# TCDS A-787: Univair Aircraft Corporation

- Type: Type certificate data sheet
- Status: Current
- Holder: Univair Aircraft Corporation
- Revision: 33
- Revised: July 14, 2005
- Product: Aircraft, Small Airplane
- Certification basis: Part 1, CAR 3
- Registered aircraft: 440, by the registry models matched to it (OpenAirDocs)
- Data sheet PDF: https://openairdocs.org/files/sha256/c1/ff/c1ff18fff47108afc1b56721e82b40ed0d18a8d2cef93c3d86c057ede5eab8e8
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/10C96A9E594F363E8625706D006FF764.0001
- Page: https://openairdocs.org/tcds/A-787

## Models (8)

As the data sheet lists them.

- M10
- F-1A
- A-2
- F-1
- A2-A
- 415-D
- 415-G
- 415-E

## 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 5 6 7 8 9 10 11 
Rev. No. 33 32 32 31 33 33 31 33 33 32 33 
 
DEPARTMENT OF TRANSPORTATION 
FEDERAL AVIATION ADMINISTRATION 
   TYPE CERTIFICATE DATA SHEET NO. A-787  
 
Type Certificate Holder:  Univair Aircraft Corporation 
 2500 Himalaya Road 
 Aurora, Colorado 80011 
 
Model 415-D, 2 PCLM (Normal Category), Approved June 13, 1947 
 
Engine  Continental C75-12, -12F (See NOTE 4 for C85-12 or 12F) 
 
Fuel 73 minimum grade aviation gasoline 
 
Engine Limits  For all operations, 2275 r.p.m. (75 hp.) 
 
Airspeed Limits Maneuvering 108 mph ( 94 kts) True Ind.  
 Max. structural cruising 114 mph ( 99 kts) True Ind.  
 Never exceed 144 mph (125 kts) True Ind.  
 
C. G. Range (+26.8) to (+30.4)     
Empty wt. C. G. Range (+26.2) to (+27.2) - range not valid for nonstandard arrangements. 
 When empty weight C.G. falls within this range, computation of critical fore and aft 
 C.G. positions is unnecessary. 
 
Maximum Weight 1400 lbs. 
  
No. of Seats 2 (+37) 
 
Maximum baggage 65 lbs. (+57) 
 
Fuel Capacity 24 gal. [9 gal. each wing (+25), 6 gal. in fuselage (+7)] 
 
Oil Capacity 4 qt. (-14) 
  
Control Surface Movements Elevator trim tab Up  0° Down  60° 
 Elevator Up  9° Down  12° 
 Aileron Up  40.5° Down  9.5°  
 Rudders Out  20° In 3°  
 
Serial Nos. Eligible 4424 and up. See Note 3 regarding S/N 113 thru 4423. 
 
Required Equipment In addition to the pertinent require d basic equipment specified in CAR 3, the following 
items of equipment must be installed: 1, 101(a), 102, 201(a), 202(a), 205(a), 206(a), 
401(a). 
A-787 
Revision 33 
Univair 
(ERCO)  415-D 
(ERCO) E 
(ERCO) G 
(Forney) F-1 
(Forney) F-1A 
(Alon) A-2 
(Alon) A2-A 
(Mooney) M10 
July 14, 2005

A-787 Page 2 of 11 
 
 
 
II. Model E, 2 PCLM (Normal Category), Approved July 8, 1948 
Model G, 2 PCLM (Normal Category), Approved January 28, 1949 
(Model E is similar to Model 415-D except for engine installation, redesigned elevator, addition of low speed warning 
cushion to elevator control and other changes of a minor nature. Model G is similar to E except for installation of "Kiddy 
Seat", increased baggage capacity, compound curved windshield, revised nose cowling support, revised engine baffles, 
revised seat back structure and other changes of a minor nature.) 
 
Engine  Continental C85-12, C85-12F 
 
Fuel 73 minimum grade aviation gasoline 
 
Engine Limits  For all operations, 2575 r.p.m. (85 hp.) 
 
Airspeed Limits  Maneuvering 108 mph (94 kts)  True Ind. 
 Max. structural cruising 114 mph (99 kts)  True Ind. 
 Never exceed 144 mph (125 kts)  True Ind. 
 
C. G. Range (+26.4) to (+30.3)   
  
Empty wt. C. G. Range  Model E: (+25.7) to (+26.9)  
 Model G: (+25.9) to (+26.7)  
 Ranges not valid for nonstandard arrange ments. When empty weight C.G. falls 
 within the pertinent range, computation of critical fore and aft C.G. positions is 
 unnecessary. 
 
Maximum Weight 1400 lbs. 
 
No. of Seats 2 (+37). Model G incorporates "Kiddy Seat" for maximum passenger weight of  
 75 lbs. at (+57).  Weight of bagga ge and passenger not to exceed 75 lbs. 
 
Maximum baggage  Model E: 65 lbs. (+57)  
Model G: 75 lbs. (+57) Total weight of passenger on "Kiddy Seat" plus baggage not to 
exceed 75 lbs. 
 
Fuel Capacity 24 gal. [9 gal. each wing (+25), 6 gal. in fuselage (+7)] 
 
Oil Capacity 4.5 qt. (-14)     
Control Surface Movements Elevator trim tab Up 10° Down 36° 
 Elevator Up 20° Down 10° 
 Aileron Up 40° Down 10° 
 Rudders Out 20° In 3° 
 
Serial Nos. Eligible Model E: 3779, 4869 and up 
 Model G: 4997 and up 
 
Required Equipment  In addition to the pertinent required basic equipment specified in CAR 3, the 
following items of equipment must be installed: 1, 101(a), 102, 201(a), 202(a), 
205(b), 206(b), 401(b).

A-787 Page 3 of 11 
 
 
III. Model F-1, 2 PCLM (Normal Category), Approved September 18, 1956 
(Model F-1 is similar to Model G except for engine and propeller combination, revised engine cowling, metal covered 
outer wing panels, extended baggage compartment, and modified seats and instrument panel.) 
 
Engine  Continental C90-12F 
 
Fuel 80 minimum grade aviation gasoline 
 
Engine Limits  For all operations, 2475 r.p.m. (90 hp.) 
 
Airspeed Limits Maneuvering 108 mph  (94 kts)  True Ind. 
 Max. structural cruising 114 mph  (99 kts)  True Ind. 
 Never exceed 144 mph  (125 kts) True Ind. 
 
C. G. Range (+26.4) to (+30.3) 
   
Empty wt. C. G. Range (+25.9) to (+26.7) - range not valid for nonstandard arrangements. When empty 
weight C.G. falls within the pertinent range, computation of critical fore and aft 
C.G. positions is unnecessary. 
 
Maximum Weight  1400 lbs. 
 
No. of Seats 2 (+37). "Kiddy Seat" incorporated for maximum passenger weight of 75  
 lbs. at (+57). 
 
Maximum baggage 75 lbs. (+57). Total weight of passenger on "Kiddy Seat" plus baggage not to 
 exceed 75 lbs. 
 
Fuel Capacity 24 gal. [9 gal. each wing (+25), 6 gal. in fuselage (+7)] 
  
Oil Capacity 4.5 qt. (-14)  
    
Control Surface Movements Elevator trim tab Up 10° Down  36° 
 Elevator Up 20° Down  10° 
 Aileron Up 40° Down  10° 
 Rudders Out 20° In 3° 
 
Serial Nos. Eligible 5600 and up (see NOTE 5 for eligibility under section IV) 
 
Required Equipment  In addition to the pertinent required basic equipment specified in CAR 3, the 
following items of equipment must be installed: 4, 101(b), 102, 201(a), 202(a), 205(b), 
206(b), 401(b) and 401(c). 
 
IV. Model F-1A, 2 PCLM (Normal Category), Approved December 22, 1959 
(Model F-1A is similar to Model F-1 except for larger control rods, nose wheel fork, rear spar and minor changes.) 
Engine  Continental C90-12F 
 
Fuel 80 minimum grade aviation gasoline 
 
Engine Limits  For all operations, 2475 r.p.m. (90 hp.) 
 
Airspeed Limits Maneuvering 108 mph  (94 kts) True Ind. 
 Max. structural cruising 114 mph  (99 kts)  True Ind. 
 Never exceed 144 mph (125 kts)  True Ind. 
 
C. G. Range (+26.4) to (+30.3)

A-787 Page 4 of 11 
 
 
IV. Model F-1A, 2 PCLM (Normal Category) (cont'd)     
Empty wt. C. G. Range (+25.9) to (+26.7) - range not valid for nonstandard arrangements. When empty 
weight C.G. falls within the pertinent range, computation of critical fore and aft  
 C.G. positions is unnecessary. 
 
Maximum Weight 1450 lbs. 
 
No. of Seats 2 (+37). Optional "Kiddy Seat" at (+57) 
 
Maximum baggage 75 lbs. (+57). Total weight of passenger on "Kiddy Seat" plus baggage not to 
 exceed 75 lbs. 
 
Fuel Capacity 24 gal. [9 gal. each wing (+25), 6 gal. in fuselage (+7)] 
 
Oil Capacity 4.5 qt. (-14) 
     
Control Surface Movements Elevator trim tab Up 10° Down 36° 
 Elevator Up 20° Down 10° 
 Aileron Up 40° Down 10° 
 Rudders Out 20° In 3° 
 
Serial Nos. Eligible 5715 and up 
 
Required Equipment In addition to the pertinent re quired basic equipment specified in CAR 3, the 
following items of equipment must be installed: 4, 101(b), 102, 201(a), 202(a), 205(b), 
206(b), 401(d). 
 
V. Model A-2, 2 PCLM (Normal Category), Approved November 12, 1964, Model A-2A, 2 PCLM (Normal Category),  
Approved June 21, 1967 
(Model A-2 is similar to Model F-1A except for revised canopy, control column and wheel, toe brake, welded fuel 
tanks, exhaust system, induction system and minor changes.) 
 
Engine Continental C90-12F or C90-16F 
 
Fuel 80 minimum grade aviation gasoline 
 
Engine Limits For all operations, 2475 r.p.m. (90 hp.) 
 
Airspeed Limits Maneuvering  Maneuvering  108 mph  (94 kts)  True Ind.  
 Max. structural cruising  114 mph  (99 kts)  True Ind.  
 Never exceed 144 mph  (125 kts)  True Ind. 
 
C. G. Range (+27.0) to (+30.1) at 1450 lbs.  
 (+26.4) to (+30.3) at 1400 lbs. or less  
 Linear variation between points given. 
 
Maximum Weight 1450 lbs. 
 
No. of Seats 2 (+37). "Kiddy Seat" (optional) at (+57). 
 
Maximum baggage Model A-2:  75 lbs. (+57) 
 Model A2-A:  90 lbs. (+68). "Family Seat" optional.  
 See Note 2, B. for placard. 
 
Fuel Capacity 24 gal. [9 gal. each wing (+25), 6 gal. in fuselage (+7)]

A-787 Page 5 of 11 
 
 
V. Model A-2, 2 PCLM (Normal Category) (cont’d) 
 
Oil Capacity 5 qt. (-14) 
     
Control Surface Movements Elevator trim tab Up 10° Down 36° 
 Elevator Up 20° Down 10° 
 Aileron Up 40° Down 10° 
 Rudders Out 20° In 3° 
 
Serial Nos. Eligible  A-2:  A-2 thru A-245  
 A2-A:  B-246 thru B-297 
 
Required Equipment In addition to the pertinent re quired basic equipment specified in CAR 3, the 
following items of equipment must be installed:  4, 101(c), 102, 201(b), 202(a), 
205(d) or 205(e), 206(b) and 404. 
 
VI. Model M10, 2 PCLM (Normal Category), Approved September 27, 1968 
(Model 10 is similar to Model A2-A except for new design empennage, ailerons and fuel tank vent.) 
 
Engine Continental  C90-12F or C90-16F 
 
Fuel 80 minimum grade aviation gasoline 
 
Engine Limits  For all operations, 2475 r.p.m. (90 hp.) 
 
Airspeed Limits  Maneuvering 108 mph  (94 kts)  True Ind. 
 Max. structural cruising 114 mph  (99 kts)  True Ind. 
 Never exceed 144 mph  (125 kts)  True Ind. 
 
C. G. Range (+27.0) to (+30.1) at 1450 lbs.  
 (+26.4) to (+30.3) at 1400 lbs. or less 
 Linear variation between points given. 
   
Maximum Weight 1450 lbs.  
  
No. seats 2 (+37). "Kiddy Seat" (optional) at (+57) 
 
Maximum baggage 90 lbs. (+68). "Family Seat" (optional) 
 
Fuel Capacity 24 gal. [9 gal. each wing (+25), 6 gal. in fuselage (+7)] 
 
Oil Capacity 5 qt. (-14)  
   
Control Surface Movements Elevator trim tab Up  7° to 10° Down 32° to 36° 
 Elevator Up  25° to 29° Down 20° to 24° 
 Aileron Up  24° to 28° Down 9° to 11° 
 Rudders Left  25° to 27° Right 25° to 27° 
 
Serial Nos. Eligible 690001 and up  
 
Required Equipment In addition to the pertinent re quired basic equipment specified in CAR 3, the 
following items of equipment must be installed:  4 or 8, 101(d), 102(e), 201(b), 202, 
205(d) or 205(e), 206(b), 401(e), 405. 
 
Specifications Pertinent to All Models 
  
Datum Firewall Bulkhead 
 
Leveling means Hatch sill on either side of the fuselage

A-787 Page 6 of 11 
 
 
Certification basis  CAR 3, effective December 15, 1946 with no amendments, no exemptions. Type 
Certificate No.787 issued June 13, 1947. Application for Type certificate dated 
February 6, 1947. 
 
Production basis Alon Models A-2 and A2-A (subsequent to March 1, 1968), Erco Models 415-D, E, G, 
Forney Models F-1, F-1A and Mooney Model M10 - None. Prior to original 
certification of each aircraft manufactured, an FAA 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 e xport to all countries subject to the provisions of Advisory Circular 21-
2, except as follows: Canada, Landplane eligible; Skiplane not eligible; however, 
structure complies with Canadian requirements. Maximum pedestal height 8-1/2 
in. to center of axle; tread identical with landplane. 
 
Equipment: A plus (+) or mi nus (-) sign preceding the weight of an item of equipment 
indicates the net weight change when that item is installed. Approval for the 
installation of all items of equipment listed herein has been obtained by the aircraft 
manufacturer except those items preceded by an asterisk (*). The asterisk denotes 
that approval has been obtained by someone other than the aircraft manufacturer. 
An item marked with an asterisk may not have been manufactured under an FAA 
monitored or approved quality control system, and therefore conformity must be 
 determined if the item is not identified by a Form FAA-186 or 8130-3 
Airworthiness Approval Tag, TSO, PMA, or other evidence of FAA production 
approval. 
Propellers and Propeller Accessories 
 
 1. Sensenich 74CT48 or 74KT48 14 lbs.  (-32) 
  (For flanged type crankshaft) or any other fixed pitch wood propeller,  
  rated for the engine power and sp eed which meets the following limits: 
   Static r.p.m. at max. permissible throttle setting: 
   (Model 415-D with C75 engine): not over 2100, not under 2000. 
   (Models 415-D, E and G with C85 engine): not over 2100, not under 1900. 
  No additional tolerance permitted. 
  Diameter: not over 74 inches, not under 72 inches. 
  
 2. McCauley 1A90CF or 1B90CM (Model 415-D with C75 engine) +12 lbs. (-32) 
   Static r.p.m. at maximum permissible throttle setting: 
   Not over 2110, not under 2010. 
  No additional tolerance permitted. 
  Diameter: not over 73 inches, not under 71.5 inches. 
  
 3. Hartzell hub HA12UO or HA12UF 18 lbs.  (-32)  
  Blades 7414 to 7014 or 7214M to 7014M (ground adjustable) 
  Eligible on all engines with static r.p.m. and diameter limits shown for fixed 
  pitch wood propellers. 
 
 4. Fixed pitch metal, McCauley 1A90CF or 1B90CM +12 lbs.  (-32) 
  Eligible on Models M10, A2, A2-A, 415-D (per note 4(b)), E, G, F-1 and F-1A. 
   Static r.p.m. at maximum permissible throttle settings: 
   For Models 415-D, E, or G: not over 2225, not under 2025. 
   For Models M10, A-2, A2-A, F-1, F-1A: not over 2375, not under 2250. 
  No additional tolerance permitted. 
  Diameter: not over 71 inches, not under 69.5 inches.  
 5. Koppers Aeromatic F200 hub, 00-73 or -73F blades +16 lbs.  (-32)  
  Parts List Assembly No. 4305-A

A-787 Page 7 of 11 
 
 
  Static r.p.m. at maximum permissible throttle setting: 
   Not over 2575, not under 2465. 
  No additional tolerance permitted. 
  Pitch settings: 
  (a) With Continental C85 engine:   low 11°, high 20° 
  (b) With Continental C75 engine:   low 13°, high 20.3° 
  Diameter: not over 73 inches, not under 71.5 inches. 
  When this item is installed, the following note will be inserted in the Airplane Flight Manual: 
  "Aeromatic Propeller  (F200/00-73 or -73F)  
  Installation and operation must be accomplished in accordance with Koppers  
  Installation Procedure and Operation Limitations dated April 27, 1948". 
 
 6. Fixed pitch metal, Sensenich M76AK-2 24 lbs.  (-32) 
  (a) Model 415-D with C75 engine: 
   Static r.p.m. at maximum permissible throttle setting: 
         Not over 2125, not under 2050  
   No additional tolerance permitted. 
   Diameter: not over 74 inches, not under 72.5 inches. 
  (b) Models 415-D (per NOTE 4(b)), or E or G: 
   Static r.p.m. at maximum permissible throttle setting: 
         Not over 2250, not under 2175  
   No additional tolerance permitted. 
   Diameter: not over 74 inches, not under 72.5 inches. 
 
 7. Controllable Beech R002 or R003 w ith R003-225-72T blades 26 lbs.  (-32)  
  Eligible on Models 415-D (per NOTE 4(b)), or E or G: 
  Diameter: not over 72 inches, not under 70.5 inches. 
  Pitch settings at 27 in. sta.: High 18.5° to 20.5°, low 13° to 14°. 
  Note: Check aircraft weight and balance to determine if ballast is required in  
    the baggage compartment when the aircraft is flown solo.  
  Propeller control 1 lb.  (-10) 
 
 8. Fixed pitch metal, McCauley 1A105/SCM 7153 20 lbs.  (-32) 
 Eligible for Models M10, A-2 and A2-A with C90 engine 
 Static r.p.m. at maximum permissible throttle setting: 
  Not over 2375, not under 2250. 
 No additional tolerance permitted. 
 Diameter: not over 71 inches, not under 69.5 inches. 
 
 101. Carburetor air heater  
 (a) Models 415-D, E and G Engineering & Research Corp. Dwg. 415-40400 5 lbs.  (-2) 
 (b) Models F-1, F-1A, Forney Mfg. Co., Dwg F-40400 5 lbs.  (-2) 
 (c) Models A-2, A2-A, Forney Mfg. Co., Dwg F-40400 2 lbs.  (-10) 
  (d) Model M10, Mooney Dwg. 600275 2 lbs.  (-10) 
 
102. Fuel Pump - The following are eligible with C75, C85 and C90-12F engines only 2 lbs.  (-27) 
  (a) AC P/N 1539051, Continental P/N 40585 
 (b) AC P/N 1539076, Continental P/N 40695 
 (c) AC P/N 1539003, Continental P/N 40281 
 (d) AC P/N 1537973, Continental P/N 40452 
 (e) AC P/N 5656861, Continental P/N 631391 (eligible with C90-16F engines only). 
 
 103. Starter - Delco-Remy No. 1109656, P/N 50309 16 lbs.  (-7) 
  
 104. Baffle plate, ERCO P/N 405-40252 (optiona l - Neglect wt. change with all engines) 
   * 105. Davis exhaust silencer - Model D-75-85ER installed per Davis 2 lbs.  (-19.5) 
  Silencer Co. Dwg. D-75-85-ERI

A-787 Page 8 of 11 
 
 
  
 106. Engine - Continental C85-12, -12F +12 lbs. 
  (Eligible on Model 415-D in accordance with NOTE 4) 
  Engine limits - for all operations, 2575 r.p.m. (85 hp.) 
  Fuel - 73 min. grade aviation gasoline. 
  Oil capacity - 5 qt. (-14) 
  
   * 107. Oil Filter - Fram PB-5, Kit No. K-510, Fram installation Dwg. 61614 5 lbs.  (-2) 
 
 108. Engine primer per Alon Dwg. A-48304 1 lb. (+23)  
Landing Gear 
 
 201. Two main wheel-brake assemblies, 6.00-6, Type III  
  (a) Goodyear LF6HBD 12 lbs.  (+44) 
   Wheel assy. 511960-M 
   Brake assy. 9520285 
  (b) Cleveland 6.00-6 12 lbs.  (+44) 
   Model 27-100D (Type 40-16) wheel and 30-4 brake 
  
 202. Two main 4-ply rating tires 6.00-6, Type III, with regular tubes.  18 lbs.  (+44) 
  
 205. One nose wheel, Type III  
  (a) ERCO 5.00-4, assy. 415-34204 3 lbs.  (-16)  
  (b) Firestone 5.00-5, Model DFA531, assy. DFA531  Neglect wt. change 
   Eligible on Model 415-D with item 206(b) when revised nose wheel fork is 
   installed per ERCO Dwg. 415-34360. 
  (c) Goodyear 6.00-6, Model L6NBD, assy. 511500-M 
   Eligible with item 206(c) when revised nose wheel fork is installed per 
   ERCO Dwg. 415-34365.  
  (d) Cleveland 5.00-5, Model 21-100D (Type 40-17)  Neglect wt. change 
  (e) Goodyear 5.00-5, P/N 9532926  Neglect wt. change 
 
 206. One nose wheel tire, Type III, 4-ply rating with regular tube.  
  (a) 5.00-4 6 lbs.  (-16) 
  (b) 5.00-5 Neglect wt. change 
  (c) 6.00-6 +3 lbs.  (-16) 
 
   * 210. Wilson Fendaire Model LW-1 (nose wheel only). 1 lb.  (-16) 
  Installed per Wilson Fendaire Co. instructions dated 6-2-60.  
 
Electrical Equipment  
 
 301. Battery 
 For list of approved batteries with their arms and weights,   Use act. wt. 
 see Univair Service Memorandum No. 67 
 
 302. Generator  
  (a) Delco-Remy 1101876, P/N 40435 10 lbs.  (-8) 
  (b) Delco-Remy No. 1101890 10 lbs.  (-8) 
  (c) Delco-Remy No. 1101898 16 lbs.  (-8) 
 
   * 303.  Two landing lights (Aviation Accessories Corp.  4 lbs.  (+29) 
  Model E) installed per AAC Dwg. E-1001.

A-787 Page 9 of 11 
 
 
304. Two landing lights installed per Sanders Aviation Co. dwg. 415-54108 and 3 lbs.  (+29) 
  installation instructions SK28. 
  
 305. Two landing lights, G.E. P/N 4509, installed per Alon Dwg. F14094 and F14095. 3 lbs.  (+29) 
 
Interior Equipment 
 
 401.  FAA Approved Airplane Flight Manuals 
  (a) Model 415-D dated June 13, 1947 
  (b) (1)  Model E (tentative) dated July  1, 1948; (final) dated September 15, 1948 
     Revision "A", dated July 1, 1993 
   (2)  Model G dated January 28, 1949 
     Revision "A", dated July 1, 1993 
  (c) Model F-1, Supplem ent dated September 7, 1956 
   Revision "A", dated July 1, 1993 
  (d) Model F-1A dated January 5, 1960 
  (e) Model M10 dated September 20, 1968 
  
 402. Trim-O-Matic Control Kit installed per ERCO Neglect wt. change 
  Service Memorandum No. 54 and ERCO Dwg. 415-52175. 
  
 403. Rudder pedals installed per ERCO Kit Instructions 6 lbs.  (+18) 
  (Service Memoranda Nos. 59 and 59A) and Dwg. 415-52389. 
  
 404. Placards for Models Alon A-2 and A2-A per NOTE 2, B. Neglect wt. change 
 
 405. Placards for Model Mooney M10 per Note 2, C.  Neglect wt. change  
 
Miscellaneous (not listed above) 
 
   * 601. Metal plating of wings 32 lbs.  (+36)  
  Models 415-D, E and G are eligible for certification when wings are covered with  
  metal per Technical Instruction Report No. 103000 by Birtcraft Engineering Co.,  
  11836 Cherry Ave., Inglewood, Calif. 
 
 
NOTES 
 
NOTE 1. A current weight and balance report including a list of the equipment included in the certificated empty 
weight, and loading instructions, when necessary, must be in each aircraft at the time of original 
certification and at all times thereafter except in the case of operators having an approved weight 
control system. 
 
NOTE 2. Placards 
 A. Models ERCO 415-D, E, G, Forney F-1, F-1A 
  (1) On instrument panel in full view of the pilot: 
    (a)  "This airplane must be operated as  a Normal Category airplane in compliance with 
    operating limitations, Secs. A and B, Approved Airplane Flight Manual." 
   (b) "This airplane character istically incapable of spinning." 
   (c)  "No acrobatic maneuvers are approved." 
  (2) To be displayed in Cabin: "No Smoking."

A-787 Page 10 of 11 
 
 
B. Models Alon A-2 and A2-A 
  (1) On instrument panel in full view of the pilot: 
   (a) "This airplane must be operated as a Normal Category airplane in compliance with 
    the operating limitations stated in  the form of placards and markings."  
   (b) "Do not open canopy in excess of 100 m.p.h. IAS."  
   (c) "This airplane character istically incapable of spinning." 
   (d) "No aerobatic or inverted maneuvers approved."  
   (e) "Maximum maneuver speed - 108 m.p.h. TIAS." 
   (f)  "Flight load factor positive 3.8g 
    Maximum gross weight - 1450 lbs. 
    Center of gravity limits: 
    (+26.4) to (+30.3) (Datum Firewall) to 1400 lbs. 
    (+27.0) to (+30.1) (Datum Firewall) 
    Linear variation between 1400 lbs. and 1450 lbs." 
   (2)  Passenger and cargo compartment: 
    A-2: "Capacity this co mpartment 75 lbs. maximum."  
    A2-A: "Capacity this compartment 90 lbs. maximum." 
 
 C.  Model Mooney M10 (150059) 
  (1) On instrument panel in full view of the pilot: 
   (a) "This airplane must be operated as a Normal Category airplane in compliance 
    with the Airplane Flight Manual." 
   (b) "Do not open canopy in excess of 100 m.p.h. CAS."  
   (c) "No aerobatic maneuvers including spins approved."  
   (d) "Maximum maneuver speed - 108 m.p.h. CAS."  
   (e) "Flight load factor positive - 3.8g 
    Maximum gross weight - 1450 lbs. 
    Center of gravity limits: 
    26.4 to 30.3 (Datum, firewall) to 1400 lbs.  
    27.0 to 30.1 (Datum, firewall) 
    Linear variation between 1400 and 1450 lbs." 
   (f) "Check fuselage tank gage for floatation." 
  (2)  Passenger and cargo compartment: "Cap acity this compartment 90 lbs. maximum." 
 
NOTE 3. S/N 113 thru 4423 and 4500 and up, designated Model 415-C, also eligible as Model 415-D under terms 
of this specification provided the following changes are incorporated:  
 (a) Correct propeller and propeller limits. 
 (b)  Correct control surface travel for the elevator. 
 (c)  Incorporate elevator tab per ERCO Dwg. 415-22031 (applies to S/N 113 thru 4423 only). 
 (d)  Mark instruments per the FAA approved operating limitations in the Airplane Flight Manual.  
 (e)  Include placards on the instrument panel and in the cabin per NOTE 2 above.  
 (f)  Revise the orifices for the main and nose gear piston as follows: 
 
        S e r i a l  N o s .  Orifice Size   
  Main Gear   113 thru 812  .067" diameter 
  Nose Gear  113 thru 1622 .281" diameter 
 
 (g)  Alter the nameplate to indicate the date  of the conversion, new model number and type 
certificate number. 
 (h)  Install stainless steel upper skin in fuselage  aft of firewall per ERCO Dwg. 415-31245. (S/N 113 
thru 4423 only). 
 
NOTE 4. Model 415-D eligible for installation of C85-12 or -12F engines provided:  
 (a) Item 1, 3 or 5 propeller or 
 (b)  Item 4, 6 or 7 propeller and additional ERCO baffles (P/N 415-40487 left and right; 
  415-40488, one; 415-40597, two; 415-40598, two) installed.  
 (c) Item 401(a), Airplane Flight Manual, is revised as follows:

A-787 Page 11 of 11 
 
 
  I. "Limitations" section to include: 
   (1) Description of C 85 engine and operating limits. 
   (2)  Maximum cylinder head temperature: 540°F 
   (3)  Description of propeller (Item 1, 3, 4, 6, or 7) installed, including static r.p.m., diameter 
    limits and pertinent placard. 
  II. "Performance section to include th e following statement, as applicable: 
   "Performance" with C85-12  or -12F engine and the   model propeller has been 
demonstrated to equal or exceed that presented herein over the altitude and temperature  
   range shown." 
 (d) Conversion of the C75 engine to the C85 must be accomplished per Continental Service Bulletin 
M47-16 dated June 7, 1948 and the oil sump dip stick recalibrated to indicate full sump when 
serviced with 4.5 qt. of oil. 
 
NOTE 5. Forney Model F-1 airplanes, S/N 5611 thru 5714 are eligible for operation under the provisions of 
Section IV of this specification, provided: 
 (a) Larger control rods are installed per Forney Dwg. F-52085. 
 (b) New type nose fork, F-34371, is installed per Univair Service Kit SK-17C or new type nose gear 
is installed per Univair Service Kit SK-17. 
 (c) Belleville springs are installed in the main landing gear per Forney Dwg. F-33253.  
 
 
 
....END....
```

## ADs (32, 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
- [AD 2012-08-06](https://openairdocs.org/ad/2012-08-06): Flight Controls · Univair 415-C, 415-CD, 415-D and 7 more. Effective Oct 3, 2012
- [AD 2003-21-01](https://openairdocs.org/ad/2003-21-01): Outer wing panels · Univair 415-C, 415-CD, 415-D and 7 more. Effective Dec 1, 2003
- [AD 2002-26-02](https://openairdocs.org/ad/2002-26-02): Wing Center Section · Univair 415-C, 415-CD, 415-D and 7 more. Effective Feb 14, 2003
- [AD 2002-16-04](https://openairdocs.org/ad/2002-16-04): Fuel Line Nipples, Aluminum Fuel Line elbows, and Gascolator · Univair 415-C, 415-CD, 415-D and 4 more. Effective Sep 13, 2002
- [AD 96-09-06](https://openairdocs.org/ad/96-09-06): Air Filter Assemblies · Maule Aerospace Technology 7ACA, 7ECA, 7FC and 180 more. Effective Jun 7, 1996
- [AD 67-06-03](https://openairdocs.org/ad/67-06-03): Rudder bellcrank · Univair 415-C, 415-CD, 415-D and 4 more. Effective Feb 11, 1967
- [AD 59-25-05](https://openairdocs.org/ad/59-25-05): Rudder reinforcement · Univair 415-C, 415-CD, 415-D and 3 more
- [AD 59-05-04](https://openairdocs.org/ad/59-05-04): Rear spar reinforcement · Univair 415-C, 415-CD, 415-D and 2 more
- [AD 57-02-01](https://openairdocs.org/ad/57-02-01): Rudder horn attachment · Univair 415-C, 415-CD, 415-D and 3 more
- [AD 54-26-02](https://openairdocs.org/ad/54-26-02): Control cable fraying · Univair 415-C, 415-CD, 415-D and 2 more
- [AD 46-23-01](https://openairdocs.org/ad/46-23-01): Muffler Replacement · Univair 415-C, 415-CD and 415-D
- [AD 46-23-02](https://openairdocs.org/ad/46-23-02): Engine breather line hose · Univair 415-C, 415-CD and 415-D
- [AD 46-23-03](https://openairdocs.org/ad/46-23-03): Aileron control column fitting · Univair 415-C, 415-CD and 415-D
- [AD 46-38-02](https://openairdocs.org/ad/46-38-02): Aileron control stop · Univair 415-C, 415-CD and 415-D
- [AD 46-46-01](https://openairdocs.org/ad/46-46-01): Fuselage Gas Tank Overflow Line · Univair 415-C, 415-CD and 415-D
- [AD 46-49-01](https://openairdocs.org/ad/46-49-01): Nose wheel replacement · Univair 415-C, 415-CD and 415-D
- [AD 47-20-03](https://openairdocs.org/ad/47-20-03): Fuel pump line alteration · Univair 415-C, 415-CD and 415-D
- [AD 47-20-04](https://openairdocs.org/ad/47-20-04): Baggage Compartment Zipper · Univair 415-C, 415-CD and 415-D
- [AD 47-20-05](https://openairdocs.org/ad/47-20-05): Belly skin reinforcement · Univair 415-C, 415-CD and 415-D
- [AD 47-20-06](https://openairdocs.org/ad/47-20-06): Aileron reinforcement · Univair 415-C, 415-CD and 415-D
- [AD 47-20-08](https://openairdocs.org/ad/47-20-08): Battery box drain · Univair 415-C, 415-CD and 415-D
- [AD 47-20-09](https://openairdocs.org/ad/47-20-09): Voltage regulator check · Univair 415-C, 415-CD and 415-D
- [AD 47-42-20](https://openairdocs.org/ad/47-42-20): Control column shaft · Univair 415-C, 415-CD and 415-D
- [AD 50-07-01](https://openairdocs.org/ad/50-07-01): Elevator trim tab stop · Univair 415-C, 415-CD and 415-D
- [AD 55-22-02](https://openairdocs.org/ad/55-22-02): Wing Tank Replacements · Univair 415-C, 415-CD and 415-D
- [AD 60-09-02](https://openairdocs.org/ad/60-09-02): Nose gear bolts · Univair 415-C, 415-CD, 415-D and 1 more
- [AD 70-17-02](https://openairdocs.org/ad/70-17-02): Rudder bellcrank tie rod service · Univair M10
- [AD 94-18-04 R1](https://openairdocs.org/ad/94-18-04-R1) (historical): Outer Wing Panels · Univair 415-C, 415-CD, 415-D and 7 more. Effective Mar 24, 1995
- [AD 86-22-09](https://openairdocs.org/ad/86-22-09) (historical): Fuel Line Nipple · Univair 415-C, 415-CD, 415-D and 4 more. Effective Nov 13, 1986
- [AD 46-38-03](https://openairdocs.org/ad/46-38-03) (historical): Fuel system elbow fitting · Univair 415-C, 415-CD and 415-D
- [AD 52-02-02](https://openairdocs.org/ad/52-02-02) (historical): Aileron Balance Assembly · Univair 415-C, 415-CD, 415-D and 2 more

## Registered aircraft by registry model (OpenAirDocs)

- [Alon A2](https://openairdocs.org/model/alon-a2): 144 aircraft (registry code 0540102)
- [Ercoupe 415-D](https://openairdocs.org/model/ercoupe-415-d): 101 aircraft (registry code 0420326)
- [Forney F-1](https://openairdocs.org/model/forney-f-1): 50 aircraft (registry code 0420202)
- [Mooney M10](https://openairdocs.org/model/mooney-m10): 39 aircraft (registry code 5872018)
- [Engineering & Research 415-D](https://openairdocs.org/model/engineering-research-415-d): 24 aircraft (registry code 0420306)
- [Alon A-2A](https://openairdocs.org/model/alon-a-2a): 21 aircraft (registry code 0540104)
- [Ercoupe 415-E](https://openairdocs.org/model/ercoupe-415-e): 18 aircraft (registry code 0420328)
- [Aircoupe F-1A](https://openairdocs.org/model/aircoupe-f-1a): 10 aircraft (registry code 0420104)
- [Forney F-1A](https://openairdocs.org/model/forney-f-1a): 8 aircraft (registry code 0420204)
- [Engineering & Research 415-E](https://openairdocs.org/model/engineering-research-415-e): 7 aircraft (registry code 0420308)
- [Erco 415-D](https://openairdocs.org/model/erco-415-d): 4 aircraft (registry code 0420406)
- [Mooney A-2A](https://openairdocs.org/model/mooney-a-2a): 4 aircraft (registry code 5872014)
- [Engineering & Research 415-G](https://openairdocs.org/model/engineering-research-415-g): 3 aircraft (registry code 0420310)
- [Ercoupe 415-G](https://openairdocs.org/model/ercoupe-415-g): 3 aircraft (registry code 0420330)
- [Forney 415-D](https://openairdocs.org/model/forney-415-d): 2 aircraft (registry code 0420336)
- [Forney 415-E](https://openairdocs.org/model/forney-415-e): 1 aircraft (registry code 0420338)
- [Univair 415-D](https://openairdocs.org/model/univair-415-d): 1 aircraft (registry code 9230411)
- [Erco 415-E](https://openairdocs.org/model/erco-415-e): 0 aircraft (registry code 0420408)
- [Erco 415-G](https://openairdocs.org/model/erco-415-g): 0 aircraft (registry code 0420410)

## STCs approved under this data sheet (141, first 50)

- [STC SA02156CH](https://openairdocs.org/stc/SA02156CH): Installation of a 30-gallon fuel system. Duckboy America, 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 SA02636SE](https://openairdocs.org/stc/SA02636SE): Installation of Garmin GPS 175 Navigation System and GNX 375 Navigation System with ADS-B In/Out Transponder.. Garmin International Inc.
- [STC SA00079NY](https://openairdocs.org/stc/SA00079NY): Installation of Airwolf remote mounted engine oil filter kit AFC-K008 on single and multi engine fixed wing light aircraft incorporating Teledyne Continental reciprocating engines of 450 horsepower or less.. Airwolf Filter Corporation
- [STC SA01005DE](https://openairdocs.org/stc/SA01005DE): Installation of a EarthX ETX900-TSO Lithium battery. EarthX Inc.
- [STC SA00081NY](https://openairdocs.org/stc/SA00081NY): Installation of Iceman Aviation Supplies, Inc. Carburetor Ice Detector.. Alcor LLC
- [STC SA04046CH PAGE 2](https://openairdocs.org/stc/SA04046CH%20PAGE%202): Installation of L-3 GENESIS  (TM) Electronic Standby Instrument System (ESI-500/MAG-500). Acron Aviation Inc.
- [STC SA7965SW](https://openairdocs.org/stc/SA7965SW): Application of fabric and polyurethane finishing system.. Shady Aviation LLC
- [STC SA04378CH](https://openairdocs.org/stc/SA04378CH): Installation of an engine modified per STC SE04349CH. SureFly Partners Ltd.
- [STC SA01757WI](https://openairdocs.org/stc/SA01757WI): To allow the use of UL91 or UL94 (minimum) grade aviation fuel. Swift Fuels LLC
- [STC SA03898NY](https://openairdocs.org/stc/SA03898NY): Installation and maintenance of ORATEX covering and coating material. Aircraft Design & Certification Ltd
- [STC SA04568CH](https://openairdocs.org/stc/SA04568CH): Installation of the uAvionix tailBeaconX, a tail mounted position light with integrated Automatic Dependent Surveillance - Broadcast (ADS-B) Out and 1090MHz Mode-S transponder functionality. uAvionix Corporation
- [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 SA127GL](https://openairdocs.org/stc/SA127GL): Install Cleveland Wheel and Brakes conversion kit, P/N 199-69.. 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 SA04550CH](https://openairdocs.org/stc/SA04550CH): Installation of firewall mounted Electric Fuel Transfer Pump, reroute of fuel transfer lines and removal of engine driven mechanical fuel transfer pump. Alpha Aviation Inc.
- [STC SA01818WI](https://openairdocs.org/stc/SA01818WI): Installation of Garmin G5 Electronic Flight Instrument. Garmin International Inc.
- [STC SA00410BO](https://openairdocs.org/stc/SA00410BO): Installation of an AV-30-C Multi-Mode Indicator. uAvionix Corporation
- [STC SA01831WI](https://openairdocs.org/stc/SA01831WI): To allow the use of UL91 (minimum) grade aviation fuel. Petersen Aviation Inc
- [STC SA02268CH](https://openairdocs.org/stc/SA02268CH): Installation of Airwolf Filter Corp. Air Oil Separator. Airwolf Filter Corporation
- [STC SA2128CE](https://openairdocs.org/stc/SA2128CE): Operation of airplane on unleaded automotive gasoline, 87 minimum antiknock index and leaded automotive gasoline, 88 minimum antiknock index (RON+MON)/2. Intermixing with aviation gasoline also approved.. Petersen Aviation Inc
- [STC SA2628WE](https://openairdocs.org/stc/SA2628WE): Installation of Continental O-200-A engine, McCauley 1A101/DCM 6948 propeller, electric fuel transfer pump and associated changes.. Alpha Aviation Inc
- [STC SA3502WE](https://openairdocs.org/stc/SA3502WE): Installation of fiberglass nose bowl.. Alpha Aviation Inc
- [STC SA04362CH](https://openairdocs.org/stc/SA04362CH): Installation of the uAvionix skyBeacon Automatic Dependent Surveillance-Broadcast (ADS-B) Out. uAvionix Corporation
- [STC SA02503AK](https://openairdocs.org/stc/SA02503AK): Installation of AMSAFE State of the Art Restraint System (SOARS) inflatable restraints. AMSAFE Inc.
- [STC SA02481AK](https://openairdocs.org/stc/SA02481AK): Installation of pilot and copilot shoulder harnesses. Alpha Aviation Inc
- [STC SA02493CH](https://openairdocs.org/stc/SA02493CH): Installation of a Three Point Torso Restraint System. Alpha Aviation Inc
- [STC SA02601CH](https://openairdocs.org/stc/SA02601CH): Installation of a Battery Master Relay.. Alpha Aviation Inc
- [STC SA02757CH](https://openairdocs.org/stc/SA02757CH): Installation of the Univair Model E elevator assembly. Alpha Aviation Inc
- [STC SA10077SC](https://openairdocs.org/stc/SA10077SC): Installation of push-button starter system.. Hartzell Engine Technologies, LLC
- [STC SA00780SE](https://openairdocs.org/stc/SA00780SE): Installation of the True Lock Safety Retention Axle Lock Nut System. True Lock LLC
- [STC SA01246CH](https://openairdocs.org/stc/SA01246CH): Replace existing glass bowl gascolator with Skyport Services metal bowl Gascolator Part No. SS13100.. Alpha Aviation Inc
- [STC SA01247CH](https://openairdocs.org/stc/SA01247CH): Replace existing main LG strut seal with MLG Oleo Restoration Kit.. Alpha Aviation Inc
- [STC SA01407CH](https://openairdocs.org/stc/SA01407CH): Replace existing brake master cylinder with replacement brake master cylinder.. Alpha Aviation Inc
- [STC SA01409CH](https://openairdocs.org/stc/SA01409CH): Replace existing brake reservoir with replacement brake reservoir.. Alpha Aviation Inc
- [STC SA1097GL](https://openairdocs.org/stc/SA1097GL): Installation of single lamp landing light. Alpha Aviation Inc
- [STC SA1180GL](https://openairdocs.org/stc/SA1180GL): Installation of main and nose gear fairings. Alpha Aviation Inc
- [STC SA2230WE](https://openairdocs.org/stc/SA2230WE): Installation of main gear wheel fairings.. Alpha Aviation Inc
- [STC SA330GL](https://openairdocs.org/stc/SA330GL): Installation of 9-cu. ft. Baggage Compartment. Alpha Aviation Inc
- [STC SA11172SC](https://openairdocs.org/stc/SA11172SC): Installation of an ADS600-B Automatic Dependent Surveillance-Broadcast (ADS-B) Universal Access Transceiver (UAT) and Global Positioning System (GPS) antenna. NavWorx Inc
- [STC SA00478CH](https://openairdocs.org/stc/SA00478CH): Installation of Cooper Superflite 102 Fabric.. Aviation Products Systems Inc.
- [STC SA01768SE](https://openairdocs.org/stc/SA01768SE): Installation of an oil cooler system.. Steve's Aircraft
- [STC SA02442AK PAGE 2](https://openairdocs.org/stc/SA02442AK%20PAGE%202): Approval of the L-3 Communications NGT 2000/2500 ADS-B system. ADS-B Technologies, LLC
- [STC SA01669CH](https://openairdocs.org/stc/SA01669CH): Installation of Challenger Reusable Air Filter. Challenger Aviation Products Inc.
- [STC SA10921SC](https://openairdocs.org/stc/SA10921SC): Installation of an alternator and regulator as a replacement to existing OEM generators and mechanical voltage regulators. Hartzell Engine Technologies, LLC
- [STC SA02283SE PAGE 2](https://openairdocs.org/stc/SA02283SE%20PAGE%202): Installation of Electronics International Inc. Glass Panel Engine Monitor (with In Flight Data) CGR-30P. Electronics International Inc.

All 141: https://openairdocs.org/tcds/A-787/stcs.md

---
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