What it approves
Installation of GTCP Garrett36-150W APU.
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.
FAA Form 8110-2 (5/14) Page 1 of
Part of the
Signature
Title SA755NE Textron Aviation Inc.
One Cessna Boulevard Wichita, KS 67215 25 Federal Aviation Regulations.
Cessna 650 3 A9NM Installation of GTCP Garrett 26-150W APU in accordance with the data listed in PATS, Inc. Installation Drawing List:
Configuration 1; No. 651-1-000, Rev. B dated February 14, 1990 Configuration 2; No. 651-1-000, Rev. D dated March 20, 1992 Configuration 3; No. 651-1-000, Rev. E dated April 23, 1992 Configuration 4; No. 651-1-000, Rev. K dated January 29, 1993, or later FAA approved revision.
1. APU Operation is approved for ground and non-essential in-flight usage.
2. Configuration 1 is approved only for airplanes having STC SA490NE previously incorporated.
(see continuation sheet 3 of 3) July 6, 1992; April 27, 2017 April 20, 1992; May 8, 1992; July 8, 1992;
February 26, 1993 October 11, 1989 May 2, 1990 Mark Fuller STC ODA administrator ODA-100129-CE
FAA Form 8110-2 (5/14) Page 2 of
To (Name and address of transferee)
From (Name and address of grantor)
FAA Form 8110-2 (5/14) Page 3 of
Date of Issuance: May 2, 1990 Date Amended: February 26, 1993 Date Reissued: April 27, 2017
3. Configuration 2 is eligible for Model 650, Citation VI Serial Number 213.
4. Configuration 3 is eligible for Model 650, Citation VI Serial Number 0220 through 7000 and Citation VII Serial Number 7005 and up.
5. Configuration 4 is eligible for Model 650, Citation III Serial Number 650-0082 and 650-0152.
6. PATS, Inc. Airplane Flight Manual Supplement No. 11, dated May 2, 1990, or later FAA approved revision is required with Configuration No. 1.
a. PATS, Inc., Airplane Flight Manual Supplement No. 12, dated April 20, 1992, or later FAA approved revision, is required with Configuration No. 2.
b. PATS, Inc., Airplane Flight Manual Supplement No. 12, dated April 20, 1992, or later FAA approved revision, is required with Configuration No. 3, Citation VI and VII or :
c. Cessna Citation VI Flight Manual Supplement 19, dated June 22, 1992, or later FAA approved revision.
d. Cessna Citation VII Flight Manual Supplement 18, dated June 22, 1992, or later FAA approved revision.
e. Cessna Citation III Flight Manual Supplement 67, dated January 25, 1993, or later FAA approved revision is required with Configuration No. 4.
7. PATS, Inc., Maintenance Manual Report No. 433 "Cessna 650-GTCP 36-150W, Auxiliary Power Unit," in accordance with STC SA755NE dated May 2, 1990, is required for continued airworthiness of Configuration 1.
8. PATS, Inc., Maintenance Manual Report No. 482 "Cessna 650 GTCP 36-150W Auxiliary Power Unit," are required for continued airworthiness of Configuration 2, 3 and 4.
9. This approval should not be extended to other specific airplanes of this model on which other previously approved modifications are incorporated, unless it is determined that the interrelationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of that airplane.
-- END -- 3 SA755NE
ADs that name this STC · 0
An AD can apply because an STC is installed, or mention one in its text.
Approved models · 1
| Make | Model | Data sheet |
|---|---|---|
| The Cessna Aircraft Company | 650 | A9NM |
Every issue · 2
DRS keeps each issue of an STC as its own record, with its own certificate and attachments.
| Date | Status | Files |
|---|---|---|
| April 27, 2017 | Reissued, current | Certificate |
| February 26, 1993 | Amended, earlier issue | Certificate |