N21154

Part: PUMP — INOPERATIVE (HYD SYSTEM) · airframe 49,056 hrs · 33,126 cycles

#1 HYD SYSTEM INDICATION SHOWED ZERO MOMENTARILY IN FLIGHT. DURING INITIAL INSPECTION FOUND NO LEAKS PRESENT AND HYD QTY OKAY. PERFORMED GEAR SWINGS. WHILE SWINGING WAS ABLE TO DUPLICATE HYD 1 LOW WTY AND HYD 1 FAILURE. FOUND EMDP TO BE CAVITATING CAUSING LOW PRESSURES AND HYDRAULIC SYS 1 FAILURE. REMOVED AND REPLACED LH EMDP AND BLED HYD 1 SYSTEM FROM RESERVIOR EDP. LEAK CHECK SAT. OPS CHECK SAT. NO MESSAGES OR FAULTS FOUND THROUGHOUT OPS CHECK AND GEAR SWINGS. PERFORMED LG FREE FALL INSPECTION. NO DEFECTS NOTED, PERFORMED OPS CHECK. OPS CHECK SAT. NO DEFECTS NOTED.

Part: ROLLER — OUT OF ADJUST (ZONE 800) · airframe 49,009 hrs · 33,082 cycles

MAIN CABIN DOOR IS HARD TO OPEN AND CLOSE. READJUSTED MAIN CABIN DOOR ROLLERS. OPS CHECK SAT.

Part: OXYGEN BOTTLE — INOPERATIVE (ZONE 100) · airframe 48,962 hrs · 33,039 cycles

CREW OXYGEN PRESSURE IS AT ZERO PSI. REMOVED AND REPLACED CREW OXYGEN CYLINDER. LEAK CHECK SAT

Part: ELEC CONNECTOR — DISCONNECTED (ZONE 200) · airframe 48,962 hrs · 33,039 cycles

BOTH EMERGENCY LIGHTS NEAR RH WING ROOT IS INOPERATIVE. RECONNECTED CANNON PLUGS OF BOTH RH WING-TO-FUSELAGE FAIRING EMERGENCY LIGHTS.

Part: SKIN — CRACKED (ZONE 400) · airframe 48,962 hrs · 33,039 cycles

LH LOWER ENGINE COWL SKIN CRACKED ALONG UPPER EDGE NEAR FWD HINGE. INSTALLED NEW FILLER AND DOUBLER AT LH LOWER ENGINE COWL SKIN, UPPER EDGE NEAR FWD HINGE

Part: STRUCTURE — CRACKED (ZONE 800) · airframe 48,962 hrs · 33,039 cycles

ZONE 500 RACK, AFT CARGO DOOR INTERNAL AFT LOWER CORNER HAS A CRACK. REPAIRED CRACK ON AFT CARGO DOOR INTERNAL AFT LOWER CORNER BY CUTTING OUT CRACKED AREA AND INSTALLING A DOUBLER AND FILLER.

Part: WINGLET — CORRODED (ZONE 500) · corrosion level 2 · airframe 48,962 hrs · 33,039 cycles

UPON REMOVAL OF TOP STATIC DISCHARGER BASE ON LH WINGLET FOUND CORROSION AND MATERIAL MISSING. REMOVED AND REPLACED WINGLET ON RACK.

Part: SILL DRAIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 48,962 hrs · 33,039 cycles

CORROSION ON MOP SILL FRAMES 42-49 STR 16R. REMOVED CORRODED MOP SILL AND INSTALLATION OF NEW MOP SILL LOCATED AT FR 42-49 STGR 16L

Part: SEAL — DAMAGED (ZONE 500) · airframe 48,962 hrs · 33,039 cycles

SEAL DAMAGE TO THE LH UPPER AILERON SHROUD. REMOVED AND REPLACED SEAL ON THE LH UPPER AILERON SHROUD .

Part: GUSSET — CORRODED (ZONE 200) · corrosion level 2 · airframe 48,962 hrs · 33,039 cycles

RH AFT SERVICE DOOR SIDEWALL GUSSET AT FR 23, STR 6R HAS CORROSION. INSTALLED NEW RH SERVICE DOOR AFT SIDEWALL GUSSET AT FR 23 STR 6R

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 48,962 hrs · 33,039 cycles

CORROSION ON FLOOR BEAM FRAME 37 TO 38 STR 16L. REMOVED AND REPLACED OF FLOOR SILL BETWEEN FRAMES 35-39, STRINGER 16L

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 48,962 hrs · 33,039 cycles

CORROSION FRAME 18 STR 18R. REMOVED AND REPLACED DOUBLER AT FRAME 18 STR 18R.

Part: SILL DRAIN — CORRODED (ZONE 200) · corrosion level 2 · airframe 48,962 hrs · 33,039 cycles

LEFT MOP SILL AT FR 35 TO FR 34, STR 6L HAS CORROSION. LT MOP SILL AT FR34 TO FR33, STR 6L HAS CORROSION. LT MOP SILL AT FR 31, STR 6L HAS CORROSION. INSTALLED NEW MOP SILL AT FR30-FR35 STR 16L

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 48,962 hrs · 33,039 cycles

SURFACE CORROSION LOCATION: FLOOR BEAM, CENTER ISLE, UNDER PANEL 231FF. INSTALLED NEW FLOOR BEAM, CENTER AISLE, UNDER PANEL 231FF

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 48,962 hrs · 33,039 cycles

RH FLOOR GUSSET AT FR 35, STR 4R IS BENT WITH DAMAGED FASTENER HEADS. REMOVED RH FLOOR GUSSET AT FR35, STR 4R DOUBLER AND REPLACED.

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 48,962 hrs · 33,039 cycles

CORROSION FRAME 20 STR 18. INSTALLED NEW DOUBLER AT FRAME 20 STR 18

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 48,962 hrs · 33,039 cycles

CORROSION ON FLOOR BEAMS FRAME 44-45 AT STR 16L. REMOVED MOP SILL FROM FR 42 TO FR 48 AND REPLACED WITH NEW.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 48,962 hrs · 33,039 cycles

LH FLOOR BEAM AT FR61 STR 4L HAS CORROSION. INSTALLED NEW FROM STOCK LH FLOOR BEAM GUSSET PLATE AT FR 61.

Part: SILL DRAIN — CORRODED (ZONE 200) · corrosion level 2 · airframe 48,962 hrs · 33,039 cycles

RH MOP SILL, FWD SECTION, AT FR 24 STR 6R HAS CORROSION. INSTALLED NEW MOP SILL, FWD SECTION AT FR 24, FR 25, AND FR 26 STR 6R.

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 48,962 hrs · 33,039 cycles

CORROSION FRAME 15 STR 21R. REMOVED CORROSION AND INSTALLED DOUBLER REPAIR

Part: SILL DRAIN — CORRODED (ZONE 200) · corrosion level 2 · airframe 48,962 hrs · 33,039 cycles

CORROSION ON THE MOP SILL FRAME 29 AT STR 16. REMOVED AND INSTALLED NEW RH FLOOR SILL AT FR 35-39

Part: STRAP — CRACKED (ZONE 200) · airframe 48,962 hrs · 33,039 cycles

CRACK ALONG FASTENER HOLE IN PANEL 195EL UPPER RETAINING STRAP AT FRAME 41. REMOVED AND REPLACED PANEL 195EL UPPER RETAINING STRAP AT FRAME 41.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 48,962 hrs · 33,039 cycles

LH OMEGA BEAM HAS MULTIPLE AREAS OF CORROSION. PERFORMED BLEND OUT PROCEDURE ON 3 LOCATIONS ON THE LH OMEGA BEAM BETWEEN FR 58 TO FR 61

Part: STRAP — CRACKED (ZONE 200) · airframe 48,962 hrs · 33,039 cycles

CRACK ALONGSIDE FASTENER HOLE IN PANEL 194ER UPPER RETAINING STRAP AT FRAME 48. REMOVED DAMAGED STRAP AND INSTALLED NEW UPPER RETAINING STRAP FOR PANEL 194ER AT FRAME 48.

Part: FLOOR SUPPORT — WORN (ZONE 200) · airframe 48,962 hrs · 33,039 cycles

BARE METAL. LOCATION: CABIN UNDER FLOOR PANEL 231HF. REMOVED AND REPLACED FLOOR SILL AT FR 24.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 48,962 hrs · 33,039 cycles

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

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 48,962 hrs · 33,039 cycles

MID FLOOR BEAM AT FR 61, STR 1R HAS CORROSION. REMOVED DAMAGED GUSSET AND INSTALLED NEW MID FLOOR BEAM GUSSET PLATE AT FR61

Part: GUSSET — CORRODED (ZONE 100) · corrosion level 2 · airframe 48,962 hrs · 33,039 cycles

CORROSION AT FRAME 20 STR 21R. REMOVED AND REPLACED GUSSET AT FR 18 TO FR 24

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 48,962 hrs · 33,039 cycles

SURFACE CORROSION LOCATION: FLOOR BEAM, UNDER PANEL 231HF ZONE 140-142. REMOVED DAMAGED LH FLOOR SILL FROM FR 19-23 AND INSTALLED NEW FLOOR SILL.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 48,962 hrs · 33,039 cycles

CORROSION FOUND UNDERNEATH FLOORBOARD 232DF AT FRAME 17 RIGHT ON THE GUSSET. INSTALLED NEW FROM STOCK GUSSET (145-21725-025) AFT OF SERVICE DOOR AND UNDERNEATH FLOORBOARD 232DF.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 48,962 hrs · 33,039 cycles

CORROSION FOUND ON SEAT TRACK MEGA BIN STRUCTURE ( UNDERNEATH FLOORBOARD 232DF) BETWEEN FRAMES 25 AND 30 ). REMOVED GUSSET AND INSTALLED NEW FROM STOCK GUSSET ON OMEGA BEAM STRUCTURE UNDERNEATH FLOORBOARD 242DF BETWEEN FR 30 AND FR 35

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 48,962 hrs · 33,039 cycles

SURFACE CORROSION FLOORBEAM. LOCATION: 232BF. (FWD SERVICE DOOR AREA) REMOVED 1EA DAMAGED FLOOR RECESS ( ON 145-22466-009 ), INSTALLED 1EA NEW FLOOR RECESS UNDER FOOR PANEL 232BF( PN 145-22466-009 )

Part: SILL DRAIN — CORRODED (ZONE 200) · corrosion level 2 · airframe 48,962 hrs · 33,039 cycles

RH MOP SILL FWD SECTION AT FR 53 HAS CORROSION, INSTALLED NEW FROM STOCK R/H FLOOR SILL(P/N:145-29495-005) AT FR53 TO FR59

Part: FLOOR PANEL — CORRODED (ZONE 200) · corrosion level 2 · airframe 48,962 hrs · 33,039 cycles

PANEL 197AB HAS CORROSION ON TAB. REMOVED DAMAGED TAB ON PENAL 197AB AND REPLACED WITH NEW

Part: BRACKET — CRACKED (ZONE 200) · airframe 48,962 hrs · 33,039 cycles

1 EA BRACKET FOR AIR PRESSURE LINES AT FR 51, RH, STR 6R, IS CRACKED, MARKED. REMOVED AND REPLACED 1EA. DISCREPANT BRACKECT ( PN 145-26345-401) @FS 51 STR 16 R

Part: SILL DRAIN — CORRODED (ZONE 200) · corrosion level 2 · airframe 48,962 hrs · 33,039 cycles

RH MOP SILL AT FR 54 TO 55, RH, HAS CORROSION, MARKED. INSTALLED NEW FROM STOCK R/H FLOOR SILL(P/N:145-29495-005) AT FR53 TO FR59

Part: LAMP — INOPERATIVE (ZONE 200) · airframe 48,805 hrs · 32,885 cycles

LH LATERAL WTF FAIRING EMERGENCY LIGHT OUT. REMOVED AND REPLACED LAMP. OPS CHECK GOOD

Part: DOOR — STUCK (EMERGENCY EXIT) · airframe 47,429 hrs · 31,550 cycles

PASSENGER EMERGENCY DOOR JAMMED CLOSED AND WOULD NOT OPEN CORRECTLY. REMOVED SIDEWALL PANEL SURROUNDING RH EMERGENCY ESCAPE DOOR AND RENINSTALLED CORRECTLY. REMOVED BOTH EMERGENCY ESCAPE WINDOWS. REMOUNTED BOTH EMERGENCY ESCAPE WINDOW SHADE ASSEMBLIES. INSTALLED LH EMERGENCY ESCAPE WINDOW. INSTALLED RH ESCAPE WINDOW LINER AND INSTALLED LH EMERGENCY ESCAPE WINDOW. OPS CHECK OF LH AND RH ESCAPE WINDOW GOOD

Part: ROLLER — LACK OF LUBE (ZONE 800) · airframe 47,159 hrs · 31,290 cycles

MCD DIFFICULT DOOR HARD TO OPEN FROM INSIDE. LUBED MCD ROLLERS AND STOPS. OPS CHECK GOOD

Part: LAMP — INOPERATIVE (UNKNOWN) · airframe 4,623,029 hrs · 30,440 cycles

LEFT WING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT BULB FOR LH WING. OPS CHECK SAT.

Part: INVERTER — INOPERATIVE · airframe 44,983 hrs · 29,325 cycles

EMERGENCY LIGHT ABOVE FA JUMP SEAT INOPERATIVE, EXIT LIGHT. REMOVED AND REPLACED DC/AC INVERTER. OPS CHECK SAT.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 44,930 hrs · 29,270 cycles

FWD MOST CEILING LINING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED FORWARD AISLE CEILING EMERGENCY LIGHT BULB. OPS CHECK GOOD.

Part: BULB — DIM (EMERGENCY LIGHT) · airframe 44,930 hrs · 29,270 cycles

MAIN DOOR EMERGENCY LIGHT IS DIM AND FLICKERS. REMOVED AND REPLACED MAIN DOOR EMERGENCY LIGHT BULB. OPS CHECK GOOD

Part: NONE — NONE · airframe 44,074 hrs · 28,513 cycles

AT REAR FUSE II EXT, SUSPECTED CRACKS (9X) FOUND ON RIGHT SIDE SKIN BTW FR 77 - FR 78 AND BTW STR 3R - 9R. REPAIR DOUBLER ON RH REAR FUSE 2 SKIN, ON FR 78 BTW STR 5R-7R. EXTERNAL DETAILED VISUAL INSPECTION, AT REPAIR, INTERVAL OF 30000 FC

Part: NONE — NONE · airframe 44,074 hrs · 28,513 cycles

AT REAR FUSE II EXT, SUSPECTED CRACKS (14X) FOUND ON LH SIDE SKIN BTW FR 77-80 AND BTW STR 3R-9R. 7 BUSHING REPAIRS ON LH REAR FUSE 2 SKIN, AT FR 77-79 AND BTW STR 3L-9L. EXTERNAL GVI, AT REAPIR, INTERVAL OF 9000 FC

Part: NONE — NONE · airframe 44,074 hrs · 28,513 cycles

DENT ON WING ROOT INSIDRE OF DENT ALREADY MAPPED ON LEADING EDGE. REPAIR DOUBLER ON LH WING LEADING EDGE #1, ON NOSE SECTION BTW INBD EDGE - RIB STA YS723.7

Part: NONE — NONE · corrosion level 2 · airframe 44,074 hrs · 28,513 cycles

CENTER FLOOR SUPPORT GUSSET CORRODED BTW FRA 59 & 61. REPAIR DOUBLER ON CENTER FUSE 4, ON CENTER OMEGA BEAM BTW FR 60-61

Part: NONE — NONE · airframe 44,074 hrs · 28,513 cycles

FR 25 CRACKED SIDE BEHIND RH SILL BTW STR 15R-16R. EXTENDED SPLICE REPAIR ON RH CENTER FUSE 2 FRAME 25, BTW STR 14R-16R. INTERNAL DETAILED VISUAL INSPECTION, AT REPAIR, INTERVAL OF 10000 FC

Part: NONE — NONE · airframe 44,074 hrs · 28,513 cycles

EXTERNAL FWD VENTRAL TANK DRAIN VENT SKIN CORRODED. REPAIR DOUBLER ON CENTER FUSE VENTRAL TANK RIB 1

Part: NONE — NONE · airframe 44,074 hrs · 28,513 cycles

SHEAR CLIP FOUND CRACKED AT RH FR 68 BTW STR 6-10. SHEAR CLIP AT FR 68 RH BTW STR 6-10 REPLACED WITH MADE REPAIR PART AND MASTER PART

Part: NONE — NONE · airframe 44,074 hrs · 28,513 cycles

SHEAR CLIP FOUND CRACKED AT FR 71 LH BTW STR 6-10. SHEAR CLIP AT FR71 LH BTW STR 6-10 REPALCED WITH MADE REPAIR PART.

Part: NONE — NONE · airframe 44,074 hrs · 28,513 cycles

AT REAR FUSE I EXT, CRACK FOUND ON RH TOP SKIN AT FR 75 AND BTW STR 1R-3R. CRACK ON RH TOP SKIN AT FR75 AND BTW STR 1R AND 3R REPAIRED WITH DOUBLER.

Part: BATTERY PACK — INOPERATIVE · airframe 43,610 hrs · 28,112 cycles

FWD EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY BATTERY PACK. OPS CHECK SAT

Part: UNKNOWN — ODOR (COCKPIT) · airframe 43,562 hrs · 28,061 cycles

ELECTRICAL SMELL IN COCKPIT DURING TAKEOFF AND CLIMB PHASES. OPS CHECK FAILED FOR PACK 1 HAD OVERHEAT MESSAGE DURING PACK 1 POWER RUNS ALTHOUGH NO ELECTRICAL SMELLS. NO CMC MESSAGES FOUND AT THIS TIME. PERFORMED HIGH POWER RUNS WITH PACK 2 WITH NO SMELLS OR MESSAGES.

Part: NONE — NONE · airframe 43,505 hrs · 28,012 cycles

EXIT ROW ARROW POINTED WRONG DIRECTION. RR LH LOWER EXIT SIGN ON ROW 18A. OPS CHECK SAT

Part: ARMREST — CRACKED (SEAT 10A) · airframe 42,530 hrs · 27,140 cycles

FOUND CRACK IN PAX SEAT ARMREST AT 10A. RR PAX SEAT 10A.

Part: PLACARD — MISLOCATED (CABIN) · airframe 41,636 hrs · 29,296 cycles

EMERGENCY FLOOR SAF-T-GLO EXIT PLACARDS AT ROW 21A AND 21CD ARE WRONG, NEEDS TO BE EXCHANGED WITH ROW 24A AND 24CD. RE-POSITIONED EXIT PLACARDS ON FLOOR PATH STRIPS.

Part: LAMP — INOPERATIVE (INSTRUMENT PANEL) · airframe 41,636 hrs · 26,296 cycles

MULTIPLE LIGHTS INOPERATIVE ON FLIGHT GUIDANCE CONTROLLER BUTTONS. R&R INOPERATIVE LAMPS ON FLIGHT GUIDANCE CONTROLLER. OPS CHECK SAT

Part: LIGHT — DETACHED (CABIN) · airframe 39,986 hrs · 24,792 cycles

EMERGENCY EXIT AT 1/2A FALLING DOWN. SECURED THE EMERGENCY SIGN AT 1/2A.

Part: CONTACT — DIRTY (EMERGENCY LIGHT) · airframe 39,755 hrs · 24,590 cycles

MAIN DOOR EXTERNAL EMERGENCY LIGHT INOPERATIVE. FOUND EMERGENCY LIGHT GROUNDING CABLE CONTACT TO BE DIRTY. CLEANED THE CONTACT AS REQUIRED. OPS CHECK SAT.

Part: SWITCH — FAILED (RUDDER SYS) · airframe 39,665 hrs · 24,506 cycles

RUDDER SYS 1 & 2 INOP IN FLIGHT MULTIPLE TIMES. REMOVED AND INSTALLED PRESSURE RUDDER SWITCHES 1 AND 2.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,099 hrs · 24,001 cycles

BELOW APU DRAIN AT DATA PLATE ON EDGE HAS CORROSION AS MARKED. INSTALLED REPAIR DOUBLER AND FILLER BETWEEN FR 80-81 BELOW DATA PLATE.

Part: FITTING — CRACKED (FUSELAGE) · corrosion level 2 · airframe 39,099 hrs · 24,001 cycles

SHEAR CLIP CRACKED AT FR65 STR 17L AS MARKED. REMOVED AND REPLACED SHEAR CLIP AT FR 65 STR 17L.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,099 hrs · 24,001 cycles

LT OMEGA BEAM HAS CORRODED FASTENER ON INBD FACE AT FR 20, AT RAMP ANGLE. INSTALLED EXTERNAL ANGLE, FILLER AND SHIM FOR LT OMEGA BEAM REPAIR ON INBD FACE AT FR 20.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,099 hrs · 24,001 cycles

RT OMEGA BEAM HAS CORROSION AT FASTENER HOLE AT FR 23. INSTALLED REPAIR DOUBLER ON RT OMEGA BEAM AT FR 23.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 39,099 hrs · 24,001 cycles

STRINGER COASTAL HAS CRACK AT STRINGER 3L FR20. REMOVED AND REPLACED STRINGER COASTAL AT STRINGER 3L FR20.

Part: SUPPORT — CRACKED (FUSELAGE) · corrosion level 2 · airframe 39,099 hrs · 24,001 cycles

OMEGA BEAM SUPPORT CRACK FOUND FRAME 47-48 LEFT SIDE OMEGA BEAM AS MARKED. INSTALLED NEW OMEGA BEAM SUPPORT AT FRAME 47-48 LEFT SIDE.

Part: ANGLE — CRACKED (LT MLG DOOR) · airframe 39,099 hrs · 24,001 cycles

LH MLG AUX DOOR ANGLE CRACKED AS MARKED. THERE IS A 3" CRACK IN THE RADIUS OF THE LH MLG AUX DOOR STIFFENER. PREPPED, PRIMED, AND PAINTED LH MLG AUX DOOR REPAIR.

Part: BEAM — CORRODED (THRESHOLD) · corrosion level 2 · airframe 39,099 hrs · 24,001 cycles

CORROSION-SERVICE DOOR THRESHOLD BEAM HAS CORROSION AT 3 FASTENER HOLES. REMOVED AND REPLACED FWD SERVICE DOOR BEAM. CORROSION FOUND TO BE LEVEL 2.

Part: LIGHT — MISSING (CABIN) · airframe 39,099 hrs · 24,001 cycles

CABIN EMERGENCY LIGHT STRIP 5LH MISSING 1 SEGMENT OF THE PHOTO LUMINESCENT STRIP. REMOVED AND REPLACED #5 PHOTO LUMINESCENT FLOOR-PROXIMITY STRIP LIGHT ASSEMBLY.

Part: COVER — CRACKED (EMERGENCY LIGHT) · airframe 39,099 hrs · 24,001 cycles

CABIN 1 LH EMERGENCY LIGHT STRIP PLASTIC COVER CRACKED. REMOVED AND REPLACED CRACKED #1 LH PHOTO LUMINESCENT FLOOR PROXIMITY STRIP LIGHT ASSEMBLY.

Part: COVER — CRACKED (EMERGENCY LIGHT) · airframe 39,099 hrs · 24,001 cycles

CABIN EMERGENCY LIGHT STRIP 1RH PLASTIC IS CRACKED AND PHOTO LUMINESCENT STRIP IS FADED. REMOVED AND REPLACED CRACKED AND FADED #1 RH PHOTO LUMINESCENT FLOOR PROXIMITY STRIP LIGHT ASSEMBLY.

Part: SEAL — DAMAGED (PANEL) · airframe 39,099 hrs · 24,001 cycles

PANELS 155BZ AND 156BZ HAVE DAMAGED MESH SEALS. REMOVED AND REPLACED PANELS 155BZ AND 156BZ MESH SEALS ON RACK.

Part: FLOOR SUPPORT — CORRODED (FRAME 18) · airframe 39,099 hrs · 24,001 cycles

CORROSION - RH O-MEGA BEAM HAS CORRODED FASTENER HOLE AT FR 18. REMOVED CORROSION ON FASTENER HOLE FR 18 R/H O-MEGA BEAM. MAT. LOSS 0.019" FOUND TO BE OUT OF LIMITS. CUTOUT DAMAGED AREA ON R/H OMEGA BEAM FR 18. HFEC INSPECTED CUTOUT. REQUESTED VERIFICATION OF MATERIAL FOR FABRICATION OF DOUBLER FOR CUTOUT ON R/H OMEGA BEAM, 2024T3 0.050". APPLIED TREAT, PRIME AND TOP COAT TO CUTOUT AREA ON R/H OMEGA BEAM ON FR 18. FABRICATED, DRILLED, TREATED, AND PRIMED DOUBLER FOR R/H OMEGA BEAM FR 18. PERFORMED POST REMOVAL INSPECTION, NO DEFECTS NOTED. INSTALLED TOP COATED DOUBLER FOR R/H OMEGA BEAM OF FR 18.

Part: RIB — CRACKED (WNG-BDY FAIRING) · airframe 39,057 hrs · 23,958 cycles

CRACKED RIB END ON AFT WING-TO-FUSELAGE FAIRING SUPPORT IN LH MLG WELL. FOUND ADDITIONAL CRACK IN FAIRING SUPPORT WEB STOP-DRILLED CRACK ENDS OF FAIRING SUPPORT WEB. PERFORMED NDI USING 30X MAGNIFIER AND FOUND NO FURTHER CRACKING. RIB END REPLACEMENT AND DEFERRAL OF PERMANENT REPAIR STILL REQUIRED.

Part: SCREW — MISSING (EXIT SIGN) · airframe 38,954 hrs · 23,857 cycles

EMERGENCY SIGN OVER FA JUMPSEAT BROKEN. FOUND SCREW MISSING AND INSTALLED NEW SCREW, OPS CK SAT. NO DE3FECTS NOTED.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 36,948 hrs · 21,816 cycles

EMERGENCY LIGHT BY MAIN DOOR AND VARIOUS CEILING EMERGENCY LIGHTS INOPERATIVE. R & R THE NR 1 AND 2 EMERGENCY LIGHTS BATTERIES.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 34,484 hrs · 19,886 cycles

THE CREW REPORTED THAT THE EMERGENCY LIGHTS WERE NOT WORKING PROPERLY. MAINTENANCE INSPECTED THE ACFT AND R & R THE EMERGENCY LIGHT BATTERY PACK IN THE GALLEY. OPS CHECKS WERE PERFORMED WITH NO DEFECTS NOTED AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONTROL MODULE — FAULTY (CABIN LIGHTS) · airframe 32,735 hrs · 18,642 cycles

CREW REPORTED EMERGENCY LIGHT NOT ARMED MESSAGE ON EICAS WITH SWITCH IN NORMAL POSITION. MX R & R THE CABIN LIGHTS CONTROL MODULE WITH OPS CHECK GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONTROL MODULE — ODOR (CABIN LIGHTS) · airframe 32,733 hrs · 18,640 cycles

CREW REPORTED APPREARS TO BE AN ELECTRICAL BURNING ODOR IN GALLEY AREA. MX R & R THE CABIN LIGHTS CONTROL MODULE, SIDEWALL LIGHT HARNESS AT SEAT 1A, AND LIGHT BULBS. OPS CHECK GOOD. ACFT WAS APRROVED TO RETURN TO SERVICE.

Part: CONTROLLER — FAULTY (CABIN PRESSURE) · airframe 31,634 hrs · 17,909 cycles

THE CREW REPORTED AT 36000 FT ERRATIC CABIN ALTITUDE OF 8100 FT AND CLIMBING. WENT AMBER AND WENT UP TO 8800FT. WENT TO MANUAL MODE AND WASN'T ABLE TO CONTROL IT BACK TO WITHIN TOLLERANCES. EMERGENCY DESCENT TO 10000 FT THE CREW ALSO REPORTED SECTION OF MAIN CABIN DOOR SEAL WAS MISSING. MAINTENANCE REPLACED THE AUTO PRESSURIZATION CONTROLLER AND REPAIRED MAIN CABIN DOOR SEAL. OPS CHECKED GOOD.

Part: SKIN — CRACKED (FRAME 80) · airframe 29,758 hrs · 16,680 cycles

DURING C-CK. LT FUSELAGE SKIN CRACKED AROUND RIVETS AT FRAME 80. REPAIRED SKIN IAW EC5330-02879. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SUPPORT — CORRODED (FRAMES 65-68) · airframe 29,758 hrs · 16,680 cycles

DURING C-CHECK. CARGO DOOR LOWER CUT OUT CORRODED. R & R CARGO DOOR LOWER CUT OUT SUPPORT IAW SRM 51-40-02. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FRAMES 23-30) · airframe 29,758 hrs · 16,680 cycles

DURING C-CHECK. LT OMEGA BEAM CORRODED BETWEEN FRAMES 23-30. REPAIRED LT OMEGA BEAM IAW SRM 53-21-10. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FRAMES 45-53) · airframe 29,785 hrs · 16,680 cycles

DURING C-CHECK, LEFT OMEGA BEAM CORRODED BETWEEN FRAME 45-53. REPAIRED LEFT OMEGA BEAM IAW EC5320-01914. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 24,076 hrs · 13,023 cycles

CRACKED SHEAR FOOT AT FRAME 73 AT THE 9 O'CLOCK POSITION AT STR 8R AND 9R. R & R SHEAR FOOT.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 24,076 hrs · 13,023 cycles

SHEAR FOOT CRACKED AT FRAME 73 AT THE 9 O'CLOCK POSITION AT STR 8R AND 9R. R & R SHEAR FOOT.

Part: SILL — CORRODED · corrosion level 2 · airframe 24,076 hrs · 13,023 cycles

RT FWD SERVICE DOOR SILL CORRODED, BEYOND LIMITS AFTER BLENDING. R & R SILL.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,076 hrs · 13,023 cycles

RIGHT FWD SERVICE DOOR SILL CORRODED. BLENDED CORROSION AND FOUND OUT OF LIMITS. R & R SILL.

Part: POWER SUPPLY — INOPERATIVE (ZONE 200) · airframe 23,306 hrs · 12,564 cycles

DURING ROUTINE SCHEDULED MX, FOUND THE EMERGENCY EXIT LIGHTS ON MAIN CABIN DOOR, COCKPIT CEILING AND STEP, AND GALLEY EXIT SIGN WOULD NOT ILLUMINATE. MX R & R NR 1 EMERGENCY LIGHT POWER SUPPLY AND BATTERY ALONG WITH NR 2 EMERGENCY LIGHT BATTERY IAW AMM 33-50-04 WITH OPS CHECKS SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 20,380 hrs · 10,828 cycles

LIGHTNING STRIKE BURN MARK 20 INCHES AFT OF FORWARD JACK POINT PAD AND LS DAMAGE BETWEEN FRAME 26 AND 27 ON STRINGER 17L. CUT OUT DAMAGE, FABRICATED DOUBLER AND FILLER. INSTALLED, PRIMED AND PAINTED IAW ETD2010-145/11244 AND 135/145 SRM 53-22-01.

Part: COUPLING — BLOWN (AC BAY) · airframe 20,345 hrs · 10,810 cycles

IAH - FLIGHT 2184, THE CREW REPORTED A PACK ONE VALVE CLOSED MESSAGE DURING CLIMB. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE ACM BLEED COUPLINGS ON THE LEFT ACM, OPERATIONALLY AND LEAK CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 20,163 hrs · 10,712 cycles

TYS - A/C WAS IN CLT WHEN THE CREW GOT A NR 3 EMERGENCY LIGHT BATTERY INOP MESSAGE. MAINTENANCE REMOVED AND REPLACED THE NR 3 EMERGENCY BATTERY IAW EMB 145AMM 33-50-04. OPS CHECK GOOD AND WAS RELEASED.

Part: MOUNT FLANGE — CORRODED (NACELLE) · airframe 19,076 hrs · 10,103 cycles

NR 1 ENG INLET MOUNTING FLANGE HOLES CORRODED. REPAIRED INLET HOLES IAW EC5420-01158. AIRCRAFT CURRENTLY IN C CHECK.

Part: CAP — CORRODED (FUSELAGE) · airframe 19,076 hrs · 10,103 cycles

LAV CENTER CAP IS CORRODED AROUND FASTENER HOLE AS MARKED. REMOVED AND REPLACED CENTER TOP CAP IAW EMB 145 SRM 51-40-02.

Part: RIB — BURNED (ZONE 300) · airframe 14,735 hrs · 7,788 cycles

RT ELEVATOR TIP FAIRING SUPPORT NUT PLATE FASTENER HOLE WAS ELONGATED FROM A LIGHTNING STRIKE. THE DAMAGED TIP WAS CUT OUT AND A FILLER AND DOUBLER WERE FABRICATED AND INSTALLED IAW EC5520-01162. THE ELEVATOR WAS REMOVED, BALANCED, AND INSTALLED IAW EMB AMM 27-30-00.

Part: DOOR FRAME — CORRODED (FUSELAGE)

DURING C-CHECK MAIN DOOR STRUCTURE HAS CORROSION AROUND LOWER NUTPLATE HOLE. MX REPAIRED MAIN DOOR LOWER NUT PLATE HOLES IAW EC 5210-01154. THE ACFT WAS APPROVED TO RETURN FOR SERVICE. (K)

Part: HINGE — DAMAGED (SERVICE DOOR)

DURING C-CHECK, SERVICE DOOR UPPER HINGE AT FUSELAGE HAS MIGRATED HAT BUSHING. MX REMOVED AND REPLACED SERVICE DOOR UPPER HINGE AT FUSELAGE HAT BUSHING IAW EC5240-01036. THE ACFT WAS APPROVED TO RETURN FOR SERVICE. (K)

Part: INVERTER — INOPERATIVE (CABIN) · airframe 14,137 hrs · 7,439 cycles

IAH FLIGHT 2073 THE CREW REPORTED THAT THE RT EMERGENCY LIGHT STRIP WAS INOPERATIVE. MX R&R THE NR 4 INVERTER. OPS CHECKED WITH NO DEFECTS AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PROXIMITY SENSOR — INOPERATIVE (RT MLG)

IAH FLIGHT 2097 - THE CREW REPORTED LG AIR/GND FAIL AFTER TO COULD NOT MOVE GEAR LEVER HANDLE INTO UP POSITION. THE ACFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED NR 2 PROX SWITCH ON RT GEAR PER EMB -145 MM 32-61-01. OPS CHECK GOOD, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. (S)

Part: WIRE — BROKEN (LT MLG)

IAH - FLIGHT 2110, THE CREW REPORTED A LANDING GEAR AIR/GRND FAIL. THE ACFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REPAIRED A BROKEN WIRE ON CONNECTOR P0045. OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. (S)

Part: LANDING GEAR — MALFUNCTIONED · airframe 13,698 hrs · 7,203 cycles

PHX - FLIGHT 2899, THE CREW REPORTED A LANDING GEAR AIR GROUND FAIL MESSAGE ON CLIMB AND THE GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO PHX WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, RESET THE AIR GROUND SYSTEM, OPERATIONALLY CHECKED WITH NO DEFECTS AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (A)

Part: ENGINE — OVERTEMP (NR 1)

CLE FLIGHT 2531 - THE CREW REPORTED ENGINE NR 1 HP INDICATION IN YELLOW RANGE AFTER TAKEOFF. THE AIRCRAFT RETURNED TO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NR 1 ENGINE. OPERATIONAL CHECKS WERE GOOD. SUPPLEMENT TO FOLLOW. (A)

Part: ELECTRONIC UNIT — INOPERATIVE (MLG) · airframe 11,009 hrs · 5,825 cycles

TUS - FLIGHT 3150, THE CREW REPORTED AN AIR/GRND FAILURE INDICATION AFTER TAKEOFF. THE AIRCRAFT RETURNED TO TUS WHERE IT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS INSPECTED FOR THE PURPOSES OF A FERRY FLIGHT, AND WAS FERRIED IAH WHERE MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR ELECTRONIC UNIT, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ENGINE — SHUTDOWN (NR 2) · airframe 10,685 hrs · 2,660 cycles

OKC - FLIGHT 2726, THE CREW REPORTED THAT THE NUMBER TWO ENGINE SHUTDOWN IN FLIGHT. THE AIRCRAFT LANDED IN OKC WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO ENGINE, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. OPEN