N104FE

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 17,236 hrs · 6,971 cycles

MDCC SEAT TRACK DAMAGED AT STA610 - STA632 LBL11 REPAIRED THE MDCC DAMAGED SEAT TRACK AT STA610 - STA632 LBL11 PER B767 SRM53-00- 52-2R REPAIR9. THIS REPAIR IS A CAT A REPAIR. MAJOR REPAIR IAW FEDEX GMM 6-2-100.

Part: FUSIBLE PLUG — FAILED (NR 2 WHEEL) · airframe 15,108 hrs · 6,084 cycles

NR 2 MAIN WHEEL TIRE FUSE PLUG MELTED DUE TO REJECTED TAKE-OFF. REMOVED AND REPLACED NR 2 MAIN WHEEL TIRE PER AMM-32-45-01-4. OKAY FOR SERVICE.

Part: ADIRU — INOPERATIVE (COCKPIT) · airframe 14,561 hrs · 5,828 cycles

PDIS 104 34-11 7994 03JUN21 GSO IN THE DESCENT FROM FL 410 WITH SAT -61* RECEIVED A ALT DISAGREE CAUTION WITH INTERMITTENT IAS DISAGREE CAUTION. SUMMIZED THAT CAPTAINS S SIDE WAS IN ERROR. F/O SIDE MATCHED STBY INSTRUMENTS. CAPTAIN S SIDE WAS APPROX 5-6 KNOTS SLOWER AND 300 FEET LOW. CAUTIONS CLEARED BELOW 10,000 FT IN CLEAR AIR. FACT 12JUN21 18:46 MEM R/R'D LH ADIRU PER AMM 34-26-01-4. CHECKS GOOD. AIR DATA SEL SWITCH RETURNED TO LEFT POS AND SAFETIED.

Part: TUBE — LEAKING (PITOT/STATIC SYS) · airframe 8,932 hrs · 3,628 cycles

ALTITUDE DISAGREE AND AIRSPEED DISAGREE EICAS MESSAGES ILLUMINATED AT FL 270. CAPTAIN ALTIMETER 500 FT LOW AND CAPTAIN AIRSPEED INDICATOR 8 KTS SLOW. STANDBY INSTRUMENTS AND FIRST OFFICER ALTIMETER AND AIRSPEED INDICATOR MATCHED. PERFORMED LEAK CK AND FOUND AIR LEAK AT STATIC LINE QUICK DISCONNECT FITTING (S1) AT CAPT PITOT/STATIC TUBE. R&R CAPT PITOT/STATIC TUBE, ALL SYSTEM TEST PASSED AND PITOT HEAT TEST PASSED PER AMM 34-11-01-4 AND 34-11-00-5.

Part: D-RING — MISSING (ESCAPE HARNESS) · airframe 5,721 hrs · 2,407 cycles

ON ARRIVAL CHK FOUND 2 EMERGENCY ESCAPE HARNESS BELOW SUPERNUMERARY SEAT MISSING CARABINER(D-RING). REMOVED BOTH HARNESS AND PLACED IN TSP BOX PER MEL. A/C OK FOR SERVICE. INSTALLED THE SUPERNUMERARY EMERGENCY ESCAPE HARNESS D-RING BACK ON AND INSTALLED THE D-RING EMERGENCY ESCAPE HARNESS BELOW SUPERNUMERARY SEAT PER SMP, A/C OK FOR SERVICE.

Part: ESCAPE ROPE — UNSECURE (CABIN) · airframe 20 hrs · 912 cycles

MAIN CABIN ENTRY ESCAPE ROPE NEEDS TO BE REPACKED. INSTALLED MAIN ENTRY EMER ESCAPE ROPE IAW AMM 25-10-00-2. PERFORMED RII.

Part: SENSOR — FAULTY (ENTRY DOOR) · airframe 18 hrs · 867 cycles

LEFT FWD ENTRY DOOR EICAS MSG WITH OVERHEAD PANEL, ENTRY DOORS, ILLUMINATED WITH LT ENTRY DOOR CLOSED. R & R CREW ENTRY DOOR CLOSED LATCH SENSOR S 195.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 17 hrs · 809 cycles

RIGHT OTBD AFT FLAP LOWER SURFACE HAS DELAMINATED AREA 35 INCHES FROM OTBD END OF AFT FLAP. REMOVED DAMAGE & REPAIRED AREA OF DELAMINATION IAW EA H-5750-T0315554 PT 1.

Part: SKIN — DENTED (NR 4 SLAT) · airframe 17 hrs · 809 cycles

LEFT WING, LE NR 4 SLAT, UPPER SURFACE HAS A DENT AT WS 590. REPAIRED IAW EA H 5750-T0315441 PT1.

Part: ACM — FAILED (LEFT HAND)

01-305 IN CLIMB CREW NOTICED ODOR IN COCKPIT. R&R LT ACM PER MM 21-51-001-4.

Part: OVERHEAT LOOP — INOP (NR 1 ENGINE)

NR 1 ENG STRUT FLICKERED ON T/O ROLL MOMENTARILY AND THEN EXTINGUISH AT 4,000' ALT, LIGHT ILLUM STEADY. *S/D* REMOVED AND REPLACED OVERHEAT LOOP PER MM 26-14-1, LEAK CK NORMAL. LIGHT OPER CK NORM. OK FOR SERVICE.

Part: RIB — CORRODED (BS 870)

NR 0391 006, WHILE WORKING NR 0375, FOUND CORROSION ON WING PLUS CHORD ON BOTTOM PORTION BS 870, LBL 67 AT INBOARD, AFT FASTENER HOLES AND OUTBOARD AFT FASTENER HOLE.

Part: SPAR CHORD — CORRODED (BS 740)

NR 0323 005, CORROSION (C53-224-05) WING CENTER SECTION UPPER FWD SPAR CHORD, BS 740, LBL 38-44 AND 53-57, WL 202.

Part: SPAR CHORD — CORRODED (BS 740)

CORROSION (C53-132-02-1/2) WING CENTER SECTION LWR SPAR CHORD BS 740, LBL 32 TO 42, WL 169. *S/D* ACCESSED AREA REMOVED LOWER BS 740 CENTER TANK SPAR CHORD RBL 70.5 TO LBL 70.5, WL 169. INSPECTED FASTENER HOLES, COLD WORKED FASTENER HOLES, FLAP PEENED SKIN, FABRICATED SPLICE PLATES, DRILLED CHORD AND REPAIR PARTS AND INSTALLED IAW FED 7-5710-36197. REINSTALLED ACCESSED ITEMS.

Part: CHORD — CORRODED (BS 863- 870)

NR 0385 007, WHILE WORKING NR 0245 FOUND CORROSION ON OUTBOARD FLANGE OF THE LONGITUDINAL BEAM LOWER CHORD FROM BS 863-870, LBL 45, WL 188.

Part: BULKHEAD WEB — CRACKED (BS 740)

NR 0392 004, WHILE WORKING (NR 0246) FOUND CRACK IN 740 BULKHEAD WEB AT BLO, WL 168 AND CORROSION AT LBL 6, WL 170 AND AT RBL 1 AND 2 WL 170.

Part: STRINGER — CORRODED (BS 448)

CORROSION (C53-224-03) FOUND ON STRINGER 22R AT BS 448. *S/D* REPAIRED STRINGER 22R AT BS 448 IAW FED-EX SRM 53-10-3.

Part: WEB — CORRODED (BS 351-360)

CORROSION (C53-224-06) ON WEB AT BS 351 TO 360, LBL 65, WL 208.

Part: SPAR CHORD — CORRODED (BS 870)

NR 0245 001 CORROSION (C53-132-02-1/2) WING CENTER SECTION UPPER REAR SPAR CHORD BS 870, RBL 70-LBL 70, WL 188. REMOVED AND REPLACED DAMAGED 870 UPPER CHORD PER FED-EX EA 7-5710-36196.

Part: OIL PRESS SW — FAILED (NR 1 ENGINE)

97-0136 NR 1 LOW OIL BYPASS LIGHT CAME ON AFTER TAKEOFF. NR 1 THRUST LEVER TO IDLE LIGHT OUT .30 SECONDS LATER LIGHT CAME ON AND STAYED ON. OIL PRESS 48 PSI OIL TEMPERATURE NORMAL. ENGINE SHUT DOWN AFTER 2 MINUTE WIND MILLING. REMOVED AND INSPECTED MAIN OIL FILTER. NO DEFECTS NOTED. INSTALLED NEW FILTER. REMOVED AND REPLACED LOW OIL PRESS SWITCH PER MAINTENANCE MANUAL 79-33-2. CHECKED WIRING NO DEFECTS NOTED. RAN NR 1 ENGINE PER JET RUN HANDBOOK. LOW BYPASS LIGHT OPERATIONAL CHECKS NORMAL. NO LEAKS NOTED. OK FOR SERVICE.

Part: WEB — CRACKED (BS 520)

CRACK IN WEB AT BS 520 WL 198 RBL 58. REMOVED, FABRICATED NEW WEB AND INSTALLED THE WEB AT BS 500 TO 560 RBL 58 WL 198, AS PER BOEING DRAWING 65-19309.

Part: ANGLE — CORRODED (BS 310-343)

NRO-777, CORROSION AROUND NUTPLATES ON FORWARD ENTRY DOOR AT BS 310 TO 343 LBL 62 WL 309. REMOVED CORRODED SUPPORT AT BS 310 TO 343 LBL 62 WL 309, IAW FEDEX SRM 51-IC-1.

Part: SEAT TRACK — CORRODED (BS 344-349)

NRO-780, CORROSION ON SEAT TRACK FLANGE AT BS 344 TO BS 349 LBL 58 WL 208.1. REMOVED CORROSION ON SEAT TRACK FLANGE AT BS 344 TO BS 349 LBL 58 WL 208.1, FOUND TO BE OUT OF LIMITS IAW FEDEX SRM 53-10-01. INSTALLED NEW ONE.

Part: FLOORBEAM — CORRODED (BS 344)

NRO-777, CORROSION ON TOP CHORD OF FLOORBEAM AT BS 344 RBL 20 TO LBL 60 WL 208 STR 8. REMOVED TOP CHORD FLOORBEAM AT BS 344 RBL 70 TO LBL 70 WL 208 STR 8, IAW FEDEX REPAIR DRAWING NR SR27-53-007, DUE TO TOP CHORDS OF FLOORBEAM OUT OF LIMITS.

Part: FRAME — DAMAGED (BS 380)

(NRO 783) MECHANICAL DAMAGE TO FRAME AT BS 380, STR 7 L/H WL 280 CORRECTIVE ACTION FOUND DAMAGE TO BE OUT OF LIMITS PER FEDEX SRM 53-10-1. REPAIRED FRAME AT STATION 380 STR 7 L/H WL 280 PER FEDEX SRM 53-10-4 .

Part: SEAT TRACK — CORRODED (BS 360)

NRO-781, CORROSION ON SEAT TRACK FLANGE AT BS 360 LBL 60 WL 208.1. REMOVED CORROSION ON SEAT TRACK FLANGE AT BS 360 LBL 60 WL 208.1, IAW FEDEX SRM 53-10-01.

Part: FRAME — DENTED (BS 560)

DENTED FRAME AT BS 560, STR 6 RT. REPAIRED DENTED FRAME IAW FEDEX SRM 53-10-4.

Part: SHEAR TIE — CRACKED (BS 640)

CRACKED AND DAMAGED SHEAR TIE AT BS 640, LT STR 8. REPAIRED DAMAGED SHEAR TIE IAW FEDEX EA 7-5310-24654.