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 DJFA20131009001Fdu · low pressureDURING INITIAL DESCENT FROM CRUISE, CREW NOTED SLIGHT (200LBS) FUEL IMBALANCE. CROSSFEED FROM RT TANK WAS ACTIVATED MANUALLY. WITHIN 15 TO 30 SECONDS CREW NOTED INDICATIONS OF UNCOMMANDED LT ENGINE SHUTDOWN. ENGINE RESTART PROCEDURE WAS INITIATED WITH SUCESOct 9, 2013 · N410FL · Beech 400A · Fuel Controlling SystemSDR DJFA20130925001Cap · misinstalledDURING CRUISE, CREW NOTED LOW OIL PRESSURE INDICATION ON THE RT ENGINE. FOLLOWING THE CHECKLIST PROCEDURE, ENGINE WAS SHUTDOWN AND THE ACFT DIVERTED TO ANOTHER LANDING SITE. MX INSPECTION FOUND THAT THE OIL CAP WAS NOT INSTALLED ON THE OIL FILLER NECK.Sep 25, 2013 · N427FL · Beech 400A · Reciprocating Engine Oil SystemSDR 9JLA2013120404241Gcu · defectiveTHE CREW REPORTED THAT THE LT GEN FAILED IN FLIGHT & THEY WERE UNABLE TO RESET THE GEN IAW THE ACFT CHECKLIST. TROUBLESHOOTING IDENTIFIED THE LT GCU AS DEFECTIVE, PN 51539-006J, SN Y1434. THE DEFECTIVE GCU WAS REMOVED & AN OVERHAULED GCU WAS INSTALLED. OPERASep 17, 2013 · N92LP · Beech 400A · AC RegulatorSDR DJFA20130912001Transducer · unsecureDURING LANDING, CREW REPORTED STIFF BRAKES FOLLOWED BY INTERMITTENT ANTI-SKID OPERATION. MX FOUND THE WHEEL SPEED TRANSDUCER NOT ENGAGED WITH THE WHEEL HUB CAP ASSY. MX CORRECTED THE CONDITION.Sep 12, 2013 · N438LX · Beech 400A · Brake Anti-Skid SectionSDR 9JLA2013092303777Switch · defectiveFLIGHT CREW REPORTED THAT DURING DESCENT TO LANDING, NORMAL PITCH TRIM OPERATED MUCH SLOWER THAN NORMAL. MX TROUBLESHOT THE NORMAL PITCH TRIM OPERATION AND FOUND THE 250 KT AIRSPEED SWITCH IN THE NR 1 ADC DEFECTIVE.Sep 10, 2013 · N393GH · Beech 400A · Airspeed/Mach IndicatorSDR DJFA20130910002Duct · contaminatedPASSENGER REPORTED BURNING ODOR IN THE CABIN DURING FLIGHT. AFTER LANDING, CREW NOTED LOWER FORWARD RT SIDE WALL AND FOLDING TABLE WERE HOT TO THE TOUCH. MX FOUND HEATER DUCT TO BE CONTAMINATED WITH CARBONATED DRINK FROM PASSENGER SPILL. THE DUCT WAS CLEANESep 10, 2013 · N438LX · Beech 400A · Air Distribution SystemSDR DJFA20130908001Transducer · failedDURING LANDING, CREW REPORTED ANTI-SKID OPERATION SLUGGISH RESULTING IN DECREASED BREAKING EFFECTIVENESS. MX INSPECTED THE SYS AND FOUND THE RT WHEEL SPEED TRANSDUCER OUT OF LIMITS. THE TRANSDUCER WAS REPLACED.Sep 8, 2013 · N438LX · Beech 400A · Brake Anti-Skid SectionSDR 9JLA2013090504239Actuator · defectiveTHE FLIGHT CREW REPORTED THAT THE RT RETRACTABLE LANDING LIGHT WOULD NOT RETRACT AND STOW. TROUBLESHOOTING IDENTIFIED THE LANDING LIGHT ACTUATOR AS DEFECTIVE. REMOVED THE RT LANDING LIGHT ACTUATOR AND INSTALLED AN OVERHAULED UNIT. FUNCTIONAL CHECKED SATISFACTAug 30, 2013 · N314TL · Beech 400A · Exterior LightingSDR DJFA20130724001Brake Sys · malfunctionedCREW REPORTED AFTER TOUCHDOWN THE ACFT BRAKES CAME ON HARD BUT THEN RELEASED, WHILE PEDALS WERE STILL STIFF, THEY HAD NO BRAKING ACTION. AFTER THE ANTI-SKID SYS WAS TURNED OFF THE BREAKS FUNCTIONED. MX INSPECTED THE SYS, BUT COULD NOT DUPLICATE THE DISCREPANJul 24, 2013 · N426FL · Beech 400A · Landing Gear Brake SystemSDR DXTA2013070505432Coalescer Bag · odorPASSENGERS COMPLAINED OF MUSTY ODOR THAT AFFECTED THE EYES. REMOVED & REPLACED THE WATER COALESCER IAW MM 21-70-00. REMOVED AND CLEANED FWD AND AFT EVAPORATOR FILTER. INSTALLED FILTERS IAW MM 21-51-00. PERFORMED ENGINE RUN AND VAPOR CYCLE CHECK. NO FURTHER DJul 3, 2013 · N125QS · Beech 400A · Humidity Control SystemSDR 2013FA0000437Tube · brokenFOUND A CRACKED FITTING LEAKING BLEED AIR INTO THE ENGINE COMPARTMENT. BLEED AIR HAD MELTED A WIRE BUNDLE ABOVE IT AT THE CONNECTOR PLUG, CAUSING THE RT GENERATOR TO TRIP OFF LINE.Jun 19, 2013 · N75RL · Beech 400A · Pneumatic Distribution SystemSDR DJFA20130606001Unknown · odorBURNING ELECTRICAL ODOR IN THE AFT AREA OF THE BAGGAGE COMPARTMENT. MX INSPECTED THE AREA WITH ENGINES AND AIR CONDITONER RUNNING BUT COULD NOT DUPLICATE THE DISCREPANCY, NO REPEATS TO DATE.Jun 6, 2013 · N422FL · Beech 400A · Air Distribution SystemSDR LCPR20130606025Former · crackedRT THRUST REVERSER FAN DUCT UPPER FORMER RING IS CRACKED JUST ABOVE THE OTBD SPLICE TO LOWER RING. 9:00 POSITION.Jun 4, 2013 · N497AS · Beech 400A · Engine Thrust ReverserSDR 9JLA2013052203762Printed Ckt Board · defectiveCREW EXPERIENCED SEVERAL INTERMITTENT PROBLEMS WITH EXTERNAL POWER. FOUND DIODE ON CIRCUIT CARD P182 GOING TO PIN 36. PCB P182 WAS REPLACED WITH NEW AND FUNTIONAL CHECKS WERE SATISFACTORY.May 16, 2013 · N393GH · Beech 400A · External Power SystemSDR L7OA201305142002Unknown · unknownDURING TAKE OFF ROLL RT WING DIP DOWN. PILOT VERBALLY REPORTED LOUD THUMP/SUSPECTED TIRE FAILURE. INSPECTED RT LANDING GEAR STRUT, BRAKE AND MAIN WHEEL. FOUND NO DEFECTS, COULD NOT DUPLICATE PROBLEM DONE IAW AMM 32-00-00-201 & 12-00-00-201.May 11, 2013 · N999YB · Beech 400A · Standard Practices/StructuresSDR L7OA20130513001Lamp · burned outRIGHT MAIN GEAR INDICATOR LAMP OUT.May 10, 2013 · N999YB · Beech 400A · Landing Gear Position and WarningSDR 9JLA2013052303759Pcb · defectiveTHE FLIGHT CREW REPORTED THE THE "PLT WARN" CIRCUIT BREAKER POPPED DURING FLGHT. THE CIRCUIT BREAKER DID NOT RESET AFTER 1 ATTEMPT. TROUBLESHOOTING ISOLATED THE PROBLEM DOWN TO THE A172 PCB, PN 128-364086-1. THE PCB WAS REPLACED WITH A REPAIRED UNIT IAW THE Apr 29, 2013 · N393GH · Beech 400A · Electrical Power SystemSDR 9JLA2013052204235Adc · defectiveTHE FLIGHT CREW REPORTED THAT THE NR 1 PDF INDICATED THE LOSS OF IAS AND ALT ON THE CAPTAINS SIDE WHILE ENROUTE. TROUBLESHOOTING INDICATED THE NR 1 ADC DEFECTIVE. THE ADC WAS REPLACED WITH AN O/H UNIT IAW AMM 34-10-01.Apr 19, 2013 · N314TL · Beech 400A · Air Data ComputerSDR 9JLA201304262365Actuator · defectiveCREW REPORTED STAB PITCH TRIM FAILS IN FLIGHT. TROUBLESHOOTING INDENTIFIED THAT THE STAB TRIM ACTUATOR DEFECTIVE. REMOVED ACTUATOR. INSTALLED REPAIRED ACTUATOR. FUNCTIONAL CHECKED SATISFACTORY.Apr 7, 2013 · N202TT · Beech 400A · Stabilizer ActuatorSDR 9JLA2013040903756Transmitter · intermittentCREW REPORTED AN INTERMITTENT FLAP ASYMMETRY INDICATION ISSUE . DISCREPANCY WAS NOT DUPLICATED WHILE ACFT WAS IN MX FOR TROUBLESHOOTING AND THUS MADE IT VERY DIFFICULT TO CORRECT. CONFIRMED THAT THE LT INBD FLAP POSITION TRANSMITTER WAS DEFECTIVE. UNIT REPLAApr 1, 2013 · N393GH · Beech 400A · Trailing Flap Position Indicating SystemSDR DXTA2013032205330Pressure Switch · failedJUST PRIOR TO LEVELING OFF AT FL 270, RT FUEL TRANSFER PRESSURE LOW ANNUNCIATOR BEGAN CYCLING ON AND OFF ERRATICALLY. FUSELAGE TANK ALMOST EMPTY, AND TRANSFER PUMP SWITCHES WERE IN AUTO. WITHIN ONE MINUTE, THE LT SIDE DID, AS WELL. ACCOMPLISHED ABNORMAL CHEMar 22, 2013 · N131QS · Beech 400A · Aircraft Fuel Distribution SystemSDR L7OA20130314001Resistor · burnedAFTER TAKEOFF, NOTICED SMOKE IN CABIN. FOUND AFT EVAPORATOR BLOWER RESISTOR BURNED.Mar 14, 2013 · N999YB · Beech 400A · Air Distribution FanSDR DXTA2013030805310Brake Sys · malfunctionedRT BRAKES NOT BRAKING SYMETRICALLY. DURING TAXI BRAKES BEGAN TO BRAKE UNEVENLY. WHILE PRESSURING BOTH LT AND RT PADS, LT BRAKE BECAME MORE EFFECTIVE AS RT BRAKE BECAME HARDER WHICH PULLED AC TO THE LT REQUIRING RT RUDDER TO MAINTAIN CENTERLINE. THIS SEQUENCEMar 7, 2013 · N125QS · Beech 400A · Landing Gear Brake SystemSDR DJFA20130220001Brake Sys · malfunctionedCREW REPORTED DURING LANDING ROLL-OUT AND TAXI THE PILOTS SIDE LT TOE BRAKE DID NOT APPLY BRAKE PRESSURE ON INTITAL APPLICATION. AFTER PUMPING THE BRAKE IT WAS NOTED THAT THE BRAKE THEN FELT CORRECT. MX FOUND AIR IN THE SYS AND BLED THE SYS AND SERVICED BRAKFeb 20, 2013 · N463LX · Beech 400A · Landing Gear Brake SystemSDR DJFA20130219002Rib · crackedDURING INSPECTION FOR CRACKS ON THE RIB FLANGES OF THE HORIZONTAL STABILIZER ASSY, RIB FOUND CRACKED (ALONG WITH 8 OTHER RIBS; EACH RIB FAILURE IS DOCUMENTED ON SEPARATE SDR FORMS) ON THE LOWER FLANGE AT RT HORIZONTAL STAB CANTED STATION 29.92, BETWEEN THE FWDFeb 19, 2013 · N422FL · Beech 400A · Horizontal Stabilizer, Spar/RibSDR DJFA20130219001Rib · crackedDURING INSPECTION FOR CRACKS ON THE RIB FLANGES OF THE HORIZONTAL STABILIZER ASSY, RIB FOUND CRACKED (ALONG WITH 8 OTHER RIBS; EACH RIB FAILURE IS DOCUMENTED ON SEPARATE SDR FORMS) ON THE LOWER FLANGE AT LT HORIZONTAL STAB CANTED STATION 46.06, BETWEEN THE FWDFeb 19, 2013 · N422FL · Beech 400A · Horizontal Stabilizer, Spar/RibSDR DJFA20130219003Rib · crackedREMOVED LT HORIZONTAL STAB RIB L2M, INSTALLED HORIZONTAL STAB RIB L2M.Feb 19, 2013 · N422FL · Beech 400A · Horizontal Stabilizer, Spar/RibSDR DJFA20130219004Rib · crackedDURING INSPECTION FOR CRACKS ON THE RIB FLANGES OF THE HORIZONTAL STABILIZER ASSY, RIB FOUND CRACKED (ALONG WITH 8 OTHER RIBS; EACH RIB FAILURE IS DOCUMENTED ON SEPARATE SDR FORMS) ON THE LOWER FLANGE AT RT HORIZONTAL STAB CANTED STATION 46.06, BETWEEN THE FWDFeb 19, 2013 · N422FL · Beech 400A · Horizontal Stabilizer, Spar/RibSDR DJFA20130219005Rib · crackedDURING INSPECTION FOR CRACKS ON THE RIB FLANGES OF THE HORIZONTAL STABILIZER ASSY, RIB FOUND CRACKED (ALONG WITH 8 OTHER RIBS; EACH RIB FAILURE IS DOCUMENTED ON SEPARATE SDR FORMS) ON THE LOWER FLANGE AT LEFT HORIZONTAL STAB CANTED STATION 13.78, BETWEEN THE FFeb 19, 2013 · N422FL · Beech 400A · Horizontal Stabilizer, Spar/RibSDR DJFA20130219006Rib · crackedDURING INSPECTION FOR CRACKS ON THE RIB FLANGES OF THE HORIZONTAL STABILIZER ASSY, RIB FOUND CRACKED (ALONG WITH 8 OTHER RIBS; EACH RIB FAILURE IS DOCUMENTED ON SEPARATE SDR FORMS) ON THE LOWER FLANGE AT RT HORIZONTAL STAB CANTED STATION 62.20, BETWEEN THE FWDFeb 19, 2013 · N422FL · Beech 400A · Horizontal Stabilizer, Spar/RibSDR DJFA20130219007Rib · crackedDURING INSPECTION FOR CRACKS ON THE RIB FLANGES OF THE HORIZONTAL STABILIZER ASSY, RIB FOUND CRACKED (ALONG WITH 8 OTHER RIBS; EACH RIB FAILURE IS DOCUMENTED ON SEPARATE SDR FORMS) ON THE LOWER FLANGE AT RIGHT HORIZONTAL STAB CANTED STATION 29.92, BETWEEN THE Feb 19, 2013 · N422FL · Beech 400A · Horizontal Stabilizer, Spar/RibSDR DJFA20130219008Rib · crackedDURING INSPECTION FOR CRACKS ON THE RIB FLANGES OF THE HORIZONTAL STABILIZER ASSY, RIB FOUND CRACKED (ALONG WITH 8 OTHER RIBS; EACH RIB FAILURE IS DOCUMENTED ON SEPARATE SDR FORMS) ON THE LOWER FLANGE AT RT HORIZONTAL CANTED STATION 46.06, BETWEEN THE FWD AND Feb 19, 2013 · N422FL · Beech 400A · Horizontal Stabilizer, Spar/RibSDR DJFA20130219009Rib · crackedDURING INSPECTION FOR CRACKS ON THE RIB FLANGES OF THE HORIZONTAL STABILIZER ASSY, RIB WAS FOUND CRACKED (ALONG WITH 8 OTHER RIBS; EACH RIB FAILURE IS DOCUMENTED ON SEPARATE SDR FORMS) ON THE LOWER FLANGE AT LT HORIZTONAL CANTED STATION 29.92, BETWEEN THE FWDFeb 19, 2013 · N422FL · Beech 400A · Horizontal Stabilizer, Spar/RibSDR E07A201302200001Lamp · inoperativeCREW NOTICED RT MAIN GEAR DOWN GREEN LIGHT DID NOT ILLUMINATE, UP GEAR WAS SELECTED DOWN. ACFT RETURNED TO ICT AND LANDED WITHOUT INCIDENT. AFTER GEAR WAS INSPECTED AND INDICATOR BULB WAS REPLACED ACFT WAS RETURNED TO SERVICE.Feb 19, 2013 · N498AS · Beech 400A · Landing Gear Position and WarningSDR DXTA2013021105280Solenoid · failedAFTER APPROX 15 MINUTES INTO FLIGHT, ALTITUDE FL180, THE LT ENG EFC CIRCUIT BREAKER TRIPPED, THE LT EFC ANNUNCIATOR ILLUMINATED WITH ASSOCIATIATED LOSS OF THRUST ON LT ENGINE AND A STRONG ODOR OF BURNED ELECTRICAL NOTED. THE ODOR CLEARED QUICKLY. REPLACED Feb 10, 2013 · N154QS · Beech 400A · Engine (Turbine/Turboprop)SDR DXTR20130207002Attach Angle · crackedLT LOWER OTBD THRUST REVERSER CRACKED FROM RIVET. R & R THE LT LOWER OTBD THRUST REVERSER CRACKED ANGLE IAW THE A SRM 51-40-01 AND 51-41-00.Feb 5, 2013 · N115QS · Beech 400A · Engine Thrust ReverserSDR DJFA2013F00035Flex Hose · chafedDURING TAKE OFF, LT AND RT HYDRAULIC LEVEL LOW LIGHTS CAME ON CLIMBING THROUGH 5000 FT AND WITHIN TWO MINUTES LT AND RT HYD PRESSURE LOW LIGHTS CAME ON. HYD PRESS WENT TO 0 WITHIN 15 SEC RAN CHECKLISTS DECLARED AN EMERGENCY AND LANDING UNEVENTFULLY. LT ENGINJan 28, 2013 · N451FL · Beech 400A · Hydraulic System, MainSDR L7OA20130122001Light · false activationRED LIGHT IN GEAR HANDLE WILL NOT EXTINGUISH ON GEAR RETRACTION. INSPECTED GEAR AND GEAR DOORS, NO DEFECTS NOTED AT THIS TIME. CHECKED NOSE GEAR STRUT FOR PROPER SERVICE. PERFORMED LANDING GEAR EXTENSION AND RETRACTION CHECK SATISFACTORY. IAW MM 32-00-00 ANDJan 21, 2013 · N999YJ · Beech 400A · Landing Gear Position and WarningSDR DXTR20130118002Skin · crackedFOUND CRACKS AROUND THREE OUTER SKIN FASTENERS OF THE RT UPPER THRUST REVERSER. ACCOMPLISHED SKIN REPAIR OF RT UPPER THRUST REVERSER IAW CMM 78-30-07, REPAIR NR 18.Jan 14, 2013 · N122QS · Beech 400A · Engine Thrust ReverserSDR L7OA20130109001Pressure Valve · defectivePILOT STATED NOTICED CABIN AT 10,000 FT AND CLIMBING. DONNED MASKS AND STARTED AN EMERGENCY DESCENT. CABIN CONTINUED TO CLIMB AT ABOUT 2,200 FPM AND RECEIVED A CABIN ALTITUDE ANNUNCIATOR AND THEN THE PAX MASKS DROPPED AUTOMATICALLY AROUND 14,000 CABIN ALTITUDJan 9, 2013 · N999YB · Beech 400A · Cabin Pressure Control SystemSDR DXTR20130118001Seat Track · crackedSEAT 7, AFT INBD MOUNTING CLEAT CRACKED. R & R NR 7 SEAT MOUNTING RAIL, REF COMPONENT, MM 25-20-90.Jan 7, 2013 · N122QS · Beech 400A · Fuselage, Seat/Cargo Attach FittingsSDR CA130117003Engine · shutdown(CAN) DURING TAXI AFTER NORMAL ENGINE START THE NR 1 ENGINE SHUTDOWN ON ITS OWN. BEFORE SECOND ENGINE START ATTEMPT, EXECUTED A SHUTDOWN AND START CHECKLIST, BUT THE NR 1 ENGINE N2 NEVER WENT ABOVE 41 PERCENT.Jan 2, 2013 · Beech 400A · Engine (Turbine/Turboprop)SDR DXTA2013020505270Fuel Control · malfunctionedDURING TAXI, AFTER NORMAL ENGINE START, NR 1 ENGINE SHUTDOWN ON ITS OWN. BEFORE SECOND ENGINE START ATTEMPT, EXECUTED SHUTDOWN AND START CHECKLIST, BUT THE NR 1 ENGINE N2 NEVER WENT ABOVE 41 PERCENT. REMOVED DEFECTIVE LT FUEL CONTROL. INSTALLED REPAIRED LTJan 2, 2013 · N102QS · Beech 400A · Fuel Control/Turbine EnginesSDR ZKFR2013011001Tire · failedTHE LT MAIN TIRE BLEW OUT ON TAKEOFF ROLL. THE RT WHEEL & TIRE ASSY WAS REPLACED. MX CHECKS OF THE ANTI-SKID SYS WERE PERFORMED WITH NO DEFECTS NOTED.Dec 28, 2012 · N48MF · Beech 400A · TireSDR DXTA2012123105219Line · disconnectedAPPROX TWO HOURS AFTER FUELING AND 1.5 HOURS OF CLOSED CABIN, FUEL ODOR WAS NOTICED ENTERING CABIN. INSPECTING LUGGAGE COMPARTMENT REVEALED EVEN STRONGER ODOR, ESPECIALLY COMING OUT OF INSPECTION PANELS. GAINED ACCESS TO AFT FUSELAGE FUEL TANK. INSPECTED AFTDec 28, 2012 · N131QS · Beech 400A · Fuel StorageSDR DXTA2012122605215Line · misinstalledON TAXI OUT, WENT TO MAKE A LEFT TURN AND PUSHED ON THE LEFT BRAKE TO HELP AND THE PLANE TURNED RIGHT. THEN PUSHED ON THE RIGHT BRAKE AND THE PLANE TURNED LEFT. THEN TRANSFERED CONTROL TO MY PARTNER IN THE RIGHT SEAT AND HE HAD THE SAME PROBLEM. FOUND LT ADec 25, 2012 · N132QS · Beech 400A · Brake Anti-Skid SectionSDR DXTA2012122605214Unknown · odorAPPROX 2 HOURS AFTER FUELING AND 1.5 HRS OF CLOSED CABIN, FUEL SMELL WAS NOTICED ENTERING CABIN. INSPECTING LUGGAGE COMPARTMENT REVEALED EVEN STRONGER SMELL, ESPECIALLY COMING OUT OF INSPECTION PANELS. INSPECTED AFT BAGGAGE AREA FOR FUEL LEAKS. NO DEFECTS NODec 25, 2012 · N131QS · Beech 400A · Air Distribution SystemSDR DJFA20121222001Switch · dirtyCREW REPORTED, DURING MISSED APPROACH, WHEN GEAR WAS SELECTED TO RETRACT, GEAR REMAINED DOWN. DUE TO EXTRA DRAG FROM GEAR AND CURRENT FUEL LOAD CREW DECLARED AN EMERGENCY AND LANDED SAFELY AT DESTINATION. MX CLEANED LANDING POSITION SWITCH AND PERFORMED LANDDec 22, 2012 · N406LX · Beech 400A · Landing Gear Position and WarningSDR DJFA20121221001Adapter · failedCREW AND PASSENGERS REPORTED AN ELECTRICAL ODOR WHILE ENROUTE AT ALTITUDE AND DURING DESCENT/LANDING. MX FOUND BOTH IPAD ADAPTERS HAD FAILED AND REPLACED THEM.Dec 21, 2012 · N480LX · Beech 400A · Flight Compartment EquipmentSDR L7OA201212140001Flap System · malfunctionedFLAP ASYMMETRY LIGHT ILLUMINATED AFTER FLAP RETRACTION. RESET CIRCUIT BREAKERS FOR FLAP ASYMMETRY, OPS CHECKED GOOD ON GROUND SEVERAL TIMES IAW 27-50-00-201.Dec 14, 2012 · N870BB · Beech 400A · Trailing Edge Flap Control System
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