N803AE

Part: LIGHT — INOPERATIVE (LT OVERWING) · airframe 34,374 hrs · 30,358 cycles

L/H OVERWING EMERGENCY LIGHT INOP-C/A-RAR LEFT OVERWING EMERGENCY LIGHT ASSY OPC GOOD AMM 33-50-01

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 34,339 hrs · 30,313 cycles

EMERGENCY EXIT CEILING LIGHT AT ROW 6/7 IS INOP-C/A-RAR EMERGENCY EXIT CEILING LAMP AT ROW 6/7 IAW EMB 140 AMM 33-50-08. OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 34,316 hrs · 30,282 cycles

LH SIDE CENTER FAIRING EMERGENCY LIGHT INOP-C/A-REMOVED AND REPLACED LH CENTER FAIRING EMERGENCY LIGHT IAW AMM 33-50-10 OPS CHK GOOD

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 34,209 hrs · 30,137 cycles

LEFT CENTER FAIRING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE LAMP IAW AMM 33-50-10. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,051 hrs · 29,980 cycles

COCKPIT ENTRY EMERGENCY LIGHT INOP. C/A-RAR COCKPIT ENTRY EMERGENCY LIGHT IAW AMM 33-50-05. OPS CHECK GOOD.

Part: CONTROLLER — FAILED (CABIN PRESSURE) · airframe 33,744 hrs · 29,655 cycles

AFTER TAKE OFF THE AIRPLANE WAS NOT PRESSURIZING. CAB ALT WENT UP TO 11300-C/A-T/S REF FIM 21-31-00-810-801. REMOVED AND REPLACED PRESSURIZATION DIGITAL CONTROLLER IAW AMM 21-31-01. OPC GOOD IAW AMM 21-31-00.

Part: TUBE — DISCONNECTED (AC BAY) · airframe 33,743 hrs · 29,653 cycles

BLEED 1 LEAK IN FLIGHT PACK 1 AND PACK 2 FAIL ADVISORY PACK 2 ABNORMAL LOUD CRACKING NOISE CABIN WOULD NOT PRESSURE. C/A-REMOVED SLEEVE CONNECTING Y-DUCT TO DTCV ON PACK 1 REFERENCE TO AMM 21-51-14 SUBTASK J(A) AND IAW SUPPLEMENTAL AMM 21-60-01 SUBTASK 020-002-A J(K). INSTALLED IAW AMM 21-60-01 SUBTASK 420-002-A I(E) REF AML 4535660/1. OPC GOOD. NO LEAKS NOTED. PERFORMED OPC OF BLEED AIR SYS IAW AMM 36-00-00-700-803-A. OPC GOOD. NO LEAKS NOR MESSAGES NOTED. REMOVED TUBE IAW AMM 21-60-01 PART J(D) FROM DUAL HEAT EXCHANGER SIDE, AND RE-INSTALLED IT. DEFERRED PACK #2 PER MEL 21-30 REF: MEL 21-30 AUTH: 070520D-C. AFTER PACK 1 OPC GOOD. PERFORMED PRESSURIZATION TEST IAW AMM 21-31-00. OPC GOOD. NO DEFECTS NOTED AT THIS TIME. UPON INSPECT OF PACK 2 FOUND TUBE BTWN DUEL HEAT XCHANGER AND DTCV NOT ATTACHED AND LOOSE FROM DTCV SIDE. ALSO FOUND TUBE DENT. REMOVED AND REPLACED PRIMARY DUCT TUBE IAW ETN-EM-21-056 ON PACK 2. OPS CHECK GOOD IAW AMM-21-50-00-700-802. MEL RESTORED. NO LEAKS FOUND. PERFORMED OPC OF #1 PACK IAW AMM 21-51-00. OPC GOOD. ALSO PERFORMED FIM 21-20-00-810-801 FOR ABNORMAL SMELL NOTED IN KVA WITH NO SMOKE/ABNORMAL SMELL NOTED. MEL RESTORED. NO M PROCEDURES APPLICABLE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 33,697 hrs · 29,612 cycles

LT FWD EXTERANL EMERGENCY LIGHT INOP. C/A-REMOVED AND REPLACED LT FWD EXTERNAL EMERGENCY LIGHT LAMP IAW AMM TASK 33-50-10-000-801-A AND 33-50-10-400-801-A. OPC GOOD.

Part: CONTROL LEVER — MALFUNCTIONED (MLG) · airframe 33,623 hrs · 29,551 cycles

LANDING GEAR LEVER DISAGREE, RT MAIN DID NOT INDICATE UP, QRH PROCEDURED RAN, CYCLED GEAR, INDICATED UP AFTER 1 CYCLE. COMPLIED WITH LANDING GEAR LEVER DISAGREEMENT FIM 32-32-00. NO CMC MESSAGES NO TED. NO DEFECT NOTED. FOR PRECAUTIONARY MEASUREMENTS RAR LG/LEVER CONTROL MODULE. OPC CHECKED GOOD

Part: LIGHT — INOPERATIVE (AFT CABIN) · airframe 33,576 hrs · 29,509 cycles

AFT FLOOR EMERGENCY PROXIMITY LIGHT STRIP INOPERATIVE. REMOVED AND REPLACED AFT FLOOR PROXIMITY LIGHT IAW AMM. 33-50-12. OPC GOOD. NO DEFECTS NOTED.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 33,576 hrs · 29,509 cycles

LEFT OVERWING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED L/H OVERWING EMERGENCY LIGHT BULB IAW AMM 33-50-10. OPS CHECKED GOOD.

Part: VALVE — FAILED (BLEED AIR SYS) · airframe 33,266 hrs · 29,196 cycles

REJECTED TAKEOFF PRIOR TO 80 KTS DUE TO "HS VLV 1 FAIL" MSG. C/A-REMOVED AND REPLACED HSV 1 IAW AMM 36-11-02 OPS CHECK GOOD AT THIS TIME. OPERATIONAL CHECK OF THE HIGH STAGE PRESSURE SWITCH GOOD IAW 36-11-07.

Part: PRESSURE SWITCH — FAILED (RT ENGINE) · airframe 32,930 hrs · 28,813 cycles

BLD 1 OVERHEAT WX MSG CAME ON WHILE CUMBING THROUGH 210 IN CLEAR AIR . QRH PROCEDURE FOLLOLWED TEMP STILL STAYED HIGH IN THE RED EVEN WITH PWR PULLED BACK ON NO 1 ENGINE TEMP CAME DOWN AFTER DECENT INITATED AND NO 2 ENGINE THRUST CAME DOWN TOO. TRANSFERRED TO NRWC 803-DFW-02244-. PACK #2 HAS BLOWN DUCT. AFTER 5 MINUTES OPERATING WITH APU, LOUD RUSH OF AIR HEARD FROM R/H PACK ACM.C/A- REMOVED AND REPLACED RH ENG HIGH STAGE PRESSURE SWTCH IAW AMM 36-11-07. OPC IS GOOD. PERFORMED AIR BLEED OPC IAW AMM 36-00-00-700-803. OPC IS GOOD. RESECURED RH ACM BLEED DUCT TUBE ASSY IAW EMB 140 AMM 21-51-03 OPS CHECK GOOD NO LEAKS NOTED

Part: CONTROL UNIT — FAILED (HORIZONTAL STAB) · airframe 32,892 hrs · 28,766 cycles

PTRIM BACKUP INOP PTRIM MAIN INOP IN FLIGHT. RUDDER SYS 2 INOP FLIGHT-C/A-REMOVED AND REPLACED HORIZONTAL STAB CONTROL UNIT IAW EMB 140 AMM 27-40-01. OPC GOOD IAW EMB 140 AMM 27-40-00-700-802-A. REMOVED AND REPLACED EDP PRESSURE SWITCH I.A.W EMB 140 AMM 29-10-19. OPC & LEAK CHECK GOOD AT THIS TIME. REMOVED AND REPLACED EMPD PRESSURE SWITCH I.A.W EMB 140 AMM 29-30-04. OPC & LEAK CHECK GOOD AT THIS TIME. PRESSURE SWITCH P/N 368192-105 S/N RC5448 P/N 368192-111 S/N RC5357

Part: CONNECTOR — DEFECTIVE (SPOILER) · airframe 32,676 hrs · 28,555 cycles

SUPPLEMENTAL SPOILER FAIL ON EICAS DURING FLIGHT "TRANSFERRED TO NRWC 803-DFW-02162" C/A- REMOVED AND REPLACED CONNECTOR ON LT OUTBOURD SPOILER PROX SWITCH IAW SWPM 20-50-00 OPS CHECKS GOOD IAW AMM 27-63-01. REMOVED AND REPLACED CONNECTOR ON LT O/B SPOILER PROX SWITCH IAW SWPM 20-50-00 OP CHECKS GOOD IAW AMM 27-63-01.

Part: WARNING MESSAGE — FALSE ACTIVATION (BLEED SYSTEM) · airframe 32,417 hrs · 28,255 cycles

MECH BLD 1 OVR TEMP. CAUTION MSG DECLARED EMERGENCY.FLT CXLD.-C/A-REF FIM 36-11-00 NO DISCREPANCIES NOTED AT THIS TIME. NO ASSOCIATED CMC OR EICAS MSGS. PERFORMED OPERATIONAL TEST IAW AMM 36-00-00-700-803-A OPS CHECK GOOD.

Part: DISPLAY — MALFUNCTIONED (COCKPIT) · airframe 32,105 hrs · 27,975 cycles

CA MFD FAILED, NO RED X, BRIEF PERIOD OF BURNING ELEC SMELL CB DID NOT POP. VERIFIED C/A MFD WAS SOURCE OF ELEC BURNING SMELL. DEFERRED C/A MFD (M) PROCEDURES C/W.

Part: FLOOR SUPPORT — CRACKED (FRAME 23) · airframe 31,464 hrs · 27,266 cycles

CENTER OMEGA BEAM FLANGE WAS CRACKED, AFT OF FRAME 23. FABRICATED AND DRILLED DOUBLER AND FILLER, AND INSTALLED IAW ERS-EM-53MR-3275.

Part: SHEAR TIE — CORRODED (FRAME 65) · airframe 31,464 hrs · 27,266 cycles

REAR FUSELAGE FRAME 65 SHEAR TIE WAS CORRODED ON CARGO DOOR CUTOUT. REMOVED AND REPLACED THE SHEAR TIE IAW ETD2018-145-048787.

Part: WIRE — BROKEN (EMEGENCY LIGHT) · airframe 31,464 hrs · 27,266 cycles

EMERGENCY LIGHT NR 3 WILL NOT ILLUMINATE. REPAIRED WIRES W192-8680-22 AND W192-8681-22 AT FRAME 31 STRINGER 16L IAW SWPM 20-21-00. OPS CHECKED GOOD IAW AMM 33-50-00.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 31,464 hrs · 27,266 cycles

NR 2 EMERGENCY LIGHT HADS BROKEN WIRES. R & R THE EMERGENCY LIGHT STRIP IAW AMM 33-50-12.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 31,464 hrs · 27,266 cycles

NR 7 EMERGENCY LIGHT STRIP HAD BROKEN WIRES. R & R THE EMERGENCY LIGHT IAW AMM 33-50-12.

Part: SHEAR TIE — CORRODED (FRAME 65) · airframe 31,464 hrs · 27,266 cycles

CORROSION FOUND ON THE SHEAR TIE AT FRAME 65. REMOVED AND REPLACED THE SHEAR TIE IAW ERS-EM-53MR-3273.

Part: FLOOR SUPPORT — CRACKED (FRAME 23) · airframe 31,464 hrs · 27,266 cycles

CABIN CENTER OMEGA BEAM CRACKED JUST AFT OF FRAME 23. REPAIRED THE OMEGA BEAM IAW ERS-EM-53MR-3275.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 31,464 hrs · 27,266 cycles

NR 6 EMERGENCY LIGHT STRIP HAD BROKEN WIRES. R & R THE EMERGENCY LIGHT STRIP IAW AMM 33-50-12.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 31,464 hrs · 27,266 cycles

NR 1 EMERGENCY LIGHT STRIP HAD BROKEN WIRES. R & R NR 1 EMERGENCY LIGHT STRIP IAW AMM 33-50-12.

Part: TERMINAL — BROKEN (EMERGENCY LIGHT) · airframe 31,464 hrs · 27,266 cycles

EMERGENCY LIGHT HAD A BROKEN TERMINAL. REMOVED AND REPLACED THE TERMINAL IAW SWPM 20-21-00, AND 20-50-00.

Part: COMPUTER — MALFUNCTIONED (LEFT) · airframe 30,846 hrs · 26,704 cycles

NO RAIM AT MAP, INTEG, LOSS OF CDI ON FIRST OFFICER`S SIDE, WENT AROUND DIVERTED FOR AN ILS. ACFT WAS REMOVED FROM SERVICE. INSPECTED & CLEANED ELECT CONNECTOR OF BOTH INAV RT & DRAINED ADC TRAPS & REPLACED NR 1 AHRC COMPUTER IAW MM 34-21-01 & 34-32-00, OPS CHECKED GOOD & LEAK TESTD GOOD.

Part: SMOKE GOGGLES — DAMAGED (COCKPIT) · airframe 30,766 hrs · 26,626 cycles

OBSERVER`S SMOKE GOGGLES DAMAGED. R & R OBSERVER'S SMOKE GOGGLE IAW AMM 35-10-00, NO FURTHER FAULTS.

Part: LENS — CRACKED (CABIN DOOR) · airframe 30,565 hrs · 26,414 cycles

EMERGENCY LIGHT COVER ON MAIN CABIN DOOR CRACKED. DEFER EMERGENCY LIGHT LENS INOPERATIVE IAW NEF 25-20A AUTH 030621M N. LIGHT FUNCTIONS NORMALLY. R & R PAX DOOR EMERGENCY LIGHT LENS COVER IAW AMM 25-23-04 NEF 25-20A AUTH 030621M N RESTORED.

Part: DOOR — LACK OF LUBE (MAIN PAX) · airframe 29,842 hrs · 25,771 cycles

MAIN CABIN DOOR DIFFICULT TO OPEN. LUBED MAIN CABIN DOOR IAW AE STANDARD MAINTENANCE PRACTICES NO FURTHER ACTION REQ.

Part: PLUG — INOPERATIVE (LT ENGINE) · airframe 29,746 hrs · 25,695 cycles

LEFT NR 1 ENGINE HAS EXHAUST SMOKE FROM TAIL PIPE AFTER SHUTDOWN AND ODOR OF BURNING OIL. R & R LT ENGINE SHAFT PLUG IAW EO-EM-7200-139. PERFORMED ENGINE RUNS, NO SMOKE NOTICED ON LT ENGINE SHUTDOWN.

Part: DOOR — LACK OF LUBE (MAIN PAX) · airframe 29,617 hrs · 25,585 cycles

F/A REPORTS CABIN DOOR DIFFICULT TO OPEN. LUBE AND OPS CHECK CABIN DOOR IAW AMM 53-21-02. OPS CHECK GOOD.

Part: ROLLER — LACK OF LUBE (PAX DOOR) · airframe 29,107 hrs · 25,174 cycles

MAIN DOOR VERY HARD TO OPEN. PERFORMED INSPECTION, CLEANED AND LUBRICATED DOOR ROLLERS IAW AMM 52-11-00 AND OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 28,728 hrs · 24,883 cycles

DURING B-INSPECTION, FOUND CABIN EMERGENCY LIGHTS BEHIND OVERWING EXITS NOT COMING ON. CFT REMOVED FROM SERVICE. R & R BATTERY POWER SUPPLY NR 4 IAW AMM 33-50-04. OPS CHECKED GOOD. ACFT RETURNED TO SERVICE.

Part: FLASHLIGHT — DEFECTIVE (COCKPIT) · airframe 28,427 hrs · 24,606 cycles

ON FLIGHT 3327 THE CREW REPORTED THE CAPTAIN’S FLASHLIGHT WAS DIM. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CAPTAIN’S FLASHLIGHT IAW EMB 140 AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 27,710 hrs · 24,007 cycles

DURING B INSPECTION FOUND THE RIGHT FWD EXTERIOR EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 2 EMERGENCY BATTERY AND POWER SUPPLY IAW EMB 140 AMM 33-50-04. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CRADLE — BROKEN (FLASHLIGHT) · airframe 27,596 hrs · 23,904 cycles

DURING MAINTENANCE INSPECTION FOUND THE FIRST OFFICER’S FLASHLIGHT CRADLE BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED & REPLACED THE FIRST OFFICER’S FLASHLIGHT CRADLE IAW AMM 33-50-16. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 27,232 hrs · 23,543 cycles

DURING B INSPECTION FOUND THE FORWARD CABIN FLASHLIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FORWARD CABIN FLASHLIGHT IN REFERENCE WITH EMB AMM TASKS 33-50-16-000-801-A AND 33-50-16-400-801-A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,192 hrs · 23,505 cycles

DURING MAINTENANCE INSPECTION FOUND THE EMERGENCY FLOOR LIGHT STRIP IN FRONT OF LAV HAS 1 SECTION THAT WOULD NOT LIGHT. NO PARTS. ITEM DEFERRED PER MEL. REMOVED AND REPLACED THE FLOOR PROXIMITY STRIP LIGHTS IAW AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD IAW 33-50-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,137 hrs · 23,452 cycles

DURING B INSPECTION FOUND THE FURTHEST AFT CEILING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LAMP IN FURTHEST AFT CEILING EMERGENCY LIGHT IAW EMB AMM TASKS 33-50-08-000-801-A AND 33-50-08-400-801-A. THE OPERATIONAL CHECK WAS GOOD AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: PROXIMITY SENSOR — DEFECTIVE (RT MLG) · airframe 26,944 hrs · 23,262 cycles

ON FLIGHT 4100 THE CREW REPORTED THEY RECEIVED A LANDING AIR/GROUND FAIL CAUTION MESSAGE WHEN THE GEAR CAME DOWN ON FINAL. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT MAIN LANDING GEAR WEIGHT ON WHEELS PROXIMITY SWITCH IAW EMB 140 AMM 32-63-01. THE OPERATIONAL CHECK WAS GOOD IAW EMB 140 32-63-00, MULTIPLE GEAR SWINGS ALSO WERE SATISFACTORY. OTHER PARTS REMOVED AND REPLACED: NUT PLATE, PART NUMBER MS14145L4. BOLT PART, NUMBER AN4-23. COTTER PIN, PART NUMBER MS24665-134. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE — BROKEN (CABIN) · airframe 26,964 hrs · 23,282 cycles

DURING MAINTENANCE INSPECTION FOUND THE NR 1 FORWARD LEFT EMERGENCY LIGHT STRIP WIRE BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CONNECTOR ON NR 1 EMERGENCY LIGHT STRIP REF EMB 145 SWPM 20-21-00. THE NR 1 EMERGENCY LIGHT STRIP OPERATIONAL CHECK WAS GOOD REF EMB 145 AMM 33-50-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 26,939 hrs · 23,258 cycles

DURING MAINTENANCE INSPECTION FOUND A CRACK IN LEFT OMEGA BEAM OUTBOARD SUPPORT BETWEEN FRAMES 47 AND 48. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT OMEGA BEAM SUPPORT FROM FRAME 47 TO 53 PER SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 26,939 hrs · 23,258 cycles

DURING MAINTENANCE INSPECTION FOUND A CRACK IN THE RIGHT OMEGA BEAM OUTBOARD SUPPORT BETWEEN FRAMES 47 AND 48. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED SUPPORT ON OMEGA BEAM FRAME 47 TO 48 RIGHT IAW SRM 51-40-06. RECEIVED NEW PARTS P/N 140-04213-607/ P/N 140-04213-601 LUCARDED AND DRILLED HOLES RFM EMB 140 SRM 51-20-03. INSTALLED NEW RIGHT OUTBOARD OMEGA BEAM SUPPORT BETWEEN FRAMES 47 & 48 REF EMB 140 SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ROLLER — LACK OF LUBE (PAX DOOR) · airframe 26,710 hrs · 23,036 cycles

FLIGHT 4216, FLIGHT ATTENDANT REPORTED MAIN CABIN DOOR IS DIFFICULT TO OPEN. AIRCRAFT REMOVED FROM SERVICE. LUBED MAIN DOOR ROLLERS, OPEN AND CLOSE PAX CABIN DOOR FOUND TO BE NORMAL ALL IAW AMM 52-10-00. AIRCRAFT RETURNED TO SERVICE.

Part: CRADLE — DAMAGED (CABIN) · airframe 26,413 hrs · 22,737 cycles

DURING MAINTENANCE INSPECTION FOUND THAT THE FORWARD PASSENGER CABIN FLASHLIGHT CRADLE SHOWS EVIDENCE OF OVERHEATING. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FORWARD PASSENGER CABIN FLASHLIGHT CRADLE IAW EMB 140 AMM CHAPTER 33-50-16. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CRADLE — CRACKED (COCKPIT) · airframe 26,413 hrs · 22,737 cycles

DURING MAINTENANCE INSPECTION FOUND THE CAPTAINS FLASHLIGHT CRADLE CRACKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CAPTAINS FLASHLIGHT CRADLE IAW EMB 14- AMM CHAPTER 33-50-16. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: MOUNT — GOUGED (LT ENGINE) · airframe 26,283 hrs · 22,615 cycles

DURING B INSPECTION, FOUND ON THE LEFT ENGINE THE LEFT AFT LOWER ENGINE MOUNT INNER SURFACE GOUGED AND CORRODED. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT ENGINE AFT LOWER MOUNT IAW AMM 71-20-00-000-801-A AND 71-20-00-400-801-A. AIRCRAFT RETURNED TO SERVICE.

Part: CRADLE — BROKEN (FLASHLIGHT) · airframe 26,204 hrs · 22,535 cycles

FLIGHT 4227, CAPTAIN’S FLASHLIGHT HOLDER IS BROKEN. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED FLASHLIGHT HOLDER IAW AMM 33-50-16. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: DOOR — OUT OF ADJUST (LAVATORY) · airframe 25,691 hrs · 22,087 cycles

DURING MAINTENANCE INSPECTION FOUND THE FIRE EXTINGUISHER DOOR IN LAV VERY DIFFICULT TO OPEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. ADJUSTED AND LUBE DOOR IAW AMM 25-20-00. NO PARTS REMOVED OR REPLACED. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 25,681 hrs · 22,078 cycles

DURING MAINTENANCE INSPECTION FOUND THE EMERGENCY LIGHTS FLOOR STRIPS AT 10 AND 11 WOULD NOT ILLUMINATE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 3 BATTERY AND BATTERY CHARGER EMERGENCY LIGHT POWER SUPPLY IAW EMB 1340 AMM 33-50-09. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LATCH — FAILED (INSPECTION PANEL) · airframe 25,488 hrs · 21,928 cycles

FLIGHT 2782, CREW REPORTED THE PANEL IN THE LAVATORY TO INSPECT FIRE EXTINGUISHER IS DIFFICULT TO OPEN. AIRCRAFT REMOVED FROM SERVICE. REPLACED LATCH ON LAVATORY UNDERSINK DOOR IAW AMM 25-40-08. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,277 hrs · 21,778 cycles

DURING MAINTENANCE BASE INSPECTION FOUND THE EMERGENCY LIGHT INOPERABLE AT SEAT/ ROW 3. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AISLE EMERGENCY LIGHT LAMP AT ROW 3 IAW EMB 140 AMM 33-50-08. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: DOOR — OUT OF ADJUST (CABIN) · airframe 23,992 hrs · 20,749 cycles

ON FLIGHT 4289 THE CREW REPORTED THE MAIN CABIN DOOR WAS HARD TO OPEN, IT SEEMED TO JAM ON THE UPPER RIGHT SIDE. THE AIRCRAFT WAS REMOVED FROM SERVICE. ADJUSTED MAIN CABIN DOOR IAW EMB AMM 52-18-00-820-012. THE OPERATIONAL CHECK WAS GOOD. REF NRWC 803-ORD-00341. NO PARTS REMOVED OR REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ISIS UNIT — MALFUNCTIONED (COCKPIT) · airframe 22,387 hrs · 19,451 cycles

ON FLIGHT 3201 DURING THE CLIMB THE CREW REPORTED THE STANDBY HORIZONTAL WENT BLANK ON THE INTERGRATED STANDBY INSTRUMENT SYSTEM. THE CREW ELECTED TO RETURN TO DFW DUE TO WEATHER. THE AIRCRAFT LANDED WITHOUT INCIDENT AND WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE INTERGRATED STANDBY INSTRUMENT SYSTEM IAW AMM 34-01-01. THE FUNCTIONAL AND LEAK CHECK WAS GOOD IAW AMM 34-13-00, NO LEAKS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FRAME — CRACKED (FUSELAGE) · airframe 22,345 hrs · 19,413 cycles

DURING MAINTENANCE BASE VISIT FOUND FRAME 23 TO BE CRACKED IN TWO PLACES BETWEEN STRINGERS 15 RIGHT AND 17 RIGHT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED FRAME 23 IAW EO EM-53MR-1695. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 22,288 hrs · 19,368 cycles

FOR FLIGHT 980 PERFORMED PERMANANT REPAIR OF THE RIGHT FORWARD FUSELAGE SKIN PART B OF EO EM-53MR-1682 TDMI 803530692 DUE TO BIRD STRIKE DAMAGE. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED REPAIR ON RIGHT FUSELAGE NOSE SECTION IAW AEA EO EM-53MR-1682R1 PART B TDMI 803530692. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: POTENTIOMETER — OUT OF ADJUST (NLG STEERING) · airframe 21,276 hrs · 18,590 cycles

ON FLIGHT2777 DURING TAXI THE CREW REPORTED THE STEERING DISENGAGED WHEN USING THE RUDDER PEDALS. THE AIRCRAFT WAS REMOVED FROM SERVICE. ADJUSTED THE LOAD POTENTIOMETER IAW AMM 32-50-05. NO PARTS REMOVED OR REPLACED. THE OPERATIONAL AND STEERING CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 20,605 hrs · 18,000 cycles

DURING A MAINTENANCE CHECK FOR FLIGHT 4452 FOUND THE EMERGENCY AISLE LIGHT NR 2 AND RIGHT FORWARD OVERWING LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 2 BATTERY CHARGER AND BATTERY IAW MTX WC 33-700-19. PERFORMED AN OPERATIONAL CHECK IAW MAINTENANCE WORKCARD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 19,262 hrs · 18,281 cycles

ON FLIGHT 3482, CREW REPORTED EXIT ROW 12 EMERGENCY EXIT LIGHT IN THE CEILING DOES NOT ILLUMINATE. AIRCRAFT REMOVED FROM SERVICE. PERFORMED OPERATIONAL CHECK OF EMERGENCY LIGHT SYSTEM IAW EMB145 AMM 33-50-00. NO FAULTS NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: ALTIMETER — MALFUNCTIONED (COCKPIT) · airframe 15,199 hrs · 13,355 cycles

ABORTED TAKEOFF, DURING TAKEOFF ROLL AT 50 KNOTS THE STAND BY ALTIMETER INDICATOR WENT TO CAGE. REPLACED STAND BY ATT INDICATOR AIRCRAFT RETURNED TO SERVICE.

Part: TIRE — DEFLATED (MLG) · airframe 14,828 hrs · 13,080 cycles

AFTER LANDING, DURING TAXI IT TOOK MORE POWER THAN NORMAL TO TAXI. A BRAKE OVERHEAT INDICATION WAS OBSERVED ON EICAS. NR 3 TIRE WAS FOUND TO BE FLAT. REMOVED AND REPLACED NR 3 MLG WHEEL AND TIRE ASSY IAW WORK CARD NR 32-700-11 2. REMOVED AND REPLACED NR 3 MLG BRAKE ASSY IAW WORK CARD NR 32-600-14 3. REMOVED AND REPLACED NR 4 MLG WHEEL AND TIRE ASSY IAW WORKCARD NR 32-700-11. NR 3 BRAKE PN-21707 SN-0100 NR 4 MLG TIRE PN-31641 SN-1872. AIRCRAFT RETURNED TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 13,064 hrs · 11,779 cycles

FOUND SERVICED DOOR FRAME LOWER CENTER SILL FOUND CORRODED. REMOVED EXISTING SILL, CLEANED AND TREATED REPAIR AREA. INSTALLED NEW SILL IAW EMB EMB SRM 51-40-02. RESTORED PROTECTED FINISH, RETURNED AIRCRAFT TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 13,064 hrs · 11,779 cycles

PREVIOUS REPAIR ON LEFT OMEGA BEAM AT FRAME 20 CORRODED. REMOVED EXISTING REPAIR, CLEANED AND TREATED REPAIR AREA. FABRICATED AND INSTALLED REPAIR DOUBLER IAW EMB SRM 53-00-10. RESTORED PROTECTIVE FINISH, RETURNED AIRCRAFT TO SERVICE.

Part: FRAME — GOUGED (FUSELAGE) · airframe 13,064 hrs · 11,779 cycles

FOUND LOWER SECTION OF FRAME 81 GOUGED. PERFORM BLEND AND NDT INSPECTION OF GOUGE. FABRICATED INTERNAL AND EXTERNAL REPAIR DOUBLERS. INSTALLED DOUBLERS IAW EMB SRM 53-32-04 AND C2007-145/00878. RETURNED AIRCRAFT TO SERVICE.

Part: SEAL — DAMAGED (WINDSHIELD) · airframe 12,683 hrs · 11,510 cycles

BANGING NOISE HEARD IN COCKPIT AFTER TAKEOFF. FOUND CAPTAIN'S HUMP SEAL LIFTING. PERFORMED TEMPORARY REPAIR, RETURNED AIRCRAFT TO SERVICE.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT)

LGA - LEFT SIDE FORWARD EXTERIOR EMERGENCY LIGHT, EMERGENCY LIGHT AT ROW 3 AND COCKPIT CEILING EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY POWER SUPPLY CHARGER NR 1 IAW MM 33-50-04. OPS CHECK GOOD. (M)

Part: SILL — CORRODED (CARGO BAY)

ABI - THE CARGO DOOR OPENING LOWER SILL WAS FOUND TO BE CORRODED. REMOVED THE CORRODED LOWER DOOR SILL. INSTALLED NEW SILL IAW EMB SRM, SRM 145.1142 REV 28, CHAPTER 51-40-02 AND 51-20-03. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

THE LEFT OMEGA BEAM AT FRAME 20 WAS FOUND CORRODED. PERFORMED A CUTOUT OF THE DAMAGED AREA TO REMOVE THE CORROSION. FABRICATED AN EXTERNAL ANGLE, FILLER AND TWO SHIMS. REPAIR DONE IAW EMB 145 SRM, SRM EMB-145/1142 REV 28, CHAPTER 53-21-10 FIG 202. (M)

Part: STRINGER — CHAFED (FUSELAGE)

FOUND STRINGER 19L WAS FOUND CHAFED. BLENDED THE CHAFED AREA AND PERFORMED NDT. FABRICATED A REINFORCEMENT ANGLE AND TWO SHIMS. REPAIR DONE IAW EMB 145 SRM, SRM EMB 145/1142 REV 28 CHAPTER 53-24-02. (M)

Part: STRINGER — CHAFED (FUSELAGE)

ABI - FOUND STRINGER 19R WAS FOUND CHAFED. BLENDED THE CHAFED AREA AND PERFORMED NDT. FABRICATED A REINFORCEMENT ANGLE AND TWO SHIMS. REPAIR DONE IAW EMB 145 SRM, SRM EMB 145/1142 REV 28 CHAPTER 53-24-02. (M)

Part: BOLT — BROKEN (RT AILERON)

DURING PHASE 2A INSPECTION, FOUND RIGHT AILERON DAMPER ROD END BOLT BROKEN. REMOVED AND REPLACED BOLT. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: RELAY — INOPERATIVE (NR 2 FIRE DETECT) · airframe 7,547 hrs · 7,284 cycles

ICE CONDITION ANTI-ICE WARNING. ENGINE 2, FIRE DETECTION FAIL EICAS MESSAGE. REPLACED AIR GROUND RELAY AT LT RELAY SUPPORT B14. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.(K)

Part: FAN — OVERHEATED (AVIONICS BAY)

SJC - FLT 3183 - DURING CRUISE FLIGHT CREW REPORTED A STRONG ELECTRICAL BURNING ODOR IN THE COCKPIT. NO EMERGENCY DECLARED. LANDED SAFELY WITHOUT INCIDENT. MAINTENANCE FOUND INSULATION IN FORWARD AVIONICS FAN CAUSING OVERHEAT CONDTION. INSULATION WAS REMOVED AND OPERATIONAL CHECK OF FAN WAS SATISFACTORY. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: RELAY — INOPERATIVE (PITOT SYSTEM)

CREW RECEIVED A PITOT THREE INOPERATIVE ON EICAS. MESSAGE FLICKERING THEN EXTINGUISHED. AFTER MESSAGE EXTINGUISHED FA REPORTED SMOKE IN GALLEY AND CREW NOTED ODOR IN COCKPIT. CREW DECLARED EMERGENCY. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED NR 3 PITOT TUBE CURRENT SENSING RELAY, AND RELAY BASE, IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: STRINGER — CHAFED (FUSELAGE)

ABI - DUIRNG A MBV INSPECTION, STRINGER 19L AT FRAME 53 WAS FOUND CHAFED BELOW SRM LIMITS. BLENDED THE CHAFED AREA AND PERFORMED AN NDT INSPECTION WITH NO REJECTABLE INDICATIONS. FABRICATED A REPAIR ANGLE AND SHIMS. REPAIR DONE IAW EMB SRM, SRM 145/1142 REV 21, CHAPTERS 53-24-02 FIGURE 201. (M)

Part: SILL — CORRODED (SERVICE DOOR)

ABI - DURING AN IMBV INSPECTION, THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED BELOW SRM LIMITS. REMOVED NUTPLATE AND BLENDED THE CORRODED AREA OF THE CENTER SILL AND PERFORMED AN NDT INSPECTION WITH NO DEFECTS NOTED. FABRICATED A DOUBLER. REPAIR DONE IAW AEA ETN EM-53-036R1 AND STANDARD EMB SRM, SRM 145/1142 REV 20, PRACTICES. (M)

Part: GUSSET — CORRODED (GALLEY)

THIS IS A LEVEL TWO FINDING FOUND DURING A MBV INSPECTION, GALLEY FORWARD DIAMOND GUSSET CORRODED. INSTALLED NEW DIAMOND GUSSET IN GALLERY AREA IAW EMB 140 SRM 51-40-02. (M)

Part: DOUBLER — CORRODED (SERVICE DOOR)

THIS IS A LEVEL TWO FINDING FOUND DURING A MBV INSPECTION, SERVICE DOOR CENTER SILL CORRODED. INSTALLED SERVICEABLE DOUBLER IAW ETN NR EM-53-036R1. (M)

Part: SUPPORT — CORRODED (GALLEY)

THIS IS A LEVEL TWO FINDING, FOUND DURING A MBV INSPECTION, INBOARD GALLEY RAMP SUPPORT CORRODED. REMOVED AND INSTALLED NEW INBOARD GALLEY RAMP SUPPORT IAW EMB 140 SRM 51-40-02. (M)

Part: ECU — FAILED (T/E FLAP)

BOS - FLT 4757 - DURING APPROACH WHEN FLAPS WERE SELECTED CREW RECEIVED A FLAP FAIL, FLAP LOW SPEED, AND LOST FLAP INDICATION ON EICAS. AN EMERGENCY WAS DECLARED AND AIRCRAFT WAS LANDED WITHOUT FURTHER INCIDENTS. MAINTENANCE REMOVED AND REPLACED THE FLAP ELECTRONIC CONTROL UNIT IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)