N931AE

Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 45,637 hrs · 41,587 cycles

BLEED 1 LEAK DISPLAYED IN FLIGHT. INSPECTED FOR BLEED 1 LEAK/ NO DEFECTS NOTED. OPS CHECKED IAW AMM 36-00-00. OPS CHECKED GOOD. COULD NOT DUPLICATE. AC OK FOR SERVICE

Part: BLEED VALVE — FAILED (NR 1 ENGINE) · airframe 45,270 hrs · 41,153 cycles

BLEED 1 VALVE FAILED MESSAGE ON TO ROLL. R & R THE BLEED VALVE IAW AMM 36-11-05. OPS CHECKED GOOD IRT AMM 36-00-00-700-803-A. GROUND RAN AIRCRAFT. NO LEAKS NOTED AT THIS TIME. OKAY FOR SERVICE.

Part: BLEED VALVE — ACTIVATION ERROR (ENGINE) · airframe 44,128 hrs · 39,848 cycles

ON TAKEOFF ENGINE BLEED VALVE FAIL ON EICAS, GOING 20 KNOTS AND REFKECTED TAKEOFF. FACT 08MAR25 18:48 CLT REMOVED AND REPLACED ENGINE BLEED AIR VALVE IRW AMM 36-11-05. PERFORMED OPS CHECK IAW AMM 36-11-05-700-802-A, OPS CHECK IS GOOD NO LEAKS NOTED. AIRCRAFT IS OK FOR SERVICE.

Part: COMPUTER — FAULTED (STALL PROTECTION) · airframe 42,623 hrs · 38,142 cycles

SPS 2 INOP DISPLAYED IN FLT FACT 06JUN24 20:04 PHL REMOVED AND REPLACED STALL PROTECT COMPUTER IAW AMM 27-36-02. PREFORMED OPS CHECK IAW AMM 27-36-00. OPS CHECK GOOD. A/C OK FOR SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 42,579 hrs · 38,094 cycles

BURNING SMELL DURING TAXI. CLEARED WITH PACK 1 SELECTED OFF FACT 29MAY24 19:10 CLT INSPECTED BOTH PACKS FOR DEFECTS. NONE NOTED AT THIS TIME. PERFORMED OPS CHECK OF THE COOLING PACK SYSTEM IRT AMM 21-51-00. NO BURNING SMELL NOTED AT THIS TIME. A/C OK FOR SERVICE

Part: BOOT — DAMAGED (NR 1 A/C PACK)

IN CLIMB OUT SLOW TO RAPID DEPRESSURIZATION AT FL 290.BEGAN TO STABALIZE AT FL 230 IN AUTO MODE. FACT 16APR24 20:05 PHL INSPECTED PACK 1 AREA AND FOUND DAMAGED BOOT BETWEEN AIRFRAME AND CONDENSER/MIXER. R+R BOOT IAW AMM 25-51-04. PERFORMED MANUAL/AUTO MODE PRESS TEST IAW AMM 21-31-00. OPS/LEAK CHECK GOOD. OK FOR SERVICE AT THIS TIME.

Part: FLOOR SUPPORT — CORRODED (FRMS 48-50) · corrosion level 2 · airframe 42,307 hrs · 37,776 cycles

00210 LH Y-479 FLOOR BEAM CAP IS CORRODED BETWEEN FRM48 AND FRM50. REMOVED AND REPLACED LH Y-479 FLOOR BEAM CAP BETWEEN FRM46 AND FRM53 IAW EMB-145 SRM 51-40-02-PR

Part: SEAT TRACK — CORRODED (FRMS 37-38) · corrosion level 2 · airframe 42,307 hrs · 37,776 cycles

00203 CENTER Y 0 FLOOR SEAT TRACK IS CORRODED BETWEEN FRM37 AND FRM38. INSTALLED CENTER Y 0 FLOOR SEAT TRACK BETWEEN FRM36 TO FRM46 IAW EMB145 AMM 53-01-06-400-801-A.

Part: FLOORBEAM — CORRODED (CABIN) · corrosion level 2 · airframe 42,307 hrs · 37,776 cycles

00207 LH Y-479 FLOOR BEAM CAP IS CORRODED BETWEEN X13200 AND X15125. INSTALLED NEW SERVICEABLE FLOOR BEAM CAP (GUSSET) PN: 145-30634-005 IAW EMB-145 SRM 51-40-02-PR.

Part: FLOOR SUPPORT — CORRODED (CABIN) · corrosion level 2 · airframe 42,307 hrs · 37,776 cycles

00206 CENTER Y 0 FLOOR BEAM CAP IS CORRODED BETWEEN X11990 AND X13200. : INSTALLED NEW SERVICEABLE CENTER Y 0 FLOOR BEAM CAP BETWEEN X11990 AND 13200 IAW EMB145 SRM 51-40-02.

Part: FLOORBEAM — CORRODED (FRM 22) · corrosion level 2 · airframe 42,307 hrs · 37,776 cycles

00178 RH FLOOR BEAM CAP AT FRM22 AND Y+479 IS CORRODED. REMOVED AND REPLACED WITH NEW RH FLOOR BEAM CAP (P/N: 145-22461-011) IAW EMB145LR SRM 51-40-02

Part: FLOOR SUPPORT — CORRODED (FRMS 28-29) · corrosion level 2 · airframe 42,307 hrs · 37,776 cycles

00192 CENTER Y 0 FLOOR BEAM LH FLANGE IS CORRODED BETWEEN FRM28 AND FRM29. REPAIRED CENTER Y 0 FLOOR BEAM LH FLANGE IS CORROSION BETWEEN FRM28 AND FRM29 IAW EMB-145 SRM 53-22-10-RE AND PIEDMONT EO1-53-24-0210

Part: STRAP — CORRODED · corrosion level 2 · airframe 42,307 hrs · 37,776 cycles

00182 LH FLOOR SUPPORT STRAP AT X7578 BETWEEN Y-479 AND Y 0 IS CORRODED.

Part: STRAP — CORRODED (FLOORBEAM) · corrosion level 2 · airframe 42,307 hrs · 37,776 cycles

LH FLOOR SUPPORT SRTRAP AT X7578 BETWEEN Y-479 AND Y 0 IS CORRODED. REMOVED AND REPLACED STRAP IAW EMB145 SRM 51-40-02.

Part: FLOORBEAM — CORRODED (FRM 20) · corrosion level 2 · airframe 42,307 hrs · 37,776 cycles

00179 CENTER Y 0 FLOOR BEAM CAP IS CORRODED BETWEEN FRM20 AND X7038. INSTALLED NEW CENTER Y 0 FLOOR BEAM CAP PN# 145-22460-013 BETWEEN FRM20 AND X7038 IAW EMB 145 SRM 51-40-02-PR.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,718 hrs · 37,134 cycles

LEFT I/B MAIN TIRE DAMAGED (TREAD CAME OFF). R&R #200 MLG TIRE IAW EMB AMM 32-49-02-000-801-A/32-49-02-400-801-A INSPECTED AND FOUND ADDITIONAL DAMAGE SEE SEQ 2,3, THIS LP. SEQ 1 OF L.P. 301128

Part: FLASHLIGHT — INOPERATIVE · airframe 41,010 hrs · 36,356 cycles

AFT FLIGHT ATTENDANT EMERGENCY FLASHLIGHT NOT CHARGING-C/A-RAR AFT FLIGHT ATTENDANT EMERGENCY FLASHLIGHT BATTERY. OPC GOOD PER EMB AMM 33-51-01

Part: LAMP — INOPERATIVE (12A) · airframe 40,901 hrs · 36,242 cycles

12A PSU EMERRGENCY LIGHT INOP-C/A-RAR 12A PSU EMERGENCY LIGHT LAMP IN REFERENCE WITH EMB AMM 33-50-08-000-801-A AND 33-50-08-400-801-A. OPC GOOD. END.

Part: FLASHLIGHT — INOPERATIVE (AFT CABIN) · airframe 40,577 hrs · 35,896 cycles

FA AFT EMERGENCY FLASHLIGHT NOT CHARGING. R & R FA AFT EMERGENCY FLASHLIGHT ASSEMBLY IAW EMB AMM 33-50-16-000-801-A AND 33-50-16-400-801-A. OPS CHECKED GOOD.

Part: APU — CLOSED (COCKPIT) · airframe 39,883 hrs · 35,075 cycles

MECH / FLT CREW REPORTS SMOKE/ODOR IN COCKPIT AND CABIN SHUT OFF APU AND PACKS;SMOKE WENT AWAY. NO FIRE INDICATIONS NO FIRE BOTTLES DISCHARGED.- UNKNOWN SOURCE. CA PERFORMED EMB 145 FIM 21-20-00-810-801-A SMOKE/ABNORMAL SMELL IN THE CABIN/COCKPIT - UNKNOWN SOURCE PER ATS TRIAD WORK SCOPE. REF. NRWC # 931-ORD-06158 FOR ADDITIONAL FINDING. NO FURTHER DISCREPANCIES FOUND. RAR R/H OUTLET MUFFLER IAW EMB 145 AMM 21-23-04. PERFORMED OPS CHECK OF AIR DISTRIBUTION SYSTEM IAW EMB 145 AMM 21-20-000 OPS CHECK GOOD.

Part: INVERTER — INOPERATIVE (12A) · airframe 39,725 hrs · 34,901 cycles

SEAT 12A EMERGENCY EXIT PLACARD LIGTH INOP-C/A-RAR #5 EMERGENCY LIGHT INVERTER IAW EMB AMM 33-50-11-000-801-A AND 33-50-11-400-801-A. OPC GOOD. END.

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 39,370 hrs · 34,550 cycles

LAV SMOKE WARNING IN FLIGHT NO EVIDENCE OF SMOKING OR VAPING. NO ACTUAL SMOKE WAS OBSERVED.-C/A-PERFORMED THE OPERATIONAL TEST OF THE SMOKE DETECTOR SYSTEM IAW AMM 26-14-00 NO FAULTS NOTED AT THIS TIME

Part: NONE — NONE · airframe 39,343 hrs · 34,523 cycles

AFT EMERGENCY FLASHLIGHT CRADLE BROKENMEL 25-32 AUTH# 030074M-C LOG PG 4797230 ITEM #2-C/A-RAR AFT EMERGENCY FLASHLIGHT CRADLE ASSY IAW AMM 33-50-16 MEL ITEM RESTORED

Part: BRACKET — CRACKED (CARGO DOOR) · airframe 37,820 hrs · 32,791 cycles

BAGGAGE DOOR FWD TORSION BAR BRACKET IS CRACKED.-C/A-RAR BAGGAGE DOOR FWD TORSION BAR BRACKET IAW SRM-51-40-02

Part: SUPPORT ANGLE — CRACKED (FRMS 47-48) · airframe 37,820 hrs · 32,791 cycles

RT OMEGA BEAM SUPPORT ANGLE IS CRACKED , BETWEEN FR 47 AND FR 48 -C/A-REPLACED RH OMEGA BEAM SUPPORT ANGLE BETWEEN FR 47 AND FR 48 IAW SRM 53-23-02 AND SRM 51-40-02. RT OMEGA BEAM SUPPORT ANGLE IS CRACKED , BETWEEN FR 47 AND FR 48 -C/A-REPLACED RH OMEGA BEAM SUPPORT ANGLE BETWEEN FR 47 AND FR 48 IAW SRM 53-23-02 AND SRM 51-40-02.

Part: STIFFENER — CRACKED (DOOR FRAME) · airframe 37,820 hrs · 32,791 cycles

STIFFENER ON AFT SIDE OF FRAME 68 FOR CARGO DOOR HOLD OPEN STRUT RECEPTACLES IS CRACKED. -C/A-INSTALLED NEW STIFFENER IAW SRM 51-40-02.

Part: BRACKET — CRACKED (CARGO DOOR) · airframe 37,820 hrs · 32,791 cycles

BAGGAGE DOOR AFT TORSION BAR BRACKET IS CRACKED. -C/A-RAR BAGGAGE DOOR TORSION BAR BRACKET IAW SRM 51-40-02.

Part: SHEAR TIE — CRACKED (FRM 65 S18L) · airframe 37,820 hrs · 32,791 cycles

SHEAR CLIP ON FRAME 65 AT STR 18L HAS A 1/2" CRACK. -C/A-INSTALLED NEW SHEAR CLIP IAW SRM 51-40-02.

Part: SHEAR TIE — CRACKED (FRM 21 S1-2R) · airframe 37,820 hrs · 32,791 cycles

CRACKED SHEAR CLIP AT FR 21 BETWEEN STR 1 RT AND STR 2 RT. -C/A-TRIMMED, DRILLED, AND INSTALLED SERVICEABLE FABRICATED SHEAR CLIP IAW SRM 51-40-02.

Part: STUD — MISSING (EMERGENCY LIGHT) · airframe 37,820 hrs · 32,791 cycles

CEILING PANEL 253CLC AFT EMERGENCY EXIT SIGN MISSING MOUNTING STUD-C/A-COMPLETE:RAR CEILING PANEL 253CLC AFT EMERGENCY EXIT SIGN IAW AMM 20-10-01

Part: LIGHT — DAMAGED (CABIN) · airframe 37,820 hrs · 32,791 cycles

LH EMERGENCY FLOOR LIGHT STRIP EXTRUSIONS #1,2,3,4,7,AND 8 ARE DAMAGED-C/A-COMPLETE:REPLACED L/H EMERGENCY FLOOR LIGHT STRIP EXTRUSIONS #1,#2,#3,#4,#7 AND #8 IAW AMM 33-50-12.

Part: LIGHT — MISSING (CABIN) · airframe 37,820 hrs · 32,791 cycles

3 EMERGENCY FLOOR LIGHT INTERCONNECT STRIPS MISSING (STANDARD LENGTH)-C/A-COMPLETE:INSTALLED 3 EMERGENCY FLOOR LIGHT INTERCONNECT STRIPS DURING LIGHT STRIP INSTALL IAW AMM 33-50-12.

Part: RETAINER — MISSING (FLASHLIGHT) · airframe 36,638 hrs · 31,589 cycles

BOTH FA FLASH LIGHT MISSING WRIST RETAINING STRING.-C/A-REMOVED AND REPLACED BOTH FA FLASH LIGHT IAW EMB 145 AMM 33-50-16. OPC GOOG. NO FUTHER DEFECT NOTED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,523 hrs · 31,472 cycles

ROW 12 OVERHEAD EMERGENCY LIGHT INOP-C/A-REMOVED AND REPLACED ROW 12 OVERWING EMERGENCY LIGHT IAW AMM TASK 33-50-07-000-801-A AND 33-50-07-400-801-A. OPC GOOD. END.

Part: TRANSDUCER — FAILED (LT ENGINE ANTIIC) · airframe 36,225 hrs · 31,189 cycles

INFLIGHT GOT E1 ANTI ICE FAIL. RAN QRH AND PROBLEM DID NOT FIX ITSELF AND NEVER GOT BACK E1 ANTI ICING. "TRANSFERRED TO NRWC 931-ORD-04500"-C/A-REPLACED SEALS AND TORQUED BLEED AIR CHECK VALVED IAW EMB 145 AMM 36-11-01, OPS CHECK AND LEAK CHECK GOOD. REMOVED AND REPLACED E1 PRESSURE TRANSDUCER IAW EMB 145 AMM 30-21-06. OPS CHECK AND LEAK CHECK GOOD. REPLACED CONNECTOR P2859 HEATSHRINK BOOT IAW SWPM. REMOVED AND REPLACED CONNECTOR P0321 IAW SWPM. C/W OPS CHECK OF HIGH STAGE VALVE AS PER EMB-145 M/M 36-11-02, OPS CHECK AND LEAK CHECK GOOD

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 35,088 hrs · 30,176 cycles

COCKPIT EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED COCKPIT EMERGENCY LIGHT LAMP IAW AMM 33-50-05. OPC GOOD

Part: CONTROL PANEL — MALFUNCTIONED (SMOKE DETECTOR) · airframe 34,723 hrs · 29,817 cycles

LAV SMOKE EN ROUTE NO EVIDENCE OF SMOKE IN THE CABIN. TROUBLESHOT PER FIM 26-14-00-810-802-A. R & R SMOKE DETECTOR PANEL IAW EMB 145 AMM 26-14-02. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 34,404 hrs · 29,579 cycles

F/A FLASHLIGHT DOESN'T WORK. C/A-FWD FLIGHT ATTENDANT FLASHLIGHT REPLACED WORKING NORMAL AMM25-60-00.

Part: UNKNOWN — MALFUNCTIONED (BRAKE SYSTEM) · airframe 34,162 hrs · 29,343 cycles

DURING LANDING WHILE BRAKING FROM 100 KIAS-80KIAS BRAKE SURGING AT ONE PER TIRE ROTATION. SIMILAR TO ANTI-SKID ENGAUGING AND DISENGAUGING."TRANSFERRED TO NRWC 931-ORD-03974". C/A-PERFORMED BRAKE ASSEMBLY INSPECTION ON ALL MLG BRAKE ASSEMBLIES IAW AMM 32-49-03. NO DEFECTS NOTED. PERFORMED MAIN WHEEL ASSEMBLY INSPECTION ON ALL MLG WHEELS IAW AMM 32-49-02. NO DEFECTS NOTED. FIELD ANYLIZER CHECK PERFORMED IAW AMM 32-41-00. OPS CHECK GOOD. NO PREVIOUS PIREPS NOTED.

Part: STRUCTURE — DENTED (FUSELAGE) · airframe 34,103 hrs · 29,307 cycles

ERS-EM-53MR-3597-RF II - RT SIDE - SCRATCHES AND DENTS BTW FR. 77 & 78, STR. 16R & 17R ? PERMANENT REPAIR. C/A-COMPLETED IAW ERS-EM-53MR-3597.

Part: FITTING — DAMAGED (LT AILERON) · airframe 34,103 hrs · 29,307 cycles

LT AILERON PCA FITTING REQUIRES REPLACEMENT DUE TO HOLES MISALIGNMENT. LT AILERON DAMPER FITTING ON AILERON HAS AREA OF DAMAGE. C/A- REMOVED AND REPLACED LT AILERON PCA FITTING IAW EO-EM27MR-112. REMOVED AND REPLACED LT AILERON DAMPER FITTING IAW R FITTING IAW EO-EM-27MR-112. FITTING P/N 145-69382-609.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 34,103 hrs · 29,307 cycles

NUMEROUS SPOTS OF CORROSION ON AFT CARGO DOOR SILL BETWEEN FRAMES 65 AND 68. C/A-REMOVED AND REPLACED CARGO SILL IAW SRM CH. 51-40-02.

Part: BRACKET — CRACKED (LT WING) · airframe 34,103 hrs · 29,307 cycles

LEFT HAND UPPER WING, CENTER, PANEL "L" BRACKET CRACKED. C/A-REPLACED BRACKET IAW SRM 51-40-02.

Part: SUPPORT BRACKET — CRACKED (NLG) · airframe 34,103 hrs · 29,307 cycles

NOSE LANDING GEAR UPLOCK BOX SUPPORT BRACKET IS CRACKED, LEFT SIDE. C/A-REPLACED BRACKET IAW SRM 51-40-02.

Part: STRUCTURE — CRACKED (EMERGENCY LIGHT) · airframe 34,103 hrs · 29,307 cycles

#8 LT EMERGENCY LIGHT EXTRUSION IS CRACKED. C/A-COMPLETE:INSTALLED NEW EXTRUSION FOR #8 LT EMERGENCY FLOOR LIGHT IAW AMM 33-50-12.

Part: CRADLE — CRACKED (HANDSET) · airframe 32,783 hrs · 28,034 cycles

FWD FA HANDSET CRACKED. R&R FWD F/A CRADLE IAW AMM 23-31-03, OPS CHECK GOOD.

Part: SEAL — TORN (PAX DOORWAY) · airframe 32,546 hrs · 27,828 cycles

FLIGHT ATTENDENT REPORTED A WHISTLING SOUND COMING FROM THE MAIN CABIN DOOR DURING THE DECENT. FOUND TWO TEARS IN THE AIRFRAME SEAL. REPAIRED IAW AMM 53-21-01, PRESSURIZED TO 4.5, NO NOISE OR SQUEAL NOTED. OPS CHECKED GOOD.

Part: DISPLAY — FAILED (COCKPIT) · airframe 32,493 hrs · 27,800 cycles

PFD 2 SCREEN FAILED INTERMITTENTLY. SWAPPED MFD 2 TO PFD2. REMOVED AND REPLACED PFD2 IAW AMM 34-22-01. OPS CHECKED GOOD

Part: CARBON SEAL — LEAKING (ENGINE) · airframe 31,761 hrs · 27,104 cycles

COCKPIT AND CABIN SMOKE VISIBLE AND DETECTABLE. VERIFIED SMOKE ODOR & VISIBLE SMOKE HAZE. INSPECTED ENGINE INLETS AND FOUND OIL PUDDLE IN BOTTOM OF THE LT ENGINE UNDER FAN BLADES & RUNNING DOWN BACKSIDE OF FAN BLADES INDICATING THE 0 CARBON SEAL HAD FAILED. REPLACED THE CARBON SEAL IAW MM 72-25-25-000-801, & 72-25-25-400-801. PERFORMED APPLICABLE ENGINE RUNS IAW MM , AND ETN-EM-72-034. NO FURTHER LEAKS OR ODORS NOTED.

Part: LIGHT — INOPERATIVE (RT OVERWING) · airframe 31,493 hrs · 26,878 cycles

RIGHT OVERWING EMERGENCEY LIGHT INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY LIGHT IAW AMM 33-50-10. OPS CHECKED GOOD

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 30,858 hrs · 26,283 cycles

AFT CABIN CEILING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED NR 4 EMERGENCY LIGHT CHARGER IAW AMM 33-50-04.

Part: DUCT — INOPERATIVE (NR 2) · airframe 30,694 hrs · 26,098 cycles

NR 1 PACK IS ALREADY MEL'D AND WHILE TAXING NOTICED PACK 2 KICKING OFF WITH NO MESSAGE IVE HAD ISSUE BEFORE AND PACK WORKED IN FLIGHT BUT AFTER TAKEOFF RECYCLED PACK AFTER TO-1 AND AFTER 5 SECONDS GOT PACK 2 VALVE CLOSED AND TRIED A COUPLE RESETS AND SAME THING HAPPENED. REPLACED NR 2 DUCT, PRIMARY INLET IAW AMM 20-60-01 OPS GOOD

Part: DISPLAY — FAILED · airframe 29,244 hrs · 24,751 cycles

PFD 1 CA INOP PFD1 CB D13 POPPED ELECTRIC SMOKE SMELL IN COCKPIT-C/A-FO FMD DISPLAY TRANSFERRED TO CAPTAINS PFD AND DEFERRED PER MEL 34-1 M PROCEDURES C/W. SWAPPED FO'S MFD BACK TO CAPT'S PFD. REMOVED AND REPLACED CAPT'S PFD IAW AMM/EMB 34-22-01. CAPT'S PFD AND F/O'S MFD OPC GOOD IAW EMB AMM 34-22-00-700-801 MEL ITEM RESTORED

Part: CUP — CORRODED (LAVATORY) · airframe 29,165 hrs · 24,672 cycles

DURING IMBV INSPECTION, QA FOUND TOILET WASTE DRAIN VALVE CUP CORRODED. AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE TOILET WASTE DRAIN VALVE CUP IAW SRM 51-40-02, 51-20-01 AND 51-20-03.

Part: CUP — CORRODED (RT) · airframe 29,165 hrs · 24,672 cycles

DURING IMBV INSPECTION, FOUND THE TOILET WASTE DRAIN VALVE CUP CORRODED. AIRCRAFT WAS REMOCED FROM SERVICE FOR IMBV INSPECTION AND WILL BE RETURNED TO SERVICE AFTER IMBV INSPECTION. REMOVED AND REPLACED THE TOILET WASTE DRAIN VALVE CUP IAW EMB 145 SRM 51-40-02, 51-20-01 AND 51-20-03. AIRCRAFT WILL BE RETURNED TO SERVICE AFTER IMBV INSPECTION.

Part: SKIN — CRACKED (FRAME 77) · airframe 29,165 hrs · 24,672 cycles

DURING IMBV INSPECTION, QA FOUND A CRACK AROUND ONE FASTENER AT FRAME 77 JUST ABOVE STRINGER 4R. AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED IAW SRM 53-32-01 AND ETN EM-53-194.

Part: SKIN — CRACKED (FRAME 78) · airframe 29,165 hrs · 24,672 cycles

DURING IMBV INSPECTION, QA FOUND THE FUSELAGE EXTERNAL SKIN CRACKED AROUND ONE FASTENER AT FRAME 78, STRINGERS 3-4L . AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED PERMANENT REPAIR IAW SRM 53-32-01 AND ETN-EM-53-194 .

Part: DOOR SILL — CORRODED (FRAMES 64-68) · airframe 29,165 hrs · 24,672 cycles

DURING IMBV INSPECTION, QA FOUND THE CARGO DOOR CUTOUT LWR SILL CORRODED. AIRCRAFT WASREMOVED FROM SERVICE. REMOVED AND REPLACED CARGO DOOR LWR SILL IAW SRM 51-40-02 AND 51-20-03.

Part: SHEAR TIE — CORRODED (FRAME 65) · airframe 29,165 hrs · 24,672 cycles

DURING IMBV INSPECTION, QA FOUND THE CARGO DOOR CUTOUT FWD LWR SHEAR TEI ON FR 65 CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED SHEAR TIE IAW SRM 53-31-04 RE STEP 4F.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 29,165 hrs · 24,672 cycles

PROXIMITY LIGHTS 2,3,7,8 AND 9 ARE INOPERATIVE. REMOVED AND REPLACED EMERGENCY BATTERY PACK ASSEMBLIES 2 AND 4 IAW AMM 33-50-04, OPS CHECKED GOOD.

Part: FLOOR SUPPORT — CRACKED (FRAMES 47-48) · airframe 29,165 hrs · 24,672 cycles

RIGHT OMEGA BEAM INBD SUPPORT IS CRACKED BETWEEN FRAMES 47-48. REMOVED AND REPLACED NEW RH OMEGA BEAM INBD SUPPORTS IAW SRM 53-23-02.

Part: SOCKET — CRACKED (EMERGENCY LIGHT) · airframe 29,165 hrs · 24,672 cycles

THREE PROXIMITY LIGHT HOLDERS ARE CRACKED. REMOVED AND REPLACED THE LIGHT HOLDERS IAW AMM 33-50-12.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 29,165 hrs · 24,672 cycles

EMERGENCY LIGHT IN MAIN DOOR INOP. REMOVED AND REPLACED NR 1 EMERGENCY BATTERY PACK ASSEMBLY IAW AMM 33-50-04, OPC GOOD.

Part: FLOOR SUPPORT — CRACKED (FRAMES 47-48) · airframe 29,165 hrs · 24,672 cycles

LEFT OMEGA BEAM OUTBD SUPPORT IS CRACKED BETWEEN FRAMES 47-48. REMOVED AND REPLACED THE OMEGA BEAM OUTBD SUPPORT IAW SRM 53-23-02, 51-40-02.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 28,333 hrs · 23,895 cycles

RIGHT INSIDE SIDEWALL WING EMERGENCY EXIT LIGHT INOPERATIVE. R & R NR 5 EMERGENCY LIGHT INVERTER. OPS CHECKED GOOD IAW AMM 33-50-11.

Part: CONTROLLER — FAILED (CABIN PRESSURE) · airframe 27,475 hrs · 23,138 cycles

AIRCRAFT WILL NOT PRESSURIZE, CAB RATE 0 ALL THE WAY TO 13-13000 FEET, ^P 5.3 & 5.4, CABIN ALT WAS 0, ALSO AT 12000 FEET. OVERWEIGHT LANDING 47500 LBS SINK RATE WAS 200 FEET PER MIN, LANDING WAS SMOOTH NO BOUNCES. R & R DIGITAL CONTROLLER IAW AMM 21-31-01. OPERATIONS CHECKED GOOD, PARTS INTERCHANGEABLE IAW IPC. ACFT DESCEND RATE WITH LIMIT IAW AMM 05-50-25.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,383 hrs · 23,074 cycles

LEFT OVERWING EMER LIGHT INOPERATIVE. R & R LT OVERWING EMER LIGHT LAMP IAW AMM 33-50-10. OPERATIONS CHECKED GOOD.

Part: GASPER FAN — FAILED (CABIN) · airframe 25,808 hrs · 21,633 cycles

ENROUTE AT 32000 FEET STRONG ODOR OF SOMETHING BURNING IN THE COCKPIT & CABIN, SEEMED TO BE ELECTRICAL. TRANSFERRED TO NRWC 931-DFW-02186. AT FINAL INSPECTION, FOUND GASPER FAN WITH GRINDING NOISE WHEN OPERATING. R & R IAW AMM 21-23-03. OPERATIONS CHECKED GOOD. HOT JUG RECEPTACLES INSPECTION & NO DAMAGE FOUND. SEE NRWC 931-DFW-02186 FOR INSPECTION PERFORMED. COMPLIED WITH ETN EM 72- 034.

Part: PROXIMITY SENSOR — DAMAGED (NLG) · airframe 25,442 hrs · 21,316 cycles

CLIMBING THROUGH 1000 - 1500 FT LG AIR GND FAIL EICAS DISPLAYED. 1 - 2 MINUTES LATER ENG 1 - 2 REV DISAGREE EICAS DISPLAYED. BOTH MSGS STAYED ON FOR SEVERAL MINUTES & THEN EXTINGUISHED. SOMETIME LATER LG AIR GND FAIL MSG DISPLAYED FOR PERHAPS 30 SECONDS & THEN EXTINGUISHED. ACFT PERFORMED NORMALLY DURING THE WHOLE TIME. TRANSFERRED TO NRWC 931-DFW-02092. FOUND NLG WOW SWITCH WITH A BROKEN ELEC PIN. R & R SWITCH IAW AMM 32-63-02. OPERATIONS CHECKED GOOD.

Part: FLASHLIGHT ASSY — INOPERATIVE (COCKPIT) · airframe 25,076 hrs · 20,965 cycles

CAPTAIN`S FLASHLIGHT INOPERATIVE. R & R THE FLASHLIGHT ASSEMBLY IAW AMM TASKS 33-50-16-000-801-A & 33-50-16-400-801-A. OPS CHECKED GOOD.

Part: CRADLE — BROKEN (FLASHLIGHT) · airframe 24,900 hrs · 20,838 cycles

FLIGHT ATTENDANT'S EMER FLASHLIGHT CRADLE BROKEN. R & R FLIGHT ATTENDANT'S EMER FLASHLIGHT CRADLE IAW AMM 33-50-16-000-801-A & 33-50-16-400-801-A. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: SWITCH — BROKEN (FLASHLIGHT) · airframe 24,533 hrs · 20,501 cycles

FIRST OFFICERS EMER FLASHLIGHT SWITCH HAS BROKEN OFF. REPLACED FIRST OFFICER`S FLASHLIGHT IAW AMM 25-60-11.

Part: LINE — LEAKING (APU FUEL) · airframe 24,440 hrs · 20,423 cycles

DURING TAKEOFF ROLL, NOTICED A STRONG ODOR OF FUEL. FOUND APU FUEL PRESSURE LINE LEAKING ON SHUTOFF VALVE.

Part: SKIN — CRACKED (FUSELAGE) · airframe 24,227 hrs · 20,245 cycles

LEFT UPPER FUSELAGE SKIN CRACKED JUST AFT OF FRAME 75 ABOVE STRINGER 2L. PERFORMED PERMANENT REPAIR OF LT FUSELAGE SKIN IAW ERS-EM-53MR-700.

Part: WIRE — BROKEN (CABIN) · airframe 24,227 hrs · 20,245 cycles

NUMBER 1 EMER LIGHT STRIP HAS BROKEN WIRE. R & R NR 1 EMER LIGHT STRIP IAW AMM 33-50-12.

Part: SKIN — CRACKED (FUSELAGE) · airframe 24,227 hrs · 20,245 cycles

RIGHT UPPER FUSELAGE SKIN CRACKED JUST AFT OF FRAME 75 ABOVE STRINGER 2R. PERFORMED PERMANENT REPAIR IAW ERS-EM-53MR-701.

Part: STRIP — CRACKED (CABIN) · airframe 24,227 hrs · 20,245 cycles

LEFT EMER LIGHT STRIP EXTRUSION AT 231GF IS CRACKED. R & R LT EMER LIGHT STRIP EXTRUSION AT 231GF IAW 145 AMM 33-50-12.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 24,227 hrs · 20,245 cycles

CARGO DOOR AFT UPPER LIFTING LOWERING MECHANISM SUPPORT BRACKET CRACKED NEAR LOCK FASTENER. R & R SUPPORT BRACKET FOR CARGO DOOR AFT UPPER LIFTING & LOWERING MECHANISM IAW SRM 51-40-02. SEE WIP & TASK FOR DETAILS.

Part: ATTACH BRACKET — CRACKED (RT WING) · airframe 24,227 hrs · 20,245 cycles

RIGHT WING LOWER OVERWING NR 2 ATTACH BRACKET CRACKED. R & R RT WING LOWER OVERWING NR 2 ATTACH BRACKET IAW SRM 51-40-02.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 24,227 hrs · 20,245 cycles

CENTER OMEGA BEAM GUSSET CORRODED UNDER LAVATORY FLOOR, FWD OF CARBON CROSSBEAM. REMOVED CORRODED & INSTALLED SERVICEABLE CTR BEAM GUSSET IN LAVATORY IAW SRM 51-40-02.

Part: BLEED VALVE — FAILED (RT ENGINE) · airframe 24,126 hrs · 20,147 cycles

FROM REDUCING THRUST AT CRUISE FOR DECENT HEARD & FELT A LOUD BANG. FLIGHT ATTENDANT REPORTS LOUDEST IN CTR OF CABIN. ENGINE INDICATIONS ALL NORMAL DURING CRUISE, POSSIBLE COMPRESSOR STALL. TROUBLESHOT IAW FIM 72-00-00-810-817. R & R RT ENGINE 9TH STAGE VALVE IAW NRWC 931-SGF-01852. ACCOMPLISHED HIGH POWER RUNS, NO DEFECTS NOTED IAW RR MM 72-00-00-790-002.

Part: WIRE — BROKEN (NLG) · airframe 23,877 hrs · 19,923 cycles

RECEIVED AROUND 6 LOUD BANGS FROM THE NOSE AREA UNDER OUR FEET, DID NOT MATTER WHAT AIRSPEED WE WERE GOING. AS WE SLOWED DOWN AFTER THE FIRST BANG, SOUND LIKE WHAT A SPRING THAT BREAKS WOULD SOUND LIKE. DECLARED ON EMER & LOWERED THE LANDING GEAR & GOT THREE GREEN INDICATIONS & VISUAL CONFIRMATION OF GEAR DOWN FROM TOWER SO WE LANDED. FOUND WIRE W012-0001-22 BROKEN AT P0772 PIN A. RECONNECTED WIRE IAW SWPM CA 20-00-03. OPERATIONS CHECKED OK IAW AMM CH 32-63-05.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 23,568 hrs · 19,668 cycles

AFT EMER FLOOR LIGHTS INOPERATIVE. R & R NR 4 EMER LIGHT INVERTER IAW AMM 33-50-11.

Part: PITOT LINE — CONTAMINATED (PITOT/STATIC SYS) · airframe 23,249 hrs · 19,413 cycles

IAS, 8KIAS, DIFFERENCE DESCENDING THROUGH 31,000 FT. BOTH ALTITUDE & AIRSPEED WERE COMPLETELY ERRONEOUS, SHOWING DECREASING AIRSPEED TO 156 KTS WITH THRUST LEVERS IN DETENT, STANDBY WORKED NORMAL. DRAINED PITOT & STATIC 1 & 2 IAW AMM 34-13-00. ACCOMPLISHED PITOT & STATIC 1 & 2 LEAK CHECK IAW AMM 34-13-00. ACCOMPLISHED ADC 1 & 2 OPERATIONS CHECK IAW AMM 34-15-00, ALL CHECKED OK. ACFT IS RVSM ELIGIBLE, ACFT IS COMPLIANT FOR CONTINUED CAT II OPERATION.

Part: CABLE — OUT OF ADJUST (CABIN DOOR) · airframe 22,612 hrs · 18,907 cycles

MAIN CABIN DOOR WON’T OPEN FROM OUTSIDE. ADJUSTED REAR LOCK BOX CABLE IAW AMM 52-10-01.

Part: LAMP — UNSERVICEABLE (LANDING LIGHT) · airframe 21,343 hrs · 17,895 cycles

LEFT LANDING LIGHT BULB IS CRACKED. R & R LANDING LIGHT IAW AMM 33-42-01. OPS CHECKED GOOD.

Part: DOOR — BINDING (MAIN ENTRY) · airframe 21,338 hrs · 17,891 cycles

DURING B INSPECTION, FOUND MAIN DOOR GETS CAUGHT WHILE OPENING. ACFT REMOVED FROM SERVICE. FWD UPPER SWITCH TRIM COVER REMOVED. INSTALLED MAIN DOOR FWD SWITCH COVER OPS CHECKED GOOD IAW AMM 25-23-04 TASK I. (3).(C) AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 20,726 hrs · 17,383 cycles

DURING B INSPECTION FOUND THE LEFT HAND FORWARD OVERWING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. THE AIRCRAFT WAS REMOVED FROM SERVICE. C/A: REMOVED AND REPLACED THE LAMP IN THE FORWARD OVERWING EMERGENCY LIGHT ON FORWARD WING TO FUSELAGE FAIRING IAW EMB 145 AMM 33-50-10-000-801-A AND 33-50-10-400-801-A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: HOLDER — BROKEN (FLASHLIGHT) · airframe 20,526 hrs · 17,232 cycles

ON FLIGHT 3572 THE CREW REPORTED THE FLIGHT ATTENDANT FORWARD FLASHLIGHT HOLDER WAS BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FLIGHT ATTENDANT FORWARD FLASHLIGHT ASSEMBLY IAW AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: MECHANISM — LACK OF LUBE (PAX DOOR) · airframe 20,190 hrs · 16,962 cycles

DURING MAINTENANCE INSPECTION FOUND THE OUTSIDE PASSENGER MAIN DOOR HANDLE WOULD NOT OPEN DOOR. INSIDE HANDLE OPERATES NORMALLY. THE AIRCRAFT WAS REMOVED FROM SERVICE. LUBRICATED MAIN PAX DOOR ACTUATING AND LOCKING MECHANISM SYSTEM, REF EMB AMM 52-11-00. DOOR OPENS OK FROM OUTSIDE, REF EMB AMM 1 / 52-18-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FAN — INOPERATIVE (NR 1) · airframe 20,059 hrs · 16,864 cycles

ON FLIGHT 4234 THE CREW REPORTED A VERY STRONG ELECTRICAL BURNING ODOR IN THE COCKPIT AND FORWARD CABIN. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED FIM TASK 21-20-00-810-801-A. FOUND NR 1 RECIRCULATION FAN INOP. REMOVED AND REPLACED THE NR 1 RECIRCULATION FAN IAW EMB 145 AMM 21-24-01. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONTROLLER — FAULTY (WINDOW HEAT) · airframe 20,059 hrs · 16,864 cycles

ON FLIGHT 4281 THE CREW REPORTED THAT JUST PRIOR TO LANDING AII CREW MEMBERS BEGAN SMELLING A FAINT ABNORMAL ODOR. THE ODOR BECAME PROGRESSIVELY MORE PUNGENT AND WAS VERY STRONG. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 2 WINDSHIELD TEMP CONTROLLER IAW AMM 30-42-01. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,764 hrs · 16,623 cycles

DURING MAINTENANCE CHECK FOUND THE MAIN DOOR COURTESY LIGHT INOPERABLE. REMOVED AND REPLACED THE MAIN DOOR ENTRY COURTESY LIGHT FIXTURE. THE OPERATIONAL CHECK WAS GOOD IAW EMB AMM 33-26-04. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · airframe 19,499 hrs · 16,408 cycles

DURING MAINTENANCE INSPECTION FOUND THE CARGO DOOR SILL CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND INSTALLED NEW CARGO DOOR CENTER SILL IAW EMB SRM 51-40-02. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · airframe 19,499 hrs · 16,408 cycles

DURING MAINTENANCE INSPECTION FOUND THE SERVICE DOOR FORWARD SILL CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED SERVICE DOOR FORWARD SILL IAW EMB SRM 51-40-02. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SHEAR TIE — CORRODED (FRAME 65) · airframe 19,494 hrs · 16,402 cycles

FRAME 65 SHEAR TIE CORRODED. REPAIRED SHEAR TIE IAW AEA EO EM-53MR-1129.

Part: BATTERY — DISCHARGED (CABIN) · airframe 19,493 hrs · 16,402 cycles

DURING MAINTENANCE INSPECTION FOUND THE PROXIMITY FLOOR STRIP FAILED TO ILLUMINATE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY LIGHTING BATTERY. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETUNRED TO SERVICE.

Part: ISIS — MALFUNCTIONED (COCKPIT) · airframe 19,348 hrs · 19,348 cycles

ON FLIGHT 3329 THE CREW REPORTED THAT ON TAKEOFF HAD A RED FLAG ON THE INTEGRATED STANDBY INSTRUMENT SYSTEM (ISIS). THE INTEGRATED STANDBY INSTRUMENT SYSTEM (ISIS) WAS INOPERABLE. THE CREW RETURNED TO DFW. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. RESET ISIS, THE TEST WAS GOOD IAW AMM 34-01-01 AND NO FAULTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT ASSY — INOPERATIVE (FWD CABIN) · airframe 18,829 hrs · 15,813 cycles

FLIGHT 4312, THE CREW REPORTED THE FORWARD FLIGHT ATTENDANT FLASHLIGHT CRADLE WAS NOT INDICATING A CHARGING MODE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE FLASHLIGHT ASSEMBLY IAW AMM 33-50-16. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 18,609 hrs · 15,634 cycles

DURING MAINTENANCE INSPECTION, FOUND THE EMERGENCY FLOOR LIGHTING AFT OF SEAT ROW 12 IS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 4 EMERGENCY POWER SUPPLY UNIT (BATTERY AND CHARGER) IAW AMM 33-50-04. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 18,284 hrs · 15,371 cycles

ON FLIGHT 3971 THE CREW REPORTED THE CAPTAIN’S FLASHLIGHT WAS INOPERABLE. ITEM DEFERRED PER MEL 25-53. REMOVED AND REPLACED THE CAPTAIN'S FLASHLIGHT IAW EMB 145 AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD AT THIS TIME. MEL RESTORED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ELECTRONIC UNIT — MALFUNCTIONED (LANDING GEAR) · airframe 17,740 hrs · 14,946 cycles

ON FLIGHT 3946 DURING TAKEOFF THE CREW REPORTED THEY RECEIVED AN EICAS LANDING/GROUND AIR FAIL MESSAGE. THE CREW RAN THE CHECKLIST AND DECLARED AN EMERGENCY. THE CREW RETUNRED TO ORD AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. THE OPERATIONAL CHECK WAS GOOD ON ALL WEIGHT ON WHEELS PROXIMITY SENSORS IAW AMM 32-63-05. REMOVED AND REPLACED LANDING ELETRONIC GEAR UNIT IAW AMM 32-32-01. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,174 hrs · 21,334 cycles

DURING MAINTENANCE BASE VISIT FOUND THE EMERGENCY LIGHT IN CELING PANEL 243DLC TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED LIGHT BULB AT CELING PANEL 243DLC IAW EMB 145 AMM 33-50-08. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ANGLE — CRACKED (PAX DOOR) · airframe 14,660 hrs · 12,600 cycles

DURING MAINTENANCE BASE VISIT FOUND THE PASSENGER DOOR INNER HANDLE BOX HAS CRACKED ANGLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. STOP DRILLED CRACK AND FABRICATED REINFORCEMENT IAW EO EM-53-MR-250. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — OVERHEATED (MAIN) · airframe 12,830 hrs · 11,091 cycles

ON FLIGHT 3614 DURING CRUISE THE CREW REPORTED, RECEIVED A BATTERY OVERTEMP MESSAGE. THE BATTERY TEMPERATURE WENT TO 88 DEGREES CELSIUS. THE CREW DECLARED AN EMERGENCY AND ELECTED TO DIVERT TO RSW. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED BOTH MAIN BATTERIES IAW AMM 24-36-01. THE OPERATIONAL CHECK WAS GOOD AT THIS TIME AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: PRINTER — OVERHEATED (ACARS) · airframe 10,160 hrs · 8,706 cycles

ON FLIGHT 3815, DURING DESCENT CREW NOTED THE ACARS PRINTER OVERHEATED. CREW DECLARED A EMERGENCY AND LANDED WITHOUT INCIDENT, ISSUED MEL 23-6.

Part: PRINTER — OVERHEATED (ACARS) · airframe 10,160 hrs · 8,706 cycles

ON FLIGHT 3815, DURING DESCENT CREW NOTED THE ACARS PRINTER OVERHEATED. CREW DECLARED A EMERGENCY AND LANDED WITHOUT INCIDENT, ISSUED MEL 23-6. REMOVED AND REPLACED PRINTER AND OPS CHECKS GOOD IAW AMM 23-22-00 MEL RESTORED. ACFT RETURNED TO SERVICE.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 4,768 hrs · 4,346 cycles

LEFT OMEGA BEAM CORRODED AT FRAME 20. PERFORM CUTOUT OF CORROSION, FABRICATED AND INSTALLED REPAIR PARTS IAW EMB SRM 53-00-10. RETURNED AIRCRAFT TO SERVICE.

Part: FRAME — DAMAGED (ZONE 100) · airframe 4,768 hrs · 4,346 cycles

ADDITIONAL HOLE DRILLED DURING ACCOMPLISHMENT OF EMB SB 145-53-0068 AT FRAME 47 BETWEEN STRINGER 10L AND STRINGER 11L. FABRICATED AND INSTALLED REINFORCEMENT ON FRAME 47 BETWEEN STRINGER 10L AND 11L IAW EMB IC2007-145-02316. AIRCRAFT RETURNED TO SERVICE.

Part: UNKNOWN — UNKNOWN (SPOILERS) · airframe 4,460 hrs · 4,063 cycles

SPOILER FAILED, EMERGENCY DECLARED. PERFORMED SPOILER OPERATIONAL CHECK IAW EMB AMM 27-63-01 WITH NO DEFECTS NOTED, RETURNED AIRCRAFT TO SERVICE.

Part: SKIN — DENTED (FUSELAGE) · airframe 4,032 hrs · 3,671 cycles

FOUND DAMAGE TO LEFT RVSM AREA. REMOVED DAMAGE, PERFORMED NDT. FABRICATED FILLER AND DOUBLER AND INSTALLED IAW EMB IC2006-145/9588. PERFORMED REMAPPING OF RVSM AREA AND RETURNED AIRCRAFT TO SERVICE.

Part: SMOKE DETECTOR — MALFUNCTIONED

LAVATORY SMOKE EICAS MESSAGE CAME ON IMMEDIATELY AFTER TAKEOFF. PERFORMED ENGINE RUNS AND LAVATORY SMOKE DETECTOR TEST WITH OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (K)

Part: HINGE — CRACKED (VERT STAB)

LIT - UPON REMOVAL OF RUDDER ASSY, DURING HEAVY MAIN BASE VISIT, UPPER VERTICAL STABILIZER TO RUDDER HINGE HAD FATIGUE CRACKING AROUND THE CENTER LUG OF THE HINGE. REMOVED AND REPLACED HINGE.

Part: ENGINE — FAILED (LEFT)

BNA - FLT 4539 - PILOT REPORTS: ON TAKEOFF, THE LEFT ENGINE FAILED, CAPTAIN LOOKED OUT THE WINDOW AND VERIFIED FLAMES. CREW ABORTED TAKEOFF AND FIRED BOTTLES. UPON TAXIING BACK IN, CFR STOPPED THE A/C AND TOLD THEM THERE WERE STILL RESIDUAL FLAMES. PASSENGER DEPLANED ON THE RAMP WITH NO INJURIES.