N617AE

Part: BLEED VALVE — FAULTED (NR 1) · airframe 48,650 hrs · 46,059 cycles

BLD 1 VALVE CLOSED MSG IN FLT AND WOULD NOT CLEAR UNTIL STARTED APPROACH. R & R BLD 1 VLV REGULATOR IAW AMM 36-11-05.NO FIX. CONTINUE T/S. R/R PANEL ASSY AIR COND / PNEUMATIC IAW AMM 20-13-10 OPS CHECK GOOD OK FOR SERVICE.

Part: SOLENOID VALVE — FAULTED (NLG) · airframe 48,269 hrs · 45,647 cycles

LOUD AIR NOISE AND VIBERATION FROM NLG AREA AFTER RETRATION OF GEAR. R&R NLG DOOR SOLENOID VALVE REF 32-33-02. LEAKS AND OP CKS GOOD OK FOR SERVICE.

Part: CLAMP — LOOSE (ANTI-ICE SYSTEM) · airframe 47,505 hrs · 44,833 cycles

ICE CONDDITION. A/I INOPERABLE AND WING A/I FAIL MESSAGES ON EICAS WITH WING 1 AND 2 VALVE FAIL AND WING 2 A/I LEAK MESSAGES ON CMC. FOUND SERVERAL LOOSE CLAMPS IN NR 2 PACK AREA. TIGHTENED CLAMPS AS REQ. OPERATIONS AND LEAK CHECKED WITH CREW, IAW AMM 30-00-00-700-802-A. LEAK CHECK GOOD OPERATIONS CHECK FAIL.

Part: CONNECTOR — DAMAGED (MLG HANDLE) · airframe 47,162 hrs · 44,453 cycles

AFTER TAKEOFF, GEAR LEVER SELECTED UP, LANDING GEAR STAYED DOWN WITH AMBER INDICATIONS. CREW C/W ARH LANDING GEAR STAYED DOWN. TROUBLESHOT IAW AMM 32-32-00-700-802-A STEPS J2(F) AND J2(G) FAILED, 2.5 VDC WAS INTERMITTENTLY READING ON P0037 BETWEEN PINS A AND B. RESTORED AC TO ORIGINAL POSITION AND REINSTALLED CANNON PLUGS. NO PARTS AVAILABLE IN CLT. NO FIX. R&R LANDING GEAR MODULE LEVER ASSEMBLY I/A/W AMM32-32-02. OPERATIONS CHECK GOOD. OK FOR SERVICE. PERFORMED GEAR SWING I/A/W 32-32-00-700-801-A LANDING GEAR EXTENSION AND RETRACTION. OPERATIONS CHECK GOOD.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 47,045 hrs · 44,309 cycles

DURING TAKE OFF, AT 100KTS, A BURNING SMELL IN COCKPIT WAS NOTICED BY FO AND CAPT. REJECTED TAKE OFF. WITHIN 5 SECONDS BURNING SMELL DISSIPITATED. INSPECTED AND RAN BOTH ENGINES WITH BLEEDS ON AND OFF FOR 20 MINS. INSPECTED NOSE BAY COMPARTMENT NO DEFECTS OR BURING SMELL FOUND. OK FOR SERVICE

Part: WARNING SYSTEM — MALFUNCTIONED · airframe 46,932 hrs · 44,190 cycles

NO TAKE OFF CONFIG WARNING ON TAKE OFF. RERACKED AWU IAW AMM 31-51-01-04. OPS CHK GOOD. OKAY FOR SERVICE.

Part: PRESSURE SWITCH — FAILED (PARKING BRAKE) · airframe 46,932 hrs · 44,190 cycles

NO TAKE OFF CONFIG WARNING ON TAKEOFF. RNR PARK BRAKE PRESS SW IAW AMM 32-44-07-04. OPS CHECK GOOD OKAY FOR SERVICE.

Part: PRESSURE SWITCH — FAILED (PARKING BRAKE) · airframe 46,932 hrs · 44,190 cycles

PARKING BRAKE ON LIGHT PRESENTED INFLIGHT AND WILL NOT EXTINGUISH. RNR PARK BRAKE PRESS SWITCH IAW AMM 32-44-07-04. OPS CHECK GOOD OKAY FOR SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 46,912 hrs · 44,166 cycles

L/H EMERGENCY DOOR MAIN EXIT LIGHT INOP (EXIT IDENT SIGN). REMOVED AND REPLACED EXIT IDENT SIGN IAW AMM 33-50-13. NO FIX TROUBLE SHOOT PER FAULT ISOLATION MANUAL 33-50-0-810-804-A. REMOVED AND REPLACED INVERTER #4 IAW AMM 33-50-11 OPTS CHECK GOOD.

Part: NUT PLATE — CORRODED (CARGO DOOR SILL) · airframe 46,289 hrs · 43,471 cycles

CORRODED NUTPLATE HOLES ON CARGO CUTOUT STRUCTURE LOWER CENTER SILL. R & R THE CARGO DOOR SILL IAW SRM 51-40-02.

Part: YOKE — CRACKED (LT ENGINE) · airframe 46,289 hrs · 43,471 cycles

LEFT ENGINE FWD LOWER YOKE HAS CRACK ON FWD LOWER CORNER. R & R LH FWD YOKE FITTING AND GUSSET PLATE IAW EO1-71-19-0565.

Part: NUT PLATE — CORRODED (CARGO DOOR) · airframe 46,289 hrs · 43,471 cycles

CARGO DOOR WEB HAS 2 AREAS AROUND NUTPLATES CORRODED. REPAIRED IAW EMB SRM 52-30-01RE AND EO1-52-19-0557

Part: PROFILE — CORRODED (CARGO DOOR) · airframe 46,289 hrs · 43,471 cycles

CARGO DOOR LOWER I/B PROFILE CORRODED AROUND NUTPLATES....FIX:R&RD CARGO DOOR LWR INBD PROFILE IAW EMB145 SRM 51-40-02

Part: SKIN — CRACKED (CARGO DOOR) · airframe 46,289 hrs · 43,471 cycles

CARGO DOOR SKIN WAS CRACKED AT THE AFT END OF THE HANDLE. INSTALLED A REPAIR DOUBLER AND FILLER IAW EO1-52-19-0555.

Part: SKIN — GOUGED (LT WING LE) · airframe 46,289 hrs · 43,471 cycles

LH WING LEADING EDGE NR 1 EXTERIOR HAD ONE GOUGE. FABRICATED AND INSTALLED A REPAIR IAW SRM 51-20-01, AND EO1-57-19-0566.

Part: WARNING MESSAGE — FALSE ACTIVATION (PITCH TRIM) · airframe 46,224 hrs · 43,399 cycles

PDIS 617 27-41 2119051 10NOV19 PHL CLOSE MAIN PITCH TRIM INOP MSG DURING FLIGHT. FACT 10NOV19 16:43 PHL T/S IN REF TO FIM TASK 27-43-00, ELECTRICAL CHECKS G OOD. OPS CHECK IN REF TO AMM 27-40-00. OPS CHECK GOO D NO DEFECTS NOTED AT THIS TIME AIRCRAFT OK FOR SERV ICE.

Part: DISPLAY — MALFUNCTIONED (EICAS) · airframe 44,273 hrs · 41,175 cycles

DIS 617 34-28 1723962 29NOV18 MHT CLOSE SITTING AT GATE WITH ELECTRICAL POWER ON. EICAS SHUT DOWN FOLLOWED BY ELECTRICAL FUMES SMELT IN COCKPIT. NO C/BS POPPED. HISTORY: NO FACT 29NOV18 04:22 PHL RESET EICAS DU C/B, TEST REVERSIONARY PANEL SWITCH,EICAS POWERED UP FOR 3 HRS WITH GPU POWER A/C WITH APU, NO DEFECTS NOTED AT THIS TIME.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 43,409 hrs · 40,178 cycles

EMERGENCY SIGN INOPERATIVE BY SEAT 12A. R & R EMERGENCY SIGN. OPS CHECKED GOOD.

Part: A/C PACK — SEIZED (NR 1) · airframe 42,942 hrs · 39,669 cycles

DURING PUSHBACK STRONG RUBBER BURNING ODOR GENERATED, ODOR STOPPED ONCE PUSHBACK WAS COMPLETE. MX INSPECTED AND FOUND NR 1 PACK SEIZED. R &R THE NR 1 ACM IAW AMM 21-51-03. OPS CHECKED GOOD. LEAK CHECKED GOOD. OK FOR SERVICE.

Part: DUCT — DETACHED (RECIRCULATION) · airframe 42,926 hrs · 39,651 cycles

WITH BOTH PACKS RUNNING ON APU, THE NR 2 PACK WAS SELECTED OFF AND NR 1 PACK MADE AN ABNORMAL NOISE, THE FLT DECK FILLED WITH SMOKE AND ODOR. INSPECTED, NO FUMES OR ODOR WITH THE NR 2 PACK. FOUND THE RECIRCULATION FAN DUCT OFF, REINSTALLED THE DUCT. OPS CHECKED GOOD. FOUND THE DUCT TO BE CHAFED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 42,075 hrs · 38,765 cycles

RIGHT EMERGENCY DOOR UPPER EXIT LIGHT IS INOPERATIVE. R & R THE LIGHT IAW AMM 33-50-14-000/400-801-A. OPS CHECKED GOOD. OK FOR SERVICE.

Part: RELAY — DAMAGED (ZONE 100) · airframe 41,881 hrs · 38,564 cycles

DURING INSPECTION OF RELAY K0058 & RELAY BASE XK0058, SAID RELAY AND BASE FAIL STEP-11IN FCD1-30-165-0276. FOUND DAMAGE AND BURNED PINS ON PITOT STATIC NR 3. BOTH RELAYS K0058, AND RELAY SOCKET XK0058 AND PINS WERE R & R.

Part: HOLDER — CRACKED (EMERGENCY LIGHT) · airframe 41,877 hrs · 38,562 cycles

NR 2 LT FLOOR LIGHT STRIP HOLDER CRACKED. REMOVED AND REPLACED THE NR 2 EMERGENCY LIGHT HOLDER IAW AMM 33-50-12.

Part: LIGHT — CRACKED (CABIN) · airframe 41,877 hrs · 38,562 cycles

LEFT NR 6 PROXIMITY LIGHT EXTRUSION CRACKED. REMOVED AND REPLACED THE LIGHT IAW AMM 33-50-12.

Part: BRACKET — CORRODED (EMERGENCY EXIT) · airframe 41,877 hrs · 38,562 cycles

CORROSION ON RT EMERGENCY ESCAPE HATCH INTERNAL LOWER BRACKET. REMOVED AND REPLACED RT EMERGENCY EXIT LOWER BRACKET IAW SRM 51-40-02.

Part: HOLDER — CRACKED (EMERGENCY LIGHT) · airframe 41,877 hrs · 38,562 cycles

NR 1 LT FLOOR EMERGENCY LIGHT STRIP HOLDER CRACKED. REMOVED AND REPLACED THE EMERGENCY LIGHT HOLDER IAW AMM 33-50-12.

Part: STIFFENER — CRACKED (APU BAY) · airframe 41,877 hrs · 38,562 cycles

FOUND APU COWLING PROFILE 17D CRACKED APPROX 28 INCHES FROM FWD EDGE. COMPLETE:REPAIRED THE APU COWLING INTERNAL STIFFENER IAW SRM 53-32-17.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 41,877 hrs · 38,562 cycles

LEFT NR 6 EMERGENCY LIGHT STRIP HAS BROKEN WIRES. REMOVED AND REPLACED THE LIGHT IAW AMM 33-50-12.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 41,877 hrs · 38,562 cycles

CARGO DOOR CENTER SILL IS CORRODED ON FWD END. REMOVED AND REPLACED CARGO DOOR CENTER SILL WITH NEW SERVICEABLE SILL IAW SRM 51-40-02.

Part: LIGHT — CRACKED (CABIN) · airframe 41,877 hrs · 38,562 cycles

NR 1 RT EMERGENCY LIGHT STRIP CRACKED. REMOVED AND REPLACED THE EMERGENCY LIGHT IAW AMM 33-50-12.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 41,877 hrs · 38,562 cycles

BRACKET IS CRACKED ON INTERNAL FUSELAGE AT FRAME 20 STRINGERS 3L. REMOVED AND REPLACED BRACKET ON INTERNAL FUSELAGE AT FRAME 20 STRINGERS 3L IAW SRM 51-40-02.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 41,877 hrs · 38,562 cycles

EMERGENCY EXIT LIGHT IN 233ALC IS INOP. UPON FURTHER INVESTIGATION FOUND ELECTRICAL CONNECTOR ABOVE MAIN DOOR REGION CEILING PANEL DISCONNECTED. RECONNECTED ELECTRICAL CONNECTOR IAW AMM 25-22-04. EMERGENCY EXIT LIGHT IN 233ALC OPERATIONAL CHECKS GOOD IAW AMM 33-50-00.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 41,877 hrs · 38,562 cycles

LT COCKPIT BULKHEAD EMERGENCY EXIT LIGHT INOP. UPON FURTHER INVESTIGATION FOUND ELECTRICAL CONNECTOR ABOVE MAIN DOOR REGION CEILING PANEL DISCONNECTED. RECONNECTED ELECTRICAL CONNECTOR IAW AMM 25-22-04. EMERGENCY EXIT LIGHT IN LT COCKPIT BULKHEAD OPERATIONAL CHECKS GOOD IAW AMM 33-50-00.

Part: SKIN — BENT (EMERGENCY EXIT) · airframe 41,877 hrs · 38,562 cycles

RIGHT EMERGENCY EXIT EXTERNAL SKIN UPPER EDGE BENT. CONTOURED BENDED IAW SRM 51-10-08.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 41,854 hrs · 38,536 cycles

LEFT FWD OVERWING EMERGENCY LIGHT INOPERATIVE. FOUND EMERGENCY LIGHT BATTERY CHARGER NR 1 CONNECTOR REMOVED FROM CHARGER. SECURED THE CONNECTOR, OPS CHECKED GOOD IAW AMM 33-50-00.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 41,807 hrs · 38,485 cycles

EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED THE EXIT LIGHT IAW AMM 33-50-14, OPS CHECKED GOOD.

Part: WARNING MESSAGE — ILLUMINATED (SPS 1-2) · airframe 41,547 hrs · 38,262 cycles

HIGH SPEED ABORT FOR MASTER WARNING SPS 1-2 INOPERATIVE, AT 120 KTS. NORMAL BRAKING AND NO OVERHEATING ON BRAKES. -TIGHTENED SPC MOUNTING TRAY KNOBS AS NEEDED. PERFORMED OPS CHECKS IAW AMM 27-36-00. OPS CHECKS GOOD.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT) · airframe 40,515 hrs · 37,330 cycles

EMERGENCY LIGHTS INOPERATIVE AT SEATS 7-11. REMOVED AND REPLACED THE NR 3 EMERGENCY POWER SUPPLY AND BATTERY PACK IAW AMM 33-50-04. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 40,515 hrs · 37,330 cycles

EMERGENCY LIGHTS STRIP INOPERATIVE SEATS 7-11.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 39,453 hrs · 36,391 cycles

LEFT EMER LIGHT FWD OF WING INOPERATIVE. R & R EMER LIGHT FWD OF WING IAW AMM 33-50-10-000-801 & 33-50-10-400-801. OPERATIONS CHECKED GOOD.

Part: ROD — DEFECTIVE (SERVICE DOOR) · airframe 39,223 hrs · 36,167 cycles

MAIN CABIN DOOR WILL NOT OPEN. DEPLANED VIA SERVICE DOOR. R&R ROD CONNECTED TO CAM ASSEMBLY FOR PAX DOOR FLAP ASSEMBLY IAW AMM 52-18-02. OPERATIONS CHECKED GOOD.

Part: STRINGER — DENTED (FUSELAGE) · airframe 38,895 hrs · 35,878 cycles

DENT & SCRATCH AT FRAME & STRINGER 8R WITH 1 MISS-DRILLED HOLE IN STRINGER 8R. PERFORMED PERMANENT REPAIR OF DENT, SCRATCH & MISS-DRILLED HOLE ON FRAME 75, STRINGER 8R IAW ERS-EM-53MR-1904.

Part: CONNECTOR — MISSING (CABIN) · airframe 38,895 hrs · 35,878 cycles

EMERGENCY LIGHT STRIP NR 8 CONNECTOR AT FLOOR PANEL 261BF MISSING, ACFT SIDE. INSTALLED MISSING CONNECTORS SP9212 WIRE W192-8832-22 & SP9213 WIRE W192-8833-22 IAW SWPM 20-50-00. CONTACT PN M39029-32-248.

Part: WIRE — BROKEN (EXIT SIGN) · airframe 38,895 hrs · 35,878 cycles

EXIT SIGN ON COCKPIT HAS A BROKEN WIRE. PERFORMED SPLICE REPAIR TO WIRE W762-8044-20 IAW SWPM 20-21-00.

Part: SKIN — CRACKED (FUSELAGE) · airframe 38,895 hrs · 35,878 cycles

LEFT UPPER FUSELAGE SKIN HAS 2 CRACKS. ONE ABOVE STRINGER 2L, & ONE BELOW STRINGER 2L. PERFORMED PERMANENT REPAIR OF LT UPPER SKIN AT FRAME 75 ABOVE & BELOW STRINGER 2L IAW ERS-EM-53MR-1902.

Part: WIRE — BROKEN (CABIN) · airframe 38,886 hrs · 35,871 cycles

LEFT NR 5 FLOOR PROXIMITY LIGHT STRIP HAS BROKEN WIRE AT BASE OF LIGHT. R & R NR 5 PROXIMITY LIGHT STRIP IAW AMM 33-50-12.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 38,886 hrs · 35,871 cycles

SERVICE DOOR CTR SILL, AFT NUTPLATE HOLE CORRODED. INSTALLED DOUBLER REPAIR IAW SRM 53-21-02.

Part: RIB — CRACKED (LT WING) · airframe 38,886 hrs · 35,871 cycles

LEFT RIB 5 HAS POSSIBLE CRACK IN THIRD LIGHTENING HOLE, AT 5 O'CLOCK POSITION LOOKING INSIDE 532AB. R & R IAW ERS-EM-57MR-571.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 38,886 hrs · 35,871 cycles

LAVATORY WASTE BUCKET HAS CORROSION. FABRICATED & INSTALLED DOUBLER ON LAVATORY TOILET WASTES VLV SUPPORT IAW 145 SRM 53-31-02.

Part: CROSSBEAM — CORRODED (FUSELAGE) · airframe 38,886 hrs · 35,871 cycles

CROSSBEAM AT FRAME 20 CORRODED AT PREVIOUS BLEND. R & R CROSSBEAM AT FRAME 20 IAW SRM 53-21-10 & ETN-EM-53-139R4.

Part: SMOKE DETECTOR — FAULTY (LAVATORY) · airframe 38,834 hrs · 35,822 cycles

LAVATORY SMOKE INDICATOR, FLIGHT ATTENDANT CHECKED WITH NO SMOKE. INDICATOR LAVATORY SMOKE PERSISTED & WE DIVERTED. R & R LAVATORY SMOKE DETECTOR PANEL IAW AMM 26-14-02.

Part: TAPE — MELTED (AC BAY) · airframe 38,566 hrs · 35,568 cycles

DURING CRUISE & DESCENT A BURNING SMELL WAS NOTICED & THEN WENT AWAY. POST FLIGHT INSPECTION REVEALED SPEED TAPE MELTED AWAY FROM ACM AREA. TRANSFERRED TO NRWC 617-DFW-02434. COMPLIED WITH ETN-EM-72-034 IAW NRWC 617-DFW-02437, NO ODOR NOTED. REPLACED LIGHTING BALLAST AT SEAT 6 & 7BC IAW AMM 33-21-04. OPERATIONAL CHECKED GOOD. NO FURTHER DEFECT'S NOTED AT THIS TIME.

Part: DOOR — LACK OF LUBE (CABIN) · airframe 37,751 hrs · 34,734 cycles

MAIN CABIN DOOR VERY HARD TO OPEN FROM INSIDE. LUBED MAIN CABIN DOOR IAW AMM 52-18-00. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: LIGHT — INOPERATIVE · airframe 37,630 hrs · 34,628 cycles

AFT OVERHEAD EMER LAMP INOPERATIVE. R & R AFT OVERHEAD EMER LAMP IAW AMM TASK 33-50-08-000-801-A & 33-50-08-400-801-A. OPERATIONS CHECKED GOOD.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 37,560 hrs · 34,568 cycles

NUMBER 1 EMER FLOOR STRIP, LOWER GALLEY SERVICE DOOR & UPPER SERVICE DOOR EMER LIGHT INOPERATIVE. R & R NR 2 EMER LIGHT INVERTER IAW AMM 33-50-11. OPERATIONS CHECKED GOOD.

Part: ROLLER — LACK OF LUBE (CABIN DOOR) · airframe 37,514 hrs · 34,529 cycles

CABIN DOOR HARD TO OPEN & CLOSE. CLEANED CABIN DOOR ROLLERS IAW AMM 53-21-12.

Part: DUCT — LEAKING (BLEED AIR SYS) · airframe 37,423 hrs · 34,453 cycles

BLEED 1 LK ON CLIMB OUT. COMPLIED WITH EPC & AOM 1. REPAIRED ALL BLEED LEAKS IN CARGO COMPARTMENT, LT ENG PYLON & SERVICE MANIFOLD AREA IAW AMM 36-11-09 & 36-11-10. OPERATIONS CHECKED BLEED NR 1 SYS IAW AMM 36-00-00 & NO LEAKS OR FAULTS NOTED AT THIS TIME.

Part: SKIN — DAMAGED (RT ELEVATOR) · airframe 37,340 hrs · 34,368 cycles

HAIL DAMAGE EVENT. REPLACE RT ELEVATOR UPPER CTR SKIN. R & R RT ELEVATOR UPPER CTR SKIN IAW SRM 51-20-01, 51-20-03, 51-40-02, 51-40-06, 55-20-01 & ETN-EM-55-073R2 & ETN-EM-55-076.

Part: SKIN — DAMAGED (LT HORIZ STAB) · airframe 37,342 hrs · 34,369 cycles

HAIL DAMAGE EVENT. REPLACE LT STAB UPPER SKIN. R & R LT STAB UPPER SKIN IAW SRM 55-10-01SI, 51-40-02, 51-40-06, 51-20-03, 51-20-01 & ETN-EM-55-073R2 & ETN-EM-55-074.

Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 37,340 hrs · 34,368 cycles

HAIL DAMAGE EVENT. REPLACE LT ELEVATOR OTBD UPPER SKIN TIP. R & R LT ELEVATOR OTBD UPPER SKIN TIP IAW SRM 51-40-02, 51-20-01, 51-20-03, 51-40-06, 55-20-01 & ETN EM-55-073R2 & ETN EM-55-076.

Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 37,340 hrs · 34,368 cycles

HAIL DAMAGE EVENT. REPLACE LT ELEVATOR MID SKIN TIP. R & R LT ELEVATOR MID SKIN TIP IAW SRM 51-40-02, 51-20-01, 51-20-03, 51-40-06, 55-20-01 & ETN EM-55-073R2 & ETN-EM-55-076.

Part: SKIN — DENTED (LT ELEVATOR) · airframe 37,340 hrs · 34,368 cycles

HAIL DAMAGE EVENT. REPLACE LT ELEVATOR UPPER CTR SKIN. R & R LT ELEVATOR UPPER CTR SKIN IAW SRM 51-20-01, 51-20-03, 51-40-02, 51-40-06, 55-20-01 & ETN-EM-55-073R2 & ETN-EM-55-076.

Part: SKIN — DAMAGED (RT ELEVATOR) · airframe 37,340 hrs · 34,368 cycles

HAIL DAMAGE EVENT. REPLACE RT ELEVATOR MID SKIN TIP. R & R RT ELEVATOR MID SKIN TIP IAW SRM 51-40-02, 51-20-03, 51-20-01, 51-40-06, 55-20-01 & ETN EM-55-073R2 & ETN-EM-55-076.

Part: HOLDER — LOOSE (FLASHLIGHT) · airframe 37,217 hrs · 34,263 cycles

CAPTAIN'S FLASHLIGHT HOLDER LOOSE. DEFERRED IAW MEL 25-53. R & R CAPTAIN`S FLASHLIGHT ASSEMBLY IAW AMM 33-50-16. OPERATIONS CHECKED GOOD & MEL RESTORED.

Part: UNKNOWN — ODOR · airframe 37,130 hrs · 34,188 cycles

AFTER NR 1 ENG STARTED WITH APU ON TAXI TO RUNWAY WE SMELLED A STRONG BURNING SMELL. STARTED NR 2, IT WENT AWAY, SLIGHTLY CAME BACK WITH SAME BURNING SMELL. TROUBLE SHOT ODOR TO NR 1 PACK, DEFERRED 31 PACK, ACM MEL 21-27. COMPLIED WITH ETN-EM-72-034. TROUBLE SHOT USING ETN-EM-72-034(SEE LG PG 3819895 1, COULD NOT FIND ANY ABNORMAL SMELL AFTER RUNNING BOTH ENGS IAW RR 72-00-00. RAN NR 1 PACK, OPERATIONS CHECKED GOOD IAW AMM 21-51-00. MEL RESTORED.

Part: O-RING — DAMAGED (LT ENGINE) · airframe 36,861 hrs · 33,981 cycles

WHILE BEING VECTORED FROM APPROACH, WE NOTICED THE NR 1 FUEL QTY ON EICAS QUICKLY WHEN TO 830 LBS & AMBER VENSES 1200 LBS ON NR 2. WE THOUGHT IT TO BE AN INDICATION PROBLEM AT FIRST BUT DECIDED TO DECLARE AN EMER & LANDED WITH NO PROBLEM. CFR CONFIRM MASSIVE FUEL LEAK OUT OF NR 1 ENG COWLING. SHUT DOWN NR 1 ENG & COMPLETED APPROPRIATE CHECKLISTS. R & R O RING & FUEL FILTER ON LT ENG RR AMM 73-21-10. OPERATIONS & LEAK CHECKED GOOD.

Part: UNKNOWN — MALFUNCTIONED (RUDDER) · airframe 36,776 hrs · 33,906 cycles

DURING CLIMB RECEIVED AN EICAS CAUTION RUDDER SYS 1 -2 INOPERATIVE. TRANSFERRED TO NRWC 617-MIA-02059. PERFORMED FIM 27-22-00-810-804-A. R & R RUDDER SYS 2 IAW AMM 27-23-04. OPERATIONS CHECKED GOOD. NO LEAKS NOTED, ON PRESS SWITCH.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,707 hrs · 33,839 cycles

WHILE PERFORMING PS 2 INSPECTION FOUND SERVICE DOOR EMER EXIT LOCATOR FLOOR PROXIMITY STRIP INOPERATIVE. R & R THE SERVICE DOOR EMER EXIT LOCATOR FLOOR PROXIMITY STRIP IAW AMM 33-50-12. OPERATIONS CHECKED GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 36,670 hrs · 33,794 cycles

FORWARD CABIN EMER LIGHTS DO NOT ILLUMINATE. AFT LIGHTS WERE ON UPON ENTERING ACFT WITH ALL POWER & SWITCHES OFF. R & R NR 1 EMER LIGHT BATTERY SUPPLY IAW AMM 33-50-04. OPERATIONS CHECKED GOOD IAW ITEM 3 4 LG PG 3690621 & ITEM 1 LG PG 3690622 FOR BATTERY 2, 3 & 4.

Part: PROXIMITY SENSOR — FAILED (LEFT) · airframe 36,435 hrs · 33,536 cycles

NR 1 THRUST REVERSER DISAGREE MAST CAUTION DURING TAKEOFF. FEW SECONDS AFT THRUST SET LOW SPEED ABORT. CLEANED AND SECURED THE LT WOW PROXIMITY SWITCH IAW AMM 32-63-01 AND PERFORMED THRUST REVERSER OPS CHECK IAW AMM 78-30-00 NO DISCREPANCIES FOUND.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,287 hrs · 33,366 cycles

LEFT EMER EXIT TOP LIGHT INOPERATIVE. R & R THE LT EMER EXIT TOP LIGHT IAW AMM 33-50-14. OPERATIONS CHECKED GOOD.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 36,265 hrs · 33,339 cycles

DURING PS1 INSPECTION FOUND EMER LIGHTING SYS 2 INOPERATIVE. R & R EMER LIGHT DC & AC INVERTER 3 IAW AMM 33-50-11. OPERATIONS CHECKED OK.

Part: DOOR SEAL — OBSTRUCTED (CABIN DOOR) · airframe 36,154 hrs · 33,238 cycles

MAIN CABIN DOOR DIFFICULT TO OPEN WITH HANDLE IN FULL OPEN & UNLATCH POSITION. WIPED OFF DUST FROM EXPOSED SURFACES OF DOOR FRAME SEAL & REMOVED REMNANTS OF EXPIRED SECURITY STICKERS FROM SAME. COULD NOT DUPLICATE DISCREPANCY. MAIN CABIN DOOR OPERATES NORMALLY AT THIS TIME. OK FOR CONTINUED SERVICE.

Part: ROLL PIN — LACK OF LUBE (CABIN DOOR) · airframe 36,113 hrs · 33,198 cycles

MAIN CABIN ENTRY DOOR VERY DIFFICULT TO OPEN. HANDLE HANGS AROUND THE 12 O’CLOCK POSITION WHEN ROTATED TO OPEN DOOR. LUBRICATED ROLL PINS & MECHANICS OPERATIONS ON MAIN DOOR WORKING PROPERLY AMM 20-30-02--AMM 52-10-00.

Part: O-RING — LEAKING (BLEED AIR SYS) · airframe 36,100 hrs · 33,183 cycles

BLEED 1 LEAK AFTER DEPARTURE. OVERWEIGHT LANDING 44,500 LBS SINK RATE LESS THAN 100 FPM. REPLACED AIR BLEED O RINGS AT ZONE 271 IAW AMM 36-11-10. PERFORMED TASK 36-11-09-200-803-A SATISFACTORILY. SINK RATE WITHIN LIMITS IAW OVERWEIGHT LANDING INSPECTION FLOW CHART AMM 5-50-25. NO INSPECTION REQUIRED.

Part: CLAMP — FAILED (BLEED AIR SYS) · airframe 36,000 hrs · 33,094 cycles

DURING CLIMB OUT THRU 1500 FT BLEED 1 LEAK MASTER WARNING & EICAS MSG WITH RED LEAK ILLUMINATED ON BLEED 1 BUTTON. DECLARED EMER & RAN EPC, SEE LOG 3629618 PREVIOUS. FOUND JOINT NR 30 OF BLEED LINE LEAKING. R & R O RING & CLAMP OF JOINT NR 30 IAW AMM 36-11-10. LEAK CHECKED GOOD AT THIS TIME.

Part: BATTERY — DISCHARGED (CABIN) · airframe 35,808 hrs · 32,881 cycles

EMERGENCY CABIN CEILING LIGHT NR 1 & WING FUSELAGE FRONT FAIRING LT EMER LIGHT INOPERATIVE. BULBS REPLACED STILL INOPERATIVE. R & R POWER SUPPLY & BATTERY FOR NR 1 EMER LIGHT SYS IAW WC 33-700-19. BATTERY CHARGER ASSEMBLY PN 11-0049 & SN C02844.

Part: HOLDER — BROKEN (FLASHLIGHT) · airframe 35,718 hrs · 32,774 cycles

FLIGHT ATTENDANT REAR FLASHLIGHT HOLDER BROKEN. R & R FLASHLIGHT ASSEMBLY IAW AMM 33-50-16. OPERATIONS CHECKED GOOD.

Part: O-RING — DAMAGED (BLEED AIR SYS) · airframe 35,671 hrs · 32,727 cycles

BLEED 1 LEAK EICAS INDICATION LEAK LIGHT ON BLEED 1 CLIMBING THROUGH 5000 FT. FOLLOW AOM & EPC PROCEDURES INDICATIONS EXTINGUISHED REPEAT WRITE UP SEE LP 3404339 1. R & R E 1 BLEED LINE O RINGS AT LOCATIONS 15, 17 & 19 IAW AMM CH36-11-10 LEAK CHECKED GOOD.

Part: SENSE LINE — UNSECURE (AC BAY) · airframe 35,669 hrs · 32,725 cycles

BLEED 1 LEAK EICAS INDICATION & LEAK LIGHT ON BLEED 1 BUTTON WHILE CLIMBING THROUGH 15000 FEET. FOLLOWED AOM ONE PROCEDURE & INDICATIONS EXTINGUISHED. SECURED PACK ONE VLV SENSE LINE IAW MM 21-51-01. SECURED DUAL TEMP CONTROL VLV CLAMP IAW MM 21-60-01. NO DUCT LEAKS FOUND IAW MM 36-11-09.

Part: HANDLE — BROKEN (ENTRY DOOR) · airframe 35,328 hrs · 32,391 cycles

FR, UNABLE TO CLOSE FWD ENTRY DOOR SECURITY, UNABLE TO OPEN DOOR FROM INSIDE. WE ARE STUCK! FOUND MAIN DOOR INTERNAL ACTUATING HANDLE BROKEN. R & R HANDLE IAW AMM 52-18-05, OPERATIONS CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 34,765 hrs · 31,885 cycles

FLIGHT ATTENDANT'S REAR FLASHLIGHT IS INOPERATIVE. R & R REAR FLASHLIGHT ASSEMBLY IAW AMM 33-50-16, OPERATIONS CHECKED GOOD.

Part: HOLDER — BROKEN (FLASHLIGHT) · airframe 34,538 hrs · 31,699 cycles

AFT FLASHLIGHT HOLDER BROKEN. R & R AFT FLASHLIGHT HOLDER IAW AMM 33-50-16. OPERATIONS CHECKED GOOD.

Part: CONNECTOR — NOT SEATED (LT MLG) · airframe 34,475 hrs · 31,647 cycles

ON FLIGHT 3506 AFTER LANDING CREW REPORTED GEAR EXTENSION LT AIR GND FAIL EICAS MESSAGE & DECLARED EMERGENCY. THE ACFT WAS REMOVED FROM SERVICE. PERFORMED FUNCTIONAL CHECK OF ALL MLG PROX SWITCHES, FOUND CONNECTOR ON THE LT SHOCK ABSORBER SWITCH NOT FULLY SEATED. SECURED CONNECTOR & ALL OPERATIONS CHECKED GOOD IAW FIM TASK 32-63-05-700-801-A.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 34,335 hrs · 31,531 cycles

AFT FLASHLIGHT INOPERATIVE. R & R BATTERY FOR AFT FLASHLIGHT PERFORMED OPERATIONS CHECK IAW 145 33-51-01. OPERATIONS CHECKED GOOD.

Part: FITTING — WORN (LT AILERON) · airframe 34,285 hrs · 31,495 cycles

LEFT AILERON OTBD PCA PLUG, OTBD HAT BUSHING MIGRATED. C/A R & R LT AILERON ACTUATOR FITTING IAW AEA EO EM-27MR-112.

Part: SKIN — CRACKED (FUSELAGE) · airframe 34,285 hrs · 31,495 cycles

RIGHT REAR FUSELAGE I SKIN CRACK AT FRAME 75 ABOVE STRINGER 2R. C/A REPAIRED IAW ERS-EM-53MR-010.

Part: SHEAR TIE — CORRODED (FRAME 65) · airframe 34,285 hrs · 31,495 cycles

FRAME 65, LATERAL L SHAPE IS CORRODED AT LWR END. FRAME 65 SHEAR TIE CORRODED. REPAIRED IAW EO EM-53MR-1129.

Part: CONNECTOR — DAMAGED (CABIN) · airframe 34,285 hrs · 31,495 cycles

EMERGENCY LIGHT STRIP WIRE CONNECTOR TORN FROM WIRE AT FR 33. INSTALLED SERVICEABLE CONNECTOR AT FR 33 FOR EMERGENCY LIGHT, IAW 145 SWPM 20-50-01. SEE NRTC E346938 FOR EMERGENCY LIGHT OPERATIONAL CHECK.

Part: WIRE — NICKED (COCKPIT) · airframe 34,285 hrs · 31,495 cycles

FIRST OFFICER’S FLASHLIGHT WIRE ON A/C SIDE NICKED. REPAIRED, SPLICED, COPILOTS FLASHLIGHT WIRES IAW 145 SWPM 20-21-00. SEE NRTC 348783 FOR OPERATIONAL CHECK OF FLASHLIGHT.

Part: BATTERY — DISCHARGED (CABIN) · airframe 34,285 hrs · 31,495 cycles

EMERGENCY LIGHTS FROM EXIT DOORS TO AFT OF AIRCRAFT ARE INOPERATIVE. APPLIED EXTERNAL POWER TO RECHARGE EMERGENCY LIGHT BATTERIES, OPERATIONALLY CHECKED EMERGENCY LIGHTS IAW 145 AMM 33-50-00, OPERATIONS CHECKED GOOD.

Part: LIGHT — DAMAGED (CABIN) · airframe 34,285 hrs · 31,495 cycles

NUMBER 4 EMERGENCY LIGHT SIDEWALL ASSEMBLY HAS ELONGATED HOLES. R & R NR 4 EMERGENCY LIGHT SIDEWALL ASSEMBLY IAW 145 AMM 33-50-12.

Part: CONNECTOR — DAMAGED (CABIN) · airframe 34,285 hrs · 31,495 cycles

EMERGENCY LIGHT STRIP WIRE CONNECTOR TORN FROM WIRE AT FR 25. INSTALLED SERVICEABLE CONNECTOR AT FRAME 25 FOR EMERGENCY LIGHT IAW EMB 145 SWPM 20-50-01. SEE NRTC E346938 FOR OPERATIONAL CHECK.

Part: LIGHT — CRACKED (CABIN) · airframe 34,285 hrs · 31,495 cycles

NUMBER 7 EMERGENCY LIGHT SIDEWALL ASSEMBLY CRACKED. R & R NR 7 EMERGENCY LIGHT SIDEWALL ASSEMBLY IAW 145 AMM 33-50-12. SEE NRWC E346938 FOR OPERATIONS CHECK.

Part: FLASHLIGHT ASSY — INOPERATIVE (CABIN) · airframe 34,125 hrs · 31,355 cycles

F/O FLASHLIGHT INOPERATIVE. REMOVED AND INSTALLED FLASHLIGHT IAW AMM 25-60-00.

Part: RADIO ALTIMETER — MALFUNCTIONED · airframe 33,970 hrs · 31,233 cycles

AT APPROXIMATELY 300 FT AURAL WARNING TO LOW GEAR, GO AROUND RETURN. EMERGENCY GEAR, EXT 3 GREEN INDICATION. R & R RADIO ALTIMETER UNIT IAW AMM 34-31-00. PERFORMED OPS CHECK AND NO DEFECTS FOUND.

Part: FLASHLIGHT ASSY — INOPERATIVE (CABIN) · airframe 33,834 hrs · 31,126 cycles

AFT FLASHLIGHT INOPERATIVE. R & R AFT FLASHLIGHT ASSY IAW AMM 33-50-16, OPS CHECKED GOOD.

Part: WIRE — LOOSE (EMERGENCY LIGHT) · airframe 33,801 hrs · 31,101 cycles

FIRST STRIP OF EXIT PATH LIGHTING INOP BY 1A & 2A. FOUND LOOSE CONNECTION. SECURED AND OPS CHECKED IAW AMM 33-50-00. OPS CHECKED GOOD.

Part: DISPLAY — FAILED (COCKPIT) · airframe 33,355 hrs · 30,714 cycles

CREW REPORTED THAT IN FLIGHT THE PFD WENT BLANK AND THE CIRCUIT BRAKER D13 TRIPPED FOLLOWED BY AN ODOR IN COCKPIT FROM PFD. R & R THE PFD 1 IAW AMM 34-22-01. ODOR CONFIRMED FROM THE PFD AFTER IT WAS REMOVED BY MX. OPS CHECKED GOOD. ACFT RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 32,816 hrs · 30,268 cycles

FOR FLIGHT 4329 THE CREW REPORTED A STRONG FISH SMELL IN THE COCKPIT. REFERENCE PREVIOUS WRITEUPS--- SUBMITTED SDR’S FOR SAME ISSUE---4/11 SIMA20130411005 AND 4/13 SIMA20130413004. THE AIRCRAFT WAS REMOVED FROM SERVICE. CLEANED COCKPIT IAW EMB 145 AMM 20-30-04. NO SMELL NOTED AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 32,797 hrs · 30,254 cycles

ON FLIGHT 4346 THE CREW REPORTED THE COCKPIT SMELLED LIKE DEAD FISH. THE AIRCRAFT WAS REMOVED FROM SERVICE. CLEANED FLIGHT DECK IAW EMB AMM STANDARD PRACTICES. CLEANED AND VACUUMED COCKPIT FLOOR. MAINTENANCE LOOKED UNDER CENTER COCKPIT FLOORBOARD. ODOR DIMINISHED BUT STILL PERSISTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: UNKNOWN — DIRTY (COCKPIT) · airframe 32,782 hrs · 30,242 cycles

ON FLIGHT 4303 THE CREW REPORTED THE COCKPIT SMELLED LIKE DEAD FISH. THE AIRCRAFT WAS REMOVED FROM SERVICE. CLEANED AIRCRAFT COCKPIT IAW EMB 145 AMM 25-00-00. NO FURTHER DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: HOLDER — BROKEN (FLASHLIGHT) · airframe 32,573 hrs · 30,089 cycles

DURING B INSPECTION FOUND THE FIRST OFFICER’S FLASHLIGHT HOLDER BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FIRST OFFICER’S FLASHLIGHT IAW EMB AMM 33-50-16-000-801-A AND 33-50-16-400-801-A. THE OPERATIONAL CHECK WAS GOOD. NO DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 32,573 hrs · 30,089 cycles

DURING B INSPECTION FOUND THE COCKPIT EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE COCKPIT EMERGENCY LIGHT IAW EMB 145 AMM 33-50-05-000-801-A AND 33-50-05-400-801-A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,104 hrs · 29,707 cycles

DURING B INSPECTION FOUND THE MAIN DOOR OVERHEAD EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE MAIN DOOR EMERGENCY LIGHT BULB IAW EMB 145 AMM 33-50-06-000-801-A AND 33-50-06-400-801-A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 31,830 hrs · 29,507 cycles

DURING B INSPECTION FOUND THE LEFT FORWARD EXTERNAL EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY LIGHT BULB IAW EMB 33-50-10-000-801-A AND 33-50-10-400-801-A. PART NUMBER 1317. NO FIX. REMOVED AND REPLACED THE NR 1 EMERGENCY LIGHT BATTERY IAW WORK CARD 33-700-19. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,825 hrs · 29,502 cycles

DURING B INSPECTION FOUND THE FORWARD CEILING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FORWARD CEILING EMERGENCY LIGHT IAW EMB 145 AMM 33-50-08-000-801-A AND 33-50-08-400-801-A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LAMP — INOPERATIVE (EXTERIOR) · airframe 31,531 hrs · 29,288 cycles

DURING B INSPECTION FOUND THE LEFT EXTERIOR OVER WING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT EXTERIOR OVER WING EMERGENCY LIGHT LAMP IAW EMB 145 AMM TASKS 33-50-10-000-801-A & 33-50-10-400-801-A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,494 hrs · 29,258 cycles

DURING MAINTENANCE INSPECTION FOUND THE LEFT FORWARD EMERGENCY EXIT LIGHT ON FUSELAGE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE BULB. THE OPERATIONAL CHECK WAS GOOD PER EMB AMM 33-50-07. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT ASSY — INOPERATIVE (CABIN) · airframe 31,080 hrs · 28,916 cycles

DURING B INSPECTION, FOUND THE AFT FLASHLIGHT INOPERATIVE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AFT FLASHLIGHT AND CRADLE ASSEMBLY. THE OPERATIONAL CHECK WAS GOOD IAW EMB AMM33-50-16. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT ASSY — INOPERATIVE (AFT CABIN) · airframe 30,764 hrs · 28,623 cycles

ON FLIGHT 2817, CREW REPORTED THE FLIGHT ATTENDANT’S AFT FLASHLIGHT WAS INOPERATIVE. REMOVED AND REPLACED THE FLASHLIGHT ASSEMBLY IAW EMB AMM 33-50-16 MEL RESTORED MIC SHEET CLEAR. OP CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,635 hrs · 28,511 cycles

DURING B INSPECTION FOUND THE MAIN DOOR EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE MAIN DOOR EMERGENCY LIGHT LAMP. THE OPERATIONAL CHECK WAS GOOD IAW EMB AMM 35-50-06. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,939 hrs · 27,937 cycles

DURING MAINTENANCE INSPECTION FOUND THE MAIN DOOR EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE MAIN DOOR EMERGENCY LIGHT IAW AMM TASKS 33-50-06-000-801-A AND 33-50-06-400-801-A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · airframe 29,926 hrs · 27,921 cycles

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

Part: STRUCTURE — TORN (CABIN) · airframe 29,926 hrs · 27,921 cycles

DURING B-INSPECTION FOUND THE NR 6 EMERGENCY FLOOR LIGHT EXTRUSION TORN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 6 EMERGENCY FLOOR LIGHT EXTRUSION IAW EMB 145 AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 29,926 hrs · 27,921 cycles

DURING B-INSPECTION FOUND THE LAVATORY RIGHT GUSSET BEAM CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED THE CORRODED RIGHT GUSSET BEAM, PREPPED AND INSTALLED SERVICEABLE GUSSET I IAW EMB SRM 51-40-02 AND EMB SRM 51-20-03. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 29,921 hrs · 27,915 cycles

DURING MAINTENANCE INSPECTION FOUND THE AISLE EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 1 BATTERY POWER SUPPLY AND BATTERY CHARGER. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 29,926 hrs · 27,921 cycles

DURING MAINTENANCE INSPECTION FOUND THE FLIGHT ATTENDANT’S AISLE EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY PACK AND INVERTER ASSEMBLY IAW EMB 145 AMM 33-50-04. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: TERMINAL — BROKEN (CABIN) · airframe 29,926 hrs · 27,921 cycles

DURING B-INSPECTION FOUND THE EMERGENCY LIGHT STRIP AT EXIT ROW HAS A BROKEN TERMINAL. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE TERMINAL ON THE EMERGENCY LIGHT STRIP AT EXIT ROW AW EMB-145 SWPM 20-21-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: STRIP — CRACKED (EMERGENCY LIGHT) · airframe 29,926 hrs · 27,921 cycles

DURING B-INSPECTION FOUND THE EMERGECNY LIGHT STRIP NR 1 CRACKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 1 EMERGENCY LIGHT STRIP IAW EMB 145 AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: PIN — BROKEN (FLASHLIGHT) · airframe 29,926 hrs · 27,921 cycles

DURING MAINTENANCE INSPECTION FOUND THE WIRE FOR FLASHLIGHT CHARGER ON RIGHT LAV WALL HAS 1 BROKEN PIN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPLACED SPLICE CONNECTOR FOR FLASHLIGHT CHARGER ON RIGHT LAV WALL IAW EMB-145 SWPM 20-21-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · airframe 29,926 hrs · 27,921 cycles

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

Part: LEAD — BROKEN (EMERGENCY LIGHT) · airframe 29,926 hrs · 27,921 cycles

DURING B-INSPECTION FOUND THE EMERGENCY LIGHT STRIP NR 8 HAS A BROKEN LEAD. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 8 EMERGENCY LIGHT STRIP AW EMB 145 AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE — BROKEN (CABIN) · airframe 29,926 hrs · 27,921 cycles

DURING MAINTENANCE INSPECTION FOUND THE NR 4 EMERGENCY LIGHT STRIP HAS BROKEN WIRE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 4 EMERGENCY LIGHT STRIP IAW EMB 145 AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: STRUCTURE — DAMAGED (PAX DOOR) · airframe 29,921 hrs · 27,915 cycles

FOR FLIGHT 2898 FLIGHT ATTENDANT REPORTS MAIN CABIN DOOR DIFFICULT TO OPEN. PERFORMED PERMAMENT REPAIR ON PASSENGER DOOR LOWER AFT CORNER IAW AEA EO EM-5200-257 PART C. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE — BROKEN (CABIN) · airframe 29,926 hrs · 27,921 cycles

DURING MAINTENANCE INSPECTION FOUND THE SERVICE DOOR FORWARD LOWER TRIM SHROUD EXIT LIGHT HAS BROKEN WIRE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE SERVICE DOOR LOWER TRIM SHROUD EXIT LIGHT IAW EMB 145 AMM 33-50-13. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — CRACKED (CABIN) · airframe 29,845 hrs · 27,852 cycles

DURING MAINTENANCE INSPECTION DURING REMOVAL OF THE FIRST CENTER AISLE FLOORBOARD (NEXT TO SEAT 1A) FOUND THE FIRST FLOOR PROXIMITY LIGHTING STRIP TO BE CRACKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. INSTALLED CENTER AISLE FLOORBOARD PROXIMITY LIGHT STRIP IAW EMB 145 AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 29,764 hrs · 27,780 cycles

ON FLIGHT 4262 THE CREW REPORTED THE FLASHLIGHT BEHIND THE CAPTAIN’S SEAT DOES NOT SEEM TO HOLD A CHARGE. RED LIGHT WILL ONLY APPEAR MOMENTARLY WHEN FLASHLIGHT REMOVED AND INSTALLED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED FLASHLIGHT ASSEMBLY IAW 145 AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FIRE BOTTLE — UNSECURE (LAVATORY) · airframe 28,324 hrs · 26,678 cycles

ON FLIGHT 4078 THE CREW REPORTED THE LAVATORY FIRE EXTINGUSHER CONTENTS SHOWED TO BE IN THE RED ZONE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LAVATORY FIRE EXTINGUISHER IAW EMB-145 AMM 26-25-01. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ENGINE — POWER LOSS · airframe 27,923 hrs · 26,335 cycles

DURING CLIMBOUT AT APPROXIMATELY 22000 FEET AT 240-250 KNOTS BOTH ENGINES SPOOLED DOWN APPROX 5-10 DEGREES FOLLOWED BY NOTICABLE THRUST INCREASE. THE AIRCRAFT WAS REMOVED FROM SERVICE. ACCOMPLISHED FLIGHT DATA RECORDER DATA DOWNLOAD IAW AE WORK CARD 31-700-05. NO FAULTS FOUND ON DATA REPORT. PERFORMED POWER RUN’S ON BOTH ENGINES WITH BOTH FADECS IAW EMB 145 AMM 71-00-00. NO DEFECTS NOTED. NO PARTS REMOVED OR REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 26,171 hrs · 25,016 cycles

DURING THE MAINTENANCE BASE VISIT FOUND THE MAIN DOOR EXTERNAL EMERGENCY LIGHT TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE MAIN DOOR EXTERNAL EMERGENCY LIGHT. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: DOOR — OUT OF ADJUST (MAIN PAX) · airframe 19,371 hrs · 18,212 cycles

ON FLIGHT 4348 FLIGHT ATTENDANT REPORTS MAIN CABIN DOOR IS HARD TO OPEN. AIRCRAFT REMOVED FROM SERVICE. PASSENGER DOOR ENTERED INTO TDMI 6175208DF PER ETN EM-52-029. PERFORM THE ADJUSTMENT OF THE PASSENGER MAIN DOOR IN ACCORDANCE WITH AMM 52-18-00 TO REDUCE THE AVERAGE MAXIMUM LOAD OF THE INTERNAL HANDLE PULL TEST TO A VALUE OF LESS THAN (45 LBS) ON BEFORE 200FC. AIRCRAFT RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 25,289 hrs · 24,290 cycles

ON FLIGHT 4001 AFTER TAKEOFF ON INITIAL CLIMBOUT THE CREW REPORTED, NOTICED AN OIL SMELL IN COCKPIT. THE FLIGHT ATTENDANT REPORTED A SLIGHT SMELL IN THE FORWARD CABIN. THE PASSENGERS DID NOT SEEM TO NOTICE ANY ODORS. THE AUXILIARY POWER UNIT WAS OFF. NO VISIBLE SMOKE WAS NOTICED. THE CREW ELECTED TO RETURN TO FSD. THE CREW DID NOT DECLARE AN EMERGENCY. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. THE CORRECTIVE ACTION INFORMATION IS PENDING.

Part: OIL SYSTEM — OVERSERVICED (ENGINE) · airframe 25,216 hrs · 24,239 cycles

ON FLIGHT 9802 THE CREW ABORTED THE TAKEOFF ROLL DUE TO SMOKE IN COCKPIT. THE CREW REPORTED THAT BOTH ENGINES HAD 116 PSI OIL BEFORE THE ABORT. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND BOTH ENGINES OVER SERVICED. REMOVED OIL FROM BOTH ENGINES BY REMOVING CHIP DETECTORS AND INSTALLING DETECTORS BACK IAW RR MM 79-37-40. PERFORMED ENGINE RUNS IAW RR MM 72-00-00 FOUND BOTH ENGINE OIL PRESSURES TO BE WITHIN LIMITS AND NO FURTHER SMELL OF OIL IN COCKPIT. THE OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LINE — UNSECURE (WING) · airframe 25,053 hrs · 24,109 cycles

ON FLIGHT 3654 DURING CRUISE THE CREW REPORTED A WING ANTI ICE FAIL MESSAGE INFLIGHT DURING ICE TEST. THE CREW ELECTED TO DIVERT TO RDU AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. RE-SECURED WING MONITORING REFERENCE LINE IAW AMM 30-11-02. ALL OPERATIONAL CHECKS WERE GOOD. NO PARTS CHANGED OR REMOVED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 25,046 hrs · 24,104 cycles

DURING MAINTENANCE BASE VISIT FOUND THE PASSENGER DOOR EMERGENCY LIGHT INOPERABLE AND THE MID-CABIN FORWARD EMERGENCY EXIT SIGN (CEILING) TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 1 POWER SUPPLY AND BATTERY IAW W/C 33-700-19 AND REMOVED AND REPLACED THE MID CABIN EMERGENCY EXIT SIGN IAW EMB AMM 33-50-15. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SKIN — DENTED (FUSELAGE) · airframe 25,046 hrs · 24,103 cycles

DURING MAINTENANCE BASE VISIT FOUND THE FUSELAGE DENTED BETWEEN FRAME 11 AND FRAME 12 AND STRINGER 20 LEFT AND STRINGER 21 LEFT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED DENT BETWEEN FRAMES 11 AND 12 AND STRINGERS 20 LEFT ANT 21 LEFT IN ACCORDANCE WITH ENGINEERING ORDER EM-53MR-1503 AND ETA EM-5300-1153. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: TIRE — SEPARATED (NLG) · airframe 24,778 hrs · 23,889 cycles

ON FLIGHT 3610 DURING TAKEOFF THE CREW REPORTED, FELT A VIBRATION AND AN UNUSUAL NOISE IN THE NOSE GEAR AREA. THE CREW ASKED ATC TO CHECK THE RUNWAY. GSP REPORTED A SECTION OF TIRE AND SOME GLASS ON THE RUNWAY. THE CREW DECLARED AN EMERGENCY AND CONTINUED TO DFW. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT NOSE TIRE IAW EMB W/C 32-700-17. REMOVED AND REPLACED THE LEFT NOSE LANDING GEAR TIRE ASSEMBLY AS PER EMB 145WORK CARD 32-700-17. REMOVED AND REPLACED THE RIGHT STEERING ACTUATOR RIGHT CYLINDER HYDRAULIC LINE IAW CMM LIEBHERR 32-21-09. OPERATIONAL CHECK GOOD AT THIS TIME AND LEAK CHECK GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LINE — LEAKING (BLEED SYS) · airframe 23,764 hrs · 22,936 cycles

SUPPLEMENTAL SDR - ON FLIGHT 4451, ABOUT 10 MINUTES AFTER TAKEOFF THE CREW RECEIVED A BLEED NR 1 LEAK INDICATION MESSAGE. THE CREW FOLLOWED THE CHECKLIST AND THE BLEED LEAK WENT AWAY. THE CREW ELECTED TO RETURN TO JFK. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE DUCT LINE BEHIND PANEL 271DLW IN THE COMPARTMENT IAW AMM 36-11-09. LEAK AND OPERATIONAL CHECK ARE NORMAL. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: DUCT — DEFECTIVE (BLEED AIR SYS) · airframe 23,764 hrs · 22,936 cycles

ON FLIGHT 4451 ABOUT 10 MINUTES AFTER TAKEOFF THE CREW RECEIVED A BLEED NR 1 LEAK INDICATION MESSAGE. THE CREW FOLLOWED THE CHECKLIST AND THE BLEED LEAK WENT AWAY. THE CREW ELECTED TO RETURN TO JFK. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE DUCT LINE BEHIND PANEL 271DLW IN THE CARGO COMPARTMENT IAW AMM 36-11-09. LEAK AND OPERATIONAL CHECKS ARE NORMAL. THE AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 22,320 hrs · 21,641 cycles

ON FLIGHT 3546, CREW REPORTED EMERGENCY LIGHTS WON’T COME ON TO TEST. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED NR 1, 2, 3, 4 POWER SUPPLY ASSEMBLY PER EMB 145 AMM 33-50-04. OPERATIONAL CHECKED GOOD. AIRCRAFT RETURN TO SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 22,198 hrs · 21,528 cycles

ON FLIGHT 3243 CREW REPORTED RELAYS CLICKING BEHIND CAPTAINS SEAT HAD LIGHT ELECTRICAL ODOR OBSERVED FUEL AND ELECTRICAL PAGE WHILE CLICKING DID NOT NOTICE ANYTHING COMING ON OR OFF. AIRCRAFT REMOVED FROM SERVICE. PERFORMED LT AND RT RELAYS VISUAL INSPECTION, INSPECTED FWD AVIONICS COMPARTMENT. PERFORMED OPERATIONAL CHECK OF MAIN CIRCUIT SWITCHING UNIT IAW AMM 24-31-00. ALL OPERATIONAL CHECK NORMAL AT THIS TIME. CND. NO ELECTRICAL ODOR NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: ALTIMETER — MALFUNCTIONED · airframe 22,004 hrs · 21,371 cycles

ON FLIGHT 3474, CREW REPORTED AT 300 FEET AGL THEY GOT AURAL GPWS WARNING AND LANDING GEAR WOULD NOT COME DOWN WITH GEAR TOO LOW. WITH GEAR DOWN AND CONFIGURED CORRECTLY CREW DID A GO AROUND AND RECYCLED GEAR. TOWER CONFIRMED GEAR DOWN. REQUESTED CFR AND LANDED AIRCRAFT SAFELY. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED RADIO ALT UNIT IAW AMM 34-31-01. OPERATIONAL TEST GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: FAN — FAILED (COCKPIT)

ON FLIGHT 3989 CREW REPORTED ON SHORT FINAL, GOT A BURNING OR HOT ODOR IN THE FLIGHT DECK AND FORWARD PART OF CABIN. TURNED THE RECIRCULATION FAN OFF AND FLIGHT ATTENDANT REPORTED NO ODOR AFT OF ROW 5. SMELL DISSIPATED AFTER LANDING WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED COCKPIT RECIRCULATION FAN IAW EMB-145 AMM 21-24-01. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (A)

Part: ALTIMETER — MALFUNCTIONED (RADIO)

ON FLIGHT 4111 CREW REPORTED ON APPROACH, AFTER LANDING GEAR DEPLOYMENT SHOWING DOWN AND LOCK, GPWS WARNING TOO LOW GEAR AC WAS IN POSITIVE CLEARANCE WITH GROUND. CREW ABORTED APPROACH AND DECLARED EMERGENCY. CREW HAD TOWER CONFIRM LANDING GEAR DEPLOYMENT. AC LANDED SAFELY AND TAXIED TO THE GATE WITHOUT FURTHER INCIDENT. AC REMOVED FROM SERVICE C/A MEL 34-20. REMOVED AND REPLACED RADIO ALTIMETER IAW AMM 34-31-01, OPS TEST GOOD. AC RETURNED TO SERVICE MEL RESTORED. (K)

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,057 hrs · 19,691 cycles

DURING MBV INSPECTION, FOUND FLOOR SILL AT FRAME 71 ABOVE STR 17R WITH CORROSION. REMOVED AND REPLACED RT FLOOR SILL AT FRAME 71 IAW SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE.

Part: ODOR — DETECTED (CABIN)

DFW - FLT 3788 - FLT ATTENDANT AND PAX SMELLED A BURNED RUBBER SMELL IN CABIN. COCKPIT CREW DID NOT SENSE THE PROBLEM UNTIL COCKPIT DOOR WAS OPENED UPON ARRIVAL. DID DVI ON ALL LIGHTING SYSTEM IN CABIN, ALL FUNCTIONED NORMAL, APU BLEED SYSTEM NORMAL, GROUND RUN BOTH ENGINES FOR 10 MINUTES WITH ALL BLEEDS AND PACKS ON AND NO AROMAS NOTED. APU AND ENGINES 1 AND 2 WERE RUN WITH ALL PACKS AND BLEEDS ON. NO SMELL EN COUNTERED DURING ALL OPERATIONS. PASSED FCF. RELEASED FROM TRIAD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BEAM — CORRODED (FUSELAGE)

DURING HMBV THE LT OMEGA BEAM AT 38 WAS FOUND CORRODED. PERFORMED A CUT OUT TO REMOVE THE CORROSION, PREPARED A REPAIR DOUBLER, FILLER, 2 SHIMS. REPAIR DONE IAW SRM. (K)

Part: BEAM — CORRODED (FUSELAGE)

DURING A HMBV THE LT OMEGA BEAM AT FRAME 33 WAS FOUND CORRODED. PERFORMED A CUT OUT OF THE BEAM TO REMOVE CORROSION. PREPARED A DOUBLER, FILLER, AND 2 SHIMS. REPAIR DONE IAW SRM. (K)

Part: BEAM — CORRODED (FUSELAGE)

DURING HMBV THE CENTER OMEGA BEAM AT FRAME 24 WAS FOUND CORRODED. PERFORMED A CUTOUT OF THE CENTER OMEGA BEAM TO REMOVE CORROSION. FABRICATED A REPAIR DOUBLER, FILLER AND 2 SHIMS. REPAIR DONE IAW SRM. (K)

Part: BEAM — CORRODED (FUSELAGE)

DURING HMBV THE LT OMEGA BEAM BETWEEN FRAMES 43 AND 44 WAS FOUND CORRODED. PERFORMED A CUT OUT OF THE LT OMEGA BEAM TO REMOVE THE CORROSION. PREPARED A DOUBLER, FILLER AND 2 SHIMS. REPAIR DONE IAW SRM. (K)

Part: BEAM — CORRODED (FUSELAGE)

DURING HMBV THE LT OMEGA BEARM AT FRAME 24 WAS FOUND CORRODED. PERFORMED A CUTOUT OF THE OMEGA BEAM TO REMOVED THE CORROSION. PREPARED A REPAIR DOUBLER. FABRICATED A FILLER AND 2 SHIMS. REPAIR DONE IAW SRM. (K)

Part: BEAM — CORRODED (FUSELAGE)

DURING HMBV A PREVIOUS REPAIR ON THE LT OMEGA BEAM AT FRAME 20 WAS FOUND CORRODED. REMOVED THE PREVIOUS REPAIR AND CLEANED THE AREA. PREPARED A DOUBLER, FILLER, REPAIR PLATE AND 2 SHIMS. REPAIR DONE IAW SRM. (K)

Part: BEAM — CORRODED (FUSELAGE)

DURING HMBV THE LT OMEGA BEAM AT FRAME 53 WAS FOUND CORRODED UNDER THE CARBON CROSSBEAM. PERFORMED A CUT OUT OF THE OMEGA BEAM TO REMOVE THE CORROSION. PREPARED A DOUBLER, FILLER AND 2 SHIMS. REPAIR DONE IAW SRM. (K)

Part: SILL — CORRODED (GALLEY)

DURING HMBV THE SERVICE DOOR CENTER SILL WAS FOUND CORRODED. INSTALLED SERVICEABLE SILL IAW SRM. (K)

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

THE CARGO DOOR CUT OUT LOWER SILL WAS FOUND TO BE CORRODED. REMOVED THE CORRODED CARGO DOOR LOWER SILL. INSTALLED NEW SILL. REPAIR DONE IAW SRM. (K)

Part: POWER SUPPLY — DISCHARGED (CABIN)

AFT TWO EMERGENCY LIGHTING STRIPS WILL NOT ILLUMINATE DURING TEST. REPLACED THE NR 4 EMERGENCY LIGHT POWER SUPPLY. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: WARNING LIGHT — ILLUMINATED (CARGO DOOR)

ORD - FLT 4015 - BAG EXT LIGHT ILLUMINATED DURING CLIMB-OUT, AIRCRAFT LANDED SAFELY WITH NO FURTHER INCIDENTS. PERFORMED OPERATIONAL CHECK OF FIRE DETECTIONS SYSTEM IAW EMB 145 AMM 26-10-00. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. (M) SIMA

Part: BATTERY — FAILED (CABIN)

SUBMITTED OPEN AWAITING DISCREPANCY AND TIMES AND CYCLES AND SERIAL NUMBER. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERY IAW MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE.

Part: TURBINE WHEEL — INOPERATIVE (APU)

APU FAILED INITIAL OBSERVATION WAS SMOKE IN CABIN AND COCKPIT. UPON FURTHER INVESTIGATION FOUND APU TURBINE WHEEL DAMAGED. APU THEN DEFERRED IAW MEL 49-1. MAINTENANCE REMOVED AND REPLACED THE APU IAW EMB MM. OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: LIGHT — INOPERATIVE (CABIN)

XNA - FLT 3854 - CREW REPORTED THE FLOOR PROXIMITY EMERGENCY LIGHTING AT EMERGENCY EXIT ROW WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED FLOOR PATH LIGHT STRIP NR 7 IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: FLASHLIGHT — INOPERATIVE (FWD CABIN)

ORD - FLT 4061 - CREW REPORTED A STRONG ODOR IN CABIN SIMILAR TO ELECTRICAL BURNING SMELL IN FORWARD CABIN NEAR THE FLIGHT ATTENDANT JUMPSEAT. MAINTENANCE FOUND THE FLIGHT ATTENDANT FLASHLIGHT ASSEMBLY OVERHEATED AND MELTED. ALSO, NOTED WIRING HARNESS DAMAGE TO INSULATION. MAINTENANCE REPLACED FLASHLIGHT ASSEMBLY AND REPAIRED DAMAGED WIRES. AIRCRAFT WAS THEN RETURNED TO SERVICE. (M)

Part: POWER SUPPLY — DISCHARGED (CABIN)

LSE - FLT 4186 - DURING CABIN CHECK, CREW REPORTED THE MID CABIN FLOOR PROXIMITY EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 3 POWER SUPPLY UNIT IAW EMB MM. OPERATIONAL CHECK WAS SATISFACTORY AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

ABI - DURING INSPECTION, FOUND CORROSION ON GALLEY RIGHT FLOORBEAM AT FRAME 20. REMOVED CORROSION BY BLENDING. FABRICATED AND INSTALLED DOUBLER IAW EMB GST-1707/02, ITEM NR 2, AND STANDARD SRM PRACTICES. (M)

Part: STRINGER — CHAFED (FUSELAGE)

ABI - DURING INSPECTION FOUND STRINGER 19R CHAFED AT FRAME 53. BLENDED CHAFE, FABRICATED AND INSTALLED DOUBLER, WITH TWO SHIMS IAW EMB 145 SRM 145/1142, CHAPTER 53, REV 18 53-25-02, ETN EM 51-020, AND STANDARD SRM PRACTICES. (M)

Part: DOUBLER — CORRODED (FUSELAGE)

ABI - DURING INSPECTION FOUND CORROSION ON LEFT OMEGA BEAM, PREVIOUS REPAIR AT FRAME 20. REMOVED PREVIOUS REPAIR FABRICATED AND INSTALLED NEW DOUBLER ANGLE, FILLER, PLATE AND TWO SHIMS IAW EMB 145, SRM 145/1142, CHAPTER 53, REV 18 53-21-10, AND STANDARD SRM PRACTICES. (M)

Part: DOUBLER — CORRODED (FUSELAGE)

ABI - DURING INSPECTION, FOUND CORROSION ON PREVIOUS REPAIR AFT DIGITAL. REMOVED PREVIOUS REPAIR. FABRICATED AND INSTALLED NEW DOUBLER IAW EMB 145 SST-249/00 AND STANDARD SRM PRACTICES. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

ABI - DURING INSPECTION FOUND CORROSION ON PREVIOUS REPAIR, FORWARD DIGITAL. REMOVED PREVIOUS REPAIR. FABRICATED AND INSTALLED NEW DOUBLER IAW EMB SST-249/00, AND STANDARD SRM PRACTICES. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

ABI - DURING INSPECTION FOUND CORROSION ON GALLEY CENTER FLOORBEAM. REPLACED GALLEY CENTER BEAM IAW EMB 145 SRM 145/1142, CHAPTER 51, REV 18, ETN EM-53-028, AND STANDARD SRM PRACTICES. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

ABI - DURING INSPECTION FOUND CORROSION ON GALLEY RIGHT FLOORBEAM FRAME 23. REMOVED CORROSION BY BLENDING. FABRICATED AND INSTALLED DOUBLER IAW EMBGST1707/02, ITEM NR 2, AND STANDARD SRM PRACTICES. (M)

Part: STRINGER — CHAFED (STR 19R)

DURING AN IMBV INSPECTION, FOUND STRINGER 19R, CHAFED. BLENDED CHAFE. PERFORMED AN NDT INSPECTION NO DEFECTS. TWO DOUBLERS AND FOUR SHIMS. REPAIR DONE IAW STANDARD SRM PRACTICES.

Part: SILL — CORRODED (CARGO DOOR)

ABI - DURING AN IMBV INSPECTION MAINTENANCE, FOUND THE CARGO DOOR CUT OUT LOWER SILL CORRODED. REMOVED CORRODED SILL BEAM. INSTALLED NEW BEAM IAW EMB 145 SRM 145/1142, CHAPTER 51, REV 17 51-40-02 AND STANDARD SRM PRACTICES. (M)

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

ABI - THIS IS A LEVEL 2 FINDING, GALLEY RIGHT FLOORBEAM AT FRAME 20 CORRODED. REPAIRED GALLEY FLOORBEAM IAW EMB145 SRM 51-40-02. (M)

Part: STRINGER — DAMAGED (STR 19, FR 52)

DURING AN IMBV INSPECTION, ONE RIVET HOLES WAS MISDRILLED ON STRINGER 19L, AT FRAME 52. REAMED HOLE, INSTALLED A HST10BJ-8-6, AND HST79CK-8 FASTERNS. REPAIR DONE IAW STANDARD SRM PRACTICES.

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

ABI - THIS IS A LEVEL 2 FINDING, CENTER BEAM RAMP SUPPORT CORRODED. REMOVED AND REPLACED RAMP SUPPORT IAW EMB145 SRM 51-20-02. (M)

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

ABI - THIS IS A LEVEL 2 FINDING, RIGHT HAT BEAM AT FRAME 23 CORRODED. FABRICATED AND INSTALLED DOUBLER IAW EMB 145 GST-1707/02. (M)

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

ABI - THIS IS A LEVEL 2 FINDING, LEFT CABIN SILL CORRODED BETWEEN FRAMES 19 TO 21. REMOVED AND INSTALLED SERVICEABLE SILL IAW EMB 145 SRM 51-40-02. (M)

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

ABI - THIS IS A LEVEL 2 FINDING, PAX DOOR AFT THRESHOLD SUPPORT CORRODED. REMOVED AND INSTALLED SUPPORT IAW EMB145 SRM 51-40-02. (M)

Part: DOUBLER — CORRODED (FUSELAGE)

ABI - FOUND LEFT OMEGA BEAM PREVIOUS REPAIR CORRODED. FABRICATED AND INSTALLED A DOUBLER IAW EMB 145 SRM 53-21-10. (M)

Part: WINDOW FRAME — CORRODED (FUSELAGE)

DURING AN IMBV INSPECTION FOUND CORROSION IN SCREW HOLES/NUTPLATES OF WINDSHIELD CUTOUT LOWER EDGE. REAMED BEAM/BELT PILOTS SIDE LEFT LOWER CORNER (4) HOLES UP TO .313 TO REMOVE CORROSION. INSTALLED BUSHING, REAMED HOLES IN BUSHING TO .190 INCHES INSTALLED NUTPLATES AND RESTORED FINISH. REPAIR DONE IAW STANDARD SRM PRACTICES.

Part: CONTROL UNIT — INOPERATIVE (HORIZONTAL STAB)

DFW - FLT 3756 - DURING CRUISE INTO DFW, CREW NOTED PITCH TRIM 1 FAIL ON EICAS; LOST OF AP; LOST OF PITCH TRIM ON BOTH YOKES. STANDBY PITCH AT THIS POINT WAS STILL WORKING. UPON DESCENT INTO DFW CREW STILL HAD PREVIOUS ITEMS BUT NOW STANDBY IS NOT WORKING. CREW DECLARED AN EMERGENCY LANDING. LANDED SAFELY. NO FURTHER INCIDENTS WERE REPORTED. REMOVED AND REPLACED BACK UP PITCH TRIM SWITCH AND HSCU IAW AMM. OPS CHECK GOOD. (M)

Part: CONTROL UNIT — INOPERATIVE (PITCH TRIM)

DFW - FLT 3756 - DURING CRUISE INTO DFW, CREW NOTED PITCH TRIM 1 FAIL ON EICAS; LOST OF AP; LOST OF PITCH TRIM ON BOTH YOKES. STANDBY PITCH AT THIS POINT WAS STILL WORKING. UPON DESCENT INTO DFW CREW STILL HAD PREVIOUS ITEMS BUT NOW STANDBY IS NOT WORKING. CREW DECLARED AN EMERGENCY LANDING. LANDED SAFELY. NO FURTHER INCIDENTS WERE REPORTED. REMOVED AND REPLACED BACK UP PITCH TRIM SWITCH AND HSCU IAW AMM. OPS CHECK GOOD. REF SIMA0892. (M)

Part: LIGHT — INOPERATIVE (ENTRY DOOR)

DFW - DURING SCHEDULED PS-2 CHECK, MAINTENANCE REPORTED TWO EMERGENCY LIGHTS INOPERATIVE BY THE ENTRANCE DOOR. MAINTENANCE REPLACED THE BULBS. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: POWER SUPPLY — INOPERATIVE (CABIN)

DFW - DURING SCHEDULED PS-2 CHECK, MAINTENANCE REPORTED THE FORWARD LEFT EMERGENCY LIGHT IS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT POWER SUPPLY UNIT. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: LAMP — INOPERATIVE (CABIN)

ORD - FLT 4114 - FLIGHT ATTENDANT REPORTS ONE OVERHEAD EMERGENCY LIGHTS IS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BULB IAW EMB145 AMM 33-50-08. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: BATTERY — INOPERATIVE (CABIN) · airframe 3,813 hrs · 4,044 cycles

ORD - FLT 4152 - CREW REPORTED EMERGENCY EXIT SIGN INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BATTERY PACK. OPERATIONAL CHECK GOOD, AIRCRAFT RETURNED TO SERVICE. (X)

Part: SKIN — SCRATCHED (FUSELAGE)

ABI - SCRATCH WAS FOUND BETWEEN FRAMES 74 AND 75 AND BETWEEN STRINGERS 18R AND 19R. MAINTENANCE REPAIRED DAMAGE IAW EMB SRM 53-30 AND SRM 51-00. AIRCRAFT RETURNED TO SERVICE. (X)

Part: ECU — MALFUNCTIONED (MLG)

ORD - FLT 4150 - ON APPROACH, BELOW 1000 FT AGL, BEFORE LANDING CHECKLIST COMPLETED, WITH GREEN GREEN GEAR LIGHTS, AURAL WARNING OF GEAR UNSAFE, WENT AROUND ANOTHER APP WITH NO PROBLEMS THIS TIME. REMOVED AND REPLACED LGEU AND GPWS COMPUTER. COULD NOT DUPLICATE. LGEU ON 355022002 S/N 1110. EGPWS COMPUTER ON 9650976003202202 S/N 1455. (M)

Part: BATTERY PACK — INOPERATIVE (CABIN)

DFW - FLT 3618 - OVERHEAD EMERGENCY LIGHTS OUT AT ROW 7. REMOVED AND REPLACED EMERGENCY POWER SUPPLY. OPS CHECK GOOD. (M)

Part: LIGHT — FAILED (EMERGENCY EXIT)

ORD - FLT 4112 - LEFT AND RIGHT OVERWING EMERGENCY EXITS SIGNS FAIL TO ILLUMINATE. REMOVED AND REPLACED BOTH EMERGENCY EXIT SIGN LIGHT ASSEMBLIES. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

ORD - FLT 4023 - WHEN FLIGHT ATTENDANT TESTED THE EMERGENCY LIGHTS, THEY INITIALLY CAME ON, THEN IMMEDIATELY WENT DIM, AND THEN, FAILED TO ILLUMINATE AT ALL AFTER 10 SECONDS. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACKS 1 THROUGH 4 IAW EMB-145 AMM 33-90-04. OPERATIONAL CHECK GOOD. REF: OPER CNTRL NR SIMA990779, AND, 99ZZZX1654 AND 99ZZZX1655.

Part: BATTERY PACK — DISCHARGED (CABIN)

ORD - FLT 4023 - WHEN FLIGHT ATTENDANT TESTED THE EMERGENCY LIGHTS, THEY INITIALLY CAME ON, THEN IMMEDIATELY WENT DIM, AND THEN, FAILED TO ILLUMINATE AT ALL AFTER 10 SECONDS. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACKS 1 THROUGH 4 IAW EMB-145 AMM 33-90-04. OPERATIONAL CHECK GOOD. REF: OPER CNTRL NR SIMA990779, AND, 99ZZZX1655 AND 99ZZZX1656.

Part: BATTERY PACK — DISCHARGED (CABIN)

ORD - FLT 4023 - WHEN FLIGHT ATTENDANT TESTED THE EMERGENCY LIGHTS, THEY INITIALLY CAME ON, THEN IMMEDIATELY WENT DIM, AND THEN, FAILED TO ILLUMINATE AT ALL AFTER 10 SECONDS. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACKS 1 THROUGH 4 IAW EMB-145 AMM 33-90-04. OPERATIONAL CHECK GOOD. REF: OPER CNTRL NR SIMA990779, AND, 99ZZZX1654 AND 99ZZZX1656.

Part: BATTERY PACK — DISCHARGED (CABIN)

ORD - FLT 4023 - WHEN FLIGHT ATTENDANT TESTED THE EMERGENCY LIGHTS, THEY INITIALLY CAME ON, THEN IMMEDIATELY WENT DIM, AND THEN, FAILED TO ILLUMINATE AT ALL AFTER 10 SECONDS. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACKS 1 THROUGH 4 IAW EMB-145 AMM 33-90-04. OPERATIONAL CHECK GOOD. REF: OPER CNTRL NR 99ZZZX1654 THROUGH 99ZZZX1656. (X)