# TCDS TC 5E-5: Pratt & Whitney Division - Type: Type certificate data sheet - Status: Current - Holder: Pratt & Whitney Division - Revision: 0 - Product: Engine - Data sheet PDF: https://openairdocs.org/files/sha256/b6/9e/b69e58f13034706d1f825e29ebf6ac48181ac224559746970b950a489730e6c4 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/1F78AA99851224C58525676A0067217F.0001 - Page: https://openairdocs.org/tcds/TC%205E-5 ## Models (1) As the data sheet lists them. - Military R-2000 Series ## What the data sheet says This is OCR from the scanned FAA data sheet. OCR can misread letters and numbers. ```text Fratt & whitney Military k-2000 Series I.C. NUMBER: 5I-5 Model - R-2000 -9M2,-9M3 - 11A47191, -743 -976 11м2, -11M3 Type " to thon rearing 11M4) 10-5-3200- 1100-2550- 1100-2550- 110 0-2550 5-520 36-5-8300 37.5-10000 36,5-8300 2550- 1200-2550 1100-2550- 1100-2550- 1100-2550- 42.0-S.L. 38.5-S.L. 39.5-S.L. 38.5-S.L. 1450-2700 1350-2700- 1350-2700- 135 0-2700- 45.0-3500 45-5-5800 0-3500 1350-2700- 1350-2700- 135 0-2700- (with 10t 9.52: 46.0-S. I. (not 46.5-S.I. 9.52:1 46. 0-S. I. - 1151) 50- 1000-2550- 37.5-17700 1000-2550- 39.0-10000 in. noU 10-6 1-9M2. 10.9 -11M3,-4) 10.9 1-441 -9M3,-11M2 in. Carturetior. Stromber Ignition timing, 25 on - 11M2 25 20 25 137 in degrees BTC automatic 25(37 1 cruise) auto cruise on -4, -4M1, -9M2 and 3) NOIE 1. degrees egree pluggi kete "75 degrees F. well tyre head Fsi sprir.g spring owing accessory raue Maximum Overhary Static Moment (in. 1bs.) Starter (R-2000-7 and -11 24600 200 series only) 16500 220 Ger.ezator (R-2000-7 and -11 1700 dedes ony. 3:1 2000 25 0 FUEl FUrE 12 or. -7 ard - 11 cc 450 10 Vacuum pump (rear locatior.) 22 50 40 (side location) 90 800 20 Hydraulic pump 2250 70 Propeller governor 100 600 Tachometer 20 60 10 *"C" is clockwise viewing pad; "CC" is counter-clockwise viewing pad. **Speed ratio is based on crankanaft speed. NOTE 4. The following engines incorporate the additional detailed characteristics: R-2000 Model Wt. dry 1bs. Certificated Twin wasp Characteristics 1570 2SD-G sit agony on be cone can to at fest overal. for cargo only and Generally used Magnetos used are Scintilla SF14IN-8. 1605 2SD13-G Identical to certificated Twin Wasp 2SD13-6. Magnetos used are - 4M1 1585 2SD13-G except incorporates single ratio supercharging -4M2 2SD13-G similar to -4 except incorporates -11 cylinders and has -9 ratings. 2SD- G Basic model; identical to certificated Twin wasp 2sD-6. ма у incorporate the -11 type cam; this will result in a slight increase in power, but this increase is insufficient to neces- oatate a change in che power racinds May be modified to amproved pistons andklain type incorporate Iwin wasp master rods, followers and rollers, 2SD13-G type power section which main bearings, crankshaft and a larger capacity nose scavenge pump. Engines modified in this manner should be identified by means of the letter mcm stamped on the engine after the engine serial number. Magnetos -7M2 1585 2SD- G Similar to -7 except has single ratio supercharging. used are Scintilla SF14RN-8. 2SD-G Similar to -7M1 except has muffed barrel cylinders and 2SD13-G CY SE DOWEL SECTON The - is is eligible with the automatic cruise spark advance as used on the -9M4. Incorporation of the Such engine Such engine should be dentified by the letter my a heretary. "y» after the engine serial number. Also may be accomplished by using 2SD13-G - 7М3 1595 2SD-G Similar to -7M2 or Twin Wasp D5 with R-1830-75 or -94 reductio: gear assembly, and reduced ratings. - 9 1590 2SD1-G asic model, ldentical to certificated Iwin wasp 2SD1-G, ha all plain tyre main bearings and grooved face supercharger Maqnetos used are Scintilla SF 14LN-8. - 9A 1590 2SD1-G Similar to -9 except has -11 nose section and rocker sump, and magnetos used are Scintilla SF14RN-8. -9M1 1570 2SD1-G Similar to -9 except has Twin Wasp D3 type single ratio -9M2 1595 2SD1-G Similar to -9 except has Twin Wasp 2SD13-G muff type cylinders - 9M3 1575 2SD1-G - 9M4 1575 2SD1-G -9M6 1615 2SD13-G - 11 1580 All these center main bearings should be removed and replaced with either a satisfactory roller bearing or have the power section converted to the Twin wasp 2SD13-G the 18 2 340 if ting of the a one on was a for Scintilla SF14RN-8. - 11M1 1560 - 11M: 1595 - 11M3 1605 Similar to -11M2 except it has both high and low blower super- charder ratios. - 11M4 1590 Similar to -11 except has R-1830-75 or -94 reduction gear assembly. thin metal plate ive the pain mur bering to tenance at shade on we she of 10 at the 7 1a that me which ratings are not All R-2000 engines listed are eligible for operation on Grade 91 fuel provided the following reduced High ratio supercharger drives, when available, should not be used with grade 91 fuel. Take-off Maximum continuous 100 hp at 2700 rp NOTE 8. The following spark plugs are approved on these engines: AC Autolite BG Champion Lodge NOIE 9. Continuous operation between 2310 rpm and 2510 Ipm frohibited on all R-2000 model engines. ``` ## ADs (2, in force first) - [AD 53-09-01](https://openairdocs.org/ad/53-09-01): Link Pins · Pratt & Whitney Division Military R-2000 Series - [AD 56-06-02](https://openairdocs.org/ad/56-06-02): Cylinder Flange Attaching Stud · Pratt & Whitney Division Double Wasp CA15, Double Wasp CA17, Double Wasp CA18 and 115 more ## STCs approved under this data sheet (3) - [STC SE873SW](https://openairdocs.org/stc/SE873SW): Modification of Pratt and Whitney R2800-B Series cylinder heads to the R2000-2SD-13G configuration. Continental Motors, Inc. - [STC SE01203WI](https://openairdocs.org/stc/SE01203WI): Installation of R-1830-94 supercharger impeller and diffuser in place of existing hardware.. Dempsay William A. - [STC SE01208WI](https://openairdocs.org/stc/SE01208WI): Installation of R-1830-94 supercharger impeller and diffuser in place of existing hardware.. Dempsay William A. --- 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.