N658AE

Part: MIXER BOX — ODOR (CONDENSER)

AFTER T/O, CREW REPORTS STRONG BURNING SMELL, MORE RUBBBER THAN ELECTRICAL. RAR CONDENSER/ MIXER OPS CHECK GOOD.

Part: DUCT — BLOWN (NR 2 A/C PACK) · airframe 47,556 hrs · 43,817 cycles

PARKED AT GATE WITH APU SELECTED, LEAK DISPLAYED ON BLEED 2 BUTTON AND EICAS WITH BURNING SMELL IN CABIN. FACT 04JUN25 22:13 ORD RAN PACKS 1 AND 2 OFF OF APU BLEED. NO BURNING SMELL NOTED.HEARD AIR RUSHING FROM PACK 2 AREA REMOVED PACK 2 PANEL AND FOUND BLOWN DUCT ON PACK 2 Y DUCT. R&R SLEEVE ON PACK 2Y DUCT IN REF TO AMM TASK 21-51-01-000/400-801-A OPS CHECK GOOD LEAK CHECK GOOD OK FOR SERVICE

Part: INVERTER — FAULTED (ZONE 200) · airframe 47,326 hrs · 43,581 cycles

RH EMERGENCY EXIT IDENTIFIER LIGHT INOP. RAR INVERTER IAW AMM33-50-11

Part: NONE — NO DISCREPANCY (NONE)

BIRDSTRIKE LEFT OUTBD FLAP. C/W BIRDSTRIKE INSP IAW AMM 05-50-08 CLEANED BIRD REMAINS NO DEFECTS NOTED.

Part: A/C PACK — MALFUNCTIONED (ZONE 100) · airframe 46,469 hrs · 42,697 cycles

DURING MAX TAKE OFF PACKS DID NOT SHUT OFF RESULTING IN BURNING SMELL IN FLIGHT DECK AND CABIN. COMPLIED WITH FIM TASK 21-00-00-810-801-A BLOCK 1 PG 202 TO 208 BLOCK 9 SUBTASK 813-045-A BLOCK 60 PG 208 FAILURE OF L/H ACM SEE LP 318817 SEQ 2 FOR MEL PROCEDURES. PDIS 658 21-51 318817 TRI CLOSE PACK 1 INOP SEE LP 318816 SEQ 1 FOR T/S TRI C34217 21-15-21 AIR COND PACK N650 AND ABOVE FACT 10DEC24 04:29 MDT R/R'D RELAY K0071 AS REQ. OPS CHECK GOOD. OK FOR SERVICE AT THIS TIME.

Part: APU — FAILED (ZONE 100) · airframe 46,341 hrs · 42,551 cycles

WITH PACK 2 ON AND RUNNING ON APU, ODOR AND SMOKE FROM VENTS ON FLT DECK AND CABIN. SELECTED PACK OFF AND APU FAILED AFTER 3 MINUTES OF SMOKE OCCURING. MESSAGE OF APU OIL HIGH TEMP MEL 11NOV24 15:31 CAE C31614 49-1 APU

Part: ANGLE — CRACKED (ZONE 200) · airframe 46,328 hrs · 42,534 cycles

53-2302 FLT DECK, ANGLE CRACKED AT FR13 STR4R. RAR ANGLE IAW SRM 51-40-02

Part: SKIN — CRACKED (ZONE 300) · airframe 46,328 hrs · 41,534 cycles

55-2261 RUDDER II, LH SKIN CRACKED AT UPPER MID HINGE FITTING ATTACHMENT. REPAIRED IAW ETD 2024-145-026648 AND EO1-55-24-0624

Part: ANGLE — CRACKED (ZONE 200) · airframe 46,328 hrs · 42,534 cycles

53-2246 LOWER ANGLE #2 CRACKED AT X15506-5. RAR ANGLE IAW SRM 51-40-02

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 46,328 hrs · 42,534 cycles

53-2214 SHEAR CLIP CRACKED AT FR80 BTW STR5-7R. RAR SHEAR CLIP IAW SRM 51-40-02

Part: SUPPORT ANGLE — CRACKED (BODY FAIRING) · airframe 46,328 hrs · 42,534 cycles

53-2243 BODY FAIRING 195EL UPPER SUPPORT ANGLECRACKED AT X14216.5. RAR ANGLE IAW SRM 53-23-12

Part: SUPPORT ANGLE — CRACKED (BODY FAIRING) · airframe 46,328 hrs · 42,534 cycles

53-2245 BODY FAIRING 195EL LWR SUPPRT ANGLE CRACKED AT X13801.5. REPAIRED IAW SRM 57-20-07

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 46,328 hrs · 42,534 cycles

53-2171 SHEAR CLIP CRACKED AT FR61 BTW STR6-7L. RAR SHEAR CLIP IAW SRM 51-40-02

Part: PROFILE — CRACKED (ZONE 100) · airframe 46,328 hrs · 42,534 cycles

53-2168 CARGO ENTRY, FLOOR STRUCTURE PROFILE CRACKED. RAR PROFILE IAW SRM 51-40-02

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 46,328 hrs · 42,534 cycles

53-2170 SHEAR CLIP CRACKED AT FR61 BTW STR6-7R. RAR SHEAR CLIP IAW SRM 51-40-02

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 46,534 hrs · 42,534 cycles

53-2162 SHEAR CLIP CRACKED AT FR62 BTW STR6-8R. RAR SHEAR CLIP IAW SRM 51-40-02

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 46,328 hrs · 42,534 cycles

53-2163 SHEAR CLIP CRACKED AT FR62 BTW STR6-8L. RAR SHEAR CLIP IAW SRM 51-40-02

Part: SUPPORT — CRACKED (ZONE 800) · airframe 46,328 hrs · 42,534 cycles

53-2165 CARGO DOOR MECHANISM SUPPORT STRUCTURE CRACKED AT BTW FR67-68 STR5R. RAR SUPPORT STRUCTURE IAW SRM 51-40-02

Part: ATTACH BRACKET — DAMAGED (ZONE 500) · airframe 46,328 hrs · 42,534 cycles

57-2180 LH WING LATERAL FAIRING, LWR MID ATTACH BRACKET DAMAGED. RAR BRACKET IAW SRM 51-40-02

Part: SUPPORT CHANNEL — CRACKED (ZONE 800) · airframe 46,328 hrs · 43,534 cycles

53-2164 CARGO DOOR MECHANISM SUPPORT CHANNEL CRACKED AT FR62 BTW STR5-6R. RAR CHANNEL IAW SRM 51-40-02

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 46,328 hrs · 42,534 cycles

53-2125 SHEAR CLIP CRACKED AT FR60 BTW STR15-16L. RAR SHEAR CLIP IAW SRM 51-40-02

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 46,328 hrs · 42,534 cycles

53-2089 SHEAR CLIP CRACKED AT FR24 BTW STR15-16R. RAR SHEAR CLIP IAW SRM 51-40-02

Part: SUPPORT — CORRODED · corrosion level 2 · airframe 46,328 hrs · 42,534 cycles

53-2059 RH SILL CORRODED BTW FR23-29. RAR SILL IAW SRM 51-40-02

Part: SUPPORT — CORRODED · corrosion level 2 · airframe 46,328 hrs · 42,534 cycles

53-2047 LH SILL CORODED BTW FR36-41. RAR SILL IAW SRM 51-40-02

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 46,328 hrs · 42,534 cycles

53-2090 LH UNDERFLOOR SILL CORRODED AT BTW FR23-29. RAR SILL IAW SRM 51-40-02

Part: SUPPORT — CORRODED · corrosion level 2 · airframe 46,328 hrs · 42,534 cycles

53-2048 LH SILL CORRODED BTW FR41-48. RAR SILL IAW SRM 51-40-02

Part: SUPPORT — CORRODED · corrosion level 2 · airframe 46,328 hrs · 42,534 cycles

53-2046 RH SILL CORRODED BTW FR36-41. RAR SILL IAW SRM 51-40-02

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,991 hrs · 41,789 cycles

53-2084 LH UNDERFLOOR OMEGA BEAM CRACKED AND CORRODED AT FR29. REPAIRED IAW SRM 53-00-10 AND EO 1-53-24-0559

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 46,328 hrs · 42,534 cycles

53-2083 LH UNDERFLOOR OMEGA BEAM CRACKED AT FR34. REPAIRED IAW ETD2024-145-027329 AND EO1-53-24-0598

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 46,328 hrs · 42,534 cycles

53-2083 LH UNDERFLOOR OMEGA BEAM CORRODED AT FR31. REPAIRED OMEGA BEAM IA ETD2024-145-027329 AND EO1-53-24-0548

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 46,328 hrs · 42,534 cycles

53-2087 CORRODED RH UNDERFLOOR SILL AT FR29-35. RAR SILL IAW SRM 51-40-02

Part: SUPPORT — CORRODED · airframe 46,328 hrs · 42,534 cycles

53-2091 LH UNDERFLOOR SILL CORRODED AT BTW FR29-35. RAR SILL IAW SRM 51-40-02

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 46,328 hrs · 42,534 cycles

53-2040 OMEGA BEAM CRACKED AT BTW FR21-22. REPAIED IAW ETD 2024-145-026389 AND EO1-53-24-0597

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 46,328 hrs · 42,534 cycles

53-2036 CF1 OMEGA BEAM SMALL ANGLE CRACKED. RAR SMALL ANGLE IAW SRM 51-40-02

Part: STRUCTURE — CORRODED · corrosion level 2 · airframe 46,328 hrs · 42,534 cycles

53-2034 CF1 FWD DIGITAL CORRODED. RAR DIGITAL IAW SRM 51-40-02

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 46,328 hrs · 42,534 cycles

53-2040 OMEGA BEAM CRACKED AT BTW FR21-22. REPAIRED IAW ETD 2024-145-026389 AND EO1-53-24-0597

Part: CHANNEL — CORRODED (ZONE 200) · corrosion level 2 · airframe 46,328 hrs · 42,534 cycles

53-2037 SERVICE DOOR CUT OUT LWR CHANNEL CORRODED. RAR CHANNEL IAW SRM 51-40-02

Part: STRUCTURE — CORRODED · corrosion level 2 · airframe 46,328 hrs · 42,534 cycles

53-2035 CF1 AFT DIGITAL CORRODED. RAR DIGITAL IAW SRM 51-40-02

Part: SKIN — DENTED (ZONE 300) · airframe 46,328 hrs · 42,534 cycles

53-2016 MULTIPLE DENTS ON SIDES OF DORSAL FIN ATTACHMENTS. REPAIRED IAW ETD 2024-145-025466 AND EO1-53-24-0641

Part: PIN — SEIZED (ZONE 300) · airframe 46,313 hrs · 42,520 cycles

LH HORIZONTAL STAB ANTI-ROTATIONAL PIN HAS ROTATED AFT WITH SIGNS OF SEIZURE. REPAIRED IAW EO1-55-24-0532

Part: NUT PLATE — MISSING (ZONE 300) · airframe 46,328 hrs · 42,534 cycles

714 SKIN ON LH SIDE OF RUDDER II PROTRACTOR HAS MISSING NUTPLATE WITH ELONGATED RIVET ATTACHMENT HOLES. REPAIRED IAW EO1-55-24-0640

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 46,313 hrs · 42,520 cycles

RH EMERGENCY DOOR AFT EXIT LIGHT INOP. RAR BATTERY PACKS IAW WC 33-70-17

Part: SKIN — CRACKED (ZONE 500) · airframe 46,312 hrs · 42,519 cycles

LH WING LOWER SKIN CRACK 4.25 IN LENGTH BETWEEN RIB 11 AND 12 SPAR 2 CRACK GOES FROM AFT EDGE THROUGH THE SCREW HOLE FOR THE INBD MOST SCREW ON THE OTBD LOWER FLAP SHROUD. REPAIRED IAW EO1-57-24-0508

Part: ENGINE — POWER LOSS (NR 2) · airframe 45,889 hrs · 42,057 cycles

ENGINE #2 ROLLED BACK WITH LOUD BANG ON TAKEOFF ROLL. ( CAPTAIN SAID HE REJECTED TAKEOFF AND REQUESTED MAINTENANCE TO TOW THE PLANE BACK, AFTER WHICH HE SHUT DOWN THE PACKS WHEN HE STARTED TO SMELL THE FUMES )

Part: CONTROL UNIT — FAULTED (H/S PITCH TRIM) · airframe 45,597 hrs · 41,722 cycles

PITCH TRIM MAIN INOP IN FLIGHT. FACT 02APR24 03:58 FWA TROUBLE SHOT PER FIM TASK 27-43-00-810-803-A NO EICAS MESSEGE UPON ARRIVAL R/R HORIZONTAL STAB CONTROL UNIT IAW AMM 27-40-01. OPS CHECK GOOD. NO DEFECTS NOTED. A/C OK FOR SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 45,566 hrs · 41,686 cycles

RUBBER BURNING SMELL INSIDE AND OUTSIDE OF AIRCRAFT. PERFORMED GI. GRD RAN BOTH ENGS, CYCLED AVIONICS ON-OFF. CK'D BATT COMP. WHEEL WELL, BATT. RECEPTICAL AREA, AND COCKPIT. NO ODD SMELLS NOTED. OK FOR SERVICE

Part: TRIM SYSTEM — FAULTED (MAIN)

MAIN PITCH TRIM INOP IN FLIGHT. PERFORMED OPS TEST OF THE HORIZONTAL STAB ELECTRICAL/ELECTRONIC OPS CHECK IRT AMM 27-40-00-700-802-A/500.OPS CHECK GOOD PER FIM TASK 27-43-00-810-801-A BOXES 1 AND 7 TRANSITORY CONDITION OF THE CMC. OK FOR SERVICE.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 45,005 hrs · 41,046 cycles

BIRD STRIKE TO NOSE AND R/H FUSELAGE. CLEANED AREA AND INSPECTED A/C IAW AMM 05-50-08. FOUND 2 DENTS ON FUSELAGE AND RADOME LATCH DAMAGED. REPAIRED DENTS IAW EO1-53-23-0396. R&R'D LATCH IAW AMM 53-11-01-820-801-A

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 44,309 hrs · 40,224 cycles

PACK 1 AND 2 VLV CLSD DURING CLIMB. FACT 02JUL23 14:08 CLT R&R'D 2 SLEEVES ON DSCV ON #1 SIDE AS REQUIRED AND 2 SLEEVES ON HEAT EXCHANGER GOING TO DSCV ON #2 SIDE. OPS CHECK GOOD. A/C OK FOR SERVICE

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 43,975 hrs · 39,853 cycles

WITH E2 A/I VALVE ON MEL E2 A/I FAIL ON EICAS MSG DISPLAYED WHEN IN ICE CONDITION, AND OVERRIDE KNOB IN ENG OR ALL POSITION FACT 01MAY23 20:57 PHL R&R'S E2 A/I VALVE IN REFERENCE TO AMM 30-21-01 R&R'S E2 A/I PRESSURE TRANSDUCER IN REFERENCE TO AMM 30-21-06. PERFORMED A/I VALVE TEST IAW AMM 30-00-00. OPS TEST SATISFACTORY OK FOR SERVICE AT THIS TIME.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 43,769 hrs · 39,626 cycles

PDIS 658 72-01 2837031 20MAR23 CLT CLOSE #2 ENGINE LP AND HP VIBRATIONS OUT OF RANGE HISTORY: NONE FACT 20MAR23 19:58 CLT FOUND EVM TO BE DEFECTIVE. R&R EVM IAW AMM 77-41-03. OPS CHECKS AND GOOD IAW77-41-03-700-801-A. NO OTHER DEFECTS AT THIS TIME. OK FOR SERVICE

Part: SMOKE WARNING — FALSE ACTIVATION (CARGO) · airframe 41,124 hrs · 37,550 cycles

PDIS 658 26-15 2698361 11JUN22 ROC CLOSE BAGGAGE SMOKE INDICATION, PERFORMED ACTION ITEMS. USED THE BAGGAGE EXTINGUISHER, POSSIBLE FALSE INDICATION. FACT 11JUN22 22:30 ROC REMOVED AND REPLACED TOP AND BOTTOM BAG BAY FIRE BOTTLES AND TEE CHECK VALVE IAW EMB 145 AMM 26-23-01, OPS CHECK GOOD. REMOVED AND REPLACED FORWARD AND AFT BAG BAY SMOKE DETECTOR IAW EMB AMM 26-15-01, OPS CHECK GOOD.

Part: ANTI-ICE VALVE — FAILED (ZONE 400) · airframe 42,360 hrs · 38,053 cycles

658 30-21 2640972 05MAY22 MDT CLOSE DURING T/O ROLL E1 A/ICE FAIL WITH ICE DET OVERRIDE KNOB SET TO ENG. ABORTED T/O THEN FOLLOWED QRH. FACT 05MAY22 09:03 MDT R/R'D E1 A/I VALVE IN REFERENCE TO 30-21-01-000/400-801-A OPS CHECK GOOD OK FOR SERVICE AT THIS TIME.

Part: NOT REPORTED — NOT REPORTED · corrosion level 2 · airframe 41,993 hrs · 37,656 cycles

E901498 - RH #1 OUTBOARD FLOOR SILL CORRODED .... REMOVED AND REPLACED RH #1 OUTBOARD FLOOR SILL IAW EMB145 SRM 51-40-02. SEE TURNOVER FOR DETAILS.

Part: NOT REPORTED — NOT REPORTED · corrosion level 2 · airframe 41,993 hrs · 37,656 cycles

E901425 - CORROSION ON LH INBD #1 SEAT TRACK .... REMOVED AND REPLACED THE LH INBD #1 SEAT TRACK IAW EMB145 AMM 53-01-06 EASI 7248

Part: NOT REPORTED — NOT REPORTED · airframe 41,993 hrs · 37,656 cycles

E900513 - FUSELAGE SKIN HAS POSSIBLE CRACK AT FRAME 79 BETWEEN STRINGERS 06R AND 07R MARKED .... REPAIRED FUSELAGE SKIN CRACK AT FRAME 79 BETWEEN STRINGERS 06R AND 07R IAW PIEDMONT EO1-53-22-0025.

Part: NOT REPORTED — NOT REPORTED · airframe 41,993 hrs · 37,656 cycles

E900517 - FUSELAGE SKIN HAS 2 POSSIBLE CRACKS AT FRAME 77 BETWEEN STRINGERS 05R AND 07R .... REPAIRED FUSELAGE SKIN CRACK AT FRAME 77 BETWEEN STRINGERS 06R AND 07R IAW PIEDMONT EO1-53-22-0025. ONE AREA NOT FOUND TO BE CRACKED, SEE TASK #1.

Part: NOT REPORTED — NOT REPORTED · airframe 41,993 hrs · 37,656 cycles

E900666 - RH UPPER FUSELAGE SKIN CRACKED JUST AFT OF FRAME 75 AND ABOVE STRINGER 2R. CRACK IS 3/8' LONG, MARKED. EASI #8071 USED. 50-500 KHZ PROBE, FREQ= 400 KHZ, V-GAIN= 78.0, H-GAIN= 65.0, LPF= 100 .... REPAIRED RH UPPER FUSELAGE SKIN CRACKED JUST AFT OF FRAME 75 AND ABOVE STRINGER 2R IAW PIEDMONT EO1-53-22-0024

Part: NOT REPORTED — NOT REPORTED · corrosion level 2 · airframe 41,993 hrs · 37,656 cycles

E901417 - CORROSION ON DIAMOND GUSSET AT FRAME 22 .... REMOVED CORRODED DIAMOND GUSSET AT FRAME 22, POSITIONED DRILLED AND INSTALLED SERVICEABLE DIAMOND GUSSET IAW EMB 145 SRM 51-20-03, 51-40-02.

Part: NOT REPORTED — NOT REPORTED · corrosion level 2 · airframe 41,993 hrs · 37,656 cycles

E901608 - SERVICE DOOR AFT SILL CORRODED .... REMOVED AND REPLACED SERVICE DOOR CUTOUT AFT SILL IAW EMB145 SRM 51-40-02. RESTORED PROTECTIVE COATING AS REQUIRED

Part: NOT REPORTED — NOT REPORTED · corrosion level 2 · airframe 41,993 hrs · 37,656 cycles

E901499 - LH #2 OUTBOARD FLOOR SILL CORRODED .... REMOVED AND REPLACED LH #2 OUTBOARD FLOOR SILL IAW EMB145 SRM 51-40-02. SEE TURNOVER FOR DETAILS.

Part: NOT REPORTED — NOT REPORTED · corrosion level 2 · airframe 41,993 hrs · 37,656 cycles

E901506 - RH #1 (CENTER) FLOOR BEAM GUSSET CORRODED .... REMOVED AND REPLACED RH #1 (CENTER) FLOOR BEAM GUSSET IAW EMB145 SRM 51-40-02. RESTORED PROTECTIVE COATING AS REQUIRED

Part: NONE — NONE · airframe 41,386 hrs · 36,977 cycles

PDIS 658 36-21 2148011 24SEP21 ROC CLOSE BLEED 1 LEAK SHORTLY AFTER LIFTOFF WITH TO1 THRUST .... T/S BLEED LEAK FOUND HOT SECTION AT PANEL 414DB, OPENED PANEL IAW AMM 06 43 00. FOUND HOT SECTION ACROSS FROM EBV1. R+R EBV1 IAW AMM 36 11 05. PERFORMED ENG RUNS, NO FIX R+R PRE COOLER #1, REPLACED O RING ON #1 FAN AIR THERMOSTAT, R+R LH PYLON DUCT LEAK THERMAL SWITCH, R+R APU BLEED AIR CHECK VLV, ALL NO FIX. FOUND AFT LOWER SIDE CARGO DOOR BLEED COUPLING LOOSE. TIGHTED PER AMM 36 11 09. OPS AND LEAK CHECK GOOD.

Part: SOLENOID — STICKING (GUST LOCK) · airframe 40,989 hrs · 36,546 cycles

GUST LOCK WILL NOT DISENGAGE. MAINTENANCE PERFORMED: INSPECTED GUST-LOCK AND FOUND PLUNGER FOR GUST-LOCK SOLENOID STICKING, CLEANED AND LUBED PLUNGER. OPERATED GUST-LOCK SEVERAL TIMES. OPS CHECK GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (RT GLIDESLOPE) · airframe 40,386 hrs · 35,860 cycles

GLIDESLOPE LEFT AND RIGHT SIDE DID NOT MATCH ON ILS APPROACH. FOR THE ENTIRE APPROACH. R & R RT NAV UNIT, IAW EMB AMM 34-32-01. OPERATIONS CHECK GOOD OK FOR SERVICE. PERFORMED ILS CHECK, IAW TIC BOX, NAV SENSITIVITY CHECK GOOD. CLEAR MEL 34-10 AND SIL 34-51.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 39,796 hrs · 35,195 cycles

PDIS 658 36-11 2157741 26MAR20 MGM CLOSE BLEED 1 OVER TEMP MESSAGE AT 24000FT REMAINED ON FOR 5 MINS AND THEN EXTINGUISHED APPROX AT 10000FT. FACT 26MAR20 09:26 SBY REMOVED PYLON PANELS 414DB 414CB INSPECTED COMPONENT S INSIDE PYLON AREA FOUND NO DEFECTS AT THIS TIME IN STALLED PANELS 414DB 414CB USING RETAINED HARDWARE I NBOUND REPOTTED NO DISCREPANCY OPS AND BLEED CHECKS GOOD. NO DISCREPANCIES

Part: UNKNOWN — MALFUNCTIONED (COCKPIT) · airframe 39,768 hrs · 35,160 cycles

PDIS 658 21-32 2157674 19MAR20 CLT CLOSE ON CLIMB-OUT CREW FOUND EICAS WAS SHOWING AMBER DASH LINES ON RATE AND CABIN ALTITUDE. 24853 00 CFG FACT 19MAR20 14:07 CLT PWR DOWN PWR UP W/ELEC RESET DISPLAYS RETURNED TO NORMAL INDICATIONS OPS CK GOOD AT THIS TIME.

Part: CONTROL UNIT — MALFUNCTIONED (BRAKE SYS) · airframe 39,531 hrs · 34,882 cycles

BRK I/B INOP, EICAS MESS. ON APPROACH. R&R BCU IAW AMM 32-41-02 MAIN BRAKE SYS FUNCTIONAL CHECKED IAW AMM 32-41-00 OPS CHECK GOOD OK FOR SERVICE AT THIS TIME.

Part: WARNING MESSAGE — FALSE ACTIVATION (BRAKES) · airframe 39,525 hrs · 34,876 cycles

BRK INBD INOP MSG ON EICAS CREW C/W QRH. R+R BRAKE CONTROL VALVE IAW AMM 32-41-06. OPS CHECK IAW AMM 29-10-00-860-802-A/200. OPS CHECK GOOD. OK FOR SERVICE AT THIS TIME.

Part: LINE — LEAKING (BRAKES) · airframe 39,376 hrs · 31,701 cycles

PDIS 658 29-13 2122882 05JAN20 PHL CLOSE L/H INB BRAKE AREA APPEARS TO BE LEAKING FACT 05JAN20 18:51 PHL CLEANED AND IN SPECTED AREA FOR LEAKS. NO LAKS NOTED . PERF OPS CHECK OF BRAKE SYSTEN, OPS CHECK GOOD, NO LEAKS NOTED. OK FOR SERVICE.

Part: HOSE — BROKEN (HYD SYSTEM) · airframe 39,376 hrs · 31,701 cycles

PDIS 658 29-13 2122881 05JAN20 PHL CLOSE LOSS HYD FLUID ON SYS 1 FOLLOWED BY HYD SYS 1 FAILURE FOR APPOX 3-5 MINS NOTE: PILOT REPORTED EVENT HAPPENED WITH-IN THE LAST 5 MIN OF OPERATION. GEAR DOWN. FACT 05JAN20 15:14 PHL INSPECTED AND FOUND LH MLG OTBD HYD HOSE ON ACUATOR BROKEN. R&R HYD HOSE PN# 145-70264-401 AS REQUIRED. SERVICED #1 HYD TO FULL AS REQUIRED. PERFORMED LH SWING IAW EMB 145 AMM 32-34-00. OPS CHECK / LEAK CHECKGOOD AT THIS TIME. OK FOR SERVICE.

Part: PUMP — LEAKING (HYD SYSTEM) · airframe 39,376 hrs · 31,701 cycles

PDIS 658 29-13 2122873 04JAN20 PHL CLOSE HYDRAULIC FLUID LOSS ON SYSTEM 1 FOLLOWED BY HYDRAULIC SYSTEM 1 FAILURE. ( CAPTAIN SAID HYD LOSS WAS GRADUAL, BY THE TIME IT REACHED NEAR AMBER RANGE THEY DECIDED TO DIVERT TO PHL. BY THE TIME THEY LANDED THE SYSTEM WAS EMPTY.) FACT 04JAN20 23:35 PHL R&R ELECTRIC MOTOR DRIVEN PUMP & HYD LINE IAW AMM 29-10-04. OPS CHECK GOOD. OK FOR SERVICE. R&R ENGINE DRIVEN PUMP IAW AMM 29-10-03. OPS CHECK GOOD. OK FORSERVICE.

Part: LINE — LEAKING (HYD SYSTEM) · airframe 39,376 hrs · 34,701 cycles

NDIS 658 29-13 0008050 04JAN20 PHL CLOSE HYDRAULIC FLUID LOSS ON SYSTEM 1 FOLLOWED BY HYDRAULIC SYSTEM 1 FAILURE. (CAPTAIN SAID HYD LOSS WAS GRADUAL, BY THE TIME IT REACHED NEAR AMBER RANGE THEY DECIDED TO DIVERT TO PHL. BY THE TIME THEY LANDED THE SYSTEM WAS EMPTY. FACT 04JAN20 10:56 PHL R&R ELECTRIC DRIVEN MOTOR PUMP & HYDRAULIC LINE IAW AMM 29-10-04. OPS CHECK GOOD. R&R ENGINE DRIVEN PUMP IAW AMM 29-10-03. REQUIRES OPERATIONAL & LEAK TEST. LEAK CHECK GOOD. OK FOR SERVICE

Part: ANTI-ICE VALVE — MALFUNCTIONED (NR 2 ENGINE) · airframe 39,059 hrs · 34,336 cycles

PDIS 658 30-21 2087271 02NOV19 PHL ASSGN ON CLIMBOUT E2 ANTI ICE FAIL EICAS MSG. RAN QRH, MSG PERSISTED. 27720 00 AR MEL 02NOV19 21:16 PHL C30614 30-8-1 ENG ANTI-ICING VALVE CURRENTLY ON THE MEL

Part: WARNING MESSAGE — FALSE ACTIVATION (NR 2 BLEED VALVE) · airframe 38,611 hrs · 33,821 cycles

CREW CALLED WITH REJECTED TAKE-OFF, NR 2 BLEED VALVE FAILED MESSAGE. MESSAGE WENT AWAY AND CREW CONTENT WITH CONTINUING FLIGHT.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 38,488 hrs · 33,685 cycles

BLEED 2 VALVE FAIL MESSAGE DISPLAYED ON TAKEOFF. FIX: GROUND RAN AIRCRAFT WITH THE CREW IAW SRT MANUAL NO MESSAGES NOTED AT THIS TIME. CMC CLEAR,OK FOR SERVICE.

Part: STATIC INVERTER — INOPERATIVE (CABIN) · airframe 38,461 hrs · 33,653 cycles

BACK SIDE 0F EXIT SIGN ON ROOF AT ROW 12 DOES NOT ILLUMINATE WHEN EMERGENCY LIGHTS ARE TESTED. FIX: R&RD #4 EMERGENCY LIGHT STATIC INVERTER ASSY. IAW AMM 33-50-11-000/400-801-A. OK FOR SERVICE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 38,346 hrs · 33,520 cycles

MID CEILING AFT EMERGENCY LOCATOR SIGN INOP... FIX: TROUBLESHOT WIRES LEADING TO SIGN AND FOUND LOW VOLTAGE. R & R D EMERGENCY BATTERY #300 IAW AMM TASKS 33-50-04-000-801-A AND 33-50-04-400-801-A. OPS CHK GOOD

Part: SWITCH — MALFUNCTIONED (BLEED AIR SYS) · airframe 38,163 hrs · 33,300 cycles

658 36-12 1880731 23MAY19 ROA CLOSE ON T/O ROLL AT APROX 50KNOTS BLEED 1 VALVE FAIL MESSAGE DISPLAYED AND DURING ABORT NO TAKEOFF CONFIG WARNING SOUNDED MOMENTARILY AND CANCELED WITHOUT CREW INPUT. 24930 00 SMK HISTORY: FACT 23MAY19 10:52 ROA R AND R NR 1 BLEED SWITCH IAW AMM 20-13-64 OPS CHECKED NR 1 BLEED IAW AMM 36-11-02 FUNCTION CHECK SECTION NO DEFECTS NOTED AT THIS TIME OK FOR SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 38,082 hrs · 33,205 cycles

PDIS 658 21-01 1880552 08MAY19 PHL CLOSE BURNING SMELL IN GALLEY 28786 00 AR FACT 08MAY19 04:04 PHL REMOVED ACCESS PANELS 223ELW, 223UZ, 224MZ TO FOM. INSPECTED COMPARTMENTS NO FEFECTS NOTED AT THIS TIME AND REINSTALLED PANELS 223ELW, 223UZ 224MZ AS REQUIRED.

Part: WIRE — DAMAGED (GUST LOCK) · airframe 38,073 hrs · 33,195 cycles

658 27-70 0001800 05MAY19 RIC CLOSE GUST LOCK SYSTEM OPERATIONAL CHECK FAILED. GUST LOCK LEVER DOES NOT LOCK WHEN TAKING TARGET OUT FROM WOW PROX SWITCH.DISCOVERED PIN 57 , WIRE W102-13771-22, CONNECTOR DFRL 05MAY19 11:00 RIC P0838 BARE AND MAKING CONTACT AND ARCING AGAINST PIN 36. REMOVED WIRE AND PIN W102-13771-22, PIN 57 FROM CONNECTOR P0838, THEN REPINNED AND TEMRINATED PIN57, TO P0838. GUST LOCK OPERATIONAL CHECK GOOD AT THIS TIME. STILL REQUIRES AREA SAFETY CHECK. FACT 05MAY19 11:02 RIC PERFORMED GUST LOCK OPERATIONAL CHECK REF AMM 27-71-00-700-803-A. OK FOR SERVICE AT THIS TIME.

Part: RELAY — FAILED · airframe 38,073 hrs · 33,195 cycles

DISCREPANCY: RELAY K0058 FAILED INSPECTION UNDER FCD1-30-16-0276. ACTION TAKEN: R&R RELAY IAW AMM 20-13-02-0001400-801-A. OPS CHECK GOOD.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 38,070 hrs · 33,193 cycles

EMERGENCY EXIT SIGN ON CEILING PANEL AT EMERGENCY ROW IS NOT ILLUMINATED ON AFT SIDE-C/A-REMOVED AND REPLACED CEILING PANEL EXIT LOCATING AFT SIGN AT EMERGENCY ROW IAW EMB 145 AMM 33-50-15.

Part: SKIN — CORRODED (FRAMES 3-4) · airframe 38,070 hrs · 33,193 cycles

FUSELAGE INTERNAL SKIN CORRODED BETWEEN FR 3-4 AND BELOW STR 17R-C/A-RAR SKIN PANEL AT FR 3-4 STR 17R IAW EMB 145 SRM 51-40-02

Part: FRAME — CRACKED (FRM 10) · airframe 38,070 hrs · 33,193 cycles

FRAME 10 CRACKED RH SIDE BELOW COPILOT?S DV WINDOW-C/A-REMOVED AND REPLACED RH FRAME 10 IAW EMB 145 SRM 51-40-02

Part: STRINGER — CORRODED (FRAMES 3-4) · airframe 38,070 hrs · 33,193 cycles

STR 17R BTW FR 3-4 HAS CORROSION ALONG UPPER EDGE. REPAIRED STR 17R BTW FR 3-4 IAW ERS-EM-53MR-3742

Part: SKIN — DAMAGED (CARGO DOOR) · airframe 38,070 hrs · 33,193 cycles

ACCOMPLISH PERMANENT REPAIR OF BAGGAGE DOOR SKIN DENT WITH GOUGE-C/A-REPAIRED THE BAGGAGE DOOR SKIN DENT WITH GOUGE IAW ERS-EM-52DF-919 PART C, AND EMB145 SRM 52-30-01

Part: FRAME — CORRODED (FRM 65) · airframe 38,070 hrs · 33,193 cycles

SSI 53-30-48; FRAME 65 IS CORRODED AT STAINLESS GUIDE PLATE BETWEEN STRINGERS 16L-17L-C/A-REPAIRED FRAME 65 AT STAINLESS GUIDE PLATE BTW STRINGERS 16L-17L IAW ERS-EM-53MR-3741

Part: DOOR SILL — CORRODED (CARGO BAY) · airframe 38,070 hrs · 33,193 cycles

CARGO DOOR SILL IS CORRODED BEYOND REPAIR-C/A-REMOVED AND REPLACED CARGO DOOR CUTOUT LOWER SILL IAW EMB145 SRM 51-40-02

Part: SUPPORT — CORRODED (TOILET WASTE) · airframe 38,070 hrs · 33,193 cycles

TOILET WASTE VALVE SUPPORT IS CORRODED-C/A-REPAIRED TOILET WASTE VALVE SUPPORT IAW EMB145 SRM 53-31-02

Part: SKIN — CHAFED (FRAMES 67-68) · airframe 38,070 hrs · 33,193 cycles

FUSELAGE SKIN CHAFED INSIDE 424DB-C/A-REPAIRED FUSELAGE SKIN CHAFE INSIDE 424DB IAW EMB145 SRM 53-31-01

Part: SKIN — CHAFED (FRAMES 67-68) · airframe 38,070 hrs · 33,193 cycles

FUSELAGE SKIN CHAFED INSIDE 414DB-C/A-REPAIRED FUSELAGE SKIN CHAFE INSIDE 414DB IAW EMB145 SRM 53-31-01

Part: FRAME — CRACKED (FRM 66) · airframe 38,070 hrs · 33,193 cycles

FR 66 FRAME END CRACKED BETWEEN STR 17L AND 18L-C/A-REPAIRED FR 66 IAW ERS-EM-53MR-3731

Part: SHEAR TIE — CORRODED (FRAME 65) · airframe 38,070 hrs · 33,193 cycles

FRAME 65 SHEAR CLIP IS CORRODED AT THE BOTTOM NEAR CARGO DOOR SILL-C/A-REPAIRED FRAME 65 SHEAR CLIP IAW EMB145 SRM 53-31-04

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 38,070 hrs · 33,193 cycles

LH EMERGENCY PROXIMITY LIGHT #4 WIRES MISSING-C/A-REMOVED AND REPLACED LH EMERGENCY LIGHT #4 IAW EMB145 AMM 33-50-12

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 37,770 hrs · 32,933 cycles

18A FLASHLIGHT INOP. REMOVED AND REPLACED AFT FLASHLIGHT ASSY IAW MM 33-50-16. OPS CK GOOD.

Part: DISPLAY — MALFUNCTIONED (COCKPIT) · airframe 37,668 hrs · 32,822 cycles

PFD NR 2 SCREEN WENT OUT AT GATE WITH ELECTRICAL BURNING SMELL. C/A- VERFIRED SMELL ELECTRICAL BURNING COMING FROM BAD PFD PERFORMED OPS CHECK IAW AMM 34-22-00 NO SMELL NOTED. FO'S MFD DISPLAYED TRANSFERED TO FO'S PFD PER MEL 34-01 DEFERRED FOS' MFD IAW MEL 34-1 AUTH # 010573DM-B.

Part: ANTI-ICE VALVE — FAULTY (RT WING) · airframe 37,508 hrs · 32,697 cycles

PNEUMATIC A/I TEST FAIL ON GROUND. WING A/I FAIL EICAS MSG ON BOTH 1 & 2 ON MULTIPLE ATTEMPTS. C/A-T/S PER FIM TASK 30-11-00-810-805. RAR WING ANTI ICING ASSYMETRY PRESS TRANS IAW AMM 30-11-13-000-801-A & 30-11-13-400-801-A. OPC GOOD AND FOUND ACCESS PANEL 192AR OK TO CLOSE. END PERFORMED PNEUMATIC A/I TEST IN AIR GOT WG A/ICE FAIL EICAS MSG. FOUND MULTIPLE OCCURANCES OF CMC MESSAGE WING A/ICE ASYMMETRY. PERFORMED FIM TASK 30-11-00-810-805-A BLOCK DIAGRAM 002. FOUND RT WING TO FAIL WING THERMAL ANTI-ICING SYSTEM FUNCTIONAL TEST. RT WING A/I VALVE OUTLET ONLY INDICATED 9.5 PSI. (SHOULD BE 19.5 +/- 1.5). REPLACED RT WING ANTI-ICING VALVE IAW AMM TASKS 30-11-01-000-801-A & 30-11-01-400-801-A. PERFORMED FUNCTIONAL TEST AGAIN AND FOUND VALVE OUTLET PRESSURE TO HAVE INCREASED TO 11.5 PSI BUT STILL BELOW LIMITATIONS. REPLACED RT WING A/I VALVE & PICCOLO TUBE COUPLINGS OF RT WING. OPS CHECK IAW 30-00-00-700-802-A GOOD. NO FURTHER DEFECTS NOTED.

Part: CONTROL LEVER — FAILED (COCKPIT) · airframe 37,204 hrs · 32,382 cycles

DURING GEAR RETRACTION NOISE SIMILAR TO GEAR DOORS OPEN- NORMAL EICAS INDICATIONS DURING RETRACTION + EXTENSION-C/A-TROUBLESHOT IAW FIM TASK 32-32-00. REMOVED AND REPLACED LANDING GEAR CONTROL LEVER IAW AMM TASK 32-32-02. NO DISCREPANCIES FOUND OPS CHECK GOOD.

Part: LATCH — UNSECURE (FUEL DOOR) · airframe 37,066 hrs · 32,229 cycles

FUEL DOOR OPEN INDICATION ON T/O. BACK TO ORD NO OVERWEIGHT LANDING. INSP AND FOUND ONLY 1 LATCH SECURED, 5 OTHER LATCHES NOT SECURED. CLOSED ALL 6 LATCHES AS REQUIRED. NO DEFECTS NOTED.

Part: PROXIMITY SENSOR — FAILED (RT MLG) · airframe 36,330 hrs · 31,583 cycles

DURING CLIMB AND ENROUTE INTERMITTENT TO OCCASIONAL CLUNKING BANGING SOUND IN THE COCKPIT FLOOR AND FELT ON THE FLOOR. F/A ADVISED THAT SHE COULD FEEL THE SAME ON THE FLOOR BELOW HER JUMP SEAT. STEERING POWER PACK WAS SUSPECT BY FLIGHT CREW. REMOVED AND REPLACED TWO PROX SWITCHES ON RT MLG UPLOCK BOX IAW 32-61-01 OPS CHECK GOOD. PROXIMITY SENSOR P/N 80-057-01 S/N 43746

Part: CONTROLLER — FAILED (CABIN PRESSURE) · airframe 36,225 hrs · 31,479 cycles

LOST PRESSURIZATION DURING DESCENT, CABIN ALTITUDE 8000 FT AND INCREASING DESCENDED AS SOON AS POSSIBLE TO 10,000 FT, CABIN ALTITUDE REACHED 11,000 FT. CABIN REMAINED UNPRESSURIZED FOR REMAINDER OF FLIGHT. OXYGEN MASKS DID NOT DEPLOY. REMOVED AND REPLACED THE DIGITAL PRESSURIZATION CONTROLER. OPS CHECKED GOOD IAW AMM 21-31-00. NO DEFECTS NOTED IN AUTO OR MANUAL.

Part: DISPLAY — FAILED (FIRST OFFICER'S) · airframe 35,886 hrs · 31,136 cycles

FIRST OFFICER PFD WENT BLACK THEN NOTICED A STRONG ELECTRICAL BURNING ODOR IN COCKPIT. VERIFIED ODOR FAULT, REMOVED AND REPLACED THE FIRST OFFICER`S PFD IAW AMM 34-22-01. OPS CHECKED OK IAW AMM 34-22-00.

Part: ENGINE — ODOR (RIGHT) · airframe 35,201 hrs · 30,575 cycles

LAV SMOKE WARNING WITH HAZE IN THE CABIN WHILE IN THE CLIMB WITH FULL POWER. PERFORMED ETN-EM-72-034 AND RR FIM 72-00-00-810-814 STEPS 1 THROUGH 9 FOUND OIL SMELL SOURCE TO BE RH ENGINE.

Part: UNKNOWN — ODOR (LAVATORY) · airframe 35,201 hrs · 30,574 cycles

AFTER TAKEOFF FLIGHT ATTN ADVISED CABIN FILLING WITH SMOKE LAV SMOKE WARNING ON EICAS. CONFIRMED APU IS NOT THE SOURCE OF THE ODOR. OPC APU IAW EMB AMM 49-13-00. OPC GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,996 hrs · 30,395 cycles

AFT AISLE EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY LIGHT IAW AMM 33-50-08. OPS CHECKED GOOD.

Part: UNKNOWN — MALFUNCTIONED (COCKPIT) · airframe 34,702 hrs · 30,122 cycles

INBD TO DTW DUE MTX. LOST SBY IND ISIS OUT OF ORDER DECLARED EMERGENCY. RESET POWER & CHECKED ELECTRICAL CONNECTIONS BEHIND ISIS REF AMM 34-01-01 NO DEFECTS NOTED & REF FIM TASK 34-01-00-810-801-A FOUND TO BE IN A TRANSITORY CONDITION.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 34,109 hrs · 29,579 cycles

LAST 3 FLOOR EMERGENCY LIGHT STRIPS INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY LIGHT INVERTER IAW AMM 33-50-11, OP CHECKED GOOD

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT) · airframe 33,550 hrs · 29,120 cycles

FIRST SET OF AISLE FLOOR LIGHTS AND LOWER SERVICE DOOR LIGHT INOPERATIVE. REMOVED AND REPLACED NR 2 INVERTER IAW AMM 33-50-11. OPS CHECKED GOOD.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 33,072 hrs · 28,695 cycles

DURING MBV INSPECTION, QA FOUND THE GALLEY RT OMEGA BEAM CORRODED AT FR 19. AIRCRAFT WAS REMOVED FROM SERVICE FOR MBV INSPECTION AND WILL BE RETURNED TO SERVICE AFTER MBV INSPECTION. PERFORMED PERMANENT REPAIR TO GALLEY RT OMEGA BEAM AT FR 19 IAW ERS-EM-53MR-2503. AIRCRAFT WILL BE RETURNED TO SERVICE AFTER MBV INSPECTION.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 33,072 hrs · 28,695 cycles

DURING MBV INSPECTION, QA FOUND THE SERVICE DOOR CENTER SILL CORRODED. AIRCRAFT WAS REMOVED FROM SERVICE FOR MBV INSPECTION AND WILL BE RETURNED TO SERVICE AFTER MBV INSPECTION. PERFORMED PERMANENT REPAIR ON SERVICE DOOR CENTER SILL IAW ERS-EM-53MR-2501. AIRCRAFT WILL BE RETURNED TO SERVICE AFTER MBV INSPECTION.

Part: BOLT — SHEARED (LT AILERON) · airframe 33,072 hrs · 28,695 cycles

DURING REMOVAL OF LT LOWER AILERON SHROUD FOR MBV INSPECTION, FOUND LT AILERON DAMPER BOLT BROKEN AT AILERON FITTING. AIRCRAFT WILL BE REMOVED FROM SERVICE FOR MBV INSPECTION. INSTALLED AILERON DAMPER BOLT AT AILERON FITTING IAW AMM 27-12-03. AIRCRAFT WILL BE RETURNED TO SERVICE AFTER MBV INSPECTION.

Part: FITTING — GOUGED (LT AILERON) · airframe 33,072 hrs · 28,695 cycles

DURING MBV INSPECTION, QA FOUND LT AILERON DAMPENER FITTING GOUGED. AIRCRAFT WAS REMOVED FROM SERVICE FOR MBV INSPECTION AND WILL BE RETURNED TO SERVICE AFTER MBV INSPECTION. REMOVED AND REPLACED LT AILERON DAMPENER FITTING IAW EO EM-27MR-112. AIRCRAFT WILL BE RETURNED TO SERVICE AFTER MBV INSPECTION.

Part: SUPPORT — BENT (RT AILERON) · airframe 33,072 hrs · 28,695 cycles

DURING MBV INSPECTION, QA FOUND RT AILERON PCA FITTING INBOARD LUG BENT. AIRCRAFT WAS REMOVED FROM SERVICE FOR MBV INSPECTION AND WILL BE RETURNED TO SERVICE AFTER MBV INSPECTION. REMOVED AND REPLACED RT AILERON PCA FITTING IAW EO EM-27MR-112. AIRCRAFT WILL BE RETURNED TO SERVICE AFTER MBV INSPECTION.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT) · airframe 32,896 hrs · 28,516 cycles

FOUND AFT GALLEY EMERGENCY LIGHT INOPERATIVE DURING PS-2 INSPECTION. REMOVED AND REPLACED THE NR 3 INVERTER IAW AMM 33-50-11. OPS CHECKED GOOD.

Part: PRESSURE SWITCH — INOPERATIVE (RUDDER) · airframe 32,576 hrs · 28,201 cycles

RUDDER SYSTEM 1 AND 2 INOPERATIVE DURING FLIGHT. RAN CHECKLIST, AND PERFORMED EMERGENCY LANDING. FOLLOWED FIM 27-22-00-810-804-A FOR RUDDER SYSTEMS 1-2. REMOVED AND REPLACED THE NR 2 RUDDER PRESSURE SWITCH IAW AMM 27-23-04. OPS CHECKED GOOD

Part: CRADLE — BROKEN (FLASHLIGHT) · airframe 32,336 hrs · 28,023 cycles

FA FLASHLIGHT HOLDER IS BROKEN AND FLASHLIGHT DOES NOT STAY IN BRACKET. R & R F/A FLASHLIGHT/FLASHLIGHT ASSY IAW AMM 33-50-16. OPS CHECK GOOD.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 31,408 hrs · 27,158 cycles

STRONG SOLVENT SMELL ON FLIGHT DECK. SOLVENT ODOR INCREASED SUBSTANTIALLY WHEN ACFT CONFIGURED FOR GATE DEPARTURE. CLEANED COCKPIT PEDESTAL AREA, VENTED COCKPIT BY OPENED SIDE WINDOW FOR A COUPLE OF MINUTES. PERFORMED OPERATIONAL CHECK OF RECIRCULATING SYS & AT THIS TIME NO STRONG SOLVENT SMELL NOTED.

Part: BATTERY — DISCHARGED (CABIN) · airframe 31,092 hrs · 26,867 cycles

DURING PS 2 CHECK FOUND EMER FLOOR LIGHTS AT GALLEY & GALLEY WALL EXIT LIGHT INOPERATIVE. R & R NR 2 EMER BATTERY IAW AMM 33-50-04. OPERATIONS CHECKED GOOD. BATTERY CHARGER ASSEMBLY PN 11-0049 & SN 15060.

Part: LIGHT — INOPERATIVE (OVERWING EXIT) · airframe 30,557 hrs · 26,377 cycles

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

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 29,956 hrs · 25,815 cycles

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

Part: CONTROL UNIT — FAULTY (HORIZ STAB) · airframe 29,796 hrs · 25,693 cycles

CLIMBING THROUGH 7,000 FT, PITCH TRIM INDICATION HAD DASHES & POINTER DISAPPEARED. AFTER INDICATIONS RETURNED NORMALLY. THE AUTO PILOT DISCONNECTED APPROX 3 TIMES & THE PITCH TRIM DASHES REAPPEARED. OBSERVED FAULT CODE 274M0700. TROUBLE SHOT IAW FIM TASK 27-43-00-810-821-A & 27-43-00-810-820A. R & R HORIZONTAL STABILIZER CONTROL UNIT. PERFORMED HORIZONTAL STABILIZER ELECTRICAL & ELECTRONIC OPERATIONAL TEST. OPERATIONS CHECKED GOOD IAW AMM CHAPTER 27-40-01, 27-40-00, REF ITEM 2 LOG PAGE 3885849 FOR OPERATIONAL CHECK OF AUTOPILOT SYS.

Part: ACM — FAILED (AC BAY) · airframe 29,715 hrs · 25,618 cycles

FLIGHT ATTENDANT REPORTED SMOKE IN CABIN. OBSERVED & SMELLED SMOKE IN COCKPIT, SMELLED ELEC IN NATURE. FLIGHT ATTENDANT NOTICED AT ROW 15 FIRST, CONTD, DURING DESCENT TO NEAREST SUITABLE AIRPORT. SMOKE CLEARED NO OTHER INDICATIONS. NOTE FL 250 CRUISE FLIGHT NR 2 PACK OFF. FOUND NR 1 PACK ACM IMPELLER & EXHAUST TURBINE BLADES BROKEN & GRINDING AGAINST CASING. R & R ACM IAW MM 21-51-03. OPERATIONS CHECKED GOOD AT THIS TIME. NO ODOR NOTED AT THIS TIME.

Part: LIGHT — UNKNOWN (CABIN) · airframe 29,534 hrs · 25,461 cycles

EMERGENCY LIGHT ADJACENT TO 1A INOPERATIVE. INSPECTED AND FOUND NO DEFECTS NOTED. NORMAL OPS IAW AMM 33-50-00.

Part: LIGHT — INOPERATIVE (FLASHLIGHT) · airframe 28,866 hrs · 24,860 cycles

COCKPIT CAPTAINS EMER FLASHLIGHT INOPERATIVE. R & R CAPTAINS SIDE EMER FLASHLIGHT BULB. OPERATIONS CHECKED GOOD IAW CMM 25-60-11, 4.0 & 3.0.

Part: LIGHT — MALFUNCTIONED (INTERPHONE SYS) · airframe 28,732 hrs · 24,706 cycles

FORWARD FLIGHT ATTENDANT HANDSET EMERGENCY PILOT LIGHT STAYS ON. ACCOMPLISHED FUNCTION OF PAX ADDRESS & CABIN INTERPHONE SYS, NO DEFECTS NOTED. COULD NOT DUPLICATE PROBLEM IAW AMM 23-31-00.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 28,668 hrs · 24,625 cycles

FIRST OFFICER`S FLASHLIGHT INOPERATIVE. R & R FIRST OFFICER`S FLASHLIGHT IAW AMM 33-50-16.

Part: NUT PLATE — BROKEN (EXTERIOR LIGHT) · airframe 28,647 hrs · 24,602 cycles

LEFT WING FWD FUSELAGE EMER EXIT LAMP INOPERATIVE. TROUBLE SHOT FOUND INTERNAL NUTPLATES BROKEN. R & R ASSEMBLY IAW AMM 33-50-10-000-801-A & 33-50-10-400-801-A. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 28,350 hrs · 24,322 cycles

FIRST OFFICER`S FLASHLIGHT NOT CHARGING RED INDICATOR LIGHT NOT LIT IN CRADLE. REPLACED IAW AMM 33-50-16 RED CHARGE INDICATOR ILLUMINATED.

Part: WARNING MESSAGE — FALSE ACTIVATION (BLEED VALVES) · airframe 28,274 hrs · 24,237 cycles

DURING PNEUMATIC ICE PROTECTION TEST IN FLIGHT, THE FOLLOWING MESSAGE PRESENTED; NR 2 BLEED VALVE FAIL, NR 2 BLEED VALVE CLOSED, WING ANTI-ICE FAIL, NO ICE ANTI-ICE ON DIVERT. R & R RELAY IAW SMP & WM 36-11-51. OPS CHECK OF ENGINE BLEED VALVES & ANTI-ICE SYS GOOD.

Part: BLEED VALVE — FAILED (RT ENGINE) · airframe 28,265 hrs · 24,231 cycles

BLEED 2 VLV FAIL N FLIGHT, IN ICING CONDITIONS, FOLLOWED BY WING ANTI-ICE FAIL. TRANSFERRED TO NRWC 658-MIA-01753. R & R RT ENG BLEED VLV IAW AMM 36-11-05 & PERFORMED AIR BLEED SYS OPERATIONAL TEST. OPERATIONS CHECKED GOOD.

Part: ACTUATOR — MALFUNCTIONED (HORIZ STAB) · airframe 28,166 hrs · 24,146 cycles

PITCH TRIM MAIN INOPERATIVE WARNING ON EICAS ASSOCIATED WITH MAIN PITCH TRIM FAILURE. R & R HORIZONTAL STABILIZER ACTUATOR IAW AMM 27-40-02. OPERATIONS CHECKED GOOD.

Part: SKIN — CRACKED (FUSELAGE) · airframe 28,161 hrs · 24,142 cycles

LEFT AFT FUSELAGE FRAME 75 STRINGER 2L UPPER AREA, SKIN CRACKED AT FASTENER. ACCOMPLISHED REPAIR IAW ERS-EM-53MR-755.

Part: SKIN — CRACKED (FUSELAGE) · airframe 28,161 hrs · 24,142 cycles

EXTERNAL RT FUSELAGE SKIN CRACKED AROUND TWO RIVETS ON FRAME 79. ACCOMPLISHED REPAIR ON SKIN CRACK ON IAW ERS-EM-5300-736 & CPM'S 51-21-01, 51-21-05, 51-21-06 & ETN'S GN-51-016 R5 01, EM-51-091 R3 & EM-51-075.

Part: SKIN — CRACKED (FUSELAGE) · airframe 28,161 hrs · 24,142 cycles

EXTERNAL LT FUSELAGE SKIN CRACKED AROUND THREE RIVETS ON FRAME 79. ACCOMPLISHED REPAIR IAW ERS-EM-5300-737 & CPM 51-21-01, 51-21-05, 51-21-06 & ETN GN-51-016 R5 01, EM-51-091 R3 & EM-51-075.

Part: SKIN — CRACKED (FUSELAGE) · airframe 28,161 hrs · 24,142 cycles

EXTERNAL RT FUSELAGE SKIN CRACKED AROUND TWO RIVETS ON FRAME 78. ACCOMPLISHED REPAIR IAW ERS-EM-5300-736 & CPM 51-21-01, 51-21-05, 51-21-06 & ETN GN-51-016 R5 01, EM-51-091 R3 & EM-51-075.

Part: SKIN — CRACKED (FUSELAGE) · airframe 28,161 hrs · 24,142 cycles

EXTERNAL LT FUSELAGE SKIN CRACKED AROUND THREE RIVETS ON FRAME 77. EXTERNAL LT FUSELAGE SKIN INSTALLED BUSHING TWO RIVETS ON FRAME 77 IAW ERS-EM-5300-737. SEE TURNOVER FOR DETAILS.

Part: RELIEF VALVE — FAILED (BRAKE SYSTEM) · airframe 28,161 hrs · 24,142 cycles

EMERGENCY PARKING BRAKE SYS THERMAL RELIEF VLV FAILED FUNCTIONAL CHECK. R & R EMER PARKING BRAKE SYS THERMAL RELIEF VLV IAW AMM 32-44-06, CHECKED GOOD.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 28,161 hrs · 24,142 cycles

L ANGLE SUPPORT UNDER FRAME 20 CROSS MEMBER CORRODED. R & R L ANGLE UNDER FRAME 20 CROSS MEMBER IAW SRM 51-40-02 & 51-20-03. SEE NRWC E407859 FOR CROSSBEAM INSTALLATION. SEE TURNOVER FOR DETAILS.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 28,161 hrs · 24,142 cycles

GALLEY FWD DIGITAL CORRODED AT PREVIOUS BLEND AT RT PULLEY SUPPORT. PERFORMED REPAIR IAW ERS-EM-5300-747. SEE TASK & WIPS FOR DETAILS.

Part: SKIN — CRACKED (FUSELAGE) · airframe 28,161 hrs · 24,142 cycles

EXTERNAL RT FUSELAGE SKIN CRACKED AROUND TWO RIVETS ON FRAME 77. ACCOMPLISHED REPAIR IAW ERS-EM-5300-736 & CPM'S 51-21-01, 51-21-05, 51-21-06 & ETN'S GN-51-016 R5 01, EM-51-091 R3 & EM-51-075.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 28,161 hrs · 24,142 cycles

MAIN DOOR EMER LIGHT OUT. R & R NR 1 EMER POWER SUPPLY & BATTERY IAW AMM 33-50-04. LIGHT OPERATIONS CHECKED GOOD.

Part: SKIN — CRACKED (FUSELAGE) · airframe 28,161 hrs · 24,142 cycles

EXTERNAL LT FUSELAGE SKIN CRACKED AROUND THREE RIVETS ON FRAME 78. ACCOMPLISHED REPAIR IAW ERS-EM-5300-737 & CPM 51-21-01, 51-21-05, 51-21-06 & ETN GN-51-016 R5 01 & EM-51-091 R3.

Part: ACM — FAILED (AC BAY) · airframe 28,089 hrs · 24,086 cycles

CLIMBING THROUGH FL 190 SMOKE & FUMES IN THE CABIN & COCKPIT. LOUD NOISE HEARD AROUND ROW 10 & 11 ON LT SIDE OF ACFT. WHEN ISOLATING THE PROBLEM SMOKE & FUMES SEEMED TO GO AWAY WHEN DESELECTING PACK 1. NUMBER 1 PACK VERIFIED INOPERATIVE & DEFERRED IAW MEL 21-29. R & R NR 1 AIR CYCLE MACHINE IAW MM 21-51-03. OPERATIONS CHECKED GOOD IAW MM 21-51-00. MEL RESTORED.

Part: BATTERY PACK — DISCHARGED (FLASHLIGHT) · airframe 27,680 hrs · 23,738 cycles

FLASHLIGHT OVER CAPTAINS SEAT IS NOT WORKING. REPLACED BATTERY PACK IAW CMM 25-60-11. OPERATIONS CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 27,340 hrs · 23,450 cycles

CABIN FLASHLIGHT STOPPED FLASHING AT 18B. R & R RECHARGEABLE FLASHLIGHT AT 18B IAW AMM 33-51-01, OPERATIONS CHECKED NORMALLY.

Part: HOLDER — BROKEN (FLASHLIGHT) · airframe 26,535 hrs · 22,761 cycles

CAPTAIN'S FLASHLIGHT HOLDER BROKEN. R & R CAPTAIN'S FLASHLIGHT HOLDER IAW AMM 33-50-16. OPERATIONS CHECKED GOOD.

Part: INVERTER — UNSERVICEABLE (EMERGENCY LIGHTS) · airframe 25,619 hrs · 22,059 cycles

RT UPPER EMERGENCY EXIT SIGN AT ROW 12 INOPERATIVE. R & R EMERGENCY LIGHT NR 5 INVERTER IAW MM 33-50-11. OPS CHECKED GOOD.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 25,320 hrs · 21,794 cycles

RT OVERWING EMERGENCY LIGHT INOPERATIVE. REPLACED NR 4 EPSU IAW AMM 33-50-04, OPS CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (AFT CABIN) · airframe 25,050 hrs · 21,569 cycles

DURING B INSPECTION FOUND THE AFT CABIN FLASHLIGHT INOPERATIVE. ACFT REMOVED FROM SERVICE. R & R THE AFT CABIN FLASHLIGHT IN REF WITH 33-50-16-000-801-A AND 33-50-16-400-801-A. OPS CHECKED GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: ACTUATOR — MALFUNCTIONED (HORIZ STAB) · airframe 24,243 hrs · 20,921 cycles

ON FLIGHT 3373 DURING CRUISE FLIGHT AT 29000 FT GOT "PTRIM BACKUP INOP" WARNING ON EICAS. COMPLIED WITH CHECKLIST "TRANSFERRED TO NRWC 658-DFW-01173". THE AIRCRAFT WAS REMOVED FROM SERVICE. REPLACED HORIZONTAL STABILIZER ACTUATOR AS PER AMM 27-40-02. OPS CHECK GOOD AT THIS TIME. AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 24,091 hrs · 20,806 cycles

DURING MAINTENANCE INSPECTION FOUND THE EMERGENCY RIGHT UPPER EXIT SIGN EMERGENCY ROW INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE BATTERY AND CHARGER NR 3 FOR EXIT SIGN AT RIGHT EMERGENCY EXIT ROW IAW EMB AMM 33-50-04. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: HOLDER — LOOSE (FLASHLIGHT) · airframe 23,992 hrs · 20,740 cycles

ON FLIGHT 3423 THE FLIGHT ATTENDANT REPORTED THE FLASHLIGHT HOLDER WAS LOOSE AND WOULD NOT HOLD FLASHLIGHT AGAINST CONTACTS. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPLACED FORWARD FLIGHT ATTENDANT FLASHLIGHT HOLDER IAW AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 23,863 hrs · 20,637 cycles

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

Part: WIRE — DAMAGED (CABIN) · airframe 23,570 hrs · 20,391 cycles

DURING MAINTENANCE INSPECTION FOUND THE EMERGENCY LIGHT ON SERVICE DOOR WORKING INTERMITTENTLY. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED WIRE AT SERVICE DOOR EMERGENCY LIGHT IAW EMB 145 SWPM 20-21-00. THE OPERATIONAL CHECK WAS GOOD IAW EMB 145 AMM 33-50-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — DAMAGED (CABIN) · airframe 23,582 hrs · 20,399 cycles

DURING MAINTENANCE INSPECTION FOUND THE NR 2 EMERGENCY LIGHT STRIP DAMAGED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 2 EMERGENCY LIGHT STRIP IAW EMB 145 AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE — BROKEN (CABIN) · airframe 23,581 hrs · 20,398 cycles

DURING B INSPECTION FOUND THE NR 1 FORWARD EMERGENCY LIGHT STRIP HAS BROKEN WIRES. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 1 FORWARD EMERGENCY LIGHT STRIPS IAW EMB 145 AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SENSOR — FAILED (OIL SYSTEM) · airframe 23,433 hrs · 20,270 cycles

ON FLIGHT 4271 THE CREW REPORTED AT FLIGHT LEVEL 370 THE NR 1 ENGINE OIL WENT FROM 10 QUARTS TO AMBER AT 1 QUART. THERE WAS NO EICAS MESSAGE NOTED. THE CREW CONTACTED MAINTENANCE AND DIVERTED TO CVG. THE CREW DECLARED AN EMERGENCY AS A PRECAUTIONARY MEASURE AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED OIL LEVEL AND LOW-LEVEL WARNING SENSOR IAW RR MM 79-35-20-000-801 AND 79-35-20-400-801. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,413 hrs · 20,252 cycles

DURING B INSPECTION FOUND THE MAIN DOOR OVERHEAD EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE MAIN DOOR OVERHEAD EMERGENCY LIGHT BULB IN REFERENCE WITH 33-26-04-000-801-A AND 33-26-04-400-801-A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETUNRED TO SERVICE.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 22,694 hrs · 19,658 cycles

DURING B INSPECTION, FOUND THE EMERGENCY FLOOR STRIP 2 AND 3 LIGHTS INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 3 EMERGENCY LIGHT INVERTER IAW AMM 33-50-11. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CONNECTOR — LOOSE (CABIN) · airframe 22,452 hrs · 19,471 cycles

ON FLIGHT 2965 THE CREW REPORTED THE EMERGENCY LIGHTING SYSTEM FLOOR PROXIMITY STRIPS AT ROWS 3A, 5A, 6A, & 7A WERE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. RE-INSTALLED ELECTRICAL CONNECTION IAW EMB 145 AMM 30-50-12. THE LIGHT CHECK WAS GOOD AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 22,158 hrs · 19,241 cycles

DURING MAINTENANCE INSPECTION, FOUND THE FORWARD CABIN EMERGENCY LIGHTS INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 2 EMERGENCY POWER SUPPLY BATTERY AND CHARGER IAW W/C 33-700-19. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,266 hrs · 18,555 cycles

DURING MAINTENANCE INSPECTION FOUND THE AFT EMERGENCY FLOOR STRIP INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY FLOOR STRIP IAW EMB 145 AMM 33-50-01. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 21,032 hrs · 18,364 cycles

DURING MAINTENANCE BASE INSPECTION FOUND LEFT EXTERIOR OVERWING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE BULB IN LEFT EXTERIOR OVERWING EMERGENCY LIGHT IAW EMB 145 AMM 33-50-10-000-801-A/33-50-10-400-801-A. OPC GOOD AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SEAL — DEFECTIVE (COCKPIT WINDOW) · airframe 20,319 hrs · 17,858 cycles

ON FLIGHT 3320 THE CREW REPORTED A LOAD SQUEAL AFTER TAKEOFF FROM THE CAPTAIN’S WINDOW SIDE. THE AIRCRAFT DID NOT PRESSURIZE PROPERLY CLIMBING THROUGH 15000 FEET. IT DID NOT PRESSURIZE AT A NORMAL RATE. THE CREW DECLARED AN EMERGENCY AND RETURNED TO GLD. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. RE-SECURED FILET SEAL ON DV WINDOW AND PRESSURIZED THE AIRCRAFT IAW EMB-145 AMM 21-31-00. THE PRESSURIZATION WAS NORMAL. THE WINDOW SEALED PROPERLY. THE OPERATIONAL PRESSURIZATION CHECK WAS NORMAL IAW EMB 145 AMM 21-31-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SUPPORT FITTING — WORN (RT AILERON) · airframe 18,792 hrs · 16,679 cycles

DURING MAINTENANCE BASE VISIT INSPECTION FOUND THE RIGHT AILERON PCA FITTING MID HAT BUSHING MIGRATED OUT OF THE AIRLERON. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED ACTUATOR SUPPORT ASSEMBLY IAW EMB 145 SRM 51-20-03 AND SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: O-RING — FAILED (BLEED AIR SYS) · airframe 18,586 hrs · 16,533 cycles

ON FLIGHT 4261 THE CREW REPORTED THAT DURING THE CLIMBOUT RECEIVED A BLEED 2 LEAK WARNING. THE CREW RAN THE CHECKLIST, AND DE-SELECTED THE BLEED AND THE WARNING WENT OUT WITHIN 3 MINUTES. THE CAPTAIN DECLARED AN EMERGENCY AND ELECTED TO RETURN TO TUL. THE AICRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED O-RINGS LOCATION 8, 7, 15 AND 25 IAW EMB-145 MM 36-11-10. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,474 hrs · 15,696 cycles

DURING MAINTENANCE BASE VISIT FOUND THE LEFT OVERWING EMERGENCY LAMP TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT OVERWING EMERGENCY LIGHT LAMP IAW EMB145 AMM TASK 33-50-10-000-801-A AND 33-50-10-400-801-A. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SKIN — CHAFED (RUDDER) · airframe 14,770 hrs · 13,410 cycles

DURING A MAINTENANCE INSPECTION THE RUDDER 1 LOWER LEFT LEADING EDGE WAS FOUND TO BE CHAFED. AIRCRAFT REMOVED FROM SERVICE. REPAIRED RUDDER IAW EO-EM-55MR-305. AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — ODOR (CABIN)

ON FLIGHT 3354 CREW REPORTED ELECTRICAL SMELL IN BACK OF CABIN. CREW DECLARED AN EMERGENCY AND LANDED IN MCI. SMELL GOT STRONGER ON THE GROUND. AC TOWED TO GATE, AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE AFT HAND HELD FLASHLIGHT. OPERATION CHECK GOOD NO SMOKE NOTED. AIRCRAFT RETURNED TO SERVICE. (A)

Part: WIRE HARNESS — DAMAGED (SEAT PSU 17A) · airframe 9,733 hrs · 8,715 cycles

ON FLIGHT 3403 CREW REPORTED SEAT BELT/NO SMOKING SIGN AT 17A IS MISSING AND SPARKS WERE COMING FROM THE WIRES WHERE THE SIGN WAS LOCATED. DEADHEAD CAPT SEPARATED THE WIRES AND THE FLYING CAPT TURNED THE SEATBELT/NO SMOKING SIGN SWITCHES OFF. AIRCRAFT REMOVED FROM SERVICE. ISSUED MEL FOR SEAT BELT SIGN, INSULATED WIRES, REPLACED SEAT BELT SIGN. MEL RESTORED. AIRCRAFT RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 10,373 hrs · 9,683 cycles

FLT 3483 SMOKE IN COCKPIT (NOT VISIBLE) ALSO DETECTED BY FLT ATTENDANT NEAR FWD CABIN AT COCKPIT DOOR. DISSIPATED WITHIN ABOUT 3 MINUTES. NO OTHER PROBLEMS NOTED. DECLARED EMERGENCY AND LANDED ASAP. NO SYSTEM OR BREAKER ABNORMALITIES NOTED. PERFORMED CABIN/COCKPIT ODOR EVENT TROUBLESHOOTING CHECKLIST AS PER ETN NR EM-72-034, ALSO PERFORMED ABNORMAL SMELL IN THE CABIN/COCKPIT TROUBLESHOOTING PROCEDURE AS PER EMB-FIM 21-20-00-810-801A, INSPECTED ALL ELECTRICAL BUSSES, RELAY, FUSES, AND W/S'S CONTROLLERS, PERFORMED ELEC SYSTEM TEST USING ALL ELECTRICAL SOURCES. ALL OPER TESTS GOOD. NO SMOKE/ODOR NOTED. PERFORMED FCF AIRCRAFT RETURNED TO SERVICE.

Part: SILL — CORRODED (SERVICE DOORWAY) · corrosion level 2 · airframe 9,840 hrs · 9,203 cycles

DURING MBV INSPECTION, THE SERVICE DOOR SILL WAS FOUND TO BE CORRODED. REPLACED SILL WITH NEW SILL IAW EMB 145 SRM 51-20-01, 51-20-03, 51-40-02, 51-40-06 AND CPM 51-21-04, 51-21-05, AND 51-21-06. AIRCRAFT RETURNED TO SERVICE.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,840 hrs · 9,203 cycles

DURING A MBV INSPECTION, THE BAGGAGE DOOR CUT OUT LOWER CENTER BEAM WAS FOUND CORRODED. REPLACED BEAM WITH NEW BEAM PN 145-25480-006 IAW EMB SRM CHAPTERS 51-40--02, 51-20-03, AND 51-40-06. AIRCRAFT RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,840 hrs · 9,203 cycles

DURING A MBV INSPECTION, THE LT OMEGA BEAM BETWEEN FRAMES 24 AND 25 WAS FOUND CORRODED. REPAIRED BEAM IAW REPAIR STATEMENT IC2007-145/06287 PARA 1 DATED SEPT 11, 2007. AIRCRAFT RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (OMEGA BEAM) · corrosion level 2 · airframe 9,840 hrs · 9,203 cycles

DURING A MBV INSPECTION, THE CENTER OMEGA BEAM BETWEEN FRAMES 24 AND 25 WAS FOUND CORRODED. REPAIRED BEAM IAW SRM CHAPTER 53-00-10 FIG 203. AIRCRAFT RETURNED TO SERVICE.

Part: INVERTER — FAILED (EMERGENCY LIGHTS) · airframe 9,731 hrs · 9,105 cycles

OVERHEAD EXIT SIGN INOPERATIVE. REMOVED AND REPLACED NR 4 LIGHT DC/AC INVERTER IAW EMB AMM 33-50-11. OPERATIONAL CHECK GOOD, AIRCRAFT RETURNED TO SERVICE.

Part: INVERTER — FAILED (EMERGENCY LIGHTS) · airframe 9,267 hrs · 8,647 cycles

REAR CEILING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED NUMBER SIX DC/AC INVERTER IAW EMB AMM 33-50-11. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FS 20)

THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. REMOVED THE CORROSION BY MAKING CUTOUT. FABRICATED A PLATE, FILLER AND TWO SHIMS. REPAIR DONE IAW EMB SRM, SRM 145/1142 REV 30, CHAPTER 53-00-10 FIG 201 SHEET 1, 51-40-02, 51-20-03, 51-40-06 AND ETN EM-53-087. (M)