N11150

Part: DOOR — STUCK (ZONE 800) · airframe 49,075 hrs · 32,552 cycles

MCD STUCK CLOSED. FREED MCD AND PERFORMED OPS CHECK. MCD CLOSED AND OPENED NORMALLY. NO FURTHER DEFECTS NOTED.

Part: SKIN — DAMAGED (ZONE 200) · airframe 48,845 hrs · 32,323 cycles

CREASE IN SKIN FWD FUSELAGE AT FR3 BTW STR 14L-15L. REMOVED CREASE AT FWD FUSELAGE SKIN SURFACE AT FR 3 BTW STR 14L-15L AND FABRICATED REPAIR DOUBLER 2024T3 .050. COMPLETED INSTALLED OF REPAIR DOUBLER WITH FILLER NEAR FR3 BTW STR 14L-15L.

Part: LANDING GEAR — COLLAPSED (NOSE) · airframe 48,347 hrs · 31,860 cycles

NOSE LANDING GEAR COLLAPSED UPON PUSH BACK. INSPECTED NOSE LANDING GEAR FOR ADDITIONAL DAMAGE. PERFORMED DVI OF FLOOR STRUCTURE OF FORWARD FUSELAGE. NO DEFECTS NOTED. PERFORMED DVI OF FWD 1 AND II EXTERIOR SKINS, ONLY DEFECTS NOTED WAS 2 PULLED THRU RIVETS AT DAMAGED FRAME 1 ASSEMBLY. RIVETS WILL BE REPLACED DURING FRAME 1 ASSEMBLY. PERFORMED DVI OF NLG COMPARTMENT GEAR FITTINGS, NLG BEARING CAPS AND HARDWARE, NLG BAY WEBS, CROSS CHANNELS AND SUPPORT ASSEMBLY. NO DEFECTS NOTED.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 47,563 hrs · 31,144 cycles

AFT CEILING PANEL EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED AFT AISLE EMERGENCY LIGHT. OPS CHECK SAT.

Part: FIRE DETECTOR — WARNING MESSAGE (NR 2 ENGINE) · airframe 47,272 hrs · 30,879 cycles

E2 FIRE DET FAIL ON EICAS IN FLIGHT R&R OF THE ENGINE FIRE DETECTOR OPS CHECK SAT

Part: FLASHLIGHT — ODOR (UNKNOWN) · airframe 46,251 hrs · 29,919 cycles

ODOR OF BURNING ELECTRICAL UPON "ON" USE OF IGNITION "ON" AT 36000 FT, BOTH IGNITERS TURNED ON. PERFORMED FIM, FOUND FLASHLIGHT ASSEMBLY HAVING SMOKE SMELL. REMOVED AND REPLACED FLASHLIGHT ASSEMBLY. OPS CHECK GOOD. NO DEFECTS NOTED. INSPECTED FUEL MODULE, INSPECTED POWERPLANT MODULE. NO DEFECTS.

Part: LAMP — UNKNOWN (UNKNOWN) · airframe 46,172 hrs · 29,848 cycles

LH OVERWING EMERGANCY LIGHT OUT R+R BULB OPS CHECK SAT

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 45,996 hrs · 29,682 cycles

FOUND CORROSION ON STRINGER 18R  NEAR FRAME 14. REMOVED CORRODED SECTION OF STRINGER 18R. PERFORMED SPLICE REPAIR AT STR 18R BTWN FR16-17R AND REPLACED  STR 18R FROM FR16-UP TO ATTACH POINT OF NEXT STR FWD FR14 DUE TO CORROSION.

Part: SKIN — DENTED (ZONE 200) · airframe 45,996 hrs · 29,682 cycles

DENT LOCATED BELOW RVSM AREA ON RH SIDE OF AC BETWEEN FRAMES 14&15 AT SKIN SPLICE. "REMOVED RIVETS IN AFFECTED AREA & RECONTOURED AREA. PERFORMED HIGH FREQ EDDY CURRENT INSPECTION OF RECONTOURED AREA, INTERNAL AND EXTERNAL AREAS, NO DAMAGE NOTED. ENLARGE CUT-OUT FROM ADJACENT REPAIR. FABRICATED DOUBLER/FILLER, MATCH DRILLED FASTENER LOCATIONS, COUNTER SUNK FOR BRF2AD5 RIVETS, BEGAN INSTALLATION OF REPAIR, USING BRILES RIVETS, APPLIED SEALANT TO PATCH AND RIVETED PATCH INTO PLACE , PERFORMED RII INSPECTION ON THE FABRICATED DOUBLER, WITNNESSED THE INSTALLATION OF THE REPAIR, PERFORMED INSPECTION BUY BACK FOR THE PATCH  INSTALLATION.. PRE PARED & PAINTED EXTERIOR REPAIR AREA. PERFORMED RVSM SKIN WAVINESS INSPECTION VERIFIED RVSM SKIN WAVINESS INSPECTION. SKIN WAVINESS ANALYSIS PASS, PERFORMED LEAK CHECK OF REPAIR AREA. LEAK CHECK SAT."

Part: SKIN — DENTED (ZONE 100) · airframe 45,996 hrs · 29,682 cycles

DENTS AT FR16 & FR15 BETWEEN STRINGER 16R & 17R NEAR SKIN SPLICE HAS OIL CANNING. PERFORMED HFEC ON THE CUT STRINGER. NO CRACKS FOUND. ENLARGE CUT-OUT. FABRICATED DOUBLER/FILLER, MATCH DRILLED FASTENER LOCATIONS, COUNTER SUNK FOR BRF2AD5 RIVETS, BEGAN INSTALLATION OF REPAIR, USING BRILES RIVETS, APPLIED SEALANT TO PATCH AND RIVETED PATCH INTO PLACE , PERFORMED RII INSPECTION ON THE FABRICATED DOUBLER, WITNNESSED THE INSTALLATION OF THE REPAIR, PERFORMED INSPECTION BUY BACK FOR THE PATCH  INSTALLATION.. PRE PARED & PAINTED EXTERIOR REPAIR AREA. PERFORMED RVSM SKIN WAVINESS INSPECTION VERIFIED RVSM SKIN WAVINESS INSPECTION. SKIN WAVINESS ANALYSIS PASS, PERFORMED LEAK CHECK OF REPAIR AREA. LEAK CHECK SAT.

Part: UNKNOWN — INOPERATIVE · airframe 45,645 hrs · 29,377 cycles

MAIN CABIN DOOR DIFFICULT TO OPEN. REMOVED AND REPLACED NUTPLATE. REMOVED AND REPLACE MCD BOX ASSEMBLY. ADJUSTED MAIN CAIN DOOR FOLDING FLAP. FUNCTIONAL TEST FOR CABIN LEAKAGE SAT. NO FURTHER DEFECTS AT THIS TIME.

Part: NONE — NONE · airframe 45,246 hrs · 29,024 cycles

DAMAGE FOUND ON LH SIDE SKIN BTW FR 61-64 AND BTW STR 17L-18L. REPAIR DOUBLER ON LH REAR FUSE 1 SKIN, BTW FR 61-63 AND BTW STR 16L-18L

Part: NONE — NONE · airframe 45,246 hrs · 29,024 cycles

CF3 CORROSION FOUND ON LH SILL #4. AFTER INVESTIGATION, FITTING DAMAGED UNDERNEATH SILL. FITTING REPAIRED WITH 2 BUSHINGS

Part: NONE — NONE · airframe 45,246 hrs · 29,024 cycles

CF2 LH OMEGA BEAM #2, 2 SUSPECTED CRACKS AT FR 26, 28. CRACKS ON LH OMEGA BEAM #2 REPAIRED. 2 REPAIR DOUBLERS ON LH CENTER FUSE 2 OMEGA BEAM O INBD FLANGE AT FR 26 & 28

Part: NONE — NONE · airframe 45,246 hrs · 29,024 cycles

3 CRACKS SUSPECTED ON LH OMEGA BEAM #1 AT FR 21, 22, 23. BEAM REPAIRED WITH 3 DOUBLERS. 3 REPAIR DOUBLERS ON LH CENTER FUSE 1 OMEGA BEAM, ON INBD FLANGE AT FR 21, 22 AND 23

Part: NONE — NONE · airframe 45,246 hrs · 29,024 cycles

CENTER FUSE 4, FRAME 59 CRACKED BTW STR 15L-16L. CENTER FUSE 4, ON FRAME 59 BTW STR 15L-16L, RIVETS REMOVED FOR INVESTIGATION. FR 59 BTW 14L-15L SPLICE REMOVED. MADE REPAIR PART LOCALLY FABRICATED. CENTER FUSE 4, FRAME 59 BTW 15L-16L, CRACK REPAIRED

Part: NONE — NONE · corrosion level 2 · airframe 45,246 hrs · 29,024 cycles

CF3 LH OMEGA BEAM FOUND CORRODED AND 2 CRACKS SUSPECTED AT FR51 AND FR 52. AFTER NDT INSPECTION (2X) CRACKS CONFIRMED ON LH OMEGA BEAM #2. CUT OUT AT 2X CRACK LOCATION AT FR 51 AND FR 52 PERFORMED. CF3 LH OMEGA BEAM CRACKS REPAIRED.

Part: NONE — NONE · airframe 45,246 hrs · 29,024 cycles

CORROSION FOUND ON RAD ALT #2 ANTENNA BASE DOUBLER BTW FR68-69 AND BTW STR 21L-21R IN RF1 AREA. AT RAD ALT #2, AFTER INVESTIGATION INNER AND EXTERNAL DOUBLER CORROSION FOUND OUT OF LIMIT AND SKIN CRACKED AROUND FASTENERS. DOUBLER AND FILLER FOR #2 ANTENNA FABRICATED. INNER AND EXTERNAL DOUBLER BTW FR 68-69 AND STR 21L-21R REPALCED. RADIO ALT #2 ANTENNA BASE DOUBLER BTW FR 68-69 BTW STR 21L-21R REPLACED. SKIN AT RADIO ALT #2 ANTENNA REPAIRED

Part: NONE — NONE · airframe 45,246 hrs · 29,024 cycles

CRACK SUSPECTED (6X) ON RH SKIN AROUND FASTENERS BTW FR 77-80 BTW STR 3L-9L. SKIN REPAIRED WITH 8 BUSHINGS REPAIR

Part: FRAME — CORRODED (FRM 59 S20L/R) · corrosion level 2 · airframe 45,246 hrs · 29,027 cycles

CENTER FUSE 4, FRAME 59 CORRODED BTW STR 20L-20R. CENTER FUSE 4, ON FRAME BTW STR 20L-20R CORROSION BLENDED AND FOUND T BE OUT OF LIMIT. MADE REPAIR PART, LOCALLY FABRICATED. CENTER FUSE 4, FRAME 59 BTW STR 20L-20R AREA REPAIRED.

Part: MOUNT BRACKET — NOT REPORTED (FWD FUSELAGE) · airframe 45,246 hrs · 29,027 cycles

PERMANENT REPAIR TO PERFORM PER ETD 2020-145-003599 FOR FWD FUSELAGE LH UPPER LATERAL MOUNTING BRACKET. STRUCTURE REPAIRED WITH COLDWORKING OF 11 HOLES

Part: SKIN — CORRODED (FRMS 61-65) · corrosion level 2 · airframe 45,246 hrs · 29,027 cycles

REAR FUSE I, RH SILL BTW FRAME 61-65 CORRODED. RH SILL BTW FR61-65 CORROSION BLENDED AND FOUND OUT OF LIMIT. RH SILL BTW FR 61-65 REPLACED. IN ADDITION MIS DRILLED HOLE AT FR 63 REPAIRED.

Part: FLOOR SUPPORT — CORRODED (FRMS 18-23) · corrosion level 2 · airframe 45,246 hrs · 29,027 cycles

CF1 CORROSION FOUND ON RH OUTBD OMEGA BEAM REPAIR BTW FR18-19 AND AT FR 23. CF1 ON RH OMEGA BEAM BTW FR 18-19 SURFACE CORROSION BLENDED WITHIN LIMIT AND REPROTECTED. CF1 ON RH OMEGA BEAM AT FR23 OLD REPAIR REMOVED FOR INVESTIGATION AND FOUND CORRODED OUT OF LIMITS. CF1 ON RH OMEGA BEAM AT FR23 NEW SRM REPAIR CARRIED OUT.

Part: GUSSET — CORRODED (FRAMES 59-61) · airframe 45,246 hrs · 29,027 cycles

CENTER FUSE 4, RH GUESSET BTW FRAME 59-61 CORRODED. OMEGA BEAM IS CORRODED. BEAM REPAIRED WITH A DOUBLER

Part: SKIN — CRACKED (FRMS 77-80 S3-9L) · airframe 45,246 hrs · 29,027 cycles

CRACK SUSPECTED (5X) ON LH SKIN AROUND FASTENERS BTW FR77-80 BTW STR 3L-9L. SKIN REPAIRED WITH 5 BUSHINGS REPAIR.

Part: LAMP — INOPERATIVE · airframe 44,969 hrs · 28,760 cycles

RH FWD WTF EMERGENCY LIGHT INOP. R/R FWD WTF EMERGENCY LIGHT LAMP. OP CHECK SAT

Part: NONE — INOPERATIVE · airframe 44,952 hrs · 28,742 cycles

SERVICE DOOR EXTERNAL EMERGENCY LIGHT INOP R/R SERVICE DOOR EXTERNAL EMERGENCY LIGHT ASSY. OPS CHECK SAT

Part: NONE — NONE · airframe 44,872 hrs · 28,669 cycles

EMERGENCY FLOOR LIGHT STRIP DETACHED BY GALLEY. RESECURED EMERGENCY LIGHT STRIP

Part: LIGHT — INOPERATIVE · airframe 44,009 hrs · 27,928 cycles

EMERGENCY LIGHTS ON LH AND RH WING LADDER FAIRING INOPERATIVE. REMOVED AND REPLACED RH EXTERNAL EMERGENCY LIGHT BULB. REMOVED AND REPLACED LH EXTERNAL EMERGENCY LIGHT ASSEMBLY. OPS CHECK SAT.

Part: STRAP — MISSING · airframe 43,884 hrs · 27,806 cycles

FLOOR PATH EXIT LOCATION NOT CORRECT PER FA. REPLACED MISSING SECTION OF PHOTOLUMINESCENT STRIP

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 43,186 hrs · 27,175 cycles

ROW 18 EMERGENCY EXIT CEILING LIGHT INTERMITTENT. R&R #3 EMERGENCY BATTERY. OPS CHECK SAT.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 42,595 hrs · 26,634 cycles

CABIN EMERGENCY LIGHTS FAILED TO ILLUMINATE AT EMERGENCY EXITS AND AFT AISLE LIGHTS. REMOVED AND REPLACED BATTERY POWER SUPPLY NR 2 AND BATTERY POWER SUPPLY NR 3. OPERATIONS CHECK GOOD.

Part: SKIN — DAMAGED (FWD FUSELAGE) · airframe 42,421 hrs · 26,493 cycles

FWD FUSELAGE SKIN DAMAGED ABOVE CAPTS WINDOW.................REMOVED DAMAGED AREA INSTALLED DOUBLER AND TRIPLER ON FWD FUSELAGE SKIN ABOVE CAPTS WINDOW IAW ETD 2020-145-005075

Part: SHEAR TIE — CRACKED (FRAME 72) · airframe 42,420 hrs · 26,493 cycles

CRACKED SHEAR CLIP FROM EDGE OF CLIP TO ATTACHING RIVET HOLE----REMOVED AND REPLACED WITH NEW ITEM

Part: SHEAR TIE — CRACKED (FRAME 66) · airframe 42,420 hrs · 26,493 cycles

CRACKED RAMP ANGLE FROM EDGE OF ANGLE TO ATTACH RIVET HOLE----REMOVED AND REPLACED WITH NEW ITEM

Part: SHEAR TIE — CRACKED (FRAME 68) · airframe 42,420 hrs · 26,493 cycles

SHEAR CLIP CRACKED FROM EGDE TO ATTACHING RIVET HOLE-----REMOVED AND REPLACED CLIP WITH NEW ITEM

Part: SHEAR TIE — CRACKED (FRAME 67) · airframe 42,420 hrs · 26,493 cycles

CRACKED SHEAR CLIP FROM EDGE OF CLIP TO ATTACH RIVET HOLE----REMOVED AND REPLACED WITH NEW ITEM

Part: ANGLE — CORRODED (BS 65-68) · corrosion level 2 · airframe 42,420 hrs · 26,493 cycles

CORRODED "Z" ANGLE AT FUSELAGE CARGO DOOR OPENING --REMOVED AND REPLACED WITH NEW ITEM

Part: SHEAR TIE — CRACKED (FRAME 71) · airframe 42,420 hrs · 26,493 cycles

CRACKED SHEAR CLIP FROM EDGE OF CLIP TO ATTACH RIVET HOLE----REMOVED AND REPLACED WITH NEW ITEM

Part: SHEAR TIE — CRACKED (FRAME 65) · airframe 42,420 hrs · 26,493 cycles

CRACKED SHEAR CLIP FROM EDGE OF CLIP TO ATTACH RIVET HOLE----REMOVED AND REPLACED WITH NEW ITEM

Part: SUPPORT ANGLE — CRACKED · airframe 42,421 hrs · 26,493 cycles

L/H SUPPORT ANGLE BETWEEN #5 AND #6 PROFILE BRACKET IS CRACKED .........REMOVED AND REPLACED SUPPORT ANGLE BETWEEN #5 AND #6 PROFILE BRACKET

Part: BRACKET — CRACKED (FRAME 60) · airframe 42,273 hrs · 26,384 cycles

CRACKED BRACKET AT R/H FRAME 60 CARGO DOOR TORSION ASSY FWD MOUNT ......................REMOVED AND REPLACED BRACKET AT R/H FRAME 60 CARGO DOOR TORSION ASSY FWD MOUNT

Part: BRACKET — CRACKED (LT PYLON) · airframe 42,421 hrs · 26,493 cycles

L/H PYLON #5 AND #6 PROFILE BRACKET IS CRACKED.....................REMOVED AND REPLACED L/H PYLON #5 AND #6 PROFILE BRACKETS

Part: ANGLE — CORRODED (PAX DOOR RAMP) · airframe 42,420 hrs · 26,493 cycles

SIGNS OF CORROSION ON PASSENGER FLOOR RAMP ANGLE AFT END....R&R DAMAGED ANGLE.

Part: SUPPORT — CORRODED (GALLEY) · airframe 42,273 hrs · 26,384 cycles

SIGNS OF CORROSION AROUND NUT PLATE HOLE ON FWD GALLEY SILL,,,,,,,,,,,,, REMOVED AND REPLACED FWD GALLEY SILL

Part: GUSSET — CORRODED (FRAME 40) · airframe 42,421 hrs · 26,493 cycles

R/H CENTER OMEGA BEAM GUSSET AT FRAME 40 SHOWS SIGNS OF CORROSION............... REMOVED AND REPLACED R/H CENTER OMEGA BEAM GUSSET AT FRAME 40

Part: FRAME — CORRODED (FRM 22) · airframe 42,273 hrs · 26,384 cycles

SIGNS OF CORROSION ON STOP SIGN R/H SIDE AT FRAME 22................REMOVED AND REPLACED STOP SIGN R/H SIDE AT FRAME 22

Part: SHEAR TIE — CRACKED (FRAME 26) · airframe 42,273 hrs · 26,384 cycles

SHEAR CLIP CRACKED AT FR 26 STR 15R.................REMOVED AND REPLACED SHEAR CLIP AT FRAME 26 STR15R

Part: SHEAR TIE — CRACKED (FRAME 25) · airframe 42,273 hrs · 26,384 cycles

SHEAR CLIP CRACKED AT FRAME 25 STR 15R..........REMOVED AND REPLACED SHEAR CLIP AT FRAME 25 STR 15R

Part: CHANNEL — CRACKED (COCKPIT) · airframe 42,421 hrs · 26,493 cycles

L/H COCKPIT OVERHEAD LATERAL CHANNEL CRACKED NEAR FWD END WINDSHIELD TIE IN...................REPAIRED IAW ETD 2020-145-003599 AND EO EMB145-53-074-0

Part: SHEAR TIE — NOT REPORTED (FRAME 24) · airframe 42,273 hrs · 26,384 cycles

SHEAR CLIP AT FRAME 24 15R-16R...................REMOVED AND REPLACED SHEAR CLIPAT FRAME 24 1STR 15R-16R

Part: SHEAR TIE — CRACKED (FRAME 72) · airframe 42,273 hrs · 26,384 cycles

SHEAR CLIP AT FRAME 72 AND STR 17L-18L .............REMOVED AND REPLACED SHEAR CLIP AT FRAME 72AN D STR17L-18L

Part: BRACKET — CRACKED · airframe 42,421 hrs · 26,493 cycles

R/H L/E #1 HORSE SHOE BRACKET IS CRACKED............... REMOVED AND REPLACED R/H #1HORSE SHOE BRACKET

Part: BRACKET — CRACKED (WING TO FUSELAGE) · airframe 42,421 hrs · 26,493 cycles

R/H WING TO FUSELAGE LOWER #1 MOUNTING BRACKET IS CRACKED................REMOVED CRACKED SECTION OF R/H WING TO FUSELAGE #1 MOUNTING BRACKET FABRICATED REPAIR PARTS AND DOUBLER INSTALLED REPAIR PARTS AND DOUBLER IAW SRM 51-40-02 AND 57-20-01

Part: FIREWALL — CRACKED (NR 1 NACELLE) · airframe 42,273 hrs · 26,384 cycles

#1 PYLON FIRE WALL HAS CRACK AT FRM 67......... REPAIRED #1 PYLON FIREWALL AT FRAME 67

Part: FRAME ANGLE — CRACKED (FRM 10) · airframe 42,420 hrs · 26,493 cycles

CRACKED SIDEWALL VERTICAL FRAME IN COCKPIT AREA AT ATTACHMENT TO WINDOW LOWER HORIZONTAL FRAME COUPE RAIL AT RIVET LOCATION----REMOVED AND REPLACED VERTICAL FRAME WITH NEW ITEM

Part: BRACKET — CRACKED (LT OVERWING) · airframe 42,421 hrs · 26,493 cycles

L/H OVERWING FWD L BRACKET IS CRACKED.............REMOVED AND REPLACED L/H OVERWING FWD L BRACKET

Part: FAN — INOPERATIVE (RECIRCULATION) · airframe 41,049 hrs · 25,381 cycles

SMOKE IN COCKPIT AND CABIN WITH AN ELECTRICAL SMELL. DECLARED AN EMERGENCY. R & R RECERC FAN. OPS CHECK GOOD.

Part: ELEVATOR — STIFF · airframe 38,327 hrs · 23,141 cycles

ELEVATOR CONTROL FEEL STIFF ON BOTH ENDS OF TRAVEL. PERFORMED GVI OF ELEVATOR CABLES, PULLEYS AND QUADRANTS, ALSO CHECKED TENSIONS OF ELEVATOR CABLES. NO DEFECT NOTED.

Part: ELECTRONIC UNIT — FAILED (MLG) · airframe 38,209 hrs · 23,030 cycles

MLG AIR/GROUND FAIL ON EICAS. SWAPPED LT AND RT MLG NR 1 WOW PROXIMITY SWITCHES WITH THE LT AND RT LOWER UPLOCK PROXIMITY SWITCHES. REMOVED AND REPLACED THE LGEU, OPS CHECKED GOOD.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 37,787 hrs · 22,681 cycles

FWD CEILING EMERGENCY SIGN ADJACENT TO GALLEY INOPERATIVE. SECURED THE CONNECTOR ON THE SIGN, R & R THE NR 1 INVERTER, OPS CHECKED GOOD.

Part: BULB — INTERMITTENT (EMERGENCY LIGHTS) · airframe 37,042 hrs · 22,020 cycles

SERVICE DOOR FLOOD LIGHT NR 8, INTERMITTENT. R & R THE BULB, OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 37,042 hrs · 22,020 cycles

MAIN DOOR FLOOD LIGHT NR 13 FOUND INOPERATIVE. R & R THE BULB, OPS CHECKED GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 36,516 hrs · 21,605 cycles

LT EMERGENCY DOOR FLOOD LIGHT NR 21 IS INOP. R&R LT EMERGENCY DOOR FLOOD LIGHT NR 21 BATTERY OPS CHECK GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 36,516 hrs · 21,605 cycles

RT EMERGENCY DOOR FLOOD LIGHT NR 22 IS INOP. R&R RT EMERGENCY DOOR FLOOD LIGHT NR 22 BATTERY, OPS CHECK GOOD.

Part: TRANSDUCER — FAULTY (BRAKES) · airframe 36,003 hrs · 21,213 cycles

CREW REPORTED RIGHT MLG BRAKES GRAB AND LET GO UNDER 25KTS WHEN CONSTANT BRAKE PRESSURE IS APPLIED. MX REMOVED AND REPLACED NR 3 WHEEL SPEED TRANSDUCER WITH OPS CHECKED GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,331 hrs · 20,734 cycles

DURING C-CHECK THE RT OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 18-19. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW SRM 53-21-10. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,331 hrs · 20,734 cycles

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

Part: BEAM — CORRODED (CARGO DOOR) · airframe 35,331 hrs · 20,734 cycles

DURING C-CHECK, CARGO DOOR LOWER BEAM HAS CORROSION. R & R WITH NEW CARGO DOOR LOWER BEAM IAW SRM 51-40-02. ACFT APPROVED FOR RETURN TO SERVICE.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 35,331 hrs · 20,734 cycles

DURING C-CHECK, TOILET SUPPORT STRUCTURE AT FRAME 61 HAS AREAS OF CORROSION. R & R WASTE DRAIN DUMP CUP ASSY IAW SRM 51-40-02. ACFT APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 35,331 hrs · 20,734 cycles

DURING C-CHECK. FRAME 20 CENTER OMEGA BEAM AT INBD CROSSBEAM MOUNT HAS CORROSION. REMOVED AND INSTALLED NEW CENTER OMEGA BEAM BETWEEN FROM 18-24 IAW SRM 51-40-02. ACFT APPROVED FOR RETURN TO SERVICE.

Part: FITTING — CORRODED (FUSELAGE) · airframe 35,331 hrs · 20,734 cycles

DURING C-CHECK, FWD SHEAR CLIP FRAME 65 AT CARGO DOOR LOWER BEAM CORRODED. REPAIRED SHEAR CLIP AT FRAME 65 UNDER STRIKER PLATE IAW EC5330-03108, ORIGINAL. ACFT APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT) · airframe 33,009 hrs · 19,077 cycles

DURING MAINTENANCE INSPECTION, THE SERVICE DOOR CEILING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE R & R THE NR 2 EMERGENCY LIGHT INVERTER, OPERATIONALLY TESTED WITH NO DEFECTS AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 32,887 hrs · 19,002 cycles

THE CREW REPORTED A ODOR OF BURNING ELECTRICAL ODOR WHEN PACK 2 WAS TURNED ON. OPEN

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,223 hrs · 17,247 cycles

PILOT REPORTED THE CENTER OVERHEAD EMERGENCY EXIT LIGHT INOPERATIVE. MX R & R THE AISLE OVERHEAD EMERGENCY LIGHT SIGN WITH OPS CHECK SUCCESSFUL. ACFT APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — ARCED (CABIN) · airframe 30,136 hrs · 17,198 cycles

CREW REPORTED SMOKE AND SMALL FLAMES COMING OUT OF THE OVERHEAD LIGHTS NEAR ROW 9 & 10. CONTRACT MAINTENANCE PLACED ON MEL 33-20-00-2 AND REMOVED LAMP. MX R & R THE CABIN CEILING LIGHT ASSY ABOVE SEATS 9 & 10 WITH OPS CHECK GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — SMOKE (GALLEY) · airframe 30,099 hrs · 17,173 cycles

THE CREW REPORTED SMOKE FROM GALLEY LIGHTS. MAINTENANCE INSPECTED AND REPLACED THE GALLEY LIGHT ASSEMBLY. OPS CHECKED GOOD.

Part: SKIN — DENTED (ZONE 200) · airframe 29,583 hrs · 16,836 cycles

SKIN AT REAR LOWER FUSELAGE BETWEEN BS 71-72 AT STR 20L. REMOVED DAMAGE, FABRICATED REPAIR PARTS AND, INSTALLED IAW ETD 2014-145-016911 AND EC 5330.02870. NDT PERFORMED BY INSPECTION SERVICES, NO INDICATIONS NOTED. EXTERNAL GVI MUST BE ACCOMPLISHED AT EVER 5645 FLIGHT CYCLES, NEXT INSPECTION DUE AT 22481 FLIGHT CYCLES.

Part: FLOOR SUPPORT — CORRODED (FRAMES 68-71) · airframe 29,583 hrs · 16,836 cycles

RT FLOOR SUPPORT FROM FRAMES 68-71 CORRODED. R & R FLOOR SUPPORT IAW SRM 51-42-02.

Part: DOUBLER — CORRODED (PARTITION) · airframe 29,583 hrs · 16,836 cycles

FRAME 61, LT FWD PARTITION DOUBLER CORRODED. R & R PARTITION DOUBLER IAW SRM 51-40-02, 53-31-02,51-40-04, 51-40-06, AMD CPM 51-21-03.

Part: FLOOR SUPPORT — CORRODED (FRAMES 68-71) · airframe 29,583 hrs · 16,836 cycles

RT FLOOR SUPPORT FROM FRAMES 68-71 CORRODED. R & R FLOOR SUPPORT IAW SRM 51-42-02.

Part: FLOORBEAM — CORRODED (FRAME 19A) · airframe 29,583 hrs · 16,836 cycles

FLOORBEAM AT FRAME 19A X5633 AND Y0 TO 479.0 IS CORRODED. R & R FLOORBEAM IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FRAME 61) · airframe 29,583 hrs · 16,836 cycles

FLOOR SUPPORT AT FRAME 61 RT SIDE CORRODED. REPAIRED RT OMEGA BEAM AT FRAME 61 IAW ETD 2014-145-017735. NDT PERFORMED.

Part: FLOOR SUPPORT — CORRODED (FRAMES 68-71) · airframe 29,583 hrs · 16,836 cycles

LT FLOOR SUPPORT FROM FRAMES 68-71 CORRODED. R & R FLOOR SUPPORT IAW SRM 51-40-04,51-40-02, AND SWPM 20-00-05.

Part: FLOOR SUPPORT — CORRODED (FRAMES 58-62) · airframe 29,583 hrs · 16,836 cycles

RIGHT FLOOR SUPPORT FROM FRAMES 58-62 IS CORRODED. R & R FLOOR SUPPORT BETWEEN FRAMES 53-59 IAW SRM 51-40-02, 51-40-06,51-40-04, CPM 51-21-04, 51-21-05.

Part: FLOOR SUPPORT — CORRODED (BS 5292-6523) · airframe 29,583 hrs · 16,836 cycles

LT FLOOR SUPPORT BS 5292-6523 CORRODED. R & R LT FLOOR SUPPORT IAW SRM 51-40-02, 51-40-06, 51-20-03, CPM 51-21-04 AND SWPM 20-00-05.

Part: FLOOR SUPPORT — CORRODED (FRAMES 59-61) · airframe 29,583 hrs · 16,836 cycles

FLOOR SUPPORT FROM FRAMES 59-61 AT Y 0.0 CORRODED. R & R FLOOR SUPPORT IAW SRM 51-40-00, 51-20-03, CPM 51-21-06 AND 51-21-04.

Part: DOUBLER — CORRODED (PARTITION) · airframe 29,583 hrs · 16,836 cycles

RIGHT FRAME 61 FWD PARTITION DOUBLER CORRODED. REMOVED DOUBLER AND NINE (9) NUT PLATES. RECIEVED NEW DOUBLER. REINSTALLED ORIGINAL NINE (9) NUT PLATES AND INSTALLED NEW DOUBLER IAW SRM 51-40-02, 51-49-09, 51-20-03, 51-40-06, SWPM 20-20-00 AND CPM 51-21-03. WO 80204, WORK CARD 2297.

Part: SILL — CORRODED (FRAMES 61-68) · airframe 29,583 hrs · 16,836 cycles

RIGHT SILL AT FRAME 61-68 CORRODED. R & R CORRODED SILL IAW SRM 51-40-04, 51-40-06, 51-40-00 AND SPM 51-21-03.

Part: FLOOR SUPPORT — CORRODED (FRAME 61-65) · airframe 29,583 hrs · 16,836 cycles

LT FLOOR SUPPORT AT FRAMES 61 - 65 CORRODED. R & R FLOOR SUPPORT IAW SRM 51-40-00, 51-40-02, 51-40-04, 51-40-06, AND CPM 51-21-03.

Part: FLOOR SUPPORT — CORRODED (FRAME 50) · airframe 29,583 hrs · 16,836 cycles

RT FLOOR SUPPORT AT FRAME 50 CORRODED. R & R FLOOR SUPPORT IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FRAMES 59-61) · airframe 29,583 hrs · 16,836 cycles

FLOOR SUPPORT FRAMES 59 - 61, Y479.0 CORRODED. R & R FLOOR SUPPORT IAW SRM 51-40-00, 51-20-03, AND CPM 51-21-06, AND 51-21-04.

Part: FLOOR SUPPORT — CORRODED (FRAMES 59-61) · airframe 29,583 hrs · 16,836 cycles

FLOOR SUPPORT FRAMES 59-61 Y479.0 CORRODED. R & R FLOOR SUPPORT IAW SRM 51-40-00, 51-20-03, AND ERJ145, CPM51-21-06, 51-21-04.

Part: LIGHT — BURNED (CABIN) · airframe 27,919 hrs · 15,812 cycles

THE CREW REPORTED A BURNING ODOR IN THE CABIN. MX INSPECTED THE ACFT AND FOUND THE SIDEWALL LIGHT ASSY AT ROW 10 TO BE BURNED. MX R & R THE AFFECTED LIGHT ASSY, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ENGINE — OVERSPEED (NR 1) · airframe 27,692 hrs · 15,655 cycles

ACFT WAS ON TAXI WHEN CREW ABORTED TAKEOFF DUE TO E1 EXCEEDENCE. MX AND INSPECTION FOUND DAMAGE TO ENGINE THRU A BOROSCOPE INSPECTION. THE NR 1 ENGINE WAS R & R IAW TASKCARD 6271001. ECN CONTROL NR JW 111150061313. ALL WORK ACCOMPLISHED WITH LEAK CHECKS AND RUNS AND WAS RELEASED TO SEVICE.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 27,132 hrs · 15,329 cycles

DURING ROUTINE MX THE GALLEY EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MX REPLACED THE NR 2 EMERGENCY LIGHT BATTERY. OPS CHECKS WERE GOOD.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 25,631 hrs · 14,328 cycles

DURING MX INSPECTION THE NR 4 EMERGENCY LIGHT BATTERY WAS FOUND TO BE DISCHARGED AND INOPERATIVE. MX R & R NR 4 EMERGENCY LIGHT BATTERY WITH OPS CHECK SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: WARNING MESSAGE — FALSE ACTIVATION (FIRE DETECTION) · airframe 25,492 hrs · 14,226 cycles

CREW REPORTED AURAL FIRE WARNING ON EICAS DURING TAKEOFF. MX R & R THE AURAL WARNING UNIT WITH OPS CHECK SUCCESSFUL. UNABLE TO DUPLICATE FAULT. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 24,068 hrs · 13,283 cycles

MX REPORTED THE LT EXTERNAL EMERGENCY LIGHT WAS INOPERATIVE. MX REPLACED THE EXTERNAL EMERGENCY LIGHT ASSY. OPS CHECKS WERE GOOD.

Part: FUSE — BLOWN (EMERGENCY LIGHT) · airframe 23,654 hrs · 12,960 cycles

THE CREW REPORTED PANEL 191, LEFT SIDE EMERGENCY LIGHT INOPERATIVE. MX REPLACED THE FUSE ON THE NR 1 BATTERY POWER SUPPLY. OPS CHECKED GOOD.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 22,980 hrs · 12,537 cycles

ORD FLT 6019 THE CREW REPORTED EMERGENCY LIGHTS WERE INOPERATIVE AT ROW 12. MAINTENANCE INSPECTED AND RESET SYSTEM. OPERATIONAL CHECKS WERE GOOD.

Part: FUEL LINE — LEAKING (APU) · airframe 22,166 hrs · 11,963 cycles

FLIGHT 5855 - IAD - FLIGHT CREW REPORTED BURNING SMELL IN COCKPIT WITH APU AND PACKS RUNNING. IAD MX REMOVED AND REPLACED FUEL LINE FROM FUEL FILTER TO FUEL CONTROL UNIT AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: VALVE — FAILED (ZONE 400) · airframe 22,164 hrs · 11,962 cycles

FLT 5832, CREW REPORTED AN ENGINE 1 HIGH STAGE BLEED VALVE FAIL MESSAGE ON CLIMBOUT. THE AIRCRAFT RETURNED AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NR 1 ENGINE HIGH STAGE BLEED VALVE. OPERATIONAL CHECKS WERE GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,388 hrs · 11,476 cycles

EMERGENCY LIGHT AT SEAT 12BC INOP. REMOVED AND REPLACED LIGHT BULB IAW EMB 145 AMM 33-50-08, OPS CHECK GOOD.

Part: ENGINE — LEAKING (NR 1) · airframe 21,258 hrs · 11,407 cycles

DFW - FLIGHT 2463 THE CREW REPORTED A STRONG BURNING OIL SMELL FROM THE NUMBER ONE ENGINE BLEED AT HIGH POWER SETTINGS. THE AIRCRAFT LANDED AT DFW WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND IT WAS FERRIED TO IAH WHERE MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE ENGINE, OPERATIONALLY AND LEAK CHECK WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DUCT — BLOWN (NR 1) · airframe 21,233 hrs · 11,389 cycles

SUPPLEMENT INFORMATION: CORRECTED PART NUMBER IAD FLT 5850 THE CREW REPORTED SMOKE IN THE COCKPIT ON CLIMBOUT. THE AIRCRAFT RETURNED TO IAD AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NR 1 NOISE ATTENUATOR DUCT. OPERATIONAL CHECKS WERE GOOD.

Part: RMU — MALFUNCTIONED (COCKPIT) · airframe 19,662 hrs · 10,521 cycles

LOST BOTH TRANSPONDER SYSTEMS IN FLIGHT-RMU 1/2 ALL DASHES IN ATC/TCAS & TCAS DISPLAY. FLIGHT DIVERTED INTO TYS PERFORMED ELECTRICAL RESET OF RMU 1 & 2 IAW EMB 145XR AMM 34-32-00, OPS CHECK GOOD. AIRCRAFT RELEASED AND RETURNED TO SERVICE.

Part: HOUSING — OUT OF LIMITS (VERTICAL STAB) · airframe 18,925 hrs · 10,125 cycles

TYS - LT AND RT SPHERICAL BEARING HOUSING OUT OF LIMITS. REAMED LT AND RT VERTICAL STAB. SPHERICAL BEARING HOUSING TO FIRST OVERSIZE.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 18,461 hrs · 9,882 cycles

RIC - DURING ROUTINE MAINTENANCE, RIC MX FOUND LT FWD EXTERIOR EMERGENCY LIGHT AND NR 1 AISLE EMERGENCY LIGHT WOULD NOT ILLUMINATE. MX REMOVED AND REPLACED NR 1 EMERGENCY BATTERY CHARGER AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: LOCK — DIRTY (CABIN DOOR) · airframe 18,206 hrs · 9,732 cycles

FLIGHT 2893 - EWR - FLIGHT CREW REPORTED THAT MAIN CABIN DOOR JAMMED HALF WAY OPEN/CLOSED. EWR MX CLEANED AND LUBED MAIN CABIN DOOR LOCKS AND ROLLERS AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: CONTROLLER — INOPERATIVE (CABIN PRESSURE) · airframe 17,488 hrs · 9,344 cycles

IAH - FLIGHT 2547, DURING CRUISE THE CREW REPORTED THAT PRESSURIZATION WAS INOP IN AUTO, AND COULD NOT BE CONTROLLED IN MANUAL. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE PRESSURIZATION CONTROLLER, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 17,029 hrs · 9,081 cycles

DURING ROUTINE MAINTENANCE THE EMERGENCY EXIT LIGHT OVER THE EXIT ROW WAS FOUND INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY LIGHT INVERTER. OPERATIONAL CHECKS WERE GOOD.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 15,600 hrs · 8,224 cycles

EMERGENCY EXIT ROW CEILING PANEL AFT LIGHT DIMMING OUT. REMOVED AND REPLACED EXIT ROW EMERGENCY LIGHT INVERTER IAW EMB 145XR AMM 33-51-11. OPS CHECK GOOD.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 15,943 hrs · 8,492 cycles

RIC MX - DURING ROUTINE MAINTENANCE, RIC MX FOUND SERVICE DOOR EMERGENCY LIGHT INOPERATIVE. MX REMOVED AND REPLACED NR 3 INVERTER AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 15,943 hrs · 8,492 cycles

RIC MX - DURING ROUTINE MAINTENANCE, RIC MX FOUND EMERGENCY LIGHT SIGN IN GALLEY INOPERATIVE. MX REMOVED AND REPLACED NR 2 INVERTER AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: SWITCH — MALFUNCTIONED (AC PACK) · airframe 15,476 hrs · 8,246 cycles

A/C N11150 HAD PACK 2 OVERLOAD IN FLIGHT. PUT ON MEL 21-51-00/2 CERT 163709 CAT C. CLE MAINTENANCE REMOVED AND REPLACED PACK 2 TEMP SWITCH, OPERATIONAL AND LEAK CHECKS GOOD IAW EMB 145XR AMM 21-51-08. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 15,287 hrs · 8,138 cycles

EWR MX - DURING ROUTINE MAINTENANCE, MX FOUND AIR/GND FAIL MESSAGE ON EICAS. MX RESET THE SYSTEM AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS)

DURING ROUTINE MX THE AFT EMERGENCY EXIT SIGN WAS FOUND INOPERATIVE. MX INSPECTED AND REPLACED THE AFT EMERGENCY EXIT SIGN. OPS CHECKS WERE GOOD.

Part: CONTROL MODULE — ODOR (CABIN LIGHTS)

FLIGHT CREW REPORTED LT SIDE CABIN LIGHT INOPERATIVE AND BURNING SMELL IN CABIN. EWR MX REMOVED AND REPLACED CONTROL MODULE FOR SIDE LIGHTS. CLEANED GROUND STUD FOR PINK FOR THE MODULE. (K)

Part: BRACKET — WORN (RT AILERON)

SHV - DURING C-CHECK IT WAS FOUND THAT THE RT AILERON PCA BRACKET HAD A MIGRATED HAT BUSHING. THE HOLE WAS WORN OUT OF LIMITS AND WOULD NOT RETAIN THE BUSHING. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET IAW EMB 145XR SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE. (S)

Part: INVERTER — FAULTY (EMERGENCY LIGHTS)

CLE FLIGHT 2519. THE CREW REPORTED THE EMERGENCY LIGHT OVER THE EXIT ROW WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY LIGHT INVERTER. OPERATIONAL CHECKS WERE GOOD. (S)

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 13,105 hrs · 6,955 cycles

FLIGHT 2383, DURING PREFLIGHT INSPECTION THE CREW REPORTED, ROW 12 OVERHEAD EMERGENCY LIGHT EXIT SIGN NOT LIGHTING UP. MAINTENANCE RESET THE EMERGENCY LIGHT SYSTEM, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 11,521 hrs · 6,150 cycles

THE RIGHT FWD FUSELAGE II, CENTRAL FUSELAGE I SKIN AND SEVERAL UNDERLYING STRUCTURAL MEMBERS WERE DAMAGED AS A RESULT OF A TUG STRIKING THE AIRCRAFT. THE DAMAGE IS CONTAINED BETWEEN FRAMES 7 & 14, STR 16R & 20R. THE A/C IS BEING REPAIRED IAW EA5330-01106.

Part: STRIP — LOOSE (CABIN) · airframe 10,726 hrs · 5,725 cycles

CLE FLIGHT 2322 - THE CREW REPORTED THE AISLE PATH LIGHT STRIP WAS LOOSE ON THE FLOOR. MAINTENANCE INSPECTED AND RE-ATTACHED THE AISLE PATH LIGHT STRIP. OPERATIONAL CHECKS WERE GOOD.

Part: BEVEL GEAR — FAILED (NR 2 ENGINE) · airframe 8,847 hrs · 4,730 cycles

PVD FLIGHT NR 2366 THE CREW REPORTED ENGINE NR 2 FAILED IN FLIGHT ON DESCENT INTO PVD. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT.MAINTENANCE REPLACED THE NR 2 ENGINE. OPERATIONAL CHECKS WERE GOOD. DFDR DATA SHOWED NR 2 ENGINE DECREASED FROM 91% TO 0 IN 1 SECOND.THIS IS INDICATIVE OF A RADIAL DRIVE SYSTEM FAILURE.TEAR DOWN REPORT INDICATED THE ENGINE FAILURE WAS CAUSED BY THE UPPER BEVEL GEAR FAILURE. CAUSE OF GEAR FAILURE : RESONANCE MODE (2DOC).

Part: DOOR — OUT OF ADJUST (PAX) · airframe 6,361 hrs · 3,381 cycles

IAH - FLIGHT 2375, DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE MAIN CABIN DOOR WAS HARD TO OPEN AND CLOSE. MAINTENANCE RE-RIGGED THE PASSENGER DOOR, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ODOR — DETECTED (CABIN) · airframe 3,061 hrs · 1,636 cycles

DURING CRUISE CREW REPORTED STRONG ODOR IN THE CABIN. AIRCRAFT DIVERTED TO PHL AS PRECAUTION. INSPECTED AIRCRAFT, PERFORMED ENGINE AND APU WITH BLEEDS ON. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE.