STC SA106SW

Supplemental type certificate · Signature Flight Support Corporation

Holder
Signature Flight Support Corporation · United States
Status
Current · Reissued
Status date
August 31, 2000
Applied
August 1, 1962
Product
Aircraft · Large Airplane
Certification basis
Part 21
Data sheet
TCDSA-723

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

What it approves

Installation of Model M-4 autopilot.

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.

jState* ©f of tEr»nsp0rteit0tt - Jtfeaeral ^(nation Certificate SA106SW Signature Flight Support Corporation, a Delaware Corporation 7511 Lenunon Avenue, Hangar C Dallas, TX 75209 at £f f> Civil Air 723 Lockheed 18 Installation of Model M-4 Autopilot in accordance with data listed on Aerodyne Engineering Corp. Drawing List titled, "Model M-4 Autopilot Installation - L-18" Revision 3 dated 11/14/62, or later FAA approved revision.

(See continuation sheet 3 of 3) f .

.• August 01, 1962 July 11, 1963 ; 12/21/98; 8/31/00

- June 30, 1982 Rev. 6 0 (Signature) . „, J. Frances Cox / Manager, Special Certification Office, / Southwest Region (Title) tltfcatlon of Cflld certificate Js punishable t/y 4 fine of not SI'000, or jcnjwrtC not exceeding 3 years, or Forn B110-2 I10-6B) Poga 1 of 3 This certificate nay be transferred In accoi-daaee wlttt FAR 21.41.

JHnttsb Jitat^E <Sf ^mrrica department nf Wranspartaium - ,3jp&eral J^&lattnn ,A&mmtetratinit Certificate ((ttonttttuatimt SA106SW Date of Issuance: July 11, 1963 Date Amended: June 30, 1982 Reissuance Date: August 31, 2000 (Continued):

1. This modification is eligible only on Standard SR407 Lockheed 18 aircraft with FAA approved spring rudder tab installation.

2. FAA approved Airplane Flight Manual Supplement dated 11/30/62 is required.

3. Servo clutch settings are as follows:

Rudder 60 pounds Ailerons 150 pounds Elevators 150 pounds Elevator Trim 30 pounds -END- Any alteration of this certiflcate Is punishablf by a fine of not exceeding $1,QQO, or ioprlsofiofnt not exceeding 3 years, or both, FAA Form 8llO~2-l{lQ-69) Page 3 of 3 Tftls certificate may be tfJnsrWred in accordance vllh FAR 21-47.

1 N3TRI IUT] ONS '['he iriinsfcr endorse me in Ijdovi may be used lo rionK ihc .i|>jin>|>rialc FA A I1 rgional Of lire of [hi- tr.inslrr of this Supplemental Type Crriifualt' I'lii1 I -\A "ill rnssue thr <.erLJhrale in the name ol ihi- Iransferee and luruaril n lo linn

TRANSFER ENDORSEMENT Transfer the ownership of Supplemental Type Certificate Number __ lo (Name of transferee) (Address of t'ansjeref) __ /umbfi and street) (City, StaU. and %1P aidtj from (Name of grantor) (Print or type) (Address vj grantor) (ffumtir anil Uriel/ I City, SlaU, ami ?IP cade I Exlent of Authority (if licensing agreement):

Signature of grantor (In ink):.

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
Lockheed Martin Aeronautics Company18A-723