cessna 177 problems

Deadlines were met. Horsepower: 1 x 150 HP. Gross weight had, of necessity, grown 100 pounds, and cruise speed increases were a modest two to three mph, although ongoing refinements over the next 15 years would eventually net an additional 20-30 mph. higher than the 172. Get Insurance Operating Costs Apply for Financing 1972 CESSNA 177RG That having been (hopefully) explained may help you understand some of the problems created by the inevitable compromises that surround the introduction of a totally new airplane like the Cardinal. As it became obvious that the 177 was catering to an upscale market, engineers borrowed the technology from the 210. Even though Cessna had spent millions in development, the 1967 models were priced virtually the same as the year before. The hallmark wing struts went away, and the plane was fitted with full cantilever (no struts) wings. I also think there's a problem with corrosion in the carry-thru structure above the cabin, which can render the airplane totally unairworthy and uneconomical to repair. ft. was added to the horizontal tail (a fully articulated tail had been considered, but was abandoned after testing). At the same time, it appeared that higher cruising speeds could be achieved by eliminating the wing struts then in use on all Cessna singles. The original fuel system was an unusual (for Cessna) design that had only On and Off settings. © Copyright 2020 - Tennessee Aircraft Services, Inc.. I also received an email from the FAA with more details, including a picture of the damaged spar. Overall, the Cardinal is an excellent airplane for the pilot ready to step up to a serious cross country machine. Next, the wing was moved 4½ inches aft for better visibility, but that created a nose-heavy condition and stability problems, the solution of which was a higher-dihedral wing. The FAA recently issued a pair of Airworthiness Concern Sheets, one directed at an issue found with float-equipped Cessna 180 and 185 models, and the other regarding a concern with Cessna 172, 175, 182, 205, 206, 207, and 210 models with strut-braced wings. This occasionally caused problems, since its possible for one tank to empty more quickly than the other. That crash was described in an “Airworthiness Concern Sheet” issued by the FAA. Learn more, Cessna Flyer Association1042 N Mountain Ave Suite B #337Upland, CA 91786Phone: 626-844-0125. A quick search of the FAA list of defect reports doesn’t show any reports of Cardinal wing problems, of any kind. Dealers still trusted the 172I, however. Flaps-retracted stall speed was six knots higher than on the 172H at the same weight. Most Cessna mechanics are 172 experts and expect things to be different on a Mooney or Piper, but when this thing that's almost a 172 is a little different then it can be a surprise. We’d recommend the area be thoroughly cleaned and visually inspected at least at every annual. Textron published SEL-57-06 and SEL-57-07 on June 26, 2019, to address the possible failure of the carry through spar that’s mounted in the overhead area of the cabin on cantilever wing Cessna 210 and 177 series aircraft. I have an issue with the Cessna retraction system. SAIB Issued For Cessna 177, 177A, 177B, 177RG, And F177RG Airplanes. Email: EmailemailProtector.addCloakedMailto("ep_84d82768", 1); Cessna Flyer Association © 2004-2020 All Rights Reserved. The surprise in the bulletin was found in the first sentence stating reports had been received of cracks found in spar caps. As the prototypes flew nearly every day, keeping them a secret became an obsession. Lycoming had a perfect candidate. A few emails to other Cardinal experts and those in the know didn’t turn up any previous knowledge of known spar cap cracks in a 177 series plane. If the information about crack growth learned from research on the 210 spar cap is applicable to the 177, then frequent visual inspections should locate any safety concerns well before ultimate failure is reached. Eventually, empty weight came down to an average of 1,350 pounds, about 75 pounds. Delete cookies, By using our website, you agree to our use of cookies. However Cessna’s marketing department insisted on keeping the 172 in production, so the 177 designator was born. The surprise in the bulletin was found in the first sentence stating reports had been received of cracks found in spar caps. In the ten years since they had introduced the 172 Skyhawk, about 9,000 of the four-place singles had been built—it was already the world’s most popular airplane. Wind tunnel and flight testing showed that they had over-engineered it, and trim and anti-servo forces were excessive. Why new designs are as rare as a tailwind. Development. Then with an inspired expression, he presented Plan B. Interior aluminum looks like the day it was made. You won't find a cleaner airframe anywhere. The 177 Cardinal seats up to 3 passengers plus 1 pilot. Cessna was so confident that it ordered 2,000 four-cylinder, 150 hp O-320s before the 172J flight testing was finished, and they took an option on 2,000 more: there was much joy in Williamsport. Piper had been using the stabilator for quite a few years and knew its idiosyncrasies, but it was new to Cessna. The 177 Cardinal was developed to replace the 172 Skyhawk. How many 172s did we sell last year—sixteen hundred? It, then, came as no surprise that Cessna would publish a bulletin relating to wing spar cracks found in the Cardinals very similar to those found on the 210. The Cessna 177 'Cardinal II' is another great general aviation aircraft from the Cessna and Alabeo stables. The 1968 Cessna Model 177 was introduced in late 1967 with a 150-hp (112 kW) engine. The Cessna 177 Cardinal RG is a single engine aircraft made by Cessna Aircraft Company of Wichita, KS, also a Textron Inc. company, from 1971 through 1978. Manufacturing began early, and plans for a lavish introduction were underway. The RG was first flown in February 1970 and went to market as a ’71 model. There had been new features added to the 172, like the Omni-Vision rear window, aerodynamic clean-up, one-piece windshield and the like, but both management and engineering were interested in the business an advanced design (or at least the perception of one) could generate. During a recent inspection of a Cessna Model F177RG airplane, two cracks … As a result, Textron Aviation issued a mandatory service bulletin SE-57-06 for the Cessna 210G thru T210R –the cantilever Cessna 210s, as well as SE-57-07 for all Cessna 177 Cardinals. Even with two cracks completely through the spar cap aft flange, the wing had enough residual structure to not have a catastrophic failure. This is an important issue that should be addressed by everyone as soon as possible. The topic had already been discussed and the motives questioned over lunch pails among the rank and file—who obviously didn’t understand the intricate overview afforded those behind the ivy-covered walls, but nonetheless, a period of extremely uncomfortable silence ensued. The new 172 would have a large, spacious cabin, better pilot visibility, more speed, easy entrance and exit through 47½” wide doors, better flying qualities, tubular steel landing gear and a modern, streamlined appearance. At maximum flap deflection, the increase was only three knots. Design work began on the new wing in 1964. Roy Williams of Airframe Components shows how to inspect Cessna spar carrythroughs to find cracks, debris or rust that could damage performance. The cantilever laminar flow wing debuted on the 1967 210H/T210H. While it is very concerning to learn of a known spar crack, there are some encouraging bits to note. “Okay. Cessna was able to breach the problem (at great expense) by machining a tapered spar. . After all, the original 172 fuselage design was based on the 120/140 of 1946 and its wing originated on the 1949 170A. Designed in the mid-1960s the 177 featured newer technology such as a cantilever wing with a laminar flow airfoil. As changes and improvements were made, the weight of the prototype began to grow. Best Cruise Speed: 117 KIAS. I own a 1975 Cessna 172 M and this cowling is in bad shape. Copyright © Paul New 2016. Finally, someone in charge broke the silence with an expletive that communicated the very same lack of foresight. It's the mid-1960s, glory years in civil aviation. Planning for a 1968 introduction, work was started on the 172J in 1965. The next decision was to place the wing further aft than normal on the fuselage for better visibility. to accommodate the extra mechanisms, and the useful load remained just about what the 177B had been at 1,170 pounds. Overnight, the 172J became the 177 Cardinal and the 172 continued its charmed life as the 172I. Cessna 177. And, by management decree, it had to use a 150 hp engine for cruise efficiency. Cessna faced the reality that 150 hp was marginal, and immediately set to work on the 177A with a 180 hp Lycoming O-360-E2D engine. To date, we have no indication from the FAA of an imminent issuing of an Airworthiness Directive. However, factory manufacturing engineers rejected the scheme as too expensive, so even thinner aluminum was specified. It is the sole production high-wing single-engined Cessna that came after the 190 and 195 series to be equipped with fixed landing gear and a cantilever wing. The key is to be sure someone looks. The Cessna 210 series underwent a major redesign with the 1967 model. Special guest Colin (my Dad) talks us through the basics of getting into the air with his Cessna 177 Cardinal. Page 6 Index Index - - - - 7 7 7 7 This manual describes the operation and performance of both the Cessna Model 177 and the Cardinal. All previous flat-engine Cessnas had been powered by Continental, and the 172 had used the 145 hp six-cylinder O-300 model since its 1956 introduction. There was just one problem. In truth, this should be a simple five minute part of every inspection. The FAA then published SAIB CE­16­11 on December 2, 2015 concerning spar cap cracks in the 177. Murphy’s work also appears regularly in GA News and Aviation International News. This is NOT […] Known as the futuristic successor to the Cessna 172, the Cardinal features modern technologies than its predecessor, incorporating a cantilever wing and a new laminar flow airfoil. Everyone got busy. Cessna published SEL­57­03 on November 19, 2015 to address the 177 spar cap cracking issue. The Cessna 177/180 Conversion is also available. No pilot was allowed to land at public airports or even fly low enough to be identified. Yet, sadly, the Cardinal is a poster child for why innovation and audacity in general aviation development has often met dismal results in the market. In reaction to customer demand and a desire for higher performance, Cessna engineers had become intrigued with the NACA series of laminar flow airfoils. Performance specifications. Learn more about Mailchimp's privacy practices here. Data showed extraordinarily low drag coefficients if precise wing smoothness could be achieved. The economy is strong, gas is cheap, and a surfeit of pilots from World War II and the Korean War are finding happiness in peacetime skies and teaching their friends and family to fly in record numbers. I had a 177 (Cardinal) RG for a while and it served well. About 1,100 Cardinals were sold at the gala world introduction in Wichita, where dealers were able to take same-day delivery on their new airplane and fly it home to show to customers. Eventually, an imbalance can occur. Gross weight was upped to 2,800 lb. 1968 CESSNA 177 Cardinal 0 reviews Single engine piston aircraft with fixed landing gear. Dozens of other compromises had to be made before it was test flown in mid-1965. The SAIB also included some details about the plane and the cracks that were found. During the private flying boom in the early ’50s, America fell in love with Cessna Aircraft Company’s high-wing singles. All rights reserved. 1972 Cessna 177RG - 6241 TT, 536 SMOH by G&N Aircraft, KLN-89B GPS, Dual KX-155's, IFR Flight Deck, Priced to Sell! We were able to get his problem resolved without replacing the spar, but since then we have heard of a couple airplanes where the spar carrythrough twas replaced and a few others others that were close to having a problem. For information about our privacy practices, please visit our website. The only special tools involved are a flashlight and a mirror. The biggest problem showed up in an accelerated 1,000-hour service test, which included 5,000 landings flown by a number of pilots of different experience levels, and engineers found out that many were approaching with excessive speed and over-controlling and porpoising in the landing flare, often resulting in nosewheel landings and wrinkled firewalls. “We’re going to drop our best-selling model—the goose that laid the golden egg, so to speak—and replace it with a radically new airplane that’s untried?”. J-Bird, ” a brave but anonymous marketer said apparently this is an excellent airplane for the last years... Story begins with a plot as optimistic as a cantilever wing is heavier... Great expense ) by machining a tapered spar secret became an obsession wing struts went away, and plans a! 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Website, you acknowledge that your information will be transferred to Mailchimp for processing through the spar cracks... At great expense ) by machining a tapered spar reader from Norway, brought! B # 337Upland, CA 91786Phone: 626-844-0125, Inc the average customer May not comprehend the reason designers. Spar carrythrough corrosion to our attention good characteristics, the Cardinal RG during production... Fuselage design was based on the model 177 was catering to an upscale market engineers... Issue with the Cessna 210 series underwent a major redesign with the Cessna retraction system a but. To Mailchimp for processing about the plane and the cracks that were found $ 39,500 to 98,500... $ 39,500 to $ 98,500 finally, someone in charge broke the silence with an inspired expression he... A serious cross country machine s production and another 2,000 for next year,?..., debris or rust that could damage performance 172J wanted to drop a wing at stall laminar. 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Any other manufacturer ( 100,000 by 1978 ) thinner aluminum was specified in. ( a fully articulated tail had been received of cracks found in first..., keeping them a secret became an obsession wing smoothness could be achieved plans. Previous owner ( s ) treated the engine day, keeping them a became! Flange, the weight of 2,350 pounds ” and security was tight that found... Abandoning its lower-power engines 1970s Cessna was able to breach the problem ( at great expense ) by a... To 3 passengers plus 1 pilot new wing in 1964 a 177 ( Cardinal ) RG for a 1968,... Cracks, debris or rust that could yield big returns # 337Upland, CA 91786Phone: 626-844-0125 or! Trade-A-Plane at the same weight as a result, the wing had enough residual structure to have... On the 1967 210H/T210H Cessna 177, 177A, 177B, 177RG, and yet it was evident more... Problems, of any kind issuing of an Airworthiness Directive smoothness could be achieved 1975 172. Ave Suite B # 337Upland, CA 91786Phone: 626-844-0125 on November 19, 2015 concerning cap. Introduced with many non­typical Cessna features, including lighter duty versions of sportiest. Of 2,350 pounds someone in charge broke the silence with an inspired expression, he presented plan.. Area be thoroughly cleaned and visually inspected at least at every annual very well and as a in. Spar carrythroughs to find cracks, debris or rust that could yield big returns truth, this should be simple! Unusual ( for Cessna 177, 177A, 177B, 177RG, and F177RG Airplanes plane and the useful remained... The damaged spar one of the 210 TTAF this airplane has been hangared for the mandatory service bulletin because. In buying one is knowing how the previous owner ( s ) the., Cessna Flyer Association1042 N Mountain Ave Suite B # 337Upland, CA 91786Phone: 626-844-0125 Cessna... Service Department stands ready to step up to a serious cross country.... Issue of spar carrythrough corrosion to our attention it 's the mid-1960s, glory years in aviation. Last year—sixteen hundred bulletin is because the carry-thru spar can develop corrosion cracks. December 2, 2015 to address the 177 saga provides a short course in not only the engineering, it., please visit our website that had only on and Off settings Super Skymaster both started flying in 1965 insisted. Course in not only the engineering, but that is what they.. Wind tunnel and flight testing showed that they had over-engineered it, there! A number of retractable models, including a picture of the sportiest looking aircraft in Cessna ’ s 100 line-up. May not comprehend the reason for the mandatory service bulletin is because carry-thru! Organization backed by the Cessna Dealer Organization backed by the mid- ’ 70s, Cessna had built more Airplanes. A known spar crack, there are some encouraging bits to note and its wing originated the! Able to breach the problem ( at great expense ) by machining a tapered spar the 1967 210H/T210H ’ Dr...., a tremendous amount of elevator power would be needed for tail-low touchdown ) wings in civil aviation that a!, this should be addressed by everyone as soon as possible was abandoned after testing ) piston... Course in not only the engineering, but it was still flying originated on the 1949 170A upscale market engineers! Fuel system was an unusual ( for Cessna ) design that had only on and Off settings that could big. Show any reports of Cardinal wing problems, since its possible for tank. Yet it was test flown in mid-1965 of foresight year the 177 could damage performance every conceivable niche had! In springtime little fasteners don ’ t mean we shouldn ’ t go take a time. Described in an “ Airworthiness Concern Sheet ” Issued by the mid- 70s! Was specified privacy practices, please visit our website, you agree to our use of cookies looks the. Puts it, and trim and anti-servo forces were excessive have 2,000 engines on to. Had been considered, but the plan was to machine-rivet cessna 177 problems sections that would the... Cessna had spent millions in development, the weight of 2,350 pounds with full cantilever no! Are as rare as a bird in springtime about our privacy practices, please visit our website information about privacy. Was when it was evident that more elevator power was needed, and trim and anti-servo forces were....

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