N723EV

Service difficulty reports · 250

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 = 'N723EV' 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 ASOA2016012114411Seat Track · corrodedLEFT SEAT TRACK SEGMENT HAS CORROSION AT BS 374. FOUND TO BE OUT OF LIMITS IAW REO 670-53-00-013. REPLACED SEAT TRACK IAW AMM 53-00-49-400-801-A03, AND 53-00-49-000-801-A03.Jan 21, 2016 · N723EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2016012114410Seat Track · corrodedRT SEAT TRACK SEGMENT BETWEEN BS 581 AND 677 HAS CORROSION IN MULTIPLE AREAS. FOUND TO BE OUT OF LIMITS IAW REO 670-53-00-013. REPLACED THE SEAT TRACK IAW AMM 53-00-49-400-801-A03, AND 53-00-49-000-801-A03.Jan 21, 2016 · N723EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2016012114409Seat Track · corrodedRT SEAT TRACK SEGMENT BETWEEN BS 485 AND 581 HAS CORROSION IN MULTIPLE AREAS. FOUND TO BE OUT OF LIMITS IAW REO 670-53-00-013. REPLACED THE SEAT TRACK IAW AMM 53-00-49-400-801-A03, AND 53-00-49-000-801-A03.Jan 21, 2016 · N723EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2016012114408Seat Track · corrodedRT SEAT TRACK SEGMENT BETWEEN BS 350 AND 485 HAS CORROSION IN MULTIPLE AREAS. FOUND TO BE OUT OF LIMITS IAW REO 670-53-00-013. REPLACED THE SEAT TRACK IAW AMM 53-00-49-400-801-A03, 53-00-49-000-801-A03.Jan 21, 2016 · N723EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2016012014459Angle · corrodedCORROSION ON PAX DOOR SILL ANGLE. REMOVED UPPER MID-CAP ANGIE AT PAX DOOR IAW SRM 51-41-02-001-001 A01. INSTALLED UPPER MID CAP ANGLE IAW SRM 51-41-02-001-001-A01. LOCATED AND DRILLED NEW SERVICABLE MIDCAP ANGLE IAW SRM 51-40-11-001-001 A01. REMOVED LOWEJan 20, 2016 · N723EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2016012014458Fitting · corrodedJACK SUPPORT FITTING AT FS 278.00 AND BL0.00 CORRODED. LT FWD AJCK SUPPORT FITTING CORRODED THRU ATTACH FLANGE AND CRACKED RT FWD JACK SUPPORT FITTING CORRODED ENTIRE LENGTH OF ATTACH FLANGE SERVICE INTERGRANULATE CORROISON ON INTERCOSTAL REQUIRES REPLACEMENTJan 20, 2016 · N723EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2016012014457Diaphragm · crackedFUSELAGE EXTERNAL DIAPHRAM AT STR 24L FS909.00 IS CRACKED. RECEIVED & COMPLIED WITH EA 15-216-006, P4. REPAIRED IAW REO 670-53-82-487. COMPLIED WITH REO 670-53-82-478, R-A DATED 11-12-2014. REPAIRED WING FUSELAGE AFT FAIRING SUP FS 909.00, LBL 17.63 IAW Jan 20, 2016 · N723EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2016012014434Door Sill · corrodedCORROSION ON SERVICE DOOR SILL AT VARIOUS LOCATIONS ALONG THE SURFACE FROM FS 319.70 - FS 349.00. REMOVED S/D SILL IAW SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. LOCATED AND DRILLED NEW S/D SILL IAW SRM 51-40-11-001-001-A01. INSTALLED NEW S/D SILL IJan 20, 2016 · N723EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2016012014433Stringer · corrodedCORROSION ON STRINGER 26R BETWEEN FS 319.7 - 349. BLENDED DAMAGE BETWEEN FS 319 & FS 349 FOUND DEEP PITTING TO BE OUT OF LIMITS REF SRM 53-21-03-101-002-A01. REMOVED CLEATS AT FS 319, FS 333, FS 349 IAW SRM 51-42-0-001-001-A01. REMOVED STRINGER CLEATS ON THEJan 20, 2016 · N723EV · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR ASOA2016012014426Frame · corrodedCORROSION ON CIRCUMFERENTIAL JOINT AT FS 280.00 BETWEEN STR 26L-24R. BLENDED CORROSION ON CIRCUMFIRENTIAL JOINT AT S 280 BETWEEN STR 26L-24R. COMPLIED WITH EA 26-2016-024 SECTION 1-PERMANENT REPAIR.Jan 20, 2016 · N723EV · Cndair CL6002C10 · Fuselage Main, FrameSDR ASOA2016012014407Floor Support · corrodedCORROSION ON RT FLOOR SUPPORT AT BS 350 AND RBL 45. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01.Jan 20, 2016 · N723EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2016012014406Floor Support · corrodedCORROSION ON RT FLOOR SUPPORT AT FS 319.70 AND RBL 45. BLENDED CORROSION IAW SRM, 51-21-06-001-001-A01. COMPLIED WITH EC/TC REO 670-53-00-390 AND REO 670-53-00-390, REV DATED 01/22/2014.Jan 20, 2016 · N723EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2016012014405Floorbeam · corrodedCORROSION ON COCKPIT FLOORBEAM ANGLE AT FS 280 BETWEEN RBL9-LBL9. REMOVED CORRODED FLOORBEAM ANGLE IAW SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01. LOCATED, TRANSFERED, DRILL MOUNTING HOLES AND INSTALLED SERVICABLE FLOORBEAM ANGLE IAW SRM 51-40-11-Jan 20, 2016 · N723EV · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR ASOA2016012014404Floorbeam · corrodedCORROSION ON RT FLOORBEAM AT RBL 45 AND FS 280.00. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. COMPLIED WITH EC/TC REO 670-53-00-390 AND REO 670-53-00-390, REV DATED 01/22/2014.Jan 20, 2016 · N723EV · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR ASOA2015092413827Bulb · burned out12CD LOWER EXIT SIGN HAD ONE BULB BURNED OUT. R & R THE BULB IAW AMM 33-51-05. OPS CHECKED GOOD.Sep 24, 2015 · N723EV · Cndair CL6002C10 · Emergency LightingSDR ASOA2015092413826Bulb · burned out12 AB LOWER EXIT SIGN HAD ONE BULB BURNED OUT. R & R THE BULB IAW AMM 33-51-05. OPS CHECKED GOOD.Sep 24, 2015 · N723EV · Cndair CL6002C10 · Emergency LightingSDR ASOA2015080513448Unknown · smokeAFTER TAKEOFF, RECEIVED AFT SMOKE LAV, ACFT RETURNED TO DEPARTURE AFTER T/O, EMERGENCY DECLARED. COMPLIED WITH COMPARTMENT WASH, DRY-OUT RUNS IAW AMM 72-00-00. ACFT OK FOR SERVICE.Aug 5, 2015 · N723EV · Cndair CL6002C10 · Air Distribution SystemSDR ASOA2015051412826Circuit Breaker · malfunctionedEMERGENCY LIGHTS ON WHILE ARMED. CIRCUIT BREAKER RESET SYSTEM POWER TO EMERGENCY LIGHTS IAW FIM PG 12 FAULT NO LONGER EXIST IAW MCC NO FURTHER ACTION IS REQUIRED.May 10, 2015 · N723EV · Cndair CL6002C10 · Emergency LightingSDR ASOA2014112411721Pump · leakingNR 1 HYD QUANTITY EVACUATED IN FLIGHT TO 0 PERCENT. EDP RAN 1 HOUR 1 MIN W/OUT FLUID, EMERGENCY DECLARED AS A PRECAUTION. R & R LT ENGINE HYD PUMP IAW AMM 29-11-01, REF AIPC 29-11-01, ITEM 5. OPS AND LEAK CHECKS GOOD AT THIS TIME. ACFT RETURNED TO SERVICENov 18, 2014 · N723EV · Cndair CL6002C10 · Hydraulic Pump (Electric/Engine), MainSDR ASOA2014090911186Retainer · bentFWD CARGO DOOR SEAL RETAINER BENT AT FWD SIDE. REPAIRED IAW EC/TC REO 670-52-35-127 01 FOR PERMANENT REPAIR TO THE FWD CARGO DOOR SEAL LOWER RETAINER.Sep 5, 2014 · N723EV · Cndair CL6002C10 · Cargo/Baggage DoorsSDR ASOA2014072910981Battery Pack · failedFWD EMERGENCY LIGHTS WILL NOT STAY ILLUMINATED. R & R FWD EMERGENCY LIGHT BATTERY IAW AMM 33-51-17. OPS CHECKED GOOD.Jul 25, 2014 · N723EV · Cndair CL6002C10 · Emergency LightingSDR ASOA2014052010510Skin · damagedWHILE INVESTIGATING COFFEEMAKER, FOUND HEAT DAMAGE TO FUSELAGE SKIN ABOVE GALLEY 1. PERFORMED VISUAL INSPECTION FOR BUCKLING OR WARPING IAW SRM 51-11-06 NO DEFECTS NOTED. CLEANED DAMAGED AREAS IAW SRM 51-26-00.May 16, 2014 · N723EV · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR ASOA2014032110160Lamp · burned outCABIN SECOND FROM FRONT CEILING EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP AND OPS CHECKED GOOD IAW AMM 33-51-00.Mar 19, 2014 · N723EV · Cndair CL6002C10 · Emergency LightingSDR ASOA2014031410130Linkage · unsecureSERVICE DOOR WILL NOT OPEN. SECURED LINKAGE ON SERVICE DOOR LATCH IAW AMM 52-41-03. OPS CHECKED GOOD IAW AMM 52-41-00. ACFT OK FOR SERVICE.Mar 11, 2014 · N723EV · Cndair CL6002C10 · Service DoorsSDR ASOA2014013109831Skin · damagedFOUND 1EA OVERSIZED HOLE IN WING SKIN AND ONE FREEZE PLUG ON LT SIDE. COMPLIED WITH REO 670-57-21-658, REV (P1). MAJOR REPAIR.Jan 5, 2014 · N723EV · Cndair CL6002C10 · Wing, Plate/SkinSDR ASOA2014013109830Floor Support · crackedFOUND LEFT COCKPIT FLOOR SUPPORT AT FS 280 ANGLE CRACKED AND GUSSET UNSERVICEABLE. REMOVED LT COCKPIT FLOOR SUPPORT ANGLE AND GUSSET IAW SRM 51-42-06-001-001-A01. LOCATED, DRILLED AND DEBURRED ASSEMBLED NEW SUPPORT ANGLE AND GUSSET IAW SRM 51-40-11-001-001-Jan 4, 2014 · N723EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2014013109829Floorbeam · crackedLT COCKPIT FLOORBEAM FOUND CRACKED. REPAIRED IAW REO 670-53-11-893, REV "B".Jan 4, 2014 · N723EV · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR ASOA2014011509753Floorbeam · crackedWHILE PERFORMING SB 670BA-53-041, FOUND RT COCKPIT BS 280 FLOORBEAM ANGLE CRACKED AND GUSSET UNSERVICEABLE. REMOVED FLOORBEAM ANGLE AND GUSSET IAW SRM 51-42-06-001-001-A01. LOCATED, DRILLED AND DEBURRED AND ASSY NEW FLOORBEAM ANGLE AND GUSSET IAW SRM 51-40Jan 4, 2014 · N723EV · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR ASOA2013123109734Bulkhead Web · corrodedRT 280, LOWER BULKHEAD WEB CORRODED. REPAIR RT LOWER BULKHEAD WEB IAW SRM 53-11-10-201-003-A01. REPAIR "A" IF BEYOND LIMITS OF REPAIR "A" REPAIR IAW GREO. HAND BLENDED AREAS OF CORROSION & FOUND AREAS, WITHIN LIMITS, IAW SRM 53-11-10-201-003-A01 & TREATED Dec 28, 2013 · N723EV · Cndair CL6002C10 · Fuselage Main, BulkheadSDR ASOA2014011509752Seat Track · corrodedSEAT TRACK CORRODED BS 693 RBL 9. REMOVED DAMAGED SEAT TRACK IAW AMM 53-00-49-000-801-803. INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-801.Dec 27, 2013 · N723EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2014011509751Seat Track · corrodedSEAT TRACK CORRODED AT BS 549. R & R SEAT TRACK IAW AMM 53-00-49-400-801.Dec 27, 2013 · N723EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2014013109827Bulkhead Web · corrodedLEFT 280 BULKHEAD WEB CORRODED. REMOVED CORROSION & FOUND AREA TO BE OUT OF LIMITS IAW SRM 53-11-10-201-003-A01. COMPLIED WITH EC/TC REO 670-53-11-594 AND GREO 670-53-11-594 REV.Dec 24, 2013 · N723EV · Cndair CL6002C10 · Fuselage Main, BulkheadSDR ASOA2014013109826Post · corrodedLEFT 280 WEB POST CORRODED AT BOTTOM. REMOVED CORROSION IAW SRM 51-21-06-001-01-A01. RESTORED FINISH IAW SRM 51-25-16-001-001.Dec 24, 2013 · N723EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2014013109825Post · corrodedRT 280 WEB POST CORRODED AT BOTTOM. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. RESTORED FINISH IAW SRM 51-42-06-001-001-A01, 51-42-10-001-001-A01, 51-21-16-001-001-A01 AND DWG CC670-34010.Dec 24, 2013 · N723EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2014013109824Floor Support · corrodedRT FLOOR SUPPORT CORRODED BS 280 - 319.7. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. 100 PERCENT MATERIAL LOSS AT 3 LOCATIONS IS BEYOND LIMITS OF SRM 53-00-00-101-001-A01. REMOVED FLOOR SUPPORT IAW SRM 51-40-11-001-001-A01 AND DWG SH670-32170. INSTALLDec 24, 2013 · N723EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2014013109823Track · dentedAFT BAGGAGE BAY FWD AND AFT DOOR TRACKS HAVE DENTS. REPLACED DOOR TRACKS IAW REO 670-53-62-0102. MAJOR REPAIR.Dec 24, 2013 · N723EV · Cndair CL6002C10 · Cargo/Baggage DoorsSDR ASOA2014013109822Doubler · chafedRIGHT ENGINE LOWER CORE COWL, INNER SKIN DOUBLE REPAIR HAS CHAFE DAMAGE. REMOVED DOUBLER ON RT LOWER COWL DOOR IAW SRM 51-42-06-001-001. COMPLIED WITH REPAIR OF THE FWD CORE COWL IAW REO 670-54-23-959. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW ASA SOPDec 24, 2013 · N723EV · Cndair CL6002C10 · Nacelle/Pylon, Plate/SkinSDR ASOA2014011509750Floorbeam · corrodedFLOORBEAM ANGLE AT FS 280 CORRODED. R & R FLOORBEAM ANGLE IAW DWG CC670-334010, REV H, SRM 51-42-15-001-001-A01, 51-42-21-001-001-A01, & 51-42-06-001-001-A01.Dec 24, 2013 · N723EV · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR ASOA2013123109733Floorbeam · corrodedBS 280 FLOORBEAM CORRODED. REMOVED AND INSTALLED NEW, DURING INCORPATION OF SB 670BA-53-041, PART A.Dec 24, 2013 · N723EV · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR ASOA2013123109732Floorbeam · corrodedFLOORBEAM ANGLE BS 280 CORRODED. R & R WITH A NEW ANGLE DURING INCORPORATION OF SB 670BA-53-041, PART A.Dec 24, 2013 · N723EV · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR ASOA2014013109821Doubler · chafedFUSELAGE SKIN DOUBLER AT STRINGER 27 BS 977 HAS CHAFE DAMAGE FROM CHANNEL ON PANEL 195DL/196DR AND SCREW INDENTIONS. REPAIRED IAW REO 670-53-00-290. MAJOR REPAIR.Dec 23, 2013 · N723EV · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR ASOA2014011509749Structure · crackedLEFT TRU BAY STRUCTURE CRACKED AT BS 193. COMPLIED WITH REO PL 670-53-11-509. MAJOR REPAIR.Dec 23, 2013 · N723EV · Cndair CL6002C10 · Fuselage Main, StructureSDR ASOA2013121309643Lens · discoloredEMERGENCY LIGHT LENS DISCOLORED. R & R LIGHT LENS IAW AMM 33-51-05.Dec 10, 2013 · N723EV · Cndair CL6002C10 · Emergency LightingSDR ASOA2012120702613Control Panel · malfunctionedAT 4000 FT, RUDDER IMMEDIATLEY WENT FULL LT, RUDDER TRIM ATTEMPTED TO TRIM BACK TO RT AND TRIM WENT FULL RT TRIM, TRIM CONTINUED TO MOVE UNCOMMANDED AND FINALLY STOPPED AT HALF RT RUDDER TRIM. AUTO PILOT WAS NOT ENGAGED. ACFT RETURNED TO DEPARTURE AFTER T/ODec 6, 2012 · N723EV · Cndair CL6002C10 · Rudder Tab Control SystemSDR ASOA2012102402397Lamp · burned outCEILING EMERGENCY LIGHT OUT AT 17ABCD. LAMPED IAW AMM 33-51-09.Oct 20, 2012 · N723EV · Cndair CL6002C10 · Emergency LightingSDR ASOA201201717Megaphone · inoperativeF/A MEGAPHONE INOPERATIVE. R & R F/A MEGAPHONE IAW AMM 25-61-14, REF IPC 25-25-61-14, ITEM 5, OPS TESTED GOOD.Jun 1, 2012 · N723EV · Cndair CL6002C10 · Emergency EquipmentSDR ASOA201102459Charger · failedEMERGENCY LIGHTS INOPERATIVE. FOUND BURNED OUT FUSE IN NR 1 ESPU BATTERY CHARGER. REMOVED NR1 ESPU BATTERY CHARGER IAW AMM 33-51-17-00-802. REMOVED NR 1 BATTERY CHARGER IAW AMM 33-51-17-00-802. INSTALLED NEW NR 1 ESPU BATTERY CHARGER REF AMM 33-51-17-400-80Dec 30, 2011 · N723EV · Cndair CL6002C10 · Emergency LightingSDR ASOA201102446Support · damagedDURING REMOVAL OF FUEL CAP FOR O-RING REPLACEMENT, DAMAGE TO THE LIGHTNING HOLE OCCURED. FABRICATED MOUNTING SUPPORT AND MOUNTING SUPPORT AFT IAW SRM 51-24-16-001-001-A01, 51-24-21-001-001-A01, 51-24-36-001-001-A01, AND DWS SH670-3967-5 AND SH670-39065-5. Dec 24, 2011 · N723EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA201102360Angle · corrodedSERVICE DOOR THRESHOLD MOUNTING BRACKET CORRODED. FABRICATED ANGLE AND INSTALLED IAW EO 700-53-0224.Dec 15, 2011 · N723EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA201102359Angle · corrodedCABIN SERVICE DOOR LOWER ANGLE CORRODED.Dec 15, 2011 · N723EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
Back to N723EV