N487FE

Part: WIRE HARNESS — BURNED (APU) · airframe 42,969 hrs · 29,386 cycles

DURING APU START AT APPROX 55 SECONDS SMOKE POURING FROM APU - EGT APPROX 525. SHUTDOWN USING FIRE HANDLE & SHOT FIRE BOTTLE. STRONG BURNED RUBBER/WIRE INSULATION TYPE ODOR IN W/W. NO FIRE INDICATION IN COCKPIT. AS PRECAUTION APU CONTROL BREAKER PULLED & COLLARED ON J9 PANEL IN E&E. OPENED APU SHROUD PANEL IN RT W/W & REMOVED SHROUD OVER BURNER CAN. FOUND FIRE DAMAGE TO WIRING AND CLAMP INSULATORS IN AREA AROUND UPPER END OF COMBUSTION CAN. TORCHED MARK ON APU CASE NEXT TO LINE COMING FROM THERMOSTAT SELECTOR SOLENOID VALVE. NO DAMAGE FOUND ANYWHERE EXTERNAL OF THE APU SHROUD IN EITHER WHEEL WELL.

Part: AIR DUCT — CONTAMINATED (AIR CON) · airframe 42,913 hrs · 29,344 cycles

STRONG ODOR OF FUEL FUMES IN COCKPIT, INCREASED AFTER TAKEOFF DURING CLIMB. UPON ARRIVAL, NOTICED STRONG DIESEL ODOR IN ACFT EE AND PIT AREAS ALSO IN FLT DECK. OUR HEAT DUCTING WAS ALSO STRONG ODOR. CHECKING COALASTER BAGS. SUSPECT HEAT CART CONTAMINATION INTO CONDITIONED AIR MANIFOLD. ATB, EMERG DECLARED. OUR GSE VERIFIED THE HEAT CART INJECTOR LINE WAS LEAKING DIESEL INTO THE HEAT CART AIR SUPPLY FAN. COALASTER BAGS HAD HEAVY SMELL CONTAMINATION. R & R BOTH COALASTER BAGS REF MM 21-55-051-4. RAN APU AND PACKS. CONDITIONED AIR CLEARED UP NO ODORS NOTICED. RAN ENGS JRH WITH PACKS AND BLEEDS ON. SYS GRD OPS CHECKS OK. OK TO CONTINUE.

Part: SKIN — MISREPAIRED (BS 1175-1183) · airframe 42,731 hrs · 29,193 cycles

IMPROPER REPAIR INSTALLED STA 1175 TO 1183, STR'S 23L - 24L". REMOVED PREVIOUS REPAIR. FABRICATED DOUBLER USING 2024T-3 .090 DIMS 8.25" X 10 5/8" AND FILLER USING 2024T-3 .080 DIMS 3" X 3.2" AND INSTALLED IAW EA 6-5330-135578.

Part: SKIN — GOUGED (CARGO DOOR) · airframe 42,731 hrs · 29,193 cycles

MCD INTERIOR SKIN GOUGED STA 618 STR 8L. TRIMMED DAMAGED AREA AT MCD INTERIOR SKIN STA 618 STR 8L, FABRICATED REPAIR DOUBLER FROM 2024T3 0.071" DIM 6" X 10.6250" AND INSTALLED DOUBLER REPAIR IAW EA 7-5230-142192.

Part: SHEAR TIE — CORRODED (BS 950A) · corrosion level 2 · airframe 42,731 hrs · 29,193 cycles

AFT CARGO COMP BS 950A FRAME SHEAR TIE STRINGERS 28L - 29L HAVE CORROSION CUT OUT DAMAGED SHEAR TIE FLANGE DIM 6 3/4" IAW SRM 53-10-4 FIG 15 FABRICATED REPAIR DOUBLER FROM 7075 T6 .080" DIM 6 3/4" X 2 3/8'" IAW SRM 53-10-4 FIG 15. INSTALLED REPAIR DOUBLER IAW SRM 51-30-2 AND 53-10-4 FIG 15 REV 103

Part: SKIN — MISREPAIRED (BS 1183-1200) · airframe 42,731 hrs · 29,193 cycles

IMPROPER REPAIR INSTALLED AT STA 1183-1200 S23-24L ACCOMPLISHED REPAIR AT BS 1183-1200 S23-24L, FABRICATED DOUBLER FROM 2024T3 0.080" DIM. 16 3/4 X 17 1/4", FILLER 2024T3 0.071" DIM. 4 1/4" X 9 1/2" AND 7 1/2" X 1" STRUCTURAL FILLER PER SRM 53-30-3 FIG 3A. INSTALLED ALL REPAIR PARTS IAW SRM 53-30-3.

Part: SKIN — PUNCTURED (RUDDER) · airframe 42,731 hrs · 29,193 cycles

PUNCTURE IN SKIN LOWER RUDDER LT SIDE, APPROX VERTICAL STABILIZER FIN STA 110. CUT DAMAGED SECTION OF RUDDER SKIN DIM 1" X 1 1/2" IAW SRM 51-10-1 AND 55-20-3 FIG 1. FABRICATED REPAIR DOUBLER FROM 2024T3 .032" DIM 4 3/4 X 4 3/4" IAW SRM 55-20-3 FIG 1 INSTALLED REPAIR DOUBLER IAW SRM 51-30-2 AND 55-20-3 FIG 1 REV 103.

Part: SKIN — CRACKED (BS 1223) · airframe 42,731 hrs · 29,193 cycles

AFT AIRSTAIR AREA- LT LOWER TORQUE BOX LIGHTING HOLE IS CRACKED AT BS 1223. CUT OUT DAMAGED AREA OF LOWER TORQUE BOX WEB AT BS 1223 LT IAW SRM 51-40-2 FIG1. FABRICATED REPAIR DOUBLER FROM 7075-T6 .032"X 17/8"X53/4" IAW SRM 51-40-2 FIG 1. INSTALLED DOUBLER IAW SRM 51-40-2 FIG 1 REV 103.

Part: SHEAR TIE — CORRODED (BS 950B S27-28L) · corrosion level 2 · airframe 42,731 hrs · 29,193 cycles

CORROSION ON SHEAR TIE AT BS 950B BETWEEN STRINGERS 28L AND 27L CUT DAMAGED SHEAR TIE FLANGE DIM 5 5/8" IAW SRM 53-10-4 FIG 15 FABRICATED SHEAR TIE FROM 7075 T6 .080" DIM 5 5/8" X 2 1/2" IAW SRM 53-10-4 FIG 15 INSTALLED SHEAR TIE IAW SRM 51-30-2 AND 53-10-4 FIG 15 REV 103

Part: SKIN — CRACKED (NR 6 SLAT) · airframe 42,731 hrs · 29,193 cycles

NUMBER 6 SLAT TE IS CRACKED AT OUTBD HOOK AFT MOUNT BOLT C/W HFEC IAW NDTM PT6 51-00-00 FIG 23 CRACKS STOP AT EXISTING FASTENER HOLES. FABRICATED REPAIR DOUBLER FROM 2024T3 .125" DIM 4" X 3 1/2" IAW SRM 57-50-3 FIG 10. INSTALLED DOUBLER IAW SRM 57-50-3 FIG 10 AND 51-30-2 REV 103

Part: SHEAR TIE — CORRODED (BS 700 S26-27R) · corrosion level 2 · airframe 42,731 hrs · 29,193 cycles

CORROSION ON SHEAR TIE AT BS 700 BETWEEN STRINGERS 27R AND 26R REMOVED SHEAR TIE TEE CLIP IAW SRM 51-30-2 FABRICATED NEW SHEAR TIE FROM BAC 1505-100044 7075 T6511 DIM 6 1/2" IN LENGTH IAW DRAWING 65-15938 AND SRM 51-30-5 INSTALLED NEW SHEAR TIE TEE CLIP IAW SRM 51-30-2 REV 103.

Part: KEELBEAM — CRACKED (BS 870) · airframe 42,731 hrs · 29,193 cycles

RT MLG WW, RT KEEL BEAM IS CRACKED AT FWD FASTENER, BS 870 PLUS 3" RBL6. REPAIRED KEEL BEAM IAW EA 7-5310-135573.

Part: SEAT TRACK — DAMAGED (BS 600) · airframe 42,731 hrs · 29,193 cycles

SEAT TRACK DAMAGED STA 600, BL 0. REMOVED SEAT TRACK SECTION. FABRICATED NEW SECTION USING BAC1520-792 7178 T6511 DIMS 120" AND INSTALLED IAW SRM 53-10-2 AND SRM 51-30-2.

Part: SKIN — MISREPAIRED (BS 259 S18L) · airframe 42,731 hrs · 29,193 cycles

NON-COMPLIANT REPAIR LOCATED AT STA 259, STR 18L. REMOVED PREVIOUS REPAIR, CUT OUT DAMAGE AREA DIM 17.5" X 22", FABRICATED REPAIR DOUBLERS (-1) FROM 2024T3 .090" DIM 25.X22.125" (-2) FROM 2024T3 .063 DIM 27.375"X13.625", REPAIR PARTS AND INSTALLED 2EA REPAIR DOUBLERS, 03EA STRUCTURAL FILLERS, BUTT STRAP DOUBLER, BUTT STRAP PLATE, 04EA FILLERS, TAPER FILLER AND AFT UPPER SKIN FILLER IAW EA 7-5330-135577.

Part: FLOORBEAM — CORRODED (BS 720) · corrosion level 2 · airframe 42,731 hrs · 29,193 cycles

CORROSION ON LOWER FLANGE OF MAIN CABIN FLOORBEAM AT BS 720, BL0 TO LBL 35. CUT OUT 2 EACH DAMAGED AREAS DIMS 1.75" X .9" EACH, FABRICATED TWO ANGLES USING 7075-O .071 DIMS 34.25" X 2.75" AND 29 5/8" X 2.5", HEAT TREATED ANGLES FROM 7075-O TO T6 CONDITION IAW FASI ENG REPORT 2-37153-801 REV A. FABRICATED 2 FILLERS USING 7075T- 6 .125 DIMS 1.75" X .9" EACH AND INSTALLED ALL REPAIR PARTS IAW SRM 53-10-8 AND 51-30-2.

Part: STRINGER — CORRODED (BS 550 S27L) · corrosion level 2 · airframe 42,731 hrs · 29,193 cycles

CORROSION ON STR 27L, AT BS 550 UNDER CLAMP STAND-OFF BRACKET. REMOVED CORROSION IAW SRM 51-10-6 FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1. CUT OUT DAMAGED AREA IAW SRM 53-10-3 FIG 1. FABRICATED NEW SECTION OF STRINGER 20" X 2 1/2" IAW SRM 53-10-3 FIG 1 REV 103. FABRICATED NEW SECTION OF STRINGER FROM BAC1498-139 FABRICATED 4 ANGLES FROM BAC1493-513 AND 2 CHANNELS FROM BAC1493-412 IAW SRM 53-10-3 FIG 1. INSTALLED IAW SRM 53-10-3 FIG 1 REV 103

Part: SKIN — GOUGED (RT WING TE FLAP) · airframe 42,731 hrs · 29,193 cycles

PREVIOUS REPAIR DOUBLER GOUGED- RT WING INBD FOREFLAP L/E LOWER SURFACE AT INBD MOUNT FITTING, REMOVED PREVIOUS REPAIR DOUBLER IAW SRM 51-30-2 REV 103 FABRICATED NEW REPAIR DOUBLER FROM 2024T3 .063" PO 9009134 DIM 6" X 6 3/4" IAW SRM 57-50-4 FIG 1 AND 57-50-3 FIG 3. INSTALLED NEW REPAIR DOUBLER IAW SRM 57-50-4 FIG 1 AND 51-30-2 REV 103

Part: SHEAR TIE — CORRODED (BS 1050 S26-27L) · corrosion level 2 · airframe 42,731 hrs · 29,193 cycles

AFT CARGO BAY BS 1050 - BETWEEN S26 & 27L FRAME SHEAR TIE IS BULGED. REMOVED SHEAR TIE IAW SRM 51-30-2. FABRICATED NEW SHEAR TIE FROM BAC1506-1054 DIM 6" IN LENGTH IAW DRAWING 69-20689 AND SRM 51-30-5 INSTALLED NEW SHEAR TIE IAW SRM 51-30-2 REV 103.

Part: SEAT TRACK — CORRODED (BS 480-690) · corrosion level 2 · airframe 42,731 hrs · 29,193 cycles

CORROSION SEAT TRACK FLANGES MAIN CABIN BS 480-690, RBL 45. REMOVED SEAT TRACK SECTION. FABRICATED NEW SEAT TRACK SECTION USING BAC1520-792-7178T6 DIMS 209.250", FABRICATED ANGLES SPLICE USING BAC1503-100122-7178T6 DIMS 14" (2 EACH), FABRICATED STRAP USING 7075T-6 .250 DIMS 8" X 2" AND INSTALLED IAW SRM 53-10-5.

Part: SHEAR TIE — CORRODED (BS 500 S26-27R) · corrosion level 2 · airframe 42,731 hrs · 29,193 cycles

CORROSION ON SHEAR TIE AT BS 500 BETWEEN STRINGERS 27R AND 26R. REMOVED CORRODED SHEAR TIE IAW SRM 51-30-2. FABRICATED NEW CLIP FROM BAC 1505-100044 7075 T6511, DIM 6.5" LENGTH IAW MFG DWG NR 69-43683, REV 17A AND SRM 51-30-5. INSTALLED NEW SHEAR TIE IAW SRM 51-30-2, REV 103.

Part: SEAT TRACK — CORRODED (BS 480-680) · airframe 42,731 hrs · 29,193 cycles

SEAT TRACK CORRODED, STATION 480 - 680, LBL 25. REMOVED SEAT TRACK SECTION. FABRICATED NEW SECTION USING BAC 1520-7927178T6511, DIMS 209 1/2", FABRICATED SPLICE USING BAC1503-100122-7178 DIMS 14" EACH, FABRICATED ANGLE AND PLATE USING 7075T6 .250 DIMS 8" X 2" AND INSTALLED IAW SRM 53-10-5 AND SRM 53-10-2.

Part: FRAME — CORRODED (BS 500 S26-27R) · airframe 42,731 hrs · 29,193 cycles

CORROSION ON FRAME AT BS 500 BETWEEN STRINGERS 27R AND 26R. CUT OUT CORRODED SECTION OF FRAME IAW SRM 51-40-2, FIG 1 FABRICATED FILLER AND DOUBLER IAW SRM 51-40-2, FIG 1 AND 53-10-2 INSTALLED REPAIR PARTS IAW SRM 51-40-2 FIG 1 AND 51-30-2, REV 103.

Part: FLOORBEAM — CORRODED (BS 620) · corrosion level 2 · airframe 42,731 hrs · 29,193 cycles

FLOORBEAM CORRODED STATION 620, LBL 25-45. CUT OUT DAMAGED AREA DIMS 2 3/8" X 1". FABRICATED 2 EACH ANGLES USING 7075-O .090 DIMS 15 3/4" X 2 1/2" AND 10 3/8" X 2 3/8", HEAT TREATED ANGLES TO T6 CONDITION IAW ER 2-37153-801 REV A. FABRICATED FILLER USING 7075T-6 .125 DIMS 2 3/8" X 1" AND INSTALLED ALL REPAIR PARTS IAW SRM 53-10-8.

Part: FRAME — DENTED (BS 1090 S26L) · airframe 42,731 hrs · 29,193 cycles

AFT CARGO COMPARTMENT BS 1090 ABOVE STR 26L FRAME UPPER FLANGE IS DENTED AT RADIUS. CUT OUT DAMAGED UPPER FLANGE OF FRAME ABOVE STR 25L DIM 1"X1" AND ABOVE STR 26L, DIM 1"X1" IAW SRM 51-10-1. FABRICATED REPAIR DOUBLER FROM 7075 0 .080 DIM 24"X6.3750" IAW SRM 51-40-3, FIG 1 AND 53-10-2 FIG 5 INSTALLED REPAIR DOUBLER IAW SRM 51-30-2, REV 103.

Part: SEAT TRACK — CORRODED (BS 480-620) · corrosion level 2 · airframe 42,731 hrs · 29,193 cycles

SEAT TRACK CORRODED STATION 480 - 620, LBL 45 REMOVED SEAT TRACK SECTION. FABRICATED NEW SECTION USING BAC1520-792 7178T6511 DIMS 206", FABRICATED 2 ANGLES USING BAC1503-100122 7178-T6 DIMS 14" X 2 1/2" AND ONE STRAP USING 7075-T6 .250 DIMS 9" X 2" AND INSTALLED IAW SRM 53-10-5.

Part: SEAT TRACK — CORRODED (BS 690-740) · corrosion level 2 · airframe 42,731 hrs · 29,193 cycles

SEAT TRACK CORRODED STATION 690 - 740, RBL 45 REMOVED SEAT TRACK SECTION. FABRICATED NEW SEAT TRACK SECTION USING BAC1520-792-7075T6 DIMS 172" AND INSTALLED IAW SRM 53-10-2 AND SRM 51-30-2.

Part: SKIN — GOUGED (LT WING TE FLAP) · airframe 42,731 hrs · 29,193 cycles

LT INBD FORE FLAP GOUGED AT OUTBD LOWER LEADING EDGE SURFACE. REMOVED PREVIOUS REPAIR IAW SRM 51-30-2. FABRICATED REPAIR DOUBLER USING 2024 T-3, .063" X 5" X 5" IAW SRM 57-50-4 FIG 1 AND 57-50-2 FIG 3. INSTALLED NEW REPAIR DOUBLER IAW SRM 57-50-4 FIG 1 AND 51-30-2, REV 103.

Part: FLOORBEAM — CORRODED (BS 1130) · corrosion level 2 · airframe 42,731 hrs · 29,193 cycles

FLOORBEAM CORRODED STA 1130 RBL35-55. CUT OUT DAMAGED AREAS DIMS 3 1/8" X 1" AND 2 3/4" X 7/8". FABRICATED ANGLE USING 7075-O .071 DIMS 27 1/8" X 2 1/2", HEAT TREATED PART TO T6 CONDITION IAW FASI ENG REPORT 2- 37153-801 REV A. FABRICATED TWO FILLERS USING 7075T-6 .160 DIMS 3 1/4" X 1" AND 2 5/8" X 7/8", FABRICATED STRAP USING 7075T-6 .063 DIMS 29 3/4" X 7/8" AND INSTALLED ALL REPAIR PARTS IAW SRM 53-10-8.

Part: FITTING — GOUGED (BS 600-620) · airframe 42,731 hrs · 29,193 cycles

MAIN CARGO DOOR HINGE AFT END SECOND LOBE FROM THE END IS GOUGED REMOVED DAMAGED HINGE SECTION. FABRICATED NEW HINGE SECTION AND INSTALLED IAW DWG B27-53-070 AND DWG 52FX1433

Part: SKIN — GOUGED (RT WING TE FLAP) · airframe 42,731 hrs · 29,193 cycles

RT INBD FORE FLAP GOUGED AT OTBD LOWER L/E SURFACE. CUT OUT DAMAGED AREA OF SKIN DIM. 1/2" X 1 1/2" IAW SRM 57-50-4 FIG1. FABRICATED REPAIR DOUBLER FROM 2024 T-3 .063" DIM. 3 7/8" X 4 1/2" IAW SRM 57-50-2 FIG 3 AND 57-50-4 FIG 1. INSTALLED REPAIR DOUBLER IAW SRM 57-50-4 FIG 1 AND 51-30-2, REV 103.

Part: FLOORBEAM — CORRODED (BS 380) · corrosion level 2 · airframe 42,731 hrs · 29,193 cycles

FLOORBEAM CORRODED STA 380 RBL 25 T0 45 CUT OUT DAMAGED AREAS DIMS 2" X 9". FABRICATED 2 ANGLES USING 7075-O .090 DIMS 24" X 1.8" AND 17.375" X 1.6" AND FILLER USING 7075T-6 .125 DIMS 2" X 9". HEAT TREATED PARTS TO T6 CONDITION IAW FASI ENG REPORT 2-37153-801 REV A AND INSTALLED ALL REPAIR PARTS IAW SRM 53-10-8.

Part: SEAT TRACK — CORRODED (BS 360-480) · corrosion level 2 · airframe 42,731 hrs · 29,193 cycles

SEAT TRACK CORRODED STA 360-480 BL0 REMOVED SEAT TRACK SECTION. FABRICATED NEW SECTION USING BAC1520-792 7178T6 DIMS 136" AND INSTALLED IAW SRM 53-10-5 AND SRM 51-30-2.

Part: FLOORBEAM — CORRODED (BS 560) · corrosion level 2 · airframe 42,731 hrs · 29,193 cycles

FLOORBEAM CORRODED STA 560 LBL 25-45 CUT OUT DAMAGED AREA DIMS 5.8" X .8". FABRICATED 2 ANGLES USING 7075-O .090 DIMS 18 3/4" X 2 7/8" AND 14" X 2 5/8". HEAT TREATED PARTS TO T6 CONDITION IAW FASI ENG REPORT 2-37153-801 REV A. FABRICATED FILLER USING 7075T-6 .125 DIMS 5.8" X .8" AND INSTALLED ALL REPAIR PARTS IAW SRM 53-10-8.

Part: SEAT TRACK — CORRODED (BS 480-600) · corrosion level 2 · airframe 42,731 hrs · 29,193 cycles

SEAT TRACK CORRODED, STA 480-600, BL0, REMOVED SEAT TRACK SECTION. FABRICATED NEW SECTION USING BAC1520-792 7178 T6511, DIMS 120" AND INSTALLED IAW P-F SRM 53-10-2 AND SRM 51-30-2.

Part: SEAT TRACK — CORRODED (BS 344-480) · airframe 42,731 hrs · 29,193 cycles

SEAT TRACK CORRODED ON BOTH FLANGES STA 380-480 LBL 45. REMOVED SEAT TRACK SECTION. FABRICATED NEW SEAT TRACK SECTION USING BAC1520- 792 7178-T6 DIMS 136" AND INSTALLED IAW SRM 53-10-5 AND P-F SRM 53-10-2.

Part: FLOORBEAM — CORRODED (BS 720A) · corrosion level 2 · airframe 42,731 hrs · 29,193 cycles

FLOORBEAM CORRODED STA 720A RBL 45 TO 62.5 CORROSION OUT OF LIMITS. CUT OUT DAMAGED AREA DIMS 5" X .9". FABRICATED REPAIR USING BAC1505-100617 DIMS 21.3", FABRICATED SUPPORT ANGLE USING BAC1490-2685 DIMS 16.75" X 2.5" AND BAC1490-2785 DIMS 21.3" X 2.7", FABRICATED RADIUS FILLER USING 7075T- 6 .125 DIMS 6.75" X .9", FABRICATED REINFORCEMENT STRAPS USING BAC1512-3353 DIMS 21.3" X .9" AND BAC1512-3396 DIMS 16.75" X .9" AND INSTALLED IAW SRM 53-10-8

Part: SEAT TRACK — CORRODED (BS 360-400) · corrosion level 2 · airframe 42,731 hrs · 29,193 cycles

SEAT TRACK CORRODED STA 360-400, RBL 45. REMOVED SEAT TRACK SECTION. FABRICATED NEW SEAT TRACK SECTION USING BAC1520-792 7178-T6511 DIMS 136" AND INSTALLED IAW SRM 51-30-2 AND P-F SRM 53-10-2.

Part: SEAT TRACK — CORRODED (BS 970-1010) · corrosion level 2 · airframe 42,731 hrs · 29,193 cycles

SEAT TRACK CORRODED, STA 970-1010, RBL 45. CORROSION OUT OF LIMITS. REMOVED SEAT TRACK SECTION. FABRICATED NEW SECTION USING BAC1520-792-7178-T6511 DIMS 174 5/8", FABRICATED SPLICE USING BAC1503-100122-7178 DIMS 13", FABRICATED 2 EACH PLATES USING 7075T-6 .250 DIMS 7" X 2" AND INSTALLED IAW SRM 51-30-2 AND 53-10-5.

Part: SEAT TRACK — CORRODED (BS 1085) · corrosion level 2 · airframe 42,731 hrs · 29,193 cycles

SEAT TRACK CORRODED, STA 1085, BL 0. CORROSION OUT OF LIMITS. REMOVED SEAT TRACK BS 1000 TO BS 1130. FABRICATED NEW SEAT TRACK SECTION USING BAC1520-792-7178-T6511 DIMS 129 3/8", FABRICATED STRAP USING 7075T-6 .250 DIMS 7 1/8" X 2 1/8", FABRICATED 2 ANGLES USING BAC1503-100122-7178-T6511 DIMS 14 1/8" X 2 1/2" EACH AND INSTALLED IAW SRM 51-30-2 AND 53-10-5.

Part: FLOORBEAM — CORRODED (BS 440) · corrosion level 2 · airframe 42,731 hrs · 29,193 cycles

FLOORBEAM CORRODED STA 440 LBL 45 TO 62.5 CUT OUT DAMAGED AREA DIMS 2.15" X .90". FABRICATED TWO ANGLES USING 7075-O .090 DIMS 14.5" X 2.5" AND 11.3" X 2.4" HEAT TREATED PARTS FROM 7075-O TO 7075T-6 CONDITION IAW FASI ENG REPORT 2-37153-801 REV A, FABRICATED FILLER USING 7075T-6 .125 DIMS 2.15" X .90" AND INSTALLED REPAIR PARTS IAW SRM 53-10-8.

Part: SEAT TRACK — CORRODED (BS 360-390) · corrosion level 2 · airframe 42,731 hrs · 29,193 cycles

SEAT TRACK PREVIOUS REPAIR CORRODED STA 360-390, LBL 25. REMOVED DAMAGED SEAT TRACK SECTION. FABRICATED NEW SECTION USING BAC1520-792 7178-T6511 DIMS 136" AND INSTALLED IAW SRM 53-10-5

Part: SKIN — CHAFED (100) · airframe 42,731 hrs · 29,193 cycles

SKIN GOUGED STA 720E, STR 19L LAP SEAM. CUT-OUT DAMAGED AREA DIMS 4.7500" X 2.7500". FABRICATED REPAIR DOUBLER USING 2024T- 3 .071 DIMS 12.5" X 9.2500", FABRICATED FILLER USING 2024T-3 .063 DIMS 4.7500" X 2.7500" AND TAPERED SHIMS USING 2024T-3 .071 DIMS 3" X 4" AND INSTALLED IAW SRM 51-30-2 AND 53-30-3.

Part: SKIN — DENTED (BS 1112 S20R) · airframe 42,731 hrs · 29,193 cycles

DENT ON LAP SEAM, STA 1112, STR 20R. CUT OUT DAMAGED AREA DIMS 4" X 2 1/4". FABRICATED REPAIR DOUBLER USING 2024T-3 .071 DIMS 11.75" X 9.25", FABRICATED FILLER USING 2024T-3 .080 DIMS 11.5" X 9" , FABRICATED FILLER USING 2024T-3 .080 DIMS 2.25" X 1.3" AND INSTALLED IAW SRM 53-30-3 AND SRM 51-30-2.

Part: SKIN — MISREPAIRED (BS 1175-1183) · airframe 42,731 hrs · 29,193 cycles

IMPROPER REPAIR INSTALLED STA 1175 TO 1183, STR'S 23L TO 24L. REMOVED PREVIOUS REPAIR AT STA 1175 TO 1183 STR 23-24L IAW SRM 51-30-2. ACOMPLISHED REPAIR PER EA 7-5330-135578.

Part: SUPPORT — CORRODED (ZONE 600) · corrosion level 2 · airframe 41,777 hrs · 28,439 cycles

APU EXHAUST DUCT MOUNT FLANGE AT UPPER WING PANEL, AFT Z ANGLE SUPPORT CORRODED. REPLACED FLANGE SUPPORT/STIFFENER REF SRM 51-30-02 PG 2 AND 5. THIS IS CLASSIFIED AS A MINOR REPAIR.

Part: LINE — CRACKED (HYD SYSTEM) · airframe 41,543 hrs · 28,258 cycles

AT FL 320 "A" SYS QUANTITY DECREASED TO ZERO. RAN QRH FOR HYD SYS "A" LEAK CHECKS PERFORMED. MANUAL GEAR EXT AND ALT FLAPS LANDING. SYS "A" FLUID SHUTOFF WAS CLOSED AT 05:09, ENGINE SHUTDOWN AT 05:51. FOUND THE NR 2 SPOILER RETURN LINE CRACKED. WORKING ON FABRICATING LINE. SPLICED IN NEW SECTION OF HYD LINE FROM THE RETURN LINE OF THE NR 2 SPOILER ACTUATOR OPS AND LEAK CHECK GOOD IAW MM 20-10-005-8. SERVICED "A" SYS HYD TO FULL IAW MM 12-12-000-2. CLOSED FINAL.

Part: LINE — CRACKED (HYD SYSTEM) · airframe 41,543 hrs · 28,258 cycles

AT FL 320 "A" SYS QUANITY DECREASED TO ZERO. RAN QRH FOR HYD SYS "A" LEAK CHECKS PERFORMED. MANUAL GEAR EXT AND ALT FLAPS LANDING. SYS "A" FLUID SHUTOFF WAS CLOSED AT 05:09, ENGINE SHUT DOWN AT 05:51. FOUND THE NR 2 SPOILER RETURN LINE CRACKED. WORKING ON FABRICATING LINE. SPLICED IN NEW SECTION OF HYD LINE FROM THE RETURN LINE OF THE NR 2 SPOILER ACTUATOR OPS AND LEAK CHECK GOOD IAW B-727-200 MM 20-10-005-8. SERVICED "A" SYSTEM HYD TO FULL IAW B-727-200 MM 12-12-000-2.

Part: FRAME — CRACKED (ZONE 200) · airframe 41,518 hrs · 28,233 cycles

FRAME CRACKED AT LOCK FASTENER, STA 800 STRINGER 14R. REMOVED DAMAGED PORTION OF FRAME ANGLE, FABRICATED REPAIR ANGLE AND FRAME FILLER. HEAT TREATED, ALODINED AND PRIMED AND INSTALLED. REF SRM 51-40-2 FIG 1, 51-30-2 PG 2, THIS IS CLASSIFIED AS A MAJOR REPAIR.

Part: FRAME — CHAFED (ZONE 100) · airframe 41,518 hrs · 28,233 cycles

ORIGINAL DISCREPANCY STILL EXISTS. AFT PIT LT SIDE WALL BODY FRAME IB FLANGE CHAFED, 1148, STR 21L - L CHECKED WEAR AREA FOR MATERIAL LOSS, ORIGINAL THICKNESS "T' .065' MATERIAL LOSS MEASURE .017', REMAINING MATERIAL .048' AND IS OUT OF LIMITS REF SRM 53-10-1 FIG 1. FABRICATED REPAIR MATERIAL REF SRM 51-40-3, INSTALL REPAIR, REF SRM 51-40-3. THIS IS CLASSIFIED AS A MAJOR REPAIR.

Part: DOOR FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,518 hrs · 28,233 cycles

AFT PIT DOOR OPENING AFT FRAME STA 990 IS CORRODED ON LOWER SURFACE OF FRAME, UPPER ANGLE BETWEEN STR 26R AND STR 27R REMOVED CORROSION, FORMED REPAIR ANGLE, HEAT TREATED AND CAD PLATED REPAIR ANGLE. INSTALLED REPAIR ANGLE. REFERENCE EA NR 75310-113992.

Part: STIFFENER — CORRODED (ZONE 600) · airframe 41,518 hrs · 28,233 cycles

SEAL RETAINER STIFFENER RT WING AFT LWR SPAR WS 181-220 IS CORRODED REMOVED CORROSION FROM STIFFENER AT STA 181-220 RT WING ORIGINAL MATERIAL .040 MATERIAL LOSS .010 REMAINING MATERIAL .030 OUT OF LIMITS. REMOVED STIFFENER AND FABRICATED NEW STIFFENER MATERIAL 2024-T3-.040 AND INSTALLED. TREATED AND PRIMED. REF DWR 65-21656 AND SRM 51-10-2. THIS IS CLASSIFIED AS A MINOR REPAIR.

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,518 hrs · 28,233 cycles

AFT PIT BILGE SKIN HAS CORROSION AT STATION 1008 OB OF STRINGER 28L REMOVED CORROSION REF SRM 51-10-1 ORIG T .082 REMAINING .047, .035 LOSS USING TOOL IN22-0028, OUT OF LIMITS. REF SRM 53-10-1 FIG 1. FABRICATED REPAIR DOUBLER REF EA 7-5330-113 990. INSTALLED NEW STRINGER SPLICE REF SRM 51-30-2. THIS IS CLASSIFIED AS A MAJOR REPAIR.

Part: STIFFENER — CORRODED (ZONE 600) · corrosion level 2 · airframe 41,518 hrs · 28,233 cycles

RT MLG STRUT WELL LWR FIXED PNL SEAL RETAINER ASSY IS CRACKED/CORRODED ALONG WING SPAR CHORD WS 190-220 REMOVED 4 HYD STANDOFFS AND 2 SEAL DEPRESSORS FROM STA 180-220. REMOVED DRAIN TUBE, TE FAIRING PANEL, TE FIXED PANEL RT. FABRICATED 2 NEW SEAL RETAINERS OUT OF LIMITS. MATERIAL 2024-T3 INSTALLED NEW SEAL AND SEAL RETAINERS. INSTALLED OLD 1 EA STIFFENERS. TREATED AND PRIMED REF DWG 65-21656 AND SRM 51-10-2. THIS IS CLASSIFIED AS A MINOR REPAIR.

Part: FLOOR SUPPORT — CORRODED (BS 1140-1146) · corrosion level 2 · airframe 41,518 hrs · 28,233 cycles

MAIN DECK BS 1140-1146 RBL 11-12 WL 208 FLOOR SUPPORT "T" HAS CORROSION ON UPPER AND LOWER SURFACES OF I/B FLANGE. REMOVED CORROSION, ORIGINAL "T" .080, REMOVED .025, REMAINING .055 - OUT OF LIMITS REF SRM 51-10-1. REMOVED OLD SUPPORT BEAM, FABRICATED, HEAT TREATED, TREATED AND PRIMED, INSTALLED ON AIRCRAFT REF GMM 7-0-1001, SRM 51-10-2 AND SRM 51-30-02. THIS IS CLASSIFIED AS A MINOR REPAIR.

Part: STRINGER — CORRODED (BS 620-624 S2R) · corrosion level 2 · airframe 41,518 hrs · 28,233 cycles

STR-2R HAS CORROSION, BS: 620-624 REMOVED CORROSION REF SRM 51-10-6 P 12-14, VERIFIED MATERIAL LOSS WITHIN LIMITS REF SRM 53-10-1. ORIGINAL "T" .036", MATERIAL REMOVED .002" REMAINING "T" = .034. TREATED AND PRIMED REF SRM 51-10-2 P. 1-2. THIS IS CLASSIFIED AS A MINOR REPAIR.

Part: SHEAR TIE — CORRODED (BS 990) · corrosion level 2 · airframe 41,518 hrs · 28,233 cycles

DOT 114-010 AFT PIT BILGE SHEAR TIE IS CORRODED AT STATION 990 FRAME, STRINGER 29 RIGHT TO STR 30. MANUFACTURED AND INSTALLED NEW SHEAR TIE AT STA 990 STR 29 TO 30. FOUND OLD SHEAR TIE OUT OF LIMITS. ORIGINAL T .063 AFTER REMOVAL .051 REF SRM 53-10-1. INSTALL REF SRM 53-10-4 PG 1 - 4. THIS IS CLASSIFIED AS A MINOR REPAIR.

Part: FRAME — GOUGED (BS 1130) · corrosion level 2 · airframe 41,518 hrs · 28,233 cycles

AFT CARGO PIT FUSELAGE FRAME 1130 HAS GOUGES AND CORROSION ON UPPER FLANGE, RBL: 22-23, UNDER Z ANGLE. REMOVED CORROSION AND GOUGES, ORG MATERIAL THICKNESS .071" REMOVED .030", REMAINING .041". FOUND TO BE OUT OF LIMITS, FABRICATED REPAIR PART, TREATED AND PRIMED REPAIR AND INSTALLED, REF SRM 51-10-2 PG 7, SRM 51-30-2 PG 2, SRM 53-10-1, SRM 53-10-2 FIG 5, SRM 51-40-3 FIG 1. THIS IS CLASSIFIED AS A MAJOR REPAIR.

Part: STRINGER — CORRODED (BS 520-540 S28L) · corrosion level 2 · airframe 41,518 hrs · 28,233 cycles

FWD LOWER CARGO PIT, CORROSION ON STRINGER L28 BETWEEN FS 520 AND FS 540 REMOVED CORROSION ON STRINGER L28 FWD LOWER CARGO PIT FS 520-540. FOUND CORROSION AREA TO BE OUT OF LIMITS WITH A .020 MATERIAL LOSS FROM ORIGINAL "T" = .063. REMOVED DAMAGE SECTION OF STRINGER, FABRICATED, TREATED, PRIMED, PAINTED AND INSTALLED STRINGER SPLICE REPAIR REF SRM 53-10-3 PG 1B DETAIL I. CORROSION ON SKIN REPAIRED ON N/R 00635, 00636, 00637. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR.

Part: STRINGER — CORRODED (BS 540-560 S28L) · corrosion level 2 · airframe 41,518 hrs · 28,233 cycles

FWD LOWER CARGO PIT, CORROSION ON STRINGER L28 BETWEEN FS 540 AND FS 560 CORROSION FOUND ON LOWER CARGO PIT STRINGER L28 BETWEEN FS 540 AND 560 WAS OUT OF LIMITS (EXFOLIATION). REMOVED DAMAGED SECTION OF STRINGER FROM 551-575 FS. FABRICATED, TREATED PRIMED PAINTED AND INSTALLED STRINGER SPLICE REPAIR REF SRM 53-10-3 FIG 1. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR.

Part: STRINGER CLIP — CORRODED (BS 660) · corrosion level 2 · airframe 41,518 hrs · 28,233 cycles

CORROSION ON STRINGER CLIP AT BS 660 STRINGER S-2R REMOVED AND REPLACED STRINGER CLIP IAW SRM 51-30-02 PG-2-8. THIS IS CLASSIFIED AS A MAJOR REPAIR IAW, GMM 6-2-100 PG 2 AND 3.

Part: STRINGER — CORRODED (BS 576-584) · corrosion level 2 · airframe 41,518 hrs · 28,233 cycles

STR-3R HAS CORROSION, BS 576-584 REMOVED CORROSION REF SRM 53-10-1. AREA FOUND TO BE OUT OF LIMITS. REMOVED STRINGER SECTION REF SRM 51-30-02 P 6-7. FABRICATED NEW SECTION REF SRM 53-10-2 FIG 9. INSTALLED NEW SECTION REF SRM 51-30-02. THIS IS CLASSIFIED AS A MAJOR REPAIR.

Part: THRESHOLD — CRACKED (ZONE 200) · airframe 41,518 hrs · 28,233 cycles

RIGHT AFT SERVICE DOOR THRESHOLD CRACKED NEAR STOP PAD. SENT TO SHOP FOR WELD ON NR N00707, THRESHOLD WILL GET INSTALLED ON CLOSE CARD 72C201-01. THIS IS CLASSIFIED AS A MINOR REPAIR.

Part: STRINGER — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,518 hrs · 28,233 cycles

CORROSION ON INSIDE OF STRINGER S-3R AT STA 520 REMOVED .008' CORROSION FROM ORIGINAL STRINGER. THICKNESS OF .036'. REMAINING THICKNESS IS .028" AND STRINGER WHERE DAMAGE IS OUT OF LIMITS. REMOVED DAMAGE SECTION OF STRINGER, FABRICATED REPAIR PARTS, TREATED, PRIMED AND INSTALLED, REFERENCE SRM 53-10-1/FIG NR 1 AND SRM 53-10-3/FIG NR 3, CLASSIFIED AS A MAJOR REPAIR.

Part: THRESHOLD — CRACKED (BS 1070-1090) · airframe 41,518 hrs · 28,233 cycles

R2 DOOR OPENING, THRESHOLD CRACKED 2 PLACES SENT TO SHOP FOR WELD REPAIR ON NR N00707. THRESHOLD WILL BE INSTALLED ON CLOSE CARD 72C201-01 THIS IS CLASSIFIED AS A MINOR REPAIR.

Part: STRINGER CLIP — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,518 hrs · 28,233 cycles

CORROSION ON STRINGER CLIPS, BS 520 STRINGER, S-4R AND S-3R REMOVED STR 3R CLIP AT STA 520 AND REMOVED CORROSION ORIG THICKNESS .032' LOSS .005 REMAINING .027. FOUND OUT OF LIMITS. REMOVED STR 4R AND REMOVED CORROSION FOUND TO BE CRACKED. INSTALLED 2 NEW STR CLIPS REF SRM 53-10-1 PG 2 AND 51-30-2 PG 1-3. THIS IS CLASSIFIED AS A MAJOR REPAIR.

Part: STRINGER CLIP — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,518 hrs · 28,233 cycles

CORROSION ON STRINGER CLIP AT BS 660, STRINGER, S-1R INSTALLED 1 EA CLIP, NEW CLIP AT STR 1, F/S 660 PER REF SRM 51-30-02. THIS IS CLASSIFIED AS A MAJOR REPAIR.

Part: FRAME — CRACKED (ZONE 100) · airframe 41,518 hrs · 28,233 cycles

LT WHEEL WELL STA 913.5 FRAME IS CRACKED OUT OF UPPER FILLER, END. CRACK IS WITHIN THE SHADED AREA OF JOB CARD FIGURE 1A REPAIRED LT WHEEL WELL FRAME AT STA 913.5, PER EO 7-5310-7-4329 PART 3, THIS IS CLASSIFIED AS A MINOR REPAIR.

Part: SKIN — CORRODED (BS 566-572) · corrosion level 2 · airframe 41,518 hrs · 28,233 cycles

FWD PIT FUSELAGE SKIN HAS CORROSION, BS 566 - 572, STR 28L REMOVED CORROSION FROM FWD PIT FUSELAGE SKIN, BS 566 - 572 STR 28L. NDT FOR MATERIAL REMOVAL. FOUND TO BE OUT OF LIMITS. .035 INCH REMOVED AT DEEPEST POINT. ORIGINAL .100 INCH REMOVED DAMAGE/PREVIOUS REPAIR NEAR CUT OUT. FABRICATED, TREATED AND PRIMED AND INSTALLED DOUBLER REF SRM 53-30-3 FIG 3. THIS REPAIR IS A CATAGORY "B'' REPAIR THIS IS CLASSIFIED AS A MINOR REPAIR.

Part: WEB — CRACKED (ZONE 300) · airframe 41,518 hrs · 28,233 cycles

AIR STAIR COMPARTMENT ABOVE "S" DUCT AT STA 1303, LT SIDE OF YELLOW VERTICAL WEB WHERE STIFFENER PASSES THROUGH CUT OUT, CRACKED. DOT ON AFT SIDE OF WEB AND ACCESS THROUGH VERT STAB PANEL 9504 REMOVED DAMAGE, FABRICATED, TREATED, PRIMED AND INSTALLED REPAIR PARTS. REF SRM'S 51-30-02 PG 32, 51-40-02 PG 1-6, MM'S 51-20-021-7, 51-20-031 PGS 1-3, NAD BOEING DOC 65-17506 ITEM 31. THIS IS CLASSIFIED AS A MINOR REPAIR.

Part: WEB — CRACKED (ZONE 300) · airframe 41,518 hrs · 28,233 cycles

AIR STAIR COMPARTMENT ABOVE "S" DUCT AT STA 1303, RT SIDE OF YELLOW VERTICAL WEB WHERE STIFFENER PASSES THROUGH CUTOUT, CRACKED. DOTS ARE ON AFT SIDE ACCESING THROUGH VERT STAB PANEL. REMOVED DAMAGED, FABRICATED, TREATED, PRIMED, AND INSTALLED. REPAIR REF SRM'S 51-30-02 PG 32, 51-40-02 PG 1-6, AMM`S 51-20-021-7 PG 1-3, 51-20-031, PG 1-3, AND DOC PL 65-17506 ITEM 31. THIS IS CLASSIFIED AS A MINOR REPAIR.

Part: SUPPORT ANGLE — CRACKED (CARGO DOOR) · airframe 41,518 hrs · 28,233 cycles

FWD LOWER CARGO DOOR, FWD FRAME HAS CRACK IN SUPPORT ANGLE AT 3RD STOP FITTING UP FROM BOTTOM REMOVED DAMAGE PARTS. FABRICATED NEW TEE CLIP AND GUSSET. INSTALLED NEW PARTS. REF SRM 51-30-02, 51-30-05 P 1-34 DWG NR 65-69145. TREATED AND PRIMED (GUSSET AND TEE) REF SRM 51-10-2 PG 1-27. THIS IS CLASSIFIED AS A MINOR REPAIR.

Part: PANEL — DELAMINATED (ZONE 500) · airframe 41,518 hrs · 28,233 cycles

LEFT WING L/E PANEL 6220, CORNER SKIN DISBONDED REPAIRED PANEL 6620 REF SRM 51-20-9 PAR 3D AND 7 PG 3-11 AND AMM 51-20-051-7 PG 1 AND 51-20-151-7 PG1, THIS IS CLASSIFIED AS A MINOR REPAIR.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 39,450 hrs · 29,513 cycles

LT WING O/B FLAP I/B END BY END FITTING IS DELAMED (TOP SKIN ) OF FORE FLAP REPAIRED LT WING OUTBOARD FORE FLAP REF SRM 51-40-20 PAR'S 7,14,15,18,20,21 PGS 12-62 SRM 57-50-02 FIG 4 PG 7, AND AMM 51-20-151-7 PG 1. THIS IS CLASSIFIED AS A MINOR REPAIR.

Part: REPAIR — UNKNOWN (FUSELAGE) · airframe 39,743 hrs · 26,767 cycles

FOUND PREVIOUSLY REPAIR INSTALLED AT STA 1158, STR 30 WAS DETERMINED TO BE ACCOMPLISHED IAW EO 7-2500-7-2348, ITEM 12, BASED ON AN EXTERNAL VISUAL EVALUATION, CONSISTS OF LOCATION, SHAPE, SIZE, MATERIAL TYPE AND THICKNESS, FASTENER SPACING AND NUMBERS, GENERAL WORKMANSHIP, REPAIR IS CLASSIFIED AS MAJOR PER FEDEX GMM 6-2-100.

Part: REPAIR — NONE (FUSELAGE) · airframe 39,743 hrs · 26,767 cycles

FOUND PREVIOUSLY REPAIR INSTALLED AT STA. 360, STR 13L WAS DETERMINED TO BE ACCOMPLISHED IAW E.O. 7-5100-7-2307F, BASED ON AN EXTERNAL VISUAL EVALUATION, CONSISTS OF LOCATION, SHAPE, SIZE, MATERIAL TYPE AND THICKNESS, FASTENER SPACING AND NUMBERS, GENERAL WORKMANSHIP, REPAIR IS CLASSIFIED AS MAJOR PER FEDEX GMM 6- 2-100.

Part: REPAIR — NONE (FUSELAGE) · airframe 39,743 hrs · 26,767 cycles

FOUND PREVIOUSLY REPAIR INSTALLED AT STA. 1050, STR 27R WAS DETERMINED TO BE ACCOMPLISHED IAW SRM 53-30-3 FIG 1, BASED ON AN EXTERNAL VISUAL EVALUATION, CONSISTS OF LOCATION, SHAPE AND SIZE, MATERIAL THICKNESS AND TYPE, FASTENER SPACING AND NUMBERS, GENERAL WORKMANSHIP, REPAIR IS CLASSIFIED AS MAJOR PER FEDEX GMM 6-2-100.

Part: REPAIR — UNKNOWN (ZONE 500) · airframe 39,743 hrs · 26,767 cycles

FOUND REPAIR ON LEFT I/B FORE FLAP UPPER SURFACE. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA.

Part: REPAIR — NONE (RT WING) · airframe 39,743 hrs · 26,767 cycles

FOUND PREVIOUSLY REPAIR INSTALLED AT RIGHT WING LEADING EDGE, ON FRAME OF LANDING LIGHT WAS DETERMINED TO BE ACCOMPLISHED IAW SRM 57-10-4 FIG. 4, 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 — UNKNOWN (FUSELAGE) · airframe 39,743 hrs · 26,767 cycles

FOUND PREVIOUS REPAIR INSTALLED AT AFT END OF TAIL SKID CUTOUT, DETERMINED TO BE ACCOMPLISHED IAW SRM 53-30-3, FIG 1, BASED ON AN EXTERNAL VISUAL EVALUATION, CONSISTS OF LOCATION, SHAPE, SIZE, FASTENER SPACING AND NUMBERS, MATERIAL TYPE AND THICKNESS, GENERAL WORKMANSHIP, REPAIR IS CLASSIFIED AS MAJOR PER FEDEX GMM 6-2-100.

Part: REPAIR — UNKNOWN (L/E SLAT) · airframe 39,743 hrs · 26,767 cycles

FOUND PREVIOUS REPAIR INSTALLED ON NR 8 LEADING EDGE SLAT UPPER SURFACE WAS DETERMINED TO BE ACCOMPLISHED IAW SRM 57-50-3 FIG 10. BASED ON AN EXTERNAL VISUAL EVALUATION, CONSISTS OF LOCATION, SHAPE, SIZE, MATERIAL THICKNESS AND TYPE, FASTENER SPACING AND NUMBERS, GENERAL WORKMANSHIP, REPAIR IS CLASSIFIED AS MAJOR PER FEDEX GMM 6-2-100.

Part: REPAIR — UNKNOWN (FUSELAGE) · airframe 39,743 hrs · 26,767 cycles

FOUND PREVIOUS REPAIR INSTALLED AT STA 1183, STR 23R WAS NOT ACCOMPLISHED IAW FAA APPROVED DATA, REMOVED EXISTING REPAIR AND ACCOMPLISHED REPAIR IAW SRM 53-30-3 FIG 3A AND SRM 51-30-2, REPAIR IS CLASSIFIED AS MAJOR PER FEDEX GMM 6-2-100.

Part: REPAIR — UNKNOWN (LT FOREFLAP) · airframe 39,743 hrs · 26,767 cycles

FOUND PREVIOUS REPAIR INSTALLED ON LT INBOARD FOREFLAP LEADING EDGE WAS DETERMINED TO BE ACCOMPLISHED IAW SRM 57-50-4 FIG 1. BASED ON AN EXTERNAL VISUAL EVALUATION, CONSISTS OF LOCATION, SHAPE AND SIZE, MATERIAL TYPE AND THICKNESS, FASTENER SPACING AND NUMBER, GENERAL WORKMANSHIP, REPAIR IS CLASSIFED AS MAJOR PER FEDEX GMM 6-2-100.

Part: REPAIR — UNKNOWN (ZONE 100) · airframe 39,743 hrs · 26,767 cycles

FOUND REPAIR LOCATED AT STA 660, STR 30. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA.

Part: REPAIR — UNKNOWN (FUSELAGE) · airframe 39,743 hrs · 26,767 cycles

FOUND REPAIR LOCATED AT STA 188, STR 27L. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA.

Part: REPAIR — NONE (FUSELAGE) · airframe 39,743 hrs · 26,767 cycles

FOUND PREVIOUSLY REPAIR INSTALLED AT STA 1050, STR 27L WAS DETERMINED TO BE ACCOMPLISHED IAW SRM 53-30-3, FIG 3, BASED ON AN EXTERNAL VISUAL EVALUATION, CONSISTS OF LOCATION, SHAPE AND SIZE, FASTENER SPACING AND NUMBERS, MATERIAL TYPE AND THICKNESS, GENERAL WORKMANSHIP, REPAIR IS CLASSIFIED AS MAJOR PER FEDEX GMM 6-2-100.

Part: REPAIR — UNKNOWN (ZONE 100) · airframe 39,743 hrs · 26,767 cycles

FOUND REPAIR LOCATED AT STATION 188, FORWARD OF NOSE ACCESS DOOR REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING APPROVED DATA.

Part: REPAIR — UNKNOWN (ZONE 100) · airframe 39,743 hrs · 26,767 cycles

FOUND REPAIR AT STA 259.5 STR 17L, REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA.

Part: REPAIR — UNKNOWN (ZONE 500) · airframe 39,743 hrs · 26,767 cycles

FOUND REPAIR LOCATED ON NR 2 L/E SLAT. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA (LEFT WING).

Part: REPAIR — UNKNOWN (ZONE 800) · airframe 39,743 hrs · 26,767 cycles

FOUND REPAIR LOCATED ON MAIN CARGO DOOR LOWER FWD EDGE REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA.

Part: REPAIR — NONE (SLAT) · airframe 39,743 hrs · 26,767 cycles

FOUND PREVIOUSLY REPAIR INSTALLED AT NR 1 LEADING EDGE SLAT , LOWER AFT SURFACE WAS DETERMINED TO BE ACCOMPLISHED IAW SRM 57-50-3 FIG.1, BASED ON AN EXTERNAL VISUAL EVALUATION, CONSISTED OF LOCATION, SHAPE, SIZE, MATERIAL TYPE AND THICKNESS, FASTENER SPACING AND NUMBERS, GENERAL WORKMANSHIP, REPAIR IS CLASSIFIED AS MAJOR PER FEDEX GMM 6-2-100.

Part: REPAIR — UNKNOWN (FUSELAGE) · airframe 39,743 hrs · 26,767 cycles

FOUND PREVIOUS REPAIR INSTALLED AT STA 1183, STR 24L WAS NOT ACCOMPLISHED IAW FAA APPROVED DATA. REMOVED EXISTING REPAIR AND ACCOMPLISHED REPAIR IAW SRM 53-30-3 FIG 3A, REPAIR IS CLASSIFIED AS MAJOR PER FEDEX GMM 6-2-100.

Part: REPAIR — UNKNOWN (RUDDER) · airframe 39,743 hrs · 26,767 cycles

FOUND PREVIOUS REPAIR INSTALLED ON LOWER RUDDER, LT SIDE WAS DETERMINED TO BE ACCOMPLISHED IAW SRM 55-40-3 FIG 1, BASED ON AN EXTERNAL VISUAL EVALUATION, CONSISTS OF LOCATION, SHAPE, SIZE, MATERIAL TYPE AND THICKNESS, FASTENER SPACING AND NUMBER, GENERAL WORKMANSHIP, REPAIR IS CLASSIFIED AS MAJOR PER FEDEX GMM 6-2-100.

Part: REPAIR — UNKNOWN (HORIZ STAB) · airframe 39,743 hrs · 26,767 cycles

FOUND PREVIOUS REPAIR INSTALLED AT RT HORIZONTAL STAB LOWER SURFACE WAS DETERMINED TO BE ACCOMPLISHED IAW SRM 55-10-3 FIG 1. BASED ON AN EXTERNAL VISUAL EVALUATION, CONSISTS OF LOCATION, SHAPE, SIZE, MATERIAL TYPE AND THICKNESS, FASTENER SPACING AND NUMBERS, GENERAL WORKMANSHIP, REPAIR IS CLASSIFIED AS MAJOR PER FEDEX GMM 6-2-100.

Part: REPAIR — UNKNOWN (HORIZ STAB) · airframe 39,743 hrs · 26,767 cycles

FOUND PREVIOUS REPAIR INSTALLED ON RT HORIZONTAL STAB LOWER I/B SURFACE WAS DETERMINED TO BE ACCOMPLISHED IAW SRM 55-10-3 FIG 3. BASED ON AN EXTERNAL VISUAL EVALUATION, CONSISTS OF LOCATION, SHAPE, SIZE, MATERIAL TYPE AND THICKNESS, FASTENER SPACING AND NUMBER, GENERAL WORKMANSHIP, REPAIR IS CLASSIFIED AS MAJOR PER FEDEX GMM 6-2-100.

Part: REPAIR — UNKNOWN (ZONE 600) · airframe 39,743 hrs · 26,767 cycles

FOUND 2 REPAIRS LOCATED ON UPPER SURFACE OF RT WING AFT OF NR 6 L/E, STA 546. REPAIRS REQUIRE EVALUATION FOR MAJOR MINOR DETERMINATION AND IF REPAIRS WERE ACCOMPLISHED USING FAA APPROVED DATA.

Part: REPAIR — NONE (FUSELAGE) · airframe 39,743 hrs · 26,767 cycles

FOUND PREVIOUSLY REPAIR INSTALLED AT FWD END OF AFT AIRSTAIRS CUTOUT WAS DETERMINED TO BE ACCOMPLISHED IAW SR27-53-024, BASED ON AN EXTERNAL VISUAL EVALUATION, CONSISTS OF LOCATION, SHAPE, SIZE, MATERIAL TYPE AND THICKNESS, FASTENER SPACING AND NUMBERS, GENERAL WORKMANSHIP, REPAIR IS CLASSIFED AS MAJOR PER FEDEX GMM 6-2-100.

Part: REPAIR — NONE (RT WING) · airframe 39,743 hrs · 26,767 cycles

FOUND PREVIOUSLY REPAIR INSTALLED AT R/H WING LEADING EDGE 12 INCHES OUTBD OF LANDING LIGHT WAS DETERMINED TO BE ACCOMPLISHED IAW SRM 57-30-4, FIG 2, BASED ON AN EXTERNAL VISUAL EVALUATION, CONSISTS OF LOCATION, SHAPE AND SIZE, MATERIAL TYPE AND THICKNESS, FASTENER SPACING AND NUMBERS, GENERAL WORKMANSHIP, REPAIR IS CLASSIFIED AS MAJOR PER FEDEX GMM 6-2-100.

Part: REPAIR — UNKNOWN (ZONE 600) · airframe 39,743 hrs · 26,767 cycles

FOUND REPAIR ON RIGHT OUTBOARD FORE FLAP L/E REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA.

Part: REPAIR — UNKNOWN · airframe 39,743 hrs · 26,767 cycles

FOUND REPAIR LOCATED ON UPPER SURFACE OF LEFT WING AFT OF NR 4 L/E FLAP, STA 410. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA.

Part: REPAIR — NONE (FUSELAGE) · airframe 39,743 hrs · 26,767 cycles

FOUND PREVIOUSLY REPAIR INSTALLED AT AFT CUT OUT AFT AIRSTAIRS WAS DETERMINED TO BE ACCOMPLISHED IAW SRM 51-10-1 AND SRM 51-30-1, PARA F, BASED ON AN EXTERNAL VISUAL EVAULATION, CONSISTS OF LOCATION, SIZE AND SHAPE, MATERIAL THICKNESS AND TYPE, FASTENER SPACING AND NUMBERS, GENERAL WORKMANSHIP, REPAIR IS CLASSIFIED AS MAJOR PER FEDEX GMM 6-2-100.

Part: SKIN — DAMAGED (BS 1345) · airframe 39,743 hrs · 26,767 cycles

FOUND BELLY SKIN AND RIB ANGLE DAMAGED AND WRINKLED AFT OF AIR STAIRS AT BS 1345. REMOVED AND FABBED NEW BELLY SKIN STRAP AND SHIM IAW SRM 51-10-1, INSTALLED BELLY SKIN AND SHIM IAW SRM 51-30-2 AND RIB FOUND NO DAMAGE AFTER FURTHER EVALUATION.

Part: INDICATOR — MALFUNCTIONED (TE FLAPS) · airframe 38,806 hrs · 25,977 cycles

INBOARD FLAP ASYM INDICATION UPON RETRACTION. REMOVED AND REPLACED INBD FLAP POSITION INDICATOR PER MM 27-52-021-2, OPS CHECK NORMAL. R/I FROM FACT PREMATURE REMOVAL/INSTALLATION OFF MFG 18-1299-5-2F1 POS 2 SRL 0778AN TAG 680660 ON MFG 2061-13-1 SRL 252 TAG 258731.

Part: SENSOR — FAILED (ZONE 700) · airframe 37,848 hrs · 25,203 cycles

AT FL270 AND .84 MACK, THE RED AND GREEN RIGHT GEAR LIGHTS ILLUMINATED. THE LANDING GEAR HANDLE WAS PLACED UP. ALSO THE LEFT GREEN GEAR LIGHT WOULD NOT TEST INFLIGHT. PER FLIGHT CREW DEBRIEF: WHEN GEAR HANDLE WAS MOVED FROM "OFF" TO "UP" THERE WAS NO CHANGE. ALL INDICATION RETURNED TO NORMAL WITH GEAR EXTENSION AND LANDING WAS UNEVENTFUL. R&R'D UPLOCK PROX SENSOR PER MM 32-61-081-4. OPS NORMAL.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,666 hrs · 25,046 cycles

CORROSION AFT CARGO BAY STA 950D STR 29 LT SHEAR TIE HAS CORROSION. REPAIRED SHEAR TIE AT BS 950D STR 29 LT IAW FED EX EA 7-5310-54855.

Part: KEELBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,666 hrs · 25,046 cycles

N00389 CORROSION AFT CARGO BAY, STA 950C TO 950F STR 29L HAS CORROSION. REPAIRED LT KEEL BEAM STR 29L IAW FED EX E.A. 7-5310-54856.

Part: SKIN — LIGHTNING STRIKE (FUSELAGE) · airframe 37,666 hrs · 25,046 cycles

EXTERIOR SKIN, LIGHTNING STRIKE BS 355, .5 INCH BELOW STRINGER 21 LT.

Part: ANGLE — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 37,666 hrs · 25,046 cycles

CORROSION (C53-111-02) ON FWD CARGO DOOR LOWER BEAM ANGLE 27 INCHES AFT OF FWD EDGE 1.5 INCH UP FROM BOTTOM EDGE. REMOVED CORROSION ON FWD CARGO DOOR LOWER BEAM ANGLE AND T-ANGLE AT FWD EDGE AT 27 INCHES. FOUND TO BE OUT OF LIMITS. LOCATED HOLES ON NEW T-ANGLE AND LOWER BEAM AND INSTALLED PART IAW SRM 51-30-2.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,666 hrs · 25,046 cycles

CORROSION (C53-113-01), ON FRAME BS 950D STR 29R. CUT OUT AND REMOVED DAMAGED AREA OF FRAME. FABRICATED AND INSTALLED REPAIR BS 950D, STR 29R IAW SRM 53-10-4, FIG 15.

Part: SKIN — CRACKED (PAX DOOR) · airframe 37,666 hrs · 25,046 cycles

FWD ENTRY DOOR FWD UPPER CORNER OF DOOR SKIN IS CRACKED JUST BELOW UPPER GATE. REPAIRED FWD ENTRY DOOR, AFT UPPER CORNER OF DOOR SKIN, IAW SRM 52-00-2, 52-00-3, FIG 4.

Part: ANGLE — CORRODED (CARGO DOOR BEAM) · airframe 37,666 hrs · 25,046 cycles

WHILE WORKING CARD 00357 (DOOR 6030) DISCOVERED A CORROSION ON LOWER BEAM ANGLE WEB 45 INCHES AFT OF FWD EDGE 1.5 INCHES UP FROM BOTTOM EDGE ON NR 1 CARGO DOOR. REMOVED CORROSION ON LOWER BEAM ANGLE WEB 45 INCHES AFT OF FWD EDGE, FOUND TO BE OUT OF LIMITS. LOCATED HOLES ON NEW ANGLE AND INSTALLED PART IAW SRM 51-30-2.

Part: ODOR — DETECTED (CABIN) · airframe 37,314 hrs · 24,788 cycles

LEFT PACK CAUSES FUMES IN COCKPIT WHEN SELECTED TO MOMENTARY WARM TEMP. TWO CREW MEMBERS NOTICED DULL HEADACHE AND ONE CREW MEMBER COMPLAINED OF BURNING EYES. RAN LEFT PACK WARM POSITION WITH NO FUMES OR OTHER DEFECTS NOTED PER B727- 200MM 21-55-000-5. OK FOR SERVICE.

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO BAY)

CARGO SMOKE LIGHT CAME ON AFT APPROX 1 MIN NO BOTTLES FIRED. LIGHT WENT OUT. SYS CK OK. *S/D* TROUBLESHOT SYS PER MM 26-17-001-1. PERF BITE TEST ON CEU''S NR 1 AND 2, NO FAULTS. NO FAULTS ON FIRE PROTECTION CONTROL PNL. ALL SQUIB LIGHTS ILLUM. SYS TEST NORMAL.

Part: SEAL — LEAKING (RT ELEV HYD)

CLIMBOUT FL260 NOTICED THE HYD SYS-A QTY HAD DECREASE TOWARD THE 0 GAL IND WITH NORM SYS PRES OF 3000 PSI. THE FLUID QTY IND BRKR WAS PULL THE RESET. SYS PRESS AND QTY REMAIN SAME, THE HYD SYS-A PUMP LO PRESS LIGHT BOTH FLICKERED AND SYS-A PRESS DECREASE THEN TOWARD 0 PSI. PERFORM STAB PROC AND THE CKLIST NAMED IN THE FOLLOW ORDER: HYD SYS LEAK OR LOSS, SYS-A RESTORATION LOSS, HYD SYS LEAK OR LOSS IN RANGE APPRO AND BEFORE LAND CKLIST. PERFORM A MAIN GEAR EXT PROC AND QTY LOSS. PER CKLIST CLOSED THE HYD SYS-A FLUID SHUTOFF SWITCH WITH THE ENG RUNNING. THE FLUID SOV SWITCH WERE CLOSED FOR APPROX 10 MIN. FND AFT FILT ER HOUSING LEAK ON RT ELEV PKG. REPLACED HSNG CAP AND SEALS, LEAK CK OK.

Part: AIR DISTR — ODOR (CABIN)

AFTER LEVEL OFF AT FLT LEVEL 310, SMELLED A FAINT SCENT OF HOT ELECTRICAL INSULATION. TURNED OFF THE GASPER FAN AND THE SMELL WENT AWAY, THOUGHT WE HAD ANOTHER WHIFF ABOUT 30 MINUTES LATER. SMELL WAS VERY FAINT AND MOMENTARY SLIGHTLY STRONGER BEHIND S/O PANEL, 30 MINUTES LATER WE SMELLED IT AGAIN, NO HAZARDOUS MATERIAL ON A/C. INSPECTED GASPER FAN MOTOR, E/E COMPT, BEHIND SECOND OFFICER'S PANEL. RAN GASPER FAN AND PACKS 2 HOURS, NO SMELL NOTES. REMOVED AND REPLACED LEFT AND RIGHT WATER SEPARATOR FILTERS, OPERATIONAL CHECKS GOOD.

Part: STRINGER — CRACKED (BS 440)

UPPER LOBE STR 3L STA 440 CRACKED. INSTALLED REPAIR ON STR 3L STA 440 PER MM 53-10-3 PG 5 WITH FAB PARTS ON SHOP ORDER FE7X, FM7K, FM69.

Part: SKIN — CORRODED (BS 720)

FWD CARGO FUSELAGE SKIN CORRODED BETWEEN STR 28 LT AND RT STA 720C PLUS 5. CUT OUT CORRODED AREA AND INSTALLED DOUBLER PER SRM 53-30-3.

Part: SEAT TRACK — CORRODED (BS 804-848)

UPPER LOBE FLOOR, OVER WING AREA CORR ON O/B FLANGE FLOOR TRACK LBL 45 STA 804 TO 848 LT. INSTALLED NEW SEAT TRACK AND CHORD PER SRM 51-10-1. INSTALLATION OF FLOATING SEAT TRACK FROM STA 740 TO 760 COVERED ON NR 1415 LBL 45.

Part: BELL FRAME — CRACKED (BS 804.5)

CABIN BELL FRAME ANGLE CRACKED STA 804.5 STR 14R. INSTALLED REPAIR PER 51-40-3 PG 1 TO 4.

Part: BELL FRAME — CRACKED (BS 804.5)

CABIN, BELL FRAME CRACKED STA 804.5 STR 14R. STOP DRILLED CRACK AND INSTALLED DOUBLER 7075T6.090 PER 53-30-4 FIG 1.

Part: STRINGER — CORRODED (BS 950)

AFT CX COMP STR 29L IS CORRODED ON O/B SIDE AT BELLFRAME STA 950E, AFT SIDE OF BELLFRAME. BEYOND LIMITS PER SRM 53-10-1, REPAIRED PER FEDEX EA 7-5310-26899.

Part: DOOR JAMB — CORROSION (BS 416)

AFT LWR CORNER OF FWD GALLEY DOOR JAMB, AFT SIDE OF FRAME HEAVY CORROSION FOUND STA 416 ABOVE STR 17R. FOUND WITHIN SRM LIMITS.

Part: FLOORBEAM — CORROSION (BS 380)

CORROSION ON FLOORBEAM STA 380 RBL 23 TO 51.25 GROUND FASTENER HOLES. FOUND WITHIN SRM LIMITS.

Part: BELLFRAME — CRACKED (BS 804.5)

CABIN BELL FRAME CRACKED AT RADIUS STA 804.5, JUST ABOVE STA 145. INSTALLED REPAIR PER SRM 51-40-3 PAGE 1 TO 4 REF NR0141.

Part: STRINGER — CRACKED (BS 970)

UPPER LOBE, CRACK IN STR 7L STA 970. INSTALLED STR REPAIR PER SRM 53-10-3 PG 5 FIG 3.

Part: ANGLE — CRACKED (BS 804.5)

CABIN BELL FRAME ANGLE CRACKED STA 804.5 STR 14R. STOP DRILLED CRACK AND INSTALLED DOUBLER PER 53-10-4 FIG 1.

Part: FLOORBEAM — CORRODED (BS 344)

TOP SURFACE OF FLOORBEAM AT STA 344 CORRODED IN NUMEROUS AREAS FROM LBL 52 TO RBL 38. INSTALLED DOUBLER REPAIR ON TOP CAP OF FLOORBEAM PER DRAWING SR 27-53-007 FROM FEDEX STANDARD REPAIR DRAWING.