N793AX

Part: ANGLE — CRACKED (RT WING) · airframe 54,690 hrs · 43,629 cycles

FRONT SPAR TO LE ANGLE, ABOVE & AFT OF SLAT PDU CRACKED AT LOWER END. REMOVED & INSTALLED SERVICEABLE LOWER FRONT SPAR TO LE ANGLE ABOVE & AFT OF SLAT PDU IAW SRM 51-40-02 PARA 7, NO LEAKS NOTED. CRACKED 2 INCHES, PN 14T1342U105, PART NAME ANGLE, WING LE, SN 299780, FS & BS 780 - 786, STRINGER & WS, WS 187 - 195. ACFT WAS GNDED.

Part: STRUCTURE — CORRODED (RT WING) · corrosion level 2 · airframe 54,690 hrs · 43,269 cycles

SMALL AREA OF CORROSION ON UPPER TE PANEL ATTACH CHORD ON INBD END AS SEEN THRU PANEL 552AB OPENING. R & R ATTACH CHORD SECTION IAW SRM 57-51-02. CORRODED L2, PN 113T1406-5, SN N/A, PART NAME CHORD, WS LOCATION ON ACFT WS 280 - 298, ACFT WAS GNDED.

Part: SUPPORT BEAM — CORRODED (RT WING) · corrosion level 2 · airframe 54,690 hrs · 43,269 cycles

RIGHT WING UPPER TE PANEL SUPPORT BEAM AT WS 349 - 325 HAS A HOLE CORRODED THRU AT A NUTPLATE. R & R RT WING TE PANEL SUPPORT BEAM AT WS 349 - 325 IAW SRM 51-40-02 PARA 7 D. CORRODED L2, PN 113T1632-70AX, SN N/A, PART NAME SUPPORT, STR & WS LOCATION ON ACFT WS 349 - 325. ACFT WAS GNDED.

Part: SUPPORT — CORRODED (RT WING) · corrosion level 2 · airframe 54,690 hrs · 43,269 cycles

REAR SPAR TO TE UPPER PANEL, ATTACH CHORD AT WS 360, CORRODED AROUND NUTPLATES AT AFT END. R & R REAR SPAR TO TE UPPER PANEL ATTACH CHORD AT WS 360 IAW DWG 113T1626 & REA B657-61627. CORRODED L2, PN 113T1626-44, SN NONE, PART NAME CHORD, UPPER SUPPORT, STRINGER & WS LOCATION ON ACFT WS 349.7 TO WS 360. ACFT WAS GNDED.

Part: SUPPORT BEAM — CORRODED (RT WING) · corrosion level 2 · airframe 54,690 hrs · 43,269 cycles

RIGHT WING, TE UPPER CHORD OF THE INBD SPOILER SUPPORT BEAM IS CORRODED AT WS 365 - 370. INSTALLED NEW CHORD PART 113T1406-6 IAW REA B657-61649MR & SRM 51-40-02. CORRODED L2, PN 113T1406-6, SN N/A, PART NAME CHORD, FS & BS LOCATION ON ACFT RT WING TO TE, STR & WS LOCATION ON ACFT WS 365 TO WS 370. ACFT WAS GNDED.

Part: STRUCTURE — CORRODED (RT WING) · corrosion level 2 · airframe 54,690 hrs · 43,629 cycles

WING TE LOWER PANEL ATTACH CHORD, 32 INCHES FROM REAR SPAR & 25 INCHES FROM OTBD SIDE OF INBD FLAP, OTBD HINGE PARALLEL TO REAR SPAR SPLIT ON EDGE. R & R PANEL ATTACH CHORD FOR PANEL 652JB IAW SRM 51-40-02 & REA B657-61646-MR. CORRODED LEVEL 2, PN 113T1407-2, PART NAME CHORD, EXACT STRINGER & WS LOCATION ON ACFT 431 - 461. ACFT WAS GNDED.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 54,690 hrs · 43,269 cycles

UPPER LONGERON WEB HAS A 2 INCH CRACK AT FS 1800 - 1806. INSTALLED NEW WEB & BRACKETS IAW SRM 51-40-02. SDR INFO, CRACK 2 INCHES, PART NUMBER 148T9120-11, PART NAME LONGERON WEB, SN NA, EXACT FS & BS LOCATION ON ACFT 1800 TO 1806. ACFT WAS GNDED.

Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 54,690 hrs · 43,269 cycles

ALL THREE HYD LINE CLAMP BLOCKS CORRODED AT BRACKET ATTACH POINT AS SEEN THRU PANEL 552AB OPENING. REMOVED, FABRICATED & REPLACED THREE HYD LINE CLAMP BOCKS INSIDE PANEL 552AB OPENING IAW DWG 113T1101 & SRM 51-40-02. CORRODED L2, PN 65B80254-304, SN N/A, PART NAME CHANNEL, STRINGER & WS LOCATION ON ACFT 285 TO 290. ACFT WAS GNDED.

Part: SUPPORT RIB — CORRODED (RT WING) · corrosion level 2 · airframe 54,690 hrs · 43,269 cycles

WING REAR SPAR TO TE PANEL ATTACH BEAM FWD OF HINGED ACCESS PANEL 651YBX, SPLIT ON EDGE. REMOVED PANEL 651YBX. R & R PANEL ATTACH BEAM IAW SRM 51-40-02 PARA 7D & REA B657-61642. RE-INSTALLED PANEL 651YBX IAW SRM 51-40-02 PARA 7D. CORRODED LEVEL 2, PN 113T1634-22, PART NAME SUPPORT RIB, EXACT FS LOCATION WS 388. ACFT WAS GNDED.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 54,690 hrs · 43,269 cycles

LEFT 1809 OUTER CHORD SHOWS A CRACK INDICATION, AT 3 EACH FASTENERS IN AREA 3, ON THE AFT SIDE OF CHORD. REPLACE LT 1809-5 CHORD SECTION, PN 015T1059-3 IAW REA B653-61651-MR. SDR INFO CRACKED 1/8", NO CRACK HOLES WERE ELONGATED. PN 015T1059-3, SN NA, PART NAME CHORD 809 LT, FS & BS LOCATION ON ACFT FS 1809.5. ACFT WAS GNDED.

Part: PANEL SUPPORT — CORRODED (RT WING) · corrosion level 2 · airframe 54,690 hrs · 43,269 cycles

LOWER TE PANEL, ATTACH CHORD AT WS 827, CORRODED AROUND NUTPLATE. R & R LT WING TE PANEL SUPPORT CHORD IAW SRM 51-40-02, EA B657-61631. CORRODED L2, PN 113T1672-5, SN NSN, PART NAME PANEL SUPPORT, STRINGER & WS LOCATION ON ACFT WS 827. ACFT WAS GNDED.

Part: PANEL SUPPORT — CORRODED (RT WING) · corrosion level 2 · airframe 54,690 hrs · 43,629 cycles

REAR SPAR TO TE LOWER PANEL ATTACH CHORD SPLIT ON EDGE, AT WS 1054, AT AUX TANK VENT. R & R RT WING TE LOWER PANEL ATTACH CHORD WING STATION 1054 IAW 51-40-02 & REA B657-61635. CORRODED L2, PN 113T1676-22, SN NA, PART NAME PANEL SUPPORT, STRINGER & WS LOCATION ON ACFT WS 1054. ACFT WAS GNDED.

Part: PANEL SUPPORT — CORRODED (RT WING) · corrosion level 2 · airframe 54,690 hrs · 43,629 cycles

REAR SPAR TO WING TE LOWER PANEL ATTACH CHORD SPLIT ON EDGE, AT WS 930. R & R RT WING TE LOWER PANEL ATTACH CHORD AT WS 930 IAW SRM 51-40-02 & REA B657-61634. CORRODED L2, PN 113T1683-28, SN N/A, PART NAME PANEL SUPPORT, STRINGER & WS LOCATION ON ACFT WS 930. ACFT WAS GNDED.

Part: PANEL SUPPORT — CORRODED (RT WING) · corrosion level 2 · airframe 54,690 hrs · 43,269 cycles

LOWER WING TE PANEL ATTACH CHORD AT WS 1054, SPLIT ON EDGE INBD OF AUX TANK VENT. R & R LT WING TE PANEL SUPPORT CHORD WS 1054 IAW SRM 51-40-02 & REA B657-61637. CORRODED L2, PN 113T1676-19, SN NSN, PART NAME PANEL SUPPORT CHORD, STRINGER & WS LOCATION ON ACFT. ACFT WS 1054. ACFT WAS GNDED.

Part: PANEL SUPPORT — CORRODED (RT WING) · corrosion level 2 · airframe 54,690 hrs · 43,629 cycles

REAR SPAR TO TE LOWER PANEL ATTACH CHORD SPLIT ON EDGE, AT WS 944. R & R RT WING TE LOWER PANEL ATTACH CHORD, AT WS 9644 IAW SRM 51-40-02 & REA B657-61636. CORRODED L2, PN 113T1675-22, SN N/A, PART NAME PANEL SUPPORT, STRINGER & WS LOCATION ON ACFT WS 944. ACFT WAS GNDED.

Part: BEAM — CORRODED (RT WING) · corrosion level 2 · airframe 54,690 hrs · 43,269 cycles

REAR SPAR TO TE PANEL, ATTACH BEAM UPPER CHORD EXFOLIATED AROUND OTBD NUTPLATES AT STATION 288, INBD OF GEAR TRUNNION. REMOVED PANELS FOR ACCESS, REMOVED CORRODED UPPER CHORD. INSTALLED NEW UPPER CHORD, PN 113T1623-125, RE-INSTALLED, REMOVED PANELS, PANELS TO BE PAINTED ON NR 0494 IAW SRM 51-40-02. CORRODED L2, PN 113T1623-125, SN N/A, PART NAME CHORD, STRINGER & WS LOCATION ON ACFT, WS 281.65. ACFT WAS GNDED.

Part: STRUCTURE — CORRODED (RT WING) · corrosion level 2 · airframe 54,690 hrs · 43,629 cycles

UPPER CHORD SPLIT ON EDGE & CORRODED AROUND NUTPLATES ON REAR SPAR TO TE BEAM, AT WS 285, 14 INCHES FROM REAR SPAR M, INBD OF GEAR TRUNNION. REMOVED RT WING UPPER TE PANELS. R & R TE UPPER CHORD AT WW 285.14 IAW SRM 51-40-02 PARA 4.6 & 7D. INSTALLED PANEL AT RT WING UPPER TE IAW SRM 51-40-02. CORRODED L2, PN 113T1623-126, SN N/A, PART NAME CHORD, FS & BS LOCATION ON ACFT WW 281.61. ACFT WAS GNDED.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 54,690 hrs · 43,269 cycles

LOWER ANGLE AT KEEL TO STATION 999 BULKHEAD CORRODED. REMOVED PANEL 149AL FOR ACCESS. REMOVED LOWER ANGLE, FOUND OUT OF LIMITS. REPLACED LOWER ANGLE IAW DWG 145T8610, INSTALLED LOWER ANGLE IAW SRM 51-40-02. INSTALLED PANEL 149 AL IAW SRM 51-40-02. CORRODED L2, PN 145T8610Y37, SN NSN, PART NAME LOWER ANGLE, FS & BS LOCATION ON ACFT 999 TO 1009, STRINGER LOCATION ON ACFT S39L. ACFT WAS GNDED.

Part: STIFFENER — CORRODED (LT WING) · corrosion level 2 · airframe 54,690 hrs · 43,269 cycles

LEFT WING TE PANEL SUPPORT AT WS 280 HAS A CORRODED T STIFFENER, 31" AFT OF THE WING SKIN TE, PN 113T1623-19. REMOVED CORRODED STIFFENER, FABRICATED NEW FROM & 10136-2001 PO 0020699, TAG 1386185 IAW DWG 113T1623. INSTALLED NEW STIFFENER IAW SRM 51-40-02. SDR INFO, PART NUMBER 113T1623-19, PART NAME STIFFENER, SN NSN, CORRODED LEVEL 2, EXACT FS & BS LOCATION ACFT, 31" AFT OF TE SKIN, EXACT STRINGER & WS LOCATION ON ACFT WS TO 280. ACFT WAS GNDED.

Part: STRUT — CORRODED (RT WING) · corrosion level 2 · airframe 54,690 hrs · 43,629 cycles

NUMBER 2 SLAT OTBD AUX TRACK ATTACH FITTING, LOWER OTDB STRUT CORRODED AROUND NUTPLATE AT FWD END. R & R STRUT IAW DWG 114T2224 & SRM 51-40-02 STEP 7. CORRODED L2, PN 114T2224-15, PART NAME STRUT, STRINGER LOCATION WS 937 4 EDGE. ACFT WAS GNDED.

Part: SUPPORT FITTING — CORRODED (LT WING) · corrosion level 2 · airframe 54,690 hrs · 43,269 cycles

LEFT WING NR 1 FLAP SUPPORT, RIB NR 4 HOLE SHOWS CRACK INDICATION WITH EDDY CURRENT. REAMED HOLE TO FINAL SIZE OF .7495 .7505 ON FLAP SUPPORT NR 1, HOLE NR 4 IAW REA B657-61641-MR. SDR INFO CORRODED L2, PN 113T1345-43, SN NONE, PART NAME NR 1 FLAP SUPPORT FITTING, STRINGER & WS LOCATION ON ACFT WS 797. ACFT WAS GNDED.

Part: SUPPORT FITTING — CORRODED (LT WING) · corrosion level 2 · airframe 54,690 hrs · 43,269 cycles

LEFT WING NR 1 FLAP SUPPORT, RIB NR 3 HOLE SHOWS CRACK INDICATION WITH EDDY CURRENT. REAMED HOLE TO FINAL SIZE OF .7495 .7505 ON FLAP SUPPORT NR 1, HOLE NR 3 IAW REA B657-61641-MR. SDR INFO CORRODED L2, PN 113T1345-43, SN NONE, PART NAME NR 1 FLAP SUPPORT FITTING, STRINGER & WS LOCATION ON ACFT WS 797. ACFT WAS GNDED.

Part: SUPPORT FITTING — CORRODED (LT WING) · corrosion level 2 · airframe 54,690 hrs · 43,269 cycles

REAMED HOLE TO FINAL SIZE OF 3.7495 .7505 ON FLAP SUPPORT NR 1, HOLE NR 2 IAW REA B657-61641-MR. CORRODED L2, PN 113T1345-43, SN NONE, PART NAME NR 1 FLAP SUPPORT FITTING, STRINGER & WS LOCATION ON ACFT WS 797. ACFT WAS GNDED.

Part: SUPPORT — CORRODED (RT WING) · corrosion level 2 · airframe 54,690 hrs · 43,269 cycles

RIGHT WING NR 8 FLAP SUPPORT, RIB NR 3 HOLE SHOWS CRACK INDICATION WITH EDDY CURRENT. REAMED HOLE TO FINAL SIZE OF .7495 & .7505 IAW REA NR B767-61641-MR. SDR CORRODED L2, PN 113T1345-44, PART NAME 8 FLAP SUPPORT F1 WING, SN NSN, STRINGER LOCATION WS 807. ACFT WAS GNDED.

Part: SUPPORT FITTING — CORRODED (RT WING) · corrosion level 2 · airframe 54,690 hrs · 43,269 cycles

RIGHT WING NR 8 FLAP SUPPORT, RIB NR 2 HOLE SHOWS CRACK INDICATION WITH EDDY CURRENT. REAMED HOLE TO FINAL SIZE OF .7493 .7505 ON FWD SUPPORT NR 8, HOLE NR 2 IAW REA B767-61641-MR. SDR CORRODED L2, PN 113T1345-44, PART NAME 8 FLAP SUPPORT FITTING, SN NSN, STRINGER LOCATION WS 807. ACFT WAS GNDED.

Part: SUPPORT FITTING — CORRODED (LT WING) · corrosion level 2 · airframe 54,690 hrs · 43,269 cycles

LEFT WING NR 1 FLAP SUPPORT, RIB NR 1 HOLE SHOWS CRACK INDICATION WITH EDDY CURRENT. REAMED HOLES TO FINAL SIZE OF .7495 & .7505 IAW REA NR B657-61641MR. SDR INFO CORRODED L2, PART NUMBER 113T1345-43, PART NAME NR 11 FLAP SUPPORT FITTING, STRINGER & WS LOCATION WS 797. ACFT WAS GNDED.

Part: SUPPORT FITTING — CORRODED (RT WING) · corrosion level 2 · airframe 54,690 hrs · 43,269 cycles

RIGHT WING NR 7 FLAP SUPPORT, RIB 11 HOLE SHOWS CRACK INDICATION WITH EDDY CURRENT. REAMED HOLE TO FINAL SIZE OF .8745 & .8755 IAW REA NR B657-61641-MR. SDR CORRODED L2, PN 113T1345-48, PART NAME NR 2FLAP SUPPORT FITTING, SN NSN, STRINGER LOCATION WB 61G.2. ACFT WAS GNDED.

Part: SUPPORT FITTING — CORRODED (RT WING) · corrosion level 2 · airframe 54,690 hrs · 43,269 cycles

RIGHT WING NR 7 FLAP SUPPORT, RIB NR 4 HOLE SHOWS CRACK INDICATION WITH EDDY CURRENT. REAMED HOLE TO FINAL SIZE OF .8745 & .88.55 IAW REA NR B657-61641-MR. CORRODED L2 PN 113T1345-48, PART NAME NR 7 FLAP SUPPORT FITTING, SN NSN, STRINGER LOCATION WB 61G.2. ACFT WAS GNDED.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 54,690 hrs · 43,269 cycles

LOWER ANGLE AT KEEL TO STATION 977 BULKHEAD LBL 5 CORRODED. R & R LOWER ANGLE KEEL STATION 977 IAW SRM 51-40-02 & DWG 145T8610. CORRODED L2, PN 145T8610-9, SN NSN, PART NAME ANGLE, FS LOCATION ON ACFT, 977 LT WW, KEEL STRINGER & WS LOCATION ON ACFT LBL 5. ACFT WAS GNDED.

Part: RIB — CORRODED (RT WING) · corrosion level 2 · airframe 54,690 hrs · 43,629 cycles

NUMBER 5 SLAT OTBD AUX TRACK, INBD LOWER STRUT CORRODED AROUND FWD NUTPLATE. REMOVED DAMAGED STRUT RIB & INSTALLED NEW STRUT RIB PN 114T2203 13AX IAW SRM 51-40-02. CORRODED LEVEL 2, PN 114T2203-15, PART NAME STRUT AIR LOAD RIB, FS & BS LOCATION LW, STRINGER & WS LOCATION LES TO 475. ACFT WAS GNDED.

Part: STRUT — CORRODED (LE SLAT) · airframe 52,833 hrs · 42,623 cycles

NUMBER 5 SLAT INBD AUX TRACK OTBD LOWER STRUT HAS CORROSION UNDER NUTPLATES. R & R NR 5 SLAT INBD AUX TRACK OTBD LOWER RIB STRUT PN 114T2201-23 IAW REA NR B657-60734-MR AND B767 SRN 51-40-02. PN 114T2201-23, NSN, STRUT RIB CORRODED AT 433.1 TO 434.1. AIRCRAFT WAS GROUNDED.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 52,833 hrs · 42,623 cycles

DURING A HFEC INSPECTION OF THE Y RING ATTACHMENT OF THE AFT PRESSURE BULKHEAD A CRACK WAS INDICATED AT A FASTENER HOLE LOCATED AT STRINGER 10R B STATION 1582 INTERIOR OF THE FUSELAGE. TIMED OUT VERIFIED CRACK & REPAIRED IAW REA B653-60742-MR, TRIM OUT MEASURED 1.5 X 4.2 WITH 2.5 RADIUS. OPEN HOLE HFEC & SURFACE HPEC CHECKS PERFORMED WITH NO OTHER DAMAGE NOTED. REINSTALLED ALL FASTENERS REMOVED FOR ENGINEERING IAW B767 SRM 51-40-02. CRACKED LENGTH APPROXIMATELY .625 PN 148T2610-156 SN NSN PART NAME AFT PRESSURE BULKHEAD EXACT FS & BX LOCATION ON A/C FROM 1582 TO 1582 EXACT STRINGER & WS LOCATION ON A/C FROM STRINGER 10R TO STRINGER 10R. AIRCRAFT WAS GROUNDED.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 52,833 hrs · 42,623 cycles

FORWARD LOWER CARGO STRINGER 23L AFT OF STATION 767 FRAME HAS A 1.1 INCH CRACK AT STRINGER END FITTING LOC. REPAIRED STRINGER 23L AT STATION 676 TO 700 IAW B767-SRM 53-00-03 FIG 201 REPAIR 2. PN143T3001, NSN, STRINGER CRACKED 1.3 INCHES AT 676, 23L. AIRCRAFT WAS GROUNDED.

Part: BRACKET — CRACKED (TE FLAP) · airframe 52,833 hrs · 42,623 cycles

BRACKET ON FLAP ANGLE GEARBOX 18 INCHES FROM FUSELAGE ON WING TE CRACKED. R & R ANGLE GEARBOX BRACKET IAW B767-SRM 51-40-02 P. 10 PN 256T3022+-7, NSN, BRACKET CRACKED 1/2 INCH AT WBL 121 TO WBL 124. AIRCRAFT WAS GROUNDED.

Part: STRUT — CORRODED (LE SLAT) · airframe 52,833 hrs · 42,623 cycles

NUMBER 2 SLAT INBD AUX TRACK OTBD LOWER STRUT SPLIT AT FWD EDGE. NES STRUT RIB WAS FABRICATED ON REA B657-60736-MR. INSTALLED NEW STRUT RIB PN 114T2221-17 & A NEW TRACK FTG SHIM PACK IAW B767 SRM 51-40-02 PARA 4 & 7. PN 114T2221-17, NSN, STRUT CORRODED AT OSS 881.73. AIRCRAFT WAS GROUNDED.

Part: CONTACT — DIRTY (CABIN) · airframe 52,197 hrs · 42,244 cycles

EXTERIOR EMERGENCY EXIT LIGHT FAILS TO ILLUMINATE. CLEANED CENTER CONTACT IN LIGHT SOCKET ASSEMBLY OPS CHECK GOOD IAW B767 AMM 33-51-00, ACFT WAS GROUNDED.

Part: DOOR — MISSING (RT MLG) · airframe 51,755 hrs · 41,946 cycles

UPON MX POST FLIGHT WALK AROUND FOUND RIGHT MAIN GEAR SHOCK STRUT DOOR MISSING AND DAMAGE TO RIGHT TRUNNION DOOR. REMOVED AND REPLACED MLG TRUNNION DOOR ASSY W AMM 32-12-11-4, REMOVED AND REPLACED RIGHT MLG SHOCK STRUT DOOR ASSY IAW 32-12-06 AND 32-12-05 JACK A/C IAW AMM 07-11-01-02, C/W GEAR SWING IAW AMM 32-32-00-5 DOOR FIT FAIR CHECK O/C, AIRCRAFT WAS GROUNDED.

Part: BATTERY — DISCHARGED (CABIN) · airframe 51,614 hrs · 41,857 cycles

ON SERVICE CHECK FOUND EMERGENCY LIGHTS INOP FOR CREW SERVICE AREA. REMOVED AND REPLACED IAW AMM 33-51-07-2, INSTALLED SPARE EMERGENCY LIGHT BATTERY OPS CHECK NORMAL, ACFT WAS GROUNDED.

Part: FASTENER — CORRODED (CARGO DOOR) · airframe 51,425 hrs · 41,745 cycles

MDCD FWD MID LATCH CAM HOOK PITTED (.0075). REPAIRED MDCD FWD MID LATCH CMA PER REA NO: B652-59812-MR AND 767 MM 52-32-09-2, ACFT WAS GROUNDED.

Part: FASTENER — CORRODED (CARGO DOOR) · airframe 51,425 hrs · 41,745 cycles

MDCD AFT MID LATCH CAM HOOK PITTED (.005). REPAIRED MDCD AFT MID LATCH CAM PER REA NO: B652-59813-MR AND 767MM 52-32-09-S, ACFT WAS GROUNDED.

Part: BEAM — CRACKED (RT PYLON) · airframe 51,425 hrs · 41,745 cycles

RIGHT PYLON LOWER FWD INBD ANGLE CRACKED AND HAS PULLED THROUGH RIVETS, INBD SIDE OF PYLON AT LOWER FWD CORNER OF HYDRAULIC COMPARTMENTS. REMOVED AND REPLACED NR 2 INBD PYLON BEAM IAW B767 SRM 51-40-02, ACFT WAS GROUNDED.

Part: BEAM — WORN (ZONE 600) · airframe 51,425 hrs · 41,745 cycles

RIGHT WING OUTBD FLAP I/B HINGE CARRIER BEAM (ATTACHED TO FLAP) WHERE 3-10 LINK ATTACHS TO FLAP I/B FLANGE BOTH BUSHINGS LOOSE IN FLANGE AND I/B BUSHING ON O/B FLANGE LOOSE. REPAIRED ON REA B657-59823, ACFT WAS GROUNDED.

Part: SKIN — DENTED (CARGO DOOR) · airframe 51,425 hrs · 41,745 cycles

BULK CARGO DOOR EXTERIOR SURFACE HAS SEVERAL DENTS. REPAIRED DAMAGED AREA IAW B767-200 SRM 52-30-01. REPAIR G. RFTS NO. 45886, ACFT WAS GROUNDED.

Part: RIB — CORRODED (LE SLAT) · airframe 51,425 hrs · 41,745 cycles

NR 11 SLAT OUTBOARD AUX TRACK ATTACH FITTING OUTBOARD RIB CORRODED AROUND NUT PLATE. REMOVED AND REPLACED FIXED L/E RIB IAW 767 SRM 51-40-02, ACFT WAS GROUNDED.

Part: FITTING — DAMAGED (RT WING) · airframe 51,425 hrs · 41,745 cycles

RIGHT WING BACK UP FITTINGS FWD OF RIB 8 I/B AND O/B HAS TOOLING MARKS. REMOVED TOOLING MARKS PER ENGINEERING REQUEST IAW B767 SRM 51-10-02, ACFT WAS GROUNDED.

Part: FITTING — DAMAGED (RT WING) · airframe 51,425 hrs · 41,745 cycles

RIGHT WING BACK UP FITTING BETWEEN RIB 8 AND 9 AT FWD SPAR HAS TOOLING MARKS. REMOVED TOOLING MARKS PER ENGINEERING REQUEST IAW B767 SRM 51-10-02, ACFT WAS GROUNDED.

Part: RIB — CORRODED (LE SLAT) · airframe 51,425 hrs · 41,745 cycles

NR 9 SLAT OUTBOARD AUX TRACK ATTACH FITTING INBOARD RIB CORRODED AROUND NUT PLATES AT FORWARD LOWER END. REMOVED AND REPLACED NR 9 SLAT OUTBOARD AUX TRACK ATTACH FITTING INBOARD RIB IAW B767-200 SRM 51-40-0, ACFT WAS GROUNDED.

Part: FITTING — GOUGED (LT WING) · airframe 51,425 hrs · 41,745 cycles

LW KICK FITTING HAS A GOUGE (UPPER AFT SPAR A 5 OB). REPAIRED IAW REA B657-59799-MR, AIRCRAFT WAS GROUNDED. BS 955, WBL 97.95, LEFT WING.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,425 hrs · 41,745 cycles

STA 1654.5 CRACKS .406 AND .219 IN LENGTH FOUND ON THE OUTER CIRCUMFERENCE OF A FASTENER AT S-3L. CUT OUT DAMAGED AREA IAW B767 SRM 53-80-01 FIG 201, PERFORM HFEC IAW B767 PART6 51-00-19, FAB FILLERS & DBLRS IAW B767-200 SRM 53-80-01, INSTALLED REPAIR IAW B767-200 SRM 53-80-01 PG 201 REP 4, SEAM SEAL REPAIR IAW B767 SRM 51-20-5. PREP, PRIME, PAINT REPR DOUBLER AT B STA 1654.5 S-3L IAW B767 MM 51-21-10-7. PRIME INTERIOR OF REPAIR IAW B767 SRM 53-80-01, ACFT WAS GROUNDED.

Part: BEAM — CRACKED (NR 2 PYLON) · airframe 51,425 hrs · 41,745 cycles

NAC STA 295 NR 2, INBD ANGLE AT BOTTOM MOUNTING HOLES FOR PANEL 447ERX IS CRACK AND WORN. REMOVED AND REPLACED NR 2 O/B PYLON BEAM IAW B767-200 SRM 51-40-02, ACFT WAS GROUNDED.

Part: MOUNT — CORRODED (NR 1 ENGINE) · airframe 51,425 hrs · 41,745 cycles

NR 1 PYLON AFT ENGINE MOUNT RUSTED. REMOVED AND REPLACED NR 1 ENGINE AFT ENGINE MOUNT IAW B767 AMM 71-21-2 ENGINE, ACFT WAS GROUNDED.

Part: STRUCTURE — CORRODED (RT ELEVATOR) · airframe 51,425 hrs · 41,745 cycles

RT ELEVATOR APPROX STA 265 AT STAB T/E CORROSION FOUND. REMOVED AND REPLACED CHORD IAW B767 SRM 51-40-02, ACFT WAS GROUNDED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 51,092 hrs · 41,566 cycles

EMERGENCY LIGHT BELOW MAIN ENTRY DOOR IS INOP. REMOVED AND REPLACED ESCAPE LT BULB IAW B767 AMM 33-51-06. OPS CHECK GOOD AT THIS TIME, AWG.

Part: SIGN — INOPERATIVE (CABIN) · airframe 50,554 hrs · 41,263 cycles

EMERGENCY EXIT THRESHOLD SIGN, LOWER PORTION DOES NOT ILLUMINATE. REF REA B633-59369, EFFECTIVE ON N797AX WORK STEP 02 REMOVED AND REPLACED L1 DOOR EMERGENCY SIGN PER 767 MAINTENANCE MANUAL, USING P/N 82000-08704 SIGN IN LIEU OF P/N 82000-08707 SIGN. VERIFIED OPERATION AND ILLUMINATION.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 48,113 hrs · 39,532 cycles

EXIT IDENTIFIER LIGHT AT L1 DOOR INOP. REMOVED AND REPLACED POWER SUPPLY, AND BATTERY PER 767 MM 33-41-07-2, REMOVED AND REPLACED LIGHT ASSY PER 767 MM 33-51-03-002-802, OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 48,104 hrs · 39,524 cycles

EMERGENCY LIGHTS ARE INOPERATIVE AT ENTRANCE DOOR COCKPIT AND GROUND EXTERIOR LIGHT OK SWAPPED EMERGENCY LIGHTS POWER SUPPLY IAW B767 MM 33-51-07-2. CHECKS GOOD AS PER SAME. SPARE EMERGENCY LIGHTS BATTERY PACK USED. DEFERRED DI 62333 SPARE EMERGENCY LIGHTS BATTERY PACK DEFERRED FOR MAINT TRACKING IAW ABX GMM CHAP 1 SEC 07.04. REPLACED THE SPARE EMERGENCY LIGHT BATTERY WITH 7 DAYS. THE SPARE EMERGENCY LIGHT BATTERY PACK WILL BE REPLACED ON OR BEFORE NOV. 5, 2008 ALL PER B767 MM 33-51-07-2. CLEAR DI 62333, REMOVED SPARE EMERGENCY LIGHT BATTERY PACK AND BATTERY CHARGER ASSY IAW 33-61-02-2 DI CLEARED PLACARD REMOVED.

Part: JACKSCREW — DAMAGED (HORIZ STAB) · airframe 47,998 hrs · 39,479 cycles

HORIZONTAL STAB BALL SCREW INSPECTION FAILED IAW J/C 27-030-01. REPLACED HORIZONTAL STABILIZER ACTUATOR. STAB TRIM ACTUATOR ASSY SENT OUT ON R/O 501586374 TO REPAIR VENDOR DELTA AIRLINES INC. REASON FOR REMOVAL STATED AS JACKSCREW PITTED. UNIT WAS EXCHANGED.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 47,998 hrs · 39,479 cycles

DURING INSPECTION, LOWER TWO FASTENER HOLES OF RIGHT CHORD SHOWED CRACK INDICATION. CRACK LENGTH = .0625 INCH. REPLACED CHORD IAW EA 53800002-003.

Part: SPAR — CORRODED (LT WING) · airframe 47,998 hrs · 39,479 cycles

LEFT WING LOWER L/E WING SPAR WAS CORRODED I/B OF TAI DUCT, APPROXIMATELY WS 433. WING SPAR WAS REPAIRED IAW REA B657-57753.

Part: PANEL — MISSING (RT WING) · airframe 46,661 hrs · 38,775 cycles

THE RIGHT WING 651VB AND 651WB PANELS MISSING, THE SCREWS PULLED THROUGH PART OF PANEL. REPLACED RIGHT WING LANDING GEAR SUPPORT BEAM ACCESS PANELS IAW REA B657-50994 AND B657-55014.

Part: ANGLE — CRACKED (NR 2 PYLON) · airframe 46,285 hrs · 38,578 cycles

CRACKS AT FASTENER HOLES LEFT AND RIGHT ON ANGLE INSIDE OF STRUT LOOKING UP THROUGH LIGHTNING HOLE ON AFT END. REMOVED AND REPLACED CRACKED ANGLE IAW B767 SRM 51-40.

Part: FRAME — CORRODED (RT WING) · airframe 46,285 hrs · 38,578 cycles

RIGHT WING T-FRAME JUST INBOARD OF INBOARD FLAP HINGE HAD CORROSION. REPAIRED RIGHT WING T-FRAME IAW B767 SRM 57-51-02.

Part: BEAM — CORRODED (CARGO DOOR) · airframe 46,285 hrs · 38,578 cycles

FORWARD LOWER CARGO DOOR BEAM BELOW VENT DOORS WAS CORRODED AT NUT PLATE HOLES. REPLACED DOOR BEAM AS REQUIRED IAW B767 SRM.

Part: ANGLE — CRACKED (NR 1 PYLON) · airframe 46,285 hrs · 38,578 cycles

NR 1 PYLON TRAILING EDGE PANEL HAS CRACKED ANGLE ON INBOARD SIDE AND BROKEN NUT PLATE ON FORWARD OUTBOARD SIDE. REMOVED AND REPLACED ANGLE ON NR 1 PYLON TRAILING EDGE PANEL ON INBOARD SIDE AND REPLACED NUT PLATE IAW B767 SRM.

Part: IDG — FAILED (LT ENGINE) · airframe 46,173 hrs · 38,536 cycles

EICAS LEFT GENERATOR OFF DISPLAYED, OFF LIGHT ILLUMINATED. GENERATOR SWITCH RESET, DID NOT CORRECT CONDITION. APU SHUT DOWN AT TOP OF DESCENT, FOLLOWED PROCEDURES, WOULD NOT RESET. RESTARTED ON VECTORS FOR APPROACH INTO IND. EMERGENCY AIR DIVERSION INTO IND DUE TO GEN/APU ISSUES. REPLACED IDG IAW B767 MM 24-11-005. LEAK CHECKED GOOD. PERFORMED APU BITE PROCEDURE IAW B767 MM 49-11-00-12. SYSTEM CHECKED NORMAL.

Part: IDG — DEFECTIVE (LEFT) · airframe 46,173 hrs · 38,536 cycles

EICAS MESSAGE LEFT GENERATOR OFF DISPLAYED, OIL LIGHT ILLUMINATED. GENERATOR SWITCH RESET DID NOT CORRECT CONDITION. APU SHUT DOWN AT TOP OF DESCENT, FOLLOWED PROCEDURES WOULD NOT RESET. RESTARTED ON VECTORS FOR THE APPROACH INTO IND, EMERGENCY AIR DIVERSION. REMOVED AND REPLACED LEFT IDG IAW B767 AMM 24-11-01-4. PERFORMED APU BITE PROCEDURE IAW B767 AMM 49-11-00-12, FIGURE 103. SYSTEM CHECKED GOOD.

Part: CAM — OBSTRUCTED (L1 DOOR SLIDE) · airframe 46,076 hrs · 38,493 cycles

L1 DOOR SLIDE WOULD NOT ARM. FOUND A PIECE OF DOOR GUARD IN THE CAM AREA, REMOVED FOD. DOOR SLIDE ARMED AS REQUIRED IAW B767 MM.

Part: GIRT BAR — DIRTY (L1 DOOR) · airframe 41,141 hrs · 36,685 cycles

L-1 DOOR EMERGENCY SLIDE WOULD NOT ARM WITH DOOR CLOSED. FOUND DEBRIS IN GIRT BAR MECHANISM. CLEANED DEBRIS FROM GIRTH BAR MECHANISM. EMERGENCY ESCAPE SLIDE ARMING MECHANISM OPS CHECKED GOOD IAW B767 AMM 25-66-00-2.

Part: GIRT BAR — OBSTRUCTED (PAX DOOR) · airframe 38,968 hrs · 35,923 cycles

GIRT BAR WOULD NOT ARM ON MAIN CABIN DOOR. REMOVED TAPE FROM THE MAIN ENTRANCE DOOR GIRT BAR. OPS CHECKED GOOD IAW B767 AMM CHAPTER 52.

Part: SKIN — CORRODED · airframe 38,930 hrs · 35,908 cycles

RIGHT HORIZONTAL STABILIZER, UPPER SKIN P/N 182T3200-2, AT STRINGER 3, RSS 42, WAS CORRODED OUT OF LIMITS. REPAIRED AREA IAW REA B655-43586-MR.

Part: SKIN — CORRODED (RIGHT WING) · airframe 38,930 hrs · 35,908 cycles

CORROSION AT RIGHT WING LOWER SKIN PANEL NO. 1 AT REAR SPAR, BETWEEN STRINGER 230 AND 277. REPAIRED AREA IAW REA B657-43583-MR.

Part: SKIN — GOUGED (CARGO DOOR) · airframe 38,930 hrs · 35,908 cycles

GOUGE IN 146T6334-1 BULK CARGO DOOR INNER SKIN, STATION 1439, WATER LINE 131. REPAIRED AREA IAW REA B652-43447-MR.

Part: RIB · airframe 38,930 hrs · 35,908 cycles

LEFT WING LEADING EDGE SLAT #6 AUXILIARY RIB ASSEMBLY P/N 1143170, AUXILIARY RIB HAD MISDRILLED HOLE. REPAIRED AREA IAW REA B657-43455-MR.

Part: SKIN — CRACKED (LEFT WING) · airframe 38,930 hrs · 35,908 cycles

A 0.06" LONG CRACK WAS FOUND IN ONE FASTENER HOLE IN THE UPPER LEFT WING SKIN PANEL AS SHOWN IN REF. (5) - SB 767-54-0081. REPAIRED AREA IAW REA B657-43511-MR.

Part: CONTROL QUADRANT — DAMAGED (AILERON) · airframe 38,930 hrs · 35,908 cycles

AILERON CONTROL QUADRANT ASSEMBLY, FOUND DAMAGE AT BEARING SEAT. REPAIRED AREA IAW REA B627-43542-MR.

Part: SKIN — CRACKED (RIGHT WING) · airframe 38,930 hrs · 35,908 cycles

A 0.06" LONG CRACK WAS FOUND IN ONE FASTENER HOLE IN THE RIGHT UPPER WING WHILE ACCOMPLISHING SERVICE BULLETIN SB 767-54-0081. REPAIRED AREA IAW REA B657-43512-MR.

Part: STRAP — CORRODED (FUSELAGE) · airframe 38,930 hrs · 35,908 cycles

FUSELAGE SKIN TEAR STRAP WAS CORRODED AT STATION 742, BUTT LINE 0, BETWEEN STRINGER 39 LEFT TO STRINGER 39 RIGHT, UNDER SHEAR TIE, AFTER BLENDED OUT, FOUND REMAINING THICKNESS OUT OF LIMITS. REPAIRED AREA IAW REA B653-43559-MR.

Part: SHEAR TIE · airframe 38,930 hrs · 35,908 cycles

SHEAR TIE INSTALLED AT STATION 1417, BETWEEN STRINGER 20 LEFT TO STRINGER 21 LEFT, HAD SHORT EDGE MARGIN TO FASTENER. REPAIRED AREA IAW REA B653-43456-DE.

Part: FAILSAFE — CORRODED (FUSELAGE) · airframe 38,930 hrs · 35,908 cycles

FAIL-SAFE STRAP LOCATED AT STATION 539, BETWEEN STRINGER 31 RIGHT TO STRINGER 32 RIGHT FORWARD CARGO DOOR. CORROSION WAS FOUND ON FAIL-SAFE. REPAIRED AREA IAW REA B653-43524.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 38,930 hrs · 35,908 cycles

FUSELAGE STATION 1540 FRAME OUTER CHORD DAMAGE BETWEEN STRINGER 10 LEFT AND STRINGER 11 LEFT AT HORIZONTAL FLANGE. REPAIRED DAMAGED AREA IAW REA B653-43564-MR.

Part: SEAT TRACK · airframe 38,930 hrs · 35,908 cycles

SEAT TRACK P/N 96FS667743-101 LOWER HORIZONTAL OUTBOARD FLANGE AT STATION 753-45, LEFT BUTT LINE 86.38, DRILLED BY MISTAKE. REPAIRED AREA IAW REA B653-43514-DE.

Part: ANGLE — CORRODED (FWD LWR CARGO) · corrosion level 2 · airframe 38,930 hrs · 35,908 cycles

CORRODED ANGLE BETWEEN STATIONS 632 - 654 AND BETWEEN STRINGERS 34 - 35. REPLACED ANGLE IAW B767 AMM.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,930 hrs · 35,908 cycles

DEEP CORROSION ON UPPER CHORD AT STATION 544. REPLACED UPPER CHORD IAW B767 AMM.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,930 hrs · 35,908 cycles

DEEP CORROSION ON UPPER CHORD AT STATION 720, BETWEEN RIGHT BUTT LINE 45 - LEFT BUTT LINE 45. REPLACED UPPER CHORD IAW B767 AMM.

Part: SUPPORT FITTING — CORRODED (RIGHT MLG) · airframe 38,930 hrs · 35,908 cycles

MIGRATED BUSHING, RIGHT MAIN LANDING GEAR SIDE STRUT SWIVEL SUPPORT FITTING, AFTER REMOVAL OF PART 113T1108-25, FOUND DEEP CORROSION ON FITTING. REPAIRED AREA IAW REA B657-43443-MR.

Part: SHEAR TIE — CORRODED (FWD LWR CARGO) · airframe 38,930 hrs · 35,908 cycles

CORRODED SHEAR TIE AT STATION 720 BETWEEN STRINGERS 37 RIGHT - 37 LEFT. REPLACED SHEAR TIE IAW B767 AMM.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,930 hrs · 35,908 cycles

CRACK AND DEEP CORROSION ON UPPER CHORD AT STATION 676, RIGHT BUTT LINE 45. REPLACED T-CHORD IAW B767 AMM.

Part: PANEL — CORRODED (FUSLEAGE) · airframe 38,930 hrs · 35,908 cycles

CORRODED SHEAR PANEL BETWEEN STATIONS 544-610, LEFT BUTT LINE - RIGHT BUTT LINE - 20. REPLACED PANEL IAW B767 AMM.

Part: SHEAR TIE — CORRODED (FWD LWR CARGO) · airframe 38,930 hrs · 35,908 cycles

DEEP CORROSION ON SHEAR TIE AT STATION 764 BETWEEN STRINGERS 36 - 37. REPLACED SHEAR TIE IAW B767 AMM.

Part: SHEAR TIE — CORRODED (FWD LWR CARGO) · airframe 38,930 hrs · 35,908 cycles

DEEP CORROSION ON SHEAR TIES AT STATION 742, BETWEEN STRINGERS 36 LEFT - 39 RIGHT. REPLACED SHEAR TIES INAW B767 AMM.

Part: PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,930 hrs · 35,908 cycles

CORRODED SHEAR PANEL BETWEEN STATIONS 566 - 610, LEFT BUTT LINE 35 - 45. REPLACED PANEL IAW B767 AMM.