N902BC

Part: BLEED VALVE — ABNORMAL (ENGINE) · airframe 45,319 hrs · 41,071 cycles

BLD 1 LEAK WARNING MESSAGE APPEARED DURING CLIMB. AFTER RUNNING QRH INSCRIPTION MESSAGE WENT AWAY. REMOVED AND REPLACED PNEUMATIC CROSS BLEED VALVE IRT AMM 36-10-01-000/400-801-A OPS CHECK GOOD OK FOR SERVICE

Part: PRECOOLER — CRACKED (ZONE 400) · airframe 45,079 hrs · 40,816 cycles

ON CLIMB OUT OF PHL BLEED 2 LEAK WARNING MESSAGE PRESENTED. FOUND CRACK IN #2 ENG PRECOOLER R+R #2 ENG PRECOOLER IAW AMM 36-11-04. OPS CHECK GOOD

Part: ACTUATOR — CRACKED (ZONE 500) · airframe 44,947 hrs · 40,671 cycles

HYD 2 FAIL MSG ON EICAS DFRL 11MAY25 15:46 CLT INSPECTED AND FOUND #1 SPEED BRAKE ACTUATOR CRACKED (SS) FACT 11MAY25 22:51 CLT R&R L/H SPEED BRAKE ACTUATOR. LEAK CHECK GOOD. OPS CHECK GOOD IAW AMM 27-62-02.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,763 hrs · 37,102 cycles

IN FLIGHT PTRIM BACK UP INOP DISPLAYED ON EICAS FACT 29JUL23 18:31 PHL PDPU THE AC/ PERFORMED OPS IAW AMM 27-40-00-700-802-A. OPS CHECK GOOD, OK FOR SERVICE

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,559 hrs · 36,872 cycles

DURING PS2 CHECK FOUND LH EXTERIOR EMERGENCY LIGHT INOP-C/A-RAR EMERGENCY LIGHT ASSY IAW EMB 145 AMM 33-50-10. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED AT THIS TIME.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,550 hrs · 36,864 cycles

LH EXTERNAL OVERWING EMERGENCY LIGHT INOP-C/A-RAR LH EXTERNAL OVERWING EMERGENCY LIGHT BULB IAW AMM 33-50-10.OPS CHECK GOOD

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,540 hrs · 36,857 cycles

LH OVERWING EMERGENCY LIGHT INOP-C/A-RAR LH EXTERNAL OVERWING EMERGENCY LIGHT BULB IAW EMB AMM 33-50-10-000-801-A AND 33-50-10-400-801-A OPC GOOD END

Part: LAMP — INOPERATIVE (LH) · airframe 41,517 hrs · 36,834 cycles

LH OVER WING EMERGENCY LIGHT INOP.-C/A-FOUND H OVERWING EMERGENCY LIGHT LAMP BURNT OUT RAR LIGHT LAMP ON L/H OVERWING EMERGENCY LIGHT ASSEMBLY IAW EMB-145 AMM 33-50-10. OPS CHECK GOOD

Part: NONE — NONE · airframe 41,415 hrs · 36,729 cycles

FLAP FAIL CAUTION ON EICAS FLAP 45 INDICATION ON THE EICAS AND RMU DECLARED EMERGENCY. THE FAIL MESSAGE CAME ON AFTER SELECTING FLAPS 45 AND INDICATING FLAPS 45-C/A-DOWNLOADED CMC AND FOUND FLAP DRIVE TX FAIL MESSAGE ON CMC T/S FLAP DRIVE TX FAIL IAW FIM 27-51-00-801-804 SUBTASK 1 OPS CHECK FLAP SYS IAW EMB AMM 27-51-00-700-801 FOUND TO BE A TRANSITORY CONDITION NO FUTHER DEFECTS NOTED AT THIS TIME

Part: LAMP — INOPERATIVE (LH) · airframe 41,407 hrs · 36,725 cycles

LH OVERWING EMERGENCY LIGHT INOP-C/A-RAR LH WING EMERGENCY LIGHT LAMP IAW AMM 33-50-07-000-801-A AND 33-50-07-400-801-A. OPS CHECK GOOD. END.

Part: ROLLER — LACK OF LUBE (PAX DOOR) · airframe 40,938 hrs · 36,222 cycles

MAIN CABIN DOOR HARD TO OPEN-C/A-CLEANED AND LUBED MAIN DOOR FRAME ROLLERS IAW EMB 145 AMM 53-21-02. OPC GOOD

Part: NONE — UNSERVICEABLE ([0000] [2] [) · airframe 40,866 hrs · 36,143 cycles

FIRST 3 CABIN FLOOR EMERGENCY LIGHTS INOP.-C/A-RAR BATTERY CHARGER ASSY (2) AS PER EMB 145 AMM 33-50-04 OPS CHECK GOOD

Part: LAMP — INOPERATIVE (LH) · airframe 40,738 hrs · 35,990 cycles

LH OVERWING EMERGENCY LIGHT INOP-C/A-RAR LH OVERWING EMERGENCY LIGHT LAMP IAW AMM 35-50-10

Part: DUCT — LOOSE (CP SEAT) · airframe 40,284 hrs · 35,475 cycles

COCKPIT HAS WEIRD FUME SMELL.-C/A-WHEN TROUBLESHOOTING FIM TASK 21-20-00-810-801-A UP TO PAGE 204 BLOCK 41, FOUND AND RESECURED LOOSE DUCTING UNDER FO'S FLOOR PANEL (222BF) IAW EMB145 AMM 21-20-04.

Part: NONE — INOPERATIVE (LH) · airframe 40,177 hrs · 35,346 cycles

LH OVERWING EMERGENCY LIGHT INOP-C/A-RAR LH OVERWING EMERGENCY LIGHT IAW EMB 145 AMM 33-50-07 OPS CHECK GOOD

Part: LAMP — INOPERATIVE (LH) · airframe 40,166 hrs · 35,332 cycles

LH EXTERIOR OVER WING EMERGENCY LIGHT INTERMITTENT-C/A-RESEATED LH EXTERIOR OVER WING EMERGENCY LAMP IAW EMB 145 AMM 33-50-10. OPC GOOD

Part: LAMP — INOPERATIVE (LH) · airframe 40,139 hrs · 35,303 cycles

LH OVERWING EMERGENCY LIGHT INOP-C/A-RAR LH 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 (LH) · airframe 40,063 hrs · 35,221 cycles

LH OVERWING EMERGENCY LIGHT INOP-C/A-RAR LH OVERWING EMERGENCY LIGHT LAMP IAW EMB AMM 33-50-07-000-801-A AND 33-50-07-400-801-A. OPC GOOD. END.

Part: LAMP — INOPERATIVE (LH) · airframe 39,950 hrs · 35,110 cycles

DURING PS-2 CHECK FOUND LH OVER WING EMERGENCY LIGHT INOP-C/A-RAR LH OVER WING EMERGENCY LIGHT LAMP IAW EMB 145 AMM 33-50-10. OPS CHECK GOOD. NO DEFECTS FOUND

Part: NONE — NONE · airframe 39,868 hrs · 35,029 cycles

LH OVER WING EMERGENCY LIGHT INOP-C/A-RAR LH OVERWING EMERGENCY LAMP IAW EMB AMM 33-50-10 OPC GOOD

Part: NONE — NONE · airframe 39,847 hrs · 35,006 cycles

DURING PS-1 CHECK OVERWING LEFT AFT EMERGENCY LIGHT FOUND INOP-C/A-RAR EXTERNAL EMERGENCY LIGHT BULB IAW EMB 145 AMM 33-50-10. OPS CK GOOD.

Part: NONE — NONE · airframe 39,798 hrs · 34,954 cycles

THIS IS ANOTHER SUPPLEMENTAL WITH ADDITIONAL PART NO. INFORMATION: PN473597-13 SN3436/ PN473597-13 SN 2460A. BAGG SMOKE DURING CRUISE FLIGHT DIVR IND BAG SMOKE / DECLARED EMERGENCY / EQP SWAP FLT CONT AND FIRED BAGG EXTINGUISHER BOTTLEREF LG. PG. 4728490 ITEM #1 BAGGAGE SMOKE DETECTORS REQUIRE OPS CHECK.-C/A-PERFORMED OPS CHECK IAW EMB 145 AMM 26-15-10 REF TASK 26-15-00-700-804-A OPS CHECK GOOD.NO FURTHER DEFECTS NOTED.RAR CARGO SMOKE DETECTORS IAW EMB 145 AMM 26-15-01 AS REQUIRED.OPS CHECK GOOD. NO FURTHER DEFECTS NOTED AT THIS TIME.-C/A-PERFORMED OPS CHECK IAW EMB 145 AMM 26-15-10 REF TASK 26-15-00-700-804-A OPS CHECK GOOD. NO FURTHER DEFECTS NOTED. RAR CARGO SMOKE DETECTORS IAW EMB 145 AMM 26-15-01 AS REQUIRED. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED AT THIS TIME.

Part: SMOKE WARNING — ILLUMINATED (CARGO) · airframe 39,797 hrs · 34,953 cycles

BAGG SMOKE DURING CRUISE FLIGHT DIVR IND BAG SMOKE / DECLARED EMERGENCY / EQP SWAP FLT CONT AND FIRED BAGG EXTINGUISHER BOTTLE-C/A-PER CAPTAIN, FIRE DEPT INSPECTED PAX BAGS AND CARGO COMPT WITH GAS DETECTOR AND THERMAL IMAGING. NO DISCREPANCIES NOTED. SEE ITEM 2 FOR GVI OF CARGO COMPARTMENT. DEFERRED BAGGAGE FIRE EXTINGUISHER SYSTEM. MEL 26-9 AUTH 030272D-C. INSPECTED CARGO LINERS IAW EMB 145 AMM 25-51-01-200-801-A. NO INDICATION OF FIRE OR SMOKE EVENT ON ANY CARGO LINER. NO FURTHER ACTION REQUIRED

Part: NONE — NONE · airframe 39,770 hrs · 34,917 cycles

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

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 39,622 hrs · 34,735 cycles

LAV SMOKE WARNING IN FLIGHT, NO INDICATION OF FIRE. PERFORMED OPERATIONAL CHECK OF LAV SMOKE DETECTION IAW AMM 26-14-00. OPERATIONAL CHECK GOOD. NO DEFECTS NOTED AT THIS TIME.

Part: BATTERY — OVERTEMP (MASTER) · airframe 39,046 hrs · 34,086 cycles

BATT OVR TEMP AFTER LANDING / DECLARED EMERGENCY NO INJURIES RPRTD #1 BATT HOT 85 C-C/A-RAR #1 MAIN BATTERY IAW AMM W/C 24-600-00 OPC GOOD

Part: ROLLER — LACK OF LUBE (PAX DOOR) · airframe 38,680 hrs · 33,663 cycles

MAIN PASSENGER ENTRY DOOR (1L) IS VERY DIFFICULT TO OPEN.-C/A-LUBRICATED MAIN CABIN DOOR ROLLERS ,OPS CHECK GOOD IAW AMM 52-10-00.

Part: FLASHLIGHT — INOPERATIVE (FWD CABIN) · airframe 38,577 hrs · 33,530 cycles

FA FORWARD EMERGENCY FLASHLIGHT INOP. R & R FA FORWARD EMERGENCY FLASHLIGHT ASSY IAW EMB 145 - AMM 33 - 50 - 16, OPC IS GOOD.

Part: FLASHLIGHT — INOPERATIVE (FWD CABIN) · airframe 38,555 hrs · 33,502 cycles

FA FORWARD EMERGENCY FLASHLIGHT INOP-C/A-FLIGHT CREW PLACARDED FORWARD FA EMERGENCY FLASHLIGHT-M PROCEDURES C/W AUTH# 060188-D REF# 25-32 MOC# 206396

Part: ROLLER — LACK OF LUBE (DOOR) · airframe 38,484 hrs · 33,401 cycles

FA REPORTS DOOR IS VERY HARD TO OPEN. (MAIN CABIN DOOR)-C/A-PERFORMED SERVICING OF THE MAIN DOOR FRAME - LUBED ROLLERS IAW AMM 53-21-02. OPS CHECK GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 38,363 hrs · 33,261 cycles

EMERGENCY/PARKING BRAKE LIGHT INOP-C/A-RAR 4 EA. BULBS ON EMERGENCY/PARKING BRAKE LIGHT ASSY IAW 20-13-04 OPS CHECK GOOD

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 38,363 hrs · 33,261 cycles

INTERIOR CEILING OVERWING EMERGENCY EXIT AFT LIGHT IS INOP.-C/A-REMOVED EMERGENCY LIGHTS DC/AC INVERTER #4 AND INSTALLED A NEW INVERTER IAW EMB145 AMM 33-50-11. OPS CHECK GOOD.

Part: ROLLER — LACK OF LUBE (PAX DOOR) · airframe 38,140 hrs · 33,044 cycles

MAIN DOOR VERY DIFFICULT TO OPEN FA NEEDED MULTIPLE ATTEMPTS.-C/A-LUBRICATED THE MAIN DOOR ROLLER DOOR OPEN AND CLOSED OK AFTER REF. AMM 52-10-01

Part: DOOR FRAME — CORRODED (MAIN) · corrosion level 2 · airframe 38,065 hrs · 32,960 cycles

MAIN DOOR LOWER FRAME CORRODED AT NUTPLATES (4 EA.) CORROSION LEVEL 2-C/A-REPAIRED MAIN DOOR LOWER FRAME CORRODED AT NUTPLATES IAW EMB 145 SRM 52-10-02 AND ETN-EM-52-041.

Part: DOOR FRAME — CORRODED (CARGO BAY) · corrosion level 2 · airframe 38,065 hrs · 32,960 cycles

CARGO DOOR LOWER FRAME PROFILE CORRODED AT 2 NUTPLATESCORROSION LEVEL 2-C/A-RAR CARGO DOOR LOWER FRAME PROFILE IAW EMB 145 SRM 51-40-02

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 38,065 hrs · 32,960 cycles

LEFT OMEGA BEAM OUTBD SUPPORT AT FR 47-48 CRACKED. CRACK LENGTH .25 NUMBER OF CRACKS 1-C/A-PERFORMED A PERMANENT REPAIR OF THE LT OMEGA BEAM OUTBD SUPPORT AT FR 47-48 IAW EMB 145 SRM 53-23-02RE.

Part: FLOOR SUPPORT — CRACKED (CABIN) · airframe 38,065 hrs · 32,960 cycles

RIGHT OMEGA BEAM INBD SUPPORT AT FR 47-48 CRACKED 1 CRACK, .25 IN LENGTH. C/A-PERFORMED PERMANENT REPAIR TO RT OMEGA BEAM INBD SUPPORT AT FR 47-48 IAW EMB 145 SRM 53-23-02RE.

Part: DOOR SILL — CORRODED · corrosion level 2 · airframe 38,065 hrs · 32,960 cycles

SERVICE DOOR CENTER SILL CORRODED CORROSION LEVEL 2-C/A-RAR SERVICE DOOR CENTER SILL IAW EMB 145 SRM 51-40-02.

Part: SUPPORT BRACKET — CRACKED (PAX DOOR) · airframe 38,065 hrs · 32,960 cycles

PAX DOOR INTERNAL ROTATING HANDLE SUPPORT BRACKET CRACKED1 CRACK .5" IN LENGTH. C/A-R & R PAX DOOR INTERNAL ROTATING HANDLE SUPPORT BRACKET IAW EMB 145 SRM 51-40-02.

Part: DOOR SILL — CORRODED (CARGO) · corrosion level 2 · airframe 38,065 hrs · 32,960 cycles

CARGO DOOR LOWER SILL IS CORRODED BETWEEN FR 65-66 CORROSION LEVEL 2. C/A-R & R CARGO DOOR LOWER SILL IAW EMB 145 SRM 51-40-02.

Part: PROFILE — CORRODED (ESCAPE HATCH) · corrosion level 2 · airframe 38,065 hrs · 32,960 cycles

RIGHT CABIN ESCAPE HATCH LOWER L PROFILE CORRODED CORROSION LEVEL 2. C/A-R & R RT CABIN ESCAPE HATCH LOWER L PROFILE IAW EMB 145 SRM 51-40-02.

Part: RIB — CRACKED (RT WING) · airframe 38,065 hrs · 32,960 cycles

RIGHT WING RIB 21 IS CRACKED 1 CRACK, 0.3 IN LENGTH. C/A-PERFORMED REPAIR AT THE RT WING RIB 21 IAW EMB 145 SRM 57-20-07 ITEM 4. FIG 203.

Part: PROFILE — CORRODED (ESCAPE HATCH) · corrosion level 2 · airframe 38,065 hrs · 32,960 cycles

LEFT CABIN ESCAPE HATCH LOWER L PROFILE CORRODED CORROSION LEVEL 2. C/A-R & R LT CABIN ESCAPE HATCH LOWER FRAME L PROFILE IAW EMB 145 SRM 51-40-02.

Part: BUSHING — MIGRATED (RT SPLR HINGE) · airframe 38,065 hrs · 32,960 cycles

RIGHT WING SPOILER OUTBD HINGE HAS MIGRATED BUSHING-C/A-REMOVED AND REPLACED RT WING OUTBD SPOILER HINGE FITTING IAW EMB 145 SRM 51-20-03,51-40-02 AND AMM 20-10-01.

Part: YOKE — CRACKED (RT ENGINE MOUNT) · airframe 38,065 hrs · 32,960 cycles

RIGHT ENGINE FWD YOKE LOWER FWD SIDE CRACKED. 1 CRACK .25" IN LENGTH. C/A-REMOVED AND REPLACED RT ENGINE FWD LOWER YOKE FITTING IAW ERS-EM-54MR-698.

Part: RIB — CRACKED (LT WING) · airframe 38,065 hrs · 32,960 cycles

LEFT WING RIB 21 IS CRACKED. 1 CRACK . 0.3 IN LENGTH. C/A-PERFORMED REPAIR AT THE LT WING RIB 21 IAW EMB 145 SRM 57-20-07 ITEM 4. FIG 203.

Part: YOKE — CRACKED (LT ENGINE) · airframe 38,065 hrs · 32,960 cycles

LEFT ENGINE FWD YOKE LOWER FWD SIDE CRACKED. CRACK LENGTH .20 NUMBER OF CRACKS 1-C/A-REMOVED AND REPLACED LT ENGINE FWD LOWER YOKE FITTING IAW ERS-EM-54MR-698.

Part: SKIN — CRACKED (FUSELAGE) · airframe 38,065 hrs · 32,960 cycles

FUSELAGE UPPER AFT SKIN CRACKED AT FR 75 AT THE FIRST FASTENER BELOW STGR 2L 1 CRACK .25" IN LENGTH. C/A-ACCOMPLISHED A PERMANENT REPAIR OF FUSELAGE SKIN CRACK AT FR 75 BETWEEN STGR 2L-3L IAW ERS-EM-53MR-4269.

Part: LIGHT — BROKEN (CABIN FLOOR) · airframe 38,065 hrs · 32,960 cycles

FLOOR PANEL 231 AF EMERGENCY LIGHT ASSY BROKEN-C/A-COMPLETE:RAR COCKPIT STEP LIGHT ASSEMBLY ON PANEL 231AF IAW EMB 145 AMM 33-26-06. EASI #7606. OPC GOOD

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 38,065 hrs · 32,960 cycles

NUMBER 4 EMERGENCY LIGHT STRIP HAS BROKEN WIRE-C/A-COMPLETE:REMOVED AND REPLACED LH NUMBER 4 EMERGENCY LIGHT STRIP IAW EMB 145 AMM 33-50-12 OPS CHECK GOOD

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 37,837 hrs · 32,742 cycles

RT FWD OVERWING EMERGENCY LIGHT INOPERABLE. C/A: R & R RT FWD OVERWING EMERGENCY LIGHT LAMP, IAW EMB AMM 33-50-07-000-801-A AND 33-50-07-400-801-A. NO FIX R & R RT FWD OVERWING EMERGENCY LIGHT ASSEMBLY, IAW EMB AMM 33-50-07-000-802-A AND 33-50-07-400-802-A. NO FIX R & R NR 2 BATTERY AND CHARGER ASSEMBLY, IAW EMB AMM 33-50-04-000-801-A AND 33-50-04-400-801-A. OPERATIONS CHECK GOOD.

Part: CONNECTOR — INOPERATIVE (EMERGENCY LIGHTS) · airframe 37,637 hrs · 32,559 cycles

REF AML PAGE 4674487 ITEM NR 1 "SERVICE DOOR EMERGENCY LIGHT INOPERABLE" MEL 33-29 AUTH NR 100120D-C. C/A: REPLACED CONNECTOR P178 & REPAIRED WIRE AT PIN C OF CONNECTOR P7128, IAW SWPM 20-50-01 & 20-21-00 SERVICE DOOR EMERGENCY LIGHT. OPERATIONS CHECK GOOD, IAW EMB AMM 33-50-00. MEL ITEM RESTORED.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 37,636 hrs · 32,558 cycles

SERVICE DOOR EMERGENCY LIGHT INOPERABLE. C/A: R & R SERVICE DOOR EMERGENCY LIGHT LAMP, IAW AMM 33-50-09-000-801-A AND 33-50-09-400-801-A, NO FIX. FOUND SERVICE DOOR EMERGENCY LIGHT BROKEN WIRE, IAW WM 30-50-50-001. NEEDS WIRE AND CONNECTOR DEFERRED DUE TO LACK OF PARTS, PER MEL 33-29.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 37,636 hrs · 32,558 cycles

COCKPIT EMERGENCY LIGHT INOPERABLE. C/A: R & R COCKPIT EMERGENCY LIGHT LAMP, IAW EMB AMM 33-50-05-000-801-A AND 33-50-05-400-801-A. OPERATIONS CHECK GOOD.

Part: SIGN — INOPERATIVE (CABIN) · airframe 37,273 hrs · 32,147 cycles

CABIN OVERHEAD AFT FACING EMERGENCY EXIT SIGN INOP. REMOVED AND REPLACED CABIN OVERHEAD AFT FACING EMERGENCY EXIT SIGN IAW AMM 33-50-15. OPS CHECK GOOD.

Part: ROLLER — DEFECTIVE (DOOR FRAME) · airframe 37,213 hrs · 32,085 cycles

MAIN CABIN DOOR HARD TO OPEN. REMOVED AND REPLACED MAIN-DOOR FRAME ROLLER IAW AMM 53-21-02. OPS CHECK GOOD

Part: LIGHT — INOPERATIVE (CABIN) · airframe 37,184 hrs · 32,053 cycles

LH ESCAPE HATCH EMERGENCY EXIT LIGHT INOP-C/A- REMOVED AND REINSTALLED LH ESCAPE HATCH EMERGENCY EXIT LIGHT IAW EMB 145 AMM 33-50-14 OPS CHECK GOOD

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 37,156 hrs · 32,010 cycles

DURING PS-1 CHECK FOUND RH FWD EXTERIOR EMERGENCY LIGHT INOP-C/A-REMOVED AND REPLACED LAMP ON RH FWD EXTERNAL EMERGENCY LIGHT REF AMM 33-50-10. OPS CHECK GOOD.

Part: SEAL — DAMAGED (CARGO DOOR) · airframe 36,203 hrs · 31,127 cycles

CABAIN PRESSURIZATION FAILED DURING CRUSE FLIGHT BOTH IN AUTO AND MANUAL MODE RECIVED AURAL WARING AT FL 250 WHEN CABIN REACHED 10000 FEET RAN CHECKLIST CABAIN MAXED OUT AT 13200 WHILE DESENDING PAX O2 DID NOT DEPLOY-C/A-INSP AC FOUND CARGO DOOR SEAL DAMAGED / MISSING DEFERRED PRESSURIZATION SYSTEM AUTO AND MANUAL MODES IAW MEL 21-19 M PROCEDURES C/W AUTH # 100704DM-C. REMOVED AND REPLACED CARGO DOOR SEAL IAW EMB 145 AMM 52-30-02 OPS AND LEAK CHECK GOOD MEL ITEM RESTORED MEL PROCEDURES RESTORED

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 36,022 hrs · 31,015 cycles

EMERG LT TURNED ON IN FLIGHT. ONLY ILLUMINATED THE FIRST ROW IN THE CABIN , THE COCKPIT JS, AND FA JS.-C/A-REMOVED AND REPLACED #1 (FWD) BATTERY PACK AND POWER SUPPLY AS PER AMM 33-50-04. OPS CHECK OK AS PER AMM 33-50-00. BATTERY CHARGER ASSY P/N 11-0049 S/N 24450

Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,973 hrs · 30,980 cycles

RT OVERWING EMERGENCY LIGHT INOP. C/A-REMOVED AND REPLACED RT OVERWING EMERGENCY LIGHT LAMP IAW AMM 33-50-07. OPS CHECKS GOOD NO FURTHER DEFECTS NOTED.

Part: HANDLE — UNSECURE (EMERGENCY EXIT) · airframe 35,850 hrs · 30,887 cycles

FAA REPORT EMERG EXIT DOOR HANDLE AT ROW 12A FELL OFF. C/A-REINSTALL EMERG EXIT DOOR HANDLE AT ROW 12A AS REQURIED.

Part: UNKNOWN — ODOR (CABIN & COCKPIT) · airframe 35,521 hrs · 30,579 cycles

SUPPLEMENTAL WHILE LEVEL AT FL240 AN ELECTRICAL FUMES SMELL IN THE COCKPIT AND PASSENGER CABIN. RAN EPC AND QRH AND FUMES WENT AWAY. NO VISUAL HAZE. C/A- TROUBLESHOT CABIN AND COCKPIT ODOR AND FOUND NO DEFECTS NOTED IAW FIM TASK 21-20-00-810-801A. ALSO ACCOMPLISHED ETN-EM-72-034 WITH NO DEFECTS NOTED. PERFORMED GVI OF INSTRUMENT PANEL, PEDESTAL, LT/RT SIDE CONSOLES, AND LT/RT ELECTRICAL POWER DISTRIBUTION BOXES. NO ODORS PRESENT. FCF FOUND SATISFACTORY.

Part: INDICATOR — INOPERATIVE (CABIN PRESSURE) · airframe 35,348 hrs · 30,404 cycles

CABIN ALTITUDE & CABIN RATE INDICTION INOPERATIVE. PERFORMED ELECTRICAL RESET OF A/C ELECTRICAL SYSTEM IAW FIM TASK 24-20-00, OPS CHECK GOOD NO DEFECTS NOTED. A/C OK FOR SERVICE.

Part: SKIN — GOUGED (FUSELAGE) · airframe 35,182 hrs · 30,253 cycles

4238 ORF-ORD N902 AIRCRAFT DAMAGE ON RT FUSELAGE 2 SCRATCHES ON LOWERCASE "A" ON RIGHT SIDE OF AIRCRAFT. C/A-INSPECTED TWO GOUGES ON LOWERCASE "A" OF AMERICAN LOGO ON RT FUSELAGE, IAW SRM 53-22-01. SEE ITEM#2 AT THIS AML PAGE FOR CORRECTIVE ACTION.

Part: WIRE — BROKEN (EXTERIOR LIGHT) · airframe 35,112 hrs · 30,183 cycles

SERVICE DOOR EXTERNAL EMERGENCY LIGHT INOP. C/A-REMOVED AND REPLACED SERVICE DOOR EXTERNAL EMERGENCY LIGHT LAMP IAW AMM 33-50-10-000-801-A AND 33-50-10-400-801-A. NO FIX. FOUND BROKEN WIRE AND SPLICED WIRE IAW SWPM 20-21-00. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED.

Part: GASPER FAN — FAILED (CABIN) · airframe 35,077 hrs · 30,154 cycles

SUPPLEMENTAL STRONG ODOR FUMES IN COCKPIT AND CABIN. "TRANSFERRED TO NRWC 902-MIA-03935"-C/A- REMOVED AND REPLACED RECIRCULATION FAN NR 1 LT SIDE IAW AMM 21-24-01. OPS CHECK GOOD. BORROWED 1/2" TORQUE WRENCH P/N: M100-1 S/N: WRE9175 EXP DATE: 07/09/20.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 34,949 hrs · 30,049 cycles

RH WING FWD EXTERIOR EMERGENCY LIGHT INOP-C/A-REMOVED AND REPLACED RH WING FWD EXTERIOR EMERGENCY LIGHT LAMP IAW AMM 33-50-10-000-801-A AND 33-50-10-400-801-A. OPS CHECK GOOD. END.

Part: BRACKET — EXCESS PLAY (LT MLG DOOR) · airframe 34,716 hrs · 29,842 cycles

AFTER TAKEOFF LG AIR/GND FAIL ON EICAS, MESSAGE DID NOT GO AWAY, UPON LANDING EVERYTHING WORKED AS NORMAL "TRANSFERRED TO NRWC 902-MIA-03838". C/A-REMOVED AND REPLACED LT MLG DOOR SUPPORT/PROX SWITCH BRACKET IAW CMM 32-10-01. INSTALLED LT MLG DOOR FITTING ASSY IAW CMM 32-10-01. PERFORMED PROX SWITCH PROXIMITY CHECK IAW AMM 32-63-08. AIRCRAFT OK FOR SERVICE. JACKED AIRCRAFT IAW AMM 07-10-00 AN PERFORMED CLEARANCE ADJUSTMENT CHECK IAW AMM 32-63-05. LOWERED AIRCRAFT IAW AMM 7-10-00. REMOVED BRAKE OUT BOX GSE 344 TO LEGU IAW AMM 32-63-05. PERFORMED CMC DOWNLOAD IAW W/C #45-900-00. INSPECTED LT GEAR AND FOUND PROX SWITCH/DOOR SUPPORT BRACKET HAS EXCESSIVE PLAY.

Part: ROLLER — CONTAMINATED (CABIN DOOR) · airframe 34,327 hrs · 29,483 cycles

MAIN CABIN DOOR LATCH HANDLE HARD TO OPEN DOOR. C/A-FOUND RESIDUE ON MAIN CABIN DOOR ROLLERS CLEANED AND LUBED DOOR ROLLERS IAW AMM53-21-02. OPS CHECK GOOD.

Part: SEAL — DAMAGED (PAX DOOR) · airframe 34,149 hrs · 29,305 cycles

F/A HAVING DIFFICULTY CLOSING AND UNABLE TO OPEN DOOR W/O ASSISTANCE FROM THE AGENT ON THE BRIDGE-C/A-FOUND MAIN PAX DOOR FRAME SEAL DAMAGED AND INHIBITING PROPER OPERATION OF THE MAIN PAX DOOR. RAR MAIN PAX DOOR FRAME SEAL IAW EMB 145 AMM 53-21-01. PRESSURIZATION CHECK GOOD MAIN DOOR TESTS GOOD IAW EMB 145 AMM 52-18-00. SEE NRWC 902-ORD-03700 FOR WORK PERFORMED.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 34,047 hrs · 29,200 cycles

SERVICE DOOR EXTERNAL EMERGENCY LIGHT INOP-C/A-RAR SVC DOOR HINGE EXTERNAL EMERGENCY LAMP IAW EMB AMM 33-50-10-000-801-A/33-50-10-400-801-A OPC GOOD

Part: UNKNOWN — ODOR (CABIN) · airframe 33,818 hrs · 28,955 cycles

FA REPORTS BURNING SMELL COMING FROM FORWARD TO MID CABIN. C/A-PERFORMED ETN- EM-72-034. COULDN'T REPLICATE DISCREPANCY OF RUBBER BURNING SMELL ANYWHERE IN COCKPIT OR CABIN.

Part: ROLLER — DIRTY (CABIN DOOR) · airframe 33,758 hrs · 28,892 cycles

F/A HAVING DIFFICULTY CLOSING AND ESPECIALLY OPENING THE MAIN CABIN DOOR. -C/A-FOUND 2 FROZEN ROLLER ON AFT PART OF MAIN CABIN DOOR. CLEANED AND LUBRICATED ROLLERS NO DEFECTS NOTED. REF AMM 53-21-02.

Part: BUSHING — DAMAGED (PAX DOOR) · airframe 33,373 hrs · 28,548 cycles

F/A REPORTS DIFFICULTY OPENING AND CLOSING THE MAIN CABIN DOOR. REMOVED WORN HARDWARE, BUSHINGS, AND BELLCRANK FROM MAIN PAX DOOR SUPPORT LINK. INSTALLED NEW HARDWARE, PLAIN BUSHING, AND BELLCRANK ASSY ON SUPPORT LINK ASSY. OPS AND LEAK CHECKED GOOD. REMOVED AND REPLACED THE PAX DOOR UPPER HINGE FITTING BUSHINGS IAW AMM 52-18-00, INSTALLATION TASK I. STEPS 4 AND 6.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,306 hrs · 28,486 cycles

CARGO DOOR CUT OUT LOWER SILL CORRODED. BLENDED MULTIPLE SPOTS OF CORROSION ON LOWER CARGO DOOR SILL IAW SRM 51-10-03, DETERMINED TO BE OUT OF SRM 53-31-15 LIMITS. REMOVED LOWER SILL IAW SRM 51-40-02. LOCATED, DRILLED AND ALODINED NEW LOWER SILL IAW SRM 51-20-03 AND CPM 51-21-04. INSTALLED NEW LOWER SILL IAW SRM 51-40-02. APPLIED SURFACE PROTECTION IAW CPM 51-21-05, 51-21-06 AND ETN GN-51-017.

Part: TRUNNION — CORRODED (LT MLG) · corrosion level 2 · airframe 33,306 hrs · 28,486 cycles

LEFT MLG AFT UPPER TRUNNION WAS PITTIED IN THE BEARING TRACK. REMOVED AND REPLACED THETRUNNION IAW TI-145-18-181LH, ETD-2018-145-072655, AND EM-57-167

Part: CONNECTOR — MISSING (CABIN) · airframe 33,306 hrs · 28,486 cycles

CENTER AISLE EMERGENCY LIGHT STRIP ON FLOOR BOARD PANEL 241DF IS MISSING ELECTRICAL CONNECTOR. REPLACED MISSING CONNECTOR FOR NR 3 CENTER AISLE EMERGENCY LIGHT STRIP IAW SWPM 20-21-00. PIN FEMALE P/N M39029/32-247.

Part: FITTING — CORRODED (FUSELAGE) · airframe 33,306 hrs · 28,486 cycles

FRAME 65 CARGO DOOR CUT OUT STRUCTURE LOWER FWD CORNER SHEAR CLIP CORRODED. BLENDED CORRODED SHEAR CLIP, FOUND TO BE OUT OF LIMITS IAW SRM 51-31-04. REMOVED SHEAR CLIP IAW SRM 51-40-02. LOCATED, DRILLED AND ALODINED NEW SHEAR CLIP IAW SRM 51-20-03 AND CPM 51-21-04. INSTALLED NEW SHEAR CLIP IAW SRM 51-40-02 AND APPLIED SURFACE PROTECTION IAW CPM 51-21-04, 51-21-05, 51-21-06 AND ETN GN-51-017.

Part: FITTING — CORRODED (FUSELAGE) · airframe 33,306 hrs · 28,486 cycles

FRAME 68 CARGO DOOR CUT OUT STRUCTURE LOWER FWD CORNER SHEAR CLIP CORRODED. BLENDED CORRODED SHEAR CLIP, FOUND TO BE OUT OF LIMITS IAW SRM 51-10-03 AND 51-31-04. REMOVED SHEAR CLIP IAW SRM 51-40-02. LOCATED, DRILLED AND ALODINED NEW SHEAR CLIP IAW SRM 51-20-03 AND CPM 51-21-04. INSTALLED NEW SHEAR CLIP IAW SRM 51-40-02 AND APPLIED SURFACE PROTECTION IAW CPM 51-21-04, 51-21-05, 51-21-06 AND ETN GN-51-017.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 33,306 hrs · 28,486 cycles

FRAME 65 CARGO DOOR CUT OUT STRUCTURE CORRODED IN THE LOWER FWD CORNER. BLENDED CORROSION ON FRAME 65 , FOUND TO BE OUT OF LIMITS IAW SRM 51-10-03 AND 51-31-04. CUT OUT DAMAGED AREA IAW SRM 53-31-04, PERFORMED HFEC INSP ALONG CUT LINES IAW NDTM 51-00-00-916-801-A00, NO DEFECTS NOTED. FABRICATED DOUBLER IAW SRM 53-31-04. LOCATED, DRILLED, ALODINED AND PRIMED NEW FRAME PIECE AND DOUBLER IAW SRM 53-31-04 AND CPM 51-21-04AND 51-21-05 INSTALLED NEW FRAME PIECE AND DOUBLER IAW SRM 53-31-04 AND 51-40-02. APPLIED SURFACE PROTECTION IAW CPM 51-21-05, 51-21-06 AND ETN GN-51-017.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 33,306 hrs · 28,486 cycles

RT OMEGA BEAM BETWEEN FRAMES 60 AND 61 HAS TWO CRACKS MIGRATING FROM THE HOLE FOR THE NUTPLATE. REMOVED DAMAGED AREA OF OMEGA BEAM BY CUTTING IAW SRM 53-24-10. PERFORMED HFEC INSP OF CUTOUT IAW NDTM 51-00-00-916-801-A00, NO DEFECTS NOTED. FABRICATED REPAIR DOUBLER, PERFORMED FPI OF DOUBLER IAW ASTM E1417 TYPE 1, METHOD A SENSITIVITY LEVEL 3, NO DEFECTS NOTED. INSTALLED DOUBLER IAW EMB 145 SRM 53-24-10 AND 51-40-02.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,306 hrs · 28,486 cycles

FWD SERVICE DOOR CUT OUT STRUCTURE THRESHOLD LOWER HORIZONTAL BEAM HAS SPOTS OF CORROSION BETWEEN FRAMES 20 AND 22. BLENDED CORROSION ON LOWER SILL IAW SRM 51-10-03, DETERMINED TO BE OUT OF SRM LIMTS. REMOVED LOWER SILL IAW SRM 51-40-02. INSTALLED NEW LOWER SILL IAW SRM 51-40-02. PRIMED AND TOPCOATED FASTENERS AND APPLIED CIC IAW EMB CPM 51-20-05, 51-21-06 , ETN EM-51-091 AND CPM 51-61-00.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,306 hrs · 28,486 cycles

RT OMEGA BEAM AT FRAME 59 CORRODED AROUND HOLE FOR NUTPLATE. REMOVED DAMAGE BY CUTTING IAW SRM 53-24-10. PERFORMED HFEC INSP OF CUT OUT AREA IAW NDTM 51-00-00-916-801-A00 NO DEFECTS NOTED. FABRICATED REPAIR DOUBLER FROM 2024 T3 0.040IAW SRM 53-24-10. PERFORMED FPI OF REPAIR DOUBLER IAW ASTM E1417 TYPE 1 METHOD A SENSITIVITY LEVEL 3. NO DEFECTS NOTED. LOCATED AND DRILLED DOUBLER IAW SRM 53-24-10. ALODINED, AND PRIMED DOUBLER AND CUT OUT AREA IAW CPM 51-21-04 AND 51-21-05. INSTALLED REPAIR DOUBLER ON RT OMEGA BEAM AT FRAME 59 IAW SRM 53-24-10 AND 51-40-02

Part: ROLLER — LACK OF LUBE (PAX DOOR) · airframe 33,141 hrs · 28,313 cycles

MAIN CABIN DOOR HARD TO OPEN. LUBRICATED THE PAX DOOR ROLLERS IAW AMM 52-11-00, PERFORMED A DOOR ACTUATING HANDLE TEST IAW AMM 52-18-00, EM-52-029. OPS CHECKED GOOD. THE DOOR OPENS AT 35 LBS.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 32,740 hrs · 27,940 cycles

LT AND RT OVERWING EMERGENCY LIGHTS FOUND INOPERATIVE. REMOVED AND REPLACED THE NR 4 BATTERY AND CHARGER ASSEMBLY IAW FIM 33-50-00-810-804-A, AND AMM 33-50-10. OPS CHECKED GOOD,

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 32,652 hrs · 27,855 cycles

LEFT AND RIGHT EXTERIOR AFT OVERWING EMERGENCY LIGHTS INOPERATIVE. PERFORMED TROUBLESHOOTING OF EXTERIOR AFT OVERWING EMERGENCY LIGHTS IAW WMM 33-50-50. R & R THE NR 4 EMERGENCY LIGHT BATTERY AND CHARGER ASSY IAW AMM 33-50-04. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (SEAT 8 & 9) · airframe 32,588 hrs · 27,814 cycles

FLOOR EMERGENCY LIGHT BETWEEN SEATS 8, & 9 INOPERATIVE. INSTALLED A NEW LIGHT IAW AMM 35-50-12. OPS CHECKED SATISFACTORY.

Part: LIGHT — INOPERATIVE (SEATS 3-5) · airframe 32,588 hrs · 27,814 cycles

FLOOR EMERGENCY LIGHT BETWEEN SEATS 3, 4, AND 5A INOPERATIVE. REMOVED AND REPLACED FLOOR EMERGENCY STRIP LIGHT IAW EMB AMM 33-50-12. OPC SATISFACTORY. OPC GOOD. NO FURTHER DEFECTS NOTED.

Part: INVERTER — FAILED (EMERGENCY LIGHTS) · airframe 32,560 hrs · 27,789 cycles

FLOOR EMERGENCY LIGHT AT SEATS 3, 4, & 5A INOPERATIVE. TROUBLESHOT THE EMERGENCY LIGHT IAW WMM 33-50-50. REMOVED AND REPLACED THE EMERGENCY LIGHT INVERTERS NR 3 AND 5 IAW AMM 33-50-11. OPS CHECKED GOOD IAW AMM 33-50-00.

Part: OUTFLOW VALVE — DEACTIVATED (CABIN PRESSURE) · airframe 32,378 hrs · 27,603 cycles

LOST PRESSURIZATION AT FL 240. REACTVATION PROCEDURE FOR ELECTRONEUMATIC OUTFLOW VALVE PERFORMED. OPS TESTED IAW AMM 21-30-00. NORMAL.

Part: WARNING LIGHT — FALSE ACTIVATION (LAVATORY) · airframe 32,278 hrs · 27,511 cycles

LAVATORY SMOKE WARNING DURING CRUISE, FA SMELLED SMOKE IN THE LAVATORY, WARNING PERSISTED UNTIL ACFT POWERED DOWN. PERFORMED ETN-EM-72-034 ENG ODOR EVENT TROUBLESHOOTING SUPPLEMENT. NO ODOR OR SMOKE DETECTED IN CABIN, COCKPIT, OR LAVATORY. FCF FOUND SATISFACTORY

Part: BATTERY — DISCHARGED (CABIN) · airframe 31,531 hrs · 26,715 cycles

EMERGENCY FLOOR PATH STRIPS 2 AND 3 INOP. REMOVED AND REPLACED NR 2 EMERGENCY BATTERY AND POWER SUPPLY IAW MX WC 33-700-19.

Part: HOSE — FAILED (HYD SYSTEM) · airframe 29,950 hrs · 25,275 cycles

IN FLIGHT HYD LOW QTY E1 HYD PUMP FAIL. REMOVED AND REPLACED E1 HYD PRESSURE HOSE IAW AMM 29-10-03. OPS AND LEAK CHECKED GOOD. NO DEFECTS NOTED.

Part: ACM — SEIZED (NR 2) · airframe 29,224 hrs · 24,616 cycles

CRUISE ALTITUDE OF 25000 FT, DENSE SMOKE THRU COCKPIT VENTS AS WELL AS CABIN. SMOKE CLEARED AT 18000 FT. FOUND NR 2 ACM SEIZED. REMOVED AND REPLACED NR 2 ACM IAW MM 21-51-03. OPS AND LEAK CHECKED GOOD. NO SMOKE NOTED. COMPLIED WITH ENGINE ODOR EVENT T/S PER ETN-EM-72-034. NO ODOR NOTICED.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 28,648 hrs · 24,108 cycles

CARGO DOOR CUT OUT LOWER FLOOR SILL CORRODED. INSTALLED SERVICEABLE CARGO DOOR CUT OUT LOWER FLOOR SILL IAW SRM 51-40-02.

Part: FITTING — CORRODED (FUSELAGE) · airframe 28,648 hrs · 24,108 cycles

FRAME 68 SHEAR CLIP CORRODED LOWER AFT CORNER OF CARGO DOOR CUT OUT. REPAIRED SHEAR CLIP AT FRAME 68 IAW SRM 53-31-04 & ETN EM-53-272.

Part: WIRE — DAMAGED (CABIN) · airframe 28,579 hrs · 24,045 cycles

SERVICE DOOR EMER LIGHT IS INOPERATIVE. SEE IPC 33-50-10 FIGURE 40 FOR LOCATION. REPAIRED WIRE W716-0007 IAW SPWM 20-21-00. OPERATIONS CHECKED GOOD.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 28,494 hrs · 23,968 cycles

FORWARD EMER FLOOR STRIP INOPERATIVE. R & R EMER LIGHTING INVERTOR NR 2 IAW AMM 33-50-11. OPERATIONS CHECKED GOOD IAW AMM 33-50-00.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 27,918 hrs · 23,466 cycles

FLOOR PROX LIGHTS 6, 7 & 8 INOPERATIVE. R & R NR 6 INVERTER IAW AMM 33-50-11. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,918 hrs · 23,466 cycles

FLOOR PROX LIGHT 1 INOPERATIVE. R & R FLOOR PROX LIGHT 1 STRIP IAW AMM 33-50-12. OPERATIONS CHECKED GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 27,668 hrs · 23,238 cycles

AFT EMER LIGHT FLOOR STRIPS INOPERATIVE. REPLACED NR 4 BATTERY & POWER CHARGER ASSEMBLY IAW AMM 33-50-04. OPERATIONS CHECKED GOOD. CHARGER ASSEMBLY BATTERY PN BA5-0933-901, SN C00513.

Part: FCU — FAILED (APU) · airframe 27,126 hrs · 22,682 cycles

WHEN APU BLEED SELECTED, A STRONG ODOR OF FUEL WAS IN ACFT. ALSO FUEL DRIPPING FROM TAIL CONE ON POST FLIGHT. R & R FUEL CONTROL ASSEMBLY IAW CMM 49-32-01. OPS CHECKED GOOD, NO LEAKS NOTED.

Part: DOOR SEAL — DIRTY (CABIN DOOR) · airframe 26,895 hrs · 22,489 cycles

CLIMBING THRU 10,000, FLIGHT ATTENDANT REPORTS EXTREMELY LOUD WHISTLING COMING FROM EITHER SERVICE DOOR OR MAIN DOOR. AS WE CONTINUE TO CLIMB WHISTLING NOISE IS GETTING WORSE. CLEANED PAX DOOR SEAL & SERVICE DOOR SEAL IAW AMM 52-00-04. PERFORMED OPERATIONS CHECK & NO LEAKS NOTED AT THIS TIME IAW AMM 21-31-00.

Part: CAP — OUT OF POSITION (ANTI-ICE SYSTEM) · airframe 26,537 hrs · 22,183 cycles

E2 ANTI-ICE FAIL DURING PNEUMATIC TEST IN CLIMB TWICE. GAINED ACCESS TO E2 ANTI-ICE VLV & FOUND ANTI-ICE VLV PRESS TRANSDUCER MANIFOLD PRESS TEST PORT CAP NOT INSTALLED. LOCATED & INSTALLED PORT CAP & TIGHTENED. PERFORMED OPERATIONAL CHECK OF E2 ANTI-ICE IAW AMM 30-21-00-700-803-A. OPERATIONAL TESTED NORMAL, NO FURTHER DEFECTS NOTED. SECURED PANEL 422AT AS REQUIRED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,475 hrs · 22,125 cycles

OVERHEAD EMER LIGHT AT ROW 3 INOPERATIVE. R & R OVERHEAD EMER LAMP AT ROW 3 IAW TASK 33-50-08-000-801-A & TASK 33-50-08-400-801-A. OPERATIONS CHECKED GOOD.

Part: MOUNT BRACKET — BROKEN (FLASHLIGHT) · airframe 26,222 hrs · 21,852 cycles

FLIGHT DETECTOR EMER FLASHLIGHT ON BULKHEAD, MOUNTING BRACKET BROKEN. R & R CAPTAINS FLASHLIGHT BASE ASSEMBLY IAW AMM 33-51-01. OPERATIONS CHECKED GOOD.

Part: RETURN SPRING — FAILED (RUDDER PEDAL) · airframe 25,462 hrs · 21,218 cycles

LOST RT BRAKE, BRAKE STUCK IN PUSH DOWN. R & R RT RUDDER PEDAL RETURN SPRING IAW 27-21-00. OPERATIONS CHECKED GOOD.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 24,364 hrs · 20,207 cycles

DIAMOND GUSSET ON RT FLOORBEAM & FRAME 20 IS CORRODED. R & R DIAMOND GUSSET ON RT FLOORBEAM & FRAME 20 IAW SRM 51-20-01, 51-40-02 & 51-20-03. RESTORED SURFACE PROTECTION TO DIAMOND GUSSET ON RT FLOORBEAM & FRAME 20 IAW CPM 51-21-06 & ETN'S GN-51-011R4, EM-51-075 & EM-51-091R5.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 24,364 hrs · 20,207 cycles

STRINGER 21R IS CORRODED BETWEEN FRAMES 12 - 13. REMOVED & INSTALLED NEW STRINGER 21R IAW SRM 51-40-02, SEE TURNOVER FOR DETAILS.

Part: FRAME — CRACKED (ACCESS HATCH) · airframe 24,364 hrs · 20,207 cycles

COCKPIT UNDERFLOOR ACCESS HATCH FRAME IS CRACKED UNDER ATTACHMENT PIN BRACKET. COMPLIED WITH ERS-EM-5200-140.

Part: CONNECTOR — BROKEN (CABIN) · airframe 24,364 hrs · 20,207 cycles

PANEL 811XW EMERGENCY LIGHT CONNECTOR BROKEN. R & R ELEC CONNECTOR, PLASTIC FEMALE RECEPTACLE ONLY, ON PAX DOOR EMERGENCY LIGHT, PANEL 811XW IAW SWPM 20-50-00 & 20-21-00 & IAW AMM 33-50-00. OPERATIONAL TEST GOOD.

Part: ENGINE — MALFUNCTIONED (NR 2) · airframe 23,954 hrs · 19,885 cycles

AFTER TAKEOFF AT 1500 FEET LAVATORY SMOKE WARNING ON EICAS. RETURNED TO KCMH. FLIGHT ATTENDANT REPORTED SMOKE IN LAST 3 ROWS. ACCOMPLISHED FIM ASK 21-20-00, FOUND SMALL AMOUNT OF DEICING FLUID AT NR 2 ENG AIR INLET. CLEANED AS REQUIRED, RUN ENG IAW ETN-EM-72-034. NO SMOKE& NO WARNING, OPERATIONS CHECKED GOOD. REMOVED AND REPLACED NR 2 ENG IAW 71-000-00. ALL LEAK AND OPS CHECKS GOOD.

Part: HOLDER — BROKEN (FLASHLIGHT) · airframe 23,907 hrs · 19,850 cycles

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

Part: SKIN — PUNCTURED (FUSELAGE) · airframe 23,277 hrs · 19,341 cycles

TRANSFERRED FROM AML PAGE 3483333 ITEM 1. 8 INCH LONG SCRATCH WITH PUNCTURE UNDER NR 2 ENG RT SIDE AFT FUSELAGE. COMPLETED REPAIR OF RT SIDE AFT FUSELAGE IAW SRM 53-31-01 PRESSURIZATION LEAK CHECKED GOOD.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 22,555 hrs · 18,759 cycles

PASS COMPT FWD EMERGENCY LIGHT WILL NOT ILLUMINATE. FOUND LOOSE CONNECTOR FOR CABIN FWD EMERGENCY LIGHT IAW AMM 33-50-12. OPS CHECKED GOOD.

Part: ROLLER — LACK OF LUBE (MAIN DOOR) · airframe 22,540 hrs · 18,750 cycles

MAIN CABIN DOOR HARD TO OPEN AND CLOSE. INSPECTED MAIN CABIN DOOR AND FOUND ALL 4 GUIDE ROLLERS VERY DRY CLEANED AND LUBRICATED ROLLER OPS. CK OF OPENING AND CLOSING MECHANISM WORKING NORMAL IAW AMM 52-10-00.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 21,573 hrs · 17,979 cycles

DURING MAINTENANCE INSPECTION FOUND THE FORWARD EMERGENCY FLOOR LIGHT STRIP INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. RECONNECTED CONNECTOR. THE OPERATIONAL CHECK WAS NORMAL IAW EMB145 33-50-12. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: DOOR SEAL — OBSTRUCTED (CABIN DOOR) · airframe 21,357 hrs · 17,800 cycles

ON FLIGHT 42408 THE FLIGHT ATTENDANT REPORTED A LOUD SQUEAL FROM THE MAIN CABIN DOOR AND COULD SEE LIGHT THROUGH GAP IN DOOR SEAL. SAME NOISE WAS HEARD FROM FLIGHT DECK. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED SECURITY STICKERS FROM PASSENGER DOOR/FRAME INTERFACE. DOOR FRAME SEAL APPEARS OTHERWISE SOUND AS PER EMB AMM 53-21-01. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 21,139 hrs · 17,612 cycles

DURING B INSPECTION FOUND THE SERVICE DOOR EXTERNAL EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE SERVICE DOOR EXTERNAL EMERGENCY LIGHT BULB IAW EMB AMM 33-50-10. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SENSOR — DEFECTIVE (BLEED AIR SYS) · airframe 20,759 hrs · 17,312 cycles

ON FLIGHT 4198 THE CREW REPORTED THEY RECEIVED A BLEED 1 OVERTEMP MESSAGE. THE CREW COMPLIED WITH AOM PROCEDURES AND NOTIFIED SOC, OPS & FLIGHT ATTENDANT. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. TROUBLESHOT IAW EMB 145 FIM 36-11-00-810-803A FOUND BAGGAGE COMPARTMENT OUTLET TEMP SENSOR BAD REMOVED AND REPLACED IAW EMB 145 AMM 36-20-01 PERFORMED OPC IAW EMB 145 AMM 36-00-00-700-803-A OPC GOOD NO FURTHER DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 20,589 hrs · 17,173 cycles

DURING POST FLIGHT INSPECTION FOUND THE CAPTAIN’S FLASHLIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CAPTAIN’S FLASHLIGHT ASSEMBLY IAW EMB 145 AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BULB — UNSERVICEABLE (EMERGENCY LIGHT) · airframe 19,851 hrs · 16,625 cycles

DURING MAINTENANCE INSPECTION, FOUND SERVICE DOOR EMERGENCY LIGHT INOPERATIVE. THE AIRCRAFT WAS REMOVE FROM SERVICE. REMOVED AND REPLACED BULB IAW MM 33-50-09. OPS CHECKED GOOD IAW MM 33-50-00. THE AIRCRAFT RETURN TO SERVICE.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 19,765 hrs · 16,570 cycles

DURING B INSPECTION, FOUND THE LEFT AFT EXTERNAL OVERWING EXIT EMERGENCY LIGHT INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 4 BATTERY POWER SUPPLY IAW AMM 33-50-04 AND PERFORMED OPS CHECK IAW AMM 33-50-00. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 19,765 hrs · 16,570 cycles

DURING B INSPECTION, FOUND THE RIGHT AFT EXTERNAL OVERWING EXIT EMERGENCY LIGHT INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 4 BATTERY POWER SUPPLY IAW AMM 33-50-04 AND PERFORMED OPS CHECK IAW AMM 33-50-00. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,703 hrs · 16,520 cycles

DURING MAINTENANCE INSPECTION, FOUND THE LEFT NR 8 EMERGENCY LIGHT STRIP INOPERATIVE. AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED LEFT NR 8 EMERGENCY LIGHT IAW AMM 33-50-12. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SKIN — GOUGED (FUSELAGE) · airframe 19,704 hrs · 16,520 cycles

CARGO DOOR CUTOUT AT FRAME 65 HAS DEEP GOUGE. R & R LOWER SECTION OF CARGO DOOR CUTOUT AT FRAME 65 SHEAR CLIP IAW EM-53MR-2001.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 19,713 hrs · 16,529 cycles

DURING B INSPECTION, FOUND THE LEFT CARBON CROSSBEAM SUPPORT ON FRAME 61 CORRODED LOWER FORWARD CORNER. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT CARBON CROSSBEAM SUPPORT ON FRAME 61 IAW SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE.

Part: HANDLE — CRACKED (PAX DOOR) · airframe 19,704 hrs · 16,520 cycles

MAIN DOOR INNER HANDLE BRACKET CRACKED, UPPER AFT CORNER. INSTALLED REPAIR DOUBLER ON MAIN DOOR INNER HANDLE BRACKET IAW EO-EM-52MR-250.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 19,704 hrs · 16,520 cycles

CARGO DOOR CUTOUT AT FRAME 68 SHEAR TIE CORRODED AT LOWER END. REPAIRED SHEAR TIE IAW EO EM-53MR-1129.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 19,713 hrs · 16,529 cycles

DURING MAINTENANCE INSPECTION, FOUND THE NR 1 FLOOR PROXIMITY LIGHT HAS A BROKEN WIRE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 1 FLOOR PROXIMITY LIGHT IAW AMM 33-50-12. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,670 hrs · 16,496 cycles

DURING B INSPECTIONS FOUND THE EMERGENCY FLOOR STRIP AT 11A INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY FLOOR STRIP AT 11A IAW EMB AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD IAW EMB WC 33-700-17. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE — BROKEN (CABIN) · airframe 19,670 hrs · 16,496 cycles

DURING B INSPECTIONS FOUND THE AFT EMERGENCY LIGHT FLOOR STRIP HAS LEAD BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. INSTALLED WIRE SPLICE CONNECTOR AT AFT EMERGENCY FLOOR STRIP (PLANE SIDE) IAW WM 20-21-00. OPERATIONAL CHECK REF NRWC 902-SGF-00809. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — BROKEN (COCKPIT) · airframe 19,282 hrs · 16,171 cycles

DURING B INSPECTION FOUND THE CO-PILOT FLASHLIGHT ASSEMBLY BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FLASHLIGHT ASSEMBLY IAW EMB 145 AMM33-50-16-000-801-A AND 33-50-16-400-801-A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — BROKEN (CABIN) · airframe 18,817 hrs · 15,841 cycles

DURING B-INSPECTION FOUND THE MAIN DOOR FLASHLIGHT BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED FLASHLIGHT IN REFFERENCE WITH TASK 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CRADLE — BROKEN (CABIN) · airframe 18,015 hrs · 15,240 cycles

DURING MAINTENANCE BASE VISIT FOUND THE FORWARD FLIGHT ATTENDANT FLASHLIGHT CRADLE BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FORWARD FLIGHT ATTENDANT FLASHLIGHT ASSEMBLY IAW EMB 145 AMM 33-50-16-000-801-A/33-50-16-400-801-A. THE OPERATIONAL CHECK WAS GOOD AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 14,711 hrs · 12,748 cycles

DURING MAINTENANCE BASE VISIT MISDRILLED HOLE ON FRAME 66, RIGHT SIDE AT STRINGER 16 RIGHT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED FRAME IAW SRM 53-00-04 FIG 206. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: A/C PACK — INOPERATIVE (NR 2) · airframe 14,498 hrs · 12,571 cycles

ON FLIGHT 3636 THE CREW REPORTED THAT THE NUMBER 2 PACK WAS INOPERABLE AT FLIGHT LEVEL 23000 AND WOULD NOT RESET. THE CAPTAIN DECLARED AN EMERGENCY AND ELECTED TO DIVERT CAE. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. RE-ACTIVATED OUTFLOW VALVES IAW EMB AMM 21-31-04. THE OPERATIONAL CHECK WAS GOOD IAW EMB AMM TASK 21-31-00-700-804-A. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: DISPLAY — FAILED (EICAS) · airframe 13,389 hrs · 11,711 cycles

ON FLIGHT 4398 DURING THE DESCENT THE CREW REPORTED, SMELLED SMOKE IN THE COCKPIT. THE CREW PERFORMED THE PROCEDURES FOR COCKPIT SMOKE AND FUMES AND AIRCRAFT OPERATING MANUAL PROCEDURES. THE CREW DECLARED AN EMERGENCY AND LANDED IN ORD WITHOUT INCIDENT. THE CREW CANCELED THE EMERGENCY IN BOUND AFTER PARKING CHECKS NOTICED CIRCUIT BREAKER FOR EICAS WAS POPPED. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND THE EICAS DISPLAY UNIT TO BE THE CAUSE OF THE SMELL. REMOVED AND REPLACED THE EICAS DISPLAY UNIT IAW EMB MM 31-41-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BRAKE ASSY — FAILED (MLG) · airframe 11,180 hrs · 9,790 cycles

ON FLIGHT 3410, CREW REPORTED A BRAKE DEGRADE MESSAGE ON TAXI IN. AIRCRAFT REMOVED FROM SERVICE. FOUND NR 2 BRAKE ASSEMBLY AND SHUTTLE VALVE DAMAGED. REMOVED AND REPLACED NR 2 BRAKE ASSY AS PER EMB 145-WORK CARD 32-600-14 OPERATIONAL CHECK AND LEAK CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: BRAKE — FAILED (MLG) · airframe 11,180 hrs · 9,790 cycles

ON FLIGHT 3410, CREW REPORTED A BRAKE DEGRADE MESSAGE ON TAXI IN. AIRCRAFT REMOVED FROM SERVICE. FOUND NR 2 BRAKE ASSEMBLY AND SHUTTLE VALVE DAMAGED. REMOVED AND REPLACED NR 2 BRAKE ASSY AS PER EMB 145-WORK CARD 32-600-14. OPERATIONAL CHECK AND LEAK CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: TRANSDUCER — MALFUNCTIONED (ANTI ICE SYS) · airframe 7,336 hrs · 6,741 cycles

WING ANTI ICE FAIL ON CLIMB-OUT. ELECTED TO RETURN BACK TO ORD DUE TO WEATHER. REPLACED NUMBER 2 PRESS TRANSDUCER IAW EMB 145 MM 30-11-11. OPS CHECK GOOD, AIRCRAFT RETURNED TO SERVICE.