N495FE

Part: CONTROL UNIT — FAILED (FIRE DETECTION) · airframe 39,930 hrs · 28,057 cycles

AT ALTITUDE, RECEIVED WHEELWELL LIGHT & BELL, PERFORMED PHASE 1, LOWERED GEAR & OPENED MAIN GEAR DOORS, LIGHT REMAINED ON, ON TEST, BELL DID NOT SOUND. AFTER ACFT PULL IN THE GATE, INSPECTED WHEEL WELL TIRES AND BRAKES NO DISCREPANCY FOUND. INSPECTED FIRE LOOP IN WW NO CHANGE. R & R FIRE DETECTION CONTROL UNIT IAW MM 26-12-001-1-0. LIGHT CK GOOD. OPS TEST SEVERAL TIME SYS CK GOOD. ACFT OK FOR FLT.

Part: CONTROLLER — MALFUNCTIONED (OVERHEAT SYSTEM) · airframe 39,928 hrs · 28,056 cycles

PRIOR TO TAKEOFF, WHEEL WELL FIRE LIGHT AND BELL CAME ON INTERMITTENTLY APPROX 5 TIMES. AFTER WHICH WHEEL WELL FIRE WARNING WOULD NOT TEST. CHECKED MLG WW WIRING & SENSING ELEMENTS IAW WDM 26-12-01 & MM 26-12-001, ALL CHECKED GOOD. POWER & GROUND TO FIRE & OVERHEAT CONTROLLER UNIT M113 ALSO CHECKED GOOD. R & R FIRE & OVERHEAT DETECTOR CONTROLLER UNIT M113 IAW MM 20-10-017-2. FIRE & OVERHEAT DET SYS CHECKED GOOD REF 26-12-001-5.

Part: FRAME — DAMAGED (BS 990 S26R) · airframe 39,677 hrs · 27,858 cycles

AFT PIT STA 990, STR 26R HAS (3) RIVETS GROUPED TOGETHER IN FRAME. REPAIRED AFT PIT BS990 STRINGER 26R FRAME WEB AND LOWER CHORD IAW EA 7-5310-153050.

Part: SKIN — GOUGED (BS 620-640) · airframe 39,677 hrs · 27,858 cycles

INNER SURROUND SKIN GOUGED NUMEROUS PLACES STA 620 - 640, S4-10L. REMOVED INNER SKIN IAW SRM 51-30-2. FABRICATED INNER SKIN IAW SRM 53-10-2, FIG 3A AND DWG 53FX1551. INSTALLED MCD AFT UPPER INNER SKIN IAW SRM 51-30-2.

Part: FLOORBEAM — CORRODED (BS 950) · corrosion level 2 · airframe 39,677 hrs · 27,858 cycles

MAIN CABIN, FLOORBEAM UPPER SURFACE HAS EXFOLIATION CORROSION AT BS 950, BTW LBL 24.75 AND LBL 45.50. REMOVED TEE SECTION OF FLOORBEAM IAW SRM 51-30-2. FABRICATED, LOCATED, AND DRILLED NEW TEE SECTION IAW SRM 51-30-5. INSTALLED TEE SECTION IAW SRM 51-30-2 AND 53-10-2, FIG 7.

Part: SEAT TRACK — CORRODED · corrosion level 2 · airframe 39,677 hrs · 27,858 cycles

CABIN SEAT TRACK AT BS 950 TO 950A, RBL 25 HAS CORRODED SPLICE. REMOVED CORRODED SEAT TRACK SPLICES IAW SRM 51-30-2, FABIRCATED 2 EA. NEW SPLICE ANGLES FROM BAC 1503-160122 DIM 15" X 2.5" EACH AND 1 SPLICE STRAP FROM 7075T6 0.0250 DIM 9" X 2" IAW SRM 53-10-5, FIG 1, TREATED AND PRIMED PARTS IAW SRM 51-10-2 AND INSTALLED NEW SEAT TRACK SPLICES AT CABIN SEAT TRACK IAW SRM 51-30-2.

Part: FRAME — CRACKED (BS 680 S24R) · airframe 39,677 hrs · 27,858 cycles

FWD LOWER CARGO COMPARTMENT BS 680 FRAME HAS A DENT AT STRINGER 24R REWORKED DENTED AREA AND FOUND CRACKED AND OUT OF LIMITS IAW SRM 53-10-1, FIGURE 1, CUTOUT DAMAGE ( 1.5" X 1") AND FABRICATED REPAIR ANGLE FROM 7075-0 0.063 DIM 12.2500" X 3" IAW SRM 51-40-3, FIG 1 & 53-10-2 FIG 3, TREATED AND PRIMED REPAIR ANGLE & AREA IAW SRM 51-10-2, INSTALLED REPAIR ANGLE AT FWD LOWER CARGO COMPARTMENT BS 680, FRAME, STRINGER 24R IAW SRM 51-30-2. REPAIR ACCOMPLISHED IAW EA 7-5310-136784RA.

Part: SKIN — DAMAGED (BS 480 S26L) · airframe 39,677 hrs · 27,858 cycles

3 HOLES AT STR 26L INBD SIDE, STA 480. REPAIRED FUSELAGE SKIN AT BS 480 STRINGER 26LEFT IAW EA 7-5330-136776

Part: ANGLE — CRACKED (NR 1 SLAT) · airframe 39,677 hrs · 27,858 cycles

LT WING NR 1 SLAT HAS CRACKED LOWER ANGLE AT INBD SIDE OF SLAT, OTBD UPPER STOP PAD. REMOVED NR 1 SLAT ANGLE AND FABRICATED NEW ANGLE AND SPLICE. IAW SRM 57-50-2 FIG 2 AND 51-40-4 FIG 1. INSTALLED NEW ANGLE AND SPLICE IAW SRM 51-30-2

Part: STRINGER — CORRODED (BS 450 S28R) · corrosion level 2 · airframe 39,677 hrs · 27,858 cycles

STRINGER 28R CORRODED JUST AFT OF E AND E DOOR STA 450. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW IAW SRM 53-10-1, FIG 1 & 51-10-6. REMOVED STRINGER SECTION BS 440 TO BS 469, STR 28R IAW SRM 51-30-2, FABRICATED NEW STRINGER SECTION FROM BAC 1498-138 7075T6, DIM 29" LONG IAW SRM 53-10-2, FIG 9 & 51-30-5, TREATED AND PRIMED NEW STRINGER IAW SRM 51-10-2, INSTALLED NEW STRINGER 28R BETWEEN BS 440-469 IAW SRM 51-30-2.

Part: FLOORBEAM — CORRODED (BS 620) · corrosion level 2 · airframe 39,677 hrs · 27,858 cycles

FLOORBEAM, BS 620, BL0 TO LBL 25 UPPER SURFACE HAS CORROSION. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 51-10-6 - FLOORBEAM BS 620 BL 0 - LBL 25. CUTOUT DAMAGE AREA FLOORBEAM IAW SRM 53-10-8 - FABRICATED REPAIR PARTS IAW SRM 53-10-8 FIG 3. TREATED & PRIMED IAW SRM 51-10-2 AND INSTALLED REPAIR PARTS IAW SRM 53-10-8 FIG 3.

Part: SHEAR TIE — CORRODED (BS 990 S28-30R) · corrosion level 2 · airframe 39,677 hrs · 27,858 cycles

AFT PIT STA 990, SHEAR TIE AT STR 30 T0 28R HAS LIGHT SURFACE CORROSION. CUTOUT DAMAGED AREA IAW SRM 51-40-3 FIG 1. FABRICATED REPAIR SHEAR TIE IAW SRM 53-10-4 FIG 11. INSTALLED SHEAR TIE REPAIR IAW SRM 51-30-2.

Part: FRAME — DENTED (BS 1030 S26R) · airframe 39,677 hrs · 27,858 cycles

RT SIDE OF FUSELAGE FRAME HAS A DENT AT BS 1030 ABOVE STR 26R. CUTOUT DAMAGED AREA AND FABRICATED REPAIR PARTS IAW SRM 51-40-3 FIG 1. INSTALLED REPAIR PARTS IAW SRM 51-30-2.

Part: SEAT TRACK — CORRODED (BS 480-680) · corrosion level 2 · airframe 39,677 hrs · 27,858 cycles

SEAT TRACK AT BS 480-680, LBL 45 HAS CORROSION. REMOVED SEAT TRACK BS 480 TO 690 LBL 45 IAW SRM, REV 103, 51-30-2. FABRICATED AND INSTALLED NEW SEAT TRACK AND SPLICES IAW SRM 51-30-2 AND 53-10-5 FIG 1.

Part: SEAT TRACK — CORRODED (BS 720F-740) · corrosion level 2 · airframe 39,677 hrs · 27,858 cycles

SEAT TRACK AT BS 720E-740 BL0 HAS CORROSION. REMOVED SEAT TRACK SECTION IAW SRM 51-30-2 REV 103, FABRICATED NEW SEAT TRACK IAW SRM 53-10-2 FIG7A, INSTALLED NEW SEAT TRACK IAW SRM 51-30-02

Part: SEAT TRACK — CORRODED (BS 950D-950F) · corrosion level 2 · airframe 39,677 hrs · 27,858 cycles

SEAT TRACK AT BL 0 LT FLANGE CORRODED BTWN BS 950D-950F. FOUND OUT OF LIMITS IAW SRM 53-10-1. REMOVED DAMAGED SEAT TRACK SECTION IAW SRM 51-30-2. FABRICATED AND INSTALLED NEW SEAT TRACK SECTION IAW SRM 53-10-2 AND SRM 51-30-2.

Part: SEAT TRACK — CORRODED (BS 720A-720B) · corrosion level 2 · airframe 39,677 hrs · 27,858 cycles

SEAT TRACK AT BS 720A-720B, RBL 45 HAS CORROSION. REMOVED SEAT TRACK SECTION IAW SRM 51-30-2 REV 103. FABRICATED NEW SEAT TRACK IAW SRM 53-10-5 FIG 1. INSTALLED SEAT TRACK SECTION IAW SRM 51-30-2

Part: SEAT TRACK — CORRODED (BS 480-690) · corrosion level 2 · airframe 39,677 hrs · 27,858 cycles

SEAT TRACK AT BS 480-690, LBL 25 HAS CORROSION. FOUND OUT OF LIMITS IAW SRM 53-10-1. REMOVED DAMAGED SEAT TRACK SECTION IAW SRM 51-30-2. FABRICATED AND INSTALLED NEW SEAT TRACK SECTION IAW SRM 53-10-5 FIG1 AND SRM 51-30-2.

Part: SEAT TRACK — CORRODED (BS 950F-970) · corrosion level 2 · airframe 39,677 hrs · 27,858 cycles

SEAT TRACK AT BL0 RT FLANGE CORRODED BETWEEN BS 950F-970. CORROSION OUT OF LIMITS IAW SRM 53-10-1. REMOVED DAMAGED SEAT TRACK SECTION IAW SRM 51-30-2. FABRICATED AND INSTALLED NEW SEAT TRACK SECTION IAW SRM 53-10-2 AND SRM 51-30-2.

Part: SEAT TRACK — CORRODED (BS 690-740) · corrosion level 2 · airframe 39,677 hrs · 27,858 cycles

SEAT TRACK AT BS 690 -740, LBL 25 HAS CORROSION. FOUND OUT OF LIMITS IAW SRM PF 53-30-1 FIG 3A. REMOVED SEAT TRACK SECTION, FABRICATED NEW SEAT TRACK SECTION FROM BAC1520-792 7178-T6511 DIM. 172" LONG IAW SRM 53-10-2 FIG 7. TREATED AND PRIMED NEW SEAT TRACK IAW SRM 51-10-2. INSTALLED NEW SEAT TRACK IAW SRM 51-30-2 REV 103.

Part: FLOORBEAM — DAMAGED (BS 520) · airframe 39,677 hrs · 27,858 cycles

UPON REMOVAL OF SEAT TRACK FOUND DOUBLE DRILLED HOLE AT MAIN CABIN FLOORBEAM BS 520, BL 0. CUT OUT DAMAGED AREA DIM 1" X 0.800" AND FABRICATED 2EA REPAIR ANGLES FROM 7075-O 0.090" DIM 15 1/8" X 3" AND 11 1/2" X 2 7/8" AND 1EA REPAIR FILLER FROM 7075-T6 0.125" DIM 1" X 0.800" IAW SRM 53-10-8 FIG 8, HEAT TREATED REPAIR ANGLES TO 7075-T6, TREATED AND PRIMED AND INSTALLED REPAIR PARTS IAW SRM 51-10-2, 51-30-2 AND 53-10-8 FIG 8 REV 103.

Part: SEAT TRACK — CORRODED (BS 600-700) · corrosion level 2 · airframe 39,677 hrs · 27,858 cycles

SEAT TRACK AT BS 600 -700 BL0 HAS CORROSION. CORROSION OUT OF LIMITS IAW SRM 53-10-1. REMOVED DAMAGED SEAT TRACK SECTION IAW SRM 51-30-2. FABRICATED AND INSTALLED NEW SEAT TRACK SECTION IAW SRM 53-10-2 AND SRM 51-30-2.

Part: FRAME — CORRODED (BS 1130 S17R) · corrosion level 2 · airframe 39,677 hrs · 27,858 cycles

FRAME CORRODED AT BS 1130 AT STR 17R. REMOVED CORROSION IAW SRM 51-10-6. FABRICATED REPAIR PLATE IAW SRM 51-40-3 FIG 1. INSTALLED REPAIR PLATE IAW SRM 51-30-2.

Part: SHEAR TIE — CORRODED (BS 950E S28-29L) · corrosion level 2 · airframe 39,677 hrs · 27,858 cycles

BS 950E SHEAR TIE CORRODED STRINGER 28L TO 29L. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 51-10-6 AND 53-10-1 FIG 1. REMOVED SHEAR TIE IAW SRM 51-30-2, FABRICATED NEW SHEAR TIE IAW SRM 53-10-4 FIG 11 AND 53-10-2 FIG 5. HEAT TREATED SHEAR TIE TO T6, LOCATED AND DRILLED IAW SRM 51-30-5 AND 53-10-4 FIG 11. TREATED PRIMED AND INSTALLED SHEAR TIE BS 950E STR 28L-29L IAW SRM 51-10-2 AND 51-30-2 REV 103.

Part: SEAT TRACK — CORRODED (BS 360-480) · corrosion level 2 · airframe 39,677 hrs · 27,858 cycles

SEAT TRACK AT BS 360-480, RBL 45 HAS CORROSION. CORROSION OUT OF LIMITS IAW SRM 53-10-1. REMOVED DAMAGED SEAT TRACK SECTION IAW SRM 51-30-2. FABRICATED AND INSTALLED NEW SEAT TRACK SECTION IAW SRM 53-10-2 AND SRM 51-30-2.

Part: SEAT TRACK — CORRODED (BS 360-480) · corrosion level 2 · airframe 39,677 hrs · 27,858 cycles

SEAT TRACK AT BS 360-480, LBL 45 HAS CORROSION. CORROSION OUT OF LIMITS IAW SRM 53-10-1. REMOVED DAMAGED SEAT TRACK SECTION IAW SRM 51-30-2. FABRICATED AND INSTALLED NEW SEAT TRACK SECTION IAW SRM 53-10-2 AND SRM 51-30-2.

Part: SKIN — GOUGED (BS 410) · airframe 39,677 hrs · 27,858 cycles

GOUGE LWR FUS. STA 410 BELOW STR 23R. BLENDED AREA AND FOUND OUT OF LIMITS IAW SRM 51-10-1 AND 53-30-1. CUT OUT DAMAGED AREA IAW SRM 53-30-3. FABRICATED DOUBLER AND INSTALLED IAW SRM 53-30-3.

Part: SEAT TRACK — CORRODED (BS 380-480) · corrosion level 2 · airframe 39,677 hrs · 27,858 cycles

SEAT TRACK AT BS 380-480 LBL 25 HAS CORROSION. CORROSION OUT OF LIMITS IAW SRM 53-10-1. REMOVED DAMAGED SEAT TRACK SECTION IAW SRM 51-30-2. FABRICATED AND INSTALLED NEW SEAT TRACK SECTION IAW SRM 53-10-2 AND SRM 51-30-2.

Part: SEAT TRACK — CORRODED (BS 720D-740) · airframe 39,677 hrs · 27,858 cycles

SEAT TRACK AT BS 720D-740, RBL 25 HAS CORROSION. CORROSION. CORROSION OUT OF LIMITS IAW SRM 53-10-1. REMOVED DAMAGED SEAT TRACK SECTION IAW SRM 51-30-2. FABRICATED AND INSTALLED NEW SEAT TRACK SECTION IAW SRM 53-10-5 FIG1 AND SRM 51-30-2.

Part: SEAT TRACK — CORRODED (BS 480-690) · corrosion level 2 · airframe 39,677 hrs · 27,858 cycles

SEAT TRACK AT BS 480-690, RBL 45 HAS CORROSION. FOUND OUT OF LIMITS IAW SRM 53-10-1. REMOVED DAMAGED SEAT TRACK SECTION IAW SRM 51-30-2. FABRICATED AND INSTALLED NEW SEAT TRACK SECTION IAW SRM 53-10-2 AND SRM 51-30-2.

Part: SEAT TRACK — CORRODED (BS 480-600) · corrosion level 2 · airframe 39,677 hrs · 27,858 cycles

SEAT TRACK AT BS 480-600 BL 0 HAS CORROSION. REMOVED SEAT TRACK SECTION IAW SRM51-30-2, REV 103. FABRICATED NEW SEAT TRACK IAW SRM 53-10-2 FIG 7A. INSTALLED SEAT TRACK SECTION IAW SRM 51-30-2.

Part: SEAT TRACK — CORRODED (BS 480-690) · corrosion level 2 · airframe 39,677 hrs · 27,858 cycles

SEAT TRACK AT BS 480-690 RBL 25 HAS CORROSION. CORROSION OUT OF LIMITS IAW SRM 53-10-1. REMOVED DAMAGED SEAT TRACK SECTION IAW SRM 51-30-2. FABRICATED AND INSTALLED NEW SEAT TRACK SECTION IAW SRM 53-10-2 AND SRM 51-30-2.

Part: SEAT TRACK — CORRODED (BS 360-480) · corrosion level 2 · airframe 39,677 hrs · 27,858 cycles

SEAT TRACK AT BS 360-480 RBL 25 HAS CORROSION. CORROSION OUT OF LIMITS IAW SRM 53-10-1. REMOVED SEAT TRACK SECTION IAW SRM 51-30-2. FABRICATED AND INSTALLED NEW SEAT TRACK SECTION IAW SRM 53-10-2, 53-42-00-04 AND SRM 51-30-2.

Part: SEAT TRACK — CORRODED (BS 348-480) · corrosion level 2 · airframe 39,677 hrs · 27,858 cycles

SEAT TRACK AT BS 348-480, BL 0 HAS CORROSION. CORROSION OUT OF LIMITS IAW SRM 53-10-1. REMOVED DAMAGED SEAT TRACK SECTION IAW SRM 51-30-2. FABRICATED AND INSTALLED NEW SEAT TRACK SECTION IAW SRM 53-10-2 AND SRM 51-30-2.

Part: FRAME — DENTED (BS 1130 S25-26R) · airframe 39,677 hrs · 27,858 cycles

RT SIDE OF FUSELAGE, FRAME HAS A DENT AT BS 1130 BETWEEN STRINGER 25R AND 26R. CUTOUT DAMAGED AREA, FABRICATED REPAIR ANGLE, AND INSTALLED REPAIR IAW SRM 51-40-3 FIG 1.

Part: FRAME — DENTED (BS 660 S25R) · airframe 39,677 hrs · 27,858 cycles

ZEE FRAME DENTED AT STA 660 JUST OTBD OF STR 25R. CUTOUT DAMAGE AREA IAW SRM 51-40-3 FIG 1, FABRICATED REPAIR IAW SRM 51-40-3 FIG FIG1, HEAT TREATED REPAIR TO T6 IAW FASI REPORT 2-37153-801 REV A, TREATED & PRIMED REPAIR IAW SRM 51-10-2, INSTALLED REPAIR IAW SRM 51-30-2. REPAIR ACCOMPLISHED IAW EA 7-5310-136783.

Part: FLOORBEAM — CORRODED (BS 680) · corrosion level 2 · airframe 39,677 hrs · 27,858 cycles

FLOORBEAM AT BS 680, LBL 45 TO RBL 25 HAS CORROSION. REMOVED CORROSION, CUTOUT DAMAGED AREA IAW SRM 51-10-6, FABRICATED REPAIR PARTS IAW SRM 53-10-8, INSTALLED REPAIR PARTS IAW SRM 51-30-5, 51-10-2, 51-30- 2.

Part: SKIN — DENTED (BS 1308) · airframe 39,677 hrs · 27,858 cycles

AFT AIRSTAIRS LT TORQUE BOX EXTERIOR SKIN AT STA 1308, LIGHTING CUT-OUT, SKIN HAS DENT AND CRACK ALONG EDGE. CUTOUT DAMAGED AREA & FABRICATED REPAIR DOUBLER IAW SRM 51-40-2 FIG 1 & 53-10-2 FIG 6, TREATED & PRIMED PARTS IAW SRM 51-10-2, INSTALLED REPAIR DOUBLER IAW SRM 51-30-2.

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 38,272 hrs · 26,695 cycles

BS 1183 TO 1148 AT STR 26L HAS SURFACE CORROSION ON INNER SKIN REMOVED CORROSION AND FOUND OUT OF LIMITS REPAIRED SKIN IAW EA 7-5330-126867.

Part: SKIN — DAMAGED (BS 440) · airframe 38,272 hrs · 26,695 cycles

NUMEROUS FASTENERS WITH IMPROPER ED AND SPACING STA 440 STR'S 8L TO 10L. REPAIRED THE AFFECTED AREA IAW FEDEX EA NR 7-5330-126864, FUSELAGE SKIN AD 98-11-03R1. MCD CUTOUT REINFORCEMENT DOUBLER AND FUSELAGE SKIN LAP JOINT REPAIR AT STA 440, S10L.

Part: SPAR — CORRODED (ZONE 100) · corrosion level 2 · airframe 38,272 hrs · 26,695 cycles

CORROSION IN NLG LT STRUT DOOR SPAR BOX, APPX FUSELAGE STA 290. REMOVED WEB IAW SRM 51-30-2 AND REMOVED CORROSION IAW SRM 51-10-6. FOUND OUT OF LIMITS IAW SRM 53-10-1 FIG 1. REMOVED 2ND WEB LT AREA FOR ACCESS IAW SRM 51-30-2 AND REMOVED NLG SPAR IAW SRM 51-30-2. REMOVED EXISTING CORROSION FROM SPAR IAW SRM 51-10-6 AND EA 7-5310-126865. TREATED AND PRIMED SPAR IAW SRM 51-10-2 & EA 7-5310-126865. FABRICATED REPAIR ANGLE FROM BAC 1503-101053 IAW FEDEX EA 7-5310-126865. TREATED AND PRIMED ANGLE. INSTALL REPAIR PARTS IAW EA 7-5310-126865 AND SRM 51-30-2.

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 38,272 hrs · 26,695 cycles

BS 1183 - 1148 OB AND STR 26L HAS SURFACE CORROSION. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 53-30-1 FIG 1 AND 2 AND 53-30-2 FIG 2. REPAIRED SKIN IAW EA NR 7-5330-126867 FUSELAGE SKIN AD 98-11-03 R1, STA 1152 STA 1175 STR 26L 65-54583 LAP JOINT UPPER AND LOWER SKINS CORROSION REPAIR.

Part: FAILSAFE — CORRODED (BS 950) · corrosion level 2 · airframe 38,272 hrs · 26,695 cycles

AFT CARGO COMP BS 950 AT STR 29R OTBD SIDE HAS LEVELING COMPOUND CRACKED, BELOW FAILSAFE. CORROSION ON FAILSAFE BS 950 STR 29R TO STR 28R. REMOVED LEVELING COMPOUND AND FOUND CORROSION OUT OF LIMITS IAW SRM 53-10-1 FIG 1. CUT OUT DAMAGE AREA IAW SRM 51-10-1 AND 51-40-4 FIG 1. FABRICATED REPAIR ANGLE AND REPAIR FILLER IAW SRM 51-40-4 FIG 1 AND 53-10-2 FIG 5. TREATED AND PRIMED REPAIR PARTS IAW SRM 51-10-2. INSTALLED REPAIR PARTS IAW SRM 51-40-4 FIG 1 AND 51-30-2. REAPPLIED LEVELING COMPOUND IAW SOPM 20-41-05.

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 38,272 hrs · 26,695 cycles

NLG W/W SHEAR TIE AT STA 312 BETWEEN STR 24R - 25R IS CRACKED AT BOTTOM HOLE. REMOVED FASTENERS A ND CUT OUT SHEAR TIE IAW B727 SRM 51-30-2 AND 53-10-4 FIG 15. REPAIRED NLG W/W SHEAR TIE AT BS 312 BETWEEN STR 24R AND STR 25R IAW B727 SRM 53-10-4 FIG 15. TREATED AND PRIMED PARTS IAW B727 SRM 51-10-2. INSTALLED SHEAR TIE, REPAIR IAW B727 SRM 51-30-2 AND 53-10-4 FIG 15.

Part: SKIN — DENTED (ZONE 800) · airframe 38,272 hrs · 26,695 cycles

E&E DOOR DENTED & HAS GOUGE MARKS AT LH EDGE OF DOOR EXTERIOR SKIN. DENTS FOUND TO BE OUT OF LIMITS BY MECHANICAL MEANS IAW SRM 52-100-2. CUT OUT DAMAGE (DIMS: 2 1/8 X 1 1/8) IAW SRM 52-00-3 FIG 1. FABRICATED DOUBLER AND FILLER REPAIR IAW SRM 52-00-3 FIG AND 52-40-1 FIG 2. TREATED AND PRIME REPAIR PARTS IAW SRM 51-10-2 AND INSTALLED PARTS IAW SRM 51-30-2.

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 38,272 hrs · 26,695 cycles

NLG W/W WEB AT STA 312 UPPER SECTION OF SHEAR TIE WEB IS CORRODED AT LBL 22. CUT OUT DAMAGE AREA DIM: 5 1/2 BY 4 AND REPAIRED NLG W/W WEB AT STA 312 SHEAR TIE LBL 22 IAW B727 SRM 53-10-4 FIG 11 AND 53-10-2 FIG 1.

Part: SKIN — CANNING (ZONE 200) · airframe 38,272 hrs · 26,695 cycles

EVIDENCE OF SKIN OIL CANNING AT BS 1347.65 BETWEEN STR 6 R AND STR 7R. CUT OUT DAMAGE AREA IAW SRM 53-30-5 FIG 26. FAB REPAIR PART IAW SRM 53-30-3 FIG 26 AND 54-30-2 FIG 4. TREATED AND PRIMED IAW SRM 51-10-2. INSTALLED REPAIR IAW SRM 51-30-2.

Part: FRAME — CORRODED (FWD CARGO PIT) · corrosion level 2 · airframe 38,272 hrs · 26,695 cycles

CORROSION ON THE FWD CARGO BILGE AREA AT ST 480 BETWEEN STR 27R AND STR 26R. CUT OUT DAMAGE AREA SHEAR TIE IAW SRM 53-10-4 FIG 15. FAB SHEAR TIE IAW SRM 53-10-2 FIG 3. HEAT TREAT PART IAW ENGINEERING REPORT NR 2-37153-801 REV A. TREATED AND PRIMED IAW SRM 51-10-2. INSTALLED SHEAR TIE IAW SRM 51-30-2.

Part: SKIN — CRACKED (NR 6 SLAT) · airframe 38,272 hrs · 26,695 cycles

RT WING L/E SLAT NR 6 LOWER SURFACE SKIN IS CRACKED AROUND RIVET HOLE. REMOVED RT NR 6 SLAT COVE PNL FOR ACCESS IAW SRM 51-30-2. FABRICATED REPAIR DOUBLE IAW SRM 57-50-3 FIG 1. TREATED AND PRIMED IAW SRM 51-10-2. INSTALLED REPAIR IAW SRM 57-50-3 FIG 1, REINSTALLED RT NR 6 SLAT COVE PNL IAW SRM 51-30-2.

Part: SKIN — ERODED (ZONE 400) · airframe 38,272 hrs · 26,695 cycles

NR 1 NOSE COWL L/E SKIN AT BOTTOM HAS AREAS OF EROSION AND 3 CRACKS. REMOVED ACCESS PANEL IAW B727 SRM 51-30-2, CUT OUT DAMAGE DIMS 9 3/4 BY 3/4 IAW B727 SRM 54-30-3 FIG 3. FAB DOUBLER MAT 2024T3 .050 PO NR 9007861 DIMS 19 3/8 BY 3 1/2 AND FILLER MATERIAL 2024T3 .040 PO NR 9007927 DIMS 9 3/4 BY 3/4 IAW B727 SRM 54-30-3 FIG 3A AND 54-30-2 FIG 1. TREATED AND PRIMED REPAIR PARTS IAW B727 SRM 51-10-2. INSTALLED PARTS IAW B727 SRM 51-30-2 AND REINSTALLED PANEL IAW B727 SRM 51-30-2.

Part: SKIN — CORRODED (BS 950F-970) · corrosion level 2 · airframe 38,272 hrs · 26,695 cycles

AFT CARGO COMP BS 950F - 970 OUTBD OF STR 28L HAS SURFACE CORROSION RUNNING AFT BEHIND INTERCOSTAL. REMOVED FLOOR SUPPORT AND INTERCOSTAL FOR ACCESS IAW SRM 51-30-2. CUT OUT DAMAGE AREA. FABBED DOUBLER REPAIR AND 2 FILLER IAW SRM 53-30-3 FIG 3 AND 53-30-2 FIG 2. TREATED AND PRIMED IAW SRM 51-10-2. INSTALLED REPAIR PARTS AND INTERCOSTAL AND FLOOR SUPPORT IAW SRM 51-30-2. INSTALLED COUNTER SINK WASHER IAW SRM 51-30-8.

Part: SKIN — WORN (ZONE 500) · airframe 38,272 hrs · 26,695 cycles

LT WING NR 2 SLAT UPPER T/E LIP DAMAGED AT INBD UP STOP HOOK. TRIMMED OUT DAMAGE AREA IAW SRM 57-50-1, REMOVED SLAT HOOK IAW SRM 51-30-2, FAB REPAIR PLATE IAW SRM 57-50-3. TREATED AND PRIMED IAW SRM 51-10-2. INSTALLED COUNTERSINK WASHERS IAW SRM 51-30-8 FIG 4. INSTALLED REPAIR DOUBLER IAW SRM 51-30-2. REINSTALLED HOOK IAW SRM 51-30-2.

Part: SUPPORT BEAM — DAMAGED (ZONE 500) · airframe 38,272 hrs · 26,695 cycles

FASTENERS LOOSE LWR SIDE OF NR 7 SPOILER FITTING. UPON FURTHER EVALUATION FOUND IMPROPER REPAIR IAW DRAWING SR27-57-038. REPAIRED LT WING INBD SPOILER SUPPORT BEAM IAW DRAWING SR 27-57-038 REV C, SEE WO NR 00042909, N/R N00197, JPF FOR DETAILS.

Part: SKIN — GOUGED (RT WING FLAP) · airframe 38,272 hrs · 26,695 cycles

RT INBD FOREFLAP L/E O/B CORNER IS GOUGED ON PREVIOUS REPAIR. REMOVED PREVIOUS REPAIR IAW B727 SRM 51-30-2. FABRICATED NEW REPAIR PART, MAT USED 2024T3 .063 PO NR 9007835, DIMENSION 4 INCH BY 3 3/4 INCH IAW B727 57-50-4 FIG 1. TREATED AND PRIMED AREA AND PART IAW B 727 SRM 51-10-2. INSTALLED NEW DOUBLER IAW B 727 SRM 51-30-2.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,713 hrs · 24,610 cycles

SEAT TRACK LBL 24.5 HAS CORROSION FROM STA 480 TO 540. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-30-2.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,713 hrs · 24,610 cycles

SEAT TRACK STA 682 TO 686 HAS CORROSION BL 0. REMOVED & REPLACED SECTION OF SEAT TRACK STA 600 - 720 BL 0 IAW SRM 51-30-2.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 35,713 hrs · 24,610 cycles

SEAT TRACK, RBL 24, FS 480 - 690 HAS CORROSION AND EXISTING BLEND REPAIRS AND REQUIRES REPLACEMENT PER 7-5340-7-5002. REMOVED AND REPLACED TRACK, FABBED ON TRAVERLER T5-524062 AND INSTALLED IAW SRM 51-30-2.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 35,713 hrs · 24,610 cycles

SEAT TRACK, RBL 45, FS 500 - 540 HAS CORROSION AND FROM STATIONS 580 TO 690 HAS EXISTING BLEND REPAIRS AND REQUIRES REPLACEMENT PER EO 7-5340-7-5002. REMOVED AND REPLACED SEAT TRACK, STA 480-690 IAW SRM 51-30-2. SEAT TRACK FABBED ON TRAVELER T5-524064.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 35,713 hrs · 24,610 cycles

SEAT TRACK, RBL 24 FS 690, SPLICE FOUND CORRODED UPON REMOVAL OF SPLICE PARTS. SPLICED IN SECTION OF SEAT TRACK STA 690 - 710 RBL 24 IAW SRM 53-10-5 FIG 1. SEAT TRACK FABBED ON TRAVELER T5/524451. SPLICES FABBED FROM P/N 60-3338/24, BATCH 913828, SPLICE PLATE FABBED FROM 7075-T6 .250.

Part: PUMP — MALFUNCTIONED (HYD SYSTEM) · airframe 35,104 hrs · 24,140 cycles

NR 2 B-PUMP LOW PRESS LIGHT ILLUMINATED WITH APPROX 1.4 GALS LOSS IN B-QTY. TURNED NR 2 B-PUMP OFF, GROUND CREW FOUND HYD LEAK IN B-PUMP AREA, B-SPOILER SWITCH TURNED OFF. REMOVED AND REPLACED CASE DRAIN FILTER REF 727-200 M/M 29-12-021-2. STILL NEEDS LEAK CHECK. INSTALLED NEW HYD PUMP. SERVICED HYD FLUID AND LEAK CHECKED. NO LEAKS NOTED.

Part: LINKAGE — MISSING (NR 1 ENG CONTROL) · airframe 34,372 hrs · 23,556 cycles

INFLIGHT TOTAL LOSS OF NR 1 ENGINE THROTTLE CONTROL. ENGINE NR 1 ACCELERATED TO 90 PERCENT N1 & N2, SUSPECT ZERO SPEED PROTECTION HAS ENGAGED. ENGINE SHUTDOWN IAW CHECKLIST. FOUND NR 1 ENG THROTTLE CONTROL LINKAGE AFT ROD-END BEARING MISSING. CAPT CONFIRMED SHUTDOWN DURATION OF LESS THAN 20 MINUTES WITH A POSITIVE OIL PRESSURE ABOVE 10 PSI DURING WINDMILLING. ACCOMPLISHED THE ENGINE WINDMILLING INSPECTION REFERENCING THE P & W JT8D MAINTENANCE MANUAL 72-00. T/S FOUND THAT THE BOLT WHICH ATTACHES THRUST LEVER INPUT ROD TO NR 1 ENG FUEL CONTROL HAD FALLEN OUT. INSTALLED NEW BOLT, NUT, WASHER AND COTTER KEY TO INPUT ROD. RIGGING WAS NOT AFFECTED REF M/M 76-11-001-4. OK FOR SERVICE.

Part: WARNING LIGHT — ILLUMINATED (COCKPIT) · airframe 33,445 hrs · 22,802 cycles

LOUD BOOM & AIRFRAME SHUDDER EXPERIENCED ON CLIMBOUT, AUTOPACK TRIP ACTIVATED. ENGINE FAIL LIGHT BLINKED MOMENTARILY, BUT STAYED OUT. SUSPECT COMPRESSOR STALL BUT UNABLE TO IDENTIFY ENG. ALL ENG INSTRUMENTS NORM. BORESCOPED ENGINES 1, 2, 3 PER MM 72-00-00-1. NO DAMAGE BEYOND MM LIMITS WAS NOTED. ENG RUN WAS COMPLIED WITH, ALL CHECK OK.

Part: SCREEN — DIRTY (BLEED CONTROL)

ON T/O LOUD BANG OCCURRED. PACKS TRIPPED. TROUBLESHOT NO DEFECTS NOTED. CLEANED PRBC SCREENS.

Part: FITTING — SHEARED (LT MLG) · airframe 32,310 hrs · 21,914 cycles

LT MLG DOOR ACTUATOR RIB FITTING SHEARED IN FLIGHT. LOG PAGE 00199388 IND TEST FLT UNSAT DUE TO MLG DOOR BROKEN IN FLT. *S/D* REMOVED AND REPLACED LT MLG INBOARD DOOR ASSY, (P/N 65-24764-129) ACTUATOR (P/N 7-3141-4), PUSHROD ASSY (P/N 69-21445).

Part: LANDING GEAR — MALFUNCTIONED (LT MAIN)

AFT GEAR RETRACT AND HANDLE OFF, LEFT GEAR GREEN & RED LIGHT CAME ON. FLAPS WERE UP AND AILERONS LEVEL AFT GEAR EXT LEFT RED GEAR LIGHT STAY ON WITH NORM DOWN GRN LIGHT. *S/D* PERF MLG UPLOCK SPRING BUNGEE TEST PER MM 32-32-71, CK GOOD. NO DEFECTS NOTED.

Part: ENGINE — FAILED (NR 3)

99-150 - NR 3 ENGINE OIL TEMP CLIMB TO OFF SCALE HIGH, ENGINE WAS SHUT DOWN PER CK LIST. REPLACED NR 3 ENGINE PER WORK CARD 70T001.

Part: BEAM — CORRODED (BS 760-850)

NR 212 WHILE WORKING NR 199 FOUND CORROSION ON LONGITUDINAL BEAM BS 760 TO 850, LBL 25, WL 205. *S/D* REMOVED AND REPLACED LONG BEAM BS 760 TO 850, LBL 25, WL 208 PER FEDEX SRM 51-30-2 AND BOEING DWG 65-16279.

Part: KEEL BEAM — CORRODED (BS 950-967)

NR 152 CORROSION ON OUTBOARD FLANGE OF L/H KEEL BEAM BS 950F+17. ** S/D ** REPAIRED L/H KEEL BEAM PER FEDEX SR 27-53-023 & FEDEX SRM 53-10-4 AT BS 950F+17.

Part: FRAME — MISDRILLED (CARGO DOOR)

NR 161 UPON REMOVAL OF #2 CARGO DOOR SEAL RETAINER, FOUND MISDRILLED HOLE IN FRAME AT BS 990, STR 26 R/H. ** S/D ** INSTALLED FASTENERS IN OPEN HOLES AS PER FEDEX SRM 51-30-02.

Part: KEEL BEAM — CORRODED (BS 950-955)

NR 150 CORROSION ON OUTBOARD FLANGE OF LT KEEL BEAM, BS 950 D+5. *S/D* REMOVED CORROSION FROM KEEL BEAM LT OUTBOARD FLANGE BS 950D+5 MATERIAL LOSS WAS .040 DEEP X 1 X 4. FOUND AREA TO BE OUT OF LIMITS. REPAIRED IAW FEDEX SR 27-53-023.

Part: KEEL BEAM — CORRODED (BS 950-967)

NR 149 CORROSION ON OUTBOARD FLANGE OF LT KEEL BEAM BS 950C+6 TO BS 950C+17. *S/D* INSTALLED REPAIR STRAP BS 950C+6 TO 950C+17 LT KEEL BEAM PER FEDEX SRD 27-53-023.

Part: KEEL BEAM — CORRODED (BS 950)

NR 148 CORROSION ON OUTBOARD FLANGE OF LT KEEL BEAM BS 950 B+F. *S/D* REPAIRED OUTBOARD FLANGE OF LT KEEL BEAM BS 950B+7 IAW FEDEX DRAWING NR SR27-53-023.

Part: KEEL BEAM — CORRODED (BS 950-955)

NR 151 CORROSION ON OUTBOARD FLANGE OF LT KEEL BEAM BS 950E+5 AND BS 950 E+11. *S/D* REMOVED CORROSION AND INSTALLED DOUBLER, STRAP, FILLER AT BS 930E TO 950E+15 STR 29 LT IAW FEDEX SR DRAWING 27-33-023.

Part: AIR DISTRIBUTION — ODOR (COCKPIT)

AFTER TAKEOFF HAD STRONG BURNING SMELL IN COCKPIT FOR ABOUT 10 MINUTES DURATION. RAN BOTH PACKS FOR 20 MINUTES WITH NO SMELL COMING OUT OF AIR VENTS. OK FOR SERVICE.

Part: WINDOW — LOOSE (L1 COCKPIT)

ON CLIMB 11,400 FT, SEAL ON CAPTAIN'S L1 WINDSHIELD WENT. AIR TURNBACK. INSPECTED WINDOW FOR DAMAGE, NONE FOUND. RETIGHTENED WINDOW ASSEMBLY PER MAINTENANCE MANUAL 56-11-11. PRESSURIZED AIRCRAFT UP TO 7 PSID, NO LEAK NOTED.

Part: GATE BEAM — CRACKED (FWD ENTRY DOOR)

NR 0177. DISCREPANCY: FWD ENTRY DOOR LOWER GATE BEAM HAS CRACK INDICATION ADJACENT TO LOWER FORWARD STOP PM FITTING INBOARD FASTENERS. ****S/D ****** COMING. CORRECTIVE ACTION: REMOVED AND REPLACED FORWARD ENTRY DOOR LOWER GATE BEAM IAW OHM 20-50-01.

Part: SHEAR TIE — CORRODED (BS 705)

AFTER REMOVAL OF CRACKED LEVELING COMPOUND AT BS 705 STR 28 RT AND LT, FOUND FRAME SHEAR TIE CORRODED OUT OF LIMITS. REMOVED CORRODED SHEAR TIE, CLEANED AND TREATED CORROSION ON EXTERNAL SKIN UNDER SHEAR TIE. FOUND SKIN TO BE WITHIN LIMITS IAW FEDEX SRM 53-30-1, INSTALLED NEW SHEAR TIE.

Part: REINFORCE CHORD — CORRODED (BS 1176.9)

CORROSION ON BS 1176.9 REINFORCEMENT CHORD IS OUT OF LIMITS FROM LBL 47 TO 57 WL 208. REMOVED AND REPLACED DAMAGED REINFORCEMENT CHORD FROM LBL TO RBL 65 STA 1176.9 WL 208.

Part: SHEAR TIE — CORRODED (BS 950)

CORROSION (C53-111-01(3), ON SHEAR TIE AT BS 950E LBL 9 WL 138 BETWEEN STR 28 TO 29L. REPAIRED SHEAR TIE PER FEDEX SRM 53-10-4.

Part: STRINGER — CORRODED (BS 700-720)

CORROSION (C53-224-01, -1) ON STR NR 4R BS 720 A TO 700. MECHANICALLY REMOVED CORROSION ON STR NR 4R BS 720 A TO 700 FOUND TO BE OUT OF LIMITS PER FEDEX SRM 53-10-1. REPLACED STR 720 PLUS 10 TO BS 720 A PLUS 10 PER FEDEX SRM 53-10-3.

Part: SHEAR WEB — CORRODED (BS 720)

WHILE WORKING NR0475 FOUND CORROSION ON WEB BS 720D TO 720E WL 20 RBL 68 TO 75. REMOVED CORRODED WEB FROM BS 720D TO 720E WL 208 RBL 68 TO 75. FABRICATED NEW WEB AND INSTALLED. FABRICATED IAW FEDEX SRM 53-10-2.

Part: STRINGER CLIP — CRACKED (BS 680)

CRACKED STR CLIP AT BS 680 STR 3L. REMOVED STR CLIP AT BS 680 STR 3L AND INSTALLED NEW STR CLIP PER FEDEX SRM 51-10-1.

Part: STRINGER CLIP — CRACKED (BS 660)

CRACKED STR CLIPS AT BS 660 STR 3 AND 4L. REMOVED STR CLIPS AT BS 660 STR 3 AND 4L AND INSTALLED NEW STR CLIPS PER FEDEX SRM 51-10-1.

Part: BULKHEAD WEB — DAMAGED (BS 1183)

MECHANICAL DAMAGE TO THE AFT SIDE OF THE 1183 BULKHEAD WEB AT LBL 36 WL 261. REPAIRED AFT SIDE OF THE 118.3 BULKHEAD WEB AT LBL 36 WL 261 IAW FEDEX SRM 53-10-09 FIG 4.

Part: STRINGER — GOUGES (BS 720)

GOUGES IN STR 7L BS 720B PLUS 15. GOUGES IN STR 7L OUT OF LIMITS, FABRICATED AND INSTALLED REPAIR PARTS PER FEDEX SRM 53-10-3.

Part: FRAME — CORRISION (BS 1110)

NR 0317 (018C), CORROSION (C53-224-01) ON FWD SIDE OF BS 1110 FRAME AT STR 4 LT. REPAIRED FRAME FWD SIDE OF BS 1110 FRAME AT STR 4 LT IAW FEDEX SRM 51-40-3.

Part: STRINGER — CORROSION (BS 950)

NR 0314, 032 CORROSION (C53-224-01, -3) AND TOOLING MARKS BS 950A, STR 7 RT AFT SIDE OF FRAME. *S/D* REMOVED AND REPLACED STRINGER 7 RT FROM BS 950 TO 950B PLUS 10 IAW SRM 53-10-1 SRM 53-10-3 FIG 3.

Part: FLOOR BEAM — CORROSION (BS 1130)

NR 0391 (034), CORROSION (C53-111-01, -3) ON LOWER CHORD OF FLOOR BEAM AT NUTPLATE HOLES BS 1130 LBL 54 TO RT 54 LT 200.

Part: STRINGER — CORRISION (BS 950)

NR 0314 (032), CORROSION (C53-224-01, -3) AND TOOLING MARKS BS 950A, STR 7 RT AFT SIDE OF FRAME MARKED IN RED.

Part: FRAME — CORROSION (BS 1110)

NR 0317 (018C), CORROSION (C53-224-01) ON FWD SIDE OF BS 1110 FRAME AT STR 4 LT. REPAIRED FRAME FWD SIDE OF BS 1110 FRAME AT STR 4 LT IAW FEDEX SRM 51-40-3.

Part: FLOOR BEAM — CORRISION (BS 1130)

NR 0391 (034), CORROSION (C53-111-01(3) ON LOWER CHORD OF FLOOR BEAM AT NUTPLATE HOLES BS 1130 LBL 54 TO RT 54 LT 200.

Part: FLOOR BEAM — CORRODED (BS 480)

CORROSION C53-224-01 AND BARE METAL AT BS 480 BEAM FROM LBL 44 - RBL 23, WL 208.1. REPAIRED BS 480 FLOOR BEAM FROM RBL 16 - LBL 17, WL 208 PER FEDEX SRM 53-10-8 AND ALODINED AND PRIMED BARE METAL AREAS.

Part: EDGE BEAM — CRACKED (ENTRY DOOR)

FORWARD ENTRY DOOR AFT SIDE FRAME IS CRACKED AND GOUGED AT UPPER END. REMOVED AND REPLACED FORWARD ENTRY DOOR, AFT SIDE FRAME.

Part: FLOOR BEAM — CORRODED (BS 344)

CORROSION C53-224-01 ON 344 BEAM FROM LBL 59 - RBL 37, WL 208.1. REPAIRED BS 344 FLOOR BEAM UPPER CHORD PER FEDEX DRAWING SR 27-53-007.

Part: STRINGER — CORRODED (BS 1060)

CORROSION C53-111-01(3) ON STR 28L BETWEEN SKIN AND STR, BS AT BS 1060, STR 28L. REPAIRED CORRODED STRINGER PER FEDEX SRM 53-10-3.

Part: SKIN — CORRODED (BS 1055)

CORROSION C53-100-01 ON SKIN BS 1055, STR 28L. AT BS 1055 STR 28L, REPAIRED CORRODED SKIN PER FEDEX SRM 53-30-3.

Part: STRINGER — GOUGED (BS 540)

GOUGES IN STRINGER AT BS 540, STR 7R. REPAIRED, OUT OF LIMITS, STR 7R, BS 540 IAW FEDEX SRM 53-10-3.

Part: SKIN — GOUGED (BS 400-510)

GOUGES AND PITS ON EXTERIOR OF SKIN BS 400-BS 510, STR 26R - BL ZERO. REPAIRED DAMAGED SKIN THAT WAS OUT OF LIMITS IAW FEDEX SRM 53-30-3.

Part: BULKHEAD WEB — DAMAGED (BS 1183)

NR0064 AND 024, MECH DAMAGE TO THE FWD SIDE OF THE 1183 BULKHEAD AT LBL 56 WL 226. REPAIRED BULKHEAD WEB PER SRM 53-10-9.

Part: FRAME — CORRODED (BS 720)

CORROSION C53-224-01(1) ON FRAME AT BS 720C, STR 17R - STR 10R. REPAIRED FRAME STA 720C, STR 17R - STR 10R OUT OF LIMIT AREA IAW FEDEX SRM 53-10-4.

Part: FRAME — DENTED (BS 950)

NR0373 AND 026, DENTS IN FRAME BS 950F LBL 29 TO 36 WL 148 TO 152. REPAIRED FRAM AT BS 950, LBL 29 TO 36, WL 148 TO 152, IAW FED EX SRM 51-40-3.

Part: STRINGER — CORROSION (BS 1060)

NR0925 AND 028, CORROSION (C53-111-01, -3) ON STR 28L BETWEEN SKIN AND STRINGER BS 1060. *S/D* BS 1060 STR 28 LEFT REPAIRED CORRODED STRINGER PER FEDEX SRM 53-10-3.

Part: TERMINAL PIN — CORRODED (WING/FUS ATTACH)

CORROSION C53-100-05-1/3 LEFT AFT WING TO BODY FITTING TERMINAL PIN. REMOVED AND REPLACED LEFT WING REAR SPAR TO BODY FITTING TERMINAL PIN PER FEDEX MM 57-41-1.

Part: TERMINAL PIN — CORRODED (WING/FUS ATTACH)

CORROSION C53-100-05-2/4 RIGHT WING REAR SPAR TO BODY FITTING TERMINAL PIN FOUND TO BE CORRODED. REMOVED AND REPLACED RIGHT WING REAR SPAR TO BODY FITTING TERMINAL PIN PER FEDEX MM 57-41-1.

Part: FRAME — DENTED (BS 520)

DENTS IN FRAME AT BS 520 LBL 32 WL 160. CUT OUT DAMAGE AND REPAIRED FRAME AT BS 520 LBL 32 WL 160 PER FEDEX SRM 51-40-3.

Part: FRAME — DENTED (BS 660)

FOUND DENT IN FRAME BS 660 BETWEEN STR 22 TO 23R. CUT OUT DAMAGE AND REPAIRED FRAME AT BS 660 BETWEEN STR 22 TO 23R PER FEDEX SRM 51-40-3.

Part: FRAME — DENTED (BS 660)

FOUND DENT IN FRAME STA 660 LT BETWEEN STR 22 TO 23L, FWD BAY. CUT OUT DAMAGE AND REPAIRED FRAME AT BS 660 BETWEEN STR 22 TO 23L PER FEDEX SRM 51-40-3.

Part: FRAME — DENTED (BS 680)

FOUND DENT IN FRAME STA 680 LT BETWEEN STR 23 TO 4L, FWD BAY. CUT OUT DAMAGE AND REPAIRED FRAME AT BS 680 BETWEEN STR 23 TO 24L PER FEDEX SRM 51-40-3.

Part: FLOOR BEAM — CORROSION (BS 1070)

NR 0392 AND NR 005, CORROSION C53-111-01(3) ON LOWER CHORD OF FLOOR BEAM AT NUTPLATE HOLES BS 1070, LBL 41 - RBL 52 WL 200. *****S/D****COMING. REMOVED CORROSION BS 1070, LBL 41 TO RBL 52. AT RBL 12.75, REMOVED 1X1 X .047 INCH BEYOND LIMITS TRIMMED OUT DAMAGE, FABRICATED REPAIR PARTS AND INSTALLED ALL PER SRM 53-10-8, SRM 53-10-1.

Part: SKIN — DENTED (BS 1120)

DENT IN SKIN BS 1120 BETWEEN STR 28 TO 29L. REPAIRED SKIN PER FEDEX SRM 53-30-3.

Part: DOUBLER — CORRODED (BS 731)

NR 0354 AND NR 004, CORROSION C53-132-01-2 UNDER MOUNTING FLANGE OF DISTRIBUTION DUCT STA 740 - 9, RBL 18 UNDER FAIRING ACCESS OF LOWER DUCT REQUIRED. ****S/D***** COMING. CORRECTIVE ACTION: REMOVED CORROSION FROM DOUBLER IN A 3 INCH X 14 INCH AREA. MAXIMUM MATERIAL LOSS IS .010 INCH. ORIGINAL DOUBLER THICKNESS WAS .125 INCH FOUND TO BE WITHIN LIMITS PER FED EX SRM 53-30-01. TREATED AND RE-FINISHED DOUBLER IAW SRM 53-10-03.

Part: FLOOR BEAM — CORROSION (BS 400)

NR 0342 AND NR 003. CORROSION C53-224-01 ON BS 400 FLOOR BEAM FROM RBL 3-12, WL 208. S/D: REPAIRED TOP CHORD OF FLOOR BEAM AT BS 400, RBL 9-12, WL 208.1 PER FEDEX SRM 53-10-8.

Part: SKIN — CORRODED (BS 1120-1130)

NR0253 AND 002, CORROSION (C53-100-01) UNDER SKIN BS 1120 TO 1130 STR 30.

Part: SKIN — DENT (BS 286)

DENT AT BS 286 STR 23R SKIN. FOUND DENT ON SKIN TO BE OUT OF LIMITS PER FEDEX SRM 53-30-3 AT BS 286 STR 23R. REPAIRED SKIN PER FEDEX SRM 53-30-3.

Part: ENGINE — FAILED (NR 2)

CGN - ENG NR 2 FAILED JUST AFTER LIFT OFF CGN; FLAPS 15 DEG A/C VIBRATION, WITH NR 2 ENG N1, N2 DROPPING, FUEL FLOW DROPPING, OIL QTY AND PRESS NORMAL. ENG SHUTDOWN WITH APPROPRIATE CHECKLIST ACCOMPLISHED.