N608LM

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT) · airframe 49,622 hrs · 43,518 cycles

AISLE FLOOR SECTIONS 4-5 EMERGENCY LIGHTS INOPERABLE. MAINTENANCE: R & R NR 5 EMERGENCY LIGHT INVERTER, IAW AMM 33-50-11-000-801-A. OPERATIONS CHECK GOOD, OK FOR SERVICE.

Part: FCU — MALFUNCTIONED (FUEL SYSTEM) · airframe 49,105 hrs · 42,941 cycles

REJECTED TAKEOFF DUE TO FUEL 2 LO LEVEL WARNING MSG ON EICAS. WING TANK FUEL QTY INDICATIONS ON EICAS AND MFD NORMAL. MOC ISSUED MEL 28-12 WITH CREW. MAINTENANCE: R/R'D FCU REF AMM 28-41-01. OPS CHECK GOOD, OK FOR SERVCIE.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 48,623 hrs · 42,395 cycles

MDIS 608 33-50 2106261 27NOV19 LEX CLOSE OVERHEAD EMERGENCY EXIT LIGHT AT ROW 12 INOP DUE TO BROKEN WIRE AND DAMAGED FIXTURE AT CONNECTOR. 42300 00 DEW OVERHEAD EMERGENCY EXIT LIGHT AT ROW 12 INOP DUE TO BROKEN WIRE AND DAMAGED FIXTURE AT CONNECTOR. FACT 28NOV19 04:12 PHL INSTALLED NEW CEILING PANEL AT ROW 12 IAW 25-22-04 OK FOR SERVICE.

Part: SPOILER SYS — MALFUNCTIONED · airframe 48,596 hrs · 42,365 cycles

SPOILER FAIL MESSAGE ON DESCENT WITH STRONG LEFT ROLLING TENDENCY....FIX: INSPECTED AND CLEANED PROX SWITCH FOR SPOILER SYSTEM, NO DEFECTS NOTED.PERFORMED SPOILER OPS CK IAW AMM 27-63-01.TRANSITORY CONDITION OF SCU. T/S IAW FIM 27-63-00-810-802-A

Part: ACTUATOR — FAULTY (STICK PUSHER) · airframe 48,490 hrs · 42,241 cycles

PDIS 608 27-31 2128242 03NOV19 CLT CLOSE CONTROL COLUMN FEELS LIKE IT CATCHING ON SOMETHING WITH INCREASED FRICTION WHEN PULLED BACK ACCOMPANIED BY FAINT CLICKING NOISES FACT 03NOV19 06:54 ROA FOUND STICK PUSHER ACTUATOR BINDING. R&R'D STICK PUSHER ACTUATOR IAW AMM 27-36-04-04. PERFORMED ADJUSTME NT & TEST IAW AMM 27-36-04-05. OPS CK GOOD.

Part: CONNECTOR — NOT SEATED (CABIN) · airframe 47,418 hrs · 40,983 cycles

NDIS 608 33-51 0021790 30APR19 RIC CLOSE AISLE 12 EMERGENCY EXIT SIGN AFT PORTION NOT ILLUMINATED 36218 00 NGR FACT 30APR19 09:55 RIC RESEATED CONNECTORS FOR AFT EXIT LOCATING SIGN AT ROW 12 IN REF TOAMM 33-50-15-000/400-801-A. OPS CHECK GOOD OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 47,418 hrs · 40,983 cycles

NDIS 608 33-51 0021800 30APR19 RIC CLOSE EMERGENCY EXIT AISLE ILLUMINATION LIGHT AT RT WING EXIT DOOR INOP. 36218 00 NGR FACT 30APR19 09:57 RIC R/R LAMP FOR PSU EMERGENCY LIGHT AT SEAT 12B AND 12C IN REF TO AMM 33-50-08-000/400-801-A. OPS CHECK GOOD. OK FOR SERVICE P/N ON LAMP 1317 P/N OFF LAMP 1317.

Part: WARNING LIGHT — ILLUMINATED (CARGO DOOR) · airframe 47,413 hrs · 40,977 cycles

PDIS 608 52-30 1869733 29APR19 PHL ASSGN ON CLIMBOUT, RECEIVED BAG DOOR OPEN INDICATION. RETURN TO FIELD. LARRYS HISTORY: NONE MEL 29APR19 22:27 PHL C11918 52-3-2 BAGGAGE DOOR WARNING / POSITION WARNING

Part: SKIN — CORRODED · corrosion level 2 · airframe 47,403 hrs · 40,696 cycles

DURING HVY CHK MAINTENANCE FOUND CORROSION ON FUSELAGE INTERNAL SKIN UNDER FR 61 TEAR STRAP BETWEEN STGR 17L-18L. REPAIRED IAW SRM 53-31-01

Part: ROD END — DAMAGED (RT AILERON) · airframe 47,403 hrs · 40,696 cycles

R/H AILERON ACTUATOR ROD END FITTING O/B HAT BUSHING HOLE OVERSIZED FOUND IN HVY CHK. INSTALLED BUSHING PER SRM 51-20-09

Part: DOOR SILL — CORRODED (SERVICE DOOR) · corrosion level 2 · airframe 47,403 hrs · 40,969 cycles

DURING HVY CHK MAINTENANCE FOUND CORROSION AROUND SERVICE DOOR FWD SILL NUT PLATE HOLES. R&R.

Part: HOUSING — CRACKED (CARGO DOOR) · airframe 47,403 hrs · 40,696 cycles

DURING HVY CHECK CARGO DOOR EXTERNAL HANDLE CUTOUT IS CRACKED AT THE END. REPAIRED IAW SRM 52-30-01RE.

Part: SKIN — DENTED (CARGO DOOR) · airframe 47,403 hrs · 40,696 cycles

DISCREPANCY: DURING HVY CHK MAINTENANCE FOUND CARGO DOOR EXTERNAL SKIN HAS A DENT WITH A GOUGE ON THE FWD LOWER CORNER. CORRECTIVE ACTION: REPAIRED IAW ETD2019-145-044683

Part: UPLOCK — FAILED (MLG) · airframe 46,296 hrs · 39,689 cycles

PDIS 608 32-30 1576422 23AUG18 PHL CLOSE ON GEAR UP SELECTION LANDING GEAR DISAGREE MESSAGE D ISPLAYED ON EICAS AND LEFT GEAR DID NOT RETRACT CREW PERFORMED QRH AND GEAR STAYED IN DOWN POSITION. NO EMERGENCY WAS DECLARED. FACT 23AUG18 20:54 PHL FINNISHED STEPS FOR REMOVAL OF L/H UPLOCK BOX. INSTA LLED NEW IAW 32-33-10. PERFORMED GEAR SWINGS AND OPS CHECK IAW 32-30-00. OPS AND LEAK CHECK GOOD

Part: ANTI-ICE VALVE — FAILED · airframe 44,417 hrs · 37,679 cycles

IN ICING CONDITIONS, WING ANTI-ICE FAILED MESSAGE. CMC SHOWS WING 2 ANTI-ICE LEAK. PUSHED BUTTON OPEN INSCRIPTION SHOWED VALVE CLOSED DURING ICING IN AUTO MODE. R & R THE ANTI-ICE VALVE IAW 30-11-01. GROUND RUN, OPS CHECKED IAW AMM 30-00-00-700-802A/500, OPS CHECKED GOOD, OK FOR SERVICE.

Part: ENGINE — FAILED (NR 1) · airframe 44,188 hrs · 37,437 cycles

NR 1 ENGINE FAILURE DURING LANDING ROLLOUT. EICAS MESSAGES FOR NR 1 ENGINE EXCEEDANCE, HS VALVE NR 1 FAILED. CREW STATED A STRONG ELECTRICAL ODOR IN COCKPIT AND FORWARD CABIN THAT GOT WORSE WHEN APU TURNED ON. CMC MESSAGES FOUND WHERE HS VALVE NR 1 FAILED. PERFORMED A GENERAL VISUAL INSPECTION IAW AMM 72-00-00-200-801. NO DEFECTS NOTED AT THIS TIME.

Part: SWITCH — DIRTY (CARGO DOOR) · airframe 43,977 hrs · 37,213 cycles

DURING TAKE OFF, RECEIVED A MASTER CAUTION EICAS MESSAGE FOR THE CARGO DOOR OPEN. ABORTED TAKE OFF AND RETURNED TO GATE. CLEANED AND LUBED FWD AND AFT CARGO DOOR SWITCHES.

Part: WARNING MESSAGE — FALSE ACTIVATION (ANTI ICE SYSTEM) · airframe 43,766 hrs · 36,989 cycles

ANTI ICE FAIL MESSAGE ILLUMINATED ON EICAS AT 65 KTS DURING TAKEOFF. THE TAKEOFF WAS ABORTED. GROUND RAN AIRCRAFT AND PERFORMED OPS CHECK IAW AMM 30-00-00. NO DEFECTS FOUND AT THIS TIME. EICAS MESSAGE CLEARED. OKAY FOR SERVICE.

Part: PRESSURE SWITCH — FAILED (ANTI ICE SYSTEM) · airframe 43,736 hrs · 36,956 cycles

DURING CLIMBOUT, WING ANTI ICE FAIL EICAS CAUTION FOLLOWED BY ANTI ICE WARNING EICAS , COMPLIED WITH QRH AND MESSAGE DISAPPEARED SHORTLY BEFORE REAPPEARING. R & R RIGHT WING ANTI-ICE VALVE IAW MM 30-11-01 AND RT WING ANTI ICE LOW PRESSURE SWITCH IAW 30-11-02. GROUND RAN ACFT, OPS CHECKED GOOD IAW 30-00-00. OK FOR SERVICE.

Part: ANTI-ICE SYSTEM — MALFUNCTIONED · airframe 42,721 hrs · 36,938 cycles

DURING DESCENT AT 66% POWER, WING ANTI ICE FAIL CAUTION LIGHT ILLUMINATED WITH NO ICE CONDITION. MESSAGE CHANGED TO ANTI ICE FAIL ICE CONDITION ON ENTERING ICE CONDITIONS. ALL MESSAGE CLEARED AFTER EXITING ICE COND,LEVELING OFF AND PUSHING POWER LEVERS FWD. CMC/MFD SHOWS WING 2 ANTI ICE LOW PRESSURE. INSPECTED AND CLEANED THE WING 2 ANTI ICE LOW PRESSURE SWITCH. GROUND RAN THE ENGINE IAW AMM 30-00-00-700-802-A/500, OP CHECKED GOOD. OK FOR SERVICE.

Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 43,712 hrs · 36,924 cycles

AURAL TAKEOFF TRIM DURING TAKEOFF. TRIM WAS IN GREEN. COMPLIED WITH TASK 27-40-00-700-805-A. OPS CHECKED GOOD. OKAY FOR SERVICE.

Part: PRESSURE SWITCH — MALFUNCTIONED (NR 2 BLEED) · airframe 43,710 hrs · 36,920 cycles

DURING CLIMB, NR 2 BLEED LEAK EICAS MESSAGE ILLUMINATED ALONG WITH PB LEAK ILLUMINATED. CLEARED MESSAGE. REMOVED AND REPLACED NR 2 LOW PRESSURE, OPS CHECKED OK AT THIS TIME. SWITCH REPLACED IAW MM 30-11-00-810-811-A.

Part: ANTI-ICE SYSTEM — NO TEST · airframe 43,530 hrs · 36,711 cycles

DURING AN ANTI-ICE TEST IN FLIGHT, EICAS MESSAGE STAB ANTI ICE FAILED DISPLAYED. ATTEMPTED TEST 3 TIMES.

Part: FRAME — BENT (FRAME 72) · airframe 43,505 hrs · 36,680 cycles

FRAME 72 IS BENT AT STRINGER 16R INSIDE CARGO. REMOVED AND REPLACED THE FRAME LOWER SECTION IAW SRM 51-40-02.

Part: SHEAR TIE — CORRODED (FRAME 68) · airframe 43,502 hrs · 36,678 cycles

FRAME 68 SHEAR TIE IS CORRODED AT CARGO DOOR CUT LOWER CORNER. REPAIRED THE SHEAR TIE IAW SRM 53-31-04.

Part: RIB — CHAFED (LT WING) · airframe 43,502 hrs · 36,678 cycles

LEFT WING RIB LOCATED BETWEEN 551CB AND 551DB, CHAFED UNDER THE PCA HOSES. REPAIRED THE RIB IAW ERS-EM-57MR-723.

Part: FRAME — CRACKED (FRM 66) · airframe 43,502 hrs · 36,678 cycles

OUTBOARD RIVET HOLE CRACKED ON LOWER END OF FRAME 66. REPAIRED THE FRAME IAW ERS-EM-53MR-2405.

Part: SHEAR TIE — CORRODED (FRAME 65) · airframe 43,502 hrs · 36,678 cycles

FRAME 65 SHEAR TIE CORRODED BELOW CARGO LOWER GUIDE AND AT CARGO DOOR SILL . REPAIRED THE SHEAR TIE IAW SRM 53-31-04.

Part: SKIN — CRACKED (FR 75) · airframe 43,502 hrs · 36,678 cycles

LEFT REAR FUSELAGE SKIN CRACKED AT FRAME 75, BETWEEN STRINGERS 1 AND 2L. REPAIRED THE SKIN IAW SRM 53-31-01.

Part: DOOR SILL — CORRODED (FRAMES 65-68) · airframe 43,502 hrs · 36,678 cycles

CARGO DOOR LOWER SILL CORRODED REMOVED AND REPLACED CARGO DOOR SILL IAW SRM 53-40-02.

Part: FRAME — CRACKED (FRAME 68) · airframe 43,502 hrs · 36,678 cycles

AFT CARGO DOOR CUTOUT FRAME 68 FRAME CRACKED. REMOVED AND REPLACED THE FRAME IAW SRM 51-40-02.

Part: STRINGER — CRACKED (FRAME 13) · airframe 43,502 hrs · 36,678 cycles

STRINGER 6R CRACKED AT FRAME 13. REMOVED AND REPLACED THE STRINGER IAW SRM 51-40-02.

Part: DOOR FRAME — CORRODED (EMERGENCY EXIT) · airframe 43,502 hrs · 36,678 cycles

LEFT OVERWING EMERGENCY EXIT LOWER FRAME CORRODED AT AFT GUIDE BLOCK AND FWD GROUNDING CLIP. REMOVED AND REPLACED THE DOOR FRAME IAW SRM 51-40-02

Part: SKIN — CORRODED (FRAMES 20-21) · airframe 43,502 hrs · 36,678 cycles

FUSELAGE SKIN HAS CORROSION BENEATH TDR MODE-S ANTENNA, BETWEEN FRAMES 20 AND 21. REPAIRED THE SKIN IAW SRM 53-00-23.

Part: DOOR SILL — CORRODED (SERVICE DOOR) · airframe 43,502 hrs · 36,678 cycles

SERVICE DOOR CUTOUT LOWER CENTER SILL CORRODED. REPAIRED SERVICE DOOR CUTOUT LOWER CENTER SILL IAW EMB145 53-21-02, AND 51-20-03

Part: SKIN — CORRODED (FRAMES 10-11) · airframe 43,502 hrs · 36,678 cycles

FUSELAGE SKIN HAS CORROSION JUST AFT OF 123BL ACCESS PANEL BENEATH TCAS II ANTENNA, BETWEEN FRAMES 10 AND 11. REPAIRED THE SKIN IAW SRM 53-00-23.

Part: CONTACT — MISSING (EMERGENCY LIGHT) · airframe 43,502 hrs · 36,678 cycles

LEFT NR 1 EMERGENCY LIGHT CONTACT MISSING. INSTALLED CONTACT IAW SWPM 20-00-03.

Part: YOKE — CRACKED (RIGHT) · airframe 43,502 hrs · 36,678 cycles

RT FWD LOWER YOKE CRACKED FWD UPPER EDGE. REMOVED AND INSTALLED SERVICEABLE YOKE IAW EO EM-54MR-386

Part: SKIN — CRACKED (FRAME 75) · airframe 43,502 hrs · 36,678 cycles

UPPER LEFT FUSELAGE SKIN HAS TWO CRACKS, ONE CRACK IS JUST AFT OF FRAME 75 AND ABOVE STRINGER 2L, AND 3/8 INCH LONG, AND THE OTHER CRACK IS AT FRAME 75 TOP FASTENER JUST BELOW LT DRAG ANGLE, APPROX. 1/4 INCH LONG. PERFORMED REPAIR IAW SRM 53-31-01

Part: CHARGER — FAILED (CABIN) · airframe 43,496 hrs · 36,672 cycles

LT AND RT EXTERIOR OVERWING EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EPSU NR 4 IAW W/C 33-700-19 AND OPS CHECK GOOD IAW W/C 33-700-17. EMERGENCY LIGHTING BATTERY P/N 2013-1ASMI S/N 76324.

Part: LIGHT — INOPERATIVE (LT WING) · airframe 43,478 hrs · 36,657 cycles

LEFT WING EMEGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY LIGHT AW AMM 33-50-10. OPS CHECKED GOOD.

Part: PUMP — FAILED (HYD SYSTEM) · airframe 42,915 hrs · 36,135 cycles

HYD2 LO QTY FOLLOWED BY HYD SYS 2 FAILED. REMOVED AND REPLACED ENGINE NR 2 HYDRAULIC EDP IAW EMB 145 AMM 29-10-03 PERFORMED LEAK AND OPS CHECK IAW AMM 72-00-00 NO LEAKS DETECTED

Part: BRAKE — FAILED (LT MLG) · airframe 42,852 hrs · 36,074 cycles

LEFT MAIN BRAKES ON FIRE, REPORTED BY TOWER, PERFORMED GROUND EVACUATION. REF ITEMS NR 1 AND NR 2 LOG PAGE 4036786, ITEMS NR 1,2 AND 3. NR 2 BRAKE FAILURE. R & R NR 2 BRAKE ASSY IAW W/C 32-600-14. R & R NR 2 BRAKE LINES IAW CMM 32-10-01. NO LEAKS NOTED. R & R NR 1 MAIN WHEEL ASSY IAW WC 32-700-11 PN 31641, SN 49534953. R & R NR 1 BRAKE ASSY IAW WC 32-600-14, PN 2-1707-2, SN 2665. R & R NR 2 TIRE ASSY IAW WC 32-700-11, PN 31641, SN 17143687P. REMOVED AND INSTALLED INBD BRAKE PRESSURE SW IAW AMM 32-41-04. NO LEAKS NOTED. MAIN BRAKE SYS OPS CHK GOOD IAW AMM 32-41-00-700-801-A. PRESSURE SWITCH, PN 15622-101, SN 2550.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 42,654 hrs · 35,882 cycles

LEFT & RIGHT OVERWING EMER LIGHTING INOPERATIVE. TROUBLE SHOT LT & RT OVERWING EMER LIGHTING & ISOLATED PROBLEM TO EMER BATTERY POWER SUPPLY. R & R EMER BATTERY POWER SUPPLY IAW AMM-33-50-04.

Part: GCU — FAILED (NR 4) · airframe 42,043 hrs · 35,298 cycles

ON FINAL WE TURNED THE APU ON IAW MEL 24-4, ONCE APU ON LINE, RECVD GEN 1 - 4 OFF BUS, SHORTLY AFTER WE LOST EICAS FOR 5 - 10 SECONDS, GEN 1 WAS SHOWING 7.4 VOLTS 0 A. SUSPECT NR 4 GCU. R & R GCU IAW AMM 24-31-02. PERFORMED OPERATIONS CHECK IAW AMM 24-31-00. OPERATIONS CHECKED GOOD.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 41,762 hrs · 35,030 cycles

EMERGENCY EXIT SIGN OVER SERVICE DOOR INOPERATIVE. R & R EMER LIGHT INVERTER NR 2 IAW AMM 33-50-11. OPERATIONS CHECKED GOOD.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 41,633 hrs · 34,909 cycles

DURING PS1 CHECK, FOUND FWD OVERWING EMER EXIT SIGN LIGHT INOPERATIVE. R & R EMER LIGHT DC & AC INVERTER NR 6 IAW AMM 33-50-11.

Part: GENERATOR — FAILED (NR 4) · airframe 41,266 hrs · 34,586 cycles

ON TAXI IN GEN 4 OFF BUS MSG RECEIVED. STARTED APU & NOTICED THAT APU GEN WAS NOT SHARING THE LOAD. IT REMAINED AT 0 AMPS, FLIGHT ATTENDANT REPORTED STRONG ELEC BURNING SMELL IN CABIN. UPON SHUTTING DOWN ENG 1, DC BUS 1 WENT UNPOWERED. AT GATE, AIRPLANE WOULD NOT POWER OFF EVEN WITH EVERYTHING SHUTDOWN & BATTERIES IN OFF. R & R NR 4 BUSS CONTACTOR, PN 464CC01Y1 & SN 1091 IAW AMM 20-13-02, DID NOT FIX. SEE ITEM 2 OF THIS LG PG. R & R NR 4 MAIN GEN IAW AMM 24-31-01. OPERATIONS CHECKED GOOD IAW AMM 24-31-00. LEAK CHECKED GOOD IAW LOG PG 3860476 ITEM 1 FOR APU GEN CORRECTIVE ACTION. FOUND TO BE CAUSED BY GEN 4. PERFORMED OPERATIONS CHECK OF APU GEN IAW 24-34-00. OPERATIONS CHECKED GOOD. INSPECTED PAX CABIN LIGHTS IAW AMM 33-21-00. FOUND SIDEWALL LIGHT AT 2A BROKEN AT PIN SIDE & STRONG SMELL. R & R SIDEWALL LIGHT 2A IAW AMM 33-21-06. OPERATIONS CHECKED GOOD. NO ELEC BURNING SMELL NOTED. LIGHTS AT SIDEWALL 5C - 6C R & R. OPERATIONS CHECKED GOOD AMM 33-21-06. INSPECTED FLASHLIGHTS & FOUND FLIGHT ATTENDANT FWD FLASHLIGHT STRONG ELEC SMELL. R & R FWD FLASHLIGHT PN P2-07-0009-520 IAW AMM 33-50-16. OPERATIONS CHECKED GOOD. NO ELEC BURNING SMELL NOTED.

Part: CONNECTOR — DEFECTIVE (FLASHLIGHT) · airframe 41,074 hrs · 34,399 cycles

CAPTAINS FLASHLIGHT INOPERATIVE. REPLACED BAD CONNECTOR & PIGTAIL FOR CAPTAINS FLASHLIGHT IAW SWPM 20-21-00. CAPTAINS FLASHLIGHT CHARGING INDICATOR NOW ILLUMINATES & FLASHLIGHT WORKS. MEL RESTORED.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 40,628 hrs · 33,975 cycles

EMERGENCY FLASHLIGHT ABOVE FLIGHT ATTENDANT JUMP SEAT IS INOPERATIVE. R & R EMER FLASHLIGHT IAW AMM CH 33-50-16. OPERATIONS CHECKED GOOD.

Part: UNKNOWN — ODOR (COCKPIT & CABIN) · airframe 40,603 hrs · 33,946 cycles

AT CRUISE ELEC SMELL IN COCKPIT & CABIN WAS VERY STRONG. EMER DECLARED. LANDED & GND EVACUATION. SMELLED LIKE OZONE. TROUBLESHOOTING YIELDED INCONCLUSIVE RESULTS FOR DEFINITIVE REASON FOR SMELL, COULD NOT DUPLICATE SMELL. REFERENCE ITEM 1 OF AML PAGE 3737800 FOR FCF TO DETERMINE SMELL NO LONGER EXISTS. RECONNECTED MAIN BATTERIES IAW TASK 24-36-01-400-801-A. NO OTHER DEFECTS NOTED.

Part: SIGN — INOPERATIVE (CABIN) · airframe 40,514 hrs · 33,861 cycles

SERVICE DOOR EXIT MARKING SIGN INOPERATIVE. R & R SERVICE DOOR EXIT SIGN. OPERATIONS CHECKED GOOD AMM 33-50-14.

Part: ROLLER — LACK OF LUBE (PAX DOOR) · airframe 40,477 hrs · 33,830 cycles

PASSENGER DOOR HARD TO OPEN & CLOSE. LUBRICATED MAIN DOOR FRAME ROLLERS. PERFORMED OPERATIONS CHECK OPENING & CLOSING, FOUND WORKING PROPERLY IAW AMM 52-18-00

Part: DOOR — LACK OF LUBE (CABIN) · airframe 40,358 hrs · 33,713 cycles

CABIN HARD TO OPEN. LUBED & PERFORMED OPERATIONS CHECK IAW AMM 52-10-01. OPERATIONS CHECKED GOOD.

Part: FLASHLIGHT — INTERMITTENT (CABIN) · airframe 40,265 hrs · 33,637 cycles

FORWARD FLIGHT ATTENDANT FLASHLIGHT INTERMITTENT CHARGING. R & R FWD FLIGHT ATTENDANT FLASHLIGHT IAW AMM 33-50-16. OPERATIONS CHECKED GOOD.

Part: HANDLE — LACK OF LUBE (CABIN DOOR) · airframe 40,192 hrs · 33,575 cycles

MAIN CABIN DOOR HARD TO OPEN. LUBED MAIN DOOR EXTERNAL HANDLE. MAIN CABIN DOOR HANDLE, 30 LBS FORCE TO ACTUATE. OPERATIONS CHECKED OK IAW AMM 52 18 00.

Part: SPLICE — BROKEN (CABIN) · airframe 40,081 hrs · 33,496 cycles

SERVICE DOOR EMER LIGHT INOPERATIVE. FOUND SERVICE DOOR EMER LIGHT WIRE SPLICE TO BE BROKEN. R & R SPLICE IAW SWPM 20-21-00. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (SERVICE DOOR) · airframe 39,936 hrs · 33,361 cycles

SERVICE DOOR FAIRING EMER LIGHT INOPERATIVE. R & R SERVICE DOOR FAIRING EMER LIGHT LAMP IAW AMM 33-50-09-000-801-A & 33-50-09-400-801-A. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 39,904 hrs · 33,327 cycles

SERVICE DOOR EXT EMER LAMP INOPERATIVE. R & R IAW AMM 33-50-10-000-801-A & 33-50-10-400-801-A. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: SENSOR — FAILED (STALL WARNING) · airframe 39,742 hrs · 33,160 cycles

DURING STALL PROTECTION TEST THE STALL PROTECTION FAILED, SPS 2 INOPERATIVE & SPS ADVANCED WARNING & CAUTION MSGS PRESENTED ON EICAS. SYS FAILED, SAME WAY MULTIPLE TIMES. TRANSFERRED TO NRWC 608-ORD-01965. IAW NRWC 608-ORD-01965 R & R RT & LT AOA SENSOR IAW AMM 27-36-01. PERFORMED STALL PROTECTION. OPERATIONS CHECKED IAW WC 27-700-20. NO DEFECT NOTED AT THIS TIME.

Part: COUPLING — FAILED (BLEED AIR SYS) · airframe 39,690 hrs · 33,107 cycles

ON CLIMB OUT HEARD A LOUD BANG THEN BLEED 2 LEAK. COMPLIED WITH AOM 1 PROCEDURE, MSG EXTINGUISHED WITHIN 2 MINUTES 30 SECONDS. RETURNED FOR NORMAL LANDING. REPLACED COUPLING IAW AMM 36-11-10. LEAK CHECKED GOOD.

Part: LIGHT — INOPERATIVE (OVERWING EXIT) · airframe 39,690 hrs · 33,106 cycles

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

Part: FLAP — MALFUNCTIONED (WING) · airframe 39,661 hrs · 33,074 cycles

FLAPS WOULD NOT COME INTO THE TAKEOFF POSITION, FLAP HANDLE WAS SET BUT THEY WERE STILL PHYSICALLY IN THE UP POSITION & 0 ON EICAS, NO FLAP FAIL MASTER WARNING WAS INDICATED. PERFORMED RESET PROCEDURE OF FLAP SYS IAW FIM 27-51-00-810-801-A. OPERATIONS CHECKED GOOD. ACFT OK FOR SERVICE.

Part: DOOR — OBSTRUCTED (CABIN) · airframe 39,638 hrs · 33,053 cycles

MAIN DOOR WILL NOT CLOSE. REMOVED DISCARDED HARDWARE & DEBRIS ON DOOR THRESHOLD. OPERATIONS CHECKED GOOD IAW SMP.

Part: SKIN — CANNING (FUSELAGE) · airframe 39,482 hrs · 32,927 cycles

LEFT FUSELAGE SKIN HAS AN AREA OF OIL CANNING BETWEEN FRAME 21 & 22 LT NEAR STRINGER 18LT APPROX 7 INCHES BY 20 INCHES. REPAIRED IAW ERS-EM-53MR-837.

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 39,482 hrs · 32,927 cycles

LEFT OVERWING PANEL SUPPORT ANGLE IS CRACKED AT LT FRAME 48. R & R LT OVERWING SUPPORT ANGLE AT LT FRAME 48 IAW ETN-EM-53-142.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 39,482 hrs · 32,927 cycles

CENTER BELLY PANEL SUPPORT FLANGE IS CRACKED IN THE LT MLG WELL AT FRAME 49. R & R CTR BELLY SUPPORT ANGLE AT LT FRAME 49 IAW ETN-EM-53-142.

Part: PROFILE — CRACKED (APU COWLING) · airframe 39,482 hrs · 32,927 cycles

APU COWL UPPER CTR INSIDE PROFILE IS CRACKED. REPAIRED IAW ERS-EM-53MR-825.

Part: SUPPORT — CRACKED (CARGO DOOR) · airframe 39,482 hrs · 32,927 cycles

BAGGAGE DOOR LIFTING & LOWERING MECHANISM FWD TORSION BAR SUPPORT HAS A CRACK AT BASE OF SUPPORT. R & R BAGGAGE DOOR LIFTING & LOWERING MECHANISM FWD TORSION BAR SUPPORT IAW AMM 52-32-00.

Part: FITTING — DAMAGED (LT AILERON) · airframe 39,482 hrs · 32,927 cycles

LEFT AILERON TO PCA ATTACHMENT FITTING LUG BORE IS DAMAGED ON AILERON. REPLACED FITTING IAW EO EM-27MR-112.

Part: SUPPORT ANGLE — CRACKED (RT WING) · airframe 39,482 hrs · 32,927 cycles

RIGHT OVERWING PANEL SUPPORT ANGLE IS CRACKED AT RT FRAME 50. R & R SUPPORT ANGLE IAW SRM CH 51-40-02.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 39,482 hrs · 32,927 cycles

SUPPORT AT FRAME 61 FOR BAGGAGE DOOR TORSION ROD SUPPORT IS CRACKED. R & R SUPPORT AT FRAME 61 FOR BAGGAGE DOOR TORSION ROD SUPPORT IAW SRM 51-40-02.

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 39,482 hrs · 32,927 cycles

LEFT OVERWING PANEL SUPPORT ANGLE IS CRACKED AT LT FRAME 46. REPAIRED LT OVERWING PANEL SUPPORT ANGLE AT LT FRAME 46 IAW ETN-EM-53-142.

Part: SUPPORT ANGLE — CRACKED (RT WING) · airframe 39,482 hrs · 32,927 cycles

RIGHT OVERWING PANEL SUPPORT ANGLE IS CRACKED AT RT FRAME 47. R & R SUPPORT ANGLE IAW SRM CH 51-40-02.

Part: SPAR — CRACKED (LT WING) · airframe 39,482 hrs · 32,927 cycles

LEFT WING FWD SPAR 1 HAS A CRACK, LOWER SECTION OTBD OF RIB 9, 20.5 MM OTBD OF LOWER SKIN SEAM. COMPLIED WITH SPAR REPAIR IAW ERS-EM-57MR-324.

Part: UNKNOWN — ODOR · airframe 39,124 hrs · 32,657 cycles

STRONG ODOR, OIL, IN FLIGHT STRONGEST SMELL ON TAKEOFF & LANDING. CHRONIC DISCREPANCY. COMPLIED WITH ETN-EM-72-034 IAW NRWC 608-ORD-01848 NO ODOR NOTED. IAW NRWC 608-ORD-01849 COMPLIED WITH RR MM TASK 72-00-00-200-802 NO EVIDENCE OF OIL PUDDLING IN ENG 1 OR 2 IAW LOG PAGE 3682262 FOR FCF.

Part: A/C PACK — ODOR (AC BAY) · airframe 39,109 hrs · 32,635 cycles

OILY SMELL DURING CLIMB OUT. REFERENCE NRWC 608-ORD-01823 FOR TROUBLESHOOTING. PERFORMED ENG RUNS AS OUTLINED IN ETN EM-72-034 R9. PERFORMED PACK BURN OUT PROCEDURES. NO DEFECTS NOTED POST PACK BURN OUT. ACFT RELEASED FOR FUNCTIONAL CHECK FLIGHT PURPOSES ONLY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 39,023 hrs · 32,534 cycles

ROW 7 OVERHEAD AISLE EMER LIGHT INOPERATIVE. R & R ROW 7 OVERHEAD AISLE EMER LIGHT IAW MM 33-50-08-000-801-A & 33-50-08-400-801-A. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: HANDLE — DETACHED (CABIN DOOR) · airframe 38,739 hrs · 32,274 cycles

MAIN CABIN DOOR HANDLE CAME OFF DURING OPENING OF DOOR. SECURED HANDLE IAW AMM 52-11-00.

Part: QUICK DISCONNECT — DEFECTIVE (CABIN) · airframe 38,665 hrs · 32,197 cycles

MAIN DOOR EMER LIGHT QUICK DISCONNECT DOES NOT PLUG IN PROPERLY. R & R EMER LIGHT QUICK DISCONNECT ON MAIN DOOR IAW SWPM 20-00-03.

Part: WIRE — DAMAGED (SERVICE DOOR) · airframe 38,065 hrs · 31,607 cycles

SERVICE DOOR LINER EMERGENCY LIGHT IS INOPERATIVE. REPAIRED WIRES AT SP 7376 & SP 7377 SPLICES ON SERVICE DOOR LINER HINGE AREA IAW SWPM 20-21-00 & 20-00-03. OPERATIONS TEST OF EMERGENCY SERVICE DOOR LIGHT CHECKED OK IAW AMM 33-50-00.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 38,021 hrs · 31,571 cycles

MAIN CABIN DOOR EMERGENCY LIGHT INOPERATIVE. R & R MAIN CABIN DOOR EMERGENCY LIGHT LAMP IAW AMM 33-50-06-000-801-A & 33-50-06-400-801-A. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 37,843 hrs · 31,419 cycles

DURING MX INSPECTION ON FLIGHT 2945 FOUND AFT CABIN FLASHLIGHT INOPERATIVE. ACFT WAS REMOVED FROM SERVICE. REMOVE & REPAIR AFT CABIN FLASH LIGHT ASSEMBLY IAW AMM 256000 MEL RESTORED.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 37,787 hrs · 31,367 cycles

FIRST OFFICER NOTED ELEC OZONE SMELL IN COCKPIT. PERFORMED GVI OF APU LINE & STARTING CONTRACTORS REFERENCING EMB CH 24. NO DEFECTS NOTED, NO OZONE OR OTHER SMELLS NOTED DURING APU START.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 37,736 hrs · 31,327 cycles

LEFT EXTERNAL EMERGENCY LIGHT FWD OF LT WING INOPERATIVE. R & R LT EXTERNAL EMERGENCY LIGHT FWD OF LT WING IAW AMM 33-50-10. LAMP OPERATIONS CHECKED GOOD.

Part: SERVICE DOOR — LACK OF LUBE (CABIN) · airframe 37,620 hrs · 31,249 cycles

FLIGHT 3744 CREW REPORTED SERVICE DOOR VERY HARD TO CLOSE FROM INSIDE ACFT. THE ACFT WAS REMOVED FROM SERVICE. LUBRICATED SERVICE DOOR & OPERATIONAL CHECK IAW AMM 52-43-00. THE ACFT RETURNED TO SERVICE.

Part: CRADLE — DAMAGED (FLASHLIGHT) · airframe 37,089 hrs · 30,805 cycles

FLASHLIGHT ABOVE SEAT 18BC WILL NOT STAY SECURED IN BRACKET. R & R FLASHLIGHT BASE.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 36,860 hrs · 30,616 cycles

WHEN ACFT POWER REMOVED, THE AFT EMERGENCY LIGHTS TURN ON AND STAYING ON THE COCKPIT EMERGENCY LIGHT SWITCH OFF CABIN SWITCH IS NORMAL. OPS CHECKED GOOD IAW REF AMM 25-60-00.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 36,579 hrs · 30,378 cycles

NR 1 BATTERY PACK INOPERATIVE. R & R NR 3 BATTREY PACK IAW AMM 33-50-04. OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 36,579 hrs · 30,378 cycles

BATTERY PACK NR 4 INOPERATIVE. R & R NR 4 BATTERY PACK IAW AMM 33-50-04. OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 36,579 hrs · 30,378 cycles

NR 1 BATTERY PACK, INOPERATIVE. R & R NR 2 BATTREY PACK IAW AMM 33-50-04, OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (FUSELAGE) · airframe 36,578 hrs · 30,377 cycles

RAMP REPORTS EMERGENCY LIGHTS INOPERATIVE.

Part: PROXIMITY SWITCH — INOPERATIVE (MLG) · airframe 36,447 hrs · 30,277 cycles

AFTER GEAR RETRACTION NOTICED A GEAR NOISE WAS VERY LOUD WITH SEVERAL BANGS AND NO SPECIFIC RHYTHM. DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. CMC DOWNLOADED AND FOUND RT MLG UPLOCK PROXIMITY SWITCH FAILED AND R & R BOTH UPLOCK PROXIMITY SWITCHES ON RT MLG UPLOCK IAW AMM 32-61-01. THE FUNCTIONAL CHECK WAS PERFORMED IAW AMM 32-63-05 AND FOUND GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 36,343 hrs · 30,195 cycles

CREW REPORTED THE EMERGENCY FLASHLIGHT AT LAVATORY INOPERATIVE. REMOVED AND INSTALLED NEW FLASHLIGHT IAW AMM 33-50-16. THE OPS CHECKED GOOD.

Part: INDICATOR — UNKNOWN (AIRSPEED) · airframe 36,320 hrs · 30,172 cycles

RECEIVED A "SPS ADVANCED" ON EICAS AT 370, AT SAME TIME RECEIVED A BLINKING YELLOW IAS ON THE AIRSPEED INDICATOR ON BOTH PFD'S. STARTED DOWN TO 240 AND CAPTAIN`S AIRSPEED INDICATOR BLED OFF BELOW 200 KTS MEANWHILE STANDBY AIRSPEED AND F/O AIRSPEED SHOW 300 KTS AND WE WERE ALSO GETTING AN OVERSPEED AURAL WARNING OF "HIGH SPEED". THE CREW PRESSED THE ADC BUTTON ON THE CAPTS REVERSIONARY PANEL AND EVERYTHING APPEARED NORMALLY AGAIN BECAUSE CAPTAIN'S SIDE WAS BORROWING INFO FROM F/O'S SIDE. NOTE, THE CREW WERE IN NIGHT IMC CONDITIONS THE ENTIRE TIME. WITH AUTOPILOT ENGAGED THEY HAD AN UNCOMMANDED LEFT BANK. THE F/O DISCONNECTED THE AUTOPILOT AND FELT VIBRATION IN THE YOKE. IT GOT WORSE WHEN THEY WOULD TURN. IT WAS AN ALARMING HUMMING VIBRATING NOISE. THE CREW SLOWED BELOW 250 KTS AND IT DID GET A LITTLE BETTER BUT CONTINUED UNTIL LANDING. NOTICED A LOT OF CONDENSATION IN THE COCKPIT ON THE WINDOWS. UPON LANDING THE F/A REPORTED THE LIGHTS WERE FLICKERING IN THE CABIN AND CONDENSATION LEAKING ON A PASSENGER IN ROW 10A. PERFORMED MAX VMO EXCEEDANCE PHASE 1 INSP FOR AURAL WARNING "HIGH SPEED" WARNING. NO DEFECTS NOTED IAW AMM TASK 05-50-04-212-001-A00. REQUIRES DFDR DATA ANALYSIS TO DETERMINE PHASE 2 AND 3 DISPOSITION WITHIN 10 FC PER AMM 05-50-04 TABLE 604. COMPLIED WITH WORKCARD 12-200-01 THRU STEP 3 OF CLOSE JOB. FCF REQUIRED. NO DEFECTS NOTED AT THIS TIME. AEA WC 12-200-01 VIBRATION- DETAILED VISUAL INSPECTION STEPS 4 THRU 5 C/W. FCF WAS SATIFACTORY. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: INVERTER — FAILED (EMERGENCY LIGHTS) · airframe 36,016 hrs · 29,941 cycles

DURING MX INSPECTION, FOUND THE EMERGENCY LIGHT FLOOR STRIP LOCATED FIRST IN CABIN AT SEAT 2A INOPERABLE. THE ACFT WAS REMOVED FROM SERVICE. TROUBLESHOT AND FOUND NR 2 EMERGENCY LIGHT DC/AC INVERTER HAD FAILED. R & R THE NR 2 EMERGENCY LIGHT DC/AC INVERTER IAW AMM 33-50-11. THE OPS CHECK WAS GOOD IAW AMM 33-50-00. THE ACFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,928 hrs · 29,873 cycles

DURING B INSPECTION FOUND THE FORWARD FLOOR EMERGENCY LIGHT FLOOR STRIP INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FORWARD FLOOR EMERGENCY LIGHT STRIP. THE OPERATIONAL CHECK WAS GOOD IAW EMB AMM 33-50-12. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: GUSSET — DAMAGED (FUSELAGE) · airframe 35,923 hrs · 29,868 cycles

DURING B INSPECTION FOUND THE RIGHT OUTBOARD GUSSET AT FRAME 22 BLEND OUT OF LIMITS. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT OUTBOARD GUSSET AT FRAME 22 IAW EMB SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SKIN — CRACKED (FUSELAGE) · airframe 35,904 hrs · 29,844 cycles

DURING MAINTENANCE INSPECTION FOUND THE FUSELAGE HAS CRACKS AROUND RIVETS ON FRAME 75, 77, 78, AND 79 RIGHT SIDE. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED REPAIR OF REAR FUSELAGE SKIN CRACKS AT FRAME 75 IAW AEA EO EM-53MR-2121. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: DRAG ANGLE — DAMAGED (FUSELAGE) · airframe 35,904 hrs · 29,844 cycles

DURING MAINTENANCE INSPECTION FOUND THE RIGHT VERTICAL STABLIZER TO FUSELAGE DRAG ANGLE DAMAGED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE DRAG ANGLE IAW AEA EO EM-53MR-1281. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BUTTSTRAP — CORRODED (FUSELAGE) · airframe 35,904 hrs · 29,844 cycles

DURING MAINTENANCE INPECTION FOUND THE BUTTSTRAP BETWEEN FR 13 - 14 CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED BUTTSTRAP BETWEEN FR 13 - 14 IAW EMB SRM 53-00-02. LEVEL OF CORROSION NOT SPECIFIED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: RIB — CRACKED (RT WING) · airframe 35,904 hrs · 29,844 cycles

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

Part: WIRE HARNESS — DAMAGED (CABIN) · airframe 35,923 hrs · 29,869 cycles

DURING MAINTENANCE INSPECTION FOUND THE FLOOR PROXIMITY STRIP LIGHT NR 4 & 5 AIRCRAFT SIDE WIRE HARNESS HAS MISSING CONNECTOR AND NR 5 ALSO HAS A NICKED WIRE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPLACED FLOOR PROXIMITY STRIP LIGHT NR 4 & 5 AIRCRAFT SIDE WIRE HARNESS MISSING CONNECTOR IAW EMB 145 SWPM 20-21-00 STEP 5 AND EMB 145 SWPM 20-50-01 STEP 4. REPAIRED NICKED WIRE ON NR 5 IAW EMB 145 SWPM 20-21-00 STEP 7.B. THE OPERATIONAL FLOOR PROXIMITY STRIP LIGHT CHECKS WERE GOOD IAW EMB 145 AMM 33-50-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — DAMAGED (CABIN) · airframe 35,923 hrs · 29,868 cycles

DURING B INSPECTION FOUND THE EMERGENCY LIGHT STRIPS NR 2 & 7 DAMAGED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 2 & 7 DAMAGED EMERGENCY LIGHT STRIPS AND PLACED NR 1 AND 8 IN THE CORRECT POSITION IAW EMB 145 AMM 33-50-12. THE OPERATIONAL CHECK OF THE LIGHT STRIPS WAS GOOD IAW EMB 145 AMM 33-50-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: HOLDER — BROKEN (COCKPIT) · airframe 34,718 hrs · 28,933 cycles

DURING B INSPECTION FOUND THE FLASHLIGHT HOLDER BEHIND PILOT'S SEAT BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FLASHLIGHT ASSEMBLY IAW EMB 145 AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETUNRED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,618 hrs · 28,853 cycles

DURING B INSPECTION FOUND ROW 3 EMERGENCY LIGHT FLOOR STRIP INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY LIGHT IN ROW 3 IAW EMB AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 34,288 hrs · 28,608 cycles

ON FLIGHT 2838 THE CREW REPORTED THE CAPTAIN’S FLASHLIGHT WAS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CAPTAIN’S FLASHLIGHT. THE OPERATIONAL CHECK WAS GOOD IAW EMB 145 AMM 33-50-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ROLLER — DIRTY (CABIN DOOR) · airframe 34,230 hrs · 28,557 cycles

FOR FLIGHT 3415 THE CREW REPORTED THE MAIN CABIN DOOR WAS HARD TO OPEN & CLOSE. THE AIRCRAFT WAS REMOVED FROM SERVICE. CLEANED AND LUBED ROLLER ON MAIN FRAME IAW AMM 53-21 -02. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE — BROKEN (CABIN) · airframe 32,443 hrs · 27,172 cycles

DURING MAINTENANCE BASE INSPECTION FOUND THE SERVICE DOOR EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. TROUBLESHOT AND FOUND BROKEN WIRE. REPAIRED WIRE IAW EMB WM 20-21-00 NO FURTHER DEFECTS NOTED. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 32,376 hrs · 27,126 cycles

ON FLIGHT 4035 THE CREW REPORTED THE FIRST OFFICER’S FLASHLIGHT WOULD NOT HOLD A CHARGE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FLASHLIGHT ASSEMBLY IAW EMB-145 AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FRAME — GOUGED (FUSELAGE) · airframe 31,159 hrs · 26,182 cycles

DURING MAINTENANCE BASE VISIT FOUND FRAME 65 GOUGED AT STRINGER 12 RIGHT IN CARGO. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED FRAME 65 IAW AE EO EM-53MR-1835. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,964 hrs · 24,525 cycles

DURING MAINTENANCE BASE VISIT FOUND THE LAST OVERHEAD EMERGENCY LIGHT OUT IN THE AFT CABIN. THE AIRCRAFT WAS REMOVED FROM SERVICE. CHANGED EMERGENCY LIGHT BULB. THE OPERATIONAL CHECK WAS GOOD IAW EMBRAER AMM 33-50-08. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 28,824 hrs · 24,418 cycles

DURING MAINTENANCE BASE VISIT FOUND THE AISLE EMERGENCY LIGHTS ON ROWS 1-3 AND ROWS 8-11 TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED BATTERIES. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONNECTOR — LOOSE (BRAKE SYSTEM) · airframe 28,080 hrs · 23,841 cycles

ON FLIGHT 3941 DURING THE LANDING ROLL THE CREW REPORTED, RECEIVED AN `INBOARD BRAKE INOPERABLE` MESSAGE ON EICAS. THE CREW FELT BRAKES FAIL AFTER SEVERAL SECONDS. THE MESSAGE WENT AWAY AND NORMAL BRAKING RETURNED. THE AIRCRAFT WAS REMOVED FROM SERVICE. TROUBLESHOT PER EMB 145 FIM 32-41-00-810-802-A. FOUND INBOARD FAIL MESSAGE ON THE CENTRAL MAINTENANCE COMPUTER. COMPLIED WITH THE FAULT ISOLATION MANUAL 32-41-00-810-801-A. FOUND AN ELECTRICAL CONNECTOR LOOSE. CLEANED AND RE-SECURED CONNECTOR. NO PARTS REMOVED OR REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 27,657 hrs · 23,486 cycles

DURING MAINTENANCE BASE INSPECTION FOUND EMERGENCY FLOOR STRIPS LOCATED ON THE LEFT LOWER AND RIGHT LOWER AT OVERWING EXIT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 5 INVERTER IAW EMB AMM 33-50-11. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 27,421 hrs · 23,273 cycles

DURING THE MAINTENANCE BASE VISIT DURING A COURTESY CHECK FOUND THE EMERGENCY EXIT SIGN ON THE BULKHEAD AFT OF THE GALLEY INOPERATIVE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NUMBER 3 EMERGENCY LIGHT POWER INVERTER. THE OPERATIONAL CHECK WAS GOOD IAW EMBRAER AMM 33-50-11. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 11,652 hrs · 10,333 cycles

DURING MAINTENANCE INSPECTION, ROWS NUMBERED 1-3 EMERGENCY LIGHTS AND SERVICE DOOR OVERHEAD LIGHT WERE FOUND TO BE INOPERABLE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE NUMBER 2 BATTERY AND CHARGER IAW 33-700-19 MANUAL. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 26,410 hrs · 22,318 cycles

DURING A MAINTENANCE INSPECTION ROWS NUMBERED 1 - 3 EMERGENCY LIGHTS AND SERVICE DOOR OVERHEAD LIGHT WERE FOUND TO BE INOPERABLE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE NUMBER 2 BATTERY AND CHARGER IAW 33 -700-19. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: FRAME — CORRODED (FUSELAGE) · airframe 26,357 hrs · 22,271 cycles

MAJOR REPAIR DURING THE MAIN BASE VISIT INSPECTION FRAME 20 WAS FOUND TO BE CORRODED BELOW SERVICE DOOR AT SPLICE. CUT OUT CORRODED AREA. FABRICATED A 3.5" X 1.0" DOUBLER FROM AL7475-T761 0.040" AND A 1.5" X 1.0" FILLER FROM AL2024T3 0.040". PREPPED, CLEANED, ALODINED, PRIMED AND INSTALLED REPAIR PIECES IAW AEA EO EM-53MR-1345. AIRCRAFT RETURNED TO SERVICE.

Part: FRAME — DAMAGED (FUSELAGE) · corrosion level 2 · airframe 26,357 hrs · 22,271 cycles

MAJOR REPAIR DURING THE MAIN BASE VISIT INSPECTION A PREVIOUS REPAIR WAS FOUND TO HAVE BEEN ACCOMPLISHED TO THE LEFT HAND FUSELAGE SKIN AT FR 24 AND 14L AREA. THE REPAIR WAS REMOVED FOR EVALUATION DUE TO LACK OF INFORMATION. DURING EVALUATION ADDITIONAL DAMAGE WAS NOTED ON FRAME 24 AT STRINGER 14 LEFT. CUT OUT DAMAGE. FABRICATED A 3.0" X 2.0" FILLER USING AL2024T3 0.050" AND A 9.5" X 8.5" DOUBLER FROM AL2024T3 0.050". PREPPED, CLEANED, ALODINED, PRIMED AND INSTALLED REPAIR IAW AEA EO EM-53MR-1343. AIRCRAFT RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,357 hrs · 22,271 cycles

MAJOR REPAIR DURING THE INTERMEDIATE MAIN BASE VISIT INSPECTION A PREVIOUS REPAIR ON THE LEFT HAND OMEGA BEAM AT FRAME 20 WAS FOUND CORRODED. REMOVED THE PREVIOUS REPAIR AND CLEANED THE AREA. PREPARED A 18.25 X 3.8 REPAIR DOUBLER FROM AL2024T3 0.050, A 12.3 X 3.2 FILLER FROM EPNEMEP54703, FABRICATED TWO SHIMS, ONE 1.1 X 5.6 AND ONE 1.1 X 4.35 AND A 1.15 X 6.6 REPAIR PLATE FROM AL2024T3 0.125. PREPPED, CLEANED, ALODINED, PRIMED AND INSTALLED REPAIR PIECES. IAW EMB SRM 53-00-10. AIRCRAFT RETURNED TO SERVICE.