N659AE

Part: SIGN — INOPERATIVE (ZONE 200) · airframe 47,352 hrs · 44,675 cycles

COCKPIT STEP EMERGENCY LIGHT INOPERATIVE. R & R STEP EXIT IDENTIFIER SIGN IAW AMM 33-50-13.

Part: CONTROLLER — OUT OF ADJUST (ZONE 200) · airframe 45,872 hrs · 43,006 cycles

ON CLIMB AT APROX 8000 FT CABIN ALT FLAGGED RED AND AURAL WARNING CABIN ANNUNCIATED. CREW FOUND MANUAL PRESSURE CONTROLLER KNOB IN FULL DUMP POSITION FACT 10MAR25 11:37 RIC PERFORMED OPS CHECK IN NORMAL MODE AMM 21-31-00-700-801-A PERFORMED CHECK IN AUTO MODE AMM 21-31-00-700-802-A BOTH CHECKS GOOD OK FOR SERVICE

Part: UNKNOWN — ODOR (CABIN) · airframe 45,833 hrs · 42,964 cycles

INTERMITTENT BURNING ELECTRICAL SMELL ON TAXI IN FLIGHT DECK AND CABIN WITH PACKS SELECTED ON. FACT 04MAR25 19:13 CLT OPERATED PACKS IAW 21-00-00-860-801-A FOR APPROX 20 MINUTES NO SMELL DETECTED. A/C OK FOR SERVICE.

Part: CHARGER — INOPERATIVE (ZONE 200) · airframe 45,770 hrs · 42,892 cycles

LH AND RH EXTERNAL OVERWING EMERGENCY LIGHTS INOP. FOUND BONDING WIRE CAUSING SHORT CIRCUIT. REROUTED BONDING WIRE AND RAR #400 EMERGENCY CHRGER ASSY

Part: DISTRIBUTION VLV — FAULTED (ZONE 100) · airframe 45,491 hrs · 42,581 cycles

AIR PRESSURE IN FLIGHT DECK SURGES ON PACK 1 WITH APU BLEED AIR SELECTED. ALSO A OIL BURNING SMELL IS NOTED WITH PACK OPERATION. FACT 31DEC24 01:48 CLT REMOVED AND REPLACED AIR DISTRIBUTION VALVE IAW EMB 145 AMM21-22-01. OPS CHECK AND LEAK CHECK GOOD. ACFT OK FOR SERVICE

Part: UNKNOWN — FAULTED · airframe 45,411 hrs · 42,496 cycles

DUAL RED X'S DISPLAYED ON LOC DURING APPROACH TO CLT 36R WITH-IN 15 MILES. DIVERTED TO CAE AND C/W R-NAV APPROACH. FACT 16DEC24 11:34 CAE PERFORMED VOR/ILS/GS/MB ADJUSTEMENT TEST IAW AMM 34-32-00 OPS CHECK GOOD AC OK FOR SERVICE

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 45,400 hrs · 42,485 cycles

53-2433 LH OMEGA BEAM SUPPORT ASSY CRACKED AT FR55. RAR SUPPORT ASSY IAW SRM 51-40-02

Part: SKIN — CRACKED (ZONE 300) · airframe 45,400 hrs · 42,485 cycles

55-2383 VERTICAL STAB, AFT OF SPAR 3, LWR LH SKIN PROFILE CRACKED. RAR PROFILE IAW SRM 51-40-02

Part: BRACKET — CRACKED (ZONE 100) · airframe 45,400 hrs · 42,485 cycles

53-2201 AT CARGO ENTRY, LWR POST BRACKET CRACKED AT FR66. RAR BRACKET IAW SRM 51-40-02

Part: DOUBLER — CORRODED (ZONE 100) · corrosion level 2 · airframe 45,400 hrs · 42,485 cycles

53-2204 WASTE WATER RH SIDE DOUBLER IS CORRODED. REPAIRED IAW ETD2024-145-030691 AND EO1-53-24-0703

Part: SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,400 hrs · 42,485 cycles

53-2081 RH SILL CORRODED BTW FR60-65. RAR SILL IAW SRM 51-40-02

Part: DOOR — CRACKED (THRUST REVERSER) · airframe 45,400 hrs · 42,485 cycles

54-2089 LH TR LWR DOOR, OB LWR LIP CRACKED AT MID SECTION. REPAIED IAW ESR 1-78-24-001A

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 45,400 hrs · 42,485 cycles

53-2122 SHEAR CLIP CRACKED AT FR60 BTW STR15-16L. RAR SHEAR CLIP IAW SRM 51-40-02

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 45,400 hrs · 42,485 cycles

53-2078 SHEAR CLIP CRACKED AT FR15 BTW STR15-16R. RAR SHEAR CLIP IAW SRM 51-40-02

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 45,400 hrs · 42,485 cycles

53-2077 LH OMEGA BEAM CRACKED AT FR21, FR22 AND FR23. REPAIRED IAW ETD2024-145-030109 REV A AND EO1-53-24-0684

Part: STRUCTURE — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,400 hrs · 42,485 cycles

53-2082 PAX ENTRY, LWR AFT U-SHAPE CORRODED. RAR U-SHAPE IAW SRM 51-40-02

Part: FRAME — CRACKED (THRUST REVERSER) · airframe 45,400 hrs · 42,485 cycles

54-2088 LH TR IN ACCESS PANEL 416QL, FRAME CRACKED AT NUPLATE LOCATION. REPAIRED IAW ESR 1-78-23-0036 AND SRM 54-30-04

Part: REHEATER — CORRODED (ZONE 800) · corrosion level 2 · airframe 45,400 hrs · 42,485 cycles

53-2070 LH SIDE, ON ESCAPE HATCH REINFORCEMENT FWD AND AFT CENTERING HOLE IS CORRODED. REPAIRED IAW ETD2024-145-031088 AND RECORDED ON EO1-05-24-0709

Part: ANGLE — CRACKED (ZONE 200) · airframe 45,400 hrs · 42,485 cycles

53-2108 ANGLE CRACKED AT FR10 STR9R. RAR ANGLE IAW SRM 51-40-02

Part: REHEATER — CORRODED (ZONE 800) · corrosion level 2 · airframe 45,400 hrs · 42,485 cycles

53-2071 LH SIDE ON ESCAPE HATCH REINFORCEMENT HAS CORROSION AROUND DOOR STOP. REPAIRED IAW ETD2024-145-031088 AND RECORDED ON EO1-05-24-0709

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 45,400 hrs · 42,485 cycles

53-2073 SHEAR CLIP CRACKED AT FR67 BTW STR6-7R. RAR SHEAR CLIP IAW SRM 51-40-02

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 45,400 hrs · 42,485 cycles

53-2074 SHEAR CLIP CRACKED AT FR73 BTW STR8-10L. RAR SHEAR CLIP IAW SRM 51-40-02

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 45,400 hrs · 42,485 cycles

53-2051 SHEAR CLIP CRACKED AT FR24 BTW STR16-17R. RAR SHEAR CLIP IAW SRM 51-40-02

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 45,400 hrs · 42,485 cycles

53-2048 SHEAR CLIP CRACKED AT FR26 BTW STR15-16R. RAR SHEAR CLIP IAW SRM 51-40-02

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,400 hrs · 42,485 cycles

53-2047 CTR GUSSET CORRODED BTW FR29-36. RAR GUSSET IAW SRM 51-40-02

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 45,400 hrs · 42,485 cycles

53-2050 SHEAR CLIP CRACKED AT FR24 BTW STR15-16R. RAR SHEAR CLIP IAW SRM 51-40-02

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 45,400 hrs · 42,485 cycles

53-2057 SHEAR CLIP CRACKED AT FR25 BTW STR 16-17R. RAR SHEAR CLIP IAW SRM 51-40-02

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 45,400 hrs · 42,485 cycles

53-2068 SHEAR CLIP CRACKED AT FR58 BTW STR15-16R. RAR SHEAR CLIP IAW SRM 51-40-02

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 45,400 hrs · 42,485 cycles

53-2049 SHEAR CLIP CRACKED AT FR25 BTW STR15-16R. RAR SHEAR CLIP IAW SRM 51-40-02

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 45,400 hrs · 42,485 cycles

53-2058 LH OMEGA BEAM IB ANGLE CRACKED BTW FR46-50. REPAIRED ANGLE IAW SRM 53-23-02

Part: SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,400 hrs · 42,485 cycles

53-2046 RH SILL CORRODED AT FR29-36. RAR SILL IAW SRM 51-40-02

Part: BEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 45,400 hrs · 42,485 cycles

53-2066 BAG DOOR LWR BEAM CORRODED. RAR BEAM IAW SRM 51-40-02

Part: ANGLE — CRACKED (ZONE 100) · airframe 45,400 hrs · 42,485 cycles

53-2033 LH WING TO BODY FAIRING, LWR ANGLES #2 AND #3 CRACKED. RAR ANGLES IAW SRM 51-40-02

Part: ANGLE — CRACKED (WNG-BDY FAIRING) · airframe 45,400 hrs · 42,485 cycles

53-2032 LH WING TO BODY FAIRING, UPPER ANGLE #2 CRACKED. REPAIRED IAW SRM 53-23-12

Part: ANGLE — CRACKED (ZONE 100) · airframe 45,400 hrs · 42,485 cycles

53-2030 RH WING TO BODY FAIRING, LWR ANGLE#2 CRACKED. RAR ANGLE IAW SRM 51-40-02

Part: GUSSET — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,400 hrs · 42,485 cycles

53-2126 LH GUSSET CORRODED BTW FR59-61. RAR GUSSET IAW SRM 51-40-02

Part: DOOR — CRACKED (THRUST REVERSER) · airframe 44,595 hrs · 41,546 cycles

HA #7: #1 TR CRACKED AT LOWER DOOR PIVOT POINT. RAR IAW AMM 78-31-01

Part: RELAY — FAULTED (ANTI-ICE) · airframe 44,298 hrs · 41,185 cycles

ICE COND AND A/ICE INOP EICAS MESSAGES DISPLAYED ON T/O ROLL. REMOVED AN REPLACED RELAYS K0532 AND K0531 IAW AMM 20-13-02, PERFORMED OPS CEHCK IAW AMM 30-00-00 NO DEFECTS NOTED AT THIS TIME. OKAY FOR SERVICE

Part: UNKNOWN — FAULTED (CABIN PRESSURE) · airframe 44,146 hrs · 41,006 cycles

ON CLIMB OUT AT 10000 FEET AUTO PRESSURIZATION FAIL ALL INDICATIONS DASHED OUT. C/W FLT CREW PROCEDURES. PRESS CONTROL AUTO AND MANUAL DFRL 01MAR24 06:46 BGR CREW RTF DUE TO UNABLE TO CONTROL PRESSURIZATION DUE TO INDICATIONS DASHED. FACT 01MAR24 10:49 PHL PERFORMED OPS CHECK IN AUTO/MAN MODE IAW AMM 21-31-00 OPS CHECK GOOD AIRCRAFT OK FOR SERVICE AT THIS TIME. CLEAR MEL 21-12-03

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 43,360 hrs · 40,110 cycles

BURNING SMELL COMING FROM PACK 2 STARTED 13,000 FT FOLLOW BY PACK 2 TURNING OFF AND BLEED 2 TURNING OFF.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 42,568 hrs · 39,198 cycles

BAG BAY FIRE INDICATION LIGHT ILLUMINATED HISTORY: NONE FACT DISCONNECTED AND RECONNECTED CANNON PLUGS ON BOTH BAG BAY SMOKE DECTECTORS. OPS CHECK GOOD AT THIS TIME. OK FOR SERVICE.

Part: CONTROL UNIT — FAULTED (PITCH TRIM) · airframe 41,509 hrs · 37,984 cycles

MAIN PITCH TRIM INOP WARNING WHILE USING CA YOKE TRIM. R/R HSCU IAW EMB 145 AMM 27-40-01 OPS CHECK GOOD

Part: NONE — NONE · corrosion level 2 · airframe 41,060 hrs · 37,485 cycles

E914513 - SERVICE DOOR CUTOUT FWD LOWER CORNER SEAL FLANGE FITTING IS CORRODED .... REMOVED AND REPLACED SERVICE DOOR CUTOUT FWD LOWER CORNER SEAL FLANGE FITTING IAW EMB145 SRM 51-40-02

Part: NONE — NONE · corrosion level 2 · airframe 41,060 hrs · 37,485 cycles

E914506 - RH OMEGA BEAM HAS A CORRODED NUTPLATE HOLE BETWEEN FR 23-24 .... REPAIRED RH OMEGA BEAM CORROSION AT NUTPLATE HOLE BETWEEN FR 23-24 IAW PIEDMONT EO1-53-22-0113.

Part: NONE — NONE · airframe 41,060 hrs · 37,485 cycles

SUPPLEMENTAL INFORMATION - CORRECT REGISTRATION # TO 659AE AS WELL AS AIRCRAFT INFO IN 3.(A) ABOVE

Part: CONTAINER — CORRODED (LAVATORY) · airframe 48,865 hrs · 46,304 cycles

E913322 - LAV WASTE BUCKET SHOWS SIGNS OF CORROSION ON EXTERIOR SIDE .... ACCOMPLISHED REPAIR ON LAV WASTE BUCKET EXTERNAL SIDE IAW EMB145 SRM 53-31-02RE, FIG 201 AND EO1-53-22-0100.

Part: NONE — NONE · corrosion level 2 · airframe 41,060 hrs · 37,485 cycles

E914514 - SERVICE DOOR CUTOUT AFT LOWER CORNER SEAL FLANGE FITTING IS CORRODED .... RAR SERVICE DOOR CUTOUT AFT LOWER CORNER SEAL FLANGE FITTING IAW EMB145 SRM 51-40-02

Part: NONE — NONE · corrosion level 2 · airframe 41,060 hrs · 37,485 cycles

E914519 - RH OMEGA BEAM HAS A CORRODED NUTPLATE HOLE AT FR 18 ... ACCOMPLISHED PERMANENT REPAIR TO RH OMEGA BEAM HAS NUTPLATE HOLE AT FR 18 IAW EO1-53-22-0101

Part: FLOOR SUPPORT — CORRODED · corrosion level 2 · airframe 41,060 hrs · 37,485 cycles

E914349 - LH #6 OTBD FLOOR SILL HAS PITTING .... REMOVED AND REPLACED LH #6 OTBD FLOOR SILL IAW EMB145 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED · corrosion level 2 · airframe 41,060 hrs · 37,485 cycles

E914351 - RH #6 OTBD FLOOR SILL HAS PITTING .... REMOVED AND REPLACED RH #6 MOTBD FLOOR SILL IAW EMB145 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED · airframe 41,060 hrs · 37,485 cycles

E914332 - RH #3 OTBD FLOOR SILL HAS PITTING. R & R RH #3 OTBD FLOOR SILL IAW EMB145 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED · corrosion level 2 · airframe 41,060 hrs · 37,485 cycles

E914350 - LH #7 OTBD FLOOR SILL HAS PITTING .... REMOVED AND REPLACED LH #7 OTBD FLOOR SILL IAW EMB145 SRM 51-40-02.

Part: NONE — NONE · airframe 41,060 hrs · 37,485 cycles

E913854 - FR 72 IS CRACKED BTW STR 17L-16L ....REPAIRED FR 72 CRACK BETWEEN STR 17L-16L IAW PIEDMONT EO1-53-22-0093.

Part: FLOOR SUPPORT — CORRODED · corrosion level 2 · airframe 41,060 hrs · 37,485 cycles

E914503 - GALLEY LH INBD SEAT TRACK #1 IS CORRODED .... RAR GALLEY LH INBD SEAT TRACK #1 IAW EMB 145 AMM 53-01-06

Part: NONE — NONE · airframe 40,914 hrs · 37,329 cycles

PDIS 659 29-13 2671141 13MAR22 DAY CLOSE HYD 2 LO QTY MSG ON EICAS IN FLIGHT, CREW FOUND SOME POSSIBLE HYD LEAK UNDER #2 ENGINE LOWER COWLING. FACT 14MAR22 12:54 DAY LEAK UNDER NO2 ENG IS ANTI ICE FLUID. DISCOVERED BOTH RUDDER BLEED VALVES ON TOP ACTUATOR LOOSE AND LEAKING TIGHENED VALVES AS REQUIRED PERFORMED RUDDER ACTIVATION AND T/R DEPLOYMENT WHILE RUNNING HYD PUMPS FOR OVER HALF HOUR ALL OPERATIONS OF SYS PERFORMED AS REQUIRED NO LEAKS NOTED 1 AND 2 AT FULL LEVEL AC IS OK FOR SVC AT THIS TIME.

Part: NONE — NONE · airframe 40,315 hrs · 36,661 cycles

PDIS 659 30-10 2572471 18NOV21 ALB CLOSE WING A/I FAIL ON EICAS WHEN ENTERING ICING CONDITIONS. FOLLOWED QRH (TURN OFF WG A/I) WITH WING 1&2 A/I VLV FAIL AND WING 2 A/I LEAK FACT 18NOV21 18:32 ALB FOUND SPLICE AT #2 WING THERMOSTAT INCORRECTLY INSTALLED. R&R'D SPLICE IAW SWPM 20-21-00. OPS CHECK GOOD

Part: NONE — NONE · airframe 40,315 hrs · 36,661 cycles

PDIS 659 30-10 2572473 18NOV21 PHL CLOSE WING A/I FAIL DISPLAYED IN AND OUT OF ICING CONDITIONS. FACT 19NOV21 16:10 PHL R/R CLAMPS OPS/LEAK CHECK FAIL.STILL LEAKING. FOUND ANOTHER COUPLING LEAKING SAME AREA. TRANSCRIBED TO HA-300 DATED 11/18/21 SEQ 6 REFERENCE HA-300 FOR WORK COMPLETED.

Part: NONE — NONE · airframe 40,315 hrs · 36,661 cycles

PDIS 659 36-11 2572481 18NOV21 PHL CLOSE BLD 2 LOW TEMP DISPLAYED ON DESENT WITH N2 ABOVE 86 PERCENT. FACT 19NOV21 16:03 PHL CMC MESSEGE PRECOOLER 2 TEMP CTL FAIL.R/R FAN AIR CONT THERMOSTAT.REQUIRES OPS CHECK.REF AMM 36-11-06.OPS CHECK IAW AMM 36-00-00-700-803-A. OKAY FOR SERVICE OPS CHECK GOOD.

Part: BULB — SMOKE (GALLEY LIGHT) · airframe 39,964 hrs · 36,252 cycles

DURING TAKEOFF BETWEEN 400-2000FT FUMES SMELL IN COCKPIT AND FWD CABIN. SEE LP 249922-2 AND 249923-1 FOR TROUBLESHOOTING AND ENGINE RUNS. WHILE TROUBLESHOOTING, FOUND GALLEY COURTESY LIGHT BULB TO BE SMOKING WHILE OPERATING. R+R'D LIGHT BULB. NEW BULB OPERATES NORMALLY WITH NO SMOKE OR SMELLS. OK FOR SERVICE

Part: FUSE — OVERHEATED (ELEC DISTRIBUTIO) · airframe 39,958 hrs · 36,246 cycles

ON DESCENT FROM 19K - 10K FT BURNING SMELL IN COCKPIT AND CABIN APPEARED 3 TIMES WITH BOTH BLEEDS AND PACKS RUNNING AND APU OFF. RAN BOTH ENGINE BLEED AND PACKS. NO DEFECTS NOTED. SEE ALSO W/C 36-10-03 FOR OTHER MX DONE. INSPECTED R/H+L/H ELECTRICAL DIST BUS PANELS. FOUND 3 FUSES OVERHEATED ON R/H SIDE. REMOVED AND REPLACED ALL FUSES ON R/H ELECTRICAL DIST BUS PANEL IAW AWM 24-61-50. OPS CHECK GOOD. OK FOR SERVICE.

Part: SLEEVE — FAILED (ANTI-ICE DUCT) · airframe 39,833 hrs · 36,110 cycles

WING AI FAIL MSG DURING AI TEST IN FLT (TWICE) W NO OPEN INSCRIPTION AND NOT IN ICING CONDITIONS. R&R FLEX SLEEVE ON #1 WING A/ICE DUCT IAW AMM 30-11-01. REQUIRES OPERATIONAL CHECK. OPS CHECK ANTI ICE SYSTEM IAW AMM 30-00-00 OPS CHECK GOOD. OK FOR SERVICE.

Part: A/C PACK — ODOR (NR 1) · airframe 39,480 hrs · 35,699 cycles

DURING CRUISE FLT AT 25000FT STRONG BURNING PLASTIC SMELL IN COCKPIT FOLLOWED SHORTLY IN CABIN. FOLLOWED QRH AND SMELL MITIGATED BUT REMAINED UNTIL ON GROUND. NO SMOKE NOTED. INSPECTED PACK SYSTEMS FOR BURNING SMELL. MX FOUND BURNING SMELL IS FROM PACK 1. SEE LP 217821 SEQ 2 FOR DISCREPANCY AND RELIEF

Part: WARNING MESSAGE — FALSE ACTIVATION (NR 1 SPS) · airframe 39,099 hrs · 35,280 cycles

SPS 1 INOP ON TAKEOFF ROLL. CMC MSG OF SPC FAIL. CMC MSG SPC FAIL FOLLOWED FIM 27-36-00-810-807-A BLOCK 1 OPS CHECK AMM 27-36-00-700-801-A SPS OPS CHECK GOOD FOUND TO BE TRANSITORY CONDITION. OK FOR SERVICE.

Part: A/C PACK — OVERHEATED (NR 2) · airframe 38,904 hrs · 35,057 cycles

PACK 2 OVERHEAT WITH STRONG BURNING SMELL WHEN THRUST LEVERS AT HIGH SETTING. C/W FIM TASK 21-51-00-810-804-A BLOCK 2 RESULT IN NO PACK 2 OVERHEAT EICAS MESSAGE. NO RESULT BLOCK II TRANSITORY CONDITION OF AIR CONDITIONING SYSTEM. FOUND WON AND LEAKING SLEEVE AT NR 2 PACK VALVE Y DUCT, REPLACED SLEEVE. SYSTEM OPERATIONS CHECK GOOD, OK FOR SERVICE.

Part: LEVER — BINDING (MLG) · airframe 38,796 hrs · 34,933 cycles

PDIS 659 32-30 2423781 19SEP20 CLT CLOSE IN FLIGHT, LANDING GEAR LEVER WAS JAMMED AND WOULD NOT RAISE FACT 19SEP20 17:03 CLT. R & R RELAY K0024. PERFORMED OPS CHECK OF LANDING GEAR LEVER, IAW AMM 32-32-00-700-802-A. OPS CHECK GOOD. OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 38,284 hrs · 34,359 cycles

LH SIDE OVERWING EMERGENCY LIGHT INOP....FIX: R&RD EMERGENCY LIGHT ON LHS IN REF TO AMM 33-50-10-000/400-801-A. OPS CHECK GOOD.OK FOR SERVICE.

Part: WARNING MESSAGE — FALSE ACTIVATION (BRAKES) · airframe 37,936 hrs · 33,965 cycles

PDIS 659 32-41 2242582 02JAN20 CLT CLOSE MULTIPLE BRAKE DEGRADED MSG DURING TAXI DFRL 04JAN20 00:13 MDT TRANSCRIBED TO HA300 SEQ 5 ON WORK PACKAGE DATED 01/03/2020.///CHECKED WIRES @ P3718 CANNON PLUG PIN 23 TO 24,78 TO 77, & 4 TO 7, AND RELAYS K0479, K0481,& K0480,K0482-NO DEFECTS NOTED BLEED HYDRAULIC SYSTEM IN REFERENCE WITH AMM 32-40-00.REMOVED AND REPLACED OUTBD BRAKES CIRCUIT BREAKER IN REFERENCE WITH AMM 20-13-06.//HOOKED UP FIELD ANAYLIZER,TAXIED AIRCRAFT-NO DEFECTS IN REF TO AMM 32-41-00.NO MESSAGES ON ICAS OR CMC AT THIS TIME

Part: FILTER — DIRTY (FAN VALVE) · airframe 73,813 hrs · 33,809 cycles

REJECTED TAKEOFF DUE TO BLD 2 OVTEMP WARNING. FOLLOWED BY PACK 2 OVERHEAT. MX PERFORMED C/W VISUAL INSPECTION OF PRE COOLER LINE REGION. NO DISCONNECTED OR DAMAGED COMPONENTS. CLEANED FAN VALVE FILTER AND C/W OPS CHECK I/A/W M/M 36-11-03 AND TASK 36-00-00-700-803-A/500. OPS CHECK GOOD.

Part: UNKNOWN — SMOKE (COCKPIT) · airframe 37,678 hrs · 33,665 cycles

PDIS 659 05-50 2243021 10NOV19 CLT CLOSE TOW TEAM REPORTED SMOKE IN COCKPIT DURING TOW. 25722 00 VAG HISTORY: NONE FACT 10NOV19 13:58 CLT OPS CK APU BLEEDS RAN HYD PUMP FOR SEVERAL MINS NO S MOKE NOTED AT THIS TIME OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 37,155 hrs · 33,078 cycles

RH AND LH OVERWING PANEL EMERGENCY LIGHTS DO NOT COME ON....FIX: R&RD LH & RH EXTERNAL EMERGENCY LIGHT ASSY,S AND OPS CHECK GOOD IAW EMB AMM 33-50-10

Part: WEB — DAMAGED (CARGO DOOR) · airframe 37,155 hrs · 33,078 cycles

CARGO DOOR INNER WEBBING IS CORRODED AROUND 6 SCREW HOLES AND NUMEROUS SCREW HOLES HAVE PRIMER DAMAGE. ONE AREA REPAIRED IAW PIEDMONT EO1-52-19-0299 THE OTHER FIVE AREAS WERE FOUND TO BE WITH-IN LIMITS OF EMB145 SRM 52-30-01 TABLE 104.

Part: WEB — DAMAGED (CARGO DOOR) · airframe 37,155 hrs · 33,078 cycles

CARGO DOOR INNER WEBBING IS GOUGED IN 5 AREAS. REPAIRED IAW EO1-52-19-0300 AND 3 AREAS TO BE WITH-IN LIMITS OF SRM 52-30-01 TABLE 104

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 37,049 hrs · 32,966 cycles

THE SERVICE DOOR EMERGENCY EXIT LIGHT IS INOP. INVESTIGATION FOUND WIRE W716-0007-20 BROKEN. REPAIRED WIRE, OPS CHECK GOOD

Part: BLEED VALVE — INOPERATIVE (NR 1 ENGINE) · airframe 36,993 hrs · 32,901 cycles

BLEED 1 VALVE FAIL MESSAGE WITH ASSOCIATED WING AND STAB ANTI-ICE MESSAGE. R & R THE NR 1 ENG BLEED VALVE IAW AMM TASK 36-11-05-000/4-00-801-A, OPS CHECK GOOD, NO BLEED FAIL MESSAGES OR LEAK MESSAGES,OK FOR SERVICE

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 36,823 hrs · 32,725 cycles

PDIS 659 30-10 1922203 03MAY19 GRR CLOSE ON TAKEOFF ROLL MASTER WARNING OF ICE COND ANTI ICE FAIL. CMC MESSAGE OF WG 2 ANTI ICE LEAK. FACT 03MAY19 21:53 GRR C/W FIM TASK 30-11-00-810-807-A FOUND NO DEFECTS, PERFORMED OPS CHECK IAW AMM 30-00-00-05 OPS CHECK GOOD OK FOR SERVICE.

Part: FLASHLIGHT — ODOR (COCKPIT) · airframe 36,188 hrs · 31,993 cycles

PDIS 659 25-60 1868881 28DEC18 PHL CLOSE COCKPIT FLASHLIGHT ASSY HAS A HOT ELECTRICAL SMELL. FACT 28DEC18 08:28 PHL REPLACED FLASHLIGHT ASSY IN COCKPIT. OPS CHECK GOOD. OK FOR SERVICE

Part: BULB — MALFUNCTIONED (EMERGENCY LIGHT) · airframe 36,149 hrs · 31,951 cycles

R/H FWD FUSELAGE EMERGENCY LIGHT DIM. R/R BULB IAW AMM 33-50-10-400-801-A

Part: HYDRAULIC SYSTEM — CONTAMINATED (NR 1 & 2) · airframe 35,386 hrs · 31,036 cycles

BRAKE DEGRADED EICAS CAUTION MESSAGE DISPLAYED WHILE TAXIING. RETURNED TO GATE AND NR 1 HYD FLUID DOWN 25 PERCENT. BLED AIR FROM NR 1 AND NR 2 HYD SYSTEMS IAW AMM 29-10-00-803-A. PRESSURIZED HYD SYSTEM IAW AMM 29-10-00-860-801-A. OPS CHECK GOOD. NO LEAKS NOTED. OK FOR SERVICE AT THIS TIME.

Part: FUSE — BLOWN (EMERGENCY LIGHT) · airframe 35,337 hrs · 30,979 cycles

EMERGENCY LIGHT ON PAX DOOR INOP. REMOVED EMERGENCY BATTERY ASSY AND BOUGHT TO SHOP TO CHECK. FOUND NR 2 LIGHT CIRCUIT INOP. R&R F2 PICO FUSE. RE-INSTALLED BATTERY ASSY WITH RETAINED HARDWARE, PERFORMED SELF TEST ON THE BATTERY ASSY, SELF TEST GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 35,337 hrs · 30,979 cycles

EMERGENCY LIGHT AT LT EMERGENCY DOOR INOP. INSTALLED EMERGENCY BATTERY ASSY 3 AND RE SECURED WITH RETAINED HARDWARE.

Part: WARNING MESSAGE — FALSE ACTIVATION (EMERGENCY LIGHTS) · airframe 34,652 hrs · 30,247 cycles

EMERGENCY LIGHTS NOT ARMED CAUTION MESSAGE, DISPLAYED RANDOMLY 4 - 5 TIMES ON EICAS, SWITCH WAS VERIFIED TO BE IN THE ARMED POSITION. OPS CHECKED THE EMERGENCY LIGHTING SYSTEM, FOUND GOOD AT THIS TIME IAW 33-50-00. NO ERRONEOUS MESSAGES NOTED. OK FOR SERVICE.

Part: UNKNOWN — MULTIPLE FAIL · airframe 34,652 hrs · 30,247 cycles

AT APPROXIMATELY 500 FT, THE AUTOPILOT WAS SELECTED ON, ONLY YAW DAMPER ENGAGED, LANDING GEAR AIR GROUND FAIL MESSAGE DISPLAYED ON EICAS. APPROXIMATELY 20 SECONDS LATER, NR 1 & 2 ENGINE REVERSERS DISAGREE MESSAGE DISPLAYED ON EICAS. OPS CHECK OF THE AIR - GROUND WOW SYSTEM GOOD AT THIS TIME IAW 32-60-00. FUNCTIONAL CHECK OF THE PROXIMITY SWITCHES USING BREAKOUT BOX GOOD IAW 32-63-05. NO ERRONEOUS MESSAGES NOTED. OPS CHECKED OF THE THRUST REVERSERS WAS GOOD IAW 78-31-01. NO ERRONEOUS MESSAGES NOTED. OK FOR SERVICE.

Part: FUSE — FAILED (NR 1 HYD SYSTEM) · airframe 34,512 hrs · 30,093 cycles

HYDRAULIC SYSTEM 1 FAIL EICAS MESSAGE. HYD PRESSURE ZERO PSI WITH ELECTRIC PUMP IN AUTO OR ON POSITION. R & R NR 1 HYDRAULIC FUSE F0155 IAW SB 145-29-007. OPS CHECKED OK.

Part: DOOR — UNSECURE (CARGO BAY) · airframe 34,275 hrs · 29,852 cycles

CARGO DOOR OPEN INDICATION CAME ON AT FL 300, FELT DECOMPRESSION IN CABIN. CREW VERIFIED DECOMPRESSION ON EICAS. PERFORMED A CARGO DOOR ACTUATING AND LOCKING MECHANISM OPS CHECK IAW AMM 52-31-00-700-801-A.

Part: WARNING MESSAGE — FALSE ACTIVATION (CARGO DOOR) · airframe 33,748 hrs · 29,327 cycles

CARGO DOOR OPEN EICAS MESSAGE AND INDICATION ON MFD. MAINTENANCE PERFORMED AMM 52-76-01-000-801-A, DUE TO NUISANCE MESSAGE. COMPLIED WITH FLIGHT CREW PROCEDURES.

Part: ELEC CONNECTOR — DIRTY (BRAKES) · airframe 33,432 hrs · 28,980 cycles

BRAKES DEGRADE EICAS MESSAGE DISPLAYED WHEN BRAKES WERE APPLIED. CLEANED THE ELECTORICAL CONNECTORS AT BCU, OPS CHECKED IAW AMM32-41-00. OPS CHECKED GOOD, OK FOR SERVICE.

Part: FADEC — FAILED (NR 1) · airframe 33,189 hrs · 28,738 cycles

NR 1 ENGINE HAS NO FADEC INDICATION, CYCLED THE CIRCUIT BREAKER, NO FIX. R & R THE NR 1 FADEC IAW MM 73-25-10. GROUND RAN ENGINES IAW MM 72-00-00. OPS CHECKED GOOD. OK FOR SERVICE.

Part: CUP — CORRODED (FRAME 60) · airframe 32,973 hrs · 28,497 cycles

DURING INSPECTION, QA FOUND THE TOILET WASTE DRAIN VALVE CUP CORRODED. AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE TOILET WASTE DRAIN VALVE CUP IAW SRM 51-40-02, 51-20-01, 51-40-06, AND 51-20-03.

Part: BEAM — CORRODED (FUSELAGE) · airframe 32,973 hrs · 28,497 cycles

DURING MBV INSPECTION, QA FOUND CORROSION AT THE FWD NUT PLATE HOLE OF THE LAV RT HAT BEAM. AIRCRAFT WAS REMOVED FROM SERVICE FOR MBV INSPECTION AND WILL BE RETURNED TO SERVICE AFTER MBV INSPECTION. REMOVED DAMAGE AND INSTALLED DOUBLER TO RT HAT BEAM AT FWD NUT PLATE HOLE IAW SRM 53-24-10 REREPAIR 3. AIRCRAFT WILL BE RETURNED TO SERVICE AFTER MBV INSPECTION.

Part: BEAM — CRACKED (FUSELAGE) · airframe 32,973 hrs · 28,497 cycles

DURING MBV INSPECTION, QA FOUND A CRACK AT AFT NUT PLATE HOLE ON LAV RT HAT BEAM. AIRCRAFT WAS REMOVED FROM SERVICE FOR MBV INSPECTION AND WILL BE RETURNED TO SERVICE AFTER MBV INSPECTION. REMOVED DAMAGE AND INSTALLED DOUBLER TO RT HAT BEAM AT AFT NUT PLATE HOLE IAW SRM 53-24-10 REREPAIR 3. AIRCRAFT WILL BE RETURNED TO SERVICE AFTER MBV INSPECTION.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 32,973 hrs · 28,497 cycles

DURING MBV INSPECTION, QA FOUND CORROSION ON FR 22 AROUND LOWER NUT PLATE HOLE. AIRCRAFT WAS REMOVED FROM SERVICE FOR MBV INSPECTION AND WILL BE RETURNED TO SERVICE AFTER MBV INSPECTION. REPAIRED FR 22 CORROSION AROUND LOWER NUT PLATE HOLE IAW SRM 53-00-04 RE STEP 16. AIRCRAFT WILL BE RETURNED TO SERVICE AFTER MBV INSPECTION.

Part: YOKE — CRACKED (LT PYLON) · airframe 32,973 hrs · 28,497 cycles

DURING MBV INSPECTION, QA FOUND LT PYLON LOWER FORWARD ENGINE MOUNT SUPPORT YOKE CRACKED. AIRCRAFT WAS REMOVED FROM SERVICE FOR MBV INSPECTION AND WILL BE RETURNED TO SERVICE AFTER MBV INSPECTION. REMOVED AND REPLACED LT PYLON LOWER FORWARD ENGINE MOUNT SUPPORT YOKE IAW EO EM-54MR-386. AIRCRAFT WILL BE RETURNED TO SERVICE AFTER MBV INSPECTION.

Part: YOKE — CRACKED (RT ENGINE) · airframe 32,973 hrs · 28,497 cycles

DURING MBV INSPECTION, QC FOUND RT ENGINE FWD LOWER YOKE FITTING CRACKED. AIRCRAFT WAS REMOVED FROM SERVICE FOR MBV INSPECTION AND WILL BE RETURNED TO SERVICE AFTER INSPECTION. REMOVED AND REPLACED RT ENGINE FWD LOWER YOKE FITTING IAW EO-EM-54MR-386. AIRCRAFT WILL BE RETURNED TO SERVICE AFTER MBV INSPECTION.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 32,797 hrs · 28,340 cycles

EXTERNAL EMERGENCY LIGHT ON THE RT LOWER FAIRING BURNED OUT. R & R EXTERNAL EMERGENCY LIGHT BULB IAW AMM 33-50-10. OPS CHECKED GOOD

Part: CONNECTOR — BROKEN (CABIN) · airframe 32,783 hrs · 28,328 cycles

EMERGENCY FLOOR STRIP BETWEEN SEAT ROW 14 AND ROW 16 HAS A BROKEN CONNECTOR. REMOVED AND REPLACED EMERGENCY FLOOR STRIP BETWEEN SEAT ROW 14 AND ROW IAW AMM 33-50-12

Part: DOOR — DIRTY (CABIN) · airframe 32,267 hrs · 27,894 cycles

F/A HAVING DIFFCULTY OPENING MAIN DOOR. CLEAN AND LUBED PASSENGER DOOR IAW AMM 52-10-00. OPC GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 32,258 hrs · 27,883 cycles

SERVICE DOOR EMERGENCY LIGHT INOPERATIVE. R & R SERVICE DOOR EXTERNAL EMERGENCY LIGHT LAMP IAW AMM 33-50-10-000-801-A & 33-50-10-400-801-A, OPS CHECK GOOD AT THIS TIME.

Part: LOCK — FOD (PAX DOOR) · airframe 32,194 hrs · 27,811 cycles

MAIN CABIN DOOR WILL NOT OPEN FROM THE INSIDE WILL ONLY OPEN FROM THE OUTSIDE. INSPECTED MAIN CABIN DOOR IAW AMM 52-10-01 FOUND LATCH SPRING MECHANISM BRKOEN. DURING TROUBLESHOOTING FOUND FOD IN LOCK MECHANISM, REMOVED FOD AND C/W OPS CHECK IAW AMM 52-18-00, OPS CHECK GOOD

Part: BRAKE — FIRE (LT MLG) · airframe 31,740 hrs · 27,361 cycles

BRAKE FIRE AND HYD LEAK LT INBD BRAKE. R & R NR 2 BRAKE ASSY IAW WC 32-600-14. R & R NR 2 BRAKE LINES IAW AMM CH 20-10-03.

Part: CONTROL UNIT — FAILED (HORIZ STAB) · airframe 31,404 hrs · 27,077 cycles

PTRIM MAIN INOPERATIVE WARNING ON CLIMB OUT. R & R HORIZONTAL STABILIZER CONTROL UNIT IAW AMM 27-40-01. OPERATIONS CHECKED GOOD.

Part: DISPLAY — MALFUNCTIONED (COCKPIT) · airframe 31,194 hrs · 26,885 cycles

CAPTAINS MFD OUT, IT PRODUCED A STRONG ELEC SMELL AFTER THE SCREEN WENT BLANK. INSPECTED NR 1 MFD & FOUND TO BE THE SOURCE OF THE ODOR. DEFERRED MFD 1, M PROCEDURES COMPLIED WITH. R & R CAPTAINS MFD DU-2 IAW AMM 34-22-01. OPERATIONS CHECKED GOOD MEL 34-02 RESTORED.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 31,086 hrs · 26,789 cycles

CAPTAINS FLASHLIGHT INOPERATIVE, WILL NOT HOLD A CHARGE. R & R FLASHLIGHT & ASSEMBLY IAW AMM 33-50-16. OPERATIONS CHECKED GOOD. EMER FLASHLIGHT PN P2-07-0011-500.

Part: FLAP — MALFUNCTIONED (WING) · airframe 30,973 hrs · 26,688 cycles

FLAP FAIL AFTER TAKEOFF AT FLAP 9 DEGREES, OBSERVED FAULT CODE 27M0100. RESET & OPERATIONS CHECKED FLAPS IAW AMM 27-53-00-5. OPERATIONS CHECKED GOOD, NO DEFECTS OR RELATED CMC MSGS NOTED.

Part: FLAP — MALFUNCTIONED (WING) · airframe 30,800 hrs · 26,529 cycles

UPON FLAPS 9 SELECTION ON APPROACH, FLAPS FAIL MSG ON EICAS. TROUBLE SHOT IAW FIM TASK 27-51-00-810-808-A TRANSITORY CONDITION OF FLAP MECH SYS. RESET & PERFORMED OPERATIONS CHECK OF FLAP SYS IAW AMM 27-51-00. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAP) · airframe 30,744 hrs · 26,473 cycles

FLAP FAIL MSG ON EICAS, OCCURRED WHEN SELECTED FLAPS 9. IMMEDIATE MSG ON EICAS, FLAPS REMAINED AT 0. COMPLIED WITH FIM TASK 27-51-00-810-816A. CONSIDERED TO BE TRANSITORY CONDITION OF THE INBD & OTBD FLAP CONTROL SYS. PERFORMED OPERATIONAL CHECK OF THE FLAP CONTROL SYS IAW AMM 27-51-00-700-801. OPERATIONS CHECKED GOOD.

Part: ROLLER — DIRTY (FUSELAGE) · airframe 30,013 hrs · 25,795 cycles

FLIGHT ATTENDANT REPORTS MAIN DOOR HARD TO CLOSE. CLEANED & LUBED DOOR ROLLERS IAW AMM 53-21-02. OPERATIONS CHECKED GOOD.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 29,659 hrs · 25,465 cycles

GALLEY DOOR UPPER EMER LIGHT INOPERATIVE. R & R EMER LIGHT DC & AC INVERTER 2 IAW AMM 33-50-11. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 28,852 hrs · 24,781 cycles

EXTERIOR EMER LIGHT INOPERATIVE, RT SIDE FWD OF WING. R & R EXTERIOR EMER LIGHT LAMP RT FWD OF WING IAW AMM 33-50-10. OPERATIONS CHECKED GOOD.

Part: DOOR — LACK OF LUBE (CABIN) · airframe 28,707 hrs · 24,676 cycles

MAIN CABIN DOOR HARD TO CLOSE. LUBRICATED MAIN CABIN DOOR IAW AMM 52-18-00. TESTED SATISFACTORY.

Part: LIGHT — MISINSTALLED (EXTERIOR) · airframe 28,566 hrs · 24,570 cycles

RIGHT OVERWING EMER LIGHT INSTALLED BACKWARDS. REPOSITIONED AFT EXTERNAL RT EMER LIGHT ASSEMBLY IAW AMM 33-50-10. OPERATIONS CHECKED GOOD.

Part: SKIN — CRACKED (FUSELAGE) · airframe 28,454 hrs · 24,487 cycles

DURING MBV INSPECTION, QA FOUND RT UPPER FUSELAGE SKIN CRACKED AT FRAME 75 STRINGER 2R. ACFT WAS REMOVED FROM SERVICE FOR MBV INSPECTION & WILL BE RETURNED TO SERVICE AFTER MBV INSPECTION. PERFORMED PERMANENT REPAIR TO FUSELAGE SKIN AT FRAME 75 STRINGER 2R IAW ERS-EM-53MR-1024. REPAIR MATERIALS, FILLER 2024T3 .063, REPAIR DOUBLER 2024T3 .080, REPAIR ANGLE 2024T3 .050 & ANGLE FILLER 2024T3 .032.

Part: SKIN — CRACKED (FUSELAGE) · airframe 28,454 hrs · 24,487 cycles

DURING MBV INSPECTION, QA FOUND LT UPPER FUSELAGE SKIN CRACKED AT FRAME 75 STRINGER 2L. ACFT WAS REMOVED FROM SERVICE FOR MBV INSPECTION & WILL BE RETURNED TO SERVICE AFTER MBV INSPECTION. PERFORMED PERMANENT REPAIR TO FUSELAGE SKIN AT FRAME 75 STRINGER 2L IAW ERS-EM-53MR-1024. REPAIR MATERIALS, FILLER 2024T3 .063, REPAIR DOUBLER 2024T3 .080, REPAIR ANGLE 2024T3 .050 & ANGLE FILLER 2024T3 .032.

Part: CONNECTOR — BROKEN (CABIN) · airframe 28,454 hrs · 24,487 cycles

AIRCRAFT ARRIVED FOR IMBV INSPECTION WITH MEL 33-50 FOR FLOOR PROXIMITY STRIP JUST OUTSIDE OF LAVATORY INOPERATIVE. ACFT WAS REMOVED FROM SERVICE FOR IMBV INSPECTION & WILL BE RETURNED TO SERVICE AFTER IMBV INSPECTION. FOUND CONNECTOR BROKEN ON ACFT SIDE OF HARNESS. REPLACED CONNECTOR IAW SWPM 20-00-03.

Part: CONNECTOR — BROKEN (EMERGENCY LIGHTS) · airframe 28,435 hrs · 24,470 cycles

LEFT EMERGENCY LIGHT INOPERATIVE. FOUND CONNECTOR BROKEN. REPLACED CONNECTOR IAW SWPM 20-00-03.

Part: UNKNOWN — MALFUNCTIONED (LANDING GEAR) · airframe 28,391 hrs · 24,424 cycles

DURING TAKEOFF & DURING GEAR UP SELECTION THE LT MAIN GEAR INDICATED RED X THEN MOMENTARY UP & THEN RED X AGAIN WITH THE HYD PUMP PULSATING LOUDLY. DURING GEAR SELECTION DOWN ALL GEAR POSITION DOWN & GREEN WITHOUT PUMP PULSATING. A NORMAL APPROACH TO LAND WAS ACCOMPLISHED & TOUCHDOWN OCCURRED WITH A LESS THAN 100 FT PER MIN, SOFT TOUCHDOWN & LANDING. PERFORMED FUNCTIONAL CHECK OF PROX SWITCH IAW AMM 32-63-05-710-002-A00 & GEAR SWING FOR SEVEN TIMES IAW 32-30-00. RE TAPED NOSE UPLOCK PROX SWITCH IAW ETN-EM-32-176. OPERATIONS CHECKED GOOD. NO DEFECTS NOTED.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 27,963 hrs · 23,969 cycles

RIGHT OVERWING EMER EXIT IDENTIFIER PANEL INOPERATIVE. R & R EMER LIGHT DC AC INVERTER IAW AMM 33-50-11. ALL OPERATIONS CHECKED GOOD.

Part: ROLLER — LACK OF LUBE (FUSELAGE) · airframe 27,120 hrs · 23,257 cycles

MAIN CABIN DOOR STUCK TRYING TO CLOSE. HAD TO OPEN FROM OUTSIDE. LUBRICATED ROLLERS IAW 53-21-02. NO DEFECTS NOTED.

Part: BEARING — LACK OF LUBE (CABIN DOOR) · airframe 26,778 hrs · 22,920 cycles

MAIN CABIN DOOR WILL NOT OPEN & CLOSE CORRECTLY. LUBED MAIN DOOR EXTERNAL HANDLE BEARINGS & FUSELAGE ROLLER GUIDES. OPERATIONS CHECKED OK IAW AMM 52 10 01.

Part: CONNECTOR — LOOSE (SERVICE DOOR) · airframe 26,608 hrs · 22,797 cycles

SERVICE DOOR EMERGENCY LIGHT INOPERATIVE. FOUND LOOSE CONNECTOR ON SERVICE DOOR ELECTROLUMINESCENT EXIT LAMP. RECONNECTED ELEC CONNECTION IAW AMM 33-50-14-400-801-A. PERFORMED OPERATIONS CHECK OF EMERGENCY LIGHTS IAW AMM 33-50-00-700-801-A. OPERATIONS CHECKED GOOD.

Part: HANDLE — LACK OF LUBE (PAX DOOR) · airframe 25,857 hrs · 22,221 cycles

PASSENGER ENTRY DOOR HANDLE HARD TO OPERATE. LUBRICATED MAIN PAX DOOR IAW AMM 52-18-00, OPERATIONS CHECKED GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 25,788 hrs · 22,173 cycles

SERVICE DOOR EMERGENCY LIGHT INOPERATIVE. R & R SERVICE DOOR EMERGENCY LIGHT LAMP IAW AMM 33-50-10.

Part: INDICATOR — MALFUNCTIONED (MAIN DOOR) · airframe 25,576 hrs · 22,001 cycles

MAIN DOOR KEEPS POPPING OPEN DURING TAXI OUT AND INDICATING OPEN ON EICAS. RETURNED TO GATE AFTER PHYSICALLY SHUTTING DOOR TWO TIMES AND SHOWING CLOSED, THEN CHIME OPEN AGAIN DURING TAXI. AFTER OPS CHECKS DETERMINED THAT MAIN DOOR DOES NOT POP OPEN. MAIN DOOR CLOSED FIRM AND SECURE. DETERMINED PROBLEM TO BE AN INTERMITTENT DOOR OPEN INDICATION. CLEANED AND LUBRICATED PASSENGER DOOR LOCKING MECHANISM AND ADJUSTED SWITCHES IAW AMM 52-10-01 & 52-11-00. PERFORMED OPS TEST OF DOOR INDICATION SEVERAL TIMES WITH NO DISCREPANCIES NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT) · airframe 25,444 hrs · 25,444 cycles

EMERGENCY LIGHT PANEL OVER SERVICE DOOR IS INOPERATIVE. R & R NR 3 EMERGENCY LIGHT POWER INVERTER IAW AMM 33-50-11, OPS CHECKED GOOD IAW WC 33-700-17.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 25,241 hrs · 21,732 cycles

F/O FLASHLIGHT INOPERATIVE. R & R F/O'S FLASHLIGHT IAW AMM 33-50-16. TESTED SATISFACTORY.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 25,036 hrs · 21,560 cycles

F/O'S FLASHLIGHT IS INOPERATIVE. R & R FLASHLIGHT IAW AMM 25-60-00, OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY — UNSERVICEABLE (EMERGENCY LIGHT) · airframe 24,746 hrs · 21,331 cycles

DURING B INSPECTION, FOUND THE RT AND LT OVER WING EMERGENCY LIGHT INOPERABLE. THE ACFT WAS REMOVED FROM SERVICE. R & R THE NR 4 BATTERY AND CHARGER IAW AMM TASK 33-50-04-000-801-A, TASK 33-50-04-400-801-A, 33-50-04-000-802-A AND 33-50-04-400-802-A. ALSO PERFORMED OPC OF EMERGENCY LIGHTING SYS IAW W/C 33-700-17. NO DEFECTS NOTED AT THIS TIME AND OPC OF EMERGENCY LIGHTING SYS POWER SUPPLIES IAW W/C 33-700-19, NO DEFECTS NOTED AT THIS TIME. THE ACFT WAS RETURNED TO SERVICE.

Part: ACCESS DOOR — CORRODED · airframe 24,664 hrs · 21,268 cycles

DURING HEAVY CHECK FOUND ACCESS DOOR/ PANEL 272DR CORROSION REPAIR. THE ACFT WAS REMOVED FROM SERVICE. LEVEL OF CORROSION NOT IDENTIFIED. PERFORMED REPAIR IAW AEA EO-EM-52MR-358. THE ACFT WAS RETURNED TO SERVICE.

Part: TERMINAL — BROKEN (EMERGENCY LIGHTS) · airframe 24,721 hrs · 21,314 cycles

DURING B-INSPECTION, FOUND PROXIMITY LIGHTS NR 1 & NR 2 TO HAVE BROKEN TERMINALS. ACFT REMOVED FROM SERVICE. R & R PROXIMITY LIGHTS NR 1 & NR 2 IAW AMM 33-50-12. OPS CHECKED GOOD. ACFT RETURNED TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 24,059 hrs · 20,778 cycles

DURING B INSPECTION FOUND THE COCKPIT STEP AND GALLEY AISLE OVERHEAD EMERGENCY LIGHTS WILL NOT ILLUMINATE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 1 EMERGENCY LIGHT INVERTER ASSEMBLY IAW EMB AMM 33-50-11. THE OPERATIONAL CHECK WAS GOOD IAW W/C 33-700-17. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONTROLLER — INOPERATIVE (CABIN PRESSURE) · airframe 24,047 hrs · 20,770 cycles

FLIGHT 3537. DURING DESCENT, CABIN PRESSURE CONTROLLER MALFUNCTIONED. CABIN PRESSURE STARTED TO CLIMB TO 9000 FT WHILE DESCENDING FROM FL360. DECLARED AN EMERGENCY AND CONTINUED BELOW 10000 FT. CABIN OXYGEN MASK DID NOT DEPLOY AND AIRCRAFT LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. PERFORMED OPS CHECK OF MANUAL MODE IAW MM 21-31-00 OP'S CHECKED GOOD, REMOVED AND REPLACED DIGITAL CONTROLLER IAW AMM 21-31-01 OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: DOOR SEAL — SEPARATED (CABIN DOOR) · airframe 23,978 hrs · 20,720 cycles

DURING MAINTENANCE INSPECTION FOUND THE MAIN CABIN DOOR SEAL SEPARATING FROM THE UPPER AFT CORNER, IT WAS SEPARATING FROM THE INFLATABLE SEAL ALONG 5 - 6 INCHES OF THE CORNER. THE AIRCRAFT WAS REMOVED FROM SERVICE. COMPLIED WITH FILLER STRIP REPAIR IAW EMB 145 AMM 52-00-01. NO DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,759 hrs · 20,551 cycles

DURING PS-1 CHECK, FOUND BOTH REAR OVERWING EMERGENCY LIGHTS INOPERABLE. REMOVED AND REPLACED OVERWING LEFT EMERGENCY LIGHT ASSEMBLY IAW 33-50-07 AMM OPS CHECK GOOD. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 23,759 hrs · 20,551 cycles

DURING MAINTENANCE INSPECTION FOUND BURNED OUT FUSE ON CHARGER ASSEMBLY NR 4 REF AML PAGE 3360640 ITEM 4. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CHARGER ASSEMBLY NR 4 IAW EMB AMM 33-50-04. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 23,649 hrs · 20,469 cycles

ON FLIGHT 4083 THE CREW REPORTED A SMELL OF SMOKE IN CABIN AT THE GATE. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED DETAILED VISUAL AND OLFACTORY INSPECTION OF COCKPIT AND CABIN. RAN PACKS REFERENCING AMM CH 21. NO DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,152 hrs · 20,067 cycles

DURING B INSPECTION FOUND THE 2ND FROM FRONT CEILING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LAMP AT LOCATION INDICATED PER 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 23,121 hrs · 20,033 cycles

DURING B INSPECTION FOUND THE 3RD AFT EMERGENCY CEILING LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LAMP AT CEILING LIGHT INDICATED PER 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: INVERTER — INOPERATIVE (CABIN) · airframe 22,143 hrs · 19,283 cycles

DURING B INSPECTION FOUND THE EXIT LOCATOR CENTER AISLE FORWARD EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY LIGHT INVERTER NR 6 IAW EMB AMM 33-50-15. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CRADLE — DAMAGED (FLASHLIGHT) · airframe 21,112 hrs · 18,533 cycles

FLIGHT 3962, CREW REPORTED FLASHLIGHT BEHIND THE CAPTAIN'S SEAT WILL NOT STAY IN HOLDER, FALLS OUT IN FLIGHT. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED CAPTAIN’S FLASHLIGHT ASSEMBLY IAW AMM 33-50-16. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 21,112 hrs · 18,533 cycles

FLIGHT 3962, CREW REPORTED FIRST OFFICER’S FLASHLIGHT WILL NOT ILLUMINATE, WHILE IN CRADLE THE RED LIGHT IS ON. AIRCRAFT REMOVED FROM SERVICE. SECURE FIRST OFFICER’S FLASHLIGHT IAW AMM 33-50-16. NO PARTS REMOVED OR REPLACED. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: DOOR — LACK OF LUBE (CABIN) · airframe 21,077 hrs · 18,502 cycles

ON FLIGHT 4165 THE FLIGHT ATTENDANT REPORTED THE MAIN CABIN DOOR WAS STIFF TO OPERATE. THE AIRCRAFT WAS REMOVED FROM SERVICE. LUBRICATED THE MAIN DOOR IAW EMB 145 AMM 52-18-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: DUCT — DEFECTIVE (AC BAY) · airframe 20,940 hrs · 18,393 cycles

ON FLIGHT 4031 THE CREW REPORTED THAT AT FLIGHT LEVEL 250 CABIN ALT ROSE ABOVE 14,600 FEET AND DECENDED TO BELOW 10,000 FEET. THE CABIN STARTED TO PRESSURIZE AGAIN AT 4000 FEET IN ICE CONDITIONS, RECEIVED PACK 1 OVERHEAT AND ICE CONDITIONS FAIL MESSAGE ON EICAS. THE PASSENGER OXYGEN MASK DEPLOYED. THE CREW DECLARED AN EMERGENCY AND DIVERTED TO MCI. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED OPERATIONAL CHECK OF CABIN PRESSURIZATION IN AUTO AND MANUAL MODES OPC GOOD IAW AMM 21-31-00-700-801-A. TROUBLESHOT USING FIM TASK 21-51-00-810-803A AND FOUND TO BE TRANSITORY CONDITION. THE OPERATIONAL CHECK WAS GOOD OF PACK 1 IAW EMB AMM 21-51-00. REMOVED AND REPLACED THE PACK 2 DUAL TEMPERATURE CONTROL VALVE DUCT IAW AMM 21-60-01 PT 2J(2)(G) AND 3I(1)(H) OPC GOOD IAW AMM 21-51. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: MASK — MISSING (CABIN)

ON FLIGHT 3998 THE CREW REPORTED THE O2 DEMO MASK WAS MISSING. THE AICRAFT WAS REMOVED FROM SERVICE. REPLACED THE DEMO MASK IAW EMB-145 STANDARD PRACTICES. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BRACKET — GOUGED (RT AILERON) · airframe 19,720 hrs · 17,447 cycles

DURING MAINTENANCE BASE VISIT FOUND THE RIGHT AILERON DAMPENER BRACKET HAS GOUGES ON THE INNER FACE OF FLANGE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED RT AILERON DAMPER BRACKET IAW EO EM-27MR-112

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,720 hrs · 17,447 cycles

DURING MAINTENANCE BASE VISIT FOUND THE LEFT OMEGA BEAM CORRODED AT CROSSBEAM AT FRAME 23. THE AIRCRAFT WAS REMOVED FROM SERVICE. THE CORRECTIVE ACTION INFORMATION IS PENDING.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,720 hrs · 17,447 cycles

DURING MAINTENANCE BASE VISIT FOUND THE CENTER OMEGA BEAM CORRODED AT CROSSBEAM AT FRAME 25. THE AIRCRAFT WAS REMOVED FROM SERVICE. C/A: THE CORRECTIVE ACTION IS PENDING.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 19,720 hrs · 17,447 cycles

LEFT OMEGA BEAM CORRODED AT CROSSBEAM AT FRAME. REPAIRED LEFT OMEGA BEAM AT FR 25 IAW SRM 53-00-10.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,621 hrs · 16,675 cycles

DURING MAINTENANCE BASE VISIT FOUND THE CEILING EMERGENCY LIGHT AT ROW 7 INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CEILING EMERGENCY LAMP ROW 7 IAW EMB 145 AMM TASK 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 30,520 hrs · 25,513 cycles

DURING MAINTENANCE BASE VISIT FOUND THE RIGHT FORWARD EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT FORWARD EMERGEMCY LIGHT LAMP IAW EMB 145 AMM TASK 33-50-07-000-801-A AND 33-50-07 -400-801-A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 18,475 hrs · 16,559 cycles

(REQUEST TO MAKE SEPARATE SDR’S) FOR FLIGHT 3951 THE FORWARD EMERGENCY LIGHT ON THE RIGHT WING TO FUSELAGE PANEL WAS FOUND TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED BATTERY CHARGER ASSEMBLY IAW AE W/C 33-700-19. THE OPERATIONAL CHECK WAS GOOD IAW AE W/C 33-700-17. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 18,475 hrs · 16,559 cycles

FOR FLIGHT 3951 THE FORWARD EMERGENCY LIGHT ON THE RIGHT WING TO FUSELAGE PANEL WAS FOUND TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NUMBER 2 EMERGENCY BATTERY IAW AE W/C 33-700-19. THE OPERATIONAL CHECK WAS GOOD IAW AE W/C 33-700-17. THE AIRCRAFT WAS RETURNED TO SERVICE. (REQUEST TO MAKE SEPARATE SDR’S)

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 17,843 hrs · 16,082 cycles

DURING MAINTENANCE BASE VISIT FOUND THE SERVICE DOOR EMERGENCY LIGHT TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPLACED THE SERVICE DOOR EXTERIOR EMERGENCY LIGHT LAMP IAW EMB AMM TASKS 33-50-10-000-801-A AND 33-50-10-400-801-A. NO FIX. TROUBLESHOT FOUND WIRING TO BE GOOD. REPLACED NR 2 EMERGENCY LIGHT BATTERY AND POWER SUPPLY IAW W/C 33-700-19 IAW W/C 33-700-17 GOOD. NO FURTHER DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 16,533 hrs · 150,201 cycles

DURING MAINTENANCE BASE VISIT FOUND THE AFT EMERGENCY FLASHLIGHT TO HAVE AN INOPERABLE BATTERY. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AFT FLASHLIGHT BATTERY. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 16,138 hrs · 3,350 cycles

DURING PS-1 CHECK FOUND THE RIGHT AND LEFT OVER-THE-WING EMERGENCY LIGHTS TO NOT BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND INSTALLED THE NR 4 BATTERY CHARGER IAW EMB AMM 33-50-10. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ENGINE — MALFUNCTIONED (NR 1) · airframe 14,883 hrs · 13,641 cycles

ON FLIGHT 3355 DURING THE TAKEOFF AT ABOUT 40 KNOTS THE CREW REPORTED GRAYISH WHITE SMOKE IN THE COCKPIT THAT INCREASED RAPIDLY. THE CREW ELECTED TO ABORT THE TAKEOFF. SMOKE REMOVAL PROCEDURES WERE APPLIED WITH THE APU AND PACKS AND THE SMOKE CLEARED TO 84 PERCENT. THE FLIGHT ATTENDANT CONFIRMED SMOKE IN THE CABIN BUT NOT IN THE LAVATORY. HEAT AND FIRE WERE NOT NOTED BY THE CREW. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED NR 1 ENGINE IAW EMB 145W/C72-00-00. OPERATIONAL CHECK AND LEAK CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

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

DURING MAINTENANCE BASE VISIT THE INSPECTION FOUND A LAVATORY SERVICE BUCKET CORRODED. AIRCRAFT REMOVED FROM SERVICE. FABRICATED REPAIR DOUBLER. DRILLED FASTENER HOLES, ALODINED AND PRIMED. INSTALLED DOUBLER ON LAVATORY SERVICE BUCKET IAW SRM 53-31-02. AIRCRAFT RETURNED TO SERVICE.

Part: CONTROL UNIT — MALFUNCTIONED (PITCH TRIM) · airframe 11,277 hrs · 10,337 cycles

ON FLIGHT 4489, CREW REPORTED SHORTLY AFTER TAKEOFF ON CLIMB, THEY GOT A PITCH TRIM MAIN INOP. CREW DECLARING AN EMERGENCY AND RETURN TO ORD. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED HSCU AND FO'S YOKE PITCH TRIM SWITCH, OPS CHECKS WERE GOOD AT THIS TIME. WORK PERFORMED IAW AMM 27-40-01 AND 27-40-03. AIRCRAFT RETURNED TO SERVICE.

Part: WARNING MESSAGE — ILLUMINATED (CARGO DOOR)

SHORTLY AFTER TAKE OFF CREW GOT A BAGGAGE DOOR WARNING. CREW CHOOSE TO RETURN TO CLT. ISSUED MEL 52-05 IN CLT.

Part: ACTUATOR — MALFUNCTIONED (PITCH TRIM) · airframe 9,764 hrs · 8,940 cycles

EN ROUTE RECEIVED PITCH TRIM MAIN INOP ON EICAS CUT OUT SYSTEM.

Part: ACTUATOR — FAILED (PITCH TRIM) · airframe 9,764 hrs · 8,940 cycles

EN ROUTE RECEIVED PTRIM MAIN INOP ON EICAS CUT OUT SYSTEM.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,753 hrs · 8,933 cycles

DURING MBV INSPECTION, FOUND FORWARD SERVICE DOOR SILL BETWEEN FRAMES 17-20 CORRODED. REPAIRED SILL. AIRCRAFT WAS RETURNED TO SERVICE.

Part: PLATE — CORRODED · corrosion level 2 · airframe 9,753 hrs · 8,933 cycles

DURING MBV INSPECTION, FOUND INTERSECTING PLATE BETWEEN RIGHT HAT BEAM AND FLOORBEAM 22 IS CORRODED. REMOVED AND REPLACED PLATE IAW EMB SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,753 hrs · 8,933 cycles

DURING MBV INSPECTION, FOUND DIGITAL BEAM CORRODED AT FRAME 17. REPAIRED BEAM, A/C RETURNED TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,753 hrs · 8,933 cycles

DURING MBV INSPECTION, FOUND DIGITAL BEAM CORRODED AT FRAME 17. REPAIRED BEAM. A/C RETURNED TO SERVICE.

Part: PLATE — CORRODED (FUSLEAGE) · corrosion level 2 · airframe 9,753 hrs · 8,933 cycles

DURING MBV INSPECTION FOUND INTERSECTING PLATE BETWEEN RIGHT HAT BEAM AND FLOORBEAM 22 IS CORRODED. REMOVED AND REPLACED PLATE IAW EMB SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,753 hrs · 8,933 cycles

UPPER FLOORBEAM AT FRAME 23 CORRODED DURING MBV FOUND UPPER FLOORBEAM AT FRAME 23 CORRODED. REMOVED FLOORBEAM AND INSTALLED NEW FLOORBEAM AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,753 hrs · 8,933 cycles

UPPER FLOORBEAM AT FRAME 23 CORRODED DURING MBV FOUND UPPER FLOORBEAM AT FRAME 23 CORRODED. REMOVED FLOORBEAM AND INSTALLED NEW FLOORBEAM. AIRCRAFT WAS RETURNED TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,753 hrs · 8,933 cycles

DURING MBV INSPECTION, FOUND FORWARD SERVICE DOOR SILL BETWEEN FRAMES 17-20 CORRODED. REPAIRED SILL. AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,753 hrs · 8,933 cycles

DURING MBV INSPECTION, FOUND FLOOR SUPPORT ANGLE ON LEFT OMEGA BEAM JUST FORWARD OF FRAME 20 CORRODED. REMOVED AND REPLACED FLOOR SUPPORT IAW EMB SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,753 hrs · 8,933 cycles

DURING MBV INSPECTION, FOUND FLOOR SUPPORT ANGLE ON LEFT OMEGA BEAM JUST FORWARD OF FRAME 20 CORRODED. REMOVED AND REPLACED FLOOR SUPPORT IAW EMB SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE.

Part: CHARGER — FAILED (EMERGENCY LIGHTS)

FOUND EMERGENCY LIGHT IN CEILING INOPERATIVE. RAI NR 2 BATTERY CHARGER, IAW EMB 145, AMM 33-50-04. OPS CHECK GOOD. RETURNED AIRCRAFT TO SERVICE. (M)

Part: GENERATOR — FAILED (NR 3)

ORD - FLT 4462 - NR 3 GEN VOLTS WENT TO ZERO. RESET GEN 3 AND THE NR 2 AND 4 GENS WENT OFF LINE. RETURNED TO ORD. (M)

Part: FLANGE — CRACKED (FRAME 68)

FRAME 68 IB FLANGE WAS FOUND TO BE CRACKED AT THE CARGO DOOR OPEN ROD CUP. CUT OUT THE CRACKED AREA OF THE FRAME. PREPARED A REPAIR SECTION OF NEW FRAME. FABRICATED 2 FRAME SPLICES AND REPAIR ANGLE. REPAIR DONE IAW SRM. (K)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. REMOVED THE CORROSION BY MAKING A CUT OUT. PREPARED A DOUBLER, FILLER, FABRICATED A PLATE AND TWO SHIMS. REPAIR DONE IAW EMB SRM, SRM 145/1142 REV 31, CHAPTER 53-00-10. (M)

Part: LIGHT — WRONG PART (CABIN)

FLT 3640 - GSP - CREW NOTED ON PREFLIGHT THAT THE EMERGENCY LIGHTS AT THE OVERWING EXITS ARE GREEN AND NOT AMBER. REPLACED EMERGENCY FLOOR LIGHT STRIP AT OVERWING EXIT. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: CONNECTOR — LOOSE (BATTERY PACK)

SHV - FLT 3473 - CENTER SECTION OF FLOOR EMERGENCY LIGHTS AND OUTER WING EMERGENCY EXIT LIGHTS INOPERATIVE. FOUND LOOSE CONNECTOR ON BATTERY PACK NR 3 AND RESECURED. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (M)