# TCDS TC 2-9: Miller Edward B.

- Type: Type certificate data sheet
- Status: Current
- Holder: Miller Edward B.
- Revision: 0
- Product: Aircraft, Glider
- Data sheet PDF: https://openairdocs.org/files/sha256/8e/0d/8e0dd0b6846786e1e5803a996fee5bcdf6180a54f9ab0088ed7b32fb415ef019
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/569887E2B4422FCF8525673C0054EACA.0001
- Page: https://openairdocs.org/tcds/TC%202-9

## Models (1)

As the data sheet lists them.

- Dawydoff Cadet UT 1

## What the data sheet says

This is OCR from the scanned FAA data sheet. OCR can misread letters and numbers.

```text
MILLER, EDWARD E.
MODELS: Miller Dawydoff-Cadet UT-1 (Glider), 1 PCLM
T.C. NUMBER: 2-9
I - Model UT-1, 1 PCIM (Approved 11/30/43)
•YpE
irspeed limit:  Glide or dive - 65 mph True Ind.
Auto-winch tow - 45 mph True Ind.
C.G. range  (28.1 percent MAC) to (+17.8)
(+32.5 percent MAC)
Datum  Wing leading edge at side of fuselage
MAC  54.6 in. I.E. MAC (0)
leveling means  Longerons at cockpit horizontal
Standard weight
No. seats  1 (-4) (See NOTE 1)
Baggage
Control surface  flevator  Up 34 degrees  Down 34 degrees
movements  Rudder  Right 28 degrees  Left 26 degrees
Aileron  Up  8 degrees  Down 29 degrees
Stabilizer  Up  1 degree  Down O degrees
Serial Nos.  • onli  eligible
Required equirment  tems 401 and 40
SPECIFICATIONS PERTINENT TO ALL MODELS:
Certification basis  CAR 05.031
EQUIPtems included in required lists under specifications pertinent to individual  models may not be removed unless replaced by approved equivalent items.
The effect upon balance of all equipment changes must be computed and the
aircraft operation record revised accordingly.
Values in inches shown in parenthesis after each item represent horizontal
arms to the C.G. of the item measured minus (-) ahead and plus (+) to the rear
of the datum.
A plus (+) or minus (-) sign preceding the weight of an optional item
indicates the net weight change between that item and the equivalent required
Interior Equipment:
401.  Air speed indicator  • 5 IDE  - 19
402. Altimeter  E 108  - 19
Miscellaneous (not listed above):
600.  Miscellaneous items as noted in
approved weight and balance report.
NOTE (İ¡  The following placards must be installed in full view of the pilot:
"Inverted flying prohibited."
"Shock-cord launching prohikited."
"Aircraft tow prohibited."
(a)  "visual-contact day flying only permitted.
(2)  Authorized Loadings
(a)  Maximum weight of pilot and parachute 170 lbs.
b) Minimum weight of pilot and parachute 120 lbs.
```

## ADs

None name its models.

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