N935AE

Part: THERMOSTAT — FAULTED (ANTI ICE) · airframe 45,397 hrs · 41,383 cycles

ENGINE #2 BLEED OVERHEAT FOLLOWED BY WING ANTI ICE FAIL, STAB ANTI ICE FAIL, AND ICE COND ANTI ICE INOP. R&R #200 THERMOSTAT AFN AC POSTMOD IN REF TO EMB 145 AMM 36-11-06. NO DEFECTS NOTED OPS CHK REQ. (SS) OPS AND LEAK CHECK GOOD. ANTI ICING SYSTEM OPS CHECK GOOD IAW AMM 30-00-00. A/C OK FOR SERVICE AT THIS TIME.

Part: WARNING MESSAGE — ILLUMINATED (ENGINE ANTI-ICE) · airframe 43,996 hrs · 39,787 cycles

E1 A/I FAIL MSG WITH ICE DETECTION OVERRIDE KNOB SET TO ENG AS WELL AS ALL. ENGINE ANTI-ICING SYSTEM.

Part: DUCT — CRACKED (ENGINE ANTI-ICE) · airframe 43,996 hrs · 39,787 cycles

E1 A/ICE FAIL IN FLIGHT MEL 12APR25 18:42 BWI C10218 30-8-1 ENGINE ANTI-ICING VALVES FACT 14APR25 04:30 ROA FOUND #100 ENGINE A/I DUCT CRACKED AT XDUCER SENSE LINE FITTING. R/R'D DUCT IAW MM 30-21-05-04, C/W ENG THERMO A/I SYSTEM OPS CK IAW MM TASK 30-21-00-700-803-A. OPS CK GOOD NO FURTHER DEFECTS NOTED. #100 A/I VALVE REACTIVATED IAW MM 31-21-01-04, CLEAR MEL.

Part: ENGINE — FAILED (NR 2) · airframe 43,326 hrs · 39,052 cycles

AT FL320 E2 FAIL AFTER CREW HEARD BANG & POP WITH E2 UNCOMMANDED SHUTDOWN. R & R #2 ENG IAW WC 71-00-00.

Part: WARNING MESSAGE — FALSE ACTIVATION (CARGO DOOR) · airframe 42,385 hrs · 38,017 cycles

ON T/O ROLL BAG DOOR OPEN IND. RETURNED TO GATE VERI FIED BAG DOOR SHUT. INSPECTED BAG BAY DOOR & SWITHES FOR PROPER OPERATION AND DEFECTS. NO DEFECTS NOTED, CLEANED AND LUBED MICROSWITCHES, OPEN AND CLOSED DOOR SEVERVAL TIMES. ALL INDICATIONS NORMAL. OK FOR SERVICE.

Part: CONTROLLER — FAULTED (CABIN PRESSURE) · airframe 42,318 hrs · 37,942 cycles

DURING CLIMB WHILE PERFORMING A/I TEST CABIN PRESS RATE JUMPED TO 3200FT/MIN. THEN DURING DESCENT CABIN PRESS RATE SPIKED TO 2000FT/MIN. AT LEVEL FLT CABIN PRESS RATE SPIKED TO -400FT/MIN. DURING ANOTHER DESCENT CABIN PRESS RATE SHOWED CLIMB TO 1000FT/MIN. R/R'D DIGITAL CONTROLLER PER MM 21-31-01. PERFORMED AUTO PRESSURE OPS CHECK PER MM 21-31-00-700-802-A.

Part: CHANNEL — CORRODED (RT WING) · corrosion level 2 · airframe 42,002 hrs · 37,581 cycles

57-2259 CORROSION ON RH WING FRONT SPAR LE II LWR ATTACHMENT GANG CHANNELS (4). R&R'S GANG CHANNELS IAW SRM51-40-02

Part: SUPPORT — CORRODED (FRMS 24-25) · corrosion level 2 · airframe 42,002 hrs · 37,581 cycles

53-2233 CORROSION ON CTR FUSE 2 CTR OMEGA BEAM LR VERT FLANGE AT BTW FR24-25. REPAIRE IAW EO1-53-24-0173

Part: SUPPORT — CORRODED (FRMS 23-24) · corrosion level 2 · airframe 42,002 hrs · 37,581 cycles

53-2114 CORROSION ON CF1 RH OMEGA BEAM AT BTW FR23-24. REPAIRED IAW EO1-53-24-0164

Part: SUPPORT — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 42,002 hrs · 37,581 cycles

53-2122 CORROSION ON RH OMEGA BEAM AT CF4. REPAIRED OMEGA BEAM IAW EO1-53-24-0165

Part: SUPPORT — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 42,002 hrs · 37,581 cycles

53-2124 CORROSION ON LH OMEGA BEAM ANCHOR NUT LOCATIONS AT CF4. REPAIRED IAW EO1-53-24-0165

Part: SUPPORT — CORRODED (FRMS 29-32) · corrosion level 2 · airframe 42,002 hrs · 37,581 cycles

53-2145 CORROSION ON CF2 LH SILL BTW FR29-32. R&R'D SILL IAW SRM51-40-02

Part: SUPPORT — CORRODED (FRMS 24-28) · corrosion level 2 · airframe 42,002 hrs · 37,581 cycles

53-2137 CORROSION ON CF2 CTR OMEGA BEAM BTW FR24-28. REPAIRED IAW EO1-53-24-0170

Part: CHANNEL — CRACKED (FRM 43) · airframe 42,002 hrs · 37,581 cycles

53-2115 LH OMEGA BEAM CRACKED ON IB SIDE AT CF1 FR43. REPAIRED IAW EO1-53-24-0169

Part: SUPPORT — CORRODED (FRMS 24-25) · corrosion level 2 · airframe 42,002 hrs · 37,581 cycles

53-2136 CORROSION ON CF2 RH OMEGA BEAM DOUBLER REPAIR BTW FR24-25. R&R'D DOUBLER REPAIR AND OMEGA BEAM IAW SRM53-22-10 AND EO1-53-24-0174

Part: SUPPORT — CORRODED (FRMS 19-23) · corrosion level 2 · airframe 42,002 hrs · 37,581 cycles

53-2131 CORROSION ON CTR OMEGA BEAM BTW FR19-23. R&R'D OMEGA BEAM IAW SRM51-40-02

Part: SUPPORT — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 42,002 hrs · 37,581 cycles

53-2123 CORROSION ON TOP OF CTR OMEGA BEAM ANCHOR NUT LOCATIONS AT CF4. REPAIRED OMEGA BEAM IAW EO1-53-24-0165

Part: CHANNEL — CORRODED (RT DOOR AREA) · corrosion level 2 · airframe 42,002 hrs · 37,581 cycles

53-2113 CORROSION ON RH SERVICE DOOR CHANNEL OROUND SCREW HOLES. R&R'D DOOR CHANNEL IAW SRM51-40-02

Part: GUSSET — CORRODED (FRMS 31-35) · corrosion level 2 · airframe 42,002 hrs · 37,581 cycles

53-2142 CORROSION ON CF2 LH GUSSET BTW FR31-35. R&R'D GUSSET IAW SRM51-40-02

Part: SUPPORT — CORRODED (FRMS 19-20) · corrosion level 2 · airframe 42,002 hrs · 37,581 cycles

53-2148 CORROSION ON CTR OMEGA BEAM AROUND NUTPLATE AT BTW FR19-20. REPAIRED IAW EO1-53-24-0168

Part: GUSSET — CORRODED (FRMS 59-61) · corrosion level 2 · airframe 42,002 hrs · 37,581 cycles

53-2075 CORROSION ON RH GUSSET BTW FR59-61. R&R'D IAW SRM53-40-02

Part: SUPPORT — CORRODED (FRMS 46-52) · corrosion level 2 · airframe 42,002 hrs · 37,581 cycles

53-2085 CORROSION ON SILL #6 BTW FR46-52. R&R'D SILL #6 IAW SRM53-40-02

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,002 hrs · 37,581 cycles

53-2092 CORROSION ON LH GUSSET #6. R&R'D GUSSET IAW SRM51-40-02

Part: BRACKET — CRACKED (FRM 43) · airframe 42,002 hrs · 37,581 cycles

53-2090 BRACKET CRACKED AT FR46 LH WING BOX. R&R'D BRACKET IAW EMB145 SRM51-40-02

Part: SUPPORT — CORRODED (FRM 30) · corrosion level 2 · airframe 42,002 hrs · 37,581 cycles

53-2100 CORROSION ON CF2 RH SILL #2 AT FR 30. R&R'D SILL IAW SRM51-40-02

Part: GUSSET — CORRODED (FRMS 59-61) · corrosion level 2 · airframe 42,002 hrs · 37,581 cycles

53-2074 CORROSION ON CTR GUSSET BTWFR59-61. R&R'D GUSSET IAW SRM53-40-02.

Part: SHEAR TIE — CRACKED (FRM 46 S13-14R) · airframe 42,002 hrs · 37,581 cycles

53-2088 SHEAR CLIP CRACKED AT FR46 BTW STR13R-14R. R&R'D SHEAR CLIP IAW EMB SRM51-40-02

Part: BRACKET — CRACKED (FRM 43) · airframe 42,002 hrs · 37,581 cycles

53-2091 BRACKET CRACKED AT FR46 RH WING BOX. R&R'D BRACKET IAW EMB145 SRM51-40-02

Part: SHEAR TIE — CRACKED (FRM 72 S16-17L) · airframe 42,002 hrs · 37,581 cycles

53-2078 SHEAR CLIP CRACKED AT RF1 FR72 BTW16L-17L. R&R'D IAW EMB SRM 51-40-02

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,002 hrs · 37,581 cycles

53-2095 CORROSION ON RH SILL#3. R&R'D SILL IAW SRM51-40-02

Part: GUSSET — CORRODED (FRMS 59-61) · corrosion level 2 · airframe 42,002 hrs · 37,581 cycles

53-2073 CF4 LH GUSSET CORRODED BTW FR59-61. R&R'D GUSSET IAW SRM51-40-02

Part: SHEAR TIE — CRACKED (FRM 49 S13-14R) · airframe 42,002 hrs · 37,581 cycles

57-2089 SHEAR CLIP CRACKED AT FR49 STR13R-14R. R&R'D SHEAR CLIP IAW EMB145 SRM51-40-02

Part: SHEAR TIE — CRACKED (FRM 65 S18-19L) · airframe 42,002 hrs · 37,581 cycles

53-2079 SHEAR CLIP CRACKED AT RF1 FR65 BTW STR18L-19L. R&R'D SHEAR CLIP IAW EMB SRM51-40-02

Part: CROSSBEAM — CORRODED (FRM 29) · corrosion level 2 · airframe 42,002 hrs · 37,581 cycles

53-2103 CORROSION ON CROSS BEAM AT FR29. R&R'D IAW EO1-05-24-0166

Part: SKIN — DENTED (THRUST REVERSER) · airframe 42,002 hrs · 37,581 cycles

78-2049 DENT ON LE OF LH TR LOWER DOOR SKIN. REPAIRED IAW EO1-54-24-0163

Part: SHEAR TIE — CRACKED (FRM 61 S6-7R) · airframe 42,002 hrs · 37,581 cycles

53-2061 SHEAR CLIP CRACKED AT RF1 FR61 BTW STR6R-7R. R&R'D SHEAR CLIP IAW EMB SRM51-40-02

Part: SUPPORT BRACKET — CRACKED (WNG-BDY FAIRING) · airframe 42,002 hrs · 37,581 cycles

57-2028 LH WING TO FUSELAGE LATERAL FAIRING SUPPORT BRACKET #3 IS CRACKED. R&R'D BRACKET IAW EMB SRM 51-40-02

Part: SHROUD — CRACKED (RT TE FLAP HINGE) · airframe 42,002 hrs · 37,581 cycles

57-2037 RH LOWER WING, OB LOWER SHROUD FLAP IB HINGE CRACKED. R%R'D HINGE IAW EMB SRM51-40-02

Part: SHROUD — CRACKED (LT TE FLAP HINGE) · airframe 42,002 hrs · 37,581 cycles

53-2036 LH LOWER WING OB LOWER SHROUD FLAP HAS CRACKED IB AND OB HINGES

Part: BRACKET — CRACKED (WNG-BDY FAIRING) · airframe 42,002 hrs · 37,581 cycles

57-2027 LH WING TO FUSELAGE LATERAL FAIRING BRACKET #2 IS CRACKED. R&R'D BRACKET IAW EMB SRM 51-40-02

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,442 hrs · 36,934 cycles

WINDSHEAR INOP, EGPWS INOP WITH RAD ALT FAIL MSG IN FLIGHT PERFORMED GVIOF GROUND STUD GSO383. CHECKS GOOD R/RD CONNECTORS P2227 &J2227 AS PRECAUTION CHECKED COAX CABLES WITH TDR CABLES W1979, W0036,& W0037 AU CHECK GOOD. PERFORMED RAD ALT SYS. OPERATIONAL TEST IAW 34-31-00. OPS CHECK GOOD.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,165 hrs · 36,595 cycles

L/G LEVER DISAGREE MSG IN FLIGHT. T/S IAW FIM TASK 32-32-00-810-803A STEPS 1,2,9 AND 22. NO DEFECTS NOTED TRANSITORY CONDITION.

Part: LAMP — INOPERATIVE (AFT) · airframe 41,122 hrs · 36,545 cycles

STARBOARD AFT EMERGENCY LAMP INOP-C/A-RAR STARBOARD AFT OVER WING EMERGENCY LIGHT LAMP OPS CHECK GOOD PER EMB AMM 33-50-10

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,046 hrs · 36,465 cycles

ELEC BURNING SMELL BEFORE DOOR CLOSE-C/A-FOUND #1 RECIRC FAN TO BE INOP DEFFERED AS REQUIREDM PROCEDURES C/W . PERFORMED ABNORMAL SMOKE /BURN SMELL CHECKS IAW FIM TASK 21-20-00-810-801-A

Part: LAMP — INOPERATIVE (AFT) · airframe 40,907 hrs · 36,335 cycles

AFT CEILING EMERGENCY LIGHT INOP-C/A-RAR AFT CEILING EMERGENCY LIGHT LAMP IAW EMB AMM 33-50-08-000-801-A AND 33-50-08-400-801-A. OPC GOOD. END.

Part: LAMP — INOPERATIVE (MAIN) · airframe 40,813 hrs · 36,236 cycles

MAIN DOOR EMERGENCY LIGHT INOP-C/A-RAR MAIN DOOR EMERGENCY LIGHT LAMP IAW EMB AMM 33-50-06-000-801-A AND 33-50-06-400-801-A. OPS CHECK G00D. END.

Part: LAMP — INOPERATIVE (LH & RH) · airframe 40,668 hrs · 36,090 cycles

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

Part: CRADLE — BROKEN (FLASHLIGHT) · airframe 40,477 hrs · 35,891 cycles

FA FLASHLIGHT HOLDER BROKEN. R & R FLASHLIGHT HOLDER IAW AMM 33-50-16. OPS CHECKED GOOD, NO FURTHER DEFECTS NOTED.

Part: NUT PLATE — BROKEN (RH) · airframe 40,450 hrs · 35,864 cycles

RH OVERWING EMERGENCY LIGHT INOP-C/A-FOUND BROKEN NUT PLATES ON ASSY. RAR RH OVERWING EMERGENCY LIGHT ASSY IAW EMB AMM 33-50-07-000-802-A AND 33-50-07-400-802-A. OPC GOOD. END.

Part: INVERTER — INOPERATIVE (FWD) · airframe 39,951 hrs · 35,308 cycles

LOWER FWD SERVICE DOOR EMERGENCY LIGHT INOP.-C/A-RAR EMERGENCY LIGHT INVERTER # 2 IAW AMM 33-50-11, ALL EMERGENCY LIGHTS OPC CHECK GOOD IAW AMM 33-50-04.

Part: INVERTER — INOPERATIVE (1ST) · airframe 39,951 hrs · 35,308 cycles

1ST FLOOR EMERGENCY LIGHT STRIP INOP.-C/A-RAR EMERGENCY LIGHT INVERTER # 2 IAW AMM 33-50-11, ALL EMERGENCY LIGHTS OPC CHECK GOOD IAW AMM 33-50-04.

Part: LIGHT — BURRED (CABIN) · airframe 39,564 hrs · 34,841 cycles

ELECTRICAL BURNING SMELL IN CENTER OF CABIN.-C/A-REF. NRWC 935-DFW-05862 AND NRWC 935-DFW-05861 RAR CELLING LIGHT 4A HOLDER HARNESS AND BALLAST UNIT PER AMM 33-21-06 AND 33-21-05. OPS CK GOOD

Part: NONE — BROKEN (LH) · airframe 39,219 hrs · 34,455 cycles

SUPPLEMENTAL C/A- LH OVERWING EMERGENCY LIGHT NUT PLATE BROKEN-C/A-DEFERRED PER ERS-EM-33DF-039 TDMI AUTHORIZATION NUMBER 935T3385. -C/A-RAR LH OVR WG EMER LIGHT IAW EMB 145 AMM 33-50-10 TDMI RESTORED

Part: LAMP — INOPERATIVE (LH) · airframe 39,219 hrs · 34,455 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 OPS CHECK GOOD

Part: NONE — NONE · airframe 39,181 hrs · 34,415 cycles

LH AND RH OVERWING EMERGENCY LIGHT INOP-C/A-TROUBLESHOT LH AND RH OVERWING EMERGENCY LIGHT IAW FIM TASK 33-50-00-810-804-A. RAR BATTERY POWER SUPPLY IAW EMB AMM 33-50-04-000-801-A AND 33-50-04-400-801-A. RAR BATTERY PACK IAW EMB AMM 33-50-04-000-802-A AND 33-50-04-400-802-A. OPC GOOD. END.

Part: CRADLE — BROKEN (FLASHLIGHT) · airframe 39,084 hrs · 34,315 cycles

FLT DECK/ATTENDANT EMERGENCY FLASHLIGHT/HOLDER CA FLASHLIGHT HOLDER CLIP BROKEN.-C/A-RAR FA EMERGENCY FLASHLIGHT ASSY IAW AMM 33-50-16. OPS CHECK GOOD. MEL RESTORED

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 39,070 hrs · 34,297 cycles

CEILING EMERGENCY LIGHT BETWEEN ROW 16 AND 17 INOP-C/A-RAR CEILING EMERGENCY LIGHT BULB BETWEEN ROW 16 AND 17. OPS CHECKED GOOD IAW AMM 33-50-08

Part: NONE — NONE · airframe 38,598 hrs · 33,782 cycles

DURING PS-2 CHECK FOUND THE EMERGENCY LIGHTS ON THE #2 SYSTEM DIM AND DIE OUT.-C/A-RAR #2 EMERGENCY LIGHTING SYSTEM POWER SUPPLY IAW ENVOY W/C 33-700-19. OPS CHECK GOOD. NO DEFECTS NOTED. END.

Part: NONE — NONE · airframe 38,527 hrs · 33,694 cycles

EMERGENCY EXIT ROW WINDOW SHADE INOP REF AML PAGE 4622257 ITEM 1 MEL 25-57 AUTH# 110119-N-C/A-RAR EMERGENCY EXIT ROW WINDOW SHADE IAW EMB 145 AMM 25-23-03 MEL RESTORED

Part: NONE — NONE · airframe 38,340 hrs · 33,475 cycles

FWD PROX LIGHT STRIP INOP-C/A-MADE REPAIR TO WIRE ON FWD CABIN FLOOR PROX STRIP LIGHT IAW EMB SWPM 20-21-00

Part: NONE — NONE · airframe 38,287 hrs · 33,412 cycles

DURING PS-2 CHK FOUND EMERGENCY FLOOR PPROXIMITY STRIP LIGHT AND EXIT IDENTIDIER SIGNON SERVICE DOOR INOP-C/A-RAR #2 BATTERY POWER SUPPLY IAW EMB145 33-50-04. OPC CHK GOOD FOR ALL LIGHTS.

Part: PARTITION — DAMAGED (LEFT) · airframe 37,586 hrs · 32,634 cycles

THE LH COCKPIT/PASSENGER PARTITION, BOTH OF THE GUIDE PIN HOLES ARE ELONGATED-C/A-MECHANICALLY MEASURED THE LH COCKPIT/CABIN PARTITION HOLES (UPPER.739? / LOWER .953?). THE UPPER GUIDE PIN HOLE IS WITHIN LIMITS IAW EMB 145 SRM 53-21-02. ACCOMPLISHED PERMANENT REPAIR ON THE LOWER GUIDE PIN HOLE IAW EMB 145 SRM 53-21-02 AND ETN-EM-53-153

Part: DOOR SILL — CORRODED · corrosion level 2 · airframe 37,586 hrs · 32,634 cycles

AT THE SERVICE DOOR, THE RH CENTER SILL HAS CORROSION DAMAGE (LEVEL 2 CORROSION)-C/A-RAR RH SERVICE DOOR CENTER SILL IAW EMB 145 SRM 51-40-02

Part: FLOOR SUPPORT — CORRODED (FRAME 20) · corrosion level 2 · airframe 37,586 hrs · 32,634 cycles

SSI 53-20-11 POSSIBLE CORROSION DAMAGE ON THE LH OMEGA BEAM AT FR 20 ON THE JUNCTION WITH THE CROSSBEAM.(LEVEL 2 CORROSION) -C/A-REMOVED, FABRICATED AND INSTALLED EXTERNAL ANGLE, FILLER AND SHIM ON LH OMEGA BEAM AT FR 20 ON THE JUNCTION WITH THE CROSSBEAM IAW EMB 145 SRM 53-00-10 FIGURE 201. SSI 53-20-11 POSSIBLE CORROSION DAMAGE ON THE LH OMEGA BEAM AT FR 20 ON THE JUNCTION WITH THE CROSSBEAM.(LEVEL 2 CORROSION) -C/A-REMOVED, FABRICATED AND INSTALLED EXTERNAL ANGLE, FILLER AND SHIM ON LH OMEGA BEAM AT FR 20 ON THE JUNCTION WITH THE CROSSBEAM IAW EMB 145 SRM 53-00-10 FIGURE 201.

Part: WEB — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 37,586 hrs · 32,634 cycles

CARGO DOOR LOWER FWD INNER WEB NUTPLATE HOLE CORRODED-C/A-INSTALLED CARGO DOOR INNER WEB LOWER FWD NUTPLATE HOLE REPAIR DOUBLER IAW EMB 145 SRM 52-30-01 ITEM 12 (LEVEL 2 CORROSION)

Part: WEB — DAMAGED (CARGO DOOR) · airframe 37,586 hrs · 32,634 cycles

CARGO DOOR INNER WEB HAS TOOL MARK ABOVE LOCKING MECHANISM-C/A-REPAIRED TOOLING MARK ON CARGO DOOR INNER WEB ABOVE LOCKING MECHANISM IAW EMB 145 SRM 52-30-01 ITEM 12 FIGURE 213

Part: DOOR SILL — CORRODED (FRMS 64-69 S16L) · corrosion level 2 · airframe 37,586 hrs · 32,634 cycles

CARGO DOOR SILL IS CORRODED. (LEVEL 2 CORROSION)-C/A-REMOVED AND REPLACED CARGO DOOR SILL (PN 145-25480-603) IAW EMB 145 SRM 51-40-02

Part: PROFILE — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 37,586 hrs · 32,634 cycles

CARGO DOOR UPPER INBD L PROFILE HAS 3 CORRODED NUTPLATE HOLES (1 BEING AT PREVIOUS BLEND) (LEVEL2 CORROSION)-C/A-RAR CARGO DOOR UPPER INBD L PROFILE IAW EMB 145 SRM 51-40-02

Part: STRUCTURE — DENTED (CARGO DOOR) · airframe 37,586 hrs · 32,634 cycles

CARGO DOOR LOWER OUTBD L PROFILE HAS DENT-C/A-RAR CARGO DOOR LOWER OUTBD L-PROFILE IAW EMB 145 SRM 51-40-02

Part: DOOR FRAME — CORRODED (FRAME 65) · corrosion level 2 · airframe 37,586 hrs · 32,634 cycles

CARGO DOOR CUTOUT LATERAL L-SHAPE IS CORRODED AT FR 65 (LEVEL 2 CORROSION)-C/A-ACCOMPLISHED REPAIR OF THE CARGO DOOR CUTOUT LATERAL L-SHAPE AT FR 65 BETWEEN STGR 15L-16L IAW EMB 145 SRM 53-31-04 AND ETN-EM-53-272

Part: DOOR FRAME — DAMAGED (CARGO DOOR) · corrosion level 2 · airframe 37,586 hrs · 32,634 cycles

CARGO DOOR LOWER AFT FRAME PREVIOUS BLENDED NUTPLATE HOLE CORRODED (LEVEL2 CORROSION)-C/A-UPON FURTHER INVESTIGATION DAMAGE IS ACTUALLY ON THE CARGO DOOR LOWER FWD LATERAL FRAME AT PREVIOUSLY BLENDED NUT-PLATE HOLE. ACCOMPLISHED PERMANENT REPAIR ON THE CARGO DOOR AT THE NUT-PLATE HOLE ON THE LOWER FWD LATERAL FRAME IAW EMB 145 SRM 52-30-04

Part: YOKE — CRACKED (LT ENGINE) · airframe 37,586 hrs · 32,634 cycles

LH ENGINE FWD LOWER PYLON YOKE CRACKED-C/A-REMOVED AND REPLACED LH ENGINE FWD LOWER PYLON YOKE FITTING IAW ERS-EM-54MR-698. NEW FITTING P/N EPNEM54EP487-02

Part: YOKE — CRACKED (RT ENGINE) · airframe 37,586 hrs · 32,634 cycles

RH ENGINE FORWARD LOWER PYLON YOKE CRACKED.-C/A-REMOVED AND REPLACED RH ENGINE FORWARD LOWER PYLON YOKE ASSEMBLY IAW ERS-EM-54MR-698 PT. A,

Part: SKIN — CHAFED (LT NACELLE) · airframe 37,586 hrs · 32,634 cycles

LH PYLON SKIN CHAFFED BETWEEN FR 67-68 AND STGR 7L-8L INSIDE 414DB-C/A-REPAIRED FUSELAGE SKIN INSIDE LH PYLON BETWEEN FRAMES 67-68 AND STRINGERS 7L-8L IAW EMB 145 SRM 53-31-01

Part: DOOR FRAME — CORRODED (PAX DOORWAY) · corrosion level 2 · airframe 37,586 hrs · 32,634 cycles

PAX DOOR LOWER FRAME CORRODED AROUND AFT NUT PLATE HOLE.(LEVEL 2 CORROSION)-C/A-REMOVED AND REPLACED PAX DOOR LOWER FRAME PROFILE (PN 145-34499-002) IAW EMB 145-SRM 51-20-03 AND 51-40-02.

Part: DOOR FRAME — CORRODED (SERVICE DOOR) · corrosion level 2 · airframe 37,586 hrs · 32,634 cycles

SERVICE DOOR LOWER FRAME CORRODED AROUND LOWER NUTPLATE HOLES.(LEVEL 2 CORROSION)-C/A-ACCOMPLISHED PERMANENT REPAIR ON SERVICE DOOR LOWER FRAME IAW ERS-EM-52MR-1121

Part: SKIN — DAMAGED (CARGO DOOR) · airframe 37,586 hrs · 32,634 cycles

CARGO DOOR EXTERIOR SKIN HAS A PREVIOUS BLEND (PAINTED OVER AND NOT ADDRESSED IN ADL) APPRX 12? FROM AFT EDGE, 24? FROM TOP-C/A-ACCOMPLISHED PERMANENT REPAIR OF CARGO DOOR EXTERNAL SKIN APPROX.. 12? FROM AFT EDGE AND 24? FROM TOP EDGE IAW EMB 145 SRM 52-30-01 RE ITEM 4 AND EMB 145 SRM 51-75-10 FOR REPAIR WITHOUT FINGERS

Part: SUPPORT — BROKEN (FLASHLIGHT) · airframe 37,011 hrs · 32,083 cycles

COCKPIT EMEEGENCY FLASHLIGHT PIN BOTTOM SUPPORT BROKEN. C/A: R & R EMERGENCY FLASHLIGHT ASSEMBLY, IAW AMM 35-50-16. OPERATIONS CHECK GOOD.

Part: BULB — INOPERATIVE (EXTERIOR LIGHT) · airframe 36,694 hrs · 31,758 cycles

RT FWD EXTERIOR EMERGENCY LIGHT INOP. C/A R & R RT FWD EXTERIOR EMERGENCY LIGHT BULB, IAW EMB 145 AMM 33-50-10. OPS CHK GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 36,658 hrs · 31,722 cycles

RT EXTERIOR LOWER EMERGENCY LIGHT INOP. C/A-R & R RT LOWER EXTERIOR EMERGENGY LIGHT BULB. OPS CHECK GOOD, IAW AMM 33-50-10.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 36,658 hrs · 31,722 cycles

FRONT HALF FLOOR EMERGENCY LIGHTS INOP. C/A-RAR EMERGENCY LIGHTING BATTERY ASSY AND CHARGER 1 AND 2, IAW W/C 33-700-19. PERFORMED OPC OF EMERGENCY LIGHT SYSTEM. OPC GOOD, IAW W/C 33-700-17.

Part: PRESSURE SWITCH — MALFUNCTIONED (RUDDER) · airframe 36,414 hrs · 31,517 cycles

EMERG DECLRD DUE TO RUDDER 1-2 INOP MSG. FLT LANDED-RUDDER SYST 2 INOP. REMOVED AND INSTALLED #2 RUDDER SYS PRESSURE SWITCH AMM 27-23-04 OPC GOOD NO LEAKS NOTED PN OFF: 98505 SN OFF:1542PN ON: 150048PH SN OFF: 3324

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 36,389 hrs · 31,488 cycles

FA FLASHLIGHT NOT CHARGING-C/A-RAR FA FLASHLIGHT IAW EMB 145 AMM 33-50-16. OPS CHECK GOOD..

Part: INVERTER — FAILED (CABIN) · airframe 36,341 hrs · 31,437 cycles

CENTER AISLE FWD EXIT IDENTIFIER SIGN INOP. REMOVED AND REPLACED NR 6 EMERGENCY LIGHT DC/AC INVERTER IAW AMM 33-50-11. OPC GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 36,267 hrs · 31,353 cycles

LT OVERWING EXTERIOR EMERGENCY LIGHT INOP. C/A-REMOVED AND REPLACED LT OVERWING EXTERIOR EMERGENCY LIGHTIAW AMM 33-50-10 OPC GOOD.

Part: INVERTER — FAILED (CABIN) · airframe 36,192 hrs · 31,278 cycles

DURING PS-1 CHK FOUND AFT EMER EXIT LOCATING SIGN FWD SIDE INOP.-C/A-REMOVED AND REPLACED AFT EMER EXIT LOCATING SIGN FWD SIDE IAW AMM 33-50-15 AND EMER LIGHT DC/AC INVERTER IAW AMM 33-50-11. OPS CHK GOOD. SIGN ASSY EXIT P/N 8232-1

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 36,175 hrs · 31,261 cycles

AFT LH EXTERIOR EMERGENCY LIGHT INOP-C/A-REMOVED AND REPLACED AFT LH EXTERIOR EMERGENCY LIGHT IAW EMB 145 AMM 33-50-10. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED

Part: LIGHT — INOPERATIVE (OVERWING EXIT) · airframe 36,151 hrs · 31,236 cycles

FOUND LH OVERWING EMG LIGHT INOP DURING PS-1-C/A-REPLACE LAMP IAW AMM 33-50-10 OPS CHECK GOOD

Part: LIGHT — INOPERATIVE (RT OVERWING) · airframe 36,132 hrs · 31,209 cycles

RH OVERWING EMERGENCY LIGHT LAMP INOP-C/A-REMOVED AND REPLACED RH OVERWING EMERGENCY LIGHT LAMP IAW EMB 145 AMM 33-50-10. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 36,050 hrs · 31,122 cycles

DURING PS-1 CHECK FOUND EXTERNAL LH EMERGENCY LIGHT INOP-C/A-REMOVED AND REPLACED EXTERNAL LH EMERGENCY LIGHT LAMP IAW EMB 145 AMM 33-50-10

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 35,952 hrs · 31,024 cycles

DURING PS-1 FOUND EXTERIOR EMERGENCY LIGHT OVER LH WING INOP-C/A-REMOVED AND REPLACED LIGHT BULB IAW 145 AMM 33-50-10 OPS-CHECK GOOD NO FUTHER DEFECTS NOTED AT THIS TIME

Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,917 hrs · 30,986 cycles

CENTER ISLE EXIT LIGHT INOP-C/A-REPLACED CENTER ISLE EXIT LIGHT IAW AMM 33-50-15-04 OPS CHECK GOOD

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 35,842 hrs · 30,913 cycles

LH OVERWING EMERGENCY LIGHT INOP-C/A-REMOVED AND REPLACED LH OVERWING EMERGENCY LIGHT LAMP IAW EMB AMM 33-50-10-000-801-A AND 33-50-10-400-801-A. OPS CHECK GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 35,656 hrs · 30,721 cycles

LH AFT OVERWING EMERGENCY LIGHT INOP-C/A-REMOVED AND REPLACED LH AFT OVERWING EMERGENCY LIGHT LAMP IAW EMB 145 AMM 33-50-10. OPS CHECK GOOD.

Part: FIRE DETECTOR — FAILED (NR 1 ENGINE) · airframe 35,501 hrs · 30,562 cycles

NR 1 ENGINE FIRE LOOP FAILED MESSAGE DURING CLIMB. PERFORMED OP CHECK OF E1 FIRELOOP DETECTOR IAW EMB 145 AMM 26-10-00. FOUND WOP E1 FIRE DETECTOR-REMOVED AND REPLACED E1 ENGINE FIRE DETECTOR IAW AMM 26-11-01, OPS CHECKED GOOD

Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,142 hrs · 30,227 cycles

SERVICE DOOR EMERGENCY FLOOD LIGHT INOPERATIVE. REMOVED AND REPLACED SERVICE DOOR EMERGENCY FLOOD LIGHT ASSY IAW EMB 145 AMM 33-50-10

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 34,869 hrs · 30,007 cycles

DURING PS-2 CHECK, FOUND THE CEILING EMERGENCY EXIT SIGN NEAR OVERWING EMERGENCY ROW INOPERATIVE. REMOVED AND REPLACED THE NR 4 EMERGENCY BATTERY IAW AMM 33-50-04. OPS CHECKED GOOD.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 34,869 hrs · 30,007 cycles

DURING PS-2 CHECK, FOUND EMERGENCY EXIT LIGHT NEAR PAX DOOR ABOVE FA HEADREST INOPERATIVE. REMOVED AND REPLACED THE NR 1 INVERTER IAW AMM 33-50-11. OPS CHECKED GOOD. NO OTHER DEFECTS NOTED.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 34,551 hrs · 29,697 cycles

DURING PS-2 CHECK, FOUND EXTERNAL EMERGENCY LIGHT ON THE LEFT HAND SIDE CENTER FAIRING WILL NOT ILLUMINATE. C/A-FOUND LAMP TP BE BURNT OUT. REMOVED AND REPLACED LAMP IAW AMM 33-50-10. OPS CHECK GOOD.

Part: PIPE — DEFECTIVE (AC BAY) · airframe 34,274 hrs · 29,400 cycles

RECE'VED PACK 1 VLV CLOSED AND BLEED 1 CLOSED ON TAKE OFF. RECYCLED 4 TIMES + FOLLOWED QRH AND COULD NOT GET THE PACK TO STAY ON. C/A-DEFERRED PER MEL 21-28. AUTH # 050962D-C. MEL HAS TO BE CHANGE FROM 21-28 TO 21-30, DUE TO WRONG MEL ISSUE ON "N" REG. ITEM DEFERRED PER MEL # 21-30 AUTH # 050962D-C AS PER MOC # 680993. REMOVED AND REPLACED PIPE, COUPLINGS, AND CLAPS FROM DUAL TEMPERATURE CONTROL VALVE TO HEAT EXCHANGER IAW AMM 21-51-02, OPS CHK GOOD, LEAK CHK GOOD. MEL RESTORED.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 34,147 hrs · 29,286 cycles

DURING PS-1 CHECK FOUND EXTERNAL OVERWING EMERGENCY LIGHT NOT WORKING ON LEFT HAND SIDE. C/A-REMOVED AND REPLACED EMERGENCY LIGHT LAMP IAW AMM 33-50-10. OPS CHECK GOOD.

Part: WINDSHIELD — LEAKING (COCKPIT) · airframe 33,960 hrs · 29,123 cycles

DURING TAKEOFF AFTER ROTATING FELT WATER DRIP ON HIS HAND. AFTER LOOKING UP THE SOURCE OF THE LEAK WAS THE MAGNETIC COMPASS. WHERE THE COMPASS CONNECTS TO THE WINDSHIELD FRAME. PERFORMED RETORQUE OF CAPT AND FO WINDSHIELD IAW AMM 56-10-01 OPS CHECK GOOD

Part: NOT REPORTED — DAMAGED (FUSELAGE) · airframe 33,589 hrs · 28,761 cycles

COMPLETED MEASURING OF BLENDED SPOT NR 1 BETWEEN FRAMES 57AND 58 JUST OUTBD OF STGR 01R. AND FOUND TO BE OUT OF LIMITS IAW SRM 53-24-01. REPAIRED IAW ERS-EM-53MR-3634.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 33,589 hrs · 28,761 cycles

DURING REMOVAL OF SHEAR CLIP AT FRAME 73 (REFER TO NON-ROUTINE E687963) FOUND ANGLE THAT ATTACHES LT PYLON RIB 5 TO FUSELAGE TO BE CRACKED. C/A-REPLACED ANGLE IAW SRM 51-40-02.

Part: BUSHING — MISSING (RT AILERON) · airframe 33,589 hrs · 28,761 cycles

RT AILERON DAMPER FITTING IS MISSING A HAT BUSHING. REPAIRED IAW EO EM-27MR-112.

Part: SUPPORT BRACKET — CRACKED (RT WING) · airframe 33,589 hrs · 28,761 cycles

RIGHT WING TO FUSELAGE PANEL SUPPORT BRACKET IS CRACKED ON UPPER WING SURFACE. C/A-REPLACED RT WING-TO-FUSELAGE ANGLE (SECOND SECTION BACK) IAW ETN-EM-53-142 AND SRM 51-40-02.

Part: CLEAT — CRACKED (FUSELAGE) · airframe 33,589 hrs · 28,761 cycles

RT SHEAR CLEAT AT FRAME 80RT., BETWEEN STRS. 6-7 HAS A CRACK APPROX. 1/2". C/A-REMOVED AND REPLACED RT SHEAR CLEAT AT FRAME 80 BETWEEN STRINGERS 6-7 IAW SRM 51-40-02.

Part: FITTING — CRACKED (FUSELAGE) · airframe 33,589 hrs · 28,761 cycles

CARGO SHEAR CLEAT AT FRAME 73LT., BETWEEN STRS. 8-9 HAS A CRACK APPROX. 1/4". C/A-INSTALLED NEW SHEAR CLIP AT FRAME 73 LT BETWEEN SRTINGERS 8-9 IAW SRM 51-40-02.

Part: FITTING — CRACKED (FUSELAGE) · airframe 33,589 hrs · 28,761 cycles

CARGO SHEAR CLEAT AT FRAME 73RT., BETWEEN STRS. 8-9 HAS A CRACK APPROX. 3/4". C/A-REPLACED SHEAR CLIP IAW SRM 51-40-02.

Part: CLEAT — CRACKED (FUSELAGE) · airframe 33,589 hrs · 28,761 cycles

CARGO SHEAR CLEAT AT FRAME 68LT. BETWEEN STRS. 6-7 HAS A CRACK APPROX. 1". C/A-REMOVED AND REPLACED CARGO SHEAR CLEAT AT FRAME 68LT., BETWEEN STRS. 6-7 IAW SRM 51-40-02.

Part: CLEAT — CRACKED (FUSELAGE) · airframe 33,589 hrs · 28,761 cycles

LT SHEAR CLEAT AT FRAME 80LT., BETWEEN STRS. 6-7 HAS A CRACK APPROX. 1/2". C/A-REMOVED AND REPLACED LH SHEAR CLEAT AT FRAME 80 BETWEEN STRINGERS 6-7 IAW SRM 51-40-02.

Part: SUPPORT BRACKET — CRACKED (CARGO DOOR) · airframe 33,589 hrs · 28,761 cycles

CARGO DOOR TORSION BAR FWD SUPPORT BRACKET AT FRAME 61 HAS A CRACK APPROX. 1/4". C/A-REMOVED AND REPLACED CARGO DOOR TORSION BAR FWD SUPPORT BRACKET IAW SRM 51-40-02.

Part: CONNECTOR — CRACKED (CABIN) · airframe 33,589 hrs · 28,761 cycles

FLOOR EMERGENCY PROXIMITY LIGHT #8 WIRE HAS CRACKED CONNECTOR (A/C SIDE). C/A-COMPLETE:REPAIRED EMERGENCY FLOOR PROXIMITY LIGHT #8 WIRE CONNECTOR IAW SWPM 20-00-03. REF NRWC E687625 FOR OPTS TEST.

Part: WIRE — BROKEN (CABIN) · airframe 33,589 hrs · 28,761 cycles

EMERGENCY FLOOR PROXIMITY LIGHT #6 HAS BROKEN WIRE (A/C SIDE). C/A-COMPLETE:REPAIRED EMERGENCY FLOOR PROXIMITY LIGHT #6 WIRE IAW SWPM 20-00-03. REF NRWC E687625 FOR OPTS TEST.

Part: CONNECTOR — BROKEN (CABIN) · airframe 33,589 hrs · 28,761 cycles

2ND FROM FWD FLOOR EMERGENCY LIGHT STRIP HAS BROKEN CONNECTOR AT AIRCRAFT FLOOR. C/A-COMPLETE:REPLACED CONNECTOR SHELL IAW SWPM 20-50-01. REF NRTC# E687625 FOR OPS CHECK.

Part: INVERTER — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 32,704 hrs · 27,889 cycles

EMERGENCY EXIT SIGN AT SEAT 3B INOPERATIVE. TROUBLESHOT THE EMERGENCY EXIT SIGN IAW WIRING MANUAL 33-50-50-005. FOUND THE NR 3 INVERTER TO BE AT FAULT. REMOVED AND REPLACED THE INVERTER IAW AMM 33-50-11-000-801-A, AND 33-50-11-400-801-A, OPS CHECKED GOOD.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 32,319 hrs · 27,579 cycles

RT OVERWING EXIT IDENTIFIER INOP. REMOVED AND REPLACED NR 5 INVERTER ASSY, OPERATIONAL CHECK GOOD.

Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE) · airframe 31,845 hrs · 27,111 cycles

RETURN TO FIELD, UNABLE TO CONTROL CABIN PRESSURIZATION IN FLIGHT. NO MASKS DROPPED. RECEIVED A NR 1 PACK OVLD CAUTION AFTER LANDING. REMOVED AND REPLACED THE PRESSURIZATION DIGITAL CONTROLLER IAW AMM 21-31-01, FUNCTIONAL TESTED GOOD IAW AMM 21-31-00.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 31,791 hrs · 27,046 cycles

DURING PS-1 CHECK, FOUND MAIN DOOR EMERGENCY EXIT SIGN LIGHT INOPERATIVE. REMOVED AND REPLACED MAIN DOOR EMERGENCY EXIT SIGN LIGHT IAW CMM 25-28-24. OPS CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 31,745 hrs · 26,995 cycles

FWD CABIN FLASHLIGHT INOP. -C/A-REMOVED AND REPLACED FWD CABIN FLASHLIGHT IAW AMM 33-50-16-000-801-A AND 33-50-16-400-801-A OPC GOOD END.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 31,689 hrs · 26,952 cycles

EMERGENCY EXIT SIGN BY SEAT 3BC FWD BULKHEAD INOPERATIVE. REMOVED AND REPLACED THE SIGN IAW AMM 33-50-13. OPS CHECKED GOOD.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 30,407 hrs · 25,772 cycles

FUMES IN COCKPIT AT 12,000 SEEMED TO COME FROM THE NR 1 PACK. PERFORMED ODOR/FUMES IN COCKPIT INSPECTION IAW ETN-EM-72-034. NO DEFECTS NOTED.

Part: ACM — FAILED (AC BAY) · airframe 30,407 hrs · 25,772 cycles

ON AFTER START CHECKLIST, TURNING ON PACK 1, STRONG ODOR PRESENT. REMOVED & REPLACED AIR CYCLE MACHINE IAW AMM 21-51-03. OPS CHECK GOOD.

Part: WIRE — CHAFED (COCKPIT) · airframe 28,700 hrs · 24,332 cycles

ELECTRICAL SMOKE IN COCKPIT DURING THE DESCENT. IT APPEARED TO FOG OUT ON THE LEFT SIDE JUST BELOW THE GLARESHIELD. FOUND CHAFED WIRES ON CONNECTOR J1268 BEHIND CA WX CONTROLLER, REPAIRED WIRES ON CONNECTOR J1268 IAW SWPM 20-21-00 AND SWPM 20-13-01. OPC GOOD IAW AMM 31-51-00 AND AMM 31-41-00 WM 31-52-50.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 28,664 hrs · 24,299 cycles

LT OMEGA BEAM IS CRACKED AT NUTPLATE HOLE ABOVE FRAME 29. REPAIRED LT OMEGA BEAM AT FR 29 IAW ERS-EM-53MR-2358.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 28,664 hrs · 24,299 cycles

PROTRUSION ON EXTERNAL SKIN BETWEEN FR 20 - 21 STR 17L - 18L. REPAIRED PROTRUSION ON EXTERNAL SKIN BETWEEN FR 20 - 21 STR 17L - 18L IAW SRM 53-21-01 FIG 206.

Part: SKIN — CRACKED (FUSELAGE) · airframe 28,664 hrs · 24,299 cycles

RT REAR FUSELAGE SKIN CRACK AT FRAME 75, ABOVE STRINGER 2R. PERFORMED PERMANENT REPAIR RT REAR FUSELAGE SKIN CRACK AT FRAME 75, ABOVE STRINGER 2R IAW SRM 53-31-01 ITEM 11.

Part: WEB — CHAFED (CARGO DOOR) · airframe 28,668 hrs · 24,302 cycles

BAGGAGE DOOR INNER LOWER WEB HAS MULTIPLE CHAFES. PERFORMED CUTOUT AND FABRICATED AND INSTALLED DOUBLER IAW TN-EM-52-043 AND SRM 51-40-02.

Part: FITTING — CORRODED (FUSELAGE) · airframe 28,664 hrs · 24,299 cycles

CORROSION ON BAGGAGE DOOR CUTOUT AT FR 68 AFT LOWER STRUCTURE. REPAIRED CORROSION ON BAGGAGE DOOR CUTOUT AT FR 68 AFT LOWER STRUCTURE IAW SRM 53-31-04 ITEM 4F.

Part: FITTING — CHAFED (FUSELAGE) · airframe 28,664 hrs · 24,299 cycles

INTERNAL BAGGAGE DOOR CUTOUT LOWER FWD LATERAL L SHAPE CHAFED. REPAIRED BAGGAGE DOOR CUTOUT FWD LATERAL L SHAPE IAW ERS-EM-53MR-2338.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 28,664 hrs · 24,299 cycles

CARGO DOOR ENTRANCE SILL CORRODED. REMOVED AND REPLACED CARGO DOOR SILL IAW SRM 51-40-02.

Part: FRAME — CRACKED (FUSELAGE) · airframe 28,664 hrs · 24,299 cycles

FRAME 81 CRACKED IN RADIUS BETWEEN STRINGER 1L AND 2L. PERFORMED REPAIR OF FRAME 81 CRACKED IN RADIUS BETWEEN STRINGER 1L AND 2L IAW ERS-EM-53MR-2344.

Part: DISPLAY — FAILED (COCKPIT) · airframe 28,044 hrs · 23,736 cycles

MFD WENT DARK AND WE SMELLED ELECTRICAL FUMES. IT COINSIDED WITH MFD GOING OUT. R & R CAPTAIN SIDE MFD DUE TO BURNED MFD. R & R IAW AMM 34-22-00 AND 34-22-01. OPS CHECK GOOD.

Part: INVERTER — MALFUNCTIONED (ELECTRICAL SYS) · airframe 27,950 hrs · 23,647 cycles

ON TAKEOFF LOW SPEED ABORT, EICAS MSG 115, VAC BUS OFF DAU 1A FAIL, DFDR FAIL. ACFT STATIC INVERTER IAW AMM 24-20-01, OPS GOOD.

Part: CONTROL UNIT — FAULTY (BRAKE SYSTEM) · airframe 27,769 hrs · 23,466 cycles

WHEN TAXING OUT NOTICED RT BRAKE WAS NOT WORKING, THEN GOT BRAKE DEGRADED MSG. REPLACED BRAKE CONTROL UNIT IAW 32-41-02 AMM. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,126 hrs · 22,876 cycles

RIGHT FWD OVERWING EMER LIGHT INOPERATIVE. REPLACED THE BULB IN THE RT FWD OVERWING EMER LIGHT IAW AMM 33-50-10. OPERATIONS CHECKED GOOD.

Part: DOOR — DENTED (CABIN) · airframe 26,625 hrs · 22,414 cycles

LOG PAGE 3952767 ITEM 1 TDMI 935T5229, MAIN PAX DOOR HAS A DENT & GOUGE AT LOWER RT CORNER REPAIR IAW ERS-EM-52DF-456. COMPLIED WITH PERMANENT REPAIR IAW ERS-EM-52DF-456 PART C. TDMI RESTORED.

Part: BATTERY — DISCHARGED (CABIN) · airframe 26,160 hrs · 21,954 cycles

NUMBER 4 EMER LIGHT BATTERY DEAD. R & R NR 4 EMER LIGHT BATTERY IAW MM 33-50-04. OPERATIONS CHECKED GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 26,160 hrs · 21,954 cycles

NUMBER 1 EMER LIGHT BATTERY DEAD. R & R NR 1 EMER LIGHT BATTERY IAW MM 33-50-04. OPERATIONS CHECKED GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 26,160 hrs · 21,954 cycles

NUMBER 2 EMER LIGHT BATTERY DEAD. R & R NR 2 EMER LIGHT BATTERY IAW AMM 33-50-04. OPERATIONS CHECKED GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 26,160 hrs · 21,954 cycles

NUMBER 3 EMER LIGHT BATTERY DEAD. R & R NR 3 EMER LIGHT BATTERY IAW AMM 33-50-04. OPERATIONS CHECKED GOOD.

Part: CRADLE — FAILED (FLASHLIGHT) · airframe 26,065 hrs · 21,860 cycles

AT 26000 FT, NOTICED AN ELECTRICAL ODOR IN THE COCKPIT, THE ODOR INTENSIFIED. THE FLIGHT ATTENDANT COMMENTED THAT THE CABIN HAD A STRONG ELECTRICAL BURNING ODOR. DECLARED AN EMERGENCY, RAN EMERGENCY MEMORY ITEMS, A FUNCTIONAL CHECKLISTS FOR FIRE SMOKE FUMES IN COCKPIT. RAN ACFT SYSTEMS FOUND PILOTS FLASHLIGHT ASSEMBLY & AFT FLIGHT ATTENDANTS FLASHLIGHT ASSEMBLY TO BE THE CAUSE OF ODOR IAW AMM 05-20-00. R & R AFT CABIN FLASHLIGHT ASSEMBLY IAW AMM 33-50-16. OPS CHECKED & FOUND WORKING NORMAL. NO BURNED ODOR FOUND AT THIS TIME. R & R CAPTAIN`S FLASHLIGHT ASSEMBLY IAW AMM-33-50-16. OPS CHECKED & FOUND WORKING NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,466 hrs · 21,324 cycles

FORWARD AISLE EMER LIGHT FAILS TO ILLUMINATE. R & R FWD AISLE EMER LIGHT BULB IAW AMM 33-50-08. OPERATIONAL CHECKED GOOD.

Part: LIGHT — INOPERATIVE (FLASHLIGHT) · airframe 25,078 hrs · 20,992 cycles

AFT FLASHLIGHT IS INOPERATIVE. R & R AFT FLASHLIGHT BULB IAW SMP. OPERATIONS CHECKED GOOD.

Part: STEERING SYS — INOPERATIVE (NLG) · airframe 24,813 hrs · 20,761 cycles

STEER INOPERATIVE WHEN TILLER TURNED TO FULL LEFT. R & R FEEDBACK POTENTIOMETER. OPERATIONS CHECK FAILED. NO FIX IAW AMM 32-50-07. REF LOG PAGE 3703888 ITEM 2.

Part: LIGHT — INOPERATIVE (SERVICE DOOR) · airframe 24,197 hrs · 20,229 cycles

SERVICE DOOR EXIT LIGHT INOPERATIVE. R & R SERVICE DOOR EMER LIGHT IAW AMM 33-50-09. OPERATIONS CHECKED GOOD.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 23,983 hrs · 20,036 cycles

LEFT WALL SEAT TRACK SUPPORT FLANGE IS CORRODED AT RIVETS NEAR FRAME 45 & 46. R & R LT WALL SEAT TRACK SUPPORT IAW SRM 51-40-02.

Part: SUPPORT BRACKET — CRACKED (CARGO DOOR) · airframe 23,983 hrs · 20,036 cycles

RIGHT SUPPORT BRACKET FOR THE CARGO DOOR HANDLE CUP IS CRACKED, BOTH UPPER & LOWER ATTACHMENT POINTS ON FRAME 68. R & R IAW SRM 51-40-02.

Part: TORQUE BOX — CRACKED (PAX DOOR) · airframe 23,983 hrs · 20,036 cycles

PASSENGER DOOR INTERIOR HANDLE TORQUE BOX HAS A 3/8 INCH CRACK ON THE AFT UPPER CORNER. REPAIRED CRACK IAW EO-EM-52MR-250.

Part: SKIN — CRACKED (E&E BAY) · airframe 23,983 hrs · 20,036 cycles

REAR ELECTRONICS COMPARTMENT DOOR INNER STRUCTURE CRACKED. COMPLIED WITH ERS-EM-52MR-211 FOR REPAIR OF DAMAGED AREA.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 23,983 hrs · 20,036 cycles

RIGHT OMEGA BEAM SUPPORT FLANGE IS CRACKED AT FRAME 47. R & R IAW SRM 53-23-02.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,767 hrs · 19,831 cycles

EMERGENCY FLOOR LIGHT STRIP AT ROW 5 & 6 INOPERATIVE. R & R EMER FLOOR LIGHT STRIP IAW AMM 33-50-12.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 23,646 hrs · 19,716 cycles

MASTER CAUTION AFTER ABORTED TAKEOFF, E1-2 EXCEEDANCE, WITH THE THRUST LEVERS IN THE DETENT BOTH ETTS WENT TO ABOVE 920 DURING THE ABORTED TAKEOFF. WE WERE DOING AN ALT TO 1 TAKEOFF WITH TEMP SET TO 25, MAX ACFT SPEED WAS 80 KTS LOW SPEED ABORT. PERFORMED A THRUST ASSURANCE CHECK ON BOTH ENGS, NO EXCEEDANCES NOTED. NO FURTHER ACTION REQUIRED IAW RR MM 71-00-00-200-801. ACFT OK FOR SERVICE.

Part: ACM — DAMAGED (AC BAY) · airframe 23,032 hrs · 19,183 cycles

WHILE CRUISING AT FL250, WE ENCOUNTERED INSTANTANEOUS SMOKE IN THE COCKPIT & CABIN. VISUAL INSPECTION FOUND LT ACM DAMAGE. R & R LT ACM IAW AMM 21-51-03. OPERATIONAL CHECK FOUND OK. NO SMOKE IN THE COCKPIT OR CABIN AT THIS TIME.

Part: CONTROL PANEL — DEFECTIVE (GALLEY) · airframe 22,970 hrs · 19,137 cycles

DURING DESCENT & APPROACH TO MIA, FLIGHT ATTENDANT REPORTS FAINT SMOKE SMELL IN GALLEY. AOM1 PROCEDURES COMPLIED WITH. INSPECTED GALLEY & FOUND ELEC CONTROL PANEL TO THE GALLEY, THE BOARD WITH BURN SMELL. R & R GALLEY ELEC CONTROL PANEL, OPERATIONS CHECKED GOOD IAW CMM 25-32-94 & ALSO FOUND THE LT HOT CONTAINER POPPING BREAKER. REMOVED CONTAINER & DUE TO LACK OF TIME MEL THE LT HAND HOT CONTAINER HEATING SYS IAW MEL 25-50.

Part: HOLDER — BROKEN (FLASHLIGHT) · airframe 22,032 hrs · 18,438 cycles

DURING MAINTENANCE INSPECTION FOUND REAR FLIGHT ATTENDANT`S FLASHLIGHT HOLDER IS BROKEN. THE ACFT WAS REMOVED FROM SERVICE. REMOVE AND REPLACED THE REAR FLIGHT ATTENDANT FLASHLIGHT HOLDER IAW EMB AMM 33-50-16. OPC GOOD. MEL ITEM RESTORED. THE AIRCRAFT RETURN TO SRVICE

Part: DISPLAY — ODOR (COCKPIT) · airframe 21,012 hrs · 17,588 cycles

CAPTAIN'S MFD WENT DARK AND STRONG ELECTRICAL ODOR. R & R CAPT'S MFD IAW MM 34-22-01. OPS CHECKED GOOD. NO ELECTRICAL ODOR.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 20,920 hrs · 17,510 cycles

REAR HALF OF EMERGENCY LIGHTS CAME ON WHEN ACFT IS COMPLETELY UNPOWERED. PERFORMED OPS CHECK OF EMERGENCY LIGHTING SYSTEM IAW 33-700-17. OPS CHECKED GOOD. NO DEFECTS FOUND.

Part: ACM — FAILED (NR 1)

CREW REPORTED AN ACRID BURNING SMOKE ODOR IN CABIN AND COCKPIT DURING CLIMBOUT. DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE, LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REMOVED RELAY K0528 AND INSTALLED JUMPER RELAY, FOR FURTHER TROUBLESHOOTING TO ISOLATE ODOR ORIGIN. HEAVY ODOR WAS PRESENT WHEN OPERATING NR 1 PACK WITH NR 1 & 2 ENGINES. SUSPECT NR 1 ACM TO BE AT FAULT. R & R NR 1 ACM IAW MM 21-51-03. OPS AND LEAK CHECKED GOOD IAW MM 21-51-00. ACFT RETURNED TO SERVICE.

Part: SEAL — MISSING (WINDOW) · airframe 20,896 hrs · 17,491 cycles

CREW REPORTED THEY HEARD A LOUD SQUEALING IN FLIGHT. CREW DETECTED BURNING RUBBER BEFORE LANDING. DURING POST FLIGHT INSPECTION, FOUND THE HUMP SEAL ON THE CAPTAIN’S SIDE MISSING. ACFT REMOVED FROM SERVICE. INSPECTED INTAKE AND SURROUNDING AREAS, NO DEFECTS NOTED. RAN ENGINES AND PACKS, NO ODOR NOTED. OK FOR SERVICE. ACFT RETURNED TO SERVICE.

Part: ECU — FAULTY (TE FLAP) · airframe 19,919 hrs · 16,687 cycles

ON FLIGHT 2750 THE CREW REPORTED THAT CLIMBING TO FLIGHT LEVEL 250 THEY RECEIVED A FLAP LOW SPEED MESSAGE ON EICAS. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED FLAP ELECTRONIC CONTROL UNIT PER 27-53-02. THE OPERATIONAL CHECK WAS GOOD PER 27-50-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,467 hrs · 16,320 cycles

DURING MAINTENANCE INSPECTION FOUND THE RIGHT OUTBOARD SEAT TRACK SUPPORT CORRDED AT FRAME 50. THE AIRCRAFT WAS REMOVED FROM SERVICE. ACCOMPLISHED REPAIR ACCORDING TO THE EO EM-53-MR-2059. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · airframe 19,546 hrs · 16,386 cycles

DURING B INSPECTION FOUND THE CARGO DOOR SILL CORRODED AT THE FORWARD END. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED SERVICEABLE CARGO DOOR SILL IAW EMB SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SUPPORT — CORRODED (SEAT TRACK) · airframe 19,467 hrs · 16,320 cycles

RT OTBD SEAT TRACK SUPPORT CORRODED AT FR-50. SUPPORT REPAIRED IAW AEA EO EM-53MR-2059.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 19,467 hrs · 16,320 cycles

SERVICE DOOR CUT-OUT CORRODED AT AFT LOWER TRIM FASTENER HOLE. REPAIRED SERVICE DOOR CUT-OUT CORROSION AT AFT LOWER TRIM FASTENER HOLE IAW EO EM-53MR-2058.

Part: SEAL — WORN (PAX DOOR) · airframe 19,546 hrs · 16,386 cycles

DURING MAINTENANCE INSPECTION FOUND THE PASSENGER DOOR SEAL WORN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE PASSENGER DOOR SEAL IAW EMB 145 AMM 52-18-04. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SCREW — UNSECURE (CABIN) · airframe 19,546 hrs · 16,386 cycles

DURING B INSPECTION FOUND THE RIGHT OVERWING EMERGENCY EXIT CATCHING ON PANEL WHEN OPENING. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND TO BE LEFT OVERWING EMERGENCY EXIT. SECURED LEFT OVERWING EMERGENCY EXIT SIDEWALL LINER UPPER SCREWS IAW EMB 145 AMM 20-10-01. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INTERMITTENT (CABIN) · airframe 19,044 hrs · 16,000 cycles

DURING B INSPECTION FOUND THE MAIN CABIN DOOR EMERGENCY LIGHT INTERMITTENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE MAIN CABIN DOOR EMERGENCY LIGHT ASSEMBLY IAW EMB 145 AMM TASKS 33-50-06-000-802-A & 33-50-06-400-802-A . THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: HOLDER — BROKEN (COCKPIT) · airframe 18,670 hrs · 15,726 cycles

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

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 18,569 hrs · 15,651 cycles

DURING MAINTENANCE INSPECTION, FOUND THE BOTTOM LIGHT ON THE PASSENGER DOOR INOPERATIVE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED LAMP IAW AMM 33-26-03. OPS CHECKED GOOD. NO OTHER DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: LENS — UNSERVICEABLE (EMERGENCY LIGHT) · airframe 18,569 hrs · 15,651 cycles

DURING MAINTENANCE INSPECTION, FOUND THE MAIN DOOR EMERGENCY LIGHT LENSE BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE MAIN DOOR EMERGENCY LIGHT LENSE IAW EMB AMM 33-26-03. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONTROLLER — INOPERATIVE (CABIN PRESSURE) · airframe 18,508 hrs · 15,595 cycles

DURING FLIGHT 3407, CREW REPORTED LOSS OF PRESSURIZATION AND DECLARED EMERGENCY AND LANDED AT DESTINATION WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE DIGITAL CONTROLLER. MANUAL AND AUTO OPC GOOD RAR ELECTRO PNEUMATIC OUTFLOW VALVE OPC GOOD AMM 21-31-00-103 THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 18,339 hrs · 15,460 cycles

DURING B INSPECTION, FOUND THE EMERGENCY LAMP ON MAIN DOOR HINGE INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE MAIN DOOR HINGE EMERGENCY LAMP IAW AMM TASK 33-50-10-000-801/33-50-10-400-801. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CONNECTOR — BROKEN (FLASHLIGHT) · airframe 18,339 hrs · 15,460 cycles

DURING B INSPECTION, FOUND THE FIRST OFFICER’S FLASHLIGHT BATTERY CONNECTOR CLIP BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FIRST OFFICER’S FLASHLIGHT WHILE PERFORMING WORK CARD 33-700-00. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: BEZEL — FAILED (COCKPIT) · airframe 18,181 hrs · 15,323 cycles

ON FLIGHT 3941 THE CREW REPORTED THAT WHILE DESCENDING THROUGH FL185, WHEN SETTING NEW ALTIMETER SETTING WITH ALTIMETER BEZEL, BOTH PRIMARY ALTIMETERS FAILED W/RED X'S AND ASEL DASHED OUT. CAME BACK TEMPORARILY WHEN STD BUTTON WAS PRESSED. NO EICAS MSGS PRESENT. ALL OTHER ADC INFO PRESENT. THE CAPTAIN DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPLACED CAPT'S PFD BEZEL. THE OPERATIONAL CHECKS WERE GOOD IAW EMB 145 AMM 342202. ADC 1 AND 2 OPERATIONAL CHECKS GOOD IAW EMB 145 AMM 34-15-00. AIRCRAFT IS RVSM ELIGIBLE. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: DOOR — MALFUNCTIONED (MLG) · airframe 17,982 hrs · 15,149 cycles

FLIGHT 4069, AFTER TAKEOFF, RECEIVED EICAS LG AIR/GND FAIL, E2 REV FAIL, E1-2 REV FAIL MESSAGE. COMPLIED WITH AOM CHECKLIST AND DECLARED AN EMERGENCY AND CFR WERE CALLED. LANDING SMOOTH, ON CENTERLINE AND NOT OVERWEIGHT. AS ACFT SLOWED DOWN, IT BECAME UNRESPONSIVE AND SWERVED RIGHT. BRAKES WERE NOT WORKING. ACFT DRIFTED ONTO A GRASSY AREA AND CAPTAIN HAD TO PULL EMERGENCY PARK BRAKE TO STOP. CREW SMELLED SMOKE, BUT CFR DID NOT DETECT FIRE. ACFT REMOVED FROM SERVICE. REMOVED AND REPLACED LT HAND MLG MAIN DOOR ASSEMBLY IAW AMM 32-10-06. REMOVED AND REPLACED LT MLG AUXILIARY DOOR IAW AMM 32-10-07. COMPLIED WITH EXTENSION CHECK OF LT LANDING GEAR IAW AMM 32-30-00. AIRCRAFT RETUTNED TO SERVICE.

Part: PROXIMITY SENSOR — INOPERATIVE (NLG) · airframe 17,981 hrs · 15,148 cycles

FLIGHT 3927, AFTER TAKEOFF, LANDING GEAR AIR/GND FAIL EICAS MESSAGE APPEARED WHEN LANDING GEAR RETRACTED. AFTER LANDING GEAR RETRACTED E1-2 REV DISAGREE EICAS MESSAGE APPEARED. DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE. DURING APPROACH WHEN GEAR SELECTED DOWN, E 1-2 REV DISAGREE DISAPPEARED AND GEAR INDICATIONS SHOWED DOWN AT THE SAME TIME ALONG WITH THE CONTINUING "LG AIR/GND FAIL" BEING DISPLAYED. DID A "LOW PASS" OVER FIELD AND THE TOWER SAID THE GEAR APPEARED NORMAL. ON SECOND APPROACH THE INITIAL TOUCHDOWN OF THE MAINS WERE NORMAL THEN WHEN NOSEWHEEL TOUCHED AIRCRAFT SWERVED RIGHT. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED NLG WEIGHT ON WHEELS PROXIMITY SWITCH IAW AMM 32-63-02. OPS CHECKED GOOD AND THRUST REVERSERS OPS CHECKED GOOD IAW AMM 78-31-01. AIRCRAFT RETURNED TO SERVICE.

Part: ELECTRONIC UNIT — INOPERATIVE (MLG) · airframe 17,982 hrs · 15,149 cycles

FLIGHT 4340, AFTER TAKEOFF SELECTED THE LANDING GEAR LEVER UP AND RECEIVED EICAS LANDING GEAR AIR/GND FAIL MESSAGE FOLLOWED BY EICAS E 1-2 REV FAIL MESSAGE. COMPLETED CHECKLIST AND DECIDED TO RETURN TO DEPARTURE. DECLARED AN EMERGENCY AND THE LANDING GEAR CYCLED NORMALLY. LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE LANDING GEAR ELECTRONIC UNIT IAW AMM 32-32-01. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 17,936 hrs · 15,113 cycles

DURING B INSPECTION, FOUND THE MAIN DOOR MOUNTED EMERGENCY LIGHT INTERMITTENT. AIRCRAFT REMOVED FROM SERVICE. TROUBLESHOT MAIN DOOR EMERGENCY LIGHT ASSEMBLY AND WIRING AND FOUND LAMP FILAMENT TO HAVE BEEN BROKEN BUT STILL MOMENTARILY MAKING CONTACT. REMOVED AND REPLACED LAMP IAW AMM 33-50-10-000-801-A AND 33-50-10-400-801-A. THE OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 17,709 hrs · 14,920 cycles

DURING B-INSPECTION FOUND THE MAIN DOOR EMERGENCY EXTERNAL LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE MAIN DOOR EMERGENCY EXTERNAL LIGHT LAMP IAW EMB AMM 33-50-10-000-801-A AND 33-50-10-400-801-A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: DOOR — LACK OF LUBE (CABIN) · airframe 17,295 hrs · 14,603 cycles

FOR FLIGHT 3464 FOUND MAIN CABIN DOOR DIFFICULT TO CLOSE AND OPEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. LUBE AND CLEANED MAIN CABIN DOOR IAW EMB AMM 52-18-00 OPERATIONAL WAS CHECK GOOD. THE AIRCRAFT RETURN TO SERVICE.

Part: BULB — BURNED OUT (FLASHLIGHT) · airframe 17,235 hrs · 14,551 cycles

ON FLIGHT 4129 THE CREW REPORTED THE FLIGHT ATTENDANT FLASHLIGHT BULB BURNED OUT FORWARD IN CABIN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FORWARD FLIGHT ATTENDANT FLASHLIGHT PER STANDARD MAINTENANCE PROCEDURES. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: HOLDER — BROKEN (FLASHLIGHT) · airframe 17,115 hrs · 14,457 cycles

ON FLIGHT 3550 THE CREW REPORTED THE FIRST OFFICER’S FLASHLIGHT HOLDER WAS BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FIRST OFFICER’S FLASHLIGHT CRADLE IAW EMB AMM25-60-10. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ISIS — INOPERATIVE (COCKPIT) · airframe 16,785 hrs · 14,216 cycles

ON FLIGHT 4047 THE CREW REPORTED THAT IN CRUISE FLIGHT AT FL 370 THE ISIS WENT BLANK. SHOWED ATT, AS, AND ALT FLAGS FOR SEVERAL MINUTES THEN THE AIRSPEED AND ALT CAME BACK BUT NOT THE ATTITUDE INDICATOR. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE INTERGRATED ELECTRICAL STANDBY INSTRUMENTS IAW EMB-145 AMM 34-01-01. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ISIS — INOPERATIVE (COCKPIT) · airframe 16,785 hrs · 14,216 cycles

ON FLIGHT 4047 THE CREW REPORTED THAT IN CRUISE FLIGHT AT FLIGHT LEVEL 370 THE ISIS WENT BLANK. SHOWED ATT, AS, AND ALT FLAGS FOR SEVERAL MINUTES THEN THE AIRSPEED AND ALT CAME BACK BUT NOT THE ATTITUDE INDICATOR. THE CREW ELECTED TO DIVERT TO CMH. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE INTERGRATED ELECTRICAL STANDBY INSTRUMENTS IAW EMB-145 AMM 34-01-01. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,371 hrs · 13,887 cycles

DURING MAINTENANCE BASE INSPECTION FOUND THE MAIN DOOR EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE MAIN DOOR EMERGENCY LIGHT IAW AMM TASKS 33-50-06-000-801-A AND 33-50-06-400-801-A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 16,063 hrs · 13,631 cycles

ON FLIGHT 4026 THE COCKPIT CREW REPORTED, UPON DESCENT AT ABOUT 11,000 FEET SMELLED AN ELECTRICAL BURNING ODOR FOR ABOUT 2 MINUTES THEN IT WENT AWAY (THE FLIGHT ATTENDANT COULD NOT SMELL ANYTHING IN THE CABIN). THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. COMPLIED WITH EMB 145 FIM 21-20-00-810-801-A SUPPLIED POWER TO THE AIRCRAFT FROM THE GPU FOR 3 HOURS. APU FOR 10 MIN AND ENG FOR 33 MIN WITH NO DEFECTS. COMPLIED WITH OPERATIONAL CHECKS FOR WINDSHIELD HEAT, HYD PUMP, PITOT/STATIC HEAT, AND ALL LANDING LIGHTS IAW EMB 145 AMM 30-42-01, 29-10-00, 30-31-06, 33-41-00, AND 33-42-00. COULD NOT DUPLICATE. NO PARTS REMOVED OR REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: HANDLE — LACK OF LUBE (CABIN DOOR) · airframe 15,954 hrs · 13,547 cycles

ON FLIGHT 3962 THE CREW REPORTED THE MAIN CABIN DOOR WAS VERY HARD TO CLOSE. THE AIRCRAFT WAS REMOVED FROM SERVICE. LUBRICATED DOOR HANDLE IAW EMB-145 AMM 52-18-00-600-801-A. NO PARTS REMOVED OR REPLACED. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FRAME — CHAFED (FUSELAGE) · airframe 14,628 hrs · 12,589 cycles

DURING MX BASE VISIT, FOUND CHAFE ON FRAME 19 IN THE GALLEY BELOW STRINGER 3 RT. THE ACFT WAS REMOVED FROM SERVICE. REPAIRED FRAME 19 IAW EO-EM-53MR-1778. THE ACFT WAS RETURNED TO SERVICE.

Part: CARBON SEAL — SMOKE (NR 1 ENGINE) · airframe 12,973 hrs · 11,320 cycles

ON FLIGHT THE CREW REPORTED AN ELECTRICAL BURNING ODOR IN FLIGHT AND NOTICED THE NR 1 ENGINE SMOKING AFTER SHUTDOWN. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 1 ENGINE IAW WC 71-000-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. THE CAUSE OF THE SMOKE WAS DETERMINED TO BE MADE BY THE NR 7 CARBON SEAL.

Part: BATTERY — DISCHARGED (CABIN) · airframe 12,299 hrs · 10,791 cycles

ON FLIGHT 3263 THE CAPTAIN REPORTED THAT THE AFT EMERGENCY LIGHTS DID NOT SHUT OFF AND THE BATTERIES HAVE DRAINED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED ALL FOUR EMERGENCY BATTERY PACKS AND CHARGERS NR 4 BATTERY P/N 2013-BR S/N B4901 NR 2 BATT P/N 2013-A S/N 04853 NR 3 BATT 2013-A S/N 67343 NR 1 BATT P/N 2013-A S/N 72769, NR 1 CHARGER P/N BA5-0933-901 S/N 00600 NR 4 CHARGER P/N BA5-0933-901 S/N C01178 NR 2 CHARGER P/N BA5-0933-901 S/N C01492 NR 3 CHARGER P/N 11-0049 S/N 16952. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — SHORTED (CABIN) · airframe 10,524 hrs · 9,415 cycles

DURING A MAINTENANCE INSPECTION OF THE CABIN FOUND THE AFT EMERGENCY FLASHLIGHT TO HAVE SHORT. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED FLASHLIGHT ASSEMBLY. OPERATIONAL CHECK GOOD IN ACCORDANCE WITH EMBRAER MAINTENANCE MANUAL 33-50-16. AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY PACK — CRACKED (CABIN) · airframe 10,383 hrs · 9,293 cycles

ON MAINTENANCE CHECK FOUND EMERGENCY LIGHT POWER SUPPLY BATTERY PACK CRACKED. REPLACED NUMBER 5 POWER BATTERY PACK. AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT) · airframe 9,452 hrs · 8,361 cycles

ON FLIGHT 4229 - CREW REPORTED THE FIRST 2 AND LAST 3 EMERGENCY FLOOR STRIP LIGHT COME ON FOR 1 SEC THEN BECOME INOPERATIVE WHEN LIGHT SWITCH IS TURNED ON. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED NR 2 BATTERY HOLDER AS PER EMB 145 AMM 33-50-04, OPERATION CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT)

ON FLIGHT 3574 CREW REPORTED ALL EMERGENCY LIGHTS LT ON AND WILL NOT TEST. AIRCRAFT REMOVED FROM SERVICE. REPLACED ALL EMERGENCY BATTERIES IAW EMB AMM 33-50-04. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (A)

Part: HANDLE — MALFUNCTIONED (MLG)

ON FLIGHT 3676 - CREW REPORTED ON LANDING GEAR EXTENSION THE AURAL WARNING ALERTED LANDING GEAR. CREW EXECUTED A MISSED APPROACH AND CHECKED AOM ITEMS. GEAR EXTENDED WHEN LANDING GEAR LEVER WAS PLACED IN THE DOWN POSITION BUT THE GEAR WAS ABNORMALLY SLOW. ACFT LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REMOVED AND REPLACED GEAR HANDLE IAW EMB 145 AMM 32-52-02, OPERATIONAL CHECKED GOOD. ACFT RETURNED TO SERVICE. (S)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 7,094 hrs · 6,357 cycles

ON FLIGHT 3890, CREW REPORTED EMERGENCY FLOOR TRACK LIGHTING BY SEATS 8-11 AND WING EMERGENCY EXIT LIGHTS AT THE BOTTOM OF BOTH DOORS INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED BATTERY PACK NR 3 IAW 145 AMM 33-50-04. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 5,159 hrs · 4,624 cycles

WITH APU BLEEDS TO PACKS A STRONG ODOR FILLED THE FLIGHT DECK. AFTER DESELECTING BLEEDS TO BOTH PACKS ODOR BECOMES STRONGER, DISSIPATED BY 15,000 FEET. FOUND APU INLET FILLED WITH LOCUST. REMOVED LOCUST FROM INLET AND PERFORMED OPERATIONAL CHECK OF APU, ENGINE BLEED SYSTEMS WITH NO DEFECTS NOTED. RETURNED AIRCRAFT TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 4,909 hrs · 4,401 cycles

LEFT OUTBOARD FLOOR SUPPORT BETWEEN FRAMES 60 AND 61 CORRODED. C/A - REPLACED FLOOR SUPPORT IN ACCORDANCE WITH EMB SRM. RETURNED AIRCRAFT TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 4,909 hrs · 4,401 cycles

LEFT OUTBOARD FLOOR SUPPORT BETWEEN FRAMES 60 AND 61 CORRODED. REPLACED FLOOR SUPPORT IN ACCORDANCE WITH EMB SRM, RETURNED AIRCRAFT TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 4,909 hrs · 4,401 cycles

LEFT OMEGA BEAM CORRODED ON INBOARD SIDE OF FRAME 20. REPAIRED DAMAGE IAW EMB SRM. RETURNED AIRCRAFT TO SERVICE.

Part: CONTROL UNIT — FAILED (FLT GUIDANCE)

ABORTED TAKEOFF FOR YAW DAMP FAIL WITH YAW DAMP ENGAGED. REMOVED AND REPLACED FLIGHT GUIDANCE CONTROL UNIT, OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)