N942LL

Part: NUT PLATE — CORRODED (ACCESS PANEL) · corrosion level 2 · airframe 42,392 hrs · 37,471 cycles

00125 WING LOWER SKIN ACCESS HOLE FOR 6532AB INTERNAL NUTPLATE RING IS CORRODED. REMOVED CORRODED RING ASSY AND INSTALLED NEW SERVICABLE NUTPLATE MOUNTING RING ASSY P/N 145-67342-402 IAW EMB145 SRM 51-40-02

Part: SUPPORT BRACKET — CRACKED (RT WING) · corrosion level 2 · airframe 42,392 hrs · 37,471 cycles

00252 RH WING PANEL SUPPORT BRACKETS ON WING UPPER SURFACE ALONG Y 1085 ARE CRACKED. INSTALLED NEW SERVICEABLE ANGLES P/N 145-67034-002,P/N 145-67291-002 AND P/N 145-67290-004 @ RH OVERWING IAW EMB145LR SRM 51-40-02. SPLICED AND LOCATED AND DRILLED NEW FAIRING ANGLE AND INSTALLED AS PER SRM 57-20-01-RE IAW ETD2024-145-005780 AND INSTALLED FREEZE PLUGS IN O/S HOLE IAW ETD2024-145-005780 & EO1-57-24-0155

Part: FLOOR SUPPORT — CORRODED (FRMS 20-22) · corrosion level 2 · airframe 42,392 hrs · 37,471 cycles

00161 RH SERVICE DOOR FLOOR SILL IS CORRODED BETWEEN FRM20 AND FRM22. INSTALLED NEW R/H SERVICE DOOR SILL "CHANNEL" BETWEEN FRM 20 AND FRM 22 IAW EMB145 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FRMS 22-23) · corrosion level 2 · airframe 42,392 hrs · 37,471 cycles

00160 RH FLOOR SILL PLATE ANGLE IS CORRODED BETWEEN FRM22 AND FRM23. INSTALLED NEW R/H FLOOR SILL PLATE ANGLE BETWEEN FRAME 22 AND FRAME 23 IAW EMB145 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FRMS 28-29) · corrosion level 2 · airframe 42,392 hrs · 37,471 cycles

00183 RH FLOOR SILL IS CORRODED BETWEEN FRM28 AND FRM29. INSTALLED NEW RH FLOOR SILL FROM FRM 23.4 TO 29.4 PN: 145-20609-005 IAW EMB 145 SRM 51-40-02-PR

Part: FRAME — CORRODED (FRM 22 S15-16R) · corrosion level 2 · airframe 42,392 hrs · 37,471 cycles

00235 FRAME 22 IS CORRODED BETWEEN STRINGER 15R AND 16R. REPAIRED FRAME 22R BETWEEN STR15R AND 16R IAW EMB 145 SRM 53-00-04-RE

Part: FLOOR SUPPORT — CORRODED (FRMS 59-60) · corrosion level 2 · airframe 42,392 hrs · 37,471 cycles

00233 AFTER REMOVAL OF CENTER Y0 FLOOR SUPPORT CAP FOUND ATTACHING BEAM IS CORRODED BETWEEN FRM59 AND FRM60. COMPLIED WITH EMB145 ETD 2024-145-004237 REV A PERMANENT REPAIR PROCEDURE

Part: FLOOR SUPPORT — CORRODED (FRMS 29-36) · corrosion level 2 · airframe 42,392 hrs · 37,471 cycles

00215 LH FLOOR SILL IS CORRODED OUT OF LIMITS BETWEEN FRM 29 AND FRM 36 AND REQUIRES REPLACEMENT. REMOVED CORRODED SILL AND INSTALLED NEW SERVICEABLE LH FLOOR SILL P/N 145-20609-003 AT FRM 29 TO FRM 36 IAW EMB-145 SRM 145/1142 51-40-02-PR

Part: FLOOR SUPPORT — CORRODED (FRMS 23-29) · corrosion level 2 · airframe 42,392 hrs · 37,471 cycles

00214 LH FLOOR SILL IS CORRODED OUT OF LIMITS BETWEEN FRM 23 AND FRM 29 AND REQUIRES REPLACEMENT. REMOVED CORRODED SILL AND INSTALLED NEW SERVICEABLE SILL P/N 145-20609-001 AT FRM 23 TO FRM 29 IAW EMB-145 SRM 145/1142 51-40-02-PR

Part: FLOOR SUPPORT — CORRODED (FRMS 52-59) · corrosion level 2 · airframe 42,392 hrs · 37,471 cycles

00199 LH FLOOR SILL IS CORRODED FROM FRM52 TO FRM59. REMOVED AND INSTALLED NEW SERVICEABLE SILL P/N 145-20609-001 AT FRM 52 TO FRM 59 IAW EMB-145 SRM 145/1142 51-40-02-PR

Part: FLOOR SUPPORT — CORRODED (FRMS 59-60) · corrosion level 2 · airframe 42,392 hrs · 37,471 cycles

00205 CENTER Y0 FLOOR SUPPORT CAP IS CORRODED BETWEEN FRM59 AND FRM60. REMOVED AND REPLACE CENTER Y0 FLOOR SUPPORT CAP @ FR. 59-60 IAW EMB 145 SRM 51-40-02

Part: FLOOR SUPPORT — CORRODED (FRMS 59-61) · corrosion level 2 · airframe 42,392 hrs · 37,471 cycles

00204 RH Y+479 FLOOR SUPPORT CAP IS CORRODED BETWEEN FRM59 AND FRM61. REMOVED CORRODED CAP AND INSTALLED NEW R/H +479 FLOOR SUPPORT CAP BETWEEN FR59-FR 61 IAW EMB 145LR SRM 51-40-00 AND IAW EMB 145LR SRM 51-40-09.

Part: FLOOR SUPPORT — CORRODED (FRMS 59-61) · corrosion level 2 · airframe 42,392 hrs · 37,471 cycles

00206 LH Y-479 FLOOR SUPPORT CAP IS CORRODED BETWEEN FRM59 AND FRM61. REPLACED FLOOR SUPPORT CAP (GUSSET) BETWEEN FRAME 59 AND FRAME 61 IAW EMB-145 SRM 53-24-10-RE

Part: FLOOR SUPPORT — CORRODED (FRMS 52-59) · corrosion level 2 · airframe 42,392 hrs · 37,471 cycles

00198 RH FLOOR SILL IS CORRODED FROM FRM52 TO FRM59. REMOVED R/H FLOOR SILL FROM FRM 52 TO FRM 59 IAW EMB145 SRM 51-40-02. INSTALLED R/H FLOOR SILL FROM FRM 52 TO FRM 59 IAW EMB145 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FRMS 36-40) · corrosion level 2 · airframe 42,392 hrs · 37,471 cycles

00196 CENTER Y0 FLOOR SUPPORT CAP IS CORRODED BETWEEN FRM36 AND FRM40. REMOVED CORRODED GUSSET AND INSTALLED NEW SERVICEABLE GUSSET PN/ 145-30634-003 @ CENTER Y0 FLOOR SUPPORT FROM FR. 36 - 40 IAW EMB145-LR 51-40-02

Part: FRAME — CORRODED (FRM 59 S19-20R) · corrosion level 2 · airframe 42,392 hrs · 37,471 cycles

00200 FRAME 59 IS CORRODED BETWEEN STGR 19R AND 20R. UPON FURTHER EVALUATION FOUND TO BE CORRODED SHEAR CLIP ONLY. INSTALLED FABRICATED SHEAR CLIP @ FR 59 BETWEEN STRGS 19R AND 20R IAW EMB145 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FRMS 36-40) · corrosion level 2 · airframe 42,392 hrs · 37,471 cycles

00194 LH Y-479 FLOOR SUPPORT CAP IS CORRODED BETWEEN FRM35 AND FRM40. REMOVED CORRODED GUSSET AND INSTALLED A NEW SERVICEABLE GUSSET PN: 145-30634-001 IAW EMB-145 SRM 51-40-02-PR

Part: FLOOR SUPPORT — CORRODED (FRMS 29-36) · corrosion level 2 · airframe 42,392 hrs · 37,471 cycles

00185 RH FLOOR SILL IS CORRODED BETWEEN FRM29 AND FRM36. : BLENDED CORROSION IAW EMB-145 SRM 51-10-03-PR. FOUND TO BE OUT OF LIMITS IAW EMB-145 SRM 53-23-10-AD DUE TO DEPTH OF CORROSION. DEEPEST BLEND DEPTH IS .027. MAX ALLOWED IS .015. LOCATED AND DRILLED NEW SILL PN 145-20609-007 IAW EMB145 SRM 51-20-03PR. INSTALLED NEW SILL IAW EMB145 SRM 51-40-02PR

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,970 hrs · 36,990 cycles

FLAP LOW SPEED FOLLOWED BY SPS ADVANCE AFTER TAKEOFF. R+R FLAP ELECTRONIC CONTROL UNIT IAW 27-53-02. FLAPS OPS CHECK GOOD IAW 27-53-00. A/C GOOD FOR SERVICE

Part: DOOR — UNSECURE (MAIN) · airframe 40,623 hrs · 35,557 cycles

MAIN DOOR LEVER GETS STUCK HALFWAY. UNABLE TO OPEN DOOR FROM INSIDE. NEED ASSIST FROM OUTSIDE WITH EXTERNAL LEVER. FOUND MAIN DOOR LEVER NOT PROPERLY SECURED. RESECURED IAW AMM 52-18-05 OPS CHECK GOOD. ORIG SUBMISSION DATE: 11/15/2022

Part: NONE — BROKEN (CABIN) · airframe 40,529 hrs · 35,451 cycles

FLT ATTD FLASH LIGHT HOLDER FWD CABIN BROKEN-C/A-RAR OF FLASHLIGHT CLIP ABOVE FLT ATTD SEAT OPS CHK GOOD IAW CMM 25-60-14

Part: NONE — NONE · airframe 40,337 hrs · 35,224 cycles

FA FLASHLIGHT CRADLE BROKEN-C/A-RAR FA FLASHLIGHT ASSEMBLY IAW EMB AMM 33-50-16-000-801-A AND 33-50-16-400-801-A. OPC GOOD. END.

Part: LIGHT — BURNED OUT (12) · airframe 40,103 hrs · 34,960 cycles

ROW 12 AISLE EMERGENCY LIGHT INOP-C/A-RAR ROW 12 AISLE EMERGENCY LIGHT LAMP IAW EMB AMM 33-50-08-000-801-A AND 33-50-08-400-801-A. OPC GOOD.

Part: NONE — NONE · airframe 39,708 hrs · 34,499 cycles

SUPPLEMENTAL C/A FOR FA FORWARD FLASHLIGHT HARD TO TURN ON AND OFF-C/A-DEFERRED FA FLASHLIGHT PER MEL 25-32 M PROCEDURES C/W -C/A-RAR FA FLASHLIGHT IAW PS-2 CHECK. OPS CHECK GOOD. MEL RESTORED.

Part: NONE — NONE · airframe 39,213 hrs · 33,951 cycles

AFT FLASHLIGHT HOLDER BROKEN-C/A-RAR AFT FLASHLIGHT ASSY IAW EMB 145 AMM 33-50-16. NO FURTHER DEFECTS NOTED.

Part: NONE — NONE · airframe 38,989 hrs · 33,710 cycles

EMERGENCY LIGHTS IN GALLEY AND STRIP LIGHTS ROWS 1-7 COM ON INTERMITTENTLY WITH SWITCH IN OFF POSITION-C/A-REMOVED AMD REPLACED BATTERY CHARGER #2 AND BATTERY PACK #2 IAW EMB145 AMM 33-50-04. OPS CHECK GOOD

Part: NONE — NONE · airframe 38,889 hrs · 33,594 cycles

AFT CABIN FLASHLIGHT HOLDER BROKEN-C/A-RAR AFT CABIN FLASHLIGHT ASSEMBLY IAW ETN-EM-33-059 OPS CHECK GOOD

Part: SUPPORT — UNDERTORQUED (PAX DOOR HANDLE) · airframe 38,269 hrs · 32,878 cycles

MAIN CABIN DOOR DIFFICULT TO OPEN AND CLOSE-C/A-C/W ETN-EM-52-052 RE-TORQUED HANDLE SUPPORT ASSEMBLY. REFERENCE AML PAGE # 4406449 ITEM #1 FOR TDMI FOR REPAIR.OPS CHECK GOOD.

Part: UNKNOWN — ODOR (CABIN) · airframe 38,043 hrs · 32,644 cycles

LAV SMOKE EICAS IN FLIGHT. NO INDICATIONS OF FIRE OR SMOKE-C/A-C/WLAV SMOKE DETECTION SYS TEST IAW EMB 145 MM 24-14-00. OPS CHECK GOOD. ALSO GVI LAV TRASH AND ENG INTAKE FOR POSSIBLE OIL. NO DEFECTS NOTED

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 38,001 hrs · 32,591 cycles

PSU EMERGENCY LIGHT AT SEAT 12A INOP.-C/A-RAR OVERWING EMERGENCY LIGHT LAMP AT SEAT 12A IAW EMB145 AMM 33-50-07. OPC GOOD.

Part: FRAME — CRACKED (FRM 68) · airframe 37,988 hrs · 32,576 cycles

LH Z FRAME AT FRAME 68 IS CRACKED JUST BELOW THE BOTTOM FASTENER HOLE FOR THE CARGO DOOR ROD HOLD OPEN SUPPORT.-C/A-REPAIRED LH Z FRAME AT FR.68 AT CARGO DOOR ROD HOLD OPEN SUPPORT IAW SRM 53-31-04 ITEM#6.

Part: FITTING — DAMAGED (LT AIL ACTUATOR) · airframe 37,988 hrs · 32,576 cycles

LT AILERON ACTUATOR FITTING IS DAMAGED ON THE AILERON.-C/A-INSTALLED NEW LH AILERON DAMPER FITTING IAW EO# EM-27MR-112.

Part: FITTING — WORN (LT AILERON) · airframe 37,988 hrs · 32,576 cycles

LT AILERON FITTING FOR THE DAMPER REQUIRES PAINT TOUCH UP ON THE AILERON. -C/A-INSTALLED NEW LH AILERON DAMPER FITTING IAW EO# EM-27MR-112.

Part: SUPPORT — CRACKED (CARGO DOOR ROD) · airframe 37,988 hrs · 32,576 cycles

BAGGAGE DOOR ROD REINFORCEMENT SUPPORT IS CRACKED.-C/A-REMOVED AND REPLACED BAGGAGE DOOR ROD REINFORCEMENT SUPPORT IAW SRM 51-40-02.

Part: SUPPORT — CRACKED (TORSION BAR) · airframe 37,988 hrs · 32,576 cycles

CARGO DOOR TORSION BAR WHEEL SUPPORT ON FRAME 68 AT STR. 4R HAS A 3/8" CRACK-C/A-REMOVED AND REPLACED SUPPORT IAW EMB-145 SRM CH. 51-40-02.

Part: FRAME — CRACKED (FRM 80 S7-8L) · airframe 37,988 hrs · 32,576 cycles

FRAME 80 L/H FRAME CLIP BETWEEN STR. 7L-8L IS CRACKED-C/A-RAR FRAME 80 LH FRAME CLIP BETWEEN STRINGERS 7L-8L IAW SRM 51-40-02.

Part: FRAME — CRACKED (FRM 80 S7-8R) · airframe 37,988 hrs · 32,576 cycles

FRAME 80 R/H FRAME CLIP BETWEEN STR. 7R-8R IS CRACKED-C/A-RAR FRAME 80 RH FRAME CLIP BETWEEN STRINGERS 7R-8R IAW SRM 51-40-02.

Part: LIGHT — DETACHED (CABIN) · airframe 37,988 hrs · 32,576 cycles

LH EMERGENCY FLOOR PATH LIGHT STRIP HAS BROKEN OFF WIRES AT BASE-C/A-COMPLETE:RAR #8 LH EMERGENCY FLOOR PATH LIGHT STRIP IAW AMM 33-50-12. OPS CK GOOD

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 37,815 hrs · 32,395 cycles

COCKPIT OVERHEAD EMERGENCY LIGHT INOPERABLE. C/A: R & R COCKPIT OVERHEAD EMERGENCY LIGHT, IAW EMB 145 AMM 33-50-05. OPERATIONS CHECK GOOD.

Part: SEAL — LEAKING (PAX DOOR) · airframe 37,324 hrs · 31,862 cycles

VERY LOUD SQUEAL FROM MAIN CABIN DOOR DURING DESCENT FROM FL 200 TO 11000. TRANSFERRED TO NRWC 942-DFW-04837 SL 222468. C/A REF NRWC 942-DFW-04828 ITEM 1 FOR CORRECTIVE ACTION. LEAK CK GOOD, NO FURTHER FAULT FOUND.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 37,119 hrs · 31,609 cycles

REJECTED TAKEOFF AT 90 KTS DUE TO A BLD 2 VLV FAIL. RED EICAS MSG WAS ALSO DISPLAYED W/ MASTER RED WARNING BUT REJECTED BEFORE BOTH PILOTS COULD READ THE RED MSG. CHECKED OK FOR DEFERRAL PER MEL 36-3. M PROCEURES C/W. PLACARD INSTALLED.

Part: DOOR SEAL — LEAKING (CABIN DOOR) · airframe 37,117 hrs · 31,608 cycles

LOUD SCREECHING NOISE FROM MAIN CABIN DOOR FROM 5,000 FT- THROUGH FL20. PERFROMED PRESSURIZATION OF AIRCRAFT IAW AMM 21-31-00 AND APPLIED DC4 ON SEAL OF MAIN DOOR IAW AMM 52-00-04. NO LEAKS NOTED AT THIS TIME.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 36,907 hrs · 31,451 cycles

COCKPIT EMERGENCY LIGHT INOP-C/A-REMOVED AND REPLACED COCKPIT EMERGENCY LIGHT LAMP IAW EMB AMM 33-50-05-000-801-A AND 33-50-05-400-801-A. OPS CHECK GOOD. END.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 36,349 hrs · 30,830 cycles

RH EXIT ROW OVERHEAD EMERGENCY LIGHT INOP-C/A-REMOVED AND REPLACED RH EXIT ROW OVERHEAD (OVERWING) EMERGENCY LIGHT LAMP IAW EMB 145 AMM 33-50-07. OPERATIONAL CHECK GOOD.

Part: UNKNOWN — UNKNOWN (CABIN PRESSURE) · airframe 35,984 hrs · 30,475 cycles

A/I MIA ACCT MECH NO PRESS, DECLRED EMERGENCY. FLIGHT CONTINUED.-C/A-FLIGHT CREW PLACARDED PACK 1 MEL 21-30 AUTH 110336D-C MOC 056048. T/S PER FIM 21-51-00-810-803 TO BLOCK 11. PERFORMED OPC OF PACK IAW AMM 21-51-00. OPC GOOD. RAN PACK FOR TWO HRS WITH NO ISSUES. MEL RESTORED. NO M PROCEDURES APPLICABLE

Part: LIGHT — INOPERATIVE (ROW 15A) · airframe 35,659 hrs · 30,201 cycles

ROW 15A FLOOR PROXIMITY STRIP INOP. REMOVED AND REPLACED 15A FLOOR PROX LIGHT IAW AMM 33-50-12 OPS CHECK GOOD.

Part: WIRE — NOT REPORTED (ELECTRICAL SYS) · airframe 35,167 hrs · 29,740 cycles

WHEN APU WAS STARTED ON THE GND BOTH PFDS WENT BLACK AND 115 VAC BUS OFF MESSAGE WAS DISPLAYED FOLLOWED BY A BURING SMELL "TRANSFERRED TO NRWC 942-ORD-04043". C/A-REMOVED AND REPLACED WIRE W126-0003-00 AND W126-0004-00 IAW AMM 24-65-00 AND SWPM 20-21-00. REMOVED AND REPLACED INTERCONNECTION BAR W1007 IAW AMM 24-60--01 AND SWPM 20-21-00. PERFORMED OPS TEST DC ELECTRICAL LOAD DISTRIBUTION SYSTEM IAW AMM 24-60-00, OPS TEST GOOD NO DEFECTS NOTED.

Part: VALVE — LEAKING (AC BAY) · airframe 35,152 hrs · 29,726 cycles

THROUGH 19,000 FT WE NOTICED THE CABIN ALT WAS RISING RAPIDLY. CABIN RATE WAS 2,000 FMP AT THE MAX. CABIN ALT HIT 11,500 DURING OUR DECENT TO 10,000. AROUND 15,000 FT SEEM LIKE AUTO PRESURIZATION WAS BACK TO NORMAL. C/A-AUTO AND MANUL MODE PRESSURIZATION DEFERRED PER MEL 21-19 AUTH # 070306DM-C. "M" PROCEDURES C/W. WHILE TROUBLSHOOT PRESSURIZATION PROBLEM FOUND AIR CONDITIONING GROUND CONNECTION VALVE LEAKING. INSTALLED AIR CONDITIONING GROUND CONNECTION VALVE O'RING AS PER AMM 21-22-04. LEAK CHECK GOOD. FOUND RT RAM AIR VAVLE CHECK VAVLE INSTALLED BACKWARDS INSTALLED RAM AIR CHECK VAVLE IAW AMM 21-25-02 REMOVED OPENING TOOLS ON ELEC. PNUEMATICE AND MANUAL OUTFLOW VAVLES PERFORMED OPERATIONAL TEST AUTO/MANUAL IAW AMM 21-31-00 SYSTEM REACTIVATED MEL 21-9 RESTORED.

Part: SWITCH — FAULTY (BLEED AIR SYS) · airframe 35,151 hrs · 29,725 cycles

SUPPLEMENTAL BLD 2 OVERTEMP IN FLIGHT "TRANSFERRED TO NRWC 942-MIA-04021". C/A-REMOVED AND REPLACED SENSOR IAW AMM 36-20-01 OPTS CHECK GOOD. REMOVED AND REPLACE BLEED LINES ORINGS AT LOCATION 2.,4,8,10,12,14,16,20,26 OPTS CHECK FAIL NO HELP IAW AMM 38-11-10. REMOVED AND REPLACED S0791 TEMP SWITCH IAW EMB AMM 36-20-02. OPS CHECK GOOD. REMOVED AND REPLACED # 2 ENGINE BLEED AIR DUCT 36-11-09.

Part: O-RING — DAMAGED (NR 1 BRAKE) · airframe 35,125 hrs · 29,704 cycles

UPON ARRIVAL AT GATE , RAMPERS ADVISED THAT NUMBER 1 FIRE WAS SMOKING. UPON FURTHER INSPECTION, NOTICED #1 BRAKE SPEWING LIQUID AND STEAM. C/A-INSPECTEWD FOUND NO FIRE ON #1 BRAKE FOUND HYDRAULIC FLUID MIST FROM #1 BRAKE BLEEDER SCREW ORING. REMOVED AND REPLACED #1 BRAKE UPPER BLEEDER VAVLE ORING IAW AMM 32-49-03 LEAK CHECK GOOD.OPS CHECK GOOD.

Part: WHEEL — FAILED (MLG) · airframe 34,938 hrs · 29,547 cycles

RIGHT AFTER LANDING TOWER REPORT SMOKE COMING OUT FROM THE RIGHT LANDING GEAR. HOLDING SHORT OF THE GATE FIRE TRUCKS REPORT FIRE COMING OUT FROM THE GEAR ALSO WHEN HOLDING SHORT OF THE GATE ALSO WE GOT THE HYD 2 LOW QTY MSG AND HYD 2 FAIL MSG.-C/A- REMOVED AND REPLACED OF RH MLG BRAKES #3 AND #4. REMOVED AND REPLACED MLG BRAKES ASSY #3 AND #4. SERVICE HYD SYSTEM IAW EMB AMM 12-13-01. A/C OK FOR SERVICE. LR MAIN WHEEL P/N 31641 S/N 01601306P #4. LR MAIN BRAKE ASSY P/N 2-1707-2 S/N 2636 #3 AND S/N 2360 #4

Part: FITTING — MISSING (RT AILERON) · airframe 33,941 hrs · 28,679 cycles

RH AILERON PCA FITTING MISSING 2EA BUSHINGS-C/A-REMOVED AND REPLACED PCA FITTING ASSEMBLY IAW EO EM-27MR-112.

Part: SUPPORT ANGLE — CRACKED (RT WING) · airframe 33,941 hrs · 28,679 cycles

RT WING TORQUE BOX NR 1, L SUPPORT ANGLE IS CRACKED. REPLACED SUPPORT ANGLE IAW SRM 51-40-02.

Part: SUPPORT ANGLE — CRACKED (WNG/BDY FAIRING) · airframe 33,941 hrs · 28,679 cycles

LH UPPER WING TO FUSELAGE SUPPORT ANGLE. JUST FWD OF FRAME 41 HAS EVIDENCE OF 1/4" CRACK. PROCEEDING DOWNWARD FROM THE RIVET. -C/A-REPAIRED LH UPPER WING TO FUSELAGE SUPPORT ANGLE JUST FWD OF FRAME 41 IAW SRM 53-23-12. SEE NRTC E683553 FOR PAINT.

Part: CROSSBEAM — CORRODED (BTWN FRMS 59-60) · airframe 33,941 hrs · 28,679 cycles

LH OMEGA BEAM HAS EVIDENCE OF CORROSION BY THE CROSS BEAM BETWEEN FRAMES 59-60.-C/A- IN REFERENCE TO WIP #6. COMPLETED REPAIR TO LH OMEGA BEAM AT FR 59-60 IAW EO EM-53MR-1518 PART A.

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 33,941 hrs · 28,679 cycles

LT LOWER NR 3 WING TO FUSELAGE SUPPORT ANGLE. HAS 1 1/2" CRACK ON THE FWD END. REMOVED AND REPLACED LT LOWER NR 3 WING TO FUSELAGE ANGLE IAW SRM 51-40-02.

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 33,941 hrs · 28,679 cycles

LT LOWER NR 1 WING TO FUSELAGE SUPPORT ANGLE. HAS 1 1/2" CRACK ON THE AFT PREVIOUS REPAIRED SPLICE. REMOVED AND REPLACED LT LOWER NR 1 WING TO FUSELAGE SUPPORT ANGLE AFT SPLICE IAW SRM 51-40-02.

Part: SUPPORT ANGLE — CRACKED (WNG/BDY FAIRING) · airframe 33,941 hrs · 28,679 cycles

RH LOWER #4 WING TO FUSELAGE SUPPORT ANGLE. HAS 2" CRACK ON THE FWD END. -C/A-REPAIRED IAW SRM 57-20-01.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 33,941 hrs · 28,679 cycles

LT UPPER WING TO FUSELAGE SUPPORT ANGLE. HAS 1" CRACK BETWEEN FRAMES 48-49. WILL BE REPAIRED DURING COMPLIANCE OF FRAME 50 CRACK NRTC E680918.

Part: SUPPORT ANGLE — CRACKED (WNG/BDY FAIRING) · airframe 33,941 hrs · 28,679 cycles

RH UPPER WING TO FUSELAGE SUPPORT ANGLE. JUST AFT OF FRAME 50 HAS EVIDENCE OF 1/2" CRACK.-C/A-REMOVED AND REPLACED RH UPPER WING-TO-FUSELAGE FAIRING SUPPORT FROM FRAME 48 TO 52 IAW SRM 51-40-02. REFER TO NRTC E684169 FOR PAINT.

Part: SUPPORT ANGLE — CRACKED (WNG/BDY FAIRING) · airframe 33,941 hrs · 28,679 cycles

LH UPPER WING TO FUSELAGE SUPPORT ANGLE. JUST AFT OF FRAME 50 HAS EVIDENCE OF 1" CRACK. -C/A-REPAIRED LH UPPER WING TO FUSELAGE SUPPORT ANGLE IAW SRM 53-23-12 AND SRM 51-40-02.

Part: SKIN — CRACKED (FRAME 75) · airframe 33,941 hrs · 28,679 cycles

1/4 INCH DIAGONAL CRACK ( TOP L TO BOTTOM R) FOUND IN FUSELAGE SKIN AT FRAME 75 JUST ABOVE STRINGER 2L. 1" AREA OF PAINT REMOVED AND AREA DYE PEN'D FOR BETTER VISIBILITY AND LOCATION OF CRACK. AREA AROUND FLAW TAPED OFF.-C/A-REPAIRED CRACK IN FUSELAGE SKIN AT FR 75 JUST ABOVE STR 21L, IAW SRM 53-31-01 AND SRM 51-40-02.

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 33,941 hrs · 28,679 cycles

LT LOWER NR 4 WING TO FUSELAGE SUPPORT ANGLE. HAS 1 1/2" CRACK ON THE FWD END. REPAIRED IAW ETN-EM-53-142.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 33,941 hrs · 28,679 cycles

RT CABIN OUTBD OMEGA BEAM LOWER SUPPORT ANGLE. HAS 3/4" CRACK ON THE INBD SUPPORT FWD END JUST AFT OF FRAME 47. REMOVED AND REPLACED RT CABIN OUTBD OMEGA BEAM LOWER INBD SUPPORT ANGLE IAW SRM 53-23-02 AND SRM 51-40-02.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 33,941 hrs · 28,679 cycles

RT CABIN OUTBD OMEGA BEAM LOWER SUPPORT ANGLE. HAS 1 1/2" CRACK ON THE OUTBD SUPPORT FWD END JUST AFT OF FRAME 47. REMOVED AND REPLACED RT CABIN OUTBD OMEGA BEAM LOWER OUTBD SUPPORT ANGLE IAW SRM 53-23-02 AND SRM 51-40-02.

Part: WIRE — DAMAGED (CABIN) · airframe 33,941 hrs · 28,679 cycles

ALL EMERGENCY LIGHT STRIPS WIRING TO EACH STRIP SEEM TO HAVE DAMAGE OR WIRE EXPOSED. C/A-COMPLETE:INSPECTED AND FOUND 2ND FROM FWD HAD A BROKEN WIRE REPLACED LIGHT IAW AMM 33-50-12.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 33,941 hrs · 28,679 cycles

CENTER OMEGA BEAM HAS EVIDENCE OF CORROSION BY THE CROSS BEAM BETWEEN FRAMES 59-60. C/A-COMPLETE:REPAIRED CENTER OMEGA BEAM AT CROSS BEAM BETWEEN FR.59-60 IAW SRM 53-24-10.

Part: WIRE — DAMAGED (CABIN) · airframe 33,941 hrs · 28,679 cycles

EMERGENCY LIGHTS ILLUMINATE WHEN AIRCRAFT POWER TURNED OFF. C/A-COMPLETE:REPAIRED DAMAGED WIRES (2 EA) BETWEEN P8524 AND SPLICE SP9000 IAW SWPM 20-21-00. PERFORMED OPS CHECK OF EMERGENCY LIGHTS IAW AMM 33-50-00. OPS CHECK GOOD, ISSUE RESOLVED.

Part: WIRE — BROKEN (CABIN) · airframe 33,941 hrs · 28,679 cycles

EMERGENCY LIGHTING SYSTEM FAILED OPERATIONAL CHECK. (LIGHTS COME ON MOMENTARILY AND THEN GO OUT AN 2 AISLE LIGHT STRIPS INOP). C/A-COMPLETE:FOUND 2 INOP AISLE LIGHT STRIPS TO HAVE BROKEN WIRES AND RAR LIGHT STRIPS IAW AMM 33-50-12. AND OPC GOOD IAW AMM 33-50-00.

Part: FITTING — FAILED (LT MLG) · airframe 33,885 hrs · 28,622 cycles

SUPPLEMENTAL FUNCTIONAL CHECK FLIGHT REQUIRED FOR ITEM ON AML #4412501/1 LG AIR/GND FAIL MSG AFTER TAKEOFF GEAR WOULD NOT RETRACT. NORMAL LANDING BACK AT MIA. AIRCRAFT RELEASED FOR FCF PURPOSES ONLY. PERFORM MULTIPLE GEAR CYCLES DURING FLIGHT. AIRCRAFT RELEASED FOR FCF PURPOSES ONLY 580315-C/A-FCF FAIL 814498. REMOVED AND REPLACED LH MLG CARDAN FITTING IAW EMB 145 AMM 32-10-09 OPS CHECKS GOOD. ADJUSTED LH MLG AFT WOW SWITCH IAW EMB 145 AMM 32-63-05 OPS CHECKS GOOD FCF FOUND SATISFACTORY

Part: ELECTRONIC UNIT — MALFUNCTIONED (LANDING GEAR) · airframe 33,885 hrs · 28,621 cycles

LG AIR/GND FAIL MSG AFTER TAKEOFF GEAR WOULD NOT RETRACT. NORMAL LANDING BACK AT MIA. REMOVED AND REPLACED LEGU IAW AMM 32-32-01 OPS CHECK GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 32,924 hrs · 27,814 cycles

CREW REPORTED THAT EMERGENCY LIGHTS WOULD NOT TURN OFF. FOUND ALL FOUR EMERGENCY LIGHT BATTERIES TO HAVE NO CHARGE. REMOVED AND REPLACED NR 1 BATTERY IAW AMM 33-50-04. OPS CHECK GOOD PER AMM 33-50-00.

Part: BATTERY — DISCHARGED (CABIN) · airframe 32,924 hrs · 27,814 cycles

NR 4 EMERGENCY LIGHT BATTERY INOP. REMOVED AND REPLACED NR 4 EMERGENCY LIGHT BATTERY IAW 33-50-04 OPS CHECK GOOD PER AMM 33-50-00.

Part: BATTERY — DISCHARGED (CABIN) · airframe 32,924 hrs · 27,814 cycles

NR 3 EMERGENCY LIGHT BATTERY INOP. REMOVED AND REPLACED NR 3 EMERGENCY LIGHT BATTERY IAW AMM 33-50-04. OPS CHECK GOOD PER AMM 33-50-00.

Part: BATTERY — DISCHARGED (CABIN) · airframe 32,924 hrs · 27,814 cycles

NR 2 EMERGENCY LIGHT BATTERY INOP. REMOVED AND REPLACED NR 2 EMERGENCY BATTERY IAW AMM 33-50-04. OPS CHECK GOOD PER AMM 33-50-00.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,436 hrs · 27,433 cycles

FLOOR EMERGENCY LIGHT STRIP BETWEEN ROWS 8 AND 9 INOPERATIVE. REMOVED AND REPLACED THE LIGHT AND OPS CHECKED GOOD IAW AMM 33-50-12.

Part: INVERTER — FAILED (EMERGENCY LIGHTS) · airframe 30,494 hrs · 25,585 cycles

CENTER AISLE OVERHEAD EMERGENCY EXIT LIGHT AT SERVICE DOOR INOPERATIVE. REMOVED AND REPLACED NR 1 BATTERY POWER SUPPLY IAW AMM 33-50-04, OPS CHECKED FAILED. REMOVED AND REPLACED THE NR 1 EMERGENCY LIGHT DC & AC INVERTER IAW AMM 33-50-11, AND OPS CHECKED FAILED. REMOVED AND REPLACED THE NR 1 EMERGENCY LIGHT DC & AC INVERTER IAW AMM 33-50-11,AND OPS CHECKED OK IAW AMM 33-50-00.

Part: CRADLE — BROKEN (AFT FLASHLIGHT) · airframe 29,666 hrs · 24,793 cycles

AFT CABIN FLASHLIGHT CRADLE IS BROKEN, FLASHLIGHT FALLS OUT. R & R THE FLASHLIGHT ASSY IAW MM 33-50-16, OPS CHECKED GOOD.

Part: HANDLE — OUT OF POSITION (PAX DOOR) · airframe 29,516 hrs · 24,651 cycles

PASSENGER DOOR DIFFICULT TO OPEN FROM INSIDE. JET BRIDGE DRIVER HAD TO OPEN FROM OUTSIDE. FOUND MAIN DOOR INTERNAL ACTUATING HANDLE OFF POSITION. REMOVED AND INSTALLED THE DOOR ACTUATING HANDLE IAW AMM TASK 52-18-05. OPS CHECK GOOD.

Part: FLOOR SUPPORT — CORRODED (COCKPIT) · airframe 29,159 hrs · 24,320 cycles

COCKPIT AFT FLOOR SUPPORT HAS CORROSION. INSTALLED A NEW FLOOR SUPPORT IAW SRM 51-20-03.

Part: DOOR FRAME — CORRODED (SERVICE DOOR) · airframe 29,159 hrs · 24,320 cycles

SERVICE DOOR LWR FRAME CORRODED. REPLACED SERVICE DOOR FRAME IAW SRM 51-40-2-02.

Part: SHEAR TIE — CORRODED (FRAME 65) · airframe 29,159 hrs · 24,320 cycles

FRAME 65 SHEAR TIE AT CARGO DOOR CUT-OUT LOWER SILL IS CORRODED. REMOVED THE SHEAR TIE AND INSTALLED A SERVICEABLE SHEAR TIE SECTION IAW SRM 53-31-04.

Part: SHEAR TIE — DAMAGED (FRAME 68) · airframe 29,159 hrs · 24,320 cycles

FRAME 68 SHEAR TIE AT CARGO DOOR CUT-OUT LWR SILL HAS MISDRILLED HOLES. REMOVED SHEAR TIE SECTIONL, PREPPED AND INSTALLED A NEW SHEAR TIE SECTION IAW SRM 53-31-04

Part: DOOR SILL — CORRODED (CARGO DOOR) · airframe 29,159 hrs · 24,320 cycles

CARGO DOOR LOWER SILL IS CORRODED. INSTALLED A NEW DOOR SILL IAW SRM 51-40-02.

Part: DOOR SILL — CORRODED (CARGO DOOR) · airframe 29,159 hrs · 24,320 cycles

CARGO DOOR LOWER SILL IS CORRODED. INSTALLED SERVICEABLE DOOR SILL IAW SRM 51-40-02.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,616 hrs · 23,807 cycles

AFT LT OVERWING EMERGENCY LIGHT INOPERATIVE. LEFT AFT OVERWING EMERGENCY LIGHT LAMP IAW AMM 33-50-10-000-801-A & 33-50-10-400-801-A. OPS CHECK GOOD AT THIS TIME.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 27,611 hrs · 22,820 cycles

FIRST OFFICERS FLASHLIGHT INOPERATIVE. FLIGHT CREW PLACARDED FIRST OFFICERS FLASHLIGHT MEL 2553. R & R FIRST OFFICERS FLASHLIGHT. OPERATIONS CHECKED GOOD. MEL ITEM RESTORED.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 27,090 hrs · 22,324 cycles

FORWARD SIDE OF OVERHEAD EXIT LOCATION SIGN AT EMER EXIT INOPERATIVE. R & R NR 6 EMER LIGHT INVERTER. OPERATIONS CHECKED GOOD IAW AMM 33-50-11.

Part: LIGHT — INOPERATIVE (OVERWING EXIT) · airframe 26,549 hrs · 21,797 cycles

LEFT LATERAL PANEL OVERWING EMER LIGHT INOPERATIVE. R & R LT LATERAL PANEL OVERWING EMER LIGHT ASSEMBLY IAW AMM 33-50-10. OPERATIONS CHECKED GOOD, NO DEFECTS NOTED.

Part: FLASHLIGHT — INTERMITTENT (CABIN) · airframe 25,707 hrs · 21,006 cycles

FLIGHT ATTENDANT REPORTS FLASHLIGHT ABOVE JUMP SEAT CHARGE LIGHT INTERMITTENT. R & R FWD FLIGHT ATTENDANT FLASHLIGHT IAW AMM 33-50-16. OPERATIONS CHECKED GOOD.

Part: SMOKE DETECTOR — OUT OF ADJUST (LAVATORY) · airframe 25,246 hrs · 20,568 cycles

WHILE SITTING AT GATE HAD LAVATORY SMOKE WARNING MSG ON EICAS & FLIGHT ATTENDANT`S HORN ON LAVATORY DETECTOR PANEL WAS SOUNDING. PERFORMED LAVATORY SMOKE DETECTION SYS ADJUSTMENT & TEST IAW AMM 26-14-00.

Part: DUCT — DAMAGED (LT ENGINE) · airframe 24,918 hrs · 20,280 cycles

TRANSFERRED FROM NRWC 942-SGF-02022 ITEM 1. LT ENG INNER RT BYPASS DUCT HAS LARGE BURN HOLE IN IT. R & R LT ENG ASSEMBLY IAW WC 71-000-00. OPERATIONS CHECK & LEAK CHECKED GOOD.

Part: ANTI-ICE VALVE — FAILED (NR 1 ENGINE) · airframe 24,617 hrs · 20,054 cycles

DURING FIRST FLIGHT OF THE DAY ANTI-ICE TEST, E1 ANTI-ICE FAIL MSG APPEARED. THE REST OF THE TEST WAS NORMAL. R & R NR 1 ANTI-ICING VLV & CHECKED OK IAW MM 30-21-01.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 24,584 hrs · 20,025 cycles

DURING MBV INSPECTION, QA FOUND SERVICE DOOR CUT OUT CORRODED AT LOWER AFT FASTENER HOLE. ACFT WAS REMOVED FROM SERVICE FOR MBV INSPECTION & WILL BE RETURNED TO SERVICE AFTER MBV INSPECTION. PERFORMED PERMANENT REPAIR ON SERVICE DOOR CUT OUT AT FRAME 22 IAW ERS-EM-53MR-726. REPAIR MATERIALS, FRAME SECTION 145-22191-015 & STOCK L ANGLE AL-T761-.080.

Part: YOKE — CRACKED (LT PYLON) · airframe 24,584 hrs · 20,025 cycles

DURING MBV INSPECTION, QA FOUND LT PYLON LOWER FWD ENG MOUNT SUPPORT YOKE CRACKED. ACFT WAS REMOVED FROM SERVICE FOR MBV INSPECTION & WILL BE RETURNED TO SERVICE AFTER MBV INSPECTION. R & R LT PYLON LOWER FWD ENG MOUNT SUPPORT YOKE IAW EO EM-54MR-386. ACFT WILL BE RETURNED TO SERVICE AFTER MBV INSPECTION.

Part: FAIRING — CRACKED (WINDSHIELD) · airframe 24,584 hrs · 20,025 cycles

COCKPIT WINDSHIELD UPPER CTR FAIRING IS CRACKED. REPAIRED IAW ETN GN-20-023R3 STEPS 2 - 5 AMM 25-00-00.

Part: BATTERY — DISCHARGED (CABIN) · airframe 24,584 hrs · 20,025 cycles

PASSENGER DOOR ENTRANCE CEILING EMER LIGHT INOPERATIVE. R & R BATTERY & CHARGER IAW WC 33-700-19. EMER LIGHTING BATTERY PN 2013-1A.

Part: MOUNT FLANGE — CORRODED (WINDSHIELD) · airframe 24,584 hrs · 20,025 cycles

PILOT'S WINDSHIELD INTERNAL MOUNTING FLANGE ON WINDSHIELD HAS CORROSION ON LOWER EDGE. REMOVED CORROSION IAW CMM 56-10-01APPLIED SURFACE PROTECTION IAW CPM 51-21-04 FOUND TO BE ACCEPTED AS IS IAW ERS-EM-5600-044 SEE TURNOVER FOR DETAILS.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 24,584 hrs · 20,025 cycles

LAVATORY RT FLOOR SUPPORT ONE AREA OF CORROSION. BLENDED LAVATORY RT FLOOR SUPPORT ONE AREA OF CORROSION ACCEPTED AS IS IAW ERS-EM-5300-702. SEE WIPS & TASK FOR ADDITIONAL INFORMATION.

Part: SUPPORT — CRACKED (NLG WW) · airframe 24,584 hrs · 20,025 cycles

NLG UPLOCK BOX SUPPORT CRACKED AT THE FWD LOWER RT CORNER. REMOVED CRACKED NLG UPLOCK BOX RT SUPPORT & INSTALLED NEW SERVICEABLE RT SUPPORT & RESTORED PROTECTIVE COATING IAW SRM 51-40-02, CPM 51-21-05, CPM 51-21-06, ETN-EM-51-075, ETN-GN-51-016R5 & ETN-EM-51-091R3.

Part: MOUNT FLANGE — CORRODED (WINDSHIELD) · airframe 24,584 hrs · 20,025 cycles

COPILOT'S WINDSHIELD INTERNAL MOUNTING FLANGE ON WINDSHIELD HAS CORROSION ON LOWER EDGE. REMOVED CORROSION IAW CMM 56-10-01, APPLIED SURFACE PROTECTION IAW CPM 51-21-04 FOUND TO BE ACCEPTED AS IS IAW ERS-EM-5600-043 SEE TURNOVER FOR DETAILS.

Part: BRACKET — CRACKED (LT NACELLE) · airframe 24,584 hrs · 20,025 cycles

LEFT PRE COOLER FWD BRACKET CRACKED. REMOVED & INSTALLED SERVICEABLE PRE COOLER BRACKET IAW SRM 51-40-02.

Part: DECK PLATE — CRACKED (E&E BAY) · airframe 24,584 hrs · 20,025 cycles

FORWARD AVIONICS BAY CTR LOWER DECK IS CRACKED AT THE RT AFT SIDE OF THE UPLOCK BOX SUPPORT AFT CROSSBEAM. REPAIRED FWD AVIONICS BAY CTR LOWER DECK AT THE RT AFT SIDE OF THE UPLOCK BOX SUPPORT AFT CROSSBEAM IAW ERS-EM-5300-725.

Part: SWITCH — FAULTY (AC PACK) · airframe 24,582 hrs · 20,023 cycles

PACK 2 WAS MELED & PACK 1 KICKED OFF TWO TIMES IN FLIGHT. R & R TEMP SWITCH PN 815291-5 & PN 815291-2 IAW AMM 21-51-08. OPERATIONS CHECKS OF PACK ONE IS GOOD. NO FURTHER DEFECTS NOTED. PACK OVER TEMP SWITCH PN 815291-5 & SN 5578. PACK 2 ON MEL FOUND LOOSE & OPEN DUCT SURROUNDING THERMAL SWITCHES. RE-TAPED DUCTING IAW AMM 21-20-02. OPERATIONS CHECKED TEMP CONTROL, OPERATIONS CHECK IS GOOD. NO FURTHER DEFECTS AT THIS TIME. MEL RESTORED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,437 hrs · 19,893 cycles

MAIN DOOR EMER LIGHT INOPERATIVE. R & R MAIN DOOR EMER LIGHT BULB. OPERATIONS CHECKED GOOD IAW AMM 33-50-10.

Part: SENSOR — LOOSE (LANDING GEAR) · airframe 23,141 hrs · 18,795 cycles

AFTER TAKEOFF, GEAR HANDLE MOVED UP BUT LG DID NOT RETRACT, DOWN & LOCKED. FOUND WOW A 0062 NR 1 & A0218 NR 2, LOOSE & FUSION TAPE DETERIORATED. CLEANED & SECURED WOW NR 1 & 2 IAW AMM 20-50-00. PERFORMED LANDING GEAR EXTENSION & RETRACTION, SYS WORKING PROPERLY IAW AMM 32-30-00.

Part: CRADLE — BROKEN (FLASHLIGHT) · airframe 23,067 hrs · 18,730 cycles

AFT CABIN WALL MOUNTED EMERGENCY FLASH LIGHT CRADLE BROKEN. R & R AFT CABIN WALL MOUNTED EMERGENCY FLASH LIGHT IAW AMM 33-50-16.

Part: CRADLE — BROKEN (FLASHLIGHT) · airframe 22,430 hrs · 18,241 cycles

F/A FLASHLIGHT MOUNT BROKEN, FORWARD POSITION. REPLACED FWD F/A FLASHLIGHT HOLDER/CHARGER IAW 33-50-16.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,872 hrs · 17,768 cycles

MAIN DOOR EMERGENCY LIGHT INOPERATIVE. R & R MAIN DOOR EMERGENCY LIGHT IAW AMM TASK 33-50-06-000-801-A, 33-50-06-400-801-A.. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 21,834 hrs · 17,732 cycles

RIGHT FWD OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. R & R RT FWD OVERWING LIGHT BULB IAW AMM 33-50-10. OPS CHECKED GOOD.

Part: HYDRAULIC SYSTEM — OVERSERVICED (NR 1 & 2) · airframe 21,730 hrs · 17,640 cycles

CREW RECEIVED A "HYD 1 LOW QTY" BLUE MESSAGE IN FLIGHT. DECLARED AN EMERGENCY AND DIVERTED. ACFT LANDED WITHOUT INCIDENT. ACFT WAS REMOVED FROM SERVICE. FOUND NR 2 HYD SYSTEM OVERSERVICED. BALANCED BOTH NR 1 & 2 IAW ETN EM-29-023. REPLENISHED NR 1 & NR 2 HYD SYSTEMS ABOVE REFILL IAW AMM TASK 12-13-01-600-802-A. NO LEAKAGE. ACFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,097 hrs · 17,109 cycles

DURING B INSPECTION FOUND THE CABIN AISLE CEILING EMERGENCY LIGHT 2ND FROM FORWARD INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CABIN AISLE CEILING EMERGENCY LIGHT BULB IAW EMB AMM 33-50-08-000-801-A AND 33-50-08-400-801-A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,097 hrs · 17,109 cycles

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

Part: FLASHLIGHT — UNSECURE (COCKPIT) · airframe 20,878 hrs · 16,919 cycles

DURING MAINTENANCE INSPECTION FOUND CAPTAIN'S FLASHLIGHT HOLDER REAR UPPER CLIP MISSING AND FLASHLIGHT IS NOT SECURE. REMOVED AND REPLACED CAPT'S FLASHLIGHT ASSY AS PER EMB-145 AMM 33-50-16. OPS CHECK GOOD. THE AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,586 hrs · 16,714 cycles

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

Part: GUSSET — CORRODED (FUSELAGE) · airframe 19,898 hrs · 16,165 cycles

DURING B INSPECTION FOUND THE LAV CENTER FLOORBEAM GUSSET CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CORRODED LAV CENTER FLOORBEAM GUSSET IAW EMB SRM 51-40-02. THE AIRCRAFT WAS RETUNRED TO SERVICE.

Part: WIRE — DAMAGED (CABIN) · airframe 19,898 hrs · 16,165 cycles

DURING MAINTENANCE INSPECTION FOUND THE EMERGENCY LIGHT STRIP WIRE BELOW FLOOR AT SEAT 9A/10A DAMAGED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED EMERGENCY LIGHT STRIP WIRE BELOW FLOOR AT SEAT 9A/10A IAW EMB145 AWM 20-21-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETUNRED TO SERVICE.

Part: WIRE — BROKEN (CABIN) · airframe 19,898 hrs · 16,165 cycles

DURING MAINTENANCE INSPECTION FOUND THE FLOOR PROXIMITY LIGHT STRIP AT EMERGENCY EXIT WINDOW HAS BROKEN WIRES. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FLOOR PROXIMITY LIGHT STRIP AT EMERGENCY EXIT WINDOW IAW EMB 145 AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETUNRED TO SERVICE.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 2,729 hrs · 16,165 cycles

DURING B INSPECTION FOUND THE LAV LEFT FLOORBEAM GUSSET CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CORRODED LAV LEFT FLOORBEAM GUSSET IAW EMB SRM 51-40-02. THE AIRCRAFT WAS RETUNRED TO SERVICE.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 19,898 hrs · 16,165 cycles

DURING B INSPECTION FOUND THE LAV RIGHT FLOORBEAM GUSSET CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CORRODED LAV RIGHT FLOORBEAM GUSSET IAW EMB SRM 51-40-02. THE AIRCRAFT WAS RETUNRED TO SERVICE.

Part: SCREW — BROKEN (LIGHT STRIP) · airframe 19,898 hrs · 16,165 cycles

DURING MAINTENANCE INSPECTION FOUND THE FLOOR PROXIMITY LIGHT STRIP NR 1 HAS A BROKEN SCREW IN THE NUT PLATE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 1 FLOOR PROXIMITY LIGHT STRIP INSERT IAW EMB 145 AMMM 25-00-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETUNRED TO SERVICE.

Part: BATTERY PACK — INOPERATIVE (FLASHLIGHT) · airframe 19,392 hrs · 15,781 cycles

DURING MAINTENANCE INSPECTION, FOUND CAPTAIN`S FLASHLIGHT INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED CAPTAINS FLASHLIGHT BATTERY IAW AMM TASK 33-50-16-000-801-A AND 33-50-16-400-801-A. OPS CHECKED GOOD. AIRCRAFT RETURN TO SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 19,392 hrs · 15,781 cycles

DURING MAINTENANCE INSPECTION, FOUND MAIN DOOR EMERGENCY LIGHT INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED MAIN DOOR EMERGENCY LIGHT IAW AMM 33-50-10-000-801-A AND 33-50-10-400-801-A. OPS CHECKED GOOD. AIRCRAFT RETURN TO SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 19,327 hrs · 15,734 cycles

DURING PS-2 CHECK, FOUND THE RIGHT WING OVERWING EMERGENCY LIGHT INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT WING OVERWING EMERGENCY LIGHT BULB IAW AMM 33-50-10. OPS CHECKED GOOD. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (LT OVERWING) · airframe 19,162 hrs · 15,598 cycles

DURING MAINTENANCE INSPECTION, FOUND THE LEFT OVERWING EMERGENCY LIGHT INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE AFT LEFT OVERWING EMERGENCY LIGHT ASSEMBLY REF AMM TASK 33-50-07. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 18,802 hrs · 15,301 cycles

DURING B INSPECTION, FOUND EMERGENCY LIGHT ON MAIN PASSENGER DOOR INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY LIGHT ON MAIN PASSENGER DOOR IAW AMM 33-50-10. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,702 hrs · 15,215 cycles

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

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 3,348 hrs · 15,182 cycles

DURING B INSPECTION FOUND THE FORWARD CABIN RECHARGEABLE FLASHLIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FORWARD CABIN FLASHLIGHT ASSEMBLY IAW AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,213 hrs · 14,807 cycles

DURING B-INSPECTION FOUND THE LEFT OVERWING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT OVERWING EMERGENCY 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: LIGHT — INOPERATIVE (CABIN) · airframe 17,989 hrs · 14,645 cycles

DURING B-INSPECTION FOUND THE LEFT OVERWING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT OVERWING EMERGECNY LIGHT IAW EMB 145 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: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 17,542 hrs · 14,322 cycles

DURING MAINTENANCE INSPECTION FOUND THE LEFT AND RIGHT OVERWING EMERGENCY LIGHTS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 4 BATTERY HOLDER AND POWER SUPPLY. THE OPERATIONAL CHECK WAS GOOD IAW AMM 33-50-04. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 6,193 hrs · 13,245 cycles

FOR FLIGHT 2712 DURING THE PREFLIGHT INSPECTION FOUND THE LEFT AFT OVERWING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT AFT OVERWING EMERGENCY EXIT LIGHT IAW EMB 145 AMM 33-50-10. THE SYSTEM OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,193 hrs · 13,245 cycles

FOR FLIGHT 2712 DURING THE PREFLIGHT INSPECTION FOUND THE LAST OVERHEAD EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LAST OVERHEAD EMERGENCY LIGHT LAMP IAW EMB 145 AMM 30-50-08. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 14,942 hrs · 12,322 cycles

DURING MAINTENANCE BASE VISIT FOUND SHEAR CLIP AT FRAME 65 CORRODED AT CARGO DOOR OPENING LOWER CORNER. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED SHEAR CLIP AT FRAME 65 AT CARGO DOOR OPENING IAW EO EM-53MR-1129 PART A. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,569 hrs · 12,026 cycles

DURING MAINTENANCE BASE VISIT FOUND THE RIGHT AND OVER WING EMERGENCY LIGHT TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED BULB IAW EMBRAER AMM 33-50-07. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,258 hrs · 11,757 cycles

FOR FLIGHT 4224 DURING INSPECTION FOUND THE LEFT OVERWING EMERGENCY LIGHT TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY LIGHT BULB. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 13,693 hrs · 11,299 cycles

ON MAINTENANCE INSPECTION FOR FLIGHT 3301 FOUND THE AFT NR 4 FLASHLIGHT BATTERY TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FLASHLIGHT BATTERY. THE OPERATIONAL CHECK WAS GOOD IAW EMB AMM 33-51-01. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FAN — MALFUNCTIONED (NR 1) · airframe 13,588 hrs · 11,228 cycles

ON FLIGHT 3314 DURING THE ON DESCENT INTO DFW OUT OF FLIGHT LEVEL 360 THE CREW NOTICED A FAINT ODOR OF BURNING /SMOLDERING RUBBER /PLASTIC IN THE COCKPIT. THE FLIGHT ATTENDANT NOTICED THE ODOR IN THE FRONT OF THE CABIN BUT NOT IN THE REAR OF CABIN. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 1 RECIRCULATION FAN. THE OPERATIONAL CHECK WAS GOOD IAW AMM 21-24-01. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,911 hrs · 8,260 cycles

DURING IMBV INSPECTION FOUND LEFT OMEGA BEAM CORRODED AT FRAME 20 CROSSMEMBER. REPAIRED OMEGA BEAM IAW SRM 53-00-10. AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 9,843 hrs · 8,191 cycles

MAINTENANCE FOUND EMERGENCY LIGHT INOPERATIVE AT GATE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED SERVICEABLE EMERGENCY LIGHT BATTERIES IAW EMB 33-50-04. OPERATION CHECK GOOD. AIRCRAFT RETURN TO SERVICE.

Part: ATTACH FITTING — DRILLED (CARGO AREA) · airframe 4,931 hrs · 4,249 cycles

MISDRILLED FASTENERS ON FORWARD CARGO NET FITTING BETWEEN FRAME 63, FRAME 64, STRINGER 11L AND STRINGER 12L. REAMED HOLES AND INSTALLED OVERSIZE FASTENERS IAW EMB, RETURNED AIRCRAFT TO SERVICE.

Part: FRAME — DAMAGED (ZONE 100) · airframe 4,931 hrs · 4,249 cycles

THREE FASTENER HOLES MISDRILLED ON FRAME 64AT STRINGER 11R. REAMED HOLES AND INSTALLED OVERSIZE FASTENERS IAW EMB. RETURNED AIRCRAFT TO SERVICE.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 4,931 hrs · 4,249 cycles

LEFT OMEGA BEAM CORRODED AT FRAME 20. CUTOUT CORROSION, FABRICATED AND INSTALLED REPAIR PARTS IAW EMB SRM 53-00-10, FIGURE 201, SHEET 1. AIRCRAFT RETURNED TO SERVICE.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 4,931 hrs · 4,249 cycles

FOUND CORROSION AROUND A NUT PLATE ON THE RIGHT OMEGA BEAM. REMOVED CORROSION, PERFORMED NDT WITH NO REJECTABLE INDICATIONS. FABRICATED AND INSTALLED A DOUBLER IAW EMB SRM 53-21-10 AND 53-40-02. AIRCARFT RETURNED TO SERVICE.

Part: FRAME — DAMAGED (ZONE 100) · airframe 4,931 hrs · 4,249 cycles

MISDRILLED RIVET HOLE AT FRAME 52 AND STRINGER LH10. INSTALLED OVERSIZE FASTENERS IAW EMB IC2007-145/03228, PARAGRAPH 3.

Part: SILL — CORRODED (ZONE 100) · corrosion level 2 · airframe 4,391 hrs · 4,249 cycles

SERVICE DOOR CENTER SILL CORRODED. REMOVED CORROSION, PERFORMED NDT WITH NO REJECTABLE DEFECTS NOTED. FABRICATED AND INSTALLED DOUBLER IAW EMB SRM 53-21-02.

Part: COMPARATOR — MALFUNCTIONED

BOTH TRANSPONDERS INOPERATIVE. RETURN TO FIELD A/C LANDED WITHOUT INCIDENT. REPLACED ICU600, OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: DOOR — LIGHTNING STRIKE (FUSELAGE)

DEFERRED MAINTENANCE ITEM. LIGHTNING STRIKE DAMAGE ON PASSENGER DOOR. INSTALLATION OF DOUBLER IAW SRM 52-10-01. AIRCRAFT RETURNED TO SERVICE. (M)