# TCDS A5PC: Williams Harry E. - Type: Type certificate data sheet - Status: Current - Holder: Williams Harry E. - Revision: 0 - Revised: August 15, 1968 - Product: Aircraft, Small Airplane - Certification basis: Part 21 - Registered aircraft: 8, by the registry models matched to it (OpenAirDocs) - Data sheet PDF: https://openairdocs.org/files/sha256/85/f1/85f1d01e1876933c36da125277a57eef6f1a9414f6f90bc2f6853c1a2eb84c70 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/70D05D0C0F37C51585256732006206A8.0001 - Page: https://openairdocs.org/tcds/A5PC ## Models (1) As the data sheet lists them. - DH 82A ## 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. - - - - Reformatted 1/95. FEDERAL AVIATION ADMINISTRATION A5PC DE HAVILLAND DH 82A August 15, 1968 TYPE CERTIFICATE DATA SHEET NO. A5PC This data sheet which is a part of type certificate No. A5PC 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 Harry E. Williams 5 N.W. Road Randolph AFB, Texas 78148 I - De Havilland (Australia) Model DH 82A 2POLB (Normal and Utility Category), approved August 5, 1968 Engine Bristol Siddeley Gipsy Major 1 or 1F or 1C or 1J General Motors - Holden's Gipsy Major 1 Fuel Gipsy Major 1 - Minimum grade 69 Octane, lead content - nil. (Fuels containing not more than 3.33 mls. Tetra Ethyl lead/U.S. gallon may be used provided aluminum alloy cylinder heads, or aluminum-bronze cylinder heads modified to incorporate steel exhaust valve seat inserts, are installed.) Gipsy Major 1F - Minimum grade 69 Octane, containing not more than 3.33 mls. Tetra Ethyl lead/U.S. gallon. Gipsy Major 1C - Minimum grade 77 Octane, containing not more than 3.33 mls. Tetra Ethyl lead/U.S. gallon. Gipsy Major 1J - Minimum grade 80 Octane, containing not more than 3.33 mls. Tetra Ethyl lead/U.S. gallon. Engine limits Gipsy Major 1 - Maximum takeoff and climb (60 minutes limit): and 1F 2100 rpm (122 bhp) Maximum continuous (sea level) 2100 rpm (112 bhp) Maximum overspeed, full throttle (5 minutes limit) 2400 rpm Gipsy Major 1C - Maximum takeoff and climb (60 minutes limit): 2100 rpm (130 bhp) Maximum continuous (sea level) 2100 rpm (120 bhp) Maximum overspeed, full throttle (5 minutes limit): 2400 rpm Gipsy Major 1J - Maximum takeoff and climb (60 minutes limit): 2400 rpm (142 bhp) Maximum continuous (sea level) 2300 rpm (138 bhp) Maximum overspeed, full throttle (5 minutes limit): 2550 rpm A5PC 2 Propellers Manufacturer Gipsy Major 1, 1F and 1J Diameter (ft.) Pitch (ft.) Geo Adams and Son A16 6.33 5.25 " A37 6.58 4.58 " A44 6.50 4.58 " A49 6.75 4.17 " DH5220/H/26 6.33 4.92 De Havilland DH5212/D 6.17 5.42 " DH5218/B 6.50 5.10 " DH5220/B 6.33 5.08 " DH5220/G 6.33 4.58 " DH5220/H 6.33 4.92 " DH5220/K 6.33 5.00 " DH5220/L 6.33 4.75 " DH5220/M 6.33 4.50 " DH5220/P 6.33 4.58 " DH5232/A 6.50 5.10 " DH5232/B 6.50 5.30 Lang Propellers LA506/3 6.50 4.35 " LA594/2 6.50 4.35 " LA596 6.50 5.00 " LA604 6.50 4.58 Perfectus Airscrew Co. F5 6.17 5.42 " PA-1 6.33 5.25 " PA12 6.33 4.92 " PA13 6.33 4.75 " PA14 6.33 4.58 " PA15 6.50 4.58 " PA20 6.42 5.25 " PA21 6.50 5.25 " PA22 6.50 4.33 " PA25 6.66 4.08 " PA31 6.75 4.50 " PA44-08 6.75 4.08 " PA44-33 6.50 4.33 " PA44-75 6.33 4.75 " PA44-92 6.33 4.92 " PA44-425 6.33 5.25 " PA44-525 6.42 5.25 " PA44-625 6.50 5.25 " PA44-658 6.50 4.58 " PA44-992 6.75 3.86 Airscrew Co. ZD5220/1 6.33 4.83 " Z973 6.23 5.50 " Z3101/1 6.42 5.22 Fairey Reed A66016/X4 7.00 4.58 " C66969/X1 5.92 4.50 " 67104A/X4 7.00 4.77 " 67104A/X7 7.00 4.71 " 67104A/X10 7.00 4.60 " 67104A/X14 7.00 4.52 " 67575A/X1 7.00 4.71 " 84723A/X1 7.00 4.84 " 94234A/X1 6.20 5.85 Gipsy Major 1C De Havilland DH5220/P 6.33 4.58 Airscrew Co. Z8010 6.84 3.53 Fairey Reed B104951/X2 6.75 5.02 " A66875/X4 6.50 5.84 3 A5PC Airspeed limits (IAS) Never exceed 139 knots (160 m.p.h.) C.G. range (+10.2) to (+16.5) when anti-spinning strakes not fitted (+10.2) to (+17.0) when anti-spinning strakes are fitted Empty weight C.G. range None Datum Leading edge of the lower mainplane at the root, which is 14.2 inches aft of the front levelling stud on the right hand side of the front fuselage (joint E). Leveling means Longitudinal: Straight-edge on the studs on the outside of the fuselage right hand top longeron. Lateral: Straight-edge clamped to underside of left hand and right hand top longerons in the front cockpit. Maximum weight 1825 lb. normal category 1770 lb. utility category No. of seats 2 (1 at +17.0, 1 at +49.0) Maximum baggage 60 lb. (+76.0) Fuel capacity 22.8 U.S. gal. (1 tank in upper mainplane at -5.8) 12 U.S. gal. or 14.4 U.S. gal. auxiliary (1 tank in fuselage at -8.2) Oil capacity 2.5 U.S. gal. (-9.5) Control surface movements Elevator: Up 11 1/2 + 3/4 inches at T.E. Down 8 + 1/2 inch at T.E. Rudder: 14 1/2 inches left and right at T.E. Aileron: 8 inches up at T.E. 1 1/4 inches down at T.E. Slat travel: 3 1/4 inches ertification basis FAR 21.29 (FAA letter of February 6, 1968) Type Certificate No. A5PC issued August 5, 1968 Date of application for Type Certificate - July 7, 1968 Import requirements A U.S. Airworthiness Certificate may be issued on the basis of an Australian Certificate of Airworthiness for Export signed by the Director-General of Civil Aviation or his authorized delegate containing the following statement: "The aircraft covered by this Certificate has been examined and found to meet the airworthiness requirements of the Commonwealth of Australia current at the time of certification of the first of the type in Australia and has been modified to comply with all Air Navigation Orders requiring its modification as a condition of the continued validity of its Certificate of Airworthiness. The aircraft conforms to Type Certificate No. A5PC." Serial Nos. eligible An Australian 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 Australian Certificate of Airworthiness for Export is valid as a basis for issue of the U.S. Airworthiness Certificate for period of 60 days. If application for U.S. certification is made after 60 days from the date of issue of the Australian export certificate, this certificate must be reissued. Equipment The basic required equipment as prescribed in the applicable airworthiness regulations (see "Certification basis") must be installed in the aircraft for certification. 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: (1) "Speed must not exceed 139 knots (160 m.p.h.)" (2) Engine limitations: (a) Gipsy Major 1 and 1F. "Normal Full r.p.m. 2100 Max. permissible for not more than 5 mins. 2400 r.p.m." (b) Gipsy Major 1C "Normal full r.p.m. 2100 Max. permissible for not more than 5 mins. 2400 r.p.m." (c) Gipsy Major 1J "Normal full r.p.m 2400 Max. permissible for not more than 5 mins. 2550 r.p.m." (3) "Smoking prohibited" A5PC 4 (4) "Normal Category. Maximum design weight 1825 lbs. No acrobatic maneuvers including spins approved." (5) "Utility Category. Maximum design weight 1770 lbs. No acrobatic maneuvers approved except those listed below. Maneuver Entry Speed Chandelles 105 knots (120 m.p.h.) Lazy eights 105 knots (120 m.p.h.) Steep turns 80 knots ( 92 m.p.h.) Stalls (except whip stalls) Slow deceleration Spins Slow deceleration (6) "Maximum baggage 60 lbs. For additional loading instructions, see Weight and Balance Data." NOTE 3. The aircraft must be assembled in accordance with the rigging instructions of the De Havilland Maintenance Manual. NOTE 4. The aircraft must be flight checked after assembly. .....END..... ``` ## ADs (2, in force first) - [AD 2014-24-01](https://openairdocs.org/ad/2014-24-01): Fuselage, Wing Attach Fittings · de Havilland D.H.83 Fox Moth, D.H.82A Tiger Moth and DH 82A. Effective Jan 6, 2015 - [AD 2014-17-09](https://openairdocs.org/ad/2014-17-09): Fuselage, Wing Attach Fittings · Williams Harry E. D.H.83 Fox Moth, D.H.82A Tiger Moth and DH 82A. Effective Sep 18, 2014 ## Registered aircraft by registry model (OpenAirDocs) - [Dehavilland DH82A](https://openairdocs.org/model/dehavilland-dh82a): 8 aircraft (registry code 2800101) - [Morris Motors DH82A](https://openairdocs.org/model/morris-motors-dh82a): 0 aircraft (registry code 2802711) ## STCs approved under this data sheet (9) - [STC SA04652CH](https://openairdocs.org/stc/SA04652CH): To allow use of 100R grade aviation fuel meeting Swift Fuel, LLC specification. Swift Fuels LLC - [STC SA01967WI](https://openairdocs.org/stc/SA01967WI): Use of GAMI G100UL High Octane Unleaded Avgas. General Aviation Modifications 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 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 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 SA4005NM](https://openairdocs.org/stc/SA4005NM): Precise Flight Inc. Pulselite Control System. 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. --- 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.