STC SA4995NM

Supplemental type certificate · Rockwell Collins Aerospace & Electronics Inc. Flight Dynmics Division

Holder
Rockwell Collins Aerospace & Electronics Inc. Flight Dynmics Division · United States
Status
Current · Reissued
Status date
March 7, 2012
Applied
November 15, 1990
Product
Aircraft · Large Multi-Engine
Certification basis
Part 21, Part 25
Data sheet
TCDSA-817

From FAA DRS, with our copy of the certificate PDF. DRS record last changed December 5, 2025.

What it approves

Installation of model 1500 head up guidance system.

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.

Number SA4995NM

This certificate, issued to Rockwell Collins, Inc.

27300 SW Parkway Ave Wilsonville, OR 97070

Part 25 of the Federal Aviation Regulations.

Original ProductType Certificate Number: A-817 Make: Fokker Model: F27-500

Description of the Type Design Change: Installation of Flight Dynamics, Model 1500, Head-Up Display Guidance System per Flight Dynamics Master Drawing List 9701-0960, Revision H, dated November 26, 1990, or later Federal Aviation Administration (FAA) approved revision.

Limitations and Conditions: The approval of this change in type design applies to Fokker F27-500, serial numbers 10191 through 10504, equipped as listed on Continuation Sheet, page 3. This approval should not be extended to other aircraft of this model on which other previously approved modifications are incorporated unless it is determined by the installer that the interrelationship between this change and any other previously approved modifications will introduce no adverse effect upon the airworthiness of that aircraft.

Date of application: November 15, 1990 Date reissued: 6/14/93; 4/16/03; 1/21/10; 3/7/12 Date of issuance: November 27, 1990 Date amended: April 16, 2003

(Signature) Acting Manager, Seattle Aircraft Certification Office (Title)

Number SA4995NM

Rockwell Collins, Inc.

Issued: November 27, 1990 Reissued: 6/14/93; 4/16/03; 1/21/10; 3/7/12 Amended: April 16, 2003

This change has only been demonstrated to be acceptable for use in operations associated with Category I and II Landing Minima as defined in FAA Advisory Circular 120-29.

AIRCRAFT EQUIPMENT LIST AND

SENSOR TYPE

NUMBER MANUFACTURER MODEL Inertia Navigation System 1 Litton LTN-92 Digital Air Data Computer 2 Penny & Giles D60163MK3 Navigation Receiver 2 King KNR-6030 Radio Altimeter 2 Rockwell-Collins 860F-4 Distance Measuring Equipment 1 Rockwell-Collins 860E-2 Vertical Gyro 1 Honeywell 311, 312, or 313 Directional Gyro 1 Honeywell 242

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.

-END-

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 · 1

MakeModelData sheet
Fokker ServicesF.27 Mark 500A-817

Every issue · 2

DRS keeps each issue of an STC as its own record, with its own certificate and attachments.

DateStatusFiles
March 7, 2012Reissued, currentCertificate
January 21, 2010Reissued, currentCertificate