# Aero Commander 680FL P

- Type: Aircraft model (FAA registry)
- Registry code: 0141610
- Manufacturer (registry): AERO COMMANDER
- Model: 680FL P
- Aircraft type: Fixed wing multi engine
- Category: Airplane
- Engines: 2 · Reciprocating
- Seats: 11
- Weight class: Up to 12,499 lb
- Cruise speed: 188 mph
- Certification: Type certificated
- Data sheet: [TCDS 2A4](https://openairdocs.org/tcds/2A4) (OpenAirDocs)
- Holder: Twin Commander Aircraft LLC
- Registered aircraft: 5
- Page: https://openairdocs.org/model/aero-commander-680fl-p

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 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 2000-02-30](https://openairdocs.org/ad/2000-02-30): Airframe Pneumatic Deicing Boots · Twin Commander 680, 680-E, 680-F and 15 more. Effective Mar 24, 2000
- [AD 98-20-34](https://openairdocs.org/ad/98-20-34): Airplane Flight Manuals--Severe Icing Conditions · Twin Commander 500, 500-A, 500-B and 24 more. Effective Nov 3, 1998
- [AD 98-14-03](https://openairdocs.org/ad/98-14-03): Transponders · Cessna 172, 172A, 172B and 230 more. Effective Aug 16, 1998
- [AD 98-07-17](https://openairdocs.org/ad/98-07-17): Flap System · Twin Commander 500, 500-A, 500-B and 27 more. Effective May 29, 1998
- [AD 98-08-19](https://openairdocs.org/ad/98-08-19): Wing to Fuselage Attachment Brackets and Straps · Twin Commander 500, 500-A, 500-B and 27 more. Effective May 18, 1998
- [AD 94-04-14](https://openairdocs.org/ad/94-04-14): Spar Cap · Twin Commander 500-S, 500-U, 680-FL(P) and 6 more. Effective Apr 12, 1994
- [AD 94-04-13](https://openairdocs.org/ad/94-04-13): Spar Cap · Twin Commander 500, 500-A, 500-B and 17 more. Effective Apr 12, 1994
- [AD 87-21-07 R1](https://openairdocs.org/ad/87-21-07-R1): Fuel Filler Openings · Twin Commander 500, 500-A, 500-B and 16 more. Effective May 5, 1989
- [AD 79-07-02](https://openairdocs.org/ad/79-07-02): Batteries · Aircraft Parts & Development A, A-2, A-3 and 149 more. Effective Apr 3, 1979
- [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 73-06-02](https://openairdocs.org/ad/73-06-02): Fuel Siphoning · Twin Commander 500, 500-A, 500-B and 13 more. Effective Mar 19, 1973
- [AD 67-26-04](https://openairdocs.org/ad/67-26-04): Altimeters · Bell Helicopter Textron Canada 206A, 150G, 172H (USAF T-41A) and 36 more
- [AD 67-22-01](https://openairdocs.org/ad/67-22-01): Main Landing Gear · Twin Commander 500-A, 500-B, 560-F and 4 more. Effective Aug 28, 1967
- [AD 64-02-01](https://openairdocs.org/ad/64-02-01): Main Landing Gear · Twin Commander 500-A, 500-B, 560-F and 2 more. Effective Feb 20, 1964
- [AD 62-05-01](https://openairdocs.org/ad/62-05-01): Alternate Induction Air Valve · Twin Commander 680-F, 680-FL, 680-FL(P) and 1 more. Effective Mar 6, 1962

Historical (superseded or no longer in force):

- [AD 94-04-17](https://openairdocs.org/ad/94-04-17) (historical): Flap System Cable · Twin Commander 500, 500-A, 500-B and 27 more. Effective Apr 15, 1994

## Information bulletins (advisory) (1)

- [SAIB 2023-14](https://openairdocs.org/saib/2023-14): Landing Gear Retract/Extend System. Issued Nov 14, 2023

## Registered aircraft (5)

- [N102RR](https://openairdocs.org/aircraft/N102RR): [Moyer Aviation Ll C](https://openairdocs.org/faa-owner/MOYER%20AVIATION%20LL%20C), [Katy, TX](https://openairdocs.org/faa-place/TX/Katy), S/N 1477-5
- [N385CG](https://openairdocs.org/aircraft/N385CG): [Owensboro Warehouse Leasing LLC](https://openairdocs.org/faa-owner/OWENSBORO%20WAREHOUSE%20LEASING%20LLC), [Owensboro, KY](https://openairdocs.org/faa-place/KY/Owensboro), built 1965, S/N 1495-14
- [N401MG](https://openairdocs.org/aircraft/N401MG): [Leff William J](https://openairdocs.org/faa-owner/LEFF%20WILLIAM%20J), [Dayton, OH](https://openairdocs.org/faa-place/OH/Dayton), built 1965, S/N 1527-29
- [N411WR](https://openairdocs.org/aircraft/N411WR): [Forbes Greg](https://openairdocs.org/faa-owner/FORBES%20GREG), [Placerville, CA](https://openairdocs.org/faa-place/CA/Placerville), S/N 1505-19
- [N991BD](https://openairdocs.org/aircraft/N991BD): [Afk Corp](https://openairdocs.org/faa-owner/AFK%20CORP), [Ripon, WI](https://openairdocs.org/faa-place/WI/Ripon), S/N 1483-8

## NTSB investigations (8)

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 LAX99FA001](https://openairdocs.org/ntsb/LAX99FA001), Oct 1, 1998: Aero Commander 680 FPL (N5YZ), Palm Springs, CA, destroyed, 1 fatal. Probable cause: The pilot's failure to properly use the manual turbocharger wastegates and to monitor the manifold pressure during takeoff.
- [NTSB CHI98LA105](https://openairdocs.org/ntsb/CHI98LA105), Mar 13, 1998: Aero Commander 680FLP (N777MX), Fond Du Lac, WI, substantial damage. Probable cause: the pilot's misjudged weather evaluation . Factors were turbulence, the pilot's inability to attain a proper climb rate, unsuitable terrain encountered in the landing area, and crops.
- [NTSB LAX89FA307](https://openairdocs.org/ntsb/LAX89FA307), Sep 11, 1989: Aero Commander 680FLP (N22LR), Kailua-Kona, HI, destroyed, 1 fatal. Probable cause: INADEQUATE MAINTENANCE, AND OPERATION BY THE PILOT WITH KNOWN DEFICIENCIES IN THE AIRCRAFT. FACTORS RELATED TO THE ACCIDENT WERE: EXCESSIVE WEAR IN BOTH ENGINES, IMPROPER USE OF POWERPLANT CONTROLS…
- [NTSB FTW89LA077](https://openairdocs.org/ntsb/FTW89LA077), Apr 1, 1989: Gulfstream 680FLP (N721F), Lohn, TX, destroyed. Probable cause: ARSON UNDERTAKEN TO CONCEAL ILLEGAL ACTIVITY.
- [NTSB NYC83FA060](https://openairdocs.org/ntsb/NYC83FA060), Feb 3, 1983: Aero Commander 680FL P (N12LF), Sunbury, PA, destroyed, 2 fatal
- [NTSB ATL81FLG02](https://openairdocs.org/ntsb/ATL81FLG02), Oct 17, 1980: Aero Comdr 680FLP (N1167Z), Columbia, SC, destroyed
- [NTSB LAX80FVD32](https://openairdocs.org/ntsb/LAX80FVD32), Aug 2, 1980: Aero Comdr 680FLP (N27VF), Emeryville, CA, substantial damage
- [NTSB FTW80FA096](https://openairdocs.org/ntsb/FTW80FA096), Jul 25, 1980: Aero Comdr 680FLP (N6515V), Iola, TX, destroyed, 2 fatal

## FAA accident and incident reports (12)

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 20090623047309I](https://openairdocs.org/incident/20090623047309I), Jun 23, 2009: Aero Comman 680FL P (N91ES), Birmingham, AL, No damage. While in cruise flight, lost hydraulic pressure due to a broken line. Landed uneventful with no brakes or steering. The pilot used differintial power to steer…
- [Incident 20070423011959I](https://openairdocs.org/incident/20070423011959I), Apr 23, 2007: Gulstm 680FLP (N385CG), Baton Rouge, LA, No damage. (-23) Aircraft had departed on local VFR flight and was operating under FAR 91 flight rules. Aircraft had recently undergone major maintenance on the left…
- [Accident 19981001027439A](https://openairdocs.org/incident/19981001027439A), Oct 1, 1998: Gulstm STC680 (N5YZ), Palm Springs, CA, Destroyed, 1 fatal. Acft was on a maintence test flight when it reported a fuel problem shortly after takeoff, the acft was attempting to return to the arpt when it struck power…
- [Accident 19980313042069A](https://openairdocs.org/incident/19980313042069A), Mar 13, 1998: Gulstm 680FLP (N777MX), Fond Du Lac, WI, Substantial damage. (.4)The airplane took off on runway 18 with winds reported to be 190 degrees at 14 knots with gusts to 21 knots. The pilot said that during initial climb to…
- [Incident 19961014032159I](https://openairdocs.org/incident/19961014032159I), Oct 14, 1996: Gulstm 680FLP (N662DJ), Las Vegas, NV, Minor damage. Narrative: pilot stated he departed kremling, Colorado approximately 21/2 hours earlier in VFR conditions. Before departure aircraft was completely serviced…
- [Incident 19950701026479I](https://openairdocs.org/incident/19950701026479I), Jul 1, 1995: Gulstm 680FLP (N5YZ), Boulder, CO, Minor damage. During check out in 680 flp nose gear collapsed landing. Had loose steering missing bushing and loose gear.
- [Accident 19890910034089A](https://openairdocs.org/incident/19890910034089A), Sep 10, 1989: Gulstm 680FLP (N22LR), Kailua-Kona, HI, Destroyed, 1 fatal. Smoke from right engine on climbout,lost both returning. Engines had 4790 hours since overhaul. Detonation damage.
- [Accident 19890401005199A](https://openairdocs.org/incident/19890401005199A), Apr 1, 1989: Gulstm 680FLP (N721F), Lohn, TX, Destroyed. Farmer found aircraft destroyed by fire in his field. Indicates illegal activity and destroyed by operators.
- [Accident 19830203002289A](https://openairdocs.org/incident/19830203002289A), Feb 3, 1983: Gulstm 680FLP (N12LF), Sunbury, PA, Destroyed. Pilot proceeded into icing conditions when aircraft was not certified to operate in icing conditions.
- [Accident 19801017057629A](https://openairdocs.org/incident/19801017057629A), Oct 17, 1980: Rkwell 680FLP (N1167Z), West Columbia, SC, Destroyed. Lost engines on long final. Crashed short of runway. Possible fuel misuse. Outboards dry. Engines checked ok.
- [Accident 19800802033179A](https://openairdocs.org/incident/19800802033179A), Aug 2, 1980: Rkwell 680FLP (N27VF), Emeryville, CA, Substantial damage. Engines lost power on climb to cruise. Plane had been fuel with jet a fuel. Required 100 oct gasoline. Laned in bay
- [Accident 19800725030659A](https://openairdocs.org/incident/19800725030659A), Jul 25, 1980: Rkwell 680FLP (N6515V), Iola, TX, Destroyed, 1 fatal. Airplane overloaded with marijuana ran out of fuel. Pilot lost control of airplane, attempting emergency landing.

## Service difficulty reports (4)

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

- [SDR CA091020006](https://openairdocs.org/sdr/CA091020006), Sep 2, 2009: LINE. RUPTURED. (CAN) PILOT DECLARED EMERGENCY UPON DISCOVERING HYD SYS FAILURE AND LANDED. AFTER LANDING, THE PILOT HAD NO CONTROL OF NOSE WHEEL STEERING OR BRAKES AND ACFT VE
- [SDR AUS20031061](https://openairdocs.org/sdr/AUS20031061), Oct 20, 2003: IGNITION LEAD. FAULTY. (AUS) RT ENGINE NR 7 CYLINDER LOWER IGNITION LEAD DEFECTIVE AT SPARK PLUG END.
- [SDR AU971386](https://openairdocs.org/sdr/AU971386), Oct 7, 1997: BLADE. CRACKED. (AUS) PROPELLER BLADE CRACKED. CRACK ORIGINATED FROM A NICK IN THE BLADE LOCATED APPROXIMATELY 76.2MM (3IN) FROM THE BLADE TIP.CRACK LENGTH 12.7MM (0.5IN). SUSP
- [SDR AU960147](https://openairdocs.org/sdr/AU960147), Jan 26, 1996: GASKET. LEAKING. (AUS) ENGINE DRIVEN FUEL PUMP RELIEF VALVE GASKET LEAKING

## STCs that may be installed (OpenAirDocs) (211, 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 SA11300DS](https://openairdocs.org/stc/SA11300DS): Upgrade previously installed Collins Aerospace Radar Altimeter. BHE & Associates Ltd
- [STC SA5581SW](https://openairdocs.org/stc/SA5581SW): Installation of ALCOR true-flow/ totalizer system. Alcor LLC. Lists 680 Series
- [STC SA8408SW](https://openairdocs.org/stc/SA8408SW): Replace the o-ring seals in the landing gear lower strut seal. Metrea Special Aerospace ISR 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 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 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 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 SA497GL](https://openairdocs.org/stc/SA497GL): Install Aircraft Wheel and Brake conversion kit 199-80 (MIL-H-5606 system). Kaman Corporation Aircraft Wheel and Brake LLC
- [STC SA1458GL](https://openairdocs.org/stc/SA1458GL): Installation of a Cleveland nose wheel. Kaman Corporation Aircraft Wheel and Brake LLC
- [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 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 SA02265SE](https://openairdocs.org/stc/SA02265SE): Installation of a camera housing. Airborne Sensor LLC
- [STC SA02075SE](https://openairdocs.org/stc/SA02075SE): Installation of a Mid-Continent MD835( ) Lithium Ion Battery. Mid-Continent Instrument Co. Inc
- [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 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 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 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 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 SA02503AK](https://openairdocs.org/stc/SA02503AK): Installation of AMSAFE State of the Art Restraint System (SOARS) inflatable restraints. AMSAFE 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 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 SA2586NM](https://openairdocs.org/stc/SA2586NM): Installation of J.P. Instruments temperature monitoring systems. J P Instruments
- [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 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 SA1177GL](https://openairdocs.org/stc/SA1177GL): Install Aero Medical Products Mfg., Inc. Air Ambulance Stretcher P/N 125 using Installation Kit P/N 800 in accordance with Installation and Operating Instructions, Form EA 109K, dated April 23, 2001, or later FAA approved revisions. The Medical Oxygen System Kit P/N 807 is an FAA approved option. The Inverter/Pump Kit No. 812 may be installed in accordance with Inverter/Pump Installation Instructions, EA Form 170, dated June 9, 2001, or later FAA approved revisions. Paul/ Lanna Egan LLC

All 211: https://openairdocs.org/model/aero-commander-680fl-p/stcs.md

## The same model under other registry codes

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

- [Aero Commander 680FL](https://openairdocs.org/model/aero-commander-680fl): 10 registered aircraft, registry code 0141608

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