# Reims F406 - Type: Aircraft model (FAA registry) - Registry code: 7535723 - Manufacturer (registry): REIMS - Model: F406 - Aircraft type: Fixed wing multi engine - Category: Airplane - Engines: 2 · Turbo-prop - Seats: 14 - Weight class: Up to 12,499 lb - Certification: Type certificated - Data sheet: [TCDS A54EU](https://openairdocs.org/tcds/A54EU) (OpenAirDocs) - Holder: ASI Aviation - Registered aircraft: 2 - Page: https://openairdocs.org/model/reims-f406 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. - [AD 2021-23-09](https://openairdocs.org/ad/2021-23-09): Flight Control System · ASI F406. Effective Jan 10, 2022 - [AD 2021-22-21](https://openairdocs.org/ad/2021-22-21): Electrical Power System · ASI F406. Effective Jan 3, 2022 - [AD 2016-19-15](https://openairdocs.org/ad/2016-19-15): Stabilizers · Reims F406. Effective Nov 2, 2016 - [AD 2013-06-04](https://openairdocs.org/ad/2013-06-04): Flight Controls · Reims F406. Effective May 3, 2013 - [AD 2013-04-02](https://openairdocs.org/ad/2013-04-02): Landing Gear · Reims F406. Effective Mar 28, 2013 - [AD 2011-07-03](https://openairdocs.org/ad/2011-07-03): Flight Controls · Reims F406. Effective Apr 26, 2011 - [AD 2007-26-08 R1](https://openairdocs.org/ad/2007-26-08-R1): Landing gear · Reims F406. Effective Dec 4, 2009 - [AD 2007-11-04](https://openairdocs.org/ad/2007-11-04): Ailerons bearings · Reims F406. Effective Jun 26, 2007 - [AD 2007-10-02](https://openairdocs.org/ad/2007-10-02): Bracket-hinge of the rudder · Reims F406. Effective Jun 13, 2007 - [AD 2007-09-02](https://openairdocs.org/ad/2007-09-02): Connection of the center wing and the fuselage · Reims F406. Effective May 31, 2007 - [AD 2007-05-09](https://openairdocs.org/ad/2007-05-09): Nose landing gear collapse · Reims F406. Effective Apr 11, 2007 - [AD 2003-09-09 R1](https://openairdocs.org/ad/2003-09-09-R1): Fuel pump boost wiring · Cessna 441 and F406. Effective Jan 22, 2004 - [AD 2001-23-07](https://openairdocs.org/ad/2001-23-07): Center Wing Carry-Through Area · Reims F406. Effective Jan 7, 2002 - [AD 98-04-28](https://openairdocs.org/ad/98-04-28): AFM - Limitations Section - Icing · Cessna 310R, 335, 340A and 12 more. Effective Mar 13, 1998 - [AD 97-01-13](https://openairdocs.org/ad/97-01-13): Fuel, Oil and Hydraulic Hoses · Cessna 150, 150A, 150B and 232 more. Effective Feb 3, 1997 - [AD 92-16-18](https://openairdocs.org/ad/92-16-18): Passenger Seat Reinforcement · Cessna 401, 402, 402A and 9 more. Effective Sep 10, 1992 Historical (superseded or no longer in force): - [AD 2015-16-07 R1](https://openairdocs.org/ad/2015-16-07-R1) (historical): Flight controls. · Reims F406. Effective Dec 28, 2015 - [AD 2015-16-07](https://openairdocs.org/ad/2015-16-07) (historical): Flight Controls · Reims F406. Effective Aug 18, 2015 - [AD 2007-26-08](https://openairdocs.org/ad/2007-26-08) (historical): Landing gear emergency blowdown bottle · Reims F406. Effective Jan 31, 2008 - [AD 2007-02-12](https://openairdocs.org/ad/2007-02-12) (historical): Rudder pulley bracket · Reims F406. Effective Feb 13, 2007 - [AD 2003-09-09](https://openairdocs.org/ad/2003-09-09) (historical): Fuel Boost Pump Wiring · Cessna Aircraft Company, The 441 and F406. Effective Jun 24, 2003 ## Information bulletins (advisory) (1) - [SAIB ACE-98-03](https://openairdocs.org/saib/ACE-98-03): . Issued Oct 17, 1997 ## Registered aircraft (2) - [N27NW](https://openairdocs.org/aircraft/N27NW): [Csc Delaware Trust Co Trustee](https://openairdocs.org/faa-owner/CSC%20DELAWARE%20TRUST%20CO%20TRUSTEE), [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington), built 1987, S/N 008 - [N406SD](https://openairdocs.org/aircraft/N406SD): [Tvpx Aircraft Solutions Inc Trustee](https://openairdocs.org/faa-owner/TVPX%20AIRCRAFT%20SOLUTIONS%20INC%20TRUSTEE), [North Salt Lake, UT](https://openairdocs.org/faa-place/UT/North%20Salt%20Lake), built 1991, S/N 0063 ## NTSB investigations None matched to aircraft with this model. ## FAA accident and incident reports (2) From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [Incident 20120128001599I](https://openairdocs.org/incident/20120128001599I), Jan 28, 2012: Reims Aviation S.A. F406/CARAVAN II (N406SD), Shishmaref, AK, Substantial damage. After landing at Shishmaref on runway 5, upon aircraft roll out (taxi), the left wing of the aircraft dropped and the aircraft pulled to the left and could not… - [Incident 20001204022539I](https://openairdocs.org/incident/20001204022539I), Dec 4, 2000: Reims F406 (N406SD), Minor damage. (-23) Ptrs#ALO122001B0528 on December 4, 2000 at approx. 1018 local time, the pilot of this twin engine Cessna caravan N406SD, model #F-406-406, could not get… ## Service difficulty reports (77, newest 50) As reported by operators and repair stations, by the model named in the report. - [SDR CA151228007](https://openairdocs.org/sdr/CA151228007), Dec 13, 2015: ENGINE. SMOKE. (CAN) WHILE LANDING ON A TRAINING FLIGHT, AFTER THE REVERSE WAS APPLIED AND STOWED NORMALLY, THE LT ENGINE LOW OIL PRESSURE LIGHT ILLUMINATED. THE PILOT TRIED T - [SDR EPUA20151006001](https://openairdocs.org/sdr/EPUA20151006001), Oct 6, 2015: CIRCUIT BREAKER. OVERHEATED. DURING CRUISE FLIGHT WITH LT & RT PROP DE-ICE SELECTED ON, THE PILOT OBSERVED SMOKE COMING OUT OF THE LT PROP DE-ICE SWITCH & CB. THE PILOT ATTEMPTED TO TURN TH - [SDR EPUA20151006002](https://openairdocs.org/sdr/EPUA20151006002), Oct 2, 2015: BAR. CRACKED. DURING INSPECTION IAW SB F406-104 PART B & AD 2015-16-07, CRACKS WERE DISCOVERED ON PN 5115260-1 LT & PN 5115260-3. RT RUDDER BARS VIA MAGNETIC PARTICLE INSPECT - [SDR EPUA080415004](https://openairdocs.org/sdr/EPUA080415004), Aug 4, 2015: BAR. CRACKED. DURING INSPECTION IAW SB F406-104 PART B A CRACK WAS DETECTED ON RT RUDDER BAR ASSEMBLY, PN 5115260-2, RT & LT RUDDER BAR ASSEMBLY PN 5115260-1 VIA MAG PARTICLE - [SDR EPUA080415003](https://openairdocs.org/sdr/EPUA080415003), Aug 4, 2015: BAR. CRACKED. DURING INSPECTION IAW SB F406-104 PART B A CRACK WAS DETECTED ON RT RUDDER BAR ASSEMBLY PN 5115260-2 VIA MAG PARTICLE INSPECTION. THIS SERVICE BULLETIN IS REQUI - [SDR CA150408006](https://openairdocs.org/sdr/CA150408006), Mar 27, 2015: ENGINE. MALFUNCTIONED. (CAN) DURING ROUTINE SURVEILLANCE MISSION, CREW REPORTED LOUD NOISE FOLLOWED BY A ROLL BACK IN TORQUE TO ZERO & CORRESPONDING YAW. THE HIGH PRESS NH & LOW PRESS - [SDR EPUA20141121001](https://openairdocs.org/sdr/EPUA20141121001), Nov 21, 2014: CALIPER. LEAKING. RIGHT BRAKE LEAKING HYD FLUID & NOT WORKING. REPLACED RT BRAKE CALIPER ASSEMBLY, BLED BRAKES & PERFORMED BRAKE BURN IN PROCEDURE. - [SDR EPUA20140919001](https://openairdocs.org/sdr/EPUA20140919001), Sep 17, 2014: O-RING. LEAKING. DURING GND OPERATIONS THE LT MAIN BRAKE SYS FAILED. REPLACED THE O RINGS FOR THE LT MLG CALIPER & BLED THE HYD FLUID. - [SDR EPUA20140220001](https://openairdocs.org/sdr/EPUA20140220001), Feb 20, 2014: DOOR. UNSECURE. AFTER LANDING & DURING TAXI TO PARKING AREA, THE RT MLG DOOR WAS SEEN FALLING OFF OF ACFT. NO ADDITIONAL DAMAGE TO ACFT OCCURRED DURING THIS EVENT. DETERMINED T - [SDR CA131021018](https://openairdocs.org/sdr/CA131021018), Oct 15, 2013: BLADE. FRACTURED. (CAN) DURING CLIMB, THE PILOT HEARD A LOUD NOISE FROM NR 2 ENGINE. HE THEN NOTICED TORQUE HAD DROPPED TO 20 PERCENT BUT HE FELT NO PHYSICAL POWER CHANGE AND ASS - [SDR CA130513003](https://openairdocs.org/sdr/CA130513003), Apr 23, 2013: ENGINE. FLAMED OUT. (CAN) THE OPERATOR REPORTED THE ENGINE FLAMED OUT WHILE TRANSITIONING FROM REVERSE TO IDLE AFTER LANDING. THE ACFT WILL BE FERRIED FOR AN INVESTIGATION WITH THE - [SDR EPUA20121107001](https://openairdocs.org/sdr/EPUA20121107001), Nov 7, 2012: LANDING GEAR. INOPERATIVE. DURING LANDING PROCEDURES, ON APPROACH, THE PILOT REPORTED THE NOSE GEAR FAILED TO EXTEND. ACFT LANDED WITH THE NOSE LANDING GEAR RETRACTED. - [SDR CA120813014](https://openairdocs.org/sdr/CA120813014), Aug 7, 2012: ENGINE. STOPPED. (CAN) REPORTEDLY, THE NR 1 ENGINE HAD A SUDDEN STOPPAGE IN FLIGHT. THE ACFT LANDED SAFELY. FSR REQUESTING FURTHER DETAILS. MFG IS FULLY COMMITTED TO ADDRESS THI - [SDR EPUA20120530001](https://openairdocs.org/sdr/EPUA20120530001), May 29, 2012: SWITCH. CONTAMINATED. LANDING GEAR POPPED BREAKER WHEN GEAR HANDLE SWITCHED DOWN TO UP; CLEANED MOISTURE IN NOSE GEAR SWITCHES, SWUNG GEAR IAW F406 MM NUMEROUS TIMES. CHECKED GOOD. S - [SDR EPUA20120320003](https://openairdocs.org/sdr/EPUA20120320003), Mar 17, 2012: BRAKE. MALFUNCTIONED. NO LEFT BREAK, RT & LT MAIN BRAKE CALIPER, LEAK AND OPS CHECKED GOOD. - [SDR 2012FA0000118](https://openairdocs.org/sdr/2012FA0000118), Jan 28, 2012: FORK. SHEARED. AFTER LANDING AND WHILE TAXIING TO THE END OF A ROUGH ASPHALT RUNWAY, THE 2 INCH ROUND BAR SHEARED 9 INCHES FROM THE AXLE. NO PREVIOUS INDICATION OF POTENTIAL F - [SDR EPUA20120112002](https://openairdocs.org/sdr/EPUA20120112002), Dec 7, 2011: SWITCH. FAULTY. GREEN LIGHT-GEAR DOWN LIGHT ON NOSE WHEEL DOES NOT TURN ON, MX REPLACED 602EN600-6 SWITCH FOR THE NOSE GEAR DOWN LOCK OVER CENTER INDICATOR SYS. - [SDR CA110627012](https://openairdocs.org/sdr/CA110627012), Jun 16, 2011: TURBINE BLADES. FRACTURED. (CAN) UNCONTAINED EVENT SHORTLY AFTER DEPARTURE, THE PILOT NOTED THAT THE LT ENGINE TORQUE WAS FLUCTUATING, WHICH WAS FOLLOWED BY A LOUD NOISE AND FLAMES FROM T - [SDR EPUA040808](https://openairdocs.org/sdr/EPUA040808), Apr 8, 2008: SKIN. CRACKED. DURING A ROUTINE INSPECTION A LARGE STRESS CRACK WAS DISCOVERED EMANATING FROM THE BASE OF THE UPPER VHS COMM ANTENNA BASE AT FS 154.80 RIGHT OF CENTERLINE. THE - [SDR EPUA120107](https://openairdocs.org/sdr/EPUA120107), Dec 1, 2007: SPAR. CRACKED. DURING ROUTINE SCHEDULED MAINTENANCE, A CRACK WAS DISCOVERED APPROX 6.5" LONG IN A U-SHAPED PATTERN ON THE LT WING MAIN SPAR AT LT CWS 51.00 TO CWS 48.00, EMANA - [SDR CA070704012](https://openairdocs.org/sdr/CA070704012), May 11, 2007: SEAL. FRACTURED. (CAN) IN CRUISE, ENGINE OIL PRESSURE WAS SEEN TO FLUCTUATE AND SUBESQUENTLY DECREASE. OIL WAS SEEN ESCAPING FROM THE ENGINE NACELLE. THE ENGINE WAS SHUTDOWN IN - [SDR AU510002062](https://openairdocs.org/sdr/AU510002062), Dec 12, 2005: TIRE. DEFLATED. (AUS) RT MAIN LANDING GEAR TIRE DEFLATED. SUSPECT TIRE DAMAGED BY FOD.(OTHER CAUSE: MATERIAL ) (CASA NR 510002062) - [SDR AU510001897](https://openairdocs.org/sdr/AU510001897), Dec 12, 2005: COOLING FAN. ODOR. (AUS) ODOR IN COCKPIT. INVESTIGATION FOUND ODOR ONLY BECAME PRESENT WHEN THE AIR CONDITIONING SYSTEM WAS SELECTED OFF. FURTHER INVESTIGATION FOUND THE ODOR CAME - [SDR AU510001479](https://openairdocs.org/sdr/AU510001479), Dec 12, 2005: INDICATOR. FAULTED. (AUS) LH VERTICAL SPEED INDICATOR (VSI) NEEDLE FLUCTUATING. GROUND TEST COULD FIND NO FAULTS WITH THE SYSTEM. NO FURTHER REPORTS OF PROBLEMS. (OTHER CAUSE: UNKN - [SDR AU510001853](https://openairdocs.org/sdr/AU510001853), Nov 9, 2005: CONTROL COLUMN. STICKING. (AUS) CONTROL YOKE STICKING DURING ROLL INPUT. INVESTIGATION FOUND THE CONTROL YOKE CONTACTING THE LT DEFOG VENT. FURTHER INVESTIGATION FOUND THE BOLT HOLES CON - [SDR AU510001986](https://openairdocs.org/sdr/AU510001986), Oct 10, 2005: ENGINE. FAILED. (AUS) RT ENGINE FAILED DURING LANDING ROLL WHEN REVERSE THRUST WAS DE-SELECTED. THOROUGH INVESTIGATION COULD FIND NO CAUSE FOR THE DEFECT. SUSPECT THE FUEL FLOW - [SDR AU510001441](https://openairdocs.org/sdr/AU510001441), May 6, 2005: ANTENNA. FAILED. (AUS) NR 2 HF ANTENNA BROKE AT EMPENNAGE ATTACHMENT POINT. - [SDR AU510001450](https://openairdocs.org/sdr/AU510001450), Apr 6, 2005: ODOR. DETECTED. (AUS) ELECTRICAL BURNING ODOR IN CABIN. INVESTIGATION CONTINUING. (OTHER CAUSE: PENDING FINAL REPORT ) (CASA 510001450) - [SDR AU510001480](https://openairdocs.org/sdr/AU510001480), Apr 5, 2005: MOTOR. FAILED. (AUS) REAR AIR CONDITIONING SYSTEM ELECTRIC MOTOR FAILED. (CASA# 510001480) - [SDR AU510001669](https://openairdocs.org/sdr/AU510001669), Jan 8, 2005: WHEEL. CRACKED. (AUS) LT MLG WHEEL ASSEMBLY HAD 2 SECTIONS OF THE BEAD MISSING. TIRE DEFLATED DURING LANDING ROLL. (CASA NR 510001669) - [SDR CA050419002](https://openairdocs.org/sdr/CA050419002), Nov 25, 2004: ENGINE. INOPERATIVE. (CAN) DURING TAKEOFF, THE ENGINE EXPERIENCED AN UNCOMMANDED POWER REDUCTION. MFG WILL MONITOR THE INVESTIGATION OF THIS INCIDENT AND WILL ADVISE OF ROOT CAUSE, - [SDR AUS20040496](https://openairdocs.org/sdr/AUS20040496), Jun 7, 2004: TRUSS. CORRODED. (AUS) LT ENGINE LOWER LT ATTACHMENT TRUSS CORRODED. - [SDR AUS20040374](https://openairdocs.org/sdr/AUS20040374), May 7, 2004: WIRE. BROKEN. (AUS) FLAP CONTROL SYSTEM WIRE BROKEN. FAULT TRACE TO BROKEN WIRE A157B-A25799200 TO FLAP UP CONTROL SWITCH. - [SDR AUS20040350](https://openairdocs.org/sdr/AUS20040350), Apr 23, 2004: STRIP. SEPARATED. (AUS) STALL STRIP MISSING. - [SDR AUS20040385](https://openairdocs.org/sdr/AUS20040385), Apr 14, 2004: COMPUTER. FAULTY. (AUS) AUTOPILOT COMPUTER FAULTY. - [SDR AUS20040214](https://openairdocs.org/sdr/AUS20040214), Mar 20, 2004: CLAMP. FAILED. (AUS) LT ENGINE PROPELLER REVERSING LEVER CABLE CLAMP BOLT FAILED ALLOWING PROPELLER REVERSING PY LEVER TO DISCONNECT FROM PUSH/PULL CABLE. - [SDR EPUA070304A](https://openairdocs.org/sdr/EPUA070304A), Mar 7, 2004: FIRE LOOP. CHAFED. AS FLIGHT ENTERED DOWNWIND, THE RT FIRE WARNING LIGHT ILLUMINATED. ENGINE WAS SHUTDOWN AND FLIGHT LANDED WITHOUT INCIDENT. MX FOUND THE AFT FIRE LOOP WAS CHAFFE - [SDR AUS20040137](https://openairdocs.org/sdr/AUS20040137), Feb 29, 2004: SERVO. FAULTY. (AUS) AUTOPILOT ROLL SERVO CAPSTAN FOUND IN PIECES ON AIRCRAFT FLOOR. SIX FASTENEING SCREWS FOUND IN CLOSE PROXIMITY TO THE SERVO MOUNT. - [SDR AUS20040060](https://openairdocs.org/sdr/AUS20040060), Feb 3, 2004: ALTIMETER. FAULTY. (AUS) ALTIMETER FITTED TO AIRCRAFT WITH INCORRECT ALTITUDE RANGE. PERSONNEL/MAINTENANCE ERROR. - [SDR AUS20040059](https://openairdocs.org/sdr/AUS20040059), Feb 3, 2004: ALTIMETER. FAULTY. (AUS) ALTIMETER FITTED TO AIRCRAFT WITH INCORRECT ALTITUDE RANGE. PERSONNEL/MAINTENANCE ERROR. - [SDR AUS20040071](https://openairdocs.org/sdr/AUS20040071), Jan 25, 2004: CONTROLLER. FAILED. (AUS) COMMUNICATION SYSTEM CONTROL BOX FAILED. - [SDR AUS20031121](https://openairdocs.org/sdr/AUS20031121), Nov 6, 2003: TIRE. DEFLATED. (AUS) NOSE WHEEL TIRE DEFLATED. NO DAMAGE TO WHEEL RIM. NOSE WHEEL MUD GUARD MISSING. INVESTIGATION FOUND THE VALVE STEM SHEARED FROM THE TUBE. SUSPECT VALVE ST - [SDR AUS20031067](https://openairdocs.org/sdr/AUS20031067), Oct 15, 2003: SPAR CAP. CORRODED. (AUS) RT WING MAIN SPAR LOWER SPAR CAP CORRODED. MICROBIOLOGICAL GROWTH FOUND ON INSIDE OF FUEL ACCESS PANELS 621BB AND 521BB AND 521CB. - [SDR AUS20031013](https://openairdocs.org/sdr/AUS20031013), Oct 2, 2003: SWITCH. FAULTY. (AUS) RT MAIN LANDING GEAR UPLOCK SWITCH FAILED. - [SDR AUS20031155](https://openairdocs.org/sdr/AUS20031155), Aug 29, 2003: WIRE. BROKEN. (AUS) FLAP UP MICROSWITCH WIRE BROKEN. SWITCH IS LOCATED BEHINDFLAP SELECTOR. - [SDR AUS20030775](https://openairdocs.org/sdr/AUS20030775), Jul 31, 2003: MOTOR. FAILED. (AUS) FORWARD AIR CONDITIONER ELECTRIC MOTOR FAILED. - [SDR AUS20030575](https://openairdocs.org/sdr/AUS20030575), Jun 4, 2003: RADOME. BIRD STRIKE. (AUS) BIRDSTRIKE ON SURVEILLANCE RADOME. - [SDR AUS20030457](https://openairdocs.org/sdr/AUS20030457), Apr 22, 2003: SWITCH. FAILED. (AUS) NOSE LANDING GEAR ACTUATOR FAULTY. SWITCH OUT OF ADJUSTMENT. - [SDR AUS20030403](https://openairdocs.org/sdr/AUS20030403), Apr 6, 2003: CLAMP. CORRODED. (AUS) NR 1 ENGINE SHUT DOWN FOLLOWING LT WING OVERHEAT WARNING.INVESTIGATION FOUND THE CLAMP ATTACHED TO THE PNEUMATIC FLOWCONTROL VALVE DOWNSTREAM FROM THE NO1 - [SDR AUS20030378](https://openairdocs.org/sdr/AUS20030378), Mar 20, 2003: ACTUATOR. FAULTY. (AUS) NOSE LANDING GEAR ACTUATOR FAULTY. All 77: https://openairdocs.org/model/reims-f406/reports.md ## STCs that may be installed (OpenAirDocs) (33) Approved for this model: the STC's model list names it on its data sheet, or a series that includes it. In force first, then newest. The registry doesn't record which STCs an aircraft has. - [STC SA04837NY](https://openairdocs.org/stc/SA04837NY): Installation of AeroLED's Holdings, LLC., position lights, navigation lights, strobe lights and beacon lights. AeroLED's Holdings, LLC - [STC SA02019SE-D](https://openairdocs.org/stc/SA02019SE-D): Installation of Garmin Model GTN 625/635/650; 725/750 Navigation System. Garmin International Inc - [STC SA02511SE](https://openairdocs.org/stc/SA02511SE): Installation of replacement fuel quantity indicator sending unit(s). CiES Inc - [STC SA02738CH](https://openairdocs.org/stc/SA02738CH): Installation of L-3 Communications Avionics Systems. Acron Aviation Inc - [STC SA04046CH PAGE 2](https://openairdocs.org/stc/SA04046CH%20PAGE%202): Installation of L-3 GENESIS (TM) Electronic Standby Instrument System (ESI-500/MAG-500). Acron Aviation Inc - [STC SA00279SE](https://openairdocs.org/stc/SA00279SE): Installation of American Aviation Inc. redesigned engine exhaust stacks. American Aviation Inc - [STC SA02658SE](https://openairdocs.org/stc/SA02658SE): Installation of Garmin GI 275 Multi-Function Display System. Garmin International Inc - [STC SA02444AK](https://openairdocs.org/stc/SA02444AK): Approval of the L-3 Communications NGT 9000/9000R ADS-B system installed. ADS-B Technologies LLC - [STC SA09856AC](https://openairdocs.org/stc/SA09856AC): Installation of BendixKing Aerowave 100 In-flight Data Link System for non-essential, non-required aircraft Cabin Systems & Equipments. Honeywell International Inc (Bendix King) - [STC SA11174SC PAGE 2](https://openairdocs.org/stc/SA11174SC%20PAGE%202): Installation of BendixKing by Honeywell KSN 770 and KSN 765 WAAS LPV approach capable nav/comm systems. Honeywell International Inc (Bendix King) - [STC SA00401BO](https://openairdocs.org/stc/SA00401BO): Installation of a SkyTrax100B UAT receiver. Avidyne Corporation - [STC SA02426AK](https://openairdocs.org/stc/SA02426AK): Approval of the FreeFlight FDL-978-TX ADS-B system installed. FreeFlight Systems - [STC SA02268CH](https://openairdocs.org/stc/SA02268CH): Installation of Airwolf Filter Corp. Air Oil Separator. Airwolf Filter Corporation - [STC SA01452CH](https://openairdocs.org/stc/SA01452CH): Installation of an air ambulance conversion kit. Med-Pac Inc - [STC SA01714WI](https://openairdocs.org/stc/SA01714WI): Installation of a Garmin transponders: (a) GTX 330/330D/33/33D with ADS-B Out functionality; (b) GTX 335/335R/345/345R with ADS-B Out and In functionality; or (c) GTX 335R/345R with ADS-B Out functionality in select airplanes installed with G950/G1000 systems. Garmin International Inc - [STC SA00344BO PAGE 2](https://openairdocs.org/stc/SA00344BO%20PAGE%202): Installation of Parmetheus Plus LED PAR36 and PAR46 taxi and landing lights. Whelen Aerospace Technologies - [STC SA00765DE](https://openairdocs.org/stc/SA00765DE): Installation of Automatic Dependent Surveillance Broadcast (ADS-B) Out functionality using the BendixKing KT74 Transponder and qualified position sensor. Peregrine - [STC SA02153LA-D PAGE 2](https://openairdocs.org/stc/SA02153LA-D%20PAGE%202): Installation of Garmin G600 Primary Flight Display (PFD) and Multifunction Display (MFD) System. Garmin International Inc - [STC SA02132AK](https://openairdocs.org/stc/SA02132AK): Reduction/limitation of passenger seats to 9. Hageland Aviation Services, Inc - [STC SA02212AK](https://openairdocs.org/stc/SA02212AK): Replacement of existing landing and/or taxi light reflector and bulbs with high intensity discharge (HID) lighting systems. Seaplanes North LLC - [STC SA02428SE](https://openairdocs.org/stc/SA02428SE): Installation of an Air Stream Switch for an electric time recording device on non-pressurized aircraft. Henry F Rogers/David E Polley - [STC SA00343BO](https://openairdocs.org/stc/SA00343BO): Installation of a single configuration or a dual configuration Avidyne Corporation Integrated Flight Display, Model IFD540 loaded with Release 10.0 software (or later FAA approved release). Avidyne Corporation - [STC SA00352BO PAGE 2](https://openairdocs.org/stc/SA00352BO%20PAGE%202): Installation of an Avidyne Corporation Mode A/C/S Transponder with ADS-B Out capability, Model AXP340 loaded with Version 3.13 software (or later FAA approved version),. Avidyne Corporation - [STC SA02119SE PAGE 2](https://openairdocs.org/stc/SA02119SE%20PAGE%202): Installation of Garmin GDL 88 ADS-B UAT Transceiver System. Garmin International Inc - [STC SA02442AK PAGE 2](https://openairdocs.org/stc/SA02442AK%20PAGE%202): Approval of the L-3 Communications NGT 2000/2500 ADS-B system. ADS-B Technologies, LLC - [STC SA02121SE](https://openairdocs.org/stc/SA02121SE): Installation of Garmin GTS 825 (TAS) or GTS 855 (TCAS I) Traffic System. Garmin International Inc - [STC SA02016SE-D](https://openairdocs.org/stc/SA02016SE-D): Installation of Garmin GTS 800, GTS 820 or GTS 850 Traffic System. Garmin International Inc - [STC SA02168AK](https://openairdocs.org/stc/SA02168AK): Installation of hourmeter airspeed switch. For unpressurized aircraft only. Pressurized aircraft must have pressurization system deactivated. Avalaska Inc - [STC SA00198WI](https://openairdocs.org/stc/SA00198WI): Installation of R134a Air Conditioning System. Guernsey Co - [STC SA00765DE PAGE 1](https://openairdocs.org/stc/SA00765DE%20PAGE%201) (historical): Installation of Automatic Dependent Surveillance Broadcast (ADS-B) Out functionality using the BendixKing KT74 Transponder and qualified position sensor. Peregrine - [STC SA02019SE-D PAGE 2](https://openairdocs.org/stc/SA02019SE-D%20PAGE%202) (historical): Installation of Garmin GTN 6XX/7XX Navigation System. Garmin International Inc - [STC SA02153LA-D](https://openairdocs.org/stc/SA02153LA-D) (historical): Installation of Garmin G600 Primary Flight Display (PFD) and Multifunction Display (MFD) System. Garmin International Inc - [STC SA02153LA](https://openairdocs.org/stc/SA02153LA) (historical): Installation of Garmin G600 Primary Flight Display (PFD) and Multifunction Display (MFD) System. Garmin AT Inc ## The same model under other registry codes Amateur-built copies and renamed makers get their own codes. - [Reims Aviation S A F406](https://openairdocs.org/model/reims-aviation-s-a-f406): 2 registered aircraft, registry code 7534006 --- 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.