TCDS TC 659

DOOL NO GETTE AERO RET AIRORAFT SРFО1F30/7200 An airorals confoming with authenticated data on file with the Oivil Aeronautics Adninistration will be iesued an airworthiness certificate upon shoving compliance with the terms of this spocification. Such certificate ahall incorporate the operation restrictions listed hereone Manufacturer Harlow Airero't Company Alhambra Airport Alhambra, California Model PJC-1 (SoO NOTE 3) PJC-2 Designation 204 POLI (See NOTE 4) Incine Harmor Super Scarab Series 00 or 501 Placard limits Maximum, except tate-off =- in, Ic., 2050 rum (145 hp) Tako-oft (one minute) -in, Ice, 2050 rpm (145 hp) Propeller Static IF et Maximum Pormissible throttle setting Not nore than 1690 lot less than 1690 (See 1OCB 4) Diamoter Let nore than 04 in. Tot less then 84 in. Placara specds Lovol Flight or clint 163 mph Ind. (See NOTE 4) Olide or divo 195 mph Inda (Sce LOT: 4) Flaps extorded 105 mph Ind. Puol capecity 31 gals, (One bank center section of wing) (450) Oil capacity & Gals. No. pacsengers (446) (Sce NOTE 4) 80 lbs. (Aft of pilot's coat) (477) (See item 301 and FOr! 4) Standard weight 2086 1ba, (Seo HOTE 4) C. G. limits (445.2) 15.02 210) & (452.7) (26.6% илс) нАС 67.8 10ng. Il. at (454.6), Lovoling neans: Raise tail until front wing shear beam is vertical. Specification basis Typo cersificcte No. 659 Seriel numbers 1 and up eligible (See HOTT A) EQUIP TIT: (Valucs in inches show in parenthesis after each item represent horizontal arms to C. G, of the item measured (minus) ahead and (plus) to the rear of firewall) (*tears not increase) Class I.. Reguired equipment which must be installed unless replaced by cither Olass Il or III equivalent items (such itoms then to be marked "required" on the mirorthiness certificate) subject to inspootion and 0, 0e check. 101e Propoller - fixed metal (Curtiss 55516-1 or 4) 100. Collector ring - Solar 12=413 14 Ibs. 100, Genorator (Belipse Type 809) and cortrol box 104, Bettery (Reading R 33L) 27 Ibsa (=3) 10% 21 in, streanline wheels (Air Assoc, 220-0) wibh bracos and 6 ply bires 57.5 2b3. 29) 100% 6 in, shroonline steerablo beil wheel and sire 3 Ibs. 216) 10. Two min landing coar shod stride A.P.T.I« 00025 46 206. 434) shook strut (Draming Do. 000) # 108051 11 288: (2213] ANI 97 CUCATION 10, 659 Pace 2 of 8 paces Tarlos NJC-1, 1302 Class II? Ophional equipment which ney be instalted or renovo?, subjoot to inspection and shock of C: Gs Loite. mits 200. Miscollaneous itens as noted in approved woight and balance report, 201. Cabin heater (Up. To, 1004) 202, Landing lights (S & 11 2001) 1 18. 08. (433) 203, Starter (Helipse Y-150) 204, Battery box (DwE. No. 1210) 4 I050 205% Generator - Mlectrical Developmont Type E-15 25 Amp. 12 V. 11 1bs. speor 206, Starter (Flectrical Development Type 10935 12V) (-G,5) 207, Battery pon (Droving Io. 1091) 208, 21" Strenaline wheels (Autofan 2100 2l) with brakes pooit and 6 ply tiros 50.5 10. 429) 200. Rear seet (Uraving Io. 1366) (See 10TE 4) seng! Class 1210 Optional equipment which nay be installed or removed, subject to inspootion only, except when the sirplane is already equipped with any Class 1l iton, in which casc a 0.G. check nust be ande for the effoct on 0. G, limits of the Class TIT ifem installas tion. (Note that when any Class II item is installed, all Class III items are in effect Class II itens.) 1 T22 301. Bagcego compartment (150 lbs, coposity replacing sta, comperiment.) (DrE. 1096) (473) TOIL A, Each airereft certificated must satisfactorily passs (a) An inspoction for worlmanship, materials and conformity beforo final assembly. (D) A finel inspection of tho completed airerafe, (c) A chock of flight charafteristics. NOTE 1, Eligible for export as follows, subject to inspoction for equirent specified in Chapter XII of Inspection Hendbook: (December 12, 1910) (a) Canada - Landplane Shiplane = not eligible, (b) All othor countries except Great Dritsin, Australia and licw Zealand, FOT! 2c The following placard must be conspicuously posted in full View of the pilot: "Intentionel spins prohibited with flaps and/or for 6o0r extended. " HOTT 3. Approval of model PJC-1 expired July 26, 1940. No aircraft of this nodel in existence. 28r1or 200-1, 200-2 For. A then iton 200 is installed, the follin: values should be usod: Placard spoods Level flight or elinb 150 mph Ind, Io. passengers Glide or dive 1(446) 2(486) 190 mph Ind, baccage Hone Standard weight 2600 Ibs. Propeller Static RP at maxim throttle sotting Lot nore then 1780 Hot less than 1740 Diametor: hot moro than 84" Tot loss than 84" SEE ALCO PARTIENT "AIMMORTIUESS HAITTELALOO INSPACTIOT HOTTS" I. P. Crews, Chief Aircraft Airmorchiness Section Billeyhugh: PV