N816AE

Part: O-RING — LEAKING (NR 2 BLEED) · airframe 34,358 hrs · 29,475 cycles

ON DEPARTURE AT 1000' AGL AFTER SELECTING CLIMB POWER #2 BLEED LEAK ILLUMINATED DECLARED EMERGENCY AND RETURNED TO KALO-C/A-REMOVED AND REPLACED BLEED DUCT O-RINGS AT JOINTS 14,18,20 IAW EMB 140 AMM 36-11-10. GROUND RAN AIRCRAFT, NO LEAKS NOTED AND NO BLEED LEAK MESSAGES POSTED.

Part: FAN — DIRTY (E&E BAY) · airframe 33,877 hrs · 28,987 cycles

STRONG ELECTRICAL SMELL IN COCKPIT AFTER LANDING. C/A-PERFORMED FIM TASK PROCEDURES IAW 21-20-00-810-801A FOR STRONG ELECTRICAL SMELL. FOUND BOTH FWD AVIONICS FANS DIRTY CLEANED AND PERFORMED OPERATIONAL CHECK IAW 21-26-00 OCK GOOD. NO FURTHER DEFECTS NOTED.

Part: CRADLE — INOPERATIVE (AFT FLASHLIGHT) · airframe 33,810 hrs · 28,901 cycles

AFT CABIN FLASHLIGHT WILL NOT STAY IN HOLDER-C/A-REMOVED AND REPLACED AFT CABIN FLASHLIGHT HOLDER IAW AMM 33-50-16 OPC GOOD

Part: INSULATION — LOOSE (E&E BAY) · airframe 33,139 hrs · 28,179 cycles

SPS ADVANCED IN FLIGHTT NUMEROUS TIMES. C/A-TROUBLESHOT PER FIM 34-22-00. FOUND INSULATION BLANKET LOOSE IN FWD ELECTRONIC BAY AND TWO DROPS OF WATER IN NR 1 PITOT DRAIN TUBE. RESECURED INSULATION BLANKET IAW AMM 25-81-01 AND DRAINED WATER FROM NR 1 PITOT DRAIN TUBE IAW AMM 34-13-00. PERFORMED PITOT 1,2, AND 3 SYSTEM AIRSPEED PRESSURE TEST. ADJUSTED AIRSPEED TO 300 KNOTS AND VERIFIED ALL 3 SYSTEMS READ THE SAME AT 300 KNOTS AND NO LEAKS AFTER ONE MINUTE IAW AMM 34-13-00. ALL SYSTEMS OPS CHECK GOOD AT THIS TIME.

Part: ANTI-ICE VALVE — FAILED (WING) · airframe 32,212 hrs · 27,307 cycles

ANTI ICE FAIL AND WING ANTI ICE FAIL IN ICING CONDITIONS-C/A-REMOVED AND REPLACED WING 1 A/I VLV IND RELAY K0435 IAW EMB 140 AMM 20-13-02.NO DEFECTS NOTED,REF LOG PAGE 4400635 ITEM 1 FOR OPS CHECK

Part: SMOKE DETECTOR — DEFECTIVE (CARGO BAY) · airframe 31,935 hrs · 27,071 cycles

DURING THE FIRE DETECTION TEST THE BAGG EXT LIGHT DOES NOT COME ON UNTIL AFTER RELEASING THE TEST BUTTON. -C/A-R&R CARGO SMOKE DETECTOR NR 2 IAW AMM 26-15-01. OPC GOOD AT THIS TIME.

Part: SKIN — TORN (RT ELEVATOR) · airframe 30,747 hrs · 25,937 cycles

RIGHT UPPER ELEVATOR SKIN TORN AT YH-1310. ACCOMPLISHED A REPAIR IAW SRM 55-20-01, AND ETN-EM-55-022R1.

Part: STRIP — WRONG PART (CABIN) · airframe 30,714 hrs · 25,909 cycles

EMER LIGHT STRIP ON FLOOR FWD OF EMER EXIT ROW SHOULD NOT HAVE ARROWS. R & R FLOOR PROX EMER STRIP IAW AMM 33-50-12 -020-003-A00.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 30,403 hrs · 25,636 cycles

FORWARD MID CEILING EXIT SIGN FAILS TO ILLUMINATE. R & R NR 6 EMER LIGHT INVERTER IAW AMM 33-50-11. OPERATIONS CHECKED GOOD.

Part: PBE — UNSERVICEABLE (CABIN) · airframe 30,334 hrs · 25,576 cycles

AFT PBE LOST ITS AIRTIGHT SEAL. R & R AFT CREW PBE AS REQUIRED IAW 140-EEL=-9=12.

Part: HANDLE — LACK OF LUBE (BRAKE SYSTEM) · airframe 29,681 hrs · 24,984 cycles

PARKING & EMERGENCY BRAKE STICKS & HARD TO ENGAGE. LUBRICATED PARKING BRAKE HANDLE IAW EMB 140 STANDARD MTX PRACTICES.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,480 hrs · 24,790 cycles

DURING MAINTENANCE INSPECTION ON FLIGHT 3039 FOUND FLOOR PROXIMITY EMERGENCY LIGHT STRIP BY SEAT 4A INOP. AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED FLOOR PROXIMITY STRIP LIGHT BY SEAT 4A IAW EMB-140 AMM REF 33-50-12. OPS CHECK GOOD.

Part: LIGHT — BROKEN (CABIN) · airframe 29,344 hrs · 24,662 cycles

DURING RECIRCULATION FAN FOUND THE 4TH FROM FWD GALLEY EMERGENCY FLOOR LIGHTING STRIP TO BE BROKEN. R & R FLOOR PROXIMITY STRIP LIGHT IAW AMM 33-50-12, OPERATIONS CHECKED GOOD.

Part: FLASHLIGHT ASSY — BROKEN (AFT CABIN) · airframe 28,312 hrs · 23,700 cycles

AFT FLASHLIGHT BROKEN. R & R AFT FLASHLIGHT IAW AMM 33-51-01. OPS CHECKED OK.

Part: WIRE — BROKEN (CABIN) · airframe 27,825 hrs · 23,260 cycles

DURING B-INSPECTION, FOUND THE 2ND TO LAST EMERGENCY LIGHT FLOOR STRIP ASSEMBLY HAS BROKEN A WIRE. THE ACFT WAS REMOVED FROM SERVICE. R & R THE 2ND TO LAST EMERGENCY LIGHT FLOOR STRIP ASSEMBLY. THE OPS CHECK WAS GOOD IAW AMM 33-50-12. THE ACFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,793 hrs · 23,232 cycles

DURING B INSP, FOUND THE SECOND TO LAST FLOOR EMERGENCY LIGHT INOPERABLE. THE ACFT WAS REMOVED FROM SERVICE. R & R THE SECOND TO LAST FLOOR EMERGENCY LIGHT IAW AMM 33-50-12. THE OPS CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — MISSING (COCKPIT) · airframe 27,544 hrs · 23,027 cycles

DURING MAINTENANCE INSPECTION FOUND THE CAPTAIN’S FLASHLIGHT MISSING. THE AIRCRAFT WAS REMOVED FROM SERVICE. INSTALLED CAPTAIN’S FLASHLIGHT IAW 20-10-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (RT WING) · airframe 27,070 hrs · 22,592 cycles

DURING B INSPECTION FOUND THE RIGHT WING FORWARD EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE BULB IN THE RIGHT WING FORWARD EMERGENCY LIGHT LOCATION. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SMOKE DETECTOR — FALSE ACTIVATION (CARGO BAY) · airframe 26,949 hrs · 22,484 cycles

ON FLIGHT 3434 THE CREW REPORTED THEY RECEIVED A BAGGAGE SMOKE EICAS MESSAGE AND BAGGAGE THE EXT BUTTON ILLUMINATED DURING CLIMB THROUGH ABOUT FTL 350. BAGG EXG BUTTON PRESSED EICAS MSG CLEARED NO SMOKE EVIDENT FROM FLIGHT ATTEDANT INSPECTION FROM LAV PEEP HOLE INSPECTED CARGO COMPARTMENT FOR FIRE OR SMOKE DAMAGE NO DAMAGE NOTED. THE CREW DECLARED A PRECAUTIONARY EMERGENCY AND RETURNED TO GCK. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. INSPECTED CARGO COMPARTMENT FOR FIRE OR SMOKE DAMAGE NO DAMAGE NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,923 hrs · 22,458 cycles

DURING MAINTENANCE INSPECTION FOUND THE AISLE EMERGENCY LIGHT INOPERABLE AT ROW 10. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED LIGHT BULB ON EMERGENCY LIGHT AT ROW 10 IAW EMB 1140 AMM 33-50-08. THE OPERATIONAL CHECK WAS GOOD NO DEFECTS NOTED AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,832 hrs · 22,383 cycles

DURING MAINTENANCE INSPECTION FOUND THE SQUARE EMERGENCY EXIT LIGHT 11C INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE BURNT LIGHT BULB IAW AMM 33-50-08. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 27,001 hrs · 22,532 cycles

DURING B INSPECTION FOUND THE FLIGHT ATTENDANT’S FLASHLIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FLIGHT ATTENDANT’S FLASHLIGHT ASSEMBLY IAW EMB AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 26,831 hrs · 22,382 cycles

DURING MAINTENANCE INSPECTION FOUND THE EMERGENCY LIGHT STRIPS AT AFT ROW 12 INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE BATTERY & BATTERY CHARGER. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — CRACKED (CABIN) · airframe 27,001 hrs · 22,532 cycles

DURING B INSPECTION FOUND THE VERY AFT LEFT AND RIGHT EMERGENCY LIGHT EXTRUSIONS JUST FORWARD OF LAV DOOR CRACKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE VERY AFT LT AND RT EMERGECY LT EXTRUSIONS JUST FWD OF LAV DOOR IAW W/C 25-700-08. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONNECTOR — LOOSE (CABIN) · airframe 27,001 hrs · 22,532 cycles

DURING B INSPECTION FOUND THE CEILING EMERGENCY LIGHT AT PASSENGER SEAT 11A FLICKERS ON AND OFF. THE AIRCRAFT WAS REMOVED FROM SERVICE. UNPLUGGED AND RE-PLUGGED CONNECTION. FOUND TO BE OK IAW EMB M/M 33-50-15. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — CRACKED (CABIN) · airframe 27,001 hrs · 22,532 cycles

DURING B INSPECTION FOUND THE NR 1 RT EMERGENCY LIGHT EXTRUSION IS CRACKED, & NR 4 RT EMERGENCY LIGHT EXTRUSION IS CRACKED, & NR 5 RT EMERGENCY LIGHT EXTRUSION IS CRACKED & NR 6 RT EMERGENCY LIGHT EXTRUSION IS CRACKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE DURING B INSPECTION FOUND THE NR 1 RT EMERGENCY LIGHT EXTRUSION IS CRACKED, & NR 4 RT EMERGENCY LIGHT EXTRUSION IS CRACKED, & NR 5 RT EMERGENCY LIGHT EXTRUSION IS CRACKED & NR 6 RT EMERGENCY LIGHT EXTRUSION IS CRACKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE 1, 4, 5 & 6 RT EMERGENCY LIGHT EXTRUSION IAW AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. EMERGENCY LIGHT EXTRUSION IAW AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 27,001 hrs · 22,532 cycles

DURING B INSPECTION FOUND THE EMERGENCY LIGHT STRIP ON THE CABIN FLOOR AFT OF SEAT 12 NOT OPERATIONAL. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 4 BATTERY & CHARGER IAW AMM 33-50-04. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — CRACKED (CABIN) · airframe 27,001 hrs · 22,532 cycles

DURING B INSPECTION FOUND THE LEFT NR 5, & 6 LIGHT EMERGENCY LIGHT EXTRUSION CRACKED AND THE NR 3 RIGHT EMERGENCY LIGHT EXTRUSION IS CRACKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED NR 5 & 6 LEFT EMERGENCY LIGHT EXTRUSION IAW EMB AMM 33-50-12. REMOVED AND REPLACED THE NR 3 RIGHT EMERGENCY LIGHT EXTRUSION IAW AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,001 hrs · 22,532 cycles

DURING B INSPECTION FOUND THE EMERGENCY EXIT LIGHT IN CABIN ABOVE SEAT 1C INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CEILING EXIT SIGN ASSEMBLY ABOVE SEAT 1C IAW EMB140 AMM 33-50-13. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONNECTOR — MISSING (CABIN) · airframe 27,001 hrs · 22,532 cycles

DURING B INSPECTION FOUND THE CABIN EMERGENCY LIGHT STRIP WIRE JUST AFT OF FRAME 20 IS MISSING CONNECTOR. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE MISSING CONNECTOR ON CABIN EMERGENCY LIGHT STRIP WIRE JUST AFT OF FRAME 20. OPS CHECK OF CABIN EMERGENCY LIGHT STRIP WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONNECTOR — DIRTY (CABIN) · airframe 27,001 hrs · 22,532 cycles

DURING B INSPECTION FOUND THE EMERGENCY LIGHT JUST FORWARD OF THE SERVICE DOOR INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED THE EMERGENCY LIGHT, INSPECTED AND CLEANED CONNECTORS, RE-INSTALLED AND ACCOMPLISHED OPERATIONAL CHECK IAW WC 33-700-17. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,001 hrs · 22,532 cycles

DURING B INSPECTION FOUND THE FORWARD CEILING EMERGENCY LIGHT ASSEMBLY BY EMERGENCY EXIT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FORWARD CEILING EMERGENCY LIGHT ASSEMBLY IAW EMB 140 AMM 33-50-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (RT WING) · airframe 26,618 hrs · 22,212 cycles

DURING MAINTENANCE INSPECTION FOUND THE RIGHT FORWARD WING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FORWARD WING EMERGENCY LIGHT IAW AMM 33-50-07. THE OPERATIONAL LIGHT CHECK WAS GOOD IAW AMM 33-50-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 26,529 hrs · 22,138 cycles

ON FLIGHT 3403 THE CREW REPORTED THE CAPTAIN’S FLASHLIGHT WAS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPLACED THE CAPTAIN’S FLASHLIGHT POWER SUPPLY AND BULB. THE OPERATIONAL CHECK WAS GOOD IAW AMM 33-51-01. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: TRIM SWITCH — DIRTY (COCKPIT) · airframe 26,227 hrs · 21,884 cycles

ON FLIGHT 3023 THE CREW REPORTED THE CAPTAIN’S PITCH TRIM SWITCH STUCK IN TRIM DOWN POSITION. SIX SECONDS LATER THE CREW RECEIVED A MASTER WARNING "PTRIM CPT SW FAIL". THE AIRCRAFT WAS REMOVED FROM SERVICE. CLEANED & LUBED CAPTAIN’S PITCH TRIM SWITCH IAW EMB AMM: 23-40-03. THE OPERATIONAL CHECK WAS GOOD IAW EMB 140 AMM 23-40-03. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CRADLE — BROKEN (CABIN) · airframe 25,594 hrs · 21,364 cycles

DURING MAINTENANCE INSPECTION FOUND THE EMERGENCY FLASHLIGHT CRADLE BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AFT WALL EMERGENCY FLASHLIGHT BASE IAW EMB AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 25,335 hrs · 21,138 cycles

DURING B INSPECTION, FOUND THE AFT AISLE CEILING EMERGENCY LIGHT INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE AFT AISLE CEILING EMERGENCY LIGHT LAMP IAW AMM 33-50-08. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 25,335 hrs · 21,138 cycles

DURING B INSPECTION, FOUND THE EMERGENCY LIGHT AT EMERGENCY EXIT ROW "A" IN THE PSU PANEL INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE ROW "A" EMERGENCY EXIT ROW PSU EMERGENCY LIGHT LAMP IAW AMM 33-50-08. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: BULB — INOPERATIVE (FLASHLIGHT) · airframe 25,293 hrs · 21,093 cycles

ON FLIGHT 4424, THE CREW REPORTED THE CAPTAIN'S FLASHLIGHT WAS INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE CAPTAIN'S FLASHLIGHT BULB IAW AMM 33-50-16. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,202 hrs · 21,002 cycles

DURING B INSPECTION FOUND THE OVERHEAD AISLE AFT EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AFT AISLE OVERHEAD EMERGENCY LIGHT BULB IAW EMB AMM 33-50-08. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE HARNESS — DEFECTIVE (NLG) · airframe 25,054 hrs · 20,870 cycles

ON FLIGHT 2724 THE CREW REPORTED THAT DURING LANDING RECEIVED A GEAR EXTENTION, "LG AIR/GND FAIL" MESSAGE THAT ILLUMINATED MOMENARILY THEN EXTINGUISHED. THE CREW DECLARED AN EMERGECNY AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NOSE LANDING GEAR WEIGHT ON WHEELS HARNESS AND WOW SWITCH IAW AMM 32-63-02 AND USING IPC 32-63-02. THE OPERATIONAL CHECK WAS GOOD IAW AMM 32-63-00. ADDITIONAL INFORMATION USED FROM WM 2--50-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 2,844 hrs · 20,725 cycles

DURING B-INSPECTION FOUND THE EMERGENCY LIGHT OVER RIGHT EMERGENCY EXIT DOOR INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT OVERWING EMERGENCY LIGHT IAW EMB 140 AMM 33-50-07. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,527 hrs · 20,441 cycles

DURING B-INSPECTION FOUND THE RIGHT OVERWING REAR EMERGENCY LAMP INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED LAMP IAW AMM 33-50-10. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ELECTRONIC UNIT — INOPERATIVE (LANDING GEAR) · airframe 24,429 hrs · 20,356 cycles

ON FLIGHT 4463 THE CREW REPORTED THAT ON FINAL APPROACH TO LANDING WITH FLAPS 9 DEGREES AND SPEED AT 180 KNOTS THEY SELECTED LANDING GEAR DOWN AND IMMIDIATELY GOT EICAS "LANDING GEAR AIR GROUND FAIL". EICAS SHOWED THE RIGHT MAIN THEN LEFT GEAR THEN NOSE DOWN FOLLOWED BY THE "LANDING AIR/ GROUND FAIL" EXTINGUSHED. RMU SHOWED GEAR DOWN & LOCKED AND EICAS SHOWED GEAR DOWN & LOCKED. THE CREW DECLARED AN EMERGECNY AND DIVERTED TO MCI. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LANDING GEAR ELECTRONIC UNIT IAW AMM 72-32-01. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE — BROKEN (CABIN) · airframe 23,325 hrs · 19,438 cycles

EMERGENCY LIGHT PROXIMITY STRIP WIRE BROKEN ON AIRCRAFT SIDE 5TH FROM FRONT. INSTALLED NEW TERMINAL ON WIRE ON AIRCRAFT SIDE FOR EMERGENCY LIGHT PROXIMITY STRIP 5TH FROM THE FRONT IAW SWOM20-00-03 OPS CHECK GOOD.

Part: WIRE — BROKEN (CABIN) · airframe 23,325 hrs · 19,438 cycles

EMERGENCY LIGHT PROXIMITY STRIP WIRE BROKEN ON AIRCRAFT SIDE 5TH FROM THE FRONT. INSTALLED NEW TERMINAL ON WIRE ON AIRCRAFT SIDE FOR EMERGENCY LIGHT PROXIMITY STRIP, 5TH FROM THE FRONT IAW SWPM 20-00-03. OPS CHECK GOOD.

Part: TUBE — CRACKED (BLEED AIR SYS) · airframe 22,650 hrs · 18,910 cycles

ON FLIGHT 4479 THE CREW REPORTED THAT DURING CRUISE RECEIVED A HIGH INTERMEDIATE TURBINE TEMERATURE. THE CAPTAIN DECLARED AN EMERGENCY AND DIVERTED TO BOS. THE AIRCRAFT HAD A HIGH ITT EXCEEDANCE UPON LANDING. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT ENGINE INBOARD CUSTOMER BLEED AIR TUBE IAW RRMM CH 75-00-00-400-801. THE OPERATIONAL CHECK WAS GOOD AT THIS TIME. NO LEAKS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FRAME — CRACKED (FUSELAGE) · airframe 22,354 hrs · 18,648 cycles

DURING MAINTENANCE BASE VISIT FOUND FRAME 23 CRACKED BETWEEN STRINGERS 15 RIGHT AND 16 RIGHT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED FRAME 23 IAW EO EM-53MR-1789. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FITTING — CHAFED (AILERON) · airframe 22,354 hrs · 18,648 cycles

DURING MAINTENANCE BASE VISIT FOUND THE RIGHT AILERON DAMPER FITTING CHAFING AGAINST THE ROD END. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED RIGHT AILERON DAMPER FITTING IAW EO EM-27MR-112. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FITTING — CRACKED (FUSELAGE) · airframe 22,354 hrs · 18,648 cycles

DURING MAINTENACE BASE VISIT FOUND SHEAR CLIP CRACKED AT FRAME 80, STRINGER 7 RIGHT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED FRAME 23 IAW EO EM-53MR-1789. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — LOW (COCKPIT) · airframe 22,224 hrs · 18,542 cycles

ON FLIGHT 4555 THE FIRST OFFICERS FLASHLIGHT WAS FOUND TO BE DIM. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FIRST OFFICERS EMERGENCY FLASHLIGHT ASSEMBLY IAW AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONTROLLER — MALFUNCTIONED (WINDSHIELD) · airframe 22,044 hrs · 18,384 cycles

ON FLIGHT 3292 THE CREW REPORTED THAT ON DESCENT THROUGH 10,000 FEET WITH THE ANTI-ICE ON, A STRONG ODOR OF ELECTRICAL SMOKE WAS NOTICED IN THE COCKPIT. THE ODOR DISSIPATED IN A FEW MINUTES. AT SAME TIME THE ANTI-ICE WENT OFF AND RECEIVED A WINDSHIELD 2 FAIL MESSAGE ON EICAS (CAUTION) APPEARED. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 2 WINDSHIELD HEAT CONTROLLER IAW AMM 30-42-01. THE OPERATIONAL CHECK WAS GOOD. NO ELECTRICAL SMOKE DETECTED. OK FOR SERVICE. (CONTROLLER CONFIRMED SOURCE OF ELECTRICAL ODOR). THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,753 hrs · 18,183 cycles

FOR FLIGHT 4555 FOUND THE REAR OVERHEAD EMERGENCY LIGHT TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE REAR OVERHEAD EMERGNECY LIGHT IAW EMB AMM 33-50-08. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,297 hrs · 17,766 cycles

DURING MAINTENANCE BASE VISIT FOUND THE LEFT OVERWING EMERGENCY LIGHT TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE BULB WITH NO FIX. REMOVED AND REPLACED THE LIGHT ASSEMBLY IAW EMB 140 AMM TASK 33-50-10-000-801-A/33-50-10-400-801-A. THE OPERATIONAL CHECK WAS GOOD AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 20,612 hrs · 17,218 cycles

DURING MAINTENANCE BASE VISIT FOUND THE LEFT EMERGENCY OVERWING LIGHT TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED LEFT EXTERNAL OVERWING LIGHT LAMP IAW EMB 140 AMM 33-50-10. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: THERMOSTAT — MALFUNCTIONED (BLEED AIR SYS) · airframe 18,881 hrs · 15,722 cycles

ON FLIGHT 3395 THE CREW REPORTED THAT IN ICING CONDITIONS A HOT ELECTRICAL SMELL WAS NOTICED IN THE COCKPIT. NO OVER TEMPERATURE MESSAGES NOTED. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED FAN AIR CONTROL THERMOSTAT IAW EMB 140 AMM 36-11-06. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

DURING A HMBV INSPECTION, A PREVIOUS REPAIR ON THE CENTER OMEGA BEAM BETWEEN FRAMES 24 AND 25 WAS FOUND TO BE CORRODED, CAUSED BY MOISTURE BEING CONTAINED AT THE OMEGA BEAM AND CROSS MEMBER. DO NOT HAVE ENOUGH INFORMATION AT THIS TIME TO DETERMINE THE CAUSE OF DAMAGE. (K)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

DURING A HMBV INSPECTION A PREVIOUS REPAIR ON THE LT OMEGA BEAM AT FRAME 20 WAS FOUND TO BE CORRODED, CAUSED BY MOISTURE BEING CONTAINED AT THE OMEGA BEAM AND CROSS MEMBER. DO NOT HAVE ENOUGH INFORMATION AT THIS TIME TO DETERMINE CAUSE OF DAMAGE. (K)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

DURING A HMBV INSPECTION, A PREVIOUS REPAIR ON THE CENTER OMEGA BEAM ABOVE THE CARBON CROSSBEAM FWD OF FRM 27 WAS FOUND TO BE CORRODED CAUSE BY MOISTURE BEING CONTAINED AT THE OMEGA BEAM A CROSS MEMBER. DO NOT HAVE ENOUGH INFORMATION AT THIS TIME TO DETERMINE THE CAUSE OF DAMAGE. (K)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

DURING A HMBV INSPECTION, A PREVIOUS REPAIR ON THE LT OMEGA BEAM ABOVE THE CARBON CROSSBEAM FWD OF FRAME 27 WA FOUND TO BE CORRODED, CAUSED BY MOISTURE BEING CONTAINED AT THE OMEGA BEAM AND CROSS MEMBER. DO NOT HAVE ENOUGH INFORMATION AT THIS TIME TO DETERMINE THE CAUSE OF DAMAGE. (K)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 18,034 hrs · 15,003 cycles

DURING HMBV, THE LEFT OMEGA BEAM WAS FOUND CORRODED BETWEEN FRAMES 37 AND 38. PERFORMED A 4.0 INCH BY 1.0 INCH CUT OUT OF THE LT OMEGA BEAM TO REMOVE THE DAMAGE. PREPARED A 15.0 INCH BY 2.0 INCH DOUBLER. FABRICATED A 13.0 INCH BY 1.0 INCH FILLER AND TWO SHIMS. PREPPED, CLEANED AND TREATED REPAIR PARTS AND REPAIR AREA. INSTALLED REPAIR PARTS IAW SRM 53-00-10. AIRCRAFT RETURNED TO SERVICE.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 14,665 hrs · 12,308 cycles

MAINTENANCE FOUND BOTH EMERGENCY EXIT OVERWING LIGHTS ARE INOP. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED POWER SUPPLY AND BATTERY IAW AMM 33-50-04. OPERATIONAL CHECK GOOD IAW AMM 33-50-00 AFTER BATTERIES CHARGED. AIRCRAFT RETURNED TO SERVICE.

Part: PROXIMITY SWITCH — OUT OF LIMITS (NLG) · airframe 14,160 hrs · 11,936 cycles

LANDING GEAR AIR/GND FAIL ON TAKEOFF. COULD NOT RAISE GEAR. RETURNED TO FIELD AND MADE NORMAL LANDING. INSP MLG PROX SWITCH CLEARANCES. ALL WITHIN. INSP NLG PROX SWITCHES AND FOUND TO BE OUT OF LIMITS. ADJUSTED AS PER AMM 32-63-05-700-803A. PERFORMED GEAR RETRACTION AND NO DEFECTS NOTED. AIRCRAFT RETURN TO SERVICE.

Part: PROXIMITY SWITCH — OUT OF ADJUST (NLG) · airframe 14,160 hrs · 11,936 cycles

LANDING GEAR LEVER FAIL ON TAKEOFF RETURNED TO MIA. JACKED ACFT INSPECTED MLG PROX SWITCH CLEARANCES WITHIN LIMITS. INSP NLG PROX SWITCHES AND ADJUSTED PROX SWITCH. PERFORMED GEAR RETRACTION OF LANDING GEAR OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 13,301 hrs · 11,324 cycles

LEFT INBOARD SEAT TRACK CORRODED BETWEEN FRAMES 36 TO 47. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-10-06. AIRCRAFT RETURNED TO SERVICE.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 13,301 hrs · 11,324 cycles

RIGHT OUTBOARD SEAT TRACK CORRODED BETWEEN FRAMES 47 TO 53. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-10-06. AIRCRAFT RETURNED TO SERVICE.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 13,301 hrs · 11,324 cycles

LEFT OUTBOARD SEAT TRACK CORRODED BETWEEN FRAMES 19 TO 23. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-10-06. AIRCRAFT RETURNED TO SERVICE.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 13,301 hrs · 11,324 cycles

LEFT FORWARD INBOARD SEAT TRACK CORRODED BETWEEN FRAMES 18 TO 23. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-10-06. AIRCRAFT RETURNED TO SERVICE.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 13,301 hrs · 11,324 cycles

LEFT OUTBOARD SEAT TRACK CORRODED BETWEEN FRAMES 23 TO 28. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-10-06. AIRCRAFT RETURNED TO SERVICE.

Part: SILL — CORRODED (ZONE 100) · corrosion level 2 · airframe 13,301 hrs · 11,324 cycles

SERVICE DOOR MIDDLE SILL CORRODED. REMOVED AND REPLACED SILL IAW EMB SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE.

Part: CHANNEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 13,301 hrs · 11,324 cycles

GUSSET OVER CENTER HAT BEAM BETWEEN FRAMES 19 AND 23 CORRODED. REMOVED AND REPLACED GUSSET IAW EMB SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 13,301 hrs · 11,324 cycles

LEFT OUTBOARD SEAT TRACK CORRODED BETWEEN FRAMES 28 TO 36. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-10-06. AIRCRAFT RETURNED TO SERVICE.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 13,301 hrs · 11,324 cycles

RIGHT OUTBOARD SEAT TRACK CORRODED BETWEEN FRAMES 28 TO 36. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-10-06. AIRCRAFT RETURNED TO SERVICE.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 13,301 hrs · 11,324 cycles

RIGHT OUTBOARD SEAT TRACK CORRODED BETWEEN FRAMES 23 TO 28. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-10-06. AIRCRAFT RETURNED TO SERVICE.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 13,301 hrs · 11,324 cycles

RIGHT INBOARD SEAT TRACK CORRODED BETWEEN FRAMES 24 TO 28. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-10-06. AIRCRAFT RETURNED TO SERVICE.

Part: ATTACH ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 13,301 hrs · 11,324 cycles

PASSENGER DOOR THRESHOLD FORWARD ATTACH ANGLE CORRODED. REMOVED AND REPLACED ATTACH ANGLE IAW EMB SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 13,301 hrs · 11,324 cycles

LEFT INBOARD SEAT TRACK CORRODED BETWEEN FRAMES 47 TO 53. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-10-06. AIRCRAFT RETURNED TO SERVICE.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 13,301 hrs · 11,324 cycles

RIGHT OUTBOARD SEAT TRACK CORRODED BETWEEN FRAMES 36 TO 47. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-10-06. AIRCRAFT RETURNED TO SERVICE.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 13,301 hrs · 11,324 cycles

LEFT INBOARD SEAT TRACK CORRODED BETWEEN FRAMES 23 TO 28. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-10-06. AIRCRAFT RETURNED TO SERVICE.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 13,301 hrs · 11,324 cycles

LEFT OUTBOARD SEAT TRACK CORRODED BETWEEN FRAMES 36 TO 47. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-10-06. AIRCRAFT RETURNED TO SERVICE.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 13,301 hrs · 11,324 cycles

LEFT OUTBOARD SEAT TRACK CORRODED BETWEEN FRAMES 47 TO 53. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-10-06. AIRCRAFT RETURNED TO SERVICE.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 13,301 hrs · 11,324 cycles

RIGHT INBOARD SEAT TRACK CORRODED BETWEEN FRAMES 47 TO 53. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-10-06. AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 12,728 hrs · 10,946 cycles

EMERGENCY LIGHTS NO TEST, FOUND ALL FOUR EMERGENCY BATTERIES DEAD. REMOVED AND REPLACED BATTERY PACKS IAW EMB 33-50-04. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE.

Part: ODOR — DETECTED (COCKPIT)

ORD - FLT 4169 - AIR TURN BACK TO ORD FOR ELECTRICAL SMELL IN COCKPIT. MOC WAS NOTIFIED BY DISPATCH. RIGHT LANDING LIGHT STOPPED WORKING DURING TROUBLESHOOTING FURTHER INVESTIGATION REVEALED ARCING AND BURNING ON THE LANDING LIGHT CONTACTOR. RAI CONTACTOR IAW 33-41-00, OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO BAY)

AFTER PARKING AT THE GATE BAG SMOKE INDICATION. RAID BOTH SMOKE DETECTORS IN THE BAGGAGE COMPT. FORWARD SMOKE DETECTOR P/N 473597-13, S/N NOT GIVEN OPS CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SKIN — DENTED (PAX DOOR)

PAX DOOR HAS DENT 16.5 INCHES FROM BOTTOM OF DOOR. REPAIRED ENT BY CUTTING OUT DAMAGED AREA AND INSTALLING AN EXTERNAL DOUBLER IAW EO EM-52MR-089. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: GUSSET — CORRODED (FUSELAGE)

DURING IMBV INSPECTION, FOUND CENTER HAT BEAM GUSSET CORRODED ON TOP. REMOVED AND INSTALLED NEW HAT BEAM GUSSET IAW SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SUPPORT — CORRODED (FUSELAGE)

SAW - DURING IMBV INSPECTION, FOUND CENTER HAT BEAM RAMP CORRODED. REMOVED AND INSTALLED NEW HAT BEAM RAMP IAW SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: FLOOR SUPPORT — CORRODED (FR 24-25)

SAW - DURING IMBV INSPECTION, FOUND LEFT OMEGA BEAM CORRODED BETWEEN FRAMES 24 AND 25 AT CROSSBEAM ATTACH POINT. REPAIRED LEFT OMEGA BEAM WITH DOUBLER IAW SRM 53-00-10 FIGURE 202. AIRCRAFT RETURNED TO SERVICE. (M)

Part: FLOOR SUPPORT — CORRODED (FR 24-25)

SAW - DURING IMBV INSPECTION, FOUND RIGHT OMEGA BEAM CORRODED BETWEEN FRAMES 24 AND 25 BY CROSS BEAM ATTACHMENTS POINTS. REPAIRED RIGHT OMEGA BEAM WITH DOUBLER IAW SRM 53-22-10 FIGURE 202. AIRCRAFT RETURNED TO SERVICE. (M)

Part: FLOOR SUPPORT — CORRODED (FR 27)

SAW - DURING IMBV INSPECTION, FOUND RIGHT OMEGA BEAM CORRODED AT FRAME 27 AT CROSSBEAM ATTACH POINT. REPAIRED RIGHT OMEGA BEAM WITH DOUBLER IAW SRM 53-22-10 FIGURE 201 SHEET 1. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

ALB - FLT 4155 - CREW REPORTED THE FIRST THREE STRIPS OF FLOOR PROXIMITY EMERGENCY LIGHTS TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED FOUR BATTERY PACKS IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: CONTROL UNIT — FAILED (E/E BAY)

DURING CRUISE FLIGHT THE CREW REPORTED PITCH TRIM .5 INOPERATIVE. MASTER WARNING WHEN A/P DISCONNECTED MOMENTARILLY. MAINTENANCE REMOVED AND REPLACED THE HORIZONTAL STABILIZER CONTROL UNIT IAW MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (SW21200501202)

Part: STRINGER — CHAFED (FUSELAGE)

ABI - DURING AN MBV INSPECTION, STRINGER 19R WAS FOUND AT FRAME 53. BLENDED THE CHAFE AREA AND PERFORMED NDT INSPECTION. FABRICATED A REPAIR ANGLE AND TWO SHIMS. REPAIR DONE IAW EMB REPAIR STATEMENT IC2003-145/2577 AND EMB SRM, SRM EMB 145/1142 REV 22, CHAPTER 53-24-02 FIGURE 201. (M)

Part: STRINGER — CHAFED (FUSELAGE)

ABI - DURING AN MBV INSPECTION, STRINGER 19L WAS FOUND CHAFED AT FRAME 53. BLENDED THE CHAFED AREA AND PERFORMED NDT INSPECTION. FABRICATED A REPAIR ANGLE AND TWO SHIMS. REPAIR DONE IAW EMB SRM, SRM EMB145/1142 REV 22, CHAPTER 53-24-02 FIG 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 DAMAGE SECTION OF LEFT OMEGA BEAM. FABRICATED AN EXTERNAL ANGLE, FILLER AND TWO SHIMS. REPAIR DONE IAW EMB SRM, SRM 145/1142, REV 22, CHAPTER 53-21-10 FIG 201, SHEET 3 CPM 51-61-00 AND STANDARD SRM PRACTICES. (M)

Part: CONTROL COLUMN — VIBRATION (COCKPIT)

DURING CLIMB THROUGH 25000 FT AT 290 KNOTS CREW REPORTED A VIBRATION IN THE CONTROL YOKE AND RUDDER PEDELS. VIBRATION LESSENED AS AIRCRAFT SPEED WAS LOWERED AND STOPPED AT 230 KNOTS. AIRCRAFT WAS RETURNED AND LANDED WITH NOT FURTHER INCIDENTS. MAINTENANCE INSPECTED AIRCRAFT WITH NO DEFECTS NOTED. A FUNCTIONAL CHECK FLIGHT WAS PERFORMED WITH NO DISCREPANCIES NOTED. AIRCRAFT WAS THEN RETURNED TO SERVICE.