEC INSPECTION WAS ACCOMPLISHED AND NO CRACKS WERE FOUND AFTER TRIM OUT IAW NDT SPM 06-10-01. 001. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 56-2Nov 6, 2016 · N937AT · Boeing 717200 · Passenger Compartment Windows
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