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Thiara TT Group

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Caleb Torres
Caleb Torres

Jr (12) 'LINK'



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jr (12)



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Regression methods were used to select and score 12 items from the Medical Outcomes Study 36-Item Short-Form Health Survey (SF-36) to reproduce the Physical Component Summary and Mental Component Summary scales in the general US population (n=2,333). The resulting 12-item short-form (SF-12) achieved multiple R squares of 0.911 and 0.918 in predictions of the SF-36 Physical Component Summary and SF-36 Mental Component Summary scores, respectively. Scoring algorithms from the general population used to score 12-item versions of the two components (Physical Components Summary and Mental Component Summary) achieved R squares of 0.905 with the SF-36 Physical Component Summary and 0.938 with SF-36 Mental Component Summary when cross-validated in the Medical Outcomes Study. Test-retest (2-week)correlations of 0.89 and 0.76 were observed for the 12-item Physical Component Summary and the 12-item Mental Component Summary, respectively, in the general US population (n=232). Twenty cross-sectional and longitudinal tests of empirical validity previously published for the 36-item short-form scales and summary measures were replicated for the 12-item Physical Component Summary and the 12-item Mental Component Summary, including comparisons between patient groups known to differ or to change in terms of the presence and seriousness of physical and mental conditions, acute symptoms, age and aging, self-reported 1-year changes in health, and recovery for depression. In 14 validity tests involving physical criteria, relative validity estimates for the 12-item Physical Component Summary ranged from 0.43 to 0.93 (median=0.67) in comparison with the best 36-item short-form scale. Relative validity estimates for the 12-item Mental Component Summary in 6 tests involving mental criteria ranged from 0.60 to 107 (median=0.97) in relation to the best 36-item short-form scale. Average scores for the 2 summary measures, and those for most scales in the 8-scale profile based on the 12-item short-form, closely mirrored those for the 36-item short-form, although standard errors were nearly always larger for the 12-item short-form.


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The Lockheed Model 12 Electra Junior, more commonly known as the Lockheed 12 or L-12, is an eight-seat, six-passenger all-metal twin-engine transport aircraft of the late 1930s designed for use by small airlines, companies, and wealthy private individuals. A smaller version of the Lockheed Model 10 Electra, the Lockheed 12 was not popular as an airliner but was widely used as a corporate and government transport. Several were also used for testing new aviation technologies.


After Lockheed had introduced its 10-passenger Model 10 Electra, the company decided to develop a smaller version which would be better suited as a "feeder airliner" or a corporate executive transport.[1] At the same time, the U.S. Bureau of Air Commerce had also sensed the need for a small feeder airliner and announced a design competition for one. In order for a candidate to qualify for the competition, a prototype had to fly by June 30, 1936.[2][3]


Lockheed based its candidate, which it named the Model 12 Electra Junior, around a scaled down Electra. It would carry only six passengers and two pilots but would use the same 450 hp (340 kW) Pratt & Whitney R-985 Wasp Junior SB radial engines as the main Electra version, the 10A.[2] This made it faster than the Electra, with a top speed of 225 mph (362 km/h) at 5,000 ft (1,500 m).[2][4] Like the Electra, the Model 12 had an all-metal structure, trailing-edge wing flaps,[4] low-drag NACA engine cowlings, and two-bladed controllable-pitch propellers (later changed to constant-speed propellers).[3] It also had the Electra's twin tail fins and rudders, which were becoming a Lockheed trademark. The landing gear was a conventional tail-dragger arrangement, with the main wheels retracting backwards into the engine nacelles; as was often the case with retractable gear of the period, the wheel bottoms were left exposed in case a wheels-up emergency landing was necessary, or the pilot simply forgot to deploy his novel landing gear.[4]


As in the Electra and the Boeing 247, the Model 12's main wing spar passed through the passenger cabin; small steps were placed on either side of the spar to ease passenger movement.[4] The cabin had a lavatory in the rear.[4] Although the standard cabin layout was for six passengers, Lockheed also offered roomier, more luxurious layouts for corporate or private owners.[2][4]


The new transport had its first flight on June 27, 1936,[2][3] three days before the competition deadline, at 12:12 PM local time, a time deliberately chosen for the Model 12's number.[2] As it turned out, the other two competition entries, the Beechcraft Model 18 and the Barkley-Grow T8P-1, weren't ready in time for the deadline, so Lockheed won by default. The "Electra Junior" name did not catch on in the way that the original Electra's name had. Most users simply referred to the aircraft by its model number, as the Lockheed 12.[3]


The original Lockheed 12 version, with Wasp Junior engines, was the Model 12A.[4] Almost every Lockheed 12 built was a 12A or derived from the 12A. There was also a Model 12B, using 440 hp (330 kW) Wright R-975-E3 Whirlwind radials, but only two of this model were built.[3] Although Lockheed had also announced a Model 12F, powered by Wright R-760 Whirlwind seven-cylinder radials, and a Model 12M, powered by 290 hp (220 kW) Menasco six-cylinder inline engines,[5] neither of these versions reached production.


Even though the Lockheed 12 had won the government's feeder airliner competition, most of the airlines rejected it, and very few Lockheed 12s were used as airliners.[3][6] One notable airline user was the newly renamed Continental Air Lines, which had a fleet of three Lockheed 12s that ran on its route between Denver, Colorado and El Paso, Texas in the late 1930s.[7][8][9] Another was British West Indian Airways Ltd., which flew the Lockheed 12 on Caribbean routes in the Lesser Antilles during the mid-1940s.[10][11][12]


The Lockheed 12 proved much more popular as a transport for company executives or government officials.[3] Oil and steel companies were among the major users.[3] A number were purchased as military staff transports by the United States Army Air Corps, which designated the type as the C-40, and by the United States Navy, which used the designation JO, or in one peculiar case, R3O-2. With the arrival of World War II, many civilian Lockheed 12s were requisitioned by the U.S. Army and Navy, Britain's Royal Air Force, and the Royal Canadian Air Force.[13]


Two civil Lockheed 12s ordered by British Airways Ltd. were actually intended for covert military reconnaissance flights.[6] Sidney Cotton modified these aircraft for aerial photography and in civilian guise, overflew and surreptitiously photographed many German and Italian military installations during the months preceding World War II.[14][15]


The main military user of the Lockheed 12 was the Royal Netherlands East Indies Army Air Force, which bought 36.[6] Sixteen of these were the Model 212, a version created by Lockheed for training bomber crews, which had a .303 in (7.696 mm) caliber machine gun in an unpowered, partly retractable gun turret on top of the fuselage, a second .303-caliber machine gun fixed in the nose, and bomb racks under the wing center section that could hold eight 100 lb (45 kg) bombs.[1] The other 20 aircraft were transport versions.[3]


Several Lockheed 12s were used as technology testbeds. The U.S. National Advisory Committee for Aeronautics (NACA) bought two, adding a center vertical fin to each of them to test stability improvements. One of the NACA Lockheed 12s was used to test "hot-wing" deicing technology, in which hot exhaust air from the engines was ducted through the wing's leading edge to prevent ice accumulation.[16][17]


Three other Lockheed 12s were used to test tricycle landing gear.[18] These had their normal landing gear replaced by a non-retracting version with a large nosewheel and with the main wheels shifted further back on the engine nacelles.[18] (The tailwheel from the normal conventional gear was retained.[18]) The gear was non-retractable because there wasn't room within the structure to stow it in retracted position.[13] Streamlined fairings were placed on the gear to reduce drag. One of the tricycle gear Lockheed 12s went to the U.S. Navy as the XJO-3 and performed carrier landing tests on the USS Lexington to study the suitability of a twin-engined tricycle-gear aircraft for carrier operations.[17][18] Another went to the U.S. Army as the C-40B, and still another was retained by Lockheed for its own testing; both of these were eventually converted back to the normal landing gear configuration.[17][18]


Milo Burcham flew a Lockheed 12A in the 1937 Bendix Trophy Race from Burbank, California to Cleveland, Ohio. This 12A had extra fuel tanks in the cabin, allowing it to save time by making the entire 2,043 mi (3,288 km) trip non-stop.[17] The 12A came in fifth at an average speed of 184 mph (296 km/h); this was an impressive performance, since the first and fourth-place winners were both privately owned Seversky P-35 fighters.[17] 041b061a72


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