# Woods 65

- Type: Aircraft model (FAA registry)
- Registry code: 0560285
- Manufacturer (registry): WOODS
- Model: 65
- Aircraft type: Rotorcraft
- Category: Rotorcraft
- Engines: 1 · Reciprocating
- Seats: 2
- Weight class: Up to 12,499 lb
- Cruise speed: 86 mph
- Certification: Not type certificated
- Registered aircraft: 0
- Page: https://openairdocs.org/model/woods-65

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 (241, 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 SA00068SE](https://openairdocs.org/stc/SA00068SE): Installation of fuel flow/pressure instruments. (W/TSIO-360-MB1). Electronics International Inc.
- [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 SA00237WI](https://openairdocs.org/stc/SA00237WI): Installation of a Bendix/King EFIS-4 0electronic flight instrument system. Elliott Aviation Technical Products
- [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 SA00622WI](https://openairdocs.org/stc/SA00622WI): Shoulder harness anchor installation. Aviation Fabricators 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 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 SA01085LA](https://openairdocs.org/stc/SA01085LA): Installation of the VNS 1000 Voice Navigation System.. VNS Incorporated
- [STC SA01110CH](https://openairdocs.org/stc/SA01110CH): Installation of wing fuel tank quick valve drains.. Storehouse LLC
- [STC SA01114CH](https://openairdocs.org/stc/SA01114CH): Installation of P2 Incorporated 6600 Audio Advisory system. P2 Incorporated
- [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 SA01146AT](https://openairdocs.org/stc/SA01146AT): Installation of left hand side and right hand side leading edge fuel cell assemblies. (F90 S/N LJ1 AND UP, 99 ALL S/N'S, B100 S/N B1-89 AND UP, 65-B80 S/N LD-151 AND UP). FFC Manufacturing
- [STC SA01157LA](https://openairdocs.org/stc/SA01157LA): Installation of Electronics International Model FP-5 or FP-5L fuel flow/fuel pressure instrument as a replacement instrument.. Electronics International Inc.
- [STC SA01158WI](https://openairdocs.org/stc/SA01158WI): Installation of Aero Enhancements UV250-1 Supplemental Instrument Panel Lightning System.. Aero Enhancements Inc.
- [STC SA01191AT](https://openairdocs.org/stc/SA01191AT): Installation of Left Hand and Right Hand Box Section Inboard Fuel Cell Assemblies. (E90, F90, B100, B200 ALL S/N'S, 65-B80 S/N LC230 AND UP, LD280 AND UP). FFC Manufacturing
- [STC SA01203AT](https://openairdocs.org/stc/SA01203AT): Installation of left-hand side and right-hand side center section fuel cell assemblies.. FFC Manufacturing
- [STC SA01229SE PAGE 2](https://openairdocs.org/stc/SA01229SE%20PAGE%202): Installation of GNS 480 (CNX80) GPS WAAS Navigator with integrated VHF Navigation and Communication radios. Garmin International Inc
- [STC SA01280CH](https://openairdocs.org/stc/SA01280CH): Installation of Challenger Spin-On Oil Filters.(For Cessna 182 model, s/n 67042 and up) (For Cessna 421C model, s/n 1017 thru 1404). D & K Aviation
- [STC SA01335AT-D](https://openairdocs.org/stc/SA01335AT-D): Installation of replacement fuel cell assemblies. FFC Manufacturing
- [STC SA01452CH](https://openairdocs.org/stc/SA01452CH): Installation of an air ambulance conversion kit.. Med-Pac Inc.
- [STC SA01473SE (5 OF 5)](https://openairdocs.org/stc/SA01473SE%20(5%20OF%205)): Installation of a GTX 32 (mode C), GTX 33 (mode S), or GTX 33D (mode S with diversity) Remote Transponde. Garmin AT Inc.
- [STC SA01487SE (4 OF 5)](https://openairdocs.org/stc/SA01487SE%20(4%20OF%205)): Installation of a GDL 69 or GDL 69A XM Satellite Receiver in accordance with Garmin Supplemental Type Certificate Master Data List, P/N 005-C0217-00, Revision A, dated December 20, 2004, or later FAA approved revision.. Garmin AT Inc.
- [STC SA01487SE-D](https://openairdocs.org/stc/SA01487SE-D): Installation of a GDL 69 or GDL 69A XM Satellite Receiver. Garmin International Inc
- [STC SA01625AT-D](https://openairdocs.org/stc/SA01625AT-D): Installation of replacement fuel cell assemblies. FFC Manufacturing
- [STC SA01626AT-D](https://openairdocs.org/stc/SA01626AT-D): Installation of replacement fuel cell assemblies. FFC Manufacturing
- [STC SA01639NY](https://openairdocs.org/stc/SA01639NY): Replacement of 12 refrigerant in air conditioning system with Enviro Refrigerant Hotshot R414B.. Scale Modelbuilders Inc.
- [STC SA01692SE  (PAGE 1 OF 2)](https://openairdocs.org/stc/SA01692SE%20%20(PAGE%201%20OF%202)): Installation of a Garmin GMX 200 Multi-Function Display. Garmin International Inc
- [STC SA01695SE (5 OF 5)](https://openairdocs.org/stc/SA01695SE%20(5%20OF%205)): Installation of an antenna. Garmin AT Inc.
- [STC SA01714WI (2 OF 2)](https://openairdocs.org/stc/SA01714WI%20(2%20OF%202)): 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 SA01800SE](https://openairdocs.org/stc/SA01800SE): Fabrication and installation of new or replacement of  existing instrument panel lights dimmer control.. TCW Technologies, LLC
- [STC SA01809WI](https://openairdocs.org/stc/SA01809WI): Installation of an Operator Seat onto an existing Cabin Seat Track.. Aviation Fabricators Inc
- [STC SA01814AT-D](https://openairdocs.org/stc/SA01814AT-D): Modification of Nose Gear Doors. Summit Aviation Inc.
- [STC SA01828SE](https://openairdocs.org/stc/SA01828SE): Installation of J.P. Instruments (JPI) EDM-960 Primary Engine Data Management System. J. P. Instruments
- [STC SA01835WI](https://openairdocs.org/stc/SA01835WI): Installation of Trig Avionics TY-96 or TY-97 VHF Communications Radio. Peregrine
- [STC SA01860NY (2 OF 3)](https://openairdocs.org/stc/SA01860NY%20(2%20OF%203)): Installation of Graphic Engine Monitors (GEM) Models GEM-610 and GEMINI 1200.. Insight Instrument Corporation
- [STC SA01861SE](https://openairdocs.org/stc/SA01861SE): Fabrication and installation of Landing Light Controller. TCW Technologies, LLC

All 241: https://openairdocs.org/model/woods-65/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 (20)

As reported by operators and repair stations, by the model named in the report.

- [SDR 2023F00235](https://openairdocs.org/sdr/2023F00235), Jul 18, 2023: BRAKE SYS. INTERMITTENT. WHILE TAXIING OUT TO RUNWAY, PILOT REPORTED LEFT HAND BRAKES OUT / INTERMITTENT. THE PILOT TAXIED BACK TO THE RAMP, SHUT DOWN AND REPORTED THE INCIDENT TO MAINT
- [SDR 2023F00234](https://openairdocs.org/sdr/2023F00234), Jul 17, 2023: BRAKE SYS. INTERMITTENT. WHILE TAXIING OUT TO RUNWAY, PILOT REPORTED LEFT BRAKE SOFT. THE PILOT TAXIED BACK TO THE RAMP, SHUT DOWN AND REPORTED THE INCIDENT TO MAINTENANCE AND OPERATION
- [SDR BEMA202009230001](https://openairdocs.org/sdr/BEMA202009230001), Aug 24, 2020: ALTERNATOR. BROKEN. RT ENGINE ALTERNATOR POWER SUPPLY STUD BROKE OFF RECTIFIER PLATE, AT THE PLATES 90 DEGREE BEND NEXT TO MADE IN CHINA STICKER. LOOKED LIKE CRACK STARTED FROM STR
- [SDR 2019FA0000313](https://openairdocs.org/sdr/2019FA0000313), Sep 13, 2019: CLEVIS. BROKEN. INVESTIGATION REVEALED A BROKEN CLEVIS ON THE NOSE GEAR ACTUATOR. DURING THE GEAR CYCLE, THE BROKEN END OF THE ACTUATOR ROTATED DOWN WHILE THE NOSE GEAR SWUNG F
- [SDR BEMA20120628002](https://openairdocs.org/sdr/BEMA20120628002), Jun 25, 2012: LIMIT SWITCH. OUT OF RIG. LANDING GEAR LIMIT SWITCH FAILED TO STOP MOTOR DURING RETRACTION CAUSING LANDING GEAR CIRCUIT BREAKER TO POP. PILOT CHOSE TO MANUALLY EXTEND THE GEAR AND LAND W
- [SDR 2008F00014](https://openairdocs.org/sdr/2008F00014), Apr 28, 2008: CLEVIS BOLT. CORRODED. NO NOSE GEAR DOWNLOCK INDICATION CAUSED BY THE SEIZURE OF DOWNLOCK HOOK BOLT.
- [SDR BEM2004F00000](https://openairdocs.org/sdr/BEM2004F00000), Jul 8, 2004: BEARING. FAILED. NR 1 ALTERNATOR WENT INOPERATIVE IN FLIGHT INVESTIGATION FOUND REAR ROTOR BEARING OF ALTERNATOR HAD NO GREASE AND FAILED.
- [SDR KZ52003F00002](https://openairdocs.org/sdr/KZ52003F00002), Oct 13, 2003: STIFFENER. CRACKED. INSPECTION REVELAED THE PARTS TO BE CRACKED BETWEEN RIVET HOLES WHERE STIFFENER WAS ATTACHED TO AFT BULKHEAD. NO FURTHER DAMAGE WAS NOTED AFTER PART WAS REMOVED
- [SDR KZ52003F00000](https://openairdocs.org/sdr/KZ52003F00000), Oct 8, 2003: STIFFENER. CRACKED. INSPECTION REVEALED THE PART TO BE CRACKED BETWEEN RIVET HOLES WHERE STIFFNER WAS ATTACHED TO AFT BULKHEAD. NO FURTHER DAMAGE WAS NOTED AFTER PART WAS REMOVED.(
- [SDR KZ52003F00001](https://openairdocs.org/sdr/KZ52003F00001), Oct 2, 2003: STIFFENER. CRACKED. INSPECTION REVEALED THE PARTS TO BE CRACKED BETWEEN RIVET HOLES WHERE STIFFENER WAS ATTACHED TO AFT BULKHEAD. NO FURTHER DAMAGE WAS NOTED AFTER PART WAS REMOVED
- [SDR KZ52002F00002](https://openairdocs.org/sdr/KZ52002F00002), Aug 28, 2002: SERVO. FAILED. PILOT REPORTED RT ENGINE TO BE LOW ON POWER, FOUND ENGINE TO BE RUNNING VERY RICH, WHICH CAUSED PLUGS TO FOUL, INSTALLED OVERHAULED FUEL SERVO AND CLEANED PLUGS
- [SDR KZ52002F00001](https://openairdocs.org/sdr/KZ52002F00001), Aug 15, 2002: GEAR. BROKEN. A NEW STARTER NEEDS TO BE DESIGNED. ENGINE DID NOT KICK BACK DURING START.
- [SDR 99ZZZX1934](https://openairdocs.org/sdr/99ZZZX1934), Apr 13, 1999: ADAPTER. CRACKED. OIL LEAK WAS FOUND AT THE REAR OF ENGINE. AFTER INSPECTION, AN OBVIOUS CRACK WAS SEEN ON ADAPTER FLANGE. ADAPTER FLANGE SHOULD BE REINFORCED TO PREVENT FAILURE 
- [SDR 99ZZZX1567](https://openairdocs.org/sdr/99ZZZX1567), Mar 26, 1999: DRIVE. LOOSE. DRIVE TEETH CAME LOOSE ON STARTER.
- [SDR 99ZZZX1006](https://openairdocs.org/sdr/99ZZZX1006), Feb 1, 1999: RIVETS. LOOSE. ALL RIVETS HOLDING TORQUE TUBE, PN 50-630000-126, TO FITTING, PN 50-600016, AND FITTING, PN 50-600017, HAVE SHEARED OFF. UNKNOWN REASONS. UNDER NORMAL USE CONDI
- [SDR 99ZZZX1007](https://openairdocs.org/sdr/99ZZZX1007), Dec 2, 1998: ADAPTER. CRACKED. WHILE INSPECTING ENGINE, LEAK WAS FOUND COMING FROM REAR. AFTER CLOSER INSPECTING, SUSPECTED CRACK WAS FOUND AND ADAPTER WAS REMOVED FOR POSITIVE VERIFICATION. 
- [SDR 98ZZZX1581](https://openairdocs.org/sdr/98ZZZX1581), Apr 13, 1998: BOLT. CORRODED. IN C/W AD 85-22-05, WING BOLT REJECTED DUE TO MINUTE GALLING CORROSION SPOT IN THE INNER RADIUS. BOLT REMOVED FROM THE LT LOWER FORWARD OUTER WING PANEL ATTACHM
- [SDR 98ZZZX710](https://openairdocs.org/sdr/98ZZZX710), Jan 30, 1998: VALVE ASSY. FAILED. A NEW OIL TEMP CONTROL VALVE WAS USED FOR ENGINE OVERHAUL PN 5E19600. ENGINE OIL TEMP FOR FIRST 100 HRS TIS WAS NORMAL. THE NEXT 31.2 HRS TIS, OIL TEMP INCREASE
- [SDR AU960278](https://openairdocs.org/sdr/AU960278), Feb 6, 1996: FUEL TANK. LEAKING. (AUS) LH WING INBOARD FUEL TANK DETERIORATED AND LEAKING - THE TANK WAS REMOVED AND FOUND TO BE SEALED EXTERNALLY IN NUMEROUS PLACES WITHPR1422 COMPOUND - 2 BUT
- [SDR 95ZZZX2616](https://openairdocs.org/sdr/95ZZZX2616), May 15, 1995: ACTUATOR. JAMMED. UPON TEAR-DOWN INSPECTION OF LT MLG ACTUATOR, THE FOLLOWING ITEMS WERE NOTED: 1. TOTAL ACTUATOR EXTENSION WAS 8 INCHES COMPARED TO TOTAL EXTENSION ON THE GOOD R

## The same model under other registry codes

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

- [Beech 65](https://openairdocs.org/model/beech-65): 22 registered aircraft, registry code 1152802
- [Beech 65 (LF-23F)](https://openairdocs.org/model/beech-65-lf-23f): 6 registered aircraft, registry code 1152804
- [Beech 65 (L23F)](https://openairdocs.org/model/beech-65-l23f): 1 registered aircraft, registry code 1152798
- [Rockwell International 65](https://openairdocs.org/model/rockwell-international-65): 1 registered aircraft, registry code 7630704

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