N12195

Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 43,452 hrs · 29,758 cycles

MID FLOOR SUPPORT AT FRAME 20 HAS CRACK. REMOVED AND REPLACED MID FLOOR ANGLE AND ATTACHED SUPPORT AT FR20.

Part: WINDOW FRAME — CORRODED (ZONE 200) · corrosion level 2 · airframe 43,452 hrs · 29,758 cycles

FOUND CORROSION AROUND MULTIPLE SCREW HOLES BY THE RH DV WINDOW FRAME. RECEIVED NEW OUTER FRAME HALF FOR RH DV WINDOW, LOCATED AND DRILLED NEW HALF FOR INSULATION.

Part: RIB — DAMAGED (ZONE 600) · airframe 43,452 hrs · 29,758 cycles

RIGHT HAND MIDDLE LEADING EDGE DAMAGED ON REMOVAL AND HAS DAMAGE ON INBOARD EDGE. REMOVED AND REPLACED RH MIDDLE LEADING EDGE INBD RIB.

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 43,452 hrs · 29,758 cycles

FUSELAGE EXTERNAL LOWER SKIN LH AT FR 61, STR 18L, HAS CORROSION. COMPLIED WITH REAR FUSELAGE I - PERMANENT REINFORCING REPAIR OF SKIN AT FRAME 61 AND STRINGER 18L

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 43,452 hrs · 29,758 cycles

LH FLOOR BEAM LOWER IB LIP DOUBLER AT FR 22, STR 4L, HAS CORROSION. REMOVED CORRODED DOUBLER, FABRICATED AND INSTALLED NEW LH FLOOR BEAM LWR IB LIP DOUBLER AT FR22

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 43,452 hrs · 29,758 cycles

LH FLOOR BEAM LOWER IB LIP AT FR 20, STR 4L, HAS CORROSION. REMOVED CORRODED DOUBLER, FABRICATED AND INSTALLED NEW LH FLOOR BEAM LWR IB LIP DOUBLER AT FR20

Part: ACCESS PANEL — WORN (ZONE 100) · airframe 43,452 hrs · 29,758 cycles

ACCESS PANEL #412 CL SHOWS BARE METAL. RECEIVED NEW PANEL AND PAINTED.

Part: MOUNT — CORRODED (RADIO ALTIMETER) · airframe 43,452 hrs · 29,758 cycles

RADIO ALTIMETER (RAR 2) MOUNT HAS CORROSION/PITTING ON CONNECTOR HOLE LOWER EDGE. INSTALLED COMPLETE RADIO ALTIMETER (RAR 2) MOUNT

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 43,452 hrs · 29,758 cycles

LH FLOOR BEAM LOWER IB LIP DOUBLER AT FR 21, STR 4L, HAS CORROSION. REMOVED CORRODED DOUBLER, FABRICATED AND INSTALLED NEW LH FLOOR BEAM LWR IB LIP DOUBLER AT FR 21

Part: SKIN — CORRODED (ZONE 600 AILERON) · corrosion level 2 · airframe 43,452 hrs · 29,758 cycles

RH AILERON IB SKIN HAS CORROSION. NEW RH AILERON INSTALLED.

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 43,452 hrs · 29,758 cycles

CRACK IN THE OMEGA BEAM SPLICE DOUBLER AT MOST FWD IB FASTENER HOLE AT FR 23 / STR 15L. REMOVED AND REPLACED OMEGA BEAM SPLICE DOUBLER.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 43,452 hrs · 29,758 cycles

LH FLOOR BEAM LOWER IB LIP DOUBLER AT FR 23, STR 4L, HAS CORROSION. REMOVED CORRODED DOUBLER, FABRICATED AND INSTALLED NEW LH FLOOR BEAM LWR IB LIP DOUBLER AT FR23

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 43,452 hrs · 29,758 cycles

LH FLOOR BEAM LOWER IB LIP AT FR 22, STR 4L, HAS CORROSION. REMOVED CORRODED DOUBLER, FABRICATED AND INSTALLED NEW LH FLOOR BEAM LWR IB LIP DOUBLER AT FR22

Part: SKIN — DENTED (ZONE 100) · airframe 43,452 hrs · 29,758 cycles

FUSELAGE LOWER SKIN LH AT FR73 TO FR74, STR 21L HAS A DENT. RECONTOURED DENT ON FUSELAGE LOWER SKIN LH AT FR 73 TO FR 74, STR 21L.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 43,452 hrs · 29,758 cycles

LH FLOOR BEAM AT FR 23, STR 4L, HAS CORROSION AT FWD END. INSTALLED 1EA GUSSET.

Part: SKIN — CORRODED (ZONE 500 AILERON) · corrosion level 2 · airframe 43,452 hrs · 29,758 cycles

LH AILERON IB INTERNAL SKIN HAS CORROSION. NEW LH AILERON INSTALLED.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 43,452 hrs · 29,758 cycles

MID FLOOR BEAM GUSSET AT FR 73, STR 1R, HAS CORROSION. REMOVED AND REPLACED MID FLOOR BEAM GUSSET AT FR73.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 43,452 hrs · 29,758 cycles

RH FLOOR BEAM SILL DOUBLER AT FR20, STR 16R HAS CORROSION. FABRICATED DOUBLER. PREPPED, CLEANED, AND APPLIED ALODINE. INSTALLED RH FLOOR BEAM SILL DOUBLER AT FR20, STR 16L

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 43,452 hrs · 29,758 cycles

UPON REMOVAL OF THE MID FLOOR BEAM GUSSET FROM FR20 TO FR21 STR 1R FOUND OMEGA BEAM HAS MULTIPLE AREAS OF CORROSION. COMPLIED WITH REPAIR TO MID FLOOR OMEGA BEAM AT FR20 TO FR21.

Part: SILL DRAIN — CORRODED (ZONE 200) · corrosion level 2 · airframe 43,452 hrs · 29,758 cycles

RH MOP SILL AT FR 30, STR 16R, HAS CORROSION. REMOVED AND REPLACED RH FLOOR SILL AT FR 25 - FR 31.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 43,452 hrs · 29,758 cycles

RH FLOOR BEAM SILL AT FR 23, STR 16R, HAS CORROSION. REMOVED AND REPLACED RH FLOOR BEAM SILL AND FLOOR SUPPORT AT FR 22- FR23.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 43,452 hrs · 29,758 cycles

RH FLOOR BEAM GUSSET AT FR 22, STR 4R, HAS CORROSION. REMOVED AND REPLACED RH FLOOR BEAM GUSSET AT FR22.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 43,452 hrs · 29,758 cycles

UPON REMOVAL OF MID OMEGA BEAM GUSSET FOUND CROSS SUPPORT AT FR61 HOLE DAMAGED BEYOND LIMITS. REMOVED AND REPLACED PROFILE T-ANGLE

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 43,452 hrs · 29,758 cycles

SERVICE DOOR, R1, FLOOR SUPPORT AT FR 21, STR 16R, HAS CORROSION. REMOVED AND REPLACED SERVICE DOOR SILL AT R1, FLOOR SUPPORT FR21, STR 16R.

Part: SEAT TRACK — DAMAGED (ZONE 200) · corrosion level 2 · airframe 43,452 hrs · 29,758 cycles

MID SEAT TRACK AT FR 38 HAS DAMAGE. REMOVED AND REPLACED SEAT TRACK FR 38

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 43,452 hrs · 29,758 cycles

MID FLOOR BEAM GUSSET FROM FR 20 TO FR 21, STR 1R, HAS CORROSION. REMOVED AND REPLACED MID FLOOR BEAM GUSSET AT FR20-FR21.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 43,452 hrs · 29,758 cycles

LH FLOOR SUPPORT AT FR 20, STR 2L, HAS CORROSION. REMOVED AND REPLACED LH FLOOR SUPPORT AT FR20

Part: SILL DRAIN — CORRODED (ZONE 200) · corrosion level 2 · airframe 43,452 hrs · 29,758 cycles

"LH MOP SILL AT FR 26, STR 16L, HAS CORROSION. LH MOP SILL AT FR 24 HAS CORROSION AT FWD END. REMOVED AND REPLACED LH MOP SILL AT FR26

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 43,452 hrs · 29,758 cycles

LH FLOOR GUSSET DOUBLER AT FR 16, STR 4L, HAS CORROSION. REMOVED AND REPLACED LH FLOOR GUSSET DOUBLER AT FR16.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 43,452 hrs · 29,758 cycles

RH FLOOR BEAM GUSSET AT FR 20, STR 4R, HAS CORROSION. REMOVED AND REPLACED RH FLOOR BEAM GUSSET AT FR20.

Part: SILL DRAIN — CORRODED (ZONE 200) · corrosion level 2 · airframe 43,452 hrs · 29,758 cycles

LH MOP SILL FROM FR 19 TO FR 20 HAS CORROSION. LH MOP SILL FROM FR 22 TO FR 23 HAS CORROSION. REMOVED AND REPLACED LH MOP SILL FROM FR18 TO FR23

Part: FLOOR SUPPORT — CORRODED (ZONE 15) · corrosion level 2 · airframe 43,452 hrs · 29,758 cycles

RIGHT FLOOR GUSSET AT FR 61, STR 4R HAS CORROSION. REMOVED AND REPLACED RH FLOOR BEAM GUSSET AT FR 61, STR 4R.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 43,452 hrs · 29,758 cycles

"LH FLOOR GUSSET AT FR 61, STR 4L, HAS CORROSION. LH FLOOR GUSSET AT FR 60, STR 4L, HAS CORROSION. REMOVED AND REPLACED 1EA. LH FLOOR GUSSET AT FR 61, STR 4L.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 43,452 hrs · 29,758 cycles

RIGHT FLOOR GUSSET AT FR 61, STR 4R, HAS CORROSION. REMOVED AND REPALCED RT FLOOR BEAM GUSSET AT FR61, STR 4R.

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 42,627 hrs · 28,971 cycles

MULTIPLE EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY #2. OPS CHECK SAT.

Part: LAMP — INOPERATIVE (ZONE 200) · airframe 42,620 hrs · 28,965 cycles

RH WING FWD EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED BULB ON RH WING FWD EMERGENCY LIGHT. OPS CHECK SAT.

Part: OIL SYSTEM — OVERTEMP (NR 2 ENGINE) · airframe 42,294 hrs · 28,664 cycles

E2 HIGH OIL TEMP. PERFORMED E2 SHUT DOWN. MAX E2 OIL TEMP 142C. PERFORMED BORESCOPE INSPECTION OF THE MID-SPAN ROLLER BEARING ASSEMBLY. NO DEFECTS NOTED. REMOVED AND REPLACED RH ENGINE. OPS/LEAK CHECK SAT.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 41,782 hrs · 28,162 cycles

AFT EMERGENCY CEILING LIGHT INOPERATIVE. REMOVED AND REPLACED AFT EMERGENCY AISLE LIGHT BULB. OPS CHECK SAT

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 40,950 hrs · 27,392 cycles

PANEL 263ALC EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED AISLE EMERGENCY LIGHT LAMP. OPS CHECK SAT.

Part: GROUND WIRE — UNRELIABLE (EMERGENCY LIGHT) · airframe 40,896 hrs · 27,347 cycles

MCD EMERGENCY LIGHT OUT . REMOVED AND REPLACED BULB. OPS CHECK FAIL. REMOVED EMERGENCY LIGHT HOUSING. INSPECTED WIRING AND IDENTIFIED POORLY BONDED GROUND AT TERMINATION OF W734-0002-20. DISSASSMBLED, CLEANED, AND REASSEMBLED TERMINAL AND GROUNDING POINT AND VERIFIED PROPER BONDING. NO OTHER ELECTRICAL FAULTS OBSERVED. REINSTALLED EMERGENCY LIGHT. OPS CHECK SAT.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 40,816 hrs · 27,270 cycles

FOUND MAIN DOOR EXTERNAL EMERGENCY LIGHT INOPERATIVE INTERMITTENTLY. REMOVED MAIN DOOR EXTERNAL EMERGENCY LIGHT ASSEMBLY TO BEGIN. FOUND ISSUE TO BE THE CONTACTORS INSIDE HOUSING AND WIRING HARNESS END TERMINAL. INSTALLED EMERGENCY LIGHT ASSEMBLY ON MAIN CABIN DOOR. OPS CHECK SAT.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 40,715 hrs · 27,182 cycles

RAMP REPORTED DENT IN CARGO DOOR. PERFORMED RECOUNTOUR AT DENT. NO CHANGE IN SHAPE OF DENT NOTED. REMOVED DAMAGED SKIN AT AFT LOWER CARGO DOOR SKIN. PERFORMED HFEC INSPECTION ON CUTOUT SECTION. NO CRACKS INDICATION FOUND. FABRICATED REPAIR DOUBLER AND FILLER FOR INSTALL AFT LOWER CARGO DOOR SKIN. COMPLETED INSTALL OF MAJOR REPAIR AT LOWER AFT CORNER OF CARGO DOOR SKIN. REG PRESS LEAK CHECK. PRESSURE LEAK CHECK PERFORMED LEAK CHECK GOOD.

Part: PRESSURE SYSTEM — INOPERATIVE · airframe 38,581 hrs · 25,231 cycles

CABIN PRESSURIZATION INOPERATIVE IN MAN AND AUTO MODE DURING CLIMB OUT. PERFORMED OPERATIONAL CHECK OF AUTO AND MANUAL PRESSURIZATION. OPS CHECK GOOD. PERFORMED LEAK CHECK OF #1 AND #2 PACKS. NO LEAKS NOTED. REMOVED AND REPLACED DIGITAL CONTROLLER. PERFORMED PRESSURIZATION CHECK. OPS CHECK SAT

Part: DOOR — LACK OF LUBE · airframe 38,518 hrs · 25,170 cycles

MAIN CABIN DOOR IS HARD TO OPEN FROM THE INSIDE. PERFORMED OPS CHECK OF MAIN CABIN DOOR. NO DEFECTS NOTED

Part: BULKHEAD — CRACKED · airframe 38,512 hrs · 25,164 cycles

AT LH MLG WHEEL WELL, AFT BULKHEAD CRACKED AT 2 PLACES. INNER REINFORCEMENT ANGLE ON LH WING STUB SPAR 3 (WHEEL WELL AFT BULKHEAD) FAIRING ATTACHMENT ANGLE.

Part: FRAME — CRACKED · airframe 38,512 hrs · 25,164 cycles

RF1 LH FRAME 68 CRACKED ABOVE FLOOR LEVEL. RF1 LH CRACKED FRAME 68 REPAIRED.

Part: SKIN PANEL — DENTED · airframe 38,512 hrs · 25,164 cycles

LIGHTNING STRIKE SUSPECTED UNDER SERVICE DOOR BTW FR 20-21 AND STR 17-18. AFTER INVESTIGATION, NO LIGHTNING STRIKE FOUND. DAMAGE ON SKIN RH SIDE UNDER SERVICE DOOR IS A NICK BLENDED OUT OF LIMITS. DAMAGE REMOVED BY CUTOUT ON RH SKIN BTW FR20-21 AND BTW STR 17-18. RH SKIN BTW FR 20-21 AND BTW STR 17 TO SKIN 18 REPAIRED WITH A PATCH DOUBLER.

Part: SKIN PANEL — DENTED · airframe 38,512 hrs · 25,164 cycles

VERT STAB LH SKIN DENT BETWEEN SPAR 1 AND SPAR 2 AND BETWEEN RIB ZV 1423 AND RIB ZV 1677. VERT STAB LH SKIN SPAR 1 AND 2 AND BTW RIB ZV1423 AND ZV1677 PAINT STRIPPED. VERT STAB LH SKIN BTW SPAR 1 AND 2 AND BTW RIB ZV 1423 AND ZV 1677. DAMAGE CUTOUT DONE. VERT STAB LH SKIN BTW SPAR 1 AND 2 AND BTW RIB ZV 1423 AND ZV 1677 REPAIRED.

Part: SKIN PANEL — CORRODED · corrosion level 2 · airframe 38,512 hrs · 25,164 cycles

CORROSION FOUND ON INTERNAL SKIN AN ANTENNA DOUBLER BTW STR 21L-21R BTW FR 68-69. AFTER CORROSION INVESTIGATION ON SKIN AT ANTENNA LOCATION BTW FR 68-69 AND STR 21L-21R CRACKS FOUND AROUND RIVET HOLE AND REPAIR IS REQUIRED. SKIN AT FR 68-69 BTW STR 21-21R REPAIRED WITH DOUBLER.

Part: BEAM — CRACKED (ZONE 100) · airframe 38,512 hrs · 25,164 cycles

LH OMEGA BEAM FOUND CRACKED (X3) AT FR 21, FR 22. 3 REPAIR DOUBLES ON L/H CENTER FUSE 1 OMEGA BEAM, ON INBD FLANGE AT 21,22 &23

Part: WEB — CRACKED · airframe 38,512 hrs · 25,164 cycles

COCKPIT RH OVERHEAD HORIZONTAL WEB CRACKED AT GRAB HANDLE SUPPORT. REPAIR DOUBLER ON RH FWD FUSE 2 WINDOW FLIGHT COMPARTMENT OVERHEAD PANEL

Part: DOOR FRAME — INADEQUATE (ZONE 800) · airframe 38,512 hrs · 25,164 cycles

EXISTING REPAIR ON PAX DOOR LOWER FRAME NOT PROPERLY PERFORMED (DOUBLE DOESN'T FIT WELL). EDDY CURRENT INSPECTION CARRIED OUT ON CUTOUTS LINES (2X) AND SURROUNDING AREA, NO CRACKS FOUND. REPAIR ON PAX DOOR LOWER FRAME REDONE.

Part: NONE — NONE · airframe 38,512 hrs · 25,164 cycles

EXISTING REPAIR DOUBLE ON FWD PRESSURE BULKHEAD NEED TO BE REMOVED FOR INVESTIGATION. FWD PRESSURE BULKHEAD REPAIRED WITH DOUBLER.

Part: NONE — NONE · airframe 38,512 hrs · 25,164 cycles

LOOSE RIVET ON R/H FF2 SKIN BTW FRAME 7&8 AND BTW STR 19&20. LOOSE RIVET ON R/H FF 2 SKIN REMOVED. AFTER RIVET REMOVAL, DAMAGE FOUND AND BLENDED OUT OF LIMITS. DAMAGE ON R/H SKIN BTW FM 7&8 AND BTW STR 19&20 REPAIRED WITH A PATCH DOUBLER.

Part: NONE — NONE · airframe 38,489 hrs · 25,143 cycles

HYD 1 LOW QTY "ON EICAS" & HYD FLUID 1 IN AMBER IN FLIGHT. HYD 1 FAIL AFTER LANDING

Part: NOT REPORTED — NOT REPORTED · airframe 38,205 hrs · 24,903 cycles

PACK 2 VALVE CLOSED IN FLIGHT. PACK 1 VALVE CLOSED APPEARED. RAN QRH MSG EXTINGUISHED THEN RETURNED NUMEROUS TIMES. R&R BLOWN DUCT AT DUAL TORQUE MOTOR. PACK 1 & 2 OPS CHECK SAT.

Part: LIFE VEST — TORN · airframe 37,852 hrs · 24,581 cycles

FO LIFE VEST BAG TORN OPEN. R&R FO LIFE VEST

Part: VALVE — INOPERATIVE · airframe 37,764 hrs · 24,504 cycles

ENG 2 A/ICE FAIL IN FLIGHT (FL 200 CLIMBING OUT, IN ICING, CLIMBED OUT OF ICING TO FL 230, ON FOR 1 MIN, "ICING CONDITION WITH ANTI ICING INOPERATIVE WARNING MSG", THROTTLES AT 89N2). R&R #2 ENG ANTI ICE VALVE. R&R E2 ANTI ICE PRESS XDUCER. PERFORMED OPS CHECK AND INSPECTED FOR LEAKS AND INSPECTED VISIBLE AREAS OF HARNESS. OPS CHECK GOOD.

Part: SEAT FRAME — CRACKED (SEAT 8A) · airframe 36,919 hrs · 23,767 cycles

SEAT 8A AISLE SIDE FRAME CRACKED. R&R PASSENGER SEAT 8A.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 36,399 hrs · 23,298 cycles

MOST AFT EMERGENCY CEILING LIGHTS WILL NOT ILLUMINATE. REMOVED AND REPLACED EMERGENCY LIGHT LAMP. OPERATIONS CHECK SATISFACTORY.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 36,377 hrs · 23,280 cycles

LEFT SIDE EMERGENCY ROW OVERHEAD EMERGENCY LIGHT INOPERATIVE AT SEAT 18A. R & R LEFT SIDE EMERGENCY ROW OVERHEAD EMERGENCY LIGHT BULB AT SEAT 18A. OPERATIONS CHECK SATISFACTORY.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 36,297 hrs · 23,197 cycles

MAIN DOOR EMERGENCY LIGHT INTERMITTENT OPERATION. R & R BATTERY CHARGER ASSEMBLY. OPERATIONS CHECK SATISFACTORY.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 36,054 hrs · 22,934 cycles

EMERGENCY EXIT IDENTIFIER LIGHT, LOCATED ON LH AFT IS INOPERATIVE. R&R LH FWD EMERGENCY HATCH IDENTIFIER EMERGENCY LIGHT. OPS CHECK FAILED. R&R #5 EMERGENCY LIGHT DC/AC INVERTER. OPS CHECK SAT.

Part: DOOR FRAME — CORRODED (PAX DOOR) · corrosion level 2 · airframe 35,022 hrs · 22,025 cycles

CORROSION - PAX DOOR LOWER FRAME. INSTALLED REPAIR DOUBLER AND FILLERS ON THE PASSENGER DOOR LOWER FRAME.

Part: SKIN PANEL — NOT REPORTED (FUSELAGE) · airframe 35,022 hrs · 22,025 cycles

PERMANENT REPAIR OF FORWARD RH FUSELAGE SKIN PANEL 120-22656-048 REQUIRED WITHIN 3000 FLIGHT CYCLES. MADE PERMANENT REPAIR OF FORWARD RH FUSELAGE SKIN PANEL 120-22656-048.

Part: SIGN — INOPERATIVE (FWD CABIN) · airframe 34,656 hrs · 21,672 cycles

FWD RH EMERGENCY EXIT LOCATOR LIGHT INOPERATIVE. R&R ILLUMINATED PLACARD. OPS CHECK SAT.

Part: LIGHT — INOPERATIVE (LT OVERWING) · airframe 34,619 hrs · 21,632 cycles

LH FWD OVER WING EMERGENCY EXIT LOCATOR LIGHT INOPERATIVE. R&R LH FWD OVER WING EMERGENCY LOCATOR LIGHT. OPS CHECK SAT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,613 hrs · 21,625 cycles

SERVICE DOOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED SERVICE DOOR EMERGENCY LIGHT LAMP AND ASSEMBLY. OPS CHECK SAT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,613 hrs · 21,625 cycles

SERVICE DOOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED SERVICE DOOR EMERGENCY LIGHT LAMP AND ASSEMBLY. OPS CHECK SAT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,602 hrs · 21,613 cycles

LT EMERGENCY EXIT DOOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED LIGHT. OPS CHECK SAT.

Part: SIGN — UNSECURE (CABIN) · airframe 34,596 hrs · 21,608 cycles

EMERGENCY EXIT SIGN AT 18D FALLING OFF. R&R AFT CENTER AISLE EXIT SIGN. OPS CHECK SAT.

Part: SIGN — DETACHED (CABIN) · airframe 34,594 hrs · 21,606 cycles

ROW 18 EMERGENCY EXIT SIGN DETACHED. SECURED AS REQUIRED.

Part: LIGHT — INOPERATIVE (ROW 18CD) · airframe 33,062 hrs · 20,222 cycles

EMERGENCY LIGHT ABOVE ROW 18CD WAS INOPERATIVE. R & R THE EMERGENCY LIGHT ABOVE. OPS CHECKED SATISFACTORY.

Part: SUPPORT — CORRODED (ANTENNA) · airframe 30,654 hrs · 18,450 cycles

AFT RADIO ALTIMETER ANTENNA SUPPORT CORRODED. ANTENNA SUPPORT REPLACED.

Part: PLATE — CORRODED (FUSELAGE) · airframe 30,654 hrs · 18,450 cycles

AFT RADIO ALTIMETER PLATE ASSEMBLY CORRODED. PLATE ASSEMBLY REPLACED. FUSELAGE SKIN WAS BLENDED AND INSPECTION PERFORMED PER SRM 51-10-03. HFEC INSPECTION PERFORMED WITH NO FAULTS FOUND.

Part: FITTING — CORRODED · airframe 30,654 hrs · 18,450 cycles

VERTICAL STAB TO HORIZONTAL STAB LT SPHERICAL BEARING HOLE CORRODED. CORROSION REMOVED IAW SRM 54-30-02, TABLE 201, REWORK 1.

Part: BEAM — CORRODED (CARGO DOOR) · airframe 30,654 hrs · 18,450 cycles

CARGO DOOR LOWER BEAM CORRODED. THE BEAM WAS REPLACED IAW SRM 51-40-02.

Part: FRAME — CORRODED (FUSELAGE) · airframe 30,654 hrs · 18,450 cycles

FRAME 65 BETWEEN STRINGER 16-17 FOUND CORRODED. REPAIRED AS PER ETD2017-145-039725A AND SRM 53-31-04 ITEM E FIG 212

Part: BEARING CAP — CORRODED (NOSE GEAR) · airframe 30,654 hrs · 18,450 cycles

CORROSION FOUND ON NOSE LANDING GEAR L/H LOWER BEARING CAP. LOWER BEARING CAP REPLACED AS PER 32-20-01.

Part: ANGLE — CRACKED (FLOOR SUPPORT) · airframe 30,654 hrs · 18,450 cycles

CENTER FUSELAGE 3 RT OMEGA BEAM ANGLES CRACKED. ANGLE REPAIRED IAW SRM 1142 53-23-02 AND ETD2017-145-039741.

Part: BRACKET — CORRODED (PAX DOOR) · airframe 30,654 hrs · 18,450 cycles

PAX DOOR LOWER FORWARD U SHAPE BRACKET CORRODED. THE BRACKET WAS REPLACED IAW SRM 51-40-02.

Part: ANGLE — CRACKED (FLOOR SUPPORT) · airframe 30,654 hrs · 18,450 cycles

CENTER FUSELAGE RT OMEGA BEAM ANGLE CRACKED. ANGLE REPAIRED IAW SRM 1142 53-23-02, AND ETD2017-145-039741.

Part: STRINGER — CRACKED (VERTICAL STAB) · airframe 30,654 hrs · 18,450 cycles

VERTICAL STAB LT LOWER STRINGER CRACKED AT TRAILING EDGE. THE STRINGER WAS REPLACED IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 30,654 hrs · 18,450 cycles

CENTER FUSELAGE FLOOR STRUCTURE LT FORWARD DIGITAL CORRODED AT ANCHOR NUT. DIGITAL REPAIRED IAW SRM 53-21-10, FIG 201, SHEET 5, DET C, WITH DOUBLER AND FILLER.

Part: ANGLE — CRACKED (FLOOR SUPPORT) · airframe 30,654 hrs · 18,450 cycles

CENTER FUSELAGE RT OMEGA BEAM ANGLE CRACKED. ANGLE REPAIRED IAW SRM 53-23-02 AND ETD2017-145-039741.

Part: ANGLE — CRACKED (FLOOR SUPPORT) · airframe 30,654 hrs · 18,450 cycles

CENTER FUSELAGE RT OMEGA BEAM ANGLE CRACKED. ANGLE REPLACED IAW SRM 1142 53-23-02 AND ETD2017-145-039741.

Part: BRACKET — CORRODED (PAX DOOR) · airframe 30,654 hrs · 18,450 cycles

PAX DOOR LOWER AFT U SHAPED BACKET CORRODED. LOWER AFT BRACKETT WAS REPLACED IAW SRM 51-40-02.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 30,654 hrs · 18,450 cycles

RIGHT GUSSET CORRODED AT CENTER FUSELAGE 4 TOILET AREA. THE GUSSET WAS REPLACED.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 30,654 hrs · 18,450 cycles

LEFT GUSSET CORRODED AT CENTER FUSELAGE 4 TOILET AREA. THE GUSSET WAS REPLACED IAW SRM 51-40-02

Part: ANGLE — CRACKED (STEP) · airframe 30,654 hrs · 18,450 cycles

CENTER FUSELAGE ONE LT, AFT STEP ANGLE CRACKED. THE ANGLE WAS REPLACED IAW SRM 51-40-02.

Part: BRACKET — CRACKED (CARGO DOOR) · airframe 30,654 hrs · 18,450 cycles

CARGO DOOR AFT MECHANISM LOWER BRACKET CRACKED. THE BRACKET WAS REPLACED IAW SRM 51-40-02.

Part: SHEAR TIE — CRACKED (FRAME 80) · airframe 30,654 hrs · 18,450 cycles

LEFT SHEAR TIE CRACKED AT FRAME 80. THE SHEAR TIE WAS REPLACED IAW SRM 51-40-02.

Part: SHEAR TIE — CORRODED (FRAME 52) · airframe 30,654 hrs · 18,450 cycles

SHEAR TIE CORRODED AT FRAME 52 BETWEEN STRINGERS 19 AND 20. THE SHEAR TIE WAS REPLACED IAW SRM 51-40-02.

Part: FLOORBEAM — CORRODED (FRAME 20) · airframe 30,654 hrs · 18,450 cycles

CENTER CABIN FLOORBEAM AT FRAME 20 CORRODED. THE FLOORBEAM WAS REPLACED IAW SRM 51-40-02.

Part: CONTROL MODULE — SHORTED (CABIN LIGHTS) · airframe 28,690 hrs · 17,080 cycles

ELECTRICAL BURNING ODOR IN THE CABIN REPORTED. MAINTENANCE FOUND ELECTRICAL ODOR COMING FROM CABIN LIGHT CONTROL MODULE. R & R CONTROL MODULE WITH OPS CHECK GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 28,535 hrs · 16,968 cycles

RT EMERGENCY EXIT LIGHT OUT ON AFT SIDEWALL PANEL AT ROW 18. R & R EXIT MARKING SIGN. OPS CHECKED GOOD. ACFT RELEASED AND RETURNED TO SERVICE.

Part: FLAPPER VALVE — WORN (ZONE 500) · airframe 22,468 hrs · 12,859 cycles

DURING CLIMB, FLUID LOSS FROM THE LT WING AND CREW ELECTED TO RETURN TO DEPARTURE. LANDED WITHOUT INCIDENT. REPLACED THE LT WING RIB 19 FLAPPER VALVE AND CLEARED THE DISCREPANCY.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHTS) · airframe 22,381 hrs · 12,805 cycles

DURING ROUTINE MAINTENANCE, CABIN EMERGENCY LIGHTS WERE FOUND INOPERATIVE AT FORWARD CEILING ABOVE F/A SEAT AND ON FOWARD BULKHEAD. MAINTENANCE REPLACED THE NR 1 EMERGENCY LIGHT BATTERY. OPS CHECKED GOOD.

Part: ACM — FROZEN (ZONE 100) · airframe 22,210 hrs · 12,674 cycles

DURING CLIMBOUT, CREW REPORTED THAT AT FL240 THE FLIGHT CREW AND F/A EXPERIENCED A STRONG ODOR OF SMOKE. THE ACFT RETURNED TO DEPARTURE WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE ACFT AND PLACED THE PACK ON MEL 21-51-00-3, CAT-C, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. MAINTENANCE R & R THE NR 1 ACM, OPERATIONALLY TESTED WITH NO DEFECTS, CLEARED THE MEL, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ACM — SEIZED (NR 1) · airframe 22,084 hrs · 12,590 cycles

CREW REPORTED A RUBBERY BURNING ODOR DURING TAKEOFF, PACK NOT COOLING , FELT VIBRATION UNDER FLOOR. ACFT RETURNED TO DEPARTURE, & LANDED WITHOUT INCIDENT. MX INSPECTED AND FOUND NR 1 ACM TO BE SEIZED. R & R THE NR 1 ACM, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ACM — SEIZED (NR 1) · airframe 22,084 hrs · 12,590 cycles

RUBBERY BURNING ODOR DURING TAKEOFF, PACK NOT COOLING, FELT VIBRATION UNDER FLOOR. ACFT RETURNED TO DEPARTURE & LANDED WITHOUT INCIDENT. MX INSPECTED ACFT AND FOUND NR 1 ACM TO BE SEIZED CAUSING THE ODOR AND OTHER ISSUES.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT) · airframe 21,576 hrs · 12,276 cycles

DURING ROUTINE MX, THE EMERGENCY EXIT ROW AFT LIGHT WAS INOPERATIVE. MX REPLACED THE NR 4 EMERGENCY LIGHT INVERTER. OPS CHECKED GOOD.

Part: FLAPPER VALVE — LEAKING (FUEL SYSTEM) · airframe 19,619 hrs · 11,038 cycles

DURING CLIMB FUEL WAS REPORTED TO BE LEAKING FROM THE RT WING. THE ACFT RETURNED TO DEPARTURE WHERE OIT LANDED WITHOUT INCIDENT. MX R & R THE OTBD FLAPPER VALVE AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 19,226 hrs · 10,756 cycles

DURING MX INSPECTION, EMERGENCY LIGHTS AT SEAT 7A AND ABOVE SEAT 12A WERE FOUND TO BE INOPERATIVE. MX R & R THE LAMPS AT SEAT 7A AND 12A WITH OPS CHECK SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FRAME — DAMAGED (ZONE 100) · airframe 18,842 hrs · 10,474 cycles

DURING C-CHECK, LIGHTNING HOLE DAMAGED AT FRAME 13 WHERE PILOTS FWD OTBD AILERON CABLE PASSES THROUGH. MX PERFORMED REPAIR IAW EC5310-01620. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 18,842 hrs · 10,474 cycles

DURING C-CHECK, STRINGER 21R HAS CORROSION BETWEEN FRAMES 13-14. MX PERFORMED REPAIR ON STRINGER 21R BETWEEN FRAMES 13-14 IAW EC5310-01619. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SILL — CORRODED (SERVICE DOORWAY) · corrosion level 2 · airframe 18,842 hrs · 10,474 cycles

DURING C-CHECK, SERVICE DOOR CENTER SILL FRAMES 20-22 IS CORRODED. MX R & R SERVICE DOOR CENTER SILL BETWEEN FRAMES 20-22 IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONTROLLER — INOPERATIVE (CABIN PRESSURE) · airframe 18,870 hrs · 10,495 cycles

MANUAL PRESSURIZATION INOPERATIVE, DURING CLIMB, FLT DIVERTED. MX R & R DIGITAL CONTROLLER IAW AMM 21-31-01. OPS CHECKED GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 18,409 hrs · 10,186 cycles

DURING A-CHECK INSPECTION, THE GALLEY SERVICE DOOR EMERGENCY LIGHT BULB ON DOOR BOTTOM WAS FOUND TO BE INOPERATIVE. MX R & R THE AFFECTED LIGHT BULB, OPS TESTED WITH NO DEFECTS NOTED.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 16,332 hrs · 8,905 cycles

RIC - DURING ROUTINE MAINTENANCE, RIC MX FOUND GALLEY LOWER EXIT SIGN INOPERATIVE. MX REMOVED AND REPLACED NR 2 INVERTER AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: FILTER — DIRTY (BLEED AIR SYS) · airframe 16,309 hrs · 8,888 cycles

DEN - DURING CLIMB THE CREW REPORTED BLEED ONE AND TWO TO BE INOPERATIVE. THE AIRCRAFT RETURNED TO DEN WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE CLEANED BOTH BLEED AIR VALVE FILTERS, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — DENTED (RT WING) · airframe 17,753 hrs · 8,502 cycles

TYS - A/C WAS ON GROUND ON ORD WHEN REPORTS OF A TORNADO ACTIVITY AT THE FIELD, A/C WAS EVALUATED FOR DAMAGE OVER THE WINGS DUE TO FLYING DEBRIS. ALL PAX WAS DEPLANED AND NO INJURIES REPORTED. AC WAS FERRIED TO TYS WHERE MAINTENANCE REPLACED THE RT WING NR 3 LEADING EDGE IAW 145 AMM 57-43-00-400-801A. ALSO REMOVED, REPAIRED AND REINSTALL THE RT AILERON IAW EMB 145XR AMM 27-10-00. OPS CHECK GOOD AND WAS RELEASED BACK TO SERVICE.

Part: LIGHT — LOOSE (CABIN) · airframe 14,611 hrs · 7,815 cycles

FLIGHT 2943 - EWR - FLIGHT CREW REPORTED EMERGENCY LIGHT STRIP LOOSE. EWR MX RE-SECURED EMERGENCY LIGHT AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: CROSSBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 13,985 hrs · 7,462 cycles

SHV - DURING C-CHECK CROSS BEAM (TRIANGLE SHAPE) AT FRAME 65 BETWEEN STRINGER 16L-19L HAS CORROSION (LEVEL 2 LOCAL) AROUND SCREW HOLE. MAINTENANCE PERFORMED REPAIR ON CROSSBEAM (TRIANGLE SHAPE) AT FRAME 65 BETWEEN STRINGER 16L-19L IAW EC5320-01479. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BULKHEAD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 13,985 hrs · 7,462 cycles

SHV - DURING C-CHECK MACHINE BULKHEAD AT FRAME 65 HAS CORROSION (LEVEL 2 LOCAL) AT STRINGER 16R. MAINTENANCE PERFORMED REPAIR ON MACHINE BULKHEAD AT FRAME 65 STRINGER 16R IAW EMB-145XR SRM 51-10-03 AND CPM 51-21-06. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY — OVERTEMP (ZONE 100) · airframe 12,897 hrs · 6,857 cycles

IAH - FLIGHT 2377, THE CREW REPORTED A BATTERY TWO OVERTEMP INDICATION IN FLIGHT. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO BATTERY, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: TRIM SWITCH — INOPERATIVE (COCKPIT) · airframe 11,962 hrs · 6,345 cycles

IAH - FLIGHT 2738, THE CREW REPORTED THE CAPTAINS PITCH TRIM SWITCH TO BE INOPERATIVE. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SWITCH, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 10,541 hrs · 5,568 cycles

IAH - DURING PREFLIGHT INSPECTION THE CREW REPORTED THAT THE MOST FORWARD EMERGENCY LIGHT STRIP WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT STRIP, OPERATIONALLY TESTED WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRIP — BROKEN (CABIN) · airframe 9,643 hrs · 5,088 cycles

CLE - FLIGHT 3100 - THE CREW REPORTED THE EMERGENCY FLOOR LIGHTING STRIP BY GALLEY WAS BROKEN. MAINTENANCE INSPECTED AND REPLACED THE GALLEY FLOOR LIGHT STRIP. OPERATIONAL CHECKS WERE GOOD.

Part: LIGHT — LOOSE (CABIN) · airframe 9,527 hrs · 5,019 cycles

FLIGHT 2055 - EWR - FLIGHT CREW REPORTED EMERGENCY LIGHT STRIP LOOSE BY GALLEY AREA. EWR MX RE-SECURED LIGHT STRIP AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: SUPPORT BEAM — CORRODED (FUSELAGE) · airframe 9,115 hrs · 4,805 cycles

SHV - DURING C-CK-CARGO DOOR CUTOUT LWR BEAM HAS CORROSION FR 65-68. REMOVED AND REPLACED CUTOUT LOWER BEAM IAW EMB 145 SRM 51-40-02. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: HANDLE — LOOSE (PAX DOOR)

FLT 0022 - ONT - FLIGHT CREW REPORTED MAIN CABIN DOOR HARD TO OPEN. MX PERSONNEL RESECURED LOOSE BOLT AT THE BASE OF HANDLE ON MAIN CABIN DOOR. OPERATIONALLY CHECKED SATISFACTORY AND ACFT WAS RELEASED TO RETURN FOR SERVICE. (S)

Part: LIGHT — OUT OF POSITION (CABIN) · airframe 6,476 hrs · 3,380 cycles

FLT 501 - SAT TO RDU - FLIGHT CREW REPORTED EMERGENCY FLOOR PROXIMITY STRIP MISSING ROW 9. CONTRACT MX WAS DISPATCHED TO RECOVER. CONTRACT MX FOUND MISSING LIGHT STRIP WAS UNDER ANOTHER ONE AND RESECURED STRIP ON ITS ORIGINAL POSITION OPERATIONALLY CHECKED SATISFACTORY. AIRCRAFT WAS RELEASED FOR RETURN TO SERVICE.

Part: CABIN PRESSURE — MALFUNCTIONED · airframe 6,180 hrs · 3,210 cycles

FLT 103 - COS TO ONT - FLIGHT CREW REPORTED A/C WOULD NOT PRESSURIZE DURING WINDSHEAR ISSUES ON CLIMBOUT. BLEED WERE OFF, THEN TURNED ON. A/C RETURNED TO BLOCK WITHOUT INCIDENT. CONTRACT MX (ARNIC) RAN THE ENGINES WITH FLIGHT CREW AND OPERATIONALLY CHECKED GOOD AND PRESSURIZATION PASSED SATISFACTORY. A/C WAS RELEASED TO RETURN FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 5,158 hrs · 2,682 cycles

FLT MX - ONT - WHILE PERFORMING 3A CHECK AND OPERATIONAL INSPECTION OF THE EMERGENCY LIGHTING SYSTEM. QC INSPECTOR FOUND SERVICE DOOR EMERGENCY LIGHT DID NOT ILLUMINATE (DOOR PATH LIGHTING). MX PERSONNEL REMOVED AND REPLACED SERVICE DOOR EMERGENCY LIGHT BULB IAW EMB 145XR AMM 33-50-09. OPERATIONALLY CHECKED GOOD AND AIRCRAFT WAS RELEASE TO RETURN FOR SERVICE IN AIRWORTHY CONDITIONS.

Part: WARNING SYSTEM — ACTIVATED (FLAP SYSTEM) · airframe 4,027 hrs · 2,111 cycles

FLT 17 - ONT - CREW ABORTED TAKEOFF DUE TO FLAP FAIL INDICATION. ONT MX PERFORMED FLAP SYSTEM RESET. MX PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 2,250 hrs · 1,163 cycles

IAH - FLIGHT 3162, THE CREW REPORTED A STRANGE SMELL AND LOUD POP AFTER SUSPECTING THE AIRCRAFT WAS HIT BY LIGHTNING. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT IAW EMB-145-XR AMM 05-50-01 AND 21-00-00.