# TCDS A-688: National Aeronca Association

- Type: Type certificate data sheet
- Status: Current
- Holder: National Aeronca Association
- Revision: 2
- Revised: March 7, 2005
- Product: Aircraft, Small Airplane
- Registered aircraft: 3, by the registry models matched to it (OpenAirDocs)
- Data sheet PDF: https://openairdocs.org/files/sha256/c7/98/c79813b0dbe54b5d30c6b44e8e5a694569e654274c16e09b6f596942991a72a9
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/0AEE66147D49C68C8625746A005B6D6F.0001
- Page: https://openairdocs.org/tcds/A-688

## Models (3)

As the data sheet lists them.

- 50-F
- KF
- S-50F

## What the data sheet says

From the PDF's text layer, line by line; tables lose their columns. The PDF is the record.

```text
DEPARTMENT OF TRANSPORTATION 
FEDERAL AVIATION ADMINISTRATION 
 
A-688 
Revision 2 
AERONCA 
KF 
50-F 
S-50-F 
March 7, 2005 
AIRCRAFT SPECIFICATION NO. A-688
 
Type Certificate Holder National Aeronca Association 
  806 Lockport Road 
  P.O. Box 2219 
  Terre Haute, IN  47802 
 
Name change from Aeronca to National Aeronca Association March 7, 2005. 
 
I - Model KF, 2 PCLM, Approved June 28, 1938.
 
 Engine  Franklin 4AC-150 Series 50 
 Engine limits  Maximum, except takeoff   -- in. Hg., 2300 rpm (50 hp) 
   Takeoff (one minute) -- in. Hg., 2300 rpm (50 hp) 
 Airspeed limits  Level flight or climb - 100 mph True Ind. 
    Glide or dive  -- 135 mph True Ind. 
 Propeller  Maximum permissible diameter 81 in. 
 C.G. range (+13.4) to (+20.5) 
 Empty weight 
  C.G. range (See Note 3) (+14.0) to (+20.4)  (Item 310 not installed.) 
    (+14.0) to (+18.2)  (Item 310 installed.) 
 Maximum weight 1150 lbs. 
 Number of Passengers 1 (+21) 
 Maximum baggage 40 lbs. (aft of seat) (+45) 
 Fuel capacity  10 gallons (-10) 
 Oil capacity 1 gallon (-31) 
 Serial Nos. eligible KF-1 and up manufactured prior to 12-11-42 eligible.  Approval expired as of  that date. 
 
II - Model 50-F, 2 PCLM, Approved October 3, 1938.
 (Same as model KF except for wider cabin.  No structural changes.) 
 
 Engine  Franklin 4AC-150 Series 50 
 Engine limits  Maximum, except takeoff   -- in. Hg., 2300 rpm (50 hp) 
   Takeoff (one minute) -- in. Hg., 2300 rpm (50 hp) 
 Airspeed limits  Level flight or climb - 100 mph True Ind. 
    Glide or dive  -- 135 mph True Ind. 
 Propeller  Maximum permissible diameter 81 in. 
 C.G. range (+13.4) to (+20.5) 
 Empty weight 
  C.G. range (See Note 3) (+14.5) to (+20.7)  (Item 310 not installed.) 
    (+14.5) to (+18.5)  (Item 310 installed.) 
 Maximum weight 1150 lbs. 
 Number of Passengers 1 (+21) 
 Maximum baggage 40 lbs. (aft of seat) (+45) 
 Fuel capacity  12 gallons (-10) 
 Oil capacity 1 gallon (-31) 
 Serial Nos. eligible F-1018 and up manufactured prior to 12-11-42 eligible.  Approval expired as of that date.

A-688  Page 2 of 3 
 
III - Model S-50-F, 2 PCLM, Approved October 3, 1938.
 
 Engine  Franklin 4AC-150 Series 50 
 Engine limits  Maximum, except takeoff   -- in. Hg., 2300 rpm (50 hp) 
   Takeoff (one minute) -- in. Hg., 2300 rpm (50 hp) 
 Airspeed limits  Level flight or climb - 95 mph True Ind. 
    Glide or dive  -- 129 mph True Ind. 
 Propeller  Maximum permissible diameter 76 in. 
 C.G. range (+14.3) to (+21.4) 
 Empty weight 
  C.G. range (See Note 3) (+15.0) to (+21.0)  (Item 310 not installed) 
    (+15.0) to (+18.8)  (Item 310 installed.) 
 Maximum weight 1253 lbs. 
 Number of Passengers 1 (+21) 
 Maximum baggage 40 lbs. (aft of seat) (+45) 
 Fuel capacity  12 gallons (-10) 
 Oil capacity 1 gallon (-31) 
 Serial Nos. eligible F-1018 and up manufactured prior to 12-11-42 eligible.  Approval expired as of that date. 
 
Specifications Pertinent to all Models
 Datum  Wing leading edge 
 Leveling means Not available 
 Certification basis Approved Type Certificate 688 (expired) (CAR 04) 
    Production Certificate No. 2 
 
 Equpment:  (* Means net increase.) 
 
 Class I. 
 A. Landplane 
  101. Propeller - wood (fixed or adj. pitch) 9 lbs. (-43) 
  102. 6.00-6 wheels (Shinn 6C4) with tires 21 lbs. (-  1) 
  103. Tail skid 
  104. Carburetor air heater   2 lbs. (-31) 
  105. Wheel type control (Drawing 7-35) 
  106. Single magneto - Scintilla 
 B. Seaplane - Items 101, 104, 105, 106 PLUS 
  151. Edo 60-1320 float installation 
   including auxiliary fin, 169 lbs. 112 lbs.* (+25) 
 
 Class III. 
  301. Wheels    (-  1) 
   (a) 3 in. (Goodyear 3-LMBM) with brakes     10 lbs.* 
   (b) 6.00-6 (Shimm 6C4B or 6C4HB) with brakes       5 lbs.* 
   (c) 3 in. (Goodyear 3-LMBM)       1 lb.* 
  302. Tires 
   (a) 18x8-3 with tubes        4 lbs.* (-  1) 
   (b) 16x7-3 with tubes Neglect weight 
  303. Tail wheel installation 
   (a) Shock cord type with 6x2.00 wheel and 
    pneumatic tire (Dwg. 7-27)       1 lb.* (+174) 
   (b) Leaf spring type with 6 in. wheel and 
    solid tire (Dwg. 4-104)       2 lbs.* (+180) 
   (c) 6x2.00 steerable        3 lbs.* (+179) 
  304. Cabin heater         2 lbs. (+  28)   
  305. Carpet         2 lbs. (+    1) 
  306. Magnetos 
   (a) Single Wico or Eisemann Net door     3 lbs.* (-  23)  
   (b) Dual Scintilla     11 lbs.* (-  23) 
   (c) Dual Wico or Eisemann     5 lbs.* (-  23) 
  307. Wheel streamlines       8 lbs. (-    1) 
  308. Battery   Maximum  20 lbs. (+ 48) 
  309. Extra door        2 lbs. (+ 21)

A-688  Page 3 of 3 
 
  310. 5-gallon auxiliary fuel tank (See Note 1)    10 lbs. (+ 29) 
  311. Special instruments          6 lbs. (-    1) 
  312. Parachutes (one or two)      20 lbs. each 
  313. Radio equpment 
   (a) Receiver (RCA AVR-15 or -15A)     11 lbs. (-    5) 
   (b) Receiver (RCA AVR-10 or -10A)       9 lbs. (-    7) 
   (c) Receiver (Learadio AMR-1 or AMRL-1)     11 lbs. (+ 43) 
   (d) Transmitter (Learadio AMT-1)       9 lbs. (+ 45) 
   (e) Loop antenna          2 lbs. (+ 36) 
   (f) Trailing antenna         1 lb. 
   (g) "T" type antenna    Neglect weight 
   (h) Reel type trailing antenna       3 lbs. (+ 79) 
  314. Anchor and rope         7 lbs. (+   2) 
  315. Ski type axle (Dwg. 3-43 or 3-44)  Neglect weight 
  316. Landing lights (Grimes ST-250) One or Two      5 lbs. each (+ 17) 
  317. Stick type control (Dwg. 7-70)  No weight change 
  318. Parking brake installation       1 lb.* (-   6) 
  319. Generator - wind-driven (Air Assoc. G-6 or G-12)      8 lbs. (+  9) 
  320. Seaplane fittings    Neglect weight 
  321. Steps (two)    Neglect weight 
  322. Skis    Use actual weights 
   (a) Washington Aircraft 1200 
   (b) Federal SA-1 or SA-2 
   (c) Federal SC-1 or SC-2 
   (d) Marston MFS-1200 
   (e) Marston MFS-1600 
   (f) Jennings TY-2 
   (g) Richards 1-B 
   (h) Graf-Shupe A 
   (i) Heath 655 
  323. Oil filter, Fram PB-5 (Models 50-F and S-50-F only)       4 lbs. (- 31) 
   Fram Installation Drawing No. 61552 
   Weight includes one quart of oil. 
 
 
NOTE 1. Fuel arm (+48) with item 310. 
 
NOTE 2. Eligible for export as follows, subject to provisions of Chapter XII of 
   Inspection Handbook:  (6-2-41) 
   (a) Canada 
    Landplane - eligible. 
    Skiplane - not eligible.  Howe ver, structure complies with Canadian 
    requirements for ski installati on when item 315 is installed, with 
    tread not exceeding that with wheels and a maximum ski height of 
    12 inches. 
    Seaplane - maximum weight1253 lbs. 
   (b) Australia 
    Landplane only. 
   (c) All other countries except New Zealand. 
 
NOTE 3. If empty weight C.G. for a particul ar airplane falls wtihin range given, it 
   is unnecessary to check critical forward and aft C.G. positions.  These 
   ranges are not valid fo r non-standard arrangements. 
 
 
 
-END-
```

## ADs

None name its models.

## Registered aircraft by registry model (OpenAirDocs)

- [Aeronca 50-F](https://openairdocs.org/model/aeronca-50-f): 3 aircraft (registry code 0190702)
- [Aeronca KF](https://openairdocs.org/model/aeronca-kf): 0 aircraft (registry code 0190407)

## STCs approved under this data sheet (9)

- [STC SA01967WI](https://openairdocs.org/stc/SA01967WI): Use of GAMI G100UL High Octane Unleaded Avgas. General Aviation Modifications Inc.
- [STC SA02503AK](https://openairdocs.org/stc/SA02503AK): Installation of AMSAFE State of the Art Restraint System (SOARS) inflatable restraints. AMSAFE Inc.
- [STC SA01026SE](https://openairdocs.org/stc/SA01026SE): Improved fuel gascolator assembly.. Steve's Aircraft
- [STC SA1626NM PAGE 1](https://openairdocs.org/stc/SA1626NM%20PAGE%201): Installation of Electronics Int'l Digital EGT/CHT Instruments and accessories. (201 Series). Electronics International
- [STC SA2350NM PAGE 1](https://openairdocs.org/stc/SA2350NM%20PAGE%201): 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 1](https://openairdocs.org/stc/SA3862NM%20PAGE%201): Installation of Electronics International Primary TIT/EGT/CHT instruments, remote switches and associated accessories.. Electronics International
- [STC SA2190NM PAGE 1](https://openairdocs.org/stc/SA2190NM%20PAGE%201): Installation of electronics International Digital Volt/Amp Gauges and Accessories.. Electronics International
- [STC SA2350NM](https://openairdocs.org/stc/SA2350NM) (historical): Installation of Electronics International Inc digital carburetor/outside air temperature gauges listed on the attached continuation sheet and the associated accessories.. Electronics International

---
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.
