STC SA441NW

Supplemental type certificate · AAR Aircraft Services Inc

Holder
AAR Aircraft Services Inc · United States
Status
Current · Reissued
Status date
March 5, 1999
Applied
March 14, 1977
Product
Aircraft · Small Multi-Engine
Certification basis
Part 21
Data sheet
TCDS1A10

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

What it approves

Installation of two Hartzell HC-E3VR-2ATF/FC7663-2R three-bladed propellers, and Piper Navajo spinner assembly (P/N 43940-00) and associated systems.

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.

jantteb ^tates ©f , department of 'Sransportatton - Jifcheral ^fetation ^hmtntstratton (Eerttftotte SA441NW AAR Aircraft Services, Inc.

DBA: AAR Aircraft Services-Oklahoma 6611 South Meridian Oklahoma City, OK 73159-1104 Civil Air dated November 11, 1949.

1 Al 0 Piper PA 23-250 Installation of two Hartzell HC-E3YR-2ATF/FC7663-2R three-bladed propellers, and Piper Navajo spinner assembly (P/N 43940-00} and associated systems in accordance with Western Skyways Installation Instructions No. WS-601.

(See continuation sheet 3 of 4) r/a/a ca/iein .• March 14, 1977 o/eMaasice . April 26, 1977 . 7/22/88; 3/5/99 January 12, 1978 f (^S) I (Signature) S. Francfes-^Cox, Managei Special Certification Office, Southwest Region (Title)—————————— Any alteration o/ t/iis certificate is punishable by a fine of not exceeding 51,000, or imprisonment not exceeding 3 years, or both.

PJmttb plates Pepartnuml of tEranspartattmt - Jfeberal ,A&tatt0tt ^Ahmtniatration (Eerttftcate (Olotttmuatttttt tSVeisrb&est SA441NW Date of Issuance: April 26, 1977 Reissuance Date: March 5, 1999 (Continued):

Approval of this change in type design applies to the above model aircraft only.

This approval should not be extended to aircraft of this model on which other previously approved modifications are incorporated unless it is determined that the interrealtionship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of that aircraft. This approval is intended for installation in the above model with the Lycoming 10-540 series and TIO-540-C1A engines. A copy of this Certificate, Addendum No. SA441NW, FAA Approved Flight Manual Supplement, and Installation Instructions No. WS-601 shall be maintained as part of the permanent records for the modified aircraft.

SUPPLEMENTAL TYPE CERTIFICATE ADDENDUM NUMBER SA441SW The conditions and limitations of Type Certificate Data Sheet No. 1A10 apply except as follows:

This STC Addendum, which is part of Supplemental Type Certificate No. SA441SW, prescribes conditions and limitations under which the product for which the STC was issued meets the airworhtiness requirements of the Civil Air Regulations. A copy of this STC Addendum is required to be maintained as part of the modified aircraft's permanent records.

SUPPELEMENTAL TYPE CERTIFICATE HOLDER: AAR Aircraft Services, Inc.

DBA: AAR Aircraft Services-Oklahoma I. PIPER MODEL PA-23-250 5 PCLM (NORMAL CATEGORY) OR 6 PCLM (NORMAL CATEGORY) WHEN ITEM 603(b) IS INSTALLED Serial Nos. Eligible: 27-2505 through 27-7654001 Required Equipment: (Serial No. 27-2505 through 27-3836, 27-3838 through 27-3943 at 4800 Ibs. maximum weight) Add 1 (o).

(Serial No. 27-2505 through sy-3836, 27-3838 through 27-3943 at 5200 Ibs. maximum weight) Add 1 (o).

(Serial No. 27-3837, 27-3944 through 27-4425, 27-4427 through 27-4573) Add 1(o).

(Serial No. 27-4426, 27-4574 through 27-7654001) Add l(o).

FAA Form 8110-2-1(10-69) Page 3 of 4

pCwtteh plates ©f J^nertca of transportation - ^hcral Jk&iatton ^Jmtimstratton (tterttftcate SA441NW Date of Issuance: April 26, 1977 Reissuance Date: March 5, 1999 asw£(ye>sMdi&0rt<i (Continued):

Production Basis: None. Parts manufactured under this STC may have been produced without an FAA approved quality control procedure. Prior to installation, such parts must be inspected for conformity and airworthiness in accordance with FARs 21 and 43.

Prior to returning modified aircraft to service, conformity with approved installation data must be determined.

Propeller and Propeller Accessories: 1. (o) Hartzell HC-E3YR-2ATF with FC7663-2R blades. 81.0 Ibs. ea. (+24) Pitch settings at 30" Sta:

Low: 13.0; High: 80.0° (feathered) Diameter: Not over 76.0"; Not under 75.0" NOTE: Eligible only on PA-23-250, Serial Numbers 27-2505 through 27-7654001 when installed in accordance with STC SA441NW. NOT TO BE INTERMIXED WITH OTHER PROPELLERS.

2. (a) Piper spinner consisting of: Cap assembly, Part No. 43929-00; Bulkhead assembly, Part No. 43933-00; and Spinner assembly, Part No. 43940-00.

Interior Equipment: 401 (CR) WE602 dated April 26, 1977, is the FAA Approved Flight Manual Supplement and is required on Piper PA-23-250, Serial Number 27-2505 through 27-7654001 when Item 1 (c) and 2 (a) are installed in accordance with STC SA441NW.

-END-

47.

TRANSFER ENDORSEMENT Transfer the ownership of Supplemental Type Certificate Number to (Name of transferee) (Address of transferee) (dumber and street) (City, Slate, and ^IP code) from (Name of grantor) (Print or type) .

(Address of grantor) (Number and street} (City, Slate, and <7/> code) Extent 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
Piper Aircraft Inc.PA-23-2501A10