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Barrymountstm for General Aviation

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Barrymountstm for General Aviation Popular Name Model # Per Engine Barry P/N Popular Name Model # Per Engine Barry P/N Popular Name Model # Per Engine Barry P/N Popular Name Model # Per Engine Barry P/N TM AEROSTAR A/C BRITISH AEROSPACE Continued CESSNA Continued CESSNA Continued BarryMounts for General Aviation Aerostar 600 PA-60-600 4 94011-01 Skyknight 320-1 4 94016-03 Cessna Citation S/II S550 1+1+1, 96026-02, -03, -04 Maintenance and Inspection of Engine Mounts Aerostar 601 PA-60-601 4 94011-01 Jetstream 3101 Jetstream 3201 93438-2 320A 4 94016-03 Cessna T182 4 94011-02 Dirt and hydrocarbons should be (as visi - Any circumstance not identified Aerostar 601P PA-60-601P 4 94011-01 Tuned Damper Jetstream 4101 96000-5, -6 320B 4 94016-03 *Yates Aircraft Conv. T188C 4 94007-01 Ī Inspect the metal washers Ī Aerostar 602P PA-60-602P 4 94011-01 removed by wiping with a clean rag. ble) for corrosion or damage such as above that would indicate the C.A.S.A. Skyknight 320C 4 94016-03 *Yates Aircraft Conv. T188C 4 94110-02 Soap and water or isopropyl alcohol *Aerostar 700P PA-60-700P 4 94011-40 Skyknight 320D 4 94006-01 Alt: 94017-01 Turbo Skywagon T207 2+2 94030-01, +94031-01 nicks, dings, etc. Minor damage can airworthiness of the isolator(s) may Aviocar (212-100) C-212-CB 93266 System can be used, but any other solvents AIR ILLINOIS Executive Skynight 320E,F 4 94006-01 Alt: 94017-01 Skywagon/Stationair T207A 2+2 94030-01, +94031-01 be blended out by hand, as long as have been compromised (age Aviocar (212-200) C-212-CC, -CD, 93396 System should not be used as they can *Jetstream Conv. HP 137 Mk 1 3 93880-6 -CE, -CF, -DF 335 4 94006-01 T210F-H 2+1+1 94030-01, +94031-01, +-02 depth of rework does not exceed weathering, deterioration, etc.). * C-295 96049-1 System damage the elastomer or the elas - AIR PLAINS Skymaster 336 4 94016-01 T210J 2+1+1 94030-01, +94031-01, +-02 10% of material thickness. Removed isolators should be Super Skymaster 337 4 94017-01 Turbo Centurian T210K-L 2+1+1 94030-01, +94031-01, +-02 tomer-to-metal bond. Any lubricants *180HP Conv. 172B-P 4 94011-20 CESSNA Super Skymaster 337A USAF 02B 4 94017-01 T210M 2+1+1 94030-01, +94031-01, +-02 or solvents spilled onto the isolators Ī Check structure around engine (such inspected to the same criteria as *172B-P 180 HP Conv. 172B-P 4 94011-20 152 4 94150-40 as the cowling, prop spinner) for installed mounts. The areas not nor - 172I, K-L 4 94011-20 337B 4 94017-01 Turbo Centurion T210N 2+1+1 94030-01, +94031-01, +-02 should be removed from the isolators AIR TRACTOR Skyhawk 172M 4 94011-20 337C,D 4 94017-01 Crusader T303 4 94011-02 as soon as possible. signs of damage caused by exces - mally visible when the isolators are AT-302 4 5906-13SA2 Skyhawk 172N 4 94011-20 Super Skymaster 337E 4 94017-01 T310P, Q 4 94006-01 sive drift of the engine. If damage is installed will now be available for in - AT-400 3 5906-2SA1 Skyhawk 172P 4 94011-20 Super Skymaster 337F 4 94017-01 T310R 4 94006-01 Inspection of Installed Mounts found, investigate cause. Excessive spection also. Two additional checks AT-400A 3 5906-2SA1 Skylark 175 4 94110-40 337G 4 94017-01 T337B 4 94017-01 drift can be caused by a too-soft of the molded assemblies should AT-402 3 5906-2SA5 During annual or 100-hour inspection Skylark 175A,B 4 94110-40 337H 4 94017-01 T337C, D 4 94017-01 isolator, delamination, or by elas - also be performed. AT-402A 3 5906-2SA5 of an aircraft or scheduled inspections Skylark 175C 4 94110-40 340 4 94006-01 T337E, F 4 94017-01 tomer creep that occurs over time. AT-502 4 5906-2SA5 Cardinal 177 4 94011-20 340A 4 94006-01 T337H 4 94017-01 of an aircraft’s engine(s), the engine Ī Check the free height of the molded AT-502A 4 93880-13 Cardinal 177A 4 94011-20 401 4 94006-01 TP206A, B 2+2 94030-01, +94031-01 mounts should be inspected. The If any of the above conditions are assembly. This dimension should AT-502B 4 5906-2SA5 Cardinal Classic 177B 4 94011-20 401A,B 4 94006-01 TP206C, D, E 2+2 94030-01, +94031-01 inspection can be accomplished with noted, the isolators should be only be measured with the molded AT-503 4 93880-13 Skywagon 180 4 94110-40 402 4 94006-01 CessnaTurbo Skylane RG TR182 4 94011-02 the isolators mounted on the aircraft removed, disassembled, inspected, assembly is in an unrestrained (off AT-503A 4 5906-2SA5 Skywagon 180A 4 94110-40 402A, B 4 94006-01 TU206A, B 2+2 94030-01, +94031-01 and repaired or replaced. the aircraft) condition. The minimum AT-602 4 96078-01 and the isolators supporting the Skywagon 180B 4 94110-40 Business Liner, Utililiner 402C 4 94006-01 TU206C, D, E, F 2+2 94030-01, +94031-01 dimension is equal to 90% of the AT-802 4 96078-01 weight of the engine. The criteria for 180C, D, E, F 4 94110-40 Titan 404 4 94001-01 TU206G 2+2 94030-01, +94031-01 AT-802A 4 96078-01 inspection include: Bench Inspection of Mounts free height of a new molded 180G 4 94110-40 411 4 94001-01 Super Skywagon U206 2+2 94030-01, +94031-01 assembly. ALLIANCE Skywagon 180H 4 94110-40 411A 4 94001-01 U206A 2+2 94030-01, +94031-01 Ī Condition of the elastomer: The Engine vibration isolators should be Courier H-250 4 94011-02 Skylane 182 4 94110-40 U206B 2+2 94030-01, +94031-01 elastomer should be free of dam - removed and inspected under the Ī Checking the eccentricity. This di - Courier H-295 USAF U10D 4 94110-40 Skylane 182A-D 4 94110-40 Golden Eagle 421B 4 94001-01 U206C, D, E, F 2+2 94030-01, +94031-01 age, cracking, or other deterioration. following circumstances: mension should only be measured Courier H-395 USAF L-28A 4 94110-40 Skylane 182E-G 4 94110-40 Golden Eagle 421C 4 94001-01 U206G 2+2 94030-01, +94031-01 with the molded assembly off the or U-10B Skylane 182H, J-M 4 94110-40 Corsair or Conquest I 425 6+3 00-13849-01, 00-13854-01 CIRRUS Ī Integrity of the metal-to-elastomer Ī When an engine is removed for aircraft. The maximum eccentricity Courier HT-295 4 94110-40 Skylane 182N, P 4 94110-40 Conquest 441 6+2+1+1 00-13849-01, 00-13851-01 SR20 4 96355-01 bond: The elastomer should remain overhaul. 00-13850-01, 85-9342-01 of a molded assembly is equal to ALLIED AG-CAT Skylane 182Q 4 94110-40 SR22 6 96301-01 bonded to the metal washers. Fail - Citation & Citation 1 500 2+1 96026-01, -02 Ī When sudden stoppage of the 3% of the outside diameter. G-164-34T 3 5906-2SA1 *SMA Engine Conv. 182Q, 182R 4 96150-01 Citation 501 2+1 96026-01, -02 COMMANDER ure of the bond can cause excessive propeller or engine occurs. G-164B-15T 3 5906-2SA1 182R 4 94110-40 Citation II 550 1+1+1 96026-03, -04, -05 112 2+2 94011-02, -20 drift of the powerplant. If delamina - Skywagon 185 4 94110-40 ATLANTIC AERO, INC. Citation II 551 1+1+1 96026-03, -04, -05 112B 2+2 94011-02, -20 tion is suspected, it can be investi - Ī When the nacelle engine bay has Skywagon 185A-E 4 94110-40 *Smooth Ride System 206, 207, & 210 4+2 94030-01, 94030-03 *Citation VI 650 1+1+1+1 93326-09, -10, -11, -12 112TC 2+2 94011-02, -20 gated by probing with a blunt-edged been exposed to excessive heat Cessna 206, 207, 210 AgWagon 230 188 4 94110-40 *Citation VII 650 1+1+1+1 93326-09, -10, -11, -12 112TCA 2+2 94011-02, -20 instrument. If more than 30% of (i.e. engine fire). AVIAT Super SkyWagon 206 2+2 94030-01, +94031-01 S/N 650-7001 - 7067 Barry Controls Aerospace SkyWagon 207 2+2 94030-01, +94031-01 DORNIER LUFTFAHRT the edge of a bonded interface is Ī When excessive vibration is *Husky A-1A 4 94150-02 *Citation III 650 1+1+1+1 93326-09, -10,-11,-12 SkyWagon/Stationair 207A 2+2 94030-01, +94031-01 Skyservant 228-100,-200,-212 93469 System debonded over ¼” in depth, the experienced or reported. *Husky Pup A-1B 4 94150-02 Aerobat A152 4 94150-40 a unit of Caravan I 208, 208A-B 6+3 00-13849-01, 00-13855-01 ECLIPSE AVIATION Hutchinson Aerospace isolator should be replaced. *Husky A-1B 4 94150-02 Skywagon/AGCarryall A185F 4 94110-40 210, 210A 4 94110-40 *Eclipse 500 500 2+1 96133-01, 96133-02 * S-2B 8 96005-1 Ag Wagon 300 A188 4 94110-40 210-5 (205) 4 94110-40 S-2C 8 96005-1 *Yates Aircraft Conv. A188A 4 94110-02 EMBRAER 210-5A (205A) 4 94110-40 * S-2S 8 96005-1 Agwagon “A” & “B” A188A 4 94110-40 Bandeirante EMB-110P1, 3 5906-2SA5 Centurion 210B, C 4 94110-40 BASLER *Yates Aircraft Conv.
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