N540EG

Service difficulty reports · 111

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 = 'N540EG' 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 WRXR20241209002Stringer Clip · corrodedCORROSION FOUND ON RH, STRG CLIP COMMON TO STRINGER 20R, INTERCOSTAL PART # SH670- 32004-1 AND FRAME PART # SH670-32029 -2 AT FS319.70. REMOVED AND REPLACED WITH NEW, STRG CLIP, RH, PART # SH670-32045-1 COMMON TO STRINGER 20R, INTERCOSTAL PART # SH670- 32004-Dec 9, 2024 · N540EG · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR WRXR20241209001Skin · chafedRH WS128 HAS CHAFFING ON WING LOWER SKIN COMMON TO THE 686AB FAIRING SEAL. BLENDED RH WS128 WING LOWER SKIN COMMON TO THE 686AB FAIRING SEAL IAW CRJ 700 SRM 51-12-00-001-A01. NDI REPORT F281024.PDF IN ATTACHMENTS, NO CRACKS NOTED. SHOT-PEEN REWORKED AREA IAW CDec 9, 2024 · N540EG · Cndair CL6002C10 · Wing, Plate/SkinSDR WRXR20241206004Stringer · corrodedMODERATE CORROSION AT RH STRINGER SPLICE 24 AND FWD OF FS333.00. REMOVED AND REPLACED SPLICE JOINT PIECE PN: SH670-32429-4S, WITH NEW IAW CRJ700 SRM 51-42-00 AND SRM 51-42-06-001-001-A01.Dec 6, 2024 · N540EG · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR WRXR20241206003Intercostal · corrodedINTERCOSTAL C/T STRINGER 20R, BETWEEN FRAMES AT FS319.70 AND FS333 HAS SEVERE CORROSION ON THE UPPER FACE. REMOVED INTERCOSTAL PART # SH670-32047-1, IAW CRJ700 SRM 51-42-00 AT FS 310 TO FS 319 COMMON TO RH, STRG 20. INSTALLED NEW INTERCOSTAL PART # SH670-32047Dec 6, 2024 · N540EG · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR WRXR20241206002Skin · chafedRH WS54.55 HAS CHAFFING ON LOWER WING SKIN COMMON TO THE 683AB FAIRING SEAL. BLENDED RH WS54.55 LOWER WING SKIN COMMON TO 683AB FAIRING SEAL IAW CRJ 700 SRM 51-12-00-001-A01. NDI REPORT E281024.PDF IN ATTACHMENTS, NO CRACKS NOTED. ROTO-PEENED REWORKED AREA IAWDec 6, 2024 · N540EG · Cndair CL6002C10 · Wing, Plate/SkinSDR WRXR20241206001Stringer · corrodedSTRINGER 19R AT FS 319 TO FS349 IS CORRODED BEYOND THE SRM LIMITS. REMOVED AND REPLACED STRG 19R, P/N # SH670-32427-1, BETWEEN FS 319 AND FS 349, WITH NEW IAW CRJ 700 SRM 51-42-06-001-001-A01, IAW CRJ 700 SRM 51-23-00-001-001-A01 AND IAW CRJ 700 SRM 51-21-16-0Dec 6, 2024 · N540EG · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR WRXR202405003Intercostal · corrodedINTERCOSTAL C/T STRINGER 20R, BETWEEN FRAMES AT FS310.00 AND FS319.70, BELOW AND FORWARD OF THE SERVICE DOOR LOWER SILL (WL72.50), HAS SEVERE CORROSION ON THE UPPER FACE. INSTALLED NEW INTERCOSTAL PART # SH670-32047-1 AT FS 310 TO FS 319 COMMON TO RH, STRG 20,Dec 5, 2024 · N540EG · Cndair CL6002C10 · Fuselage Main, Attach FittingsSDR WRXR20241205002Channel · corrodedCORROSION FOUND ON THE TCAS CHANNEL PN:SH670-32364-7 BETWEEN FS295 - FS310 AT STR. 27. REMOVED TCAS CHANNEL PN:SH670-32364-7 BETWEEN FS 295 - FS310 AT STR. 27, INSTALLED NEW TCAS CHANNEL PN: SH670-32364-7S IAW CRJ 700 SRM 51-42-06-001-001-A01.Dec 5, 2024 · N540EG · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR WRXR20241205001Skin · corrodedAFT BAGGAGE BAY SURROUND STRUCTURE/ LOWER SILL PN:MM670-35655-003 HAS MULTIPLE AREAS OF CORROSION. REMOVED AND REPLACED AFT BAGGAGE BAY LOWER SILL P/N: MM670-35655-003 IAW CRJ700 SRM 53-61-23-201-003-A01, 51-42-13-001-001-A01, 51-45-00-001-001-A01, 51-42-20-0Dec 5, 2024 · N540EG · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR WRXR2024001Skin · chafedRH WS220 HAS CHAFFING ON WING LOWER SKIN COMMON TO 695AB FAIRING SEAL. BLENDED DAMAGE ON RH LOWER SKIN COMMON TO PANEL 695AB L/E SEAL IAW CRJ 700 SRM 51-12-00-001-A01. REF C281024.PDF IN ATTACHMENTS FOR NDI REPORT, NO CRACKS. ROTO-PEENED REWORKED AREA IAW CRJ7Dec 4, 2024 · N540EG · Cndair CL6002C10 · Wing, Plate/SkinSDR WRXR20241203006Splice · corrodedFOUND MODERATE CORROSION AT RH STRINGER 23 AND FWD OF FS333.00. REMOVED AND INSTALLED NEW JOINT SPLICE SH670-32429-4S ON STRG 23R FS. 333 IAW CRJ 700 SRM 51-42-06-001-001-A01, IAW CRJ 700 SRM 51-23-00-001-001-A01 AND IAW CRJ 700 SRM 51-21-16-001-001-A01.Dec 3, 2024 · N540EG · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR WRXR20241203005Skin · elongatedTHE SLAT NO.2 AFT SKIN WAS FOUND TO HAVE ELONGATED FASTENER HOLE THROUGH PANEL CC670-12717-2 AND IN STRUCTURE. FABRICATED AND INSTALLED REPAIR DOUBLER STRAP IAW CRJ700 EA NO. A1-670-57-00060 REV A.Dec 3, 2024 · N540EG · Cndair CL6002C10 · Leading Edge DevicesSDR WRXR20241203004Panel · damagedGOUGE FOUND ON R/H I/B PANEL 684JB 1 5/16" X 1/16", .009 DEEP. BLENDED RH I/B PANEL 684JB IAW CRJ700 SRM 51-12-00-001-001-A01. NDI NO CRACKS. REPAIRED IAW REO 670-57-52-583, REV --.Dec 3, 2024 · N540EG · Cndair CL6002C10 · Trailing Edge FlapsSDR WRXR20241203003Panel · chafedCHAFING FOUND ON L/H I/B PANEL 584HT. BLENDED LH I/B PANEL 584HT IAW CRJ700 SRM 51-12-00-001-001-A01. NDI NO CRACKS. REPAIR COMPLIED WITH IAW EA A1-670-57-00079.Dec 3, 2024 · N540EG · Cndair CL6002C10 · Trailing Edge FlapsSDR WRXR20241203002Skin · chafedCHAFING FOUND ON R/H I/B PANEL 684LB. PERFORMED BLENDING ON RH I/B PANEL 684LB IAW CRJ700 SRM 51-12-00-001-001-A01. NDI, JOB NO. K211024, NO CRACKS NOTED. PERFORMED REPAIR IAW REO 670-57-52-582, REV --.Dec 3, 2024 · N540EG · Cndair CL6002C10 · Trailing Edge FlapsSDR WRXR20241203001Panel · chafedCHAFING FOUND ON LH I/B FLAP PANEL 584EB. PERFORMED BLENDING ON LH I/B FLAP PANEL 584EB IAW CRJ700 SRM 51-12-00-001-001-A01. PERFORMED NDI, NO CRACKS NOTED.Dec 3, 2024 · N540EG · Cndair CL6002C10 · Trailing Edge FlapsSDR WRXR202402002Support Splice · corrodedCORROSION FOUND ON STRINGER 21R FACTORY SPLICE JOINT @FS333. REMOVED AND REPLACED PART # SH670-32429-4S. ACCOMPLISHED AND COMPLETED IAW CRJ700 SRM 51-42-06-001-001-A01.Dec 2, 2024 · N540EG · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR WRXR20241202001Support Angle · corrodedFOUND AFT BELLY FAIRING SUPPORT ANGLE, PN:SH670-39189-1, TO BE CORRODED AND OUT OF LIMITS. REMOVED AND REPLACED ANGLE P/N SH670-39189-1 CENTERED BETWEEN LH AND RH AFT FAIRING SUPPORT FRAMES AT FS 939 IAW CRJ 700 SRM 51-42-06-001-001-A01.Dec 2, 2024 · N540EG · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR WRXR20241119001Seat Track · corrodedMULTIPLE AREAS OF CORROSION FOUND ON RH FLOOR SEAT, FS571.00 TO FS683.00, RBL9.00, RAIL #51. REMOVED SEAT TRACK # 51 IAW CRJ 700 AMM 53-00-49-000-801-A03. FABRICATED SEAT TRACK IAW CRJ700 REO 670-53-00-589 REV C. INSTALLED SEAT TRACK #51 IAW AMM 53-00-49-400-8Nov 19, 2024 · N540EG · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR WRXR20241115004Flap · gougedCHAFING FOUND ON RH I/B FLAP PANEL 684ET. PERFORMED BLENDING ON RH I/B FLAP PANEL 684ET IAW EA# A1-670-57-00066 REV-- REV DATE 2024-11-08. PERFORMED NDI, NO CRACKS NOTED. APPLIED ALODINE-BONDERITE, M-CR 1132, PB31454331, EXP:04/03/25. REMOVED AND REPLACED FANov 15, 2024 · N540EG · Cndair CL6002C10 · Wing, Control SurfacesSDR WRXR20241113001Seat Track · corrodedMULTIPLE AREAS OF CORROSION FOUND FOR CENTER FLOOR ( LBL 9.00) SEAT RAIL #50. REMOVED OLD SEAT TRACK IAW CRJ 700 AMM 53-00-49-000-801-A03 FABRICATED SEAT TRACK IAW CRJ700 REO 670-53-00-589 REP C. INSTALLED FABRICATED SEAT TRACK IAW CRJ 700 AMM 53-00-49-400-80Nov 13, 2024 · N540EG · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR WRXR20241108001Seat Track · corrodedMULTIPLE AREAS OF CORROSION FOUND FOR CENTER FLOOR SEAT RAIL #50. REMOVED SEAT TRACK # 50 IAWCRJ 700 AMM 53-0049-000-801-A03. FABRICATED (96 ") OF RH # 50 SEAT TRACK IAW CRJ 700 REO670-53-589 REV. C. INSTALLED SEAT TRACK # 50 IAW CRJ 700 AMM 53-0049-400-801-A0Nov 8, 2024 · N540EG · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR WRXR20241106005Seat Track · corrodedRH FLOOR SEAT TRACK #59 (RBL27.00) HAS MULTIPLE CORRODED FASTENERS AND PITTING AROUND MULTIPLE FASTENER HOLE. REMOVED OLD SEAT TRACK IAW CRJ 700 AMM 53-00-49-000-801-A03. FABRICATED SEAT TRACK IAW CRJ700 REO 670-53-00-589 REV. C. INSTALLED FABRICATED SEAT TRACNov 6, 2024 · N540EG · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR WRXR20241106004Seat Track · corrodedRH FLOOR SEAT TRACK #58 (RBL9.00) HAS PITTING AROUND MULTIPLE FASTENER HOLES. REMOVED OLD SEAT TRACK IAW CRJ 700 AMM 53-00-49-000-801-A03. FABRICATED SEAT TRACK IAW CRJ700 REO 670-53-00-589 REV. C. INSTALLED FABRICATED SEAT TRACK IAW CRJ 700 AMM 53-00-49-400-8Nov 6, 2024 · N540EG · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR WRXR20241106003Seat Track · corrodedRH FLOOR SEAT TRACK #54 (RBL9.00) HAS MULTIPLE AREAS OF NICKS, GOUGES, AND CORROSION. REMOVED OLD SEAT TRACK IAW CRJ 700 AMM 53-00-49-000-801-A03. FABRICATED SEAT TRACK IAW CRJ700 REO 670-53-00-589 REV. C. INSTALLED FABRICATED SEAT TRACK IAW CRJ 700 AMM 53-00-Nov 6, 2024 · N540EG · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR WRXR20241106002Seat Track · corrodedLH FLOOR SEAT TRACK #54 (LBL9.00) HAS MULTIPLE AREAS OF NICKS, GOUGES, AND CORROSION. REMOVED OLD SEAT TRACK IAW CRJ 700 AMM 53-00-49-000-801-A03 FABRICATED SEAT TRACK IAW CRJ700 REO 670-53-00-589 REV. C. INSTALLED FABRICATED SEAT TRACK IAW CRJ 700 AMM 53-00-4Nov 6, 2024 · N540EG · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR WRXR20241106001Seat Track · corrodedMULTIPLE AREAS OF CORROSION FOUND ON RH FLOOR SEAT RAIL #51 (RBL9.00). REMOVED OLD SEAT TRACK IAW CRJ 700 AMM 53-00-49-000-801-A03, FABRICATED SEAT TRACK IAW CRJ700 REO 670-53-00-589 REV. C, INSTALLED FABRICATED SEAT TRACK IAW CRJ 700 AMM 53-00-49-400-801-A03.Nov 6, 2024 · N540EG · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR WRXR20241025002Seat Track · corrodedMULTIPLE AREAS OF CORROSION FOUND FOR RH FLOOR SEAT RAIL #50R. REMOVED SEAT TRACK # 50 IAW CRJ 700 AMM 53-0049-000-801-A03. FABRICATED ( 96 " ) OF RH # 50 SEAT TRACK IAW CRJ 700 REO 670-53-589 REV. C INSTALLED SEAT TRACK # 50 IAW CRJ 700 AMM 53-0049-400-801-A0Oct 25, 2024 · N540EG · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR WRXR20241025001Seat Track · corrodedAREAS OF CORROSION FOUND AND MARKED FOR FLOOR SEAT RAIL #48. REMOVED SEAT TRACK # 48 IAW CRJ 700 AMM 53-0049-000-801-A03. FABRICATED (135 ") OF RH # 48 SEAT TRACK IAW CRJ 700 REO 670-53-589 REV. C, INSTALLED SEAT TRACK # 48 IAW CRJ 700 AMM 53-0049-400-801-A03 Oct 25, 2024 · N540EG · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202306051112Unknown · unknownR BLEED DUCT WARNING IN FLIGHT DURING CLIMBOUT/ AUTOMATICALLY WENT TO R BLEED CAUTION. / PERFORMED T/S PER CRJ 700 FIM 36-10-00-810-828-A01, FOUND LEAK DETECTED AT MT145 / MT146. INSPECTED AIR DUCTS FOUND LOOSE V-BAND CLAMP AT PRSOV2, RE-SECURED V-CLAMP IAW AMJun 3, 2023 · N540EG · Cndair CL6002C10 · Pneumatic SystemSDR VNAA2023012719991Hinge Fitting · damagedLEFT WING IB FWD FLAP HINGE FITTING, HOLES THROUGH WINGPLANK AT W.S. 54.55 ARE REAMED TO .410" AND STILL HAVE DAMAGE IN WING PLANK STRUCTURE INSIDE HOLES.Jan 27, 2023 · N540EG · Cndair CL6002C10 · Trailing Edge FlapsSDR VNAA202205091111Engine · shutdownWHILE ON BASE TO FINAL INTO GRR, THE LEFT ENGINE FAILED AND SHUTDOWN, CAPTAIN VERIFIED THEY DID NOT SHUT THE ENGINE. DUE TO THE PHASE OF FLIGHT (LANDING), THEY CONTINUED ON WITH THE APPROACH AND THE CAPTAIN HAD THE FO CALL BACK TO THE FA TO ASK IF THEY SAW ANYMay 6, 2022 · N540EG · Cndair CL6002C10 · Engine (Turbine/Turboprop)SDR VNAA202002299992Bulkhead Web · crackedFS 280 WEB IS CRACKED OB OF RBL 9. FABRICATED AND DRILLED PARTS IAW CRJ 700 SRM 53-11-10-201-004-A01 AND 51-40-11-001-010-A01.Jan 23, 2020 · N540EG · Cndair CL6002C10 · Fuselage Main, BulkheadSDR VNAA202002299991Crossbeam · corrodedFS 280 CROSSBEAM IS CORRODED OB OF RBL 9 LOCATED,AND DRILLED NEW SERVICEABLE RH FS280 CROSSBEAM IAW CRJ 700 SRM 51-21-06-001-001-A01 AND 51-40-11-001-001-A01.Jan 23, 2020 · N540EG · Cndair CL6002C10 · Fuselage Main, StructureSDR VNAA2020022999910Frame · corrodedIB AND ATTACH ANGLES ON BOTTOM OF KEEL BEAM FOUND TO BE CORRODED.REPAIR OR REPLACEMENT REQUIRED.Jan 20, 2020 · N540EG · Cndair CL6002C10 · Fuselage Main, FrameSDR VNAA202002299999Frame · corrodedKEEL BEAM IN MLG WHEEL WELL HAS CORROSION ON THE BOTTOM AND NICKS ON EDGE.REMOVED CORROSION ON KEEL BEAM ASSY IAW CRJ 700 SRM 51-21-06-001-001-A01,Jan 19, 2020 · N540EG · Cndair CL6002C10 · Fuselage Main, FrameSDR VNAA202002299997Angle · corrodedSERVICE DOOR LOWER MOUNTING ANGLE IS CORRODED.INSTALLED NEW SERVICEABLE SERVICE DOOR LOWER MOUNTING ANGLE IAW CRJ700 SRM 51-42-06-001-001-A01, 51-41-02-001-001-A01 AND 51-42-34-001-001-A01. 51-42-21-001-001-A01Jan 19, 2020 · N540EG · Cndair CL6002C10 · Service DoorsSDR VNAA202002299996Floorbeam · crackedFLIGHT DECK FLOOR BEAM AT RBL 11 IS CRACKED WHERE FS 280 CROSSBEAM ANGLE ATTACHES. LOCATED, DRILLED AND INSTALLED ANGLE IAW CRJ700 SRM'S 51-40-11-001-001-A01, 51-42-06-001-001-A01.Jan 19, 2020 · N540EG · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR VNAA202002299995Frame · crackedFLIGHT DECK FLOOR BEAM AT LBL 11 IS CRACKED WHERE F.S. 280 CROSSBEAM ANGLE ATTACHES. LOCATED, DRILLED & INSTLLED NEW SERVICABLE ANGLE IAW CRJ 700 SRM'S 51-40-11-001-001-A01, 51-42-06-001-001-A01.Jan 19, 2020 · N540EG · Cndair CL6002C10 · Fuselage Main, FrameSDR VNAA202002299994Crossbeam · corrodedFS 280 CROSSBEAM IS CORRODED BETWEEN LBL9 AND LBL18 LOCATED AND DRILLED NEW SERVICEABLE LH FS280 CROSSBEAM IAW CRJ 700 SRM 51-40-11-001-001-A01.Jan 19, 2020 · N540EG · Cndair CL6002C10 · Fuselage Main, StructureSDR VNAA2019072811101Pcu · failedIB FLT SPLRS/IBN SPLR & IB SPOILRONS CAUTION MESSAGES RECEIVED. THE FLIGHT LANDED AND TAXIED TO GATE IN CVG WITHOUT INCIDENT. AS A PRECAUTION THE CREWDECLARED AN EMERGENCY INTO CVG. EMERGENCY TRUCKS WERE DISPATCHED TO RUNWAY. REMOVED & REPLACED LT IB MULTIFUNJul 28, 2019 · N540EG · Cndair CL6002C10 · Drag Control ActuatorSDR VNAA2018121871101Warning Message · false activationTHE CREW RECEIVED A SLATS FAIL MESSAGE AT ZERO. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT FURTHUR INCIDENT. MAINTENANCE JCLEARED INHIGITS AND SLATS OPS CHECKED GOOD.Dec 17, 2018 · N540EG · Cndair CL6002C10 · Central WarningSDR VNAA2017110711102A/C Pack · failedRIGHT PACK AUTO FAIL, ELECTRICAL BURNING ODOR IN THE CABIN. MX INSPECTED THE AFT EQIPMENT BAY & ALL AREAS OF CABIN, NO ODOR DETECTED.Nov 7, 2017 · N540EG · Cndair CL6002C10 · Cabin Cooling SystemSDR SIMA20170611002Skin · crackedPAX DOOR FWD SIDE SKIN CENTER STEP RADIUS APPEARS TO BE CRACKED. REPAIRED IAW SRM 52-11-04-201-004 TR 52-025.Jun 11, 2017 · N540EG · Cndair CL6002C10 · Passenger/Crew DoorsSDR SIMA20170606007Shear Tie · crackedPAX DOOR AFT SIDE SKIN ANGLE IS CRACKED. REPAIRED IAW SRM 52-11-04 TR 52-0026, REPAIR TYPE 1.Jun 6, 2017 · N540EG · Cndair CL6002C10 · Passenger/Crew DoorsSDR SIMA20161211003Doubler · corrodedUNDERFLOOR ANTENNA DOUBLER BETWEEN FS295.00 AND FS310.00 IS CORRODED BETWEEN STRINGERS 26L AND 26R. INSTALLED NEW ANTENNA DOUBLER BETWEEN FS295.00 AND FS310.00 IAW SRM 51-42-06.Dec 11, 2016 · N540EG · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR SIMA20160512001Charger · inoperativeFLIGHT ATTENDANT REPORTS MULTIPLE EMER LIGHTS ON THROUGHOUT THE CABIN. REGARDLESS OF SWITCH POSITION. R & R NR 2 EPSU CHARGER ASSEMBLY IAW CRJ 33-51-17. OPERATIONS CHECKED GOOD.May 12, 2016 · N540EG · Cndair CL6002C10 · Emergency LightingSDR SIMA20151112006Unknown · vibrationON TAKEOFF DURING GEAR RETRACTION FLIGHT ATTENDANT & PAXS REPORTED UNUSUAL VIBRATION. VIBRATION STOPPED AFTER GEAR WAS RETRACTED. CONDITION ON RNWY 22L, STRONG CROSS WINDS 260 DEG AT 18 GUSTING TO 26 KNOTS. NORMAL GEAR EXTENSION & NO VIBRATION DURING LANDINNov 12, 2015 · N540EG · Cndair CL6002C10 · Landing Gear SystemSDR SIMA20150701002Strip · crackedFLOOR PATH LIGHT STRIP CRACKED AT ROW 1A. R & R LIGHT STRIP IAW MM 33-51-01.Jul 1, 2015 · N540EG · Cndair CL6002C10 · Emergency LightingSDR SIMA20141204010Web · crackedRIGHT FWD EQUIPMENT COMPARTMENT FLOOR WEB IS CRACKED. REPAIRED IAW ETN-CR-53-099.Dec 4, 2014 · N540EG · Cndair CL6002C10 · Fuselage Miscellaneous Structure
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