N811MD

Part: FITTING — GOUGED (LT MLG) · airframe 26,944 hrs · 20,138 cycles

DURING C-CHECK, LT MLG UPPER SIDE BRACE FITTING CROSS SUPPORT FOUND GOUGED. MAINTENANCE R & R THE SUPPORT IAW SRM 51-43-02. MAJOR REPAIR.

Part: BATTERY PACK — WEAK (FLASHLIGHT) · airframe 24,403 hrs · 18,195 cycles

CAPTAIN'S FLASHLIGHT IS VERY DIM WITH FULL CHARGE. R & R BATTERY. OPS CHECKED GOOD IAW AMM 25-51-00.

Part: LINKAGE — OUT OF ADJUST (DOOR INDICATOR) · airframe 24,014 hrs · 17,901 cycles

CREW REPORTED THAT THE L2 DOOR INDICATION WAS NOT SHOWING GREEN. MAINTENANCE ADJUSTED VISUAL INDICATOR LINKAGE IAW AMM AND OPS CHECKED GOOD. ACFT IS GOOD FOR SERVICE.

Part: WARNING MESSAGE — MULTIPLE FAIL · airframe 23,929 hrs · 17,836 cycles

RECEIVED AN "AVNX MAU 3B FAIL", "SPOILER FAULT" AND "CMF 1" FAIL MESSAGES. CONSULTED MAINTENANCE AND CONTINUED ON TO DESTINATION AND DECLARED AN EMERGENCY. ON SELECTING FLAPS 1, RECEIVED A "FLAP FAIL" MESSAGE THAT WENT OUT A FEW SECONDS LATER. PERFORMED A FULL FLAPS LANDING AND LANDED WITHOUT INCIDENT WITH SPOILERS DEPLOYED AND ALL SYSTEMS OPERATIVE. MAINTENANCE INSPECTED AND RESET MAU 3 IAW AMM, FAULT CLEARED AND ACFT IS GOOD FOR SERVICE.

Part: DEFLECTOR — DAMAGED (L2 DOOR) · airframe 23,583 hrs · 17,577 cycles

CREW REPORTED THAT THE L2 DOOR WAS MAKING A BANGING AND RUMBLING NOISE IN FLIGHT. AN EMERGENCY WAS NOT DECLARED AND CREW LANDED WITHOUT INCIDENT. MX INSPECTED AND TRIMMED THE DOOR DEFLECTOR AND PLACED DEFLECTOR ON CDL. ACFT IS GOOD FOR SERVICE.

Part: BOLT — CORRODED (R2 DOOR SLIDE) · corrosion level 2 · airframe 23,539 hrs · 17,541 cycles

DURING HEAVY CHECK, FOUND R2 DOOR SLIDE LOWER MOUNTING BOLT CORRODED. MX R & R LOWER MOUNTING BOLT IAW AMM 52-42-40.

Part: DEPRESSOR — DAMAGED (PAX DOOR FRAME) · airframe 23,539 hrs · 17,541 cycles

DURING HEAVY CHECK, FOUND FORWARD PASSENGER DOOR SEAL CHANNEL ON AIRFRAME HAS MULTIPLE RIVET HEADS DAMAGED. MX R & R FORWARD PASSENGER DOOR SEAL DEPRESSOR IAW SRM 51-40-02, 51-41-01, & 51-43-01.

Part: SCREW — CORRODED (R2 DOOR) · corrosion level 2 · airframe 23,539 hrs · 17,541 cycles

DURING HEAVY CHECK, FOUND R2 DOOR COMMAND RAMP ADJUSTMENT HARDWARE CORRODED. MX R & R ROLLER HIGHT ADJUSTMENT HARDWARE IAW AMM 53-23-25,.

Part: NUT — CORRODED (L1 DOOR) · corrosion level 2 · airframe 23,539 hrs · 17,541 cycles

DURING HEAVY CHECK, FOUND DOOR STOP ON FWD SIDE, L1 DOOR NUT CORRODED. MX R & R NUT.

Part: DEPRESSOR — WORN (L1 DOORWAY) · airframe 23,539 hrs · 17,541 cycles

DURING HEAVY CHECK, FOUND L1 DOOR SEAL DEPRESSOR ON FRAME WORN LOWER SECTIONS FWD AND AFT. MX R & R SEAL DEPRESSOR IAW SRM 51-40-02.

Part: NUT — CORRODED (ZONE 800) · corrosion level 2 · airframe 23,539 hrs · 17,541 cycles

DURING HEAVY CHECK, REPORTED L1 DOOR AFT LOWER STOP NUT CORRODED. MX R & R AFT LOWER STOP NUT IAW AMM 52-11-23.

Part: STRUCTURE — CORRODED (GALLEY) · corrosion level 2 · airframe 23,539 hrs · 17,541 cycles

DURING HEAVY CHECK, AFT GALLEY SPLIT JOINTS ON FWD SECTION, AND TRIM STRIPS HAVE CORROSION. MX R & R SPLIT JOINTS ON FWD SECTION AND ALL TRIM STRIPS IAW SRM 51-40-00 & AMM 25-00-23, 25-0017, 25-00-10, PN 170-87021-001, FITTING, TRIM 170-59522. ACFT REMAINS FOR HEAVY CHECK COMPLETION.

Part: BOLT — CORRODED (L1 DOOR SLIDE) · corrosion level 2 · airframe 23,539 hrs · 17,541 cycles

DURING HEAVY CHECK, L1 DOOR LOWER EMERGENCY EVACUATION SLIDE MOUNTING HARDWARE CORRODED. R & R SLIDE MOUNTING HARDWARE IAW AMM 52-11-40.

Part: ADJUSTER — CORRODED (L1 DOOR) · corrosion level 2 · airframe 23,539 hrs · 17,541 cycles

DURING HEAVY CHECK, FOUND FORWARD LOWER COMMAND RAMP ADJUSTMENT HARDWARE CORRODED AT L1 DOOR. MX REMOVED AND REPLACED ROLLER GUIDE ADJUSTMENT SCREW AND JAM NUT IAW AMM 53-10-21. PN AN565F524H16, SET SCREW. ACFT REMAINS FOR COMPLETION OF HEAVY CHECK.

Part: CROSSBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 23,539 hrs · 17,541 cycles

DURING HEAVY CHECK, CROSSBEAM AT FRAME 14 CORRODED. MX R & R CROSSBEAM IAW SRM 51-40-2, 51-43-03, 51-41-01, 51-43-01.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 23,539 hrs · 17,541 cycles

DURING HEAVY CHECK, LT HORIZONTAL L/E HAS TWO CRACKED RIBS, BOTH ON LOWER EDGE NR 4 HAS 1 INCH CRACK, R5 HAS .43 INCH CRACK. REPAIRED BOTH CRACKED RIBS IAW ETD 2013-170-029512.

Part: RIB — CRACKED (RT WING) · airframe 23,539 hrs · 17,541 cycles

DURING HEAVY CHECK, REPORTED RT WING RIB 10 EXTENSION IS CRACKED GOING FWD AND AFT FROM UPPER SKIN HI-LOCK HOLE, THIRD FROM AFT SIDE, CRACK LENGTH .320 FROM AFT EDGE OF HOLE,.480 FROM FWD EDGE OF HOLE. MX R & R RIB 10 EXTENSION IAW SRM 51-43-02, SRM 51-43-03. PERFORMED FCBS 57-10-00-005 NO ADDITIONAL INSPECTIONS REQUIRED. PN 170-32161-612/RIB 10. MAJOR REPAIR, ACFT REMAINS FOR COMPLETION OF HEAVY CHECK.

Part: RIB — CRACKED (ZONE 300) · airframe 23,539 hrs · 17,541 cycles

DURING HEAVY CHECK, RT HORIZONTAL STAB L/E NR 4 RIB HAS .40" CRACK AT UPPER EDGE. MX REPAIRED CRACKED RIB IAW ETD 2013-170-029512.

Part: RIB — CRACKED (LT WING) · airframe 23,539 hrs · 17,541 cycles

WHILE IN HEAVY CHECK, REPORTED LT WING RIB 10 EXTENSION IS CRACKED. MX R & R RIB 10 IAW SRM 51-40-02, 51-43-01, & 51-43-02.

Part: RIB — CRACKED (ZONE 500) · airframe 23,539 hrs · 17,541 cycles

DURING HEAVY CHECK, LT WING RIB 10 EXTENSION IS CRACKED GOING FORWARD AND AFT FROM UPPER SKIN HI-LOC HOLE THIRD FROM AFT SIDE CRACK LENGTH .240 FROM AFT EDGE OF HOLE, .200 FROM FORWARD EDGE OF HOLE. MX R & R RIB 10 IAW SRM 51-4-02, 51-40-01, 51-43-02. PN 170-32161-611 RIB 10.

Part: STOP — CORRODED (L2 DOOR) · corrosion level 2 · airframe 23,539 hrs · 17,541 cycles

DURING HEAVY CHECK, L2 DOOR STOPS ON DOOR WERE CORRODED. MX R & R HARDWARE IAW AMM 52-12-13.

Part: BRACKET — CRACKED (ZONE 100) · airframe 23,539 hrs · 17,541 cycles

DURING HEAVY CHECK, LT PACK DUCT SUPPORT BRACKET CRACKED. MX R & R LT PACK DUCT SUPPORT BRACKET IAW SRM 51-41-01,

Part: WASHER — CORRODED (L2 DOOR) · airframe 23,539 hrs · 17,541 cycles

DURING HEAVY CHECK, L2 DOOR LOWER WASHER IS CORRODED ON INNER RED DOOR HANDLE ADJUSTABLE. MX R & R LOWER WASHER IAW AMM 52-12-52.

Part: STOP — CORRODED (ZONE 800) · corrosion level 2 · airframe 23,539 hrs · 17,541 cycles

DURING HEAVY CHECK, L2 DOOR STOPS 2A, 5A, 6A, ARE CORRODED. MX R & R HARDWARE IAW AMM 52-12-23. PN NAS509-7.

Part: BOLT — CORRODED (L2 DOOR) · corrosion level 2 · airframe 23,539 hrs · 17,541 cycles

DURING HEAVY CHECK, L2 DOOR LOWER BOLT ON AFT LOWER ROLLER GUIDE IS CORRODED. MX R & R IAW 53-23-21.

Part: WASHER — CORRODED (L2 DOOR) · airframe 23,539 hrs · 17,541 cycles

DURING HEAVY CHECK, L2 DOOR LOWER WASHER IS CORRODED ON INNER RED DOOR HANDLE ADJUSTABLE. MX R & R LOWER WASHER IAW AMM 52-12-52.

Part: DAMPENER — CORRODED (L2 DOOR) · corrosion level 2 · airframe 23,539 hrs · 17,541 cycles

DURING HEAVY CHECK WAS REPORTED L2 DOOR DAMPENER IS CORRODED. MX R & R L2 DOOR DAMPENER IAW AMM 52-12-27.

Part: SPAR — CRACKED (ZONE 500) · airframe 23,539 hrs · 17,541 cycles

DURING HEAVY CHECK, LT WING UPPER SKIN CRACKED ABOUT .750 LONG AT SPAR 2 RIB 10. MX REPAIRED LT WING UPPER SKIN IAW ETD 2013-170-028510.

Part: SKIN — CRACKED (RT WING) · airframe 23,539 hrs · 17,541 cycles

DURING HEAVY CHECK, REPORTED RT UPPER WING SKIN CRACKED AT SPAR 2, RIB 10 ABOUT 1" LONG FROM T/E- VERIFIED WITH DYE PEN INSP. THE UPPER RT WING SKIN (FCBS 57-10-00-003) AT RIB 10 AND SPAR 2 WAS REPAIRED IAW ETD 2013-170-028489, REV D, DATED AUG 27, 2013. REF CONTINUATION CARD VP 022689-2013-137 C1, C2, C3, C4, C5 FOR C/A AND ORIGINAL SIGNITURES. THIS REPAIR IS TEMPORARY, VALID FOR A TIME OF 12 MONTHS DURING THIS PERIOD, PERMANENT REPAIR INSTRUCTIONS WILL BE SENT. NO CHANGES TO TO THE CURRENT REVIOSION OF THE MPG ARE REQUIRED. DURING THE 12 MONTHS OF THIS TEMPORARY REPAIR TRANSFERED TO NON-MEL DMI 415988-2 FOR 12 MONTHS UNTIL STRUCTURE ANALYSIS IS COMPLETED IAW GMM 9.5.4. APPROVED.

Part: SEAL — DIRTY (L2 DOOR) · airframe 23,469 hrs · 17,492 cycles

CREW REPORTED THAT THE L2 DOOR WAS MAKING A VERY LOUD NOISE DURING FLIGHT. AN EMERGENCY WAS NOT DECLARED AND LANDED WITHOUT INCIDENT. MX INSPECTED L2 DOOR SEAL, VENT FLAP SEAL AND CLEANED DEBRIS FROM L2 DOOR SEAL IAW AMM. ACFT IS GOOD FOR SERVICE.

Part: UNKNOWN — UNKNOWN (L2 DOOR) · airframe 23,443 hrs · 17,474 cycles

L2 DOOR WAS MAKING NOISE IN CRUISE AND ON DESCENT. MX INSPECTED L2 DOOR SEAL AND DEFLECTOR IAW AMM AND NO DEFECTS NOTED. ACFT IS GOOD FOR SERVICE.

Part: BLADE — DAMAGED (NR 1 ENGINE) · airframe 22,984 hrs · 17,134 cycles

DURING CLIMB, CREW REPORTED A BIRD INGESTION INTO ENGINE NR 1. CREW DID NOT DECLARE AN EMERGENCY BUT DIVERTED TO PIT DUE TO HIGH LP VIBES. ACFT LANDED WITHOUT INCIDENT. MX FOUND 2 FAN BLADES DAMAGED, BUT CHANGED 4 TO KEEP ENGINE IN BALANCE IAW AMM. OPS CHECKED GOOD.

Part: GLOWSTRIP — LOOSE (CABIN) · airframe 22,492 hrs · 16,777 cycles

CREW REPORTS THAT THE PHOTO LUMINESCENT STRIP HALF WAY BACK ON THE RIGHT SIDE OF THE AIRCRAFT IS COMING UP. MAINTENANCE RE-SECURED STRIP PER EMB AMM 33-50-21 AND OPS CHECKED GOOD.

Part: SLIDE — UNWANTED DEPLOY (L2 DOOR) · airframe 22,085 hrs · 16,497 cycles

CREW REPORTED THAT WHEN CATERING OPENED THE L2 DOOR, THE GIRT BAR DID NOT DISENGAGE AND THE SLIDE NOW NEEDS TO BE REPLACED. MAINTENANCE REMOVED AND REPLACED L2 DOOR CABLE PER EMB AMM AND OPS CHECKED GOOD.

Part: ATTACH FITTING — OUT OF ADJUST (L1 DOOR) · airframe 20,498 hrs · 15,321 cycles

CREW REPORTS L1 DOOR WILL NOT ARM. MAINTENANCE ADJUSTED AFT GIRT BAR ATTACHMENT PER EMB AMM.

Part: LINER — OUT OF POSITION (R1 DOOR) · airframe 19,361 hrs · 14,446 cycles

CREW REPORTED R-1 DOOR WAS DIFFICULT TO DISARM. MAINTENANCE RE-POSITIONED R-1 DOOR LINER PER EMB AMM, OPS CHECK GOOD.

Part: BONDING STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,353 hrs · 14,438 cycles

WHILE AIRCRAFT WAS IN FOR HEAVY CHECK, LEVEL 2 CORROSION WAS FOUND ON THE AFT DRAIN SHROUD BONDING STRAPS. MAINTENANCE REPAIRED THE AFT DRAIN SHROUD BONDING STRAPS IAW EMB 170 SRM 51-73-00. AIRCRAFT IS CURRENTLY STILL OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: SERVICE PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,353 hrs · 14,438 cycles

WHILE AIRCRAFT WAS IN FOR HEAVY CHECK, LEVEL 2 CORROSION WAS FOUND ON THE WASTE SERVICE PANEL INSIDE THE FUSELAGE. MAINTENANCE REMOVED AND REPLACED THE WASTE SERVICE PANEL BOX ASSY IAW EMB 170/175 SRM 51-43-03, 51-43-04, 51-43-01, 51-23-04, 51-23-05 AND 51-23-06. REF P/N'S 170-85084-405 (BOX ASSY) & 170-86655-003 (DOUBLER). AIRCRAFT IS CURRENTLY STILL OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 19,331 hrs · 14,422 cycles

CREW REPORTED STRONG ODOR THAT SMELLED LIKE BURNING OIL DURING TAKEOFF. MAINTENANCE PERFORMED INSPECTION OF ENGINES IAW GE ENGINE MANUAL, NO DEFECTS FOUND.

Part: BELLCRANK — OUT OF ADJUST (R1 DOOR) · airframe 18,801 hrs · 14,006 cycles

CREW REPORTED R-1 DOOR WOULDN'T CLOSE ALL OF THE WAY. MAINTENANCE ADJUSTED R-1 DOOR STOP BELLCRANK PER EMB AMM, OPS CHECK GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 18,191 hrs · 13,523 cycles

CREW REPORTED LAST CABIN EMERGENCY EXIT LIGHT IS INOP. MAINTENANCE REMOVED AND REPLACED AFT RT BATTERY POWER UNIT, OPS CHECK GOOD.

Part: SENSOR — FAULTY (LE SLAT) · airframe 16,516 hrs · 12,244 cycles

CREW RECEIVED SLAT FAIL MESSAGE ON EICAS WHILE ON APPROACH TO MCI. FLAPS AND SLATS WOULD NOT DEPLOY AND WERE SET AT ZERO. CREW DECLARED AN EMERGENCY LANDING AND CFR WAS DISPATCHED. AIRCRAFT LANDED SAFELY WITHOUT INCIDENT AND TAXIED TO GATE UNDER ITS OWN POWER. MX REPLACED 3/4 & 2/3 RIGHT SKEW SENSORS, AND 2/3 & 3/4 HARNESS PER EMB AMM.

Part: GUST LOCK — OUT OF ADJUST (L1 DOOR) · airframe 15,599 hrs · 11,468 cycles

CREW REPORTED L-1 DOOR WAS HARD TO CLOSE. MAINTENANCE ADJUSTED THE GUS LOCK PER EMB AMM, AND PERFORMED OPS CHECKS. THE A/C WAS THEN RETURNED TO SERVICE.

Part: PIN — UNSECURE (EVAC SLIDE) · airframe 15,245 hrs · 11,156 cycles

CREW REPORTED L-2 DOOR WOULDN'T DISARM. OCM RE-SECURED SLIDE COVER PIN PER EMB AMM, THE DOOR THEN OPERATED NORMALLY.

Part: UNKNOWN — MALFUNCTIONED (L1 DOOR) · airframe 15,052 hrs · 11,004 cycles

CREW REPORTED L-1 DOOR DISARMING LEVEL WAS INOP. MAINTENANCE PERFORMED OPS CHECK OF DOOR 5 TIMES PER EMB AMM, NEW CREW ATTEMPTED TO OPERATE THE DOOR AND OPS CHECK GOOD.

Part: PIN — OUT OF POSITION (SLIDE COVER) · airframe 15,026 hrs · 10,988 cycles

CREW REPORTED L-2 DOOR WOULDN'T LOCK/ARM PROPERLY. MAINTENANCE RESET PIN IN DOOR SLIDE COVER POSITION PER EMB AMM, OPS CHECK GOOD.

Part: DOUBLER — CORRODED (LAV SERVICE DOOR) · corrosion level 2 · airframe 14,714 hrs · 10,714 cycles

WHILE IN HEAVY CHECK, MAINTENANCE REPORTED THE INTERNAL FWD DOUBLER OF WASTE SERVICE PANEL BOX ASSY WAS CORRODED. MAINTENANCE REMOVED AND REPLACED THE FWD DOUBLER (INTERNAL) OF WASTE SERVICE PANEL BOX ASSY IAW SRM 51-43-02.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 14,714 hrs · 10,714 cycles

WHILE AC WAS IN FOR HEAVY CHECK, LEVEL TWO CORROSION WAS FOUND ON RT AFT DOOR SILL, AROUND SCREW HOLE AT FR 89. MAINTENANCE REMOVED AND REPLACED SILL SUPPORT PER THE EMB SRM. AC STILL OUT OF SERVICE FOR REMAINDER OF HEAVY CHECK.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 14,714 hrs · 10,714 cycles

WHILE AC WAS IN FOR HEAVY CHECK, LEVEL TWO CORROSION WAS FOUND ON RT AFT DOOR SILL, FR 90. MAINTENANCE REMOVED AND REPLACED DOOR SILL PER EMB SRM. AC STILL OUT OF SERVICE FOR HEAVY CHECK.

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 14,714 hrs · 10,714 cycles

WHILE AC WAS IN FOR HEAVY CHECK, LEVEL TWO CORROSION WAS FOUND ON RT FLOORBEAM GUSSET AT FR 90. MAINTENANCE REMOVED AND REPLACED GUSSET PER EMB SRM. AC STILL OUT OF SERVICE FOR HEAVY CHECK.

Part: POWER UNIT — INOPERATIVE (CABIN) · airframe 13,254 hrs · 9,501 cycles

CREW REPORTED THAT THE EMERGENCY LIGHTING FOR L-2 DOOR EXIT LIGHT WAS INOP. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT POWER UNIT PER EMB AMM.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 12,902 hrs · 9,218 cycles

CREW REPORTED THAT THE EMERGENCY LIGHTS ARE NOT WORKING PROPERLY. MAINTENANCE RESET THE EMERGENCY POWER PER THE EMB 170 AMM, OPS CHECKED AND FOUND OK FOR SERVICE.

Part: SLAT SYSTEM — MALFUNCTIONED (LE SLATS) · airframe 12,650 hrs · 9,021 cycles

CREW RECEIVED A SLAT FAIL MESSAGE ON EICAS DURING APPROACH INTO PHL. CREW DECLARED AN EMERGENCY AND LANDED INTO PHL WITHOUT INCIDENT. MAINTENANCE WAS DISPATCHED TO THE A/C AND TESTED OUT SKEW SENSORS, CLEARED INHIBITS, RAN FLAPS/SLATS SEVERAL TIMES AND COULDN'T DUPLICATE THE DISCREPANCY PER EMB AMM. NO PREVIOUS HISTORY NOTED. A/C WAS THEN RELEASED BACK INTO SERVICE.

Part: FADAC — MALFUNCTIONED (NR 1 ENGINE)

FLT 1620 - ATL-PIT - ON CLIMB, CAPTAIN RECEIVED INDICATIONS OF NR 1 ENGINE POWER SURGE TEMPERATURE EXCEEDANCE AND FOUR FAULT MESSAGES. THE CAPTAIN DECLARED AN EMERGENCY AND RETURNED TO THE FIELD WITHOUT INCIDENT. MAINTENANCE REPLACED NR 1 ENGINE FADAC. PERFORMED GROUND RUN AND POWER ASSURANCE, NO DEFECTS NOTED. (M)