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 ASOA2013092709105Megaphone · malfunctionedMEGAPHONE INOPERATIVE. RESET MEGAPHONE AS OPS CHECKS IAW AMM 25-61-14, OK FOR SERVICE.Sep 26, 2013 · N719EV · Cndair CL6002C10 · Emergency EquipmentSDR ASOA2013071808723Sign · unserviceableFLT 5071 EMERGENCY EXIT SIGN OVER SERVICE DOOR HAS FALLEN OFF. R & R SERVICE DOOR EXIT SIGN. OP'S CHECKED GOOD IAW MM 33-51-05.Jul 14, 2013 · N719EV · Cndair CL6002C10 · Emergency LightingSDR ASOA2013040403287Battery · dischargedEMEREGENCY LIGHT WILL NOT COME ON FROM FLT DECK OR F/A POSITION. RECHARGED BATTERIES WITH APU, OPS CHECKED GOOD, AMM 33-24-07.Mar 31, 2013 · N719EV · Cndair CL6002C10 · Emergency LightingSDR ASOA2013032903280Door · lack of lubeGALLEY SERVICE DOOR DIFFICULT TO OPEN. HANGS WITH HANDLE AT ABOUT 12 O`CLOCK POSITION. LUBRICATED SEAL AND PERFORMED OPS CHECK IAW AMM 52-41-00. NO FURTHER DEFECTS NOTED.Mar 28, 2013 · N719EV · Cndair CL6002C10 · Service DoorsSDR ASOA2013031903237Battery · dischargedF/A REPORTS FLASHLIGHT IS INOPERATIVE. REPLACED BATTERY IAW AMM 25-60-00.Mar 15, 2013 · N719EV · Cndair CL6002C10 · Emergency EquipmentSDR ASOA2013031103145Fitting · crackedFOUND FWD JACK FITTING CRACKED. REMOVED FWD JACK FITTING ASSY IAW SRM 51-42-21-001-001-A01. LOCATED, DRILLED AND DEBURRED NEW FWD JACK FITTING IAW SRM 51-40-11-001-001-A01. INSTALLED NEW JACK FITTING IAW SRM 51-42-21-001-001-A01 DWG CC670-32050. MAJOR REFeb 16, 2013 · N719EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2013031103144Intercostal · corrodedNOSE JACK POINT LT INTERCOSTAL CORRODED. REMOVED TWO STAND OFF NUTPLATES FROM SUPPORT INTERCOSTAL IAW SRM 51-42-06-001-001-A01. INSTALLED TWO STANDOFF NUTPLATES ONTO LT INTERCOSTAL IAW SRM 51-42-06-001-001-A01. REMOVED GUSSET IAW SRM 51-42-06-001-001-A01. Feb 14, 2013 · N719EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2013031103143Pressure Panel · crackedRT MLG WHEEL WELL PRESSURE PANEL BETWEEN RBL 18 AND RBL 27 AT FS 810 IS CRACKED. COMPLIED WITH EO KSH670-35824-503P1.Feb 5, 2013 · N719EV · Cndair CL6002C10 · Fuselage Main, BulkheadSDR ASOA2013031103142Angle · corrodedSERVICE DOOR LOWER SEAL STRIKER ANGLE CORRODED IN MULTIPLE LOCATIONS FOUND DURING SILL REPLACEMENT. REMOVED LOWER SILL STRIKER IAW SRM 51-42-06-001-001. LOCATED AND DRILLED SERVICE DOOR LOWER SEAL STRIKER IAW SRM 51-40-11-001-001. STEPPED UP SCREW HOLES ANFeb 5, 2013 · N719EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2013031103141Angle · corrodedSERVICE DOOR SILL CAP ANGLE CORRODED IN MIDDLE FOUND DURING SILL REPLACEMENT. OBTAINED AND DRILLED NEW SERVICEABLE SILL CAP ANGLE, AS REQUIRE TRANSFER CLIPS AND INSTALLED NEW NUTPLATES IAW SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-45-60-001-001-A01. Feb 5, 2013 · N719EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2013031103140Floor Support · crackedCENTER COCKPIT FLOOR SUPPORT ANGLE AT FS 259.2-280 AT RBL 12 CRACKED IN AFT INBD RADIUS. REMOVED FLOOR SUPPORT ANGLE IAW SRM 51-42-06-001-001 AND REPLACED WITH NEW SUPPORT ANGLE IAW SRM 51-42-06-001-001-A01. MAJOR REPAIR.Feb 4, 2013 · N719EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2013031103139Floor Support · crackedCENTER COCKPIT FLOORBOARD 221ALF LT SUPPORT ANGLE AT FS 259-280 AT LBL 12 CRACKED IN AFT INBD RADIUS. REMOVED CENTER COCKPIT FLOOR SUPPORT ANGLE IAW SRM 51-42-06-001-001. DRILLED AND INSTALLED NEW FLOOR SUPPORT IAW SRM 51-42-06-001-001-A01. MAJOR REPAIR.Feb 4, 2013 · N719EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2013031103138Floor Support · crackedFLIGHT COMPARTMENT LT SIDE AFT FLOOR SUPPORT ANGLE CRACKED AT BS 280 VERTICAL SUPPORT BEAM. R & R ANGLE WITH SERVICEABLE ANGLE ALL WORK DONE IAW SRM 51-42-06-001-001-A01 LT SIDE AFT FLOOR SUPPORT ANGLE.Feb 4, 2013 · N719EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2013031103137Intercostal · corrodedNOSE JACK POINT, RT INTERCOSTAL CORRODED AT ATTACH FLANGE. REMOVED RT JACKPOINT, NOSE INTERCOSTAL & AFT ATTACH ANGLE IAW SRM 51-42-06-001-001-A01. LOCATED & DRILLED NEW INTERCOSTAL IAW SRM 51-40-11. OK TO INSTALL. INSTALLED NEW RT INTERCOSTAL AT NOSE JACKFeb 1, 2013 · N719EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2013031103136Floor Panel · crackedFWD EQUIPMENT COMPARTMENT FLOOR CRACKED LT SIDE DOOR FRAME, OTBD OF BRAKE GAUGE SUPPORT BRACKET. REPAIRED IAW REO 670-53-11-509.Feb 1, 2013 · N719EV · Cndair CL6002C10 · Fuselage Floor PanelSDR ASOA2013031103135Angle · corrodedPAX DOOR FWD BOTTOM CORNER FOUND TO BE CORRODED. REMOVED ASD BOTTOM CORNER IAW SRM 51-42-06-001-001. INSTALLED ASD BOTTOM CORNER IAW SRM 51-42-06-001-001 WITH SERVICABLE PARTS.Jan 30, 2013 · N719EV · Cndair CL6002C10 · Passenger/Crew DoorsSDR ASOA2013031103134Angle · corrodedFOUR HINGE SIDE LOWER L ANGLES FOUND TO BE CORRODED. REMOVED ANGLES IAW SRM 51-42-06-001-001. INSTALLED SERVICABLE LOWER ANGLES IAW SRM 51-42-06-001-001.Jan 29, 2013 · N719EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2013031103133Channel · corrodedPAX DOOR LOWER CENTER CHANNEL FOUND TO BE CORRODED. REMOVED ASD LOWER CENTER CHANNEL IAW SRM 51-42-06-001-001. INSTALLED LOWER CENTER CHANNEL WITH SERVICABLE PARTS IAW SRM 51-42-06-001-001.Jan 29, 2013 · N719EV · Cndair CL6002C10 · Passenger/Crew DoorsSDR ASOA2013031103132Riser · corrodedFWD STEP RISER HAS CORROSION - UPPER END. COMPLIED WITH EC/TC REO 670-52-11-104 AND MET THE REQUIREMENTS OF REO 670-52-11-104, REV F AS WRITTEN.Jan 29, 2013 · N719EV · Cndair CL6002C10 · Passenger/Crew DoorsSDR ASOA2013031103131Stringer Splice · corrodedSPLICE CORRODED AT STR 25RT AT FRAMES 333.00 - 319.70. REMOVED STRINGER SPLICE IAW SRM 51-42-06-001-001-A01. LOCATED AND DRILLED NEW STRINGER SPLICE AND INSTALLED IAW SRM 51-42-06-001-001.Jan 28, 2013 · N719EV · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR ASOA2013031103130Frame · corrodedCIRCUMFERENTIAL FRAME AT FS 280 BL 0 HAS CORROSION ON AFT WEB. RECEIVED AND COMPLIED WITH REO 670-53-11-789 P1 IAW NDTM PART 1, 51-20-006.Jan 28, 2013 · N719EV · Cndair CL6002C10 · Fuselage Main, FrameSDR ASOA2013031103129Stringer · corrodedSTRINGER 19 AT FS 330 HAS EXFOLIATION CORROSION AT PASSENGER DOOR HARNESS BRACKET MOUNTING LOCATION. R & R STRINGER IAW SRM 51-42-06.Jan 26, 2013 · N719EV · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR ASOA2013031103128Crossbeam · crackedBS 280 CROSSBEAM CORRODED AND CRACKED IN CENTER. COMPLIED WITH EC/TC REO 670-53-11-047 AND REO 670-53-11-047, REV E.Jan 26, 2013 · N719EV · Cndair CL6002C10 · Fuselage Main, StructureSDR ASOA2013031103127Sill · corrodedSERVICE DOOR CUTOUT UNDER SILL PLATE HAS TWO CORRODED LT BRACKETS. REMOVED CORRODED ANGLES 2(EA) IAW SRM 51-42-06-001-001-A01. INSTALLED 2EA ANGLES AT SERVICE DOOR CUTOUT UNDER SILL PLATE IAW SRM TASK 51-42-06-001-001-A01. OBTAINED AND DRILLED TWO ANGLES ATJan 24, 2013 · N719EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2013031103126Sill · corrodedSERVICE DOOR CUTOUT SILL CORRODED AT MULTIPLE LOCATIONS. REMOVED CORRODED MOUNTING ANGLE IAW SRM 51-42-06-001-001-A01. OBTAINED AND DRILLED NEW MOUNTING ANGLE AS RQUIRED IAW SRM TASK 51-40-11-001-001-A01. INSTALLED MOUNTING ANGLE, PN SH670-31996-3 ON SERVICJan 24, 2013 · N719EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2013031103125Channel · corrodedLOWER FUSELAGE ACCESS PANEL 192BB & 191BB CENTER NUTPLATE CHANNEL CORRODED IN SEVERAL AREAS. BLENDED CORROSSION FROM CENTER TEE CHANNEL STRUCTURE REF 51-12-00-001-001-A01. DAMAGE BEYOND ALLOWABLE LIMIS IAW SRM 53-82-55-101-001-A01.Jan 23, 2013 · N719EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2013031103124Post · corrodedCOCKPIT ENTRY DOOR POST AT BS 280 CORRODED AT RT LOWER SECTION. REMOVED CORROSION FROM INBD & OTBD SIDE OF RT LWR DOOR POST AT FS280 IAW SRM 51-42-06-001-001, 51-21-06-001-001. ORIG MAT THICKNESS .032" IAW SRM 53-11-10-991-803. RECEIVED AND COMPLIED WITH REOJan 23, 2013 · N719EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2013030803123Post · corrodedCOCKPIT ENTRY DOOR POST AT FS280 CORRODED AT LT LOWER SECTION. REMOVED CORROSION FROM INBD & OTBD SIDE OF LT LWR DOOR POST AT FS280 IAW SRM 51-42-06-001-001, 51-21-06-001-001 ORIG MAT THICKNESS .032" IAW SRM 53-11-10-991-803. RECEIVED AND COMPLIED WITH REO 6Jan 23, 2013 · N719EV · Cndair CL6002C10 · Fuselage Main, StructureSDR ASOA2013030803122Floor Support · corrodedAFT FLOOR SUPPORT ANGLE CORRODED FOR COCKPIT FLOOR PANEL 221ALF. REMOVED FLOOR SUPPORT ANGLE AND LOCATED ALL HOLES EXCEPT 2EA LT & RT OTBD UPPER GUSSET ATTACH HOLES IAW 51-42-06-001-001 & DWG CC670-33052 HOLES IN NEW ANGLE. REDRILLED AND INSTALLED NEW ANGLE Jan 23, 2013 · N719EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2013030803121Web · corrodedLEFT WEB CORRODED AT FS 280. REPAIRED IAW EC/TC 670-53-11-594 AND REO 670-53-11-594 REV.Jan 23, 2013 · N719EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2013030803120Web · corrodedRT WEB CORRODED AT FS 280. COMPLIED WITH EC/TC REO 670-53-11-594 01 AND REO 670-53-11-594 REV.Jan 23, 2013 · N719EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2013030803119Stringer Clip · corrodedSTRINGER CLIP 26R CORRODED, BETWEEN FRAMES 349.00 & 364.00. REMOVED CORROSION IAW SRM 51-42-06-001-001-A01 AND 51-21-06-001-001-A01. BLENDED AREA IS OUT OF LIMITS IAW SRM 53-21-23-101-003-A01. DAMAGE NEEDS TO BE SBMITTED TO THD FOR FURTHER ACTION. PROVIDEDJan 22, 2013 · N719EV · Cndair CL6002C10 · Fuselage Main, Attach FittingsSDR ASOA2013030803118Stringer · corrodedSTRINGER 26R CORRODED BETWEEN FRAMES 333 & 349. REMOVED CORROSION AT FS 339.5, STGR 26R IAW SRM 51-42-06-001-001. NO DAMAGE ALLOWED AT THIS LOCATION IAW SRM 53-21-03-001-001. COMPLIED WITH REO 670-53-21928.Jan 22, 2013 · N719EV · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR ASOA2013030803117Stringer · corrodedSTGR 26LT CORRODED BETWEEN FRAMES 333 & 349. REMOVED CORROSION ON STGR 26LT BETWEEN FS333-349 IAW SRM 51-21-06-001-001-A01 AND 51-42-06-001-001-A01. RECEIVED AND COMPLIED WITH REO 670-53-21-925.Jan 22, 2013 · N719EV · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR ASOA2013030803116Stringer · corrodedSTRINGER 25R CORRODED BETWEEN FRAMES 333.00 & 319.70. REMOVED STR 25RH, FS X280-X333 AND 4EA STRINGES ATTACH CLIPS FS X294-X333, STR 25 RT IAW SRM 51-42-06-000-001-A01. INSTALLED SERVICABLE STRINGER 25, RT FS 28.00- FS333.0 AND 2EA STRINGER ATTACH CLIPS FS Jan 22, 2013 · N719EV · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR ASOA2013030703114Frame · corrodedFRAME BS 333 CORRODED AT S27. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01 AND 51-42-06-001-001-A0. DAMAGE IS NOT PERMITTED ON FRAME IAW SRM 53-21-06-101-002-A01,-006-A01. COMPLIED WITH REO 670-53-21-826 AND REO 670-53-21-926.Jan 22, 2013 · N719EV · Cndair CL6002C10 · Fuselage Main, FrameSDR ASOA2013030703113Frame · corrodedFRAME BS 319.70 CORRODED BETWEEN STGR 26L AND 27. REMOVED FRAME 319.70 STR21L-23R IAW SRM 51-42-06-001-001-A01. INSTALLED NEW SERVICEABLE FRAME AT FS319.0, STGR23L TO STGR23R IAW SRM 51-40-11-00-001-001-A01 AND 51-42-06-001-001-A01.Jan 22, 2013 · N719EV · Cndair CL6002C10 · Fuselage Main, FrameSDR ASOA2013030703112Frame · corrodedFRAME 310 CORRODED BETWEEN STGR 26RT & 26LT. REMOVED CORROSION FROM PREVIOUSLY TREATED AREA IAW SRM 51-21-26-001-001-A01 FROM FS 310 BETWEEN STGR 26 RT AND 26 LT. COMPLIED WITH STEP 1 REO 670-53-21-923.Jan 22, 2013 · N719EV · Cndair CL6002C10 · Fuselage Main, FrameSDR ASOA2013030703111Skin · corrodedCIRCUMFERENTIAL JOINT INTERNAL SKIN BELOW FLOOR AT BS 280 CORRODED BETWEEN STGR 26LT & 26RT. BLENDED DAMAGE AS NEEDED REF SRM 51-42-06-001-001 & SRM 51-21-06-001-001. COMPLIED WITH REO 670-53-21-921.Jan 22, 2013 · N719EV · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR ASOA2013030703110Floor Support · corrodedCRAWLWAY FLOOR SUPPORT ANGLE CORRODED. REMOVED CRAWLWAY FLOOR SUPPORT ANGLE IAW SRM 51-42-03-001-001. LOCATED AND DRILLED AND DEBURED NEW ANGLE IAW SRM 51-40-11-001-001-A01. INSTALLED NEW ANGLE IAW SRM 51-42-21-001-001-A01 AND 51-42-06-001-001-A01. THIS REJan 22, 2013 · N719EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2013030703109Seat Track · corrodedRT SIDE WALL SEAT TRACK BS 708 IS CORRODED. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801, CONF A03. INSTALLED SEAT TRACK IAW AMM 53-00-49-400-801.Jan 22, 2013 · N719EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2013022103056Doubler · corrodedTCAS ANTENNA DOUBLE CORRODED AT S27 BETWEEN BS 295 AND 310. REMOVED TCAS ANTENNA DOUBLER, LOCATED AND DRILLED NEW TCAS DOUBLER AND INSTALLED IAW SRM 51-42-06-001-001. REPAIR IS CLASSIFIED AS MAJOR.Jan 22, 2013 · N719EV · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR ASOA2013022103055Frame · corrodedFRAME BS 295 CORRODED AT S27 FWD & AFT SIDES. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. COMPLIED WITH REO 670-53-21-922.Jan 22, 2013 · N719EV · Cndair CL6002C10 · Fuselage Main, FrameSDR ASOA2013022103054Stringer · corrodedSTRINGER 27 CORRODED AT FS 280. REMOVED STRINGER 27 FROM FS 280-298 REF SRM 51-42-06-001-001 & SRM 51-42-21-001-001. LOCATED, DRILLED & INSTALLED NEW STRINGER 27 SECTION IAW SRM 51-40-11-001-001-A01, 67-25-01-001-001-A01.Jan 22, 2013 · N719EV · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR ASOA2013022103053Seat Track · corrodedRT SIDE WALL SEAT TRACK AT FS 724.08 IS CORRODED. REPLACED SEAT TRACK IAW GREO 670-55-00-013 AND AMM 53-00-49-400-801.Jan 22, 2013 · N719EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2013022103052Seat Track · corrodedSIDE WALL SEAT TRACK ON THE RT SIDE AT FS 736.05 IS CORRODED. SEAT TRACK REMOVED FROM FS 713 TO 763 IAW IAW AMM 53-00-49-000-801. INSTALLED SEAT TRACK IAW AMM 53-00-49-400-801.Jan 22, 2013 · N719EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2013030703108Seat Track · corrodedSEAT TRACK ON THE LT SIDE AT BS 797 ON THE SIDE WALL IS CORRODED. R & R SEAT TRACK IAW AMM 53-00-49-000-81.Jan 21, 2013 · N719EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2013021403015Seat Track · corrodedSEAT TRACK ON THE RIGHT INBD SIDE AT FS 250 JUST FWD OF FS364.00 IS CORRODED. REMOVED CORRODED SEAT TRACK & INSTALLED TRACK IAW SRM 53-00-49-400-801.Jan 21, 2013 · N719EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2013021403014Floor Panel · crackedFWD EQUIPMENT COMPARTMENT FLOOR CRACKED LT SIDE DOOR FRAME, OTBD OF BRAKE GAUGE SUPPORT BRACKET. REPAIRED IAW GREO 670-53-11-509.Jan 20, 2013 · N719EV · Cndair CL6002C10 · Fuselage Floor PanelSDR ASOA2013021403013Door · lack of lubeLT EMERGENCY DOOR FAILED FUNCTIONAL TEST IAW JOB 0/4041 CADR. ST52-830-104 FORCE WAS 50 LBS. SERVICED LT EMERGENCY DOOR WITH LUBRICATION IAW AMM 12-20-52-640-802 AND FUNCTIONAL TEST IAW AMM 52-21-00-720-801 PULL FORCE WAS 32LBS FUNCTIONAL TEST GOOD.Jan 19, 2013 · N719EV · Cndair CL6002C10 · Emergency Exits
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