# TCDS A24NM: Aero Union Corporation - Type: Type certificate data sheet - Status: Current - Holder: Aero Union Corporation - Revision: 1 - Revised: September 25, 1987 - Product: Aircraft, Large Airplane - Certification basis: Part 21, Part 43, Part 91, CAR 4b - Data sheet PDF: https://openairdocs.org/files/sha256/54/e0/54e0e0c2ac088c2819ba105a7fcccebac8de3af0f05844fd87a1995affd07612 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/A26F4CDC8EC0F3D886256E0D005E5EAD.0001 - Page: https://openairdocs.org/tcds/A24NM ## Models (1) As the data sheet lists them. - SP-2H (P2V-7) ## What the data sheet says From the PDF's text layer, line by line; tables lose their columns. The PDF is the record. ```text DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION A24NM Revision 1 Aero Union Corporation U.S. Navy SP-2H (P2V-7) September 25, 1987 TYPE CERTIFICATE DATA SHEET NO. A24NM This data sheet, which is a part of Type Certificate A24NM prescribes conditions and limitations under which the product for which the type certificate was issued meets the airworthiness requirements of the Federal Aviation Regulations. Type Certificate Holder Aero Union Corporation 100 Lockheed Avenue Chico, California 95926 I. Model SP-2H (P2V-7) (Restricted Category) approved September 25, 1987 Engines (a) 2 Curtiss-Wright R3350-32WA Reduction gear ratio 16:7 (2 Jet Engines Removed) Fuel MIL-G-5572 Grade 100/130 Engine Limits* (a) R-3350-32WA (Fuel Grade 100/130 Low Blower) BHP RPM M.P. in HG ALT (FT) Takeoff (5 minutes wet) 3696 2900 59.0 Sea Level Takeoff (5 minutes wet) 3716 2900 59.0 2000 Takeoff (5 minutes dry) 2900 2900 54.0 Sea Level Takeoff (5 minutes dry) 2900 2900 53.0 2000 Max. Continuous 2600 2600 48.5 Sea Level Max Continuous 2655 2600 47.5 4000 *Reverse pitch operation are restricted to a maximum of 2600 rpm. See Aero Union Corporation Operating Manual, P2V Operation, for Engine Operating Limits Tables. Airspeed Limits VNE (Never exceed) 270 KIAS V FE (Flaps extended 5°) 210 KIAS V FE (Flaps extended 10°) 210 KIAS V FE (Flaps extended 15°) 200 KIAS V FE (Flaps extended 20°) 175 KIAS V FE (Flaps extended 25°) 155 KIAS V FE (Flaps extended 32°) 145 KIAS V LE (Max. gear extend) 155 KIAS V A (Max maneuvering) 160 KIAS V MC (Min. Control) 97 KIAS Page No. 1 2 3 4 Rev. No. - - - 1 Page 2 of 4 A24NM Propeller and Propeller Limits Hubs - 2 Hamilton Standard 24260-313 or 24260-337 or 24260-223 Blades - 4 2J17H3-36S or 2J17Z3-36S or 2FJ17C3-36S Diameters limits 14 ft. 2 in. - No cutoff permitted Continuous ground operation between 2000 and 2400 is prohibited. Pitch setting at 72-inch station: Low Pitch 14° (± 0.5°) Feathered +82° (± 0.5°) Reverse -22° (± 0.5°) Interchangeable Blades - These blades can be used interchangeably in the same propeller provided they are used in pairs and installed in opposite arms and that the prefix letters for opposite blades and the cut-off dash numbers for all blades are the same. Fire Retardant Dumping Envelope (See NOTE 2) 120 KIAS to 145 KIAS Flap extended 10° Min. C.G. Range Aft of datum, landing gear extended, MAC (Sta.): 19.4% (354.58) to 36% (375.53) @ 46,000 lbs 19.4% (354.58) to 36% (375.53) @ 61,400 lbs 21.56% (357.31) to 36% (375.53) @ 67,500 lbs. Straight line variation between points given. Empty Weight C.G. Range None Datum The reference datum is located at fuselage station 0. Mean Aerodynamic Chord (MAC) The leading edge of the MAC is located at fuselage station 330.1. The length of the MAC is 126.2 inches. Leveling Means Level the aircraft by dropping a plumb bob from the leveling hook through the leveling grid in the nose wheel well. Maximum Weight Takeoff 67,500 lbs Landing 67,500 lbs Zero fuel, oil, and ADI 59,100 lbs Crew & Number of Seats Pilot and co-pilot 2 at 158”, occupancy limited to persons essential to perform the special purpose operation. Fire Retardant 2000 gallons (U.S.) 18,000 lbs at +394.6”. Fuel Capacity Total Fuel Per Tank No. Tanks U.S. Gal Lbs. Lbs. ARM . 2 715 1430 8580 +376.5” Wing (main) All other fuel tanks permanently removed Oil Capacity Total Fuel Per Tank No. Tanks U.S. Gal Lbs. Lbs. ARM . Nacelle Tank 2 60 120 852 +382.7” (expansion space) 20 - - Water Injection Tank Capacity Total ADI Per Tank No. Tanks U.S. Gal Lbs. Lbs. ARM Nacelle Tank 2 25 50 375 +316” Fluid – AMS – 3006 Type I which specifies 48 – 52% methyl alcohol by volume and 45 – 52% water by volume Page 3 of 4 A24NM Control Surface Movements Aileron Up 22° ± -1° Down 15° 30’ ± 1° Aileron Tab Up 15°45’ ± -2° Down 16° 20’ ± -2° Elevator Up 27°37’ ± -1°30’ Down 27 ° ± -1°30’ Elevator Trim Panel Up 7° + 1/4° -0° Down 3 ° + 1/4 -0° Spoiler Up 55° - 60° Rudder Trim Tab Left 10° Right 10°30’ Rudder Left 21° Right 21° Aileron Spring Tab: Adjust spring tab in accordance with NAVWEPS 01-76EEB-2-3 figure 3-16. Serial Numbers Eligible U.S. Navy Bureau Numbers: 135596 140963 145903 145917 145920 147959 147964 147967 147968 148339 148343 150281 150283 Production Basis None. Prior to original airworthiness certification of each aircraft, FAA personnel must perform an airworthiness inspection determining condition for safe operation and determine the applicant has conducted a satisfactory flight test. See NOTE 5 for data on Service Bulletins and ADs. Certification Basis 14 CFR part 21 § 21.25 (a) (2) and (b). Type Certificate issued September 25, 1987 for the special purpose of forest and wildlife conservation (firefighting). Date of application May 20, 1986. The modifications incorporated are considered appropriate to the special purpose operation, forest and wildlife conservation (firefighting). The criteria established in Civil Air Regulations Part 4B appropriate to the special purpose operation has been used to evaluate these particular changes and demonstrate that the original level of airworthiness established by the military requirements has not been reduced. A Finding of No Significant Impact (FONSI) for the modified Lockheed (Navy) Model SP-2H (P2V-7) Aircraft has been accomplished and approved on September 23, 1987. A finding under the applicable provisions of the Noise Control Act of 1972 has been accomplished and approved on September 23, 1987, for the modified Lockheed SP-2H (P2V-7) Aircraft (Restricted Category-Military Surplus). Equipment The basic required equipment, as prescribed in the applicable airworthiness regulations (see Certification Basis) must be installed in the aircraft for certification. Equipment necessary for the particular special purpose operation must be installed. In addition, an FAA approved Airplane Flight Manual Supplement is required. (See NOTES 2 & 4) NOTE 1 Current weight and balance report including list of equipment included in certificated empty weight, and loading instructions when necessary must be provided for in each aircraft at the time of original airworthiness certification. NOTE 2 The aircraft shall be operated in accordance with NATOPS Flight Manual Navy Model SP-2H Aircraft NAVAIR 01-75EEB-1 (procedures and limitations) and Flight Handbook Navy Model P2V-6 Aircraft AN-01-75EEA-1 (performance) except wherein superseded by Aero Union Corporation FAA Approved Airplane Flight Manual Supplement dated September 22, 1987 original issue or later approved revision. Page 4 of 4 A24NM NOTE 3 Prior to civil certification compliance with the following Department of the Navy Service Bulletins Aircraft and Aircraft Service Changes must be accomplished: SP-2H (P2V-7) Airframe and Interim Airframe Bulletins - - Nos. 1, 4, 5, 6, 8, 9, 10, 12, 13, 14, 17, 18, 19, 20 Rev. B, 21 and Amend 1, 22, 23, 24, 25, 26 and Amend 1, 27 Rev. A., 31 and Amend 1, 63, 65, 67, 69 and Amend 1, 72, 74, 75, 78, 81, 82, 83 Amend 1, 86, 88, 90, 91, 92, 93, 94, 95 and Amend 1, 98, 100, 101, 102, 103, 104, 105, 107, 108, 110, 114 Rev. A, 115, 116 and Amend 1, 117, 118, 119. P2V-7 Aircraft Service Changes - - 605, 676, 681, 688, 694, 697, 699, 709, 714, 721, 722, 724, 733, 735, 737, 751, 752, 753A, 758A, 765A, 768, 770, 781, 783, 787A, 793, 795, 798, 802, 803A, 806A, 807, 812, 815, 816, 817, 819, 822, 826, 831B, 839C, 843, 845A, 848A, 851, 856, 861A, 862, 864, 878, 894 Amend 1, 896 Amend 1, 898, 900, 903, 912, 923, 924 Amend 1, 928, 929, 931 Amend 1, 934, 935, 937, 940, 948, 952, 953 Amend 1, 955A, 979, 980, 981, 987, 991. Wright R3350-32WA engine Bulletins - - 469 Rev A Amend 2, 474 Rev A, 494 Rev B, 490 Rev A, 516, 517, 518, 519 Amend 1, 520 Amend 1, 562 Rev A, 564 Rev. B Amend 2, 566 Rev B, 625 Rev A Amend 1, 635 Rev C, 646 Rev A, 656 Rev A, 663, 681, 682 Rev A, 687, 693, 694 Amend 1, 698, 707, 708, 709, 711Amend 1, 713 Rev A, 714 Rev B, 716 Amend 1, 720, 721 Rev B Amend 1, 722, 726 Amend 1, 727, 731, 732, 735, 736, 737, 742 Amend 2, 750, 751 Rev A, 752. NOTE 4 Modification to these aircraft and installation of special equipment will be necessary (reference § 21.25(a)(2)) or (b)(2), prior to civil airworthiness certification to the special purpose of forest and wildlife conservation (firefighting) and for any other FAA approved special purpose operation in accordance with Aero Union Master Drawing List 10801, Rev. H, dated September 8, 1987. NOTE 5 Restricted Aircraft Airworthiness Certificates issued are effective under § 21.181(a) (1) as long as maintenance and preventive maintenance are performed in accordance with part 43 and part 91, Subpart E. ....END..... ``` ## ADs None name its models. ## STCs approved under this data sheet (4) - [STC SA563CH](https://openairdocs.org/stc/SA563CH): Authorizes installation of engines equipped w/Unison Limited Authority Spark Advance Regulator (LASAR) ignition system w/Cylinder Head Temp. (CHT) monitoring capability on airframes. engines.. Champion Aerospace LLC - [STC SA3345WE](https://openairdocs.org/stc/SA3345WE): Recognition light installation on horizontal stabilizer.. DeVore Aviation Corporation of America, a New Mexico Corporation - [STC SA3112WE](https://openairdocs.org/stc/SA3112WE): Installation of flap slot closures.. Thermal Aircraft Company - [STC SA2790WE](https://openairdocs.org/stc/SA2790WE): Installation of angle of attack indicator.. Thompson Aircraft Company --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.