N528EG

Service difficulty reports · 126

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 = 'N528EG' 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 VNAA202206269996Skin · corrodedCORROSION ON EXTERNAL FUSELAGE SKIN AT SETTLEMENT AREA OF WING-TO-FUSELAGE FAIRING BTW FS STA 847.00 TO FS STA 1015.00.May 8, 2022 · N528EG · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR VNAA202206279994Access Door · corrodedCORROSION ON ACCESS PANEL 182BR OF SERVICE DOOR.May 7, 2022 · N528EG · Cndair CL6002C10 · Air Conditioning DoorsSDR VNAA2022062699910Fastener · corrodedCORROSION ON FASTENERS AT AFT KEEL BEAM LOWER SIDE BTW FS STA 695.00/909.00.May 7, 2022 · N528EG · Cndair CL6002C10 · Fuselage Main, KeelSDR VNAA202206269995Web · corrodedCORROSION ON SEVERAL LOCATIONS OF LOWER WEB AT FWD BAGGAGE BAY DOOR SURROUND.May 7, 2022 · N528EG · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA202206269994Intercostal · corrodedCORROSION ON INTERCOSTAL DD4 BETWEEN FS347.27 - FS338.963 AT PASSENGER DOOR.May 7, 2022 · N528EG · Cndair CL6002C10 · Passenger/Crew DoorsSDR VNAA202206269993Former · corrodedCORROSION ON FORMER OF FS347.27 BETWEEN INTERCOSTAL DD6 - INTERCOSTAL DD5 AT PASSENGER DOOR.May 7, 2022 · N528EG · Cndair CL6002C10 · Passenger/Crew DoorsSDR VNAA202206269992Intercostal · corrodedCORROSION ON INTERCOSTAL DD6 BETWEEN FS338.963 - FS327.763 AT PASSENGER DOOR.May 7, 2022 · N528EG · Cndair CL6002C10 · Passenger/Crew DoorsSDR VNAA202206269991Former · corrodedCORROSION ON FORMER OF FS 311.75 BETWEEN INTERCOSTAL DD2 - INTERCOSTAL DD3 AT PASSENGER DOOR.May 7, 2022 · N528EG · Cndair CL6002C10 · Passenger/Crew DoorsSDR VNAA202206269990Cargo Fitting · corrodedCORROSION & WEAR MARK ON CARGO MACHINED BRAKETS (CARGO NET FITTING PLATES), FWD CARGO FLOOR STRUCTURE.May 7, 2022 · N528EG · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202206259990Hinge Bracket · corrodedCORROSION ON UPPER BRACKET HINGE AT SERVICE DOOR 196ER.May 6, 2022 · N528EG · Cndair CL6002C10 · Air Conditioning DoorsSDR VNAA202206269998Diaphragm · corrodedCORROSION ON DIAPHRAGM AT SETTLEMENT AREA LOWER SECTION OF WING-TO-FUSELAGE FAIRING BTW FS879.00/909.00 AND STR 24RH.May 5, 2022 · N528EG · Cndair CL6002C10 · Fuselage, Wing Attach FittingsSDR VNAA202204061111Flap System · faultedMTC DIVERSION DUE TO FLAP ISSUE ON TAKE OFF WITH FLAPS 20, ONE FLAP DID NOT MOVE, OTHER FLAP STOPPED AT 18 DEGREES DECLARED EMERGENCY, BURNED OFF FUEL, LANDED AT IAD TRUCKS ROLLED AT TOWER'S DIRECTION (FLIGHT DID NOT REQUEST) PAX DID *NOT* BRACE. FLAPS FAIL CAApr 3, 2022 · N528EG · Cndair CL6002C10 · Trailing Edge Flap Control SystemSDR VNAA202202231113Target · missingEMR DIV-GEAR DISAGREE AGREE WARNING MESSAGE ON TAKEOFF PERFORMED QRH CH 10-3, ALL THREE GEARS INDICATED DOWN AND LOCKED, LANDING GEAR DID NOT MOVE, NO CHANGE ON THE EITHER 3A OR 3B PUMP, VERIFIRED SYSTEM 3 HYDRAULICS AT 3000 PSI, MDC FLAGGING B1 CODE 007697, 0Feb 20, 2022 · N528EG · Cndair CL6002C10 · Landing Gear Retraction/Extension SystemSDR VNAA202202181113Swivel · brokenDURING DEPARTURE FROM DCA, CREW NOTIFIED DISPATCH VIA ACARS THAT THEY WERE DIVERTING TO IAD BECAUSE THEY HAD LOST HYDRAULIC SYSTEM 3. THEY DID DECLARE AN EMERGENCY. THE FLIGHT HELD FOR A SHORT WHILE TO BURN OFF FUEL, THEN WENT INTO IAD. FLIGHT LANDED ON RWY 19Feb 17, 2022 · N528EG · Cndair CL6002C10 · Landing Gear Brake SystemSDR VNAA202102191111Terminal · looseLOW SPEED REJECTED TAKEOFF WAS AT 60-65KT ON TAKEOFF ROLL WHEN THE FO SIDE PFD STARTED FLICKERING CREW IMMEDIATELY REJECTED TAKEOFF AND RETURNED TO GATE. NO INJURIES AND AIRCRAFT WAS ABLE TO RETURN TO GATE UNDER OWN POWER. REJECTED TAKEOFF DUE TO COPILOT MFDFeb 17, 2021 · N528EG · Cndair CL6002C10 · Electrical Power System WiringSDR VNAA202102151111Controller · failedIDG FAILED INFLIGHT (DAY-CLT) AFTER TO. RETURNED TO FIELD. AFTER TAKEOFF,THE FO SIDE ELECTRICAL FAILURED. NO PRESSURIZATION. MFD AND PFD BLANKED ON FO SIDE. MULTIPLE STATUS AND CAUTION MESSAGE BUT WENT AWAY QUICKLY. RETURNED TO FIELD DUE TO ELECTRICAL ANOMALYFeb 11, 2021 · N528EG · Cndair CL6002C10 · DC Power Distribution SystemSDR SIMA20190911002Stringer · corrodedSTR 26 RT BETWEEN FS349 AND FS 364 IS CORRODED. C/A-INSTALLED NEW STR 26 BETWEEN FS349-FS364 IAW SRM 51-42-06.Sep 11, 2019 · N528EG · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SIMA20190909001Stringer · corrodedSTR 26 RT IS CORRODED BETWEEN FS280 AND FS295. C/A-INSTALLED NEW STR 26R FROM FS280.00 TO FS333.00 IAW SRM 51-42-06.Sep 9, 2019 · N528EG · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SIMA20190909002Stringer · corrodedSTR 25 RT IS CORRODED BETWEEN FS280 AND FS295. C/A-INSTALLED STR 25R FROM FS280.00 TO FS333.00 IAW SRM 51-42-06.Sep 9, 2019 · N528EG · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SIMA20190908001Bulkhead · corrodedBULKHEAD AT FS280.00 IS CORRODED ON THE INBD EDGE JUST ABOVE THE CROSSBEAM. C/A-REPAIRED IAW SRM 53-11-10.Sep 8, 2019 · N528EG · Cndair CL6002C10 · Fuselage Main, BulkheadSDR SIMA20190829008Frame · corrodedFRAME AT FS 295 FWD AND AFT SIDES CORRODED BETWEEN STRINGER'S 26 LT AND 26 RT. C/A-REMOVED CORRODED FRAME 295.00 AT STRINGER 25L TO 25R AND INSTALLED SERVICEABLE FRAME IAW SRM 53-00-06.Aug 29, 2019 · N528EG · Cndair CL6002C10 · Fuselage Main, FrameSDR SIMA20190829007Frame · corrodedFRAME AT FS 310 FWD SIDE IS CORRODED BETWEEN STRINGER'S 26 LT AND 26 RT. C/A-REPAIRED FRAME AT FS310 IAW SRM 53-00-06.Aug 29, 2019 · N528EG · Cndair CL6002C10 · Fuselage Main, FrameSDR SIMA20190828005Crossbeam · corrodedLT SIDE FS280.00 CROSSBEAM TOP FLANGE IS CORRODED AND HAS PULLED RIVETS. C/A-R&R LT SIDE FS280.00 CROSSBEAM IAW SRM 51-42-06.Aug 28, 2019 · N528EG · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SIMA20190828006Crossbeam · corrodedRT SIDE FS280.00 CROSSBEAM TOP FLANGE IS CORRODED AND HAS PULLED RIVETS. C/A-R&R RT SIDE FS280.00 CROSSBEAM IAW SRM 51-42-06.Aug 28, 2019 · N528EG · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SIMA20190828004Door Sill · corrodedAFT BAGGAGE DOOR SILL CORRODED. C/A-R&R AFT BAGGAGE DOOR SILL IAW SRM 51-42-06 AND 51-42-21.Aug 28, 2019 · N528EG · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SIMA20190827007Floorbeam · crackedRT CENTER COCKPIT FLOORBEAM BL 12.00 IS CRACKED JUST FWD OF FS 280.00. C/A-COMPLETED REPAIR ON THE RT CENTER COCKPIT FLOORBEAM BL 12.00 IAW SRM 53-11-43.Aug 27, 2019 · N528EG · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR SIMA20190827006Floorbeam · crackedLT CENTER COCKPIT FLOORBEAM BL 12.00 IS CRACKED JUST FWD OF FS 280.00. C/A-COMPLETED REPAIR ON THE LT CENTER COCKPIT FLOORBEAM BL 12.00 IAW SRM 53-11-43.Aug 27, 2019 · N528EG · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR SIMA20190819008Battery · not reported[PSR] MISC WORK REQUEST: WR-2019-09-04 528-0037 - REMOVE AND REPLACE EMERGENCY BATTERY PN 2013-1A SN 101791-C/A-RAR #4 EMERGENCY BATTERY AND POWER SUPPLY IAW AMM TASK 33-51-17. OPS CHECKS GOOD AT THIS TIME.Aug 19, 2019 · N528EG · Cndair CL6002C10 · Emergency LightingSDR SIMA20190719001Light · inoperativeLT FUSELAGE EMERGENCY LIGHT INOP JUST AFT OF MAIN DOOR. C/A-REMOVED AND REPLACED LT FUSELAGE EMERGENCY LIGHT IAW AMM 33-51-15. OPT CHECK GOOD.Jul 19, 2019 · N528EG · Cndair CL6002C10 · Emergency LightingSDR SIMA201906254002O-Ring · damagedLEFT BLEED DUCT WARNING MESSAGE. DUCT WENT RED FROM THE ISOLATION VALVE FROM LEFT ENGINE ON ANTI-ICE PAGE. ASSOCIATED WITH A BURNING ODOR IN THE ENTIRE AIRCRAFT. PLASTIC BURNING ODOR. TROUBLESHOT BLEED LEAK REPAIR, BLEED LEAK AND ODOR EVENT OPS CHECKED GOODJun 24, 2019 · N528EG · Cndair CL6002C10 · Pneumatic Indicating SystemSDR SIMA20190502007Door · openORD GND CREW LEFT EXT PWR ACCESS DOOR OPEN FOUND DOOR OPEN ON ARRIVAL IN LEX. C/A-GVI PERFORMED ON EXT PWR DOOR IAW SRM-51-11-51 NO DAMAGE NOTED.May 2, 2019 · N528EG · Cndair CL6002C10 · Accessory Compartment DoorsSDR SIMA2019041109006Bulb · inoperativeRIGHT HAND FORWARD OVER WING EMERGENCY EXIT LIGHT IS INOP.-C/A-REMOVED AND REPLACED RIGHT HAND FORWARD OVER WING EMERGENCY EXIT LIGHT BULB IAW AMM TASK 33-51-15. OPS CK GOOD.Apr 9, 2019 · N528EG · Cndair CL6002C10 · Emergency LightingSDR SIMA201809198001Strut · defectiveWARNING MSG LAND GEAR DISAGREE. MSG EXTINGUISHED AFTER CHECKLIST AFTER ROTATION. FOUND FAULT TO BE CAUSED BY NLG STRUT NOT FULLY EXTENDING WHILE IN THE AIR AND ALSO LEAKING BOTH DUE TO DAMAGED INTERNAL SEALS. ACCOMPLISHED NLG STRUT REPACK IAW W/C 32-019 REF NRSep 18, 2018 · N528EG · Cndair CL6002C10 · Nose/Tail Landing Gear Strut/AxleSDR SIMA2018072322001Fan · malfunctionedF/A CALLED IN 8 MINS FROM LANDING REPORTING FUMES BUT NO SMOKE IN CABIN. PLASTIC LIKE SMELL WAS STRONGEST FROM EXIT ROW AFT BUT SPREAD THROUGHOUT CABIN. FEINT ODOR WAS NOTICED IN COCKPIT ALSO. SAME TYPE OF SMELL. NO FIRE, NO SMOKE. CKPT O2 USED. PACKS WERE ON Jul 22, 2018 · N528EG · Cndair CL6002C10 · Air Distribution FanSDR SIMA2018071615002Outflow Valve · inoperativeAIRCRAFT WOULD NOT PRESSURIZE DURING FLIGHT. CLIMB WAS HALTED AT 11,500 DECENT TO 10,000. UNPRESSURIZED FLIGHT PROCEDURE APPLIED VIA QRH. INTERROGATED MDC MSG AND FOUND ID B1-006165. REF FIM TASK 21-32-01-810-801. FOUND OUTFLOW VLV INOP. R&R OUTFLOW VALVE IAW Jul 15, 2018 · N528EG · Cndair CL6002C10 · Pressure Regulator/Outflow ValveSDR SIMA20180617002Connector · unsecureFIRE SYS FAILED STATUS MESSAGE AND L FIRE FAIL CAUTION MESSAGE DESCENDING THROUGH 9000 FT. INSPECTED FIDEEX CONTROL UNIT AND SECURRED THE CONNECTION IAW AMM 26-10-01. PERFORMED AN OPERATIONAL CHECK OF THE SYSTEM IAW AMM 26-10-00, ALL CHECKED GOOD, ACFT OK Jun 17, 2018 · N528EG · Cndair CL6002C10 · Fire Protection System WiringSDR SIMA20180612004Unknown · odorBURNING RUBBER SMELL ON FLIGHT DECK WHEN HYD SYS ARE TURNED ON. SMOKE FUMES WERE ALSO PRESENT. PERFORMED A GVI FOR ANY LEAKS OUTSIDE OF AIRCRAFT. NONE NOTED. PERFORMED AN OPERATIONAL TEST OF THE AIR CONDITIONING DISTRIBUTION SYSTEM IAW AMM 21-51-00-710-801. NOJun 12, 2018 · N528EG · Cndair CL6002C10 · Air Distribution SystemSDR SIMA20180206001Latch · obstructedFA REPORT MAIN CABIN DOOR DIFFICULT TO OPEN. CLEANED DEBRIS FROM LATCHING MECHANISM AND ROLLERS, PERFORMED OPERATIONAL CHECK IAW 52-11-02 OPS CK GOOD.Feb 6, 2018 · N528EG · Cndair CL6002C10 · Passenger/Crew DoorsSDR SIMA20171225004Unknown · odorFA REPORTED TO PILOTS ABNORMAL ODOR INSIDE OF CABIN. TROUBLESHOT DISTRIBUTION SYSTEM IAW FIM 21-22-00, INTERROGATED MDC NO CODE, PERFORMED OPS CHECKED IAW AMM 21-51-00. OPS CHECKED GOOD. NO ODORS NOTED.Dec 25, 2017 · N528EG · Cndair CL6002C10 · Air Distribution SystemSDR SIMA20171030001Unknown · odorFA'S AND PAX COMPLAINED OF ODD ODOR ON TOUCHDOWN. SAID IT WAS A SULPHER, MATCHES ODOR THAT BURNED THERE EYES AND IT GOT BETTER AFTER STARTING THE APU. NO SMOKE NOTICED. PERFORMED TROUBLESHOOTING OF ABNORMAL ODOR IN CABIN AND COMPLETED FIM 21-22-00-810-806. Oct 30, 2017 · N528EG · Cndair CL6002C10 · Air Distribution SystemSDR SIMA20170315002Line · failedHYD 1 LOW PRESSURE CAUTION. PRESSURE REMAINED QUANTITY 5%. HYD ENGINE DRIVEN PUMP 1A NO PRESSURE QUANTITY 0%. REMOVED AND REPLACED THE NR 1 HYD PRESSURE TUBE RUNNING FROM SPLIT LINE BRACKET TO IDG COMPRESSOR RAFT IAW MM 29-11-52, LEAK CHECKED GOOD. REMOVED Mar 15, 2017 · N528EG · Cndair CL6002C10 · Hydraulic System, MainSDR SIMA20170201004Skin · damagedDURING POSTFLIGHT WALKAROUND, F/O REPORTS A DENT ON LOWER SKIN OF LEFT INBOARD FLAP IN LINE WITH #2 TIRE. DENT IS ALSO IN LINE AND ON A ROW OF FASTENERS. REF LOG PAGE 4054862 ITEM 3. ALSO REFERENCE ERS-CR-57DF-677 PTC SMALL DENT ON LH INBD FLAP LOWER SURFACE Feb 1, 2017 · N528EG · Cndair CL6002C10 · Trailing Edge FlapsSDR SIMA20170128001Skin · crackedPAX DOOR AFT SIDE SKIN HAS A CRACK BETWEEN TOP STEP AND MID STEP AT PREVIOUS REPAIR. REPAIRED IAW SRM 52-11-04.Jan 28, 2017 · N528EG · Cndair CL6002C10 · Passenger/Crew DoorsSDR SIMA20170125007Angle · crackedPAX DOOR AFT ANGLE CRACKED. REPAIRED THE ANGLE IAW SRM 52-11-04.Jan 25, 2017 · N528EG · Cndair CL6002C10 · Passenger/Crew DoorsSDR SIMA20170125005Skin · crackedPAX DOOR CRACKED ON PREVIOUS SKIN REPAIR REPAIRED IAW SRM 52-11-04.Jan 25, 2017 · N528EG · Cndair CL6002C10 · Passenger/Crew DoorsSDR SIMA20170125002Floor Panel · crackedFWD EQUIPMENT BAY FLOOR HAS 1/8 INCH CRACK BY THE LEFT AFT CORNER OF CUTOUT FOR 211AL. COMPLETED REPAIR TO LT FWD EQUIPMENT BAY FLOOR IAW ETN-CR-53-099.Jan 25, 2017 · N528EG · Cndair CL6002C10 · Fuselage Floor PanelSDR SIMA20160707001Control Panel · malfunctionedAFT LAVATORY SMOKE WARNING DURING FLIGHT, PERFORMED VISUAL INPECTION OF AFT LAVATORY, NO SMOKE DETECTED, AIRPORT CFR REPORTED NO EVIDENCE OF SMOKE OR FIRE IN LAVATORY. PERFORMED OPS CHECK OF LAVATORY SMOKE SYSTEM IAW AMM 26-16-00. OPS CHECKED GOOD. THE SMOKE Jul 7, 2016 · N528EG · Cndair CL6002C10 · Cabin Pressure Control SystemSDR SIMA20160706002Pressure Panel · faultyDURING ENROUTE CLIMB TO 14000 FT, RECEIVED AN AUTO PRESSURE CAUTION MESSAGE. WHILE RUNNING THE AUTO PRESSURE CHECKLIST A CABIN ALTITUDE WARNING MESSAGE WAS RECIEVED. THE PAX OXYGEN ON CAUTION MESSAGE ALERTED AND ON AUTO PRESSURE 1/2 FAIL STATUS MESSAGE ON EDJul 6, 2016 · N528EG · Cndair CL6002C10 · Cabin Pressure Control SystemSDR SIMA20160408003Outflow Valve · openCABIN ALT CAUTION AT 10,000 FT, ACFT NOT PRESSURIZE AT ANY TIME, FLIGHT CONTINUED. FOUND GND VLV OPEN, DEACTIVATED GND VLV IAW MEL PROCEDURE 21-6 SECTION 4. ACFT OK FOR SERVICE.Apr 8, 2016 · N528EG · Cndair CL6002C10 · Pressure Regulator/Outflow ValveSDR SIMA20151203003Slider · damagedPROXIMITY SYS FAULT 1 STATUS MSG DISPLAYED SHORTLY AFTER TAKEOFF. PERFORMED PERMANENT REPAIR TO UPPER RT THRUST REVERSER LATCH BEAM SLIDER IAW ERS-CR-78DF-108R1 PART B. ALL MDC INDICATIONS NORMAL FUNCTIONAL CHECK GOOD.Dec 3, 2015 · N528EG · Cndair CL6002C10 · Engine Thrust Reverser
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