N468FE

Part: SENSE LINE — DIRTY (NR 2 ENGINE) · airframe 52,750 hrs · 37,535 cycles

REJECTED TAKE OFF DUE LOW NR 2 EPR INDICATION. REJECTED TAKE OFF AT 80 KTS AND APPLIED BRAKES AT 60KTS, NO BRAKE COOLING REQUIRED. ON SUBSEQUENT TAKE OFF NORMAL EPR WAS OBTAINED, BUT IT REQUIRED ALMOST FULL THROTTLE THROW ON NR 2 (LARGE SPLIT). OPENED NR 2 ENGINE COWLING REF MM 77-11-031-6-0 AND INSPECTED EPR SENSE LINES BOTH PT7, PT2, NO OBVIOUS DAMAGE NOTED IAW REF MM 77-11-011-4, DISCONNECTED SENSE LINES & FORCED AIR THROUGH CLEANING LINES. RECONNECTED LINES & CLOSED NACELLE. PERFORMED TAKE OFF EPR TEST. ALL INDIACTIONS NORMAL. NR 1 & 2 ENGINE THROTTLES EVEN, BUT NR 3 WAS AT LEAST 1 KNOB BEHIND. NO NOISE THROTTLE ALIGNMENT REQUESTED.

Part: ENGINE — OVERTEMP (NR 3) · airframe 52,671 hrs · 37,468 cycles

NR 3 ENGINE OVERTEMP. R & R NR 3 ENGINE IAW WORKCARD 70T0001-03,70T003-03 AND 70T0301-03, OPS CHECKED GOOD.

Part: ENGINE — OVERTEMP (NR 2) · airframe 52,671 hrs · 37,468 cycles

NR 2 ENGINE OVERTEMP. R & R NR 2 ENGINE IAW WORKCARD 70T0002, 70T0301-02, AND 70T0003-02, OPS CHECKED GOOD.

Part: ENGINE — DAMAGED · airframe 52,655 hrs · 37,454 cycles

AFTER TAKEOFF, RECEIVED A RED WINDSHEAR WARNING LIGHT PERFORMED WINDSHEAR ESCAPE MANUVER W/FIREWALL POWER, APPROX 1 MIN. INSPECTED ALL EXHAUST AREAS FOR DAMAGE DUE TO OVERTEMP CONDITION. NO DAMAGE FOUND. R & R ENGINE. OPS CHECKED GOOD.

Part: SKIN — MISREPAIRED (CARGO DOOR) · airframe 52,524 hrs · 37,317 cycles

MCD EXTERNAL SKIN DOUBLER TO EXTERNAL SKIN STA 560 STR 10L. REMOVED REPAIR AT MCD EXTERNAL SKIN STA 560 STR 10L IAW SRM 51-30-2. FABRICATED DOUBLER AND FILLER, AND INSTALLED FILLER AND DOUBLER REPAIR PER EA 7-5230-136752.

Part: STRINGER — CORRODED (BS 1010 S27L) · corrosion level 2 · airframe 52,524 hrs · 37,317 cycles

AFT CARGO STA 1010, STR 27L CORROSION AROUND RIVET TAIL. REMOVED AND REPLACED PRODUCTION SPLICE STRINGER 27L STA 1010 IAW B727 SRM 51-30-2 REV 103

Part: SKIN — DAMAGED (ZONE 800) · airframe 52,524 hrs · 37,317 cycles

C-1 DOOR FWD LOWER OUTER SKIN IS OIL CANNED AT BS 560 3" CUT OUT DAMAGED AREA OF SKIN ( DIM 2" X 1 13/16" ) IAW SRM 52-00-3 FIG 3 FABRICATED REPAIR DOUBLER IAW SRM 52-00-3 FIG 3. INSTALLED REPAIR DOUBLER IAW SRM 52-00-3 FIG 3 AND 51-30-2 REV 103 AND EA 7-5210-123593

Part: STRINGER — CRACKED (RT WING) · airframe 52,524 hrs · 37,317 cycles

RT WING STA 686.5 STR 9 IS CRACKED. FABRICATED REPAIR ANGLES AND RADIUS FILLERS. INSTALLED REPAIR PARTS IAW EO 7-5710-7-4322 PT1 AT RT WING STA 686.5 STR 9.

Part: STRINGER — CRACKED (LT WING) · airframe 52,524 hrs · 37,317 cycles

LT WING, STA 686.5 STR 14 IS CRACKED. CUT ACCESS HOLE IN LT WING STR 14 VENT BOX, FABRICATED REPAIR PARTS, AND INSTALLED REPAIR PARTS IAW EO 7-5710-7-4322 PT1 AT LT WING STA 686.5 STR 14.

Part: STRINGER — CRACKED (LT WING) · airframe 52,524 hrs · 37,317 cycles

LT WING STA 629.0, STR 8 IS CRACKED. FABRICATED REPAIR ANGLES AND RADIUS FILLERS. INSTALLED REPAIR PARTS IAW EO 7-5710-7-4322 PT1 AT LT WING STA 629.0 STR 8.

Part: ANGLE — CHAFED (BS 640) · airframe 52,524 hrs · 37,317 cycles

HEADER BEAM, LOWER ANGLE STRAP CHAFED BS 640.

Part: FRAME — BENT (BS 1050 S28R) · airframe 52,524 hrs · 37,317 cycles

AFT CARGO STATION 1050 AT STRINGER 28R, FRAME BENT. FABRICATED REPAIR DOUBLER IAW SRM 53-10-2 FIG 5 AND 51-40-3 FIG 1. INSTALLED DOUBLER IAW SRM 51-30-2 AND 51-40-3 FIG 1.

Part: FRAME — DAMAGED (BS 783) · airframe 52,524 hrs · 37,317 cycles

BS 783 FRAME HAS DOUBLE DRILLED HOLE AT FLANGE 3" ABOVE STRINGER 17R. REMOVED DAMAGED HOLE AND INSTALLED FASTENER IAW EO 7-5310-7-3367 PT 4 AND SRM 51-30-2.

Part: SKIN — GOUGED (LT WING TE FLAP) · airframe 52,524 hrs · 37,317 cycles

LEFT WING, INBD FLAP, FORE FLAP HAS AREA AT MOST OUTBD L/E GOUGED. REMOVED PREVIOUS REPAIR FROM LT INBD FOREFLAP IAW SRM REV 103, 51-30-2. FABRICATED NEW REPAIR IAW SRM 57-50-4, FIG 4 AND 57-50-2, FIG 3 INSTALLED DOUBLER IAW SRM 51-30-2 AND 57-50-4, FIG 4 AND EA 7-5750-123594.

Part: SKIN — DAMAGED (NR 3 NACELLE) · airframe 52,524 hrs · 37,317 cycles

NR 3 ENGINE NOSE COWL O/B T/E SKIN DAMAGED AT 4:30 POAITION. REMOVED DAMAGE, FABRICATED FILLER AND DOUBLER, AND INSTALLED REPAIR PARTS IAW SRM 51-10-1, 51-30-2, 54-30-3 FIG 8.

Part: BEAM — DAMAGED (1183 BULKHEAD) · airframe 52,524 hrs · 37,317 cycles

BS 1183 BULKHEAD LBL 20 BEAM AND WEB HAVE CLOSE ON CENTER SPACING BETWEEN FASTENERS. ACCOMPLISHED EA 7-5310-123586.

Part: ACTUATOR — MALFUNCTIONED (NR 4 SLAT) · airframe 52,517 hrs · 37,310 cycles

DURING CLIMBOUT NR 4 LT L/E SLAT DID NOT RETRACT. RAN QRH. RETURNED TO DEPARTURE. JUMPER INSTALLED ON NR 4 SLAT ACTUATOR. DO TO IND OF EXTEND POSITION. MM 27-82-000-1-0, INSTALLED NR 4 L/E SLAT EXTEND SWITCH JUMPER. SYS GROUND CHECKS NORMAL. JUMPER INSTALLED TRANSFERED TO OIL NR 471234. R & R NR 4 SLAT ACTUATOR IAW MM 27-81-032-4. REMOVED JUMPER IAW BSWPM 20-60-06. R& R NR4 SLAT POSITION EXTEND SWITCH IAW MM 27-82-011-4. OPS & LEAK CHECKED NORMAL IAW MM 27-81-000-5 AND 27-82-011-4.

Part: ACTUATOR — FAILED (NR 7 SLAT) · airframe 51,225 hrs · 36,241 cycles

NR 7 LEADING EDGE DEVICE FAILED TO RETRACT AFTER TAKEOFF. WHEN GOING FROM 2 DEG TO 0 DEG. RAN QRH LED DID NOT RETRACT FLIGHT CONTROL INPUTS INDICATE THE LEADING EDGE DEVICE WAS ACTUALLY EXTENDED. R & R NR 7 SLAT ACTUATOR IAW MM 27-81-032-4. OPS CK AND LEAK CKS NML.

Part: ACTUATOR — FAILED (NR 7 SLAT) · airframe 51,225 hrs · 36,241 cycles

NR 7 LED FAILED TO RETRACT AFTER TAKEOFF. WHEN GOING FROM 2 DEG TO 0 DEG, RAN QRH LED DID NOT RETRACT FLIGHT CONTROLS INPUTS INDICATE THE LED WAS ACTUALLY EXTENDED. REMOVED AND REPLACED NR 7 SLAT ACTUATOR PER M/M 27-81-032-4. OPS CKS AND LEAK CKS NML.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 51,186 hrs · 36,210 cycles

CORROSION SEAT TRACK STA. 950 LBL 45. REMOVED SEAT TRACK IAW SRM 51-30-2. FABRICATED SEAT TRACK AND 2 SPLICE ANGLES IAW SRM 53-10-5 FIG 1 AND 51-30-8. TREATED & PRIMED REPAIR PARTS IAW SRM 51-10-2. INSTALLED TRACK & REPAIR PARTS IAW SRM 53-10-5 & 51-30-5, AND 51-30-8. FABRICATED, DRILLED, DEBURRED SEAT TRACK & SPLICE ANGLES.

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 51,186 hrs · 36,210 cycles

CORROSION ON SEAT TRACK BS 950 LBL 24. REMOVED SEAT TRACK IAW SRM 51-30-2. FABRICATED, LOCATED, DRILLED, AND DEBURRED SEAT TRACK IAW SRM 53-10-5 AND 51-30-5 AND 51-30-8. TREATED & PRIMED TRACK & REPAIR PARTS IAW SRM 51-10-2. INSTALLED SEAT TRACK & REPAIR PARTS IAW SRM 51-30-2.

Part: SKIN — DENTED (ZONE 100) · airframe 51,186 hrs · 36,210 cycles

SKIN DENTES AND HOLES BS 620 TO 635 S25R.

Part: SEAT TRACK — MISALIGNED (BS 720F-750) · airframe 51,186 hrs · 36,210 cycles

STA 720F LBL 45 HAS HOLE FOR FLOORBOARD DRILLED ON EXISTING SEAT TRACK SPLICE ON A FASTENER. REMOVED SEAT TRACK AND SPLICE BS 720F - 750 LBL 45 IAW SRM 51-30-2. LOCATED, DRILLED, DEBURRED NEW SEAT TRACK SECTION IAW SRM 53-10-5. FABRICATED SPLICE ANGLE IAW SRM 53-10-2 FIG 7, AND 51-30-5, AND 51-30-8. TREATED AND PRIMED IAW SRM 51-10-2. INSTALLED, IAW SRM 51-30-2.

Part: CABIN PRESSURE — MALFUNCTIONED · airframe 50,980 hrs · 36,053 cycles

FL270 AND .80 MACH, UPON COMP OF THROTTLE ALIGN CK AND RECYCLING OF NR 1 AND NR 2 ENG BLEED S CABIN PRESS BEGAN TO CLIMB AT 500-1000' FPM. COULD NOT STOP CLIMB AND APPROACHING 10K CAB PRESS WE WERE FORCED TO DESCEND TO 10K' AND DIVERT INTO DSM. IAW QRH ATTEMPTED TO STAB CABIN PRESS IN BOTH STANDBY AND MANUAL MODES

Part: SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 50,810 hrs · 35,912 cycles

LOWER AFT CARGO PIT, LT SIDE EDGE SUPPORT FROM FS 950F TO FS 1030 HAS AREAS OF SURFACE CORROSION AS MARKED REMOVED CORROSION. ORIGINAL THICKNESS .056", .017 INCH REMAINING, .036 INCH MAT REMOVED. OUT OF LIMITS. REPAIR DOUBLER FABRICATED, TREATED AND PRIMED AND INSTALLED AT BS 991 REF SRM 51-10-1 FIG 7, 53-10-2 PG 45-46, 51-40-2, FIG 1 PG 1, 2, 3, 6, AMM 51-20-021-7 PG 1-7, 51-20-031-7 PG 1-7 THIS IS CLASSIFIED AS A MINOR REPAIR.

Part: SKIN — CHAFED (BS 1100-1175) · airframe 49,405 hrs · 34,789 cycles

FOUND RIGHT HAND LOWER FUSELAGE OUTER SKIN HAVE MULTIPLE CHAFED DAMAGE APPROX BETWEEN STA 1100 TO STA 1175, AREA BETWEEN STA 1100 TO STA 1110 AND STA 1175 FOUND OUT OF LIMITS. CUT OUT DAMAGE, FABRICATED REPAIR PARTS IAW SRM 53-30-3 FIG 1 AND REINSTALLED ALL REPAIR PARTS IAW SRM 53-30-1, REPAIR IS CLASSIFIED AS MAJOR PER FEDEX GMM 6-2-100.

Part: SKIN — DAMAGED (BS 1050-1070) · airframe 49,405 hrs · 34,789 cycles

FOUND LOWER CARGO COMPARTMENT EXTERIOR SKIN SURFACE IS DAMAGED BETWEEN STA 1050 TO STA 1070, STR 25R. REMOVED DAMAGE PARTS IAW SRM 53-30-3, FABRICATED REPAIR PARTS IAW SRM 53-30-2 FIG 4 AND INSTALLED DOUBLER REPAIR PARTS IAW SRM 51-30-2 AND SRM 53-30-3 FIG 3 AND REPAIR IS CLASSIFED AS MAJOR PER FEDEX GMM 6-2-100.

Part: REPAIR — UNKNOWN · airframe 49,405 hrs · 34,789 cycles

FOUND PREVIOUSLY REPAIR INSTALLED AT STA 1140 STR 19L WAS DETERMINED TO BE ACCOMPLISHED IAW SRM 51-30-3 FIG 5 BASED ON AN EXTERNAL VISUAL EVALUATION CONSISTS OF LOCATION, SHAPE, SIZE, MATERIAL TYPE AND THICKNESS, FASTENER SPACING AND NUMBERS, GENERAL WORKMANSHIP AND REPAIR IS CLASSIFIED AS MAJOR PER FEDEX GMM 6-2-100.

Part: REPAIR — MISINSTALLED (BS 1140) · airframe 49,405 hrs · 34,789 cycles

FUSELAGE SKIN REPAIR AT FS 1140 & STR 19L DOES NOT COMPLY WITH SRM REPAIR. REMOVED AND REPLACED EXISTING REPAIR DOUBLERS IAW SRM 53-30-3 FIG 5.

Part: REPAIR — UNKNOWN (FUSELAGE) · airframe 49,405 hrs · 34,789 cycles

FOUND REPAIR LOCATED AT STN 1150 STR 21R REPAIR REQUIRES EVALUATION FOR MAJOR /MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR CLASSIFIED AS MAJOR AND WAS ACCOMPLISHED USING FAA APPROVED DATA.

Part: REPAIR — UNKNOWN · airframe 49,405 hrs · 34,789 cycles

FOUND REPAIR LOCATED AT 720D AND STR 25L REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR WAS DETERMINED TO MAJOR AND WAS ACCOMPLISHED USING FAA APPROVED DATA.

Part: REPAIR — UNKNOWN · airframe 49,405 hrs · 34,789 cycles

FOUND REPAIR LOCATED AT STA 720E (WING ROOT) AND STR 19L REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR WAS DETERMINED TO BE MAJOR, AND WAS ACCOMPLISHED USING FAA APPROVED DATA.

Part: REPAIR — UNKNOWN · airframe 49,405 hrs · 34,789 cycles

FOUND PREVIOUSLY REPAIR INSTALLED AT STA 1090 STR 26L WAS ACCOMPLISHED IAW SRM 53-30-3 FIG 3 BASED ON AN EXTERNAL VISUAL EVALUATION CONSISTS OF LOCATION, SHAPE, SIZE, FASTENER SPACING AND NUMBERS, MATERIAL TYPE AND THICKNESS. GENERAL WORKMANSHIP AND REPAIR IS CLASSIFIED AS MAJOR PER FEDEX GMM 6-2-100.

Part: REPAIR — UNKNOWN · airframe 49,405 hrs · 34,789 cycles

FOUND PREVIOUSLY REPAIR INSTALLED AT STA 415 STR 17R WAS ACCOMPLISHED IAW EO 7- 5313-7-2304 PT2 SECT A, BASED ON AN EXTERNAL VISUAL EVALUATION CONSISTING OF LOCATION, SIZE, SHAPE, FASTENER SPACING AND NUMBERS, MATERIAL TYPE AND THICKNESS, GENERAL WORKMANSHIP, REPAIR IS CLASSIFIED AS MAJOR PER FEDEX GMM 6-2-100.

Part: REPAIR — UNKNOWN · airframe 49,405 hrs · 34,789 cycles

FOUND PREVIOUSLY REPAIR INSTALLED AT STA 1050 STR 28R WAS ACCOMPLISHED IAW SRM 53-30-3 FIG 3, BASED ON AN EXTERNAL VISUAL EVALUATION, CONSISTS OF LOCATION, SIZE, SHAPE, FASTENER SPACING AND NUMBERS, MATERIAL TYPE AND THICKNESS, GENERAL WORKMANSHIP. REPAIR IS CLASSIFIED AS MAJOR PER FEDEX GMM 6-2-100.

Part: REPAIR — UNKNOWN · airframe 49,405 hrs · 34,789 cycles

FOUND PREVIOUSLY REPAIR INSTALLED AT STA 1100 STR 23R WAS ACCOMPLISHED IAW SRM 53-30-3 FIG 1, BASED ON AN EXTERNAL VISUAL EVALUATION CONSISTS OF LOCATION, SIZE, SHAPE, FASTENER SPACING AND NUMBERS, MATERIAL TYPE AND THICKNESS, GENERAL WORKMANSHIP. REPAIR IS CLASSIFIED AS MAJOR PER FEDEX GMM 6-2-100.

Part: REPAIR — UNKNOWN · airframe 49,405 hrs · 34,789 cycles

FOUND PREVIOUSLY REPAIR INSTALLED AT STA 1140 STR 29L WAS ACCOMPLISHED IAW SRM 53-30-3 FIG 3 BASED ON AN EXTERNAL VISUAL EVALUATION, CONSISTS OF LOCATION, SHAPE, SIZE, FASTENER SPACING AND NUMBERS, MATERIAL TYPE AND THICKNESS. REPAIR IS CLASSIFED AS MAJOR PER FEDEX GMM 6-2-100.

Part: SKIN — DENTED (FUSELAGE) · airframe 49,405 hrs · 34,789 cycles

FORWARD LEFT FUSELAGE HAS DENT OUTER SKIN APPROX STA 196 STR 25L.

Part: BOLT — MISSING (TE FLAPS) · airframe 47,332 hrs · 33,029 cycles

AFTER SEVERAL SUCCESSFUL FLAP RETRACTION CYCLES, OUTBOARD FLAPS STOPPED AT 5 DEG & STAYED THERE WHILE FLAPS 2 WERE COMMANDED, ALTERNATE FLAP SELECTION WAS UNABLE TO MOVE THEM FURTHER UP OR DOWN. USE OF NORMAL HYD MOTOR WAS ABLE TO DRIVE OUTBOARDS DOWN. BUT NO SECOND ATTEMPT WAS MADE TO RETRACT THEM. TROUBLESHOT O/B FLAP DRIVE SYS IAW FEDEX MM, FOUND BOLT MISS NR 7 FLP CARRIAGE LOWER ACCESS CVR I/B SIDE. SPCT MISSING BOLT OF BIND BETWEEN MIDFLAP/FLAP TRCK CAUSE OB FLAP SYS TEMPORARILY INACTIVE. REPLACED MISSING BOLT. INSPECTED OB FLAP SYS/SAFETYS, NO ISSUES. OP CHECK FLAP DRIVE SYS TO FULL EXTREMES 50 TIMES. NO PROBLEMS.

Part: SKIN — GOUGED (FUSELAGE) · airframe 47,331 hrs · 33,028 cycles

RT FUSELAGE SKIN GOUGE STRINGER 19R LAP BS 720D 14. REPAIRED RT FUSELAGE SKIN GOUGE PER SRM 53-30-3, AND SR DRAWING SR 27-57-056.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,331 hrs · 33,028 cycles

CORROSION (C53-111-01(3)) ON BS 1148 FLOORBEAM LOWER CHORD BL 0, WL 200. *S/D* CORROSION ON FLOORBEAM AT BS 1148 LOWER CHORD BL 0 WL 200 WAS FOUND TO BE OUT OF LIMITS. REPAIRED FLOORBEAM PER FED EX EA 7-5310-55019.

Part: STRINGER — CRACKED (LT WING) · airframe 47,331 hrs · 33,028 cycles

N01203 LT WING STA 656.5, STRINGER 12 UPPER TAB CRACKED (VENT BOX) REPAIRED IAW EA 7-5710-55011.

Part: STRINGER — CRACKED (LT WING) · airframe 47,331 hrs · 33,028 cycles

LT WING STR 10 UPPER CRACKED AT TAB WING STA 656.50 ** SD ** COMING

Part: VENT — CRACKED (LT WING) · airframe 47,331 hrs · 33,028 cycles

LT WING FWD VENT BOX TAB CRACKED AT STA. 656.60. REPAIRED IAW EA 7-5710-55011.

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,331 hrs · 33,028 cycles

LT 930 FRAME CRACKED AT LOWER SHEAR TIE FASTENER HOLE ABOVE STR 14. REPAIRED CRACKED FRAME AT BS 930 STR 14 LT, PER SRM 53-10-4, EA 7-5310-55032.

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,331 hrs · 33,028 cycles

RT 930 FRAME CRACKED AT LWR SHEAR TIE FASTENER HOLE ABOVE STR 14. REPAIRED CRACKED FRAME AT BS 930 STR 14 RT, PER SRM 53-10-4, EA 7-5310-55032.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,331 hrs · 33,028 cycles

N01643, CORROSION ON UPPER SURFACE OF LOWER SECTION OF FLOORBEAM BS 1070 LBL 7 WL 200. ** SD ** COMING

Part: FRAME — DAMAGED (FUSELAGE) · airframe 47,331 hrs · 33,028 cycles

N01698, BS 950F FRAME DAMAGED BETWEEN STR 25L AND 27L, REPAIR AND FASTENERS NOT INSTALLED WITH SEALANT, MECHANICAL DAMAGE ON FAIL SAFE CHORD AT TOP HORZ FASTENER, LARGE GAP BETWEEN DOUBLER AND FRAME, 1 FASTENER TO SHORT WITH GAPPED COLLAR, 1 FASTENER WITH NUT AND WASHER ON EDGE OF BRACKET. ** SD ** COMING

Part: STRUCTURE — GOUGED (NLG WW) · airframe 47,331 hrs · 33,028 cycles

NLG WHEEL WELL HAS NUMEROUS GOUGES AROUND RT AFT PRESSURE PANEL CUTOUT. REPAIRED AS PER SRM 51-40-2.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 47,331 hrs · 33,028 cycles

STRINGER CLIP 5 RT CRACKED AT BS 720C. REMOVED AND REPLACED STRINGER CLIP AT BS 720C, STR 5R PER SRM 51-30-2, 51-30-5.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,331 hrs · 33,028 cycles

CORROSION ON FLOORBEAM, UPR & LWR SURFACE AROUND FASTENER HOLES AND TOP, BS 344, LBL 45 TO RBL 13, WL 208.

Part: FRAME — DENTED (FUSELAGE) · airframe 47,331 hrs · 33,028 cycles

DENT IN FRAME BS 1030 AT STR 26L. *S/D* DAMAGE ON FRAME AT BS 1030 AT STR 26L FOUND TO BE OUT OF LIMITS. REMOVED DAMAGE AND INSTALLED REPAIR ANGLE ON FRAME AT BS 1030, STR 26L IAW SRM 51-40-3.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 47,331 hrs · 33,028 cycles

STRINGER CLIP 7R CRACKED AT B.S 720B. REPLACED STR CLIP AT BS 720B STR 7R, PER SRM 51-30-2, 51-30-5.

Part: FRAME — DENTED (FUSELAGE) · airframe 47,331 hrs · 33,028 cycles

DENT IN FRAME BS 600, ABOVE STR 25L. REPAIRED DENT IN FRAME BS 600 ABOVE STR 25L PER FED-EX E.A. 7-5310-70526A.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,331 hrs · 33,028 cycles

CORROSION ON BS 1130 FLOORBEAM LOWER SECTION LBL 2 - LBL 40 WL 200. REPAIRED FLOORBEAM BS 1130 LOWER CHORD, LBL 65 TO RBL 65 PER FED EX EA 7-5310- 55008.

Part: FRAME — DENTED (FUSELAGE) · airframe 47,331 hrs · 33,028 cycles

AFT CARGO BAY, FRAME DENTED BS 1110 STR 26R. DAMAGE ON FRAME AT BS 1110, STR 26R (DENT) FOUND TO BE OUT OF LIMITS. REMOVED DAMAGE ON FRAME AND INSTALLED REPAIR ANGLE AT BS 1110, STR 26R IAW SRM 51-40-3 AND EA 7-5310-54986.

Part: STRINGER CLIP — CRACKED (BS 440) · airframe 47,331 hrs · 33,028 cycles

BS 440 STR 6 LT STR CLIP CRACKED. REMOVED DAMAGED STR CLIP AT BS 440, STR 6L. DRILLED NEW STR CLIP AND INSTALLED IAW SRM 51-30-2, 51-30-5.

Part: FRAME — DENTED (FUSELAGE) · airframe 47,331 hrs · 33,028 cycles

DENT IN FRAME BS 660, ABOVE STR 25L. *S/D* REPAIRED DENT IN FRAME BS 660 ABOVE STR 25L PER FED EX EA 7-5310-70526A AND APPLIED BMS 3-23 PER FED EX JOB CARD 71C209-01.

Part: FRAME — DENTED (FUSELAGE) · airframe 47,331 hrs · 33,028 cycles

AFT CARGO BAY, FRAME DENTED BS 1050 STR 26R. *S/D* DAMAGE ON FRAME AT BS 1050, STR 26R (DENT) FOUND TO BE OUT OF LIMITS. REMOVED DAMAGE ON FRAME AND INSTALLED REPAIR ANGLE AT BS 1050, STR 26R IAW SRM 51-40-3 AND EA 7-5310-54986.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 47,331 hrs · 33,028 cycles

BS 950F FRAME DAMAGED BETWEEN STR 25L AND 27L. *S/D* DAMAGE ON FRAME AT BS 950F BETWEEN 25L & 27L FOUND TO BE OUT OF LIMITS. REMOVED DAMAGE ON FRAME AND INSTALLED REPAIR ANGLE AT BS 950F FRAME BETWEEN STR 25L AND 27L IAW SRM 51-40-3.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 47,331 hrs · 33,028 cycles

BS 440 STR 3 LT STRINGER CLIP CRACKED. REMOVED AND REPLACED STR CLIP AT BS 440 STR 3 LT PER SRM 51-30-2, 51-30-5.

Part: SKIN — DENTED (FUSELAGE) · airframe 47,331 hrs · 33,028 cycles

FUSELAGE SKIN DENTED AT APPROX STA 1130 STR 18R.

Part: FRAME — DENTED (FUSELAGE) · airframe 47,331 hrs · 33,028 cycles

2 DENTS IN 3 INCH AREA, ON FWD CARGO FRAME, BS 500 BETWEEN STR 23R AND 24 R. **SD** COMING

Part: FAILSAFE — FAILED (FRAME) · airframe 47,331 hrs · 33,028 cycles

FRAME FAIL SAFE CRACKED AT BS 890 STR 14R ATTACH POINT. **SD** COMING.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 47,331 hrs · 33,028 cycles

CORROSION ON SHEAR TIE BETWEEN STR 26L AND 27L, BS 1050. REMOVED AND REPLACED SHEAR TIE.

Part: FRAME — DENTED (FUSELAGE) · airframe 47,331 hrs · 33,028 cycles

N00564 DENT IN FWD CARGO FRAME, BS 500 BETWEEN STR 23L AND 24L. **SD** COMING

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 47,331 hrs · 33,028 cycles

STRINGER CLIP 8R CRACKED AT BS 720D. REMOVED AND REPLACED CLIP IAW SRM 51-30-2, 51-30-5.

Part: FLOORBEAM — GOUGED (FUSELAGE) · airframe 47,331 hrs · 33,028 cycles

CORROSION C53-224-01 AND GOUGED METAL AT FASTENER HOLE LOCATIONS ON FLOORBEAM AT BS 950F, LBL 42-RBL 38. REPAIRED FLOORBEAM IAW SRM 53-10-8 FIG 8.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 47,331 hrs · 33,028 cycles

CORROSION ON FLOORBEAM AT BS 1070, RBL 10.5, WL 208. **SD** COMING

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,331 hrs · 33,028 cycles

CORROSION ON SHEAR TIE AFT SIDE OF FRAME BS 1150 BETWEEN STR 26L AND 27L. REPAIRED SHEAR TIE IAW SRM 53-10-1, 53-10-4.

Part: FLOORBEAM — DAMAGED (FUSELAGE) · airframe 47,331 hrs · 33,028 cycles

LWR SURFACE, FWD SIDE OF TOP FLANGE OF FLOOR BEAM BS 440, LBL 35, WL 208 HAS TOOLING DAMAGE. REPAIRED FLOORBEAM IAW SRM 53-10-8 FIG 8.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 47,331 hrs · 33,028 cycles

CORROSION ON FLOORBEAM AT BS 1050, LBL 35, WL 208. **SD** COMING

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 47,331 hrs · 33,028 cycles

BS 440, STR 5 LT STR CLIP CRACKED. REMOVED DAMAGED STR CLIP AT BS 440 STR 5 LT DRILLED NEW STR CLIP AND INSTALLED IAW SRM 51-30-2, 51-30-5.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 47,331 hrs · 33,028 cycles

CORROSION ON FLOOR BEAM UPR SURFACE BS 328, LBL 29, WL 208. **SD** COMING

Part: FRAME — DENTED (FUSELAGE) · airframe 47,331 hrs · 33,028 cycles

N00560 2 DENTS IN 3.5 INCHES AREA, ON FWD CARGO FRAME BS 560 AT STR 24L. **SD** COMING

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,331 hrs · 33,028 cycles

CRACKED FRAME AT BS 380, 3 INCHES BELOW STR. 7R FWD UPPER END OF DOOR CUTOUT. ** SD ** COMING

Part: SKIN — CHAFED (FUSELAGE) · airframe 47,331 hrs · 33,028 cycles

FUSELAGE SKIN EXTERNAL REPAIR DOUBLER HAS CHAFE DAMAGE, BS 720D 10 INCHES AT STR 19L. FABRICATED REPAIR DOUBLER IAW SRM 53-30-3 FIG 5.

Part: FAILSAFE — CRACKED (FRAME) · airframe 47,331 hrs · 33,028 cycles

N00917 FRAME FAIL SAFE CHORD CRACKED BS 804 AT STR 14L. **SD** COMING

Part: FRAME — DENTED (FUSELAGE) · airframe 47,331 hrs · 33,028 cycles

DENT IN FWD CARGO FRAME, BS 520 BETWEEN STR 22R AND 23R. **SD** COMING

Part: STRINGER — CORRODED (FUSELAGE) · airframe 47,331 hrs · 33,028 cycles

CORROSION INSIDE STRINGER CHANNEL BS 1090, STR 27 LT. **SD** COMING

Part: FRAME — DENTED (FUSELAGE) · airframe 47,331 hrs · 33,028 cycles

N00561 DENT IN FWD CARGO FRAME BS 660 AT STR 22R. **SD** COMING

Part: SKIN — CORRODED (FUSELAGE) · airframe 47,331 hrs · 33,028 cycles

CORROSION ON SKIN BS 684 BETWEEN STRINGER 27 RT AND STR 28 RT. REMOVED CORROSION FOUND TO BE OUT OF LIMITS FABRICATED REPAIR PLATE IAW SRM 53-30-3 FIG 3A.

Part: STRINGER CLIP — CRACKED (440) · airframe 47,331 hrs · 33,028 cycles

BS 440, STR 7 LT STR CLIP CRACKED. REMOVED DAMAGED STR CLIP AT BS 440 STR 7L DRILLED NEW STR CLIP AND INSTALLED IAW SRM 51-30-2, 51-30-5.

Part: FLAP — MISSING (T/E FLAP) · airframe 46,714 hrs · 32,540 cycles

FOUND APPROXIMATELY 5.5 FT INBOARD SECTION OF THE LEFT FORE FLAP MISSING ON POST FLIGHT INSPECTION. REMOVED LEFT INBOARD FORE FLAP ASSEMBLY IAW MM. INSTALLED LEFT INBOARD FORE FLAP IAW M/M, SYSTEMS OPS, CHECK NORMAL.

Part: SKIN — CORRODED (FUSELAGE)

BULGING SKIN AROUND FASTENERS BS 352, RBL 13, WL 148. *S/D* REMOVED, REPLACED AND FAB CHORD PER IAW FEDEX SRM 51-30-21, 51-10-2, 51-30-5 & 51-10-6.

Part: DOUBLER — CORRODED (FUSELAGE)

BULGING SKIN AT AFT LAV PAN UPPER FWD CORNER AND AFT LOWER CORNER. *S/D* REMOVED, REPLACED AND FAB NEW DOUBLER AND AFT LAV PAN PER IAW FEDEX SRM 51-30-5, 53-10-1 AND 51-20-151.

Part: SKIN — DENTED (FUSELAGE)

DENT IN SKIN BETWEEN BS 720A AND 720B BS 17 RT. *S/D* REMOVED, REPLACED AND FAB DOUBLER AND FILLER PER IAW FEDEX SRM 53-30-3 FIG 3.

Part: HOSE — LEAKED (LT MLG)

99-110 - UPON RAISING GEAR HANDLE, A SYS HYD PRESSURE AND QUANTITY BOTH WENT TO ZERO. REMOVED AND REPLACED LEFT MAIN LAND GEAR ACTUATOR HOSE. LEAK AND OPER CK GOOD PER MM 29-11-000-1.

Part: ANTI-ICE DUCT — RUPTURED (BS 1203-1223)

NR 1 ENG ANTI-ICE VALVE FELL OPEN AND CAUSE NUMEROUS ALERTS ON STBY HYD SYS AND ELEV FEEL DIFFERENTIAL LIGHT. ALSO, AFT AIRSTAIRS LIGHT ON WITH LWR AFT BODY OVERHEAT LIGHT AND DUCT OVERHEAT LIGHT ON. UNABLE TO EXTINGUISH ANY LIGHTS USING PUB PROC. EMERGENCY LANDING DUSSELDORF. FND NR 1 ENG WING THERMAL ANTI-ICE DUCT RUPTURED BETWEEN STA 1203 AND 1223. ALSO, FND INSULATION OF WIRE BUNDLES W2338 AND W344 MELTED AT 3 FT LENGTH. SPLICED WIRE PER ENG AUTHORIZATION 7-2400-36718.

Part: BYPASS SWITCH — DISCONNECTED (NR 2 ENG OIL)

97-0156 - AFTER T/O CRUISE FROM TLV NR 2 ENGINE LOW OIL PRESSURE OR FILTER BYPASS LIGHT ILLUMINATED (1012Z - 0+40 EN ROUTE). ACCOMPLISHED CHECKLIST OIL PRESS PLUS QTY OK, BUT LIGHT STAYED ON PER C/L SHUTDOWN NR 2 ENG (1023Z-0+50). RETURN TLV. A/C RELEASED FOR SERV PER MEL/COL: 79-2. MAIN OIL FILTER CHECKED CLEAN, FILTER REPLACED, LOW OIL PRESS SWITCH REPLACED. BYPASS SWITCH DISCONNECTED AND SECURED. RUN UP CHECKED FOR OPERATION AND LEAKS OK.

Part: WEB — CORRODED (BS 950)

FOUND CORROSION UNDER LOWER DOOR STOP ON THE AFT CARGO DOOR FWD FRAME BS 950E WL 155. REPAIRED CORRODED FRAME AT BS 950E WL 155 PER FEDEX EA 7-5310-28290.

Part: SEAL DEPRESSOR — CRACKED (NR 1 CARGO DOOR)

0379 -012C, NR 1 CARGO DOOR LWR CENTER SEAL DEPRESSOR IS CRACKED AND DENTED. REMOVED AND REPLACED LWR CENTER SEAL DEPRESSOR ON NR 1 CARGO DOOR.

Part: SEAL DEPRESSOR — CRACKED (NR 1 CARGO DOOR)

0378 -011C, NR 1 CARGO DOOR LWR FWD CORNER SEAL DEPRESSOR IS CRACKED AND DENTED. REMOVED AND REPLACED LWR SEAL DEPRESSOR ON NR 1 CARGO DOOR.

Part: STRINGER — CRACKED (BS 960.5)

CORROSION (C53-224-01, -3) AND TOOL MARKS BS 970. REMOVED DAMAGED STR BS 960.5, FABRICATED REPAIR PARTS AND INSTALLED PER FEDEX SRM 727 53-10-3 FIG 3.

Part: SEAL DEPRESSOR — CRACKED (NR 1 CARGO DOOR)

0370 -010C, NR 1 CARGO DOOR LWR AFT CORNER SEAL DEPRESSOR IS CRACKED AND DENTED. REMOVED AND REPLACED AFT SEAL DEPRESSOR ON NR 1 CARGO DOOR.

Part: SKIN — GOUGED (BS 378)

GOUGE IN SKIN AT BS 378 BETWEEN STRS 17-18L, LBL 70. CUT OUT DAMAGED SKIN AND INSTALLED DOUBLER PER SRM 53-30-3 FIG 1.

Part: DOOR FRAME — CORROSION (BS 950)

NR0408 AND 008, FOUND CORROSION UNDER LOWER DOOR STOP ON THE AFT CARGO DOOR FWD FRAME, BS 950E WL 155. *S/D* REPAIRED CORRODED FRAME AT BS 950E, WL 155 PER EA 7-5310-28290.

Part: SKIN — CANNED (BS 490)

SKIN IS OIL CANNED AT BS 490 BETWEEN STR 20 TO 21R RBL 65. DAMAGED AREA CUT OUT, FABRICATED DOUBLER FROM 2024 T-3.063, INSTALLED REPAIR PARTS PER FEDEX SRM 53-30-3 FIG 1.

Part: CLIP — CRACKED (BS 580)

CRACKED STRINGER CLIP BS 580 STR 27L. REMOVED CLIP, FABRICATED NEW CLIP AND INSTALLED.

Part: WEB — CRACKED (BS 1120-1125)

WEB IS DAMAGED FROM BS 1120 TO 1125 BL 0 WL 201. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PARTS ON WEB AT BS 1120 TO 1125 BL 0 WL 201 PER FEDEX SRM 51-40-2.

Part: CLIP — CRACKED (BS 600)

CRACKED STRINGER CLIP AT BS 600 STR 27L. REMOVED CLIP, FABRICATED NEW CLIP AND INSTALLED.

Part: WEB — CORROSION (NR 2 CARGO DOOR)

NR0335 AND 006, ON NR 2 CARGO DOOR AFT SUPPORT WEB FRAME, CORROSION EXITS I/B OF FRAME WEB C17 LOWER L-BRACKET, C/T LOWER DOOR GUIDE ROLLER. CORROSION ON NR 2 CARGO DOOR I/B OF FRAME WEB FOUND TO BE OUT OF LIMITS. REPAIRED PER SRM 51-40-3 FIG 1 ON AFT SUPPORT WEB FRAME.

Part: WEB — CRACKED (BS 1241)

PUNCTURE/CRACK IN TORQUE BOX WEB BS 1241 RBL 20 WL 178. REPAIRED DAMAGE IN TORQUE BOX WEB AT BS 1241 RBL 208 PER FEDEX SRM 51-40-2.

Part: FLAP — CORRODED (NR 5 LE FLAP)

CORROSION UNDER NR 5 K-FLAP O/B LOWER BONDING JUMPER UPPER ATTACH POINT WENT BEYOND LIMITS. REMOVED DAMAGED SECTION, FABRICATED AND INSTALLED REPAIR PER FEDEX SRM 57-50-3.

Part: PACK — MALFUNCTIONED (RIGHT)

ON CLIMBOUT, FLT ENG NOTICED FLUX OF 30 TO 40 DEGREES IN R/PACK TEMP AND ABNORMAL LOW R/BLEED PRESS. ALMOST SIMULTANEOUSLY ENG NR 3 OVERHEAT LIGHT ON FLT ENG'S PANEL ILLUMINATED. R/PACK WAS SHUTDOWN AND R/BLEED CLOSED. THE NR 3 ENG STRUT OVERHEAT LIGHT WENT OUT IMMEDIATELY. RAN ALL 3 ENG AT 80 PERCENT AND BOTH PACKS. CND MALFUNCTION, OK FOR SERVICE.