N14153

Part: GUSSET — CORRODED (ZONE 200) · corrosion level 2 · airframe 48,728 hrs · 32,921 cycles

CORROSION ON GUSSET AT FRAME 16 RBL 4. REMOVED CORROSION ON GUSSET AT FRAME 16 RBL 4 GUSSET FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED GUSSET FROM FRAME 16 RBL 4.

Part: GUSSET — CORRODED (ZONE 200) · corrosion level 2 · airframe 48,728 hrs · 32,921 cycles

CENTER OMEGA BEAM GUSSET FROM FRAME 22 TO FRAME 27 IS CORRODED. CENTER OMEGA BEAM GUSSET AT FRAME 22 - FRAME 27 FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED CENTER OMEGA BEAM GUSSET.

Part: GUSSET — CORRODED (ZONE 200) · corrosion level 2 · airframe 48,728 hrs · 32,921 cycles

GUSSET AT FRM 20 RBL 19 IS CORRODED. REMOVED CORROSION FROM FRAME 20 RBL 19, FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED GUSSET.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 48,728 hrs · 32,921 cycles

RH #1 OB FLOORSILL IS CORRODED. REMOVED AND INSTALLED NEW RH #1 OB FLOORSILL.

Part: RIB — CRACKED (ZONE 100) · airframe 48,728 hrs · 32,921 cycles

LH AFT MLG WHEEL WELL RIB CRACKED AT UPPER OUTBD CORNER. REMOVED AND REPLACED LH AFT MLG WHEEL WELL RIB.

Part: GUSSET — CORRODED (ZONE 900) · corrosion level 2 · airframe 48,728 hrs · 32,921 cycles

UNDER LAV ALL 3 GUSSETS ARE CORRODED. REMOVED TWO CORRODED GUSSETS UNDER LAV AND INSTALLED NEW GUSSETS.

Part: GUSSET — CORRODED (ZONE 900) · corrosion level 2 · airframe 48,728 hrs · 32,921 cycles

LH IB AND OB GUSSETS UNDER LAV SINK ARE CORRODED. REMOVED LH IB AND OB GUSSETS UNDER LAV SINK AND INSTALLED NEW GUSSETS.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 48,728 hrs · 32,921 cycles

FLOORSILL IN CARGO MOST FWD SILL IS CORRODED. REMOVED MOST FORWARD FLOORSILL IN CARGO BAY ON LEFT SIDE AND INSTALLED NEW FLOORSILL.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 48,728 hrs · 32,921 cycles

RH FLOORSILL MOST FWD IN CARGO IS CORRODED. REMOVED RH MOST FORWARD FLOORSILL IN CARGO BAY AND INSTALLED NEW SILL AND PROFILE.

Part: ENGINE — SHUTDOWN (LEFT) · airframe 48,248 hrs · 32,482 cycles

E-1 AUTO SHUTDOWN ON FINAL. REMOVED AND REPLACED LH ENGINE. OPS AND LEAK CHECK SAT.

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 47,458 hrs · 31,742 cycles

SEVERAL PHOTO-LUMINESCENT STRIPS NOT ILLUMINATING IN AFT CABIN. PERFORMED OPERATIONAL CHECK OF EMERGENCY LIGHTING AND PHOTO-LUMINESCENT STRIPS. OPS CHECK GOOD.

Part: PUMP — INOPERATIVE (NR 1 HYD SYSTEM) · airframe 46,674 hrs · 30,982 cycles

HYD 1 FAIL IN FLIGHT. REMOVED AND REPLACED #1 EDP AND REMOVED AND REPLACED 3 HYD FILTER ELEMENTS ON #1 HYD SYSTEM. PERFORMED HIGH ENGINE POWER RUNS. OPS AND LEAK CHECK SAT. NO DEFECTS NOTED. EXAMINED #1 HYD PRESSURE AND CASE DRAIN FILTERS WITH NO CONTAMINATION AND REMOVED AND REPLACED HYD FILTERS. OPS AND LEAK CHECK SAT.

Part: LAMP — INOPERATIVE (UNKNOWN) · airframe 46,288 hrs · 30,629 cycles

LH OVERWING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED BULB. OPS CHECK GOOD.

Part: PUMP — INOPERATIVE (UNKNOWN) · airframe 45,842 hrs · 30,207 cycles

HYD 1 LOW QUANTITY EICAS MESSAGE AFTER LANDING GEAR DEPLOYMENT. FLUID QTY READING IN YELLOW. REMOVED AND REPLACED RH MLG MANEUVERING ACTUATOR HOSES AND LH EDP. BLED AND SERVICED HYDRAULIC SYSTEM 1. OPS CHECK SAT. PERFORMED MULTIPLE LANDING GEAR SWINGS. OPS CHECK SAT. LEAK CHECK SAT.

Part: FUSE — INOPERATIVE · airframe 45,446 hrs · 29,824 cycles

LH EXTERNAL EMERGENCY FWD LIGHT INOPERATIVE. REPLACED LAMP OF LH FWD EMERGENCY LIGHT. NO FIX. EXTERNAL LIGHT HOUSING SUSPECT INOPERATIVE DUE TO CHAFFED WIRES. REMOVED AND REPLACED LH FWD EMERGENCY LIGHT ASSEMBLY. CHECKED CONTINUITY TO PINS FOR CANNON PLUG TO EMERGENCY LIGHT FOUND NO VOLTAGE. OPS CHECK FAILED. REMOVED AND REPLACED F1 FUSE ON BATTERY 1 POWER SUPPLY. OPS CHECK SAT. NO FURTHER DEFECTS AT THIS TIME.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 45,227 hrs · 29,639 cycles

ALL EMERGENCY LIGHTS TURN ON THEN IMMEDIATELY OFF. REMOVED AND REPLACED FOUR EMERGENCY LIGHT BATTERIES. OPS CHECK SAT.

Part: DAU — UNKNOWN · airframe 44,264 hrs · 28,774 cycles

SUPPLEMENTAL: FUEL QTY DISAGREE EICAS MSG.  AT CRUISE FL290  RECEIVED FUEL CONFIG DISAGREE FOLLOWED BY ENGINE #1 LOST INDICATION OF GEN 1 AND 3, ENGINE FUEL FLOW, ENGINE TEMPS, ENGINE OIL PRESSURE, AND ALL 3 GEAR INDICATIONS. CREW REPORTED THEY RAN QRH FOR FUEL FLOW PRESSURE AND ABNORMAL LANDING GEAR EXTENSION.

Part: NONE — INOPERATIVE · airframe 43,738 hrs · 28,302 cycles

PSU ATTENDANT CALL LIGHT AT SEAT ROW 18A NOT ILLUMINATED. PSU PRINTED CIRCUIT BOARD REPLACED

Part: NONE — NONE · corrosion level 2 · airframe 43,738 hrs · 28,302 cycles

AT REAR FUSE AREA, CORROSION FOUND ON FWD L-SHAPE CARGO DOOR SURROUND STRUCTURE AT FR65 AND BTW STR 16L-17L. AT REAR FUSE, AT FR65 BTW STR 16L-17L L-SHAPE IS OUT OF LIMITS. REPLACED WITH NEW PART SECTION AT REAR FUSE AREA ON FWD L-SHAPE CARGO DOOR SURROUND STRUCTURE AT FR 65 BTW STR 16L-17L AND REPROTECTION APPLY ON OUTER SKIN DOOR SURROUND BTW FR 65-FR 68

Part: NONE — NONE · corrosion level 2 · airframe 43,738 hrs · 28,302 cycles

CF1 REPAIR ON RH FLOOR BEAM AT FR 23 FOUND CORRODED. CF1 REPAIR ON RH FLOOR BEAM AT FR23 BLENDED OUT OF LIMITS. REMOVED CF1 REPAIR ON RH FLOOR BEAM AT FR23 FOR REPLACEMENT. FABRICATED REPAIR DOUBLER FOR RH FLOOR BEAM AT FR23. INSTALLED NEW FABRICATED REPAIR DOUBLER ON RH FLOOR BEAM AT FR23

Part: NONE — NONE · airframe 43,738 hrs · 28,302 cycles

AT CF IV AREA, CRACKS FOUND ON LH FRAME 59 BTW STR 15L-17L. LH SPLICE FR59 BTW STR 15L-17L REMOVED. AT CFIV AREA ON LH FRAME 59 BTW STR 15L-17L INSTALLED REPAIR SPLICE. DURING INSPECTION, FRAME REPAIR AND SPLICE FOUND TO BE FABRICATED WITH WRONG THICKNESS

Part: SMOKE DETECTOR — DAMAGED (LAVATORY) · airframe 42,706 hrs · 27,372 cycles

LAV SMOKE EICAS MESSAGE IN FLIGHT. FOUND LAV SMOKE DETECTOR CONTROL PANEL TO BE SMELLING BURNT. R&R LAV SMOKE DETECTOR CONTROL PANEL. OPS CHECK GOOD. (PN TRA72-20)

Part: SKIN — CORRODED (FRAMES 38-39) · airframe 41,253 hrs · 26,126 cycles

MAIN CABIN BELLY SKIN HAS CORROSION BETWEEN STR 21LH & 21RH BETWEEN FRAME 38 & 39- REMOVED CORROSION FROM BELLY OF FUSELAGE INTERNAL SKIN BETWEEN FR38-39, STR21L-21R, FABRICATED DOUBLER & BEGAN INSTALLATION. COMPLETED REPAIR ON MAIN BELLY SKIN AT FR 38-39 BETWEEN STR 21L & 21R, REMAINING THICKNESS 0.056".

Part: SUPPORT — CORRODED (FRAME 61) · airframe 41,253 hrs · 26,126 cycles

AFT LAV L/H SIDEWALL CARBON RING SUPPORT HAS CORROSION AT FR 61....R&R AFT LAV L/H SIDEWALL CARBON RING SUPPORT.

Part: SUPPORT — CORRODED (FRAME 61) · airframe 41,253 hrs · 26,126 cycles

AFT CARGO R/H SIDEWALL CARBON RING SUPPORT ABOVE R/H FLOOR SILL HAS CORROSION AT FR 61....R&R AFT CARGO R/H SIDEWALL SUPPORT FOR CARBON RING AT FR 61.

Part: SUPPORT — CRACKED (RT WING) · airframe 41,253 hrs · 26,126 cycles

RH WING L/E I/B HORSE SHOE NUTPLATE SUPPORT RING IS CRACKED IN BEND RADIUS- REMOVED & REPLACED RH WING I/B L/E HORSE SHOE, INSTALLED NEW NUTPLATES.

Part: FLOOR SUPPORT — CORRODED (FRAME 29) · airframe 41,253 hrs · 26,126 cycles

MAIN CABIN R/H FLOOR SILL HAS CORROSION ON UPPER SURFACE AT FR 29....R&R R/H FLOOR SILL AT FR 29.

Part: FLOOR SUPPORT — CORRODED (FRAME 30) · airframe 41,253 hrs · 26,126 cycles

MAIN CABIN RH FLOOR SILL HAS CORROSION ON UPPER SURFACE AT FRAME 30- REMOVED RH FLOOR SILL AT FRAME 30. INSTALLED RH FLOOR SILL AT FRAME 30.

Part: SUPPORT — CORRODED (FRAME 23) · airframe 41,253 hrs · 26,126 cycles

MAIN CABIN RH STEP UP SUPPORT AND CORNER SUPPORT AT FRAME 23 HAS CORROSION- R&R RH STEP UP SUPPORT AND CORNER SUPPORT AT FR 23.

Part: SUPPORT ANGLE — CRACKED (ZONE 100) · airframe 41,253 hrs · 26,126 cycles

RH I/B FIN UPPER RH ANGLE SUPPORT BRACKET IS CRACKED- REMOVED CRACKED ANGLE SUPPORT LOCATED & DRILLED UP NEW ANGLE SUPPORT BRACKET. INSTALLED NEW ANGLE SUPPORT BRACKET.

Part: FLOOR SUPPORT — CORRODED (FRAMES 36-37) · airframe 41,253 hrs · 26,126 cycles

MAIN CABIN CENTER OMEGA BEAM UPPER SUPPORT HAS CORROSION ON UPPER SURFACE BETWEEN FRAME 36 & 37- R&R MAIN CABIN CENTER OMEGA BEAM UPPER SUPPORT AT FR36 & 37.

Part: FLOOR SUPPORT — CORRODED (FRAME 44) · airframe 41,253 hrs · 26,126 cycles

MAIN CABIN RH FLOOR SILL HAS CORROSION ON UPPER SURFACE AT FRAME 44- REMOVED OLD FLOOR SILL. INSTALLED RH FLOOR SILL AT FR44, WAITING ON HI-LOK TO FINISH INSTALLATION. INSTALLED HI-LOKS AND FINISHED INSTALLING FL SILL.

Part: SHEAR TIE — CRACKED (FRAME 15) · airframe 41,253 hrs · 26,126 cycles

MAIN CABIN FR 15 R/H SHEER CLIP IS CRACKED AT STR 15 R/H....R&R MAIN CABIN FR 15 R/H SHEER CLIP AT STR 15 R/H.

Part: ANGLE — CRACKED (BELLY FAIRING) · airframe 41,253 hrs · 26,126 cycles

RH W/W FWD O/B CORNER BELLY FAIRING LOWER NUTPLATE L ANGLE SUPPORT IS CRACKED- REMOVED DAMAGED L ANGLE FABRICATED NEW L CHANNEL & DOUBLER. INSTALLED NEW L CHANNEL & DOUBLER.

Part: SKIN — GOUGED (FRAMES 67-68) · airframe 41,253 hrs · 26,126 cycles

#1 ENGINE PYLON INSIDE ACCESS PANEL 414DB FUSELAGE SKIN IS GOUGED BETWEEN FRAME 67 & 68- REMOVED #1 PYLON BLEED VALVE TO F.O.M. CUT OUT DAMAGED AREA, FABRICATED DOUBLER, DRILLED-UP, ALODINE & PRIMED NEW DOUBLER. FABRICATED FILLER, LOCATED, DRILLED, INSTALLED DOUBLER & FILLER. INSTALLED #1 PYLON BLEED VALVE, OPS CHECK REQUIRED. OPS CHECKED PERFORMED, OPS CHECK GOOD.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 41,253 hrs · 26,126 cycles

MAIN CABIN FRAME 27 SHEAR CLIP IS CRACKED AT STR 15 RH- R&R MAIN CABIN SHEAR CLIP AT FR 27 STR 15 ON RH SIDE.

Part: SHEAR TIE — CRACKED (FRAME 24) · airframe 41,253 hrs · 26,126 cycles

MAIN CABIN FRAME 24 SHEAR CLIP IS CRACKED AT STR 15 RH- R&R SHEAR CLIP AT FR 24 STR 15 RH.

Part: SHEAR TIE — CRACKED (FRAME 25) · airframe 41,253 hrs · 26,126 cycles

MAIN CABIN FRAME 25 SHEAR CLIP IS CRACKED AT STR 15 RH- R&R SHEAR CLIP AT FR 25, STR 15 RH.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 41,253 hrs · 26,126 cycles

MAIN CABIN RH OMEGA BEAM STOP SIGN HAS CORROSION AT FRAME 22- R&R MAIN CABIN RH OMEGA BEAM STOP SIGN AT FR22.

Part: FLOOR SUPPORT — CORRODED (FRAME 61) · airframe 41,253 hrs · 26,126 cycles

AFT LAV L/H FLOOR SILL HAVE CORROSION AROUND NUTPLATE HOLE AT FR 61....R&R AFT LAV L/H FLOOR SILL AT FR 61.

Part: FLOOR SUPPORT — CORRODED (FRAMES 28-31) · airframe 41,253 hrs · 26,126 cycles

MAIN CABIN L/H OMEGA BEAM UPPER SURFACE HAS LIGHT CORROSION AT FR 28 & 31....R&R L/H OMEGA BEAM GUSSET AT FR 28 TO 31.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 41,253 hrs · 26,126 cycles

MAIN CABIN RH FLOOR SILL HAS CORROSION AROUND NUTPLATE HOLE FWD OF SERVICE DOOR- R&R RH FLOOR SILL FWD OF SERVICE DOOR.

Part: FLOOR SUPPORT — CORRODED (FRAMES 22-23) · airframe 41,253 hrs · 26,126 cycles

MAIN CABIN RH FLOOR SILL HAS CORROSION AROUND NUTPLATE HOLES AT FRAME 22 & 23- R&R MAIN CABIN RH FLOOR SILL AT FR22-23.

Part: ANGLE — CRACKED (FRAMES 16-17) · airframe 41,253 hrs · 26,126 cycles

MAIN CABIN LH OMEGA BEAM LOWER I/B SPLICE ANGLE IS CRACKED BETWEEN FRAME 16 & 17- R/R LH OMEGA BEAM I/B SPLICE ANGLE BETWEEN FR16-FR17.

Part: ANGLE — CRACKED (FRAMES 16-17) · airframe 41,253 hrs · 26,126 cycles

MAIN CABIN LH OMEGA BEAM LOWER O/B SPLICE ANGLE CRACKED BETWEEN FRAME 16 & 17- R/R THE LH OMEGA BEAM LOWER O/B SPLICE ANGLE BETWEEN FR16-FR17.

Part: ANGLE — CRACKED (FRAME 67) · airframe 41,253 hrs · 26,126 cycles

AFT CARGO LOWER THRESHOLD 'T' PROFILE UPPER ANGLE BRACKET IS CRACKED AT FRAME 67- REMOVE & REPLACED 'T' PROFILE ANGLE.

Part: FLOOR SUPPORT — CORRODED (FRAMES 23-24) · airframe 41,253 hrs · 26,126 cycles

MAIN CABIN LH FLOOR SILL LOWER SPLICE ANGLE IS CRACKED BETWEEN FRAME 23 & 24 LH- R&R SLICE ANGLE ON LH FLOOR SILL BETWEEN FR23 & 24.

Part: FLOOR SUPPORT — CORRODED (FRAMES 48-49) · airframe 41,253 hrs · 26,126 cycles

MAIN CABIN RH FLOOR SILL HAS CORROSION AT FRAME 48 & 49- REMOVED RH FLOOR SILL AT FRAME 48-49. PICKED UP NEW HOLES AND STARTED INSTALLING NEW FLOOR SILL AT FRAME 48-49. FINISHED INSTALLATION OF RH FLOOR SILL AT FRAME 48-49.

Part: FLOOR SUPPORT — CORRODED (FRAME 20) · airframe 41,253 hrs · 26,126 cycles

MAIN CABIN FLOOR SUPPORT BETWEEN LH & CENTER OMEGA BEAM HAS CORROSION ON UPPER SURFACE AT FRAME 20- REMOVED FLOOR BOARD SUPPORT BETWEEN LH & CENTER OMEGA BEAM AT FR20. INSTALLED FLOOR BOARD SUPPORT BETWEEN LH & CENTER OMEGA BEAM AT FR20.

Part: FLOOR SUPPORT — CORRODED (FRAME 26) · airframe 41,253 hrs · 26,126 cycles

MAIN CABIN LH FLOOR SILL HAS CORROSION ON UPPER SURFACE AT FRAME 26 LH- REMOVED LH FLOOR SILL AT FRAME 26 LH. INSTALLED LH FLOOR SILL AT FRAME 26 LH.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 41,253 hrs · 26,126 cycles

MAIN CABIN RH OMEGA BEAM UPPER SURFACE HAS CORROSION AROUND FASTNER HOLE AT FRAME 23- REMOVED REPAIR DOUBLER ON RH OMEGA BEAM AT FR23, FABRICATED NEW ONE & ATTACHED IT ON SIDES. RIVETS THROUGH TOP & NUTPLATE NEED TO BE INSTALLED YET. INSTALLED NUTPLATE & TOP RIVETS IN THE REPAIR DOUBLER ON THE RH OMEGA BEAM AT FR23.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 41,253 hrs · 26,126 cycles

MAIN CABIN RH OMEGA BEAM STOP SIGN HAS CORROSION AT FR 20- R&R MAIN CABIN RH OMEGA BEAM STOP SIGN AT FR20.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 41,253 hrs · 26,126 cycles

SERVICE DOOR LOWER THRESHOLD HAS CORROSION ON UPPER SURFACE AROUND NUTPLATE HOLES BETWEEN FRAME 20 THRU 22- R&R SERVICE DOOR LOWER THRESHOLD.

Part: ANGLE — CRACKED (FRAME 20) · airframe 41,253 hrs · 26,126 cycles

CENTER OMEGA BEAM RAMP ANGLE IS CRACKED AT FRAME 20 AFT END RADIUS- REMOVED CENTER OMEGA BEAM RAMP ANGLE. INSTALLED CENTER OMEGA BEAM RAMP ANGLE AT FR20.

Part: FLOOR SUPPORT — CORRODED (FRAME 61) · airframe 41,253 hrs · 26,126 cycles

AFT LAV R/H FLOOR SILL HAS CORROSION AROUND FASTNER HOLE AT FR 61....R&R AFT LAV R/H FLOOR SILL AT FR 61.

Part: ANGLE — CRACKED (RT MLG WW) · airframe 41,253 hrs · 26,126 cycles

RH W/W REAR WEB LOWER ANGLE IS CRACKED AT O/B END- R&R RH W/W WEB LOWER ANGLE.

Part: FLOOR SUPPORT — CORRODED (FRAME 18) · airframe 41,253 hrs · 26,126 cycles

MAIN CABIN FLOOR SUPPORT STEP DOWN HAS CORROSION O/B OF CENTER OMEGA BEAM AT FRAME 18- R/R THE LOWER SUPPORT ANGLE ON THE STEP DOWN AT FR18.

Part: FLOOR SUPPORT — CORRODED (FRAME 18) · airframe 41,253 hrs · 26,126 cycles

CENTER OMEGA BEAM UPPER DIGITAL SUPPORT HAS CORROSION ON UPPER SURFACE AT FRAME 18- REMOVED THE UPPER DIGITAL SUPPORT AT FR18. BEGAN INSTALLING AFT UPPER DIGITAL SUPPORT AT FR 18 AT CENTER OMEGA BEAM. FINISHED INSTALLING AFT UPPER DIGITAL SUPPORT AT FR18 AT CENTER OMEGA BEAM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 41,253 hrs · 26,126 cycles

MAIN CABIN CENTER OMEGA BEAM UPPER DIGITAL SUPPORT HAS CORROSION FROM FRAME 20 THRU 20- REMOVED CENTER OMEGA BEAM GUSSET FROM FR16-FR23 & BEGAN INSTALLATION. FINISHED INSTALLATION OF CENTER OMEGA BEAM GUSSET FROM FR16-FR23.

Part: ANGLE — CRACKED (FRAMES 16-17) · airframe 41,253 hrs · 26,126 cycles

MAIN CABIN CENTER OMEGA BEAM O/B LOWER SPLICE ANGLE IS CRACKED BETWEEN FRAME 16 & 17- R/R CENTER OMEGA BEAM O/B LOWER SPLICE ANGLE BETWEEN FR16-FR17.

Part: THRESHOLD — CRACKED (FRAME 15) · airframe 41,253 hrs · 26,126 cycles

FWD PASSENGER DOOR CUT OUT AT LOWER THRESHOLD FRAME 15 LOWER UPPER DIGITAL SUPPORT END FITTING IS CRACKED AT STR 15 LH- R/R THE FR15 LOWER TO UPPER DIGITAL SUPPORT END FITTING AT STR 15L.

Part: FLOOR SUPPORT — CORRODED (FRAMES 19-20) · airframe 41,253 hrs · 26,126 cycles

MAIN CABIN LH FLOOR SILL HAS CORROSION ON UPPER SURFACE BETWEEN FRAME 19 & 20- R/R LH FLOOR SILL FROM FR18-FR22.

Part: SHEAR TIE — CRACKED (FRAME 80) · airframe 41,253 hrs · 26,126 cycles

AFT FUSELAGE INSIDE ACCESS 312AR FR 80 SHEER CLIP IS CRACKED BETWEEN STR 5 & 6 R/H SIDE....R&R FR 80 SHEER CLIP AT STR 5R & 6R.

Part: SHEAR TIE — CRACKED (FRAME 73) · airframe 41,253 hrs · 26,126 cycles

AFT CARGO FRAME 73 LH SHEAR CLIP IS CRACKED BELOW STR 8 LH- REMOVED CRACKED SHEAR CLIP, INSTALLED NEW SHEAR CLIP. PRIMED & PAINTED AREA.

Part: SHEAR TIE — CRACKED (FRAME 62) · airframe 41,253 hrs · 26,126 cycles

AFT CARGO FRAME 62 SHEAR CLIP IS CRACKED BELOW STR 6LH- R/R SHEAR CLIP AT FR62 STR 6L.

Part: SHEAR TIE — CRACKED (FRAME 71) · airframe 41,253 hrs · 26,126 cycles

AFT CARGO FR 71 SHEER CLIP IS CRACKED BELOW STR 9 R/H....R&R SHEER CLIP AT FR 71 BELOW STR 9 R/H.

Part: SHEAR TIE — CRACKED (FRAME 80) · airframe 41,253 hrs · 26,126 cycles

AFT FUSELAGE INSIDE ACCESS 312AR FR 80 SHEER CLIP IS CRACKED BETWEEN STR 5 & 6 L/H SIDE....R&R FR 80 SHEER CLIP AT STR 6L.

Part: SUPPORT — CRACKED (AFT CARGO DOOR) · airframe 41,253 hrs · 26,126 cycles

AFT CARGO DOOR SUPPORT ROD CLIP HOLDER SUPPORT BRACKET IS CRACKED ON UNDERNEITH- REMOVED & REPLACED SUPPORT.

Part: SHEAR TIE — CRACKED (FRAME 67) · airframe 41,253 hrs · 26,126 cycles

AFT CARGO FRAME 67 SHEAR CLIP IS CRACKED BETWEEN STR 6 & 7 LH- REMOVED & STARTED INSTALLING SHEAR CLIP AT FR 67. FINISHED INSTALLING SHEAR CLIP AT FR 67.

Part: SHEAR TIE — CRACKED (FRAME 80) · airframe 41,253 hrs · 26,126 cycles

AFT FUSELAGE INSIDE ACCESS 312AR FR 80 SHEER CLIP IS CRACKED BETWEEN STR 3 & 4 L/H SIDE....R&R FR 80 SHEER CLIP AT STR 3L & 4L.

Part: SHEAR TIE — CRACKED (FRAME 73) · airframe 41,253 hrs · 26,126 cycles

AFT CARGO FRAME 73 RH SHEER CLIP IS CRACKED BELOW STR 8- REMOVED & REPLACED SHEER CLIP AT FR 73.

Part: SHEAR TIE — CRACKED (FRAME 68) · airframe 41,253 hrs · 26,126 cycles

AFT CARGO FRAME 68 SHEAR CLIP IS CRACKED BETWEEN STR 6 & 7 LH- STARTED REMOVING SHEAR CLIP AT FR 68. FINISHED REMOVING & INSTALLED NEW SHEAR CLIP

Part: SKIN — CRACKED (LT WING LE) · airframe 41,253 hrs · 26,126 cycles

LH #2 L/E HAS CRACK ON PREVIOUS REPAIR- REMOVED LH L/E #2. INSTALLED LH L/E #2, O/B COUPLING, GASKET SEALS AND SPLICES REQUIRE INSTALLATION.INSTALLED SPLICES, O/B COUPLING & GASKET SEALS INSTALLED.

Part: DOOR FRAME — GOUGED (AFT CARGO) · airframe 41,253 hrs · 26,126 cycles

AFT CARGO DOOR LOWER FRAME IS GOUGED- REMOVED AFT CARGO DOOR LOWER FRAME ANGLE AND PICKED UP HOLES IN NEW PART. INSTALLED AFT CARGO DOOR LOWER FRAME ANGLE. STILL NEEDS SEAL TO BE INSTALLED AND LOWER FRAME PAINTED. INSTALLED SEAL & PAINTED AFT CARGO DOOR LOWER FRAME.

Part: ACCESS DOOR — CRACKED (COCKPIT) · airframe 41,253 hrs · 26,126 cycles

COCKPIT UNDERFLOOR ACCESS HATCH 123BL IS CRACKED UNDERNEITH HINGE BRACKET- CUT OUT DAMAGED AREA, FABRICATED DOUBLER AND FILLER, LOCATED AND DRILLED DOUBLER. INSTALLED DOUBLER AND FILLER.

Part: SKIN — CORRODED (FRAMES 80-81) · airframe 41,253 hrs · 26,126 cycles

AFT FUSELAGE EXTERIOR SKIN HAS CORROSION UNDER AND AROUND DATA PLATE BETWEEN FRAME 80 & 81 BETWEEN STR 20 & 21 LT- REMOVED CORROSION FROM THE AFT FUSELAGE EXTERNAL SKIN BETWEEN FR80-FR81 ON THE BELLY & REMOVED DATA PLATES. AWAITING TECHNICAL DISPOSITION FROM EMBRAER. BLENDING DONE. FABRIACATED DOUBLER, CUT-OUT DAMAGE, DRILLED HOLES, FABRICATED FILLER. INSTALLED REPAIR PARTS ON THE AFT FUSELAGE BELLY BETWEEN FR80-FR81 & INSTALLED DATA PLATE, PAINTED TO ORIGINAL FINISH.

Part: SPAR — CRACKED (HORIZONTAL STAB) · airframe 41,253 hrs · 26,126 cycles

LH HORIZONTAL STAB O/B SPAR IS CRACKED @ YH2965- REMOVED LH HORIZONTAL STAB O/B RIB AND REPAIRED, READY FOR INSTALL. REPAIRED AND REINSTALLED LH HORIZONTAL STAB O/B RIB.

Part: SUPPORT BRACKET — CRACKED (FRAME 46) · airframe 41,253 hrs · 26,126 cycles

LH OVER WING BELLY FAIRING NUTPLATE L ANGLE SUPPORT BRACKET ON TOP OF WING AT FRAME 46 IS CRACKED- REMOVED CRACKED L ANGLE SUPPORT, LOCATED & DRILLED UP NEW L ANGLE SUPPORT. INSTALLED NEW L ANGLE SUPPORT BRACKET.

Part: HINGE — CRACKED (RT WING TE FLAP) · airframe 41,253 hrs · 26,126 cycles

RH WING O/B FLAP SHROUD I/B FWD HINGE HALF HAS 3 CRACKED LUGS- REMOVED HINGE FROM FLAP SHROUD & STARTED DRILL UP. R&R RH WING O/B FLAP SHROUD I/B HINGE.

Part: HINGE — CRACKED (LT WING TE FLAP)

L/H WING T/E O/B FLAP SHROUD I/B FWD HINGE HALF IS CRACKED....R&R L/H WING T/E O/B FLAP SHROUD I/B FWD HINGE HALF.

Part: HINGE — CRACKED (RT WING TE FLAP) · airframe 41,253 hrs · 26,126 cycles

RH WING O/B FLAP SHROUD I/B AFT HINGE HALF IS CRACKED AT O/B END- REMOVED RH O/B FLAP I/B HINGE, STARTED TO DRILL UP. R&R RH WING O/B SHROUD I/B AFT HINGE.

Part: SUPPORT BRACKET — CRACKED (PAX DOOR HANDLE) · airframe 41,253 hrs · 26,126 cycles

PASSENGER DOOR INTERIOR DOOR HANDLE SUPPORT BRACKET IS CRACKED IN BEND RADIUS- REMOVED PASSENGER DOOR INTERIOR HANDLE ACTUATING AND LOCKING MECHANISM. REMOVED AND REPLACED DOOR HANDLE SUPPORT BRACKET. INSTALLED PAX DOOR INTERIOR HANDLE ACTUATING AND LOCKING MECHANISM.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 41,253 hrs · 26,126 cycles

AFT FUSELAGE EXTERIOR R/H SIDE AT FR 57 BLEED AIR DUCT SUPPORT BRACKET IS CRACKED AT STR 17 R/H....R&R BLEED AIR DUCT SUPPORT BRACKET FROM AFT FUSELAGE EXTERIOR R/H SIDE AT FR 57.

Part: SUPPORT BRACKET — CRACKED (FRAME 47) · airframe 41,253 hrs · 26,126 cycles

RH OVER WING BELLY FAIRING NUTPLATE L ANGLE SUPPORT BRACKET ON TOP OF WING AT FRAME 47 IS CRACKED- REMOVED CRACKED L ANGLE SUPPORT, LOCATED & DRILLED UP NEW L ANGLE SUPPORT. INSTALLED NEW L ANGLE.

Part: HINGE — CRACKED (LT WING TE FLAP)

L/H WING T/E O/B FLAP SHROUD O/B AFT HINGE HALF IS CRACKED....R&R L/H WING T/E O/B FLAP SHROUD O/B AFT HINGE HALF.

Part: SUPPORT ROD — CORRODED (LT MLG DOOR) · airframe 41,253 hrs · 26,126 cycles

LH MLG DOOR FWD & AFT SUPPORT RODS HAVE RUST- R/R LH MLG DOOR FWD & AFT SUPPORT RODS.

Part: SUPPORT — CRACKED (LT WING) · airframe 41,253 hrs · 26,126 cycles

LH WING L/E I/B HORSE SHOE NUTPLATE SUPPORT RING IS CRACKED IN BEND RADIUS- REMOVED & REPLACED LH L/E I/B HORSESHOE, INSTALLED NEW NUT PLATES.

Part: STRINGER FITTING — CRACKED (FRAME 20) · airframe 41,253 hrs · 26,126 cycles

MAIN CABIN STR 3 L/H END FITTING FINGER CRACKED AT FR 20....R&R STR 3L CASTING AT FR 20.

Part: SUPPORT BRACKET — CRACKED (BELLY FAIRING) · airframe 41,253 hrs · 26,126 cycles

RH OVERWING BELLY FAIRING NUTPLATE L ANGLE SUPPORT BRACKET ON TOP OF WING L/E AT FRAME 41 IS CRACKED- REPAIRED RH OVER WING BELLY FAIRING NUTPLATE L ANGLE SUPPORT BRACKET AT FR 41, NEEDS NUTPLATES LOCATED AND INSTALLED. LOCATED AND INSTALLED NUT PLATES ON L ANGLE AT FRAME 41.

Part: SPAR — CRACKED (HORIZONTAL STAB) · airframe 41,253 hrs · 26,126 cycles

RH HORIZONTAL STAB O/B SPAR IS CRACKED @ YH2965- REMOVED RH HORIZONTAL STAB O/B RIB AND REPAIRED. READY FOR INSTALL. REPAIRED AND REINSTALLED RH HORIZONTAL RIB O/B.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 41,253 hrs · 26,126 cycles

AFT FUSELAGE EXTERIOR L/H SIDE AT FR 57 BLEED AIR DUCT SUPPORT BRACKET IS CRACKED AT STR 17 L/H....R&R BLEED AIR DUCT SUPPORT BRACKET AFT FUSELAGE EXTERIOR L/H SIDE AT FR 57.

Part: ROD END — CORRODED (LT MLG DOOR) · airframe 41,253 hrs · 26,126 cycles

LEFT MLG DOOR FWD & AFT SUPPORT RODS HAVE RUST. R & R THE LT MLG DOOR FWD & AFT SUPPORT ROD ENDS.

Part: HINGE — CRACKED (LT WING TE FLAP)

L/H WING T/E O/B FLAP SHROUD O/B FWD HINGE HALF IS CRACKED....R&R L/H WING T/E O/B FLAP SHROUD O/B FWD HINGE HALF.

Part: DOOR FRAME — CRACKED (E&E DOOR) · airframe 41,253 hrs · 26,126 cycles

REAR ELECTRONIC COMPT ACCESS DOOR 272DR FRAME IS CRACKED UNDERNEITH HINGE BRACKET- REPAIRED REAR ELECTRONIC COMP ACCESS DOOR.

Part: SUPPORT BRACKET — CRACKED (FRAME 45) · airframe 41,253 hrs · 26,126 cycles

RH OVER WING BELLY FAIRING NUTPLATE L ANGLE SUPPORT BRACKET ON TOP OF WING AT FRAME 45 IS CRACKED- REPAIRED RH OVER WING BELLY FAIRING NUTPLATE L ANGLE SUPPORT BRACKET AT FR 45, NEEDS NUTPLATES LOCATED AND INSTALLED. LOCATED AND INSTALLED NUT PLATES ON L ANGLE AT FRAME 45.

Part: MANIFOLD — BYPASSING (HYDRAULIC SYS) · airframe 39,376 hrs · 24,698 cycles

HYD SYSTEM 1 FAIL IN FLIGHT PRECEDED BY E1 HYD PUMP FAILADVISORY. HYD SYSTEM SHOWED PRESSURE 2900 PSI. AIRCRAFT TAXIED TO GATE UNDER OWN POWER. DEFERED NR 1 EDP PRESSURE SWITCH. R&R HYD NR 1 MANIFOLD. OPS CHECK GOOD AT THIS TIME.

Part: HANDLE — OUT OF ADJUST (PAX DOOR) · airframe 38,566 hrs · 24,051 cycles

MAIN DOOR HANDLE LAYS ON FAIRING WHEN CLOSED. PERFORMED AN ADJUSTMENT AND TEST OF THE MAIN DOOR HANDLE. OPS CHECKED GOOD. NO FURTHER DEFECTS NOTED.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 37,764 hrs · 23,389 cycles

MAIN DOOR EXTERIOR FLOOD LIGHT FOUND INOPERATIVE. R & R THE BULB. OPS CHECKED GOOD.

Part: SEAL — LEAKING (NR 2 BLEED) · airframe 37,252 hrs · 22,949 cycles

NR 2 BLEED LEAK IN FLIGHT. PERFORMED A NR 2 BLEED LEAK INSPECTION, FOUND A SUBSTANTIAL LEAK ON JUNCTION NR 28. REMOVED AND REPLACED THE BLEED SEALS ON THE NR 28, NO LEAKS FOUND. OPS CHECKED GOOD. THE FOLLOWING WAS CLEARED IN CONJUNCTION WITH PREVIOUS DISCREPANCY. WING ANTI-ICE FAILED IN FLIGHT. INTERIGATED CMC WING ANTI ICE LOW PRESSURE MESSAGE INDUCED BY BLEED 2 LEAK.

Part: ANTI-ICE SYSTEM — MALFUNCTIONED · airframe 35,518 hrs · 21,451 cycles

WING ANTI/ICE FAIL IN ICING CONDITIONS. PERFORMED ANTI-ICE OPS CHECK, NO DEFECTS NOTED AT THIS TIME.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 34,865 hrs · 20,914 cycles

ALL FOUR EMERGENCY LIGHT BATTERIES ARE LOW. R & R THE BATTERIES, OPS CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 34,483 hrs · 20,578 cycles

COCKPIT EMERGENCY FLASHLIGHT IS NOT WORKING. R & R THE FLASHLIGHT, OPS CHECKED GOOD

Part: FLAP SYSTEM — MALFUNCTIONED · airframe 34,271 hrs · 20,393 cycles

FLAP FAIL IN FLIGHT. RESET FLAP SYSTEM, OPS CHECK FLAP SYS NO DEFECTS NOTED.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 33,913 hrs · 20,100 cycles

LEFT OVERWING EMERGENCY LIGHT INOPERATIVE. R & R LT OVERWING EMERGENCY LIGHT. OPS CHECKED GOOD.

Part: ACM — INOPERATIVE (NR 1) · airframe 33,092 hrs · 19,411 cycles

RETURNED FROM FLIGHT WITH REPORTED SMOKE IN THE COCKPIT AND CABIN WHEN ACFT CAME OUT OF ICING CONDITIONS. REMOVED AND REPLACED NR 1 ACM. OPS CHECK GOOD.

Part: PROXIMITY SWITCH — INOPERATIVE (MLG) · airframe 33,056 hrs · 19,376 cycles

LANDING GEAR AIR TO GROUND FAIL. R & R NOSE WOW PROXIMITY SWITCH, ADJUSTED TARGET. OPS CHECK GOOD.

Part: DRIVE UNIT — INOPERATIVE (TE FLAPS) · airframe 32,357 hrs · 18,833 cycles

FLAP FAIL EICAS MSG WITH FLAP STUCK AT 9 DEGREES ON APPROACH. MAINTENANCE RESET FLAPS, OPS CHECK GOOD, SAFE FOR 1 TIME FERRY FLIGHT. MAINTENANCE REPLACED FLAP DRIVE UNIT, OPS CHECK GOOD AND RELEASE FOR REVENUE SERVICE.

Part: ENGINE — CONTAMINATED · airframe 31,661 hrs · 18,292 cycles

SMOKE IN COCKPIT AFTER TAKEOFF, RETURNED TO BLOCK. MAINTENANCE PERFORMED SMOKE TROUBLESHOOTING, FOUND TRACES OF DE-ICE FLUID IN ENGINE INLETS, CLEANED AND REMOVED DE-ICE FLUID, OPS CHECKS AND NO OTHER DEFECTS NOTED, OPS CHECK GOOD.

Part: SIGN — INOPERATIVE (CABIN) · airframe 27,346 hrs · 15,515 cycles

THE CREW REPORTED OVERHEAD EXIT SIGN 12A WAS INOPERATIVE. REPORTED BURN MARK AT EXIT PORTION OF SIGN. MX INSPECTED AND REPLACED THE OVERHEAD EXIT SIGN. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,344 hrs · 15,514 cycles

THE CREW REPORTED EXIT ROW LIGHTS ON CEILING AND CAPTAINS SIDE WALL AFT OF EXIT HATCH ARE INOPERATIVE. MX PERFORMED RESET OF EMERGENCY LIGHTS AND OPS CHECKS WERE GOOD.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 27,153 hrs · 15,394 cycles

DURING SCHEDULED MX INSPECTION, THE EMERGENCY LIGHT SIGN AT SEAT 12A WAS FOUND INOPERATIVE. MX R & R THE EMERGENCY EXIT SIGN WITH OPS CHECK SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: WIRE HARNESS — CHAFED (NR 2 ENGINE) · airframe 22,314 hrs · 12,318 cycles

ORD FLT 5826 THE CREW REPORTED DURING FIRE TEST ON ENGINE NR 2 THE FIRE DETECT MESSAGE FAILED TO APPEAR ON THE EICAS. MAINTENANCE INSPECTED AND REPLACED THE NR 2 ENGINE HARNESS. OPERATIONAL CHECKS WERE GOOD.

Part: SEAL — LOOSE (COCKPIT WINDOW) · airframe 22,317 hrs · 12,321 cycles

ORD FLT 6054 THE CREW REPORTED ON CLIMBOUT THERE WAS A VERY LOUD NOISE AND VIBRATION AT CAPTAINS WINDOW. THE AIRCRAFT DIVERTED INTO CLE WITHOUT INCIDENT. MAINTENANCE INSPECTED AND RE-SECURED TRIM SEAL ON CAPTAINS DV WINDOW. LEAK CHECKS WERE GOOD.

Part: UNKNOWN — SMOKE (CABIN) · airframe 20,691 hrs · 11,072 cycles

ORD FLT 5922 THE CREW REPORTED SMOKE IN THE CABIN AFTER DE-ICING AT THE GATE. MAINTENANCE INSPECTED AND RAN PACKS AND BLEED SYSTEM WITH BOTH APU AND ENGINES. NO SMOKE NOTED. SUSPECT DE-ICE FLUID IN THE APU INLET CREATED SMOKE.

Part: INVERTER — FAULTY (CABIN) · airframe 20,180 hrs · 10,760 cycles

DURING ROUTINE MAINTENANCE THE EMERGENCY EXIT SIGN OVER THE SERVICE DOOR WAS FOUND INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE NR 2 EMERGENCY LIGHT INVERTER. OPERATIONAL CHECKS WERE GOOD.

Part: BATTERY — OVERTEMP (NR 2) · airframe 19,459 hrs · 10,368 cycles

IAH - FLIGHT 2023, DURING DESCENT THE CREW REPORTED A BATTERY TWO OVERTEMP. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO MAIN BATTERY, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SMOKE DETECTOR — FALSE ACTIVATION (CARGO BAY) · airframe 19,882 hrs · 10,598 cycles

BHM - FLIGHT 2729 THE CREW REPORTED A BAGGAGE SMOKE INDICATION, AND DISCHARGED THE FIRE BOTTLES AS A PRECAUTION. THE AIRCRAFT LANDED AT BHM WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND NO EVIDENCE OF SMOKE. REMOVED AND REPLACED BOTH BLOWN FIRE BOTTLES. REMOVED AND REPLACED THE BAGGAGE SMOKE DETECTOR AS A PRECAUTION. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BALLAST — MALFUNCTIONED (CABIN) · airframe 18,976 hrs · 10,102 cycles

IAH - FLIGHT 3104, THE CREW REPORTED AN ELECTRICAL BURNING SMELL COMING FROM THE FLOOR NEAR 1A DURING CRUISE. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE CABIN LIGHTING BALLAST IN THE GALLEY, OPERATIONALLY TESTED WITHOUT DEFECT. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FRAME — CRACKED (FUSELAGE) · airframe 18,820 hrs · 10,007 cycles

SHV - DURING C-CHECK FRAME 79 STR 3L-7L HAS (8) RIVETS WITH CRACK INDICATIONS. MAINTENANCE REPAIRED FRAME 79 STR 3L-7L IAW EC 5330-02154. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (FUSELAGE) · airframe 18,820 hrs · 10,007 cycles

SHV - DURING C-CHECK FRAME 78 EXTERNAL SURFACE HAS CRACK INDICATIONS AROUND RIVET HEADS BETWEEN STR 2R AND 5R. MAINTENANCE REPAIRED FRAME 77 EXTERNAL SURFACE AROUND RIVET HEADS BETWEEN STR 2R AND 5R IAW EC5330-02154. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (FUSELAGE) · airframe 18,820 hrs · 10,007 cycles

SHV - DURING C-CHECK FRAME 77 EXTERNAL SURFACE HAS CRACK INDICATIONS AROUND RIVET HEADS BETWEEN STR 2R AND 5R. MAINTENANCE REPAIRED FRAME 77 EXTERNAL SURFACE AROUND RIVET HEADS BETWEEN STR 2R AND 5R IAW EC5330-02154. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,820 hrs · 10,007 cycles

SHV - CENTER OMEGA BEAM RAMP ANGLE CORRODED (LEVEL 2 LOCAL) ON LWR SIDE AT FRAME 20. MAINTENANCE REMOVED AND REPLACED CENTER OMEGA BEAM RAMP ANGLE IAW EMB-145 SRM 51-40-00. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (FUSELAGE) · airframe 18,820 hrs · 10,007 cycles

SHV - DURING C-CHECK FRAME 79 EXTERNAL SURFACE HAS CRACK INDICATIONS AROUND RIVET HEADS BETWEEN STR 2R AND 7R. MAINTENANCE REPAIRED FRAME 79 EXTERNAL SURFACE AROUND RIVET HEADS BETWEEN STR 2R AND 7R IAW EC5330-02154. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 18,820 hrs · 10,007 cycles

SHV - DURING C-CHECK FLOOR SUPPORT FROM AFT SERVICE DOOR CENTER SILL TO RT OMEGA BEAM HAS CRACK AND TOOLING MARKS AROUND RIVETS (FRAME 22). MAINTENANCE REMOVED AND REPLACED FLOOR SUPPORT FROM AFT SERVICE DOOR CENTER SILL TO RT OMEGA BEAM AT FRAME 22 IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,820 hrs · 10,007 cycles

SHV - SERVICE DOOR ENTRY CENTER SILL IS CORRODED (LEVEL 2 LOCAL) AT MARKED LOCATIONS. MAINTENANCE REMOVED AND REPLACED SERVICE DOOR ENTRY CENTER SILL IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: THERMOSTAT — MALFUNCTIONED (BLEED AIR SYS) · airframe 15,111 hrs · 8,008 cycles

FLIGHT 2944 (AIRCRAFT N14153-SERIAL NUMBER 761) ON JANUARY 27, 2009 HAD BLD (1) OVERTEMP IN FLT. NO EMERGENCY BUT FLIGHT DIVERTED IAH TO SHV. MAINTENANCE REMOVED AND REPLACED LT FWD AND AFT FAN AIR CONTROL THERMOSTATS IAW EMB 145XR AMM 36-11-06. OPERATIONAL CHECK GOOD. THE AIRCRAFT WAS APPROVED TO RETURN SERVICE. FAN AIR CONTROL THERMOSTATS LT FWD P/N 816624-10, S/N 200302010, LT AFT P/N 816624-9, S/N 200302055.

Part: COFFEEMAKER — FAULTY (GALLEY) · airframe 14,417 hrs · 7,635 cycles

SDR C2XA08IA235, FLIGHT 2459 CREW REPORTED THAT THE NUMBER ONE COFFEEMAKER SMOKES WHEN TURNED ON. MAINTENANCE PLACED ON NEF GL-01 CAT D CTL NR 157681, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ON 11/07/08 MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE COFFEEMAKER, OPERATIONALLY CHECKED WITH NO DEFECTS, CLEARED THE NEF, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: COFFEEMAKER — SMOKE (GALLEY) · airframe 14,417 hrs · 7,635 cycles

IAH - FLIGHT 2459 THE CREW REPORTED THAT THE NUMBER ONE COFFEEMAKER SMOKES WHEN TURNED ON. MAINTENANCE INSPECTED THE AIRCRAFT AND PLACED THE NUMBER ONE COFFEEMAKER ON NEF GL-01 CAT D CTL 157681, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. SDR FILED OPEN AWAITING FINAL COPRRECTIVE ACTION.

Part: SWITCH — INOPERATIVE (WINDSHIELD HEAT)

CLE FLIGHT 2786 - THE CREW REPORTED A WINDSHIELD NR 2 HEAT FAIL ON CLIMB. THE ACFT RETURNED TO CLE WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NR 2 WINDSHIELD HEAT PUSH BUTTON. OPERATIONAL CHECKS WERE GOOD. (S)

Part: CONTROL MODULE — FAULTY (COCKPIT) · airframe 12,751 hrs · 6,756 cycles

CLE FLIGHT 2285 THE CREW REPORTED A ENGINE 2 FIRE DETECT FAIL TWICE IN FLIGHT FOR 1-2 MINUTES EACH TIME. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NR 2 ENGINE FIRE CONTROL MODULE. OPERATIONAL CHECKS WERE GOOD.

Part: MODULE — INOPERATIVE (COCKPIT) · airframe 10,401 hrs · 5,558 cycles

IAH - DURING MAINTENANCE INSPECTION, IT WAS NOTED THAT THE TAKEOFF DATA HAD UNCONTROLLABLE COMMANDS. MAINTENANCE REMOVED AND REPLACED THE POWER PLANT CONTROL MODULE, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SEAL — DAMAGED (PAX DOOR) · airframe 6,568 hrs · 3,496 cycles

CLE FLIGHT NR 2933, THE CREW REPORTED THE PASSENGER DOOR WAS HARD TO OPEN. MAINTENANCE INSPECTED THE MAIN CABIN DOOR SEAL AND FOUND IT SWELLED UP. THE MAIN CABIN DOOR SEAL WAS REPLACED BY MAINTENANCE AND THE DOOR OPERATED PROPERLY WITH NO FURTHER DIFFICULTIES REPORTED.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 4,083 hrs · 2,155 cycles

FLT NR 2124 - LEFT EMERGENCY EXIT DOOR LIGHT INOP. PERFORMED OPS CHECK OF EMERGENCY LIGHTS AND LEFT EXIT DOOR LIGHT OPS CHECK GOOD. NO DISCREPANCY FOUND. AIRCRAFT RELEASED AND RETURNED TO SERVICE.