N882RW

Part: WARNING MESSAGE — ILLUMINATED (ZONE 300) · airframe 32,507 hrs · 24,832 cycles

PITCH TRIM INDICATION AMBER. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. PERFORMED RETURN TO SERVICE TEST.

Part: FINGER DOUBLER — CORRODED (ZONE 100) · corrosion level 2 · airframe 31,097 hrs · 23,761 cycles

WHILE IN HEAVY CHECK - FWD CARGO- DOOR CUTOUT LOWER FWD FINGER DOUBLER AREAS OF POSSIBLE CORROSION AS MARKED. REMOVED AND REPLACED FWD CARGO-DOOR CUTOUT LOWER FWD FINGER DOUBLE REF EMB SRM 51-40-08

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 31,097 hrs · 23,761 cycles

WHILE IN HEAVY CHECK - AFT CARGO COMPARTMENT LOWER FUSELAGE SKIN SHEAR CLIP/SUPPORT BAG IS CORRODED AT FR 79 AND STGR 29R. REPLACED SHEAR CLIP AT FR 79 BETWEEN STGR 29R-29L.

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 31,097 hrs · 23,761 cycles

WHILE IN HEAVY CHECK - AFT CARGO COMPARTMENT LOWER FUSELAGE SKIN SHEARCLIP AT FR 77 AND STGR 29L-29R IS CORRODED. REMOVED AND REPLACED SHEARCLIP AT FR 77 AND STGR 29L-29R, REF EMB SRM 51-40-08.

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 31,097 hrs · 23,761 cycles

WHILE IN HEAVY CHECK - AFT CARGO COMPARTMENT LOWER FUSELAGE SKIN SHEAR CLIP/SUPPORT BAG IS CORRODED AT FR 79 AND STGR 29L. REMOVED AND REPLACED AFT CARGO LOWER FUSELAGE SHEAR CLIP/SUPPORT BAG AT FR 79 AND STGR 29L. REF EMB SRM 51-40-08.

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 31,097 hrs · 23,761 cycles

WHILE IN HEAVY CHECK - AFT CABIN BELOW FLOOR FUSELAGE SKIN SHEAR CLIP AT FR 86 STGR 27R-28R IS CORRODED. REMOVED AND REPLACED AFT CABIN BELOW FLOOR FUSELAGE SKIN SHEAR CLIP AT FR 86 STGR 27R--28R REF EMB SRM 51-4-08.

Part: SMOKE DETECTOR — FALSE ACTIVATION (ZONE 900) · airframe 28,336 hrs · 21,574 cycles

LAV SMOKE MASTER WARNING ON DESCENT WITH FORWARD LAV SMOKE ALARM ACTIVATING, NO VISUAL SMOKE. PERFORMED OPS CHECK OF PACK 1, NO ODOR NOTED.

Part: SLIDE — PARTIAL DEPLOY (ZONE 800) · airframe 28,049 hrs · 21,330 cycles

L1 EMERGENCY SLIDE DOOR ACCIDENTALLY PARTIALLY DEPLOYED. R&R L1 DOOR EMERGENCY EVACUATION SLIDE.

Part: SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 27,794 hrs · 21,109 cycles

CENTER FUSELAGE III, LH FLOOR SUPPORT PANEL BETWEEN FR 88-90 FOUND CORRODED BEYOND ALLOWABLE LIMITS. REPLACED IAW SRM 51-42-03

Part: SHEAR PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 27,794 hrs · 21,109 cycles

CENTER FUSELAGE III FLOOR SUPPORT SHEAR PANEL BETWEEN FR 87-88 FOUND CORRODED BEYOND ALLOWABLE LIMITS. REPLACED IAW SRM 51-42-03 & 51-42-04

Part: DOOR — CORRODED (ZONE 100) · corrosion level 2 · airframe 27,794 hrs · 21,109 cycles

CENTER FUSELAGE III, CORROSION FOUND ON WASTE ACCESS DOOR SKIN AND HINGE FOUND DAMAGED. REPLACED IAW AMM 53-03-62/400

Part: SKIN — DAMAGED (FUSELAGE) · airframe 24,444 hrs · 18,507 cycles

MAJOR REPAIR: COMPLIED WITH ETD2018-170-100804 REV A FOR A PERMANENT REPAIR OF ELONGATED HOLE IN SKIN AT FR 13-14 AND STR 17R-18R BEHIND THE FWD SERVICE DOOR PROTECTION PLATE. AIRCRAFT REMAINS IN HEAVY CHECK BNA.

Part: NOT REPORTED — DAMAGED (FUSELAGE) · airframe 24,444 hrs · 18,507 cycles

MAJOR REPAIR: COMPLIED WITH ETD2018-170-100804 REV A FOR REPAIR OF ELONGATED SCREW HOLE AT FR 17-18 AND STR 16R-17R. AIRCRAFT REMAINS IN HEAVY CHECK BNA.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,444 hrs · 18,507 cycles

AFTER REMOVAL OF RT INBD GUSSET AT FRAME 89, CORROSION FOUND ON INTERCOSTAL (P/N 170-65177-003) BETWEEN FRAME 89 AND 90. LOCATED DRILLED AND ALODINED NEW RT INBD GUSSET AT FRAME 89 REF SRM 51-40-02 SRM 51-23-04 INSTALLED RT INBD GUSSET AT FRAME 89 REF SRM 51-40.-08 APPLIED TOPCOAT REF SRM 51-23-06 APPLIED CIC TO INTERCOSTAL AT FR 89-90 REF CPM 51-25-00. AIRCRAFT REMAINS IN HEAVY CHECK BNA.

Part: FLOOR SUPPORT — CORRODED (FRAME 90) · corrosion level 2 · airframe 24,444 hrs · 18,507 cycles

CORROSION- AFT WET AREA- RH PANEL SUPPORT AT FR 90 AS MARKED. REMOVED DAMAGED AFT WET AREA- RH PANEL SUPPORT AT FR 90 REF SRM 51-40-08, DRILLED NEW PART AND APPLIED ALODINE REF SRM 51-40-02 AND 51-23-04. INSTALLED NEW AFT WET AREA- RH PANEL SUPPORT AT FR 90 SRM 51-40-08 APPLIED TOPCOAT PO # 256614 REF SRM 51-23-06 SEE EAMS W/O H6415 SN 343 FOR WORK DETAILS. AIRCRAFT REMAINS IN HEAVY CHECK BNA.

Part: GUSSET — CORRODED (FRAME 90) · corrosion level 2 · airframe 24,444 hrs · 18,507 cycles

CORROSION- AFT WET AREA- RH I/B GUSSET AT FR 90 AS MARKED. LOCATED DRILLED AND ALODINED NEW RH I/B GUSSET AT FR 90 AS REF SRM 51-40-02 SRM 51-23-04 INSTALLED RH I/B GUSSET AT FR 90 AS MARKED REF SRM 51-40-08 APPLIED TOPCOAT PO # 256614 REF SRM 51-23-06 SEE EAMS W/O H6415 SN 321 FOR WORK DETAILS. AIRCRAFT REMAINS IN HEAVY CHECK BNA.

Part: FLOOR SUPPORT — CORRODED (FRAME 86) · corrosion level 2 · airframe 24,444 hrs · 18,507 cycles

CORROSION- AFT WET AREA- RH PANEL SUPPORT BROKEN AT FR 86 AS MARKED. LOCATED DRILLED AND ALODINED NEW RH PANEL SUPPORT AT FR 86 REF SRM 51-40-02 SRM 51-23-04 INSTALLED NEW RH PANEL SUPPORT AT FR 86 REF SRM 51-40-08 APPLIED TOPCOAT PO # 256614 AND CIC REF SRM 51-23-06 CPM 51-25-00 SEE EAMS W/O H6415 SN 328 FOR WORK DETAILS. AIRCRAFT REMAINS IN HEAVY CHECK BNA.

Part: SPLICE — CORRODED (FRAME 89) · corrosion level 2 · airframe 24,444 hrs · 18,507 cycles

CORROSION- AFT WET AREA- RH I/B SPLICE AT FR 89 AS MARKED. LOCATED DRILLED AND ALODINED NEW RH I/B SPLICE AT FR 89 AS MARKED REF SRM 51-40-02 SRM 51-23-04 INSTALLED RH I/B SPLICE AT FR 89 AS MARKED REF SRM 51-40-08 APPLIED TOPCOAT PO # 256614 REF SRM 51-23-06 SEE EAMS W/O H6415 SN 324 FOR WORK DETAILS. AIRCRAFT REMAINS IN HEAVY CHECK BNA.

Part: SHEAR PANEL — CORRODED (FRAMES 87-88) · corrosion level 2 · airframe 24,444 hrs · 18,507 cycles

CORROSION-AFT WET AREA- RH SHEAR PANEL FR 87-88 AS MARKED. DRILLED AND ALODINED AFT WET AREA RH SHEAR PANEL FR 87-88 REF SRM 51-40-02, 51-23-04 INSTALLED NEW AFT WET AREA RH SHEAR PANEL FR 87-88 REF SRM 51-40-08 APPLIED TOPCOAT PO # 256614 REF SRM 51-23-06. SEE EAMS W/O H6415 SN 332 FOR WORK DETAILS. AIRCRAFT REMAINS IN HEAVY CHECK BNA.

Part: STIFFENER — CORRODED (FRAMES 89-90) · corrosion level 2 · airframe 24,444 hrs · 18,507 cycles

CORROSION- AFT WET AREA- RH STIFFENER BETWEEN FR 89 AND FR 90 AS MARKED. LOCATED DRILLED AND ALODINED NEW RH STIFFENER BETWEEN FR 89 AND FR 90 REF EMB SRM 51-40-02 SRM 51-23-04 INSTALLED RH STIFFENER BETWEEN FR 89 AND FR 90 REF EMB SRM 51-40-08 APPLIED TOPCOAT PO # 256614 REF SRM 51-23-06 APPLIED CIC TO RH STIFFENER REF CPM 51-25-00 SEE EAMS W/O H6415 SN 415 FOR WORK DETAILS. AIRCRAFT REMAINS IN HEAVY CHECK BNA.

Part: SUPPORT PLATE — CORRODED (FRAME 84) · corrosion level 2 · airframe 24,444 hrs · 18,507 cycles

CORROSION- AFT WET AREA- RH MONUMENT SUPPORT PLATE AT FR 84. LOCATED DRILLED AND ALODINED NEW RH MONUMENT SUPPORT PLATE AT FR 84 REF SRM 51-40-02 SRM 51-23-04 INSTALLED RH MONUMENT SUPPORT PLATE AT FR 84 REF SRM 51-40-08 APPLIED TOPCOAT PO # 256614 REF SRM 51-23-06 SEE EAMS W/O H6415 SN 347 FOR WORK DETAILS. AIRCRAFT REMAINS IN HEAVY CHECK BNA.

Part: BEAM — CORRODED (FRAMES 85-87) · corrosion level 2 · airframe 24,444 hrs · 18,507 cycles

MAJOR REPAIR: WHILE PERFORMING 170EO-53-15-0003 R2 DOOR LOWER BEAM REWORK, CORROSION FOUND ON TOP FLANGE AT FWD AND AFT GIRT BAR FITTINGS. REMOVED DAMAGED R2 DOOR LOWER BEAM AND DRILLED NEW LOWER BEAM REF SRM 51-40-08 APPLIED ALODINE ON NEW PART REF SRM 51-23-04 INSTALLED NEW R2 DOOR LOWER BEAM REF SRM 51-40-08 APPLIED TOPCOAT PO # 256614 REF SRM 51-23-06 APPLIED CPC TO BEAM REF CPM 51-25-00 SEE EAMS W/O H6415 SN 261 FOR WORK DETAILS. AIRCRAFT REMAINS IN HEAVY CHECK BNA.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 24,444 hrs · 18,507 cycles

MAJOR REPAIR: REPAIRED 2 EACH GOUGES ON EXTERNAL SKIN BETWEEN FR 13 AND 14 AND STR 16L AND 18L BY CUTTING OUT DAMAGE AND INSTALLING DOUBLER, TRIPLER AND FILLER. REF SRM 53-10-01 REPAIR 12P AND 51-75-17 RE-CURRENT INSPECTION PER SRM 53-10-01 REPAIR 12 TABLE 201. AIRCRAFT REMAINS IN HEAVY CHECK BNA.

Part: PIN — DAMAGED (ANTI ICE SYS) · airframe 23,079 hrs · 17,570 cycles

WING ANTI-ICE LEAK AFTER TAKEOFF. DECLARED EMERGENCY, RETURNED TO FIELD, LANDED WITHOUT INCIDENT. R&R CERAMIC PINS AT J104R, P1044, P1053, J1054.