N672AE

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 44,616 hrs · 42,455 cycles

53-2222 LH OMEGA BEAM IB FLANGE CRACKED AT FR21. REPAIRED FLANGE IAW ETD2024-145-901010 AND EO1-53-25-0016.

Part: STRUCTURE — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,616 hrs · 42,455 cycles

53-2233 CARGO DOOR ENTRY FWD L-SHAPE CORRODED AT FR65. REPAIRED IAW SRM 53-31-01 AND EO 1-53-25-0008

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 44,616 hrs · 42,455 cycles

53-2209 FR66 CRACKED BTW STR18-19L UNDER T-POST SUPPORT ANGLE. REPAIRED FRAME IAW EO1-53-24-0744.

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 44,616 hrs · 42,455 cycles

53-2214 FLOOR STRUCTURE AREA, CRACK ON RH BEAM BTW FR59-60 AROUND NUTPLATE HOLE. REPAIRED IAW SRM 53-24-10

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 44,616 hrs · 42,455 cycles

53-2213 FLOOR STRUCTURE AERA, RH BEAM HAS CRACK AT BTW FR60-61 AROUND ANCHOR NUT HOLE. REPAIRED IAW SRM 53-24-10

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 44,616 hrs · 42,455 cycles

53-2209 FR66 CRACKED AT FR66 BTW STR18-19L. REPAIRED FRAME IAW ETD2024-145-900971 AND EO1-53-24-0744

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 44,616 hrs · 42,455 cycles

53-2210 FR 67 CRACKED AT BTW STR18-19L UNDER T-POST SUPPORT ANGLE. REPAIRED IAW EO1-53-24-0744

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 44,616 hrs · 42,455 cycles

53-2216 FLOOR AREA STRUCTURE, LH BEAM CRACKED AT BTW FR60-61 AROUND NUTPLATE HOLE. REPAIRED BEAM IAW SRM 53-24-10

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 44,616 hrs · 42,455 cycles

53-2215 FLOOR STRUCTURE AREA, LH BEAM CRACKED AT BTW FR59-60 AROUND NUTPLATE HOLE. REPAIRED BEAM IAW SRM 53-24-10

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 44,616 hrs · 42,455 cycles

53-2196 FLOOR STRUCTURE AREA, RH GUSSET CORRODED AT BTW FR59-62. RAR GUSSET IAW SRM 51-40-02

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 44,616 hrs · 42,455 cycles

53-2198 FLOOR STRUTURE AREA, LH GUSSET CORRODED BTW FR59-62. RAR GUSSET IAW SRM 51-40-02

Part: PROFILE — CRACKED (ZONE 300) · airframe 44,616 hrs · 42,455 cycles

55-2160 VERTICAL STAB, AFT OF REAR SPAR 3, RH UPPER PROFILE CRACKED UNDER UPPER RIB. REPAIRED IAW ETD2024-145-900968 REV 1 AND EO 1-53-24-0743

Part: PROFILE — CRACKED (ZONE 200) · airframe 44,616 hrs · 42,455 cycles

53-2139 OMEGA PROFILE ABOVE PLATE 123-06510-001 CRACKED. RAR PROFILE IAW SRM 51-40-02

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 44,616 hrs · 42,455 cycles

55-2177 IN AFT COMPARTMENT, SHEAR CLIP CRACKED AT FR 80 BTW STR5-7R. RAR SHEAR CLIP IAW SRM 51-40-02

Part: PROFILE — CRACKED (ZONE 300) · airframe 44,616 hrs · 42,455 cycles

55-2159 VERT STAB, AFT OF SPAR #3, LH UPPER PROFILE CRACKED ABOVE RUDDER UPPER MID HINGE. RAR PROFILE IAW SRM 51-40-02

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 44,616 hrs · 42,455 cycles

53-2103 SHEAR CLIP CRACKED AT FR65 BTW STR7-9L. RAR SHEAR CLIP IAW SRM 51-40-02

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 44,616 hrs · 42,455 cycles

53-2084 LH OMEGA BEAM CRACKED AT FR27. REPAIRED IAW ETD2025-145-900013 AND EO1-53-25-0017

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 44,616 hrs · 42,455 cycles

53-2088 LH OMEGA BEAM CRACKED AT FR34. REPAIRED IAW SRM 53-00-10 AND EO1-53-25-0019

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 44,616 hrs · 42,455 cycles

53-2085 LH OMEGA BEAM CRACKED AT FR28. REPAIRED IAW ETD2025-145-900013 AND EO1-53-25-0017

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 44,616 hrs · 42,455 cycles

53-2077 SHEAR CLIP CRACKED AT FR24 BTW STR16-17R. RAR SHEAR CLIP IAW SRM 51-40-02

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 44,616 hrs · 42,455 cycles

53-2102 SHEAR CLIP CRACKED AT FR65 BTW STR5-7R. RAR SHEAR CLIP IAW SRM 51-40-02

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 44,616 hrs · 42,455 cycles

53-2082 LH OMEGA BEAM CRACKED AT FR26. REPAIRED IAW ETD2025-145-900013 AND EO 1-53-25-0017

Part: SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,616 hrs · 42,455 cycles

53-2121 RH SILL #4 CORRODED AT BTW FR41-48. RAR SILL IAW SRM 51-40-02

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 44,616 hrs · 42,455 cycles

53-2087 CTR OMEGA BEAM CRACKED AT FR29. REPAIRED IAW SRM 53-00-10 AND EO1-53-25-0021

Part: SUPPORT — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 44,616 hrs · 42,455 cycles

53-2090 LH SILL #3 CORRODED. RAR SILL IAW SRM 51-40-02

Part: SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 44,616 hrs · 42,455 cycles

53-2114 RH SILL #3 CORRODED BTW FR35-41. RAR SILL IAW SRM 51-40-02

Part: SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 44,616 hrs · 42,455 cycles

5-2080 RH SILL #2 CORRODED. RAR SILL IAW SRM 51-40-02

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 44,616 hrs · 42,455 cycles

53-2101 SHEAR CLIP CRACKED AT FR67 BTW STR6-7R. RAR SHEAR CLIP IAW SRM 51-40-02

Part: SUPPORT — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 44,616 hrs · 42,455 cycles

53-2089 LH SILL #2 CORRODED. RAR SILL IAW SRM 51-40-02

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 44,616 hrs · 42,455 cycles

53-2086 LH OMEGA BEAM CRACKED AT FR29. REPAIRED IAW SRM 53-00-10 AND EO 1-53-25-0020

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 44,616 hrs · 42,455 cycles

53-2087 CTR OMEGA BEAM CRACKED AT FR29 REPAIRED IAW SRM 53-00-10 AND EO1-53-25-0021

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 44,616 hrs · 42,455 cycles

LH OMEGA BEAM CRACKED AT FR24. REPAIRED IAW ETD2025-145-900013 AND EO1-53-25-0017

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 44,616 hrs · 42,455 cycles

53-2076 SHEAR CLIP CRACKED AT FR24 BTW STR15-16R. RAR SHEAR CLIP IAW SRM 51-40-02

Part: SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 44,616 hrs · 42,455 cycles

53-2115 LH SILL #4 CORRODED BTW FR35-41. RAR SILL IAW SRM 51-40-02

Part: ANGLE — CRACKED · airframe 44,616 hrs · 42,455 cycles

53-2112 RH ANGLE ON FLOOR LEVEL CRACKED AT FR46. RAR ANGLE IAW SRM 51-40-02

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 44,616 hrs · 42,455 cycles

53-2079 SHEAR CLIP CRACKED AT FR27 BTW STR15-16R. RAR SHEAR CLIP IAW SRM 51-40-02

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 44,616 hrs · 42,455 cycles

53-2052 SHEAR CLIP CRACKED AT FR15 BTW STR15-16R. RAR SHEAR CLIP IAW SRM 51-40-02

Part: BEAM — CORRODED (ZONE 800) · corrosion level 2 · airframe 41,616 hrs · 42,455 cycles

BAG DOOR SURROUND LWR BEAM CORRODED. R & R BEAM IAW SRM 51-40-02

Part: DOOR SILL — CORRODED (ZONE 200) · corrosion level 2 · airframe 44,616 hrs · 42,455 cycles

53-2063 SERVICE DOOR AFT SILL CORRODED. RAR SILL IAW SRM 51-40-02.

Part: PLATE — CORRODED · corrosion level 2 · airframe 44,616 hrs · 42,455 cycles

53-2062 RH DIGITAL PLATE CORRODED. RAR DIGITAL PLATE IAW SRM 51-40-02

Part: ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,616 hrs · 42,455 cycles

53-2064 STEP ANGLE CORRODED ON RH SIDE AT BTW FR23-24. RAR STEP ANGLE IAW SRM 51-40-02

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 44,616 hrs · 42,455 cycles

53-2066 ANGLE ON LH OMEGA BEAM IB SIDE CORRODED AT FR19-20. RAR ANGLE IAW SRM 51-40-02

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 44,616 hrs · 42,455 cycles

53-2053 SHEAR CLIP CRACKED AT FR16 BTW STR15-16R. RAR SHEAR CLIP IAW SRM 51-40-02

Part: PLATE — CORRODED · corrosion level 2 · airframe 44,616 hrs · 42,455 cycles

53-2061 RH DIGITAL PLATE CORRODED AT FR20. RAR DIGITAL PLATE IAW SRM 51-40-02

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 44,616 hrs · 42,455 cycles

53-2068 LH OMEGA BEAM IB FLANGE CORRODED BTW FR19-23. REPAIRED IAW SRM 53-21-10

Part: PLATE — CORRODED · corrosion level 2 · airframe 44,616 hrs · 42,455 cycles

53-2062 RH DIGITAL PLATE CORRODED AT FR22. RAR DIGITAL PLATE IAW SRM 51-40-02

Part: FIREWALL — CRACKED (APU BAY) · airframe 44,616 hrs · 42,455 cycles

53-2029 APU FIREWALL CRACKED AT APU CANNON PLUG FITTING ATTACHMENT SCREW. REPAIRED IAW SRM 53-32-13 AND EO1-53-24-0734

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 42,811 hrs · 40,486 cycles

BURNING SMELL OBSERVED IN FLIGHTDECK DISSIPATED AFTER TURNING OFF PACK 1. INSP PACK 1 AND FOUND ALL 4 DUCTS ON THE DUAL TEMP CONTROL VLV TO BE MELTED AND LEAKING AIR. RAN PACK 2 ONLY FOR 15 MIN WITH NO BURNING SMELL NOTED SEE LP 288484 SEQ 1 FOR PACK 1 W/U

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,984 hrs · 39,568 cycles

REJECTED T/O FOR WARNING MESSAGE T/O CONFIG AND CAUTION MSG BRAKE TEMP NO DISPLAY ON R/H BRAKE TEMP IND. C/W DEACTIVATION OF NO.4 BRAKE TEMP SENSOR IAW MEL APPENDIX 1, R & R BRAKE TEMP SENSOR #400 IAW AMM 32-47-01. OPS CHECK GOOD. OK FOR SERVICE. CLEAR MEL 32-2-1.

Part: NONE — NONE · airframe 41,134 hrs · 38,590 cycles

MUSTY SMELL FROM PACK 2 IN FLIGHT DECK.

Part: ACTUATOR — DAMAGED (GUST LOCK SWITCH)

GUST LOCK WOULD NOT UNLOCK ON RUNWAY. PERFORMED ELECTRICAL RESET, FOUND GUST LOCK TO OPERATE NORMALLY. PERFORMED GUST LOCK OPS CHECK IAW AMM 27-70-00. OPS CHECK SATISFACTORY, ACFT OK FOR SERVICE. ACCESSED SOLENOID UNDER GUST LOCK LEVER MANUALLY DEPRESSED SOLENOID AND MOVED GUST LOCK LEVER TO FULL UNLOCKED POSITION. ELEVATOR GUST LOCK STILL ENGAUGED. INSPECTED CONTROL COLUMN POSITION SWITCH. FOUND FLAT SPOT ON SWITCH ACTUATOR ROLLER. R & R ACTUATOR IAW AMM 27-71-11. PERFORMED GUST LOCK OPS CHECK IAW 27-71-00-700-801-A, OPS CHECKED GOOD.

Part: NONE — NONE · airframe 40,402 hrs · 37,743 cycles

E932899 - LH AND RH STAB BEARING BORES OUT OUT OF LIMITS .... REPAIRED THE LH AND RH STAB BEARING BORES IAW PIEDMONT EO1-55-22-0177.

Part: NONE — NONE · corrosion level 2 · airframe 40,402 hrs · 37,743 cycles

E932336 - SSI# 53-20-11 GALLEY CENTER OMEGA BEAM GUSSET HAS CORROSION .... REMOVED CORRODED GALLEY CENTER OMEGA BEAM GUSSET, PREPPED AND INSTALLED SERVICEABLE GUSSET IAW EMB 145 SRM 51-40-02, EMB 145 SRM 51-20-03.

Part: NONE — NONE · corrosion level 2 · airframe 40,402 hrs · 37,743 cycles

E932337 - SSI# 53-20-11 GALLEY L/H #1 FLOOR BOARD SUPPORT HAS CORROSION .... REMOVED CORRODED GALLEY LH #1 FLOORBOARD SUPPORT AND INSTALLED SERVICEABLE FLOOR BOARD SUPPORT IAW EMB145 SRM 51-40-02 AND EMB 45 SRM 51-20-03.

Part: NONE — NONE · airframe 40,402 hrs · 37,743 cycles

E932058 - SSI# 52-30-09 CARGO DOOR UPPER WEB L BRACKET HAS CORROSION AT NUT PLATE HOLES 8EA .... REMOVED AND REPLACED CARGO DOOR UPPER WEB L BRACKET IAW EMB 145 SRM 51-40-02, AND SRM 51-40-09.

Part: NONE — NONE · airframe 39,077 hrs · 36,229 cycles

PDIS 672 78-33 2575331 16NOV21 ROC ASSGN E1 REV DISAGREE MSG DURING TAKEOFF ROLL. C/W MAINT PROCEDURES ... CURRENTLY ON THE MEL, IT REQUIRES MORE TROUBLESHOOTING

Part: NONE — NONE · airframe 39,013 hrs · 36,149 cycles

NDIS 672 78-34 0033960 05NOV21 FLO CLOSE CREW DID A REJECTED TAKE OFF THEY HAD AN E1 REV DISAGREE NO HISTORY IN 90 FACT 05NOV21 03:54 FLO HAD CREW CYCLED POWER LEVER A COUPLE TIMES NO MSG NOTED IRREGULARITY CLEARED

Part: RADAR — FAILED (WX SYSTEM) · airframe 38,497 hrs · 35,551 cycles

WX RADAR FAIL IN FLIGHT ALONG WITH AMBER WX DISPLAYED ON MFDS. R&R RADAR RTA IAW 34-42-01.OPS CHK GOOD CLEAR MEL 34-12.

Part: UNKNOWN — ODOR (CABIN) · airframe 38,403 hrs · 35,458 cycles

AT 29,000 FT IN CRUISE FLT BURNING RUBBER SMELL NOTED IN COCKPIT AND CABIN. SMELL DISSIPATED WITHIN ONE MINUTE. GROUND RAN AC AND PACK SYSTEMS AND INSPECTED PACK, APU, AND RECIRC SYSTMES IAW FIM TASK 21-20-00-810A. NO SMOKE SMELL NOTED OK FOR SERVICE.

Part: UNKNOWN — SMOKE (CABIN) · airframe 37,502 hrs · 34,514 cycles

WITH APU RUNNING, SMOKE FROM AFT FLT DECK VENTS WAS NOTICED WITH PACK 1 RUNNING, NO SMOKE WITH PACK 1 OFF. OPERATIONS NORMAL WITH PACK 2 RUNNING. GROUND RAN APU WITH CREW WITH NR 2 PACK RUNNING, NO EVIDENCE OF SMOKE OR FUMES NOTICED. SEE SEQ 2 FOR NEW DISCREPENCY.

Part: PRESSURE SWITCH — INOPERATIVE (RUDDER) · airframe 37,075 hrs · 34,049 cycles

IN CRUISE, 310 KNOTS @ 13000FT, AUTOPILOT FAIL EICAS WARNING MSG, FOLLOWED BY YAW DAMPER FAIL CAUTION, FOLLOWED BY RUD SYS 1-2 INOP WARNING. A/P AND YAW DAMPER MSGS CLEARED. AFTER QRH, RUD SYS 1 BECAME OPERATIONAL, RUD SYS 2 REMAINED INOP. MAINTENANCE: PERFORMED FIM TASK 27-22-00-810-804-A BLOCKS 1 AND 8. R+R RUDDER SYS #2 PRESSURE SWITCH. IAW 27-23-04. LEAK CHECK AND OPS CHECK GOOD PER AMM 27-23-00. OK FOR SERVICE AT THIS TIME.

Part: ACM — SEIZED (AC BAY) · airframe 36,902 hrs · 33,849 cycles

SMOKE IN COCKPIT IN FLIGHT, WENT AWAY WHEN PACKS, GASPERS AND RECIRC'S WERE SELECTED OFF. FOUND NR 2 ACM FROZEN UP. R & R ACM IAW MM 21-51-03. OPERATIONS LEAK CHECKED GOOD. OK FOR SERVICE AT THIS TIME.

Part: SWITCH — FAILED (THRUST REVERSER) · airframe 36,024 hrs · 32,855 cycles

AT 30-40 KNOTS, RECEIVED AN ENG REVERSER DISAGREE CAUTION MESSAGE ON EICAS, FOLLOWED BY MASTER WARNING THRUST LEVER DISAGREE MESSAGE. FOUND THE NR 1 THRUST REVERSER UP STOWOUT SWITCH FAIL MESSAGE ON CMC. R & R THE NR 1 THRUST REVERSER UP STOWOUT SWITCH IAW AMM 78-34-01. OPS CHECKED GOOD. OK FOR SERVICE.

Part: WARNING MESSAGE — FALSE ACTIVATION (COCKPIT) · airframe 35,973 hrs · 32,801 cycles

CMC SHOWS MESSAGE OF ENG 1 FADEC A. CREW RETURNED TO GATE DUE TO MESSAGE. CREW REPORTED POWER SURGE WHEN SWITCHING FROM GPU TO AIRCRAFT PWR. FIX: AIRCRAFT CREW OPERATED BOTH ENGINES. NO EICAS MESSAGE. SYS OPERATES NORMALLY.

Part: ENGINE — SMOKE (NR 1) · airframe 35,932 hrs · 32,753 cycles

WHITE SMOKE OBSERVED FROM ENG #1,EXHAUST AND INLET, FOR APPROX 10 MINS AFTER ENGINE SHUTDOWN. FIX: INSPECTED #1 ENG NO VISUAL SIGN OF OIL LEAKAGE OR POOLING IAW NTO # AE3007A-120. NO FURTHER ACTION REQUIRED. NOTE: HAPPENED AFTER FLIGHT/TAXI WHEN SHUTTING ENGINES DOWN ON RAMP.

Part: WIRE — BROKEN (CABIN) · airframe 35,883 hrs · 32,703 cycles

EMERGENCY LIGHT AT SERVICE DOOR HINGE ASSY IS INOP. FOUND BROKEN WIRE. SPLICED WIRE, OPS CHECK GOOD.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 34,600 hrs · 31,283 cycles

LANDING GEAR LEVER DISAGREE MSG ON DEPARTURE UPON GEAR RETRACTION. SELECTED GEAR DOWN ALL MESSAGES EXTINGUISHED, RETURNED TO THE FIELD. HYD PRESSURE OK NO LEAKS NOTED ON WALKAROUND. HISTORY: YES FACT 31DEC18 11:30 BUF CHECKED CMC NO RELEVANT MESSAGES DISPLAYED JACKED AIRCRAFT AND PERFORMED NUMEROUS GEAR CYCLES NO DEFECTS NOTED PERFORMED GENERAL VISUAL INSPECTION OF ALL GEAR WELLS NO OBVIOUS DEFECTS NOTED ALL WORK PERFORMED IAW AMM 32-30-00 OK FOR SERVICE.

Part: SERVO — FAULTY (ELEVATOR) · airframe 33,970 hrs · 30,527 cycles

DURING CLIMB/CRUISE PHASES OF FLT A LOUD BANG/THUD SOUND WAS NOTED. IT APPEARED TO COME FROM FLOOR BELOW BOTH PILOTS SEATS SIMULTANEOUSLY AND BOTH CONTROL YOKES JERKED. EVENT OCCURED THREE TIMES DURING FLT. R&R ELEVATOR SERVO IAW AMM 22-11-04. A/P FUNC CHECK GOOD AT THIS TIME OK FOR SERVICE.

Part: CONNECTOR — FAILED · airframe 32,872 hrs · 29,290 cycles

NO TAKEOFF CONFIGURATION EICAS MESSAGE DISPLAYED DURING TAKEOFF ROLL. PARKING BRAKE LIGHT ILLUMINATED WHEN THRUST LEVERS WERE ADVANCED. TAKEOFF CONFIGURATION TESTED OK PRIOR TO TAKEOFF ROLL. R & R THE CONNECTOR IAW SWPM 20-50-01. OPS CHECKED IAW AMM 32-44-00. OPS CHECKED GOOD.

Part: PRESSURE SWITCH — FAULTED (BRAKES) · airframe 32,860 hrs · 29,278 cycles

NO TAKEOFF CONFIG EICAS MESSAGE DUE TO PARKING BRAKE ON LIGHT REMAINED ILLUMINATED WITH PARKING BRAKE OFF. TAKEOFF CONFIG BUTTON STILL SAYS OK WHEN PRESSED. EICAS MESSAGE APPEARS WHEN POWER LEVERS ARE AVANCED. INSPECTED THE EMERGENCY BRAKE SYS IAW FIM 32-44-00-810-802A - 816-001A. FOUND THE EMERGENCY BRAKE SYS PRESSURE SWITCH AT FAULT. REMOVED AND REPLACED THE PRESSURE SWITCH IAW AMM 32-44-07. OPS CHECKED GOOD.

Part: RELAY — FAILED (BRAKE) · airframe 32,856 hrs · 29,274 cycles

NO TAKEOFF CONFIGURATION EICAS MESSAGE DUE TO PARKING BRAKE ON LIGHT REMAINED ILLUMINATED WITH PARKING BRAKE OFF. OPS CHECK OF THE EMERGENCY PARKING BRAKE HANDLE RELAY K0212, MADE A FEW CLICKING NOISES WITH IN A SECOND WITH BRAKE LIGHT COMING ON AND OFF RESPECTIVELY A FEW TIMES. REMOVED AND REPLACED THE RELAY K021, IAW 20-13-02. OPS CHECKED GOOD.

Part: RELAY — FAILED (PARKING BRAKE) · airframe 32,856 hrs · 29,274 cycles

PARKING BRAKE ON LIGHT ILLUMINATED. R & R THE PARKING BRAKE RELAY K0212. OPS CHECKED OK.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 32,162 hrs · 28,558 cycles

SERVICE DOOR CENTER SILL CORRODED. REPAIRED SERVICE DOOR CENTER SILL IAW SRM 53-21-02 ITEM 2 FIG 201.

Part: SKIN — CRACKED (FUSELAGE) · airframe 32,162 hrs · 28,558 cycles

RT AFT FUSELAGE FR 75 BELOW STR 2R SKIN CRACKED AT FASTENER HOLE. REPAIRED CRACKED AREA ON RT AFT FUSELAGE FR 75 BELOW STR 2R SKIN AT FASTENER HOLE IAW SRM 53-31-01 ITEM 11 FIG 219.

Part: DOOR FRAME — CRACKED (DOOR) · airframe 32,162 hrs · 28,558 cycles

123BL AFT FRAME CRACKED BELOW THE RT AFT LOCK PIN SUPPORT. REMOVED AND REPLACED 123BL AFT FRAME BELOW THE RT AFT LOCK PIN SUPPORT IAW SRM 51-40-02.

Part: SUPPORT — CRACKED (LT PYLON) · airframe 32,162 hrs · 28,558 cycles

LT ENGINE PYLON FWD LOWER YOKE CRACKED. REMOVED AND REPLACED LT FWD LOWER YOKE IAW EO EM-54MR-386.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 31,966 hrs · 28,357 cycles

LEFT WING AFT EXTERIOR EMERGENCY LIGHT INOPERATIVE. R & R THE LAMP IAW AMM 33-50-10. OPS CHECKED GOOD.

Part: SMOKE DETECTOR — FALSE ACTIVATION (CARGO BAY) · airframe 28,607 hrs · 24,775 cycles

THE CREW REPORTED BAG SMOKE DETECTOR LIGHT AT 10,000' ON DEPARTURE. THE CREW DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE WHERE THE ACFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE ACFT AND FOUND NO EVIDENCE OF SMOKE, OPERATIONALLY TESTED THE BAG SMOKE DETECTORS WITH NO DEFECTS NOTED, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FIRE LOOP — FAILED (NR 1 NACELLE) · airframe 28,375 hrs · 24,533 cycles

DURING DESCENT, THE NR 1 ENGINE FIRE DETECTION SYSTEM FAILED. THE ACFT WAS FERRIED FOR REPAIR. MAINTENANCE R & R THE NR 1 ENGINE FIRE LOOP IAW AMM 26-11-01. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SOCKET — DIRTY (CABIN) · airframe 27,853 hrs · 24,029 cycles

EMERGENCY LIGHT ON MAIN CABIN DOOR FLICKERS ON & OFF. CLEANED MAIN CABIN DOOR EMER LIGHT SOCKET IAW SWPM 20-50-00. OPERATIONS CHECKED GOOD.

Part: SOCKET — DIRTY (CABIN) · airframe 27,853 hrs · 24,029 cycles

EMERGENCY LIGHT ON SERVICE DOOR INOPERATIVE. CLEANED SERVICE DOOR EMER LIGHT SOCKET IAW SWPM 20-50-00. OPERATIONS CHECKED GOOD.

Part: LIFE VEST — UNKNOWN (COCKPIT) · airframe 27,852 hrs · 24,027 cycles

A131 OVERHEAD CREW LIFE VEST CMM 25-60-06, CMM 25-64-02 CAPTAIN. R & R CAPTAIN CREW LIFE VEST IAW 145-EEL-08-12 REV 08. SEE BOW 187763 FOR FINAL INSTALL ON ACFT.

Part: WIRE — BROKEN (CABIN) · airframe 27,852 hrs · 24,027 cycles

NR 6 EMER LIGHT STRIP HAS BROKEN WIRE. R & R NR 6 EMER LIGHT FLOOR STRIP IAW AMM 33-50-12. OPERATIONS CHECKED GOOD.

Part: SKIN — CRACKED (FUSELAGE) · airframe 27,852 hrs · 24,027 cycles

LEFT AFT FUSELAGE, SKIN CRACK AT FRAME 75 ABOVE STRINGER 2L. ACCOMPLISHED REPAIR LT AFT FUSELAGE AT FRAME 75 ABOVE STRINGER 2L IAW ERS-EM-53MR-1322. SEE WIPS & TASKS FOR DETAILS.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 27,852 hrs · 24,027 cycles

FRAME 65 CORRODED AROUND LOWER CARGO DOOR STRIKER PLATE. REPAIRED FRAME 65 LOWER CARGO DOOR STRIKER PLATE IAW ERS-EM-53MR-1321.

Part: LIGHT — DAMAGED (CABIN) · airframe 27,851 hrs · 24,026 cycles

NUMBER 6 LT EMER LIGHT STRIP EXTRUSION DAMAGED. R & R NR 6 EMER LIGHT STRIP EXTRUSION IAW AMM 33-50-12. SEE BOW 187762 FOR FINAL INSTALL.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 27,851 hrs · 24,026 cycles

LEFT BEAM OTBD SUPPORT IS CRACKED AT FRAME 48. R & R OTBD SUPPORT FOR LT BEAM BETWEEN FRAME 45 - 50 OVER THE WING BOX IAW SRM 53-23-02.

Part: LIGHT — DAMAGED (CABIN) · airframe 27,851 hrs · 24,026 cycles

NUMBER 1 LT EMER LIGHT STRIP EXTRUSION DAMAGED. R & R NR 1 LT EMER LIGHT STRIP EXTRUSION IAW AMM 33-50-12. SEE BOW 187762 FOR FINAL INSTALL.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 27,851 hrs · 24,026 cycles

LEFT OMEGA BEAM IS CORRODED NEAR CROSSBEAM AT FRAME 58. BLENDED AREA ON LT OMEGA BEAM AT FRAME 58, ACCEPTED AS IS IAW ERS-EM-5300-1299.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 27,850 hrs · 24,024 cycles

ON CLIMB OUT, CARGO DOOR SHOWS OPEN, RETURNED. DEFER IAW MEL 52-5.

Part: SKIN — CRACKED (FUSELAGE) · airframe 27,851 hrs · 24,026 cycles

LEFT AFT FUSELAGE, SKIN CRACK AT FRAME 75 ABOVE STRINGER 2L. ACCOMPLISHED REPAIR LT AFT FUSELAGE AT FRAME 75 ABOVE STRINGER 2L IAW ERS-EM-53MR-1328. SEE WIPS & TASKS FOR DETAILS.

Part: LIGHT — INOPERATIVE (OVERWING EXIT) · airframe 27,554 hrs · 23,782 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,422 hrs · 23,674 cycles

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

Part: LIGHT — INOPERATIVE (OVERWING EXIT) · airframe 27,383 hrs · 23,641 cycles

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

Part: SKIN — DAMAGED (RT ELEVATOR) · airframe 27,117 hrs · 23,447 cycles

HAIL DAMAGE EVENT. R & R RT ELEVATOR UPPER CTR SKIN IAW SRM 51-20-03, 51-40-02, 51-20-03, 51-40-06, 55-20-01, 55-10-01-SI & ETN EM-55-073. SEE NRTC BOW 173731 FOR PAINT & NRTC BOW173670 FOR WEIGHT & BALANCE.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 27,114 hrs · 23,442 cycles

HAIL DAMAGE EVENT. REPLACE FWD FUSELAGE II SKIN. R & R FWD FUSELAGE II SKIN IAW SRM 51-40-02, 53-12-01, 51-40-03, 51-20-01, 51-40-06 & ETN EM-51-118 & EM-53-206.

Part: SKIN — DAMAGED (RT ELEVATOR) · airframe 27,117 hrs · 23,447 cycles

HAIL DAMAGE EVEN. REPLACE RT ELEVATOR MID SKIN TIP. R & R RT ELEVATOR MID SKIN TIP WITH SERVICEABLE SKIN IAW SRM 51-20-01, 51-20-03, 51-40-02, 51-40-06, 55-20-01 & ETN EM-55-073. SEE NRTC BOW 173731 FOR PAINT & NRTC BOW 173670 FOR WEIGHT & BALANCE.

Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 27,117 hrs · 23,447 cycles

HAIL DAMAGE EVENT. REPLACE LT ELEVATOR OTBD UPPER SKIN TIP. R & R LT ELEVATOR OTBD UPPER SKIN TIP IAW SRM 51-20-01, 51-20-03, 51-40-02, 51-40-06, 55-20-01 & ETNS EM-51-118, EM-55-073 & EM-55-076. SEE NRTC BOW173732 FOR PAINT & BOW 173670 FOR WEIGHT & BALANCE.

Part: SKIN — DAMAGED (RT ELEVATOR) · airframe 27,117 hrs · 23,447 cycles

HAIL DAMAGE EVENT. REPLACE RT ELEVATOR OUTER LE. R & R RT ELEVATOR OUTER LE IAW CPM 51-21-01, SRM 51-40-02, 51-20-03, 51-40-06, 51-40-02, 55-20-01-SI & ETN EM-55-073. SEE NRTC BOW 173731 FOR PAINT & NRTC BOW 173670 FOR WEIGHT & BALANCE.

Part: SKIN — DAMAGED (RT ELEVATOR) · airframe 27,117 hrs · 23,447 cycles

HAIL DAMAGE EVENT. REPLACE RT ELEVATOR OTBD UPPER SKIN TIP. R & R RT ELEVATOR OTBD UPPER SKIN TIP IAW CPM 51-21-01, SRM 51-40-02, 51-20-01, 51-40-06, 51-40-02, 51-20-03, 55-20-01 & ETNS EM-55-073. SEE NRTC BOW 173731 FOR PAINT & NRTC BOW 173670 FOR WEIGHT & BALANCE.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 27,117 hrs · 23,447 cycles

HAIL DAMAGE EVENT. REPLACE REAR FUSELAGE I SKIN. R & R REAR FUSELAGE I UPPER SKIN IAW SRM 51-40-02, 51-20-01, 51-20-03, 51-40-06, 53-31-01-SI & ETN-EM-51-118 & EM-53-266.

Part: SKIN — DAMAGED (RT HORIZ STAB) · airframe 27,117 hrs · 23,447 cycles

HAIL DAMAGE EVENT. REPLACE RT STAB UPPER SKIN. R & R RT HORIZONTAL STABILIZER UPPER SKIN IAW SRM 55-10-01-SI, 51-20-01, 51-20-03, 51-40-02, 51-40-03, 51-40-06 & ETNS EM-55-073 & EM-55-074.

Part: SKIN — DAMAGED (RT ELEVATOR) · airframe 27,117 hrs · 23,447 cycles

HAIL DAMAGE EVENT. REPLACE RT ELEVATOR INBD LE. R & R RT ELEVATOR INBD LE IAW CPM 51-21-01, SRM 51-40-02, 51-20-03, 51-40-06, 51-40-02, 55-20-01-SI & ETN EM-55-073. SEE NRTC BOW 173731 FOR PAINT & NRTC BOW 173670 FOR WEIGHT & BALANCE

Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 27,114 hrs · 23,442 cycles

HAIL DAMAGE EVENT. REPLACE LT ELEVATOR UPPER CTR SKIN. R & R LT ELEVATOR UPPER CTR SKIN IAW SRM 51-20-01, 51-40-02, 51-20-03, 51-40-06, 55-20-01 & ETNS EM-51-118, EM-55-073 & EM-55-076. SEE NRTC BOW 173732 FOR PAINT & NRTC BOW 173670 FOR WEIGHT & BALANCE.

Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 27,117 hrs · 23,447 cycles

HAIL DAMAGE EVENT. REPLACE LT ELEVATOR OUTER LE. R & R LT ELEVATOR OUTER LE IAW SRM 51-40-02, 51-20-03, 51-20-01, 51-40-06, 55-20-01-SI & ETN EM-55-073, ERS-EM-5300-205. SEE NRTC BOW 173732 FOR PAINT & NRTC BOW 173670 FOR WEIGHT & BALANCE.

Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 27,114 hrs · 23,442 cycles

HAIL DAMAGE EVENT. REPLACE LT ELEVATOR INBD LE. R & R LT ELEVATOR INBD LE IAW SRM 51-40-02, 55-20-01 & ETN EM-55-073. SEE NRTC BOW 173670 FOR WEIGHT & BALANCE & NRTC BOW 173732 FOR PAINT.

Part: SKIN — DAMAGED (LT HORIZ STAB) · airframe 27,117 hrs · 23,447 cycles

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

Part: SKIN — DAMAGED (FUSELAGE) · airframe 27,117 hrs · 23,447 cycles

HAIL DAMAGE EVENT. REPLACE CTR FUSELAGE II SKIN TOP. R & R CTR FUSELAGE II TOP SKIN IAW SRM 51-40-03, 51-20-01, 51-20-03, 51-40-02, 51-40-06 & ETN-EM-51-118 & EM-53-263.

Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 27,117 hrs · 23,447 cycles

HAIL DAMAGE EVENT. REPLACE LT ELEVATOR MID SKIN TIP. R & R LT ELEVATOR MID SKIN TIP IAW SRM 51-20-01, 51-20-03, 51-40-02, 51-40-06, 55-20-01 & ETN EM-55-073. SEE NRTC BOW 173732 FOR PAINT & NRTC BOW 173670 FOR WEIGHT & BALANCE.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 27,114 hrs · 23,442 cycles

RIGHT STAB RIB 2 CRACKED. ACCOMPLISHED REPAIR OF RT STAB RIB 2 IAW ERS-EM-55MR-210.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 27,109 hrs · 23,440 cycles

HAIL DAMAGE EVENT. REPLACE RT CTR FUSELAGE I. R & R RT CTR FUSELAGE 1 SKIN IAW SRM 53-22-01 SI, 51-40-02, 51-20-01, 51-20-03, 51-40-06, ETN-EM-53-263 & ETN-EM-51-118.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 27,109 hrs · 23,440 cycles

HAIL DAMAGE EVENT. REPLACE LT CTR FUSELAGE 1 SKIN. R & R LT CTR FUSELAGE 1 SKIN IAW SRM 53-22-01 SI, 51-40-02, 51-20-01, 51-20-03, 51-40-06, ETN-EM-53-263 & ETN-EM-51-118.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,929 hrs · 23,274 cycles

LEFT OVERWING EMER LIGHT IS INOPERATIVE. R & R LT OVERWING EMER LIGHT LAMP ASSEMBLY IAW AMM 33-50-07. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 26,092 hrs · 22,531 cycles

LEFT AFT EXTERNAL OVERWING EXIT EMER LIGHT INOPERATIVE. RE SEATED LAMP AT LT AFT EXTERNAL OVERWING EXIT EMER LIGHT IAW AMM 33-50-10. OPERATIONS CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 25,798 hrs · 22,307 cycles

DURING FLIGHT 3514 FOUND CABIN COMPARTMENT AFT FLASHLIGHT INOPERABLE. THE ACFT WAS REMOVED FROM SERVICE. CORRECTIVE ACTION R & R CABIN COMPARTMENT AFT FLASHLIGHT IAW AMM 33-50-16. OPERATIONS CHECKED GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 25,741 hrs · 22,255 cycles

EMERGENCY LIGHTS HAD BEEN LEFT ON. FRONT 2/3 OF AISLE LIGHTS DO NOT WORK. R & R EMERGENCY LIGHTING BATTERY PACKS NR 1, 2 & 3 IAW AMM 33-50-04. OPERATIONS CHECKED NORMALLY IAW AMM 33-50-00. NR 2 PN 2013-1A & SN 67267.

Part: LIGHT — INOPERATIVE (OVERWING EXIT) · airframe 25,549 hrs · 22,082 cycles

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

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 25,297 hrs · 21,805 cycles

FLIGHT ATTENDANT FWD FLASHLIGHT INOPERATIVE. REPLACED FWD FLIGHT ATTENDANT FLASHLIGHT, OPERATIONS CHECKED NORMAL IAW AMM 33-51-01.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 25,205 hrs · 21,735 cycles

FLASHLIGHT INTERMITTENT TURN ON FOR JUMP SEAT. R & R FWD FLIGHT ATTENDANT FLASHLIGHT ASSEMBLY IAW AMM 33-50-16, OPERATIONS CHECKED GOOD.

Part: MANIFOLD — BROKEN (APU) · airframe 25,104 hrs · 21,653 cycles

STRONG SMELL OF RAW FUEL IN CABIN & COCKPIT DURING TAXI. AIRCRAFT WAS REMOVED FROM SERVICE. OUTER APU FUEL MANIFOLD ASSEMBLY LINE BROKEN, FOUND DURING T-SHOOTING OF FUEL SMELL. REMOVED AND REPLACED SECONDARY APU FUEL MANIFOLD ASSY IAW AMM 49-31-06. OPC GOOD AT THIS TIME.

Part: FLASHLIGHT — MISSING (CABIN) · airframe 24,972 hrs · 21,539 cycles

FLIGHT ATTENDANT ROW 18 FLASHLIGHT MISSING. INSTALLED AFT FLIGHT ATTENDANT FLASHLIGHT IAW AMM 33-50-16. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,726 hrs · 21,352 cycles

LT OVERWING EMERGENCY LIGHT INOPERATIVE. R & R LT OVERWING EMERGENCY LIGHT IAW EMB 145 AMM 33-50-10-000-801-A & 33-50-10-400-801-A, OPERATIONS CHECKED GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 24,362 hrs · 21,064 cycles

LT OVERWING EMERGENCY LIGHT INOPERATIVE. R & R LAMP IAW AMM TASK 33-50-10-000-801-A AND 33-50-10-400-801-A. OPS CHECKED GOOD.

Part: LIGHT — WRONG PART (ROW 9A) · airframe 23,779 hrs · 20,601 cycles

F/A REPORTED EMERGENCY FLOOR LIGHT STRIP IS INCORRECT AT OVERWING EXIT. R & R EMERGENCY LIGHT STRIP AT EMERGENCY ROW SEAT 9A IAW AMM 33-50-12. OPS CHECK GOOD

Part: LIGHT — BROKEN (CABIN) · airframe 23,736 hrs · 20,563 cycles

EMERGENCY LIGHTS BROKEN. R & R EMERGENCY LIGHT IAW AMM 33-50-12.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 23,736 hrs · 20,563 cycles

EMERGENCY LIGHT AT OVERWING EXIT CEILING PANEL INOPERATIVE. R & R LAMP IAW AMM 33-50-08. OP CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,736 hrs · 20,563 cycles

EMERGENCY LIGHT INOPERATIVE. R & R EMERGENCY LIGHT IAW AMM 33-50-12. OPS CHECKED GOOD.

Part: CRADLE — OVERHEATED (FWD FLASHLIGHT) · airframe 23,620 hrs · 20,473 cycles

DURING B INSPECTION, FOUND FORWARD PASSENGER CABIN FLASHLIGHT CRADLE HAD EVIDENCE OF OVERHEATING. ACFT REMOVED FROM SERVICE. R & R FLASHLIGHT ASSY IAW AMM 33-50-16. OPS TESTED GOOD. ACFT RETURNED TO SERVICE.

Part: INTERPHONE — MALFUNCTIONED · airframe 23,612 hrs · 20,466 cycles

F/A CALLED TO REPORT THAT PILOT INPHONE AND PILOT EMERGENCY LIGHTS HAD COME ON BOTH CABIN ICUS. NO LIGHTS WERE ON IN COCKPIT ICU. ALL BUTTONS WERE CYCLE ON COCKPIT AND BOTH ICUS AND BOTH HANDSETS WERE RESETED ON BOTH CABIN ICUS. ALSO PA WOULD NOT SWITCH FROM ANY STATION AND CHIMES WOULD NOT RING IF CYCLING ATTD CALL BUTTON OR NOT SMOKING OR SEAT BELT SIGNS. DECALRED AN EMERGENCY AND LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. PERFORMED OPS TEST OF THER PASSENGER ADDRESS AND CABIN INTERPHONE SYS IAW AMM 23-31-00. THE OPS TESTED GOOD. ACFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 23,407 hrs · 20,305 cycles

DURING B INSPECTION, FOUND THE EMERGENCY LIGHT OVER THE LT WING TO FUSELAGE FAIRING INOPERABLE. THE ACFT WAS REMOVED FROM SERVICE. REPLACED BULB IAW MM 33-50-10. THE OPS CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: OUTFLOW VALVE — FAULTY (CABIN PRESSURE)

THE CREW REPORTED THEY LOST CABIN PRESSURIZATION AT 35,000 FEET. THE CREW DIVERTED AND DECLARED AN EMERGENCY. THE ACFT LANDED WITHOUT INCIDENT. THE ACFT WAS REMOVED FROM SERVICE. PLACED ON MEL 21-21, AUTH 060332 DMCM PROCEDURES COMPLIED WITH. R & R ELECTROPNEUMATIC OUT FLOW VALVE IAW AMM 21-31-00. PRESSURIZATION CHECK GOOD AT THIS TIME. MEL RESTORED. THE ACFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (OVERWING EXIT) · airframe 22,363 hrs · 19,510 cycles

DURING B INSPECTION FOUND THE RIGHT UPPER OVERWING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT UPPER OVERWING EMERGENCY LIGHT LAMP IAW EMB AMM 33-50-10-000-801-A AND 33-50-10-400-801-A . THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: PUMP — LEAKING (LT ENGINE) · airframe 22,304 hrs · 19,462 cycles

ON FLIGHT 3551 THE CREW REPORTED THEY OBSERVED HYD 1 LO QTY IN FLIGHT. QTY CONTINUED TO DROP IN FLIGHT. DECLARED EMERGENCY AND DIVERTED TO RDU. HYD QTY NEAR "0" UPON LANDING. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. INSPECTED AND FOUND NR 1 HYD PUMP ENGINE TO BE LEAKING REMOVED AND REPLACED E-1 HYD PUMP IAW AMM 29-10-03 AND PERFORM ALL RUNS LEAK CHECKS ALL GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: HOLDER — UNSERVICEABLE (FLASHLIGHT) · airframe 22,243 hrs · 19,417 cycles

ON FLIGHT 4096 THE CREW REPORTED THE REAR CABIN FLASHLIGHT HOLDER INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPLACED FLASHLIGHT HOLDER IAW EMB-145 M/M 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONNECTOR — LOOSE (FLASHLIGHT) · airframe 22,223 hrs · 19,399 cycles

ON FLIGHT 4033 THE CREW REPORTED THE FLASHLIGHT ABOVE SEAT 18B WAS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. RE-SECURED POWER PLUG TO BATTERY. THE OPERATIONAL CHECK WAS GOOD IAW AMM 33-50-16. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 22,197 hrs · 19,380 cycles

DURING PS-2 CHECK FOUND THE LEFT FORWARD WING FAIRING, FIRST CABIN CEILING, COCKPIT AND MAIN PASSENGER DOOR EMERGENCY LIGHTS FAILED TO ILLUMINATE. THE AIRCRAFT WAS REMOVED FROM SERVICE. TROUBLESHOT PER WM 33-50-50 AND REMOVED AND REPLACED THE NR 1 EMERGENCY BATTERY & CHARGER ASSEMBLY IAW EMB AMM 33-50-04. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 22,139 hrs · 19,339 cycles

DURING MAINTENANCE INSPECTION FOUND THE NR 1 EMERGENCY LIGHT BATTERY UNABLE TO PROVIDE POWER. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMVOED AND REPLACED THE NR 1 EMERGENCY LIGHT BATTERY IAW AMM 33-50-04. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 21,230 hrs · 18,648 cycles

DURING B INSPECTION FOUND THE RIGHT FORWARD EXTERIOR OVERWING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT EXTERNAL OVERWING EMERGENCY LIGHT LAMP IAW EMB AMM 33-50-07-000-801-A AND EMB AMM 33-50-07-400-801-A. THE OPERATIONAL CHECK WAS GOOD IAW EMB AMM 33-50-00-700-801-A. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CRADLE — BROKEN (FLASHLIGHT) · airframe 20,965 hrs · 18,427 cycles

FLIGHT 3962, CREW REPORTED THE FLASHLIGHT CRADLE BEHIND THE CAPTAIN’S SEAT HAS A BROKEN CLIP. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE FLASHLIGHT ASSEMBLY PER MM 33-50-16. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CRADLE — BROKEN (FWD FLASHLIGHT) · airframe 20,828 hrs · 20,828 cycles

FLIGHT 3914, FLIGHT ATTENDANT FORWARD CABIN FLASHLIGHT HOLDER BROKEN. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE FORWARD CABIN FLASHLIGHT AND HOLDER IAW AMM 33-50-16. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — DEFECTIVE (EXTERIOR) · airframe 19,674 hrs · 17,448 cycles

DURING B-INSPECTION FOUND MAIN CABIN DOOR MOUNTED EMERGENCY LIGHT DIM. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED MAIN DOOR EXTERNAL EMERGENCY LAMP IAW EMB AMM 33-50-10-000-801-A AND 33-50-10-400-801-A OPERATIONAL WAS CHECK GOOD. THE AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — DEFECTIVE (CABIN) · airframe 19,334 hrs · 17,164 cycles

DURING MAINTENANCE INSPECTION FOUND THE LEFT AFT OVERWING EMERGENCY EXIT LIGHT TO BE DIM. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE SERVICEABLE LEFT AFT OVERWING EMERGENCY EXIT LIGHT ASSEMBLY IAW EMB 145 AMM 33-50-07. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: PROXIMITY SENSOR — FALSE INDICATION (SPOILERS)

FLIGHT 2915, CREW REPORTED THAT AT 20,000 WITH CRUISE THRUST SETTING, RECIVED EICAS SPOILER FAIL, EICAS INDICATED SPOILER OPEN. COMPLIED WITH AOM 1 PROCEDURE FOR INADVENTENT SPOILER OPENING IN FLT. AFTER PULLING C/B F13, F14, &F21, CONTINUED TO GET AN INTERMITTENT EICAS SPOILER FAIL & GREEN OPEN SPOILER INDICATION. DURING FLIGHT AIRCRAFT SEEMED NORMAL NO AIRSPEED OR PITCH CHANGES WERE NOTED SPEED BRAKES WERE NOT USED AT ANY TIME. DURING APPROCH & LANDING ALL SYSTEMS INDICATION NORMAL AND EICAS SPOILER FAIL MSG WAS NOT PRESENT. DECLARED AN EMERGENCY AND LANDED AT DESTINATION. ACFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT OUTBOARD SPOILER PROXIMITY SENSOR IAW AMM 27-63-04. THE SPOILER OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: PROXIMITY SENSOR — INOPERATIVE (SPOILER) · airframe 18,988 hrs · 16,931 cycles

ON FLIGHT 2780 THE CREW REPORTED AT 34,000 FEET WITH CRUISE THRUST SETTING RECEIVED EICAS MESSAGE "SPOILER FAIL" AND GREEN SPOILER "OPEN" INDICATION. THE CREW COMPLIED WITH AOM PROCEDURES FOR INADVERTENT SPOILER OPENING IN FLIGHT. AFTER PULLING CB`S F13 F14 & F21", CONTINUED TO INTERMITTENTLY GET "SPOILER FAIL" AND "OPEN" INDICATION THROUGHOUT THE DESCENT. UPON LANDING THE SPOILER INDICATE "CLD, UPON TAXI IN RECEIVED "SPOILERS FAIL". THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE PROXIMITY SENSOR IAW AMM 27-63-04. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: VALVE — INOPERATIVE (CABIN PRESSURE) · airframe 18,151 hrs · 16,289 cycles

ON FLIGHT 3512 THE CREW REPORTED THAT DURING THE CIMBOUT AT 14000 FEET, RECEVIED THE CABIN ALT WENT THROUGHT 10, 000, CAB P WAS 1.7. THE CREW WAS UNABLE TO PRESSURIZE THE CABIN IN EITHER AUTO OR MANUAL MODES. THE CREW COMPLETED THE REQUIRED CHECKLISTS. THE CREW ELECTED TO DIVERT TO TLH. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPLACED GROUND CONNECTION VALVE IAW EMB AMM 21-22-04. PERFORMED MANUAL PRESSURATION IAW EMB AMM 21-31-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: HOLDER — BROKEN (FLASHLIGHT) · airframe 18,117 hrs · 16,262 cycles

FOR FLIGHT 4165 MAINTENANCE REPORTED THE FORWARD FLIGHT ATTENDANT EMERGENCY FLASHLIGHT HOLDER WAS BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FORWARD FLIGHT ATTENDANT FLASHLIGHT HOLDER IAW AMM 33-50-16. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: TARGET — OUT OF ADJUST (NLG) · airframe 16,008 hrs · 14,664 cycles

ON FLIGHT 3959 AFTER ROTATION THE CREW RECEIVED A LAND AIR/GROUND FAIL MESSAGE ON EICAS. THE GEAR LEVER WOULD NOT RISE. THE CREW ELECTED TO RETURN FOR A NORMAL LANDING. THE AIRCRAFT LANDED UNDER MAXIMUM LANDING WEIGHT. THE EICAS CAUTION MESSAGE WENT AWAY ON TAXI IN. THE AIRCRAFT WAS REMOVED FROM SERVICE. ADJUSTED NOSE LANDING GEAR (WEIGHT ON WHEELS) TARGET IAW EMB - 145 AMM 32-63-05 AND PERFORMED EXTENSION AND RETRACTION TEST. NO PARTS REMOVED OR REPLACED. THE OPERATIONAL CHECK WAS GOOD.

Part: SLEEVE — BLOWN (AC BAY) · airframe 14,686 hrs · 13,615 cycles

ON FLIGHT 3617 DURING TAKEOFF THE CREW RECEIVED PACK 2 VALVE CLOSED AND BLEED 2 VALVE CLOSED MESSAGE ON EICAS. THE CREW NOTICED THE CABIN ALTITUDE WAS CLIMBING INTO AMBER. THE CREW DECLARED AN EMERGENCY AND RETURNED TO MIA LANDING WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED BLOWN SLEEVE AT NR 2 ENVIRO UNIT IAW AMM 21-51-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,655 hrs · 13,589 cycles

FOR FLIGHT 3468 DURING A MAINTENANCE CHECK FOUND THE EMERGENCY LIGHTING-PROXIMITY FLOOR STRIP ROWS 10 THRU 12 TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED LIGHT STRIP-FLOOR PROXIMITY ROWS 10 THRU 12 IAW EMB 145 AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: TORQUE BOX — DAMAGED (RT WING) · airframe 14,420 hrs · 13,380 cycles

DURING THE MAINTENANCE BASE VISIT THE RIGHT LOWER WING TORQUE BOX RIB WAS FOUND TO HAVE AN OVERSIZED HOLE OUTBOARD FORWARD OF THE HOLE WITH BUSHING INSTALLED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED, FABRICATED AND INSTALLED BUSHING ON THE RIGHT LOWER WING TORQUE BOX IAW EO EM-57MR-465. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 14,420 hrs · 13,380 cycles

DURING MAINTENANCE BASE VISIT FOUND THE SERVICE DOOR CENTER SILL TO BE CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED NEW SERVICE DOOR CENTER SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FITTING — CORRODED (LAVATORY) · corrosion level 2 · airframe 14,420 hrs · 13,380 cycles

DURING MAINTENANCE BASE VISIT FOUND THE LAVATORY BUCKET HAD CORRODED AROUND THE DUMP FITTING AND LOWER FASTENERS. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED LAVATORY BUCKET IAW EMB SRM 53-31-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SKIN — DEFORMED (ZONE 100) · airframe 9,755 hrs · 9,109 cycles

ON FLIGHT 4177 - DURING PUSHBACK CREW PUSHED AIRCRAFT BACK OVER BAGGAGE CART DAMAGING AIRCRAFT SKIN AT FRAMES 74-75 AND BETWEEN STRINGERS 19R-19L. AIRCRAFT REMOVED FROM SERVICE. REPAIRED BY REMOVING AND REPLACING DAMAGED MATERIALS, SKIN, FRAMES, STRINGERS IN THE EFFECTIVE AREA IAW EO NR EM53MR-1033R1 AND EMB SRM 53-00-03. AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY — OVERTEMP (NR 2)

NR 2 BATTERY OVERTEMP INDICATION DURING FLIGHT. DECLARED EMERGENCY NO EVENT. REMOVED AND REPLACED NR 2 MAIN BATTERY IAW EMB AMM 24-36-00, OPS CHECK GOOD. RETURNED AIRCRAFT TO SERVICE. (M)

Part: BEAM — CORRODED (FUSELAGE)

DURING MBV FOUND THE LT OMEGA BEAM AT FRAME 20 WAS CORRODED. PERFORMED CUTOUT OF THE OMEGA BEAM TO REMOVE CORROSION. PREPARED DOUBLER, FILLER, 2 SHIMS AND PLATE. REPAIR DONE IAW SRM. (K)