737NG自动减速板系统保留很常见,有同事提过关于SFP的疑问,虽然我们执管的飞机目前没有SFP构型,但是其他分子公司有,需要能找到判断的手册依据。
自动减速板系统失效保留,应该按MEL27-07-01还是MEL27-07-02?
MEL27-08襟翼负载限制器系统保留也有SFP构型区分,并且对于SFP构型的飞机,O项或限制项有些区别,所以有必要搞清楚按哪条款保留。
解答这个问题的关键是弄清SFP。
关于SFP,AMM手册并没有提到。但是在MEL有相关信息,我们使用SFP搜索发现,SFP飞机的一个特点是襟翼手柄放到30以上,前缘缝翼才全伸出。
反查AMM SDS,对于30度缝翼全伸出的飞机有GUN 041, 043, 215, 224, 226, 229-999。
MEL27-04-02
AMM SDS
也可以查询波音 737-700/800 快速检查单,带短跑道性能构型的飞机有YR302, YR310,YS966-YS977, YS981 -YS987;YW401 -YW430;YW441 -YW444。
再反查有效性页面就能确认哪些飞机属于SFP构型了。包括B-5586/5598/1737/1776/1780等。
关于SFP,详细说明可查阅阮工频道这两篇文章:
在网上也搜了 关于SFP的一些背景和资料,大部分内容阮工的文章已涵盖。
The 737 design enhancements allow operators to fly increased payload in and out of airports with runways less than 5,000 feet long.
737的设计增强功能使运营者可以在跑道长度小于5000英尺的进场和离场飞行增加有效载荷。
The design enhancements include a two-position tail skid that enables reduced approach speeds, sealed leading-edge slats that provide increased lift during takeoff, and increased flight spoiler deflection on the ground that improves takeoff and landing performance.
设计改进包括一个可以降低进近速度的双位置尾橇,在起飞期间提供更多升力的密封缝翼,和在地面提高起飞和着陆性能的增加偏转角的飞行扰流板。
The short-field performance changes were developed in 2004 in response to Brazilian airline GOL's needs at Santos Dumont airstrip in Rio de Janeiro. The 4,300-foot runway is short compared to other runways and could not accommodate larger aircraft at higher approach speeds with full payloads.
为应对巴西航空公司GOL在里约热内卢桑托斯杜蒙机场的需求,2004年对短场性能进行了调整。4300英尺的跑道与其他跑道相比很短,无法容纳更高进近速度和满负荷的飞机。
The short-field design package is an option on the 737-600, -700 and -800 and is standard equipment for the 737-900ER.
短场设计包在737-600,-700和-800飞机是一种选装构型,在737-900ER是标准构型。
The enhancements increase payload capability for landing up to 8,000 pounds and increase payload capability for takeoff up to 2,000 pounds on the 737-800.
在737-800飞机增强性,为着陆提高载荷能力高达8000磅,为起飞提高载荷能力高达2000磅。
Short Runway Package Technical Aspects:
短跑道包技术方面:
A winglet lift credit, achieved through additional winglet testing, that allows the use of lower landing-approach speeds。
通过测试实现的翼梢,允许使用较低的着陆接近速度。
Takeoff performance improvements such as using sealed leading-edge slats on all takeoff flap positions, which allows the airplane to climb up and away more rapidly on shorter runways.
起飞性能的提高,比如起飞全襟翼使用密封的前缘缝翼,这使得飞机在较短的跑道上爬升和离场更快。
A reduced idle thrust transition delay between approach- and ground-idle speeds, which improves stopping distances and increases field-length-limited landing weight.
减少了进近和地面怠速之间的怠速推力过渡延迟,改善了滑行距离,提高了跑道长度有限的着陆重量。
Increased flight-spoiler deflection from 30 degrees to 60 degrees, which aids brake performance when landing.
飞行扰流板偏转从30度增加到60度,这有助于着陆时刹车性能。
A two-position tailskid at the rear of the aircraft. The tailskid protects longerbodied 737-800s against inadvertent tailstrikes during landing, which allows higher aircraft approach attitudes and lower landing speeds.
飞机尾部有两个位置尾翘。在着陆过程中,尾翘保护长机体737-800飞机,避免着陆时机尾擦地。从而允许飞机以更高的姿态和更低的速度着陆。