GE CF34-8C5B1

Service difficulty reports · 418

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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 engine_model_key = 'CF348C5B1'
  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 QXEA2010110500712Floorbeam · corrodedC3 CHECK - AVIONICS BAY FLOOR SUPPORT ANGLE ATTACHED TO FS 280 IS CORRODED. REMOVED SUPPORT ANGLE IAW SRM 51-42-06-001-001-A01. LOCATED FASTENER HOLES IN NEW ANGLE IAW SRM 51-40-11-001-001-A01. INSTALLED NEW ANGLE IAW SRM 51-42-06-001-001-A01. TOPCOATED INov 5, 2010 · N619QX · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR QXEA2010110800716Sill · corrodedC3 CHECK - SERVICE DOOR SURROUND STRUCTURE LOWER SILL HAS SEVERAL SPOTS OF CORROSION. BLENDED AREAS TO REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. PERFORMED ECI ON SERVICE DOOR LOWER SILL BLENDED AREA. NO CRACKS OR CORROSION FOUND AT THIS TIME IAW NDTM Nov 5, 2010 · N619QX · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR QXEA2010110800717Intercostal · corrodedC3 CHECK - AVIONICS BAY DOOR STRUCTURE LT INTERCOSTAL HAS CORROSION. REMOVED INTERCOSTAL IAW SRM 51-42-06-001-001-A01. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. FOUND REMAINING MATERIAL TO BE OUT OF LIMITS IAW SRM 53-21-23-101-003-A01. PERFORMED ECI Nov 5, 2010 · N619QX · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR QXEA2010110500707Floorbeam · crackedC3 CHECK - 280 BEAM IS CRACKED ON LT AND RT SIDE. PERFORMED CUTLINE ON NEW BEAM IAW REO 670-53-11-047. REMOVED LT AND RT 280 DRIP PANS AND INTERCOSTALS IAW SRM 51-42-21-001-001-A01. FOUND COCKPIT FLOOR ANGLE OF FS 280 CRACKED. PERFORMED LPI ON CUTLINE NO Nov 4, 2010 · N619QX · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR QXEA2010110500708Web · crackedRFD - C3 CHECK - DURING INSP FOUND A CRACK OTBD OF ADG STOW PUMP ON WEB FLOOR AT FS 192.00 LOCATED IN FWD EQUIPMENT BAY. REMOVED ADG RESTOW PUMP ASSY IAW AMM 24-23-19-000-801-A01. PERFORMED CUT OUT IAW REO 670-53-11-509 ON RT SIDE. PERFORMED LPI ON CUT LINE,Nov 4, 2010 · N619QX · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR N6WA20101101Light · inoperativeOVERHEAD EMERGENCY LIGHT INOP. R & R OVERHEAD EMERGENCY LIGHT IAW AMM 33-51-11 OPS CHECK GOOD. NO FURTHER DEFECTS.Nov 4, 2010 · N163GJ · Cndair CL6002C10 · Emergency LightingSDR QXEA2010110500713Intercostal · corrodedC3 CHECK - AVIONICS BAY DOOR STRUCTURE RT INTERCOASTAL HAS CORROSION. REMOVED FASTENERS FOM IAW SRM 51-42-06-001-001-A01. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. REMOVED .002" MATERIAL, REMAINING MATERIAL IS .078". NO DAMAGE ALLOWED AREA. PERFORMEDNov 4, 2010 · N619QX · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR QXEA2010110500714Bulkhead · corrodedC3 CHECK - RT FS 280 LOWER BULKHEAD WEB IS CORRODED. REMOVED CORRODED RT FS 280 LOWER BULKHEAD WEB IAW SRM 51-42-06-001-001-A01. LOCATED FASTENERS HOLES IN NEW WEB IAW SRM 51-40-11-001-001-A01 AND 53-11-10-201-003-A01. INSTALLED NEW WEB IAW SRM 53-11-10-201-Nov 4, 2010 · N619QX · Cndair CL6002C10 · Fuselage Main, BulkheadSDR QXEA2010110500715Bulkhead · corrodedC3 CHECK - LT FS 280 LOWER BULKHEAD WEB IS CORRODED. REMOVED CORRODED LT FS 280 LOWER BULKHEAD WEB IAW SRM 51-42-06-001-001-A01. LOCATED FASTENERS HOLES IN NEW WEB IAW SRM 51-40-11-001-001-A01 AND 53-11-10-201-003-A01. INSTALLED NEW WEB IAW SRM 53-11-10-201Nov 4, 2010 · N619QX · Cndair CL6002C10 · Fuselage Main, BulkheadSDR QXEA2010110500703Structure · crackedC3 CHECK - CRACK FOUND ON PAX DOOR UNDER TOP STEP ASSY. REMOVED DAMAGED AREA IAW SRM 51-11-04-201-001-A01. PERFORMED LPI ON CUT LINE, NO CRACKS FOUND AT THIS TIME IAW NDTM LPI 51-20-008-230-A01 AND REO 670-52-11-154. FABRICATED ANGLE AND FILLER, DRILLED TRINov 3, 2010 · N619QX · Cndair CL6002C10 · Passenger/Crew DoorsSDR QXEA2010110500704Angle · damagedC3 CHECK - DURING INSP FOUND DAMAGE TO PAX DOOR STRIKER ANGLE AT FS 310 NEXT TO FWD UPPER LATCH FITTING. PERFORMED CUT OUT IAW REO 670-53-22-001. PERFORMED LPI ON CUT LINE NO CRACKS FOUND AT THIS TIME IAW NDTM LPI 51-20-008-230-A01 AND REO 670-53-22-001. FANov 3, 2010 · N619QX · Cndair CL6002C10 · Passenger/Crew DoorsSDR QXEA2010110500705Frame · corrodedC3 CHECK - FRAME 310 HAS CORROSION BETWEEN STR 25R AND 26L. REMOVED 19 RIVETS TO ACCESS CORROSION IAW SRM 51-42-06-001-001-A01. BLENDED OUT CORROSION, REMOVED .003" OF MATERIAL, REMAINING MATERIAL IS .047" WITHIN LIMITS IAW SRM 53-21-06-001-002-A01. TREATEDNov 3, 2010 · N619QX · Cndair CL6002C10 · Fuselage Main, FrameSDR QXEA2010110500706Attach Angle · corrodedC3 CHECK - AVIONICS BAY DOOR FWD STRUCTURE ATTACHMENT ANGLE AT STR 26L IS CORRODED. BLENDED OUT CORROSION IAW SRM 51-21-06-001-001-A01, REMOVED .003" OF MATERIAL, REMAINING MATERIAL IS .060" WITHIN LIMITS IAW SRM 53-21-23-001-003-A01. TREATED, PRIMED AND PANov 3, 2010 · N619QX · Cndair CL6002C10 · Fuselage Main, Attach FittingsSDR QXEA2010110300699Skin · gougedC3 CHECK - AVIONICS BAY DOOR SURROUND HAS SEVERAL GOUGES AND ONE SMALL AREA OF PITTING. REMOVED DAMAGE IAW SRM 51-21-06-001-001-A01. REMOVED .002" FROM ORIGINAL .125" MATERIAL. MATERIAL REMAINING IS .123" WITHIN LIMITS IAW REO 670-53-21-242. PERFORMED LPI Nov 2, 2010 · N619QX · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR QXEA2010110200697Sill · gougedC3 CHECK - AFT BAGGAGE DOOR SILL IS GOUGED AND CORRODED. BLENDED OUT GOUGES AND SCRATCHES IAW SRM 51-12-00-001-001-A01. PERFORMED ECI ON AFT BAGGAGE DOOR SILL BLEND AREA. NO CRACKS OR CORROSION FOUND AT THIS TIME IAW ECI 51-20-006-250-A01. DEEPEST AREA BLENNov 1, 2010 · N619QX · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR QXEA2010110300700Structure · chafedC3 CHECK - INBD LT EDGE CHAFED UNDER CANOE. BLENDED CHAFED AREA ON LT INBD FLAP IAW SRM 51-12-00-001-001-A01. CHAFED AREA MEASURED INBD PORTION 27" X .0625" MAX X .004" MAX, OTBD PORTION 15" X .0625 MAX X .003" MAX. ORIGINAL MATERIAL IS .063, REMAINING MATENov 1, 2010 · N619QX · Cndair CL6002C10 · Trailing Edge FlapsSDR QXEA2010110100678Seat Track · corrodedC3 CHECK - LT SIDE SEAT TRACK FS 667-708 HAS SURFACE CORROSION. BLENDED LT SIDE SEAT TRACK FS 667-708, REMAINING MATERIAL IS .078 AND FOUND TO BE OUT OF LIMITS. RECEIVED BULK MATERIAL AND LOCATED AND DRILLED IAW SRM 51-40-11-001-001-A01. CUT TRACK IAW SRM 5Oct 30, 2010 · N619QX · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR QXEA2010110100677Seat Track · corrodedC3 CHECK - LT SIDE SEAT TRACK FS485-573 HAS SURFACE CORROSION. BLENDED LT SIDE SEAT TRACK FS 485-573, ALL POINTS BLENDED WERE FOUND TO BE WITHIN LIMITS IAW REO670-53-00-013. TREATED AFFECTED AREAS IAW SRM 51-21-11-001-001-A01.Oct 29, 2010 · N619QX · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR QXEA2010110100679Seat Track · corrodedC3 CHECK - LT SIDE SEAT TRACK FS 708-761 HAS SURFACE CORROSION. BLENDED LT SIDE SEAT TRACK FS 708-761, REMAINING MATERIAL IS .097 AND FOUND TO BE WITHIN LIMITS. TREATED BLENDED AREAS IAW IAW SRM 51-21-11-001-001-A01.Oct 29, 2010 · N619QX · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR QXEA2010110100680Seat Track · corrodedC3 CHECK - LT SIDE SEAT TRACK FS 785-863 HAS SURFACE CORROSION. BLENDED LT SIDE SEAT TRACK FS 785-863, MAX ALLOWABLE BLEND IS .035, MAX BLENDED MATERIAL .024, REMAINING MATERIAL IS .081, FOUND ALL BLENDS WITHIN LIMITS IAW REO 670-55-00-013. TREATED AFFECTEDOct 29, 2010 · N619QX · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR QXEA2010110100681Seat Track · corrodedC3 CHECK - RT SIDE SEAT TRACK FS 485-573 HAS SURFACE CORROSION. BLENDED RT SIDE SEAT TRACK FS 485-573, MAX ALLOWABLE BLEND IS .035, MAX BLENDED MATERIAL .013, REMAINING MATERIAL IS .092 AND FOUND ALL BLENDS WITHIN LIMITS IAW REO 670-55-00-013. TREATED AFFECOct 29, 2010 · N619QX · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR QXEA2010110100683Seat Track · corrodedC3 CHECK - RT SIDE SEAT TRACK FS 677-708 HAS SURFACE CORROSION. BLENDED RT SIDE SEAT TRACK FS 677-708, MAX ALLOWABLE BLEND IS .035, MAX BLENDED MATERIAL .011, REMAINING MATERIAL IS .094, FOUND ALL BLENDS WITHIN LIMITS IAW REO 670-55-00-013. TREATED AFFECTEDOct 29, 2010 · N619QX · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR QXEA2010110100684Seat Track · corrodedC3 CHECK - RT SIDE SEAT TRACK FS 708-761 HAS SURFACE CORROSION. BLENDED RT SIDE SEAT TRACK FS 708-761, MAX ALLOWABLE BLEND IS .035, MAX BLENDED MATERIAL .018, REMAINING MATERIAL IS .087, FOUND ALL BLENDS TO BE WITHIN LIMITS IAW REO 670-55-00-013. TREATED AFOct 29, 2010 · N619QX · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR QXEA2010110100685Seat Track · corrodedC3 CHECK - RT SIDE SEAT TRACK FS 785-863 HAS SURFACE CORROSION. BLENDED RT SIDE SEAT TRACK FS 785-863, MAX ALLOWABLE BLEND IS .035, MAX BLENDED MATERIAL .011, REMAINING MATERIAL IS .094, FOUND ALL BLENDS TO BE WITHIN LIMITS IAW REO 670-55-00-013. TREATED AFOct 29, 2010 · N619QX · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR QXEA2010110100688Seat Track · corrodedC3 CHECK - LT SIDE SEAT TRACK FS 573-677 HAS SURFACE CORROSION. BLENDED LT SIDE SEAT TRACKS FS 573-677, MAX ALLOWABLE BLEND IS .035" BLENDED .023" MATERIAL REMAINING IS .082, FOUND ALL BLENDS TO BE WITHIN LIMITS IAW REO 670-53-00-013. TREATED ALL AFFECTED AOct 29, 2010 · N619QX · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR QXEA2010110100689Seat Track · corrodedC3 CHECK - LT SIDE SEAT TRACK FS 379-485 HAS SURFACE CORROSION. BLENDED LT SIDE SEAT TRACKS FS 379-485, MAX ALLOWABLE BLEND IS .035" BLENDED .023" MATERIAL REMAINING IS .082, FOUND ALL BLENDS TO BE WITHIN LIMITS IAW REO 670-53-00-013. TREATED ALL AFFECTED AOct 29, 2010 · N619QX · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR QXEA2010110100690Seat Track · corrodedC3 CHECK - RT SIDE SEAT TRACK FS 863-985 HAS SURFACE CORROSION. BLENDED LT SIDE SEAT TRACKS FS 863-985, MAX ALLOWABLE BLEND IS .035" BLENDED .005" MATERIAL REMAINING IS .100, FOUND ALL BLENDS TO BE WITHIN LIMITS IAW REO 670-53-00-013. TREATED ALL AFFECTED AOct 29, 2010 · N619QX · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR QXEA2010110100691Seat Track · corrodedC3 CHECK - RT SIDE SEAT TRACK FS 374-485 HAS SURFACE CORROSION. BLENDED RT SIDE SEAT TRACK FS 374-485, FOUND ALL BLENDS TO BE WITHIN LIMITS IAW REO 670-53-00-013. TREATED ALL AFFECTED AREAS IAW SRM 51-21-11-001-001-A01.Oct 29, 2010 · N619QX · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR QXEA2010110100682Seat Track · corrodedC3 CHECK - RT SIDE SEAT TRACK FS 573-677 HAS SURFACE CORROSION. BLENDED LT SIDE SEAT TRACK FS 573-677, MAX ALLOWABLE BLEND IS .035, MAX BLENDED MATERIAL .028, REMAINING MATERIAL IS .087 AND FOUND ALL BLENDS WITHIN LIMITS IAW REO 670-55-00-013. TREATED AFFECOct 28, 2010 · N619QX · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR QXEA2010110100687Seat Track · corrodedC3 CHECK - LT SIDE SEAT TRACK FS 863-985 HAS SURFACE CORROSION. BLENDED LT SIDE SEAT TRACKS FS 863-985, MAX ALLOWABLE BLEND IS .035" BLENDED .010" MATERIAL REMAINING IS .095, FOUND ALL BLENDS TO BE WITHIN LIMITS IAW REO670-53-00-013. TREATED AFFECTED AREAS Oct 28, 2010 · N619QX · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR N6WA20101005Cover · missingSERVICE DOOR BOTTOM RT EMERGENCY LIGHT COVER MISSING. DEFFERED LIGHT COVER IAW MEL 33051-01C CAT C ON DMI 14609 IAW MX CONTROL.Oct 26, 2010 · N171GJ · Cndair CL6002C10 · Emergency LightingSDR N6WA20101003Cover · looseEMERGENCY EXIT HANDLE COVER LOOSE. RESECURED EMERGENCY EXIT HANDLE COVER REF AMM 52-21-00. NOTED ON FUTHER DEFECTED AT THIS TIME.Oct 24, 2010 · N161GJ · Cndair CL6002C10 · Emergency ExitsSDR N6WA20101004Cover · unsecureEMERGENCY EXIT HANDLE COVER AT 12 A/B WIL NOT STAY ON. RESECURED EMEGENCY HANDLE COVER AT SEAT 12 A/B IN REF WITH AMM 25-26-09.Oct 24, 2010 · N161GJ · Cndair CL6002C10 · Emergency ExitsSDR N6WA20101002Slat System · warning messageSLAT FAIL CAUTION MSG. MANUALLY LOWERED SLATS AND FLAPS TO THE 8 DEGREE POSITION IAW AMM 27-81-00. INSPECTED SLATS AND FLAPS AND FOUND ACFT SAFE FOR 1 TIME FERRY FLIGHT. VERIFIED FLAPS CONFIG MSF NOT PRESENT.Oct 18, 2010 · N166GJ · Cndair CL6002C10 · Leading Edge Slat Control SystemSDR N6WA20100904Bulb · inoperativeEMERGENCY LIGHT OUT AT ROW NR7 (OVERHEAD CEILING LIGHT). R & R LIGHT BULB AND OPS CHECKED ROW 7 EMRGENCY LIGHT IAW AMM 33-51-00.Sep 28, 2010 · N157GJ · Cndair CL6002C10 · Emergency LightingSDR N6WA20100902Lens · missingRED LENS COVER MISSING ON ROW 12 EXIT SIGN. DEFFERRED LENS COVER ROW 12 IAW MEL 23-40-01J, CAT B, DMI 17184, MX.Sep 14, 2010 · N171GJ · Cndair CL6002C10 · Emergency LightingSDR N6WA20100901Bulb · inoperativeCEILING LEVEL EMERGENCY FLOOD LIGHT OUT 2ND LIGHT FROM AFT. R & R BULB IN EMERGENCY FLOOD LIGHT IAW AMM 33-24-01. OPS CHECK GOOD.Sep 5, 2010 · N165GJ · Cndair CL6002C10 · Emergency LightingSDR CA110920005Engine · flamed out(CAN) RIGHT ENGINE ITT EXCEEDED, FOLLOWED BY RT ENGINE FLAME OUT, CREW RAN QRH. THE ACFT LANDED SINGLE ENGINE UNEVENTFULLY.Sep 3, 2010 · Cndair CL6002C10 · Engine (Turbine/Turboprop)SDR VNAA2010090900001Duct · crackedAT 16,000 FEET AFTER DEPARTURE FROM GPT, CREW REPORTED LEFT ENGINE OIL PRESSURE DROPPED TO ZERO AND THEN DISPLAYED DASHES. FUEL FEED TEMPERATURE ALSO DISPLAYED DASHES. CREW RETURNED TO GPT AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT AND FOUND THE LSep 1, 2010 · N702PS · Cndair CL6002C10 · Engine Cooling SystemSDR N6WA20100805Bonding Strap · unsecureLT BLEED DUCT WARNING MESSAGE RESECURED BONDING STRAP ON HEAT EXCHANGER TO FUSELAGE IAW AMM 20-21-00 AND OPS CKD SYS GOOD IAW PNEUMATIC WARNING SYS IAW AMM 36-11-00.Aug 18, 2010 · N160GJ · Cndair CL6002C10 · Pneumatic System WiringSDR N6WA20100804Lamp · inoperativeSECOND FROM MOST AFT CEILING EMERGENCY LIGHT INOP. RE-LAMPED SAID EMERGENCY LIGHT ASSY OPS CHECKED GOOD REF TO AMM 33-51-00.Aug 17, 2010 · N163GJ · Cndair CL6002C10 · Emergency LightingSDR N6WA20100803Lens · missingSMALL RED LIGHT COVER ON BACK OF OVERWING EXIT SIGN IS MISSING. REPLACED MISSING LENS COVER IAW AMM 33-24-00.Aug 9, 2010 · N157GJ · Cndair CL6002C10 · Emergency LightingSDR N6WA20100801Light · no testEMERGENCY LIGHTS WILL NOT TEST. COMPLIED WITH OPS TEST OF EMERGENCY LIGHT IAW AMM 33-51-00. NO DEFECTS NOTED.Aug 5, 2010 · N153GJ · Cndair CL6002C10 · Emergency LightingSDR N6WA20100720Computer · malfunctionedFUEL CH 1/2 FAIL CAUTION MESSAGE IN FLIGHT. R & R FUEL QUANTITY GAUGING COMPUTER IAW AMM 28-41-22, OPS CHECK GOOD AT THIS TIME.Jul 29, 2010 · N158GJ · Cndair CL6002C10 · Fuel Indicating SystemSDR N6WA20100718Light · intermittentEMERGENCY DOOR CAUTION LIGHT CAME ON THEN WENT BACK OUT. INSPECTED AND RESET LT EMERGENCY EXIT DOOR, OPS CHECK GOOD IAW AMM 52-21-00.Jul 27, 2010 · N151GJ · Cndair CL6002C10 · Emergency LightingSDR N6WA20100717Flap System · malfunctionedFLAP FAIL ENROUTE, PERFORMED QRH PROCEDURE, LANDED FLAPS 1 PHL. PERFORMED OPS CHECK OF FLAPS AND SLATS IAW AMM 27-51-05. SELECTED FLAPS 8. ACFT SAFE FOR (1) TIME FERRY.Jul 26, 2010 · N156GJ · Cndair CL6002C10 · Trailing Edge Flap Control SystemSDR N6WA20100715Flap System · warning lightFLAPS FAIL CAUTION MSG IN FLIGHT. CLEARED INHIBITS OF SFECU 1 AND 2 PERFORMED FIM TASK 27-52-00. FLAP FAIL MESSAGE IS NOT NOTED AT THIS TIME.Jul 25, 2010 · N156GJ · Cndair CL6002C10 · Trailing Edge Flap Control SystemSDR N6WA20100606Circuit Breaker · trippedRT OVERWING EMERGENCY LIGHT, INTERIOR LOWER INOP. RESET CIRCUIT BREAKERS TO EMERGENCY LIGHT SYS TEST GOOD AT THIS TIME IAW AMM 33-51-00.Jun 21, 2010 · N166GJ · Cndair CL6002C10 · Light System WiringSDR N6WA20100605Light · inoperativeEMERGENCY EXIT LIGHTS AT 12D BY WINDOW AND ROW 13 AND 16 IN ISLE CEILING INOP. POWERED DOWN A/C REBOOTED E EXIT LIGHT SYS OPS CHECK NORMAL AT THIS TIME. ALL WORK DONE IAW AMM CHAP 33-51-00.Jun 7, 2010 · N166GJ · Cndair CL6002C10 · Emergency LightingSDR N6WA20100601ALight · malfunctionedEMERGENCY LIGHTS ON IN ARMED POSITION. PERFORMED OPS CHECK ON EMERGENCY LIGHT SYS PER AMM 33-51-00. OPS CHECK GOOD AT THIS TIME.Jun 1, 2010 · N158GJ · Cndair CL6002C10 · Emergency Lighting
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