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NTSB Safety Alert SA-042 - Mechanics Prevent Misrigging Mistakes
Reproduced for study. Always verify against the official GACAR at gaca.gov.sa.
Mechanics: Prevent Misrigging Mistakes
Verify correct directional travel of controls and trim
The problem
Incorrect rigging of flight control and trim systems has led to in -flight emergencies,
accidents, and even deaths.
Four such mishaps within a 2 -year span share common safety issues:
o Maintenance personnel who serviced or checked the systems did not
recognize that the control or trim surfaces were moving in the wrong direction.
o Pilots who flew the airplanes did not noti ce the control anomalies during their
preflight checks.
Anyone can make mistakes. In some cases, the mechanics who performed the work
incorrectly were highly experienced.
Related incident and accidents:
In December 2014, the pilot of a Cessna T182T airplan e experienced extreme
nose -down control forces on the yoke shortly after takeoff. The airplane had just
undergone maintenance on the elevator trim system, and the mechanic briefed the
pilot about the work before the flight. Both the pilot and the pilot -certificated
passenger needed to pull hard aft on the yoke to prevent the airplane from pitching
down, even though the elevator pitch trim indicator showed a nearly full nose -up trim
position. The pilot remembered that work had been done on the elevator trim system,
and he thought that there might be some kind of control -reversal problem. While
maneuvering for the emergency landing, the pilot applied nose -down trim control
inputs and found that the extreme control forces lessened, and he successfully
landed th e airplane. The elevator trim control cables were misrigged such that the
elevator trim control was reversed. The mechanic who performed the work had 26
years of experience and described that he had carefully checked the trim tab
deflection angles. However, he did not recognize that the trim tab moved in the wrong
direction. The mechanic who checked the work had 24 years of experience and noted
that the cable rigging problem could not be clearly visually identified through the
airplane’s access panel . The maintenance manual provided the following information:
SA-042 March 2015 , revised December 2015 “Make sure that the trim tab moves in the correct direction when it is operated by the
trim wheel. NOTE: Nose down trim corresponds to the tab UP position.”
(CEN15IA079 )1
In May 2013, the pilot of a Schweizer SGS 2 -33A glider received serious injuries after
the glider crashed due to imprope r rigging of the rudder control cables. The glider had
just received an annual inspection, and its rudder had been removed and reinstalled.
The mechanic who conducted a flight control check after the annual inspection with
assistance from another pilot sea ted in the cockpit stated that he confirmed
movement of the rudder while at the rear of the glider; however, he did not see which
pedal the pilot was pushing and did not verbally confirm the corresponding position of
the rudder pedals. The mechanic had 35 years of experience and had assembled
hundreds of gliders. ( ERA13LA229 )
In October 2013, the private pilot and passenger in a Piper PA -22 received serious
injuries when the airplane crashed during takeoff on its first flight since an annual
inspection in which frayed elevator control cables were replaced. During the takeoff
roll, when the pilot ap plied forward stick controls to raise the tail, the tail did not rise,
and the airplane instead “jumped” off the runway. The pilot reduced engine power
and attempted to control the airplane’s pitch, but it responded abnormally and
crashed. The elevator con trol cables were installed incorrectly such that the elevator
moved in the direction opposite to that commanded. (ERA14LA015 )
In July 2014 , the pilot of a Piper PA -12 airplane was fatally injured after his airplane
pitched up steeply during takeoff and crashed after the airplane had undergone
extensive maintenance. The elevator control cables were installed incorrectly such
that the elevator moved in the direction opposite to that commanded. (ANC14FA050 )
What can maintenance personnel d o?
Become familiar with the normal directional movement of the controls and surfaces
before disassembling the systems. It is easier to recognize “abnormal” if you are very
familiar with what “normal” looks like.
Carefully follow manufacturers’ instructions to ensure that the work is completed as
specified. Always refer to up -to-date instructions and manuals —including
airworthiness directives, maintenance alerts, special airworthiness information
bulletins, and unapproved parts not ifications —when performing a task.
Be aware that some maintenance information, especially for older airplanes, may be
nonspecific . Ask questions of another qualified person if something is unfamiliar.
Remember that well -meaning, motivated, experienced te chnicians can make
mistakes: fatigue, distraction, stress, complacency, and pressure to get the job done
are some common factors that can lead to human errors. Learn about and adhere to
sound risk management practices to help prevent common errors.
1 These pilots and the mechanic are featured in the NTSB’s safety video, “ Airpla ne Misrigging: Lessons
Learned F rom a Close Call ,” which is available on the NTSB’s Safety V ideos web page at
http://www.ntsb.gov/safety/safety -alerts/Pages/Safety -Videos.aspx .
SA-042 March 2015 , revised December 2015 Ensure that the aircraft owner or pilot is thoroughly briefed about the work that has
been performed. This may prompt them to thoroughly check the system during
preflight or help them successfully troubleshoot if an in -flight problem occurs.
Interested in more i nformation ?
The reports for the accidents referenced in this safety alert are accessible by NTSB accident
number from the Aviation Accident Database & Synopses web page at
http://www.ntsb.gov/_layouts/ntsb.aviation/index.aspx .2 Each accident’s public docket is
accessible from the NTSB’s Docket Management System web page at
http://dms.ntsb.gov/pubdms/ .
Education and training are cri tical to improving GA safety. The Federal Aviation
Administration (FAA) Safety Team ( FAASTeam ) provides access to online training courses,
seminars, and webinars to provide mechanics with recurrent training that focuses on
accident and incident causal factors, special emphasis items, and regulatory issues. The
courses listed below (and many others ), as well as seminar and webinar information, can be
accessed from the FAASTeam website at www.faasafety.gov . (Course access requires login
through an existing free FAASTeam account or creatin g a new one .)
Dirty Dozen: Human Error in Aircraft Maintenance
Human Factors Prim er for Aviation Mechanics
Failure to Follow Procedures: Installation
Failure to Follow Procedures: Inspections
Aircraft Maintenance Documentation for AMTs
Fatigue Countermeasure Training
Aviation Maintenance Technician Handbook — General (FAA -H-8083 -30) includes an
“Addendum/Human Factors ,” which discusses the human factors -related conditions behind
most maintenance errors. The addendum (which is also called chapt er 14) can be accessed
from the FAA’s website at www.faa.gov .
“Acceptable Methods, Techniques, and Practices —Aircraft Inspection and Repair ” (FAA
Advisory Circular 43. 13-1B) contains a Personal Minimums Checklist in chapter 13 that lists
actions to reduce maintenance errors.
Aircraft Safety Alerts , including airworthiness directives, maintenance alerts, special
airworthiness information bulletins, and unapproved parts notifications, can be accessed
from www.faa.gov/aircraft/safety/alerts .
This NTSB safety alert and others can be accessed from the NTSB’s Safety Alerts web
page at http://www.ntsb.gov/safety/safety -alerts/Pages/default.aspx or searched from the
NTSB home page at http://www.ntsb.gov/Pages/default.aspx .
2 Less-recent fatal accidents that may also be of interest are CHI05FA038 , CHI08MA270 , and
DCA03MA022 .
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