N921AT

Service difficulty reports · 236

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 = 'N921AT' 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 DALA2025042303169Doubler · corrodedCORROSION ON INTERNAL DOUBLER AND ON INNER SIDE OF WASTE SERVICE PANEL BTW STA Y=1022 AND STA Y=1037 BTW LONG 23L AND LONG 25L AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00232: CORROSION LEVEL 2. INTERNAL DOUBLER AT INNER SIDE OF WASTE SERVICE PANEL BTW STA Y=10Apr 22, 2025 · N921AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2024100709751Compressor Wheel · damagedSHIP 9577 -FUME/DE- ON CLIMB OUT THROUGH FL200, AN ODOR SIMILAR TO MELTING PLASTIC WAS BRIEFLY NOTED. ABOUT ONE MINUTE LATER THE CREW EXPERIENCED SOME ENGINE VIBRATION ON THE LEFT SIDE AND AT THE SAME TIME, THE "ENG COMP L STALL" MESSAGE ILLUMINATED. SHORTLY TOct 5, 2024 · N921AT · Boeing 717200 · Turbine Engine Compressor SectionSDR DALA2024050805015Skin · dentedBIRD STRIKE DAMAGE TO RT HORIZONTAL STAB AT XFS 169.50. OVERALL DENT LENGHTH IS 12 IN LONG BY 7 IN WIDE. SECONDARY DENT IS 2.75 IN LONG BY 2.0 IN WIDE 0.125 DEPTH. THIRD DENT IS 4 IN LONG BY 3 IN WIDE 0.030 IN DEPTH. PERFORMED DAMAGE CONTAINMENT HFEC IAW TOPP Mar 7, 2024 · N921AT · Boeing 717200 · Horizontal Stabilizer, Plate/SkinSDR DALA2024021502205Display · inoperativeSHIP 9577 -MISC/DE- THE FLIGHT CREW REPORTED ELECTRICAL ISSUES, VIA FAILURE, FCP BLANKING, NAV DISPLAY BLANKING, FLIGHT DIRECTORS NOT WORKING, AND ALL ARE CAUSING UNRELIABLE PRIMARY NAVIGATION. THE QRH WAS COMPLIED WITH AND THE SITUATION STABILIZED ONCE THE EMFeb 14, 2024 · N921AT · Boeing 717200 · Central ComputersSDR DALA2024020801688Sign · damagedTHE FORWARD EMERGENCY EXIT SIGN IS DAMAGED. MAINTENANCE REINSTALLED AND SECURED THE FORWARD EMERGENCY EXIT SIGN. OK FOR SERVICE. (LP #0191155)Feb 7, 2024 · N921AT · Boeing 717200 · Emergency LightingSDR DALA2023092007729Unknown · unknownTHE EMERGENCY WINDOW, EXIT ROW, EMER EXIT COVER DIFFFUSER LENS FELL OFF. MAINTENANCE RESECURED COVER. (LP #2978024)Sep 19, 2023 · N921AT · Boeing 717200 · Emergency LightingSDR DALA2023072606039Unknown · unknownCREW TURNED ON WINDOW ANTI-FOG AND IMMEDIATELY NOTICED SMOKE FROM NEAR WINDOW FIN, ACCOMPANIED WITH AN ELECTRICAL BURN SMELL. CONTRACT MAINTENANCE INSPECTED F/O WINDOW AND CONFIRMED THE SMOKE AND ODOR WHEN THE SWITCH IS TURNED ON. NO EVIDENCE OF SMOKE OR ODOR Jul 9, 2023 · N921AT · Boeing 717200 · Windshield/Door Rain/Ice RemovalSDR DALA2023032602314Unknown · unknownAIRCRAFT 9577, TAIL COMPT FRAME CRACKED STA 1133 AT STR 2R-MARKED. CORRECTIVE ACTION: COMPLIED WITH ER/A 607133-14 REV. ORIG. PRI REV. "0" ALL INSTRUCTIONAL STEPS. I ALL INSTRUCTIONAL STEPS ON ER/A 607133-14 REV. ORIG. PRI REV. "0" MATCH FINALE ER/A 607133-14 Mar 24, 2023 · N921AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2023031802047Unknown · unknownAIRCRAFT 9577, TAIL COMPT STR 2L CRACKED AT STA 1133. CORRECTIVE ACTION: REPAIRED PER B717 SRM 53-00-05-2R PROCEDURE 2. (LP 2675309)Mar 17, 2023 · N921AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2023022701430None · noneFLOOR NEAR 1ST CLASS COAT CLOSET SEEMS SOFT. REMOVED AND FABRICATED FLOOR PANEL PER B717 AMM 53-21 AND SRM 53-20-50 PG 2. FIG 3. FOUND SUPPORT ANGLE BROKEN AT STA 237. REMOVED, FABRICATED, DRILLED UP, PRIMED, AND PAINTED A NEW SUPPORT ANGLE. INSTALLED FLOOR SUFeb 24, 2023 · N921AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2022101406661Battery Pack · dischargedAIRCRAFT 9577, ROW 20 EMERGENCY EXIT LOWER LIGHTS INOP. CORRECTIVE ACTION: REPLACED EMERGENCY BATTERY ROW 19 RT AND EMERGENCY PWR SUPPLY ROW 23 RIGHT. LP 9383357Oct 11, 2022 · N921AT · Boeing 717200 · Emergency LightingSDR DALA2022033102147Doubler · damagedAFT ATG ANTENNA AND DOUBLER DAMAGED REF 0514-2001, NRC 11. COMPLIED WITH REPAIR AT ATG ANTENNA PER ER/A 598111-14, PRI REV 0,1,2,3. FINAL REV A. ASSOCIATED ER/A 14-598111 ADDED FOR AC 9577. (LP #2176117)Mar 29, 2022 · N921AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2023032802390Unknown · unknownAIRCRAFT 9577, 7 EXPERIENCED A TAILSTRIKE UPON ARRIVAL INTO ATL. SKIN PANEL 5919707-521 AND THE EXTERNAL DOUBLER (PN P28538) ASSOCIATED WITH THE AFT ATG4 ANTENNA INSTALLATION (ASSY P19112-2005) WERE FOUND DAMAGED BETWEEN STA 974 TO STA 994 AND LONGERON 29L TO Mar 27, 2022 · N921AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2021120807571None · noneTHE AFT FLIGHT ATTENDANT JUMPSEAT SEAT BELT BUCKLE DISCONNECTED FROM THE BELT. THIS COULD PREVENT PROPER RETENTION OF THE OCCUPANT IN THE SEAT RESULTING IN PERSONAL INJURY AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. THE BELT DISCREPANCY WAS FORWARDEDDec 6, 2021 · N921AT · Boeing 717200 · Passenger Compartment EquipmentSDR DALA2021072204141Lens · missingTHE THE FLIGHT ATTENDANT FOUND THAT THE OVERWING FWD SIDE EMERGENCY EXIT SIGN COVER DIFFUSER LENS IS MISSING. DFRD BY WEISS 00389354 HSV 21JUL21 RII: N ENTR 00389354 P MCC FCP DEFERRAL, FLIGHT CREW PLACARD REQUIRES VALIDATION FLIGHT CREW PLACARD INSTALLED. FOUJul 21, 2021 · N921AT · Boeing 717200 · Emergency LightingSDR DALA2021061403202Skin · corrodedLT WING UPPER SURFACE CORRODED. AFT OF #5 SLAT, APROX 6 FEET INBD FROM WING-TIP. MARKED. REPAIRED PER ER/A 591833-14 REV. ORIGINAL (PRI AND ER/A MATCHES). (LP# 1838785)Jun 13, 2021 · N921AT · Boeing 717200 · Leading Edge DevicesSDR DALA2021061403200Cargo Track · corrodedCORROSION FOUND ON BOTTOM SIDE OF AFT CARGO TRACK SECTION. MARKED. REPLACED TRACK, REF. BAC DWG 5956331. (LP #1836707)Jun 11, 2021 · N921AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2021062403413Door Frame · corrodedFWD CARGO DOOR SURROUND HAS CORROSION IN MULTIPLE LOCATIONS (MARKED). SUMMARY NRC 133-0009:5300-2007/006 00257: FABRICATED AND INSTALLED 2 SPLICES REF B717 SRM 53-20-15-2R. SUMMARY NRC 133-0009:5300-2007/006 00257: FABRICATED AND INSTALLED 2 SPLICES REF B717 SJun 10, 2021 · N921AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2021061403201Door Frame · corrodedFWD CARGO DOOR SURROUND HAS CORROSION IN MULTIPLE LOCATIONS (MARKED). FABRICATED AND INSTALLED 2 SPLICES REF B717 SRM 53-20-15-2R. (LP #1836365)Jun 10, 2021 · N921AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2021060203011Door Sill · corrodedLOWER DOOR SILL IS CORRODED AT LOC C-2 DOOR CUT OUT. REPAIRED PER B717 SRM 53-20-15-2R. (LP #1826803)Jun 1, 2021 · N921AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2021060203010Cam · out of adjustTHE TAILCONE RELEASE CAM IS OUT OF ADJUSTMENT. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. NRC 102-0001:5352-2001/001 00303: ADJUSTED TAILCONE RELEASE MECHANISM CAM REF. B717 AMM 53 -52-03. (LP #May 28, 2021 · N921AT · Boeing 717200 · Aerodynamic FairingsSDR DALA2025011500351Door Frame · damagedR1 DOOR CUTOUT SURROUND WAS DAMAGED BY GROUND EQUIPMENT. PERFORM A DAILY INSPECTION OF THE R1 DOOR REWORK AREA REF ER/A 584985-14 REV ORIGINAL, SECTION 2. ACCOMPLISHED DURING LAYOVER IN MSP 31JAN20. FOLLOW ON ACTION IS REQUIRED. ACCOMPLISH SECTION II EVERY DAYJan 31, 2020 · N921AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2019111106537Battery Pack · inoperativeTHE FLOOR LEVEL EXIT SIGNS FOR THE LEFT AND RIGHT AFT OVERWING EXITS ARE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK AT ROW 22 PER B717 AMM 33-51. THE OPERATIONAL CHECK WAS GOOD. (LP #6108599)Nov 8, 2019 · N921AT · Boeing 717200 · Emergency LightingSDR DALA2019092305441Lens · missingTHE EMERGENCY EXIT COVER DIFFUSER LENS IS MISSING. MAINTENANCE REPLACED THE AFT EMERGENCY LIGHT COVER. (LP #1279759)Sep 20, 2019 · N921AT · Boeing 717200 · Emergency LightingSDR DALA2023031702018Unknown · unknownAIRCRAFT 9577, FOUND EVIDENCE OF LIGHTENING STRIKE ON RH FUSELAGE AT STATION 465 AND LONGERON 20. CORRECTIVE ACTION: REMOVED FASTENER WIP 715288. REPAIRED PER B717 SRM 53-02-01-2R PROCEDURE 1. TEMPORARY REPAIR REQUIRES VISUAL INSPECTION AT 3000 CYCLES, PERMANEJun 8, 2019 · N921AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2023031702014Unknown · unknownAIRCRAFT 9577, FOUND EVIDENCE OF LIGHTENING STRIKE ON RH FUSELAGE AT STATION 503 AND LONGERON 19. CORRECTIVE ACTION: REMOVED FASTENER WIP 715288. REPAIRED PER B717 SRM 53-02-01-2R PROCEDURE 1. TEMPORARY REPAIR REQUIRES VISUAL INSPECTION AT 3000 CYCLES, PERMANEJun 8, 2019 · N921AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2023031702013Unknown · unknownAIRCRAFT 9577, FOUND EVIDENCE OF LIGHTENING STRIKE ON RH FUSELAGE AT STATION 465 AND LONGERON 21. CORRECTIVE ACTION: REMOVED FASTENER WIP 715288. REPAIRED PER B717 SRM 53-02-01-2R PROCEDURE 1. TEMPORARY REPAIR REQUIRES VISUAL INSPECTION AT 3000 CYCLES, PERMANEJun 8, 2019 · N921AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2023031702012Unknown · unknownAIRCRAFT 9577, FOUND EVIDENCE OF LIGHTENING STRIKE ON RH FUSELAGE AT STATION 446 AND LONGERON 20. CORRECTIVE ACTION: REMOVED FASTENER WIP 715288. REPAIRED PER B717 SRM 53-02-01-2R PROCEDURE 1. TEMPORARY REPAIR REQUIRES VISUAL INSPECTION AT 3000 CYCLES, PERMANEJun 8, 2019 · N921AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2023031702011Unknown · unknownAIRCRAFT 9577, FOUND EVIDENCE OF LIGHTENING STRIKE ON RH FUSELAGE AT STATION 332 AND LONGERON 20. CORRECTIVE ACTION: REMOVED FASTENER WIP 715288. REPAIRED PER B717 SRM 53-02-01-2R PROCEDURE 1. TEMPORARY REPAIR REQUIRES VISUAL INSPECTION AT 3000 CYCLES, PERMANEJun 8, 2019 · N921AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2023031702010Unknown · unknownAIRCRAFT 9577, FOUND EVIDENCE OF LIGHTENING STRIKE ON RH FUSELAGE AT STATION 313 AND LONGERON 21. CORRECTIVE ACTION: REMOVED FASTENER WIP 715288. REPAIRED PER B717 SRM 53-02-01-2R PROCEDURE 1. TEMPORARY REPAIR REQUIRES VISUAL INSPECTION AT 3000 CYCLES, PERMANEJun 8, 2019 · N921AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2023031702009Unknown · unknownAIRCRAFT 9577, FOUND EVIDENCE OF LIGHTENING STRIKE ON RH FUSELAGE AT STATION 256 AND LONGERON 21. CORRECTIVE ACTION: REMOVED FASTENER WIP 715288. REPAIRED PER B717 SRM 53-02-01-2R PROCEDURE 1. TEMPORARY REPAIR REQUIRES VISUAL INSPECTION AT 3000 CYCLES, PERMANEJun 8, 2019 · N921AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2018052903623Skin · puncturedPUNCTURED AFT MOVABLE FLAP VANE LOWER SKIN, LT WING. THE FLAP VANE LOWER SKIN WAS REPAIRED IAW SRM 57-53-01-2R.May 22, 2018 · N921AT · Boeing 717200 · Trailing Edge FlapsSDR DALA2018052303515Frame · crackedCRACKED FRAME BELOW LONGERON 2R BS 1133. THE FRAME WAS REPLACED IAW SRM 51-41-02-0G, SRM 51-41-05-0G, AND DWG 5913595, REV AP.May 22, 2018 · N921AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2018052303514Frame · crackedCRACKED FORMER BS 715 LT SIDE AT CANTED KEEL INTERNAL STRUCTURE. THE FORMER WAS REPAIRED IAW SRM 51-70-11, REPAIR 2.May 22, 2018 · N921AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2018052303513Access Panel · corrodedCORROSION ON COUNTERSINK HOLES OF FUEL ACCESS PLATE 620EB ON THE RT WING. FOUND TO BE OUT OF LIMITS AND WAS REPLACED.May 22, 2018 · N921AT · Boeing 717200 · Wing, Plate/SkinSDR DALA201805213459Access Panel · corrodedFUEL ACCESS PANEL 520DB CORRODED OUT OF LIMITS IAW SRM 57-10-01-2R, PAR 5. THE ACCESS PANEL WAS REPLACED IAW SRM 57-10-01-2R, PAR 5.May 18, 2018 · N921AT · Boeing 717200 · Wing, Plate/SkinSDR DALA201805213458Former · crackedCRACKED FORMER AT BS 679, RT SIDE AT CANTED KEEL BEAM INTERNAL STRUCTURE. REPAIRED IAW SRM 51-70-11-2R, 51-41-02-0G, AND 51-41-05-0G.May 18, 2018 · N921AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2018051803428Strap · corrodedCORROSION STRAP UNDER LONGERON 26L BTW STA Y=946 TO Y=1002 AT AFT CARGO COMPARTMENT. NEW REPAIR PART WAS INSTALLED PER SRM 51-41-02-0G.May 17, 2018 · N921AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2018051803427Skin · crackedCRACK ON EXTERNAL FUSELAGE SKIN STA Y=1037 BTW LONG 13R-14R. PERMANENT REPAIR WAS ACCOMPLISHED PER ETI-17-18-078 R5 AND ER/A 568647-14 REV ORIGINAL.May 17, 2018 · N921AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2018051803426Longeron · crackedCRACK ON LONGERONS 16R AND 17R STA Y=1022 AT PAX CABIN. LONGERONS 16 AND 17 RT WERE REPAIRED PER SRM 53-00-05-2R-2 FIG 201 AND ER/A 568581-14 REV ORG AND ETI-17-18-093 REV 1.May 17, 2018 · N921AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2018051703392Access Panel · corrodedCORROSION ON SETTLMENT AREA AND COUNTERSINK HOLES OF FUEL ACCESS PANEL 520EB ON THE LT WING. THE ACCESS PANEL WAS REPLACED IAW AMM 28-00-00, AND CARD 2040-0010.May 16, 2018 · N921AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2018051703391Access Panel · corrodedCORROSION ON SETTLMENT AREA AND COUNTERSINK HOLES OF FUEL ACCESS PANEL 520CT ON THE LT WING. THE ACCESS PANEL WAS REPLACED IAW AMM 28-00-00, AND CARD 2040-0010.May 16, 2018 · N921AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2018051703390Access Panel · corrodedCORROSION ON SETTLMENT AREA AND COUNTERSINK HOLES OF FUEL ACCESS PANEL 620CT ON THE RT WING. THE ACCESS PANEL WAS REPLACED IAW AMM 28-00-00, AND CARD 2040-0012.May 16, 2018 · N921AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2018051703389Frame Angle · crackedCRACKED FRAME ANGLE BS 1087, BETWEEN LONGERONS 14 AND 15. THE FRAME ANGLE WAS REPLACED IAW SRM 51-41-05-0G, & DWG 9971140, REV F.May 16, 2018 · N921AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2018051603371Doubler · corrodedCORROSION ON SEVERAL POINTS ON EXTERNAL SKIN AT FUSELAGE EXTERNAL DOUBLER FROM STA Y=851 TO STA Y=870 BTW LONG 27L AND 27R. CORROSION LEVEL 2, DOUBLERS WERE REPLACED PER SRM 53-20-70-2R REPAIR 1.May 15, 2018 · N921AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2018051503325Angle · corrodedCORROSION FOUND ON THE R1 CUSP ANGLE BETWEEN BS 164 - 200. THE ANGLE WAS REPAIRED IAW ER/A 568469-14, REV ORG, AND ETI -17-18-085, REV ORIG.May 15, 2018 · N921AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2018051403296Skin · puncturedPUNCTURE FOUND ON THE AFT MOVABLE LT WING FLAP VANE LOWER SKIN. REPAIRED IAW SRM 57-53-01-2R.May 14, 2018 · N921AT · Boeing 717200 · Trailing Edge FlapsSDR DALA2018051403295Seat Track · corrodedCORROSION FOUND ON THE RT SEAT TRACK, X-44, BS 200 - 205. THE SEAT TRACK WAS REPLACED IAW SRM 51-41-01-0G, 51-41-02-0G, AND 51-41-05-0G.May 13, 2018 · N921AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2018051403294Longeron · crackedCRACKED LONGERON 5L, BS 1022. THE LONGERON WAS REAPIRED IAW SRM 53-00-05-2R-2.May 13, 2018 · N921AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2018051403293Skin · crackedCRACK FOUND ON THE EXTERNAL SKIN BS 1022 BETWEEN LONGERONS 13L - 14L. REPAIRED IAW ER/A 568451-14, REV ORIGINAL, AND ETI-17-18-083, REV 3.May 13, 2018 · N921AT · Boeing 717200 · Fuselage Main, Plate/Skin
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