What it approves
Installation of a Hartzell HC-C3YR-1RF/F7282, constant speed propeller, and Hartzell 835-47(P) or 835-52(P) spinner.
What the certificate saysOCR
This is OCR from the scanned FAA certificate. OCR can misread letters and numbers.
United States of America SA95Y CH-A Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number SA4528NM This certificate issued to: Hartzell Propeller, Inc.
One Propeller Place Piqua, OH 45356-2634 Certifies that the change in the type design for the following product with the limitations and conditions therefor as speciful heronmple the air saliate garan ente Pro. 22% 1 the Civil Air Regulations. certification basis. for complete Original Product -TypeCertificate Number: 2A13 Make: Piper Model: PA-28R-180, PA-28R-200, PA-28R-201, PA-28RT-201 In Deniption of Types and Hartzell 835-47 (P) or 835-52(P) spinner, in accordance with either Desigaltangi HC-C3YR-1RF/F7282, constant speed propeller Robert A. Craner Installation Instructions No. 6, dated November 28, 1989 or Hartzell Instructions For Installation dated March 31, 1993, or later FAA approved revision.
Limitations and Conditions: 1. Compatibility of this design change with previously approved modifications must be determined by the installer.
2. Robert A. Craner Airplane Flight Manual Supplement No. 6, dated November 30, 1989, or Hartzell Airplane Flight Manual Supplement dated February 10, 1995, or later FAA approved revision is required with this installation. (See Continuation Sheet Page 3 For Additional Limitations.)
Date of Application: JUIY 5, 1988 Jule wissued: December 21, 1992 Date of Issuance: January 26, 1989 Jale umended: December 14, 1989, FEDERAL AVIATION By Direction of the Administrator 'ebryary 1 1995 pore 1. Plate Royace H. PrathéSignature) TAMINISTRAIO Manager, Propulsion Branch Chicago Aircraft Certification Office (Title)
47.
United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number SA4528NM Date Amended: February 10, 1995 Limitations and Conditions: (continued):
3. Propeller and Propeller Limits:
Hub Model: HC-C3YR-1RF Hartzell HC-C3YR-1RF/F7282 constant speed.
Blade Model: F7282 Diameter: 74" Maximum 73" Minumum Pitch Settings at 30' Station LOW : 9.2° ÷ 0.1° High: 30° ÷ 0.5° 4 . pressure between 1950 and 2350 RPM. Avoid continuous operation below 15 inches manifold Tachometer: Normal operating range (Green Arc) 500 to 2700 RPM.
Maximum continuous power (Red Radial) 2700 RPM.
Note 1. Noise Characteristics:
and was not considered an "acoustical change" as defined in This modification did not increase the noise level Regulations. Paragraph 21.93 (b), Amendment 21.63, of the Federal Aviation
- END - FAA FORM 8110-2-1 (10-69)
United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number SA4528NM This certificate issued to: Hartzell Propeller, Inc.
One Propeller Place Piqua, Ohio 45356 Purt 3* of the Civil Air *See Type Certificate Data Sheet No. 2A13 for complete certification Original Product -Type Certificate Number: 2A13 Make: Piper Model:
PA-28R-200 constant speed propeller in accordance with Robert A. Craner Installatio Description of Type Design Change: Installation of a Hartzell HC-C3YR-1RF/F7282 installation. November 30, 1989, or later FAA approved revision is required with this Robert A. Craner FAA Approved Airplane Flight Manual Supplement No. 6, dated Instructions No. 6, dated November 28, 1989, or later FAA approved revision and Limitations and Conditions:
Continued on Page 3 of this STC. and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of that airplane. incorporated, unless it is determined that the interrelationship between this change airplanes of these models on which other previously approved modifications are
Date of Application: July 5, 1988 Jute rissued: December 21, 1992 Date of Issuance: January 26, 1989 Sale unended: December 14, 1989 FEDERAL AVIATION By Direction of the Administrator TO MINISTRATO Acting Manager, Los Angeles Aircraft Certification Office 47
United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number SA4528NM Supplemental Type Certificate ADDENDUM Limitations and Conditions:
1. Propeller and Propeller Limits Hub Model: HC-C3YR-1RF Hartzell HC-C3YR-1RF/F7282 constant speed Blade Model: F7282 Diameter: 74" maximum 73" minimum Pitch Settings at 30" station High: 302+0.51-0.53°
2. Avoid continuous operation below 15 inches manifold pressure between 1950 and 2350 RPM.
3. Tachometer: Normal operating range (Green Arc) 500 to 2700 RPM, Maximum continuous power (Red Radial) 2700 RPM.
NOTE 1. Noise Characteristics: This modification did not increase the noise level 21.93 (b), Amendment 21.63, of the Federal Aviation Regulations. and was not considered an "acoustical change" as defined in Paragraph
- END- FAA FORM 8110-2-1 (10-69) PAGE OF 3 PAGES
SUPERSEDED Number: SA4528NM A REISSUANCE DATED. 12 AMENDMENT 2.9 This certificate issued to: Robert A. Craner Federal Aviation Administration
NORTHWEST MOUNTAIN REGION
LOS ANGELES AIRCRAFT CERTIFICATION OFFICE Part 3* of the Civil Air Regulations. *See Type Certificate Data Sheet No. 2A13 for complete certification basis.
Original Product - Type bertificate Number: 2A13 Make: Piper Model: PA-28R-200 Description of Type Design Change: Installation of a Hartzell HC-C3YR-1RF/F7282 constant speed propeller in accordance with Robert A. Craner Installation and Robert A. Craner FAA Approved Airplane Flight Manual Supplement No. 6, Instructions No. 6, dated November 28, 1989, or later FAA approved revision dated November 30, 1989, or later FAA approved revision is required with this installation.
Limitations and Conditions: This approval should not be extended to other specific airplanes of these models on which other previously approved modifications are incorporated, unless it is determined that the interrelationship between this change and any of those other previously of that airplane. approved modifications will introduce no adverse effect upon the airworthiness Continued on Page 3 of this STC.
Date of Application: JULY 5, 1988 Date Reissued:
Date of Issuance: January 26, 1989 Date Amended: December 14, 1989 FEDERAL AVIATION By Direction of the Administrator hedeucKO *MINISTRATIO Manager, Lo Whgeles Aircraft Certification Office (Title)
TRANSFER ENDORSEMENT Transfer the ownership of Supplemental Type Certificate Number _ SA4 5 2 8 NM to (Name of transferee) _ HARTZELL PROPELLER INC.
(Address of transferee) ONE PROPELLER PLACE (Number and street) PIQUA, OHIO 45356 (City, State, and ZIP code) from (Name of grantor) (Print or type). _ROBERT A. CRANER (Address of grantor) 2401 GONDAR AVENUE (Number and street) LONG BEACH, CA 90815 (City, State, and ZIP code) Extent of Authority (if licensing agreement):
Date of Transfer: 4/18/91 Dano 2 of 2 Damao
United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA4528NM Supplemental Type Certificate ADDENDUM Limitations and Conditions:
1. Propeller and Hartzell HC-C3YR-1RF/F7282 constant speed Propeller Limits Hub Model: HC-C3YR-1RF Blade Model: F7282 Diameter: 74" maximum 73" minimum Hien: 308 + 0:5/0 30tion LOW:
2. Avoid continuous operation below 15 inches manifold pressure between 1950 and 2350 RPM.
3. Tachometer: Normal operating range (Green Arc) 500 to 2700 RPM, Maximum continuous power (Red Radial) 2700 RPM.
NOTE 1. Noise Characteristics: This modification did not increase the noise level and was not considered an "acoustical change" as defined in Paragraph 21.93(b), Amendment 21-63, of the Federal Aviation Regulations.
-END-
FAA FORM 8110-2-1 (10-69) PAGE 3 OF 3 PAGES
United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SA4528NM This certificate issued to: Robert A. Craner Part 3* of the Civil Air Regulations. *See Type Certificate Data Sheet No. 2A13 for complete certification basis.
Original Product -Typebertificate Number: 2A13 Make: Piper Description of Type Design Change: Robert A. Craner FAA Approved Airplane Flight Mand RESSUANCE DATE Model: PA-28R-200, Serial Nos. 28R-35001 throug! • Installation of a Hartzel1 HC-C31R-1RF/F/202 -8R-7635516 Craner Installatior approved revision and January 25, 1989, or later FAA approved rey 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.
Continued on Page 3 of this STC.
Date of Application: JUIY 5, 1988 Date Reissued:
Date of Issuance: January 26, 1989 Date Amended:
FEDERAL AVIATION By Direction of the Administrator TAMINISTRATOE Manager, Los Angeles Aircraft Certification Office (Title)
FAA FORM 8110-2 (10-68) Dano 1 of 2 Damar
United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA4528NM Supplemental Type Certificate ADDENDUM Limitations and Conditions:
1. Propeller and Propeller Limits Hartze11 HC-C3YR-1RF/F7282 constant speed Hub Model: HC-C3YR-1RF Blade Model: F7282 Diameter: 74i maximum 73" minimum wen: 308 0135/038ton High: 30
2. Avoid continuous operation below 15 inches manifold pressure between 1950 and 2350 RPM.
3. Tachometer: Normal operating range (Green Arc) 500 to 2700 RPM, Maximum continuous power (Red Radial) 2700 RPM.
4. Noise Characteristics: This modification did not increase the noise level and was not considered on "acoustical change" as defined in paragraph
21.93(b) of the Federal Aviation Regulations.
-END- FAA FORM 8110-2-1 (10-69)
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