26426 Federal Register / Vol. 61, No. 103 / Tuesday, May 28, 1996 / Rules and Regulations

Need for the Correction

The AD incorrectly references the

‘‘. . . upper surface of the wing. . .’’

instead of the lower surface of the wing.

Cessna Models 208 and 208B airplanes

are designed with the wings sitting high

on the body of the airplane, which

would not allow the pilot to visually

check the upper surface of the wings on

the airplane during flight without

exiting the airplane.

Correction of Publication

Accordingly, the publication of May

7, 1996 (61 FR 20641), of Amendment

39–9591; AD 96–09–15, which was the

subject of FR Doc. 96–10729, is

corrected as follows:

§ 39.13 [Corrected]

On page 20642, in the third column,

§ 39.13, paragraph (a)(1) of the AD, line

15 from the top of the column, correct

‘‘—Accumulation of ice on the upper

surface’’ to read ‘‘—Accumulation of ice

on the lower surface’’.

Action is taken herein to clarify this

requirement of AD 96–09–15 and to add

this AD correction to § 39.13 of the

Federal Aviation Regulations (14 CFR

39.13).

The effective date remains June 11,

1996.

Issued in Kansas City, Missouri on May 17,

1996.

Michael Gallagher,

Manager, Small Airplane Directorate, Aircraft

Certification Service.

[FR Doc. 96–13061 Filed 5–24–96; 8:45 am]

BILLING CODE 4910–13–U

14 CFR Part 39

[Docket No. 96–CE–04–AD; Amendment 39–

9590; AD 96–09–14]

RIN 2120–AA64

Airworthiness Directives; Dornier 228

Series Airplanes; Correction

AGENCY: Federal Aviation

Administration, DOT.

ACTION: Final rule; correction.

SUMMARY: This action makes a

correction to Airworthiness Directive

(AD) 96–09–14 concerning all Dornier

228 series airplanes, which was

published in the Federal Register on

May 7, 1996 (61 FR 20639). That

publication incorrectly references a cue

for the pilot or crew member in severe

icing conditions. The AD currently

requires the pilot to follow certain

visual cues during flight in icing

conditions and the second of these cues

requires the pilot to look at the upper

surface of the wing. The word ‘‘upper’’

is wrong in the second cue. The intent

of the AD in paragraph (a)(1), first

bullet, second cue, is to require the pilot

or crew member to look at the ‘‘lower’’

surface of the wing. This action corrects

the AD to reflect this change.

EFFECTIVE DATE: June 11, 1996.

FOR FURTHER INFORMATION CONTACT: Mr.

John Dow, Aerospace Engineer, FAA,

Small Airplane Directorate, 1201

Walnut, suite 900, Kansas City, Missouri

64106; telephone (816) 426–6934;

facsimile (816) 426–2169.

SUPPLEMENTARY INFORMATION: On May 7,

1996, the Federal Aviation

Administration (FAA) issued AD 96–

09–14, Amendment 39–9590 (61 FR

20639, May 7, 1996), which applies to

all Dornier 228 series airplanes. This AD

requires a revision in the Airplane

Flight Manual (AFM) by incorporating a

warning into the Limitations Section of

the AFM. Within this warning (in the

first bulleted paragraph) are cues for the

pilot to follow during flight in severe

icing conditions. The second cue

references accumulation of ice on the

upper surface of the wing aft of the

protected area.

Need for the Correction

The AD incorrectly references the

‘‘* * * upper surface of the wing

* * *’’ instead of the lower surface of

the wing. Dornier 228 series airplanes

are designed with the wings sitting high

on the body of the airplane, which

would not allow the pilot to visually

check the upper surface of the wings on

the airplane during flight without

exiting the airplane.

Correction of Publication

Accordingly, the publication of May

7, 1996 (61 FR 20639), of Amendment

39–9590; AD 96–09–14, which was the

subject of FR Doc. 96–10722, is

corrected as follows:

§ 39.13 [Corrected]

On page 20641, in the first column,

§ 39.13, paragraph (a)(1) of the AD, line

12 from the top of the column, correct

‘‘—Accumulation of ice on the upper

surface’’ to read ‘‘—Accumulation of ice

on the lower surface’’.

Action is taken herein to clarify this

requirement of AD 96–09–14 and to add

this AD correction to § 39.13 of the

Federal Aviation Regulations (14 CFR

39.13).

The effective date remains June 11,

1996.

Issued in Kansas City, Missouri on May 17,

1996.

Michael Gallagher,

Manager, Small Airplane Directorate, Aircraft

Certification Service.

[FR Doc. 96–13060 Filed 5–24–96; 8:45 am]

BILLING CODE 4910–13–U

14 CFR Part 39

[Docket No. 96–CE–03–AD; Amendment 39–

9589; AD 96–09–13]

RIN 2120—AA64

Airworthiness Directives; Beech

Aircraft Corporation Models 99, 99A,

A99A, B99, C99, B200, B200C, 1900,

1900C, and 1900D Airplanes;

Correction

AGENCY: Federal Aviation

Administration, DOT.

ACTION: Final rule; correction.

SUMMARY: This action makes a

correction to Airworthiness Directive

(AD) 96–09–13 concerning Beech

Aircraft Corporation (Beech) Models 99,

99A, A99A, B99, C99, B200, B200C,

1900, 1900C, and 1900D airplanes,

which published in the Federal Register

on May 7, 1996 (61 FR 20638). That

publication incorrectly references a cue

for the pilot or crew member in severe

icing conditions. The AD currently

requires the pilot to follow certain

visual cues during flight in icing

conditions and the second of these cues

requires the pilot to look at the lower

surface of the wing. The word ‘‘lower’’

is wrong in the second cue. The intent

of the AD in paragraph (a)(1), first

bullet, second cue, is to require the pilot

or crew member to look at the ‘‘upper’’

surface of the wing. This action corrects

the AD to reflect this change.

EFFECTIVE DATE: June 11, 1996.

FOR FURTHER INFORMATION CONTACT: Mr.

John Dow, Aerospace Engineer, FAA,

Small Airplane Directorate, 1201

Walnut, suite 900, Kansas City, Missouri

64106; telephone (816) 426–6934;

facsimile (816) 426–2169.

SUPPLEMENTARY INFORMATION: On May 7,

1996, the Federal Aviation

Administration (FAA) issued AD 96–

09–13, Amendment 39–9589 (61 FR

20638, May 7, 1996), which applies to

Beech Models 99, 99A, A99A, B99, C99,

B200, B200C, 1900, 1900C, and 1900D

airplanes. This AD requires a revision in

the Airplane Flight Manual (AFM) by

incorporating a warning into the

Limitations Section of the AFM. Within

this warning (in the first bulleted

paragraph) are cues for the pilot to

follow during flight in severe icing

conditions. The second cue references
Federal Register / Vol. 61, No. 103 / Tuesday, May 28, 1996 / Rules and Regulations 26427

accumulation of ice on the lower surface

of the wing aft of the protected area.

Need for the Correction

The AD incorrectly references the

‘‘* * * lower surface of the wing

* * *’’ instead of the upper surface of

the wing. Beech Models 99, 99A, A99A,

B99, C99, B200, B200C, 1900, 1900C,

and 1900D airplanes are designed with

the wings sitting low on the body of the

airplane, which would not allow the

pilot to visually check the lower surface

of the airplane during flight without

exiting the airplane.

Correction of Publication

Accordingly, the publication of May

7, 1996 (61 FR 20638), of Amendment

39–9589; AD 96–09–13, which was the

subject of FR Doc. 96–10723, is

corrected as follows:

§ 39.13 [Corrected]

On page 20639, in the second column,

§ 39.13, paragraph (a)(1) of the AD, line

10 from the top of the column, correct

‘‘—Accumulation of ice on the lower

surface’’ to read ‘‘—Accumulation of ice

on the upper surface’’.

Action is taken herein to clarify this

requirement of AD 96–09–13 and to add

this AD correction to § 39.13 of the

Federal Aviation Regulations (14 CFR

39.13).

The effective date remains June 11,

1996.

Issued in Kansas City, Missouri on May 17,

1996

Michael Gallagher,

Manager, Small Airplane Directorate, Aircraft

Certification Service.

[FR Doc. 96–13059 Filed 5–24–96; 8:45 am]

BILLING CODE 4910–13–U

14 CFR Part 39

[Docket No. 96–CE–02–AD; Amendment 39–

9588; AD 96–09–12]

RIN 2120–AA64

Airworthiness Directives; Empresa

Brasileiro de Aeronautico, S.A. Models

EMB–110P1 and EMB–110P2

Airplanes; Correction

AGENCY: Federal Aviation

Administration, DOT.

ACTION: Final rule; correction.

SUMMARY: This action makes a

correction to Airworthiness Directive

(AD) 96–09–12 concerning Empresa

Brasileiro de Aeronautico, S.A.

(EMBRAER) Models EMB–110P1 and

EMB–110P2 airplanes, which published

in the Federal Register on May 7, 1996

(61 FR 20636). That publication

incorrectly references a cue for the pilot

or crew member in severe icing

conditions. The AD currently requires

the pilot to follow certain visual cues

during flight in icing conditions and the

second of these cues requires the pilot

to look at the lower surface of the wing.

The word ‘‘lower’’ is wrong in the

second cue. The intent of the AD in

paragraph (a)(1), first bullet, second cue,

is to require the pilot or crew member

to look at the ‘‘upper’’ surface of the

wing. This action corrects the AD to

reflect this change.

EFFECTIVE DATE: June 11, 1996.

FOR FURTHER INFORMATION CONTACT: Mr.

John Dow, Aerospace Engineer, FAA,

Small Airplane Directorate, 1201

Walnut, suite 900, Kansas City, Missouri

64106; telephone (816) 426–6934;

facsimile (816) 426–2169.

SUPPLEMENTARY INFORMATION: On May 7,

1996, the Federal Aviation

Administration (FAA) issued AD 96–

09–12, Amendment 39–9588 (61 FR

20636, May 7, 1996), which applies to

EMBRAER Models EMB–110P1 and

EMB–110P2 airplanes. This AD requires

a revision in the Airplane Flight Manual

(AFM) by incorporating a warning into

the Limitations Section of the AFM.

Within this warning (in the first

bulleted paragraph) are cues for the

pilot to follow during flight in severe

icing conditions. The second cue

references accumulation of ice on the

lower surface of the wing aft of the

protected area.

Need for the Correction

The AD incorrectly references the

‘‘* * * lower surface of the wing

* * *’’ instead of the upper surface of

the wing. The EMBRAER Models EMB–

110P1 and EMB–110P2 airplanes are

designed with the wings sitting low on

the body of the airplane, which would

not allow the pilot to visually check the

lower surface of the airplane during

flight without exiting the airplane.

Correction of Publication

Accordingly, the publication of May

7, 1996 (61 FR 20636), of Amendment

39–9588; AD 96–09–12, which was the

subject of FR Doc. 96–10725, is

corrected as follows:

§ 39.13 [Corrected]

On page 20637, in the second column,

§ 39.13, paragraph (a) (1) of the AD, the

second to the last line from the bottom

of the column, correct ‘‘—Accumulation

of ice on the lower surface’’ to read ‘‘—

Accumulation of ice on the upper

surface’’.

Action is taken herein to clarify this

requirement of AD 96–09–12 and to add

this AD correction to § 39.13 of the

Federal Aviation Regulations (14 CFR

39.13).

The effective date remains June 11,

1996.

Issued in Kansas City, Missouri, on May

17, 1996.

Michael Gallagher,

Manager, Small Airplane Directorate, Aircraft

Certification Service.

[FR Doc. 96–13058 Filed 5–24–96; 8:45 am]

BILLING CODE 4910–13–U

14 CFR Part 39

[Docket No. 95–SW–32–AD; Amendment

39–9634; AD 96–11–09]

RIN 2120–AA64

Airworthiness Directives; Robinson

Helicopter Company Model R44 Helicopters

AGENCY: Federal Aviation

Administration, DOT.

ACTION: Final rule.

SUMMARY: This amendment adopts a

new airworthiness directive (AD),

applicable to Robinson Helicopter

Company (Robinson) Model R44

helicopters, that requires an adjustment

to the low-RPM warning unit threshold

to increase the revolutions-per-minute

(RPM) at which the warning horn and

caution light activate, and revisions to

the R44 Rotorcraft Flight Manual that

prohibit flight with the throttle governor

(governor) selected off, except in certain

situations. This amendment is prompted

by an FAA Technical Panel Review of

Robinson accident history data which

revealed that main rotor (M/R) blade

stall at abnormally low M/R RPM

resulted in accidents. The actions

specified by this AD are intended to

minimize the possibility of pilot

mismanagement of the M/R RPM, which

could result in unrecoverable M/R stall

and subsequent loss of control of the

helicopter.

EFFECTIVE DATE: July 2, 1996.

FOR FURTHER INFORMATION CONTACT: Ms.

Elizabeth Bumann, Aerospace Engineer,

FAA, Los Angeles Aircraft Certification

Office, 3960 Paramount Blvd.,

Lakewood, California 90712–4137,

telephone (310) 627–5265; fax (310)

627-5210.

SUPPLEMENTARY INFORMATION: A

proposal to amend part 39 of the Federal

Aviation Regulations (14 CFR part 39) to

include an airworthiness directive (AD)

that is applicable to Robinson Model

R44 helicopters was published in the

Federal Register on February 2, 1996

(61 FR 3882). That action proposed to

require resetting the warning unit to

activate the warning horn and caution