# TCDS A19EU: Aeronautica Macchi S.p.A. & Aerfer-Industrie Aerospaziali Meridionali S.p.A.

- Type: Type certificate data sheet
- Status: Current
- Holder: Aeronautica Macchi S.p.A. & Aerfer-Industrie Aerospaziali Meridionali S.p.A.
- Revision: 1
- Revised: February 26, 1969
- Product: Aircraft, Small Airplane
- Certification basis: Part 21, Part 23
- Data sheet PDF: https://openairdocs.org/files/sha256/85/6b/856bc59340fdd25662f76fcdf357b07fa6bba0a0b96011be98532e53ccfb268d
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/77666705A41998A48525672A0070C283.0001
- Page: https://openairdocs.org/tcds/A19EU

## Models (1)

As the data sheet lists them.

- AM-3

## 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
Rev No. 1 1 1
DEPARTMENT OF TRANSPORTATION
FEDERAL AVIATION ADMINISTRATION
A19EU
Revision 1
AERONAUTICA MACCHI
AERFER
AM-3
February 26, 1969
TYPE CERTIFICATE DATA SHEET NO. A19EU
This data sheet which is a part of type certificate No. A19EU prescribes conditions and limitations under which the product for
which the type certificate was issued meets the airworthiness requirements of the Federal Aviation Regulations.
 Type Certificate Holders AERONAUTICA MACCHI S.p.A.        & AERFER-INDUSTRIE AEROSPAZIALI
(See NOTE 4) Via Sanvito Silvestro, 80 MERIDIONALI S.p.A.
Varese, Italy Pomigliano D'Arco,
Napoli, Italy
I.  Model AM-3 (Normal and Utility Category), Approved November 15, 1968.
Engine Continental GTSIO-520-C
Fuel 100/130 minimum grade aviation gasoline
Engine Limits For all operations:
   34.5 in.hg., 3200 r.p.m. (340 h.p.)
Propeller and Hartzell HC-A3VF-4/V8833
   Propeller Limits Diameter:  Maximum 88 3/8 in., Minimum allowable for repair 86 3/8
in.       (No further reduction permitted)
Pitch setting at 30 in. radius:  Low 15.0 degrees, High 36.7 degrees
Airspeed Limits (IAS) Never exceed 172 knots  (198 m.p.h.)
Maximum structural cruising 125 knots  (144 m.p.h.)
Maneuvering 123 knots  (142 m.p.h.)
Flaps extended 93 knots  (107 m.p.h.)
C.G. Range Utility Category:
  (+124.0) to (+133.8) at 3086 lb. or less
  (+125.3) to (+133.8) at 3307 lb.
  Straight line variation between points given.
Normal Category:
  (+124.0) to (+133.8) at 3086 lb. or less
  (+125.2) to (+133.8) at 3307 lb.
  (+128.0) to (+132.3) at 3858 lb.
  Straight line variation between points given.
Empty Weight C.G. Range None.
Datum 110.16 in. forward of leading edge of wing at wing root.
Levelling Means Cabin floor, front seat rails.

A19EU, Rev 1
Page 2
Maximum Weight    Utility Category Normal Category
Takeoff 3307 lbs       3858 lbs
Landing 3307 lbs        3664 lbs
No. Seats 3;  1 (+118.1), 1 (+157.5), 1 (+183.9)
Maximum Baggage 200 lb. (+183.9)
Fuel Capacity 63 gal. total; 58.5 gal. usable (2 wing tanks)  (+137.5)
Oil Capacity 13 qt. (+50.4), usable 9 qt.
See NOTE 1 for unusable fuel and oil.
Control Surface Movements Wing Flaps Down 37° + 1°
Aileron      Up 18° + 1° Down 11° 30'  + 1°
Elevator      Up 30° + 1° Down 20° + 1°
Rudder  Right 19° + 1° Left 20° + 1°
Horizontal   (Plus) 3° + 1/2° (Minus) 7° + 1/2°
   Stabilizer
Serial Numbers Eligible The Registro Aeronautico Italiano (R.A.I.) Certificate of
Airworthiness endorsed as noted below under "Import Requirements"
must be submitted for each individual aircraft for which
certification is made.
Certification Basis FAR 21.29, FAR 23 effective February 1, 1965, including Amendment 23-1
through 23-3.
Type Certificate No. A19EU issued November 15, 1968.
Date of Application for Type Certificate:  November 16, 1965.
Import Requirements A U.S. Airworthiness Certificate may be issued on the basis of a
 Certificate of Airworthiness for Export signed by a representative of
the Registro Aeronautico Italiano (R.A.I.) containing the following
statement:  "The airplane covered by this certificate has been examined
and found to comply with U.S. Federal Aviation Regulation FAR 23,
effective February 1, 1965 including Amendment 23-1 through 23-3
and conforms to T.C. A19EU."
Equipment The basic required equipment as prescribed in the applicable
airworthiness regulations (See Certification Basis) must be installed
in the aircraft for certification.  In addition, the following items
of equipment are required:
(a) Pre-stall warning indicator, Safe Flight Instrument Corp. 164 R.
(b) R.A.I. approved Airplane Flight Manual dated October 31, 1968.
NOTE 1. Current weight and balance report including list of equipment included in certificated
empty weight, and loading instructions when necessary, must be provided for each aircraft
 at time of original certification.
The certificated empty weight and corresponding center of gravity locations must include
unusable oil of 7.5 lb. at (+50.4) and unusable fuel of 27 lb. at (+137.5).

A19EU, Rev 1
Page 3
NOTE 2. The following placard must be displayed on the forward instrument panel in front and in
clear view of the pilot:
"THIS AIRPLANE MUST BE OPERATED AS A NORMAL OR UTILITY CATEGORY
AIRPLANE IN COMPLIANCE WITH THE APPROVED AIRPLANE FLIGHT MANUAL.
ALL MARKINGS AND PLACARDS ON THIS AIRPLANE APPLY TO ITS OPERATIONS
AS A NORMAL CATEGORY AIRPLANE, FOR UTILITY CATEGORY OPERATIONS,
 REFER TO THE AIRPLANE FLIGHT MANUAL.
NO ACROBATIC MANEUVERS, INCLUDING SPINS, ARE APPROVED FOR
NORMAL CATEGORY OPERATIONS."
FOOTNOTE:
All placards required in the approved Airplane Flight Manual must be installed in the
appropriate locations.
NOTE 3. Each individual airplane will be supplied with a placard that specifies the kinds of
operation such as VFR or IFR, Day or Night, to which the operation of the airplane is
limited by the equipment installed.
NOTE 4. Aeronautica Macchi S.p.A. is the responsible Company and contact for any notification and
action with the Federal Aviation Administration.
-END-
```

## ADs (2, 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 2005-01-19](https://openairdocs.org/ad/2005-01-19): Mode S transponders · GARMIN International GTX 330D, GTX 330, GTX 33D and 830 more. Effective Feb 23, 2005

## Registered aircraft by registry model (OpenAirDocs)

- [Macchi AM-3](https://openairdocs.org/model/macchi-am-3): 0 aircraft (registry code 5400105)

## STCs approved under this data sheet (29)

- [STC SA12406WI](https://openairdocs.org/stc/SA12406WI): Installation of a Garmin AXIS Flight Display System. Garmin International Inc.
- [STC SA239SW](https://openairdocs.org/stc/SA239SW): Installation of Alcor exhaust gas temperature (EGT) indicator kits. Alcor LLC
- [STC SA5581SW](https://openairdocs.org/stc/SA5581SW): Installation of ALCOR true-flow/ totalizer system. Alcor LLC
- [STC SA02738CH](https://openairdocs.org/stc/SA02738CH): Installation of L-3 Communications Avionics Systems. Acron Aviation Inc.
- [STC SA02571SE](https://openairdocs.org/stc/SA02571SE): Installation of Garmin G500/G600 TXi Integrated Avionics System (Primary Flight Display, Multi-Function Display, and Engine Indicating System Display).. Garmin International Inc.
- [STC SA01899WI](https://openairdocs.org/stc/SA01899WI): Installation of Garmin G3X Touch Electronic Flight Instrument System. Garmin International Inc.
- [STC SA01818WI](https://openairdocs.org/stc/SA01818WI): Installation of Garmin G5 Electronic Flight Instrument. Garmin International Inc.
- [STC SA11174SC PAGE 1](https://openairdocs.org/stc/SA11174SC%20PAGE%201): Installation of BendixKing by Honeywell KSN 770 and KSN 765 WAAS LPV approach capable nav/comm systems. Honeywell International Inc (Bendix King)
- [STC SA00401BO](https://openairdocs.org/stc/SA00401BO): Installation of a SkyTrax100B UAT receiver. Avidyne Corporation
- [STC SA02268CH](https://openairdocs.org/stc/SA02268CH): Installation of Airwolf Filter Corp. Air Oil Separator. Airwolf Filter Corporation
- [STC SA04165NY](https://openairdocs.org/stc/SA04165NY): Installation of Latitude Technologies Skynode S200 Satcom system must be performed. Latitude Technologies Corporation
- [STC SA02153LA-D PAGE 1](https://openairdocs.org/stc/SA02153LA-D%20PAGE%201): Installation of Garmin G600 Primary Flight Display (PFD) and Multifunction Display (MFD) System. Garmin International Inc.
- [STC SA01933LA-D](https://openairdocs.org/stc/SA01933LA-D): Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System. Garmin International Inc
- [STC SA00382BO](https://openairdocs.org/stc/SA00382BO): Installation of Globalstar Antenna and Cradle provisions to support a Globalstar GPS-1700 in non-composite airplanes. Avidyne Corporation
- [STC SA00343BO](https://openairdocs.org/stc/SA00343BO): Installation of a single configuration or a dual configuration Avidyne Corporation Integrated Flight Display, Model IFD540 loaded with Release 10.0 software (or later FAA approved release). Avidyne Corporation
- [STC SA00352BO PAGE 1](https://openairdocs.org/stc/SA00352BO%20PAGE%201): Installation of an Avidyne Corporation Mode A/C/S Transponder with ADS-B Out capability, Model AXP340 loaded with Version 3.13 software (or later FAA approved version),. Avidyne Corporation
- [STC SA01229SE PAGE 1](https://openairdocs.org/stc/SA01229SE%20PAGE%201): Installation of GNS 480 (CNX80) GPS WAAS Navigator with integrated VHF Navigation and Communication radios. Garmin International Inc
- [STC SA01933LA-D PAGE 1](https://openairdocs.org/stc/SA01933LA-D%20PAGE%201): Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation
System. Garmin International Inc
- [STC SA02717NY PAGE 1](https://openairdocs.org/stc/SA02717NY%20PAGE%201): Installation of VoiceFlight Systems LLC VFS101 Speech Recognition Module. VoiceFlight Systems LLC
- [STC SA02015SE-D](https://openairdocs.org/stc/SA02015SE-D): Installation of Garmin G500 Primary Flight Display (PFD) and Multifunction Display (MFD) System.. Garmin International Inc
- [STC SA03148NY](https://openairdocs.org/stc/SA03148NY): The installation of the Latitude Technologies Corporation S100 Tracking System. Latitude Technologies Corporation
- [STC SA02016SE-D](https://openairdocs.org/stc/SA02016SE-D): Installation of Garmin GTS 800, GTS 820 or GTS 850 Traffic System. Garmin International Inc
- [STC SA01487SE-D](https://openairdocs.org/stc/SA01487SE-D): Installation of a GDL 69 or GDL 69A XM Satellite Receiver. Garmin International Inc
- [STC SA2683NM](https://openairdocs.org/stc/SA2683NM): Installation of Precise Flight, Inc. stand-by vacuum system (SVS). Precise Flight Inc
- [STC SA02154AK](https://openairdocs.org/stc/SA02154AK): Installation of the UPS Aviation Technologies Inc. Apollo MX20 multi-function display, P/N 430-0270-500.. Garmin AT Inc.
- [STC SA2820SW](https://openairdocs.org/stc/SA2820SW): Operation with right door removed for parachute jumping.. Hurst Jack A
- [STC SA02153LA-D](https://openairdocs.org/stc/SA02153LA-D) (historical): Installation of Garmin G600 Primary Flight Display (PFD) and Multifunction Display (MFD) System. Garmin International Inc
- [STC SA02717NY](https://openairdocs.org/stc/SA02717NY) (historical): Installation of VoiceFlight Systems LLC VFS101 Speech Recognition Module. VoiceFlight Systems LLC
- [STC SA02153LA](https://openairdocs.org/stc/SA02153LA) (historical): Installation of Garmin G600 Primary Flight Display (PFD) and Multifunction Display (MFD) System.. Garmin AT Inc.

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