N17146

Part: CONTROL LEVER — INOPERATIVE (TE FLAPS) · airframe 48,687 hrs · 31,475 cycles

FLAP FAIL IN FLIGHT. FOLLOWED FIM. FOUND NO DEFECTS. COULD NOT DUPLICATE FLAP FAIL FAULT. CHECKED ELECTRICAL CONNECTORS P1100 AND P110415 IS PROPERLY PLUGGED. OPS CHECK SAT. REMOVED AND REPLACED FLAP SELECTOR LEVER. OPS CHECK SAT

Part: LIGHT — MISINSTALLED (RT CABIN) · airframe 48,085 hrs · 30,893 cycles

RH OVERWING EMERGENCY EXIT LIGHT INSTALLED UPSIDE DOWN. REMOVED AND REINSTALLED OVERWING EMERGENCY EXIT LIGHT CORRECTLY.

Part: SIGN — INOPERATIVE (ZONE 200) · airframe 48,085 hrs · 30,893 cycles

FWD EXIT EMERGENCY SIGN ABOVE ROW 18 INOPERATIVE. REMOVED AND REPLACED FWD EXIT EMERGENCY SIGN ABOVE ROW 18. OPS CHECK SAT.

Part: DOOR — LACK OF LUBE (MAIN) · airframe 47,969 hrs · 30,795 cycles

MAIN CABIN DOOR IS HARD TO CLOSE WITH HANDLE. LUBRICATED DOOR. OPS CHECK SAT.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 47,692 hrs · 30,534 cycles

FOUND MULTIPLE EMERGENCY LIGHTS INOPERATIVE. FOUND CONNECTOR DISCONNECTED, RE-CONNECTED CONNECTOR. OPS CHECK SAT

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 47,684 hrs · 30,527 cycles

COCKPIT EMERGENCY LIGHT OUT. REMOVED AND REPLACED BULB. OPS CHECK SAT.

Part: DOOR — FAULTED (MAIN) · airframe 47,647 hrs · 30,494 cycles

MCD WONT OPEN FROM OUTSIDE OF AIRCRAFT. PERFORMED OPS CHECK ON MCD. OPS CHECK SAT

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 46,713 hrs · 29,616 cycles

RT EMERGENCY EXIT DOOR SHOWING OPEN. CLEANED MICRO SWITCH. OPS CHECK SAT.

Part: SIGN — LOOSE (UNKNOWN) · airframe 46,628 hrs · 29,539 cycles

CENTRAL CABIN OVERHEAD FWD EMERGENCY LIGHT INOP. FOUND CONNECTOR LOOSE, RECONNECTED. OPS CHECK SAT

Part: NONE — NONE · airframe 45,953 hrs · 28,917 cycles

MAIN CABIN DOOR WON'T COMPLETELY CLOSE. CLEANED DOOR SEAL AND LUBED THE ROLLER. OPS CHECK GOOD.

Part: SKIN — GOUGED (CARGO DOOR) · airframe 45,452 hrs · 28,487 cycles

GOUGE ON BAGGAGE DOOR FORWARD OF VENT HANDLE AS MARKED. REMOVED DAMAGE AND INSTALLED REPAIR DOUBLER AND FILLER ON BAGGAGE DOOR FWD LOWER EDGE SKIN.

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 45,452 hrs · 28,487 cycles

REAR FUSELAGE I SKIN HAS CORROSION UNDER RAR #2 ANTENNA BASE. REPAIRED SKIN UNDER RAR #2 ANTENNA WITH REPAIR DOUBLER FILLER

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 45,452 hrs · 28,487 cycles

CORROSION FOUND ON INTERNAL FUSELAGE SKIN AROUND CUTOUT FOR RAT #2 ANTENNA CABLE. REPAIRED REAR FUSELAGE SKIN AT RAT #2 ANTENNA.

Part: SKIN — DENTED (FRMS 26-27) · airframe 45,452 hrs · 28,487 cycles

EXTERNAL FUSELAGE - DENT LOCATED BETWEEN FR 26 AND FR 27 BETWEEN STGR 20 AND 21 LH. REPAIRED DENT FR26-27 STRINGERS 20L-21L WITH CUTOUT AND DOUBLER/FILLER

Part: YOKE — DAMAGED (NR 1 NACELLE) · airframe 45,452 hrs · 28,487 cycles

DAMAGED HOLE #1 PYLON YOKE UPPER FLANGE, AFT FASTENER. REPAIRED HOLE ON #1 PYLON YOKE UPPER FLANGE AT AFT FASTENER LOCATION.

Part: LIGHT — INOPERATIVE · airframe 45,448 hrs · 28,484 cycles

EMERGENCY FLOOR STRIP LIGHTING POTENTIALLY IN INCORRECT POSITIONS. REINSTALLED EMERGENCY FLOOR STRIP TO CORRECT LOCATIONS

Part: GEAR — UNLATCHED · airframe 45,401 hrs · 28,445 cycles

LG AIR /GND FAIL IN FLIGHT. R&R LEFT MLG FORWARD PROX SWITCH & RIGHT MLG AFT PROX SWITCH. PERFORMED GEAR SWINGS WITH BREAK OUT BOX

Part: NONE — NONE · airframe 45,131 hrs · 28,207 cycles

FRONT SIDE OF EMERGENCY EXIT LIGHT IS INOPERATIVE. RESECURED EMERGENCY EXIT LIGHT CONNECTION

Part: UNKNOWN — ODOR (NOT REPORTED) · airframe 43,841 hrs · 27,090 cycles

DIRTY SOCK SMELL ON CLIMB OUT AND APPROACH. PERFORMED BOROSCOPE INSPECTION OF COMPRESSOR FLOWPATH EXTENSION FOR FRONT SUMP OIL LEAKAGE. NO DEFECTS NOTED. #1 PERFORMED BACK LIGHT INSPECTION OF ENGINE #1 FOR OIL LEAKAGE. .0 CARBON SEAL, NO FAULT NOTED. PERFORMED BOROSCOPE INSPECTION OF COMPRESSOR FLOW PATH EXTENSION FROM SUMP OIL LEAKAGE. NO DEFECTS NOTED. PERFORMED ISOLATION PROCEDURE. NO FAULT FOUND. REMOVED AND REPLACED #1 ENGINE.

Part: PROXIMITY SWITCH — OUT OF ADJUST (RT MLG) · airframe 43,241 hrs · 26,530 cycles

LANDING GEAR AIR/GROUND FAIL MESSAGE ON EICAS. WITH POWER OFF PINS D&V OF P7164 TO GROUND AT .4 OHM & WITH POWER ON AT 1.7 OHMS AND SLOWLY RISING. REBONDED & SEALED GS0366DC. NOW READING .5 OHM WITH POWER ON. JACKED A/C FOUND RT GEAR SHOCK ABSORBER AIR/GRN PROXIMITY SWITCH SHOWING GROUND. ADJUSTED RT SHOCK ABSORBER PROXIMITY SWITCH. OPERATIONAL CHECK OF LANDING GEAR PROX SWITCHES & AIR GROUND SYSTEM GOOD.

Part: PROXIMITY SWITCH — OUT OF ADJUST (LT MLG) · airframe 43,222 hrs · 26,509 cycles

LG AIR/GROUND FAIL ON EICAS AND LANDING GEAR WOULD NOT RETRACT. FOUND LEFT SHOCK MLG WOW PROX SWITCH GAP OUT OF LIMITS ADJUSTED GAP. FOUNT RT MLG SHOCK WOW PROX SWITCH DEFECTIVE REMOVED AND REPLACED RIGHT MLG SHOCK WOW PROX SWITCH. OPERATIONS CHECK GOOD.

Part: PUMP — FAILED (NR 2 HYD SYS) · airframe 42,629 hrs · 26,028 cycles

HYDRAULIC SYSTEM 2 FAIL. R&R #2 HYDRAULIC PUMP. OPS CHECK GOOD.

Part: DOOR FRAME — CORRODED (FRM 65) · airframe 42,493 hrs · 25,921 cycles

Z FRAME AT CARGO DOOR FR 65 HAS CORROSION.... PERFORMED TEMP REPAIR ON Z ANGLE REP ETD2019-145-150902

Part: ANGLE — CRACKED (FWD CARGO) · airframe 42,493 hrs · 25,921 cycles

CARGO RAMP FWD L ANGLE IS CRACKED.... REMOVED AND REPLACED CARGO RAMP FWD L ANGLE

Part: DOOR — CORRODED (FWD CARGO) · airframe 42,493 hrs · 25,921 cycles

FWD CARGO DOOR AT FRM 65 AND STG 15 RIB HAS CORROSION.... REMOVED AND REPLACED RIB AT FRM 65 AND STG 15..

Part: FLOOR SUPPORT — CORRODED (FRAMES 48-52) · airframe 42,493 hrs · 25,921 cycles

R/H FLOOR SILL HAS CORROSION AT FR 48-FR52... REMOVED AND REPLACED FLOOR SILL...

Part: FLOOR SUPPORT — CORRODED (FRAMES 24-29) · airframe 42,493 hrs · 25,921 cycles

L/H FLOOR SILL HAS CORROSION AT FR 24-FR29... REMOVED AND REPLACED FLOOR SILL...

Part: ANGLE — CORRODED (CARGO DOOR OPEN) · airframe 42,493 hrs · 25,921 cycles

CARGO DOOR CUTOUT Z-ANGLE HAS CORROSION....REMOVED AND REPLACED CARGO DOOR CUTOUT Z-ANGLE

Part: FLOOR SUPPORT — CORRODED (FRAMES 42-47) · airframe 42,493 hrs · 25,921 cycles

R/H FLOOR SILL HAS CORROSION AT FR 42-FR47... REMOVED AND REPLACED FLOOR SILL...

Part: FLOOR SUPPORT — CORRODED (FRAMES 30-35) · airframe 42,493 hrs · 25,921 cycles

RH FLOOR SILL HAS CORROSION BETWEEN FR30 & FR 35- REMOVED RH FLOOR SILL BEWTEEN FR30 TO FR35. INSTALLED NEW RH FLOOR SILL FR 30 - FR35.

Part: FLOOR SUPPORT — CORRODED (FRAME 23) · airframe 42,493 hrs · 255,921 cycles

R/H OMEGA BEAM HAS CORROSION AT FR23.... REMOVED DAMAGED AREA AND INSTALLED DOUBLER ON R/H OMEG BEAM AT FR 23

Part: SUPPORT — CRACKED (CARGO DOOR) · airframe 42,493 hrs · 25,921 cycles

CARGO DOOR HOLD OPEN ROD CUP SUPPORT IS CRACKED- REMOVED CARGO DOOR HOLD OPEN ROD CUP. INSTALLED CARGO DOOR HOLD OPEN CUP SUPPORT.

Part: FLOOR SUPPORT — CORRODED (FRAMES 36-41) · airframe 42,493 hrs · 255,921 cycles

R/H FLOOR SILL HAS CORROSION BETWEEN FR36-FR41... REMOVED AND REPLACED R/H FLOOR SILL BETWEEN FR36-FR41

Part: FLOOR SUPPORT — CORRODED (FRAMES 36-41) · airframe 42,493 hrs · 25,921 cycles

L/H FLOOR SILL HAS CORROSION AT FR 36-FR41... REMOVED AND REPLACED FLOOR SILL...

Part: FLOOR SUPPORT — CORRODED (FRAMES 18-23) · airframe 42,493 hrs · 25,921 cycles

L/H FLOOR SILL HAS CORROSION AT FR 18-FR23... REMOVED AND REPLACED FLOOR SILL...

Part: FLOOR SUPPORT — CORRODED (AFT CARGO BAY) · airframe 42,493 hrs · 25,921 cycles

L/H FLOOR SILL AFT OF CARGO DOOR HAS SIGNS OF CORROSION..... REMOVED AND REPLACES L/H FLOOR SILL AFT OF CARGO DOOR.

Part: FLOOR SUPPORT — CORRODED (FRAMES 30-35) · airframe 42,493 hrs · 25,921 cycles

L/H FLOOR SILL HAS CORROSION AT FR 30-FR35... REMOVED AND REPLACED FLOOR SILL...

Part: SHEAR TIE — CORRODED (FRAME 53) · airframe 42,493 hrs · 255,921 cycles

SHEAR CLIP HAS CORROSION AT FR 53 STG20-21R.... REMOVED AND REPLACED SHEAR CLIP AT FR 53 ATE STG 20-21R

Part: FLOOR SUPPORT — CORRODED (FRAMES 48-52) · airframe 42,493 hrs · 25,921 cycles

LH FLOOR SILL HAS CORROSION BETWEEN FR48 TO FR52- REMOVED LH FLOOR SILL BETWEEN FR48-FR52. INSTALLED LH FLOOR SILL.

Part: FLOOR SUPPORT — CORRODED (FRAMES 48-52) · airframe 42,493 hrs · 25,921 cycles

L/H FLOOR SILL HAS CORROSION BETWEEN FR 48 FR52.... REMOVED AND REPLACED L/H FLOOR SILL BETWEEN FR 48- FR 52

Part: SPAR — CRACKED (HORIZONTAL STAB) · airframe 42,493 hrs · 25,921 cycles

L/H HORIZONTAL STAB O/B SPAR IS CRACKED..... REMOVED AND L/ HORIZONTAL STAB O/B SPAR, REMOVED DAMAGE AND INSTALLED DOUBLER IAW ETD2019-145-150917

Part: LINE — CUT (HYD SYSTEM) · airframe 42,362 hrs · 25,819 cycles

TOTAL LOSS OF HYD FLUID IN SYS NR 1. FOUND LASCERATION ON E1 HYD PUMP PRESSURE LINE. R & R THE LINE SERVICED THE HYD SYS NR 1, RAN ENGINES AT POWER, OPS AND LEAK CHECK GOOD.

Part: PACKING — WORN (BLEED AIR SYS) · airframe 41,593 hrs · 25,212 cycles

#1 BLEED LEAK ON EICAS DURING FLIGHT. FOUND LOCATIONS 5 AND 7 PACKING S WORN. R&R PACKING AS AT 5 AND 7. OPS CHECK GOOD AT THIS TIME.

Part: COUPLING — LOOSE (NR 1 BLEED) · airframe 41,433 hrs · 25,076 cycles

BLEED 1 LEAK IN FLIGHT WITH PACK 2 DEFERED. A/C DIVERTED INTO STL. TIGHTENED LOOSE COUPLING ON #1 PAC. PERFORMED LEAK CHECK. CHECK GOOD.

Part: BATTERY — DEFECTIVE (ELT) · airframe 41,031 hrs · 24,768 cycles

ELT COMES ON DURING TAXI OUT. DEACTIVARD THE ELT. REMOVED AND REPLACED ELT BATTERY. OPS CHECK GOOD.

Part: TRIM SYSTEM — MALFUNCTIONED (HORIZ STAB) · airframe 40,059 hrs · 24,004 cycles

APPROX 25K FT, PTRIM MAIN INOP EICAS MSG. R&R HSCU. OPS CHECK GOOD. R&R STAB TRIM ACTUATOR SYSTEM, OPERATED NORMALLY AND TESTED GOOD, BUT MSG RETURNED FOR NO FIX. INDIVIDUALLY SLAVED IN BOTH CAPT AND FO'S MAIN PTRIM SWX'S. PITCH TRIM MAIN INOP ON EICAS DID NOT GO SOLVE PROBLEM. WILL FWD MORE INFORMATION WHEN AVAILABLE.

Part: SEAL — UNSECURE (DOOR GATE)

PAX DOOR FLAP NOT SEALING AND HANGING LOOSE. SECURED MAIN CABIN DOOR FLAP SEAL. NO DEFECTS NOTED AT THIS TIME.

Part: CONTROL SYSTEM — BINDING (ELEVATOR)

BINDING FOUND IN ELEVATOR TRAVEL DURING FLT CONTROL TEST. PERFORMED DETAILED VISUAL INSPECTION OF ELEVATOR CABLES. NO DEFECTS NOTED. R&R ACCESS DOOR 123B. R&R FLIGHT DECK FLOOR PANELS 223316R, 241DF. OPENED AND CLOSED ACCESS DOORS 272DR, 312AR. PERFORMED VISUAL INSPECTION OF CABLES, PULLEYS, AND BELL CRANKS. MNO DEFECTS OR ABNORMALITIES NOTED.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 39,009 hrs · 23,139 cycles

LEFT EXTERIOR FWD EMERGENCY LIGHT INOPERATIVE. R & R THE EMERGENCY LIGHT ASSY, OPS CHECKED GOOD.

Part: CONTROL PANEL — MALFUNCTIONED (SMOKE DETECTOR) · airframe 38,895 hrs · 23,036 cycles

LAVATORY SMOKE WARNING EICAS AND AUDIBLE IN FLT. REMOVED AND REPLACED SMOKE DETECTOR PANEL OPS CHECKED GOOD

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 38,888 hrs · 23,029 cycles

LAVATORY SMOKE WARNING IN FLIGHT. FOLLOWED QRH, FA CONFIRMED NO SMOKE PRESENT OR ODOR OF ANY SMOKE. CLEANED THE LAVATORY SMOKE DETECTOR AND OPS CHECKED GOOD.

Part: INDICATOR — FAILED (CABIN PRESSURE) · airframe 38,835 hrs · 22,981 cycles

PRESSURIZATION INDICATION SHOWING DASHES. R & R THE CPAM, OPS AND LEAK CHECKED GOOD.

Part: FLOOR SUPPORT — CORRODED (FRAMES 59-62) · airframe 38,629 hrs · 22,802 cycles

LEFT FLOOR SUPPORT AT FRAMES 59 - 62 HAS CORROSION. R & R THE FLOOR SUPPORT.

Part: FLOOR SUPPORT — CORRODED (FRAMES 59-62) · airframe 38,629 hrs · 22,802 cycles

SIDEWALL FLOOR SUPPORT AT FRAMES 59 - 62 HAS CORROSION. R & R THE SIDEWALL FLOOR SUPPORT.

Part: FLOOR SUPPORT — CORRODED (FRAMES 59-62) · airframe 38,629 hrs · 22,802 cycles

CENTER FLOOR SUPPORT AT FRAMES 59 - 62 HAS CORROSION. R & R THE FLOOR SUPPORT.

Part: FLOOR SUPPORT — CORRODED (FRAMES 59-61) · airframe 38,629 hrs · 22,802 cycles

RIGHT FLOOR SUPPORT, FRAMES 59 - 61 HAS CORROSION. R & R THE FLOOR SUPPORT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 38,312 hrs · 22,546 cycles

MAIN PAX DOOR EXTERIOR FLOOD LIGHT (NR 1) INOP. R & R MAIN PAX DOOR EXTERIOR FLOOD LIGHT BULB, OPS CHECK GOOD.

Part: SKIN — DENTED (FRAMES 19-20) · airframe 37,076 hrs · 21,464 cycles

DURING MAINTENANCE INSPECTION, A DENT WAS FOUND APPROXIMATELY 12 INCHES FROM THE FWD LOWER CORNER OF THE FIRST LT CABIN WINDOW. MAINTENANCE REMOVED THE DAMAGE AND INSTALLED A DOUBLER REPAIR. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONTROLLER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 35,821 hrs · 20,535 cycles

THE CREW REPORTED THAT THE EMERGENCY LIGHTS STAYED ON. MAINTENANCE R & R THE EMERGENCY LIGHT CONTROLLER, OPERATIONALLY TESTED WITH NO DEFECTS NOTED, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CHARGER — FAULTY (EMERGENCY LIGHT) · airframe 35,782 hrs · 20,506 cycles

DURING ROUTINE MAINTENANCE SEVERAL EMERGENCY LIGHTS WOULD NOT ILLUMINATE DURING TEST. MAINTENANCE REPLACED THE NR 3 AND NR 4 EMERGENCY LIGHT BATTERY CHARGERS. OPS CHECKS WERE GOOD.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 35,518 hrs · 20,308 cycles

THE CREW REPORTED THAT EMERGENCY LIGHTS 1 & 2 WERE INOPERATIVE. MAINTENANCE R & R THE NR 2 EMERGENCY LIGHT BATTERY PACK, OPERATIONALLY TESTED WITH NO DEFECTS NOTED AND THE AFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 35,518 hrs · 20,308 cycles

THE CREW REPORTED THAT EMERGENCY LIGHTS 3 & 4 WERE INOPERATIVE. MAINTENANCE R & R THE NR 3 EMERGENCY LIGHT BATTERY PACK, OPERATIONALLY TESTED WITH NO DEFECTS NOTED AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 35,518 hrs · 20,308 cycles

THE CREW REPORTED THAT EMERGENCY LIGHTS 3 & 4 WERE INOPERATIVE. MAINTENANCE R & R THE NR 4 EMERGENCY LIGHT BATTERY PACK, OPERATIONALLY TESTED WITH NO DEFECTS NOTED AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: RELAY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 35,518 hrs · 20,308 cycles

THE CREW REPORTED THAT THE EMERGENCY LIGHTS WOULD NOT TEST OR TURN OFF FROM THE FLIGHT ATTENDANT CONTROL PANEL. MAINTENANCE R & R RELAY K0275, OPS TESTED WITH NO DEFECTS NOTED, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 35,518 hrs · 20,308 cycles

THE CREW REPORTED THAT EMERGENCY LIGHTS 1 & 2 WERE INOPERATIVE. MAINTENANCE R & R THE NR 1 EMERGENCY LIGHT BATTERY PACK, OPERATIONALLY TESTED WITH NO DEFECTS NOTED AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FRAME — CRACKED (FRM 10) · airframe 35,515 hrs · 20,304 cycles

DURING C-CHECK, COCKPIT LT FRAME 10 IS CRACKED. R & R COCKPIT LT FRAME 10 UNDER DV WINDOW IAW SRM 51-40-02. ACFT APPROVED FOR RETURN TO SERVICE.

Part: CARBON SEAL — LEAKING (ENGINE) · airframe 35,309 hrs · 20,170 cycles

ACFT WAS REPORTED BY PILOTS THAT SMOKE WAS IN THE CABIN FROM THE PACKS AND TURNED OFF RECIRCULATING FANS DIDN'T HELP. IT GOT WORSE. ACFT WAS FERRIED, WHERE MAINTENANCE FOUND THE 0 CARBON SEAL LEAKING. R & R THE 0 CARBON SEAL REF MM 72-25-25. OPS AND LEAK CHECKS GOOD AND WAS RELEASED BACK TO SERVICE.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 33,285 hrs · 18,739 cycles

DURING MX INSPECTION THE LT FWD OVERWING EMERGENCY EXIT LIGHT AND CEILING EMERGENCY LIGHT WOULD NOT ILLUMINATE. MX R & R THE NR 1 EMERGENCY LIGHT SYS BATTERY CHARGER WITH OPS CHECK GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FIRE WARNING — FALSE ACTIVATION (APU BAY) · airframe 28,277 hrs · 15,519 cycles

THE CREW REPORTED AT 10,000 STARTED THE APU AND RECEIVED A FIRE INDICATION. RAN THE QRH AND DEPLETED THE FIRE BOTTLE. MX INSPECTED AND FOUND NO EVIDENCE OF FIRE. RELEASED ACFT IAW MEL 26-22-00. OPEN

Part: SMOKE DETECTOR — INOPERATIVE (LAVATORY) · airframe 21,309 hrs · 11,359 cycles

FLIGHT 2337 - GSP - FLIGHT CREW REPORTED LAV SMOKE INDICATION ON EICAS. EWR MX REMOVED AND REPLACED SMOKE DET SENSOR AND REMOVED REPLACED SMOKE DETECTOR TEST PANEL IN GALLEY AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. (SMOKE DETECTOR SENSOR REPORTED ON SDR C2XA11RI002, SMOKE DETECTOR PANEL REPORTED ON C2XA11RI003).

Part: PANEL — INOPERATIVE (SMOKE DETECTION) · airframe 21,309 hrs · 11,359 cycles

FLIGHT 2337 - GSP - FLIGHT CREW REPORTED LAV SMOKE INDICATION ON EICAS. EWR MX REMOVED AND REPLACED SMOKE DET SENSOR AND REMOVED REPLACED SMOKE DETECTOR TEST PANEL IN GALLEY AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. (SMOKE DETECTOR SENSOR REPORTED ON SDR C2XA11RI002, SMOKE DETECTOR PANEL REPORTED ON C2XA11RI003)

Part: IGNITER — INOPERATIVE (NR 2 ENGINE) · airframe 21,152 hrs · 11,277 cycles

IAH - FLIGHT 2176, THE CREW REPORTED A HUNG START FOLLOWED BY STRONG SMELL OF SMOKE IN THE COCKPIT. THE AIRCRAFT RETURNED TO THE GATE WHERE MAINTENANCE REMOVED AND REPLACED THE "A" IGNITOR ON THE NUMBER TWO ENGINE, OPERATIONALLY TESTED WITH NO DEFECTS, AND NO SMELL OF SMOKE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONNECTOR — CORRODED (BLEED AIR SYS) · airframe 21,133 hrs · 11,266 cycles

CLE FLT 2057 THE CREW REPORTED A BLEED 2 LOW TEMP WARNING MESSAGE IN CLIMBOUT. THE AIRCRAFT RETURNED TO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NR 2 HIGH STAGE BLEED VALVE CONNECTOR. OPERATIONAL CHECKS WERE GOOD.

Part: ENGINE — LEAKING (NR 2) · airframe 21,128 hrs · 11,264 cycles

CLE FLT 2786 THE CREW REPORTED A LAV SMOKE INDICATION AFTER TAKEOFF. THE AIRCRAFT RETURNED TO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NR 2 ENGINE. OPERATIONAL CHECKS WERE GOOD.

Part: SMOKE DETECTOR — FAULTY (LAVATORY) · airframe 21,028 hrs · 11,201 cycles

FLIGHT 3082 - EWR - FLIGHT CREW REPORTED LAV SMOKE WARNING ON EICAS IN FLIGHT. EWR MX REMOVED AND REPLACED LAV SMOKE DETECTOR AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: PANEL — DEFECTIVE (SMOKE DETECTION) · airframe 20,804 hrs · 11,075 cycles

MCI - FLIGHT 2598, THE CREW REPORTED A LAV SMOKE EICAS MASTER WARNING IN FLIGHT. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT AND MAINTENANCE REMOVED AND REPLACED THE SMOKE DETECTOR PANEL, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED OFR RETURN TO SERVICE.

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 20,706 hrs · 11,203 cycles

IAH - FLIGHT 2644, THE CREW REPORTED A MOMENTARY LAV SMOKE INDICATION. MAINTENANCE VERIFIED NORMAL OPERATION OF THE LAV SMOKE DETECTOR, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SLEEVE — LOOSE (NR 2 PACK) · airframe 19,797 hrs · 10,526 cycles

FLT 2780 THE CREW REPORTED A PAC 2 VALVE FAILED CLOSED IN FLIGHT. THE CREW DIVERTED INTO CLT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE DUCT (SLEEVE) ON THE NR 2 PACK SYSTEM. OPERATIONAL CHECKS WERE GOOD.

Part: DAU — FAULTY (NR 2) · airframe 19,196 hrs · 10,197 cycles

CLE FLT 2710 THE CREW REPORTED A BAG SMOKE WARNING MESSAGE ON THE EICAS AFTER APU START. MAINTENANCE INSPECTED AND REPLACED THE NR 2 DAU AND OPERATIONAL CHECKS WERE GOOD.

Part: RIVET — LOOSE (FUSELAGE) · airframe 18,968 hrs · 10,063 cycles

SHV - DURING C-CHECK RT FRM 79 WORKING RIVETS BETWEEN STR 2R-9R. MAINTENANCE PERFORMED REPAIR TO RT FRM 79 WORKING RIVETS BETWEEN STR 2R & 9R IAW EMB-145 EC5330-02085. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: RIVET — LOOSE (FUSELAGE) · airframe 18,968 hrs · 10,063 cycles

SHV - DURING C-CHECK LT FRM 74 WORKING RIVETS BETWEEN STRS 3L-7L. MAINTENANCE PERFORMED REPAIR OF LT FRM 79 WORKING RIVETS BETWEEN STR 3L-7L IAW EC5330-02055. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: RIVET — LOOSE (FUSELAGE) · airframe 18,968 hrs · 10,063 cycles

SHV - DURING C-CHECK LT FRM 78 WORKING RIVETS BETWEEN STRS 3L-7L. MAINTENANCE PERFORMED REPAIR OF LT FRM 78 WORKING RIVETS BETWEEN STR 3L-7L IAW EC5330-02085. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 3 · airframe 18,968 hrs · 10,063 cycles

SHV - DURING C-CHECK CENTER OMEGA BEAM CORRODED (LEVEL 3 LOCAL) THROUGH (100 PERCENT) AT FRAME 20, 2 PLACES. MAINTENANCE REMOVED AND REPLACED CENTER OMEGA BEAM AT FRAME 20 IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — DAMAGED (FUSELAGE) · airframe 18,968 hrs · 10,063 cycles

SHV - DURING C-CHECK CENTER OMEGA BEAM AT FRAME 59-61 FOUND TO BE OUT OF LIMITS AROUND NUT PLATE HOLES IAW EMB-145XR SRM 53-24-10. MAINTENANCE REMOVED AND REPLACED THE CENTER OMEGA BEAM AT FRAMES 59-61 IAW EMB-145XR SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: THERMOSTAT — FAULTY (NR1 ENGINE)

EWR FLIGHT 2373. THE CREW REPORTED A BLEED 1/2 OVERTEMP MESSAGE IN ICING CONDITIONS. THE ACFT DIVERTED INTO CLE WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NR 1 BLEED THERMOSTAT. OPERATIONAL CHECKS WERE GOOD. (S)

Part: UNKNOWN — SMOKE (COCKPIT) · airframe 13,595 hrs · 7,159 cycles

CLE FLIGHT 2846 THE CREW REPORTED SMOKE IN THE COCKPIT. EMERGENCY WAS DECLARED. THE AIRCRAFT LANDED IN CLE WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND PERFORMED HIGH POWER ENGINE RUNS WITH BLEEDS, PACKS, AND ANTI ICE SYSTEMS ON. ALSO RAN ALL A/C ELECTRICAL SYSTEMS AND NO SMOKE OR BURNING SMELLS WERE NOTED. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 9,006 hrs · 4,768 cycles

TYS - DURING A 2C INSPECTION A SHEAR CLIP WAS FOUND CORRODED AT FR 68. MAINTENANCE REMOVED THE CORROSION, FABRICATED A DOUBLER AND INSTALL IAW EC 5330-01458. A/C WILL BE RELEASED UPON COMPLETION OF ALL WORK.

Part: FUEL TANK — CORRODED (FUSELAGE) · airframe 9,006 hrs · 4,768 cycles

TYS - DURING A CURRENT 2C INSPECTION THE VENTRAL TANK FWD BULKHEAD WAS FOUND CORRODED AT THE FUEL LINE SUPPORT BRACKET. MAINTENANCE CUT OUT THE EFFECTED AREA, FABRICATED AND INSTALL A DOUBLER AND FILLER. ALODINED AND PRIMED IAW EC 2810-01027. A/C WILL BE RELEASED AT THE END OF THE 2C INSPECTION.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 9,006 hrs · 4,768 cycles

TYS - DURING A CURRENT 2C INSPECTION A SHEAR CLIP AT FR 65 WAS FOUND. MAINTENANCE REMOVED THE CORROSION AND FABRICATED A DOUBLER AND INSTALL IAW EC 5530-01458. A/C WILL BE RELEASED AT THE END OF THE 2C INSPECTION.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 9,006 hrs · 4,768 cycles

SHEAR TIE CORRODED AT FRAME 65 AND FRAME 68. REMOVED CORROSION, FABRICATED DOUBLER AND INSTALLED IAW COEX EC5330-01458.

Part: SWITCH — STICKING (EMERGENCY EXIT)

DURING ROUTINE MAINTENANCE THE RIGHT OVERWING EMERGENCY EXIT DOOR SWITCH ACTUATOR WAS STICKING. THE DOOR DID NOT INDICATE OPEN INDICATION ON THE ECIAS WHEN THE DOOR WAS OPENED. MAINTENANCE CLEANED AND LUBED THE RIGHT EMERGENCY EXIT SWITCH ACTUATOR. OPERATIONAL CHECKS WERE GOOD I/A/W 52-75-00.

Part: SCREW — WRONG PART (EMERGENCY EXIT)

DURING ROUTINE MAINTENANCE THE LEFT OVERWING EMERGENCY EXIT WOULD NOT OPEN. MAINTENANCE INSPECTED AND FOUND THE WRONG GRIP LENGTH SCREW INSTALLED ON THE DOOR SURROUND LINER. THE SCREW WAS REPLACED AND OPERATIONAL CHECKS WERE GOOD OF THE DOOR.