N855AE

Part: SKIN — DENTED (FUSELAGE) · airframe 32,722 hrs · 29,368 cycles

SUPPLEMENTAL FUSELAGE DENTED BETWEEN FR1 AND FR3. C/A-REPLACED RT FF1 SKIN PANEL IAW SRM 51-40-02 AND 51-21-01.

Part: CRADLE — CRACKED (FLASHLIGHT) · airframe 32,530 hrs · 29,163 cycles

FA'S FLASHLIGHT BASE CRACKED-C/A-RAR FLIGHT ATTENDANTS FLASHLIGHT BASE IAW EMB AMM 33-50-16-000-801-A & 33-50-16-400-801-A OPC GOOD AT THIS TIME NO FURHTER DEFEDCTS NOTED END

Part: INVERTER — INOPERATIVE (EMEGENCY LIGHTS) · airframe 32,210 hrs · 28,860 cycles

CABIN RH EMERGENCY EXIT IDENTIFIER INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT DC/AC INVERTER #5 IAW AMM 33-50-11. EMERGENCY LIGHT OPERATIONAL CHECK GOOD.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 32,022 hrs · 28,659 cycles

COCKPIT CEILING EMERGENCY LIGHT INOP. C/A-RELAMPED COCKPIT CEILING EMERGENCY LIGHT OPC GOOD AMM 35-50-00.

Part: BATTERY — DISCHARGED (CABIN) · airframe 31,375 hrs · 28,075 cycles

BOTH LT AND RT AFT OVERWING EXTERIOR EMERGENCY LIGHTS FAILED FUNCTIONAL CHECK IAW MTX WC 33-700-17. REMOVED AND REPLACED EMERGENCY LIGHT CHARGER AND BATTERY AT POSITION NR 4 IAW MTX WC 33-700-19, OPC GOOD IAW MTX WC 33-700-17. BATTERY CHARGER ASSY 11-0049 S/N 12823

Part: BATTERY — DISCHARGED (CABIN) · airframe 31,275 hrs · 27,969 cycles

FOUND EXTERNAL EMERGENCY LIGHTS ABOVE WING ON RT & LT INOP. C/A-REMOVED AND REPLACED BATTERY & BATTERY POWER SUPPLY IAW AMM 33-50-04. OPC GOOD. NO FURTHER DEFECTS NOTED AT THIS TIME. BATTERY CHARGER ASSY P/N 11-0049 S/N 18121.

Part: OIL SYSTEM — WITHIN LIMITS (NOT AN SDR) · airframe 31,136 hrs · 27,849 cycles

HIGH SPEED ABORT TAKEOFF AT 80KTS DUE TO #2 ENGINE OIL PRESSURE BEING IN THE CAUTION RANGE IN TAKE OFF POWER. PRESSURE WAS ABOUT 150-155 PSI AFTER ABORT ALL INDICATION WAS IN TH GREEN.CORRECTIVE ACTION PERFORMED POWER ENGINE WITH CREW OIL PRESSURE INDICATION MAX PSI WAS 120PSI. PRESSURE IS WITHIN LIMITS PER ROLLS ROYCE AE3007A SERIES MM TASK 79-00-00-20-801 TABLE 6

Part: FLASHLIGHT — INOPERATIVE (AFT CABIN) · airframe 31,110 hrs · 27,830 cycles

MEL 25-53 AUTH # 120588-C LG PG 4420629-1 AFT EMERGENCY FLASH LIGHT NOT CHARGING-C/A-PERFORMED FUCTIONAL TEST OF AFT F/A FLASH LIGHT IAW E-140 AMM 33-51-01 AND CHECKS GOOD MEL RESTORED

Part: BATTERY — DISCHARGED (CABIN) · airframe 31,080 hrs · 27,799 cycles

LT AND RT EXTERNAL OVERWING EMERGENCY LIGHTS INOP. REMOVED AND REPLACED #4 EMERGENCY BATTERY IAW AMM 33-50-04 AND ETN-EM-33-020R1 OPC GOOD.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 31,080 hrs · 27,799 cycles

CABIN AFT EMER FLASHLIGHT RED CHARGING LIGHT INOP. REMOVED AND REPLACED FLASHLIGHT AND HOLDER ASSY IAW AMM 33-50-16 NO FIX.

Part: DISPLAY — MALFUNCTIONED (ISIS) · airframe 30,994 hrs · 27,694 cycles

ISIS WENT DARK, THEN RE-APPEARED WITH WHITE "ATT" INSIDE RED BOX. NO ATTITUDE INFORMATION PRESENTED. OTHER INSTRUMENTATION MATCHED PRIMARY DISPLAYS QRH PROC APPLIED, NO EFFECT. EMERGENCY DECLARED.-C/A-ACCOMPLISHED FIM TASK 34-1-00-810-801-A STEPS 1 &3. DISCREPENCY IS TRASITORY CONDITION. AIRCRAFT OKAY FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,757 hrs · 27,466 cycles

ROW 11 CEILING EMERGENCY LT INOP. REMOVED AND REPLACED ROW 11 CEILING EMERGENCY LIGHT BULB IAW AMM 33-50-08-000-801-A AND 33-50-08-400-801-A OPC GOOD END.

Part: ELECTRONIC UNIT — FAILED (LANDING GEAR) · airframe 30,723 hrs · 27,438 cycles

AFTER TAKEOFF FO CALLED FOR GEAR UP. EICAS INDICATION WENT FROM DOWN (GREEN) TO UP (WHITE) WITH NO INTRANSIT. AFTER REACHING 10,000 CA LOOKED AT RMU BACKUP AND IT SHOWED GEAR DOWN AND LOCKED. EICAS SHOWING GEAR UP. CREW RAN ABNORMAL LANDING GEAR EXTENSION. CREW DID A COUPLE LOW PASSES TO A MISSED APPROACH. WE HAD A FEW ATC AND OTHER A/C SAY IT APPEARED THE RIGHT MAIN WAS SWINGING. IN LANDING CONFIG WITH FLAPS 22 OF 45 THRUST RATING LEVER CHANGED FROM CRZ TO T/O EMERGENCY LANDING CHECKLIST WAS PERFORMED-C/A-. SUPPLEMENTAL PERFORMED CMC DNLD IAW 45-45-00. CMC = LG UP/DN PROX SW / LEGU FAIL WITH 1 OCCURRENCE ON 10-10-18 AT 19:00:05 GMT. PERFORMED LDG EXTENSION / RETRACTION CHECK IAW CH 32-00-00. EXT/RET CHK OK WITH NO ABNORMAL INDICATIONS. REMOVED AND REPLACED LGEU IAW AMM 32-32-01. REPERFORMED LDG EXTENSION/RETRACTION ADJUSTMENT TEST IAW AMM 32-30-00. NO ABNORMAL INDICATIONS OPS CHECK GOOD.

Part: UNKNOWN — ODOR · airframe 30,683 hrs · 27,398 cycles

BURNING PLASTIC SMELL-C/A-PERFORMED ETN-EM-72-034 NO BURNING PLASTIC SMELL NOTED TEST PASSED WITH ODOR ATTRIBUTES NR 1

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 30,452 hrs · 27,208 cycles

LEFT AFT EXTERIOR EMERGENCY LIGHT WAS INOPERATIVE. R & R THE LAMP IAW AMM 33-50-10. OPS CHECKED GOOD. NO DEFECTS NOTED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,452 hrs · 27,208 cycles

EMERGENCEY LIGHT ON THE PAX DOOR WAS INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY LIGHT ASSY IAW AMM 33-50-10. OPS CHECKED GOOD. NO DEFECTS NOTED.

Part: LIGHT — INOPERATIVE (ROWS 5 & 6A) · airframe 29,949 hrs · 26,683 cycles

ROWS 5 & 6A EMERGENCY LIGHT WAS INOPERATIVE. R & R THE EMERGENCY LIGHT IAW AMM 33-50-12, OPS CHECKED GOOD.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 28,988 hrs · 25,654 cycles

NR 4 AND 5 EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED THE NR 3 BATTERY AND CHARGER IAW AMM 33-50-04. OPS CHECKED GOOD.

Part: FLOOR SUPPORT — CORRODED (FRAMES 22-23) · airframe 28,988 hrs · 25,654 cycles

LEFT OMEGA BEAM CORRODED ON THE SIDE WALL, FRAMES 22 - 23. REPAIRED IAW ERS-EM-53MR-2985.

Part: SKIN — CHAFED (RUDDER) · airframe 28,988 hrs · 25,654 cycles

RUDDER LEADING EDGE CHAFED. ACCOMPLISHED A REPAIR TO THE RUDDER LEADING EDGE IAW ERS-EM-55MR-584.

Part: FLOOR SUPPORT — CORRODED (FRAMES 56-59) · airframe 28,988 hrs · 25,654 cycles

CENTER OMEGA BEAM CORRODED FRAMES 56 - 59. REPAIRED IAW EO EM-53MR-1518R3, PART B.

Part: FLOOR SUPPORT — CORRODED (FRAMES 57-59) · airframe 28,988 hrs · 25,654 cycles

LEFT OMEGA BEAM CORRODED AT AND AROUND THE CROSSBEAM, FRAMES 57 - 59. REPAIRED IAW EO EM-53MR-1518R3, PART A.

Part: DOOR SILL — CORRODED (SERVICE DOOR) · airframe 28,988 hrs · 25,654 cycles

SERVICE DOOR LOWER CENTER SILL CORRODED. REMOVED AND REPLACED THE DOOR SILL IAW SRM 51-40-02.

Part: STRUCTURE — CORRODED (E/E BAY DOOR) · airframe 28,988 hrs · 25,654 cycles

AFT AVIONICS DOOR CORRODED UNDER THE FWD LOWER GUIDE. ACCOMPLISHED A PERMANENT REPAIR IAW ERS-EM-52MR-818

Part: ATTACH FITTING — WORN (RT AILERON) · airframe 28,988 hrs · 25,654 cycles

FOUND RT AILERON ACTUATOR ATTACH FITTING BUSHING HOLES TO BE WORN BEYOND LIMITS. REPLACED THE ATTACH FITTING IAW EO EM-27MR-112.

Part: RETAINER — CORRODED (WINDSHILED) · airframe 28,988 hrs · 25,654 cycles

CO-PILOT`S WINDSHIELD OUTER RETAINER HAS CORROSION ON THE BOTTOM. WORKED THE AREA, FOUND THE RETAINER TO BE WITHIN ALLOWABLE LIMITS IAW ERS-EM-5600-107.

Part: FRAME — CRACKED (FRM 23) · airframe 28,988 hrs · 25,654 cycles

FRAME 23 CRACKED BETWEEN STRINGERS 15R - 16R. ACCOMPLISHED A SPLICE REPAIR IAW EO EM-53MR-1808.

Part: FRAME — CORRODED (FRM 65) · airframe 28,988 hrs · 25,654 cycles

FRAME 65 CORRODED AT STRINGER 16L. REPAIRED THE FRAME IAW ERS-EM-53MR-2982.

Part: BEAM — CORRODED (FRAMES 37-38) · airframe 28,988 hrs · 25,654 cycles

CENTER AISLE BEAM CORRODED AND CHAFED BETWEEN FRAMES 37-38. REMOVED AND REPLACED THE BEAM IAW SRM 51-40-02.

Part: CROSSBEAM — CORRODED (FRAME 20) · airframe 28,988 hrs · 25,654 cycles

FRAME 20 CENTER AISLE CROSSBEAM CORRODED. REMOVED AND REPLACED THE CROSSBEAM IAW SRM 51-40-02.

Part: STRUCTURE — CORRODED (STRINGER 16L) · airframe 28,988 hrs · 25,654 cycles

LATERAL L SHAPE CORRODED AT STRINGER 16L.REPAIRED THE LATERAL L SHAPE IAW ERS-EM-53MR-2982.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,857 hrs · 25,522 cycles

NUMBER 1 & NUMBER 8 EMER LIGHT STRIPS ARE INOPERATIVE. R & R NR 1 & NR 8 EMER LIGHT STRIP IAW AMM 33-50-12. OPERATIONS CHECKED GOOD. FLOOR PROXIMITY LIGHT STRIP PN 6690-3 POSITION 1.

Part: HANDLE — DEFECTIVE (PAX DOOR) · airframe 28,719 hrs · 25,361 cycles

FLIGHT ATTENDANT REPORTS MAIN PASSENGER DOOR DIFFICULT TO OPEN & CLOSE PROPERLY. INSTALLED & INDEXED MAIN CABIN DOOR HANDLE IAW 52-11-01.

Part: DOOR — LACK OF LUBE (CABIN) · airframe 28,684 hrs · 25,321 cycles

PREVIOUS CREW REPORTED PAX DOOR HARD TO OPEN. LUBRICATED MAIN PAX DOOR IAW AMM 52-18-00. OPERATIONS CHECKED GOOD.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 28,681 hrs · 25,318 cycles

EMERGENCY FLOOR PATH LIGHTS AT SEATS 15 & 16 HAVE BROKEN WIRES. REPAIRED IAW WM 33-50-50 & SWPM 20-21-00. OPS CHECKED GOOD IAW AMM 33-50-12.

Part: ROLLER — LACK OF LUBE (CABIN DOOR) · airframe 28,614 hrs · 25,257 cycles

FLIGHT ATTENDANT ADVISES MAIN CABIN DOOR HANDLE HARD TO OPEN. CLEANED & LUBED MAIN PAX DOOR ROLLERS AS REQUIRED. DOOR OPENS & CLOSES NORMALLY WITH NO DEFECTS NOTED. REF MM 52-18-00.

Part: DOOR — OUT OF ADJUST (CABIN) · airframe 28,507 hrs · 25,139 cycles

MAIN CABIN DOOR IS DIFFICULT TO OPEN & CLOSE. PERFORMED & ADJUSTED PAX MAIN DOOR IAW AMM 52-18-00 TO REDUCE AVERAGE MAX LOAD OF THE INTERNAL HANDLE PULL TEST TO A VALUE LESS THAN 45 LBS ON OR BEFORE 200 FC ETN EM 52-029.

Part: ROLLER — LACK OF LUBE (FUSELAGE) · airframe 28,464 hrs · 25,103 cycles

FLIGHT ATTENDANT REPORTS MAIN PAX DOOR HARD TO OPEN & CLOSE. TRANSFERRED TO NRWC 855-DFW-01910. LUBED MAIN DOOR FRAME ROLLERS IAW AMM 53-21-02. ALSO LUBED BOTH MAIN DOOR & FRAME SEALS. OPERATIONS CHECKED GOOD IAW AMM 52-18-00.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,453 hrs · 25,097 cycles

SERVICE DOOR EMER LIGHT INOPERATIVE. R & R LIGHT BULB AT SERVICE DOOR EMER LIGHT IAW AMM 33-50-10. OPERATIONS CHECKED GOOD.

Part: DOOR — OUT OF ADJUST (CABIN) · airframe 28,424 hrs · 25,073 cycles

MAIN CABIN DOOR DIFFICULT TO OPEN. TRANSFERRED TO NRWC 855-ORD-01906. ADJUSTED ROLLERS, LOWER GUIDES & UPPER & LOWER BARS IAW AMM 52-18-00-820-805 & AMM 52-18-00-820-806. OPERATIONS CHECKED IAW AMM 52-18-00-820-001. OPERATIONS CHECKED GOOD. REF NRWC 855-ORD-01906.

Part: GUIDE — DEFECTIVE (CABIN DOOR) · airframe 28,389 hrs · 25,040 cycles

MAIN DOOR HANDLE VERY HARD TO OPEN & CLOSE. R & R ALL FOUR GUIDES IAW AMM 52-18-00. ADJUSTED UPPER & LOWER BARS IAW AMM 52-18-00. OPERATIONS CHECKED GOOD.

Part: DOOR — OBSTRUCTED (CABIN) · airframe 28,388 hrs · 25,039 cycles

MAIN DOOR VERY HARD TO OPEN & CLOSE. REMOVED DEBRIS & OPERATIONS CHECK DOOR IAW AMM 52-00-00. OPERATIONS CHECKED GOOD.

Part: MECHANISM — LACK OF LUBE (CABIN DOOR) · airframe 28,367 hrs · 25,021 cycles

MAIN CABIN DOOR HARD TO OPERATE. LUBRICATION OF MAIN DOOR & LOCKING MECHANISM IAW AMM 52-11-00-PAGE 301.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 27,696 hrs · 24,444 cycles

RIGHT FWD EXTERNAL EMER LIGHT INOPERATIVE. R & R RT FWD EXTERNAL EMER LIGHT ASSEMBLY IAW AMM 33-50-10. OPERATIONS CHECKED GOOD.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 27,432 hrs · 24,237 cycles

RIGHT & LEFT REAR FUSELAGE EXTERNAL EMER LIGHTS INOPERATIVE. R & R NR 4 EMER LIGHT BATTERY CHARGER ASSEMBLY IAW AMM 33-50-04. OPERATIONS CHECKED GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 27,406 hrs · 24,215 cycles

BOTH LT & RT OVERWING EMER LIGHT INOPERATIVE. R & R BATTERY & POWER SUPPLY NR 4 IAW AMM 33-50-04. OPERATIONS CHECKED GOOD. BATTERY CHARGER ASSEMBLY PN 11-0049 & SN 14336.

Part: RADAR — FAILED (WEATHER RADAR) · airframe 27,024 hrs · 23,919 cycles

RADAR WAS TURNED ON INFLIGHT & AMBER WX WAS DISPLAYED ON PFD, WHEN TESTED RADAR FAIL WAS DISPLAYED WITH CODE 11. R & R WX RADAR ASSEMBLY IAW AMM 34-42-01. OPERATIONS CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 26,943 hrs · 23,852 cycles

CAPTAIN`S COCKPIT FLASHLIGHT RED LIGHT NOT ON, FOR RECHARGING. R & R CAPTAIN`S COCKPIT FLASHLIGHT AS REQUIRED.

Part: MANIFOLD — FAULTY (ANTI-ICE SYSTEM) · airframe 26,643 hrs · 23,603 cycles

CLIMBING OUT IN ICING CONDITION STAB ANTI-ICE FAIL ON EICAS. FOLLOWED AOM CHECKLIST & WAS NOT ABLE TO RESTORE SYS. R & R HORIZONTAL STAB SWITCH MANIFOLD IAW AMM 30-12-14. PERFORMED OPERATIONAL CHECK OF ANTI-ICING SYS IAW AMM 30-00-00-700-802A. OPERATIONS CHECKED GOOD.

Part: CONNECTOR — DIRTY (EXTERIOR LIGHT) · airframe 26,339 hrs · 23,332 cycles

RIGHT OVERWING EXTERIOR EMER LIGHT INOPERATIVE. REMOVED PANEL OVERWING LIGHT ASSEMBLY. CLEANED CONNECTOR & SECURED CONNECTOR & PANEL. OPERATIONS CHECKED GOOD IAW SWPM 20-50-00.

Part: WIRE — DAMAGED (EMERGENCY LIGHTS) · airframe 26,335 hrs · 23,326 cycles

EXTERIOR SERVICE DOOR MOUNTED EMERGENCY LIGHT INOPERATIVE. REPAIRED WIRE W716-0007-20 IAW SWPM 20-21-00. EMERGENCY LIGHTS CHECKED GOOD IAW AMM 33-50-00.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 26,193 hrs · 23,201 cycles

FLIGHT ATTENDANT FLASHLIGHT EMERGENCY LIGHT SWITCH IS INOPERATIVE. R & R FLIGHT ATTENDANT EMERGENCY FLASHLIGHT IAW AMM 33-50-16. OPERATIONS CHECKED GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 25,885 hrs · 22,921 cycles

SERVICE DOOR EMERGENCY LAMP INOPERATIVE. R & R SERVICE DOOR EMERGENCY LIGHT LAMP IAW AMM 33-50-09-000-801-A & 33-50-09-400-801-A. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: SIGN — INOPERATIVE (OVERWING) · airframe 24,594 hrs · 21,786 cycles

OVERWING CEILING EMERGENCY EXIT SIGN INOPERATIVE, AFT SIDE. R & R SIGN IAW AMM 33-50-13. OPS CHECKED GOOD.

Part: BRACKET — BROKEN (FLASHLIGHT) · airframe 24,002 hrs · 21,182 cycles

THE CREW REPORTED THE F/O’S FLASHLIGHT BRACKET WAS BROKEN. THE ACFT WAS REMOVED FROM SERVICE. R & R THE F/O’S FLASHLIGHT HOLDER BRACKET. THE OPS CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,656 hrs · 20,888 cycles

DURING B INSPECTION FOUND THE CEILING EMERGENCY LIGHT AT SEAT 3A INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CEILING EMERGENCY LIGHT AT SEAT 3A IAW EMB 140 AMM33-50-08. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — INTERMITTENT (CABIN) · airframe 23,302 hrs · 20,601 cycles

DURING B INSPECTION FOUND THE AFT CABIN BULKHEAD MOUNTED FLASHLIGHT HAS AN INTERMITTENT SWITCH. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AFT CABIN BULKHEAD MOUNTED FLASHLIGHT IAW EMB 140 AMM 33-51-01. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,302 hrs · 20,601 cycles

DURING B INSPECTION FOUND THE LEFT OVERWING EMERGENCY EXIT LIGHT ON PSU INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. RELAMPED THE LEFT OVERWING EMERGENCY EXIT LIGHT ON PSU IAW EMB 140 AMM 33-50-07. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ELECTRONIC UNIT — MALFUNCTIONED (LANDING GEAR) · airframe 22,371 hrs · 19,749 cycles

ON FLIGHT 2717 THE CREW REPORTED THAT AFTER TAKEOFF THE GEAR RETRACTION SHOWED NO IN TRANSIT LIGHTS AND IMMEDIATELY SHOWED "UP" MAIN LANDING LIGHTS SHOWED RMU SHOWED DOWN AND LOCKED NO IN TRANSIT UPON GEAR EXTENSION. THE CREW ELECTED TO RETURN TO DFW. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LANDING GEAR ELECTRONIC UNIT IAW EMB 32-32-0. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: PLUG — DEFECTIVE (NR 1 ENGINE) · airframe 19,581 hrs · 16,834 cycles

ON FLIGHT 3306 MAINTENANCE REPORTED SMOKE COMING OUT OF THE FRONT OF THE NR 1 ENGINE ON POST FLIGHT. THE NR 1 ENGINE HAD BEEN SHUT DOWN FOR OVER 10 MINUTES WHEN THIS WAS OBSERVED. ALL SHUTDOWN INDICATIONS HAD BEEN NORMAL. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED NR 1 ENGINE LOW PRESSURE TURBINE SHAFT PLUG IAW ROLLS ROYCE MM 72-59-15. THE OPERATIONAL CHECK AND LEAK CHECKS WERE GOOD. REF NRWC'S 855-DFW-00349 AND 855-DFW-00350. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SWITCH — OUT OF ADJUST (EMERGENCY EXIT) · airframe 19,011 hrs · 16,373 cycles

DURING MAINTENANCE BASE INSPECTION FOUND THE RIGHT OVERWING EMERGENCY EXIT HAS AN OPEN INDICATION ON EICAS WITH THE HATCH INSTALLED. THE AIRCRAFT WAS REMOVED FROM SERVICE. ADJUSTED THE RIGHT OVERWING EMERGENCY EXIT SWITCH AND OPERATIONALLY CHECKED IAW EMB AMM TASK 52-75-01-700-801-A. NO PARTS REMOVED OR REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 19,011 hrs · 16,373 cycles

DURING MAINTENANCE BASE INSPECTION FOUND THE LEFT AND RIGHT OVERWING LIGHTS AND LAST 3 EMERGENCY LIGHT STRIPS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED BATTERY POWER SUPPLY IAW AMM 33-50-04. THE OPERATIONAL CHECK WAS GOOD IAW EMB 140 AMM 33-50-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FRAME — CORRODED (FUSELAGE) · airframe 19,011 hrs · 16,373 cycles

DURING MAINTENANCE BASE VISIT INSPECTION FOUND FRAME 23 CRACKED JUST BELOW FLOOR LEVEL. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIR COMPLIED WITH AS PER EO EM-53MR-1805 FOR FRAME 23RT SPLICE. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,011 hrs · 16,373 cycles

DURING MAINTENANCE BASE VISIT FOUND CARGO DOOR SILL TO HAVE CORROSION. THE AIRCRAFT WAS REMOVED FROM SERVICE. THE CORRECTIVE ACTION INFORMATION IS PENDING.

Part: UNKNOWN — VIBRATION (NLG) · airframe 18,769 hrs · 16,079 cycles

ON FLIGHT 3045 THE CREW REPORTED A NOISE AND SMALL VIBRATION IN NOSE AREA AFTER TAKEOFF. APPROXIMATLEY 20 MINUTES AFTER LIFTOFF THE NOISE SUDDENLY STOPPED. THE CAPTAIN DECLARED AN EMERGENCY AND ELECTED TO RETURN TO DEN. AFTER SECOND GEAR RETRACTION AT 10,000 FEET THE SAME NOISE RETURNED. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. INSPECTED NOSE GEAR AREA FOR OBVIOUS DEFECTS, NONE NOTED. PERFORMED LANDING GEAR RETRACTION OPERATIONAL CHECK IAW ERJ 140 AMM 32-30-00, THE OPERATIONAL CHECK WAS GOOD. PERFORMED OPERATIONAL CHECK OF THE LANDING GEAR PROXIMITY SWITCHES IAW ERJ 140 AMM 32-32-00. THE OPERATIONAL CHECK WAS GOOD. NO DEFECTS NOTED. NO PARTS REMOVED OR REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: STATIC INVERTER — MALFUNCTIONED (ELECTRICAL SYS) · airframe 17,640 hrs · 14,642 cycles

FOR FLIGHT 3175 DURING THE PREFLIGHT OPERATIONAL CHECK DETECTED A VERY DISTINCT BURNED WIRE ODOR EMANATING FROM THE LEFT SIDE OF THE NOSE CONE AREA. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE STATIC INVERTER IAW EMB 140 AMM 24-20-01. THE OPERATIONAL CHECK WAS GOOD AT THIS TIME IAW EMB 140 AMM 24-20-01. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SMOKE DETECTOR — NO TEST (CARGO BAY) · airframe 17,012 hrs · 13,875 cycles

DURING PREFLIGHT CHECK FOR FLIGHT 3472 THE BAGGAGE SMOKE DETECTOR DID NOT TEST. NO LIGHT CAME ON THE OVERHEAD PANEL DURING THE TEST. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 1 BAGGAGE SMOKE DETECTOR IAW EMB-140 AMM 26-15-01. THE OPERATIONAL CHECK WAS OK. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ACM — FAILED (NR 1) · airframe 16,416 hrs · 13,365 cycles

ON FLIGHT 4199 THE CREW REPORTED SMOKE IN THE COCKPIT AND CABIN WITH THE AUXILARY POWER UNIT BLEED AND AIR CYCLE MACHINE PACKS NR 1 AND 2 ON. THE SMOKE CLEARED WHEN BOTH PACKS WERE TURNED OFF. THE AIRCRAFT RETURNED TO BLOCKAND WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 1 AIR CYCLE MACHINE IAW EMB 140 AMM 21-51-03. THE OPERATIONAL CHECK WAS GOOD. NO HAZE NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SKIN — CRACKED (FUSELAGE) · airframe 14,557 hrs · 11,723 cycles

MTX NOTED BIRD STRIKE DAMAGE AT 65 INCH AFT FROM RADOME RIGHT FUSELAGE ABOUT 3 FEET WIDE AND 4 FEET LONG AND ABOUT 40 RIVETS PULLED THROUGH SKIN. AIRCRAFT FERRIED TO MQT FOR REPAIRS. MAINTENANCE REMOVED AND REPLACED FORWARD FUSELAGE UPPER SKIN, UPPER FRAMES 2R, 3R, 4R, 5R, LOWER FRAME 2R, 3R REPAIRED UPPER FRAME 6R, AND REPLACED STRINGERS 4R AND 6R IN ACCORDANCE WITH SRM 51-40-02, 51-30-01, EO-EM-53MR-1264 AND EO-EM-53MR-1268. AIRCRAFT WAS RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 11,664 hrs · 9,306 cycles

ON FLIGHT 3616, CREW REPORTED CLIMBING THRU FL 250 NOTICED A SWEET BURNING ODOR FOR APPROX 45 SEC TO 1 MIN AND THEN IT WENT AWAY. NO OTHER ABNORMALITIES OR EICAS MESSAGES AIRCRAFT REMOVED FROM SERVICE. PERFORMED OPERATIONAL CHECK WITH APU AND PAC AIR TO FULL HOT AND FULL COLD. FOUND NO ODOR IAW EMB 140 AMM 36-00-00. OPERATIONAL CHECK GOOD. NO PARTS REMOVED, TRIAD PASSED. AIRCRAFT RETURNED TO SERVICE.

Part: STATIC INVERTER — FAILED · airframe 11,659 hrs · 9,302 cycles

ON FLIGHT 3833 CREW REPORTED IN FLIGHT THAT THE PFD1-2, FMS ONE, TCAS, GPWS, AND TRANSPONDER FAILED. CREW REPORTED DETECTED SMOKE. AIRCRAFT REMOVED FROM SERVICE. C/A- REMOVED AND REPLACED STATIC INVERTER IAW EMB AMM 24-20-01. AIRCRAFT RETURNED TO SERVICE

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 9,744 hrs · 7,920 cycles

LEFT OMEGA BEAM CORRODED AT FRAME 27. CUT OUT DAMAGE, FABRICATED AND INSTALLED REAPAIR PARTS IAW EMB SRM 53-00-10, FIGURE 202. AIRCRAFT RETURNED TO SERVICE

Part: SILL — CORRODED (ZONE 100) · corrosion level 2 · airframe 9,744 hrs · 7,920 cycles

BAGGAGE DOOR LOWER SILL FOUND CORRODED. REMOVED AND REPLACED LOWER SILL IAW EMB SRM 51-20-01, 51-20-03, 51-40-02, 51-40-04 AND 51-40-06. AIRCRAFT RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 9,744 hrs · 7,920 cycles

CENTER OMEGA BEAM CORRODED AT FRAME 24 AND 25. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PARTS IAW EMB SRM 53-00-10, FIGURE 203. RETURNED AIRCRAFT TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 9,744 hrs · 7,920 cycles

LEFT OMEGA BEAM CORRODED AT FRAME 20. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PARTS IAW EMB SRM 53-00-10 AND 51-40-02. AIRCRAFT RETURNED TO SERVICE.

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 9,744 hrs · 7,920 cycles

SHEAR TIE AT FRAME 65 CORRODED. REMOVED AND REPLACED SHEAR TIE IAW EMB IC2007-145-03768, PARGRAPH ONE. RETURNED AIRCRAFT TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 9,744 hrs · 7,920 cycles

LEFT OMEGA BEAM CORRODED AT FRAME 27. CUT OUT DAMAGE, FABRICATED AND INSTALLED REPAIR PARTS IAW EMB SRM 53-00-10. AIRCRAFT RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 9,744 hrs · 7,920 cycles

LEFT OMEGA BEAM CORRODED AT FRAME 24 AND 25. CUT OUT DAMAGED, FABRICATED AND INSTALLED REPAIR PARTS IAW EMB SRM 53-00-10, FIGURE 202. AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY — ODOR (FLASHLIGHT)

MIA - FLT 4328 - BURNING SMELL IN COCKPIT. FOUND SMELL COMING FROM FIRST OFFICERS FLASHLIGHT BATTERY. REMOVED AND REPLACED FLASHLIGHT ASSEMBLY. OPERATIONAL CHECK GOOD. RETURNED AIRCRAFT TO SERVICE. (M)