N466FE

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 54,947 hrs · 39,248 cycles

RT DOOR MOUNTED EMERGENCY ESCAPE SLIDE LIGHT INOPERATIVE, BATTERY DEAD. R & R EMERGENCY ESCAPE SLIDE LIGHT BATTERY BACK IAW MM 33-50-121-2-0. OPS CHECKED NORMAL.

Part: GAUGE — OUT OF POSITION (ESCAPE SLIDE) · airframe 54,850 hrs · 39,157 cycles

FWD ENTRY DOOR ESCAPE SLIDE NEEDS TO BE REPLACED/ADJUSTED TO ALLOW PRESSURE GAUGE TO BE VIEWED. REPOSITIONED SLIDE TO ACCOMODATE THE VIEWING IAW MM 25-60-015-2-0.

Part: WIRE — SHORTED (EMERGENCY LIGHTS) · airframe 54,756 hrs · 39,076 cycles

EVACUATION SLIDE LIGHT ON MAIN ENTRANCE DOOR INOP. R & R BATTERY REF MM 33-50-121-2, OPS CHECKED BAD. CHECKED ORIGINAL BATTERY AND IT WAS SHOWING GOOD, REINSTALLED ORIGINAL BATTERY. REPLACED ALL 4 BULBS MM 33-50-121-2, OPS CHECKED BAD. NEW LIGHT ASSY, ATTEMPTED TO INSTALL BUT ACFT WIRING HAD SPLICES VS QUICK DISCONNECTS IAW AMM AND NEW LIGHT. RELEASED FOR SERVICE IAW MEL: 33-16-02-A. CHECKED SWITCH, BATTERY AND LAMP ASSY ALL CHECKED GOOD FOUND SHORT TO GROUND AT TEST CONNECTION AND WIRE BUNDLE INSIDE BATTERY HOUSING. EMERGANCY ESCAPE SLIDE LIGHT OPERATES NORMAL IAW MM 33-50-121-2. ITEM CLEARED

Part: SOLENOID VALVE — CRACKED (RUDDER) · airframe 54,733 hrs · 39,053 cycles

SYSTEM A QTY DECREASED DURING CLIMBOUT AT 10,000 FT. ON LOWER RUDDER POWER UNIT CONTROL, HYD SOLENOID VALVE LEAKING. REPLACED VALVE ASSY AND SEALS IAW MM 27-20-142-4. SYS "A" HYD SYS FILTERS REPLACED IAW MM 29-11-062-3, NO METAL FOUND IN SYS. R & R SYS A HYD PUMP CASE DRAIN FILTERS IAW MM 29-11-041-2, NO METAL FOUND. OPS CHECK OF RUDDER SYS AND LEAK CHECKED HYD VALVE AND FILTERS, OK. RAN ENGS 1 & 2, EXCERCISED ALL FLIGHT CONTROL SYS & FLAPS AND RESERVICED HYD SYS AFTER ENG RUNS. ACFT DOWNGRADED TO CHECK CAT II.

Part: CONTROL VALVE — FAILED (CABIN PRESSURE) · airframe 54,392 hrs · 38,767 cycles

ACFT DID NOT PRESSURIZE AFTER TAKEOFF. OUTFLOW VALVE SHOWED CLOSED, CARGO HEAT OUTFLOW CLOSED. ALL DOOR LIGHTS INDICATED CLOSED. PRESSURIZATION SYS APPEARED TO BE WORKING, NORMAL OTHERWISE. ALSO COULD NOT GAIN CONTROL IN STBY MODE. RESEALED NOSE GEAR AREA PRESSURIZED AC TO 8 PSID NO LEAKS NOTED AT NOSE GEAR. CHECK PRESSURIZATION. NOTED SLOW RISE IN PRESSURE. RAN NR1 ENGINE IAW JRH. PERFORMED DECAY CHECK IAW JRH. FOUND DUCT LEAKING FWD OF APU. REMOVED DUCT AND ORDERED COUPLING. R & R FLOW CONTROL VALVE PRECAUTIONARY. OPS AND LEAK CHECKS GOOD WITH NO DISCREPANCIES NOTED. ALL WORK DONE REF AMM 21-58-012-4.

Part: FLAP SYSTEM — MALFUNCTIONED (LE FLAPS) · airframe 54,384 hrs · 38,760 cycles

AT FLAPS 2 POSITION THE AMBER L/E FLAPS LIGHT STAYS ILLUMINATED. L/E DIVICES POSITION INDICATOR SHOWS NORMAL LED CONFIGURATION. RELEASED FOR SERVICE IAW MEL: 27-06-C CATEGORY: C EXPIRATION: 07DEC10 "MEL 27-06-C: AMBER L/E FLAPS LIGHT ON THE FWD INSTRUMENT PANEL - INOP. AIRSPEED LIMITED TO 0.80 MACH. FLT CREW REPORTED NO DEFECTS ON TAKEOFF OR LANDING IN RST. NO PREVIOUS HISTORY FOR 30 DAYS, PERFORMED OPS CHECK OF SYS IAW MM 27-82-000-0. NO DEFECTS NOTED, ALL OPS CHECK NORMAL, DEFERRAL CLEARED, ACFT GOOD FOR CONT SERVICE.

Part: VALVE — INOPERATIVE (RT AIR MIX) · airframe 54,320 hrs · 38,704 cycles

RT AIR MIX VALVE STUCK FULL COLD. FOLLOWED BY LOSS OF CABIN PRESSURIZATION. RAN PACKS INDIVIUALY AND TOGETHER. PERFORMED LEAK CK OF DUCTS, PACKS, MIX VLVS. NO DEFECTS NOTED. PERFORMED BITE TEST OF 35 DEG VALVE AND WATCHED VALVES OPERATE. PULLED C/B ON PACK FANS AND CHECKED FOR INTERNAL LEAKS OF THE HEAT EXCHANGERS. ALL CHECKS GOOD. PERFORMED PRESSURAZATION CHECK USING APU THEN NR 1 & 3 ENGINES. COULD NOT DUPLICATE, REF JRH CHAPTER NR 8, AS A PRECAUTION R & R LT & RT COALESCER BAGS REF MM 21-55-051-4, LEAKED CHECKS GOOD. NO HISTORY, OK FOR SERVICE. R & R RT MIX VALVE REF MM 21-61-011-4, PERFORMED OPS CHECK OF RT MIX VALVE IAW MM21-61-011-4, OPS CHECKS GOOD AT THIS TIME.

Part: STRINGER — MISREPAIRED (ZONE 100) · airframe 54,205 hrs · 38,606 cycles

ILLEGAL REPAIR (STRINGER) STR 27L BS 540 - BS 560 FWD PIT. CUT OUT STRINGER SECTION FROM STA 550 TO 590 STR 27L IAW SRM 53-10-3 FIG 1. FAB REPAIR PARTS HAT SECTION MAT USED BAC1498-141 7075-T6 2 EA DIM 21" LONG AND 22" LONG. 2 EA SPLICERS, MAT USED BAC1498-132 7075-T6 DIM 13" LONG & 13.5" LONG AND 6 EA STRAP'S MAT USED 7075-T6 .050" DIM 4 EA (10.5" X .7500") AND 2 EA (13.2500" X .7500") IAW SRM 53-10-3, FIG 1 AND 53-10-2, FIG 9, INSTALLED REPAIR STRINGER IAW SRM 51-30-2, REV 103.

Part: STRINGER — CORRODED (BS 720E S23R) · corrosion level 2 · airframe 54,205 hrs · 38,606 cycles

FWD CARGO COMPARTMENT STR 23R CORRODED BELOW FRAME AT BS 720E. FOUND DURING CLEANING. CUT OUT DAMAGED SECTION OF STRINGER IAW SRM 53-10-3 FIG 1. FABRICATED STRINGER REPAIR FROM BAC 1498 -144, 7075-T6 DIM 16 1/4", SPLICES FFROM BAC 1498-132, 7075-T6, DIM 16 1/2" AND 14 3/4" (2EA) IAW SRM 53-10-2 AND 53-10-3. TREATED AND PRIMED STRINGER REPAIR PARTS IAW SRM 51-10-2. INSTALLED STRINGER REPAIR PARTS IAW SRM 51-30-2 AND 53-10-3 FIG.1.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 54,205 hrs · 38,606 cycles

LT HORIZ STAB HAS PROTRUDING DENT AT ELEV STA 140 WITH CRACK INDICATION. CUTOUT DAMAGED AREA DIM .7500" X .7500" AND FABRICATED REPAIR DOUBLER FROM 2024-T3, 0.032" DIM. 3" X 3" IAW SRM 55-20-3, FIG 4. TREATED AND PRIMED PARTS IAW SRM 51-10-2. INSTALLED REPAIR DOUBLER AT LT HORIZ STAB AT ELEV STA 140 IAW SRM 51-30-2.

Part: SKIN — GOUGED (ZONE 100) · airframe 54,205 hrs · 38,606 cycles

MCD INNER SURROUND SKIN GOUGED STA 620-630, STR 16L. REPAIRED MCD INNER SURROUND SKIN IAW EA 7-5330-135571.

Part: SKIN — CRACKED (ZONE 100) · airframe 54,205 hrs · 38,606 cycles

BS 1290 LIGHTNING HOLE HAS CRACK LBL18 TRIMMED OUT DAMAGE DIM. 1" X 1" AND FABRICATED REPAIR DOUBLER FROM 7075-T6 0.032" DIM. 3 1/2" X 21/2" IAW SRM 51-40-2 FIG. 1. TREATED, PRIMED AND INSTALLED DOUBLER AT BS 1290 LIGHTING HOLE LBL 18 IAW SRM 51-10-2, 51-30-2, AND 51-40-2 FIG. 1. A DAMAGE TOLERANCE INSPECTION (DTI) IS NECESSARY PER SRM 51-40-02.

Part: SEAT TRACK — CORRODED (BS 760-789) · corrosion level 2 · airframe 54,205 hrs · 38,606 cycles

SEAT TRACK AT BS 760 TO 789 RBL 45 IS CORRODED. REMOVED SEAT TRACK AND TEE SECTION BS 760 TO BS 848 RBL 45 IAW SRM 51-30-2. LOCATED AND DRILL NEW TEE SECTION FROM BAC1506-1108 7075-T6 DIM. 110" LONG IAW SRM 53-10-2 FIG. 7 AND 51-30-5. TREATED AND PRIMED NEW TEE IAW SRM 51-10-2. INSTALLED NEW TEE AND SEAT TRACK AT BS 760-848 RBL 45 IAW SRM 51-30-2.

Part: SKIN — GOUGED (CARGO DOOR) · airframe 54,205 hrs · 38,606 cycles

MCD INNER SURROUND SKIN GOUGED STA 620 STR 4L. REMOVED MCD INNER SKIN AFT UPPER SECTION BS 620 STR4L IAW SRM 51-30-2. FABRICATED NEW MCD INNER SKIN SECTION FROM 2024 T3 0.125" DEMINSION 79" X 48" IAW SRM 53-10-2 FIGURE 3A REV J. TREATED AND PRIMED AND INSTALLED NEW MCD AFT UPPER INNER SKIN SECTION BS 620 STR4L IAW SRM 51-30-2 REV 103.

Part: FLOORBEAM — DAMAGED (BS 480) · airframe 54,205 hrs · 38,606 cycles

FLOORBEAM HAS DOUBLE DRILL HOLES BS 480 LBL 45. OVERSIZED HOLES TO 5/32" AND INSTALLED FASTENERS IAW SRM 51-30-5. WITHIN LIMITS IAW SRM 53-10-1 FIGURE 4B.

Part: SUPPORT — CRACKED (BS 620) · airframe 54,205 hrs · 38,606 cycles

MAIN CARGO COMPARTMENT INNER UPPER, DOOR FRAME SUPPORT FASTENER HOLE CRACKED STA 620. REPAIRED MAIN CARGO COMPARTMENT INNER UPPER DOOR FRAME SUPPORT STA 620 IAW EA 7-5310-135576.

Part: FRAME — CORRODED (BS 1148 S26-27L) · corrosion level 2 · airframe 54,205 hrs · 38,606 cycles

CORROSION ON UPPER FLANGE OF FRAME AT BS 1148 BETWEEN STRINGER 27L AND 26L. REMOVED CORROSION. ORIGINAL MATERIAL THICKNESS .063, MATERIAL LOSS .003. FOUND WITHIN LIMITS IAW SRM 53-10-1 AND 53-10-2.

Part: SKIN — GOUGED (ZONE 200) · airframe 54,205 hrs · 38,606 cycles

MCD INNER SURROUND SKIN GOUGED STR 620 STR 8L. BLENDED OUT DAMAGE AND FOUND ORIGINAL MAT 0.125", REMAINING MATERIAL 0.115", MATERIAL LOSS 0.010", REMOVED INNER SKIN SPLICE AND FABRICATED NEW SECTION FROM 2024-T3 0.125" DEMENSION 22"X11" IAW SRM 51-30-2 AND SRM 53-10-2 FIG 3A, REV J, TREATED AND PRIMED AND INSTALLED NEW MCD INNER SKIN SPLICE SEC STA 620 STR 8LT IAW SRM 51-10-2 AND 51-30-2, REV 103.

Part: SEAT TRACK — CORRODED (BS 620-660) · corrosion level 2 · airframe 54,205 hrs · 38,606 cycles

SEAT TRACK CORRODED STA 620 - 660 LBL 45. REMOVED SEAT TRACK IAW SRM 51-30-2. FABRICATED NEW SEAT TRACK SECTION FROM BAC1520-792 7178-T651 DIM. 17.5 FT. IAW SRM 53-*10-2 FIG 7A REV J AND SRM 51-30-5. TREATED, PRIMED AND INSTALLED MAIN CABIN SEAT TRACK SECTION AT BS 480-690 LBL 45 IAW SRM 51-10-2 AND 51-30-2.

Part: SKIN — CORRODED (BS 1070 S28L) · corrosion level 2 · airframe 54,205 hrs · 38,606 cycles

FUSELAGE SKIN STA 1070 STR 28L HAS CORROSION AND FASTENER NO E.D. CUTOUT DAMAGED AREA DIMENSION 5 1/8" X 2 7/8" AND 4 1/8" X 1 1/8" AND FABRICATED REPAIR DOUBLER FROM 2024T3 .063 DIMENSION 28 1/2" X 9 1/2" AND FILLERS FROM 2024T3 .050 DIMENSION 5 1/8" X 2 7/8" AND 4 1/8" X 1 1/8" IAW SRM 53-30-3 FIG 3. TREATED AND PRIMED AND INSTALLED FILLERS AND DOUBLER AT FUSELAGE SKIN IAW SRM 53-30-3 FIG 3, 51-10-2, AND 51-30-2.

Part: SKIN — MISINSTALLED (BS 540-600) · airframe 54,205 hrs · 38,606 cycles

FWD CARGO COMPARTMENT, STRINGER 25L HAS SEVERAL FASTENERS IMPROPERLY INSTALLED FROM STA 540-600. CUT-OUT SKIN DOUBLER AND TRIPLER (6EA) BS 560 - 620 STR 25L DIM. 2 3/4" X 2 1/8" AND FABRICATED REPAIR FILLER FROM 2024-T3 0.125" DIM. 71.5" X 11.5", REPAIR DOUBLER FROM 2024-T3 0.080" DIM. 69.5" X 16" AND REPAIR TRIPLER FROM 2024-T3 0.125" DIM. 67.5" X 11" AND FILLERS FROM 2024-T3 0.125" DIM 2.70" X 2.1" IAW B727 P-F SRM 53-30-3 FIG 1B. TREATED AND PRIMED AND INSTALLED REPAIR PARTS AT EXTERNAL FUSELAGE BS 555-626 STR 23L TO 26L IAW B727 SRM 51-10-2 AND 51-30-2.

Part: SKIN — CHAFED (ZONE 100) · airframe 54,205 hrs · 38,606 cycles

BS 720B, 8" RBL 2 RAM AIR DUCT STIFFENING BOLT CHAFING HOLE IN FUSELAGE SKIN. CUT OUT DAMAGED AREA FUSELAGE SKIN BS 720C 8 RBL2. DIMENSIONS (1 3/8" X 1 3/8") IAW SRM 53-30-3 FIG 3. FABRICATED REPAIR DOUBLER MAT USED 2024 T3 .125" DIM (12 1/4" X 9 7/8") AND FILLER 2024 T3 .125" DIM (1 3/8" X 1 3/8") IAW SRM 53-30-3 FIG. 3 REV.103. INSTALLED DOUBLER AND FILLER IAW SRM 51-30-2.

Part: STRINGER — CORRODED (BS 1100 S27L) · corrosion level 2 · airframe 54,205 hrs · 38,606 cycles

CORROSION ON STRINGER 27L AT BS 1100. REMOVED CORROSION. EVALUATED AREA ORIGINAL .063 MATERIAL LOSS .015 MATERIAL REMAINING .048 FOUND AREA TO BE OUT OF LIMITS. CUTOUT DAMAGED AREA APPROX DIM: 5". FABRICATED STRINGER FILLER FROM BAC 1498-145 7075T6 APPROX DIM: 5". FABRICATED STRINGER SPLICE FROM BAC 1498-131 7075T6 APPROX DIM: 19". INSTALLED STRINGER FILLER AND STRINGER SPLICE, IAW SRM 51-10-6, SRM 53-10-1 FIG 1, SRM 53-10-3 FIG 1 REV 103, SRM 51-10-2, AND SRM 51-30-2.

Part: STRINGER — CORRODED (BS 720B S27L) · corrosion level 2 · airframe 54,205 hrs · 38,606 cycles

CORROSION ON STRINGER 27L AT BS 720B. CUT OUT DAMAGED STRINGER SECTION DIMENSION 14" LONG AND FABRICATED NEW STRINGER SECTION FROM BAC 1498-145 DIMENSION 14" LONG AND 2EA SPLICES FROM BAC 1498-131 DIMENSION 10" LONG EACH, TREATED AND PRIMED AND INSTALLED AT FWD PIT STRINGER 27LT BS 720A 13" TO 720B 7" IAW SRM 51-10-2, 53-10-3 FIG1 & 51-30-2 REV 103.

Part: STRINGER — DAMAGED (BS 520 S25L) · airframe 54,205 hrs · 38,606 cycles

FASTENER HOLE IS ELONGATED IN STR 25L AT BS 520. CUT OUT DAMAGED SECTION OF STRINGER DIM. 16" LONG IAW SRM 53-10-3 FIG 1. FABRICATED STRINGER REPAIR PARTS USING BAC1498-139 7075 T6 DIM 16" 7075 T6 .050" DIM. 10 1/4" X 5/8" (4 EACH), BAC1493-412 7075 T6 DIM 12" (2 EACH) AND BAC1493-513 7075 T6, DIM 10 1/4" (4 EACH) IAW SRM 53-10-2 FIG 9 AND 53-10-2 FIG 1 INSTALLED STRINGER REPAIR IAW SRM 51-30-2 REV. 103.

Part: SKIN — CANNING (BS 1303-1323) · airframe 54,205 hrs · 38,606 cycles

RT FUSELAGE SKIN STR 17R BETWEEN BS 1303 TO BS 1323 IS OIL CANNED. CUTOUT DAMAGED AREA ( DIM: 6" X 3") AND FABRICATED REPAIR DOUBLER FROM 2024T3 .071 DIMENSION 15" X 10" IAW SRM 53-30-3, FIG 1 & 53-30-2, FIG 3. TREATED AND PRIMED AND INSTALLED REPAIR DOUBLER AT RT FUSELAGE SKIN STR 17R BETWEEN BS 1303 AND BS 1323 IAW SRM 51-10-2, 51-30-2, & 53-30-3 FIG 1.

Part: SKIN — GOUGED (BS 460-480 S4L) · airframe 54,205 hrs · 38,606 cycles

MAIN CARGO DOOR INNER SURROUND SKIN GOUGED STA 460-48- STR 4L. REMOVED MAIN CARGO DOOR INNER SKIN FWD UPPER SECTION IAW SRM 51-30-2. FABRICATED NEW INNER SKIN IAW DWG 53FX2022, REV C AND 53FX1535 REV H, TREATED AND PRIMED IAW SRM 51-10-2 AND INSTALLED NEW INNER SKIN IAW SRM 51-30-2, REV 103.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,750 hrs · 37,405 cycles

MAIN CARGO COMPATRMENT, SEAT TRACK IC CORRODED FROM BS 870-848, LBL 25. REMOVED SEAT TRACK AT MAIN CARGO COMPARTMENT IAW SRM 51-30-2. LOCATED AND DRIILED NEW TRACK, DIM 16 INCH LONG IAW SRM 51-30-5 AND 53-10-2 FIG 7. TREATED AND PRIMED AFFECTED AREAS IAW CSRM 51-1-2. INSTALLED NEW TRACK IAW SRM 51-30-2.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,750 hrs · 37,405 cycles

MAIN CARGO COMP STA 760-848 LBL 24 T-CAP CORRODED REMOVED SEAT TRACK AND T-CAP IAW SRM 51-30-2. LOCATED AND DRLLED NEW T-CAP IAW SRM 53-10-2 FIG 7 AND 51-30-5. TREATED AND PRIMED NEW T-CAP IAW SRM 51-10-2. INSTALLED NEW T-CAP AND SEAT TRACK AT MAIN CARGO COMPARTMENT STA 760 TO 848, LBL 24 IAW SRM 51-30-2 AND 53-10-2 FIG 7.

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 52,750 hrs · 37,405 cycles

MAI CARGO COMPARTMENT, SEAT TRACK CORRODED STA 570-580 RBL 45 REMOVED SEAT TRACK SECTION OUT OF LIMITS AT STA 530 TO 690 RBL 45 IAW SRM 51-30-2. FABRICATED, LOCATED AND DRILLED NEW SEAT TRACK IAW SRM ER-01-049 AND SRM 53-10-5 FIG 7. TREATED AND PRIMED PARTS IAW SRM 51-10-2. INSTALLED SEAT TRACK IAW SRM 51-30-2.

Part: SKIN — DENTED (ZONE 100) · airframe 52,750 hrs · 37,405 cycles

DENT RT AFT LWR FUSELAGE BS 1243 S21R CUT OUT DAMAGED AREA 3" BY 3/4" IAW SRM 53-30-3 FIG 1. FABRICATED DOUBLER REPAIR IAW SRM 53-30-3 FIG 1, AND 53-30-2 FIG 3. TREATED AND PRIMED IAW SRM 51-10-2. INSTALLED REPAIR DOUBLER IAW SRM 51-30-2.

Part: SKIN — DENTED (ZONE 100) · airframe 52,750 hrs · 37,405 cycles

DENT LT AFT FUSELAGE STA 1350 STR 17L, FOUND OUT OF LIMITS IAW SRM, EVALUATED DENT AND FOUND OUT OF LIMITS. CUT OUT DAMAGED AREA DIM 1 1/2 BY 1 INCH AND FABRICATED REPAIRED DOUBLER IAW SRM 54-30-3 FIG7. TREATED AND PRIMED PARTS IAW SRM 51-10-2. INSTALLED REPAIR DOUBLER AT FUSELAGE STA 1350, STR 17L IAW SRM 54 30-3 FIG 7 AND 51-30-2.

Part: SKIN — DELAMINATED (LT TE FLAP) · airframe 52,750 hrs · 37,405 cycles

LT I/B FLAP HAS AN AREA OF DELAMINATION ON UPPER SURFACE, WS 275 CUT OUT DELAMINATED AREA 7 1/2 INCH BY 7 1/2 INCH ON LT I/B FORG FLAP UPPER SURFACE AND REMOVED DAMAGED CORE 7 1/2 BY 7 1/2. SHAPED SECTION OF CORE 7 1/2 INCH BY 7 1/2 INCH. FABRICATED DOUBLER 10 1/2 INCH BY 10 1/2 INCH. BONDED CORE PLUG AND DOUBLER, CLEANED, PRIMED AND SEALED IAW SRM 51-40-24 FIG 1.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,750 hrs · 37,405 cycles

MAIN CARGO COMPARTMENT, SEAT TRACK CORRODED STA 950B BL 0. REMOVED SEAT TRACK-OUT OF LIMITS BETWEEN STA 890-950C BL 0 IAW SRM 51-30-2 LOCATED AND DRILLED NEW SEAT TRACK IAW SRM ER-01-049 AND 53-10-5 FIG 7. TREATED AND PRIMED PARTS IAW SRM 51-10-2. INSTALLED NEW SEAT TRACK IAW SRM 51-30-2.

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 52,750 hrs · 37,405 cycles

MAIN CARGO COMPARTMENT, CORROSION ON SEAT TRACK FORM STA 700-720 BL 0. REMOVED SEAT TRACK OUT LIMITS BTW STA 600-720 BL 0 IAW SRM 51-30-2. FABRICATED, LOCATED, AND DRILLED NEW SEAT TRACK IAW SRM EA-01-049 AND SRM 53-10-5 FIG 7. TREATED AND PRIMED IAW SRM 51-10-2. INSTALLED NEW SEAT TRACK IAW SRM 51-30-2.

Part: SKIN — CRACKED (BS 980-990) · airframe 52,750 hrs · 37,405 cycles

AFT LOWER CARGO DOOR LOWER AFT FUSELAGE EDGE BENT AND CRACKED AT STA 980-990. REPAIRED BY TRIMMING THE AFFECTED PER EA 7-5330-116976.

Part: FLOORBEAM — CORRODED (BS 560) · airframe 52,750 hrs · 37,405 cycles

MAIN CARGO COMPARTMENT, FLOORBEAM CORRODED AT BS 560, RBL 0-25. REMOVED CORROSION IAW SRM 51-10-6, AND FOUND OUT OF LIMITS IAW SRM 53-10-1 FIG 4. REMOVED SPLICE ANGLE AND DISPLACED SEAT TRACK FOR ACCESS IAW SRM 51-30-2. CUT OUT DAMAGED SECTION FROM RBL 32 TO LBL 14. FABRICATED REPAIR PARTS IAW SRM 51-10-2. INSTALLED REPAIR PARTS AND PREVIOUSLY REMOVED AND DISPLACED PARTS IAW SRM 53-10-8 FIG1 AND 51-30-2.

Part: VERTICAL BEAM — SHEARED (ZONE 100) · airframe 52,750 hrs · 37,405 cycles

STA 1183 FWD SIDE VERTICAL BEAM AT APPROX LBL 12 HAS FASTENERS WITH NO EDGE DISTANCE. REPAIRED IAW EA 7-5310-116973.

Part: SKIN — DENTED (BS 1050-1054) · airframe 52,750 hrs · 37,405 cycles

DENT RT AFT FUSELAGE STA 1050 STR 23R (DENT FOUND OUT OF LIMITS). CUT OUT DAMAGED AREA IAW SRM 53-30-1 FIG1. FABRICATED REPAIR DOUBLER TREATED AND PRIMED REPAIR PART AND AREA IAW SRM 51-10-2. INSTALLED DOUBLER IAW SRM 51-30-2.

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 52,750 hrs · 37,405 cycles

MAIN CABIN COMPARTMENT, SEAT TRACK CORRODED AT BS 950C, 8 BL 0. REMOVED SEAT TRACK SECTION- OUT OF LIMITS BL 0 STA 950C TO STA 1010 IAW SRM 51-30-2. FABRICATED, LOCATED AND DRILLED NEW SEAT TRACK IAW SRM ER 01-049 AND SRM 53-10-5 FIG7. TREATED AND PRIMED IAW SRM 51-10-2. INSTALLED NEW SEAT RTACK IAW SRM 53-30-2.

Part: SKIN — WORN (ZONE 200) · airframe 52,750 hrs · 37,405 cycles

LT FUSELAGE SKIN WORN AT BS 310 BTW S10L AND S11L, WORN BY FWD ENTRY DOOR MECHANISM LONG BOLT INSTALLED. REPAIRED FWD ENTRY DOOR MECHANISM IAW SRM 51-30-2 AND EA 7-5330-116972.

Part: SUPPORT BEAM — CRACKED (ZONE 500) · airframe 52,750 hrs · 37,405 cycles

MIGRATING SHIMS AND LOOSE HARDWARES AT LWR SIDE OF NR 7 SPOILER SUPPORT BEAM FITTING WS 198. REPAIRED NR 7 SPOILER ACTUATOR SUPPORT BEAM FITTING IAW DRAWING SR27-57-038 REV "C".

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,750 hrs · 37,405 cycles

MAIN CARGO COMPARTMENT, FLOORBEAM CORRODED BETWEEN BL 0 BL 25L, BS 950D. CUT OUT DAMAGE IAW SRM 53-10-3 FIG 3 & SRM ER-01-049 REV E. FABRICATED SECTION, SUPPORT ANGLES AND REINFORCEMENT STRAPS IAW SRM 53-10-3 FIG 3 TREATED AND PRIMED IAW SRM 51-10-2. INSTALLED REPAIR PARTS IAW SRM 51-30-2.

Part: SHIM — MIGRATED (ZONE 100) · airframe 52,750 hrs · 37,405 cycles

MIGRATING SHIMS AND LOOSE HARDWARE AT LWR SIDE OF NR 8 SPOILER ACTUATOR SUPPORT BEAM FITTING, WS 198. REPAIRED SUPPORT BEAM FITTING IAW DRAWING SR27-57-038 REV "C".

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,750 hrs · 37,405 cycles

MAIN CARGO COMPARTMENT, FLOORBEAM CORRODED BETWEEN BL 0 BL 25L , B.S. 950D

Part: BEAM — CRACKED (ZONE 500) · airframe 52,750 hrs · 37,405 cycles

RT WING I/B T/E "J " BEAM AT WING STATION 92 CRACKED, WING T/E SUPPORT BEAM FOR NR 7 SPOILER. TRIMMED OUT CRACKED AREA LENGTH 0.75" IAW SRM 51-10-1. TREATED AND PRIMED AREA "J" BEAM IAW SRM 51-10-2 DRAWING SR27-57-025.

Part: ACTUATOR — FAULTY (L/E SLAT) · airframe 51,480 hrs · 36,428 cycles

NR 4 SLAT W/N RETRACT AFTER T/O. RAN QRH CK LIST W/NEGATIVE RESULTS. RETURNED TO MEM. EXPERIENCED UNCOMMANDED ROLLING INPUT), CREW REPORTED DURING DEBRIEF THAT THEY CYCLED FLAPS TO 5 DEGREES AND BACK TO FLAPS 2 WITH NO HELP. A/C STILL EXPERIENCED UNCOMMANDED ROLL. CYCLED FLAPS SEVERAL TIMES AND SLATS OPERATED NORMALLY ON GROUND. WITH FURTHER INFO FROM OUTGOING FLT CREW, THE UNCONTROLLABLE ROLL WAS TO THE LEFT. RAN SYSTEM THROUGH SEVERAL TIMES AND HAD THE NR 4 SLAT ACT POPPING IN THE CLOSE POS. T/S IAW 727-200 AMM 27-81-000-1 AND FOUND NR 4 L/E SLAT BINDING. REMOVED AND REPLACED NR 4 L/E SLAT ACT, OPS AND LEAK CK OK REF TO AMM 27-81-032-4.

Part: REPAIR — DAMAGED (FLOORBEAM) · airframe 50,970 hrs · 35,999 cycles

EXISTING FLOORBEAM REPAIR UPPER CHORD AT BS 1130, RBL 5.5 - RBL 15.5 (10 X 2 INCH). REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIRED PER FED EX EA 7-5310-91426.

Part: PANEL — MISINSTALLED (HORIZONTAL STAB) · airframe 50,970 hrs · 35,999 cycles

INCORRECT REFERENCE WAS USED TO DETERMINE IF HORZ STAB REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA - PREVIOUS REPAIR ON LEFT HORIZONTAL STABILIZER AT STAB STA 115, 3" WIDE X 3" LONG, 15" AFT OF STAB REAR SPAR. ** SD ** COMING REPLACED PREVIOUS REPAIR ON LEFT HORIZONTAL STABILIZER AT STAB STA 115, IAW EA#7- 5510-91418. THIS REPAIR IS DEEMED MAJOR.

Part: REPAIR — UNKNOWN (BS 1217) · airframe 50,970 hrs · 35,999 cycles

EXISTING EXTERNAL REPAIR WITH BLIND FASTENERS AT BS 1217 S28R 4" BY 4" BY 0.032". REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THIS REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. ALL WORK ACCOMPLISHED IAW FED EX EA 7-5330-91417. REPAIR WAS FOUND TO BE A MAJOR

Part: SKIN — MISDRILLED (TE FLAP) · airframe 50,970 hrs · 35,999 cycles

LT IB TE MIDFLAP LWR AFT SKIN HAS NUMEROUS FASTENER HOLES DOUBLE DRILLED OR EXCESSIVELY COUNTERSUNK, O/B OF O/B FLAP TRACK. REPAIRED LT IB MIDFLAP LOWER AFT SKIN PER SRM 51-40-2.

Part: REPAIR — UNKNOWN (BS 860-880) · airframe 50,970 hrs · 35,999 cycles

EXISTING EXTERNAL REPAIR ON FUSELAGE BS 860-880 STR 8R-10R. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. ALL WORK WAS ACCOMPLISHED IAW FED EX E.A. 7-5330-91421. REPAIR WAS DETERMINED TO BE A MAJOR REPAIR.

Part: DEPRESSOR — CRACKED (CARGO DOOR) · airframe 50,970 hrs · 35,999 cycles

UPON REMOVAL OF AFT CARGO DOOR LOWER SEAL DEPRESSOR, FOUND STUB FRAME CRACKED AT BS 950F, RBL 40, WL 148 SECOND FRAME AFT FROM FWD SIDE OF DOOR. REMOVED AND REPLACED STUB FRAME AT BS 950F, RBL 40 WL 148 IAW SRM 51-30-2 AND SRM 51-30-5.

Part: REPAIR — UNKNOWN (BS 376) · airframe 50,970 hrs · 35,999 cycles

EXISTING EXTERNAL REPAIR ON FUSELAGE BS 376 STR 21R-22R. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. ALL WORK ACCOMPLISHED IAW FED EX EA 7-5330-91422. DETERMINED TO BE A MAJOR REPAIR.

Part: REPAIR — IMPROPER (BS 620-637) · airframe 68,537 hrs · 50,294 cycles

EXISTING EXTERNAL REPAIR ON FUSELAGE BS 620-637 STR 27R-28R. REPAIR REQURIES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REMOVED REPAIR DOUBLER, FABBED AND INSTALLED NEW DOUBLER IAW SRM 53-30-3 FIG 1 MAJOR REPAIR

Part: REPAIR — IMPROPER (BS 720-720B) · airframe 50,970 hrs · 35,999 cycles

FOUND EXISTING STRINGER REPAIR IN FWD CARGO BAY AT BS 720 10" - BS 720B 15", S27R. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. EVALUATED EXISTING REPAIR STR 27R BS 720B 15 AND DETERMINED THAT THIS EXISTING REPAIR DOUBLERS HAD THE CORRECT NUMBER OF FASTENERS PER ROW HOWEVER THIS INCORRECT FASTENERS WERE INSTALLED PER SRM 53-10-3 FIG 1 SHT 1-4. REMOVED EXISTING FASTENERS IN REPAIR AND INSTALLED CORRECT FASTENERS IN EXISTING REPAIR IAW SRM 51-30-2 AND SRM 53-10-3 FIG 1 MAJOR REPAIR

Part: REPAIR — IMPROPER (BS 675-699) · airframe 50,970 hrs · 35,999 cycles

FOUND EXISTING STRINGER REPAIR IN FWD CARGO BAY AT BS 675 - BS 699, S27R. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. EVALUATED EXISTING REPAIR AT STR 27R BS 675-699 AND FOUND REPAIR DOUBLER BS 687- BS699 TO NOT COMPLY WITH SRM 53-10-3 FIG 1. FABRICATED AND INSTALLED REPAIR DOUBLER BS695-699 STR 27R PER SRM FIG 1 MAJOR REPAIR

Part: REPAIR — DAMAGED (HORIZONTAL STAB) · airframe 50,970 hrs · 35,999 cycles

EXISTING REPAIR ON LEFT HORIZONTAL STAB LEADING EDGE WITH SOLID FASTENERS AT L/E STA 61.0 10" WIDE BY 10" LONG. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REMOVED EXISTING REPAIR, FABRICATED AND INSTALLED NEW REPAIR AT LEFT HORIZ STAB LE STA 61.0 IAW SRM 55-10-3 AND SRM 51-30-5 AND SRM 51-30-2.

Part: REPAIR — DAMAGED (STRINGER) · airframe 50,970 hrs · 35,999 cycles

EXISTING STRINGER REPAIR IN FWD CARGO BAY AT BS 710 - BS 720 18", S27R. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REMOVED EXISTING STR REPAIR AND FABRICATED AND INSTALLED REPAIR PER SRM 53-10-3 AND SRM 51-30-2.

Part: REPAIR — IMPROPER (BS 643-660) · airframe 50,970 hrs · 35,999 cycles

FOUND EXISTING STRINGER REPAIR IN FWD CARGO BAY BS 643 - BS 660 S27L. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REMOVED PREVIOUS REPAIR, FABRICATED AND INSTALLED REPAIR BS 646 TO 660 STR 27L PER SRM 53-10-3 FIG 1 THIS IS A MAJOR REPAIR.

Part: REPAIR — UNDAMAGED (SERVICE DOOR) · airframe 50,970 hrs · 35,999 cycles

EXISTING FLUSH REPAIR ON FWD SERVICE DOOR BS 380 STR 9R. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR FOUND NOT TO BE WITHIN COMPLIANCE WITH FAA APPROVED DATA, REMOVED FASTENERS FAB REPAIR DOUBLER INSTALLED FILLER WASHERS IN COUNTERSINKS CHEM TREATED AND PRIMED. SEALED, INSTALLED FASTENERS AND PAINTED WHITE REF SRM 52-00-3 FIG 4. BS 380 STR 9R ON FWD SERVICE DOOR THIS IS A MAJOR REPAIR.

Part: REPAIR — IMPROPER (BS 500) · airframe 50,970 hrs · 35,999 cycles

EXISTING FRAME REPAIR IN FWD CARGO BAY, BS500, S23L - S25L. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REMOVED EXISTING FRAME REPAIR BS 500 STR 23-25L/H FABRICATED ALODINED PRIMED AND INSTALLED NEW REPAIR IAW SRM 51-40-3 FIG 1 THIS IS A MAJOR REPAIR

Part: REPAIR — IMPROPER (BS 385) · airframe 50,970 hrs · 35,999 cycles

EXISTING SPLICE REPAIR ON STR 15L BS 385, REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REMOVED EXISTING REPAIR AT BS 385 STR 15L. INSTALLED NEW REPAIR BS 385 STR 15L PER SRM 53-10-3 FIG 1 DETAIL II. MAJOR REPAIR.

Part: REPAIR — DAMAGED (DOOR) · airframe 50,970 hrs · 35,999 cycles

EXISTING EXTERNAL REPAIR ON AFT CARGO DOOR BS 950E STR 26R. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REMOVED AND REPLACED REPAIR ON AFT CARGO DOOR PER SRM 52-00-3.

Part: FLAP TRACK — CORRODED (NR 6 FLAP) · airframe 50,970 hrs · 35,999 cycles

NR 6 FLAP TRACK, AFT MOUNTING SURFACE IS CORRODED. RECEIVED NR 6 FLAP TRACK INSTALLED ON FED EX WC 27X5708-03.

Part: FLAP TRACK — CORRODED (NR 6 FLAP) · airframe 50,970 hrs · 35,999 cycles

NR 6 FLAP TRACK, FWD MOUNT BUSHINGS ARE CORRODED. NR 6 FLAP TRACK REPLACED ON FED EX WC 27X5708-03.

Part: SKIN — UNKNOWN (LE K-FLAPS) · airframe 50,970 hrs · 35,999 cycles

EXISTING EXTERNAL REPAIRS ON NR 5 K-FLAP INNER TAI SKIN, 14 EACH 2" ROUND REPAIRS. REPAIRS REQUIRE EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIRS WERE ACCOMPLISHED USING FAA APPROVED DATA. REMOVED FASTENERS, INSTALLED WASHERS AND INSTALLED FASTENERS PER SRM 57-50-3.

Part: STRINGER — DAMAGED (BS 480-530) · airframe 50,970 hrs · 35,999 cycles

EXISTING STRINGER REPAIR IN FWD CARGO BAY BS 480-530 S28R. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REMOVED AND REPLACED AFT SPLICE PER SRM 53-10-3.

Part: SHEAR TIE — UNKNOWN (BS 680) · airframe 50,970 hrs · 35,999 cycles

EXISTING FRAME SHEAR TIE REPAIR AT BS 680 STR 26L-27L. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR WAS ACCOMPLISHED PER SRM 53-10-4.

Part: STRINGER — UNKNOWN (BS 705-720) · airframe 50,970 hrs · 35,999 cycles

FOUND EXISTING STRINGER REPAIR IN FWD CARGO BAY AT BS 705 - BS 720 15", S26R. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIRED STRINGER IAW SRM 53-10-3. DETERMINED TO BE A MAJOR REPAIR.

Part: FRAME — DAMAGED (BS 680) · airframe 50,970 hrs · 35,999 cycles

EXISTING FRAME REPAIR IN FWD CARGO BAY AT BS680, S28R RBL 6, WL 154 (6" X 3"). REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REMOVED EXISTING FRAME REPAIR AT BS 680 RBL 6 AND FABRICATED NEW REPAIR FROM 7075T6 .071 LOT 586672. ALODINE, PRIMED AND INSTALLED NEW REPAIR IAW SRM 51-40-3, FIG 1. THIS WAS FOUND TO BE A MAJOR REPAIR

Part: REPAIR — IMPROPER (BS 1120-1133) · airframe 50,970 hrs · 35,999 cycles

FOUND EXISTING EXTERNAL REPAIR ON FUSELAGE BS 1120-1133 STR 18-20R. REPAIR REQURIES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPLACED REPAIR AT BS 1120-1133 STR 18R-20R PER SRM 53-30-3 FIG 3.

Part: STRINGER — UNKNOWN (BS 643-674) · airframe 50,970 hrs · 35,999 cycles

EXISTING STRINGER REPAIR IN FWD CARGO BAY AT BS 643-674 S28R. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIRED STRINGER AT BS 643-674, STR 28R PER SRM 53-10-3.

Part: STRINGER — UNKNOWN (BS 720F-740) · airframe 50,970 hrs · 35,999 cycles

MAPPED EXISTING REPAIR ON STRINGER, BS 720 F-740, STR 26R. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. STRINGER REPAIR AT BS 720F-740 STR 26 RT ORIGINAL THICKNESS IS 0.080 HAT SECTION IS 0.090 IT HAS 7 EACH FASTENERS IN ROW -A- 3/16" LOCK FASTENERS AND 5 EACH IN ROW -B- 3/16" LOCK FASTENERS REPAIR IS PER SRM 53-10-3 FIG 1 BASED ON A VISUAL EVALUATION WITH THE REPAIR INSTALLED AND GMM 6-2-100 CRITERIA IS A MAJOR REPAIR.

Part: FRAME — DAMAGED (BS 321) · airframe 50,970 hrs · 35,999 cycles

STA 321 STR 22L, FRAME CRACKED AT PREVIOUS REPAIR. REMOVED PREVIOUS REPAIR DOUBLER, FABRICATED, DRILLED, ALODINED, PRIMED REPAIR DOUBLER CAP, AND INSTALLED BS 321 STR 22L PER SRM 51-40-3.

Part: FRAME — DAMAGED (BS 312) · airframe 50,970 hrs · 35,999 cycles

STA 312 STR 22L, FRAME CRACKED AT PREVIOUS REPAIR. REMOVED AND REPLACED FRAME WEB BS 312 STR 21-23L PER SRM 51-30-2

Part: FLOORBEAM — DAMAGED (BS 1030) · airframe 50,970 hrs · 35,999 cycles

EXISTING UPPER FLOOR BEAM REPAIR AT BS 1030 LBL 10 WL 208, REPAIR REQUIRED EVALUATION FOR MAJ OR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USIING FAA APPROVED DATA. EVALUATED EXISTING REPAIR TO BS 1030 UPPER FLOORBEAM LBL 10 WL 208, TO BE A MAJOR REPAIR ACCOMPLISHED IAW SRM 53-10-2 FIG 7 AND SRM 53-10-8 FIG 3. REPAIR EVALUATION BASED ON A VISUAL INSPECTION WITH REPAIR INSTALLED. MAJOR REPAIR DETERMINATION BASED ON GMM 6-2-100 CRITERIA.

Part: FRAME — CRACKED (BS 613) · airframe 50,970 hrs · 35,999 cycles

FOUND CRACK IN STUB FRAME UPPER FLANGE IN FWD CARGO BAY BILGE AT BS 613, STR 26R. REPLACED STUB FRAME AT BS 613 STR 26R PER SRM 51-30-2.

Part: STRINGER — CRACKED (BS 915) · airframe 50,970 hrs · 35,999 cycles

FOUND LT W/W, 18A SHELF IS CRACKED, STA 915, LBL 63, WL 189. REMOVED AND REPLACED LEFT MLG W/W 18A SHELF STA 870-940 LBL 63 WL 189 PER SRM 51- 30-2

Part: REPAIR — IMPROPER (BS 1110) · airframe 50,970 hrs · 35,999 cycles

FOUND EXISTING FLOORBEAM REPAIR AT BS 1110, RBL 16 - LBL 35, WL 208. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. INSTALLED FLOORBEAM REPAIR AT B.S. 1110 RBL 16-LBL 35 WL 208 PER SRM 53-10-8.

Part: DOOR FRAME — GOUGED (EMERGENCY EXIT) · airframe 50,970 hrs · 35,999 cycles

AFT FRAME IS GOUGED NEXT TO THE CRANK ARM FITTING OF THE LEFT AFT EMERGENCY ESCAPE DOOR. REPAIRED FRAME AT LEFT AFT EMERGENCY ESCAPE DOOR PER SRM 51-40-3.

Part: STRINGER CLIP — CORRODED (BS 560) · airframe 50,970 hrs · 35,999 cycles

FOUND CORROSION ON STRINGER CLIP IN FWD CARGO BAY AT BS 560, STR 26L. REPLACED STRINGER CLIP AT BS 560 STR 26L PER SRM 51-20-1.

Part: SKIN — DENTED (BS 330) · airframe 50,970 hrs · 35,999 cycles

FOUND SIX INCH DENT IN SKIN AT BS 330 STR 20R. REMOVED DAMAGE ON SKIN BS 330 BETWEEN STR 20R & 21R FABRICATED REPAIR DOUBLER AND FILLER. ALODINE, PRIME INSTALLED AND PAINTED AT BS 330 BETWEEN STR 20R & 21 R IAW SRM 53-30-3 FIG 1.

Part: ACCESS DOOR — OUT OF POSITION (BULKHEAD) · airframe 50,968 hrs · 35,998 cycles

A/C TOOK OFF AND RETURNED TO GATE. FLT CREW SAID THE A/C WOULD NOT PRESSURIZE. MAIN ENTRY DOOR WAS CLOSED DOOR WAS JAMMED WOULDN'T OPEN. REMOVED DOOR SLIDE DOOR TRIM FOUND THE AFT ROLLERS WERE NOT IN THE ROLLER GUIDES OR IN THE CAMS. FOUND SOLID BULKHEAD ACCESS DOOR INTERFERING WITH ENTRY DOOR WHEN CLOSING. REPOSITIONED BULKHEAD ACCESS DOOR IN ITS TRACK. OPERATED MAIN ENTRY DOOR SEVERAL TIMES OPERATES NORMAL, ROLLERS ENGAGE CAMS AT ALL 4 POSITIONS AND HANDLE GOES OVER CENTER INDICATION NORMAL.

Part: TRANSMITTER — MALFUNCTIONED (NR 2 EPR) · airframe 50,777 hrs · 35,850 cycles

ON TAKEOFF ROLL, NR 2 EPR WOULD NOT ADVANCE PAST 1.4. ALL OTHER ENG INDICATIONS WERE NORMAL. REMOVED AND REPLACED NR 2 ENGINE EPR TRANSMITTER IAW AMM 77-11-011-4. NO HELP. RAN NR 2 ENG TO MAX PWR AND EPR INDICATION WOULD GO TO 1.6 EPR AND DROP TO 1.4 EPR WITH PWR ADVANCED. CONNECTED NR 3 EPR WIRING TO NR 2 EPR XMITTER. ENG CKS GOOD. WITH NR 3 ENG CONNECTED TO NR 2 WIRING GOT NO EPR INDICATION. WIRING IS SUSPECTED PROBLEM BETWEEN NR 2 EPR XMITTER AND NR 2 EPR INDICATOR.

Part: HANDLE — MALFUNCTIONED (MLG) · airframe 50,765 hrs · 35,842 cycles

AFTER GEAR RETRACTION, WITH GEAR HANDLE IN OFF POSITION, R GEAR DOOR LIGHT ON SO PANEL AND RED DOOR LIGHT ILLUMINATED. LIGHTS WENT OUT WHEN GEAR HANDLE WAS PUT BACK UP. RECYCLED ONCE THEN GEAR HANDLE LT UP PER QRH. ADJUSTED RT GEAR DOOR WARNING SWITCH REF M/M 32-62-011-4. A/C OK FOR SERVICE.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,850 hrs · 34,263 cycles

CORROSION (C53-111-01) ON TOP OF FRAME BS 720D, LBL 8-22 WL 156. REPAIRED PER EA 7-5310-69680 AND SRM 51-40-3.

Part: SKIN — CHAFED (FUSELAGE) · airframe 48,850 hrs · 34,263 cycles

THE FUSELAGE OUTER SKIN IS CHAFED AT BS 720D+13 INCHES STR 19L. BLENDED CHAFED AREA 1 X 2 X .027 FROM ORIGINAL .064 OUTER SKIN BS 720D+13 INCHES STR 19L. FOUND OUT OF LIMITS PER SRM 53-30-01. REPAIRED CHAFED AREA PER SRM 53-30-03 AND FED EX SR 27-57-056.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,850 hrs · 34,263 cycles

CORROSION (C53-224-01) ON FLOORBEAM UPPER FLANGE BS 480 LBL 25 TO LBL 45 WL 208. REPAIRED PER EA 7-5310-69493.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,850 hrs · 34,263 cycles

CORROSION (C53-111-01) ON STRINGER BS 660 STR 28R .

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,850 hrs · 34,263 cycles

CORROSION ON FUSELAGE OUTER SKIN AT FASTENER HOLE BS 700 BL 0 WL 148.5.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,850 hrs · 34,263 cycles

CORROSION ON FRAME BS 660 LBL 25 WL 149.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,850 hrs · 34,263 cycles

CORROSION ON FLOORBEAM UPPER FLANGE BS 312, LBL 23, WL 208.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,850 hrs · 34,263 cycles

CORROSION ON FLOORBEAM UPPER FLANGE BS 360, LBL 3 TO RBL 2, WL 208.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,850 hrs · 34,263 cycles

N00516 CORROSION (C53-111-01) ON FRAME B.S 640, RBL 4, WL 148.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,850 hrs · 34,263 cycles

CORROSION ON FLOORBEAM UPPER FLANGE B/S 344, LBL 25-45, WL 208. REMOVED CORROSION ON SEAT TRACK FLANGE BS 460, LBL 25, WL 208. FOUND TO BE OUT OF LIMITS PER SRM 53-10-01. REMOVED & REPLACED SEAT TRACK BS 344 TO 480, LBL 25, WL 208 PER SRM 51-30-02, 53-10-05.

Part: FRAME — CORRODED (FUSELAGE) · airframe 48,850 hrs · 34,263 cycles

BS 1090 FRAME PUNCTURED BY FLOOR PANEL FASTENERS, LBL 21 WL 156. INSTALLED THE FABRICATED DOUBLER AT BS 1090 FRAME LBL 21 WL 156 IAW SRM 51-40-3. REINSTALLED STANTION PER SRM 51-30-2.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,850 hrs · 34,263 cycles

CORROSION ON FRAME BS 720C, LBL 4 - RBL 4, WL 148. REPAIRED PER SRM 53-10-4.

Part: SKIN — DENTED (FUSELAGE) · airframe 48,850 hrs · 34,263 cycles

DENT IN FUSELAGE SKIN BS 430, STR 20-21 RT.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,850 hrs · 34,263 cycles

CORROSION ON FLOORBEAM UPPER FLANGE BS 328, LBL 33 TO LBL 23, WL 208.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,850 hrs · 34,263 cycles

CORROSION ON FRAME BS 720C, LBL 10, WL 149. REPAIRED PER SRM 53-10-4.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,850 hrs · 34,263 cycles

CORROSION ON FLOORBEAM UPPER FLANGE BS 620, RBL 25 TO LBL 45, WL 208. CORROSION ON FLOORBEAM UPPER FLANGE BS 620, RBL 25. FOUND TO BE OUT OF LIMITS. REMOVED DAMAGED AND REPAIR FLOORBEAM UPPER FLANGE AT BS 620, RBL 25 IAW SRM 53- 10-8.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,850 hrs · 34,263 cycles

CORROSION (C53-111-01) ON SKIN BS 720A LBL 2 WL 148.

Part: FRAME — PUNCTURED (FUSELATGE) · airframe 48,850 hrs · 34,263 cycles

BS 1050 FRAME PUNCTURED BY FLOOR PANEL FASTENER, RBL 21, WL 156. BS 1050 FRAME RBL 21 W/L 156 FOUND TO BE OUT OF LIMITS. REMOVED DAMAGED & INSTALLED REPAIR DOUBLER AT BS 1050, RBL 21, WL 156 IAW SRM 51-30-2.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,850 hrs · 34,263 cycles

CORROSION (C53-224-01, 3) ON BS 1176 FRAME, WL 208, LBL 60 TO SKIN. REPAIRED PER 51-30-2, 51-30-5 AND 65C33557, FEDEX MM 36-00-01.

Part: FRAME — PUNCTURED (FUSELAGE) · airframe 48,850 hrs · 34,263 cycles

BS 1130 FRAME PUNCTURED FROM FLOOR PANEL FASTENER LBL 21 - WL 153.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,850 hrs · 34,263 cycles

CORROSION (C53-111-01) ON STRINGER 27L BS 700.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,850 hrs · 34,263 cycles

CORROSION ON SKIN BS 720D-720E LBL 24 - WL 151.

Part: SKIN — CANNING (FUSELAGE) · airframe 48,850 hrs · 34,263 cycles

LWR FUSELAGE EXTERIOR SURFACE BS 450 STR 21R - 22R SKIN OIL CANNING. DENT AT BS 450, STR 21 - 22 RT FOUND TO BE OUT OF LIMITS PER SRM 53-30-1. REPAIRED DENT PER FED EX EA 7-5330-54488.

Part: SPLICE — CORRODED (STRINGER) · corrosion level 2 · airframe 48,850 hrs · 34,263 cycles

CORROSION (C53-111-01) ON STRINGER SPLICE BS 585-595 STR 26L.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,850 hrs · 34,263 cycles

CORROSION AROUND FASTENER HOLES, BS 740-759, LBL 6-RBL 6, WL 138. REPAIRED PER SRM 53-10-1, 53-10-2, AND 51-40-2.

Part: WARNING LIGHT — ILLUMINATED (COCKPIT)

USING NR 2 ENG RT BLEED TO PROVIDE AIR TO RT PACK, LWR AFT BODY OVERHEAD LIGHT ILLUM. RED TABS FOLLOWED.

Part: WEB — CORRODED (FUSELAGE)

CORROSION (C53-224-04) BS 1148, LBL 1.5 TO LBL 5, WL 208 AT NUT PLATE HOLE IN SHEAR WEB PREVIOUS BLEND. *S/D* REMOVED AND REPLACED PER EA 7-5310-52471 AND FEDEX SRM 51-40-2.

Part: STRINGER — CORRODED (FUSELAGE)

CORROSION (C53-113-01,1) ON STRINGER 26 RT AT BS 720F+16 INCHES. *S/D* REMOVED AND REPLACED PER FEDEX SRM 53-10-3 USING MATERIAL BAC 1498-147, LOT 381472, BAC 1498-131 LOT 269814.

Part: ANGLE — CORRODED (FUSELAGE)

WHILE WORKING NR 495 FOUND CORROSION (C53-113-01) ON BS 740 CIRCUMFERENTIAL CHORD BETWEEN STR 27 RT AND STR 28 RT. *S/D* REMOVED AND REPLACED PER FEDEX SRM 51-30-2, 51-10-2, 51-20-4.

Part: FLOORBEAM — CORRODED (FUSELAGE)

WHILE WORKING CORROSON BS 1166, LBL 11.5 TO LBL 5, WL 208 AT NUT PLATE HOLE IN SHEAR WEB, PREVIOUS BLEND. FOUND TOP FLANGE UNDER NUT PLATE CORRODED OUT OF LIMITS. *S/D* REPAIRED PER IAW FEDEX SRM 53-10-1, EA 7-5310-53825.

Part: FLOORBEAM — CORRODED (FUSELAGE)

WHILE WORKING EO 7-2610-733195 PT 1 FOUND 1130 FLOORBEAM LWR CHORD CORRODED LBL 8 TO LBL 40. *S/D* REMOVED AND REPLACED PER IAW FEDEX EA 7-5310-52469.

Part: FRAME — CORRODED (FUSELAGE)

CORROSION (C53-224-05) ON LONGITUDINAL UPPER CHORD AROUND NUT PLATE HOLES BS 760 - 846, LBL 45, WL 208. *S/D* REMOVED AND REPLACED PER FEDEX SRM 53-10-1, FIG 8, 51-30-5, 51-60-6, 51-30-8 & FEDEX DRAWING 65-16279.

Part: SILL — CRACKED (FUSELAGE)

CRACK IN RT WHEEL WELL STRUCTURAL WEB ABOVE TERMINAL FITTING AT BS 875, RBL 69, WL 188. *S/D* FAB AND REPAIR DOUBLER PER IAW FEDEX SRM 51-40-2, FIG 1, 51-30-3 FIG 1.

Part: BEAM — GOUGED (FUSELAGE)

GOUGE IN VERTICAL BEAM RBL 26.83, WL 264 I/B SIDE BS 1182. *S/D* BLENDED GOUGE PER IAW FEDEX SRM 53-10-1, 51-40-3.

Part: DUCT — BROKEN (NR 1 PYLON)

98-0180 STA-MEM: SHORTLY AFTER T/O THE ENG 1 STRUT OVERHEAT LIGHT CAME ON. COMPLETE THE RED TAB PROCEDURES PAGES 2-7-10 AND 2-7-11 AND THE LIGHT EXTINGUISHED AFTER RETARD THE NR 1 THRUST LEVER NR 1 THRUST WAS SLOWLY RESTORED AND THE LIGHT REMAIN EXTINGUISH WITH A GOOD OVERHEAT SYS TEST. RED TABS SAY BLEED AIR LEAK IS ON THE FUSELAGE SIDE OF THE BLEED AIR VALVE. FOUND BROKEN THRUST REVERSER PNEUMATIC SUPPLY LINE FROM 8TH AND 13TH STAGE DUCT. FITTING ON DUCT ELBOW ALSO HAS DAMAGE THREADS. REINSTALLED BLEED DUCT. NEED LEAK CHECK ON DUCT AND SHIMMING OF FIREWALL SWIVEL AND LEAK CHECK. ADJUSTED THEN TIGHTENED SWIVEL COUPLING AND V CLAMPS. ALSO, REMOVED AND REPLACED NR 1 ENG BLEED DUCTING ALL FITTINGS AND CL

Part: DUCT — CRACKED (NR 1 ENGINE)

98-0181- STA-MEM, NR 1 ENG HAD STRUT OVERHEAT ON TAKEOFF PULLED THRUST LEVER BACK AND PERFORMED RED TAB PROCEDURES. REMOVED PANELS FROM LWR STRUT. FOUND LINE PN S145061408-0090 IS A BRAID LINE CRACK IN MIDDLE HALFWAY. CHECK VALVE FOR PROPER INSTALL. VALVE INSTALLED CORRECT PER MM 78-30-10 PG 3. REMOVED THRUST REVERSER DUCT FROM NR 1 ENGINE HYDRAULIC LINE ABOVE. REMOVED DUCT AND VALVES IAW 36-10-00. REINSTALLED DUCT, BLEED VALVE 13TH STAGE VALVE. NEED LEAK CK AT PWR FOR 8 MIN PERFORM HIGH PWR RUN. NO LEAK, NO STRUT OVERHEAT.

Part: BELLFRAME — DAMAGED (BS 680)

STA-TUL: LOWER FWD CARGO HAS DAMAGED BELLFRAME BS 680 BETWEEN STR 25R AND 23R. DAMAGED AREA OF BELLFRAME REMOVED. REPAIR OF FRAME PER SRM 51-40-3.

Part: SKIN — CORRODED (BS 684-689)

CORROSION ON SKIN BS 684 TO 689 AT STR 27R. REMOVED CORRODED SKIN AND REPAIRED WITH DOUBLER PER SRM 53-30-3.

Part: STRINGER — DAMAGED (BS 683-710)

DRILL MARKS ON BOTH SIDES OF STR 26R, BS 683 TO 710 IN FWD CARGO. REMOVED DAMAGED AREA OF STRINGER PER SRM 51-10-6. INSTALLED REPAIR PER SRM 53-10-3.

Part: STRINGER — CORRODED (BS 680-715)

LWD FWD CARGO CORROSION ON STR 27R BETWEEN BS 680 TO 715. REMOVED STR 27R CORRODED SECTION BETWEEN BS 680 TO 715. REINSTALLED NEW STR SECTION BS 680 TO 715 PER SRM 53-10-3.

Part: FLOORBEAM — DAMAGED (BS 950)

MAIN CARGO, PREVIOUS DAMAGE DOUBLER DRILLED HOLE IN FLOORBEAM BS 950F, RBL 3. REMOVED DAMAGE AND REPAIRED FLOORBEAM PER SRM 53-10-8 FIG 8.

Part: FRAME — DENTED (BS 500)

LOWER FWD CARGO FRAME DENTED BS 500, BETWEEN STR 24L AND 25L. REPAIRED BELL FRAME BS 500 PER SRM 51-40-3 AND EA 7-5310-29526.

Part: FRAME — DENTED (BS 1010)

DENT IN FRAME BS 1010 ABOVE STR 26R IN AFT CARGO. REMOVED DAMAGE FROM FRAME PER SRM 53-10-4, INSTALLED REPAIR DOUBLER PER SRM 53-10-4 FIG 1 PG 3 AND 4.

Part: FRAME — DENTED (BS 520)

LOWER FWD CARGO COMP LT FS 520 BELL FRAME IS DENTED IN SEVERAL AREAS BETWEEN STR 23L AND 26L. REPAIRED BELL FRAME PER SRM 51-40-3 AND WA 7-5310-29526.

Part: FRAME — DAMAGED (BS 1090)

NR 1321 71C709-02, AFT LWR CARGO 2 EA DENTS IN BELLFRAME BS 1090, STR 26L - 27L. REMOVED DAMAGED AREA OF FRAME PER SRM 53-10-4. INSTALLED REPAIR DOUBLER PER SRM 53-10-4 FIG 1 PG 3 AND 4.

Part: FRAME — DAMAGED (BS 580)

NR 0322 71C207-00, LOWER FWD, CARGO BELLFRAME DAMAGED ABOVE STR 25L TO STR 24L BS 580. REMOVED DAMAGED AREA, INSTALLED REPAIR DOUBLER PER SRM 51-40-3.

Part: KEEL BEAM — CRACKED (BS 872)

NR 0507 71C503-00, KEEL BEAM BS 872, ABOVE FWD 870 KEEL BEAM FITTING CHORD CRACKED IN RADIUS THROUGH 2ND FASTENER LEFT SIDE. REMOVED DAMAGED AREA AND INSTALLED DOUBLER PER EA 7-5310-29533 AND SERVICE BULLETIN 727-53-208.

Part: FRAME — DAMAGED (BS 500)

NR 0328, FWD LOWER CARGO. DAMAGED BELLFRAME, BS 500, STR 23 TO 24R. REPAIRED BELLFRAME BS 500 PER SRM 53-10-04.

Part: SWITCH — INOPERATIVE (RT MLG DOOR)

RIGHT MAIN GEAR DOOR REMAINED LIT DURING RETRACTION. RECYCLED GEAR PER EMERGENCY PROCEDURES CHECK LIST. LIGHT REMAINED ILLUMINATED DURING RECYCLE, LIGHT WAS OUT DURING PREFLIGHT/GND OPERATION. REMAINED ON FOR EXTENSION/LDG. DUPLICATED RIGHT DOOR LIGHT ON/OFF AND FRONT PANEL DOOR WARNING LIGHT ON/OFF. REMOVED AND REPLACED RIGHT MAIN LANDING GEAR DOOR WARNING SWITCH, PER MAINTENANCE MANUAL 32-62-11. OPERATION CHECKED PER MAINTENANCE MANUAL 32-62-11 PAGE 501.

Part: HYD SYST — FAILED (A-HYD SYST)

AFTER LOWERING GEAR AND FLAPS TO 5 DEGREES A-SYSTEM FAILURE OCCURRED. ENGINES OPERATED APPROX 4 MINUTES WITH PUMPS SHUT OFF. QUANTITY AND PRESSURE BOTH ZERO. ALL CHECKLIST PERFORMED AND LANDING NORMAL. *S/D* REPAIRED SLAT ACTUATOR BRACKET PER SRZ 27-57-028. COMPLIED WITH BRACKET MOD PER ENG AUTH 7-5700-35565, OK FOR SERVICE. REMOVED AND REPLACED A-SYS PUMP PRESS AND CASE DRAIN FILTERS, NO METAL FD. REMOVED AND REINSTALL NR 2 SLAT ACTUATOR PER M/M 27-81-32. REPLACED DAMAGED NR 2 SLAT ACTUATOR PRESS AND RETURN LINES AND DAMAGED WING ANTI-ICE DUCT. SERVICED A-SYS HYD PER M/M 12-12-0 BLED. OPERATED LEAK CK NR 2 SLAT ACTUATOR, LINES AND FILTERS. LEAK CKD GOOD.

Part: SKIN — DAMAGED (BS 1342)

MISC WORKING FASTENERS IN SKIN AT BS 1342 LBL 45 WL 260 TO 270. ACCESSED AREA, CUT OUT DAMAGED SKIN AND U-CHANNEL, REPAIRED PER SRM 54-30-3 FIG 7, INSTALLED ALL ITEMS REMOVED FOR ACCESS.

Part: STRINGER — CORROSION (FUSELAGE)

CORROSION IN SEVERAL PLACES IN STR AND TWO STR CLIPS AT BS 560, 568, AND 574, RBL 15, WL 150. REMOVED CORROSION, FABRICATED REPLACEMENT PARTS, AND INSTALLED PER FEDEX SRM 53-10-3 AND SRM 53-10-2.

Part: TRACK — CRACKED (NR 5 TE FLAP)

RT WING NR 5 FLAP TRACK AUXILIARY SPAR HAS A 1 INCH CRACK JUST ABOVE INBOARD AUXILIARY SPAR FLAP TRACK BOLT. REPAIRED PER FEDEX EA 7-5710-26103.

Part: KEEL BEAM — CORRODED (BS 720)

CORROSION ON FWD BAY KEEL BEAM BS 720B +1 AND +9, RBL 7, WL 150. REMOVED CORROSION ON KEEL BEAM FLANGES AND REPAIRED PER FEDEX EA NR 7-5310-26107. ADDITIONAL CORROSION WAS DISCOVERED BENEATH A PREVIOUS REPAIR ON SKIN AROUND RAM AIR INLET ACTUATOR ACCESS DOOR. REMOVED PREVIOUS REPAIR AND REPAIRED DAMAGE PER FEDEX EA NR 7-5330-26134.

Part: SHEAR TIE — CORRODED (BS 680)

CORROSION (C53-113-01-1) ON FRAME AND SHEAR TIE AT BS 680 LBL 17 - 20, WL 150. CORROSION REMOVAL ON FRAME FOUND TO BE WITHIN LIMITS PER FEDEX SRM 53-10-1, CORROSION ON SHEAR TIE FOUND TO BE OUT OF LIMITS PER FEDEX SRM 53-10-1, TREATED, ALODINED, PRIMED CORRODED AREA ON FRAME AND INSTALLED NEW SHEAR TIE BS 680, LBL 17 - 20, WL 150.

Part: FLOOR BEAM — DAMAGE (BS 920)

WHILE ACCESSING FOR EO 7-5300-7-2304M PART 3, DISCOVERED TOOLING DAMAGE ON TOP OF THE BS 920 FLOOR BEAM FROM LBL 15.5 TO LBL 19, WL 208. REPAIRED TOOLING DAMAGE PER FEDEX 7-5310-7-22611 AND EWO 95-3210.

Part: ELEV SUPT RIB — CRACKED (ELEVATOR)

LT ELEVATOR SUPPORT RIB AT ELEVATOR STA 99.79 IS CRACKED AT I/B LOWER CORNER. REMOVED AND REPLACED LT ELEVATOR SUPPORT RIB AT ELEVATOR STA 99.79.

Part: SKIN — CORRODED (BS 620)

CORROSION ON BILGE SKIN ALONG STR AT BS 620 - 640, RBL 8 WL 150. REMOVED CORROSION ON BILGE SKIN ALONG STR AT BS 620 - 640 RBL 8 WL 150, BS 620 - 628 AND BS 631 - 640 FOUND TO BE WITHIN LIMITS. BS 629 - 630 FOUND TO BE OUT OF LIMITS PER FEDEX SRM 53-30-1 FABRICATED AND INSTALLED REPAIR DOUBLER AT BS 629 - 630 PER FEDEX SRM 53-30-3, FIG 3.

Part: STRINGER — CRACKED (VERT FIN)

NR 7 STR IS CRACKED AT VERTICAL FIN STA 133.80 LT SIDE. REMOVED DAMAGE, FABRICATED REPAIR PARTS AND INSTALLED PER FEDEX 55-30-4.

Part: STRINGER — CORROSION (BS 720)

CORROSION ON STRINGER AT BS 720F PLUS 16 LBL 23 WL 152. REPAIRED STR PER FEDEX SRM 53-10-5.

Part: STRINGER — CRACKED (VERT FIN)

NR 8 STRINGER IS CRACKED AT VERTICAL FIN STA 133.80 RT SIDE. REMOVED DAMAGE, FABRICATED REPAIR PARTS AND INSTALLED PER FEDEX 55-30-4.

Part: FRAME — CRACKED (BS 320)

CRACK IN FRAME AT BS 320, JUST ABOVE STR 22L APPROX WL 175 LBL 49. REPAIRED CRACK IN FRAME AT BS 320, JUST ABOVE STR 21L APPROX WL 175 LBL 49 PER FEDEX SRM 51-40-02.

Part: STRINGER — CORRODED (BS 1613)

CORROSION IN STRINGER AT BS 1613 LBL 15 WL 150. REPAIRED STR PER SRM 53-40-3.