# TCDS A44EU: Rust Robert E. - Type: Type certificate data sheet - Status: Current - Holder: Rust Robert E. - Revision: 2 - Revised: July 10, 2014 - Product: Aircraft, Small Airplane - Certification basis: Part 21 - Data sheet PDF: https://openairdocs.org/files/sha256/6d/ac/6dac730a5a2dc7f2c361a5a1a8c7f60b08a95afda6c808eb7df906902203d4d3 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/3EAABC2CCEAF66AD86257D18006BBA37.0001 - Page: https://openairdocs.org/tcds/A44EU ## Models (3) As the data sheet lists them. - DHC-1 Chipmunk Mk 21 - DHC-1 Chipmunk Mk 22A - DHC-1 Chipmunk Mk 22 ## 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. 2 2 2 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION A44EU Revision 2 Rust (de Havilland) DHC-1 Chipmunk Mk 21 Mk 22 Mk 22A July 10, 2014 TYPE CERTIFICATE DATA SHEET NO. A44EU This data sheet which is a part of Type Certificate No. A44EU 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 Robert E. Rust, Jr. 2382 Highway 92 South Fayetteville, Georgia 30215 Type Certificate Holder Record Robert E. Rust transferred TC A44EU to Robert E. Rust, Jr. September 30, 2005 I. Model DHC-1 Chipmunk Mk 21, 2 PCLM, (Normal and Utility Category), approved November 18, 1977. Model DHC-1 Chipmunk Mk 22A, 2 PCLM, (Normal and Utility Category), approved November 18, 1977. (Model names were misidentified in Revisions 0 and 1 of this data sheet and in airworthiness directives as DH.C1 Chipmunk 21 and DH.C1 Chipmunk 21A.) Engine Rolls-Royce (1971) Ltd. Gipsy Major 10 MK2 Fuel Minimum grade 80 octane (maximum lead content 4.58 milliliters TEL/US gallon) Engine limits Maximum takeoff 2,550 rpm (145 bhp) (5 minutes limit) full throttle. Maximum continuous (sea level) 2400 rpm (142 bhp) Maximum weak mixture, 3000 ft. and above (26 in Hg) 2300 rpm (120 bhp) Maximum overspeed (20 seconds), full throttle 2675 rpm Propellers Fairey Aviation Ltd. A66753/X1 Diam. (ft.) 6.75 Pitch (ft.) 5.01 A67889 Diam. (ft.) 6.75 Pitch (ft.) 5.01 D104967/X1 Diam. (ft.) 6.75 Pitch (ft.) 5.01 Airspeed limits (IAS) Never exceed 155 knots (179 mph) Maneuvering speed 117 knots (135 mph) Wing flaps shall not be extended above 93 knots (107 mph) nor beyond 15° position at greater than 71 knots (82 mph). C.G. range (-6.8 inches) to (-0.77 inches) Distances shown are plus (+) behind and minus (-) ahead of the datum. Empty weight C.G. range None Maximum weight 2100 lb. No. of seats 2 (1 at 0.0 inches and 1 at +33.6 inches) A44EU 2 Maximum baggage 40 lb. in fuselage locker at +50.0 inches Fuel capacity 28.8 U.S. gallons (24 Imp gallons) at -12.0 inches, one tank of 14.4 U.S. gallons (12 Imp gallons) in each wing Oil capacity 2.4 U.S. gallons (2.0 Imp gallons) at -45.6 inches. Control surface Ailerons Up 21° ± 2° Down 16° ± 2° Flaps Takeoff 15° ± 3° Landing 30° ± 3° Elevators Up 38° ± 2° Down 15° ± 2° Rudder 31° ± 2° Left and right of center line II - Model DHC-1 Chipmunk Mk 22, 2 PCLM, (Normal and Utility Category), Approved November 18, 1977. (Model name was misidentified in Revisions 0 and 1 of this data sheet and in airworthiness directives as DH.C1 Chipmunk 22.) This aircraft is identical to the DHC-1 Chipmunk Mk 21 and Chipmunk Mk 22A except for revised fuel capacity as follows: Fuel capacity 21.6 U.S. gallons (18 Imp gallons) at -12.0 inches, one tank of 10.8 U.S. gallons (9 Imp gallons) in each wing DATA PERTINENT TO ALL MODELS Datum 42.0 inches aft of the firewall measured on the horizontal datum line. Leveling means Longitudinal: Straight-edge across two pegs at port side of front cockpit 7.0 inches below top of longeron and 6.0 inches and 42.0 inches aft of the firewall, or when pegs not fitted, use top surface of either canopy rail. Lateral: Straight edge across canopy rails at front cockpit. Import requirements A U.S. Airworthiness Certificate may be issued on the basis of a United Kingdom Certificate of Airworthiness for Export in the General Purpose Category signed by a representative of the Civil Aviation Authority containing the following statement: “The aircraft covered by this certificate has been examined, tested, and found to meet the airworthiness requirements of the United Kingdom current at the time of first application for a United Kingdom Certificate of Airworthiness in respect of a DHC-1 Chipmunk aircraft and conforms to U.S. Type Certificate No. A44EU. Certification basis 14 CFR Part 21.29 (FAA letter of January 19, 1977). Type Certificate No. A44EU issued November 18, 1977. Date of application for Type Certificate, August 23, 1977. Serial Nos. eligible C1-0198, C1-0281, C1-0390, C1-0482, C1-0611, C1-0615, C1-0710, C1-0713, C1-0714, C1-0748, C1-0824, C1-0895, and C1-0907. Other serial numbers will only be eligible by amending type certificate A44EU through the FAA Atlanta Aircraft Certification Office. Serial numbers which could potentially be added are C1-001 through C1-1014 (all of United Kingdom manufacture only). A United Kingdom Certificate of Airworthiness for Export endorsed as noted under Import Requirements, must be submitted for each individual aircraft for which application for a U.S. Airworthiness Certificate is made. The UK Certificate of Airworthiness for Export is valid as a basis for issuance of the U.S. Airworthiness Certificate for a period of 60 days. If application for U.S. certification is made after 60 days from the date of issuance of the UK export certificate, this certificate must be reissued. 3 A44EU Equipment The basic required equipment as prescribed in the applicable airworthiness regulations (see Certification Basis) must be installed in the aircraft for certification. Engine Accessories Weight Arm Starter*, Type S7 MK2 (Coffman) Plessy Part No. CK2821, (Post Modification H.22) 20 lb. (-45) or Starter*, electric, Rotax Part No. CO 225 (Post Modification H85) 18 lb. (-45) *Optional equipment alternative to hand starting. Generator, Rotax Part No. B.1804 11 lb. (-48) Vacuum pump, Plessey Part No. B3X MK1 5 lb. (-54) Landing Gear Wheels, Dunlop Part No. AH9389 or Dunlop Part No. AH51981 (post modification H260) 6 lb. (+22) Tires, Dunlop Part No. 1A-TR19 size 6.00 -6 1/2, or Dunlop Part No. DB 3065 or DN 3065 size 6.00 - 6 1/2 5 lb. (+22) Tube Dunlop Part No. 1A-3 2 lb. (+22) Hydraulic Brakes, Dunlop Part No. AH9220 2 lb. (+22) Tail Wheel, Dunlop Part No. AHO 5047 2 lb. (+186) or Dunlop Part No. AH9869 2 lb. (+186) Tire, Dunlop Part No. WP-R11 size 3.00 - 3 1/2 2 lb. (+186) Tube, Dunlop Part No. WP-2 1 lb. (+186) Electrical Equipment Batteries 2 of 12 v 15AH (lead acid) 43 lb. (+78) Service Information Service bulletins, structural repair manuals, vendor manuals, AFMs, and overhaul and maintenance manuals, which contain a statement that the document is approved by the United Kingdom Civil Aviation Authority, are accepted by the FAA and are considered FAA approved. (These approvals pertain to the design data only). 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. NOTE 2 The following placards must be displayed: Those placards which are required to be displayed in accordance with the UK Civil Aviation Authority Flight Manual for the DHC-1 Chipmunk Mk 21 (or DHC-1 Chipmunk Mk 22 or DHC-1 Chipmunk Mk 22A when applicable). NOTE 3 The safe fatigue lives determined in accordance with the aircraft manufacturer’s (de Havilland Support Limited) Technical News Sheet CT(C1) No. 138 Issue 6 must not be exceeded. NOTE 4 Aerobatics, including spinning, as specified in the UK Civil Aviation Authority approved Flight Manual may only be performed when Modification H.231 is installed (for spin recovery refer to the Flight Manual). NOTE 5 The aircraft must be operated in compliance with the UK Civil Aviation Authority approved Flight Manual for DHC-1 Chipmunk Mk 21 (or DHC-1 Chipmunk Mk 22 or DHC-1 Chipmunk Mk 22A) with FAA Supplement dated November 18, 1977 (Noise). NOTE 6 When a propeller of other than 6.75 to 6.76 feet diameter and other than 5.01 feet pitch is fitted, the performance data in the Flight Manual is not valid. NOTE 7 The aircraft must be assembled in accordance with the instructions in the de Havilland Chipmunk Maintenance and Repair Manual Publication C.M.R.-1 and must be flight checked after assembly. ...END... ``` ## ADs (1, in force first) - [AD 2022-03-15](https://openairdocs.org/ad/2022-03-15): Fuel Quantity Indicator · Garmin G3X Touch Electronic Flight Instrument System (STC SA01899WI or SA02658SE). Effective Mar 21, 2022 ## STCs approved under this data sheet (60, first 50) - [STC SA01800SE](https://openairdocs.org/stc/SA01800SE): Fabrication and installation of new or replacement of existing instrument panel lights dimmer control.. TCW Technologies, LLC - [STC SA01861SE](https://openairdocs.org/stc/SA01861SE): Fabrication and installation of Landing Light Controller. TCW Technologies, LLC - [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 SA02738CH](https://openairdocs.org/stc/SA02738CH): Installation of L-3 Communications Avionics Systems. Acron Aviation Inc. - [STC SA04046CH PAGE 1](https://openairdocs.org/stc/SA04046CH%20PAGE%201): Installation of L-3 GENESIS (TM) Electronic Standby Instrument System (ESI-500/MAG-500). Acron Aviation Inc. - [STC SA03898NY](https://openairdocs.org/stc/SA03898NY): Installation and maintenance of ORATEX covering and coating material. Aircraft Design & Certification Ltd - [STC SA4503NM](https://openairdocs.org/stc/SA4503NM): Remove original cloth covering and install Ceconite covering. Ceconite Division of Poly-Fiber Inc. - [STC SA02658SE](https://openairdocs.org/stc/SA02658SE): Installation of Garmin GI 275 Multi-Function Display System. Garmin International Inc. - [STC SA1011SO](https://openairdocs.org/stc/SA1011SO): Installation of Cleveland main wheels and brakes.. Kaman Corporation Aircraft Wheel and Brake LLC - [STC SA01967WI](https://openairdocs.org/stc/SA01967WI): Use of GAMI G100UL High Octane Unleaded Avgas. General Aviation Modifications Inc. - [STC SA04776NY](https://openairdocs.org/stc/SA04776NY): The HIPEC Covering and Finishing System must be performed and maintained. HIPEC Aircraft Coatings Inc. - [STC SA02444AK](https://openairdocs.org/stc/SA02444AK): Approval of the L-3 Communications NGT 9000/9000R ADS-B system installed. ADS-B Technologies LLC - [STC SA11174SC PAGE 2](https://openairdocs.org/stc/SA11174SC%20PAGE%202): Installation of BendixKing by Honeywell KSN 770 and KSN 765 WAAS LPV approach capable nav/comm systems. Honeywell International Inc (Bendix King) - [STC SA10822SC](https://openairdocs.org/stc/SA10822SC): Installation of EFD1000 Primary Flight Display. Aspen Avionics Inc. - [STC SA00401BO](https://openairdocs.org/stc/SA00401BO): Installation of a SkyTrax100B UAT receiver. Avidyne Corporation - [STC SA10236SC](https://openairdocs.org/stc/SA10236SC): Installation of a GDC 31 Roll Steering Converter. DAC International Inc - [STC SA04165NY](https://openairdocs.org/stc/SA04165NY): Installation of Latitude Technologies Skynode S200 Satcom system must be performed. Latitude Technologies Corporation - [STC SA01933LA-D](https://openairdocs.org/stc/SA01933LA-D): Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System. Garmin International Inc - [STC SA00382BO](https://openairdocs.org/stc/SA00382BO): Installation of Globalstar Antenna and Cradle provisions to support a Globalstar GPS-1700 in non-composite airplanes. Avidyne Corporation - [STC SA00343BO](https://openairdocs.org/stc/SA00343BO): Installation of a single configuration or a dual configuration Avidyne Corporation Integrated Flight Display, Model IFD540 loaded with Release 10.0 software (or later FAA approved release). Avidyne Corporation - [STC SA00352BO PAGE 2](https://openairdocs.org/stc/SA00352BO%20PAGE%202): Installation of an Avidyne Corporation Mode A/C/S Transponder with ADS-B Out capability, Model AXP340 loaded with Version 3.13 software (or later FAA approved version),. Avidyne Corporation - [STC SA02119SE PAGE 1](https://openairdocs.org/stc/SA02119SE%20PAGE%201): Installation of Garmin GDL 88 ADS-B UAT Transceiver System. Garmin International Inc - [STC SA00192LA](https://openairdocs.org/stc/SA00192LA): Replacement of BTH AG4 impluse and nonimpulse magnetos with Slick Magnetos on Gipsy I, Gipsy II, and Gipsy III model engines and Gipsy major series 1 through 10MK2 model engines.. Moth Aircraft Company - [STC SA3216NM](https://openairdocs.org/stc/SA3216NM): Modification of DeHavilland piston P/N 2200-25/2.. Moth Aircraft Company - [STC SA00478CH](https://openairdocs.org/stc/SA00478CH): Installation of Cooper Superflite 102 Fabric.. Aviation Products Systems Inc. - [STC SA01229SE PAGE 1](https://openairdocs.org/stc/SA01229SE%20PAGE%201): Installation of GNS 480 (CNX80) GPS WAAS Navigator with integrated VHF Navigation and Communication radios. Garmin International Inc - [STC SA02442AK PAGE 1](https://openairdocs.org/stc/SA02442AK%20PAGE%201): Approval of the L-3 Communications NGT 2000/2500 ADS-B system. ADS-B Technologies, LLC - [STC SA01933LA-D PAGE 1](https://openairdocs.org/stc/SA01933LA-D%20PAGE%201): Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System. Garmin International 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 SA02717NY PAGE 1](https://openairdocs.org/stc/SA02717NY%20PAGE%201): Installation of VoiceFlight Systems LLC VFS101 Speech Recognition Module. VoiceFlight Systems LLC - [STC SA02825NY PAGE 1](https://openairdocs.org/stc/SA02825NY%20PAGE%201): Installation of Aerospace Logic Aircraft Instruments. Aerospace Logic Inc. - [STC SA03148NY](https://openairdocs.org/stc/SA03148NY): The installation of the Latitude Technologies Corporation S100 Tracking System. Latitude Technologies Corporation - [STC SA01487SE-D](https://openairdocs.org/stc/SA01487SE-D): Installation of a GDL 69 or GDL 69A XM Satellite Receiver. Garmin International Inc - [STC SA00243BO](https://openairdocs.org/stc/SA00243BO): Installation of Centurion Consulting, Inc. GPS Steering Assist Module (SAM) with roll steering (p/n 0025-5100), or without roll steering (p/n 0025-5200).. Icarus Avionics, LLC - [STC SA00068SE](https://openairdocs.org/stc/SA00068SE): Installation of fuel flow/pressure instruments. (W/TSIO-360-MB1). 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 SA01473SE](https://openairdocs.org/stc/SA01473SE): Installation of a GTX 32 (mode C), GTX 33 (mode S), or GTX 33D (mode S with diversity) Remote Transponde. Garmin AT Inc. - [STC SA01695SE](https://openairdocs.org/stc/SA01695SE): Installation of an antenna. Garmin AT Inc. - [STC SA01487SE](https://openairdocs.org/stc/SA01487SE): Installation of a GDL 69 or GDL 69A XM Satellite Receiver in accordance with Garmin Supplemental Type Certificate Master Data List, P/N 005-C0217-00, Revision A, dated December 20, 2004, or later FAA approved revision.. Garmin AT 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 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 SA02154AK](https://openairdocs.org/stc/SA02154AK): Installation of the UPS Aviation Technologies Inc. Apollo MX20 multi-function display, P/N 430-0270-500.. Garmin AT Inc. - [STC SA02217AK](https://openairdocs.org/stc/SA02217AK): Installation of Garmin AT Model GDL90 UAT Data Link System, in accordance with Garmin AT, Inc., GDL 90 UAT Master Data List, P/N 560-0278-01, Revision A, dated November 12, 2004, or later FAA approved revision.. Garmin AT Inc. - [STC SA1362GL](https://openairdocs.org/stc/SA1362GL): Surrendered and incorporated into STC SA00478CH.. Cooper Aviation Supply Company, 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 SA2350NM PAGE 2](https://openairdocs.org/stc/SA2350NM%20PAGE%202): Installation of Electronics International Inc digital carburetor/outside air temperature gauges. Electronics International All 60: https://openairdocs.org/tcds/A44EU/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.