Cessna Model 402C airworthiness concern
Cessna Model 402C airworthiness concern
Aviation Safety INFORMATION BULLETIN
SUBJ: Hydraulic Power – Indicating Date: August 9, 2010
This is information only. Recommendations aren’t mandatory.
This Special Airworthiness Information Bulletin alerts owners and operators of Cessna Model 402C
airplanes of an airworthiness concern, specifically a reminder of the meaning of the “HYD PRESS”
indication, and what may happen if this indication is not addressed.
At this time, the airworthiness concern is not an unsafe condition that would warrant Airworthiness
Directive (AD) action under Title 14 of the Code of Federal Regulations (14 CFR) Part 39.
Six minutes after takeoff from a busy airport, a pilot reported smoke in the cockpit and declared an
emergency. The aircraft landed without incident and all passengers and crew deplaned successfully.
Maintenance determined that the hydraulic pressure did not relieve due to the nose gear not fully
retracting. The nose strut did not extend completely, which prevented the nose gear from going in the
up and locked position. This caused the hydraulic system to remain pressurized, which caused the
fluid to heat up enough to melt the hydraulic reservoir sight tube. The hot hydraulic fluid then spilled
out into the nose baggage compartment, releasing fumes into the cockpit and causing the perceived
The Model 402C uses a hydraulically actuated landing gear system. When the landing gear is locked
Up or Down, the hydraulic fluid is continually circulated through the system by the engine driven
hydraulic pumps at a nominal pressure up to 50 psi. When the gear is selected from one position to
another, the pressure varies but can reach as high as 1750 psi. When the system is pressurized above
150-175 psi, a pressure switch in the system activates an annunciator light (“HYD PRESS”). This
light indicates that hydraulic pressure is flowing to the landing gear system. Any time the landing
gear is in transit, the HYD PRESS annunciator should be illuminated.
Although we were unable to verify this, the HYD PRESS light in the above incident should have
been illuminated starting at the time when the pilot selected gear Up, and should have remained
illuminated for an extended time because the nose gear did not fully retract.
Cessna has since released temporary revisions (TRs) to the pilots operating handbook (POH) for this
aircraft with the following information:
1. To make it easier for pilots to find the correct procedures, the procedures for “Hyd Pressure
Light Illuminated After Gear Cycle” were moved from Landing Gear Emergency
Procedures to Hydraulic System Emergency Procedures (this new section was created by
2. A Caution statement was added to the Amplified Procedures to emphasize that if the
hydraulic system remains pressurized for an extended period of time, the sight tube could
rupture. (Previously, the POH stated without a Caution statement that damage to the system
3. The Emergency Procedures, both the Abbreviated and the Amplified procedures, for “Hyd
Pressure Light Illuminated After Gear Cycle” were enclosed in a box, making them
immediate action items that are to be committed to the pilot’s memory. This point is
especially important because this issue is most likely to occur shortly after takeoff, when the
pilot is busy. If this were to occur, the pilot should not have to look through the POH in an
attempt to find the correct procedure to address the indication; the pilot should already
understand the issue and know how to resolve it.
We recommend that pilots do the following:
1. Incorporate the TRs above into your POH; and
2. When the HYD PRESS light remains illuminated for an extended time (longer than the
normal landing gear cycle time), complete the procedures for “Hyd Pressure Light Illuminated
After Gear Cycle” that they previously committed to memory. Please see the TRs to the POH
for these procedures. Delaying completion of the procedures could result in damage to the
hydraulic system and smoke/vapors in the cockpit.
For Further Information Contact
Ann Johnson, Aerospace Engineer, 1801 Airport Rd., Wichita, KS 67209; phone: (316) 946-4105;
For Related Service Information Contact
Cessna Aircraft Company, Product Support, PO Box 7706, Wichita, KS 67277; phone: (316) 517-
5800; fax: (316) 517-7271.
Executive Director of the Cessna Owner Organization
(715) 445-5000, ext. 116
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