# TCDS E-162: Air Repair Inc. - Type: Type certificate data sheet - Status: Current - Holder: Air Repair Inc. - Revision: 13 - Revised: September 7, 2011 - Product: Engine - Certification basis: Part 13, CAR 13 - Registered aircraft: 89, by the registry models matched to it (OpenAirDocs) - Data sheet PDF: https://openairdocs.org/files/sha256/1a/cf/1acfb634b27c4b6ae4f0d02f06cdccb8c38e0c2fff063646ac8540d18257c5de - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/F37A306BA748520486257C27004C50C7.0001 - Page: https://openairdocs.org/tcds/E-162 ## Models (7) As the data sheet lists them. - W670-24 - W670-K - W670-6A - W670-23 - W670-M - W670-16 - W670-6N ## What the data sheet says From the PDF's text layer, line by line; tables lose their columns. The PDF is the record. ```text Page No. 1 2 3 Rev. No. 13 12 12 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION E-162 Revision 13 CONTINENTAL W670-6A (R-670-3, -5) W670-6N (R-670-4) W670-16 (R-670-8, -11, -11A) W670-K W670-M W670-23 W670-24 September 7, 2011 TYPE CERTIFICATE DATA SHEET NO. E-162 Engines of models described herein conformation with this data sheet (which is part of Type Certificate No. 162) and other approved data on file with the Federal Aviation Administration, meet the minimum standards for use in certificate aircraft in accordance with pertinent aircraft data sheets and applicable portions of the Federal Aviation Regulations provided they are installed, operated and maintained as prescribed by the approved manufacturer’s manuals and other approved instructions. Type Certificate Holder Air Repair, Inc. 920 Airport Service Road Cleveland, MS 38732 Type Certificate Holder Record Teledyne-Continental Motors (Previous TC Holder) Transferred TC 162 to Air Repair, Inc. on August 25, 2011 Model W670 -6A -6N -16 -K -M -23 -24 Type 7RA - - - - - - - - - - - - Rating Max. continuous, hp., r.p.m. sea level pressure altitude 220-2075-S.L. - - - - 225-2175-S.L. 240-2200-S.L. - - 220-2075-S.L. Takeoff, h.p. r.p.m. 220-2075 - - - - 225-2175 240-2200 - - 220-2075 Fuel (min. grade aviation gasoline) 65 - - - - - - 80/87 - - 65 Lubricating Oil Ambient air temperature Above 40°F. Below 40°F. Oil Grade SAE 50 SAE 30 - - - - - - - - - - - - - - - - - - - - - - - - Bore and stroke, in. 5.125 x 4.625 - - - - - - - - - - - - Displacement, cu. in. 668 - - - - - - - - - - - - Compression ratio 5.4:1 - - - - - - 6.1:1 - - 5.4:1 Weight (dry), lb. 470 479 486 450 455 519 492 Propeller shaft. SAE No. 20 - - - - - - - - - - - - Carburetion Bendix- Stromberg NA-R6, -R6D with 1-15/16 in. venturi - - Bendix- Stromberg NA-R6G with 1-15/16 in. venturi Bendix- Stromberg NA-R6D with 1-15/16 in. venturi - - Bendix- Stromberg NA-R6G with 2-1/16 in. venturi Bendix- Stromberg NA-R6G with 1-15/16 in. venturi E-162 2 Model W670 -6A -6N -16 -K -M -23 -24 Ignition, dual Scintilla VMN7-DF magnetos or WL7A battery ignition, or magneto and battery combination Scintilla SF7R-1 magnetos - - Scintilla MN7- DF magnetos or WL7A battery ignition, or magneto and battery combination - - Scintilla VMN7-DFA magnetos or WL7A battery ignition or magneto and battery combination - - Ignition timing, °BTC (No. 1 cyl.) Right magneto 32 - - - - - - - - - - - - Left magneto 29 - - - - - - - - - - - - Battery distributor 5 Ä Ä 5 - - - - - - Spark Plugs See NOTE 7 - - - - - - - - - - - - NOTES 1,2,3,4,7 1,3,4,7 1,3,4,7 1,2,4,7 1,2,4,7 1,2,5,7 1,2,4,6,7 “- -” indicates “same as preceding model”. “Ä“ indicates “does not apply”. Certification basis Aeronautics Bulletin 7-A effective as amended to 10/1/34; Civil Air Regulation Part 13 effective 8/1/41. Type Certificate No. 162 issued. Production basis Production Certificate No. 7. NOTE 1. Maximum permissible cylinder head, barrel, and oil inlet temperatures, 550°F., 325°F., and 210°F., respectively. NOTE 2. Combination magneto and battery ignition, and battery ignition (only), entail weight increase of approximately 10 lb. and 3 lb., respectively. NOTE 3. Military engines models R-670-3, -4, -5, -8, and -11 are eligible at a dry weight of 486 lb. with the same ratings as the W670-6A, -6N, and -16. The engines are all basically similar, but differ mainly as follows: Military Model Corresponding Certificated Model Carburetor Model Magneto Models Miscellaneous R-670-3 W670-6A NA-R6 VMN7-DF or MN7-DF -3 model, early type oil pump, crankcases, accessory case, and cylinders. R-670-4 W670-6N NA-R6 or -R6D SF7RN-1 or SF7R-1 -4 identical to W670-6N. R-670-5 W670-6A NA-R6 or -R6D VMN7-DF -5 identical to W670-6A. R-670-11, -8, -11A W670-16 NA-R6G SF7RN-1 -11 identical to W670-16. -8 and -11A same except have 7th order torsional damper. W670-6N NA-R6D SF7R-1 or SF7RN-1 Late type engine with latest type crankcase, accessories section, etc. differs mainly from -6A in accessories section. The corresponding certificated model designation of military engines and T.C. No. 162 should be included on the engine designation plate when installed in certificated aircraft. NOTE 4. These engines are eligible with facilities for two position propeller control valves at a weight increase of approximately 2 lb. NOTE 5. The W670-23 engine incorporates AN standard propeller governor pad for mounting and driving a constant speed propeller governor on the nose section of the crankcase, clockwise rotation at 1-1/7 crankshaft speed. 3 E-162 NOTE 6. Approval of the following model has expired: No engines of this model manufactured after the date shown or with serial numbers above those listed below are eligible for use in certificated aircraft. Model Date Serial No. W670-24 8-20-47 911050 NOTE 7. The following spark plugs are approved for use on these engines: AC SR83IR, HSR83IR, SR83P, HSR83P, SR87, HSR87, A88, HS88, HSR88, S88, S88D, SR88, SR88D, HSR93, SR93 Auto Lite 18-A1, SH2K, SH2M, SH15, SH15R, SH20, SH20A, SH150, SH200A BG 4B2, 4B2S, 417S, RB485S, SU485, SU485S, 706S, 706SR, 919SR5, RB955S Champion M26, C27, C27S, REM38P, RHM38P, REM38W, RHM38W, REM40E, RHM40E, D41N, ED41N, EM41E, EM41N, M41N, HM41E, EM42E, M42E Red Seal SE190, SJ190, SE230, SJ230 .....END..... ``` ## ADs (1, in force first) - [AD 50-12-01](https://openairdocs.org/ad/50-12-01): Propeller Blade · Hamilton Standard Propeller Blades, W670-16, W670-6A and 1 more ## Registered aircraft by registry model (OpenAirDocs) - [Continental W670-6N](https://openairdocs.org/engine/continental-w670-6n): 52 aircraft (registry code 17318) - [Continental W670-6A](https://openairdocs.org/engine/continental-w670-6a): 37 aircraft (registry code 17317) - [Continental W670-16](https://openairdocs.org/engine/continental-w670-16): 0 aircraft (registry code 17319) - [Continental W670-23](https://openairdocs.org/engine/continental-w670-23): 0 aircraft (registry code 17322) - [Continental W670-24](https://openairdocs.org/engine/continental-w670-24): 0 aircraft (registry code 17323) - [Continental W670-K](https://openairdocs.org/engine/continental-w670-k): 0 aircraft (registry code 17320) - [Continental W670-M](https://openairdocs.org/engine/continental-w670-m): 0 aircraft (registry code 17321) ## STCs approved under this data sheet (19) - [STC SE04651CH](https://openairdocs.org/stc/SE04651CH): To allow use of l00R grade aviation fuel meeting Swift Fuel, LLC specification SPEC-l00R-22. Swift Fuels LLC - [STC SE01966WI](https://openairdocs.org/stc/SE01966WI): Use of GAMI G100UL High Octane Unleaded Avgas in spark ignition piston aircraft engines. General Aviation Modifications Inc. - [STC SE8776SW](https://openairdocs.org/stc/SE8776SW): Installation of coated cylinders and piston rings.. Continental Motors, Inc. - [STC SE7492SW](https://openairdocs.org/stc/SE7492SW): Install Delco starter P/N 1108684 or Eclipse/Bendix Utica model E80 starters. Rare Aircraft Ltd - [STC SE04136AT](https://openairdocs.org/stc/SE04136AT): Installation of Bendix Scintilla WL-7A Battery Ignition Timer (distributor) modified from a breaker points and condenser design to a Hall Effect electronic sensor design. Air Repair Inc - [STC SE00809WI](https://openairdocs.org/stc/SE00809WI): Installation of a modified alternate source of supply, engine ignition coil assembly and condenser. Air Repair Inc - [STC SE01652WI](https://openairdocs.org/stc/SE01652WI): Modification of engine to replace contact points and condenser controlled Bendix Scintilla WL-7A battery timer (distributor) with an electronically controlled WL-7A-M battery timer.. Radial Engines Ltd - [STC SE01144SE](https://openairdocs.org/stc/SE01144SE): Installation of Olde Thyme Aviation, Inc. pistons, P/N OTA-4032-T6 or Air Repair, Inc. pistons, P/Ns AR4177 (5 each) and AR4177-1 (2 each), to replace Teledyne Continental Motors pistons P/N 4177.. Air Repair Inc - [STC SE01243WI](https://openairdocs.org/stc/SE01243WI): Installation of Barron Aviation intake tube drain kits on the engines listed on the attached FAA Approved Model List (AML) No. SE01243WI, dated April 26, 2004, or later FAA Approved revision.. Barron Aviation - [STC SE01145SE](https://openairdocs.org/stc/SE01145SE): Option 1) Installation of Olde Thyme Aviation Inc. crankshaft bearings OTA-21201-AB (rear) and OTA-21301-FB (front) Option 2) Installation of Olde Thyme Aviation Inc. replacement intake valve guides P/N OTA-20241-IG Option 3) Installation of Olde Thyme Aviation Inc. replacement exhaust valve guides P/N OTA-20406-EG. Air Repair Inc - [STC SE01146SE](https://openairdocs.org/stc/SE01146SE): Option 1) Installation of Gold Coast Aviation crankshaft bearings GCA-21201-AB (rear) and GCA-21301-FB (front) Option 2) Installation of Gold Coast Aviation replacement intake valve guides P/N GCA-20241-IG Option 3) Installation of Gold Coast Aviation replacement exhaust valve guides P/N GCA-20406-EG. Gold Coast Aviation Service Inc - [STC SE00946LA](https://openairdocs.org/stc/SE00946LA): Installation of engine crankshaft front and rear bearings.. Holloway Engineering Co - [STC SE00372LA](https://openairdocs.org/stc/SE00372LA): Installation of a Jacobs shielded ignition harness on Teledyne Continental Motors engine models.. Aero Engines Inc - [STC SE7491SW](https://openairdocs.org/stc/SE7491SW): Install Scintilla VNM-7DFA magnetos on W-670-6A and -6N engines.. Air Repair - [STC SE5879SW](https://openairdocs.org/stc/SE5879SW): Use of Phillips X/C II 20W-50 and25W-60 oil (OSS 55875) in all Avco reciprocating aircraft engines from 65 to 450 BHP.. Phillips Petroleum Co - [STC SE4127SW](https://openairdocs.org/stc/SE4127SW): Install modified W-670-23 piston, P/N 4180, to replace W-670-6A piston, P/N 4177.. Air Repair - [STC SE2028CE](https://openairdocs.org/stc/SE2028CE): Add the following approved fuel: unleaded automotive gasoline, 87 minimum antiknock index, and leaded automotive gasoline, 88 minimum antiknock index(RON+MON)/2. Intermixing with aviation gasoline also approved.. Petersen Aviation Inc - [STC SE5WE](https://openairdocs.org/stc/SE5WE): Compression ratio tank pistons. Salinas Engine Works - [STC SE03079AT](https://openairdocs.org/stc/SE03079AT) (historical): Modify the Teledyne Continental W670 Series aircraft engines by replacing the crankshaft front and rear main ball bearings with higher capacity roller bearings. Air Repair Inc. --- 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.