- Holder
- Curtiss-Wright Corporation
- Revision
- 0
- Status
- Current
- Product
- Aircraft · Small Airplane
- Models
- 1
- Registered
- 1 aircraft
The release keeps the latest revision of each data sheet. Model names are as the data sheet lists them.
On this page
Models · 1
| Model | Also known as | Note |
|---|---|---|
| Travel Air 16-E |
Airworthiness directives · 0
ADs whose products are models on this data sheet, matched by model and maker.
No ADs matched this data sheet’s models
Registered aircraft
Registry models that point at this data sheet, with their registered aircraft.
STCs approved under this data sheet · 4
STC SA04652CHTo allow use of 100R grade aviation fuel meeting Swift Fuel, LLC specificationSTC SA01406NYInstallation of Airwolf remote mounted engine oil filter kit AFC-K017 on single and multi-engine fixed light aircraft and
rotary wingSTC SA00478CHInstallation of Cooper Superflite 102 Fabric.STC SA1256GLSurrendered and incorporated into STC SA00478CH.
What the data sheet saysOCR
This is OCR from the scanned FAA data sheet. OCR can misread letters and numbers.
MODELS: Curtiss-Wright Trarel Air 16-E, 2-3 PO-CLB, 3 POSB
I.C. NUMBER: ATC 463
Engine Wright R-540 175 bp
Propeller Adj. metal
Fuel 33 gallons (one wing CS tank)
oil 4 gallons
No. passengers
Baggage Landplane - 55 1bs. as 3-place; 60 1bs. as 2-place
Seaplane - 42 1bs.
Standard weight Landplane - 2150 1bs.
Seaplane - 2380 1bs.
Spec. basis Approved Type Certificate No. 463
Serial Nos. 3501 and up manufactured prior to 9/30/39 eligible.
Approval expired as of that date. (See NOTE 1)
Class I equipment:
Battery 30 1bs.; starter 32 lbs.; 6.50-10 wheels and brakes 68 lbs. or
Edo I-2260 gloats.
Class III equipment:
(Landplane only) coupe top 47 1bs., 10x3 tail wheel; (Landplane and
Seaplane) Extra 20 gallon fuel tank installed in front cockpit replacing tvo
passengers, net increase 9 1bs. (Tank installation 17 1bs., seat cushions and
safety belt removed 8 lbs.)
Seaplane eligible provided:
fuselage member from forward landing
point to upper engine mount attachment point is 1"x0.049 4130 steel
at Se todated in to 35 to 3. 8e, at es he tones gear strut attachment fitting
composed of a 1"1.049 4130 steel tube 22-1/2 in. long split along
center line and held in place over the longeron with 4 clamps.
Serials 3508 and up must have 7/8":x.049 steel tube (was 7/8"7.035).
The auxiliary fin on lower side of fuselage must be installed.
All must include fuselage side truss and longeron reinforcement at
front wing fitting made in accordance with manufacturer's Drawing
16E401, dated 12/30/36.