N526EA

Service difficulty reports · 112

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 = 'N526EA' 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 VNAA202509250003Hinge Fitting · excess playDURING INSPECTION OF TASK CARD :55-30-203-JIC GVI OF THE VERTICAL STABILIZER INTERNAL AREA AROUND RUDDER POWER CONTROL UNIT WAS FOUND FREEPLAY ON BEARING OF LOWER HINGE FITTING AT REAR SPAR OF VERTICAL STABILIZER. HINGE FITTING #3 (P/N: AV670-21081-013 ) WAS Aug 2, 2025 · N526EA · Cndair CL6002C10 · Vertical StabilizerSDR VNAA202509250002Hinge · corrodedCORROSION ON HINGES (2EAS) AT ACCESS PANEL 832ET. HINGES (2EAS AT ACCESS PANEL 832ET WERE REPLACED PER CRJ700 SRM 51-42-06-001-A01 AND CRJ 700 SRM 51-41-02-001-001-A01Aug 2, 2025 · N526EA · Cndair CL6002C10 · Fuselage, Door HingeSDR VNAA202509260009Seal Rest · corrodedCORROSION ON SEAL REST WAS FOUND. SEALS REST WERE CLEANED PER CRJ-700 SRM 51-26-00-001-001-A01 AND FWD CORNER SEAL RETAINER BAGG DR NO CORROSION WAS FOUND ALSO RETAINER SEAL MID SECTION AND RETAINER SEAL AFT CORNER WERE REPLACED PER CRJ- 700 SRM 51-42-06-00Aug 1, 2025 · N526EA · Cndair CL6002C10 · Fuselage Main, StructureSDR VNAA202509250023Seat Track · corrodedCORROSION ON SEAT RAIL AT RBL9 (03) SEGMENTS: (01) FS375 - FS485. (02) FS485 - FS581. (03) FS581 - FS677. OF THE PAX CABIN.. SEAT RAILS AT RBL9 (03) SEGMENTS: (01) FS375 - FS485. (02) FS485 - FS581. (03) FS581 - FS677. OF THE PAX CABIN. WERE EVALUATE OUT LIAug 1, 2025 · N526EA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202509250019Hinge · corrodedCORROSION ON HINGES (1EAS) AND HINGE FITTINGS (2EAS) OF THE AFT LAVATORY SERVICE DOOR 196ER. HINGES (1EAS) AND HINGE FITTINGS (2EAS) OF THE AFT LAVATORY SERVICE DOOR 196ER. WERE REPLACED PER CRJ700 AMM 52-45-01Aug 1, 2025 · N526EA · Cndair CL6002C10 · Fuselage, Door HingeSDR VNAA202509250001Angle · corrodedCORROSION ON INTERNAL REINFORCEMENT ANGLE OF LP GROUND CONNECTION ACCESS DOOR (182BR). CORROSION ON INTERNAL REINFORCEMENT ANGLE OF LP GROUND CONNECTION ACCESS DOOR (182BR) WAS EVALUATED OUT OF LIMITS PER CRJ-700 SRM 53-00-00-101-001-A01 AND REPLACED PER CRJ-Aug 1, 2025 · N526EA · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA202509250016Skin · dentedDENT ON EXTERNAL LOWER FUSELAGE BTW FS310.00 TO FS319.00 AND STGR#21 TO STGR#20 RH SIDE. DENT ON EXTERNAL LOWER FUSELAGE BTW FS310.00 TO FS319.00 AND STGR#21 TO STGR#20 RH SIDE WAS REPAIRED PER REO 670-53-21 -2673 REV-.Jul 31, 2025 · N526EA · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR VNAA202509250015Door Frame · wornWEAR ON SURROUND OF HANDLE OF AFT COMPARTMENT DOOR. WEAR ON SURROUND OF HANDLE OF AFT COMPARTMENT DOOR WAS REPAIRED PER REO 670-52-31-031 REV BJul 31, 2025 · N526EA · Cndair CL6002C10 · Fuselage Main, StructureSDR VNAA202509250009Fairing · damagedFAIRING ASSY, LOWER VISOR (LH) 326CL WITHIN 2016.46 FLIGHT HOURS AFTER SECTION I, ACCOMPLISH A PERMANENT REPAIR AT DISCREPANT AREA IN ACCORDANCE WITH APPROVED PROCEDURES OR REPLACE PART. FAIRING ASSY, LOWER VISOR (LH) 326CL WAS REPLACED BY NEW FAIRNG PER EA 5Jul 31, 2025 · N526EA · Cndair CL6002C10 · Vertical Stabilizer Miscellaneous StructureSDR VNAA2025073111101Gcu · faultedACFT ESS BUSS CAUTION MSG IN FLIGHT. REMOVED AND REPLACED IDG GCU 1 IAW AMM 24-11-07-000/400-801-A01, PERFORMED OPS TEST IAW AMM 24-11-01-710-801-A01-PSA, OPS CHECK GOOD.Jul 24, 2025 · N526EA · Cndair CL6002C10 · AC Generator-AlternatorSDR VNAA2025052911101Water Separator · odorNOTED A SMELL IN FD AFTER INITIATING O2 MASK TEST. FD FILLED WITH SMOKE AND ELECTIRCAL BURING SMELL. RAN EVACUATION QRC. NO MEDICAL ATTENTION WAS REQUIRED. / REMOVED AND REPLACED L PACK WATER EXTRACTER IAW CRJ700 AMM-21-51-18-000/400-801-A01. OPS AND LEAK CHECMay 25, 2025 · N526EA · Cndair CL6002C10 · Humidity Control SystemSDR VNAA2024100911101Sensor · faultedR PACK TEMP CAUTION MSG IN FLIGHT. / REMOVED AND REPLACED RH PACK COMPRESSOR-DISCHARGE TEMPERATURE SENSOR IAW CRJ 700 AMM 21-51-10-000/400-801. OPS CHECK GOOD.Oct 1, 2024 · N526EA · Cndair CL6002C10 · Cabin Cooling SystemSDR VNAA2024062711101Skin · puncturedPUNTURE/GASH IN AIRCRAFT SKIN NEAR PANEL 196DR. / REO 670-53-61-2302 REPAIR TO FUSELAGE SKIN PANEL AND FRAME BTW FS985.00 - FS1015.00 & BTW STR19R - STR22R.Jun 24, 2024 · N526EA · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR VNAA202307051113Unknown · unknownSMOKE IN MAIN CABIN ON APPROACH CENTERED AROUND EXIT ROWS / PERFORMED TROUBLESHOOTING IAW CRJ700 FIM 21-22-00-810-806-A01. NOTED ELECTRICAL SMELL WITH RECIRCULATION FANS ON, NO SMELL PRESENT WITH RECIRCULATION FANS OFF. SEE LOGBOOK PAGE 22690263 FOR RECIRCULATJul 2, 2023 · N526EA · Cndair CL6002C10 · Air Distribution SystemSDR VNAA202304121112Unknown · unknownSPARKS COMING ELECTRICAL POWER CONTROL PANEL / INSTALLED ELECTRICAL CONTROL PANEL IAW CRJ 700 AMM 24-13-01-400-800-A01. OPS CHECK GOODApr 10, 2023 · N526EA · Cndair CL6002C10 · Alternator-Generator DriveSDR VNAA202302221111None · none1 DENT WAS DISCOVERED ON THE FUSELAGE SKIN PANEL BETWEEN FS193.00-FS202.75 AND STR BL22-STR 14. THE DENT HAS THE FOLLOWING DIMENSIONS (0.750€?L X 0.750€?W X 0.0005€?D). / COMPLIED WITH PERMANENT REPAIR EA 22-C7-53-1105 REV B IAW EA INSTRUCTIONS. "Feb 19, 2023 · N526EA · Cndair CL6002C10 · Fuselage Structure (General)SDR VNAA202203301111Windshield · crackedRH WINDSCREEN CRACKED IN FLIGHT AND ARCED / REMOVED AND REPLACED RT WINDSHIELD IAW CRJ7 AMM 56-11-01-000/400-801-A01 PSA. C/W OPERATIONAL & LEAK CHECK OF R/H WINDSHIELD IAW CRJ700 AMM 30-41-06-710-801-A01 & AMM 21-31-00-910-801/802 & AMM 56-11-01-400-801-A01-PMar 29, 2022 · N526EA · Cndair CL6002C10 · Flight Compartment WindowsSDR VNAA2022012899911Intercostal · corroded(N0366) CORROSION FOUND AT STRG 27 , AFT INTERCOASTAL (LH , INB) BETWEEN FS349.00 AND FS 364.00. REPAIR FOR AFT INTERCOASTAL L/H INBOARD BETWEEN FS349.00 & FS364.00 STRINGER 27 IS ACCOMPLISHED AFTER REMOVING THE INTERCOASTAL PROX SENSOR REMOVED THE CORROSION FJan 28, 2022 · N526EA · Cndair CL6002C10 · Fuselage Main, StructureSDR VNAA2022012899910Angle · corroded(N0300) CORROSION FOUND ON FWD FACE ANGLE OF CROSS BEAM FS280.00 BETWEEN LBL12.00 AND RBL12.00. REMOVED AND REPLACED ANGLE OF CROSS BEAM FS280.00 BETWEEN LBL12.00 AND RBL 12.00 IAW CRJ 700 SRM 51-42-06 AND 51-77-00.Jan 28, 2022 · N526EA · Cndair CL6002C10 · Fuselage Main, StructureSDR VNAA202201289999Intercostal · corroded(N0299) AT FS349:00 & FS364:00 FWD INTERCOSTAL HAS CORROSION AROUND SKIN RIVETS. INTERCOSTAL OVER STRG 27 BTW F.S. 349.0 TO 364.0 REMOVED I.A.W. CRJ700 SRM 51-42-06 NEW INTERCOSTAL DRILLED AND DRILL HOLES TREATED AND PRIMED I.A.W. CRJ700 SRM 51-40-11, 51-25-4Jan 28, 2022 · N526EA · Cndair CL6002C10 · Fuselage Main, FrameSDR VNAA202201289998Door Sill · corroded(N0263) PASSENGER DOOR LOWER SILL FRAME HAS CORROSION BETWEEN APPROX. FS310.00 TO FS349.00 AND WL72.00 UNDER THE FLOORBOARD. HEAT TREATED 1EA REPAIR ANGLE FROM 7075-0 TO T6/ .063 THICK IAW AMS 2770R. ROCKWELL HARDNESS TESTED MATERIAL @HRB 86 IAW SRM 51-11-11Jan 28, 2022 · N526EA · Cndair CL6002C10 · Passenger/Crew DoorsSDR VNAA202201289997Stringer · corroded(N0133) CORROSION FOUND ON STRINGER 26R BETWEEN FS319.70 TO FS349.00, TO INCLUDE CORROSION ON STGR26R UNION SPLICE BETWEEN FS333.00 TO FS349.00. CLEAN AND EVALUATE. STRINGER 26RH REMOVED BTW F.S. 333.0 TO 364.0 I.A.W. CRJ700 SRM 51-42-06 AND 51-42-21STRINGER SJan 28, 2022 · N526EA · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR VNAA202201289996Stringer Splice · corroded(N0130) CORROSION FOUND ON STRINGER UNION SPLICE LOCATED AT STGR25RH BETWEEN FS319.70 TO FS333.00. CLEAN AND EVALUATE. IVETS REMOVED ON STRINGER UNION SPLICE 25RH AT F.S. 333.0 IN ORDER TO GAIN ACCESS I.A.W. CRJ700 SRM 51-42-06CORROSION REMOVED AND EVALUATED. Jan 28, 2022 · N526EA · Cndair CL6002C10 · Fuselage Structure (General)SDR VNAA202201289995Stringer · corroded(N0124) CORROSION ON STGR26LH TO STGR25RH AND BETWEEN FS 295.00 TO FS 310.00. STRINGERS 26RH AND 25RH BTW F.S. 280.0 TO 333.0 REMOVED PER CRJ700 SRM 51-42-21 AND 51-42-06 NEW SRINGERS DRILLED AND ADJUSTED I.A.W. CRJ700 SRM 51-40-11 DRILL HOLES TREATED AND PRJan 28, 2022 · N526EA · Cndair CL6002C10 · Horizontal Stabilizer StructureSDR VNAA2021112899991Skin Panel · damagedDENT AND GOUGE DAMAGE ON FUSELAGE SKIN AT FS 518 STR 16LNov 28, 2021 · N526EA · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR VNAA2020041211101Selector Valve · faultyLANDING GEAR HANDLE WILL NOT EXTEND OR RETRACT LANDING GEAR IN FLIGHT, PERFORMED QRH MANUAL GEAR EXT. WAS SUCCESSFUL. REMOVED AND REPLACED MLG SELECTOR VALVE IAW CRJ700 AMM 32-32-10-000/400-801. OPS CHECK GOOD.Apr 9, 2020 · N526EA · Cndair CL6002C10 · Landing Gear SelectorSDR VNAA2019121099906Floorbeam · crackedWHILE PERFORMING SB670BA-53-041, FOUND RH COCKPIT FLOORBEAM AT RBL 11.00 TO BE CRACKED FWD OF THE ANGLE FITTING. PERFORMED EDDY CURRENT OF CRACKED AREA OF RBL 11/12 FLOORBEAM AND FOUND INDICATIONS EXTENDING BEYOND TYPE III CUTOUT OF SRM CRJ 700 53-11-43-201-0Dec 10, 2019 · N526EA · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR VNAA2019121099905Floorbeam · crackedWHILE PERFORMING SB670BA-53-041, FOUND LH COCKPIT FLOOR BEAM AT LB 11.00 OT BE CRACKED FWD OF ANGLE FITTING. APPLIED PROTECTIVE BARRIER OVER EWIS COMPONENTS BETWEEN FS280 AND FS265 UNDER FLOORBOARDS. VERIFIED ALL APPLIED PROTECTIVE BARRIER OVER EWIS COMPONENDec 10, 2019 · N526EA · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR VNAA2019121099904Bulkhead Web · corrodedWHILE PERFORMING SB670BA-53-041 FOUND BOTH LH AND RH FS280.00 BULKHEAD LOWER WEBS TO BE CORRODED. UPON FURTHER INVESTIGATION FOUND LOWER WEBS ON BOTH LH AND RH TO BE CORRODED BEYOND LIMITS REQUIRING REPAIR. COMPLIED WITH 280 BULKHEAD LOWER WEB REPAIRS (LH ANDec 10, 2019 · N526EA · Cndair CL6002C10 · Fuselage Main, BulkheadSDR VNAA2019121099903Gusset · crackedWHILE PERFORMING SB670BA-53-041 FOUND BOTH LH AND RH FS 280.00 COCKPIT DOOR POSTS TO HAVE CORROSION T THE BOTTOM EDGES. CUT AWAY LH DOOR POST LOWER END. REF CRJ 700 SRM 53-11-10-201-006-A01. REPAIRED LH LOWER PORTION OF DOOR POST IAW CRJ 700 SRM 53-11-10-201Dec 10, 2019 · N526EA · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA2019121099902Angle · corrodedFS280 FWD J ANGLE IS CORRODED. UPON FURTHER INVESTIGATION, FOUND FS280 FWD J-ANGLE TO BE CORODED BEYOND LIMITS IAW CRJ700 SRM SB 00-00-101-001-A01 REQUIRES REPLACEMENT. REMOVED CORRODED J-ANGLE IAW CRJ700 SRM 51-42-00-001-001-A01, 51-42-13-001-001-A01, 51-42Dec 10, 2019 · N526EA · Cndair CL6002C10 · Fuselage Main, StructureSDR VNAA2019121099901Floorbeam · corrodedFS280 IS CORRODED AT LBL 9 AND RBL 9 UNDER TITANIUM CAP. UPON FURTHER INVESTIGATION FOUND BOTH LH AND RH FS280.00 BEAMS TO BE CRACKED AND CORRODED REQUIRES REPLACEMENT OF BOTH. REMOVED BOTH LH AND RH FS280.00 BEAMS AS REQUIRED IAW CRJ 700 SRM 51-42-06-001-0Dec 10, 2019 · N526EA · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR VNAA2019100391104Plenum · leakingFLIGHT 5116 HAD A LOSS OF PRESSURIZATION AT 6000FT OUT OF STL. CAPTAIN STATED THEY LOST THE RIGHT HAND PACK WITH THE LEFT HAND PACK ALREADY DEFERRED. DECLARED AN EMERGENCY AND RETURN TO DEPARTURE. AIRCRAFT IS OUT OF SERVICE. TROUBLESHOT IAW FIM 75-30-00-81Sep 30, 2019 · N526EA · Cndair CL6002C10 · Cabin Pressure Control SystemSDR VNAA2019090711102Packing · damagedFLIGHT 5647 CLT-HSV RETURNED TO FIELD DUE TO A RIGHT PACK DUCT WARNING FOLLOWED BY A CAUTION MSG DURING THE FLOW OF THE QRH. LEFT PACK WAS ALREADY DEFERRED. CREW REDUCED ALTITUDE TO 10K AND RETURNED TO CLT DUE TO CABIN TEMPERATURES BEING UNCOMFORTABLE FOR PASep 7, 2019 · N526EA · Cndair CL6002C10 · Pneumatic Distribution SystemSDR VNAA2019090311102Duct · damagedWHILE CLIMBING OUT. CREW RECEIVED A BLEED DUCT WARNING MESSAGE. CREW RAN THE QRH WHICH TOLD THEM TO SWAP TO THE OTHER PACK. OTHER PACK WAS ALREADY DEFERRED AND COULD NOT BE USED. CREW TURNED OFF WORKING PACK AND FLEW UNPRESSURIZED BACK. NO EMERGENCY WS DESep 3, 2019 · N526EA · Cndair CL6002C10 · Pneumatic Distribution SystemSDR VNAA2019062811102Warning System · false activationDURING INITIAL CLIMB, CREW RECEIVED HIGH OIL TEMP WARNING. CREW DECIDED TO RETURN TO CLT. FAA AND TOWER REPORTS CREW DID DECLARE AN EMERGENCY. PERFORMED RH ENGINE START TO MONITOR OIL TEMPERATURE AND FOUND OIL TEMP TO BE WITHIN LIMITS. AFTER 30 MINUTES RUNNINGJun 28, 2019 · N526EA · Cndair CL6002C10 · Engine Oil TemperatureSDR SIMA20170325001Safety Valve · failedAIRCRAFT NOT PRESSURIZING AFTER TAKE OFF GOING THROUGH 9,000 FEET AND 11,000, LEVELED OFF AT 10,000 FT AND RETURN TO DEPARTURE. REMOVED AND REPLACED SAFETY VALVE IAW AMM 21-32-03. OPS CHECKED GOOD.Mar 25, 2017 · N526EA · Cndair CL6002C10 · Pressure Regulator/Outflow ValveSDR SIMA20170212002Ignition Lead · failedSTRONG FUEL SMELL AFTER A FAILED ATTEMPT TO START RIGHT ENGINE. DEFERRED NR 2 ENG IGNITION B. NO FURTHER FUEL SMELL NOTED. REMOVED AND REPLACED RT IGN "B" LEAD AND IGNITER IAW AMM 74-20-03 AND 74-20-01. OPS CHECK GOOD. IGNITOR P/N CH31926Feb 12, 2017 · N526EA · Cndair CL6002C10 · Ignition Harness (Distribution)SDR SIMA20161120003Flashlight Assy · inoperativeFA FORWARD FLASHLIGHT NOT CHARGING. REMOVED AND REPLACED THE FLASHLIGHT ASSY IAW AMM 25-61-02, OPS CHECKED GOOD.Nov 20, 2016 · N526EA · Cndair CL6002C10 · Emergency EquipmentSDR SIMA20161106004Stringer · damagedSTRINGER 14L BETWEEN BS 193 AND 202.75 IS DAMAGED. INSTALLED A NEW STRINGER IAW SRM 51-42-06.Nov 6, 2016 · N526EA · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SIMA20161106003Frame · damagedUPPER FRAME AT BS 193 IS DAMAGED. REPAIRED UPPER FRAME IAW ERS-CR-53MR-2408.Nov 6, 2016 · N526EA · Cndair CL6002C10 · Fuselage Main, FrameSDR SIMA20160818003Warning System · false activationSLATS FAIL MESSAGE POSTED. CLEARED INHIBITS AND PERFORMED FLAPS AND SLATS ADJUSTMENT TEST IAW AMM 27-50-00. OPS CHECK OK.Aug 18, 2016 · N526EA · Cndair CL6002C10 · Leading Edge Slat Position Indicating SystemSDR SIMA20160725001Acm · malfunctionedRIGHT PACK AUTO FAIL AFTER PUSH BACK AND LT ENGINE STARTED, ACCOMPANIED WITH SMOKE IN THE CABIN. PERFORMED GVI OF PACK 2 RT PACK SYS REF AMM 21-51-00. CREW RAN ACFT BLEED SYSTEMS AND NO SMOKE NOTED OR ELECTRIC ODORS. RIGHT PACK WAS ISOLATED. DEFERRED RT PAJul 25, 2016 · N526EA · Cndair CL6002C10 · Cabin Cooling SystemSDR SIMA20160615002Pcu · malfunctioned1B FILTER SPOILER AND 1B SPOILERONS POSTED ON DESCENT AS SPOILER LEVER WAS SELECTED AOM VOL 1, EMERGENCY AMBER NORMAL PROCEDURES COMPLIED WITH, EMERGENCY WAS DECLARED. INTERROGATED MDC, FOUND MDC MESSAGE, SPOILERS LT INBD MFS PCU MPE33 FAILED, PCU JAM EQUATIOJun 15, 2016 · N526EA · Cndair CL6002C10 · Drag Control SystemSDR SIMA20160517005Apu · leakingWHILE SITTING AT THE GATE WITH THE APU & PACKS RUNNING, WE GOT SMOKE IN THE CABIN. AFTER SHUTTING DOWN THE APU, THE SMOKE CLEARED. UPON INSPECTION OF APU, FOUND OIL LEAKING FROM EXHAUST. REF ITEM NR 3 BELOW THIS LOG PAGE FOR CORRECTIVE ACTION.May 17, 2016 · N526EA · Cndair CL6002C10 · APU Core EngineSDR SIMA20160429002Web · crackedLEFT SIDE OF FWD EQUIPMENT COMPARTMENT FLOOR WEB IS CRACKED. REPAIRED LT SIDE OF FWD EQUIPMENT COMPARTMENT FLOOR WEB IAW ETN-CR-53-099.Apr 29, 2016 · N526EA · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SIMA20151229004Actuator · failedSLATS FAIL, ACT & CN, MSG ON APPROACH. R & R NR 6 SLAT ACTUATOR ON RT WING IAW AMM 27-81-09. OPERATIONS TESTED GOOD.Dec 29, 2015 · N526EA · Cndair CL6002C10 · Leading Edge Slat ActuatorSDR SIMA20140224010Pin · dirtyMAIN CABIN DOOR PIN STUCK, HAD DIFFICULTY OPENING, RT PIN LOOKING FROM OUTSIDE, IN. CLEANED & LUBED AFT HANDRAIL PIN AS REQUIRED.Feb 24, 2014 · N526EA · Cndair CL6002C10 · Passenger/Crew DoorsSDR SIMA20140127001Shelf · crackedDURING 2C CHECK FOUND RT FWD SHELF IN THE NOSE EQUIPMENT COMPARTMENT BY THE DOUBLER. CUT OUT IS CRACKED APPROXIMATELY 3/8 INCHES LONG. REPAIRED CRACK IN RIGHT HAND FWD SHELF IN NOSE EQUIPMENT COMPARTMENT IAW ERS CR-5300-206.Jan 27, 2014 · N526EA · Cndair CL6002C10 · Electronic Shelf SectionSDR SIMA20140118003Light · wrong partCABIN EMERGENCY FLOOR PATH MARKINGS AT RT & LT EMERGENCY EXIT ROWS APPEAR TO BE DEFORMED & WRONG PART INSTALLED. R & R CABIN EMERGENCY FLOOR PATH MARKINGS AT RT & LT EMERGENCY EXIT ROWS IAW AMM TASK 33-51-01-400-801 & ETN-CR-33-019.Jan 18, 2014 · N526EA · Cndair CL6002C10 · Emergency Lighting
Back to N526EA