# TCDS LTC-5: R. M. Lewis - Type: Type certificate data sheet - Status: Current - Holder: R. M. Lewis - Revision: 2 - Revised: February 19, 1947 - Product: Aircraft, Large Airplane - Certification basis: CAR 9 - Data sheet PDF: https://openairdocs.org/files/sha256/cf/57/cf5727deab62cc26c066d8b52b2866a970da13687079c7088ba867970f38b00a - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/CF002311BE21F60C852567370051EB65.0001 - Page: https://openairdocs.org/tcds/LTC-5 ## Models (5) As the data sheet lists them. - PB2Y-5 (Navy) - PB2Y-5Z (Navy) - PB2Y-3 (Navy) - PB2Y-5R (Navy) - PB2Y-3R (Navy) ## What the data sheet says This is OCR from the scanned FAA data sheet. OCR can misread letters and numbers. ```text MODELS: General (C2/1olidated-vultee) (Mavy) PB21-3, -38, -5, -59, -5Z SPEC. NUMBER: L-5-2 (Eligible for Certification in Limited Category only.) (Holder of Limited Type Certificate, Robert H. Lewis, San Prancisco, CA) Engines 4 Pratt & Whitney R-1830-88, -92, -94 or -82 with decoupled nose Fuel 100 minimum octane (-94 engines) 90 minimum octane (-92 and -82 engines) AH Grade 125 (-88 engines) Engine limits except take-off (low blower) (10,000 ft.) 42.2 in. Hg.. 2600 pm (1000 hp 41.5 in. Hg.. 2600 Ipm (1000 hp) 2800 pm (1350 hp) R-1830-92 and -82: except take-off (low blower only) (7500 ft.) 39.5 in. Hg., 2550 rpm (1050 hp) 48.0 in. Hg.. 700 pm (1200 hp) or except take-off (neutral auxiliary) Maximum. ft.) (50 850e taken to Bore B2oree)100 hg)) 45.0 in. Hg., 2550 rpm (1035 hp) 45.0 in. Hg.. 2550 Ipm (1050 hp) except take-off (high blower) 44.0 in. Hg.. 44.0 in. Hg., 2550 rpm (1000 hp) Propellers Curtiss C5423-A38 hubs; 714 blades. Curtiss C5325D-A2 or Came 121-4 hubs: Airspeed limits Glide or dive - 247 mph (See NOTE 2) Maximum weight C.G. range In flight 24 percent MAC to 30 percent MAC Landing 26.5 percent MAC to 30 percent MAC Datum 267.5 inches forward of center line of main gear MAC 194.3 inches LE MAC 290.56 inches Other Operating avy Technica. Order 28-44 dated 3/3/4t Certification basis ‚imited Type Certificate No. 5 (CAR ° effective Export eligibility Production basis None may be produced under this approval Not eligible for a Certificate of Airworthiness for Export No equipment other than engines and propellers are specified. such equipment as required by Civil Air Regulations Part 43.30 for the any additional equipment necessary for the proper operation of the aircraft. particular operation authorized for NC aircraft must be installed. In addition, the aircraft may incorporate such military equipment (except armament) as was originally incorporated in the type for military or naval Additional equipment may be installed as can be substantiated on the basis that it presents no obvious hazard to safety. Weight and Balance Report including list of equipment included n the certificated empty weight must be submitted for each aircraf Army or Navy weight records in current ondition may be submitted i an actual weight. The equipment list need include no more than Required equipment as defined under "EQUIPMENT" above. Additional items as may be reasonably considered removable and are so located or of such weight that their removal or addition could noticeably affect the weight and balance of the aircraft. Items built into the aircraft structure need not be listed. of can be itate eresentation imitations. et theecertist must be prepared by the applicant for the approval The following placards must be prominently displayed in the positions In full view of all passengers: This is a military type aircraft d under the Civil Air Regulations shall not be used for th irriage of passengers or cargo for compensation or hire. placard and lettering shall be of a type which can be read easily In the cockpit in full view of the pilot: "Maximum take-off weight from rough water - 54,000 1bs.i "Do not lower flaps above 125 mph." "Do not exceed 161 mph in rough air." #Avoid operation of inboard propellers between 2350 - 2525 "Avoid operation of outboard propellers between 2275 - 2525 rpm." The following statement must appear on the Operation Limitations, ¿This airplane must be operated at all times within the limitations set forth in Navy Technical Order 28-44 except for limitations specifically called out in Aircraft Specification AL-S in which the values given in the specification must be observed. A copy of the pertinent Navy Technical Orders and Aircrait Specification AL-5 must be carried durino In all cases it will be the responsibility of the applicant to secure a copy of the correct Technical The CAA does not have these documents available for distribution. NOT 4 NI Certification,, If any repairs or modifications are nade prior to or subsequent it is the responsibility of the owner to furnish sufficient evidence to a Civil Aeronautics Administration representative to show that the modified airplane maintains the same dedree of airworthi- The C.A.A. can give no technical assistance on such matters since complete structural data for VL aircraft are not required by Part ? and therefore are not available in the C.A.A. prior to obtaining certificatior for night operation, the following modifications to the exterior lighting must be made in order to comply with the general requirements of the Civil Ais Regulations. Position Lights I1p - The AN-3033-9 Or AN-3033-1 through -4 or the AN-3032-1 through -4 light assemblies are satisfactory without modification. Tail - If Type D-1 (AN-3091-1 through -3) or the Type D-2 (AN-3092-1 through -3) light assembly is irstalled on the tail cone it must be replaced with a type certificated unit. Position Light Installation. Position lights shall be installed to comply with the requirements of the CAP, Parts 15.2 and 3.539. Position Light Circuit and Control. Position lights (wing tips and tail) shall be controlled by one SeST switch. Circuit should be protected by its own fuse or circuit breaker. tip and tail light switches with din and bright positions shall be removed and the dinming resistors shall be disconnected. With the exception of landing and anchor ny other exterior lights are not required and may b obtained from CAA Aircraft ``` ## ADs None name its models. ## Registered aircraft by registry model (OpenAirDocs) - [Consolidated PB2Y-3](https://openairdocs.org/model/consolidated-pb2y-3): 0 aircraft (registry code 2421002) - [Consolidated PB2Y-3R](https://openairdocs.org/model/consolidated-pb2y-3r): 0 aircraft (registry code 2421004) - [Consolidated PB2Y-5](https://openairdocs.org/model/consolidated-pb2y-5): 0 aircraft (registry code 2421006) - [Consolidated PB2Y-5R](https://openairdocs.org/model/consolidated-pb2y-5r): 0 aircraft (registry code 2421008) - [Consolidated PB2Y-5Z](https://openairdocs.org/model/consolidated-pb2y-5z): 0 aircraft (registry code 2421010) ## STCs approved under this data sheet (3) - [STC SA01967WI](https://openairdocs.org/stc/SA01967WI): Use of GAMI G100UL High Octane Unleaded Avgas. General Aviation Modifications Inc. - [STC SA02268CH](https://openairdocs.org/stc/SA02268CH): Installation of Airwolf Filter Corp. Air Oil Separator. Airwolf Filter Corporation - [STC SA01282NY](https://openairdocs.org/stc/SA01282NY): Installation of Airwolf remote mounted engine oil filter kit AFC-K015 on aircraft powered by Pratt & Whitney radial reciprocating engine Series R-985, R-1340 and R-1830.. Airwolf Filter Corporation --- 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.