N892AT

Service difficulty reports · 110

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 = 'N892AT' 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 DALA2026051903064O-Ring · failedDRIVER DO NOT DISPATCH THE AIRCRAFT" - W/O MCC APPROVAL" - CREW REPORTS STRONG FUEL ODOR AFTER APU SHUT DOWN. REMOVED AND REPLACED LT ENG FUEL RETURN LINE O-RING AND RECONNECTED LINE REF B717 AMM 28-24 (1591786) (AIRCRAFT GROUNDED)May 13, 2026 · N892AT · Boeing 717200 · Fuel StorageSDR DALA2025121509132Bolt · missingMISSING AND SUNKEN BOLTS ALONG DOUBLER SPLICE APPROX BTW STA ZFS=49 AND ZFS=76 AT VERTICAL STABILIZER LEADING EDGE. REPAIRED PER ER/A 630634-14. (1338826)Dec 6, 2025 · N892AT · Boeing 717200 · Vertical StabilizerSDR DALA2025121009008Skin · crackedTWO CRACKS ON FUSELAGE SKIN PANEL APPROX ON BS 1076 & 1095, L14R. DAMAGED AREA WERE REPAIRED IAW ER/A 630576-14. (1335394)Dec 4, 2025 · N892AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2025111208300Oil Cap · unsecureNOTICED UNPLEASANT ODOR ON TAXI IN AFTER APU START AND OBSERVED LEAKING DARK FLUID UNDERNEATH APU COMPARTMENT ON SUBSEQUENT WALK AROUND. APU OIL CAP NOT PROPERLY SEATED AND APU AND COMPARTMENT AND AFT FUSELAGE COVERED WITH OIL. THE APU OIL CAP WAS PROPERLY SNov 3, 2025 · N892AT · Boeing 717200 · APU Oil SystemSDR DALA2025071105225Relay · faultedSHIP 9552-DIV- FLIGHT DIVERSION TO CLE DUE TO LOSS OF LEFT GEN AND LEFT AC BUS CROSS TIE LOCKOUT. / CORRECTIVE ACTION: RESET LEFT PCDU & RESET LEFT BUS TIE SWITCH. AS PRECAUTIONARY REPLACED EPCU, PCDU, L GENERATOR RELAY AND L BUS TIE RELAY. OPS NORMAL AND RETUJul 10, 2025 · N892AT · Boeing 717200 · AC Generator-AlternatorSDR DALA2025051903831Tab · damagedSHIP 9552 RT AILERON CONTROL TAB HAS DAMAGE. CORRECTIVE ACTION: RMEOVED RT AILERON CONTROL TAB PER B717 AMM 27-10 WIP 374716. (0967220)May 15, 2025 · N892AT · Boeing 717200 · AileronsSDR DALA2024072607481Oxygen Mask · inoperativeSHIP 9552 -MISC- REFERENCE LOG PAGE #5879904 ABOUT A RAPID DECOMPRESSION EVENT. MASKS AT SEAT ROWS 11C, 18A, 19C, 21C, 24C, 25A, 29A, & AFT F/A SEAT DID NOT DROP DURING THE ODI EVENT. MAINTENANCE FORWARDED THE O2 SYSTEM TO MEL 35-21-01A. "M" PROCEDURES COMPLIEJul 25, 2024 · N892AT · Boeing 717200 · Passenger Oxygen SystemSDR DALA2024072607480Duct · disconnectedSHIP 9552 -DIV/PRESS/DE- THE FLIGHT CREW DIVERTED THE AIRCRAFT TO MEM FOLLOWING THE RAPID LOSS OF CABIN PRESSURIZATION. CREW DONNED O2 MASKS, DECLARED AN EMERGENCY, AND INITIATED AN EMERGENCY DESCENT TO 10K FEET. CABIN MASKS AUTOMATICALLY DEPLOYED. LANDED SAFEJul 25, 2024 · N892AT · Boeing 717200 · Air Distribution SystemSDR DALA2024060305738Battery Pack · inoperativeTHE FORWARD DOOR LEVER EXIT SIGN IS NOT ILLUMINATING. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY PACK REF B717 AMM 33-61. OPERATIONAL TEST WAS GOOD. (LP #5920917)Jun 1, 2024 · N892AT · Boeing 717200 · Emergency LightingSDR DALA2024040404053None · noneTHE EMERGENCY EXIT SIGNS WERE DISCOVERED TO BE INOPERATIVE AT LOCATIONS: 600, 601, 604, AND 605. THE EXIT SIGNS WERE NOT ILLUMINATED WHEN THE CABIN LIGHTING WAS OFF AS DESIGNED. MAINTENANCE CHECKED AND DETERMINED THAT ALL EMERGENCY EXIT SIGNS OPERATED NORMALLYMar 25, 2024 · N892AT · Boeing 717200 · Standard Practices/StructuresSDR DALA2024011500579Unknown · unknownON WALK AROUND FOUND RIGHT REAR EXIT EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED THE RIGHT OVERWING EMERGENCY EXIT LIGHT ASSEMBLY REF B717 AMM 33-51. (LP #5049081)Jan 15, 2024 · N892AT · Boeing 717200 · Emergency LightingSDR DALA2023121810335Unknown · unknownCRACKS ON LONGERONS 2L AND 2R OF FRAME STA Y=1133 AT AFT ACCESSORY COMPARTMENT. SUMMARY OF NRC 00273: CRACKS ON LONGERONS 2L AND 2R OF FRAME STA Y=1133 AT AFT ACCESSORY COMPARTMENT WERE REPAIRED PER B717-200 SRM 51-41-05-0G, 51-41-01-0G, 51-41-02-0G, 53-00-05-Dec 15, 2023 · N892AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2023121810334Unknown · unknownCRACK ON BEAM 1 BTW STA Y=195 AT FWD PASSENGER DOOR. SUMMARY OF THE NRC 00081: BEAM 1 BTW STA Y=195 AT FWD PASSENGER DOOR WAS REPAIRED PER B717-200 SRM 52-10-02-2R REPAIR 7. (LP #0111304)Dec 15, 2023 · N892AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2023121510288Unknown · unknownSKIN DELAMINATION ON LOWER SURFACE OF VANE. SUMMARY OF NRC 00495: SKIN ON LOWER SURFACE OF VANE WAS REPAIRED PER ERA 613937-14 REV ORIG. SECCTION I: PERMANENT REPAIR. SEC II: ACCOMPLISH WITHIN EVERY 24 MONTHS OR 3,000 CYCLES, WHICHEVER OCCURS FIRTS UNDER LOGPADec 13, 2023 · N892AT · Boeing 717200 · Trailing Edge FlapsSDR DALA2023120810060Unknown · unknownCRACK ON UPPER AFT CORNER OF SKIN AT LH SLIDING WINDOW CUTOUT IN REF NRC 00408. SUMMARY OF NRC 00487: UPPER AFT CORNER OF SKIN AT LH SLIDING WINDOW CUTOUT WAS REPAIRED PER PRI 614087-14 REV 2 AND ER/A 614087-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. ASSOCIADec 7, 2023 · N892AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2023120810059Unknown · unknownCORROSION ON PREVIOUS REPAIR ON FRAME STA 927 BTW LONGERONS 29L-28L AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00145: CORROSION LEVEL 2. PREVIOUS REPAIR ANGLE ON FRAME STA 927 BTW LONGERONS 29L-28L AT AFT CARGO COMPARTMENT WAS REPLACED PER B717-200 SRM 53-20-07-Dec 7, 2023 · N892AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2023120109871Unknown · unknownCRACK ON OUTER PAN BTW L26R AND STA Y=415 AT FWD CARGO DOOR. SUMMARY OF NRC 00059: OUTER PAN BTW L26R AND STA Y=415 AT FWD CARGO DOOR WAS REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDURE 1, REPAIR 1. (LP #0089031)Nov 30, 2023 · N892AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2023113009840Unknown · unknownCORROSION ON DOOR JAMB LOWER AT AFT CARGO DOOR. SUMMARY OF NRC 00067: CORROSION LEVEL 2. DOOR JAMB LOWER AT AFT CARGO DOOR WAS REPAIRED PER B717-200 SRM 53-20-15-2R REP 7. (LP #0088493)Nov 30, 2023 · N892AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2023112709726Unknown · unknownCORROSION ON CABIN SEAT TRACK X=-44.5, BTW Y =200/256. SUMMARY OF NRC 00226: CORROSION LEVEL 2. SEAT TRACK X=-44.5, BTW Y=200/256 WAS REPAIRED PER B717-200 SRM 53-20-52-2R PROCEDURE 5 REPAIR 5 FIG 201 SHEET 1,2,9,10,11. (LP #0081182)Nov 25, 2023 · N892AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2023112209648Unknown · unknownA CRACK ON FLOOR WEB, STA Y=196 TO 200 X-30 TO X-35 APROX WAS FOUND AT PASSENGER CABIN IN REF NRC #00226. SUMMARY OF NRC 00490: REPAIR WAS PERFORMED PER B717 SRM 51-70-10-2R PAR 4 FIG 201. (LP #0075520)Nov 21, 2023 · N892AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2023112109571Unknown · unknownCRACK ON REAR SPAR RUDDER ACCESS PANEL 1. SUMMARY OF NRC 00312: REAR SPAR RUDDER ACCESS PANEL 1 WAS REPAIRED PER B717-200 SRM 55-00-00-2R PROCEDURE 2, REPAIR 2, PARAGRAPH A, FIGURE 201. (LP #0074053)Nov 20, 2023 · N892AT · Boeing 717200 · Rudder, Plate/SkinSDR DALA2023112009528Unknown · unknownCORROSION ON CABIN FLOOR SUPPORT, STA X=7, BTW Y=148/200. SUMMARY OF NRC 00214: CORROSION LEVEL 2. FLOOR SUPPORT, STA X=7, BTW Y=148/200 WAS FABRICATED PER DWG 9936534 REV BW AND REPLACED PER B717-200 SRM 51-41-01-0G. (LP #0072026)Nov 19, 2023 · N892AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2023112009527Unknown · unknownCORROSION ON CABIN FLOOR SUPPORT, STA X=-7, BTW Y=148/200. SUMMARY OF NRC 00211: CORROSION LEVEL 2. FLOOR SUPPORT, STA X=-7, BTW Y=148/200 WAS FABRICATED PER DWG 9936534 REV BW AND REPLACED PER B717-200 SRM 51-41-01-0G. (LP #0071998)Nov 19, 2023 · N892AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2023112009525Unknown · unknownCRACK INTERCOSTAL BTW BEAM NO 4 TO BEAM NO 5 AND STA Y=185.5 AT FWD PASSENGER DOOR INTERNAL EXTRUCTURE. SUMMARY OF NRC 00368: INTERCOSTAL BTW BEAM NO 4 TO BEAM NO 5 AND STA Y=185.5 AT FWD PASSENGER DOOR INTERNAL EXTRUCTURE WAS FABRICATED AND REPLACED PER DOUGLNov 18, 2023 · N892AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2023112009524Unknown · unknownCORROSION ON CABIN FLOOR SUPPORTS (2 EA) STA Y=200, BTW X=7/-7, AND BTW X=-45.5/-56.5 (OUT OF LIMITS). SUMMARY OF NRC 00412: CORROSION LEVEL 2. FLOOR SUPPORTS (2 EA) STA Y=200, BTW X=7/-7, AND BTW X=-45.5/-56.5 WERE FABRICATED PER B717 DWG 9936534 REV BW AND RNov 18, 2023 · N892AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2023111609436Unknown · unknownCORROSION ON CABIN FLOOR SUPPORT, STA X=44.5, BTW Y=160/196. SUMMARY OF NRC 00215: CORROSION LEVEL 2. FLOOR SUPPORT, STA X= 44.5, BTW Y=160/196 WAS FABRICATED PER DWG 9936534 REV BW AND REPLACED PER B-717-200 SRM 51-41-02-0G AND 51-41-05-0G. (LP #0065622)Nov 15, 2023 · N892AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2023111409352Unknown · unknownCORROSION ON CABIN FLOOR SUPPORT, STA X=-44.5, BTW Y=160/200. SUMMARY OF NRC 00212: CORROSION LEVEL 2. CABIN FLOOR SUPPORT STA X=-44.5 BTW Y=160/200 WAS REPLACED PER DWG 9936534 REV BW AND PER B717-200 SRM 51-41-02-0G. (LP #0063456)Nov 13, 2023 · N892AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2023111309296Unknown · unknownCORROSION ON CABIN FLOOR SUPPORTS (2 EA), STA Y=180, BTW X=13/38 AND BTW X=-7/-44.5. SUMMARY OF NRC 00210: CORROSION LEVEL 2. FLOOR SUPPORT (2 EA), STA Y=180, BTW X=13/38 AND BTW X=-7/-44.5, WERE FABRICATED AND REPLACED PER DWG 9936534 REV BW AND B717-200 SRM Nov 9, 2023 · N892AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2023111309295Unknown · unknownCORROSION ON FLOOR WEB, STA Y=196 TO 200 X-50 TO X-55 AND Y=201 AT X- 44 TO X-48 AT PASSENGER CABIN (OUT OF LIMIT). PER NRC 0411: CORROSION LEVEL 2. FLOOR WEB STA Y= 196 TO 200 X-50 TO X-55 AND Y=201 AT X-44 TO X-48 AT PASSENGER CABIN WAS REPAIRED PER B-717-20Nov 8, 2023 · N892AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2023110909225Unknown · unknownCORROSION ON CABIN FLOOR SUPPORT, STA Y=196, BTW X=22/44.5. SUMMARY OF NRC 00221: CORROSION LEVEL 2. FLOOR SUPPORT STA Y=196, BTW X=22/44.5 WAS REPLACED PER DWG 9936534 REV BW AND PER B717-200 SRM 51-41-02-0G PAR 4. (LP #0055761)Nov 8, 2023 · N892AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2018102206192Lens · missingEMERGENCY EXIT COVER DIFFUSER LENS DAMAGED OR MISSING AT LOCATIONS: 600. EMERGENCY EXIT COVER IS MISSING AND BARE WIRES ARE EXPOSED. MAINTENANCE REPLACED THE EMERGENCY EXIT SIGN EQUIPMENT L2-832 AT DOOR R1 PER WDM 33-51-14. OPERATIONAL CHECK IS GOOD. (LP 07917Oct 19, 2018 · N892AT · Boeing 717200 · Emergency LightingSDR DALA201808064878Lens · damagedEMERGENCY EXIT LIGHT LENS DAMAGED. MAINTENANCE SECURED THE DAMAGED EXIT SIGN LENS.Aug 2, 2018 · N892AT · Boeing 717200 · Emergency LightingSDR DALA201808064877Lens · damagedEMERGENCY EXIT LENS WAS DAMAGED. MAINTENANCE SECURED THE DAMAGED EXIT SIGN LENS.Aug 2, 2018 · N892AT · Boeing 717200 · Emergency LightingSDR DALA2018072504673Cover · looseTHE FWD CENTER AISLE CEILING EMERGENCY EXIT SIGN COVER IS LOOSE. MAINTENANCE REATTACHED THE EXIT SIGN. OPERATIONAL CHECK IS GOOD.Jul 23, 2018 · N892AT · Boeing 717200 · Emergency LightingSDR DALA2018071604490Light · unsecureTHE FORWARD MOST EMERGENCY EXIT LIGHT IS NOT SECURELY FASTENED TO THE CEILING AS DESIGNED. MAINTENANCE SECURED THE LIGHT ASSEMBLY AS REQUIRED. OK FOR SERVICE.Jul 14, 2018 · N892AT · Boeing 717200 · Emergency LightingSDR DALA2018040902285Bracket · brokenLOUD BUZZING NOISE AND VIBERATION UNDER THE FLOOR AT ROW 19A. FOUND EIGHT RUBBER NUTS AT THE LT OVERWING FILLET PANEL. RAN HYD PUMPS AND FUEL PUMPS, ALL SOUND OK. INSPECTED THE UPPER LT WING FILLET AREA AND FOUND MIDDLE SUPPORT BRACKET FOR FWD OVERWING FILLEApr 8, 2018 · N892AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2018030301831Skin · crackedCRACKED LOWER SKIN AT RT UPPER MOVABLE VANE. RT UPPER MOVABLE VANE WAS REPAIRED PER SRM 57-53-01-2R-1 PARAGRAPH 4 FIG 201.Mar 2, 2018 · N892AT · Boeing 717200 · Trailing Edge FlapsSDR DALA2018022801266Door Frame · crackedA CRACK WAS FOUND ON THE AFT CARGO DOOR FRAME AFT EDGE. THE DOOR FRAME WAS REPAIRED IAW SRM 53-20-15-2R, PROCEDURE 12, PARAGRAPH 6 A.Feb 27, 2018 · N892AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2018022801265Door Frame · crackedCRACK FOUND ON THE LT NLG DOOR FRAME BEAM Y=40. REPAIRED IAW SRM 53-10-14-2R, PROCEDURE 2, REPAIR 2.Feb 27, 2018 · N892AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2018022801264Door Frame · crackedCRACK ON THE RT NLG DOOR FRAME BEAM Y=40. REPAIRED IAW SRM 53-10-14-2R, PROCEDURE 2, REPAIR 2.Feb 27, 2018 · N892AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2018021500906Lamp · inoperativeDURING A SERVICE CHECK, FOUND THE TAIL CONE EMERGENCY LIGHT INOPERATIVE. TROUBLESHOT THE EMERGENCY LIGHT IAW AMM 33-51. CLEANED AND REPLACED THE LAMPS. OPS CHECKED GOOD.Feb 15, 2018 · N892AT · Boeing 717200 · Emergency LightingSDR DALA2016102407460Pylon · crackedNUMBER 1 PYLON UPPER AND LOWER AFT COWL ATTACH POINTS HAVE CRACKS IN CUTOUTS ON SKIRT FAIRING. REMOVED BRACKETS, FITTINGS, GUSSETS, AND SHIMS. BLENDED OUT CRACKS IN RADIUS. PERFORMED PENETRANT INSPECTION OF CUTOUT LOCATIONS IAW ER/A 552108-14 REV. A SECTION 1 Oct 23, 2016 · N892AT · Boeing 717200 · Nacelle/Pylon, Main FrameSDR DALA2016102307459Pylon · crackedLEFT ENGINE PYLON APRON FOUND TO BE CRACKED IN FOUR LOCATIONS. REPAIRED IAW ER/A 552108-14.Oct 22, 2016 · N892AT · Boeing 717200 · Nacelle/Pylon, Main FrameSDR DALA2016100306961Skin · damagedREV ORIG, PERFORMED CUT OUT OF DAMAGE AS SHOWN FIG 1. C/W HFEC AND BHEC PER PRI 551316-14 REV ORIG NR ITEMS 2034. FABRICATED REPAIR PARTS AS SHOWN FIG 1 REF PRI 551316-14 REV ORIG. COMPLETED REPAIR PER PRI 551316-14 REV ORIG COMPLETING ER/A 551316-14 REV OROct 2, 2016 · N892AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2016050203478Battery Pack · inoperativeDURING LINE CHECK, MAINTENANCE FOUND THAT THE OVERHEAD EMERGENCY LIGHTING BETWEEN ROWS 16 AND 17 WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKS FOR THE NOTED LIGHTED AREAS AND THE OPS CHECK WAS GOOD.Apr 29, 2016 · N892AT · Boeing 717200 · Emergency LightingSDR DALA2016102807813Cusp Web · corrodedLEFT OUTER CUSP WEB CORRODED AT BS 488. CORRISION BLENDED AND FOUND BEYOND ALLOWABLE LIMITS. REPAIRED THE CUSP WEB IAW SRM 53-00-55 ALLOWABLE DAMAGE 1 AND 53-00-55 REPAIR 4.Feb 22, 2016 · N892AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016022201276Fuel Tank · corrodedLEFT WHEEL WELL TO RT WHEEL WELL FUEL TANK SKIN PLANK PANEL T/E CORRODED AT SEVERAL LOCATIONS. CLEAN/ EVAL, TREAT & PAINT REF OR NRC 62937-0100-0065. BLENDED OUT CORROSION ON RT WHEEL WELL FUEL TANK SKIN PLANK PANEL. MEASURED THICKNESS LOSS OF .015 TAG 3310Feb 21, 2016 · N892AT · Boeing 717200 · Fuel StorageSDR DALA2016102707773Seat Track · corrodedCENTER SEAT TRACK HAS MULTIPLE DEFECTS FROM BS 148 TO 1022. CLEANED RH CENTER SEAT TRACK AS MARKED, STA 148-STA 1032 AND FOUND ALL DEFECTS TO BE NEGLIGIBLE IAW SRM 51-10-02 PG. 65 PAR. F(1). REPLACED THE SEAT TRACK IAW SRM 51-41-05 PG. 32 ITEM 10, 51-40-Feb 16, 2016 · N892AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2016022001268Cusp Web · corrodedRIGHT CUSP WEB HAS CORROSION AROUND FWD LIGHTING HOLE AFT OF BS 522. BLENDED AREA IAW 53-00-00, PG 105, FIG 103. REMOVING .006", FOUND TO BE OUT OF LIMITS, DRILLED & LOCATED NEAR CUSP WEB IAW SRM 51-40-08, PG 2, TABLE 6 AND 51-40-08, PG 7, FIG 1, INSTALLED NFeb 16, 2016 · N892AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016021801160Cusp Web · crackedRT CUSP WEB IS CRACKED AT APPROXIMATELY RBL 47 UNDER SEAT TRACK BS 674. REMOVED OLD CUSP WEB FROM BS 656 TO 715 INSTALLED NEW CUSP WEB IAW SRM 51-41-05 & 51-41-02 AND REINSTALLED. REMOVED SEAT TRACKS RBL 45 & RBL 54, BS 598-715 IAW SRM 51-41-01, PG 3, FIG 1.Feb 16, 2016 · N892AT · Boeing 717200 · Fuselage Miscellaneous Structure
Back to N892AT