STC SA819EA

Supplemental type certificate · Honeywell International Inc.

Holder
Honeywell International Inc. · United States
Status
Current · Reissued
Status date
June 4, 2007
Applied
February 10, 1970
Product
Aircraft · Single-Engine
Certification basis
Part 3, Part 21, Part 23
Data sheets
TCDS3A16TCDS2A13

From FAA DRS, with our copy of the certificate PDF. DRS record last changed December 6, 2025.

What it approves

Alteration to replace standard anti-collision light with Grimes Series 550 single anti-collision red or white strobe kit.

What the certificate says

From the PDF’s text layer, without the form’s printed wording. Layout and order may differ; the PDF is the record.

550 Route 55 Urbana, OH 43078

Part 3/23 of the Civil Air / Federal Aviation Regulations.

(See Type Certificate Data Sheet as shown on Eligibility List STC Continuation Sheet Page 3 of 3 for complete certification basis).

See Eligibility List Original Product--Type Certificate Number :

Make : STC Continuation Sheet Model : Page 3 of 3

Alteration to replace the standard anticollision light with Grimes Series 550 single anticollision Red or White Strobe Kit P/N 34- 0001-1 or 34-0001-2 in accordance with Grimes Manufacturing Company Specification Sheets P/N 34-0001-1, -2, -3, and -4, dated January 7, 1972, revised March 7, 1978, or later FAA approved revision.

1) Install following placard or other FAA Approved equivalent:

“CAUTION TURN OFF STROBE LIGHT WHEN TAXIING NEAR OTHER AIRCRAFT OR WHEN FLYING IN FOG OR CLOUDS. STANDARD POSITION LIGHTS MUST BE USED FOR ALL NIGHT OPERATIONS.”

(See STC Continuation Sheet Page 3)

Date of application : February 10, 1970 Date reissued : May 5, 1988, November 5, 1991, June 4, 2007

Date of issuance : May 18, 1970

Date amended : September 17, 1970, May 2, 1972, March 30, 1978

( Signature) Charles L. Smalley Manager, Systems and Flight Test Branch Chicago Aircraft Certification Office

( Title)

FAA FORM 8110-2-1(10-69) PAGE 3 of 3 PAGES

Number SA819EA Date Reissued: June 4, 2007

Limitations and Conditions: Cont.

2. This approval applies only to replacement of lights installed as part of FAA approved original type design.

3. Minimum required operating voltage is:

12.6 volts on 14 VDC systems using power supplies P/N’s 60-1431-1, or 60-1473-1

24 volts on 28 VDC systems using power supplies P/N’s 60-1431-3, or 60-1473

12.6 volts on either 14 or 28 VDC system using power supply P/N 60-2927-1.

4. The P/N 60-1431-1 or -3 Power Supplies may be used in place of 60-1473- or -3 Power Supplies, respectively, or Power Supply 60-2927-1 , may be used in place of any of the above power supplies, in order to provide for an additional Grimes anticollision strobe light. The preceding is a statement of compatibility of power supplies only. This STC does not approve the installation of additional anticollision lights.

5. The combination of the Power Supplies listed in limitation 4 with light P/N 30-0504-1 or -3 which have been manufactured under FAA-PMA meets the requirements of FAR 23.1401 (b), (c) and (d) when the minimum operating voltage requirements have been met. P/N 30-0504-3 (Red) meets FAR 23.1401 (f) prior to 8/11/71. P/N 30-0504-1 (White) meets FAR 23.1401 (f) effective 8/11/71.

6. The approval of this change in type design applies basically to the aircraft listed on the Eligibility List. This approval should not be extended to other aircraft of these models on which other previously approved modifications are incorporated unless it is determined by the installer that the interrelationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of that aircraft.

7. If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other person written evidence of that permission.

ELIGIBILITY LIST

The following aircraft have been approved for installation of the Grimes Series 550 Single Anticollision Red or White Strobe Kit P/N 34-0001-1 or 34-0001-2 (applicability depends on matching aircraft electrical system voltage).

AIRCRAFT MANUFACTURE MODEL TYPE CERTIFICATE

Beech 95, B95, B95A, 95-55, 95-A55, 95-B55, 95-B55b (T-42A), 95-C55 3A16

Piper PA-28-140, PA-28-150, PA-28-160, PA-28-180, PA-28-235, PA-28-S-160, PA-28-S-180, PA-28R-180, PA-28R-200 3A13

…END…

FAA FORM 8110-2-1(10-69) PAGE 3 of 3 PAGES

ADs that name this STC · 0

An AD can apply because an STC is installed, or mention one in its text.

No AD in this release names this STC

Approved models · 16

MakeModelData sheet
Hawker Beechcraft Corporation953A16
Hawker Beechcraft Corporation95-553A16
Hawker Beechcraft Corporation95-A553A16
See all 16 models