# TCDS 2A2: Fred Garcia

- Type: Type certificate data sheet
- Status: Current
- Holder: Fred Garcia
- Revision: 7
- Revised: March 13, 2002
- Product: Aircraft, Small Airplane
- Certification basis: CAR 3
- Registered aircraft: 8, by the registry models matched to it (OpenAirDocs)
- Data sheet PDF: https://openairdocs.org/files/sha256/90/8b/908b6a703c7bf2de4959daee55796b03180129ed26983edce4854b390d71252c
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/FE27B35E0AF3BFD7862577B20070254B.0001
- Page: https://openairdocs.org/tcds/2A2

## Models (1)

As the data sheet lists them.

- 480

## What the data sheet says

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

```text
P a g e  N o . 1234
R e v .  N o . 7666
Address change for Fred Garcia
DEPARTMENT OF  TRANSPORTATION
FEDERAL AVIATION ADMINISTRATION
2A2
Revision 7
CAMAIR
480
March 13, 2002
TYPE CERTIFICATE DATA SHEET NO. 2A2
Type Certificate Holder Fred Garcia
P.O. Box 231
Remsenburg New York  11960
I. - Model 480,   4 PCLM   (Normal Category),   Approved May 12, 1955
Engine 2  Continental O-470-B  (See Item 107 for optional engine)
Fuel 91/96 minimum grade aviation gasoline
Engine Limits For all operations, 2600 rpm (240 hp)
Airspeed Limits Maneuvering 148 mph (129 knots)
Maximum structural cruising 180 mph (156 knots)
Never exceed 220 mph (191 knots)
Flaps extended 120 mph (104 knots)
Landing gear extended 120 mph (104 knots)
C. G. Range (+96.5) to (+98.2) at 4323 lb.
(landing gear extended) (+93.5) to (+98.2) at 3400 lb. or less
Straight line variation between points given.
93 94 95 96 97 98 99
3200
3400
3600
3800
4000
4200
4400
FWD.
LIMIT
REAR
LIMIT
LBS.
INCHES
Empty Weight C. G. Range None
Maximum Weight 4323 lb.
Number of Seats 4 (2 at +96, and 2 at +132)
Maximum Baggage Nose compartment - 100 lb. (+32)
Rear compartment - 180 lb. (+139)

2A2 Page 2 of 4
Fuel Capacity 107.5 gallons total usable (2 interconnected main tanks in wing center section, 39.5
gallons at +103, and two tip tanks, 34.0 gallons each at +107)
Oil Capacity 6 gallons total usable (3 gallons integral sump in each engine) (+60)
Control Surface Movements Elevators 35° Up 16° Down
Elevator Trim Tab 23° Up 29° Down
Rudder 20° Left 20° Right
Rudder Trim Tab 24° Left 24° Right
Aileron 23° Up 17° Down
Flaps 35° Down
Serial Numbers Eligible CAMAIR Serial Numbers 1-050 and up.  Serial Numbers 1-081 and up are equipped
with a 24-volt electrical system.
Required Equipment In addition to the pertinent required basic equipment specified in CAR 3, the following
items of equipment must be installed:
1, 102, 103, 104 or 109*, 105, 201, 202, 205, 206, 304 or 305*, 401(a), 402.
Specifications Pertinent to All Models
Datum Fuselage Station 0, 93.25 inches forward of the forward bolt centerline (jig point) in wing
lower surface bolting angle.
Leveling Means External lugs on right side of fuselage at Station 58 and Station 89.4.
Certification Basis Type Certificate No. 2A2 (CAR 3 through Amendment 3-7).
Production Basis None.  Prior t original certification 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.
Equipment Items marked with an asterisk (*) are eligible only on aircraft equipped with 24-volt
electrical system.
Propellers and Propeller Accessories
1. (a) 2 Hartzell feathering type propellers 128 lb.  (+40)
Hubs HC-82XF-2B, blades 8433-2
Diameter:  Maximum 83 inches, Minimum allowable for repairs 80.5 inches
No further reduction permitted.
Pitch settings at 30 inch station:  Low 12°, High (Feathered) 78°.
Placard required:  "Avoid continuous ground operation between 2200 and 2500 rpm."
(b) 2 governors, Hamilton Standard 1Q12 or Woodward 210065 8 lb.  (+46)
(c) 1 propeller spinners, Hartzell bulkhead C-8067-1 and Hartzell dome C-888 7 lb.  (+37)
2. (a) 2 Hartzell feathering-type propellers 128 lb.  (+40)
Hubs 82XF-2B, blades 8433-4 required with Item 107.
Diameter:  Maximum 80 inches, Minimum allowable for repairs 78 inches.'
Pitch settings at 30 inch station:  Low 13.5°, High 35°, (Feathered) 78°.
(b) 2 governors, Hamilton Standard No. 1Q12 or Woodward 210065 8 lb.  (+46)
(c) 2 propeller spinners, Hartzell bulkhead C-807-1 and Hartzell dome C-888 7 lb.  (+37)
3. (a) 2 Hartzell feathering-type propellers 130 lb.  (+40)
Hubs HC-A2XF-2, blades 8433-04; with Item 107.
(b) 2 governors, Hartzell B-4-3; with Item 107.
(c) 2 propeller spinners, Hartzell bulkhead C-987-1, and Hartzell dome C-888 7 lb.  (+37)

Page 3 of 4 2A2
Engine and Engine Accessories - Fuel and Oil Systems
  101. 2 starters, Delco-Remy 1109471 32 lb.  (+75)
  102. 2 oil radiator, Harrison 8522493 13 lb.  (+48)
  103. 2 fuel pumps, Lear RD-7430-2 2 lb.  (+76)
  104. 2 fuel boost pumps, Lear RG-10340 14 lb.  (+70)
  105. 2 hydraulic pumps, New York Air Brake 67-AC-025  (67A025) 4 lb.  (+76)
  106. 2 vacuum pumps, Pesco 3P-194-E 8 lb.  (+77)
  107. 2 Continental IO-470-D engines  (Same limits as for O-470-B). Use Actual Weight
Engine mount modification required per CAMAIR Drawing 1-1021-19       Increase
modified by E.O. 947.  Installation to be in accordance with CAMAIR
Drawing 1-1081, Revision A.
Fuel 100/130 minimum grade gasoline
Propeller as listed under Item 2, and Item 401(c) required.
The propeller must be installed in the 102° position in relation
to the No. 1 crank pin location.  This is the position the propeller
is in when the dowel pins are located 90° to the centerline of the
blades and in the only dowel holes in the engine.
*108. 2 starters, Delco-Remy 1108234 32 lb.  (+75)
*109. (a) 2 fuel boost pumps, Lear RG-9480A 14 lb.  (+70)
(b) 2 fuel boost pumps, Weldon 4032-B; per CAMAIR Drawing 1-1052 13 lb.  (+70)
  110. 20 gallon auxiliary fuel tank; installed per CAMAIR Drawing 1-1085 19 lb.  (+151)
Landing Gear and Flats
  210. Two main wheel-brake assemblies, 6.50-8 18 lb.  (+114)
Goodyear wheel assy. No. 9531319, brake assy. No. 9531138
  101. Two 7.00-8 main wheel tires, y-ply rating, with tubes 31 lb.  (+114)
  205. One 7.00-6 nose wheel assy., Type III, Firestone 6C-5 or Goodrich 613MD 5 lb.  (+20)
  206. One 6.00-6 nose wheel tire, 6-ply rating, with tube 9 lb.  (+20)
Electrical Equipment
  301. 2 generators, Delco-Remy 1001892 33 lb.  (+74)
  302. 2 generator regulators, Delco-Remy 1118840 4 lb.  (+153)
  303. Paralleling relay, Delco-Remy 1116887 1 lb.  (+153)
  304. Battery, 12-volt, Gould U-37 37 lb.  (+151)
*305. Battery, 12-volt (2) Reading or Exide, S-24 46 lb.  (+151)
*306. Generator voltage regulator (2) Delco-Remy, 1118976 4 lb.  (+153)
*307. Starter relay (2) Autolite or Hart, B-8 2 lb.  (+153)
*308. Battery relay (2) Autolite or Hart, B-4 2 lb.  (+153)

2A2 Page 4 of 4
*309. Generator parallel relay, Delco-Remy, 1116902 2 lb.  (+153)
*310. Generator, 25-amp. (2), Delco-Remy, 1101911 38 lb.  (+74)
*311. 2 generators, 50 amp., Delco-Remy, 1105057 48 lb.  (+74)
Interior Equipment
  401. (a) FAA approved Airplane Flight Manual, dated September 20, 1955
(b) AFM Supplement for Lear L-2B Autopilot, dated June 25, 1955
(c) FAA Approved Airplane Flight Manual, Revision 3, dated March 18, 1959, pertinent to Items 2 and 107.
(d) AFM Supplement for Mitchell Autopilot AK045 (11-14-55)
(e) AFM Supplement covering approved operation of Auxiliary fuel tank neg
  402. Hand hydraulic power and control unit per CAMAIR Drawing No. 1-4005 3 lb.  (+80)
  403. (a) Heater assembly, Stewart Warner 940-B12, installed in accordance with
CAMAIR Drawing 1-4030. 20 lb.  (+45)
*(b) Heater assembly, Stewart Warner 940-B24 (24v), installed per
CAMAIR Drawing 1-4030. 20 lb.   (+45)
  404. Automatic pilot, Lear L-2B, installed in accordance with Lear Drawing No. 82894 41 lb.  (+170)
  and CAMAIR Engineering Order No. 461.
Servo Stall torque measured on the ground:  Elevator 30 ± 5 in. lb.;
   Aileron 25, +0, -10 in. lb; Rudder 50, +10, -0 in. lb.
Model 121G servo unit with 1-5/8 in. diameter capstans used.
  405. Mitchell Autopilot Model AKO45 installed in accordance with
Mitchell Bulletin No. 109 (wt. does not include gyros) 10 lb.  (+58)
  501. Wing Fairings; when installed per CAMAIR Drawing 1-3041 7 lb.  (+168)
  503. Grimes, D-7080, Rotating Beacon, when installed as per CAMAIR Drawing 1-4144 1 lb.  (+305)
  505. Flush Windshield Installation, when installed as per CAMAIR Drawing 1-4008 2 lb.  (+80)
NOTE 1. Current weight and balance report, including list of equipment included in certificated weight empty, and
loading instructions must be in each aircraft at the time of original airworthiness certification adn at all times
thereafter (except in the case of air carrier operators having an approved weight control system).
NOTE 2. In addition to the placards specified in the Airplane Flight Manual, Item 401(a), the following placard must
be displayed in front of and in clear view of pilots when propeller Item 1 is installed:
"Avoid continuous ground operation between 2200 and 2500 rpm."
NOTE 3. All of the aircraft covered by this specification are conversions of the single-engine Navion,
Specification A-782.  Aircraft produced under this type certificate will be identified by CAMAIR name-plate
only, and airworthiness considerations pertaining to the single-engine Navion only do not apply to the
CAMAIR 480.
...END...
```

## ADs (1, in force first)

- [AD 63-21-05](https://openairdocs.org/ad/63-21-05): Main and Nose Retraction Links · American Navion Society D-16, D-16A, 480 and 8 more

## Registered aircraft by registry model (OpenAirDocs)

- [Camair 480](https://openairdocs.org/model/camair-480): 8 aircraft (registry code 1890102)

## STCs approved under this data sheet (27)

- [STC SA04652CH](https://openairdocs.org/stc/SA04652CH): To allow use of 100R grade aviation fuel meeting Swift Fuel, LLC specification. Swift Fuels LLC
- [STC SA11137SC](https://openairdocs.org/stc/SA11137SC): Installation of Plane-Power ALT-FLX alternator. Hartzell Engine Technologies, LLC
- [STC SA01967WI](https://openairdocs.org/stc/SA01967WI): Use of GAMI G100UL High Octane Unleaded Avgas. General Aviation Modifications Inc.
- [STC SA03286CH](https://openairdocs.org/stc/SA03286CH): Install an electronic engine ignition system. Electroair Acquisition Corporation
- [STC SA04032CH](https://openairdocs.org/stc/SA04032CH): Install rocker switch assemblies. Electroair Acquisition Corporation
- [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.
- [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 SA1315WE](https://openairdocs.org/stc/SA1315WE): Installation of Mixture Monitor (exhaust gas temperature probe, gage and selector) in accordance with Delta Products Part Lists A-192 and A-193,  or in accordance with Tri-Star Corporation Mixture Monitor Installation Instructions dated December 9, 1981,  or later FAA approved revision and/or Drawing List MM-127 dated November 15, 1981,  or later FAA approved revision in aircraft models listed in Master Eligibility List P-80-A-6 revised March 29, 1968,  copy attached,  or later FAA approved revision.. Universal Corporation
- [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 SA1512WE](https://openairdocs.org/stc/SA1512WE): Installation of exhaust gas temperature monitoring systems Model EGT-1.. K S Avionics Inc
- [STC SA489EA](https://openairdocs.org/stc/SA489EA): Installation of ARP Inc. carburetor ice detection system. Aircraft & Rotorcraft Products (ARP) Inc
- [STC SA3328SO](https://openairdocs.org/stc/SA3328SO): Install landing gear wheel cover.. Goldman Don
- [STC SA142SO](https://openairdocs.org/stc/SA142SO): Installation of control wheel.. Garcia Joaquin
- [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 SA4302NM](https://openairdocs.org/stc/SA4302NM): Installation of Electronics Int'l digital automatic engine analyzer.. Electronics International
- [STC SA334SW](https://openairdocs.org/stc/SA334SW): Installation of InterAv Alternator.. InterAv, Inc
- [STC SA308EA](https://openairdocs.org/stc/SA308EA): Installation of carburetor ice detection system 105AP in single and twin engine aircraft and single engine helicopters powered by Continental, Franklin, and Lycoming type engines equipped with Marvel-Schebler MA-2, MA-3, MA-4, MA-4-5, MA-6 and HA-6 series carburetors. (Normal,Utility and Acrobatic Category airplanes and helicopters equipped with engines and carburetors as described.). Alfred R Puccinelli
- [STC SA1675WE](https://openairdocs.org/stc/SA1675WE): Installation of exhaust gas temperature monitoring systems EGT-2.. K S Avionics, Inc
- [STC SA798EA](https://openairdocs.org/stc/SA798EA): Installation of Monitair exhaust gas combustion monitor kit.. Rosemount Engineering Co
- [STC SA2105WE](https://openairdocs.org/stc/SA2105WE): Installation of Model EGT-3 exhaust gas temperature monitor(with rising temperature alarm). (DC-6B (NAVY R6D-1Z) 680). K S Avionics, Inc
- [STC SA219EA](https://openairdocs.org/stc/SA219EA): Installation of Katz integrated flight indicator Model KIFI-2 or KIFI-2A.. Forest City Avn Svc Inc
- [STC SA162EA](https://openairdocs.org/stc/SA162EA): Modification of Navion retract link assembly 145-34106.. Rudolph Chalow
- [STC SA200CE](https://openairdocs.org/stc/SA200CE): Nose and main gear retracting link replacement.. Western Machine Repair Service
- [STC SA262SO](https://openairdocs.org/stc/SA262SO): 24-volt starting system.. Atlanta Aero Service Inc
- [STC SA278SO](https://openairdocs.org/stc/SA278SO): Main and nose landing gear retract links.. William E Freeman
- [STC SA492WE](https://openairdocs.org/stc/SA492WE): Full flow lube oil filter 40409A with element 1A0235.. Winslow Aerofilter Corp
- [STC SA1-396](https://openairdocs.org/stc/SA1-396): Navion retract links 143-33165 and 143-33165-10 modified.. Rudolph Chalow

---
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