Copy · TR 28-1 · 2 pages

© Embraer S.A. Filed by the FAA in regulations.gov docket FAA-2016-9507, the docket of AD 2017-10-04. Not covered by OpenAirDocs’ CC0 dedication.

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EMB-120 BRASILIA MRB REPORT (MRB-HI-200) MRB - TEMPORARY REVISION N° 28-1 TO: HOLDERS OF PUBLICATION No. MRB-HI-200 - "MAINTENANCE REVIEW BOARD", APPLICABLE TO EMB-120 "BRASILIA" AIRCRAFT.

This Temporary Revision (TR) is to address technical changes on MRB-HI-200 Revision 27, SECTION 6 - PART C: LANDING GEAR LIFE-LIMITED COMPONENTS/PARTS.

Reason: To add life limited part numbers to the MLG and NG in the EMB-120 MRB-HI-200 Section 6 Part C (Airworthiness Limitations), based on administrative re-identification.

FILLING INTRUCTIONS: Insert this TR, facing on pages 6.II.1 (MLG) and 6.II.2 (NLG) .

PNs to be included for MLG:

PART NUMBERD DESCRIPTION LIMITS AS PER CERTIFICATION NOTES

CTA/FAA DGAC CAA (UK) IAC - AR 19699-001-00 PIN DRAG STRUT, LOWER 104, 054LD 83,243LD 69,369LD 69,369LD (1) / (3) 19429-000-00 PISTON TUBE 30, 000LD 24,000LD 20, 000LD 20,000LD (1) / (2) /(3) 19946-001-00 PIN LEG HINGE 90,000LD 72,000LD 60,000LD 60,000LD (1) / (3) 20030-001-00 PIN TORQUE LINK 90, 000LD 72,000LD 60,000LD 60, 000LD (1) / (3) 19437-000-00 DRAG STRUT, UPPER HALF 104, 054LD 83,243LD 69,369LD 69,369LD (1) / (3) 20031-001-00 PIN DRAG STRUT HINGE 104, 054LD 83, 243LD 69,369LD 69,369LD (1) / (3) PNs to be included for NG:

PART NUMBERD DESCRIPTION LIMITS AS PER CERTIFICATION NOTES

CTA/FAA DGAC CAA (UK) IAC - AR 19414-000-00 PISTON TUBE 90, 000LD 72,000LD 60,000LD 60,000LD (1) /(3) 19919-000-00 PIN LEG HINGE 90, 000LD 72, 000LD 60,000LD 69, 000LD (1) / (3) NOTE:

(1): These life limits are based on the fatigue tests already concluded.

(2): After accomplishment of SB 120-032-0514, Life Limit becomes 90,000LD (CTA/ FAA), 72,000LD (DGAC), and 60,000LD (CAA).

(3): Part Number, life limit based on previous part number (reidentification for administrative purpose).

1R28-1 DATE: 17 MAY 2016 PAGE: 1 of 2

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EMB-120 BRASH12 KgB REPORT

THIS PAGE INTENTIONALLY LEFT BLANK TR28-1 DATE: 17 MAY 2016 PAGE: 2 of 2