N786TW

Part: ACCESS PANEL — CORRODED (ZONE 500) · corrosion level 2 · airframe 39,966 hrs · 38,789 cycles

LT WING L/E SECTION , LOWER ACCESS PANEL NR 1144C UPPER SUFACE CORRODED. THE DAMAGE REQUIRED REPAIR APPROVAL.

Part: SKIN PANEL — DAMAGED (FUSELAGE) · airframe 39,966 hrs · 38,789 cycles

LOWER FUSELAGE AT STA 114.5 BETWEEN LONGERONS 27L AND 28L SKIN WITH LIGHTNING STRIKE. THE SKIN PANEL IS GOING TO BE REPAIRED AS PER SRM REQUIREMENTS.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 39,966 hrs · 38,789 cycles

DURING THE INSPECTION COOPESA FOUND THE LOWER FUSELAGE AT STA 138.5 BETWEEN LONG 27 LT AND 28 LT SKIN WITH LIGHTNING STRIKE. PERMANENT REPAIR WILL BE PERFORMED AS PER DER APPROVAL.

Part: SKIN — BULGED (FUSELAGE) · airframe 39,966 hrs · 38,789 cycles

DURING THE INSPECTION COOPESA FOUND THE LOWER EXTERNAL FUSELAGE FROM STA 1201 TO 1207 AT LONG 30 BULGED SKIN. PERMANENT REPAIR WILL BE PERFORMED AS PER DER APPROVAL.

Part: FRAME — CRACKED (FUSELAGE) · airframe 39,966 hrs · 38,789 cycles

DURING THE INSPECTION COOPESA FOUND THE AFT ACCESSORY COMPARTMENT CANTED STA 1463, -X8.5 OUTBOARD CHORD CRACKED. PERMANENT REPAIR WILL BE PERFORMED AS PER DER APPROVAL.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 39,966 hrs · 38,789 cycles

DURING THE INSPECTION COOPESA FOUND THE LOWER FUSELAGE AT STA 169 BETWEEN LONG 28 LT AND LONG 29 LT SKIN WITH LIGHTNING STRIKE. PERMANENT REPAIR WILL BE PERFORMED AS PER DER APPROVAL.

Part: SKIN — DENTED (FUSELAGE) · airframe 39,966 hrs · 38,789 cycles

LOWER EXTERNAL FUSELAGE AT STA Y120.5 BETWEEN LONGERONS 18L AND 19L SKIN WITH DENT. DAMAGED SKIN WAS REPAIRED IAW LOCAL FAA DER INSTRUCTIONS AND APPROVAL.

Part: FRAME — CRACKED (FUSELAGE) · airframe 39,966 hrs · 38,789 cycles

LOWER FUSELAGE AFT ACCESSORY COMPARTMENT AT CANT STA 1485 RT SIDE STAIR ACTUATOR SUPPORT FRAME WITH CRACK. THE DAMAGED PART WAS REPAIRED AS PER MD-80 SRM 53-03 FIGURE 43 VIEW C.

Part: SKIN — DENTED (FUSELAGE) · airframe 39,966 hrs · 38,789 cycles

LOWER EXTERNAL FUSELAGE AT STA 536.25 BETWEEN LONGERONS 24L AND 25L SKIN WITH DENT. DAMAGED SKIN WAS REPAIRED PER MD-80 DWG SG0953002 VIEW C1 SHEET 1 AND 4.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,966 hrs · 38,789 cycles

LOWER FUSELAGE AFT CARGO COMPARTMENT STA 1219 BETWEEN LONGERONS 29R AND 29L FRAME WITH CORROSION. DAMAGED FRAME WAS REPAIRED PER MD-80 SRM 53-03 FIGURE 3.

Part: SKIN — DENTED (FUSELAGE) · airframe 39,966 hrs · 38,789 cycles

LOWER EXTERNAL FUSELAGE AT STA 536.25 BETWEEN LONGERONS 24L AND 25L SKIN WITH DENT. DAMAGED SKIN WAS REPAIRED PER MD-80 DWG SG0953002 VIEW C1 SHEET 1 AND 4.

Part: DOUBLER — CRACKED (LT WING) · airframe 39,966 hrs · 38,789 cycles

LT WING UPPER SKIN REAR SPAR MAIN LANDING GEAR SUPPORT FITTING DOUBLER WITH CRACK. REPAIRED MAIN LANDING GEAR SUPPORT UPPER DOUBLER IN ACCORDANCE WITH MD-80 SRM 57-03 FIGURE 34.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,966 hrs · 38,789 cycles

UPPER FUSELAGE PAX CABIN, FLOORBEAM UPPER CHORD LOWER SURFACE WITH CORROSION AT Y STA 1322 AND +X23. DAMAGED AREA WAS REPAIRED PER MD-80 SRM 53-05 FIGURE 79A.

Part: SKIN — SCRATCHED (FUSELAGE) · airframe 39,966 hrs · 38,789 cycles

LOWER EXTERNAL FUSELAGE SKIN AT STA 1304 BETWEEN LONGERONS 18R AND 19R WITH SCRATCH. DAMAGED SKIN WAS REPAIRED PER BOEING DWG SG09530001 VIEW D1 SHEETS 1 AND 3.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,966 hrs · 38,789 cycles

LOWER FUSELAGE AFT CARGO COMPARTMENT FORMER (SHEAR TIE) WITH CORROSION AT STA Y 1193 BETWEEN LONGERON 29L AND LONGERON 29R. DAMAGED PART WAS REPAIRED PER MD-80 SRM 53-03 FIGURE 3.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,966 hrs · 38,789 cycles

UPPER FUSELAGE PAX CABIN AT STA 218, -X55 SEAT TRACK WITH CORROSION. DAMAGED SEAT TRACK WAS REPAIRED IN ACCORDANCE WITH MD-80 SRM 53-05 FIGURE 4F VIEW E.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 39,966 hrs · 38,789 cycles

LOWER FUSELAGE SKIN DAMAGED LOCATED AT STA Y429, BETWEEN LONG 28R AND LONG 29R. PERMANENT REPAIR APPROVED BY LOCAL DER.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 39,966 hrs · 38,789 cycles

LOWER FUSELAGE SKIN DAMAGED LOCATED AT STA Y429, BETWEEN LONG 28R AND LONG 29R. PERMANENT REPAIR APPROVED BY LOCAL DER.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,966 hrs · 38,789 cycles

AFT CARGO COMPT STA 1211 WITH CLIP DAMAGED, BETWEEN LONG 26L AND LONG 29R.

Part: SKIN — DENTED (FUSELAGE) · airframe 40 hrs · 39 cycles

(EE4Y) DURING STRUCTURAL INSP, REPORTED AT UPPER EXTERNAL FUSELAGE BETWEEN STA 55 AND STA 62 AT +Z15 RT SIDE SKIN WITH DENT.

Part: SKIN — DENTED (FUSELAGE) · airframe 39,966 hrs · 38,789 cycles

LOWER EXTERNAL FUSELAGE SKIN DENTED AT STA Y363.5 BETWEEN LONG 28R AND LONG 29R. PERMANENT REPAIR APPROVED BY LOCAL DER.

Part: SKIN — DENTED (ZONE 100) · airframe 39,966 hrs · 38,789 cycles

(EE4Y) LOWER EXTERNAL FUSELAGE AT STA 1288 BETWEEN LONGERONS 25L AND 26L SKIN WITH DENT. PERMANENT REPAIR WAS PERFORMED ON THE FUSELAGE SKIN IAW SG09530002 VIEW H1, SHEETS 1 AND 10.

Part: SKIN — CORRODED (FUSELAGE) · airframe 40 hrs · 39 cycles

DURING STRUCTURAL INSPECTION COOPESA REPORTED AT LOWER FUSELAGE FWD CARGO COMPARMENT LT FWD LAVATORY SERVICE PANEL INTERNAL SKIN WITH CORROSION.

Part: SKIN — DENTED (FUSELAGE) · airframe 40 hrs · 39 cycles

(EE4Y) DURING STRUCTURAL INSP, REPORTED AT LOWER EXTERNAL FUSELAGE AT STA 38-Z 2.5 RT SIDE SKIN WITH DENT.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 39,966 hrs · 38,789 cycles

EMPENNAGE VERTICAL STABILIZER DORSAL FIN JOINT ANGLE RT SIDE AT CANT STATION WITH CRACK. THE PART WAS REPAIRED FOLLOWING MD-80 SRM 53-05 FIGURE 23 REV 106.

Part: LONGERON — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,966 hrs · 38,789 cycles

AFT CARGO COMPT STA Y1203 LONGERON 30 DAMAGED.

Part: SKIN — DELAMINATED (DOOR) · airframe 39,966 hrs · 38,789 cycles

LT WING T/E BUTTE DOOR DELAMINATED.

Part: FRAME — CRACKED (ZONE 200) · airframe 39,965 hrs · 38,789 cycles

(EE4Y) REAR FUSELAGE, FRAME CANTED STA 1463 -X8.5 OTBD CHORD (CAP) WITH CRACK. NOTE: THE CAP CRACK REQUIRES A MAJOR REPAIR.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 39,965 hrs · 38,789 cycles

RT WING, FRONT SPAR AREA STA XFS 129 , L/E LOWER PLATING WITH CORROSION. NOTE: THE CORROSION REQUIRES A MAJOR REPAIR.

Part: SUPPORT FITTING — CORRODED (ZONE 200) · airframe 40 hrs · 39 cycles

(EE4Y) DURING STRUCTURAL INSP, REPORTED AT UPPER FUSELAGE PAX CABIN FWD RT DOOR CUTOUT SLIDE SUPPORT FITTING WITH CORROSION

Part: SKIN — DAMAGED (ZONE 200) · airframe 40 hrs · 39 cycles

DURING STRUCTURAL INSP, REPORTED AT UPPER EXTERNAL FUSELAGE AT STA 214 BETWEEN LONGERONS 17L AND 18L SKIN WITH BLEND OUT.

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 39,966 hrs · 38,789 cycles

(EE4Y) EXTERNAL FUSELAGE SKIN AT AFT TOILET SERVICE PANEL CUTOUT YSTA 1311, BETWEEN LONG 21L AND 22L, SKIN CORRODED.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 39,966 hrs · 38,789 cycles

(EE4Y) LOWER FUSELAGE, AFT CARGO COMPARTMENT AT STA 1117, BETWEEN LONG 28L AND LONG 29L, FLOOR SUPPORT CORRODED.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 39,966 hrs · 38,789 cycles

(EE4Y) LOWER FUSELAGE, AFT CARGO COMPARTMENT, ST YSTA 1152, BETWEEN LONG 30 AND 28R, FLOOR SUPPORT CORRODED.