LORD Mounts for General Aviation - Pilot Supplies and ...

1 lord Mounts for General AviationLORD Mounts for General AviationLORD set the standard for elastomeric engine Mounts more than 70 years ago by providing the first Dynafocal engine Mounts for aircraft. Today, lord Mounts continue to provide superior performance and life at all levels of General Aviation . Millions of lord Mounts have been produced, sold into the market place and flown by operators all over the world. With best-in-class quality and performance, most major OEMs and service shops specify lord of our strong history of vibration and motion control products, we offer a wide array of innovative solutions for the aerospace industry. We can work with you to determine the lord mount for your aircraft. For more information, contact customer support at or +1 877 ASK lord (275 5673).Maintenance of Bonded Sandwich Mountings and AssembliesFor type certificated aircraft, you must use the FAA approved component maintenance manual.

2 1. General COMMENTSB onded sandwich assemblies are natural rubber or specially blended synthetic compounds bonded to two plates. The normal installation requires four assemblies, each consisting of two sandwich mountings and one spacer. Satisfactory performance requires that the spacer be designed to the correct length to precompress each mounting to guarantee proper positioning of the mountings. When properly installed, these mountings provide excellent isolation of engine vibration, resulting in smoother, quieter flight. Always order replacement mountings by the mounting assembly number to ensure the correct VISUAL INSPECTION OF INSTALLED MOUNTINGSAt each annual inspection and at FAA-required inspections of the aircraft s engines, all mounting assemblies should be visually inspected in their installed state while supporting the engine weight.

3 The correct visual inspection procedure is as follows:a. Inspect all bonded sandwich mountings for metal-to-rubber bond separations, flex cracks, rubber deterioration due to exposure to fluids, and mechanical damage such as cuts in the rubber Visually inspect all bonded steel parts for cracks and excessive nicks, scratches or Inspect all nut locking wires for looseness and tighten as When applicable, measure all drift indicators in each mounting assembly for excessive Whenever any of the conditions detailed above in steps a, b and d are found, remove the mounting assembly from the engine, disassemble, inspect and repair it as described in the maintenance : WHENEVER THE AIRCRAFT S ENGINES ARE CLEANED DURING A NORMAL INSPECTION, COVER EACH MOUNTING ASSEMBLY TO PROTECT IT FROM CONTAMINATION BY CLEANING FLUIDS OR SOLVENTS.

4 THIS ALSO APPLIES TO ENGINE LUBRICANTS. SHOULD ANY SUCH MATERIALS ACCIDENTALLY GET ON A MOUNTING ASSEMBLY, WIPE IT OFF THOROUGHLY AS SOON AS POSSIBLE WITH A CLEAN, DRY RAG. 3. DISASSEMBLYTo remove mounting assemblies from the installation, it is necessary to remove the engine weight from the mountings, by the use of a chain hoist or equivalent, and disconnect the nuts and bolts which hold the mountings in place. In General , removal of one mounting at a time can usually be accomplished, if necessary, without removing the engine weight from the CLEANING & INSPECTIONa. Wipe oil and dirt from bonded mountings, but do not dip in cleaning Steel bolts and spacers should be inspected for cracks or damaged threads. Examine spacers for crushing of ends, caused by excessive tightening torque on bolt. Replace if either condition is Examine bonded rubber mounting for oil swelling, bond or rubber separation and shear or compression set.

5 Bond separation, oil swelling or flex cracks in the surface of the rubber are cause for rejection. The effects of shear and compression set are determined by measuring the dimensions shown on the sketch. Reject parts which have an eccentricity greater than dimension A or an overall thickness less than dimension B .Mounting Series NumberEccentricity Max. A Thickness Min. B * * * * * * (BTR-II)0 . (BTR-II)0 . (BTR-II)0 . *From original position (see installation drawing) lord ENGINE Mounts FOR YOUR AIRCRAFT APPLICATIONFor reference only oem aircraft manual is governing documentFor reference only oem aircraft manual is governing documentMODELLORD PART PER A/CSPECIALINFORMATIONAEROMACCHIAL-60C5/F 5J-9613-9/-242 , S-1S, S-2AJ-7401-28 BELLANCA17-30AJ-12453-1/-22 30847 & up17-31, 17-31A, 17-31 TCJ-9868-547 ECA, 7 GCAA, 7 GCBC, 7 KCABJ-6230-148 GCBC, 8 GCBC-CS, 8 GCBC-FPJ-6230-148 KCAB, 8 KCAB-CS, 8 KCAB-FP, 8 KCAB-180J-6230-14 BRITTON-NORMAN UNITED KINGDOMBN-2J-7402-208BN-2A-26J-7402-208B N-2A Mk.

6 3J-7402-2012 CESSNA152J-7402-14S/N 15279406-85594A152J-7402-14S/N 15279406-85594172I-PJ-9613-494172QJ-9613 -49J-9613-7222S/N 17275869 & up172 RGJ-9613-49 J-9613-7222R172EJ-9613-424S/N R172-0302 to -0335 R172KJ-9613-42S/N R1722000 & up177A, 177BJ-9613-494177 RGJ-9613-594180J-3804-14 J-3804-1522S/N 30002-32150180, 180A-G, 180HJ-6545-14S/N 32151-32661182, 182A-PJ-6545-14T182, TR182J-9613-124185, 185A-EJ-6545-14188A, 188BJ-15198-1 J-15198-22 2S/N 18802349 & upT188J-6545-6 J-15198-12 2S/N T1883297T & up205,205AJ-6545-1 J-6984-644P206, P206A-EJ-12453-1 J-12453-22 2TP206A-EJ-12453-1 J-12453-22 2TU206A-FJ-12453-1 J-12453-22 2207, 207A, 207A IIJ-12453-1 J-12453-22 2 MODELLORD PART PER A/CSPECIALINFORMATION208LM600-9 (Sand) LM600-20 (Spacer)6 3210, 210A-C, 210CJ-6545-14210D-LJ-12453-1 J-12453-22 2T210M,NJ-12453-1/-2/(MOD) 2/1/1T210F-L, T210J-LJ-12453-1 J-12453-22 2P210R (1985-86)J-12453-1 J-12453-24 2310J-QJ-12390-18 Non-turbo-charged models only310R, T310P,Q,RJ-9613-588320, 320A-CJ-7764-48320D-FJ-9613-31 or -588335J-9613-588336J-7764-108337, 337AJ-9613-318T337B-G, T337GJ-9613-318P337HJ-9613-318340, 340AJ-9613-588401,401A,BJ-9613-588402, 402A, 402B, 402CJ-9613-588404J-9613-548414, 414AJ-9613-588421, A, B, CJ-9613-548425LM-600-9(Sand) LM-600-20 (Spacer)12 6441LM-600-9(Sand) LM-600-12(Spacer) 200PE1210-4512 4 2500 / 501LM-420-SA5 LM-420-SA64 2550, 551LM-420-SA30 LM-420-SA31 LM-420-SA232 2 2 COMMANDER AIRCRAFT CORP.

7 (includes Twin Commander)111, 112, 112B, 112T, 112 TCAJ-9613-40/-532 eaDASSAULT BERQUET FRANCEF alcon 50LM-833-SA9/ -SA20-34/2 Falcon 50LM-833-SA21/ -SA222/1 Center Engine IsolatorFalcon 50, 900LM-833-SA102 Center EngineFalcon 50, 900, 900 EXLM-833-SA132 Engine 2 IsolatorEMBRAER BRAZILEMB-810J-9613-588 EMB-820J-9613-128 MODELLORD PART PER A/CSPECIALINFORMATIONGAF AUSTRALIAN 22B, N24 ALM-206-SA8-1 6 GULFSTREAM (formerly Israel Aircraft Corporation)1125LM-833-SA20-6 LM-833-SA18-32 2 GULFSTREAM AMERICAN , AA-lC, AA-5, AA-5AJ-7402-244AA-5BJ-9613-494AA-IJ-6113 -58AA-lA, -IBJ-6113-58AG-5BJ-9613-594GA7J-9613-498 HAWKERMU-2B-20LM-821-SA40LM-821-SA4142S/ N 224 & upMU-2B-25, -26LM-821-SA47LM-821-SA4842S/N 280 & upMU-2B-35LM-821-SA40LM-821-SA4142S/N 239-279MU-2B-60LM-821-SA47LM-821-SA4842M U-300LM-420-SA15LM 420-SA1642MU-300-10LM-420-SA15LM-420-SA4 042 BEECHCRAFTE18S, H18SJ-5384-1 J-5385-12/419A, Bl9, M19AJ-7402-164A23, A23AJ-10778-44C-23J-7402-16424, A24, A24R, B24R, C24RJ-10778-14J-10778-162 2C33AJ-10520-14E33, F33J-7518-24E33A, E33C, F33A, F33C, G33J-10520-1435, A35, B35J-2245-18H35, J35, K35, M35, N35, P35J-7518-24S35, T35, V35, V35A, V35BJ-10520-1436, A36J-10520-14A36TC, B36 TCJ-10520-14V35A-TCJ-10520-14B50, C50J-3804-10855, A55, B55, B55AJ-9613-58C55 (1967)

8 , D55, D55A, E55, E55AJ-10778-168S/N TE1-TE-84956TC / A56 TCJ-9613-958J-10778-16858PJ-12453-12858 TCJ-12453-12860, A60, B60J-9613-9865, A65J-6545-18 MODELLORD PART PER A/CSPECIALINFORMATION76TC, 76J-9613-49 J-9613-502 277J-7402-1480, A80, B80J-6545-18C90, C90A, E90, F90LM-427-SA7695,95A,95B, D95A, E95J-7402-18A100LM-427-SA76B100LM-821-SA 49 LM-821-SA504 2200, 200C, 200CT, B200LM-427-SA78C90, E90, C99, 200, C, CT, A200, C, CT, B200, C, CT, TLM-427-SA128 Overhaul Kit for Barry Controls P/N5906-25A91900 DLM-421-SA258400, 400A, 400 TLM-420-SA15 LM-420-SA164 2 HELIO AIRCRAFTH-250J-9613-124 KELOWNA FLIGHTCRAFT (formerly General Dynamics, Convair)580LM-207-SA14 LAKE AIRCRAFTC-2J-7402-14LA-4-200, LA-4AJ-7402-64 LEARJET23, 24, 25LM-308-SA4/-19 /-332 ea24D, 24 ELM-308-SA4/-19 /-332 ea24F, 25D, 25F, 28, 29LM-308-SA4/-19 /-332 ea35, 35A, 36, 36 ALM-833-SA4/-52/4M2 (formerly Fairchild & Swearingen)SA-226 ATLM-600-SA9LM-421-SA12J-7401-25442SA-22 7 ACLM-600-SA9LM-421-SA12J-7401-25422SA227 -ACLM 600-SA9LM 600-SA17J-7401-25422 MAULEM-5-210CJ-7764-104M-5-235CJ-7764-20 4 MOONEYM20BJ-7402-14S/N 101 to 260M20C J-7402-14S/N 101 to 470M20D J-7402-14471 to 21-1180M20E J-9613-124S/N 670001 to 22-1438M20E J-7402-164S/N 680001 to 700006M20F (1966-77)J-9613-124M20G (1968-70)J-7402-14M20J (1976-up)J-9613-404S/N 24-0001 & upMODELLORD PART PER A/CSPECIALINFORMATIONM20K (1979-85)J-9613-5841 Con TSIO-360-GB1M20K (1979-85)J-9613-75 J-9613-761 31 Con TSIO-360-GB3 or MB1M20K (1986-up)

9 J-9613-75 J-9613-761 3 NEW ZEALAND AEROSPACE NEW ZEALANDFU24-954, FU24A-954J-9613-9J-9613-2422 PARTENAVIA ITALYP-68J-9613-404 PIPERPA-23-236J-9613-12PA-23-250J-9613-1 28S/N 27-1to27-2504PA-23-250J-3804-20 J-3804-244 4PA-23-250TJ-9613-128PA-24-250J-3804-204 PA-24-250J-3804-414with McCauley prop STC-SA00773 CHPA-24-260J-3804-204S/N 24-3364 to 24-4803PA-24-400J-9613-9 J-9613-242 2PA-25-235J-3804-204PA-25-250J-3804-204P A-25-260J-3804-204PA-28-140J-7402-164S/N 20002-24999PA-28-140J-9613-402S/N 25000-25641PA-28-140J-9613-402S/N 7225001 & upPA-28-150J-7402-164S/N 20002-24999PA-28-150J-7402-24 4S/N 1479 to 1760PA-28-150J-7402-16 4S/N 1761-4377PA-28-151J-9613-40 J-9613-532 2PA-28-160J-7402-164S/N 1-507PA-28-160J-7402-164S/N 28-508 to 28-1478PA-28-160J-7402-244S/N 28-1479 to 28-3299PA-28-161J-9613-40 J-9613-532 2PA-28-180J-7402-244S/N 28-330 to 4377PA-28-180J-7402-244S/N 28-4378 to

10 5149PA-28-180J-7402-164S/N 1761-4377PA-28-181J-9613-404PA-28-236J-9 613-124PA-28R-180J-9613-404S/N 30001 & upPA-28R-200J-9613-404S/N 35001 & upPA-28R-201J-9613-404S/N 28R-7737002 & upPA-28R-201TJ-9613-584PA-28S-160J-7402- 164 MODELLORD PART PER A/CSPECIALINFORMATIONPA-30J-9613-198PA-3 1J-9613-128PA-31-300J-9613-308S/N 31228-31511PA31-310J-9613-128PA-31-325J- 9613-128PA-31-350J-9613-298PA-31 TLM-423-SA16PA-31T-1,-500LM-423-SA16PA-3 1T-620,LM-423-SA14PA-31T-2LM-423-SA16PA- 32-260J-7402-204S/N 1-569PA-32-260J-3804-274S/N 570 & upPA-32-300J-3804-274S/N 40001-7240055PA-32-300J-3804 -404S/N 7240056 & upPA-32-301J-9613-19 J-9613-122 2PA-32R-300J-3804-314S/N 32R7680001 & upPA-32R-300J-3804-404S/N 32R7680141 & upPA-32R-301J-9613-19 J-9613-122 2PA-32RT-300J-3804-404S/N 32RT7885001 & upPA-32RT-300TJ-3804-37 (bottom) J-3804-39 (top)2 2PA-34-200J-9613-408PA-38-112J-7402-164P A-39J-9613-198PA-44-180TJ-9613-408PA-46- 310PJ-9613-554PA-46-350PJ-9613-558S/N 4622001 & upRILEY TURBOSTREAM 400 SIAI MARCHETTI ITALYS-208J-3804-204SF-260, M, WJ-3804-204 SOCATA FRANCE235C,EJ-9613-404 lord provides valuable expertise in adhesives and coatings, vibration and motion control, and magnetically responsive technologies.