# Beech 65 (L23F) - Type: Aircraft model (FAA registry) - Registry code: 1152798 - Manufacturer (registry): BEECH - Model: 65 (L23F) - Aircraft type: Fixed wing multi engine - Category: Airplane - Engines: 2 · Reciprocating - Seats: 9 - Weight class: Up to 12,499 lb - Certification: Type certificated - Data sheet: [TCDS 3A20](https://openairdocs.org/tcds/3A20) (OpenAirDocs) - Holder: Textron Aviation Inc. - Registered aircraft: 1 - Page: https://openairdocs.org/model/beech-65-l23f 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 2023-10-02](https://openairdocs.org/ad/2023-10-02): Indicating/Recording System, Navigation · Boeing 18, 23, 35 and 1,060 more. Effective May 26, 2023 - [AD 2005-18-20](https://openairdocs.org/ad/2005-18-20): "FASTprop" propeller de-icers · Hartzell PHC-C3YF-1RF/F8468A(B,K)-8R constant speed propeller (STC SA00718LA or 17 others). Effective Oct 14, 2005 - [AD 2005-01-19](https://openairdocs.org/ad/2005-01-19): Mode S transponders · GARMIN International GTX 330D, GTX 330, GTX 33D and 830 more. Effective Feb 23, 2005 - [AD 99-05-13 R1 WD](https://openairdocs.org/ad/99-05-13-R1-WD): Withdrawal of AD 99-05-13 · Beech B17B, B17L, B17R (Army UC-43H) and 107 more. Effective Jul 5, 2000 - [AD 95-26-15 R1](https://openairdocs.org/ad/95-26-15-R1): Traffic Alert and Collision Avoidance Systems · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 159 more. Effective Dec 26, 1996 - [AD 95-20-01 R1](https://openairdocs.org/ad/95-20-01-R1): Placard - Cabin Door · Textron 65. Effective Nov 3, 1995 - [AD 89-25-08](https://openairdocs.org/ad/89-25-08): Wing Main Spar Inspection · Textron 65, 65-80, 65-A80 and 1 more. Effective Jan 4, 1990 - [AD 88-04-07](https://openairdocs.org/ad/88-04-07): Wing Spar Nuts Inspection · Textron 100, 65, 65-80 and 18 more. Effective Apr 18, 1988 - [AD 85-22-05](https://openairdocs.org/ad/85-22-05): Nuts and Bolts Replacement · Textron 100, 200, 200C and 60 more. Effective Nov 12, 1985 - [AD 81-23-01 R1](https://openairdocs.org/ad/81-23-01-R1): Beech Kit or Supplemental Type Certificate · Textron 100, 65, 65-88 and 20 more. Effective Jan 4, 1982 - [AD 79-01-02 R2](https://openairdocs.org/ad/79-01-02-R2): In-Flight Fires · Textron 65, 65-80, 65-88 and 17 more. Effective Sep 22, 1980 - [AD 79-16-01](https://openairdocs.org/ad/79-16-01): Wing Structure · Textron 65, 65-80, 65-90 and 2 more. Effective Aug 6, 1979 - [AD 78-11-01](https://openairdocs.org/ad/78-11-01): Powerplant Fires · Textron 65, 65-80, 65-88 and 11 more. Effective Feb 6, 1979 - [AD 78-22-05](https://openairdocs.org/ad/78-22-05): Elevator Control Push Rods · Textron 100, 50, 65 and 31 more. Effective Nov 6, 1978 - [AD 77-22-01](https://openairdocs.org/ad/77-22-01): Fuselage Structure · Textron 65, 65-80, 65-88 and 11 more. Effective Aug 23, 1978 - [AD 78-05-06](https://openairdocs.org/ad/78-05-06): Flexible Fuel Cells · Cessna 180, 182, 185 and 98 more. Effective Jun 30, 1978 - [AD 76-09-01](https://openairdocs.org/ad/76-09-01): Emergency Exit Door · Textron 65, 65-80, 65-A80 and 5 more. Effective Apr 30, 1976 - [AD 62-08-03](https://openairdocs.org/ad/62-08-03): Control Wheels · Textron 35, 35-33, 35-A33 and 33 more. Effective Jul 9, 1970 - [AD 66-02-01](https://openairdocs.org/ad/66-02-01): Air Conditioners · Beechcraft 56TC, 58, 58A and 39 more. Effective Feb 10, 1966 - [AD 64-24-02](https://openairdocs.org/ad/64-24-02): Wing Attach Bolts · Textron 65, D50E and J50. Effective Nov 20, 1964 Historical (superseded or no longer in force): - [AD 99-05-13](https://openairdocs.org/ad/99-05-13) (historical): Fuel Tank Selector · Beech B17B, B17L, B17R (Army UC-43H) and 107 more. Effective Apr 19, 1999 - [AD 87-22-01 R1](https://openairdocs.org/ad/87-22-01-R1) (historical): Nose Landing Gear Fork · Raytheon 100 Model or Series (all), 1900, 1900C and 50 more. Effective Sep 30, 1989 ## Information bulletins (advisory) (6) - [SAIB CE-10-34R2](https://openairdocs.org/saib/CE-10-34R2): Alternative Methods of Compliance (AMOC) to Airworthiness Directive (AD) 89-25-10 and 89-25-08. Issued Aug 30, 2013 - [SAIB CE-10-34R1](https://openairdocs.org/saib/CE-10-34R1) (historical): Alternative Methods of Compliance (AMOC) to Airworthiness Directive (AD) 89-25-10 and 89-25-08. Issued Aug 20, 2013 - [SAIB CE-12-36](https://openairdocs.org/saib/CE-12-36): Flight Controls: Aileron. Issued Jun 19, 2012 - [SAIB CE-11-04](https://openairdocs.org/saib/CE-11-04): Wings Wing Spar. Issued Dec 2, 2010 - [SAIB CE-10-34](https://openairdocs.org/saib/CE-10-34) (historical): Alternative Methods of Compliance (AMOC) to Airworthiness Directive (AD) 89-25-10 and AD 89-25-08. Issued May 18, 2010 - [SAIB CE-02-19](https://openairdocs.org/saib/CE-02-19): . Issued Mar 11, 2002 ## Registered aircraft (1) - [N41HW](https://openairdocs.org/aircraft/N41HW): [Fresh Air Aviation Inc](https://openairdocs.org/faa-owner/FRESH%20AIR%20AVIATION%20INC), [Charlevoix, MI](https://openairdocs.org/faa-place/MI/Charlevoix), S/N LF73 ## 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 ## STCs that may be installed (OpenAirDocs) (230, first 50) 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 SA02571SE](https://openairdocs.org/stc/SA02571SE): Installation of Garmin G500/G600 TXi Integrated Avionics System (Primary Flight Display, Multi-Function Display, and Engine Indicating System Display). 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 SA01861SE](https://openairdocs.org/stc/SA01861SE): Fabrication and installation of Landing Light Controller. TCW Technologies, LLC - [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 SA800EA](https://openairdocs.org/stc/SA800EA): Installation of Whelen Anti-Collision, Position, or Anti-Collision/Position Light System, and applicable associated power supplies. Whelen Aerospace Technologies - [STC SA02511SE](https://openairdocs.org/stc/SA02511SE): Installation of replacement fuel quantity indicator sending unit(s). CiES Inc - [STC SA11158SC](https://openairdocs.org/stc/SA11158SC): Demonstration of aircraft tolerance to potential electromagnetic interference from certain Transmitting Potable Electronic Devices (T-PEDS). Liberty Partners Inc - [STC SA02738CH](https://openairdocs.org/stc/SA02738CH): Installation of L-3 Communications Avionics Systems. Acron Aviation Inc - [STC SA04046CH PAGE 1](https://openairdocs.org/stc/SA04046CH%20PAGE%201): Installation of L-3 GENESIS (TM) Electronic Standby Instrument System (ESI-500/MAG-500). Acron Aviation Inc - [STC SA378CH](https://openairdocs.org/stc/SA378CH): Installation of TCAS I. Acron Aviation Inc - [STC SA09887AC](https://openairdocs.org/stc/SA09887AC): Installation of an Avionica MK-III mini Quick Access Recorder (QAR) and optional 4G or LTE Avionica Cellular Module (avCM. Aircraft Systems and Manufacturing Inc - [STC SA02386AK](https://openairdocs.org/stc/SA02386AK): Replacement of existing landing and/or taxi light reflector and bulbs with Light Emitting Diode (LED) lighting systems. AeroLED's Holding LLC - [STC SA02658SE](https://openairdocs.org/stc/SA02658SE): Installation of Garmin GI 275 Multi-Function Display System. Garmin International Inc - [STC SA02532AT](https://openairdocs.org/stc/SA02532AT): Installation of subject Michelin tires on appropriate aircraft. For Michelin 5, 6, 8, and 10-inch rim diameter tires on General Aviation Aircraft. Michelin North America Inc - [STC SA02014WI](https://openairdocs.org/stc/SA02014WI): Installation of a swept vertical stabilizer and rudder assembly. Bemidji Aviation Services, Inc - [STC SA01814AT-D](https://openairdocs.org/stc/SA01814AT-D): Modification of Nose Gear Doors. Summit Aviation 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 SA02010WI](https://openairdocs.org/stc/SA02010WI): Installation of the Mid-Continent Instruments & Avionics MD23 FLEX Custom Function Display (CFD). Mid-Continent Instruments and Avionics - [STC SA1686WE](https://openairdocs.org/stc/SA1686WE): Installation of Vibration Isolation Products (VIP) engine mount P/Ns VIP 50525-1 and VIP 50545-1 on various aircraft as shown on FAA Approved Model List (AML) No. SA1686WE. FTG, Inc - [STC SA1077GL](https://openairdocs.org/stc/SA1077GL): Replace existing nose wheel with Cleveland nose wheel P/N 40-204. KAMAN Corporation Aircraft Wheel and Brake LLC - [STC SA673GL](https://openairdocs.org/stc/SA673GL): Install wheels and brakes according to Parker Hannifin 'Installation Instructions' for 199-123. Kaman Corporation Aircraft Wheel and Brake LLC1160 Center Road, Avon, OH 44011 - [STC SA01967WI](https://openairdocs.org/stc/SA01967WI): Use of GAMI G100UL High Octane Unleaded Avgas. General Aviation Modifications Inc - [STC SA02203AK](https://openairdocs.org/stc/SA02203AK): Installation of FlightLogic Synthetic Vision Electronic Flight Information System (EFIS-SV). Genesys Aerosystems Inc - [STC SA02254AK](https://openairdocs.org/stc/SA02254AK): Installation of "Single Screen", "2 or 3 Screen", "Dual Screen", or "4 or 6 screen". Genesys Aerosystems 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 1](https://openairdocs.org/stc/SA11174SC%20PAGE%201): Installation of BendixKing by Honeywell KSN 770 and KSN 765 WAAS LPV approach capable nav/comm systems. Honeywell International Inc (Bendix King) - [STC SA02265SE](https://openairdocs.org/stc/SA02265SE): Installation of a camera housing. Airborne Sensor LLC - [STC SA02430SE](https://openairdocs.org/stc/SA02430SE): Fabrication and installation of a camera housing. Airborne Sensor LLC - [STC SA04062NY](https://openairdocs.org/stc/SA04062NY): Installation of Garmin G600 Avionics System. airplus engineering GmbH - [STC SA10236SC](https://openairdocs.org/stc/SA10236SC): Installation of a GDC 31 Roll Steering Converter. DAC International Inc - [STC SA02268CH](https://openairdocs.org/stc/SA02268CH): Installation of Airwolf Filter Corp. Air Oil Separator. Airwolf Filter Corporation - [STC SA2326CE-D](https://openairdocs.org/stc/SA2326CE-D): Installation of the Bendix/King KLN 88 LORAN C system. Honeywell International Inc - [STC SA1562CE-D](https://openairdocs.org/stc/SA1562CE-D): Install King KFC 200 flight control system, two or three axis, with flight director and with optional KAS 297 altitude selector. Honeywell International Inc - [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 1](https://openairdocs.org/stc/SA00344BO%20PAGE%201): Installation of Parmetheus Plus LED PAR36 and PAR46 taxi and landing lights. Whelen Aerospace Technologies - [STC SA615EA](https://openairdocs.org/stc/SA615EA): Installation of a Whelen Anti-Collision Strobe Light System as replacement for originally installed anti-collision lights. Whelen Aerospace Technologies - [STC SA159CH](https://openairdocs.org/stc/SA159CH): Convert left- or right-side cockpit window into a crew door and disconnect pressurization system. Resource Aircraft Conversions - [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 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 SA04165NY](https://openairdocs.org/stc/SA04165NY): Installation of Latitude Technologies Skynode S200 Satcom system must be performed. Latitude Technologies Corporation - [STC SA02153LA-D PAGE 1](https://openairdocs.org/stc/SA02153LA-D%20PAGE%201): Installation of Garmin G600 Primary Flight Display (PFD) and Multifunction Display (MFD) System. Garmin International Inc - [STC SA02013CH](https://openairdocs.org/stc/SA02013CH): Installation of Avidyne Corporation Traffic Advisory System (TAS). Avidyne Corporation - [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 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 SA01933LA-D](https://openairdocs.org/stc/SA01933LA-D): Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System. Garmin International Inc - [STC SA2586NM](https://openairdocs.org/stc/SA2586NM): Installation of J.P. Instruments temperature monitoring systems. J P Instruments All 230: https://openairdocs.org/model/beech-65-l23f/stcs.md ## 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 - [Rockwell International 65](https://openairdocs.org/model/rockwell-international-65): 1 registered aircraft, registry code 7630704 - [Woods 65](https://openairdocs.org/model/woods-65): 0 registered aircraft, registry code 0560285 --- 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.