N738EV

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 = 'N738EV' 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 SWI2025F00385Stand Off · crackedR/H LWR TRANSCOWL INBD "A" BRACKET STANDOFF IS CRACKED (C-CHECK RO 3/14/2025) REMOVED AND REPLACED I/B STAND-OFF ANGLE P/N CN624-2082-201 ON R/H LOWER TRANSCOWL, REF. REO 670-54-21-971, REV. B, 2023-11-28. COMPLIED WITH MAJOR REPAIR M-337 AND SKY CARD Nov 19, 2024 · N738EV · Cndair CL6002C10 · Engine Thrust ReverserSDR SWI2025F00384Stand Off · crackedR/H UPPER TRANSCOWL OTBD "A" BRACKET STANDOFF IS CRACKED (C-CHECK RO 3/14/2025) INSTALLED 1 EA. NEW A-BRACKET P/N CN624-2082-201 ON OTBD. SIDE OF R/H UPPER TRANSCOWL. REF. REO 670-54-21-971, REV. B, 2023-11-28. COMPLIED WITH STEPS 1-3 AND 51-900-1002-SNov 19, 2024 · N738EV · Cndair CL6002C10 · Engine Thrust ReverserSDR SWIA2025031701119Stand Off · crackedR/H UPPER TRANSCOWL INBD "A" BRACKET STANDOFF IS CRACKED (C-CHECK RO 3/14/2025) INSTALLED 1 EA. NEW A-BRACKET P/N CN624-2082-201 ON INBD. SIDE OF R/H UPPER TRANSCOWL, REF. REO 670-54-21-971, REV. B, 2023-11-28. COMPLIED WITH STEPS 1-3. AND COMPLIED WITNov 19, 2024 · N738EV · Cndair CL6002C10 · Engine Thrust ReverserSDR SWIA202503171110Structure · crackedFORWARD FUSELAGE JUST AFT OF FS 169.00 LEFT HAND TRU LATCH CUT OUT , SUSPECTED CRACKS ( 2 ). MARKEDMX # 29132843. (C-CHECK RO 3/14/2025) INSTALLED A NEW REPLACEMENT HYDRAULIC BAY SKIN ON THE FWD FUSELAGE USING ALL NEW FASTENERS, REF BOMBARDIER DWG# CCNov 10, 2024 · N738EV · Cndair CL6002C10 · Fuselage Main, StructureSDR SWIA202503171109Skin · gougedR/H OTBD FLAP HAS GOUGE ON LWR SURFACE INBD OF CENTER FARING @ 41/2" FROM T/E (C-CHECK RO 3/14/2025) CUT OUT DAMAGE AND PERFORMED SKINS AND PLATINGS, METALLIC OUTBOARD FLAP REPAIR TYPE III. REF. CRJ700 SRM 57-53-01-201-001-A01 REPAIR TYPE III.COMPLIED WNov 9, 2024 · N738EV · Cndair CL6002C10 · Trailing Edge FlapsSDR SWIA202305090013Windshield · crackedTRANSFER FROM EAML 1131261 : LH WINDSHIELD INNER PANE CRACKED. (FILED CLOSED)REMOVED AND REPLACED THE PILOTS WINDSHIELD PER THE APPLICABLE STEPS OF AMM 56-11-01. OPS AND LEAK CHECK GOOD AT THIS TIMEMay 3, 2023 · N738EV · Cndair CL6002C10 · Flight Compartment WindowsSDR SWIA20230423Seat Track · corrodedR/H SEAT TRACK AT RBL9 BETWEEN FS847.00 TO FS977.00 SEVERAL AREAS HAS CORROSION (MARKED) (C-CHECK RO 5/18/2023) REMOVED AND REPLACED RH SEAT TRACK RAIL AT RBL9.00 BETWEEN FS847.00 TO FS977.00 REF CRJ700 AMM 53-00-49-000-801-A03 & 53-00-49-400-801-A03Apr 23, 2023 · N738EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA202304240003Unknown · smokeUPON TOUCHDOWN IN SAF, THE ENTIRE CABIN WAS FILLED WITH A SMOKE LIKE SCENT. WE NOTICED THE SMELL IN THE FLIGHT DECK AS WELL. (FLT 4989 FILED OPEN)THIS IS CURRENTLY A WORK IN PROGRESSApr 23, 2023 · N738EV · Cndair CL6002C10 · Air Conditioning SystemSDR SWIA202157727Window Post · crackedTRANSFERRED FROM ML 22676393 CRACK FOUND ON THE RH SIDE POST TOP HOLE, CRACK APPEARS TO BE DOWN TO THE NUT PLATE. PER GMM 3-26 THIS HAS BEEN DETERMINED TO BE A MAJOR REPAIR AND FORM M-337 WILL BE REQUIRED (FILED CLOSED) REMOVED AND REPLACED DAMAGED RTApr 23, 2021 · N738EV · Cndair CL6002C10 · Fuselage Main, StructureSDR SWIA202156754Attach Bracket · crackedR/H SLAT CANNISTER 1-3 AFT ATTACH BRACKET IS CRACKED AT BOTTOM OF WELD. (C-CHECK) RO 3/8/2021 REPAIRED R/H SLAT CANNISTER 1-3 AFT ATTACH BRACKET REF BOMBARDIER GENERIC REO 670-57-42-577 REV -- DATE 2016-12-02 AND CRJ700 SRM 51-42-21-001-001-A01. COMPLIEJan 27, 2021 · N738EV · Cndair CL6002C10 · Wing, Attach FittingsSDR SWIA202156753Attach Bracket · crackedL/H SLAT CANNISTER 1-3 AFT ATTACH BRACKET IS CRACKED AT BOTTOM OF WELD. (C-CHECK) RO 3/8/2021 REPAIRED L/H SLAT CANNISTER 1-3 AFT ATTACH BRACKET, COMPLIED WITH ALL STEPS BOMBARDIER GENERIC REO 670-57-42-577 REV -- DATE 2016-12-02 AND COMPLIED WITH TASK CJan 27, 2021 · N738EV · Cndair CL6002C10 · Wing, Attach FittingsSDR SWIA202156752Angle · corrodedFOUND CORROSION ON REINFORCING ANGLE ON FS379.00 AT STGR 22R (C-CHECK) RO 3/8/2021 REMOVED AND REPLACED REINFORCEMENT ANGLE P/N SH670-32119-1 COMMON TO FRAME AT FS 379.00 REF CRJ700 SRM 51-42-06-001-001-A01 AND DWG# SH670-32050 REV J DATE 2012/08/09. COMJan 22, 2021 · N738EV · Cndair CL6002C10 · Fuselage Main, FrameSDR SWIA202156751Frame · corrodedFS319.70 FRAME HAS EXISTING CORROSION ON AFT SIDE CUTOUT OF STGR 26L (C-CHECK) RO 3/8/2021 REMOVED AND REPLACED FRAME FS 319.00 FROM STGR 25L TO 24R REF CRJ700 SRM 53-00-06-201-006-A01 AND SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01. COMPLIED WIJan 21, 2021 · N738EV · Cndair CL6002C10 · Fuselage Main, FrameSDR SWIA202156750Frame · corrodedFOUND CORROSION ON R/H AFT SIDE OF FRAME AT F.S.379.00 AT STGR 21R (MARKED). (C-CHECK) RO 3/8/2021 REMOVED AND REPLACED FRAME AT FS 379.00 REF DWG SH670-32050 REV J AND REF CRJ700 SRM 51-42-06-001-001-A01. COMPLIED WITH TASK CARD 51-900-1002-SKY. LEAK CHEJan 21, 2021 · N738EV · Cndair CL6002C10 · Fuselage Main, FrameSDR SWIA202156748Skin · crackedCRACK FOUND ON SKIN COMMUN TO ONE OF 6 ATTACH POINTS OF LATCH ASSY. REF. CAMP # 22107482 ( JOB 1, OP. 274) (C-CHECK) RO 3/8/2021 DAMAGE ON SKIN REPAIRED. REF. REO 670-54-21-1419 REV.-- DATED 2021-01-21Jan 17, 2021 · N738EV · Cndair CL6002C10 · Nacelle/Pylon, Plate/SkinSDR SWIA202156747Coaming · chafedLH LWR TRANS COWL LATCH DOOR COAMING IS CHAFFED. (C-CHECK) RO 3/8/2021 INSTALLED NEW L/H LWR TRANS COWL DOOR COAMING. / ALL STEPS COMPLIED WITH IN BOMBARDIER REO 670-54-21-1207 REV A DATED 2015-08-27 / COMPLIED WITH 51-900-1002 SKYJan 16, 2021 · N738EV · Cndair CL6002C10 · Engine Thrust ReverserSDR SWIA202156746Skin · crackedLH UPPER TRANSCOWL, I/B STAND-OFF CRACKED AT FASTENER HOLE. (C-CHECK) RO 3/8/2021 INSTALLED NEW STANDOFF PN 624-2082-201. REF GREO 670-54-21-971. REV. A DATED 2017/05/11 / COMPLIED WITH TASK CARD 51-900-1002-SKY AND COMPLETED M-337Jan 7, 2021 · N738EV · Cndair CL6002C10 · Nacelle/Pylon, Plate/SkinSDR SWIA202156745Floorbeam · corrodedFLOOR SILL, F.S. 280 TO SERVICE DOOR CUTOUT APPEARS CORRODED. (C-CHECK) RO 3/8/2021 REMOVED CORROSION AT FLOOR SILL AT FS 280 TO SERVICE DOOR CUTOUT REF CRJ 700 SRM 51-21-06-001-001-A01. 100% MATERIAL LOSS OUT OF LIMITS REF CRJ 700 SRM 53-00-45-201-001-A0Jan 7, 2021 · N738EV · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR SWIA202156744Lintel · crackedFS285 STRG3L LINTEL FOUND CRACKED. COMPLY WITH SB 670BA-53-040 REV: C DATED 09/20/2012 (C-CHECK) RO 3/8/2021 COMPLIED WITH PERMANENT REPAIR OF THE LINTEL STRIGER 3L IAW SB NO. 670BA-53-040 REV C DATED 09/20/2012 WITH THE INCORPORATION OF REO NO. 670-53-21Jan 4, 2021 · N738EV · Cndair CL6002C10 · Fuselage Main, StructureSDR SWIA202156743Floorbeam · crackedSUSPECT CRACK IN THE RADIUS OF THE COCKPIT FLOORBEAM AT LBL12 ON THE FWD SIDE OF THE FS280 BULKHEAD (C-CHECK) RO 3/8/2021 REPAIREDCOCKPIT FLOORBEAM AT LBL 12 FWD OF FS 280 REF CRJ-700 SRM 53-11-43-201-003-A01 REV 38 DATED JUL 25/2020 & CRJ-700 SRM 51-42-Jan 4, 2021 · N738EV · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR SWIA202056742Stringer · corrodedCORROSION ON STRINGER 21R FS379 BUT ACTUALLY ON TIE IN CLIP (C-CHECK) RO 3/8/2021 REMOVED AND REPLACED TIE CLIP P/N SH670-32301-5 PER REF DWG BOMBARDIER INC, CANADAIR SH670-32280 REV H AND REF CRJ700 SRM 51-42-06-001-001-A01 COMPLIED WITH SKY CARD 51-900Dec 24, 2020 · N738EV · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA202056741Skin · corrodedUPON REMOVAL OF EXISTING DOUBLERS AT STA 977 STR 27 FOUND CORROSION AT AFT END OF DOUBLER FOOPRINT COMMON TO FAIRING ATTACHMENT AT STA 985 STR 26L-26R (C-CHECK) RO 3/8/2021 REPAIRED CORROSION DAMAGE IAW REO 670-53-61-1806 REV -- DATED 2021-01-14 COMPLIEDDec 22, 2020 · N738EV · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR SWIA202056758Anchor Fitting · corrodedPASSENGER DOOR FORWARD AND AFT ANCHOR FITTINGS HAVE MISCELLANEOUS CORRODED HARDWARE, FS310.00 & FS349.00. (C-CHECK) RO 3/8/2021 REMOVED AND REPLACED CORRODED HARDWARE ON PASSENGER DOOR FORWARD AND AFT ANCHOR FITTINGS AS PER CRJ 700 AMM 52-11-17-400-804Dec 19, 2020 · N738EV · Cndair CL6002C10 · Passenger/Crew DoorsSDR SWIA202056740Floor Support · corroded*FLOOR SUPPORT, FS1051.30 €“ RBL40.0, IS CORRODED. (MARKED) (C-CHECK) RO 3/8/2021 REPAIRED FS1051 FLOOR BEAM AT RBL40 IAW CRJ700 REO 670-53-61-1805 REV-- 2021-02-03, CRJ-700 SRM 51-42-06-001-001-A01, CRJ-700 SRM 51-42-21-001-001-A01, CRJ700SRM 51-23-00-Dec 18, 2020 · N738EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA202056739Floor Support · gouged*RBL9 FLOOR BEAM OUTBOARD FLANGE GOUGED, FS863.00 €“ FS953.00. (MARKED) (C-CHECK) RO 3/8/2021 REPAIRED DAMAGED FLOOR BEAM AT RBL9 FS 855-885 IAW CRJ700 SRM 53-00-41-201-001-A01 FIG 53-00-41-991-830. COMPLIED WITH 51-900-1002-SKY ( CL600-2C10), AND M-Dec 18, 2020 · N738EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA202056738Floor Support · corroded*RIGHT HAND FLOOR SILL IS CORRODED AT THE FORWARD END FS969.00 €“ FS985.00. (MARKED) (C-CHECK) RO 3/8/2021 REMOVED AND INSTALLED NEW RH FLOOR SILL P/N SH670-31518-1 BETWEEN FS969.00 - FS985.00 REF CRJ700-SRM51-42-06-001-001-A01 AND DWG SH670-32170, REV Dec 18, 2020 · N738EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA202056737Plate · corroded*FORWARD AND AFT LOWER JOINT PLATES FOR THE FORWARD BAGGAGE BAY SURROUND STRUCTURE HAVE CORROSION, FS536.00 & FS575.00, STGR25L (MARKED) (C-CHECK) RO 3/8/2021 REMOVED AND REPLACED FWD AND AFT LWR JOINT PLATE AT FS 536.00 AND FS 575.00 STGR 25L REF CRJ700 Dec 17, 2020 · N738EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA202056736Floorbeam · cracked*SUSPECT CRACK IN THE RADIUS OF THE COCKPIT FLOORBEAM AT RBL12 ON THE FWD SIDE OF THE FS280 BULKHEAD/CROSSBEAMS (FLAGGED) (C-CHECK) RO 3/8/2021 REPAIRED COCKPIT FLOORBEAM AT RBL 12 FWD OF FS 280 REF CRJ-700 SRM 53-11-43-201-003-A01 REV 38 DATED JUL 25/20Dec 16, 2020 · N738EV · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR SWIA202056735Floor Support · corroded*PRESSURE FLOOR STRUCTURE €ŒFLOOR BEAM€? AT RBL9 BETWEEN APPROX. FS693 AND FS847 HAS CORROSION(MARKED). (C-CHECK) RO 3/8/2021 REMOVED CORROSION AND COMPLIED WITH REO 670-53-41-505 REV--, 2021-01-14 AND, / COMPLIED WITH TASK CARD 51-900-1002-SKYDec 16, 2020 · N738EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA202056734Stringer · corroded*STRINGER, STGR21R, NOTED CORROSION BETWEEN FS364 AND FS379 (MARKED). (C-CHECK) RO 3/8/2021 REMOVED AND REPLACED STGR 21R, REF (DWG SH670-31383, REV NC, DATED 29-8-98) AND (CRJ700 SRM 51-42-06-001-001-A01). RESTORED FINISH REF CRJ700 SRM 51-25-01-001-0Dec 16, 2020 · N738EV · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA202056733Plate · corroded*AVIONICS BAY DOOR SURROUND: JOINT PLATE ON THE FS364 FRAME AND STGR25L LONGERON IS CORRODED (MARKED). (C-CHECK) RO 3/8/2021 REPLACED A-BAY DOOR SURROUND JOINT PLATE WITH A NEW ONE. REF: CRJ-700 SRM 51-42-21-001-001-A01, REO-670-53-21-1934 REV -- DATE 202Dec 16, 2020 · N738EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA202056732Plate · corroded*AVIONICS BAY DOOR SURROUND: JOINT PLATE ON THE FS364 AND STGR25R LONGERON IS CORRODED (MARKED). (C-CHECK) RO 3/8/2021 REPLACED AVIONICS BAY DOOR SURROUND: JOINT PLATE ON THE FS364 AND STGR25R LONGERON. REF. DWG SH670-32050 REV. D / COMPLIED WITH 51-900-1Dec 16, 2020 · N738EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA202056731Stringer Splice · corroded*FS333 JOINT, STRINGER SPLICE AT STGR25L HAS CORROSION (MARKED). (C-CHECK) RO 3/8/2021 CORROSION ON STRINGER SPLICE AT STRINGER 25L FS 333 ASSESSED. NO DAMAGE ALLOWED IN AREA. REF CRJ700 SRM 53-21-03-101-002-A01. REPLACED JOINT SPLICE STRIP WITH NEW PART Dec 16, 2020 · N738EV · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA202056730Stringer · corroded*STRINGER, STGR26R, HAS CORROSION BETWEEN FS280 AND FS310. (MARKED) (C-CHECK) RO 3/8/2021 REMOVED AND REPLACED STGR 26R FS 280.00 TO FS 333.00 REF CRJ700 SRM 51-42-06-001-001-A01 AND AND DWG# SH670-31630 REV J AND RESTORED FINISH REF CRJ700 SRM 51-21-06-0Dec 16, 2020 · N738EV · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA202056729Stringer · corroded*STRINGER, STGR27, HAS CORROSION JUST AFT OF THE FS295 FRAME. (MARKED) (C-CHECK) RO 3/8/2021 REPLACED STGR27 FROM FS295 - FS280 P/N SH670-31642-1 REF. CRJ 700 SRM 51-42-06-001-001-A01 AND CRJ 700 SRM 51-42-20-001-001-A01 AND DWG SH670-31630 REV NC. LEAK CDec 16, 2020 · N738EV · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA202056728Stringer · corroded*STRINGER, STGR19R, HAS CORROSION BETWEEN FS280 AND FS295. (MARKED) (C-CHECK) RO 3/8/2021 CORROSION AT STRINGER 19R BETWEEN FS 280 TO FS 295. CORRODED ALL THE WAY THROUGH NO DAMAGE ALLOWED. REPLACED DAMAGED PORTION OF STRINGER REF CRJ 700 SRM 53-00-03--20Dec 16, 2020 · N738EV · Cndair CL6002C10 · Fuselage Main, StructureSDR SWIA202056727Intercostal · corroded*GALLEY SERVICE DOOR SURROUND STRUCTURE, INTERCOSTAL AT STGR20R, BETWEEN FS310 TO FS319 IS CORRODED. (MARKED) (C-CHECK) RO 3/8/2021 REMOVE AND REPLACED INTERCOSTAL AT STGR 20R BWTN FS 310.00 TO 319.00 REF DWG SH670-32047 REV NC AND REF CRJ700 SRM 51-42-21Dec 16, 2020 · N738EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA202056726Door Sill · corroded*PASSENGER DOOR SURROUND, BACK-UP SILL AT STRG21L, BETWEEN FS310 AND FS333 IS CORRODED. (MARKED) (C-CHECK) RO 3/8/2021 REPLACED PASSENGER DOOR SURROUND, BACK UP SILL AT STGR 21L BETWEEN FS310-FS333 WITH NEW. REF CRJ-700 SRM 51-42-21-001-001-A01, CRJ-700 SDec 16, 2020 · N738EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA202056725Doubler · chafed*DOUBLER UNDER PNLS.195DR/DL CHAFED IN SEVERAL AREAS. (MARKED) (C-CHECK) RO 3/8/2021 REPAIRED DAMAGED DOUBLER IAW REO 670-53-00-290 REV F DATED 2019/04/26. PRESSURE LEAK CHECK GOOD. COMPLIED WITH TASK CARD 51-900-1002-SKY.Dec 15, 2020 · N738EV · Cndair CL6002C10 · Fuselage Main, StructureSDR SWIA202056757Hinge Fitting · corrodedRIGHT WING OUTBOARD FLAP - OUTBOARD FORWARD HINGE BOX SUPPORT FITTING HAS CORRODED HARDWARE. (C-CHECK) RO 3/8/2021 REPLACED RH WING OUTBOARD FLAP, OUTBOARD FORWARD HINGE BOX SUPPORT FITTING CORRODED HARDWARE WITH NEW REF CRJ-700 AMM 57-54-02-400-808-A01, Dec 11, 2020 · N738EV · Cndair CL6002C10 · Trailing Edge FlapsSDR SWIA202056756Hinge Fitting · corrodedLEFT WING OUTBOARD FLAP - INBOARD AFT LOWER HINGE LUG FITTING HAS CORRODED HARDWARE. (C-CHECK) RO 3/8/2021 REMOVED LEFT WING OUTBOARD FLAP - INBOARD AFT LOWER HINGE LUG FITTING HARDWARE REF CRJ700 AMM 57-53-27-000-801(CONFIG A01) STEPS 4.A(2)(3)(4)(5)(6)(Dec 11, 2020 · N738EV · Cndair CL6002C10 · Trailing Edge FlapsSDR SWIA202056755Hinge Fitting · corroded*LEFT WING OUTBOARD FLAP - OUTBOARD AFT LOWER HINGE LUG FITTING HAS CORRODED HARDWARE. (C-CHECK) RO 3/8/2021 REMOVED LEFT WING OUTBOARD FLAP - OUTBOARD AFT LOWER HINGE LUG FITTING HARDWARE REF CRJ700 AMM 57-53-27-000-803 (CONFIG A01) STEPS 4.A.(4)(5)(6). Dec 11, 2020 · N738EV · Cndair CL6002C10 · Trailing Edge FlapsSDR ASOA201810084063Light · inoperativeSBN - FLIGHT 2986 MAINTENANCE INSPECTIOON DISCOVERED THE NR 1 INTERIOR OVERHEAD EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT BULB, OPERATIONALLY TESTED WITH NO DEFECTS AND THE AIRCRAFT WAS APPROVED FOR RETURNOct 8, 2018 · N738EV · Cndair CL6002C10 · Emergency LightingSDR ASOA201707315096Ground Wire · unsecureDURING MX INSPECTION, THE GALLEY FLOOR EMERGENCY EXIT SIGN WOULD NOT ILLUMINATE. MX SECURED GROUND WIRE FOR CONNECTOR P372 WITH OPERATIONAL CHECK GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.Jul 31, 2017 · N738EV · Cndair CL6002C10 · Emergency LightingSDR ASOA201707311814Ground Wire · unsecureGALLEY FLOOR. NEXT TO SERVICE DOOR, EMERGENCY EXIT SIGN WILL NOT ILLUMINATE. SECURED THE GROUND WIRE FOR CONNECTOR P372 IAW AMM 20-23-00. EMEGENCY LIGHTS OPS CHECKED GOOD IAW AMM 33-51-00.Jul 31, 2017 · N738EV · Cndair CL6002C10 · Light System WiringSDR ASOA201703195027Relay · faultyEMERGENCY LIGHTS CYCLING ON AND OFF WITH GROUND POWER AND APU POWER. CONTRACT MX REMOVED AND REPLACED RELAY K135 WITH OPERATIONAL CHECK GOOD. A/C WAS APPROVED FOR RETURN TO SERVICE.Mar 19, 2017 · N738EV · Cndair CL6002C10 · Emergency LightingSDR ASOA201703193052Relay · inoperativeTHE CREW REPORTED EMERGENCY LIGHTS ARE CYCLING ON AND OFF WITH GROUND POWER AND APU POWER. MAINTENANCE REPLACED THE RELAY KJ35 IAW ESPM 20-39-00. OPS CHECKED GOOD.Mar 19, 2017 · N738EV · Cndair CL6002C10 · Emergency LightingSDR ASOA201702281275Floorbeam · corrodedFLOORBEAM CORRODED LBL9 FS 1031.00. REPAIRED FLOORBEAM IAW EC/TC REO 670-53-61-1331 AND REO 670-53-61-1331 AND EC/TC EO 700-53-10-00017, EO 700-53-10-00017.Feb 28, 2017 · N738EV · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR ASOA201702271268Seat Track · corrodedLEFT SEAT TRACK RETAINER BS 673 - 720 CORRODED. COMPLIED WITH EC/TC EA 25-2017-026 AND EA 25-2017-026.Feb 27, 2017 · N738EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201702271267Seat Track · corrodedLEFT SEAT TRACK RETAINER BS 783 - 854 CORRODED. COMPLIED WITH EC/TC EA 25-2017-027 AND EA 25-2017-027.Feb 27, 2017 · N738EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
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