N656AE

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 49,388 hrs · 46,495 cycles

FWD EMERGENCY LIGHT STRIP INOP. RAR STRIP IAW AMM 33-50-12. OPS CHECK GOOD.

Part: LAMP — INOPERATIVE (ZONE 200) · airframe 49,034 hrs · 46,095 cycles

EMERGENCY LIGHT 261BF INOPERATIVE. R & R EMERGENCY LIGHT 261BF IAW AMM 33-50-08. ACFT OK FOR SERVICE.

Part: WARNING MESSAGE — ILLUMINATED (ZONE 800) · airframe 48,772 hrs · 45,785 cycles

BAGGAGE DOOR OPEN MESSAGE DURING FLIGHT. BAGGAGE DOOR WARNING / POSITION WARNING

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 48,639 hrs · 45,640 cycles

ROWS 8/9 AND 10/11 EMERGENCY LIGHT FLOOR PROXIMITY STRIPS INOPERATIVE. R&R #400 FLOOR PROXIMITY LIGHT IRT AMM 33-50-12 R&R#5 EMERGENCY LIGHT AC/DC INVERTER IRT AMM 33-50-11 PN ON 1013194 FLOOR PROX LIGHT PN OFF 6636-7 FLOOR PROX LIGHT PN ON 1330312 AC/DC INVERTER PN ON 1824-1 AC/DC INVERTER

Part: STRUT — DISCHARGED (ZONE 700) · airframe 48,381 hrs · 45,336 cycles

LDG AIR GRND FAIL WITH E1-E2 REV DISAGREE MESSAGE IN FLIGHT MESSAGE DISAPEARED WHEN GEAR DOWN AND LOCKED. SERVICED NLG SHOCK STRUT IAW AMM 32-20-01. PERFORMED AIR/GROUND SYSTEM SIMULATION ADJUSTMENT TEST IAW 32-63-00 & SWUNG GEARS MULTIPLE TIMES. NO DEFECTS NOTED. A/C OK FOR SERVICE AT THIS TIME

Part: BALLAST — FAILED (ZONE 200) · airframe 47,798 hrs · 44,696 cycles

FUMES NOTICED BY MAIN CABIN DOOR. FACT 29MAR25 00:41 CLT INSPECTED AND FOUND SIDEWALL LIGHT BALLAST AT 1A TO HAVE A BURNT ODOR. R+R BALLAST IAW AMM 33-21-03. OPS CHECK GOOD. NO MORE BURNING ODOR SMELT

Part: UNKNOWN — FUMES (CABIN) · airframe 46,718 hrs · 43,526 cycles

SLIGHT SMELL OF FUMES IN FLT DECK AND CABIN AROUND 26000FT. SMELL OCCURRED WHEN F/A WAS USING TEMP CONTROL. FACT 19SEP24 07:24 CLT PERFORED FIM TASK# 21-20-00-810-801-A. BLOCKS 1-11. NO DEFECTS NOTED. PACKS 1-2 RAN FOR EXTENDED TIME WITH NO FUMES DETECTED. OK FOR SERVICE.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 46,406 hrs · 43,146 cycles

00179 UPON REMOVAL OF FLOOR BEAM CAP @ FRM 59 - 61 FOUND FLOOR BEAM TO HAVE EXCESSIVE CORROSION @ FRM 60 + 10" Y= + 479.0 AND REQUIRES REPAIR. COMPLETED ALL STEPS OF EMB ETD2024-145-017954 REV: / DATED 07/01/2024. REPAIR MATERIAL: 2024-T3 .08

Part: SHEAR TIE — NOT REPORTED (ZONE 100) · airframe 46,406 hrs · 43,146 cycles

00166 SHEAR CLIP ON FRAME 65 BETWEEN STR15L-17L REQ REPLACED/REPAIR.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 46,406 hrs · 43,146 cycles

00131 RH FLOOR BEAM CAP AT Y +479 AT FR20 IS CORRODED. REMOVED AND INSTALLED NEW SERVICEABLE FLOOR BEAM CAP P/N 145-22461-011 IAW EMB-145LR SRM 51-40-02-PR

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 46,406 hrs · 43,146 cycles

00135 CORROSION FOUND ON +479.0 FLOOR BEAM CAP BETWEEN FRM 59-61. REMOVED AND INSTALLED NEW SERVICEABLE FLOOR BEAM GUSSET PN: 145-26437-001 IAW EMB-145 SRM 51-20-03-PR AND 51-40-02-PR

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 46,406 hrs · 43,146 cycles

00133 FLOOR BEAM CAP AT FR22 AND Y +479 IS CORRODED. : REMOVED AND REPLACED DAMAGED FLOOR BEAM CAP (DOUBLER P/N 145-22461-011) IAW EMB-145LR SRM 51-40-02-PR.

Part: BEAM — CORRODED (CARGO DOOR FRAME) · corrosion level 2 · airframe 46,406 hrs · 43,146 cycles

00073 MULTIPLE SPOTS OF CORROSION FOUND ON BOTTOM AREA OF BAGGAGE DOOR SURROUND STRUCTURE. REMOVED AND INSTALLED BEAM ASSY PN# 145-25480-603 (CARGO DOOR SILL) @ AFT CARGO DOOR LOWER SILL IAW EMB145-LR SRM 51-40-02-PR

Part: PITOT SYSTEM — FAULTED (NR 2) · airframe 46,315 hrs · 43,029 cycles

PITOT 2 INOP CAUTION MESSAGE DISPLAYED. FACT 20MAY24 14:22 CLT R+R # 2 PITOT SENSOR IAW AMM 34-13-01. PERFORMED PITOT/STATIC SYS 2 LEAKAGE TEST IAW AMM 34-13-00-790-803A/500 PERFORMED OPS CK IAW AMM 30-31-00-700-803A/500

Part: INSULATION — UNSECURE (NR 1 PACK AREA) · airframe 45,696 hrs · 42,327 cycles

IN CRUISE STRONG ELECTRICAL BURNING SMELL IN FLIGHT DECK. FACT 26JAN24 01:13 TRI RAN PACK SYSTEMS 1 AND 2 USING APU AND ENGINE BLDS, INSPECTED AND OPERATED FLIGHT DECK EQUIPMENT WITH NO SMELLS NOTED. INSPECTED PACKS 1 AND 2 AND UNDERFLOOR DUCTS FOR OBVIOUS DEFECTS, SUSPECT DETERIORATED INSULATION ON PACK 1 PIPE AS CAUSE FOR SMELL AND REMOVED LOOSE INSULATION. NO OTHER OBVIOUS DEFECTS NOTED OK FOR SERVICE.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 45,360 hrs · 41,991 cycles

DURING TAKE OFF WENT OFF. REVERSIONARY SWITCHED. EICAS SCREEN SHOWED PFD AND WOULD NOT RETURN. AFTER TOUCHDOWN EICAS SCREEN BLANKED OUT. R&R EICAS IAW AMM 34-22-01 AND R&R EICAS BEZEL IAW MM 31-41-02. PERFOREMD OPS CHECK IAW AMM 34-22-00. OPS CHECK GOOD. A/C OK FOR SERVICE

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 45,348 hrs · 41,975 cycles

EXCESSIVE NOSE WHEEL SHIMMY AFTER WHICH EICAS SCREEN WENT BLANK UNTIL SPEED WAS REDUCED. R+R'D NOSE WHEEL ASSYS IAW AMM 32-49-05. GREASED TORQUE LINGS AND TAXIED A/C 20 KNOTS, NO EXCESSIVE SHIMMY NOTED. A/C OKAY FOR SERVICE.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 49,816 hrs

3FLOOR STRIP EMERGENCY LIGHTS FROM LAV DOOR TO SEAT #12 ARE INOP. R & R INVERTER # 6 IAW AMM 33-50-11 OP TEST GOOD

Part: ENGINE — HUNG START (NR 2) · airframe 43,151 hrs · 39,433 cycles

ENGINE 2 HUNG START, AFTER START WAS ABORTED FUMES WERE NOTED IN CABIN AND FLIGHT DECK. INSPECTED #2 ENGINE FOR POSSIBLE FUEL LEAK. NONE FOUND. PERFORMED #2 ENGINE START FROM APU BLEEDS, PACKS OFF, AND #1 ENGINE BLEEDS, WITH PACKS OFF. BOTH TIMES ENGINE STARTS NORMALLY IAW RUN UP MANUAL. BOTH ENGINE 2 STARTS FROM DIFFERENT FADECS. RAN BOTH ENGINE APU AND PACKS, NO FUME SMELL OK FOR SERVICE

Part: FADEC — FAULTED (2B) · airframe 43,151 hrs · 39,433 cycles

HUNG START OF #2 ENG FOLLOWED BY EXHAUST FUMES. OIL NOTED DRIPPING FROM #2 LOWER COWLING. RAN E2 OFF FADEC A WITH NO DEFECTS NOTED. RAN E2 OFF FADEC B WITH HUNG START MULTIPLE TIMES. R/R FADEC 2B IAW AMM 73-22-01NO FIX. NO SIGN OF OIL LEAK DURING E2 ENGINE RUN.CONTINUE T/S DISCREPANCY REF SAME LP SEQ 2. AIRCRAFT IS CURRENTLY IN WORK. WILL SUPPLY MORE INFO WHEN REPAIRS ARE MADE.

Part: NOT REPORTED — NOT REPORTED · airframe 42,143 hrs · 38,319 cycles

PDIS 656 27-62 2706562 09FEB22 CLT CLOSE IN FLT SPEED BRAKE HANDLE TO CLOSE, SPOILER FAIL MSG, A/C ROLLED RT AND AUTO PILOT FAILED. RAN QRH WITH SPOILERS REMAINING CLOSED REST OF THE FLIGHT DURING DECENT ABOUT 13K FT FACT 09FEB22 16:08 CLT TS USING FIM 27-63-00-810-800-A BLOCKS 1-11 AND FIM 27-63-00-810-807-A. R&R'D SPOILER CONTROL UNIT IAW 27-63-02. PERFORMED SPOILER SYSTEM OPS CHECK IAW AMM 27-63-01-700-801-A. OPS CHECK GOOD. SPOILER FAIL MESSAGE NO LONGER PRESENT. A/C OK FOR SERVICE.

Part: NOT REPORTED — NOT REPORTED · airframe 42,058 hrs · 38,216 cycles

E894481 - THE PASSENGER DOOR FORWARD FRAME EDGE HAS CHAFE SPOTS FROM CONTACT WITH THE LINER .... REMOVED AND REPLACED PASSENGER DOOR FORWARD FRAME IAW EMB145 SRM 51-40-02.

Part: NOT REPORTED — NOT REPORTED · airframe 42,056 hrs · 38,216 cycles

E894714 - RH WING RIB 21 UPPER FLANGE CRACKED .... PERFORMED REPAIR TO RH WING RIB 21 IAW EO1-57-22-0005.

Part: NOT REPORTED — NOT REPORTED · airframe 42,056 hrs · 38,216 cycles

E894713 - LH WING RIB 21 UPPER FLANGE CRACKED .... PERFORMED REPAIR TO LH WING RIB 21 IAW EO1-57-21-0376

Part: NOT REPORTED — NOT REPORTED · airframe 42,058 hrs · 38,216 cycles

E893957 - REAR ELECTRONICS DOOR HAS DENT APPROXIMATELY 3" BELOW HANDLE .... ACCOMPLISHED REPAIR OF REAR ELECTRONIC COMPARTMENT DOOR SKIN APPROX. 3 INCHES BELOW HANDLE IAW EO1-52-21-0373.

Part: NOT REPORTED — NOT REPORTED · airframe 42,058 hrs · 38,216 cycles

E896607 - R/H ENGINE CONTAINMENT RING GOUGED AT LOWER SURFACE .... BLENDED OUT GOUGE ON RH ENGINE CONTAINMENT RING LOWER SURFACE IAW EMB 145 SRM 51-- 10-03. NO DAMAGE LIMITS FOR THIS AREA. MAPPED DAMAGE AND SENT OUT FOR FURTHER EVALUATION IAW PIEDMONT MPPM 13.2. BLENDED AREA MEASURES 1.1"X.- 65"X.105. DEPTH GAGE #524

Part: NOT REPORTED — NOT REPORTED · airframe 42,058 hrs · 38,216 cycles

E894799 - LH INBD FLAP SHROUD HINGE HAS 2 FASTENERS THAT ARE PULLING THRU AT INBD END .... REMOVED LH INBOARD FLAP SHROUD HINGE SECTION WITH 2 FASTENERS PULLING THROUGH AT INBOARD END, PREPPED AND INSTALLED SERVICEABLE HINGE SECTION IAW EMB 145 SRM 51-20-03, EMB 145 SRM 51-40-06.

Part: NOT REPORTED — NOT REPORTED · airframe 42,056 hrs · 38,216 cycles

E894680 - STR 2L CHAFED BTW FR 20-21 .... REPAIRED STR 2L CHAFE BETWEEN FRAMES 20 - 21 IAW PIEDMONT EO1-53-22-0001.

Part: NOT REPORTED — NOT REPORTED · corrosion level 2 · airframe 42,056 hrs · 38,216 cycles

E894625 - THE RH WALL #1 FLOOR SUPPORT HAS CORROSION NEAR FRAME 24 AND FRAME 28 .... PERFORMED BLEND OUT OF DAMAGE ON RH WALL #1 FLOOR SUPPORT NEAR FRAME 24 AND FRAME 28 IAW EMB 145 SRM 51-10-03. REMAINING THICKNESS AT BLENDED AREAS ON THE RH WALL #1 FLOOR SUPPORT NEAR FRAME 24 AND FRAME 28 FOUND TO BE BEYOND LIMITS IAW EMB145 SRM 53-22-10AD. REQUIRES PART REPLACEMENT. REMOVED CORRODED RH WALL #1 FLOOR SUPPORT NEAR FRAME 24 AND FRAME 28 AND POSITIONED AND DRILLED SERVICEABLE RH WALL #1 FLOOR SUPPORT NEAR FRAME 24 AND FRAME 28 IAW EMB 145 SRM 51-40-02 AND SRM 51-20-03. COMPLETED INSTALLATION OF RH WALL #1 FLOOR SUPPORT NEAR FRAME 24 AND FRAME 28 IAW EMB-145 SRM 51-40-02. PAINTED FASTENER HEADS IAW EMB 145 CPM 51-21-06

Part: NOT REPORTED — NOT REPORTED · corrosion level 2 · airframe 42,056 hrs · 38,216 cycles

E894621 - THE LH CENTER SEAT TRACK #3 HAS EVIDENCE OF CORROSION ON SEVERAL SPOTS ALONG ITS ENTIRE LENGTH .... REMOVED AND REPLACED THE LH CENTER SEAT TRACK #3 IAW EMB 145 AMM 53-01-06.

Part: NOT REPORTED — NOT REPORTED · airframe 42,056 hrs · 38,216 cycles

PAX DOOR ENTRANCE FWD AND AFT FLOOR BOARD SUPPORT BRACKETS ARE CORRODED. RAR PAX DOOR ENTRANCE FWD AND AFT FLOOR SUPPORT BRACKETS IAW EMB-145 SRM 51-40--02.

Part: NOT REPORTED — NOT REPORTED · corrosion level 2 · airframe 42,056 hrs · 38,216 cycles

E894627 - THE RH WALL #2 FLOOR SUPPORT HAS CORROSION BETWEEN FRAMES 33 AND 35 .... REMOVED AND REPLACED SERVICEABLE RH WALL #2 FLOOR SUPPORT IAW EMB 145 SRM 51-40-02.

Part: NOT REPORTED — NOT REPORTED · airframe 42,056 hrs · 38,216 cycles

E895312 - FRAMED CRACKED ON UNDERSIDE AT FR 72 AT STR 16L .... REMOVED AND REPLACED FRAME 72 (LH SIDE FRAME SECTION) IAW EMB145 SRM 51-40-02

Part: VALVE — BROKEN (CABIN PRESSURE) · airframe 41,313 hrs · 37,391 cycles

A/C WILL NOT PRESSURIZE IN AUTO OR MANUAL MODE. MAINTENANCE FOUND GROUND AIR CONDITIONING FLAPPER VALVE BROKEN. R&R'D GROUND CONNECT VALVE IAW AMM 21-22-04 , OPS CHECK GOOD. OPS CHECKED PRESSURIZATION IAW AMM 21-31-00. OPS CHECK GOOD. A/C OK FOR SERVICE

Part: RELAY — FAILED (NR 2 BLEED VALVE) · airframe 40,867 hrs · 36,891 cycles

NR BLEED VALVE FAILED AT 60-65 KNOTS. REMOVED AND REPLACED RELAY K0172 IN REF TO AMM TASK 20-13-02-000-400-801-A. OPS CHECK GOOD. NO DEFECTS NOTED. AIRCRAFT OK FOR SERVICE. OPS CHECK 36-00-00-700-803-A

Part: O-RING — FAILED (BLEED 2) · airframe 40,816 hrs · 36,835 cycles

BLD 2 LEAK EICAS MESSAGE AND INSCRIPTION APPEARED AT 8000 FT DURING FLIGHT. FOLLOWED QRH AND MESSAGE WENT AWAY. R&R O-RINGS ON BLEED 2 PIPES AFT COUPLING IN BAG BAY, AFT 2 COUPLINGS IN AFT CENTER WING PANEL. INSPECTED ALL #2 BLEED PIPE COUPLINGS FOR LEAKS. LEAK CHECK GOOD IAW 36-11-10. CLEAR MEL.

Part: CHECK VALVE — FAILED (NR 2 BLEED) · airframe 40,816 hrs · 36,835 cycles

BLEED 2 LEAK ON CLIMB IN FLIGHT. R+R GRND AIR CHECK VLV IN REF TO AMM 36 10 02. OPS CHECK AND LEAK CHECK GOOD. GROUND RAN #2 ENG AT POWER WITH BLEEDS AND PACKS ON. NO LEAK MSG PRESENT. OK FOR SERVICE

Part: SLEEVE — LEAKING (NR 2 HT EXCHNGER) · airframe 39,234 hrs · 35,430 cycles

PDIS 656 36-21 2384272 07APR21 CLT CLOSE BLD 2 LEAK DURING CLIMB. RAN QRH, RESET OK FACT 07APR21 04:14 CLT R&R'D SLEEVE AT #2 HEAT EXCHANGER TO ACM Y SLEEVE FWD OF PACK VALVE. ALSO FOUND CLAMP AT #2 ENG PRSOV LEAKING R/R'D CLAMP. RAN #2 ENG NO LEAKS FOUND AT THIS TIME OK FOR SERVICE.

Part: INDICATION SYS — INTERMITTENT (NR 1 FUEL) · airframe 40,547 hrs · 36,540 cycles

FUEL 1+2 LOW LEVEL EICAS ON TAKEOFF ATTEMPT. INTERMITTANTLY LOSE #1 FUEL INDICATIONS. VISUALLY INSPECTED SPR PANEL FOR OVBIOUS DEFECTS. NO DEFECTS NOTED. CYCLED ALL SWITCHES TO ENSURE PROPER POSITIONING FOR NORMAL OPERATIONS. PERFORMED TAXI CHECK. TEXI CHECK GOOD. NO FUEL ABNORMALITIES NOTED. OK FOR SERVICE

Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 40,273 hrs · 36,234 cycles

PURPOSES. CREW CONTACTED MOC STATED ABORTED TAKEOFF DUE TO MOM ENTARY BLEED 2 VALVE FAIL MESSAGE ON TAKEOFF. MESSAGE SELF EXTINGUISHED, NO HISTORY, RECONFIG A/C, SYSTEM OPERATIONS NORMAL. CREW/MOC DETERMINED NO AIRCRAFT FAULT. HISTORY: NONE. THIS DISCREPANCY CLOSED. MIR CREATED.

Part: CONNECTOR — LOOSE (NLG UPLOCK) · airframe 40,229 hrs · 36,185 cycles

PDIS 656 32-30 2415291 30OCT20 CLT. CLOSE ON GEAR RETRACTION LOUD NOISE WAS HEARD FROM NOSE GEAR AREA. NOISE WAS CONTINUOUS UNTIL GEAR WAS CYCLED, HAS HISTORY FROM 06OCT20. FACT 31OCT20 02:32 SBY. REFERRING MTL 2017-E-7. INSPECTED MLG UPLOCK BOXES AND NLG UPLOCK BOX FOUND CANNON PLUG ON THE NLG UPLOCK BOX LOOSE. REMOVED AND CLEANED CANNON PLUGS, PER SWPM 20-50-00. RECONNECTED BOTH CANNON PLUGS. PERFORMED RETRACTION AND EXTENSION. OPERATIONS CHECK, IAW AMM 32-30-00. NO THUMPING OR OTHER DEFECTS NOTED. OPERATIONS CHECK GOOD. OK FOR SERVICE AT THIS TIME.

Part: ACM — DAMAGED · airframe 39,996 hrs · 35,919 cycles

IN FLIGHT, FA REPORTS A LOUD REVING SOUND IN CABIN, FOLLOWED BY ELECTRICAL AND DUST ODOR. AFTER LANDING PACK 2 OVHT MESSAGE ON EICAS. CHECKED THE PACK #2 AND FOUND ACM TO BE DAMAGED. R & R THE ACM IAW AMM 21-51-03. OPS CHECKED GOOD. OK FOR SERVICE.

Part: WARNING SYSTEM — FALSE ACTIVATION (ANTI-ICE SYS) · airframe 39,735 hrs · 35,612 cycles

DUE TO POSSIBLE ERRONEOUS INDICATIONS, VERIFICATION OF E1 ANTI-ICE VALVE DEACTIVATION IS REQUIRED.MAINTENANCE VERIFIED E1 ANTI ICE VALVE IS IN THE LOCK POSITION IAW 30-21-01-040-801-A.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 39,735 hrs · 35,612 cycles

E1 ANTI ICE VALVE INDICATED CLOSED IN FLIGHT WITH VALVE DEACTIVATED PER MEL. MAINTENANCE: VERIFIED E1 ANTI ICE VALVE IS SECURED OPEN IN LOCKED POSITION PER MEL.

Part: ANTI-ICE VALVE — MALFUNCTIONED (NR 1 ENGINE) · airframe 39,719 hrs · 35,599 cycles

ENG 1 ANTI ICE FAIL MESSAGE APPEARED IN FLIGHT. ACC OPER. PROC. MAINTENANCE R&R'D #1 ENGINE ANTI-ICEING VALVE REFERENCING AMM 30-21-05. PERFORMED OPS CHECK IAW AMM 30-00-00-700-803-A/500. OPS CHECK GOOD. CLEAR MEL.

Part: LIGHT — INOPERATIVE (RT OVERWING) · airframe 39,562 hrs · 35,413 cycles

RH OVER THE WING EMERGENCY LIGHT WONT ILLUMINATE....FIX: REPLACED LIGHT IN REFERENCE TO EMB 145 AMM 33-50-10-000/400-801-A OPS CK GOOD.OK FOR SERVICE

Part: BRAKE — OVERHEATED · airframe 39,278 hrs · 35,091 cycles

NDIS 656 30-21 758 04JAN20 AVP CLOSE -FOR MIR PURPOSES ONLY- FACT 04JAN20 14:22 AVP FLIGHT 4894 ABORTED TAKE OFF DUE TO ONE BRAKE ASSY TEMPERATURE GOING UP INTO THE YELLOW. AIRCRAFT TAXIED BACK TO THE GATE ALL BRAKE TEMPERATURE CAME DOWN BRAKES OPERATE NORMAL WITH NO DEFECTS NOTED.AIRCFRAT DID NOT PULLED TO THE LEFT OR RIGHT. ADVISED CREW TO RE-CONFIGURE AIRCRAFT AND WAIT FOR ALL BRAKE TEMPS

Part: ACTUATOR — FAILED (NLG DOOR) · airframe 38,760 hrs · 34,503 cycles

ON GEAR RETRACTION, NLG DOORS REMAINED OPEN. NORMAL GEAR INDICATION. FOUND THE LT NLG DOOR ACTUATOR TO AT FAULT. R & R THE NLG DOOR ACTUATOR IAW TASK 32-33-03, OPS CHECKED GOOD. NO DEFECTS NOTED. PERFORMED A LG RETRACTION TEST AND LEAK CHECK. OPS AND LEAK CHECKED GOOD. OK FOR SERVICE.

Part: LANDING GEAR — NOISE · airframe 38,742 hrs · 34,483 cycles

DURING CLIMB AFTER GEAR RETRACTION A VERY LOUD NOISE APPEARED AT ABOUT 4000 FT AS THOUGH A GEAR DOOR OPENED. PERFORMED GVI OF THE LANDING GEAR WITH NO DEFECTS NOTED. RETRACTED AND EXTENDED LANDING GEAR SEVERAL TIMES WITH NO DEFECTS NOTED IAW AMM 32-30-00-05. EVAL FLIGHT, SATISFACTORY.

Part: WIRE — DAMAGED (CABIN) · airframe 38,679 hrs · 34,407 cycles

PAX DOOR EMERGENCY LIGHT INTERMITTENT. FIX: REPAIRED DAMAGED WIRE AT LIGHT ASSY BY REPLACING TERMINAL END PIN.

Part: RELAY — FAULTY (NLG DOOR) · airframe 38,659 hrs · 34,382 cycles

NLG DOOR OPENED UNCOMMANDED DURING APPROACH, CREW C/W QRH, NO FURTHER DEFECTS NOTED. FIX: T/S PER FIM SHOWS TRANSITORY CONDITION. CYCLED GEAR SEVERAL TIMES OPS CHECK GOOD PER AMM 32-30-00. NLG DOORS NOT DESIGNED TO INDICATE OPEN OR CLOSE. REPLACED RELAY K0642 "DOOR CONTROL RLY ON RT AUX RLY SUPPORT, OPS CHECK GOOD. OK FOR SERVICE.

Part: UNKNOWN — MALFUNCTIONED (NLG DOOR) · airframe 38,593 hrs · 34,305 cycles

PDIS 656 32-20 1899841 08SEP19 PHL CLOSE ON GEAR RETRACTION NLG DOORS REMAINDS OPEN FACT 08SEP19 17:21 PHL PERFORMED OPS CHECK OF LANDING GEAR. OPS CHECK GOOD. NO DEFECTS NOTED. OK FOR SERVICE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 38,433 hrs · 34,131 cycles

MAIN DOOR EMERGENCY LIGHT DOES NOT ILLUMINATE. R & R THE BULB IAW AMM TASK 33-50-06-000/400-801-A.OK FOR SERVICE

Part: LIGHT — INOPERATIVE · airframe 37,969 hrs · 33,589 cycles

656 33-51 0003170 14MAY19 SBY CLOSE RT LATERAL PANEL EMERGENCY LIGHT INOP. 30100 00 CRH FACT 14MAY19 09:32 SBY R&RED RT LATERAL PANEL EMERGENCY LIGHT LIGHT BULB IAW AMM 33-50-10-000-801-A AND 33-50-01-700-801-A. P/N ON BULB 1317 P/N OFF BULB 1317.

Part: CONTACTOR — FAULTED (WINDSHIELD HEAT) · airframe 37,758 hrs · 33,325 cycles

656 30-41 1919182 01APR19 PHL CLOSE WINDSHIELD HEAT 1 INOP EICAS MSG 27626 00 RNR HISTORY: 31MAR (3X) FACT 01APR19 06:46 ALB TROUBLESHOT WS HEAT 1 INOP MSG PER EMB145 FIM TASK 30-42-00-810-801-A AND FOUND CONTATCTOR K001 TO BE FAULT. REMOVED AND REPLACED CONTACTOR -K001 PER EMB145 AMM 30-42-02. OPS CHECK GOOD.

Part: FIREWALL — CHAFED (APU BAY) · airframe 37,678 hrs · 33,234 cycles

APU FIREWALL AFT SIDE LOWER EDGE HAS NUMEROUS CHAFED AREAS. C/A-REPAIRED APU FIREWALL IAW ERS-EM-53MR-3662.

Part: WIRE — BROKEN (CABIN) · airframe 37,678 hrs · 33,234 cycles

CABIN CEILING PANEL 253CLC HAS BROKEN WIRE ON BACK OF PANEL FOR EMERGENCY EXIT LIGHT. C/A-REPAIRED WIRE ON BACK OF CEILING PANEL 253CLC FOR EMERGENCY EXIT LIGHT IAW SWPM 20-21-00.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 37,678 hrs · 33,234 cycles

SERVICE DOOR CENTER SILL CORRODED AT FORWARD AND AFT ENDS. C/A-REMOVED AND REPLACED SERVICE DOOR CENTER SILL IAW SRM 51-40-02.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 37,678 hrs · 33,234 cycles

EMERGENCY LIGHT STRIP NR 6 INOP. C/A-REMOVED AND REPLACED NR 6 EMERGENCY LIGHT STRIP IAW AMM 33-50-12.

Part: WIRE — BROKEN (CABIN) · airframe 37,678 hrs · 33,234 cycles

EMERGENCY LIGHT STRIP AT 231GF HAS BROKEN WIRES ON AIRCRAFT SIDE. C/A-REPAIRED EMERGENCY LIGHT WIRES (AT 231GF) W192-8630-22 (SP9019) AND W192-8631-22 (SP9020 IAW SWPM 20-21-00.

Part: WIRE — BROKEN (CABIN) · airframe 37,678 hrs · 33,234 cycles

EMERGENCY LIGHT STRIP WIRE AT 241BF IS BROKEN. C/A-REPAIRED EMERGENCY LIGHT WIRE W192-8680-22 (SP9037) AT 241BF IAW SWPM 20-21-00.

Part: WIRE — BROKEN (CABIN) · airframe 37,678 hrs · 33,234 cycles

EMERGENCY LIGHT STRIP WIRE AT 251DF IS BROKEN. C/A-REPAIRED EMERGENCY LIGHT WIRE W192-8761-22 (SP9119 AT 251DF IAW SWPM 20-21-00.

Part: WIRE — BROKEN (CABIN) · airframe 37,678 hrs · 33,234 cycles

EMERGENCY LIGHT STRIP WIRE AT 251DF IS BROKEN. C/A-REPAIRED EMERGENCY LIGHT WIRE W192-8761-22 (SP9119 AT 251DF IAW SWPM 20-21-00.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 37,678 hrs · 33,234 cycles

LT OMEGA BEAM SIDEWALL HAS POSSIBLE CORROSION ABOVE THE CROSSBEAM AFT OF FRAME 49. C/A-REPAIRED THE LT OMEGA BEAM CORROSION ABOVE THE CROSSBEAM AFT OF FRAME 49 IAW ERS-EM-53MR-3680.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 37,678 hrs · 33,234 cycles

LT OMEGA BEAM HAS POSSIBLE CORROSION ABOVE THE CROSSBEAM AT FRAME 44. C/A-REPAIRED THE LT OMEGA BEAM CORROSION ABOVE THE CROSSBEAM AT FRAME 44 IAW ERS-EM-53MR-3679.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 37,678 hrs · 33,234 cycles

RT HAT BEAM INBD AND OTBD SUPPORTS ARE CRACKED FWD OF FR 48. C/A-REMOVED AND REPLACED RT HAT BEAM INBD AND OTBD SUPPORTS IAW SRM 53-23-02. ANGLE P/N 145-28364-005.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 37,678 hrs · 33,234 cycles

LT OMEGA BEAM FLOOR SUPPORT CORRODED BETWEEN FR58 ? 59; LT OMEGA BEAM CORRODED ON LOWER FLANGE AND WEB UNDER CROSSBEAM AT FR 59. C/A-REPAIRED THE LT OMEGA BEAM FLOOR SUPPORT CORROSION BETWEEN FR58-59, AND LOWER FLANGE AND WEB UNDER CROSS BEAM AT FR 59 IAW ERS-EM-53MR-3674.

Part: BEARING CAP — CORRODED (RT MLG) · airframe 37,678 hrs · 33,234 cycles

RT MLG AFT LOWER BEARING CAP IS PITTED AND GOUGED. C/A-REMOVED AND REPLACED RT MLG AFT BEARING CAP IAW AMM 32-10-01.

Part: FITTING — CHAFED (LT AILERON) · airframe 37,678 hrs · 33,234 cycles

LT AILERON DAMPER FITTING CHAFE. C/A-REMOVED AND REPLACED LT AILERON DAMPER FITTING IAW EM-27MR-112.

Part: FITTING — GOUGED (RT AILERON) · airframe 37,678 hrs · 33,234 cycles

RT AILERON DAMPER FITTING BOLT HOLE GOUGED. C/A-REMOVED AND REPLACED RT AILERON DAMPER FITTING IAW EM-27MR-112.

Part: FITTING — CORRODED (FUSELAGE) · airframe 37,678 hrs · 33,234 cycles

FRAME 65 SHEAR CLIP CORRODED AT CARGO DOOR LOWER SILL. C/A-REPAIRED FRAME 65 SHEAR CLIP IAW SRM 53-31-04.

Part: BRACKET — CORRODED (FUSELAGE) · airframe 37,678 hrs · 33,234 cycles

FRAME 68 CARGO DOOR CUTOUT LOWER SILL T BRACKET CORRODED. C/A-REMOVED AND REPLACED FRAME 68 CARGO DOOR CUTOUT LOWER SILL T BRACKET IAW SRM 51-40-02.

Part: PROFILE — BENT (CARGO DOOR) · airframe 37,678 hrs · 33,234 cycles

CARGO DOOR LOWER PROFILE IS BENT NEAR FORWARD ROLLER. C/A-REMOVED AND REPLACED CARGO DOOR LOWER PROFILE IAW SRM 51-40-02.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 37,678 hrs · 33,234 cycles

CARGO DOOR CUTOUT LOWER SILL CORRODED. C/A-REMOVED AND REPLACED CARGO DOOR CUTOUT LOWER SILL IAW SRM 51-40-02.

Part: BRACKET — CORRODED (FUSELAGE) · airframe 37,678 hrs · 33,234 cycles

FRAME 65 CARGO DOOR CUTOUT LOWER SILL T BRACKET CORRODED. C/A-REMOVED AND REPLACED FRAME 65 CARGO DOOR CUTOUT LOWER SILL T BRACKET IAW SRM 51-40-02.

Part: STRUCTURE — DAMAGED (EMERGENCY LIGHT) · airframe 37,678 hrs · 33,234 cycles

ALL RT FLOOR SIDEWALL EXTRUSIONS ARE DAMAGED. C/A-COMPLETE:REMOVED AND REPLACED ALL RT FLOOR SIDEWALL EXTRUSIONS IAW AMM 33-50-12. SEE BOW313523 FOR INSTALLATION.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 37,678 hrs · 33,234 cycles

SSI 53-20-11 LT OMEGA BEAM CORRODED ON LOWER FLANGE AND WEB UNDER CROSSBEAM AT FR59. C/A-COMPLETE:COMPLIED WITH ERS-EM-53MR-3674 LT OMEGA BEAM CORROSION FRAME 58 -59 - PERMANENT REPAIR.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 37,678 hrs · 33,234 cycles

SSI 53-20-11 LT OMEGA BEAM FLOOR SUPPORT CORRODED BETWEEN FR 58/59 (MARKED). C/A-COMPLETE:FURTHER INVESTIGATION OF CORROSION ON LT OMEGA BEAM FLOOR SUPPORT BETWEEN FR 58/59 SHOWS ADDITIONAL CORROSION THAT EXCEEDS THE REPAIR LIMITS OF EM-53MR-1518. SEE NRTC E696071 FOR BEAM REPAIR.

Part: STRUCTURE — TORN (EMERGENCY LIGHT) · airframe 37,678 hrs · 33,234 cycles

EXTRUSIONS FOR EMERGENCY LIGHT STRIPS #1, #4, #5, #6, #7 AND #8 ARE TORN. C/A-COMPLETE:REMOVED AND REPLACED EXTRUSIONS FOR EMERGENCY PROXIMITY LIGHTS #1,#4,#5,#6,#7 AND #8 IAW AMM 33-50-12. SEE BOW313523 FOR OPS CHECK.

Part: CONTROLLER — MALFUNCTIONED (WINDOW HEAT) · airframe 37,521 hrs · 33,095 cycles

W/S 1 HEAT FAIL ON CLIMBOUT. HEARD CLICKING NOISE. C/A-DEFERRED W/S HEAT AS PER MEL 30-24 AUTH 010172DM-C M-PROCEDURES COMPLIED WITH. REMOVED AND REPLACED LT WINDSHIELD TEMP CONTROLLER IAW AMM 30-42-01. PERFORMED OPERATIONAL TEST OF WINDSHIELD HEATING SYSTEM IAW AMM 30-42-00. OPS TEST GOOD. MEL ITEM RESTORED.

Part: CRADLE — BROKEN (FLASHLIGHT) · airframe 37,253 hrs · 32,794 cycles

REF AML PAGE 4419251 ITEM # 1 MEL 2553 - AUTH# 110658-C REAR FLASHLIGHT HOLDER BROKEN-C/A-RAR AFT FLASHLIGHT HOLDER IAW EMB AMM 33-50-16-000-801-A AND 33-50-16-400-801-A OPC GOOD NO DEFECTS NOTED AT THIS TIME MEL RESTORED END.

Part: CRADLE — BROKEN (FLASHLIGHT) · airframe 37,251 hrs · 32,790 cycles

AFT FA FLASHLIGHT HOLDER ASSEMBLY BROKEN-C/A-FLIGHT CREW PLACARDED AFT FA FLASHLIGHT HOLDER REF: MEL 25- 60 AUTH: 110658-CMOC: 056020

Part: CHARGER — FAILED (CABIN) · airframe 36,983 hrs · 32,512 cycles

SUPPLEMENTAL BOTH AFT OVERWING EMERGENCY LIGHTS INOP. -C/A-DEFERRED PER MEL 33-29. REMOVED AND REPLACED BATTERY CHARGE ASSY PER W/C 33-700-19 NO FIX . REMOVED AND REPLACED NR 4 BATTERY CHARGER IAW AMM 33-50-04 OPS CHECK GOOD. MEL ITEM RESTORED. BATTERY CHARGER P/N 11-0049 S/N 18035 NR 4

Part: HANDLE — LOOSE (CABIN DOOR) · airframe 36,347 hrs · 31,913 cycles

FA WAS UNABLE TO OPEN CABIN DOOR. DOOR HAD TO BE OPENED FROM OUTSIDE. UPON INVESTIGATION FOUND INTERIOR DOOR HANDLE TO BE LOOSE. TIGHTENED DOOR HANDLE IAW AMM 52-18-05. OPC GOOD.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 36,335 hrs · 31,901 cycles

PTRIM MAIN INOP WARNING MSG ON EICAS WHILE CRUISING AT FL320 SPEED M .23. PERFORMED OPS CHECK IAW AMM 27-40-00-700-802-A OPS CHECK OK, NO DEFECTS NOTICED.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 36,024 hrs · 31,580 cycles

OVERWING EMERGENCY LIGHT AT SEAT 12A WAS FOUND INOPERATIVE. R & R THE OVERWING EMERGENCY LIGHT LAMP IAW 33-50-07-000-801-A, AND 33-50-07-400-801-A. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,965 hrs · 30,687 cycles

OVERHEAD ENTRANCE EMERGENCY LIGHT INOP-C/A-REMOVED AND REPLACED OVERHEAD ENTRANCE EMERGENCY LIGHT OPC GOOD IAW EMB AMM 33-50-06

Part: CRADLE — CRACKED (AFT FLASHLIGHT) · airframe 34,696 hrs · 30,427 cycles

AFT CABIN FLASHLIGHT CHARGING CRADLE CRACKED. R & R THE FLASHLIGHT CHARGING CRADLE IAW AMM 33-50-16-000-801-A, AND 33-50-16-400-801-A. OPS CHECKED GOOD.

Part: HANDLE — LOOSE (CABIN DOOR) · airframe 34,594 hrs · 30,322 cycles

FA INFORMED, MAIN CABIN DOOR HANDLE NEEDS TO BE FIXED DIFFICULT TO OPEN DOOR. FOUND MAIN HANDLE TO BE LOOSE AND FELL OFF. REATTACHED HANDLE IAW AMM 52-18-05. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED

Part: DOOR — LACK OF LUBE (MAIN PAX) · airframe 34,073 hrs · 29,803 cycles

FA REPORTED THE MAIN CABIN DOOR VERY HARD TO OPEN AND CLOSE. INSPECTED AND LUBRICATED THE DOOR IAW 52-00-00, OPS OK

Part: CHARGER — FAILED (CABIN) · airframe 33,665 hrs · 29,446 cycles

DURING PS-2 FOUND LT AND RT OVERWING EMERGENCY LIGHTS INOP. REMOVED AND REPLACED LT SIDE CENTER FAIRING EXTERNAL EMERGENCY LIGHT ASSEMBLY IAW AMM 33-50-10. REMOVED AND REPLACED BATTERY POWER SUPPLY 3 AND 4 IAW AMM 33-50-04. R&R BATTERY CHARGER 4 IAW AMM 33-50-04. OPS CHECK GOOD. EMERGENCY LIGHTING BATTERY P/N 2013-1ASMI S/N 74818 3; P/N 2013-1A S/N 123941 4; LIGHT EMERGENCY LT P/N 30-2510-3

Part: LIGHT — INOPERATIVE (RT OVERWING) · airframe 33,551 hrs · 29,335 cycles

RIGHT OVERWING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY LIGHT ASSEMBLY IAW AMM 33-50-10. OPS CHECKED GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 33,510 hrs · 29,293 cycles

RIGHT AFT OVERWING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED RT AFT OVERWING EMERGENCY LIGHT LAMP IAW AMM TASK 33-50-10-000-801-A, AND 33-50-10-400-801-A. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,454 hrs · 29,241 cycles

RT EXTERNAL AFT EMERGENCY LT INOP. REMOVED AND REPLACED RT EXTERNAL AFT EMERGENCY LT LAMP IAW AMM 33-50-10-000-801-A AND 33-50-10-400-801-A. OPC GOOD AT THIS TIME.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 33,349 hrs · 29,133 cycles

LEFT AND RIGHT OVERWING EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED POWER SUPPLY BATTERY PACK IAW 33-700-19. OPS CHECKED GOOD.

Part: CHARGER — FAILED (EMERGENCY LIGHTS) · airframe 33,266 hrs · 29,057 cycles

LT AND RT OVERWING EXTERNAL EMERGENCY LIGHTS FAIL TO ILLUMINATE. REMOVED AND REPLACED POWER SUPPLY AND BATTERY IAW AMM 33-50-04. OPS CHECKED GOOD.

Part: CHARGER — FAILED (EMERGENCY LIGHT) · airframe 33,220 hrs · 29,027 cycles

OVERWING EMERGENCY AFT LIGHT INOPERATIVE. TROUBLESHOT THE EMERGENCY LIGHT IAW FIM 33-50-00-810-804-A. R & R THE BATTERY CHARGER ASSY AND BATTERY IAW AMM 33-50-04. OPS CHECKED GOOD AT THIS TIME.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 33,062 hrs · 28,884 cycles

FIRST INTERIOR CEILING EMERGENCY LIGHT IS INOPERATIVE. REPLACED THE BULB IN THE FIRST INTERIOR CEILING EMERGENCY LIGHT. OPS CHECKED GOOD IAW AMM 33-50-08.

Part: SKIN — CRACKED (FUSELAGE) · airframe 33,018 hrs · 28,845 cycles

LT UPPER FUSELAGE SKIN CRACKED AFT OF FRAME 75, AND ABOVE STRINGER 2L. PERFORMED REPAIR OF LT UPPER FUSELAGE SKIN CRACK AFT OF FRAME 75, AND ABOVE STRINGER 2L IAW SRM 53-31-01.

Part: SKIN — BENT (CARGO DOOR) · airframe 33,018 hrs · 28,845 cycles

BAGGAGE DOOR TRAILING EDGE IS BENT IN 2 PLACES. REPAIRED BAGGAGE DOOR TRAILING EDGE IAW ERS-EM-52MR-671.

Part: DOOR FRAME — CORRODED (CARGO DOOR) · airframe 33,018 hrs · 28,845 cycles

BAGGAGE DOOR FWD END HAS CORROSION AROUND 4 NUTPLATES. REPAIRED BAGGAGE DOOR FWD END IAW ERS-EM-52MR-672.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 33,018 hrs · 28,845 cycles

SERVICE DOOR CUTOUT LOWER CENTER SILL CORRODED. REPAIRED SERVICE DOOR CUTOUT LOWER CENTER SILL IAW ERS-EM-53MR-2453.

Part: MOUNT BRACKET — CRACKED (FUSELAGE) · airframe 33,018 hrs · 28,845 cycles

LT LATERAL UPPER MOUNT BRACKET CRACKED ABOVE LT DV WINDOW FWD UPPER CORNER. REMOVED AND REPLACED REINFORCEMENT ABOVE LATERAL POST IAW SRM 51-40-02.

Part: LIGHT — DAMAGED (CABIN) · airframe 33,018 hrs · 28,845 cycles

LT EMERGENCY LIGHT EXTRUSION NR 1 AND NR 3 DAMAGED. R&R LT EMERGENCY LIGHT EXTRUSION NR 3 IAW AMM 33-50-12, SEE NRTC BOW233027 FOR THE INSTALLATION OF NR 1 EXTRUSION.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,018 hrs · 28,845 cycles

THE SECOND EMERGENCY LIGHT STRIP FROM THE BACK INOP. REMOVED AND REPLACED THE SECOND EMERGENCY LIGHT STRIP FROM THE BACK IAW AMM 33-50-12,AND OPS CHECKED GOOD.

Part: EPSU — INOPERATIVE (CABIN) · airframe 32,841 hrs · 28,666 cycles

LT AND RT EXTERIOR OVERWING LIGHTS INOP. REMOVED AND REPLACED EPSU NR 4 IAW W/C 33-700-19 AND OPS CHECK GOOD IAW W/C 33-700-17. BATTERY CHARGER ASSY P/N 11-0049 S/N 20114R.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 32,816 hrs · 28,646 cycles

SECOND AND THIRD EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE BATTERY PACK. OPS CHECKED GOOD IAW AMM 33-50-12.

Part: CHARGER — FAILED (EMERGENCY LIGHTS) · airframe 32,777 hrs · 28,612 cycles

LT AND RT CENTER FAIRING EXTERNAL EMERGENCY LIGHT FAILS TO ILLUMINATE. REMOVED AND REPLACED THE NR 4 EPSU BATTERY CHARGER ASSY IAW AMM 33-50-04. OPS CHECKED GOOD. NO OTHER DEFECTS NOTED.

Part: BATTERY — DISCONNECTED (CABIN) · airframe 32,708 hrs · 28,558 cycles

SEVERAL EMERGENCY SIGNS AND LIGHTS INOP, EXTERIOR LIGHT FWD OF LT WING, MAIN DOOR LIGHT, MAIN ENTRANCE OVERHEAD LIGHT & FWD CABIN EXIT SIGN. FOUND EMERGENCY BATTERY 1 UNINSTALLED ON COMPARTMENT FLOOR. REINSTALLED BATTERY 1 IN REFERENCE WITH 33-50-04-400-801-A. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 31,360 hrs · 27,351 cycles

COCKPIT EMER LAMP INOPERATIVE. R & R COCKPIT EMER LAMP IAW AMM 33-50-05-000-801-A & 33-50-05-400-801-A. OPERATIONS CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 30,633 hrs · 26,678 cycles

REAR CABIN FLASHLIGHT INOPERATIVE. R & R REAR CABIN FLASHLIGHT IAW AMM SMP. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,269 hrs · 26,307 cycles

PASSENGER DOOR EMER LIGHT INOPERATIVE. R & R PAX DOOR EMER LIGHT LAMP IAW AMM 33-50-10-000-801-A & 33-50-10-400-801-A. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (RT OVERWING) · airframe 29,869 hrs · 25,940 cycles

RIGHT OVERWING EMER LIGHT INOPERATIVE. RT OVERWING EMER LIGHT LAMP R & R IAW AMM 33-50-10. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,472 hrs · 25,574 cycles

RIGHT OVERWING EMER LIGHT INOPERATIVE. R & R RT OVERWING EMER LIGHT LAMP IAW AMM 33-50-10. OPERATIONS CHECKED GOOD.

Part: CRADLE — CRACKED (FLASHLIGHT) · airframe 29,472 hrs · 25,574 cycles

CAPTAIN`S EMER FLASHLIGHT CRADLE IS CRACKED. R & R REPLACED CAPTAIN`S EMER CRADLE FLASHLIGHT ASSEMBLY IAW MNTC WC 33-700-20.

Part: CRADLE — BROKEN (FLASHLIGHT) · airframe 29,472 hrs · 25,574 cycles

FORWARD PAX CABIN FLASHLIGHT CRADLE IS BROKEN. R & R FWD PAX CABIN CRADLE & FLASHLIGHT ASSEMBLY IAW MNTC WC 33-700-20. OPERATIONS CHECKED GOOD.

Part: PITOT LINE — CONTAMINATED (NR 2) · airframe 29,436 hrs · 25,552 cycles

DURING FLIGHT AT FL 370 ALL COCKPIT WINDSHIELDS FROSTED OVER, STARTED DESCENT. BOTH PRIMARY AIRSPEEDS SLOWED TO UNDER 200 KTS, STDBY READ NEAR RED LINE. FOUND WATER IN NR 2 PITOT LINE, CLEANED LINES IAW AMM 34-13-00, ADC 1 & 2 OPERATIONS CHECKED GOOD IAW AMM 34-15-00 ADC 1 & 2 LEAK CHECKED GOOD IAW AMM 34-13-00, NO LEAKS NOTED. ACFT WAS STILL PRESSURIZED UPON LANDING. DELTA P WAS ABOVE 1.2. PRESSURIZATION OPERATIONS CHECKED GOOD IAW AMM CH 21-31-00, NO DEFECTS NOTED. IAW ITEM NR 1 THIS AML PAGE. PITOT STATIC LINES NEED TO BE CHECKED FOR WATER. PERFORMED PITOT STATIC SYS SERVICING IAW AMM 31-13-00. NO WATER FOUND. REQUIRES FURTHER TROUBLESHOOTING.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 29,282 hrs · 25,412 cycles

RIGHT AFT EMER EXTERIOR LIGHT FAILS TO ILLUMINATE. R & R BULB FOR RT AFT EMER EXTERIOR LIGHT. OPERATIONAL CHECKED GOOD.

Part: EPSU — INOPERATIVE (CABIN) · airframe 29,005 hrs · 25,154 cycles

LEFT & RIGHT OVERWING EXTERNAL EMER LIGHTS INOPERATIVE. R & R NR 4 EPSU IAW WC 33-700-19. OPERATIONS CHECKED GOOD IAW WC 33-700-17. EMER LIGHTING BATTERY PN 2013-1A & SN 108533.

Part: CRADLE — BROKEN (FLASHLIGHT) · airframe 28,782 hrs · 24,919 cycles

FIRST OFFICER'S EMER FLASH LIGHT CRADLE BROKEN. R & R FIRST OFFICER'S EMER FLASHLIGHT ASSEMBLY IAW AMM 33-50-16-000-801-A & 33-50-16-400-801-A. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,709 hrs · 24,832 cycles

FLOOR PROXIMITY STRIP LIGHT INOPERATIVE. R & R FLOOR PROXIMITY STRIP LIGHT IAW AMM 33-500-12. OPERATIONS CHECKED GOOD.

Part: CONTROL UNIT — FAILED (BRAKE SYSTEM) · airframe 28,544 hrs · 24,702 cycles

ON APPROACH, LOWERED LG, BRK INBD INOP MSG. MSG CLEARED WHEN GEAR WAS RAISED ON THE GO AROUND, MSG REAPPEARED ON SECOND APPROACH & LANDING & REMAINED AFTER LANDING. INBD BRK TEMPS GREEN AT THE BOTTOM OF THE SCALE. R & R BRAKE CONTROL UNIT IAW AMM 32-41-02-000-801-A & 32-41-02-400-801-A. OPERATIONS CHECKED GOOD.

Part: SKIN — CRACKED (FUSELAGE) · airframe 28,471 hrs · 24,647 cycles

DURING MBV INSPECTION, FOUND LT UPPER FUSELAGE SKIN CRACKED AT FRAME 75 STRINGER 2R. ACFT WAS REMOVED FROM SERVICE FOR MBV INSPECTION & WILL BE RETURNED TO SERVICE AFTER MBV INSPECTION. PERFORMED PERMANENT REPAIR IAW ERS-EM-53MR-814. REPAIR MATERIALS FILLER 2024T3 .063, REPAIR DOUBLER 2024T3 .080, REPAIR ANGLE 2024T3 .063 & ANGLE FILLER 2024T3 .032.

Part: FLOOR SUPPORT — MECHANIC ERROR (FUSELAGE) · airframe 28,471 hrs · 24,647 cycles

DURING IMBV INSPECTION, FOUND THE LT LAVATORY FLOOR OMEGA BEAM HAD A MISDRILLED HOLE AFT OF FRAME 61. ACFT WAS REMOVED FROM SERVICE FOR IMBV INSPECTION & WILL BE RETURNED TO SERVICE AFTER IMBV INSPECTION. PERFORMED PERMANENT REPAIR IAW EO-EM-53MR-846. REPAIR MATERIALS FILLER AL2024-T3 0.050 INCHES, DOUBLER AL2024-T3 0.050 INCHES.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 28,471 hrs · 24,647 cycles

DURING IMBV INSPECTION, FOUND THE RT LAVATORY FLOOR OMEGA BEAM CRACKED NEAR A NUTPLATE CUT OUT. ACFT WAS REMOVED FROM SERVICE FOR IMBV INSPECTION & WILL BE RETURNED TO SERVICE AFTER IMBV INSPECTION, PERFORMED PERMANENT REPAIR ON THE RT LAVATORY FLOOR OMEGA BEAM CRACK NEAR NUTPLATE CUT OUT IAW EO-EM-53MR-845. REPAIR MATERIALS FILLER AL2024-T3 0.050 INCHES, DOUBLER AL2024-T3 0.050 INCHES.

Part: FITTING — GOUGED (RT AILERON) · airframe 28,471 hrs · 24,647 cycles

DURING MBV INSPECTION, FOUND RT AILERON DAMPNER FITTING GOUGED. ACFT WAS REMOVED FROM SERVICE FOR MBV INSPECTION & WILL BE RETURNED TO SERVICE AFTER MBV INSPECTION. R & R RT AILERON DAMPNER FITTING IAW EO EM-27MR-112.

Part: WIRE — BROKEN (CABIN) · airframe 28,471 hrs · 24,647 cycles

PROXIMITY LIGHT NR 1, 2 & 3 HAVE BROKEN WIRES. R & R PROX LIGHT NR 1, 2 & 3 IAW AMM 33-50-12 SEE NRTC BOW 168084 FOR FINAL INSTALLATION & OPERATIONS CHECK.

Part: WIRE — BROKEN (CABIN) · airframe 28,471 hrs · 24,647 cycles

NUMBER 4 EMER LIGHT STRIP HAS BROKEN WIRE. R & R NR 4 EMER LIGHT STRIP IAW AMM 33-50-12. SEE NRTC BOW 168084 TASK NR 1 FOR OPERATIONS CHECK.

Part: SKIN — CRACKED (FUSELAGE) · airframe 28,471 hrs · 24,647 cycles

RIGHT EXTERIOR FUSELAGE SKIN CRACKED AROUND 3 RIVETS FRAME 79 MARKED. REPAIRED RT EXTERIOR FUSELAGE SKIN AROUND 3 RIVETS FRAME 79 BY INSTALLING BUSHING IAW ERS EM-5300-822. SEE TURNOVER FOR DETAILS.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 28,471 hrs · 24,647 cycles

EXTERNAL FUSELAGE SKIN HAS FIVE BURN MARKS FROM FRAME 21 - 26 & BETWEEN STRINGER 19R & 21R MARKED. TWO BURN MARKS BETWEEN FRAME 25 - 26, STRINGER 20R - 19R & ONE BURN MARK BETWEEN FRAME 23 - 24, STRINGER 21R - 20R ACCEPTED IAW ERS-EM-5300-832. AFT BURN MARK BETWEEN FRAME 22 - 23, STRINGER 21R - 20R FOUND WITHIN LIMITS IAW EMB SRM 51-10-05. PERFORMED REPAIR TO FWD BURN MARK BETWEEN FRAME 22 - 23, STRINGER 21R - 20R IAW SRM 53-21-01. SEE TASK & WIP ENTRIES FOR DETAILS.

Part: SKIN — CRACKED (FUSELAGE) · airframe 28,471 hrs · 24,647 cycles

LEFT EXTERIOR FUSELAGE SKIN CRACKED AROUND RIVET FRAME 80 MARKED. REPAIRED LT EXTERIOR FUSELAGE SKIN AROUND RIVET FRAME 80 BY INSTALLING BUSHING IAW ERS EM-5300-820. SEE TURNOVER FOR DETAILS.

Part: SKIN — CRACKED (FUSELAGE) · airframe 28,471 hrs · 24,647 cycles

LEFT EXTERIOR FUSELAGE SKIN CRACKED AROUND 2 RIVETS FRAME 78 MARKED. REPAIRED LT EXTERIOR FUSELAGE SKIN AROUND 2 RIVETS FRAME 78 BY INSTALLING BUSHING IAW ERS ERS-EM-5300-820.

Part: SKIN — CRACKED (FUSELAGE) · airframe 28,471 hrs · 24,647 cycles

LEFT EXTERIOR FUSELAGE SKIN CRACKED AROUND 2 RIVETS FRAME 75 MARKED. REPAIRED LT EXTERIOR FUSELAGE SKIN AROUND 2 RIVETS FRAME 75 BY INSTALLING BUSHING IAW ERS EM-5300-820. SEE TURNOVER FOR DETAILS.

Part: SKIN — CRACKED (FUSELAGE) · airframe 28,471 hrs · 24,647 cycles

LEFT EXTERIOR FUSELAGE SKIN CRACKED AROUND 2 RIVETS FRAME 79 MARKED. REPAIRED LT EXTERIOR FUSELAGE SKIN AROUND 2 RIVETS FRAME 79 BY INSTALLING BUSHING IAW ERS EM-5300-820. SEE TURNOVER FOR DETAILS.

Part: BATTERY — DISCHARGED (CABIN) · airframe 28,471 hrs · 24,647 cycles

LEFT & RIGHT OVERWING EMER LIGHTS INOPERATIVE. R & R NR 4 EMER LIGHT POWER SUPPLY & BATTERY IAW AMM 33-50-04. OPERATIONS CHECKED GOOD.

Part: SKIN — CRACKED (FUSELAGE) · airframe 28,471 hrs · 24,647 cycles

LEFT EXTERIOR FUSELAGE SKIN CRACKED AROUND 3 RIVETS FRAME 77 MARKED. REPAIRED LT EXTERIOR FUSELAGE SKIN AROUND 3 RIVETS FRAME 77 BY INSTALLING BUSHING IAW ERS EM-5300-820. SEE TURNOVER FOR DETAILS.

Part: SKIN — CRACKED (FUSELAGE) · airframe 28,471 hrs · 24,647 cycles

RIGHT EXTERIOR FUSELAGE SKIN CRACKED AROUND RIVET FRAME 77 MARKED. REPAIRED RT EXTERIOR FUSELAGE SKIN AROUND RIVET FRAME 77 BY INSTALLING BUSHING IAW ERS EM-5300-822. SEE TURNOVER FOR DETAILS.

Part: SKIN — CRACKED (FUSELAGE) · airframe 28,471 hrs · 24,647 cycles

RIGHT EXTERIOR FUSELAGE SKIN CRACKED AROUND RIVET FRAME 78 MARKED. REPAIRED RT EXTERIOR FUSELAGE SKIN AROUND RIVET FRAME 78 BY INSTALLING BUSHING IAW ERS EM-5300-822. SEE TURNOVER FOR DETAILS.

Part: VALVE — BROKEN (LAVATORY TANK) · airframe 28,368 hrs · 24,558 cycles

LEVER ON DRAIN PORT OF EXTERNAL LAVATORY SERVICE DUMP VALVE IS BROKEN. REMOVED AND REPLACED LAVATORY TANK IAW 38-32-01, OPS CHECKED GOOD.

Part: HANDLE — OUT OF POSITION (MAIN DOOR) · airframe 27,712 hrs · 23,996 cycles

CREW UNABLE TO OPEN MAIN DOOR FROM INSIDE ACFT. DOOR HAD TO OPENED BY RAMP FROM OUTSIDE. REPEAT WRITE UP IAW PAGE 3595075. REPOSITIONED INTERNAL DOOR HANDLE ON TORQUE TUBE IAW AMM 52-11-01. NORMAL OPERATION NOTED.

Part: DOOR — LACK OF LUBE (CABIN) · airframe 27,710 hrs · 23,995 cycles

ON ARRIVAL PAX DOOR COULD NOT BE OPENED FROM THE INSIDE. GND CREW OPENED DOOR FROM THE OUTSIDE. COMPLIED WITH DOOR LUBRICATION TASK 53-21-02-600-801-A. OPERATIONS CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 27,374 hrs · 23,712 cycles

FORWARD CABIN EMERGENCY FLASHLIGHT INOPERATIVE. R & R FWD CABIN EMERGENCY FLASHLIGHT ASSEMBLY IAW AMM 33-50-16. OPERATIONS CHECKED GOOD.

Part: ESCAPE ROPE — UNSECURE (COCKPIT) · airframe 26,766 hrs · 23,192 cycles

FIRST OFFICER`S ESCAPE ROPE DOOR OPENS DURING TAKEOFF & LANDING & DURING LIGHT CHOP. RE-SECURED FIRST OFFICER`S ESCAPE ROPE IAW AMM 25-60-00, OPERATIONS CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 26,754 hrs · 23,182 cycles

AFT GALLEY FLASHLIGHT INOPERATIVE. R & R AFT GALLEY FLASHLIGHT.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 26,754 hrs · 23,182 cycles

FORWARD GALLEY FLASHLIGHT INOPERATIVE. R & R FWD GALLEY FLASHLIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,141 hrs · 22,709 cycles

FLOOR PROXIMITY STRIP LIGHT AT SEAT 8 IS INOPERATIVE. R & R FLOOR PROXIMITY STRIP LIGHT AT SEAT 8 IAW 145 AMM 33-50-12. OPERATIONS CHECKED GOOD, NO FURTHER DEFECTS NOTED.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 25,732 hrs · 22,394 cycles

OVERHEAD EMERGENCY LIGHT AT MAIN DOOR INOPERATIVE. R & R BULB IAW AMM 33-50-08. OPS GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 25,698 hrs · 22,366 cycles

RT OVERWING EMERGENCY LIGHT INOPERATIVE. R & R LAMP IAW AMM 33-50-10. OPS CHECKED GOOD.

Part: CONTROLLER — FAILED (CABIN PRESSURE) · airframe 25,310 hrs · 22,043 cycles

FLIGHT 3051, CREW REPORTED A RAPID DECOMPRESSION AT 34000 FT. CABIN ALTITUDE CLIMBED ABOVE 10000. PERFORMED MEMORY ITEMS AND INITIATED AN EMERGENCY DESCENT. 02 MASK DEPLOYED AUTOMATICALLY. ACFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. R & R CABIN PRESSURE CONTROL SYSTEM DIGITAL CONTROLLER IAW AMM 21-31-01. THE FUNCTIONAL CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: PUMP — FAILED (HYD SYSTEM) · airframe 25,208 hrs · 21,960 cycles

DURING CLIMB, RECEIVED EICAS MESSAGE HYD 1 LOW QTY. FOLLOWED AOM PROCEDURES MONITORED HYD 1 QTY INDICATION. HYD 1 QTY INDICATION BELOW AMBER RANGE AND PRESSURE DROP TO 2900 PSI. AN EMERGENCY WAS DECLARED AND DIVERTED. LANDING WAS UNEVENTFUL AND HYD 1 QTY AND HYD 1 SYS NEVER FAILED. HYD 1 SYS INDICATOR IS IN THE AMBER RANGE WITH NO PRESSURE APPLIED. CREW NOTICED A BURNING ODOR AT THE GATE DURING THE WALK AROUND AND FOUND LEAKING HYD FLUID FROM THE BOTTON OF THE NR 1 ENGINE NACELLE. ACFT REMOVED FROM SERVICE. R & R ENGINE DRIVEN PUMP 1 IAW 29-10-03. OPS AND LEAK CHECKED GOOD. ACFT RETURNED TO SERVICE.

Part: INVERTER — UNSERVICEABLE (EMERGENCY LIGHTS) · airframe 24,938 hrs · 21,768 cycles

DURING B INSPECTION, FOUND THE FWD RT PASSENGER CABIN EMERGENCY EXIT SIGN INOPERATIVE. ACFT REMOVED FROM SERVICE. TROUBLESHOT AND FOUND THE EMERGENCY LIGHT DC/AC INVERTER NR 3 THE PROBLEM. R & R THE EMERGENCY LIGHT DC/AC INVERTER NR 3 IAW AMM 33-50-11. OPS CHECKED GOOD. ACFT RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (COCKPIT & CABIN) · airframe 24,713 hrs · 21,572 cycles

DURING MX INSP SMELLED SMOKE ODOR WHEN ENTERED INTO THE COCKPIT AND NOTICED THUR TO THE FRONT OF THE CABIN. NO SMOKE OR POPPED BREAKERS. THE ACFT WAS REMOVED FROM SERVICE. COMPLIED WITH OPS CHECK OF CONDITION AIR DISTRIBUTION SYS IAW 21-20-00.THE CHECK WAS GOOD, NO ODOR NOTED AT THIS TIME. PERFORMED ENGINE RUNS FOR ODOR EVENT TROUBLESHOOTING IAW ETN-EM-72-034. NO DEFECTS NOTED, ODOR RATING ALL CATEGORIES 1. THE ACFT WAS RELEASED FOR FUNCTIONAL CHECK FLIGHT PURPOSES ONLY. THE FUNCTIONAL CHECK FLIGHT WAS SATISFACTORY. ACFT OK FOR SERVICE.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 24,110 hrs · 21,126 cycles

DURING MAINTENANCE INSPECTION FOUND THAT WITH GROUND POWER APPLIED AND AIRCRAFT POWER ON, A STRONG BURNING ODOR AND SMOKE WAS OBSERVED COMING FROM UNDER COCKPIT FLOOR. THE AIRCRAFT WAS REMOVED FROM SERVICE. ACCESSED COCKPIT FLOOR PANELS, PERFORMED GENERAL VISUAL INSEPCTION FOR DAMAGE. PERFORMED OPERATIONAL CHECKS. INSPECTED EXTERNAL POWER RECEPTACLE, LEFT AND RIGHT POWER DISTRIBUTION BOXES. CHECKED TORQUE OF ELECTRICAL CABLE TO WINDSHIELD TEMPERTURE CONTROLLER. AUTOPILOT FUNCTIONAL TEST. NO EVIDENCE WAS NOTED OVER A PERIOD OF 3 DAYS. ALL SYSTEMS CHECKED GOOD. NO DAMAGE WAS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: RETAINER — BROKEN (CABIN) · airframe 24,116 hrs · 21,132 cycles

DURING B INSPECTION FOUND THE LEFT FAR AFT NR 8 AISLE EMERGENCY LIGHT STRIP RETAINER BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT FAR AFT NR 8 AISLE EMERGENCY LIGHT STRIP RETAINER AS REQUIRED. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SKIN — CANNING (FUSELAGE) · airframe 24,110 hrs · 21,126 cycles

SKIN, FRAMES 22 AND 23 BELOW STRINGER 5L OIL CANNING. INSTALLED REPAIR DOUBLER AND FILLER IAW AE EO EM-53MR-2104.

Part: SILL — CORRODED (FUSELAGE) · airframe 24,115 hrs · 21,131 cycles

DURING MAINTENANCE INSPECTION FOUND THE CARGO DOOR LOWER SILL CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CARGO DOOR LOWER SILL IAW EMB SRM 51-40-02 AND ETN# ETN-EM-53-224. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE — BROKEN (CABIN) · airframe 24,115 hrs · 21,131 cycles

DURING MAINTENANCE INSPECTION FOUND THE AFT AISLE EMERGENCY LIGHT STRIP CONNECTOR BROKEN WIRE. THE AIRCRAFT WAS REMOVED FROM SERVICE. INSTALLED SERVICEABLE CONNECTOR ON THE AFT AISLE EMERGENCY LIGHT STRIP IAW EMB 145 SWPM 20-21-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONNECTOR — MISSING (CABIN) · airframe 24,116 hrs · 21,132 cycles

DURING MAINTENANCE INSPECTION FOUND THE CONNECTOR FOR EMERGENCY LIGHT STRIP AT PANEL 251HF MISSING. THE AIRCRAFT WAS REMOVED FROM SERVICE. INSTALLED SERVICEABLE FOR EMERGENCY LIGHT STRIP CONNECTOR AND PIN AT FLOORBOARD 251HF AT SPLICE SP9114; IAW EMB 145 SWPM 20-50-01 AND EMB 145 SWPM 20-21-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — BROKEN (CABIN) · airframe 24,116 hrs · 21,132 cycles

DURING MAINTENANCE INSPECTION FOUND THE EMERGENCY LIGHT STRIP NR 6 EXTRUSION BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 6 EMERGENCY LIGHT STRIP ASSEMBLY. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE — BROKEN (CABIN) · airframe 24,116 hrs · 21,132 cycles

DURING MAINTENANCE INSPECTION FOUND THE AFT AISLE EMERGENCY LIGHT STRIP HAS A BROKEN WIRE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 8 EMERGENCY LIGHT STRIP IAW EMB-145 AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: STRIKER — CORRODED (CARGO DOORWAY) · airframe 24,110 hrs · 21,126 cycles

CARGO DOOR CUTOUT CORRODED JUST BELOW LT AND RT LWR STRIKER PLATES. REPAIRED STRIKER PLATE AREA IAW AEA EO EM-53MR-1129.

Part: DOOR SEAL — TORN (MAIN DOOR) · airframe 24,116 hrs · 21,132 cycles

DURING MAINTENANCE INSPECTION FOUND THE MAIN DOOR SEAL TORN AT THE FOLDING FLAP. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE MAIN DOOR SEAL IAW EMB 145 AMM 52-18-04 LEAK CHECK GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN)

LEFT EXTERNAL OVERWING EMERGENCY LIGHT INOP. REPLACED NR 4 BATTERY AND CHARGER.

Part: WIRE — CHAFED (EMERGENCY LIGHT)

BOTH EXTERNAL OVERWING EMERGENCY LIGHTS INOP. RELACED LIGHT ASSY ON RIGHT SIDE DUE TO CHAFED WIRES.

Part: BATTERY — DISCHARGED (CABIN) · airframe 23,479 hrs · 20,621 cycles

DURING MAINTENANCE INSPECTION FOUND THE BATTERY PACK NR 4 EMERGENCY LIGHTS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 4 EMERGENCY LIGHTS BATTERY CHARGER AND BATTERY IAW EMB 145 AMM 33-50-04. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 23,479 hrs · 20,621 cycles

ON FLIGHT 4200 THE CREW REPORTED THE CAPTAIN'S FLASHLIGHT WAS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CAPTAIN'S FLASHLIGHT ASSEMBLY IAW EMB MM 25-60-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONNECTOR — LOOSE (EXIT SIGN) · airframe 23,195 hrs · 20,398 cycles

DURING B INSPECTION FOUND THE FORWARD BULKHEAD EMERGENCY "EXIT" SIGN WILL NOT ILLUMINATE. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND LOOSE CONNECTOR ON LIGHT SECURED AS REQUIRED. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 23,062 hrs · 20,286 cycles

DURING B INSPECTION FOUND THE OVERWING EMERGENCY LIGHTS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. TROUBLESHOT OVERWING EMERGENCY LIGHTS, FOUND THE PROBLEM TO BE THE NR 4 EMERGENCY LIGHTING BATTERY AND CHARGER. REMOVED AND REPLACED THE NR 4 CHARGER AND BATTERY ASSEMBLY IAW W/C 33-700-19. THE OPERATIONAL CHECK WAS GOOD IAW W/C 33-700-17. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 22,742 hrs · 20,050 cycles

DURING B INSPECTION FOUND THE FORWARD GALLEY EMERGENCY FLASHLIGHT NOT CHARGING. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FORWARD FLIGHT ATTENDANT FLASHLIGHT ASSEMBLY. THE OPERATIONAL CHECK WAS GOOD IAW EMB AMM 33-50-16. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: PANEL — DAMAGED (CABIN) · airframe 21,531 hrs · 19,101 cycles

DURING B-INSPECTION FOUND THE MAIN DOOR EMERGENCY LIGHT PANEL DAMAGED AND CRACKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED MAIN DOOR EMERGENCY LIGHT PANEL IAW EMB AMM 25-23-04. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,512 hrs · 18,290 cycles

DURING MAINTENANCE BASE VISIT FOUND THE AFT CEILING EMERGENCY LAMP INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AFT AISLE EMERGENCY LAMP IAW EMB AMM TASK 33-50-08-000-801A/33-50-08-400-801A. THE OPERATIONAL TEST WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: STRIP — DAMAGED (CABIN) · airframe 20,135 hrs · 17,983 cycles

DURING MAINTENANCE BASE VISIT FOUND THE FLOOR PROXIMITY LIGHTING STRIP LIGHT AT ROWS 8-9 DAMAGED. THE AIRCRAFT WAS REMOVED FROM SERVICE. THE FLOOR PROXIMITY STRIP WAS REPLACED IAW EMB 145 AMM 33-50-12. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: DETECTION SYS — FALSE ACTIVATION (CARGO SMOKE) · airframe 22,205 hrs · 19,185 cycles

ON FLIGHT 3545 AFTER PUSHBACK THE CREW RECEIVED A BAGGAGE SMOKE WARNING MESSAGE. DISCHARGED EXTINGUISHING BOTTLE AND FOLLOWED EPC & AOM PROCEDURES. INDICATIONS REMAINED UNTIL FIRE DEPARTMENT, OPENED CARGO DOOR AND THE FIRE DEPARTMENT FOUND NO INDICATION OF FIRE OR SMOKE IN CARGO COMPARTMENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED FIRE EXTINGUISHER BAGGAGE PUSH BUTTON SWITCH IAW AMM 20-13-04 AND REMOVED AND REPLACED BOTH CARGO SMOKE DETECTOR AT CARGO COMPARTMENT IAW AMM 26-15-01. ALSO REMOVED AND REPLACED TEST RELAY FOR BAGGAGE SMOKE (K0629) IAW AMM STAND PRACT 20-13-02. THE OPERATIONAL CHECK FOR THE SYSTEM TEST IS OK AT THIS TIME.

Part: CONNECTOR — DISCONNECTED (EXIT SIGN) · airframe 19,355 hrs · 17,422 cycles

DURING MAINTENANCE BASE INSPECTION FOUND THE EMERGENCY EXIT IDENTIFIER SIGN INSTALLED ON THE FORWARD CABIN SEALING PANEL INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED THE FORWARD CABIN CEILING PANEL. FOUND CONNECTOR FOR EMERGENCY LIGHT NOT CONNECTED. RECONNECTED CONNECTOR AND REINSTALLED CEILING PANEL IAW EMB AMM 25-22-04-020-001 ITEM (3) AND 25-22-04-420-001 (2). THE OPERATIONAL CHECK WAS GOOD. NO PARTS REMOVED OR REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,160 hrs · 17,283 cycles

DURING MAINTENANCE BASE VISIT FOUND THE CARGO DOOR SILL CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED CARGO SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FAN — FAULTY (E&E BAY) · airframe 18,931 hrs · 17,103 cycles

ON FLIGHT 2731 THE CREW REPORTED A BUZZING/VIBRATION NOISE IN CLIMB FROM 8K TO 13K WITH AN ODD ODOR. THE CAPTAIN ELECTED TO RETURN TO DFW. THE NOISE RETURNED DESCENDING THROUGH 8,7K WITH AN ELECTRICAL MELTING ODOR. THE NOISE SUBSIDED AT 5K AND THE ODOR DISSIPATED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT FORWARD AVIONICS FAN PART NUMBER 526484, S/N 104407326 AND NR 2 FAN INVERTER PART NUMBER 524864, S/N E03092215. AN OPERATIONAL CHECK WAS PERFORMED ON THE LEFT AND RIGHT RAM AIR VALVE. PERFORMED GROUND RUN OF AIRCRAFT, NO ODOR OR DEFECTS NOTED AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FAN — SEIZED (COCKPIT) · airframe 18,913 hrs · 17,092 cycles

ON FLIGHT 2920 DURING CLIMBOUT TESTING THE ANTI ICE THE CREW REPORTED, RECEIVED FUMES IN THE COCKPIT. THE CAPTAIN DECLARED AN EMERGENCY AND RETURNED TO CLE. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. TROUBLESHOT AND FOUND A SLIGHT BURNING ODOR FROM THE COCKPIT RECIRCULATION FAN . WHEN THE FAN WAS SUPPOSE TO BE RUNNING, THE FAN BLADES WERE FROZEN IN POSITION. REMOVED AND REPLACED THE RECIRCULATION FAN IAW EMB 145 AMM 21-24-01-000-801-A AND 21-24-01-400-801-A. THE OPERATIONAL CHECK WAS GOOD AND NO ELECTRICAL ODOR WAS NOTICED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 18,506 hrs · 16,787 cycles

DURING MAINTENANCE BASE VISIT THE OVERWING EXTERIOR EMERGENCY LIGHT WAS FOUND TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY POWER SUPPLY. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 14,794 hrs · 13,859 cycles

DURING MAINTENANCE BASE INSPECTION THE FORWARD SERVICE DOOR WAS FOUND TO BE CORRODED. FRAME 19 AT SILL ATTACHMENT HAS 3 MISDRILLED HOLES. FRAME 17 HAS 2 MISDRILLED HOLES JUST ABOVE STRINGER 16 AT SILL ATTACHMENT. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED FORWARD SERVICE DOOR SILL IAW EMBRAER SRM 51-40-02. REPAIRED MISDRILLED HOLES ON FRAME 19 EO EM53MR-1375. REPAIRED MISDRILLED HOLES ON FRAME 17 IAW EO EM-53MR-1376. AIRCRAFT WAS RETURNED TO SERVICE. ALL PARTS REMOVED: FORWARD SILL PART NUMBER 145-21725-613. FRAME 19-PART NUMBER 145-24145-002. FRAME 17-PART NUMBER 145-22186-611. AIRCRAFT RETURNED TO SERVICE.

Part: SIGN — INOPERATIVE (CABIN) · airframe 14,603 hrs · 13,692 cycles

ON FLIGHT 3200: DURING A PS-2 CHECK, AN EMERGENCY EXIT SIGN ON SEAT 12A WAS FOUND INOPERABLE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED EMERGENCY EXIT SIGN ON SEAT 12A. AIRCRAFT RETURNED TO SERVICE.

Part: SILL — CORRODED (ZONE 100) · corrosion level 2 · airframe 9,807 hrs · 9,319 cycles

DURING A HMBV INSPECTION, THE CARGO DOOR CUT OUT LOWER SILL WAS FOUND TO BE CORRODED. REPLACED LOWER SILL WITH PART NUMBER 145-25480-603 IAW SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE.

Part: FAN — SEIZED (ZONE 100) · airframe 8,748 hrs · 8,305 cycles

BURNING ELECTRICAL ODOR IN CABIN AND FLIGHT DECK DURING TAXI OUT, RETURNED TO BLOCK. REMOVED AND REPLACED RECIRCULATION FAN AND PACK VALVE IAW EMB AMM. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE.

Part: SKIN — DENTED (FS 16-17)

A DENT WITH A SCRATCH WAS DISCOVERED ON THE SKIN PANEL BETWEEN FRAMES 16 AND 17 AD BETWEEN STRINGERS 18L AND 19L. PERFORMED A CUTOUT OF THE SKIN PANEL TO REMOVE THE DAMAGE. FABRICATED A FILLER AND REPAIR DOUBLER. REPAIR DONE IAW EMB REPAIR STATEMENT IC2005-145/5137 PARA 3 DATED SEPT 15, 2003. (M)

Part: FLOOR SUPPORT — CORRODED (FR 20)

THE LEFT OMEGA BEAM AT FRAME 20 WAS FOUND CORRODED. PERFORMED A CUT OUT OF LEFT OMEGA BEAM TO REMOVE CORROSION. PREPARED DOUBLER, FILLER, REPAIR PLATE AND TWO SHIMS. REPAIR DONE IAW EMB145 SRM, SRM 145/1142 REV 30 CHAPTER 53-00-10 FIG 201. (M)

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT)

CREW REPORTED THE AFT SECTION, ROW 12, FLOOR PROXIMITY, OVERHEAD EXIT LIGHT, AND SEVERAL FORWARD EMERGENCY LIGHTS TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 2 POWER SUPPLY TO CORRECT THE PROBLEM. THE NR 1,3, AND 4 POWER SUPPLY UNITS AND ALL 4 BATTERIES WERE ALSO CHANGED AS A PRECAUTION. ALL WORK AND OPERATIONAL CHECKS WERE DONE IAW THE MM. (SW21200500265)