N759EV

Service difficulty reports · 201

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 = 'N759EV' 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 SWI2025F01573Slat Track · wornLH WING SLAT TRACK 2-1 HAS WEAR MARKS IN MULTIPLE SPOTS. (MARKED) (C-CHECK RO 11/22/2025)COMPLIED WITH REO 670-57-42-2209 REV-- DATED 2025-09-15. OPS TEST GOOD AT THIS TIME PER CRJ700 AMM 27-50-00-710-801-A02. COMPLIED WITH SKYWEST TASK CARD 27-900-1009-SKY Aug 25, 2025 · N759EV · Cndair CL6002C10 · Leading Edge DevicesSDR SWI2025F01572Slat Track · wornLH WING SLAT TRACK 3-2 HAS WEAR MARKS AND PITTING. (MARKED) (C-CHECK RO 11/22/2025)COMPLIED WITH REO 670-57-42-2205 REV -- DATED 2025-09-15. OPS TEST GOOD AT THIS TIME PER CRJ700 AMM 27-50-00-710-801-A02. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY.Aug 25, 2025 · N759EV · Cndair CL6002C10 · Leading Edge DevicesSDR SWI2025F01571Slat Track · wornRH WING SLAT TRACK 2-3 HAS WEAR MARKS IN MULTIPLE SPOTS. (MARKED) (C-CHECK RO 11/22/2025)COMPLIED WITH REO 670-57-42-2201 REV -- DATED 2025-09-12PERFORMED OPERATIONAL TEST OF THE FLAPS AND SLAT SYSTEM CRJ700 AMM 27-50-00-710-801-A02 TEST OK AT THIS MOMENTCOAug 25, 2025 · N759EV · Cndair CL6002C10 · Leading Edge DevicesSDR SWI2025F01570Slat Track · wornRH WING SLAT TRACK 1-3 HAS WEAR MARKS IN MULTIPLE SPOTS. (MARKED) (C-CHECK RO 11/22/2025)COMPLIED WITH REO 670-57-42-2195 REV-- DATED 2025-09-12PERFORMED OPERATIONAL TEST OF THE FLAPS AND SLAT SYSTEM CRJ700 AMM 27-50-00-710-801-A02 TEST OK AT THIS MOMENTCOMPAug 25, 2025 · N759EV · Cndair CL6002C10 · Leading Edge DevicesSDR SWIA202511240825Slat Track · wornLH WING SLAT TRACK 1-3 HAS WEAR MARKS IN MULTIPLE SPOTS. (MARKED) (C-CHECK RO 11/22/2025)COMPLIED WITH REO 670-57-42-2198 REV-- DATED 2025-09-12. OPS TEST GOOD AT THIS TIME PER CRJ700 AMM 27-50-00-710-801-A02. COMPLIED WITH SKYWEST TASK CARD 27-900-1009-SKYAug 25, 2025 · N759EV · Cndair CL6002C10 · Leading Edge DevicesSDR SWI2025F01580Stringer · corroded3 FASTENERS CORRODED AT FS1015.00 AT APPROXIMATELY STGR17L AS MARKED (C-CHECK RO 11/22/2025)REMOVED AND WET INSTALLED 3EA NEW NAS1670-08L4 - BOLT BLIND FLUSH HD IN REWORKED AREAS. REF CRJ-700 SRM 51-42-22-001-001-A01, REV-38 DATED JUL 25-2020, DWG NO: MM670Aug 24, 2025 · N759EV · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA202511240824Door Frame · chafedPAX DOOR SURROUND AFT CAM FITTING AT FS349.00 IS CHAFED. (MARKED) (C-CHECK RO 11/22/2025) REMOVED AND INSTALLED NEW PAX DOOR SURROUND AFT CAM FITTING REF CRJ 700 SRM 51-42-21-001-001-A01 AND DWG. NO. SH670-31810 REV.AE COMPLIED WITH SKYWEST TASK CARD 51-900Aug 24, 2025 · N759EV · Cndair CL6002C10 · Fuselage Main, StructureSDR SWI2025F01583Door Frame · gougedMAIN AVIONICS DOOR FWD FRAME HAS MULTIPLE GOUGES. CAMP # 30715427. (C-CHECK RO 11/22/2025)BLENDED GOUGES AT MAIN AVIONICS DOOR FWD FRAME. INSTALLED NEW RH FWD ANGLE CC670-38665-1. INSTALLED NEW LH FWD ANGLE CC670-38664-1. INSTALLED STOP FITTING 601R38352-1 &Aug 23, 2025 · N759EV · Cndair CL6002C10 · Fuselage Main, StructureSDR SWI2025F01582Door Frame · misinstalledMAIN AVIONICS DOOR FWD FRAME HAS MULTIPLE RIVETS NOT INSTALLED CORRECTLY. CAMP # 30715426. (C-CHECK RO 11/22/2025)REMOVED AND REPLACED IMPROPERLY INSTALLED RIVETS. REF: CRJ-700-SRM 51-42-06-001-001-A01 AND DWG CC670-38651 REV E. LEAK AND OPERATIONAL CHECK GOAug 23, 2025 · N759EV · Cndair CL6002C10 · Fuselage Main, StructureSDR SWI2025F01581Door Sill · corrodedSERVICE DOOR LOWER SILL CORRODED AT APPROXIMATELY FS320.00 ON THE INBOARD SIDE OF SILL MARKED IN RED (C-CHECK RO 11/22/2025)REMOVED AND INSTALLED NEW ANGLE MOUNTING, FLOOR PROTECTOR P/N:SH670-31996-3. PER DWG.SH670-31950 REV. Y, REF.CRJ/700 SRM.51-42-06-001-Aug 23, 2025 · N759EV · Cndair CL6002C10 · Fuselage Main, StructureSDR SWIA202511240823Bracket · corrodedFWD BAGGAGE BAY BRACKET BETWEEN FS517 TO FS533 AND STRG 23LAND STRG22L HAS CORROSION (MARKED) (C-CHECK RO 11/22/2025)FWD BAGGAGE BAY BRACKET BETWEEN FS517 TO FS533 AND STRG 23LAND STRG22L FOUND TO BE OUT OF LIMITS PER REF.CRJ/700 SRM.53-32-58-101-001-A01. REAug 23, 2025 · N759EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWI2025F01585Plate · corrodedRBL9 TOP PLATE CORRODED IN MULTIPLE AREAS AS MARKED BETWEEN FS693.00 - FS847.00 (C-CHECK RO 11/22/2025)REMOVED CORROSION ON RBL9 TOP PLATE BETWEEN FS693.00 - FS847.00 FS693.00 REF. CRJ700 SRM 51-21-06-001-001-A01, PART FOUND WITH 100% MATERIAL LOSS AND REQUAug 22, 2025 · N759EV · Cndair CL6002C10 · Fuselage Main, StructureSDR SWI2025F01584Slat Track · gougedLEFT WING LEADING EDGE SLAT TRACK 3-3 HAS GOUGE MARKS (FLAGGED) CAMP# 30713603 (C-CHECK RO 11/22/2025)COMPLIED WITH REO 670-57-42-2204 REV -- DATED 2025-09-12. OPS TEST GOOD AT THIS TIME PER CRJ700 AMM 27-50-00-710-801-A02. COMPLIED WITH SKYWEST TASK CARD 27Aug 22, 2025 · N759EV · Cndair CL6002C10 · Leading Edge DevicesSDR SWIA202511240822Slat Track · corrodedCORROSION FOUND ON RIGHT WING LEADING EDGE SLAT TRACK 1-2 (MARKED) CAMP# 30712069 (C-CHECK RO 11/22/2025)COMPLIED WITH REO 670-57-42-2196 REV-- DATED 2025-09-12 PERFORMED OPERATIONAL TEST OF THE FLAPS AND SLAT SYSTEM CRJ700 AMM 27-50-00-710-801-A02 TEST OK ATAug 22, 2025 · N759EV · Cndair CL6002C10 · Leading Edge DevicesSDR SWI2025F01592Door Frame · damagedMAIN AVIONICS COMPARTMENT DOOR EXTERNAL SURROUND STRUCTURE DOOR LANDING HAS FRETTING AROUND ENTIRE SURFACE (C-CHECK RO 11/22/2025)WET INSTALLED 4EA NEW SACRIFICIAL ALUMINUM STRIPS ON MAIN AVIONICS COMPARTMENT DOOR EXTERNAL SURROUND STRUCTURE DOOR LANDING. REAug 21, 2025 · N759EV · Cndair CL6002C10 · Fuselage Main, StructureSDR SWI2025F01591Floor Support · corrodedLH CABIN FLOOR SILL HAS CORROSION AS MARKED BETWEEN FS1000.00 - FS1051.30 (C-CHECK RO 11/22/2025)REMOVED CORROSION ON LH CABIN FLOOR SILL BETWEEN FS1000.00 - FS1051.30, FOUND TO BE OUT OF LIMITS REF CRJ700 SRM 51-21-06-001-001-A01. REMOVED AND INSTALLED NEW Aug 21, 2025 · N759EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWI2025F01590Crossbeam · corrodedCROSSBEAM HAS CORROSION BETWEEN RBL9 AND LBL9 AT FS549.00 (MARKED) (C-CHECK RO 11/22/2025)WET INSTALLED ALL FASTENERS THRU ENTIRE STACKUP INCLUDING CROSS-BEAM AND FLOOR BEAM. INSTALLED ALL REPAIR PARTS,-1 AND -2 REPAIR ANGLE, -3 AND -4 CLEAT, -5 FILLER, -6 -Aug 21, 2025 · N759EV · Cndair CL6002C10 · Fuselage Main, StructureSDR SWIA202511240821Floor Support · corrodedL/H FLOOR BEAM LBL9 HAS CORROSION APPROXIMATELY BETWEEN FS477.00 TO FS581.00 (MARKED) (C-CHECK RO 11/22/2025)REPAIRED L/H FLOOR BEAM LBL9 BETWEEN FS477.00 TO FS581.00 REF REO 670-53-31-1089 REV -- DATE 2025-09-08. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-Aug 21, 2025 · N759EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWI2025F01589Floorbeam · corrodedFWD SIDE OF FS 280.0 LBL 9 TO RBL 9 COCKPIT FLOOR PNL SUPPORT HAS CORROSION CAMP # 30706947 (C-CHECK RO 11/22/2025)INSTALLED NEW FLOOR SUPPORT AT FS 280.00 BETWEEN RBL9 AND LBL9 REF CRJ 700 SRM 51-42-06-001-001-A01 REVISION 38: JUL 25/2020, CRJ 700 SRM 51-42-Aug 21, 2025 · N759EV · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR SWI2025F01588Skin · corrodedFS1051.30 NEXT TO RIGHT SILL HAS CORROSION AS MARKED (C-CHECK RO 11/22/2025)COMPLIED WITH STEPS 1-13 OF REO 670-53-61-2569 REV -- DATE 2025-09-28 STEP 1) ENSURE CORROSION DAMAGE WAS BLENDED TO SMOOTH CONTOUR, STEP 2) INSPECT REWORKED AREA USING LPI OR EDDY CUAug 21, 2025 · N759EV · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR SWI2025F01587Doubler · crackedCRACK IN RADIUS OF DOUBLER UNDER ADG HYDRAULIC STOW PUMP. (C-CHECK RO 11/22/2025)REPAIRED CRACK IN RADIUS OF DOUBLER UNDER ADG HYDRAULIC STOW PUMP. REF REO 670-53-11-2186 REV -- DATED 2025-10-21 AND REO 670-53-11-509 REV -E DATED 2018-02-08. COMPLIED WITH SKAug 21, 2025 · N759EV · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR SWI2025F01586Floor Support · corrodedR/H FLOOR BEAM RBL9 HAS CORROSION APPROXIMATELY BETWEEN FS565.00 TO FS684.00 (MARKED) (C-CHECK RO 11/22/2025) REAPIRED R/H FLOOR BEAM RBL9 BETWEEN FS565.00 TO FS684.00 REF CRJ 700 SRM 53-00-41-201-001-A01 AND REO 670-53-31-1090 REV -- DATED 2025-09-18. COMPLAug 21, 2025 · N759EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA202511240808Drag Angle · crackedRH VERTICAL STAB-TO-FUSELAGE AFT DRAG ANGLE POSSIBLY CRACKED (MARKED) (C-CHECK RO 11/22/2025)REMOVED RH AFT DRAG ANGLE REF CRJ700 SRM 51-42-13-001-001-A01, CRJ700 SRM 51-42-21-001-001-A01,CRJ700 SRM 51-42-22-001-001-A01. INSTALLED NEW RH AFT DRAG ANGLE REF CAug 8, 2025 · N759EV · Cndair CL6002C10 · Fuselage, Stabilizer Attach FittingsSDR SWIA20251124808Drag Angle · crackedLH VERTICAL STAB-TO-FUSELAGE AFT DRAG ANGLE POSSIBLY CRACKED (MARKED) (C-CHECK RO 11/22/2025)INSTALLED -5 AFT ANGLE DOUBLER & -7 AFT ANGLE FILLER ON L/H AFT DRAG ANGLE REPAIR REF CRJ 700 SRM 55-31-00-201-001-A01. COMPLIED WITH SKY WEST TASK CARD 51-900-1002-Aug 8, 2025 · N759EV · Cndair CL6002C10 · Fuselage, Stabilizer Attach FittingsSDR SWI2025F01593Fan Cowl · damagedRT UPPER FAN COWL HAS A DAMAGED HOLE (C-CHECK RO 11/22/2025)EVALUATED. MEASURES OF DAMAGE: LENGTH: 0.570", WIDTH: 0.398", DEPTH #1: 0.032" , DEPTH#2: 0.029". NO ALLOWABLE DAMAGE REF CRJ700 SRM 54-14-00-101-001-A01. RECIEVED ENGINEERING INSTRUCTION AND PERFORMAug 7, 2025 · N759EV · Cndair CL6002C10 · Nacelle/Pylon StructureSDR SWIA202511240807Handle · damagedAFT CARGO DOOR HANDLE HOUSING HAS SEVERAL AREAS OF IMPACT DAMAGE FROM THE HANDLE (MARKED) (C-CHECK RO 11/22/2025)REMOVED AND INSTALLED NEW AFT CARGO DOOR HANDLE HOUSING REF CRJ700 SRM 51-42-21-001-001-A01 ,DWG#601R35027 REV-AY. LEAK AND OPERATIONAL TESTS GOAug 7, 2025 · N759EV · Cndair CL6002C10 · Cargo/Baggage DoorsSDR SWIA202157567Window · crackedLEFT SIDE WINDOW IS CRACKED IN 2 PLACES. (FLIGHT 3091 - FILED CLOSED) REMOVED AND REPLACED LH SIDE WINDOW IN REFERENCE WITH AMM 56-12-01. PERFORMED OPERATIONAL CHECK OF WINDOW HEAT IN REFERENCE WITH AMM 30-41-06 OPS CHECK GOOD AT THIS TIME. PERFORMED PREApr 12, 2021 · N759EV · Cndair CL6002C10 · Flight Compartment WindowsSDR SWIA2019062145998Mount · corrodedCORROSION ON TOP OF GALLEY MOUNT FS285.00 BL17R. (C-CHECK) RO: 06/20/2019 REPLACED FWD INBD GALLEY MOUNT FITTING IAW SRM.May 21, 2019 · N759EV · Cndair CL6002C10 · Fuselage Main, Attach FittingsSDR SWIA2019062146000Floor Support · corrodedPASSENGER CABIN LBL9 BETWEEN FS565.0 AND FS581.0 I/B FLOOR SUPPORT HAS CORROSION. (C-CHECK) RO: 06/20/2019 REMOVED AND REPLACED I/B FLOOR SUPPORT AT LBL9 BETWEEN FS565.00 AND FS597.00 IAW SRM.May 20, 2019 · N759EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA2019062145999Stringer · corrodedAVIONICS BAY STGR26R/H AT FS333.0 SPLICE HAS CORROSION. REMOVED & INSTALLED JOINT STRINGER SPLICE 26R LOCATED AT FS333.00 IAW SRM. ALL CHECKS GOOD.May 20, 2019 · N759EV · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA2019062145997Stringer · corrodedAVIONICS BAY STGR26 R/H BETWEEN FS333.0 AND FS341.0 HAS CORROSION. (C-CHECK) RO: 06/20/2019 REMOVED & INSTALLED STRINGER 26R BETWEEN FS333.00 TO FS364.00 IAW SRM.ALL CHECKS GOOD.May 20, 2019 · N759EV · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA2019062146001Housing · wornGALLEY SERVICE DOOR , EXTERNAL OUTER HANDLE ASSEMBLY HAS GROOVE WORN INTO DOOR HANDLE HOUSING. REPLACED GALLEY SERVICE DOOR EXTERNAL OUTER HANDLE ASSEMBLY IAW SRM. LEAK CHECK GOOD.May 14, 2019 · N759EV · Cndair CL6002C10 · Galley DoorsSDR SWIA2018092745098Adc · failedRECEIVED LH PROBE CAUTION MESSAGE, FOLLOW QRH AND DIVERTED TO SUITABLE AIRPORT. EMERGENCY DECLARED. (FLT#3075) FO: 09/27/2018 CLOSED REMOVED AND REPLACED THE #1 ADC IAW AMM. OPS CHECK GOOD AT THIS TIME.Sep 26, 2018 · N759EV · Cndair CL6002C10 · Airspeed/Mach IndicatorSDR ASOA2018422012Frame · corrodedDURING C-CHECK, THE BS 319.7 FRAME WAS FOUND CORRODED AT STRINGER 21L. MAINTENANCE REMOVED AND REPLACED THE FRAME IAW SRM 51-40-11-001-A01, 51-42-06-001-001-A01, AND 51-42-21-001-001-A01. THE AIRCRAFT IS GOOD FOR RETURN TO SERVICE.Apr 2, 2018 · N759EV · Cndair CL6002C10 · Fuselage Main, FrameSDR ASOA201803235091Doubler · gougedPREVIOUS REPAIR IS GOUGED AT TWO LOCATIONS, STRINGER 27 BETWEEN BS 969 AND 985. REPLACED THE DOUBLER IAW REO 670-53-00-537, REV AND EC/TC REO 670-53-00-537.Mar 23, 2018 · N759EV · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR ASOA201803215090Frame · corrodedBS 310 FRAME IS CORRODED BETWEEN STRINGERS 26L AND 26R. REPAIRED IAW EC/TC REO 670-53-21-799, REV A.Mar 21, 2018 · N759EV · Cndair CL6002C10 · Fuselage Main, FrameSDR ASOA201803215089Doubler · corrodedTCAS ANTENNA DOUBLER CORRODED BETWEEN BS 295 TO 310. REPLACED THE DOUBLER IAW IAW SRM 51-42-06-001-001-A01.Mar 21, 2018 · N759EV · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR ASOA201803215088Frame · corrodedBS 319 FRAME IS CORRODED BETWEEN STRINGER 25L AND 26R. REPLACED THE FRAME SECTION IAW REO 670-53-21-7992, REV A, AND ECTC REO 670-53-21-799 02.Mar 21, 2018 · N759EV · Cndair CL6002C10 · Fuselage Main, FrameSDR ASOA201803215087Butt Joint · corrodedFS 280 CIRCUMFENETIAL JOINT IS CORRODED BETWEEN STRINGER 26L AND 26R. BLENDED THE CORROSION IAW REO 670-53-21-1502, REV -, AND ECTC REO 670-53-21-1502.Mar 21, 2018 · N759EV · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR ASOA201803155096Frame · corrodedFS 295.00 FRAME IS CORRODED BETWEEN STRINGER 24R AND 25R. REPAIRED IAW REO 670-53-21-799 REV A DATED 2016-11-27 AND 670-53-21-1501.Mar 15, 2018 · N759EV · Cndair CL6002C10 · Fuselage Main, FrameSDR ASOA201803155095Structure · crackedRT TRU BAY FLOOR CRACKED BY ADG PUMP AT FS193. REPAIRED IAW REO 670-53-11-509 REV D, DATED 2016-06-29.Mar 15, 2018 · N759EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA201803155072Skin · dentedA DENT WITH A GOUGE WAS FOUND ON FUSELAGE SKIN BETWEEN BS 250 - 265, STRINGERS 18L - 19L. THE SKIN WAS REPAIRED IAW REO 670-53-11-1378, AND EC/TC REO 670-53-11-1378.Mar 15, 2018 · N759EV · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR ASOA201803135071Floor Panel · crackedLEFT TRU BAY FLOOR CRACKED, BS 193, WL 79.5. REPAIRED THE FLOOR PANEL IAW BOMBARDIER REO 670-53-11-509 REV D AND EXPRESSJET EC/TC 670-53-11-509 REV C.Mar 13, 2018 · N759EV · Cndair CL6002C10 · Fuselage Floor PanelSDR ASOA201803135070Skin · dentedLEFT INBD FLAP LOWER SKIN IS DENTED JUST OTBD OF THE INBD FLAP HINGE ARM. REPAIRED THE SKIN IAW SRM 57-52-01-201-001-A01, TYPE IV.Mar 13, 2018 · N759EV · Cndair CL6002C10 · Trailing Edge FlapsSDR ASOA201812305007Battery Pack · inoperativePILOT REPORTED THE EMERGENCY LIGHTS ILLUMINATED WHILE IN ARMED POSITION. MX REMOVED AND REPLACED THE NR 1 EMERGENCY LIGHT BATTERY, OPS CHECKED GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.Dec 30, 2017 · N759EV · Cndair CL6002C10 · Emergency LightingSDR ASOA2015113014135Bulb · burned out12 AB LOWER EXIT SIGN HAVE 1 BULB BURNED. R & R SEAT 12AB LOWER EXIT SIGN LIGHT BULB IAW AMM 33-51-05. OPS CHECK GOOD.Nov 30, 2015 · N759EV · Cndair CL6002C10 · Emergency LightingSDR ASOA2015113014136Bulb · burned out12 CD LOWER EXIT SIGN HAVE 1 LIGHT BULB BURNED. R & R SEAT 12 CD LOWER EXIT SIGN LIGHT BULB IAW AMM 33-51-05, OPS CHECK GOOD.Nov 30, 2015 · N759EV · Cndair CL6002C10 · Emergency LightingSDR ASOA2015100913878Seal · leakingMAIN CABIN DOOR DIFFICULT TO OPEN AND AIR LEAKING & SQUEALING FROM TOP OF DOOR DURING FLIGHT. R & R PAX DOOR SEAL IAW AMM 52-11-07. OPS AND LEAK CHECKS GOOD, NO FURTHER DEFECTS NOTED AT THIS TIME.Oct 9, 2015 · N759EV · Cndair CL6002C10 · Passenger/Crew DoorsSDR ASOA2015082413587Bulb · burned outMAIN ENTRANCE LOWER EXIT SIGN BELOW FLASHLIGHT HAD TWO LIGHT BULBS BURNED OUT. REPLACED THE BULBS IAW AMM 33-51-05 AND 33-51-00. OPS CHECKED GOOD.Aug 24, 2015 · N759EV · Cndair CL6002C10 · Emergency LightingSDR ASOA2015082413586Bulb · burned outGALLEY FWD LOWER EXIT SIGN HAS ONE LIGHT BULB BURNED OUT. REPLACED THE LAMP IAW AMM 33-51-05 AND 33-51-00. OPS CHECKED GOOD.Aug 24, 2015 · N759EV · Cndair CL6002C10 · Emergency Lighting
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