AD 96-09-22

AD Final Rules - DRS_96-09-22.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
96-09-22
Document Type:
AD Final Rules
Docket Number:
96-NM-17-AD
Subject Heading:
Airworthiness Directives; CONSTRUCCIONES AERONAUTICAS, S.A. CASA Model C-212 and CN-235 Series Airplanes
Subject:
AFM - Icing
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
06/11/1996
Make:
EADS CASA
Model:
C-212-CB | C-212-CC | C-212-CD | C-212-CE | C-212-CF | C-212-DE | C-212-DF | CN-235 | CN-235-100 | CN-235-200
Product Type:
Aircraft
Product Subtype:
Large Airplane
Affected AD:
Superseded AD:
Affected By:
Superseded By:
Service/Office:
Office of Primary Responsibility:
CFR Part Reference:
Part 39
Comments:
AIRWORTHINESS DIRECTIVES FINAL RULES: 96-09-22
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   96-NM-17-AD

AMENDMENT:   39-9598

AD NUMBER:   96-09-22

SUBJECT HEADING:   Airworthiness Directives; CONSTRUCCIONES AERONAUTICAS, S.A. CASA Model C-212 and CN-235 Series Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective June 11, 1996.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
96-09-22 CONSTRUCCIONES AERONAUTICAS, S.A. CASA: Amendment 39-9598. Docket 96-NM-17-AD.
Applicability: All Model C-212 and CN-235 series airplanes, certificated in any category.

NOTE 1: This AD applies to each airplane identified in the preceding applicability provision, regardless of whether it has been modified, altered, or repaired in the area subject to the requirements of this AD. For airplanes that have been modified, altered, or repaired so that the performance of the requirements of this AD is affected, the owner/operator must request approval for an alternative method of compliance in accordance with paragraph (b) of this AD. The request should include an assessment of the effect of the modification, alteration, or repair on the unsafe condition addressed by this AD; and, if the unsafe condition has not been eliminated, the request should include specific proposed actions to address it.

Compliance: Required as indicated, unless accomplished previously.

To minimize the potential hazards associated with operating the airplane in severe icing conditions by providing more clearly defined procedures and limitations associated with such conditions, accomplish the following:

(a) Within 30 days after the effective date of this AD, accomplish the requirements of paragraphs (a)(1) and (a)(2) of this AD.

NOTE 2: Operators must initiate action to notify and ensure that flight crewmembers are apprised of this change.

(1) Revise the FAA-approved Airplane Flight Manual (AFM) by incorporating the following into the Limitations Section of the AFM. This may be accomplished by inserting a copy of this AD in the AFM.

"WARNING

Severe icing may result from environmental conditions outside of those for which the
airplane is certificated. Flight in freezing rain, freezing drizzle, or mixed icing conditions
(supercooled liquid water and ice crystals) may result in ice build-up on protected
surfaces exceeding the capability of the ice protection system, or may result in ice
forming aft of the protected surfaces. This ice may not be shed using the ice protection
systems, and may seriously degrade the performance and controllability of the airplane.

o During flight, severe icing conditions that exceed those for which the airplane is
certificated shall be determined by the following visual cues. If one or more of these
visual cues exists, immediately request priority handling from Air Traffic Control to facilitate
a route or an altitude change to exit the icing conditions.

- Unusually extensive ice accreted on the airframe in areas not normally observed to
collect ice.

- Accumulation of ice on the lower surface of the wing aft of the protected area.

- Accumulation of ice on the propeller spinner farther aft than normally observed.

o Since the autopilot may mask tactile cues that indicate adverse changes in handling
characteristics, use of the autopilot is prohibited when any of the visual cues specified
above exist, or when unusual lateral trim requirements or autopilot trim warnings are
encountered while the airplane is in icing conditions.

o All icing detection lights must be operative prior to flight into icing conditions at night.
[NOTE: This supersedes any relief provided by the Master Minimum Equipment List
(MMEL).]"

(2) Revise the FAA-approved AFM by incorporating the following into the Procedures Section of the AFM. This may be accomplished by inserting a copy of this AD in the AFM.

"THE FOLLOWING WEATHER CONDITIONS
MAY BE CONDUCIVE TO SEVERE IN-FLIGHT ICING:

o Visible rain at temperatures below 0 degrees Celsius ambient air temperature.

o Droplets that splash or splatter on impact at temperatures below 0 degrees Celsius
ambient air temperature.

PROCEDURES FOR EXITING
THE SEVERE ICING ENVIRONMENT:

These procedures are applicable to all flight phases from takeoff to landing. Monitor the
ambient air temperature. While severe icing may form at temperatures as cold as -18
degrees Celsius, increased vigilance is warranted at temperatures around freezing with
visible moisture present. If the visual cues specified in the Limitations Section of the AFM
for identifying severe icing conditions are observed, accomplish the following:

o Immediately request priority handling from Air Traffic Control to facilitate a route or an
altitude change to exit the severe icing conditions in order to avoid extended exposure to
flight conditions more severe than those for which the airplane has been certificated.

o Avoid abrupt and excessive maneuvering that may exacerbate control difficulties.

o Do not engage the autopilot.

o If the autopilot is engaged, hold the control wheel firmly and disengage the autopilot.

o If an unusual roll response or uncommanded roll control movement is observed, reduce
the angle-of-attack.

o Do not extend flaps during extended operation in icing conditions. Operation with flaps
extended can result in a reduced wing angle-of-attack, with the possibility of ice forming
on the upper surface further aft on the wing than normal, possibly aft of the protected
area.

o If the flaps are extended, do not retract them until the airframe is clear of ice.

o Report these weather conditions to Air Traffic Control."

(b) An alternative method of compliance or adjustment of the compliance time that provides an acceptable level of safety may be used if approved by the Manager, Standardization Branch, ANM- 113, FAA, Transport Airplane Directorate. Operators shall submit their requests through an appropriate FAA Principal Operations Inspector, who may add comments and then send it to the Manager, Standardization Branch, ANM-113.

NOTE 3: Information concerning the existence of approved alternative methods of compliance with this AD, if any, may be obtained from the Standardization Branch, ANM-113.

(c) Special flight permits may be issued in accordance with sections 21.197 and 21.199 of the Federal Aviation Regulations (14 CFR 21.197 and 21.199) to operate the airplane to a location where the requirements of this AD can be accomplished.

(d) This amendment becomes effective on June 11, 1996.

FOOTER: