N807MD

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,190 hrs · 21,969 cycles

CREW REPORTED THAT THE ENTRY EMERGENCY LIGHT STRIP WAS WORN AND INOPERATIVE. MAINTENANCE R & R THE LIGHT STRIP IAW AMM AND OPS CHECKED GOOD.

Part: HANDLE — BROKEN (MEGAPHONE) · airframe 28,972 hrs · 21,795 cycles

CREW REPORTED THAT THE MEGAPHONE HANDLE WAS BROKEN. MAINTENANCE R & R MEGAPHONE IAW AMM AND OPS CHECKED GOOD.

Part: FLASHLIGHT — BROKEN (FWD CABIN) · airframe 28,492 hrs · 21,419 cycles

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

Part: ATTACH FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 27,475 hrs · 20,613 cycles

DURING HEAVY CHECK, AFT BELLY PANEL 195NL FWD ATTACH CENTER ATTACH STRIP IS CORRODED. MX R & R AFT BELLY PANEL, 195NL FWD ATTACH CENTER ATTACH STRIP IAW AMM 53-04-50.

Part: GUSSET — CORRODED (ZONE 100) · corrosion level 2 · airframe 27,475 hrs · 20,613 cycles

DURING HEAVY CHECK, CENTER GUSSET AT FRAME 90 IS CORRODED. MAINTENANCE R & R CENTER GUSSET AT FRAME 90 IAW SRM 51-43-90.

Part: UPPER SHEET — CORRODED (FRAMES 85-86) · corrosion level 2 · airframe 27,475 hrs · 20,613 cycles

DURING HEAVY CHECK, LT UPPER SHEET AT FRAME 85-86 IS CORRODED. MAINTENANCE R & R LT UPPER SHEET AT FRAME 85-86 IAW SRM 51-43-07, 51-41-01.

Part: FLOOR SUPPORT — CORRODED (FRAMES 88-90) · corrosion level 2 · airframe 27,475 hrs · 20,613 cycles

DURING HEAVY CHECK, LT PANEL SUPPORT FRAME 88-90 IS CORRODED. MAINTENANCE R & R LT PANEL SUPPORT FRAME 88-90 IAW SRM 51-41-01, 51-42-01, 51-43-03.

Part: UPPER SHEET — CORRODED (FRAMES 85-86) · corrosion level 2 · airframe 27,475 hrs · 20,613 cycles

DURING HEAVY CHECK, RT UPPER SHEET AT FRAME 85-86 IS CORRODED. MAINTENANCE R & R RT UPPER SHEET AT FRAME 85-86 IAW 51-43-03, 51-41-01. AIRCRAFT REMAINS UNTIL HEAVY CHECK IS COMPLETED

Part: GUSSET — CORRODED (FRAME 91) · corrosion level 2 · airframe 27,475 hrs · 20,613 cycles

DURING HEAVY CHECK, RT FRAME 91, Y10.78 GUSSET IS CORRODED. MAINTENANCE R & R RT FRAME 91, Y10.78 GUSSET IAW SRM 51-41-02.

Part: GUSSET — CORRODED (FRAME 91) · corrosion level 2 · airframe 27,475 hrs · 20,613 cycles

DURING HEAVY CHECK LT GUSSET AT FRAME 91 IS CORRODED. MAINTENANCE R & R LT GUSSET AT FRAME 91 IAW SRM 51-41-02. ACFT REMAINS UNTIL HEAVY CHECK IS COMPLETED.

Part: SPLICE PLATE — CORRODED (FRAMES 87-88) · corrosion level 2 · airframe 27,475 hrs · 20,613 cycles

DURING HEAVY CHECK, SPLICE PLATE RT SHEAR PLATE AT FRAMES 87-88. MAINTENANCE R & R SPLICE PLATE RT SHEAR PLATE AT FR 88/87 IAW SRM 51-21-02, 51-40-02, PN 170-65644-001, SPLICE PLATE. ACFT REMAINS UNTIL HEAVY CHECK IS COMPLETED.

Part: STRINGER — CORRODED (FRAME 88) · corrosion level 2 · airframe 27,475 hrs · 20,613 cycles

DURING HEAVY CHECK, STRINGER 27R AT FRAME 88 IS CORRODED. MX R & R STRINGER 27R AT FRAME 88 IAW ETD 2015--170--027169, REV A. ACFT REMAINS UNTIL HEAVY CHECK IS COMPLETED.

Part: BRACKET — CORRODED (ZONE 100) · corrosion level 2 · airframe 27,475 hrs · 20,613 cycles

DURING HEAVY CHECK, WING TO FUSELAGE FAIRING ATTACH BRACKET AIR FRAME SIDE WHERE FAIRING 191FL IS CORRODED. MAINTENANCE R & R 4 EACH ATTACH FAIRING BRACKETS IAW SRM 51-41-02, 51-42-02. AIRCRAFT REMAINS UNTIL HEAVY CHECK IS COMPLETED.

Part: SEAT TRACK — CORRODED (FRAMES 12-20) · corrosion level 2 · airframe 27,475 hrs · 20,613 cycles

DURING HEAVY CHECK, LT FWD SEAT TRACK FRAME 12/20 AT FRAME 17 HAS CORROSSION. MAINTENANCE R & R LT SEAT TRACK FRAME 12/20 AT FRAME 17 IAW SRM 51-40-01, 51-41-03, 51-43-03, 51-43-02,51-23-06. PN 170-03264-001, SEAT TRACK ACFT REMAINS UNTIL HEAVY CHECK IS COMPLETED.

Part: GUSSET — CORRODED (FRAMES 87-88) · corrosion level 2 · airframe 27,475 hrs · 20,613 cycles

DURING HEAVY CHECK, CENTER STRESS PANEL AT GALLEY MOUNTHOLE BETWEEN FRAME 87-88 IS CORRODED. MAINTENANCE R & R SHEAR PANEL, PN 170-65928-001, GUSSET. AIRCRAFT REMAINS UNTIL HEAVY CHECK IS COMPLETED.

Part: CLOSEOUT PANEL — CORRODED (CARGO BAY) · corrosion level 2 · airframe 27,475 hrs · 20,613 cycles

WHILE IN HEAVY CHECK WAS REPORTED THAT AFT CARGO DOOR THRESHOLD CLOSE OUT PANEL IS CORRODED. MAINTENANCE R & R AFT CARGO DOOR THRESHOLD CLOSE OUT PANEL IAW SRM 51-21-01, PN 170-27618-001. ACFT REMAINS UNTIL HEAVY CHECK IS COMPLETED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,039 hrs · 20,256 cycles

CREW REPORTED THAT THE EMERGENCY LIGHT STRIP AT ROW 1 WAS INOPERATIVE. MAINTENANCE R & R EMERGENCY LIGHT STRIP AT ROW 1 IAW AMM AND OPS CHECKED GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION (TE FLAPS) · airframe 26,966 hrs · 20,196 cycles

AFTER SELECTING FLAPS FROM 2 TO 3 CREW RECEIVED A FLAPS FAIL MESSAGE. CREW RAN QRH AND DECLARED AN EMERGENCY. LANDED AND TAXIED TO GATE WITHOUT INCIDENT. MAINTENANCE FOLLOWED FIM 27-51-00-810-802-A AND CLEARED INHIBITS IAW AMM AND ACFT, OPS CHECKED GOOD.

Part: STIFFENER — CRACKED (RT NACELLE) · airframe 25,560 hrs · 19,069 cycles

DURING HEAVY CHECK, RT PYLON STIFFENER ON OTBD SIDE CRACKED, MX R & R STIFFENER IAW SRM 51-43-02, 51-41-02.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 25,560 hrs · 19,069 cycles

DURING HEAVY CHECK, AREA BETWEEN FWD AND AFT SECTION OF GALLEY HAS CORROSION. MX R & R ALL CORRODED PIECES ON AFT GALLEY WHERE 2 HALVES MEET IAW AMM 25-00-23, 25-00-05, P/N 170-59522-001, TRIM.

Part: LEAF SPRING — CORRODED (ZONE 800) · corrosion level 2 · airframe 25,560 hrs · 19,069 cycles

DURING HEAVY CHECK LEAF SPRING AND NUT R1 DOOR NR 4 FWD STOP FITTING AND NUT NR 3 FWD STOP FITTING ARE CORRODED. MX R & R LEAF SPRING AND NUT R1 DOOR NR 4 FWD STOP FITTING AND NUT NR 3 FWD STOP FITTING IAW AMM 52-41-23.

Part: SPRING — CORRODED (SERVICE DOOR) · corrosion level 2 · airframe 25,560 hrs · 19,069 cycles

DURING HEAVY CHECK, FOUND LEAF SPRING AND NUT AT NR 3 AND 4 FWD STOP FITTING ON R1 DOOR CORRODED. MX R & R LEAF SPRINGS IAW AMM 52-11-23.

Part: STOP — CORRODED (SERVICE DOOR) · corrosion level 2 · airframe 25,560 hrs · 19,069 cycles

DURING HEAVY CHECK, FOUND THE LOWEST TWO DOOR STOPS ON FWD SERVICE DOOR FWD EDGE CORRODED. MAINTENANCE R & R DOOR STOPS HARDWARE IAW AMM 52-41-23.

Part: DOOR FRAME — GOUGED (SERVICE DOOR) · airframe 25,560 hrs · 19,069 cycles

DURING HEAVY CHECK, FWD SERVICE DOOR AFT OF FRAME 17 AFT DOOR FRAME GOUGED. MAINTENANCE R & R IAW SRM 51-41-02.

Part: CLAMP — CORRODED (HYD LINE) · corrosion level 2 · airframe 25,560 hrs · 19,069 cycles

DURING HEAVY CHECK, FOUND CORROSION BETWEEN HORZIONAL STAB LT AND RT RIBS 1 & 2 THERE ARE SEVERAL HYDRAULIC LINE CLAMPS AND HARDWARE CORRODED. MAINTENANCE R & R ADEL CLAMPS AND HARDWARE IAW AMM 20-10-01, PN PE2701RE6E.

Part: NUT — CORRODED (ZONE 800) · corrosion level 2 · airframe 25,560 hrs · 19,069 cycles

DURING HEAVY CHECK, L1 DOOR STOP SCREW NUT ON DOOR STOP FITTINGS NR 3, & 4 SHOW SIGNS OF CORROSION. MX R & R L1 DOOR STOP SCREW NUT ON DOOR STOP FITTING IAW AMM 20-10-02.

Part: CLAMP — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 25,560 hrs · 19,069 cycles

DURING HEAVY CHECK, FOUND BETWEEN RIBS 1 AND 2 LT AND RT HORIZONAL STAB THERE ARE SEVERAL HARNESS ADEL CLAMPS AND HARDWARE CORRODED. MX R & R ADEL CLAMPS AND HARDWARE BETWEEN RIBS 1 AND 2 LT AND RT HORIZONAL STABILIZER IAW AMM 20-10-01.

Part: WASHER — CORRODED (FLAP TRACK) · corrosion level 2 · airframe 25,560 hrs · 19,069 cycles

DURING HEAVY CHECK FOUND RT WING NR 3 MIDDLE, FLAP TRACK SUPPORT FWD ATTACHMENT TO WING HARDWARE CORRODED. MX R & R RT WING NR 3, MIDDLE, FLAP TRACK SUPPORT FWD ATTACHMENT TO WING HARDWARE, PN 170-18284-001, MS24665-319, MS14145L8 IAW AMM 57-57-31.

Part: BOLT — CORRODED (ZONE 500) · corrosion level 2 · airframe 25,560 hrs · 19,069 cycles

DURING HEAVY CHECK, LT WING SPOILER ACTUATORS NR 4, & 5 INBD-OTBD HARWARE IS CORRODED. MX R & R LT WING SPOILER ACTUATOR HARWARE IAW AMM 27-65-01. PN NAS6121-31D, BOLT.

Part: PANEL — CRACKED (APU BAY) · airframe 25,560 hrs · 19,069 cycles

DURING HEAVY CHECK, PANEL 351BZ CORNERS ARE CRACKED. MAINTENANCE TRIMED OUT DAMAGE WITH NO REINENFORCEMENT INSTALLATION ON PANEL 351BZ, HFEC NO CRACKS NOTED IAW SRM 53-31-21.

Part: DOOR — CORRODED (WASTE WATER) · corrosion level 2 · airframe 25,560 hrs · 19,069 cycles

DURING HEAVY CHECK, WASTE WATER DOOR INSIDE HAS CORROSION. MX R & R WASTE WATER DOOR IAW AMM 53-03-60. PN 170-86668-403 PANEL.

Part: SUPPORT — CORRODED (TE FLAP TRACK) · corrosion level 2 · airframe 25,560 hrs · 19,069 cycles

DURING HEAVY CHECK, LT WING NR 3 MIDDLE FLAP TRACK SUPPORT FWD ATTACHMENT TO WING HARDWARE IS CORRODED. MX R & R LT WING 3 MIDDLE FLAP TRACK SUPPORT FWD ATTACHMENT TO WING HARDWARE IAW AMM 57-57-31.

Part: BOLT — CORRODED (ZONE 600) · corrosion level 2 · airframe 255 hrs · 19,069 cycles

DURING HEAVY CHECK, RT WING SPOILER ACTUATORS NR 4, & 5 INBD AND OTBD HARDWARE IS CORRODED. MX R & R HARDWARE IAW AMM 27-65-01.

Part: BRACKET — CRACKED (ZONE 100) · airframe 25,560 hrs · 19,069 cycles

DURING HEAVY CHECK BRACKET ON FUSELAGE PANEL 195ER IS CRACKED. MX R & R BRACKET ON FUSELAGE PANEL 195ER IAW SRM 51-41-01, PN 170-15840-003 PROFILE.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 25,560 hrs · 19,069 cycles

DURING HEAVY CHECK, INBD RIB OF LT L/E OF HORIZONTAL STAB IS CRACKED. MAINTENANCE REMOVED DAMAGED SECTION OF RIB FABRICATED AND INSTALLED.

Part: BRACKET — CORRODED (LAVATORY) · corrosion level 2 · airframe 25,560 hrs · 19,069 cycles

DURING HEAVY CHECK, AFT LAV TOILET BOWL MOUNTING BRACKET AND HARDWARE IS CORRODED. MX R & R AFT LAV TOILET BOWL MOUNTING BRACKET AND HARDWARE IAW CMM 25-42-03, PN 170-43685-001 DOUBLER.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 25,560 hrs · 19 cycles

DURING HEAVY CHECK, RT HORIZONTAL STAB L/E HAS RIB ON INBD SIDE CRACKED. MX CUT OUT DAMAGE INSTALLED FILLER AND DOUBLER IAW ETD 2014-170-045417.

Part: DOOR — LACK OF LUBE (L1) · airframe 23,686 hrs · 17,682 cycles

CREW REPORTED THAT THE L1 DOOR IS HARD TO OPEN FROM THE OUTSIDE. MX LUBED L1 DOOR AND PERFORMED OPS TEST IAW AMM. DOOR OPS CHECK GOOD.

Part: GLOWSTRIP — LOOSE (CABIN) · airframe 23,365 hrs · 17,435 cycles

CREW REPORTED THAT THE PHOTO LUMINESCENT STRIP JUST AFT OF THE FRONT GALLEY IS LOOSE. MX REINSTALLED PHOTO LUMINESCENT STRIP IAW AMM AND OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (FLASHLIGHT) · airframe 22,826 hrs · 17,015 cycles

CREW REPORTED THAT THE CAPTAINS FLASHLIGHT WAS INOP. MAINTENANCE REMOVED AND REPLACED FLASHLIGHT BULB PER EMB AMM 33-51-01, OPS CHECKED GOOD.

Part: GLOWSTRIP — UNSECURE (CABIN) · airframe 22,351 hrs · 16,645 cycles

CREW DISCOVERED PHOTO LUMINESCENT STRIP COMING UP AT ROW 18, SEATS D & F. MAINTENANCE RE-INSTALLED STRIP PER EMB AMM 33-50-2 AND OPS CHECKED GOOD.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 22,290 hrs · 16,602 cycles

WHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND SUPPORT BRACKET AT FRAME 86 BROKEN. MAINTENANCE REMOVED AND REPLACED THE BRACKET AT FRAME 86 IAW EMB 170 SRM 51-41-01. THE AIRCRAFT IS OUT OF SERVICE IN HEAVY CHECK.

Part: BEAM — CRACKED (FUSELAGE) · airframe 22,290 hrs · 16,602 cycles

WHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND BEAM CRACKED FOR OUTBOARD TCAS MOUNTING BRACKET. MAINTENANCE REMOVED AND REPLACED BEAM IAW EMB 170 SRM 51-41-01, 51-40-02, AND 51-43-01. THE AIRCRAFT IS OUT OF SERVICE IN HEAVY CHECK.

Part: RIB — CRACKED (LT WING) · airframe 22,290 hrs · 16,602 cycles

WHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND THE LEFT WING RIB 10 CRACKED. MAINTENANCE REMOVED AND REPLACED THE LEFT WING RIB 10 IAW EMB 170 SRM 51-40-02, 51-43-01, AND 51-43-02. "MAJOR REPAIR", THE AIRCRAFT IS OUT OF SERVICE IN HEAVY CHECK.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,290 hrs · 16,602 cycles

WHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND THE RIGHT SHEAR PLATE AT FRAMES 87 TO 88 CORRODED. MAINTENANCE REMOVED AND REPLACED THE RIGHT SHEAR PLATE AT FRAMES 87 TO 88 IAW EMB 170 SRM 51-42-02, 51-42-01, AND 51-43-03. THE AIRCRAFT IS OUT OF SERVICE IN HEAVY CHECK.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,290 hrs · 16,602 cycles

WHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND LEFT SEAT TRACK AT FRAME 88 CORRODED. MAINTENANCE REMOVED AND REPLACED THE LEFT SEAT TRACK AT FRAME 88 IAW EMB 170 SRM 51-40-02, 51-43-03, AND 51-42-01. THE AIRCRAFT IS OUT OF SERVICE IN HEAVY CHECK.

Part: PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,290 hrs · 16,602 cycles

WHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND THE CENTER SHEAR PANEL FRAMES 87 TO 88 CORRODED. MAINTENANCE REMOVED AND REPLACED THE CENTER SHEAR PANEL FRAMES 87 TO 88 IAW EMB 170 SRM 51-42-01. THE AIRCRAFT IS OUT OF SERVICE IN HEAVY CHECK.

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,290 hrs · 16,602 cycles

WHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND THE RIGHT GUSSET PLATE AT FRAME 90 CORRODED. MAINTENANCE REMOVED AND REPLACED RIGHT GUSSET PLATE AT FRAME 90 IAW EMB 170 SRM 51-40-02, AND 51-41-02. THE AIRCRAFT IS OUT OF SERVICE IN HEAVY CHECK.

Part: STOP FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,290 hrs · 16,602 cycles

WHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND THE LOWER STOP ON L2 DOOR CUTOUT CORRODED. MAINTENANCE REMOVED AND REPLACED STOP IAW EMB 170 AMM 53--23-21. THE AIRCRAFT IS OUT OF SERVICE IN HEAVY CHECK.

Part: CLAMP — CRACKED (AC BAY) · airframe 22,290 hrs · 16,602 cycles

WHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND THE RIGHT ACM INLET DUCT SUPPORT CLAMP CRACKED. MAINTENANCE REMOVED AND REPLACED THE RIGHT ACM INLET DUCT CLAMP SUPPORT IASW EMB 170 SRM 51-41-01, AND 51-40-02. THE AIRCRAFT IS OUT OF SERVICE IN HEAVY CHECK.

Part: DAMPENER — CORRODED (L2 DOOR) · corrosion level 2 · airframe 22,290 hrs · 16,602 cycles

WHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND THE L2 DOOR DAMPNER CORRODED. MAINTENANCE REMOVED AND REPLACED THE L2 DOOR DAMPNER IAW EMB 170 AMM 52-12-27. THE AIRCRAFT IS OUT OF SERVICE IN HEAVY CHECK.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,290 hrs · 16,602 cycles

WHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND THE LEFT SHEAR PLATE AT FRAMES 87 AND 88 CORRODED. MAINTENANCE REMOVED AND REPLACED THE LEFT SHEAR PLATE AT FRAMES 87 AND 88 IAW EMB 170 51-40-02, 51-42-01, AND 51-43-01. THE AIRCRAFT IS OUT OF SERVICE IN HEAVY CHECK.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,290 hrs · 16,602 cycles

WHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND THE RIGHT PANEL SUPPORT AFT OF R2 DOOR CORRODED. MAINTENANCE REMOVED AND REPLACED THE PANEL SUPPORT AFT OF THE R2 DOOR IAW EMB 170 SRM 51-40-02, 51-42-01, AND 51-43-01. THE AIRCRAFT IS OUT OF SERVICE IN HEAVY CHECK.

Part: SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,290 hrs · 16,602 cycles

WHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND THE LEFT SHEAR PLATE SPLICE AT FRAMES 87 AND 88 CORRODED. MAINTENANCE REMOVED AND REPLACED THE LEFT SHEAR PLATE SPLICE AT FRAMES 87 AND 88 IAW EMB 51-40-02, AND 51-42-02. THE AIRCRAFT IS OUT OF SERVICE IN HEAVY CHECK.

Part: STRUCTURE — CORRODED (LAVATORY) · corrosion level 2 · airframe 22,290 hrs · 16,602 cycles

WHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND THE AFT WASTE BOX CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFT WASTE BOX IAW EMB 170 SB 170-53-0095. THE AIRCRAFT IS OUT OF SERVICE IN HEAVY CHECK.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 22,267 hrs · 16,583 cycles

EN ROUTE FROM PHL TO CYHZ, CREW REPORTED A LOUD BANG WAS HEARD. CAPTAIN NOTICED THAT HIS WINDSHIELD WAS SHATTERED AND RETURNED TO PHL WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED WINDSHIELD PER EMB AMM AND OPS CHECKED GOOD.

Part: GIRT BAR — LOOSE (L1 DOOR) · airframe 20,932 hrs · 15,583 cycles

CREW REPORTS UNABLE TO ARM L1 DOOR AND IT APPEARS THAT THE FWD PART OF THE GIRT BAR IS HANGING DOWN A BIT. MAINTENANCE RE-SECURED GIRT BAR, OPS CHECK GOOD.

Part: GIRT BAR — UNSECURE (L1 DOOR) · airframe 20,392 hrs · 15,142 cycles

CREW REPORTED L1 DOOR HARD TO CLOSE. MAINTENANCE RE-SECURED L1 DOOR GIRT BAR PER EMB AMM, OPS CHECK GOOD.

Part: GIRT BAR — LOOSE (L1 DOOR) · airframe 19,956 hrs · 14,815 cycles

CREW REPORTED L-1 DOOR WOULDN'T ARM PROPERLY. MAINTENANCE RE-SECURED L-1 DOOR GIRT BAR PER EMB AMM, OPS CHECK GOOD.

Part: GIRT BAR — DISLODGED (L1 DOOR) · airframe 19,647 hrs · 14,571 cycles

L1 DOOR WOULD NOT ARM. MAINTENANCE FOUND BUSTLE PIN LANYARD TANGLED IN GIRT BAR FITTING AND GIRT BAR DISLODGED FROM SPRING CLIP. MAINTENANCE RE-SECURED BUSTLE PIN AND GIRT BAR IAW EMB AMM, DOOR OPS CHECK GOOD.

Part: PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,486 hrs · 14,452 cycles

WHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND 5 BONDING PLATES ON 195 AL DOOR PANEL CORRODED. MAINTENANCE REMOVED AND REPLACED DOOR PANEL 195AL IAW EMB 170 AMM 53-04-50. AIRCRAFT WAS RELEASED FROM HEAVY CHECK ON 12/31/2011.

Part: SKIN — DENTED (HORIZ STAB) · airframe 19,485 hrs · 14,451 cycles

WHILE AIRCRAFT WAS IN FOR HEAVY CHECK, MAINTENANCE FOUND A DENT ON THE UPPER LT HORIZ STAB SKIN. (REF: DMI 075393/2). MAINTENANCE PERFORMED A MAJOR REPAIR TO THE UPPER LT HORIZ STAB SKIN IAW EMB 170 SRM 50-10-01, 55-10-01, 51-23-06, 51-41-02, 51-21-03 AND EMB ETD 2011-170-109960. FABRICATED FILLER MADE OF 2024-T3, .040 REF PO #024093 AND DOUBLER MADE OF 2024-T3, .050 REF PO #019339. AIRCRAFT IS CURRENTLY STILL OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: HINGE — OBSTRUCTED (L1 DOOR) · airframe 19,320 hrs · 14,323 cycles

CREW REPORTED MAIN CABIN DOOR WAS DIFFICULT TO CLOSE. MAINTENANCE REMOVED DEBRIS FROM FWD PASSENGER DOOR LINING FLAP HINGE AND PERFORMED OPS CHECK OF L-1 DOOR PER EMB AMM, OPS CHECK GOOD.

Part: STRUCTURE — DAMAGED (VERTICAL STAB) · airframe 19,198 hrs · 14,234 cycles

*** MAJOR REPAIR *** MAINTENANCE PERFORMED MAJOR REPAIR TO TOP OF VERTICAL STABILIZER PER EMB ETD 2011-170-107849.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 18,676 hrs · 13,843 cycles

MAINTENANCE PERFORMED MAJOR REPAIR TO LT SIDE OF CENTER FUSELAGE AT FR 25, STR 16L PER EMB ETD 2011-170-102287.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,315 hrs · 12,765 cycles

WHILE THE AIRCRAFT WAS IN FOR HEAVY CHECK LEVEL 2 CORROSION AND GOUGES FOUND ON RIGHT INBOARD SEAT TRACK CF3 IN 10 SPOTS. MAINTENANCE REMOVED AND REPLACED THE RIGHT INBOARD SEAT TRACK CF3 IAW SRM 51-40-00. THE AIRCRAFT REMAINS IN HEAVY CHECK CMH FOR COMPLETION. FCS NOT AFFECTED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,315 hrs · 12,765 cycles

WHILE AIRCRAFT WAS IN FOR HEAVY CHECK, LEVEL 2 CORROSION WAS FOUND ON THE RIGHT I/B SEAT TRACK, PAX CABIN CF1. MAINTENANCE REMOVED AND REPLACED THE RT INBOARD SEAT TRACK PAX CABIN CF1 IAW EMB 170 SRM 51-43-01, 51-43-02, 51-43-03 & 51-43-04. A/C IS CURRENTLY STILL OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 16,580 hrs · 12,172 cycles

AC N807MD HAS A MAJOR REPAIR BEING ACCOMPLISHED. DAMAGE IS FROM A PREVIOUS BIRD STRIKE ON THE RT FORWARD FUSELAGE SKIN, BETWEEN FRAMES 4 AND 5, STRINGERS 12R AND 11R. DAMAGE MEASURED AT 3.25" X 3.90" X .050. ENGINEERING ISSUED A ENGINEERING ORDER TO REPLACE THE FUSELAGE SKIN PANEL. MAINTENANCE REMOVED AND REPLACED THE SKIN PANEL PER THE ENGINEERING ORDER AND THE EMB SRM.

Part: BATTERY — DISCHARGED (COCKPIT) · airframe 15,922 hrs · 11,630 cycles

CREW REPORTED COCKPIT EMERGENCY LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PER EMB AMM. A/C WAS THEN RETURNED TO SERVICE.

Part: SLIDE — FAILED (R1 DOOR) · airframe 15,356 hrs · 11,157 cycles

MX REPORTED R-1 DOOR FAILED IT'S OPS CHECK. MAINTENANCE REMOVED AND REPLACED THE R-1 DOOR SLIDE PER EMB AMM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 14,854 hrs · 10,752 cycles

WHILE AC WAS IN FOR HEAVY CHECK, LEVEL TWO CORROSION WAS FOUND ON LT FLOORBEAM BETWEEN FR 86 AND FR 87. MAINTENANCE REMOVED AND REPLACED FLOORBEAM PER EMB SRM. AC WAS RELEASED AFTER THE COMPLETION OF THE HEAVY CHECK.

Part: BATTERY — DISCHARGED (CABIN) · airframe 14,780 hrs · 10,690 cycles

MAINTENANCE REPORTS EMERGENCY EXIT LIGHT WAS OUT. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT PER EMB AMM.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 14,587 hrs · 10,531 cycles

CREW REPORTED ELECTRICAL BURNT SMELL IN THE COCKPIT WHILE ON APPROACH INTO PHL. A/C LANDED WITHOUT EVENT AT PHL, MAINTENANCE WAS DISPATCHED TO THE AIRCRAFT AND WAS UNABLE TO DUPLICATE THE ODOR. A/C WAS THEN RETURNED TO SERVICE.

Part: CONNECTOR — BURNED (TAT SENSOR)

CREW DETECTED ODOR SMOKE IN THE COCKPIT FOLLOWED QRH PROCEDURES DECLARED AN EMERGENCY, AND LANDED WITHOUT INCIDENT. MAINT TROUBLESHOT PROBLEM, FOUND THE TOTAL AIR TEMPERATURE CONNECTOR BURNED. REMOVED AND REPLACED CONNECTOR AND TAT SENSOR AS A PRECAUTION, OPERATIONAL CHECK OF SYSTEM CHECKED GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (K)

Part: PUMP — LEAKING (NR 2 HYD SYSTEM)

BNA FLT 1647, EN ROUTE DCA TO BNA - ABOUT 50 MILES FROM BNA, THE NR 2 HYDRAULIC SYSTEM QUANTITY DROPPED TO ZERO. THE FLIGHT CREW FOLLOWED THE QRH PROCEDURES, WHICH INCLUDED AN ALTERNATE GEAR EXTENSION. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 2 ENGINE HYDRAULIC PUMP. OPERATIONALLY CHECKS OK.

Part: COMPUTER — FAILED (FADAC)

PIT - ENGINE NR 1 FADEC REMOVED FOR TROUBLESHOOTING FOR ENGINE NR 1 FADEC FAULT. MAINTENANCE REPLACED NR 1 ENGINE FADAC. (M)