N11199

Part: SIGN — INOPERATIVE (ZONE 200) · airframe 39,710 hrs · 28,130 cycles

SERVICE DOOR UPPER EXIT LIGHT INOPERATIVE. REMOVED SIGN RESET CONNECTORS. REINSTALLED SIGN. OPS CHECK SAT.

Part: SKIN — DENTED (ZONE 100) · airframe 39,606 hrs · 28,027 cycles

DENT ON LH FWD FUSE I SKIN, BTW FR 6-7 AND BTW STR 13L-15L UNDER GPU ACCESS DOOR. REPAIR DOUBLER ON LH FWD FUSE II SKIN, BTW FR 6-7 AND AT STR 15L UNDER ACCESS DOOR.

Part: SKIN — CHAFED (ZONE 200) · airframe 39,606 hrs · 28,027 cycles

SKIN FOUND DAMAGE BY CHAFING AT RH PYLON JUNCTION, NEAR ACCESS PANEL 424DB. REPAIR DOUBLER ON RH REAR FUSE I SKIN, BTW FR 67-68 AND BTW STR 7R-9R

Part: FRAME — DENTED (ZONE 200) · airframe 39,606 hrs · 28,027 cycles

CF4 ON LT FUSE ON FR 59 BTW STR 2L-3L DENT FOUND AT FLANGE. SPLICE REPAIR ON CENTER FUSE IV FRAME 59 BTW STR 1L-2L

Part: FRAME — CRACKED (ZONE 100) · airframe 39,606 hrs · 28,027 cycles

FR 29 LH FOUND CRACKED BTW STR 15L-16L. EXTENDED SPLICE REPAIR ON LH CENTER FUSE IV FRAME 59 BTW STR 14L-16L

Part: TORQUE BOX — CORRODED (ZONE 600) · airframe 39,606 hrs · 28,027 cycles

CORROSION FOUND INSIDE UPPER HOLE OF RH TORQUE BOX #1. HOLE OVERSIZED ON RH TORQUE BOX AT RIB 01A AND SPAR III

Part: SKIN — DENTED (ZONE 200) · airframe 39,606 hrs · 28,027 cycles

2 DENTS ON LH CENTER FUSE I SKIN, BTW FR 19-20 AND BTW STR 12L-13L. REPAIR DOUBLER ON LH CENTER FUSE I SKIN, BTW FR 19-20 AND BTW STR 11L-13L

Part: WEB — CORRODED (ZONE 100) · corrosion level 2 · airframe 39,606 hrs · 28,027 cycles

SKIN UNDER FLOOR BTW FR 66-67 AND BTW STR 21L-21R AT DRAIN VALVE FOUND CORRODED. REPAIR DOUBLER ON REAR FUSELAGE I LOWER SKIN PANEL AT FR 67 AND BTW 21L-21R

Part: PLATE — CRACKED (ZONE 100) · airframe 39,606 hrs · 28,027 cycles

NLG UPPER PLATE FOUND CRACKED. REPAIR DOUBLER ON FWD FUSE I NLG UPPER PLATE ON RH FWD SIDE

Part: SKIN — DENTED (ZONE 200) · airframe 39,606 hrs · 28,027 cycles

FWD FUSELAGE 1, BTW STR 1-4R FRAME 06 FOUND DENTED. SPLICE REPAIR ON FWD FUSE II FRAME 6, BTW STR 4R-6R AND BTW STR 4L-6L.

Part: NUT — MISSING (ZONE 300 RUDDER) · airframe 39,606 hrs · 28,027 cycles

RUDDER II, MIDDLE OF LH SKIN, ANCHOR NUT MISSING FOR DEFLECTION TOOL INSTALLATION. AT RUDDER II, MIDDLE OF LH SKIN, ELONGATED SCREW HOLE REPAIR INSTALLED.

Part: PLATE — CORRODED (ZONE 200) · airframe 39,606 hrs · 28,027 cycles

DIGITAL PLATE BTW FR 15-16 FOUND CORRODED. DIGITAL PLATE BTW FR 15-18 CORRODED AREA THRU AND THRU AND OUT OF LIMIT. DIGITAL PLATE BTW FR 15-18 PERFORMED AREA REPAIRED. CORROSION LEVEL 1.

Part: SKIN — SCRATCHED (ZONE 100) · airframe 39,606 hrs · 28,027 cycles

REAR FUSELAGE I, SCRATCH FOUND ON BELLY SKIN AT FR 71 AND BTW STR 20L-21L. REAR FUSELAGE I, BELLY SKIN AT FR 71 BTW STR 20L-21L. SCRATCH ON BELLY SKIN FR 71 BTW STR 20L-21L FOUND OUT OF LIMIT. BELLY SKIN AT FR 71 BTW STR 20L-21L CUT OUT PERFORMED AND REPAIR PART FABRICATED. REAR FUSELAGE I, SCRATCH OUT OF LIMIT ON BELLY SKIN AT FR 71 BTW STR 20L-21L REPAIRED.

Part: SKIN — DENTED (ZONE 200) · airframe 39,606 hrs · 28,027 cycles

CF4 ON L/H FUSE ON FR59 BTW STR 2L-3L DENT FOUND AT FLANGE NEW FRAME SECTION AND SPLICE FABRICATED. FRAME REPAIRED WITH A SPLICE.

Part: SKIN — CRACKED (ZONE 200) · airframe 39,606 hrs · 28,027 cycles

RF 1 FUSE SKIN AT FR 75 AND AT STR 2R CRACKED. REPAIR DOUBLER ON RH REAR FUSE I SKIN AT FR 75 AND AT STR 2R

Part: NUT PLATE — BROKEN (ZONE 500) · airframe 39,606 hrs · 28,027 cycles

LH LEADING EDGE #2 OUTBD RIB, X2 NUT PLATE FOUND BROKEN. LH WING LEADING EDGE #2, LOWER SKIN CUT-OUT AND FILLER INSTALLED INBD OF STA YS=6405.

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 39,606 hrs · 28,027 cycles

LH OMEGA BEAM AT FR22 FOUND CRACKED. REPAIR DOUBLER ON CF I LH OMEGA BEAM ON INBD VERTICAL FLANGE AT FR 22.

Part: SUPPORT — CRACKED (ZONE 100) · corrosion level 2 · airframe 39,606 hrs · 28,027 cycles

LH SILL #1 BTW FR 18-22 FOUND CORRODED. LH SILL #1 BTW FR 18-22 CORRODED OUT OF LIMITS. REMOVED AND REPLACED

Part: SKIN — CRACKED (ZONE 200) · airframe 39,606 hrs · 28,027 cycles

RF1 FUSE SKIN AT FR 75 AND AT STR 2L CRACKED. REPAIR DOUBLER ON LH REAR FUSE I SKIN AT FR 75 AND AT STR 2L

Part: BRACKET — CRACKED (ZONE 600) · airframe 39,606 hrs · 28,027 cycles

INSIDE RH FUEL PANEL 631DB, 2 BRACKETS FOUND CRACKED. RH WING LOWER SKIN AT RIB 8 PAINT REMOVED. RH FUEL PANEL 631DB RIB 8, 2 BRACKETS REPLACED.

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 39,606 hrs · 28,027 cycles

SHEAR CLIP AT FR 68 AND BTW STR 6L-9L FOUND CRACKED. AT FR68 AND BTW STR 6L-9L SHEAR CLIP REMOVED AND INSTALLED.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 39,606 hrs · 28,027 cycles

CF1, ANGLE ON INBD SIDE OF CENTER OMEGA BEAM BTW FR 18-20 FOUND CORRODED. AT CF1 ANGLE ON INBD SIDE OF CENTER OMEGA BEAM BTW FR 18-20, ANGLE FOUND CORRODED OUT OF LIMIT. ANGLE REMOVED. CF1, ANGLE ON INBD SIDE OF CENTER OMEGA BEAM BTW FR 18-20 REPLACED.

Part: FRAME — CRACKED (ZONE 200) · airframe 39,606 hrs · 28,027 cycles

LH COCKPIT, OVERHEAD PANEL, FRAME FOUND CRACKED. LH COCKPIT OVERHEAD PANEL FRAME REMOVED AND REPLACED.

Part: PARTITION — CORRODED (ZONE 200) · airframe 39,606 hrs · 28,027 cycles

RH PARTITION AT FR61 FOUND CORRODED. AFTER INVESTIGATION, CRACK FOUND ON RH PARTITION AT FR61. AT PARTITION RH FR 61 CUT AWAY SECTION REPLACED WITH MADE REPAIR PART LOCALLY FABRICATED. AT FR61 RH PARTITION REPAIRED.

Part: FLOOR SUPPORT — MISREPAIRED (ZONE 200) · airframe 39,606 hrs · 28,027 cycles

RH OMEGA BEAM REPAIR BTW FR 23-24 WAS NOT DONE PROPERLY. REPAIR AT RH OMEGA BEAM BTW FR 23-24 REMOVED. REPAIR AT RH OMEGA BEAM BTW FR 23-24 REPLACED. OMEGA BEAM SURFACE AT RH BTF 23-24 REPROTECTED.

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 39,606 hrs · 28,027 cycles

LH OMEGA BEAM FR27 FLANGE IB CRACKED. REPAIR DOUBLER ON CFII LH OMEGA BEAM ON INBD VERTICAL FLANGE AT FR 27

Part: ANGLE — CRACKED (ZONE 100) · airframe 39,606 hrs · 28,027 cycles

CRACK ON LH WING TO BODY FAIRING LOWER ANGLE #2 AT FR 47. LOWER ANGLE #2 AT LH WING TO BODY FAIRING, FR 47 REMOVED. ANCHOR NUTS ON ANGLE REMOVED. HOLES TRANSFERRED ON NEW ANGLE. ANCHOR NUTS REINSTALLED. NEW ANGLE INSTALLED AND SEALED. SURFACE REPROTECTED.

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 39,606 hrs · 28,027 cycles

CF3 LH OMEGA AT FR 36 FLANGE IB CRACKED. CF3 LH OMEGA BEAM FR 36 CUTOUT PERFORMED. CF2 LH OMEGA BEAM FR 36 DOUBLER AND FILLER FABRICATED. CF3 LH OMEGA BEAM FR 36 DOUBLER REPAIR INSTALLED

Part: DOOR SILL — CORRODED (ZONE 200) · corrosion level 2 · airframe 39,606 hrs · 28,027 cycles

SERVICE DOOR CENTER SILL BTW FR 20-22 FOUND CORRODED. SERVICE DOOR CENTER SILL BTW FR 20-22 REMOVED FOR REPLACEMENT. SERVICE DOOR CENTER SILL BTW FR 20-22 REPLACED

Part: ANGLE — CRACKED (ZONE 100) · airframe 39,606 hrs · 28,027 cycles

ON CARGO LOWER BEAM AT T-PROFILE FR 66 ANGLE FOUND CRACKED. ON CARGO LOWER BEAM AT T-PROFILE FR 66 ANGLE REMOVED AND INSTALLED.

Part: DOOR SILL — CORRODED · corrosion level 2 · airframe 39,606 hrs · 28,027 cycles

CF3 RH FUSE BTW FR 41-48 SILL CORRODED. CF3 RH FUSE BTW FR 41-48 SILL BLENDED AND FOUND OUT OF LIMIT. CF3 RH FUSE BTW FR41-48 SILL REMOVED AND REPLACED

Part: SUPPORT — CRACKED (ZONE 400) · airframe 39,606 hrs · 28,027 cycles

RH PRECOOLER SUPPORT CRACKED R/H PRECOOLER AFT SUPPORT REMOVED AND REPLACED.

Part: PROFILE — CORRODED (ZONE 200) · corrosion level 2 · airframe 39,606 hrs · 28,027 cycles

CF2 RH T PROFILE BTW FR 28 CORRODED. AT CF2 RH T PROFILE BTW FR 28 CORROSION OUT OF LIMIT. AT CF2 RH T PROFILE BTW FR 28, 9 RIVETS REMOVED ON SILL FOR ACCESS. AT CF2 RH T PROFILE BTW FR 28 REMOVED AND INSTALLED.

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 39,606 hrs · 28,027 cycles

IN REAR FUSELAGE COMPARTMENT AT BULKHEAD 80, RH SHEAR CLIP CRACKED BETWEEN STRINGER 5 AND STRINGER 7. IN REAR FUSELAGE COMPARTMENT, AT BULKHEAD 80, RH SHEAR CLIP BTW STR 5 AND STR 7 REMOVED AND REPLACED

Part: ANGLE — CORRODED (ZONE 800) · corrosion level 2 · airframe 39,606 hrs · 28,027 cycles

BAGGAGE DOOR FWD L-SHAPE ANGLE AT FR65 BTW STR 16-17 FOUND CORRODED. BAGGAGE DOOR FWD L SHAPE ANGLE AT FR65 BTW STR 16-17 REMOVED AND REPAIRED.

Part: BEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 39,606 hrs · 28,027 cycles

BAGGAGE DOOR LOWER BEAM BTW FR 65-68 FOUND CORRODED. BAGGAGE DOOR LOWER BEAM BTW FR 65-68 REMOVED AND REPLACED.

Part: SUPPORT ANGLE — CRACKED (ZONE 100) · airframe 39,606 hrs · 28,027 cycles

UPLOCK NLG STRUCTURE, LH AND RH SUPPORT ANGLE FOUND CRACKED. UPLOCK NLG STRUCTURE LH AND RH SUPPORT ANGLE REMOVED AND REPLACED

Part: SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 39,606 hrs · 28,027 cycles

RH SILL BTW FR 53-39 FOUND CORRODED. AT RH SILL BTW FR 53-59 SILL FOUND CORRODED OUT OF LIMITS. AT RH SILL BTW FR 53-59, DRILL NEW HOLES FOR NEW SILL. AT RH SILL BTW FR 53-39 NEW SILL INSTALLED

Part: GUSSET — CORRODED (ZONE 100) · corrosion level 2 · airframe 39,606 hrs · 28,027 cycles

MIDDLE GUSSET BTW FR 59-61 FOUND CORRODED. MIDDLE GUSSET BTW FR 59-61 FOUND CORRODED OUT OF LIMITS. MIDDLE GUSSET BTW FR 59-61 REMOVED AND REPLACED

Part: GUSSET — CORRODED (ZONE 100) · corrosion level 2 · airframe 39,606 hrs · 28,027 cycles

RH GUSSET BTW FR 59-61 FOUND CORRODED. RH GUSSET BTW FR 59-61 FOUND CORRODED OUT OF LIMIT. RH GUSSET BTW FR 59-61 REMOVED AND REPLACED.

Part: SUPPORT — CRACKED (ZONE 800) · airframe 39,606 hrs · 28,027 cycles

BAGGAGE DOOR MECHANISM SUPPORT BTW FR 61-62 AND BTW STR 4R-5R FOUND CRACKED. AT FR61-62 BTW STR 4R-5R BAGGAGE DOOR MECHANISM SUPPORT REMOVED AND REPLACED

Part: SUPPORT — CRACKED (ZONE 800) · airframe 39,606 hrs · 28,027 cycles

RH BAGGAGE DOOR MECHANISM LOWER SUPPORT AT STR 5 BTW FR 68-69 FOUND CRACKED. RH BAGGAGE DOOR MECHANISM LOWER SUPPORT AT STR 5 BTW FR 68-69 REMOVED AND REPLACED

Part: GUSSET — CORRODED (ZONE 200) · corrosion level 2 · airframe 39,606 hrs · 28,027 cycles

LH GUSSET BTW FR 59-61 FOUND CORRODED. LH GUSSET BTW FR 59-61 FOUND CORRODED OUT OF LIMIT. LH GUSSET BTW FR 59-61 REMOVED AND REPLACED

Part: SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 39,606 hrs · 28,027 cycles

CF3 RH FUSE BTW FR 35-41 SILL CORRODED. CF3, RH SILL BTW FR 35-41 BLENDED AND FOUND OUT OF LIMIT. CF3 RH FUSE BTW FR 35-41 SILL REPLACED

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 39,606 hrs · 28,027 cycles

SHEAR CLIP AT FR 73 AND BTW STR 8L-10L FOUND CRACKED. SHEAR CLIP AT FR 73 AND BTW STR 8L-10L REMOVED AND INSTALLED

Part: ANGLE — CRACKED (ZONE 100) · airframe 39,606 hrs · 28,027 cycles

CRACK ON LH WING TO BODY FAIRING LOWER ANGLE #4 BTW FR 48-49. ON LH WING TO BODY FAIRING LOWER ANGLE #4 BTW FR 48-49 REPAIRED

Part: SUPPORT — CRACKED (ZONE 800) · airframe 39,606 hrs · 28,027 cycles

RH BAGGAGE DOOR MECHANISM UPPER SUPPORT AT STR 4 BTW FR 68-69 FOUND CRACKED. RH BAGGAGE DOOR MECHANISM UPPER SUPPORT AT STR 4R BTW FR 68-69 REMOVED AND REPLACED

Part: GUSSET — CORRODED (ZONE 100) · corrosion level 2 · airframe 39,606 hrs · 28,027 cycles

CF3, CENTER GUSSET BTW FR 53-45 CORRODED. CF3, CENTER GUSSET BTW FR 45-53 BLENDED AND FOUND OUT OF LIMIT. CF3, CENTER GUSSET BTW FR 53-45 REMOVED AND REPLACED.

Part: NUT — CORRODED (ZONE 200) · corrosion level 2 · airframe 39,606 hrs · 28,027 cycles

RH SILL BTW FR 60-61 FOUND CORRODED. CORRODED ANCHOR NUT REMOVED ON RH SILL BTW FR 60-61. CORRODED RH SILL BTW FR 60-61 FOUND OUT OF LIMITS. CORRODED RH SILL BTW FR 60-61 REMOVED AND REPLACED.

Part: SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 39,606 hrs · 28,027 cycles

LH SILL BTW FR 60-61 FOUND CORRODED. CORRODED ANCHOR NUT REMOVED ON LH SILL BTW FR 60-61. LH SILL BTW FR 60-61 CORRODED, FOUND OUT OF LIMITS. CORRDED LH SILL BTW FR 60-61 REMOVED. LH SILL BTW FR 60-61 REMOVED AND INSTALLED.

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 39,606 hrs · 28,027 cycles

SHEAR CLIP AT FR59 AND BTW STR 15L-16L FOUND CRACKED. AT FR59 BTW STR 15L-16L SHEAR CLIP REMOVED AND REPLACED

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 39,606 hrs · 28,027 cycles

CF3, RH ANGLE OMEGA BEAM OB AND IB BTW FR 48-50 CRACKED. CF3, RH AT FR51 ANGLE BTW ANGLE OMEGA BEAM OB AND IB 8 RIVETS REMOVED FOR ACCESS. CF3, RH ANGLE OMEGA BEAM OB AND IB BTW FR 48-50 REMOVED AND REPLACED.

Part: SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 39,606 hrs · 28,027 cycles

CF2 RH SILL BTW FR 29-35 CORRODED. AT CF2 RH SILL BTW R 29-35 SILL FOUND CORRODED OUT OF LIMIT. CF2 RH SILL BTW FR 29-39 REMOVED AND REPLACED

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 39,606 hrs · 28,027 cycles

SHEAR CLIP AT FR 72 AND BTW STR 17L-18L FOUND CRACKED. SHEAR CLIP AT FR72 AND BTW STR 17L-18L REMOVED AND REPLACED

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 39,606 hrs · 28,027 cycles

SHEAR CLIP AT FR73 AND BTW STR 16L-17L FOUND CRACKED. SHEAR CLIP AT FR73 AND BTW STR 16L-17L REMOVED AND REPLACED

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 39,606 hrs · 28,027 cycles

SHEAR CLIP AT FR 62 AND BTW STR 6R-8R FOUND CRACKED. AT FR62 AND BTW STR 6R-8R SHEAR CLIP REPLACED

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 39,606 hrs · 28,027 cycles

RH OMEGA BEAM AT FR 22 FLOOR DOUBLER FOUND CORRODED. AT RH OMEGA BEAM AT FR 22, DOUBLER FOUND CORRODED OUT OF LIMITS. DOUBLER REMOVED, DRILLED NEW HOLES FOR NEW DOUBLER. AT RH OMEGA BEAM AT FR22, NEW DOUBLER INSTALLED.

Part: DOUBLER — CORRODED (ZONE 200) · corrosion level 2 · airframe 39,606 hrs · 28,027 cycles

RH OMEGA BEAM AT FR20 FLOOR DOUBLER FOUND CORRODED. AT RH OMEGA BEAM AT FR20 DOUBLER FOUND CORRODED OUT OF LIMITS. DOUBLER REMOVED, DRILLED NEW HOLES FOR NEW DOUBLER. AT RH OMEGA BEAM AT FR20, NEW DOUBLER INSTALLED

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 39,606 hrs · 28,027 cycles

CF1 CENTER OMEGA BEAM BTW FR 18-20 FOUND CORRODED. AT CF1 CENTER OMEGA BEAM BTW FR 18-20 WIRES UNSECURED FOR ACCESS, CORROSION BLENDED OUT OF LIMIT. CF1 CENTER OMEGA BEAM BTW FR 19-24 REMOVED FOR REPLACEMENT. CF1 NEW CENTER OMEGA BEAM BTW FR 19-24 DRILLED. CF1 CENTER OMEGA BEAM BTW FR 19-24 REPLACED. AT CF1 CENTER OMEGA BEAM BTW FR 18-20 WIRE REINSTALLED.

Part: GUSSET — CORRODED (ZONE 200) · corrosion level 2 · airframe 39,606 hrs · 28,027 cycles

MIDDLE GUSSET BTW FR 18-23 FOUND CORRODED. AT CF1 MIDDLE GUSSET BTW FR 18-23 GUSSET FOUND CORRODED OUT OF LIMIT. GUSSET REMOVED. MIDDLE GUSSET BTW FR 18-23 REPLACED.

Part: SIGN — INOPERATIVE (ZONE 200) · airframe 39,411 hrs · 27,821 cycles

EMERGENCY EXIT LIGHT ON CEILING FWD AT ROW 18 IS INOPERATIVE. REMOVED AND REPLACED EMERGENCY EXIT SIGN. OPS CHECK SAT

Part: PROXIMITY SWITCH — FAULTED (ZONE 700) · airframe 39,401 hrs · 27,812 cycles

LG WOULD NOT GO UP. PERFORMED DVI OF MLG AND NLG. NO VISUAL DEFECTS NOTED. PROCEEDED TO INSPECT NLG AND MLG PROXIMITY SWITCHES. NO DEFECTS NOTED. INSPECT NLG AND MLG HARNESSES. NONE FOUND TO BE LOOSE OR VISUALLY DAMAGE. NO CANNON PLUGS WERE FOUND TO BE LOOSE. REMOVED AND REPLACED NLG PROX SWITCH. PERFORMED GEAR SWINGS. OPS CHECK SAT. GEAR TIMINGS WITHIN LIMITS. PERFORMED INSPECTION OF NOSE STRUT SERVICING. FOUND TO BE WITHIN LIMITS AT 9 1/4, 260 PSI AND 16 DEGREE C. PERFORMED TROUBLESHOOTING AND LG BREAKOUT BOX, FOUND CHANNEL 2 TO BE OFFLINE. REMOVED AND REPLACED LEGU AND LANDING GEAR CONTROL LEVEL. PERFORMED GEAR SWINGS AND CHANNEL 2 CAME BACK ONLINE. STILL SUSPECT MLG WOW PROX SWITCHES TO BE FAULTY. REMOVED AND REPLACED BOTH LH MLG (WOW) PROX SWITCHES AND THE RH MLG SHOCK ABSORBER WOW PROX SWITCH. REMOVED AND REPLACED RH TRAILING EDGE MLG WOW PROX SWITCH. PERFORMED GEAR SWINGS. OPS CHECK AND LEAK CHECK SAT. NO DEFECTS NOTED AT THIS TIME. WHILE PERFORMING GEAR SWINGS, FOUND NLG LEFT DOOR TO BE DELAYED. REMOVED AND REPLACED LEFT DOOR NLG ACTUATOR. PERFORMED NLG DOOR ACTUATOR OPS AND LEAK CHECK. NO DEFECTS FOUND. PERFORMED GEAR SWINGS. OPS CHECK AND LEAK CHECK SAT. NO DEFECTS NOTED AT THIS TIME.

Part: SIGN — INOPERATIVE (ZONE 200) · airframe 39,222 hrs · 27,634 cycles

INTERIOR EMERGENCY LIGHT ABOVE SERVICE DOOR INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT ABOVE SERVICE DOOR. OPS CHECK SAT

Part: LAMP — INOPERATIVE (ZONE 200) · airframe 39,222 hrs · 27,634 cycles

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

Part: SIGN — INOPERATIVE (ZONE 200) · airframe 38,697 hrs · 27,143 cycles

SERVICE DOOR UPPER EXIT LOCATING SIGN INOPERATIVE. REMOVED AND REPLACED SERVICE DOOR UPPER EXIT LOCATING SIGN. OPS CHECK SAT.

Part: LATCH — LACK OF LUBE · airframe 38,689 hrs · 27,142 cycles

EMERGENCY LANDING GEAR EXTENSION DOOR WONT OPEN. LUBRICATED FREE FALL ACTUATOR LATCH. OPS CHECK SAT, NO FURTHER DEFECTS NOTED.

Part: LAMP — DIM (ZONE 200) · airframe 38,636 hrs · 27,083 cycles

AFT CEILING EMERGENCY LIGHT INTERIOR DIM. REMOVED AND REPLACED EMERGENCY LAMP. OPS CHECK SAT.

Part: LAMP — INOPERATIVE (ZONE 200) · airframe 38,636 hrs · 27,083 cycles

CEILING EMERGENCY LIGHT INTERIOR AT SEATS 18 INOPERATIVE. REMOVED AND REPLACED EMERGENCY LAMP. OPS CHECK SAT

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 38,396 hrs · 26,843 cycles

EMERGENCY LIGHT SIGN INOPERATIVE ABOVE SERVICE DOOR. REMOVED AND REPLACED EMERGENCY BATTERY #2. OPS CHECK SAT.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 37,746 hrs · 26,230 cycles

GALLEY EMERGENCY EXIT SIGN INOPERATIVE. REMOVED AND REPLACED POWER SUPPLY 2 BATTERY. OPS CHECK SAT

Part: LIGHT — FAULTED (GALLEY) · airframe 37,745 hrs · 26,228 cycles

GALLEY EMERGENCY EXIT SIGN INOPERATIVE. GALLEY EMERGENCY LIGHT OPS CHECK SAT. NO DEFECTS NOTED.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 40,381 hrs · 27,481 cycles

CF2, FRAME 25, RH SHEAR CLIP FOUND CRACKED BTW STR 16R-17R. REPLACED.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 400,381 hrs · 27,481 cycles

CF2, FRAME 26, RH SHEAR CLIP FOUND CRACKED BTW STR 16R-17R. REPLACED.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 40,381 hrs · 27,481 cycles

CF2, FRAME 25, RH SHEAR CLIP FOUND CRACKED BTW STR 15R-16R. REPLACED

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 40,381 hrs · 27,481 cycles

CF2, FRAME 24, RH SHEAR CLIP FOUND CRACKED BTW STR 15R-16R. REPLACED

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 40,381 hrs · 27,481 cycles

CF1, FRAME 16, RH SHEAR CLIP FOUND CRACKED BTW STR 15R-16R. RH SHEAR CLIP FRAME 16 BTW STR 15R-16R REPLACED WITH NEW.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 36,543 hrs · 25,103 cycles

RH OVERWING EXTERNAL EMERGENCY LIGHT INSTALLED UPSIDE DOWN. REMOVED AND REORIENTED RH OVERWING EXTERNAL EMERGENCY LIGHT. OPS CHECK SAT

Part: LAMP — INOPERATIVE · airframe 36,506 hrs · 25,067 cycles

MCD EXTERNAL EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED EXTERNAL EMERGENCY LIGHT LAMP. OPS CHECK SAT.

Part: SEAT — LOOSE (CABIN) · airframe 35,858 hrs · 24,469 cycles

FWD PAX SEAT FEET AT SEATS 3, 5, 6, 8, 9, 10, 11, 19, 20, 21, 22 AND 23CD AND 7, 8, 9, 22A WERE FOUND TO BE SEVERELY LOOSE AND NOT FULLY TIGHTENED. RESCURED ALL DISCREPANT SEATS

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 35,637 hrs · 24,252 cycles

AFT CABIN CEILING PANEL EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED AFT CABIN CEILING PANEL EMERGENCY LIGHT. OPS CHECK GOOD

Part: NONE — INOPERATIVE · airframe 35,111 hrs · 23,767 cycles

EMERGENCY EXIT SIGN ABOVE FA CHAIR INOPERATIVE. REMOVED AND REPLACED EMERGENCY EXIT SIGN. OPS CHECK FAIL. REINSTALLED ORIGINAL EXIT SIGN. REMOVED AND REPLACED INVERTER. OPS CHECK SAT

Part: NONE — NONE · airframe 34,777 hrs · 23,460 cycles

VERY PUNGENT ODOR IN COCKPIT AND CABIN AFTER PERFORMING THE B TEST (14,000 FT). REMOVED AND REPLACED #2 WS TEMP CPNTROLLER. DID NOT FIX. FOUND TERMINAL (G) DAMAGED AT WIRE W102-0850-6N OF WINDSHIELD 2 HEATING SYSTEM. REMOVED AND REPLACED GROUND WIRE TERMINAL AT WIRE W102-0850-6N

Part: CONTROLLER — OVERHEATED (WINDOW HEAT) · airframe 34,765 hrs · 23,447 cycles

WINDSHIELD HEAT TERMINALS OVERHEATING PRODUCED BURNING SMELL. REMOVED AND REPLACED WINDSHIELD HEAT TEMP CONTROLLER. NO BURNING SMELL. OPS CHECK SAT.

Part: NOT REPORTED — NOT REPORTED · airframe 34,758 hrs · 23,442 cycles

RH WING PANEL 541CB RIB 14 LOWER ANGLE BRACKETS (2EA) ARE CRACKED. REPAIRED RH WING RIB 14 LOWER SHEAR CLIP FEET (3EA)

Part: NOT REPORTED — NOT REPORTED · corrosion level 2 · airframe 34,758 hrs · 23,442 cycles

CORROSION ON THE SKIN UNDER THE #2 RAR ANTENNA BASE. REPAIRED SKIN UNDER THE #2 RAR ANTENNA BASE.

Part: NOT REPORTED — NOT REPORTED · corrosion level 2 · airframe 34,758 hrs · 23,442 cycles

CORROSION ON THE OMEGA BEAM AT MULTIPLE PLACES FROM FRAME 22 TO 31 STRINGER 19R Y = 479.0. REMOVED AND REPLACED OMEGA BEAM FROM FR22 - FR31

Part: NOT REPORTED — NOT REPORTED · airframe 34,758 hrs · 23,442 cycles

1 EA DOUBLE DRILLED HOLE AT FRAME 21 STR 15L COMMON TO FLOOR SILL. REPAIRED HOLES AT FRAME 21 STR 15L COMMON TO FLOOR SILL.

Part: BULB — INOPERATIVE (EXTERIOR LIGHT) · airframe 33,552 hrs · 22,373 cycles

RH LATERAL FAIRING EMERGENCY LIGHT INOPERATIVE. R&R EMERGENCY LIGHT BULB. OPS CHECK SAT.

Part: STRUCTURE — CRACKED (LE) · airframe 32,900 hrs · 21,784 cycles

NR 3 LEADING EDGE RT SHOWS EVIDENCE OF CRACK AT NR 8 VORTILON. R & R RT LEADING EDGE NR 3. OPS CHECK SAT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 32,885 hrs · 21,770 cycles

EXTERNAL EMERGENCY LIGHT FWD OF LH WING INOPERATIVE. R&R EXTERNAL EMERGENCY LIGHT LAMP FWD OF LH WING. OPS CHECK SAT

Part: UNKNOWN — ODOR (CABIN) · airframe 32,023 hrs · 21,030 cycles

STRONG ODOR IN FLIGHT AND WENT AWAY AFTER PACK SHUTDOWN. PERFORMED APU/PACK RUN WITH NO FAULT FOUND. PERFORMED TI E145-7200-2019-01 AND FOUND NO DEFECTS. PERFORMED FIM WITH NO DEFECTS. PERFORMED ENGINE ANTI ICE TEST AND FOUND NO DEFECTS. PERFORMED RUNS/HIGH POWER RUNS AT MULTIPLE SETTINGS AND COULD NOT DUPLICATE THE PROBLEM.

Part: HOUSING — LOOSE (EMERGENCY LIGHT) · airframe 31,693 hrs · 20,734 cycles

MAIN DOOR HINGE EMERGENCY LIGHT INOPERATIVE. IDENTIFIED LOOSE HOUSING BONDING. RE SECURED AS REQUIRED. OPS CHECK SAT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 31,164 hrs · 20,239 cycles

MAIN DOOR EXTERNAL EMERGENCY LIGHT INOPERATIVE. R & R MAIN DOOR EXTERNAL EMERGENCY LIGHT. OPS CHECK SAT.

Part: ENGINE — SHUTDOWN (NR 2) · airframe 31,089 hrs · 20,171 cycles

E2 SHUTOFF DURING CRUISE FLIGHT (UNCOMMANDED). R&R #2 ENGINE. OPS AND LEAK CHECK SAT.

Part: SIGN — INOPERATIVE (CABIN) · airframe 29,909 hrs · 19,129 cycles

EMERGENCY EXIT SIGN ABOVE FLIGHT ATTENDANT SIGN INOPERATIVE. REMOVED, REPLACED AND INSTALLED NEW EMERGENCY EXIT SIGN ABOVE FLIGHT ATTENDANT SEAT.

Part: DOOR FRAME — CHAFED (CARGO DOOR) · airframe 29,909 hrs · 19,129 cycles

BAGGAGE DOOR INTERNAL FRAME HAS 6 CHAFF MARKS FWD LOWER CORNER FROM HARDWARE AS MARKED. PERFORMED REPAIR DOUBLER REPAIR TO BOTTOM FWD INTERNAL SKIN (FRAME AREA). DAMAGE LOCATED IN CARGO FROM STR 15L WITH DAMAGE AREA LENGTH - 3.75" WIDTH 4.0" AND DEPTH .018" CORROSION LEVEL 0.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 29,909 hrs · 19,129 cycles

CRACK IN RT I/B OMEGA BEAM SUPPORT BETWEEN FR 47-48. REMOVED AND REPLACED RT I/B OMEGA BEAM SUPPORT BETWEEN FR 47-48. CORROSION LEVEL 0.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 29,909 hrs · 19,129 cycles

CRACK IN RT O/B OMEGA BEAM SUPPORT BETWEEN FR 47-48. REMOVED AND REPLACED RT O/B OMEGA BEAM SUPPORT BETWEEN FR 46-50. CORROSION LEVEL 0. DAMAGE LENGTH 1.5".

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 29,909 hrs · 19,129 cycles

CRACK IN LT O/B OMEGA BEAM SUPPORT BETWEEN FR 47-48. REMOVED AND REPLACED LT O/B OMEGA BEAM SUPPORT BETWEEN FR 46-50. APPLIED TOP COAT TO FASTENERS ON LT O/B OMEGA BEAM SUPPORT BETWEEN FR 46-50. CORROSION LEVEL 0

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 29,909 hrs · 19,129 cycles

CENTER OMEGA BEAM FRAMES 59 TO 61 HAS CORROSION FOR NUT PLATES UNDERNEATH BEAM AND AT ATTACH L ANGLE BOTH SIDES FR61. BLENDED AREAS OF CORROSION FR59-FR61 FOUND TO BE OUTSIDE ALLOWABLE DAMAGE LIMITS. FABRICATED AND INSTALLED REPAIR DOUBLERS ON DAMAGED AREAS FR59 AND FR61. APPLIED SURFACE TO REPAIR DOUBLERS. CORROSION LEVEL 1 DAMAGE AREA 1: LENGTH - 0.75" WIDTH - 0.6" DEPTH 0.063" DAMAGE AREA 2: LENGTH - 1.0" WIDTH - 0.5" DEPTH - 0.020"

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 29,909 hrs · 19,129 cycles

CRACK IN LT I/B OMEGA BEAM SUPPORT BETWEEN FR 47-48. REMOVED AND REPLACED LT I/B OMEGA BEAM SUPPORT BETWEEN FR46-50. APPLIED TOPCOAT TO FASTENERS ON LT I/B OMEGA BEAM SUPPORT BETWEEN FR 46-50.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 28,862 hrs · 18,058 cycles

CABIN EMERGENCY PASSAGEWAY EXIT C/D SIDE INOP. R&R BULB. OPS CHECK SAT.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 28,862 hrs · 18,058 cycles

CABIN EMERGENCY PASSAGEWAY EXIT C/D SIDE INOP R&R BULB OPS CHECK SAT.

Part: GROUND WIRE — BROKEN (THERMAL SWITCH) · airframe 28,411 hrs · 17,623 cycles

APU BLEED LEAK MESSAGE. APU WAS SHUTDOWN AT GATE. RAN QRH AND MESSAGE PERSISTED. FOUND BROKEN GROUND WIRE ON THERMAL SWITCH 34. R & R THE THERMAL SWITCH.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 28,352 hrs · 17,572 cycles

EMERGENCY LIGHTS AT ROW 18 INOPERATIVE. R & R THE SIGN ASSY.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 27,720 hrs · 16,988 cycles

CEILING EMERGENCY LIGHT OVER ROW 18 INOP. R&R NR 4 EMERGENCY LIGHT INVERTER. OPS CHECK SAT.

Part: CONNECTOR — LOOSE (CABIN) · airframe 27,696 hrs · 16,969 cycles

CENTER AISLE EMERGENCY LIGHTING INOP. INSP FOUND THE CONNECTOR LOOSE. RESECURED ELECTRICAL CONNECTION. OPS CK SAT.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 27,657 hrs · 16,937 cycles

EMERGENCY EXIT SIGN AT ROW 18 NOT ILLUMINATING. R & R THE NR 4 INVERTER. OPS CHECKED GOOD. NO DEFECTS NOTED.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 27,653 hrs · 16,934 cycles

EMERGECNY EXIT LIGHT OVER ROW 18 INOPERATIVE. SPLICED CONNECTING WIRES TO LIGHT. OPS CHECKED SAT.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 27,593 hrs · 16,875 cycles

OVERWING EMERGENCY EXIT LIGHT FOR THE LT DOOR INOPERATIVE. REPLACED THE LAMP. OPS CHECKED GOOD.

Part: INVERTER — FAILED (EMERGENCY LIGHTS) · airframe 27,546 hrs · 16,833 cycles

EMERGENCY EXIT SIGNS BY F/A JUMPSEAT AND LT EMERGENCY EXIT INOPERATIVE. R & R THE STATIC INVERTER. OPS CHECKED GOOD. NO DEFECTS NOTED.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 27,523 hrs · 16,818 cycles

EMERGENCY LIGHT ABOVE FLT ATT JUMP SEAT INOPERATIVE. RESEATED BULB OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 27,491 hrs · 16,790 cycles

ROW 18C EMERGENCY EXIT LIGHT INOPERATIVE. R & R THE BULB. OPS CHECKED GOOD.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 27,470 hrs · 16,773 cycles

AFT EMERGENCY EXIT SIGN INOPERATIVE. R & R THE SIGN. OPS CHECKED GOOD.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHT) · airframe 27,470 hrs · 16,773 cycles

EXIT SIGN BY LEFT EMERGENCY EXIT INOPERATIVE. R & R THE SIGN. OPS CHECKED GOOD. NO DEFECTS NOTED.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 27,323 hrs · 16,629 cycles

LEFT EMERGGENCY EXIT EMERGENCY LIGHT INOPERATIVE. REPAIRED A WIRE AND OPS CHECKED GOOD. NO DEFECTS NOTED.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHTS) · airframe 27,212 hrs · 16,515 cycles

EMERGENCY LIGHT LEFT EXIT ROW 18 INOPERATIVE. CLEANED AND SECURED THE BATTERY CONNECTOR. OPS CHECKED GOOD.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 27,278 hrs · 16,581 cycles

ROW 18 EXIT LIGHT IS INOPERATIVE ON LEFT SIDE. RESET ACFT POWER, LIGHT IS OPERATIONAL.

Part: LIGHT — INOPERATIVE (ROW 18A) · airframe 27,241 hrs · 16,541 cycles

EMERGENCY LIGHT OVER ROW 18A INOPERATIVE. SEATED THE LIGHT STRIP. OPS CHECKED GOOD.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHT) · airframe 27,235 hrs · 16,536 cycles

LEFT EMERGENCY EXIT LIGHT AT ROW 18 IS INOPERATIVE. SECURED THE CONNECTOR PLUG.

Part: BATTERY — DISCHARGED (CABIN) · airframe 27,217 hrs · 16,519 cycles

EMERGENCY EXIT SIGN OVER 18 INOP. R&R NR 3 EMERGENCY LIGHT BATTERY. OPS CHECK SAT.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 27,217 hrs · 16,519 cycles

LEFT WING CENTER EMERGENCY EXIT LIGHT IS INOPERATIVE. CHARGED THE BATTERY. OPS CHECK GOOD.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHTS) · airframe 27,197 hrs · 16,498 cycles

ROW 18 EMERGENCY EXIT LIGHT INOPERATIVE. SECURED ELECTRICAL CONNECTOR TO ROW 18 EMG EXIT LIGHT. OPS CHECKED GOOD.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHTS) · airframe 27,187 hrs · 16,487 cycles

MULTIPLE EMERGENCY LIGHTS INOPERATIVE. SECURED THE CONNECTOR OPS CHECKED GOOD.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHTS) · airframe 27,184 hrs · 16,485 cycles

ROW 18A EMERGENCY AISLE LIGHT INOPERATIVE. SEATED THE CONNECTOR. OPS CHECKED GOOD.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 27,165 hrs · 16,465 cycles

NUMEROUS EXIT LIGHTS NOT ILLUMINATING. R & R THE BATTERY PACKS, OPS CHECKED GOOD. NO OTHER DEFECTS NOTED.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 27,165 hrs · 16,465 cycles

LEFT SIDE VERTICAL EMERGENCY EXIT ROW SIGN INOPERATIVE. EMERGENCY LIGHTS OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 27,165 hrs · 16,465 cycles

EMERGENCY LIGHT OVER SEAT 18A WILL NOT TEST. R & R EMERGENCY BATTERY PACK OPS CHECK GOOD.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHT) · airframe 27,078 hrs · 16,379 cycles

EMERGENCY LIGHT AT SEAT 18A INOPERATIVE. SECURED LIGHT CONNECTORS. OPS CHECKED GOOD.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHTS) · airframe 27,078 hrs · 16,379 cycles

EMERGENCY EXIT LIGHT AT SEAT 18A INOPERATIVE. REMOVED AND SECURED THE CONNECTORS. OPS CHECK GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 27,003 hrs · 16,304 cycles

EMERGENCY LIGHTS DO NOT COME ON. R & R 3 EMERGENCY LIGHT BATTERIES. OPS CHECK SATISFACTORY, NO DEFECTS NOTED. 2 ADDITIONAL 2013-1A, SN 90766, TT 25395.50, TC 17407 AND SN 102953, TT 16681.50, TC 11336.

Part: WIRE — UNSECURE (EMERGENCY LIGHT) · airframe 26,901 hrs · 16,201 cycles

LEFT EMERGENCY EXIT SIGN AT 18 IS NOT ILLUMINATING. SECURED WIRES AS REQUIRED. NO FURTHER DEFECTS NOTED.

Part: LIGHT — UNSECURE (CABIN) · airframe 26,881 hrs · 16,181 cycles

EMERGENCY EXIT LIGHT OVER AND AT WINDOW ARE NOT WORKING. SECURED BULB AS REQUIRED.

Part: SUPPORT — CORRODED (FRAME 60-61) · corrosion level 2 · airframe 25,673 hrs · 15,297 cycles

DURING C-CHECK, THE WASTE DUMP VALVE SUPPORT WAS FOUND TO BE CORRODED. MAINTENANCE R & R THE SUPPORT IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BEAM — CORRODED (FRAMES 65-68) · corrosion level 2 · airframe 25,673 hrs · 15,297 cycles

DURING C-CHECK THE CARGO DOOR CUTOUT LOWER BEAM WAS FOUND TO BE CORRODED. MAINTENANCE R & R THE BEAM IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: RIB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 25,673 hrs · 15,297 cycles

DURING C-CHECK THE VENTRAL FUEL TANK FORWARD WALL, RIB 1, WAS FOUND TO BE CORRODED BY THE FUEL LINE SUPPORT BRACKET. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EC5320-02082. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SHEAR TIE — CORRODED (FRAME 65) · corrosion level 2 · airframe 25,673 hrs · 15,297 cycles

SHV-DURING C-CHECK THE SHEAR CLIP AT FRAME 65 WAS FOUND TO BE CORRODED BETWEEN STRINGERS 15L-16L. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A SPLICE REPAIR IAW EC5335-03072. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FRAMES 59-61) · corrosion level 2 · airframe 25,673 hrs · 15,297 cycles

DURING C-CHECK, THE RT OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 59-61. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EC5310-01473, REV D. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: WIRE HARNESS — FAILED (CABIN LIGHTS) · airframe 22,557 hrs · 13,191 cycles

AT GATE, THE LOWER SIDEWALL LIGHT AT 1A CAUGHT ON FIRE AT THE CERAMIC CONNECTOR. MAINTENANCE INSPECTED, AND DEACTIVATED THE AFFECTED LIGHT CIRCUIT, REMOVED THE AFFECTED LIGHT BULB AND APPROVED THE ACFT FOR FERRY FLIGHT. MAINTENANCE R & R THE WIRING HARNESS, REACTIVATED THE CIRCUITS, OPS TESTED WITH NO DEFECTS NOTED, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (FRAME 78) · airframe 22,136 hrs · 12,900 cycles

DURING 1A INSPECTION, THE LT AFT FUSELAGE SKIN WAS FOUND TO BE CRACKED AT A RIVET ON FRAME 78, 1 RIVET BELOW STRINGER 06L. MAINTENANCE REMOVED THE DAMAGE AND INSTALLED A BUSHING REPAIR IAW DER APPROVED ETD2014-145-050302, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: HINGE FITTING — WORN (ZONE 500) · airframe 20,192 hrs · 11,678 cycles

DURING C-CHECK, THE LT GROUND SPOILER CENTER HINGE FITTING WAS FOUND TO BE WORN AND WOULD NOT RETAIN THE HAT BUSHINGS. MX REPAIRED THE FITTING IAW EC5740-01152. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: HINGE FITTING — WORN (ZONE 500) · airframe 20,192 hrs · 11,678 cycles

DURING C-CHECK, THE LT SPEED BRAKE CENTER HINGE FITTING WAS FOUND TO BE WORN AND WOULD NOT RETAIN THE HAT BUSHINGS. MX REPAIRED THE FITTING IAW EC5740-01152. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 20,192 hrs · 11,678 cycles

DURING C-CHECK THE RT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 23. MX REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EC5320-01443. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: HINGE FITTING — WORN (GROUND SPOILER) · airframe 20,192 hrs · 11,678 cycles

DURING C-CHECK, THE RT GROUND SPOILER CENTER HINGE FITTING WAS FOUND TO BE WORN AND WOULD NOT RETAIN THE HAT BUSHINGS. MX REPAIRED THE HINGE IAW EC5740-01152. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: HINGE FITTING — WORN (ZONE 600) · airframe 20,192 hrs · 11,678 cycles

DURING C-CHECK THE RT SPEED BRAKE CENTER HINGE FITTING WAS FOUND TO BE WORN AND WOULD NOT RETAIN THE HAT BUSHINGS. MX REPAIRED THE FITTING IAW EC5740-01152. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PUMP — FAILED (HYD SYSTEM) · airframe 16,614 hrs · 9,355 cycles

NR 1 HYD PUMP FAILED AND LOST ALL HYD FLUID IN FLIGHT. R & R NR 1 ENGINE DRIVEN HYD PUMP IAW AMM 29-10-03, LEAK AND OPS CHECKED GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: HEATER — MALFUNCTIONED (LAVATORY DRAIN) · airframe 12,361 hrs · 6,730 cycles

CAE - FLIGHT 2622, DURING PREFLIGHT INSPECTION THE CREW REPORTED A BURNING SMELL COMING FROM THE LAV SINK. MAINTENANCE INSPECTED THE AIRCRAFT AND PLACED THE DRAIN HEATER ON MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. MAINTENANCE RESET THE DRAIN HEATER CIRCUIT BREAKER INSPECTED THE LAV SINK AREA AND POTABLE WATER SYSTEM, VERIFIED OPERATION OF THE HEATED NIPPLES, COULD NOT DUPLICATE ANY BURNING ODOR, REMOVED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FIRE DETECTOR — DEFECTIVE (NR 1 ENGINE) · airframe 11,918 hrs · 6,477 cycles

MCI - FLT 2484 THE CREW REPORTED A NR 1 ENGINE FIRE DETECT FAIL MESSAGE ON TAXI OUT. THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED AND REPLACED THE NR 1 ENGINE FIRE DETECTOR. OPERATIONAL CHECKS WERE GOOD.

Part: HANDLE — OUT OF ALIGNMENT (CABIN DOOR) · airframe 10,944 hrs · 5,298 cycles

FLIGHT 2205 - EWR - FLIGHT CREW REPORTED MAIN CABIN DOOR HARD TO OPEN. EWR MX RE-ALIGNED AND RESECURED MAIN CABIN DOOR INTERNAL HANDLE AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: ENGINE — LEAKING (NR 1) · airframe 9,590 hrs · 5,187 cycles

CLE - DURING MAINTENANCE INSPECTION, AN OIL HAZE IN THE CABIN WAS REPORTED WITH 31 ENGINE HIGH OIL PRESSURE. MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE ENGINE, OPERATIONALLY AND LEAK CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 3 · airframe 9,450 hrs · 5,108 cycles

SHV - DURING C-CHECK LT OMEGA BEAM FROM FRAME 18-23 HAS CORROSION (LEVEL 3 LOCAL). MAINTENANCE REPAIRED LT OMEGA BEAM AT FRAMES 18-23 IAW EMB-145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ACM — FAILED (NR 1) · airframe 7,981 hrs · 4,288 cycles

FLIGHT NR 2022, THE CREW REPORTED A ELECTRICAL BURNING SMELL AND BURNED RUBBER SMELL AFTER CLIMBOUT. THE ACFT LANDED WITHOUT FURTHER INCIDENT. MX INSPECTED AND REPLACED THE NR1 AIR CYCLE MACHINE. OPS CHECKS WERE GOOD.

Part: B-NUT — LOOSE (HYDRAULIC SYS) · airframe 7,793 hrs · 4,192 cycles

IAH - FLIGHT 2240, THE CREW REPORTED A HYD 1 LOW QUANTITY IN CLIMB. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE TIGHTENED A LOOSE B-NUT ON THE ELBOW SWIVEL ADAPTER 90 DEGREE BEHIND THE LEFT HYD SERVICE PANEL, SERVICED THE HYDRAULICS, OPERATIONAL; AND LEAK CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — DEFECTIVE (CABIN) · airframe 6,596 hrs · 3,529 cycles

IAH - FLIGHT 2166, THE CREW REPORTED A BURNING ODOR IN THE CABIN NEAR ROW 12. THE AIRCRAFT LANDED AT IAH WITH NO INCIDENTS. MAINTENANCE INSPECTED THE AIRCRAFT, REMOVED AND REPLACED THE LAMP AT ROW 12BC, OPERATIONALLY CHECKED WITH NO DEFECTS. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DUCT CLAMP — LOOSE (NR 2 ENGINE) · airframe 4,873 hrs · 2,620 cycles

FLT 210 - SMF TO ONT - FLIGHT CREW REPORTED E2 ITT JUMPED 110 DEGREES AFTER T/O WITH WF INCREASE & N1 DROP-BLEED SELECTION ONLY 10 DEGREES. MX PERSONNEL RE-ADJUSTED AND TORQUED V-BAND CLAMP OPERATIONALLY CHECKED SATISFACTORY AND A/C WAS RELEASED TO RETURN FOR SERVICE.