N732DH

Part: UNKNOWN — LEAKING (NR 2 ENGINE) · airframe 13,742 hrs · 12,418 cycles

NR 2 SHUTDOWN DUE TO A LOUD POP FOLLOWED BY ENGINE OIL QUANTITY DROPPING TO 3 QUARTS, ITT IN AMBER RANGE EXCEEDING 930 DEGREES, AIRSPEED 280 KNOTS, FLIGHT LEVEL 350. MULTIPLE EICAS MESSAGES, PUNGENT WHITE SMOKE ENTERED CABIN, DISSIPATED AFTER SHUTDOWN OF NR 2 PACK AND BLEEDS. REMOVED AND REPLACED NUMBER 2 ENGINE IAW AMERICAN EAGLE WORK CARD - OPERATIONAL CHECK GOOD - RETURNED AIRCRAFT TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CENTER OMEGA BEAM AT FRAME 25 WAS FOUND CORRODED. CUT OUT A SECTION OF THE OMEGA BEAM TO REMOVE DAMAGE. FABRICATED A REPAIR ANGLE, FILLER AND SHIMS. REPAIR DOEN IAW EMB 145SRM (SRM EMB 145/1142 REV 27) CHAPTER 53-22-10, FIG 203. (SW21200500268)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CORROSION WAS FOUND ON A PREVIOUS REPAIR ON THE LT OMEGA BEAM AT FRAME 20. REMOVED RPREVIOUS REPAIR. FABRICATED A DOUBLER ANGLE, FILLER, REINFORCEMENT PLATE AND 2 SHIMS. REPAIR DONE IAW EMB 145 SRM (SRM 145/1142, CHAPTER 53, REV 27) 53-21-10 ITEM 2 FIGURE 201 AND STANDARD SRM PRACTICES.

Part: STRINGER — CHAFED (FUSELAGE)

ABI - DURING AN IMBV INSPECTION, STRINGER 19R WAS FOUND CHAFED. BLENDED THE CHAFED AREA AND PERFORMED AN EDDY CURRENT INSPECTION WITH NO REJECTABLE INDICATIONS. FABRICATED A REPAIR ANGLE AND SHIMS. REPAIR DONE IAW EMB REPAIR STATEMENT IC2003-145/3093A DATED SEPT 16, 2003 AND EMB 145 SRM, SRM EMB 145/1142 REV 27, CHAPTER 53-24-02. (M)

Part: SILL — CORRODED (SERVICE DOOR)

ABI - DURING AN IMBV INSPECTION, THE SERVICE DOOR CENTER SILL WAS FOUND CORRODED. REMOVED DAMAGED SILL AND INSTALLED NEW SILL IAW EMB REPAIR STATEMENT IC 2003/145-0818 DATED MARCH 6, 2003, AND AMERICAN EAGEL ENGINEERING TECHNICAL NOTICE EB 53-009. (M)

Part: BEAM — CORRODED (GALLEY)

DURING AN IMBV INSPECTION THE GALLEY CENTER BEAM WAS FOUND CORRODED. CUTOUT A SECTION OF THE DAMGAED AREA. FABRICATED A U SHAPE DOUBLER. REPAIR DONE IAW EMB 145 SRM, SRM 145/1142 REV 27, CHAPTER 53-21-10 PARA 5 FIG 204 SHEET 2. (M)

Part: FLOOR SUPPORT — CORRODED (GALLEY)

DURING AN IMBV INSPECTION, THE FORWARD GALLEY FLOOR DIGITAL WAS FOUND CORRODED. CUT OUT A DAMAGED SECTION FROM EXISTING DIGITAL AND CLEANED AREA. FABRICATED TWO REPAIR DOUBLERS AND SHIMS. REPAIR DONE IAW EMB 145 SRM, SRM 145/1142 REV 27, CHAPTER 53-21-10 AND 51-40-06. (M)

Part: FRAME — BENT (APU COWLING)

APU COWLING INTERIOR FORWARD FRAME IS BENT ABOVE THE TOP LEFT MOUNT HOLE, RECONTOURED FORWARD FRAME, PERFORMED NDT, NO DEFECTS. DONE IAW SRM AND MFG GST.

Part: SKIN — GOUGED (FUSELAGE)

THREE GOUGES BETWEEN FRAMES 15-16, BETWEEN STRINGERS 16L AND 17L. (SUP) BLENDED GOUGES, PERFORMED NDT WITH NO DEFECTS. GOUGES ACCEPTED AS IS IAW MFG GST.

Part: SKIN — GOUGED (PAX DOOR)

GOUGE ON FORWARD EDGE OF MAIN DOOR SKIN. BLENDED GOUGE, PERFORMED NDT, NO DEFECTS. GOUGED ACCEPTED AS IS IAW MFG GST.

Part: STRUCTURE — GOUGED (FUSELAGE)

GOUGE BETWEEN JUNCTION 1 AND FRAME 14, ALONG STRINGER 15L. BLENDED GOUGE, PERFORMED NDT, NO DEFECTS. ACCEPTED AS IS IAW MFG GST.

Part: SKIN — GOUGED (FUSELAGE)

GOUGE IN FUSELAGE SKIN BETWEEN FRAMES 71 AND 72 AND STRINGERS 16R AND 17R. BLENDED GOUGE, PERFORMED NDT WITH NO DEFECTS. GOUGE ACCEPTED AS IS IAW MFG GST.

Part: STRUCTURE — GOUGED (FUSELAGE)

GOUGE BETWEEN FRAMES 16-17 BETWEEN STRINGERS 16L AND 17L. BLENDED GOUGE, PERFORMED NDT, NO DEFECTS. ACCEPTED AS IS IAW MFG GST.

Part: SKIN — GOUGED (LT WING)

LEFT NR 1 LEADING EDGE GOUGED 11 INCH INBOARD OF LANDING LIGHT LENS COVER. BLENDED GOUGE, PERFORMED NDT, NO DEFECTS. ACCEPTED AS IS IAW MFG GST.

Part: FIRE WARNING — FALSE ACTIVATION (COCKPIT)

RDU - FLT 4549 - ON CLIMB-OUT, CREW HAD CARGO COMPARTMENT SMOKE WARNING AND DISCHARGED FIRE BOTTLES. DECLARED EMERGENCY AND RETURNED TO RDU. NO FIRE NOTICED. REPLACED CARGO FIRE BOTTLES. PERFORMED SYSTEMS OPS. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SMOKE — DETECTED (COCKPIT)

LGA - FLT 4521 - DURING INITIAL POWER UP ON AIRCRAFT WITH BATTERY AND AVIONICS SWITCHES ON, SMOKE WAS OBSERVED POURING OUT OF THE CENTER CONSOLE. MAINTENANCE COULD NOT DUPLICATE DISCREPANCY. PERFORMED APU START AND RAN ELECTRICAL SYSTEM AND FOUND NO EVIDENCE OF SMOKE. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: STRUCTURE — LEAKING (FUSELAGE)

LGA - FLT 4559 - DURING CLIMB, CREW REPORTED A PRESSURIZATION LEAK IN THE FORWARD NOSE GEAR AREA. CABIN PRESSURE STARTED TO CLIMB TO 6 PSI AT 5000 FEET. MAINTENANCE COULD NOT DUPLICATE DISCREPANCY. OPERATIONAL CHECK IAW EMB MM 21-31-00 WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)