# Sabre 95 - Type: Aircraft model (FAA registry) - Registry code: 05904R7 - Manufacturer (registry): SABRE AIRCRAFT - Model: 95 - Aircraft type: Weight-shift-control - Engines: 1 ยท 2 cycle - Seats: 2 - Weight class: Up to 12,499 lb - Certification: Light sport - Registered aircraft: 1 - Page: https://openairdocs.org/model/sabre-95 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 (1) - [N98XT](https://openairdocs.org/aircraft/N98XT): [Dutton Bradley E](https://openairdocs.org/faa-owner/DUTTON%20BRADLEY%20E), [Navarre, OH](https://openairdocs.org/faa-place/OH/Navarre), built 2007, S/N SD1647 ## STCs approved for it (303, first 50) - [STC SA00024NY](https://openairdocs.org/stc/SA00024NY): Installation of Airwolf remote mounted engine oil filter kit AFC-K007 on single or multi-engine fixed wing light aircraft incorporating Lycoming reciprocating engines of 450 horsepower or less.. Airwolf Filter Corporation - [STC SA00061LA](https://openairdocs.org/stc/SA00061LA): Installation of JPI digital tachometer.. J P Instruments - [STC SA00063LA](https://openairdocs.org/stc/SA00063LA): Installation of Acoustical/Thermal insulation.. Luminary Air Group LLC - [STC SA00068SE](https://openairdocs.org/stc/SA00068SE): Installation of fuel flow/pressure instruments. (W/TSIO-360-MB1). Electronics International Inc. - [STC SA00089WI](https://openairdocs.org/stc/SA00089WI): Installation of control cable operated cowl flaps in place of electric controls. MidWest School of Aeronautics - [STC SA00143LA](https://openairdocs.org/stc/SA00143LA): Installation of control yoke retainer lock.. ELT Engineering - [STC SA00149BO](https://openairdocs.org/stc/SA00149BO): Installation of Aircraft Components, Inc. Volt and Vac Alert System, P/N 2044-1. Aircraft Components Inc - [STC SA00161BO (3 OF 3](https://openairdocs.org/stc/SA00161BO%20(3%20OF%203): Installation of Avidyne Corporation FlightMax 700-00007-( ) EX500 Multi-Function Display.. Avidyne Corporation - [STC SA00165BO](https://openairdocs.org/stc/SA00165BO): Installation of Avidyne Corporation Datalink Coupler, part number 700-00015-000 per Avidyne Corporation Master Document List, Document No. AVACP-006 dtd 1/2/93 or later FAA-approved revisions.. Avidyne Corporation - [STC SA00204NY](https://openairdocs.org/stc/SA00204NY): Installation of .250 inch, .312 inch, or .375 inch thick one piece windshields (two piece windshield to one piece windshield conversion).. Knots 2U, Ltd - [STC SA00215NY](https://openairdocs.org/stc/SA00215NY): Installation of CAVU Model AM100 AVMIX engine fuel/air mixture setting system.. CAVU Products Limited - [STC SA00243BO (4 OF 5)](https://openairdocs.org/stc/SA00243BO%20(4%20OF%205)): Installation of Centurion Consulting, Inc. GPS Steering Assist Module (SAM) with roll steering (p/n 0025-5100), or without roll steering (p/n 0025-5200).. Icarus Avionics, LLC - [STC SA00269BO](https://openairdocs.org/stc/SA00269BO): Installation of Avidyne Corporation TWX 670 Tactical Weather Detection System P/N 850-00026-000-( ) consisting of Avidyne Processor P/N 700-00033-000-( ), Sensor Systems Inc. Antenna P/N S72-1715-1 with doubler plate P/N S72-171530-1, and Avidyne Mounting Tray P/N 700-00034-000.. Avidyne Corporation - [STC SA00281BO](https://openairdocs.org/stc/SA00281BO): Installation of Avidyne Corporation MLX770 MultiLink Broadcast Transceiver P/N 700-00163-( ), Sensor Systems Inc. Antenna P/N S67-1575-109, or equivalent, and optional Avidyne Mounting Tray P/N 700-00165-000. Avidyne Corporation - [STC SA00290BO](https://openairdocs.org/stc/SA00290BO): Installation of Avidyne Corporation Part Number 700-00167-XXX Multi-Function Display and Mounting Tray Assembly Part Number 700-00168-XXX. Avidyne Corporation - [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 SA00344BO PAGE 1](https://openairdocs.org/stc/SA00344BO%20PAGE%201): Installation of Parmetheus Plus LED PAR36 and PAR46 taxi and landing lights.. Whelen Aerospace Technologies - [STC SA00352BO PAGE 1](https://openairdocs.org/stc/SA00352BO%20PAGE%201): 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 SA00382BO](https://openairdocs.org/stc/SA00382BO): Installation of Globalstar Antenna and Cradle provisions to support a Globalstar GPS-1700 in non-composite airplanes. Avidyne Corporation - [STC SA00401BO](https://openairdocs.org/stc/SA00401BO): Installation of a SkyTrax100B UAT receiver. Avidyne Corporation - [STC SA00432SE](https://openairdocs.org/stc/SA00432SE): Installation of EGT 701 series fuel flow instrument.. J P Instruments - [STC SA00523AT-D](https://openairdocs.org/stc/SA00523AT-D): Installation of replacement fuel cell assemblies. FFC Manufacturing - [STC SA00575SE](https://openairdocs.org/stc/SA00575SE): Installation of vortex generators on wing leading edge and vertical stabilizer.. Micro AeroDynamics Inc - [STC SA00695SE](https://openairdocs.org/stc/SA00695SE): Replacement of certain Rotomaster and Rayjay scavenge pumps. Machen Inc - [STC SA00712CH](https://openairdocs.org/stc/SA00712CH): Installation of Insight Avionics Strike Finder model SF 2000.. Insight Instrument Corp - [STC SA00722CH](https://openairdocs.org/stc/SA00722CH): Installation of Hartzell HC-C2YK-2CUF/FC7666C(B)-4 propellers and 836-29(P) spinners.. Hartzell Propeller Inc - [STC SA00729SE](https://openairdocs.org/stc/SA00729SE): Installation of twin temperature indicating system with fuel flow in accordance with J.P. Instruments (JPI) Installation manual Report No. 760, Revision -, dated 7/20/99, or later FAA approved revision.. J P Instruments - [STC SA00744DE](https://openairdocs.org/stc/SA00744DE): Installation of the Automatic Dependent Surveillance Broadcast (ADS-B) Out Equipment using a Trig Avionics TT31 Transponder and an approved position sensor. Peregrine - [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 SA00756DE](https://openairdocs.org/stc/SA00756DE): Installation of Automatic Dependent Surveillance Broadcast (ADS-B) Out Equipment using a Trig Avionics TT22 Transponder and an approved Global Positioning System (GPS) Position Sensor. Peregrine - [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 SA00780SE](https://openairdocs.org/stc/SA00780SE): Installation of the True Lock Safety Retention Axle Lock Nut System. True Lock LLC - [STC SA00789LA](https://openairdocs.org/stc/SA00789LA): Installation of Clear View Sunvisor.. Vantage Associates Inc - [STC SA00802NY](https://openairdocs.org/stc/SA00802NY): Installation of Main Landing Gear Auxiliary Landing Lights.. Gallagher Aviation LLC - [STC SA00804SE](https://openairdocs.org/stc/SA00804SE): Installation of an engine failure indicator system, also referred to as a 'low Thrust Detector system.'. Advanced Aero Safety Inc. - [STC SA00861SE](https://openairdocs.org/stc/SA00861SE): Installation of J.P. Instruments (JPI) fuel flow indicating system. J P Instruments - [STC SA00862NY](https://openairdocs.org/stc/SA00862NY): Installation of gas spring cargo door retainer.. Perimeter Aviation Ltd - [STC SA00899CH](https://openairdocs.org/stc/SA00899CH): Installation of pneumatic luggage door strut on those models with an extended luggage door.. Knots 2U, Ltd - [STC SA00901NY](https://openairdocs.org/stc/SA00901NY): Installation of a wing tip recognition lights.. Gallagher Aviation LLC - [STC SA01002AT](https://openairdocs.org/stc/SA01002AT): Installation of left and right hand side auxiliary fuel cell assemblies.. FFC Manufacturing - [STC SA01029AT](https://openairdocs.org/stc/SA01029AT): Installation of a Chelton Aviation Corp (CAC) AP-3C autopilot.. Chelton Aviation Corporation - [STC SA01033WI](https://openairdocs.org/stc/SA01033WI): Replacement of original outboard main landing gear doors with a one-piece monolithic machined metal door.. Machining Programming Manufacturing Inc - [STC SA01077SE](https://openairdocs.org/stc/SA01077SE): Installation of fluoropolymer film.. Columbia Pacific Airlines - [STC SA01078NY](https://openairdocs.org/stc/SA01078NY): Installation of Left and Right Side Windows.. LP Aero Plastics - [STC SA01085LA](https://openairdocs.org/stc/SA01085LA): Installation of the VNS 1000 Voice Navigation System.. VNS Incorporated - [STC SA01085SE](https://openairdocs.org/stc/SA01085SE): Installation of BAS, Inc. of Shoulder Harness per the appropriate BAS Report listed on FAA AML SA01085SE, dated May 13, 2002, or later FAA approved revision.. BAS Inc - [STC SA01110CH](https://openairdocs.org/stc/SA01110CH): Installation of wing fuel tank quick valve drains.. Storehouse LLC - [STC SA01120SE](https://openairdocs.org/stc/SA01120SE): Installation of Door Steward.. Mountain View Aviation LLC - [STC SA01126WI](https://openairdocs.org/stc/SA01126WI): Replacement of wing tie down ring assembly on Classic Beechcraft model airplanes with one piece machined part number APMA35-115632. DER Associates Ltd. - [STC SA01148WI-D](https://openairdocs.org/stc/SA01148WI-D): Installation of the Bendix/King KI 825 Electronic Horizontal Situation Indicator (EHSI).. Honeywell International Inc All 303: https://openairdocs.org/model/sabre-95/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 (17) As reported by operators and repair stations, by the model named in the report. - [SDR 2023FA0000816](https://openairdocs.org/sdr/2023FA0000816), Nov 17, 2023: ROD END. SEVERED. FORWARD RUDDER TRIM TAB CONTROL ROD END BROKE. UN CONTROLLED RUDDER TAB CAUSED SEVERE OSCILLATIONS RESULTING IN WINDSHIELD SEPARATED FROM THE AIRCRAFT. - [SDR 2021FA0000346](https://openairdocs.org/sdr/2021FA0000346), Nov 28, 2021: NONE. NONE. DURING LANDING TOUCHDOWN RUSSELLVILLE, AR (RUE) THE NOSE LANDING GEAR COLLAPSED. INVESTIGATION REVEALED THE NOSE GEAR RETRACT DRAG BRACE P/N 002-820017-1 AT THE - [SDR 2012FA0000500](https://openairdocs.org/sdr/2012FA0000500), Jul 3, 2012: ROD END. SEPARATED. THE ROD END, PN HMXL6FG, CONNECTED TO GEAR RETRACT ROD, SEPARATED AT THAT CONNECTION CAUSING THE NOSE GEAR TO COLLAPSE DURING THE LANDING ROLL OUT. - [SDR 2010FA0000296](https://openairdocs.org/sdr/2010FA0000296), Apr 7, 2010: LINE. SPLIT. DURING FLIGHT, SHUTDOWN THE RT ENGINE DUE TO OIL LOSS. AN INITIAL ASSESSMENT OF THE CAUSE WAS DUE TO THE ONE OF THE OIL LINE FROM THE OIL COOLER APPEARED TO SPL - [SDR CA061117004](https://openairdocs.org/sdr/CA061117004), Nov 4, 2006: CYLINDER HEAD. CRACKED. (CAN) DURING A ROUTINE 100 HOUR INSPECTION A CRACK WAS FOUND ON THE RH ENGINE #4 CYLINDER STARTING AT THE TOP SPARK PLUG HOLE AND CONTINUING DOWN TO THE EXHAUST - [SDR 2005FA0000089](https://openairdocs.org/sdr/2005FA0000089), Dec 2, 2004: ARMATURE. FAILED. THE GENERATOR WAS JUST O/H, WITHOUT DISASSEMBLING THE GENERATOR, LOOKING IN TO PULLEY SIDE, YOU COULD SEE THAT THE ARMATURE HAD PARTIALLY UNWOUND. TO THE POINT - [SDR CA030506006](https://openairdocs.org/sdr/CA030506006), Mar 14, 2003: WIRE. FAILED. (CAN) THE AME INSTALLED THE COMPONENT (OVERHAULED JAN/02) DURING 2002-2003 WINTER MAINTENANCE. A FUNCTION CHECK OF THE UNIT REVEALED INTERMITTENT INDICATIONS. R - [SDR 2001F00165](https://openairdocs.org/sdr/2001F00165), Jun 27, 2001: ARM. CRACKED. DURING A RECENT INVESTIGATION OF AN INCIDENT OF A BEECH 95 THAT THE NOSE GEAR COLLAPSED ON ROLL OUT AFTER LANDING. IT WAS DISCOVERED THAT THE LANDING GEAR CRANK - [SDR 2001FA0000067](https://openairdocs.org/sdr/2001FA0000067), May 3, 2001: ARM. CRACKED. UPON LANDING ROLL-OUT THE NOSE GEAR COLLAPSED. THE CRACK ON THE SPLINE PORTION OF ARM CAUSED THE ARM TO FLEX AND OPEN CAUSING MATING GEARS TO SEPARATE AND THE N - [SDR 2000ZZZX379](https://openairdocs.org/sdr/2000ZZZX379), Jan 11, 2000: SPRING. BROKEN. LOW OIL PRESSURE DURING FLIGHT CAUSING PROPELLER TO GO TO LOW PITCH AND EVENTUALLY FEATHER. AIRCRAFT LANDED SAFELY AND AFTER TROUBLESHOOTING PROBLEM, FOUND BROK - [SDR AU990914](https://openairdocs.org/sdr/AU990914), Sep 2, 1999: NUT. CRACKED. (AUS) PROPELLER RETENTION NUT CRACKED. EVIDENCE OF CRACK HIGHLIGHTED BY MARKER PEN. SUBMITTER SUSPECTED CRACK HAD BEEN FOUND PREVIOUSLY AND THE UNSERVICEABLE NU - [SDR 99ZZZX1886](https://openairdocs.org/sdr/99ZZZX1886), Apr 10, 1999: SECTOR GEAR. FAILED. DURING ANNUAL INSPECTION GEAR OPERATION, ADJUSTED DOORS TO FIT TIGHTER, AND ACTUATOR SECTOR SHEARED TEETH. ACCORDING TO BEECH SHOP MANUAL AND OWNER'S MANUAL, IF - [SDR 98ZZZX2116](https://openairdocs.org/sdr/98ZZZX2116), May 13, 1998: SKIN. CHAFED. DURING ANNUAL PREPARATIONS, FOUND BEHIND BOTH ENGINES THAT LOWER AFT NACELLES WERE CHAFING THROUGH WING SKIN JUST AFT OF FRONT SPAR FLANGE AND LEFT UNTREATED WO - [SDR 98ZZZX2115](https://openairdocs.org/sdr/98ZZZX2115), May 13, 1998: SKIN. CHAFED. DURING ANNUAL PREPARATIONS, FOUND BEHIND BOTH ENGINES THAT LOWER AFT NACELLES WERE CHAFING THROUGH WING SKIN JUST AFT OF FRONT SPAR FLANGE AND LEFT UNTREATED WO - [SDR 96ZZZX1965](https://openairdocs.org/sdr/96ZZZX1965), Mar 18, 1996: MOUNT. CRACKED. MAIN DYNA FOCAL ATTACH RING TUBE AT TIME OF INSPECTION WAS FOUND TO HAVE CRACKS AT TOP RT ATTACH POINT AND AFT OF ATTACH PLATE APPROXIMATELY .75 INCH AND .50 IN - [SDR CA960509202](https://openairdocs.org/sdr/CA960509202), Mar 8, 1996: RIBS. BENT. (CAN) RIGHT WING RIBS AT W.S. 94.864, 108.281 AND 122.500 FOUND BENT AND BUCKLED UNDER THE UPPER WING SKIN. POSSIBLY CAUSED BY OVERPRESSURE OF FUEL IN AUXILIARY - [SDR 95ZZZX3325](https://openairdocs.org/sdr/95ZZZX3325), Jun 1, 1995: SCREW. BROKEN. DURING DISASEMBLY, INNER CLAMP SCREW FOUND BROKEN OFF ON THE SHANK AT TOP THREAD, ENTERING CLAMP. SURFACE OF BREAK APPEARED CLEAN WITH A SMALL PIT ORIGINATING I ## The same model under other registry codes Amateur-built copies and renamed makers get their own codes. - [Beech 95](https://openairdocs.org/model/beech-95): 95 registered aircraft, registry code 1153402 - [Boeing 95](https://openairdocs.org/model/boeing-95): 0 registered aircraft, registry code 1380095 - [Lark 95](https://openairdocs.org/model/lark-95): 0 registered aircraft, registry code 5160202 --- 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.