N814AE

Part: ENGINE — VIBRATION (NR 2) · airframe 31,272 hrs · 27,033 cycles

NUMBER 2 ENG HIGH PRESS VIBRATION NEAR TOP OF AMBER DURING ENG START. ABORTED START, AOM PROCEDURE. COMPLIED WITH IAW AML PAGE 3662714 ITEM 4. R & R E2 IAW WORK CARD 71-000-00. OPERATIONS CHECKED GOOD, LEAK CHECKED GOOD & VIBRATION CHECKED GOOD.

Part: UNKNOWN — MALFUNCTIONED (INDICATION SYS) · airframe 30,871 hrs · 26,680 cycles

UPON GEAR RETRACTION NO HASH TRANSITION INDICATION WAS SEEN. PERFORMED LG EXTENSION & RETRACTION ELEC. OPERATIONS CHECKED IAW AMM 32-32-00. ALL LG INDICATIONS ARE OPERATIONAL IAW AMM 32-63-05.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 30,519 hrs · 26,302 cycles

EXIT EMER LIGHT OVER FLIGHT ATTENDANT SEAT DOES NOT ILLUMINATE. R & R NR 1 INVERTER IAW AMM 33-50-11. OPERATIONS CHECKED GOOD.

Part: RETAINING CLIP — BROKEN (FLASHLIGHT) · airframe 30,178 hrs · 25,947 cycles

CAPTAIN`S FLASHLIGHT HOLDER HAS A BROKEN RETAINING CLIP. R & R WITH SERVICEABLE CAPTAIN`S FLASHLIGHT ASSEMBLY IAW AMM 33 50 16, OPERATIONS CHECKED OK.

Part: O-RING — DAMAGED (BLEED AIR SYS) · airframe 30,090 hrs · 25,867 cycles

BLEED 1 LEAK WARNING DURING CLIMB AT 10,000 FT. IAW AOM CLOSED BLEED VLV & MSG EXTINGUISHED. R & R BLEED LINE O RINGS AT JOINT 19 IAW AMM 36-11-10, LEAK CHECKED GOOD.

Part: CRADLE — BROKEN (FLASHLIGHT) · airframe 29,646 hrs · 25,490 cycles

BRACKET ON FIRST OFFICER`S FLASHLIGHT CRADLE BROKEN. R&R FIRST OFFICER`S EMERGENCY FLASHLIGHT BASE IAW AMM 33-50-11. OPERATIONS CHECKED GOOD MEL RESTORED.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 29,376 hrs · 25,231 cycles

ENGINE 2 REV DISAGREE CAME ON DURING TAKEOFF. ABORTED TAKEOFF, DEFERRED IAW MEL 78-02.

Part: UNKNOWN — ODOR (CABIN) · airframe 28,749 hrs · 24,673 cycles

ELECTRICAL BURING ODOR COMING FROM ROW 7 AREA. INSPECTED AROUND ROW 7 AREA AND PSU PWLS. FOUND NO EVIDENCE OF ANY ELECTRICAL DEFECT WITH ACM ON/OFF IAW SRM 140 21-20-00.

Part: CRADLE — BROKEN (FLASHLIGHT) · airframe 27,944 hrs · 23,956 cycles

DURING B INSPECTION, FOUND THE REAR CABIN FLASHLIGHT BASE BROKEN. THE ACFT WAS REMOVED FROM SERVICE. R & R THE REAR CABIN FLASHLIGHT CRADLE IAW AMM 33-50-16. THE OPS CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 27,347 hrs · 23,454 cycles

DURING MAINTENANCE INSPECTION FOUND THE FORWARD LEFT EXTERIOR EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FORWARD LEFT EXTERIOR EMERGENCY LIGHT IAW EMB AMM 33-50-07. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · airframe 27,156 hrs · 23,296 cycles

DURING B INSPECTION FOUND THE SERVICE DOOR AFT SILL CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE SERVICE DOOR AFT SILL IAW EMB SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FRAME — CRACKED (FUSELAGE) · airframe 27,136 hrs · 23,279 cycles

FRAME 23 CRACKED BETWEEN STRINGERS 15 AND 16 RIGHT. REPAIRED FRAME IAW EO EM-53MR-1808.

Part: BRACKET — CORRODED (FUSELAGE) · airframe 27,156 hrs · 23,296 cycles

DURING B INSPECTION FOUND THE CARGO DOOR LOWER SILL CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FORWARD AND AFT ANGLE BRACKET IAW EMB SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — MISINSTALLED (CABIN) · airframe 27,156 hrs · 23,296 cycles

DURING B INSPECTION FOUND THE CABIN FLOOR EMERGENCY LIGHT STRIPS INSTALLED INCORRECTLY WITH THE ARROWS FORWARD OF EXIT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED TWO CABIN FLOOR EMERGENCY LIGHT STRIPS AND INSTALLED THEM INTO THEIR CORRECT POSITIONS IAW EMB 140 AMM 33-50-12. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE — DAMAGED (CABIN) · airframe 27,156 hrs · 23,296 cycles

DURING B INSPECTION FOUND THE EMERGENCY LIGHT STRIP WIRE DAMAGED AT FRAME 28 ADJACENT TO WIRE BUNDLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED EMERGENCY LIGHT STRIP WIRE THAT HAD DAMAGE AT FRAME 38 ADJACENT TO WIRE BUNDLE IAW EMB140 AWM 20-21-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SEAL — TORN (FUSELAGE) · airframe 27,156 hrs · 23,296 cycles

DURING B INSPECTION FOUND THE MAIN PASSENGER DOOR FRAME SEAL TORN AT NUMEROUS AREAS. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE MAIN PASSENGER DOOR FRAME SEAL FOR BEING TORN AT NUMEROUS AREA'S IAW EMB 140 AMM 53-21-01. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — BROKEN (CABIN) · airframe 27,156 hrs · 23,296 cycles

DURING MAINTENANCE INSPECTION FOUND THE LEFT FLOOR EMERGENCY LIGHT STRIP EXTRUSION NR 3 BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT FLOOR EMERGENCY LIGHT STRIP EXTRUSION NR 3 IAW EMB 140 AMM 33-50-12. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 26,798 hrs · 22,964 cycles

DURING B INSPECTION FOUND THE MAIN DOOR EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE MAIN DOOR EMERGENCY LIGHT ASSEMBLY; PART NUNMBER B-6245-305, IAW EMB 140 AMM 33-50-07-000-802-A AND THE NR 1 BATTERY AND BATTERY CHARGER 33-50-07-400-802-A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BRACKET — BROKEN (FLASHLIGHT) · airframe 26,599 hrs · 22,763 cycles

DURING MAINTENANCE INSPECTION FOUND THE FLASHLIGHT BRACKET ABOVE THE FLIGHT ATTENDANT’S SEAT BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FLASHLIGHT BRACKET ABOVE THE FLIGHT ATTENDANT’S SEAT. THE OPERATIONAL CHECK WAS GOOD IAW EMB 140 AMM CHAPTER 33-50-16. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 26,559 hrs · 22,724 cycles

DURING B INSPECTION FOUND THE EMERGENCY LIGHTS ON MAIN DOOR AND ENTRANCE WAY INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 1 EMERGENCY LIGHTS POWER SUPPLY AND BATTERY IAW AMM 33-50-04. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,450 hrs · 22,615 cycles

DURING B INSPECTION FOUND THE AFT CABIN EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AFT CABIN EMERGENCY LIGHT LAMPS IAW EMB 145 AMM 33-50-06-000-801-A AND 33-50-06-400-801-A. THE OPERATIONAL CHECK WAS GOOD.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 26,039 hrs · 22,203 cycles

DURING THE OPS CHECK OF EMERGENCY LIGHTS, FOUND MAIN DOOR EMERGENCY LIGHT AND PASSENGER ENTRY EMERGENCY LIGHT FAILED TO ILLUMINATE. AIRCRAFT REMOVED FROM SERVICE. DURING TROUBLESHOOTING, PIN "D" ON CONNECTOR P8011 WAS FOUND TO BE NOT SEATED FULLY. SEATED PIN, OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: ENGINE — DEFECTIVE (NR 1) · airframe 25,174 hrs · 21,446 cycles

DURING MAINTENANCE INSPECTION FOUND AIR CONDITIONING PACK SYSTEM, LEFT PACK OIL SMELL WITH PACK ON NO OIL SMELL WITH PACK OFF. THE AIRCRAFT WAS REMOVED FROM SERVICE. E1 CAUSES OIL SMELL IN COCKPIT. REMOVED AND REPLACED THE ENGINE IAW MTX WC 71-000-00. THE OPERATIONAL CHECKS AND LEAK CHECKS WERE GOOD. NO DEFECTS NOTED AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 25,141 hrs · 21,411 cycles

ON FLIGHT 4481 THE CREW REPORTED, SMELLED OIL WITH NR 1 PACK ON. TURNED OFF PACK & SMELL WENT AWAY. DEFERRED PER MEL 21- 29. AUTH # 030976D-C. THE AIRCRAFT WAS REMOVED FROM SERVICE. USING APU BLEED AIR PERFORMED OPERATIONAL CHECK OF NR 1 PACK IAW AMM 21-51-00 & ETN EM-72-034 NO OIL SMELL NOTED. MEL ITEM RESTORED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: UNKNOWN — CONTAMINATED (AC SYSTEM) · airframe 24,953 hrs · 21,255 cycles

ON FLIGHT 2712 PASSENGER REPORTED MUSKY SMELL ON CLIMBOUT AND DESCENT, CREW CONCURS. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED EMB-140 FIM TASKS 21-20-00-810-801-A AND 21-20-00-810-803-A, AND PERFORMED DECONTAMINATION PROCEDURE OF THE AIR CONDITIONING SYSTEM IAW EMB-140 AMM 21-20-00-100-804-A. NO FURTHER ODOR WAS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: HANDLE — LACK OF LUBE (PAX DOOR) · airframe 24,879 hrs · 21,199 cycles

FLIGHT 3262, THE CREW REPORTED THE MAIN CABIN DOOR WOULD NOT CLOSE. AIRCRAFT REMOVED FROM SERVICE. LUBRICATED MAIN CABIN DOOR HANDLE. OPS CHECKED GOOD IAW AMM 52-18-00. AIRCRAFT RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 24,875 hrs · 21,196 cycles

ON FLIGHT 4106 THE CREW REPORTED THE FIRST OFFICER’S FLASHLIGHT WAS INOPERABLE. REMOVED AND REPLACED THE FLASHLIGHT IAW AMM 33-50-16. MEL CLEARED MIC SHEET CLEARED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: DUCT — BLOWN (CABIN) · airframe 23,856 hrs · 20,312 cycles

DURING TAXI FLIGHT ATTENDANT REPORTED SMELLING SMOKE NEAR ROW 8. RETURNED TO GATE, OCE BACK AT GATE AND WALKING BACK TO CABIN IT WAS NOTICEABLY HOT. TEMPERATURE SELECTOR FOR CABIN WAS IN FLIGHT ATTENDANTS CONTROL THE WHOLE TIME IN FULL COLD. INSPECTED AND FOUND BLOWN DUCT UNDERNEATH CABIN FLOOR SHOOTING CONDENSED MIST. F/A HAD SET TO FULL COLD. PERFORMED OPS CHECK IN DIFF TEMP SETTINGS AND WITH ENGINE BLEED WITH RE-CONNECTED DUCT. NO DEFECTS/SMELLS NOTED. PER EMB 140 AMM 21-54-00. CC 665430.

Part: INVERTER — MALFUNCTIONED (CABIN) · airframe 23,831 hrs · 20,293 cycles

ON FLIGHT 4060 THE CREW REPORTED THE RIGHT INTERIOR AFT OVERWING EMERGENCY EXIT MARKER DID NOT ILLUMINATE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AC/DC INVERTER ASSEMBLY NR 5 IAW EMB AMM 33-50-11. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 23,569 hrs · 20,054 cycles

ON FLIGHT 4515 THE CREW REPORTED THAT WHILE LEVELING OFF AT FL360 HEARD A LOUD POP FOLLOWED BY THE CAPTAIN’S OUTER PAIN ON WINDSHIELD CRACKED. ALSO RECEIVED EICAS MESSAGE FOR ICE DET 1 FAIL. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED CAPTAINS WINDSHIELD IAW EMB 140 AMM 56-10-01. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 22,638 hrs · 19,346 cycles

DURING MAINTENANCE BASE VISIT FOUND THE ASILE OVERHEAD EMERGENCY SIGN AT SERVICE ENTRANCE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. RECONNECTED CONNECTOR AT AISLE OVERHEAD EMERGENCY EXIT MARKING SIGN AT SERVICE ENTRANCE IAW EMB 140 AMM 33-50-14. NO PARTS REMOVED OR REPLACED. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 22,638 hrs · 19,346 cycles

DURING MAINTENANCE BASE VISIT FOUND THE RIGHT OVERWING AFT EMERGENCY ESCAPE HATCH EXIT SIGN INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. RECONNECTED CONNECTOR AT RIGHT AFT EMERGENCY ESCAPE HATCH MARKING SIGN AW EMB 140 AMM 33-50-14. NO PARTS REMOVED OR REPLACED. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FUSE — BLOWN (BATTERY CHARGER) · airframe 22,101 hrs · 18,896 cycles

ON FLIGHT 4060 THE LEFT EXTERNAL FORWARD EMERGENCY LIGHT FAILED TO ILLUMINATE AND THE FORWARD CEILING AISLE EMERGENCY LIGHT FAILED TO ILLUMINATE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED F1 FUSE ON NR 1 EMERGENCY BATTERY CHARGER ASSEMBLY IAW CMM 25-60-03 AND EMB AMM 33-50-04. THE OPERATIONAL CHECK WAS GOOD IAW EMB AMM 33-50-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 21,153 hrs · 18,043 cycles

ON FLIGHT 4263 DURING THE TAKEOFF THE CREW REPORTED A STRONG OILY ODOR IN THE COCKPIT. BLEEDS OPEN AND BOTH PACKS WERE ON. THE FLIGHT ATTENDANT REPORTED THE CABIN SMELLED NORMAL. THE AIRCRAFT WAS REMOVED FROM SERVICE. ENGINE RUNS COMPLETED IAW ETN EM-72-034 R4. NO DEFECTS NOTED. NO PARTS REMOVED OR REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 20,409 hrs · 18,127 cycles

DURING MAINTENANCE BASE VISIT FOUND THE AFT WING EMERGENCY LIGHTS TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 4 BATTERY AND CHARGER. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 20,138 hrs · 17,167 cycles

FOR FLIGHT 4684 THE FLIGHT ATTENDANTS EMERGENCY FLASHLIGHT ABOVE SEAT NEAR THE FORWARD GALLEY WAS DISCOVERED NOT TO BE WORKING AND THE FLASHLIGHT BRACKET IS BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FLASHLIGHT ASSEMBLY AND CRADLE IAW 140 AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — FAILED (CABIN) · airframe 20,023 hrs · 17,068 cycles

DURING THE PS-2 CHECK FOUND THE NR 1 EMERGENCY BATTERY AND CHARGER ASSEMBLY TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 1 BATTERY AND CHARGER ASSEMBLY EMERGENCY LIGHTING SYSTEM IAW WC 33-700-19. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS)

DURING INSPECTION, FOUND THE RIGHT OVERWING INTERNAL EMERGENCY LIGHT INOPERABLE. AIRCRAFT REMOVED FROM SERVICE. REPLACED LIGHT ASSEMBLY IAW AMM 33-50-00. OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONNECTOR — DIRTY (EMERGENCY LIGHTS) · airframe 18,960 hrs · 16,164 cycles

DURING MAINTENANCE INSPECTION FOUND THE RIGHT EMERGENCY EXIT UPPER EXIT SIGN WILL NOT ILLUMINATE. REMOVED AIRCRAFT FROM SERVICE. CLEANED THE CONNECTOR FOR THE RIGHT EMERGENCY EXIT UPPER EXIT SIGN EMB 140 AMM 33-50-00. NO PARTS REMOVED OR REPLACED. OPERATIONAL CHECK IS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SPLICE — DIRTY (CABIN) · airframe 18,883 hrs · 16,104 cycles

ON FLIGHT 4191 THE CREW REPORTED THAT THE LIGHTED EMERGENCY EXIT MARKER ON THE RIGHT INTERIOR EXIT HATCH OVER THE WING DOES NOT ILLUMINATE. AIRCRAFT REMOVED FROM SERVICE. CLEANED ELECTRICAL CONNECTOR CONTACTS OF THE RIGHT OVERWING HATCH LIGHTED EMERGENCY MARKER REUSABLE SPLICES. AIRCRAFT RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,913 hrs · 15,139 cycles

DURING HMBV INSPECTION, FOUND CENTER OMEGA BEAM AT FRAME 24 CORRODED BEYOND MANUAL LIMITS UNDER CARBON CROSSBEAM. OMEGA BEAM REPAIRED IAW EMBRAER SRM 53-00-10 FIG 203. AIRCRAFT WAS RETURNED TO SERVICE.

Part: FUSE — BLOWN (EMERGENCY LIGHTS) · airframe 15,204 hrs · 12,906 cycles

ON FLIGHT 3900, CREW REPORTED EMERGENCY LIGHT INOP AT ROW 11C. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED EMERGENCY BATTERY POWER SUPPLY FUSE IAW CMM 25-60-03. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 13,063 hrs · 11,383 cycles

LEFT OMEGA BEAM INBOARD SIDE CORRODED AT FRAME 20 CROSSBEAM. REMOVED DAMAGE AND INSTALLED DOUBLER IAW EMB SRM 53-00-01, FIGURE 201. AIRCRAFT RETURNED TO SERVICE.

Part: SILL — CORRODED (ZONE 200) · corrosion level 2 · airframe 13,063 hrs · 11,383 cycles

SERVICE DOOR CENTER SILL CORRODED BETWEEN FRAME 20 AND FRAME 22. REMOVED AND REPLACED SILL IAW EMB SRM 51-40-02. RETURNED AIRCRAFT TO SERVICE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 12,692 hrs · 11,144 cycles

FOUND EMERGENCY BATTERIES FAILED TO TEST. REMOVED AND REPLACED EMERGENCY BATTERIES IAW EMB AMM 33-50-04. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN)

FLT 3197 - OVERHEAD EMERGENCY EXIT SIGN ROW 11 WILL NOT ILLUMINATE. REPLACED BATTERY AND BATTERY POWER SUPPLY OVER ROW 14. OPERATIONAL CHECK GOOD. POWER SUPPLY P/N OFF 11-0049, S/N OFF 12700. AIRCRAFT RETURNED TO SERVICE. (M)

Part: FLAPPER VALVE — BROKEN (RT WING)

CONTROL TOWER REPORTED VAPOR TRAIL COMING FROM RT WING. REMOVED AND REPLACED THE RT FUEL TANK FLAPPER VALVE AT RIB 19. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (K)

Part: SILL — CORRODED (FUSELAGE)

THE CARGO DOOR OPENING LOWER SILL WAS FOUND CORRODED. REMOVED EXISTING LOWER SILL AND INSTALLED NEW SILL IAW EMB 145 SRM, SRM EMB-145/1142 REV 29) CHAPTERS 51-40-02 AND 51-20-03. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

ABI - DURING AN INSPECTION, THE LEFT OMEGA BEAM BETWEEN FRAMES 24 AND 25 WAS FOUND CORRODED. PERFORMED CUT OUT OF THE OMEGA BEAM TO REMOVE THE CORROSION. FABRICATED AN EXTERNAL ANGLE, FILLER AND TWO SHIMS. REPAIR DONE IAW EMB 145 SRM, SRM EMB 145/1142 REV 29, CHAPTER 53-22-10 FIG 202. (M)

Part: ENGINE — FAILED (NR 1)

DURING CLIMB AT FL290, CREW REPORTED A NR 1 ENGINE VIBRATION FOLLOWED BY A PUFF OF SMOKE IN THE COCKPIT. POWER WAS REDUCED AND A/C WAS DIVERTED TO CLT. DURING APPROACH WHEN NR 1 WAS BROUGH OUT OF IDLE CREW REPORTED MAX VIBRATION AND LOSS OF OIL PRESSURE. ENGINE WAS SHUT DOWN AND AN EMERGENCY WAS DECLARED. AIRCRAFT WAS LANDED SAFELY. REPLACED NR 1 ENGINE ASSEMBLY. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: CONTROL UNIT — INOPERATIVE (HORIZONTAL STAB)

ORD - FLT 4303 - DURING DESCENT, CREW REPORTED PITCH TRIM ONE AND TWO TO BE INOPERATIVE WITH NO EICAS MESSAGE. MAINTENANCE COMPLIED WITH ETN EB 27-022 AND REMOVED AND REPLACED THE HORIZONTAL STABILIZER CONTROL UNIT AND HSCU SHOCK MOUNTS. OPERAITONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: STRINGER — CHAFED (FUSELAGE)

ABI - DURING AN MBV INSPECTION, STRINGER 19R WAS FOUND CHAFED AT FRAME 53. BLENDED THE CHAFED AREA AND PERFORMED NDT INSPECTION. FABRICATED A REPAIR ANGLE SHIMS. REPAIR DONE IAW EMB SRM EMB 145/1142 REV 21, CHAPTER 53-241-02 FIGURE 201. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

ABI - DURING AN MBV INSPECTION, THE LEFT OMEGA BEAM AT FRAME 20 WAS FOUND TO BE CORRODED BELOW SRM LIMITS. CUTOUT DAMAGED SECTION OF LEFT OMEGA BEAM CLEANED AND TREATED THE REPAIR AREA. FABRICATED AN EXTERNAL ANGLE, FILLER AND TWO SHIMS. REPAIR DONE IAW EMB SRM, EMB 145/1142 REV 22, CHAPTER 53-21-10 FIG 201, SHEET 1 AND CPM 51-61-00. (M)

Part: STRINGER — CHAFED (FUSELAGE)

ABI - DURING AN MBV INSPECTION, FOUND STRINGER 19L WAS CHAFED AT FRAME 53. BLENDED THE CHAFED AREA AND PERFORMED NDT INSPECTION. FABRICATED TWO REPAIR ANGLES AND SHIMS. REPAIR DONE IAW EMB STATEMENT IC2003-145/2225-A AND SRM, SRM EMB 145/1142 REV 21, CHAPTER 53-24-01 FIGURE 201. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

ABI - DURING AN MBV INSPECTION, THE LEFT OMEGA BEAM AT FRAME 20 WAS FOUND TO BE CORRODED BELOW SRM LIMITS. CUT OUT DAMAGED SECTIN OF OMEGA BEAM, CLEANED AND TREATED THE REPAIR AREA. FABRICATED AND EXTERNAL ANGLE, ANGLE, FILLER, AND TWO SHIMS. REPAIR DONE IAW EMB SRM 53-21-10 AND CPM 51-61-00. (M)

Part: WINDSHIELD — FAILED (COCKPIT)

ORD - FLT 4148 - CREW REPORTED THE CAPTAINS WINDSHIELD SHATTERED IN FLIGHT, OUTER PANE ONLY. MAINTENANCE REMOVED AND REPLACED THE CAPTAINS WINDSHIELD IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)