N615AE

Part: NONE — NONE · airframe 48,858 hrs · 45,168 cycles

MEL 2532 - AUTH# 12-67M-C REPAIR REPAIR - POSITION AFT FA ATTENDANT EMERGENCY FLASHLIGHT/HOLDER AFT FA FLASHLIGHT BASE INOP PLACARDED -C/A-RAR F/A EMERGENCY FLASHLIGHT ASSY IAW ETN-EM-33-059. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED. MEL RESTORED.

Part: WARNING MESSAGE — ILLUMINATED (CARGO DOOR) · airframe 48,050 hrs · 44,270 cycles

ABORTED TAKE OFF (HIGH SPEED) 90KTS DUE CGO DOOR WARNING -BAGGAGE DOOR INDICATION AFTER ADVANCING THRUST LEVERS. HIGH SPEED ABORT, VERIFIED NO BRAKE OVERHEAT MSG.-C/A-FLIGHT CREW PLACARDED BAGGAGE DOOR INDICTION. MEL 52-05 AUTH# 060276-CMOC 222749

Part: CRADLE — BROKEN (AFT FLASHLIGHT) · airframe 47,875 hrs · 44,081 cycles

FA AFT EMERGENCY FLASHLIGHT RETENTION CLAMP BROKEN AUTH#050285M-C REFERENCE LOG PAGE #4709038 ITEM #2 FOR DISCREPENCY-C/A-RAR FA AFT EMERGENCY FLASHLIGHT ASSEMBLY IAW EMB 145 AMM 33-50-16. OPS CHECK GOOD. MEL ITEM RESTORED.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 47,700 hrs · 43,931 cycles

COCKPIT CEILING EMERGENCY LIGHT INOP-C/A-RAR COCKPIT CEILING EMERGENCY LIGHT LAMP IAW EMB 145 AMM 33-50-05. OPC GOOD

Part: LAMP — INOPERATIVE (EXTERIOR LIGHT) · airframe 47,678 hrs · 43,904 cycles

MAIN DOOR EXTERNAL EMERGENCY LIGHT INOP-C/A-RAR MAIN DOOR EXTERNAL EMERGENCY LIGHT LAMP IAW EMB AMM 33-50-10-000-801-A AND 33-50-10-400-801-A. OPC GOOD. END.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 47,678 hrs · 43,904 cycles

EMERGENCY FLOOR STRIPS 2 AND 3 INOP-C/A-RAR #2 BATTERY POWER SUPPLY AND #2 BATTERY IAW ENVOY WC 33-700-19. OPC GOOD. END.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,591 hrs · 43,814 cycles

COCKPIT UPPER SKIN CRACKED 2 CRACKS 1.5" IN LENGTH-C/A-INSTALLED DOUBLER/ TRIPLER PER ERS-EM-53MR-4302R

Part: LANDING GEAR — MALFUNCTIONED · airframe 47,420 hrs · 43,649 cycles

LANDING GEAR AIR FAIL MESSAGE UNABLE TO RETRACT IN ICING CONDITION.MESSAGE EXTINGUISHED 30 MINS. AFTER ILLUMINATED. EMERGENCY DECLARED.. THIS AIRCRAFT HAS BEEN INSPECTED TO THE EXTENT NECESSARY FOR A FERRY FLIGHT AND FOUND TO BE IN A SAFE CONDITION FOR A FERRY FLIGHT

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 46,867 hrs · 43,105 cycles

EMERGENCY EXIT AISLE CEILING LIGHT INOPERABLE. C/A RAR EMERGENCY EXIT AISLE CEILING LIGHT LAMP IAW EMB AMM 33-50-08-000-801-A AND 33-50-08-400-801-A. OPERATIONS CHECK GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION (BLEED 1) · airframe 46,788 hrs · 43,035 cycles

DURING CLIMB AROUND FL 180 PERFORMED THE PNEUMATIC ICE TEST AND RECEIVED BLEED 1 FAIL. DID NOT DECLARE EMERGENCY. SWAP A/C CONT. PERFORMED OPERATIONAL TEST OF AIR BLEED SYSTEM GOOD IAW AMM 36-00-00

Part: DOOR FRAME — CORRODED (FRAME 65) · airframe 46,711 hrs · 42,983 cycles

CARGO DOOR CUTOUT AT FR 65 CORRODED AROUND NUTPLATE BETWEEN STGR 13L-14L. PERFORMED PERMANENT REPAIR ON CARGO DOOR CUTOUT AT FR 65 BETWEEN STGR 13L-14L IAW ERS-EM-53MR-4139.

Part: SKIN — GOUGED (FUSELAGE) · airframe 46,711 hrs · 42,983 cycles

EXTERNAL FUSELAGE SKIN IS GOUGED BETWEEN FRAMES 74-75 AND STR 12L-13L. PERFORMED PERMANENT REPAIR ON LT FUSELAGE EXTERNAL SKIN BETWEEN FR 74-75 AND STR 12L-13L IAW ERS-EM-53MR-4132. REPAIR MATERIALS: DOUBLER AL2024-T3, 0.050 FILLER - AL2024-T3, 0.040.

Part: FRAME — CORRODED (FUSELAGE) · airframe 46,711 hrs · 42,983 cycles

FUSELAGE BAGGAGE DOOR LATERAL L-SHAPE AT FR 68 BETWEEN STGR 16L-17L CORRODED. REPAIRED FRAME 68 BETWEEN STGR 16L-17L IAW SRM 53-31-04. PART REPLACED: SHEAR CLIP PN 145-25369-603.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 46,711 hrs · 42,983 cycles

CARGO DOOR CUTOUT LOWER SILL CORRODED IN MULTIPLE AREAS. REMOVED AND REPLACED CARGO DOOR LOWER SILL IAW SRM 51-40-02. REPLACEMENT PART: SILL PN 145-25480-603SD.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 46,711 hrs · 42,983 cycles

FUSELAGE BAGGAGE DOOR LATERAL L-SHAPE AT FR 65 BETWEEN STR 16L-17L CORRODED. REMOVED AND REPLACED FR 65 SHEAR CLIP IAW SRM 53-31-04. REPLACEMENT PART: SHEAR CLIP, PN 145-25175-601.

Part: SKIN — CHAFED (FUSELAGE) · airframe 46,711 hrs · 42,983 cycles

FUSELAGE SKIN INSIDE RT PYLON ACCESS PANEL 424DB IS CHAFFED. REPAIRED FUSELAGE SKIN CHAFE INSIDE RT PYLON ACCESS PANEL 424DB IAW ERS-EM-53MR-4134 REV ORIGINAL.

Part: RIB — CRACKED (LT WING) · airframe 46,711 hrs · 42,983 cycles

LT WING RIB 21 IS CRACKED. REPAIRED LT WING RIB 21 CRACK IAW SRM 57-20-07, ITEM 4 REPAIR TO CRACK IN RIB 21. REPLACEMENT PARTS: FILLER: AL CLAD 2024 T3, DOUBLER: AL 7475 T761, SHIM: AL CLAD 2024 T.

Part: PROFILE — CORRODED (EMERGENCY EXIT) · airframe 46,711 hrs · 42,983 cycles

RT CABIN EMERGENCY EXIT LOWER EDGE FWD AND AFT PLASTIC GUIDE BLOCKS HAVE SURFACE CORROSION ON AND AROUND SHIMS. REMOVED AND REPLACED LOWER OUTER PROFILE ON RT EMERGENCY EXIT DOOR IAW SRM 51-20-03 AND 51-40-02. PART REPLACED 145-27696-001 PROFILE L.

Part: CONNECTOR — BROKEN (EMERGENCY LIGHT) · airframe 46,711 hrs · 42,983 cycles

EMERGENCY LIGHT STRIP 3 HAS BROKEN CONNECTOR. R & R THE CONNECTOR IAW SWPM 20-21-00, AND 20-50-00.

Part: CONNECTOR — BROKEN (EMERGENCY LIGHTS) · airframe 46,711 hrs · 42,983 cycles

EMERGENCY LIGHT STRIP #2 HAS BROKEN CONNECTOR. R & R THE CONNECTOR IAW SWPM 20-21-00, AND 20-50-00.

Part: HOUSING — OUT OF LIMITS (BEARING) · airframe 46,711 hrs · 42,983 cycles

LEFT AND RIGHT SPHERICAL BEARING HOUSINGS FOUND TO BE OUT OF LIMITS IAW SRM 55-30-02. REPAIRED THE SPHERICAL BEARING HOUSINGS IAW SRM 55-30-02.

Part: LIGHT — INOPERATIVE (GALLEY) · airframe 46,425 hrs · 42,685 cycles

GALLEY EMERGENCY LIGHT INOP-C/A-REMOVED AND REPLACED GALLEY EMERGENCY LIGHT IAW EMB AMM 33-50-09-000-801-A AND 33-50-09-400-801-A OPC GOOD END

Part: ENGINE — FAILED (NR 1) · airframe 46,407 hrs · 42,672 cycles

10,00'',300KTS OVER CHICAGO. NUMBER 1 ENGINE NOISE,EICAS E1 SHUT DOWN,OIL QTY ENGINE 1 IN AMBER AND 4QTS,RAN EPC CHECLIST.SMOKE IN CABIN AND COCKPIT,CFD INSPECTED ENGINE 1 AND FOLLOWED US TO GATE G19 WITHOUT FUTHER INCIDENT.-C/A-REPLACED #1 ENGINE IAW W/C 71-000-00 OPS CHECK LEAK CHECK GOOD.END. ACCOMPLISHED ETN-EM-72-034. NO FURTHER ENG ODER AT THIS TIME.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 46,213 hrs · 42,487 cycles

DURING PS-2 CHECK FOUND COURTESY LIGHT INOP AT GALLEY.-C/A-REMOVED AND REPLACED COURTESY LIGHT IAW EMB 145 AMM 33-26-05 OPS CHECK GOOD

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 46,072 hrs · 42,325 cycles

LH DOOR FWD EMERGENCY EXIT LIGHT INOP-C/A-RAR LH DOOR FWD EMERGENCY EXIT LIGHT LAMP IAW EMB AMM 33-50-10-000-801-A AND 33-50-10-400-801-A. OPC GOOD.

Part: LIGHT — INOPERATIVE (OVERWING EXIT) · airframe 45,498 hrs · 41,813 cycles

DURING PS-1 CHK FOUND RT OVERWING EMERGENCY LIGHT INOP. C/A-REMOVED AND REPLACED RT OVERWING EMERGENCY LIGHT BULB IAW AMM 33-50-10. OPS CHK GOOD.

Part: ACM — FAILED (AC BAY) · airframe 45,453 hrs · 41,760 cycles

PACK 1 OVERLOAD PACK 1 OVERHEAT HAPPENED ON GROUND THERE WAS A BURNING SMELL THAT WAS THERE FOR A SHORT TIME AT 2K FEET NO MESSAGES APPEARED. "TRANSFERRED TO NRWC 615-ORD-03102". C/A-FOUND LT ACM DAMAGE, REMOVED AND REPLACED OF LT ACM, OPS CHECK GOOD, AND ODOR EVENT ETN PERFORMED. NO ODORS NOTED. COMPLIED WITH EO EM-2100-048 AS REQUIRED DUE TO LT ACM R&R. REMOVED AND REPLACED #2 PACK VALVE Y-DUCT, CLAMPS AND HOSES BETWEEN DUAL TEMP CONTROL VALVE AND PACK VALVE IAW AMM 21-51-01 AND 21-60-01. IAW MM 21-51-01. OPS CHECK LEAK CHECK GOOD. REMOVED AND REPLACED DAMAGED LT CONDENSER/MIXER IAW AMM 21-51-04. OPS CHECK AND LEAK CHECK GOOD. PERFORMED ENGINE RUNS ETN-EM-72-034. NO ODORS NOTED. PACK PRESSURE REGULATOR P/N 816604-1 S/N 9807106. TUBE ASSY BLEED P/N 145-27547-409. CONDENSER/MIXER LT P/N 816650-1 S/N 9901051.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 45,415 hrs · 41,730 cycles

EMER. LIGHT WIRES BROKEN AT PANEL 251BF. SECURED WIRING CONNECTORS ON FLOOR PROXIMITY LIGHTS AT ROW 5/6 IAW AMM 33-50-12 OPS CHECK GOOD.

Part: SHUNT — FAILED (APU) · airframe 45,286 hrs · 41,605 cycles

APU FAILED ON START ATTEMPT, DURING TAXI IN WITH BOTH ENG RUNNING. REPAIRED APU SHUNT MOUNT IAW ERS-EM-53MR-3849. OPS CHECKED GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 45,271 hrs · 41,592 cycles

MAIN DOOR EXTERNAL EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPAIRED MAIN DOOR EXTERNAL EMERGENCY LIGHT LAMP IAW AMM 33-50-10-000-801-A, AND 33-50-10-400-801-A. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (SEATS 8&9) · airframe 44,932 hrs · 41,243 cycles

FLOOR PROX LIGHT STRIP BETWEEN SEAT 8 AND 9 INOP.-C/A-DEFERRED FLOOR PROX LGHT STRIP BETWEEN SEAT 8 AND 9. REMOVED AND REPLACED THE FLOOR PROX STRIP IAW EMB 145 AMM 33-50-12. OPS CHECK GOOD.

Part: LINE — LEAKING (HYD SYSTEM) · airframe 44,924 hrs · 41,232 cycles

CABIN HAD FUMES OF STINKY SOCKS AFTER LANDING PEOPLE EXITED THE AIRCRAFT COUGHING-C/A- INSPECTED FOUND HYDRAULIC LEAK IN EMERGENCY PARKING BRAKE LINE BETWEEN FR 38 AND FR 40. REMOVED AND REPLACED AFFECTED LINE IAW EMB 145 AMM 20-10-03. LEAK CHECK GOOD. PERFORMED ENGINE RUNS FOR STINKY SOCK SMELL IN CABIN IAW EMB 145 GHC AND ETN-EM-72-034 REV 10.

Part: NOT REPORTED — DAMAGED (FUSELAGE) · airframe 44,745 hrs · 41,077 cycles

RT SIDE RVSM CRITICAL AREA, 1" CREASE LEFT OF CENTER. "TRANSFERRED TO NRWC 615-ORD-02843". C/A- C/W ERS-EM-5300-3770. AC IS GOOD FOR RETURN TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (AFT CABIN) · airframe 44,646 hrs · 40,965 cycles

REAR FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED AFT CABIN EMERGENCY FLASH LIGHT IAW AMM 33-51-01. OPS CHECK GOOD.

Part: CONTROLLER — FAILED (CABIN PRESSURE) · airframe 44,645 hrs · 40,964 cycles

AIRCRAFT BEGAN TO LOOSE PRESSURAZATION DURING CLIMB CABIN ALTITTUDE CONTINUED TO INCREASE UNTIL CLIMB STOPPED DESCENT BEGAN-C/A-DEFERRED AUTO AND MANUAL PRESSURAZATION M PROCEDURES C/W REF MEL 21-19 AUTH 040646DM-C. TS IAW 21-31-00-810-801-A REMOVED AND REPLACED DIGITAL CONTROLLER IAW EMB145 21-31-01 PERFORMED FUNCTION TEST OF AUTO MODE IAW 21-31-00-700-802-A AND FUNCTION TEST OF MANUAL MODE IAW 21-31-00-700-801-A BOTH OPS CHECK GOOD MEL ITEM RESTORED REVERSED M PROCEDURES

Part: CONTROL UNIT — FAILED (HORIZ STAB) · airframe 44,416 hrs · 40,728 cycles

MAIN PTRIM INOP WARNING MESSAGE AFTER T/O TRYING TO TRIM NOSE DOWN. C/A-INTERROGATED CMC FOUND CORRELATED HSCU FAILURE MSG. REMOVED AND REPLACED HSCU IAW AMM 27-40-01. OPERATIONAL CHECK GOOD. FOUND NO OTHER PTRIM MSG'S. AIRCRAFT OK FOR SERVICE.

Part: FITTING — EXCESS PLAY (LT AILERON) · airframe 43,865 hrs · 40,200 cycles

LEFT HAND AILERON HAS PLAY AT PCA ATTACH POINT.-C/A-REMOVED AND REPLACED AILERON PCA/ACTUATOR FITTING IAW EO EM-27MR-112.

Part: BLANKING PLATE — LEAKING (CONDENSER MIXER) · airframe 42,651 hrs · 39,150 cycles

LOSS OF PRESSURIZATION AT ABOUT 19000 FT. REINSTALLED CLAMP AND BLANKING PLATE FOR THE NR 2 CONDENSER MIXER. PERFORMED AN OPS CHECK OF PRESSURIZATION CONTROL SYSTEM, NO FAULTS NOTED.

Part: DOOR SILL — CORRODED (CARGO BAY) · airframe 42,116 hrs · 38,690 cycles

SSI 53-30-07 CORROSION ON FRAMES AND SKIN AT LOWER FORWARD CARGO DOOR. R & R CARGO DOOR SILL AND SHEAR CLIP. SUPPORTING DOCUMENTS HAVE BEEN SENT TO [email protected] WITH THE SUBJECT: 615AE SDR # RAIA201710310001 WITH THE SUBJECT: 615AE SDR # RAIA201710310001

Part: SKIN — DAMAGED (FRAME 67) · airframe 42,116 hrs · 38,690 cycles

SSI 53-30-07 EXTERNAL FUSELAGE SKIN PROTRUDED AND HAS NUMEROUS FASTNER HEADS PULLING THROUGH SKIN FR 67 STRINGER 20L THROUGH 19R. REMOVED AND INSTALLED SKIN AT SKIN FR 67 STRINGER 20L THROUGH 19R. SUPPORTING DOCUMENTS HAVE BEEN SENT TO [email protected] WITH THE SUBJECT: 615AE SDR # RAIA201710270001 TO [email protected] WITH THE SUBJECT: 615AE SDR # RAIA201710270001

Part: SKIN — CRACKED (FRAME 75) · airframe 42,116 hrs · 38,690 cycles

RH AFT FUSELAGE FR 75 HAS A SKIN CRACKE ABOVE STR 2R, MARKED. REPAIRED RH AFT FUSELAGE SKIN CRACK AT FR 75 ABOVE STR 2R. SUPPORTING DOCUMENTS HAVE BEEN SENT TO [email protected] WITH THE SUBJECT: 615AE SDR # RAIA201710270001 TO [email protected] WITH THE SUBJECT: 615AE SDR # RAIA201710270002

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 40,130 hrs · 36,974 cycles

CEILING EMERGENCY LIGHT AT PAX DOOR ENTRANCE IS INOPERATIVE. REMOVED AND REPLACED CEILING EMERGENCY LIGHT BULB, OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EXTERIOR LIGHT) · airframe 39,418 hrs · 36,391 cycles

SERVICE DOOR EXTERIOR FLOOD LIGHT NR 2 INOPERATIVE. R & R SERVICE DOOR EXTERIOR FLOOD LIGHT BULB. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,341 hrs · 20,557 cycles

SERVICE DOOR EMERGENCY LIGHT NR 2 INOPERATIVE. R & R SEVICE DOOR EMERGENCY FLOOD LIGHT NR 2. OPS CHECK GOOD.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 35,341 hrs · 20,557 cycles

PAX DOOR EMERGENCY FLOOD LIGHT NR 1 INOPERATIVE. R & R EMERGENCY BATTERY POWER SUPPLY. OPS CHECK GOOD.

Part: RUDDER — BINDING · airframe 38,484 hrs · 35,640 cycles

RUDDER JAMMED IN FLIGHT. MAINTENANCE PERFORMED CABLE TENSIONS, NO DEFECTS NOTED. MAINTENANCE INSPECTED CABLE SYSTEM, NO DEFECTS NOTED. OK FOR SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 38,445 hrs · 35,607 cycles

NUMBER 2 EMER BATTERY & CHARGER INOPERATIVE. R & R NR 2 EMER BATTERY & CHARGER IAW AMM 33-50-04. OPERATIONS CHECKED GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 38,445 hrs · 35,607 cycles

NUMBER 1 EMER BATTERY & CHARGER INOPERATIVE. R & R NR 1 EMER BATTERY & CHARGER IAW AMM 33-50-04. OPERATIONS CHECKED GOOD.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 38,445 hrs · 35,607 cycles

LIGHTNING STRIKE AFT OF FRAME 5 JUST ABOVE STRINGER 13R. REPAIRED LIGHTNING STRIKE IAW ERS-EM-53MR-1558.

Part: SPAR — CRACKED (LT WING) · airframe 38,445 hrs · 35,607 cycles

LEFT WING SPAR I LE LOWER ATTACHMENT FLANGE IS CRACKED AT RIB 9. REPAIRED LT WING SPAR I LE LOWER ATTACHMENT FLANGE AT RIB 9 IAW ERS-EM-57MR-495.

Part: BATTERY — DISCHARGED (CABIN) · airframe 38,445 hrs · 35,607 cycles

NUMBER 4 EMER BATTERY & CHARGER INOPERATIVE. R & R NR 4 EMER BATTERY & CHARGER IAW AMM 33-50-04. OPERATIONS CHECKED GOOD.

Part: SKIN — CRACKED (FUSELAGE) · airframe 38,444 hrs · 35,605 cycles

LEFT REAR FUSELAGE I SKIN CRACKS AT FRAME 75, BETWEEN STRINGERS 1L & 3L. PERFORMED PERMANENT REPAIR OF LT REAR FUSELAGE I SKIN AT FRAME 75 BELOW STRINGER 2L IAW ERS-EM-53MR-1533.

Part: FRAME — CORRODED (FUSELAGE) · airframe 38,444 hrs · 35,605 cycles

FRAME 22 HAS CORROSION ABOUT 3 INCHES ABOVE SERVICE DOOR SILL. REPAIRED FRAME 22 ABOVE SERVICE DOOR SILL IAW ERS-EM-53MR-1526.

Part: MOUNT — CRACKED (RT ENGINE) · airframe 38,444 hrs · 35,605 cycles

RIGHT ENGINE FORWARD YOLK CRACKED, LOWER FORWARD CORNER. REMOVED & INSTALLED SERVICEABLE YOKE IAW EO EM-54MR-386.

Part: MOUNT — CRACKED (LT ENGINE) · airframe 38,444 hrs · 35,605 cycles

LEFT ENGINE FORWARD YOLK CRACKED, LOWER FORWARD CORNER. REMOVED & INSTALLED SERVICEABLE YOKE IAW EO EM-54MR-386.

Part: YOKE — CRACKED (RT ENGINE) · airframe 38,444 hrs · 35,605 cycles

RIGHT ENG FWD YOKE CRACKED, LOWER FWD CORNER. R & R RT ENG FWD YOKE IAW EO-EM-54MR-386.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHT) · airframe 38,444 hrs · 35,605 cycles

ELECTRICAL CONNECTOR P8563 TO THE LT EXTERIOR OVERWING EMER LIGHT HAS A DAMAGED HEAT SHRINK BOOT. R & R HEAT SHRINK BOOT AT ELEC CONNECTOR P8563 TO THE LT EXTERIOR OVERWING EMER LIGHT IAW SWPM 20-50-00 STEP 17.

Part: BATTERY — DISCHARGED (CABIN) · airframe 38,444 hrs · 35,605 cycles

NUMBER 4 EMER BATTERY & CHARGER INOPERATIVE. R & R NR 4 EMER BATTERY & CHARGER IAW AMM 33-50-04. OPERATIONS CHECKED GOOD.

Part: BATTERY — UNKNOWN (CABIN) · airframe 38,444 hrs · 35,605 cycles

A3265 R & R EMER LIGHTING BATTERY ASSEMBLY & BATTERY CHARGER NR 1 IAW WC 33-700-19, WC 33-002 & SN109808.

Part: BATTERY — DISCHARGED (CABIN) · airframe 38,444 hrs · 35,605 cycles

NUMBER 2 EMER BATTERY & CHARGER INOPERATIVE. R & R NR 2 EMER BATTERY & CHARGER IAW AMM 33-50-04. OPERATIONS CHECKED GOOD.

Part: TRANSCEIVER — FAILED (WEATHER RADAR) · airframe 38,207 hrs · 35,404 cycles

TURNED ON WX RADAR IN FLIGHT & TILT APPEARS TO NOT BE FUNCTIONING. RADAR PAINTING WIDE YELLOW & RED BAND LIKE POINTED AT GND AT ALL TILT VALUES. KNOWN CELL 30 MI FROM ACFT, WOULD NOT SHOW UP ON RADAR DISPLAY. R & R WX RADAR RTA ASSEMBLY IAW AMM 34-42-01. OPERATIONS CHECKED GOOD.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT) · airframe 38,145 hrs · 35,355 cycles

RIGHT EXTERNAL OVERWING EMER LIGHT INOPERATIVE. R & R RT EXTERNAL OVERWING EMER LAMP IAW TASK 33-50-07-000-801-A & TASK 33-50-07-400-801-A. OPERATIONS CHECKED, NO GOOD. AFTER PERFORMING TASK 33-50-07-000-802-A, FOUND CONNECTOR TO BE UNPLUGGED, PLUGGED IN CONNECTOR. PERFORMED TASK 33-50-07-400-802-A. OPERATIONS CHECKED GOOD.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 38,116 hrs · 35,321 cycles

RIGHT OVER THE WING EMER LIGHT INOPERATIVE. FOUND CONNECTOR OFF LIGHT CONNECTION. REINSTALLED CONNECTOR IAW AMM 33-50-10. OPERATIONS CHECKED GOOD.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 38,045 hrs · 35,245 cycles

RIGHT OVERWING EMER LIGHT IS INOPERATIVE. FOUND CONNECTOR IN BACK OF LIGHT ASSEMBLY TO BE DISCONNECTED, RECONNECTED IT AS REQUIRED. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 37,721 hrs · 34,961 cycles

RIGHT AFT EXTERIOR EMER LIGHT ON FUSELAGE INOPERATIVE. R & R LIGHT BULB ON RT AFT EXTERIOR EMER LIGHT IAW AMM 33-50-10. OPERATIONS CHECKED GOOD.

Part: MODULE — INOPERATIVE (CABIN) · airframe 37,700 hrs · 34,939 cycles

WHILE PERFORMING WC 33-700-17, EMER LIGHTING SYS OPERATIONAL CHECK. EMER LIGHTS DO NOT COME ON. SEE WORK PERFORMED ON TURNOVER THIS NRWC. R & R MODULE ASSEMBLY IAW 2O-13-10. OPERATIONAL CHECKED GOOD IAW WORK CARD 33-700-17. RELAY PN REBC410J-2000CB.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 37,334 hrs · 34,568 cycles

FLASHLIGHT BY FLIGHT ATTENDANT SEAT IS INOPERATIVE. DEFERRED IAW MEL 25-53. MX PROCEDURES COMPLIED WITH. R & R FLASHLIGHT IAW AMM 33-50-16. MEL RESTORED & PLACARDS REMOVED.

Part: LIGHT — INOPERATIVE (OVERWING EXIT) · airframe 37,158 hrs · 34,411 cycles

RIGHT OVERWING EMER LIGHT INOPERATIVE. REMOVED & REINSTALLED RT OVERWING EMER LIGHT IAW AMM 33-50-10. OPERATIONS CHECKED GOOD.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 37,158 hrs · 34,411 cycles

RIGHT LOWER EMER EXIT LIGHT INOPERATIVE. R & R RT NR 5 INVERTER IAW AMM 33-50-11.

Part: CONNECTOR — BURNED (COFFEEMAKER) · airframe 37,101 hrs · 34,362 cycles

ELECTRICAL ODOR IN COCKPIT & FWD GALLEY APU WAS RUNNING, GPU WAS CONNECTED BUT NOT SELECTED, BOTH BATTERIES OFF PACKS OFF & NO GROUND AIR. R & R NR 1 COFFEE JUG CONNECTOR, OPS CHECKED GOOD IAW CMM 25-32-94 STEPS 2A2 AND 2A11.

Part: CRADLE — BROKEN (FLASHLIGHT) · airframe 36,454 hrs · 33,724 cycles

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

Part: ACTUATOR — DIRTY (CABIN DOOR) · airframe 36,313 hrs · 33,582 cycles

MAIN CABIN DOOR DIFFICULT TO OPERATE. CLEAN & LUBE DOOR ACTUATOR ASSEMBLY ON MAIN DOOR. OPERATIONS CHECKED GOOD IAW AMM 52-18-00-600-801A.

Part: TIRE — SEPARATED (MLG) · airframe 36,180 hrs · 33,471 cycles

NUMBER 3 TIRE MLG TIRE HAD 175 PSI UPON REMOVAL & NR 4 MAIN TIRE HAD 173 PSI IAW ITEM NR 2 LG PG 3529059 NR 3 MLG TIRE TREAD SEPARATED. R & R NR 3 MLG TIRE & WHEEL ASSEMBLY IAW AEAI MNTC HUB CAP ASSEMBLY PN 118-145.

Part: BATTERY — DISCHARGED (CABIN) · airframe 36,042 hrs · 33,345 cycles

DURING PS 1, FOUND LT & RT REAR OVERWING EMER LIGHTS INOPERATIVE. R & R EMER LIGHT BATTERY & BATTERY CHARGER NR 4 IAW 33-50-04. OPERATIONS CHECKED GOOD. CHARGER ASSEMBLY BATTERY PN BA5-0933-901 & SN C01829.

Part: CRADLE — BROKEN (FLASHLIGHT) · airframe 35,299 hrs · 32,669 cycles

AFT CABIN EMERGENCY FLASHLIGHT CRADLE BROKEN. R & R AFT CABIN EMERGENCY FLASHLIGHT CRADLE IAW AMM TASK 33-50-16-000-801-A & 33-50-16-400-801-A. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 35,045 hrs · 32,465 cycles

LEFT FWD OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. R & R LT FWD OVERWING EXTERNAL EMERGENCY EXIT LIGHT ASSEMBLY IAW AMM 33-50-10, OPERATIONS CHECKED GOOD.

Part: FLASHLIGHT — DEFECTIVE (COCKPIT) · airframe 35,032 hrs · 32,452 cycles

ELECTRICAL BURN SMELL COMING FROM CAPTAIN`S FLASHLIGHT. R & R CAPTAIN`S FLASHLIGHT IAW 33-50-10.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,648 hrs · 32,148 cycles

AFT CABIN CEILING EMERGENCY LAMP INOPERATIVE. R & R AFT CABIN CEILING EMERGENCY LIGHT LAMP IAW EMB AMM 33-50-08-000-801-A & 33-50-08-400-801-A. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (RT WING) · airframe 34,638 hrs · 32,134 cycles

RIGHT WING UPPER EMERGENCY LIGHT INOPERATIVE. R & R RT WING UPPER EMERGENCY LIGHT BULB IAW EMB AMM 33-50-10. OPERATIONS CHECKED GOOD IAW AE WC 33-700-17.

Part: RIB — CRACKED (LT WING) · airframe 34,200 hrs · 31,782 cycles

DURING HMBV INSPECTION, QC FOUND LT WING RIB 5 CRACKED. ACFT WAS REMOVED FROM SERVICE. R & R LT RIB 5 IAW EO EM-57MR-594.

Part: FRAME — CORRODED (FUSELAGE) · airframe 34,200 hrs · 31,782 cycles

DURING HMBV INSPECTION, FOUND FRAME 65 ZEE FRAME CORRODED AROUND LOWER NUTPLATE HOLE ON LT SIDE. ACFT REMOVED FROM SERVICE. PERFORMED PERMANENT REPAIR ON FRAME 65 IAW EO-EM-53MR-2199.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 34,200 hrs · 31,782 cycles

SERVICE DOOR LWR EMERGENCY EXIT LIGHT INOPERATIVE. R & R SERVICE DOOR EMERGENCY EXIT IDENTIFIER LIGHT IAW AMM 33-50-13, REPAIRED BROKEN WIRE W192-8628-22 ON SERVICE DOOR EMERGENCY EXIT IDENTIFIER IAW SWPM 20-21-00. OPS CHECKED GOOD.

Part: SPAR — CRACKED (RT WING) · airframe 34,200 hrs · 31,782 cycles

RT WING SPAR III HAS POSSIBLE CRACKS BETWEEN RIBS 3 AND RIB 4. UPON FURTHER INVESTIGATION, NO CRACK FOUND ON RT SPAR III, ACCOMPLISHED LT WING SPAR III REPAIR BETWEEN RIBS 3 AND 4 IAW EO EM-57MR-710 R1. WIP/TURNOVER'S FOR DETAILS.

Part: RIB — CRACKED (LT WING) · airframe 34,200 hrs · 31,782 cycles

LT WING RIB 5 CRACKED. ACCOMPLISHED EO-EM-57MR-594R1. R & R OF LT WING RIB.

Part: SKIN — CORRODED (CARGO CUTOUT) · airframe 34,200 hrs · 31,782 cycles

CARGO DOOR CUT-OUT LOWER INTERNAL STRUCTURE CORRODED AT FWD LOWER CORNER. REPAIRED THE CARGO DOOR CUT-OUT LOWER INTERNAL STRUCTURE AT FWD LOWER CORNER IAW EO EM-53MR-1129, PART A.

Part: SHEAR TIE — CORRODED (FUELAGE) · airframe 34,200 hrs · 31,782 cycles

SHEAR TIE ON FR 68, AFT OF LOWER CARGO DOOR CUTOUT CORRODED. REPAIRED SHEAR TIE ON FR 68 AFT OF LOWER CARGO DOOR CUT OUT IAW EO EM-53MR-1129, PART B.

Part: MOUNT — CRACKED (EMERGENCY LIGHT) · airframe 34,200 hrs · 31,782 cycles

FOUR PROXIMITY LIGHT HOLDER CRACKED AND THREE RT FLOOR TRIM CRACKED. R & R IAW AMM 33-50-12.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT) · airframe 33,896 hrs · 31,532 cycles

RT OVERWING EMERGENCY LIGHT NOT WORKING. CONNECTED THE ELECTRICAL CONNECTOR TO THE EMERGENCY LIGHT ASSY. OP'S CHECKED GOOD IAW AMM 33-50-10.

Part: LIGHT — MISINSTALLED (RT OVERWING) · airframe 33,812 hrs · 31,471 cycles

CREW REPORTED THE EXTERIOR EMERGENCY EXIT LIGHT WAS INSTALLED UPSIDE DOWN. ACFT REMOVED FROM SERVICE. INSTALLED RT OVERWING EMERGENCY LIGHT IAW AMM 33-50-10. OPS CHECKED GOOD. ACFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,678 hrs · 31,365 cycles

DURING MX INSPECTION, FOUND EMERGENCY LIGHT AT SEATS 1A & 2A INOPERATIVE. ACFT REMOVED FROM SERVICE. R & R LIGHT IAW MM 33-50-12. OPS CHECKED GOOD. ACFT RETURNED TO SERVICE.

Part: FLASHLIGHT — FAULTY (COCKPIT) · airframe 33,422 hrs · 31,163 cycles

DURING B-INSPECTION, FOUND THE CAPTAIN’S FLASHLIGHT NOT CHARGING. THE ACFT WAS REMOVED FROM SERVICE. R & R THE CAPTAIN’S FLASHLIGHT ASSY IAW AMM 33-50-16-000 801-A AND 33-50-16-400-801-A. THE OPS CHECK WAS GOOD. NO DEFECTS NOTED AT THIS TIME. THE ACFT WAS RETURNED TO SERVICE.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 33,015 hrs · 30,838 cycles

DURING MAINTENANCE INSPECTION FOUND THE EMERGENCY FLOOR LIGHTS FROM ROW 12-18 FAILED AFTER A FEW SECONDS. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED BATTERY POWER SUPPLY NR 4 IAW EMB 145 AMM 33-50-04. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 32,781 hrs · 30,652 cycles

WHILE PERFORMING PS1 FOUND THE LEFT OVERWING EXIT EMERGENCY SIGN NOT ILLUMINATED DURING TEST (INTERIOR}. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 4 POWER INVERTER IAW EMB MM 33-50-11. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: TUBE — DEFECTIVE (BLEED AIR SYS) · airframe 32,268 hrs · 30,244 cycles

ON FLIGHT 4285 DURING THE CLIMB THE CREW RECEIVED A BLEED LEEK MESSAGE ON EICAS. THE CREW COMPLIED WITH AOM VOL 1 PROCEDURES. THEY CONTACTED DISPATCH AND ELECTED TO DIVERT TO RDU. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED O-RINGS AT JOINT 19. REMOVED AND REPLACED TUBE ASSEMBLY BELOW JOINT 19. PERFORMED AIR BLEED SYSTEM OPERATIONAL CHECK IAW EMB AMM 36-00-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,944 hrs · 29,965 cycles

DURING B INSPECTION FOUND THE AISLE CEILING EMERGENCY LIGHT AT ROW 3ABC INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AISLE CEILING EMERGENCY LIGHT LAMP AT ROW 3ABC IAW EMB 145 AMM 33-50-08. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ENGINE — SHUTDOWN (NR 2) · airframe 31,440 hrs · 29,557 cycles

ON FLIGHT 3563, ENGINE 2 UNCOMMANDED SHUTDOWN AT FL370 FLIGHT ATTENDANT NOTED HEARING A BANG NOISE AT SHUTDOWN. DECLARED AN EMERGENCY AND DIVERTED. LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 2 ENGINE IAW W/C 71-000-00. THE OPS AND LEAK CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,253 hrs · 28,645 cycles

DURING B-INSPECTION FOUND THE AISLE CEILING PANEL EMERGENCY LIGHT AT ROW 3 TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AISLE CEILING PANEL EMERGENCY LIGHT LAMP AT ROW 3 IAW EMB 145 AMM 33-50-08. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 29,997 hrs · 28,454 cycles

DURING B-INSPECTION FOUND THE LEFT AND RIGHT OVERWING EMERGENCY LIGHTS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 4 EMERGENCY BATTERY AND BATTERY CHARGER ASSEMBLY IAW EMB AMM 33-50-04. THE OPERATIONAL CHECK WAS GOOD IAW WC 33-700-17. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 29,804 hrs · 28,314 cycles

DURING MAINTENANCE BASE INSPECTION FOUND BOTH LEFT AND RIGHT OVERWING EMERGENCY LIGHTS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 4 EMERGENCY LIGHT BATTERY AND BATTERY CHARGER IAW EMB 145 AMM 33-50-04. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,768 hrs · 28,285 cycles

DURING MAINTENANCE INSPECTION FOUND THE LEFT AND RIGHT OVERWING EMERGENCY LIGHTS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 4 EMERGENCY POWER SUPPLY UNIT IAW EMB 145 AMM 33-50-04. REMOVED AND REPLACED THE RIGHT OVERWING LIGHT LAMP IAW EMB 145 AMM 33-50-01. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,663 hrs · 28,214 cycles

RT AFT OVERWING EMERGENCY LIGHT INOP. REMOVED AND REPLACED RT AFT OVERWING EMERGENCY LIGHT LAMP IAW EMB AMM 33-50-10. OPS CHECKS GOOD IAW EMB AMM 33-50-00.

Part: RIB — CRACKED (RT WING) · airframe 29,605 hrs · 28,165 cycles

DURING MAINTENANCE BASE VISIT FOUND THE RIGHT WING 5 CRACKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. COMPLIED WITH AEA EO EM-57MR-595. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ACCESS PANEL — CRACKED (FUSELAGE) · airframe 29,605 hrs · 28,165 cycles

DURING MAINTENANCE BASE VISIT FOUND ACCESS PANEL 272DR UPPER FRAME CRACKED UNDER RETAINING RING. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED DOOR IAW EO EM-52MR-298. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ACM — INOPERATIVE (NR 1) · airframe 29,432 hrs · 28,040 cycles

FOR FLIGHT 3520 MAINTENANCE REPORTED SMOKE IN THE COCKPIT WITH PACK NR 1 RUNNING ON THE APU. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED NR 1 PACK (AIR CYCLE MACHINE) IAW AMM 21-51-03. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SMOKE DETECTOR — FALSE ACTIVATION (CARGO BAY) · airframe 29,216 hrs · 27,883 cycles

ON FLIGHT 3308 THE CREW REPORTED THAT RECEIVED A BAGGAGE SMOKE WARNING MESSAGE ON SHORT FINAL BEFORE LANDING. FOLLOWED EPC PROCEDURES AND DISCHARGED BAGGAGE EXTINGUISHER. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED FWD AND AFT BAGGAGE SMOKE DETECTORS IAW EMB 145 M/M 26-15-01. THE OPERATIONAL CHECK WAS GOOD. REMOVED AND REPLACED THE BAGGAGE COMPARTMENT FIRE EXTINGUSHER BOTTLES IN REF TO 26-23-01 AMM. PART NUMBERS: M30903870, M30903870, 346000731 AND 337000271. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SWITCH — INOPERATIVE (FLASHLIGHT) · airframe 31,329 hrs · 29,479 cycles

FLIGHT 4244, CREW REPORTED THE ON/OFF SWITCH WAS BROKEN ON THE FLASHLIGHT BEHIND THE CAPTAIN’S SEAT. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED FLASHLIGHT IAW 33-50-16. AIRCRAFT RETURNED TO SERVICE.

Part: HANDLE — LOOSE (MAIN DOOR) · airframe 28,735 hrs · 27,521 cycles

ON FLIGHT 4393 THE FLIGHT ATTENDANT REPORTED THE MAIN DOOR WAS DIFFICULT TO CLOSE. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND THE INTERNAL DOOR HANDLE LOOSE- RE-INSTALLED HANDLE AS PER EMB145AMM 52-18-05. THE OPERATIONAL CHECK WAS GOOD PER 52-18-00-820-801-A. NO PARTS REMOVED OR REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — FAILED (EMERGENCY LIGHTS) · airframe 28,490 hrs · 27,343 cycles

FOR FLIGHT 3468, DURING THE PREFLIGHT INSP FOUND BOTH LT AND RT EXTERIOR OVERWING LIGHTS AND INTERIOR EMERGENCY EXIT LIGHTS AT ROW 12 TO BE INOPERABLE. THE ACFT WAS REMOVED FROM SERVICE. TROUBLESHOT SYS. FOUND NR3 EMERGENCY LIGHT BATTERY TO BE FAULTY. REPLACED NR3 BATTERY IAW AMM 33-50-04. THE OPS CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: ECU — MALFUNCTIONED (TE FLAP) · airframe 28,449 hrs · 27,310 cycles

ON FLIGHT 2819 THE CREW REPORTED DURING THE DESCENT THE FLAP FAILED IN REACHING NINE DEGREES. THE CAPTAIN DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. TROUBLESHOT IAW FIM TASK 27-51-00-810-801-A. REPLACED THE FLAP ELECTRONIC CONTROL UNIT (FECU) IAW AMM 27-53-00. THE OPERATIONAL CHECK WAS GOOD IAW AMM 27-51-00-700-801-A. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (COCKPIT & CABIN) · airframe 27,929 hrs · 26,925 cycles

ON FLIGHT 4278 THE CREW REPORTED THAT DURING THE CLIMBOUT WHILE DOING AN ANTI-ICE TEST, HAD A BURNING ODOR IN THE COCKPIT AND CABIN. THE CREW CONTINUED ON TO ORD AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. GROUND RAN ENGINES IAW ETN EM-72-034 R4, NO SMELLS, SMOKE OR DEFECTS NOTED AT THIS TIME. NO PARTS REMOVED OR REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SWITCH — DEFECTIVE (HORIZ STAB) · airframe 26,994 hrs · 26,217 cycles

ON FLIGHT 3393 DURING THE CLIMB (DURING A TEST AT FLIGHT LEVEL 210) DISPATCH REPORTED THE AIRCRAFT WAS RETURNING WITH A STABILIZER ANTI ICE FAIL EICAS MESSAGE ON THE OVERHEAD PANEL. WEATHER WAS NOT AN ISSUE. THE CAPTAIN ELECTED TO RETURN TO DFW. THE AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED THE STABILIZER TEMPERATURE SWITCH (OVERHEAT) HORIZONTAL) AT THE LEFT LEADING EDGE WITH REF TO AMM 30-12-05. THE OPERATIONAL CHECK WAS GOOD AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE — BROKEN (CABIN) · airframe 24,674 hrs · 24,416 cycles

DURING MAINTENANCE CHECK, FOUND THE NR 1 EMERGENCY FLOOR LIGHT STRIP TO HAVE A BROKEN WIRE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED BROKEN WIRE ON THE NR 1 EMERGENCY LIGHT STRIP BY INSTALLING SERVICEABLE CONNECTOR IAW EMB 145 AWM 20-10-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,674 hrs · 24,416 cycles

DURING MAINTENANCE BASE VISIT CORROSION WAS FOUND ON THE FORWARD FUSELAGE II LOWER SKIN, CENTER FUSELAGE LOWER SKIN AND FRAME 12. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED DAMAGE IAW EO EM-53MR-1447. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: DOOR FRAME — CRACKED (CARGO BAY) · airframe 24,674 hrs · 24,416 cycles

DURING THE MAINTENANCE BASE VISIT FOUND THAT THE BAGGAGE DOOR FRAME WAS BENT AND THE LOWER FORWARD CORNER WAS CRACKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FRAME (CONTINUOUS STOP) IAW EMB SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SKIN — TORN (EVELAVTOR) · airframe 24,674 hrs · 24,416 cycles

DURING MAINTENANCE BASE VISIT FOUND THE LEFT ELEVATOR TIP LOWER AFT MOUNTING POINT HAS BEEN WORN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED THE TORN SKIN IAW AEA EO EM-53MR-3321. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,674 hrs · 24,416 cycles

DURING MAINTENANCE BASE INSPECTION FOUND THE LAVATORY CENTER BEAM GUSSET CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPLACED THE LAVATORY CENTER BEAM GUSSET WITH SERVICEABLE GUSSET IAW EMB SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,674 hrs · 24,416 cycles

DURING MAINTENANCE BASE INSPECTION FOUND THE LAVATORY RIGHT BEAM GUSSET TO BE CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED THE LAVATORY RIGHT BEAM GUSSET AND INSTALLED SERVICEABLE GUSSET IAW EMB SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,674 hrs · 24,416 cycles

DURING THE MAINTENANCE BASE VISIT FOUND THE CARGO DOOR LOWER SILL TO BE CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. BLENDED OUT CORROSION IAW EMB 145 51-103 AND DETERMINED TO BE WITHIN ALLOWABLE LIMITS IAW ETA-EM-5300-977. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SUPPORT — CORRODED (BS 3770-4154) · corrosion level 2 · airframe 24,674 hrs · 24,416 cycles

DURING THE MAINTENANCE BASE HEAVY CHECK FOUND THE RIGHT SIDE WEB CORRODED UNDER THE AILERON TORQUE TUBE BETWEEN FRAME 12 AND FRAME 13 AT STRINGER 21 RIGHT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND INSTALLED NEW WEB BETWEEN FRAME 12 AND 13, IAW SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,674 hrs · 24,416 cycles

DURING MAINTENANCE BASE CHECK FOUND THE RIGHT 21 STRINGER TO BE CORRODED BETWEEN FRAME 12 AND FRAME 13. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND INSTALLED NEW STRINGER 21R BETWEEN FRAME 12 AND FRAME 13 IAW SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: UNKNOWN — SMOKE (EXTERIOR) · airframe 23,817 hrs · 23,561 cycles

ON FLIGHT 3596 CREW HEARD A VERY LOUD NOISE FROM BACK OF AIRCRAFT AND NOTED VISIBLE SMOKE OUTSIDE. SMOKE FUMES IN CABIN AND COCKPIT. CREW COULD NOT DETERMINE IF IT WAS AUXILIARY POWER UNIT OR PASSENGER PACK. ISSUED MEL.

Part: ACM — MALFUNCTIONED (AC BAY) · airframe 23,817 hrs · 23,561 cycles

REMOVED AND REPLACED AN AIR CYCLE MACHINE. AIRCRAFT RETURNED TO SERVICE.

Part: CARBON SEAL — WORN (RT ENGINE) · airframe 22,679 hrs · 22,616 cycles

ON FLIGHT 4041 CREW REPORTED, DURING CLIMB LAV SMOKE. LAST 2 MINUTES FLIGHT ATTENDANT REPORTED OIL SMELL. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED RIGHT ENGINE IAW W/C 71-000-00. PERFORMED OPERATIONAL CHECK. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 22,697 hrs · 22,616 cycles

ON FLIGHT 4041 - CREW REPORTED DURING CLIMB LAV SMOKE LAST 2 MIN FA REPORTED OIL SMELL.

Part: CONTROLLER — FAILED (CABIN PRESSURE) · airframe 19,897 hrs · 19,872 cycles

AT 36000 CABIN ALTITUDE BEGAN TO CLIMB AFTER CONTROLLER WAS WORKING FOR ONE + HOURS. RATE OF CLIMB SUCH THAT HABITUAL LEVELS COULD NOT BE MAINTAINED W/O DESCENT TO LOWER ALT, AUTO SYSTEM WORKED GOOD AND SCHEDULED DIFFERENTIALS AND ALTS MAINTAINED AS DESIGNED. REMOVED AND REPLACED DIGITAL CONTROLLER AS PER EMB AMM 21-31-01. OPS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: TRANSDUCER — FAILED (ZONE 100) · airframe 19,271 hrs · 19,373 cycles

FLAPS FAILED AT NINE DEGREE ON APPROACH. REMOVED AND REPLACED FLAP POSITION TRANSDUCER AND RIGHT VELOCITY SENSOR IAW EMB AMM 27-51-12. OPERATIONAL CHECK GODD WITH NO DEFECTS. RETURNED AIRCRAFT TO SERVICE.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 19,139 hrs · 19,254 cycles

SELECTED FLAPS TO 9 DEGREES AND RECEIVED FLAP LOW SPEED AND FLAP FAIL MESSAGE, FLAP INDICATOR REMAINED AT ZERO, CMC SHOWED FLAP DRIVE SENSOR FAIL MESSAGE. TROUBLESHOT FLAP DRIVE SENSOR FAIL MESSAGE WITH NO DEFECTS. RESET SYSTEM PER EMB FIM TASK 27-51-06-810-805. SYSTEM OPERATIONAL CHECKED GOOD, RETURNED AIRCRAFT TO SERVICE.

Part: FLAPPER VALVE — FAILED (ZONE 500) · airframe 18,765 hrs · 18,946 cycles

FUEL LEAKING FROM LEFT WING, RETURNED TO DFW. REMOVED AND REPLACED FUEL FLAPPER VALVE IAW EMB AMM 28-11-04. OPERATIONAL CHECK GOOD. RETURNED AIRCRAFT TO SERVICE.

Part: FITTING — WORN (LT AILERON)

THE LT AILERON OB HINGE POINT BEARING HOLE WAS FOUND TO BE WORN BEYOND MANUAL LIMITS. REMOVED DAMAGED HINGE FITTING. LOCATED AND DRILLED IN NEW FITTING. APPLIED ALODINE AND PRIMER TO ALL BARE SURFACE. REPAIR DONE IAW SRM. (K)

Part: SILL — CORRODED (FUSELAGE)

THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED. REMOVED THE CORRODED CENTER SILL AND INSTALLED NEW CENTER SILL IAW SRM AND CPM. (K)

Part: CONTROL UNIT — INOPERATIVE (AVIONIC BAY) · airframe 13,205 hrs · 13,800 cycles

DURING CRUISE FLIGHT THE CAPTAIN REPORTED A DUAL PITCH TRIM FAILURE. MAINTENANCE REMOVED AND REPLACED THE HORIZONTAL STABILIZER CONTROL UNIT IAW MM AND CLEANED THE BACKUP TRIM SWITCHES. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (SW21200502358) (K)

Part: CHARGER — MALFUNCTIONED (EMERGENCY LIGHT)

CREW REPORTED THE FORWARD EMERGENCY EXIT LIGHTS STAY ON WITH SWITCH IN THE OFF POSITION. MAINTENANCE REMOVED AND REPLACED NR 1 EMERGENCY LIGHT BATTERY CHARGER AND BATTERY PACK (P/N 20131A) IAW EMB 145 AMM 33-50-06. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: BATTERY — INOPERATIVE (NR 1)

ORD - FLT 3956 - FOUND FORWARD OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED NR 1 EMERGENCY BATTERY. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: POWER SUPPLY — INOPERATIVE (NR 1)

BNA - NR 1 EMERGENCY LIGHTNG SYSTEM INOPERATIVE. REPLACED NR 1 EMERGENCY BATTERY SUPPLY. AIRCRAFT RETURNED TO SERVICE. (M)

Part: FADEC — MALFUNCTIONED (APU)

MQT - FLT 4331 - DURING APU START THE APU HUNG AT 25 PERCENT GROUND CREW NOTICED FIRE AT APU. MAINTENANCE FOUND THE PROBLEM TO BE THE FADEC. THE FADEC WAS REMOVED AND REPLACED IAW EMB MM ALONG WITH A WIRING HARNESS AND FUEL DRAIN LINE. OPERATIONAL AND LEAK CHECKS WERE GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: APU — FIRE (APU BAY)

ORD - FLT 4036 - DURING GROUND OPERATIONS, CREW RECEIVED AN APU FIRE WARNING. APU WAS SHUTDOWN. MAINTENANCE INSPECTION REVEALED EVIDENCE OF FIRE WITH THE WIRING HARNESS AND COWLING BURNED. MAINTENANCE COMPLIED WITH AN APU FIRE INSPECTION IAW EMB MM FOLLOWED BY REMOVING AND REPLACING THE APU IAW EMB MM. OPS AND LEAK CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: WIRE HARNESS — DAMAGED (APU)

CREW REPORTED AN APU FIRE WARNING ON GROUND WITH BLACK SMOKE COMING FROM EXHAUST. GROUND EMERGENCY DECLARED. NO EVIDENCE OF FIRE WAS FOUND AND APU WAS PUT ON MEL. MAINTENANCE FOUND THE APU HARNESS DAMAGED. HARNESS WAS REPLACED IAW EMB MM AND OPERATIONAL CHECK WAS COMPLIED WITH, NO DEFECTS NOTED. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: CLAMP — LOOSE (BLEED AIR SYS)

FWA - FLT 4173 - DURING CRUISE FLIGHT, CREW REPORTED A 'BLEED NUMBER 1 LEAK' MESSAGE ON EICAS. CREW DIVERTED TO FWA DUE TO NO CABIN/COCKPIT HEAT AND WEATHER AT DESTINATION. AN EMERGENCY WAS DECLARED. MAINTENANCE FOUND AND TIGHTENED SOME LOOSE CLAMPS IN THE NR 1 BLEED SYSTEM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: FRAME — DENTED (FUSELAGE)

ABI - DURING INSPECTION, FOUND DENT WITH GOUGE ON LEFT FUSELAGE AT FRAME 19A-20, BETWEEN STRINGERS 15-16L. REMOVED DAMAGE SKIN BY CUTOUT. INSTALLED DOUBLER IAW EMB 145 SRM 145/1142, CHAPTER 53, REV 1, 53-21-01, EMB GST-1478/02 DATED MAY 4, 2002 AND STANDARD SRM PRACTICES. (M)

Part: SKIN — DAMAGED (FUSELAGE)

ABI - DURING INSPECTION, FOUND DAMAGED SKIN AT FRAME 12A AND STRINGER 13R. REMOVED DAMAGED SKIN BY CUT OUT. FABRICATED DOUBLER, AND FILLER. REPAIR DONE IAW EMB GST 1420/02-A AND STANDARD SRM PRACTICES. (M)

Part: STRINGER — CHAFED (FUSELAGE)

ABI - DURING INSPECTION, FOUND STRINGER 19L CHAFED. BLENDED CHAFED, FABRICATED TWO DOUBLER ANGLES, AND FOUR SHIMS IAW GST-1405/02 ITEM 2 AND STANDARD PRACTICES. (M)

Part: FRAME — DAMAGED (FUSELAGE)

ABI - DURING INSPECTION, FOUND ELONGATED RIVET HOLE ON RIGHT FORWARD FUSELAGE II, FRAME 12A. INSTALLED OVERSIZED RIVET IAW EMB GST-1368/02 AND STANDARD SRM PRACTICES. (M)

Part: STRINGER — CHAFED (FUSELAGE)

ABI - DURING INSPECTION, FOUND STRINGER 19R CHAFED. BLENDED CHAFE, FABRICATED DOUBLER ANGLES AND FOUR SHIMS. REPAIRED IAW EMB GST-1405/02 ITEM 2, AND STANDARD SRM PRACTICES. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

ABI - DURING INSPECTION OF AIRCRAFT, FOUND CENTER HAT BEAM CORRODED THROUGH IN TWO SPOTS. REPLACED CENTER HAT BEAM IAW EMB 145 (SRM 145/1142, CHAPTER 51, REV 17), 51-40-02, GST-1128/02, AND STANDARD SRM PRACTICES. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

ABI - DURING AN IMBV INSPECTION OF AIRCRAFT, FOUND CORROSION ON FORWARD DIGITAL. REMOVED CORROSION BY CUT OUT. PERFORMED AN NDT INSPECTION OF THE AREA AND FOUND NO REJECTABLE INDICATIONS. REPAIRED IAW EMB145 SRM 145/1142, CHAPTER 53, REV 17, 53-21-10, AND STANDARD SRM PRACTICES. (M)

Part: SILL — CORRODED (FUSELAGE)

ABI - DURING IMBV INSPECTION OF AIRCRAFT, FOUND CARGO DOOR LOWER SILL CORRODED BETWEEN FRAMES 65 AND 68. REMOVED CORRODED SILL (BEAM). INSTALLED NEW BEAM IAW EMB145 SRM 145/1142, CHAPTER 51, REV 17, 51-40-02 AND STANDARD SRM PRACTICES. (M)

Part: FRAME — GOUGED (FUSELAGE)

ABI - DURING AN IMBV INSPECTION OF AIRCRAFT, FOUND FRAME 81 GOUGED LOWER HALF. REMOVED GOUGED FRAME. INSTALLED NEW FRAME IAW EMB 145 SRM 145/1142 CHAPTER 51, REV 17, 51-20-01, 51-20-03, 51-40-02, 51-40-04 AND STANDARD SRM PRACTICES. (M)

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

ABI - THIS IS A LEVEL 2 FINDING, LOWER CARGO DOOR SILL CORRODED BETWEEN FRAME 65 AND 68. INSTALLED NEW SILL IAW EMB 145 SRM 51-40-02, 51-40-06, 51-20-03. (M)

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

ABI - THIS IS A LEVEL 2 FINDING, FORWARD SERVICE DOOR SILL CORRODED. INSTALLED NEW SILL IAW EMB 145 SRM 51-40-02. (M)

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

ABI - THIS IS A LEVEL 2 FINDING, AFT RIGHT HAT BEAM GUSSET CORRODED. INSTALLED NEW HAT BEAM GUSSET IAW EMB145 SRM 51-40-02. (M)

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

ABI - THIS IS A LEVEL 2 FINDING, FORWARD RIGHT HAT BEAM DIAMOND GUSSET CORRODED. INSTALLED SERVICEABLE GUSSET IAW EMB 145 SRM 51-40-02. (M)

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

ABI - THIS IS A LEVEL 2 FINDING, AFT SERVICE DOOR SILL CORRODED. REMOVED AND REPLACE AFT SERVICE DOOR SILL, IAW EMB 145 SRM 51-40-02. (M)

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

ABI - THIS IS A LEVEL 2 FINDING, FORWARD DIGITAL CORRODED. INSTALLED SERVICEABLE SECTION OF FORWARD DIGITAL IAW EMB 145 SRM 53-21-10. (M)

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

ABI - THIS IS A LEVEL 2 FINDING, LEFT OMEGA BEAM REPAIR CORRODED AT FRAME 20. REPAIRED IAW EMB145 SRM 51-40-02, 51-20-03 AND 53-21-10. (M)

Part: CONTROL UNIT — MALFUNCTIONED (PITCH TRIM)

ORD - FLT 4225 - CREW REPORTED THE NR 1 PITCH TRIM TO BE INOPERATIVE. MAINTENANCE COULD NOT DUPLICATE DISCREPANCY. OPERATIONAL CHECK WAS GOOD IAW EMB MM AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: FUEL CELL — LEAKING (RT WING)

GRR - FLT 3532 - AFTER TAKEOFF TOWER NOTED A VAPOR TRAIL COMING FROM AIRCRAFT, F/O''S THOUGHT SOMETHING WAS COMING FROM RT WING AREA. DECLARED AN EMERGENCY AND RETURNED TO FIELD. AIRCRAFT EXPERIENCED AN OVERWEIGHT LANDING. PERFORMED OPERATIONAL CHECK AND INSPECTION OF FUEL SYSTEM. OPS CHECK GOOD. PERFORMED OVERWEIGHT LANDING INSPECTION. NO DEFECTS NOTED. PERFORMED FCF OF AIRCRAFT, FOUND SATISFACTORY AIRCRAFT RETURNED TO SERVICE. (M)

Part: LIGHT — BROKEN (CABIN)

ORD - FLT 4080 - EMERGENCY EXIT ROW FLOOR PROXIMITY LIGHT STRIP IS MISSING ORANGE STRIPE. REMOVED AND REPLACED EMERGENCY LIGHT STRIP. OPERATIONAL CHECK GOOD. (M)

Part: LIGHT — INOPERATIVE (OVERWING EXIT)

ORD - FLT 4306 - OVERWING EMERGENCY FLOOR PROXIMITY LIGHTS DO NOT ILLUMINATE. REMOVED AND REPLACED OVERWING EXIT FLOOR PROXIMITY LIGHT STRIP. OPERATIONAL CHECK GOOD. (X)