N856RW

Part: POWERPACK — INOPERATIVE (ZONE 100 EMER LT) · airframe 41,977 hrs · 25,200 cycles

EMERGENCY LIGHTS, WHEN TURNED ON, DON'T ILLUMINATE IN THE FORWARD CABIN. EMERGENCY LIGHT FAULT. R & R FWD LT EMERGENCY LIGHT POWER UNIT, IAW AMM 33-50-01.

Part: DOOR — OUT OF ADJUST (L1) · airframe 41,226 hrs · 24,647 cycles

L1 DOOR DIFFICULT TO OPEN FROM THE OUTSIDE. PERFORMED ADJUSTMENT AND TEST OF L1 DOOR.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,644 hrs · 23,663 cycles

DURING HEAVY CHECK MAINTENANCE FOUND CORRODED SHEAR CLIP FR 17 STR 27-28R. REMOVED AND REPLACED SHEAR CLIP AT FR17 STR 28R-27R REF SRM 51-40-08, APPLIED SURFACE PROTECTION TO SHEAR CLIP AT FR 17 STR 27-28R REF SRM 51-23-06 PAINT AND CPM 51-25-00. A/C REMAINS IN CHECK

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,644 hrs · 23,663 cycles

DURING HEAVY CHECK MAINTENANCE FOUND CORRODED SHEAR CLIP FR 17 STR 26-27 L. REMOVED AND REPLACED SHEAR CLIP FR17 STRG 26-27 L. REF: SRM 51-21-01, SRM 51-40-08. APPLIED SURFACE PROTECTION TO SHEAR CLIP FR 17 STR 26-27 L. REF: SRM 51-23-05,SRM 51-23-06, CPM 51-25-00. A/C REMAINS IN CHECK

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 39,644 hrs · 23,663 cycles

DURING HEAVY CHECK MAINTENANCE FOUND RT HORIZONTAL STAB RIB 10A FORWARD UPPER ANGLE CRACKED. REMOVED AND REPLACED RIB 10 RT HORIZONTAL STABILIZER BETWEEN FRONT AND MID-SPARS REF SRM 51-40-08, 51-23-05, 51-23-06. A/C REMAINS IN CHECK.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 39,644 hrs · 23,663 cycles

DURING HEAVY CHECK MAINTENANCE FOUND RT HORIZONTAL STAB RIB 11A FORWARD UPPER ANGLE CRACKED. REMOVED, REPAIRED AND REPLACED RIB 11A RT HORIZONTAL STABILIZER BETWEEN FRONT AND MID SPARS REF SRM 51-40-08, ETD2019-170-118232. A/C REMAINS IN CHECK.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,644 hrs · 23,663 cycles

DURING HEAVY CHECK MAINTENANCE FOUND CORRODED SHEAR CLIP FR 17 STR 27-28 L. REMOVED AND REPLACED SHEAR CLIP FROM FR 17 STR 27-28 L. REF: SRM 51-21-01,SRM 51-40-08, APPLIED SURFACE PROTECTION TO SHEAR CLIP AT FR 17 STRG 27-28 L REF SRM 51-23-06. A/C REMAINS IN CHECK.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,644 hrs · 23,663 cycles

DURING HEAVY CHECK MAINTENANCE FOUND CORRODED SHEAR CLIP FR 17 STR 25-26 R. REMOVED AND REPLACED SHEAR CLIP FOR FR17 STR 25-26 R. REF: SRM 51-21-01, SRM 51-40-08., APPLIED SURFACE PROTECTION TO SHEAR CLIP AT FR 17 STR 25-26 R REF SRM 51-23-06 PAINT AND CPM 51-25-00. A/C REMAINS IN CHECK.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,644 hrs · 23,663 cycles

DURING HEAVY CHECK MAINTENANCE FOUND CORRODED SHEAR CLIP @ FR89 ST21L-23L. REMOVED AND REPLACED SHEAR CLIP @ FR89 ST21L-23L. REF: SRM 51-21-01.SRM 51- 40-08,51-23-06. A/C REMAINS IN CHECK

Part: RIB — CRACKED (LT WING) · airframe 39,644 hrs · 23,663 cycles

DURING HEAVY CHECK MAINTENANCE FOUND LT WING LE RIB FRAME 18 CRACKED. REMOVED AND REPLACED LT WING RIB FRAME 18. REF SRM 51-40-08. A/C REMAINS IN CHECK.

Part: BEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 39,644 hrs · 23,663 cycles

DURING HEAVY CHECK MAINTENANCE WHILE PERFORMING L1 DOOR LOWER BEAM REWORK CORROSION FOUND AT FWD AND AFT GIRT BAR FITTING ATTACHMENT AREAS. REMOVED AND REPLACED L1 DOOR LOWER BEAM REF SRM 51-40-08, 51-23-06. A/C REMAINS IN CHECK.

Part: SEAT TRACK — CORRODED (FRAMES 34-74) · corrosion level 2 · airframe 39,644 hrs · 23,663 cycles

**WHILE IN HEAVY CHECK** MAINTENANCE FOUND LEVEL 2 CORROSION IN A FEW LOCATIONS ON THE RH INBD (FLOOR) SEAT-TRACK FR 34/43 THRU 59/74 (P/N 170-99451-003). MAINTENANCE REMOVED AND REPLACED RH INBD (FLOOR) SEAT-TRACK FR 34/43 THRU 59/74 PER SRM 51-40-08. SEE EAMS W/O H6948 SN 00506. AIRCRAFT REMAINS IN HEAVY CHECK DURING THE DURATION OF THE CHECK.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,644 hrs · 23,663 cycles

DURING HEAVY CHECK MAINTENANCE FOUND BUBBLED PAINT AND EVIDENCE OF CORROSION AT AIRCRAFT DATA PLACARD ON REAR FUSELAGE LOWER SKIN. PERFORMED PERMANENT REPAIR OF REAR FUSELAGE SKIN AT AIRCRAFT DATA PLACARD BY THE WAY OF CUTTING OUT DAMAGE AND FABRICATING AND INSTALLING REPAIR DOUBLER IAW ETD2019-170-117637. A/C REMAINS IN CHECK

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,644 hrs · 23,663 cycles

DURING HEAVY CHECK MAINTENANCE FOUND LT INBD (FLOOR) SEAT-TRACK FR 34/43 THRU 59/74 (P/N 170-02064-011) HAS SPOT(S) OF CORROSION. REMOVED AND REPLACED LT INBD (FLOOR) SEAT-TRACK FR 34/43 THRU 59/74 (P/N 170-02064-011) REFER SRM 51-40-08. APPLIED SURFACE PROTECTION TO FASTENERS AT LT SEAT TRACK FR 34/43 THRU 59/74 PER SRM 51-23-06. A/C REMAINS IN CHECK.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,644 hrs · 23,663 cycles

DURING HEAVY CHECK MAINTENANCE FOUND CORROSION ON 3 EA LOWER ANGLES ON PANEL 1431DL. REMOVED AND REPLACED 3 EA LOWER ANGLES ON PANEL 1431DL REF SRM 51-45-00. A/C REMAINS IN CHECK.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 39,640 hrs · 23,660 cycles

EMERGENCY LIGHT INOP, 4TH LIGHT OVER AISLE. TROUBLESHOT EMERGENCY LIGHT #4 BETWEEN SEAT 15 ABCD CONNECTION, PLUGS, AND GROUND IAW WM 33-21-53, OPS CHECK GOOD.

Part: POWER SUPPLY — FAULTY (EMERGENCY LIGHTS) · airframe 39,570 hrs · 23,615 cycles

FOURTH OVERHEAD EMERGENCY CEILING LIGHT OUT. R&R EMERGENCY LIGHT POWER UNIT, OPS CHECK GOOD IAW AMM 33-50-01.

Part: POWER SUPPLY — FAULTY (EMERGENCY LIGHTS) · airframe 39,550 hrs · 23,603 cycles

4TH EMERGENCY LIGHT FROM FRONT TO BACK IS INOP. R&R EMERGENCY LIGHT POWER UNIT IAW AMM 33-50-01.

Part: POWER SUPPLY — FAULTY (EMERGENCY LIGHTS) · airframe 39,548 hrs · 23,602 cycles

OVERHEAD EMERGENCY LIGHT, 2ND LIGHT BACK, NOT WORKING. R&R FWD EMERGENCY LIGHT POWER UNIT REF MM 33-50-01.

Part: ENGINE — VIBRATION (NR 1) · airframe 37,659 hrs · 22,451 cycles

ON CLIMB OUT THROUGH FL150 E1 STARTED VIBRATING, N1 WENT TO 0% AND ITT WENT RED TO 1008 FOR A COUPLE SECONDS WITH HIGH VIBE 4.1 FOR 2 SECONDS. CREW PERFORMED ENGINE FIRE SEVERE DAMAGE QRC PROCEDURE AND SECURED MOTOR AND FIRED #1 BOTTLE. DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. R&R E1, LEAK AND OPS CHECK GOOD.

Part: SKIN — DENTED (FRAMES 10-11) · airframe 37,542 hrs · 22,375 cycles

***WHILE AIRCRAFT WAS IN FOR C-CHECK*** MAINTENANCE REPORT DENTS BELOW PILOT'S WINDOW BETWEEN FR 10 & 11, STR 14L & 15L. MAINTENANCE PERFORMED A MAJOR REPAIR TO DENTS BELOW PILOT'S WINDOW BETWEEN FR 10 & 11, STR 14L & 15L IAW EMBRAER ETD2018-170-084906. REF AAR N/R 6705889 FOR DETAILS.

Part: SKIN — CRACKED (LT WING) · airframe 34,069 hrs · 20,215 cycles

MAINTENANCE REPORTED A CRACK 0.8 INCH, ON THE LT WING LOWER FRONT SKIN INBD OF RIB 17. MAINTENANCE PERFORMED A MAJOR REPAIR TO THE LT WING LOWER FRONT SKIN IAW ETD2017-170-071633, SRM 51-41-02, 51-43-01, 51-43-02, 51-43-04, & 51-23-05.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,069 hrs · 20,215 cycles

WHILE AIRCRAFT WAS IN FOR HEAVY CHECK, MAINTENANCE REPORTED LEVEL 2 CORROSION ON THE LT I/B SEAT TRACK BETWEEN FRAME 28 & 29. MAINTENANCE REMOVED CORROSION AND INSTALLED SPLICE DEVICES AT FRAME 28 AND FRAME 29 (P/N'S 171-00439-005 & 171-00441-003) IAW E170 SRM 51-10-03, 51-23-04, 51-23-05, 51-23-06, 53-21-10 & 53-00-10/REPAIR 02. AIRCRAFT IS CURRENTLY STILL OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,069 hrs · 20,215 cycles

WHILE AIRCRAFT WAS IN FOR HEAVY CHECK, MAINTENANCE REPORTED LEVEL 2 CORROSION ON THE RT I/B SEAT TRACK BETWEEN FRAMES 78 & 82. MAINTENANCE REMOVED AND REPLACED THE RT I/B SEAT TRACK BETWEEN FRAMES 78 & 82 IAW SRM 51-43-03, 53-23-10, 51-40-02 & 51-23-06. AIRCRAFT IS CURRENTLY STILL OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,069 hrs · 20,215 cycles

WHILE AIRCRAFT WAS IN FOR HEAVY CHECK, MAINTENANCE REPORTED LEVEL 2 CORROSION ON THE LT I/B SEAT TRACK BETWEEN FRAME 28 & 29. MAINTENANCE REMOVED CORROSION AND INSTALLED SPLICE DEVICES AT FRAME 28 AND FRAME 29 (P/N'S 171-00439-005 & 171-00441-003) IAW SRM 51-10-03, 51-23-04, 51-23-05, 51-23-06, 53-21-10 & 53-00-10/REPAIR 02. AIRCRAFT IS CURRENTLY STILL OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,069 hrs · 20,215 cycles

WHILE AIRCRAFT WAS IN FOR HEAVY CHECK, MAINTENANCE REPORTED LEVEL 2 CORROSION ON THE LT I/B SEAT TRACK AT FRAME 78. MAINTENANCE REMOVED AND REPLACED THE LT I/B SEAT TRACK AT FRAME 78 IAW SRM 51-43-04, 51-43-03, 51-41-01, 51-40-02 & 51-40-03. AIRCRAFT IS CURRENTLY STILL OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,069 hrs · 20,215 cycles

WHILE AIRCRAFT WAS IN FOR HEAVY CHECK, MAINTENANCE REPORTED LEVEL 2 CORROSION ON THE RT I/B SEAT TRACK BETWEEN FRAMES 23 & 34. MAINTENANCE REMOVED AND REPLACED THE RT I/B SEAT TRACK BETWEEN FRAMES 23 & 34 IAW SRM 51-40-02, 51-41-01, 51-43-02 & 51-43-03. AIRCRAFT IS CURRENTLY STILL OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,069 hrs · 20,215 cycles

WHILE AIRCRAFT WAS IN FOR HEAVY CHECK, MAINTENANCE REPORTED LEVEL 2 CORROSION ON THE RT O/B SIDE OF THE FLOOR SUPPORT CROSS BEAM AT FRAME 84. MAINTENANCE REMOVED AND REPLACED THE RT O/B SIDE OF THE FLOOR SUPPORT CROSS BEAM AT FRAME 84 IAW SRM 51-41-01, 51-40-04, 51-40-03, 51-10-03 & 51-41-02. AIRCRAFT IS CURRENTLY STILL OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,069 hrs · 20,215 cycles

WHILE AIRCRAFT WAS IN FOR HEAVY CHECK, MAINTENANCE REPORTED LEVEL 2 CORROSION ON THE GUSSET AT FRAME 90 AT RBL 25. MAINTENANCE REMOVED AND REPLACED THE GUSSET AT FRAME 90 AT RBL 25 IAW SRM 51-41-02, 51-10-03 & 51-23-06. AIRCRAFT IS CURRENTLY STILL OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: SHEAR PANEL — CORRODED (FRAME 87) · corrosion level 2 · airframe 34,069 hrs · 20,215 cycles

CORROSION WAS FOUND ON THE RT SHEAR PANEL AT FRAME 87. MAINTENANCE REMOVED AND REPLACED THE RT SHEAR PANEL AT FRAME 87 IAW E170 SRM 51-42-01, 51-40-02, 51-10-03 & 53-23-10 AIRCRAFT IS CURRENTLY STILL OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: SKIN — CRACKED (LT WING) · airframe 34,069 hrs · 20,215 cycles

WHILE AIRCRAFT WAS IN FOR HEAVY CHECK, MAINTENANCE REPORTED A CRACK (5/16") ON THE LT WING LEADING EDGE SKIN AT NR 2 SLAT O/B TRACK CUTOUT ON UPPER END. MAINTENANCE REMOVED CRACK FROM THE LT WING LEADING EDGE SKIN AT NR 2 SLAT O/B TRACK CUTOUT ON UPPER END IAW SRM 57-49-01, REPAIR 06. 51-23-04, 51-23-05 & 51-23-06. AIRCRAFT IS CURRENTLY STILL OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: CONNECTOR — LOOSE (LAVATORY PCB) · airframe 32,561 hrs · 19,243 cycles

CREW REPORTED THAT THE SMOKE ALARM INDICATOR LIGHT ON FORWARD RAINBOW INDICATOR PANEL WAS NOT ILLUMINATING WHEN TESTED. MAINTENANCE FOUND FORWARD THE CONNECTOR PLUG ON FORWARD LAV PCB LOOSE. MAINTENANCE ATTACHED THE CONNECTOR IAW AMM AND OPS CHECKED GOOD.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHTS) · airframe 32,417 hrs · 19,145 cycles

CREW REPORTED THAT THE EMERGENCY LIGHT AT ROW 15 DID NOT ILLUMINATED WITH THE LIGHTS ON. MAINTENANCE FOUND EMERGENCY LIGHT CONNECTOR AT ROW 15 LOOSE, SECURED IAW AMM AND OPS CHECKED GOOD.

Part: STRUT — UNDERSERVICED (NLG) · airframe 32,417 hrs · 19,145 cycles

DURING FLIGHT, CREW RECEIVED A LANDING GEAR DISAGREE MESSAGE AND THE GEAR WOULD NOT RETRACT. CREW RETURNED TO DEPATURE AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NLG SHOCK STRUT UNDER SERVICED. MAINTENANCE SERVICED STRUT SERVICE AND PERFORMED STRUT EXTENSION AND RETRACTION CHECK IAW AMM AND OPS CHECKED GOOD.

Part: FLAP — OUT OF ADJUST (L2 DOOR) · airframe 32,040 hrs · 18,909 cycles

CREW REPORTED THAT THE L2 DOOR LOCK INDICATOR WAS NOT SHOWING GREEN WHEN LOCKED. MAINTENANCE ADJUSTED VENT FLAP PER EMB AMM AND OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 32,018 hrs · 18,894 cycles

MAINTENANCE REPORTED THAT THE LIGHT OVER ROW 23 WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY BATTERY IAW AMM AND OPS CHECKED GOOD.

Part: WARNING LIGHT — FALSE INDICATION (L2 DOOR) · airframe 31,893 hrs · 18,805 cycles

CREW REPORTED THAT THE L2 DOOR SHOWED OPEN. MAINTENANCE INSPECTED L2 DOOR IAW AMM AND FOUND NO DEFECTS. AIRCRAFT IS GOOD FOR SERVICE.

Part: WARNING MESSAGE — FALSE ACTIVATION (PAX DOOR) · airframe 31,737 hrs · 18,705 cycles

CREW RECEIVED A MESSAGE THAT THE AFT DOOR PAX WAS OPEN. FLIGHT ATTENDANTS REPORTED LOCK INDICATIONS WERE NORMAL AND PRESSURIZATION WAS NORMAL. AN EMERGENCY WAS NOT DECLARED AND CREW LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED OPS CHECK OF THE L2 DOOR IAW AMM AND OPS CHECKED GOOD.

Part: PROCESSOR — FAILED (NR 1 MAU) · airframe 31,304 hrs · 18,409 cycles

AVIONICS MAU 1A FAILED ON APPROACH. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. R & R THE PROCESSOR 1 IN MAU 1 IAW AMM 31-41-04.

Part: WARNING LIGHT — FALSE ACTIVATION (L2 DOOR) · airframe 31,165 hrs · 18,319 cycles

DURING CLIMB, MESSAGE PAX OPEN ON EICAS L2 DOOR SHOWING OPEN. FA VERIFIED INDICATIONS AND PRESSURE STAYED STEADY. PERFORMED OPS CHECK OF L2 DOORS IAW AMM 52-72-21. OPS CHECK GOOD.

Part: LENS — MISSING (EXIT SIGN) · airframe 31,018 hrs · 18,225 cycles

FWD R1 DOOR CEILING EMERGENCY EXIT SIGN COVER MISSING. FERRIED TO DESTINATION. R & R EMERGENCY EXIT SIGN LENS COVER AS REQUIRED, OPS CHECK GOOD REF AMM 33-50-15.

Part: LIGHT — FADED (CABIN) · airframe 29,978 hrs · 17,597 cycles

EMERGENCY LIGHT STRIP BY CLOSET HAS FADED. R & R THE LIGHT STRIP IAW AMM 33-50-25.

Part: ROLLER — BINDING (L1 DOOR) · airframe 29,978 hrs · 17,597 cycles

L1 DOOR STICKING HARD TO OPEN. R & R ROLLER ON FWD SIDE OF L1 DOOR IAW SRM 51-41-00. OPS CHECK GOOD.

Part: ATTACH FITTING — CRACKED (LT NACELLE) · airframe 29,399 hrs · 17,197 cycles

LT PYLON, INBD AFT ATTACH LINK LUG IS CRACKED. CUTOUT DAMAGE SECTION OF RT CHORD ASSY AND SPLICED IN NEW SECTION OF CHORD ASSY INTO PYLON IAW ETD2015-170-098790.

Part: A/C PACK — ODOR (NR 1) · airframe 28,423 hrs · 16,534 cycles

NR 1 A/C PACK BLOWS NOXIOUS SMOKE ODOR LIKE BURNING MATCHBOOKS. ODOR DISSIPATES WHEN PACKS TURNED OFF. R & R THE NR 1 A/C PACK IAW 21-51-05 AND 21-51-04. OPS CHECKED GOOD.

Part: ACM — FAILED (NR 1) · airframe 28,424 hrs · 16,535 cycles

CABIN ALTITUDE HIGH, TEMPERATURE CONTROL WOULD NOT HOLD EITHER. CABIN TEMP REACHED 28C. DECLARED EMERGENCY, RETURNED TO FIELD, LANDED WITHOUT INCIDENT, FERRIED. R & R ALL PAX CABIN OXYGEN MASKS AND GENERATOR, R & R DAMAGED PBE. R & R ACM AND HEAT EXCHANGER 1.

Part: GUSSET — CORRODED (FRAME 90) · corrosion level 2 · airframe 28,119 hrs · 16,323 cycles

RT GUSSET PLATE FR 90. R & R GUSSET .

Part: HOUSING — CORRODED (ZONE 200) · corrosion level 2 · airframe 28,119 hrs · 16,323 cycles

CORROSION ON SPLICE FLANGE ON DRAIN MAST HOUSING NR 1, FWD SECTION. R & R SUPPORT DOUBLER.

Part: DOOR — CORRODED (WASTE SERVICE) · corrosion level 2 · airframe 28,119 hrs · 16,323 cycles

WASTE SERVICE DOOR HAS CORROSION ON BOTH SIDES. R & R WASTE SERVICE DOOR IAW SRM 51-40-02, AMM 20-10-07, 20-13-21.

Part: SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 28,119 hrs · 16,323 cycles

CORROSION AROUND FASTENER HOLES ALONG ENTIRE LENGTH OF ATTACHMENT FLANGE OF FWD/CENTER BELLY FAIRING LATERAL SUPPORT, FRAME 45. R & R SUPPORT RIB.

Part: SHEAR TIE — CORRODED (FRAME 16) · airframe 28,119 hrs · 16,323 cycles

CORROSION FOUND ON SHEAR TIE AT FRAME 16, STR 27-28L. R & R SHEAR TIE. MAJOR REPAIR.

Part: BRACKET — CORRODED (ZONE 900) · corrosion level 2 · airframe 28,119 hrs · 16,323 cycles

CORROSION ON BRACKET ON WASTE BOX. R & R THE BRACKET.

Part: SHEAR TIE — CORRODED (FRAME 16) · corrosion level 2 · airframe 28,119 hrs · 16,323 cycles

CORROSION, SHEAR TIE AT FRAME 16, STR 28-27R. R & R SHEAR TIE. MAJOR REPAIR.

Part: SHEAR TIE — CORRODED (FRAME 16) · corrosion level 2 · airframe 28,119 hrs · 16,323 cycles

CORROSION ON SHEAR TIE AT FRAME 16, STR 26-27L. R & R SHEAR TIE. MAJOR REPAIR.

Part: FLANGE — CORRODED (ZONE 200) · corrosion level 2 · airframe 28,119 hrs · 16,323 cycles

MULTIPLE AREAS OF CORROSION ON ATTACHMENT FLANGES ON PANEL 195GR. R & R SPLICE.

Part: PANEL — CORRODED (ZONE 200) · airframe 28,119 hrs · 16,323 cycles

FWD CARGO CLOSE AT PANEL HAS AREA OF CORROSION. R & R SUPPORT.

Part: FLOOR SUPPORT — CORRODED (FRAMES 87-88) · corrosion level 2 · airframe 28,119 hrs · 16,323 cycles

CORROSION RT FLOOR SUPPORT SPLICE, FRAMES 87-88. R & R FLOOR SUPPORT.

Part: SUPPORT — CORRODED (FRAMES 86-90) · airframe 28,119 hrs · 16,323 cycles

CORROSION RT PANEL SUPPORT FRAMES 86-90. R & R.

Part: SPLICE — CORRODED (ZONE 200) · corrosion level 2 · airframe 28,119 hrs · 16,323 cycles

MULTIPLE AREAS OF CORROSION ON ATTACHMENT FLANGES ON PANEL 195HL. R & R SPLICE.

Part: UPPER SHEET — CORRODED (FRAMES 85-86) · airframe 28,119 hrs · 16,323 cycles

CORROSION ON LT Y= -10.748" UPPER SHEET FRAMES 85-86. R & R UPPER SHEET.

Part: UPPER SHEET — CORRODED (FRAMES 85-86) · airframe 28,119 hrs · 16,323 cycles

CORROSION ON THE RT Y= +10.748", UPPER SHEET FRAMES 85-86. R & R UPPER SHEET.

Part: SHEAR PLATE — CORRODED (FRAMES 87-88) · corrosion level 2 · airframe 28,119 hrs · 16,323 cycles

CORROSION RT SHEAR PLATE FRAMES 87-88. R & R.

Part: GUSSET — CORRODED (FRAME 90) · airframe 28,119 hrs · 16,323 cycles

CORROSION RT GUSSET PLATE FRAME 90. R & R GUSSET.

Part: DOOR — CORRODED (WASTE SERVICE) · airframe 28,119 hrs · 16,323 cycles

WASTE SERVICE DOOR HAS CORROSION ON BOTH SIDES. R & R WASTE SERVICE DOOR, REF SRM 51-40-02, AMM 20-10-07, 20-13-21.

Part: LIGHT — DIRTY (ZONE 100) · airframe 27,551 hrs · 15,954 cycles

EMERGENCY LIGHTS ARE DULL. CLEANED AND TESTED GOOD IAW AMM 33-50-21.

Part: DEFLECTOR — TORN (L1 DOOR) · airframe 27,518 hrs · 15,934 cycles

DURING DESCENT, THE CREW REPORTED HEARING A POPPING SOUND AND HAVING THE COCKPIT FLOOR VIBRATE. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. FOUND L1 DOOR DEFLECTOR IS TORN. R & R L1 DOOR DEFLECTOR REF AMM 52-11-28.

Part: DOOR — DETACHED (L1) · airframe 27,510 hrs · 15,929 cycles

L1 DOOR CAME OFF TRACK WHILE TRYING TO CLOSE IT. SEQUENCED L1 DOOR IAW AMM 52-11-20. ADJUSTMENT AND TEST OPS CHECKED GOOD.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 27,005 hrs · 15,628 cycles

DURING EMERGENCY LIGHT FUNCTION CHECK, FOUND AFT SERVICE DOOR EXIT IDENTIFIER SIGN INOPERATIVE. R & R AFT SERVICE DOOR EXIT IDENTIFIER SIGN IAW AMM 33-50-15. OPS CHECK GOOD.

Part: ROLL PIN — BROKEN (DOOR LATCH) · airframe 26,618 hrs · 15,381 cycles

IN CRUISE AT FL390, DOOR PAX FWD OPEN EICAS MESSAGE. L1 DOOR INDICATED OPEN ON MFD. THE AFT MOST DOOR LATCH INDICATION SHOWED HALF GREEN. THE FWD 2 INDICATIONS WERE FULL GREEN. FOUND ROLL PIN ON L1 DOOR LATCH INDICATION BROKEN. R & R ROLL PIN ON L1 DOOR LATCH INDICATOR IAW MM 53-10-21. OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,334 hrs · 15,219 cycles

FWD TWO RT EMERGENCY LIGHT INDICATOR STRIPS NOT INDICATING. R & R EMERGENCY LIGHT STRIPS IAW AMM 33-50-01.

Part: WARNING MESSAGE — FALSE ACTIVATION (FWD PAX DOOR) · airframe 25,209 hrs · 14,567 cycles

FWD PAX DOOR OPEN AT 31,000 FT. NO OTHER ABNORMALITIES ASSOCIATED AND PHYSICAL INDICATORS ALL NORMAL ON DOOR. PERFORMED INSPECTION AND ADJUSTMENT OPS TEST IAW AMM 52-11-00. NO DEFECTS NOTED.

Part: INDICATOR — OUT OF ADJUST (L2 DOOR GIRT BAR) · airframe 25,108 hrs · 14,503 cycles

L2 DOOR GIRT BAR INDICATOR OUT OF ADJUSTMENT. ADJUSTED L2 DOOR GIRT BAR INDICATOR IAW CMM 52-12-22. OPS CHECK GOOD.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 23,173 hrs · 13,631 cycles

CORROSION FOUND ON RIGHT FF SEAT TRACK. R & R SEAT TRACK.

Part: SILL — CORRODED (CARGO DOORWAY) · airframe 23,173 hrs · 13,631 cycles

SILL CORRODED BEHIND CENTER TWO LATCH FITTINGS FOR FWD CARGO DOOR. R & R SILL. MAJOR REPAIR

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 23,173 hrs · 13,631 cycles

CORROSION FOUND ON SEAT TRACK, AFT REPAIR DOUBLER. R & R SEAT TRACK.

Part: WARNING MESSAGE — FALSE ACTIVATION (L1 DOOR) · airframe 23,855 hrs · 13,748 cycles

L1 DOOR INDICATION SHOWS OPEN ON MFD IN FLIGHT. PERFORMED OPS CHECK ON L1 DOOR IAW AMM 52-11-00-05. OPS CHECK GOOD.

Part: PIN — UNSECURE (GIRT BAR) · airframe 23,330 hrs · 13,429 cycles

PIN HANGING FROM A CANAL BELOW MAIN CABIN DOOR SLIDE. SECURED GIRT BAR BUSTLE PIN IAW AMM 52-11-41.

Part: CONNECTOR — DETACHED (EMERGENCY LIGHTS) · airframe 23,002 hrs · 13,212 cycles

OVERHEAD EMERGENCY LIGHT IN CABIN INOPERATIVE. ATTACHED EMERGENCY LIGHT CONNECTOR IAW SWPR 20-52-00, OPS CHECKED GOOD.

Part: SENSOR — OUT OF ADJUST (PAX DOOR) · airframe 22,947 hrs · 13,174 cycles

L1 DOOR OPEN INDICATION ABOVE FL200 AND WENT AWAY BELOW 15,000. ADJUSTED FWD PAX DOOR WARNING SENSOR IAW AMM 52-72-20.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 22,938 hrs · 13,167 cycles

CORROSION ON AFT WET AREA RT FLOORBEAM GUSSET. R & R AFT WET AREA RT FLOORBEAM GUSSET.

Part: FLOORBEAM — BROKEN (ZONE 100) · airframe 22,938 hrs · 13,167 cycles

FLOORBEAM AT FR 86 SUPPORT BROKEN OFF. R & R SUPPORT BRACKETS.

Part: SHEAR PLATE — CORRODED (ZONE 100) · airframe 22,938 hrs · 13,167 cycles

CORROSION ON RT SHEAR PLATE FR87-88. R & R RT SHEAR PLATE.

Part: SPAR — CHAFED (ZONE 600) · airframe 22,938 hrs · 13,167 cycles

RT WING HYD LINE FITTING FOR SYS NR 2 PUMP PRESSURE HAS WORN INTO SPAR III FEED THOUGH AFT OF MLG ACTUATOR. R & R FABRICATED REPAIR BUSHING IAW ETD 2013-170-012216. MAJOR REPAIR.

Part: DOUBLER — CORRODED (SEAT TRACK) · corrosion level 2 · airframe 22,938 hrs · 13,167 cycles

CORROSION ON DOUBLER, FR 89 AFT RT SEAT TRACK. R & R RT SEAT TRACK DOUBLER.

Part: RIB — CRACKED (ZONE 500) · airframe 22,938 hrs · 13,167 cycles

CRACK ON LT WING, RIB 10 EXTENSION AT FASTENER HOLE ON UPPER FLANGE. R & R RIB 10 EXTENSION.

Part: RIB — CRACKED (ZONE 600) · airframe 22,938 hrs · 13,167 cycles

CRACK ON RT WING, RIB 10 EXTENSION AT FASTENER HOLE ON UPPER FLANGE. R & R RIB 10 EXTENSION.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 22,938 hrs · 13,167 cycles

CORROSION ON RT SEAT TRACK EXTENSION. R & R RT SEAT TRACK EXTENSION.

Part: STRUCTURE — CORRODED (ZONE 100) · corrosion level 2 · airframe 22,938 hrs · 13,167 cycles

CORROSION ON FLANGE AROUND WASTE BOX. REMOVED AND DISCARDED DOUBLERS AND REPLACED FASTENERS.

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 22,938 hrs · 13,167 cycles

CORROSION ON LT FRAME 19 ON AND AROUND RIVETS. CUTOUT DAMAGE, FABRICATED REPAIR DOUBLER AND FILLER, INSTALLED.

Part: PLATE — CORRODED (ZONE 100) · airframe 22,938 hrs · 13,167 cycles

CORROSION ON CENTER SEAL PLATE FR87-88. R & R CENTER SEAL PLATE.

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 22,938 hrs · 13,167 cycles

CORROSION ON FRAME 84 OTBD SEAT TRACK. DRILLED OUT CORROSION AND INSTALLED FASTENERS.

Part: SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 22,938 hrs · 13,167 cycles

CORROSION ON FWD CARGO DOOR SUPPORT AND LOWER LT SUPPORT NUT PLATE. R & R FWD CARGO DOOR CUTOUT LOWER SEAL REST.

Part: HANDLE — OBSTRUCTED (L2 DOOR) · airframe 22,081 hrs · 12,635 cycles

L2 DOOR HANDLES JAMMED. REMOVED DEBRIS FROM L2 DOOR HANDLE, OPS CHECK GOOD IAW AMM 52-12-0.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,748 hrs · 11,829 cycles

EMERGENCY AISLE LIGHTING STRIP NEAR SEAT 1D INOP. REPLACED EMERGENCY FLOOR IND STRIP IAW EMB 170 AMM 33-50-21.

Part: GLOWSTRIP — DEFECTIVE (CABIN) · airframe 19,055 hrs · 10,774 cycles

PHOTOLUMINESCENT ESCAPE PATH STRIP NEAR SEATS 8D AND F IS OUT. PERFORMED ADJUSTMENT TEST OF PHOTOLUMINESCENT STRIP IAW EMB 170 MM 33-52-21. A/C OK FOR SERVICE, NO DEFECTS NOTED.

Part: ROLLER — OUT OF ALIGNMENT (CABIN DOOR) · airframe 17,892 hrs · 10,039 cycles

MAIN CABIN DOOR EXTREMELY DIFFICULT TO OPEN FROM OUTSIDE AIRCRAFT. FOUND FWD UPPER ROLLER FITTING MISALIGNED. ADJUSTED FWD UPPER ROLLER, OPS CHECK GOOD IAW EMB 170 MM 52-11-01.

Part: DOOR — OUT OF ADJUST (CABIN) · airframe 17,767 hrs · 9,977 cycles

L1 DOOR VERY DIFFICULT TO OPEN FROM OUTSIDE. PERFORMED ADJUSTMENT TEST IAW EMB 170 MM 52-11-00. OPS CHECK GOOD.

Part: DOOR — OUT OF ADJUST (CABIN) · airframe 17,759 hrs · 9,973 cycles

L1 DOOR HARD TO OPEN FROM OUTSIDE, HANGS UP. INSPECTED AND ADJUSTED L1 DOOR IAW EMB MM 52-11-00. OPS CHECK NORMAL.

Part: WINDOW — OUT OF ADJUST (R1 DOOR) · airframe 17,740 hrs · 9,963 cycles

1R DOOR ARMED INDICATOR DOES NOT SHOW CLEARLY THROUGH VIEWING WINDOW. ADJUSTED ARM/DISARM VIEWING WINDOW AS REQUIRED IAW EMB MM 52-41-40. OPS CHECK GOOD.

Part: INDICATOR — DEFECTIVE (L1 DOOR) · airframe 17,731 hrs · 9,957 cycles

DOOR L1 VENT FLAP INDICATIONS DO NOT SHOW CLOSED WHEN CLOSED AND LOCKED. EICAS ALSO SHOWS OPEN. FERRIED TO IND. REPLACED FWD DOOR VISUAL INDICATOR PER AMM 52-11-22. OPS CHECK GOOD.

Part: BOTTLE — LOW PRESSURE (L1 DOOR) · airframe 17,653 hrs · 9,921 cycles

FLIGHT CREW REPORT L1 DOOR DIFFICULT TO OPEN FROM OUTSIDE. INSPECTED AND FOUND DOOR ASSIST BOTTLE LOW, SERVICED AND LUBED ALL ROLLERS AND LINKAGE IAW EMB 170 MM 52-11-5.

Part: PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,548 hrs · 9,866 cycles

LEVEL 2 CORROSION AROUND MOUNT BOLT HOLES FOR FWD GALLEY IN FLOOR STRUCTURE. REMOVED AND REPLACED SILL PLATE IAW EMB 170 SRM 51-41-02 AND 51-43-02.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · corrosion level 2 · airframe 17,548 hrs · 9,866 cycles

LEVEL 2 CORROSION AND GOUGES RIGHT I/B CF I SEAT TRACK ALL ALONG FWD EDGE OF TRACK. REMOVED AND REPLACED RIGHT I/B CF I SEAT TRACK IAW EMB 170 SRM 51-40-02, 51-45-03, 51-45-04.

Part: SEAT TRACK — UNKNOWN (FUSELAGE) · airframe 17,548 hrs · 9,866 cycles

RE-INSPECT PREVIOUS REPAIR AT FORWARD RT SEAT TRACK BEAM AT FRAME 14 IAW NON ROUTINE CARD TO CONFIRM INSTALLATION WORKMANSHIP. REMOVED AND REPLACED RT SEAT TRACK IAW EMB 170 SRM 51-41-02 AND 51-42-00.

Part: GIRT BAR — OUT OF POSITION (L2 DOOR) · airframe 16,964 hrs · 9,521 cycles

L2 DOOR GIRT BAR INDICATOR HALF RED. MAINTENANCE DEFERRED. 5/19/11 MEL CLEARED - RESET GIRT BAR IAW EMB 170 MM 25-65-01. OPS CHECK GOOD.

Part: UNKNOWN — MALFUNCTIONED (L2 DOOR) · airframe 16,956 hrs · 9,515 cycles

CREW REPORTED UNABLE TO OPEN L2 DOOR FROM OUTSIDE. MAINTENANCE PERFORMED OPS CHECK OF L2 DOOR WITH NO DEFECTS NOTED, OPS CHECK GOOD IAW EMB 170 MM 52-12-00.

Part: ENGINE — LEAKING (RIGHT)

CREW REPORTS SMELL OF SMOKE IN THE CABIN/COCKPIT AFTER TAKEOFF. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. RAN ENGINE, FOUND EVIDENCE OF LEAK AT NR 2 ENG A SUMP. CONSUMPTION MINIMAL, WITHIN LIMITS IAW GE MM 72-00-00. FERRIED TO IND. REMOVED AND REPLACED RT ENGINE IAW ENGINE CHANGE JOBCARD. ALL CHECKS GOOD AT THIS TIME.

Part: LENS — MISSING (EVAC SLIDE) · airframe 14,969 hrs · 8,325 cycles

R2 SLIDE COVER MISSING LENS. INSTALLED VIEWING LENS FOR R2 DOOR BUSTLE IAW EMB 170 MM 25-23-06.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 12,405 hrs · 6,757 cycles

RT SHEAR PLATE AT FR87 AND FR88 BETWEEN RT SILL BEAM AND RT SEAT TRACK BEAM LEVEL 2 CORROSION. FABRICATED AND INSTALLED NEW SHEAR PLATE IAW IC2009-170/00325.

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 12,405 hrs · 6,757 cycles

RT FLOORBEAM GUSSET LEVEL 2 CORROSION IN AFT GALLEY AREA AT FR 90 FWD OF AFT BATTERY COMPARTMENT. REMOVED AND REPLACED RT FLOOR GUSSET IAW IC2009-170/00325.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 12,405 hrs · 6,757 cycles

FWD CABIN LT SEAT TRACK BEAM FRAME 17 HAS LEVEL 2 CORROSION. REMOVED AND REPLACED LT SEAT TRACK BEAM IAW EMB 170 SRM 51-41-00, 51-43-03, 51-43-04.

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 12,405 hrs · 6,757 cycles

RIGHT SEAT TRACK BEAM GUSSET LEVEL 2 CORROSION AT FR 90. REMOVED AND REPLACED RT SEAT TRACK GUSSET IAW IC2009-170/00325.

Part: COMPUTER — MALFUNCTIONED · airframe 8,501 hrs · 4,333 cycles

AT CRUISE ALTITUDE CREW RECEIVED AN EICAS MESSAGE ELEV THRU COMP FAIL. SHORTLY THEREAFTER WE NOTICED THE N1 AND ITT GAUGES ON BOTH ENGINE WERE FLUCTUATING WHILE IN CRUISE FLIGHT WITH NO ADJUSTMENTS TO THE THROTTLES. AS CREW STARTED THEIR DESCENT THEY RECEIVED AN EICAS MESSAGE "GROUND SPOILERS FAIL" AND SHORTLY AFTER RECEIVED "AOA LIMIT FAIL EICAS" MESSAGE. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE DOWNLOAD OF FHDB/DVDR FAULT CODES POINTING AT ADSP NR 3. MAINTENANCE RESET POWER, PERFORMED RTS TO VERIFY ALL FMC ARE GOOD AND CLEARED INHIBITS ON FLAP CHANNELS. MAINTENANCE ACCOMPLISHED A FINAL RESET OF AIRCRAFT POWER, CYCLED FLAPS AND RAN ENGINES; ALL FAULTS CLEARED, NO CORRELATIONS FOUND.

Part: SENSOR — DEFECTIVE (LEFT) · airframe 5,276 hrs · 2,370 cycles

FLIGHT 6472 DFW TO JFK AFTER DEPARTING DFW IN CRUISE FLIGHT THE CREW RECEIVED AN AMBER FLAP FAILURE EICAS WARNING. DIVERT TO IND AND DECLARED AN EMERGENCY. MAINTENANCE REMOVED AND REPLACED THE LEFT O/B T4 SKEW SENSOR.

Part: TIRE — FAILED (MLG) · airframe 1,579 hrs · 579 cycles

FLIGHT 6460 SLC TO IND ON TAXI CREW NOTICED A BUMP AND ATTRIBUTED TO A POT HOLE, NO ABNORMAL TAXI CHARACTERISTICS NOTED. ON T/O ROLL AT APPROX 110 KTS CREW EXPERIENCED ABNORMAL VIBRATION AND REJECTED TAKEOFF. A/C WAS BROUGHT TO A FULL STOP BUT COULD NOT EXIT RUNWAY, TOWER SCRAMBLED CRASH CREW WITH NO INCIDENT. ON INSPECTION BOTH RIGHT MAIN TIRES WERE FOUND TO HAVE BLOWN. INCIDENT IS UNDER INVESTIGATION TO DETERMINE THE CAUSE AND CORRECTIVE ACTION.

Part: CABIN PRESSURE — MALFUNCTIONED

FLIGHT 6438 JFK-AUS AUTO PRESSURIZATION MALFUNCTION, PASSENGER OXYGEN MASKS DEPLOYED. AIRCRAFT MADE A EMERGENCY DESCENT & DIVERTED TO SHV.