N632RW

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,094 hrs · 25,708 cycles

LEVEL 2 CORROSION FUSELAGE SHEAR CLIP FR 17 AND STR 25-26R. SHEAR CLIP REPLACED IAW SRM 51-41-01 AND -02

Part: HINGE — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,094 hrs · 25,708 cycles

LEVEL 2 CORROSION CFIII WASTE WATER ACCESS PANEL HINGE. PANEL HINGE REPLACED IAW SRM 51-43-04 AND -02

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,094 hrs · 28,892 cycles

CORROSION FOUND ON CENTER FUSELAGE III LOWER FRAME SHEAR CLIP AT FR75 BETWEEN STRG 24L & STRG 25L REPLACED IAW SRM 51-41-01 & 51-41-02

Part: SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,094 hrs · 28,892 cycles

CFIII FLOOR STRUCTURE CORROSION FOUND ON RH FLOOR SUPPORT BETWEEN FR88 & FR90 REPLACED IAW SRM 51-41-01

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,094 hrs · 28,892 cycles

CORROSION FOUND ON CENTER FUSELAGE III LOWER FRAME SHEAR CLIP AT FR76 BETWEEN STRG 24L & STRG 25L REPLACED IAW SRM 51-41-01 & 51-41-02

Part: ROD — DAMAGED (ZONE 100) · airframe 46,094 hrs · 25,708 cycles

** WHILE AIRCRAFT WAS IN HEAVY CHECK** LANDING GEAR EMERGENCY SELECTOR VALVE ROD IS DAMAGED. ROD ASSY WAS REPLACED IAW 32-34-17-400-801A

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,094 hrs · 28,892 cycles

CORROSION FOUND ON CENTER FUSELAGE III LOWER FRAME SHEAR CLIP AT FR81 BETWEEN STRG 27R & STRG 28R REPLACED IAW SRM 51-41-01 & 51-41-02

Part: DOUBLER — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,094 hrs · 25,708 cycles

**DURING HEAVY CHECK FOUND: CORROSION FOUND ON SPLICE AT LH SHEAR PANEL BETWEEN FR 87-88. REPLACED SPLICE IAW SRM 51-42-02

Part: DOUBLER — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,094 hrs · 25,708 cycles

**DURING HEAVY CHECK FOUND: CORROSION FOUND ON FLOOR SUPPORT AT LH SIDE BETWEEN FR 88 90. REPLACED FLOOR SUPPORT AT LH SIDE BETWEEN FR88 90 IAW SRM 51-41-01

Part: DOUBLER — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,094 hrs · 25,708 cycles

CORROSION FOUND ON LH DOUBLER PLAE BETWEEN FR12-16. REPLACED DOUBLER PLATE IAW SRM 51-41-02

Part: DOOR — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,094 hrs · 25,708 cycles

**DURING HEAVY CHECK FOUND: CORROSION FOUND ON WASTE DOOR SKIN PANEL BETWEEN FR88-89 BETWEEN STR 23-25 RH. REPLACED WASTE DOOR SKIN PANEL IAW SRM 51-41-02

Part: SUPPORT — CORRODED (FRAMES 24-27) · corrosion level 2 · airframe 43,976 hrs · 27,511 cycles

WHILE THE A/C WAS IN FOR HEAVY CHECK FOUND FWD CARGO DOOR CUTOUT CORROSION ON 4 NUTPLATE SUPPORT AT LOWER SILL BEAM BETWEEN FR 24-27. REPLACED FWD CARGO DOOR CUTOUT CORROSION FOUND ON 4 NUTPLATE SUPPORT PN 170-67176-403 AT LOWER SILL BEAM BETWEEN FR 24-27, IAW EMB SRM 51-41-01, 51-21-02. FOR DETAILS OF WORK PERFORMEED SEE AAR NRC NR 4500797-1000-0127. A/C REMAINS IN YQG FOR COMPLETION.

Part: FRAME — CRACKED (FRM 52) · airframe 43,976 hrs · 27,511 cycles

WHILE A/C WAS IN FOR HEAVY CHECK FOUND LT GEAR WELL FR 52 CRACK, DMI NR R794484/1. REPLACED FR 52 RIB PN 170-08669-005, IAW SRM 51-41-01. A/C REMAINS IN YQG FOR COMPLETION. SEE AAR NRC NR 4500797-1000-0063 FOR WORK PERFORMED.

Part: SLAT TRACK — CRACKED (LT WING) · airframe 43,976 hrs · 27,511 cycles

WHILE A/C WAS IN FOR HEAVY CHECK FOUND LT WING SLAT NR 2 INBOARD TRACK CUT OUT CRACKED. REPAIRED LT WING SLAT NR 2 INBOARD TRACK PN 170-31032-021, IAW ETD 2020-170-031775. SEE AAR NRC NR 4500797-5000-0011. A/C RETURNED TO SERVICE.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 43,976 hrs · 27,511 cycles

LT HORIZONTAL STAB RIB 10A, (P/N 170-62571-003), 11A (P/N 170-62783-003 & 12A (P/N 170-62642-003) FOUND CRACKED. REPLACED IAW REPUBLIC AIRWAYS EO 170EO-55-10-0004-1.

Part: SLAT TRACK — CRACKED (RT WING) · airframe 43,976 hrs · 27,511 cycles

WHILE A/C WAS IN FOR HEAVY CHECK FOUND RT WING FIXED LEADING EDGE SKIN CRACK FOUND ON SLAT TRACK NR 4. REPAIRED SLAT TRACK NR 4, IAW SRM 57-49-01 R6. SEE AAR NRC NR 4500797-6000-0013 FOR WORK PERFORMED. A/C REMAINS IN YQG FOR COMPLETION.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 43,976 hrs · 27,511 cycles

RT HORIZONTAL STAB RIB 10A, (P/N 170-62571-004) 11A (P/N 170-62783-004) & 12A (P/N 170-62642-004) FOUND CRACKED. REPLACED IAW REPUBLIC AIRWAYS EO 170EO-55-10-0004-1.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 43,976 hrs · 27,511 cycles

DURING HEAVY CHECK MAINTENANCE FOUND CORROSION CFII FLOOR STRUCTURE RT INBOARD SEAT TRACK BEAM BETWEEN FR 43 AND FR 59. CFII FLOOR STRUCTURE HRIB SEAT TRACK BEAM BETWEEN FR 43 AND FR 59 REPLACED, IAW EMB 170SRM 51-42-01 AND 51-43-01. A/C REMAINS IN CHECK.

Part: SKIN — CRACKED (LT WING) · airframe 43,976 hrs · 27,511 cycles

DURING HEAVY CHECK MAINTENANCE FOUND LT WING SLAT NR 2 INBOARD SLAT TRACK CUTOUT CRACKED. LT WING, SLAT NR 2 INBOARD SLAT TRACK CUTOUT REPAIRED, IAW ETD2020-170-031775. A/C REMAINS IN CHECK.

Part: SKIN — CRACKED (LT WING TE) · airframe 43,976 hrs · 27,511 cycles

LT WING, CRACK FOUND ON LT UPPER SKIN TRAILING EDGE BETWEEN RIB 10-11, SPOILER 3, INBOARD HINGE NEAR EXISTING REPAIR. REPAIRED IAW EMB ETD2020-170-031776.

Part: SLAT TRACK — CRACKED (LT WING SLAT) · airframe 43,976 hrs · 27,511 cycles

WHILE AC WAS IN FOR HEAVY CHECK FOUND LT WING NR 2 SLAT OUTBOARD SLAT TRACK CUTOUT CRACKED. REPAIRED LT WING NR 2 SLAT OUTBOARD SLAT TRACK, IAW EMB ETD2020-170-031774. SEE AAR NRC NR 4500797-5000-0012 FOR WORK PERFORMED. AC RETURNED TO SERVICE.

Part: SKIN — CRACKED (LT WING) · airframe 43,976 hrs · 27,511 cycles

DURING HEAVY CHECK MAINTENANCE FOUND LT WING NR 2 SLAT OUTBOARD SLAT TRACK CUTOUT CRACKED. LT WING NR 2 SLAT, OUTBOARD SLAT TRACK CUT OUT REPAIRED, IAW ETD2020-170031774. A/C REMAINS IN CHECK.

Part: GUSSET — CORRODED (FRAME 90) · corrosion level 2 · airframe 43,976 hrs · 27,511 cycles

WHILE A/C WAS IN FOR HEAVY CHECK FOUND CORROSION ON FLOOR STRUCTURE AT FR 90 GUSSET PN 170-60257-001 AT LBL 16 GUSSET. REPLACED IAW EMB SRM 51-41-02.

Part: SHEAR PANEL — CORRODED (FRAMES 87-88) · corrosion level 2 · airframe 43,976 hrs · 27,511 cycles

WHILE A/C WAS IN FOR HEAVY CHECK FOUND CF3 FLOOR SUPPORT STRUCTURE RT SHEAR PANEL BETWEEN FR 87-88 HAS CORROSION. SHEAR PANEL PN 170-91919-001 REPLACED, IAW EMB SRM 51-42-01, 51-42-02. SEE AAR NRC NR 4500797-2000-0096. A/C REMAINS IN YQG FOR COMPLETION.

Part: DOUBLER — CORRODED (FRM 84 SEAT TRAC) · corrosion level 2 · airframe 43,976 hrs · 27,511 cycles

WHILE A/C WAS IN FOR HEAVY CHECK FOUND CF3 RT INBOARD SEAT TRACK AT FR 84 EXISTING REPAIR DOUBLER HAS CORROSION. REPLACED REPAIR DOUBLER, IAW EMB SRM 53-23-10. SEE AAR NRC NR 4500797-2000-0103 FOR WORK PERFORMED. A/C REMAINS IN RQG FOR COMPLETION.

Part: SEAT TRACK — CORRODED (FRAME 84) · corrosion level 2 · airframe 43,976 hrs · 27,511 cycles

WHILE A/C WAS IN FOR HEAVY CHECK FOUND CORROSION FOUND ON CF 3 LT INBOARD SEAT TRACK UPPER FLANGE AT FR 84. REPLACED SEAT TRACK UPPER FLANGE AT FR 84, IAW EMB SRM 53-23-10. SEE AAR NRC NR 4500797-2000-0104. A/C REMAINS IN YQG FOR COMPLETION.

Part: BEAM — CORRODED (FRAME 87) · corrosion level 2 · airframe 43,976 hrs · 27,511 cycles

WHILE A/C WAS IN FOR HEAVY CHECK FOUND CORROSION FOUND ON CENTER FUSELAGE 3 STRUCTURE LONGITUDINAL BEAM AT FR 87 RT SIDE. REPLACED BEAM AT FR 87, IAW EMB SRM 51-41-01, 51-43-03. SEE AAR NRC NR 4500797-2000-0095 FOR WORK PERFORMED. A/C REMAINS IN YQG FOR COMPLETION.

Part: GUSSET — CORRODED (FRAME 90) · corrosion level 2 · airframe 43,976 hrs · 27,511 cycles

WHILE A/C WAS IN FOR HEAVY CHECK FOUND CORROSION FOUND ON FLOOR SUPPORT STRUCTURE AT FR 90 GUSSETS AT RBL 16. REPLACED GUSSET PN 170-60257-001, IAW EMB SRM 51-41-01. SEE AAR NRC NR 4500797-2000-0098 FOR WORK PERFORMED. A/C REMAINS IN YQG FOR COMPLETION.

Part: FLOOR SUPPORT — CRACKED (FRAME 12) · airframe 43,976 hrs · 27,511 cycles

DURING HEAVY CHECK MAINTENANCE FOUND CRACK FOUND ON FLOOR SUPPORT CLIP AT FR 12, BL 0. FLOOR SUPPORT CLIP AT FR 12, BL 0 REPLACED, IAW EMB SRM 51-41-01. A/C REMAINS IN CHECK.

Part: DOUBLER — CORRODED (FRAMES 13-14) · corrosion level 2 · airframe 43,976 hrs · 27,511 cycles

WHILE A/C WAS IN FOR HEAVY CHECK FOUND CORROSION FOUND ON PREVIOUS REPAIR DOUBLER BETWEEN FR 13-14 RT SIDE AT MONUMENT MOUNT FLOOR SUPPORT. REPLACED DOUBLER PN 2024-T3.080 BETWEEN FR 13-14 RT SIDE AT MONUMENT MOUNT FLOOR SUPPORT, IAW EMB SRM 53-10-10 REPAIR 01. FOR DETAILS SEE AAR NRC NR 4500797-2000-0081. A/C REMAINS IN YQG FOR COMPLETION.

Part: SHEAR TIE — CORRODED (FRAMES 19-20) · corrosion level 2 · airframe 43,976 hrs · 27,511 cycles

WHILE A/C WAS IN FOR HEAVY CHECK FOUND CORROSION ON SHEAR WEB BETWEEN FR 19-20 LT SIDE BEHIND L1 DOOR. AAR MX REPLACED SHEAR WEB (PN 170-07311-001) BETWEEN FR 19-20 LT SIDE BEHIND L1 DOOR, IAW EMB SRM 51-43-02, SRM 51-41-02. FOR DETAILS OF WORK PERFORMED SEE AAR NRC NR 4500797-2000-0084. A/C REMAINS IN YQG FOR COMPLETION.

Part: DOUBLER — CORRODED (FRAMES 12-13) · corrosion level 2 · airframe 43,976 hrs · 27,511 cycles

WHILE A/C WAS IN FOR HEAVY CHECK FOUND CORROSION FOUND ON PREVIOUS REPAIR DOUBLER BETWEEN FR 12-13 AT MONUMENT MOUNT. INSTALLED NEW DOUBLER, IAW SRM 53-10-10 REPAIR 01. SEE AAR NRC NR 4500797-2000-0080. A/C REMAINS IN YQG FOR COMPLETION.

Part: SEAT TRACK — CORRODED (FRAMES 12-20) · corrosion level 2 · airframe 43,976 hrs · 27,511 cycles

WHILE A/C WAS IN FOR HEAVY CHECK CORROSION FOUND ON FWD LT INBOARD SEAT TRACK BETWEEN FR 12-20. SEAT TRACK PN 170-03264-001 REPLACED, IAW EMB SRM 51-41-01, 51-43-01. SEE AAR NRC NR 4500797-2000-0085 FOR DETAILS OF WORK PERFORMED. A/C REMAINS IN YQG FOR COMPLETION.

Part: CHANNEL — CORRODED (FRAME 16) · corrosion level 2 · airframe 43,976 hrs · 27,511 cycles

WHILE THE A/C WAS IN FOR HEAVY CHECK FOUND FWD CARGO COMPARTMENT CORROSION FOUND ON FR 16 OUTER FLANGE BETWEEN STR 27-28 RT. REPLACED FWD CARGO COMPARTMENT CORROSION FOUND ON FR 16 OUTER FLANGE PN 170-03860-003 BETWEEN STR 27-28 RT, IAW EMB SRM 51-41-01. FOR DETAILS OF WORK PERFORMED SEE AAR NRC NR 4500797-1000-0076. A/C REMAINS IN YQG FOR COMPLETION.

Part: SHEAR TIE — CORRODED (FRAME 16) · corrosion level 2 · airframe 43,976 hrs · 27,511 cycles

WHILE AC WAS IN FOR HEAVY CHECK FOUND CORROSION ON LOWER FUSELAGE FR 16 AT SHEAR CLIP BETWEEN STR 27-28R. AAR MX REPLACED SHEAR CLIP (PN 170-03859-002) BETWEEN STR 27-28R, IAW MB SRM 51-41-01, SRM 51-41-02. SEE AAR NRC NR 4500797-1000-0072 FOR WORK PERFORMED. AC REMAINS IN YQG FOR COMPLETION.

Part: DOUBLER — CORRODED (FRAMES 16-17) · corrosion level 2 · airframe 43,976 hrs · 27,511 cycles

WHILE AC WAS IN FOR HEAVY CHECK FOUND CORROSION ON LOWER FUSELAGE ANTENNA DOUBLER BETWEEN FR 16-17 AND STR 27-28L. AAR MX REPLACED LOWER FUSELAGE ANTENNA DOUBLER (P/N 170-14431-001) BETWEEN FR 16-17 AND STR 27-28L, IAW EMB SRM 51-41-02. FOR DETAILS OF WORK PERFORMED SEE AAR NRC NR 4500797-1000-0074. AC REMAINS IN YQG FOR COMPLETION.

Part: SHEAR TIE — CORRODED (FRAME 17) · corrosion level 2 · airframe 43,976 hrs · 27,511 cycles

WHILE AC WAS IN FOR HEAVY CHECK FOUND CORRISION ON SHEAR CLIP FWD CARGO COMPARTMENT FR 17 BETWEEN STR 27-28R. AAR MX REPLACED SHEAR CLIP (PN 170-03335-001) FWD CARGO COMPARTMENT FR 17 BETWEEN STR 27-28R, IAW EMB SRM 51-41-01, SRM 51-43-03. FOR DETAILS OF WORK PERFORMED SEE AAR NRC NR 4500797-1000-0073. A/C REMAINS IN YQG FOR COMPLETION.

Part: SEAL REST — CORRODED (FRAME 27) · corrosion level 2 · airframe 43,976 hrs · 27,511 cycles

WHILE A/C WAS IN FOR HEAVY CHECK FOUND FWD CARGO DOOR. CUT OUT CORROSION FOUND ON AFT CORNER SEAL REST AT LOWER BEAM SILL AT FR 27 AND STR 25L. REPLACED CORNER SEAL REST PN 170-66803-404, IAW EMB SRM 51-21-01, AMM 20-10-01. SEE AAR NRC NR 4500797-1000-0036 FOR WORK PERFORMED. A/C REMAINS IN YQG FOR COMPLETION.

Part: SEAL REST — CORRODED (FRAMES 25-26) · corrosion level 2 · airframe 43,976 hrs · 27,511 cycles

WHILE A/C WAS IN FOR HEAVY CHECK FOUND FWD CARGO DOOR CUT OUT CORROSION FOUND ON MID SEAL REST AT LOWER BEAM BETWEEN FR 25-26 AND STR 25RH. AAR MX REPLACED MID SEAL REST PN 170-66804-401 AT LOWER BEAM BETWEEN FR 25-26 AND STR 25RH, IAW EMB SRM 51-4101, 51-21-01. FOR DETAILS OF WORK PERFORMED SEE AAR NRC NR 45007978-1000-0037. A/C REMAINS IN YQG FOR COMPLETION.

Part: POWER UNIT — INOPERATIVE (CABIN) · airframe 43,519 hrs · 27,175 cycles

AFT RT OUTBOARD ELPU BATTERY FAULT. R&R AFT RT OUTBOARD ELPU IAW AMM 33-50-01.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 42,585 hrs · 26,614 cycles

RIGHT HAND SERVICE DOOR EMERGENCY LIGHT BATTERY INOP. R&R RIGHT HAND SERVICE DOOR EMERGENCY LIGHT BATTERY IAW AMM 33-50-01.

Part: ENGINE — SHUTDOWN (NR 1) · airframe 42,262 hrs · 26,418 cycles

E1 SHUTDOWN IN FLIGHT. DECLARED EMERGENCY, DIVERTED TO BNA, LANDED WITHOUT INCIDENT. R&R LH ENGINE IAW JC 72-10-400-0001.

Part: SENSOR — OUT OF ADJUST (NLG STEERING) · airframe 42,177 hrs · 26,361 cycles

LANDING GEAR HANDLE WOULD NOT RETRACT GEAR. HANDLE WOULD MOVE. SWITCH IN NORMAL (EMERGENCY EXTENSION PANEL, GREEN ON ALL GEAR). NO EICAS MESSAGE FOR WOW SYSTEM. NO CB OUT, NO OTHER INDICATIONS IN COCKPIT. GEAR DID NOT MOVE. DECLARED EMERGENCY, RETURNED TO FIELD, LANDED WITHOUT INCIDENT. R&R WOF1 AND WOF2 SENSORS IAW AMM 32-62-01 AND ADJUSTED NOSE STEER FEEDBACK SENSOR 1/2 IAW AMM 32-53-09. FAULTS CLEARED. OPS CHECK OF EXTENSION AND RETRACTION SYSTEM OPS CHECK GOOD.

Part: BATTERY — FAULTY (EMERGENCY LIGHT) · airframe 41,615 hrs · 26,005 cycles

EMERGENCY LIGHT BATTERY FAULT ADVISORY MESSAGE DISPLAYED DURING EMERGENCY LIGHTS TEST. R&R RH FWD EMERGENCY LIGHT BATTERY IAW AMM 33-50-01.

Part: BONDING JUMPER — OUT OF POSITION (L1 DOOR) · airframe 39,991 hrs · 25,034 cycles

L1 DOOR IS HARD TO MOVE AND OPEN/CLOSE. FOUND BONDING JUMPER CATCHING IN LOWER GUIDE PINION. RELOADED BONDING JUMPER, OPERATIONAL CHECK OF DOOR WAS GOOD IAW AMM 52-11-30.

Part: DISPLAY — FAILED (NR 1) · airframe 39,834 hrs · 24,942 cycles

MCDU 2 BLANKED OUT, DIVERTED TO MSY. SWAPPED MCDU 1 AND 2, DEFERRED MCDU 1 IAW MEL 34-61-02-1. (LATER R&R MCDU 1 IAW AMM 34-61-02, OPS CHECK GOOD.)

Part: NUT PLATE — CORRODED (FRAMES 88-98) · corrosion level 2 · airframe 38,363 hrs · 24,026 cycles

MAINTENANCE FOUND CORROSION AT THE WASTE BOX NUT HOLDER AT FRAME 88 TO 98. THE NUT HOLDER WAS REMOVED AND REPLACED IAW SRM 51-43-03, 51-10-03, 51-75-16, AND 51-40-02.

Part: INTERCOSTAL — CORRODED (BS 86-87) · corrosion level 2 · airframe 38,363 hrs · 24,026 cycles

MAINTENANCE DISCOVERED CORROSION ON AFT DRAIN MAST INTERCOSTALS, BETWEEN FRAMES 86 AND 87, STRINGERS 27R AND 28R. REMOVED AND REPLACED THE INTERCOSTALS, AND ANGLES IAW SRM 51-40-03.

Part: STRUCTURE — CORRODED (WASTE BOX) · corrosion level 2 · airframe 38,363 hrs · 24,026 cycles

MAINTENANCE DISCOVERED CORROSION ON THE WASTE BOX. REMOVED AND REPLACED THE WASTE BOX IAW SRM 51-43-04. SRM 51-75-16, SRM 51-41-02, AND AMM 53-01-09.

Part: SEAT TRACK — CORRODED (FRAMES 12-14) · corrosion level 2 · airframe 38,363 hrs · 24,026 cycles

MAINTENANCE FOUND CORROSION ON THE FLOOR SEAT TRACK NEAR FORWARD GALLEY MOUNT POINTS, FRAMES 12 TO 14. THE CORROSION WAS REMOVED AND DETERMINED TO BE OUT OF SRM LIMITS. DOUBLERS WERE FABRICATED AND INSTALLED IAW ETD2018-170-057239, AND SRM 53-10-10, REPAIR 3.

Part: SHEAR TIE — CORRODED (FRAME 88) · corrosion level 2 · airframe 38,363 hrs · 24,026 cycles

MAINTENANCE DISCOVERED CORROSION ON A SHEAR TIE. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-41-01, AND SRM 51-41-02.

Part: SHEAR PANEL — CORRODED (FRAME 87) · corrosion level 2 · airframe 38,363 hrs · 24,026 cycles

MAINTENANCE DISCOVERED CORROSION ON THE CENTER SHEAR PANEL AT FRAME 87. REMOVED AND REPLACED THE SHEAR PANEL IAW SRM 51-42-01.

Part: SHEAR TIE — CORRODED (FRAME 87) · corrosion level 2 · airframe 38,363 hrs · 24,026 cycles

MAINTENANCE DISCOVERED CORROSION ON THE SHEAR TIE. REMOVED AND REPLACED SHEAR TIE IAW SRM 51-41-01, AND SRM 51-41-02.

Part: BRACKET — CORRODED (FRAME 88) · airframe 38,363 hrs · 24,026 cycles

MAINTENANCE DISCOVERED CORROSION ON THE BRACKET LOCATED ON TOP OF THE WASTE BOX. REMOVED AND REPLACED BRACKET IAW E170 SRM 510-10-03, SRM 51-75-16, SRM 51-40-02 AND SRM 51-43-03.

Part: REINFORCEMENT — CORRODED (FWD CARGO) · corrosion level 2 · airframe 38,363 hrs · 24,026 cycles

MAINTENANCE DISCOVERED CORROSION ON FWD CARGO REINFORCEMENT ABOVE THE OXYGEN BOTTLE, WHERE THE BONDING WIRE ATTACHES. REMOVED AND REPLACED REINFORCEMENT IAW SRM 51-40-03.

Part: FLOOR SUPPORT — CORRODED (FRAME 89) · corrosion level 2 · airframe 38,363 hrs · 24,026 cycles

MAINTENANCE DISCOVERED CORROSION ON THE FLOOR SUPPORT AT FRAME 89, RBL35. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-42-01.

Part: FLOORBEAM — CORRODED (FRAME 87) · corrosion level 2 · airframe 38,363 hrs · 24,026 cycles

MAINTENANCE DISCOVERED CORROSION ON THE FLOORBEAM ANGLE AT FRAME 87. REMOVED AND REPLACED THE FLOORBEAM ANGLE IAW SRM 51-41-01.

Part: SUPPORT ANGLE — CORRODED (WASTE BOX) · corrosion level 2 · airframe 38,363 hrs · 24,026 cycles

MAINTENANCE DISCOVERED CORROSION ON THE SUPPORT ANGLE ON TOP OF WASTE BOX. REMOVED AND REPLACED THE SUPPORT ANGLE IAW SRM 51-40-02.

Part: SHEAR PANEL — CORRODED (FRAME 87) · corrosion level 2 · airframe 38,363 hrs · 24,026 cycles

MAINTENANCE DISCOVERED CORROSION ON THE RT SHEAR PANEL AT FRAME 87. REMOVED AND REPLACED THE SHEAR PANEL IAW SRM 51-42-01.

Part: SEAT TRACK — CORRODED (FRAME 84) · corrosion level 2 · airframe 38,363 hrs · 24,026 cycles

MAINTENANCE DISCOVERED CORROSION ON THE RT INBD SEAT TRACK AT FRAME 84. BLENDED AND INSTALLED A FABRICATED REPAIR DOUBLER IAW SRM 53-23-10 .

Part: RIB — CORRODED (WNG-BDY FAIRING) · corrosion level 2 · airframe 38,363 hrs · 24,026 cycles

MAINTENANCE FOUND CORROSION ON WING TO FUSELAGE FAIRING AT FRAME 45, RBL 6. CORROSION WAS BLENDED IAW SRM 51-10-03. RIB AND NUTPLATE WERE REMOVED AND REPLACED IAW SRM 51-41-01, AND 51-45-00.

Part: BRACKET — CORRODED (FRAME 80) · corrosion level 2 · airframe 38,363 hrs · 24,026 cycles

MAINTENANCE FOUND CORROSION ON THE AFT CARGO DOOR CUTOUT BRACKET JUST AFT OF LOWER CLOSURE PLATE AT FRAME 80. THE BRACKET WAS REMOVED AND REPLACED IAW SRM 51-41-01, AND SRM 51-41-12.

Part: SEAL REST — CORRODED (CARGO DOORWAY) · corrosion level 2 · airframe 38,363 hrs · 24,026 cycles

MAINTENANCE FOUND CORROSION AROUND AFT CARGO DOOR CUTOUT LOWER SEAL NUTPLATES AND ATTACH RIVETS AT FRAME 77 TO 79. THE LOWER SEAL REST WAS REMOVED AND REPLACED IAW SRM 51-41-01.

Part: SHEAR TIE — CORRODED (FRAME 17) · corrosion level 2 · airframe 38,363 hrs · 24,026 cycles

MAINTENANCE FOUND CORROSION AT FWD FUSELAGE SHEAR TIE, FRAME 17, STRINGERS 26 - 27. THE SHEAR TIE WAS REMOVED AND REPLACED IAW SRM 51-41-01, AND 51-41-02.

Part: PANEL — CORRODED (WASTE BOX) · corrosion level 2 · airframe 38,363 hrs · 24,026 cycles

MAINTENANCE FOUND LEVEL 2 CORROSION ON WASTE SERVICE PANEL AT FRAMES 86 TO 89. WASTE SERVICE PANEL WAS REMOVED AND REPLACED IAW AMM 53-03-60, 51-10-03, AND 51-75-16.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 37,532 hrs · 23,520 cycles

COCKPIT DOME EMERGENCY LIGHT DOES ILLUMINATE WHEN EMERGENCY LIGHT SYSTEM TESTED. R & R THE BATTERY. LIGHT CAME ON IAW AMM 33-50-00.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 27,532 hrs · 23,520 cycles

L2 EMERGENCY LIGHT INOPERATIVE. R & R THE BATTERY IAW AMM 33-50-00. OPS CHECKED GOOD.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 37,532 hrs · 23,520 cycles

BATTERY FAULT ON EICAS COMES ON ONLY IN THE ON POSITION. R & R THE AFT EMERGENCY BATTERY IAW AMM 33-50-00.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 37,089 hrs · 23,564 cycles

AFT EMERGENCY EXIT LIGHT INOP. R&R #3 EMERGENCY LIGHT BATTERY IAW AMM 33-50-01. OPS CHECK GOOD.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 36,498 hrs · 22,879 cycles

FLOOR EXIT SIGN AT R1 DOOR IS INOPERATIVE. R & R THE POWER SUPPLY IAW AMM 33-50-01. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,937 hrs · 21,164 cycles

FIRST CLASS EMERGENCY LIGHT STRIPS INOPERATIVE. R & R IAW AMM 33-50-21. OPS TEST GOOD.

Part: MOUNT — CORRODED (ZONE 100) · airframe 32,934 hrs · 20,435 cycles

AFT GALLEY, FWD RT FLOOR MOUNT HAS EVIDENCE OF CORROSION AT ATTACH WEB, UNDER FLOORBOARD 252 ERF. R & R SHEAR PANEL IAW SRM 51-42-01.

Part: MOUNT — CORRODED (ZONE 100) · airframe 32,934 hrs · 20,435 cycles

AFT GALLEY, FWD LT FLOOR MOUNT HAS EVIDENCE OF CORROSION AT ATTACH WEB UNDER FLOORBOARD 252ERF. R & R SHEAR PANEL IAW SRM 51-42-01.

Part: DOOR — CORRODED (ZONE 100) · corrosion level 2 · airframe 32,934 hrs · 20,435 cycles

WASTE WATER DOOR HAS CORROSION AROUND FWD EDGE AT HINGE LINE. R & R DOOR IAW AMM 20-10-07 AND 20-13-21.

Part: BRACKET — CORRODED (ZONE 100) · corrosion level 2 · airframe 32,934 hrs · 20,435 cycles

CORROSION ON FWD LAVATORY BRACKETS, SINGLE SPLIT JOINT AND DOUBLER SINGLE SPLIT JOINT. R & R 2 EACH DOUBLERS AND BRACKETS ON FWD LAV REF CMM 25-41-03.

Part: DOOR — OUT OF ADJUST (L2) · airframe 32,578 hrs · 20,210 cycles

L2 DOOR OFF TRACK. PUT L2 DOOR BACK IN TRACK AS REQUIRED, OPS CHECK GOOD REF AMM 52-12-00.

Part: LIGHT — OUT OF POSITION (CABIN) · airframe 32,376 hrs · 30,082 cycles

EMERGENCY LIGHT STRIP IN AFT PAX AISLE SLID OUT OF PLACE. MOVED THE LIGHT STRIP TO NORMAL POSITION AND RESECURED IAW AMM 33-50-21.

Part: DOOR — LACK OF LUBE (R2 DOOR) · airframe 31,338 hrs · 19,370 cycles

R2 DOOR VERY HARD TO OPEN VIA THE ARM DISARM LEVER. LUBRICATED R2 DOOR IAW AMM 52-42-00, OPS CHECK GOOD.

Part: PIN — SHEARED (L1 BELLCRANK) · airframe 30,908 hrs · 19,072 cycles

PIN SHEARED ON HOISTING BELLCRANK ASSEMBLY INSIDE L1 DOOR. R & R LOWER HOIST BELLCRANK IAW AMM 52-11-20.

Part: LIGHT — UNSECURE (CABIN) · airframe 30,426 hrs · 18,753 cycles

ROW 2C FLOOR ILLUMINATION STRIP MISSING. RESECURED FLOOR ILLUMINATION STRIP AT ROW 2C REF AMM 33-50-21. OPS CHECK NORMAL.

Part: UNKNOWN — ODOR (CABIN) · airframe 30,326 hrs · 18,685 cycles

ON DEPARTURE, TOGA SELECTED AND THERE WAS A SEVERE ODOR OF BURNED PLASTIC PERMEATING THE CABIN. ODOR LINGERED FOR 5-10 MINUTES AFTER TAKEOFF. PERFORMED COMP WASH ON LT ENGINE IAW S72-00-00-100-802A. OPS CHECK GOOD, NO ODOR NOTED.

Part: LIGHT — UNSECURE (ROW 9) · airframe 30,306 hrs · 18,671 cycles

PHOTO LUMINESCENT STRIP CAME LOOSE FROM ROW 9, ACFT RT SIDE. RESECURED PHOTO LUMINESCENT STRIP AT ROW 9 IAW AMM 33-50-21.

Part: GLOWSTRIP — INOPERATIVE (CABIN) · airframe 29,426 hrs · 18,109 cycles

GLOWSTRIP NOT GLOWING IN LOW LIGHT OPS. R & R THE GLOWSTRIP.

Part: TRIGGER — INOPERATIVE (PAX DOOR) · airframe 28,541 hrs · 17,573 cycles

MAIN CABIN DOOR RELEASE TRIGGER FOR CLOSING IS INOPERATIVE, LEVER GETS CAUGHT ON ROLLER WHEN OPENING DOOR. LUBED. TESTED IAW AMM 52-12-52, OPS CHECK GOOD.

Part: HANDLE — BROKEN (R1 DOOR) · airframe 28,292 hrs · 17,414 cycles

R1 DOOR ARMING HANDLE BROKEN. RESECURED R1 ARMING HANDLE DOOR WITH AERODYNAMIC SEAL IAW SRM 51-21-03. OPS CHECKED GOOD.

Part: FLAP SYSTEM — MALFUNCTIONED (ZONE 500) · airframe 28,157 hrs · 17,335 cycles

FLAPS FAILED DURING APPROACH. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. CLEARED FLAP INHIBITS IAW FIM 27-53-00-810-841A. ALL MESSAGES CLEARED. OPS CHECKED GOOD FOR FLAPS IAW AMM 27-50-00.

Part: SENSOR — MALFUNCTIONED (TE FLAPS) · airframe 28,158 hrs · 17,336 cycles

FLAP FAIL ON APPROACH. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. R & R RT OB FLAP SKEW SENSOR IAW AMM 27-53-06. OPS CHECK GOOD. PERFORMED HIGH ENERGY STOP CONDITION INSPECTION IAW AMM 05-50-12. NO DEFECTS NOTED.

Part: CABLE — DAMAGED (R1 DOOR GIRT BAR) · airframe 28,072 hrs · 17,281 cycles

R1 GIRT BAR NOT SHOWING DISENGAGED WITH REST OF THE DOOR SHOWING UNARMED, DISENGAGED. R & R R1 DOOR EMERGENCY EVACUATION SLIDE FLEX BALL CABLE IAW AMM 52-41-40. OPS CHECK GOOD.

Part: FITTING — OUT OF ADJUST (GIRT BAR) · airframe 27,938 hrs · 17,203 cycles

R2 DOOR VERY HARD TO DISARM. FOUND R2 DOOR AFT GIRT BAR FLOOR FITTING OUT OF ADJUSTMENT. ADJUSTED FITTING AS REQUIRED AND PERFORMED OPS CHECK IAW AMM 52-42-40. OPS CHECK GOOD AT THIS TIME.

Part: LATCH — CONTAMINATED (R2 DOOR SLIDE) · airframe 27,930 hrs · 17,195 cycles

F/A REPORTS UNABLE TO DISARM R2 DOOR. REMOVED DEBRIS FROM R2 EMERGENCY SLIDE LATCH IAW AMM 52-42-21. OPS CHECK GOOD.

Part: SEAL — OBSTRUCTED (L2 DOOR) · airframe 27,894 hrs · 17,177 cycles

L2 DOOR SQUEALS IN FLIGHT. NO PRESSURIZATION ISSUES. SMOOTHED LOOSE SEALANT ON ACFT DOOR FRAME SEALING SURFACE. NO DEFECTS NOTED. ACFT OK FOR SERVICE.

Part: SPAR — UNKNOWN (RT WING) · airframe 27,848 hrs · 17,149 cycles

SPAR 2 LOWER FLANGE REINFORCEMENTS. COMPLIED WITH SHUTTLE EO 170EO-57-10-0003. MAJOR REPAIR.

Part: SHEAR TIE — CORRODED (FRAME 75) · airframe 27,833 hrs · 17,143 cycles

CORROSION FOUND ON SHEAR TIE AT FRAME 75, S28-29R. R & R SHEAR TIE IAW SRM51-40-02. FABRICATED AND INSTALLED NEW SHEAR TIE IAW SRM51-41-01, 51-43-03.

Part: SHEAR TIE — CORRODED (FRAME 74) · corrosion level 2 · airframe 27,833 hrs · 17,143 cycles

SHEAR TIE AT FRAME 74 BETWEEN STRINGERS 28 - 29R CORRODED. R & R SHEAR TIE IAW SRM 51-40-02, 51-41-01 AND 51-41-02.

Part: FRAME — DEFORMED (12) · airframe 27,833 hrs · 17,143 cycles

PERMANENT DEFORMATION IN LT FWD FRAME 12, S17L. REPAIRED FRAME IAW SRM 53-10-01.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 27,833 hrs · 17,143 cycles

RT HORIZONTAL STABILIZER LEADING OTBD RIB CRACKED. REPAIRED IAW ETD2014-170-036753.

Part: SHEAR TIE — CORRODED (FRAME 76) · corrosion level 2 · airframe 27,833 hrs · 17,143 cycles

SHEAR TIE AT FRAME 76 BETWEEN STRINGERS 28 - 29R CORRODED. R & R SHEAR TIE IAW SRM 51-40-01.

Part: BRACKET — CRACKED (LT NACELLE) · airframe 27,833 hrs · 17,143 cycles

LEFT ENGINE PYLON PANEL 419QR AFT RETAINING BRACKET CRACKED. R & R IAW SRM 51-43-01, AND 51-43-02.

Part: BULKHEAD — CRACKED (LT MLG WW) · airframe 27,833 hrs · 17,143 cycles

CRACKED LT MLG WHEELWELL FWD BULKHEAD IS CRACKED OTBD OF AILERON CABLE TOWER. REMOVED RIB PANEL OTBD LT WHEELWELL FWD BULKHEAD, TRIMMED OFF LOWER FLANGE AND ATTACHED TO NEW RIB PANEL AND INSTALLED IAW ETD2014-170-036468, REV A.

Part: DOOR — FOD (R1) · airframe 26,911 hrs · 16,593 cycles

R1 DOOR DOES NOT ARM. REMOVED FOREIGN DEBRIS FROM DOOR. PERFORMED OPS CHECK OF DOOR IAW AMM 52-11-00, OPS CHECK GOOD.

Part: DOOR — DIRTY (MAIN PAX) · airframe 25,779 hrs · 15,931 cycles

MAIN CABIN DOOR CLOSES BUT CAN'T GET VENT TO ARM. REMOVED DEBRIS THAT WAS BINDING DOOR, OPERATES NORMAL IAW AMM 52-11-40.

Part: PROCESSOR — FAILED (ZONE 100) · airframe 24,960 hrs · 15,422 cycles

ON CLIMBOUT AT 24,000 FT, EICAS MESSAGE "AVNX MAU 1A FAIL" AND "ADS 1 FAIL". DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. R & R NIC PROC 1 IAW AMM 31-41-04, R & R POWER MOD 1, NAD 2 IN MAU 1 IAW AMM 24-61-13, OPS CHECK GOOD.

Part: PROCESSOR — FAULTY (ZONE 100) · airframe 24,758 hrs · 15,300 cycles

ON DESCENT AT FL270, AUTO PILOTS AND AUTO THROTTLE SIMULTANEOUSLY DISCONNECTED. EICAS MESSAGE AVNX MAU 1A FAIL APPEARED. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. REMOVED AND REPLACED NIC PROC 1.

Part: INDICATOR — OUT OF ADJUST (L2 DOOR) · airframe 24,565 hrs · 15,178 cycles

L2 DOOR NOT INDICATING COMPLETEDY DISARMED. ADJUSTED INDICATOR ON GIRT BAR AND PERFORMED OPS CHECK GOOD IAW AMM 52-12-41.

Part: WIRE — DAMAGED (COCKPIT) · airframe 23,649 hrs · 14,622 cycles

EMER LIGHT IN COCKPIT DOES NOT WORK. REPAIRED WIRE NR 1 EMERGENCY LIGHT POWER UNIT TO FWD COCKPIT EMERGENCY LIGHT IAW SWPM 20-41-20, OPS CHECK GOOD IAW AMM 33-50-00.

Part: HANDLE — MISALIGNED (L1 DOOR) · airframe 23,095 hrs · 14,285 cycles

L1 DOOR ARMING HANDLE NOT CLOSING CORRECTLY. ALL INDICATIONS CORRECT, HANDLE MISALIGNED. RE-SECURED GIRT BAR INTO CLAMP AND PERFORMED OPS CHECK IAW AMM 52-12-40.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,317 hrs · 13,827 cycles

LEVEL 2 CORROSION AT WASTE BOX. REMOVED AND REPLACED CORRODED WASTE BOX IAW EMB 170 SRM 51-43-02 AND 51-41-02.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,317 hrs · 13,827 cycles

LEVEL 2 CORROSION RT LOWER SEAT TRACK BEAM (CFI). REMOVED AND REPLACED RT LOWER SEAT TRACK BEAM (CFI) IAW EMB 170 SRM 51-43-00, 57-40-02, 51-43-07, AND 51-43-02.

Part: STRUCTURE — CORRODED (ZONE 100) · airframe 22,318 hrs · 13,827 cycles

CORROSION ON WASTE BOX AND SEPARATING. R & R WASTE BOX.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 22,318 hrs · 13,827 cycles

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

Part: SLIDE — UNSERVICEABLE (CABIN) · airframe 20,583 hrs · 12,696 cycles

AFT RT SLIDE LACING CORD UNDONE. REPLACED AFT RT EVAC SLIDE IAW AMM 25-65-01.

Part: STRUCTURE — LEAKING (LT WING) · airframe 20,039 hrs · 12,347 cycles

SLIGHT ODOR OF JET FUEL NOTICEABLE ON DESCENT, CONTINUED TO GET PROGRESSIVELY STRONGER LOWER. VERY STRONG IN COCKPIT UPON SHUTDOWN, SEEMS TO GET BETTER WHEN DESELECTING PACK 1. FERRIED TO IND. REPAIRED FUEL LEAK FOUND LT WING STUD SPAR 1, NO LEAKS NOTED.

Part: SIGN — UNSECURE (CABIN) · airframe 19,760 hrs · 12,125 cycles

EXIT SIGN BY FWD JUMP SEAT IS FALLING OFF. RE-SECURED EXIT SIGN BY FWD F/A SEAT/L1 DOOR IAW EMB 170 MM 33-50-13.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 19,579 hrs · 12,073 cycles

EMERGENCY LIGHTS CAME ON IN FLIGHT. RESET AC POWER, COULD NOT DUPLICATE IAW EMB 170 MM 24-00-00.

Part: SENSOR — OUT OF ADJUST (SERVICE DOOR)

DOOR SERVICE AFT OPEN MESSAGE IN FLIGHT. MESSAGE WENT OUT ON DESCENT AROUND FL250. FOUND SENSOR OUT OF ADJUSTMENT. REMOVED AND REPLACED AFT SERVICE DOOR WARNING SENSOR.

Part: LANDING GEAR — LOW (NLG) · airframe 18,101 hrs · 11,183 cycles

CREW REPORTED AFTER TAKEOFF LG WOW SYS FAIL MESSAGE AND LANDING GEAR RETRACT LEVER WOULD NOT MOVE. GEAR STAYED DOWN AND GREEN. CREW DECLARED EMERGENCY AND RETURNED TO FIELD, LANDED WITHOUT INCIDENT. MAINTENANCE SERVICED THE NOSE LANDING GEAR, JACKED A/C AND PERFORMED GEAR SWINGS IAW EMB 170 MM 32-33-00.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,231 hrs · 10,630 cycles

LEVEL 2 CORROSION AFT CARGO DOOR CUTOUT LOWER SEAL REST, FRAMES 78-79. REMOVED AND REPLACED AFT CARGO DOOR CUTOUT LOWER SEAL REST IAW EMB 170 SRM 51-41-01.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,231 hrs · 10,630 cycles

LEVEL 2 CORROSION RT FLOORBEAM BETWEEN FR 84 AND FR 85. REMOVED TOP SHEET ON RT FLOORBOARD IAW EMB 170 SRM 51-40-02, FABRICATED TOP SHEET AND INSTALLED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,231 hrs · 10,630 cycles

LEVEL 2 CORROSION RT SEAT TRACK BEAM AT FR 87. REMOVED AND REPLACED SEAT TRACK BEAM AT FR87 IAW EMB 170 SRM 51-41-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,231 hrs · 10,630 cycles

LEVEL 2 CORROSION LT SEAT TRACK BEAM AT FR 17. REMOVED AND REPLACED IAW EMB 170 SRM 51-40-02.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,231 hrs · 10,630 cycles

LEVEL 2 CORROSION SEAL PLATE AT FR 17. INSTALLED SERVICEABLE SILL PER EMB SRM 51-41-00 AND 51-43-04.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,231 hrs · 10,630 cycles

LEVEL 2 CORROSION AT FR90 AND RT SEAT TRACK BEAM. REMOVED AND REPLACED GUSSET AT FR90 AND RT SEAT TRACK IAW EMB 170 SRM 51-40-02 AND 51-41-02.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,231 hrs · 10,630 cycles

LEVEL 2 CORROSION LT SEAT TRACK BEAM BETWEEN FR18 AND FR19. REPLACED LT SEAT TRACK BEAM.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · airframe 17,231 hrs · 10,630 cycles

LEVEL 2 CORROSION SHEAR PLATE BETWEEN RT SEAT TRACK BEAM AND RT CREASE BEAM AND BETWEEN FR87 AND FR88. REMOVED AND REPLACED SHEAR PLATE IAW EMB 170 SRM 51-42-01.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,231 hrs · 10,630 cycles

LEVEL 2 CORROSION SHEAR PLATE BETWEEN LT SEAT TRACK BEAM AND RT SEAT TRACK BEAM BETWEEN FR87 AND FR88. REMOVED AND REPLACED SHEAR PANEL IAW EMB 170 SRM 51-40-02 AND 51-42-00.

Part: CROSSBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,231 hrs · 10,630 cycles

LEVEL 2 CORROSION LT CROSS BEAM AT FR 89. REMOVED AND REPLACED 4 RIVETS ON FR89 ON LT CROSS BEAM IAW EMB 170 SRM 51-41-01. REMOVED AND REPLACED TOP COAT AND FOUND NO SURFACE CORROSON IAW EMB 170 SRM 51-23-02 AND 51-23-06.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,231 hrs · 10,630 cycles

LEVEL 2 CORROSION RT SEAT TRACK BEAM FR 13 TO FR 17. REMOVED AND REPLACED SEAT TRACK IAW EMB 170 SRM 51-40-02.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,231 hrs · 10,630 cycles

LEVEL 2 CORROSION SHEAR PLATE BETWEEN LT SEAT TRACK BEAM AND RT SEAT TRACK BEAM BETWEEN FR87 AND FR 88. REMOVED SHEAR PLATE IAW EMB 170 SRM 51-40-02. DRILLED NEW SHEAR PLATE, INSTALLED IAW SRM 51-40-02.

Part: WIRE HARNESS — DEFECTIVE (LE SLAT) · airframe 14,667 hrs · 9,123 cycles

SLAT FAIL ON EICAS DURING APPROACH. SLATS FAILED IN FULL POSITION. CREW DECLARED EMERGENCY. LANDED UNEVENTFULLY. MAINTENANCE REMOVED AND REPLACED RT SLAT 3/4 HARNESS IAW EMB 170 MM 27-83-07. OPS CHECK GOOD.

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,394 hrs · 7,176 cycles

THREE GUSSETS FOUND WITH LEVEL 2 CORROSION AT FR 90. REPLACED GUSSETS (3) AT FR 90 IAW SRM 51-41-02.

Part: ACM — FAILED (A/C BAY) · airframe 7,819 hrs · 5,033 cycles

FLIGHT 7509 IAD TO ROC ON DESCENT THE CREW SMELLED A BURNING ODOR. FLIGHT ATTENDANTS CONFIRMED A BURNING ODOR IN THE CABIN. CREW SHUT OFF THE RECIRCULATION FANS AND DECLARED AN EMERGENCY. SHORTLY AFTER THE RECIRCULATION FANS WERE SHUT OFF THE SMELL WENT AWAY FOLLOWED BY A -PACK 2 FAIL- EICAS MESSAGE A SHORT TIME LATER. CREW RAN THE QRH PROCEDURE AND TURNED THE NR 2 PACK OFF. FLIGHT LANDED UNEVENTFULLY. MAINTENANCE REPLACED THE NR 2 PACK ACM AND HEAT EXCHANGER.

Part: AUTOTHROTTLE SYS — MALFUNCTIONED (COCKPIT) · airframe 5,172 hrs · 3,370 cycles

FLIGHT 7596 TAKEOFF, AT 40 KNOTS GOT MASTER CAUTION -THRUST LEVERS NOT IN TOGA-. ABORTED THE T/O. PRESSED THE A/T BUTTON BEFORE T/O, BUT IT DID NOT ARM. FAILED TO CHECK ON THE PFD TO MAKE SURE IT ARMED.

Part: ROD — BROKEN (LE FLAPS) · airframe 3,140 hrs · 2,030 cycles

AFTER TAKEOFF IN INITIAL CLIMB BELOW 10000 FT, SELECTED FLAPS FROM POSITION 1 TO UP AND RECEIVED A FLAP DISAGREEMENT THEN FLAP LOW RATE INDICATION AND FINALLY A FAIL FAIL MESSAGE. RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. UPON INSPECTION FOUND 2 FLAP ROD ASSEMBLY’S BROKEN. REMOVED AND REPLACED RODS AND RETURNED AIRCRAFT TO SERVICE.

Part: SLIDE — UNSERVICEABLE (CABIN) · airframe 33 hrs · 18 cycles

DURING FAA EMERGENCY EVACUATION DEMONSTRATION, THE FORWARD RIGHT EMERGENCY EXIT SLIDE DEPLOYED PRIOR TO THE EXIT DOOR FULLY OPENING. THE SLIDE DEPLOYED SIDEWAYS AND LODGED BETWEEN THE EXIT DOOR AND THE FUSELAGE BELOW THE FIRST OFFICER'S SIDE WINDOW RENDERING IT UNUSABLE. REMOVED AND REPLACED EMERGENCY EVACUATION SLIDE ASSY IAW EMB 170MM 25-65-07.