N76156

Part: COMPUTER — FAILED (E&E BAY) · airframe 49,360 hrs · 7,297 cycles

AFTER TAKEOFF, GOT "AUTOPILOT" EICAS MESSAGE & RED M/C LIGHT. SWITCHED AND TRIED ALL 3 AUTOPILOTS. ALL THE SAME, HAD NO STAB TRIM. PERF'D MCDP LAST FLT FAULT REVIEW, FOUND MULTIPLE CODES REFERENCING L FCC FAULT ACROSS MULTIPLE CHANNELS. R&R'D L FCC IAW AMM 22-11-01 & INSTALLED CURRENT SOFTWARE. FCC OPS CK GOOD. PERF'D MCDP TEST 30 PER AMM 22-00-02, NO FAULTS NOTED, ACFT REMAINS CA TIII/LAND3. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1474502 SN OFF 08006. COMPUTER, FLIGHT OFF 99-2211-9-0001 8006 ON 99-2211-9-0001 8537

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 45,736 hrs · 6,816 cycles

CABIN - BS 400-412 RBL 20 SEAT TRACK CRACKED. CRACKED SEAT TRACK REPLACED AS PER SRM 51-10-02 AND NEW SEAT TRACK INSTALLED AS PER SRM 51-40-02 AT STA 340-423.45 RBL 20 AND FORM 44.0008 ATTACHED ITEM 1-4 ACCOMPLISHED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 45,736 hrs · 6,816 cycles

CABIN - BS 340-344 RBL 88 SEAT TRACK FOUND CORRODED. SEAT TRACK CORROSION BLENDED OUT DEPTH 0.030" (ORIG 0.071) OUT OF SRM 53-00-52 ALLOWABLE DAMAGE 1 FIG 101 LIMIT AND CORRODED SEAT TRACK REPLACED AS PER SRM 51-10-02 AND NEW SEAT TRACK INSTALL AS PER SRM 51-40-02 AT STA 340-423.5 RBL 88.5 AND FORM 44.0008 ATTACHED ITEM 1-7 ACCOMPLISHED.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 45,736 hrs · 6,816 cycles

CABIN BS 325 RBL 35-80 FLOOR SUPPORT FOUND CORRODED. CABIN FLOORBEAM UPPER CHOCK CORROSION REMOVED OUT OF SRM 53-00-51 ALLOWABLE DAMAGE 1 FIG 101 LIMIT AND CORRODED UPPER CHORD REPAIRED AS PER ECRA 5320-02017 REV AT BS 325 RBL 26 TO RBL 86 AND FORM 44.0008 ATTACHED ITEM 1-39 ACCOMPLISHED.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 45,736 hrs · 6,816 cycles

CABIN - BS303 LBL20-30 FLOOR SUPPORT FOUND CORRODED CABIN BS303 LBL20-30 FLOORBEAM UPPER CHORD CORROSION REMOVED OUT OF SRM 53-00-51 ALLOWABLE DAMAGE 1 FIG 101 LIMIT AND FLOORBEAM UPPER CHORD CORRODED AREA REPAIRED AS PER SRM 53-00-51 FIG 201 REPAIR 1 AT BS 303 LBL 1 TO LBL 41 AND FORM 44.0008 ATTACHED ITEM 1-16 ACCOMPLISHED.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 45,736 hrs · 6,816 cycles

CABIN - BS 325 LBL 23-59 FLOOR SUPPORT FOUND CORRODED CABIN BS 325 LBL 23"-59" FLOORBEAM UPPER CHORD CORROSION REMOVED OUT OF SRM 53-00-51 ALLOWABLE DAMAGE 1 FIG 101 LIMIT AND FLOORBEAM CORRODED UPPER CHORD REPAIRED AS PER SRM 53-00-51 FIG 201 REPAIR 1 AT BS 325 LBL 12" TO LBL 66" AND FORM 44.0008 ATTACHED ITEM 1-14 ACCOMPLISHED.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 45,736 hrs · 6,816 cycles

CABIN - BS 303 RBL 80 FLOOR SUPPORT FOUND CORRODED. CABIN BS 303 RBL 80 FLOORBEAM UPPER CHORD CORROSION REMOVED OUT OF SRM 53-00-51 ALLOWABLE DAMAGE 1 FIG 101 LIMIT AND FLOORBEAM UPPER CHORD CORRODED AREA REPAIRED AS PER SRM 53-00-51 FIG 201 REPAIR 1 AT BS 303 RBL 40.25 TO RBL 80 AND FORM 44.0008 ATTACHED ITEM 1-32 ACCOMPLISHED.

Part: LATCH — DIRTY (CABIN) · airframe 38,847 hrs · 5,889 cycles

LAV "H" OXYGEN MODULE DOOR FAILED TO OPEN PERFORM AMM 35-21-00 STEP F (7). CLEANED LATCH MECHANISM, OPS CHECK GOOD REF AMM 35-21-00.

Part: LATCH — DIRTY (CABIN) · airframe 38,847 hrs · 5,889 cycles

AFT LT F/A STATION OXYGEN MODULE DOOR FAILED TO OPEN PER AMM 35-21-00 STEP F (7). CLEANED LATCH MECHANISM, OPS CHECKS GOOD REF 35-21-00.

Part: LUG — CORRODED (LT MLG) · airframe 35,123 hrs · 5,361 cycles

EA3210-01986 REV B LEFT MAIN LANDING GEAR INNER CYLINDER PIVOT BORE OF INBOARD LUG FOUND CORROSION AFTER BUSHING REMOVED. MAIN LANDING GEAR INNER CYLINDER INBOARD LUG PIVOT BORE REPAIRED IAW ECRA 3210-02114. GEAR RETRACTION TEST COMPLETED IAW AMM 32-32-00.

Part: SEAT TRACK — CRACKED (CABIN) · airframe 35,123 hrs · 5,361 cycles

FORWARD CARGO STATION 412 CABIN FLOORBEAM SEAT TRACK FOUND CRACKED AT LBL 20. CABIN FLOORBEAM SEAT TRACK AT STATION 412 LBL 20 REPAIRED PER ECRA 5320-01907, HFEC FOUND NO CRACK.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 35,123 hrs · 5,361 cycles

CABIN FLOOR SUPPORT FOUND CORRODED AT BODY STATION 325 BETWEEN LBL 21-58. FLOOR SUPPORT BEAM BODY STATION 325 LBL 14 - 63 REPAIRED PER SRM 53-00-51 REPAIR 1 FIG 201, HFEC FOUND NO CRACK.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 35,123 hrs · 5,361 cycles

E&E COMPARTMENT LEFT STATION 246 CABIN FLOORBEAM LBL 40 VERTICAL STIFFENER FOUND CRACKED. E&E COMPARTMENT LEFT STATION 246 CABIN FLOORBEAM LBL 40 VERTICAL STIFFENER REPAIRED PER ECRA 5310-04844.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 35,123 hrs · 5,361 cycles

E&E COMPARTMENT STATION 246 LBL 40 CABIN FLOOR MID CHORD FOUND CRACKED. E&E COMPARTMENT STATION 246 LBL 40 CABIN FLOOR MID CHORD REPAIRED PER SRM 53-10-51, REPAIR 2 FIG 201 AND ECRA 5310-04844.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 35,123 hrs · 5,361 cycles

E&E COMPARTMENT LEFT STATION 246 CABIN FLOORBEAM LBL 25 VERTICAL STIFFENER FOUND CRACKED. E&E COMPARTMENT LEFT STATION 246 CABIN FLOORBEAM LBL 25 VERTICAL STIFFENER REPLACED PER SRM 51-10-02 AND FASTENERS INSTALLED PER SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 35,123 hrs · 5,361 cycles

CABIN FLOOR SUPPORT FOUND CORRODED AT BODY STATION 303 BETWEEN LBL 31- 41. CABIN FLOOR SUPPORT REPAIRED PER SRM 53-00-51, REPAIR 1, FIG 201.

Part: FLOORBEAM — CORRODED (BS 325) · airframe 23,449 hrs · 3,703 cycles

INSPECTION FOUND FLOORBEAM CORRODED AT BS 325, LBL 25 TO 55. REPAIRED IAW SRM 53-00-51, FIGURE 201, REPAIR 1.

Part: FLOORBEAM — CORRODED (BS 303) · airframe 23,449 hrs · 3,703 cycles

INSPECTION FOUND FLOORBEAM CORRODED AT STA 303, LBL 5 TO LBL 32. REPAIRED IAW SRM 53-00-51, REPAIR 1, FIGURE 201.