N662EH

Part: ENGINE — HUNG START (NR 2) · airframe 48,180 hrs · 44,016 cycles

HUNG START DURING E2 START AT 31.5% N2, REJECTED START AND FUEL SMELL WAS EVIDENT FACT 17JUN25 13:44 CLT STARTED E2 ON BOTH FADEC CHANNELS. BOTH STARTS NORMAL AND NO FUEL SMELL PRESENT. OPS CHECK GOOD. OK FOR SERVICE.

Part: PIN — OUT OF POSITION (ZONE 200) · airframe 48,008 hrs · 43,822 cycles

EMERGENCY LIGHTS COMING ON UNCOMMANDED IN ARM POSITION FACT 21MAY25 15:21 SBY DURING TROUBLE-SHOOTING FOUND PIN #13 AT P8012 PUSHED BACK IN CONNECTOR. RESEATED AND LOCKED PIN 13 IN LOCATION. EMERGENCY LIGHTS SYSTEM OPS CHECKS GOOD IAW W/C 33-70-17, AT THIS TIME.

Part: CONTROL PANEL — ABNORMAL (ZONE 200) · airframe 47,999 hrs · 43,811 cycles

EMERGENCY LIGHT INTERMITEN ON AND OFF IN FLIGHT. REMOVED AND REPLACED ATTD CONTROL PANEL ASSY IAW AMM 25-27-09 OPS CHECK GOOD.P/N ON CONTROL PANEL 1013629 NSN P/N OFF CONTROL PANEL 1013629 NSN

Part: CHARGER — INOPERATIVE (ZONE 200)

WITH EMERGENCY LIGHTS IN ARM, AFTER CLOSING PAX DOOR RECEIVED EMERGENCY LIGHTS NOT ARMED ON EICAS, THEN MESSAGE EXTINGUISHED AND EMERGENCY LIGHTS CAME ON. RAR #1, 2, 3 AND 4 EMER LTS BATTERY CHARGERS IAW AMM 33-50-04. #1, 2, 3 PN:11-0049. #1 TAT:4350.6 TAC:4994, #2 TAT:8328.3 TAC:9490, #3 TAT:40333.9 TAC:36714 TIME SINCE OVERHAUL: 8341.5, TIME FOR #4 BELOW.

Part: MODULE — ABNORMAL (ZONE 200) · airframe 47,973 hrs · 43,777 cycles

IN FLIGHT EMERGENCY LIGHTS COME ON IN ARM POSITION. FACT 12MAY25 23:43 PHL R&R MODULE ASSY IRW 20-13-10. OPS CHECK GOOD, A/C OK FOR SERVICE AT THIS TIME

Part: CONTROL PANEL — FAULTED (ZONE 200) · airframe 47,945 hrs · 43,739 cycles

EMERGENCY LIGHTS ON CONTINUOUSLY IN ARM POSITION. R&R'D EMERGENCY LIGHTS OVERHEAD LIGHTS PANEL IAW EMB AMM 20-13-10. OPS CHECK GOOD IAW EMB AMM 33-50-00-700-801-A.

Part: BATTERY — FAULTED (ZONE 200)

AFT CABIN EMERGENCY LIGHTS WILL NOT REMAIN OFF WITH SWITCH IN ARMED POSITION. FACT 20APR25 19:13 CLT FOUND FA EMERGENCY LIGHTS ON. REPLACED EMERGENCY LIGHT BATTERY PACKS 1,2,3, AND 4. IAW AMM 33-50-04-400-302-A. OPS CHECK GOOD

Part: CONTROL MODULE — FAULTED (ZONE 200)

EMERGENCY LIGHTS ON IN ARM POSITION FACT 18MAR25 18:04 CLT R&R'D CONTROL MODULE IAW AMM 33-21-01. OP CHECK GOOD AT THIS TIME. A/C OK FOR SERVICE

Part: TEST PANEL — FAULTED (ZONE 200)

EMERGENCY LIGHTS ON WHEN SWITCH IN ARM POSITION (NO EICAS MSGS) FACT 11MAR25 17:01 CLT R&R'D RELAY K0275. NO FIX. R&R'D EMERGENCY LIGHTS OVERHEAD PANEL LIGHTS PANEL IAW EMB AMM 20-13-10. OPS CHECK GOOD IAW EMB AMM 33-50-00-700-801-A.

Part: WARNING MESSAGE — ILLUMINATED (SERVICE DOOR) · airframe 46,761 hrs · 42,373 cycles

IRREGULARITY REPORTED BY CREW: A SERVICE DOOR WAS REPORTED BY CREW INTERMITTENTLY SHOWED OPEN AND THEY REJECTED TAKE OFF, THEY CALLED MOCC AND REFERRED HIM TO THE MEL 52-3-1 IT WAS A REGULAR OCCURRANCE WITH THIS AIRCRAFT, READ THRU THE MEL BUT THEN WANTED A GUARANTEE THAT THE DOOR WOULD NOT OPEN IN FLIGHT, TOLD HIM THE DOOR WAS VERIFIED CLOSED AND LATCHED AND REF THE PIC IN APP #1 52-3-1, HE WAS GOOD TO GO, BUT THAT IF IT CAME BACK IN FLT HE WOULD HAVE THE NUISANCE MSG. HE AGAIN WANTED MY GUARANTEE THAT HE DOOR WOULDN'T OPEN.

Part: LIGHT — MALFUNCTIONED (ZONE 200)

SERVICE DOOR EXIT LIGHT AND EXIT LIGHT AT F/A SEAT COME ON SPORADICALLY AND STAYS ON TILL LANDING.

Part: LIGHT — MALFUNCTIONED (ZONE 200) · airframe 46,636 hrs · 42,232 cycles

FLIGHT DECK AND F/A EMERGENCY LIGHT CAME ON COMMANDED DURING PUSHBACK WITH EMERGENCY LIGHT SWITCH IN ARMED POSITION.

Part: RELAY — MALFUNCTIONED (ZONE 200) · airframe 46,617 hrs · 42,208 cycles

CABIN EMERGENCY LIGHT UNCOMMANDLY CYCLED ON/OFF. FACT 20AUG24 13:09 REMOVED AND REPLACED FA CONTROL PANEL IAW AMM 25-27-09 OPS CHECK GOOD AC OK FOR SERVICE AT THIS TIME. NDIS 662 33-50 0013480 21AUG24 MDT FOLLOW UP ITEM AT THE NEXT RON INSPECT THE CABIN EMERGECY LIGHT SYSTEM DUE TO RECENT HISTORY OF CABIN EMER LIGHTS FLICKERING ON AND OFF INTERMEITTENTLY. NOTE ANY DEFECTS AND REPAIR AS NECESSARY. IF NO DEFECTS FOUND. REPLACED RELAY K0275 AS PRECAUTION. FACT 21AUG24 08:44 MDT PERFORMED INSPECTION OF EMERGENCY LIGHTS. FOUND NO DEFECTS NOTED. R&RD RELAY K0275 IRT AMM 20-13-02. PDIS 662 33-50 3138821 21AUG24 ORD CLOSE CABIN EMERGENCY LIGHTS FLICKERING ON AND OFF IN FLT (EMERGENCY LIGHT SWITCH IN ARM POSITION) FACT 21AUG24 19:34 ORD PERFORMED ELECTRICAL RESET & EMERGENCY LIGHT OPS CHECK PER AMM 33-50-00-700-801-A ALL CHECK GOOD AT THIS TIME..

Part: CONTROL PANEL — FAULTED (EMERGENCY LIGHTS) · airframe 46,526 hrs · 42,108 cycles

EMERGENCY LIGHTS CAME ON INTERMITTENTLY IN FLIGHT AND ON GROUND WHEN SELECTED TO ARM. R & R EMERGENCY LIGHTS PANEL IRW AMM 20-13-10 PERFORMED OPS CHECK IAW AMM 33-50-00. OPS CHECK GOOD OK FOR SERVICE AT THIS TIME.

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 46,454 hrs · 41,019 cycles

53-2315 SHEAR CLIP CRACKED ON RHSIDE OF BULHEAD 80 BTWSTR5-7R. RAR SHEAR CLIP IAW SRM 51-40-02

Part: BRACKET — CRACKED (ZONE 300) · airframe 46,454 hrs · 41,019 cycles

55-2317 TOP OF VTR STAB AFT OF SPAR3, BRACKET FOR 321BL IS CRACKED. RAR BRACKET IAW SRM51-40-02

Part: FRAME — CRACKED (ZONE 200) · airframe 46,454 hrs · 43,019 cycles

53-2326 LH COCKPIT OVERHEAD FRAME CRACKED. REAIRED IAW EO1-53-24-0392

Part: SKIN — CRACKED (ZONE 300) · airframe 46,454 hrs · 42,019 cycles

55-2318 VERTICAL STAB LH SKIN CRACKED ON UPPER PROFILE. R & R PROFILE IAW SRM 51-40-02

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 46,454 hrs · 41,019 cycles

53-2188 CF1, SHEAR CLIP CRACKED ST FR15 BTW STR15-16R. RAR SHEAR CLIP IAW SRM 51-40-02

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 46,454 hrs · 42,019 cycles

53-2190 SHEAR CLIP CRACKED AT FR16 BTW STR15-16R. RAR SHEAR CLIP IAW SRM 51-40-02

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 46,454 hrs · 42,019 cycles

53-2121 REAR FUSE I, SHEAR CLIP CRACKED AT FR72 BTW STR16-17L. RAR SHEAR CLIP IAW SRM 51-40-02

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 46,454 hrs · 42,019 cycles

53-2124 REAR FUSE I, SHEAR CLIP CRACKED AT FR73 STR8-10L. RAR SHEAR CLIP IAW SRM 51-40-02

Part: SKIN — DAMAGED (FUSELAGE) · airframe 46,454 hrs · 42,019 cycles

71-2123 PROFILE DAMAGED ABOVE OF AIR STATER VALVE ACCESS DOOR BTWEEN XN3167.5 AND XN2905.0. RAR PROFILE IAW SRM 51-40-02

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 46,454 hrs · 42,019 cycles

53-2120 REAR FUSE I, SHEAR CLIP CRACKED AT FR71 BTW STR17-18L. RAR SHEAR CLIP IAW SRM 51-40-02

Part: SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 46,454 hrs · 42,019 cycles

53-2119 REAR FUSE I, LH SILL CORRODED BTW FR61-65. RAR SILL IAW SRM 51-40-02

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 46,454 hrs · 42,019 cycles

53-2122 REAR FUSE I, SHEAR CLIP CRACKED AT FR73 STR 16-17L. RAR SHEAR CLIP IAW SRM 51-40-02

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 46,454 hrs · 42,019 cycles

53-2110 REAR FUSEI, SHEAR CLIP CRACKED AT FR67 STR6-7L. RAR SHEAR CLIP IAW SRM 51-40-02

Part: NONE — NONE (NONE) · airframe 46,454 hrs · 42,019 cycles

53-2091 REAR FUSE I, UNRECORDED PATCH AT FR67 STR17-18R. RAR PATCH IAW EO1-53-24-0370

Part: ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,454 hrs · 42,019 cycles

53-2081 CORROSION ON L-SHAPED ANGLE LWR SECTION ON CARGO DOOR SURROUND AT FR68. REPAIRED IAW EO1-53-24-0371

Part: ANGLE — CRACKED (ZONE 200) · airframe 46,454 hrs · 42,019 cycles

53-2072 CF3, LH UNDERFLOOR ANGLE AT BTW FR46-47 IS CRACKED. R & R ANGLE IAW SRM 51-40-02

Part: SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 46,454 hrs · 42,019 cycles

53-2069 CF3, RH SILL CORRODED BTW FR40-41. RAR SILL IAW SRM 51-40-02.

Part: GUSSET — CORRODED (ZONE 200) · corrosion level 2 · airframe 46,454 hrs · 42,019 cycles

53-2074 CF3, RHGUSSET CORRODED BTW FR47-50. RAR GUSSET IAW SRM 51-40-02

Part: DOOR SILL — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,454 hrs · 42,019 cycles

53-2079 CARGO DOOR SILL CORRODED. R & R SILL IAW SRM 51-40-02

Part: ANGLE — CORRODED (ZONE 800) · corrosion level 2 · airframe 46,454 hrs · 42,019 cycles

53-2080 CORGO DOOR STRUCTURE L-SHAPE ANGLE LWR SECTION CORRODED. REPAIRED IAW EO1-53-24-0366

Part: SUPPORT — CRACKED (ZONE 100) · airframe 46,454 hrs · 42,019 cycles

53-2084 REARFUSE I, BAGAGE DOOR MECHANISM SUPPORT CRACKED AT FR61-62 BTW4-5R. RAR IAW SRM51-40-02

Part: SUPPORT — CRACKED (ZONE 100) · airframe 46,454 hrs · 42,019 cycles

53-2085 REAR FUSE I, UPPER AND LOWER SUPPORT FOR CARGO DOOR MECHANISM IS CRACKED AT FR68 STR4-5R. RAR UPPER AND LOWER SUPPORT IAW SRM 51-40-02

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 46,454 hrs · 42,019 cycles

53-2052 CTR FUSEII, LH OMEGA BEAM CRACKED AT FR30. RPERAIRED IAW EO1-53-24-0367

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 46,454 hrs · 41,019 cycles

53-2063 CF3, RH OMEGA BEAM IB ANGLE CRACKED AT FR47-48. RAR ANGLE IAW STR 51-40-02.

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 46,454 hrs · 41,019 cycles

53-2064 CF3, RH OMEGA BEAM OB ANGLE CRACKED AT FR47-48. RAR ANGLE IAW SRM 51-40-02

Part: SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 46,454 hrs · 41,019 cycles

53-2065 CF3, RH SILL CORRODED BTW FR40-47. RAR SILL IAW SRM 51-40-02

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 46,454 hrs · 41,019 cycles

53-2057 CTR FUE II, SHEAR CLIP CRACKED AT FR26 BTW STR15-16R. RAR SHEAR CLIP IAW SRM 51-40-02

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 46,454 hrs · 41,019 cycles

53-2054 CTR FUSE II, SHEAR CLIP CRACKED AT FR24 STR16-17R. RAR SHEAR CLIP IAW SRM 51-40-02

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 46,454 hrs · 41,019 cycles

53-2053 CTR FUSE II, CTR OMEGA BEAM CRACKED AT FR33. REPAIRED IAW EO1-53-24-0368

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 46,454 hrs · 41,019 cycles

53-2055 CTR FUSE II, SHEAR CLIP CRACKED AT FR24 STR15-16R, RAR SHEAR CLIP IAW SRM 51-40-02

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 46,454 hrs · 41,019 cycles

53-2051 CTR FUSE II, LH UNDERFLOOR OMEGA BEAM CRACKED AT FR24-27. RAR OMEGA BEAM IAW SRM 51-40-02

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 46,454 hrs · 41,019 cycles

53-2056 CTR FUSE II, SHEAR CLIP CRACKED AT FR25 STR15-16R. RAR SHEAR CLIP IAW SRM 51-40-02

Part: STRUCTURE — CRACKED (ZONE 200) · airframe 46,454 hrs · 42,019 cycles

53-2025 RH REAR FUSE II, CRACK AROUND 8 RIVETS BTW FR77-80 STR3-7R. REPAIRED IAW EO1-53-24-0364

Part: STRUCTURE — CRACKED (ZONE 200) · airframe 46,454 hrs · 42,019 cycles

53-2024 LH REAR FUSE II, CRACK SUSPECTED AROUND 9 RIVETS BTW FR77-80 STR3-7L. REPAIRED IAW EO 1-53-24-0362.

Part: CONTROL UNIT — FAULTED (SPOILERS) · airframe 46,202 hrs · 41,726 cycles

SPOILER WARNING MSG DURING T/O ROLL. REJECTED TO AT 90 KTS FACT 08APR24 13:22 PHL R/R SCU IAW AMM 27-63-02 OPS CHECK GOOD FDR COMFIRMED ISSUE OK FOR SERVICE

Part: INVERTER — FAULTED (EMERGENCY LIGHTS) · airframe 46,636 hrs · 42,232 cycles

FLIGHT DECK AND F/A EMERGENCY LIGHT CAME ON UNCOMMANDED DURING PUSHBACK WITH EMERGENCY LIGHT SWITCH IN ARMED POSITION. T/S UNCOMMANDED EMERG LIGHT ISSUE PER WM 33-50-50. R & R NR 2 INVERTER AND CLEANED PLUG P8572 IAW AMM 33-50-11. OPS CK GOOD. NO DISCREPANCIES NOTED AT THIS TIME. A/C IS OK FOR SERVICE.

Part: POWER SUPPLY — FAULTED (ZONE 200) · airframe 46,636 hrs · 42,232 cycles

SERVICE DOOR EXIT LIGHT ANS EXIT LIGHT AT F/A SEAT COME ON SPORADICALLY AND STAYS ON TILL LANDING. R&R #2 BATTERY POWER SUPPLY AND BATTERY PACK PER AMM 33-50-04. PS CHECK GOOD.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 45,000 hrs · 40,368 cycles

ELECTRICAL BURNING SMELL NOTED ON FLT DECK AND IN CABIN NEAR ROWS 2 AND 3. SMELL GOT STRONGER ON TAXI IN. SMELL STRTED TO DISIPATE AFTER APU SHITDOWN AND BLEED AIR OFF FACT 06AUG23 18:46 CHO ON INSPECTION FOUND CONTACTOR K0081 LOCATED BEHIND CAPT SEAT AND UNDER FA SEAT TO HAVE SCORCH MARKS. R+R'D IAW AMM 24-60-01-000/400-801-A. OPS CHECKED IAW AMM 24-60-00-700-802-A, OPS CHECK GOOD. ELECTRICAL POWER ON FOR 30 MIN, NO SMELL. OK FOR SERVICE. USED CHO CONTRACT MX (SIGNATURE AVIATION) TORQUE WRENCH SN-0603302913. CERT DATE-06/21/23.

Part: UNKNOWN — UNKNOWN (UNKNOWN)

BLEED 1 LEAK WITH PACK 1 SURGING & PERSISTANT PACK 1 VALVE CLOSED MESSAGE. REMOVED PANEL 191EL. FOUND BLACK FLEX DUCT AT HEAT EXCHANGER OFF. RESECURED DUCT AND OPERATED PACK, LEAK CHECK FAILED AS DUCT BLEW OFF AGAIN. REINSTALLED PANEL. BLACK DUCT ON PACK ONE HEAT EXCHANGER CONTINUES TO BLOW OFF WHEN PACK 1 IS USED AND CLAMP MIS BROKEN. 21-15-21 AIR COND PACK N650 AND ABOVE. INSTALLED NEW CLAMP @ HEAT EXCHANGER DUCT PER AMM 21-20-04-04. OPS AND LEAK CHECK GOOD PER AMM 21-00-00. CLEAR MEL 21-15-2. OK FOR SERVICE.

Part: NOT ENTERED — NOT ENTERED (NOT ENTERED) · airframe 44,267 hrs · 39,522 cycles

FA REPORTS SMOKE /ABNORMAL SMELL IN CABIN/COCKPIT AND ELECTRICAL SMELL IN AFT CABIN. SMELL WENT AWAY WHEN PACK 2 TEMP TURNED DOWN DECLARED EMERGENCY-C/A-COMPLIED WITH OPS CHECK OF #2 PACK. OPS CHECK GOOD IAW AMM 21-51-00.MEL IS RESTORED. PERFORMED FIM TASK21-20-00-810-801-A NO DEFECTS FOUND.

Part: WARNING MESSAGE — ILLUMINATED (NR 2 BLEED SYS) · airframe 43,986 hrs · 39,201 cycles

BLEED 2 LEAK HAPPENED IN THE CLIMB WE HAD ICE BEFORE THE BLEED 2 LEAK MESSAGE WE WERE IN CLEAR AIR NO ICING WHEN THE LEAK HAPPENED-C/A-DEFERRED RH BLEED SYSTEM. M PROCEDURES C/W. MEL 36-3 AUTH 110093DM-C

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 43,985 hrs · 39,200 cycles

RH OVERWING EMERGENCY LIGHT INOP-C/A-RAR RH OVERWING EMERGENCY LIGHT LAMP WITH REFERENCE TO EMB AMM 33-50-10-000-801-A AND 33-50-10-400-801-A. OPC GOOD. END.

Part: LAMP — INOPERATIVE (RH) · airframe 43,616 hrs · 38,777 cycles

RH FWD OF WING EMERGENCY LIGHT INOP-C/A-RAR RH FWD OF WING EMERGENCY LIGHT LAMP IN REFERENCE WITH EMB AMM 33-50-10-000-801-A AND 33-50-10-400-801-A. NO FIX. RAR RH FWD OF WING EMERGENCY LIGHT ASSEMBLY IAW EMB AMM 33-50-10-000-801-A AND 33-50-10-400-801-A. OPC GOOD. END.

Part: LAMP — INOPERATIVE (RH) · airframe 43,088 hrs · 38,219 cycles

RH OVERWING EMERGENCY LIGHT INOP-C/A-RAR RH OVERWING EMERGENCY LIGHT LAMP IAW EMB AMM 33-50-10-000-801-A AND 33-50-10-400-801-A. OPC GOOD. END.

Part: LAMP — INOPERATIVE (SD) · airframe 43,088 hrs · 38,219 cycles

SERVICE DOOR EMERGENCY LIGHT INOP-C/A-RAR SERVICE DOOR EMERGENCY LIGHT LAMP IAW EMB AMM 33-50-10-000-801-A AND 33-50-10-400-801-A. NO FIX. CHECKED WIRES AND VOLTAGE IAW FIM 33-50-00-810-804-A. RAR DC/AC INVERTER 3 IAW EMB AMM 33-50-11-000-801-A AND 33-50-11-400-801-A. NO FIX. SUSPECT FAULTY LAMP HOUSING. NO PARTS AT CMI.

Part: NONE — UNSERVICEABLE ([0000] [2] [) · airframe 43,072 hrs · 38,199 cycles

EMERGENCY FLOOR LIGHT STRIPS FROM SEAT 3A TO 7A AND AFT GALLEY SIGN INOP-C/A-RAR #2 EMERGENCY LIGHT BATTERY AND CHARGER ASSY IAW W/C 33-700-19. OPC GOOD.

Part: NONE — NONE · airframe 42,882 hrs · 37,999 cycles

LAV SMOKE ALARM IN GALLEY GOING OFF DURING DESCENT AROUND 12,000 FA CHECKED IT OUT AND THERE WAS NO SMOKE /FIRE HORN AND LIGHT WAS GOING OFF DURING FLIGHT AND ONLY LIGHT WAS GOING ON ONCE WE PARKED AT THE GATE-C/A-PERFORMED LAVATORY SMOKE DETECTOR SYSTEM TEST IAW EMB-145 AMM 26-14-00 OPS CHECK GOOD

Part: NONE — NONE · airframe 42,876 hrs · 37,993 cycles

R/H OVERWING EMERGENCY LIGHT INOP-C/A-RAR R/H OVERWING EMER. LIGHT IAW AMM 33-50-10 OPS CHECK GOOD

Part: NONE — NONE · airframe 42,492 hrs · 37,555 cycles

RH OVERWING EMERGENCY LIGHT INOP-C/A-RAR RH OVERWING EMERGENCY LIGHT LAMP IAW EMB-145 AMM 33-50-10. OPC GOOD.

Part: NONE — NONE · airframe 42,443 hrs · 37,501 cycles

COCKPIT EMERGENCY LIGHT INOP-C/A-RAR COCKPIT EMERGENCY LIGHT BULB IAW EMB AMM 33-50-05-000-801-A AND 33-50-05-400-801-A OPC GOOD END

Part: NONE — NONE · airframe 42,420 hrs · 37,474 cycles

STUDS BROKEN ON OVERHEAD EMERGENCY EXIT SIGN-C/A-REMOVED AND REPLACED OVERHEAD EMERGENCY EXIT LOCATING SIGN IAW EMB145 33-50-15. SEE NRWC 662-ORD- 05751 FOR OPS CHECK.

Part: NONE — NONE · airframe 42,196 hrs · 37,222 cycles

#5 EMERGENCY LIGHT STRIP HAS A BROKEN WIRE.-C/A-COMPLETE:RAR LH AISLE FLOOR #5 EMERGENCY LIGHT STRIP IAW AMM 33-50-12.

Part: NONE — NONE · airframe 42,196 hrs · 37,222 cycles

RT WING RIB 21 IS CRACKED , LOCATED IN PCA COMPT-C/A-COMPLETE:REPAIRED RH WING RIB 21 IAW SRM 57-20-07-RE,

Part: NONE — NONE · airframe 42,196 hrs · 37,222 cycles

#4 EMERGENCY LIGHT STRIP HAS EXPOSED WIRING.-C/A-COMPLETE:RAR #4 LH AISLE EMERGENCY LIGHT STRIP IAW AMM 33-50-12.

Part: NONE — NONE · airframe 42,196 hrs · 37,222 cycles

W/C 33-700-19 REPLACE #1 EPSU (PN 11-0049 SN 13473) ALSO REMOVE AND REPLACE EMERGENCY LIGHTING BATTERY ASSY/ BATTERY CHARGER (PN 2013-1A SN 107233) A110 A3265-C/A-COMPLETE:W/C 33-700-19 REPLACE #1 EPSU (PN 11-0049 SN 13473) AND REMOVE AND REPLACE EMERGENCY LIGHTING BATTERY ASSY/ BATTERY CHARGER (PN 2013-1A SN 107233)C/W

Part: NONE — NONE · airframe 42,196 hrs · 37,222 cycles

#7 #8 AND #1 EMERGENCY LIGHT STRIP FLOOR EXTRUSIONS (LH) ARE DAMAGED.-C/A-COMPLETE:RAR LH AISLE FLOOR EXTRUSIONS #7 AND #8 IAW AMM 33-50-12.

Part: FLASHLIGHT — NOT SEATED (CABIN) · airframe 41,545 hrs · 36,476 cycles

EMERGENCY FLASHLIGHT ABOVE F/A SEAT WILL NOT CHARGE. (ONLY SHOWS RED LIGHT WHEN TEST BUTTON PRESSED, AFTER RE-SEATING)-C/A-RAR FLASHLIGHT ASSEMBLY ABOVE F/A SEAT IAW EMB145 AMM 33-50-16. OPC GOOD.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 41,241 hrs · 36,139 cycles

SULFUR SMELL IN COCKPIT AND FRONT HALF OF CABIN DURING TAKEOFF AND DESCENT-C/A-PERFORMED FIM TASK 21-20-00-810-801-A AND RAN ENGINES WITH CREW IAW ETN-EM-72-034. TROUBLESHOOTING LEANING TO PACK 1MALFUNCTION. SEE ITEM 2 OF AML PG# 4594727 FOR CONTINUED DISCREPANCY

Part: LIGHT — INOPERATIVE (GALLEY CEILING) · airframe 40,885 hrs · 35,758 cycles

GALLEY CEILING EMERGENCY LIGHT INOPERABLE. C/A: R & R GALLEY CEILING EMERGENCY LIGHT, IAW AMM TASK 33-50-09-000-801-A AND 33-50-09-400-801-A. OPERATIONS CHECK GOOD.

Part: HANDLE — LACK OF LUBE (PARKING BRAKE) · airframe 40,025 hrs · 34,887 cycles

ABNORMALLY DIFFICULT TO SET THE PARKING BRAKE. A LOT OF FORCE REQUIRED TO LOCK IN.-C/A-LUBRICATED EMER/PARK BRAKE HANDLE AND PERFOMED OPS CHECK IAW AMM 32-44-11 SUBTASK 720-002-A STEPS (2) THROUGH (5). OPS CHECK GOOD AT THIS TIME.

Part: NONE — NONE (NONE) · airframe 39,065 hrs · 33,989 cycles

STRONG ELECTRICAL SMELL ON THE FLIGHT DECK-C/A-VERIFIED WITH FLIGHT CREW THAT ELECTRICAL SMELL TO BE PAU EXHAST COMING INTO THE AIRCRAFT. NO DEFECTS NOTED

Part: PUMP — FAILED (HYD SYSTEM) · airframe 38,906 hrs · 33,843 cycles

AFTER ENIGE SHUT DOWN HYDRAULIC SYST 1 FAIL-C/A-REMOVED AND REPLACED HYD PUMP #1 IAW EMB 145 AMM 29-30-04 OPS CHECK GOOD

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 38,508 hrs · 33,509 cycles

DURING PS-2 FOUND EMERGENCY EXIT LOCATING SIGN INOP-C/A-REMOVED AND REPLACED # 1 INVERTER IAW 145 AMM 33-50-11 OPS CHECK GOOD NO FURTHER DEFECTS NOTED

Part: TRUNNION — CORRODED (NLG) · airframe 38,097 hrs · 33,152 cycles

NLG LEG RH UPPER HALF BEARING TRUNNION FITTING HAS EVIDENCE OF PITTING CORROSION. COMPLETED INSTALLIATIION OF RH TRUNION IAW ERS EM-53MR-2242.

Part: TRUNNION — CORRODED (NLG) · airframe 38,097 hrs · 33,152 cycles

NLG LEG LH UPPER HALF BEARING TRUNNION FITTING HAS EVIDENCE OF PITTING CORROSION.-C/A-COMPLETED INSTALIATION OF LH TRUNNION IAW ERS-EM-53MR-2242.

Part: FRAME — DAMAGED (FRM 70) · airframe 38,097 hrs · 33,152 cycles

FRAME 70 HAS ELONGATED HOLE BETWEEN STRINGER 16L AND 17L (FLOOR SUPPORT ATTACH POINT) -C/A-REPAIRED FRAME 70 IAW ERS-EM-53MR-3819

Part: FRAME — CORRODED (FR 80) · airframe 38,097 hrs · 33,152 cycles

FR80 HAS CORROSION IN THE SHUNT CONNECTION BAR CONTACT AREA-C/A-REPAIRED FR 80 SHUNT CONNECTION BAR CONTACT AREA IAW ERS-EM-53MR-3802.

Part: FRAME — GOUGED (FRM 60) · airframe 38,097 hrs · 33,152 cycles

LH FRAME 60 IS GOUGED NEAR STR 5 LH-C/A-CW WITH REPAIR TO LH FRAME 60 NEAR STR 5L IAW SRM 53-00-04 FIGURE 206.

Part: FRAME ANGLE — CORRODED (FRM 65) · airframe 38,097 hrs · 33,152 cycles

FRAME CLIP ON FRAME 65 AT CARGO DOOR SILL CORRODED. -C/A-COMPLIED WITH REPAIR IAW SRM 53-31-04.

Part: BUSHING — WORN (LT AILERON) · airframe 38,097 hrs · 33,152 cycles

LH AILERON PCA FITTING HAS WEAR MARKS IN INBD LUG FROM LOOSE BUSHINGS.-C/A-C/W EO# EM-27MR-112

Part: YOKE — CRACKED (LT ENGINE) · airframe 38,097 hrs · 33,152 cycles

LT ENGINE FORWARD LOWER YOKE, FORWARD AFT RADIUS CRACKED (ERS-EM-54MR-698) -C/A-REMOVED AND REPLACED LH ENGINE FWD LOWER YOKE, FWD FITTING IAW ERS-EM-54MR-698.

Part: DOOR SILL — CORRODED (AFT CARGO BAY) · airframe 38,097 hrs · 33,152 cycles

AFT BAGGAGE DOOR SILL IS CORRODED BETWEEN FRAMES 65 AND 68. REMOVED DAMAGED CARGO DOOR SILL AND INSTALLED SERVICEABLE SILL IAW SRM 51-40-02.

Part: DOOR SILL — DAMAGED (SERVICE DOOR) · airframe 38,097 hrs · 33,152 cycles

EM-53MR-1412 PTB FWD & AFT SERVICE DOOR SILL - REPAIR -C/A-REFERENCE NRTC E718245 FOR FWD SILL REPAIR. AND NRTC E717864 FOR THE AFT SILL REPAIR.

Part: FITTING — GOUGED (RT AILERON) · airframe 38,097 hrs · 33,152 cycles

RIGHT AILERON DAMPER FITTING IS GOUGED, LOCATED ON AILERON.-C/A-C/W EO# EM-27MR-112.

Part: FITTING — GOUGED (LT AILERON) · airframe 38,097 hrs · 33,152 cycles

LEFT AILERON DAMPER LUG GOUGED ON INNER SURFACE. C/W EO# EM-27MR-112.

Part: SKIN — CHAFED (RUDDER) · airframe 38,097 hrs · 33,152 cycles

RUDDER II R/H SKIN IS CHAFFED ON THE INTERIOR AROUND RIB 1419.0 (3RD FROM BOTTOM) TRAILING EDGE-C/A-REPAIRED RUDDER II R/H SKIN IAW ERS-EM-55MR-763

Part: LIGHT — DAMAGED (CABIN) · airframe 38,097 hrs · 33,152 cycles

RT FLOOR PROXIMITY STRIP HAS DAMAGED RT FWD PROFILE. C/A-COMPLETE: INSTALLED NEW RT FLOOR PROXIMITY SIDEWALL ASSY. IAW AMM 33-50-12.

Part: LIGHT — DAMAGED (CABIN) · airframe 38,097 hrs · 33,152 cycles

LT FLOOR PROXIMITY STRIP LIGHTS #8 STRIP LIGHTING ASSY IS DAMAGED. C/A-COMPLETE: REPLACED LIGHT STRIP IAW AMM 33-50-12.

Part: SKIN — DAMAGED (RUDDER) · airframe 38,097 hrs · 33,152 cycles

TDMI-662T5574 FOUND HOLE MID/AFT RUDDER II-ERS-EM-55DF-756 PTC-C/A-ERS-EM-55DF-756 HAS BEEN SUPERCEEDED BY ERS-EM-55MR-764 RUDDER II REPAIRED IAW ERS-EM-55MR-764 REF AML PG 4430639 ITEM 1, TDMI RESTORED

Part: OXYGEN MASK — BROKEN (COCKPIT) · airframe 37,767 hrs · 32,820 cycles

FO OXYGEN MASK BROKE IN FLIGHT DURING USEING TO RELIEVE CA FOR THE LAV.-C/A-REMOVED AND REPLACED FO'S O2 MASK OPS CHECK GOOD LEAK CHECK GOOD IAW AMM CH 35-10-10.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 37,427 hrs · 32,479 cycles

COCKPIT EMERGENCY LAMP INOP. C/A-REMOVED AND REPLACED COCKPIT EMERGENCY LAMP IAW AMM 33-50-05-000-801-A/33-50-05-400-801-A OPC GOOD.

Part: ACTUATOR — FAILED (AC BAY) · airframe 37,342 hrs · 32,385 cycles

SUPPLEMENTAL PACK NR 1 CLOSED AT 25000 FEET CAUSING THE CABIN ALT. TO GO TO RED ON THE EICAS WE FOLLOW THE CHECKLIST, STARTED WORKIN FINE. FEW MINUTES LATER CABIN ALTITUDE STARTED TO INCRESE TO RED ON EICAS. C/A-REMOVED AND REPLACED COUPLING & CLAMPS AFT OF DUAL VALVE TORQUE MOTOR IN NR 1 PACK AREA IAW AMM 21-51-00 OPS CHECK GOOD. REMOVED AND REPLACED RT LINEAR ACTUATOR IAW AMM 21-25-01. PERFORMED OPERATIONAL CHECK IAW AMM 21-25-01. INSTALLED PANEL 191EL IAW AMM 06-41-01

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,787 hrs · 31,893 cycles

GALLEY AREA EMERGENCY LIGHT INOP. C/A-REMOVED AND REPLACED GALLEY AREA EMERGENCY LIGHT LAMP IAW AMM TASK 33-50-09-000-801-A AND 33-50-09-400-801-A. OPS CHECK GOOD.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 36,593 hrs · 31,762 cycles

FIRST EMERGENCY LIGHT FLOOR STRIP AND EMERGENCY LIGHT NEXT TO LOWER SERVICE DOOR INOP.-C/A-T/S EMERGENCY LIGHTING FLOOR STRIP AND LOWER SERVICE DOOR EMERGENCY LIGHTS INOP AND FOUND NR 2 AC INVERTER BAD. REMOVED AND REPLACED NR 2 EMERGENCY LIGHT INVERTER OPS CHECK GOOD IAW AMM 33-50-11

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 35,864 hrs · 31,177 cycles

LEFT OVERWING EMERGENCY LIGHT WAS INOPERATIVE. REMOVED AND REPLACED THE BULB IAW AMM 33-50-07. OPS CHECKED GOOD.

Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE) · airframe 35,127 hrs · 30,456 cycles

CABIN ALTITUDE WARNING FOR AUTO PRESSURE CONTROLLLER FAILED. COULD NOT PERFORM THE FUNCTIONALTEST IN AUTO MODE TO CHECK FOR FAILURE CODE TO DISPLAY ON DIGITAL CONROLLER IAW FIM 21-31-00-801-A. PERFORMED OPS CHECK OF AUTO AND MANUAL MODES OF PRESSURIZATION CONTROL SYSTEM IAW AMM 21-31-00. OPS CHECKED GOOD.

Part: ENGINE — CONTAMINATED (NR 1) · airframe 35,024 hrs · 30,378 cycles

CLIMBING OUT OF 16,000 FT, AN ODOR OF BURNING RUBBER WAS IN THE COCKPIT AND GALLEY. ODOR CAME AND WENT IN WAVES. FOUND EXCESSIVE AMOUNT OF DEICE FLUID IN THE NR 1 ENGINE AND APU COWLINGS, CLEANED. PERFORMED ENGINE RUNS IAW MM 72-00-00, AND NO DEFECTS NOTED IAW ETN-EM-72-034.

Part: COUPLING — DEFECTIVE (AC BAY) · airframe 34,861 hrs · 30,221 cycles

"PACK 1 VALVE CLSD" DURING CLIMB. REMOVED AND REPLACED FLEX COUPLING FOR NR 1 PACK VALVE Y-DUCT IAW AMM 21-51-01. NO LEAKS NOTED. REF NRWC 662-MIA-03305 FOR WORK ACCOMPLISHED. REMOVED AND REPLACED PACK 2 DUCT OFF HEAT EXCHANGER AS PER AMM 21-60-01. OPC GOOD. NO LEAKS NOTED. REF NRWC 662-MIA-03306 FOR WORK ACCOMPLISHED.

Part: A/C PACK — MALFUNCTIONED (NR 1) · airframe 34,848 hrs · 30,214 cycles

NR 1 A/C PACK VALVE CLOSED MESSAGE ACTIVATED AT 230 FT. WOULD NOT RESET. ON REACHING 10K FT. PACK RESET WITHOUT INCIDENT AND REMAINED ON UNTIL WE TOUCHED DOWN. REPLACED THE CLAMPS ON THE NR 1 PACK. OPS CHECKED GOOD IAW ETN-EM-21-056.

Part: PANEL — INOPERATIVE (EMERGENCY LIGHTS) · airframe 34,592 hrs · 30,006 cycles

EMERGENCY LIGHT NOT ARMED, INTERMITTENT ON & OFF AFTER ENGINE START AND INFLIGHT. R & R THE EMERGENCY LIGHT SWITCH PANEL IAW AMM 33-12-01. OPS CHECKED GOOD IAW AMM 33-50-00.

Part: TERMINAL — DAMAGED (EMERGENCY LIGHT) · airframe 34,551 hrs · 29,975 cycles

EMERGENCY LIGHT INOPERATIVE. REPAIRED THE TERMINAL ENDS ON THE EMERGENCY LIGHT IAW SWPM 20-21-00. OPS CHECKED GOOD, ACFT OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,477 hrs · 29,915 cycles

AFT EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY LIGHT IAW AMM 33-50-12. OPS CHECKED GOOD.

Part: WIRE — UNSECURE (EMERGENCY LIGHT) · airframe 34,217 hrs · 29,693 cycles

EMERGENCY LIGHT SIGN INOPERATIVE. TROUBLESHOT IAW W/M 33-50-50, SECURED THE WIRE SPLICES SP9016 AND SP9017, NO FURTHER DEFECTS NOTED.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,292 hrs · 28,821 cycles

TEMPORARY REPAIR TO FRAME 73 CRACK AT STRINGER 17R. REMOVED AND REPLACED LOWER SECTION OF FRAME 73 IAW SRM 51-40-02.

Part: SKIN — CRACKED (FUSELAGE) · airframe 33,248 hrs · 28,782 cycles

3 CRACKS AROUND RIVETS ON RT FRAME 78. PERFORMED PERMANENT REPAIR OF 3 CRACKS AROUND RIVETS ON RT FRAME 78 IAW ERS-EM-53MR-2633.

Part: PROFILE — CORRODED (SERVICE DOOR) · airframe 33,231 hrs · 28,766 cycles

SERVICE DOOR UPPER AND LOWER U PROFILES NUTPLATE HOLES CORROSION. REPAIRED SERVICE DOOR UPPER AND LOWER U PROFILES NUTPLATE HOLES CORROSION IAW ERS-EM-52MR-720.

Part: CONNECTOR — INTERMITTENT (CABIN) · airframe 33,231 hrs · 28,766 cycles

EMERGENCY EXIT FLOOR STRIP BTW 1A AND 2A INTERMITTENT. CORRECTLY ARRANGED CONNECTORS ON CEILING PANEL 233 BLC IAW AMM 25-22-04 AND 33-50-15.

Part: CONNECTOR — OUT OF POSITION (CABIN) · airframe 33,231 hrs · 28,766 cycles

EMERGENCY EXIT SIGN UNDER COCKPIT DOOR INOP. CORRECTLY ARRANGED CONNECTORS ON CEILING PANEL 233 BLC IAW AMM 25-22-04 AND 33-50-15.

Part: CONNECTOR — INTERMITTENT (CABIN) · airframe 33,231 hrs · 28,766 cycles

EMERGENCY EXIT SIGN BOTTOM LEFT OF SERVICE DOOR INTERMITTENT. CORRECTLY ARRANGED CONNECTORS ON CEILING PANEL 233 BLC IAW AMM 25-22-04 AND 33-50-15.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,231 hrs · 28,766 cycles

EMERGENCY EXIT FLOOR STRIP BTW 8A AND 9A INOP. REMOVED AND REPLACED EMERGENCY EXIT FLOOR STRIP BTW 8A AND 9A IAW AMM 33-50-12.

Part: CONNECTOR — OUT OF POSITION (CABIN) · airframe 33,231 hrs · 28,766 cycles

EMERGENCY EXIT SIGN ON CEILING ABOVE 1A INOP. CORRECTLY ARRANGED CONNECTORS ON CEILING PANEL 233 BLC IAW AMM 25-22-04 AND 33-50-15.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,231 hrs · 28,766 cycles

FRAME 73 CRACKED AT STRINGER 17R. REPAIRED FR 73 AT STRINGER 17R IAW ERS-EM-53MR-2638 PART A.

Part: DOOR FRAME — CORRODED (CARGO DOOR) · airframe 33,231 hrs · 28,766 cycles

CARGO DOOR FWD /AFT TRIM ATTACHMENT NUTPLATE HOLES HAVE CORROSION. REPAIRED CARGO DOOR FWD /AFT TRIM ATTACHMENT NUTPLATE HOLES IAW ERS-EM-52MR- 718.

Part: SKIN — CRACKED (FUSELAGE) · airframe 33,231 hrs · 28,766 cycles

LT REAR FUSELAGE SKIN CRACK JUST AFT OF FRAME 75, ABOVE STRINGER 2L. PERFORMED PERMANENT REPAIR OF LT REAR FUSELAGE SKIN JUST AFT OF FRAME 75 ABOVE STRINGER 2L IAW SRM 53-31-01.

Part: FRAME — CORRODED (FUSELAGE) · airframe 33,231 hrs · 28,766 cycles

FRAME 65 IS CORRODED AT LOWER GUIDE PLATE. FABRICATED AND INSTALLED REPAIR DOUBLER ON FRAME 65 AT LWR GUIDE PLATE IAW ERS-EM-53MR-2619.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 33,231 hrs · 28,766 cycles

LT SIDEWALL SEAT TRACK SUPPORT IS CORRODED AT FR 46. REPAIRED LT SIDEWALL SEAT TRACK SUPPORT FR 46 IAW SRM 53-00-11.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 33,231 hrs · 28,766 cycles

EMERGENCY LIGHT SIGN JUST FORWARD OF THE SERVICE DOOR ENTRANCE IS INTERMITTENT. REPAIRED THE WIRE ON THE SIGN JUST FORWARD OF THE SERVICE DOOR ENTRANCE IAW SWPM 20-21-00, AND SWPM 20-30-00. OPS CHECKED GOOD.

Part: CONTROL UNIT — FAILED (HORIZ STAB) · airframe 32,105 hrs · 27,697 cycles

PTRIM MAIN INOPERATIVE, RED AUTO TRIM FAIL, AMBER, PRESENTED ON EICAS. R & R HORIZONTAL STABILIZER CONTROL UNIT REF AMM 27-40-01. OPS CK GOOD. NO DEFECTS NOTED. MAINTENANCE NOTE: HORIZONTAL STABILIZER CONTROL UNIT FAIL MESSAGE ON CMC 4X PRIOR TO UNIT REPLACEMENT.

Part: PROXIMITY SWITCH — INTERMITTENT (RT MLG) · airframe 31,378 hrs · 27,037 cycles

IN CRUISE LOUD NOISE IN NOSE GEAR AREA. MULTIPLE BANGING & COULD FEEL IN PEDALS. A CMC LG RT UP PROXIMITY SWITCH FAIL ON THIS DATE AT 1704 GMT. VERIFIED INTERMITTENT FAILURE ON RT UP PROXIMITY SWITCH NR 1. R & R CONNECTOR P4669 IAW AWM 20-50-06 & SWITCH IAW 32-61-01, FUNCTIONAL CHECKED OK IAW 32-63-05.

Part: WARNING UNIT — FAILED (COCKPIT) · airframe 31,166 hrs · 26,848 cycles

TRIPLE CHIME & AURAL TAKEOFF CONFIG TRIM. TAKEOFF CONFIG FLAPS, FROM CLIMB OUT TO FL 240 BEFORE WE RETURNED, NOT PRESENT ON THE DESCEND ON LANDING. NO EICAS MSGS ASSOCIATED, NO FLASHING RED MASTER WARNING. NO OVERWEIGHT LANDING. R & R AWU IAW AMM 31-51-01. OPERATIONS CHECKED GOOD.

Part: ELECTRONIC UNIT — FAILED (LANDING GEAR) · airframe 31,166 hrs · 26,849 cycles

AFTER TAKEOFF CLIMBING THROUGH 8,000 FT TAKEOFF CONFIG WARNING. TAKEOFF CONFIG TRIM & FLAPS STARTED REPEATING. RETURNED, LG WEIGHT 43,300. TRANSFERRED TO NRWC 662 02488. R & R LGEU IAW AMM 32-32-01. OPERATIONS CHECKED GOOD.

Part: SMOKE WARNING — FALSE ACTIVATION (COCKPIT) · airframe 31,019 hrs · 26,730 cycles

BAGG EXTINGUISHER BUTTON ILLUMINATED. BUTTON PRESSED THEN BAGG SMOKE WARNING & BAGG EXTINGUISHER INOPERATIVE EICAS. PERFORMED GVI OF BAGGAGE AREA FOR POSSIBLE DEFECTS, NO DEFECTS NOTED. REF ITEM 2 OF THIS LOG PAGE FOR DISCREPANCY OF BAGGAGE COMPARTMENT FIRE EXTINGUISHER SYS, NO VISIBLE SIGNS OF SMOKE OR FIRE.

Part: SWITCH — FAILED (DOOR WARNING) · airframe 30,819 hrs · 26,555 cycles

ACCESS DOOR OPEN, DURING INITIAL CLIMB & FWD AVIONICS DOOR INDICATED OPEN. CAUTION EXTINGUISHED ON APPROACH. FOUND FWD ELEC COMPARTMENT DOOR MICRO SWITCH OUT OF ADJUSTMENT, ADJUSTED SWITCH IAW 52-71-01-400-801-A. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: FIRE BOTTLE — DISCHARGED (CARGO BAY) · airframe 30,791 hrs · 26,516 cycles

CARGO EXTINGUISHER BOTTLE DISCHARGED. PERFORMED OPERATIONS CHECK OF BAGGAGE SMOKE DETECTION SYS IAW AMM 26-15-00. OPERATIONS CHECKED GOOD. DEFERRED BAGGAGE FIREX SYS MEL 26-9. R & R CARGO HIGH RATE & METERING BOTTLES IAW AMM 26-23-01. MEL ITEM RESTORED. FIREX BOTTLE 630 LOWER PN 34600073-1, SN 25272F1. CARTRIDGE HIGH RATE & METERING PN M30903870.

Part: FMU — FAILED (RT ENGINE) · airframe 30,526 hrs · 26,271 cycles

AT FL 350 NR 2 ENG SURGED BY INCREASING & DECREASING N1 & N2 RPM'S. NO ITT LIMITS WERE EXCEEDED. EICAS CHECK MSG ON BOTH MFD'S WHILE ENG WAS SURGING. THE ACFT YAWED & HAD TO BE TRIMMED AFTER APPROX 5 MINS. THE NR 2 ENG WAS NORMAL, WITH NO MSGS NOTED. ALL ENG PARAMETERS WERE NORMAL. TRANSFERRED TO NRWC 662-DFW-02316. R & R RT FPMU IAW RR MM 73-21-10. OPERATIONS CHECKED GOOD & NO LEAKS NOTED AT THIS TIME. REF NRWC 662-DFW-02316.

Part: DUCT — DEFECTIVE (AC BAY) · airframe 29,331 hrs · 25,161 cycles

PACK 2 VLV CLOSED, MSG ON EICAS WHILE AIRBORN. TRIED TO RESET & MAKES A BURBLING SOUND & THEN CLOSES AGAIN. ITEM DEFERRED IAW MEL 21-29. REPLACED DUCT ON RT PACK IAW ETN EMM-21-056. OPERATIONS CHECKED GOOD IAW AMM 21-50-00. MEL RESTORED.

Part: SWITCH — BROKEN (WINDSHIELD HEAT) · airframe 29,112 hrs · 24,963 cycles

ON ROUTE RECEIVED WINDSHIELD HEAT 1 INOPERATIVE. PERFORMED OPERATIONS CHECK OF WINDSHIELD HEAT 1 IAW AMM 30-42-00, CHECKED GOOD. FOUND WINDSHIELD HEAT TEST SWITCH ON MX PANEL BROKEN & STUCK ON WINDSHIELD 1 HEAT. R & R SWITCH IAW AMM 20-13-03. CHECKED GOOD SEE ITEM 1.

Part: LATCH — INOPERATIVE (GPU DOOR) · airframe 28,740 hrs · 24,626 cycles

LOUD POP & ABNORMAL VIBRATION IN FLIGHT FROM NOSE AREA. FOUND GPU ACCESS DOOR OPEN ON ACFT ARRIVAL. INSPECTED DOOR & SURROUNDING AREA. NO DAMAGE TO FUSELAGE SKIN. GPU DOOR LATCH INOPERATIVE. INSTALLED NEW GPU ACCESS DOOR IAW AMM 52-40-01. OPS CHECKED GOOD CDL RESTORED.

Part: FLASHLIGHT ASSY — BROKEN (COCKPIT) · airframe 28,519 hrs · 24,460 cycles

FIRST OFFICER`S FLASHLIGHT ON & OFF SWITCH BROKEN & MISSING. R & R FLASHLIGHT ASSEMBLY IAW AMM 33-50-16. OPS CHECKED GOOD.

Part: ANTI-ICE VALVE — MALFUNCTIONED (RT WING) · airframe 28,424 hrs · 24,379 cycles

CLIMBING THROUGH 10,000 FT IN ICING CONDITIONS, NO OPEN INSCRIPTION ON WING ANTI -ICE BUTTON FOLLOWED BY CAUTION WING ANTI-ICE FAIL & WARNING ICE COND ANTI-ICING INOPERATIVE. EXITED ICING COND & RAN AOM VOL CHECKLIST & DECLARED EMER. TRANSFERRED TO NRWC 662-CMH-01947. R & R RT WING ANTI-ICE VLV IAW AMM 30-11-01. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: FITTING — CORRODED (LT AILERON) · airframe 28,330 hrs · 24,287 cycles

LEFT AILERON DAMPER FITTING IS CHAFED. R & R IAW EO EM-27MR-112.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 28,330 hrs · 24,287 cycles

LEFT OMEGA BEAM CORRODED AROUND HAT BEAM BETWEEN FRAMES 58 - 59. REPAIRED IAW ERS-EM-53MR-945.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 28,330 hrs · 24,287 cycles

LEFT OMEGA BEAM IS CORRODED AT CARBON CROSS MEMBER AT FRAME 28. REPAIRED IAW SRM 53-00-01 & ETN-EM-53-114.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 28,330 hrs · 24,287 cycles

FORWARD SERVICE DOOR SILL BETWEEN FRAMES 18 - 20 HAS EVIDENCE OF CORROSION. R & R FWD SERVICE DOOR SILL IAW SRM 51-40-02.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 28,330 hrs · 24,287 cycles

CABIN LT LOWER FLOOR ANGLE BETWEEN FRAMES 14 - 15 HAS A 1 INCH CRACK. R & R LOWER FLOOR ANGLE IAW SRM 51-40-02.

Part: ATTACH ANGLE — CORRODED (RT WING) · airframe 28,330 hrs · 24,287 cycles

RIGHT OVERWING LOWER ATTACHMENT ANGLE NR 2 HAS A 1 INCH CRACK ON THE TE. R & R RT OVERWING LOWER ATTACHMENT ANGLE NR 2 IAW ENT-EM-53-142.

Part: ATTACH ANGLE — CORRODED (RT WING) · airframe 28,330 hrs · 24,287 cycles

RIGHT OVERWING LOWER ATTACHMENT ANGLE NR 1 HAS A 1 1/2 INCH CRACK ON THE PREVIOUS SPLICE REPAIR TE. R & R RT OVERWING LOWER ATTACHMENT ANGLE NR 1 PREVIOUS SPLICE IAW ETN-EM-53-142. APPLIED SEALANT IAW ETN-GN-51-009 & ANTI-MICROBIAL PRIMER IAW AMM 28-11-00 TO LOCK COLLARS INSIDE THE FUEL TANK.

Part: ATTACH ANGLE — CORRODED (LT WING) · airframe 28,330 hrs · 24,287 cycles

LEFT LOWER ATTACHMENT ANGLE NR 2 HAS 3/8 INCH CRACK ON THE LE. REMOVED & INSTALLED A NEW ANGLE IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 28,330 hrs · 24,287 cycles

LEFT OMEGA BEAM HAS CORROSION BY THE CROSS MEMBER AT FRAME 20. COMPLETED REPAIR IAW ETN-EM-53-547 & SRM 51-00-10.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 28,330 hrs · 24,287 cycles

CARGO DOOR SILL HAS EVIDENCE OF CORROSION. REPLACED CARGO DOOR SILL WITH NEW SILL IAW SRM 51-40-02 & SRM 51-20-03.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 28,330 hrs · 24,287 cycles

RIGHT OVERWING ATTACHMENT UPPER ANGLE HAS 3/8 INCH CRACK & PULLED RIVETS BETWEEN FRAMES 48 - 49. REPAIRED OVERWING ATTACHMENT UPPER ANGLE IAW SRM 53-23-12 REPAIR 3.

Part: ATTACH ANGLE — CORRODED (RT WING) · airframe 28,330 hrs · 24,287 cycles

RIGHT OVERWING LOWER ATTACHMENT ANGLE NR 4 HAS A 1 1/4 INCH CRACK ON THE LE. R & R RT OVERWING LOWER ATTACHMENT ANGLE NR 4 IAW ETN-EM-53-142.

Part: ENGINE — MALFUNCTIONED (NR 1) · airframe 28,320 hrs · 24,274 cycles

AFTER E1 SHUTDOWN STRONG SMELL OF BURNING & VISUALLY SAW VERY HUGE AMOUNT OF SMOKE COMING OUT OF FRONT & BACK OF ENG FOR AT LEAST 15 MINUTES. INSPECTED ENG NR 1 IAW ETN-EM-79-015 UP TO ITEM 13 FOUND ENG REQUIRES REPLACEMENT.

Part: SEAL — DEFECTIVE (NR 1 ENGINE) · airframe 28,108 hrs · 24,084 cycles

NUMBER 1 ENG SMOKING. TRANSFERRED TO NRWC 662-ORD-01891. IAW NRWC 662-ORD-01891 R & R THE SHAFT PLUG SEAL AT ENG 1 IAW RR MM 72-59-15. GND RAN IAW RR MM 72-00-00 WITH NO DEFECTS.

Part: BLEED AIR SYS — LEAKING · airframe 27,607 hrs · 23,620 cycles

WHILE CLIMBING THROUGH 14,000 FT, RECEIVED A BLEED 1 LEAK MESSAGE ON THE EICAS & A RED LEAK ILLUMINATED ON THE BLEED 2 BUTTON. COMPLIED WITH THE PROCEDURES IN THE AOM. WHEN THE BLEED WAS CLOSED, LEAK WENT AWAY. R & R SEALS AT JOINTS & APU CHECK VALVE GASKETS.. OPS & LEAK CHECKED GOOD IAW AMM 36-00-00-700-803-A.

Part: O-RING — DAMAGED (BLEED AIR SYS) · airframe 27,377 hrs · 23,443 cycles

CLIMBING THROUGH 10,000 FEET BLEED 1 LEAK COME ON WE IMMEDIATELY RETURNED TO LAND. WHEN ISOLATED BLEED 1 INDICATION WENT AWAY IAW AOM VOL 1. R & R GAMAH COUPLING O RINGS BLEED AIR JOINT NR 11. OPERATIONS CHECKED GOOD, LEAK CHECKED GOOD IAW AMM 36-11-09.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,075 hrs · 23,211 cycles

FLOOR PROXIMITY STRIP ASSEMBLY INOPERATIVE AT ROW 10 - 12. R & R FLOOR PROXIMITY STRIP LIGHT AT ROW 10 - 12 IAW AMM 33-50-12. OPERATIONS CHECKED GOOD AT THIS TIME WITH NO DEFECTS NOTED.

Part: WARNING SYSTEM — FALSE ACTIVATION (CARGO DOOR) · airframe 26,778 hrs · 22,912 cycles

AFTER ROTATION BAGGAGE DOOR OPEN INDICATION, FOUND CARGO STRAP IN DOOR NO INDICATION ON GND, CHECKED OK FOR SERVICE.

Part: CRADLE — BROKEN (FLASHLIGHT) · airframe 26,460 hrs · 22,653 cycles

FWD CABIN EMERGENCY FLASHLIGHT CRADLE BROKEN. R & R FWD CABIN EMERGENCY FLASHLIGHT HOLDER IAW 33-50-16-000-801 33-50-16-400-801, OPERATIONS CHECKED GOOD.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 25,391 hrs · 21,777 cycles

SERVICE DOOR EMERGENCY EXIT IDENTIFIER LIGHT IS OUT. RESET EMERGENCY LIGHT CIRCUIT BREAKER FOR 3 MINUTES, PERFORMED OPT IAW 33-50-12.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 25,391 hrs · 21,777 cycles

FWD FLOOR EMERGENCY EXIT IDENTIFIER LIGHT IS OUT. RESET EMERGENCY LIGHT CIRCUIT BREAKER FOR 3 MIN, PERFORMED OPT IAW AMM 33-50-12.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 25,378 hrs · 21,765 cycles

EMERGENCY EXIT LIGHT ON LOWER SERVICE DOOR INOPERATIVE. R & R NR 2 EMERGENCY BATTERY IAW AMM 33-50-04. OPS CHECKED GOOD.

Part: WIRE — BROKEN (CABIN) · airframe 24,349 hrs · 20,934 cycles

DURING MX INSP FOUND THE FLOOR PROXIMITY LIGHT STRIP AT POSITION NR 1, NR 3, NR 6 & NR 8 TO HAVE BROKEN WIRES. THE ACFT WAS REMOVED FROM SERVICE. R & R THE FLOOR PROXIMITY LIGHT STRIP AT POSITION NR 1, NR 3, NR 6 & NR 8 IAW AMM 33-50-08. THE OPS CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 24,349 hrs · 20,934 cycles

DURING B INSPECTION, FOUND THE FLOOR GUSSET HAS CORROSION AT FRAME 21 & 22. THE ACFT WAS REMOVED FROM SERVICE. R & R THE FLOOR GUSSET AT FR 20 IAW SRM 51-40-02. LEVEL OF CORROSION UNKNOWN. THE ACFT WAS RETURNED TO SERVICE.

Part: LIGHT — CRACKED (CABIN) · airframe 24,349 hrs · 20,934 cycles

DURING MX INSP FOUND THE PROXIMITY FLOOR LIGHT SIDE WALL EXTRUSION AT LT POSITION NR 5 & NR 7 CRACKED. THE ACFT WAS REMOVED FROM SERVICE. R & R THE PROXIMITY FLOOR LIGHT SIDE WALL EXTRUSION AT LT POSITION NR 5 & NR 7 IAW AMM 33-50-08. THE OPS CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: WIRE — BROKEN (COCKPIT) · airframe 23,083 hrs · 19,944 cycles

ON FLIGHT 2733 THE CREW REPORTED THAT AFTER TAKEOFF THEY HEARD STRONG STATIC OVER THE INTERCOMM SYSTEM. THEY WERE UNABLE TO COMMUNICATE WITH FIRST OFFICER AND FLIGHT ATTENDANT. THE CREW ELECTED TO RETURN TO DFW AND DECLARED AN EMERGENCY. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. CHECKED OUTSIDE RAMP JACKS, NO DEFECTS NOTED. CHECKED PA AMP, NO DEFECTS AND IS WELL-SEATED. CHECKED BEHIND BOTH AUDIO PANELS, NO DEFECTS NOTED. FOUND 2 BROKEN WIRES BEHIND FIRST OFFICER’S JACK PANEL (WIRES NR 1, 5 TO AND JACK J3528). REPAIRED WIRES. THE OPERATIONAL CHECK WAS GOOD IAW WM 23-51-53, AMM 23-51-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: PRESSURE SWITCH — DEFECTIVE (RUDDER) · airframe 23,038 hrs · 19,909 cycles

ON FLIGHT 3336 THE CREW REPORTED THAT WHILE CLIMBING THROUGH FL300 AUTOPILOT FAILED (WARNING) FOLLOWED BY RUDDER SYS 1-2 INOP (CAUTION) FOLLOWED AOM PROCEDURE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RUDDER SYS 2 PRESSURE SWITCH IAW EMB MM 27-23-04. THE OPERATIONAL CHECK AND LEAK CHECK WERE OK. AUTO PILOT FUNCTIONAL TEST OK IAW EMB MM 22-11-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: UNKNOWN — MALFUNCTIONED (AUTOPILOT SYS) · airframe 23,036 hrs · 19,908 cycles

ON FLIGHT 3309 THE CREW REPORTED THAT 5 MINUTES AFTER TAKEOFF A/P FAILED FOLLOWED BY RUDDER SYS 1-2 INOP MESSAGE. THE CREW FOLLOWED AOM PROCEDURES. NO RESET WAS ACCOMPLISHED. THE CREW DECLARED AN EMERGENCY AND RETUNED TO MOB. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOLLOWED RESET PER EMB FIM 27-22-00-810-804-A NO MESSAGES NOTED AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 22,068 hrs · 19,130 cycles

DURING B INSPECTION, FOUND THE LEFT OVERWING AFT EMERGENCY LIGHT INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT OVERWING AFT EMERGENCY LIGHT LAMP IAW AMM 33-50-07-000-801-A AND 33-50-07-400-801-A. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY — MALFUNCTIONED (NR 2) · airframe 21,921 hrs · 19,010 cycles

ON FLIGHT 3559 THE CREW REPORTED THAT DURING CLIMB AFTER TAKEOFF THE NR 2 BATTERY OVERTEMP WARNING CAME ON "71" C. THE CREW DECLARED AN EMERGENCY AND RETURNED TO MIA. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 2 BATTERY. THE OPERATIONAL CHECK WAS GOOD IAW W/C 24-600-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE HARNESS — DEFECTIVE (RT MLG) · airframe 21,527 hrs · 18,702 cycles

ON FLIGHT 2990 THE CREW REPORTED AFTER LIFTING OFF THE GROUND, SELECTED GEAR UP. AS THE GEAR WAS RETRACTING RECEIVED A LANDING AIR/GND FAIL EICAS CAUTION MESSAGE APPEARED. AFTER RECEIVING MESSAGE, GLANCED DOWN AND NOTICED ONE GEAR INDICATING UP AND THE OTHER TWO INDICATING IN TRANSIT. AS SOON AS NOTICED THIS, ALL THREE INDICATED UP. THEN THE MESSAGE EXTINGUISHED. THE LANDING GEAR OPERATED NORMALLY UPON RETRACTION WITH THE EXCEPTION OF THE LANDING AIR/GND FAIL MESSAGE, WHICH ONLY STAYED ON A COUPLE OF SECONDS BEFORE IT EXTINGUISHED. THE MESSAGE NEVER CAME ON AGAIN. ALSO, THE LANDING GEAR OPERATED NORMALLY UPON EXTENSION. THE CREW PERFORMED A TOWER FLY BY. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT MAIN LANDING GEAR AIR/GROUND PROXIMITY SWITCH NR 1 HARNESS IAW AMM 32-00-03. THE OPERATIONAL CHECK WAS GOOD IAWW AMM 32-63-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONTROL UNIT — INOPERATIVE (HORIZ STAB) · airframe 21,511 hrs · 18,686 cycles

ON FLIGHT 2865 THE CREW REPORTED THAT AFTER DEPARTURE ON CLIMB THEY RECEIVED A MASTER WARNING MESSAGE THAT THE PITCH TRIM MAIN WAS INOPERABLE. THE CREW DECLARED AN EMERGENCY AND RETURNED TO DFW. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED HORIZONTAL STABILIZER CONTROL UNIT IAW EMB MM 27-40-01. THE OPERATIONAL TEST WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CRADLE — BROKEN (COCKPIT) · airframe 21,502 hrs · 18,680 cycles

DURING MAINTENANCE INSPECTION FOUND THE CAPTAIN'S FLASHLIGHT CRADLE BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CAPTAIN’S AND THE FORWARD FLIGHT ATTENDANT’S FLASHLIGHT CRADLE AS REQUIRED IN REF WITH WC 33-700-20. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SENSOR — INOPERATIVE (BRAKE TEMP) · airframe 21,227 hrs · 18,475 cycles

ON FLIGHT 2786 THE CREW REPORTED, RECEIVED A BRAKE OVERHEAT CAUTION MESSAGE MOMENTARY ON DESCENT. ALL INDICATIONS WERE GREEN THEN ON FINAL LEFT OUTBOARD TEMPERATURE INDICATION STARTED CLIMBING. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMVOED FROM SERVICE. REMOVED AND REPLACED NR 1 BRAKE TEMPERATURE SENSOR PER AMM 32-47-01. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE) · airframe 20,249 hrs · 17,711 cycles

ON FLIGHT 3597 THE CREW REPORTED THAT AFTER TAKEOFF CAB ALT WENT TO AMBER DASHES FOR APPROXIMATELY 20 MINUTES THE CAB ALT RE-APPEARED WITH NUMBERS FOR REMAINDER OF THE FLIGHT TO JAX. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED DIGITAL CONTROLLER IAW EMB145 AMM 21-31-01 AND TESTED SATISFACTORY IAW EMB145 AMM 21-31-00. THE AIRCRAFT WAS RETURNED TO SERIVCE.

Part: WIRE — BROKEN (CABIN) · airframe 20,042 hrs · 17,541 cycles

DURING MAINTENANCE BASE INSPECTION FOUND THE CENTER ASILE EMERGENCY LIGHT STRIP DIRECTLY IN FRONT OF LAV HAS A BROKEN WIRE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CENTER ASILE EMERGENCY PROXIMITY LIGHT IAW EMB AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: DRAIN VALVE — OBSTRUCTED (FUSELAGE) · airframe 19,948 hrs · 17,470 cycles

ON FLIGHT 2709 THE CREW REPORTED THAT DURING CRUISE THE CABIN DEPRESSURIZED AT 37000 FEET. THE CREW DECLARED AN EMERGENCY AND DID AN EMERGENCY DESCENT. THE PASSENGER MASKS DID NOT DEPLOY. THE FLIGHT ATTENDANT REPORTED A LOUD SOUND AT THE GALLEY DOOR. THE AIRCRAFT LANDED AT PIA WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND DEBRIS ON FUSELAGE DRAIN PLUG JUST AFT OF UNDER COCKPIT ACCESS DOOR, REMOVED DEBRIS AND PERFORMED OPERATIONAL CHECK OF CABIN PRESS IN AUTO AND MANUAL MODE IAW EMB-145 AMM 21-31-00, THE CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,963 hrs · 16,760 cycles

FOR FLIGHT 3348 DURING MAINTENANCE INSPECTION FOUND THE LEFT EXIT AFT OVERWING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT EXIT AFT OVERWING EMERGENCY LAMP. THE OPERATIONAL CHECK WAS GOOD IAW EMB AMM 33-50-07. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 17,467 hrs · 15,655 cycles

DURING MAINTENANCE BASE VISIT FOUND THE RIGHT FORWARD EXTERIOR EMERGENCY LIGHT TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. CHECKED THE FUNCTIONS OF THE RIGHT FORWARD EMERGENCY LIGHT IAW EMB 145 AMM 33-50-00. NO DEFECTS WERE FOUND. NO PARTS REMOVED OR REPLACED. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: PUMP — INOPERATIVE (VACUUM) · airframe 15,832 hrs · 14,356 cycles

ON FLIGHT 3483 DURING CRUISE THE CREW REPORTED THAT THE PRESSURIZATION WAS UNCONTROLLABLE IN AUTO AND MANUAL MODE. THE CREW ELECTED TO DIVERT TO ATL AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE VACUUM PUMP IAW AMM 21-31-06. THE PRESSURIZATION CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 11,576 hrs · 10,499 cycles

DURING MAINTENANCE INSPECTION FOUND THAT THE LEFT SIDE OF AIRCRAFT FORWARD EMERGENCY LIGHT WOULD NOT COME ON. AIRCRAFT REMOVED FROM SERVICE. REPLACED BATTERY PACK POWER SUPPLY NR 1 IN ACCORDANCE WITH EMB AMM 33-50-09. OPERATIONAL CHECK GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 14,748 hrs · 13,375 cycles

DURING MAINTENANCE CHECK, THE BAGGAGE DOOR LOWER SILL WAS FOUND TO HAVE CORROSION AROUND THE NUT PLATE AND IN THE FORWARD CORNER. IT WAS EVALUATED AND FOUND TO BE OUT OF LIMITS. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE BAGGAGE DOOR SILL IN ACCORDANCE WITH EMBRAER SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CIRCUIT BREAKER — TRIPPED (STAB SYSTEM) · airframe 14,548 hrs · 13,186 cycles

ON FLIGHT 3613 THE CREW REPORTED THAT BOTH THE PITCH TRIM BACKUP INOPERABLE WARNING AND THE PITCH TRIM MAIN INOPERABLE WARNING CAME ON IMMEDIATELY AFTER TAKEOFF. THE CREW REPORTED THAT ALL PITCH TRIM HAD FAILED. THE CHECK LIST WAS COMPLIED WITH. THE CREW DECLARED AN EMERGENCY AND ELECTED TO RETURN TO DFW. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND CIRCUIT BREAKERS A4, PITCH TRIM 2 AND C9 PITCH TRIM HAD POPPED OUT. RESET CIRCUIT BREAKERS AND PERFORMED OPERATIONAL CHECK AS PER EMB 145 AMM 27-40-00 AND FIM 27-43-00. NO PARTS WERE REMOVED OR REPLACED. OPERATIONAL CHECK GOOD, NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: UNKNOWN — SMOKE (CABIN) · airframe 14,279 hrs · 12,985 cycles

ON FLIGHT 3447 - CREW REPORTED SMOKE IN CABIN RIGHT AFTER TAKEOFF. CREW DECLARED EMERGENCY AND RETURNED TO DFW. LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,804 hrs · 9,172 cycles

DURING MBV INSPECTION FOUND, FORWARD GALLEY FLOOR-SUPPORT CORRODED AT FRAME 20, NEAR CENTER OMEGA BEAM AND CARBON CROSS-MEMBER. REMOVED AND REPLACED SUPPORT IAW SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,804 hrs · 9,172 cycles

DURING MBV INSPECTION FOUND RAMP FLOOR SUPPORT CORRODED AT FRAME 20 NEAR CARBON CROSS MEMBER. REMOVED AND REPLACED SUPPORT IAW EMB SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,804 hrs · 9,172 cycles

DURING MBV INSPECTION FOUND, ANGLE SUPPORT AT FRAME 23 RIGHT SIDE FOR AFT GALLEY SUPPORT IS CORRODED. REMOVED AND REPLACED ANGLE SUPPORT IAW SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 8,425 hrs · 7,836 cycles

ON TAKEOFF, LAVATORY SMOKE LIGHT ILLUMINATED WITH STRONG ODOR IN CABIN, RETURNED TO CMI. REMOVED AND REPLACED NUMBER 2 ENGINE IAW AMERICAN EAGLE WORK CARD. PERFORMED OPERATIONAL AND LEAK CHECKS WITH NO DEFECTS NOTED. RETURNED AIRCRAFT TO SERVICE.

Part: CONNECTOR — DAMAGED (PROXIMITY SWITCH) · airframe 8,030 hrs · 7,466 cycles

AIR/GROUND MESSAGE ILLUMINATED ON TAKEOFF, GEAR HANDLE WOULD NOT COME UP, MESSAGE WENT WENT AWAY ON LANDING. FOUND PIN "A" BROKEN ON PROXIMITY SWITCH. REMOVED AND REPLACED NOSE LANDING GEAR PROXIMITY SWITCH IAW EMB AMM 32-63-05. PERFORMED EXTENSION AND RETRACTION CHECKS WITH NO DEFECTS. RETURNED AIRCRAFT TO SERVICE.

Part: SKIN — DENTED (FUSELAGE)

DENTS IN LT REAR FUSELAGE LOWER SKIN. REPAIRED DENTS IAW EO EM-53MR-535R2 BY CUTTING OUT DAMAGE AND INSTALLING AN EXTERNAL DOUBLER. AIRCRAFT WAS RETURNED TO SERVICE. (K)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

DURING CPCP INSPECTION FOUND OMEGA BEAM AT FRAME 20 IS CORRODED. REPAIRED OMEGA BEAM BY INSTALLING A DOUBLER IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (K)

Part: SILL — CORRODED (FUSELAGE)

DURING CPCP INSPECTION FOUND FORWARD SERVICE DOOR SILL PLATE CORRODED. INSTALLED NEW SILL PLATE IAW EMB SRM. AIRCRAFT WAS RETURNED TO SERVICE. (K)