N920EV

Service difficulty reports · 300

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 = 'N920EV' 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 ASOA201701261112Structure · crackedAFT PRESSURE BULKHEAD ZEE MEMBER CRACKED AFT SIDE OF FS 621 BL 0, WL 109. REPAIRED ZEE MEMBER IAW REO 601R-53-61-1285 REV E.Jan 26, 2017 · N920EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2017012611111Bulkhead · crackedAFT PRESSURE BULKHEAD FS 621 NUMEROUS CRACKED AREAS. REPAIRED AFT PRESSURE BULKHEAD IAW REO 601R-53-61-1285 REV E, REO 601R-53-61-2155 REV A AND REO 601R-53-61-5910 REV --.Jan 26, 2017 · N920EV · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA201701261111Bulkhead · corrodedAFT PRESSURE BULKHEAD FS 621 NUMEROUS CRACKED AREAS. REPAIRED AFT PRESSURE BULKHEAD IAW REO 601R-53-61-1285 REV E, REO 601R-53-61-2155 REV A AND REO 601R-53-61-5910 REV --.Jan 26, 2017 · N920EV · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA2016080115153Door · bindingCANNOT OPEN SERVICE DOOR FROM OUTSIDE. OPS CHECKED SERVICE DOOR IAW AMM 52-40-00. NO DEFECTS NOTED.Jul 28, 2016 · N920EV · Cndair CL6002B19 · Service DoorsSDR ASOA2015091113737Sign · damagedLIGHTED EXIT SIGN ABOVE SERVICE DOOR DAMAGED. R & R SIGN IAW AMM 33-51-13. SYSTEM OPS CHECKED GOOD. NO FURTHER ACTION.Sep 11, 2015 · N920EV · Cndair CL6002B19 · Emergency LightingSDR ASOA2014122911994Isolator · brokenBS 621 BULKHEAD HAS 6 BROKEN ISOLATORS. REMOVED 6 BROKEN ISOLATORS AND REPLACED WITH 6 NEW SERVICEABLE ISOLATORS, PN:SL2337-3 IAW SRM 51-42-06.Dec 15, 2014 · N920EV · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA2014122911993Skin · chafedLOWER WING PLANK, T/E IS CHAFED AT RBL 45 APPROXIMATELY 1.5" X 0.9" X 0.040" DEEP. COMPLIED WITH EC/TC REO 601R-57-21-880 IAW REO 601R-57-21-880, REV C.Dec 11, 2014 · N920EV · Cndair CL6002B19 · Wing, Plate/SkinSDR ASOA2014122911992Floor Support · corrodedCABIN FLOOR SUPPORT AT FS 409-115, RBL 45. CORRODED BEYOND REPAIRABLE LIMITS OF REO:601R-53-00-530. ADDITION REPAIR SCHEME REQUIRED. COMPLIED WITH REO 601R-53-31-836, REV. REO 601R-53-31-836, REV HAS BEEN ACCOMPLISHED AND ALL STEPS HAVE BEEN DOCUMENTED ADec 11, 2014 · N920EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2014122911991Skin · chafedLOWER WING PLANK, T/E IS CHAFED AT LBL 45 APPROXIMATELY 1.2" X 0.9" X 0.040" DEEP. COMPLIED WITH EC/TC REO 601R-57-21-880 IAW REO 601R-57-21-880, REV C.Dec 11, 2014 · N920EV · Cndair CL6002B19 · Wing, Plate/SkinSDR ASOA2014122911990Skin · crackedLOWER WING PLANK RT, BOOST PUMP, LANDING FOR PANEL 610CB HAS MULTIPLE INDICATIONS NOTED AROUND ENTIRE CIRCUMFERENCE GREATER THAN 50 PERCENT FSH. FAILED NDT INSP. COMPLIED WITH ST EA 32-2014-225. EA 32-2014-225 HAS BEEN ACCOMPLISHED AND ALL STEPS HAVE BEEN DODec 9, 2014 · N920EV · Cndair CL6002B19 · Wing, Plate/SkinSDR ASOA2014122911989Skin · crackedONE INDICATION NOTED ON LOWER WING PLANK LANDING FOR PANEL 550CB AT OTBD AFT SIDE APPROX .100" X .100" X 50 PERCENT FSH. FAILED NDT INSP. COMPLIED WITH EC/TC EO 600-57-81 C/W IAW REO 601R-57-21-030, REV L.Dec 8, 2014 · N920EV · Cndair CL6002B19 · Wing, Plate/SkinSDR ASOA2014122911988Stiffener · crackedBS 409+128 BL 0, RT SIDE VERT POST HAS AN INDICATION NOTED IN THE AFT FLANGE RADIUS AT WL 69 APPROXIMATELY .250" LONG BY 50 PERCENT FSH. FAILED NDT INSPECTION. REMOVED POST AT FS 409-128, BL 0 IAW SRM 51-42-06 AND SRM 51-42-21. INSTALLED 15-E RIVETS AT TOP Dec 7, 2014 · N920EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2014122911987Stiffener · crackedBS 409+128 RBL 18 INBD AND OTBD VERT POSTS HAVE INDICATIONS NOTED IN THE AFT FLANGE RADIUS AT WL 69 APPROXIMATELY .250" LONG BY 50 PERCENT FSH. BOTH FAILED NDT INSPECTION. REMOVED VERTICAL STIFFNER/POST AT FS 409.00+128 RBL 18.0 IAW SRM 51-42-06. LOCATED, DDec 7, 2014 · N920EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2014122611983Frame · crackedRT INBD AFT DRAIN HOLE AT BOOST PUMP HAS MULTIPLE INDICATIONS NOTED ON LOWER SURFACE AROUND LARGE HOLE WHERE PAINT IS REMOVED APPROX 60 PERCENT FSH. FAILED NDT INSP. COMPLIED WITH IAW STS EA 32-2014-220, REV A, EA 32-2014-220, REV A HAS BEEN ACCOMPLISHED ANDDec 5, 2014 · N920EV · Cndair CL6002B19 · Wing SparSDR ASOA2014122611982Access Panel · corrodedLEFT LOWER WING PLANK FUEL TANK ACCESS DOOR 540BB CUTOUT AT WS 54.897 HAS FRETTING CORROSION AT INBD AND OTBD ENDS AND AFT EDGE. CENTER INBD DAMAGE MEASURES APPROX 10.3" LONG X 0.11" WIDE AND 0.003" DEEP, OTBD DAMAGE MEASURES APPROX 9.3", L X 0.21" W X 0.004"Dec 3, 2014 · N920EV · Cndair CL6002B19 · Wing, Plate/SkinSDR ASOA2014122611981Access Panel · corrodedRIGHT LOWER WING PLANK FUEL TANK ACCESS DOOR 640BB CUT-OUT AT WS 54.897 HAS FRETTING CORROSION AT INBD & OTBD ENDS. INBD DAMAGE MEASURES APPROX 3.1" LONG X 0.20" WIDE X 0.003" DEEP. OTBD DAMAGE MEASURES APPROX 3.6" LONG X 0.15" WIDE X 0.002" DEEP, EXTENDS INTDec 3, 2014 · N920EV · Cndair CL6002B19 · Wing, Plate/SkinSDR ASOA2014122611980Frame · corrodedCARGO BAY FRAME BS 605 BETWEEN STRINGERS 22L - 26R CORRODED. FOUND TO BE OUT OF LIMITS IAW TEMP REV 53-27, SRM 53-00-00-01. REMOVED AND REPLACED THE FRAME IAW SRM 51-40-11, SRM 51-42-06, SRM 51-42-21, SRM 51-77-00-00, AND TR 51-32.Dec 2, 2014 · N920EV · Cndair CL6002B19 · Fuselage Main, FrameSDR ASOA2014122611979Floor Support · corrodedCARGO BAY BETWEEN BS 574 - 589 RBL 45 FLOOR SUPPORT CORRODED. REPAIRED IAW REO 601R-54-00-526 01 AND GREO 601R-53-00-520, REV.Dec 2, 2014 · N920EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2014122611978Floor Support · corrodedBS 409+98 - 409+115 RBL 45, FLOOR SUPPORT CORRODED. BLENDED IAW REO 601R-53-00-530 AND FOUND TO BE OUT OF LIMITS. REPAIRED THE FLOOR SUPPORT IAW REO 601R-53-00-530, REV A.Dec 2, 2014 · N920EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2014122611977Attach Fitting · corrodedBS 317 RBL 9 GALLEY ATTACH FITTING CORRODED. REMOVED AND REPLACED THE FITTING IAW SRM 51-42-06, 51-42-13, AND EA 32-2014-222.Dec 2, 2014 · N920EV · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR ASOA2014122611976Angle · corrodedBS 349 RBL 45, SERVICE DOOR SILL ANGLE CORRODED. REMOVED AND REPLACED THE ANGLE IAW SRM 51-42-06 AND 51-42-21.Dec 2, 2014 · N920EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2014122611975Floorbeam · corrodedBS 349 RBL 45, FLOORBEAM CORRODED. REPAIRED IAW SRM 51-42-06 AND 51-42-21.Dec 2, 2014 · N920EV · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA2014122611974Isolator · brokenIN CARGO BAY REAR PRESSURE BULKHEAD HAS BROKEN ISOLATORS. REMOVED AND REPLACED IAW SRM 51-42-06.Dec 2, 2014 · N920EV · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA2014122611973Floorbeam · crackedBS 280 LBL 11. FLOORBEAM LOWER AREA IS CRACKED. REPAIRED IAW REO 601R-53-11-171.Dec 2, 2014 · N920EV · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA2014122611972Floorbeam · crackedBS 280 RBL 11. FLOORBEAM CRACKED. REPAIRED IAW REO 601R-53-11-171.Dec 2, 2014 · N920EV · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA2014122611971Floorbeam · crackedBS 280 RBL 9 FLOORBEAM ANGLE CRACKED. R & R IAW SRM 51-42-06.Dec 2, 2014 · N920EV · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA2014122611970Floorbeam · crackedBS 280 LBL 9 FLOORBEAM ANGLE CRACKED. R & R IAW SRM 51-42-06.Dec 2, 2014 · N920EV · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA2014122611969Intercostal · crackedBS 484 INTERCOSTAL REPAIR ANGLE AT RBL 36 IS CRACKED . REPAIRED IAW REO 601R-53-41-1860 REV.Dec 2, 2014 · N920EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2014122411968Floorbeam · corrodedCARGO BAY BS 559+112 BETWEEN RBL 27 - 45 FLOORBEAM TOP PLATE CORRODED. REMOVED FLOORBEAM TOP TEE IAW SRM 51-42-06 AND INSTALLED IAW SRM 51-42-06 AND 51-40-11.Dec 2, 2014 · N920EV · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA2014122411967Floor Support · corrodedBS 559+45 - 559+65 LBL 45 FLOOR SUPPORT CORRODED. BLENDED AND REPAIRED IAW REO 601R-53-00-526 AND GREO 601R-53-00-526, REV.Dec 2, 2014 · N920EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2014122411966Floor Support · corrodedBS 559+16 RBL 45 FLOOR SUPPORT CORRODED. BLENDED IAW REO 601R-53-00-526 01. REPAIRED IAW REO 601R-53-00-526-01 AND GREO 601R-53-00-526, REV.Dec 2, 2014 · N920EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2014122411965Floor Support · corrodedBS 559+16 LBL 45 FLOOR SUPPORT CORRODED. FOUND TO BE WITHIN LIMITS IAW REO 601R-53-00-526. REPAIRED IAW REO 601R-53-00-526 AND GREO 601R-53-00-526, REV.Dec 2, 2014 · N920EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2014122411964Seat Track · corrodedBS 559 - 559+85 SEAT TRACK CORRODED. REMOVED AND REPLACED IAW GREO:601R-53-00-485.Dec 2, 2014 · N920EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2014122411963Seat Track · corrodedBS 559 - 559+85. SEAT TRACK CORRODED. REMOVED AND REPLACED IAW GREO:601R-53-00-485.Dec 2, 2014 · N920EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2014122411962Web · corrodedBS 559 LBL 45 PRESSURE WEB CORRODED. REPAIRED IAW REO 601R-53-41-666.Dec 2, 2014 · N920EV · Cndair CL6002B19 · Fuselage Main, StructureSDR ASOA2014122411961Strap · corrodedBS 559 BETWEEN RBL 27 - 45 FLOORBEAM STRAP CORRODED. REMOVED AND REPLACED IAW SRM 51-42-06 AND 51-42-13.Dec 2, 2014 · N920EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2014122411960Strap · corrodedBS 559 BETWEEN LBL 27 - 45 FLOORBEAM STRAP CORRODED. REMOVED AND REPLACED THE STRAP IAW SRM 51-42-06.Dec 2, 2014 · N920EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2014122411959Seat Track · corrodedBS 409+128 - 559 SEAT TRACK CORRODED. R & R IAW GREO 601R-53-00-485.Dec 2, 2014 · N920EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2014122411958Seat Track · corrodedBS 409+128 - 559 SEAT TRACK CORRODED. R & R IAW GREO 601R-53-00-485.Dec 2, 2014 · N920EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2014122411957Seat Track · corrodedBS 398 - 409+128 RBL 9 SEAT TRACK CORRODED. R & R IAW GREO 601R-53-00-485.Dec 2, 2014 · N920EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2014122411956Seat Track · corrodedBS 398 - 409+128 LBL 9, SEAT TRACK CORRODED. R & R IAW GREO 601R-53-00-485.Dec 2, 2014 · N920EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2014122411955Seat Track · corrodedBS 364 - 398, SEAT TRACK CORRODED. R & R IAW GREO 601R-53-00-485 REV A.Dec 2, 2014 · N920EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2014122411954Seat Track · corrodedBS 364 - 398, LT SEAT TRACK HAS CORROSION. R & R, FABRICATED A NEW SEAT TRACK IAW GREO 601R-53-00-485.Dec 2, 2014 · N920EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2014122411953Angle · corrodedIN PASSENGER COMPARTMENT, UNDER FLOORBOARD 232CRF AT BS 310 RBL 45, THE SERVICE DOOR SILL ANGLE INNER ATTACHMENT PLATE HAS PITTING CORROSION. REMOVED CORRODED INNER ATTACHMENT ANGLE FROM FS 310.00 ON RBL 45.00. FIT, DRILLED AND INSTALLED NEW ATTACHMENT ANGLE,Dec 2, 2014 · N920EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2014122411952Angle · crackedBS 625 OBLIQUE ANGLE CRACKED. R & R THE ANGLE IAW SRM TASK 51-42-06.Nov 30, 2014 · N920EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2014091811258Wire · brokenLIGHTED FLOOR LEVEL EXIT SIGN AT PAX DOOR ENTRANCE INOPERATIVE. R & R WIRE SPLICE CONNECTOR PLUG IAW SRM 20-17-31. SYSTEM OPS CHECKED GOOD. NO FURTHER ACTION.Sep 14, 2014 · N920EV · Cndair CL6002B19 · Light System WiringSDR ASOA2013072408771Lens · failedROW 7 A/B EMERGENCY LIGHT COVER ON FLOOR CAME APART. SECURED COVER IAW AMM 33-51-001.Jul 23, 2013 · N920EV · Cndair CL6002B19 · Emergency LightingSDR ASOA2013062808532Lamp · burned outNR 1 CEILING EMERGENCY LIGHT INOPERATIVE. R & R LAMP IN NR 1 CEILING EMERGENCY LIGHT IAW AMM 33-51-16. OPS CHECKED GOOD.Jun 26, 2013 · N920EV · Cndair CL6002B19 · Emergency LightingSDR ASOA2012111602477Battery Pack · inoperativeEMERGENCY BATTERY PACK 3 INOPERATIVE. R & R EMERGENCY BATTERY PACK NR 3 IAW AMM 33-51-04. OPS CHECKED GOOD, ACFT OK FOR SERVICE.Nov 12, 2012 · N920EV · Cndair CL6002B19 · Emergency LightingSDR ASOA2012111302462Glowstrip · unserviceableLT AFT PHOTOLUMINESCENT FLOOR TRACK HAS A SECTION OF GREY TRACK BASE, BROKEN AND MISSING. REPLACED BROKEN FLOOR TRACK SECTION WITH NEW GREY TRACK BASE PIECE IAW AMM 33-51-01-400-807.Nov 8, 2012 · N920EV · Cndair CL6002B19 · Emergency Equipment
Back to N920EV