N648RW

Part: SEAT TRACK — CORRODED (FRMS 74-84) · corrosion level 2 · airframe 46,583 hrs · 29,018 cycles

DURING HEAVY CHECK MAINTENANCE FOUND CORRODED RH IB SEAT TRACK AT CFIII BETWEEN FR74-84. CORRODED HR IB SEAT TRACK SEAT TRACK AT CFIII BETWEEN FR74-84 REMOVED AND REPLACED IAW EMB 170 SRM 51-43-03, 51-43-04.

Part: SKIN — CORRODED (LT WING TE) · corrosion level 2 · airframe 46,583 hrs · 29,018 cycles

DURING HEAVY CHECK MAINTENANCE FOUND RH WING TRAILING EDGE RIB 11 FOUND TO HAVE A CRACK ON THE UPPER SKIN PANEL. RH WING TRAILING EDGE RIB 11 CRACK ON THE UPPER SKIN PANEL REPAIRED IAW ETD2024-170-009342. HFEC CARRIED OUT WITH NO DEFECTS NOTED.

Part: SHEAR PANEL — CORRODED (FRM 16 LBL10) · corrosion level 2 · airframe 46,583 hrs · 29,018 cycles

DURING HEAVY CHECK MAINTENANCE FOUND FWD WET AREA FLOOR STRUCTURE DISCOVERED CORROSION AND POSSIBLE CRACKED FASTENER HEAD ON THE SHEAR PANEL UPPER SURFACE AT FR16, LBL 10. SHEAR PANEL ON FLOOR STRUCTURE AT LBL 10, FR16 WAS REPLACED IAW SRM 51-41-02 WITH FASTENERS REPLACED ON SHEAR PANEL UPPER SURFACE IAW SRM 51-41-02.

Part: PANEL — CRACKED (MLG WW) · corrosion level 2 · airframe 46,583 hrs · 29,018 cycles

DURING HEAVY CHECK MAINTENANCE FOUND INSPECTION OF A PREVIOUS REPAIR OF THE STRUCTURE THAT HOLDS THE SPIN BRAKE BRACKETS IN THE NOSE WHEEL WELL FOUND THAT THERE IS A REPAIR STRAP INSTALLED, MISSING FILLET SEALANT, A GAP BETWEEN A FASTENER HEAD AND THE REPAIR AND A GAP BETWEEN THE DOUBLER AND THE A/C STRUCTURE THAT IS NOT CONSISTENT WITH THE INSTRUCTIONS FOR REPAIR PER EDT2022-170-030541. PREVIOUS REPAIR WAS REMOVED AND REPAIRED AGAIN IAW ETD2022-170-030841.

Part: SKIN — MISREPAIRED (ZONE 100) · airframe 46,583 hrs · 29,018 cycles

DURING HEAVY CHECK MAINTENANCE FOUND EXTERIOR SKIN REPAIR DOUBLER BELOW THE AFT PASSENGER DOOR THRESHOLD AT FR85-86, STGR 19L-22L THE FIRST FASTENER AFT OF FR86 AND BELOW STGR 21L IS IN THE CHEM-MIL AREA. EXTERIOR SKIN DOUBLER BELOW THE AFT PASSENGER DOOR THRESHOLD AT FR85-86, STGR 19L-22L THE FIRST FASTENER AFT OF FR86 AND BELOW STGR 21L SPOT FACE HAS BEEN CARRIED OUT IAW SRM 51-10-08 AND ETD2024-170-005314.

Part: STRUCTURE — CRACKED (ZONE 100) · airframe 46,382 hrs · 28,841 cycles

LH NLG SPIN BRAKE WEBBING FOUND CRACKED AND PREVIOUSLY STOP DRILLED. CRACK PROGRESSED BEYOND PREVIOUS STOP DRILL. REPAIRED DAMAGE IAW ETD2022-170-030541 REV. B.

Part: ACM — FAILED (ZONE 100) · airframe 46,289 hrs · 28,765 cycles

ON TAXI OUT, AIR TEMP IN CABIN ROSE RAPIDLY ALONG WITH A STRONG SMELL OF SMOKE THROUGHOUT THE CABIN. THIS WAS FOLLOWED BY A PACK 1 FAIL EICAS MESSAGE. R&R LH ACM.

Part: SENSOR — ABNORMAL (ZONE 700) · airframe 45,515 hrs · 28,225 cycles

LANDING GEAR WOULD NOT COME UP AFTER TAKEOFF. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. COMPLIED WITH 170EI-32-60-0025. FOUND RH WOFW #1 SENSOR OUT OF TOLERANCE. ADJUSTED SENSOR IAW AMM 32-32-03 AND COMPLETED WIRING CHECKS IAW FIM 32-61-00-810-847-A. NO FAULTS FOUND.

Part: GUSSET — CORRODED (ZONE 200) · corrosion level 2 · airframe 44,692 hrs · 27,688 cycles

DURING HEAVY CHECK MAINTENANCE FOUND CFIII, FR90 RH OB GUSSET PLATE CORRODED. CFIII, FR90 RH OB GUSSET PLATE REPLACED IAW EMB SRM 51-41-02.

Part: SHEAR PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,692 hrs · 27,688 cycles

WHILE AC WAS IN FOR HVY CK FOUND INTERIOR FUSELAGE FWD CARGO SHEAR CLIP ON FR 16 BTWN STR 28-27R FOUND CORRODED. MX REPLACED SHEAR CLIP PN 170-03859-002 IAW SRM 51-41-01 SEE AAR NRC# 4500970-1000-0182 FOR WORK PERFORMED. AC WAS RTS

Part: SHEAR ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,692 hrs · 27,688 cycles

DURING HEAVY CHECK MAINTENANCE FOUND INTERIOR FUSELAGE, FWD CARGO SHEAR CLIP ON FR17 BETWEEN STR 28-27L CORRODED. INTERIOR FUSELAGE, FWD CARGO SHEAR CLIP ON FR17 BETWEEN STR 28-27L REPLACED IAW SRM 51-41-02.

Part: SHEAR PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,692 hrs · 27,688 cycles

WHILE AC WAS IN FOR HVY CK FOUND INTERIOUR FUSELAGE FWD CARGO SHEAR CLIP ON FR 16 BTWN STR 28-27L FOUND CORRODED. MX REPLACED SHEAR CLIP PN 170-03859-001 IAW SRM 51-41-01, 51-41-02. SEE AAR NRC# 4500970-1000-0180 FOR WORK PERFORMED. AC WAS RTS.

Part: SHEAR ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,692 hrs · 27,688 cycles

DURING HEAVY CHECK MAINTENANCE FOUND INTERIOR FUSELAGE FWD CARGO SHEAR CLIP ON FR17 BETWEEN STR 28-27R CORRODED. INTERIOR FUSELAGE FWD CARGO SHEAR CLIP ON FR17 BETWEEN STR 28-27R REPLACED IAW SRM 51-41-01.

Part: GUSSET — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,692 hrs · 27,688 cycles

DURING HEAVY CHECK MAINTENANCE FOUND CFIII, GUSSET PLATE AFT FR90 RBL 25 CORRODED. CFIII, GUSSET PLATE AFT FR90 RBL 25 REPLACED IAW 51-41-02.

Part: SHEAR PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,692 hrs · 27,688 cycles

WHILE AC WAS IN FOR HVY CK FOUND CF3 RH SHEAR WEB BTWN FR 87-88 FOUND CORRODED. MX REPLACED SHEAR PANEL PN 170-91919-001 IAW SRM 51-42-01, 51-43-03 SEE AAR NRC# 45000970-1000-0053 FOR WORK PERFORMED. AC WAS RTS.

Part: SHEAR PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,692 hrs · 27,688 cycles

WHILE AC WAS IN FOR HVY CK FOUND CF3 CENTER SHEAR WEB BTWN FR 87-88 FOUND CORRODED. MX REPLACED SHEAR PANEL PN 170-65928-001 IAW SRM 51-42-01. SEE AAR NRC # 4500970-1000-0052 FOR WORK PERFORMED. AC WAS RTS.

Part: RIB — CRACKED (ZONE 300) · airframe 44,692 hrs · 27,688 cycles

DURING HEAVY CHECK MAINTENANCE FOUND RH HORIZONTAL STAB RIB 11 CRACKED. RH HORIZONTAL STAB RIB REPLACED IAW SRM 51-40-08. REF AAR TASKCARD 4500469-3000-0071

Part: DOOR — UNKNOWN (L1) · airframe 42,614 hrs · 26,289 cycles

MAIN CABIN DOOR STICKY AND VERY HARD TO OPEN. PERFORMED OPERATIONAL CHECK OF L1 DOOR, OPS CHECK GOOD PER AMM 52-11-00

Part: DOUBLER — CORRODED (ZONE 200) · corrosion level 2 · airframe 39,988 hrs · 24,670 cycles

MAINTENANCE FOUND LEVEL 2 CORROSION AT AFT LAVATORY AFT INBOARD AND OUTBOARD TOILET ATTACHMENTS ON LAVATORY FLOOR. MAINTENANCE FABRICATED AND INSTALLED 4EA. AFT LAVATORY FLOOR DOUBLERS REF. EMBRAER DRAWINGS 170-43684-001 AND 170-43685-001 AND EMB SRM 51-40-02, AMM 20-10-01. APPLIED ALODINE AND PRIMER TO 4EA. AFT LAVATORY FLOOR DOUBLERS REF. EMB SRM 51-23-04,51-23-05. AIRCRAFT REMAINS IN HEAVY CHECK FOR DURATION OF THE CHECK.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,988 hrs · 24,670 cycles

**WHILE IN HEAVY CHECK** MAINTENANCE FOUND LEVEL 2 CORROSION FOUND INBOARD GALLEY SUPPORT AFTER REMOVAL OF RT SHEAR PANEL AT FR 87-88. MAINTENANCE REMOVED DAMAGED FR 87-88 INBOARD GALLEY SUPPORT. LOCATED, DRILLED AND INSTALLED NEW FR 87-88 INBOARD GALLEY SUPPORT. REF SRM 51-40-08. AIRCRAFT REMAINS IN HEAVY CHECK FOR DURATION OF THE CHECK.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,988 hrs · 24,670 cycles

**WHILE IN HEAVY CHECK** MAINTENANCE FOUND LEVEL 2 CORROSION AFTER REMOVAL OF RT SHEAR PANEL AT FR 87-88, FOUND OUTBOARD GALLEY SUPPORT. MAINTENANCE REMOVED DAMAGED FR 87-88 OUTBOARD GALLEY SUPPORT. LOCATED, DRILLED AND INSTALLED NEW FR 87-88 INBOARD GALLEY SUPPORT. REF SRM 51-40-08. AIRCRAFT REMAINS IN HEAVY CHECK FOR DURATION OF THE CHECK.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 39,988 hrs · 24,670 cycles

DURING HEAVY CHECK MAINTENANCE FOUND SUSPECT CRACK AT RIB 11 LH HORIZONTAL STABILIZER. REMOVED AND REPLACE RIB 11 IN LH HORIZONTAL STABILIZER REF 51-40-08. A/C REMAINS IN CHECK.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 39,988 hrs · 24,670 cycles

DURING HEAVY CHECK MAINTENANCE SUSPECT CRACK AT RIB 11 RH HORIZONTAL STABILIZER. REMOVED AND REPLACED RIB AT FR 11 R/H HORIZONTAL STABILIZER. REF: SRM 51-40-08. A/C REMAINS IN CHECK.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 39,988 hrs · 24,670 cycles

DURING HEAVY CHECK MAINTENANCE FOUND SUSPECT CRACK AT RIB 12 RH HORIZONTAL STABILIZER. REMOVED AND REPLACED RIB AT FR12A ON R/H HORIZONTAL STABILIZER AND APLLIED TOPCOAT TO SURFACE FASTENERS AT RH HORIZONTAL STABILIZER,REF SRM 51-23-06, 51-40-08. A/C REMAINS IN CHECK.

Part: SUPPORT BRACKET — CORRODED (ZONE 100) · corrosion level 2 · airframe 39,988 hrs · 24,670 cycles

MAINTENANCE FOUND LEVEL 2 SURFACE CORROSION ON SUPPORT BRACKET ON PANEL 195FL. MAINTENANCE REMOVED CORRODED SUPPORT BRACKET ON PANEL 195FL. FABRICATED, LOCATED , DRILLED AND INSTALLED NEW SUPPORT BRACKET REF EMB SRM 51-30-00, 51-40-02, 51-23-04, 51-23-05, 51-23-06 AND AMM 20-10-01. AIRCRAFT REMAINS IN HEAVY CHECK FOR DURATION OF THE CHECK.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,988 hrs · 24,670 cycles

**WHILE IN HEAVY CHECK** MAINTENANCE FOUND LEVEL 2 CORROSION LT SEAT TRACK FR 18-19. MAINTENANCE REMOVED DAMAGED PART AND FABRICATED REPAIR PARTS FOR LT SEAT TRACK BETWEEN FRAMES 18 AND 19 IAW SRM 53-10-10-REPAIR 03 LOCATED, DRILLED ,ALODINED AND INSTALLED REPAIR PARTS REF SRM 51-40-02,51-23-04. AIRCRAFT REMAINS IN HEAVY CHECK FOR DURATION OF THE CHECK.

Part: CROSSBEAM — CORRODED (FRAME 84) · corrosion level 2 · airframe 39,988 hrs · 24,670 cycles

DURING HEAVY CHECK MAINTENANCE FOUND CORROSION- RH CROSSBEAM AT FR 84 AS MARKED. PERFORMED PERMANENT REPAIR ON CROSSBEAM FR84 R/H SIDE BY L-ANGLE REPAIR AND RESTORED SURFACE PROTECTION IN ACCORDANCE WITH, REF ETD2019-170-066925. A/C REMAINS IN CHECK.

Part: PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,988 hrs · 24,670 cycles

**WHILE IN HEAVY CHECK** MAINTENANCE FOUND LEVEL 2 CORROSION AT RT O/B GUSSET PLATE (TEXAS) AT FR 90. MAINTENANCE REMOVED AND REPLACED RT O/B GUSSET PLATE (TEXAS) AT FR 90 REF SRM 51-40-08. RESTORED SURFACE PROTECTION TO RT O/B GUSSET PLATE (TEXAS) AT FR 90 REF. SRM 51-23-05. AIRCRAFT REMAINS IN HEAVY CHECK FOR DURATION OF THE CHECK.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,988 hrs · 24,670 cycles

**WHILE IN HEAVY CHECK** MAINTENANCE FOUND LEVEL 2 CORROSION RT SILL FR 13-14. MAINTENANCE REMOVED AND REPLACED RT SILL FR 13-14 IAW SRM 51-40-08. RESTORED SURFACE PROTECTION TO RT SILL FR 13-14 SRM 51-23-06. AIRCRAFT REMAINS IN HEAVY CHECK FOR DURATION OF THE CHECK.

Part: SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,988 hrs · 24,670 cycles

**WHILE IN HEAVY CHECK** MAINTENANCE FOUND LEVEL 2 CORROSION AT SPLICE AT FR 90. MAINTENANCE REMOVED AND REPLACED SPLICE AT FR 90 REF SRM 51-40-02, 51-40-08, 51-23-05, 51-23-06, AND CPM 51-25-00. AIRCRAFT REMAINS IN HEAVY CHECK FOR DURATION OF THE CHECK.

Part: SUPPORT BRACKET — CORRODED (ZONE 100) · corrosion level 2 · airframe 39,988 hrs · 24,670 cycles

MAINTENANCE FOUND LEVEL 2 SURFACE CORROSION ON SUPPORT BRACKET OF PANEL 195ER. MAINTENANCE REMOVED AND REPLACED SUPPORT BRACKED ON PANE 195ER PER AMM 20-10-01, 51-40-02. AIRCRAFT REMAINS IN HEAVY CHECK FOR DURATION OF THE CHECK.

Part: SHEAR PANEL — CORRODED (FRAMES 87-88) · corrosion level 2 · airframe 39,988 hrs · 24,670 cycles

DURING HEAVY CHECK MAINTENANCE FOUND CORROSION- RT SHEAR PANEL FR 87-88. REMOVED AND REPLACED RH SHEAR PANEL AT FR 87-88 AS MARKED REF. EMB SRM 51-43-03 AND 51-42-03. RESTORED SURFACE PROTECTION TO RH SHEAR PANEL AT FR 87-88 AS MARKED REF. EMB SRM 51-23-06. A/C REMAINS IN CHECK.

Part: BEAM — CORRODED (L2 DOORWAY) · corrosion level 2 · airframe 39,988 hrs · 24,670 cycles

DURING HEAVY CHECK MAINTENANCE FOUND CORROSION ON FWD AND AFT GIRT BAR CUTOUT EDGES. REMOVED AND REPLACED L2 DOOR LOWER BEAM. REF: SRM 51-40-08. A/C REMAINS IN CHECK.

Part: SHEAR TIE — CORRODED (FRAME 86) · corrosion level 2 · airframe 39,988 hrs · 24,670 cycles

DURING HEAVY CHECK MAINTENANCE FOUND CORROSION- SHEARCLIP FR 86 BETWEEN STGR 27R- STGR 28R. REMOVED AND REPLACED INTERCOASTAL /SHEAR CLIP FR 86 BETWEEN STGR 27R- STGR 28R REF EMB SRM 51-40-08. A/C REMAINS IN CHECK

Part: SEAT TRACK — CORRODED (FRAME 17) · corrosion level 2 · airframe 39,988 hrs · 24,670 cycles

DURING HEAVY CHECK MAINTENANCE FOUND CORROSION- RH SEAT TRACK AT FR 17 (3 EA. FASTENERS). PERFORMED PERMANENT REPAIR ON RH SEAT TRACK AT FR17 REF SRM 53-10-10 REPAIR/01.

Part: BEAM — CORRODED (L1 DOORWAY) · corrosion level 2 · airframe 39,988 hrs · 24,670 cycles

DURING HEAVY CHECK MAINTENANCE FOUND L1 DOOR LOWER BEAM CORROSION AROUND GIRT BAR FITTINGS AS MARKED. REMOVED AND REPLACED L1 DOOR BEAM REF SRM 51-40-08. A/C REMAINS IN CHECK.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,988 hrs · 24,670 cycles

**WHILE IN HEAVY CHECK** MAINTENANCE FOUND LEVEL 2 CORROSION AT LT DOUBLER FR 19-20. REMOVED AND REPLACED LT DOUBLER FR 19-20. SRM 51-40-08. RESTORED SURFACE PROTECTION TO LT DOUBLER FR 19-20 REF. SRM 51-23-06.AIRCRAFT REMAINS IN HEAVY CHECK FOR DURATION OF THE CHECK.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,988 hrs · 24,670 cycles

**WHILE IN HEAVY CHECK** MAINTENANCE FOUND LEVEL 2 CORROSION AT SHEAR CLIP FR 85 BETWEEN STR 27R- STR 28R. MAINTENANCE REMOVED AND REPLACED SHEARCLIP AT FR 85 BETWEEN STR 27R- STR 28R REF. SRM 51-40-08. RESTORED SURFACE PROTECTION TO SHEAR CLIP AT FR 85 BETWEEN STR 27R- STR 28R REF. SRM 51-23-06. AIRCRAFT REMAINS IN HEAVY CHECK FOR DURATION OF THE CHECK.

Part: FLOOR SUPPORT — CORRODED (FRAMES 88-89) · corrosion level 2 · airframe 39,988 hrs · 24,670 cycles

DURING HEAVY CHECK MAINTENANCE FOUND CORROSION- RH PANEL SUPPORT FR 88-89 AS MARKED. REMOVED AND REPLACED RH PANEL SUPPORT FR 88-89 AS MARKED REF. EMB SRM 51-40-08. RESTORED SURFACE PROTECTION TO RH PANEL SUPPORT FR 88-89 AS MARKED REF. EMB SRM 51-23-06. A/C REMAINS IN CHECK.

Part: CROSSBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,988 hrs · 24,670 cycles

**WHILE IN HEAVY CHECK** MAINTENANCE FOUND LEVEL 2 CORROSION AT RT CROSSBEAM FR 14. MAINTENANCE REPAIRED RT CROSSBEAM FR 14 BY REMOVING DAMAGE AND INSTALLING REPAIR DOUBLER AND FILLER REF. SRM 53-00-10/REPAIR 03. RESTORED SURFACE PROTECTION TO REPAIR ON RT CROSSBEAM FR 14 REF. SRM 51-23-06. AIRCRAFT REMAINS IN HEAVY CHECK FOR DURATION OF THE CHECK.

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,988 hrs · 24,670 cycles

**WHILE IN HEAVY CHECK** MAINTENANCE FOUND LEVEL 2 CORROSION AT RT I/B GUSSET PLATE AT FR 90. MAINTENANCE REMOVED AND REPLACED RT I/B GUSSET PLATE AT FR 90 REF SRM 51-40-02, 51-40-08, 51-23-05 AND CPM 51-25-00. AIRCRAFT REMAINS IN HEAVY CHECK FOR DURATION OF THE CHECK.

Part: ROLLER — LACK OF LUBE (L1 DOOR) · airframe 39,855 hrs · 24,590 cycles

L1 MAIN CABIN DOOR STICKY. LUBRICATED L1 DOOR ROLLERS AND OPS CHECKED L1 DOOR IAW CMM 52-11-22.

Part: GIRT BAR — LACK OF LUBE (L2 DOOR) · airframe 36,173 hrs · 22,374 cycles

L2 DOOR ARMING LEVER VERY HARD FOR FLIGHT ATTENDANT TO MOVE FOR ARMING AND DISARMING. LUBRICATED L2 DOOR GIRT BAR IAW AMM 52-12-41. OPS CHECK GOOD.

Part: GIRT BAR — OUT OF ADJUST (L2 DOOR SLIDE) · airframe 34,540 hrs · 21,334 cycles

L2 DOOR WILL NOT ENGAGE GIRT BAR. ADJUSTED L2 DOOR EMERGENCY EVACUATION SLIDE MECHANISM IAW AMM 52-12-40.

Part: SEAT TRACK — CORRODED (FRAMES 79-80) · corrosion level 2 · airframe 34,538 hrs · 21,333 cycles

DURING HEAVY CHECK, FOUND THE LT INBD SEAT TRACK BETWEEN FRAMES 79 AND 80 CORRODED. MX REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-10-03, 52-23-10, 51-40-02, 51-40-03, AND 51-43-03,

Part: SEAT TRACK — CORRODED (FRAME 86) · corrosion level 2 · airframe 34,538 hrs · 21,333 cycles

DURING HEAVY CHECK, FOUND THE SEAT TRACK AT FRAME 86, RBL 10 CORRODED. MX REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-40-01, AND 51-40-03.

Part: FLOOR SUPPORT — CORRODED (FRAME 90) · corrosion level 2 · airframe 34,538 hrs · 21,333 cycles

WHILE ACFT WAS IN FOR HEAVY CHECK, FOUND THE FLOOR SUPPORT AT FRAME 90, RBL 10 HAS CORROSION. MX REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-41-01,

Part: SHEAR PANEL — CORRODED (FRAME 87) · corrosion level 2 · airframe 34,538 hrs · 21,333 cycles

WHILE ACFT WAS IN FOR HEAVY CHECK, FOUND THE SHEAR PANEL AT FR 87, RBL 20 HAS CORROSION AROUND MOUNT HOLES. MX REMOVED AND REPLACED THE SHEAR PANEL IAW SRM 53-23-10, 51-40-01, 51-40-02, AND 51-42-01.

Part: FLOORBEAM — CORRODED (FRAME 87) · corrosion level 2 · airframe 34,538 hrs · 21,333 cycles

WHILE ACFT WAS IN FOR HEAVY CHECK, FOUND FLOORBEAM AT FRAME 87, RBL 10 HAS CORROSION. MX REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-40-01, 51-40-02, 51-41-01, AND 51-43-03.

Part: SHEAR PANEL — CORRODED (FRAME 87) · corrosion level 2 · airframe 34,538 hrs · 21,333 cycles

WHILE AC WAS IN FOR HEAVY CHECK, FOUND THE SHEAR PANEL AT FRAME 87, LBL 32 HAS CORROSION. MX REMOVED AND REPLACED THE SHEAR PANEL IAW SRM 51-75-16, 51-42-01, AND 51-42-02,

Part: SEAT TRACK — CORRODED (FRAME 84) · corrosion level 2 · airframe 34,538 hrs · 21,333 cycles

MAINTENANCE REPORTED CORROSION ON THE RT INBOARD SEAT TRACK CROWN AT FRAME 84. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK BETWEEN FRAME 79 TO 84 IAW SRM 53-23-10, 51-40-02, & 51-43-03.

Part: CIRCUIT BOARD — FAILED (EMERGENCY LIGHTS) · airframe 32,612 hrs · 20,070 cycles

MAINTENANCE REPORTED THAT AFTER THE FOWARD FLIGHT ATTENDANT PSU TEST AND RESET, ROWS 15 C & D AND 16 C & D BLUE RAINBOW LIGHTS WOULD NOT EXTINGUISH. REMOVED AND REPLACED PRINTED CIRCUIT BOARDS AT SEATS 15 C & D AND 16 C & D PER EMB AMM AND OPS CHECKED GOOD.

Part: PRINTED CKT BOARD — INOPERATIVE (CABIN) · airframe 32,240 hrs · 19,844 cycles

CREW REPORTED THAT THE PSU BLUE LIGHTS WERE STAYING ON. MAINTENANCE PLACED ON MEL IAW AMM. MAINTENANCE REMOVED AND REPLACED PSU PCB PER EMB AMM AND OPS CHECKED GOOD.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHT) · airframe 30,181 hrs · 18,544 cycles

THE FWD EMERGENCY EXIT LOCATOR SIGN IS INOPERATIVE. SECURED CONNECTOR AT FWD EMERGENCY EXIT LOCATOR SIGN IAW AMM 33-50-19.

Part: DOOR — MALFUNCTIONED (ZONE 800) · airframe 29,837 hrs · 18,302 cycles

L1 DOOR WILL NOT STAY LOCKED IN THE OPEN POSITION. L1 HOOK ASSEMBLY SPRING CLEANED AND LUBRICATED. MECHANISM EXCERCISED FOR MOVEMENT, NO OBSTRUCTION NOTED. DOOR HOOK FUNCTIONS OPERATES NORMALLY.

Part: DOUBLER — CORRODED (ZONE 100) · airframe 28,714 hrs · 17,560 cycles

CORROSION FOUND ON THE AFT HOT WATER DRAIN MAST. R & R THE DOUBLER.

Part: FITTING — CORRODED (ZONE 100) · airframe 28,714 hrs · 17,560 cycles

CORROSION FOUND ON THE PAX DOOR CUTOUT AREA AT 6 O'CLOCK POSITION AREA UNDER METALLIC SCUFF PLATE. R & R FITTING.

Part: FINGER DOUBLER — CORRODED (ZONE 100) · corrosion level 2 · airframe 28,714 hrs · 17,560 cycles

CORROSION, FWD FINGER DOUBLER FWD CARGO. R & R DOUBLER.

Part: SHEAR TIE — CORRODED (FRAME 88) · airframe 28,714 hrs · 17,560 cycles

CORROSION FOUND ON THE SHEAR TIE FRAME 88, STRINGER 27-28R. R & R THE SHEAR TIE.

Part: SUPPORT — CORRODED (FAIRING) · corrosion level 2 · airframe 28,714 hrs · 17,560 cycles

CORROSION ALONG AFT LOWER FLANGES OF FWD BELLY FAIRING ATTACHMENT TO FUSELAGE. R & R SUPPORTS, PN 170-02456-001, 170-12603-002, 170-12603-001.

Part: INTERCOSTAL — CORRODED (ZONE 100) · corrosion level 2 · airframe 28,714 hrs · 17,560 cycles

CORRODED INTERCOSTAL BETWEEN STGR 27-38R FWD SIDE OF THE DRAIN MAST ASSY, UNDER RT SIDE OF POTABLE WATER TANK. R & R INTERCOSTAL, PN 170-87560-001.

Part: SHEAR TIE — CORRODED (FRAME 88) · airframe 28,714 hrs · 17,560 cycles

CORROSION ON THE SHEAR TIE FRAME 88, STRINGERS 27-28R. R & R THE SHEAR TIE.

Part: PLATE — CORRODED (ZONE 100) · airframe 28,714 hrs · 17,560 cycles

CORROSION FOUND ON THE FWD GALLEY INBD WALL LOWER PLATE. R & R THE DOUBLER.

Part: FINGER DOUBLER — CORRODED (ZONE 100) · airframe 28,714 hrs · 17,560 cycles

CORROSION ON FWD FINGER DOUBLER FWD CARGO. R & R THE FINGER DOUBLER.

Part: DOUBLER — CORRODED (ZONE 100) · corrosion level 2 · airframe 28,714 hrs · 17,560 cycles

CORROSION FOUND ON LT FLOOR DOUBLER FRAMES 12 - 16. R & R DOUBLER.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 28,714 hrs · 17,560 cycles

CORROSION, RT GUSSET PLATE FRAME 90. R & R PANEL SUPPORT.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 28,714 hrs · 17,560 cycles

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

Part: SPLICE — CORRODED (ZONE 100) · airframe 28,714 hrs · 17,560 cycles

CORROSION FOUND ON THE LT SPLICE, FR 88-87 AT OBTD END OF LT SHEAR PANEL. R & R THE SPLICE.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 28,714 hrs · 17,560 cycles

CORROSION FOUND ON THE LT FLOOR SUPPORT FRAME 84. R & R THE FLOOR SUPPORT.

Part: SHEAR PLATE — CORRODED (FRAMES 87-88) · corrosion level 2 · airframe 28,714 hrs · 17,560 cycles

CORROSION FOUND ON LEFT SHEAR PANEL FRAMES 87-88. R & R SHEAR PANEL.

Part: BEAM — CORRODED (SERVICE DOOR) · airframe 28,714 hrs · 17,560 cycles

CORROSION FOUND ON THE AFT SERVICE DOOR AROUND FWD AND AFT FLOOR GIRT BAR FITTING. R & R BEAM.

Part: GUSSET — CORRODED (FRAME 90) · airframe 28,714 hrs · 17,560 cycles

CORROSION FOUND ON THE RT GUSSET PLATE FRAME 90. R & R THE GUSSET .

Part: SHEAR PLATE — CORRODED (FRAMES 87-88) · airframe 28,714 hrs · 17,560 cycles

CORROSION FOUND ON RT SHEAR PANEL FRAMES 87-88. R & R SHEAR PANEL.

Part: FRAME SPLICE — CORRODED (FRAME 90) · airframe 28,714 hrs · 17,560 cycles

CORROSION FOUND ON CENTER SPLICE FRAME 90. R & R THE FRAME SPLICE.

Part: FLOOR SUPPORT — CORRODED (FRAMES 88-90) · corrosion level 2 · airframe 28,714 hrs · 17,560 cycles

CORROSION FOUND ON THE LT FLOOR SUPPORT FRAME 88 - 90. R & R THE FLOOR SUPPORT.

Part: PAD — CORRODED (DOOR LATCH) · airframe 28,714 hrs · 17,560 cycles

AFT LAVATORY WASTE PANEL LATCH PADS ARE CORRODED. R & R SHIMS, PN 170-85102-001.

Part: LIGHT — INOPERATIVE (ZONE 100) · airframe 28,541 hrs · 17,460 cycles

EMERGENCY LIGHT ADJACENT TO 1C NOT CHARGING. REPLACED THE EMERGENCY LIGHT IAW AMM 33-50-21. OPS CHECKED GOOD.

Part: HANDLE — DIRTY (R1 DOOR ARMING) · airframe 27,090 hrs · 16,580 cycles

R1 ARMING HANDLE VERY STIFF. PERFORMED CLEANING ON R1 DOOR POCKET FITTINGS IAW AMM 52-41-00. OPS CHECKED GOOD.

Part: SENSOR — OUT OF ADJUST (NLG WOW) · airframe 27,083 hrs · 16,573 cycles

STEERING FAILED AND WOW FAILED DURING APPROACH. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. CONDUCTED STEERING ADJUSTMENT TEST IAW AMM 32-50-00. ALL PARAMETERS WITH NORMAL RANGE, NO DEFECTS FOUND. TROUBLESHOT SYSTEM. INTERROGATED CMC COMPUTER AND FOUND FAULT CODES 32611306 PSS AND 32612306 PSS NLG WOW 1 AND 2 SENSOR/TARGET DISAGREE. IAW FIMS 32-61-00-810-840-A AND 32-61-00-810-890-A, CONDUCTED TEST/ADJUSTMENT OF NLG SENSORS. TEST GOOD IAW AMM 32-62-01-820-801.

Part: WIRE HARNESS — DAMAGED (L2 DOOR) · airframe 26,307 hrs · 16,151 cycles

DURING TAXI, RECEIVED AN AFT PAX DOOR OPEN EICAS MESSAGE. MFD SHOWED L2 DOOR OPEN. AT GATE, INDICATES YELLOW X OVER L2 DOOR. R & R L2 DOOR ELECTRICAL HARNESS IAW AMM 52-72-21, OPS CHECKED GOOD.

Part: DOOR — LACK OF LUBE (R2) · airframe 25,765 hrs · 15,840 cycles

R2 DOOR IS TOUGH TO ARM/DISARM. LUBRICATED R2 DOOR HANDLE, OPS CHECK GOOD IAW AMM 52-42-00.

Part: GIRT BAR — FROZEN (R2 DOOR) · airframe 25,590 hrs · 15,743 cycles

R2 SERVICE DOOR WILL NOT OPEN IAW AMM 12-22-01, ICE REMOVED FROM GIRT BAR BRACKETS. DOOR OPERATIONS CHECK OK.

Part: HANDLE — LACK OF LUBE (SLIDE ARMING) · airframe 25,243 hrs · 15,524 cycles

FWD RIGHT SERVICE DOOR ARM LEVER TIGHT, HARD TO ARM. CLEANED AND LUBED ARMING HANDLE, OPS CHECKED GOOD IAW AMM 52-42-22.

Part: LINKAGE — LACK OF LUBE (R1 DOOR) · airframe 25,045 hrs · 15,399 cycles

F/A REPORTS R1 DOOR VENT FLAP AND ARMING HANDLE VERY DIFFICULT TO OPERATE. LUBED LINKAGE AND ROLLERS, OPS CHECK GOOD IAW AMM 52-11-25.

Part: UNKNOWN — ODOR (CABIN) · airframe 24,998 hrs · 15,363 cycles

ELECTRICAL BURNING ODOR DURING FLIGHT AND POST FLIGHT, NOTICEABLE BY F/A'S IN CABIN. PERFORMED FIM 21-20-00-810-801-A, NO ABNORMAL ODOR OR SMOKE NOTED IN CABIN OR COCKPIT.

Part: DOOR — BINDING (L1) · airframe 24,545 hrs · 15,095 cycles

MAIN CABIN DOOR STUCK OPEN. INSPECTED L1 DOOR AND FOUND NO DAMAGE IAW AMM 52-11-22. OPS CHECKED GOOD.

Part: WIRE HARNESS — DAMAGED (ZONE 800) · airframe 23,958 hrs · 14,751 cycles

L2 DOOR INDICATING A YELLOW CIRCLE WITH A BLACK X ON MFD. R & R AFT PASSENGER DOOR WARNING SENSOR HARNESS, OPS CHECK GOOD IAW AMM 52-72-21.

Part: DOOR FRAME — CORRODED (L2 DOORWAY) · corrosion level 2 · airframe 23,438 hrs · 14,406 cycles

CORROSION DAMAGE FOUND IN L1 LOWER ENTRY WAY FWD FRAME. R & R L2 DOOR FRAME IAW SRM 51-41-00.

Part: DOOR FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 23,434 hrs · 14,402 cycles

CORROSION ON L2 DOOR FRAME LOWER ENTRY WAY. R & R L2 DOOR LOWER FRAME.

Part: STRUCTURE — DAMAGED (HORIZONTAL STAB) · airframe 23,434 hrs · 14,402 cycles

LT HORIZONTAL STABILIZER SPHERICAL BEARING HOUSING FOUND TO BE OUT OF LIMITS ON INNER BORE. R & R LH HORIZONTAL STABILIZER SPHERICAL BEARING HOUSING. MAJOR REPAIR

Part: STRUCTURE — DAMAGED (HORIZONTAL STAB) · airframe 23,434 hrs · 14,402 cycles

RT HORIZONTAL STABILIZER SPHERICAL BEARING HOUSING FOUND TO BE OUT OF LIMITS ON INNER BORE. R & R RT HORIZONTAL STABILIZER SPHERICAL BEARING HOUSING. MAJOR REPAIR.

Part: UNKNOWN — ODOR (ZONE 100) · airframe 22,302 hrs · 13,739 cycles

ODD SMELL (NOT DE-ICE FLUID) ON ADVANCING THRUST LEVERS FOR TAKEOFF, LASTED THE REST OF FLIGHT. RAN BLEEDS AND PACKS IN VARIOUS CONFIGURATIONS AT HIGH POWER IAW EMB 170 MM 21-00-00 AND GE MM 71-00-01. NO BAD ODOR NOTED.

Part: UNKNOWN — ODOR · airframe 22,011 hrs · 13,553 cycles

FOUL ODOR COMING FROM ECS SYSTEM, PRESENT SHORTLY AFTER TAKEOFF, CLEARS IN CRUISE, THEN AGAIN DURING DESCENT. OPS CHECK BLEED 1 PER AMM 36-11-00, OPS CHECK GOOD, NO SMELLS NOTED.

Part: INDICATOR — OUT OF ADJUST (L2 DOOR) · airframe 20,076 hrs · 12,342 cycles

L2 DOOR WILL NOT CLOSE PROPERLY GIRT BAR INDICATION. ADJUSTED INDICATOR.

Part: CATCHER — DIRTY (GIRT BAR) · airframe 19,998 hrs · 12,289 cycles

F/A REPORTS L2 DOOR GIRT BAR NOT ENGAGING PROPERLY. CLEANED GIRT BAF CATCHERS AND ADJUSTED GIRT BAR CABLE. PERFORMED OPS CHECK, NO DEFECTS NOTED AT THIS TIME IAW EMB 170 MM 52-12-2.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,309 hrs · 11,862 cycles

LEVEL 2 CORROSION ON EXTERNAL SKIN. BLENDED PER SRM 51-10-03, TYPE C REPAIR, AND ETD 2011-170-109513 REV A.

Part: FCU — MALFUNCTIONED (ENGINE) · airframe 17,450 hrs · 10,700 cycles

RECEIVED "FUEL 1+2 LO LEVEL" MESSAGES IN FLIGHT. FUEL QUANTITY INDICATIONS WERE NORMAL. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. MESSAGES DISAPPEARED AFTER LANDING WHEN TAXIING IN. MAINTENANCE DEFERRED. THE FCU WAS LATER REPLACED TO CLEAR THE MEL. THE DAY AFTER THE FCU REPLACEMENT, THE MESSAGE RETURNED; NO EMERGENCY DECLARED. IT WAS PLACED ON MEL AGAIN.

Part: RIB — CRACKED (RT WING) · airframe 17,443 hrs · 10,695 cycles

MAJOR REPAIR- RT WING RIB 10 CRACKED. RT WING RIB 10 R & R IAW ETD2011-170-05193 AND SRM 51-40-02, 51-43-01, AND 51-43-02.

Part: RIB — CRACKED (LT WING) · airframe 17,437 hrs · 10,691 cycles

LEFT WING RIB 10 CRACKED. RIB R & R IAW ETD2011-170-05193, SRM 51-40-02, 51-43-01, AND 51-43-02. MAJOR REPAIR.

Part: RIB — CRACKED (LT WING) · airframe 17,437 hrs · 10,691 cycles

LEFT WING RIB 10 CRACKED, R & R LT WING RIB 10. MAJOR REPAIR.

Part: DOOR FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,443 hrs · 10,695 cycles

LEVEL 2 CORROSION FWD CARGO DOOR CUTOUT, AFT LWR CORNER SEAL REST. REPLACED CORRODED SEAL REST WITH NEW SEAL REST AND MATCH DRILLED IAW EMB 170 SRM 51-40-02.

Part: DOOR FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,443 hrs · 10,695 cycles

LEVEL 2 CORROSION FWD CARGO DOOR CUTOUT, FWD LWR CORNER SEAL REST. REPLACED CORRODED SEAL REST WITH NEW SEAL REST AND MATCH DRILLED IAW EMB 170 SRM 51-40-02.

Part: LANYARD — LOOSE (DOOR) · airframe 17,443 hrs · 10,695 cycles

PERFORMING EMERGENCY EVACUATION SLIDE OPERATIONAL CHECK, THE SLIDE INFLATED AS IT SHOULD BUT THE EMERGENCY LIGHTS DID NOT TURN ON. FOUND ONE OF THE LANYARDS ON THE BATTERY SUPPLY LOOSE, AND AS A RESULT THE PLUG TO ACTIVATE THE LIGHTS DID NOT COME OUT. RECONNECTED LANYARD.

Part: INDICATOR — INOPERATIVE (R1 DOOR) · airframe 15,957 hrs · 9,803 cycles

R1 DOOR LOCKED VISUAL INDICATOR INOP. MAINTENANCE DEFERRED.

Part: SPRING — DISENGAGED (R1 DOOR) · airframe 15,901 hrs · 9,766 cycles

R1 DOOR OPEN INDICATION ON MFD. MAINTENANCE RE-ENGAGED THE SPRING TO THE LOCK BELL CRANK OF R1 DOOR FORWARD VISUAL LOCK INDICATOR IAW EMB 170 MM 52-41-22.

Part: INDICATION SYS — MALFUNCTIONED (R1 DOOR) · airframe 15,781 hrs · 9,698 cycles

R1 DOOR LOCK VISUAL INDICATION MISSING, DISPLAYS OPEN ON MFD INDICATION. MAINTENANCE DEFERRED.

Part: SENSOR — FAULTY (TE FLAP) · airframe 15,770 hrs · 9,693 cycles

UPON REACHING CRUISE ALTITUDE, RECEIVED EICAS MESSAGE "FLAP FAIL". NO CHANGES MADE TO THE FLAP POSITION. DECLARED AN EMERGENCY AND LANDED WITH FLAPS IN THE "1" POSITION. MAINTENANCE REMOVED AND REPLACED BOTH LEFT O/B FLAP SKEW SENSORS.

Part: LINER — DEFECTIVE (R1 DOOR) · airframe 15,706 hrs · 9,657 cycles

R1 DOOR LATCH MECHANISM NOT IN NORMAL POSITION. INDICATOR, WHICH IS NORMALLY UP AGAINST PLASTIC VIEWING PORT, IS PUSHED BACK. REMOVED AND REPLACED R1 DOOR MAIN LINING ASSEMBLY IAW EMB 170 MM 25-23-06.

Part: WARNING SYSTEM — MALFUNCTIONED (R1 DOOR) · airframe 15,701 hrs · 9,655 cycles

R1 SERVICE DOOR WILL NOT SHOW CLOSED ON EICAS. PERFORMED NORMAL R1 SERVICE DOOR CLOSING AND ARMING IAW EMB 170 MM 52-74-20. COULD NOT DUPLICATE FAULT. OPS CHECK GOOD.

Part: UNKNOWN — MALFUNCTIONED (R1 DOOR) · airframe 15,645 hrs · 9,623 cycles

R1 SERVICE DOOR NOT SHOWING CLOSED ON EICAS. FAULT HAD NO CORRELATIONS, CHECKED GAP OF BOTH PROX SENSORS, FOUND WITHIN LIMITS IAW EMB 170 MM 52-74-20. OPS CHECK GOOD.

Part: INDICATOR — LACK OF LUBE (SERVICE DOOR) · airframe 15,532 hrs · 9,549 cycles

FWD SERVICE DOOR SHOWING OPEN WITH DOOR ARMED. FOUND DOOR LATCH INDICATION STUCK. LUBED INDICATOR, OPS CHECK GOOD IAW EMB MM 52-21-01.

Part: ACTUATOR — INOPERATIVE (LE SLAT) · airframe 13,713 hrs · 8,465 cycles

WHILE BEGINNING APPROACH, EXTENDING SLAT/FLAP LEVER FROM 0 TO 1 RESULTED IN SLAT FAIL EICAS MESSAGE. PERFORMED QRH. SLATS REMAINED FAILED. DECLARED AN EMERGENCY, LANDED WITHOUT INCIDENT. MAINTENANCE CLEARED INHIBITS AND RELEASED THE SLAT BRAKE. SI 278061 WAS ISSUED AND COMPLIED WITH ON 2/10/10, WITH THE 3R SLAT ACTUATOR FOUND TRIPPED, WHICH WAS REPLACED.

Part: SENSOR — DEFECTIVE (TE FLAP) · airframe 10,514 hrs · 6,562 cycles

ON APPROACH CREW RECEIVED A FLAP LO RATE MESSAGE FOLLOWED BY FLAP FAIL MESSAGE. THE CREW DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE RT T4 SKEW SENSOR.

Part: ACTUATOR — DEFECTIVE (NR 3 TE FLAP) · airframe 10,428 hrs · 6,511 cycles

CREW SELECTED FLAPS 1 AND RECEIVED FLAPS FAIL MESSAGE ON EICAS. CREW DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RT NR 3 FLAP ACTUATOR.

Part: PRESSURE SWITCH — DEFECTIVE (RT ENGINE)

CREW REPORTED ENG 2 FUEL LOW PRESSURE INDICATION AND FUEL FEED 2 FAULT. CREW FOLLOWED QRH PROCEDURES; DECLARED AN EMERGENCY, DIVERTED AND LANDED WITHOUT INCIDENT. MAINT REPLACED THE LOW PRESSURE FUEL SWITCH. (K)

Part: STEERING SYS — MALFUNCTIONED (NLG) · airframe 8,736 hrs · 5,477 cycles

FLIGHT 7658 MCI TO ORD CREW REPORTS NWS FAIL ON APPROACH THEY CYCLED CB B25 ON TAXI IN AND FAULT CLEARED. MAINTENANCE REPLACED THE NWS MODULE FOR PREVENTATIVE MAINTENANCE.

Part: TIRE — FAILED (MLG) · airframe 1,635 hrs · 1,075 cycles

CREW REPORTED, DID NOT HAVE A DOWN AND LOCKED GEAR INDICATION. DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. FOUND NR 3 TIRE BLOWN WHICH CAUSED DAMAGE TO WEIGHT ON WHEELS HARNESS.

Part: SLIDE — DEPLOYED (L1 DOOR)

ON 07-23-05 FLT 7602 ORD-GRR, DEF L1 SLIDE PARTIALLY DEPLOYED WHILE OPENING. AIRCRAFT FERRIED FROM GRR TO ORD.