N910EV

Service difficulty reports · 152

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 = 'N910EV' 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 SWIA2026100877555Landing Gear · malfunctionedNOSE GEAR DID NOT COME UP WHEN THE GEAR LEVER WAS SELECTED TO THE UP POSITION. RAN QRH, GEAR CAME DOWN. FLIGHT 5745. PERFORMED AN OPS CHECK OF NLG WOW 2 PROXIMITY SENSOR & CENTERED WOW PROXIMITY SENSOR IAW AMM 32-61-05, OPS CHKD GOOD. PERFORMED NLG GEAR SOct 8, 2026 · N910EV · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR SWI2025F01846Floorbeam · crackedTRANSVERSE FLOOR BEAM @ FS. 589 FOUND TO BE CRACKED IN MULTIPLE LOCATIONS WHERE AFT CARGO DOOR LOWER SILL SITS. REPAIRED TRANSVERSE BEAM AT FS 589.00 IAW MHIRJ REO 601R-53-61-8412 REV--. COMPLETED TASK CARD 51-900-1003-SKY. REFERENCE CONTINUE CARD FOR WORK PENov 4, 2025 · N910EV · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA2025121901104Door Sill · corrodedAFT CARGO DOOR LOWER SILL, CORRODED IN MULTIPLE LOCATIONS AND BENT, EVAL REQUIRED. REMOVED AND REPLACED CARGO DOOR LOWER SILL IAW SRM 51-42-21, 51-40-11, 51-42-06, 51-42-13, REV. 39B, AND REO 601R-53-61-8412, REV--. COMPLETED TASK CARD 51-900-1003-SKY. RNov 4, 2025 · N910EV · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA2025121901018Spar · damagedLEFT AILERON AFT SPAR MOST OUTBOARD BORES ARE OVERSIZED. REPAIRED R/H AILERON AFT SPAR MOST OTBD AND INBD BORE ON WING IAW GREO 601R-57-51-015 REV NC.Oct 18, 2025 · N910EV · Cndair CL6002B19 · AileronsSDR SWIA2025121901015Drain · misrepairedWHILE WORKING SB 601R-57-054 INADVERTENTLY REAMED SATELLITE HOLES FOR WATER DRAINS AT BL 0 ON LT & RT SIDES BETWEEN STRINGERS 14-15. REPAIRED SATELLITE HOLES FOR WATER DRAINS AT BL 0 ON LT AND RT SIDE BETWEEN STRS 14-15 IAW REO 601R-57-21-3982 REV -.Oct 15, 2025 · N910EV · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA2025121901006Intercostal · corrodedINTERCOSTAL FOUND TO BE SEVERELY CORRODED ON MORE THAN ONE ELEMENT REQUIRING REPLACEMENT LOCATED AT BS 364, S25L - 25R. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-42-06, AND 51-42-21. COMPLETED TASK CARD 51-900-1003-SKY. REFERENCE CONTINUATION CARD FOR WOct 6, 2025 · N910EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA202512190004Mount Bracket · damagedUPON INSTALLATION OF THE A/C POWER RECEPTACLE BRACKET MOUNT FOUND 1 EA FASTENER HOLE TO BE ELONGATED ON AFT O/B SIDE IN CORNER MARKED WITH RED TAPE. REPAIRED A/C POWER RECEPTACLE BRACKET MOUNT IAW MHIRJ REO 601R-53-11-4026 REV -. COMPLETED SKYCARD 51-900-100Oct 4, 2025 · N910EV · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA2025121900930Intercostal · corrodedINTERCOSTALS FOUND TO BE SEVERELY CORRODED ON MORE THAN ONE ELEMENT REQUIRING REPLACEMENT. REMOVED AND REPLACED THE INTERCOSTALS IAW SRM 51-42-06, AND 51-42-21 06. COMPLETED TASK CARD 51-900-1003-SKY. REFERENCE CONTINUATION CARD FOR WORK PERFORMED.Sep 30, 2025 · N910EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA202512190925Spar · damagedR/H AILERON AFT SPAR MOST OUTBOARD BORES ARE OVERSIZED. REPAIRED R/H AILERON AFT SPAR MOST OTBD AND INBD BORE ON WING IAW GREO 601R-57-51-015 REV NC.Sep 25, 2025 · N910EV · Cndair CL6002B19 · AileronsSDR SWIA2025121900917Floor Support · corrodedLEFT PRESSURE FLOOR SUPPORT IS CORRODED AT BS 549. REPAIRED THE CORROSION ON THE LT PRESSURE FLOOR SUPPORT AT FS 549 IAW REO 601R-53-41-666, REV C, AND SKY CARD 51-900-1003-SKY.Sep 17, 2025 · N910EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWI2025F01836Intercostal · corrodedPAX DOOR DD7A FWD INTERCOSTAL FOUND TO BE CORRODED. REQUIRES REPLACEMENT. REPLACED PAX DOOR DD7A FWD INTERCOSTAL IAW SRM 51-42-06. COMPLETED TASK CARD 51-900-1003-SKY. REFERENCE CONTINUATION CARD FOR WORK PERFORMED.Sep 15, 2025 · N910EV · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWI2025F01835Intercostal · corrodedPAX DOOR INTERCOSTAL DD3 MID CORRODED. REQUIRES REPLACEMENT. REMOVED AND REPLACED THE PAX DOOR MID INTERCOSTAL DD3 IAW SRM 51-42-06 AND 51-42-21. COMPLETED TASK CARD 51-900-1003-SKY REFERENCE CONTINUATION CARD FOR WORK PERFORMED.Sep 15, 2025 · N910EV · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA2025121900915Intercostal · corrodedPAX DOOR INTERCOSTAL DD2 MID FOUND TO BE CORRODED. REQUIRES REPLACEMENT. REMOVED AND REPLACED THE PAX DOOR MID INTERCOSTAL DD2 IAW SRM 51-42-06 AND 51-42-21, COMPLETED TASK CARD 51-900-1003-SKY AND ATTACHED COMPLETED FORM 337. CONTINUATION CARD FOR WORK PERFSep 15, 2025 · N910EV · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA202512190911Former · corrodedPAX DOOR MID FORMER, FS329.41 BETWEEN DD5 AND DD6 FOUND TO BE CORRODED REQUIRED REPLACEMENT. REPLACED PAX DOOR MID FORMER AT FS329.41 IAW SRM 51-42-06. COMPLETED TASK CARD 51-900-1003-SKY. REFERENCE CONTINUATION CARD FOR WORK PERFORMED.Sep 11, 2025 · N910EV · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA202512190909Rib · crackedRIGHT MLG BATTERY RIB IS CRACKED AT WS 53.60 FWD O/B SIDE. REMOVED AND REPLACED RT BATTERY RIB AT WS 53.60 IAW SRM 51-42-06 AND 51-42-21 COMPLETED TASK CARD 51-900-1003-SKY. REFERENCE CONTINUATION CARD FOR WORK PERFORMED.Sep 9, 2025 · N910EV · Cndair CL6002B19 · Fuselage Main, BulkheadSDR SWI2025F01845Drip Tray · damagedDRIP TRAY AT LBL 27, FS 409 IS DAMAGED. REPAIRED DRIP TRAY AND MOUNTING STRUCTURE IAW MHIRJ REO 601R-53-31-1351 REV-, AND REO 601R-53-31-1353, REV-. COMPLETED TASK CARD 51-900-1003-SKY. REF CONTINUATION CARD FOR WORK PERFORMED.Sep 8, 2025 · N910EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWI2025F01844Frame · corrodedBS 319 FRAME IS CORRODED BETWEEN S18L AND 20L. REMOVED AND REPLACED THE STUB FRAME AT IAW SRM 51-42-06. COMPLETED TASK CARD 51-900-1003-SKY. REFERENCE CONTINUATION CARD FOR WORK PERFORMED.Sep 8, 2025 · N910EV · Cndair CL6002B19 · Fuselage Main, FrameSDR SWI2025F01843Skin · crackedRIGHT FORWARD FUSELAGE SKIN IS CRACKED AT THE AFT LATCH CUTOUT OF THE TRU DOOR. REPLACED RT FORWARD FUSELAGE SKIN IAW SRM 51-42-06, 51-42-13, AND 51-42-21. COMPLETED TASK CARD 51-900-1003-SKY.Sep 8, 2025 · N910EV · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA2025121900908Skin · crackedLEFT FORWARD FUSELAGE SKIN IS CRACKED AT THE AFT LATCH CUTOUT OF THE TRU DOOR. REPLACED LT FORWARD FUSELAGE SKIN IAW SRM 51-42-06, 51-42-13, & 51-42-21. COMPLETED TASK CARD 51-900-1003-SKY.Sep 8, 2025 · N910EV · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWI2025F01834Door Sill · corrodedPAX DOOR SILL LOWER FLOOR SUPPORT ANGLE IS CORRODED. REMOVED AND REPLACED PAX DOOR LOWER SILL FLOOR SUPPORT ANGLE IAW SRM 51-42-06, 51-42-13, AND 51-42-13. COMPLETED TASK CARD 51-900-1003-SKY. REFERENCE CONTINUATION CARD FOR WORK PERFORMED.Sep 6, 2025 · N910EV · Cndair CL6002B19 · Fuselage Main, StructureSDR SWI2025F01833Floorbeam · crackedFS280 CROSSBEAM LBL9 IB ANGLE IS CRACKED. (C-CHECK RO 12/17/2025)FABRICATED 1 EA CLAP AT FS 280 CROSSBEAM LBL 9IAW CRJ 200 SRM 51-40-06, 51-40-11, 51-25-00, 51-42-22 AND 51-42-21 REV. 39B, DATED 06-NOV-11. REFERENCING REO 601R-53-11-171 REV D DATED 13 FEB 0Sep 6, 2025 · N910EV · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA2025121900906Floor Support · corrodedRBL 9 FLOOR SUPPORT TOP INBD FLANGE IS CORRODED FROM BS 409+5 TO BS 409+118. REMOVED AND REPLACED THE FLOOR SUPPORT CAP AT RBL9 FROM FS409+5-409+118 IAW SRM 51-42-06, 51-42-21, AND REO 601R-53-31-1350, REV-- DATED 2025-09-25. REF CONTINUATION CARD FOR ALL WORSep 6, 2025 · N910EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA202512190905Fitting · crackedFS 460.00 FITTING IS CRACKED ON THE OTBD SIDE OF LBL 9, FLOORBEAM. REMOVED AND INSTALLED SERVICEABLE FITTING AT BS 460 IAW REO 601R-53-41-3353, REV-. COMPLETED TASK CARD 51-900-1003-SKY. REFERENCE CONTINUATION CARD FOR WORK PERFORMED.Sep 5, 2025 · N910EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWI2025F01847Angle · crackedLEFT WING, BATTERY RIB AT WS 53.60 ANGLE ON INBD SIDE OF WEB IS CRACKED AND WEB IS CRACKED AS WELL. REMOVED AND REPLACED LT WING BATTERY RIB IAW SRM 51-42-06. COMPLETED TASK CARD 51-900-1003-SKY. REFERENCE CONTINUATION CARD FOR WORK PERFORMED.Sep 2, 2025 · N910EV · Cndair CL6002B19 · Wing Miscellaneous StructureSDR SWIA202512190902Angle · crackedLEFT WING, BATTERY RIB AT WS 48.30 ANGLE IS CRACKED. REMOVED AND REPLACED THE LT UPPER BATTERY RIB ANGLE IAW SRM 51-42-06. COMPLETED TASK CARD 51-900-1003-SKY. REFERENCE CONTINUATION CARD FOR WORK PERFORMED.Sep 2, 2025 · N910EV · Cndair CL6002B19 · Wing Miscellaneous StructureSDR SWIA202512190831Post · failed inspBS 409+128 BL 0 VERTICAL POST RT & LT SIDES HAS INDICATIONS .3" LONG BY 100% FSH IN THE AFT RADIUS AT WL69. FAILED NDT INSPECTION. REMOVED AND REPLACED BS 409+128 BL 0 VERTICAL POST IAW REO 601R-53-41-889 REV-D, COMPLETED TASK CARD 51-900-1003-SKY. REFERENCE Aug 31, 2025 · N910EV · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA202512190829Skin · misalignedSERVICE DOOR INNER SKIN HAS SEVERAL JO-BOLTS THAT ARE NOT PROPERLY INSTALLED. REPAIRED OVERSIZED HOLES AND INSTALLED FASTENERS IAW REO 601R-52-41-537 REV--. COMPLETED TASK CARD 51-900-1003-SKY.Aug 29, 2025 · N910EV · Cndair CL6002B19 · Service DoorsSDR SWI2025F01842Intercostal · corrodedPAX DOOR INTERCOSTAL DD 6 BETWEEN FS 320.163 AND FS 336.961 IS CORRODED. REMOVED AND REPLACED PAX DOOR MID INTERCOSTAL DD6 IAW SRM 51-42-06 AND 51-42-21. COMPLETED TASK CARD 51-900-1003-SKY. REFERENCE CONTINUATION CARD FOR WORK PERFORMED.Aug 27, 2025 · N910EV · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWI2025F01841Intercostal · corrodedPAX DOOR INTERCOSTAL DD 1 BETWEEN FS 323.361 AND FS 336.961 IS CORRODED. REMOVED AND REPLACED PAX DOOR INTERCOSTAL DD1 MID BETWEEN FS323.61 AND FS336.961 IAW SRM 51-42-06 AND 51-42-21. COMPLETED TASK CARD 51-900-1003-SKY. REFERENCE CONTINUATION CARD FOR WORKAug 27, 2025 · N910EV · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWI2025F01840Former · corrodedPAX DOOR AFT FORMER IS CORRODED ON THE INSIDE. REMOVED AND REPLACED PAX DOOR AFT FORMER IAW SRM 51-42-06 AND 51-42-21. COMPLETED TASK CARD 51-900-1003-SKY. REFERENCE CONTINUATION CARD FOR WORK PERFORMEDAug 27, 2025 · N910EV · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWI2025F01839Former · corrodedPAX DOOR FWD FORMER IS CORRODED ON THE INSIDE. REMOVED AND REPLACED PAX DOOR FWD FORMER IAW SRM 51-42-06 AND 51-42-21. COMPLETED TASK CARD 51-900-1003-SKY. REFERENCE CONTINUATION CARD FOR WORK PERFORMEDAug 27, 2025 · N910EV · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWI2025F01838Intercostal · corrodedPAX DOOR INTERCOSTAL DD 1A BETWEEN FS 323.361 AND FS 336.961 IS CORRODED. REMOVED AND REPLACED PAX DOOR INTERCOSTAL DD1A IAW CRJ 200 SRM 51-42-06, 51-42-21 AND 51-42-11 COMPLETED TASK CARD 51-900-1003-SKY AND ATTACHED COMPLETED FORM 337 NO WEIGHT CHANGE. REFAug 27, 2025 · N910EV · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA202512190827Intercostal · corrodedPAX DOOR INTERCOSTAL BETWEEN FS 320.163 AND FS 329.130 IS CORRODED. REMOVED AND REPLACED PAX DOOR MID INTERCOSTAL DD4 IAW CRJ 200 SRM 51-42-06 AND 51-42-21 COMPLETED TASK CARD 51-900-1003-SKY AND ATTACHED COMPLETED FORM 337 NO WEIGHT CHANGE. REFERENCE CONTIAug 27, 2025 · N910EV · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA202512190826Skin · dentedSEVERAL DENTS FROM BS 589 - 621 BETWEEN S22R AND 27R. REPAIRED THE DENTS IAW 601R-53-61-8395, REV-. COMPLETED TASK CARD 51-900-1003-SKY . REFERENCE CONTINUATION CARD FOR WORK PERFORMEDAug 26, 2025 · N910EV · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWI2025F01837Skin · chafedLEFT LOWER WING PLANK CHAFED ON TRAILING EDGE AT LWS 45.0 FROM CONTACT WITH PANEL 193AB. REPAIRED THE LT LOWER WING PLANK ON TRAILING EDGE IAW REO 601R-57-21-880, REV-D. SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED. COMPLETED AND ATTACHED MAJOR REPAug 23, 2025 · N910EV · Cndair CL6002B19 · Wing, Plate/SkinSDR SWIA2025121900823Skin · chafedRIGHT LOWER WING PLANK CHAFED ON TRAILING EDGE AT RWS 45.0 FROM CONTACT WITH PANEL 193AB. REPAIRED THE RT LOWER WING PLANK IAW REO 601R-57-21-880 REV-D. COMPLETED TASK CARD 51-900-1003-SKY AND ATTACHED COMPLETED FORM 337. REFERENCE CONTINUATION CARD FOR WORAug 23, 2025 · N910EV · Cndair CL6002B19 · Wing, Plate/SkinSDR SWIA2025121900703Door Frame · corrodedCOMPLY WITH SCHEDULED MAINTENANCE CODE: RA93189-601R-53-61-8212 MXCODEID77004-PR - FRAME FS574.00 AT CARGO DOOR FWD OPENING HAS CORROSION AT APPROX. WL 75.00. BLENDED CORROSION ON FRAME BS 574 AT CARGO DOOR FWD OPENING AT WL 75 IAW SRM 51-21-06 AND COMPLIED WJul 3, 2025 · N910EV · Cndair CL6002B19 · Fuselage Main, StructureSDR SWI2025F00525Engine · faultedMASTER WARNING LH OIL PRESSURE ON CLIMB OUT, THEN N1 AND N2 AND ITT SPOOLED DOWN ON ITS OWN TO ZERO. RAN QRH ATTEMPTED RESTART TWICE - BOTH TIMES FAILED. COMING OUT OF XWA DIVERTED TO RAP. DECLARED AN EMERGENCY. NO EXTERNAL DAMAGE NOTED ON WALKAROUND POSTFLIApr 12, 2025 · N910EV · Cndair CL6002B19 · Engine Oil QuantitySDR SWIA20250414003Oil System · leakingMASTER WARNING LH OIL PRESSURE ON CLIMB OUT, THEN N1 AND N2 AND ITT SPOOLED DOWN ON ITS OWN TO ZERO. RAN QRH ATTEMPTED RESTART TWICE - BOTH TIMES FAILED. COMING OUT OF XWA DIVERTED TO RAP. DECLARED AN EMERGENCY. NO EXTERNAL DAMAGE NOTED ON WALKAROUND POSTFLIApr 12, 2025 · N910EV · Cndair CL6002B19 · Turbine Engine Oil SystemSDR SWIA2024082600010Frame · corrodedFRAME FS574.00 AT CARGO DOOR FWD OPENING HAS CORROSION AT APPROX. WL75.00. (FILED - CLOSED)BLENDED CORROSION ON FRAME FS574.00 AT CARGO DOOR FWD OPENING AT APPROX WL75.00 WITH REFERENCE TO SRM 51-21-06 AND COMPLIED WITH REO 601R-53-61-8212 REV "--" DATED 2024-Aug 10, 2024 · N910EV · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA2024082673001Frame Angle · corrodedCORROSION ON FRAME ANGLE AT FS 605.00 BETWEEN STGR 18R AND 19R (FILED - CLOSED)REMOVED CORROSION FROM FRAME ANGLE AT FS 605.00 BETWEEN STGR 18R AND 19R WITH REFERENCE TO SRM 51-21-06 AND DISCOVERED CRACK. REPAIRED FRAME ANGLE AT FS 605.00 WITH REFERENCE TO REJul 31, 2024 · N910EV · Cndair CL6002B19 · Fuselage Main, FrameSDR SWI202408260781Floor Support · corrodedRH PRESSURE FLOOR SILL HAS SURFACE CORROSION LOCATED AT APPROX. FS 555.00, 513.00 AND 447.00. (FILED - CLOSED)BLENDED AND REPAIRED ALL OF THE CORROSION AREAS ON THE RH PRESSURE FLOOR SILL FROM APPROX FS409 + 128 TO FS559.00 PER REO 601R-53-41-666 DATED: 2012-Jul 29, 2024 · N910EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2024082672009Floor Support · corrodedLH PRESSURE FLOOR SILL HAS NUMEROUS AREAS OF CORROSION LOCATED @ APPROX. FS460-465, 470.00-474.00, 485.5, 506.00, 513.00 AND 530.50. (FILED - CLOSED)BLENDED AND REPAIRED ALL OF THE CORROSION AREAS ON THE LH PRESSURE FLOOR SILL FROM APPROX FS409 + 128 TO FS559Jul 29, 2024 · N910EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2024082672800Track · crackedCARGO DOOR FORWARD TRACK LOWER CHANNEL CRACKED. (FILED - CLOSED)REMOVED AND REPLACED THE CARGO DOOR FORWARD TRACK LOWER CHANNEL WITH REFERENCE TO SRM 51-42-06. COMPLIED WITH TASK CARD 51-900-1003-SKY. COMPLIED WITH M-337.Jul 28, 2024 · N910EV · Cndair CL6002B19 · Cargo/Baggage DoorsSDR SWIA2024082600724Stiffener · crackedCRACK INDICATION LOCATED FS409 + 128 BL0.00 ON VERTICAL BEAM/STIFFENER, FORWARD LEFT ANGLE AFT FACE, PROPAGATING OUTBOARD/AIRCRAFT LEFT FROM UPPER LEFT FASTENER (REFERENCE SRM 53-41-19 ITEM 6, FIGURE 1, SHEET 1 AND 3). (FILED - CLOSED)COMPLIED WITH REO 601R-53Jul 24, 2024 · N910EV · Cndair CL6002B19 · Fuselage Main, StructureSDR SWI202408260778Pressure Blkhd · crackedAFT SIDE OF PRESSURE BULKHEAD @ FS621.00 JUST OUTBOARD OF LBL 36.20 AND INLINE WITH STRINGER 14L, CLIP/ANGLE CRACKED. (FILED - CLOSED)REMOVED AND REPLACED CLIP/ANGLE ON AFT SIDE OF PRESSURE BULKHEAD @ FS621.00 JUST OUTBOARD OF LBL 36.20 AND INLINE WITH STRINGEJul 22, 2024 · N910EV · Cndair CL6002B19 · Fuselage Main, BulkheadSDR SWI202408260777Pressure Blkhd · crackedAFT SIDE OF PRESSURE BULKHEAD @ FS621.00 JUST OUTBOARD OF RBL 36.20 AND INLINE WITH STRINGER 14R, CLIP/ANGLE CRACKED. (FILED - CLOSED)REMOVED AND REPLACED CLIP/ANGLE ON AFT SIDE OF PRESSURE BULKHEAD @ FS621.00 JUST OUTBOARD OF RBL 36.20 AND INLINE WITH STRINGEJul 22, 2024 · N910EV · Cndair CL6002B19 · Fuselage Main, BulkheadSDR SWIA2024082600722Pressure Blkhd · gougedREAR PRESSURE BULKHEAD (FS621.00) FWD FACE HAS RIVET HEAD DAMAGE AND GOUGES ON DOUBLERS, LOCATED APPROX. LBL 18.00, 27.50, RBL 36.20, 27.50, 18.00 @ WL 87.50 AND WL 94.50. (FILED - CLOSED)UPON FURTHER INSPECTION FOUND 6 GOUGES LOCATED FS 621 BULKHEAD TOP DOUBLJul 22, 2024 · N910EV · Cndair CL6002B19 · Fuselage Main, BulkheadSDR SWIA202162173None · noneTRANSFER FROM EAML 763411 : QTY 07 MIS-DRILLED HOLES RH H/STAB LOWER SKIN O/B RIB NO 9. REF REO601R-55-11-699 DATED 2021-10-22 REV -- (FLIGHT 5459 - FILED CLOSED) REPAIRED MIS-DRILLED HOLES IN RH HORZONTAL STAB LOWER SKIN BETWEEN RIB #7 - RIB #9 AND F/SPAROct 25, 2021 · N910EV · Cndair CL6002B19 · Fuselage Structure (General)SDR SWIA2021081260114Engine · failedRIGHT ENGINE FAILURE AFTER DEPARTING KBIS THROUGH 7000€™. PERFORMED QRC, QRH PROCEDURES, RETURNED TO KBIS. (FLIGHT 5729 - FILED CLOSED) REF AML 703489 FOR CORRECTIVE. MORE INFORMATION WAS ADDED TO AML 703489 BUT BOTH ARE THE SAME DISCREPANCY. THIS DISCREAug 7, 2021 · N910EV · Cndair CL6002B19 · Engine (Turbine/Turboprop)
Back to N910EV