# Reims Aviation S A F406

- Type: Aircraft model (FAA registry)
- Registry code: 7534006
- Manufacturer (registry): REIMS AVIATION S A
- Model: F406
- Aircraft type: Fixed wing multi engine
- Category: Airplane
- Engines: 2 · Turbo-prop
- Seats: 11
- 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-aviation-s-a-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)

- [N17CK](https://openairdocs.org/aircraft/N17CK): [Agape Flights Inc](https://openairdocs.org/faa-owner/AGAPE%20FLIGHTS%20INC), [Venice, FL](https://openairdocs.org/faa-place/FL/Venice), built 1985, S/N F4060001
- [N406WT](https://openairdocs.org/aircraft/N406WT): [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), S/N F4060043

## NTSB investigations (2)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB ANC05IA048](https://openairdocs.org/ntsb/ANC05IA048), Mar 9, 2005: Reims F406 (N6591R), Nome, AK, incident, minor damage. Probable cause: The failure of the nose gear up lock actuator bracket during the landing approach due to fatigue cracking, which resulted in a nose wheel up landing. A factor associated with the incident is the…
- [NTSB ANC03FA096](https://openairdocs.org/ntsb/ANC03FA096), Aug 17, 2003: Reims 406 (N6591L), Barrow, AK, substantial damage, 2 fatal. Probable cause: An in-flight collision with ocean waters while maneuvering for an undetermined reason.

## FAA accident and incident reports (7)

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 20121107025959I](https://openairdocs.org/incident/20121107025959I), Nov 7, 2012: Reims Aviation S.A. F406/CARAVAN II (N861FT), Bethel, AK, Minor damage. At approximately 1030 on 11/7/2012, the air carrier's director of operations informed the cmt that one of their aircraft was circling the Bethel Airport with a…
- [Incident 20050308006389I](https://openairdocs.org/incident/20050308006389I), Mar 8, 2005: Reims F406 (N6591R), Nome, AK, Minor damage. (-23) [privacy data omitted] ten to fifteen minutes in cruise the pilot heard and felt two thumps under his feet. About three miles out from Nome, the pilot…
- [Incident 20050307006379I](https://openairdocs.org/incident/20050307006379I), Mar 7, 2005: Reims F406 (N6591R), Nome, AK. (-23) [privacy data omitted] the aircraft landed on runway 02 and upon aircraft roll out the aircraft's nose tire went flat. On 3/8/05 aircraft landed with…
- [Incident 20041029028779I](https://openairdocs.org/incident/20041029028779I), Oct 29, 2004: Reims F406 (N6590Y), Savoonga, AK, Substantial damage. (-23) On October 29, 2004, an aircraft, Reims aircraft F406, N6590Y operated by hageland aviation services inc. and piloted by Mr. Michael james callahan, had…
- [Accident 20030817037069A](https://openairdocs.org/incident/20030817037069A), Aug 17, 2003: Reims F406 (N6591L), Barrow, AK, Destroyed, 2 fatal. (-23) [privacy data omitted] aircraft was reportedly observed on radar as it made a tight 360 degree turn at approximately 500 feet MSL before disappearing…
- [Incident 20030710016309I](https://openairdocs.org/incident/20030710016309I), Jul 10, 2003: Reims F406 (N6591L), Kotzebue, AK, Minor damage. (-23) [privacy data omitted] pilot lowered gear for landing in shaktolik, checked mirror on left engine cowling for verification of down and locked position,…
- [Incident 20011125037019I](https://openairdocs.org/incident/20011125037019I), Nov 25, 2001: Reims F406 (N17CK), Charlotte Amali, U.S. Virgin Islands, Minor damage. (-23) On November 25, 2001, capt. clint shillingford (ATP 580099977) was parking his aircraft (Cessna N17CK) into the us customs arrival ramp area at st.…

## 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-aviation-s-a-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

## PMA parts (OpenAirDocs) (264, first 50)

Current parts manufacturer approvals (PMA): parts the FAA has approved companies to make as replacements or modifications. Each record lists its models as free text; OpenAirDocs matched them to this model on its data sheet, so check the FAA record before relying on it. Newest first.

- [CA35-231](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID197093269820260211190011.0001): Face Plate. Cygnet Aerospace Corp · PMA PQ2007NM · Modification part · Jan 28, 2026
- [CA60-524080-10](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID193266159120260211190009.0001): Beech Control Wheel Assy.. Cygnet Aerospace Corp · PMA PQ2007NM · Modification part · Jan 28, 2026
- [CA7650-10](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID182410414320260211190004.0001): Cessna Control Wheel Assy.. Cygnet Aerospace Corp · PMA PQ2007NM · Modification part · Jan 28, 2026
- [CA60-524080](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID179378962320260211190009.0001): Finished Casting. Cygnet Aerospace Corp · PMA PQ2007NM · Modification part · Jan 28, 2026
- [CA60-524080-L](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID177201931320260211190010.0001): Leather Wrapping (Optional). Cygnet Aerospace Corp · PMA PQ2007NM · Modification part · Jan 28, 2026
- [CA7652](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID172325401520260211190007.0001): Cessna Face Plate Basic. Cygnet Aerospace Corp · PMA PQ2007NM · Modification part · Jan 28, 2026
- [CA7650-L](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID170252815020260211190005.0001): Leather Wrapping (Optional). Cygnet Aerospace Corp · PMA PQ2007NM · Modification part · Jan 28, 2026
- [CA35-230](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID168327957920260211190011.0001): Thumb Plate. Cygnet Aerospace Corp · PMA PQ2007NM · Modification part · Jan 28, 2026
- [CA7653](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID147682802720260211190007.0001): Cessna Face Plate Deluxe. Cygnet Aerospace Corp · PMA PQ2007NM · Modification part · Jan 28, 2026
- [CA7651](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID134598314320260211190006.0001): Thumb Plate. Cygnet Aerospace Corp · PMA PQ2007NM · Modification part · Jan 28, 2026
- [CA7650](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID117689777020260211190005.0001): Finished Casting. Cygnet Aerospace Corp · PMA PQ2007NM · Modification part · Jan 28, 2026
- [MC0541139](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID145376008020250129214854.0001): PLUG. McFarlane Aviation Inc. · PMA PQ3732CE · Replaces 0411058-9, 0541139, 0541139-0… · Jan 24, 2025
- [MDL RR1-2-01](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID178956445720250311133057.0001): Alternate Avionic SupportStrut Assemblies forBeech, Cessna, and PiperAirplanes. Radiorax Aviation Systems LLC · PMA PQ00040WB · Modification part · Jan 17, 2025
- [MDL RR1-2-01](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID149312169820250311133056.0001): Alternate Avionic SupportStrut Assemblies. Radiorax Aviation Systems LLC · PMA PQ00040WB · Modification part · Jan 17, 2025
- [M06-201100](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID166099182020241022163145.0001): Label. Miraj Corporation · PMA PQ0870NE · Replaces Safran 06-201100 · Oct 10, 2024
- [No part number](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID124885124220220706160213.0001): Whelen Aerospace Technologies · PMA PQ1372CE · Jun 21, 2022
- [No part number](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID154071880520210622142516.0001): AeroLEDs LLC · PMA PQ5259NM · Mar 11, 2021
- [No part number](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID505004714820210702175236.0001): Aspen Avionics · PMA PQ03868SW · Jan 20, 2021
- [GMD1521203-1](https://drs.faa.gov/browse/excelExternalWindow/476B436D42F05F28862585EE0027133D.0001): Cylinder End. General Machine - Diecron Inc · PMA PQ1586CE · Replaces 1521203-1 · Jul 6, 2020
- [RM57213-9](https://drs.faa.gov/browse/excelExternalWindow/061452B97DA2A54F8625858300359B09.0001): Bearing. Rimark Manufacturing · PMA PQ10018NE · Replaces 57213-9 · Nov 26, 2019
- [700-00190-100](https://drs.faa.gov/browse/excelExternalWindow/CB6B45C441A97D20862585510065ECA1.0001): SkyTrax 100B. Avidyne Corporation · PMA PQ4035CE · Replaces N/A · May 13, 2019
- [300-010](https://drs.faa.gov/browse/excelExternalWindow/DBB68B7E4B5097ED8625812200721B55.0001): Mounting Brackets. Med-Pac Inc · PMA PQ2690CE · Modification part · May 14, 2017
- [600-001](https://drs.faa.gov/browse/excelExternalWindow/A158DEC77B9416528625812200721BDF.0001): Stretcher. Med-Pac Inc · PMA PQ2690CE · Modification part · May 14, 2017
- [400-001, 400-002](https://drs.faa.gov/browse/excelExternalWindow/8FA09485543805658625812200721A57.0001): Ambulance unit. Med-Pac Inc · PMA PQ2690CE · Modification part · May 14, 2017
- [200-001](https://drs.faa.gov/browse/excelExternalWindow/65B207434280BA2F8625812200721C6A.0001): Electrical interface wiring harness. Med-Pac Inc · PMA PQ2690CE · Modification part · May 14, 2017
- [TR-55-0295-1](https://drs.faa.gov/browse/excelExternalWindow/B8A8515B034E2D2186257FCA0052EA1C.0001): Contact. Aerospace Turbine Rotables · PMA PQ3736CE · Replaces Grimes 55-0295-1 · Jan 31, 2016
- [W/T-2752-RH](https://drs.faa.gov/browse/excelExternalWindow/F4E94AEFE30471C986257ECE0050DEA9.0001): Cessna 404/406 4th Windows (Green Right). Great Lakes Aero Products Inc · PMA PQ2056CE · Replaces 5811150-6, 5811152-4, 4061-5600-10 · Sep 24, 2015
- [W-2304-RH](https://drs.faa.gov/browse/excelExternalWindow/F19338A65953418586257ECE00527630.0001): Cessna 404 2nd Side Window (Clear Right). Great Lakes Aero Products Inc · PMA PQ2056CE · Replaces 5811150-4, 5811152-2, 4061-5600-8 · Sep 24, 2015
- [SC-W/T-2751](https://drs.faa.gov/browse/excelExternalWindow/E3DABFA4B4306F7386257ECE0051E0F9.0001): Reims F406 3rd Window - LH (SC Green Right). Great Lakes Aero Products Inc · PMA PQ2056CE · Replaces 5811152-11 · Sep 24, 2015
- [SC-W/XT-2751](https://drs.faa.gov/browse/excelExternalWindow/E22D1D1D2E6AB5C886257ECE0051E11C.0001): Reims F406 3rd Window - LH (SC Any Tint Right). Great Lakes Aero Products Inc · PMA PQ2056CE · Replaces 5811152-11 · Sep 24, 2015
- [W-2304-250-RH](https://drs.faa.gov/browse/excelExternalWindow/D4E0C23F0BD331F486257ECE005276BB.0001): Cessna 404 2nd Side Window (.250 INCH Clear Right). Great Lakes Aero Products Inc · PMA PQ2056CE · Replaces 5811150-4, 5811152-2, 4061-5600-8 · Sep 24, 2015
- [SC-W/XT-2304-RH](https://drs.faa.gov/browse/excelExternalWindow/CFCF4B121C1E645686257ECE005276AB.0001): Cessna 404 2nd Side Window (SC Any Tint Right). Great Lakes Aero Products Inc · PMA PQ2056CE · Replaces 5811150-4, 5811152-2, 4061-5600-8 · Sep 24, 2015
- [SC-W/T-2304-RH](https://drs.faa.gov/browse/excelExternalWindow/CCD7100CBA2A0FBF86257ECE00527687.0001): Cessna 404 2nd Side Window (SC Green Right). Great Lakes Aero Products Inc · PMA PQ2056CE · Replaces 5811150-4, 5811152-2, 4061-5600-8 · Sep 24, 2015
- [SC-W/G-2751](https://drs.faa.gov/browse/excelExternalWindow/C2828B3F46F7E8F586257ECE0051E10C.0001): Reims F406 3rd Window - LH (SC Gray Right). Great Lakes Aero Products Inc · PMA PQ2056CE · Replaces 5811152-11 · Sep 24, 2015
- [SC-W/XT-2752-RH](https://drs.faa.gov/browse/excelExternalWindow/BFDFB955BAD7275E86257ECE0050DF13.0001): Cessna 404/406 4th Windows (SC Any Tint Right). Great Lakes Aero Products Inc · PMA PQ2056CE · Replaces 5811150-6, 5811152-4, 4061-5600-10 · Sep 24, 2015
- [W/XT-2304-250-RH](https://drs.faa.gov/browse/excelExternalWindow/BBD31DDE2A05445186257ECE005276E5.0001): Cessna 404 2nd Side Window (.250 INCH Any Tint Right). Great Lakes Aero Products Inc · PMA PQ2056CE · Replaces 5811150-4, 5811152-2, 4061-5600-8 · Sep 24, 2015
- [W/G-2752-250-RH](https://drs.faa.gov/browse/excelExternalWindow/B88B4608FD6EAF8186257ECE0050DF43.0001): Cessna 404/406 4th Windows (.250 INCH Gray Right). Great Lakes Aero Products Inc · PMA PQ2056CE · Replaces 5811150-6, 5811152-4, 4061-5600-10 · Sep 24, 2015
- [SC-W/G-2304-RH](https://drs.faa.gov/browse/excelExternalWindow/B4163A824A131C2786257ECE0052769A.0001): Cessna 404 2nd Side Window (SC Gray Right). Great Lakes Aero Products Inc · PMA PQ2056CE · Replaces 5811150-4, 5811152-2, 4061-5600-8 · Sep 24, 2015
- [W/XT-2304-RH](https://drs.faa.gov/browse/excelExternalWindow/AB18C3DB120A5BD486257ECE00527674.0001): Cessna 404 2nd Side Window (Any Tint Right). Great Lakes Aero Products Inc · PMA PQ2056CE · Replaces 5811150-4, 5811152-2, 4061-5600-8 · Sep 24, 2015
- [SC-W/XT-2304-250-RH](https://drs.faa.gov/browse/excelExternalWindow/A9C3D35A61BE1DB086257ECE00527714.0001): Cessna 404 2nd Side Window (.250 INCH SC Any Tint Right). Great Lakes Aero Products Inc · PMA PQ2056CE · Replaces 5811150-4, 5811152-2, 4061-5600-8 · Sep 24, 2015
- [W/XT-2752-250-RH](https://drs.faa.gov/browse/excelExternalWindow/9E7EB01B5904CAF886257ECE0050DF53.0001): Cessna 404/406 4th Windows (.250 INCH Any Tint Right). Great Lakes Aero Products Inc · PMA PQ2056CE · Replaces 5811150-6, 5811152-4, 4061-5600-10 · Sep 24, 2015
- [W-2752-RH](https://drs.faa.gov/browse/excelExternalWindow/9B7921B030E595EC86257ECE0050DE7B.0001): Cessna 404/406 4th Windows (Clear Right). Great Lakes Aero Products Inc · PMA PQ2056CE · Replaces 5811150-6, 5811152-4, 4061-5600-10 · Sep 24, 2015
- [W/G-2304-250-RH](https://drs.faa.gov/browse/excelExternalWindow/9666CC2A46A63FEA86257ECE005276D5.0001): Cessna 404 2nd Side Window (.250 INCH Gray Right). Great Lakes Aero Products Inc · PMA PQ2056CE · Replaces 5811150-4, 5811152-2, 4061-5600-8 · Sep 24, 2015
- [SC-W/T-2752-RH](https://drs.faa.gov/browse/excelExternalWindow/8A93577E858E70DC86257ECE0050DEEF.0001): Cessna 404/406 4th Windows (SC Green Right). Great Lakes Aero Products Inc · PMA PQ2056CE · Replaces 5811150-6, 5811152-4, 4061-5600-10 · Sep 24, 2015
- [W-2752-250-RH](https://drs.faa.gov/browse/excelExternalWindow/8A8CC11EA98C4C8786257ECE0050DF24.0001): Cessna 404/406 4th Windows (.250 INCH Clear Right). Great Lakes Aero Products Inc · PMA PQ2056CE · Replaces 5811150-6, 5811152-4, 4061-5600-10 · Sep 24, 2015
- [W/XT-2751](https://drs.faa.gov/browse/excelExternalWindow/806D0AFF6628C77586257ECE0051E0E5.0001): Reims F406 3rd Window - LH (Any Tint Right). Great Lakes Aero Products Inc · PMA PQ2056CE · Replaces 5811152-11 · Sep 24, 2015
- [W/XT-2752-RH](https://drs.faa.gov/browse/excelExternalWindow/752605B6D71BE32186257ECE0050DED9.0001): Cessna 404/406 4th Windows (Any Tint Right). Great Lakes Aero Products Inc · PMA PQ2056CE · Replaces 5811150-6, 5811152-4, 4061-5600-10 · Sep 24, 2015
- [W-2751](https://drs.faa.gov/browse/excelExternalWindow/6ADC74EA8D3A65EF86257ECE0051E092.0001): Reims F406 3rd Window - LH (Clear Right). Great Lakes Aero Products Inc · PMA PQ2056CE · Replaces 5811152-11 · Sep 24, 2015
- [SC-W/G-2752-RH](https://drs.faa.gov/browse/excelExternalWindow/5EACE1BD370C3B0A86257ECE0050DF03.0001): Cessna 404/406 4th Windows (SC Gray Right). Great Lakes Aero Products Inc · PMA PQ2056CE · Replaces 5811150-6, 5811152-4, 4061-5600-10 · Sep 24, 2015
- [W/T-2304-250-RH](https://drs.faa.gov/browse/excelExternalWindow/3FE203D8FAFFE61586257ECE005276C6.0001): Cessna 404 2nd Side Window (.250 INCH Green Right). Great Lakes Aero Products Inc · PMA PQ2056CE · Replaces 5811150-4, 5811152-2, 4061-5600-8 · Sep 24, 2015

All of them: https://openairdocs.org/model/reims-aviation-s-a-f406/pma.md

## The same model under other registry codes

Amateur-built copies and renamed makers get their own codes.

- [Reims F406](https://openairdocs.org/model/reims-f406): 2 registered aircraft, registry code 7535723

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