TCDS P-719

Page No. 1 2 3 4 Rev. No. 8 8 8 8 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION P-719 Revision 9 Hamilton Standard 23D September 15, 1975 TYPE CERTIFICATE DATA SHEET NO. P-719 Type Certificate Holder: Hamilton Standard Division of United Technologies Corporation Windsor Locks, Connecticut 06096 Propellers of models described herein conforming with this data sheet (which is part of type certificate no. 719) and other approved data on file with the Federal Aviation Administration meet the minimum standards for use in certificated aircraft in accordance with pertinent aircraft data sheets and applicable portions of the Civil Air Regulations/Federal Aviation Regulations provided they are installed, operated, and maintained as prescribed by the approved manufacturer's manuals and other approved instructions. Type Constant speed; hydraulic (See NOTES 3 and 4) Engine Shaft SAE No. 40, SAE No. 30, or X. (X indicates special shaft sizes for foreign engines are eligible.) Hub material Steel Blade material Aluminum alloy Number of blades Three Hubs eligible 23D40, 23D30, 23DX (See Note 1.) Blade Eligible Maximum Continuous Takeoff Diameter Limits Hub and Blade Weight (See Note 2) HP RPM HP RPM (See Note 2) (Max Diameter) NOTES 6181-0 to 6181-24 825 2100 908 2310 9 '6-5/16" - 7' 6-5/16" (-0 to -24) 250 lbs. 6 6182 is the left-hand version of 6181. 5 6183-0 to 6183-24 850 2100 1000 2310 10'5/16" - 8' -5/16" (-0 to -24) 261 lbs. 6 6184 is the left-hand version of 6183. 5 6185-0 to 6185-21 850 2100 1000 2310 10' 9-5/16" - 9' 5/16" (-0 to -24) 279 lbs. 6 6186 is the left-hand version of 6185. 5 6381-0 to 6381-24 825 2100 908 2310 9' 6-5/16" - 7' 6-5/16" (-0 to -24) 250 lbs. 6 6382 is the left-hand version of 6381. 6383-0 to 6383-24 850 2100 1000 2310 10' -5/16" - 8'-5/16" (-0 to -24) 261 lbs. 6 6384 is the left-hand version of 6383. 5 6385-0 to 6385-21 850 2100 1000 2310 10' 9-5/16" - 9'-5/16" (-0 to -21) 279 lbs. 6 6386 is the left-hand version of 6385. 5 P-719 Page 2 Blade Eligible Maximum Continuous Takeoff Diameter Limits Hub and Blade Weight (See Note 2) HP RPM HP RPM (See Note 2) (Max Diameter) NOTES 6459-0 to 6459-24 850 1800 1000 1980 11' 6-5/16" - 9' 6-5/16" (-0 to -24) 301 lbs. 6 6460 is the left-hand version of 6459. 5 6505-0 to 6505-24 850 1800 1000 1980 11' 6-5/16" - 9' 6-5/16" (-0 to -24) 301 lbs. 6 6506 is the left-hand version of 6505. 5 6511-0 to 6511-24 850 1800 1000 1980 11' 6-5/16" - 9' 6-5/16" (-0 to -24) 301 lbs. 6 6512 is the left-hand version of 6511. 5 6529-0 to 6529-24 850 1800 1000 1980 11' 6-5/16" - 9' 6-5/16" (-0 to -24) 301 lbs. 6 6530 is the left-hand version of 6529. 5 6531-0 to 6531-24 825 2100 908 2310 9'6-5/16" - 7'6-5/16" (-0 to -24) 250 lbs. 6 6532 is the left-hand version of 6531. 5 6533-0 to 6533-24 850 2200 1000 2310 10' 5-1/16" - 8' 5/16" (-0 to -24) 261 lbs. 6 6534 is the left-hand version of 6533. 5 6535-0 to 6535-21 850 2100 1000 2310 10- 9-5/16" - 9' 5/16" (-0 to -21) 279 lbs. 6 6536 is the left-hand version of 6535. 5 6601-0 to 6601-26 6601-30S 550 700 1470 1350 600 800 1500 1465 11'6-5/16" (-0) to 9'4-5/16" (-26) 9' 5/16" (-30S) 327 lbs. 6 6602 is the left-hand version of 6601. 5 7005-0 to 7005-26 7005-30S 550 700 1470 1350 600 800 1500 1465 11'6-5/16" (-0) to 9'4-5/16" (-26) 9'5/16" (-30S) 327 lbs. 6 7006 is the left-hand version of 7005. 5 7035-0 to 7035-24 850 1800 1000 1980 11' 6-5/16" - 9' 6-5/16" (-0 to -24) 301 lbs. 6 7036 is the left-hand version of 7035. 5 Certification basis Type Certificate No. 719, issued July 8, 1939. Production basis Production Certificate No. 14 NOTE 1. Hub Model Designation 2 3 D 40 - 101 Minor change not affecting eligibility SAE propeller shaft size Blade shank size Number of blades Major model type Page 3 P-719 NOTE 2. Blade Model Designation A - 6181 C - 18 T (If used) indicates telescoped; "S", square cutoff Nominal reduction from basic diameter in inches Operational features (may indicate particular deicing assembly), does not affect eligibility Aerodynamic and structural features (If used) indicates shank fairing design The blade model designation suffixed with "T" indicates a diameter reduction by telescoping. Blade models with square cutoffs in accordance with Hamilton Standard blade drawings are suffixed with "S." Telescoped blades and blades with a square cut-off are eligible at the same ratings and diameter limits as blades with standard cut-off. Diameter limits shown are nominal diameters of the assembled propeller and do not include the ± 1/ 8" manufacturing tolerance permissible for propellers with basic diameter less than 14 feet or ± 1/ 4" permissible for propellers with basic diameter 14 feet or larger. NOTE 3. Pitch Control. Eligible with Hamilton Standard constant speed governor only. NOTE 4. Feathering. Eligible with full feathering control installed in accordance with the propeller manufacturer's instructions. NOTE 5. Left-hand Models. The left hand version of an approved model propeller is eligible at the same rating and diameter limitations as listed for the right hand model. NOTE 6. Interchangeable Blades. Blades with an "S" or "T" suffix (see NOTE 2) are not interchangeable aerodynamically or vibrationwise with each other or with blades having normal round cutoffs. Only blades listed in the same group of the following groups are aerodynamically similar. Only blades listed under the same type in any one group are structurally similar. A higher type number implies a higher strength. This is due to differences in alloys and in cold working of the blade surface. Type 1 includes standard alloy nonsurface treated blades: Type 2, hard alloy nonsurface treated blades; Type 3, hard alloy blades with cold worked shanks; Type 4, hard alloy blades with cold worked shanks and shot peened surfaces. The following defines the degree to which these blades may be used interchangeably in the same diameter without a flight performance test and without a vibration survey: Type 2 blades may replace Type 1 blades in the same group, but not vice-versa. Type 3 blades may replace either Type 1 or Type 2 blades in the same group, but not vice-versa. Type 4 blades may replace either Type 1, Type 2, or Type 3 blades in the same group, but not vice-versa. Reference should always be made to the ratings of the blades, and blades with different model numbers cannot be incorporated in the same propeller unless the aircraft certification specifically permits this. Type 1 Type 2 Type 3 Group (a) 6181, 6381, 6531 Group (b) 6183, 6383, 6533 Group (c) 6185, 6385, 6535 Group (d) 6511, 6529 6459, 6505 7035 Group (e) 6601 7005 P-719 Page 4 NOTE 7. Accessories. (a) Propeller Deicing. Eligible with Hamilton Standard deicing slinger ring assemblies. (b) Propeller Spinner. Eligible with spinner supplied by Hamilton Standard. NOTE 8. Shank Fairings. Not applicable. NOTE 9. Special Limits. Not applicable. NOTE 10. Special Notes. The word "eligible" as used herein does not signify approval. For approval compliance with the applicable aircraft airworthiness requirements is necessary. ....END....