N967UW

Part: NONE — DAMAGED (ZONE 800) · airframe 26,928 hrs · 20,367 cycles

DURING STRUCTURE INSPECTION IT WAS FOUND AN EXISTING REPAIR DOUBLER WITHOUT RECORDS LOCATED AT LEFT MLG DOOR OUTER SKIN AT AFT EDGE UNDER FAIRING AREA, DUE TO THIS FACT THE REPAIR DOUBLER WAS REMOVED AND EXISTING CUT OUT WAS FOUND AT SKIN ONLY. WAS REPAIRED FOLLOWING EMBRAER REPAIR INSTRUCTIONS UNDER ETD2022-190-007969 AND COPPESA EO # COO-EO-2022-15220 AND APPROVED ON ANAC F-200 FORMPROVIDED BY EMB.

Part: CONTROL MODULE — FAULTY (ZONE 100) · airframe 26,647 hrs · 20,124 cycles

AIRCRAFT WAS GROUNDED: ATL-PHL, FLIGHT CREW DECLARED AN EMERGENCY INTO PHL ACCOUNT LANDING GEAR TEMPERATURE EXCEEDANCE. IN ADDITION LEFT AND RIGHT BRAKE FAULT INDICATIONS. WHEN SELECTING AUTOBRAKES, "LG TEMP EXCEEDENCE", "BRK RH FAULT", "BRK LH FAULT" EICAS MSGS QRH COMPLIED WITH. FLIGHT LANDED WITHOUT INCIDENT. REMOVED AND REPLACED MAIN BRAKE CONTROL MODULE IAW AMM 82-41-07-000-801-A. PERFORMED OPERATIONAL TEST ON MAIN BRAKE SYSTEM IAW AMM 32-41-00-710-801-A.

Part: SIGN — DETACHED (CABIN) · airframe 25,618 hrs · 19,154 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY SIGN IN EXIT ROW FELL OFF ON TAKEOFF. MAINTENANCE RESECURED EXIT SIGN PER STANDARD PRACTICES AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: UNKNOWN — MALFUNCTIONED (TE FLAP) · airframe 25,144 hrs · 18,731 cycles

AIRCRAFT NOT GROUNDED: FLIGHT CREW DECLARED AN EMERGENCY INTO BOS ON ACCOUNT OF FLAPS PROBLEM. LANDED WITHOUT INCIDENT AND TAXIED TO THE GATE. MAINTENANCE ACCOMPLISHED OPERATIONAL TEST ON FLAP/SLAT SYSTEMS IAW AMM 27-50-00, NO FAULTS NOTED, NO HISTORY.

Part: COVER — OUT OF POSITION (L1 DOOR HANDLE) · airframe 25,040 hrs · 18,633 cycles

AIRCRAFT NOT GROUNDED: L1 DOOR GUST LATCH/LOCK: FA ADVISES THAT THE LOCK WILL NOT ENGAGE/LATCH TO HOLD/KEEP DOOR LOCKED IN THE OPEN POSITION. L1 DOOR HANDLE COVER BROKEN AND INTERFERING WITH GUST LOCK. TRIMMED BROKEN COVER AND RE-INSTALLED IAW AMM 52-11-00.

Part: SEAL REST — BROKEN (CARGO DOOR FRAME) · airframe 24,329 hrs · 18,118 cycles

MAINTENANCE FOUND A BROKEN OUT PIECE OF THE AFT CARGO DOOR SEAL SEAT AT THE LOWER FRAME. REPLACED THE DOOR SEAL SEAT IAW SRM 51-41-01, AND AMM 53-23-29.

Part: WINDOW SHADE — STUCK (CABIN) · airframe 23,547 hrs · 17,484 cycles

AIRCRAFT WAS NOT GROUNDED. LEFT SIDE EMERGENCY DOOR WINDOW SHADE STUCK. RESET WINDOW SHADE ON LEFT EMERGENCY MIDDLE DOOR PER AMM 25-20-01.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 22,359 hrs · 16,549 cycles

FORWARD LEFT LAVATORY EXIT SIGN LENS BROKEN. REPLACED THE LENS. AIRCRAFT WAS GROUNDED.

Part: RAIL — WORN (FLAP TRACK) · airframe 22,359 hrs · 16,549 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. LEFT WING NR 1 INBOARD FLAP TRACK RAIL WORN, REPLACED FLAP TRACK RAIL PER AMM 57-54-21-400.

Part: BRACKET — CORRODED (FRAMES 86-87) · airframe 22,359 hrs · 16,549 cycles

ANGLE BRACKET HAS CORRODED BETWEEN FRAMES 86 & 87 AND STRINGERS 27R & 28R. REPLACED THE ANGLE BRACKET IAW SRM 51-41-01.

Part: INTERCOSTAL — CORRODED (FRAMES 86-87) · airframe 22,359 hrs · 16,549 cycles

CORROSION FOUND ON INTERCOSTAL BETWEEN FRAMES 86 -87, STRINGERS 27R AND 28R. REPLACED THE INTERCOSTAL ON AFT CARGO IAW SRM 51-41-01.

Part: WINDOW — CRAZED (PAX CABIN) · airframe 22,359 hrs · 16,549 cycles

L1 CABIN WINDOW IS CRAZED. FRAMES 23-24. REPLACED THE WINDOW IAW E190 AMM 56-20-00.

Part: SEAT TRACK — CORRODED (FRAMES 20-34) · corrosion level 2 · airframe 22,359 hrs · 16,549 cycles

CORROSION FOUND ON THE SEAT TRACK CENTER AREA BETWEEN FRAMES 20 & 24, Y+280. REPLACED THE SEAT TRACK IAW DWG 170-67120-473.

Part: SKIN — CRACKED (LT WING) · airframe 22,359 hrs · 16,549 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. DURING C4 CHECK MAINTENANCE FOUND CRACK DAMAGE EMANATING FROM FASTENER HOLE COMMON TO THE LEFT LOWER WING SKIN, ADJACENT TO OUTBOARD OF RIB 10 DRAIN HOLE. REPAIRED SKIN PER SRM 57-10-01 REPAIR 54 & EA NR 276061.

Part: ACCESS PANEL — DAMAGED (FWD CARGO DOOR) · airframe 22,359 hrs · 16,549 cycles

FORWARD CARGO NR 2 ACCESS PANEL 132BZ IS DAMAGED IN SEVERAL AREAS. ACCOMPLISHED A PERMANENT REPAIR IAW AMM 2500-09, 25-00-21, AND SRM 51-42-01.

Part: SEAT TRACK — CORRODED (FRAME 60) · airframe 22,359 hrs · 16,549 cycles

CORROSION ON THE SEAT TRACK AT FRAME 60, WATERLINE Z-490, Y-276. REPLACED THE SEAT TRACK IAW DRAWING 190-25017-415.

Part: DOUBLER — CORRODED (FRAMES 19-20) · corrosion level 2 · airframe 22,359 hrs · 16,549 cycles

FWD MAIN CABIN FLOOR DOUBLER HAS CORROSION BETWEEN FRAMES 19 & 20, Y=-704.. REMOVED AND REPLACED THE DOUBLER IAW 53-00-00-3, REPAIR 3.

Part: FLOOR PANEL — DELAMINATED (PAX CABIN)

DELAMINATED MAIN CABIN FLOOR PANEL 252AFR. FABRICATED A NEW FLOOR PANEL IAW 53-01-39, REPAIR 1, AND AMM 25-82-01.

Part: STRUCTURE — CORRODED (FRAMES 13-14) · corrosion level 2 · airframe 22,359 hrs · 16,549 cycles

CORROSION AROUND THE SEAT TRACK, THE REINFORCEMENT STRUCTURE WAS ALSO REPLACED BETWEEN FRAMES 12 & 19, Y+280 IAW 53-00-00-3, REPAIR 3, SRM 51-41-01, AND 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FRAMES 12-13) · corrosion level 2 · airframe 22,359 hrs · 16,549 cycles

FWD MAIN CABIN FLOOR SUPPORT HAS CORROSION BETWEEN FRAMES 12 & 13, Y+370. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-43-01, 51-41-01, AND DWG 190-05555-805.

Part: SEAT TRACK — CORRODED (FRAMES 12-19) · corrosion level 2 · airframe 22,359 hrs · 16,549 cycles

CORROSION FOUND ON THE SEAT TRACK BETWEEN FRAMES 12 & 19. REPLACED THE SEAT TRACK IAW 53-00-00-3, REPAIR 3, SRM 51-41-01, AND 51-41.

Part: SEAT TRACK — CORRODED (FRAMES 73-84) · corrosion level 2 · airframe 22,359 hrs · 16,549 cycles

CORROSION FOUND ON THE SEAT TRACK BETWEEN FRAMES 73 AND 84. REPLACED THE SEAT TRACK IAW 170-65600-445.

Part: INTERCOSTAL — CRACKED (FRAMES 86-87) · airframe 22,359 hrs · 16,549 cycles

CRACK DISCOVERED ON THE INTERCOSTAL. REMOVED AND REPLACED 1EA INTERCOSTAL BRACKET SRM 51-40-02, & 51-41-01.

Part: SUPPORT — CORRODED (FRAMES 87-88) · corrosion level 2 · airframe 22,359 hrs · 16,549 cycles

CORROSION FOUND ON THE GALLEY SUPPORT BETWEEN FRAMES 87 AND 88. REPLACED THE SUPPORT IAW DWG 170-65660-497.

Part: SEAT TRACK — CORRODED (FRAMES 28-34) · corrosion level 2 · airframe 22,359 hrs · 16,549 cycles

LEFT LATERAL SEAT TRACK HAS A DEEP GOUGE AND CORROSION BETWEEN FRAMES 28 - 29, 31 - 32, AND 33 - 34. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-41-01, 51-43-01, & DWG 170-67030-465.

Part: BOLT — WORN (DOOR SLIDE) · airframe 22,359 hrs · 16,549 cycles

AFT SERVICE DOOR EMERGENCY SLIDE ATTACH BOLT IS WORN. REPLACED AFT SERVICE DOOR EMERGENCY SLIDE PACK BOARD ATTACH BOLT IAW CMM 25-60-41-400-012-A01 STEP C PAR. (1).

Part: BOLT — WORN (DOOR SLIDE) · airframe 22,359 hrs · 16,549 cycles

AFT PASSENGER DOOR EMERGENCY SLIDE ATTACH BOLT IS WORN. REPLACED THE BOLT IAW CMM 25-60-41-400-012-A01 STEP C PAR.(1).

Part: BOLT — WORN (DOOR SLIDE) · airframe 22,359 hrs · 16,549 cycles

FORWARD SERVICE DOOR EMERGENCY SLIDE ATTACH BOLT IS WORN. REPLACED THE BOLT IAW CMM 25-60-41-400-012-A01 STEP C PAR. (1).

Part: BEAM — CORRODED (FRAMES 16-19) · corrosion level 2 · airframe 22,359 hrs · 16,549 cycles

FWD MAIN CABIN L1 DOOR LOWER BEAM HAS CORROSION BETWEEN FRAMES 17 & 18, Y-1305. REPLACED THE BEAM IAW DWG 170-01330-507, AND 170-00824-505.

Part: BOLT — WORN (DOOR SLIDE) · airframe 22,359 hrs · 16,549 cycles

FORWARD PASSENGER DOOR EMERGENCY SLIDE ATTACH BOLT IS WORN. REPLACED THE BOLT IAW CMM 25-60-41-400-012-A01 STEP C PAR. (1).

Part: DOUBLER — CORRODED (FRAME 16) · corrosion level 2 · airframe 22,359 hrs · 16,549 cycles

CORROSION ON THE FORWARD MAIN CABIN DOUBLER AT FRAME 16, LEFT BUTTLINE Y-406. REPLACED THE DOUBLER IAW 53-00-00-3, REPAIR 3.

Part: FLOOR SUPPORT — CORRODED (FRAME 19) · corrosion level 2 · airframe 22,359 hrs · 16,549 cycles

FWD MAIN CABIN FLOOR SUPPORT FITTING HAS CORROSION AT FRAME 19, Y=-1104. REPLACED THE FLOOR SUPPORT IAW DWG 170-29712-807 & 170-29704-005.

Part: SEAT TRACK — CORRODED (FRAMES 12-20) · corrosion level 2 · airframe 22,359 hrs · 16,549 cycles

CORROSION ON THE FORWARD MAIN CABIN SEAT TRACK BETWEEN FRAMES 12 TO 20, WATERLINE Z-490 AT BUTTLINE Y-280. REPLACED THE SEAT TRACK IAW 53-00-00-3, REPAIR 3, SRM 51-41-01, SRM 51-41-02, SRM 51-43-03, AND SRM 51-43-04.

Part: FLAP TRACK — WORN (RT WING TE FLAP) · airframe 22,359 hrs · 16,549 cycles

RIGHT WING NR 2A INBOARD FLAP TRACK WORN. REPLACED THE FLAP TRACK IAW MM 57-54-25-400-801.

Part: SHEAR TIE — CORRODED (FRAME 87) · airframe 22,359 hrs · 16,549 cycles

AFT CARGO SHEAR TIE HAS CORROSION BETWEEN STRINGERS 27R & 28R, FRAME 87. REMOVED AND REPLACED THE SHEAR TIE IAW DWG 170-65180-445.

Part: FLOOR SUPPORT — CORRODED (FRAMES 17-18) · corrosion level 2 · airframe 22,359 hrs · 16,549 cycles

CORROSION OF FORWARD MAIN CABIN FLOOR SUPPORT BETWEEN FRAMES 17 TO 18, BUTTLINE Y+340. REPLACED THE FLOOR SUPPORT IAW DRAWING 170-00822-505.

Part: SHEAR PANEL — CORRODED (FRAMES 84-85) · corrosion level 2 · airframe 22,359 hrs · 16,549 cycles

CORROSION FOUND ON SHEAR PANEL BETWEEN FRAMES 84 AND 85, Y+1194. REMOVED AND REPLACED THE SHEAR PANEL IAW DWG 190-65140-801.

Part: FLOOR SUPPORT — CORRODED (FRAMES 19-20) · corrosion level 2 · airframe 22,359 hrs · 16,549 cycles

FWD MAIN CABIN FLOOR SUPPORT HAS CORROSION BETWEEN FRAMES 19 & 20, Y=-1205. REMOVED AND REPLACED IAW SRM 51-41-02, SRM 51-23-06.

Part: FLOOR SUPPORT — CORRODED (FRAMES 17-18) · corrosion level 2 · airframe 22,359 hrs · 16,549 cycles

CORROSION ON THE FORWARD MAIN CABIN RIGHT FLOOR SUPPORT BETWEEN FRAMES 17 TO 18, WATERLINE Z-490, RIGHT BUTTLINE Y+1160. REPLACED THE FLOOR SUPPORT IAW 53-00-00-3, REPAIR 3, FIGURE 1, SHEET 14.

Part: FLOOR SUPPORT — CORRODED (FRAME 18) · corrosion level 2 · airframe 22,359 hrs · 16,549 cycles

CORROSION ON THE FORWARD MAIN CABIN FLOOR SUPPORT AT FRAME 18, BUTTLINE Y-780. REPLACED THE FLOOR SUPPORT IAW DRAWING 170-00822-505.

Part: STRAP — CORRODED (FRAMES 85-86) · corrosion level 2 · airframe 22,359 hrs · 16,549 cycles

CORROSION ON THE AFT CABIN TOP FLOOR SUPPORT STRAP BETWEEN FRAMES 85 TO 86, BUTTLINE +Y279. REPLACED THE STRAP IAW DRAWING 170-86101-001, AND 53-00-00-3, REPAIR 3.

Part: FLOOR SUPPORT — CORRODED (FRAMES 87-85) · corrosion level 2 · airframe 22,359 hrs · 16,549 cycles

AFT MAIN CABIN FLOOR SUPPORT HAS CORROSION BETWEEN FRAMES 84 & 85, Y+330 & Y+1194. REPLACED THE FLOOR SUPPORT IAW DWG 190-65140-801.

Part: STRAP — CORRODED (FRAMES 85-86) · corrosion level 2 · airframe 22,359 hrs · 16,549 cycles

CORROSION OF AFT CABIN FLOOR SUPPORT STRAP BETWEEN FRAMES 85 & 86, LEFT BUTTLINE -Y279. REPLACED THE STRAP IAW DRAWING 170-86101-001, AND 53-00-00-3, REPAIR 3.

Part: FLOOR SUPPORT — CORRODED (FRAME 89) · corrosion level 2 · airframe 22,359 hrs · 16,549 cycles

CORROSION OF AFT MAIN CABIN FLOOR SUPPORT AT FRAME 89, WATERLINE 490, RIGHT BUTTLINE Y+914. REPLACED THE FLOOR SUPPORT IAW DRAWING 170-66000-459, SRM 51-43-01, AND SRM 51-42-01.

Part: FLOORBEAM — CORRODED (FRAME 14) · corrosion level 2 · airframe 22,359 hrs · 16,549 cycles

CORROSION ON THE FORWARD MAIN CABIN FLOORBEAM AT FRAME 14, WATERLINE 490, RIGHT BUTTLINE Y+740. REPLACED FLOORBEAM IAW SRM 53-00-10, REPAIR 53, FIGURE 203.

Part: FLOOR SUPPORT — CORRODED (FRAMES 12-14) · corrosion level 2 · airframe 22,359 hrs · 16,549 cycles

CORROSION ON THE FORWARD MAIN CABIN RIGHT FLOOR SUPPORT BETWEEN FRAMES 12 TO 14, WATERLINE Z-490, AND Y+980. REPLACED THE FLOOR SUPPORT 53-00-00-3, REPAIR 3, FIGURE 1, SHEET 13.

Part: FLOOR SUPPORT — CORRODED (FRAMES 12-16) · corrosion level 2 · airframe 22,359 hrs · 16,549 cycles

CORROSION OF FORWARD MAIN CABIN LEFT FLOOR SUPPORT BETWEEN FRAMES 12 TO 16, WATERLINE Z-490, LEFT BUTTLINE Y-1106. REPLACED IAW 53-00-00-3, REPAIR 3, FIGURE 1, SHEET 11.

Part: SEAT TRACK — CORRODED (FRAMES 73-84) · corrosion level 2 · airframe 22,359 hrs · 16,549 cycles

MAIN CABIN LT INBOARD SEAT TRACK HAS CORROSION AT SEVERAL AREAS BETWEEN FRAMES 73 AND 84. REMOVED AND REPLACED THE SEAT TRACK IAW DRAWING 170-65600-443.

Part: ANGLE — CORRODED (FRAME 13) · corrosion level 2 · airframe 22,359 hrs · 16,549 cycles

CORROSION ON THE FORWARD MAIN CABIN FLOORBEAM ANGLE AT FRAME 13, BUTTLINE Y+720 AND WATERLINE Z-490. REPLACED THE ANGLE IAW DRAWING 170-21765-407.

Part: ANGLE — CORRODED (FRAME 16) · corrosion level 2 · airframe 22,359 hrs · 16,549 cycles

CORROSION OF FORWARD MAIN CABIN FLOORBEAM ANGLE AT FRAME 16, RIGHT BUTTLINE Y+715. REPLACED THE ANGLE IAW DRAWING 170-21768-409.

Part: ANGLE — CORRODED (FRAME 17) · corrosion level 2 · airframe 22,359 hrs · 16,549 cycles

CORROSION ON THE FORWARD MAIN CABIN FLOORBEAM ANGLE AT FR 17, LEFT BUTTLINE Y-780. REPLACED THE ANGLE IAW DRAWING 170-00822-505.

Part: FLOOR SUPPORT — CORRODED (FRAME 16) · corrosion level 2 · airframe 22,359 hrs · 16,549 cycles

CORROSION FOUND ON THE FLOOR SUPPORT FITTING AT FRAME 16, Y-1105. REPLACED THE FLOOR SUPPORT IAW DWG 170-00816-505, AND SRM 51-43-03.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 22,359 hrs · 16,549 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION OF FLOOR SPLICE BETWEEN FR 87 TO FR 88 AT WATERLINE Z-490 AT LEFT BUTTLINE Y+1067. REPLACED FLOOR SPLICE BETWEEN FR 87 TO FR 88 AT WATERLINE Z-490 AT LEFT BUTTLINE Y+1067 PER 53-00-00-3 REPAIR 3.

Part: WINDSHIELD — DELAMINATED (COCKPIT) · airframe 21,962 hrs · 16,219 cycles

AIRCRAFT WAS NOT GROUNDED. DELAMINATION ON FIRST OFFICER HEATED GLASS WINDSHIELD ON TOP AND INBOARD EDGE, 8 INCHES FROM OUTBOARD TOP CORNER AND 9 INCHES DOWN FROM INBOARD TOP CORNER. REPLACED WINDSHIELD PER AMM 56-11-00-000-801.

Part: ANTI-ICE VALVE — FAULTED (LT ENGINE) · airframe 21,706 hrs · 16,013 cycles

ABORTED TAKEOFF AT 5 KTS DUE TO ENGINE REFERENCE ANTI-ICE DISAGREE AND ANTI-ICE ENGINE 1 VALVE OPEN STATUS MESSAGE ILLUMINATED. REPLACED LEFT ENGINE ANTI-ICE VALVE IAW AMM 30-21-01. ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK. AIRCRAFT WAS GROUNDED.

Part: REFLECTOR — LOOSE (CABIN) · airframe 21,566 hrs · 15,904 cycles

EXIT LIGHT REFLECTIVE FLOOR STRIP IN FIRST CLASS IS LOOSE. REATTACHED REFLECTIVE FLOOR STRIP.

Part: WARNING MESSAGE — FALSE ACTIVATION (NLG STEERING) · airframe 21,487 hrs · 15,828 cycles

STEERING FAILED CAUTION MESSAGE RECEIVED AFTER GEAR EXTENSION ON FINAL APPROACH COMPLETED QRH LANDED AND TAXIED OFF OF RUNWAY ACCOMPLISHED IAW RESET PROCEDURE AND MESSAGE CLEARED. TAXIED BACK TO THE GATE. PERFORMED FIM TASK. FAULTS CLEARED.

Part: LIGHT — MISSING (CABIN) · airframe 20,256 hrs · 14,877 cycles

FIRST SEGMENT OF EMERGENCY LIGHT STRIP 1C MISSING. INSTALLED THE MISSING EMERGENCY LIGHT IAW AMM 33-50-00.

Part: ACM — SEIZED (NR 1) · airframe 19,670 hrs · 14,472 cycles

AFTER START OF NR 2 ENGINE COCKPIT BECAME HOT AND SMELLED OF SULFER. FLIGHT ATTENDANT REPORTED ODOR OF SULFER AND A HAZE IN CABIN. AIRCRAFT WAS GROUNDED. MAINTENANCE FOUND THE NR 1 AIR CYCLE MACHINE SIEZED AND REPLACED IT IAW AMM 21-51-05. A SATISFACTORY OPS CHECK WAS ACCOMPLISHED.

Part: DOOR — UNSECURE (EMERGENCY EXIT) · airframe 19,376 hrs · 14,243 cycles

IMMEDIATELY AFTER TAKEOFF MASTER WARNING FOR DOOR EMERGENCY LT OPEN. PRESSURIZATION NORMAL. FROM EXTERIOR IT DOES LOOK AJAR. HANDLE PANEL INDENTED. MAINTENANCE FOUND LEFT OVERWING EMERGENCY EXIT ESCAPE HATCH ONLY PARTIALLY LOCKED AND SECURE. REMOVED AND INSTALLED OVERWING EMERGENCY EXIT HATCH IAW AMM 52-21-00. CHECKED OK.

Part: SWITCH — OUT OF ADJUST (EMERGENCY EXIT) · airframe 19,371 hrs · 14,237 cycles

DURING CLIMB THROUGH 300000 FEET, DOOR EMERGENCY LEFT OPEN EICAS ILLUMINATED. MAINTENANCE PERFORMED TASK 52-75-00-820-801-A/500, OVERWING ESCAPE HATCH SWITCH ADJUSTED WITH NO FAULTS NOTED.

Part: SWITCH — DIRTY (EMERGENCY EXIT) · airframe 19,166 hrs · 14,073 cycles

LEFT EMEGENCY EXIT OPEN EICAS MESSAGE CAME ON IN FLIGHT AND EXTINGUISHED DURING DESCENT. CLEANED LEFT EMERGENCY EXIT DOOR SWITCH AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 52-25-00.

Part: LINE — LEAKING (FUEL SYSTEM) · airframe 19,153 hrs · 14,055 cycles

APU FUEL FEED LINE LEAKING IN AFT SERVICE BAY COMPARTMENT. REMOVED AND REPLACED APU FUEL FEED LINE FROM APU FIREWALL TO APU FUEL SHUTOFF VALVE PER AMM 28-22-08 AND ACCOMPLISHED A SATISFACTORY LEAK CHECK.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 19,141 hrs · 14,043 cycles

ACFT WAS NOT GROUNDED. AFT F/A EMERGENCY FLASHLIGHT IS INOPERATIVE. R & R AFT F/A EMERGENCY FLASHLIGHT IAW AMM 33-51-01. OPS CHECK GOOD.

Part: COFFEEMAKER — DEFECTIVE (GALLEY) · airframe 19,076 hrs · 13,963 cycles

AIRCRAFT WAS NOT GROUNDED: CABIN CREW REPORTED FAINT HOT PLASTIC ODOR IN THE FORWARD GALLEY. THE ODOR WENT AWAY WHEN GALLEY ELECTRICAL WAS TURNED OFF. MAINTENANCE DETERMINED SOURCE TO BE THE FORWARD GALLEY COFFEEMAKERS AND REPLACED THEM IAW AMM 25-37-03. A SATISFACTORY OPS CHECK WAS ACCOMPLISHED.

Part: UNKNOWN — ODOR (CABIN) · airframe 18,785 hrs · 13,667 cycles

RETURNED & ACFT WAS GNDED. FLIGHT CREW REPORTED A BURNING & ELEC SMELL THROUGHOUT ACFT. DECLARED AN EMER & RETURNED WHERE THE ACFT LANDED SAFELY. MEDICAL ATTENTION WAS SOUGHT BY FLIGHT ATTENDANTS. ACCOMPLISHED TASK CARD 43L00021001, TROUBLESHOOT CABIN AIR QUALITY, NO DISCREPANCIES WERE NOTED & WERE UNABLE TO DUPLICATE ODOR. ACFT WAS RETURNED TO SERVICE.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,824 hrs · 12,768 cycles

C3 CHECK, CORROSION ON FWD CARGO COMPARTMENT ANTENNA DOUBLER, BETWEEN FRAME 19 & 20, STRINGER 26R & 23R. REPLACED DOUBLER IAW SRM 53-10-01 & 51-41-02.

Part: SIGN — CRACKED (CABIN) · airframe 17,824 hrs · 12,768 cycles

C3 CHECK, R2 DOOR LOWER EMER EXIT SIGN IS CRACKED. REPLACED EMER EXIT SIGN. ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 33-50-15 & 33-50-00.

Part: SIGN — CRACKED (CABIN) · airframe 17,824 hrs · 12,768 cycles

C3 CHECK, LT OVERWING DOOR SURROUND, THE LOWER EMER EXIT SIGN IS CRACKED. REPLACED EMER EXIT SIGN. ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 33-50-00-710-81A 500 & 33-50-15.

Part: BEARING — WORN (RT AILERON) · airframe 17,824 hrs · 12,768 cycles

C3 CHECK, RT WING AILERON NR 3 HINGE FITTING BEARING WORN. REPLACED HINGE FITTING IAW AMM 57-61-01.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 17,824 hrs · 12,768 cycles

C3 CHECK, WING STUB MAIN BOX UPPER STRUCTURE, FLOOR SUPPORT HAS CRACK AT SPAR 1 & LBL 8.75. REPAIRED IAW EA 255177A.

Part: RAIL — WORN (TE FLAP) · airframe 17,824 hrs · 12,768 cycles

C3 CHECK, RT WING INBD FLAP TRACK NR 1 SUPPORT GUIDE RAIL WORN. REPLACED SUPPORT GUIDE RAIL IAW AMM 57-54-21.

Part: BEARING — WORN (RT AILERON) · airframe 17,824 hrs · 12,768 cycles

C3 CHECK, RT WING AILERON NR 4 HINGE FITTING BEARING WORN. REPLACED HINGE FITTING IAW AMM 57-61-01.

Part: BEARING — RUSTED (LT AILERON) · airframe 17,824 hrs · 12,768 cycles

C3 CHECK, LT WING AILERON NR 2 HINGE FITTING HAS RUSTED BEARING. REPLACED HINGE FITTING IAW AMM 57-61-01.

Part: LENS — CRACKED (EXIT SIGN) · airframe 17,824 hrs · 12,768 cycles

C3 CHECK, THE R1 UPPER EMER EXIT SIGN LENS IS CRACKED. REPLACED EMER EXIT SIGN LENS IAW AMM 33-50-17.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 17,824 hrs · 12,768 cycles

C3 CHECK, WING STUB MAIN BOX UPPER STRUCTURE, FLOOR SUPPORT HAS CRACK AT SPAR 1 & RBL 8.75. REPAIRED IAW EA 255178.

Part: LENS — CRACKED (EXIT SIGN) · airframe 17,824 hrs · 12,768 cycles

C3 CHECK, ON THE R2 DOOR, THE UPPER EMER EXIT SIGN LENS IS CRACKED. REPLACED LENS IAW AMM 33-50-17.

Part: GLOWSTRIP — CRACKED (CABIN) · airframe 17,824 hrs · 12,768 cycles

MAIN CABIN RT PHOTO LUMINESCENT STRIPS ARE CRACKED & BROKEN, MORE THAN 10%. REPLACED MAIN CABIN RT PHOTO LUMINESCENT STRIPS IAW AMM 33-50-21 PAGE 5 OF 8.

Part: RAIL — WORN (TE FLAP) · airframe 17,824 hrs · 12,768 cycles

C3 CHECK, RT WING OTBD FLAP, OTBD GUIDE RAIL WORN. REPLACED GUIDE RAIL IAW AMM 57-50-07.

Part: GLOWSTRIP — CRACKED (CABIN) · airframe 17,824 hrs · 12,768 cycles

MAIN CABIN LT PHOTO LUMINESCENT STRIPS ARE CRACKED & BROKEN, MORE THAN 10%. REPLACED MAIN CABIN LT PHOTO LUMINESCENT STRIPS IAW AMM 33-50-21 PAGE 5 OF 8.

Part: FITTING — CORRODED (FUSELAGE) · airframe 17,824 hrs · 12,768 cycles

C3 CHECK, CORROSION ON SHEAR CLIP AT FRAME 88, BETWEEN STRINGER 27R & 28R. REPLACED SHEAR CLIP IAW DWG 170-65900-463, SRM 51-41-02, 41-43-03 & EA 255299.

Part: SEAL REST — CORRODED (FUSELAGE) · airframe 17,824 hrs · 12,768 cycles

C3 CHECK, CORROSION ON AFT CARGO COMPARTMENT DOOR CUT OUT, LOWER AFT CORNER SEAL REST, AT FRAME 80 & STRINGER 28R. REPLACED SEAL REST IAW AARD 53-00-00-3 REPAIR 3.

Part: SUPPORT BRACKET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,824 hrs · 12,768 cycles

C3 CHECK, CORROSION ON FWD CARGO FLOOR PANEL SUPPORT BRACKET AT FRAME 24, BETWEEN STRINGER 26R & 27R. REPLACED SUPPORT BRACKET IAW SRM 51-41-01.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,824 hrs · 12,768 cycles

C3 CHECK, CORROSION ON FWD CARGO DOOR SILL EXTERNAL SKIN DOUBLER, BETWEEN FRAME 26 & 27 AT STRINGER 26L - 27L. REPLACED DOUBLER IAW DWG 170-67080-461 & SRM 51-41-02.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 17,824 hrs · 12,768 cycles

C3 CHECK, CORROSION ON LT SHEAR PANEL SPLICE, BETWEEN FRAME 87 & 88, AT LBL 42. REPLACED SPLICE IAW SRM 51-40-04 & DWG 170-66009-445.

Part: BEARING — RUSTED (RT AILERON) · airframe 17,824 hrs · 12,768 cycles

C3 CHECK, RT WING AILERON NR 1 HINGE FITTING HAS RUSTED BEARING. REPLACED HINGE FITTING IAW AMM 57-61-01.

Part: PANEL — CORRODED (FUSELAGE) · airframe 17,824 hrs · 12,768 cycles

C3 CHECK, CORROSION ON SHEAR PANEL, BETWEEN FRAME 87 & 88, BETWEEN RBL 10 & 42. REPLACED SHEAR PANEL IAW AARD 53-00-00-3 & DWG 170-66000-445 REV A.

Part: BEARING — RUSTED (NR 2 AILERON) · airframe 17,824 hrs · 12,768 cycles

C3 CHECK, RT WING NR 2 AILERON HINGE FITTING BEARING RUSTED. REPLACED HINGE FITTING IAW AMM 57-61-01.

Part: PANEL — CORRODED (FUSELAGE) · airframe 17,824 hrs · 12,768 cycles

C3 CHECK, CORROSION ON LT SHEAR PANEL, BETWEEN FRAME 87 & 88 AT LBL 11. REPLACED SHEAR PANEL IAW AARD 53-00-00 REPAIR 3.

Part: GUSSET — CHAFED (SERVICE DOOR) · airframe 17,824 hrs · 12,768 cycles

C3 CHECK, AFT SERVICE DOOR, FWD UPPER CORNER GUSSET CHAFED. REPLACED GUSSET IAW DWG 170-69500-417 & SRM 51-43-05.

Part: PAN — CORRODED (FUSELAGE) · airframe 17,824 hrs · 12,768 cycles

C3 CHECK, CORROSION ON WASTE BOX WATER PAN ASSEMBLY, BETWEEN FRAME 88 & 89, STRINGER 25R - 28R. REPLACED WASTE BOX ASSEMBLY IAW EO 5313P246.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,824 hrs · 12,768 cycles

C3 CHECK, CORROSION ON FWD CARGO DOUBLER, BAG DOOR BETWEEN FRAME 24 & 25 AT STRINGER 25R. REPLACED IAW DWG 170-67080-461.

Part: SUPPORT BRACKET — CRACKED (VERTICAL STAB) · airframe 17,824 hrs · 12,768 cycles

C3 CHECK, VERTICAL STABILIZER TE SUPPORT BRACKET ABOVE RUDDER HINGE, ARM 3 IS CRACKED. REPLACED SUPPORT BRACKET IAW DWG 190-63830-401 & SRM 51-41-02.

Part: SEAL REST — CORRODED (FUSELAGE) · airframe 17,824 hrs · 12,768 cycles

C3 CHECK, CORROSION ON AFT CARGO DOOR CUT OUT LOWER FWD CORNER SEAL REST. REPLACED SEAL REST IAW AMM 20-10-01.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 17,824 hrs · 12,768 cycles

C3 CHECK, CORROSION ON GUSSET AT FRAME 90 & LBL 11. REPLACED GUSSET IAW SRM 51-30-10 & DWG 170-60385-419.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 17,824 hrs · 12,768 cycles

C3 CHECK, CORROSION ON GUSSET AT FRAME 90 & STRINGER 21R. REPLACED GUSSET IAW DWG 170-60385-419 & SRM 51-41-02.

Part: PANEL — CORRODED (FUSELAGE) · airframe 17,824 hrs · 12,768 cycles

C3 CHECK, CORROSION ON CTR SHEAR PANEL, BETWEEN FRAME 87 & 88, BL 0. REPLACED SHEAR PANEL IAW AARD 53-00-00-3 REPAIR 3.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 17,824 hrs · 12,768 cycles

C3 CHECK, COCKPIT FLOOR STRUCTURE ANGLE BRACKET IS CRACKED AT FRAME 12 & LBL 37. REPLACED ANGLE BRACKET IAW SRM 51-41-01.

Part: SEAL REST — CRACKED (FUSELAGE) · airframe 17,824 hrs · 12,768 cycles

C3 CHECK, FWD CARGO DOOR CUT OUT LOWER FWD CORNER, SEAL REST CRACKED. REPLACED SEAL REST IAW AARD 53-00-00-3 REPAIR 3.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 17,824 hrs · 12,768 cycles

C3 CHECK, CORROSION ON SPLICE AT FRAME 90 & BL 0. REPLACED SPLICE IAW SRM 51-43-03 & DWG 170-65660-477.

Part: BEARING — RUSTED (LT AILERON) · airframe 17,824 hrs · 12,768 cycles

C3 CHECK, LT WING AILERON NR 1 HINGE FITTING BEARING RUSTED. REPLACED FITTING IAW AMM 57-61-01.

Part: PANEL — CORRODED (FUSELAGE) · airframe 17,824 hrs · 12,768 cycles

C3 CHECK, CORROSION ON LT SUPPORT PANEL AT FRAME 90 & LBL 34. REPLACED PANEL IAW DWG 170-66000-445 & SRM 51-43-01.

Part: VALVE — STUCK (LAVATORY) · airframe 16,822 hrs · 11,905 cycles

EN-ROUTE, AFTER TAKEOFF ABOVE 10,000FT, FLIGHT ATTENDANT ADVISED THAT A HEAVY AMMONIA LIKE ODOR IN AFT LAVATORY. AMBER LAVATORY FAULT LIGHT DISPLAYED ON FLIGHT ATTENDANT PANEL AFT. THE FLIGHT CONTINUED & LANDED WITHOUT FURTHER INCIDENT. REPLACED THE AFT LAVATORY FLUSH VALVE ASSEMBLY.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 15,617 hrs · 10,870 cycles

EN-ROUTE CAPTAIN`S WINDSHIELD CRACKED. THE FLIGHT DECLARED AN EMER & DIVERTED. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. R & R CAPTAIN`S WINDSHIELD.

Part: SLIDE — UNSERVICEABLE (R2 DOOR) · airframe 15,552 hrs · 10,818 cycles

LACING ON R2 DOOR SLIDE IS LOOSE. REPLACED R2 SLIDE ASSEMBLY.

Part: SHEAR PIN — LOOSE (LT PYLON) · airframe 14,963 hrs · 10,267 cycles

RON, DURING ACCOMPLISHMENT OF EO 5414P124 THE LT PYLON OTBD LOWER LINK FITTING ASSEMBLY WAS FOUND LOOSE. RE-TORQUED & SAFETIED THE LOWER LINK FITTING ASSEMBLY IAW EO 5414P124.

Part: SHEAR PIN — LOOSE (RT PYLON) · airframe 14,963 hrs · 10,267 cycles

RON, DURING ACCOMPLISHMENT OF EO 5414P124 THE RT PYLON INBD LOWER LINK FITTING ASSEMBLY WAS FOUND LOOSE. RE-TORQUED & SAFETIED THE LOWER LINK FITTING ASSEMBLY IAW EO 5414P124.

Part: SHEAR PIN — LOOSE (LT PYLON) · airframe 14,963 hrs · 10,267 cycles

THE LT PYLON LOWER LINK OTBD FITTING SHEAR PIN LOCKNUTS LOOSE ON BOTH LT & RT ENGS IN BOTH INBD & OTBD POSITIONS. RE-TORQUED THE PYLON LOWER LINK OTBD FITTING SHEAR PIN LOCKNUTS FOR BOTH LT & RT ENGS IN BOTH INBD & OTBD POSITIONS & APPLIED THE APPROPRIATE SAFETIES.

Part: SHEAR PIN — LOOSE (RT PYLON) · airframe 14,963 hrs · 10,267 cycles

RON, DURING ACCOMPLISHMENT OF EO 5414P124 THE RT PYLON OTBD LOWER LINK FITTING ASSEMBLY WAS FOUND LOOSE. RE-TORQUED & SAFETIED THE LOWER LINK FITTING ASSEMBLY IAW EO 5414P124.

Part: BOTTLE — LOW PRESSURE (SERVICE DOOR) · airframe 13,915 hrs · 9,476 cycles

BOTH FWD SERVICE DOORS, DOOR ASSIST BOTTLES REQUIRE SERVICING. SERVICED DOOR ASSIST BOTTLE ON L1 DOOR.

Part: BOTTLE — LOW PRESSURE (R1 DOOR) · airframe 13,915 hrs · 9,476 cycles

BOTH FWD SERVICE DOORS, DOOR ASSIST BOTTLES REQ SERVICING. SERVICED DOOR ASSIST BOTTLE ON R1 DOOR.

Part: SUPPORT BRACKET — FAILED (CABIN) · airframe 13,112 hrs · 8,918 cycles

AFT CABIN & GALLEY CEILING IS FALLING . IT IS IMPENDING ON THE USE OF THE AFT LAV DOOR AND THE 2L DOOR HAMPERING EMERGENCY EGRESS. MX REPLACED AFT GALLEY CENTER CEILING PANEL SUPPORTING BRACKET ISOLATOR AND ALL FOUR ADJUSTABLE GRIP LOCKPINS. REINSTALLED CEILING PANEL AT AFT GALLEY CENTER. PERFORMED CHECK OF THE AFT LAV DOOR AND EXIT DOOR 2L . NO DEFECT NOTED.

Part: MODULE — FAULTY (EXTERNAL POWER)

CLT - A BURNT SMELL WAS REPORTED IN THE CABIN. MAINTENANCE FOUND THE EXTERNAL POWER MODULE BURNT. THE GROUND POWER MODULE WAS REMOVED AND REPLACED PER FIM 24-42-00-810-817A. OPERATIONAL CHECK IS SATISFACTORY.

Part: STRUT — UNDERSERVICED (NLG)

FLIGHT 9195, PIT-CLT - FOLLOWING TAKE-OFF THE CREW RECEIVED A LANDING GEAR "WEIGHT ON WHEEL" EICAS MESSAGE AFTER THE LANDING GEAR HANDLE WOULD NOT RAISE TO THE UP POSITION. THE FLIGHT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE SERVICED THE NOSE LANDING GEAR STRUT.