N836AE

Part: DISPLAY — FAILED (COCKPIT) · airframe 37,425 hrs · 32,874 cycles

WHILE AT ALTITUDE, A FISHY SMELL FILLED THE COCKPIT AND CABIN, THE SMELL DISIPATED DURING DESCENT. REMOVED AND REPLACED THE NR 1 PFD IAW AMM 34-22-01. EFIS OPT GOOD IAW AMM 34-22-00. REMOVED AND REPLACED THE NR 1 MFD IAW AMM 34-22-01. EFIS OPS TESTED GOOD IAW AMM 34-22-00.

Part: FLASHLIGHT — MISSING (AFT CABIN) · airframe 37,286 hrs · 32,742 cycles

MEL 2553 - AUTH# 11-252-CREF ORG LG PG 4500501/1 PAX STOLE AFT CABIN FLASHLIGHT-C/A-INSTALLED NEW FLASHLIGHT IAW EMB140 AMM 33-50-16. OPS CHECK GOOD. MEL RESTORED

Part: FLASHLIGHT — INOPERATIVE (AFT CABIN) · airframe 37,199 hrs · 32,652 cycles

SUPPLEMENTAL AFT CABIN FLASH LIGHT INOP. CHARGING BASE NOT WORKING.-C/A-ITEM DEFERRED PER MEL 25-53 AUTH# 100787-C. REMOVED AND REPLACED AFT CABIN FLASH LIGHT PER EMER.EQUIPMENT LIST[ EEL] . MEL RESTORED.

Part: WIRE — BROKEN (FLASHLIGHT ASSY) · airframe 37,118 hrs · 32,572 cycles

AFT EMERGENCY FLASHLIGHT INOPERATIVE. REPAIRED BROKEN GROUND WIRE ON AFT FLASHLIGHT HARNESS IAW SWPM 20-21-00. OPS CHECKED GOOD IAW AMM 33-51-01.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,566 hrs · 32,061 cycles

SUPPLEMENTAL EMERGENCY LIGHT BETWEEN ROW 7&8 INOP. C/A-DEFERRED EMERGENCY LIGHT STRIP IAW MEL 33-30. REMOVED AND REPLACED ROW 7 AND 8 EMERGENCY FLOOR PROXIMITY LIGHT IAW AMM 33-50-12. OPC GOOD. NO DEFECTS NOTED. MEL RESTORED.

Part: SWITCH — DIRTY (PITCH TRIM) · airframe 36,348 hrs · 31,879 cycles

AFTER TAKEOFF, CAPTAIN'S PITCH TRIM WOULD NOT WORK. PTRIM MAIN INOP THEN DISPLAYED ON EICAS-C/A-CLEANED CAPT'S AND 1ST OFFICERS PITCH TRIM SWITCHES. PERFORMED OPS CHECK, OPS CHECK GOOD IAW EMB 140 AMM 27-40-04

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 35,237 hrs · 30,854 cycles

LAST 3 EMERGENCY LIGHT STRIPS INOP-C/A-REMOVED AND REPLACED #4 BATT AND CHARGER AND #6 INVERTER IAW EMB 140 AMM 33-50-11 AND W/C 33-700-19. OPS CHK GOOD. INVERTER P/N 7824-1 (6), EMERGENCY LIGHTING BATTERY P/N 2013-1A S/N 104958

Part: HANDLE — DEFECTIVE (PARKING BRAKE) · airframe 34,548 hrs · 30,144 cycles

PARKING BRAKE HANDLE VERY DIFFICULT TO PULL AND TWIST TO SET. SERVICED EMERG PARKING BRAKE HANDLE IAW AMM 32-44-10.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 33,841 hrs · 29,387 cycles

LEFT EXIT ROW CEILING EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMP IAW AMM 33-50-07. OPS CHECKED GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 33,470 hrs · 29,073 cycles

ON DEPARTURE, RECEIVED NUMEROUS MESSAGES ON THE CAPTAIN`S FMS. IC600-L, RW FAIL, ADC INPUT INVALID, FAIL, TAS INVALID, IC-600-R BUSS FAIL, , NO HEADING IC600 L HEADING FAIL, IC 600R HEADING FAIL, GPS 2 FAILED. FOUND A TRANSITORY CONDITION ON MC NR 1. FMC NR 1, OPS CHECKED GOOD IAW AMM 34-62-00

Part: SKIN — DAMAGED (PAX DOOR) · airframe 33,347 hrs · 28,911 cycles

MAIN DOOR EXTERNAL DOOR SKIN HAS MULTIPLE GOUGES AND POSSIBLE CRACK. PERFORMED PERMANENT REPAIR OF PAX DOOR SKIN IAW ERS-EM-52MR-830.

Part: SKIN — CRACKED (FUSELAGE) · airframe 33,347 hrs · 28,911 cycles

SKIN CRACKED AT FR 77 STR 3R. REPAIRED FR 77 STR 3R IAW SRM 53-32-01 ITEM 3FIGURE 204 SHEET 3.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,347 hrs · 28,911 cycles

RT FRAME 10 IS CRACKED ON UPPER AFT SIDE. REMOVED AND REPLACED RT FRAME 10 IAW SRM 53-00-04.

Part: SKIN — CRACKED (FUSELAGE) · airframe 33,347 hrs · 28,911 cycles

LT UPPER AFT FUSELAGE CRACKED ABOVE STRINGER 2L JUST AFT OF FR75. REPAIRED LT UPPER AFT FUSELAGE SKIN ABOVE STRINGER 2L AND JUST AFT OF FRAME 75 IAW SRM 53-31-01 ITEM 11 FIG 219.

Part: DOOR — CRACKED (E&E BAY) · airframe 33,347 hrs · 28,911 cycles

REAR ELECTRONICS COMPARTMENT DOOR CRACKED UNDER SUPPORT BRACKET FOR PIN. REPAIRED REAR ELECTRONICS COMPARTMENT DOOR IAW SRM 52-44-02.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,347 hrs · 28,911 cycles

SEAT 11A EMERGENCY EXIT LIGHT ON PSU INOP. REMOVED AND INSTALLED SEAT 11A EMERGENCY EXIT LIGHT BULB ON PSU AS REQUIRED.

Part: UNKNOWN — ODOR (CABIN) · airframe 33,143 hrs · 28,704 cycles

FA SAYS EKECTRCAL BURN ODOR FROM FOWARD CABIN. REMOVED AND REPLACED CEILING BALLAST IAW AMM 33-21-05 REMOVED AND REPL.ACED 1A PSU ASSY IAW 25-22-05. OPS CHECKED GOOD. NO BURNING ODOR NOTED.

Part: CONTROL MODULE — INOPERATIVE (EMERGENCY LIGHTS) · airframe 33,143 hrs · 28,704 cycles

EMERGENCY LIGHT NOT ARMED ILLUMINATES OCCASIONALLY WITH SWITCH IN ARMED POSITION. REMOVED AND REPLACED CABIN LIGHT CONTROL MODULE ASSY IAW AMM 33-21-01. OPS CHECKED GOOD.

Part: CONTROL MODULE — FAILED (CABIN LIGHTS) · airframe 33,143 hrs · 28,704 cycles

AFTER GPU HOOKUP, POWER DROPPED OFFLINE WITH CHATTERING RELAYS AND STRONG ELECTRICAL BURNING ODOR IN CABIN. REMOVED AND REPLACED CEILING BALAST IAW AMM 33-21-05. REMOVED AND REPLACED CABIN LIGHTING CONTROL MODULE IAW AMM CH 33-21-01.

Part: CONTROLLER — FAILED (CABIN PRESSURE) · airframe 32,405 hrs · 27,920 cycles

AUTO PRESSURIZATION CONTROLLER FAILED, HAD TO MANUALLY CONTROL THE PRESSURIZATION. R & R AUTO PRESSURIZATION DIGITAL CONTROLLER IAW AMM 21-31-01. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 32,329 hrs · 27,831 cycles

OVERHEAD EMER LIGHT IN COCKPIT INOPERATIVE. R & R BULB IN OVERHEAD EMER LIGHT IN COCKPIT IAW AMM 33-50-05. OPERATIONS CHECKED GOOD.

Part: HOLDER — BROKEN (FLASHLIGHT) · airframe 32,159 hrs · 27,614 cycles

CAPTAINS FLASHLIGHT HOLDER BROKEN. R & R CAPTAINS FLASHLIGHT ASSEMBLY IAW AMM 33-50-16.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,540 hrs · 26,958 cycles

AFT AISLE EMER LIGHT ASSEMBLY INOPERATIVE. R & R AFT AISLE EMER LIGHT ASSEMBLY BULB IAW AMM 33-50-08. OPERATIONS CHECKED GOOD.

Part: DOOR — LACK OF LUBE (CABIN) · airframe 31,248 hrs · 26,670 cycles

FLIGHT ATTENDANT REPORTS MAIN CABIN DOOR HARD TO OPEN. LUBRICATED ALL MAIN CABIN DOOR POINTS & PERFORMED MULTIPLE DOOR CLOSURE CHECKS. OPERATIONS CHECKED NORMAL AT THIS TIME. WORK WAS REFERENCED FROM AMM SECTIONS 52-18-00 & 53-21-02. NO OTHER DEFECTS NOTED AT THIS TIME.

Part: FRAME — CRACKED (FUSELAGE) · airframe 30,873 hrs · 26,325 cycles

FRAME 17 IS CRACKED BETWEEN STRINGER 12R & 13R. THIS IS A MAJOR REPAIR. REPAIRED FRAME 17 IAW ERS-EM-53MR-1259.

Part: STRINGER — BENT (FUSELAGE) · airframe 30,873 hrs · 26,325 cycles

STRINGER 12R IS BENT BETWEEN FRAME 16 & 19. THIS IS A MAJOR REPAIR. REPAIRED STRINGER 12R IAW ERS-EM-53MR-1259.

Part: STRINGER — BENT (FUSELAGE) · airframe 30,873 hrs · 26,325 cycles

STRINGER 13R IS BENT BETWEEN FRAME 16 & 19. THIS IS A MAJOR REPAIR. REPAIRED STRINGER 13R IAW ERS-EM-53MR-1259.

Part: ENGINE — LEAKING (NR 1) · airframe 30,769 hrs · 26,226 cycles

DURING NORMAL CRUISE FLIGHT AT 36,000 FT. OBSERVE NR 1 ENGINE OIL TEMP WENT UP GRADUALLY TO THE RED ARC INDICATION 156. REDUCE THE THRUST LEVEL IAW AOM AND NOTHING HAPPENED WITH THE TEMP. ALSO THE PRESSURE WENT DOWN TO 46 PSI AND THE OIL LEVEL WENT DOWN TO 7 QTS. DECLARED AND EMERGENCY AND DIVERTED. DID NOT SHUT DOWN THE ENGINE. REMOVED AND REPLACED NR 1 ENGINE IAW 71-000-00.

Part: ACM — SEIZED (AC BAY) · airframe 30,465 hrs · 25,990 cycles

DURING CLIMB CREW HEARD A LOW INTERMITTENT NOISE FOLLOWED BY A LIGHT SMOKE ENTERING THE COCKPIT THROUGH THE CEILING VENTS. CREW TURNED OFF PACKS & SMOKE DISSIPATED. CREW DECLARED AN EMER & RETURNED WITHOUT INCIDENT. INSPECTED & PERFORMED ENG RUN AT DIFFERENT POWER SETTINGS DURING NR 1 PACK OPERATIONS. CONFIRMED RUMBLING OF NR 1 PACK & SEIZED ALL OTHER SYSTEMS. OPERATIONS CHECKED NORMAL IAW MM 72-00-00 21-51-00 REF ITEM NR 2 OF NR 1 PACK MEL. R & R LT ACM IAW AMM 21-51-03. OPERATIONS TESTED LT PACK SYS, CHECKED OK IAW AMM 21-20-00.

Part: VALVE — FAILED (NR 2 ENGINE) · airframe 30,448 hrs · 25,975 cycles

ABORTED TAKEOFF, AT LOW SPEED NR 2 ENGINE ATTCS NO MARGIN EICAS MESSAGE. NR 2 ENGINE EXCEEDENCE EICAS CAUTION. NR 2 ENGINE HAS VALVE FAIL EICAS MESSAGE. TROUBLESHOT IAW FIM 72-00-00. R & R COMPRESSOR AIR DISCHARGER TUBE & COMPRESSOR ACCELERATION BLEED CONTROL VALVE IAW MM 75-00-00 & 75-31-15-400. OPS CHECKED GOOD.

Part: DOOR — DAMAGED (CARGO BAY) · airframe 30,279 hrs · 25,833 cycles

PREFLIGHT FOUND DAMAGE TO CARGO DOOR, VENT HANDLE WILL NOT STAY FLUSHED, APPEARS TO LEAK AIR.

Part: ROLLER — LACK OF LUBE (FUSELAGE) · airframe 30,230 hrs · 25,784 cycles

FLIGHT ATTENDANT ADVICE MAIN CABIN DOOR HARD TO OPEN. CLEANED & LUBRICATED MAIN DOOR FRAME ROLLERS IAW MM 53-21-02. DOOR LOAD OPEN TEST GOOD IAW MM 52-18-00.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,368 hrs · 25,085 cycles

PAX COMPARTMENT ROW 11 RT EMER LIGHT INOPERATIVE. R & R PAX COMPARTMENT EMER LAMP AT ROW 11 RT IAW AMM 33-50-08. OPERATIONS CHECKED GOOD.

Part: PROXIMITY SENSOR — FAILED (NLG) · airframe 28,836 hrs · 24,624 cycles

LG AIR & GND FAIL CAUTION ON EICAS SHORTLY AFTER ROTATION. R & R INTERCHANGEABLE NLG PROX SWITCH IAW AMM 32-62-02, OPERATIONS CHECKED GOOD.

Part: FLASHLIGHT — DEFECTIVE (COCKPIT) · airframe 28,763 hrs · 24,550 cycles

SIGNIFICANT ELEC BURNING SMELL IN MIDDLE OF CABIN & COCKPIT DURING CRUISE FLIGHT. FOUND ODOR COMING FROM PILOTS EMERGENCY FLASHLIGHT. R & R FLASHLIGHT IAW AMM 33-50-16. RAN ENGS IAW MM 72-00-00. NO FURTHER ODORS DETECTED IAW FIM TASK 21-20-00-810-801-A.

Part: HINGE — OUT OF ADJUST (CABIN DOOR) · airframe 28,520 hrs · 24,345 cycles

CABIN ENTRY DOOR HARD TO OPEN. ADJUSTED MAIN DOOR SIDE HINGE BY INSERTING WASHER IN TO DOOR FRAME LOWER SUPPORT IAW ETN EM-52-013R1.

Part: ROLLER — LACK OF LUBE (CABIN DOOR) · airframe 28,488 hrs · 24,318 cycles

MAIN CABIN DOOR EXTREMELY DIFFICULT TO OPEN ON TWO OCCASIONS. LUBE ALL DOOR ROLLERS, DOOR OPERATION CHECK IS GOOD IAW 140 52-10-00 AMM.

Part: FITTING — CORRODED (FUSELAGE) · airframe 28,470 hrs · 24,302 cycles

FRAME 68 SHEAR CLIP CORRODED AT CARGO DOOR LOWER SILL. REPAIRED FRAME 68 SHEAR CLIP IAW AEA ERS EM-53MR-1129.

Part: FITTING — CORRODED (FUSELAGE) · airframe 28,470 hrs · 24,302 cycles

FRAME 65 SHEAR CLIP CORRODED AT CARGO DOOR LOWER SILL. PERFORMED REPAIR OF FRAME 65 SHEAR CLIP IAW AEA ERS EM-53MR-1129.

Part: FRAME — CRACKED (FUSELAGE) · airframe 28,470 hrs · 24,302 cycles

FRAME 23 CRACKED BETWEEN STRINGER 15R & 16R. REPAIRED CRACK AT FRAME 23 IAW EO EM-53MR-1808.

Part: SUPPORT BRACKET — CRACKED (RT ENGINE) · airframe 28,470 hrs · 24,302 cycles

RT ENG ATS VLV SUPPORT TRIANGLE BRACKET IS CRACKED. R & R THE RT ENG TAS VLV SUPPORT TRIANGLE BRACKET IAW CMM 80-11-93 & AMM 20-10-01.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 28,470 hrs · 24,302 cycles

CARGO DOOR LOWER SILL AFT FLOOR SUPPORT LOWER L ANGLE CRACKED. REMOVED CRACKED CARGO DOOR LOWER SILL AFT FLOOR SUPPORT LOWER L ANGLE, PREPPED & INSTALLED SERVICEABLE L ANGLE IAW SRM 51-40-02 & SRM 51-20-03.

Part: WIRE — BROKEN (CABIN) · airframe 28,470 hrs · 24,302 cycles

LT NR 1 PROXIMITY LIGHT STRIP HAS WIRES BROKEN OFF. R & R LT NR 1 PROXIMITY LIGHT STRIP IAW AMM 33-50-12. SEE NRTC BOW150062 TASK NR 1 FOR OPERATIONS CHECK.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 28,470 hrs · 24,302 cycles

LT BLEED AIR TUBE SUPPORT BRACKET, BELOW FLOOR, BETWEEN FRAME 68 & 69 CRACKED. R & R LT BLEED AIR TUBE SUPPORT BRACKET, BELOW FLOOR, BETWEEN FRAME 68 & FRAME 69 IAW SRM 51-40-02. LEAK CHECKED GOOD, SEE TURNOVER FOR DETAILS.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 28,470 hrs · 24,302 cycles

RT OMEGA BEAM OTBD SUPPORT CRACKED AT FRAME 47. R & R RT OMEGA BEAM OTBD SUPPORT BETWEEN FRAME 46 & FRAME 50 IAW SRM 53-23-02.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 28,470 hrs · 24,302 cycles

LT OMEGA BEAM OTBD SUPPORT CRACKED AT FRAME 47. REMOVED LT OMEGA BEAM OTBD SUPPORT CRACKED AT FRAME 47 & INSTALLED SERVICEABLE SUPPORT IAW SRM 53-23-02 SEE TURNOVER FOR DETAILS.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 28,470 hrs · 24,302 cycles

RT OMEGA BEAM INBD SUPPORT CRACKED AT FRAME 47. REMOVED RT OMEGA BEAM TO WING BOX INBD SUPPORT ANGLE & INSTALLED NEW TWO PIECE SUPPORT ANGLE IAW SRM 53-23-02.

Part: SUPPORT BRACKET — CRACKED (LT ENGINE) · airframe 28,470 hrs · 24,302 cycles

LT ENG ATS VLV SUPPORT TRIANGLE BRACKET IS CRACKED. R & R LT ENG ATS SUPPORT TRIANGLE BRACKET IAW CMM 80-11-93 & AMM 20-10-01.

Part: SUPPORT — CORRODED (AILERON) · airframe 28,470 hrs · 24,302 cycles

AILERON FWD TORQUE TUBE RT SUPPORT CORRODED. R & R AILERON FWD TORQUE TUBE RT SUPPORT IAW SRM 51-40-02.

Part: HOLDER — BROKEN (FLASHLIGHT) · airframe 25,011 hrs · 21,138 cycles

ON FLIGHT 4425 THE CREW REPORTED THE AFT FLIGHT ATTENDANT FLASHLIGHT HOLDER WAS BROKEN. FLIGHT CREW PLACARD PER MEL 25-53. REMOVED AND REPLACED THE AFT CABIN FLASHLIGHT IAW AMM 33-50-16. MEL ITEM RESTORED. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: UNKNOWN — SMOKE (NR 1 ENGINE)

FLIGHT 4118, NR 1 ENGINE SMOKING 10 MINUTES AFTER SHUTDOWN. AIRCRAFT REMOVED FROM SERVICE. INSPECTED INTAKE AND EXHAUST OF ENGINE FOR OIL LEAK, GROUND RAN ENGINE IAW MM 72-00-00. COULD NOT DUPLICATE. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 24,110 hrs · 20,263 cycles

DURING "C" CHECK FOUND THE LEFT OMEGA BEAM CORRODED UNDER CARBON CROSSSBEAM AT FR 38. THE AIRCRAFT WAS REMOVED FROM SERVICE. COMPLETED REPAIR TO LEFT HAND OEMGA BEAM AT FRAME 38 IAW SRM 53-00-10 STEP 3 FIG 202 SHEET 2. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FRAME — CRACKED (FUSELAGE) · airframe 24,110 hrs · 20,263 cycles

DURING MBV INSPECTION FOUND FRAME 23 IN CRACKED AT STRINGR 15 RIGHT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIR OF FRAME 23 IAW EM-53MR-1808. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — DAMAGED (CABIN) · airframe 24,166 hrs · 20,316 cycles

DURING MAINTENANCE INSPECTION, FOUND THE FLOOR PROXIMITY EMERGENCY LIGHT PLASTIC EXTRUSIONS ARE DAMAGED. AIRCRAFT REMOVED FROM SERVICE. PROCURED EXTRUSIONS AND ASSEMBLED WITH LIGHT STRIPS IAW AMM 33-50-12. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — UNKNOWN · airframe 24,166 hrs · 20,316 cycles

DURING B INSPECTION, FOUND THE COCKPIT OVERHEAD EMERGENCY LIGHT PANEL 225 INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. COULD NOT DUPLICATE. COCKPIT OVERHEAD EMERGENCY LIGHT PANEL 225 CHECKED GOOD. NO DEFECTS NOTED IAW TASK 33-50-00-700-801-A. NO PARTS REMOVED OR REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (OVERWING) · airframe 24,166 hrs · 20,316 cycles

DURING B INSPECTION, FOUND THE FLOOR EMERGENCY LIGHT STRIP AT OVERWING EMERGENCY EXIT AREA INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED FLOOR EMERGECNY LIGHT IAW AMM 33-50-12. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 24,166 hrs · 20,316 cycles

DURING MAINTENANCE INSPECTION, FOUND THE SECOND EMERGENCY LIGHT STRIP FROM BACK HAS BROKEN WIRE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE SECOND EMERGENCY LIGHT STRIP IAW AMM 33-50-12. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: ADC — MALFUNCTIONED (NR 1) · airframe 23,822 hrs · 20,013 cycles

ON FLIGHT 2702 THE AIRCRAFT WAS GOING FROM GDL TO DFW BUT DUE TO WEATHER DIVERTED TO SAT. THEN TOOK OFF FROM SAT TOWARDS DFW AND EN ROUTE GOT AIRSPEED INDICATIONS ROLLING BACK WITH SPS ADVANCED MESSAGE. THE CAPTAIN RETURNED TO SAT AND DID DECLARE EMERGENCY. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 1 AIR DATA COMPUTER IAW AMM 34-15-01. THE OPERATIONAL TEST AND LEAK CHECK IAW AMM 34-13-00 WERE GOOD. AIRCRAFT IS RVSM ELIGIBLE. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: HANDLE — MISINSTALLED (CABIN DOOR) · airframe 22,902 hrs · 195,351 cycles

F/A COULD NOT OPEN CABIN DOOR - HANDLE BINDING, 3RD WRITE UP IN 4 DAYS. FOUND MAIN DOOR HANDLE NOT INSTALLED PROPERLY. INSTALLED MAIN DOOR HANDLE IAW EMB 140 AMM 52-18-05. PERFORMED OPS CHECK OF DOOR IAW EMB 140 AMM 52-18-00. NO OTHER DEFECTS NOTED.

Part: HANDLE — MISINSTALLED (CABIN DOOR)

ON FLIGHT 3341 THE CREW REPORTED THE FLIGHT ATTENDANT COULD NOT OPEN THE CABIN DOOR (HANDLE BINDING). THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND MAIN DOOR HANDLE NOT INSTALLED PROPERLY. INSTALLED MAIN DOOR HANDLE IAW EMB 140 AMM 52-18-05. PERFORMED FUNCTIONAL CHECK OF DOOR IAW EMB 140 AMM 52-18-00. NO OTHER DEFECTS NOTED AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: UNKNOWN — SMOKE (LT ENGINE)

FOR FLIGHT 2926 DURING THE PREFLIGHT INSPECTION THE FIRST OFFICERS FOUND A TRAIL OF WHITE SMOKE COMING FROM THE EXHAUST WITH A RUBBERY SMELL TO IT. THE AIRCRAFT WAS REMOVED FROM SERVICE. INSPECTED LEFT ENGINE FOR POSSIBLE SMOKE IN EXHAUST, RAN LEFT ENGINE IAW RRMM CHAP 72-00-00. THE OPERATIONAL CHECK WAS GOOD NO SMOKE NOTED IN EXHAUST ON SHUTDOWN AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 22,873 hrs · 20,231 cycles

EMERGENCY EXIT SIGN AT EMERGENCY HATCH INOP (UPPER) LEFT SIDE OVERWING. REMOVED AND INSTALLED NR 4 INVERTER IAW EMB MM 33-50-11, OPT CHECK GOOD IAW 33-50-00.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 21,489 hrs · 18,164 cycles

ON FLIGHT 9802 THE CREW REPORTED A SMOKE SMELL WITH NO VISUAL SMOKE INDICATION. THE AIRCRAFT WAS REMOVED FROM SERVICE. MAINTENANCE REPORTED AN AIR TURNBACK DUE TO A POSSIBLE LIGHTNING STRIKE. THE AIRCRAFT RETURNED TO ABI. PERFORMED ENGINE RUNS IAW RR MM 72-00-00, NO SMOKE SMELLS NOTED. SUSPECT REMAINS OF COMP WASH WHEN THE ANTI-ICE VALVE WAS OPEN WHICH CREW INDICATED THAT IS WHEN THE SMELL OCCURRED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ENGINE — BIRD INGESTION (RIGHT) · airframe 21,487 hrs · 18,162 cycles

ON FLIGHT 2754 AFTER TAKEOFF THE CREW REPORTED SMOKE AND SMOKE ODOR IN CABIN. THE CAPTAIN DECLARED AN EMERGENCY AND RETURNED TO LFT. THE AIRCRAFT HAD AN OVERWEIGHT LANDING AT 42000 POUNDS 500 FPM SINK RATE. THE AIRCRAFT LANDED WITHOUT INCIDENT AND WAS REMOVED FROM SERVICE. REMOVED BIRD REMAINS FROM THE RIGHT ENGINE C/W ETN EM-72-034 R4. NO FURTHER SMOKE OR SMOKE ODOR DETECTED IAW EMB AMM 71-00-01. PERFORMED NR 2 ENGINE COMPRESSOR WASH IAW RR MM 72-00-00. NO PARTS REMOVED OR REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WINDSHIELD WIPER — STUCK (WINDSHIELD) · airframe 20,685 hrs · 17,528 cycles

ON FLIGHT 4264 THE CREW ELECTED TO ABORT THE LOW SPEED TAKEOFF DUE TO DEICE FLUID ON THE WINDSHIELD AND UNABLE TO USE THE WIPER TO CLEAR. THE AIRCRAFT WAS REMOVED FROM SERVICE. UNSTUCK WIPER BLADE AND PERFORMED OPERATIONAL TEST OF WINDSHIELD WIPER SYSTEM IAW EMB140 AMM 30-41-00. NO PARTS REMOVED OR REPLACED. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — LOOSE (CABIN) · airframe 20,707 hrs · 17,548 cycles

ON FLIGHT 3940 THE CREW REPORTED THE FLIGHT ATTENDANT REAR CABIN FLASHLIGHT ASSEMBLY WAS LOOSE, CAUSING INTERMITTENT CHARGING OF THE FLASH LIGHT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AFT FLIGHT ATTENDANT FLASHLIGHT ASSEMBLY. THE OPERATIONAL TEST WAS OK AS REQUIRED IAW EMB AMM 33-50-16. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 20,362 hrs · 17,245 cycles

DURING MAINTENANCE BASE VISIT FOUND THE AIRCRAFT WAS STRUCK BY A BAGGAGE CART FORWARD OF RIGHT WING ON FUSELAGE. THE RIGHT CENTER FUSELAGE NR 2 HAS SKIN DENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. FERRIED FROM ORD TO SAW FOR REPAIR. REPAIRED DAMAGE IN ACCORDANCE WITH EO EM 53MR-1697. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 20,065 hrs · 16,997 cycles

DURING MAINTENANCE BASE INSPECTION FOR FLIGHT 2712 THE NR 2 EMERGENCY FLOOR LIGHTS FAILED TO LIGHT AFTER BATTERY REPLACEMENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY POWER SUPPLY. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 19,309 hrs · 16,369 cycles

DURING MAINTENANCE BASE VISIT FOUND THE AIRCRAFT HAD SUSTAINED DAMAGE ON CENTER THE FUSELAGE I LOWER SKIN BETWEEN FRAME 21 AND FRAME 22 AT STRINGER 20 LEFT. THE AIRCRAFT WAS REMOVED FROM SERVICE. COMPLETED REPAIR OF DAMAGE IAW EO EM-53MR-1513. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 18,125 hrs · 15,248 cycles

DURING MAINTENANCE BASE INSPECTION FOUND THAT THE AFT CABIN FLASHLIGHT FAILED TO ILLUMINATE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AFT CABIN FLASHLIGHT BATTERY. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE)

DURING A MBV INSP, THE GALLEY FLOOR CENTER BEAM AT FR 20 WAS FOUND CORRODED WITH LEVEL TWO CORROSION. PERFORMED CUT OUT OF THE CENTER BEAM TO REMOVE THE DAMAGE. FAB A DOUBLER, DRILLED, APPLIED PREVENTIVE AND INSTALLED. WORK DONE IAW EMB 145 SRM (SRM EMB-14511142 REV 40) CHAPTER 53-21-10. AIRCRAFT RETURNED TO SERVICE. (A)

Part: ANTI-ICE VALVE — FAULTY (ANTI-ICE SYSTEM) · airframe 13,081 hrs · 11,117 cycles

ON T/O ROLL GOT E2 A/ICE FAIL MESSAGE. ABORTED TAKEOFF SPEED BELOW 100KTS APU WAS OFF T/O THRUST WAS 84. 2N1 MESSAGE DISAPPEARED AFTERWARDS TO IDLE. REMOVED AND REPLACED ANTI-ICE VALVE IAW MM 30-21-01 AND REMOVED AND REPLACED DELIVERY TUBE IAW AMM 36-11-00. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 11,465 hrs · 9,971 cycles

STRONG OIL ODOR IN COCKPIT DURING FLIGHT. [SUP 05-08-07] REMOVED AND REPLACED LEFT HAND ENGINE IAW AMERICAN EAGLE WORK CARD 72-000-00. OPERATIONAL AND LEAK CHECKS COMPLIED WITH NO LEAKS - RETURNED AIRCRAFT TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

DURING IMBV INSPECTION CENTER OMEGA BEAM AT FRAME 25 WAS FOUND CORRODED. REMOVED CORROSION BY CUTTING OUT SECTION OF THE CENTER OMEGA BEAM FOUND CORRODED. FABRICATED FILLER, DOUBLER AND TWO SHIMS. REPAIR DONE IAW EMB 145 SRM, SRM EMB 145/1142 REV 33, CHAPTER 53-00-10 FIG 203. RETURNED AIRCRAFT TO SERVICE. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

ABI - DURING IMBV INSPECTION, RIGHT OMEGA BEAM AT FRAME 27 WAS FOUND CORRODED. CUT OUT OF RIGHT OMEGA BEAM TO REMOVE CORROSION. FABRICATED A FILLER, REPAIR DOUBLER AND TWO SHIMS. REPAIR DONE IAW EMB 145 SRM, SRM EMB 145/1142 REV 33, CHAPTERS 53-00-10 FIG 203. RETURNED AIRCRAFT TO SERVICE. (M)

Part: SILL — CORRODED (CARGO DOORWAY)

DURING IMBV INSPECTION, FOUND CARGO DOOR CUT OUT LOWER SILL CORRODED. REMOVED THE CORRODED LOWER SILL AND INSTALLED SERVICEABLE SILL IAW EMB SRM, SRM 145/1142 REV 33, CHAPTERS 51-40-02 AND EMB CPM, CPM 145/1132 REV 13, CHAPTER 51-21-06. AIRCRAFT RETURNED TO SERVICE. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

ABI - DURING IMBV INSPECTION, LEFT OMEGA BEAM WAS FOUND TO HAVE ONE SPOT OF CORROSION 6 INCHES AFT OF FRAME 25. DRILLED A HOLE TO REMOVE THE CORROSION AND INSTALLED A RIVET. RESTORED THE SURFACE FINISH AND APPLIED CORROSION PREVENTATIVE. REPAIR DONE IAW EMB IC2006-145/STRO73 DATED JULY 14, 2006. RETURNED AIRCRAFT TO SERVICE. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

ABI - DURING IMBV INSPECTION, FOUND LEFT OMEGA BEAM CORRODED AT FRAME 27. REMOVED CORROSION BY MAKING A CUTOUT, PREPARED A DOUBLER, FILLER AND TWO SHIMS. REPAIR DONE IAW EMB SRM, SRM 145/1142 REV 33, CHAPTERS 53-00-10 FIG 202. RETURNED AIRCRAFT TO SERVICE. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

DURING IMBV INSPECTION, LEFT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 25. REMOVED CORROSION BY MAKING A CUTOUT. PREPARED A FILLER, DOUBLER, PLATE AND TWO SHIMS. REPAIR DONE IAW EMB SRM, SRM145/1142 REV 33. RETURNED AIRCRAFT TO SERVICE. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

DURING IMBV INSPECTION, LEFT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 25. REMOVED THE CORROSION BY MAKING A CUT OUT, PREPARED A FILLER, DOUBLER, AND TWO SHIMS. REPAIR DONE IAW EMB SRM, SRM 145/1142 REV 33, CHAPTER 53-00-10 FIG 202. RETURNED AIRCRAFT TO SERVICE. (M)

Part: SILL — CORRODED (SERVICE DOORWAY)

DURING IMBV INSPECTION, SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED. REMOVED THE CORRODED CENTER SILL AND INSTALLED SERVICEABLE SILL IAW EMB SRM, SRM 145/1142 REV 33, CHAPTERS 51-140-02, 03, 51-40-06 AND EMB CPM, CPM 145/1132 REV 13, CHAPTER 51-21-04. RETURNED AIRCRAFT TO SERVICE. (M)