N620AE

Part: NONE — NONE · airframe 49,726 hrs · 46,159 cycles

PDIS 620 71-10 2746611 04DEC21 CLT CLOSE EXTREME VIBRATION ON #1 ENGINE IN FLT @ 3000 FT. 00 FACT 04DEC21 15:42 CLT FOUND #1 ENGINE OIL DOOR OPEN AND AIR START VALVE DOOR OPEN AND COWL DAMAGED. R+R #1 LOWER COWL IAW 71-12-01-000-802A AND 71-12-01-400-802A

Part: UNKNOWN — ODOR (COCKPIT) · airframe 47,645 hrs · 45,318 cycles

STRONG BURNING SMELL OBSERVED IN THE COCKPIT AND CABIN IN ICING CONDITION. PERFORMED OPS CHECK OF ANTI/ICE MESSAGES AND PACKS IAW EMB 145 AMM 30-00-00-700-801-A OPS CHECK GOOD NO SMOKE SMELL NOTED.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 48,932 hrs · 45,223 cycles

STRONG ELECTRICAL ODER IN FLIGHT DECK FOLLOWED BY TCAS FAIL. PERFORMED GVI OF FLIGHT DECK AND FWD AVIONICS. RAN ENGINES AT FULL POWER WITH PACKS ON. NO EVIDENCE OF ELECTRICAL SMELL OR ANY OTHER DEFECTS NOTED REF LOGPAGE 240803 SEQ 2 FOR TCAS MEL A/C OK FOR SERVICE.

Part: CONTROL VALVE — MALFUNCTIONED (BRAKES) · airframe 48,448 hrs · 44,671 cycles

PDIS 620 32-49 2362062 31MAR21 ORD CLOSE. AFTER SELECTING GEAR DOWN, BRAKE DEGRADED MSG APPEARED ON EICAS, MSG PERSISTED AFTER LANDING. LH OTBD BRAKE TEMP HIGHER THAN NORMAL (STILL IN THE GREEN RANGE)(NO RELATED CMC MESSAGES). FACT 01APR21 13:30 ORD. R&R RH BRAKE CONTROL VALVE IAW AMM 32-41-06, OPS CHECK AND LEAK CHECK GOOD. NO EICAS MESSAGE PRESENT AT THIS TIME. ALL OTHER INDICATIONS NORMAL OK FOR SERVICE

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 48,139 hrs · 44,343 cycles

PANEL 241DF EMERGENCY LIGHT INOPERABLE. R & R PANEL 241DF EMERGENCY FLOOR STRIP LIGHT ASSEMBLY, IAW AMM 33-50-112. SPLICED NEW CONNECTORS AT PANEL 241DF EMERGENCY LIGHT, IAW STANDARD MAINTENANCE PRACTICES.

Part: SENSOR — INOPERATIVE (NR 1 PITOT TUBE) · airframe 48,048 hrs · 44,226 cycles

PITOT 1 INOPERABLE DISPLAYED ON EICAS AFTER TAKE OFF. REMOVED AND REPLACED NR 1 PITOT SENSOR, IAW AMM 34-13-01. OPERATIONS CHECK AND LEAK CHECK GOOD. OK FOR SERVICE REQUIRES FILET SEALANT AROUND BASE SEE SEQ 2 THIS LP. CORRECT LP 231995-1.

Part: ICU — FAILED (NR 1) · airframe 47,975 hrs · 44,147 cycles

IN FLT COMS 1/2 EXPERIENCED STATIC FOLLOWED BY BURNING SMELL AND COM 1 GOING OUT. MAINTENANCE: R & R NO1 ICU, IAW AMM 23-00-01. COMM 1 OPERATIONS GOOD (SHORT SIGNED). R & R NR 2 INTEGRATED COMM UNIT, IAW AMM 23 00 01. COMMS 2 OPERATIONS CHECK GOOD. OK FOR SERVICE.

Part: INDICATOR — OVERHEATED (COCKPIT) · airframe 47,959 hrs · 44,131 cycles

FOUND IC-2 C/B POPPED (D-30) WITH BURNING SMELL AT NR 2 IC-600. R & R NR 2 IC-600, REF AMM 31-42-01. PERFORMED OPERATIONS CHECK, PER AMM 31-42--00-700-801-A. ALL CHECKS NO BURNING SMELL. OK FOR SERVICE.

Part: ANTI-ICE VALVE — SEIZED (NR 2 ENGINE) · airframe 47,928 hrs · 44,095 cycles

PDIS 620 30-21 2453941 02OCT20 MDT. CLOSE E2 ANTI ICE FAIL WITH NO ICING CONDITION. FACT 03OCT20 20:29 MDT. DOWNLOADED CMC DATA, ENGINE 2 ANTI ICE VALVE FAIL OCC. BEGAN T/S W/ FIM 30-21-00-810-804. DURING BLOCK 11 VALVE SEIZED IN OPEN, FOUND DAMAGED. INSPECTED DUCT, NO FOD NOTED. R & R NR 2 ENGINE INLET VALVE, IRT AMM 30-21-01-000/400-801. LEAK CHECKS 30-00-00-700-802, 30-21-00-700-803, AND 30-21-00-700-804 GOOD. NO CMC MESSAGES. OK FOR SERVICE.

Part: CLEAT — CORRODED (FUSELAGE) · airframe 47,498 hrs · 43,616 cycles

FRAME 68 FLOOR SUPPORT CLEAT AFT BAGGAGE BAY DOOR HAS CORROSION FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED FLOOR SUPPORT CLEAT FR 68 AFT CARGO IAW EMB145 SRM 51-40-02, 51-20-03, 51-21-04, 51-21-05, AND 51-21-06.

Part: PROBE — FAILED (TAT) · airframe 47,457 hrs · 43,566 cycles

ON T/O TAT1 INOP W/ NO CONFIG MSG. C/W FIM 30-33-00-810-801A. MSG CLEARED AND D/N RETURN. TAT 1 INOP ON T/O ASSOCIATED W/ NO CONFIG WARNING. PERFORMED FIM TASK 30-33-00-810-801A. R&R RELAYS K0495,K0534,K0325,K0059. R&R TAT CURRENT SENSOR IAW 30-33-01 NO FIX. R&R TAT PROBE #1 IAW 34-15-03. OPS CHECKED TAT 1 IAW 30-33-00. OPS CHECK GOOD. OK FOR SERVICE.

Part: ENGINE — SMOKE (NR 1) · airframe 47,350 hrs · 43,447 cycles

AFTER TAKEOFF ATTEMPT, WHEN THRUST LEVERS WERE SET TO TAKEOFF THRUST, HEAVY SMOKE APPEARED IN THE COCKPIT. ONCE THRUST LEVERS WERE MOVED BACK TO IDLE, SMOKE CLEARED. MX TROUBLESHOT ISSUES AND DETERMINED TO BE THE NR 1 ENGINE BLEED SYSTEM, WHEN THRUST LEVERS ARE ADVANCED.

Part: WINDOW FRAME — CRACKED (COCKPIT) · airframe 47,163 hrs · 43,226 cycles

CAPTS WINDOW PILLAR CRACKED, BTWEEN W/S AND DV WINDOWS....FIX: PERFORMED EDDY CURRENT INSPECION AT CAPT,S PILLAR INNER AND OUTER SURFACE SKIN. NO CRACKS FOUND AT HIS TIME. PILLAR FOUND TO BE SEPARATING AT SEAM. NOTE: A/C FERRIED TO SBY WHERE 7 RIVETS REPLACED DUE TO BEING SHEARED

Part: UNKNOWN — ODOR (COCKPIT) · airframe 47,129 hrs · 43,183 cycles

AFTER T/O, IN FLIGHT, STRONG CHEMICAL ODOR IN COCKPIT, LASTED WHOLE FLIGHT....FIX: RAN ENGINES WITH BLEEDS AND PACKS FOR 20 MINUTES.CLEANED RECIRC FAN INLET SCREENS AS REQ NO ODOR NOTED AT THIS TIME.OK FOR SERVICE.SEE SEQ IN WORK PACKAGE DATED 11/11/19 FOR T/S.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 47,089 hrs · 43,138 cycles

PITOT 1 MOMENTARILY DISPLAYED ON EICAS AFTER ENG START.....FIX:PITOT 1 CAUTION MESSAGE TRANSITORY OPS CHECK PITOT STATIC HEAT IAW 30-31-00 ALL PROBED HEATED ACCORDINGLY RAN ENG 2 AND THEN #1 CAUTION LIGHT NEVER APPEARED. STARTED #1 ENGINE AND THEN #2 CAUTION NEVER APPEARED

Part: RELAY — FAILED (PITOT HEAT) · airframe 47,089 hrs · 43,138 cycles

PITOT 1 INOP CAUTION MESSAGE APPEARED INTERMITTENTLY DURING TAXI....FIX: R&RD RELAY K0111 AND K0060 IAW 32-15-02. REF FIM 30-31-00. OPS CHECK GROUND TAXI CHECK GOOD.OK FOR SERVICE

Part: SENSOR — MALFUNCTIONED (PITOT) · airframe 47,084 hrs · 43,131 cycles

PDIS 620 30-31 2202552 29OCT19 PHL CLOSE PITOT 1 INOP CAUTION MESSAGE AFTER ENG START FACT 30OCT19 05:48 PHL R/R RELAY K0056 AND PITOT CURRENT SENSOR #1 K0053 IAW SWPM 20-13-03. R/R STATIC PITOT SENSOR IAW AMM 30-31-02.SLAVED PITOT SENSOR #1 IAW AMM 34-13-01. ALL NO FIX. FURTHER TROUBLE SHOOTING IS REQ'D. SEE LOG PAGE 220256 SEQ.#1. DISCREPANCY CURRENTLY IN WORK IN PHL

Part: SWITCH — MALFUNCTIONED (NR 1 PITOT) · airframe 47,078 hrs · 43,125 cycles

PDIS 620 30-31 2202542 28OCT19 PHL CLOSE PITOT 1 INOP CAUTION LIGHT ILLUMINATED AFTER PUSH BA CK. (INTERMITTENT) 20058 00 EK FACT 28OCT19 19:57 PHL RNRD PITOT #1 SWITCH, REF AMM 20-13-03 OPS CHECK REF AMM 30-31-00, OPS GOOD. A/C OK FOR SERVICE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 46,967 hrs · 42,990 cycles

FLIGHT DECK CEILING EMERGENCY LIGHT BULB INOP. REPLACED THE BULB. OPS CHECK GOOD

Part: ENGINE — POWER LOSS (NR 2) · airframe 44,926 hrs · 40,630 cycles

PDIS 620 76-10 1911661 27SEP18 ROA CLOSE REJECTED TAKE OFF DUE NO.2 ENGINE LOSS OF POWER. 26010 00 VAG FACT 27SEP18 22:52 ROA PERFORMED AC ENGINE RUN. START AND HIGH POWER IAW EM B AMM 71-00-01 NO DEFECTS NOTED OK FOR SERVICE.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 44,232 hrs · 39,839 cycles

A BURNING MATCH ODOR IN THE COCKPIT AND AT ROWS 4 - 6 FOR APPROXIMATELY 1 MINUTE DURING DESCENT, AROUND 20K FT. NOTHING ABNORMAL NOTED. CONDITION DID NOT RETURN REST OF FLIGHT. DROPPED PSU PANELS AT ROWS 4 - 6, INSPECTED AREA AND FOUND NO DISCREPANCIES. OK FOR SERVICE.

Part: BLEED VALVE — FAILED (NR 2) · airframe 44,179 hrs · 39,781 cycles

NR 2 BLEED VALVE FAILED EICAS MESSAGE DISPLAYED DURING TAKEOFF ROLL AFTER POWER LEVELS WERE ADVANCED. ABORTED THE TAKEOFF.

Part: BLEED VALVE — MALFUNCTIONED (NR 1) · airframe 44,179 hrs · 39,781 cycles

NR 1 BLEED VALVE FAILED EICAS MESSAGE DURING TAKE OFF. REJECTED THE TAKE OFF. R & R THE NR 1 BLEED VALVE IAW AMM MPP 36-11-05-04. OPS CHECKED GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 44,179 hrs · 39,781 cycles

DURING TAKEOFF ROLL, THE SPOILERS DEPLOYED AND THE NR 1 BLEED VALVE FAILED EICAS MESSAGES DISPLAYED. INSPECTED AND DETERMINED THE SPOILER DEPLOYMENT TO BE CONSISTENT WITH NORMAL GROUND SPOILER AUTO-DEPLOY SEQUENCE. ACFT OVER 30KTS AND TL RETARDED FOR REJECTED TAKEOFF. TROUBLESHOT THE NR 1 BLEED VALVE FAIL IAW FIM 36-11-00-810-805A. GROUND RAN THE ACFT AND PERFORMED AN OPS CHECK IAW 36-11-05-700-802-A. OPS CHECKED GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION (NR 2 BLEED) · airframe 44,161 hrs · 39,762 cycles

EICAS MESSAGE FOR THE NR 2 BLEED FAIL DURING TAKEOFF, ABORTED TAKEOFF. MESSGAE CLEARED PRIOR TO CREW ENGINE SHUT DOWN. GROUND RAN CND AND NO EICAS OR CMC MESSAGE. OK FOR SERVICE.

Part: WARNING MESSAGE — ILLUMINATED (NR 1 BLEED) · airframe 44,017 hrs · 39,599 cycles

NR 1 BLEED LEAK EICAS MESSAGE DURING CLIMBOUT, FOLLOWED QRH AND MESSAGE WENT OUT AFTER 3 MINUTES 20 SECONDS. OPEN.

Part: SENSOR — FAILED (NR 1 PACK TEMP) · airframe 44,017 hrs · 39,598 cycles

NR 1 BLEED LEAK EICAS MESSAGE, DURING CLIMBOUT. COMPLIED WITH QRH. MESSAGE WENT OUT. R & R DUCT TEMP SENSOR FOR THE NR 1 PACK IAW AMM 21-60-03-400-801A. OPS CHECKED GOOD. OK FOR SERVICE AT THIS TIME.

Part: WARNING MESSAGE — FALSE ACTIVATION (NR 1 BLEED) · airframe 44,017 hrs · 39,598 cycles

NR 1 BLEED LEAK EICAS MESSAGE DURING CLIMBOUT, COMPLIED WITH QRH, MESSAGE WENT OUT. INSPECTED IAW FIM 36-20-00-810-801-A, NO DEFECTS NOTED. PERFORMED AN OPS CHECK IAW AMM 36-00-00-700-803-A/500, OPS CHECKED GOOD, NO MESSAGES. OK FOR SERVICE.

Part: PULLEY BRACKET — CRACKED (FRAME 69) · airframe 43,342 hrs · 38,877 cycles

CARGO DOOR OPEN & CLOSE CABLE PULLEY SUPPORT AT FRAME 69 BETWEEN STRINGERS 4R AND 5R IS CRACKED APPROXIMATELY ONE INCH. -REMOVED AND REPLACED CABLE PULLEY BRACKET IAW SRM 51-40-02.

Part: HINGE FITTING — CRACKED (RT WING SPOILER) · airframe 43,342 hrs · 38,877 cycles

RT WING GROUND SPOILER HAS A .500 INCH CRACK ON THE OTBD HINGE FITTING. REMOVED AND REPLACED THE HINGE FITTING IAW AMM 20-10-01.

Part: FITTING — DAMAGED (PCU) · airframe 43,342 hrs · 38,877 cycles

RT AILERON PCU ATTACH FITTING HAS OVERSIZED HAT BUSH BORES. REMOVED AND REPLACED FITTING IAW EO EM-27MR-112

Part: ATTACH ANGLE — CRACKED (WG -BDY FAIRING) · airframe 43,342 hrs · 38,877 cycles

LEFT FUSELAGE TO WING FAIRING LATERAL PANEL. LOWER ATTACH ANGLE CRACKED AT THE AFT END. R & R THE ATTACH ANGLE IAW ETN-EM-53-142.

Part: DOOR — BINDING (MAIN CABIN) · airframe 43,333 hrs · 38,866 cycles

FA REPORTS MAIN CABIN DOOR DIFFICULT TO OPEN.AIRCRAFT FOUND TO BE WITHIN 5LBS OR LESS THAN THE MAX LOAD CRITERIA (45-50LBS)-C/A-DEFERRED PER FMR REF ETN-EM-52-029 TDMI AUTHORIZATION NUMBER 620T5251. PERFORMED THE ADJUSTMENT OF THE PASSENGER MAIN DOOR IN ACCORDANCE WITH AMM 52-18-00 AND REDUCED THE AVERAGE MAXIMUM LOAD OF THE INTERNAL HANDLE PULL TEST TO A VALUE OF LESS THAN 45LBS. COMPLETE:WITH ALL THE ADJUSTMENTS AND THE REPLACEMENTS OF PARTS STATED IN THE WIPS BELOW AND THE ACFT OFF JACKS. PERFORMED A FINAL PULL TEST ON THE PAX DOOR AND RECORD THE OUT OF DOCK VALUE OF 36 LBS. WHICH IS WITH IN LIMITS IAW AMM 52-18-00 THAT GIVES YOU A 50 LBS. MAX LIMIT TDMI RESTORED

Part: ROLLER — LACK OF LUBE (PAX DOOR) · airframe 42,822 hrs · 38,366 cycles

MAIN CABIN DOOR HARD TO OPEN. LUBRICATED THE HINGE ROLLERS IAW AMM-53-21-62. OPS CHECKED GOOD.

Part: DOOR — LACK OF LUBE (MAIN PAX) · airframe 42,510 hrs · 38,094 cycles

MAIN CABIN DOOR HARD TO OPEN. LUBRICATED THE MAIN DOOR AND PULL TESTED INTERNAL ACTUATING HANDLE IAW AMM 52-18-00 AND ETN EM-52-029. FOUND TO BE WITHIN LIMITS.

Part: RIB — CRACKED (FUSELAGE) · airframe 42,413 hrs · 37,995 cycles

SHEET METAL UNDER NR 2 WING LOOKS CRACKED BY WHEEL WELL. INSPECTED A/C AND FOUND 5.5" CRACK ON RT MLG AFT RIB PN 145-72166-002 ITEM TRANSFERRED TO LOG PAGE 4069199 ITEM 1. C/W PERMANENT REPAIR ON RT MLG AFT RIB IAW ERS-EM-5300-2647.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 42,253 hrs · 37,844 cycles

AFT GALLEY AFT SIDE EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE NR 3 INVERTER IAW AMM 33-50-11. OPS CHECKED GOOD.

Part: ROLLER — LACK OF LUBE (MAIN DOOR) · airframe 42,213 hrs · 37,807 cycles

FA STATES MAIN DOOR GETTING INCREASINGLY HARD TO OPEN AND CLOSE. LUBED MCD ROLLERS PER AMM 53-21-02. NO FURTHER DEFECTS NOTED.

Part: CRADLE — BROKEN (FWD FLASHLIGHT) · airframe 41,983 hrs · 37,589 cycles

FORWARD FLT ATTENDANT FLASHLIGHT BRACKET BROKEN. REMOVED AND REPLACED FLASHLIGHT ASSY IAW MM 33-50-16. OPS CHECKED OK.

Part: TRIM SWITCH — DIRTY (HORIZ STAB) · airframe 41,956 hrs · 37,564 cycles

P TRIM MAIN INOP. CLEANED ALL 3 PITCH TRIM SWITCHES PER AMM 27-40-03. PERFORMED FIM TASK 27-43-00-810-801 OPS CHECK PITCH & TRIM SYSTEM GOOD FOUND TO BE TRANSITORY CONDITION.

Part: ROLLER — LACK OF LUBE (PAX DOOR) · airframe 41,486 hrs · 37,132 cycles

MAIN CABIN DOOR IS VERY DIFFICULT TO OPEN. PERFORMED LUBE OF MAIN DOOR FRAME ROLLERS IAW MM 53-21-02 AND MAIN DOOR HANDLE ACTUATING TEST IAW MM 52-10-01 OP TEST OK

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 41,443 hrs · 37,089 cycles

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

Part: DOOR SEAL — LACK OF LUBE (PAX DOOR) · airframe 41,219 hrs · 36,897 cycles

MAIN PASSENGER DOOR IS HARD TO OPEN. LUBRICATED MAIN ENTRANCE DOOR RUBBER SEAL IAW-AMM-52-18-04, OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 40,896 hrs · 36,614 cycles

MAIN DOOR EMERGENCY LIGHT INOPERATIVE. R & R MAIN PASSENGER DOOR EMERGENCY LIGHT IAW AMM 33-50-06-000-801. OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 40,865 hrs · 36,574 cycles

MAIN DOOR EMERGENCY LT INOPERATIVE. R & R MAIN DOOR EMERGENCY LIGHT LAMP IAW AMM 33-50-06-000-801-A AND 33-50-06-400-801-A. OPS GOOD AT THIS TIME.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 40,734 hrs · 36,465 cycles

MAIN CABIN DOOR EMER LIGHT INOPERATIVE. R & R MAIN CABIN DOOR EMER LIGHT IAW AMM 33-50-06-000-801-A & 33-50-06-400-801-A. OPERATIONS CHECKED GOOD.

Part: SHUTOFF VALVE — TRIPPED (BRAKE SYSTEM) · airframe 40,707 hrs · 36,444 cycles

BRAKE INBD INOPERATIVE MSG PRESENTED UPON GEAR EXTENSION. PERFORMED GO AROUND & COMPLETED AOM 1 PROCEDURES, NORMAL LANDING, ALL BRAKE TEMPS INDICATOR REMAINED IN THE GREEN 324M3800. FOUND INBD SOV TRIPPED, RESET INBD BRAKES OPERATIONS CHECKED OK. R & R BCU FOR PRECAUTIONARY REASONS IAW AMM CH 32-41-02. BRAKE SYS FUNCTION CHECKED OK IAW AMM CH 32-41-00.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 40,463 hrs · 36,234 cycles

MAIN CABIN DOOR EMER LIGHT INOPERATIVE. R & R MAIN DOOR EMER LIGHT BULB IAW AMM 33-50-10-000-801-A & 33-50-01-400-801-A. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 40,251 hrs · 36,041 cycles

MAIN DOOR EXTERIOR EMER LIGHT INOPERATIVE. R & R MAIN DOOR EMER LIGHT LAMP IAW AMM 33-50-06-000-801-A & 33-50-06-400-801-A. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 40,138 hrs · 35,933 cycles

ROW 3 AISLE EMER LIGHT INOPERATIVE. REPLACED ROW 3 AISLE EMER OVERHEAD LIGHT BULB IAW AMM 33-50-08-000-801-A & 33-50-08-400-801-A.

Part: BALLAST — DEFECTIVE (CABIN) · airframe 39,747 hrs · 35,617 cycles

VERY STRONG NOXIOUS ODOR COMING FROM AN AREA AROUND 10A. REPLACED CEILING LIGHT BALLAST AT SEAT 9A IAW AMM 33-21-05 & PSU PANEL AT 8 - 9A IAW AMM 25-22-04. OPERATIONS CHECKED GOOD.

Part: SKIN — CRACKED (FUSELAGE) · airframe 39,574 hrs · 35,451 cycles

LEFT UPPER FUSELAGE SKIN CRACKED AT 1ST FASTENER BELOW STRINGER 2L ON FRAME 75. CRACK IS APPROX 3/8" LONG. LT UPPER FUSELAGE SKIN CRACKED JUST AFT OF FRAME 75 & ABOVE STRINGER 2L. CRACK IS APPROX 1/4" LONG. LT UPPER FUSELAGE SKIN CRACK REPAIRED IAW ERS-EM-53MR-1754.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 39,568 hrs · 35,448 cycles

THE SERVICE DOOR CUT OUT AFT FRAME IS CORRODED JUST BELOW THE BOTTOM ROLLER. PERFORMED REPAIR ON SERVICE DOOR CUT OUT AFT FRAME FOR CORROSION JUST BELOW BOTTOM ROLLER IAW ERS-EM-53-MR-1721.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 39,593 hrs · 35,469 cycles

LIGHTNING STRIKE BETWEEN FRAME 74 - 75, BETWEEN STRINGER 21L, FOUND DURING LIGHTNING STRIKE INSPECTION. ACCOMPLISHED LIGHTNING STRIKE REPAIR IAW ERS-EM-53MR-1749.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 39,593 hrs · 35,469 cycles

LIGHTNING STRIKE BETWEEN FRAME 72 - 73, BETWEEN STRINGER 21R - 20. ACCOMPLISHED LIGHTNING STRIKE REPAIR IAW ERS-EM-53MR-1750.

Part: SKIN — CRACKED (FUSELAGE) · airframe 39,593 hrs · 35,469 cycles

RIGHT UPPER FUSELAGE SKIN CRACKED ON FRAME 75 AT THE 1ST FASTENER BELOW STRINGER 2R. CRACK IS APPROX 1/2" LONG. ACCOMPLISHED REPAIR IAW ERS-EM-53MR-1748.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 39,568 hrs · 35,448 cycles

LIGHTNING STRIKE BETWEEN FRAME 62 - 63, BETWEEN STRINGER 21L & 21R. REMOVED DAMAGE BY DRILLING NR 21 HOLE AT THE STRIKE. INSTALLED BUTTON HEAD RIVET & WASHER IN DRILLED LOCATION IAW SRM 53-00-01 & 51-20-03.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 39,574 hrs · 35,450 cycles

LIGHTNING STRIKE ON EXTERNAL SKIN AFT OF FRAME 61, BETWEEN STRINGER 21L - 21R. REPAIRED LIGHTNING STRIKE ON EXTERNAL SKIN IAW ERS-EM-53MR-173.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 39,574 hrs · 35,450 cycles

LIGHTNING STRIKE BETWEEN FRAME 60 - 61 & BELOW STRINGER 21L - 21R. REPAIRED LIGHTNING STRIKE IAW ERS-EM-53MR-1738.

Part: FRAME — GOUGED (FUSELAGE) · airframe 39,566 hrs · 35,446 cycles

FRAME 65 GOUGED UPPER CTR AREA. REPAIRED FRAME 65 GOUGE IAW ERS-EM-53MR-1731.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 39,574 hrs · 35,451 cycles

LIGHTNING STRIKE, BETWEEN FRAME 59 & 60, BETWEEN STRINGER 21L - 21R. REMOVED DAMAGE BY DRILLING NR 21 HOLE AT THE STRIKE & INSTALLED BUTTON HEAD RIVET & WASHER IN DRILLED LOCATION IAW SRM 53-00-01 & 5120-03.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 39,574 hrs · 35,450 cycles

LIGHTNING STRIKE BETWEEN FRAME 75 - 75A, STRINGER 20R - 21R. PERFORMED LIGHTNING STRIKE REPAIR IAW SRM 53-00-01.

Part: WIRE — BROKEN (CABIN) · airframe 39,574 hrs · 35,451 cycles

CEILING PANEL 253 CLC HAS BROKEN WIRE, FOUND ON OPEN UP. REPAIRED EMER EXIT LIGHT WIRE ON PANEL 253CLC IAW SWPM 20-21-00.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 39,574 hrs · 35,450 cycles

LIGHTNING STRIKE, BETWEEN FRAME 71 - 72, STRINGER 21R, FOUND DURING LIGHTNING STRIKE INSPECTION. REMOVED DAMAGE BY DRILLING NR 10 HOLE AT THE STRIKE & INSTALLED BUTTON HEAD RIVET & WASHER IN DRILLED LOCATION IAW SRM 53-00-01 & 51-20-03.

Part: SKIN — CRACKED (FUSELAGE) · airframe 39,595 hrs · 35,471 cycles

THE EXTERNAL SKIN OF THE FUSELAGE IS CRACKED AT THE RIVET, AT FRAME 75 & 4 INCHES BELOW THE RT AFT CORNER OF THE DORSAL FIN. ACCOMPLISHED REPAIR TO RT UPPER FUSELAGE SKIN CRACKS IAW ERS-EM-53MR-1748.

Part: SKIN — CRACKED (FUSELAGE) · airframe 39,595 hrs · 35,471 cycles

THE EXTERNAL SKIN OF THE FUSELAGE IS CRACKED AT THE RIVET, AT FRAME 75 & 4 INCHES BELOW THE LT AFT CORNER OF THE DORSAL FIN. LT UPPER FUSELAGE SKIN CRACK REPAIRED IAW ERS-EM-53MR-1754.

Part: SKIN — CRACKED (FUSELAGE) · airframe 39,566 hrs · 35,446 cycles

RIGHT UPPER FUSELAGE SKIN CRACKED ON FRAME 75, AT THE 1ST FASTENER BELOW STRINGER 2R. CRACK IS APPROX 1/2" LONG. EASI 8071 USED, 100-500KHZ PROBE, FREQ=400 KHZ, V-GAIN=78.0, H-GAIN=65.0, LPF=100. ACCOMPLISHED REPAIR TO RT UPPER FUSELAGE SKIN CRACKS IAW ERS-EM-53MR-1748.

Part: SKIN — CRACKED (FUSELAGE) · airframe 39,566 hrs · 35,446 cycles

LEFT UPPER FUSELAGE SKIN CRACKED JUST AFT OF FRAME 75 & ABOVE STRINGER 2L. CRACK IS APPROX 1/4" LONG. REPAIRED IAW ERS-EM-53MR-1754.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 39,566 hrs · 35,446 cycles

NUMBER 7 EMER LIGHT STRIP INOPERATIVE. R & R NR 7 EMER LIGHT STRIP IAW AMM 33-50-12. OPERATIONS CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 39,006 hrs · 34,938 cycles

RED LIGHT ON CAPTAINS FLASHLIGHT IS NOT ILLUMINATED. R & R CAPTAINS FLASHLIGHT ASSEMBLY IAW AMM 33-50-16. OPERATIONS CHECKED GOOD.

Part: CRADLE — BROKEN (FLASHLIGHT) · airframe 38,796 hrs · 34,742 cycles

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

Part: SIGN — INOPERATIVE (CABIN) · airframe 38,575 hrs · 34,537 cycles

EMERGENCY LIGHTED SIGN ON THE AFT SIDE OF G2 GALLEY INOPERATIVE. INSTALLED SERVICEABLE EMER LIGHT IAW AMM 33-50-14. OPERATIONS CHECKED GOOD.

Part: DOOR — LACK OF LUBE (CABIN) · airframe 38,254 hrs · 34,254 cycles

MAIN CABIN DOOR HARD TO OPERATE. LUBE MAIN CABIN DOOR IAW AMM 52-118-00. OPERATIONS CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 38,083 hrs · 34,073 cycles

AFT CABIN EMER FLASHLIGHT INOPERATIVE. R & R AFT CABIN EMER FLASHLIGHT IAW TASK 33-50-16-000-801-A & TASK 33-50-16-400-801-A. OPERATIONS CHECKED GOOD.

Part: DUCT — CRACKED (RT RAM AIR) · airframe 38,046 hrs · 34,034 cycles

BURNING SMELL FROM PACK 2 UNDER FLIGHT ATTENDANT CONTROL. IN AUTO MODE UNDER PILOT CONTROL THE SMELL WENT AWAY. REF LOG PAGE 3754935 ITEM 2 RT ENG DUE REPLACEMENT. REF NRWC 620-ORD-02391. END DURING TROUBLESHOOTING OF BURNING SMELL FOUND RT RAM AIR DISTRIBUTION DUCT CRACKED. R & R RT RAM AIR DISTRIBUTION DUCT IAW AMM 21-25-01. COMPLIED WITH TECHNICAL SERVICES WORK SCOPE FOR ENGINE PRODUCING SLIGHT BURNING OIL SMELL AT POWER. REFERENCE NRWC 620-ORD-02391 FOR DISCREPANCIES GENERATED BY INSPECTION.

Part: SKIN — MELTED (LT ELEVATOR) · airframe 38,035 hrs · 34,021 cycles

FOUND LT ELEVATOR REPLACEABLE TIP & SURROUNDING SKIN TO BE MELTED NRWC 620-MQT- 02377. PERFORMED PERMANENT REPAIR IAW ERS-EM-55MR-232.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 37,424 hrs · 33,452 cycles

OVERHEAD EMER EXIT LIGHT AT EXIT ROW INOPERATIVE. R & R OVERHEAD EMER EXIT LIGHT IAW AMM 33-50-08. OPERATIONS CHECKED GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 37,263 hrs · 33,316 cycles

AFT EMER LIGHTS WILL NOT ILLUMINATE. R & R NR 4 EMER LIGHT BATTERY & CHARGER ASSEMBLY. OPERATIONS CHECKED GOOD IAW WORK CARD 33-700-19. BATTERY CHARGER ASSEMBLY PN 11-0049 SN 14895.

Part: UNKNOWN — MALFUNCTIONED (FUEL SYSTEM) · airframe 37,035 hrs · 33,141 cycles

DURING CLIMB NOTICED AIRPLANE WOULDN'T BURN FUEL FROM LT TANK WITH CROSS FEED OFF. PERFORMED ENG IDLE RUN ON BOTH ENGS IAW 72-00-00 & FOUND BOTH FUEL QTY INDICATORS OPERATING NORMAL, ALSO PERFORMED CHECK OF FUEL CROSS FEED VLV IAW MM 28-21-04 & NO DEFECTS FOUND. SYS OPERATING NORMAL. COMPLIED WITH FUEL QTY MEASURING STICK IAW AMM 12-11-04 & COMPARED TO DIGITAL READING, NO FAULT NOTED. PERFORMED POWER ENG RUNS IAW AMM 71-00-01. FUEL CONSUMPTION WAS IDENTICAL FOR BOTH ENGS NO FAULTS NOTED.

Part: FLASHLIGHT — INOPERATIVE (AFT CABIN) · airframe 36,480 hrs · 32,668 cycles

AFT FLIGHT ATTENDANT FLASHLIGHT INOPERATIVE. REPLACED FLASHLIGHT IAW AMM 25-60-04. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,375 hrs · 32,555 cycles

AISLE OVERHEAD EMERGENCY LIGHT AT SEAT 17 AB INOPERATIVE. R & R AISLE OVERHEAD EMERGENCY LIGHT LAMP AT SEAT 17 AB IAW AMM 33-50-10, OPERATIONS CHECKED GOOD.

Part: MECHANISM — LACK OF LUBE (CABIN DOOR) · airframe 36,227 hrs · 32,435 cycles

CABIN DOOR IS DIFFICULT TO OPEN FROM INSIDE THE ACFT. LUBRICATED MAIN DOOR MECHANIC SYS, OPERATION OF DOOR WORKING GOOD AMM 52-10-01.

Part: ELECTRONIC UNIT — FAILED (LANDING GEAR) · airframe 35,914 hrs · 32,175 cycles

AFTER TAKEOFF SELECTED GEAR UP EICAS INSTANTLY WENT FROM DOWN TO UP WITH NO TRANSITION INDICATION. CHECKED RMU, RMU INDICATED DOWN & LOCKED, EICAS INDICATED UP. GEAR POSITION IN QUESTION RAN ABNORMAL LG EXTENSION CHECKLIST, GEAR CAME DOWN WITH GEAR ELEC OVERRIDE SWITCH IN GEARS & DOORS POSITION. DECLARED EMERGENCY, LANDED SAFELY MIA. R & R LGEU IAW AMM 32-32-01 & PERFORMED OPERATIONS CHECK IAW AMM 32-30-00.

Part: UNKNOWN — ODOR · airframe 35,780 hrs · 32,072 cycles

LIGHTNING STRIKE, SVC BUS CB POPPED. BURNING SMELL NOTICED. TRANSFERRED TO NRWC 620-CVG-01921. COMPLIED WITH LIGHTNING STRIKE INSPECTION WORK CARD 05-200-00.

Part: PROBE — FAILED (NR 1 TAT) · airframe 35,742 hrs · 32,044 cycles

AFTER DEPARTURE GOT TAT 1 HEAT FAIL ON EICAS. ACFT WAS REMOVED FROM SERVICE. R & R NR 1 TAT PROBES IAW AMM 34-15-03. OPERATIONS CHECKED GOOD AT THIS TIME, MEL 30-17 RESTORED.

Part: WIRE — DAMAGED (CABIN) · airframe 35,703 hrs · 32,011 cycles

EMERGENCY LIGHT STRIP AT ROW 17 & 18 INOPERATIVE. AIRCRAFT WAS REMOVED FROM SERVICE. INSTALLED REMOVABLE SPLICES IAW EMB 145 WM 20-21-00. OPC GOOD. MEL RESTORED

Part: LEVER — FAULTY (SPOILER SYS) · airframe 35,602 hrs · 31,927 cycles

DECLARED EMERGENCY DFW INADVERTENT SPOILER OPEN IN FLIGHT. DURING MAINTENANCE INSPECTION ON FLIGHT 2871 FOUND USED SPEDBRAKE DURING DESCENT AND FAILED TO RETRACT WHEN COMMANDED TO FOLLOWED EPC + AOM AND RETRACTED SPEED BRAKES. AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED SPEED BRAKE COMMAND LEVER IAW EMB AMM 27-63-03.OPS CHECK GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (SPOILER) · airframe 35,489 hrs · 31,827 cycles

SPOILERS WOULD NOT CLOSE AFTER ACTIVATION. CLOSED SPOILERS & THEY STAYED OPEN. TRANSFERRED TO NRWC 620-CMH-0183. R & R SPOILER CONTROL UNIT IAW AMM 27-63-02, OPERATIONS CHECKED GOOD IAW NRWC 620-CMH-01831.

Part: SPOILER — MALFUNCTIONED (WING) · airframe 35,488 hrs · 31,826 cycles

SPOILERS WOULD NOT CLOSE AFTER ACTIVATION CLOSED SPOILERS & THEY STAYED OPEN.

Part: UNKNOWN — MALFUNCTIONED (SPOILER) · airframe 35,486 hrs · 31,825 cycles

SPOILERS WOULD NOT STOW AT BOTTOM OF DESCENT WITH HANDLE IN CLOSED POSITION, THRUST LEVERS ADVANCED. PULLED CBS IAW AOM. INSPECTED SPOILER HYD ACTUATION & PERFORMED SPOILER SYS OPERATIONS CHECK IAW AMM 27-62-00 & 27-63-01. NO DEFECTS NOTED, OPERATIONS CHECKED GOOD. NO SPOILER CMC MESSAGES FROM TODAY 12-28-13.

Part: WIRE — DAMAGED (CABIN) · airframe 35,257 hrs · 31,638 cycles

FOUND 2 FLOOR PROXIMITY LIGHT WIRES AT FRAME 33 BETWEEN STRINGERS 15L & 16L DAMAGED. REPLACED 2 FLOOR PROXIMITY LIGHT AT FRAME 33 BETWEEN STRINGERS 15L & 16L IAW EMB 145 SWPM 20-21-00.

Part: SKIN — CORRODED (FRAMES 13 - 14) · airframe 35,257 hrs · 31,638 cycles

INTERNAL FUSELAGE SKIN CORRODED BETWEEN FR-13 AND FR-14 STR-20R TO STR-18R. REPAIRED IAW AEA EO-53MR-2230.

Part: SHEAR TIE — CORRODED (FRAME 65) · airframe 35,257 hrs · 31,638 cycles

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

Part: WIRE — DAMAGED (CABIN) · airframe 35,257 hrs · 31,638 cycles

EMERGENCY LIGHT STRIP NR 3 HAS DAMAGED WIRE. R & R NR 3 EMERGENCY LIGHT STRIP IAW EMB 145 AMM 33-50-10, OPERATIONS CHECKED GOOD.

Part: CONNECTOR — MISSING (CABIN) · airframe 35,257 hrs · 31,638 cycles

NUMBER 6 PROXIMITY LIGHT, ACFT SIDE CONNECTORS MISSING 2. REPLACED THE NR 6 PROXIMITY LIGHT, ACFT SIDE CONNECTORS THAT WERE MISSING 2 IAW EMB 145 SWPM 20-00-03 PG 65, OPERATIONS CHECKED GOOD.

Part: CONNECTOR — MISSING (CABIN) · airframe 35,257 hrs · 31,638 cycles

NUMBER 2 PROXIMITY LIGHT, ACFT SIDE CONNECTOR MISSING. REPLACED THE NR 2 PROXIMITY LIGHT, ACFT SIDE CONNECTOR THAT WAS MISSING IAW EMB145 SWPM 20-00-03, OPERATIONS CHECKED GOOD.

Part: HOLDER — BROKEN (CABIN) · airframe 35,257 hrs · 31,638 cycles

EMERGENCY LIGHT HOLDER FLOOR STRIP BROKEN. EMERGENCY LIGHT HOLDER FLOOR STRIP R & R IAW EMB 145 AMM 33-50-12.

Part: BATTERY — INOPERATIVE (CABIN) · airframe 35,257 hrs · 31,638 cycles

IAW AEA WC 33-700-19, REMOVED BATTERY PN 2013-1A & SN 103165.

Part: CONNECTOR — MISSING (CABIN) · airframe 35,257 hrs · 31,638 cycles

NUMBER 4 PROXIMITY LIGHT, ACFT SIDE CONNECTOR MISSING. REPLACED THE NR 4 PROXIMITY LIGHT, ACFT SIDE CONNECTOR THAT WAS MISSING IAW EMB 145 SWPM 20-00-03 PG 65, OPERATIONS CHECKED GOOD.

Part: CONNECTOR — MISSING (CABIN) · airframe 35,257 hrs · 31,638 cycles

NUMBER 5 PROXIMITY LIGHT, ACFT SIDE CONNECTOR MISSING. REPLACED THE NR 5 PROXIMITY LIGHT, ACFT SIDE CONNECTOR THAT WAS MISSING IAW EMB145 SWPM 20-00-03 PAGE 65, OPERATIONS CHECKED GOOD.

Part: HANDSET — UNKNOWN (CABIN) · airframe 35,037 hrs · 31,456 cycles

FWD F/A HEADSET IN CABIN HAS AN ODOR TO IT. R & R F/A HEAD SET, IAW AMM 23-31-03. OPS CHECK GOOD.

Part: ENGINE — SHUTDOWN (NR 2) · airframe 34,637 hrs · 31,124 cycles

WHILE AWAITING GPU CONNECTION WITH NR 2 ENGINE RUNNING, ENGINE SHUTDOWN ON ITS OWN BOTH FUEL PUMPS WERE OFF. PERFORMED A FUEL LOW PRESSURE WARNING TEST ALSO PERFORMED ENGINE RUN AND SHUTDOWN IAW GROUND HANDLING CHECKLIST SYS FOUND TO BE OPERATING NORMAL IAW AMM 28-45-00 AND 72-00-00.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 33,995 hrs · 30,594 cycles

DURING B INSEPECTION, FOUND THE SERVICE DOOR EMERGENCY EXTEROR LIGHT INOPERATIVE DUE TO A BROKEN WIRE. REPAIRED BROKEN WIRE IAW EMB WM 20-21-00. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (LT WING) · airframe 33,995 hrs · 30,594 cycles

DURING B INSPECTION FOUND THE LEFT WING EMERGENCY LANDING LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT EMERGENCY LANDING LIGHT LAMP IAW EMB AMM 33-41-02-000-801-A AND 33-41-02-400-801-A. THE OPERATIONAL CHECK WAS GOOD. NO DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 33,869 hrs · 30,501 cycles

DURING MAINTENANCE INSPECTION FOUND THE CAPTIAN’S EMERGENCY FLASHLIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CAPTAIN’S EMERGENCY FLASHLIGHT IAW EMB AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE — BROKEN (CABIN) · airframe 33,786 hrs · 30,429 cycles

DURING B INSPECTION FOUND THE SERVICE DOOR EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE SERVICE DOOR LIGHT LAMP IAW EMB 145 AMM 33-26-05-000-801-A AND 33-26-05-400-801-A, NO FIX. INSPECTED FOUND BROKEN WIRE. REPAIRED PER WIRING MANUAL 20-50-00. THE OPERATIONAL CHECK OF THE LIGHT LAMP WAS GOOD AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: O-RING — ACTIVATED (BLEED AIR SYS) · airframe 33,620 hrs · 30,290 cycles

ON FLIGHT 3572 THE CREW REPORTED THAT SHORTLY AFTER TAKEOFF THE MASTER WARNING WENT OFF AND THEY RECEIVED A RED "BLD 2 LEAK" EICAS MESSAGE. AN ASSOCIATED CONDITION: RADIOS BECAME SCRATCHY AND UNREADABLE. THE CREW DECLARED AN EMERGENCY AND ELECTED TO RETURN TO SDF. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE "O" RINGS AT BLEED SYSTEM 2 JOINT 18 IAW AMM CH 36-11-10. NO LEAKS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 33,272 hrs · 30,042 cycles

DURING B INSPECTION FOUND THE RIGHT AFT OVERWING EMERGENCY MARKED IN CABIN DID NOT ILLUMINATE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 5 AC/DC INVERTER IAW EMB AMM 33-50-11. THE OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM AND RIGHT AFT OVERWING CABIN EMERGENCY MARKER GOOD IAW EMB AMM 33-50-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: UPLOCK — FAULTY (RT MLG) · airframe 33,154 hrs · 29,951 cycles

ON FLIGHT 3564 THE CREW REPORTED THAT AFTER THEY RETRACTED THE GEAR AFTER TAKEOFF, THE CREW HEARD REPETITIVE BANGING NOISE AND RIGHT MAIN GEAR CYCLED FROM UP & LOCKED TO IN TRANSITION BACK TO UP & LOCK EVERY 2 MINUTES. CREW TOOK DELAY VECTORS TO BURN OFF GAS - LANDED BELOW MAX LANDING WEIGHT. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED & REPLACED THE RIGHT MAIN LANDING GEAR UPLOCK BOX IAW EMB 145 AMM 32-33-10. PERFORMED OPERATIONAL CHECK OF THE LANDING GEAR. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONNECTOR — LOOSE (RT MLG) · airframe 33,154 hrs · 29,951 cycles

ON FLIGHT 3458 THE CREW REPORTED THAT ON LANDING GEAR RETRACTION THEY HAD A CONSTANT BANGING NOISE WITH RIGHT MAIN GEAR LIGHT CYCLING FROM WHITE (UP) TO AMBER (UNSAFE). THE CREW DECLARED AN EMERGENCY AND RETURNED TO MIA. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND ELECTRICAL CONNECTOR BOTTOM ON RIGHT UPLOCK BOX PROX SWITCH LOOSE. RE-INSTALLED IAW EMB 145 AMM 32-33-10 AND C/W EXT AND RETRACTION, THE OPERATIONAL TEST CHECK WAS GOOD IAW EMB 145 AMM 33-30-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: HOLDER — BROKEN (FLASHLIGHT) · airframe 33,100 hrs · 29,911 cycles

FOR FLIGHT 4078 THE CREW REPORTED THE CAPTAIN’S FLASHLIGHT HOLDER WAS BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED FLASHLIGHT. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ACM — FAILED (AC BAY) · airframe 33,066 hrs · 29,881 cycles

ON FLIGHT 3207 THE CREW REPORTED THAT IMMMEDIATELY UPON SELECTING ON AIR CONDITIONING A SQUEAL SOUND WAS HEARD FOLLOWED BY AN ELECTRICAL SMOKE SMELL FROM THE NR 2 PACK. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED RIGHT HAND AIR CYCLE MACHINE AND CORECTED ALL DUCT LEAKS IAW EMB-145 AMM 21-51-03. ALL OPS CHECKS AND LEAK CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN)

RIGHT OVERWING EMERGENCY LIGHT INOPERATIVE. REPLACED NR 3 EMERGENCY BATTERY AND CHARGER.

Part: FLASHLIGHT — BROKEN (COCKPIT) · airframe 32,440 hrs · 29,369 cycles

DURING MAINTENANCE INSPECTION FOUND THE FIRST OFFICER’S FLASHLIGHT SWITCH BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FIRST OFFICER’S FLASHLIGHT IAW EMB 145 AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,258 hrs · 29,218 cycles

DURING B INSPECTION FOUND THE EMERGENCY LIGHT AT ROW 12A INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT OVERWING EMERGENCY LIGHT LAMP AT SEAT 12A IAW EMB 145 AMM 33-50-07-000-801-A AND 33-50-07-400-801-A. THE OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT IS RETURNED TO SERVICE.

Part: PITOT LINE — CONTAMINATED · airframe 31,892 hrs · 28,961 cycles

FLIGHT 3584, CREW REPORTED IN CRUISE AT FLIGHT LEVEL 370 HAD WING ICE FAIL. TROUBLESHOT PAIR AND PERFORMED AOM VOL 1. NOTHING DETECTED TO FL 210 AND EXITED IN AFTER ABOUT 5 MINUTES ICE DISAPPEARED AND AIRFRAME WAS CLEAR. IAS FLAGGED ASSOCIATED TO PROBE HEAT FAIL AFTER RESET PROCEDURE ENGINE AND STAB ICE RETURNED AND OPERATED NORMALLY WING NEVER WORKED. TURNED BACK, BOTH PFD UNRELIABLE AIRSPEED FOR 30 SEC-1 MIN ACTED LIKE ALTIMETER. DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE. LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. DURING INSPECTION, FOUND EXCESSIVE WATER ON PITOT LINES. DRAINED PITOT LINES IAW AMM 34-13-00. PERFORMED PITOT-STATIC PORTS HEATING OPS CHECK IAW AMM 30-31-00. OPS CHECKED GOOD. PERFORMED FUNCTIONAL TEST OF ADC SYSTEM IAW AMM 34-15-00. FUNCTIONAL TEST WAS GOOD AND PERFORMED OPS TEST OF ICE DETECTION SYSTEM IAW AMM 30-80-00. NO FAULTS FOUND. PERFORMED ANTI-ICING SYSTEM OPS CHECK IAW AMM 30-00-00. FOLLOWED FIM TASK 75-41-00-810-803 AND CHECKED WIRES AND CONNECTORS IAW MM 70-00-00. PERFORMED TEST OF ENGINE IAW 72-00-00. OPS CHECKED GOOD. NO FURTHER DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: CRADLE — BROKEN (FLASHLIGHT ASSY) · airframe 31,820 hrs · 28,913 cycles

FLIGHT 4314, CREW REPORTED THE FORWARD CABIN FLASHLIGHT BRACKET BROKEN. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE CABIN FLASHLIGHT BASE IAW AMM 33-50-00. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,067 hrs · 28,318 cycles

DURING B-INSPECTION FOUND THE RIGHT SIDE EXIT ROW EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERIVCE. REMOVED AND REPLACED RIGHT SIDE EXIT ROW EMERGENCY LIGHT IAW AMM 33-50-14. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 30,673 hrs · 28,006 cycles

DURING B-INSPECTION FOUND THE AFT FLASHLIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AFT FLASHLIGHT IAW EMB AMM TASKS 33-50-16-000-801-A AND 33-50-16-400-801-A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: DE-ICE VALVE — UNSERVICEABLE (RT WING) · airframe 30,649 hrs · 27,988 cycles

DURING TAKEOFF ON FLIGHT 2704 CREW RECEIVED WING ANTI-ICE FAIL CAUTION MESSAGE. ON DESCENT CREW FOLLOWED AOM PROCEDURE WING ANTI-ICE FAIL CAUTION RETURNED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED RIGHT WING ANTI-ICE LOW PRESSURE SWITCH IAW AMM#30-11-02. DID NOT SOLVE THE PROBLEM TRANSFERRED TO ITEM 2 SAME LOG PAGE REMOVED AND REPLACED THE RIGHT WING ANTI-ICE VALVE IAW EMB 145 MM CH 30-10-01 OPERATIONAL CHECKS GOOD. THE AIRCRAFT RETURN TO SERVICE.

Part: COVER — OUT OF ADJUST (EMERGENCY EXIT) · airframe 30,635 hrs · 27,978 cycles

DURING MAINTENANCE RIGHT EMERGENCY EXIT CATCHES AT THE TOP. THE AIRCRAFT WAS REMOVED FROM SERVICE. ADJUSTED RIGHT EMERGENCY EXIT HATCH COVER IAW EMB 145 AMM 25-23-03. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: RIB — CRACKED (RT WING) · airframe 30,635 hrs · 27,977 cycles

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

Part: MOUNT — CRACKED (LT ENGINE) · airframe 30,635 hrs · 27,977 cycles

DURING MAINTENANCE INSPECTION, FOUND THE LEFT ENGINE FORWARD LOWER MOUNT YOKE CRACKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED CRACKED MOUNT, PREPPED AND INSTALLED SERVIABLE MOUNT IAW AEA EO EM-53MR-386. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE — BROKEN (CABIN) · airframe 30,694 hrs

DURING B-INSPECTION FOUND THE NR 4 AND NR 5 EMERGENCY LIGHT STRIP HAS BROKEN WIRES. ALSO FOUND THE EMERGENCY LIGHT ON FORWARD LOWER SERVICE DOOR SHROUD PANEL HAS BROKEN WIRES. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 4 & NR 5 EMERGENCY LIGHT STRIP IAW EMB 145 AMM 33-50-12. REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT ON THE FORWARD LOWER SERVICE DOOR SHROUD IAW EMB 145 AMM 33-50-13. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: PUMP — FAILED (HYDRAULIC SYS) · airframe 30,397 hrs · 27,808 cycles

ON FLIGHT 3591 THE CREW REPORTED THE HYDRAULIC 2 PUMP FAILED/ELEC HYD 2 PUMP OPERATIONAL AT 2800 PSI IN AMBER QTY. THE CREW ELECTED TO DIVERT. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND BROKEN LINE ON ELECTRIC HYD PUMP. REMOVED AND REPLACED THE LINE 29-10-04. LEAK CHECK GOOD. ALSO AFTER RUNNING ELECTRIC PUMP MASS AMOUNT OF SMOKE FROM EXHAUST VENT. REMOVED AND REPLACED PUMP IAW EMB 145 AMM 24-10-04. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 29,933 hrs · 27,443 cycles

FOR FLIGHT 3358 MAINTENANCE FOUND THE CAPTION’S FLASHLIGHT LED CHARGING LIGHT DOES NOT ILLUMINATE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED CAPTAIN’S FLASHLIGHT ASSEMBLY IAW EMB-145 AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — DEFECTIVE (COCKPIT)

DURING MAINTENANCE INSPECTION FOUND THE CAPTAINS FLASHLIGHT LED CHARGING LIGHT DOES NOT ILLUMINATE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED CAPTAINS FLASHLIGHT ASSEMBLY IAW EMB-145 AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 29,008 hrs · 26,740 cycles

FOR FLIGHT 4068 MAINTENANCE DISCOVERED THE EMERGENCY LIGHTS WERE LEFT ON OVERNIGHT. ALL OF THE EMERGENCY LIGHT BATTERIES WERE DEAD. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 1, 2, 3 AND 4 EMERGENCY BATTERY AND CHARGER IAW WC 33-700-19. PART NUMBERS AND SERIAL NUMBERS FOR NR 1: 2013-1A, 71097, BA50933901, CO1622. PART NUMBERS AND SERIAL NUMBERS FOR NR 2: 2013-1A, 84695,BA509333901, CO2469. PART NUMBERS AND SERIAL NUMBERS FOR NR 3: 2013-1A, 109778,BA509333901, CO2464 .PART NUMBERS AND SERIAL NUMBERS FOR NR 4: 2013-1A, 109789,BA509333901, CO2639. THE OPERATIONAL CHECK GOOD WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CDU — OVERHEATED (COCKPIT) · airframe 28,445 hrs · 26,321 cycles

ON FLIGHT 2815 DURING THE CLIMB THE CREW REPORTED A STRONG ELECTRICAL ODOR IN THE COCKPIT AND FORWARD PORTION OF AIRCRAFT. NO VISUAL SMOKE WAS NOTED. THE CREW ELECTED TO RETURN TO DFW. THE AIRCRAFT LANDED WITHOUT INCIDENT. PERFORMED INSPECTION OF ALL ITEMS IN COCKPIT. FOUND THE NR 1 FLIGHT MANAGEMENT SYSTEM CONTROL DISPLAY UNIT OVERHEATING AND FIRST OFFICER’S FLASHLIGHT HAD ELECTRICAL BURNT SMELL. REMOVED AND REPLACED THE CAPTAINS CONTROL DISPLAY UNIT P/N OFF 1117-11 S/N OFF: 1210. REMOVED AND REPLACED THE FIRST OFFICERS FLASHLIGHT P/N OFF: P2-07-0009-520. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: UPLOCK — MALFUNCTIONED (MLG) · airframe 27,983 hrs · 26,006 cycles

ON FLIGHT 3656 THE CREW REPORTED THE NR 1 MAIN LANDING GEAR FAILED TO SHOW UP AND LOCKED. AMBER IN TRANSIT INDICATION STAYED ON UNTIL THE RED LANDING GEAR LEVER DISAGREE WARNING ACTIVATTED. RECEIVED 3 DOWN GREEN WHEN SELECTED DOWN DISAGREE MESSAGE EXTINGUISHED. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT MAIN LANDING GEAR UPLOCK BOX IAW EMB AMM 32-33-10. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONTROL UNIT — MALFUNCTIONED (SPOILER) · airframe 27,854 hrs · 25,912 cycles

ON FLIGHT 3252 THE CREW REPORTED A SPOILER FAIL MESSAGE ON EICAS WITH THE SPOILER OPEN INDICATION WITH NO NOTICEABLE ACTUAL DEPLOYMENT IN FLIGHT. THE CAPTAIN DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. TESTED LEFT AND RIGHT INBOARD PROXIMITY SWITCHES AND OPERATED NORMALLY. REMOVED AND REPLACED THE SPOILER CONTROL UNIT IAW EMB 145 AMM 27-63-0. THE OPERATIONAL CHECK WAS GOOD AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: PROFILE — CRACKED (LT PYLON) · airframe 25,654 hrs · 24,204 cycles

DURING MAINTENANCE BASE VISIT FOUND THE LEFT PYLON PROFILE TO HAVE CRACKS. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED REPAIR ON THE LEFT PYLON PROFILE IAW EO EM-54MR-312. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 25,654 hrs · 24,204 cycles

DURING THE MAINTENANCE BASE VISIT FOUND THE RIGHT OMEGA BEAM AT FRAME 25 TO BE CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED THE RIGHT OMEGA BEAM AT FRAME 25 IAW EMB 145 SRM 53-00-10 FIGURE 203 SHEET 1. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: UNKNOWN — SMOKE (COCKPIT) · airframe 23,567 hrs · 23,980 cycles

ON FLIGHT 2735 THE CREW ABORTED THE TAKEOFF AT THE START OF THE TAKE OFF ROLL DUE TO EXCESSIVE SMOKE IN THE COCKPIT AND FRONT OF CABIN. THE AIRCRAFT RETURNED TO THE GATE WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED AN OPERATIONAL CHECK OF BOTH ENGINES IAW ETN EM-72-034R4. NO SMOKE OR SMOKE SMELL WERE FOUND. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: PRESSURE SWITCH — FAULTY (RUDDER) · airframe 25,064 hrs · 23,737 cycles

ON FLIGHT 3526 DURING CRUISE THE CREW REPORTED THE RUDDER SYSTEM 1-2 INOPERABLE IN FLIGHT. SYSTEM 1 ACTIVATED WHEN NR 2 SYSTEM WAS SHUTOFF PER CHECKLIST. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 2 SYSTEM RUDDER PRESSURE SWITCH IAW AMM 27-23-04. OPERATIONAL CHECK WAS GOOD AND NO LEAKS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 24,910 hrs · 23,618 cycles

ON FLIGHT 3579 ON DESCENT THE CAPTAIN REPORTED THAT WHEN SELECTING FLAPS 9, RECEIVED A FLAP FAIL MESSAGE IMMEDIATELY. THE FLAPS DID NOT MOVE FROM THE ZERO POSITION. THE CAPTAIN DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. IT WAS NOT AN OVERWEIGHT LANDING. AFTER LANDING THE MESSAGE CLEARED PRIOR TO ARRIVING AT THE GATE. THE AIRCRAFT WAS REMOVED FROM SERVICE. RESET FLAPS AND PERFORMED FLAP CONTROL SYSTEM OPERATIONAL CHECK IAW AMM 27-51-00. NO PARTS REMOVED OR PLACED. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: HEATER — ODOR (WINDSHIELD)

ON FLIGHT 3956, CREW REPORTED ELECTRICAL BURNING ODOR AT GATE FROM COCKPIT. AIRCRAFT REMOVED FROM SERVICE. OPERATED ELECTRICAL SYSTEM AND WINDSHIELD HEAT IAW AMM 30-43-00. COULD NOT DUPLICATE. AIRCRAFT RETURNED TO SERVICE.

Part: CAP — OPEN (FUEL CELL)

ON FLIGHT 4431 - CREW REPORTED ON THE GROUND, LT WING TANK FUEL CAP CAME OPEN IN FLIGHT. FUEL CAP WAS ONLY SECURED BY THE LANYARD. CREW ELECTED TO RETURNED TO THE FIELD. AIRCRAFT REMOVED FROM SERVICE. COMPLIED WITH FUEL CAP SEAL INSPECTION. RE-INSTALLED CAP, NO DEFECTS NOTED. INSPECTED SURROUNDING AREAS. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. (A)

Part: CAP — OPEN (FUEL CELL)

ON FLIGHT 4431, CREW REPORTED ON THE GROUND. LT WING TANK FUEL CAP CAMEO OPEN IN FLIGHT. FUEL CAP WAS ONLY SECURED BY THE LANYARD. CREW DECLARED AN EMERGENCY AND ELECTED TO RETURN TO THE FIELD. AIRCRAFT REMOVED FROM SERVICE. COMPLIED WITH FUEL CAP SEAL INSPECTION. RE-INSTALLED CAP, NO DEFECTS NOTED. INSPECTED SURROUNDING AREAS. NO DEFECTS NOTED AIRCRAFT RETURNED TO SERVICE. (A)

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 18,921 hrs · 18,389 cycles

EMERGENCY LIGHTS INOPERATIVE DUE TO SWITCH LEFT IN ARM POSITION. REMOVED AND REPLACED BATTERY PACKS 1 THRU 4 IAW EMB AMM 33-50-04. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: INLET — CONTAMINATED (APU) · airframe 18,748 hrs · 18,190 cycles

BURNING SMELL IN CABIN WITH APU AND NUMBER ONE ENGINE RUNNING, FOUND BUGS IN APU INLET. CLEANED BUGS FROM APU INLET IAW EMB AMM. OPERATIONAL CHECK GOOD WITH NO SMELL DETECTED, RETURNED AIRCRAFT TO SERVICE.

Part: ACM — SEIZED (ZONE 100) · airframe 18,745 hrs · 18,185 cycles

DURING DEBOARDING NOISE HEARD FROM OUTSIDE OF AIRCRAFT FOLLOWED BY A SLIGHT SMOKE SMELL IN CABIN WITH APU AND NUMBER TWO PACK OPERATING, FOUND NUMBER TWO PACK SEIZED. REMOVED AND REPLACED NUMBER TWO PACK IAW EMB AMM 21-51-03. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE.

Part: SKIN — CRACKED (CARGO DOOR)

DURING OVERNIGHT MAINTENANCE, CARGO DOOR AFT UPPER CORNER OF SKIN WAS FOUND CRACKED. REPLACED CARGO DOOR ASSEMBLY IAW EMB AMM 52-30-01 AND 52-31-00. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: CONTROL UNIT — FAILED (HORIZONTAL STAB)

EN ROUTE TO LIT AIRCRAFT EXPERIENCED DUAL PITCH TRIM FAILURE. AIRCRAFT LANDED SAFELY WITH NO FURTHER INCIDENTS. REPLACED HORIZONTAL STABILIZER CONTROL UNIT. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SKIN — DENTED (FUSELAGE)

ABI - A 12 INCH BY 8.5 INCH DOUBLER FROM A PREVIOUS REPAIR WAS REMOVED FOR EVALUATION DUE TO PROXIMITY OF AN ADDITIONAL DENT AT FRAME 64 STRINGER 20L. RECONTOURED THE ADDITIONAL DENT AND PERFORMED AND EDDY CURRENT INSPECTION WITH NO REJECTABLE INDICATIONS. FABRICATED A NEW REPAIR DOUBLER, FILLER. REPAIR DONE IAW EMB REPAIR STATEMENT IC2004-145/4345 PARA 3 DATED SEPT 16, 2004. (M)

Part: SILL — CORRODED (SERVICE DOOR)

ABI - DURING AN MBV INSPECTION, THE SERVICE DOOR CENTER SILL WAS FOUND CORRODED. REMOVD THE EXISTING CENTER SILL AND INSTALLED NEW SILL IAW EMB 145 SRM, SRM 145/1142 REV 27, CHAPTER 51-20-01-51-20-03, 51-40-02, 51-40-04 AND 51-40-06. (M)

Part: WARNING LIGHT — FALSE ACTIVATION (COCKPIT WINDOW)

ON CLIMB-OUT CREW NOTICED YELLOW TAB INDICATING CAPTAINS DV WINDOW OPENED. CREW RETURNED TO FIELD WITH NO FURTHER INCIDENT. MAINTENANCE INSPECTED AND PERFORMED OPERATIONAL CHECK OF WINDOW WITH NO DEFECTS NOTED. LOCKED WINDOW AND RETURNED AIRCRAFT TO SERVICE. (M)

Part: CONTROL UNIT — FAILED (PITCH TRIM)

CREW HAD A DUAL PITCH TRIM FAILURE DURING DESCENT AT 210 KTS AND ALT OF 6,000 FT. FLAPS WERE AT 9 AND SPEED BRAKES WERE BEING DISENGAGED. REPLACED HSCU IAW MFG AMM. OPERATIONAL CHECK GOOD. AC RETURNED TO SERVICE. (SW21200406970)

Part: CLAMP — LOOSE (E/E BAY)

ORF - FLT 4025 - CREW REPORTED A BLEED LEAK MESSAGE ON EICAS DURING CRUISE FLIGHT. CAPTAIN DECLARED AN EMERGENCY AND CONTINUED TO ORF AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND A LOOSE V-BAND CLAMP IN THE AFT AVIONICS COMPARTMENT. CLAMP WAS TIGHTENED AND OPERATIONAL CHECK WAS COMPLIED WITH. AIRCRAFT WAS THEN RETURNED TO SERVICE. (M)

Part: DISPLAY — LIGHTNING STRIKE (COCKPIT)

CREW REPORTED A BRIGHT FLASH AT CAPTAINS WINDOW FOLLOWED BY AN ELECTRICAL SMOKE SMELL, LOSS OF NUMBER 4 GENERATOR. NUMBER 2 COMM, AND FMS SCREEN. AN EMERGENCY WAS DECLARED AND AIRCRAFT WAS LANDED WITHOUT FURTHER INCIDENTS. MAINTENANCE COMPLIED WITH A LIGHTENING STRIKE INSPECTION. GENERATOR WAS REPLACED. NUMBER 2 ICU WAS REPLACED, WHICH FIXED THE SMOKE SMELL. AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE)

DURING AN IMBV INSPECTION FOUND CORROSION ON GALLEY CENTER FLOOR BEAM. REMOVED CORRODED GALLEY CENTER BEAM. INSTALLED NEW FLOOR BEAM IAW SRM AND STANDARD SRM PRACTICES.

Part: FLOORBEAM — CORRODED (FUSELAGE)

DURING IMBV INSPECTION FOUND CORROSION ON GALLEY RIGHT HAND FLOORBEAM. REMOVED CORRODED GALLEY RT BEAM. INSTALLED NEW BEAM IAW STANDARD SRM PRACTICES.

Part: FLOORBEAM — CORRODED (FUSELAGE)

DURING IMBV INSPECTION, FOUND CORROSION ON FORWARD DIGITAL REMOVED CORROSION BY CUT OUT. FABRICATED A REPLACEMENT STRAP, TWO DOUBLERS. REPAIR DONE IAW STANDARD SRM PRACTICES.

Part: SILL — CORRODED (FUSELAGE)

DURING AN IMBV INSPECTION FOUND CORROSION ON SERVICE DOOR CENTER SILL. REMOVED CORROSION BY BLENDING. FABRICATED A REPAIR DOUBLER. REPAIR DONE IAW GST.

Part: FLOORBEAM — CORRODED (FUSELAGE)

DURING IMBV INSPECTION FOUND CORROSION ON LEFT HAND BEAM AT FRAME 20. REMOVED CORROSION BY CUT OUT. FABRICATED A DOUBLER ANGLE, PLATE, FILLER, AND SHIMS. REPAIR DONE IAW AND STANDARD SRM PRACTICES.

Part: SILL — CORRODED (FUSELAGE)

DURING AN IMBV INSPECTION FOUND CARGO DOOR LOWER SILL CORRODED BEYOND SRM LIMITS. REMOVED CORRODED SILL. INSTALLED NEW BEAM IAW SRM.

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

ABI - THIS IS A LEVEL 2 FINDING, AFT DIAMOND GUSSET CORRODED. REMOVED AND INSTALLED SERVICEABLE AFT DIAMOND GUSSET IAW EMB 145 SRM 51-40-02. (M)

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

ABI - THIS IS A LEVEL 2 FINDING. PROFILE AT FRAME 23 CORRODED. REMOVED CORRODED PROFILE ANGLE AND INSTALLED SERVICEABLE PROFILE 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 LOWER SEAT TRACK CORRODED. REMOVED AND INSTALLED SERVICEABLE LEFT FORWARD INBOARD SEAT TRACK IAW EMB 145 AMM 53-01-06. (M)

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

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

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

ABI - THIS IS A LEVEL 2 FINDING. LEFT GALLEY FLOOR SILL BETWEEN FRAMES 19 AND 23 CORRODED. DAMAGE WAS BLENDED OUT AND NDT WAS PERFORMED WITH NO DEFECTS FOUND ACCEPTED AS IS IAW EMB GST-1895/02. (M)

Part: STRINGER — CHAFED (STRING 19L)

DURING AN IMBV INSPECTION FOUND STRINGER 19L CHAFED BETWEEN FRAMES 52 AND 53. BLENDED CHAFE. PERFORMED NDT INSPECTION NO DEFECTS. FABRICATED A DOUBLER ANGLER, AND TWO SHIMS. REPAIR DONE IAW STANDARD SRM PRACTICES.

Part: STRINGER — CHAFED (ALCLAD2024T3)

DURING AN IMBV INSPECTION FOUND STRINGER 19R CHAFED BETWEEN FRAMES 52 AND 53. BLENDED AREA, PERFORMED NDT INSPECTION NO DEFECTS. FABRICATED A DOUBLER ANGLE, AND TWO SHIMS. REPAIR DONE IAW STANDARD SRM PRACTICES.

Part: DOOR — DENTED (PASSENGER DOOR)

DENT IN PASSENGER DOOR ABOVE WINDOW, .006 X 1.0 X 1.1. (SUP) DENT ACCEPTED AS IS IAW MFG GST.

Part: FRAME — DENTED (FRM19,STR13L)

DENT AFT FRAME 19 BELOW STRINGER 13L. .006 X 2.5 X 1.1. (SUP) DENT ACCEPTED AS IS IAW MFG GST.

Part: FRAME — DENTED (FRM18,STR20L)

DENT FORWARD OF FRAME 18 BELOW STRINGER 20L. .013 X 2.0 X 1.7 (SUP) DENT ACCEPTED AS IS IAW MFG GST.

Part: STRUCTURE — GOUGED (PAX DOOR)

ABI - PASSENGER DOOR FORWARD LOWER EDGE IS GOUGED. PERFORMED EDDY CURRENT INSPECTION, NO DEFECTS. GOUGE ACCEPTED AS IS IAW EMB GST-1895/02. (M)

Part: SKIN — DENTED (FUSELAGE)

DENT INBOARD OF RIGHT WIPER MOTOR ARM. THREE DENTS ACCEPTED AS IS IAW MFG GST.

Part: FRAME — DENTED (STR15R,FRM9)

DENT ON FRAME 9 BELOW STRINGER 15R .005 X .7 X 1.0. SUP, DENT ACCEPTED AS IS IAW MFG GST.

Part: DOOR — DENTED (CARGO DOOR)

CARGO DOOR NEAR MIDDLE HAS 3 DENTS 1).006 X 1.3 X 1.0 2).009 X 1.3 X 1.8 3) .003 X .3 X .5. (SUP) THREE DENTS FOUND TO BE WITHIN MFG SRM LIMITS.

Part: LIGHT — INOPERATIVE (CABIN)

ORD - FLT 4382 - CREW REPORTED THE FLOOR PROXIMITY EMERGENCY LIGHTS AT ROWS 10 AND 11 TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT STRIP IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SENSOR — INOPERATIVE

DFW - FLT 3759 - CREW REPORTED A NR 2 HOT BRAKE INDICATION ON TAKEOFF ROLL. TAKEOFF WAS ABORTED AND AIRCRAFT WAS RETURNED TO THE GATE. MAINTENANCE REMOVED AND REPLACED THE LEFT INBOARD BRAKE TEMP SENSOR IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: BATTERY — DISCHARGED (CABIN)

ABI - FLT 3502 - EMERGENCY LIGHT AFT OF GALLEY DOES NOT ILLUMINATE. REMOVED AND REPLACED ASSOCIATED EMERGENCY BATTERY. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SMOKE DETECTOR — FAILED (BAGGAGE COMPT)

GRR - FLT 3796 - BAGGAGE SMOKE WARNING CAME ON. DEPLOYED FIRE BOTTLE. VERIFIED EVENT AS A FALSE WARNING. REMOVED AND REPLACED FORWARD AND AFT SMOKE DETECTORS IN THE AFT BAGGAGE COMPARTMENT. OPERATIONAL CHECK GOOD. REF: OPER CONTROL NR 99ZZZX4083. (X)

Part: SMOKE DETECTOR — FAILED (BAGGAGE COMPT)

GRR - FLT 3796 - BAGGAGE SMOKE WARNING CAME ON. DEPLOYED FIRE BOTTLE. VERIFIED EVENT AS A FALSE WARNING. REMOVED AND REPLACED FORWARD AND AFT SMOKE DETECTORS IN THE AFT BAGGAGE COMPARTMENT. OPERATIONAL CHECK GOOD. REF: OPER CONTROL NR SIMA992593.