N722EV

Service difficulty reports · 314

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 = 'N722EV' 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 ASOA201101356Seat Track · corrodedLEFT SIDEWALL SEAT TRACK CORRODED AT BS 785. REMOVED AND REPLACED IAW SRM 51-42-02-001-001-A01.Jul 20, 2011 · N722EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201101355Seat Track · corrodedLEFT SIDEWALL SEAT TRACK CORRODED AT FS 736. REPAIRED.Jul 20, 2011 · N722EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201101333Angle · corrodedCORROSION ON FLANGE OF LOWER SILL ANGLE. REMOVED AND DRILLED NEW MID ANGLE IAW SRM 51-41-02-001-001 AND 51-42-06-001-001. INSTALLED ANGLE IAW SRM 51-41-02-001-001-A01.Jul 14, 2011 · N722EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA201101395Firewall · crackedNR 1 SYS LT PYLON FIREWALL 2ND FROM AFT UPPER ACCESS HOLE ELONGATED (NR 1 SYS PRESSURE LINE). APPEARS TO BE CRACKED AT FWD SIDE. COMPLIED WITH STEPS 1-2 OF REO 670-54-51-018. COMPLIED WITH NDT IAW STEP 3 OF REO 670-4-51-018 NDTM PART 1, 51-20-006. NO INDICJul 11, 2011 · N722EV · Cndair CL6002C10 · Nacelle/Pylon, Bulkhead/FirewallSDR ASOA201101402Seat Track · corrodedLT SIDEWALL SEAT RAIL CORRODED AT FUS STA 785. REMOVED CORROSION FROM LT SIDE WALL SEAT RAIL AT FS 785 SEAT TRACK THICKNESS IS .355, REMOVED .015 REMAINING THICKNESS IS .340 AND IS WITHIN ALLOWABLE LIMITS IAW SRM 53-41-49. THIS IS A MINOR REPAIR. BLEND AREA Jul 8, 2011 · N722EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201101299Seat Track · corrodedRIGHT SIDEWALL SEAT TRACK CORRODED BS 785. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-00-49-000-801.Jul 8, 2011 · N722EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201101298Seat Track · corrodedRIGHT SIDEWALL SEAT TRACK CORRODED AT BS 708. REMOVED CORROSION, ORIGINAL THICKNESS .355, REMOVED .037 MATERIAL, REMAINING THICKNESS IS .318. FOUND OUT OF LIMITS IAW SRM 53-41-49. REMOVED SEAT TRACK AND INSTALLED NEW SEAT TRACK.Jul 8, 2011 · N722EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201101297Seat Track · corrodedLEFT SIDEWALL SEAT TRACK CORRODED AT BS 708. REMOVED CORROSION, ORIGINAL THICKNESS IS .355, REMOVED .030 MATERIAL , REMAINING THICKNESS IS .325, WITHIN LIMITS IAW SRM 53-41-49.Jul 8, 2011 · N722EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201101296Seat Track · corrodedLT SIDEWALL SEAT TRACK CORRODED AT BS 736. REMOVED CORROSION. FOUND WITHIN ALLOWABLE LIMITS IAW SRM 53-41-49.Jul 8, 2011 · N722EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201101295Seat Track · corrodedLEFT BS 752 SIDEWALL SEAT TRACK CORRODED. REMOVED CORROSION, THICKNESS IS .355, REMOVED .011, AND IS WITHIN ALLOWABLE LIMITS IAW SRM 53-41-49. PERFORMED LPI, TYPE 1, METHOD C ON BLENDED AREA IAW NDT PROCEDURE PT-1. NO CRACK NOTED. REPAIRED IAW SRM 53-41-4Jul 8, 2011 · N722EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201101294Seat Track · corrodedLEFT BS 813 SIDEWALL SEAT TRACK CORRODED. REMOVED CORROSION, THICKNESS IS .355, REMOVED .013 AND IS WITHIN ALLOWABLE LIMITS IAW SRM 53-41-49. PERFORMED LPI, TYPE 1, METHOD C ON BLENDED AREAS IAW NDT INSPECTION PROCEDURES PT-1. NO CRACK NOTED. REPAIRED IAW 6Jul 8, 2011 · N722EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201101293Seat Track · corrodedLEFT BS 785 SIDEWALL SEAT TRACK CORRODED. REMOVED CORROSION, THICKNESS IS .355, REMOVED .015 AND IS WITHIN ALLOWABLE LIMITS IAW SRM 53-41-49. PERFORMED LPI, TYPE 1, METHOD C ON BLEND AREA IAW NDT INSPECTION PROCEDURES PT-1. NO CRACK NOTED. REMOVED SEAT TRJul 8, 2011 · N722EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201101292Floorbeam · corrodedFS 280 FWD FLOORBEAM ANGLE CORRODED. ANGLE CORRODED BEYOND REPAIR, REMOVED ANGLE, DRILLED NEW ANGLE, AND INSTALLED IAW SRM 51-42-06-001-001-A01. MINOR REPAIR.Jul 7, 2011 · N722EV · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR ASOA201101291Stringer · corrodedCORROSION ON STRINGER 26 RIGHT, BETWEEN FRAMES 295.00-310.00. FOUND TO BE OUT OF LIMITS REF SRM 53-21-03-101-002-A01. REMOVED AND REPLACED STRINGER IAW SRM 51-42-06-001-001-A01. MAJOR REPAIR.Jul 6, 2011 · N722EV · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR ASOA201101401Floorbeam · corrodedCORROSION DAMAGE EXCEEDS GENERAL ALLOWABLE DAMAGE LIMITS OF SRM 53-00-00-101-001-A01, REMOVED FS 280 BEAM WL 72 IAW SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01, 51-42-21-001-001-A01, 51-42-22-001-001-A01. CUT CROSSBEAM IAW REO 670-53-11-047. NDI IAW REOJul 5, 2011 · N722EV · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR ASOA201101338Angle · corrodedBLENDED CORROSION IAW SRM 51-21-06-001-001-A01. REMOVED LOWER SILL AND UPPER ANGLE TO BE REPLACED IAW SRM 51-42-06-001-001-A01. PARTS DAMAGED BEYOND LIMITS IAW SRM. INSTALL NEW PARTS. INSTALLED NEW LOWER SILL AND UPPER ANGLE IAW SRM 51-40-11, 51-40-00 & Jul 5, 2011 · N722EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA201101310Stiffener · crackedPAX DOOR ASSIST MOTOR LOWER VERTICAL STIFFENER CRACKED APPROX .3750" LEFT IN RADIUS. REMOVED AND REPLACED CRACKED STIFFENER IAW SRM 51-42-06-001-001-A01.Jul 5, 2011 · N722EV · Cndair CL6002C10 · Passenger/Crew DoorsSDR ASOA201101272Drag Angle · crackedPAX DOOR AFT DRAG ANGLE CRACKED. DRAG ANGLE WAS REPAIRED IAW SRM 52-11-04-201-002-A06.Jul 5, 2011 · N722EV · Cndair CL6002C10 · Passenger/Crew DoorsSDR ASOA201101271Bulkhead · corrodedBULKHEAD AT FS 280.00 IS CORRODED. REMOVED CORROSION IAW SRM 53-11-10-201-003-A01. FOUND OUT OF LIMITS. REMOVED DAMAGED BULKEHEAD WEB IAW REO 670-53-11-594 01. PERFORMED ET IAW NDT PROCEDURE ET-2. NO INDICATIONS NOTED. FABRICATED NEW WEB AND SPLICE PLATJul 5, 2011 · N722EV · Cndair CL6002C10 · Fuselage Main, BulkheadSDR ASOA201101270Bulkhead · corrodedLT BULKHEAD AT FS 280.00 IS CORRODED. REMOVED CORROSION, A LONG WL 72.5 IAW SRM 53-11-10-201-003-A01. DAMAGE EXCEEDED LIMITS. REMOVED DAMAGED WEB IAW REO 670-53-11-594. PERFORMED ET INSPECTION IAW NDT PROCEDURE ET-2. NO INDICATIONS NOTED. FABRICATED WEJul 5, 2011 · N722EV · Cndair CL6002C10 · Fuselage Main, BulkheadSDR ASOA201101269Door · obstructedLEFT OVERWING EMERGENCY EXIT FAILED FUNCTIONAL TEST IAW AMM 52-21-00-991-805. TRASH FOUND ON LOCK PINS, CLEANED AND REINSTALLED DOOR, PERFORMED FUNCTIONAL TEST IAW AMM 52-21-00-720-801, TESTED GOOD.Jul 5, 2011 · N722EV · Cndair CL6002C10 · Emergency ExitsSDR ASOA201100189Sensor · out of adjustON CLIMBOUT GEAR DISAGREE MESSAGE WITH ASSOCIATED WOW INPUT AND NOSE STEER INOP, COMPLIED WITH QRH. LANDED W/O INCIDENT, TOUCHDOWN VREF 135+5 VSI +500 MINIMAL BRAKING WEIGHT ON TOUCHDOWN 64K ONLY NOSE WHEEL CYCLED. ACFT RETURNED TO DEPARTURE AFTER TAKE OFF -Jan 31, 2011 · N722EV · Cndair CL6002C10 · Landing Gear Position and WarningSDR ASOA201000777Bulb · inoperativeERMERGENCY LIGHT BULB INOP RT ESCAPE HATCH LOWER FWD. RELAMPED CABIN EMERGENCY LIGHT AT RT ESCAPE HATCH LOWER FWD BULB OPS CHECK GOOD IAW AMM 33-51-00.May 19, 2010 · N722EV · Cndair CL6002C10 · Emergency LightingSDR ASOA201000776Bulb · burned outLEFT ESCAPE HATCH FWD LOWER EMERGENCY LIGHT 3EA BULBS BURNED OUT. RELAMPED CABIN EMERGENCY LIGHT AT LT ESCAPE HATCH LOWER FWD 5EA BULBS OPS CHECK GOOD IAW AMM 33-51-00.May 19, 2010 · N722EV · Cndair CL6002C10 · Emergency LightingSDR ASOA201000487Step · crackedTOP A/S/D STEP BROKEN. REPLACED THE TOP ASD STEP IAW AMM 52-11-04, ITEM: 1, REPLACED THE TOP ASD STEP IAW AMM 52-11-04.Apr 3, 2010 · N722EV · Cndair CL6002C10 · Entrance StairsSDR ASOA201000289Flashlight · inoperativeF/O'S FLASHLIGHT INOP. REMOVED AND REPLACED F/O'S FLASHLIGHT IAW AMM 25-61-00.Feb 21, 2010 · N722EV · Cndair CL6002C10 · Emergency EquipmentSDR ASOA200900737Angle · crackedANGLE AT FS 280, LBL 26, WL 68-78 FOUND TO BE CRACKED ON LOWER EDGE (16052 6-28-09 AAR349 PG6). REMOVED OLD AND INSTALLED NEW ANGLE IAW SRM 51-42-06.Jul 1, 2009 · N722EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA200900712Seat Track · corrodedRT PAX COMP FLOOR SEAT RAIL HAS CORROSION FROM FS 450.00 TO FS 469.00 (13259 6-24-09 AAR363 PG102). BLENDED ON RT SEAT TRACK FROM FS 450.00 TO FS 469.00 TO DETERMINE SEVERITY OF CORROSION. CORROSION ON SEAT TRACK FOUND TO BE OUT OF LIMITS FOR BLENDING IAW SJun 25, 2009 · N722EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA200900699Sill · corrodedRT FLOOR SILL CORRODED AROUND NUT PLATE AT FS 282. BLENDED DISCREPANT AREA AT FS 282 ON RT FLOOR SILL, FOUND TO BE WITHIN SERVICEABLE LIMITS IAW SRM 53-00-01.Jun 23, 2009 · N722EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA200900698Support Angle · corrodedFLT DECK FLOOR SUPPORT ANGLE AT FS 280 CORRODED. REMOVED UNSERVICEABLE FLOOR SUPPORT ANGLE. LOCATED DRILLED AND PREPARED NEW SERVICEABLE ANGLE P/N CC670-33-292-13S FOR INSTALLATION IAW SRM 51-40-11. INSTALLED SERVICEABLE FLIGHT DECK FLOOR SUPPORT ANGLE P/N Jun 23, 2009 · N722EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA200900697Bulkhead · corrodedFS 280 BULKHEAD RT LWR WEB CORRODED. REMOVED FASTENERS AS REQUIRED. BLENDED WEB TO REMOVE SURFACE CORROSION. MAX DEPTH .005 INCH (.005" ALLOWED) IAW SRM 53-11-10-201-003 REPAIR A. OK TO RESTORE FINISH, APPLIED ALODINE PRIMER AND TOPCOAT TO RESTORE FINISH CJun 23, 2009 · N722EV · Cndair CL6002C10 · Fuselage Main, BulkheadSDR ASOA200900696Bulkhead Web · corrodedFS 280 BULKHEAD LT LWR WEB CORRODED. REMOVED FASTENERS AS REQUIRED. BLENDED WEB TO REMOVE SURFACE CORROSION. MAX DEPTH .003 (.005 INCH ALLOWED) IAW SRM 53-11-10-201-003 REPAIR "A". REMOVED EDGE DAMAGE 1 INCH IN LENGTH AT I/B WEB EDGE JUST ABOVE FLOOR LEVEJun 23, 2009 · N722EV · Cndair CL6002C10 · Fuselage Main, BulkheadSDR ASOA200900695Crossbeam · corrodedFS 280 FLOOR SUPPORT CROSSBEAM CORRODED. RECEIVED SERVICEABLE CROSSBEAM. FABRICATED AND INSTALLED CROSSBEAM SPLICES. C/W EO 700-53-0061.Jun 23, 2009 · N722EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA200900679Flashlight · inoperativeF/O'S FLASHLIGHT INOPERATIVE.Jun 19, 2009 · N722EV · Cndair CL6002C10 · Emergency EquipmentSDR ASOA200900592Light · inoperativeNR 2 AND NR 3 CABIN CEILING EMERGENCY FLOOD LIGHTS INOP.May 27, 2009 · N722EV · Cndair CL6002C10 · Emergency LightingSDR ASOA200900591Light · malfunctionedEMERGENCY LIGHTS COME ON SPONTANEOUSLY WITH WITCH IN "ARM POSITION . SEE PREVIOUS LIGHTING STRIKE WRITE-UPMay 27, 2009 · N722EV · Cndair CL6002C10 · Emergency LightingSDR ASOA200900513Megaphone · inoperativeFLIGHT ATTENDANT MEGA PHONE INOP.May 3, 2009 · N722EV · Cndair CL6002C10 · Emergency EquipmentSDR ASOA200801458Light · inoperativeEMERGENCY LIGHT JUST AFT OF SERVICE DOOR HAS SEVERAL INOP BULBS.Nov 6, 2008 · N722EV · Cndair CL6002C10 · Emergency LightingSDR TRAX200701889Charger · reads lowEMERGENCY BATTERY CHARGER NR 1 READING LOW VOLTAGE.Dec 8, 2007 · N722EV · Cndair CL6002C10 · Emergency LightingSDR TRAX200701890Battery · reads lowEMERGENCY BATTERY NR 3 AND NR 4 READING LOW VOLTAGE.Dec 8, 2007 · N722EV · Cndair CL6002C10 · Emergency LightingSDR TRAX200701888Light · inoperativeFOUND EXIT LIGHT AT 1 A + B IS OUT.Dec 8, 2007 · N722EV · Cndair CL6002C10 · Emergency LightingSDR TRAX200701887Light · inoperativeEXIT LIGHT AT 1A + B IS OUT.Dec 8, 2007 · N722EV · Cndair CL6002C10 · Emergency LightingSDR TRAX200701526Seat Track · corrodedRIGHT FLOOR SEAT TRACK FS 581.00 TO FS 677.00 HAS SURFACE CORROSION.Oct 18, 2007 · N722EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR TRAX200701525Seat Track · corrodedLEFT FLOOR SEAT TRACK FS 581.00 TO FS 677.00 HAS SURFACE CORROSION.Oct 18, 2007 · N722EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR TRAX200701524Seat Track · corrodedRIGHT FLOOR SEAT TRACK FS 485.00 TO FS 581.00 HAS SURFACE CORROSION.Oct 18, 2007 · N722EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR TRAX200701523Seat Track · corrodedLEFT FLOOR SEAT TRACK FS 485.00 TO FS 581.00 HAS SURFACE CORROSION.Oct 18, 2007 · N722EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR TRAX200701522Seat Track · corrodedLEFT FLOOR SEAT TRACK FS 374.00 TO 485.00 CORRODED AND BENT (MARKED).Oct 18, 2007 · N722EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR TRAX200701518Hinge Fitting · crackedLT MFS HINGE FITTING OUTBOARD AT WS 216.95 CRACKED. 10-29-07 R & R LT MFS FITTING IAW CRJ 700 SB 670-BA-57-010. REMOVED BUTTE DOORS FROM LT WING. BEGAN REMOVING HINGE FITTING IAW BOMBARDIER SB 70BA-57-010. INSTALLED LT WING MFS PCU PER CRJ 700 AMM 27-62-Oct 17, 2007 · N722EV · Cndair CL6002C10 · Wing Miscellaneous StructureSDR TRAX200701528Web · corrodedRIGHT AND LEFT 280 WEBS HAVE SIGNS OF SURFACE CORROSION JUST ABOVE 280 TRANSVERSE BEAM. REMOVED SURFACE CORROSION ON LT AND RT 280 WEBS PER CRJ700 SRM 53-11-10.Oct 17, 2007 · N722EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR TRAX200701520Seat Track · corrodedRBL 9 SEAT TRACK CORRODED AT FS 349.00.Oct 17, 2007 · N722EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
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