N907EV

Service difficulty reports · 161

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 = 'N907EV' 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 ASOA201000755Support Bracket · crackedSUPPORT BRACKET BETWEEN F.S. 409.00+48 F.S. 409.00+64 AND BETWEEN LBL 9 AND RBL 9 IS CRACKED. REMOVED THE CRACKED SUPPORT BRACKET. LOCATED A NEW SUPPORT BRACKET AND INSTALLED THE NEW SUPPORT BRACKET IAW THE SRM 51-40-11, 51-41-02 AND 51-42-06.May 16, 2010 · N907EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201000786Placard · tornPAX DOOR EXIT PLACARD TORN. REMOVED TORN "EXIT" PLACARD IAW AMM TASK 11-30-00-000-801 & INSTALLED NEW PLACARD S1574-18 TO PAX DOOR STEP IAW AMM TASK 11-30-00-400-801.May 15, 2010 · N907EV · Cndair CL6002B19 · Placards and MarkingsSDR ASOA201000753Placard · fadedCREW ESCAPE HATCH OPEN, CLOSED AND EMERGENCY EXIT EXTERIOR PLACARDS ARE FADED. APPLIED OPEN, CLOSED, EMERGENCY EXIT SILKSCREENS ON CREW ESCAPE HATCH IAW MM 11-10-03-400-801.May 15, 2010 · N907EV · Cndair CL6002B19 · Placards and MarkingsSDR ASOA201000752Bulkhead · crackedPARKING BRAKE CABLE HOLE AT BS 202.75 BULKHEAD APPREARS TO BE CRACKED. PERFORMED EDDY CURRENT INSPECTION OF BULKHEAD AROUND BRAKE CABLE HOLE IAW NDTM 51-20-06. NO INDICATIONS NOTED AT THIS TIME.May 15, 2010 · N907EV · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA201000745Support Beam · crackedFOUND CARGO DOOR SUPPORT BEAM AFT LOWER ANGLE HAS A CRACK IN RADIUS APPROX .5" IN LENGTH. REMOVED ANGLE IAW SRM 51-42-21. REINSTALL ANGLE AFTER REAR PRESSURE BULKHEAD REPAIR HAS BEEN COMPLETED4. INSTALLED NEW ANGLE ON CARGO DOOR SUPPORT BEAM AFT LOWER IAW SRMay 14, 2010 · N907EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201000744Bulkhead · crackedFOUND REAR PRESSURE BULKHEAD WEB HAS INDICATION NOTED APPROX .3" IN LENGTH 50 PERCENT FSH AT LBL 27.50, WL 130 LOCATED TOP OF AFT CARGO DOOR TRACK. FAILED NDT INSPECTION. COMPLIED WITH EC/TC REO 601R-53-61-1541 AND MET ALL THE REQUIREMENTS OF REO 601R-53-61-May 14, 2010 · N907EV · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA201000742Stringer · crackedFOUND VISUAL EVIDENCE OF CRACK RADIATING FROM RIVET AT FS 718.00 UPPER SIDE OF STRINGER 10 LT CORNER OF STR 10 LT AND FS 718 (MARKED WITH YELLOW TAPE). PERFORMED EDDY CURRENT INSP ON NOTED AREA IAW NDTM 51-20-06. NO INDICATIONS NOTED (REMOVED YELLOW TAPE).May 14, 2010 · N907EV · Cndair CL6002B19 · Fuselage Main, Longeron/StringerSDR ASOA201000741Post · crackedFOUND FS 409.0+128 VERTICAL POST LBL 18.0 OTBD SIDE HAS INDICATION NOTED APPROX .3" IN LENGTH 80 PERCENT FSH AT WL 69.0 AFT FLANGE RADIUS. FAILED NDT INSP. REMOVED POST AT FS 409.0+128 LBL 18.00 IAW SRM 51-42-06. LOCATED AND DRILLED NEW OTBD POST TO INBD POSMay 14, 2010 · N907EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201000740Post · crackedJOB 8764825 /OPERATION 99. FOUND FS 409.0+128 VERTICAL POST BL 0.0 LT SIDE HAS INDICATION NOTED APPROX .3" IN LENGTH 80 PERCENT FSH AT WL 69.0 AFT FLANGE RADIUS. FAILED NDT INSPECTION. REMOVED VERTICAL POST COMMON TO FS 409+128 BL0 IAW 51-42-06. DRILLED UP May 14, 2010 · N907EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201000739Post · crackedFOUND FS 409.0+128 VERTICAL POST RBL 18.0 OTBD SIDE HAS INDICATION NOTED APPROX .3" IN LENGTH 60 PERCENT FSH AT WL 69.0 AFT FLANGE RADIUS. FAILED NDT INSP. REMOVED ADEL CLAMPS TO ACCESS POST IAW THE SRM 51-41-02. REMOVED THE POST IAW THE SRM 51-42-06. INSMay 14, 2010 · N907EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201000738Bulkhead · crackedFOUND FS 559 BULKHEAD WEB RT SIDE HAS INDICATION NOTED APPROX .2" IN LENGTH 60 PERCENT FSH OTBD OF RBL 9.0, WL 58.70. FAILED NDT INSPECTION. C/W ECTC REO 601R-53-41-260 IAW REO 601R-53-41-260 REV D.May 14, 2010 · N907EV · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA201000670Selector Valve · inoperativeGEAR DISAGREE NOSE GEAR UNSAFE, C/W QRH, MANUAL EXTENSION SUCCESSFUL (EMERGENCY DECLARED -- EQUIPMENT REQUESTED TO BE STANDING BY). R & R NLG SELECTOR VLV IAW CRJ 200 32-33-10 LEAK CK OF HYD SYS AND FUNCTIONAL TEST OF THE EXTENTION AND RETRACTION SYS, GOOD,May 1, 2010 · N907EV · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR ASOA201000316Bulb · inoperativeRT WING AFT EXTERIOR EMERGENCY LIGHT INOP. R & R BULB IAW AMM 33-51-21. OP CKS GOOD. R & R BULB IAW AMM 33-51-21 OP CKS GOOD.Feb 25, 2010 · N907EV · Cndair CL6002B19 · Emergency LightingSDR ASOA200901138Light · inoperativeEMERGENCY EXIT LIGHT INOP ON RT SIDE OF FUSELAGE.Oct 15, 2009 · N907EV · Cndair CL6002B19 · Emergency LightingSDR ASOA200801551Light · inoperativeRT OVERWING FWD EMERGENCY LIGHT IS INOP.Nov 22, 2008 · N907EV · Cndair CL6002B19 · Emergency LightingSDR TRAX200800712Battery Pack · inoperativeBOTH L/R AFT EXTERIOR EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED NR 4 BATTERY PACK IAW AMM 33-51-04-400-801 OPS CK GOOD. (B)May 30, 2008 · N907EV · Cndair CL6002B19 · Emergency LightingSDR TRAX200800671Fitting · crackedJOB 8764811 OPERATION 252 FS 280 CLIP AT LBL 9.0 OUTBRD IS CRACKED. REMOVED CRACKED FS 280.0 CLIP AT OUTBOARD LBL 9 AND INSTALLED NEW SERVICEABLE CLIP IAW CRJ 200 SRM 51-42-13 AND 51-42-21. [SDR CLOSED](B)May 19, 2008 · N907EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR TRAX200800658Floorbeam · crackedFS 621 RT SIDE FLOORBEAM ANGLE IS CRACKED AT RBL 40. REPAIRED PREVIOUS REPAIR AT FS 621 RT. LOCATED AND DRILLED NEW ANGLE AND REPAIR ANGLE IAW SRM 51-40-11. INSTALLED ANGLES IAW REO 601R-53-61-117 REV C. LEAK CHECK DUE. PERFORMED LEAK CHECK OF THE RT 621 May 18, 2008 · N907EV · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR TRAX200800655Floorbeam · crackedRT SIDE FS 464 FLOOR SUPPORT INTERCOSTAL HAS A CRACKED FLANGE ON THE I/B SIDE OF RBL 36 AND A CRACKED ATTACH ANGLE ON THE O/B SIDE OF RBL 27. DISCONNECTED MOUNT BOLTS ON CABLE GUIDE IAW 51-41-04. REPAIRED RT SIDE FS 484 INTERCOSTAL I/B OF RBL 36 AND O/B SIDEMay 18, 2008 · N907EV · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR TRAX200800657Floor Support · crackedLT SIDE FS 484 FLOOR SUPPORT INTERCOSTAL HAS A CRACKED FLANGE ON THE I/B SIDE OF LBL 36 AND A CRACK ATTACH ANGLE ON THE O/B SIDE OF LBL 27. DISCONNECTED MOUNT BOLTS ON CABLE GUIDE IAW 51-41-04. REPAIRED LT FS 484 LBL 36 I/B SIDE AND O/B SIDE OF LBL 27 IAW B/May 18, 2008 · N907EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR TRAX200800651Handle · crackedPAX DOOR EXTERNAL HANDLE IS CRACKED. SB 601R-51-119 REV A, DOORS, PASSENGER DOOR, REPLACEMENT OF THE OUTER HANDLE INCORPORATED. PAINTED PAX DOOR HANDLE IAW 51-25-01.May 16, 2008 · N907EV · Cndair CL6002B19 · Passenger/Crew DoorsSDR TRAX200800650Placard · unserviceableOPERATION 145 EXIT PLACARD ON PAX DOOR STEP 832BT IS UNSERVICEABLE. REMOVED AND INSTALLED NEW SERVICEABLE EXIT PLACARD ON PAX DOOR STEP 832BT IAW AMM 11-30-00-400-801.May 16, 2008 · N907EV · Cndair CL6002B19 · Placards and MarkingsSDR TRAX200800681Hinge · crackedCREW ESCAPE HATCH RT HINGE ARM IS CRACKED. REPLACED CREW ESCAPE HATCH RT HINGE ARM IAW CRJ 200 AMM 52-22-00-820-804, STEPS 3 B1, E. REQUIRES INSTALL, FIT AND CLEARANCE CHECK. FIT AND CLEARANCE CHECK OF CREW ESCAPE HATCH IAW CRJ 200 AMM 52-22-00-220-802. CRMay 11, 2008 · N907EV · Cndair CL6002B19 · Emergency ExitsSDR TRAX200800620Floorbeam · crackedFS 280 FLOOR SUPPORT STRUCTURE IS CRACKED O/B OF LBL 9 AT MLG MANUAL RELEASE PULLEY BRACKET. CUT AWAY CRACKED SECTION OF FLOOR ANGLE IAW REO 601R-53-11-138. COMPLIED WITH REO 601R-53-11-138. PERFORMED LPI OF FS 280 ANGLE LBL 9 REPAIR IAW NDTM 51-20-08. NO INMay 11, 2008 · N907EV · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR TRAX200800619Floorbeam · crackedFS 280 CLIP ON I/B SIDE OF RBL 9 IS CRACKED. REMOVED DAMAGED/CRACKED CLIP. INSTALLED NEW CLIP P/N 601R31113-58 IAW SRM 51-42-21.May 11, 2008 · N907EV · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR TRAX200800140Light · inoperativeTWO EXTERIOR EMERGENCY LIGHTS INOP ON RIGHT SIDE OF A/C.Jan 27, 2008 · N907EV · Cndair CL6002B19 · Emergency LightingSDR TRAX200701949Pin · corrodedLT GEAR SIDE STAY PIN CORRODED.Dec 16, 2007 · N907EV · Cndair CL6002B19 · Main Landing GearSDR TRAX200701948Bulkhead · crackedREAR PRESSURE BULKHEAD CRACK UNDER LINEAR FITTING OF CARGO DOOR SURROUNDING STRUCTURE, REO 601R-53-61-1230 TO BE C/OUT.Dec 16, 2007 · N907EV · Cndair CL6002B19 · Fuselage Main, BulkheadSDR TRAX200701774Anchor Fitting · crackedASD FWD ANCHOR FITTING CRACKED. FLT 4673 DEL 206 MINS.Nov 24, 2007 · N907EV · Cndair CL6002B19 · Passenger/Crew DoorsSDR TRAX200701608Flap · malfunctionedFLAPS FAIL CAUTION MESSAGE DURING CRUISE. THE FLAPS WERE AT 0 DEGREES. THERE WERE NO CHANGES ON THE ON THE FLAP SELECTOR. A NO FLAP APPROACH AND LANDING WERE DONE. REPEAT WRITE-UP. TOWER DECLARED EMERGENCY. EMERGENCY EQUIPMENT ON STANDBY.Oct 28, 2007 · N907EV · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR TRAX200701551Detection Sys · faultedFLAP FAIL CAUTION MSG AN DESCENT WITH FLAPS SET TO ZERO. FOUND SKEW DETECTION UNIT AT FAULT. EMERGENCY EQUIPMENT ROLLED AS A PRECAUTION. FLT 9970 DEL 370 MINS. NC FLTS 4583, 4652 CX. SKEW DETECTION SYSTEM.Oct 21, 2007 · N907EV · Cndair CL6002B19 · Trailing Flap Position Indicating SystemSDR TRAX200701191Flashlight · inoperativeCAPT'S FLASHLIGHT INOP (DIM).Aug 15, 2007 · N907EV · Cndair CL6002B19 · Emergency EquipmentSDR TRAX200700969Power Lever · stuckON DEPARTURE THE LEFT THRUST LEVER WAS STUCK AT TAKEOFF POWER AND WOULD NOT COME BACK. THE N1 WAS SET AT T/O POWER FOR ABOUT 25 MINUTES. AFTER APPROX 20 MINUTES, GOT IT TO COME BACK TO CRUISE POWER. EMERGENCY DECLARED. FLT 4534 DEL 20 MINS.Jul 7, 2007 · N907EV · Cndair CL6002B19 · Power LeverSDR TRAX200700800Flap System · malfunctionedFLAPS FAIL ZERO POSITON IN FLT 30000 FT, EMERGENCY DECLARED, FLT 4338 DEL 37 MINS. [07-06-07] INSPECTED FLAPS, INTERROGATED FECU & RESET SYSTEM. RESET OK, C/W EO 600-27-0054 A/C OK FOR SERVICE. MOVED TO MCO #044318, PRIORITY 1 REQUIRE C/W OF EO 600-27-0054 WJun 5, 2007 · N907EV · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR TRAX200601137Beam · crackedBOX BEAM CRACKED AT UPPER CENTER LOCATION. PERFORMED EDDY CURRENT INSPECTION OF UPPER BOX BEAM JUST FWD OF FIRE LOOP STAND OFF CLIP PER MTC REQUEST IAW CRJ 200 NDTM PART 1. 51-20-06. BOX BEAM IS CRACKED AT UPPER CENTER LOCATION. REMOVED UPPER FIRE BOTTLDec 20, 2006 · N907EV · Cndair CL6002B19 · Fuselage Main, StructureSDR TRAX200601007Inverter · inoperativeFWD EMERGENCY LIGHT LUMINESCENT INVERTER INOP.Nov 9, 2006 · N907EV · Cndair CL6002B19 · Emergency LightingSDR TRAX200600951Handle · crackedAVIONIC DOOR HANDLE IS CRACKED AROUND BOSS. REMOVED AND REPLACED AVIONICS DOOR HANDLE IAW CRJ200 AMM 52-42-00 AND SRM 51-42-06 (CLOSED 11/06/06)Oct 27, 2006 · N907EV · Cndair CL6002B19 · Electrical/Electronic Compartment DoorsSDR TRAX200600953Handle · corrodedCREW OVHD ESCAPE HATCH OUTER HANDLE SHAFT IS VERY CORRODED. REMOVED AND REPLACED HANDLE ASSY ON OVHD CREW HATCH IAW CRJ 200 SRM 51 42 06 RIG AND OPS CHECK C/W SATISFACTORY (CLOSED 11/03/06)Oct 26, 2006 · N907EV · Cndair CL6002B19 · Emergency ExitsSDR TRAX200600945Attach Fitting · crackedLEFT I/B FUSELAGE STA 280 CLIP CRACKED.Oct 26, 2006 · N907EV · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR TRAX200600932Light · damagedEMERGENCY LIGHT ON F/A STATION IS DAMAGED. REMOVED AND REPLACED EMERGENCY LIGHT ON F/A STATION IAW CRJ200 33-50-00.WPW15097. (CLOSED 11/01/06)Oct 25, 2006 · N907EV · Cndair CL6002B19 · Emergency LightingSDR TRAX200600464Light · inoperativeFWD FLOOR EMERGENCY LT TRACK LIGHT INOP.Jul 5, 2006 · N907EV · Cndair CL6002B19 · Emergency LightingSDR TRAX200600137Step · crackedFOUND CRACK UNDER TOP STEP ON ASD AFT SIDE.Apr 25, 2006 · N907EV · Cndair CL6002B19 · Entrance StairsSDR ASOA06246Carbon Seal · deterioratedDURING CLIMB OUT, AT APPROX 28,000 FT THE CREW NOTED THE RT ENGINE OIL PRESSURE DROPPED BELOW 25 PSI. THE QRH WAS COMPLIED WITH AND THE CREW BROUGHT THE RT ENGINE BACK TO IDLE. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED, WHERE A SINGLE LANDING WAS PFeb 27, 2006 · N907EV · Cndair CL6002B19 · Accessory GearboxesSDR ASOA06241Lamp · burned outDURING A GROUND INSPECTION, THE EXTERNAL RT SIDE EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE EXTERNAL RT SIDE EMERGENCY LIGHT ASSY. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)Feb 25, 2006 · N907EV · Cndair CL6002B19 · Emergency LightingSDR ASOA06123Handle · crackedDURING A HANGAR INSPECTION IN MCN, THE PASSENGER DOOR OUTER HANDLE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR OUTER HANDLE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)Jan 25, 2006 · N907EV · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA051020Warning Light · illuminatedDURING CRUISE FROM GRR-ATL, THE CREW RECEIVED A RIGHT ENGINE THRUST REVERSER DEPLOY LIGHT. THE QRH WAS COMPLIED WITH AND THE CREW DECLARED AN EMERGENCY. THE AIRCRAFT DIVERTED INTO FWA WHERE IT LANDED SAFELY. MAINTENANCE DEFERRED THE RIGHT THRUST REVERSER IANov 25, 2005 · N907EV · Cndair CL6002B19 · Engine Thrust ReverserSDR ASOA05897Relay · malfunctionedDURING A GROUND INSPECTION IN RDU, THE EMERGENCY LIGHTS REMAINED ON WITH AN ESS AC BUSS CAUTION MESSAGE. MAINTENANCE REMOVED AND REPLACED THE K1XD RELAY. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)Oct 24, 2005 · N907EV · Cndair CL6002B19 · Light System WiringSDR ASOA05772Lamp · inoperativeDURING AN OVERNIGHT INSPECTION IN VPS, THE OVERHEAD EMERGENCY LIGHT AT ROW 4 WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE OVERHEAD EMERGENCY LIGHT AT ROW 4. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)Sep 19, 2005 · N907EV · Cndair CL6002B19 · Emergency LightingSDR ASOA05573Tire · failedFLT 4456 - DURING CLIMB-OUT FROM ATL-ICT, THE TOWER ADVISED THE CREW THAT TIRE DEBRIS WERE FOUND ON THE RUNWAY FOLLOWING THEIR TAKEOFF. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO ATL AND LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED BOTH RIGHT Jun 30, 2005 · N907EV · Cndair CL6002B19 · TireSDR ASOA05390Floor Support · crackedDURING A C-CHECK IN HOT, THE FLOOR SUPPORT ANGLE AT FS 621 RIGHT WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE FLOOR SUPPORT ANGLE AT FS 621 RIGHT IAW ASA EO 600-53-0105. (M)Apr 29, 2005 · N907EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
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