N719EV

Service difficulty reports · 269

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 = 'N719EV' 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 ASOA201708081820Doubler · corrodedTCAS ANTENNA INTERNAL DOUBLER CORRODED BS 295 - 310, STRINGER 27. REMOVED AND REPLACED THE TCAS ANTENNA INTERNAL DOUBLER IAW SRM 51-42-06-001-A01, AND DRAWING SH670-32364Aug 8, 2017 · N719EV · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR ASOA201708071818Seat Track · corrodedLEFT SIDE WALL SEAT TRACK SEGMENT IS CORROSED AROUND 2 SCREW HOLES AT BS 613 AND 581. REMOVED CORRODED SEAT TRACK SEGMENT IAW AMM 53-00-49-000-801-A17. FABRICATED A NEW SEAT TRACK IAW ECTC REO 670-53-00-343 AND REO 670-53-00-343. INSTALLED THE NEW SEAT TRAug 7, 2017 · N719EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201708061819Seat Track · corrodedRIGHT SIDE WALL SEAT TRACK SEGMENT IS CORRODED OUT OF LIMITS. REMOVED CORRODED RIGHT SIDE WALL SEAT TRACK SEGMENT FROM BS 785.15 TO 866 IAW AMM 53-00-49-000-801-A03. FABRICATED A NEW SEAT TRACK IAW ECTC REO 670-53-00-343 AND REO 670-53-00-343. INSTALLED THAug 6, 2017 · N719EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201708171856Buttstrap · corrodedBS 280 BUTTSTRAP CORRODED, STRINGERS 26 - 27R AND STRINGERS 14 - 23R. COMPLIED WITH ECTC EA 45-2017-099.Aug 3, 2017 · N719EV · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR ASOA201706231708Stiffener · crackedFS 202.75 FORWARD SIDE OF BULKHEAD LBL 30 STIFFENER HAS AN INDICATION .15" LONG AT UPPER EDGE OF FLANGE, FAILED NDT INSPECTION. COMPLIED WITH SRM 53-11-10-201-005-A01 FS 202.75 POST AT LBL 30.0 (UPPERSIDE) LT SIDE REPAIR STEPS 1 THROUGH 5.Jun 23, 2017 · N719EV · Cndair CL6002C10 · Fuselage Main, BulkheadSDR ASOA201706231707Stiffener · crackedFS 202.75 FORWARD SIDE OF BULKHEAD RBL 30 STIFFENER HAS AN INDICATION .25" LONG AT UPPER EDGE OF FLANGE, FAILED NDT INSPECTION. COMPLIED WITH SRM 53-11-10-201-005-A01 FS 202.75 POST AT RBL 30.0 (UPPERSIDE) RT SIDE REPAIR STEPS 1 THROUGH 5.Jun 23, 2017 · N719EV · Cndair CL6002C10 · Fuselage Main, BulkheadSDR ASOA201705261617Door · gougedLOUD AIR SOUND NEAR PASSENGER DOOR. REPAIRED THE DAMAGED AREA IAW REO 670-52-11-956 & EC/TC REO 670-53-22-001.May 26, 2017 · N719EV · Cndair CL6002C10 · Passenger/Crew DoorsSDR ASOA201705261605Hinge · gougedPASSENGER DOOR FUSELAGE HINGE FOUND GOUGED . BLENDED OUT DAMAGE IAW REO 670-53-21-582, AND EC/TC REO 670-53-21-582 01.May 26, 2017 · N719EV · Cndair CL6002C10 · Fuselage Structure (General)SDR ASOA2016080215159Skin · damagedFUSELAGE SKIN DAMAGE SURROUNDING THE LOW PRESSURE GROUND AIR CONNECTION. BLENDED OUT THE DAMAGE BETWEEN BS 1031 - 1051, STRINGERS 22 AND 27R IAW SRM 51-12-00. FOUND TO BE OUT OF LIMITS IAW SRM 53-61-01. REPAIRED IAW REO 670-53-61-1256 REV A AND IAW SRM 5Aug 2, 2016 · N719EV · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR ASOA2016021314455Battery Pack · dischargedTHE EMERGENCY LIGHT SWITCH ON THE F/A PANEL WAS IN THE ON POSTION ON ARRIVAL AT THE ACFT, THUS NO EMERGENCY LIGHTS. PERFORMED OPS TEST OF THE EMERGENCY LIGHT SYS AFTER ALLOWING APU TO RUN, OPS TEST GOOD. ACFT OK FOR SERVICE IAW AMM 33-51-00.Feb 13, 2016 · N719EV · Cndair CL6002C10 · Emergency LightingSDR ASOA2015122214237Megaphone · not reportedCABIN MEGAPHONE REQUIRES REPLACEMENT. R & R CABIN MEGAPHONE IAW AMM 25-61-14 AND REF 25-61-14, FIG 1, ITEM 5.Dec 22, 2015 · N719EV · Cndair CL6002C10 · Emergency EquipmentSDR ASOA2015120514233Floorbeam · corrodedCORROSION FOUND ON FLOORBEAM LBL 9.00 AT FS 1031. CORROSION ON FLOORBEAM AT LBL 9.00 AND FS 1031.00 TO BE ASSESSED. NO DAMAGE, CORROSION, ALLOWED ON FLOORBEAM AT LBL 9.00 AT FS 1031.00 IAW SRM 53-61-43-101-001-A01. RECEIVED EC/TC EO 700-53-0282 FOR REPAIR ODec 5, 2015 · N719EV · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR ASOA2015120214228Floorbeam · corrodedCORROSION FOUND ON FLOORBEAM LBL 27.00 AT FS 1031.00. CORROSION FOUND IN FLOORBEAM AT LBL 27.00 & FS 1031.00. CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-61-43-101-001-A01. RECEIVED EC/TC EO 700-53-0282 FOR REPAIR OF FLOORBEAM, LBL 27.00 AT FS 1031. REPADec 2, 2015 · N719EV · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR ASOA2015082213577Bulb · burned out12 AB LOWER EXIT SIGN HAS 1 LIGHT BULB BURNED OUT. REPLACED BULB IN LOWER EXIT SIGN IAW AMM 33-51-11. OPS CHECK GOOD.Aug 22, 2015 · N719EV · Cndair CL6002C10 · Emergency LightingSDR ASOA2015052212889Bulb · burned out12 AB LOWER EXIT SIGN HAD TWO BULBS BURNED OUT. R & R THE BULBS IAW AMM 33-51-05, OPS CHECKED GOOD. OK FOR SERVICE.May 20, 2015 · N719EV · Cndair CL6002C10 · Emergency LightingSDR ASOA2015031712414Door · lack of lubeLEFT OVERWING EMERGENCY EXIT DOOR FAILED FUNCTIONAL CHECK, REF 52-21-00-720-801. COMPLIED WITH LUBE OF LT EMERGENCY EXIT 12-20-52-640-802, A01, ADJUSTED EXIT MICROSWITCH BRACKET IAW 52-21-04-400-801. OPS CHECK GOOD IAW AMM 52-21-00-710-801 (A01) AND 52-21-00Mar 12, 2015 · N719EV · Cndair CL6002C10 · Emergency ExitsSDR ASOA2015031712413Door · lack of lubeRIGHT OVERWING EMERGENCY EXIT DOOR FAILED FUNCTIONAL CHECK, REF 52-21-00-720-801. LUBED RT OVERWING EMERGENCY EXIT DOOR FUNCTIONAL CK GOOD IAW AMM 12-20-52-640-802 (A01) AND 52-21-00-720-801 (A01).Mar 12, 2015 · N719EV · Cndair CL6002C10 · Emergency ExitsSDR ASOA2015031312395Seat Track · corrodedRIGHT SIDE, SIDE SEAT RAIL, AT FS 581.00 HAS CORROSION. CORROSION BEYOND ALLOWABLE LIMITS IAW SRM 53-31-49-001-001-A01 RAIL REPLACEMENT IS REQUIRED. R & R RT SIDE SEAT RAIL AT FS 581 IAW AMM 53-00-49-000-801, A03 AND 53-00-49-400-801, A03.Feb 27, 2015 · N719EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015031312394Seat Track · corrodedLEFT SIDE, SIDE SEAT RAIL, AT FS 549.00 HAS CORROSION. CORROSION BEYOND ALLOWABLE LIMITS IAW SRM 53-31-49-001-001-A01. REMOVED LT SIDE SEAT RAIL FS549 IAW AMM 53-00-49-000-801. INSTALLED NEW TRACK IAW AMM 53-00-49-400-801.Feb 24, 2015 · N719EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015031312393Seat Track · corrodedLT SIDE, SIDE SEAT RAIL, AT FS 761.85-FS 712.00 HAS CORROSION. CORROSION BEYOND ALLOWABLE LIMITS IAW SRM 53-41-49-001-001-A01, RAIL REPLACEMENT IS REQUIRED. REMOVED LT SIDE SEAT RAIL FS 712 TO FS 761.85 IAW AMM 53-00-49-00-801, LEFT SIDEWALL. INSTALLED IAW Feb 24, 2015 · N719EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015031312392Seat Track · corrodedRIGHT SIDE, SIDE SEAT RAIL, AT FS 581.00 HAS CORROSION. CORROSION BEYOND ALLOWABLE LIMITS IAW SRM 53-31-49-001-001-A01 RAIL REPLACEMENT IS REQUIRED. R & R RT SIDE SEAT RAIL AT FS 549 IAW AMM 53-00-49-000-801 A03 AND 53-00-49-400-801 A03.Feb 24, 2015 · N719EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015031312391Floor Support · corrodedFLOOR SILL AT F/S 773.50 LT HAS CORROSION. REMOVED CORROSION FROM FLOOR AISLE LT SIDE FS 773.5 IAW SRM 51-21-06-001-001-A01. RECEVIED ECTC EA 32-2015-83. COMPLIED WITH EA 32-2015-83.Feb 24, 2015 · N719EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2015031312390Strap · crackedTIE STRAP CRACKED FOR PANEL 195DL. RECEIVED AND COMPLIED WITH ECTC REO 670-53-82-479.Feb 24, 2015 · N719EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2015031712412Door Sill · corrodedAFT CARGO BAY DOOR SILL HAS CORROSION. REPAIRED IAW REO 670-53-61-913.Feb 23, 2015 · N719EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2015031312389Floor Support · corrodedFLOOR SILL AT F/S 761.85-785.15, RT HAS CORROSION. REMOVED CORROSION FROM FLOOR ANGLE RT SIDE BETWEEN FS 761.05-785.15 IAW SRM 51-21-06-001-001-A01. RECEIVED ECTC EA 32-2015-082. COMPLIED WITH EA 32-2015-082.Feb 23, 2015 · N719EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2015031312388Seat Track · corrodedFLOOR SEAT TRACK AT LBL9, F/S 847-1000 HAS CORROSION. CORROSION BEYOND ALLOWABLE LIMITS IAW SRM 53-51-49-001-001-A01. REMOVED SEAT TRACK AT LBL9, FS847-1000 IAW AMM 53-00-49-000-801-A03. REPLACED SEAT TRACK AT LBL9 FS 847-1000. INSTALLED NEW SEAT TRACK IAWFeb 23, 2015 · N719EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015031312387Seat Track · corrodedFLOOR SEAT TRACK AT RBL9, F/S 847-1000 HAS CORROSION. CORROSION BEYOND ALLOWABLE LIMITS IAW SRM 53-51-49-001-001-A01. R & R PASSENGER SEAT RAIL AT RBL 9 AND F/S 847-1000 REF AMM 53-00-49-400-801-A03 AND 20-21-00-910-801-A01. INSTALLED NEW SEAT TRACK FITTINGFeb 23, 2015 · N719EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015031312386Seat Track · corrodedFLOOR SEAT TRACK AT RBL9, F/S 677-847 HAS CORROSION. CORROSION BEYOND ALLOWABLE LIMITS IAW SRM 53-41-49-001-001-A01. R & R SEAT RAIL AT RBL9, FS 677-847 IAW AMM 53-00-49-400-801, A03 AND 53-00-49-000-801, A03.Feb 23, 2015 · N719EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015031312385Seat Track · corrodedFLOOR SEAT TRACK AT LBL9, F/S 761-847 HAS CORROSION. RESOLUTION DESCRIPTION: FOUND DAMAGE TO BE OUT OF LIMITS IAW SRM 53-41-49-101-001-A01. R & R SEAT RAIL IAW AMM 53-00-49-000-801-A03 & AMM 53-00-49-400-801-A03.Feb 23, 2015 · N719EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015031312384Structure · corrodedPACKER IS CORRODED AT RBL9, FS 333. R & R PACKS, PN SH670-32157-3 IAW SRM 51-42-06-001-001-A01.Feb 23, 2015 · N719EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2015031312383Seat Track · corrodedFLOOR SEAT TRACK BETWEEN FS 581.00-FS 613.00, LBL 9 HAS CORROSION AROUND FASTENER HOLES. CORROSION BEYOND ALLOWABLE LIMITS IAW SRM 53-41-49-001-001-A01. R & R SEAT RAIL AT FS581-613, LBL9 IAW TASK 53-00-49-400-801-A03 AND 53-00-49-000-801-A03.Feb 23, 2015 · N719EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015031312382Seat Track · corrodedFLOOR SEAT TRACK BETWEEN FS 533.00-FS 581.00, LBL 9 HAS CORROSION AROUND FASTENER HOLES. CORROSION BEYOND ALLOWABLE LIMITS IAW SRM 53-31-49-001-001-A01. R & R SEAT RAIL AT RBL9, FS 533-581 IAW AMM 53-00-49-400-801-A03 AND 53-00-49-000-801-A03.Feb 23, 2015 · N719EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015031312381Seat Track · corrodedFLOOR SEAT TRACK BETWEEN FS 485.00-FS 581.00, RBL 9 HAS CORROSION AROUND FASTENER HOLES. FOUND DAMAGE TO BE OUT OF LIMITS IAW: SRM 53-31-49-101-001-A01. R & R SEAT RAIL AT RBL9, FS 485-581 IAW AMM 53-00-49-400-801, A03 AND 53-00-49-000-801, A03.Feb 23, 2015 · N719EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015031212376Seat Track · corrodedFLOOR SEAT TRACK BETWEEN FS 581.00-FS 693.00, RBL 9.00 HAS CORROSION AROUND FASTENER HOLES. BEYOND ALLOWABLE LIMITS IAW SRM 53-41-49-001-001-A01. R & R SEAT RAIL AT RBLQ FS 581-693 IAW AMM 53-00-49-400-801-A03 AND 53-00-49-000-801-A03.Feb 23, 2015 · N719EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015031212375Floorbeam · corrodedFS 280 CRAWLWAY FLOOR SUPPORT ANGLE HAS CORROSION. BEYOND ALLOWABLE LIMITS IAW SRM 53-00-00-101-001-A01. REMOVED CRAWLING FLOOR SUPPORT ANGLE AT FS280 IAW SRM 51-42-06-001-001-A01. LOCATED, DRILLED AND DEBURGED FASTENER HOLES IN NEW FLOOR SUPPORT ANGLE IAW Feb 22, 2015 · N719EV · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR ASOA2015031212374Angle · corrodedASD UPPER AFT ANGLE HAS CORROSION. REMOVED CORROSION AT ASD AFT UPPER ANGLE FUSELAGE SIDE IAW SRM 53-21-23-101-001-A01. BLENDED AREA IS OUT OF ALLOWABLE LIMITS IAW SRM 53-21-23-101-001-A01. R & R ANGLE ON ASD UPPER AFT IAW SRM 51-42-06-001-001-A01.Feb 22, 2015 · N719EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2015031212373Angle · corrodedSERVICE DOOR UPPER ANGLE HAS CORROSION. AFTER FURTHER EVALUATION FOUND CORROSION ON UPPER ANGLE OUT OF LIMITS IAW SRM 53-21-23-101-002-A01. REMOVED SERVICE DOOR SILL UPPER ANGLE IAW SRM 51-42-06 LOCATED + DRILLED NEW PART IAW SRM 51-40-11. INSTALLED NEW SERFeb 22, 2015 · N719EV · Cndair CL6002C10 · Service DoorsSDR ASOA2015031212372Bulkhead Web · corrodedFS 280 WEB LT HAS CORROSION. COMPLIED WITH EC/TC REO 670-53-11-594 AND GREO 670-53-11-594- REV.Feb 22, 2015 · N719EV · Cndair CL6002C10 · Fuselage Main, BulkheadSDR ASOA2015031212371Bulkhead Web · corrodedFS 280, WEB RT HAS CORROSION. COMPLIED WTIH EC/TC REO 670-53-11-594 01 AND GREO 670-53-11-594 REV.Feb 22, 2015 · N719EV · Cndair CL6002C10 · Fuselage Main, BulkheadSDR ASOA2015031212370Intercostal · corrodedINTERCOSTAL AT FS 364, 27L HAS CORROSION. REMOVED INTERCOSTAL AT F/S 364 27L IAW SRM 51-42-06-001-001-A01. LOCATED DRILLED AND DEBURRED FASTENER HOLES ON INTERCOSTAL AT F/S 364 27L IAW SRM 51-40-11-001001-A01. INSTALLED INTERCOSTAL AT F/S 364 27L IAW SRM 51Feb 22, 2015 · N719EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2015031212369Intercostal · corrodedINTERCOSTAL AT FS 364, S27R HAS CORROSION. REMOVED INTERCOSTAL AT FS 364, 27R IAW SRM 51-42-06-001-001-A01. LOCATED DRILLED AND DEBURRED FASTENER HLES ON INTERCOSTAL AT FS 364 27R IAW CRJ700 51-40-11-001-001-A01. INTERCOSTAL AT FS 364, 27R WAS INSTALLED IAFeb 22, 2015 · N719EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2015031212368Frame · corrodedF/S 310, FRAME STR 27 HAS CORROSION FWD SIDE. REMOVED CORROISON FOR FURTHER EVAL IAW 51-21-06-001-001-A01. BLENDED CORROSION FROM 27L-26R IAW SRM 51-42-06-001-001-A01/51-21-06-001-001-A01 AT FS 310. COMPLIED WITH STS EA 32-2015-076, SECTION 1, PERMANENT REPFeb 22, 2015 · N719EV · Cndair CL6002C10 · Fuselage Main, FrameSDR ASOA2015031212367Skin · corrodedPAX DOOR INNER SKIN HAS CORROSION ALONG NUTPLATE HOLES OF 832FL. INSTALLED NEW SERVICEABLE PAX DOOR INNER SKIN IAW DWC 601R318024, SRM 51-42-06-001-001, 51-42-21-00-001 & 51-42-13-001-001. DRILLED AND LOCATED NEW SERIVCABLE INNER SKIN IAW SRM 51-40-06-001-00Feb 21, 2015 · N719EV · Cndair CL6002C10 · Passenger/Crew DoorsSDR ASOA2015031312398Skin · damaged1 BURNED FASTENER 2" AFT FS 1181 AND STR 25R. R & R TEMP FASTENER WITH SOLID FASTENER IAW SRM 51-42-10-001-001-A01. REMOVED TEMPORARY FASTENER AT FS 1181 & STR25R IAW SRM 51-42-10-001-001-A01. REMOVED TOP COAT IAW 51-26-00-001-001-A01. INSTALLED PERMANENT Feb 18, 2015 · N719EV · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR ASOA2015031312397Skin · damaged1 BURNED FASTENER BETWEEN FS 421 AND FS 437, STRG 25R. COMPLIED WITH LIGHTNING STRIKE REPAIR FOR FASTENER BETWEEN FS 421 AND FS 437, STR 25R IAW TR53-0049, SRM 53-00-00-201-003-A01. REMOVED EXTERIOR FINISH AT TEMPORARY FASTENER BETWEEN FS 421-437, STR 25 IAWFeb 18, 2015 · N719EV · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR ASOA2015031312396Skin · damaged12 BURNS ON RT BOTTOM OF OUTER SKIN, TAIL CONE AREA. COMPLIED WITH PERMANENT REPAIR IAW EC/TC EA 12-2014-201. COMPLIED WITH SECTION III PERMANET REPAIR, OF EA 12-2014-201, REV B. RECEIVED AND COMPLIED WITH ECTC EA 12-2014-201.Feb 18, 2015 · N719EV · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR ASOA2014082911144Skin · damagedONE BURN ON RT FWD CENTER WING PLANK APPROX 18" AFT OF FRONT SPAR AND APPROXIMATELY 18 INCHES OTBD OF CENTER KEEL BEAM. BLENDED LIGHTNING STRIKE. REPAIRED IAW SRM 51-13-01, 51-12-00. RII COMPLIED WITH SATISFACTORY IAW GMM 3-3.Aug 27, 2014 · N719EV · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR ASOA2014022109990Lamp · burned outFORWARD MOST CABIN CEILING EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMPS. OPS CHECKED GOOD.Feb 17, 2014 · N719EV · Cndair CL6002C10 · Emergency LightingSDR ASOA2014012409809Handle · lack of lubeSERVICE DOOR HARD TO OPEN. HANDLE STICKS AT .5 OPEN. LUBRICATED & PERFORMED OPS CHECK OF SERVICE DOOR IAW AMM 52-49-00. CHECKED GOOD AT THIS TIME.Jan 23, 2014 · N719EV · Cndair CL6002C10 · Service DoorsSDR ASOA2013121109608Megaphone · inoperativeMEGAPHONE INOPERATIVE. R & R MEGAPHONE IAW AMM 25-61-14, IPC 25-61-14, ITEM 5, FIG 1. OP'S CHECKED GOOD.Dec 7, 2013 · N719EV · Cndair CL6002C10 · Emergency Equipment
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