N12136

Part: DOOR — OUT OF ADJUST (ZONE 800) · airframe 49,031 hrs · 32,311 cycles

MCD GETTING STUCK WHEN OPENING FROM INSIDE. PERFORMED OPS CHECK OF MAIN DOOR TO FUSELAGE SKIN ADJUSTMENT. FOLDING FLAP EDGE AND MAIN DOOR EXTERNAL HANDLE WONT CLOSE ALL THE WAY. PERFORMED RODS ADJUSTMENT. REMOVED AND REPLACED REAR LOCK BOX CABLE. REMOVED AND REPLACED MCD INTERNAL HANDLE ROD #2. PERFORMED MAIN DOOR TO FUSELAGE SKIN STEP. PERFORMED MAIN DOOR CABLED ADJUSTMENT. COMPLETED ADJUSTMENT OF MAIN DOOR. CABLE ADJUSTMENT SKIN STEP ADJUSTMENT, ROD ADJUSTMENT, FOLDING FLAP ADJUSTMENT, INTERNAL HANDLE ADJUSTMENT, TOPS CHECK/PRESSURIZATION SAT. DOOR OPEN AND CLOSE SAT.

Part: ROLLER — INOPERATIVE (ZONE 800) · airframe 48,995 hrs · 32,242 cycles

SIDE HINGED MAIN CABIN DOOR EXCESSIVE HARD TO CLOSE AND OPEN. REMOVED AND REPLACED UPPER AND LOWER AFT ROLLER. OPS CHECK SAT.

Part: LAMP — INOPERATIVE (ZONE 200) · airframe 48,952 hrs · 32,238 cycles

EMERGENCY LIGHTS OPS CHECK FAILED. INSTALLED ELECTRICAL CONNECTORS ON HEADLINER PANELS. EMERGENCY LIGHTS OPS CHECK SAT.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 48,952 hrs · 32,238 cycles

FOUND CORROSION ON RH OMEGA BEAM FR20 DOUBLER PIECE. REMOVED AND REPLACED DOUBLER PIECE AT RH OMEGA BEAM FR20.

Part: DOUBLER — CORRODED (ZONE 100) · corrosion level 2 · airframe 48,952 hrs · 32,238 cycles

CORROSION AROUND WATER SERVICE TUBING ON FUSELAGE DOUBLER PLATE. BLENDED CORROSION ON WATER SERVICE DOUBLER PLATE. DIMENSIONS FOR THE BLEND OUT IS 1.5"X.75"X.25" ORIGINAL THICKNESS IS .063" REMAINING IS .038" AND IS DETERMINED TO BE OUT OF LIMITS. REMOVED DOUBLER AT WATER SERVICE AREA. FABRICATED NEW DOUBLER. APPLIED PROTECTIVE COATINGS TO NEW DOUBLER. INSTALLED NEW DOUBLER AT WATER SERVICE AREA ON FUSELAGE.

Part: LINE — CORRODED (POTABLE WATER) · corrosion level 2 · airframe 48,952 hrs · 32,238 cycles

LIGHT CORROSION ON BOTH CONNECTING ENDS OF PORTABLE WATER OVERFLOW LINE LOWER SECTION. REMOVED PORTABLE WATER OVERFLOW LINE LOWER SECTION. REPLACED PORTABLE WATER OVERFLOW LINE LOWER SECTION.

Part: KEEPER — CORRODED (ZONE 300) · corrosion level 2 · airframe 48,952 hrs · 32,238 cycles

MODERATE CORROSION FOUND ON BOLT KEEPER AT SERVO TAB LINKAGE (LH ELEVATOR). REMOVED CORROSION ON BOLT KEEPER AT SERVO TAB LINKAGE. APPLIED TOP COAT FINISH ON BOLT KEEPER AT SERVO TAB LINKAGE.

Part: KEEPER — CORRODED (ZONE 300) · corrosion level 2 · airframe 48,952 hrs · 32,238 cycles

MODERATE CORROSION FOUND ON BOLT KEEPER AT SPRING TAB LINKAGE (RH ELEVATOR). REMOVED CORROSION ON BOLT KEEPER AT SPRING TAB LINKAGE ON RH ELEVATOR. PRIMED AND PAINTED BOLT KEEPER AT SPRING TAB LINKAGE ON RH ELEVATOR

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 48,952 hrs · 32,238 cycles

FRAME 60 BUTTLINE 0 FLOORBEAM HAS CORROSION AROUND NUTPLATES. REMOVED CENTER BEAM FOR FLIGHT CONTROL CABLES AT FR61. REMOVED BOTTOM CARBON FIBER PIECE ON FR61. REMOVED AND REPLACED GUSSET BETWEEN FR60 AND 61. INSTALLED BOTTOM CARBON FIBER PIECE ON FR61. INSTALLED CENTER BEAM FOR FLIGHT CONTROL CABLES AT FR61

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 48,952 hrs · 32,238 cycles

SERVICE DOOR FWD FLOOR SILL HAS CORROSION AT FRAME 20. REMOVED CORROSION AREA. PERFORMED EDDY CURRENT INSPECTION OF CORROSION REMOVAL AREA. NO DISCREPANCIES. PARTICULARLY FAB DOUBLER. APPLIED EPOXY TO DAMAGE AREA. FINISHED FAB DOUBLER. INSTALLED FOUBLER. APPLIED TOP COAT FINISH.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 48,952 hrs · 32,238 cycles

SERVICE DOOR AFT FLOOR SILL HAS CORROSION AT FRAME 22. REMOVED AND PARTIALLY LOCATED AND DRILLED NEW SERVICE DOOR SILL AT FR22. LOCATED AND DRILLED NEW SERVICE DOOR SILL AND PARTIALLY INSTALLED. FINISHED INSTALLING SERVICE DOOR SILL. REAPPLIED CIC TO NEW SERVICE DOOR SILL.

Part: ATTACH FITTING — CORRODED (ZONE 500) · corrosion level 2 · airframe 48,952 hrs · 32,238 cycles

SUSPECTED CORROSION FOUND ON THE OUTBOARD SIDE OF THE LH AILERON UPPER SHROUD ATTACHMENT. REMOVED MILD CORROSION ON THE OUTBOARD SIDE OF THE LH AILERON UPPER SHROUD OF THE LH AILERON UPPER SHROUD ATTACHMENT. PREP, PRIMED REWORK AREA ON THE OUTBOARD SIDE OF THE LH AILERON UPPER SHROUD ATTACHMENT.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 48,952 hrs · 32,238 cycles

SEAT TRACKS AT FRAME 31 AMD 33 RH FLOOR, AND FRAMES 53 AND 55 RH WALL SUSPECTED CORROSION. REMOVED AND REPLACED SEAT TRACK AT FR33 RH FLOOR FOR CORROSION OUT OF LIMITS. REMOVED AND REPLACED SEAT TRACK AT FR31 FOR CORROSION OUT OF LIMITS. BLENDED OUT SEAT TRACK AT FR53 AND 55 RH WALL AND FOUND NO CORROSION AT THIS TIME.

Part: CHARGER — INOPERATIVE (ZONE 200) · airframe 48,348 hrs · 31,660 cycles

MAIN CABIN DOOR EMERGENCY LIGHT AND FA OVERHEAD LIGHT INOPERATIVE. REMOVED AND REPLACED BULB. OPS CHECK FAIL. FOUND QUICK DICONNECT SP 7425 BROKEN. REPAIRED QUICK DISCONNECT. OPS CHECK FAIL. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY #1. OVERHEAD LIGHT OPS CHECK SAT, MCD LIGHT OPS CHECK FAIL. REMOVED AND REPLACED HOUSING. OPS CHECK FAIL. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY 1 CRADLE. OPS CHECK SAT. ALL LIGHTS WORK.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 46,876 hrs · 30,337 cycles

LT SIDE EMERGENCY EXIT SIGN DOES NOT LIGHT UP. PERFORMED EMERGENCY LIGHTS FUNCTIONAL CHECK AND FOUND ALL LIGHTS AND SIGNS ARE OPERATIONAL

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 46,702 hrs · 30,171 cycles

LOUD WHISTLE AND AIR FLOW COMING NEAR CA DV WINDOW IN CRUISE. PRESSURIZATION DIFFICULT TO CONTROL IN AUTO/MAN MODE. PRESSURIZED A/C. OPS CHECK PASSED. INSPECTED CA DV WINDOW AND FOUND MULTIPLE DISCREPANCIES ON FWD SEAL. REMOVED AND PREPPED SURFACE FOR SEAL AND SEALANT INSTALL. INSTALLED DV WINDOW SEAL. PERFORMED PRESSURIZATION LEAK CHECK, MANUAL MODE OPS CHECK, AND AUTO MODE OPS CHECK. CA DV WINDOW LEAK CHECK SAT. MANUAL AND AUTO MODE OPS CHECK SAT. INSTALLED CA DV WINDOW.

Part: LIGHT — FAULTY · airframe 46,488 hrs · 29,983 cycles

MCD EMERGENCY LIGHT OUT. REMOVED AND REPLACED MCD EMERGENCY LIGHT BULB. OPS CHECK FAILED. SSUPECT LIGHT ASSY TO BE FAULTY. REMOVED AND REPLACED MCD LIGHT ASSEMBLY. OPS CHECK SAT.

Part: LAMP — INOPERATIVE · airframe 45,624 hrs · 29,205 cycles

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

Part: LIGHT — INOPERATIVE · airframe 45,606 hrs · 29,186 cycles

EXIT SIGN ABOVE F/A JUMP SEAT NOT SECURE. RESECURED EXIT SIGN ABOVE FA JUMPSEAT

Part: SIGN — LOOSE · airframe 45,604 hrs · 29,184 cycles

EXIT SIGN ABOVE FA JUMPSEAT NOT SECURE. RESECURED EXIT SIGN ABOVE FA JUMPSEAT

Part: LIGHT — INOPERATIVE · airframe 45,525 hrs · 29,112 cycles

LIGHT STRIP ON FLOOR INOP ON ROW 1-3. R&R EMERGENCY LIGHT STRIP BETWEEN ROW 1 - 3

Part: NONE — DAMAGED · airframe 45,040 hrs · 28,667 cycles

SUPPLEMENTAL INFORMATION: REMOVED DAMAGE PORTION OF WIRES AND DAMAGED ELECTRICAL CONNECTOR PLUG TO #1 WINDSHIELD TEMP CONTROLLER. PINNED NEW ELECTRICAL CONNECTOR PLUG TO #1 WINDSHIELD TEMP CONTROLLER. PINNED ELECTRICAL CONNECTOR PINS FOR #1 WINDSHIELD TEMP CONTROLLER ELECTRICAL CONNECTOR PLUG. REPLACED ELECTRICAL POWER WIRE FROM #1 WINDSHIELD TEMP CONTROLLER TO WINDSHIELD. REMOVED AND REPLACED #1 WINDSHIELD TEMP CONTROLLER. REPLACED DAMAGED COCKPIT AIR CONDITION TUBING. OPS CHECK SAT.

Part: FLASHLIGHT ASSY — ODOR (CABIN) · airframe 44,452 hrs · 28,158 cycles

SMOKE ODOR AT FLT 190 AND REMAIN THE REMAINDER OF THE FLIGHT. REMOVED AND REPLACED BOTH THE CAPTAINS AND FLT ATTENDANTS FLASH LIGHT ASSEMBLIES.

Part: SIGN — BROKEN (EMERGENCY LIGHTS) · airframe 44,227 hrs · 27,939 cycles

EMERGENCY EXIT SIGN ABOVE FA JUMP SEAT IS BROKEN. RESECURED EMERGENCY EXIT SIGN ABOVE FA JUMP SEAT. NO FURTHER DEFECTS NOTED

Part: UNKNOWN — UNKNOWN · airframe 44,028 hrs · 27,759 cycles

SMOKE COMING FROM RT DIST PANEL IN COCKPIT. PERFORMED OPERATIONAL CHECK ON COOLING PACKS. NO SMOKE OF FAULTS DETECTED. OPS CHECK GOOD.

Part: INTERCOSTAL — CRACKED (NLG) · airframe 43,989 hrs · 27,722 cycles

NLG UPLOCK LH INTERCOATINAL CRACKED FWD INSIDE. REMOVED AND REPLACED NLG UPLOCK LH INTERCOSTAL.

Part: DOOR SILL — CORRODED (FRM 67) · airframe 43,989 hrs · 27,722 cycles

CORROSION ON CARGO DOOR CUTOUT LOWER SILL DOUBLER AT FR67 AND Y =-19". REMOVED AND REPLACED CARGO DOOR SILL DOUBLER AT AFT CARGO DOOR.

Part: ANGLE — CORRODED (FRMS 16-17) · airframe 43,989 hrs · 27,722 cycles

CORROSION ON 2 EA ANGLES AT PAX DOOR SILL BETWEEN FR 16 - FR 17. REMOVED AND REPLACED 2 EA ANGLES AT PAX DOOR SILL BETWEEN FR 16 - FR 17

Part: FLOORBEAM — CORRODED (FRM 59) · airframe 43,989 hrs · 27,722 cycles

AFT WET AREA, RH SIDE FLOOR BEAM IS CORRODED AT F59+19" AND Y+3.5". INSTALLED NEW UPPER BEAM CAP IN AFT WET AREA, RH SIDE FLOOR AT FR 59+19" AND Y+3.5".

Part: FLOORBEAM — CORRODED (FRM 58) · corrosion level 2 · airframe 43,989 hrs · 27,722 cycles

AFT WET AREA LH SIDE CROSS MEMBER FLOOR SUPPORT IS CORRODED AT F58+8" AND Y-8". REMOVED AND REPLACED LH FLOOR CROSS MEMBER SUPPORT AT F 58=8 AND Y-8.

Part: PROFILE — CORRODED (FRMS 18-19) · airframe 43,989 hrs · 27,722 cycles

CORROSION ON PANEL 231 FF SUPPORT PROFILE AT L EDGE BETWEEN FR 18-19. REMOVED AND REPLACED PROFILE FOR PANEL 231FF AT LH EDGE BETWEEN FRAME 18 AND 19

Part: DOUBLER — CORRODED (FRMS 65-68) · airframe 43,989 hrs · 27,722 cycles

CORROSION IN THE CARGO ON CENTER AT SECTION UPPER DOUBLER AT FR 65, 67, AND 68. REMOVED AND REPLACED CENTER HAT SECTION UPPER DOUBLER AT FR 65, 67, AND 68 IN CARGO.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 43,774 hrs · 27,535 cycles

FWD CABIN EMERGENCY LIGHTS INOPERATIVE. R & R EMERGENCY BATTERY POWER SUPPLY NR 1. OPERATIONS CHECK SATISFACTORY.

Part: DOUBLER — DAMAGED (LT WING LE) · airframe 43,625 hrs · 27,407 cycles

REPAIR DOUBLER ON LT WING LEADING EDGE 3 NOSE BETWEEN RIB 6-7. PATCH REPAIR ON LT WING LEADING EDGE 3 BETWEEN RIB 6-7 PERFORMED.

Part: SKIN — DENTED (FRAMES 19-21) · airframe 43,625 hrs · 27,407 cycles

MULTIPLE DENTS ON LT CENTER FUSELAGE SKIN 1 BETWEEN FR 19-21 AND BETWEEN STR 11L-14L. PATCH REPAIR ON LT FUSELAGE SKIN 1 BETWEEN FR 19-20 AND STR 13L-14L PERFORMED.

Part: SKIN — DENTED (LT WING LE) · airframe 43,625 hrs · 27,407 cycles

DENT ON LT WING LEADING EDGE 3 NOSE BETWEEN RIB 3-4. DENT ON LT WING LEADING EDGE NR 3 BETWEEN RIB 3-4 REPAIRED.

Part: SKIN — DENTED (RUDDER TE) · airframe 43,625 hrs · 27,407 cycles

DENT WITH A CREASE FOUND ON RT SIDE OF THE TRAILING RUDDER 1.10" ABOVE RIB ZV 2357.0 AND 3.90" AFT OF FRONT SPAR. PATCH REPAIR ON RT SKIN OF TRAILING RUDDER 1.00 ABOVE RIB ZV 2357.0 AND 3.900 PO AFT OF FRONT SPAR.

Part: SKIN — CRACKED (FRAME 79) · airframe 43,625 hrs · 27,407 cycles

REAR FUSELAGE 2 LT SKIN, CRACKS FOUND AROUND RIVET ON FR 79 AND BETWEEN STR 5L-6L. FOR INVESTIGATION, PAINT REMOVED ON DAMAGED SKIN AREA, AFTER 79 AND BETWEEN STR 5L-6L. FASTENER AND SKIN DAMAGE AT REAR FUSE 2 FR 79 BETWEEN STR 5-6L REMOVED. FASTENER DIAMETER 0.161 SKIN REWORK DIAMETER 0.438. REAR FUSE 2 LT CRACKED SKIN AT FR 79 BETWEEN STR 5-6L REPAINTED. AT FRAME 79 BETWEEN STR 5L-6L METAL REPROTECTED.

Part: SKIN — CRACKED (FRAME 79) · airframe 43,625 hrs · 27,407 cycles

CRACK ON RT REAR FUSE 2, AROUND RIVET, ON FR 79 AND BETWEEN STR 6R-7R. ON RT REAR FUSE 2, ON FR 79 AND BETWEEN STR 6R-7R, PAINT STRIPPED FOR INVESTIGATION. RIVET AND SKIN DAMAGE ON RT FUSE 2 ON FR 79 BETWEEN STR 6-7R REMOVED. FASTENER DIAMETER 0.161, SKIN REWORK DIAMETER 0.438. CRACK ON RT REAR FUSE 2 SKIN ON FR 79 BETWEEN STR 6-7R REPAIRED. AT FRAME 79 AND BETWEEN STR 6R-7R METAL REPROTECTED.

Part: SKIN — LOOSE (FRAME 77) · airframe 43,625 hrs · 27,407 cycles

REAR FUSELAGE 2 LT SKIN, CRACKS FOUND AROUND RIVET ON FR 77 AND BETWEEN STR 8L-9L. FOR INVESTIGATION, PAINT REMOVED ON DAMAGED SKIN AREA, AT FR 77 AND BETWEEN STR 8L-9L. FASTENER AND SKIN DAMAGE ON FR 77 BETWEEN STR 8-9L REMOVED. FASTENER DIAMETER .161. SKIN REWORK .438. CRACKED REAR FUSE 2 LT SKIN ON FR 77 BETWEEN STR 8-9L REPAIRED. AT FRAME 77 AND BETWEEN STR 8L-9L METAL REPROTECTED.

Part: SKIN — CRACKED (FRAME 79) · airframe 43,625 hrs · 27,407 cycles

REAR FUSELAGE 2 LT SKIN, CRACKS FOUND AROUND RIVER ON FR 79 AND BETWEEN STR 3L-4L. FOR INVESTIGATION, PAINT REMOVED ON DAMAGED SKIN AREA, AT FR 79 AND BETWEEN STR 3L-4L. FASTENER AND SKIN DAMAGE ON REAR FUSE 2 FR 79 BETWEEN STR 3-4L REMOVED. FASTENER DIAMETER 0.161. SKIN REWORK DIAMETER 0.438. CRACKED REAR FUSELAGE 2 LT SKIN AT FR 79 BETWEEN STR 3-4L REPAIRED. AT FRAME 79 AND BETWEEN STR 3L-4L REPROTECTED.

Part: SKIN — CRACKED (FRAME 79) · airframe 43,625 hrs · 27,407 cycles

REAR FUSELAGE 2 LT SKIN, CRACKS FOUND AROUND RIVET ON FR 79 AND BETWEEN STR 6L-7L. FOR INVESTIGATION, PAINT REMOVED ON DAMAGE SKIN AREA AT FR 79 AND BETWEEN STR 6L-7L. FASTENER AND SKIN DAMAGE LT FUSELAGE 2 FR 79 BETWEEN STR 6-7L REMOVED. FASTENER DIAMETER 0161. REWORK DIAMETER 0.438. REAR FUSELAGE 2 LT CRACKED SKIN AT FR 79 BETWEEN FR 6-7L REPAIRED. AT FRAME 79 AND BETWEEN STR 6L-7L, METAL REPROTECTED.

Part: SKIN — CRACKED (FRAME 79) · airframe 43,625 hrs · 27,407 cycles

CRACK ON RT REAR FUSE 2, AROUND RIVET, ON FR 79 AND BETWEEN STR 3R-4R. ON RT REAR FUSE 2, ON FR 79 AND BETWEEN STR 3-4R PAINT STRIPPED FOR INVESTIGATION. RIVET AND SKIN DAMAGE ON RT FUSE 2 ON FR 79 BETWEEN STR 3-4R REMOVED. FASTENER DIAMETER 0.161. SKIN REWORK DIAMETER 0.438. CRACK ON RT REAR FUSE 2 AT FR 79 BETWEEN STR 3-4 REPAIRED. AT FRAME 79 AND BETWEEN STR 3R-4R, METAL REPROTECTED.

Part: SKIN — CRACKED (FRAME 78) · airframe 43,625 hrs · 27,407 cycles

CRACK ON RT REAR FUSE 2, AROUND RIVET, ON FR 78 AND BETWEEN STR 5R-6R. ON RT REAR FUSE 2, ON FR 78 AND BETWEEN STR 5R-6R, PAINT STRIPPED FOR INVESTIGATION. RIVET AND SKIN DAMGE ON RT REAR FUSE 2 ON FR 78 BETWEEN STR 5-6R REMOVED. FASTENER DIAMETER 0.161. SKIN REWORK DIAMETER 0.438. CRACK ON RT REAR FUSE 2 SKIN ON FR 78 AND BETWEEN STR 5R-6R REPAIRED. AT FRAME 78 AND BETWEEN STR 5R-6R METAL REPROTECTED.

Part: SKIN — CRACKED (FRAME 79) · airframe 43,625 hrs · 27,407 cycles

CRACK ON RT REAR FUSE 2, AROUND RIVET, ON FR 79 AND BETWEEN STR 5R-6R. ON RT REAR FUSE 2, ON FR 79 AND BETWEEN STR 5R-6R, PAINT STRIPPED FOR INVESTIGATION. RIVET AND SKIN DAMAGE REMOVED ON RT REAR FUSE 2 ON FR 79 BETWEEN STR 5-6R. FASTENER DIAMTETER 0.161 SKIN REWORK DIAMETER 0.438. CRACK ON RT REAR FUSE 2 SKIN AT FR 79 BETWEEN STR 5-6R REPAINTED. AT FRAME 79 AND BETWEEN STR 5R AND 5-6R METAL REPROTECTED.

Part: SKIN — CRACKED (FRAME 78) · airframe 43,625 hrs · 27,407 cycles

REAR FUSELAGE 2 LT SKIN, CRACKS FOUND ON FR 78 AND BETWEEN STR 5L-6L. FOR INVESTIGATION PAINT REMOVED ON DAMAGED SKIN AREA, AT FR 78 AND BETWEEN STR 5L-6L. FASTENER AND SKIN DAMAGE ON REAR FUSE 2 FR 78 BETWEEN STR 5-6L REMOVED. FASTENER DIAMETER .161. SKIN REWORK 0.438. CRACK REAR FUSE 2 LT SKIN AT FR 78 BETWEEN STR 5-6L REPAIRED. AT FRAME 78 AND BETWEEN STR 5-6L METAL REPROTECTED.

Part: SKIN — LOOSE (FRAME 77) · airframe 43,625 hrs · 27,407 cycles

REAR FUSELAGE 2 SKIN, CRACKS FOUND AROUND RIVET ON FR 77 AND BETWEEN STR 3L-4L. FOR INVESTIGATION, PAINT REMOVED ON DAMAGED SKIN AREA, AT FR 77 AND BETWEEN STR 3L-4L. FASTENER AND SKIN DAMAGE ON FR 77 BETWEEN STR 3-4L REMOVED. FASTENER DIAMETER .161 SKIN REWORK DIAMETER .438. CRACKED REAR FUSE 2 LT SKIN AT FR 77 BETWEEN STR 3-4L REPAIRED. AT FRAME 77 AND BETWEEN STR 3L-4L METAL REPROTECTED.

Part: SIDEWALL PANEL — MISINSTALLED (OVERWING EXIT) · airframe 43,625 hrs · 27,407 cycles

IN CABIN, THE SIDEWALLS ARE NOT PROPERLY INSTALLED AROUND THE OVERWINGS EMERGENCY EXIT DOORS. CABIN, LT SIDEWALL REINSTALLED PROPERLY AROUND OVERWINGS EMERGENCY EXIT DOORS. CABIN, RT SIDEWALL REINSTALLED PROPERLY AROUND OVERWINGS EMERGENCY CABIN RT SIDEWALL BRACKET UPPER FWD GLUED.

Part: SKIN — DAMAGED (RT WING) · airframe 43,625 hrs · 27,407 cycles

REPAIR DOUBLER ON RT WING LEADING EDGE 2 BETWEEN RIB 4-5. SPLICE 613AR, 612AR, AND RT LEADING EDGE NR 2 REMOVED FOR ACCESS. PICOLO TIBE REMOVED FROM RT LEADING EDGE NR 2. LEADING EDGE NR 2 ON RT WING HAS BEEN DECLARED UNREPAIRABE DUE TO A DENT. PICOLO TUBE INSTALLED RT LEADING EDGE NR 2. INSTALLED A SERVICEABLE LEADING EDGE NR 2. INSTALLED SPLICE 613AR AND 612AR.

Part: SEAL — DEBONDED (EMERGENCY EXIT) · airframe 43,625 hrs · 27,407 cycles

COCKPIT EMERGENCY EXIT, COPILOT SIDE, STRIP SEAL DISBONDED ON SURROUND FRAME AND HARD TO OPEN. COCKPIT EMERGENCY EXIT COPILOT SIDE, STRIP SEAL SURROUND FRAME REPAIRED. COCKPIT EMERGENCY CO-PILOT ADJUSTMENT CUT OUT.

Part: LATCH — BROKEN (MLG RELEASE DOOR) · airframe 43,625 hrs · 27,407 cycles

LATCH BROKEN ON EMERGENCY LANDING GEAR FREE FALL DOOR ON COCKPIT FLOOR, UNABLE TO OPEN. LATCH REPLACED ON EMERGENCY LANDING GEAR FREE FALL DOOR ON COCKPIT FLOOR.

Part: SKIN — GOUGED (LT WING) · airframe 42,893 hrs · 26,806 cycles

*MAJOR REPAIR* L/H LOWER WING SKIN HAS GOUGE BETWEEN I/B AND O/B FLAPS(DMI#70062907...... REPAIRED L/H LOWER WING SKIN IAW EO-EMB145-57-023-0

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 42,772 hrs · 26,707 cycles

STOP SIGN DOUBLERS AT FRM 20 AND FRM 22 HAVE CORROSION ... REMOVED AND REPLACED STOP SIGN DOUBLERS AT FRM 20 AND FRM 22 IAW SRM 51-40-02

Part: ANGLE — CORRODED (DOOR FRAME) · airframe 42,772 hrs · 26,707 cycles

Z ANGLE CARGO DOOR LOWER FRM HAS CORROSION. REMOVED AND REPLACED Z ANGLE CARGO DOOR LOWER FRM.

Part: DOOR SILL — GOUGED (FUSELAGE) · airframe 42,772 hrs · 26,707 cycles

L/H FLOOR SILL FRM 68 TO FRM 71 IS GOUGED.... REMOVED AND REPLACED L/H FLOOR SILL PER SRM 51-40-02

Part: SUPPORT ANGLE — CRACKED (LT WING FAIRING) · airframe 42,772 hrs · 26,707 cycles

L/H FWD WING TO FUSELAGE FAIRING ANGLE SUPPORT IS CRACKED. REMOVED AND REPLACED L/H FWD WING TO FUSELAGE FAIRING ANGLE SUPPORT...

Part: FLOOR SUPPORT — CORRODED (FRAME 20) · airframe 42,772 hrs · 26,707 cycles

CABIN FLOOR SUPPORT L/H FRM 20 CORRODED THROUGH STRUCTURE. REMOVED AND REPLACED CABIN FLOOR SUPPORT AT FR 20...

Part: SHEAR TIE — CRACKED (FRAME 67) · airframe 42,772 hrs · 26,707 cycles

SHEAR CLIP AT FR 67 AT STR 6L 7L IS CRACKED. REMOVED AND REPLACED SHEAR CLIP AT STR 6 AT FR 67 IAW SRM 51-40-02

Part: WEB — CORRODED (CARGO RAMP) · airframe 42,772 hrs · 26,707 cycles

FWD CARGO RAMP WEB HAS CORROSION. REMOVED AND REPLACED FWD CARGO RAMP WEB ANGLE...

Part: SHEAR TIE — CRACKED (FRAME 68) · airframe 42,772 hrs · 26,707 cycles

SHEAR CLIP AT FR 68 AT STR 6L TO 9L IS CRACKED. REMOVED AND REPLACED SHEAR CLIP.....

Part: ANGLE — CORRODED (CARGO RAMP) · airframe 42,772 hrs · 26,707 cycles

CARGO RAMP FWD ANGLE HAS SURFACE CORROSION ON LOWER MOUNTING HOLE. REMOVED AND REPLACED CARGO RAMP FWD ANGLE...

Part: RADAR — INOPERATIVE (WEATHER SYSTEM) · airframe 42,210 hrs · 26,268 cycles

WEATHER RADAR FAIL. R&R WEATHER RADAR. OPS CHECK GOOD.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 41,968 hrs · 26,089 cycles

BAGGAGE DOOR INDICATION READ OPEN IN FLIGHT. CREW COULD NOT MAINTAIN CABIN PRESSURE. CHECKED INDICATION SWITCH IN CARGO DOOR. FOUND NO DISCREPANCIES. SUSPECT VENT PANEL ON CARGO DOOR NOT CLOSED PROPERLY. C/W PRESSURIZATION CHECK. OPS CHECK GOOD AND DOOR SHOWED CLOSED THROUGH OUT TEST.

Part: SENSE LINE — DEFECTIVE (BLEED AIR SYS) · airframe 41,514 hrs · 25,750 cycles

BLEED 1 AND 2 OVERTEMP. R&R REFERANCE LINE BELOW CARGO FLOOR FOR HIGH TEMP THERMOSTATS. OPS CHECK GOOD.

Part: SWITCH — OUT OF ADJUST (PAX DOOR) · airframe 41,103 hrs · 25,432 cycles

A/B TO LESS THAN 80 KTS FOR MAIN CABIN DOOR OPEN INDICATION ON EICAS. DEFERRER DOOR WARNING. READJUSTED PAX DOOR MICRO SWITCHES. OPS CHECK GOOD.

Part: DOOR — OUT OF ADJUST (CABIN) · airframe 40,844 hrs · 25,225 cycles

ON POST FLIGHT. FOUND MAIN CABIN DOOR DIFFICULT TO OPEN. ADJUSTED MAIN DOOR AND OPS CHECK GOOD AT THIS TIME.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 40,180 hrs · 24,672 cycles

AFT FA FLASHLIGHT WILL NOT ILLUMINATE YET IS SHOWING CHARGING. R&R FA FLASHLIGHT, OPS CHECK GOOD.

Part: CARBON SEAL — LEAKING (NR 1 ENGINE)

OILY SMELL WITH APPARENT HAZE IN CABIN. R&R 0 CARBON SEAL ON NR 1 ENGINE. PERFORMED OPS CHECK. OPS CHECK GOOD. PERFORMED LEAK CHECK. NO LEAKS NOTED. PERFORMED VIBRATION TESTS. NO FAULTS NOTED.

Part: O-RING — NOT REPORTED (NR 1 ENGINE) · airframe 40,142 hrs · 24,641 cycles

OIL PRESSURE DROPPED ON NR 1 ENGINE. OIL QUANTITY SHOWED 3 QTS AT CRUISE. PERFORMED PRECAUTIONARY ENGINE SHUTDOWN CHECKLIST AND LANDED WITHOUT INCIDENT. REMOVED NR 1 GENERATOR, REPLACED O-RING AND INSPECTED FOR OIL LEAK. REPLACED NR 1 GENERATOR. PERFORMED OPS CHECK OF GENERATOR. OPS CHECK GOOD. PERFORMED NR 1 ENGINE HIGH POWER RUN. OIL PRESSURE AND QUANTITY REMAINED STABLE AND WITHIN LIMITS. NO FAULTS FOUND.

Part: DOOR — OUT OF ADJUST (MAIN PAX) · airframe 39,962 hrs · 24,497 cycles

CABIN DOOR DIFFICULT TO OPEN & CLOSE. PERFORMED ADJUSTMENT AND TEST OF MAIN PAX DOOR. OPS CHECK GOOD AT THIS TIME.

Part: DOOR — LACK OF LUBE (MAIN PAX) · airframe 39,449 hrs · 24,053 cycles

MAIN CABIN DOOR DIFFICULT FOR FA TO OPEN. CLEANED AND LUBED MAIN CABIN DOOR PERFORMED OPS CHECKED.

Part: VALVE — MALFUNCTIONED (BLEED AIR SYS) · airframe 38,362 hrs · 23,135 cycles

BLEED 1 OVERTEMP IN ICING ON EICAS. PERFORMED QRH THEN GOT BLEED 2 OVERTEMP EXITED ICING. REMOVED AND REPLACED FAN AIR VALVE AND OUTLET TEMP SENSOR FOR BLEED SYSTEM 1. BOTH SYSTEMS OPS CHECK GOOD. TEMP SENSOR P/N: 0132ADT, S/N: E0380

Part: UNKNOWN — MALFUNCTIONED (BLEED AIR SYS) · airframe 37,626 hrs · 22,515 cycles

BLEED 1 LEAK IN FLIGHT. INSPECTED LT AND RT BLEED BOTH ENG'S AT PACK CARGO & AT AVIONICS NO LEAK NOTED. RAN BOTH ENGINES COULD NOT DUPLICATE.

Part: CABIN PRESSURE — MALFUNCTIONED · airframe 36,922 hrs · 21,949 cycles

LOSS OF CABIN PRESSURIZATON IN FLT, STABILIZED CABIN PRESSURE AT 3.5. COMPLIED WITH GROUND PRESSURIZATION IN AUTO AND MANUAL MODES IAW AMM 21-31-00. OPS CHECKED GOOD AT THIS TIME.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 34,655 hrs · 20,243 cycles

DURING MX INSPECTION, BOTH EXTERIOR OVERWING EMERGENCY EXIT LIGHTS WERE DISCOVERED INOPERATIVE. MX R & R THE NR 4 EMERGENCY LIGHT SYSTEM BATTERY CHARGER WITH OPS CHECK GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONTACT — DIRTY (EMERGENCY LIGHT) · airframe 33,503 hrs · 19,435 cycles

AIRCRAFT FWD EMERGENCY EXIT SIGN LIGHT INOPERATIVE. MAINTENANCE CLEANED CONTACTS FOR FWD EMERGENCY EXIT SIGN LIGHT IAW SWPM 20-21-00, OPS CHECK GOOD. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,561 hrs · 18,806 cycles

DURING MAINTENANCE INSPECTION THE MAIN DOOR EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. MX R & R THE MAIN DOOR EMERGENCY LIGHT ASSY WITH OPS CHECKED GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: GARLOCK SEAL — DAMAGED (NR 2 ENGINE) · airframe 30,557 hrs · 17,511 cycles

THE CREW REPORTED AN NR 2 ENGINE LOW OIL PRESSURE, ACFT DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE R & R NR 4 GENERATOR GARLOCK SEAL, OPS AND LEAK TESTED WITH NO DEFECTS, ACFT APPROVED FOR RETURN TO SERVICE. ON REPOSITION FLIGHT, CREW REPORTED THAT THE NR 2 ENGINE LOST OIL AT 1QT PER 5 MINUTES, WHEN LEVEL REACHED 5QTS CREW RAN QRH AND SHUTDOWN ENGINE. ACFT DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND NR 4 GENERATOR TO BE DAMAGING THE GARLOCK SEAL. MAINTENANCE R & R THE NR 4 GENERATOR AND AFFECTED GARLOCK SEAL, OPS AND LEAK CHECKED WITH NO DEFECTS NOTED, AND ACFT APPROVED FOR RETURN TO SERVICE.

Part: DOOR FRAME — CORRODED (ZONE 800) · airframe 29,196 hrs · 16,631 cycles

C-CHECK, THE CARGO DOOR FWD LWR SIDE WAS FOUND WITH 3 NUTPLATES SURROUNED BY CORROSION. MX CUT OUT THE DAMAGE AND INSTALL A FILLER WITH A INTERNAL DOUBLER IAW EC 52-30-10304.

Part: FLOOR SUPPORT — CORRODED (CENTER FUSELAGE) · airframe 29,196 hrs · 16,631 cycles

C-CHECK, CORROSION WAS FOUND ON THE RT FLOOR SUPPORT AT NUTPLATES BETWEEN FRAME 18 AND 19. MX BLENDED CORROSION BEYOND LIMITS. REMOVED THE DAMAGE PART AND LOCATED AND PLACED A NEW PART, REF SRM 51-40-02.

Part: DOUBLER — CORRODED (FRAME) · airframe 29,196 hrs · 16,631 cycles

C-CHECK, CORROSION FOUND AT THE BOTTOM OF LT CARBON FIBER FRAME SUPPORT AT FRAME 61. MX REMOVED DOUBLER ALODINED AND INSTALL A NEW DOUBLER IAW SRM 51-40-02. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 29,196 hrs · 16,631 cycles

C-CHECK, CORROSION WAS FOUND AROUND THREE NUTPLATES ON THE CENTER OMEGA BEAM AT FRAME 15 TO 16. MX REMOVED THE CORROSION AND REPLACED A NEW DIGITIAL AND REPAIR DOUBLERS REF SRM 51-40-02. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 26,196 hrs · 16,631 cycles

C-CHECK,CORROSION WAS FOUND ALONG THE RT OTBD FLOOR SUPPORT AT FRAME 41 THRU 47. MX R & R THE PART IAW SRM 53-23-00.

Part: SILL — CORRODED (CARGO DOORWAY) · airframe 29,196 hrs · 16,631 cycles

C-CHECK,THE BAGGAGE DOOR LOWER SILL WAS FOUND CORRODED AROUND THE SCREW HOLES FOR THE DOOR EDGE TRIM. MX REMOVED ALL CORROSION AND INSTALL NEW PARTS IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (CENTER FUSELAGE) · airframe 29,196 hrs · 16,631 cycles

CORROSION WAS FOUND ON THE LT OMEGA BEAM IN 2 AREAS BETWEEN FRAMES 59 THRU 61. MX R & R IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (CENTER FUSELAGE) · airframe 29,196 hrs · 16,331 cycles

C-CHECK, CORROSION WAS FOUND IN 2 AREAS OF THE LT FLOOR SUPPORT BETWEEN FRAMES 59 THRU 61. MX R & R A NEW PART IAW SRM 51-40-02 AND 51-20-03.

Part: FLANGE — CORRODED (RT ENG) · airframe 29,196 hrs · 16,631 cycles

C-CHECK, THE RT ENGINE HAD MINIOR CORROSION AT THE 12 O'CLOCK POSITION. MX REMOVED THE LIGHT CORROSION IAW SRM 51-10-03. RESTORED SURFACE PROTECTION IAW CPM 51-21-04. ALLOWABLE DAMAGE IAW EC7230-01075. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 29,196 hrs · 16,631 cycles

C-CHECK, CORROSION WAS FOUND ALONG THE LT OTBD FLOOR SUPPORT BETWEEN FRAME 36 TO 41. MX R & R IAW SRM 53-23-00.

Part: FRAME — CRACKED (FUSELAGE) · airframe 29,196 hrs · 16,631 cycles

C-CHECK, FRAME 10 WAS FOUND CRACKED NEAR THE DV WINDOW DRAIN. MX R & R FRAME IAW 53-11-00.

Part: FLOOR SUPPORT — CORRODED (CENTER FUSELAGE) · airframe 29,196 hrs · 16,631 cycles

C-CHECK , CORROSION WAS FOUND ON THE RT OMEGA BEAM IN 3 AREAS BETWEEN FRAME 59 AND 61. MX REMOVED THE CORROSION AND WAS OUT OF LIMITS. REMOVED THE DAMAGED PART AND DRILLED NEW PART AND INSTALL REF SRM 51-40-02. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 29,196 hrs · 16,631 cycles

C-CHECK, CORROSION WAS FOUND ON THE LT OTBD FLOOR SUPPORT FROM FRAME 23 THRU 35. REMOVED CORROSION AND FOUND BEYOND LIMITS. REPLACED FLOOR SUPPORT IAW SRM 53-23-00.

Part: FLOOR SUPPORT — CORRODED (CENTER FUSELAGE) · airframe 29,196 hrs · 16,631 cycles

C-CHECK, THE LT FLOOR SUPPORT WAS FOUND CORRODED FROM FRAME 41 THRU 52. MX R & R IAW SRM 51-40-02.

Part: FLANGE — CORRODED (LT ENGINE) · airframe 29,196 hrs · 16,631 cycles

C-CHECK, THE LEFT ENGINE HAD SURFACE CORROSION AT THE 12 O'CLOCK POSITION. MX REMOVED THE SURFACE CORROSION ON REAR FLANGE IAW SRM 51-10-03. RESTORED SURFACE PROTECTION REF CPM 51-21-04. ALLOWABLE DAMAGE IAW EC 7230-01075. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 29,196 hrs · 16,631 cycles

RIGHT OMEGA BEAM CORRODED BEYOND LIMITS AFTER BLEND OUT. R & R GUSSET.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 29,196 hrs · 16,631 cycles

OMEGA BEAM IS CORRODED BEYOND LIMITS AFTER BLEND-OUT IN 2 AREAS. REMOVED AND REPLACED GUSSET.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 29,196 hrs · 16,631 cycles

RIGHT FLOOR SUPPORT AT FRAME 23 THRU FRAME 25 CORRODED BEYOND LIMITS. AFTER BLEND-OUT, REMOVED AND REPLACED FLOOR SUPPORT.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 29,196 hrs · 16,631 cycles

LEFT FLOOR SUPPORT BETWEEN FRM 41-47 IS CORROED BEYOND LIMITS AFTER BLEND OUT. REMOVED AND REPLACED SUPPORT.

Part: STRAP — CORRODED (FUSELAGE) · airframe 29,196 hrs · 16,631 cycles

GUSSET OF FRAME 22 RT FLOORBEAM, Y=479 CORRODED BEYOND LIMITS AFTER BLEND-OUT. R & R STRAP.

Part: LIGHT — INOPERATIVE (EMERGENCY EXIT) · airframe 26,853 hrs · 15,132 cycles

DURING PREFLIGHT, LIGHT WAS OUT ON GALLEY DOOR EMERGENCY EXIT SIGN. MX PERFORMED OPS CHECK ON GALLEY DOOR EMERGENCY EXIT SIGN, OPS CHECK GOOD IAW AMM 33-50-00. NO FURTHER MX REQUIRED. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONTACTOR — BURNED (WINDSHIELD HEAT) · airframe 26,854 hrs · 15,132 cycles

CREW REPORTED STRONG ELECTRICAL ODOR COMING FROM F/O'S DISTRIBUTION BOX AND RETURNED TO GATE. CONTRACT MX FOUND CONTACTOR K0002, NR 2 WINDSHIELD HEAT TO BE BURNED AND SOURCE OF ODOR. DEACTIVATED SYS AND DEFERRED IAW MEL 30-42-02. ACFT WAS APPROVED FOR RETURN TO SERVICE WITH MEL. MX R & R NR 2 WINDSHIELD CONTACTOR K0002 WITH OPS CHECKS SUCCESSFUL. CLEARED MEL AND ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: MODULE — INTERMITTENT (THRUST) · airframe 24,534 hrs · 13,580 cycles

THE CREW REPORTED THAT THEY WERE UNABLE TO CONTROL THRUST SETTING IN FLIGHT. ON TAKEOFF ROLL THE THRUST SETTING WENT TO "E/T/O RESERVE". THE POWER THRUST RATINGS KEEP CHANGING RANDOMLY. THE ACFT RETURNED TO DEPARTURE AND LANDED WITHOUT INCIDENT, WHERE MX REPLACED THE THRUST SETTING MODULE SWITCH BOX, PERFORMED OPS CHECKS AND CLEARED THE DISCREPANCY.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 24,376 hrs · 13,492 cycles

DURING SCHEDULED MX INSP THE AFT EMERGENCY EXIT AT ROW 12 WAS FOUND INOPERATIVE. RIC MX R & R NR3 EMERGENCY LIGHT BATTERY IAW AMM 33-50-04 WITH OPS CHECK SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CHARGER — FAULTY (CABIN) · airframe 24,303 hrs · 13,451 cycles

DURING SCHEDULED MX INSPECTION, BOTH RIGHT AND LEFT ROW 12 EMERGENCY EXIT AISLE LIGHTS FAILED TO ILLUMINATE. RIC MX FOUND NR 4 EMERGENCY LIGHT BATTERY CHARGER TO BE FAULTY. REMOVED AND REPLACED NR 4 EMERGENCY LIGHT BATTERY CHARGER IAW EMB145 AMM 33-50-04 WITH OPERATIONAL CHECK SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: THERMOSTAT — BLOCKED (BLEED AIR SYS) · airframe 22,428 hrs · 12,030 cycles

TYS - A/C WAS EN ROUTE TO RDU FROM IAD WHEN THE BLEED 1 OVERTEMP IN ICING CONDITIONS, QRH FOLLOWED BLEED 2 OVERTEMP PEGGED TO THE TOP. A/C WAS FERRIED TO TYS WHERE MAINTENANCE REMOVED AND REPLACED THE NR 1 HIGH TEMP THERMOSTAT IAW 36-11-06. REMOVED AND REPLACED THE NR 2 PRECOOLER IAW EMB 145XR AMM 36-11-04. REMOVED AND REPLACED THE NR 2 FAN AIR VALVE IAW EMB 145XR 36-11-03, OPS CHECK GOOD ON ALL REPLACEMENT PARTS AND WAS RELEASED. PARTS INVOLVED (PRECOOLER-PN-145-30609-401/SN 3267) (THERMOSTAT- 816624-9/SN-200212148).

Part: ELECTRONIC UNIT — INTERMITTENT (COCKPIT) · airframe 22,250 hrs · 11,871 cycles

IAD FLT 6026 - THE CREW REPORTED THE THRUST RATING QUADRANT IS ERRATICALLY SELECTING HIGH TAKEOFF THRUST SETTINGS. MAINTENANCE INSPECTED AND REPLACED THE LANDING GEAR ELECTRONIC UNIT. OPERATIONAL CHECKS WERE GOOD.

Part: CONTROLLER — INOPERATIVE (CABIN PRESSURE) · airframe 20,316 hrs · 10,764 cycles

IAH - FLIGHT 2198, THE CREW REPORTED PRESSURIZATION LOST IN CRUISE. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE MANUAL PRESSURIZATION CONTROLLER, AND PNEUMATIC OUTFLOW VALVE, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: OUTFLOW VALVE — INOPERATIVE (CABIN PRESSURE) · airframe 20,316 hrs · 10,764 cycles

IAH - FLIGHT 2198, THE CREW REPORTED PRESSURIZATION LOST IN CRUISE. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE MANUAL PRESSURIZATION CONTROLLER, AND PNEUMATIC OUTFLOW VALVE, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PROXIMITY SWITCH — OUT OF ADJUST (LT MLG) · airframe 19,577 hrs · 10,369 cycles

CLE FLT 3033 THE CREW REPORTED A LANDING GEAR AIR/GROUND FAIL MESSAGE IN FLIGHT. MAINTENANCE INSPECTED AND RE-ADJUSTED THE LEFT SHOCK ABSORBER WOW PROXIMITY SWITCH. OPERATIONAL CHECKS WERE GOOD.

Part: CONNECTOR — DEFECTIVE (COMM SYS) · airframe 19,115 hrs · 10,117 cycles

FLIGHT 3000 - EWR - FLIGHT CREW REPORTED AFT FLIGHT ATTENDANCE HAND SET SHOWS EMERGENCY. EWR MX REMOVED AND REPLACED CONNECTOR (J8100 & P8100) AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: PIN — LOOSE (EMERGENCY LIGHTS) · airframe 19,062 hrs · 10,090 cycles

IAH - FLIGHT 2121, THE CREW REPORTED THAT THE EXIT ROW EMERGENCY LIGHTS ILLUMINATED IN FLIGHT AND THEN TURNED OFF AFTER ABOUT 15 MINUTES. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE RE-SECURED A LOOSE PIN IN CONNECTOR P8031, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 19,018 hrs · 10,070 cycles

THE 12A EMERGENCY LIGHT IN OVERHEAD IS INOP. REMOVED AND REPLACED BULB IAW EMB 145XR AMM33-50-08, OPS CHECK GOOD.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 18,997 hrs · 10,061 cycles

FLIGHT 2900 - EWR - FLIGHT CREW REPORTED CABIN EMERGENCY LIGHTS ON IN ARMED POSITION DURING PUSHBACK. EWR MX REMOVED AND REPLACED INVERTER NR 4 & 5 AND POWER SUPPLY NR 5 AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. C2XA09RI209 REPORTS INVERTER INFORMATION AND C2XA09RI210 REPORTS POWER SUPPLY INFORMATION.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 18,997 hrs · 10,061 cycles

FLIGHT 2900 - EWR - FLIGHT CREW REPORTED CABIN EMERGENCY LIGHTS ON IN ARMED POSITION DURING PUSHBACK. EWR MX REMOVED AND REPLACED INVERTER NR 4 & 5 AND POWER SUPPLY NR 5 AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. C2XA09RI209 REPORTS INVERTER INFORMATION AND C2XA09RI210 REPORTS POWER SUPPLY INFORMATION.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 18,994 hrs · 10,059 cycles

FLIGHT 2353 - EWR - FLIGHT CREW REPORTED EMERGENCY EXIT LIGHTS INSIDE THE CABIN, ON OVER THE WING, CAME ON DURING FLIGHT. CREW RECYCLED EMERGENCY LIGHT AND IT WOULD GO OFF, BUT CAME BACK. EWR MX PERFORMED OPERATIONAL CHECK AND COULD NOT DUPLICATE THE PROBLEM. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: ADC — FAULTY (NR 1) · airframe 18,823 hrs · 9,972 cycles

IAH FLT 2124 - THE CREW REPORTED AN IAS COMPARATOR AND SPS ADVANCED MESSAGE ON THE EICAS IN FLIGHT. THE AIRCRAFT DIVERTED INTO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NR 1 AIR DATA COMPUTER. OPERATIONAL CHECKS WERE GOOD.

Part: TRIM SWITCH — INOPERATIVE (COCKPIT) · airframe 18,125 hrs · 9,597 cycles

IAH - FLIGHT 2246, DURING CLIMB THE CREW REPORTED THAT THE PRIMARY PITCH TRIM SWITCH WAS INOPERATIVE. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE F/O'S YOKE PITCH TRIM SWITCH, OPERATIONALLY TESTED WITH NO DEFECTS. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: HEAT EXCHANGER — MALFUNCTIONED (AC BAY) · airframe 17,748 hrs · 9,379 cycles

TYS FOR IAH - THE NR 2 PACK VALVE CLOSED MESSAGE WING A/1 FAIL. CREW DIVERTED TO MOB, WAS RELEASED IAW MEL 21-51-00/2 CAT (C) CONTROL/NUMBER 171254. LATER MAINTENANCE REMOVED AND REPLACED THE DUAL HEAT EXCHANGER AND OPS CHECK GOOD AND WAS REL.

Part: ROLLER — OUT OF ADJUST (PAX DOOR) · airframe 14,570 hrs · 7,681 cycles

FLT 4920 (FERRY FLIGHT) CABIN DOOR FAIL TO CLOSE. MX ADJUSTED STABILIZER ARMS AND ROLLERS ON CABIN DOOR OPS CHECK GOOD, FORCE APPLIED CHECK 40 LBS IAW AMM 52-18-00. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.

Part: BEAM — CORRODED (CARGO BAY) · airframe 14,271 hrs · 7,521 cycles

SHV - DURING C-CHECK THE CARGO DOOR CUTOUT LOWER BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 65 THROUGH 68. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 145XR SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 14,271 hrs · 7,521 cycles

SHV - DURING C-CHECK CENTER OMEGA BEAM HAS CORROSION ON FR 20. MX REMOVED AND REPLACED CENTER OMEGA BEAM AT FR 16-24 IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 14,271 hrs · 7,521 cycles

SHV - DURING C-CHECK LT OMEGA BEAM AT PREVIOUS REPAIR BETWEEN FR 24-25 IS CORRODED. MX REMOVED AND REPLACED LT PREVIOUS REPAIR BETWEEN FR 24-25 IAW EMB 145 XR SRM 53-00-10 ITEM 3. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 14,271 hrs · 7,521 cycles

SHV - DURING C-CHECK LT OMEGA BEAM HAS CORROSION AT FR 21-23. MX REPAIRED LT OMEGA BEAM AT FR 21-23 IAW EC 5320-01406. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 14,271 hrs · 7,521 cycles

SHV - DURING C-CHECK CENTER OMEGA BEAM AT PREVIOUS REPAIR HAS CORROSION FR 24-25. MX REMOVED AND REPLACED PREVIOUS REPAIR AT CENTER OMEGA BEAM BETWEEN FR 24-25 IAW EMB 145 XR SRM 53-00-10 FIG 203 DET A. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.

Part: SOLENOID VALVE — INOPERATIVE (NLG) · airframe 11,220 hrs · 5,946 cycles

FLIGHT 2513 - EWR - CREW REPORTED VIBRATION AND EXCESSIVE NOISE IN FLIGHT AFTER GEAR RETRACTION. EWR MX FOUND NOSE GEAR DOORS NOT TO CLOSE. MX REMOVED AND REPLACED GEAR DOOR SOLENOID VALVE. MX ALSO REMOVED AND REPLACED LANDING GEAR CONTROL LEVER. MX PERFORMED OPERATIONAL CHECK OF LANDING GEAR SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO FLIGHT.

Part: SENSOR — BROKEN (LT SPOILER) · airframe 7,243 hrs · 3,853 cycles

IAH FLIGHT NR 3098, THE CREW REPORTED A SPOILER OPEN INDICIATION IN FLIGHT. THE AIRCRAFT DIVERTED INTO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE LEFT OUTBOARD PROXIMITY SENSOR. OPERATIONAL CHECKS WERE GOOD.