# Filper 400A - Type: Aircraft model (FAA registry) - Registry code: 3461404 - Manufacturer (registry): FILPER - Model: 400A - Aircraft type: Rotorcraft - Category: Rotorcraft - Engines: 1 ยท Reciprocating - Seats: 2 - Weight class: Up to 12,499 lb - Cruise speed: 67 mph - Certification: Type certificated - Registered aircraft: 0 - Page: https://openairdocs.org/model/filper-400a Model codes come from the FAA registry's reference file. ADs are matched to them by model name and maker. ## ADs that may apply (OpenAirDocs) Matched to this model by model name and maker. Each AD's applicability may narrow it by serial number, part number or equipment. None matched. ## Registered aircraft None registered with this model now. ## STCs approved for it (134, first 50) - [STC SA00749AT](https://openairdocs.org/stc/SA00749AT): Modification of flush type fuel caps for installation of a locking cylinder and keeper. (1964 and subsequent). Aero Trim, Inc - [STC SA01452CH](https://openairdocs.org/stc/SA01452CH): Installation of an air ambulance conversion kit.. Med-Pac Inc. - [STC SA01639NY](https://openairdocs.org/stc/SA01639NY): Replacement of 12 refrigerant in air conditioning system with Enviro Refrigerant Hotshot R414B.. Scale Modelbuilders Inc. - [STC SA02160CH](https://openairdocs.org/stc/SA02160CH): Installation of Medical Storage Cabinet.. Med-Pac Inc. - [STC SA09743SC](https://openairdocs.org/stc/SA09743SC): Installation of electric window shades.. Lou Martin & Associates - [STC SA2494SO](https://openairdocs.org/stc/SA2494SO): Replacement of Nickel-Cadmium Battery with Concorde Model RG-380E/40A or 40B Sealed Lead Acid Battery.. Raytheon Aircraft Services Inc - [STC SA2501SO](https://openairdocs.org/stc/SA2501SO): Installation of Whelen Flashing Anticollision Light P/N 90033.. Textron Aviation Inc - [STC SA2717CE](https://openairdocs.org/stc/SA2717CE): Installation of Fairchild A100A cockpit voice recorder.. Textron Aviation Inc - [STC SA2718CE](https://openairdocs.org/stc/SA2718CE): Alternate location for Collins HF-9000 receiver/transmitter.. Textron Aviation Inc - [STC SA2719CE](https://openairdocs.org/stc/SA2719CE): Installation of Fairchild F1000digital flight data recorder.. Textron Aviation Inc - [STC SA2746NM](https://openairdocs.org/stc/SA2746NM): Installation of tailcone baggage compartment modification, including access door modification.. Textron Aviation Inc - [STC SA2886SO](https://openairdocs.org/stc/SA2886SO): Installation of a supplemental freon air conditioning system.. Raytheon Aircraft Services Inc - [STC SA2887SO](https://openairdocs.org/stc/SA2887SO): Installation of access panels for environmental control system.. Textron Aviation Inc - [STC SA2954SO](https://openairdocs.org/stc/SA2954SO): Installation of an auxiliary ground heater.. Hangar One, Inc - [STC SA3070SO](https://openairdocs.org/stc/SA3070SO): Enlargement of baggage compartment.. Raytheon Aircraft Services Inc - [STC SA3135SO](https://openairdocs.org/stc/SA3135SO): Installation of a Fairchild GA 100cockpit voice recorder.. Raytheon Aircraft Services Inc - [STC SA3322SO](https://openairdocs.org/stc/SA3322SO): Installation of a Sundstrand MK VI GPWS.. Raytheon Aircraft Services Inc - [STC SA3895NM](https://openairdocs.org/stc/SA3895NM): Installation of medical stretcher left or right side.. Aviation Fabricators Inc - [STC SA4548SW](https://openairdocs.org/stc/SA4548SW): Installation of CAC-3001-D side facing toilet seat frame.. Aviation Fabricators Inc - [STC ST00141AT](https://openairdocs.org/stc/ST00141AT): Installation of a Collins TCAS II System.. Raytheon Aircraft Services Inc - [STC ST00227WI-D](https://openairdocs.org/stc/ST00227WI-D): Modification of a single Collins AMS-850 Avionics Management System to dual Collins AMS-850 AMS System, modification of a CMA-764-1 Global Positioning Sensor to a CMA-764-2 GPS or to a single or dual Collins GPS-4000 GPS and modified PFD-MFD-PFD (3 tube) or PFD-ND-MFD-PFD (4 tube) or PFD-MFD-MFD-PFD (4 tube) EFIS Display.. Rockwell Collins Inc - [STC ST00235WI](https://openairdocs.org/stc/ST00235WI): Modification of a single Collins AMS-850 Avionics Management System. Hawker Beechcraft Corporation - [STC ST00235WI-D](https://openairdocs.org/stc/ST00235WI-D): Modification of a single Collins AMS-850 Avionics Management System. Textron Aviation Inc - [STC ST00244AT](https://openairdocs.org/stc/ST00244AT): Installation of a Collins alpha enhancement package.. Raytheon Aircraft Services Inc - [STC ST00245AT](https://openairdocs.org/stc/ST00245AT): Installation of a Collins global positioning system.. Raytheon Aircraft Services Inc - [STC ST00276BO](https://openairdocs.org/stc/ST00276BO): Installation of Pratt & Whitney Engine Services Data Transmission Unit (DTU). Pratt & Whitney Engine Services Inc. - [STC ST00276WI](https://openairdocs.org/stc/ST00276WI): Installation of Kedeg Company 21BC11e Coaleser Assemly.. Purolator Facet, Inc - [STC ST00277BO](https://openairdocs.org/stc/ST00277BO): Installation of Pratt & Whitney Engine Services Hybrid Aircraft Data Acquisition System (ADASh). Pratt & Whitney Engine Services Inc. - [STC ST00322SE](https://openairdocs.org/stc/ST00322SE): Installation of emergency medical stretcher, oxygen, and electrical systems.. LifePort LLC - [STC ST00344AT](https://openairdocs.org/stc/ST00344AT): Installation of emergency lighting system improvement modification.. Textron Aviation Inc - [STC ST00425AT](https://openairdocs.org/stc/ST00425AT): Installation of a Pulse Lighting System.. Textron Aviation Inc - [STC ST00485WI-D](https://openairdocs.org/stc/ST00485WI-D): Modification of a single Collins AMS-850 Avionics Management System to a dual Collins AMS-5000 AMS system, modification of an APS-850 autopilot system to an APS-4000 APS, installation of a single or dual Collins GPS-4000 GPS, and modified PFD-MDF-PFD (3 tube) or PFD-MFD-MFD-PFD (4 tube) EFIS display. For model 400, serial number RJ-061 ONLY.. Rockwell Collins Inc - [STC ST00533WI](https://openairdocs.org/stc/ST00533WI): Installation of Safe Flight Instrument Corporation N1 Computer System, P/N 6810-1 MOD A.. Textron Aviation Inc - [STC ST00600AT](https://openairdocs.org/stc/ST00600AT): Installation of alternate cabin lighting.. Textron Aviation Inc - [STC ST00667AT](https://openairdocs.org/stc/ST00667AT): Installation of Collins Avionics bravo enhancement package.. Textron Aviation Inc - [STC ST00693WI-D](https://openairdocs.org/stc/ST00693WI-D): Modification of dual Collins AMS-5000 avionics management system, dual Collins APS-4000 autopilot system, and PFD-MFD-PFD (3-tube) or PFD-MFD-MFD-PFD (4-tube) EFIS display installations.. Textron Aviation Inc - [STC ST00723WI-D](https://openairdocs.org/stc/ST00723WI-D): Installation and Modification of dual Collins AMS-5000 Avionics Management System, dual Collins APS-4000 Autopilot System and Collins PFD-MFD-PFD (3 tube) or Collins PFD-MFD-MFD-PFD (4 tube) EFIS Display Pro Line 4 Avionics System.. Textron Aviation Inc - [STC ST00737AT](https://openairdocs.org/stc/ST00737AT): Installation of Autopower System.. Textron Aviation Inc - [STC ST00793AT](https://openairdocs.org/stc/ST00793AT): Installation of External Power Overvoltage. Protection System. Textron Aviation Inc - [STC ST00795WI-D](https://openairdocs.org/stc/ST00795WI-D): Modification of Canadian Marconi CMA-764 GV (CMA-764-1), Canadian Marconi part number 100-601200-101 (Collins part number 270-1306-070), VLF/OMEGA/GPS Sensor System (Single/Dual) Installation to a Collins CMA-764 GV (CMA-764-1 ), Collins part number 270-1306-071, Canadian Marconi part number 100-601200-500, GPS Sensor System (Single/Dual) Installation. Rockwell Collins Inc - [STC ST00812SE](https://openairdocs.org/stc/ST00812SE): Group airplane approval for Reduced Vertical Separation Minimum (RVSM).. Textron Aviation Inc - [STC ST00835DE](https://openairdocs.org/stc/ST00835DE): Installation of Automatic Dependent Surveillance - Broadcast (ADS-B) Out and In functionality using the Garmin GTX 335R and GTX 345R Transponders plus qualified position sensor. Peregrine - [STC ST00844WI-D](https://openairdocs.org/stc/ST00844WI-D): Modification of Collins TCAS II or TCAS-94 (TCAS II) system installation with Collins TTR-920 Change 7.0 Receiver Transmitter to a Collins TCAS II or TCAS-94 OTCAS II) system installation with Collins TTR-921 or Collins TTR-4000 Change 7.0 TCAS Receiver Transmitter.. Rockwell Collins Inc - [STC ST00874CH](https://openairdocs.org/stc/ST00874CH): Replacement of symbol generators.. ElectroSonics Div of AiRadio Corporation - [STC ST00881WI-D](https://openairdocs.org/stc/ST00881WI-D): Modification of a TCAS II system installation to Change 7.0 or Change 7.1. Rockwell Collins Inc - [STC ST00892LA](https://openairdocs.org/stc/ST00892LA): Installation of Emergency Vision Assurance System (EVAS).. VisionSafe LLC - [STC ST00938WI-D](https://openairdocs.org/stc/ST00938WI-D): Modification of Collins GPS-4000 Global Positioning Sensor installation to a Collins GPS-4000A Global Positioning Sensor installation in a part 25 aircraft per Collins Installation INstructions as listed in AML No. ST00938WI-D, latest revision.. Rockwell Collins Inc - [STC ST00966AT](https://openairdocs.org/stc/ST00966AT): Installation of pilot and co- pilot seat crotch belt.. Textron Aviation Inc - [STC ST00983CH](https://openairdocs.org/stc/ST00983CH): Installation of AlliedSignal Enhanced Ground Proximity Warning System.. Elliott Aviation Technical Products - [STC ST01070DE](https://openairdocs.org/stc/ST01070DE): Installation of the Curtiss-Wright Fortress Flight Data Recorder (with Cockpit Voice Recorder). Peregrine All 134: https://openairdocs.org/model/filper-400a/stcs.md ## NTSB investigations None matched to aircraft with this model. ## FAA accident and incident reports None matched to aircraft with this model. ## Service difficulty reports (1,397, newest 50) As reported by operators and repair stations, by the model named in the report. - [SDR 2026FA0000630](https://openairdocs.org/sdr/2026FA0000630), Aug 7, 2026: TIRE. BLOWN. ACFT BLEW THE LEFT MAIN TIRE WHILE TAXIING TO THE HANGAR AFTER LANDING. AIRCRAFT LANDED WITH NO ISSUES. AIRCRAFT WAS ABLE TO TAXI OFF THE RUNWAY AND STARTED TO - [SDR OEJA202606080001](https://openairdocs.org/sdr/OEJA202606080001), Jun 4, 2026: CONTROL VALVE. STICKING. ON TAKE OFF THE AIRCRAFT WAS CLIMING AND THE CREW HEARD A POPPPING NOISE AND THE CABIN BEGAN TO DROP, SO THE TURNED AROUND WENT BACK TO THE AIRPORT. THEY NOTIFE - [SDR 2026F00028](https://openairdocs.org/sdr/2026F00028), Mar 14, 2026: LINE. RUPTURED. BLEED AIR DUCT FAIL ANNUCIATOR ILLUMINATED DURING CLIMB. CREW RETURNED TO THE AIRPORT. MX UNABLE TO FIND LEAK ON THE GROUND DURING RUNS. ANOTHER FLIGHT TO CONFI - [SDR CVGA20260218003](https://openairdocs.org/sdr/CVGA20260218003), Feb 16, 2026: BULB. INOPERATIVE. DURING APPROACH, AFTER EXTENDING THE LANDING GEAR, THE RIGHT LANDING GEAR SAFE LIGHT DID NOT ILLUMINATE. EMERGENCY DECLARED. UPON INSPECTION OF RT LG SAFE LIGHT - [SDR CVGA20260216002](https://openairdocs.org/sdr/CVGA20260216002), Feb 13, 2026: STRUT. OVERSERVICED. ON LANDING, REVERSERS WOULD NOT DEPLOY. BELOW 60 K LOST BRAKES. USED EMERGENCY BRAKES TO STOP ACFT. AFTER TAXIING OFF RUNWAY, PLACED BRAKES IN ANTI SKID OFF POS - [SDR 2025F00291](https://openairdocs.org/sdr/2025F00291), Dec 24, 2025: BUTTON. WORN. DISCOVERED DURING PREFLIGHT, THE MAIN CABIN DOOR HANDLE WILL NOT STOW IN THE CLOSED POSITION. REMOVED HANDLE AND INTERIOR DOOR PANEL. FOUND THE HANDLE AND THE P - [SDR 3N0A2025121800284](https://openairdocs.org/sdr/3N0A2025121800284), Dec 13, 2025: WINDSHIELD. DELAMINATED. THE RIGHT WINDSHIELD SHOWED SIGNS OF DELAMINATION SHORTLY AFTER DEPARTING PWN. AFTER LANDING AT BNA A PICTURE WAS SENT TO DIR. OF MAINTENANCE AND TRIP SUPPORT, - [SDR CVGA20251114002](https://openairdocs.org/sdr/CVGA20251114002), Nov 10, 2025: SWITCH. FAULTY. FLAP ASYM LIGHT CAME ON AFTER SELECTING FLAPS 20 POSITION. FAULT COULD NOT BE DUPLICATED UPON ARRIVAL TO AIRCRAFT. MCC ELECTED TO REPLACE THE FLAP FOLLOW UP SWI - [SDR W39A202505140355](https://openairdocs.org/sdr/W39A202505140355), Apr 10, 2025: WINDSHIELD. CRACKED. RH WINDSHIELD CRACKED DESCENDING THROUGH FL 220 , CREW DETERMINED THAT IT WAS THE OUTER ACRILIC PLY, CREW COMPLIED WITH THE ABNORMAL PROCEDURE , PRESSURIZATION - [SDR CVGA20250407002](https://openairdocs.org/sdr/CVGA20250407002), Apr 3, 2025: BRAKE ASSY. MALFUNCTIONED. DURING TAXI OUT BRAKES WERE MOMENTARILY LOST ON BOTH SIDES LH & RH BRAKE PEDALS. (ONCE ON THE LEFT SIDE AND ONCE ON THE RIGHT SIDE BRAKE PEDALS) - [SDR CVGA20250303001](https://openairdocs.org/sdr/CVGA20250303001), Feb 25, 2025: DIODE. FAILED. SMOKE CAME FROM DASH AREA WHEN ENG SYNC LIGHT IS ON - REMOVED AND REPLACED CR119 DIODE WITH NEW DIODE, P/N 1N4007, ON ENGINE FUEL SYNCH ANNUN CIRCUIT IAW BE400 - [SDR CVGA20250219005](https://openairdocs.org/sdr/CVGA20250219005), Feb 15, 2025: CABIN PRESSURE. INOPERATIVE. ON TAKEOFF AND CLIMB OUT AIRPLANE NOT PRESSURIZING. CYCLED PRESS SOURCE KNOBS WITH NO CHANGE- EMERGENCY DECLARED. - [SDR CVGA20250218004](https://openairdocs.org/sdr/CVGA20250218004), Feb 13, 2025: CONTROLLER. FAILED. PITCH TRIM MOTOR FAILURE - EMERGENCY DECLARED - REMOVED RH PITCH TRIM CONTROLLER P/N 76621-4 S/N 2392. INSTALLED SERVICEABLE PITCH TRIM CONTROLLER P/N 76621-4 S - [SDR CVGA20250129006](https://openairdocs.org/sdr/CVGA20250129006), Jan 27, 2025: BRAKE. FAILED. LEFT BREAK FAILED DURING TAXING. PERFORMED FUNCTIONAL TESTING MANUAL BRAKE SYSTEM AND POWER BRAKE SYSTEM IAW 400A AMM 32-40-00. PERFORMED POWER BRAKE BLEEDING I - [SDR CVGA20250110004](https://openairdocs.org/sdr/CVGA20250110004), Jan 8, 2025: BRAKE SYS. FAILED. BRAKE FAILURE WHILE TAXI TO TAKEOFF. COMPLETED FULL ANTISKID BRAKE TEST PRIOR TO FAIL. SIC CHECKED HIS BRAKES SUCCESSFULLY AND RETURNED CONTROLS, FELT LIKE BRAK - [SDR CVGA20241205002](https://openairdocs.org/sdr/CVGA20241205002), Nov 27, 2024: CONNECTOR. FAULTED. DURING HIGH SPEED TAXI CHECK AT 75 KTS BOTH BRAKES LOCKED AND BOTH TIRES DEFLATED. - REPLACED BOTH RH & LH MAIN BRAKE ASSEMBLIES WITH OVERHAULED IAW 400A MM 32- - [SDR CVGA20241016003](https://openairdocs.org/sdr/CVGA20241016003), Oct 13, 2024: LANDING GEAR. FAULTED. WHEN SELECTING LANDING GEAR DOWN, NONE OF THE THREE GREEN LANDING GEAR SAFE LIGHTS ILLUMINATED. THE RED GEAR-HANDLE IN-TRANSIT LIGHT ILLUMINATED NORMALLY. EMERG - [SDR V7PA202402270001](https://openairdocs.org/sdr/V7PA202402270001), Sep 12, 2024: PRESSURE VALVE. FAILED. CREW REPORTED A LH ENGINE FIRE WARNING IN FLIGHT WHILE CLIMBING THRU 12,000 FEET.. PULLED THROTTLE TO IDLE AND WARNING STOPPED. CREW DECLARED EMERGENCY AND RETU - [SDR 2024FA0000705](https://openairdocs.org/sdr/2024FA0000705), Sep 6, 2024: DUCT. OUT OF POSITION. BLLED AIR DUCT FAIL CAUTION LIGHT ILLUMINATED ON CLIMB OUT PASSING FL250. - [SDR W39A2024092310001](https://openairdocs.org/sdr/W39A2024092310001), Sep 2, 2024: WINDSHIELD. CRACKED. RH WINDSHIELD CRACKED DESCENDING THROUGH FL 210, 62NM OUT OF KILM, CREW COMPLIED WITH THE ABNORMAL PROCEDURE, PRESSURIZATION WAS NORMAL, AND THEN CONTINUED WITH - [SDR CVGA20240904004](https://openairdocs.org/sdr/CVGA20240904004), Aug 31, 2024: PRESSURE SWITCH. FAULTY. CABIN PRESSURE LO ANNUNCIATOR ILLUMINATED IN FLIGHT AT FL320 CABIN ALTITUDE WAS OVER 9000FT AND CLIMBING. BY FL350 WARNING LIGHT CAME ON PERFORMED EMER DESCENT - [SDR CVGA20240812002](https://openairdocs.org/sdr/CVGA20240812002), Aug 9, 2024: THRUST REVERSER. MALFUNCTIONED. LEFT AND RIGHT TR ARM LIGHTS CAME ON RIGHT AFTER T/O AND REMAINED ON AFTER STOWED. LANDING GEAR WOULD NOT GO UP LOCK WAS DOWN. AFTER MANUALLY RELEASING LOCK GEA - [SDR CVGA20240729003](https://openairdocs.org/sdr/CVGA20240729003), Jul 26, 2024: UNKNOWN. UNKNOWN. LOST HEADING INFORMATION ON SDU, CDU, MFD - AIRPLANE DIDN'T KNOW WHERE IT WAS IN RELATION TO AIRPORT OR GUIDANCE. TROUBLESHOT AS REQUIRED WITH FSR. PERFORMED AH - [SDR CVGA20240725002](https://openairdocs.org/sdr/CVGA20240725002), Jul 21, 2024: BRAKE SYS. FAILED. AFTER LANDING ON TAXIWAY MAIN BRAKES FAILED. HAD TO USE EMERGENCY BRAKE TO STOP. - [SDR OEJA2024070300486](https://openairdocs.org/sdr/OEJA2024070300486), Jul 3, 2024: SOLENOID VALVE. FAILED. CLIMBING OUT OF TEB IN THE MID 30S THE AIRCRAFT WAS UNABLE TO MAINTAIN ADDITIONAL CABIN PRESSURE. THE CREW LEVELED OFF AND ASSESSED THE SITUATION, AND AFTER SOM - [SDR CVGA20240628002](https://openairdocs.org/sdr/CVGA20240628002), Jun 25, 2024: BRAKE ASSY. FAILED. LOST BRAKES ON TAXI. COMPLETE BRAKE VALVE ON BOTH SIDES. DEPLOYED NITROGEN EMERGENCY BRAKES. - [SDR CVGA20240530002](https://openairdocs.org/sdr/CVGA20240530002), May 26, 2024: PUMP. LOW PRESSURE. ON FINAL APPROACH INTO IAD, THE LH PUMP PRESS LO AND THE HYD LEVEL LO LIGHTS ILLUMINATED THE HYD PRESS GAUGE INDICATED NORMAL SYSTEM PRESS. AFTER LANDING BRAKIN - [SDR CVGA20240530001](https://openairdocs.org/sdr/CVGA20240530001), May 26, 2024: FIRE LOOP. CHAFED. LH ENG FIRE PUSH SWITCHLIGHT ILLUMINATED AND FIRE BELL SOUNDED AT 400' AGL TAKE OFF THRUST SET, BROUGHT LEFT ENGINE THRUST LEVER BACK TO IDLE, LIGHT EXTINGUISHE - [SDR OEJA2024032600001](https://openairdocs.org/sdr/OEJA2024032600001), Mar 23, 2024: WARNING LIGHT. ILLUMINATED. AT CRUISE AND 41,000 AGL A NO RIGHT ENGINE NO DISPACT LIGHT CAME ON AND WOULD NOT EXTINGUISH , RAN THE QRH CHECK LIST AND IT ADVISED US TO LAND AS SOON AS PRACT - [SDR CVGA20240322001](https://openairdocs.org/sdr/CVGA20240322001), Mar 15, 2024: FRAME. CRACKED. MULTIPLE CRACKS WERE FOUND AROUND FASTENER HOLES AT FS330 WHILE PERFORMING BLEED AIR TUBING INSPECTION. PERFORMED REPAIR TO LH FUSELAGE FRAME #330 IAW DOCUMENT - [SDR CVGA20240319001](https://openairdocs.org/sdr/CVGA20240319001), Mar 14, 2024: SWITCH. DEFECTIVE. ON TAKEOFF HAD AN UN-COMMANDED ROLL TRIM TO THE LEFT AT FULL DEFLECTION. INITIALLY WE WERE UNABLE TO CORRECT THE TRIM TO NORMAL. EVENTUALLY WE WERE ABLE TO NEUT - [SDR 3CMA2024022300001](https://openairdocs.org/sdr/3CMA2024022300001), Feb 22, 2024: WINDSHIELD. FAILED. WHILE COMING FROM SDF LOUISVILLE KENTUCKY AT AN ALTITUDE OF 29000 FT ON DESCENT THE COPILOT'S WINDSHIELD SHATTERED. PILOT TOOK OVER AND ABOUT 2 MINUTES LATER TH - [SDR CVGA20240124001](https://openairdocs.org/sdr/CVGA20240124001), Jan 17, 2024: SWITCH. INTERMITTENT. LH MAIN GEAR DOWN GREEN LIGHT WOULD NOT ILLUMINATE WHEN GEAR DOWN SELECTED. LIGHT WOULD TEST. PERFORMED GEAR EMERGENCY EXTENSION PROCEDURE. LH GEAR DOWN LIGHT S - [SDR 2024FA0000040](https://openairdocs.org/sdr/2024FA0000040), Jan 16, 2024: DUCT. CRACKED. PILOT REPORTED GETTING THE "BL AIR DCT FAIL" LIGHT IN FLIGHT, DURING CRUISE OPERATION. DURING TROUBLESHOOTING, IT WAS NOTED THAT THE BLEED AIR TUBE THAT CONNECT - [SDR CVGA20240118001](https://openairdocs.org/sdr/CVGA20240118001), Jan 15, 2024: UNKNOWN. UNKNOWN. "HSTAB ICE FAIL " ANNUNCIATION ILLUMINATED IMMEDIATELY AFTER SYSTEM ACTIVATION IN THE AIR. SYSTEM PASSED GROUND CHECK PRIOR TO TAKE OFF. EMERGENCY DECLARED. - [SDR CVGA20231216001](https://openairdocs.org/sdr/CVGA20231216001), Dec 12, 2023: UNKNOWN. UNKNOWN. DURING CLIMB L AND R TR ARM LIGHTS BECAME ILLUMINATED WITHOUT THE MASTER CAUTION WARNING LIGHT. AN EMERGENCY WAS DECLARED. THE LEFT AND RIGHT THRUST REVERSERS W - [SDR CVGA20231211001](https://openairdocs.org/sdr/CVGA20231211001), Dec 5, 2023: OXYGEN BOTTLE. EMPTY. O2 NEEDS SERVICE FOR POSSIBLE LEAK. READS 0 ON GAUGE. REMOVED AND REPLACED O2 BOTTLE REF B400 AMM CH 35-11-00. OPS AND LEAK CHECK PASSED AT THIS TIME. NO DEFECT - [SDR OEJA202312050001](https://openairdocs.org/sdr/OEJA202312050001), Dec 3, 2023: UNKNOWN. UNKNOWN. ON 12/3/2023 AT APX 2230 N420FL ENCOUNTERED A FLAP ASYM LIGHT ON APPROACH INTO MSP, THE FLAPS WERE LOCKED OUT AND DID NOT EXTEND. AFTER CYCLING THE FLAPS AND MA - [SDR CVGA20231127001](https://openairdocs.org/sdr/CVGA20231127001), Nov 21, 2023: LIGHT. FAILED. NOSE AND RIGHT LANDING GEAR LIGHTS INDICATOR INOP. REPLACED NOSE AND RIGHT LANDING GEAR INDICATOR LAMPS. OPS CHECK GOOD. AN EMERGENCY WAS DECLARED. - [SDR CVGA20231027001](https://openairdocs.org/sdr/CVGA20231027001), Oct 23, 2023: DOOR SEAL. FAILED. CABIN PRESS LO ANNUNCIATOR ILLUMINATED IN FLIGHT APPROXIMATELY FL280. FOUND MAIN ENTRANCE DOOR WEATHER SEAL TO BE CUT AND FOLDED OVER. REMOVED SEAL AND INSTALLE - [SDR CVGA20231016001](https://openairdocs.org/sdr/CVGA20231016001), Oct 12, 2023: SWITCH. FAULTY. IMMEDIATELY AFTER TAKEOFF, AUTOPILOT OFF, ROLL TRIM RAN TOWARDS RIGHT WING DOWN. IT STOPPED WITH LEFT INDICATOR APPROXIMATELY 2 INDICATOR MARKS UP AND RIGHT IND - [SDR OEJA202310110001](https://openairdocs.org/sdr/OEJA202310110001), Oct 7, 2023: DOOR SEAL. UNKNOWN. DURING CLIMB OUT ENROUTE TO MONTEREY CA FROM PORTLAND OR THE CREW NOTICED THE CABIN A WAS NOT CLIMBING , SO THE CREW DECIDED TO RETURN TO PORTLAND FOR A SAFE LA - [SDR CVGA20231002001](https://openairdocs.org/sdr/CVGA20231002001), Sep 27, 2023: ANTI-SKID SYS. FAILED. AFTER LANDING JUST BEFORE EXITING THE RUNWAY PIC BRAKE BRAKE PEDALS WENT ALL THE WAY TO THE FLOOR WITH NO BRAKE. EMER BRAKE WAS USED TO BRING A/C TO A STOP. PIC - [SDR CVGA20230927001](https://openairdocs.org/sdr/CVGA20230927001), Sep 23, 2023: TRANSDUCER. FAULTY. COMING INTO PARKING, BRAKES ON BOTH SIDES WENT ALL THE WAY TO THE FLOOR AND WOULD NOT STOP. BRAKES WORKED BRIEFLY AND STOPPED THE AIRCRAFT. EMERGENCY BRAKE WAS - [SDR CVGA20230918001](https://openairdocs.org/sdr/CVGA20230918001), Sep 14, 2023: SWITCH. FAILED. SUDDEN LEFT YAW AND LEFT THROTTLE UN-COMMAND REDUCED TO IDLE. THE LEFT THRUST REVERSER HAD BEEN PREVIOUSLY PLACED ON MEL. CLEARED THE MEL ITEM BY REPLACING THE - [SDR CVGA20230915001](https://openairdocs.org/sdr/CVGA20230915001), Sep 14, 2023: UNKNOWN. UNKNOWN. LEFT THRUST REVERSER DEPLOY IN FLIGHT. FOUND THRUST REVERSER LH DEACTIVATION PROCEDURE PERFORMED ON 9/13/2023 WAS INCOMPLETE. CONNECTORS P427 AND P429 WERE STIL - [SDR OEJA202308170001](https://openairdocs.org/sdr/OEJA202308170001), Aug 16, 2023: CONTROL BOX. FAILED. DURING TAKE OFF ROLL AND ABOUT 60 KNOTS THE LEFT BLEED SOURCE CAUTION LIGHT CAME ON INDICATION BLEED AIR FAILURE , SO THE TAKE OFF WAS REJECTED - [SDR CVGA20230814001](https://openairdocs.org/sdr/CVGA20230814001), Aug 10, 2023: UNKNOWN. UNKNOWN. CLIMBING OUT OF SSI AT 14,000 FT WE NOTICED AN INCREASING FUEL IMBALANCE TOWARD THE RIGHT, FOLLOWED BY A ROLL SERVO WARNING (YELLOW A IN A BOX ON PFD). WE THEN - [SDR YQKA202308090001](https://openairdocs.org/sdr/YQKA202308090001), Aug 10, 2023: STARTER GEN. MISOVERHAULED. STARTER/GENERATOR ORDERED AND RECEIVED. UPON INSPECTION OF STARTER/ GENERATOR IT WAS FOUND THAT ONE OF THE FOUR BRUSH TERMINALS WAS LOOSE AND NOT MAKING PROPER - [SDR CVGA20230727001](https://openairdocs.org/sdr/CVGA20230727001), Jul 23, 2023: UNKNOWN. UNKNOWN. SMOKE FROM COPILOT'S SIDE CABIN TRAY TABLE AREA ALONG WITH EXCESSIVE HEAT FROM COCKPIT ON COPILOT'S SIDE. A/C CIRCUIT BREAKER WAS PULLED BY PREVIOUS CREW AND DE All 1,397: https://openairdocs.org/model/filper-400a/reports.md ## The same model under other registry codes Amateur-built copies and renamed makers get their own codes. - [Raytheon 400A](https://openairdocs.org/model/raytheon-400a): 216 registered aircraft, registry code 7150010 - [Hawker Beechcraft 400A](https://openairdocs.org/model/hawker-beechcraft-400a): 39 registered aircraft, registry code 4220001 - [Beech 400A](https://openairdocs.org/model/beech-400a): 37 registered aircraft, registry code 1155402 - [Beech 400A](https://openairdocs.org/model/beech-400a): 6 registered aircraft, registry code 1155404 --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.