N546JN
Registered owner: ATARES FUNDING LLC, FL (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
DURING HEAVY MAINTENANCE AREA INSIDE THE LH HORIZONTAL STAB HAS (1) SPOT OF POSSIBLE CORROSION ON THE SPAR WEB LOWER MID SECTION @ APPROXIMATELY (XE-217.500) JUST BELOW THE FASTENER ROWS. AFTER FURTHER EVALUATION OF AREA AT INSIDE THE LH HORIZONTAL STABILIZER SPAR WEB LOWER MID-SECTION AT APPROX. XE 217.500, JUST BELOW FASTENER ROW, FOUND NO EVIDENCE OF CORROSION AT THIS TIME IAW MD-11 SRM 51-21-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
DURING HEAVY CHECK, LT WING UPPER FWD SPAR HAS CORROSION APPROX XOR372 ON FWD LEG.
DURING HEAVY MAINTENANCE, RT OUTER WING LOWER REAR SPAR HAS CORROSION AT APPROX XORS-552.
DURING HEAVY MAINTENANCE, RT OUTER WING LOWER REAR SPAR HAS CORROSION AT APPROX XORS-581. AFTER FURTHER EVALUATION BOEING CERTIFIED THE BLENDED LOCATION AS A PERMANENT REPAIR AND BEEN ACCOMPLISHED WITH ALL THE REQUESTED PROVISIONS AT RH OUTER WING LOWER REAR SPAR AT APPROX. XORS-581. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
DURING HEAVY MAINTENANCE RT OUTER WING LOWER REAR SPAR HAS CORROSION AT APPROX XORS-574. AFTER FURTHER EVALUATION BOEING CERTIFIED THE BLENDED LOCATION AS A PERMANENT REPAIR AND BEEN ACCOMPLISHED WITH ALL THE REQUESTED PROVISIONS AT RH OUTER WING LOWER REAR SPAR AT APPROX, XORS-574. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
DURING HEAVY MAINTENANCE, RT OUTER WING LOWER REAR SPAR HAS CORROSION AT APPROX XORS-536.
DURING HEAVY MAINTENANCE RH OUTER WING LOWER REAR SPAR HAS CORROSION @ APPROX (XORS-799). AFTER FURTHER EVALUATION BOEING CERTIFIED THE BLENDED LOCATION AS A PERMANENT REPAIR AND BEEN ACCOMPLISHED WITH ALL THE REQUESTED PROVISIONS AT RH OUTER WING LOWER REAR SPAR AT APPROX. XORS-799. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
DURING HEAVY MAINTENANCE LT OUTER WING UPPER REAR SPAR HAS CORROSION @ APPROX (XORS-702). FTER FURTHER EVALUATION BOEING CERTIFIED THE BLENDED AREA AS A PERMANENT REPAIR AND BEEN COMPLETED WITH ALL THE REQUESTED PROVISIONS AT LH OUTER WING UPPER REAR SPAR AT APPROX AT XORS-702 IAW MD-11 BOEING MESSAGE: WGN-WGN-25-0035-01C-03C. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
DURING HEAVY CHECK RT OUTER WING UPPER REAR SPAR HAS CORROSION AT APPROX XORS-608. AFTER FURTHER EVALUATION BOEING CERTIFIED THE BLENDED LOCATION AS A PERMANENT REPAIR AND BEEN ACCOMPLISHED WITH ALL THE REQUESTED PROVISIONS AT RH OUTER WING UPPER REAR SPAR AT APPROX XORS-608. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
DURING HEAVY MAINTENANCE LH OUTER WING UPPER REAR SPAR HAS CORROSION @ APPROX (XORS-694). AFTER FURTHER EVALUATION BOEING CERTIFIED THE BLENDED AREA AS A PERMANENT REPAIR AND BEEN ACCOMPLISHED WITH ALL THE REQUESTED PROVISIONS AT LH OUTER WING UPPER REAR SPAR AT APPROX XORS-694 IAW MD-11 BOEING MESSAGE: WGN-WGN-25-0035-01C/03C. THE AIRCRAFT WA APPROVED FOR RETURN TO SERVICE.
LEFT OUTER WING UPPER REAR SPAR HAS CORROSION @ APPROX. (XORS-702). AFTER FURTHER EVALUATION, BOEING CERTIFIED THE BLENDED OUT AREA AS A PERMANNET REPAIR AND BEEN COMPLETED WITH ALL THE REQUESTED PROVISIONS AT LH OUTER WING UPPER REAR SPAR AT APPROX AT XORS-702 IAW MD-11, BOEING MESSAGE: WGN-WGN-25-003501C/-03C. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
RIGHT OUTER WING LOWER REAR SPAR HAS CORROSION AT APPROX. XORS-574. AFTER FURTHER EVALUATION BOEING CERTIFIED THE BLENDED LOCATION AS A PERMANENT REPAIR AND BEEN ACCOMPLISHED WITH ALL THE REQUESTED PROVISIONS AT RT OUTER WING LOWER REAR SPAR AT APPROX. XORS-574. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
DURING HEAVY MAINTENANCE CHECK RT OUTER WING LOWER REAR SPAR HAS CORROSION AT APPROX XORS-581. AFTER FURTHER EVALUATION, BOEING CERTIFIED THE BLENDED LOCATION AS A PERMANENT REPAIR & BEEN ACCOMPLISHED WITH ALL THE REQUESTED PROVISIONS, AT RT OUTER WING LOWER REAR SPAR AT APPROX. XORS-581. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
DURING HEAVY MAINTENANCE CHECK RH OUTER WING LOWER REAR SPAR HAS CORROSION @ APPROX. (XORS-597). AFTER FURTHER EVALUATION, BOEING CERTIFIED THE BLENDED LOCATION AS A PERMANENT REPAIR AND BEEN ACCOMPLISHED WITH ALL THE REQUESTED PROVISIONS, AT RH OUTER WING LOWER REAR SPAR AT APPROX. XORS-597. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
DURING HEAVY MAINTENANCE LH OUTER WING UPPER REAR SPAR HAS CORROSION @ APPROX (XORS-694). AFTER FURTHER EVALUATION BOEING CERTIFIED THE BLENDED AREAS AS A PERMANENT REPAIR AND BEEN ACCOMPLISHED WITH ALL THE REQUESTED PROVISIONS AT LH OUTER WING UPPER REAR SPAR AT APPROX XORS-694 IAW MD-11 BOEING MESSAGE: WGN-WGN-25-0035-01C-03C. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
DURING HEAVY CHECK RH OUTER WING LOWER REAR SPAR HAS CORROSION @ APPROX (XORS-536).
DURING HEAVY CHECK RH OUTER WING LOWER REAR SPAR HAS CORROSION @ APPROX (XORS-574).
DURING HEAVY CHECK RH OUTER WING LOWER REAR SPAR HAS CORROSION AT APPROX (XORS-581.
DURING HEAVY MAINTENANCE CHECK RH OUTER WING UPPER REAR SPAR HAS CORROSION @ APPROX. (XORS-608). AFTER FURTHER EVALUATION, BOEING CERTIFIED THE BLENDED LOCATION AS A PERMANENT REPAIR AND BEEN ACCOMPLISHED WITH ALL THE REQUESTED PROVISIONS AT RH OUTER WING UPPER REAR SPAR AT APPROX. XORS-608. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
DURING HEAVY CHECK RH OUTER WING LOWER REAR SPAR HAS CORROSION AT APPROX XORS-601. AFTER FURTHER EVALUATION, BOEING CERTIFIED THE BLENDED LOCATION AS A PERMANENT REPAIR AND BEEN ACCOMPLISHED WITH ALL THE REQUESTED PROVISIONS AT RH OUTER WING LOWER REAR SPAR AT APPROX. XORS-601. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
DURING HEAVY MAINTENANCE CHECK RH OUTER WING LOWER REAR SPAR HAS CORROSION @ APPROX. (XORS-799). AFTER FURTHER EVALUATION, BOEING CERTIFIED THE BLENDED LOCATION AS A PERMANENT REPAIR AND BEEN ACCOMPLISHED WITH ALL THE REQUESTED PROVISIONS, AT RH OUTER WING LOWER REAR SPAR AT APPROX. XORS-799. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE
DURING HEAVY CHECK RT OUTER WING LOWER REAR SPAR HAS CORROSION AT APPROX XORS-601. AFTER FURTHER EVALUATION BOEING CERTIFIED THE BLENDED LOCATION AS A PERMANANET REPAIR AND BEEN ACCOMPLISHED WITH ALL THE REQUESTED PROVISIONS AT RH OUTER WING LOWER REAR SPAR AT APPROX. XORS-601. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
DURING HEAVY MAINTENANCE, RT OUTER WING LOWER REAR SPAR HAS CORROSION AT APPROX XORS-597. AFTER FURTHER EVALUATION BOEING CERTIFIED THE BLENDED LOCATION AS A PERMANENT REPAIR AND BEEN ACCOMPLISHED WITH ALL THE REQUESTED PROVISIONS AT RT OUTER WING LOWER REAR SPAR AT APPROX. XORS-597. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
CENTER WING UPPER PANELCORRODED AT RH APPROX STA 1219, XCW 16.0, S-16. AFTER FURTHER EVALUATION, BOEING CERTIFIED THE BLENDED OUT AREA AS A PERMANENT REPAIR AND BEEN COMPLETED WITH ALL THE REQUESTED PROVISIONS AT CENTER WING UPPER PANEL RH APPROX STA 1219, XCW 16.0, S-16 IAW MD-11, BOEING MESSAGE: WGN-WGN-25-0035-04C. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
DURING HEAVY MAINTNENANCE CENTER UPPER PANEL CORRODED AT RH APPROX STA 1204, XCW 24.5 S-18. AFTER FURTHER EVALUATION BOEING CERTIFIED THE BLENDED OUT AREA AS A PERMANENT REPAIR AND BEEN COMPLETED WITH ALL THE REQUESTED PROVISIONS AT RH APPROX. STA 1204, XCW 24.5, S-18 ON CENTER UPPER PANEL IAW MD-11 BOEING MESSAGE: WGN-WGN-25-0035-04C. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
DURING HEAVY MAINTENANCE CHECK CENTER SECTION UPPER PANEL CORRODED AT RT APPROX. STA. 1219, XCW 16.0 S-16. AFTER FURTHER EVALUATION BOEING CERTIFIED THE BLENDED OUT AREA AS A PERMANENT REPAIR AND BEEN COMPLETED WITH ALL THE REQUESTED PROVISIONS AT CENTER WING UPPER PANEL RH APPROX. STA 1219, XCW 16.0S-16 IAW MESSAGE WGN-25-0035-04C. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
DDURING HEAVY MAINTENANCE CHECK CENTER SECTION UPPER PANEL CORRODED AT RH APPROX STA 1204, XCW 24.5 S-18. AFTER FURTHER EVALUATION BOEING CERTIFIED THE BLENDED OUT AREA AS A PERMANENT REPAIR AND BEEN COMPLETED WITH ALL THE REQUESTED PROVISIONS AT RH APPROX. STA 1204, XCW 24.5 S-18 ON CENTER WING UPPER PANEL IAW MESSAGE: WGN-25-0035-04C. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
CENTER UPPER PANEL CORRODED AT LH APPROX STA 1205, XCW 7.0 S-18. AFTER FURTHER EVALUATION OF BLENDED OUT AREA AT LH APPROX STA 1205, XCW 7.0 AT S-18, BOEING FOUND BLENDED OUT LOCATION ACCEPTABLE AS A PERMANENT REPAIR IAW MD-11, MESSAGE: WGN-WGN-25-0035-4C. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
DURING HEAVY MAINTENANCE CENTER UPPER PANEL CORRODED AT RH APPROX STA 1233, XCW 76.5 AT S-14. AFTER FURTHER EVALUATION OF BLENDED OUT AREA AT RH APPROX STA 1233, XCW 76.5 AT S-14, BOEING FOUND BLENDED OUT LOCATION ACCEPTABLE AS A PERMANENT REPAIR IAW MD-11, MESSAGE: WGN-WGN-25-0035-4C. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
DURING HEAVY MAINTENANCE CHECK CENTER WING UPPER PANEL CORRODED AT RH APPROX STA 1233, XCW 76.5 AT S-14. AFTER FURTHER EVALUATION OF BLENDED OUT AREA AT RH APPROX STA 1233, XCW 76.5 AT S-14, BOEING FOUND BLENDED OUT LOCATION ACCEPTABLE AS A PERMANENT REPAIR IAW MD-11, MESSAGE: WGN-WGN-25-0035-4C. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
DURING HEAVY MAINTENENACE CHECK CENTER WING UPPER PANEL CORRDODED AT LH APPROX STA 1205, XCW 7.0 S-18. AFTER FURTHER EVALUATION OF BLENDED OUT AREA AT LH APPROX STA 1205, XCW 7.0AT S-18, BOEING FOUND BLENDED OUT LOCATION ACCEPTABLE AS A PERMANENT REPAIR IAW MD-11, MESSAGE: WGN-WGN-25-0035-4C. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
CENTER WING UPPER PANEL CORRODED AT RH APPROX STA 1229, XCW 96.0 AT S-15. AFTER FURTHER EVALUATION BOEING CERTIFIED THE BLENDED OUT AREA AS A PERMANENT AND BEEN COMPLETED WITH ALL THE REQUESTED PROVISIONS AT RH CENTER WING UPPER PANEL APPROX STA 1229, XCW 96.0 AT S-15 IAW MD-11, BOEING MESSAGE: WGN-WGN-25-0035-04C. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
DURING HEAVY MAINTENANCE UPPER PANEL CORRODED AT RH APPROX STA 1226, XCW 80.5 AT S-15. AFTER FURTHER EVALUATION, BOEING CERTIFIED THE BLENDED OUT AREA AS A PERMANENT REPAIR AND BEEN COMPLETED WITH ALL THE REQUESTED PROVISIONS AT RH CENTER WING UPPER PANEL APPROX. STA 1226, XCW 80.5 AT S-15 IAW MD-11, BOEING MESSAGE: WGN-WGN-25-0035-04C. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
DURING HEAVY MAINTENANCE CHECK CENTER WING UPPER PANEL CORRODED AT LH APPROX STA 1197, XCW 110 AT S-19. AFTER FURHTER EVALUATION BOEING CERTIFIED THE BLENDED OUT AREA AS A PERMANENT REPAIR AND BEEN COMPLETED WITH ALL THE REQUESTED PROVISIONS AT LH CENTER WING UPPER PANEL APPROX STA 1197, XCW 110 AT S-19 IAW MD-11 BOEING MESSAGE: WGN-WGN-25-0035-04C. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
DURING HEAVY MAINTENANCE CHECK CENTER WING UPPER PANEL CORRODED AT LH APPROX STA 1173, XCW 112 AT S-22. AFTER FURTHER EVALUATION BOEING CERTIFIED THE BLENDED OUT AREA AS A PERMANENT REPAIR AND BEEN COMPLETED WITH ALL THE REQUESTED PROVISIONS AT LH CENTER WING UPPER PANEL APPROX. STA 1173, XCW 112 AT S-22 IAW MD-11, BOEING MESSAGE: WGN-WGN-25-0035-04C. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
DURING HEAVY MAINTENANCE CENTER WING UPPER PANEL CORRODED AT RH AAPROX STA. 1229, XCW 17.5 AT S-15. AFTER FURTHER EVALUATION BOEING CERTIFIED THE BLENDED OUT AREA AS A PERMANENT REPAIR AND BEEN COMPLETED WITH ALL THE REQUESTED PROVISIONS AT R/H CENTER WING UPPER PANEL APPROX. STA 1229, XCW 17.5 AT S-15 IAW MD-11 MESSAGE: WGN-WGN-25-0035-04C. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
DURING HEAVY MAINTENANCE CENTER WING UPPER PANEL CORRODED AT LH APPROX STA 1214, XCW 3.0 AT S-17. AFTER FURTHER EVALUATION OF BLENDED AREA AT LH APPROX STA 1214, XCW 3.0 AT S-17, BOEING FOUND BLENDED OUT LOCATION ACCEPTABLE AS A PERMANENT REPAIR IAW MD-11, MESSAGE: WGN-WGN- 25-0035-4C. THE AIRCRAFT APPROVED FOR RETURN TO SERVICE.
DURING HEAVY MAINTENANCE CHECK CENTER WING UPPER PANEL CORRODED AT LH APPROX STA 1226, XCW 22.5 AT S-15. AFTER FURTHER EVALUATION BOEING CERTIFIED THE BLENDED OUT AREA AS A PERMANENT REPAIR AND BEEN COMPLETED WITH ALL THE REQUESTED PROVISIONS AT LH CENTER WING UPPER PANEL APPROX STA 1326, XCW 22.5 AT S-15 IAW MD-11 BOEING MESSAGE: WGN-WGN-25-0035-04C. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
DURING HEAVY MAINTENANCE CHECK CENTER WING UPPER PANEL CORRODED AT FRONT SPAR BETWEEN CL AND XCW 8.0. AFTER FURTHER EVALUATION BOEING CERTIFIED THE BLENDED OUT AREA AS A PERMANENT REPAIR AND BEEN COMPLETED WITH ALL THE REQUESTED PROVISIONS AT FRONT SPAR BETWEEN CL AND XCW 8.0 IAW MD-11, BOEING MESSAGE: WGN-WGN-25-0035-04C. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
DURING HEAVY MAINTENANCE CENTER UPPER PANEL CORRODED AT RH APPROX STA 1172, XCW 0.5 AT 5-22. AFTER FURTHER EVALUATION OF BLENDED OUT AREA AT RH APPROX STA 1172, XCW 6.5 AT S-22 BOEING FOUND BLENDED OUT LOCATION ACCEPTABLE AS A PERMANENT REPAIR IAW MD-11, MESSAGE: WGN-WGN-25-0035-4C. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
DURING HEAVY MAINTENANCE CENTER UPPER PANEL CORRODED AT RH APPROX STA. 1182, XCW 8.5 AT 5-21. AFTER FURTHER EVALUATION OF BLENDED OUT AREA AT RH APPROX. STA. 1182, XCW 8.5 AT S-21 BOEING FOUND BLENDED OUT LOCATION ACCEPTABLE AS A PERMANENT REPAIR IAW MD-11 MESSAGE: WGN-WGN-25-0035-4C. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
DURING HEAVY MAINTENANCE CENTER WING UPPER PANEL CORRODED AT L/H APPROX STA 1196, XCW 5.0 AT S-19. AFTER FURTHER EVALUATION, BOEING CERTIFIED THE BLENDED OUT AREA AS A PERMANENT REPAIR AND BEEN COMPLETED WITH ALL THE REQUESTED PROVISIONS AT L/H CENTER WING UPPER PANEL APPROX. STA 1196, XCW 5.0 AT S-19 IAW MD-11 BOEING MESSAGE, WGN-WGN-25-0035-04C. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
DURING HEAVY MAINTENANCE CHECK CENTER WING UPPER PANEL CORRODED AT RH APPROX STA. 1205, XCW 4.0 AT S-18. AFTER FURTHER EVALUATION BOEING CERTIFIED THE BLENDED OUT AREA AS A PERMANENT REPAIR AND BEEN COMPLETED WITH ALL THE REQUESTED PROVISIONS AT RH CENTER WING UPPER PANEL APPROX. STA 1205, XCW 4.0. AT S-18 IAW MD-11 BOEING MESSAGE: WGN-WGN-25-0035-04C. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
DURING HEAVY MAINTENANCE CENTER WING UPPER PANEL CORRODED AT LH APPROX STA 1226, XCW 22.5 AT S-15. AFTER FURTHER EVALUATION, BOEING CERTIFIED THE BLENDED OUT AREA AS A PERMANENT REPAIR AND BEEN COMPLETED WITH ALL THE REQUESTED PROVISIONS AT LH CENTER WING UPPER PANEL APPROX STA 1226, XCW 22.5 AT S- 15 IAW MD-11 BOEING MESSAGE: WGN-WGN-25-0035-04C. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
CENTER WING UPPER PANEL CORRODED AT LH APPROX STA 1173, XCW 112 AT S-22. AFTER FURTHER EVALUATION BOEING CERTIFIED THE BLENDED OUT AREA AS A PERMANENT REPAIR AND BEEN COMPLETED WITH ALL THE REQUESTED PROVISIONS AT LH CENTER WING UPPER PANEL APPROX. STA 1173, XCW 112 AT S-22 IAW MD-11 BOEING MESSAGE: WGN-WGN- 25-0035-04C. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
DURING HEAVY MAINTENANCE CENTER UPPER PANEL CORRODED AT LH APPROX STA 1197, XCW 110 AT S-19.
DURING HEAVY MAINTENANCE CENTER WING UPPER PANEL CORRODED AT RH APPROX STA. 1229, XCW 34.5 AT S-15. AFTER FURTHER EVALUATION, BOEING CERTIFIED THE BLENDED OUT AREA AS A PERMANENT REPAIR AND BEEN COMPLETED WITH ALL THE REQUESTED PROVISIONS AT R/H CENTER WING UPPER PANEL APPROX STA 1229, XCW 34.5 AT S-15 IAW MD-11 BOEING MESSAGE: WGN-WGN-25-0035-04C. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
DURING HEAVY MAINTENANCE CHECK CENTER WING UPPER PANEL CORRODED AT LH APPROX STA 1214, XCW 3.0 AT S-17. AFTER FURTHER EVALUATION OF BLENDED OUT AREA AT LH APPROX STA 1214, XCW 3.0 AT S-17, BOEING FOUND BLENDED OUT LOCATION ACCEPTABLE AS A PERMANENT REPAIR IAW MD-11, MESSAGE: WGN-WGN-25-0035-4C.. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
DURING HEAVY CHECK CENTER WING UPPER PANEL CORRODED AT RH APPROX STA. 1226 XCW 80.5 AT S-15. AFTER FURTHER EVALUATION BOING CERTIFIED THE BLENDED OUT AREA AS A PERMANENT REPAIR AND BEEN COMPLETED WITH ALL THE REQUESTED PROVISIONS AT R/H CENTER WING UPPER PANEL APPROX. STA 1226, XCW 80.5AT S-15 IAW MD-11, BOEING MESSAGE: WGN-WGN-35-0035-04C. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
DURING HEAVY MAINTENANCE CHECK CENTER WING UPPER PANEL CORRODED AT RH APPROX STA 1172, XCW 6.5 AT S-22. AFTER FURTHER EVALUATION OF BLENDED OUT AREA AT RH APPROX STA 1172, XCW 6.5 AT S-22, BOEING FOUND BLENDED OUT LOCATION ACCEPTABLE AS A PERMANENT REPAIR IAW MD-11, MESSAGE: WGN-WGN-25-0035-4C. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
DURING HEAVY MAINTENANCE UPPER PANEL CORRODED AT LH APPROX STA 1196, XCW 5.0 AT S-19. AFTER FURTHER EVALUATION, BOEING CERTIFIED THE BLENDED OUT AREA AS A PERMANENT REPAIR AND BEEN COMPLETED WITH ALL THE REQUESTED PROVISIONS AT LH CENTER WING UPPER PANEL APPROX STA 1196, XCW 5.0 AT S-19 IAW MD-11 BOEING MESSAGE: WGN-WGN-25-0035-04C. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
DURING HEAVY MAINTENANCE UPPER PANEL CORRODED AT RH APPROX STA 1205, XCW 4.0 AS S-18. AFTER FURTHER EVALUATION , BOEING CERTIFIED THE BLENDED OUT AREA AS A PERMANENT REPAIR AND BEEN COMPLETED WITH ALL THE REQUESTED PROVISIONS AT RH CENTER WING UPPER PANEL APPROX STA 1205, XCW 4.0 AT S-18 IAW MD-11, BOEING MESSAGE: WGN-WGN-25-0035-04C. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
DURING HEAVY MAINTENANCE UPPER PANEL CORRODED AT RH APPROX STA 1229, XCW 17.5 AT S-15. AFTER FURTHER EVALUATION BOEING CERTIFIED THE BLENDED OUT AREA AS A PERMANENT REPAIR AND BEEN COMPLETED WITH ALL THE REQUESTED PROVISIONS AT RH CENTER WING UPPER PANEL APPROX STA 1229, XCW 17.5 AT S-15 IAW MD-11 BOEING MESSAGE: WGN-WGN-25-0035-04C. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
DURING HEAVY MAINTENANCE UPPER PANEL CORRODED AT RH APPROX STA 1229, XCW 34.5 AT S-15. AFTER FURHTER EVALUATION, BOEING CERTIFIED THE BLENDED OUT AREA AS A PERMANENT REPAIR AND BEEN COMPLETE WITH ALL THE REQUESTED PROVISIONS AT RH CENTER WING UPPER PANEL APPROX. STA 1229, XCW 34.5 AT S-15 IAW MD-11 BOEING MESSAGE: WGN- WGN-25-0035-04C. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
CENTER UPPER PANEL CORRODED AT LH APPROX STA 1197, XCW 110 AT S-19. AFTER FURTHER EVALUATION BOEING CERTIFIED THE BLENDED OUT AREA AS A PERMANENT REPAIR AND BEEN COMPLETED WITH ALL THE REQUESTED PROVISIONS AT LH CENTER WING UPPER PANEL APPROX STA 1197, XCW 110AT S-19 IAW MD-11 BOEING MESSAGE: WGN-WGN-25-0035-04C. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
DURING HEAVY MAINTENANCE CENTER WING UPPER PANEL CORRODED AT FRONT SPAR BETWEEN CL AND XCW 8.0. AFTER FURTHER EVALUATION, BOEING CERTIFIED THE BLENDED UT AREA AS A PERMANENT REPAIR AND BEEN COMPLETED WITH ALL THE REQUESTED PROVISIONS AT FRONT SPAR BETWEEN CL AND XCE 8.0 IAW MD-11, BOEING MESSAGE: WGN-WGN-25-0035-04C. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
DURING HEAVY MAINTENANCE CHECK CENTER WING UPPER PANEL CORRODED AT RH APPROX STA 1172, XCW 6.5 AT S-22. AFTER FURTHER EVALUATION OF BLENDED OUT AREA AT RH APPROX STA 1172, XCW 6.5 AT S-22, BOEING FOUND BLENDED OUT LOCATION ACCEPTABLE AS A PERMANENT REPAIR IAW MD-11, MESSAGE: WGN-WGN-25-0035- 4C. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
DURING HEAVY MAINTENANCE ANGLE BELOW FWD RH PATIO FLOOR HAS A CRACK. FABRICATED AND INSTALLED ANGLE STIFFENER AT PATIO FLOOR BELOW RH FWD IAW MD-11 SRM 51-31-10 AND DRAWING AKC7546. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
DURING HEAVY MAINTENANCE CORROSION FOUND ON L/H O/B ELEVATOR ACTUATOR MOUNT BOLT SURFACE ON INNER REAR SPAR AT STA. XE 198.
DURING HEAVY MAINTENANCE CORROSION FOUND ON LH OB ELEVATOR ACTUATOR MOUNT BOLT SURFACE ON INNER REAR SPAR AT STA. XE 198.
DURING HEAVY MAINTENANCE LH #5 SLAT TRACK OB RIB HAS CORROSION AT STA. XIS 332. REMOVED SURFACE CORROSION FROM INNER DOUBLER AT LH #5 SLAT TRACK OB RIB STA XIS 332. FOUND TO BE WITHIN LIMITS IAW MD-11 SRM 57-00-00-2R -0, FIGURE 206 EXAMPLE A. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
APU DOOR LATCH LOWER HOUSING IS CRACKED.
#1 ENGINE CONTAINMENT RING FWD SIDE HAS CORROSION @ THE 8' O'CLOCK POSITION.
DURING HEAVY MAINTENANCE CHECK HYDRAULIC DRAIN LINE BRACKET ON FWD WALL, BOTTOM, CENTER INSIDE PNL 316AB CORRODED. REMOVED AND REPLACED BRACKET ON HYDRAULIC DRAIN LINE ON FWD WALL BOTTOM CENTER INSIDE PNL316AB IAW SRM 51-31-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
DURING HEAVY CHECK PAX #3 DOOR INTERCOSTAL PN: ACA3820-14 HAS A CRACK. REMOVED AND REPLACED INTERCOSTAL PN: ACA3820-14 ON PAX #3 DOOR AT MIDDLESIDE 2ND FROM TOP IAW MD-11 SRM 51-35-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
PILOTS SLIDING WINDOW AFT SHROUD COVER HAS A CRACK. REINSTALLED PILOTS SLIDING WINDOW AFT SHROUD COVER IAW MD-11, AFT SHROUD COVER REPAIRED IAW MD-11 AMM 20-20--00 AND 20-20-09. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
DURING HEAVY MAINTENANCE PAX #3 DOOR INTERCOSTAL P/N ACA3820-16 HAS A CRACK. REMOVED AND REPLACED INTERCOSTAL PN:ACA3820-16 AT PAX #3 DOOR AT MIDDLE SIDE 3RD FROM TOP IAW MD-11 SRM 51-35-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
PNL BELOW PILOTS SLIDING WINDOW TRACK, CRACKED AT FWD SCREW. REPAIRED PILOTS SLIDING WINDOW TRACK PNL IAW MD-11 SRM 51-43-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
DURING HEAVY CHECK PAX #3 DOOR INTERCOSTAL PN ACA3820-10 HAS A CRACK. REMOVED AND REPLACED INTERCOSTAL PN: ACA 3820-10 ON PAX #3 DOOR AT AFT SIDE 2ND FROM TOP IAW MD-11 SRM 51-35-01 AND SRM 51-33-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
DURING HEAVY CHECK PAX #3 DOOR INTERCOSTAL PN ACA3820 HAS A CRACK. REMOVED AND REPLACED INTERCOSTAL PN: ACA3820-4 ONPAX #3 DOOE AT MIDDLE SIDE FROM TOP IAW MD-11 SRM 51-33-01 AND SRM 51-35-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
L/H O/B AILERON O/B PNL BRACE HAS DENTED BRACE, BROKEN RIVETS, & CRACKED UPPER BRACKET. REMOVED AND REPLACED BRACE, RIVETS AND BRACKET AT LH OB AILERON OB PANEL BRACE IAW MD-11 SRM 51-35-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
COPILOTS SLIDING WINDOW AFT SHROUD COVER HAS A CRACK.
DURING HEAVY MAINTENANCE CHECK COPILOTS SLIDING WINDOW AFT SHROUD COVER HAS A CRACK. ACCOMPLISHED REPAIR AT COPILOTS SLIDING WINDOW AFT SHROUD COVER IAW MD-11 SRM 51-43-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
DURING HEAVY MAINTENANCE CHECK FLEXIBLE HYDRAULIC HOSE BRACKET FOR TRANSFER PUMP ON FWD WALL CORRODED INSIDE PANEL 316AB. REMOVED AND REPLACED BRACKET (CLIP) AT FWD WALL INSIDE PANEL 316AB ON FLEXIBLE HYDRAULIC HOSE FOR TRANSFER PUMP IAW MD-11 SRM 51-35-01 AND DWG AJK7002. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
L/H MLG AFT WIRE HARNESS BRACKET BROKEN. REMOVED AND REPLACED BRACKET AT L/H MLG AFT WIRE HARNESS IAW MD-11 AMM 20-20-00. AIRCRAFT APPROVED FOR RETURN TO SERVICE.
L/H MLG AFT WIRE HARNESS BRACKET BROKEN. REMOVED AND REPLACED BRACKET AT L/H MLG AFT WIRE HARNESS IAW MD-11 AMM 20-20-00. AIRCRAFT APPROVED FOR RETURN TO SERVICE.
DURING HEAVY MAINTENANCE CHECK COPILOTS SLIDING WINDOW AFT SHROUD COVER HAS A CRACK. ACCOMPLISHED REPAIR OF R/H COPILOTS WINDOW SLIDING COVER IAW MD-11 SRM 51-43-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
#2 ENGINE L/E OF CONTAINMENT RING HAS CORROSION AROUND BOTTOM HALF.
DURING HEAVY MAINTENANCE CHECK NR 2 ENGINE L/E OF CONTAINMENT RING HAS CORROSION AROUND BOTTOM HALF. ACCOMPLISHED WITH ENGINE REMOVAL ANF REPLACEMENT IAW MD-11 T/C: MS-71-00-03-00-00-01-WG, SEQ, W/O# 15700 AND AMM 71-00-03-000-801.THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
DURING HEAVY MAINTENANCE CHECK NR 1 ENGINE CONTAINMENT RING FWD SIDE HAS CORROSION @ 8 O'CLOCK POSITION. ACCOMPLISHED WITH ENGINE REMOVAL AND REPLACEMENT IAW MD-11 T/C: MS-71-00-01-00-00-01-WG, SEQ,1,W/O# 15701 AND AMM 71-00-03-000-801. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
#3 INLET HAS PITTING CORROSION BETWEEN 5 & 6 O'CLOCK POS. REMOVED MILD SURFACE CORROSION AND LITE PITTING BY HAND RUBBING ON #3 INLET BETWEEN 5 & 6 O'CLOCK POSITION. FOUND WITHIN LIMITS IAW MD-11 SRM 54-12-02. NO MATERIAL LOSS AT THIS TIME. O. ARILA D0011. AIRCRAFT APPROVED FOR RETURN TO SERVICE.
3# INLET HAS PITTING CORROSION AT 3 O'CLOCK POS. REMOVED MILD SURFACE CORROSION AND LITE PITTING BY HAND RUBBING ON #3 INLET AT 3 O'CLOCK POSITION. FOUND WITHIN LIMITS IAW MD-11 SRM 54-12-02-1A-0, FIGURE 103, DETAIL IV AND SRM 51-21-01. NO MATERIAL LOSS AT THIS TIME. O. AVILA D0011. AIRCRAFT APPROVED FOR RETURN TO SERVICE.
#3 INLET HAS PITTING CORROSION BETWEEN 8 & 9 O'CLOCK POS. REMOVED MILD SURFACE CORROSION AND LITE PITTING BY HAND RUBBING ON #3 INLET BETWEEN 8 AND 9 O'CLOCK POSITION. FOUND WITHIN LIMITS IAW MD-11 SRM 54-12-02-1A-0, FIGURE 103 DETAIL Q AND SRM 51-21-01. NO MATERIAL LOSS AT THIS TIME O. AVILA D0011. AIRCRAFT APPROVED FOR RETURN TO SERVICE.
#3 INLET HAS PITTING CORROSION AT 11 O'CLOCK POS. REMOVED MILD SURFACE CORROSION AND LITE PITTING BY HAND RUBBING ON #3 INLET AT 11 O'CLOCK POSITION. FOUND WITHIN LIMITS IAW MD-11 SRM 54-12-02-1A-0, FIGURE 103 DETAIL IV AND SRM 51-21-01. NO MATERIAL LOSS AT THIS TIME. OARIL D0011. AIRCRAFT APPROVED FOR RETURN TO SERVICE.
DURING HEAVY MAINTENANCE PAC #3 DOOR OUTER UPPER SKIN HAS A HOLE IN IT. ACCOMPLISHED REPAIR ON PAC #3 DOOR OUTER UPPER SKIN IAW MD-11 SRM 52-00-00-20-0, SRM 52-40-01, REPAIR 1, SRM 51-33-01 AND BOEING REPAIR SKETCH: WGN-WGN-25-0020-01C. RECEIVED FINAL APPROVAL FROM BOEING FAA FORM 8100-9. REPAIR SKETCH WGN-WGN-25-0020-07B. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
DURING HEAVY MAINTENANCE PILOTS SLIDING WINDOW FWD SHROUD COVER HAS A CRACK. REPAIRED AND RE-INSTALLED PILOT SLIDING WINDOW FWD SHROUD COVERS IAW MD-11, AMM 20-20-00 AND 20-20-09. (FWD SHROUD COVER REPAIRED). THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
DURING HEAVY MAINTENANCE CHECK HYDRAULIC DRAIN LINE BRACKET ON FWD WALL, BOTTOM, CENTER INSIDE PNL 316AB CORRODED. REMOVED AND REPLACED BRACKET ON HYDRAULIC DRAINN LINE ON FWD WALL BOTTOM CENTER INSIDE PNL 316AB IAW MD-11 SRM 51-31-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
NR# 286 - DURING HEAVY MAINTNENANCE #2 ENGINE L/E OF CONTAINMENT RING HAS CORROSION AROUND BOTTOM HALF. ACCOMPLISHED WITH ENGINE REMOVED AND REPLACEMENT IAW MD-11 T/C: MS-71-00-03-00-00-01-WG, SEQ, W/O#15700 AND AMM 71-00-03-000-801. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
DURING HEAVY MAINTENANCE CHECK PAX NR 3 DOOR OUTER UPPER SKIN HAS A HOLE IN IT. ACOMPLISHED REPAIR ON PAX NR3 DOOR OUTER UPPER SKIN IAW MD-11 SRM 52-00-00-2R-0, SRM 52-40-01. REPAIR 1, SRM 51-33-01 AND BOEING MESSAGE REPAIR SKETCH: WGN-WGN-25-0020-01C. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
PNL 513AT MOUNT FLANGE HAS SURFACE CORROSION.
DURING HEAVY MAINTENACE PNL 513AT MOUNT FLANGE HAS SURFACE CORROSION. REMOVED SURFACE CORROSION BY HAND AT LEFT WING ACCESS PNL 531AT ATTACHING FLANGE IAW MD-11 SRM 51-21-01 PAR. 36 NO MATERIAL LOSS. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
KSHV-DURING INSPECTION OF #2 ENGINE INLET POSSIBLE CORROSION WAS FOUND UNDER ACOUSTIC PANEL. MAINTENANCE REMOVED AND REPLACED CORRODED #2 ENGINE INLET T-BRACKET WITH A NEW FABRICATED ONE IAW MD-11 DRAWING AJC8118. AIRCRAFT IS GOOD FOR CONTINUED SERVICE.
AFTER 1 HOUR IN CRUISE, FUEL QUANTITY FAULT LEVEL 2 ALERT. NO FUEL INDICATION FOR TANK 2 TANKS.
INITIAL CLIMB OUT, SIMULTANEOUS FAILURE 3 SYSTEMS - RADAR ALTIMETER "ERRONEOUS AUDIO ALTITUDE", AUTO PILOT 1 & 2 FAIL - AUTO THROTTLE.
ON INITIAL CLIMB OUT, SIMULTANEOUS FAILURE 3 SYSTEMS - RADAR ALTIMETER (ERRONEOUS), AUTO PILOT 1 & 2 FAIL, AUTO THROTTLE.
FLIGHT DIRECTOR 1 FAIL, NAV WON'T ENGAGE, WON'T COME OUT OF TAKEOFF THRUST GCP MODE FMS MODE NOT ENGAGING, NO PERFORMANCE DATA CLIMB
DURING CRUISE, OBSERVED HYDRAULIC SYSTEM 1 REDUCTION IN QUANTITY .1 GALLON IN 6 MINUTES AND INCREASED TO .1 GALLON IN 4 MINUTES. RETURNED TO DEPARTURE. REMOVED AND REPLACED THE HYDRAULIC SYSTEM 1 QUANTITY TRANSMITTER IAW AMM 29-32-02. HYDRAULIC INDICATION SYSTEM CHECKED SATISFACTORY.
IN FLIGHT, THE HYDRAULIC SYSTEM 1 LEAKING 1 GALLON IN 2 MINUTES. LEVEL ONE HYDRAULIC SYSTEM OFF DISPLAYED BELOW 2.5 GALLONS REMAINING. RETURNED TO DEPARTURE. FOUND THE HYDRAULIC OUTBOARD SUPPLY LINE LOOSE IN THE NR 1 PYLON. TORQUED IAW AMM 20-50-01. OPS & LEAK CHECKED NORMAL, NO LEAKS NOTED.
BODY STATION 1741, LBL 50 - 68, WL 79 MAIN DECK FLOOR SUPPORT HAS CORROSION.
FLOOR PANEL UNDER RT OBSERVERS SEAT IS CRACKED.
FORWARD LOWER CARGO DOOR, FWD LOWER CUT OUT FRAME IS CORRODED AT FS 879.
RIGHT WING UPPER SURFACE HAS SURFACE CORROSION AT ABOUT OXRS 230 ALONG THE FWD SPAR.
LEFT WING UPPER SURFACE AT ABOUT XW152, 57" AFT OF THE FRONT SPAR HAS SURFACE CORROSION.
LEFT WING LOWER SURFACE HAS LIGHT SURFACE CORROSION ON WING TIP AT DRAIN HOLE.
RIGHT MAIN WW DOOR, RETRACTION LINK ATTACH BRACKET IS CORRODED.
RIGHT WING LOWER SKIN HAS CORROSION AT XORS 1093.629, ABOUT 16" AFT OF THE FWD SPAR.
FORWARD LOWER CARGO DOOR, FWD LOWER CUT OUT FRAME, CORRODED AT FUSELAGE STATION 879.
LEFT WING LOWER SKIN IS CORRODED AT THE REAR SPAR AREA AT XORS 1093.629.
STATION 1365 TO 1380, LONGERON 28R EXTERNAL LONGERON HAS CORROSION.
NUMBER 3 AC BAY ACCESS DOOR EXTERNAL SKIN AT TOP EDGE, 11 1/2" TO 16" AFT OF LE IS CRACKED.
RIGHT WING UPPER SURFACE HAS CORROSION AT ABOUT XORS 750, 41" FROM THE REAR SPAR.
RIGHT WING UPPER SURFACE HAS CORROSION AT ABOUT XORS 433, 33" FWD OF THE REAR SPAR.
BODY STATION 1371 TO 1386, LONGERON 28L EXTERNAL STRINGER UPPER LEG HAS CORROSION.
CENTER WING TANK UPPER SKIN EXTERNAL SURFACE IS CORRODED AT XCW 17 AT STRINGER 16R & 17R.
CENTER WING TANK UPPER SKIN EXTERNAL SURFACE IS CORRODED AT XCW 13 AT STRINGER 17R.
CENTER WING TANK UPPER SKIN EXTERNAL SURFACE IS CORRODED AT XCW 30 AT STRINGER 15R.
CENTER WING TANK UPPER SKIN EXTERNAL SURFACE IS CORRODED AT XCW 0 AT STRINGER 15.
CENTER WING TANK UPPER SKIN EXTERNAL SURFACE IS CORRODED AT XCW 103 AT STRINGER 17R.
CENTER WING TANK UPPER SKIN EXTERNAL SURFACE IS CORRODED AT XCW 112 AT STRINGER 16R.
CENTER WING TANK UPPER SKIN EXTERNAL SURFACE IS CORRODED AT XCW 106 AT STRINGER 16R.
CENTER WING TANK, UPPER SKIN EXTERNAL SURFACE IS CORRODED AT XCW 83 AT RBL 106 BETWEEN STRINGERS 17 & 18.
RIGHT WING TIP LOWER SURFACE HAS CORROSION OTBD OF ACCESS PANELS 628FW & 628HW.
MAIN DECK STATION 1179, LONGERON 23R HAS CORROSION UNDER SIDE OF LONGERON RT SIDE.
CENTER WING TANK UPPER SKIN EXTERNAL SURFACE IS CORRODED AT XCW 110 AT STRINGER 11L.
CENTER WING TANK UPPER SKIN EXTERNAL SURFACE IS CORRODED AT XCW 110 AT STRINGER 12L.
CENTER WING TANK UPPER SKIN EXTERNAL SURFACE IS CORRODED AT XCW 108 AT STRINGER 13L.
CENTER WING TANK UPPER SKIN EXTERNAL SURFACE IS CORRODED AT XCW 17 AT STRINGER 17R & 18R.
STATION 1521, PRESS BULKHEAD FWD SIDE IN WW WL 78, BL 0 T ANGLE HAS CORROSION.
RIGHT WING LOWER SURFACE HAS CORROSION AROUND VENT HOLE AT ABOUT XORS 826, ABOUT 22" AFT OF THE FRONT SPAR.
RIGHT TORQUE BOX UNDER WING BARREL HAS EVIDENCE OF CORROSION INSIDE KEEL BEAM ACCESS HOLE, ON VERTICAL STIFFENER AT APPROX STATION 1383, RBL 37.
LEFT WING TE SPAR CAP AT APPROX STATION XORS 680 HAS CORROSION.
STATION 1531 5-0, LONGERON 12L SPLICE STRAP IS CRACKED BETWEEN FASTENERS.
STATION 1531 5-123, LONGERON 2L SPLICE STRAP IS CRACKED BETWEEN FASTENERS.
MAIN DECK SEAT TRACK AT RBL 80 IS CRACKED BETWEEN STATION 755 & 775.
LEFT WING LOWER SKIN IS CORRODED AT OXRS 530 AT VENT HOLE.
NUMBER 2 PYLON RT THRUST LINK LUG IS CRACKED.
RIGHT WING REAR SPAR LOWER CHORD IS CORRODED AT XORS 738.
IN THE CTR WING TANK STRINGER 52 IS CRACKED FROM XCW 47 OTBD LT TO XCW 53.
RIGHT WING UPPER SURFACE HAS CORROSION AT XORS 231 AT STRINGER 15, 37" AFT OF THE FRONT SPAR.
RIGHT WING UPPER SURFACE HAS CORROSION AT XORS 231 AT THE FRONT SPAR.
MAIN DECK SEAT TRACK, AS VIEWED FROM THE FWD BILGE, IS CRACKED AT STATION 635, LBL 10.
MAIN DECK SEAT TRACK, AS VIEWED FROM THE FWD BILGE, IS CRACKED AT STATION 635, LBL 50.
MAIN DECK SEAT TRACK, AS VIEWED FROM THE FWD BILGE, IS CRACKED AT STATION 635 AT RBL 10.
MAIN DECK SEAT TRACK, AS VIEWED FROM THE FWD BILGE, IS CRACKED AT STATION 635 AT LBL 30.