I - Model UPF-7 2 POLB, Approved June 5, 1937
    (Same as Model YPF-7, ATC 586, except for engine installation).

Engine                   Continental W670K (See Item 325 for optional engines).
 
Fuel                     65 min. octane aviation gasoline

Engine limits            For all operations, 2175 rpm (225 hp)     

Airspeed limits          Level flight or climb    158 m.p.h. True Ind.
                         Glide or dive            214 m.p.h. True Ind.

Propeller limits         Maximum permissible diameter 99 in. (May be increased to 
                         102 in. with Item 313 installed). 

C.G. range               (-12.6) to (-4.0) 

Maximum weight           2650 lbs.  

No. seats                2 (1 (-4), pilot at (+38)) Eligible with a two-place front 
                         seat if installed in accordance with Waco Dwg. Nos. 23702    
                         to 23718, inclusive. (See NOTE 2).

Maximum baggage          25 lbs. (+69) (See NOTE 2 regarding 100 lbs. baggage 
                         capacity).

Fuel capacity            50 gals. (2 tanks in center section at 25 gals.) (-13)   

Oil capacity             4 gals. (-43)     

Control surface 
movements                Aileron             23° up          13° down
                         Elevator            40° up          17° down
                         Rudder              30° right       30° left

Serial Nos. eligible     4659 and up      

Required equipment       Items 101, 103, 104, 105 and 106.


 
 
 
 
 
 
 
 
 
 
 
 
 
 

II - Model VPF-7 2 POLB, Approved June 5, 1937
(Same as Model UPF-7 except engine. Empty weight approximately 10 lbs. greater).

Engine                   Continental W670M or M1
 
Fuel                     80 min. octane aviation gasoline

Engine limits            For all operations, 2175 rpm (240 hp M) or (250 hp M1)

Airspeed limits          Level flight or climb    158 m.p.h. True Ind.
                         Glide or dive            214 m.p.h. True Ind.

Propeller limits         Maximum permissible diameter 99 in. (May be increased to 
                         102 in. with Item 313 installed).

C.G. range               (-12.6) to (-4.0)

Maximum weight           2650 lbs.  

No. seats                2 (1 (-4), pilot at (+38)) Eligible with a two-place front 
                         seat if installed in accordance with Waco Dwg. Nos. 23702 
                         to 23718, inclusive. (See NOTE 2).

Maximum baggage          25 lbs. (+69) (See NOTE 2 regarding 100 lbs. baggage capacity).

Fuel capacity            50 gals. (2 tanks in center section at 25 gals.) (-13)

Oil capacity             4 gals. (-50)

Control surface 
movements                Aileron             23° up          13° down
                         Elevator            40° up          17° down
                         Rudder              30° right       30° left

Serial Nos. eligible     4659 and up 

Required equipment       Items 101, 103, 104, 105 and 106.

 
 
 
 
 
 
 

Specifications Pertinent to All Models

Datum                    Lower wing leading edge

Leveling means           Lower surface of upper wing at strut points.

Certification basis      Type Certificate No. 642 (Aero. Bulletin 7A requirements).

Production basis    None. Prior to original certification a CAA representative must
                    perform a detailed inspection for workmanship, materials, and
                    conformity with the approved technical data, and a check of the
                    flight characteristics.

Export eligibility Eligible for export to all countries except as follows subject to
                   the provisions of ASR 312 (MOP 2-4 contains the same information):

                         Canada - Landplane eligible
                                  Skiplane not eligible.

Equipment:         A plus (+) or minus (-) sign preceding the weight of an optional
                   items indicates the net weight change between that item and the
                   equivalent required item.

Propellers and Propeller Accessories

105. Propeller - Curtiss Model 55501 - Max. dia. 8'0" -
     must be installed with blades at right angles to engine
     crankthrow (either 90 or 270 degree position). Restrict engine
     operation to 2000 rpm maximum and placard tachometer accordingly. 54 lbs. (-77)

206 or 316. Propellers

     (a)  Fixed pitch wood                                           -12 lbs. (-77)
     (b)  Adjustable metal                                           +24 lbs. (-77)

Engines and Engine Accessories - Fuel and Oil System

101 or 307c. Starter (Eclipse E-80)                                  20 lbs. (-47)

203 or 307a & b. Starters

     (a)  (Hand inertia)                                              +2 lbs. (-47)
     (b)  (Eclipse F-141)                                            +10 lbs. (-47)

205 or 310. Engine shielding                                          11 lbs. (-60)

207 or 323. Engine ring cowl                                          28 lbs. (-61)

210 or 304. One or two extra 12-1/2 gallon fuel tanks in 
            upper wing                                            +15 lbs. ea. (-13)

305. 4-3/4 oil tank                                                No weight change

325. Engine, Continental (Model UPF-7 only)

     (a)  W670K1
          Engine limits - For all operations, 2200 rpm (230 hp)

     (b)  W670-6A or W670-6N
          Engine limits - For all operations, 2075 rpm (220 hp)

Landing Gear and Floats

103. 7.50-10 wheels (Hayes 750M) and tires                            60 lbs. (-24)

104. 10-1/2 in. streamline tail wheel                                  6 lbs. (+158)

208 or 301. Wheel streamlines      (a)  Pants                         23 lbs. (-23)
                                   (b)  Cuffs                          4 lbs. (-23)

209 or 314. Cactus Proof Tubes                                       +10 lbs. (-24)

313. 8.50-10 tires                                                    +5 lbs. (-24)

318. Tail wheel lock                                                   2 lbs. (+15)

324. 10 in. smooth contour tail wheel                                  5 lbs. (+158)

Specifications Pertinent to All Models (Cont.)

Landing Gear and Floats (Cont.)

326. Skis (Eligible on any airplane of these models provided the
     propeller installation meets the minimum 9 in. ground clearance.
     The maximum weight for the skiplane will be the same as for
     the corresponding landplane or that shown in parenthesis after
     each ski model, whichever is less)                              Use actual
                                                                     weight change
     (a)  Federal SA-6 (Maximum 3000 lbs.)
     (b)  Federal se-6 (Maximum 4600 lbs.)
     (c)  Federal SC-4 (Maximum 2850 lbs.)
     (d)  Federal SC-4B (Maximum 2850 lbs.)
     (e)  Richards Steel Ski (Maximum 4000 lbs.)

Electrical Equipment

102 or 309.    (a)  Battery (Exide 6-TS-13)                           42 lbs. (-37)
               (b)  Battery (Reading APL-11)                          25 lbs. (-37)

204 or 308. Generators

     (a)  (Eclipse LV-180)                                            18 lbs. (-47)
     (b)  (Eclipse G-2)                                               21 lbs. (-47)
     (c)  (Eclipse D-2)                                               26 lbs. (-47)

302. Landing lights (Grimes retractable)                             +11 lbs.

Interior Equipment
106 or 311. Seats

     (a)  Adjustable single front seat                                 8 lbs. (-4)
     (b)  Adjustable single rear seat                                  8 lbs. (+38)

211 or 303. Flares - Three 1-1/2 min.                                +17 lbs. (+100)

306. Miscellaneous extra instruments

     (a)  Front                                                       25 lbs. (-21)
     (b)  Rear                                                        25 lbs. (+15)

319. Parachutes or parachute type seats

320. Leather upholstering

321. Front cockpit cold air ventilator                                 5 lbs. t-48)

322. (a)  Front seat cushions                                          5 lbs. (-4)
     (b)  Rear seat cushions                                           5 lbs. (+38)

Miscellaneous (not listed above)

201. Miscellaneous items as noted in approved weight and balance report

312. Front cockpit cover                                              +6 lbs. (-4)

315. Coupe top                                                       +15 lbs. (+42)

317. Special paint                                                   +25 lbs. (+17)

327. Winter front                                                      8 lbs. (-68)

328. Blind flying hood (Dwg. No. 23649)                                3 lbs. (+38)

NOTES

NOTE 1.   

Current weight and balance report including list of equipment included in
certificated weight empty, and loading instructions when necessary, must be in
each aircraft at the time of original certification and at all times thereafter.

NOTE 2.   

Serial Nos. 4650 through 4658 eligible with upper wing dihedral, small center
section cut out, 2 passengers at (-4), baggage capacity of 100 lbs. (+69) and 
25 lbs. (-23), narrow type landing gear (approximately 75 in. tread) and minor
structural changes.

                                   - END -