AD 75-11-10

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AD Number:
75-11-10
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; MCDONNELL DOUGLAS DC-10-10, -10F, -30, -30F, and -40 Series Airplanes
Subject:
Doors
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
03/17/1976
Make:
The Boeing Company
Model:
DC-10-10 | DC-10-10F | DC-10-30 | DC-10-30F (KC-10A, KDC-10) | DC-10-40
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Superseded AD: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Superseded By: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:
Updated RGL applicability to match AD applicability; CAR C-11-185
AIRWORTHINESS DIRECTIVES FINAL RULES: 75-11-10
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-2539

AD NUMBER:   75-11-10

SUBJECT HEADING:   Airworthiness Directives; MCDONNELL DOUGLAS DC-10-10, -10F, -30, -30F, and -40 Series Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective March 17, 1976.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
75-11-10 MCDONNELL DOUGLAS: Amendment 39-2218 as amended by Amendment 39-2377 is further amended by Amendment 39-2539. Applies to Douglas Model DC-10-10, -10F, -30, -30F, and -40 Series airplanes, certificated in all categories, with factory serial or fuselage numbers as indicated in the following Douglas Service Bulletins or All Operators Letters or later FAA-approved revisions:

Para. (A), below - S/B 52-139, dated April 28, 1975

Para. (B), below - AOL 10-814, dated May 9, 1975

Para. (C), below - S/B 52-140, dated April 30, 1975

Para. (D), below - S/B 52-139, dated April 28, 1975

To prevent inadvertent opening of Type I passenger doors (most forward left and right doors) accomplish the following:

(A) Compliance required not later than 48 hours after the effective date of this AD, unless already accomplished either within 10 days prior to the effective date of this AD, or in accordance with that telegraphic AD dated April 24, 1975, amended April 28, 1975.

(1) Conduct the following one-time inspection of the Type I doors:

(a) Inspect the close (down) lock torque tube spline for damage. Repair or replace, if required.

(b) Visually inspect the door close (down) lock and spring for general condition and insure the spring is not riding over the flange of the drive spline.

(c) Functionally operate the door to insure that the close (down) lock is properly engaged.

(d) Inspect the air storage bottle control valve lever to insure that it is in its normal operating (stowed) position.

(2) Prior to each flight, except as provided herein, accomplish the following on the Type I doors:

(a) After the door is closed, and the inside operating handle is positioned in the neutral position, inspect or check the close (down) lock to insure that it is properly engaged.

(b) The inspection or check required by (A)(2)(a), above, does not have to be accomplished if it can be verified that the door handle has not been disturbed subsequent to the accomplishment of the inspection or check required by (A)(2)(a), above. Any method used to insure that the operating handle has not been disturbed must not interfere with normal and emergency operation of the door.

(c) The inspection or check required by (A)(2)(a), above, does not have to be accomplished if it can be verified during the inspection required by (A)(1), above, that a production P/N ABA8025-1 6 1/2 coil close (down) lock spring is installed, and the conditions inspected in (A)(1), above, are satisfactory.

(d) The flight crew will be advised after the inspection or check required by (A)(2)(a), above, is satisfactorily accomplished.

(e) The inspection or check required by (A)(2)(a), above, does not have to be accomplished, provided:

(i) The close (down) lock torque tube spline is reinspected for damage; and repaired or replaced, if required.

(ii) There are no less than 3 1/2 coils in the cut-off P/N ABA8025-1 close (down) lock spring.

(iii) A P/N WBA7003-7 washer is installed at the forward end, and a P/N WBA7003-5 washer is installed at the aft end, of the close (down) lock spring. (Reference Douglas Service Bulletin No. 52-139, dated April 28, 1975). And

(iv) After the P/N WBA7003-5 and -7 washers have been installed, the door is functionally operated to insure that the close (down) lock is properly engaged.

(3) Any inspection must be performed by the holder of a mechanic or repairman certificate, or by a person under the direct supervision of the holder of such certificate. A check may be performed by qualified or trained personnel designated by the operator for the purpose of performing the checks.

(4) Operators shall advise flight crews and cabin attendants of the foregoing procedures by the most immediate and practicable means.

(B) Compliance required within seven days after the effective date of this AD, unless already accomplished.

Inspect the torque tube close (down) locks on the Type I doors to insure that the P/N ABA8023-1 slide catch and P/N ABA8024-1 stop plate are installed on the left hand door, and the P/N ABA8023-2 slide catch and P/N ABA8024-2 stop plate are installed on the right hand door, in accordance with Douglas All Operators Letter No. 10-814, dated May 9, 1975, or later FAA-approved revisions.

(C) Compliance required as indicated, unless the modification required by (C)(2) is already accomplished.

(1) Within the next 1500 hours' time in service after the effective date of this AD, and thereafter at intervals not to exceed 500 hours' time in service from the last inspection,

(a) Reinspect the air storage bottle control valve lever (reference (A)(1)(d), above) to insure that it is in its normal operating (stowed) position; or

(b) Verify that the door handle has not been disturbed subsequent to the accomplishment of the inspection or check required by (A)(2)(a), above. Any method used to insure that the operating handle has not been disturbed must not interfere with normal and emergency operation of the door.

(2) Within the next 4500 hours' time in service after the effective date of this AD,

(a) Install retention springs on the Type I door air storage bottle control valve lever in accordance with Douglas Service Bulletin No. 52-140, dated April 30, 1975, or later FAA-approved revisions; or

(b) Install a new design Type I door air storage bottle control valve in accordance with Douglas Service Bulletin No. 52-154, Revision 1, dated March 1, 1976, or later FAA-approved revisions.

(D) Compliance required within the next 3000 hours' time in service after the effective date of this AD, unless already accomplished.

(1) Remove the Type I door cut-off P/N ABA8025-1 close (down) lock springs and P/N WBA7003-5 and -7 washers, and install production P/N ABA8025-1 6 1/2 coil close (down) lock springs on the torque tube.

(2) Following installation of the new springs, recheck the engagement of the close (down) lock, and adjust if required, in accordance with Douglas Service Bulletin No. 52-132, Revision 1, dated February 21, 1975, or later FAA-approved revisions.

(E) The Chief, Aircraft Engineering Division, FAA Western Region, may approve equivalent inspections and installations or alternate design modifications upon submittal of substantiating data.

(F) Airplanes may be flown to a base for performance of maintenance required by this AD per FAR's 21.197 and 21.199, provided that, with respect to the door(s) identified as in need of maintenance, the emergency evacuation slides or slide/rafts will be either removed or deactivated.

This supersedes the telegraphic AD adopted April 24, 1975, amended April 28, 1975, and distributed by telegrams dated April 24, 1975 and April 28, 1975.

Amendment 39-2218 became effective May 30, 1975.

Amendment 39-2377 became effective October 14, 1975.

This amendment 39-2539 becomes effective March 17, 1976.


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