# TCDS A11SO: Gulfstream Aerospace Corporation - Type: Type certificate data sheet - Status: Current - Holder: Gulfstream Aerospace Corporation - Revision: 6 - Revised: May 1, 1989 - Product: Aircraft, Small Airplane - Data sheet PDF: https://openairdocs.org/files/sha256/61/36/6136824e28e97c76f52339d3b0b52013a656937d9f100732ad6b2d6d38a7dbbc - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/04D0EFAD706664AD85256738005A5B4A.0001 - Page: https://openairdocs.org/tcds/A11SO ## Models (1) As the data sheet lists them. - 111 ## 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. 11 - 11 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION A11SO Revision 6 Gulfstream Aerospace Model 111 May 1, 1989 TYPE CERTIFICATE DATA SHEET NO. A11SO This data sheet, which is a part of Type Certificate A11SO, prescribes conditions and limitations under which the product for which the Type Certificate was issued meets the airworthiness requirements of the Federal Aviation Regulations. Type Certificate Holder Gulfstream Aerospace Corporation dba Gulfstream Aerospace Technologies 7400 N. W. 50th - Wiley Post Airport P. O. Box 22500 Oklahoma City, Oklahoma 73123 I. Model 111, 4 PCLM (Normal or Utility Category), Approved 1 June 1972 Engine Lycoming O-360-A4G or O-360-A1G6 Fuel 100/130 minimum grade aviation gasoline Engine Limits For all operations, 2700 r.p.m. (180 hp) Propeller and Propeller Limits Approved for use with O-360-A4G engine only Sensenich Fixed Pitch, Model 76EM8S24-0-58 Static r.p.m. at maximum permissible throttle Setting, not over 2380, not under 2280 r.p.m. No additional tolerance permitted. Diameter: 76 inches, no cut off permitted Spinner assembly: Aero Commander 46440 is required. Approved For use with O-360-A1G6 engine only Hartzell Constant Speed, Model HC-E2YR-1BF or HC-E2YR-1B Blade, Model F7666A or 7666A Pitch: High 28° - 30°, Low 13° at Blade Station 30 inches Diameter: Not over 76”, not under 72” Governor: Edo-Aire 34-828-014 Spinner: Hartzell C3533 or C3533P is required Airspeed Limits (CAS) Never exceed 153 Kts (176 m.p.h.) CAS Maximum structural cruising 136 Kts (157 m.p.h.) CAS Maneuvering (normal) 111 Kts (128 m.p.h.) CAS Maneuvering (utility) 108 Kts (124 m.p.h.) CAS Flaps extended (40°) 109 Kts (125 m.p.h.) CAS A11SO 2 C.G. Range Normal Category (+97.0) to (+110.5) at 2100 lbs.or less (+101.7) to (+110.5) at 2550 lbs. Utility Category (+97.0) to (+104.2) at 2100 lbs. or less Straight line variation between points given. Fuselage Stations - Inches Empty Wt. C.G. Range None Datum 62.5 inches forward of firewall (front face) Leveling means Bottom of fuselage, outer surface, from F.S. 62.5 to F.S. 97.6 Maximum Weight 2550 lbs. (Normal Category) 2100 lbs. (Utility Category) No. of Seats 2 occupants at (+99.0) 2 occupants at (+136.0) Normal Category only Maximum Baggage 200 lbs. (at +164.0) Fuel Capacity 64 gal. usable. (2 wing tanks) at +108.6 (See Note 1 for unusable fuel) Oil Capacity 8 qts. at +46.5 (6 qts. usable) (See Note 1 for undrainable oil) Control Surface Movements Wing flaps Up * 0° Down 40° æ 2° Aileron Up 25°æ 2° Down 9° æ 2° Rudder Left **22° æ 2° Right 28° æ 2° Elevator Up 30°æ 2° Down 15° æ 2° Elevator tab Up 15°æ 2° Down 25° æ 2°, - 0° * 0 to be æ 1/8” of trailing edge of aileron ** From vertical stabilizer centerline Nosewheel movement Steering æ 15° Castoring æ 30° 3 A11SO Serial Nos. Eligible 10001 and up Certification basis Application for Type Certificate dated 10 December 1969. FAR 23, effective 1 February 1965, including Amendments 1 thru 7, and FAR 21, effective 1 February 1965, including Amendments 1 thru 26. Type Certificate A11SO issued 1 June 1972. Production basis None. Prior to original certification of each airplane, an FAA representative must perform a detailed inspection for workmanship, material and conformity with the approved technical data, and a check of the flight characteristics. Equipment The basic required equipment as prescribed in the applicable airworthiness regulations (see certification basis) must be installed in the aircraft for certification. FAA approved Equipment List. FAA Approved Airplane Flight Manual dated 1 June 1972. NOTE 1. Current weight and balance report, including list of equipment included in the certificated empty weight, and loading instructions when necessary, must be provided for each aircraft at the time of original certification. The certificated empty weight and corresponding center of gravity locations must include undrainable engine oil (not included in the oil capacity) and unusable fuel as noted below: Unusable Fuel (3 gal. per tank) 36 lbs. at (+112.1) Undrainable Oil with O-360-A1G6 engine 5 lbs. at (+48.6) with O-360-A4G engine 4.2 lbs. at (+51.1) NOTE 2. The following placards must be displayed in front of and in clear view of the pilot. “This airplane must be operated as a normal or utility category airplane in compliance with operation limitations stated in the Airplane Flight Manual.” See approved Airplane Flight Manual for additional placards. “All placards required in the approved Airplane Flight Manual must be installed in the appropriate locations.” NOTE 3. The service life of the wing and associated structure has been established as 7921 hours maximum. ....END.... ``` ## ADs (3, in force first) - [AD 2023-10-02](https://openairdocs.org/ad/2023-10-02): Indicating/Recording System, Navigation · Boeing 18, 23, 35 and 1,060 more. Effective May 26, 2023 - [AD 2001-18-05](https://openairdocs.org/ad/2001-18-05): Flight Eagle Tires · Boeing 720 Series, 720B Series, 111 and 6 more. Effective Sep 24, 2001 - [AD 96-25-12](https://openairdocs.org/ad/96-25-12): Auxiliary Power Units · BAE Systems HS 748 Series 2A, HS 748 Series 2B, 707-100 Long Body and 74 more. Effective Jan 13, 1997 ## Registered aircraft by registry model (OpenAirDocs) - [Aero Commander 111](https://openairdocs.org/model/aero-commander-111): 0 aircraft (registry code 0140205) - [Havoc Air Racing SUPER GT 111](https://openairdocs.org/model/havoc-air-racing-super-gt-111): 0 aircraft (registry code 05637US) ## STCs approved under this data sheet (36) - [STC SA04837NY](https://openairdocs.org/stc/SA04837NY): Installation of AeroLED's Holdings, LLC., position lights, navigation lights, strobe lights and beacon lights. AeroLED's Holdings, LLC - [STC SA800EA](https://openairdocs.org/stc/SA800EA): Installation of Whelen Anti-Collision, Position, or Anti-Collision/Position Light System, and applicable associated power supplies. Whelen Aerospace Technologies - [STC SA00081NY](https://openairdocs.org/stc/SA00081NY): Installation of Iceman Aviation Supplies, Inc. Carburetor Ice Detector.. Alcor LLC - [STC SA01967WI](https://openairdocs.org/stc/SA01967WI): Use of GAMI G100UL High Octane Unleaded Avgas. General Aviation Modifications Inc. - [STC SA00344BO PAGE 1](https://openairdocs.org/stc/SA00344BO%20PAGE%201): Installation of Parmetheus Plus LED PAR36 and PAR46 taxi and landing lights.. Whelen Aerospace Technologies - [STC SA615EA](https://openairdocs.org/stc/SA615EA): Installation of a Whelen Anti-Collision Strobe Light System as replacement for originally installed anti-collision lights.. Whelen Aerospace Technologies - [STC SA02212AK](https://openairdocs.org/stc/SA02212AK): Replacement of existing landing and/or taxi light reflector and bulbs with high intensity discharge (HID) lighting systems. Seaplanes North LLC - [STC SA00149BO](https://openairdocs.org/stc/SA00149BO): Installation of Aircraft Components, Inc. Volt and Vac Alert System, P/N 2044-1. Aircraft Components Inc - [STC SA02547AT](https://openairdocs.org/stc/SA02547AT): Installation of a Voice Alert System.. Aircraft Components Inc - [STC SA03658AT](https://openairdocs.org/stc/SA03658AT): Installation of a Voice Alert System to incorporate as primary annunciators for stall and gear warnings. Aircraft Components Inc - [STC SA02283SE PAGE 1](https://openairdocs.org/stc/SA02283SE%20PAGE%201): Installation of Electronics International Inc. Glass Panel Engine Monitor (with In Flight Data) CGR-30P. Electronics International Inc. - [STC SA02402SE PAGE 1](https://openairdocs.org/stc/SA02402SE%20PAGE%201): Installation of Electronics International Inc. Glass Panel Engine Monitor (with In-Flight Data) CGR-30C. Electronics International Inc. - [STC SA02110CH](https://openairdocs.org/stc/SA02110CH): Installation of a Time Trac Data Recorder. P2 Incorporated - [STC SA2693NM](https://openairdocs.org/stc/SA2693NM): Installation of Electronics International digital volt/amp gauges and accessories.. Electronics International Inc. - [STC SA01988SE](https://openairdocs.org/stc/SA01988SE): Installation of Electronics International Inc. Glass Panel Engine Monitor (with In-Flight Data) MVP-50P.. Electronics International Inc. - [STC ST02540AT-D](https://openairdocs.org/stc/ST02540AT-D): Installation of replacement fuel tank sealant system. FFC Manufacturing - [STC SA593CH](https://openairdocs.org/stc/SA593CH): Install Champion SlickSTART magneto booster system.. Champion Aerospace LLC - [STC SA4005NM](https://openairdocs.org/stc/SA4005NM): Precise Flight Inc. Pulselite Control System. Precise Flight Inc - [STC ST00665NY](https://openairdocs.org/stc/ST00665NY): Installation of a Dual AlliedSignal GNS-XLs flight management system.. Garrett Aviation Services - [STC SA00680SE](https://openairdocs.org/stc/SA00680SE): Installation of Electronics International model UBG-16 or UBG-16T bar graph engine analyzer.. Electronics International - [STC SA01158WI](https://openairdocs.org/stc/SA01158WI): Installation of Aero Enhancements UV250-1 Supplemental Instrument Panel Lightning System.. Aero Enhancements Inc. - [STC SA2683NM](https://openairdocs.org/stc/SA2683NM): Installation of Precise Flight, Inc. stand-by vacuum system (SVS). Precise Flight Inc - [STC ST00896AT](https://openairdocs.org/stc/ST00896AT): Installation of Fairchild Model F1000 expanded parameter Flight Data Recorder.. Gulfstream Aerospace Corporation - [STC SA02795AT](https://openairdocs.org/stc/SA02795AT): Installation of a PXE7300SR, In-Flight Entertainment System. PS Engineering Incorporated - [STC ST02547AT](https://openairdocs.org/stc/ST02547AT): Installation of a voice alert system.. Aircraft Components Inc - [STC SA489EA](https://openairdocs.org/stc/SA489EA): Installation of ARP Inc. carburetor ice detection system. Aircraft & Rotorcraft Products (ARP) Inc - [STC SA1626NM PAGE 1](https://openairdocs.org/stc/SA1626NM%20PAGE%201): Installation of Electronics Int'l Digital EGT/CHT Instruments and accessories. (201 Series). Electronics International - [STC SA5159NM](https://openairdocs.org/stc/SA5159NM): Installation of chip detector system.. Northwest Aircraft Inc - [STC SA2844CE](https://openairdocs.org/stc/SA2844CE): Installation of a plastic cap enclosure over the anti-collision strobe light system.. Air Transport Inc - [STC SA4302NM](https://openairdocs.org/stc/SA4302NM): Installation of Electronics Int'l digital automatic engine analyzer.. Electronics International - [STC SA1502SW](https://openairdocs.org/stc/SA1502SW): Installation of Mitchell automatic flight system model AK364 consisting of Century I autopilot with optional omni tracker.. Century Flight Systems Inc - [STC SA1503SW](https://openairdocs.org/stc/SA1503SW): Installation of Mitchell automatic flight system model AK 363 consisting of Century IIB autopilot with optional radio coupler.. Century Flight Systems Inc - [STC SA1504SW](https://openairdocs.org/stc/SA1504SW): Installation of Mitchell automatic flight system model AK362 consisting of Century III autopilot with optional command/ electric pitch trim, optional radio and glide slope couplers.. Century Flight Systems Inc - [STC SA1505SW](https://openairdocs.org/stc/SA1505SW): Installation of Mitchell command/electric pitch trim system.. Century Flight Systems Inc - [STC SA308EA](https://openairdocs.org/stc/SA308EA): Installation of carburetor ice detection system 105AP in single and twin engine aircraft and single engine helicopters powered by Continental, Franklin, and Lycoming type engines equipped with Marvel-Schebler MA-2, MA-3, MA-4, MA-4-5, MA-6 and HA-6 series carburetors. (Normal,Utility and Acrobatic Category airplanes and helicopters equipped with engines and carburetors as described.). Alfred R Puccinelli - [STC SA2386SW](https://openairdocs.org/stc/SA2386SW): Installation of S.A.F.E., EGT, CHT Systems.. Avicon Development Corporation --- 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.