Textron 525

Service difficulty reports · 260

Newest first. General aviation reporting is voluntary.

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 aircraft_model_key = '525'
  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 9JLA20110630001Ahrs · defectiveCREW REPORTED THE NR 1 AHRS FAILED DURING THE THIRD LEG OF TRIP AND HAD TO SWITCH TO REVERSIONARY AHRS NR 2. TROUBLESHOOTING FOUND THE AHRS COMPUTER DEFECTIVE P/N 822-1110-001 S/N 49YM.Jun 30, 2011 · N726CL · Cessna 525 · Integrated Flight SystemSDR LOMA2011042201000Engine · slowUPON TAKE-OFF, ACFT ACCELERATION DETERMINED SLOW BY PILOT AND COPILOT. AT 80 KNOTS INDICATED, TAKEOFF ABORTED. CREW SLOWED AIRCRAFT TO STOP USING ACFT BRAKES. LT MAIN TIRE DEFLATED AT WALKING SPEED, FROM FUSE PLUG RELEASE, TIRE BEAD SEPARATED FROM WHEEL. ACFTApr 22, 2011 · N547TW · Cessna 525 · Engine (Turbine/Turboprop)SDR 2011FA0000071Gyro · malfunctionedDRIVES COMPASS CARD +70 DEGREES. FOUND ON INITIAL POWER UP AFTER INSTALLATION/ REPLACEMENT.Jan 14, 2011 · N115BB · Cessna 525 · Navigation SystemSDR 2011FA0000070Gyro · malfunctionedDRIVES COMPASS CARD +15 DEGREES. FOUND ON INITIAL POWER UP AFTER INSTALLATION/ REPLACEMENT.Jan 14, 2011 · N115BB · Cessna 525 · Navigation SystemSDR 2011FA0000069Gyro · malfunctionedDRIVES COMPASS CARD +10 DEGREES. FOUND ON INITIAL POWER UP AFTER INSTALLATION OF REPLACEMENT.Jan 14, 2011 · N115BB · Cessna 525 · Navigation SystemSDR CA091209004Line · cracked(CAN) PILOT REPORTED NO TAIL DE-ICE BOOT INDICATION BETWEEN 72 TO 82 N2. RAN AIC ON GROUND TAIL DEI-CE BOOT WOULD INFLATE, BUT NO INDICATION. INDICATION WOULD WORK UP TO 72 AND PAST 82N2, HOWEVER IN BETWEEN WAS VERY ERRATIC. TUBE FOUND SEPARATED FROM B NUT, FNov 26, 2009 · Cessna 525 · Hydraulic System, MainSDR 2009FA0000959Sensor · out of limitsPROBLEM WAS TROUBLESHOT TO A FAULTY BATTERY TEMP SENSOR. THE SPARE SENSOR INSIDE THE BATTERY WAS CONNECTED AND TOOK THE FAULTY SENSOR OFF LINE. BATTERY WAS REINSTALLED AND THE AIRCRAFT WAS OPS CHECKED GOOD AT THAT TIME AND WAS RELEASED.Nov 4, 2009 · N300BV · Cessna 525 · Battery/Charger SystemSDR 2009FA0000798Shaft · shearedSHAFT SHEARED ON NR1 (L) HYD PUMP WHILE ACFT WAS IN A CLIMB AFTER TAKE OFF. THIS RESULTED IN THE HYD RESERVOIR TO BE EMPTIED OVERBOARD THRU THE PUMP DRAIN. THE PILOT'S THEN GOT A HYD FLOW LOW ANNUNCIATOR, FIRST ON THE RT SIDE AND THEN A FEW SECONDS LATER ON THSep 23, 2009 · N467F · Cessna 525 · Hydraulic Pump (Electric/Engine), MainSDR EWCR44CK5250401Stud · brokenSTARTING DESCENT, VIBRATION/NOISE WAS AUDIBLE INSIDE ACFT. NO INDICATIONS OF SYSTEM ISSUES OTHER THAN THE VIBRATION BUZZ NOISE. FLT DIVERTED. WHEN LANDING GEAR WAS EXTENDED FOR LANDING VIBRATION/NOISE WENT AWAY. ACFT LANDED WITHOUT INCIDENT. AIRCRAFT WAS TUSep 15, 2009 · N44CK · Cessna 525 · Landing Gear Door Retract SectionSDR CA090617002Trim Tab · displaced(CAN) PILOT REPORTED "JERKINESS: OF ELEVATOR CONTROL - GROUNDED ACFT ELEVATOR TRIM/TAB OPERATION INSPECTED - LT TAB INGFS FOUND MIGRATED INBD. CONTRACTING TAILCONE. HINGE PIN RETAINING LOCKWING FOUND MISSING. LOCKWING HOLES (2) FOUND "PULLED THRU" TAB SKIN.Jun 4, 2009 · Cessna 525 · Elevator Tab Control SystemSDR 2009FA0000391Bearing · damaged38K FEET, AUTO PILOT COMMANDING DECENT RATE - LT ENGINE BEGAN UNCOMMANDED SPOOL DOWN. NO PRIOR INDICATIONS ON PANEL. DURING EMERGENCY SHUTDOWN PROCEDURES N1 AND N2 INDICATIONS CONFIRMED, 36K, 30K FEET SLIGHT VIBRATION FELT. AT 30K FEET VIBRATION STOPPED. INMay 6, 2009 · N413CQ · Cessna 525 · Turbine Engine Accessory DriveSDR 2009FA0000015Tube · brokenDURING AN INSP, DOC 10, LANDING GEAR PNEUMATIC BRAKE SYS FUNCTIONAL CHECK ONE OF THE LINES IN THE RT LANDING GEAR WELL BLEW. FURTHER INVESTIGATION FOUND THAT THE 6327500-12 TUBE ASSY BROKE OFF AT THE FLARE ON THE INBD END OF THE TUBE ASSY. INSP OF THE SAME LDec 30, 2008 · N793CJ · Cessna 525 · Landing Gear Brake SystemSDR CA081020001Mount · misinstalled(CAN) METAL FILINGS WERE FOUND UNDER THE RUDDER SERVO DUE TO THE MOUNTING STRUCTURE HAVING BEEN INSTALLED OFFSET FROM THE FACTORY. THIS CAUSED THE RUDDER CABLE TO EXIT THE DRUM ON AN ANGLE AND RUB THE CAPSTAN. THE SERVO WAS REPLACED AND A PERMANENT FIX IS SCHEOct 3, 2008 · Cessna 525 · Horizontal Stabilizer, Attach FittingsSDR EWC2008F00000Pressure Sensor · faultyAFTER DEPARTURE, THE CREW NOTICED THE ANNUNCIATOR WARNING LIGHT COME ON FOR THE RT ENGINE FUEL FILTER BYPASS. THE CREW NOTIFIED ATC, DECLARED AN EMERGENCY, AND WERE ROUTED FOR LANDING, AFTER ARRIVING SAFELY AND CONFERRING WITH THE MFG ON FIELD, THE RT FUEL FIOct 1, 2008 · N44CK · Cessna 525 · Fuel Flow IndicatingSDR 2008FA0000705Line · rupturedRUPTURE OF TUBE AT SIDE WHERE BENDING DIES LEFT MARKING, BOTH ABOVE AND BELOW OPENING. AFTER TAKEOFF, LOW FLUID AND PRESSURE WARNING LIGHTS CAME ON AND ACFT RETURNED TO DEPARTURE. ACFT WAS TURNED OVER TO REPAIR STATION. LEAK WAS LOCATED AND LINE REPLACED ALONSep 29, 2008 · N44CK · Cessna 525 · Hydraulic System, MainSDR 2008FA0000686Line · rupturedRUPTURE OF TUBE AT SIDE WHERE BENDING DIES LT MARKING BOTH ABOVE AND BELOW OPENING. AFTER TAKEOFF, LOW FLUID AND PRESSURE WARNING LIGHTS CAME ON AND ACFT RETURNED TO AIRPORT. ACFT WAS TURNED OVER TO SERVICE CENTER. LEAK WAS LOCATED AND THE LINE REPLACED ALONSep 29, 2008 · N44CK · Cessna 525 · Hydraulic System, MainSDR AJC2008F00001Smoke Detector · false activationIN THE DESCENT FROM ALTITUDE FL430, THE BAGGAGE SMOKE LIGHT ILLUMINATED (RED). ACTION TAKEN BY CAPTAIN WAS REQUEST FOR PRIORITY HANDLING TO A SAFE LANDING IN MINUTES WITHOUT INCIDENT. PERFORMED VISUAL INSPECTION OF THE FWD AND AFT BAGGAGE COMPARTMENTS FOUND NOSep 14, 2008 · N12GS · Cessna 525 · Smoke DetectionSDR Z5F2008F00005Switch · failedDURING CLIMB THROUGH FL 270, RT HYDRAULIC FLOW LIGHT ILLUMINATED. DIVERTED, DURING DECENT RT HYD FLOW LIGHT WENT OUT. REMOVED DEFECTIVE RT FLOW SWITCH AND INSTALLED NEW SWITCH. HYDR INDICATION CHECKS NORMAL, AND AC RETURNED TO SERVICE. (K)Sep 5, 2008 · N417CS · Cessna 525 · Hydraulic System, MainSDR 2008FA0000606Fork · brokenDURING ROUTINE TAXI TO PERFORM MAINT CHECKS AFTER AC HAD BEEN PAINTED, NOSE GEAR AXLE BROKE LOOSE FROM NOSE GEAR STRUT. INVESTIGATION SHOWED BOTH WHEEL BEARING HAD HEAVY RUST AND DID NOT TURN FREELY ON THE AXLE. VERY LITTLE GREASE WAS FOUND IN EIGHER OF THE NOAug 15, 2008 · N300BV · Cessna 525 · Nose/Tail Landing Gear Strut/AxleSDR 7302008N401CSControl Cable · chafedELEVATOR TRIM CABLE CHAFED ON PULLEY BRACKET P/N 6361201-1 IN VERTICAL STABILIZER. ENGINEERING ORDER WRITTEN TO ADD FAIRLEADS TO PREVENT FURTHER CHAFING. (S)Jul 25, 2008 · N401CS · Cessna 525 · Elevator Tab Control SystemSDR 7302008N409CSControl Cable · chafedELEVATOR TRIM CABLE CHAFED ON PULLEY BRACKET P/N 6361201-1 IN VERTICAL STABILIZER. ENGINEERING ORDER WRITTEN TO ADD FAIRLEADS TO PREVENT FURTHER CHAFING. (S)Jul 25, 2008 · N409CS · Cessna 525 · Elevator Tab Control SystemSDR 7282008N430CSControl Cable · chafedELEVATOR TRIM CABLE CHAFED ON PULLEY BRACKET P/N 6361210-1 IN VERTICAL STABILIZER. ENGINEERING ORDER WRITTEN TO ADD FAIRLEADS TO PREVENT FURTHER CHAFING. (S)Jul 25, 2008 · N430CS · Cessna 525 · Elevator Tab Control SystemSDR 7282008N406CSControl Cable · chafedELEVATOR TRIM CABLE CHAFED ON PULLEY BRACKET P/N 6361201-1 IN VERTICAL STABILIZER. ENGINEERING ORDER WRITTEN TO ADD FAIRLEADS TO PREVENT FURTHER CHAFING. (S)Jul 24, 2008 · N406CS · Cessna 525 · Elevator Tab Control SystemSDR 2008FA0000491Blade · departedDURING ROUTINE INSP, FOUND DAMAGE TO THE 1ST STAGE STATOR ASSY, UPON FURTHER INSPECTION, FOUND 1 BLADE HAD FAILED AND DEPART THE LP ROTOR ASSY CAUSING DAMAGE TO THE REST OF THE ENGINE DOWN STREAM. (K)Jul 9, 2008 · N678RF · Cessna 525 · Turbine Engine Compressor SectionSDR 070808N408CSISmoke Detector · defectiveON APPROACH INTO BOS, CREW OBSERVED BAGGAGE SMOKE ANNUNCIATION. CREW DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT, FIRE DEPARTMENT PERSONNEL FOUND NO INDICATION OF SMOKE OR FIRE. MAINTENANCE PERSONNEL TROUBLESHOT SYSTEM AND REPLACED SUSPECTED DEFECTIVE SMOJul 8, 2008 · N408CS · Cessna 525 · Smoke DetectionSDR Z5F2008F00000Smoke Detector · defectiveON APPROACH, CREW OBSERVED BAGGAGE SMOKE ANNUNCIATION. CREW DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT, FIRE DEPARTMENT PERSONNEL FOUND NO INDICATION OF SMOKE OR FIRE. MAINT PERSONNEL TROUBLESHOT SYSTEM AND REPLACED SUSPECTED DEFECTIVE SMOKE DETECTOR ANDJul 8, 2008 · N409CS · Cessna 525 · Smoke DetectionSDR Z5F2008F00002Engine · leakingLIGHT SMOKE IN CABIN, THEN LT ENG MADE A LOUD POPPING SOUND, LOW OIL PRESSURE ILLUMINATED AND ENGINE ROLLED BACK, SHUTDOWN IN FLIGHT. AFTER LANDING, FOUND THAT ENGINE HAD LOST OIL. (COMING OUT OF TAIL PIPE, DRAIN MAST AND SG EXHAUST). AC CURRENTLY IN MAINTEJul 4, 2008 · N418CS · Cessna 525 · Turbine Engine Oil SystemSDR CA080625001Line · ruptured(CAN) ACFT DEPARTED AND EXPERIENCED COMPLETE HYDR FLUID LOSS. ACFT GEAR ALTERNATE EXTENDED AND RETURNED TO AIRPORT. TROUBLESHOOTING REVEALED RUPTURED HYDR PRESSURE LINE INBD OF SERVICE QUICK CONNECT. LINE REPLACED WITH NEW, AND SYS BLED. ACFT RUN FOR 10 MIN ANJun 6, 2008 · Cessna 525 · Hydraulic System, MainSDR 26N2008F00000Valve · unserviceableWHILE ON A TRAINING FLIGHT THE FLIGHT CREW SELECTED "FLAPS" ON APPROACH. AS THEY LINED UP ON THE ILS THEY SELECTED "SPEED BRAKES" AND REALIZED THAT THY HAD NO HYDRAULICS ON THE AIRCRAFT. WHEN "GEAR DOWN" WAS SELECTED, THE CREW DID NOT SEE A DOWN AND LOCKED CMay 31, 2008 · N72JW · Cessna 525 · Hydraulic Reservoir, MainSDR 042908N412CSDetection Sys · false activationDURING APPROACH, BAGGAGE SMOKE DETECTOR LIGHT ILLUMINATED AND AC DIVERTED AND LANDED WITHOUT INCIDENT. NO SMOKE EVIDENT DURING AFTER LANDING CHECK. BOTH FWD AND AFT BAGGAGE SMOKE DETECTORS WERE REPLACED, OPERATIONALLY CHECKED GOOD AND THE AIRCRAFT RETURNED TO Apr 29, 2008 · N412CS · Cessna 525 · Smoke DetectionSDR AMCR200800001Heating Element · failedPILOT REPORTED T2 HEATER FAIL ON RT ENGINE. FOUND T2 PROBE BAD.Mar 31, 2008 · N279DV · Cessna 525 · Fuel HeaterSDR 3302008N406CSPcb · burned outDURING APPROACH, WHEN LANDING GEAR WAS SELECTED DOWN, THE DOWN AND LOCKED GREEN LIGHTS DID NOT ILLUMINATE ALTHOUGH THE GEAR FELT LIKE IT EXTENDED. THE GEAR WAS BLOWN DOWN BUT THE INDICATION DID NOT APPEAR. THE COCKPIT FLOOD LIGHTS WERE SELECTED AND THE DOWN ANMar 30, 2008 · N406CS · Cessna 525 · Landing Gear Position and WarningSDR AIH2008F00000Pump · seizedLT HYD PUMP LOW FLOW ANNUNCIATOR ILLUMINATED. MAINT FOUND THE LT HYD PUMP WAS SEIZED. PUMP WAS REPLACED WITH NEW AND PROBLEM WAS SOLVED. (K)Jan 17, 2008 · N940SW · Cessna 525 · Hydraulic Pump (Electric/Engine), MainSDR AMCR200700004Jam-Nut · wrong partDURING COMPLIANCE WITH SL525B-27-01 WHICH IS CHECKING FLAP PUSH ROD FOR IMPROPER SAFETY WIRING, FOUND THAT THE AFT JAM NUT (NAS509L6) WAS UP AGAINST THE CENTER STUD (6365028-10) RATHER THAN TIGHT AGAINST THE ROD END TUBE (6365028-9). EVERYTHING WAS SAFETIED INDec 7, 2007 · N279DV · Cessna 525 · Trailing Edge FlapsSDR 113007N423CSSmoke Detector · false indicationDURING CLIMB AT 15,000 FT, THE BAGGAGE SMOKE LIGHT ILLUMINATED. AIRCRAFT DIVERTED TO HPN AND MADE AN UNEVENTFUL LANDING. THE SYSTEM WAS TROUBLESHOT AND THE PROBLEM COULD NOT BE DUPLICATED. THE AIRCRAFT WAS RETURNED TO SERVICE.Nov 30, 2007 · N423CS · Cessna 525 · Smoke DetectionSDR 110407N420CS1Bulb · burned outDURING APPROACH CREW NOTICED NO RT GEAR DOWN INDICATION. CREW FOLLOWED EMERGENCY PROCEDURES, BLEW GEAR DOWN AND DECLARED AN EMERGENCY. AIRCRAFT LANDED WITHOUT INCIDENT . MAINTENANCE PERSONNEL FOUND CAUSE TO BE BURNED OUT BULB. BULB REPLACED, SYSTEM OPS CHECKENov 4, 2007 · N420CS · Cessna 525 · Landing Gear Position and WarningSDR CA071114008Wire Harness · shorted(CAN) THE EMERGENCY BRAKE HAD TO BE USED UPON LANDING AS IT WAS DISCOVERED THAT THE ANTI-SKID WIRING HARNESS HAD A SMALL AMOUNT OF SLACK BETWEEN THE TRAILING LINK AND THE TRUNNION. THIS ALLOWED IT TO RUB AGAINST THE TIRE, WEARING OFF THE COATING AND UPON LANDINov 2, 2007 · Cessna 525 · Landing Gear System WiringSDR 101107N423CSTire · rupturedDURING LANDING ROLL OUT, BEFORE BRAKES WERE APPLIED A SEVERE VIBRATION WAS FELT AND THE AIRCRAFT SUDDENLY PULLED TO THE RIGHT. AIRCRAFT WAS STOPPED ON A TAXIWAY AND CREW DISCOVERED RIGHT MAIN TIRE MISSING AND WHEEL DAMAGED.Oct 11, 2007 · N423CS · Cessna 525 · TireSDR 100607N409CSCowling · departedDURING FLIGHT, THE RT ENGINE LOWER COWL SEPARATED FROM THE ENGINE. DAMAGE TO THE RT HORIZONTAL STABILIZER OCCURRED CAUSED BY IMPACT DAMAGE. CREW REPORTED FEELING A SLIGHT "BUMP" DURING THE FLIGHT, HOWEVER THERE WAS NO INDICATION OR ABNORMAL FLIGHT CHARACTERISTOct 6, 2007 · N409CS · Cessna 525 · Engine Cowling SystemSDR CA080207003Converter · inoperative(CAN) MFD FAIL TO COME ON WHEN ACFT MASTER SWITCH TURNED ON. DC-DC CONVERTER REPLACED - SAME PROBLEM OCCURED AT 102.6 AIRFRAME HRS. - 66 AIRFRAME CYLES, AND DC-DC CONVERTER REPLACED AGAIN (33 HRS + 19 CYCLES) MFG IS AWARE OF THE POOR QUALITY OF THE RR18 DC-DC Sep 20, 2007 · Cessna 525 · DC Rectifier/ConverterSDR 082907N413CS1Trim System · out of adjustENROUTE, AT CRUISE ALTITUDE OF 5000 FT AIRCRAFT STARTED TO TURN RT, DISENGAGED AUTO-PILOT, TURN STILL EXISTED. DIVERTED TO TOL AND LANDED WITHOUT INCIDENT. AIRCRAFT CURRENTLY IN MAINTENANCE. CAUSE UNKNOWN AT THIS TIME. 09-03-07 ALL CONTROL RUDDER, AILERON ANAug 29, 2007 · N413CS · Cessna 525 · Elevator Control SystemSDR 2007FA0000566Fuel · contaminatedPERFORMED AN EMERGENCY LANDING, DUE TO A FUEL BYPASS LIGHT COMING ON IN FLIGHT. THE AIRCRAFT LANDED AND TAXIED TO THE SERVICE CENTER WITHOUT INCIDENT. THE CAUSE OF THE LIGHT HAS BEEN DETERMINED TO BE THE FUEL ITSELF. THE FUEL IS CONTAMINATED WITH VISIBLE DEJun 8, 2007 · N41YP · Cessna 525 · Aircraft Fuel SystemSDR 052407N412CSLanding Gear · malfunctionedON APPROACH, AFTER GEAR WAS EXTENDED, NO GEAR DOWN INDICATION WAS NOTED ON ANY OF THE (3) ANNUNCIATORS. ABORTED APPROACH INITIATED A GO-AROUND AND RAN THE GEAR CHECKLIST. TOWER ADVISED ALL GEAR APPEARED TO BE DOWN. BLEW GEAR DOWN AND REQUESTED EMERGENCY EQUIPMMay 24, 2007 · N412CS · Cessna 525 · Landing Gear Retraction/Extension SystemSDR 052107N151CSStructure · damagedON APPROACH, CREW ENCOUNTERED FLOCK OF GEESE RESULTING IN NUMEROUS STRIKES. ABORTED APPROACH, INITIATED AFM ABNORMAL CHECKLIST WITH NO ABNORMALITIES NOTED. DIVERTED, DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. AFTER LANDING AND EXITING AIRCRAFT, CREW NOMay 21, 2007 · N151CS · Cessna 525 · Aircraft StructuresSDR 050807N406CS1Unknown · unknownON DESCENT INTO CYYZ THE BAGGAGE SMOKE LIGHT ILLUMINATED. NO VISUAL OR ODOR OF SMOKE WAS DETECTED BY THE FLIGHT CREW. THE CREW DECLARED AN ENERGENCY AND DIVERTED TO BUF. LANDING WAS UNEVENTFUL. NO SIGNS OF SMOKE OR FIRE INSIDE THE BAGGAGE COMPARTMENT WAS DETECMay 8, 2007 · N406CS · Cessna 525 · Detection SystemSDR CA070427004Starter Gen · failed(CAN) GENERATOR OUTPUT FAILURE, NO OUTPUT. (TC NR 20070427004)Apr 23, 2007 · Cessna 525 · Starter-GeneratorSDR 33107N128CS1Attenuator · malfunctionedAFTER ROTATION MASTER CAUTION, HYD PRESS ON AND ATTENUATOR UNLOCKED RT ILLUMINATED. THE CREW SELECTED STOW WITH NO EFFECT AND THE ATTENUATOR COULD BE HEARD OPENING AND CLOSING IN FLIGHT. CREW NOTIFIED TOWER THEY HAD AN EMERGENCY AND REQUESTED RETURN TO ROCHEMar 31, 2007 · N128CS · Cessna 525 · Engine Thrust ReverserSDR 031307N425CS1Smoke Detector · dirtyON DESCENT FL110 THE BAGGAGE SMOKE LIGHT ILLUMINATED ON THE ANNUNCIATOR PANEL. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. NO SMOKE OR SMELL WAS NOTICED IN THE CABIN BY THE FLIGHT CREW. MAINTENANCE TROUBLESHOT THE SYSTEM FOUND DUST ON THE CEILIMar 13, 2007 · N425CS · Cessna 525 · Smoke DetectionSDR CA070213002Valve · failed(CAN) POST INSPECTION RUN REVEALED HYDRAULIC PRESSURE ON ANNUNCIATOR LIGHT DID NOT EXTINGUISH WHEN SYSTEM SHOULD HAVE BEEN AT REST. HYDAULIC LOADING VALVE FOUND FAILED. BLEED ORIFICE RECOVERED FROM HYDRAULIC MANIFOLD UNDER RELIEF VALVE (3RD FROM LOADING VALVEJan 31, 2007 · Cessna 525 · Hydraulic System, MainSDR 011607N152CS1Actuator · faultyAFTER TAKE-OFF FROM SAT, CREW NOTICED POWER BRAKE FAIL AND POWER BRAKE PRESS LOW ANNUNCIATORS. CREW PERFORMED AFM PROCEDURE CHECKS FOR THIS INDICATION WITH NO EFFECT. CREW DECLARED AN EMERGENCY AND RETURNED TO SAT FOR INSPECTION AND REPAIR OF FAULT.MAINTENANCEJan 14, 2007 · N152CS · Cessna 525 · Landing Gear Actuator
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