# STC SA2248CE - Type: Supplemental type certificate - Status: Current, Reissued - Holder: Team Luscombe LLC - Description: Installation of Continental 0-200-A engine and fixed pitch propellers. Data pertinent to this modification are considered inadequate for duplication in other airplanes. This approval is limited to the installation made in Luscombe Model 8A, Serial Number 4938, only. - Status date: September 22, 2004 - Data sheets: A-694 - Certificate PDF: https://openairdocs.org/files/sha256/08/79/087959db5daa303e7da467d070efbfaf2a5fe4d926d1123350798b4216e149ba - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/C4A8E848B855083C862570D100693188.0001 - Page: https://openairdocs.org/stc/SA2248CE ## ADs that name it None. ## Approved models (1) - The Don Luscombe Aviation History Foundation Inc. 8A (TCDS A-694) ## What the certificate says Read from the PDF's text layer, without the form's printed wording; the layout is lost and the order can differ. The PDF is the record. This Certificate issued to The Don Luscombe Aviation History Foundation, Inc. c/o 251 Washington Street Chandler, Arizona 85225 Part 4a of the Civil Air Regulations. A-694 LUSCOMBE 8A, Serial Number 4938 Description of Type Design Change: Installation of Continental 0-200-A engine and fixed pitch propellers in accordance with approved data identified on continuation sheets. Copies of this STC, including the continuation sheets, and the Operating Limitations, dated May 18, 1987, are required to be kept with the airplane. Limitations and Conditions: Data pertinent to this modification are considered inadequate for duplication in other airplanes. This approval is limited to the installation made in Luscombe Model 8A, Serial Number 4938, only. A copy of this STC must be included in the permanent records of the modified aircraft. If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other person written evidence of that permission. Date of application : March 23, 1987 Date of issuance : May 18, 1987 Date reissued : Jan. 19, 1995, Dec. 27, 2002, Dec. 10, 2003 (Signature) Manager, Technical and Administrative Support Staff, Los Angeles Aircraft Certification Office Transfer the ownership of the Supplemental Type Certificate Number to (Name of transferee) (Address of transfer) (Number and street) (City, State and Zip code) from (Name of grantor) (Print or type) (Address of grantor) (Number and street) (City, State and Zip code) Extent of Authority (if licensing agreement): Signature of grantor (In ink): Number SA2248CE TCDS A-694 applies, except as follows: Note: Required Equipment, Propellers and Propeller Accessories, Engine and Engine Accessories - Fuel and Oil System, Landing Gear, Electrical Equipment, Interior Equipment, and Miscellaneous items that conflict with items installed by the STC are superseded by the STC items. Installation of other such items on the equipment list or on the Data Sheet in conjunction with this STC must be evaluated to determine that they will introduce no adverse effect upon the airworthiness of the airplane. Engine Continental 0-200-A +17.2 lb. (-32.0 inches) Fuel 80/87 minimum octane aviation gasoline Unleaded automotive gasoline in accordance with STC's SA730GL and SE634GL Engine Limits For all operations 2750 RPM (100 Horsepower) Oil Capacity 6 quarts (-24.0 inches) Optional Equipment: Starter (Prestolite No. MZ4214) +16.0 lb. (-22.0 inches) Starter (Delco-Remy No. 1109656) +16.0 lb. (-22.0 inches) Alternator, 60 amp, 14 volt (Cessna +11.5 lb. (-22.0 inches) No. C611501-0203) Regulator, alternator, 14 volt, 60 amp +1.0 lb. (-22.0 inches) (Cessna C611001-0101) Vacuum System Pump (Airborne No. 200CC-9) +3.6 lb. (-36.4 inches) Relief valve (Airborne No. 133A14) +0.5 lb. (-18.0 inches) Gauge (Cessna C668542-0101) +0.4 lb. (-4.0 inches) Gear assembly (Cont. 625937) +2.5 lb. (-36.4 inches) Propellers: One of the following: 1. McCauley 1A101/DCM-6953, or any +1.0 lb. (-45.0 inches) other 1A101/DCM propeller which meets the following limits: Number SA2248CE Propellers: One of the following: (Cont.) a. Static RPM at maximum permissible throttle setting - not less then 2375 RPM nor More than 2475 RPM. b. Diameter not more than 69.0 inches nor less than 67.0 inches or 2. McCauley 1B90/CM-7152 or any other +1.0 lb. (-45.0 inches) 1B90/CM propeller which meets the following limits: a. Static RPM at maximum permissible throttle setting not less than 2000 RPM nor more than 2200 RPM. b. Diameter not more than 75.0 inches nor less than 71.0 inches Instrument Markings: Tachometer 2750 RPM (Red line) Oil Pressure 0 to 10 psi (Red arc) 10 to 30 psi (Yellow arc) 30 to 60 psi (Green arc) 60 psi (Red Line) Oil Temperature 225ºF (Red line) Required Data: 1. Applicants Data: a. Wittstock Letter, dated March 24, 1987, stamped "FAA Approved." b. Wittstock Supplemental Specifications, dated March 23, 1987, stamped "FAA Approved." c. Wittstock Letter, dated April 9, 1987, stamped "FAA Approved." 2. Conformity Inspection Record, FAA Form 8100.0, dated April 30, 1987. 3. Statement of Conformity, FAA Form 8130-9, dated April 30, 1987. 4. Operating Limitations, dated May 18, 1987. - END - ## Every issue (1) - December 10, 2003: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/08/79/087959db5daa303e7da467d070efbfaf2a5fe4d926d1123350798b4216e149ba) --- From OpenAirDocs.org, an independent open copy of FAA data. Only the Federal Register edition on govinfo.gov is the official legal text of an AD.