N980AT

Service difficulty reports · 245

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 = 'N980AT' 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 DALA2024071707225Cusp Web · damagedMISSING MATERIAL ON CUSP WEB MEMBRANE STA 527 X=-59 AT PAX CAB. SUMMARY OF NRC 00501: CUSP WEB MEMBRANE STA 527 X=-59 AT PAX CAB WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4 FIG 215. (LP #0450942)Jul 16, 2024 · N980AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2024071507163Beam · crackedCRACK ON DOOR BEAM 1 BETWEEN STA 170 AND STA 180 (UPPER AFT CORNER) AT FWD PASSENGER DOOR L1. SUMMARY OF NRC 00157: DOOR BEAM 1 BETWEEN STA 170 AND STA 180 (UPPER AFT CORNER) AT FWD PASSENGER DOOR L1 WAS REPAIRED PER B717-200 SRM 52-10-02-2R PROCEDURE 7. (LP #Jul 14, 2024 · N980AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2024071507162Frame · crackedCRACK ON UPPER EDGE FRAME, 2 FROM UPPER EDGE AND 38 FROM FWD EDGE AT FWD CARGO COMPARTMENT DOOR. SUMMARY OF NRC 00107: UPPER EDGE AND FWD EDGE AT FWD CARGO COMPARTMENT DOOR WAS REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDURE 1 REPAIR 1.Jul 14, 2024 · N980AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2024071507160Longeron · crackedCRACK ON LH LONGERONS 4, 5 AND 6 STA Y=1022 AT C PAX. SUMMARY OF NRC 00362: LONGERONS 4, 5, AND 6 STA Y=1022 AT C PAX WERE REPAIRED PER B717-200 SRM 53-00-05-2R PROC 2 REPAIR 2 PAR 5 FIG 201. (LP #0444631)Jul 13, 2024 · N980AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2024071507159Cusp Web · crackedCRACK ON CUSP WEB MEMBRANE STA 674 X=-46 AT PAX CAB. SUMMARY OF NRC 00499: CUSP WEB MEMBRANE STA 674 X=-46 AT PAX CAB WAS REPAIRED PER B717 SRM 53-00-55-2R PROCEDURE 4 REPAIR 4 FIG 219. (LP #0444565)Jul 13, 2024 · N980AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024071507157Frame · crackedCRACK ON FRAME STA Y=1037 AND STR 17 LH AT C. PAX. SUMMARY OF NRC 00361: FRAME AT STA Y=1037 AND STR 17 LH WAS REPAIRED PER B717-200 SRM 53-20-07-2R REPAIR 4 PAR 5 A. (LP #0444212)Jul 12, 2024 · N980AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2024071507155Cusp Web · crackedTHE CUSP WEB WAS FOUND CRACKED STA Y=218-220 / -X=44.5. SUMMARY OF NRC 00762: CUSP WEB STA Y=218-220 / -X=44.5. WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4. (LP #0443614)Jul 12, 2024 · N980AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024071207051Pan · crackedAFT REMOVAL ANGLE CRACK ON INNER AND OUTER PAN WAS FOUND BTW BEAM 1-2 AND STA Y=954 AT AFT CARGO COMPARTMENT DOOR. SUMMARY OF NRC 00665: INNER AND OUTER PAN BTW BEAM 1 TO BEAM 2 AND STA Y=954 AT AFT CARGO COMPARTMENT DOOR WERE REPAIRED PER B717-200 SRM 52-30-0Jul 11, 2024 · N980AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2025040402563Bearing · corrodedCORROSION ON BEARINGS (6 EA) AND BUSHINGS (2 EA), OF THE RH ELEVATOR TAB AND RH ELAVATOR GEARED TAB. ALSO CORROSION ON ALL HARDWARE OF THE RH ELEVATOR TAB AND RH ELAVATOR GEARED TAB. SUMMARY OF NRC 00658: CORROSION LEVEL 2. BEARINGS (6 EA) AND BUSHINGS (2 EA) Jul 10, 2024 · N980AT · Boeing 717200 · Elevator StructureSDR DALA2024081908240Skin · damagedLIGHTING STRIKE R/H O/B ELEVATOR. C/W REP CHK PER ERA 618187-14 REV A SECTION 2. NO FURTHER DAMAGE FOUND ON RIGHT ELEVATOR. OK TO CONT ON MON. TIME LIMITS FOR SECTION I: TIME LIMITED REPAIR EXTENDED FROM 24 DAYS TO 34 DAYS PER ER/A 618187-14 REV B. ASSOCIATEDJun 6, 2024 · N980AT · Boeing 717200 · Elevator, Plate/SkinSDR DALA2024060405771Engine · stalledSHIP 9546 -DIV/IFSD/DE- THE FLIGHT CREW NOTED THAT THE #1 ENGINE STALLED MULTIPLE TIMES IN FLIGHT WHICH RESULTED IN A "LT ENG SYS FAIL" MESSAGE. FLIGHT CREW SHUT DOWN THE ENGINE PER THE QRH, THEY DECLARED EMERGENCY WITH ATC, AND DIVERTED THE AIRCRAFT TO LAND AJun 2, 2024 · N980AT · Boeing 717200 · Turbine Engine Compressor SectionSDR DALA2024051605256Battery Pack · faultedAFT, CENTER EMERGENCY EXIT SIGN BECOMES ILLUMINATED THEN EXTIGUISHES INTERMITENTLY. REPLACED POWER SUPPLY ASSEMBLY AND BATTERY PACK AT B5-230 PER B717 AMM 33-51. ONCE BATTERY CHARGED, THE OPERATIONAL CHECK WAS GOOD. (LP #5822592)May 16, 2024 · N980AT · Boeing 717200 · Emergency LightingSDR DALA2024010210752Unknown · unknownCORROSION WAS FOUND ON THREADS OF ACME SCREW AT HORIZONTAL STAB PER AMDS 2740-01114-03, STEP # 2.C. CORRODED SCREW AT HORIZONTAL STAB WAS REPLACED BY SERVICEABLE SCREW AT HORIZONTAL STAB. (LP #0128653)Dec 27, 2023 · N980AT · Boeing 717200 · Horizontal Stabilizer Miscellaneous StructureSDR DALA2023122810694Unknown · unknownDENTS (8 LOCATIONS) ON UPPER SKIN OF AFT MOVABLE VANE BTW STA XRS=77 TO XRS=88 AT RH WING. SUMMARY OF NRC 00077: AFT MOVABLE VANE BTW STA XRS=77 TO XRS=88 OF RH WING WAS REPAIRED PER ER/A 614501-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. ASSOCIATED ER/A 14-6Dec 27, 2023 · N980AT · Boeing 717200 · Trailing Edge FlapsSDR DALA2023122410540Unknown · unknownCORROSION ON LOWER DOOR JAMB BTW STA:946 TO 994 AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00033: CORROSION LEVEL 2. LOWER DOOR JAMB BTW STA:946 TO 994 AT AFT CARGO COMPARTMENT WAS REPAIRED PER B717 SRM 53-20-15-2R-7 REPAIR 7. (LP #0120705)Dec 21, 2023 · N980AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2023121810336Unknown · unknownCRACK WAS FOUND ON WEB STA Y=670, X=-56 APROX AT CABIN PAX. SUMMARY OF NRC 00078: WEB STA Y=670, X=-56 WAS REPAIRED PER B717 SRM 53-00-55-2R-4. (LP #0114428)Dec 17, 2023 · N980AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2023122110467Cover · missingMAINTENANCE FOUND THAT LEFT ENGINE FORWARD HOIST POINT COVER WAS MISSING FROM THE NOSE COWLING. THE DISCREPANCY WAS DEFERRED TO NEF 71-10-02 AND THE PLACARDS WERE INSTLALLED. COWL HOIST SCREW MPN AN565AC624H20 REF CMM 71-11-05 FIG 1 SHEET 4 ITEM 220 00-2500-3-Oct 16, 2023 · N980AT · Boeing 717200 · Nacelle/Pylon, Main FrameSDR DALA2023100408161Unknown · unknownTHE AFT BULKHEAD DOOR EMERGENCY LIGHT EXIT SIGN IS NOT ILLUMINATING. RELAMPING IT DID NOT HELP. CHECKED FOR POWER AND DISCOVERED THERE WAS NO VOLTAGE. REPLACED THE B5-260 EMERGENCY LIGHT BATTERY PER B717 AMM 33-51. OPERATIONAL CHECK IS NOW NORMAL. (LP #4941969Oct 4, 2023 · N980AT · Boeing 717200 · Emergency LightingSDR DALA2023090507200Unknown · unknownTHE FLIGHT DECK OVERHEAD EMERGENCY LIGHT IS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY POWER PACK REF B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #9967944)Sep 4, 2023 · N980AT · Boeing 717200 · Emergency LightingSDR DALA2023071705778Unknown · unknown1 CRACK INDICATION ON L/H VERTICAL (MARKED) WHILE PERFORMING AA 5530-01048 AND AD 2018-10-08 BHEC INSPECTION. REINSPECTED CRACK IN STEP 16 CRACK CONFIRMED IN SKIN LAYER OF L/H VERTICAL STAB (MARKED) REF CARD AA5530-01048 AND AD 2018-10-08. C/W ERA 610480-14AD Jul 15, 2023 · N980AT · Boeing 717200 · Vertical Stabilizer, Plate/SkinSDR DALA2023071705777Unknown · unknownFOUND CRACK IN SKIN TO BE OUT OF LIMITS. COMPLIED WITH PRI 610480-14 AD REV 0. COMPLIED WITH PRI 610488-14AD REV 1 ALL INSTRUCTIONS ON PRI 610480-14AD REV 0 AND REV 1 ARE C/W AND MATCH FINAL ERA 610480-14 REV ORIGINAL. (LP #2866614)Jul 15, 2023 · N980AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2023053104339Unknown · unknownNOTED CRACK INDICATIONS IN 6 HOLES BELOW EXISTING REPAIR (MARKED). REF AA 5530-01048-02 STEP 8, AA 2018-10 -08. SEPARATED LAYERS REF STEP 9 OF AA CARD 5530-01048-02. CONFIRMED CRACKS ARE IN SKIN ONLY (7 EA). INSTALLED REPAIR DOUBLER PER ERA 609262-14 AD REV ORMay 31, 2023 · N980AT · Boeing 717200 · Vertical Stabilizer, Plate/SkinSDR DALA2022112907615Lens · detachedDURING CABIN WALK THROUGH, THE OVERHEAD EMERGENCY LIGHT COVER WAS NOTED AS MISSING. MAINTENANCE INSTALLED A NEW EMERGENCY LIGHT LENS & COVER ON AFT MOST RIGHT OVERHEAD EMERGENCY LIGHT PER AMM 33-51-08. NO FURTHER DEFECTS NOTED. (LP #9347261)Nov 28, 2022 · N980AT · Boeing 717200 · Emergency LightingSDR DALA2022091406087None · noneDURING PACK HEALTH CHECK AMT WENT TO AFT (DISARMED) DOOR TO WORK CARDS FOR HEALTH CHECK. AMT LOOKED DOWN CAT WALK AND NOTICED TAIL CONE SLIDE BUSSEL OPENED AND TAIL CONE SLIDE HALF WAY OPENED BUT NOT BLOWN. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATSep 13, 2022 · N980AT · Boeing 717200 · Escape SlideSDR DALA2022070504624None · noneTHE EMERGENCY CEILING LIGHT LENS IS MISSING AT ROW 25. MAINTENANCE INSTALLED THE CEILING LIGHT LENS COVER AT ROW 25 PER IPC 33-51-08-01, ITEM 35 40-45. (LP #8930838)Jul 1, 2022 · N980AT · Boeing 717200 · Emergency LightingSDR DALA2022070504622None · noneDURING SERVICE CHECK, MAINTENANCE FOUND THE OVERHEAD FWD EXIT LIGHT AND FWD DROP CEILING LIGHTS WERE NOT OPPERATING WITH THE EMERGENCY LIGHT SWITCH ON. THE BATTERY AND CHARGER AT POSITION B5-259 WERE REPLACED IN REF TO B717 AMM 33-51. OPERATIONAL CHECK WAS GOOJun 27, 2022 · N980AT · Boeing 717200 · Emergency LightingSDR DALA2022051803424None · noneTHE FWD CEILING EMERGENCY LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK AT ROW 10. ALL LIGHTS NOW OPERATE NORMALLY. THE AIRCRAFT IS OK FOR SERVICE PER B717AMM 33-50. (LP #8919458)May 17, 2022 · N980AT · Boeing 717200 · Emergency LightingSDR DALA2022042002745Skin · corrodedCORROSION UPPER WING SURFACE AT STA 300, STR 2.5 RIGHT WING. REMOVED CORROSION BY BLENDING AT STA 266 STR 4. MAPPED AREA AFTER BLENDING USING A 1/2" GRID. AREA FOUND TO BE OUT OF LIMITS PER B717 SRM 51-10-04 AND B717 SRM 57-10-01-1A-1 FIG 113 SHEET 3. PERFORMEApr 15, 2022 · N980AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2022042002744Skin · corrodedCORROSION UPPER WING SURFACE AT STA 266, R.S. LEFT WING. REMOVED CORROSION BY BLENDING AT STA 266, R.S.. MAPPED AREA AFTER BLENDING USING A 1/2" GRID. AREA FOUND TO BE OUT OF LIMITS PER B717 SRM 51-10-04 AND B717 SRM 57-10-01-1A-1 FIG 113 SHEET 3. PERFORMED HFApr 15, 2022 · N980AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2022042002743Skin · corrodedCORROSION UPPER WING SURFACE AT STA266, STR 4 LEFT WING. REMOVED CORROSION BY BLENDING AT STA 266 STR 4. MAPPED AREA AFTER BLENDING USING A 1/2" GRID. AREA FOUND TO BE OUT OF LIMITS PER B717 SRM 51-10-04 AND B717 SRM 57-10-01-1A-1 FIG 113 SHEET 3. PERFORMED HFApr 15, 2022 · N980AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2022031001556None · noneAT PUSHBACK, CATERING ATTEMPTED TO OPEN DOOR 1R WHILE ARMED. THE SLIDE FAILED TO DEPLOY. THIS IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. MAINTENANCE FOUND THE RELEASE LANYARD DETACHED. THE SLIDE REMAINED INTACT WITH NO DAMAGE. THE RELEASE LANYARD WAS REINSMar 8, 2022 · N980AT · Boeing 717200 · Escape SlideSDR DALA2022020800817None · noneFOUND LIGHTED EMERGENCY EXIT SIGNS ABOVE LEFT AND RIGHT FORWARD OVERWING EMERGENCY EXITS WILL NOT ILLUMINATE DURING TEST. BOTH LIGHTS ARE POWERED BY POWER SUPPLY B5-121. REPLACED EMERGENCY LIGHT BATTERY ASSEMBLY IN POWER SUPPLY B5-121 IN REF WITH B717 AMM 33- Feb 5, 2022 · N980AT · Boeing 717200 · Emergency LightingSDR DALA2021122308000None · none(LOG 2061219) DURING INSPECTION FOUND CRACKS ON HOLE #6 AND HOLE #7 BELOW STATION ZFS=52.267, ON RH SIDE VERTICAL STABILIZER LEADING EDGE FRONT SPAR CAP. RH SIDE VERTICAL STABILIZER LEADING EDGE FRONT SPAR CAP WAS REPAIRED PER ER/A 534685-14AD REV B SECTION IVDec 22, 2021 · N980AT · Boeing 717200 · Vertical Stabilizer, Plate/SkinSDR DALA2021121607774None · noneCORROSION ON AFT AND FWD DOUBLERS OF FORWARD CARGO COMPARTMENT DOOR JAMB. SUMMARY OF NRC 00116: CORROSION LEVEL 2, AFT AND FWD DOUBLERS OF FORWARD CARGO COMPARTMENT DOOR JAMB WERE REPLACED PER B717 SRM 53-20-15-2R REPAIR 6. (LP #2052502)Dec 14, 2021 · N980AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2021090205178Spar Cap · damagedERA 585576-14AD SECTION I ISSUED FOR DEVIATION TO WC5530-01048 / SB B717-55A0012 INSPECTION TO VERT STAB LEADING EDGE AND SPAR CAP ERA REVISED TO REV 'A' FOLLOWING DTE. REFER TO LP #1505142. FOLLOW ON ACTION REQUIRED. ACCOMPLISH SECTION II INSPECTION EVERY 300Aug 29, 2021 · N980AT · Boeing 717200 · Vertical Stabilizer, Spar/RibSDR DALA2024080207724Skin · damagedEVIDENCE OF LIGHTNING STRIKE 7 INCHES AFT OF STA 332 AT STRINGER 15 L REF LOG 8010442. REMOVED DAMAGED FASTENER AND INSTALLED TEMPORARY FASTENER PER B717 SRM 53-02-01-2R PARA 5 B (2) REPAIR 1. REQUIRES INITIAL VISUAL INSPECTION AT 3000 CYCLES. REPETITIVE INSPEAug 23, 2021 · N980AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2024073007626Skin · damagedEVIDENCE OF LIGHTNING STRIKE5 FWD OF STA 332 AT STRINGER 15L REF LOG 8010441. REMOVED DAMAGED FASTENER AND INSTALLED TEMPORARY FASTENER PER B717 SRM 53-02-01-2R PARA 5 B (2) REPAIR 1. REQUIRES INITIAL VISUAL INSPECTION AT 3000 CYCLES, REPETITIVE INSPECTION EVEAug 23, 2021 · N980AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2020092903191Oil System · leakingDURING CUSTOMER BOARDING, THE CABIN CREW NOTICED SMOKE IN THE CABIN. THE AIRCRAFT WAS DEPLANED NORMALLY THROUGH THE MAIN CABIN DOOR AND JET BRIDGE. CORRECTIVE ACTION: MAINTENANCE FOUND THAT THE APU WAS LEAKING OIL AND REPLACED THE APU. A DUCT BURNOUT WAS ACSep 28, 2020 · N980AT · Boeing 717200 · APU Oil SystemSDR DALA2020072762646Battery Pack · no testDURING EMERGENCY LIGHT TEST, FOUND THE OVERHEAD EMERGENCY LIGHTS ROW 24-29 INOPERATIVE. REPLACED B5-231 BATTERY IAW B717 AMM 33-51, OPERATIONAL CHECK WAS GOOD. (LP #6468795)Jul 26, 2020 · N980AT · Boeing 717200 · Emergency LightingSDR DALA2020022761448Skin · damagedTHE REMOVEABLE VERTICAL LEADING EDGE HAS 15 HOLES OUT OF TOLERANCE IN THE AD SIGNIFICANT AREA - FORWARD CROWN SIDE. MAINTENANCE OPENED UP 65 HOLES PER DWG #SG95550001. BOLT HOLE EDDY CURRENT PER SRM 06-10-01.003 - NO DEFECTS NOTED (QC1969 ). INSTALLED BUSHING Feb 26, 2020 · N980AT · Boeing 717200 · Vertical Stabilizer, Plate/SkinSDR DALA2021090205177Skin · damagedVERT STABILIZER / UPPER REMOVABLE / LE SKIN / ZFS-52 / OS HOLES / AD RELATED. ERA 585576-14 ISSUED AND IS CURRENT. AD RELATED, FOLLOW ON ACTION REQUIRED. SECTION II TO BE ACCOMPLISHED WITHIN 24 MONTHS AFTER SECT.I. SECT.II IS PENDING DAMAGE TOLERANCE ANALYSIS Feb 25, 2020 · N980AT · Boeing 717200 · Vertical Stabilizer, Plate/SkinSDR DALA2020022401345Power Supply · inoperativeTHE COCKPIT EMERGENCY LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT PWR SUPPLY [B5-123] REF B-717 AMM 33-51. OPERATIONAL TEST WAS GOOD. OK FOR SERVICE. (LP #1499012)Feb 21, 2020 · N980AT · Boeing 717200 · Emergency LightingSDR DALA2019042292552Hinge Fitting · corrodedTHE I/B LUG FACE OF RH FLAP O/B IDLER HINGE IS CORRODED. MAINTENANCE REMOVED ALL OF THE CORROSION AND FABRICATED AN OVERSIZED BUSHING AND WASHER TO FILL THE VOID CAUSED BY THE REMOVED CORROSION. COMPLIED WITH FINAL ER/A 577251-14 REV. 0. (LP #1037065)Apr 19, 2019 · N980AT · Boeing 717200 · Trailing Edge FlapsSDR DALA2019041702479Frame · crackedCRACK NOTED AT UPPER RADIUS OF THE FRAME TAB OF THE OVER WING FRAME STA 696 RH, CONDITION 3 GREATER THAN 0.125 INCH. NRC 057-0004:5310-01436-01D/001 00056: REPLACED FRAME ON AMDS 5310-01436-03B.Apr 16, 2019 · N980AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2019041542423Tape · tornRIGHT WING UPPER SURFACE TAPE WORN. SURFACE IS ALSO CORRODED JUST FORWARD OF O/B SPOILER O/B END. NRC 001-0282:5720-2003/001 00081: REPAIRED COMPLIED WITH PER ER/A 576976-14 REV 0. (LP #1027898)Apr 12, 2019 · N980AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2019041102394Cam · out of positionTHE VERY AFT END OF 48 SECTION: TAILCONE RELEASE LANYARD CAM ASSEMBLY IS CLOCKED INCORRECTLY. NRC 001-0251:5300-2004/002 00198: ADJUSTED CAM REF B717 AMM 53-52-03.Apr 10, 2019 · N980AT · Boeing 717200 · Aerodynamic FairingsSDR DALA2019030501512Lanyard · brokenTHE GIRT BAR CABLE ON DOOR 1R WAS FOUND TO BE BROKEN. MAINTENANCE REPLACED THE LANYARD ASSEMBLY, IPC REF 25-61-03-01 ITEM 085. INSTALLED PER AMM 25-61-03. RII ACCOMPLISHED. OK FOR SERVICE. (LP #5070232)Mar 1, 2019 · N980AT · Boeing 717200 · Emergency EquipmentSDR DALA2019012600562Battery · dischargedTHE OVERWING EXIT EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE FORWARD EMERGENCY BATTERY AND REPLACED THE AFT EMERGENCY POWER SUPPLY PER AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #4289937)Jan 25, 2019 · N980AT · Boeing 717200 · Emergency LightingSDR DALA2018061203969Connector · looseTHE AFT BULKHEAD EMERGENCY LIGHT EXIT SIGN WOULD NOT ILLUMINATE DURING TEST. FOUND A LOOSE CONNECTION ON LIGHT L2-938, AND POWER SUPPLY AND BATTERY PACK B5-260 FUSES BAD, TIGHTENED CONNECTION AT LIGHT L2-938 AND REPLACED EMERGENCY POWER SUPPLY AND BATTERY PACJun 11, 2018 · N980AT · Boeing 717200 · Light System WiringSDR DALA2018051503328Light · shortedTHE EMERGENCY LIGHTS INTERMITTENTLY CAME ON & OFF DURING FLIGHT. WATER WAS FOUND IN THE EXIT SIGN AT THE TAILCONE. REPLACED IAW WDM 33-51. THE EMERGENCY LIGHTS NOW OPERATE NORMALLY. ALSO REMOVED CONDENSATION ABOVE AFT DROP CEILING PANEL.May 14, 2018 · N980AT · Boeing 717200 · Emergency Lighting
Back to N980AT