N105HQ

Part: RIB — DAMAGED (ZONE 600) · airframe 41,149 hrs · 31,980 cycles

DURING HEAVY CHECK FOUND RH WING AFT FACE SPAR 2 RIB 10 ELONGATED HOLE. REMOVED AND REPLACED RIB 10 RH WING AFT FACE SPAR 2. REF EMB SRM 51-40-08. ACFT REMAINS IN HEAVY CHECK UNTIL COMPLETION

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 42,149 hrs · 31,980 cycles

WHILE IN HEAVY CHECK - CORRODED SHEAR CLIP AT FR 88, STGR 26R-27R. REMOVED AND REPLACED SHEAR CLIP AT FR 88 STGR 26R-27R. REF EMB SRM 51-40-08.

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 42,149 hrs · 31,980 cycles

WHILE IN HEAVY CHECK - CORRODED SHEAR CLIP AT FR 89, STGR 27R. REMOVED AND REPLACED SHEAR CLIP AT FR 89 STGR 27R. REF EMB SRM 51-40-08.

Part: SUPPORT BRACKET — CORRODED (ZONE 100) · corrosion level 2 · airframe 42,149 hrs · 31,980 cycles

WHILE IN HEAVY CHECK - ADDITIONAL CORROSION FOUND ON RH SIDE OF BAGGAGE SUPPORT LOCATED BETWEEN 29L-29R AT FR 84. REMOVED AND REPLACED RH SIDE BAGGAGE SUPPORT AT FR 84 STGR 29L-29R. REF EMB SRM 51-40-08.

Part: SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 42,149 hrs · 31,980 cycles

WHILE IN HEAVY CHECK - ADDITIONAL CORROSION FOUND LH SIDE OF BAGGAGE SUPPORT LOCATED BETWEEN 29L 29R FR 84. REMOVED AND REPLACED LH SIDE BAGGAGE SUPPORT LOCATED BETWEEN STGR 29L-29R AT FR 84. REF EMB SRM 51-40-08. RESTORED SURFACE PROTECTION. REF SRM 51-23-06 AND CIC PER CPM 51--25-00

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 42,149 hrs · 31,980 cycles

WHILE IN HEAVY CHECK - ADDITIONAL CORROSION FOUND ON SHEAR CLIP LOCATED BETWEEN STGR 29R 28R FR 84. REMOVED AND REPLACED SHEAR CLIP BETWEEN STGR 29R-28R AT FR 84. REF EMB SRM 51--40-08. RESTORED SURFACE PROTECTION. REF SRM 51--23-06 AND CIC PER CPM 51-25-00

Part: SHEAR ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,149 hrs · 31,980 cycles

DURING HEAVY CHECK FOUND CORRODED SHEAR CLIP AT FR 82 STGR 27R-29R. REMOVED AND REPLACED SHEAR CLIP AT FR 82 STGR 27R-29R. REF SRM 51-40-02, 51-40-08 AND 51-23-04. ACFT REMAINS IN HEAVY CHECK UNTIL COMPLETION

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,149 hrs · 31,980 cycles

DURING HEAVY CHECK FOUND CORRODED SHEAR CLIP AT FR 85 AND FR 88 STGR 27R - 28R. REMOVED AND REPLACED SHEAR CLIP AT FR 85 AND FR 88 STGR 27R-28R. REF EMB SRM 51-40-08. ACFT REMAINS IN HEAVY UNTIL COMPLETION.

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,149 hrs · 31,980 cycles

DURING HEAVY CHECK FOUND CORRODED SHEAR CLIP AT FR 83-FR84 STGR 27R-29R. REMOVED AND REPLACED SHEAR CLIP AT FR 83-FR 84 STGR 27R-29R. REF EMB SRM 51-40-02 AND 51-40-08. ACFT REMAINS IN HEAVY CHECK UNTIL COMPLETION.

Part: SHEAR ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,149 hrs · 31,980 cycles

DURING HEAVY CHECK FOUND CORRODED SHEAR CLIP AT FR 75 STGR 28R-29L. REMOVED AND REPLACED SHEAR CLIP AT FR 75 STGR 28R-29L. REF SRM 51-40-02, 51-40-08 AND 51-23-04. ACFT REMAINS IN HEAVY CHECK UNTIL COMPLETION

Part: SHEAR ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,149 hrs · 31,980 cycles

DURING HEAVY CHECK FOUND CORRODED SHEAR CLIP AT FR 86 STGR 29L-29R. REMOVED AND REPLACED SHEAR CLIP AT FR 86 STGR 29L-29R. REF EMB SRM 51-40-02 AND 51-40-08. ACFT REMAINS IN HEAVY CHECK UNTIL COMPLETION.

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 42,149 hrs · 23,761 cycles

WHILE IN HEAVY CHECK - FUSELAGE SKIN INTERNAL SHEAR CLIP HAS DAMAGE/CORROSION AT FRAME 86; STR 27R-STR 28R REMOVED AND REPLACED FUSELAGE INTERNAL SHEAR CLIP AT FR 86 STGR 27R-28R. REF EMB SRM 51-40-08.

Part: DOUBLER — CORRODED (ZONE 100) · corrosion level 2 · airframe 42,149 hrs · 23,761 cycles

WHILE IN HEAVY CHECK - FUSELAGE SKIN WASTE BOX DOUBLER HAS CORROSION FRAME 88-89 STRINGER 25R-28R, DISCOVERED DURING POST REMOVAL INSPECTION OF WASTE SERVICING PANEL REMOVAL. REMOVED AND REPLACED WASTE BOX INTERNAL DOUBLER BETWEEN FR 88-89 STGR 25R-28R. REF EMB SRM 51-40-08.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 42,149 hrs · 23,761 cycles

WHILE IN HEAVY CHECK - STGR.27R BETWEEN FR.84 TO FR.86 HAS SUSPECTED CORROSION. PERFORMED PERMANENT STRINGER SPLICE REPAIR ON STGR 27R BETWEEN FR 84-86 TO FR 88. REF EMB ETD2024-170-022817.

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 42,149 hrs · 31,980 cycles

WHILE IN HEAVY CHECK - BETWEEN STGR.29L TO STGR.28L AT FR.84 SHEAR CLIP HAS SUSPECTED CORROSION. REMOVED AND REPLACED SHEAR CLIP BETWEEN STGR.29L TO STGR.28L AT FR.84. REF EMB SRM 51-40-08. RESTORED SURFACE PROTECTION. REF SRM 51-23-06 AND CIC PER CPM 51-25-00

Part: SKIN — CRACKED (ZONE 600) · airframe 36,986 hrs · 28,276 cycles

SUSPECTED CRACK ON RH WING LOWER SKIN OUTBD OF RIB 10. COMPLIED WITH ETD2022-170-014848 WITH REAMING, FABRICATION AND INSTALLATION OF TEMPORARY REPAIR BUSHING ON RH LOWER WING SKIN OUTBD OF RIB 10.

Part: SHEAR ANGLE — CORRODED (ZONE 100) · airframe 36,986 hrs · 28,276 cycles

SHEAR CLIP FR87, STR27R/28R. REMOVED AND REPLACED SHEAR CLIP AT FR 87, STGR 27-28R. REF SRM 51-40-08.

Part: SHEAR ANGLE — CORRODED (ZONE 100) · airframe 36,986 hrs · 28,276 cycles

SHEAR CLIP FR76, STR 25L HAS CORROSION. REMOVED AND REPLACED FR76 STRINGER 25L SHEAR CLIP. REF EMB SRM 51-40-08.

Part: BRAKE — FALSE INDICATION (ZONE 700) · airframe 36,915 hrs · 28,222 cycles

PARKING BRAKE ENGAGED MESSAGE WHILE IN FLIGHT. DECLARED EMERGENCY, LANDED WITH OUT INCIDENT. REMOVED AND REPLACED EMERGENCY PARKING BRAKE PRESSURE SWITCH. OPS CHECK GOOD AT THIS TIME.

Part: SKIN — DENTED · airframe 36,777 hrs · 28,119 cycles

DENT FROM BIRD STRIKE ON FWD FUSELAGE NEAR F/O WINDSHIELD FROM FRA 2 TO FRA 4 AND STR 2R TO 4R. REPAIRES DENT IAW EMB ETD2022-170-008549. REF VP-010016-2022 N/R #1 AND LP R958122.

Part: STRINGER — CORRODED (FRAMES 76-77) · corrosion level 2 · airframe 33,094 hrs · 25,408 cycles

CORROSION MULTIPLE AREAS ON STR 29L BETWEEN FRAMES 76-77. REMOVED CORROSION ON STRINGER 29L BETWEEN FRAMES 76 TO 77 BY BLENDING. MAX MATERIAL LOSS OF .034" FOUND TO BE OUT OF LIMITS. INSTALLED REPAIR STRINGER SPLICE AND DOUBLERS. REF ETD2020-170-011700 REV A AND SRM 53-20-03/R08 SEE EAMS W/O H7207 SN 716 FOR WORK DETAILS.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,094 hrs · 25,408 cycles

MAJOR REPAIR: CORROSION ON SHEAR CLIP AT FR 85, STR 28R-27R. R & R SHEAR CLIP PN 170-66065-001 IAW EMB SRM 51-40-02. RESTORE FINISH IAW SRM 51-23-04, 51-23-05 & 51-23-06. AIRCRAFT REMAINS IN HEAVY CHECK BNA.

Part: STRINGER — CORRODED (FRAMES 76-77) · corrosion level 2 · airframe 33,094 hrs · 25,408 cycles

CORROSION AT MULTIPLE AREAS ON STRINGER 29R, BETWEEN FRAMES 76-77. REMOVED CORROSION. MEASURED BLEND OUT L=1.0"X W=0.050". 0.048" MATERIAL LOSS, FOUND TO BE OUT OF LIMITS. INSTALLED A SPLICE REPAIR IAW ETD 2020-170-011719, REV A, AND SRM 53-23-03/R08.

Part: SPLICE PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,094 hrs · 25,408 cycles

CORROSION ON SPLICE PLATE ON PANEL 195HL. REMOVED AND REPLACED SPLICE PLATE PN 170-08513-405 & 170-08513-406 REF SRM 20-10-07. SEE W/O H7207 SN 559 FOR WORK DETAILS. AIRCRAFT REMAINS IN HEAVY CHECK BNA.

Part: SPLICE PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,094 hrs · 25,408 cycles

CORROSION ON SPLICE PLATE ON PANEL 195GR. REMOVED AND REPLACED SPLICE PLATE PN 170-08513-405 REF SRM 20-10-07. SEE W/O H7207 SN 554 FOR WORK DETAILS. AIRCRAFT REMAINS IN HEAVY CHECK BNA.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,094 hrs · 25,408 cycles

CORROSION AS MARKED ON CENTER THRESHOLD TRIM SUPPORT ON AFT PASSENGER DOOR. REMOVED AND REPLACED CENTER THRESHOLD REF SRM 51-40-08, APPLIED SURFACE PROTECTION REF SRM 51-23-06. SEE W/O H7207 SN 462 FOR WORK DETAILS. AIRCRAFT REMAINS IN HEAVY CHECK BNA.

Part: THRESHOLD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,094 hrs · 25,408 cycles

CORROSION AS MARKED ON CENTER THRESHOLD TRIM SUPPORT ON AFT PASSENGER DOOR. REMOVED AND REPLACED CENTER THRESHOLD REF SRM 51-40-08, APPLIED SURFACE PROTECTION REF SRM 51-23-06. SEE W/O H7207 SN 462 FOR WORK DETAILS. AIRCRAFT REMAINS IN HEAVY CHECK BNA.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,094 hrs · 25,408 cycles

CORROSION AFT WET AREA, RT SEAT TRACK, FR84 AS MARKED. BLENDED EFFECTED AREA AND FOUND TO BE IN A NO DAMAGE ALLOWED AREA. PERFORMED PERMANENT REPAIR OF AFT WET AREA RT SEAT TRACK REPAIR AND RESTORE FINISH REF ETD2020-170-011104. SEE W/O H7207 SN 337 FOR WORK DETAILS. AIRCRAFT REMAINS IN HEAVY CHECK BNA.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,094 hrs · 25,408 cycles

CORROSION AFT WET AREA LT FLOOR SUPPORT FR88-90 AS MARKED. REMOVED AND REPLACED LT AFT FLOOR SUPPORT PN 170-86139-005 REF SRM 51-40-08. RESTORE FINISH REF SRM 51-23-04, 51-23-05 & 51-23-06. SEE W/O H7207 SN 334 FOR WORK DETAILS. AIRCRAFT REMAINS IN HEAVY CHECK BNA.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,094 hrs · 25,408 cycles

CORROSION AFT WET AREA, RT MONUMENT SUPPORT FR84. REMOVED AND REPLACED WITH NEW MONUMENT SUPPORT, APPLIED SURFACE PROTECTION REF SRM 51-40-08, 51-23-06 AND CPM 51-25-00. SEE W/O H7207 SN 351 FOR WORK DETAILS. AIRCRAFT REMAINS IN HEAVY CHECK BNA.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,094 hrs · 25,408 cycles

CORROSION-AFT WET AREA CENTER DOUBLER FR90 AS MARKED. REMOVED AND REPLACED CENTER FLOOR SUPPORT PN 170-86119-005 REF SRM 51-40-08. RESTORE FINISH REF SRM 51-23-04, 51-23-05 & 51-23-06. SEE W/O H7207 SN 332 FOR WORK DETAILS. AIRCRAFT REMAINS IN HEAVY CHECK BNA.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,094 hrs · 25,408 cycles

CORROSION-AFT WET AREA CENTER SHEAR PANEL FR87-88 AS MARKED. REMOVED AND REPLACED CENTER SHEAR PLATE PN 170-65928-001 REF SRM 51-42-01. RESTORE FINISH REF SRM 51-23-04, 51-23-05 & 51-23-06. SEE W/O H7207 SN 329 FOR DETAILS. AIRCRAFT REMAINS IN HEAVY CHECK BNA.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,094 hrs · 25,408 cycles

CORRODED 3 EA LOWER ANGLES AND 3 EA CRACK RECEPTACLE AND PANEL 1441FR. REMOVED AND REPLACED 3 EA LOWER ANGLES INCLUDING RECEPTACLES ON PANEL 1441FR, 170-10063-004, 170-10064-002 AND 170-10065-002 REF SRM 51-40-08, AMM 20-10-01. RESTORED SURFACE PROTECTION REF SRM 51-23-05, 51-23-06. AIRCRAFT REMAINS IN HEAVY CHECK BNA.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,094 hrs · 25,408 cycles

CORRODED 3 EA LOWER ANGLES AND 7 EA CRACK RECEPTACLE AND PANEL 1431DL. REMOVED CORROSION ON 3 EA LOWER ANGLES ON PANEL 1431DL BY BLENDING. MAX MATERIAL LOSS ON EACH ANGLE MEASURES .007", .010", .010". ALL ANGLES FOUND TO BE OUT OF LIMITS IAW SMB SRM 51-75-16. R & R 3 EA LOWER ANGLES, PANEL 1431DL IAW SRM 51-40-08, 51-40-02 PN 170-10063-003, 170-10064-001 AND 170-10065-001. AIRCRAFT REMAINS IN HEAVY CHECK BNA.

Part: SERVICE DOOR — CORRODED (LAV SERVICE) · corrosion level 2 · airframe 33,094 hrs · 25,408 cycles

WASTE SERVICE DOOR IS CORRODED AS MARKED. CORROSION FOUND OUT OF LIMITS REF SRM 51-75-16, REMOVED AND REPLACED WASTE SERVICE DOOR WITH NEW, APPLIED SURFACE PROTECTION REF SRM 51-23-04,51-23-05 AND 51-23-06 AMM 20-10-01. AIRCRAFT REMAINS IN HEAVY CHECK BNA.

Part: JUMPER — ABNORMAL (CABIN PRESSURE) · airframe 29,462 hrs · 22,913 cycles

RECEIVED PRESN MAN FAIL AND PRESN AUTO FAIL MESSAGES SIMULTANEOUSLY WITH SEVERAL CABIN PRESSURE BUMPS. ALSO RECEIVED CABIN DIFF PRESS FAIL. DECLARED EMERGENCY, DIVERTED TO JFK, LANDED WITHOUT INCIDENT. LOWERED RESISTANCE TO BONDING JUMPER CONTACT, OPS CHECK GOOD IAW AMM 21-31-00-710-801-A/500.

Part: SLIDE — LOW PRESSURE (L2 DOOR) · airframe 29,429 hrs · 22,891 cycles

ESCAPE SLIDE INDICATOR GAUGE IN RED FOR L2 DOOR. R&R L2 DOOR EMERGENCY EQUIPMENT SLIDE ASSY IAW MM 25-65-01, NO FURTHER DEFECTS NOTED.

Part: CABLE — BROKEN (EVAC SLIDE) · airframe 27,897 hrs · 21,756 cycles

L2 DOOR EVACUATION SLIDE PARTIALLY DEPLOYED WITH DOOR DISARM. FOUND FLEX CABLE BROKEN. R&R L2 DOOR FLEX CABLE IAW AMM 52-12-40. OPS CHECK L2 DOOR FLEX MECHANISM IAW AMM 52-10-40. R&R L2 DOOR EMERGENCY EVACUATION SLIDE IAW AMM 25-65-01. NO DEFECTS NOTED.

Part: INDICATOR — INACCURATE (R2 DOOR) · airframe 27,718 hrs · 21,614 cycles

R2 DOOR GIRT BAR INDICATOR IS RED WHEN DOOR IS DISARMED. R & R R2 DOOR FLEXBALL KIT IAW AMM 52-12-40.

Part: PANEL SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,607 hrs · 21,517 cycles

CARGO FLOOR PANEL SUPPORT ASSEMBLY CORRODED AT FR76 BETWEEN STRINGERS 29L-29R.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,607 hrs · 21,517 cycles

REMOVED AND REPLACED SHEAR CLIP AT FR 88 AND STR 27R AND 28R IAW SRM 51-40-08.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,607 hrs · 21,517 cycles

REMOVED AND REPLACED ANGLE AT FR 87 TO FR 88 AND STR 25R TO 26R IAW SRM 51-40-08.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,607 hrs · 21,517 cycles

REMOVED AND REPLACED SEAT TRACK RT INBD FR22/43 REF SRM 51-43-03, 51-43-04 AND 51-41-01.

Part: PANEL SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,607 hrs · 21,517 cycles

REMOVED AND REPLACED PANEL SUPPORT LOCATED AT AFT WET AREA FRM 86 IAW SRM 51-41-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,607 hrs · 21,517 cycles

REMOVED AND REPLACED FLOOR SUPPORT AT RT FR 14 IAW SRM 51-41-01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,607 hrs · 21,517 cycles

INSTALLED REPAIR DOUBLER AND FILLER LT SEAT TRACK FR 12 TO 20 IAW SRM 53-10-10 AND ETD 2018-170-020241.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,607 hrs · 21,517 cycles

REMOVED AND REPLACED ANGLE AT FR 87 TO FR 88 AND STR 25R TO 26R IAW SRM 51-40-08.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,607 hrs · 21,517 cycles

REMOVED AND REPLACED FLOOR SUPPORT FR 16 TO 17 REF SRM 51-40-08.

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,607 hrs · 21,517 cycles

REPLACED FRAME 90 FLOORBEAM RIGHT GUSSET REF SRM 51-23-05.

Part: PANEL SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,607 hrs · 21,517 cycles

REMOVED AND REPLACED AFT WET AREA PANEL SUPPORT AT FR 85 LT IAW SRM 51-41-01.

Part: PANEL SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,607 hrs · 21,517 cycles

REMOVED AND REPLACED FLOOR PANEL SUPPORTS AT FR76, STR 29L-29R REF SRM 51-40-08. MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,607 hrs · 21,517 cycles

REMOVED AND INSTALLED NEW RT FWD SEAT TRACK FR 12 - 20 IAW SRM 51-40-08.

Part: PANEL SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,607 hrs · 21,517 cycles

REMOVED AND REPLACED PANEL SUPPORT BRACKETS 2 EA AFT WET ARE FR 87 LT AND RT REF SRM 51-41-01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,607 hrs · 21,517 cycles

REMOVED AND INSTALLED NEW RT SEAT TRACK FR 74-84. REF SRM 51-40-08 PART 170-86082-003.

Part: SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,607 hrs · 21,517 cycles

REMOVED AND REPLACED AFT WET AREA AT FM 90 CENTER INTERCOSTAL SPLICE IAW SRM 51-43-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,607 hrs · 21,517 cycles

REMOVED AND REPLACED FLOOR SUPPORT RT FR 16 IAW SRM 51-41-01.

Part: STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,607 hrs · 21,517 cycles

REMOVED AND REPLACED FWD STRAP ON AFT SERVICE DOOR LOWER THRESHOLD BEAM IAW SRM 51-40-08.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,607 hrs · 21,517 cycles

REMOVED AND REPLACED FLOOR SUPPORT AT RT FR 17 IAW SRM 51-41-01.

Part: SERVICE DOOR — CORRODED (WASTE SERVICE) · corrosion level 2 · airframe 27,607 hrs · 21,517 cycles

REMOVED AND REPLACED WASTE SERVICE DOOR REF AMM 53-03-60.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,607 hrs · 21,517 cycles

REMOVED AND REPLACED LT FWD SILL IN FWD FUSELAGE WET AREA IAW SRM 51-40-08.

Part: A/C PACK — SMOKE (NR 1) · airframe 26,987 hrs · 21,060 cycles

HEARD A BUZZING NOISE IN FLIGHT WITH AN ELECTRICAL SMELL. NO MESSAGES OR ANYTHING, NO INDICATIONS. CREW SUSPECTS IT IS COMING FROM PACK 1, NOISE AND SMELL WENT AWAY WHEN THEY TURNED IT OFF ON THE GROUND. R & R THE 1 PACK AIR CYCLE MACHINE IAW AMM 21-51-05. OPS CHECK GOOD.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHT) · airframe 26,870 hrs · 20,966 cycles

OVERHEAD, COCKPIT EMERGENCY EXIT SIGN DOES NOT ILLUMINATE. SECURED THE CONNECTOR ON CEILING PANEL AND EMERGENCY LIGHT OPS CHECKED GOOD IAW AMM 33-50-05.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 24,873 hrs · 19,439 cycles

CREW REPORTED THAT THE COCKPIT EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BATTERY PACK NR 1 IAW AMM AND OPS CHECKED GOOD.

Part: RAMP — DEFECTIVE (L1 DOOR) · airframe 24,660 hrs · 19,267 cycles

CREW REPORTED THAT THE L1 UPPER LEFT DOOR LATCH INDICATOR WAS NOT SHOWING GREEN WHEN DOOR WAS CLOSED AND LOCKED. MAINTENANCE PLACED ON MEL AND LATER R & R GUIDE RAMP ON L1 DOOR IAW AMM AND OPS CHECKED GOOD.

Part: GIRT BAR — OUT OF ADJUST (L1 DOOR) · airframe 24,373 hrs · 19,032 cycles

CREW REPORTED THAT THE L1 DOOR WOULD NOT DISARM AND THE L2 DOOR ASSIST BOTTLE WAS BLOWN. ACFT WAS FLOWN VIA MAINTENANCE FERRY WHERE MAINTENANCE ADJUSTED L1 DOOR GIRT BAR AND SERVICED L2 DOOR ASSIST BOTTLE IAW AMM AND OPS CHECKED GOOD.

Part: SLIDE — PARTIAL DEPLOY (L1 DOOR) · airframe 24,033 hrs · 18,767 cycles

MAINTENANCE REPORTED THAT THE L1 DOOR SLIDE BECAME PARTIALLY DEPLOYED. MAINTENANCE R & R L1 DOOR SLIDE IAW AMM AND OPS CHECKED GOOD.

Part: INDICATION SYS — MALFUNCTIONED (L1 DOOR) · airframe 23,056 hrs · 18,047 cycles

CREW REPORTED THAT THE L1 DOOR SHOWS X WITH YELLOW WHEN THE DOOR IS CLOSED, LOCKED AND LATCHED.

Part: RELIEF VALVE — LEAKING (RT WING FUEL) · airframe 23,007 hrs · 18,004 cycles

F/A REPORTED A STREAM OF FLUID COMING FROM THE RT WING AND CAPTAIN NOTED RT FUEL TANK WAS 300 POUNDS LOW. CREW DECLARED AN EMERGENCY AND DIVERTED. WITH EMERGENCY VEHICLES ROLLING, CREW LANDED AND TAXIED TO GATE WITHOUT INCIDENT. ACFT WAS FLOWN VIA MAINTENANCE FERRY, WHERE MAINTENANCE R & R RT WING OTBD FUEL TANK PRESSURE RELEASE VALVE IAW AMM AND OPS CHECKED GOOD.

Part: BLADE — BIRD INGESTION (NR 2 ENGINE) · airframe 21,478 hrs · 16,798 cycles

CREW HEARD LOUD NOISE AFTER BRINGING THE GEAR UP. NR 2 ENGINE WENT AMBER, DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND NUMEROUS DAMAGED FAN BLADES DUE TO BIRD STRIKE. ACFT REMAINS OUT OF SERVICE. REPLACED THE BLADES.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,941 hrs · 16,373 cycles

CREW REPORTED THAT THE EMERGENCY LIGHT STRIP ON THE RT SIDE OF THE FIRST SECTION WAS INOPERATIVE. R & R THE EMERGENCY LIGHT STRIP IAW AMM AND OPS CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 20,896 hrs · 16,341 cycles

CREW REPORTED THAT BOTH FLIGHT DECK FLASHLIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED FLASHLIGHTS AND BATTERIES IAW AMM AND OPS CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (FWD CABIN) · airframe 20,511 hrs · 16,039 cycles

CREW REPORTED THAT THE FORWARD F/A FLASHLIGHT WAS NOT CHARGING.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 20,463 hrs · 16,002 cycles

CREW REPORTED THAT THE CAPTAIN`S FLASHLIGHT WAS INOPERATIVE. MAINTENANCE R & R THE FLASHLIGHT IAW AMM AND OPS CHECKED GOOD.

Part: CRADLE — BROKEN (FLASHLIGHT) · airframe 17,792 hrs · 13,953 cycles

CREW REPORTED THAT THE FORWARD F/A FLASHLIGHT HOLDER WAS BROKEN. MAINTENANCE R & R THE F/A FLASHLIGHT HOLDER IAW AMM AND OPS CHECKED GOOD.

Part: FLASHLIGHT — BROKEN (COCKPIT) · airframe 17,779 hrs · 13,940 cycles

CREW REPORTED THAT THE CAPTAIN`S FLASHLIGHT WAS BROKEN. MX INSTALLED A NEW FLASHLIGHT IAW AMM AND OPS CHECKED GOOD.

Part: BUSS — INOPERATIVE · airframe 17,645 hrs · 13,842 cycles

CREW REPORTED THAT THE FLIGHT DECK AND CABIN FLASHLIGHTS ARE NOT CHARGING. MAINTENANCE FOUND CIRCUIT BREAKER BUSS AND SECURED IAW AMM. OPS CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 17,390 hrs · 13,653 cycles

AFT F/A REPORTED THAT THE AFT F/A FLASHLIGHT INOPERATIVE. MX R & R FLASHLIGHT IAW AMM AND OPS CHECKED GOOD.

Part: SENSOR — FAILED (SKEW) · airframe 17,252 hrs · 13,545 cycles

AT APPROXIMATELY 1000 FT, RECEIVED A CAUTION MESSAGE AND CHIME FOR SLAT FAIL. SLATS WERE IN POSITION 3 AND FLAPS CONTINUED TO WORK. DECLARED AN EMERGENCY, RAN SLAT/FLAP FAIL PROCEDURES AND LANDED WITHOUT INCIDENT. MX FOUND THAT BOTH LT OTBD SKEW SENSORS HAD FAILED AND REPLACED IAW AMM. OPS CHECKED GOOD.

Part: GIRT BAR — OUT OF ADJUST (R2 DOOR) · airframe 16,831 hrs · 13,229 cycles

CREW REPORTED R2 DOOR WAS JAMMED AND WOULD NOT OPEN. MX FOUND THE GIRT BAR OUT OF ADJUSTMENT. ADJUSTED AFT LOWER GIRT BAR PLATE CLIP IAW AMM. OPS CHECKED GOOD.

Part: NUT — CORRODED (ZONE 800) · corrosion level 2 · airframe 16,829 hrs · 13,227 cycles

DURING HEAVY CHECK, FOUND FWD LOWER GUIDE RAMP ADJUSTMENT HARDWARE CORRODED. MX R & R HARDWARE LOCK NUT AND SET SCREW IAW AMM 53-10-21.

Part: GLOWSTRIP — BROKEN (CABIN) · airframe 16,808 hrs · 13,211 cycles

CREW REPORTED THAT THE PHOTO LUMINESCENT STRIP AT SEAT 1D WAS BROKEN. MX R & R STRIP IAW AMM AND OPS CHECKED GOOD.

Part: GLOWSTRIP — LOOSE (CABIN) · airframe 16,686 hrs · 13,109 cycles

CREW REPORTED THAT THE PHOTO LUMINESCENT STRIP CAME OFF. MX REINSTALLED PHOTO LUMINESCENT STRIP IAW AMM AND OPS CHECKED GOOD.

Part: COVER — OUT OF ADJUST (L1 DOOR) · airframe 16,471 hrs · 12,936 cycles

CREW REPORTED THAT THE L1 DOOR WILL NOT LATCH OPEN. MAINTENANCE ADJUSTED ARM COVER FOR THE L1 DOOR PER EMB AMM AND OPS CHECKED GOOD.

Part: SENSOR — LOOSE (LANDING GEAR) · airframe 15,584 hrs · 12,256 cycles

CREW REPORTED LG WOW FAIL MESSAGE SHORTLY AFTER TAKEOFF. THE MESSAGE EXTINGUISHED ONCE THE LANDING GEAR WAS FULLY RETRACTED. THE CREW DECLARED AN EMERGENCY, RETURNED TO IND WITH EMERGENCY VEHICLES ROLLED AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE R1 AND R2 WOW SENSORS SLIGHTLY LOOSE, MAINTENANCE DISCONNECTED, CLEANED AND RECONNECTED THE SENSORS PER EMB AMM. MAINTENANCE CLEANED THE STRUTS AND PERFORMED GEAR SWINGS WITH NO DEFECTS NOTED.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 14,296 hrs · 11,281 cycles

WHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND THE INBOARD FF1 FLOORBEAM AT FRAME 17 CORRODED. MAINTENANCE REMOVED AND REPLACED THE INBOARD FF1 FLOORBEAM AT FRAME 17 IAW EMB 175 SRM 51-40-02, 51-41-00, 51-41-02, 51-43-01, 51-43-02, AND 51-23-06. THE AIRCRAFT IS OUT OF SERVICE IN HEAVY CHECK.

Part: SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 14,296 hrs · 11,281 cycles

WHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND THE AFT RIGHT FLOOR SUPPORT BEAM SPLICE AT FRAME 86 TO 87 CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFT RIGHT FLOOR SUPPORT BEAM SPLICE AT FRAME 86 TO 87 IAW EMB 175 SRM 51-41-00, 51-43-00, 51-40-02, 51-42-01, AND 51-43-01. THE AIRCRAFT IS OUT OF SERVICE IN HEAVY CHECK.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 14,296 hrs · 11,281 cycles

WHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND THE AFT WASTE BOX DOUBLER CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFT WASTE BOX DOUBLER IAW EMB 175 SRM 51-40-02,AND 51-43-04. THE AIRCRAFT IS OUT OF SERVICE IN HEAVY CHECK.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 14,296 hrs · 11,281 cycles

WHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND THE LAV WASTE BOX DOUBLER CORRODED. MAINTENANCE REMOVED AND REPLACED LAV WASTE BOX DOUBLER IAW EMB 175 SRM 51-40-02 AND 51-43-04. THE AIRCRAFT IS OUT OF SERVICE IN HEAVY CHECK.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 14,296 hrs · 11,281 cycles

WHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND THE AFT RIGHT FLOOR SUPPORT BEAM AT FRAME 86 TO 87 CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFT RIGHT FLOOR SUPPORT BEAM IAW EMB SRM 51-41-00, 51-43-00, 51-40-02 51-42-01, AND 51-43-01. THE AIRCRAFT IS OUT OF SERVICE IN HEAVY CHECK.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 14,296 hrs · 11,281 cycles

WHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND THE AFT LEFT SEAT TRACK BEAM AT FRAME 86 TO 87 CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFT LEFT SEAT TRACK BEAM AT FRAME 86 TO 87 IAW EMB 175 SRM 51-40-02, 51-41-01, 51-42-01, 51-43-01, AND 51-23-01. THE AIRCRAFT IS OUT OF SERVICE IN HEAVY CHECK.

Part: WINDSHIELD — FAULTY (COCKPIT) · airframe 13,109 hrs · 10,333 cycles

WHILE IN CRUISE FLIGHT FROM PHL TO MCI, PILOTS NOTICED A ODOR THAT WAS ONLY NOTED IN THE FLIGHT DECK. THE CREW DECIDED TO DIVERT TO CMH AND DECLARED EMERGENCY. MAINTENANCE PERFORMED OPPS CHECK OF AC SYSTEMS, PACKS, RAN ENGINES, AND NOTICED THAT THE WINDSHIELD HEATER ELEMENT WAS CAUSING THE ODOR. MAINTENANCE REPLACED THE CAPTAINS WINDSHIELD PER THE EMB 175 AMM, AC WAS THEN RETURNED BACK INTO SERVICE.

Part: DOOR — OUT OF ADJUST (R1) · airframe 12,286 hrs · 9,685 cycles

CREW REPORTED R-1 DOOR DIFFICULT TO OPERATE. MAINTENANCE RE-ADJUSTED R-1 DOOR PER EMB AMM, OPS CHECK GOOD.

Part: POWER UNIT — INOPERATIVE (CABIN) · airframe 11,866 hrs · 9,360 cycles

*** GENEREATED WHILE A/C WAS IN HEAVY CHECK *** ALL EMERGENCY LIGHTS ON R-1 DOOR INOP. MAINTENANCE REMOVED AND REPLACED THE RT FWD EMERGENCY LIGHT POWER UNIT PER EMB AMM, OPS CHECK GOOD.

Part: DOUBLER — MISINSTALLED (FUSELAGE) · airframe 11,866 hrs · 9,360 cycles

*** WHILE AIRCRAFT WAS IN FOR HEAVY CHECK *** LARGE RECTANGULAR PATCH AT FR 28, STR 13L DOES NOT APPEAR TO BE EDGE SEALED. MAINTENANCE PERFORMED A MAJOR REPAIR IAW EMB ETD2011-170-101683 REV E & EMB 175 SRM 53-21-01. REFERENCE PO #'S 024093-2011 & 023526-2011 FOR PARTS INSTALLED.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,866 hrs · 9,360 cycles

WHILE AIRCRAFT WAS IN FOR HEAVY CHECK CMH, MAINTENANCE FOUND CENTER SHEAR PLATE CORRODED AT FRAME 87 AND 88. MAINTENANCE REMOVED AND REPLACED THE CENTER SHEAR PLATE IAW EMB 175 SRM 51-42-01 AND 02. AIRCRAFT REMAINS OUT OF SERVICE AND IS STILL IN C CHECK.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,866 hrs · 9,360 cycles

*** WHILE AIRCRAFT WAS IN FOR HEAVY CHECK *** LEVEL TWO CORROSION WAS FOUND IN THE AFT LAV AREA, LT SHEAR PLATE AT FR 87-88. MAINTENANCE REMOVED AND REPLACED THE LT SHEAR PLATE IAW EMB 175 SRM 51-42-01 & 02. AIRCRAFT STILL OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,866 hrs · 9,360 cycles

*** WHILE AIRCRAFT WAS IN FOR HEAVY CHECK *** LEVEL TWO CORROSION WAS FOUND IN THE AFT GALLEY/LAV AREA, CTR RT FLOORBEAM TIE PLATE AT FR 90. MAINTENANCE REMOVED AND REPLACED THE RT SHEAR PLATE AT FR 90 IAW EMB 175 SRM 51-41-02. AIRCRAFT IS STILL CURRENTLY OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,866 hrs · 9,360 cycles

*** WHILE AIRCRAFT WAS IN FOR HEAVY CHECK *** LEVEL TWO CORROSION WAS FOUND IN THE AFT LAV AREA, LT SILL TIE PLATE AT FR 87-88. MAINTENANCE REMOVED AFT LAV LT SILL SPLICE PLATE AND INSTALLED SERVICEABLE SPLICE PLATE IAW EMB 175 SRM 51-42-02. AIRCRAFT STILL OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,866 hrs · 9,360 cycles

*** WHILE AIRCRAFT WAS IN FOR HEAVY CHECK *** LEVEL TWO CORROSION WAS FOUND IN THE AFT GALLEY AREA, RT SHEAR PLATE AT FR 87-88. MAINTENANCE REMOVED AND REPLACED THE RT SHEAR PANEL IAW EMB 175 SRM 51-42-01 & 02. AIRCRAFT STILL OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: FASTENER — CORRODED (LE SLAT) · corrosion level 2 · airframe 11,866 hrs · 9,360 cycles

*** WHILE AIRCRAFT WAS IN FOR HEAVY CHECK *** LEVEL TWO CORROSION WAS FOUND ON THE LEFT WING LEADING EDGE PANEL (PAINT CHIPPING AND HARDWARE RUSTED), OUTBOARD OF NR 4 SLAT. MAINTENANCE APPLIED PAINT TO LEFT WING LEADING EDGE PANEL IAW EMB 175 SRM 51-23-06 AND INSTALLED NEW HARDWARE IAW EMB 175 AMM 20-10-01. AIRCRAFT STILL OUT OF SERVICE FOR HEAVY CHECK.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,866 hrs · 9,360 cycles

*** WHILE AIRCRAFT WAS IN FOR HEAVY CHECK *** LEVEL TWO CORROSION WAS FOUND IN THE AFT GALLEY/LAV AREA, CTR LT FLOORBEAM TIE PLATE AT FR 90. MAINTENANCE REMOVED AND REPLACED LT SHEAR PLATE AT FR 90 IAW EMB 175 SRM 51-41-02. AIRCRAFT IS CURRENTLY STILL OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: SEAL — WORN (LE SLAT) · corrosion level 2 · airframe 11,866 hrs · 9,360 cycles

WHILE A/C WAS IN FOR HEAVY CHECK FOUND LEFT WING NR 1 SLAT LOWER EDGE SEAL WORN AND RUSTED HARDWARE. MX REMOVED AND REPLACED LEFT WING HARDWARE AS WELL AS LOWER SEAL NR 1 SLAT IAW EMB 175 AMM 57-41-09. A/C REMAINS IN CMH FOR HEAVY CHECK COMPLETION. P/N'S 170-35160-001, 170-35161-001, 170-35162-001.

Part: INDICATOR — MALFUNCTIONED (R1 DOOR) · airframe 11,720 hrs · 9,245 cycles

R1 DOOR VISUAL INDICATOR NOT WORKING, LATCH NOT CLOSING CORRECTLY. MAINTENANCE CYCLED DOOR MECHANISM, DOOR INDICATION NOW CHECKS GOOD PER EMB AMM 52-41-00-0.

Part: SLIDE — DEFECTIVE (R1 DOOR) · airframe 11,625 hrs · 9,170 cycles

CREW REPORTED R-1 DOOR HANDLE WAS HARD TO OPERATE. MAINTENANCE TROUBLESHOT PER EMB AMM AND FOUND THE R-1 DOOR EMERG EVAC SLIDE ASSY TO BE AT FAULT. MAINTENANCE REMOVED AND REPLACED R-1 DOOR EMERGENCY EVACUATION SLIDE ASSY PER EMB AMM, OPS CHECK GOOD.

Part: B-NUT — LOOSE (HYDRAULIC SYS) · airframe 10,804 hrs · 8,532 cycles

CREW REPORTED HYD SYSTEM FLUID LOSS IN FLIGHT AND DIVERTED TO CLT. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED WITHOUT INCIDENT AT CLT. MAINTENANCE TROUBLESHOT AND RE-TORQUED B-NUT NEAR E-2 MANIFOLD PER EMB AMM, OPS CHECK GOOD. A/C WAS THEN RETURNED TO SERVICE.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 10,094 hrs · 7,994 cycles

CREW REPORTED EMERGENCY LIGHT BATTERY FAULT ON EICAS, MX RESET AC POWER PER EMB AMM MESSAGE CLEARED AC OK FOR SERVICE.

Part: SWITCH — FAULTY (CABIN) · airframe 9,762 hrs · 7,725 cycles

CREW REPORTED RAINBOW LIGHTS IN THE CABIN WERE INOP. MAINTENANCE TROUBLESHOT PER EMB AMM AND FOUND THE TEST SWITCH ON THE FA PANEL TO BE AT FAULT, AND PLACED ON MEL 25-22-04-1.

Part: GIRT BAR — OUT OF ADJUST (L1 DOOR) · airframe 9,282 hrs · 7,334 cycles

CREW REPORTED L-1 SLIDE ARM LEVER WAS HARD TO MOVE. MAINTENANCE ADJUSTED L-1 DOOR GIRT BAR PER EMB AMM, OPS CHECK GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 8,304 hrs · 6,544 cycles

MAINTENANCE REPORTED THE AFT SERVICE DOOR EXIT IDENTIFIER SIGN DIDN'T ILLUMINATE DURING EMERGENCY LIGHT POWER UNIT FUNCTIONAL TEST. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY BATTERY PER EMB AMM.

Part: MODULE — FAULTED (AVIONICS BAY) · airframe 6,535 hrs · 5,102 cycles

CREW RECEIVED A STEER FAIL MSG ON EICAS WHEN LOWERING GEAR WHILE ON APPROACH. CREW DECLARED EMERGENCY AND LANDED AT CLE WITHOUT INCIDENT. MTX WAS DISPATCHED TO THE A/C TO TROUBLESHOOT. MTX RESET THE STEERING C/B AND PERFORMED OPS CHECKS PER EMB AMM, NO FAULTS WERE FOUND. A/C WAS RELEASED BACK INTO SERVICE. AFTER ENGINEERING REVIEWED THE FHDB DOWNLOAD, NOTICED THE NIC/PROC 3 WAS AT FAULT. MTX REMOVED AND REPLACED NIC/PROC 3 PER EMB AMM. A/C WAS THEN RELEASED BACK INTO SERVICE.