Beech 400A

Service difficulty reports · 1,397

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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 = '400A'
  ORDER BY difficulty_date DESC"

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SDR DXTA200802740Control Unit · malfunctionedRED HSTAB FAIL WARNING LIGHT ILLUMINATED SHORTLY AFTER TAKEOFF. REPLACED 170 AND 180 KNOT AIRSPEED SWITCHES WITH NEW IAW HAWKER 400XP WIRING MANUAL CH 30-12-01. REPLACED OAT BIAS BOX WITH NEW IAW HAWKER 400XP MM CH 32-12-00. H-STAB DEICE SYSTEM OPS CHECK GOODJan 1, 2008 · N125QS · Beech 400A · Central WarningSDR DJFA2007153Downlock Switch · inoperativeON APPROACH CREW REPORTED THE LT MAIN GEAR DOWN AND LOCKED LIGHT WOULD NOT ILLUMINATE. GEAR WAS CYCLED 6 TIMES AND ON THE 6TH ATTEMPT THE DOWN AND LOCKED LIGHT FINALLY ILLUMINTATED. EMERGENCY WAS DECLARED AND AIRCRAFT LANDED SAFELY. MAINTENANCE FOUND THE LTDec 31, 2007 · N463LX · Beech 400A · Landing Gear Position and WarningSDR DJFA2007152Terminal · looseON CLIMB OUT CREW REPORTED A BURNING ODOR FROM THE PILOT'S CIRCUIT BREAKER PANEL. MAINTENANCE FOUND A LOOSE TERMIAL ON A CIRCUIT BREAKER ON THE NON-ESSENTIAL BUSS. THE TERMIAL APPEARED TO BE OVERHEATED AND WAS REPLACED.Dec 29, 2007 · N783TA · Beech 400A · Electrical Power System WiringSDR DJFA2007150Unknown · odorIN CRUISE, CREW NOTED BURNING ODOR FROM HEAT DUCTS. MAINTENANCE TESTED THE ENVIRONMENTAL SYSTEM BUT WAS UNABLE TO DUPLICATE THE DISCREPANCY.Dec 26, 2007 · N783TA · Beech 400A · Air Distribution SystemSDR DJFA2007149Rib · crackedDURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSPECTION OF THE HORIZONTAL STABILIZER IB RIB AND BRACKET ASSEMBLIES, THE LT IB RIB WAS FOUND CRACKED. DETAILED INSPECTION INSTRUCTIONS OF THIS AREA ARE OUTLINED IN COMMUNIQUDec 24, 2007 · N793TA · Beech 400A · Horizontal Stabilizer, Spar/RibSDR DXTA200702703Uplock Hook · out of adjustAFTER LANDING GEAR RETRACTION, LANDING GEAR UNLOCKED/IN-TRANSIT LIGHT REMAINED ILLUMINATED. GEAR EXTENDED NORMALLY, NORMAL LANDING. ADJUSTED NOSE GEAR UPLOCK HOOK TO PROPERLY ENGAGE IAW 400A M/M CH. 32-20-00. SWUNG GEAR MULTIPLE TIMES, OPS CHECK GOOD.Dec 23, 2007 · N141QS · Beech 400A · Landing Gear Position and WarningSDR DJFA2007148Fan · overheatedON LANDING CREW REPORTED BURNING ODOR IN THE CABIN. MAINTENANCE FOUND THE CABIN TEMP SENSOR FAN OVERHEATING. THE FAN WAS REPLACED.Dec 22, 2007 · N439LX · Beech 400A · Air Distribution FanSDR DXTA200702712Computer · inoperativeRUDDER BOOST FAIL LIGHT CAME ON AND YAW DAMPNER/AUTOPLOT KICKED OFF AT F230 LEVEL FLIGHT AT THE SAME TIME. REPLACED #1 FGC-4007 WITH OVH. UNIT IAW ROCKEWELL COLLINS MANUAL 523-0225807-0411A REV 9 OCT. 2005. GROUND OPS CHECK GOOD.Dec 21, 2007 · N117QS · Beech 400A · Autopilot SystemSDR DXTA200702711Landing Gear · malfunctionedRAISED LANDING GEAR AFTER TAKEOFF; ALL THREE GREEN LIGHTS EXTINGUSHED EXCEPT 2 RED LIGHTS IN GEAR HANDLE; SELECTED GEAR DOWN, ALL 3 GEAR LIGHTS ON AND RED EXTINGUSHED; BROUGHT GEAR UP, ALL 3 GREEN LIGHTS EXTINGUSHED AND 2 RED LIGHTS REMAINED ON IN GEAR HANDLE.Dec 21, 2007 · N139QS · Beech 400A · Landing Gear Retraction/Extension SystemSDR DXTA200702700Bulb · burned outLT MAIN GEAR DOWN AND LOCK INDICATION INOPERATIVE. REPLACED LT MAIN LANDING GEAR DOWN INDICATION BULB. OPS CHECK GOOD IAW HAWKER 400XP MM CH 32-60-00.Dec 20, 2007 · N120QS · Beech 400A · Landing Gear Position and WarningSDR DXTA200702688Switch · inoperativeAFTER TAKEOFF PITCHTRIM FAILED AT 2000 FT AGL, PITCH TRIM WOULD NOT LEAVE GREEN ARC. FOUND PILOTS PITCH TRIM SWITCH INOP. REMOVED PILOTS YOKE ASSY. PN 128284060-13 SN 0039 AND INSTALLED NEW PILOTS YOKE ASSY. PN 128384060-13, SN 0076. IAW CMM 27-10-15 OPERATIODec 18, 2007 · N101QS · Beech 400A · Control Column SectionSDR DJFA2007146Brake · malfunctionedON LANDING CREW REPORTED NO BRAKES UNTIL (2) OR (3) TIMES NORMAL PRESSURE IS APPLIED TO THE BRAKE PEDDALS THEN THE BRAKES GRAB EXTREAMLY HARD. MAINTENANCE BLED THE SYSTEM AND TAXIED THE AIRCRAFT WITH NO FURTHER PROBLEMS NOTED.Dec 17, 2007 · N470LX · Beech 400A · Landing Gear Brake SystemSDR DXTA200702678Warning System · false activationRED LIGHTS IN GEAR HANDLE REMAINED ILLUMINATED AFTER GEAR RETRACTION. UPON EXTENTION THE RED LIGHTS WENT OUT AND (3) GREENS ILLUMINATED. JACKED AC VISUALLY INSPECTED LANDING GEAR UPLOCK AND DOWN LOCK SWITCHES. VISUALLY INSPECTED MLG DOOR SWITCHES. NO DEFECTS Dec 14, 2007 · N154QS · Beech 400A · Landing Gear Position and WarningSDR DJFA2007143Rib · crackedDURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSPECTION OF THE HORIZONTAL STABILIZER INBOARD RIB AND BRACKET ASSEMBLIES, THE RIGHT INBOARD RIB WAS FOUND CRACKED. DETAILED INSPECTION INSTRUCTIONS OF THIS AREA ARE OUTLINEDDec 13, 2007 · N743TA · Beech 400A · Horizontal Stabilizer, Spar/RibSDR DJFA2007142Rib · crackedDURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSPECTION OF THE HORIZONTAL STABILIZER IB RIB AND BRACKET ASSEMBLIES, THE RT IB RIB WAS FOUND CRACKED. DETAILED INSPECTION INSTRUCTIONS OF THIS AREA ARE OUTLINED IN COMMUNIQUDec 13, 2007 · N741TA · Beech 400A · Horizontal Stabilizer, Spar/RibSDR DJFA2007141Rib · crackedDURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSPECTION OF THE HORIZONTAL STABILIZER IB RIB AND BRACKET ASSEMBLIES, THE LT IB RIB WAS FOUND CRACKED. DETAILED INSPECTION INSTRUCTIONS OF THIS AREA ARE OUTLINED IN COMMUNIQUDec 12, 2007 · N775TA · Beech 400A · Horizontal Stabilizer, Spar/RibSDR DJFA2007140Inlet · crackedDURING POSTFLIGHT, CREW REPORTED CRACKS ON THE NR2 INLET RING. MAINTENANCE CONFIRMED THE DISCREPANCY AND REPLACED THE INLET RING.Dec 7, 2007 · N449LX · Beech 400A · Turbine Engine Air Inlet SectionSDR DJFA2007139Unknown · odorON APPROACH CREW REPORTED BURNING SMELL FROM THE RT REAR FLOOR AREA. MAINTENANCE RAN THE AIRCRAFT BUT WAS UNABLE TO DETECT ANY SMELL IN ALL CABIN TEMPERATURE MODES (AUTO/MANUAL, HOT AND COLD). AIRCRAFT WAS RELEASED.Dec 5, 2007 · N709TA · Beech 400A · Air Distribution SystemSDR DXTA200702651Wire · damagedH-STAB FAIL ANNUNCIATOR LIGHT ILLUMINATED IN FLIGHT. TROUBLESHOT SYSTEM FOUND TOO LARGE OF AN OHM SPLIT AT C/P 473 OF CONTROLLER, TRACED WIRING BACK TO TB061 STILL HAD LARGE SPLIT OHM DIFFERENCE. REMOVED LT STAB LEADING EDGE, REPAIRED CONNECTIONS AT TB060 ANDec 4, 2007 · N153QS · Beech 400A · Stabilizer System WiringSDR JEMA010208002Bulkhead · crackedWHILE PERFORMING A SCHEDULED A-B INSPECTION, FOUND RT AND LT AFT FUSELAGE BLEED AIR LINE ATTACH BRACKETS PULLED FROM AFT FUSELAGE BULKHEAD RESULTING IN CRACKS IN THE BULKHEADS AT FRAME STATION 329.92. THIS IS THE 4TH AIRCRAFT IN A ROW THAT THE BULKHEAD HAS BDec 1, 2007 · N48MF · Beech 400A · Fuselage Main, BulkheadSDR JEMA010208001Window · crackedWHILE PERFORMING A SCHEDULED A-B INSPECTION FOUND NR 2 (CO-PILOT) SIDE WINDOW CRACKED USING THE PRISM INSPECTION METHOD. THE (D) INSPECTION IS THE ONLY INSPECTION THAT REQUIRES THAT BOTH WINDSHIELDS BE INSPECTED BY REMOVING THE WINDSHIELD RETAINERS OR USING ODec 1, 2007 · N48MF · Beech 400A · Flight Compartment WindowsSDR DXTA200702631Warning Light · illuminatedWHEN HORIZONTAL STAB DE ICE WAS TURNED OFF AFTER CLIMB OUT THE RED STAB ANTI-ICE FAIL LIGHT ILLUMINATED STEADY. EMERGENCY ACTION TAKEN. CANNOT DUPLICATE SQUAWK. INSPECTED COMPONENTS IN TAIL AND NOSE BAYS. MEASURED SENSOR & HEATER RESISTANCES. CHILLED LEFT Nov 28, 2007 · N141QS · Beech 400A · Airfoil Anti/De-ice SystemSDR 420CT010Sensor · contaminatedDURING CLIMB NOTICED COCKPIT VERY WARM TO HOT. BETWEEN 12000' AND 18000' IT APPEARED A THIN LAYER OF SMOKE WAS PRESENT IN THE COCKPIT. ABOUT 30 SECONDS LATER THE FIRST OFFICER VERIFIED THERE WAS SMOKE IN THE COCKPIT AND THICKER. EMERGENCY DESCENT AND LANDINNov 27, 2007 · N420CT · Beech 400A · Cabin Temperature Control SystemSDR DJFA2007137Rib · crackedDURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSPECTION OF THE HORIZONTAL STABILIZER IB RIB AND BRACKET ASSEMBLIES, THE LT IB RIB WAS FOUND CRACKED. DETAILED INSPECTION INSTRUCTIONS OF THIS AREA ARE OUTLINED IN COMMUNIQNov 23, 2007 · N750TA · Beech 400A · Horizontal Stabilizer, Spar/RibSDR 2007FA0001067Control Valve · malfunctionedTROUBLESHOT INOPERATIVE THRUST REVERSER DEPLOYMENT. FOUND LT, RT REVERSERS MECHANICALLY STIFF AND DIFFICULT TO OPERATE. THRUST REVERSER LINKS AND PIVOTS FOUND DRY, INITIAL 400 HR LUBRICATION NOT DUE FOR 55 HRS. LUBED REVERSERS IAW MM. 12-20-00, VERIFIED OPNov 19, 2007 · N420CT · Beech 400A · Engine Thrust ReverserSDR 2007FA0001066Transmitter · inoperativeTROUBLESHOT IN-FLIGHT (FLAP ASSYMETRY) ANNUNCIATOR INDICATION. FOUND RT FLAP POSITION TRANSMITTER RESISTANCE TO GO ABOVE SERVICE LIMITS WHEN COLD SOAKED. REPLACED RT FLAP POSITION TRANSMITTER AND ADJUSTED LT , RT FLAP FOLLOW-UP SWITCHES AND POSITION TRANSMITNov 19, 2007 · N420CT · Beech 400A · Trailing Flap Position Indicating SystemSDR DJFA2007136Rib · crackedDURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSPECTION OF THE HORIZONTAL STABILIZER IB RIB AND BRACKET ASSEMBLIES, THE RT IB RIB WAS FOUND CRACKED. DETAILED INSPECTION INSTRUCTIONS OF THIS AREA ARE OUTLINED IN COMMUNIQUNov 19, 2007 · N709TA · Beech 400A · Horizontal Stabilizer, Spar/RibSDR DJFA2007135Converter · failedAFTER LANDING CREW REPORTED BURNING ODOR COMING FROM AREA AROUND PAX TABLE. MAINTENANCE FOUND THE DC TO DC CONVERTOR FAILED. THE COMPONENT WAS REPLACED.Nov 18, 2007 · N454LX · Beech 400A · DC Rectifier/ConverterSDR DJFA2007134Rib · crackedDURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSPECTION OF THE HORIZONTAL STABILIZER IB RIB AND BRACKET ASSEMBLIES, THE RT IB RIB WAS FOUND CRACKED. DETAILED INSPECTION INSTRUCTIONS OF THIS AREA ARE OUTLINED IN COMMUNIQNov 16, 2007 · N794TA · Beech 400A · Horizontal Stabilizer, Spar/RibSDR DJFA2007131Unknown · odorTHE CREW REPORTED HOT ODOR FROM CABIN DUCTING. RT SIDE TABLE FELT HOT AFTER SHUTDOWN. MAINTENANCE REMOVED THE SIDEWALL PANEL AND INSPECTED DUCTING. THE AIRCRAFT WAS RUN IN FULL HOT. NO DEFECTS OR LEAKS WERE NOTED. NO (HOT) OR BURNING ODOR NOTED DURING GRONov 13, 2007 · N708TA · Beech 400A · Air Distribution SystemSDR 2008FA0000090Wire · chafedPITCH TRIM INOPERATIVE REMOVED RT FWD GALLEY AND RT FWD PARTITION. FOUND WIRE BUNDLE CHAFED BEHIND PARTITION. REPAIRED (3) WIRES THAT WERE CHAFED THROUGH TO THE CONDUCTORS. PROVIDED CLEARANCE BETWEEN WIRE BUNDLE AND PARTITION. INSTALLED ANTI-CHAFE MATERIALNov 12, 2007 · N213BK · Beech 400A · Flight Control System WiringSDR 2007FA0001069Pipe · crackedPERFORMED HOT SECTION INSPECTION PRIOR TO SCHEDULED 1800 HR INTERVAL TO INVESTIGATE COMPLAINT OF SLOW STARTING. UPON DISASSEMBLY, FOUND DIFFUSER PIPES OF GAS GENERATOR CASE CRACKED AND PORTIONS MISSING AT APPROXIMATE 10:30, 11:00 POSITION. SUSPECT CAUSED BY Nov 11, 2007 · N400MV · Beech 400A · Turbine Engine Compressor SectionSDR 2007FA0001068Bonding Jumper · frayedTROUBLESHOT REPORT OF HORIZONTAL STABILIZER ANTI-ICE SYSTEM FAIL INDICATION. NOTED ELEVATOR HORN HEAT SYSTEM RESISTANCE READINGS ERRATIC WHEN ELEVATORS MOVED. FOUND ELEVATOR BONDING JUMPERS FRAYED AND CORRODED. REPLACED ELEVATOR BONDING JUMPERS, ELEVATOR HONov 11, 2007 · N400MV · Beech 400A · Elevator Control SystemSDR DJFA2007129Rib · crackedDURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSPECTION OF THE HORIZONTAL STABILIZER INBOARD RIB AND BRACKET ASSEMBLIES, THE LT AND RT IB RIBS WERE FOUND CRACKED. DETAILED INSPECTION INSTRUCTIONS OF THIS AREA ARE OUTLINENov 10, 2007 · N441LX · Beech 400A · Horizontal Stabilizer, Spar/RibSDR DJFA2007126Rib · crackedDURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSPECTION OF THE HORIZONTAL STABILIZER INBOARD RIB AND BRACKET ASSEMBLIES, THE LT IB RIB WAS FOUND CRACKED. DETAILED INSPECTION INSTRUCTIONS OF THIS AREA ARE OUTLINED IN CONov 8, 2007 · N744TA · Beech 400A · Horizontal Stabilizer, Spar/RibSDR DXTA200702599Landing Gear · malfunctionedRED LIGHT IN MLG HANDLE STAYS ON AFTER GEAR RETRACTION. JACKED ACFT & INSTALLED HYD MULE. CHECKED MLG UPLOCK ASSY'S & ADJUSTED RT MLG UPLOCK IAW MM 32-30-00. ACCOMPLISHED GEAR SWINGS WHILE SLOWLY REDUCING HYD PRESSURE. AT 1200 PSI RED HANDLE MLG LIGHT STAYNov 6, 2007 · N138QS · Beech 400A · Landing Gear Retraction/Extension SystemSDR DJFA2007124Rib · crackedDURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSPECTION OF THE HORIZONTAL STABILIZER IB RIB AND BRACKET ASSEMBLIES, THE RT SIDE ROLLER BRACKET WAS FOUND CRACKED. DETAILED INSPECTION INSTRUCTIONS OF THIS AREA ARE OUTLINENov 4, 2007 · N484CW · Beech 400A · Horizontal Stabilizer, Spar/RibSDR DXTA200702592Relay · inoperativeWHEEL BRAKES FAILED DURING TAXI OUT. REPLACED POWER BRAKE RELAY VALVE ASSY IAW 32-40-00. OPS CK GOOD.Nov 3, 2007 · N161QS · Beech 400A · Landing Gear Brake SystemSDR DJFA2007123Hose · rupturedON APPROACH CREW EXPERIENCED COMPLETE HYDRAULIC FAILURE AT 4000' ON APPROACH INTO KDAL, LOST ALL HYDRAULIC PRESSURE WITHIN ABOUT 20 SEC. AFTER FIRST INDICATION OF A PROBLEM, DECLARED AN EMERGENCY, RAN THE EMERGENCY CK LIST FOR GEAR EXTENSION, ZERO FLAP LANDINGNov 3, 2007 · N413LX · Beech 400A · Hydraulic System, MainSDR DXTA200702589Strut · lowAFTER GEAR RETRACTION, RED IN TRANSIT LIGHT REMAINED ILLUMINATED. JACKED ACFT, REMOVED LT HYDRAULIC PUMP & INSTALLED ON HYDRAULIC POWER UNIT. CYCLED GEAR 30 TIMES WITH NO FAILURES NOTED. ACCESSED CONNECTORS P271 & P272 IN LT & RT GEAR WELLS. OHMED OUT UPLOCK Nov 2, 2007 · N138QS · Beech 400A · Nose/Tail Landing Gear Strut/AxleSDR 2007FA0000987Bulkhead · crackedWHILE PERFORMING AN A-C INSPECTION FOUND RT AFT FUSELAGE BLEED AIR LINE ATTACH BRACKET PULLED FROM FUSELAGE BULKHEAD RESULTING IN A CRACK IN THE BULKHEAD AT FRAME STATION 329.92. RECOMMEND CONTACTING MFG FOR REPAIR OPTIONS CRACK HAS BEEN FOUND ON BOTH SIDES Nov 1, 2007 · N940VA · Beech 400A · Fuselage Main, BulkheadSDR N425CT0003Hydromech Unit · restrictedPARTIAL POWER LOSS FROM RT ENGINE AT FL 390 POWER SURGED DURING APPROACH AND LANDING.Oct 31, 2007 · N425CT · Beech 400A · Fuel Control/Turbine EnginesSDR 2007FA0000988Pivot · looseWHILE PERFORMING AN A-C INSPECTION FOUND 8 LOOSE RIVETS IN THE FORWARD RIVET LINE OF THE ATTACHMENT PIVOT FITTING PN 45A2118311 ON THE BOTTOM OF THE HORIZONTAL STABILIZER. IT IS SUSPECTED THAT THE LOOSE RIVETS WERE CAUSED BY FATIGUE AND AGE.Oct 31, 2007 · N940VA · Beech 400A · Horizontal Stabilizer, Attach FittingsSDR DXTA200702577Bearing · wornAFTER TAKEOFF, NOSE GEAR WOULD NOT RETRACT. REMOVED NOSE GEAR. DISASSEMBLED AND INSPECTED. REPLACED NLG LOWER BEARING WITH NEW BEARING P/N 128-350042-1, SCRAPER RING WITH EW RING P/N 2145-24-0160 AND ALL INTERNAL AND EXTERNAL SEALS. SERVICED AND REINSTALLED SOct 28, 2007 · N153QS · Beech 400A · Nose/Tail Landing GearSDR DXTA200702568Receptacle · damagedAIRCRAFT TAXIED WITH GPU STILL ATTACHED. REMOVED AND REPLACED GPU POWER RECEPTACLE IAW 24-40-00. OPS CHECK WAS GOOD.Oct 24, 2007 · N142QS · Beech 400A · Fuselage Miscellaneous StructureSDR DXTA200702563Transducer · inoperativeON CLIMB OUT AFTER FLAP RETRACTION, ACCELERATING THROUGH 160 KIS, (RDR BST FAIL) YELLOW CAUTION LIGHT ILLUMINATED ALONG WITH DISENGAGEMENT OF THE YAW DAMPER. REMOVED NR 1 ENGINE TRANSDUCER PN APTE233A-1750300A SN 7064-16-116, 7064-16-129 AND NR 2 ENGINE TRANSDOct 23, 2007 · N132QS · Beech 400A · Trailing Edge Flap Control SystemSDR DJFA2007122Computer · out of adjustCREW REPORTED ENGINE ROLL BACK OF 5 PERCENT N1 ON THE RT ENGINE FOLLOWED BY A FLUXUATION OF 3-4 PERCENT. ENGINE STABILIZED AFTER ENGINE HEAT WAS TURNED ON. MAINTENANCE ADJUSTED THE EFC AUTHORITY.Oct 23, 2007 · N476LX · Beech 400A · Fuel Control/Turbine EnginesSDR DJFA2007121Coalescer Bag · dirtyCREW REPORTED ODOR OF SMOKE IN THE LAV AREA WITH WING HEAT ON IN ICING CONDITIONS. ODOR DISAPATED AFTER WING A/I WAS SHUTOFF. MAINTENANCE DISCOVERED THE COALESCER SOCK DIRTY. THE COALESCER SOCK WAS REPLACED.Oct 21, 2007 · N478LX · Beech 400A · Humidity Control SystemSDR 2007FA0000939Lamp · inoperativePILOT HAD NO GREEN DOWN AND LOCKED INDICATION FOR THE RT GEAR WHEN LANDING. PILOT CONFIRMED WITH THE TOWER THE GEAR WAS DOWN, ALSO THE PILOT CONFIRMED THAT THE LIGHT WOULD NOT ILLUMINATE WHEN TESTED. AFTER LANDING MAINTENANCE CHECKED OUT AIRCRAFT AND REPLACED Oct 21, 2007 · N442GJ · Beech 400A · Landing Gear Position and WarningSDR DJFA2007120Rib · crackedDURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSPECTION OF THE HORIZONTAL STABILIZER IB RIB AND BRACKET ASSEMBLIES, THE LT IB ROLLER BRACKET WAS FOUND CRACKED. DETAILED INSPECTION INSTRUCTIONS OF THIS AREA ARE OUTLINED Oct 19, 2007 · N417LX · Beech 400A · Horizontal Stabilizer, Spar/Rib
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