N663AR

Part: SIGN — INOPERATIVE (ZONE 200) · airframe 44,669 hrs · 40,058 cycles

EMERGENCY LIGHT AT ROW 12 OVERHEAD IS INOP. FACT 07AUG25 10:39 PHL R/R FWD EXIT LOCATING SIGN ASSEMBLY IAW AMM 33-50-15. OPS CHECK GOOD. A/C OK FOR SERVICE AT THIS TIME

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,511 hrs · 39,864 cycles

F048898 CARGO DOOR CUT-OUT SHEAR CLIP AT FR 65 CORRODED ON PREVIOUS REPAIR. REMOVED PREVIOUS REPAIR ON CARGO DOOR CUTOUT SHEAR CLIP AT FR 65 AND ACCOMPLISHED SHEAR CLIP REPAIR IAW PIEDMONT EO1-53-25-0189 AND EMB 145 SRM 53-31-04 RE, ITEM 4,D,FIG 212.

Part: SKIN — SCRATCHED (ZONE 200) · airframe 44,511 hrs · 39,864 cycles

F045832 SCRATCH AT FR67 BETWEEN STGR 03L AND STGR 04L BEYOND ALLOWABLE LIMITS. REPAIRED SCRATCHED AREA AT FR67 BETWEEN STGR 03L AND STGR 04L IAW PIEDMONT EO1-53-25-0200 AND ETD2025-145-920956

Part: BRACKET — CRACKED (ZONE 200) · airframe 44,511 hrs · 39,864 cycles

F045768 LH LATERAL BRACKET IS CRACKED IN COCKPIT. REMOVED CRACKED LH LATERAL BRACKET IN COCKPIT AND INSTALLED L/H LATERAL BRACKET IN COCKPIT IAW EMB 145 SRM 51-40-02.

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 44,511 hrs · 39,864 cycles

F045762 SHEAR CLIP IS CRACKED AT FRAME 10 BELOW LH DV WINDOW. REMOVED AND REPLACED SHEAR CLIP AT FRAME 10 BELOW LH DV WINDOW IAW EMB145 SRM 51-40-02.

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 44,511 hrs · 39,864 cycles

F045761 SHEAR CLIP IS CRACKED AT FRAME 10 BELOW RH DV WINDOW. REMOVED AND REPLACED SHEAR CLIP ON FRAME 10 BELOW RH DV WINDOW IAW EMB 145 SRM 51-40-02.

Part: WINDOW FRAME — CRACKED (ZONE 200) · airframe 44,511 hrs · 39,864 cycles

F045760 FRAME 10 IS CRACKED BELOW RH DV WINDOW. REMOVED AND REPLACED FRAME 10 BELOW RH DV WINDOW IAW EMB 145 SRM 51-40-02.

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 44,511 hrs · 39,864 cycles

F045464 SHEAR CLIP IS CRACKED AT FRAME 27 BETWEEN STRINGERS 15R-16R. RAR SHEAR CLIP AT FR27 BETWEEN STGR 15R-16R IAW EMB 145 SRM 51-40-02.

Part: HOUSING — OUT OF LIMITS (ZONE 300) · airframe 44,511 hrs · 39,864 cycles

F045524 LH AND RH HORIZONTAL STABILIZER SPHERICAL BEARING HOUSINGS ARE OUT OF LIMITS. PERFORMED REPAIR ON LH AND RH VERTICAL STAB SPHYRICAL BEARING HOUSINGS IAW EMB 145 SRM 55-30-02 RE AND EO1-55-25-0174.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 44,511 hrs · 39,864 cycles

F045312 CABIN RH # 5 FLOOR BOARD SUPPORT CORRODED. RAR CABIN RH #5 FLOORBOARD SUPPORT IAW EMB 145 SRM 51-40-02.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 44,511 hrs · 39,864 cycles

F045470 CORROSION ON CENTER #2 FLOOR BEAM GUSSET. RAR CENTER #2 FLOOR BEAM GUSSET. IAW EMB 145 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 44,511 hrs · 39,864 cycles

F045507 RH CENTER FLOOR GUSSET BETWEEN FR 38 AND FR 46 CORRODED. REMOVED AND REPLACED R/H CENTER FLOOR GUSSET BETWEEN FR 38 AND 46 IAW EMB 145 SRM 51-40-02, 51-10-03, 53-23-10.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 44,511 hrs · 39,864 cycles

F045432 CORROSION ON LH OTBD #3 FLOOR SILL. RAR LH OTBD #3 FLOOR SILL IAW EMB 145 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 44,511 hrs · 39,864 cycles

F045505 LH #5 FLOOR BOARD SUPPORT CORRODED. RAR LH #5 FLOOR SILL IAW EMB 145 SRM 51-40-02.

Part: TUBE — CORRODED (ZONE 300) · corrosion level 2 · airframe 44,511 hrs · 39,864 cycles

F045514 RH ELEVATOR INBD AND OUTBD MASS BALANCE TUBES CORRODED. REPAIRED CORRODED RH ELEVATOR INBD AND OUTBD MASS BALANCE TUBES IAW PIEDMONT EO-1-05-25-0210, EMB IC2003-145/1934A, EMB IC-2003-145/4043 AND SB145-55-0040 REV 1.

Part: TUBE — CRACKED (ZONE 300) · corrosion level 2 · airframe 44,511 hrs · 39,864 cycles

F045513 LH ELEVATOR INBD AND OUTBD MASS BALANCE TUBES CORRODED. REPAIRED CORRODED LH ELEVATOR INBD AND OUTBD MASS BALANCE TUBES IAW PIEDMONT EO1-05-25-0210, EMB IC2003-145/1934A, EMB IC2003-145/4043 AND SB145-55-0040 REV 1.

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 44,511 hrs · 39,864 cycles

F045262 SHEAR CLIP IS CRACKED AT FRAME 15 BETWEEN STRINGERS 15R-16R. RAR SHEAR CLIP AT FR15 BETWEEN STGR 15R-16R IAW EMB 145 SRM 51-40-02.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 44,511 hrs · 69,864 cycles

F045453 CORROSION ON LH #3 FLOOR BEAM GUSSET. RAR LH#3 FLOOR BEAM GUSSET IAW EMB 145 SRM 51-40-02.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 44,511 hrs · 39,864 cycles

F045449 CORROSION ON LH #2 FLOOR BEAM GUSSET. REMOVED AND REPLACED #2 FLOOR BEAM GUSSET IAW EMB 145 SRM 51-40-02

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 44,511 hrs · 39,864 cycles

F045468 CORROSION ON CENTER #1 FLOOR BEAM GUSSET. RAR CENTER #1 FLOOR BEAM GUSSET IAW EMB 145 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 44,511 hrs · 39,864 cycles

F045431 CORROSION ON LH OTBD #2 FLOOR SILL. RAR LH OTBD #2 FLOOR SILL IAW EMB 145 SRM 51-40-02.

Part: FRAME — CRACKED (ZONE 200) · airframe 44,511 hrs · 39,864 cycles

F045269 SHEAR CLIP IS CRACKED AT FRAME 24 BETWEEN STRINGERS 15R-16R. RAR SHEAR CLIP AT FR24 STGR15R-16R IAW EMB 145 SRM 51-40-02

Part: FRAME — CRACKED (ZONE 100) · airframe 44,511 hrs · 39,864 cycles

F044991 CARGO FR 73 IS CRACKED BETWEEN STGR 16R / 17R. REMOVED AND REPLACED FR 73 LOWER SECTION (BTW STGR 14L-16R) IAW EMB 145 SRM 51-40-02.

Part: DOOR SILL — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,511 hrs · 39,864 cycles

F044997 CARGO DOOR CUT-OUT CENTER SILL CORRODED. REMOVED AND INSTALLED CARGO DOOR CUTOUT LOWER SILL IAW EMB145 SRM 51-40-02

Part: DOOR SILL — CORRODED (ZONE 200) · corrosion level 2 · airframe 44,511 hrs · 39,864 cycles

F045106 CORROSION ON SERVICE DOOR CENTER SILL. REPAIRED CORROSION ON SERVICE DOOR CENTER SILL IAW PIEDMONT EO1-53-25-0197 AND EMB 145 SRM 53-21-02 RE, ITEM 2, FIG 201.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 44,511 hrs · 39,864 cycles

F045087 CORROSION IN GALLEY AREA ON FWD DIGITAL. BLENDED CORROSION ON FWD DIGITAL IN GALLEY AREA IAW EMB 145 SRM 51-10-03. REMAINING THICKNESS AT BLENDED AREAS ON GALLEY AREA ON FWD DIGITAL FOUND TO BE WITHIN ALLOWABLE LIMITS IAW EMB145 SRM 53-21-10AD.

Part: RIB — CRACKED (ZONE 600) · airframe 44,511 hrs · 39,864 cycles

F044753 POSSIBLE RH WING RIB 21 IS CRACKED UNDER ACCESS PANEL 651CB. PERFORMED CUTOUT OF DAMAGED AREA IAW EMB 145 SRM 57-20-07 RE, ITEM 4. ACCOMPLISHED RH WING RIB 21 REPAIR IAW EMB 145 SRM 57-20-07RE, ITEM 4, FIG 203 AND EO1-57-25-0196.

Part: DOOR FRAME — CORRODED (ZONE 800) · corrosion level 2 · airframe 44,511 hrs · 39,864 cycles

F044323 CORROSION ON SERVICE DOOR LOWER FRAME AROUND NUTPLATE HOLES. BLENDED TO REMOVE CORROSION FROM SERVICE DOOR LOWER FRAME AROUND NUTPLATE HOLES IAW EMB 145 SRM 51-10-03. NO SIGNS OF PREVIOUS BLENDS. FOUND SERVICE DOOR LOWER FRAME AROUND NUTPLATE HOLES TO BE WITHIN ALLOWABLE LIMITS IAW EMB 145 SRM 52-43-06

Part: PROFILE — GOUGED (ZONE 800) · airframe 44,511 hrs · 39,864 cycles

F044127 SEVERAL GOUGES ON BAGGAGE DOOR EXTERNAL LOWER L PROFILE. REMOVED UNSERVICEABLE AND INSTALLED SERVICEABLE BAGGAGE DOOR EXTERNAL LOWER L PROFILE IAW EMB 145 SRM 51-40-02.

Part: DOOR — CORRODED (ZONE 800) · corrosion level 2 · airframe 44,511 hrs · 39,864 cycles

F044123 CORROSION ON BAGGAGE DOOR LOWER INTERNAL L PROFILE AND RIVETS. REMOVED UNSERVICEABLE AND INSTALLED SERVICEABLE BAGGAGE DOOR LOWER INTERNAL L PROFILE IAW EMB 145 SRM 51-40-02.

Part: WEB — GOUGED (ZONE 800) · airframe 44,511 hrs · 39,864 cycles

F044132 BAGGAGE DOOR WEBBING IS GOUGED 4 EACH. REMOVED UNSERVICEABLE AND INSTALLED SERVICEABLE BAGGAGE DOOR ENTERNAL LOWER WEB IAW EMB 145 SRM 51-40-02.

Part: SKIN — GOUGED (ZONE 200) · airframe 44,511 hrs · 39,864 cycles

F043987 REAR FUSELAGE EXTERNAL SKIN HAS POSSIBLE CRACK AT FR 77 BETWEEN STGR8L / 9L. REMOVED THE CRACKED SKIN AND INSTALLED BUSHING WITH A RIVET AT REAR FUSELAGE SKIN FR 77BETWEEN STGR 8L/9L IAW EMB 145 SRM 53-32-01 ITEM 9, FIG 213, SRM 53-32-01 ITEM 9, FIG 213 AND EO1-53-25-0199.

Part: SKIN — GOUGED (ZONE 100) · airframe 44,511 hrs · 39,864 cycles

F043864 FUSELAGE EXTERNAL SKIN DOUBLER BELOW GPU DOOR GOUGED. RE-ACCOMPLISHED FUSELAGE EXTERNAL SKIN DOUBLER BELOW GPU DOOR IAW EMB 145 SRM 53-12-01, ITEM 2, FIG 201 AND EO1-53-25-0173.

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,511 hrs · 39,864 cycles

F043518 LH MLG BAY FWD AT SPAR II LOWER SKIN CORRODED. REMOVED AND REPLACED LH MLG BAY LOWER FWD SKIN IAW EMB 145 SRM 51-40-02.

Part: SIGN — INOPERATIVE (AFT) · airframe 44,200 hrs · 39,560 cycles

DURING PS-1 CHECK FOUND AFT EMERGENCY OVERHEAD EXIT SIGN AFT SIDE INOP-C/A-RAR AFT EMERGENCY OVERHEAD EXIT SIGN ON THE AFT SIDE IAW AMM 33-50-15. OPS CHECK GOOD

Part: FLASHLIGHT ASSY — BROKEN (AFT) · airframe 44,176 hrs · 39,535 cycles

AFT EMERGENCY FLASHLIGHT NOT CHARGING-C/A-RAR AFT EMERGENCY FLASHLIGHT BRACKET ASSEMBLY IN REFERENCE WITH EMB AMM 33-50-16-000-801-A AND 33-50-16-400-801-A. OPC GOOD. END.

Part: LAMP — INOPERATIVE (SD) · airframe 44,162 hrs · 39,527 cycles

SERVICE DOOR EMERGENCY LIGHT INOP-C/A-RAR SERVICE DOOR EMERGENCY LIGHT LAMP IAW EMB AMM 33-50-09-000-801-A AND 33-50-09-400-801-A. OPC GOOD. END.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 43,850 hrs · 39,213 cycles

DURING PS-1 CHECK, FOUND MAIN DOOR OVERHEAD EMERGENCY LIGHT INOP-C/A-RAR MAIN-DOOR EMERGENCY-LIGHT LAMP IAW EMB-145 AMM 33-50-06

Part: GEAR — INOPERATIVE · airframe 43,346 hrs · 38,664 cycles

GEAR HANDLE STUCK SO GEAR HANDLE WOULD NOT RETRACT. EICAS MESSAGE LG AIR/GND FAIL ON ROTATION.. DECLARED EMERGENCY.-C/A-PERFORMED FCK CHK OF LH AND RH WOW PROX SWITCHES, NO ELECTRICAL DEFECTS NOTED

Part: INVERTER — INOPERATIVE (2 & 3) · airframe 43,190 hrs · 38,488 cycles

FOUND FLOOR EMERGENCY LIGHT SRIPS 2 AND 3 INOP DURING PS-1 CHECK-C/A-RAR EMERGENCY LIGHT DC/AC INVERTER #3 IAW EMB 145 MPP 33-50-11. OPS CHECK GOOD. NO DEFECTS NOTED.

Part: LIGHT — INOPERATIVE · airframe 43,097 hrs · 38,393 cycles

SERVICE DOOR EMERGENCY LIGHT INOP-C/A-RAR SERVICE DOOR EMERGENCY LIGHT LAMP IAW EMB AMM 33-50-09-000-801-A AND 33-50-09-400-801-A. OPC GOOD. END.

Part: NONE — NONE · airframe 43,045 hrs · 38,336 cycles

DURING PS-2 CHECK FOUND EXTERNAL EMERGENCY LIGHT ON THE RIGHT SIDE CENTER FAIRING TO BE INOP.-C/A-RAR RIGHT SIDE CENTER FAIRING EMERGENCY LIGHT LAMP IAW AMM 33-50-10.OPS CHECK GOOD. NO FURTHER DEFECTS NOTED,

Part: NONE — NONE · airframe 42,848 hrs · 38,117 cycles

ROW 16 FLOOR PROXIMITY STRIP LIGHT INOP-C/A-RAR ROW 16 FLOOR PROXIMITY STRIP LIGHT IAW EMB 145 AMM 33-50-12. OPC GOOD.

Part: NONE — BROKEN (FA) · airframe 42,791 hrs · 38,052 cycles

DURING PS-2 FOUND FA EMERGENCY FLASHLIGHT HOLDER BROKEN-C/A-REMOVED AND REPLACED FA EMERGENCY FLASHLIGHT HOLDER IAW EMB 145 AMM 33-50-16 OPS CHECK GOOD

Part: NONE — NONE · airframe 42,725 hrs · 37,983 cycles

OVERHEAD AISLE EMERGENCY LIGHT INOP-C/A-RAR OVERHEAD AISLE EMERGENCY LAMP IAW AMM 33-50-08-000-801-A AND 33-50-08-400-801-A. OPS CHECK GOOD. END.

Part: NONE — NONE · airframe 42,544 hrs · 37,785 cycles

LAV SMOKE EICAS MESSAGE IN FLIGHT. EXECUTED LAV SMOKE CHECKLIST, INDICATIONS NORMAL.-C/A-PERFORMED OPERATIONAL CHECK OF LAV SMOKE DETECTION SYS IN REF TO AMM 26-14-00. OPC GOOD.

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 42,427 hrs · 37,651 cycles

LAV SMOKE ALARM. INSPECTED LAVATORY, NO SMOKE OR FIRE DETECTED. LAVATORY SMOKE SYSTEM OPS CHECKS GOOD IAW AMM 26-14-00. NO DEFECTS NOTED.

Part: NONE — NONE · airframe 42,033 hrs · 37,226 cycles

AFT EMERGENCY FLASHLIGHT CRADLE BROKEN-C/A-RAR AFT EMERGENCY FLASHLIGHT CRADLE ASSEMBLY IAW EMB AMM 33-50-16-000-801-A AND 33-50-16-400-801-A. OPC GOOD. END.

Part: NONE — NONE · airframe 41,810 hrs · 36,948 cycles

CEILING EMERGENCY LIGHT AT PAX DOOR INOP-C/A-REMOVED AND REPLACED CEILING EMERGENCY LIGHT AT PAX DOOR IAW AMM 33-50-06. OPC GOOD

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 41,768 hrs · 36,891 cycles

SEAT 3 B/C EMERGENCY EXIT SIGN PLACARD INOP-C/A-RAR EMERGENCY LIGHT AC/DC INVERTER #3 IAW EMB AMM 33-50-11-000-801-A AND 33-50-11-400-801-A OPS CHECK GOOD

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 41,746 hrs · 36,863 cycles

GALLEY AREA EMERGENCY LIGHT INOP-C/A-RAR GALLEY AREA EMERGENCY LIGHT LAMP IAW EMB AMM 33-50-09-000-801-A AND 33-50-09-400-801-A. OPC GOOD.

Part: FLASHLIGHT — MISSING (AFT CABIN) · airframe 41,536 hrs · 36,635 cycles

FLIGHT ATTENDANT AFT EMERGENCY FLASHLIGHT MISSING-C/A-DEFERRED FLIGHT ATTENDANT AFT EMERGENCY FLASHLIGHT PER MEL 25-32. M PROCEDURES COMPLIED WITH. AUTH# 070503M-C EXPIRES 8-9-21

Part: SMOKE DETECTOR — ILLUMINATED (CARGO) · airframe 41,283 hrs · 36,355 cycles

BAGG SMOKE INDICATION IN FLIGHT AT FL210 QRH PROCEDURES COMPLIED WITH EMERGENCY DECLARED "TRANSFERRED TO NRWC 663-ORD-05135"-C/A-RAR CARGO FIRE EXT BOTTLES IAW AMM 26-23-01 PERFORMED OPS CHECK OF CARGO SMOKE DETECTION SYSTEM IAW AMM 26-15-00 NO FAULTS FOUND

Part: BRACE — CORRODED (LT MLG) · airframe 41,272 hrs · 36,343 cycles

LT FWD MLG SIDEBRACE BORE (IN GEAR WELL) HAS PITTING CORROSION (LEVEL 1 CORROSION) MAJOR REPAIR-C/A-REPLACED FITTING IAW ERS-EM-57MR-1310

Part: FRAME — CORRODED (FRM 22) · airframe 41,272 hrs · 36,343 cycles

SERVICE DOOR AFT LOWER SURROUND HAS CORROSION AROUND NUTPLATE HOLE FOR LOWER TRIM. (ON FRAME 22R, BETWEEN LOCATION STR 15R AND STR 16R) (LEVEL 1 CORROSION MAJOR REPAIR)-C/A-REPAIRED SERVICE DOOR AFT LOWER SURROUND FRAME 22, BETWEEN STRINGERS 15R AND 16R IAW SRM 53-00-04 ITEM #16.

Part: RECEPTACLE — CRACKED (HOLD OPEN) · airframe 41,272 hrs · 36,343 cycles

STIFFENER ON AFT SIDE OF FRAME 68 FOR CARGO DOOR HOLD OPEN RECEPTACLE HAS A 1/2" CRACK-C/A-INSTALLED NEW STIFFENER IAW SRM 51-40--02

Part: DRAG ANGLE — CRACKED (VERTICAL STAB) · airframe 41,272 hrs · 36,343 cycles

VERTICAL STAB TO FUSELAGE RT SIDE DRAG ANGLE IS CRACKED IN 2 AREAS. (MAJOR REPAIR)-C/A-C/W VERTICAL STAB TO FISELAGE DRAG ANGLE REPAIR IAW ERS-EM-53MR-4355

Part: SUPPORT — CRACKED (CRGO TOSION BAR) · airframe 41,272 hrs · 36,343 cycles

SUPPORT FOR CARGO DOOR TORSION BAR AT FR 68 HAS A 1/4" CRACK. ( DURING EVALUATION FOUND 3 CRACKS)-C/A-RAR SUPPORT ASSEMBLY FOR CARGO DOOR TORSION BAR AT FRAME 68 IAW SRM 51-40-02.

Part: LIGHT — DAMAGED (CABIN) · airframe 41,272 hrs · 36,343 cycles

LEFT EMERGENCY LIGHT FLOOR STRIP NRS1, 4, 8 IS DAMAGED. REMOVED DAMAGED LT NR 4 EMERGENCY LIGHT FLOOR STRIP AND INSTALLED LIGHT WITH NEW FLOOR STRIP IAW AMM 33-50-12-400-801.

Part: BATTERY PACK — INOPERATIVE (EXTERIOR LIGHT) · airframe 41,272 hrs · 36,343 cycles

EXTERIOR LEFT FORWARD EMERGENCY LIGHT INOP. REPLACED BATTERY ASSY AND CHARGER IAW AMM 33-50-04 OPS CHECK GOOD

Part: ANGLE — DAMAGED (AFT BAGGAGE DOOR) · airframe 40,927 hrs · 35,990 cycles

AFT BAGGAGE DOOR FORWARD (ANGLE-EXTRUSION) CONTINUOUS STOP IS DAMAGED ON LOWER END.-C/A-REPAIRED BAGGAGE DOOR FWD CONTINUOUS STOP ANGLE IAW SRM 52-30-02.

Part: CRADLE — BROKEN (FWD FLASHLIGHT) · airframe 40,682 hrs · 35,745 cycles

FWD EMERGENCY FLASHLIGHT HOLDER BROKEN. MEL 25-53 LGPG 4615832 AUTH NR 010063-C. C/A: REPLACED FA FWD EMERGENCY CABIN FLASHLIGHT ASSEMBLY, IAW EMB 145 AMM TASKS 33-50-16-000-801-A & 33-50-16-400-801-A. OPERATIONS CHECK GOOD. MEL RESTORED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 40,236 hrs · 35,341 cycles

EMERGENCY EXIT LIGHT FLOOR STRIP FROM SEAT 7 TO 11 AND BOTH LOWER EXIT IDENTIFIERS FOR THE OVERWING EXITS INOP.-C/A-REMOVED AND REPLACED EMERGENCY EXIT LIGHT POWER SUPPLY AND BATTERY AT POSITION NUMBER 3 IAW AMM 33-50-04. OPERATIONAL CHECK GOOD IAW AMM 33-50-00.

Part: BOTTLE — ODOR · airframe 40,048 hrs · 35,125 cycles

STRONG ELECTRICAL SMELL AFTER ENGINE START, FOLLOWED RIGHT AFTER TRUNING PACKS ON. ODOR DETERMINED TO BE COMING FROM START BOTTLE. CLEARED PACKS BY RUNNING FOR 20 MINUTES IAW AMM 21-51-00. ODOR NO LONGER PRESENT. AIRCRAFT OK FOR SERVICE.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 39,977 hrs · 35,049 cycles

ROW 3 EMERGENCY SIGN INOP-C/A-INSPECTED EMERGENCY EXIT PLACARD HARNESS, TIGHTENED BACKSHELL OF CONNECTOR PLUG IAW EMB AMM 25-22-04-400-801-A. OPC GOOD.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 39,891 hrs · 34,956 cycles

ICE COND A-ICE INOP MSG ON LDG WITH ENGINE AIR INLET BUTTON ILLUMINITED BURNING SMELL IN AIRCRAFT NO 2 ENGINE WAS THE ONLY ONE INDICATING OPEN-C/A-PERFORMED OPERATIONAL TEST OF ANTI-ICE SYST IAW EMB AMM30-00-00-700-802 OPS CHECK GOOD. C/W WORKSCOPE FOR ODOR EVENT ORIGINATED, PERFORMED ETN-EM-72-034 AND FIM TASKS 21-20-00-810-801-A AND 3321-00-810-801-A NO DEFECTS NOTED

Part: LIGHT — ODOR (CABIN) · airframe 39,822 hrs · 34,881 cycles

ELECTRICAL BURNING SMELL NOTED BY FA AND MULTIPLE PASSENGERS DURING CLIMBOUT. PERFORMED FIM 25-31-00, NO ODOR NOTED. INSPECTED ALL HARNESSES AND RELAYS IN AND AROUND COCKPIT, FA FWD SEAT AND ALL ENTRY WAY LIGHTS, EMERGENCY FLASHLIGHTS. NO ODOR NOTED, GROUND RAN ACFT APU AND ENGINES IAW 72-00-00. NO ODOR NOTED FROM ENGINES OR PACKS. REMOVED AND REPLACED THE LT SIDEWALL LIGHT ASSEMBLIES INCLUDING HARNESS OVER ROWS 2A & 3A IAW AMM 33-21-06. NO FURTHER DEFECTS NOTED.

Part: DOUBLER — DAMAGED (NLG WW) · airframe 39,317 hrs · 34,397 cycles

DAMAGE ON NOSE WHEEL WELL FOUND TO BE OUT OF LIMITS PER EMBREAER "TRANSFERRED TO NRWC 663-ABI-04309"-C/A-FOUND DOUBLER ON RH SIDE OF NLG WHEEL WELL DAMAGED. REMOVED AND REPLACED DOUBLER IAW EMB 145 SRM 51-40-02, 51-20-03

Part: ACM — FAILED (NR 1) · airframe 38,564 hrs · 33,730 cycles

PACK 1 MAKES WEIRD NOISE AND BURNING SMELL, THEN GOT PACK 1 OVERHEAT CAUTION. C/W FIM TASK 21-51-00-810-804-A. FOUND TO BE TRANSITORY CONDITION NO FAULTS NOTED. PACK 1 RESTORED TO ORIGINAL CONFIGURATION, INTERROGATED CMC AND FOUND NO CORRELATED CMC MSG. PERFORMED OPC IAW AMM 21-51-00-700-802-A FOUND ACM TO BE SEIZED THEN GOT PACK 1 OVHT MSG ON EICAS. OPS CHK GOOD MULTIPLE TIMES. REMOVED AND REPLACED #1 PACK ACM IAW EM-2100-049 AND EMB-145 M/M 21-51-03, OPS CHECK GOOD.

Part: CONNECTOR — UNSECURE (CABIN) · airframe 38,024 hrs · 33,244 cycles

CENTER AISLE EMERGENCY EXIT LIGHT INOP. C/A-RESECURED LOOSE CONNECTION TO INVERTER IAW AMM 33-50-11 OPS CHECK GOOD.

Part: OUTFLOW VALVE — FAILED (CABIN PRESSURE) · airframe 37,455 hrs · 32,773 cycles

SUPPLEMENTAL AIRCRAFT WILL NOT PRESSURIZE IN AUTO OR MANUAL. C/A-AUTO AND MANUAL PRESSURIZATION DEFERRED PER MEL 21-19 AUTH#050084DM-C MEL PROCEDURES 21-19 C/W. REMOVED AND REPLACED ELECTROPNEUMATIC OUTFLOW VALVE IAW AMM 21-31-03. AUTO TEST FAILED BUT AFTER VERIFYING THAT ALL LINES WERE TIGHT ON BOTH OUT FLOW VALVES AND RESETTING POWER PERFORMED FUNCTIONAL TEST OF AUTO PRESSURIZATION IAW AMM 21-31-00-700-802-A, OPC GOOD. PERFORMED PRESSURIZEATION ON MANUAL MODE IAW AMM 21-31-00, OPS CHECK GOOD, (M) COMPLY WITH 21-19 SECTION 4, REMOVED LOCK OUT TOOL. AFTER REACTIVATING THE PNEUMATIC OUTFLOW VALVE AND CHANGING ELCTROPNEUMATIC OUTFLOW VALVE IAW AMM 21-31-03, THE PRESSURIZATION SYSTEM FUNCTIONAL CHECK GOOD IAW AMM 21-31-00-700-802-A AND MANUAL PRESSURIZATION OPC GOOD IAW AMM 21-31-00-700-801-A. THIS RESTORES MEL 21-19.

Part: PITOT SYSTEM — CONTAMINATED (NR 1 & 2) · airframe 37,454 hrs · 32,772 cycles

SPS ADVANCED CAUTION MESSAGE AT CRUISE FL 360 CA PFD SPEED & STANDBY SPEED AGREED, BUT FO PFD SPEED READ SIGNIFICANTLY LESS MESSAGE CLEARED AROUND FL250. C/A-DRAINED WATER FROM PITOT SYS 1-2 DRAINS IAW AMM 34-13-00 AND PERFORMED PITOT-STATIC LEAK CHECK AND OPC. PERFORMED ADC OPC IAW AMM 34-15-00 WITH NO FAULTS.

Part: FITTING — MIGRATED (LH AILERON) · airframe 37,338 hrs · 32,653 cycles

L/H AILERON DAMPNER FITTING BUSHING IS MIGRATING. -C/A-REMOVED AND REPLACED LH AILERON PER AMM 27-10-00.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 37,338 hrs · 32,653 cycles

SERVICE DOOR SILL IS CORRODED. C/A-COMPLETED INSTALLATION OF SERVICE DOOR SILL IAW SRM 51-40-02.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 37,338 hrs · 32,653 cycles

RT. O/B OMEGA BEAM SUPPORT BRACKET HAS A 1/4" CRACK BETWEEN FRAMES 48-49. -C/A-REMOVED AND REPLACED RT OUTBD OMEGA BEAM SUPPORT BRACKET IAW SRM 51-40-02.

Part: LIGHT — DAMAGED (CABIN) · airframe 37,338 hrs · 32,653 cycles

LT #2 EMERGENCY LIGHT STRIP HAS DAMAGED EXTRUSION. C/A-COMPLETE:COMPLETED INSTALLED THE #2 LT EMERGENCY LIGHT STRIP EXTRUSION. IAW AMM 33-50-12.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 37,338 hrs · 32,653 cycles

LT FLOOR EMERGENCY LIGHTS STRIP IN THE #6 AND #8 POSITIONS ARE BROKEN. C/A-COMPLETE:COMPLETED RAR THE LT EMERGENCY LIGHT STRIPS IN THE #6 AND #8 POSISTIONS. IAW AMM 33-50-12.

Part: STRUCTURE — DAMAGED (CABIN) · airframe 37,338 hrs · 32,653 cycles

RT #7 EMERGENCY LIGHT EXTRUSION IS DAMAGED AND REQUIRES REPLACEMENT. C/A-COMPLETE:COMPLETED INSTALLED THE #7 RT EMERGENCY LIGHT STRIP EXTRUSION. IAW AMM 33-50-12.

Part: LIGHT — DAMAGED (CABIN) · airframe 37,338 hrs · 32,653 cycles

LT EMERGENCY LIGHT STRIP #1 EXTRUSION DAMAGED. C/A-COMPLETE:COMPLETED INSTALLED THE #1 LT EMERGENCY LIGHT STRIP EXTRUSION. IAW AMM 33-50-12.

Part: LIGHT — DAMAGED (CABIN) · airframe 37,338 hrs · 32,653 cycles

LT #5 EMERGENCY LIGHT STRIP HAS DAMAGED EXTRUSION. C/A-COMPLETE:COMPLETED INSTALLED THE #5 LT EMERGENCY LIGHT STRIP EXTRUSION. IAW AMM 33-50-12.

Part: WIRE — BROKEN (FLASHLIGHT) · airframe 37,338 hrs · 32,653 cycles

COCKPIT RT EMERGENCY FLASHLIGHT ASSEMBLY WIRES SP3554 AND SP3553 BROKE AT QUICK DISCONNECT. C/A-COMPLETE:REPLACED COCKPIT RT EMERGENCY FLASHLIGHT ASSEMBLY (F/O'S) CONNECTOR (QUICK DISCONNECT) J1871 AND SPLICES SP3553 AND SP3554 IAW SWPM 20-21-00, REFERENCE NRTC E703939 FOR OPS CHECK.

Part: WIRE — BROKEN (CABIN) · airframe 37,338 hrs · 32,653 cycles

ELECTRICAL CONNECTOR PLUG FOR RT EXTERNAL EMERGENCY LIGHT ON FWD BELLY FAIRING HAS BROKEN WIRES. C/A-COMPLETE:REPAIRED ELECTRICAL CONNECTOR PLUG FOR RT EXTERNAL EMERGENCY LIGHT ON FWD BELLY FAIRING IAW SWPM 20-21-00.

Part: LIGHT — DAMAGED (CABIN) · airframe 37,338 hrs · 32,653 cycles

RT #5 EMERGENCY LIGHT EXTRUSION IS DAMAGED AND REQUIRES REPLACEMENT. C/A-COMPLETE:COMPLETED INSTALLED THE #5 RT EMERGENCY LIGHT STRIP EXTRUSION. IAW AMM 33-50-12.

Part: LIGHT — DAMAGED (CABIN) · airframe 37,338 hrs · 32,653 cycles

RT #6 EMERGENCY LIGHT EXTRUSION IS DAMAGED AND REQUIRES REPLACEMENT. C/A-COMPLETE:COMPLETED INSTALLED THE #6 RT EMERGENCY LIGHT STRIP EXTRUSION. IAW AMM 33-50-12.

Part: STRUCTURE — CRACKED (CABIN) · airframe 37,338 hrs · 32,653 cycles

RT #4 AND RT #7 FLOOR EXTRUSIONS ARE CRACKED AND NEED TO BE REPLACED. C/A-COMPLETE:COMPLETED RAR THE #4 RT AND RT #7 EMERGENCY LIGHT STRIP EXTRUSION. IAW AMM 33-50-12.

Part: LIGHT — DAMAGED (CABIN) · airframe 37,338 hrs · 32,653 cycles

RT #8 EMERGENCY LIGHT EXTRUSION IS DAMAGED AND REQUIRES REPLACEMENT. C/A-COMPLETE:COMPLETED INSTALLED THE #8 RT EMERGENCY LIGHT STRIP EXTRUSION. IAW AMM 33-50-12.

Part: SPLICE — DAMAGED (EMERGENCY LIGHT) · airframe 37,338 hrs · 32,653 cycles

LT #1 EMERGENCY LIGHT STRIP HAS DAMAGED SPLICE. C/A-COMPLETE:INSTALLED NEW LIGHT STRIP SPLICE IAW SWPM 20-50-01, REF BOW 316741 TASK #1 FOR OPTS CHECK.

Part: LIGHT — DAMAGED (CABIN) · airframe 37,338 hrs · 32,653 cycles

LT #7 EMERGENCY LIGHT STRIP HAS DAMAGED EXTRUSION. C/A-COMPLETE:COMPLETED INSTALLED THE #7 LT EMERGENCY LIGHT STRIP EXTRUSION. IAW AMM 33-50-12.

Part: FLAP — DAMAGED (RT WING) · airframe 37,338 hrs · 32,653 cycles

RIGHT #5 FFS HAS CORROSION ON ONE END AND DAMAGE TO THE OTHER END. C/A-COMPLETE:COMPLETED INSTALLATION OF RH #5 FFS IAW AMM 27-51-08.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 37,338 hrs · 32,653 cycles

LT OMEGA BEAM IS CORRODED BETWEEN FRS 58 AND 59. C/A-COMPLETE:REPAIRED LT OMEGA BEAM BETWEEN FR.58-59 IAW SRM 53-24-10. C/W D.T CHECKLIST 15-27.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 37,338 hrs · 32,653 cycles

RT OMEGA BEAM IS CORRODED BETWEEN FRS 58 AND 59. C/A-COMPLETE:REPAIRED RT OMEGA BEAM BETWEEN FR.58-59 IAW SRM 53-24-10. C/W D.T CHECKLIST 15-27.

Part: VALVE — LEAKING (GRND CONNECTION) · airframe 37,176 hrs · 32,476 cycles

CLIMBING THROUGH 19500 CABIN ALT AMBER AT 8000AND CLIMBING. STOPPED CLIMB AND BEGAN DESCENT CABIN ALT REACHED 10500 AND FOLLOWED DEPRESS CHECKLIST/EMERGENCY DESCENT QRH-C/A-DEFERRED AUTO AND MANUAL PRESSURIZATION M PROCEDURES CW MEL 2119 AUTH 020084DM-C. REMOVED AND REPLACED GROUND CONNECTION VALVE IAW E145 AMM 21-22-04. LEAK CHECK GOOD IAW E145 AMM 21-31- 00.

Part: PITOT LINE — CONTAMINATED (PITOT/STATIC SYS) · airframe 36,955 hrs · 32,261 cycles

RECEIVED "IAS" COMPARED MSG ON AIRSPEED TAPES. AIRSPEED NR 1 MATCHED STANDBY AIRSPEED. AIRSPEED NR 2 FO SIDE WAS 8 KNOTS LOW REFERENCE ITEM 1 OF THIS AML. WATER FOUND IN BOTH PITOT 1 AND 2 DRAIN LINES. DRAINED WATER FROM PITOT SYSTEM IAW AMM 34-13-00 PERFORMED ADC SYS OPC IAW AMM 34-15-00 AND PITOT SYSTEM OPC AND LEAK CHECK WITH NO FAULTS NOTED. PERFORMED OPS CHECK OF STALL PROTECTION SYSTEM IAW 27-36-00 OPS CHECK NORMAL. NO DEFECTS NOTED AT THIS TIME. NO RELATED CMC MESSAGES FOUND.

Part: SMOKE DETECTOR — FAILED (CARGO BAY) · airframe 36,848 hrs · 32,190 cycles

BAGGAGE COMPARTMENT SMOKE EICAS MESSAGE DOES NOT POST DURING FIRE TEST. CARGO FIRE PUSHBUTTON WILL NOT ILLUMINATE DURING FIRE TEST. INSPECTED SMOKE DETECTORS AND PERFORMED OPS CHECK OF SYSTEM IAW AMM 26-15-00 TEST FAILED MEL 26-03 REMAINS OPEN A/C OK FOR SERVICE. REPLACED FWD BAGGAGE SMOKE DETECTOR AS PER AMM 26-15-01. SYSTEM WORKING NORMAL.

Part: BATTERY PACK — CRACKED (CABIN) · airframe 36,811 hrs · 32,158 cycles

BATTERY POWER SUPPLY NR 2 BATTERY PACK FOUND CRACKED. REMOVED AND REPLACED NR 2 BATTERY POWER SUPPLY AND CHASSIS ASSEMBLY IAW AMM 33-50-04, EMERGENCY LIGHTING SYSTEM OPERATIONAL CHECK SATISFACTORY IAW AMM 33-50-00. EMERGENCY LIGHTING BATTERY P/N 2013-1A S/N 103127

Part: CHARGER — FAILED (EMERGENCY LIGHTS) · airframe 36,811 hrs · 32,158 cycles

ON APPROACH THERE WAS A STRONG SMELL OF SMOKE IN THE CABIN AND COCKPIT. WE DECLARED AN EMERGENCY. AND LANDED IN MIA. THERE WAS NOT VISIBLE SMOKE.-C/A-REMOVED AND REPLACED #2 BATTERY POWER SUPPLY AND CHASSIS ASSEMBLY IAW AMM 33-50-04, EMERGENCY LIGHTING SYSTEM OPERATIONAL CHECK SATISFACTORY IAW AMM 33-50-00. REMOVED AND REPLACED BULBS FROM ROW 9BC, 12A, AND GALLEY CEILING R/H SIDE IAW AMM 33-21-06 OPS CHECK GOOD. INSTALLED SEAT ASS 8BC, 9BC, AND 10BC IAW-AMM-25-21-01. INSTALLED FLOOR ACCESS PANELS 251BF, 252AF, 251HF, AND 252BF IAW-AMM-53-01-02. COMPLIEDWITH FUEL QUANITITY INDICATION HARNESS INSPECTION IAW EMB 145 AMM 28-41-00. INSPECTED RECIRCULLATION FANS (LH AND RH) FOUND BOTH WORKING IN NORMAL CONDITION IAW-AMM-21-20-00. C/A GASPER FAN DETAILED VISUAL INSPECTION AND FOUND WORKING NORMAL IAW-AMM-21-20-00. INSTALLED HEADLINER BY SERVICE DOOR IAW AMM-25-22-04. REMOVED AND REPLACED #2 BATTERY POWER SUPPLE AND CHASSIS ASSEMBLY IAW AMM 33-50-04, EMERGENCY LIGHTING SYSTEM OPERATIONA CHECK SATISFACTORY IAW AMM 33-50-00. INSTALLED ACCESS PANELS 223UZ AND 224NZ IAW AMM 06-41-03. C/W WINDSHEILD CONTACTOR DETAILED VISUAL INSPECTION AND FOUND IN NORMAL CONDITION IAW -AMM-30-42-02. FCF PASSED. EMERGENCY LIGHTING BATTERY P/N 2013-1A S/N 103127

Part: SMOKE DETECTOR — FALSE ACTIVATION (AFT CARGO) · airframe 36,798 hrs · 32,150 cycles

BAGG SMOKE INDICATION IN COCKPIT TIML367788-C/A-REMOVED AND REPLACED #1 AND #2 BAGG SMOKE DETECTOR IAW AMM 26-15-01 OPS CHK GOOD. CARGO AREA SMOKE DETECTOR P/N 473597-13 S/N 2737 FWD

Part: INVERTER — INOPERATIVE (CABIN) · airframe 36,522 hrs · 31,907 cycles

EMERGENCY EXIT LIGHT ABOVE SERVICE DOOR INOP. C/A-REMOVED AND REPLACED NR 2 EMERGENCY LIGHT INVERTER OPS CHECK GOOD IAW AMM 33-50-11.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,490 hrs · 31,866 cycles

SERVICE DOOR CEILING EMERGENCY LT INOP. -C/A-R&R SERVICE DOOR CEILING EMERGENCY LT LAMP IAW AMM 33-50-09-000-801-A AND 33-50-09-400-801-A. OPS CHECK GOOD.

Part: A/C PACK — ODOR (LEFT) · airframe 34,829 hrs · 30,270 cycles

SMOKE IN THE COCKPIT DURING TAXI OUT. PERFORMED ETN-EM-72-034, FOUND SMOKE AND ODOR COMING FROM THE LT PACK.

Part: ANTI-ICE VALVE — MALFUNCTIONED (ENGINE) · airframe 34,445 hrs · 29,928 cycles

DVT GSO ACCT MECH. EMERGENCY. DECLARED EMERGENCY.CHG EQ. FLT CONTINUED E2 A/ICE FAIL ON EICAS DURING CLIMB AFTER EXITING ICING CONDITIONS. QRH PROCEDURES COMPLIED WITH MESSAGE DISAPPEARED BUT VALVE OPEN INSCRIPTION STILL NOT ILLUMINATED. ENG 1 AIR INLET VALVE OPEN INSCRIPTION ILLUMINATED IN NON-ICING WITH OVERRIDE KNOB IN AUTO. PERFORMED OPS TEST OF ENG 1 ANTI/ICE VALVE IAW AMM 30-00-00. OPS TEST NORMAL. NO FAULTS NOTED. A/C OK FOR SERVICE. R/R #2 ANTI ICE VALVE IAW EMB 145 AMM 30-21-01. OPS CHECK REQUIRED. MEL REMAINS OPEN. PREFORMED OPS CHECK IAW AMM EMB 145 30-00-00. OPS CHECK GOOD.

Part: SENSOR — FAULTY (MLG BRAKE) · airframe 34,288 hrs · 29,789 cycles

INFLIGHT RIGHT OB BRAKE OVERHEAT. INDICATION WAS TOP OF SCALE THEN BOUNCED BETWEEN TOP OF SCALE TO MATCHING OTHER BRAKE TEMPS. INSPECTED ALL 4 BRAKE ASSEMBLIES UPON AIRCRAFT ARRIVAL AND FOUND NO HOT BRAKES. ISSUE IS INDICATION ONLY. M PROCEDURES C/W. CB E16 COLLARED AS PER MEL. REMOVED AND REPLACED NR 4 BRAKE TEMP SENSOR IAW AMM 32-47-01. OPS CHECK GOOD MEL ITEM RESTORED.

Part: SKIN — DENTED (FUSELAGE) · airframe 33,748 hrs · 29,212 cycles

DENT FOUND BY GROUND PERSONNEL, 3' FORWARD OF SERVICE DOOR 7' OFF GROUND. MAJOR REPAIR, REPAIRED DAMAGED AREA BETWEEN FR16R AND 17R BELOW STR 11R IAW SRM 53-21-01 AND SRM 51-40-02 AND APPLIED PROTECTIVE FINISH IAW CPM 51-21-06, ETN EM-075 AND ETN GN-017.

Part: UNKNOWN — MALFUNCTIONED (AC BAY) · airframe 32,779 hrs · 28,404 cycles

PACK 1 OVERLOAD. FLIGHT CREW PLACARDED PACK 1 SYSTEM REF 21-30. PERFORMED OPC OF DISTRIBUTION SYSTEM IAW AMM 21-20-00. OPC GOOD. PERFORMED OPC OF TEMPERATURE CONTROL IAW AMM 21-60-00. OPC GOOD. NO HARD FAULTS FOR PACK 1 OVLD FOUND AT THIS TIME.

Part: FLASHLIGHT — DAMAGED · airframe 31,536 hrs · 27,223 cycles

AFT EMERGENCY FLASHLIGHT BASE DAMAGED. R & R AFT EMERGENCY FLASHLIGHT BASE IAW AMM 33-50-16, ETN-EM-33-034. OPC GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 31,373 hrs · 27,087 cycles

AFT HALF OF EMERGENCY LIGHT STAY ON IN ARM POSITION. R & R NR 4 EMERGENCY LIGHT BATTERY PACK AMM 33-50-04. OPS CK GOOD.

Part: CHARGER — FAILED (CABIN) · airframe 31,373 hrs · 27,087 cycles

IN REF. ITEM NR 1 ON THIS LOG PAGE R&R BATTERY CHARGER. R&R NR 4 BATTERY CHARGER IAW AMM 33-50-04.

Part: COMPUTER — MALFUNCTIONED (COCKPIT) · airframe 31,193 hrs · 26,923 cycles

CAPTAINS PFD, CAPTAINS MFD & EICAS WENT BLANK IN FLIGHT FOR 10 MINS. THEN PRD, MFD & EICAS WITH RED X. THEN PFD, MFD & EICAS BACK TO NORMAL AFTER 15 MINS. DECLARED EMER INBD DUE LOSS OF 3 PFDS? CLEARED ON LANDING. R & R IC 600 NR 1 IAW AMM 31-42-01. OPERATIONS CHECKED GOOD. REF ITEM 2 & 3 THIS AML FOR CAT II & RVSM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 30,420 hrs · 26,234 cycles

LEFT EMER LIGHT OVER THE WING INOPERATIVE. R & R EXTERNAL EMER LIGHT, LT FWD OF WING IAW AMM 33-50-10. OPERATIONS CHECKED GOOD.

Part: HOLDER — CRACKED (FLASHLIGHT) · airframe 30,362 hrs · 26,186 cycles

PILOTS FLASHLIGHT BASE CRACKED. R & R PILOTS FLASHLIGHT ASSEMBLY IAW AMM 33-50-16. OPERATIONS CHECKED GOOD.

Part: FLASHLIGHT — ODOR (COCKPIT) · airframe 28,323 hrs · 24,289 cycles

DURING DESCENT PRONOUNCED ELEC BURNING SMELL IN COCKPIT & FWD CABIN, NO VISIBLE FUMES OR SMOKE, LASTED THROUGHOUT LANDING. COMPLIED WITH ETN-EM-72-034 UNDER CONFIGURATION OF ITEM 5. IAW 53-10-02 INSPECTED PACK 2 AIR CONDITION DUCTS, RECIRC FANS & GASPER FAN. NO ODOR OR DAMAGED NOTED. ACFT OK FOR SERVICE. REF ITEM 1 PREVIOUS LOG PAGE 3743327 ITEM 1 MOC REQUESTING FURTHER INSPECTION OF COCKPIT ELEC SYS. VISUALLY INSPECTED COCKPIT ELEC EQUIPMENT & SURROUNDINGS. NO SIGNS OF HEAT DAMAGE, SMELL OF SMOKE FOUND. FOUND SMELL OF ELEC SMOKE ON FIRST OFFICER`S OFFICERS FLASHLIGHT. R & R FIRST OFFICER`S FLASHLIGHT IAW EMB AMM 33-50-16-14.

Part: CONTROL UNIT — MALFUNCTIONED (FEEDBACK) · airframe 28,257 hrs · 24,224 cycles

ON TAKEOFF ROLL, AN UNCOMMANDED STEERING EVENT OF OSCILLATION AT HIGH SPEED. LANDING WAS NORMAL, BUT HEARD A MOMENTARY HIGH PITCH NOISE WHEN TILLER WAS ENGAGED. R & R FEEDBACK UNIT IAW AMM 32-50-07. OPS CHECKED GOOD.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 27,710 hrs · 23,719 cycles

EMERGENCY FLOOR PROXIMITY LIGHT STRIPS INOPERATIVE FROM SEAT LOCATION 13A TO LAVATORY. R & R EMER LIGHT INVERTER NR 6 IAW AMM 33-50-11.

Part: SKIN — CRACKED (FUSELAGE) · airframe 27,709 hrs · 23,718 cycles

FRAME 75 ABOVE STRINGER 2R AREA SKIN CRACKED. PERFORMED PERMANENT REPAIR OF RT UPPER SKIN JUST AFT OF FRAME 75 ABOVE STRINGER 2R IAW ERS-EM-53MR-795.

Part: SKIN — CRACKED (FUSELAGE) · airframe 27,709 hrs · 23,718 cycles

FRAME 75 ABOVE STRINGER 2L AREA SKIN CRACKED. PERFORMED PERMANENT REPAIR OF LT UPPER FUSELAGE SKIN JUST AFT OF FRAME 75 ABOVE STRINGER 2L IAW ERS-EM-53MR-795.

Part: FRAME — CHAFED (APU BAY) · airframe 27,709 hrs · 23,718 cycles

APU COWLING FWD FRAME HAS TWO CHAFES BELOW THE LT SIDE GUIDE PIN HOLE. PERFORMED PERMANENT REPAIR IAW ERS-EM-53MR-783.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 27,709 hrs · 23,718 cycles

LEFT UPPER SEAT TRACK SUPPORT CORROSION. PERFORMED PERMANENT REPAIR OF LT UPPER SEAT TRACK SUPPORT IAW ERS-EM-53MR-779.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 27,709 hrs · 23,718 cycles

RIGHT UPPER SEAT TRACK SUPPORT CORROSION. PERFORMED PERMANENT REPAIR OF RT UPPER SEAT TRACK SUPPORT IAW ERS-EM-53MR-779.

Part: FITTING — CORRODED (FUSELAGE) · airframe 27,709 hrs · 23,718 cycles

FRAME 65 CORROSION ON LOWER PORTION ABOVE CARGO DOOR SILL. REPAIRED FRAME 65 SHEAR CLIP IAW EO EM-53MR-1129 PART A FOUND DURING INSPECTION IAW WC 53-200-69.

Part: WIRE — DAMAGED (CABIN) · airframe 27,709 hrs · 23,718 cycles

LEFT EMER LIGHT STRIP NR 3 LIGHT STRIP HAS DAMAGED WIRES. R & R EMER LIGHT STRIP NR 3 IAW AMM 33-50-12.

Part: WIRE — BROKEN (CABIN) · airframe 27,709 hrs · 23,718 cycles

NUMBER 2 EMER PROXIMITY LIGHT STRIP HAS BROKEN WIRES. R & R FWD EMER LIGHT STRIP IAW AMM 33-50-12.

Part: WIRE — BROKEN (CABIN) · airframe 27,709 hrs · 23,718 cycles

NUMBER 6 EMER LIGHT STRIP HAS BROKEN WIRE. R & R EMER LIGHT STRIP NR 6 IAW AMM 33-50-12.

Part: WIRE — BROKEN (CABIN) · airframe 27,709 hrs · 23,718 cycles

NUMBER 1 EMER LIGHT STRIP HAS BROKEN WIRE. REPAIRED IAW SWPM 20-50-01 & SWPM 20-21-00.

Part: SKIN — CRACKED (FUSELAGE) · airframe 27,709 hrs · 23,718 cycles

LEFT FUSELAGE EXTERNAL SKIN IS CRACKED AROUND 3 FASTENERS AT FRAME 78 BELOW VERTICAL STAB. REPAIRED LT FUSELAGE EXTERNAL SKIN AROUND 3 FASTENERS AT FRAME 78 BELOW VERTICAL STAB IAW ERS-EM-5300-781.

Part: SKIN — CRACKED (FUSELAGE) · airframe 27,709 hrs · 23,718 cycles

RIGHT FUSELAGE EXTERNAL SKIN IS CRACKED AROUND 2 FASTENERS AT FRAME 79 BELOW VERTICAL STAB. REPAIRED RT FUSELAGE EXTERNAL SKIN AROUND 2 FASTENERS AT FRAME 79 BELOW VERTICAL STAB IAW ERS-EM-5300-781. SEE FOLLOW ON FOR DETAILS.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 27,709 hrs · 23,718 cycles

FRAME 68 AT AFT SIDE OF CGO DOOR FUSELAGE CUT OUT HAS CORROSION. REPAIRED FRAME 68 AT AFT SIDE OF CGO DOOR FUSELAGE CUT OUT IAW ERS-EM-53DF-793.

Part: SKIN — CRACKED (FUSELAGE) · airframe 27,709 hrs · 23,718 cycles

RIGHT FUSELAGE EXTERNAL SKIN IS CRACKED AROUND 1 FASTENER AT FRAME 78 BELOW VERTICAL STAB. REPAIRED RT FUSELAGE EXTERNAL SKIN AROUND 1 FASTENER AT FRAME 78 BELOW VERTICAL STAB IAW ERS-EM-5300-781. SEE FOLLOW ON FOR DETAILS.

Part: DOOR FRAME — CRACKED · airframe 27,709 hrs · 23,718 cycles

123BL INNER FWD FRAME CRACKED AT EYELET. ACCOMPLISHED REPAIR OF 123BL INNER FWD FRAME CRACK IAW ERS-EM-5200-220. SEE TURNOVER FOR DETAILS.

Part: SKIN — CRACKED (FUSELAGE) · airframe 27,709 hrs · 23,718 cycles

RIGHT FUSELAGE EXTERNAL SKIN IS CRACKED AROUND 3 FASTENERS AT FRAME 77 BELOW VERTICAL STAB. REPAIRED RT FUSELAGE EXTERNAL SKIN AROUND 3 FASTENERS AT FRAME 77 BELOW VERTICAL STAB IAW ERS-EM-5300-781. SEE FOLLOW ON FOR DETAILS.

Part: SKIN — CRACKED (FUSELAGE) · airframe 27,709 hrs · 23,718 cycles

RIGHT FUSELAGE EXTERNAL SKIN IS CRACKED AROUND 1 FASTENER AT FRAME 80 BELOW VERTICAL STAB. REPAIRED RT FUSELAGE SKIN AROUND 1 FASTENER AT FRAME 80 BELOW VERTICAL STAB IAW ERS-EM-5300-781. SEE FOLLOW ON FOR DETAILS.

Part: SKIN — CRACKED (FUSELAGE) · airframe 27,709 hrs · 23,718 cycles

LEFT FUSELAGE EXTERNAL SKIN IS CRACKED AROUND 3 FASTENERS AT FRAME 79 BELOW VERTICAL STAB. REPAIRED LT FUSELAGE EXTERNAL SKIN AROUND 3 FASTENERS AT FRAME 79 BELOW VERTICAL STAB IAW ERS-EM-5300-781. SEE FOLLOW ON FOR DETAILS.

Part: LIGHT — LOOSE (OVERWING EXIT) · airframe 27,709 hrs · 23,718 cycles

LEFT OVERWING FWD EMER LIGHT INOPERATIVE. SECURED LOOSE LT OVERWING FWD EMER LIGHT BULB IAW AMM 33-50-10 FOLLOWING STEPS 2L 1 - 4 & 3K 1 - 4. OPERATIONALLY CHECKED GOOD IAW AMM 33-50-00.

Part: SKIN — CRACKED (FUSELAGE) · airframe 27,709 hrs · 23,718 cycles

LEFT FUSELAGE EXTERNAL SKIN IS CRACKED AROUND 3 FASTENERS AT FRAME 77 BELOW VERTICAL STAB. REPAIRED LT FUSELAGE EXTERNAL SKIN AROUND 3 FASTENERS AT FRAME 77 BELOW VERTICAL STAB IAW ERS-EM-5300-781. SEE FOLLOW ON FOR DETAILS.

Part: LIGHT — LOOSE (CABIN) · airframe 27,709 hrs · 23,718 cycles

SERVICE DOOR LOWER EMER LIGHT INTERMITTENT. SECURED LOOSE LAMP ON EMER LIGHT ON SERVICE DOOR IAW AMM 33-50-10 STEPS 2 I1, 3, 2K1 & 2, STEPS 3 J 1,2 & 3. OPERATIONALLY CHECKED GOOD IAW AMM 33-50-00.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 27,430 hrs · 23,401 cycles

HAD FAINT BURNING SMELL ON TAXI IN. ALL INDICATIONS OF TEMPERATURES WERE NORMAL. ACCOMPLISHED FAULT ISOLATION OF SUSPECTED FEINT BURNING SMELL IN COCKPIT IAW ETN - EM - 72-034. NO FOREIGN SMELL DISCOVERED. TROUBLE SHOT ISSUE IAW FIM 21-20-00-810-801-A. CHECK ALL PARTS OF THE COCKPIT INCLUDING EMER FLASHLIGHTS & CHARGERS, WINDOW HEATING UNITS, CB PANELS & AREAS WITH RELAYS, DISPLAY UNITS, PACK AIR OUTLETS TO CABIN, ETC. NO NOTICEABLE SMELL NOTICED FROM ANY OF THESE ITEMS AT THIS TIME.

Part: FUEL RAIL — FAILED (APU FUEL SYS) · airframe 27,310 hrs · 23,277 cycles

STRONG ODOR OF FUEL & EXHAUST IN COCKPIT. ODOR COMES FROM AN APU FUEL LEAK AT APU DRAIN. FUEL LEAKING FROM APU FUEL MANIFOLD. APU SECURED INOPERATIVE. R & R SECONDARY FUEL RAIL. OPS & LEAK CHECKED GOOD IAW AMM 49-32-06.

Part: SENSOR — FAILED (RT ENGINE) · airframe 27,289 hrs · 23,259 cycles

WHEN THRUST WAS ADVANCED ON TAKEOFF ROLL THE NR 2 ENG HP VIB INDICATOR PEGGED HIGH. NO MASTER CAUTION EVER OCCURRED. THE INDICATOR REMAINED PEGGED EVEN WHEN THRUST WAS REDUCED TO IDLE. TAKEOFF ABORT WAS LOW SPEED WITH VERY MINIMAL BREAKING. NO UNUSUAL SOUNDS OR VIBRATIONS WERE FELT BY CREW ENG WAS SHUT DOWN IMMEDIATELY AFTER CLEARING THE RUNWAY. R & R RT ENG VIBRATION SENSOR IAW RR MANUAL 77-41-10. OPERATIONS CHECKED GOOD.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 26,582 hrs · 22,703 cycles

FLIGHT ENCOUNTERED MINOR CHOP & CREW BEGAN TO SMELL ELEC TYPE FUMES IN COCKPIT. CREW COMPLIED WITH AOM VOL 1 PROCEDURES, DECLARED AN EMERGENCY & DIVERTED TO JAX. INSPECTED BOTH ENGS 1 & 2 FOR OIL LEAKAGE IN THE INLETS & EXHAUST, NO EVIDENCE OF OIL LEAKS NOTED. INSPECTED BOTH PACKS FOR EVIDENCE OF BLEED LEAKS WHILE OPERATING, NO BLEED LEAKS NOTED. PERFORMED ETN-EM-72-034 ODOR EVENT TROUBLESHOOTING, NO DETECTABLE SMELL OR ODOR NOTED. PERFORMED FIM TASK 21-20-00-810-803-A OIL RELATED SMOKE SMELL, NO SMELL DETECTED. PERFORMED FIM TASK 21-20-00-810-801-A SMOKE ABNORMAL SMELL, NO SMELL NOTED. INSPECTED CABIN LIGHTS FOR EVIDENCE OF ELEC BURNING SMELL, NO DEFECTS NOTED AT THIS TIME.

Part: POTENTIOMETER — OUT OF ADJUST (NLG STEERING) · airframe 26,474 hrs · 22,630 cycles

ABORTED TAKEOFF IAW FULL LT RUDDER TO MAINTAIN STRAIGHT CENTERLINE DIRECTIONAL CONTROL. LOW SPEED ABORT, TOOK DELIBERATE LT CORRECTION OF TILLER TO MAINTAIN STRAIGHT TAXI. WHILE WAITING FOR TOW WE COULD HEAR STEERING CLICKING 5 TIMES, NO EICAS MSG AT ALL DURING ABORT UNTIL TOWED. TRANSFERRED TO NRWC 663-MIA-01559 IAW NRWC 663-MIA-01559 FOR CORRECTIVE ACTION LOAD POTENTIOMETER ADJUST IAW 32-50-00 ALL CHECKS PASS.

Part: PRESSURE SWITCH — FAULTY (BRAKE SYSTEM) · airframe 25,968 hrs · 22,251 cycles

CLIMBING THROUGH FL180 BRAKE ON LIGHT CAME ON & REMAINED ON FOR ENTIRE FLIGHT. LIGHT EXTINGUISHED AFTER TAXIING & STOPPING, THEN STARTING & RELEASING PB. TRANSFERRED TO NRWC 663-ORD-01469. REPLACED PARKING BRAKE PRESS SWITCH IAW MM 32-44-07, OPERATIONS CHECKED & LEAK CHECKED GOOD.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT) · airframe 25,388 hrs · 21,791 cycles

RT CABIN EMERGENCY EXIT DOOR SIGN INOPERATIVE. R & R INVERTER IAW AMM 33-50-11. OPS CHECKED GOOD IAW AMM 33-50-00.

Part: FLASHLIGHT ASSY — INOPERATIVE (COCKPIT) · airframe 25,093 hrs · 21,521 cycles

F/O FLASHLIGHT INOPERATIVE. REPLACED F/O FLASHLIGHT IAW AMM 25-60-00. OPS CHECKED GOOD.

Part: DISPLAY — FAILED (COCKPIT) · airframe 25,097 hrs · 21,524 cycles

DURING APU START WITH GPU POWER, THE F/O MFD SCREEN WENT BLANK. THE MFD 2 CIRCUIT BREAKER POPPED WITH ODOR OF ELECTRICAL SMOKE. R & R F/O MFD UNIT, OPS CHECKED GOOD IAW AMM 34-22-02.

Part: PDU — FAILED (COCKPIT) · airframe 24,940 hrs · 21,398 cycles

F/O PFD WENT BLACK WITH AN ELECTRICAL BURNING ODOR. ISOLATED ODOR TO PFD NR 2, R & R IAW AMM 34-22-01. OPS CHECKED GOOD, NO DEFECTS NOTED.

Part: UNKNOWN — UNKNOWN (EMERGENCY LIGHTS) · airframe 24,882 hrs · 21,353 cycles

MULTIPLE EMERGENCY LIGHTS OUT. PERFORMED OPS CHECK OF EMERGENCY LIGHTS IAW AE WC 33-700-17, OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 24,564 hrs · 21,115 cycles

DURING B INSPECTION, FOUND THE EMERGENCY LIGHT STRIP NR 4 INOPERATIVE. ACFT REMOVED FROM SERVICE. R & R THE NR 4 BATTERY & BATTERY CHARGER. OPS CHECKED GOOD IAW AMM 33-50-00. R & R NR 4 FLOOR PROXIMITY LIGHT STRIP. OPS CHECKED GOOD. ACFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,564 hrs · 21,115 cycles

DURING B INSPECTION, FOUND EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT IAW AMM 33-50-12. OPS CHECKED GOOD. ACFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,564 hrs · 21,115 cycles

DURING B INSPECTION, FOUND EMERGENCY LIGHT INOPERATIVE. ACFT REMOVED FROM SERVICE. R & R LIGHT. OPS CHECKED GOOD IAW AMM 33-50-12. ACFT RETURNED TO SERVICE.

Part: FRAME — CRACKED (FUSELAGE) · airframe 24,005 hrs · 20,642 cycles

ONE INCH CRACK FOUND ON FRAME 5 ABOVE STR 11. PERFORMED REPAIR TO FR 5 IAW E0-EM-53MR-2125.

Part: FLASHLIGHT ASSY — BROKEN (FWD F/A) · airframe 23,942 hrs · 20,582 cycles

FLIGHT 2761, FORWARD FLIGHT ATTENDANT’S FLASHLIGHT HOLDER IS BROKEN. REMOVED AND REPLACED THE FORWARD FLIGHT ATTENDANT FLASHLIGHT HOLDER IAW AMM 33-50-16. AIRCRAFT RETURNED TO SERVICE

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 23,917 hrs · 20,563 cycles

ON FLIGHT 2712 THE CREW REPORTED THE FLIGHT ATTENDANT’S FLASHLIGHT WAS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FLIGHT ATTENDANT’S FLASHLIGHT IAW EMB145 AMM 33-50-16 STEP J, 1 AND STEP 3, I (4) AND J 1 AND 2, ETN-EM-33-034. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: HOLDER — BROKEN (FLASHLIGHT) · airframe 23,775 hrs · 20,453 cycles

DURING MAINTENANCE INSPECTION FOUND THE FIRST OFFICER’S FLASHLIGHT HOLDER BROKEN. MEL 25-53 AUTH 030954-C LOG 3084271. REMOVED AND REPLACED THE FIRST OFFICER’S FLASHLIGHT IAW ERJ AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. MEL RESTORED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — DEFECTIVE (COCKPIT) · airframe 23,192 hrs · 20,013 cycles

DURING MAINTENANCE INSPECTION FOUND THE CAPT'S FLASHLIGHT WILL NOT CHARGE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CAPT'S FLASHLIGHT IAW EMB 145 AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. NO FURTHER DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE — BROKEN (CABIN) · airframe 22,935 hrs · 19,810 cycles

DURING B INSPECTION FOUND THE PROXIMITY LIGHT STRIP NR 5 HAS A BROKEN WIRE AND THE PANEL IS CRACKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT NR 5 PROXIMITY LIGHT STRIP IAW EMB 145 AMM 33-50-12. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 22,935 hrs · 19,810 cycles

DURING MAINTENANCE INSPECTION FOUND THE EMERGENCY LIGHT STRIPS BETWEEN THE GALLEY AND THE EMERGENCY EXIT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 2 & 3 BATTERY PACKS AND BATTERY POWER SUPPLY IAW EMB 145 AMM 33-50-04. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONNECTOR — MISSING (CABIN) · airframe 22,935 hrs · 19,810 cycles

DURING B INSPECTION FOUND THE PROXIMITY LIGHT STRIP NR 1 MISSING ONE CONNECTOR FOR WIRE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 1 PROXIMITY LIGHT STRIP IAW EMB 145 33-50-12.

Part: POWER SUPPLY — FAILED (CABIN) · airframe 22,920 hrs · 19,798 cycles

DURING B INSPECTION FOUND THE BATTERY POWER SUPPLIES FAILED CHECKS. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE BATTERY POWER SUPPLIES. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 22,935 hrs · 19,810 cycles

DURING MAINTENANCE INSPECTION FOUND THE DIAMOND GUSSET AT FRAME 20 RIGHT CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE DIAMOND GUSSET AT FRAME 20 RIGHT IAW EMB SRM 51-40-02, EMB SRM 51-20-03, EMB SRM 51-40-06. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: HOLDER — DEFECTIVE (CABIN) · airframe 22,920 hrs · 19,798 cycles

DURING B INSPECTION FOUND THE BATTERY HOLDER ASSEMBLIES FAILED THE OPERATIONAL CHECK. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE BATTERY HOLDER ASSEMBLIES. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 22,779 hrs · 19,689 cycles

ON FLIGHT 2750 THE CREW REPORTED THE AFT CABIN FLASHLIGHT WAS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AFT CABIN FLASHLIGHT IAW EMB-145 MM 25-60-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONNECTOR — UNSERVICEABLE (CABIN) · airframe 22,744 hrs · 19,662 cycles

DURING B INSPECTION FOUND THE LEFT OVERWING EMERGENCY LIGHT CONNECTOR BACK SHELL MISSING. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT EXTERIOR OVERWING EMERGENCY LIGHT CONNECTOR (P8563) AND INSTALLED NEW BACKSHELL IAW EMB145 SWPM20-50-00, WM 33-50-50 AMM33-50-10. THE OPERATIONAL CHECK WAS GOOD IAW EMB145 AMM 33-50-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 22,723 hrs · 19,635 cycles

ON FLIGHT 2878 THE CREW REPORTED THE FIRST OFFICER’S FLASHLIGHT WAS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FIRST OFFICER’S FLASHLIGHT AS PER EMB MM 25-60-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LINER — CRACKED (MAIN DOOR) · airframe 22,578 hrs · 19,521 cycles

DURING B INSPECTION FOUND THE EMERGENCY LIGHT ASSEMBLY LINING ON MAIN DOOR CRACKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY LIGHT ASSEMBLY LINING ON MAIN DOOR. THE OPERATIONAL CHECK WAS GOOD IAW EMB AMM 25-23-04 STEPS J(3)(E) AND I(3)(G). THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CRADLE — BROKEN (FLASHLIGHT) · airframe 22,253 hrs · 19,244 cycles

ON FLIGHT 3214, FOUND FLIGHT DECK FLASHLIGHT HOLDER BROKE CLAMP NARROW END. THE AIRCRAFT WAS REMOVE FROM SERVICE. REMOVED AND REPLACED FLASHLIGHT ASSY IAW EMB 145 AMM 33-50-16. OPS CHECKED GOOD. THE AIRCRAFT RETURN TO SERVICE.

Part: WARNING LIGHT — FALSE ACTIVATION (ENGINE) · airframe 22,046 hrs · 19,067 cycles

FLIGHT 3231, CREW REPORTED THAT DURING TAKEOFF THEY RECEIVED AN ATTCS NO MARGIN WARNING. TAKEOFF ABORTED AT LOW SPEED AND NO ENGINE PARAMETERS WERE EXCEEDED. AIRCRAFT REMOVED FROM SERVICE. PERFORMED ENGINE RUNS IAW FIM 73-75-00-810-846 AND MM 71-00-00. NO ISSUES OR EXCEEDANCES WERE OBSERVED IAW ETN EM-76-004. AIRCRAFT RETURNED TO SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 22,040 hrs · 19,059 cycles

DURING B INSPECTION, FOUND THE CEILING EMERGENCY LIGHT INOPERATIVE AT THE MAIN DOOR. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED LAMP IAW AMM 33-50-06. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 21,931 hrs · 18,962 cycles

DURING MAINTENANCE INSPECTION FOUND THE INVERTER NR 6 INOPERABLE AND THE NR 4 BATTERY CHARGER HAD A BLOWN INTERNAL FUSE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE INVERTER--DID NOT FIX. REMOVED AND REPLACED THE BATTERY HOLDER ASSEMBLY---DID NOT FIX. REMOVED AND REPLACED THE NR 4 BATTERY CHARGER AND INSTALLED THE OVERHEAD PANEL AT BATTERY CHARGER NR 4 IN ACCORDANCE WITH EMB 145 AMM 25-22-04. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE — LOOSE (CABIN) · airframe 21,931 hrs · 18,962 cycles

DURING MAINTENANCE INSPECTION FOUND THE OVERWING EMERGENCY LIGHTS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND WIRE TO BE LOOSE AT PIN A CONNECTOR P8563, SECURED WIRE IN ACCORDENCE WITH EMB 145 STANDARD PRACTICE 20-60-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — LOOSE (EXTERIOR) · airframe 21,919 hrs · 18,951 cycles

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

Part: BULB — LOOSE (EMERGENCY LIGHT) · airframe 21,702 hrs · 21,702 cycles

DURING MAINTENANCE INSPECTION, FOUND THE LEFT OVERWING EMERGENCY LIGHT INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. FOUND BULB LOOSE, INSTALLED BULB IAW AMM 33-50-07. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 21,384 hrs · 18,520 cycles

DURING B-INSPECTION FOUND THE NR 4 EMERGENCY LIGHTING SYSTEM INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 4 CHARGER ASSEMBLY AND BATTERY, PER WORK CARD 33-700-19. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SOCKET — DEFECTIVE (CABIN) · airframe 21,338 hrs · 18,487 cycles

DURING MAINTENANCE INSPECTION FOUND BOTH OVERWING EMERGENCY LIGHTS ARE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND LEFT OVERWING EMERGENCY LIGHT ARCHING AND SHORTING OUT. REMOVED AND REPLACED SOCKET IAW EMB 145 AMM 33-50-07. PART NUMBER FOR LEFT EMERGENCY LIGHT: 30-2510-3. REMOVED AND REPLACED NR 4 BATTERY AND CHARGER ASSEMBLY IAW EMB145 AMM 33-50-04. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SWITCH — INOPERATIVE (AC BAY) · airframe 29,170 hrs · 27,075 cycles

ON FLIGHT I 2807 THE CREW REPORTED AN INTERMITTANT AND REPEATED PACK 1 OVER TEMPERATIURE MESSAGE WHILE CLIMBING THRU 15000. THE CREW DECLARED AN EMERGECNY AND ELECTED TO RETURN TO DFW. THE AIRCRAFT WAS REMOVED FROM SERVICE. INSPECTED NR 1 PACK SYSTEM FOR LEAKS AND NONE NOTED. REMOVED AND REPLACED THE PACK OVERTEMP SWITCH IAW 21-51-08. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 20,587 hrs · 17,926 cycles

ON FLIGHT 2965 THE CREW REPORTED THAT DURING CRUISE THEY NOTICED SMOKE AND FUMES IN THE CABIN. THE CREW DECLARED AN EMERGENCY AND DIVERTED TO SAT. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. COMPLIED ETN EM 72-034 R4 NO SMOKE OR FUMES NOTED AT THIS TIME. ALSO COMPLIED WITH VISUAL CHECK OF CABIN ITEMS SUCH AS FLASHLIGHTS, CABIN LIGHTS, PSUS , LAV LIGHTS, COCKPIT RELAYS FOR ANY DAMAGE OR BURNING SMELL. PERFORMED OPERATIONAL CHECK ON PACK NR 1 IAW EMB 145-AMM 21-51-00. THE OPERATIONAL CHECK WAS GOOD AT THIS TIME AND NO DEFECTS NOTED ON VISUAL CHECK OF CABIN PACK NR 2 FOUND TO BE INOPERATIVE AND WAS DEFERRED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: O-RING — LEAKING (NR 1 ENGINE) · airframe 19,220 hrs · 16,946 cycles

ON FLIGHT 4160 THE CREW REPORTED THAT AFTER TAKEOFF AND ON CLIMBOUT NOTICED SMOKE/HAZE IN THE COCKPIT AND CABIN. THE CREW DECLARED EMERGENCY AND RETURNED TO FIELD. THE AIRCRAFT LANDED WITHOUT INCIDENT. PERFORMED ETN EM-72-034R4. RAR NR 1 ENG. SPANNER LOCK NUT PLUG O-RING IAW RRMM 72-21-05

Part: ENGINE — MALFUNCTIONED (NR 1) · airframe 1,922 hrs · 16,945 cycles

ON FLIGHT 4444 SHORTLY AFTER TAKEOFF THE CREW REPORTED THE COCKPIT STARTED TO FILL WITH SMOKE. THE FLIGHT ATTENDANT ALSO OBSERVED SMOKE IN THE CABIN. THE CREW ABORTED THE TAKEOFF AND RETURNED TO THE GATE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 1 ENGINE IAW MTX WORK CARD 71-00-00. THE OPERATIONAL AND LEAK CHECKS WERE GOOD.

Part: FLASHLIGHT — CRACKED (CABIN) · airframe 19,201 hrs · 16,932 cycles

DURING MAINTENANCE BASE VISIT DISCOVERED A BROKEN LENS RETAINER ON THE FORWARD CABIN EMERGENCY FLASHLIGHT DURING FUNCTIONAL CHECK WC 33-700-20. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FLASHLIGHT IAW WC 33-700-20. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CARBON SEAL — FAILED (NR 2 ENGINE) · airframe 18,058 hrs · 16,039 cycles

ON FLIGHT 4079 AFTER ROTATION LAVATORY SMOKE MESSAGE PRESENTED ON EICAS AND THE FLIGHT ATTENDANT REPORTED SMOKE IN THE CABIN. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO YUL WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 2 ENGINE IAW MTX WC 71-000-00. THE OPERATIONAL CHECK AND LEAK CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. TEARDOWN FOUND NR 4 CARBON SEAL FAILED, CAUSING THE SMOKE. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ATTACH FITTING — DAMAGED (HORIZONTAL STAB) · airframe 17,996 hrs · 15,995 cycles

DURING THE MAINTENANCE BASE VISIT FOUND THE HORIZONTAL STABILIZER LEFT ATTACH POINT FITTING BEARING HOUSING SCORED AND DAMAGED, BEYOND MANUAL LIMITS. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE HORIZONTAL STAB LEFT ATTACH POINT FITTING BEARING. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,996 hrs · 15,995 cycles

DURING MAINTENANCE BASE INSPECTION FOUND CARGO DOOR SILL CORRODED BETWEEN FRAMES 65 AND 68. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED BEAM IAW SRM 51-40-02 . THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: DISPLAY — MALFUNCTIONED (COCKPIT) · airframe 16,103 hrs · 14,537 cycles

ON FLIGHT 2723 DURING THE TAKEOFF ROLL AT 80 KNOTS THE EICAS SCREEN WENT BLANK THEN RED X WITH MASTER WARNING THEN CAME BACK ON. THE TAKEOFF WAS ABORTED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FIRST OFFICERS MULTI FUNCTION DISPLAY UNIT IAW EMB145 AMM 34-22-01. THE OPERATIONAL CHECK WAS GOOD IAW EMB145 AMM 34-22-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 15,591 hrs · 14,086 cycles

DURING MAINTENANCE BASE PS-2 VISIT FOUND THE EMERGENCY LIGHTS TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE BATTERY CHARGER ASSEMBLY. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 14,362 hrs · 13,025 cycles

DURING MAIN BASE VISIT INSPECTION FOUND THE LEFT OMEGA BEAM CORRODED AT FRAME 25. AIRCRAFT REMOVED FROM SERVICE. FABRICATED AND INSTALLED REPAIR DOUBLER FILLER AND SHIM AT LEFT OMEGA BEAM AT FRAME 25 IAW EMB 145 SRM 53-00-10. AIRCRAFT RETURNED TO SERVICE.

Part: PRESSURE SENSOR — FAILED (RUDDER) · airframe 9,015 hrs · 8,209 cycles

RECEIVED RUDDER 1-2 INOPERATIVE MESSAGE ABOVE FL 220 WITH AUTO PILOT ON - FOLLOWED AOM PROCEDURES. DIVERTED TO SGF. REMOVED AND REPLACED RUDDER PRESSURE SWITCH IAW EMB AMM 27-23-04. OPERATIONAL CHECK GOOD IAW EMB AMM 27-23-00-700-804A, STEP J, SECTION 2. AIRCRAFT RETURNED TO SERVICE.