N869RW

Part: UNKNOWN — UNKNOWN (ZONE 700) · airframe 36,720 hrs · 26,934 cycles

DURING CRUISE RECEIVED PARKING BRAKE NOT RELEASED MESSAGE WITH PARKING BRAKE LIGHT. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. R&R PARKING BRAKE PRESSURE SWITCH.

Part: UNKNOWN — UNKNOWN (ZONE 100) · airframe 36,353 hrs · 26,650 cycles

BLEED 2 LEAK ON CLIMB OUT. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. R&R BLEED 2 AIR DUCT ABOVE PRECOOLER.

Part: SHEAR ANGLE — CORRODED (ZONE 100) · airframe 36,352 hrs

"CORRODED SHEAR CLIP AT FR 16, STGR 23L-24L. REMOVED AND REPLACED SHEAR CLIP AT FR 16 STGR 23L-24L. REF EMB SRM 51-40-08"

Part: INTERCOSTAL — CORRODED (ZONE 100) · airframe 36,352 hrs · 26,648 cycles

"STRINGER 28R IS CORRODED AT INTERCOSTAL ATTACHMENT AREA BETWEEN FR 86 AND FR 87. : REMOVED DAMAGE PORTION OF STGR 28R BY CUTTING DAMAGE AREA BETWEEN FR85-86 AND PERFORMED SPLICE REPAIR TO STGR 28R REFER SRM 53-23-- 03/REPAIR 06P"

Part: SHEAR ANGLE — CORRODED (ZONE 100) · airframe 36,352 hrs · 26,648 cycles

"CORRODED SHEAR CLIP AT FR 17, STGR 23L-24L. REMOVED AND REPLACED SHEAR CLIP AT FR 17 BETWEEN STGR 23L-24L. REF EMB SRM 51-40-08."

Part: SHEAR ANGLE — CORRODED (ZONE 100) · airframe 36,352 hrs · 26,648 cycles

"CORRODED SHEAR CLIP AT FR 17, STGR 24L-25L. REMOVED AND REPLACED SHEAR CLIP AT FR 17 BETWEEN STGR 24L-25L. REF EMB SRM 51-40-08"

Part: SHEAR ANGLE — CORRODED (ZONE 100) · airframe 36,352 hrs · 26,648 cycles

"CORRODED SHEAR CLIP AT FR 16, STGR 25L-26L.: REMOVED AND REPLACED SHEAR CLIP AT FR 16 STGR 25L-26L. REF EMB SRM 51-40-08"

Part: SHEAR ANGLE — CORRODED (ZONE 100) · airframe 36,352 hrs · 26,648 cycles

"CORRODED SHEAR CLIP AT FR 16, STGR 27R-28R. REMOVED AND REPLACED SHEAR CLIP AT FR 16 BETWEEN STGR 27R-28R. REF EMB SRM 51-40-08. "

Part: SHEAR ANGLE — CORRODED (ZONE 100) · airframe 36,352 hrs · 26,648 cycles

"CORRODED SHEAR CLIP AT FR 86, STGR 29R-28R. REMOVED AND REPLACED SHEAR CLIP AT FR86 STGR 29R-28R REFER SRM 51-40-08"

Part: SHEAR ANGLE — CORRODED (ZONE 100) · airframe 36,352 hrs · 26,648 cycles

"CORRODED SHEAR CLIP AT FR 85, STGR 28R-29R.REMOVED AND REPLACED SHEAR CLIP AT FR 85 BETWEEN STGR 28R-29R. REF EMB SRM 51-40-08"

Part: SHEAR ANGLE — CORRODED (ZONE 100) · airframe 36,352 hrs · 26,648 cycles

"CORRODED SHEAR CLIP AT FR 83, STGR 27R-28R. REMOVED AND REPLACED SHEAR CLIP AT FR 83, STGR 27R-28R.REF EMB SRM 51-40-08"

Part: SHEAR ANGLE — CORRODED (ZONE 100) · airframe 36,352 hrs · 26,648 cycles

"CORRODED SHEAR CLIP AT FR 16, STGR 26L-27L. REMOVED AND REPLACED SHEAR CLIP AT FR 16, STGR 26L-27L. REF EMB SRM 51-40-08"

Part: SHEAR ANGLE — CORRODED (ZONE 100) · airframe 36,352 hrs · 26,648 cycles

"CORRODED SHEAR CLIP AT FR 17, STGR 27R-28R. : REMOVED AND REPLACED SHEAR CLIP AT FR 17, STGR 27R-28R. REF EMB SRM 51-40-08."

Part: SHEAR ANGLE — CORRODED (ZONE 100) · airframe 36,352 hrs · 26,648 cycles

"CORRODED SHEAR CLIP AT FR 17, STGR 26L-27L.REMOVED AND REPLACED SHEAR CLIP AT FR 17, STGR 26L-27L. REF EMB SRM 51-40-08."

Part: SHEAR ANGLE — CORRODED (ZONE 100) · airframe 36,352 hrs · 26,648 cycles

CORRODED SHEAR CLIP AT FR 17, STGR 27L-28L. REMOVED AND REPLACED SHEAR CLIP AT FR17, STGR 27L-28L. REF SRM 51-40-08.

Part: SHEAR ANGLE — CORRODED (ZONE 100) · airframe 36,352 hrs · 26,648 cycles

"CORRODED SHEAR CLIP AT FR 16, STGR 27L-28L. REMOVED AND REPLACED SHEAR CLIP AT FR 16, STGR 27L-28L. REF EMB SRM 51-40-08."

Part: SHEAR ANGLE — CORRODED (ZONE 100) · airframe 36,352 hrs · 26,648 cycles

"CORRODED SHEAR CLIP AT FRAME 86 BETWEEN STRINGERS 27R AND 28R. : REMOVED AND REPLACED SHEAR CLIP AT FR86 BETWEEN STGR 27R-28R REFER SRM 51-40-08"

Part: SLIDE — PARTIAL DEPLOY (ZONE 800) · airframe 33,629 hrs · 24,640 cycles

L1 DOOR GIRT BAR ENGAGED, SLIDE SEMI DEPLOYED. R&R SLIDE AND L1 DOOR FLEXBALL CABLE.

Part: WEB — CORRODED (FRAME 19) · corrosion level 2 · airframe 31,684 hrs · 23,205 cycles

DURING HEAVY CHECK MAINTENANCE FOUND SHEAR WEB AFT OF L1 DOOR AT FR 19 LBL 16 FOUND CORRODED. REPLACED SHEAR WEB AFT OF L1 DOOR AT FR 19 LBL 16, IAW SRM 51-41-02 AND 51-43-02.

Part: FLOOR SUPPORT — CORRODED (FRAMES 12-17) · corrosion level 2 · airframe 31,684 hrs · 23,205 cycles

DURING HEAVY CHECK MAINTENANCE FOUND FLOOR BEAM SUPPORT AT FR 12 LBL 17 CORRODED. REPLACED FLOOR BEAM SUPPORT AT FR 12 LBL 17, IAW EMB 170 SRM 51-41-02 AND SRM 51-43-02.

Part: DOOR SILL — CORRODED (FRAME 12) · corrosion level 2 · airframe 31,684 hrs · 23,205 cycles

DURING HEAVY CHECK MAINTENANCE FOUND L1 DOOR FWD SILL CORRODED AT FR 12 LBL 47. REPLACED L1 DOOR FWD SILL AT FR 12 LBL 47, IAW EMB 170 SRM 51-41-02.

Part: SUPPORT — CORRODED (MLG UPLOCK) · corrosion level 2 · airframe 31,684 hrs · 23,205 cycles

DURING HEAVY CHECK MAINTENANCE FOUND LT MLG BOX CORROSION FOUND ON AFT UPLOCK SUPPORT BETWEEN SPAR 2, SPAR 3 AND RIB 1-2. LT MLG AFT UPLOCK SUPPORT REPLACED, IAW SRM 51-43-03 AND 51-43-04.

Part: SKIN — CORRODED (SERVICE PANEL) · corrosion level 2 · airframe 31,684 hrs · 23,205 cycles

DURING HEAVY CHECK MAINTENANCE FOUND CORROSION ON WASTE SERVICE PANEL SKIN BETWEEN FR 88-89 CFIII. REPLACED AFT SERVICE DOOR PANEL BETWEEN FR 88-89, IAW EMB 170 SRM 51-41-02.

Part: HINGE — CORRODED (FRAMES 88-89) · corrosion level 2 · airframe 31,684 hrs · 23,205 cycles

DURING HEAVY CHECK MAINTENANCE FOUND CORROSION ON HINGES AT WASTE SERVICE DOOR BETWEEN FR 88-89 CFIII. REPLACED HINGES ON AFT WASTE SERVICE DOOR BETWEEN FR 88-89, IAW EMB 170 SRM 51-43-04.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 31,684 hrs · 23,205 cycles

LT HORIZ STAB, DURING HEAVY CHECK MAINTENANCE FOUND CRACK AT RIB 11A LOWER FLANGE BETWEEN MID SPAR AND FRONT SPAR. SB 170-55-0014 INCORPORATED UNDER REPUBLIC EO 170EO-55-10-0004-1 ON AAR TASK CARD 4500775-3000-0080.

Part: SHEAR PANEL — CORRODED (FRAMES 87-88) · corrosion level 2 · airframe 31,684 hrs · 23,205 cycles

DURING HEAVY CHECK MAINTENANCE FOUND CF III FLOOR STRUCTURE CORROSION ON RT SHEAR PANEL BETWEEN FR87-88. REPLACED RT SHEAR PANEL BETWEEN FR 87-88, IAW SRM 51-42-01 AND 51-42-02.

Part: FLOOR SUPPORT — CORRODED (FRAME 87) · corrosion level 2 · airframe 31,684 hrs · 23,205 cycles

DURING HEAVY CHECK MAINTENANCE FOUND CORROSION ON CF III FLOOR STRUCTURE SUPPORT AT FR 87 RT SIDE. REPLACED SHEAR PANEL FLOOR SUPPORT RT SIDE AT FR 87, IAW EMB 170 SRM 51-41-01.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 31,684 hrs · 23,205 cycles

DURING HEAVY CHECK MAINTENANCE FOUND RT HORIZ STAB CRACK AT RIB 12A UPPER FLANGE BETWEEN MID AND FRONT SPAR. SB 170-55-0014 INCORPORATED UNDER REPUBLIC EO 170EO-55-10-0004-1, REF AAR TASK CARD 4500775-3000-0080.

Part: STRUCTURE — CRACKED (AVIONICS RACK) · airframe 31,684 hrs · 23,205 cycles

DURING HEAVY CHECK MAINTENANCE FOUND FWD AVIONICS RACK LT FWD AND LT AFT POSTS CRACKED. REPAIRED FWD AVIONICS RACK, IAW EO 170EO-53-12-0000 REV 1.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 31,153 hrs · 22,799 cycles

4TH FROM THE FRONT OVERHEAD EMERGENCY LIGHT IS OUT - REPLACED EMERGENCY LIGHT POWER UNIT 2 IAW AMM 33-50-01 OPS CHECKED GOOD

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 31,153 hrs · 22,799 cycles

AFT OVERHEAD EMERGENCY EXIT LIGHT IS OUT - REPLACED AFT EMERGENCY LIGHT POWER UNIT, PER EMB 170 AMM 33-50-01. OPERATIONAL CHECK GOOD

Part: SLIDE — DETACHED (R2 DOOR) · airframe 28,117 hrs · 20,502 cycles

R2 DOOR EMERGENCY EVACUATION SLIDE DETACHED FROM BASEBOARD. R&R R2 DOOR EMERGENCY EVACUATION SLIDE AND FLEXBALL CABLE IAW R170EO-52-41-0003.

Part: GUSSET — CORRODED (FRAME 90) · corrosion level 2 · airframe 27,987 hrs · 20,409 cycles

RT OTBD GUSSET AT FRAME 90 WAS CORRODED. REMOVED AND REPLACED THE GUSSET IAW SRM 51-40-08, SRM 51-40-02, AND SRM 51-23-04.

Part: SPLICE PLATE — CORRODED (FRAMES 87-88) · corrosion level 2 · airframe 27,987 hrs · 20,409 cycles

LEFT FLOOR SPLICE PLATE BETWEEN FRAMES 87 - 88 WAS CORRODED. REMOVED AND REPLACED THE SPLICE PLATE IAW SRM 51-40-08.

Part: SPLICE PLATE — CORRODED (FRAME 90) · corrosion level 2 · airframe 27,987 hrs · 20,409 cycles

CENTER FLOOR SPLICE PLATE AT FRAME 90 WAS CORRODED. REMOVED AND REPLACED THE SPLICE PLATE IAW SRM 51-40-02, AND SRM 51-40-08.

Part: ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 27,987 hrs · 20,409 cycles

3 LOWER L ANGLES ON PANEL CORRODED. L ANGLE REMOVED AND REPLACED IAW SRM 51-40-08, 51-23-06, AND 51-40-02.

Part: GUSSET — CORRODED (FRAME 90) · corrosion level 2 · airframe 27,987 hrs · 20,409 cycles

RT GUSSET PLATE ON THE RT SEAT TRACK AND FRAME 90 CORRODED. REMOVED AND REPLACED THE GUSSET IAW SRM 51-40-08.

Part: FLOORBEAM — CORRODED (FRAME16) · corrosion level 2 · airframe 27,987 hrs · 20,409 cycles

LT OUTBOARD FLOORBEAM AT FR 16 HAD CORROSION. REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-21-01, AND SRM 51-43-03.

Part: FLOOR SUPPORT — CORRODED (FRAMES 12-14) · corrosion level 2 · airframe 27,987 hrs · 20,409 cycles

FWD RT FLOOR SUPPORT FR 12-14 HAD CORROSION. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-08.

Part: FLOOR SUPPORT — CORRODED (FRAMES 12-16) · corrosion level 2 · airframe 27,987 hrs · 20,409 cycles

FWD LT FLOOR SUPPORT FRAMES 12 TO 16 HAD CORROSION. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-08.

Part: FLOOR SUPPORT — CORRODED (FRAMES 19) · corrosion level 2 · airframe 27,987 hrs · 20,409 cycles

LEFT OUTBOARD FLOOR SUPPORT ON FR 19 HAD CORROSION. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-08.

Part: DOUBLER — CORRODED (FRAMES 19-20) · corrosion level 2 · airframe 27,987 hrs · 20,409 cycles

LEFT AFT DOUBLER, FRAMES 19 - 20 HAD CORROSION. REMOVED AND REPLACED THE DOUBLER IAW SRM 51-41-02, AND 51-43-04.

Part: ATTACH ANGLE — CORRODED (FRAMES 45-52) · corrosion level 2 · airframe 27,987 hrs · 20,409 cycles

CORROSION WAS FOUND ON 3 LOWER ANGLES FOR PANEL 1441FR. THE ANGLES WERE REMOVED AND REPLACED IAW 51-40-08, 51-23-06, 51-23-06, AND 51-40-02.

Part: DOUBLER — CORRODED (FRAMES 13-16) · airframe 27,987 hrs · 20,409 cycles

FWD LT DOUBLER, FRAMES 13 TO 16 HAD CORROSION. REMOVED, AND REPLACED THE DOUBLER IAW SRM 51-40-08, AND 51-23-06.

Part: SPLICE PLATE — CORRODED (FRAMES 87-88) · corrosion level 2 · airframe 27,987 hrs · 20,409 cycles

RT SPLICE PLATE BETWEEN FRAMES 87 - 88 CORRODED. REMOVED AND REPLACED THE SPLICE PLATE IAW SRM 51-40-08.

Part: FITTING — CORRODED (GIRT BAR) · corrosion level 2 · airframe 27,987 hrs · 20,409 cycles

CORROSION FOUND ON THE AFT & FWD GIRT BAR FITTINGS, TOP FLANGE AND LOWER BOTTOM AREAS ON THRESHOLD BEAM. REMOVED AND REPLACED L1 DOOR LOWER BEAM IAW SRM 51-40-08, AND SRM 51-23-06. MAJOR REPAIR.

Part: DOOR — CORRODED (FRAMES 88-89) · corrosion level 2 · airframe 27,987 hrs · 20,409 cycles

CORROSION ALONG THE HINGE LINE TO WASTE WATER SERVICE DOOR. REMOVED AND REPLACED WASTE SERVICE DOOR IAW AMM 53-03-60, AND SRM 51-23-06.

Part: SIGN — DAMAGED (EMERGENCY LIGHT) · airframe 23,658 hrs · 17,674 cycles

L1 DOOR LOWER EMERGENCY ENTRANCE EXIT IDENTIFICATION LIGHT DAMAGED. R&R L1 DOOR LOWER EMERGENCY EXIT SIGN IAW AMM 22-50-15. OPS CHECKED GOOD.

Part: INDICATOR — OUT OF ADJUST (R2 DOOR) · airframe 23,150 hrs · 17,275 cycles

R2 DOOR INDICATOR NOT SHOWING GREEN OR RED, ONLY SHOWS WHITE. ADJUSTED R2 DOOR INDICATOR IAW AMM 52-42-22. OPS CHECK SATISFACTORY.

Part: ROD — DAMAGED (CARGO DOOR) · airframe 23,097 hrs · 17,224 cycles

MAIN CABIN DOOR VERY DIFFICULT FOR GATE AGENTS TO OPEN FROM THE OUTSIDE. R & R THE COUNTER BALANCE RODS IAW AMM 52-11-20.

Part: PUMP — FAILED (HYD SYSTEM) · airframe 23,071 hrs · 17,209 cycles

TOTAL LOSS OF HYDRAULIC SYSTEM 2 IN FLIGHT (TOTAL LOSS). RAN QRH. FREE FALLED THE GEAR. DECLARED EMERGENCY, DIVERTED, LANDED WITHOUT INCIDENT. R & R NR 2 HYDRAULIC PUMP PRESSURE UNION AND REPAIRED LINE AT RT WING AFT SPAR AFT OF PYLON AREA IAW AMM 20-10-03. LEAK CHECK GOOD.

Part: DOUBLER — CORRODED (ZONE 100) · corrosion level 2 · airframe 23,047 hrs · 17,188 cycles

RIGHT COCKPIT FLOOR DOUBLER HAS AREAS OF CORROSION. R & R THE DOUBLER IAW ETD2016-170-057605.

Part: DOOR — DENTED (GPU) · airframe 23,047 hrs · 17,188 cycles

DENT ABOVE GPU DOOR. PERFORMED CUT-OUT OF DAMAGED AREA REF SRM 51-10-01. FABRICATED REPAIR DOUBLER AND FILLER, LOCATED AND DRILLED NEW HOLES ON SKIN AND REPAIR DOUBLER REF ETD2016-170-056193 AND SRM 53-10-01. INSTALLED REPAIR DOUBLER AND FILLER AND APPLIED EDGE SEAL REF ETD2016-170-056193 AND SRM 53-10-01. MAJOR REPAIR.

Part: SHEAR TIE — CRACKED (FRAME 9) · airframe 23,047 hrs · 17,188 cycles

SHEAR TIE CRACKED FRAME 9 STRINGERS 11 - 12L. R & R THE SHEAR TIE IAW SRM 51-41-02, 51-41-01, AND APPLIED FINISH REF SRM 51-23-06.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 23,047 hrs · 17,188 cycles

MAJOR REPAIR, RIGHT HORIZONTAL RIB HAS EVIDENCE OF A CRACKED RIB 11, UPPER SIDE, BETWEEN FRONT SPAR AND MID SPAR. R & R RT HORIZONTAL RIB 11, REF SRM 51-41-01 AND 51-41-02.

Part: RIB — CRACKED (ZONE 100) · airframe 23,047 hrs · 17,188 cycles

RIGHT HORIZONTAL RIB HAS EVIDENCE OF A CRACK, RIB 10 LOWER SIDE BETWEEN FRONT SPAR AND MID SPAR. R & R THE RIB IAW SRM 51-41-01 AND 51-41-02.

Part: SEAL REST — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 23,047 hrs · 17,188 cycles

CORROSION ON THE FWD CARGO DOOR, AFT LOWER CORNER SEAL REST. R & R THE SEAL REST.

Part: SHEAR TIE — CORRODED (FRAME 88) · corrosion level 2 · airframe 23,047 hrs · 17,188 cycles

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

Part: SHEAR PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 23,047 hrs · 17,188 cycles

CORROSION ON RT SHEAR PANEL. R & R RT SHEAR PANEL.

Part: SPAR — CRACKED (LT WING) · airframe 23,047 hrs · 17,188 cycles

LEFT STUB WING SPAR 3 SHOWS CRACK INDICATIONS AT THE FASTENER REPLACEMENT HOLE. THE SPAR WAS REAMED UNTIL CRACK WAS REMOVED AT A 0.388". COMPLIED WITH STEPS OF ETD2016-170-055367 REV C. MAJOR REPAIR.

Part: SHEAR PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 23,047 hrs · 17,188 cycles

CORROSION ON LT SHEAR PANEL AT LAVATORY ANCHOR. R & R SHEAR PANEL.

Part: SUPPORT BRACKET — CORRODED (ZONE 100) · airframe 23,047 hrs · 17,188 cycles

FWD CARGO CREW OXYGEN BOTTLE SUPPORT BRACKET UNDER BOTTLE'S NECK HAS CORROSION UNDER PAINT. R & R OXYGEN BOTTLE SUPPORT BRACKET AND SUPPORT REINFORCEMENT.

Part: SPLICE PLATE — CORRODED (FRAMES 87-88) · corrosion level 2 · airframe 23,047 hrs · 17,188 cycles

CORROSION ON LEFT SPLICE PLATE BETWEEN FRAMES 87 - 88. R & R THE SPLICE PLATE. .

Part: ROLLER — LACK OF LUBE (PAX DOOR) · airframe 22,971 hrs · 17,141 cycles

MAIN CABIN DOOR HARD TO OPEN FROM OUTSIDE. GATE AGENT CANNOT OPEN WITHOUT INSIDE HELP. LUBRICATED DOOR AND ROLLERS, DOOR OPS CHECKS GOOD IAW AMM 52-11-00.

Part: WARNING LIGHT — FALSE ACTIVATION (L1 DOOR) · airframe 22,650 hrs · 16,920 cycles

L1 DOOR OPEN EICAS MESSAGE ON CLIMB OUT THROUGH FL340, STAYED ON EICAS FOR CRUISE PORTION. MESSAGE WENT AWAY ON DESCENT THROUGH FL300. FOLLOWED GRH, ALL INDICATIONS NORMAL ON DOOR, PRESSURE ALSO NORMAL. CLEANED SENSORS ON L2 DOOR IAW AMM 52-70-00. OPS CHECK GOOD.

Part: COVER — BROKEN (EMERGENCY LIGHT) · airframe 22,212 hrs · 16,615 cycles

FWD AND AFT SERVICE DOOR EMERGENCY EXIT COVERS BROKEN. R & R FWD AND AFT SERVICE DOOR EMERGENCY EXIT COVERS.

Part: SENSOR — OUT OF ADJUST (L2 DOOR LATCH) · airframe 22,155 hrs · 16,569 cycles

DOOR PASSENGER AFT OPEN INDICATION ON MFD IN FLIGHT AT FL370. WENT AWAY DESCENDING THROUGH FL300. ADJUSTED L2 DOOR LATCH SENSOR IAW AMM 52-72-20. OPS CHECK GOOD.

Part: SIGHT TUBE — OUT OF ALIGNMENT (R1 DOOR) · airframe 21,333 hrs · 16,048 cycles

R1 DOOR RT LOCK INDICATION WINDOW DOES NOT ALIGN, PLASTIC CONE PARTIALLY DETACHED. SECURED R1 DOOR ARMING INDICATION SIGHT TUBE IAW AMM 25-23-06. OPS CHECK GOOD IAW AMM 52-41-00.

Part: SENSOR — OUT OF LIMITS (PAX DOOR) · airframe 20,591 hrs · 15,534 cycles

FWD PAX MAIN DOOR INDICATED OPEN IN FLIGHT. DIVERTED, BUT DID NOT DECLARE AN EMERGENCY. R & R SHAFT ROLLER DETECTOR IAW 53-10-21 AND SHIMMED DOOR FRAME SENSOR IAW AMM 52-71-20. OPS CHECK GOOD.

Part: BELLCRANK — OUT OF ADJUST (L1 DOOR) · airframe 19,941 hrs · 15,153 cycles

L1 DOOR WILL NOT CLOSE. ADJUSTED STOP BELLCRANK, OPS CHECKED GOOD IAW AMM 52-11-20.

Part: DOOR — OUT OF ADJUST (L1) · airframe 19,505 hrs · 14,885 cycles

L1 DOOR DIFFICULT TO OPEN ONCE FULLY DISARMED AND UNLOCKED. ADJUSTED L1 HEIGHT IAW CMM 52-11-22. OPS CHECK IS GOOD AT THIS TIME.

Part: DOOR — OBSTRUCTED (L1) · airframe 19,135 hrs · 14,654 cycles

MAIN CABIN DOOR WON'T LOCK IN THE OPEN POSITION. FOUND L1 DOOR TRIM COMPONENTS TO BE INTACT IAW AMM 25-23-04, AND L1 DOOR OPENS AND LOCKS IN PLACE AS NORMAL IAW AMM 52-11-00.

Part: CLOSEOUT PANEL — CORRODED (FWD CARGO) · corrosion level 2 · airframe 18,919 hrs · 14,489 cycles

CORROSION FOUND ON FWD CARGO CLOSE OUT PANEL. R & R CLOSE OUT PANEL.

Part: CROSSBEAM — MECHANIC ERROR (FRAME 16) · airframe 18,919 hrs · 14,489 cycles

MISDRILLED HOLE THROUGH CROSSBEAM AT FRAME 16. CUTOUT DAMAGE, FABRICATED A REPAIR FILLER AND DOUBLER, INSTALLED PARTS IAW ETD2014-170-0491107. MAJOR REPAIR

Part: DOUBLER — CORRODED (FRAMES 19-20) · corrosion level 2 · airframe 18,919 hrs · 14,489 cycles

CORROSION FOUND ON LT DOUBLER FRAMES 19-20. R & R FASTENERS.

Part: SPLICE — CORRODED (FRAME 90) · corrosion level 2 · airframe 18,919 hrs · 14,489 cycles

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

Part: DOUBLER — CORRODED (ZONE 100) · corrosion level 2 · airframe 18,919 hrs · 14,489 cycles

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

Part: SEAT TRACK — CORRODED (FRAMES 12-20) · corrosion level 2 · airframe 18,919 hrs · 14,489 cycles

CORROSION FOUND ON LT SEAT TRACK, FRAMES 12-20. R & R SEAT TRACK.

Part: SPLICE — CORRODED (FRAME 90) · corrosion level 2 · airframe 18,919 hrs · 14,489 cycles

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

Part: FINGER DOUBLER — CORRODED (ZONE 100) · corrosion level 2 · airframe 18,919 hrs · 14,489 cycles

CORROSION FOUND ON FWD CARGO AFT FINGER DOUBLER. R & R FINGER DOUBLER.

Part: THRESHOLD — CORRODED (ZONE 100) · airframe 18,919 hrs · 14,489 cycles

CORROSION AT L2 DOOR THRESHOLD IN TWO SPOTS. REMOVED CORROSION. MAJOR REPAIR

Part: FINGER DOUBLER — CORRODED (ZONE 100) · corrosion level 2 · airframe 18,919 hrs · 14,489 cycles

CORROSION ON FWD CARGO AFT FINGER DOUBLER. R & R AFT FINGER DOUBLER. MAJOR REPAIR

Part: UPPER SHEET — CORRODED (FRAMES 85-86) · corrosion level 2 · airframe 18,919 hrs · 14,489 cycles

CORROSION FOUND ON UPPER SHEET, RBL 10.748, FRAMES 85-86. R & R RT UPPER SHEET.

Part: CROSSBEAM — CORRODED (FRAME 84) · airframe 18,919 hrs · 14,489 cycles

CORROSION FOUND ON CROSSBEAM AT FRAME 84, RT Y=+10.748. CUTOUT DAMAGE SECTION, REPAIRED IAW ETD 2014-170-048295. MAJOR REPAIR

Part: SHEAR PLATE — CORRODED (FRAMES 87-88) · corrosion level 2 · airframe 18,919 hrs · 14,489 cycles

CORROSION FOUND ON LT SHEAR PLATE SPLICE, FRAMES 87-88. R & R SPLICE PLATE.

Part: BEAM — CORRODED (FRAMES 86-89) · corrosion level 2 · airframe 18,919 hrs · 14,489 cycles

CORROSION ON LT BEAM Y -10.748, FRAMES 86-89. R & R DAMAGED BEAM.

Part: SHEAR PLATE — CORRODED (FRAMES 87-88) · corrosion level 2 · airframe 18,919 hrs · 14,489 cycles

CORROSION FOUND ON CENTER SHEAR PLATE FRAMES 87-88. R & R CENTER SHEAR PLATE.

Part: FLOORBEAM — CORRODED (FRAME 84) · corrosion level 2 · airframe 18,919 hrs · 14,489 cycles

CORROSION FOUND ON FLOORBEAM AT FRAME 84, RBL 10.748. INSTALLED LT REPAIR ANGLE IAW ETD 2014-170-048295. MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (FRAMES 12-20) · airframe 18,919 hrs · 14,489 cycles

CORROSION FOUND ON RT SEAT TRACK FRAMES 12-20. R & R SEAT TRACK.

Part: FLOOR SUPPORT — CORRODED (FRAMES 12-14) · corrosion level 2 · airframe 18,919 hrs · 14,489 cycles

CORROSION FOUND ON RT FWD FLOOR SUPPORT FRAMES 12-14. R & R FLOOR SUPPORT.

Part: FINGER DOUBLER — CHAFED (ZONE 100) · airframe 18,919 hrs · 14,489 cycles

CHAFE FOUND ON FWD CARGO BAY AFT FINGER DOUBLER. REMOVED, REPAIRED AND REPLACED AFT FINGER DOUBLER IAW SRM 51-23-04, 51-23-05, 54-40-04, 51-40-02, 51-41-02, 51-43-02, 51-23-05, 51-23-06. MAJOR REPAIR

Part: BEAM — CORRODED (FRAMES 86-89) · corrosion level 2 · airframe 18,919 hrs · 14,489 cycles

CORROSION FOUND ON RT BEAM Y+10.748, FRAMES 86-89. R & R DAMAGED BEAM.

Part: RETAINER — CORRODED (ZONE 100) · corrosion level 2 · airframe 18,919 hrs · 14,489 cycles

CORROSION FOUND ON LAVATORY SERVICE PAN RETAINER AT FWD INDB CORNER. REMOVED RETAINER IAW SB170-53-0095.

Part: ATTACH FITTING — CORRODED (SERVICE DOOR) · airframe 18,919 hrs · 14,489 cycles

CORROSION FOUND ON FWD OF UPPER SLIDE ATTACH POINT ON FWD SERVICE DOOR. R & R ATTACH FITTING.

Part: BATTERY — WARNING MESSAGE (EMERGENCY LIGHTS) · airframe 18,062 hrs · 13,874 cycles

AFTER LANDING, DURING TAXI, EICAS ADVISORY EMERGENCY LIGHT BATTERY FAULT. TROUBLESHOT IAW FIM 33-50-00-810-801A. R & R GEN I/O 2 IAW AMM 31-41-06, OPS CHECK GOOD IAW AMM 33-50-00.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 14,522 hrs · 11,412 cycles

LEVEL 2 CORROSION LAV SERVICE BOX LOWER DOUBLER. REMOVED AND REPLACED LAV SERVICE BOX DOUBLER IAW EMB 170 SRM 51-40-02 AND 51-43-02.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 14,522 hrs · 11,412 cycles

LEVEL 2 CORROSION FR 88 FLOOR STRUCTURE AT RIGHT SHEAR PLATE. REMOVED AND REPLACED RT SHEAR PLATE AT FR 88 IAW EMB 170 SRM 51-42-01 AND 51-42-02.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 14,522 hrs · 11,412 cycles

LEVEL 2 CORROSION - RIGHT CENTER CF I SEAT TRACK 0.018" GOUGE IN TEETH AND 0.010" CORROSION SPOT IN CROWN BOTTOM AT 8" AFT OF FRAME 21 (BOTH SPOTS IN A LINE). REMOVED AND REPLACED SEAT TRACK IAW EMB 170 SRM 51-43-03.

Part: GIRT BAR — UNKNOWN (L1 DOOR) · airframe 13,851 hrs · 11,050 cycles

L1 DOOR WILL NOT ARM, DIFFICULT TO CLOSE. RE-INSTALLED L1 DOOR GIRT BAR IAW EMB 170 MM 52-11-41. OPS CHECK GOOD.

Part: LEVER — LACK OF LUBE (L1 DOOR) · airframe 11,697 hrs · 9,776 cycles

L1 DOOR ARMING LEVER STICKS. MAINTENANCE LUBED ALL LEVERS ON L1 DOOR, OPERATED AS REQUIRED PER MM 52-11-00.

Part: LANDING GEAR — LEAKING (ZONE 700) · airframe 11,497 hrs · 9,630 cycles

LG WOW SYS FAIL MESSAGE DISPLAYED AFTER LANDING GEAR RETRACTION. RETURNED TO FIELD AND DECLARED AN EMERGENCY. LANDED WITHOUT INCIDENT. NOSE GEAR ALREADY ON DMI FOR LEAKING, SPARE SEAL HAD BEEN ACTIVATED. MAINTENANCE REPACKED THE NLG STRUT AND THE LEAK CONTINUED. MAINTENANCE REMOVED AND REPLACED THE NOSE LANDING GEAR.

Part: UNKNOWN — ODOR (CABIN) · airframe 10,880 hrs · 9,250 cycles

NOTICED ELECTRICAL SMELL IN CRUISE FLIGHT AROUND ROW 12. COULD NOT DUPLICATE SMELL. OPS CHECKED ALL PSU LIGHTS IAW MM 33-25-01, OPS CHECKED BOTH PACKS IAW MM 21-22-00. NO DEFECTS NOTED.

Part: BOTTLE — DISCHARGED (DOOR) · airframe 9,552 hrs · 8,352 cycles

GIRT BAR WAS OUT OF CLIPS. WHILE WORKING ACCIDENTALLY BLEW DOOR ASSIST BOTTLE AND SLIDE CAME UNLACED. RE-RIGGED DOOR AND INSTALLED NEW SLIDE.

Part: FLAP — MALFUNCTIONED (WING) · airframe 5,230 hrs · 3,013 cycles

FLIGHT 6457 ALT TO MSP FLAPS STOP AT FLAPS 1 AND WITH ZERO SLATS. NO FLAPS LANDING, DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. MAINTENANCE CLEARED SF-ACE INHIBITS, AND RELEASED ELECTRONIC BRAKE. HAS NOT REPEATED THIS DATE 02/14/2008.

Part: ACTUATOR — MALFUNCTIONED (L/E SLAT) · airframe 4,610 hrs · 2,611 cycles

FLIGHT 6498 ATL TO IND ON APPROACH CREW RECEIVED THE EICAS CAUTION MESSAGE FOR SLAT FAILURE. FLAPS AND SLATS WERE AT ZERO LANDED THE AIRCRAFT WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED RT NR 4 SLAT ACTUATOR.

Part: HEAT EXCHANGER — DIRTY (RT PACK) · airframe 3,846 hrs · 2,135 cycles

DFW TO JFK FLIGHT 6496 AT CRUISE THE A FLIGHT ATTENDANT INFORMED THE FLIGHT DECK THAT THERE WAS A STRONG BURNING SMELL IN THE FORWARD PART OF THE CABIN. AT THE SAME MOMENT THE CREW NOTICE A BURNING SMELL AS WELL. CREW DECLARED AN EMERGENCY AND DIVERTED TO IND. THE SMELL SLOWLY STARTED TO DISSIPATE AFTER LANDING. MAINTENANCE REPLACED THE NR 2 DUEL HEAT EXCHANGER AND CLEANED COFFEE RESIDUE FROM ACM.

Part: WARNING MESSAGE — ILLUMINATED (NLG STEERING) · airframe 1,439 hrs · 736 cycles

FLIGHT 6440 MLI TO ATL - CREW RECEIVED STEER FAIL MESSAGE AFTER LOWERING LANDING GEAR. PERFORMED GO-AROUND, NOTIFIED ATC AND THE CABIN. LANDED WITH CFR STANDING BY AND PASSENGERS BRACING. UNEVENTFUL LANDING FOLLOWED BY BEING TUGGED TO THE GATE. OCM PERFORMED MAU NR 2 RESET, STEERING OPS CHECK GOOD. NO FAULTS FOUND IN CMC, OK FOR CONTINUED SERVICE.