# TCDS 4A19: Augustair Inc. - Type: Type certificate data sheet - Status: Current - Holder: Augustair Inc. - Revision: 11 - Revised: January 29, 2014 - Product: Aircraft, Small Airplane - Certification basis: Part 3 - Registered aircraft: 123, by the registry models matched to it (OpenAirDocs) - Data sheet PDF: https://openairdocs.org/files/sha256/1a/66/1a665502b4c94ab97444fb0580ec0bc6022f5d64e05cb773091bce28bdcd6734 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/569DE3B3EDABE52E86257C8A0076C3B2.0001 - Page: https://openairdocs.org/tcds/4A19 ## Models (3) As the data sheet lists them. - 2150 - 2150A - 2180 ## 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 4 Rev. No. 11 10 10 10 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION 4A19 Revision 11 AUGUSTAIR (Morrisey, Varga) 2150 2150A 2180 January 29, 2014 TYPE CERTIFICATE DATA SHEET NO. 4A19 This data sheet which is a part of Type Certificate No. 4A19 prescribes co nditions and limitations under which the product for which the Type Certificate was issued meets the airworthiness requirements of the Civil Air Regulations. Type Certificate Holder: Augustair, Inc. 1809 Hephzibah McBean Rd Hephzibah, GA 30815 Type Certificate Holder Morrisey Aviation, Inc. transferred 4A19 to George Varga, Jr. on June 23, 1967. Record: George Varga, Jr transferred 4A19 to Varga Aircraft Corporation on August 23, 1976. Varga Aircraft Corporation transferred 4A19 to Montanair on December 11, 1986. Montanair transferred 4A19 to Augustair, Inc. on February 28, 1992. I. Model 2150 (Normal and Utility Categories), approved June 24, 1958 Engine Lycoming O-320-A2A Fuel 80/87 min. grade aviation gasoline Engine limits For all operations, 2700 r.p.m. (150 HP) Propeller and Sensenich M74DM propeller limits Static r.p.m.: Not over 2400, not under 2200. No additional tolerance permitted. Diameter: Not over 74 in., not under 72 in. Airspeed limits Normal and Utility Categories Never exceed 170 m.p.h. (147 knots) CAS Max. structural cruise 35 m.p.h. (117 knots) CAS Maneuvering 117 m.p.h. (102 knots) CAS Flaps extended 86 m.p.h. ( 75 knots) CAS C.G. range (+10.4) to (+17.5) (Normal and Utility Categories) Empty weight C.G. None Maximum weight 1817 lb. (Normal Category) 1570 lb. (Utility Category) 4A19 2 of 4 Model 2150 (cont’d) No. seats 2. 1 (+16.8) and 1 (+45.4) Maximum baggage 50 lb. (+68.8) Fuel capacity See NOTE 1 for data on unusable fuel. Oil capacity 8 qt. (-33.8) Serial Nos. eligible MS-1-P, FP-1 and up II. Model 2150A (Normal and Utility Categories), approved July 31, 1961. Same as for the Model 2150 except for engine installation, minor changes to nose gear, wheels and brakes, and interior arrangement. Engine Lycoming O-320-A2C Fuel 80/87 min. grade aviation gasoline Engine limits For all operations, 2700 r.p.m. (150 HP) Propeller and Sensenich M74DM propeller limits Static r.p.m: Not over 2400, not under 2200. No additional tolerance permitted. Diameter: Not over 74 in., not under 72 in. Airspeed limits Normal and Utility Categories Never exceed 170 m.p.h. (147 knots) CAS Max. structural cruise 135 m.p.h. (117 knots) CAS Maneuvering 117 m.p.h. (102 knots) CAS Flaps extended 86 m.p.h. ( 75 knots) CAS C.G. range (+10.4) to (+17.5) (Normal and Utility Categories) Empty weight C.G. None Maximum weight 1817 lb. (Normal Category) 1570 lb. (Utility Category) No. seats 2. 1 (+16.8) and 1 (+45.5) Maximum baggage 50 lb. (+68.8) Fuel capacity Two 17.5 gal. tanks (+19.6) See NOTE 1 for data on unusable fuel. Oil capacity 8 qt. (-33.8) Serial Nos. eligible SFP-11 and SP-12 through SP-45. These aircraft were produced by Shinn Engineering Company, Santa Ana, California, under licensing agreement with Morrisey Aviation Inc. VAC-50 and up. These aircraft were produced by Varga Aircraft Corporation, Chandler, Arizona. See NOTE 4. 4A19 3 of 4 III. Model 2180 (Normal and Utility Categories), approved February 12, 1981 Engine Lycoming O-360-A2D Lycoming O-360-A4D Fuel 91/96, 100/130 or 100 LL min. grade aviation gasoline Engine limits For all operations, 2700 r.p.m. (180 HP) - avoid continuous operation between 2150 and 2350 r.p.m. Propeller and Sensenich 76EM8-0-60 propeller limits Static r.p.m: 2700 r.p.m. Diameter: Minimum 76 in., Maximum 76 in. (No reduction for repair permitted) Airspeed limits Normal and Utility Categories Never exceed 170 m.p.h. (147 knots) CAS Max. structural cruise 135 m.p.h. (117 knots) CAS Maneuvering 117 m.p.h. (102 knots) CAS Flaps extended 86 m.p.h. ( 75 knots) CAS C.G. range Utility - (+10.4) to (+17.5) at 1570 lb. Normal - (+12.0) to (+17.5) at 1817 lb. - (+10.4) to (+17.5) at 1570 lb. Empty weight C.G. None Maximum weight 1817 lb. (Normal Category) 1570 lb. (Utility Category) No. seats 2. 1 (+16.8) and 1 (+45.5) Maximum baggage 50 lb. (+68.8) Fuel capacity Two 17.5 gal. tanks (+19.6) See NOTE 1 for data on unusable fuel. Oil capacity 8 qt. (-33.8) Serial Nos. eligible VAC-68-77, VAC-160 and up. These aircraft were produced by Varga Aircraft Corporation, Chandler, Arizona. See NOTE 4. DATA PERTINENT TO ALL MODELS Datum Wing leading edge Leveling means Top longitudinal longeron member in cockpit Control surface movements Elevator Up 16° + 1° Down 18° + 1° Aileron Up 12° + 1° Down 11° + 1° Rudder Right 29° + 1° Left 29° + 1° Flap Down 22° + 1° 4A19 4 of 4 Certification basis CAR 3 of May 15, 1956, with Amendments 3-1 and 3-2 (See NOTE 3.) Type Certificate No. 4A19 issued June 24, 1958. Application for Type Certificate dated February 12, 1958. Production basis None. Prior to original certification of each aircraft, a FAA representative must perform a detailed inspection for workmanship, materials, 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. In addition, the following items of equipment are required: (a) Stall warning indicator, Safe Flight No. 164 0.5 lb. (-2) (b) FAA Approved Airplane Flight Manual dated: (1) June 24, 1958 for Model 2150 (Morrisey) (2) July 28, 1961 for Model 2150A (Morrisey) (3) March 17, 1975 for Model 2150A (Varga), or later FAA approved revision (4) February 12, 1981 for Model 2180 (Varga) or later FAA approved revision NOTE 1. Current weight and balance report including list of equipment in certificated empty weight, and loading instructions when necessary, must be provided for each aircraft at the time of original certification. The unusable fuel has been determined to be of negligible value and may be neglected in the computation of the empty weight of the airplane. NOTE 2. The following placard must be displayed on the instrument panel in full view of the pilot: "OPERATE IN NORMAL OR UTILITY CATEGORY IN COMPLIANCE WITH THE APPROVED AIRPLANE FLIGHT MANUAL." NOTE 3. Models 2150 and 2150A will comply with CAR 3.705 when anti-collision lights are installed in accordance with Drawing MO-51000. NOTE 4. Serial numbers for airplanes produced by Varga Aircraft Corporation show “VAC” followed by a number and then the year of manufacture. Serial Number example: VAC-58-76 Serial number in Fiscal year of manufacturing consecutive order November 1 - October 31 Exceptions to this numbering for airplanes built by Varga Aircraft Corporation are VAC-50, VAC-51, and VAC-52. Serial number VAC-68-77 was converted from a Model 2150A into a Model 2180 by Varga Aircraft Corporation. .....END..... ``` ## ADs (10, in force first) - [AD 2010-04-14](https://openairdocs.org/ad/2010-04-14): Stabilizers · Augustair 2150, 2150A and 2180. Effective Mar 24, 2010 - [AD 2006-12-07](https://openairdocs.org/ad/2006-12-07): ECi cylinder assemblies · Aerostar AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 386 more. Effective Jul 11, 2006 - [AD 96-09-06](https://openairdocs.org/ad/96-09-06): Air Filter Assemblies · Maule Aerospace Technology 7ACA, 7ECA, 7FC and 180 more. Effective Jun 7, 1996 - [AD 82-08-04](https://openairdocs.org/ad/82-08-04): Elevator Horn Assembly · Augustair 2150A and 2180. Effective Apr 15, 1982 - [AD 81-20-02](https://openairdocs.org/ad/81-20-02): Vent Tube Assembly · Augustair 2150A. Effective Mar 15, 1982 - [AD 81-15-03](https://openairdocs.org/ad/81-15-03): Engine Inlet Air Filters · Replace existing engine induction air filter (Brackett Aero Filters STC SA693CE or SA71GL). Effective Jul 20, 1981 - [AD 80-13-08](https://openairdocs.org/ad/80-13-08): Throttle Movement · Augustair 2150 and 2150A. Effective Jun 27, 1980 - [AD 80-02-08](https://openairdocs.org/ad/80-02-08): Rudder Balance Attach Bolts · Augustair 2150 and 2150A. Effective Jan 21, 1980 - [AD 65-28-05](https://openairdocs.org/ad/65-28-05): Main Landing Gear Oleos · Augustair 2150 and 2150A. Effective Dec 21, 1965 - [AD 65-12-04](https://openairdocs.org/ad/65-12-04): Elevator Horn · Augustair 2150 and 2150A. Effective Jun 2, 1965 ## Registered aircraft by registry model (OpenAirDocs) - [Varga 2150A](https://openairdocs.org/model/varga-2150a): 86 aircraft (registry code 9350102) - [Morrisey 2150A](https://openairdocs.org/model/morrisey-2150a): 18 aircraft (registry code 5940204) - [Varga 2180](https://openairdocs.org/model/varga-2180): 12 aircraft (registry code 9350104) - [Morrisey 2150](https://openairdocs.org/model/morrisey-2150): 4 aircraft (registry code 5940202) - [Montanair SPIRIT 2180](https://openairdocs.org/model/montanair-spirit-2180): 2 aircraft (registry codes 0561855, 9350202) - [Morrisey-Shinn 2150-A](https://openairdocs.org/model/morrisey-shinn-2150-a): 1 aircraft (registry code 5940302) - [Varga 2150](https://openairdocs.org/model/varga-2150): 0 aircraft (registry code 9350101) ## STCs approved under this data sheet (52, first 50) - [STC SA12406WI](https://openairdocs.org/stc/SA12406WI): Installation of a Garmin AXIS Flight Display System. Garmin International Inc. - [STC SA04652CH](https://openairdocs.org/stc/SA04652CH): To allow use of 100R grade aviation fuel meeting Swift Fuel, LLC specification. Swift Fuels LLC - [STC SA00081NY](https://openairdocs.org/stc/SA00081NY): Installation of Iceman Aviation Supplies, Inc. Carburetor Ice Detector.. Alcor LLC - [STC SA02594SE](https://openairdocs.org/stc/SA02594SE): SkyView HDX Instrumentation and Autopilot System manufactured. Dynon Avionics - [STC SA01757WI](https://openairdocs.org/stc/SA01757WI): To allow the use of UL91 or UL94 (minimum) grade aviation fuel. Swift Fuels LLC - [STC SA04568CH](https://openairdocs.org/stc/SA04568CH): Installation of the uAvionix tailBeaconX, a tail mounted position light with integrated Automatic Dependent Surveillance - Broadcast (ADS-B) Out and 1090MHz Mode-S transponder functionality. uAvionix Corporation - [STC SA00410BO](https://openairdocs.org/stc/SA00410BO): Installation of an AV-30-C Multi-Mode Indicator. uAvionix Corporation - [STC SA01831WI](https://openairdocs.org/stc/SA01831WI): To allow the use of UL91 (minimum) grade aviation fuel. Petersen Aviation Inc - [STC SA02268CH](https://openairdocs.org/stc/SA02268CH): Installation of Airwolf Filter Corp. Air Oil Separator. Airwolf Filter Corporation - [STC SA01435SE](https://openairdocs.org/stc/SA01435SE): Installation of J.P. Instruments (JPI) Primary Engine Data Management System. J. P. Instruments - [STC SA00024NY](https://openairdocs.org/stc/SA00024NY): Installation of Airwolf remote mounted engine oil filter kit AFC-K007 on single or multi-engine fixed wing light aircraft incorporating Lycoming reciprocating engines of 450 horsepower or less.. Airwolf Filter Corporation - [STC SA2586NM](https://openairdocs.org/stc/SA2586NM): Installation of J.P. Instruments temperature monitoring systems.. J P Instruments - [STC SA02428SE](https://openairdocs.org/stc/SA02428SE): Installation of an Air Stream Switch for an electric time recording device on non-pressurized aircraft. Henry F Rogers/David E Polley - [STC SA02930NY](https://openairdocs.org/stc/SA02930NY): Installation of Insight Instrument Corporation Graphic Engine Monitor (GEM 610C) models G3, G2, and G1 and 1200C model G4 as primary Cylinder Head Temperature (CHT), Exhaust Gas Temperature (EGT), and Turbine Inlet Temperature (TIT) Instruments. Insight Instrument Corporation - [STC SA02283SE PAGE 2](https://openairdocs.org/stc/SA02283SE%20PAGE%202): Installation of Electronics International Inc. Glass Panel Engine Monitor (with In Flight Data) CGR-30P. Electronics International Inc. - [STC SA02402SE PAGE 2](https://openairdocs.org/stc/SA02402SE%20PAGE%202): Installation of Electronics International Inc. Glass Panel Engine Monitor (with In-Flight Data) CGR-30C. Electronics International Inc. - [STC SA00432SE](https://openairdocs.org/stc/SA00432SE): Installation of EGT 701 series fuel flow instrument.. J P Instruments - [STC SA00861SE](https://openairdocs.org/stc/SA00861SE): Installation of J.P. Instruments (JPI) fuel flow indicating system. J P Instruments - [STC SA00068SE](https://openairdocs.org/stc/SA00068SE): Installation of fuel flow/pressure instruments. (W/TSIO-360-MB1). Electronics International Inc. - [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 SA563CH](https://openairdocs.org/stc/SA563CH): Authorizes installation of engines equipped w/Unison Limited Authority Spark Advance Regulator (LASAR) ignition system w/Cylinder Head Temp. (CHT) monitoring capability on airframes. engines.. Champion Aerospace LLC - [STC SA593CH](https://openairdocs.org/stc/SA593CH): Install Champion SlickSTART magneto booster system.. Champion Aerospace LLC - [STC SA02033AT](https://openairdocs.org/stc/SA02033AT): Modification to install an air-oil separator to prevent oil from being aspirated from the engine breather line.. M-20 Oil Separators LLC - [STC SA4005NM](https://openairdocs.org/stc/SA4005NM): Precise Flight Inc. Pulselite Control System. Precise Flight Inc - [STC SA00680SE](https://openairdocs.org/stc/SA00680SE): Installation of Electronics International model UBG-16 or UBG-16T bar graph engine analyzer.. Electronics International - [STC SA2683NM](https://openairdocs.org/stc/SA2683NM): Installation of Precise Flight, Inc. stand-by vacuum system (SVS). Precise Flight Inc - [STC SA01157LA](https://openairdocs.org/stc/SA01157LA): Installation of Electronics International Model FP-5 or FP-5L fuel flow/fuel pressure instrument as a replacement instrument.. Electronics International Inc. - [STC SA01944CH](https://openairdocs.org/stc/SA01944CH): Modify airplane to fly on unleaded automotive gasoline, 87 minimum antiknock index, per ASTM Specification D-439 or D-4818 of any volatility class, A through E, or 82UL AVGAS per ASTM D-6227.. Experimental Aircraft Association Inc. - [STC SA870GL](https://openairdocs.org/stc/SA870GL): Superseded by STC SA01944CH. Modify airplane to fly on unleaded automotive gasoline, 87 minimum antiknock index.. EAA Aviation Foundation - [STC SA489EA](https://openairdocs.org/stc/SA489EA): Installation of ARP Inc. carburetor ice detection system. Aircraft & Rotorcraft Products (ARP) Inc - [STC SA09470SC](https://openairdocs.org/stc/SA09470SC): Installation of Starter Indicator light system.. Texas Skyways Inc - [STC SA02168AK](https://openairdocs.org/stc/SA02168AK): Installation of hourmeter airspeed switch. For unpressurized aircraft only. Pressurized aircraft must have pressurization system deactivated.. Avalaska Inc - [STC SA2687NM](https://openairdocs.org/stc/SA2687NM): Installation of Truboplus/ Electronics Int'l gauges and switches.. Aero Manufacturing Inc. - [STC SA71GL](https://openairdocs.org/stc/SA71GL): Installation of air filters. Brackett Aero Filters Inc. - [STC SA3203SO](https://openairdocs.org/stc/SA3203SO): Replacement of Cleveland brake disks, P/N 164-26A and/or 164-126A, with Appalachian Accessories stainless steel brake disks P/N 75-27.. Aviation Products, Inc - [STC SA00188AT](https://openairdocs.org/stc/SA00188AT): Installation of Appalachian Accessories carbon steel brake discs that have the melonite surface treatment, P/N AA-26A.. Aviation Products, Inc - [STC SA1626NM PAGE 2](https://openairdocs.org/stc/SA1626NM%20PAGE%202): 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 SA4309WE](https://openairdocs.org/stc/SA4309WE): Installation of tail wheel type landing gear.. Augustair, Inc - [STC SA4412NM](https://openairdocs.org/stc/SA4412NM): Installation of tail wheel type landing gear.. Augustair, Inc - [STC SA4445NM](https://openairdocs.org/stc/SA4445NM): Installation of tail wheel type landing gear, large rudder, Lycoming 0-360-A4D engine, Sensenich 76EM8-0-60 propeller and associated installation components.. Augustair Inc - [STC SA2350NM PAGE 2](https://openairdocs.org/stc/SA2350NM%20PAGE%202): Installation of Electronics International Inc digital carburetor/outside air temperature gauges. Electronics International - [STC SA4302NM](https://openairdocs.org/stc/SA4302NM): Installation of Electronics Int'l digital automatic engine analyzer.. Electronics International - [STC SA3862NM PAGE 2](https://openairdocs.org/stc/SA3862NM%20PAGE%202): Installation of Electronics International Primary TIT/EGT/CHT instruments, remote switches and associated accessories.. Electronics International - [STC SA1962CE](https://openairdocs.org/stc/SA1962CE): Operation on unleaded and/or leaded automotive gasoline.. Petersen Aviation Inc - [STC SA2190NM PAGE 2](https://openairdocs.org/stc/SA2190NM%20PAGE%202): Installation of electronics International Digital Volt/Amp Gauges and Accessories.. Electronics International - [STC SA5484SW](https://openairdocs.org/stc/SA5484SW): Install new engine cowling and 2-inch propeller spacer.. Lopresti Curtis - [STC SA334SW](https://openairdocs.org/stc/SA334SW): Installation of InterAv Alternator.. InterAv, Inc - [STC SA798EA](https://openairdocs.org/stc/SA798EA): Installation of Monitair exhaust gas combustion monitor kit.. Rosemount Engineering Co All 52: https://openairdocs.org/tcds/4A19/stcs.md --- 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.