N792AX

Part: STRUCTURE — CORRODED (RT WING) · corrosion level 2 · airframe 61,007 hrs · 47,364 cycles

PER CUSTOMER REQUEST CANN RT WING UPPER BEAM PN 113T1623-126 FOR USE ON ACFT. REMOVED RT WING UPPER BEAM PN 113T1623-126 IAW CUSTOMER REQUEST INSTALL T ANGLE IAW SRM 51-40-02. FABRICATED NEW SHIMS IAW DWG 113T1623, TREATED SHIMS IAW AMM 51-21-04. INSTALLED NEW UPPER CORD IAW SRM 51-40-02. REINSTALLED ACCESS PANELS IAW AMM 06-44-00 & AMM 20-11-00. CORRODED, PN 113T1623-126, SN NA, PART NAME CHORD, EXACT FS & BS LOCATION ON ACFT FROM WS 281, EXACT STR & WS LOC ON ACFT FROM TE AFT OF REAR SPAR. ACFT WAS GNDED.

Part: STIFFENER — CORRODED (RT WING) · corrosion level 2 · airframe 61,007 hrs · 47,364 cycles

DURING REPLACEMENT OF RT WING UPPER BEAM ON NR 0983 FOUND ANGLE STIFFENER CORRODED. FABRICATED PART IAW DWG 113T1623 & SAMPLE PO 0052750 PN BAC 1503-100442-7075-T6511 ANGLE BARE ALUM EXTRUDED. CORRODED, PN 113T1623-18, SN NA, PART NAME STIFFENER, STR & WS LOC ON ACFT WS 281. ACFT WAS GNDED.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 61,007 hrs · 47,364 cycles

FOUND CORROSION ON RT WING TE SPAR WHILE WORKING NR 0983. CORROSION WAS REMOVED & AREAS WERE REPAIRED ON THE RT WING UPPER TE SURFACE AT WS 248 & 273 IAW REA B657-61093MR. M-287 WERE COMPLIED WITH ON NR 1074 & 1076. CORRODED L2, PN 112T3101-6, SN N/A, PART NAME WING SKIN, STR & WS LOC ON ACFT WS 248 TO 273, RT WING UPPER TE SURFACE. ACFT WAS GNDED.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 61,007 hrs · 47,364 cycles

CORROSION FOUND RT WING TE STATION 273. CORROSION WAS REMOVED & AREA WAS REPAIRED ON REA B657-61093MR STEPS 21 - 25. CORRODED L2, PN 112T3101-6, SN NA, PART NAME WING SKIN, FS & BS LOC ON ACFT WS 273, RT WING TE SKIN LOWER SURFACE. ACFT WAS GNDED.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 61,007 hrs · 47,364 cycles

CORROSION FOUND RT WING LE SPAR AT STATION 247. CORROSION WAS REMOVED & AREA WAS REPAIRED ON REA B657-61093 MR. SEE PARTIAL WORK ACCOMPLISHED AND PWS 57 PG 1. CORRODED L2, PN 112T3101-6, SN NA, PART NAME WING SKIN, FS & BS WS 248, RT WING TE LOWER SURFACES. ACFT WAS GNDED.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 61,007 hrs · 47,364 cycles

CORROSION FOUND AT RT WING STATION 288 UNDER TE WING SUPPORT. CORROSION WAS REMOVED & AREA WAS REPAIRED AT RT WING STATION 288 UPPER SURFACE IAW REA B657-61093MR STEPS 26 - 31. CORRODED L2, PN 112T3101-6, SN N/A, PART NAME WING SKIN, FS & BS LOC ON ACFT WS 288, TE LWR SKIN SURFACE. ACFT WAS GNDED.

Part: SPLICE PLATE — CORRODED (RT WING) · corrosion level 2 · airframe 61,007 hrs · 47,364 cycles

RIGHT WING LOWER LE FALSE SPAR CRACKED AT NR 9 SLAT AREA NEAR OTBD AUX TRACK. REMOVED DAMAGED SECTION OF RT WING LE LOWER SPLICE PLATE AT LES 612 - 708. FABRICATED NEW SECTION IAW REA B654-61068, INSTALLED NEW SECTION AT SPLICE PLATE IAW SRM 51-40-02 & REA B654-61068. TREATED & PRIMED IAW SRM 51-20-01. PAINTED AREA IAW MM 51-21-10. CORRODED L2, PN 114T0222-6, PART NAME SPLICE PLATE, SN N/A, STR & WS LOC LES 612 - 708, LE FWD OF SPAR. ACFT WAS GNDED.

Part: STRUT — CORRODED (RT WING) · corrosion level 2 · airframe 61,007 hrs · 47,364 cycles

OUTBOARD AIR LOAD STRUT CORRODED AT NR 10 SLAT INBD AUX TRACK. DRILLED, LOCATED, & INSTALLED NEW RIB SRM 51-40-05 & 51-40-02. CIC AREA IAW SOPM 20-41-05 NR 75 900444. CORRODED L2, PN 114T2216-16AX, SN NSN, PART NAME STRUT, FS & BS LOC ON ACFT OSS 732, RT LE FWD OF SPAR. ACFT WAS GNDED.

Part: STRUT — CORRODED (RT WING) · corrosion level 2 · airframe 61,007 hrs · 47,364 cycles

ALL NUTPLATES RUSTED ON INBD AIR LOAD STRUT NR 10 SLAT INBD AUX TRACK AREA. R & R INBD AIR LOAD STRUT AT NR 10 SLAT INBD AUX TRACK IAW SRM 51-40-02. R & R NUTPLATES WITH RIB. CORRODED, PN 114T2215-16, SN NA, PART NAME STRUT, EXACT FS & BS LOCATION ON ACFT FROM 055 732.840, EXACT STR & WS LOCATION ON ACFT FROM RT WING LE FWD OF SPAR. ACFT WAS GNDED.

Part: STRUT — CORRODED (LT WING) · corrosion level 2 · airframe 61,007 hrs · 47,364 cycles

INBOARD AIR LOAD STRUT CORRODED AT NR 3 SLAT NEAR INBD AUX TRACK. INSTALLED LOWER STRUT PN 114T2215-15 IAW SRM 51-40-02, INSTALLED ADEL CLAMPS IAW SRM 51-40-02 PARA 9 B. CORRODED, PN 114T2215-15, PART NAME STRUT, SN NSN, FS & BS LOC OSS 732.840 TO LW, STR & WS LOC NR 3 SLAT 4E OF SPAR. ACFT WAS GNDED.

Part: WEB — CORRODED (RT WING) · corrosion level 2 · airframe 61,007 hrs · 47,364 cycles

LEADING EDGE WEB CORRODED AT NUMBER 2 SLAT AREA NEAR OTBD AUX TRACK WS 897. FABRICATED NEW PART FROM 7075-T6-050 CLAD ALUMINUM IAW DWG 11452300, PO 0051890. INSTALLED & LOCATED NEW PART IAW SRM 51-40-05 & 51-40-02. CORRODED PN 114T2300-157, PART NAME WEB, SN: N/A, FROM 0SS 884.732, TO: 0SS 909.230, WING LE NR 2 SLAT. ACFT WAS GNDED.

Part: SUPPORT — CORRODED (RT WING) · corrosion level 2 · airframe 61,007 hrs · 47,364 cycles

RIGHT WING INNER HALF OF NR 8 FLAP SUPPORT HAS ONE FASTENER HOLE GIVING CRACK INDICATIONS. REAMED AFFECTED HOLE TO .674 INCHES TRUE & ROUND IAW SRM 51-10-02. HFEC INSP IAW NDTM PART 6, 51-00-16. NO INDICATIONS NOTED THIS HOLE REPAIRED REA BI, B657-61081-MR. CORRODED L2, PN 113T1345-22, SN N/A, PART NAME INBD ASSEMBLY HALF, STR & WS LOC ON ACFT WS 798.2, TE AFT OF SPAR. ACFT WAS GNDED.

Part: SUPPORT — CORRODED (RT WING) · corrosion level 2 · airframe 61,007 hrs · 47,364 cycles

RIGHT WING OUTER HALF OF NR 7 FLAP SUPPORT ALL SIX FASTENER HOLES GIVE CRACK INDICATIONS. REAMED AFFECTED HOLE TO 0673 CLEAN & ROUND IAW RAM 51-10-02 HFEC INSP COMPLETED IAW NDTM PART 6, 51-00-16. NO INDICATIONS AT THIS TIME. HOLE REPAIRED REA NR B657-61081MR. CORRODED L2, PN 113T1345-24, SN N/A, PART NAME OTBD ASSEMBLY HALF, STR & WS LOC ON ACFT WS 616.2, TE AFT OF SPAR. ACFT WAS GNDED.

Part: SUPPORT — CRACKED (RT WING) · corrosion level 2 · airframe 61,007 hrs · 47,364 cycles

RIGHT WING OUTER HALF OF NR 8 FLAP SUPPORT HAS ONE FASTENER HOLE GIVING CRACK INDICATIONS. REAMED AFFECTED HOLE CLEAN & ROUND AT .658 IAW SRM 51-10-02, HFEC INSP COMPLETED IAW NDTM PART 6, 51-00-16. NO INDICATIONS AT THIS TIME. HOLE REPAIRED REA NR 657-61081MR. CORRODED L2, PN 113T1345-25, SN N/A, PART NAME OTBD ASSEMBLY HALF, STR & WS LOC ON ACFT WS 798.2, TE AFT OF SPAR. ACFT WAS GNDED.

Part: SUPPORT ANGLE — CORRODED (RT WING) · corrosion level 2 · airframe 61,007 hrs · 47,364 cycles

RIGHT WING LOWER TE PANEL 661CB HAS AFT Z ANGLE CORRODED, INBD AILERON AREA. R & R RT WING LOWER TE PANEL 661CB SUPPORT Z ANGLE IAW SRM 51-40-02. CORRODED L2, PN 113T1944-44, SN NA, PART NAME PANEL SUPPORT BEAM, STR & WS LOC ON ACFT 534.27 TO 545. ACFT WAS GNDED.

Part: RIB — CORRODED (RT WING) · corrosion level 2 · airframe 61,007 hrs · 47,364 cycles

AIR LOAD STRUT CORRODED AT NR 8 SLAT AREA BY TELESCOPING DUCT. REMOVED CORRODED AIR LOAD RIB & INSTALLED NEW AIR LOAD RIB COMPLYING WITH REA NR B657-61059 IAW SRM 51-40-02 TAI DUCTING & COMPONENTS TO BE INSTALLED ON NR 0989. CORRODED L2 1 INCH PN 114T2202-8, SN NSN, PART NAME AIR LOAD STRUT, FS & BS LOC ON ACFT RT WING, STR & WS LOC ON ACFT OSS 456. ACFT WAS GNDED.

Part: RIB — CORRODED (RT WING) · corrosion level 2 · airframe 61,007 hrs · 47,364 cycles

INBOARD AIR LOAD STRUT CORRODED AT NR 8 SLAT OTBD AUX TRACK AREA. REMOVED AIR LOAD RIB. FABRICATED NEW AIR LOAD RIB IAW REA 657-61051. INSTALLED NEW AIR LOAD RIB AT NR 8 SLAT OTBD AUX TRACK INBD SIDE IAW SRM 51-40-02 PARA 7 D. CORRODED L2, PN 114T2203-16, SN N/A, PART NAME AIR LOAD STRUT, STR & WS LOC ON ACFT WS 476 RT. ACFT WAS GNDED.

Part: BEAM — CORRODED (RT WING) · corrosion level 2 · airframe 61,007 hrs · 47,364 cycles

LEADING EDGE WEB CORRODED NR 10 SLAT AREA INBD OF MAIN TRACK. REMOVED DAMAGED SECTION OF NOSE BEAM & REPAIRED IAW SRM 51-70-11 FIG 1. CORRODED L2 1 INCH, PN 114T2300-190, SN NSN, STR & WS LOC ON ACFT OSS 759 RT WING. ACFT WAS GNDED.

Part: RIB — CORRODED (LT WING) · corrosion level 2 · airframe 61,007 hrs · 47,364 cycles

OUTBOARD AIR LOAD STRUT CORRODED AT NR 1 SLAT INBD AUX TRACK. R & R AIR LOAD RIB AT NR 1 SLOT INBD AUX TRACK OTBD RIB IAW SRM 51-40-02. CORRODED L2, PN 114T2227-15, SN NSN, PART NAME STRUT, STR & WS LOC ON ACFT WS 1020 LT. ACFT WAS GNDED.

Part: RIB — CORRODED (RT WING) · corrosion level 2 · airframe 61,007 hrs · 47,364 cycles

INBOARD AIR LOAD STRUT CORRODED AT NR 10 SLAT OTBD AUX TRACK AREA. INSTALLED NEW RIB IAW SRM 51-40-05 & 51-40-02 CIC AREA JPER SOPM 20-41- 05. CORRODED L2, PN 114T2217-18, SN N/A, PART NAME AIR LOAD RIB STRUT, STR & WS LOC ON ACFT OSS 779 WING LE AT NR 10 SLAT. ACFT WAS GNDED.

Part: SUPPORT ANGLE — CORRODED (RT WING) · corrosion level 2 · airframe 61,007 hrs · 47,364 cycles

RIGHT WING TRAILING PANEL 661PB HAS A CORRODED SUPPORT ANGLE, OTBD OF AUX TANK VENT. R & R RT WING TE LOWER CHORD AT WS 1068 IAW SRM 51-40-02. CORRODED, PN 113T1683-28, PART NAME CHORD LOWER, SN N/A, STR & WS LOC WS 1068 TO TE. ACFT WAS GNDED.

Part: RIB — CORRODED (RT WING) · corrosion level 2 · airframe 61,007 hrs · 47,364 cycles

OUTBOARD AIR LOAD STRUT CORRODED AT NR 8 SLAT INBD AUX TRACK AREA. CLEANED AREA IAW SRM 51-10-00. REMOVED .005 ORIGINAL MATERIAL, AREA IS WITHIN IMITS IAW SRM 57-41-09. TREATED & PRIMED AREA IAW SRM 51-20- 01. PAINTED AREA IAW AMM 51-21-10. CORRODED L2, PN 114T2201, SN N/A, PART NAME AIR LOAD STRUT, STR & WS LOC ON ACFT LES 440. ACFT WAS GNDED.

Part: CHANNEL — CORRODED (RT WING) · corrosion level 2 · airframe 61,007 hrs · 47,364 cycles

LARGE NUTPLATE CHANNEL CORRODED RT WING LE LOWER SPAR AT NR 10 SLAT NEAR OTBD AUX. INSTALLED NEW CHANNEL BAC1493-734-2024-T42, PO 0051497 IAW SRM 51-40- 02. PAINTED IAW MM 51-26-02 & CIC IAW SOPM 20-41-05. CORRODED L2, PN 114T2400-254 BAC 1493-734-2024-T42, PART NAME NUT CHANNEL, SN N/A, STR & WS LOC ON ACFT OSS 775, RT WING LE NR 10 SLAT. ACFT WAS GNDED.

Part: CHANNEL — CORRODED (RT WING) · corrosion level 2 · airframe 61,007 hrs · 47,364 cycles

SMALL NUTPLATE CHANNEL CORRODED AT NR 10 SLAT OTBD AUX TRACK, RT WING LOWER SPAR. INSTALLED NEW CHANNEL PAPER BAC1493-734-2024-T42. PO 0051497 IAW SRM 51-40-02, PAINTED IAW MM 51-21-02 & C I C IAW SOPM 20-41-05. CORRODED L2, PN 114T2400-254, SN N/A, PART NAME NUTPLATE CHANNEL, FS & BS OC ON ACFT OSS 884, RT WING LE NR 10 SLAT. ACFT WAS GNDED.

Part: SPAR — CORRODED (RT WING) · corrosion level 2 · airframe 61,007 hrs · 47,364 cycles

LOWER LE PANEL SPAR CRACKED & CORRODED AT NR 1 SLAT INBD AUX TRACK AREA. REMOVED DAMAGED & CORRODED SECTION OF LOWER LE SPLICE PLATE & INSTALLED NEW SECTION OF SPLICE PLATE IAW REA B657-61054. ACFT WAS GROUNDED.

Part: CHANNEL — CORRODED (RT WING) · corrosion level 2 · airframe 61,007 hrs · 47,364 cycles

LOWER SPAR SMALL NUTPLATE CHANNEL CORRODED AT NR 10 SLAT INBD AUX TRACK. INSTALLED NEW CHANNEL BAC 1493-734-2024-T42, PO 0051497 IAW SRM 51- 40-02. PAINTED IAW MM 51-21-02, CIC IAW SOPM 20-41-05. CORRODED L2, PN 114T2400-152, PART NAME NUTPLATE CHANNEL, SN NA, STR & WS LOC ON ACFT OSS 733, RT WING LE NR 10 SLAT. ACFT WAS GNDED.

Part: BEAM — CORRODED (RT WING) · corrosion level 2 · airframe 61,007 hrs · 47,364 cycles

LEADING EDGE WEB CORRODED AT NR 8 SLAT OTBD AUX TRACK AREA. REMOVED NOSE BEAM WEB & NOSE FORMER AT LES 489 - 481. FABRICATED NEW NOSE BEAM WEB. INSTALLED NEW NOSE WEB BEAM IAW SRM 51-40-02. REINSTALLED NOSE FORMER IAW SRM 51-40-02. TREATED, PRIMED & PANELED AREA IAW AMM 51-21-10. CORRODED L2, PN 114T2300-102, PART NAME NOSE BEAM WEB, SN NA, STR & WS LOC AT LES 488 TO 48. ACFT WAS GNDED.

Part: BEAM — CORRODED (RT WING) · corrosion level 2 · airframe 61,007 hrs · 47,364 cycles

RIGHT WING LE FWD WEB CORRODED NR 11 SLAT AREA INBD WS 844. REMOVED DAMAGED NOSE BEAM WEB FABRICATED NEW & INSTALLED IAW DWG 114T2300 & SAMPLE SRM 51-40-02. 2 INCHES, CORRODED LEVEL 2, PN 114T2300, PART NAME NOSE BEAM, SN NSN, FS & BS LOC RT WING, STR & WS LOC OSS 834 TO 836. ACFT WAS GNDED.

Part: WEB — CORRODED (LT WING) · corrosion level 2 · airframe 61,007 hrs · 47,364 cycles

LEADING EDGE WEB CORRODED AT NR 3 SLAT AREA NEAR OTBD AUX TRACK. FABRICATED IAW DWG 114T2300 & SAMPLE. INSTALLED WEB IAW SRM 51-40-02. CORRODED L2, PN 114T2300-33 & -93, SN NA, PART NAME WEB, WS LOC ON ACFT OFS782, LT WING LE NR 3 SLAT. ACFT WAS GNDED.

Part: BEAM — CORRODED (RT WING) · corrosion level 2 · airframe 61,007 hrs · 47,364 cycles

LEADING EDGE WEB CORRODED AT WS 745 NR 10 SLAT INBD AUX TRACK AREA. REMOVED DAMAGED NOSE BEAM, FABRICATED NEW BEAM FROM 7075-T6 .050 INCHES PO 0048004. INSTALLED NEW BEAM IAW DWG 114T2300-178 & SRM 51-40-02. APPLIED TOP COAT IAW AMM 51-21-02. CORRODED L2, PN 114T2300-178, PART NAME NOSE BEAM, SN NSN, STR & WS LOC RT WING LES 737. ACFT WAS GNDED.

Part: BEAM — CORRODED (RT WING) · corrosion level 2 · airframe 61,007 hrs · 47,364 cycles

CORROSION ON BEAM NEAR OTBD END OF MLG SUPPORT BEAM. REMOVED, FABRICATED BEAM IAW DWG 113T1634 & INSTALLED BEAM NEAR OTBD END OF MLG. CORRODED L2, PN 113T1634-16, SN NA, PART NAME SUPPORT RIB ASSEMBLY, STR & WS LOC ON ACFT WS 368.704. ACFT WAS GNDED.

Part: SKIN — CORRODED (LE SLAT) · corrosion level 2 · airframe 61,007 hrs · 47,364 cycles

NUMBER 10 SLAT LE SKIN IS BULGED AT THE OTBD END. FOUND BULGE IN LOWER LE SLAT SKIN DUE TO CORROSION, REPAIRED NR 10 SLAT IAW ABX B657-61062. CORRODED, PN 114T3160, PART NAME SLAT NOSE SKIN, EXACT FS & BS LOCATION ON ACFT FROM 825.2 TO 825.2. ACFT WAS GNDED.

Part: RETAINER — CORRODED (LT WING) · corrosion level 2 · airframe 61,007 hrs · 47,364 cycles

UNDERNEATH INBD AILERON PCA ACCESS PANEL 661BB, FWD ATTACHMENT RAIL IS CORRODED BETWEEN PCA REACTION LINK ASSEMBLIES. R & R SEAL RETAINER IAW SRM 51-40-02. FABRICATED FROM 7075 T6 032 CLAD AFTER PO 0037486. CORRODED, EXACT FS & BS LOCATION ON ACFT FROM 484 TO 484. ACFT WAS GNDED.

Part: SKIN — CORRODED (LE SLAT) · corrosion level 2 · airframe 61,007 hrs · 47,364 cycles

NUMBER 8 SLAT LOWER LE SKIN IS BULGED AT APPROX OSS 467. FOUND BULGE IN SKIN CORRODED REPAIRED SKIN IAW REA B657-61064. CORRODED L2, PN 114T3160, PART NAME SLAT NOSE SKIN, STR & WS LOC ON ACFT RT WING OSS 460.2. ACFT WAS GNDED.

Part: SKIN — CORRODED (LE SLAT) · corrosion level 2 · airframe 61,007 hrs · 47,364 cycles

NUMBER 2 SLAT LOWER OTBD SKIN CRACKED & BULGING. FOUND BULGE IN LOWER SLAP SKIN DUE TO CORROSION REPAIRED NR 2 SLAT IAW ABX B657-61063. CORRODED, PN 114T3160, PART NAME SLAT NOSE SKIN, EXACT FS & BS LOCATION ON ACFT FROM 975.0 TO 975.0. ACFT WAS GNDED.

Part: SKIN — CORRODED (LE SLAT) · corrosion level 2 · airframe 61,007 hrs · 47,364 cycles

RIGHT TE NR 9 SLAT LOWER LE SKIN IS BULGED AT APPROX OSS 604. FOUND BULGE IN SKIN CORRODED REPAIRED SKIN IAW REA B657-61065. CORRODED L2, PN 114T3160, PART NAME SLAT NOSE SKIN, STR & WS LOC ON ACFT RT WING OSS 590.2. ACFT WAS GNDED.

Part: RIB — CORRODED (LT WING) · corrosion level 2 · airframe 61,007 hrs · 47,364 cycles

INBOARD AIR LOAD STRUT CORRODED AT NR 4 SLAT NEAR OTBD AUX TRACK. INSTALLED & LOCATED NEW PART IAW SRM 51-40-5 & 51-40-2. CORRODED L2, PN 114T2210-19, SN NSN, PART NAME STRUT, STR & WS LOC ON ACFT OSS 628.845, LT WING. ACFT WAS GNDED.

Part: BEAM — CORRODED (RT WING) · corrosion level 2 · airframe 61,007 hrs · 47,364 cycles

LEADING EDGE WEB CORRODED AT NR 9 SLAT INBD AUX TRACK AREA. REMOVED NOSE BEAM WEB, FABRICATED NEW WEB IAW DWG 114T2300 & SRM 57-41-13, INSTALLED NEW NOSE BEAM WEB IAW SRM 51-40-02. RESTORED TOPCOAT IN AREA IAW AMM 51-21-10. CORRODED L2, PN 114T2300-136, PART NAME NOSE BEAM WEB, SN N/A, STR & WS LOC WS 600.10 TO WS 580.10, RT WING. ACFT WAS GNDED.

Part: SUPPORT — CORRODED (LT WING) · corrosion level 2 · airframe 61,007 hrs · 47,364 cycles

NUMBER 4 SLAT OTBD AUX TRACK, FWD SUPPORT, AT THE OTBD ATTACHMENT TO STRUCTURE SUPPORT IS CORRODED AT APPROX LT WING LE STATION 633. LOCATED & INSTALLED NEW STRUT RIB IAW SRM 51-40-5 & 51-40-2. CIE WILL BE ACCOMPLISHED ON PANEL REPORT NR 2, 75 900444. CORRODED L2, PN 114T2211-19, SN NSN, PART NAME STRUT, STR & WS LOC ON ACFT WS 633.045, LW FWD LOWER LE. ACFT WAS GNDED.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 61,007 hrs · 47,364 cycles

CRACKED GUIDE SUPPORT AT FLOORBEAM UPPER CHORD RT SIDE INBD OF PDU STATION 1219. R & R GUIDE SUPPORT UPPER WEB AT FS 1219 IAW DWG 452T2051 & SRM 51-40-02. CRACKED .750 INCHES PN 452T2055-9, SN NSN, PART NAME WEB, EXACT FS BS LOCATION ON ACFT FROM 1219. ACFT WAS GNDED.

Part: RIB — CORRODED (LT WING) · corrosion level 2 · airframe 61,007 hrs · 47,364 cycles

NUMBER 5 SLAT INBD AUX TRACK LOWER RIB AT STATION 436 HAS AN AREA OF CORROSION. R & R AIR LOAD RIB AT NR 5 SLAT INBD AUX TRACK INBD RIB IAW SRM 51- 40-02. CORRODED L2, PN 114T2202-21, SN NSN, PART NAME STRUT, STR & WS LOC ON ACFT LT WING, WS 437.39. ACFT WAS GNDED.

Part: RIB — CORRODED (LT WING) · airframe 61,007 hrs · 47,364 cycles

THE NR 5 OTBD AUX TRACK AREA, THE LOWER INBD RIB AT STATION 476 HAS AN AREA OF CORROSION. R & R AIR LOAD RIB AT NR 5 SLAT OTBD AUX TRACK INBD RIB IAW SRM 51-40-02. CORRODED L2, PN 114T2203-15, SN NSN, PART NAME STRUT, STR & WS LOC ON ACFT LT WING, WS 479.54. ACFT WAS GNDED.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,007 hrs · 47,364 cycles

CORRODED INTERCOSTAL ON EITHER END BETWEEN FLOORBEAM UPPER CHORDS STATION 1329 & 1351 RT AFT BILGE AREA. R & R CORRODED INTERCOSTAL FS 1329 - 1351 AT RT AFT BILGE IAW SRM 51-40-02. CORRODED, PN 1146T5000-120, PART NAME SUPPORT FLOOR, SN NSN, FS & BS LOC 1329 - 1351. ACFT WAS GNDED.

Part: STIFFENER — CRACKED (LT WING) · airframe 61,007 hrs · 47,364 cycles

LEADING EDGE UPPER RIB STIFFENER CRACKED ON AFT END AT WS 550 NR 4 SLAT AREA, INBD. INSTALLED NEW STIFFENER PART 114T2207-5 IAW SRM 51-40-05, & 51-40-02. APPLIED CIC IAW SOPM 20-41-05 NR 75 900444. CRACKED .923, PN 114T2207-5, SN NSN, PART NAME STIFFENER, STR & WS LOC ON ACFT WS 550, LE AIR LOAD RIB STIFFENER LT WING. ACFT WAS GNDED.

Part: STIFFENER — CRACKED (LT WING) · airframe 61,007 hrs · 47,364 cycles

LEADING EDGE UPPER RIB LOWER STIFFENER IS CRACKED ON AFT END AT WS 520 NR 5 SLAT AREA OTBD. INSTALLED NEW CHORD IAW SRM 51-40-2 & 51-40-05. TREATED & PRIMED IAW SRM 51-21-02, DINETROLED IAW SOPM 51-21-02. CRACKED 1.35 INCHES, PN 114T2206-5, SN NA, PART NAME CHORD, STR & WS LOC ON ACFT LT WING WS 520. ACFT WAS GNDED.

Part: SPRING — DISLODGED (COCKPIT SWITCH) · airframe 60,793 hrs · 47,256 cycles

EMERGENCY LIGHT SWITCH GUARD WILL NOT LET THE SWITCH REMAIN IN THE ARMED POSITION. SWITCH GUARD WAS BUMPED OUT OF POSITION BY PERSONNEL ON THE FLIGHT DECK. RE POSITIONED THE LIGHT SWITCH GUARD SPRING SO THAT IT OPERATES NORMALLY.

Part: SEAL — BROKEN (DESCENT DEVICE) · airframe 59,407 hrs · 46,576 cycles

DURING SERVICE CHECK FOUND 2 EMERGENCY DESCENT DEVICE SEAL BROKEN AND ACTIVATED. R & R TWO EMERGENCY DEVICE IAW AMM 25-61-02-2, ACFT WAS GROUNDED.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 58,318 hrs · 46,079 cycles

SCRIBE LINE FOUND AT STATION 363 STRINGER S 17L 2.5 INCHES MEASURED AT .0069 DEEP. FORWARD EDGE WAS .100 FROM LAP JOINT REPAIRED ON REA #B653-60351-MR. NO CRACKS WERE FOUND, FINAL REPAIR PER SRM 53-00-01 REPAIR 12, ACFT WAS GROUNDED.

Part: SPLICE PLATE — CORRODED (LT WING) · airframe 58,313 hrs · 46,077 cycles

LEFT WING LOWER SPLICE PLATE CORRODED REQUIRES REPAIR REF: COI59797-001. REMOVED DAMAGED SECTION OF LOWER SPLICE PLATE & SPLICED IN REPLACEMENT SECTION IAW ABX REA B657-59997, ACFT WAS GROUNDED.

Part: SKIN — CORRODED (RT WING) · airframe 58,313 hrs · 46,077 cycles

RIGHT WING STA 810.0 WING SKIN CORRODED REF: COI 59796-001. REPAIRED RIGHT WING SKIN AT STA 810.0 IAW REA B657-60328-MR, DATED IR/09-04-2012, ACFT WAS GROUNDED.

Part: ATTACH ANGLE — CORRODED (LT WING) · airframe 58,313 hrs · 46,077 cycles

TRAILING EDGE PANEL ATTACH ANGLE AT LEFT WING STATION 1050 CORRODED. FABRICATED NEW ANGLE AND INSTALLED IAW B767 SRM 51-40-02 AND DRAWING 113T1912, ACFT WAS GROUNDED.

Part: SUPPORT CHANNEL — CRACKED (RT PYLON) · airframe 58,313 hrs · 46,077 cycles

RIGHT PYLON, INBOARD SIDE OF HYDRAULIC BAY SUPPORT CHANNEL IS CRACKED ACROSS THE FORWARD END BY THE FORWARD BAY DOOR LATCH PAD CRACK IS APPROX 2.5". REMOVED AND REPLACED P/N 313T1380-245 IAW B767 DWG 313T1380 AND B767 SRM 51-40-02, ACFT WAS GROUNDED.

Part: BUSHING — WORN (TE FLAP) · airframe 58,313 hrs · 46,077 cycles

LEFT WING OUTBOARD FLAP, INBOARD LINKAGE NR 10 JOINT (FLAP SIDE). BOTH BUSHING LOOSE ON INBOARD SIDE OF CARRIAGE. REPLACED 3-10 JOINT IAW B767 AMM CH 27-51-27-4, ACFT WAS GROUNDED.

Part: PIVOT ASSY — GOUGED (HORIZ STAB) · airframe 58,313 hrs · 46,077 cycles

HORIZONTAL STABILIZER TORSION BOX COMPARTMENT BS 1809 RIGHT LOWER PIVOT PIN FITTING IS GOUGED ON THE OUTBOARD VERTICAL LEG. REWORKED AREA AND COMPLIED WITH REA B653-60325-MR ON RIGHT LOWER PIVOT PIN FITTING AT STATION 1809. MATERIAL REMOVAL.004" -.024", ACFT WAS GROUNDED.

Part: PIVOT ASSY — GOUGED (HORIZ STAB) · airframe 58,313 hrs · 46,077 cycles

HORIZONTAL STABILIZER TORSION BOX COMPARTMENT BS 1809 LEFT LOWER PIVOT PIN FITTING IS GOUGED ON THE OUTBOARD VERTICAL LEG. REWORKED AREA REMOVAL .004"-.024" AND COMPLIED WITH REA B653-60325-MR ON LEFT LOWER PIVOT PIN FTG AT STATION 1809, ACFT WAS GROUNDED.

Part: PIVOT ASSY — DAMAGED (HORIZ STAB) · airframe 58,313 hrs · 46,077 cycles

HORIZONTAL STABILIZER TORSION BOX COMPARTMENT BS 1809 LEFT LOWER PIVOT PIN FITTING HAS TOOLING MARKS AROUND A FASTENER ON THE I/B VERTICAL LOG. REWORKED AREA AND COMPLIED WITH REA B653-60325-MR 04 LEFT LOWER PIVOT PIN FITTING AT STATION 1809. MATERIAL REMOVAL: .020" ACFT WAS GROUNDED.

Part: SUPPORT CHANNEL — CRACKED (RT PYLON) · airframe 58,313 hrs · 46,077 cycles

RIGHT PYLON OUTBOARD SIDE OF HYD BAY, SUPPORT CHANNEL END IS CHAFED, SPLIT AT END AND HAS HOLES IN IT BY FORWARD DOOR LATCHING PAD. REMOVED AND REPLACED P/N 313T1380-243 IAW B767 DWG 313T1380 AND B767 SRM 51-40-02, ACFT WAS GROUNDED.

Part: SKIN — DAMAGED (LT WING) · airframe 58,313 hrs · 46,077 cycles

LEFT WING TOP SIDE HAS FASTENERS (2 EA) AT WBL 310 BETWEEN STRINGERS 26 AND 27 HAVE BLENDED AREA CLOSE TO FASTENER HEADS FOR ENGINE BACK FITTINGS. REPAIRED DAMAGED AREA IAW REA B657-60326-MR, ACFT WAS GROUNDED.

Part: BEAM — GOUGED (LT PYLON) · airframe 58,313 hrs · 46,077 cycles

LEFT PYLON INBOARD LOWER HYDRAULIC BAY BEAM GOUGED. REMOVED AND REPLACED NEW INBOARD LOWER HYDRAULIC BAY BEAM IAW B767-200 SRM 51-40-02. NAC STA 295, ACFT WAS GROUNDED.

Part: BRACKET — CRACKED (PYLON) · airframe 58,313 hrs · 46,077 cycles

AT PYLON STA 308 ANGLE BRACKET CRACKED BELOW 437ELX AND 437ERX PNLS I/B AND O/B SIDES, ABOVE EXHAUST NOZZLE. REMOVED CRACKED ANGLE FROM FIRE SEAL AND REPLACED IAW B767 SRM 51-40-02 AND DRAWING 313T1380 SLT-20, ACFT WAS GROUNDED.

Part: SPLICE PLATE — CORRODED (RT WING) · airframe 58,313 hrs · 46,077 cycles

RIGHT WING LOWER ATTACH FLANGE FOR LEADING EDGE JUST O/B OF PYLON UPPER SURFACE POTTING COMPOUND BOWED UP POSSIBLE CORROSION. COMPOUND WAS REMOVED AND NOTICED CORROSION FOUND AND REMOVED, ENGINEERING EVAL AND WORK ACCOMPLISHED ON REA B657-60316-MR. RIGHT WING SPLICE PLATE 415-420, ACFT WAS GROUNDED.

Part: STIFFENER — CRACKED (NLG WW) · airframe 58,313 hrs · 46,077 cycles

NOSE WHEEL WELL VERTICAL STIFFENER CRACKED AT STA 183.00 LBL 6.0. REMOVED AND REPLACED NOSE WHEEL WELL VERTICAL STIFFENER AT STA 183 LBL 6.0 PER BOEING 767 SRM 51-40-02, ACFT WAS GROUNDED.

Part: UNKNOWN — ODOR (CABIN) · airframe 56,260 hrs · 45,263 cycles

SMOKE SMELL NOTICED IN THE SUPERNUMERARY COMPARTMENT AND SMOKE DETECTOR SOUNDED. NO SMOKE NOTED. ALL C/B'S IN PLACE. FIRE DEPARTMENT PERFORMED THERMAL IMAGING NO FAULTS NOTED. BATTERY IN SMOKE ALARM DETECTOR LOW, REMOVED AND REPLACED BATTERY DETECTOR. OPS CHECK NORMAL. NOTE: MECHANIC NOTICED K LOADED WAS RUNNING AT THE MAIN CARGO DOOR.

Part: PBE — UNSECURE (COCKPIT) · airframe 55,367 hrs · 44,924 cycles

COCKPIT PBE IS SOFT. REPLACED PBE PER IPC 25-64-57-01.

Part: SPAR CAP — CORRODED (LE SLAT) · airframe 55,168 hrs · 44,840 cycles

CORROSION ON UPPER CAP OF FRONT SPAR LES 452 JUST INBOARD OF "T" DUCT. CUT OUT CORRODED SECTIONS OF UPPER SPLICE PLATE AND REPAIRED IAW REA B657-593.

Part: SPAR CAP — CORRODED (LE SLAT) · airframe 55,168 hrs · 44,840 cycles

CORROSION ON FRONT SPAR UPPER CAP BEHIND NR 9 SLAT INBOARD AUX TRACK. REPAIRED SPAR IAW REA B657-59317.

Part: FITTING — CORRODED (FUSELAGE) · airframe 55,168 hrs · 44,840 cycles

S39R END FITTING IS CORRODED AT FS 1087. REMOVED END FITTING AT FS 1087 SR39R FOR CORROSION CLEAN UP BEYOND LIMITS. REPLACED END FITTING IAW B767 SRM 51-40-02.

Part: SKIN — CORRODED (LE SLAT) · airframe 55,168 hrs · 44,840 cycles

NR 2 SLAT LEADING EDGE UPPER SURFACE HAS AREA OF CORROSION AROUND FASTENER HAD AT APPROX WS 880. REMOVED AND INSTALLED NR 2 I/B AUX TRACK IAW B767 SRM 57-43-01 AND PANEL IAW B767 SRM 51-40-02. BLENDED CORROSION FOUND TO BE OUT OF LIMITS.

Part: STIFFENER — CRACKED (CENTER WING) · airframe 55,168 hrs · 44,840 cycles

VERTICAL STIFFENER ON CENTER WING FRONT SPAR CRACKED AT FLOOR SUPPORT. REPAIRED DAMAGED VERTICAL STIFFENER IAW B767-200 SRM 57-10-10.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 55,168 hrs · 44,840 cycles

STRINGER 17L HAS 3 INCH CRACK ON LOWER FLANGE AT BS 680. REPAIRED STRINGER IAW B767 SRM 53-00-03.

Part: RIB — CORRODED (LE SLAT) · airframe 55,168 hrs · 44,840 cycles

NR 11 SLAT OUTBOARD AUX TRACK ATTACH FITTING INBOARD RIB HAS CORROSION AROUND NUT PLATE. REMOVED AND REPLACED NR 11 SLAT O/B AUX TRACK I/B RIB ASSY IAW B767 SRM 51-40-02.

Part: RIB — CORRODED (LE SLAT) · airframe 55,168 hrs · 44,840 cycles

NR 12 SLAT INBOARD AUX TRACK OUTBOARD FITTING ATTACH RIB CORRODED AT NUT PLATE AND FITTING SHIM PACK CORRODED. REMOVED AND REPLACED NR 12 SLAT I/B AUX TRACK O/B RIB ASSY IAW B767 SRM 51-40-02.

Part: RIB — CORRODED (LE SLAT) · airframe 55,168 hrs · 44,840 cycles

NR 12 SLAT OUTBOARD AUX TRACK INBOARD FITTING ATTACH RIB CORRODED AT NUT PLATE. REMOVED AND REPLACED DAMAGED RIB ON NR 12 SLAT OB AUX TRACK I/B RIB IAW B767-200 SRM 51-40-02.

Part: RIB — CORRODED (LE SLAT) · airframe 55,168 hrs · 44,840 cycles

NR 12 SLAT INBOARD AUX TRACK OUTBOARD FITTING ATTACH RIB CORRODED AT NUT PLATE. REMOVED AND REPLACED NR 12 SLAT I/B AUX TRACK I/B ATTACH RIB IAW B767 SRM 51-40-02.

Part: RIB — CORRODED (LE SLAT) · airframe 55,168 hrs · 44,840 cycles

NR 11 SLAT INBOARD AUX TRACK ATTACH FITTING INBOARD RIB HAS CORROSION AROUND NUT PLATE. REMOVED AND REPLACED DAMAGED RIB ON NR 11 INBOARD AUX TRACK INBOARD RIB IAW SRM B767-300 51-40-02.

Part: RIB — CORRODED (LE SLAT) · airframe 55,168 hrs · 44,840 cycles

NR 9 SLAT INBOARD AUX TRACK ATTACH FITTING OUTBOARD RIB HAS CORROSION UNDER NUT PLATE AT FORWARD END. REMOVED AND REPLACED NR 9 SLAT I/B AUX TRACK O/B RIB ASSY IAW B767 SRM 51-40-02.

Part: STRUCTURE — CRACKED (NLG WW) · airframe 49,852 hrs · 38,814 cycles

RIGHT NWW CHORD AT STA 287 IS CRACKED AT RBL 25 APPROX 1 INCH IN LENGTH. REQUIRES REPAIR IAW 767 SRM 51-70-12. REPAIRED DAMAGE ON RIGHT NWW CHORD AT STA 287 RBL 25 IAW B767 SRM 51-70-12.

Part: WARNING SYSTEM — MALFUNCTIONED (CARGO DOOR) · airframe 53,034 hrs · 43,877 cycles

DURING INITIAL CLIMB AT ABOUT 2000FT AGL THE MAIN CARGO DOOR INDICATIONS WENT OFF, LIGHT & SIREN. DEFERRED MAIN CARGO DOOR INDICATION IAW B767 CODE 11 MEL 52-71-1-2. RE-INSPECT DI, VERIFY CLOSE/LATCH PLACARD INSTALLED - CLEAR - INSPECTED HOOK AND LATCH SWITCHES ALL SECURE, TESTED MAIN DECK CARGO INDICATION SYST AS PER B767 MM 52-32-00-5 NO FAULTS FOUND.

Part: UNKNOWN — MALFUNCTIONED (TE FLAP) · airframe 52,240 hrs · 43,479 cycles

ON APPROACH FROM FLAPS 28-30 DISAGREE EICAS MESSAGE - GO AROUND SLAT PERFORMED - NON NORMAL PROCEDURE OPERATIONAL SATISFACTORY. LOWERED FLAP AND SLAT INSPECT THE ENTIRE FLAP AND SLAT FOUND EVERYTHING FINE AND NORMAL. NO DAMAGE, DID THE BITE TEST ON FSCU PER AMM 27-51-00-1 FIG 104. NO MESSAGE NO FAULT. OPS CHECK FLAP WORKS GOOD. PUT A/C TO NORMAL CONFIGURATION.

Part: SPRING — OUT OF POSITION (LIGHT SWITCH) · airframe 51,848 hrs · 43,408 cycles

CLOSING SWITCH GUARD ON EMERGENCY LIGHT SWITCH TURNS EMERGENCY LIGHTS OFF. FOUND GUARD SWITCH COVER TOGGLE SPRING OFF OF EMERGENCY LIGHT TOGGLE SWITCH. RE-ATTACHED SPRING & FUNCTION CHECKED GOOD.

Part: CONNECTOR — NOT SEATED (CABIN) · airframe 51,828 hrs · 43,397 cycles

EMERGENCY EXIT LIGHT OVER R1 DOOR WILL NOT TEST. RESEATED ELECTRICAL CONNECTOR 9084. EMERGENCY EXIT LIGHT OPS CK GOOD.

Part: STRINGER — CRACKED (NLG WW) · airframe 51,788 hrs · 43,377 cycles

NOSE WHEELWELL STRINGER STA 287, LBL 25 IS CRACKED. FOUND WITH HFEC.

Part: STRINGER — CRACKED (NLG WW) · airframe 51,788 hrs · 43,377 cycles

NOSE WHEELWELL CHORD STA 287, RBL 25 IS CRACKED. FOUND WITH HFEC.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 48,677 hrs · 42,073 cycles

AFT CARGO COMPARTMENT RIGHT SIDE WALL INTERCOSTAL CRACKED. FABRICATED NEW INTERCOSTAL AND INSTALLED IN ACCORDANCE WITH B767 SRM 51-40-2.

Part: STRUCTURE — MISSING (LT WING) · airframe 45,784 hrs · 41,143 cycles

DURING MAINTENANCE POST FLIGHT INSPECTION, FOUND THE LEFT WING LEADING EDGE OUTBOARD THERMAL ANTI-ICE DUCT SEAL DOOR MISSING. REPLACED ANTI-ICE DUCT SEAL DOOR IAW B767 MM 57-41-58-04. OPS CHECKED NORMAL.

Part: A/C PACK — ODOR (RIGHT) · airframe 44,893 hrs · 40,857 cycles

OIL ODOR COMING FROM RT PACK INFLIGHT DURING DESCENT TURNED OFF RIGHT PACK, ODOR WENT AWAY. PERFORMED AIR COND OIL CONTAMINATION TEST ON SYSTEM IAW AMM 21-00-21-2. NO CONTAMINATION NOTED.