N608AE

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,081 hrs · 23,842 cycles

DURING PREFLIGHT INSPECTION FOR FLIGHT 4091 THE EMERGENCY FLOOR STRIP LIGHTING WAS DISCOVERED TO BE INOPERABLE BETWEEN 8A AND 11A. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED AN OPERATIONAL CHECK PER EMB 145 AMM 33-50-00. NO DEFECTS NOTED THIS TIME. NO PARTS REMOVED OR REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE)

ABI - DURING AN IMBV INSPECTION OF AIRCRAFT, FOUND CORROSION ON THE GALLEY AREA FORWARD DIGITAL. PERFORMED AN NDT INSPECTION OF THE AREA WITH NO REJECTABLE INDICATIONS. FABRICATED A REPLACEMENT STRAP, TWO DOUBLERS AND A SHIM. WORK DONE IAW EMB 145 SRM 145/1142, REV 17, 53-21-10, GST-0623/02, ITEM 1, AND STANDARD SRM PRACTICES. (M)

Part: STRINGER — CHAFED (FUSELAGE)

DURING INSPECTION OF AIRCRAFT, FOUND EXTERNAL STRINGER 19L CHAFED. BLENDED CHAFE. FABRICATED TWO DOUBLER ANGLE 14.5 INCH BY 1.5 INCH, .050 INCH AND FOUR SHIMS 4.5 INCH BY .75 INCH, .080 INCH THICK IAW EMB 145 (SRM 145/1142 REV 17) 53-24-02, GST-0633/02, ETN EM53-020 AND STANDARD SRM PRACTICES. (M)

Part: STRINGER — CHAFED (FUSELAGE)

ABI - DURING INSPECTION OF AIRCRAFT, FOUND EXTERNAL STRINGER 19R CHAFED. BLENDED CHAFE, FABRICATED TWO DOUBLERS ANGLE 14.5 INCH BY 1.5 INCH, .050 INCH THICK, AND FOUR SHIMS 4.5 INCH BY .75 INCH .080 INCH THICK IAW EMB 145 SRM 145/1142 REV 17 53-25-02, GST-0633/02, ETN EMB53-00-020 AND STANDARD SRM PRACTICES. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

ABI - DURING AN IMBV INSPECTION OF AIRCRAFT, FOUND CORROSION ON THE GALLEY CENTER HAT BEAM. REMOVED CORRODED GALLEY CENTER HAT BEAM. INSTALLED NEW HAT BEAM IAW EMB 145 SRM/1142, REV 17, 51-20-03, 51-40-02, GST-0623/02, ITEM 7 SEP 0114/02 AND STANDARD SRM PRACTICES. (M)

Part: DOUBLER — CORRODED (FUSELAGE)

ABI - DURING AN IMBV INSPECTION OF AIRCRAFT, FOUND CORROSION, PREVIOUS REPAIR ON THE LEFT OMEGA BEAM AT FRAME 20. REMOVED PREVIOUS REPAIR, CORROSION LIMITED TO PREV REPAIR. FABRICATED A DOUBLER ANGLE AND FILLER. A PLATE AND TWO SHIMS. WORK DONE IAW EMB 145 SRM 145/1142 CHAPTER 53 REV 16, 53-21-10, AND STANDARD SRM PRACTICES. (M)

Part: STRUCTURE — CORRODED (GALLEY)

ABI - GALLEY AREA AFT DIGITAL HAS CORROSION. BLENDED OUT, PERFORMED NDT, AND TREATED FOR CORROSION IAW EMB 145 CPM 51-21-03, 51-21-04, 51-21-05, 51-21-06. (M)

Part: FRAME — CORRODED (CORRODED)

ABI - RIGHT HAT BEAM AT FRAME 22 HAS CORROSION. BLENDED AND NDT'D AND TREATED HAT BEAM AT FRAME 22 IAW EMB GST 0623/02. (M)

Part: BEAM — CORRODED (FUSELAGE)

ABI - FOUND LEFT OMEGA BEAM BETWEEN FRAME 24 AND 25 HAS CORROSION. BLENDED AND PERFORMED NDT INSPECTION AND TREATED FOR CORROSION IAW EMB GST 0623/02. (M)

Part: BEAM — CORRODED (FUSELAGE)

ABI - CENTER OMEGA BEAM BETWEEN FRAME 23 AND 25 HAS CORROSION. BLENDED, PERFORMED NDT AND TREATED FOR CORROSION IAW EMB GST-0623/02. (M)

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2

ABI - THIS IS A LEVEL 2 FINDING, CORROSION FOUND ALONG FUSELAGE SKIN EDGE JUST BELOW BATTERY COMPARTMENT ACCESS DOOR. BLENDED, INSPECTED DAMAGE AND IT WAS ACCEPTED AS IS IAW EMB GST 0623/02. (M)

Part: SILL — CORRODED (FUSELAGE)

ABI - RIGHT SILL BETWEEN FRAME 23 AND 29 HAS CORROSION. BLENDED OUT, PERFORMED NDT AND TREATED IAW EMB GST-0623/02. (M)

Part: WARNING SYSTEM — ACTIVATED (EICAS)

GRR - FLT 4405 - ON TAKEOFF ROLL OF 90 KNOTS HAD EICAS MESSAGE OF REV DISAGREE, RETURNED TO GATE FOR MAINTENANCE. NOTE THE MESSAGE WENT AWAY VERY QUICK. INSPECTOR AND OPS CHECK IAW AMM. COULD NOT DUPLICATE PROBLEM. AIRCRAFT RETURNED TO SERVICE. (M)

Part: ACTUATOR — MALFUNCTIONED (THRUST REVERSER)

SGF - FLT 3560 - ON TAKEOFF ROLL, HAD TR1 DISAGREE, ABORTED TAKEOFF AND RETURNED TO GATE. ENGINE 1 THRUST REVERSER PUT ON MEL AT THIS TIME. MAINTENANCE ADJUSTED UPPER AND LOWER T/R ACTUATORS ON NR 1 ENGINE IAW EMB MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: PRESSURE SWITCH — LEAKING (NR 1 HYD)

DFW - FLT 3418 - AIRCRAFT LOST ALL HYDRAULIC 1 SYSTEM QTY AND PRESSURE. REPLACED NR 1 HYD SYSTEM PRESSURE SWITCH IAW AMM. OPS CHECK GOOD. (M)

Part: ENGINE — LEAKING (NR 2) · airframe 4,220 hrs · 4,509 cycles

ORD - FLT 4249 - CREW ABORTED TAKEOFF FOR ENGINE NR 2 OIL PRESSURE WENT TO RED ON TAKEOFF ROLL. FERRY TO CMH. MAINTENANCE C/W ENGINEERING ORDERS EM-7900-010 AND EM-6900-011. INSTALLATION ON OIL PRESSURE RELIEF KIT AND SMART SENSOR (NEW PN 23073475A). OPERATIONAL AND LEAK CHECKS SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. (X)

Part: SIGN — MALFUNCTIONED (CABIN)

MGM - FLT 3684 - SERVICE DOOR EMERGENCY LIGHT INOPERATIVE. MAINTENANCE RESEATED CANNON PLUG FOR SERVICE DOOR LIGHT AND PERFORMED OPERATIONAL CHECK. COULD NOT DUPLICATE DISCREPANCY. AIRCRAFT WAS RETURNED TO SERVICE. (M)