N628AE

Part: CONNECTOR — DISCONNECTED (HI STAGE VALVE) · airframe 44,311 hrs · 41,131 cycles

PDIS 628 36-12 2006092 23NOV18 PHL CLOSE ON INITAL TAKE OFF ROLL HSV 2 FAIL EICAS MESSAGE DIS PLAYED. BROUGHT POWER BACK MESSAGE EXTINGUISHED BUT CAME BACK ON AT TAXI POWER. FACT 23NOV18 20:24 PHL UPON FOUND CANON PLUG ON HIGH STAGE VALVE DISCONNECT ED PERFORM OPS CHECK IAW AMM 36-11-02 OPS CHECK GOOD OK FOR SERVICE

Part: SPLICE — LOOSE (EMERGENCY LIGHT) · airframe 44,085 hrs · 40,856 cycles

NDIS 628 33-20 0012380 13OCT18 RIC CLOSE LOWER SERVICE DOOR EMERGENCY LIGHT BULB INOP. 29490 00 BSH FACT 13OCT18 11:51 RIC SPLICE AND CONTACT WERE LOOSE. REPAIRED IAW SWPM 20-21-00. OPS CHECK GOOD.

Part: WINDSHIELD WIPER — INOPERATIVE (CAPTAIN'S SIDE) · airframe 43,019 hrs · 39,647 cycles

CAPTAIN`S WINDSHIELD WIPER IS STUCK IN CENTER OF THE WIND SCREEN AND WILL NOT PARK. OPEN

Part: UNKNOWN — ODOR (COCKPIT) · airframe 42,916 hrs · 39,532 cycles

AFTER LANDING CAPT NOTICED OIL ODOR IN COCKPIT. OPERATED BOTH ENGINES, OPERATED BLEEDS ONE AND 2 INDEPENDANT OF EACH OTHER AND PACKS 1 AND 2 . NO OIL ODOR NOTED IN AIRCRAFT. OK FOR SERVICE.

Part: CONTROL UNIT — INOPERATIVE (AFT E/E BAY) · airframe 42,757 hrs · 39,355 cycles

PITCH TRIM MAIN INOPERATIVE EICAS WARNING, AFTER TAKEOFF. MAIN PITCH TRIM INOPERATIVE, BACKUP TRIM WORKS NORMALLY. R & R THE HSCU IAW AMM 27-40-01, OPS CHECKED GOOD. R & R THE CAPTAIN`S YOKE PITCH TRIM SWITCH IAW AMM 27-40-03. OPS CHECKED GOOD, OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 42,029 hrs · 38,599 cycles

EMERGENCY LIGHT ON HINGE OF MAIN SERVICE DOOR IS NOT ILLUMINATING. REMOVED AND REPLACED MAIN SERVICE DOOR LIGHT ASSY IAW AMM 33-50-10-000-801-A/400-801-A. OPS CHECKED GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION (HSCU) · airframe 41,688 hrs · 38,249 cycles

MAIN PITCH TRIM INOPERATIVE WARNING MESSAGE ILLUMINATED ON EICAS AFTER TAKEOFF. CMC MESSAGE SAID HSCU FAILURE. PERFORMED FIM TASK 27-43-00-810-803-A. NO FAULTS FOUND. PERFORMED AN OPERATIONAL TEST IAW MM 27-40-00-700-802-A. SYSTEM OPERATES NORMALLY. DETERMINED TO BE A TRANSITORY CONDITION OF THE HSCU. OK FOR SERVICE.

Part: ENGINE — SMOKE (NR 1) · airframe 41,682 hrs · 38,241 cycles

AFTER SHUTDOWN OF THE NR 1 ENGINE, SMOKE WAS SEEN COMING OUT OF THE FRONT AND BACK OF ENGINE. INSPECTED THE INTAKE AND EXHAUST. NO LEAKS NOTED. NO SMOKE NOTED. AT SHUTDOWN DURING IDLE ENGINE RUN IAW AMM 71-00-01. OK FOR SERVICE.

Part: SKIN — DENTED (FUSELAGE) · airframe 41,388 hrs · 37,920 cycles

DURING IMBV INSPECTION, QA FOUND A DENT BELOW GPU DOOR. AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED THE SKIN IAW SRM 53-11-01RE, ITEM 2.

Part: CUP — CORRODED (DRAIN VALVE) · airframe 41,388 hrs · 37,920 cycles

DURING IMBV INSPECTION, QA FOUND THE TOILET WASTE DRAIN VALVE CUP CORRODED. AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE VALVE CUP IAW SRM 51-40-02, 51-20-01, 51-40-06, AND 51-20-03.

Part: FRAME — GOUGED (FRM 65) · airframe 41,388 hrs · 37,920 cycles

DURING IMBV INSPECTION, QA FOUND FRAME 65 GOUGED AT NUT PLATE HOLE ON RT SIDE JUST ABOVE FLOOR LEVEL. AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED THE FRAME IAW ERS-EM-53MR-2636.

Part: FRAME — GOUGED (FRM 68) · airframe 41,388 hrs · 37,920 cycles

DURING IMBV INSPECTION, QA FOUND FRAME 68 GOUGED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED THE FRAME IAW ERS-EM-53MR-2634.

Part: STRINGER — GOUGED (FRAME 52) · airframe 41,388 hrs · 37,920 cycles

DURING IMBV INSPECTION, QA FOUND PREVIOUS REPAIR ON STRINGER 19R GOUGED BETWEEN FRAMES 52 AND 53. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE PREVIOUS REPAIR IAW SRM 53-24-02 RE ITEM 2.

Part: FLOOR SUPPORT — CORRODED (FRAME 38) · airframe 41,388 hrs · 37,920 cycles

DURING IMBV INSPECTION, QA FOUND LT OMEGA BEAM CORRODED AT FR 38. AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED IAW SRM 53-00-10, ITEM 3, AND EM-53-14.

Part: STRINGER — GOUGED (FR 52) · airframe 41,388 hrs · 37,920 cycles

DURING IMBV INSPECTION, QA FOUND PREVIOUS REPAIR ON STRINGER 19L GOUGED BETWEEN FR 52 AND FR 53. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED PREVIOUS REPAIR ON THE STRINGER IAW SRM 53-24-02, RE ITEM 2.

Part: FLOOR SUPPORT — CRACKED (FRAME 29) · airframe 41,388 hrs · 37,920 cycles

CRACK FOUND ON THE LEFT OMEGA BEAM AT FRAME 29 CENTER AISLE CROSSMEMBER ATTACH POINT. REPAIRED IAW ERS-EM-53MR-2643.

Part: SPAR — CRACKED (LT WING) · airframe 41,388 hrs · 37,920 cycles

LT WING SPAR I LOWER FLANGE CRACKED AT 1ST SCREW HOLE OUTBD OF RIB 9. PERFORMED REPAIR ON LT WING SPAR I LOWER FLANGE AT 1ST SCREW HOLE OUTBD OF RIB 9 RECEIVED ERS-EM-57MR-788.

Part: BALLAST — INOPERATIVE (ROW 9) · airframe 41,167 hrs · 37,734 cycles

FA REPORTED ELECTRICAL ODOR IN FWD SIDE OF CABIN DURING APPROACH. FOUND ROW 9 BALLAST TO BE SOURCE OF ODOR. REMOVED AND REPLACED BALLAST. OPS CHECKED GOOD IAW AMM 33-21-05.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT) · airframe 40,726 hrs · 37,329 cycles

EMERGENCY EXIT SIGN ABOVE SERVICE DOOR INOPERATIVE. R & R NR 2 INVERTER IAW AMM 33-50-11 OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 40,426 hrs · 37,002 cycles

SERVICE DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. R & R SERVICE DOOR EXIT EMERGENCY LIGHT IAW AMM 33-50-10-000-801 AND 33-50-10-400-801. OPS CHECK GOOD.

Part: FLASHLIGHT — DIM (CABIN) · airframe 39,746 hrs · 36,371 cycles

REAR CABIN FLIGHT ATTENDANT FLASHLIGHT VERY DIM. BATTERY NEEDS REPLACEMENT. R & R REAR CABIN FLIGHT ATTENDANT FLASHLIGHT AS REQUIRED. NO FURTHER DEFECTS NOTED.

Part: CLAMP — LOOSE (BLEED VALVE) · airframe 39,585 hrs · 36,245 cycles

ON DEPARTURE AT 200 FT WE GOT A BLEED 2 LEAK. FOUND ENG BLEED VLV 2 V BAND CLAMPS LEAKING. REPLACED V BAND CLAMPS & RE-INSTALLED ENG BLEED VLV 2 IAW AMM 36-11-05. NO LEAKS NOTED AT THIS TIME. OPERATIONS CHECKED GOOD.

Part: OUTFLOW VALVE — MALFUNCTIONED (CABIN PRESSURE) · airframe 39,432 hrs · 36,098 cycles

DURING CLIMB THROUGH 7800 FT CABIN WAS DESCENDING 3300, APPROX FPM. AMBER EICAS MSG PRESN AUTO FAIL. CAB ALT, CAB DELTA P 8.0 PSI. R & R ELECTRO PNEUMATIC OUTFLOW VLV IAW 21-31 03. OPERATIONS CHECKED GOOD IAW 21-31-03, REF NRWC 628-DFW-02555.

Part: UNKNOWN — MALFUNCTIONED (BRAKE SYSTEM) · airframe 39,364 hrs · 36,049 cycles

BRAKE INBD INOPERATIVE WHEN LOWERING GEAR FOR LANDING, MSG REPEATED, SUBSEQUENT APPROACH COLD INBD BRAKE TEMP & AMBER OTBD TEMPS AFTER LANDING. TROUBLE SHOT IAW FIM TASK 32-41-00-810-802 NO RELATED CMC MSGS FOUND. OPERATIONS CHECKED MAIN BRAKE SYS IAW AMM 32-41-00. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: DOOR SEAL — DAMAGED (CABIN DOOR) · airframe 39,204 hrs · 35,895 cycles

LOUD SQUEAL FROM MAIN CABIN DOOR WHEN DIFFERENTIAL PRESS IS BELOW 4.6 PSI. TRANSFERRED TO NRWC 628-ORD-02495. REPAIRED LOWER AFT MAIN DOOR FRAME SEAL IAW AMM 52-21-01. LEAK CHECKED GOOD. TRANSFERRED FROM NWRC 628-ORD-02495.

Part: VALVE — FAILED (BLEED AIR SYS) · airframe 38,450 hrs · 35,237 cycles

WHILE CLIMBING THOUGH 190 - 200, OAT 7*C TAT BLEED 1 OVER TEMP MSG, WITH ICE PROTECTION ON, IN ICING CONDITIONS. R & R FAN AIR VLV IAW AMM 36-11-03 & 36-00-00. OPERATIONS CHECKED GOOD.

Part: THERMOSTAT — FAILED (BLEED AIR SYS) · airframe 38,450 hrs · 35,236 cycles

WHILE CLIMBING THROUGH FLIGHT LEVEL 180 - 190, IN ICING CONDITIONS BLEED 1 OVER TEMP WARNING ON EICAS. COMPLIED WITH AOM EMER PROCEDURES. DEFERRED THE NR 1 BLEED SYS. M PROCEDURES COMPLIED WITH IAW 36-01. R & R FAN CONTROL THERMOSTAT IAW AMM 36-11-06. OPERATIONS CHECKED GOOD IAW 36-00-00. R & R FAN AIR FILTER IAW AMM 36-11-03. OPERATIONS CHECKED GOOD.

Part: SKIN — CHAFED (FUSELAGE) · airframe 38,166 hrs · 34,956 cycles

FUSELAGE SKIN CHAFFED UNDER PANEL 424DB. REPAIRED FUSELAGE SKIN CHAFE UNDER PANEL 424DB IAW ERS-EM-53MR-1594.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 38,166 hrs · 34,956 cycles

FORWARD DIGITAL IS CORRODED. REPAIRED FWD DIGITAL CORROSION IAW ERS-EM-53MR-1597.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 38,166 hrs · 34,956 cycles

RIGHT FLOORBEAM IS CORRODED AT FRAME 23. REPAIRED RT FLOORBEAM CORROSION AT FRAME 23 IAW ERS-EM-53MR-1589.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 38,166 hrs · 34,956 cycles

SERVICE DOOR CUT OUT FWD FRAME CORRODED AT LOWER NUTPLATE HOLE. REPAIRED SERVICE DOOR CUT OUT FWD FRAME IAW ERS-EM-53MR-1586.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 38,166 hrs · 34,956 cycles

EMERGENCY FLOOR PROXIMITY LIGHTS 6 - 8 INOPERATIVE. R & R NR 4 EMER BATTERY & CHARGER IAW AMM 33-50-04 & ETN EM-33-020R1, OPERATIONALLY CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 37,259 hrs · 34,159 cycles

CAPTAINS FLASHLIGHT INOPERATIVE. R & R CAPTAINS FLASHLIGHT IAW AMM 33-50-16.

Part: HOLDER — BROKEN (FLASHLIGHT) · airframe 36,916 hrs · 33,889 cycles

CAPTAIN'S FLASHLIGHT HOLDER TAB BROKEN. R & R CAPTAIN'S FLASHLIGHT HOLDER IAW AMM 33-50-16.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 36,637 hrs · 33,669 cycles

RIGHT OVERWING EMER LIGHT IS INOPERATIVE. R & R BATTERY POWER SUPPLY NR 4 IAW AMM 33-50-04. OPERATIONS CHECKED GOOD. REFERENCE NRWC 628-DFW-02038 FOR ALL WORK PERFORMED.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 36,637 hrs · 33,669 cycles

LEFT OVERWING EMER LIGHT IS INOPERATIVE. R & R NR 4 BATTERY POWER SUPPLY IAW AMM 33-50-04. OPERATIONS CHECKED GOOD. CHARGER ASSEMBLY BATTERY PN BA5-0933-901 SN C00585.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,982 hrs · 33,078 cycles

MAIN DOOR CEILING EMER LIGHT INOPERATIVE. R & R MAIN DOOR CEILING EMER LAMP IAW TASK 33-50-06-000-801-A & TASK 33-50-06-400-801-A.

Part: WARNING MESSAGE — FALSE INDICATION (OIL PRESSURE) · airframe 35,400 hrs · 32,535 cycles

NR 1 ENGINE OIL PRESSURE HIGH DURING TAKEOFF AT 114 PSI. GROUND RAN NR 1 ENGINE IAW MM 72-00-00-700-801. NO DEFECTS NOTED OIL PRESSURE IN LIMITS.

Part: CRADLE — DAMAGED (FLASHLIGHT) · airframe 35,024 hrs · 32,190 cycles

CAPTAIN`S FLASHLIGHT BOTTOM CLIP LOOSE, FLASHLIGHT EASILY COMES OUT. REPLACED FLASHLIGHT CRADLE IAW AMM 33-50-16.

Part: HANDLE — DEFECTIVE (MAIN DOOR) · airframe 34,416 hrs · 31,732 cycles

MAIN DOOR DIFFICULT TO OPEN. R & R MAIN DOOR INTERNAL HANDLE IAW AMM 52-18-05. OPENING & CLOSING GOOD.

Part: DOUBLER — DAMAGED (E&E DOOR) · airframe 34,336 hrs · 31,672 cycles

AFT AVIONICS DOOR 272DR RELEASE PIN RECEPTACLE REPAIR DOUBLER NOT FORMED CORRECTLY & RIVETS PULLING THROUGH. PERFORMED PERMANENT REPAIR AFT AVIONICS DOOR 272DR IAW ERS-EM-52MR-035.

Part: HOLDER — FAILED (CABIN) · airframe 34,336 hrs · 31,672 cycles

BATTERY HOLDER ASSEMBLY FAILS CHECKS. R & R BATTERY HOLDER ASSEMBLY.

Part: DOOR — BINDING (MAIN CABIN) · airframe 34,038 hrs · 31,431 cycles

F/A REPORTS, MAIN CABIN DOOR DIFFICULT TO OPEN. ADJUSTED & TESTED GOOD IAW REF AMM 52-10-01.

Part: HANDLE — LOOSE (PAX DOOR) · airframe 33,988 hrs · 31,389 cycles

MAIN CABIN DOOR HANDLE LOOSE. REPAIRED IAW EM 52-052, RETORQUED BOLTS. NO DEFECTS NOTED AT THIS TIME.

Part: FLASHLIGHT ASSY — INOPERATIVE (AFT CABIN) · airframe 33,503 hrs · 30,975 cycles

CHARGING LIGHT INOPERATIVE FOR AFT CABIN FLASHLIGHT. R & R AFT FLASHLIGHT ASSY IAW AMM 33-50-16. OPS CHECKED GOOD.

Part: INVERTER — UNSERVICEABLE (EMERGENCY LIGHT) · airframe 33,263 hrs · 30,778 cycles

DURING B INSPECTION, FOUND FLOOR EMERGENCY LIGHT NR 2 AND NR 3 INOPERATIVE. ACFT REMOVED FROM SERVICE. R & R EMERGENCY LIGHT INVERTER IAW AMM 33-50-11. OPS CHECKED GOOD. ACFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 33,043 hrs · 30,599 cycles

DURING MX INSPECTION FOUND THE RT LOWER FWD EXTERIOR EMERGENCY LIGHT INOPERABLE. DEFERRED IAW MEL 33-29. R & R THE RT LOWER FWD EXTERIOR EMERGENCY LIGHT ASSY IAW AMM 33-50-10. THE OPS CHECK WAS GOOD. MEL 33-29 RESTORED. THE ACFT WAS RETURNED TO SERVICE.

Part: CONTROL PANEL — INOPERATIVE (STAB TRIM) · airframe 32,849 hrs · 30,449 cycles

THE CREW REPORTED THAT ON THE CLIMB THE MAIN PITCH TRIM FAILED. DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE AND LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. R & R THE TRIM CONTROL PANEL AND PERFORMED OPS TEST OF HORIZONTAL STABILIZER SYS IAW AMM 27-40-00. THE OPS CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 32,697 hrs · 30,332 cycles

DURING MAINTENANCE INSPECTION FOUND THE EMERGENCY LIGHT AT THE RIGHT EMERGENCY EXIT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 5 INVERTER IAW AMM 33-50-11. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 31,482 hrs · 29,407 cycles

DURING B INSPECTION FOUND THE NR 3 EMERGRNCY FLOOR LIGHT STRIP INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 3 EMERGENCY BATTERY PACK AND CHARGER IAW 33-50-04. THE OPERATIONAL CHECK OF THE EMERGENCY LIGHTS IAW 33-50-00 WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: DISPLAY — MALFUNCTIONED (COCKPIT) · airframe 31,183 hrs · 29,168 cycles

DURING MAINTENANCE INSPECTION THE NR 1 MULTI FUNCTION DISPLAY UNIT FLASHED AND THEN WENT BLACK AND THEN SMELLED LIKE SMOKE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 1 MFD IAW EMB 145 AMM 34-22-01. THE OPERATIONAL CHECK WAS GOOD 34-22-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 30,774 hrs · 28,844 cycles

DURING MAINTENANCE INSPECTION, FOUND THE COCKPIT HAS A VERY STRONG ODOR OF ROTTING FISH WHEN AIRCRAFT PACKS ARE TURNED OFF. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED GENERAL VISUAL INSPECTION OF COCKPIT AND FOUND NO DISCREPANCY AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SMOKE DETECTOR — INOPERATIVE (CARGO BAY) · airframe 30,358 hrs · 28,507 cycles

DURING B INSPECTION FOUND THE NR 2 BAGGAGE SMOKE DETECTOR INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AFT BAGGAGE SMOKE DET IAW EMB MM 26-15-01. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SMOKE DETECTOR — FALSE ACTIVATION (CARGO BAY) · airframe 30,285 hrs · 28,447 cycles

ON FLIGHT 2796 THE CREW REPORTED THAT WHILE ON FINAL RECEIVED A BAGGAGE SMOKE WARNING. THE CAPTAIN USED THE EPC AND THE FIRE BOTTLE WAS USED. UPON LANDING THE FLIGHT ATTENDANT CHECKED THE BAGGAGE COMPARTMENT USING THE PEEPHOLE AND REPORTED NO FIRE OR SMOKE. REMOVED AND REPLACED AFT BAGGAGE SMOKE DETECTOR IAW AMM 26-15-01. PART NUMBER: 473597-13, SERIAL NUMBER: 3071 LOCATION AFT. REMOVED AND REPLACED FWD BAGGAGE SMOKE DETECTOR IAW AMM 26-15-01. PART NUMBER: 473597-13, SERIAL NUMBER: 1320 LOCATION FWD. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 30,030 hrs · 28,230 cycles

DURING MAINTENANCE INSPECTION FOUND THE LEFT OVERWING EXIT LIGHT INTERIOR INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 4 EMERGENCY LIGHT INVERTER IAW ERJ AMM 33-50-11. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SERVICE PANEL — CORRODED (LAVATORY) · corrosion level 2 · airframe 29,868 hrs · 28,098 cycles

DURING MAINTENANCE INSPECTION FOUND THE CORROSION ON LAVATORY SERVICE AREA BUCKET. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED IAW EO EM-53MR-1960. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,786 hrs · 28,031 cycles

DURING MAINTENANCE INSPECTION FOUND THE FAR AFT EMERGENCY FLOOR STRIP LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED EMERGENCY FLOOR STRIP LIGHT BY FLOOR PANEL 261 BF IAW EMB-145 AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 29,612 hrs · 27,882 cycles

DURING MAINTENANCE INSPECTION FOUND THE RIGHT SIDE CENTER FAIRING EXTERNAL EMERGENCY LIGHT OUT. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT SIDE CENTER FAIRING EXTERNAL EMERGENCY LIGHT IAW AMM 33-50-10. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,561 hrs · 27,841 cycles

DURING B-INSPECTION FOUND THE EMERGENCY LAMP LEFT EXIT ROW PSU FILLER PANEL INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE OVERWING EXIT LAMP LEFT PSU FILLER PANEL IAW EMB AMM TASK 33-50-07-000-801/33-50-07-400-801A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONNECTOR — DEFECTIVE (CABIN) · airframe 29,495 hrs · 27,787 cycles

DURING MAINTENANCE INSPECTION FOUND THE AFT FLOOR EMERGENCY STRIP LIGHT HAS A BROKEN PLUG. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPLACED FLOOR PROXIMITY EMERGENCY LIGHT CONNECTOR IAW EMB WM 20-21-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: HOLDER — BROKEN (FLASHLIGHT) · airframe 29,157 hrs · 27,565 cycles

FMR: 6282507A6 MEL 12-943-C REF 2553 CREW MEMBER FLASHLIGHTS AND HOLDERS. AFT F/A FLASHLIGHT HOLDER BROKEN/MECH/680808. RESTOR OF MEL ITEMS. REMOVED AND REPLACED FLASHLIGHT ASSEMBLY IAW EMB AMM 33-51-01 AND REPAIRED BROKEN WIRE IAW WIRE MANUAL STANDARD PRACTICE 20-50-01 OPS CHECK GOOD MEL RESTORED.

Part: HOLDER — BROKEN (AFT FLASHLIGHT) · airframe 29,139 hrs · 27,554 cycles

DURING MAINTENANCE VISIT, FOUND THE AFT FLASHLIGHT HOLDER BROKEN. REMOVED AND REPLACED THE FORWARD FLASHLIGHT HOLDER IAW AMM 33-50-16-000-801-A AND 33-50-16-400-801-A. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 28,765 hrs · 27,304 cycles

DURING MAINTENANCE BASE VISIT FOUND THE FLOOR EMERGENCY ILLUMINATION STRIP AT ROWS 4-5 INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED AN OPERATIONAL CHECK OF THE EMERGENCY LIGHTS IAW EMB-145 AMM 33-50-00. NO DEFECTS NOTED AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SEAL — BROKEN (FIRE BOTTLE) · airframe 28,648 hrs · 27,212 cycles

FOR FLIGHT 3317 THE FLIGHT ATTENDANT REPORTED THE SEAL WAS BROKEN ON THE AFT CABIN FIRE EXSTINGUISHER. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPLACED SECURITY SEAL ON AFT FIRE EXT AS REQUIRED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: PITOT LINE — DAMAGED (PITOT/STATIC SYS) · airframe 27,832 hrs · 26,551 cycles

LOSS OF AIRSPEED INDICATIONS AND ERRONEOUS AIRSPEED IN IMC NO ICE AT ALL. FOUND PITOT LINES AT ADC 1&2 DAMAGED (BENT) BEYOND LIMITS CAUSING WATER TO COLLECT AND FREEZE. REPLACED BOTH PITOT LINES IAW EMB 145 AMM TASKS 34-13-05-000-801-A & 34-13-05-400-801-A NO FURTHER DEFECTS NOTED. AIRCRAFT IS RVSM ELIGIBLE.

Part: FLASHLIGHT — MISSING (COCKPIT) · airframe 26,325 hrs · 25,431 cycles

ON FLIGHT 3279 THE CAPTAIN’S FLASHLIGHT WAS DISCOVERED TO BE MISSING. REPLACED THE MISSING FLASHLIGHT IAW AMM 33-50-16. OPS CHECKED GOOD. ACFT RESUMED SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 26,196 hrs · 253,257 cycles

DURING MAINTENANCE BASE VISIT FOUND THE RIGHT OVERWING EMERGENCY LIGHT TO BE OUT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY BATTERY IAW EMB 145 AMM 33-50-04-000-801-A AND EMERGENCY BATTERY POWER IAW EMB 145 AMM 33-50-04-400. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 26,159 hrs · 25,299 cycles

FOR FLIGHT 4280 DURING TAXI THE FORWARD EMERGENCY LIGHTS WERE FOUND TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NUMBER 2 EMERGENCY BATTERY PACK (ABOVE GALLEY) IAW EMB145 AMM 33-50-04. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BALLAST — MALFUNCTIONED (CABIN) · airframe 25,587 hrs · 24,840 cycles

AFTER LANDING FLIGHT 4215 THE FLIGHT ATTENDANT REPORTED SMELLING AN ELECTRICAL BURNING ODOR IN THE CABIN. NO ODOR IN THE COCKPIT. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND GALLEY AREA LIGHT BALLAST VERY HOT. REMOVED AND REPLACED BOTH GALLEY AREA LIGHT BALLAST IAW EMB 145 AMM 33-29-03. THE OPERATIONAL TEST WAS NORMAL. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE — BROKEN (CABIN) · airframe 25,437 hrs · 24,712 cycles

DURING MAINTENANCE BASE VISIT FOUND THE LAST AISLE MARKING EMERGENCY LIGHT STRIP TO HAVE BROKEN WIRES. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LIGHT STRIP IAW EMB AMM 33-50-12. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SKIN PANEL — DAMAGED (FUSELAGE) · airframe 24,973 hrs · 24,351 cycles

DURING MAINTENANCE BASE VISIT FOUND THE FORWARD LOWER FUSELAGE SKIN PANEL DAMAGED DUE TO NUMEROUS LIGHTNING STRIKE DISCHARGES LOCATED BETWEEN FRAMES 13 AND 22A AND STRINGER 17R TO 21R. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FORWARD LOWER FUSELAGE SKIN BETWEEN 13 TO 22A STRINGER 17R TO 21R IAW EMBRAER SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 24,973 hrs · 24,351 cycles

DURING MAINTENANCE BASE VISIT FOUND FRAME NR 47 HAS ELONGATED HOLES ON RIGHT SIDE UNDER UPPER SEAT TRACK SUPPORT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED FRAME 47 IAW SRM 51-40-02, 51-20-03, 53-00-04 AND ETA EM-5300-1271. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 24,973 hrs · 24,351 cycles

DURING MAINTENANCE BASE VISIT FOUND THE RIGHT CARGO WALL FRAME 64 HAS TOOLING DAMAGE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED FRAME 64 IAW EO-EM-53MR-1557. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE — BROKEN (AC BAY) · airframe 24,466 hrs · 23,913 cycles

ON FLIGHT 3558 DURING THE CLIMB THE CREW REPORTED A STRANGE SMELL IN COCKPIT FOLLOWED BY "WG AI FAIL" EICAS MESSAGE, THEN "NO ICE AI ON" MESSAGE THEN "PACK 1 VLV FAIL" MESSAGE. THE FIRST OFFICERS ALSO REPORTED A LOUD AIR NOISE CENTER OF CABIN, IN THE VICINITY OF THE AIR CYCLE MACHINES. THE CREW ELECTED TO RETURN TO DFW AND LANDED WITHOUT INCIDENT. FOUND SEVERAL WIRES BROKEN AT P0981 CONNECTOR. REPAIRED ALL WIRES IAW AMM 20-21-00. PERFORMED OPERATIONAL CHECK IAW EMB145 AMM 30-00-00OCK OK. FOUND NR 1 DTCV SLEEVE CRACKED AND PACK VALVE HARNESS DAMAGED. REPLACED SLEEVE AND REPAIRED WIRES P0075 IAW AMM 20-21-00/21-60-00. THE OPERATIONAL CHECK WAS OK IAW 21-51-01, 21-60-01. THE PART NUMBERS OF ITEMS REPAIRED / REPLACED: QUANTITY 3 EMB-4226-24-9 3 WIRE 3 METERS AND QUANTITY 15 M22759/41-24-9 15 FEET. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,220 hrs · 23,689 cycles

DURING THE MAINTENANCE BASE INSPECTION FOUND THE EMERGENCY FLOOR LIGHT AT SEAT 9 INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED SEAT 8 AND 9 FLOOR PROXIMITY LIGHT STRIP IAW EMB145 AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,220 hrs · 23,689 cycles

DURING THE MAINTENANCE BASE INSPECTION FOUND THE RIGHT OVERWING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT OVERWING EMERGENCY LAMP IAW EMB 145 AMM 33-50-10. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 22,240 hrs · 21,886 cycles

ON FLIGHT 3490, CREW REPORTED EMERGENCY EXIT SIGN AT BULKHEAD AT MAIN DOOR WAS INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. RESECURED CONNECTOR ON EXIT IDENTIFIER IAW EMB AMM 33-50-14. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: BRAKE — BURNED (NR 1) · airframe 21,977 hrs · 21,662 cycles

ON FLIGHT 4149 - CREW REPORTED DURING TAXI IN, TOWER REPORTED SMOKE FROM LT SIDE OF AIRCRAFT. RAMP PERSONNEL NOTICED FLAMED FROM NR 1 BRAKE AND RAN UP TO WINDOW AND INFORMED THE CAPT. AIRCRAFT WAS THEN EMERGENCY EVACUATED. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED BOTH NR 1 AND NR 2 BRAKES AND WHEEL AND TIRE ASSY. ALSO, REMOVED AND REPLACED BRAKE LINES. OPERATION CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: BALLAST — ODOR (CABIN LIGHTS) · airframe 20,172 hrs · 19,958 cycles

ON FLIGHT 4183, CREW REPORTED FLIGHT ATTENDANT NOTED ELECTRICAL ODOR JUST BEFORE LANDING. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED LIGHTING BALLAST REF EMB 145 33-21-06. NO DEFECTS NOTED, NR 8194. AIRCRAFT RETURNED TO SERVICE.

Part: ENGINE — FIRE (NR 2) · airframe 19,626 hrs · 19,401 cycles

ON FLIGHT 4221 CREW REPORTED NR 2 ENGINE ON FIRE. REPORTED FROM TRAILING SINGLE ENGINE. A/C ON TAXIWAY. WHILE STARTING NR 2 ENGINE A HUNG START WAS NOTED. TAILWIND 130 DEGREES 23 GUSTING TO 29. HUNG START PROCEDURE APPLIED BUT TRAILING A/C REPORTED FLAMES AND SMOKE COMING OUT OF BOTH INTAKE AND EXHAUST AND TORCHING FUSELAGE. NO COCKPIT INDICATIONS EXCEPT SMOKE ODOR. ENGINE FIRE PROCEDURE APPLIED. CABIN AND COCKPIT FIRE SMOKE FUMES CHECKLIST APPLIED. ENGINE CHECKED AND SECURED BY CFR. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED RIGHT ENGINE IAW WORK CARD 72-00-00. THE PRIMARY REASON FOR REMOVAL WAS: ENGINE 311449 ATTEMPTED A CROSS BLEED START AND THE OTHER ENGINE WAS BELOW THE REQUIRED SPEED OF 80 PERCENT N2. ROLLS ROYCE REVIEW OF THE DATA FROM THE ENGINE 311449 FOUND THE MAXIMUM ITT WAS 264 DEGREES C. THE MAXIMUM FUEL FLOW ACHIEVED DURING THE START WAS 330 PPH. N2 NEVER REACHED SPEEDS ABOVE 15.5 PERCENT N2 AND NO FAN SPEED WAS DETECTED ON THE DFDR DATA. THE ENGINE WAS INSPECTED ACCORDINGLY FOR AN EXCESSIVE DAMAGE CAUSED BY THE FIRE AND WAS RETURNED TO SERVICE. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS)

UPON APPROACH WITH FLAPS AT 0 AND THEN SELECTED TO 9 DEGREES, FLAP FAIL APPEARED ON EICAS AND FLAPS STUCK AT 0. AN EMERGENCY WAS DECLARED WITH NO ABNORMAL LANDING AND NO OTHER ISSUES.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 18,484 hrs · 18,367 cycles

FORWARD EXIT SIGN ABOVE FLIGHT ATTENDANT SEAT WILL NOT ILLUMINATE. REMOVED AND REPLACED NR 1 EMERGENCY BATTERY IAW EMB AMM 33-50-04. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE.

Part: UNKNOWN — SMOKE (LAVATORY) · airframe 18,059 hrs · 17,937 cycles

RECEIVED LAVATORY SMOKE WARNING ON CLIMB, EMERGENCY DECLARED. RETURNED TO DFW. REMOVED AND REPLACED NUMBER TWO ENGINE IAW AMERICAN EAGLE WORK CARD 72-00-00. OPERATIONAL AND LEAK CHECKS PERFORMED WITH NO DEFECTS, AIRCRAFT RETURNED TO SERVICE.

Part: SEAT TRACK — CORRODED (CABIN)

FOUND RIGHT UPPER SEAT TRACK BETWEEN FRAMES 36 AND 47 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-01-06-400-801A. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED

FOUND RIGHT UPPER SEAT TRACK BETWEEN FRAMES 53 AND 55 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-01-06-400-801A. AIRCRAFT RETURNED TO SERVICE. (M)

Part: FRAME — CORRODED (CABIN)

FOUND FRAME 22 CORRODED UNDER LOWER SERVICE DOOR STOP. REPAIRED FRAME IAW IC2006-145/2940. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (CABIN)

SAW - RIGHT INBOARD SEAT TRACK BETWEEN FRAMES 47 AND 53 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-01-06-400-801A. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (CABIN)

SAW - FOUND LEFT INBOARD SEAT TRACK BETWEEN FRAMES 24 AND 30 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-01-06-400-801A. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (CABIN)

SAW - FOUND LEFT UPPER SEAT TRACK BETWEEN FRAMES 47 AND 52 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-01-06. AIRCRAFT RETURNED TO SERVICE. (M)

Part: FLOOR SUPPORT — CORRODED (CABIN)

FOUND FLOORBOARD SUPPORT IN CARGO BAY CORRODED AROUND NUTPLATES AT FRAME 61 LEFT TO 65 LEFT. REMOVED AND REPLACED LEFT SILL IAW SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (CABIN)

FOUND LEFT LOWER SEAT TRACK BETWEEN FRAMES 47 AND 53 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-01-06-400-801A. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (CABIN)

SAW - FOUND RIGHT LOWER SEAT TRACK BETWEEN FRAMES 53 AND 55 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-01-06-400-801A. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (CABIN)

SAW - FOUND LEFT INBOARAD SEAT TRACK BETWEEN FRAMES 17 AND 24 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-01-06-400-801A. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (CABIN)

FOUND RIGHT INBOARD SEAT TRACK BETWEEN FRAMES 24 AND 30 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-01-06-400-801A. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (CABIN)

FOUND RIGHT UPPER SEAT TRACK BETWEEN FRAMES 30 AND 36 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-01-06-400-801A. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (CABIN)

FOUND RIGHT INBOARD SEAT TRACK BETWEEN FRAMES 36 AND 47 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-01-06-400-801A. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (CABIN)

FOUND LEFT OUTBOARD SEAT TRACK BETWEEN FRAMES 30 AND 36 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-01-06-400-801A. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (CABIN)

FOUND RIGHT UPPER SEAT TRACK BETWEEN FRAMES 47 AND 52 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-01-06-400-801A. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (CABIN)

FOUND RIGHT UPPER SEAT TRACK BETWEEN FRAMES 24-30 CORRODED. REPLACED SEAT TRACK IAW EMB AMM 53-01-06. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

DURING AN MBV INSPECTION CORROSION WAS FOUND ON A PREVIOUS REPAIR TO THE LT OMEGA BEAM AT FRAME 20. REMOVED PREVIOUS REPAIR AND INSPECTION THE UNDERLYING BEAM, NO DAMAGE NOTED. FABRICATED AN EXTERNAL ANGLE, FILLER, SHIMS ND PLATE. REPAIR DONE IAW SRM. (SW21200501183)

Part: FLOORBEAM — CORRODED (FUSELAGE)

DURING A MBV INSPECTION, CORROSION WAS FOUND ON THE GALLEY CENTER FLOORBEAM AT FRAME 20. REMOVED CORROSION BY CUTOUT. FABRICATED A REPAIR DOUBLER. REPAIR DONE IAW SRM. (SW21200501183)

Part: SILL — CORRODED (SERVICE DOOR)

DURING A MBV INSPECTION THE SERVICE DOOR CENTER SILL WAS FOUND CORRODED. REMOVED EXISTING SERVICE DOOR CENTER SILL AND INSTALLED NEW SILL. REPAIR DONE IAW SRM.

Part: CONTROL UNIT — INOPERATIVE (E/E BAY)

GSP - FLT 3758 - DURING MAIN TRIM SWITCH ACTIVATION CREW REPORTED AN EICAS WARNING PITCH TRIM MAIN INOPERATIVE AND PITCH TRIM BACKUP INOPERATIVE. COMPLIED WITH CHECKLIST AND PITCH TRIM C/B RESET PROCEDURE WAS PERFORMED. MAIN AND BACKUP TRIM SYSTEMS BOTH RECOVERED. MAINTENANCE COMPLIED WITH ETN EM 27-028R1 AND REMOVED AND REPLCED THE HSCU IAW EMB MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: GEARBOX — BINDING (TE FLAPS)

LBB - FLT 3573 - ON APPROACH CREW RECEIVED FLAP FAIL MSG WITH ASSOCIATED FLAP JAM ON CMC. TROUBLESHOT SYSTEM AND FOUND THE LEFT OUTBAORD ANGLE DRIVE WHEN PUT IN A VERY COLD FREEZING STATE WOULD BIND UP. REPLACED ANGLE DRIVE GEAR BOX. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SELECTOR — MALFUNCTIONED (COCKPIT)

EVV - FLT 4010 - DURING APPROACH CREW REPORTED A FLAP FAIL MESSAGE. AFTER SELECTING FLAPS TO 45 DEGREES FLAPS STUCK AT 38 DEGREES EVEN WITH FLAP HANDLE AT 0 DEGREES. PERFORMED GO AROUND DURING WHICH AIRSPEED INCREASED TO APPROX 180KTS. PERFORMED FLAP FAIL PROCEDURE AS PER AOM AND LANDED UNEVENTFULLY. MAINTENANCE COMPLIED WITH AN EXCEEDING FLAP/DOWN SPEED CONDITION INSPECTION AND FLAP MECHANICAL LINE GENERAL VISUAL INSPECTION WITH NO DEFECTS NOTED. THE FLAP SELECTOR LEVER WAS REMOVED AND REPLACED IAW EMB MM. OPERATIONAL CEHCK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: CHANNEL — CORRODED (FUSELAGE)

ABI - DURING AN IMBV, THE GALLEY AREA RIGHT HAT BEAM WAS FOUND TO BE CORRODED BEYOND SRM LIMITS. COMPLETELY REMOVED CORROSION BY CUTOUT. FABRICATED A 'U' SHAPED DOUBLER. REPAIR DONE IAW EMB 145 GST-2990/02 AND STANDARD EMB SRM PRACTICES. (M)

Part: CHANNEL — CORRODED (FUSELAGE)

ABI - DURING AN IMBV INSPECTION, THE GALLEY AREA RIGHT HAT BEAM WAS FOUND TO BE CORRODED BEYOND SRM LIMITS. COMPLETELY REMOVED CORROSION BY CUTOUT. FABRICATED A U-SHAPED DOUBLER. REPAIR DONE IAW EMB 145 GST-2990/02 AND STANDARD EMB SRM PRACTICES. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

ABI - DURING AN IMBV INSPECTION, THE FORWARD DIGITAL IN THE GALLEY AREA WAS FOUND TO BE CORRODED BELOW SRM LIMITS. REMOVED SECTION OF EXISTING DIGITAL. FABRICATED TWO REPAIR DOUBLERS AND SHIMS. REPAIR DONE IAW EMB145 SRM, SRM 145/1142 REV 19, CHAPTER 53-21-10 PARA 4 FIG 203. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

ABI - DURING AN IMBV INSPECTION, THE FORWARD DIGITAL IN THE GALLEY AREA WAS FOUND TO BE CORRODED BELOW SRM LIMITS. REMOVED SECTION OF EXISTING DIGITAL. FABRICATED TWO REPAIR DOUBLERS AND SHIMS. REPAIR DONE IAW EMB 145 SRM, SRM 145/1142 REV 19, CHAPTER 53-21-10 PARA 4 FIG 203. (M)

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

ABI - THIS IS A LEVEL 2 FINDING, GALLEY AREA LEFT SILL HAS CORROSION. INSTALLED SERVICEABLE LEFT SILL IAW EMB 145 SRM 51-40-02. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2

ABI - THIS IS A LEVEL 2 FINDING, LEFT FORWARD INBOARD SEAT TRACK HAS CORROSION. REMOVED AND INSTALLED SERVICEABLE SEAT TRACK IAW EMB 145 AMM 53-01-06. (M)

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

ABI - THIS IS A LEVEL 2 FINDING, GALLEY AREA FORWARD GUSSET (DIAMOND) HAS CORROSION. INSTALLED SERVICEABLE GUSSET IAW EMB 145 SRM 51-40-02. (M)

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

ABI - THIS IS A LEVEL 2 FINDING, GALLEY AREA CENTER BEAM GUSSET HAS CORROSION. INSTALLED SERVICEABLE CENTER BEAM GUSSET IAW EMB 145 SRM 51-40-02. (M)

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

ABI - THIS IS A LEVEL 2 FINDING, RIGHT FORWARD SILL HAS CORROSION. INSTALLED SERVICEABLE SILL IAW EMB 145 SRM 51-40-02. (M)

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

ABI - THIS IS A LEVEL 2 FINDING, SERVICE DOOR CENTER SILL HAS CORROSION. REMOVED AND REPLACED SILL IAW EMB GST-2969/02. (M)

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

ABI - THIS IS A LEVEL 2 FINDING, RIGHT AFT SILL HAS CORROSION. INSTALLED SERVICEABLE SILL IAW EMB SRM 51-40-02, 51-40-06 AND 51-20-03. (M)

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

ABI - THIS IS A LEVEL 2 FINDING, LEFT OMEGA BEAM FLOOR SUPPORT ANGLE HAS CORROSION. REMOVED AND REPLACED FLOOR ANGLE IAW EMB 145 SRM 51-40-02. (M)

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

ABI - THIS IS A LEVEL 2 FINDING, GALLEY ARE AFT DIAMOND GUSSET HAS CORROSION. INSTALLED SERVICEABLE AFT DIAMOND GUSSET IAW EMB 145 SRM 51-40-02. (M)

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

ABI - THIS IS A LEVEL 2 FINDING, GALLEY RAMP SUPPORT HAS CORROSION. INSTALLED SERVICEABLE GALLEY RAMP SUPPORT IAW EMB 145 SRM 51-40-02. (M)

Part: CONTROL VALVE — FAULTY (AIR CONDITIONING)

ORD - FLIGHT CREW FOUND SMOKE IN CABIN ON GROUND. REMOVED AND REPLACED DUEL TEMPERATURE CONTROL VALVE IAW EMB 145 AMM. OPERATIONALLY CHECKED GOOD. (M)

Part: SENSOR — FAULTY (BRAKE SYS)

LBB - FLT 3668 - ABORTED TAKEOFF, NR 1 BRAKE TEMP INDICATOR FLUCTUATED. REMOVED AND REPLACED NR 1 BRAKE TEMP SENSOR IAW AMM. OPS CHECK GOOD. (M)

Part: CONTROL UNIT — FAILED (HORIZ STAB)

DFW - FLT 3758 - DURING CRUISE FLIGHT CREW REPORTED EICAS MESSAGE PITCH TRIM 2 INOPERATIVE, AND BACK UP TRIM INOPERATIVE CAME ON. BOTH MESSAGES STAYED ON UNTIL TOUCHDOWN THEN CLEARED. MAINTENANCE REMOVED AND REPLACED HORIZONTAL STABILIZER CONTROL UNIT IAW EMB MM. AIRCRAFT WAS RELEASED FOR FUNCTIONAL CHECK FLIGHT. FCF WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: DISPLAY — MALFUNCTIONED (COCKPIT)

CVG - FLT 4093 - AFTER AIRCRAFT WAS POWERED FOR SOMETIME, THE CREW STARTED SMELLING SOMETHING IN COCKPIT ONLY. INSPECTED AREA AND COULD NOT FIND WHERE SMELL WAS COMING FROM. SENDING MTX FROM CMH. REMOVED AND REPLACED EICAS DISPLAY UNIT IAW AMM. OPS CHECK GOOD. (M)

Part: FUEL LINE — CHAFED (NR 2 ENGINE)

ORD - FLT 4100 - OIL SMELL IN CABIN. FOUND CHAFED FUEL LINE FROM FUEL PUMP METERING UNIT TO FUEL COOLED OIL COOLER ON NR 2 ENGINE. REMOVED AND REPLACED LINE IAW AMM. OPS CHECK GOOD. (M)

Part: NOZZLE — DEFECTIVE (ENGINE)

IND - FLT 4007 - DURING ICING CONDITION WITH ANTI-ICING SELECTED F/A AND PASSENGERS SMELLED OIL/SMOKE SMELL IN CABIN. NO INJURIES. REMOVED AND REPLACED FUEL NOZZLES IAW AMM. OPS CHECK GOOD AT THIS TIME. (M)

Part: WINDSHIELD — SHORTED (COCKPIT)

ORD - FLT 4058 - SMOKE IN COCKPIT WHEN CAPTAINS WINDOW HEAT USED. REPLACED CAPTAINS WINDSHIELD IAW EMB AMM. (M)

Part: LIGHT — BROKEN (RT EMER EXIT)

ORD - FLT 4134 - RIGHT OVERWING EMERGENCY EXIT LIGHT DOES NOT ILLUMINATE. REMOVED AND REPLACED LIGHT ASSEMBLY. (M)

Part: COUPLING — LOOSE (CARGO BAY)

IND - FLT 4188 - BLEED LEAK INDICATED ON EICAS. BAGGAGE SMOKE WARNING CAME ON AFTER THAT. DISCHARGED BOTH FIRE EXTINGUISHERS. FOUND LOOSE BLEED COUPLING IN THE CARGO BAY FOR THE NR 2 BLEED SYSTEM. REMOVED AND REPLACED COUPLING SEALS AND SECURED DUCT. AIRCRAFT RETURNED TO SERVICE. (M)

Part: O-RING — FAILED (NR 2 ENGINE DUCT)

DURING CRUISE, AT 20,000 FEET, THE NR 2 BLEED WARNING LIGHT CAME ON. MINUTES LATER THE BAGGAGE COMPARTMENT SMOKE DETECTOR ILLUMINATED, PROCEEDED TO ACTIVATE THE COMPARTMENT FIRE EXTINGUISHER. RETURNED TO INDIANAPOLIS WITHOUT FURTHER INCIDENT. FOUND THE NR 2 ENGINE PNEUMATIC DUCT LOOSE AT THE AFT RIGHT BAGGAGE COMPARTMENT ACCESS PANEL. REPLACED THE O-RINGS, RESECURED THE DUCT AND NO LEAKS NOTED AT THIS TIME, OK FOR SERVICE. (M)

Part: O-RING — WORN (CARGO BAY)

IND - FLT 4188 - BLEED LEAK INDICATED ON EICAS. BAGGAGE SMOKE WARNING CAME ON AFTER THAT. DISCHARGED BOTH FIRE EXTINGUISHERS. FOUND LOOSE BLEED COUPLING IN THE CARGO BAY FOR THE NR 2 BLEED SYSTEM. REMOVED AND REPLACED COUPLING SEALS AND SECURED DUCT. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

JAN - FLT 3683 - EMERGENCY LIGHTS DO NOT ILLUMINATE. REMOVED AND REPLACED EMERGENCY BATTERY PACKS IAW EMB 145 AMM 33-50-04. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. REF: OPERATOR CNTRL NR SIMA991991 AND 99ZZZX3269.

Part: BATTERY PACK — DISCHARGED (CABIN)

JAN - FLT 3683 - EMERGENCY LIGHTS DO NOT ILLUMINATE. REMOVED AND REPLACED EMERGENCY BATTERY PACKS IAW EMB 145 AMM 33-50-04. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. REF: OPERATOR CNTRL NR SIMA991991 AND 99ZZZX3268.

Part: BATTERY PACK — DISCHARGED (CABIN)

JAN - FLT 3683 - EMERGENCY LIGHTS DO NOT ILLUMINATE. REMOVED AND REPLACED EMERGENCY BATTERY PACKS IAW EMB 145 AMM 33-50-04. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. REF: OPERATOR CNTRL NR 99ZZZX3268 AND 99ZZZX3269. (X)