N925EV

Service difficulty reports · 191

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 = 'N925EV' 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 SWIA202158196Seat Track · corroded* RH SIDE SEAT TRACK CORRODED IN MULTIPLE SPOTS FROM FS 364.00 TO FS409.00 (MARKED). (C-CHECK RO 5/16/2021) REMOVED AND INSTALLED NEW SEAT TRACK AT FS364 TO FS409+18 RBL9.0 PART # 601R38312-31 REF. CRJ200 AMM 53-01-11-400-802.Mar 30, 2021 · N925EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA202158195Seat Track · corroded* RH SIDE SEAT TRACK EXTRUSION CORRODED IN MULTIPLE SPOTS FROM FS 449.00 TO FS499.00 (MARKED). (C-CHECK RO 5/16/2021) REMOVED AND INSTALLED NEW SEAT TRACK AT FS449 TO FS501 RBL9.0 PART # 601R38312-119 REF. CRJ200 AMM 53-01-11-400-802.Mar 30, 2021 · N925EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA202158194Seat Track · corroded* LH SIDE SEAT TRACK RETAINER CORRODED FROM 559+16 TO 559+80 (MARKED). (C-CHECK RO 5/16/2021) REMOVED CORROSION FROM LH SIDE SEAT TRACK RETAINER FROM FS559+16 TO FS559+80 REF CRJ 200 SRM 51-21-06. NDT IAW CRJ 200 NDT M PART 1 REV 42 10-10 -20 51-20-04, Mar 30, 2021 · N925EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA202158172Floorbeam · corroded* THE FLOOR BEAM AT RBL 9 HAS A SHEARED NUTPLATE ON ITS INBOARD FLANGE AT APPROX. FS 559+6 AND CORROSION AROUND THE NUTPLATE ON ITS OUTBOARD FLANGE AT APPROX. FS 559+6. (MARKED WITH RED GREASE PENCIL) (C-CHECK RO 5/16/2021) REMOVED CORROSION ON FLOOR BEMar 30, 2021 · N925EV · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA202158171Strap · corroded* THE RH FLOOR SUPPORT STRAP AT FS 559 THAT EXTENDS BETWEEN RBL 24 AND RBL 40 HAS CORROSION ALONG ITS SURFACE. (C-CHECK RO 5/16/2021) REMOVED AND INSTALLED NEW R/H FLOOR SUPPORT STRAP AT FS559, BETWEEN RBL27 AND RBL40. REF: CRJ 200, DRW 601R31025, REV Mar 30, 2021 · N925EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA202158170Strap · corroded* THE LH FLOOR SUPPORT STRAP AT FS 559 THAT EXTENDS BETWEEN LBL 24 AND LBL 40 HAS CORROSION ALONG ITS SURFACE. (C-CHECK RO 5/16/2021) REMOVED AND INSTALLED NEW L/H FLOOR SUPPORT STRAP AT FS559 THAT EXTENDS BETWEEN LBL24 & LBL40, REF CRJ 200 SRM 51-42-06Mar 30, 2021 · N925EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA202158169Floorbeam · cracked* THE FS 484 BELOW FLOOR INTERCOSTAL BETWEEN RBL 27 AND RBL 36 HAS A SUSPECTED CRACK ON ITS INBOARD CLIP IN THE TOP RADIUS. (C-CHECK RO 5/16/2021) REMOVED AND REPLACED THE INBD CLIP AT FS 484.00 BELOW FLOOR INTERCOSTAL BETWEEN RBL 27 AND RBL 36 WITH NEMar 30, 2021 · N925EV · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA202158168Floorbeam · cracked* THE FS 484 BELOW FLOOR INTERCOSTAL BETWEEN LBL 27 AND LBL 36 HAS A CRACKED OUTBOARD CLIP. (C-CHECK RO 5/16/2021) REMOVED THE OTBD BRACKET AT FS484 BETWEEN LBL27 & LBL36 REF. CRJ200 SRM 51-42-21. FABRICATED NEW REPLACEMENT BRACKET PN# S6144-14, PO T000Mar 30, 2021 · N925EV · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA202158167Stringer · corroded* STR16L CORRODED AT FS310.00 (MARKED). (C-CHECK RO 5/16/2021) REMOVED CORROSION ON STGR16L INTERCOSTAL AT FS310, REF CRJ 200 SRM 51-21-06. EVALUATED AND FOUND TO BE OUT OF LIMITS. SUBMITTED TO ENGINEERING AND RECEIVED MHIRJ REO 601R-53-21-3439 REV-- DAMar 30, 2021 · N925EV · Cndair CL6002B19 · Fuselage Main, Longeron/StringerSDR SWIA202158211Cam · chafed* PAX DOOR SURROUND UPPER AFT CAM FITTING CHAFED (FLAGGED). (C-CHECK RO 5/16/2021) BLENDED CHAFE ON PAX DOOR SURROUND UPPER AFT CAM FITTING REF CRJ200 SRM 51-12-00. EVALUATED AND FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED THE PAX DOOR SURROUND UPPEMar 29, 2021 · N925EV · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA202158193Anchor Fitting · corroded* PAX DOOR SURROUND FWD AND AFT ANCHOR FITTINGS HAVE CORRODED HARDWARE. (C-CHECK RO 5/16/2021) REMOVED AND REPLACED PAX DOOR SURROUND FWD AND AFT ANCHOR FITTINGS HARDWARE WITH NEW 8EA BOLTS 12EA SCREWS, 28EA WASHERS, AND 20EA NUTS REF CRJ 200 SRM 51-4Mar 29, 2021 · N925EV · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA202158166Cup · corroded* PAX DOOR UNDERFLOOR FWD AND AFT HAND RAIL RECIEVING CUPS CORRODED IN MULTIPLE SPOTS (MARKED). (C-CHECK RO 5/16/2021) BLENDED CORROSION FROM FWD AND AFT PAX DOOR UNDERFLOOR HAND RAIL RECEIVING CUPS, (MULTIPLE AREAS). REF: CRJ 200, SRM 51-21-06. EVALUATMar 29, 2021 · N925EV · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA202158165Rib · cracked*RH MLG BATT RIB AT APPROX RBL 45 HAS A CRACK. AREA MARKED (C-CHECK RO 5/16/2021) REMOVED AND REPLACED THE RH MLG BATT RIB CAP ANGLE AT APPROX RBL 45 REF DWG 601R10204 REV J, DWG 601R10212 REV A, CRJ200 SRM 51-42-06 AND 51-42-21. / COMPLIED WITH 51-900Mar 28, 2021 · N925EV · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA202158213Skin · dented* DENT ON FUSELAGE BETWEEN FS295 AND FS310 BETWEEN STR25R AND STR26R (C-CHECK RO 5/16/2021) EVALUATED DENT DIMENSION AND FOUND TO BE OUT OF LIMITS. DENT IS LESS THEN 1 INCH FROM FASTENER REF CRJ200 SRM 53-00-31. SUBMITTED TO ENGINEERING AND RECEIVED MHIMar 25, 2021 · N925EV · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA202158212Stop Fitting · gouged* AVIONICS BAY DOOR RH AFT STOP FITTING ON FUSELAGE GOUGED. (C-CHECK RO 5/16/2021) AVIONICS BAY DOOR RH AFT STOP FITTING FOUND TO BE OUT OF LIMITS, REMOVED AND REPLACED WITH NEW AVIONICS BAY DOOR STOP FITTING REF CRJ200 SRM 51-41-02Mar 25, 2021 · N925EV · Cndair CL6002B19 · Electrical/Electronic Compartment DoorsSDR SWIA202158192Angle · corroded* RH FWD ANGLE FOR AVIONICS BAY DOOR SEAL RETAINER HAS CORROSION. (C-CHECK RO 5/16/2021) REMOVED CORROSION ON RH FWD ANGLE FOR AVIONICS BAY DOOR SEAL RETAINER REF CRJ200 SRM 51-21-06. RH FWD ANGLE IS 100% EXFOLIATED, FOUND TO BE OUT OF LIMITS REF CRJ200Mar 25, 2021 · N925EV · Cndair CL6002B19 · Electrical/Electronic Compartment DoorsSDR SWIA202158191Retainer · corroded* LH AFT ANGLE FOR AVIONICS BAY DOOR SEAL RETAINER HAS CORROSION. (C-CHECK RO 5/16/2021) REMOVED CORROSION ON LH AFT ANGLE FOR AVIONICS BAY DOOR SEAL RETAINER REF CRJ200 SRM 51-21-06. LH AFT ANGLE IS 100% EXFOLIATED, FOUND TO BE OUT OF LIMITS REF CRJ200Mar 25, 2021 · N925EV · Cndair CL6002B19 · Electrical/Electronic Compartment DoorsSDR SWIA202158164Housing · chafedCARGO DOOR HANDLE HOUSING IS CHAFED (C-CHECK RO 5/16/2021) REMOVED AND INSTALLED NEW CARGO HANDLE HOUSING ON CARGO DOOR REF DWG 601R35027 REV -AY AND CRJ200 SRM 51-42-21. COMPLIED WITH 51-900-1003-SKY AND PRESSURE CHECK GOODMar 25, 2021 · N925EV · Cndair CL6002B19 · Cargo/Baggage DoorsSDR SWIA202158163Angle · corroded* RH AFT ANGLE FOR AVIONICS BAY DOOR SEAL RETAINER HAS CORROSION. (C-CHECK RO 5/16/2021) REMOVED AND INSTALLED REPLACEMENT R/H AFT AVIONICS BAY DOOR SEAL RETAINER SUPPORT ANGLE CC670-38660-1 REF CRJ 200 SRM 51-42-06 . COMPLIED WITH 51-900-1003-SKY AND SMar 25, 2021 · N925EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA202158162Skin · chafed* R/H INBOARD FLAP VANE SKIN IS CHAFED AT THE OUTBOARD LEADING EDGE. (C-CHECK RO 5/16/2021) BLENDED CHAFE ON R/H INBOARD FLAP VANE LEADING EDGE SKIN, OUTBOARD LOCATION. REF: CRJ 200, BOMBARDIER REO 601R-57-52-004, REV-D, DATE: 2012-12-19. EVALUATED ANDMar 23, 2021 · N925EV · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA202158161Skin · chafed* R/H INBOARD FLAP VANE SKIN IS CHAFED AT THE CENTER LEADING EDGE. (C-CHECK RO 5/16/2021) BLENDED CHAFE, BLENDED AREA IS FOUND TO BE OUT OF LIMITS REF REO 601R-57-52-004 REV D DATED 2012-12-19. INSTALLED NEW FLAP VAIN SKIN PN 601R14303-10. REF. CRJ200 Mar 23, 2021 · N925EV · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA202158160Skin · chafed* R/H INBOARD FLAP VANE SKIN IS CHAFED AT THE INBOARD SIDE LEADING EDGE. (C-CHECK RO 5/16/2021) REMOVED CHAFE ON R/H I/B FLAP I/B SIDE LEADING EDGE SKIN, & FOUND TO BE OUT OF LIMIT PER REF BOMBARDIER REO 601R-57-52-004, REV -D, DATE 2012-12-19, REMOVEDMar 23, 2021 · N925EV · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA202158159Skin · eroded* RH WING CENTER LEADING EDGE PANEL (630JL) HAS EROSION. (C-CHECK RO 5/16/2021) COMPLIED WITH REO 601R-57-41-1120, REV. --, 2021-04-26 IN ITS ENTIRETY (STEPS 1-5). COMPLIED WITH 51-900-1003-SKY. REMOVED AND INSTALLED R/H WING CENTER L/E PICCOLO TUBE, REMar 20, 2021 · N925EV · Cndair CL6002B19 · Wing, Plate/SkinSDR SWIA202158158Skin · eroded* LH WING CENTER LEADING EDGE PANEL (530JL) HAS EROSION. (C-CHECK RO 5/16/2021) REMOVED EROSION DAMAGE ON L/H WING CENTER LEADING EDGE PANEL 530JL REF CRJ 200 SRM 51-12-00. COMPLIED WITH REO 601R-57-41-1119 REV (--) 2021-04-26 STEPS 1-5 DUE TO EROSION DMar 20, 2021 · N925EV · Cndair CL6002B19 · Wing, Plate/SkinSDR SWIA202158157Bulkhead Web · crackedTRANSFER FROM EAML 597316 : TRANSFER FROM EAML 427961 : WHILE PERFORMING THE NDT EDDY CURRENT INSPECTION OF THE AFT PRESS BULHEAD FWD FACE DISCOVERED CRACKS AT STATIONS: / RBL 36.20-WL 103.18 / RBL 27.50-WL 103.68 / RBL 18.00-WL 103.68 / RBL 9.50-WL 103.68 / LMar 15, 2021 · N925EV · Cndair CL6002B19 · Fuselage Main, BulkheadSDR SWIA2019052445919Bracket · failedGEAR DISAGREE ON CLIMB OUT RAN QRH AND RETURNED TO FIELD. (FLT#5326) CLOSED REMOVED AND REPLACED BENT NLG CENTERED/EXTENDED PROXIMITY SENSOR BRACKET IAW CMM. ADJUSTED NLG CENTERED/EXTENDED PROXIMITY SENSOR AND PERFORMED GEAR SWINGS IAW AMM. OPS CHECK GOOD.May 24, 2019 · N925EV · Cndair CL6002B19 · Landing Gear Position and WarningSDR SWIA2019030545596Selector Valve · failedGEAR DISAGREE AFTER TAKEOFF. NOSE GEAR WOULD NOT RETRACT. (FLT#5749) FO: 03/05/2019 CLOSED REMOVED AND REPLACED NLG SELECTOR VALVE IAW AMM. OPS CHECK GOOD AT THIS TIME. LEAK CHECK GOOD.Mar 4, 2019 · N925EV · Cndair CL6002B19 · Landing Gear SelectorSDR SWIA2019021945532Landing Gear · icedNOSE DOOR AND GEAR DISAGREE MSG ON TAKEOFF. MSG CLEARED AND GEAR CAME UP AFTER 5 SECONDS. NORMAL GEAR EXTENSION AND INDICATIONS ON LANDING. (FLT#5974) PSEU INDICATES ONLY NOSE DOOR SENSORS BEING FLAGGED. TALKED TO AIR CREW AND LEARNED GEAR WAS ICE COVERED PRIOFeb 18, 2019 · N925EV · Cndair CL6002B19 · Nose/Tail Landing GearSDR SWIA2018070244840Proximity Sensor · failedWHEN GEAR WAS EXTENDED DURING APPROACH RECEIVED WOW INPUT CAUTION MESSAGE AND A DOWN AND LOCKED 3 GREEN INDICATION. EXECUTED GO AROUND PROCEDURE TO INCLUDE GEAR RETRACTION. COMPLIED WITH QRH. ON SECOND APPROACH GEAR EXTENSION WAS NORMAL. RECEIVED NO WOW INPUT Jul 2, 2018 · N925EV · Cndair CL6002B19 · Landing Gear Position and WarningSDR SWIA2018060444656Priority Valve · failedAFTER TAKE OFF, DURING GEAR RETRACTION, NOSE GEAR FAILED TO RETRACT. NOSE GEAR INDICATION SHOWED DOWN WITH MAINS UP. FOLLOWED QRH PROCEDURE, ALL THREE GEAR SHOWED DOWN AND LOCKED. REMOVED AND REPLACED THE MLG SELECTOR VALVE AND MLG PRIORITY VALVE PN 4619-3,May 14, 2018 · N925EV · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR SWIA2018051444656Unknown · malfunctionedAFTER TAKE OFF, DURING GEAR RETRACTION, NOSE GEAR FAILED TO RETRACT. NOSE GEAR INDICATION SHOWED DOWN WITH MAINS UP. FOLLOWED QRH PROCEDURE, ALL 3 GEAR SHOWED DOWN AND LOCKED. (FLT 5195) FO: 05/14/2018 WORK IN PROGRESS.May 14, 2018 · N925EV · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR SWIA201844170Skin · dentedRIGHT FUSELAGE SKIN DENTED. APPLIED AERODYNAMIC FILLER TO DENT IAW SRM.Jan 16, 2018 · N925EV · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA201744171Seal · corrodedCORROSION ON PASSENGER DOOR SEALS. REMOVED CORROSION IAW SRM 51-21-06.Dec 17, 2017 · N925EV · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA201744173Thrust Reverser · chafedENGINE THRUST REVERSER CHAFED. R & R THE THRUST REVERSER IAW AMM.Dec 8, 2017 · N925EV · Cndair CL6002B19 · Engine Thrust ReverserSDR SWIA201744172Floorbeam · corrodedCORROSION ON FLOORBEAM. R & R THE FLOORBEAM IAW SRM.Dec 8, 2017 · N925EV · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA201744175Floorbeam · corrodedFLOORBEAM CORRODED. R & R THE FLOORBEAM IAW REO.Dec 7, 2017 · N925EV · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA201744174Floor Support · corrodedFLOOR SUPPORT CAP CORRODED. R & R THE FLOOR SUPPORT IAW REO.Dec 7, 2017 · N925EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA201744176Skin · chafedRIGHT AILERON SURFACE CHAFED. R & R THE AILERON SKIN IAW SRM.Dec 5, 2017 · N925EV · Cndair CL6002B19 · AileronsSDR ASOA2015072513386Oil System · overservicedHOT RT ENGINE OIL TEMP 170-175 ON DEPARTURE. COMPLIED WITH QRH. TEMP DID NOT DECREASE WITH THRUST REDUCTION. SHUTDOWN RT ENGINE TO COMPLY WITH QRH. LANDING WEIGHT APPROXIMATELY 46,000 LBS RT OIL PRESSURE 50-42 PSI. LANDING A/S 154 KTS, ACFT RETURNED TO DJul 25, 2015 · N925EV · Cndair CL6002B19 · Turbine Engine Oil SystemSDR ASOA2015070613264Lamp · burned outFWD RT EMGERGENCY LIGHT INOPERATIVE. TROUBLESHOT AND FOUND FWD RT EMERGENCY LIGHT BULB BLOWN. R & R LAMP IAW AMM 33-51-21-400-801. PERFORMED OPS CHECK OF RT FWD EXTERNAL EMERGENCY LIGHT IAW AMM 33-51-00-710-801. OPS TEST GOOD.Jul 1, 2015 · N925EV · Cndair CL6002B19 · Emergency LightingSDR ASOA2015070213258Sign · misinstalledLEFT AND RT LIGHTED FLOOR LEVEL EXIT SIGN FOR LT AND RT EMERGENCY OVERWING EXIT INSTALLED ON WRONG SIDE. REMOVED LT & RT LIGHTED EXIT SIGNS BY OVERWING EXITS IAW AMM 33-51-10-000-801. REINSTALLED ON CORRECT SIDES THE LT & RT LIGHTED FLOOR LEVEL EXIT SIGN IAWJul 1, 2015 · N925EV · Cndair CL6002B19 · Emergency LightingSDR ASOA2015070213245Fitting · crackedCRACKED FITTING FOUND AT FS 319. REMOVED FITTING AT FS 319, STR 18 RT IAW SRM 51-42-21. LOCATED AND DRILLED FITTING AT FS 319, STR 18 RT IAW SRM TASK 51-40-11. INSTALLED NEW FITTING AT FS 319, STR 18, RT, PN: 601R38335-15 IAW SRM 51-77-00-00 T/R 51-32 AND 5Jun 18, 2015 · N925EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2015070213257Floor Support · corrodedRT FLOOR SILL AT FS 349 THROUGH FS 364 IS CORRODED. CUT FLOOR SILL AS SHOWN IN FIG 1 IAW GREO 601R-53-21-2633 AND IAW REO 601R-53-21-326. COMPLIED WITH REO 601R-53-21-2633, REV 10 & REO 601R-53-21-326, REV NC. REO 601R-53-21-2633 HAS BEEN ACCOMPLISHED AND AJun 16, 2015 · N925EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2015070613263Channel · crackedFS 621-FS 625 INTERCOSTAL "V CHANNEL" AT STR 13L IS CRACKED ON OTBD FLANGE THAT ATTACHES TO FUSELAGE SKIN IN AFT END OF RADIUS. REMOVED FS 621-625 INTERCOSTAL U-CHANNEL AT STR 13 IAW SRM'S 51-42-06 AND 51-42-21. INSTALLED QTY 3, HI-LITES IN INTERCOSTAL U-CHAJun 13, 2015 · N925EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2015070213256Channel · crackedINDICATIONS NOTED AT FS 409+128, WL 69.0, RBL 18, CHANNEL 50 PERCENT FULL SCREEN HEIGHT, APPROXIMATELY .200" LONG AND RBL 18 OTBD CHANNEL 50 PERCENT FULL SCREEN HEIGHT .100" LONG IN RADIUS, FAILING NDT INSPECTION. REMOVED FS 409+128 POST IAW SRM 51-42-06. FAJun 13, 2015 · N925EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2015070213255Channel · crackedINDICATION NOTED AT FS 409+128, WL 69.0, LBL 18 INBD CHANNEL 55 PERCENT FULL SCREEN HEIGHT APPROXIMATELY .250" LENGTH IN RADIUS, FAILING NDT. REMOVED POST ASSEMBLY AT FS 409+128 LBL 19 IAW SRM 51-42-06. INSTALLED POST ASSY AT FS 409+128, LBL 18 IAW SRM TASK Jun 13, 2015 · N925EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2015070213254Intercostal · crackedFS 621 - 625 INTERCOSTAL "V CHANNEL" AT STR 14L IS CRACKED ON OTBD FLANGE THAT ATTACHES TO FUSELAGE SKIN IN AFT END OF RADIUS. REMOVED "U" CHANNEL AT STR 14L IAW SRM 51-42-21. LOCATED NEW FASTENER HOLES ON NEW SERVICEABLE U-CHANNEL IAW SRM 51-40-11. INSTALLJun 13, 2015 · N925EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2015070213253Bulkhead Web · crackedREAR PRESSURE BULKHEAD WEB THAT SURROUNDS THE LINTEL ATTACHMENT FITTING, HAS INDICATION NOTED, APPROXIMATELY .500" IN LENGTH 90 PERCENT FSH FAILED NDT INSPECTION. COMPLIED WITH EC/TC REO 601R-53-61-1230 & GREO 601R-53-61-1230, REV F.Jun 12, 2015 · N925EV · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA2015070213252Bulkhead Web · crackedREAR PRESSURE BULKHEAD WEB HAS INDICATIONS NOTED AT BL 0.0, WL 112, APPROXIMATELY 3.0" IN LENGTH, 50 PERCENT FSH FAILED NDT INSPECTION. COMPLIED REO 601R-53-61-1285. FINISHED REPAIR PART IAW REO 601R-53-61-1285. COMPLIED WITH REO 601R-53-61-1285. REMOVED SJun 12, 2015 · N925EV · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA2015070613262Angle · corrodedSERVICE DOOR LOWER SILL ANGLE HAS SEVERAL AREAS OF CORROSION. REMOVED UNSERVICEABLE SERVICE DOOR LOWER SILL ANGLE, PN:601R38303-253 IAW SRM 51-42-13, 51-42-06 AND 51-42-21. LOCATED AND DRILLED NEW SERVICEABLE SERVICE DOOR LOWER SILL ANGLE, PN:601R38303-253 IJun 11, 2015 · N925EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
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