N657RW

Part: NONE — NONE · airframe 45,565 hrs · 28,580 cycles

THE L1 DOOR IS STUCK. ADJUSTED L1 DOOR IAW EMB 170 AMM 52-11-00. L1 SLIDE MECHANISM IAW EMB 170 AND AMM 52-11-40. THE OPS CHECK IS GOOD.

Part: RIB — CRACKED (HOIROZNTAL STAB) · airframe 45,299 hrs · 28,370 cycles

LT AND RT HSTAB RIB 10A,11A AND 12A REPLACED DUE TO CRACKING IAW 170EO-55-10-0004_1 (MAJOR)

Part: SHEAR TIE — CORRODED (FRM 83 S28-29R) · corrosion level 2 · airframe 45,299 hrs · 28,370 cycles

CF III, AFT CARGO, SHEAR CLIP CORRODED BETWEEN STR 29R AND STR 28R. REMOVED AND REPLACED SHEAR CLIP IN CF III IN AFT CARGO AT FR83 BETWEEN STR 29R AND STR 28R. IAW SRM 51-41-01

Part: SHEAR TIE — CORRODED (FRM 81 S27-28L) · corrosion level 2 · airframe 45,299 hrs · 28,370 cycles

CF III, FR 81, AFT CARGO, SHEAR TIE CORRODED BETWEEN STR 28L AND 27L. CORRODED AFT CARGO SHEAR TIE IN CENTER FUSELAGE III LOCATED BETWEEN STRINGER 27L AND 28L WAS REMOVED AND REPLACED IAW SRM 51-41-01.

Part: FLOORBEAM — CORRODED (FRM 80 S29R-29L) · corrosion level 2 · airframe 45,299 hrs · 28,370 cycles

CF III, FR 80. AFT CARGO RH CENTER FLOOR SUPPORT CORRODED BETWEEN STR 29R AND 29L. REMOVED AND REPLACED FLOOR SUPPORT IN CF III IN AFT CARGO AT FR80 BETWEEN STR 29R AND STR 29L. IAW SRM 51-41-01

Part: SHEAR TIE — CORRODED (FRM 86 S27-28L) · corrosion level 2 · airframe 45,299 hrs · 28,370 cycles

CF III, FR 86, AFT LOWER FUSELAGE, SHEAR CLIP CORRODED BETWEEN STR 28L AND STR 27L. REPLACED SHEAR CLIP AT FR 86 BETWEEN STR 28L-27L IAW SRM 51-41-04 AND SRM 51-41-02.

Part: SHEAR TIE — CORRODED (FRM 81 S25-26R) · corrosion level 2 · airframe 45,299 hrs · 28,370 cycles

CF III, AFT CARGO, SHEAR CLIP CORRODED BETWEEN STR 26R AND 25R. REMOVED AND REPLACED SHEAR CLIP IN CF III IN AFT CARGO AT FR81 BETWEEN STR 26R AND STR 25R. IAW SRM 51-41-01, SRM 51-41-02, AND SRM 53-23-04

Part: SHEAR TIE — CORRODED (FRM 85 S28-29R) · corrosion level 2 · airframe 45,299 hrs · 28,370 cycles

CF III, FR 85, AFT CARGO, SHEAR CLIP CORRODED BETWEEN STR 29R AND STR 28R. REPLACED WITH PART MADE REPAIR PART IAW DRAWING 170-66063-001.PART INSTALLED IAW SRM 51-41-01 AND SRM 51-41-02.

Part: SHEAR TIE — CORRODED (FRM 83 S27-28R) · corrosion level 2 · airframe 45,299 hrs · 28,370 cycles

CF III, FR 83, AFT CARGO, SHEER CLIP CORRODED BETWEEN STR 28R AND 27R. REMOVED AND REPLACED CORRODED SHEAR CLIP IN AFT CARGO AT FR 83 BETWEEN STR 27R AND 28R IAW SRM 51-41-01.

Part: STRINGER — CORRODED (FRMS 88-89 S28R) · corrosion level 2 · airframe 45,299 hrs · 28,370 cycles

CFIII, STYRINGER 28R FOUND CORRODED BETWEEN FR 88- FR 89. DAMAGED STRINGER SECTION REMOVED. NEW STRINGER SECTION FITTED AND INSTALLED. ALL WORK CARRIED OUT IAW SRM 53-232-03 AND SRM 51-41-02.

Part: INTERCOSTAL — CORRODED (FRM 87 S18R) · corrosion level 2 · airframe 45,299 hrs · 28,370 cycles

CF III, INTERCOSTAL CORRODED AT FR 87, AT STR 18R. REMOVED AND REPLACED INTERCOSTAL AT FR 87 STR 18R IAW SRM 51-43-03

Part: SHEAR TIE — CORRODED (FRM 17 S25-26R) · corrosion level 2 · airframe 45,299 hrs · 28,370 cycles

WHEN AC WAS IN FOR HVY CK FOUND FWD CARGO BAY, SHEAR CLIP FOUND CORRODED ON FR 17 BETWEEN STR 26-25R.REPLACED SHEAR CLIP IN FWD CARGO BAY ON FR 17 BETWEEN STR 26-25R IAW SRM 51-41-0 AND SRM 51-41-02 AC RETURNED TO SERVICE

Part: DOUBLER — CORRODED (FRMS 19-20) · corrosion level 2 · airframe 45,299 hrs · 28,370 cycles

WHILE AC WAS IN FOR HVY CK FOUND LOWER FUSELAGE SKIN, FWD CARGO BAY, ANTENNA DOUBLER ON THE R/H SIDE BETWEEN FR 19-20 AND STR 27-26R FOUND CORRODED. REPLACED ANTENNA DOUBLER IN FWD CARGO BAY ON RH SIDE BETWEEN FR19-20 AND STR 27-26R IAW SRM 51-41-02. PN 170-14431-001. AC REMAINS IN YQU FOR COMPLETION.

Part: SHEAR TIE — CORRODED (FRM 76 S28-29R) · corrosion level 2 · airframe 45,299 hrs

WHILE AC WAS IN FOR HVY CK FOUND AFT CARGO SHEAR CLIP CORRODED AT FR 76, STR 29R TO STR 28R. REPLACD SHEAR CLIP IN AFT CARGO BAY AT FR 76 BETWEEN STR 28R TO 29R IAW SRM 51-41-02. PN 170-66664-001 AC REMAINS IN YQG FOR COMPLETION.

Part: SHEAR TIE — CORRODED (FRM 16 S27-28R) · corrosion level 2 · airframe 45,299 hrs · 28,370 cycles

WHEN AC WAS IN FOR HVY CK FOUND FWD CARGO BAY, SHEAR CLIP FOUND CORRODED ON FR 16 BETWEEN STR 28-27R. REPLACED SHEAR CLIP IN FWD XARGO BAY ON FR 16 BEWTEEN STR 28-27R IAW SRM 51-41-01. PN 170-03859-001 AC RETURNED TO SERVICE

Part: SHEAR TIE — CORRODED (FRM 17 S25-26R) · corrosion level 2 · airframe 45,299 hrs · 28,370 cycles

WHEN AC WAS IN FOR HVY CK FOUND FWD CARGO BAY, SHEAR CLIP FOUND CORRODED ON FR 17 BETWEEN STR 26-25R. REPLACED SHEAR CLIP IN FWD CARGO BAY ON FR 17 BEWTEEN STR 26-25R IAW SRM 51-41-01. PN 170-03859-002 AC RETURNED TO SERVICE

Part: SHEAR TIE — CORRODED (FRM 16 S27-28R) · corrosion level 2 · airframe 45,299 hrs · 28,370 cycles

WHEN AC WAS IN FOR HVY CK FOUND FWD CARGO BAY, SHEAR CLIP FOUND CORRODED ON FR 16 BETWEEN STR 28-27R. REPLACED SHEAR CLIP IN FWD XARGO BAY ON FR 16 BEWTEEN STR 28-27L IAW SRM 51-41-01. AC RETURNED TO SERVICE.

Part: SHEAR TIE — CORRODED (FRM 17 S27-28L) · corrosion level 2 · airframe 45,299 hrs · 28,370 cycles

WHEN AC WAS IN FOR HVY CK FOUND FWD CARGO BAY, SHEAR CLIP FOUND CORRODED ON FR 17 BETWEEN STR 28-27L. REPLACED FWD CARGO BAY SHEAR CLIP ON FR 17 BEWTEEN STR28-27L IAW SRM 51-41-01 PN 170-03870-001 AC RETURNED TO SERVICE

Part: SKIN — CORRODED (FRS19-20 S19-20L) · corrosion level 2 · airframe 45,299 hrs · 28,370 cycles

LOWER FUSELAGE SKIN, FWD CARGO BAY, ANTENNA DOUBLER ON THE L/H SIDE BETWEEN FR 19-20 AND STR 27-26L FOUND CORRODED. REPLACED ANTENNA DOUBLER IN FWD CARGO BAY ON LH SIDE BETWEEN FR19-20 AND STRL 27-26R IAW SRM 51-41-02

Part: DOUBLER — CORRODED (FRM 17 S27-28R) · corrosion level 2 · airframe 45,299 hrs

WHILE AC WAS IN FOR HVY CK FOUND FWD CARGO BAY, SHEAR CLIP FOUND CORRODED ON FR 17 BETWEEN STR 28-27R. REPLACED SHEAR CLIP IN FWD CARGO BAY ON FR 17 BETWEEN STR 28-27R IAW SRM 51-41-01. PN 170-03335-001 AC REMAINS IN YQG FOR COMPLETION.

Part: INTERCOSTAL — CORRODED (ZONE 100) · corrosion level 2 · airframe 45,299 hrs

WHILE AC WAS IN FOR HVY CK FOUND LOWER FUSELAGE III, 2 INTERCOSTALS PLUS 2 CLIPS CORRODED BETWEEN FR 86 AND FR 87, STR 28R AND 27R. REPLACED ANGLE AND INTERCOSTAL IAW SRM 51-41-02 SRM 51-41-01 MADE REPAIR PARTS FROM DRAWINGS 170-87562 AND 170-87563. PN 170-87560-001 AC REMAINS IN YQG FOR COMPLETION.

Part: SEAT TRACK — CORRODED (FRMS 12-18) · corrosion level 2 · airframe 45,299 hrs · 28,370 cycles

WHILE AC WAS IN FOR HVY CK FOUND FWD PASSENGER FLOOR STRUCTURE, RH SEAT TRACK CORRODED IN BETWEEN FR12 TO FR 13, AND FR13.5 TO FR 14, AND FR 17 TO FR 18 RBL 12. REPLACED SEAT TRACK FROM FR12 TO FR 20 IAW SRM 51-43--03 AND SRM 51-43-04 PN 170-03263-001. AC REMAINS IN YQU FOR COMPLETION.

Part: WASTE BOX — CORRODED (ZONE 100) · corrosion level 2 · airframe 45,299 hrs

WHILE AC WAS IN FOR HVY CK FOUND WASTE BOX ASSEMBLY DELAMINATED AND CORRODED. REPLACED WASTE BOX IAW SRM 51-43-04 PN 170-65078-405 AC REMAINS IN YQG FOR COMPLETION.

Part: SHEAR TIE — CORRODED (FRM 88 S27-28R) · corrosion level 2 · airframe 45,299 hrs · 28,370 cycles

WHILE AC WAS IN FOR HVY CK FOUND FR 88 BTW STR 28R AND 27R SHEAR CLIP CORRODED. REPLACED SHEAR CLLIP AT FR 88 BETWEEN STR 27R TO 28R IAW SRM SRM 51-41-01 AND SRM 51-41-02 PN 170-66531-001, AC REMAINS IN YQU FOR COMPLETION.

Part: SHEAR TIE — CORRODED (FRM 87 S27-28R) · corrosion level 2 · airframe 45,299 hrs · 28,370 cycles

WHILE AC WAS IN FOR HVY CK FOUND FRAME 87 BTW STR 28R ABD 27R SHEAR CLIP CORRODED. REPLACED SHEAR CLIP AT FR87 BETWEEN STR 27R TO 28R IAW SRM 51-41-01 AND SRM 51-41-02. PN 170-66041-002 AC REMAINS IN YQU FOR COMPLETION.

Part: DOUBLER — CORRODED (WASTE DOOR) · corrosion level 2 · airframe 45,299 hrs · 28,370 cycles

WHILE AC WAS IN FOR HVY CK FOUND CORROSION FOUND ON WASTE DOOR DOUBLER. REPLACED WASTE DOOR DOUBLER IAW SRM 51-41-01. PN 170-66931-001. AC REMAINS IN YQG FOR COMPLETION.

Part: DOOR — CORRODED (AFT WASTE) · corrosion level 2 · airframe 45,299 hrs · 28,370 cycles

WHILE AC WAS IN FOR HVY CK FOUND AFT WASTE DOOR CORRODED. REPLACED AFT WASTE DOOR IAW AMM 53-03-60-440-801-A PN 170-86668-403. AC REMAINS IN YQG FOR COMPLETION.

Part: NONE — NONE (ZONE 100) · airframe 43,040 hrs · 26,736 cycles

DAMAGED PHOTOLUMINESCENT FLOOR PATH MARKING SEGMENT IN FRONT OF WARDROBE. R&R DAMAGED SEGMENT.

Part: NONE — NONE (ZONE 100) · airframe 43,040 hrs · 26,736 cycles

DAMAGED PHOTOLUMINESCENT FLOOR PATH MARKING SEGMENT IN FRONT OF WARDROBE. R&R DAMAGED SEGMENT.

Part: BATTERY — INOPERATIVE (ZONE 100) · airframe 43,040 hrs · 26,736 cycles

RH AFT DOOR EXIT MARKING SIGN DOES NOT ILLUMINATE. R&R AFT RH EMERGENCY BATTERY.

Part: WARNING MESSAGE — FALSE ACTIVATION (LT WING TE FLAPS) · airframe 39,633 hrs · 24,532 cycles

FLAP LOW RATE EICAS MESSAGE. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. PERFORMED FIM 27-53-0081-802-A. MESSAGE CLEARED.

Part: ACTUATOR — FAILED (ZONE 500) · airframe 39,623 hrs · 24,526 cycles

FLAP FAIL ON APPROACH WITHOUT ACTUATING THE FLAP HANDLE. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. R&R SF-ACE 1 IAW AMM 27-53-02. PERFORMED ELECTRONIC RIGGING IAW AMM 27-50-00-820-802. OPS CHECK GOOD.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,616 hrs · 24,521 cycles

WHILE IN HEAVY CHECK-AFT WET AREA FR 87 RH FLOOR BEAM AT THE EDGE OF RH SHEAR PANEL HAS CORROSION.REMOVED AND REPLACED AFT WET AREA FR 86-89 RH FLOOR BEAM REF. EMB SRM 51-40-08.

Part: SHEAR PANEL — CORRODED (FUSELAGE) · airframe 39,616 hrs · 24,521 cycles

WHILE IN HEAVY CHECK-AFT WET AREA RH SHEAR PANEL HAS CORROSION AREA.REMOVED AND REPLACED SHEAR PANEL REF. EMB SRM 51-40-08.

Part: SUPPORT BRACKET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,616 hrs · 24,521 cycles

WHILE IN HEAVY CHECK-CORROSION FOUND ON SUPPORT BRACKET ATTACHED TO INTERCOSTAL STGR 26R BETWEEN FR 80-81.REMOVED AND REPLACED BRACKET REF: SRM 51-40-08

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,616 hrs · 24,521 cycles

WHILE IN HEAVY CHECK-AFT WET AREA AT FR 90 GUSSET PLATE HAS CORROSION AS MARKED. REMOVED AFT WET AREA AT FR 90 GUSSET PLATE REF: EMB SRM 51-40-08. INSTALLED NEW AFT WET AREA AT FR 90 GUSSET PLATE REF: EMB SRM 51-21-01, SRM 51-40-08

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,616 hrs · 24,521 cycles

WHILE IN HEAVY CHECK-SHEAR CLIP CORRODED AT FR 80 STRG. 27L/28L.REMOVED AND REPLACED SHEAR CLIP REF. EMB SRM 51-40-08.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,616 hrs · 24,521 cycles

DURING HEAVY CHECK MAINTENANCE FOUND CORROSION FOUND ON SHEAR CLIP AT FR81 STGR 27R-28R. REMOVED AND REPLACED SHEAR CLIP AT FR-81 STGR 27R-28R REF. EMB SRM 51-40-08. A/C REMAINS IN CHECK.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,616 hrs · 24,521 cycles

DURING HEAVY CHECK MAINTENANCE FOUND SUPPORT IS CORRODED AT FR 80 BETWEEN STRINGERS 27R AND 28R. REMOVED AND REPLACED SUPPORT AT FR 80 BETWEEN STRINGERS 27R AND 28R REF. EMB SRM 51-40-08. RESTORED SURFACE PROTECTION ON SUPPORT AT FR 80 BETWEEN STRINGERS 27R AND 28R, REF SRM 51-23-06, CPM 51-25-00. A/C REMAINS IN CHECK.

Part: THRESHOLD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,616 hrs · 24,521 cycles

DURING HEAVY CHECK MAINTENANCE FOUND FORWARD PASSENGER DOOR LOWER BEAM HAS AREAS OF CORROSION BELOW FORWARD AND AFT GIRT BAR FLOOR FITTINGS. REMOVED AND REPLACED L1 DOOR THRESHOLD PER SRM 51-40-08. A/C REMAINS IN CHECK.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,616 hrs · 24,521 cycles

DURING HEAVY CHECK MAINTENANCE FOUND FRAME 80 IS CORRODED AT STRINGER 28R. REMOVED AN REPLACED FRAME 80 REF EMB SRM 51-40-08, 51-23-05, 51-23-06, CPM 51-25-00. A/C REMAINS IN CHECK.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,616 hrs · 24,521 cycles

DURING HEAVY CHECK MAINTENANCE FOUND CORRODED SHEAR CLIP @ FR 82 ST 27R-28R. REMOVED AND REPLACED NEW SHEAR CLIP @ FR 82 STRG 27R-28R. REF: SRM 51-40-08. A/C REMAINS IN CHECK.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,616 hrs · 24,521 cycles

DURING HEAVY CHECK MAINTENANCE FOUND CORRODED SHEAR CLIP @ FR 84 ST 27-28R. REMOVED AND REPLACED SHEAR CLIP @ FR 84 ST 27-28R. REF: SRM 51-40-08, 51-23-05, 51-23-06, CPM 51-25-00. A/C REMAINS IN CHECK.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,616 hrs · 24,521 cycles

DURING HEAVY CHECK MAINTENANCE FOUND CORRODED SHEAR CLIP @ FR 85 ST 27-28L. REMOVED AND REPLACED NEW SHEAR CLIP AT FR 85 STR 27-28L REF SRM 51-40-08, RESTORED SURFACE PROTECTION TO SHEAR CLIP AT FR 85 ST 27-28L REF SRM 51-23-05 AND 51-23-06, CPM 51-25-00. A/C REMAINS IN CHECK.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,616 hrs · 24,521 cycles

DURING HEAVY CHECK MAINTENANCE FOUND CORRODED SHEAR CLIP @ FR 87 ST 27-28R. REMOVED AND REPLACED SHEAR CLIP @ FR87 STRG 27-28R. REF: SRM 51-40-08. A/C REMAINS IN CHECK.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,616 hrs · 24,521 cycles

DURING HEAVY CHECK MAINTENANCE FOUND CORRODED SHEAR CLIP @ FR 84 ST 28-29R. REMOVED AND REPLACED NEW SHEAR CLIP @ FR 84 ST 28-29R. REF: SRM 51-40-08. A/C REMAINS IN CHECK.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,616 hrs · 24,521 cycles

DURING HEAVY CHECK MAINTENANCE FOUND CORRODED SHEAR CLIP @ FR 74 ST 28-29R. REMOVED AND REPLACED SHEAR CLIP @ FR74 STGR 28-29R. REF: SRM 51-40-08, 51-23-05, 51-23-06, CPM 51-25-00. A/C REMAINS IN CHECK.

Part: SUPPORT BEAM — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 39,616 hrs · 24,521 cycles

DURING HEAVY CHECK MAINTENANCE FOUND CORROSION ON CARGO DOOR SUPPORT BEAM BETWEEN FR 80-81 @ ST 27R. REMOVED AND REPLACED CARGO DOOR SUPPORT BEAM BETWEEN FR 80-81 @ ST 27R PER SRM 51-40-08. RESTORED SURFACE PROTECTION ON CARGO DOOR SUPPORT BEAM BETWEEN FR 80-81 @ ST 27R,REF SRM 51-23-06, CPM 51-25-00. A/C REMAINS IN CHECK.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,616 hrs · 24,521 cycles

DURING HEAVY CHECK MAINTENANCE FOUND CORROSION ON ST 28L BETWEEN FR 76-77. REMOVED AND REPLACED NEW STRINGER 28L FILLER AND 2EA SPLICES REF SRM 53-23-03/REPAIR 05P. A/C REMAINS IN CHECK.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,616 hrs · 24,521 cycles

DURING HEAVY CHECK MAINTENANCE FOUND CORRODED SHEAR CLIP @ FR 86 ST 27-28R. REMOVED AND REPLACED SHEAR CLIP @ FR86 ST 27-28R. REF: SRM 51-40-08, 51-23-05, 51-- 23-06, CPM 51-25-00. A/C REMAINS IN CHECK.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,616 hrs · 24,521 cycles

DURING HEAVY CHECK MAINTENANCE FOUND CORRODED SHEAR CLIP @ FR 85 ST 27-28R. REMOVED AND REPLACED SHEAR CLIP @FR 85 STRG 27-28R. REF: SRM 51-40-08. A/C REMAINS IN CHECK.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,616 hrs · 24,521 cycles

DURING HEAVY CHECK MAINTENANCE FOUND CORRODED SHEAR CLIP @ FR 88 ST 27-28R. REMOVED AND REPLACED SHEAR CLIP @ FR88 STRG 27-28R. REF: SRM 51-40-08. A/C REMAINS IN CHECK.

Part: PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,616 hrs · 24,521 cycles

DURING HEAVY CHECK MAINTENANCE FOUND SURFACE CORROSION ON FLANGE ON PANEL 195HL. REMOVED AND REPLACED 2EA FLANGES P/N 170-08513-405, 170-16334-403, 3EA CRACKED RECEPTACLES REF EMB SRM 51-40-08, AMM 20-10-01. A/C REMAINS IN CHECK.

Part: PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,616 hrs · 24,521 cycles

DURING HEAVY CHECK MAINTENANCE FOUND LITE CORROSION ON 2 EA FLANGES AS MARKED ON PANEL 195ER. REMOVED AND REPLACED 2EACH FLANGES ON PANEL 195ER REF EMB SRM 51-40-08. A/C REMAINS IN CHECK.

Part: BRACKET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,616 hrs · 24,521 cycles

DURING HEAVY CHECK MAINTENANCE FOUND AFT CARGO DONE BRACKET CORRODED AT FR 76 BETWEEN STR 28R AND STR 28 L. CORRECTION TO ORIGINAL DISCREPANCY: LOCATION OF DOME BRACKET IS AT FR 77 STGR 28R-28L. REMOVED AND REPLACED AFT CARGO DOME BRACKET AT FR 77 BETWEEN STGR 28R-28L. A/C REMAINS IN CHECK.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,616 hrs · 24,521 cycles

DURING HEAVY CHECK MAINTENANCE FOUND RH INBD (FLOOR) SEAT TRACK FR 59/74 THRU 84 (P/N:170-86082-005) HAS SPOTS OF CORROSION. REMOVED AND REPLACED RH INBD (FLOOR) SEAT TRACK FR 59/74 THRU 84 (P/N:170-86082-005)REF EMB SRM 51-40-08, 51-23-06 AND CPM 51-25-00. A/C REMAINS IN CHECK.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,616 hrs · 24,521 cycles

DURING HEAVY CHECK MAINTENANCE FOUND LH INBD SEAT TRACK FLOOR FLANGE HAS SEVERAL SPOTS OF CORROSION AT FR 19-23. PERFORMED SEAT TRACK SPLICE REPAIR ON LH I/B SEAT TRACK FR 19-23. REF EMB SRM 53-00-10/REPAIR 01P, ETD2019-170-143569. A/C REMAINS IN CHECK.

Part: SEAT TRACK — CORRODED (FRAMES 23-43) · corrosion level 2 · airframe 39,616 hrs · 24,521 cycles

DURING HEAVY CHECK MAINTENANCE FOUND RH INBD (FLOOR) SEAT TRACK FR 23 THRU 34/43 (P/N:170-67660-431) HAS SPOTS OF CORROSION. REMOVED AND REPLACED RH INBD (FLOOR) SEAT TRACK BETWEEN FR 23 THRU 34/43 REF: SRM 51-40-08, 51-23-06, CPM 51-25-00. A/C REMAINS IN CHECK

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,616 hrs · 24,521 cycles

DURING HEAVY CHECK MAINTENANCE FOUND LH AFT DOUBLER FR 19-20 LBL 12.5"- LBL 36" HAS CORROSION. REMOVED AND REPLACED LH AFT DOUBLER FR 19-20 LBL 12.5"- LBL 36 REF. EMB SRM 51-- 40-08. A/C REMAINS IN CHECK.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,616 hrs · 24,521 cycles

DURING HEAVY CHECK MAINTENANCE FOUND LH AFT SILL HAS CORROSION FR 19-21 LBL 44"-49". REMOVED AND REPLACED LH AFT SILL AT FR 19-21 LBL 44"-49" PER SRM 51-40-08. A/C REMAINS IN CHECK.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,616 hrs · 24,521 cycles

DURING HEAVY CHECK MAINTENANCE FOUND LH INBD SEAT TRACK FLOOR FLANGE HAS SEVERAL SPOTS OF CORROSION AT FR 19-20 WITH 100% MATERIAL LOSS AT FR 19. REMOVED AND REPLACED L-H I/B SEAT TRACK FR 12-20. REF EMB SRM 51-40-08. A/C REMAINS IN CHECK.

Part: SLIDE — PARTIAL DEPLOY (L1 DOOR) · airframe 38,693 hrs · 23,953 cycles

L1 DOOR SLIDE HAS BEEN PARTIALLY DEPLOYED, GIRT BAR ENGAGED, DOOR HALF OPEN, SLIDE IS HANGING DOWN, JET BRIDGE KEEPING SLIDE FROM BLOWING THE REST OF THE WAY, BOTH HANDLES ARE UP. FERRIED TO CMH. R&R L1 EVAC DOOR SLIDE IAW AMM 25-65-01.

Part: DOOR — LACK OF LUBE (L1) · airframe 37,624 hrs · 23,327 cycles

L1 DOOR IS OPERATING DIFFICULTLY DURING OPEN/CLOSE FROM INSIDE AND OUTSIDE. LUBRICATED L1 DOOR IAW AMM 52-11-22. OPS CHECK GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION (TE FLAPS) · airframe 37,523 hrs · 23,266 cycles

FLAP FAIL AT CRUISE FL330. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. PERFORMED FIM TASK 27-51-00-810-802-A, CLEARED INHIBITS AND PERFORMED FLAPS ACE 1 AND ACE 2 MESSAGES. CLEARED ON EICAS AT THIS TIME, OPS CHECK GOOD IAW AMM 27-51-01.

Part: CONTROL LEVER — FAULTY (TE FLAPS) · airframe 37,524 hrs · 23,267 cycles

FLAP FAIL MESSAGE AT FL360 ENROUTE. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. R&R RHOB T3 SKEW SENSOR AND FLAP/SLAT CONTROL LEVER IAW AMM 27-53-01. OPS CHECK GOOD. FLAP SKEW SENSOR P/N 5912843-7 S/N 9058 TSN 2267 CSN 1403

Part: SIGN — INOPERATIVE (CABIN) · airframe 36,763 hrs · 22,802 cycles

***WHILE AIRCRAFT WAS IN HEAVY CHECK*** MAINTENANCE REPORTED EMERGENCY EXIT LIGHTED SIGNS AT L1 DOOR AND R1 DOORS TO BE NOT COMPLETELY ILLUMINATED. BOTH EMERGENCY EXIT LIGHTS WERE REMOVED AND REPLACED WITH PART NUMBERS 4028-23 AND 4028-13. OPERATIONAL CHECK GOOD IAW EAMM 33-50-15-400-801-A.

Part: SIGN — INOPERATIVE (CABIN) · airframe 36,763 hrs · 22,802 cycles

***WHILE AIRCRAFT WAS IN HEAVY CHECK*** MAINTENANCE REPORTED EMERGENCY EXIT LIGHTED SIGNS AT L1 DOOR AND R1 DOORS TO BE NOT COMPLETELY ILLUMINATED. BOTH EMERGENCY EXIT LIGHTS WERE REMOVED AND REPLACED WITH PART NUMBERS 4028-23 AND 4028-13. OPERATIONAL CHECK GOOD IAW EAMM 33-50-15-400-801-A.

Part: DOOR — LACK OF LUBE (ZONE 800) · airframe 36,361 hrs · 22,556 cycles

L1 DOOR STICKS, HARD TO OPEN/CLOSE. LUBED AND OPS CHECKED IAW AMM 52-11-00.

Part: ACTUATOR — FAILED (TE FLAPS) · airframe 35,257 hrs · 21,864 cycles

FLAPS FAILED DURING DESCENT. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. R & R THE NR 2 FLAP ACTUATOR IAW AMM 27-51-03. OPS CHECKED GOOD.

Part: FLAP SYSTEM — FAILED · airframe 35,254 hrs · 21,862 cycles

FLAP FAIL DURING DESCENT. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. PERFORMED INSPECTIONS OF FLAP ACTUATORS. NO DEFECTS OR OVERTORQUE INDICATIONS NOTED.

Part: BEARING — DIRTY (L1 DOOR) · airframe 35,202 hrs · 21,832 cycles

L1 DOOR DIFFICULT TO OPEN AND CLOSE. CLEANED THE DOOR BALL BEARING AND PERFORMED OPERATIONAL CHECK IAW AMM 52-11-00. OPS CHECKED GOOD.

Part: SENSOR — MALFUNCTIONED (TE FLAPS) · airframe 35,121 hrs · 21,784 cycles

FLAP FAIL ON EICAS. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. R & R THE RT FLAP POSITION SENSOR IAW MM 27-53-04. OPS CHECKED SATISFACTORY.

Part: CONNECTOR — DIRTY (TE FLAPS) · airframe 35,108 hrs · 21,776 cycles

FLAP FAIL. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. CLEARED INHIBITS, CLEANED THE CONNECTORS, OPS CHECKED GOOD.

Part: NUT PLATE — CORRODED (FRAMES 87-89) · corrosion level 2 · airframe 34,212 hrs · 21,252 cycles

*** WHILE AIRCRAFT WAS IN FOR HEAVY CHECK *** MAINTENANCE REPORTED LEVEL 2 CORROSION ON THE 2ND MOST AFT NUTPLATE CLIP AT THE L2 DOOR LOWER SILL BEAM. MAINTENANCE REMOVED AND REPLACED THE 2ND MOST AFT NUTPLATE CLIP AT THE L2 DOOR LOWER SILL BEAM IAW E170 SRM 51-41-01, 51-75-16 & 51-40-02. AIRCRAFT IS CURRENTLY STILL OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: DOUBLER — CORRODED (FRAMES 17-24) · corrosion level 2 · airframe 34,212 hrs · 21,252 cycles

*** WHILE AIRCRAFT WAS OUT OF SERVICE FOR HEAVY CHECK *** MAINTENANCE FOUND LEVEL 2 CORROSION ON FWD CARGO DOOR CUT OUT STRUCTURE ( FWD AND AFT DOUBLERS)THEY REMOVED AND REPLACED DOUBLERS IAW EMB 170 SRM 51-41-02, 51-43-02. AIRCRAFT REMAINS OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: SEAL REST — CORRODED (FRAMES 85-87) · corrosion level 2 · airframe 34,212 hrs · 21,252 cycles

*** WHILE AIRCRAFT WAS IN FOR HEAVY CHECK *** MAINTENANCE REPORTED LEVEL 2 CORROSION ON THE L2 DOOR LOWER SILL BEAM. MAINTENANCE REMOVED AND REPLACED THE L2 DOOR LOWER SILL BEAM IAW E170 SRM 51-43-01, 51-10-03 & 51-43-02. AIRCRAFT IS CURRENTLY STILL OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: NUT PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,212 hrs · 21,252 cycles

WHILE AIRCRAFT WAS IN HEAVY CHECK, MAINTENANCE REPORTED LEVEL 2 CORROSION AT THE L2 DOOR MOST AFT NUT-PLATE CLIP AT THE LOWER SILL BEAM. MAINTENANCE REMOVED AND REPLACED THE MOST AFT NUT-PLATE CLIP AT THE LOWER SILL BEAM AT L2 DOOR IAW SRM 51-41-01, 51-40-02 & 51-41-02. AIRCRAFT IS STILL OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: NUT PLATE — CORRODED (FRAMES 85-86) · corrosion level 2 · airframe 34,212 hrs · 21,252 cycles

*** WHILE AIRCRAFT WAS IN FOR HEAVY CHECK *** MAINTENANCE REPORTED LEVEL 2 CORROSION AT THE R2 DOOR LOWER SILL BEAM NUTPLATE BRACKET. MAINTENANCE REMOVED & REPLACED THE R2 DOOR LOWER SILL BEAM NUTPLATE BRACKET IAW E170 SRM 51-10-03, 51-75-16 & 51-40-02 AND REPUBLIC EO 170EO-53-15-0003. AIRCRAFT IS CURRENTLY STILL OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,212 hrs · 21,252 cycles

WHILE AIRCRAFT WAS IN FOR HEAVY CHECK, MAINTENANCE REPORTED LEVEL 2 CORROSION ON THE SHEAR CLIP AT FR83, STR 27R-28R. MAINTENANCE REMOVED AND REPLACED THE SHEAR CLIP AT FR83, STR 27R-28R IAW SRM 51-43-03, 51-41-02 & 51-40-02. AIRCRAFT IS CURRENTLY STILL OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: FLOOR SUPPORT — CORRODED (FRAME 89) · corrosion level 2 · airframe 34,212 hrs · 21,252 cycles

*** WHILE AIRCRAFT WAS IN FOR HEAVY CHECK *** MAINTENANCE REPORTED LEVEL 2 CORROSION ON THE AFT GALLEY FLOOR PANEL SUPPORT AT FR89. MAINTENANCE REMOVED AND REPLACED THE AFT GALLEY FLOOR PANEL SUPPORT AT FR89 IAW E170 SRM 51-42-01 & 51-40-02. AIRCRAFT IS CURRENTLY STILL OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,212 hrs · 21,252 cycles

WHILE AIRCRAFT WAS IN FOR HEAVY CHECK, MAINTENANCE REPORTED LEVEL 2 CORROSION ON THE RT FLOOR SILL AT FR12. MAINTENANCE REMOVED AND REPLACED THE RT FLOOR SILL AT FR12 IAW SRM 51-43-02, 51-41-02 & 51-40-02. AIRCRAFT IS CURRENTLY STILL OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: SPLICE PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,212 hrs · 21,252 cycles

WHILE AIRCRAFT WAS IN FOR HEAVY CHECK, MAINTENANCE REPORTED LEVEL 2 CORROSION ON THE SPLICE PLATE AT FR90. MAINTENANCE REMOVED AND REPLACED THE SPLICE PLATE AT FR90 IAW SRM 51-43-03 & 51-40-02. AIRCRAFT IS CURRENTLY STILL OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: SHEAR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,212 hrs · 21,252 cycles

WHILE AIRCRAFT WAS IN FOR HEAVY CHECK, MAINTENANCE REPORTED LEVEL 2 CORROSION ON THE RT SHEAR PANEL AT FR89, AROUND GALLEY MOUNT HOLES. MAINTENANCE REMOVED AND REPLACED THE RT SHEAR PANEL AT FR89 IAW SRM 51-42-01 & 51-40-02. AIRCRAFT IS CURRENTLY STILL OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: SPLICE PLATE — CORRODED (FRAME 88) · corrosion level 2 · airframe 34,212 hrs · 21,252 cycles

*** WHILE AIRCRAFT WAS IN FOR HEAVY CHECK *** MAINTENANCE REPORTED LEVEL 2 CORROSION ON THE RH SHEAR PANEL SPLICE PLATE AT FR88. MAINTENANCE REMOVED AND REPLACED THE RH SHEAR PANEL SPLICE PLATE AT FR88 IAW E170 SRM 51-42-02 & 51-40-02. AIRCRAFT IS CURRENTLY STILL OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,212 hrs · 21,252 cycles

WHILE AIRCRAFT WAS IN FOR HEAVY CHECK, MAINTENANCE REPORTED LEVEL 2 CORROSION ON THE GUSSET PLATE AT FR90, RBL20. MAINTENANCE REMOVED AND REPLACED THE GUSSET PLATE AT FR90, RBL20 IAW SRM 51-42-02, 51-75-16, 51-40-02 & 51-4-04. AIRCRAFT IS CURRENTLY STILL OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: UPPER SHEET — CORRODED (FRAMES 54-85) · corrosion level 2 · airframe 34,212 hrs · 21,252 cycles

*** WHILE AIRCRAFT WAS IN FOR HEAVY CHECK *** MAINTENANCE REPORTED LEVEL 2 CORROSION ON THE FLOOR BEAM CAP AT FR84-FR85, RBL10. MAINTENANCE REMOVED & REPLACED THE FLOOR BEAM CAP AT FR84-FR85, RBL10 IAW E170 SRM 51-40-08 & 51-40-02. AIRCRAFT IS CURRENTLY STILL OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: UPPER SHEET — CORRODED (FRAMES 84-85) · corrosion level 2 · airframe 34,212 hrs · 21,252 cycles

*** WHILE AIRCRAFT WAS IN FOR HEAVY CHECK *** MAINTENANCE REPORTED LEVEL 2 CORROSION ON THE FLOOR BEAM CAP AT FR84-FR85, LBL10. MAINTENANCE REMOVED AND REPLACED THE FLOOR BEAM CAP AT FR84-FR85, LBL10 IAW E170 SRM 51-40-08 & 51-40-02. AIRCRAFT IS CURRENTLY STILL OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: SUPPORT — CORRODED (OXYGEN BOTTLE) · corrosion level 2 · airframe 34,212 hrs · 21,252 cycles

*** WHILE THE AIRCRAFT WAS OUT OF SERVICE FOR HEAVY CHECK *** MAINTENANCE FOUND LEVEL 2 CORROSION ON SUPPORT STRUCTURE BELOW 02 BOTTLE FWD CARGO. THEY REMOVED AND REPLACED REINFORCEMENT ASSY 170-67676-001 IAW EMB 170 SRM 53-21-04. AIRCRAFT REMAINS OUT OF SERVICE FOR HEAVY CHECK COMPLETION

Part: STRUCTURE — CRACKED (LT WING) · airframe 34,212 hrs · 21,252 cycles

WHILE AIRCRAFT WAS IN FOR HEAVY CHECK, MAINTENANCE REPORTED A CRACK ON THE LT WING SLAT NR 2 O/B SLAT TRACK CUT OUT ON FIXED LEADING EDGE. MAINTENANCE ACCOMPLISHED REPAIR TO THE LT WING SLAT NR 2 O/B SLAT TRACK CUT OUT ON FIXED LEADING EDGE IAW SRM 57-49-01. AIRCRAFT IS CURRENTLY STILL OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: DOOR — LACK OF LUBE (L1) · airframe 31,737 hrs · 19,657 cycles

CREW REPORTED THAT THE L1 DOOR WAS DIFFICULT TO OPEN. MAINTENANCE LUBED DOOR IAW AMM AND OPS CHECKED GOOD.

Part: SPRING — MISSING (DOOR INDICATOR) · airframe 31,628 hrs · 19,588 cycles

CREW REPORTED THAT THE L1 DOOR LATCH VIUAL INDICATOR WAS NOT SHOWING IN WINDOW. MAINTENANCE INSTALLED MISSING SPRING ON INDICATOR AFT COMMAND RAMP IAW AMM AND OPS CHECKED GOOD.

Part: SIGN — INOPERATIVE (CALL) · airframe 31,352 hrs · 19,403 cycles

MAINTENANCE REPORTED THAT THE FORWARD FLIGHT ATTENDANT ORANGE RAINBOW LIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED FORWARD AREA CALL SIGN IAW AMM AND OPS CHECKED GOOD.

Part: ROLLER — OUT OF ADJUST (L1 DOOR) · airframe 29,685 hrs · 18,378 cycles

L1 DOOR HARD TO CLOSE. FERRIED, ADJUSTED FWD PASSENGER DOOR LOWER ROLLERS, OPS CHECK GOOD IAW MM 52-11-00.

Part: LIGHT — MISSING (CABIN) · airframe 29,678 hrs · 18,372 cycles

SECTION OF EMERGENCY LIGHT STRIP MISSING NEAR 2A. REPLACED THE LIGHT IAW AMM 33-50-21.

Part: DOOR — OUT OF ALIGNMENT (L1) · airframe 29,537 hrs · 18,278 cycles

L1 DOOR IS VERY STIFF TO OPERATE. ADJUSTED L1 DOOR PARALLEL ALIGNMENT COMMAND RAMPS IAW AMM 52-11-00. OPS CHECK GOOD.

Part: RAMP — OUT OF ADJUST (L1 DOOR) · airframe 29,537 hrs · 18,278 cycles

L1 DOOR IS VERY STIFF TO OPERATE. ADJUSTED L1 DOOR PARALLEL ALIGNMENT COMMAND RAMPS IAW AMM 52-11-00. OPS CHECK GOOD.

Part: LIGHT — DISCONNECTED (COCKPIT) · airframe 29,450 hrs · 18,217 cycles

COCKPIT EMERGENCY LIGHT DID NOT ILLUMINATE. CONNECTED COCKPIT EMERGENCY LIGHT IAW AMM 33-50-03. OPS CHECKED GOOD.

Part: HINGE BRACKET — CRACKED (HORIZONTAL STAB) · airframe 29,435 hrs · 18,206 cycles

RIGHT HORIZONTAL STAB NR 4 ELEVATOR HINGE BRACKET CRACKED AT UPPER RIB AFT ATTACH HOLE. THE RT HORIZONTAL STAB NR 4 ELEVATOR HINGE WAS TEMPORARILY REPAIRED IAW ETD2016-170-005210.

Part: SKIN — DAMAGED (ZONE 200) · airframe 29,435 hrs · 18,206 cycles

DAMAGED HORIZONTAL UPPER SKIN. THE RT HORIZONTAL UPPER SKIN WAS REPAIRED IAW ETD2016-170-003344.

Part: SKIN — GOUGED (ZONE 100) · airframe 29,435 hrs · 18,206 cycles

SEVERAL GOUGES ON AFT CARGO DOOR LOWER CUTOUT. R & R AFT CARGO DOOR LOWER CUT-OUT BEAM IAW SRM 51-40-02, 51-41-01, AND 51-43-01.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 29,435 hrs · 18,206 cycles

RIGHT HORIZONTAL STABILIZER RIB 11 IS CRACKED AT LOWER ATTACH POINT 6 RIVETS BACK FROM FWD SPAR. REPAIRED RIB 11A LOWER ATTACH FLANGE. TRIMMED OUT FLANGE, FABRICATED AND INSTALLED SHEAR CLIP IAW ETD2016-170-002217.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 29,435 hrs · 18,206 cycles

MAJOR REPAIR - LT HORIZONTAL STABILIZER RIB 10 IS CRACKED AT LOWER SKIN ATTACH POINT, 7 RIVETS BACK FROM FWD SPAR. REPAIRED RIB 10A, TRIMMED OUT CRACKED FLANGE, FABRICATED AND INSTALLED SHEAR CLIP IAW ETD2016-170-002217.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 29,435 hrs · 18,206 cycles

RT HORIZONTAL STABILIZER RIB 10 IS CRACKED ON LOWER SKIN ATTACH POINT 7 RIVETS BACK FROM FWD SPAR. REPAIRED RIB 10A, TRIMMED OUT 2 CRACKED FLANGES, FABRICATED AND INSTALLED 2 SHEAR CLIPS IAW ETD2016-170-002217.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 29,435 hrs · 18,206 cycles

RT HORIZONTAL STABILIZER RIB NR 12 IS CRACKED AND LOWER SKIN ATTACH POINT 6 RIVETS BACK FROM FWD SPAR. REPAIRED RIB 12A, 2 CRACKED FLANGES. TRIMMED OUT FLANGES, FABRICATED AND INSTALLED SHEAR CLIPS IAW ETD2016-170-002217.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 29,435 hrs · 18,206 cycles

RIGHT HORIZONTAL STABILIZER HAS 2 CRACKS ON RIB 11 AT UPPER SKIN ATTACH POINT 5 AND 6 RIVETS BACK FROM FWD SPAR. REPAIRED 2 UPPER FLANGES ON RIB 11A. TRIMMED OUT FLANGES, FABRICATED AND INSTALLED 2 SHEAR CLIPS IAW ETD2016-170-002217.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 29,435 hrs · 18,206 cycles

LT HORIZONTAL STABILIZER RIB 11 IS CRACKED AT LOWER SKIN ATTACH POINT, 6 RIVETS BACK FROM FWD SPAR. REPAIRED 2 CRACKED RIB 11A OF TRIMMING OUT FLANGE, FABRICATED AND INSTALLED SHEAR CLIPS IAW ETD2016-170-002217.

Part: SHEAR TIE — CORRODED (FRAME 81) · airframe 29,435 hrs · 18,206 cycles

CORROSION FOUND ON SHEAR TIE IN AFT CARGO ON FRAME 81 LOCATED BETWEEN STRINGERS 27R AND 28R. R & R SHEAR TIE.

Part: ACCESS PANEL — CORRODED · corrosion level 2 · airframe 29,435 hrs · 18,206 cycles

WASTE BOX ACCESS PANEL EVIDENCE OF CORROSION. R & R WASTE BOX ACCESS PANEL AND INSTALLED PLACARD IAW AMM 53-03-60 AND AMM 20-10-09.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 29,435 hrs · 18,206 cycles

LEFT HORIZONTAL STABILIZER L/E RIB 4 CRACKED. TRIMMED CUT OUT DAMAGE, MFG DOUBLER AND FILLER AND INSTALLED IAW ETD2016-170-000722.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 29,435 hrs · 18,206 cycles

RIGHT HORIZONTAL STAB L/E 341AR HAS 2 CRACKED RIBS AS MARKED. REPAIRED RIB 4 AND 5 IAW ETD2016-170-000261.

Part: COVER — CRACKED (EMERGENCY LIGHT) · airframe 29,327 hrs · 18,137 cycles

FWD SERVICE DOOR EMERGENCY EXIT LIGHT OVER CRACKED. R & R IAW AMM 33-50-17.

Part: FLAP SYSTEM — FAILED (ZONE 500) · airframe 28,697 hrs · 17,710 cycles

FLAP FAIL EICAS MESSAGE IN FLIGHT. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. CLEARED SLAT/FLAP INHIBITS ON ACE 1 AND 2 IAW FIM 27-51-00-810-805, NO DEFECTS NOTED. PERFORMED SLAT/FLAP OPS CHECK IAW AMM 27-50-00-05, OPS CHECK GOOD.

Part: ROLLER — STUCK (L1 DOOR) · airframe 28,437 hrs · 17,523 cycles

L1 DOOR OUTER HANDLE COMMAND BELLCRANK ROLLER STUCK. PERFORMED L1 DOOR VENT FLAP ADJUSTMENT IAW AMM 52-11-25/500. PERFORMED DOOR BOX MECHANISM INSPECTION IAW AMM 52-11-22/600. OPS CHECK GOOD.

Part: CONNECTOR — CONTAMINATED (SKEW SENSOR) · airframe 27,372 hrs · 16,805 cycles

FLAP FAIL MESSAGE IN FLIGHT. DECLARED EMERGENCY, DIVERTED, LANDED WITHOUT INCIDENT. FOUND RT T3 SKEW SENSOR CONNECTOR FULL OF FOD AND DIRTY. CLEANED CONNECTOR AS REQUIRED AND RECONNECTED TO SKEW SENSOR. OPS CHECK OF FLAPS/SLATS GOOD AT THIS TIME THROUGH MULTIPLE CYCLES IAW AMM 27-50-00.

Part: LIGHT — MISSING (SEAT 7B) · airframe 27,060 hrs · 16,601 cycles

EMERGENCY LIGHT 7B MISSING. SECURED THE LIGHT IAW AMM 33-50-21.

Part: LIGHT — WORN (CABIN) · airframe 25,973 hrs · 15,948 cycles

F/A'S REPORT THAT EMERGENCY LIGHT STRIPS ARE WORN. R & R IAW AMM 33-50-21.

Part: INDICATOR — OUT OF POSITION (R2 DOOR SLIDE) · airframe 24,902 hrs · 15,317 cycles

R2 DOOR SLIDE INDICATOR NOT VISIBLE. PERFORMED OPS CHECK OF R2 DOOR SLIDE ENGAGE/DISENGAGE INDICATION, IAW AMM 52-12-00. OPS CHECKED GOOD.

Part: CONTROL UNIT — OUT OF RIG (TE FLAPS) · airframe 23,688 hrs · 14,602 cycles

FLAP FAIL MESSAGE ON APPROACH, DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. TROUBLESHOT IAW FIM 27-51-00-810-804. PERFORMED FLAP ELECTRONIC RIGGING IAW AMM 27-50-00, MESSAGE CLEARED, OPS CHECK GOOD.

Part: SEAL DEPRESSOR — DAMAGED (FWD CARGO DOOR) · airframe 23,629 hrs · 14,597 cycles

FWD CARGO DOOR LOWER SEAL DEPRESSOR BENT AND NICKED IN SEVERAL SPOTS. REWORKED FWD CARGO DOOR LOWER CENTER SEAL RETAINER. REPAIRED FWD CARGO DOOR LOWER AFT CORNER SEAL RETAINER. INSTALLED REPAIRED SECTION OF RETAINER, MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (ZONE 100) · airframe 23,679 hrs · 14,597 cycles

CORROSION FOUND ON COCKPIT FLOORBEAM AND DOUBLER AT FRAME 11 BEHIND CENTER CONSOLE. R & R GUSSET CONNECTOR.

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 23,679 hrs · 14,597 cycles

CORROSION FOUND ON FWD GALLEY FLOOR FITTINGS. R & R FLOOR FITTINGS OF FWD GALLEY.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 23,679 hrs · 14,597 cycles

CORROSION FOUND ON COCKPIT FLOORBEAM DOUBLER BEHIND COPILOT. R & R LOWER RT CORNER OF DOUBLER.

Part: FLOOR SUPPORT — CORRODED (FRAME 86) · airframe 23,679 hrs · 14,597 cycles

CORROSION FOUND ON RT FLOOR SUPPORT ON FRAME 86 BROKEN. R & R FLOOR SUPPORT.

Part: SILL — CORRODED (ZONE 100) · corrosion level 2 · airframe 23,679 hrs · 14,597 cycles

CORROSION FOUND ON LOWER DOOR SILL AROUND NUT PLATES AFT CARGO. R & R NEW DOOR SILL.

Part: SEAT TRACK — CORRODED (FRAMES 89-90) · airframe 23,679 hrs · 14,597 cycles

CORROSION ON RT AFT SEAT TRACK AT FRAMES 89-90. R & R RT AFT FWD SEAT TRACK.

Part: GUSSET — CORRODED (FRAME 90) · airframe 23,679 hrs · 14,597 cycles

CORROSION FOUND ON RT AFT GUSSET AT FRAME 90. R & R GUSSET.

Part: GUSSET — CORRODED (FRAME 90) · airframe 23,679 hrs · 14,597 cycles

CORROSION FOUND LT AFT GUSSET AT FRAME 90. R & R GUSSET. 17060257001

Part: SPLICE — CORRODED (FRAME 89) · corrosion level 2 · airframe 23,679 hrs · 14,597 cycles

CORROSION FOUND ON LT AFT SPLICE AT FRAME 89. R & R LT AFT SPLICE PLATE, PN

Part: FLOOR SUPPORT — CORRODED (FRAMES 88-90) · airframe 23,679 hrs · 14,597 cycles

CORROSION FOUND ON RT FLOOR SUPPORT AT FRAMES 88-90. R & R RT FLOOR SUPPORT.

Part: SEAT TRACK — CORRODED (FRAME 16) · corrosion level 2 · airframe 23,679 hrs · 14,597 cycles

CORROSION FOUND ON LT FF SEAT TRACK AT FRAME 16. R & R SEAT TRACK, PN

Part: SHEAR PLATE — CORRODED (ZONE 100) · corrosion level 2 · airframe 23,679 hrs · 14,597 cycles

CORROSION ON RT OTBD SHEAR PLATE AT FRAMES 12-14. R & R RT SILL, PN

Part: SEAT TRACK — CORRODED (FRAMES 85-86) · corrosion level 2 · airframe 23,679 hrs · 14,597 cycles

CORROSION FOUND ON LT AFT SEAT TRACK AT FRAMES 85-86. R & R SEAT TRACK.

Part: SHEAR PLATE — CORRODED (ZONE 100) · airframe 23,679 hrs · 14,597 cycles

CORROSION ON LT OTBD SHEAR PLATE AT FRAMES 12-16. R & R LT SILL.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 23,679 hrs · 14,597 cycles

CORROSION ON RT AFT FLOOR SUPPORT AT FRAMES 85-86. R & R RT AFT FLOOR SUPPORT.

Part: SEAT TRACK — CORRODED (FRAME 13) · airframe 23,679 hrs · 14,597 cycles

CORROSION ON RT FWD SEAT TRACK AT FRAME 13. R & R SEAT TRACK.

Part: MOUNT — CORRODED (ZONE 100) · corrosion level 2 · airframe 23,679 hrs · 14,597 cycles

CORROSION FOUND ON OTBD RT WINDSCREEN MOUNT FRAME 84. R & R MOUNT.

Part: STRUCTURE — DIRTY (R2 DOOR) · airframe 21,214 hrs · 13,117 cycles

R2 DOOR ARMING HANDLE DIFFICULT TO MOVE UP OR DOWN. REMOVED DEBRIS FROM GIRT BAR RECESS, OPS CHECK GOOD IAW AMM 52-22-01.

Part: TUBE — LEAKING (HYDRAULIC SYS) · airframe 21,165 hrs · 13,093 cycles

HYD 2 LOW QTY IN FLIGHT, OBSERVED SYSTEM 2 QUANTITY THEN FALLING FROM APPROX 24% TO 0% WITHIN 90 SECONDS. RAN QRH FOR HYD 2 LOW PRESSURE. DECLARED EMERGENCY, DIVERTED TO IND. LANDED WITHOUT INCIDENT. FOUND PRESSURE TUBE ASSY ON NR 2 ENGINE LEAKING. REMOVED AND REPLACED PRESSURE PIPE TUBE ASSY IAW GE MM 71-00-00-800-808 AND PERFORMED OPS AND LEAK CHECK IAW AMM 29-10-00, 29-11-00, AND GE MM 72-00-00. ALL OPS AND LEAKS CHECKS GOOD.

Part: GIRT BAR — MALFUNCTIONED (R2 DOOR) · airframe 20,841 hrs · 12,895 cycles

R2 SERVICE DOOR VENT FLAP HANDLE VERY DIFFICULT TO OPERATE ON GROUND. SERVICED R2 DOOR GIRT BAR IAW AMM 52-42-41, OPS CHECK GOOD.

Part: WIRE HARNESS — DEFECTIVE (L2 DOOR) · airframe 20,445 hrs · 12,657 cycles

L2 DOOR INDICATOR IS IMTERMITTENTLY SHOWING OPEN DURING TAXI. LUBRICATED AND ADJUSTED L2 DOOR FRAME TARGET INDICATOR LATCH IAW AMM 52-72-21. REPLACED L2 DOOR SENSOR HARNESS, OPS CHECK GOOD.

Part: GIRT BAR — OUT OF ADJUST (CABIN DOOR) · airframe 20,437 hrs · 12,653 cycles

MAIN CABIN DOOR CLOSES BUT ARM/DISARM HANDLE WILL NOT GO DOWN INTO ARMED POSITION. RE-ADJUSTED GIRT BAR, LUBED CABLE, AND PERFORMED OPS CHECK IAW AMM 52-11-00.

Part: INDICATOR — OUT OF ADJUST (L1 DOOR) · airframe 19,116 hrs · 11,838 cycles

L1 MCD LEFT GREEN LOCK INDICATOR NOT INDICATING GREEN WITH DOOR CLOSED AND ARMED. ADJUSTED L1 DOOR LEFT GREEN VISUAL INDICATOR IAW AMM 52-11-20 AND CMM 52-11-22.

Part: DOOR — LACK OF LUBE (L1) · airframe 18,920 hrs · 11,714 cycles

L1 DOOR HARD TO OPEN HANDLE FROM INSIDE OF A/C. LUBED L1 DOOR, REMOVED DEBRIS, PERFORMED OPS CHECK IAW EMB 170 MM 52-11-00. OPS CHECK GOOD.

Part: SUMP — LEAKING (NR 1 ENGINE) · airframe 18,409 hrs · 11,392 cycles

ENG 1 BLEED EMITS FOUL ODOR DURING CLIMBOUT. SMELL DIMINISHES AFTER ENG 1 BLEED DESELECTED. INSPECTED A/C, FOUND A SUMP LEAKING OIL. A/C FERRIED TO IND. REMOVED AND REPLACED LT ENGINE IAW SENGCHANGE JOBCARD.

Part: WIRE HARNESS — DEFECTIVE (LE SLAT) · airframe 18,002 hrs · 11,149 cycles

CREW DECLARED EMERGENCY ON DESCENT/LANDING DUE TO SLAT FAIL WHEN FLAPS WERE SELECTED TO FLAPS 5. SLATS SHOWED STUCK AT FLAPS 3. MAINTENANCE REPLACED THE LEFT 2/3 SKEW SENSOR. THE MESSAGE RETURNED LATER WITH NO EMERGENCY DECLARED AND MAINTENANCE REPLACED THE SLAT 3/4 HARNESS PER S170EI-27-83-0005 AND OPS CHECKED GOOD.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,911 hrs · 11,087 cycles

LEVEL 2 CORROSION ON TOP SIDE OF BEAM AT FR86 TO FR89. REMOVED AND REPLACED BEAM IAW EMB 170 SRM 51-41-01 AND 51-43-03.

Part: PUMP — CORRODED (RT WING) · airframe 17,911 hrs · 11,087 cycles

MAJOR REPAIR - RT WING FUEL PUMP AND WING MATING SURFACE HAS CORROSION. BLENDED OUT DAMAGED AREA IAW EMB 170 SRM 51-10-03 AND ETD 2011-170-108897. PERFORMED HFEC TO AFFECTED AREAS, NO CRACK LIKE INDICATIONS NOTED.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,911 hrs · 11,087 cycles

MAJOR REPAIR - LEVEL 2 CORROSION SHEAR CLIP AT APPROX FR82 BELLY AREA RIGHT SIDE BELOW CARGO FLOOR SUPPORT LONGERON. REMOVED AND REPLACED SHEAR CLIP IAW EBM 170 SRM 51-41-01, 51-41-02, AND ETD 2011-170-108865.

Part: FITTING — CORRODED (FUSELAGE) · airframe 17,911 hrs · 11,087 cycles

MAJOR REPAIR - SHEAR CLIP CORRODED AT FR83 BETWEEN STGR 27-28R. REMOVED SHEAR CLIPS AT FR83 FROM STGR 26R TO 29R, BLENDED CORROSION ON FRAME, FABRICATED AND INSTALLED NEW SHEAR CLIPS, AND RE-INSTALLED FLOOR SUPPORTS.

Part: FITTING — CORRODED (FUSELAGE) · airframe 17,911 hrs · 11,087 cycles

MAJOR REPAIR - LEVEL 2 CORROSION FR87 AND 88 COMMON TO STRINGER 27R AT SHEAR CLIP UNDER WATER TANK RIGHT SIDE. REMOVED SHEAR CLIPS, FR88 CORROSION LIMITED TO TOP COAT ONLY WITH NO MATERIAL LOSS, FR87 CORROSION BEYOND LIMITS. REMOVED AND REPLACED IAW EMB 170 SRM 51-41-01, 51-41-02, AND 51-23-06.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,911 hrs · 11,087 cycles

LEVEL 2 CORROSION WATER SERVICE PANEL U-DOUBLERS. REMOVED AND REPLACED DOUBLERS IAW EMB 170 SRM 51-40-02, 51-43-02.

Part: SHEAR WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,911 hrs · 11,087 cycles

LEVEL 2 CORROSION AT SEVERAL AREAS ON SHEAR WEB. REMOVED AND REPLACED SHEAR WEB IAW EMB 170 SRM 51-41-02, 51-42-02 AND 51-43-02.

Part: PANEL — CORRODED (FUSELAGE) · airframe 17,911 hrs · 11,087 cycles

MAJOR REPAIR - AFT FUSELAGE PANEL 152AR, WASTE CUTOUT, INNER LIP, LT SIDE, FORWARD, HAS DEEP PITTING CORROSION. REMOVED AND REPLACED DOUBLER WITH NEW PART IAW EMB 170 SRM 51-41-02, 51-43-02.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,911 hrs · 11,087 cycles

LEVEL 2 CORROSION LT FLOORBEAM SHEAR PLATE. REMOVED AND REPLACED LT SHEAR PLATE IAW EMB 170 SRM 51-42-01 AND 51-42-03.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,911 hrs · 11,087 cycles

LEVEL 2 CORROSION AT JUST AFT OF R2 FLOORBEAM BETWEEN FR87 AND FR90. REMOVED CORRODED SILL AFT OF R2 IAW EMB 170 SRM 51-43-03 AND 51-42-01. INSTALLED SERVICEABLE SILL IAW EMB 170 SRM 51-43-03 AND 51-42-01.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,911 hrs · 11,087 cycles

LEVEL 2 CORROSION AT RT FLOORBEAM UNDER CUP HOLES, RT FRAME 88-89. REMOVED AND REPLACED RT BEAM AT FR 86 TO FR 89 IAW EMB 170 SRM 51-43-03 AND 51-41-01.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,911 hrs · 11,087 cycles

LEVEL 2 CORROSION AT LT FLOORBEAM JUST FWD OF FR86 UNDER CLIP HOLES. REMOVED AND REPLACED UNDER SHEET AND INSTALLED IAW EMB 170 SRM 51-41-01 AND 51-43-01.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,911 hrs · 11,087 cycles

LEVEL 2 CORROSION AROUND LAV TO FLOOR FAST HOLES. REMOVED AND REPLACED FLOOR DOUBLER IAW EMB 170 SRM 51-41-02 AND 51-42-02.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,911 hrs · 11,087 cycles

LEVEL 2 CORROSION AT CENTER FLOORBEAM, CENTER SHEAR PLATE. REMOVED AND REPLACED SHEAR PLATE IAW EMB 170 SRM 51-42-03.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,911 hrs · 11,087 cycles

LEVEL 2 CORROSION AT RT SHEAR PLATE FLOORBEAM. REMOVED AND REPLACED RT SHEAR PLATE IAW EMB 170 SRM 51-42-00 AND 51-43-01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,911 hrs · 11,087 cycles

LEVEL 2 CORROSION RT CENTER CFI SEAT TRACK (FR24 1" AFT, 3" AFT FR26, 1" AFT FR28, 2" AFT FR29) GOUGES (1" AFT FR25, 2" AFT FR30, 4" AFT FR31, 2" AFT FR21) AND MISSING/DAMAGED PAINT. INSTALLED SERVICEABLE SEAT TRACK AT CENTER CFI POSITION PER EMB 170 SRM 51-43-03 AND 51-43-04.

Part: EXTENSION — CRACKED (RT WING) · airframe 17,911 hrs · 11,087 cycles

MAJOR REPAIR - RT WING RIB 10 EXTENSION AT SPAR II CRACKED. REMOVED AND REPLACED RT WING RIB 10 EXTENSION AT SPAR II IAW SRM 51-43-01 AND 51-43-02.

Part: DOOR — DIRTY (CABINK) · airframe 17,280 hrs · 10,681 cycles

PASSENGER SERVICE DOOR L1 AND R1 ARE "STICKY" TOUGH TO OPERATE. R1 DOOR CLEANED, GIRT BAR ATTACHMENTS POINTS ON FLOOR OPS CHECK NORMAL IAW EMB 170 MM 52-41-00; L1 DOOR OPS TEST NORMAL IAW EMB 170 MM 52-11-00.

Part: COVER — LOOSE (CABIN DOOR) · airframe 16,446 hrs · 10,195 cycles

MAIN CABIN DOOR MAKES A LOUD POPPING NOISE WHEN OPENED. INSPECTED DOOR AND FOUND HINGE COVER ASSY LOOSE AND BINDING. RE-SECURED DOOR HINGE COVER, OPENS AND CLOSES NORMAL, IAW EMB 170 IPC 25-23-04.

Part: ROLLER — OBSTRUCTED (CABIN DOOR) · airframe 16,173 hrs · 10,025 cycles

MAIN CABIN DOOR CATCHES INTERNALLY WHEN OPENED FROM OUTSIDE. CLEANED AND REMOVED DEBRIS FROM MAIN CABIN DOOR VENT FLAP ROLLERS AND DOOR HANDLE AS NEEDED. OPS CHECK GOOD PER AMM 52-11-00.

Part: POWER SUPPLY — DEFECTIVE (COCKPIT) · airframe 15,148 hrs · 9,366 cycles

CREW DECLARED EMERGENCY UPON LANDING, AVNX MAU 2B FAIL EICAS MESSAGE. LANDED WITHOUT INCIDENT. CYCLED A/C POWER AND MESSAGE CLEARED. MAINTENANCE LATER REPLACED THE MAU 2 POWER SUPPLY NR 1 AND NR 2.

Part: UNKNOWN — MALFUNCTIONED (L1 DOOR) · airframe 13,953 hrs · 8,614 cycles

CREW REPORTED CANNOT ARM L1 DOOR. PERFORMED OPS CHECK ON L1 DOOR SLIDE ARMING, GOOD IAW EMB 170 MM 52-11-00. NO MAINTENANCE REQUIRED.

Part: SKIN — DENTED (FUSELAGE) · airframe 13,197 hrs · 8,180 cycles

MAJOR REPAIR - DENT IN LOWER FUSELAGE SKIN AFT OF FR 19 AND BELOW STR 27R. FABRICATED REPAIR DOUBLERS AND FILLER IAW EMB 170 SRM 53-10-01. INSTALLED REPAIR DOUBLERS AND FILLERS IAW EMB 170 SRM 53-10-01 AND ETD 2010-170/01765 REV A.

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 11,944 hrs · 7,405 cycles

LEVEL 2 CORROSION ON RT SEAT TRACK BEAM AT FR 12 THROUGH FR 17. REPAIRED SEAT TRACK BEAM IAW ETD 2009-170/10421.

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 11,944 hrs · 7,405 cycles

LEVEL 2 CORROSION ON LT SEAT TRACK BEAM AT FRAME LOC 17, 18, 19. REPAIRED AREAS OF LT SEAT TRACK BEAM IAW ETD 2009-170/10421.

Part: SHROUD — CORRODED (ZONE 100) · airframe 11,944 hrs · 7,405 cycles

LAV DUMP SHROUD LEVEL 2 CORROSION AT ATTACH FLANGE. REPLACED SHROUD AND FWD AND AFT FLANGES.

Part: FLOORBEAM — CORRODED (ZONE 100) · airframe 11,944 hrs · 7,405 cycles

LEVEL 2 CORROSION ON FLOOR GUSSETS AFT SIDE OF GALLEY. REMOVED DAMAGED GUSSETS AND FABRICATED NEW GUSSETS, INSTALLED IAW EMB IC 2009-170/00325.

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 11,944 hrs · 7,405 cycles

LEVEL 2 CORROSION ON RT SEAT TRACK BEAM AT FR 12 THROUGH FR 17. REPAIRED PER ETD 2009-170/10421.

Part: FLOORBOARD — CORRODED (CABIN) · airframe 11,944 hrs · 7,405 cycles

LEVEL 2 CORROSION OF FR 14 AT FLOORBOARDS 226ARF AND 226BRF. REPAIRED PER ETD 2009-170/10421.

Part: STEERING SYS — FAILED (NLG) · airframe 10,379 hrs · 6,474 cycles

DURING VISUAL APPROACH, RECEIVED NOSE WHEEL STEERING FAIL MESSAGE UPON "GEAR DOWN AND THREE GREEN". EXECUTED A MISSED APPROACH TO COMPLETE QRH PROCEDURE. EVEN THOUGH AIRCRAFT LOGIC RETURNS THE NOSE WHEEL STEERING TO A "CENTERED" POSITION, ELECTED TO HAVE AIRPORT FIRE RESCUE STANDBY. ON APPROACH, DECIDED TO LAND FLAPS FULL TO DECREASE LANDING SPEED. LOWERED LANDING GEAR AND RECEIVED NWS FAIL MESSAGE. LANDED WITHOUT INCIDENT. MAINTENANCE RESET C/B.

Part: UNKNOWN — ODOR (CABIN) · airframe 6,959 hrs · 4,398 cycles

FLIGHT 7553 DEN TO YEG CREW REPORTS STRONG SMELL OF ELECTRICAL SMOKE AT PUSH TIME. PASSENGERS WERE DEPLANED. MAINTENANCE COULD NOT DUPLICATE SMOKE SMELL. ANOTHER AC CART WAS HOOKED UP TO THE AIRCRAFT AND NO FURTHER DISCREPANCIES WERE NOTED.

Part: BATTERY — DISCHARGED (CABIN) · airframe 5,791 hrs · 3,683 cycles

DURING EMERGENCY LIGHT POWER UNIT FUNCTIONAL TEST THE EXIT LOCATER SIGN AT CENTER FUSELAGE IN AFT GALLEY CENTER CEILING PANEL DID NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE NR 3 EMERGENCY LIGHT POWER UNIT.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 4,699 hrs · 3,028 cycles

MAJOR REPAIR: IMPACT DAMAGE CONSISTING OF DENT AND MULTIPLE GOUGES AT REAR FUSELAGE AT REAR FUSELAGE. DAMAGE REPAIRED IAW IC2007-170/05480.

Part: HEAT EXCHANGER — CRACKED (RT A/C PACK) · airframe 4,114 hrs · 2,675 cycles

FLIGHT 7628 ORD TO HPN, AFTER TAKEOFF CREW EXPERIENCED VIBRATION IN FLIGHT, DECLARED AN EMERGENCY AND RETURNED TO FIELD. MAINT REPORTS RT PACK RAM AIR INLET LOOSE. ACFT FERRIED TO IND. MAINT REPLACED THE RIGHT HAND DUEL HEAT EXCHANGER.

Part: SLAT SYSTEM — FAILED · airframe 3,203 hrs · 2,098 cycles

FLIGHT 7586 ORD TO YUL SLAT FAIL ON APPROACH. DECLARED EMERGENCY AND LANDED SAFELY. MAINTENANCE RESET SF-ACE PER FIM; RAN UP SEVERAL TIMES NO DEFECTS AT THIS TIME AND DATE.

Part: DOOR — UNSECURE (MAIN CABIN DOOR) · airframe 2,886 hrs · 1,884 cycles

FLIGHT 7638 ORD TO IND, DURING TAKEOFF ROLL ABORTED THE TAKEOFF DUE TO A MASTER WARNING MAIN CABIN DOOR OPEN INDICATION. CLEARED RUNWAY AND HAD F/A CHECK AND RESCUER THE MAIN CABIN DOOR. TAXIED BACK TO THE RUNWAY AND TOOK OFF WITHOUT FURTHER COMPLICATIONS. NO PILOT WRITE UP, NO FURTHER DISCREPANCIES AT THIS TIME.