N610AE

Part: NONE — NONE · airframe 49,551 hrs · 45,394 cycles

FA FWD FLASHLIGHT INOP.-C/A-RAR FWD FA FLASHLIGHT IAW AMM 33-50-16. OPS CHECK GOOD.

Part: NONE — NONE · airframe 49,211 hrs · 44,991 cycles

LH OVERWING EMERGENCY LIGHT INOP-C/A-RAR LH OVERWING EMERGENCY LIGHT LAMP IAW EMB AMM 33-50-10-000-801-A AND 33-50-10-400-801-A. OPS CHECK GOOD. NO DEFECTS NOTED. END.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 49,102 hrs · 44,868 cycles

WHILE PERFORMING PS-1 INSPECTION FOUND EMERGENCY FLOOR PROXIMITY LIGHT STRIPS 4,5 INOP.-C/A-REMOVED AND REPLACED #3 BATTERY AND CHARGER IAW EMB 145 AMM 33-50-01. OPS CHECK GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 49,010 hrs · 44,764 cycles

EMERGENCY LIGHT ABOVE RIGHT WING INOP-C/A-SEE AML LOG PAGE4734718/3 DEFERRED EMERGENCY LIGHT PER MEL 33-22 RAR'D LAMP ASSY IAW 33-50-10. NO FIX. T/S TO LIGHT ASSY. PARTS ON ORDER AOG.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 48,995 hrs · 44,748 cycles

#4 AND #5 SECTIONS OF FLOOR EMER LIGHTS INOP AND L/H AND R/H OVER WING INTERNAL LIGHTS INOP-C/A-REF TURNOVER, INSTALLED ORIGINAL #5 EMERG LIGHT INVERTER IAW AMM 33-50-11 AND TRANSFERRED THIS DISCREPANCY TO LOG PG 4734713, ITEM 1 FOR FERRY FLIGHT PURPOSES.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 48,933 hrs · 44,684 cycles

RH OVERWING EMERGENCY LIGHT INOP-C/A-RAR RH OVERWING EMERGENCY LIGHT LAMP IAW EMB AMM 33-50-10-000-801-A AND 33-50-10-400-801-A. OPS CHECKED GOOD. END.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 48,755 hrs · 44,480 cycles

RH AFT OVERWING EMERGENCY LIGHT INOP-C/A-REMOVED AND REPLACED RH AFT OVERWING EMERGENCY LIGHT BULB IAW EMB 145 AMM 33-50-10-020-003-A. OP CHECKED GOOD

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 48,713 hrs · 44,425 cycles

RH AFT OVERWING EMERGENCY LIGHT INOP-C/A-RAR RH AFT OVERWING EMERGENCY LIGHT LAMP IAW EMB AMM 33-50-10-000-801-A AND 33-50-10-400-801-A. OPS CHECKED GOOD. END.

Part: CONTROL MODULE — FAULTED (EMERGENCY LIGHTS) · airframe 48,518 hrs · 44,204 cycles

EMERGENCY LIGHT NOT ARMED CAUTION ON EICAS W/ EMERG LT SWITCH ARMED TRIED CYCLING MULTIPLE TIMES"TRANSFERRED TO NRWC 610-ORD-03512" GR 417418-C/A-RAR CONTROL MODULE IAW EMB 145 MM 33-21-01. OPS CK GOOD. REF NRWC 610-ORD-03512 FOR SUPPORTING ACTION

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 48,315 hrs · 43,995 cycles

RH OVERWING EMERGENCY LIGHT FOUND TO BE INOP PER PS-1 INSP.-C/A-RAR RH OVERWING EMERGENCY LIGHT LAMP IN REF. AMM 33-50-10. OPC GOOD IN REF TO AMM 33-50-00

Part: DUCT — LOOSE (PNUEMATIC SYS) · airframe 47,823 hrs · 43,487 cycles

BLEED 2 LEAK IN FLIGHT EMERGNCY DECLARED. EQUIPMENT SWAP FLT CONT. C/A: TROUBLESHOT BLEED 2 LEAK, REF FI 36-20-00-810-802A AND FOUND DUCTS TO HEAT EXCHANGER TO BE LOOSEN. RESECURED DUCTS, REF EMB 145 AMM 36-11-09. OPERATIONS CHECK OF BLEED AIR SYSTEM. OPERATIONS CHECK GOOD. NO MESSAGE DISPLAYED ON EICAS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 47,801 hrs · 43,466 cycles

NR 5 FLOOR PROXIMITY EMERGENCY LIGHT STRIP IS INOPERABLE. C/A: R & R NR 5 FLOOR PROXIMITY EMERGENCY LIGHT STRIP, IAW EMB145 AMM 33-50-12. OPERATIONAL CHECK OF EMERGENCY LIGHTS GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 47,679 hrs · 43,342 cycles

RT SIDE AFT OVERWING EMERGENCY LIGHT INOPERABLE. C/A: R & R RT SIDE AFT OVERWING EMERGENCY LIGHTBULB, IAW EMB 145 AMM 33-50-10. OPERATIONS CHECK GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 47,556 hrs · 43,214 cycles

RT AFT OVERWING EMERGENCY LIGHT INOP. C/A: R & R RT AFT OVERWING EMERGENCY LAMP, IAW EMB 145 AMM 33-50-10. OPS CHECK GOOD, IAW EMB 145 AMM 33-50-00.

Part: LIGHT — INOPERATIVE (RT OVERWING) · airframe 47,498 hrs · 43,143 cycles

RH OVERWING EMERGENCY LIGHT INOPERATIVE. R & R RH OVERWING EMERGENCY LIGHT OPC GOOD IAW AMM 33-50-07

Part: LIGHT — INOPERATIVE (RT OVERWING) · airframe 47,434 hrs · 43,093 cycles

FOUND RH OVERWING EMERGENCY LIGHT TO BE INOP-C/A-REPLACED RH OVERWING EMERGENCY LIGHT IAW AMM 33-50-10. OPS CHECK GOOD

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 47,319 hrs · 42,993 cycles

EMERGENCY EXIT SIGN ON AFT GALLEY WALL AT SEAT 3B INOPERATIVE. TIGHTENED UP CONNECTOR PLUG BACKSHELL IN REFERENCE WITH EMB AMM 33-50-11-000-801-A AND 33-50-11-400-801-A. OPS CHECKED GOOD.

Part: WIRE SPLICE — DEFECTIVE (CABIN) · airframe 47,118 hrs · 42,792 cycles

L/H AFT OVERWING EMERGENCY LIGHT IS INOP.-C/A-FOUND SPLICE AT WIRE W101-8590-22 TO BE DEFECTIVE. REMOVED AND REPLACED SPLICE SP8928 IAW EMB 145 SWPM 20-21-00 . OPS CHECK GOOD.

Part: PLATE — DAMAGED (RUDDER) · airframe 47,113 hrs · 42,787 cycles

RUDDER #1 HAS AREA OF CHAFEING DAMAGE-C/A-COMPLIED WITH IAW ERS-EM-55MR-830 01

Part: FITTING — OUT OF TOLERANCE (RUDDER) · airframe 47,113 hrs · 42,787 cycles

RUDDER 2 LOWER ROD FITTING UPPER FLANGE FAILED DIMENSIONAL CHECK, FITTING REQUIRES REPLACEMENT.-C/A-REMOVED AND REPLACED LOWER ROD FITTING ASSY IAW SRM 55-40-02

Part: HINGE FITTING — UNSERVICEABLE (RUDDER) · airframe 47,113 hrs · 42,787 cycles

TRANSFERRED FROM TASK #1 OF NRTC E778170. UPPER HINGE FITTING, SRM 55-41-02 FIG 10 ITEM 140. UNSERVICEABLE AND REQUIRES REPLACEMENT. -C/A-INSTALLED NEW HINGE FITTING IAW EMB SRM 51-40-02.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 47,113 hrs · 42,787 cycles

LH WING-TO-FUSELAGE UPPER ATTACHMENT ANGLE. HAS EVIDENCE OF A CRACK APPROX. 1/2" LONG. JUST BELOW A RIVET AT FRAME 50.-C/A-RAR LH WING-TO-FUSELAGE UPPER ATTACHMENT ANGLE IAW SRM 51-40-02

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 47,113 hrs · 42,787 cycles

LH WING-TO-FUSELAGE #2 LOWER ATTACHMENT ANGLE. HAS A 3/8" CRACK ON THE FWD END UP TO THE FIRST RIVET.-C/A-REMOVED AND REPLACED LH WING TO FUSELAGE #2 LOWER ATTACHMENT ANGLE IAW ETN-EM-53-142, AND SRM 51-40-02.

Part: WEB — CRACKED (LT MLG WW) · airframe 47,113 hrs · 42,787 cycles

L/H GEAR WELL AFT WEB IS CRACKED IN 3 PLACES. -C/A-REMOVED AND REPLACED AND COMPLETED INSTALLATION OF LH GEAR WELL AFT WEB IAW SRM 51-40-02.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 47,113 hrs · 42,787 cycles

LH WING-TO-FUSELAGE UPPER ATTACHMENT ANGLE. HAS EVIDENCE OF A CRACK APPROX. 1/2" LONG. JUST BELOW A RIVET AT FRAME 50. -C/A-REMOVED AND REPLACED LH WING TO FUSELAGE #2 LOWER ATTACHMENT ANGLE IAW ETN-53-142, AND SRM 51-40-02.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 47,113 hrs · 42,787 cycles

RH WING-TO-FUSELAGE LOWER ATTACHMENT ANGLE #1. HAS A 1/2" CRACK ON THE FWD END OF THE PREVIOUS REPAIR SPLICE. -C/A-REPLACED BOTH AREAS (REF TASK#1) WITH ONE REPAIR IAW ETN-EM-53-142R2.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 47,113 hrs · 42,787 cycles

SUPPORT CRACKED AT FR 61 BETWEEN STR 4 RT AND 5 RT-C/A-REMOVED AND REPLACED SUPPORT AT FRAME 61 BETWEEN STRINGER 4RT AND 5 RT IAW SRM 51-40-02.

Part: ATTACH ANGLE — CRACKED (LT WING) · airframe 47,113 hrs · 42,787 cycles

LH WING-TO-FUSELAGE #4 LOWER ATTACHMENT ANGLE. HAS A 2" CRACK ON THE FWD END UP TO THE THIRD RIVET.-C/A-REMOVED AND REPLACED SECTION OF THE LH WING TO FUSELAGE #4 LOWER ATTACH ANGLE IAE ETN-EM-53-142, AND SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 47,113 hrs · 42,787 cycles

LH OMEGA BEAM HAS SIDE CORROSION PITTING NEAR THE CROSSBEAM AT FR. 38. -C/A-REPAIRED LH OMEGA BEAM NEAR THE CROSSBEAM AT FR 38 IAW SRM 53-00-10.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 47,113 hrs · 42,787 cycles

CENTER OMEGA BEAM HAS SIDE CORROSION PITTING NEAR THE CROSSBEAM AT FR. 38. -C/A-COMPLETED REPAIR ON THE CENTER OMEGA BEAM AT FRAME 38 IAW SRM 53-00-10 AND 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 47,113 hrs · 42,787 cycles

CENTER OMEGA BEAM HAS SIDE CORROSION PITTING NEAR THE CROSSBEAM AT FR. 50. -C/A-REPAIRED IAW ERS-EM-53MR-4062

Part: SPLICE — INOPERATIVE (EXTERIOR LIGHT) · airframe 47,113 hrs · 42,787 cycles

RH LATERAL WING-TO-FUSELAGE 194BR ACCESS PANEL EXTERNAL EMERGENCY LIGHT WILL NOT ILLUMINATE.-C/A-COMPLETE:REPLACED SPLICE 8930, OVERWING EMERGENCY LIGHT TEST GOOD IAW AMM 33-50-00

Part: CROSSBEAM — CORRODED (FUSELAGE) · airframe 47,113 hrs · 42,787 cycles

CABIN CROSSBEAM BETWEEN FRAMES 24-25 HAS CORROSION.-C/A-COMPLETE:REMOVED AND REPLACED CABIN CROSSBEAM BETWEEN FRAMES 24-25 IAW ETN-EM-53-139

Part: LIGHT — INOPERATIVE (CABIN) · airframe 47,113 hrs · 42,787 cycles

LH FLOOR EMERGENCY LIGHT STRIP #8 EXTRUSION ARE DAMAGED-C/A-COMPLETE:REPLACED #8 LH FLOOR EMERGENCY LIGHT STRIP EXTRUSION IAW AMM 33-50-12.

Part: LIGHT — DAMAGED (CABIN) · airframe 47,113 hrs · 42,787 cycles

LH FLOOR EMERGENCY LIGHT STRIP EXTRUSIONS #3,AND #8 ARE DAMAGED-C/A-COMPLETE:REPLACED LH FLOOR EMERGENCY LIGHT STRIP EXTRUSIONS #3,AND #8 IAW AMM 33-50-12

Part: LIGHT — DAMAGED (CABIN) · airframe 47,113 hrs · 42,787 cycles

EMERGENCY FLOOR LIGHTING LH EXTRUSION FOR RAMP PANEL IS DAMAGED.-C/A-COMPLETE:REMOVED AND REPLACED EMERGENCY FLOOR LIGHTING LH EXTRUSION FOR RAMP PANEL IAW AMM 33-50-12.

Part: LIGHT — CORRODED (EXTERIOR) · airframe 47,113 hrs · 42,787 cycles

FORWARD BELLY FAIRING, LH EXTERIOR EMERGENCY LIGHT CORRODED.-C/A-COMPLETE:RRMOVED AND REPLACED RETAINER RING IAW SRM 51-40-02

Part: RIVET — SHEARED (NLG UPLOCK BOX) · airframe 46,662 hrs · 42,459 cycles

RIVETS SHEARED OFF FROM THE RH ANGLE OF THE NLG UPLOCK BOX SUPPORT WEB ON THE RH SIDE OF THE WEB. MOVEMENT OF THIS WEB HAS ALSO CAUSED A LARGE CRACK IN THE FWD AVIONICS COMPARTMENT FLOOR AT SAME LOCATION. -C/A-COMPLETED REPAIR OF FWD AVIONICS COMPARTMENT FLOOR IAW SRM 53-11-10.

Part: PROXIMITY SWITCH — MALFUNCTIONED (NLG) · airframe 46,541 hrs · 42,340 cycles

AFTER T.O. NOSE GEAR DID NOT GO UP, GOT LG/LEVER DISAGREE WARNING RAN QRH PROCEDURE, FIXED BUT MADE A VERY LOUD UNCOMFORTABLE BANG WHEN CLOSED. "TRANSFERRED TO NRWC 610-ORD-02680"-C/A-REF NRWC 610-ORD-02680 AND 610-ORD-02681 FOR CORRECTIVE ACTION AND APPLICABLE RII. RAR NLG UPLOCK BOX AND ASSOCIATED PROXIMITY SWITCHES. OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 46,540 hrs · 42,338 cycles

DURING PS-2 FOUND EXTERIOR RH FWD EMERGENCY LIGHT INOP-C/A-RAR EXTERIOR RH FWD EMERGENCY LIGHT IAW 145 AMM 33-50-10 OPS-CHECK GOOD NO FURTHER DEFECTS NOTED

Part: INVERTER — INOPERATIVE (CABIN) · airframe 46,256 hrs · 42,059 cycles

DURING PS-2 CHECK FOUND TOP SERVICE DOOR EMERGENCY EXIT LIGHT INOP-C/A-REMOVED AND REPLACED EMERGENCY LIGHT DC/AC INVERTER #2 IAW EMB 145 AMM 33-50-11

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 46,183 hrs · 41,975 cycles

PITOT 3 INOP EICAS MESSAGE DISPLAYED ON EICAS AFTER ENGINE START. C/AREMOVED AND REPLACED #3 PITOT/STATIC SENSOR IAW AMM 34-13-02. DID NOT SOLVE PROBLEM. PERFORMED PITO/STATIC 3 LEAK TEST IAW AMM 34-13-00-790-804. LEAK CHECK GOOD. APPLY SEALANT IAW SRM 51-10-01 PR. A/C GOOD FOR SERVICE. REMOVED AND REPLACED BOTH RELAY K0058 AND RELAY SOCKET IAW AMM 20-13-02 AND REMOVED AND REPLACED WIRE W102-0268-16 IAW SWPM 20-21-00. PERFORMED OPS CHECK OF PITOT 3 HEATING IAW 30-31-00-700-803. OPS CHEHECK GOOD.

Part: WIRE HARNESS — FAILED (MLG) · airframe 45,973 hrs · 41,768 cycles

LG/LEVER DISAGREE WARNING DURING GEAR RETRACTION ON CLIMB FROM ORD. NOSE GEAR INDICATION SHOWED RED CROSS HATCH BOX. COMPLETED ABNORMAL PROCEDURE & RETURNED TO DEPARTURE. AFTER FUEL BURN OFF. LANDED UNDER MLW. TROUBLESHOT PER FIM 32-61-00-810-807-A. REMOVED AND REPLACED ELECTRICAL HARNESS W014 IAW AMM 32-00-03. OPS CHECKED GOOD

Part: CONTROL PANEL — FAILED (OBSERVER AUDIO) · airframe 45,961 hrs · 41,754 cycles

AFTER TAKEOFF, A STRONG STATIC NOISE TRANSMITTING TO ALL THREE HEADSETS MAKING IT IMPOSSIBLE TO COMMUNICATE WITH ATC. REMOVED AND REPLACED OBSERVER AUDIO CONTROL PANEL IAW AMM 23-51-01.OPERATIONAL CHECK OK IAW AMM 23-51-00. NO STATIC NOTED.

Part: CONTROLLER — FAILED (CABIN PRESSURE) · airframe 45,870 hrs · 41,707 cycles

AFTER TAKEOFF UNABLE TO GET THE A/C TO PRESSURIZE IN EITHER THE AUTO & MANUAL MODE. MANUAL PRESSURIZATION PERFORMED OPS CHECK IAW AMM 21-31-00-700-801-A OPS CHECKED GOOD. AIRCRAFT OK FOR SERVICE. REMOVED AND REPLACED DIGITAL CONTROLLER IAW AMM 21-31-01 OPS CHECK OK IAW AMM 21-31-00 .

Part: ROLLER — STICKS (CABIN DOOR) · airframe 45,854 hrs · 41,694 cycles

FA REPORTS MAIN CABIN DOOR LEVER TO CLOSE DOOR IS STICKING. IT IS DIFFICULT TO CLOSE AND DOOR IS STICKING WHILE TRYING TO OPEN IT. C/A-SERVICED THE MAIN DOOR FRAME ROLLERS IAW AMM TASK 53-21-02-600-801-A. NO FURTHER DEFECTS NOTED, DOOR MOVES SMOOTH WHEN OPENING OR CLOSING.

Part: SHUTOFF VALVE — FAILED (BRAKE SYSTEM) · airframe 45,749 hrs · 41,608 cycles

AT GEAR EXTENSION BRK INBD INOP ON EICAS, DID GO AROUND AND RETRACTED GEAR MESSAGE WENT AWAY AT GEAR EXTENSION DURING SECOND APPROACH MESSAGE DID NOT RETURN. DELARED AN EMERGENCY. C/A-FOUND BRAKE INBD SOV FAIL ON CMC MESSAGE. T/S REF FIM TASK 32-41-00-810-809. RAR BRAKE SHUTOFF VALVE #2 IAW AMM 32-41-05. OPS AND LEAK CHECK GOOD. FOUND #4 BRAKE SHUTTLE VALVE O-RNG BETWEEN OUTBOARD QUICK DISCONNECT AND HOUSING TO BE LEAKING. REMOVED AND REPLACED O-RING IAW CMM 32-49-12. OPS CHECK GOOD. NO LEAK NOTED AT THIS TIME.

Part: LIGHT — INOPERATIVE (SEATS 3 - 5) · airframe 45,516 hrs · 41,411 cycles

FOUND EMERGENCY LIGHT STRIP BETWEEN LH SEAT 3-5 INOP. RAR EMERGENCY LIGHT STRIP ON LH BETWEEN SEAT 3-5 IAW AMM 33-50-12-04. OPS CHECK GOOD

Part: UNKNOWN — ODOR (CABIN) · airframe 45,183 hrs · 41,067 cycles

CREW OF FLT #3658 ALSO REPORT OF SMELL OF PLASTIC BURNING IN THE CABIN SEE LOG PAGE 4459778 ITEM 1 AND 2 FOR CREW INF.-C/A-C/W ETN EM-72-034 NO SMELL OF PLASTIC BURNING OR ABNORMAL SMELL NOTED

Part: LIGHT — INOPERATIVE (CABIN) · airframe 45,164 hrs · 41,049 cycles

SERVICE DOOR EMERGENCY LIGHT IN CEILING PANEL INOP-C/A-REMOVED AND REPLACED EMERGENCY LIGHT IAW AMM 33-50-13

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 45,156 hrs · 41,042 cycles

LT OMEGA BEAM CORRODED AT CROSS BEAM FRAME 44. C/A-REPAIRED THE LT OMEGA BEAM CORROSION AT CROSS BEAM FRAME 44 IAW ERS-EM-53MR-3712.

Part: CONNECTOR — BROKEN (CABIN) · airframe 45,156 hrs · 41,042 cycles

LT NR 8 FLOOR PROXIMITY LIGHT CONNECTORS MISSING ON AIRCRAFT SIDE. C/A-INSTALLED NEW CONNECTORS ON WIRES W192-8832-22 AND W192-8833-22 IAW SWPM 20-21-00.

Part: WIRE — BROKEN (CABIN) · airframe 45,156 hrs · 41,042 cycles

NR 1 EMERGENCY LIGHT STRIP HAS ONE BROKEN WIRE ON AIRCRAFT SIDE. C/A-REPAIRED WIRE W192-8630-22 AT NR 1 LIGHT STRIP IAW SWPM 20-21-00.

Part: STRUCTURE — TORN (EMERGENCY LIGHT) · airframe 45,156 hrs · 41,042 cycles

#1 EMERGENCY LIGHT STRIP EXTRUSION IS TORN. C/A-COMPLETE:REMOVED AND REPLACED #1 EMERGENCY LIGHT STRIP EXTRUSION IAW AMM 33-50-12. SEE NRTC E702113 FOR OPS CHECK.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 44,954 hrs · 40,888 cycles

AFT OVERWING EMER LIGHT#5 IS INOP- R&R RH OVERWING EMERGENCY LIGHT BULB OPS CHECK GOOD

Part: FLASHLIGHT — WEAK (FWD CABIN) · airframe 44,954 hrs · 40,888 cycles

FWD FA FLASHLIGHT IS DIM- R&R FWD FA FLASHLIGHT OPS CHECK GOOD

Part: CONNECTOR — NOT SEATED (CABIN) · airframe 44,659 hrs · 40,643 cycles

RT OVERWING EMERGENCY LIGHT (LIGHT NR 6) INOP. INSPECTED RIGHT EMERGENCY LIGHT AND FOUND LIGHT'S CONNECTOR WAS NOT FULLY CONNECTED. CONNECTED RIGHT HAND EMERGENCY LIGHT CANNON PLUG. OPS CHECK GOOD.

Part: ACTUATOR — FAILED (MLG) · airframe 42,483 hrs · 38,714 cycles

LANDING GEAR LEVER DISAGREE AFTER TAKE OFF. R & R NOSE LANDING GEAR ACTUATOR, OPS CHECKED GOOD.

Part: ANGLE — CORRODED (FRAME 68) · airframe 42,350 hrs · 38,583 cycles

FRAME 68 ANGLE IS CORRODED AT THE LOWER END. PERFORMED A REPAIR ON THE FRAME 68 ANGLE.

Part: DOOR SILL — CORRODED (CARGO BAY) · airframe 42,350 hrs · 38,583 cycles

CARGO DOOR LOWER SILL IS CORRODED. R & R CARGO DOOR LOWER SILL.

Part: SHEAR TIE — CORRODED (FRAME 65) · airframe 42,350 hrs · 38,583 cycles

FRAME 65 SHEAR TIE CORRODED AT CARGO DOOR LOWER SILL. R & R THE SHEAR TIE.

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 40,176 hrs · 36,769 cycles

PAX DOOR SWING ARM EMERGENCY LIGHT LENS IS CRACKED. R & R PAX DOOR SWING ARM EMERGENCY LIGHT LENS.

Part: WARNING LIGHT — FALSE ACTIVATION (CARGO DOOR) · airframe 40,151 hrs · 36,747 cycles

CARGO DOOR OPEN EICAS MESSAGE JUST AFTER TAKEOFF. PERFORMED OPS CHECK OF CARGO DOOR. OPS CHECK GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 40,111 hrs · 36,717 cycles

MAIN DOOR EXTERIOR FLOOD LIGHT, LOCATED ON BOTTOM SIDE OF PLUG DOOR HINGE IS INOPERATIVE. R & R MAIN DOOR EXTERIOR FLOOD LIGHT BULB LOCATED ON BOTTOM SIDE OF PLUG DOOR HINGE. OPS CHECK GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 40,111 hrs · 36,717 cycles

SERVICE DOOR EXTERIOR FLOOD LIGHT IS INOPERATIVE. R & R SERVICE DOOR EXTERIOR FLOOD LIGHT BULB. OPS CHECKED GOOD.

Part: CONNECTOR — DIRTY (EMERGENCY LIGHT) · airframe 39,668 hrs · 36,028 cycles

GALLEY WALL EXIT LOCATOR NR 14 FAILS TO ILLUMINATE. ACCESSED GALLEY WALL EXIT LOCATOR LIGHT AND ELECTRICAL CONNECTIONS. DISCONNECTED AND CLEANED CONNECTORS. RECONNECTED AND PERFORMED, OPS CHECK. OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 39,978 hrs · 36,610 cycles

PAX DOOR SWING ARM EMERGENCY LIGHT INOPERATIVE AND LENS CRACKED. R & R PAX DOOR EMERGENCY LIGHT AND LIGHT LENS. OPS CHECK GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 39,890 hrs · 36,537 cycles

PAX DOOR EXTERNAL FLOOD LIGHT NR 1 INOPERATIVE. R & R PAX DOOR EXTERNAL FLOOD LIGHT BULB NR 1. OPS CHECK GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 39,890 hrs · 36,537 cycles

SERVICE DOOR EXTERNAL EMERGENCY LIGHT NR 2 INOPERATIVE. R & R SERVICE DOOR EXTERNAL EMERGENCY LIGHT NR 2 BULB. OPS CHECK GOOD.

Part: UNKNOWN — VAPOR (CABIN) · airframe 39,854 hrs · 36,505 cycles

LARGE AMOUNT VISIBLE VAPOR AND DEICE FLUID ODOR FROM PACS AFTER TAKEOFF. PERFORMED 30 MIN GROUND RUN UP. NO VISIBLE VAPOR OR ODOR EXIST. CHECKS GOOD AT THIS TIME.

Part: SOCKET — DIRTY (EMERGENCY LIGHT) · airframe 39,042 hrs · 35,832 cycles

SERVICE DOOR EMERGENCY FLOOD LIGHT NR 2 IS INOPERATIVE. MAINTENANCE CLEANED AND ADJUSTED LIGHT SOCKET, OPS CHECK GOOD.

Part: SOCKET — DIRTY (EMERGENCY LIGHT) · airframe 39,042 hrs · 35,832 cycles

PAX DOOR EMERGENCY FLOOD LIGHT NR 1 IS INOPERATIVE. MAINTENANCE CLEANED AND ADJUSTED LIGHT SOCKET, OPS CHECK GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 39,042 hrs · 35,832 cycles

RIGHT AFT OVER WING EXTERIOR FLOOD LIGHT NR 6 INOPERATIVE. MAINTENANCE REPLACED BULB, OPS CHECK GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT)

SERVICE DOOR EMERGENCY EXIT FLOOD LIGHT NR 2 INOPERATIVE. R & R TWO BULBS. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT)

PAX DOOR EMERGENCY FLOOD LIGHT NR 1 INOPERATIVE. R & R THE BULB. OPS CHECKED GOOD.

Part: BOOT — FAILED (DUCT) · airframe 38,679 hrs · 3,550 cycles

NR 2 A/C PACK OVERHEAT DURING CRUISE, RETURN TO DEPARTURE. MAINTENANCE INSPECTED AND REPLACED NR 2 DUEL TEMP CONTROL VALVE DUCT BOOT, OPS AND LEACK CHECKED GOOD.

Part: SKIN — DENTED (FUSELAGE) · airframe 38,509 hrs · 35,423 cycles

SKIN HAS DENTS & OIL CANNING BETWEEN FRAME 22 RT, SKIN SPLICE AT JUNCTION 03, BETWEEN STRINGER 9RT & 11RT. REPAIRED SKIN IAW ERS-EM-53MR-1225.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 38,509 hrs · 35,423 cycles

TWO EACH OVERSIZED & ELONGATED HOLES AT FRAME 22 STRINGER 13 RT - 14 RT & ONE EACH JUST FWD OF FRAME 22 AT STRINGER 16 RT. REPAIRED TWO EACH OVERSIZED & ELONGATED HOLES IAW ERS-EM-53MR-1208.

Part: SKIN — DAMAGED (LT WING) · airframe 38,509 hrs · 35,423 cycles

LEFT LE 512 HAS EROSION DAMAGE. LE 512 REPAIRED IAW SRM 57-40-00.

Part: BUSHING — DAMAGED (RUDDER) · airframe 38,509 hrs · 35,423 cycles

RUDDER 1, LOWER & CTR HINGE POINT, LOWER FLANGED HAT BUSHING IS DAMAGED. COMPLIED WITH REPAIR OF RUDDER 1 IAW ERS-EM-55MR-269.

Part: SKIN — CHAFED (PYLON) · airframe 38,509 hrs · 35,423 cycles

PYLON SKIN IS CHAFED FROM THE STEEL BRAIDED LANYARD INSIDE ACCESS PANEL 414DB. COMPLIED WITH PYLON SKIN REPAIR INSIDE ACCESS PANEL 414DB IAW ERS-54MR-309.

Part: SPAR — CRACKED (LT WING) · airframe 38,509 hrs · 35,423 cycles

LEFT WING SPAR NR 3 IS CRACKED BY THE WIRE BUNDLE. COMPLIED WITH LT WING SPAR 3 CRACK REPAIR IAW ERS-EM-57MR-428.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 38,509 hrs · 35,423 cycles

EM-53MR-2147 PTB CTR FUSELAGE I STRINGER 17R. COMPLIED WITH PERMANENT REPAIR IAW PART B OF EO EM-53MR-2147 CTR FUSELAGE I STRINGER 17R, REF TO AML PG 3713197 OTEM 2. TDMI RESTORED.

Part: FRAME — CORRODED (FUSELAGE) · airframe 38,509 hrs · 35,423 cycles

RIGHT FUSELAGE FRAME 22, BETWEEN STRINGER 13 - 14 IS CORRODED. REPAIRED RT FUSELAGE FRAME 22, BETWEEN STRINGERS 13 - 14R IAW SRM 53-00-04 REPAIR ITEM 17.

Part: FIREWALL — CRACKED (FUSELAGE) · airframe 38,509 hrs · 35,423 cycles

APU FIREWALL HAS ABOUT A 1" CRACK AT THE LOWER RIVET ON RT STIFFENER. APU FIREWALL HAS ABOUT 3/4" CRACK AT THE LOWER RIVET ON THE LT STIFFENER. REPLACED APU FIREWALL IAW EO-EM-53AD-1883 PART D.

Part: SKIN — CRACKED (FUSELAGE) · airframe 38,509 hrs · 35,423 cycles

FUSELAGE SKIN CRACKED AT LT FRAME 75 BETWEEN STRINGER 1LT - 3LT, APPROX 1/2" IN LENGTH. COMPLIED WITH REPAIR OF FUSELAGE SKIN CRACK AT LT FRAME 75 BETWEEN STRINGER 1LT - 3LT IAW ERS-EM-5300-1210.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 38,509 hrs · 35,423 cycles

LOWER STIFFENER IS CRACKED AT LT FLOORBEAM BETWEEN FRAMES 16 - 17. R & R LOWER STIFFENER AT LT FLOORBEAM BETWEEN FRAMES 16 - 17 IAW SRM 51-40-02.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 38,509 hrs · 35,423 cycles

LOWER STIFFENER IS CRACKED AT LT CTR FLOORBEAM BETWEEN FRAMES 16 - 17. R & R LOWER STIFFENER AT LT CTR FLOORBEAM BETWEEN FRAMES 16 - 17 IAW SRM 51-40-02.

Part: SPAR — CRACKED (RT WING) · airframe 38,509 hrs · 35,423 cycles

RIGHT WING SPAR 3 IS CRACKED BY THE WIRE BUNDLE. REPAIRED RT WING SPAR 3 IAW ERS-EM-57MR-411.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 38,509 hrs · 35,423 cycles

LEFT BRACKET WHICH CONNECTS THE OMEGA BEAM TO THE PRESS DECK IS CRACKED AT RT OMEGA BEAM BETWEEN FRAMES 47 - 48. INSTALLED NEW L BRACKET IAW SRM 53-23-02. SHEAR CLIP PN 140-04213-609.

Part: ATTACH ANGLE — CRACKED (FAIRING) · airframe 38,509 hrs · 35,423 cycles

LEFT UPPER WING TO FUSELAGE FAIRING LOWER ATTACH ANGLE NR 3 IS CRACKED 3/8" ON THE FWD & AFT ENDS, JUST FWD OF FRAME 48. R & R LT UPPER WING TO FUSELAGE FAIRING LOWER ATTACH ANGLE NR 3, JUST FWD OF FRAME 48, IAW SRM 51-40-02 & ETN-EM-53-142.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 38,377 hrs · 35,316 cycles

CABIN FWD FLASHLIGHT NOT WORKING & NOT CHARGING. R & R EMER FLASHLIGHT AS REQUIRED. OPERATIONS CHECKED GOOD.

Part: UNKNOWN — VIBRATION (NLG) · airframe 37,617 hrs · 34,599 cycles

DURING GEAR RETRACTION CREW RECEIVED THE THREE GREEN & UP INDICATIONS BUT HAD LOUD NOISE & VIBRATION IN NOSE GEAR, SOUNDED LIKE DOORS FOR NOSE GEAR DID NOT CLOSE. COMPLIED WITH AOM VOL 1 PROCEDURES. DIVERTED, DECLARED AN EMERGENCY & LANDED WITHOUT INCIDENT.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 37,576 hrs · 34,557 cycles

OVERHEAD AISLE & PAX DOOR EMER LIGHTS INOPERATIVE. R & R NR 1 EMER POWER SUPPLY IAW AMM 33-50-04. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 37,019 hrs · 34,098 cycles

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

Part: LIGHT — INOPERATIVE (OVERWING EXIT) · airframe 36,812 hrs · 33,921 cycles

RIGHT AFT OVERWING EMER LIGHT INOPERATIVE. R & R RT AFT OVERWING EMER LIGHT LAMP, OPERATIONS CHECKED GOOD IAW AMM 33-50-10.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 36,552 hrs · 33,720 cycles

AFT CABIN EMERGENCY FLASHLIGHT WILL NOT HOLD CHARGE. R & R FLASHLIGHT BATTERY IAW CMM 25-60-02. OPERATIONS CHECKED GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 36,224 hrs · 33,463 cycles

LEFT AFT OVERWING EXIT LIGHT INOPERATIVE. R & R NR 4 EMERGENCY BATTERY & POWER SUPPLY IAW AMM 33-50-04, OPERATIONS CHECKED GOOD.

Part: UNKNOWN — MALFUNCTIONED (AUTOPILOT SYS) · airframe 35,635 hrs · 33,011 cycles

DURING APPROACH ON FLIGHT 3145 CREW REPORTED BELOW 2500 RADIO ALTITUDE CAPTAIN DISCONNECTED THE AUTO PILOT USING THE QUICK DISCONNECT BUTTON. THERE WAS NO AUTOPILOT, AUTOPILOT AURAL WARNING. THE ACFT WAS REMOVED FROM SERVICE. ACCOMPLISHED AUTOPILOT FUNCTIONAL CHECK IAW AMM 22-11-00. COULD NOT DUPLICATE THE PROBLEM ALL CHECKED FOUND TO BE SATISFACTORY.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 35,061 hrs · 32,517 cycles

ENTERY EMERGENCY CABIN LIGHT INOPERATIVE. R & R LAMP IAW AMM 332605. OPS CHECKED GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 35,051 hrs · 32,508 cycles

RT OVERWING EMERGENCY LIGHT INOPERATIVE. R & R LAMP IAW AMM 33-50-10-000-801-A AND 33-50-10-400-801-A. OPS CHECKED GOOD.

Part: CRADLE — CRACKED (FLASHLIGHT) · airframe 34,516 hrs · 32,055 cycles

CAPTAIN`S FLASHLIGHT BASE IS CRACKED. R & R CAPTAIN'S FLASHLIGHT ASSY IAW AMM 33-50-16. OPS CHECKED GOOD.

Part: UNKNOWN — ODOR (COCKPIT & CABIN) · airframe 34,413 hrs · 31,968 cycles

CREW REPORTED DURING CRUISE FLT, CAPTAIN, F/O & CABIN SMELLED A SUDDEN, VERY STRONG ODOR OF BURNING ELECTRICAL. RECEIVED NO CAUTIONS OR WARNINGS ON EICAS & NO VISIBLE SMOKE. DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. INSPECTED ALL CABIN LIGHTS AND COCKPIT LIGHTS AND INSTRUMENTS. RAN BOTH PACKS SEVERAL HOURS, HOT AND COLD. RAN BOTH ENGINES WITH PACKS ON HOT AND COLD. FOUND NO ELECTRICAL ODOR IAW AMM 33-21-00, 33-15-00, 33-12-00, 33-11-00 AND PACKS AMM 21-51-00. RAN ENGINES IAW AMM 72-00-00. ACFT RETURNED TO SERVICE.

Part: SKIN — CRACKED (FUSELAGE) · airframe 34,242 hrs · 31,835 cycles

DURING MX INSPECTION, FOUND THE RT REAR FUSELAGE SKIN CRACKED AT FRAME 75. ACFT REMOVED FROM SERVICE. ACCOMPILSHED EO EM-53MR-2139. ACFT RETURNED TO SERVICE.

Part: STRINGER — CORRODED (17R) · airframe 34,241 hrs · 31,834 cycles

DURING MX INSPECTION, FOUND STRINGER 17R CORRODED. ACFT REMOVED FROM SERVICE. R & R STRINGER 17R IAW EO EM-53MR-2147. ACFT RETURNED TO SERVICE.

Part: BATTERY PACK — DISCHARGED (FLASHLIGHT) · airframe 34,242 hrs · 31,835 cycles

DURING MX INSPECTION, FOUND FORWARD CABIN FLASHLIGHT DIM. ACFT REMOVED FROM SERVICE. R & R FLASHLIGHT BATTERY IAW AMM 33-51-01 AND EM-33-038. OPS CHECKED GOOD. ACFT RETURNED TO SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 34,246 hrs · 31,840 cycles

DURING MX INSPECTION, FOUND THE NR 3 EMERGENCY LIGHT POWER SUPPLY INOPERATIVE. ACFT REMOVED FROM SERVICE. R & R POWER SUPPLY IAW AMM 33-50-04. OPS CHECKED GOOD IAW AMM 33-50-00. ACFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 34,065 hrs · 31,687 cycles

DURING MAINTENANCE INSPECTION FOUND THE EMERGENCY LIGHT BEHIND PILOT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY LIGHT BEHIND PILOT IAW AMM 33-50-03. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT ASSY — INOPERATIVE (COCKPIT) · airframe 31,913 hrs · 29,960 cycles

FLIGHT 2963, CREW REPORTED THE FIRST OFFICER’S FLASHLIGHT WAS NOT CHARGING. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE FIRST OFFICER’S FLASHLIGHT PER AMM 25-60-00. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: UPLOCK — MALFUNCTIONED (RT MLG) · airframe 31,843 hrs · 29,904 cycles

ON FLIGHT 2972 THE CREW REPORTED THAT AFTER GEAR RETRACTION HEARD A LOUD THUMPING SOUND AND THE RIGHT MAIN WAS CYCLING BETWEEN TRANSIT DASHES AND UP ABOUT EVERY 2-3 SECONDS. AFTER PUTTING THE GEAR DOWN FOR RETURN TO SHV THE NOISE WENT AWAY AND THE CREW HAD THREE INDICATIONS. THE CREW DECLARED AN EMERGENCY AND PERFORMED A FLY BY TO VERIFY THE GEAR POSITION. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT MAIN LANDING GEAR UPLOCK BOX IAW EMB 145 AMM CHAP 32-33-10. THE OPERATIONAL AND LEAK CHECKS WERE GOOD. NO DEFECTS NOTED AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 30,775 hrs · 29,044 cycles

DURING MAINTENANCE INSPECTION FOUND THE LEFT SIDE NR 4 FLOOR STRIP EMERGENCY LIGHT INOPERABLE. THIS ITEM HAS BEEN DEFFERED PER MEL 33-30 AUTH #020853-C. REMOVED AND REPLACED NR 3 BATTERY CHARGER, BATTERY AND NR 4 FLOOR LIGHT STRIP. STRIP, FLOOR PROXIMITY LIGHT 6636-7. MEL RESTORED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: HOLDER — DEFECTIVE (COCKPIT) · airframe 30,703 hrs · 28,989 cycles

DURING MAINTENANCE BASE INSPECTION FOUND THE FIRST OFFICER’S FLASHLIGHT HOLDER INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FIRST OFFICER’S FLASHLIGHT ASSEMBLY IAW EMB 145 AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — DEFECTIVE (CABIN) · airframe 30,611 hrs · 28,927 cycles

ON FLIGHT 4280 THE CREW REPORTED THE FLIGHT ATTENDANT FLASHLIGHT ABOVE THE FLIGHT ATTENDANT JUMPSEAT WAS NOT HOLDING A CHARGE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FLASHIGHT ASSEMBLY IAW M/M 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 30,499 hrs · 28,835 cycles

DURING MAINTENANCE BASE VISIT FOUND THE AFT CABIN FLASHLIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AFT CABIN FLASHLIGHT AS PER EMB145 AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ENGINE — SMOKE (NR 1) · airframe 30,106 hrs · 28,533 cycles

FOR FLIGHT 4221 THE CREW REPORTED THAT ON THE POST FLIGHT INSPECTION THEY NOTICED THE NR 1 ENGINE SMOKE FROM INTAKE. THE AIRCRAFT WAS REMOVED FROM SERIVICE. GROUND RAN NR 1 ENGINE IN ACCORDANCE WITH RR MM 72-00-00NO SMOKE NOTED AFTER SHUT DOWN, PERFORMED GENERAL VISUAL INPECTION OF NR 1 ENGINE INLET AND EXHUST AND NO DEFECTS WERE NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 30,042 hrs · 28,481 cycles

DURING MAINTENANCE BASE VISIT FOUND THE EMERGENCY LIGHTS IN ARM POSITION. THE EMERGENCY LIGHTS WERE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY LIGHTING SYSTEM POWER SUPPLIES (CHARGER NR 1, 3, 4 AND BATTERIES NR 1, 3 , 4) IAW WC 33-700-19. THE OPERATIONAL CHECK WAS GOOD IAW WC 33-700-17. BATTERY PART NUMBER 2012-1A. SERIAL NUMBERS 72440, 104958, 104941. BATTERY CHARGER PART NUMBER 11-0049. SERIAL NUMBERS 19171, 14200, C01128. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 30,011 hrs · 28,459 cycles

FOR FLIGHT 3565 THE CREW FOUND ALL EMERGENCY LIGHTS TO BE INOPERATIVE. FOUND AC 610 WITH EMERGENCY LIGHTS IN ARMED POSITION. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY LIGHTING SYSTEM POWER SUPPLIES (CHARGER NR 1, NR 3, NR 4 AND BATTERIES NR 1, NR 3 , NR 4) IAW WC 33-700-1. THE OPERATIONAL CHECK WAS GOOD IAW WC 33-700-17. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 3 · airframe 29,788 hrs · 28,275 cycles

DURING MAINTENANCE BASE VISIT FOUND THE EXTERIOR FUSELAGE SKIN CORRODED IN 2 SPOTS BETWEEN FRAME 14 AND 15 AND BETWEEN STRINGER 20 RIGHT AND 21 RIGHT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED SKIN ON SKIN SEAMS BETWEEN FRAME 13-14 AND BETWEEN STRINGER 18 LEFT 19 LEFT AND STRINGER 18 RIGHT 19 RIGHT. FABRICATED AND INSTALLED SKIN, EXTERNAL DOUBLER, INTERNAL DOUBLER AND FILLERS IAW EO EM-53MR-1868. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (RT OVERWING) · airframe 29,583 hrs · 28,115 cycles

RIGHT HAND OVERWING EMERGENCY EXIT WILL NOT ILLUMINATE. REMOVED AND REPLACED RT OVERWING EXTERIOR ASSEMBLY IAW AMM 33-50-10. OPS CHECKED GOOD.

Part: ENGINE — MALFUNCTIONED (LEFT) · airframe 29,202 hrs · 27,833 cycles

ON FLIGHT 4343 THE CREW REPORTED THAT DURING TAKEOFF, SMOKE IN THE COCKPIT. THE ODOR HAD NO DISTINCTIVE ELECTRICAL OR FUEL SMELL. NOTED THE SMOKE DISSIPATED SOME BUT FUMES REMAINED. THE CREW COMPLIED WITH COCKPIT SMOKE / FUMES CHECKLIST AS MUCH AS POSSIBLE. THE CAPTAIN DECLARED AN EMERGENCY AND ELECTED TO RETURN TO ORD. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE ENGINE NR 1 IAW MTX WC 71-000-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONTROL UNIT — MALFUNCTIONED (BRAKE SYSTEM) · airframe 25,374 hrs · 24,792 cycles

ON FLIGHT 4290 DURING LANDING THE CREW REPORTED ON LANDING ROLLOUT AT APPROXIMATELY 100 KNOTS, LOST RIGHT BRAKING FOR ½ SECOND THEN CAME BACK AT 70 KNOTS. THEN LOST ALL BRAKING UNTIL AIRCRAFT SLOWED TO 30 KNOTS, THEN NORMAL BRAKING RETURNED. THE INDICATIONS: LEFT OUTBOARD IN GREEN. LEFT INBOARD IN AMBER. RIGHT OUTBOARD IN AMBER. RIGHT INBOARD IN GREEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE BRAKE CONTROL UNIT IAW EMB 145 AMM 31-41-02. OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SKIN — CRACKED (AFT FUSELAGE) · airframe 25,011 hrs · 24,452 cycles

DURING MAINTENANCE BASE VISIT INSPECTION MULTIPLE CRACK LIKE INDICATIONS WERE NOTED ON THE EXTERIOR SKIN AROUND RIVET HEADS AT FRAMES 77, 78 AND 79 BETWEEN STRINGERS 3L AND 7L AND BETWEEN 3R AND 7R. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED FASTENERS AND REAMED HOLES TO REMOVE SKIN CRACKS. INSTALLED BUSHING REPAIRS AND DOUBLER REPAIR IAW EO EM-5300-1399. RESTORED TOP COAT IAW CPM 51-21-07 AND ETN EM-51-091. EIGHT CRACKS WERE REPAIRED WITH THE LENGTHS BEING .125 TO 1 INCH LONG.

Part: SILL — CORRODED (CARGO BAY) · corrosion level 2 · airframe 25,011 hrs · 2,452 cycles

DURING INSPECTION FOUND THE CARGO DOOR SILL CORRODED AT FRAME 66. AIRCRAFT REMOVED FROM SERVICE. REPLACED CARGO DOOR SILL IN ACCORDANCE WITH EMBRAER SRM 51-40-02. THE AIRCRAFT RETURNED TO SERVICE.

Part: WEB — CRACKED (NLG WW) · airframe 25,011 hrs · 24,452 cycles

DURING INSPECTION FOUND THE NOSE LANDING GEAR SUPPORT WEB TO BE CHAFED, FOUND IT ALSO TO HAVE A CRACK 3.5 MM LONG. THE AIRCRAFT HAS BEEN REMOVED FROM SERVICE. REPAIRED THE NOSE LANDING GEAR BAY SUPPORT IAW EO EM-5300-1470. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SKIN — CRACKED (FUSELAGE) · airframe 25,011 hrs · 24,452 cycles

DURING MAINTENANCE INSPECTION, FOUND MULTIPLE CRACK LIKE INDICATIONS ON EXTERIOR SKIN AROUND RIVET HEADS AT FRAMES 77, 78 AND 79 BETWEEN STRINGERS 3L AND 7L AND 3R AND 7R. AIRCRAFT REMOVED FROM SERVICE. REMOVED FASTENERS & REAMED HOLES TO REMOVED SKIN CRACKS. INSTALLED BUSHING REPAIRS & DOUBLER REPAIR IAW EO EM-5300-1399. RESTORED TOP COAT IAW CPM 51-21-07 AND ETN EM-51-091. EIGHT CRACKS REPAIRED WITH LENGTHS BEING .125 TO 1 INCH LONG. AIRCRAFT WAS RETURNED TO SERVICE.

Part: LINE — LEAKING (HYD SYSTEM) · airframe 23,403 hrs · 55,979 cycles

ON FLIGHT 3385 - CREW REPORTED DURING CLIMB HYDRAULIC SYSTEM 1 QUANTITY WAS IN NORMAL RANGE PRIOR TO DEPARTURE. 15-20 MINUTES INTO FLIGHT SYS 1 BEGAN TO DECREASE FAIRLY RAPIDLY. CREW REPORTED THEY COULD WATCH DECREASE OCCUR. QUANTITY INCREASED SLIGHTLY ON GEAR EXTENSION. QUANTITY NEVER REACHED AMBER RANGE BUT CAME CLOSE WAS DECREASING AT SUCH A RATE THAT SUFFICIENT QUANTITY AT STATION OBB WAS QUESTIONABLE. AIRCRAFT REMOVED FROM SERVICE. REPAIRED LINE IN HYDRAULIC SYSTEM NR 1 UNDER FLOOR AT SEAT 8 IAW JIC 20-10-03-300-801A. OPERATIONAL AND LEAK CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHTS) · airframe 20,379 hrs · 20,188 cycles

EMERGENCY EXIT SIGN OVERHEAD MID CABIN WILL NOT ILLUMINATE. RESECURED CONNECTOR PIN FOR FORWARD OVERHEAD "EXIT" SIGN AT EMERGENCY EXIT ROW. OPS CHECK GOOD IAW EMB AMM 33-50-00. AIRCRAFT RETURNED TO SERVICE.

Part: CONTROL MODULE — FAILED (EMERGENCY LIGHTS) · airframe 18,986 hrs · 18,927 cycles

DISCOVERED EMERGENCY FLOOR LIGHTING INOPERATIVE STARTING AT ROW 3A DURING CREW'S PREFLIGHT. ELECTRICAL SMELL NOTED. REMOVED AND REPLACED EMERGENCY LIGHT INVERTER IAW EMB 33-21-01. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 18,736 hrs · 18,731 cycles

FOUND EMERGENCY LIGHTS AT ROW 3BC, ROW 12 CEILING AND ROWS 12 THROUGH 18 FLOOR LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY PACK ABOVE ROW 15 IAW EMB AMM 33-50-30. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE.

Part: LIGHT — MALFUNCTIONED (CABIN)

DSM - FLT 4175 - EMERGENCY LIGHT ON GALLEY BULKHEAD INOPERATIVE. PERFORMED OPERATIONAL CHECK OF EMERGENCY LIGHTING SYSTEM IAW EMB 145, AMM 33-50-00. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SIGN — FAILED (FS 294)

GSP - FLT 3640 - FORWARD CABIN EMERGENCY EXIT LIGHT ACROSS FROM 2A WILL NOT ILLUMINATE. REMOVED AND REPLACED EXIT SIGN, OPS CHECK GOOD. RETURNED AIRCRAFT TO SERVICE. (M)

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT)

EMERGENCY LIGHTING AT ROW 3BC INOPERATIVE. REPLACED NR 2 BATTERY P/N 2013-1A, S/N 68198 AND POWER SUPPLY P/N 11-0049 S/N 19284. OPS CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: ACM — MALFUNCTIONED (A/C BAY)

100 FEET AFTER TAKEOFF SMOKE AND BURNING SULFER SMELL IN COCKPIT FOLLOWED BY THIN SMOKE MIST DECLARED EMERG RETURNED TO TYS. RAI NR 1 ACM. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BRAKE — FAILED (MLG)

ORD - FLT 4140 - MAIN BRAKES FAILED. REPLACED ALL FOUR BRAKES P/N 21624, SERIAL 19362, NR 2 P/N 24707 SERIAL 0416, NR 3 P/N 21624 S/N 2951, NR 4 P/N 21707 S/N 3025. ALL FOUR MAIN TIRES POPPED, ALL FOUR PART NUMBERS 31641. REPLACED CONTROL UNIT P/N 42-951-5 S/N 789. REPLACED TRANSDUCERS P/N 0132AFU2. REPLACED ELECTRICAL HARNESS P/N 20017560. REPLACED BRAKE PEDAL TRANSDUCER P/N 200117500. ALL OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: LIGHT — INOPERATIVE (CABIN)

FOUND EMERGENCY FLOOR LIGHTING 2ND AND 3RD STRIP INTERMITTENT/INOPERATIVE. REPLACED NR 3 EMERGENCY LIGHT INVERTER. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SKIN — PUNCTURED (FR22A/23)

SKIN PUNCTURE ON RT FUSELAGE BETWEEN FRAMES 22A/23 AND STRINGER 15R. PERFORMED CUT OUT OF THE SKIN TO REMOVE THE DAMAGE. FABRICATED FILLER AND DOUBLER. REPAIR DONE IAW SRM. (K)

Part: SILL — CORRODED (SERVICE DOOR)

THE SERVICE DOOR CENTER SILL WAS FOUND CORRODED. REMOVED EXISTING SILL AND CLEANED AREA. INSTALLED SERVICEABLE SILL. REPAIR DONE IAW EMB 145 SRM, SRM EMB 145/1142 REV 31, CHAPTER 51-40-02. (M)

Part: SKIN — CORRODED (FR 21, 22)

DURING INSPECTION OF FUSELAGE SKIN BETWEEN FRAMES 21 AND 22 AND STRINGERS 19R AND 191., WAS FOUND TO BE CORRODED. PERFORMED A CUT OUT OF CORRODED AREA. FABRICATED A FILLER AND DOUBLER. REPAIR DONE IAW SRM. (K)

Part: BEAM — CORRODED (FR 25)

DURING INSPECTION OF FUSELAGE CENTER BEAM AT FRAME 25 WAS FOUND TO BE CORRODED. PERFORMED A CUT OUT OF CORRODED AREA. FABRICATED A DOUBLER, FILLER AND 2 SHIM. REPAIR DONE IAW SRM. (K)

Part: FLOORBEAM — CORRODED (FUSELAGE)

DURING AN MBV INSPECTION, THE CENTER FLOORBEAM FLANGE WAS FOUND TO BE CORRODED BEYOND SRM LIMITS BETWEEN FRAMES 24 AND 25. COMPLETELY REMOVED CORROSION BY BLENDING. FABRICATED A REINFORCEMENT PLATE FOR REPAIR. REPAIR DONE IAW EMB REPAIR STATEMENT IC2003-145/3007 AND STANDARD SRM PRACTICES. (M)

Part: SILL — CORRODED (FUSELAGE)

DURING INSPECTION OF AIRCRAFT, FOUND CORROSION ON SERVICE DOOR CENTER SILL. BLENDED CORROSION. FABRICATED A DOUBLER IAW EMB GST-0844/02 ITEM 5, AND STANDARD SRM PRACTICES. (M)

Part: STRINGER — CHAFED (FUSELAGE)

ABI - DURING INSPECTION OF AIRCRAFT, FOUND STRINGER 19R CHAFED AT AFT BELLY PANEL. BLENDED OUT CHAFE. FABRICATED A DOUBLER AND SHIMS IAW EMB GST-0898/02, AND STANDARD SRM PRACTICES. (M)

Part: STRINGER — CHAFED (FUSELAGE)

ABI - DURING INSPECTION OF AIRCRAFT, FOUND STRINGER 19L CHAFED AT AFT BELLY PANEL. BLENDED OUT CHAFE. FABRICATED A DOUBLER AND SHIMS IAW EMB-GST-0898/02, AND STANDARD PRACTICES. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

ABI - DURING INSPECTION OF AIRCRAFT, FOUND FORWARD DIGITAL IN GALLEY AREA CORRODED. REMOVED CORROSION BY CUT OUT. FABRICATED A STRAP, DOUBLERS AND A SHIM IAW EMB145 SRM 145-1142 CHAPTER 53, REV 17, 53-21-10, AND STANDARD SRM PRACTICES. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

ABI - DURING INSPECTION OF AIRCRAFT, FOUND CORROSION ON LEFT OMEGA BEAM AT FRAME 24 BEYOND SRM LIMITS AFTER BLENDING. REMOVED CORROSION BY CUT OUT. FABRICATED A DOUBLER ANGLE, FILLER, AND TWO SHIMS. REPAIRED IAW EMB145 SRM (SRM 145-1142 CHAPTER 53, REV 17) 53-21-10 AND STANDARD SRM PRACTICES. (M)

Part: CROSSBEAM — CORRODED (FUSELAGE) · corrosion level 2

ABI - THIS IS A LEVEL 2 FINDING. GALLEY CROSSBEAM AND PROFILE CORRODED. REMOVED AND INSTALLED NEW GALLEY CROSSBEAM IAW EMB 145 51-40-02, 51-40-06, 51-20-03. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

DURING INSPECTION OF AIRCRAFT, FOUND CORROSION ON GALLEY CENTER FLOOR SUPPORT BEYOND SRM LIMITS. REMOVED CORRODED GALLEY CENTER FLOOR SUPPORT. INSTALLED NEW FLOOR SUPPORT IAW EMB145 SRM 145-1142 CHAPTER 51, REV 17, 51-40-02, GST-0844/02, ITEM 4, AND STANDARD SRM PRACTICES. (M)

Part: DOUBLER — CORRODED (FUSELAGE)

ABI - DURING AN MBV INSPECTION OF AIRCRAFT, FOUND CORROSION ON LEFT OMEGA BEAM (PREVIOUS REPAIR) AT FRAME 20. REMOVED PREVIOUS REPAIR (CORROSION LIMITED TO PREVIOUS REPAIR). FABRICATED A DOUBLER ANGLE, FILLER, A PLATE, AND SHIMS. REPAIRED IAW EMB 145 SRM 9SRM 145/1142 CHAPTER 53, REV 17) 53-21-10, AND STANDARD SRM PRACTICES. (M)

Part: SILL — CORRODED (FUSELAGE)

THIS IS A LEVEL 2 FINDING. CARGO DOOR LOWER SILL CORRODED. REMOVED DAMAGED CARGO DOOR SILL AND INSTALLED SERVICEABLE ONE IAW EMB145 SRM 51-40-02, 51-40-05, 51-20-03. (M)

Part: FRAME — CHAFED (FUSELAGE)

ABI - DURING INSPECTION OF AIRCRAFT, FOUND THE LOWER EDGE OF FRAME 81 CHAFED APPROXIMATELY 12 INCH. RAI FRAME 81 IAW EMB 145 (SRM 145-1142 CHAPTER 51, REV 17) 51-20-01, 51-40-02, 51-40-04, 51-40-07 AND STANDARD SRM PRACTICES. (M)

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2

ABI - THIS IS A LEVEL 2 FINDING. SERVICE DOOR FORWARD SILL CORRODED. REMOVED CORRODED SERVICE DOOR FORWARD SILL AND INSTALLED SERVICEABLE SILL IAW EMB 145 51-40-02 AND 51-20-03. (M)

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2

ABI - THIS IS A LEVEL 2 FINDING. GALLEY AREA FORWARD DIAMOND GUSSET CORRODED. INSTALLED NEW FORWARD GUSSET IAW EMB 145 SRM 51-40-02, 51-20-03, 51-40-06. (M)

Part: SILL — CORRODED (PAX DOOR)

ABI - THIS IS LEVEL 2 FINDING ON A CRIC NR 35573. LEFT SILL IS CORRODED BETWEEN FRAMES 19 AND 23. MAINTENANCE REMOVED LEFT SILL AND INSTALLED NEW SILL IAW EMB 145 SRM 51-40-02. (M)

Part: SUPPORT — CORRODED (FUSELAGE)

THIS IS A LEVEL 2 FINDING. GALLEY RAMP SUPPORT CORRODED. INSTALLED SERVICEABLE GALLEY RAMP SUPPORT IAW EMB145 SRM 51-40-02. (M)

Part: CROSSBEAM — CORRODED (FUSELAGE) · corrosion level 2

ABI - THIS IS LEVEL 2 FINDING. FOUND CORROSION ON GALLEY CROSSBEAM AND PROFILE. INSTALLED SERVICEABLE CROSS BEAM AND PROFILE IAW EMB145 SRM 51-20-03, 51-40-02 AND 51-40-06. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2

ABI - THIS IS A LEVEL 2 FINDING. GALLEY CENTER BEAM GUSSET CORRODED. INSTALLED SERVICEABLE CENTER BEAM GUSSET IAW EMB145 SRM 51-40-02. (M)

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2

ABI - THIS IS LEVEL 2 FINDING, DOUBLER ON LEFT HAT BEAM BETWEEN FRAMES 65 AND 68 CORRODED. REMOVED DAMAGED DOUBLER, INSTALLED NEW DOUBLER IAW EMB 145 SRM 51-40-02, 51-40-06, 51-20-03. (M)

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2

ABI - THIS IS A LEVEL 2 FINDING. CENTER GUSSET IN LAVATORY CORRODED. INSTALLED NEW GUSSET IAW EMB145 SRM 51-40-02, 51-40-06, 51-20-03. (M)

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2

ABI - THIS IS A LEVEL 2 FINDING ON CRIC NR 35576. RIGHT CABIN SILL HAS CORROSION BETWEEN FRAMES 23-29. (M)

Part: SWITCH — OUT OF ADJ (CARGO DOOR)

BMI - FLT 4427 - CARGO DOOR WARNING LIGHT CAME ON INFLIGHT. DROPPED TO 10,000. RETURNED TO BASE. ADJUSTED FORWARD AND AFT MICROSWITCHES ON CARGO DOOR IAW AMM 52-76-01-820-801-A. OPS CHECK GOOD. (M)

Part: SWITCH — OUT OF ADJ (THRUST REVERSER)

ORF - FLT 4366 - ABORTED TAKEOFF, NR 1 ENGINE REVERSE DISAGREE ICAS. PERFORMED STOW SWITCH TEST IAW EMB AMM 78-34-01-700-801A. PERFORMED ADJUSTMENT IAW 78-34-01-820-801A OF AMM. OPS CHECK GOOD. (M)

Part: CARBON SEAL — LEAKING (NR 2 ENGINE)

ORD - FLT 4051 - CREW REPORTED THE LAVATORY SMOKE WARNING MESSAGE ON EICAS AND THEN WENT OUT. TAKEOFF WAS ABORTED AND EMERGENCY WAS DECLARED. ORD FIRE DEPARTMENT FOUND NO EVIDENCE OF ANY SMOKE OR ANYTHING BURNED. MAINTENANCE FOUND THE ZERO CARBON SEAL LEAKING IN THE NR 2 ENGINE. CARBON SEAL WAS REPLACED IAW RR MM. OPERATIONAL AND LEAK CHECKS WERE GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: PITOT LINE — CONTAMINATED (PITOT STATIC SYS)

HOU - FLT 3618 - ON TAKEOFF ROLL, AIRSPEED SPLIT OF 7 KNOTS, CAPTAIN WAS 80 KNOTS AND F/OS WAS 73 KNOTS. RETURNED TO GATE FOR REPAIR. FERRIED A/C TO DFW. MOISTURE IN NUM 2 PITOT LINES. AIR OUT SYSTEM WITH NITROGEN. OPS CHECK GOOD. (M)

Part: SIGN — INOPERATIVE (CABIN)

CRP - FLT 3856 - FLIGHT CREW REPORTED BOTH OVERWING INTERIOR EXIT LIGHTS INOPERATIVE. MAINTENANCE FOUND BROKEN WIRE ON AFT EXIT SIGN. REMOVED AND REPLACED LIGHT ASSEMBLY. OPERAITONAL CHECK WAS SATISFACTORY AND AIRCRAFT WAS RETURNED TO SERVICE (M)

Part: LIGHT — INOPERATIVE (CABIN)

DFW - FLT 3561 - REAR FLOOR EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED EMERGENCY FLOOR LIGHT STRIP. OPS CHECK GOOD. (M)

Part: LIGHT — INOPERATIVE (CABIN)

ORD - FLT 4088 - EMERGENCY LIGHT ROW 7 INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT ASSY. (M)

Part: SET SCREWS — DAMAGED (SEAT 18)

XNA - PASSENGER SEAT 18BC FORWARD LOCK DOWN SET SCREWS DAMAGED. REMOVED AND REPLACED SET SCREWS. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

ORD - FLT 4265 - LEFT WING EXTERIOR EMERGENCY LIGHT DOES NOT ILLUMINATE. REMOVED AND REPLACED EMERGENCY BATTERY PACK NR 4. OPERATIONAL CHECK GOOD. (X)

Part: LIGHT — BROKEN (ROWS 17-18)

DFW - FLT 3675 - EMERGENCY FLOOR PROXIMITY LIGHT STRIP AT ROWS 17 AND 18 DOES NOT ILLUMINATE. REMOVED AND REPLACED LIGHT STRIP DUE TO A BROKEN CONNECTOR. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (X)