N668HH

Part: NONE — UNSERVICEABLE ([0000] [2] [) · airframe 43,407 hrs · 38,260 cycles

SEAT 3B EMERGENCY EXIT PLACARD INOP-C/A-RAR EMERGENCY BATTERY POWER SUPPLY 2 AND BATTERY PACK 2 IAW ENVOY WORK CARD 33-700-19. OPS CHECK GOOD. END.

Part: NONE — UNSERVICEABLE ([0000] [3] [) · airframe 43,407 hrs · 38,260 cycles

SEAT 12A EMERGENCY LIGHT PLACARD INOP-C/A-RAR EMERGENCY BATTERY POWER SUPPLY 3 AND BATTERY PACK 3 IAW ENVOY WORK CARD 33-700-19. OPS CHECK GOOD. END.

Part: LIGHT — INOPERATIVE (LH) · airframe 43,236 hrs · 38,072 cycles

LH FWD BELLY PANEL EMERGENCY LIGHT INOP.-C/A-RAR LH FWD BELLY PANEL EMERGENCY LIGHT ASSEMBLY, IAW AMM 33-50-10.

Part: LAMP — INOPERATIVE (LH) · airframe 42,955 hrs · 37,746 cycles

EXTERNAL EMERGENCY LIGHT FORWARD OF LH WING INOP-C/A-RAR EXTERNAL EMERGENCY LIGHT LAMP IAW EMB 145 AMM 33-50-10. OPC GOOD

Part: NONE — NONE (HS VALVE 2) · airframe 42,839 hrs · 37,601 cycles

HIGH SPEED ABORT TO FOR HS VALVE 2 FAIL / NO INJURIES REPORTED. HWS VLV 2 FAIL ON TAKEOFF ROLL SHORTLY AFTER SETTING TAKEOFF THRUST-C/A-PERFORMED TROUBLESHOOTING PER FIM 36-11-00-810-810-A. RAR HIGH STAGE VALVE PER AMM 36-11-02. OPC GOOD

Part: NONE — UNSERVICEABLE (AFT) · airframe 42,780 hrs · 37,541 cycles

MEL 2532 - AUTH# 05008M-C. LGPG 4874263. AFT FA FLASHLIGHT HOLDER CLIP BROKEN.-C/A-RAR AFT FA FLASHLIGHT BRACKET IAW AMM EMB145 33-51-01. NO DEFECTS NOTED. MEL ITEM RESTORED.

Part: NONE — UNSERVICEABLE (COCKPIT PARTITIO) · airframe 42,740 hrs · 37,504 cycles

EMERGENCY FLASHLIGHT ABOVE FLIGHT ATTENDANT SEAT WILL NOT CHARGE-C/A-RAR EMERGENCY FLASHLIGHT IAW AMM 33-50-16 OPS CHECK GOOD.

Part: NONE — NONE · airframe 42,338 hrs · 37,043 cycles

THIS IS A SUPPLEMENTAL SHOWING THE FWD CARGO SMOKE DETECTOR WAS REPLACED P/N 473597-13 S/N 0094. BAGGAGE SMOKE WARNING ON DURING FLIGHT. C/A BLEW BOTTLES.MECH EMERGENCY DECLARED AT 14,000FT/ BAGG EXT BUTTON PRESSED PER QRH. REST OF QRH CW-C/A-RAR BOTH BAGGAGE FIRE EXTINGUISHER BOTTLES IAW EMB 145 AMM 26-23-01. MEL RESTORED.-C/A-RAR BOTH BAGGAGE FIRE EXTINGUISHER BOTTLES IAW EMB 145 AMM 26-23-01. MEL RESTORED.

Part: NONE — NONE · airframe 41,688 hrs · 36,266 cycles

LG AIR/GND FAIL EICAS CAUTION DURING GEAR EXTENSION. WENT AWAY DURING GO AROUND."TRANSFERRED TO NRWC 668-ORD-05302" DECLARED EMERGENCY-C/A- RAR RH NLG ACTUATOR. REF NRWC 688-ORD-05302 FOR CORRECTIVE ACTIONS TAKEN.OPS CHECK GOOD. REF NWC 688-ORD-05302 FOR CORRECTIVE ACTIONS TAKEN. PERFORMED EXTENSION AND RETRACTION TEST IAW EMB 145 AMM 32-30-00. NO DEFECTS NOTED.

Part: FLASHLIGHT — INOPERATIVE (FWD CABIN) · airframe 41,609 hrs · 36,170 cycles

MEL ITEM 25-32 AUTH 090096M-CLOG PAGE 4793078/1FA FWD EMERGECNY FLASHLIGHT INOP-C/A-RAR EMERGENCY FLASHLIGHT IAW AMM 33-50-16 OPS CHECK GOOD MPROCEDUES REVERSED MEL ITEM RESTORED

Part: FLASHLIGHT — INOPERATIVE (FWD CABIN) · airframe 41,607 hrs · 36,169 cycles

FA FWD EMERGENCYFLASH LIGHT INOP-C/A-FLIGHT CREW PLACRD FWD FA EMERGENCYFLASH LIGHT IAW MEL 2532 M PROC C/W MOC # 624980

Part: SKIN — DAMAGED (RUDDER) · airframe 40,978 hrs · 35,459 cycles

RUDDER 2 SKIN AND ATTACH ANGLE DAMAGE CAUSED BY FOD JUST BELOW THE LOWER HINGE POINT.-C/A-REPAIRED IAW ERS-EM-55MR-884 AND ERS-EM-55-885

Part: BUSHING — MIGRATED (RT AILERON PCA) · airframe 40,978 hrs · 35,459 cycles

R/H AILERON PCA FITTING HAS 3 EA MIGRATING BUSHINGS.(2 OUTBD BUSHINGS ARE LOOSE IN THE FITTING BORE) -C/A-RAR RH AILERON PCA FITTING ASSY IAW EO EM-27MR-112.

Part: FLOOR SUPPORT — CORRODED (FRM 20) · airframe 40,978 hrs · 35,459 cycles

CPCP SSI: LH OUTBOARD FLOOR SUPPORT IS CORRODED AT NUTPLATE JUST AFT OF FRAME 20.-C/A-RAR'D LH OUTBD. FLOOR SUPPORT JUST AFT OF FR 20 IAW SRM 51-40-02.

Part: SHIM — MIGRATED (VERTICAL STAB) · airframe 40,978 hrs · 35,459 cycles

RUDDER #1 TO VERTICAL STAB LOWER HINGE POINT SCHACKLE HAS MIGRATING AND DAMAGED SHIMS.-C/A-RAR LOWER HINGE ASSY IAW EMB 145 SRM 51-40-02. (MAJOR REPAIR)

Part: SKIN — CRACKED (FUSELAGE) · airframe 40,978 hrs · 35,459 cycles

FUSELAGE SKIN HAS 4 EACH CRACKS AROUND RIVET (APPROX. 1/16" LONG) AT FRAME 77 BETWEEN STR 3R-4R. -C/A-REPAIRED SKIN AT FRAME 77 BETWEEN STR 3R-4R IAW SRM 53-32-01.

Part: SKIN — CRACKED (FUSELAGE) · airframe 40,978 hrs · 35,459 cycles

FUSELAGE SKIN HAS 13 EACH CRACKS AROUND RIVET (APPROX. 1/16" LONG) AT FRAME 77 BETWEEN STR 3L-7L. E854459, E854460, E854461, AND E854462-C/A-REPAIRED SKIN AT FRAME 77 BETWEEN STR 3L-4L IAW SRM 53-32-01.-REPAIRED SKIN AT FRAME 77 BETWEEN STR 4L-5L IAW SRM 53-32-01.- REPAIRED SKIN AT FRAME 77 BETWEEN STR 5L-6L IAW SRM 53-32-01.- REPAIRED SKIN AT FRAME 77 BETWEEN STR 6L-7L IAW SRM 53-32-01.

Part: SKIN — CRACKED (FUSELAGE) · airframe 40,978 hrs · 35,459 cycles

FUSELAGE SKIN HAS 9 EACH CRACKS AROUND RIVET (APPROX. 1/16" LONG) AT FRAME 78 BETWEEN STR 5L-7L. (E854463, E854464) -C/A-REPAIRED SKIN AT FRAME 78 BETWEEN STR 6L-7L IAW SRM 53-32-01. AND REPAIRED SKIN AT FRAME 78 BETWEEN STR 5L-6L IAW SRM 53-32-01.

Part: FIREWALL — CRACKED (APU BAY) · airframe 40,978 hrs · 35,459 cycles

APU FIREWALL HAS A CRACK PROTRUDING FROM THE UPPER R/H MOUNT-C/A-REPAIRED APU FIREWALL ON RH UPPER MOUNT IAW ETN-EM-53-244 R3.

Part: SKIN — CRACKED (FRM 79 S6-7R) · airframe 40,978 hrs · 35,459 cycles

FUSELAGE SKIN HAS 4 EACH CRACKS AROUND RIVET (APPROX. 1/16" LONG) AT FRAME 79 BETWEEN STR 6R-7R. -C/A-REPAIRED SKIN AT FRAME 79 BETWEEN STR 6R-7R IAW SRM 53-32-01.

Part: FLOOR SUPPORT — CRACKED (FRM 46) · airframe 40,978 hrs · 35,459 cycles

SSI CENTER OMEGA BEAM OUTBD SUPPORT ANGLE IS CRACKED JUST AFT OF FRAME 46 -C/A-REPAIRED CENTER OMEGA BEAM OUTBD SUPPORT ANGLE JUST AFT OF FR46 IAW SRM 53-23-02-RE AND SRM 51-40-02.

Part: MOUNT — CRACKED (TORSION BAR) · airframe 40,978 hrs · 35,459 cycles

CARGO DOOR TORSION BAR MOUNT FLANGE IS CRACKED ON THE FWD. END AT FR 61RH. -C/A-RAI CARGO DOOR TORSION BAR MOUNT AT FRAME 61 IAW SRM 51-40-02.

Part: SUPPORT — CORRODED (FRMS 50-57) · airframe 40,978 hrs · 35,459 cycles

CPCP SSI R/H FLOOR/WALL SUPPORT IS CORRODED FROM FRAMES 50-57.-C/A-RAR RH FLOOR/WALL SUPPORT FROM FRAMES 50-57 IAW EMB 145 SRM 51-40-02.

Part: CHANNEL — CRACKED (FRMS 47-48) · airframe 40,978 hrs · 35,459 cycles

R/H HAT BEAM SUPPORT IS CRACKED BETWEEN FRAMES 47 AND 48. -C/A-REPAIRED RH HAT BEAM SUPPORT IAW SRM 53-23-02. AND SRM 51-40-02.

Part: BRACKET — CRACKED (CARGO DOOR HOLD) · airframe 40,978 hrs · 35,459 cycles

CARGO DOOR HOLD OPEN ROD BRACKET IS CRACKED ON THE FUSELAGE. -C/A-RAR'D CARGO DOOR HOLD OPEN ROD BRACKET IAW SRM 51-40-02.

Part: CONNECTOR — DETACHED (EMERGENCY LIGHTS) · airframe 40,978 hrs · 35,459 cycles

THE SECOND EMERGENCY LIGHT BELOW FLOOR WIRING (FLOOR BOARD 241BF) NEEDS A NEW CONNECTOR DUE TO THE ONE USED HAD TO BE CUT OFF,-C/A-COMPLETE:REPLACED CONNECTOR FOR EMERGENCY LIGHT UNDER FLOORBOARD 241BF IAW SWPM 20-50-00. REF NRWC E354290 FOR OPC.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 40,978 hrs · 35,459 cycles

THE SECOND EMERGENCY LIGHT STRIP ( GOING AFT ) HAS BROKEN WIRES AT THE POTTED END, REQUIRES REPLACEMENT.-C/A-COMPLETE:INSTALLED NEW #2 EMERGENCY LIGHT STRIP IAW AMM 33-50-12, OPS CHECK GOOD

Part: UNKNOWN — ODOR (COCKPIT/CABIN) · airframe 40,770 hrs · 35,249 cycles

WHILE IN CRUISE FLIGHT FL30, COMING INTO DFW, WE EXPERIENCED HEAVY MODERATE TURBULENCE. WHILE GOING THROUGH IT, WE STARTED TO SMELL IN THE COCKPIT, AND SOME PASSENGERS SMELL IT TOO IN THE CABIN.-C/A-PERFORMED INSP. FOR SMOKE/ABNORMAL SMELL IN CABIN/COKPIT - UNKNOWN SOURCE IAW FIM TASK 21-20-00-810-801-A. FOLLOWED BLOCK DIAGRAM TASKS. NO DISCREPANCIES NOTED.

Part: CONNECTOR — BURNED (CEILING LIGHT) · airframe 40,638 hrs · 35,119 cycles

BURNING SMELL NEAR ROW 8 IN CABIN WHEN PACK AND RECIRC FANS ON. CEILING LIGHT ASSY AT SEAT 6 CB SHOWS BURN MARKS ON CONNECTOR REF. TO AML 4523826 ITEM #1 BURNING SMELL NEAR ROWS 6,7 AND 8 IN CABIN PER WORK SCOPE INSPECTION.PERFORM FIM TASK 21-20-00-810-801-A (REF. ETN-EM-21-067) PER WORK SCOPE REF. TO AML 4523826 ITEM #1 BURNING SMELL NEAR ROW 8 IN CABIN.-C/A-FOUND CEILING LIGHT ASSY AT SEAT 6 CB HAD BURNED LAMP CONNECTOR. REMOVED AND REPLACED CEILING LIGHT ASSY IAW EMB 145 AMM 33-21-06. REF. TO NRWC # 668-DFW-04912 AND NRWC # 668-DFW-04913. OPS CHECK GOOD. ALSO PERFORMED FIM TASK 21-20-00-810-801-AOIL. DECONTAMINATION BURN OUT ITEM #1 BURNING SMELL NEAR ROW 8 IN CABIN IAW AMM 21-20-00-100-806 NO SMELL

Part: CRADLE — BROKEN (AFT FLASHLIGHT) · airframe 40,533 hrs · 35,031 cycles

AFT FLASHLIGHT MOUNT CLIP BROKEN. C/A: R & R AFT FLASHLIGHT, IAW ENVOY ETN-EM-33-059. OPERATIONS CHECK GOOD.

Part: CRADLE — BROKEN (AFT FLASHLIGHT) · airframe 40,310 hrs · 34,814 cycles

REAR EMERGENCY FLASHLIGHT HOLDER BROKEN IN CABIN. C/A: R & R EMERGENCY FLASHLIGHT ASSEMBLY, IAW AMM EMB-145 AMM 33-50-16. OPERATIONS CHECK GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION (SMOKE DETECTOR) · airframe 40,215 hrs · 34,716 cycles

LAV SMOKE INDICATION WARNING IN FLIGHT. PASSENGER WAS IN LAV, FA REPORTS DID NOT SEE OR SMELL SMOKE. PASSENGER OPENED LAV DOOR. DECLARED EMERGENCY. C/A: PERFORMED OPERATIONS CHECK OF LAV SMOKE DETECTION SYSTEM, IAW AMM 26-14-00. OPERATIONS CHECK GOOD AT THIS TIME, NO DEFECTS NOTED.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 40,084 hrs · 34,578 cycles

SMOKE IN COCKPIT, BURNING SMELL IN THE AIRPLANE ON CLIMBOUT. NO SMOKE AND NO EICAS MESSAGES. TROULBESHOOTING ITEM NR 1, BURNING SMELL IN AIRPLANE. ETN -EM-72-034 DUE. C/A C/W ETN-EM-72-034.

Part: CRADLE — BROKEN (FLASHLIGHT) · airframe 40,083 hrs · 34,576 cycles

FLASHLIGHT BRACKET BEHIND CAP & SHAIR BROKEN. C/A-RAR CAP FLASHLIGHT PER EMB AMM 33-50-16.

Part: CONNECTOR — BROKEN (EMERGENCY LIGHT) · airframe 39,807 hrs · 34,307 cycles

BROKEN ELECTRICAL CONNECTOR ON FLOOR LIGHTING STRIP AT SEAT 7A.-C/A-INSTALLED NEW CONNECTOR ON LIGHTING STRIP AT SEAT 7A PER SPWM 20-50-01. OPS CK GOOD

Part: UNKNOWN — ODOR (CABIN & COCKPIT) · airframe 39,789 hrs · 34,291 cycles

FA REPORTS CHEMICAL SMELL IN CABIN AND SAYS CABIN BECAME VERY WARM. CABIN TEMP INDICATIONS SHOWED 18C. PACK 1 AND 2 OPERATIONAL TESTS GOOD WITH APU AND BOTH ENGINE PNEUMATIC SOURCES IAW AMM 21-51-00. PACK 1 AND 2 GVI AND LEAK CHECKED GOOD IAW AMM 21-51-14. NO ODORS NOTED IN CABIN OR COCKPIT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 39,718 hrs · 34,207 cycles

SERVICE DOOR EMERGENCY LIGHT IS INOP-C/A-REMOVED AND REINSTALLED SERVICE DOOR EXTERNAL EMERGENCY LIGHT LAMP IAW EMB 145 AMM 33-50-10. OPS-CK GOOD.

Part: FLASHLIGHT — BROKEN (CABIN) · airframe 39,690 hrs · 34,178 cycles

SUPPLEMENTAL AFT CABIN FLASHLIGHT BROKEN-C/A-FLIGHT CREW PLACARD AFT CABIN FLASHLIGHT AUTH 030546-C REF - 25-53 MOC 864015. REMOVED AND REPLACED AFT CABIN FLASHLIGHT IAW EMB 145 AMM 33-50-16 OPS CHECK GOOD . MEL ITEM RESTORED

Part: POWER SUPPLY — DISCONNECTED (CABIN) · airframe 39,609 hrs · 34,097 cycles

DURING PS-2 CHECK , WAS FOUND FWD CABIN EMERGENCY LIGHTS INOP.-C/A-RECOONNECTED #1 EMERGENCY KLIGHT POWER SUPPLY IAW EMB-145 AMM 33-50-04 . OPS CHECK GOOD.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 39,164 hrs · 33,744 cycles

EMERGENCY LIGHTING SYSTEM (FLOOR PROXIMITY STRIP) AT SEAT 3A WIRE BROKEN INOP-C/A-EMER FLOOR STRIP LIGHTING AT SEAT 3A DEFERRED. REPAIRED BROKEN WIRE AT FLOOR STRIP 3A IAW SWPM 20-21-00. OPS CHECK GOOD. MEL RESTORED.

Part: APU — MALFUNCTIONED · airframe 38,946 hrs · 33,566 cycles

APU FAIL & SHUTDOWN DURING STEADY STATE OPERATION AT FL360.-C/A-CHECKED OK FOR DEFERRAL PER MEL 49-1. M PROCEDURES C/W. AUTH # 110898DM-C. EXPIRES 12-6-19. PLACARD INSTALLED. PERF OPERATIONL TEST OF APU WITH BOTH ELECTRICAL AND PNEUMATIC LOADS IAW EMB 145 AMM 49-13-00. OPS TEST GOOD. NO DEFECTS NOTED. MEL ITEM RESTORED. (M) PROCEDURES REVERSED.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 38,615 hrs · 33,286 cycles

AFT CEILING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED AFT CEILING EMERGENCY LAMP IAW AMM 33-50-08-000-801-A AND 33-50-08-400-801-A. OPS CHECK GOOD.

Part: PRESSURE SWITCH — CORRODED (PARKING BRAKE) · airframe 37,956 hrs · 32,695 cycles

NO TAKEOFF CONFIG WARNING ON THRUST SET WITH PERIMETER APPEARING OK. IN PARALLEL "TAKE OFF OK" IS GIVEN WITH P. BRAKE SET. FOUND PARKING BRAKE PRESSURE SWITCH AND PARKING BRAKE PRESSURE SWITCH CONNECTOR SEVERELY CORRODED. REPLACED BOTH. OPS/CK LK/CK GOOD. TAKE OFF CONFIG CHECKS GOOD. REMOVED AND REPLACED ELECTRICAL CONNECTOR AT P0528 IAW EMB SWPM 20-51-01.

Part: BOLT — DAMAGED (DOOR HANDLE) · airframe 37,880 hrs · 32,643 cycles

MAIN CABIN DOOR JAMMED IN THE CLOSED POSITION & WOULD NOT OPEN-C/A-DURING INSPECTION FOUND BOLT AND NUT SECURING DOOR HANDLE TO BE DAMAGED. REMOVED AND REPLACED BOLT AND NUT IAW EMB AMM 52-18-05

Part: RIB — CRACKED (LT WING) · airframe 37,158 hrs · 31,991 cycles

LEFT WING UPPER RIB 21 HAS A CRACK APPROXIMATELY 1/4" ON FLANGE. C/A-COMPLETED REPAIR TO LT WING RIB 21 IAW SRM 57-20-07.

Part: AILERON — EXCESS PLAY (RT WING) · airframe 37,158 hrs · 31,991 cycles

RIGHT HAND AILERON HAS PLAY AT THE ACTUATOR ATTACHMENT. THE SHIMMY DAMPER FITTING HAS TOOL MARKS. REPLACED RT AILERON WITH SERVICEABLE PART FROM STORES. FITTING P/N 145-6982-610

Part: DOOR SILL — CORRODED (FRAMES 65-68) · airframe 37,158 hrs · 31,991 cycles

CARGO DOOR SILL IS CORRODED BETWEEN FRAMES 65-68. -C/A-REMOVED AND REPLACED CARGO DOOR SILL IAW SRM 51-41-02.

Part: ANGLE — CRACKED (FRAMES 47-48) · airframe 37,158 hrs · 31,991 cycles

R/H HAT BEAM ANGLE IS CRACKED BETWEEN FRS 47 AND 48. -C/A-INSTALLED NEW RH HAT BEAM ANGLE IAW SRM 51-40-02.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 37,158 hrs · 31,991 cycles

UPPER WING TO FUSELAGE FAIRING ATTACH ANGLE ON FUSELAGE HAS A 1" CRACK AT FRAME 42. REMOVED AND REPLACED RT UPPER WING TO FUSELAGE FAIRING ATTACH ANGLE AT FRAME 42 IAW SRM 51-40-02.

Part: BRACKET — CRACKED (NLG UPLOCK) · airframe 37,158 hrs · 31,991 cycles

NLG UPLOCK BOX BRACKET IS CRACKED IN THE FWD, LOWER, LH CORNER.-C/A-REPLACED BRACKET IAW SRM 51-40-02.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 37,158 hrs · 31,991 cycles

LT FUSELAGE SKIN FROM FR 9- FR 12 AT STR 21L TO 18L HAS 4 EACH BURN MARKS (CIRCLED). C/A-COMPLETE:REPAIRED 4EA BURN MARKS IAW SRM 53-00-01.

Part: LIGHT — CRACKED (CABIN) · airframe 37,158 hrs · 31,991 cycles

NR 5 EMERGENCY FLOOR PROXIMITY STRIP LIGHT ASSY CRACKED. C/A-COMPLETE:REPLACED NR 5 EMERGENCY FLOOR PROXIMITY STRIP LIGHT ASSY IAW AMM 33-50-12, REFERENCE BOW 314230 FOR OPS CHECK.

Part: WIRE — BROKEN (CABIN) · airframe 37,158 hrs · 31,991 cycles

NR 3 FLOOR PROXIMITY STRIP LIGHT WIRES ARE BROKEN OFF AT BASE. C/A-COMPLETE:REMOVED AND REPLACED NR 3 FLOOR PROXIMITY STRIP LIGHT IAW AMM 33-50-12.

Part: CONTROL UNIT — FAILED (HORIZONTAL STAB) · airframe 36,744 hrs · 31,572 cycles

PTRIM MAIN INOP @ FL260-C/A-REMOVED AND REPLACED HORIZONTAL STABILIZER CONTROL UNIT IAW AMM 24-40-01 OP CK GOOD IAW AMM 27-40-00

Part: STOP FITTING — LOOSE (PAX DOOR) · airframe 35,847 hrs · 30,730 cycles

PAX DOOR HARD TO OPEN. C/W INSPECTION AND LUBE OF THE PAX MAIN DOOR FOUND ONE OF DOOR STOP LOOSE STOP TIGHTENED IAW ETN-EM-52-047, DOOR OPS CHECK GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 35,269 hrs · 30,168 cycles

SERVICE DOOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE LAMP IAW AMM 33-50-10-000-801-A, AND 33-50-10-400-801-A. OPS CHECKED GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 35,232 hrs · 30,124 cycles

SERVICE DOOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE LAMP IAW AMM 33-50-10-000-801-A, AND 33-50-10-400-801-A. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (FLASHLIGHT) · airframe 32,985 hrs · 28,193 cycles

FLASHLIGHT IN COCKPIT INOPERATIVE. REMOVED AND REPLACED THE BULB. OPS CHECKED GOOD.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 32,820 hrs · 28,047 cycles

EMERGENCY LIGHT/SIGN JUST ABOVE THE SERVICE DOOR IS INOP. R&R N R2 EMERGENCY LIGHT INVERTER, OPC GOOD, IAW AMM 30-50-11.

Part: ECU — FAILED (TE FLAP SYS) · airframe 32,319 hrs · 27,614 cycles

FLAPS FAIL AND SPS ADVANCE ON EICAS DURING FLAP RETRACTION AFTER TAKE OFF FLAPS FAIL AT 9 DEGS. REMOVED AND REPLACED FLAP ELECTRONIC CONTROL UNIT IAW AMM 27-53-02. OPS CHECKED GOOD.

Part: SENSOR — FAILED (TE FLAPS) · airframe 32,304 hrs · 27,600 cycles

FLAP FAILED AFTER TAKE OFF. REMOVED AND REPLACED FVS IAW AMM 27-51-12. OPS CHECKED GOOD. NO MESSAGE FOUND

Part: SKIN — CRACKED (FRAME 75) · airframe 32,290 hrs · 27,588 cycles

LEFT AFT FUSELAGE FRAME 75 SKIN CRACKED ABOVE STRINGER 2L. REPAIRED THE SKIN IAW SRM 53-31-01 ITEM 11.

Part: STRINGER — CRACKED (FRAME 75) · airframe 32,287 hrs · 27,586 cycles

STRINGER 2L CRACKED AT FRAME 75. REPAIRED THE STRINGER IAW ERS-EM-53MR-2414.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 32,286 hrs · 27,585 cycles

SERVICE DOOR EMERGENCY LIGHT IS INTERMITTANT. REPAIRED A DAMAGED WIRE IAW SWPM 20-21-00 AND 20-50-00. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,707 hrs · 27,060 cycles

SERVICE DOOR EMERGENCY LIGHT INOPERATIVE. R AND R SERVICE DOOR EMERGENCY LIGHT LAMP IAW AMM TASK 33-50-10-000-801-A AND 33-50-10-400-801-A. OPC GOOD.

Part: ROLLER — LACK OF LUBE (CABIN DOOR) · airframe 31,481 hrs · 26,852 cycles

MAIN CABIN DOOR HANDLE DIFFICULT TO MOVE AND DOOR DIFFICULT TO OPEN AND CLOSE, MAY BE DUE TO DOOR MISALIGNMENT. LUBE ROLLERS AND DOOR HANDLE, DOOR OPS CHECK GOOD IN NORMAL OPERATION IAW AMM 52-10-00.

Part: ROLLER — LACK OF LUBE (CABIN) · airframe 31,101 hrs · 26,506 cycles

MAIN CABIN DOOR DIFFICULT TO OPEN. PERFORMED LUBRICATION OF MAIN CABIN DOOR FRAME ROLLERS IAW AMM 53-21-02. OPERATIONS CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (COCPIT) · airframe 30,932 hrs · 26,330 cycles

FIRST OFFICERS, CAPTAINS & FLIGHT ATTENDANT ALL SMELL ELEC BURNT SMELL EMANATING FROM FWD CLOSET. FOUND FLIGHT ATTENDANT FLASHLIGHT BURNED OUT. REPLACED FLIGHT ATTENDANT FLASHLIGHT IAW ACFT MX PRACTICES.

Part: HOLDER — BROKEN (FLASHLIGHT) · airframe 30,223 hrs · 25,724 cycles

CAPTAINS FLASH LIGHT HOLDER IS BROKEN, IT WILL NOT HOLD FLASHLIGHT ON LANDING & FALLS OUT. REPLACED CAPTAINS FLASHLIGHT HOLDER IAW AMM 25-60-00.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 29,768 hrs · 25,304 cycles

FORWARD OVERHEAD EMER EXIT SIGN INOPERATIVE. R & R NR 1 EMER BATTERY CHARGER & BATTERY IAW WC 33-700-19. OPERATIONS CHECKED GOOD, LIGHT STILL OUT IAW ITEM 2 OF THIS NRWC. INVERTER PN 7824-1, SN 813961 & EMER BATTERY PN 2013-1A & SN 66412.

Part: TIRE — FAILED (LT MLG) · airframe 29,451 hrs · 25,027 cycles

NUMBER 2 TIRE SHREDDED ON TAKEOFF, NOT CONFIRMED UNTIL CLOSE TO LANDING BY TOWER PERSONNEL. REPLACED NR 2 MAIN WHEEL TIRE ASSEMBLY IAW WC 32-700-11. COMPLIED WITH LG TIRE TREAD FAILURE INSPECTION CHECK IAW AMM 05-50-15. IAW AML 3944717 ITEM 3 & NRWC 686-ORD-01960, 686-ORD-01961, 686-ORD-01962 & 686-ORD-01963 FOR DISCREPANCIES FOUND. FOUND DAMAGE TO LT INBD FLAP AFTER TIRE TREAD SEPARATION. INSPECTED LT INBD FLAP IAW SRM57-52-00 FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED LT INBD FLAP IAW EMB 145 AMM 27-50-00 RIG AND OPS CHECK GOOD. INBOARD FLAP LT (RII) P/N 145-68000-627 S/N 173

Part: CHARGER — INOPERATIVE (CABIN) · airframe 29,094 hrs · 24,697 cycles

DURING PS 1 INSPECTION FOUND FLOOR PROXIMITY EMER LIGHTS SECTIONS 6,7 & 8, BOTH LT & RT EXTERIOR OVERWING LIGHTS & AISLE LIGHTS 3 & 4 INOPERATIVE. R & R NR 4 EPSU CHARGER ASSEMBLY & BATTERY PACK IAW AMM 33-50-04. OPERATIONS CHECKED OK. EMER LIGHTING BATTERY PN 2013-1A & SN 85527.

Part: DOOR FRAME — CORRODED (CARGO DOOR) · airframe 27,555 hrs · 23,409 cycles

CORROSION FOUND AROUND NUTPLATES ON CGO DOOR FWD FRAME. ACCOMPLISHED REPAIR ON CGO DOOR FWD FRAME IAW ERS-EM-52MR-238.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 27,555 hrs · 23,409 cycles

CARGO DOOR FRAME 65 CORRODED JUST ABOVE THE SHEAR CLIP. REMOVED CORROSION IAW SRM 51-10-03. ACCEPTED AS IS IAW ERS-EM-5300-807.

Part: SKIN — CRACKED (FUSELAGE) · airframe 27,555 hrs · 23,409 cycles

EXTERNAL LT FUSELAGE SKIN CRACKED AROUND RIVET FRAME 79 MARKED. REPAIRED IAW ERS EM-5300-808.

Part: SKIN — CRACKED (FUSELAGE) · airframe 27,555 hrs · 23,409 cycles

EXTERNAL RT FUSELAGE SKIN CRACKED AROUND RIVET FRAME 78 MARKED. REPAIRED EXTERNAL RT FUSELAGE SKIN CRACK AROUND RIVET AT FRAME 78 IAW ERS EM-5300-803.

Part: SKIN — CRACKED (FUSELAGE) · airframe 27,555 hrs · 23,409 cycles

EXTERNAL RT FUSELAGE SKIN CRACKED AROUND RIVET FRAME 79 MARKED. REPAIRED EXTERNAL RT FUSELAGE SKIN CRACK AROUND RIVET AT FRAME 79 IAW EM-5300-804.

Part: SKIN — CRACKED (FUSELAGE) · airframe 27,555 hrs · 23,409 cycles

EXTERNAL LT FUSELAGE SKIN CRACKED AROUND RIVET FRAME 78 MARKED. REPAIRED EXTERNAL LT FUSELAGE SKIN CRACK AROUND RIVET AT FRAME 78 IAW ERS EM-5300-808.

Part: ROLLER — LACK OF LUBE (CABIN DOOR) · airframe 26,833 hrs · 22,741 cycles

FLIGHT ATTENDANT REPORTS MAIN CABIN DOOR HARD TO OPEN & CLOSE. SERVICED MAIN DOOR ROLLER IAW AMM 53-21-02 & ETN-EM-52-061 WAS SERVICED. OPERATIONS CHECKED GOOD IAW AMM 52-18-00.

Part: ROLLER — LACK OF LUBE (CABIN DOOR) · airframe 26,717 hrs · 22,631 cycles

MAIN CABIN DOOR DIFFICULT TO OPEN & CLOSE. SERVICED MAIN DOOR FRAME ROLLERS & SUCCESSFULLY ACCOMPLISHED MAIN DOOR INTERNAL ACTUATING TEST IAW WMB-145, AMM 53-21-02 & AMM 52-10-01. OK FOR CONTINUED SERVICE. .

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,354 hrs · 22,285 cycles

DURING PS 2 CHECK FOUND SERVICE DOOR EMERGENCY LIGHT INOPERATIVE. R & R LIGHT LAMP IAW MM 33-50-09, OPERATIONS CHECKED GOOD.

Part: SIGN — INOPERATIVE (CABIN) · airframe 26,354 hrs · 22,285 cycles

FWD BULKHEAD INTERIOR EMERGENCY LIGHTING SIGN INOPERATIVE. R & R FWD BULKHEAD INTERIOR EMERGENCY LIGHTING SIGN ASSEMBLY IAW AMM 33-50-13, OPERATIONS CHECKED GOOD, NO DEFECTS NOTED.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 26,354 hrs · 22,285 cycles

LEFT WING FWD EMERGENCY LIGHT INOPERATIVE. R & R LT WING FWD EMERGENCY LIGHT BULB IAW AMM 33-50-10, OPERATIONS CHECKED GOOD, NO DEFECTS NOTED.

Part: ELT — NO TEST (CABIN) · airframe 26,321 hrs · 22,250 cycles

ELT IS FAILING THE OPS CHECK IAW WORK CARD 25-700-07. BIT TEST INDICATES A THREE FLASH FAULT CODE. R & R ELT TRANSMITTER ASSEMBLY IAW AMM 25-61-01. R & R ELT TRANSMITTER CABLE IAW SWPM 20-21-00. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 25,477 hrs · 21,610 cycles

EMERGENCY LIGHT IN COCKPIT INOPERATIVE. R & R LAMP IN COCKPIT EMERGENCY LIGHT IAW EMB 145 AMM 33-50-05-000-801-A & 33-50-05-400-801-A, OPERATIONS CHECKED GOOD.

Part: ISIS — MALFUNCTIONED · airframe 25,473 hrs · 21,607 cycles

ON FLIGHT 9533 CREW REPORTED ISIS ATT. CAGE FLAG & DECLARED EMERGENCY. THE ACFT WAS REMOVED FROM SERVICE. R & R ISIS IAW EMB-145 AMM 34-01-0. OPERATIONS CHECKED GOOD, THE ACFT RETURN TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 25,428 hrs · 21,572 cycles

FLASHLIGHT ABOVE FLIGHT ATTENDANT SEAT INOPERATIVE. R & R FLASHLIGHT IAW 145 AMM 33-50-16, OPERATIONS GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,400 hrs · 20,732 cycles

FOUND EMERGENCY LIGHT INOPERATIVE. R & R EMERGENCY LIGHT IAW AMM 33-50-12. OPS CHECKED GOOD, NO DEFECTS NOTED.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 24,394 hrs · 24,394 cycles

DURING MX INSPECTION, FOUND THE FLOOR PROXIMITY WARNING EMERGENCY LIGHT 6 & 7 WOULD NOT ILLUMINATE. ACFT REMOVED FROM SERVICE. FOUND BROKEN WIRES. R & R THE FLOOR PROXIMITY LIGHT IAW 33-50-12. OPS CHECKED GOOD. ACFT RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (AFT CABIN) · airframe 24,294 hrs · 20,643 cycles

CREW REPORTED AFT CABIN FLASHLIGHT WAS NOT CHARGING. ACFT REMOVED FROM SERVICE. R & R FLASHLIGHT IAW AMM 33-50-16. OPS CHECKED GOOD. ACFT RETURNED TO SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 24,235 hrs · 20,591 cycles

DURING B INSPECTION, FOUND THE MAIN DOOR ENTRY EMERGENCY LIGHT INOPERATIVE. ACFT REMOVED FROM SERVICE. R & R THE BATTERY IAW W/C 33-700-19. OPS CHECKED GOOD. ACFT RETURNED TO SERVICE.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 24,235 hrs · 20,591 cycles

DURING B INSPECTION, FOUND THE MAIN DOOR ENTRY EMERGENCY LIGHT INOPERATIVE. ACFT REMOVED FROM SERVICE. R & R POWER SUPPLY NR 1 IAW W/C 33-700-19. OPS CHECKED GOOD. ACFT RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 23,918 hrs · 20,325 cycles

DURING MX INSP, FOUND THE CAPTAIN’S FLASHLIGHT INOPERABLE. THE ACFT WAS REMOVED FROM SERVICE. R & R THE CAPTAIN’S FLASHLIGHT IAW AMM 33-50-16. THE OPS CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 23,315 hrs · 19,849 cycles

DURING B INSPECTION FOUND THE EXTERIOR LEFT AFT EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EXTERIOR LEFT AFT EMERGENCY LIGHT LAMP IAW EMB 145 AMM 33-50-10. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — NOT SEATED (CABIN) · airframe 23,049 hrs · 19,638 cycles

ON FLIGHT 3254 THE CREW REPORTED THE FLASHLIGHT IN THE AFT CABIN RED LIGHT DID NOT ILLUMINATE. THE AIRCRAFT WAS REMOVED FROM SERVICE. RESEATED FLASHLIGHT TO HOLDER AS REQUIRED, PERFORMED OPERATIONAL CHECK OF THE FLASHLIGHT ASSEMBLY IAW EMB 145 AMM CHAP 33-51-01. THE OPERATIONAL CHECK WAS GOOD. NO DEFECTS NOTED AT THE TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 22,965 hrs · 19,574 cycles

DURING MAINTENANCE INSPECTION FOUND THE FORWARD EMERGENCY LIGHTS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE BATTERY & BATTERY CHARGER. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — LOOSE (CABIN) · airframe 22,965 hrs · 19,574 cycles

DURING B INSPECTION FOUND THE SERVICE DOOR EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. RE-SECURED SERVICE DOOR EMERGENCY LIGHT BULB IAW EMB 145 AMM 33-50-10. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE — BROKEN (CABIN) · airframe 22,192 hrs · 18,962 cycles

DURING MAINTENANCE INSPECTION FOUND THE EMERGENCY LIGHT STRIP NR 8 (MOST AFT) HAS BROKEN WIRE LEADING TO SPLICE SP9213 ON AIRCRAFT SIDE. DIFFERED AFT EMERGENCY LIGHT STRIP PER MEL 33-30. REPAIRED SPLICE SP9213 IAW EMB WM 20-21-00. THE OPERATIONAL CHECK WAS GOOD, MEL RESTORED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: UNKNOWN — MALFUNCTIONED (ELEVATOR) · airframe 22,193 hrs · 18,964 cycles

DURING MAINTENANCE INSPECTION FOR FLIGHT 4304, TROUBLESHOT ELEVATOR IT WOULD NOT PUSH FORWARD DURING LANDING. PERFORM CHECK OF GUST LOCK SYSTEM. PERFORMED GENERAL VISUAL INSPECTION AND OPERATIONAL CHECK OF ELEVATOR GUST LOCKS. NO DEFECTS NOTED AT THIS TIME IAW EMB 145 AMM 27-31-01. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: DOOR — LACK OF LUBE (CABIN) · airframe 22,175 hrs · 18,944 cycles

FOR FLIGHT 3543 THE FLIGHT ATTENDANT REPORTED THE MAIN DOOR WAS DIFFICULT TO OPEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. LUBRICATED MAIN PASSENGER DOOR IAW EMB 145 AMM 52-18-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DEFECTIVE (MAIN) · airframe 22,146 hrs · 18,920 cycles

DURING MAINTENANCE INSPECTION FOUND THE BATTERY VOLTAGE PROPS RAPIDLY BELOW 23.5 VOLTS AS SOON AS GENERATOR POWER IS SHUTDOWN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED BATTERY 1 AND 2 IAW WC 24-600-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: COVER — DAMAGED (EMERGENCY LIGHT) · airframe 21,770 hrs · 18,606 cycles

DURING B INSPECTION, FOUND THE MAIN DOOR EMERGENCY LIGHT COVER HAS A HOLE IN IT. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE MAIN DOOR EMERGENCY LIGHT COVER IAW AMM 25-23-04 STEPS 2J(3)(G), 3I(3)(E). OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (FWD CABIN) · airframe 21,733 hrs · 18,584 cycles

DURING B INSPECTION, FOUND THE FLIGHT ATTENDANT FLASHLIGHT INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE FLIGHT ATTENDANT FLASHLIGHT IAW AMM 33-50-16-000-801-A AND 33-50-16-400-801-A. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,336 hrs · 21,336 cycles

DURING B INSPECTION FOUND THE RIGHT AFT EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT AFT OVER THE WING EMERGENGY LIGHT LAMP IAW EMB 145 AMM 33-50-10. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CRADLE — BROKEN (FLASHLIGHT) · airframe 21,251 hrs · 18,200 cycles

DURING MAINTENANCE INSPECTION FOUND THE AFT FLIGHT ATTENDANT’S FLASHLIGHT CRADLE BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AFT FLASHLIGHT CRADLE ASSEMBLY IAW 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 4,123 hrs · 18,200 cycles

DURING MAINTENANCE INSPECTION FOUND THE FORWARD ENTRY CEILING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CEILING LAMP IAW 33-50-06-000-801-A AND 33-50-06-400-801-A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: COVER — TORN (MAIN DOOR) · airframe 21,182 hrs · 18,154 cycles

ON FLIGHT 4262 THE FLIGHT ATTENDANT REPORTED THE MAIN DOOR WAS HARD TO OPEN/CLOSE. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND INNER DOOR HANDLE RUBBER COVER RIPPED, REMOVED AND REPLACED AS PER STANDARD MTX PRACTICES, WITHIN LIMITS PLUS PULL TEST FIM 52-18-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ROLLER — LACK OF LUBE (MAIN DOOR) · airframe 20,739 hrs · 17,790 cycles

ON FLIGHT 2954 THE FLIGHT ATTENDANT REPORTED THE MAIN DOOR HANDLE WAS HARD TO MOVE TO THE OPEN POSITION. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED MAIN-DOOR FRAME ROLLERS LUBRICATION PER EMB-145 AMM 53-21-02. THE OPERATIONAL CHECK WAS SATISFACTORY. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FAN — MALFUNCTIONED (CABIN) · airframe 20,603 hrs · 17,688 cycles

FLT 3220 CREW REPORTED AT CRUISE ALT, FLT LEVEL 360. NR 1 PACK OVERHEATED AND CAME OFF LINE. THEY COULD SMELL A VERY STRONG PRESENCE OF WHAT SEEMED LIKE SMOKE AND AN ELECTRICAL ODOR. CREW DECLARED AN EMERGENCY AND DIVERTED. LANDED WITHOUT INCIDENT. PERFORMED ETN FOR ENGINE ODOR EVENT AND INSPECTION OF COCKPIT AND CABIN FOR UNKNOWN ODOR SMOKE SMELL IAW ETN EM-72-034R4 NO DEFECTS NOTED AT THIS TIME NO ODOR SMOKE SMELL PRESENT IN COCKPIT AND CABIN. REMOVED AND REPLACED THE DUCT ASSEMBLY PART NUMBER: 145-21165-407 IAW EMB MM 21-60-01. REMOVED AND REPLACED CLAMPS, PART NUMBERS: TSS20S30, TSS36S30, AND SLEEVE, 2.5", PART NUMBER LA815113-8. THE NUMBER 2 RECIRCULATION FAN WAS INOPERABLE. DIFFERED NR 2 RECIRC FAN PER MEL #21-7 AUTH # 020873M-C MAINTENANCE ACTION PERFORMED. REMOVED AND REPLACED THE RICIRC FAN AND FUSE PART NUMBERS: 4611028900 & 100FU01-030. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,912 hrs · 17,209 cycles

DURING MAINTENANCE INSPECTION FOUND THE FOUND GALLEY EMERGENCY LIGHT OUT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE GALLEY EMERGENCY LIGHT IAW EMB STANDARD MTX PRACTICES. NO DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 19,868 hrs · 17,174 cycles

DURING MAINTENANCE INSPECTION FOUND FORWARD FAIRING LEFT EXTERNAL EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERIVCE. REMOVED AND REPLACED THE LEFT FORWARD EXTERIOR EMERGENCY LIGHT LAMP IAW 33-50-06-000-801-A AND 33-50-06-000-801-A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: MECHANISM — LACK OF LUBE (CABIN DOOR) · airframe 19,593 hrs · 16,991 cycles

ON FLIGHT 3390 THE CREW REPORTED THE MAIN CABIN DOOR WAS HARD TO OPEN AND CLOSE. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED INSPECTION AND LUBRICATED SIDE-HINGED MECHANISM IAW EMB 145 AMM 52-18-00. THE OPERATIONAL CHECK WAS GOOD. NO PARTS REMOVED OR REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BOLT — BROKEN (CABIN DOOR) · airframe 18,783 hrs · 16,376 cycles

FOR FLIGHT 3909 MAINTENANCE REPORTED THE CABIN ENTRY DOOR HANDLE WAS HARD TO MOVE. THE AICRAFT WAS REMOVED FROM SERVICE. DURING TROUBLESHOOTING FOUND UPPER THE FORWARD ROLLER BEARING BRACKET BOLT BROKEN OFF. REMOVED REMAINING PORTION OF BOLT AND INSTALLED NEW BOLT AND WASHER. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ANTENNA — FAILED (VHF COMM) · airframe 16,436 hrs · 14,632 cycles

ON FLIGHT 4285 DURING THE CLIMBOUT THE CAPTAIN REPORTED, WITNESSED A LIGHTNING STRIKE TO THE NOSE OF THE AIRCRAFT FOLLOWED SHORTLY AFTER WITH COMM 1 GOING INOPERABLE AND COMM 2 BEING INTERMITTENT. THE CAPTAIN DECLARED AN EMERGENCY AND RETURNED TO ORD. THE AIRCRAFT LANDED OVERWEIGHT, HOWEVER THE RATE OF DESCENT WAS BELOW 360 FEET PER MINUTE ON TOUCHDOWN. THE AIRCRAFT WAS REMOVED FROM SERVICE. SINCE LANDING WAS WITHIN CRITERA AS PER EMB-145 AMM 05-50-02; NO MAINTENANCE ACTION WAS NECESSARY IAW EMB-145 ETN : EM-05-009. REMOVED AND REPLACED NR 1 AND NR 2 VHF ANTENNA IAW EMB MM 23-12-04 AND SATISFACTORILY TESTED IAW EMB MM 23-12-00. LEFT AILERON HAS BURN MARK ON OUTBOARD TRAILING EDGE. TREATED AFFECTED AREA IAW EMB SRM 57-60-01. CLEANED AFFECTED AREA, APPLIED SPEED TAPE PER SRM 57-60-01. LEFT WING TIP HAS LIGHTNING BURN MARK ON TRAILING EDGE. REMOVED AND REPLACED THE LEFT WING TIP IAW EMB 145 AMM 57-30-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 16,030 hrs · 14,300 cycles

DURING MAINTENANCE BASE VISIT FOUND THE AISLE 12 EMERGENCY LIGHTS TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 3 EMERGENCY BATTERY AND BATTERY CHARGER IAW W/C 33-700-19. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: PUMP — DEFECTIVE (NR 2 ENGINE) · airframe 15,562 hrs · 13,928 cycles

ON FLIGHT 3919 DURING CRUISE THE CREW REPORTED, RECEIVED AN EICAS MESSAGE: HYDRAULIC 2 LOW QUANTITY FOLLOWED BY HYDRAULIC SYSTEM 2 FAIL MESSAGE. THE CREW DECLARED AN EMERGENCY AND DIVERTED TO STL. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NUMBER 2 ENGINE DRIVEN HYDRAULIC PUMP. THE OPERATIONAL CHECK WAS GOOD IAW EMB AMM 29-10-03. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: HOLDER — BROKEN (FLASHLIGHT) · airframe 15,240 hrs · 13,661 cycles

DURING THE PREFLIGHT INSPECTION FOR FLIGHT 3940 THE CREW FOUND THE AFT FLIGHT ATTENDANT FLASHLIGHT HOLDER BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AFT FLIGHT ATTENDANT FLASHLIGHT ASSEMBLY IAW EMB 145 AMM TASK 33-50-16-000801-A AND 33-50-16-400-801-A. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 146,194 hrs · 13,125 cycles

DURING MAINTENANCE BASE INSPECTION FOUND THE LEFT OMEGA BEAM CORRODED BETWEEN FRAME 24 AND 25. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED OMEGA BEAM AS REQUIRED IAW EMBRAER SRM 53-00-10, INSTALLATION OF FILLER REINFORCEMENT. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FITTING — WORN (AILERON) · airframe 14,619 hrs · 13,125 cycles

DURING MAINTENANCE BASE VISIT INSPECTION FOUND THE RIGHT AILERON POWER CONTROL ACTUATOR FITTING LUG HAS WORN HAT BUSHING BORES. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AILERON POWER CONTROL ACTUATOR FITTING WITH A NEW FITTING IAW EO EM-27MR-112. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 14,619 hrs · 13,125 cycles

DURING MAINTENANCE BASE VISIT THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. THE EXISTING REPAIR WAS FOUND TO BE CORRODED OUT OF LIMITS IAW SRM 53-21-10. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED DOUBLER AND INSTALLED NEW DOUBLER IAW EMB SRM 51-40-02, 53-00-10 AND CPM 51-21-06. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BRAKE — FAILED (NR 3)

ON FLIGHT 3402 CREW REPORTED NR 3 BRAKE CAME APART DURING LANDING. ACFT REMOVED FROM SERVICE. REPLACED NR 3 BRAKE AND WHEEL ASSY AND PERFORMED INSPECTION OF RT GEAR AXLE ASSY. NO DEFECTS NOTED, REPLACED NR 4 BRAKE FOR PRECAUTION AND INSPECTED NR 4 WHEEL ASSY. NO DEFECTS NOTED, BRAKE CHECKS GOOD. ACFT RETURNED TO SERVICE. (S)

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,666 hrs · 8,841 cycles

DURING MBV INSPECTION, FOUND GUSSET ON CENTER HAT BEAM BETWEEN FRAMES 20 TO 23 HAS SPOTS OF CORROSION. REPLACED GUSSET IAW SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,666 hrs · 8,841 cycles

DURING MBV INSPECTION FOUND, DOUBLER PLATE BETWEEN RIGHT HAT BEAM AND FLOORBEAM 21 IS CORRODED. REPLACED DOUBLER PLATE IAW SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE.

Part: WIRE — SHORTED (EMERGENCY LIGHTS) · airframe 8,363 hrs · 7,707 cycles

EMERGENCY LIGHT INOPERATIVE AT ROW 1A, 4A AND 7A. REPAIRED SHORT AND BLOWN FUSE AT FLOOD LIGHT IAW EMB AMM. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 8,211 hrs · 7,582 cycles

FORWARD EMERGENCY LIGHT STRIP INOPERATIVE. REMOVED AND REPLACED LIGHT STRIP IAW EMB AMM 33-50-12. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE.

Part: RIB — DENTED (ZONE 200) · airframe 8,008 hrs · 7,396 cycles

BIRD STRIKE INSPECTION REVEALED DENT AFT OF FRAME 10 BETWEEN STRINGER 2R AND CENTER LINE ABOVE WINDOW. REMOVED AND REPLACED RIB AT FRAME 10 ABOVE WINDOW IAW EMB SRM 51-40-02. RETURNED AIRCRAFT TO SERVICE.

Part: METERING UNIT — FAILED (NR 1 ENGINE)

CREW SHUTDOWN NR 1 ENGINE AFTER ENGINE BEGAN VIBRATING WITH NO INDICATION. ALSO ITT FLUX AND OIL PSI FLUX. AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED FPMU, CVG ACTUATOR, 14TH AND 9TH STAGE CSM TUBES AND O-RINGS AND THE FADEC 1A. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

THE LT OMEGA BEAM AT FRAME 20 WAS FOUND CORRODED. PERFORMED A CUT OUT TO REMOVE THE DAMAGE. REPARED A DOUBLER, FILLER REPAIR PLATE AND 2 SHIMS. REPAIR DONE IAW EMB SRM. (K)

Part: SILL — CORRODED (SERVICE DOOR)

THE SERVICE DOOR CENTER SILL WAS FOUND CORRODED AT THE CENTER AND AFT NUTPLATE HOLES. BLENDED THE AREAS TO REMOVE THE CORROSION. CLEANED AND APPLIED ALODINE, EPOXY PRIMER AND POLYURETHANE TOP COAT TO THE REORKED AREA. FABRICATED A REPAIR DOUBLER. REPAIR DONE IAW EMB SRM. (K)