N485FE

Part: SLIDE — DISLODGED · airframe 43,543 hrs · 29,942 cycles

ESCAPE SLIDE HAS APPEARED TO FALLEN OUT OF IT'S CONTAINER. R & R ESCAPE SLIDE IAW MM 25-60-015-2, OPS NORMAL.

Part: SLIDE — UNSECURE · airframe 43,429 hrs · 29,849 cycles

ESCAPE SLIDE NOT FULLY CONTAINED IN DOOR CASING. RESECURED DOOR ESCAPE SLIDE MM REF: 25-60-015-2-0.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 43,424 hrs · 29,846 cycles

REPLACED L1 EMERGENCY LIGHT ASSY AND BATTERIES IAW MTSI 33-50-2465, MM REF 33-50-101-2-0. OPS CHECK GOOD. REPLACED L1 EMERGENCY LIGHT ASSY AND BATTERIES IAW MTSI 33-50-2465, MM REF 33-50-101-2-0, OPS CHECK GOOD.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 43,423 hrs · 29,845 cycles

EMERGENCY LIGHT BATTERIES ABOVE FWD ENTRY DOOR ARE DEAD. R & R BATTERIES IAW AMM 33-50-101-2-0. OPS CHECKED NORMAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 43,418 hrs · 29,837 cycles

EMERGENCY EXIT LIGHT OVER ENTRY DOOR INOPERATIVE. REPLACED BATTERIES IAW MM 33-50-101-2-0,2. (CLOSED)

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 43,415 hrs · 29,834 cycles

FWD ENTRY EMERGENCY EXIT LIGHT INOP. RELAMPED OPS GOOD 33-50-101-2-0, 33-50-001-5-0.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 43,407 hrs · 29,826 cycles

L1 DOOR OVERHEAD EMERGENCY EXIT LIGHT INOPERATIVE. R & R L1 DOOR EMERGENCY LIGHT BATTERIES. OPS CHECK NORMAL, REF MM 33-50-101-2-0.

Part: SLAT SYSTEM — MALFUNCTIONED (NR 1) · airframe 43,253 hrs · 29,711 cycles

NR 1 SLAT WOULD NOT RETRACT DURING FLAP RETRACTION COMPLIED WITH QRH LED STILL FAILED TO RETRACT, RETURNED TO MEM, ACFT DID NOT HAVE A NOTICEABLE ROLL, BOTH FRONT "L/E FLAPS" & NR 1 SLAT ON AUX PANEL "POSITION TEST" WERE AMBER INDICATION NR 1 LED STILL NOT FULLY RETRACTED. NO RESTRICTION REF: 27-82-011-4, NR 1 SLAT POSITION IND AFT JUMPER INSTALLED. F/E PANEL MM REF 27-82-011-4, OPS CHECKS GOOD IAW MM 27-82-011-4. ACFT OK FOR SERVICE.

Part: RING — DENTED (NR 3 NACELLE) · airframe 43,222 hrs · 29,664 cycles

NR 3 ENGINE NOSE COWL LIP RING DENTED AT 6 O'CLOCK POSITION. CUT-OUT DAMAGED AREA AT NR 3 ENGINE NOSE COWL LIP RING AT 6 O'CLOCK POSITION, FABRICATED REPAIR PARTS AND DOUBLER, AND INSTALLED REPAIR PARTS AND DOUBLER IAW SRM 54-30-3 FIG 2, 51-10-2, AND 51-30-2 REV 103.

Part: SKIN — GOUGED (RT WING TE FLAP) · airframe 43,222 hrs · 29,664 cycles

RT WING INBD T/E FORE FLAP GOUGED, L/E LOWER SKIN NEAR OTBD END, APPROX WBL 240. REMOVED DAMAGED AREA, FABRICATED REPAIR DOUBLER, AND INSTALLED REPAIR DOUBLER AT RT WING I/B T/E FORE FLAP L/E LOWER SKIN NEAR O/B END IAW SRM 57-50-4 FIG 1, 51- 10-1, AND 51-30-02

Part: SKIN — DENTED (BS 1263 S25L) · airframe 43,222 hrs · 29,664 cycles

DENT EXTERIOR FUSELAGE SECTION 48 STA 1263 STR 25L. CUT OUT DAMAGED AREA STA 1263 STR 25L, FABRICATED DOUBLER AND FILLER AND INSTALLED IAW SRM 53-30-2 FIG 3, SRM 53-30-3 FIG 3, SRM 51-10-2 AND SRM 51-30-2.

Part: STRINGER — CRACKED (BS 720B-C) · airframe 43,222 hrs · 29,664 cycles

CABIN STRINGER 15 R IS CRACKED AFT OF ICE LIGHT INSTALLATION BETWEEN BS 720B - 720C CUT-OUT DAMAGED AREA, FABRICATED REPAIR PARTS, AND INSTALLED IAW SRM 53-10-3 FIG 5, 51-30-2, AND 51-10-2.

Part: SKIN — MISALIGNED (BS 303-346) · airframe 43,222 hrs · 29,664 cycles

FWD ENTRY DOORWAY FUSELAGE SKIN RAIN GUTTER HAS SEVERAL RIVETS WITH LOW SPACING CUTOUT DAMAGED AREAS, FABRICATED DOUBLER, FILLER, FREEZE PLUGS, AND RAIN GUTTER, AND INSTALLED AT FWD ENTRY DOOR WAY FUSELAGE SKIN RAIN GUTTER IAW EA 7-5330-143941.

Part: SEAT TRACK — CRACKED (BS 720B-720C) · airframe 43,222 hrs · 29,664 cycles

CABIN STRINGER 15L IS CRACKED AFT OF ICE LIGHT INSTALLATION BETWEEN BS 720B - 720C CUT-OUT DAMAGED AREA AT STRINGER 15L BETWEEN STA 720B TO 720C, FABRICATED REPAIR PARTS, AND INSTALLED REPAIR PARTS IAW SRM 53-10-3 FIG 3, 51-30-2, AND 51-10-2 REV 103.

Part: ANGLE — CRACKED (BS 1263) · airframe 43,222 hrs · 29,664 cycles

AFT AIRSTAIRS RT LOWER TORQUE BOX UPPER ANGLE IS CRACKED AND LOCK FASTENERS ARE WORKING AT BS 1263, FWD SIDE. REMOVED AFT AIRSTAIRS RH LOWER TORQUE BOX UPPER ANGLE AT BS 1263 FWD SIDE, FABRICATED ANGLE, AND INSTALLED IAW SRM 53-10-2 FIG 6, 51-20-1 FIG 7, 51-10- 2, AND 51-30-2.

Part: WEB — CRACKED (LWR TORQUE BOX) · airframe 43,222 hrs · 29,664 cycles

AFT AIRSTAIRS LT LOWER TORQUE BOX INBD WEB HAS CRACK AT UPPER ROW OF RIVETS BS 1253. CUT-OUT CRACK SECTION OF WEB, FABRICATED DOUBLER AND FILLER, AND INSTALLED DOUBLER AND FILLER AT AFT AIRSTAIRS LH LOWER TORQUE BOX INBD WEB BS 1253 IAW SRM 51-40-2 FIG 1, 53-10-2 FIG 6, 51-10-1, 51-30-2, AND 51-10-2.

Part: STRINGER CLIP — DAMAGED (BS 1010) · airframe 43,222 hrs · 29,664 cycles

MISDRILLED STRINGER/FRAME ATTACH CLIP (STRINGER TIE) IN RADIUS AT BS 1010 STR 8R. REMOVED DAMAGED STRINGER TIE IAW B727 SRM 51-30-2, FABRICATED STRINGER TIE IAW BOEING DWG 65-45313, AND INSTALLED IAW B727 SRM 51-30-2.

Part: STRUCTURE — DAMAGED (BS 1233) · airframe 43,222 hrs · 29,664 cycles

AFT AIRSTAIR T/R LOWER TORQUE BOX LIGHTNING HOLE HAS EXCESSIVE ROUTE OUT, BS 1233. TRIMMED OUT DAMAGED ARE, FABRICATED DOUBLER, AND INSTALLED DOUBLER AT AFT AIRSTAIRS RT LOWER TORQUE BOX LIGHTING HOLE BS 1233 IAW 53-10-2, FIG 6 AND 51-40-2, FIG 1.

Part: SEAT TRACK — CORRODED (BS 1010-1035) · corrosion level 2 · airframe 43,222 hrs · 29,664 cycles

CORROSION ON SEAT TRACK FLANGE, STA 1010 TO 1035, RBL 45. REMOVED CORROSION IAW SRM 51-10-6. FOUND TO OUT OF LIMITS IAW SRM 53-10-1. FABRICATED SEAT TRACK AND SPLICES IAW SRM 53-10-5 REV 103. INSTALLED SEAT TRACK IAW SRM 51-30-2

Part: FLOORBEAM — CORRODED (BS 620) · corrosion level 2 · airframe 43,222 hrs · 29,664 cycles

CORROSION ON TEE CAP FLOORBEAM, STA 620, BL 0 TO RBL 25. REMOVED CORROSION. EVALUATED AREA; ORIGINAL THICKNESS .125" MATERIAL LOSS .015" MATERIAL REMAINING .110" FOUND TO BE OUT OF LIMITS. CUT OUT DAMAGED AREA APPROX DIM 100". FABRICATED TEE CAP & FILLER. FABRICATED 2 SUPPORT ANGLES, 2 STRAPS AND INSTALLED ALL REPAIR PARTS IAW SRM 51-10-6, SRM 53-10-2, SRM 53-10-1 FIG 4B, SRM 51-30-2, SRM 53-10-8 FIG 8 SRM 51-10-2 AND 51-30-2 REV 103.

Part: FRAME — CRACKED (BS 540 S21-22L) · airframe 43,222 hrs · 29,664 cycles

FWD CARGO COMPARTMENT, LOWER STUB FRAME HAS CRACK AT BS 540 BETWEEN STR 22L AND 21L.

Part: SKIN — DAMAGED (ZONE 200) · airframe 43,222 hrs · 29,664 cycles

UPON FURTHER EVALUATION OF L-1 FWD ENTRY DOOR LOWER HINGE CUTOUT REPAIR. FOUND SEVERAL FASTENERS PULLING THROUGH DOUBLER. REPLACED PREVIOUS REPAIR DOUBLER AT L1 FWD ENTRY DOOR LOWER HINGE IAW EO 7-5330-7-2345 F2 PT2.

Part: FLOORBEAM — CORRODED (BS 680) · corrosion level 2 · airframe 43,222 hrs · 29,664 cycles

CORROSION ON FLOORBEAM TEE, STA 680, BL 0 TO LBL 25. CUT-OUT DAMAGED AREA, FABRICATED FILLER, 2 REPAIR ANGLES, AND INSTALLED IAW SRM 53-10-8 FIG 8.

Part: FLOORBEAM — CORRODED (BS 1030) · corrosion level 2 · airframe 43,222 hrs · 29,664 cycles

CORROSION ON TOP TEE CAP FLOORBEAM, MAIN CABIN, STA 1030, RBL 45 TO RBL 61. CUT AND REMOVED DAMAGED AREA OF FLOOR BEAM IAW SRM 53-10-8 FIG 3 FABRICATED NEW UPPER TEE, 2 REPAIR ANGLES AND 2 REINFORCEMENT STRAPS IAW SRM 53-10-8 FIG 3. INSTALLED UPPER TEE, ANGLES AND STRAPS IAW SRM 53-10-8 FIG 3 AND 51-30-2 REV 103.

Part: SKIN — CRACKED (RT ELEVATOR) · airframe 43,222 hrs · 29,664 cycles

RT ELEVATOR LOWER SURFACE HAS A POSSIBLE CRACK 16" FROM INBD END. STOP DRILLED CRACK IAW SRM 51-10-1 REV 103 FABRICATED REPAIR DOUBLER FROM 2024 T3 .032" IAW SRM 55-20-3 FIG 4 INSTALLED REPAIR DOUBLER IAW SRM 51-30-2 AND EA 7-5750-143944

Part: FLOORBEAM — CORRODED (BS 680) · corrosion level 2 · airframe 43,222 hrs · 29,664 cycles

CORROSION ON TEE CAP TOP FLOORBEAM MAIN CABIN, STA 680, LBL 45 TO LBL 25. REMOVED CORROSION FROM FLOORBEAM TEE CAP IAW SRM 51-10-6. FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1 FIG 4B. FABRICATED 1 TEE CAP 16" LONG, SUPPORT ANGLE 16" LONG, SUPPORT ANGLE 11" LONG, STRAP 16" LONG AND STRAP 11" LONG IAW SRM 53-10-8 FIG 3 REV 103. INSTALLED REPAIR PARTS IAW SRM 53-10-8 FIG 3 REV 103.

Part: FLOORBEAM — CORRODED (BS 720D) · corrosion level 2 · airframe 43,222 hrs · 29,664 cycles

CORROSION ON FLOORBEAM TEE CAP, STA 720D, BL 0 TO LBL 25. CUT-OUT DAMAGED AREA AT FLOORBEAM TEE CAP, FABRICATED REPAIR PARTS, AND INSTALLED IAW SRM 53-10-8 FIG 8.

Part: SEAT TRACK — CORRODED (BS 970-1135) · corrosion level 2 · airframe 43,222 hrs · 29,664 cycles

CORROSION ON SEAT TRACK FLANGE, STA 1135 TO 970, RBL 25. REMOVED DAMAGED SEAT TRACK SECTION, FABRICATED NEW SEAT TRACK SECTION AND INSTALLED IAW SRM 53-10-5 FIG 1 AND SRM 51-30-2.

Part: SKIN — GOUGED (HORIZONTAL STAB) · airframe 43,222 hrs · 29,664 cycles

RT HORIZ STAB LOWER SKIN AFT OF ACCESS PANEL 9206 IS GOUGED. REMOVED GOUGE ON RT HORIZONTAL STAB LOWER SKIN IAW SRM 51-10-1. FOUND TO BE OUT OF LIMITS IAW SRM 55-10-1 FIG 2 ORIGINAL MATERIAL .063" MATERIAL REMOVED .016" MATERIAL REMAINING .047". REMOVED DAMAGE IAW SRM 55-10-3 FIG 3 DIM 1" X 2". FABRICATED DOUBLER 13" X 14" AND FILLER FROM .063" IAW SRM 55-10-3 FIG 3 REV 103 INSTALLED REPAIR PARTS IAW SRM 55-10-3 FIG 3.

Part: STRINGER — CORRODED (BS 1166-1183) · corrosion level 2 · airframe 43,222 hrs · 29,664 cycles

STRINGER 22L IS CORRODED FROM BS 1166 TO 1183. REMOVED CORRODED STRINGER SECTION IAW SRM 53-10-3 FIG 1. FABRICATED NEW STRINGER SECTION AND SPLICE IAW SRM 53-10-3 FIG 1. INSTALLED NEW STRINGER AND SPLICE IAW SRM 51-30-2 AND 53-10-3 FIG 1 REV 103.

Part: SKIN — CORRODED (BS 1166-1183) · corrosion level 2 · airframe 43,222 hrs · 29,664 cycles

AFT LAV ACCESS PANEL CUT OUT INNER DOUBLER IS CORRODED BS 1166 TO 1183. REMOVED CORRODED INNER SKIN DOUBLER AND CUT OUT SKIN SECTION IAW SRM 53-30-3 FIG 12. FABRICATED NEW SKIN SECTION, INNER DOUBLER AND SKIN SPLICE IAW SRM 53-30-3 FIG 12. INSTALLED SKIN, DOUBLER AND SPLICE IAW SRM 53-30-3 FIG 12 REV 103

Part: WEB — CORRODED (BS 1166) · corrosion level 2 · airframe 43,222 hrs · 29,664 cycles

SURFACE CORROSION STA 1166, PLUS 7", LBL 50. REMOVED LAV PAN LOWER WEB AND ANGLE IAW SRM 51-30-2 FABRICATED NEW WEB AND ANGLE IAW SRM 51-20-1 FIG 7 AND 51-30-5 INSTALLED NEW WEB AND ANGLE IAW SRM 51-30-2 REV 103

Part: SEAT TRACK — CORRODED (BS 480-690) · corrosion level 2 · airframe 43,222 hrs · 29,664 cycles

CORROSION ON SEAT TRACK FLANGE STA 480-690 RBL 25. REMOVED SEAT TRACK SECTION IAW SRM 51-30-2, FABRICATED NEW SEAT TRACK AND INSTALLED IAW SRM 53-10-2 FIG 7, 51-30-5, 51-10-1, 51-10-2 AND 51-30-2 REV 103.

Part: SEAT TRACK — CORRODED (BS 690-740) · corrosion level 2 · airframe 43,222 hrs · 29,664 cycles

CORROSION ON SEAT TRACK FLANGE MAIN CABIN STA 690-740, RBL 45. REMOVED SEAT TRACK , FABRICATED NEW SEAT TRACK AND SPLICE, AND INSTALLED IAW SRM 53-10-5 FIG 1 AND 51-30-2.

Part: SEAT TRACK — CORRODED (BS 690-740) · corrosion level 2 · airframe 43,222 hrs · 29,664 cycles

CORROSION ON SEAT TRACK FLANGE, MAIN CABIN, STA 690-740, RBL 25. REMOVED SEAT TRACK IAW SRM 51-30-2 REV 103. FABRICATED SEAT TRACK AND REPAIR SPLICE IAW SRM 53-10-5 FIG 1. INSTALLED IAW SRM 53-10-5 FIG 1 AND 51-30-2.

Part: FLANGE — CORRODED (BS 950-1135) · corrosion level 2 · airframe 43,222 hrs · 29,664 cycles

CORROSION ON SEAT TRACK FLANGE MAIN CABIN STA 1135 TO STA 950 10" LBL 25. REMOVED SEAT TRACK, FABRICATED NEW SEAT TRACK, AND INSTALLED IAW SRM 53-10-2 FIG 7, 51-30-2, 51-30-5, 51-10-1, AND 51-10-2.

Part: SEAT TRACK — CORRODED (BS 480-690) · corrosion level 2 · airframe 43,222 hrs · 29,664 cycles

CORROSION ON SEAT TRACK FLANGE STA 690-480 LBL 45. REMOVED SEAT TRACK, FABRICATED NEW SEAT TRACK, AND INSTALLED IAW SRM 53-10-2 FIG 7, 51-30-2, 51-20-1, 51-30-5 AND 51-10-2.

Part: SKIN — CHAFED (BS 720D S19L) · airframe 43,222 hrs · 29,664 cycles

LT AFT FUSELAGE SKIN CHAFED AT STR 19L, BS 720D, 10". CUT-OUT DAMAGED AREA, FABRICATED DOUBLER AND STRUCTURAL FILLER, AND INSTALLED IAW SRM 53-30-1 FIG 5, 51-10-2, 51-30-8, AND 53-30-3 FIG 4.

Part: SEAT TRACK — CORRODED (BS 480-690) · corrosion level 2 · airframe 43,222 hrs · 29,664 cycles

CORROSION ON SEAT TRACK FLANGE STA 480-690, RBL 45. REMOVED SEAT TRACK SECTION, FABRICATED NEW SEAT TRACK SECTION, AND INSTALLED IAW SRM 53-10-2 FIG 7 AND 51-30-2.

Part: SEAT TRACK — CORRODED (BS 720-740) · corrosion level 2 · airframe 43,222 hrs · 29,664 cycles

CORROSION ON SEAT TRACK FLANGE, STA 740-720, BL 0. REMOVED SEAT TRACK IAW SRM 51-30-2. FABRICATED SEAT TRACK IAW SRM 53-10-2 FIG 7A AND SRM 51-20-1, 51-30-5. TREATED AND PRIMED IAW SRM 51-10-2. INSTALLED IAW SRM 51-30-2 REV 103.

Part: SEAT TRACK — CORRODED (BS 690-740) · corrosion level 2 · airframe 43,222 hrs · 29,664 cycles

CORROSION ON SEAT TRACK FLANGE STA 740-690 LBL 25. REMOVED SEAT TRACK IAW SRM 51-30-2. FABRICATED, LOCATED AND DRILLED NEW SEAT TRACK AND SPLICE IAW SRM 53-10-5 FIG 1. INSTALLED IAW SRM 51-30-2 REV 103.

Part: SEAT TRACK — CORRODED (BS 950-1135) · corrosion level 2 · airframe 43,222 hrs · 29,664 cycles

CORROSION ON SEAT TRACK MAIN CABIN STA 1135 TO STA 950, 10" LBL 45. REMOVED DAMAGED SEAT TRACK, FABRICATED NEW SEAT TRACK, AND INSTALLED IAW SRM 53-10-2 FIG 7, 51-20-1, 51-10-1, AND 51-30-2.

Part: SEAT TRACK — CORRODED (BS 690-480) · corrosion level 2 · airframe 43,222 hrs · 29,664 cycles

CORROSION ON SEAT TRACK FLANGE STA 690-480, BL 0. REMOVED DAMAGED SEAT TRACK SECTION, FABRICATED NEW SEAT TRACK AND INSTALLED IAW SRM 53-10-1 FIG 3A, SRM 53-10-2 FIG 7A, SRM 51-30-2, 51-20-1, 51-10-2, 51-30-5, AND 51-10-1.

Part: FLOORBEAM — CORRODED (BS 328) · corrosion level 2 · airframe 43,222 hrs · 29,664 cycles

CORROSION ON TOP TEE CAP FLOORBEAM MAIN CABIN ENTRY WAY, STA 328, LBL 35. CUTOUT DAMAGED AREA, FABRICATED TEE CAP AND REPAIR ANGLES, & INSTALLED IAW SRM 53-10-1, FIG 1, 53-10-8 FIG 9, 51-30-5, 51-10-2, 51-30-2, AND FAS ENGINEERING REPORT NR 2-37153-801, REV A.

Part: SEAT TRACK — CORRODED (BS 480-690) · corrosion level 2 · airframe 43,222 hrs · 29,664 cycles

CORROSION ON SEAT TRACK FLANGE MAIN CABIN STA 690-480, LBL 25. REMOVED SEAT TRACK, FABRICATED SEAT TRACK AND INSTALLED IAW SRM 53-10-2 FIG 7, 51-20-1, 51-10-1, 51-10-2, AND 51-30-2.

Part: SEAT TRACK — CORRODED (BS 690-740) · corrosion level 2 · airframe 43,222 hrs · 29,664 cycles

CORROSION ON SEAT TRACK FLANGE, STA 740-690, LBL 45. REMOVED DAMAGED SEAT TRACK, FABRICATED NEW SEAT TRACK AND SPLICE REPAIR, AND INSTALLED IAW SRM 53-10-5 FIG 1, 51-30-2, AND 51-10-2.

Part: LIGHT — INTERMITTENT (L1 DOOR) · airframe 43,085 hrs · 29,561 cycles

L1 DOOR EMERGENCY EXIT LIGHT INTERMITTENT. R & R EMERGENCY EXIT PORTABLE LIGHT ASSY, REF MM33-50-101-2-0, OPS CHECK GOOD.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 42,782 hrs · 29,319 cycles

DURING SERVICE CHECK FOUND COCKPIT EMERGENCY EXIT LIGHT INOP. INSTALLED NEW BATTERIES IN EMERGENCY LIGHT ASSY IAW AMM 33-50-001-2. OPS CHECKS GOOD.

Part: ACTUATOR — FAILED (TE FLAPS) · airframe 42,639 hrs · 29,206 cycles

AFTER TAKEOFF, DURING FLAP RETRACTION FROM FLAPS 2, DEG TO FLAPS 0 AMBER LE FLAP LIGHT REMAINED ILLUMINATED. COMPLIED WITH STABILIZER AND IDENTIFIED NR3 SLAT STILL DEPLOYED. EXECUTED RED TABS BUT UNABLE TO ATTAIN CLEAN ACFT CONFIG NR 3 SLAT. REMAINED DEPLOYED AFTER LANDING NR 3 SLAT STILL REMAINED DEPLOYED WITH FLAP HANDLE UP. R & R NR 3 LEADING EDGE SLAT ACTUATOR PER MM 27-81-032-4 NO DEFECTS NOTED. LEADING SLAT SYS OK FOR CONTINUED SERVICE.

Part: MODULE — FAILED (FLAP SYSTEM) · airframe 42,456 hrs · 29,058 cycles

DURING FLAP RETRACTION FROM 5 DEG TO 2 DEG NOTICED LE FLAPS LIGHT ILLUMINATED WITH ASSOCIATED NR 1 FLAP AMBER LIGHT ILLUMINATED ON POS TEST PANEL. CONSULTED QRH AND COMPLIED WITH LED FAILURE DURING FLAP RETRACTION CHECKLIST. HAD NO ABNORMAL ROLL WITH LIGHT ILLUMINATED. REMOVED AND REPLACED L/E POS CONTROL MODULE IAW MM 27-82-000-1. REMOVED AND REPLACED NR 1 LE FLAP MICRO SWITCH IAW SRM 27-80-000. CYCLED FLAPS SEVERAL TIME WITH "B" PUMPS AND GROUND INTERCONNECT AND ALSO WITH ENGINE NR 1 AND NR 2 RUNNING. ALL FLAP OPS AND INDICATIONS NORMAL.

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 41,780 hrs · 28,484 cycles

LEFT AFT AIR STAIR AREA, BS 1262 SHEAR TIE CRACKED BETWEEN S11-12L REMOVED CRACKED SHEAR TIE, FABRICATED, TREATED AND PRIMED AND INSTALLED SHEAR TIE REPAIR. REF SRM 51-10-2, SRM 51-30-2 PG 1-4, SRM 53-10-04, NDT HOLES AND COUNTERSINKS, NO DEFECTS NOTED, REF NDT MANUAL PART 6. 51-00-00 AND 53-30-00. THIS IS CLASSIFIED AS A MAJOR REPAIR

Part: CASTING — CORRODED (DOOR HANDLE) · corrosion level 2 · airframe 41,780 hrs · 28,484 cycles

L/H FWD EMERGENCY DOOR CASTING AROUND HANDLE HOUSING IS CORROSION REPLACED CASTING AROUND HANDLE HOUSING REF SRM 51-30-02 PG 1-5. OPS CHECK OF DOOR OK THIS IS CLASSIFIED AS A MINOR REPAIR.

Part: SHEAR TIE — SHEARED (BS 660) · airframe 41,780 hrs · 28,484 cycles

CABIN LEFT SIDE BS 660 FRAME, FWD SIDE SHEAR TIE BETWEEN STR 14L & 15L, 1 EA FASTENER BUCKTAIL SHEARED OFF BLEND OUT TRIPLER, PREFORMED HFEC, NO DEFECTS NOTED. INSTALLED RIVET, FILLED GAP WITH SEALENT, PAINT TO MATCH, ALL IN REF TO EA 7-5330-113102. THIS IS CLASSIFIED AS A MINOR REPAIR.

Part: SKIN — CRACKED (ZONE 500) · airframe 41,780 hrs · 28,484 cycles

LEFT WING UPPER SURFACE SKIN CRACKED AT NR 4 SPOILER I/B ACTUATOR HINGE CUTOUT REMOVED AND REINSTALLLED NR 4 SPOILER PANEL, FABRICATED, TREATED, PRIMED, PAINTED, AND INSTALLED DOUBLER REF SRM 57-30-4, 51-10-2, 51-30-2 AND MM 51-20-000-7, MM 27-61-081-4. STOP DRILLED CRACK TO .250" REF SRM 57-30-4, NDT STOP DRILL REF D6-48875, 51-00-00 NO DEFECTS FOUND. SPOILER BOARD OPS CHECK GOOD ON N/R N00480, THIS IS CLASSIFIED AS A MINOR REPAIR.

Part: DOOR FRAME — CRACKED (ZONE 200) · airframe 41,780 hrs · 28,484 cycles

MAIN ENTRY DOOR 1L CUTOUT, AFT FRAME, BS 344, STR 15L JUST BELOW 2ND STOP FITTING FROM BOTTOM, FRAME CRACKED FABRICATED REPAIR PARTS PER DWG 65-17685-24, -9, -7. REPLACED LWR AFT FRAME REF SRM 51-30-2. THIS IS CLASSIFIED AS A MAJOR REPAIR.

Part: PANEL — CRACKED (ZONE 100) · airframe 41,780 hrs · 28,484 cycles

FWD LOWER CARGO BAY, DOOR THRESHOLD WRAP AROUND SCUFF PLATE CRACKED IN SEVERAL AREAS REMOVED THRESHOLD REF SRM 51-30-2, WELDED CRACKS REF DWG SR27-53-025 REV.C ON N/R N00383. INSTALLED THRESHOLD REF SRM 51-30-2 PG 2-14 THIS IS CLASSIFIED AS A MINOR REPAIR.

Part: GUSSET — CORRODED (CARGO DOOR FRAME) · corrosion level 2 · airframe 41,780 hrs · 28,484 cycles

LOWER FWD CARGO DOOR S/N 822, INTERNAL LOWER FRAME, 2 GUSSETS ARE CORRODED AT LWR END. 1 AT 28" AFT, 2ND AT 39" AFT. REMOVED AND REPLACED GUSSETS REF SRM 51-30-02 P 1-4. THIS IS CLASSIFIED AS A MINOR REPAIR.

Part: WEB — CRACKED (ZONE 800) · airframe 41,780 hrs · 28,484 cycles

LT MED 1L INTERIOR LOWER FWD CORNER BOTTOM WEB CRACKED APPROX 3/4" FROM INNER SKIN. REMOVED DAMAGE REF SRM 51-40-2 VARIFIED DAMAGE REMOVAL PER HFEC NDT MANUAL PART 6, 51-00-00. FABRICATED REPAIR PARTS REF SRM 51-40-2 INSTALLED REPAIR PARTS REF SRM 51-30-2 THIS IS CLASSIFIED AS A MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,780 hrs · 28,484 cycles

CABIN SEAT TRACK RBL 45, BS 940-950 OB FLANGE UPPER SURFACE CORRODED REF SNRM N00460 REMOVED AND REINSTALLED FLOOR BOARDS BS 850-950D RBL 24-45 REMOVED CORROSION ON SEAT TRACK OUT OF LIMITS REMOVED, FABRICATED, TREATED, PRIMED, PAINTED, AND INSTALLED SEAT TRACK STA 890-950+10" REF SRM 51-30-2, 51-10-6, 53-10-1, MM 51-20-071, 53-20-012-4, DWG 65-19601.

Part: CHANNEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,780 hrs · 28,484 cycles

A/C BAY FAIRING SUPPORT CHANNEL AT BS 776 LBL9-RBL9 CORRODED ON INNER SURFACE. CORROSION FOUND OUT OF LIMITS REF SRM 53-10-1. REMOVED PANELS 3358L, 3458R & 3217 FOR ACCESS REF SRM51-30-2. REMOVED STIFFNER, BRACKET, & CHANNEL. FABRICATED NEW STIFFNER, BRACKET, & CHANNEL REF SRM 51-20-1. HEAT TREATED TO T6 REF FORM 8130-3 2008-09-134 & 2008-09-135. REINSTALLED AFTER TREAT AND PRIME REF SRM 51-10-2 &51-30-2 P1-7. REINSTALLED PANELS 3358L, 3458R &3217 REF SRM 51-30-2 P1-7. THIS IS CLASSIFIED AS A MINOR REPAIR.

Part: SEAT TRACK — CORRODED (BS 940-950) · corrosion level 2 · airframe 41,780 hrs · 28,484 cycles

CABIN SEAT TRACK, RBL 24, BS 940-950, OB FLANGE HAS LIGHT CORROSION ON UPPER SURFACE REF SNRM N00460 REMOVED AND REINSTALLED FLOOR BOARDS BS 850-950E BL 0 TO RBL 25. REMOVED CORROSION ON SEAT TRACK OUT OF LIMITS. REMOVED, FABRICATED, TREATED, PRIMED, PAINTED AND INSTALLED SEAT TRACK STA 890-950+10" REF SRM 51-30-2, 51-10-6, 53-10-1, MM 51-20-071, 53-20-012-4, DWG 65-19601, BAC1520-792. THIS IS CLASSIFIED AS A MINOR REPAIR

Part: PAN — CRACKED (ZONE 100) · airframe 41,780 hrs · 28,484 cycles

RT EXT FUSE FWD LAV SERVICE PAN IS CRACKED AT LOOSE DUMP CABLE FEED THROUGH BS 301, S18-20R GAINED ACCESS TO CRACKED AREA CLAENED AND REPAIRED CRACKS BY WELDING REF EA7-5240-114036. THIS IS CLASSIFIED AS A MINOR REPAIR

Part: PLATE — CRACKED (ZONE 100) · airframe 41,780 hrs · 28,484 cycles

AFT LOWER CARGO BAY, DOOR THRESHOLD WRAP AROUND PLATE CRACKED REMOVED AFT CARGO THRESHOLD, WELDED CRACK ON N/R NOO382 REINSTALLED THRESHOLD REF SRM 51-30-2. THIS REPAIR IS CLASSIFIED AS A MINOR REPAIR

Part: ATTACH ANGLE — CORRODED (BS 910) · corrosion level 2 · airframe 41,780 hrs · 28,484 cycles

LT MLG WHEEL WELL ABOVE GEAR UPLOCK MECANISM, BS 910 LBL 64 TO LBL 68 WL 194 FWD SIDE OF BOX FRAME LOWER ATTACH ANGLE CORRODED AND CORROSION EMINATING FROM UNDER ANGLE ON LOWER WEB REMOVED ANGLE REF SRM 51-30-2, CLEANED AREA AT SURFACE OF LOWER WEB, NO CORROSION FOUND REF SRM 51-10-2 INSTALLED ATTACH ANGLE REF SRM 51-30-2. (CLASSIFIED AS A MINOR REPAIR)

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,780 hrs · 28,484 cycles

TRACK AT STA 870 TO 890 RBL 24 IS CORRODED. REMOVED CORROSION ORIGINAL MATERIAL THICKNESS .100 MATERIAL LOSS .026 REMAINING .074 OUT OF LIMITS. FABRICATED, TREATED, AND PRIMED SEAT TRACK SECTION STA 870-890 RBL 24 SEAT TRACK SECTION TO BE INSTALLED ON N/R 00782 REF SRM 53-10-0 P16, 51-10-2P7, DWG 69-04121, THIS IS CLASSIFIED AS A MINOR REPAIR

Part: RETAINER — CORRODED (EMERGENCY EXIT) · corrosion level 2 · airframe 41,780 hrs · 28,484 cycles

RT FWD EMERGENCY EXIT HATCH, SEAL RETAINER LOWER AFT HAS CORROSION. FABRICATED SEAL RETAINER REF DWG 50-07978. DRILLED AND TRIMMED SEAL RETAINER REF SRM 51-30-5, TREATED AND PRIMED REF SRM 51-10-2, PAINTED REF MM 51-20-000-7 LABELED RETAINER 65-07978-69 REF GMM 7-0-1001 THIS IS CLASSIFIED AS A MINOR REPAIR.

Part: FLOOR SUPPORT — CRACKED (BS 950A) · airframe 41,780 hrs · 28,484 cycles

CRACKED IN FLOOR BOARD "Z" ANGLE SUPPORT WEB AT FS 950A + 16, LBL 17, WL 144 REMOVED AND REPLACED SUPPORT WEB REF SRM 51-30-2 PG 1-10 THIS IS CLASSIFIED AS A MINOR REPAIR

Part: ANGLE — CRACKED (ZONE 100) · airframe 41,780 hrs · 28,484 cycles

RT MAIN GEAR WHEEL WELL AFT BULKHEAD UPPER OB CORNER BS 950 APPROX RBL 67, PRESSURE DECK ATTACH REPAIR ANGLE CRACKED. REMOVED FLOOR PANEL FOR ACCESS, REMOVED REPAIR ANGLE REF SRM 51-30-2. FABRICATED SPLICE PLATE REF DWG 65-89360. TREATED PRIMED SPLICE PLATE REF SRM 51-10-2. DRILLED UP NEW ANGLE 69-61504-4 REF SRM 51-30-5 PG1 INSTALLED SPLICE PLATE AND ANGLE REF SRM51-30-2 PG 1-9 INSTALLED FLOOR PANELS STA 870-950D RBL 45-62 REF SRM 51-30-2 PGS 1-12 THIS IS CLASSIFIED AS A MAJOR REPAIR

Part: FITTING — WORN (ZONE 800) · airframe 41,780 hrs · 28,484 cycles

LEFT AFT ENTRY DOOR, FWD LOWER STOP PIN LUG HAS WORN FLAT SPOT REMOVED AND REPLACED L2 DOOR REF AMM 52-14-000-4. REMOVED AND REPLACED FWD LWR STOP FITTING REF SRM 51-30-02. REMOVED AND REPLACED PRESSURE SEAL REF AMM 52-12-011-4 THIS IS CLASSIFIED AS A MAJOR REPAIR.

Part: ATTACH ANGLE — CRACKED (RT WING) · airframe 41,780 hrs · 28,484 cycles

RIGHT WING, CRACK IN L/E TOP SKIN ATTACH ANGLE ON LEADING EDGE FRAME AT SLAT STATION 0 AT I/B END OF NR 5 SLAT FABRICATED NEW ATTACH ANGLE ON RT WING L/E FRAME AT SLAT STA. 0.296. AT I/B END OF NR 5 SLAT REF DWG 65-16209,TREATED, PRIMED, PAINTED AND INSTALLED REF SRM 51-10-2, MM 51-20-151-7, SRM 51-30-2. THIS IS CLASSIFIED AS A MINOR REPAIR

Part: WEB — GOUGED (ZONE 100) · airframe 41,780 hrs · 28,484 cycles

FWD MAIN ENTRY DOOR FUSELAGE CUTOUT, SILL WEB HAS NUMEROUS GOUGES, UPPER SURFACE BS 320 LBL 64, BLENDED GOUGES GENERATED EA FOR BLEND ALLOWANCE, BLEND IS WITHIN LIMITS REF EA7-5310-123801 TREATED AND PRIMED REF EA 7-5310-123801 THIS IS CLASSSIFIED AS A MINOR REPAIR.

Part: RETAINER — CORRODED (ZONE 800) · corrosion level 2 · airframe 41,780 hrs · 28,484 cycles

LEFT FWD EMERGENCYEXIT HATCH, SEAL RETAINER ON DOOR HAS CORROSION. REPLACED SEAL RETAINER TOP SIDE OF LT FWD EMERGENCY DOOR REF DWG 50-7978 AND SRM 51-30-2 THIS IS CLASSIFIED AS A MINOR REPAIR.

Part: ANGLE — CORRODED (BS 950D) · corrosion level 2 · airframe 41,780 hrs · 28,484 cycles

PANEL RACK- AFT PIT "Z" ANGLE BS 950D 10" LT SIDE HAS CORROSION ON TOP SIDE REMOVED CORROSION MATERIAL LOSS OF .015 ORIGINAL THICKNESS .056 REMAINING MATERIAL .041 FOUND OUT OF LIMITS REF SRM 53-10-1. TRANSFERED HOLES TO NEW PART (65-57568-13) AND INSTALLED NUT PLATES REF SRM51-30-2 TREATED AND PRIMED REF SRM 51-10-2 AND MM 51-20-151-7. THIS IS CLASSIFIED AS A MINOR REPAIR

Part: RETAINER — CRACKED (EMERGENCY EXIT) · airframe 41,780 hrs · 28,484 cycles

RIGHT FWD EMERGENCY EXIT HATCH, SEAL RETAINER ON DOOR, HOLE CRACKED OUT, LOWER AFT CORNER DRILLED AND INSTALLED NEW SEAL RETAINER ON RT FWD EMERGENCY EXIT HATCH ON LOWER CORNERS. REF SRM 51-30-2, PAINTED SEAL RETAINER REF MM 51-20-000-7 THIS IS CLASSIFIED AS A MINOR REPAIR.

Part: RETAINER — CRACKED (EMERGENCY EXIT) · airframe 41,780 hrs · 28,484 cycles

RIGHT AFT EMERGENCY EXIT HATCH, SEAL RETAINER ON DOOR, HAS HOLE CRACKED OUT. REPLACED UPPER SEAL RETAINER ON RT AFT EMERGENCY EXIT HATCH REF DWG 50-7978 AND SRM 51-30-2 PAINTED SEAL RETAINER REF MM 51-20-000-7 THIS IS CLASSIFIED AS A MINOR REPAIR

Part: SUPPORT ANGLE — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,780 hrs · 28,484 cycles

LT MLG WHEEL ABOVE GEAR UPLOCK MECHANISM, INSIDE BOX FRAME FWD LOWER CORNER, BS 910 LBL 64 TO LBL 68, WL 194, HAS CORROSION. REMOVED CORROSION , FOUND TO BE OUT OF LIMITS, REMOVED UP LOCK ACTUATOR. REMOVED WEB AND ANGLE ATTACHED TO FRAME. FABRICATED ANGLE, INSTALLED NEW WEB, NEW SUPPORT ANGLE FOR ACTUATOR, REINSTALLED UP LOCK ACTUATOR. REF DWG 65-24480, SRM 51-30-2. CLASSIFIED AS A MINOR REPAIR.

Part: RETAINER — CRACKED (ZONE 100) · airframe 41,780 hrs · 28,484 cycles

NR 1 CARGO DOOR SEAL RETAINER HAS TWO CRACKS, DRILLED NEW SEAL RETAINER, FWD LOWER CORNER OF NR 1 CARGO DOOR. INSTALLATION TO BE COMPLETED ON EO 7-5310-7-3369C, REF SRM 51-30-2. THIS IS CLASSIFIED AS A MINOR REPAIR

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,780 hrs · 28,484 cycles

AFT CARGO BILGE FRAME SHEAR TIE CORRODED, BS 950B S28R WL 140 . REMOVED CORROSION REF SRM 51-10-1. HFEC ORIGINAL "T" IS .100', LOSS AT DEEPEST POINT IS .018" REMAINING "T" .082", OUT OF LIMITS REF SRM 53-10-1, REMOVED WEB STIFFNER AND CARGO TIE DOWN TO F.O.M. REPLACED SHEAR TIE REF SRM 51-30-2. REINSTALLED STIFFNER AND CARGO TIE DOWN REF. 51-30-02, CLASSIFIED AS A MAJOR REPAIR.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 41,780 hrs · 28,484 cycles

MAIN ENTRY DOOR, AFT CUTOUT STRUCTURE BS 344 STR 15R INTERCOSTAL FWD ATTACH ANGLE TO FRAME CRACKED. FABRICATED ANGLE REF BOEING DRAWING 69-16970, SOPM 20-42-03 PG 3, SOPM 20-44-04-PG 3. REPLACED ANGLE REF SRM 51-30-2. THIS IS CLASSIFIED AS A MINOR REPAIR.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,780 hrs · 28,484 cycles

FWD PIT DOOR CUTOUT LWR SILL BEAM TIE DOWN FITTING ASSY ADAPTER PLATE IS CORRODED, BS 565, STR 26R, WL 155. REMOVED ADAPTER PLATED STA 580 REF 51-30-02 PG 1. MATCHED DRILLED FASTENER HOLES REF SRM 51-30-05 DWG 69-55655, PAINTED ADAPTER REF SRM 51-20-00 PG 7. INSTALLED ADAPTER PLATE REF 51-30-02 PG 1. THIS IS CLASSIFIED AS A MINOR REPAIR.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 41,780 hrs · 28,484 cycles

FWD CARGO DOOR (PIT DOOR), EXTERNAL SKIN CRACKED, 30 INCHES AFT OF LEADING EDGE, 3 INCHES ABOVE LOWER EDGE CUTOUT DAMAGE, PERFORMED HFEC INSP OF CUTOUT. NO DEFECTS NOTED. PERFORMED INSURANCE CUT. FABRICATED DOUBLER AND TREATED AND PRIMED REPAIR PARTS AND REPAIR AREA. INSTALLED AND SEALED DOUBLER. REPAIR IS A CAT "B" REPAIR DUE TO FASTENERS IN CRITICAL ROW ON INTERNAL STRUCTURE. REF SRM 52-00-3 FIG 3. THIS IS CLASSIFIED AS A MAJOR REPAIR.

Part: SUPPORT BRACKET — CRACKED (T/E FLAP) · airframe 41,780 hrs · 28,484 cycles

LEFT WING NR 1 FLAP TRACK - FLAP TRACK TO LOWER TRAILING EDGE PANEL SUPPORT BRACKET IS CRACKED. FABRICATED AND INSTALLED NEW BRACKET REF DWG 65-2289. THIS IS CLASSIFIED AS A MINOR REPAIR.

Part: SHEAR TIE — CORRODED (BS 1050 S27L) · corrosion level 2 · airframe 41,780 hrs · 28,484 cycles

AFT CARGO PIT BS 1050 AT STRINGER 27L BULGE BETWEEN SKIN AND FRAME REMOVED SHEAR TIE AND FOUND PART TO HAVE EXFOLIATION CORROSION. FABRICATED NEW SHEAR TIE FROM 7075-O AND HEAT TREATED TO T-6. DRILLED FASTENER HOLES. TREATED AND PRIMED AND PAINTED SHEAR TIE. INSTALLED SHEAR TIE. REF SRM 51-30-02 PG 1-12, DWG DOCUMENT 65-16343 / NON ROUTINE N00721, SRM 51-10-2 PG 1-12

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,780 hrs · 28,484 cycles

AFT CARGO PIT-STA 1166-1148 RBL 22 CORROSION ON FLOOR SUPPORT REMOVED CORROSION, MATERIAL OUT OF LIMITS. FABRICATED A NEW ANGLE REF BOEING DWG BAC 1490-2711. TREATED AND PRIMED, THIS IS CLASSIFIED AS A MINOR REPAIR.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,780 hrs · 28,484 cycles

MAIN CABIN BS 1110 SEAT TRACK AT RBL 45 IS CORRODED REMOVED AND REINSTALLED FLOORBOARDS RBL 24 TO RBL 62 STA 1070-1110. REMOVED CORROSION ON SEAT TRACK ORIGINAL MATERIAL THICKNESS .070 MATERIAL LOSS .022. REMAINING .048 OUT OF LIMITS AAR TOOL IN17-0112 CAL DUE 12-11-08. REMOVED SEAT TRACK SECTION STA 1110=1135. FABRICATED TREATED, PRIMED, AND INSTALLED NEW SEAT TRACK SECTION STA 1110-1135 RBL 45. DISPLACED AND REINSTALLED CEILING PANEL STA 1130-1140 RBL 25-50, REF SRM 51-30-2, 51-10-6, 53-10-1 FIG 3, AND DWG 65-19601. THIS IS CLASSIFIED AS A MAJOR REPAIR.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,780 hrs · 28,484 cycles

AFT CARGO PIT-STA 1166-1148 RBL 22 CORROSION ON FLOOR SUPPORT REMOVED CORROSION, MATERIAL OUT OF LIMITS. FABRICATED A NEW ANGLE REF BOEING DWG BAC 1490-2711. TREATED AND PRIME THIS IS CLASSIFIED AS A MINOR REPAIR

Part: ATTACH FITTING — CRACKED (NR 4 FLAP TRACK) · airframe 41,780 hrs · 28,484 cycles

"PANEL RACK" INBD T/E NR 4 FLAP TRACK AFT FAIRING HAS CRACK IN MOUNT BRACKET AT FWD OUTBOARD END. FABRICATED NEW MOUNT BRACKET AND INSTALLED REF BOEING DOCUMENT 65-21795, SRM51-30-2 PG1-8 GMM 7-0-1001, SRM 51-10-2 PG 7, MM 51-20-151-7 PG 1. THIS IS CLASSIFIED AS A MINOR REPAIR.

Part: RETAINER — CRACKED (DOOR SEAL) · airframe 41,780 hrs · 28,484 cycles

LT FWD EMERGENCY EXIT HATCH, SEAL RETAINER ON DOOR HAS SEVERAL HOLES CRACKED OUT. REPLACED AFT ATTACH ANGLE. FABRICATED ATTACH ANGLE REF: DWG NR 50-07978. TREATED, PRIMED AND PAINTED REF:SRM 51-10-2 PG 1-10 AND MM 51-20-151-7 PG 1. INSTALLED REF SRM 51-30-2 PG 1. THIS IS CLASSIFIED AS A MINOR REPAIR.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 41,780 hrs · 28,484 cycles

AFT CARGO PIT STA 1010 SIDEWALL SUPPORT CORRODED AT FASTENER HOLES OVER STRINGER 27-26L. BLENDED CORRODED AREA, ORIGINAL "T" .050, REMOVED .014 REMAINING .036 OUT OF LIMITS. SUPPORT FABRICATED FROM 2024-0-.040, HEAT TREAT T3 CONDITION, APPLIED ALODINE, PRIMED, INSTALLED SUPPORT. REF SRM 51-10-2 P7, 53-10-1 P1-2A, 51-30-2 P8 MM 51-20-151-7 P1. THIS IS CLASSIFIED A MINOR REPAIR.

Part: FLAP TRACK — GOUGED (T/E FLAP) · airframe 41,780 hrs · 28,484 cycles

LEFT WING O/B FLAP TRACK I/B EDGE OF TOP FLANGE GOUGED APPROX 14" AFT OF REAR SPAR. BLENDED GOUGE, MATERIAL REMOVED .015 WITHIN LIMITS. MAGNETIC PARTICLE INSPECTED, FLAP PEENED REWORKED AREA, APPLIED ALODINE & PRIMED REF EA 7-5750-118300 P2 PART 1 CLASSIFIED AS A MINOR REPAIR.

Part: STRINGER — CORRODED (BS 1150 S26R) · corrosion level 2 · airframe 41,780 hrs · 28,484 cycles

AFT CARGO PIT, STA 1150, RBL 24, CORROSION ON UNDER SIDE OF STRINGER 26. REMOVED CORROSION STR 26 R ORIGINAL .090, REMOVED .032, REMAINING .058 OUT OF LIMITS. FABRICATE STRINGER & SPLICES. ALODINED PRIMED PARTS, INSTALLED REPAIR PARTS REF SRM 53-10-1, 53-10-3 FIG 1, DWG65-16348. THIS IS CLASSIFIED A MAJOR REPAIR.

Part: PANEL — PUNCTURED (HORIZONTAL STAB) · airframe 39,969 hrs · 27,046 cycles

PANEL 9117 HAS PUNCTURE ON LOWER SURFACE, I/B END. *S/D* REPAIRED PANEL 9117 PER FED EX EA 7-5510-96628.

Part: TIE — CORRODED (VERTICAL STAB) · airframe 39,969 hrs · 27,046 cycles

FOUND RT FWD HORIZONTAL TENSION TIE O/B FITTING LUG, O/B FACE IS CORRODED. REPAIRED PER EA 7-5530-96626.

Part: STRINGER — DENTED (BS 367) · airframe 39,969 hrs · 27,046 cycles

REWORK REQUIRED ON STRINGER 3R BS 401 HAS OPEN HOLE, BS 367 STRINGER IS DENTED. REPAIRED PER EA 7-5310-96627.

Part: SKIN — PUNCTURED (RUDDER) · airframe 39,969 hrs · 27,046 cycles

UPPER RUDDER L/E SKIN HAS PUNCTURE AT LT SIDE AT RUDDER STA 160. REPAIRED PUNCTURE ON UPPER RUDDER L/E SKIN AT LT SIDE AT RUDDER STA 160 IAW EA 7-5530-96539.

Part: SKIN — CORRODED (BS 480-681) · airframe 39,969 hrs · 27,046 cycles

CORROSION ON FUSELAGE SKIN FROM BS 480-681 S4L &R. REPAIRED PER EA 7-5330-99457.

Part: SKIN — CORRODED (BS 740-870) · airframe 39,969 hrs · 27,046 cycles

FOUND CORROSON ON FUSELAGE SKIN FROM BS 740 - 870 FROM STRINGER 4 LEFT TO STRINGER 4 RIGHT. REMOVED AND REPLACED SKIN BS 740-870 STR 4L-4R IAW SRM 51-30-2.

Part: SKIN — CORRODED (BS 680-740) · airframe 39,969 hrs · 27,046 cycles

FOUND CORROSION ON FUSELAGE SKIN BS 680 -740 FROM STRINGER 4 LEFT TO STRINGER 10 LEFT. REMOVED AND REPLACED SKIN PANEL BS 680-740 STR 4 LT, STR 10 LT IAW SRM 51-30-2.

Part: RIB — CORRODED (HORIZONTAL STAB) · airframe 39,969 hrs · 27,046 cycles

LT HORIZONTAL STABILIZER, ELEVATOR THRUST HINGE RIB, O/B LUG, I/B & O/B FACES HAVE FRETTING CORROSION. REPAIRED LT HORIZ STAB, ELEV THRUST HINGE RIB, O/B LUG, I/B AND O/B FACES PER FED EX EA 7-5510-96625.

Part: HINGE — WORN (ELEVATOR) · airframe 39,969 hrs · 27,046 cycles

LT HORIZONTAL STABILIZER, ELEVATOR THRUST HINGE FITTING BUSHINGS ARE WORN. LT HORIZONTAL STAB. ELEVATOR THRUST HINGE FITTING BUSHINGS REPLACED PER FED EX EA 7- 5510-96625.

Part: HINGE — WORN (ELEVATOR) · airframe 39,969 hrs · 27,046 cycles

FOUND LT HORIZONTAL STABILIZER, ELEVATOR THRUST HINGE RIB, I/B LUG, O/B FACE IS WORN. I/B FACE IS WORN. REPAIRED LT HOR. STAB. THRUST HINGE RIB, I/B LUG, I/B & O/B FACES PER FED EX EA 7-5510- 96625.

Part: WEB — CRACKED (BS 895) · airframe 39,969 hrs · 27,046 cycles

CRACK ON BEADED WEB BS 895 RBL 45 WL 203. REPLACED CRACKED BEADED PRESSURE WEB AT BS 895 RBL 45, WL 203 IAW FED EX EA 7- 5310-96584.

Part: SKIN — DAMAGED (BS 430-480) · airframe 39,969 hrs · 27,046 cycles

BS 430-480 SHIM BELOW S4L SKIN LAP HAS SEVERAL HOLES WITH LESS THAN 2D OR NO EDGE MARGIN. COMPLIED WITH FED EX EA 7-5330-98585.

Part: DUCT — CRACKED (NR 2 ENGINE) · airframe 39,969 hrs · 27,046 cycles

NR 2 ENGINE S-DUCT INNER SKIN HAS A SMALL CRACK AT THE 3 O'CLOCK POSITION WHERE THE S-DUCT MEETS THE INLET. REPAIRED NR 2 ENGINE "S" DUCT INNER SKIN AT 3 O'CLOCK POSITION IAW FED EX EA 7-7160- 96621.

Part: UNKNOWN — CRACKED (BS 638) · airframe 39,969 hrs · 27,046 cycles

BS 638 STR 27 HAS A CRACK. REMOVED, REPAIRED DAMAGED STR. 27L BS 630-650 PER SRM 51-30-2, 53-10-3, 53-10-2, AND FED EX MM 51-20-021-7, 51-20-151-7.

Part: DOUBLER — UNKNOWN (FUSELAGE) · airframe 39,969 hrs · 27,046 cycles

REPLACE FWD AND AFT UPPER MCD CUTOUT DOUBLERS. FABRICATED, ALODINED AND PRIMERED UPPER MCD CUTOUT DOUBLER PER FED EX SRM 53- 30-2, 51-30-5.

Part: FRAME — MISDRILLED (BS 609) · airframe 39,969 hrs · 27,046 cycles

BS 609 LBL 22 2EA FASTENER HOLES IN STUB FRAME HAVE LESS THAT 4D SPACING. FWD HOLE HAS LESS THAT 2D EDGE MARGIN. HOLE SIZES .312, SPACING .818, EDGE MARGIN .510. *S/D* COMPLIED WITH FED EX EA 7-5310-98576.

Part: SKIN — MISINSTALLED (FUSELAGE) · airframe 39,969 hrs · 27,046 cycles

N01379 BS 451 STR 4L SKIN LAP HAS HOLES WITH LESS THAN 2D EDGE MARGIN AND LESS THAN 4D FASTENER SPACING. ** SD ** COMING

Part: SILL — DAMAGED (BS 618-623) · airframe 39,969 hrs · 27,046 cycles

BS 618-623 MCD CUTOUT I/B SILL UPPER SURFACE HAS HOLES WITH LESS THAN 2D EDGE MARGIN. COMPLIED WITH E.A. 7-5310-98572

Part: SKIN — UNKNOWN (BS 620-720) · airframe 39,969 hrs · 27,046 cycles

FILLED PILOT HOLES IN HAYES DOUBLER EXTERNAL SKIN, BS 620-720, STR 26L-27L. REPAIRED PER EA 7-5330-99479.

Part: SILL — DAMAGED (BS 481) · airframe 39,969 hrs · 27,046 cycles

BS 481 MCD CUTOUT I/B SILL UPPER SURFACE FILLER HAS FASTENER HOLE WITH NO EDGE MARGIN. COMPLIED WITH FED EX EA 7-5310-98583.

Part: SILL — WORN (BS 637-643) · airframe 39,969 hrs · 27,046 cycles

CUTOUT I/B SILL UPPER SURFACE HAS HOLES WITH LESS THAN 2D EDGE MARGIN. COMPLIED WITH E.A. 7-5310-98582

Part: SKIN — CRACKED (NR 2 INLET) · airframe 39,969 hrs · 27,046 cycles

NR 2 ENGINE INLET INNER SKIN AT 12 O'CLOCK POSITION WHERE IT MEETS THE 'S' DUCT IS BENT AND CRACKED. REPAIRED NR 2 ENGINE INLET INNER SKIN AT 12 O'CLOCK POSITION IAW FED EX EA 7-7160- 96621.

Part: STRINGER CLIP — CORRODED (BS 720C) · airframe 39,969 hrs · 27,046 cycles

STA 720C STR 3L, CORROSION ON STRINGER CLIP. REPLACED STRINGER CLIP PER SRM 51-30-2.

Part: REPAIR — UNKNOWN (FUSELAGE) · airframe 39,969 hrs · 27,046 cycles

SKIN REPAIR DOUBLER, 15" X 10" LOCATED AT BS 367-378, STR 27L, REQUIRES EVALUATION TO DETERMINE IF THE REPAIR IS MAJOR OR MINOR AND IF REPAIR IS IN ACCORDANCE WITH FAA APPROVED DATA. REINSTALLED PER E.O. 7-3450-7-3393

Part: STRINGER CLIP — CORRODED (BS 720C) · airframe 39,969 hrs · 27,046 cycles

STA 720C STR 2L, CORROSION ON STRINGER CLIP. REPLACED STRINGER CLIP PER SRM 51-30-2.

Part: STRINGER CLIP — CORRODED (BS 720C) · airframe 39,969 hrs · 27,046 cycles

STA 720C STR 1, CORROSION ON STRINGER CLIP. REPLACED STRINGER CLIP PER SRM 51-30-2.

Part: STRINGER CLIP — CORRODED (BS 720C) · airframe 39,969 hrs · 27,046 cycles

STA 720C STR 4L CORROSION ON STRINGER CLIP. REPLACED STRINGER CLIP PER SRM 51-30-2.

Part: STRINGER CLIP — CORRODED (BS 720A) · airframe 39,969 hrs · 27,046 cycles

STA 720A STR 4L CORROSION ON STR CLIP. REPLACED STRINGER CLIP PER SRM 51-30-2.

Part: STRINGER CLIP — CORRODED (BS 720C) · airframe 39,969 hrs · 27,046 cycles

STA 720C STR 2R, CORROSION ON STRINGER CLIP. REPLACED STRINGER CLIP PER SRM 51-30-2.

Part: STRINGER CLIP — CORRODED (BS 720B) · airframe 39,969 hrs · 27,046 cycles

STA 720B STR 4L CORROSION ON STRINGER CLIP. REPLACED STRINGER CLIP PER SRM 51-30-2.

Part: STRINGER CLIP — CORRODED (BS 700A) · airframe 39,969 hrs · 27,046 cycles

C53-224-01, STA 700A STR 4L, CORROSION ON STR CLIP. *S/D* REMOVED AND REPLACED STRINGER CLIP IAW SRM 51-30-2.

Part: STRINGER CLIP — CORRODED (BS 720) · airframe 39,969 hrs · 27,046 cycles

C53-224-01, STA 720 STR 4L CORROSION ON STR CLIP. *S/D* REPLACED STR CLIP IAW SRM 51-30-2.

Part: STRINGER CLIP — CORRODED (BS 720D) · airframe 39,969 hrs · 27,046 cycles

C53-224-01, STA 720D STR 4L CORROSION ON STR CLIP. *S/D* REPLACED STR CLIP IAW SRM 51-30-2.

Part: STRINGER CLIP — CORRODED (BS 720D) · airframe 39,969 hrs · 27,046 cycles

STA 720D STR 2L CORROSION ON STR CLIP. *S/D* REPLACED STR CLIP IAW SRM 51-30-2.

Part: STRINGER CLIP — CORRODED (BS 700A) · airframe 39,969 hrs · 27,046 cycles

C53-224-01, STA 700A STR 3R, CORROSION ON STR CLIP. *S/D* REPLACED STR CLIP IAW SRM 51-30-2.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 39,969 hrs · 27,046 cycles

C53-224-01, STA 720D STR 4R CORROSION ON STR CLIP. REPLACED STRINGER CLIP PER SRM 51-30-2.

Part: STRINGER CLIP — CORRODED (BS 700A) · airframe 39,969 hrs · 27,046 cycles

C53-224-01, STA 700A STR 2L, CORROSION ON STR CLIP. *S/D* REPLACED STR CLIP IAW SRM 51-30-2.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 39,969 hrs · 27,046 cycles

C53-224-01, STA 720D STR 3R CORROSION ON STR CLIP. REPLACED STRINGER CLIP PER SRM 51-30-2.

Part: STRINGER CLIP — CORRODED (BS 700A) · airframe 39,969 hrs · 27,046 cycles

C53-224-01, STA 700A STR 4R, CORROSION ON STR CLIP. *S/D* REPLACED STR CLIP IAW SRM 51-30-2.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 39,969 hrs · 27,046 cycles

C53-224-01, STA 720F STR 4L CORROSION ON STR CLIP. REPLACED STRINGER CLIP PER SRM 51-30-2.

Part: STRINGER CLIP — CORRODED (BS 720D) · airframe 39,969 hrs · 27,046 cycles

C53-224-01, STA 720D STR 3L CORROSION ON STR CLIP. *S/D* REPLACED STR CLIP IAW SRM 51-30-2.

Part: STRINGER CLIP — CORRODED (BS 700A) · airframe 39,969 hrs · 27,046 cycles

C53-224-01, STA 700A STR 1, CORROSION ON STR CLIP. *S/D* REMOVED AND REPLACED STR CLIP IAW SRM 51-30-2.

Part: STRINGER CLIP — CORRODED (BS 700) · airframe 39,969 hrs · 27,046 cycles

C53-224-01, STA 700 STR 3L, CORROSION ON STR CLIP. *S/D* REPLACED STR SLIP IAW SRM 51-30-2.

Part: STRINGER CLIP — CORRODED (BS 720D) · airframe 39,969 hrs · 27,046 cycles

C53-224-01, STA 720D STR 1 CORROSION ON STR CLIP. *S/D* REPLACED STRINGER CLIP PER SRM 51-30-2.

Part: STRINGER CLIP — CORRODED (BS 700A) · airframe 39,969 hrs · 27,046 cycles

C53-224-01, STA 700A STR 2R, CORROSION ON STR CLIP. *S/D* REPLACED STR CLIP IAW SRM 51-30-2.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 39,969 hrs · 27,046 cycles

C53-224-01, STA 720E STR 4L CORROSION ON STR CLIP. REPLACED STRINGER CLIP PER SRM 51-30-2.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 39,969 hrs · 27,046 cycles

C53-224-01, STA 720D STR 2R CORROSION ON STR CLIP. REPLACED STRINGER CLIP PER SRM 51-30-2.

Part: STRINGER — DENTED (BS 493) · airframe 39,969 hrs · 27,046 cycles

STRINGER 8 RT BS 493 IS DENTED. *S/D* REPAIRED STRINGER 8 RT PER SRM 53-10-3 FIGURE 3.

Part: REPAIR — MISINSTALLED (BS 1223-1243) · airframe 39,969 hrs · 27,046 cycles

SKIN REPAIR DOUBLER AT I/B AFT CORNER OF PNEUMATIC GROUND START CONNECTION CUTOUT, BS 1223-1243 REQUIRES EVALUATION TO DETERMINE IF THE REPAIR IS MAJOR OR MINOR AND IF REPAIR IS IN ACCORDANCE WITH FAA APPROVED DATA. *S/D* REPLACED REPAIR DOUBLER IAW EA 7-5330-96549.

Part: SKIN — CORRODED (BS 681-740) · airframe 39,969 hrs · 27,046 cycles

CORROSION ON FUSELAGE SKIN FROM BS 681 - 740 STRINGER 4 LT TO STRINGER 4 RT. REPLACED SKIN PANEL PER SRM 51-30-2. (CLOSED)

Part: SILL — MISMANUFACTURED (BS 570) · airframe 39,969 hrs · 27,046 cycles

BS 570.5 LBL 10 MCD CUTOUT I/B SILL HAS FASTENER HOLE WITH NO EDGE MARGIN. HOLE LOCATED AT SILL SPLICE. COMPLIED WITH FED EX EA 7-5310-98588.

Part: TEAR STRAP — MISMANUFACTURED (BS 640) · airframe 39,969 hrs · 27,046 cycles

BS 640 STR 4R TEAR STRAP HAS HOLES WITH LESS THAT 4D FASTENER SPACING. COMPLIED WITH FED EX EA 7-5330-98632.

Part: SKIN — SCHEDULED MAINT (BS 480-680) · airframe 39,969 hrs · 27,046 cycles

BS 480-680 STR 4L-4R, REPLACEMENT SKIN REQUIRES REMOVAL OF TEAR STRAPS TO ACCOMMODATE STRUCTURE OF MCD CUTOUT FROM STR 3L TO LT EDGE. REPAIRED PER SRM 51-10-2 AND DWG 53FX1380.

Part: TEAR STRAP — MISMANUFACTURED (BS 460) · airframe 39,969 hrs · 27,046 cycles

BS 460 STR 4R TEAR STRAP HAS HOLES WITH LESS THAT 4D FASTENER SPACING. REPAIRED TEAR STRAP, BS 460, STR 4R PER FED-EX EA 7-5330-98631.

Part: SILL — MISMANUFACTURED (BS 640) · airframe 39,969 hrs · 27,046 cycles

BS 640 MCD CUTOUT O/B SILL LOWER SURFACE HAS PILOT HOLE WITH LESS THAN 4D FASTENER SPACING FROM INNER WEB FASTENER LOCATION. COMPLIED WITH FED EX EA 7-5310-98630.

Part: TEAR STRAP — MISMANUFACTURED (BS 460) · airframe 39,969 hrs · 27,046 cycles

BS 460 STR 4L TEAR STRAP HAS HOLES WITH LESS THAT 4D FASTENER SPACING. REPAIRED PER FED EX EA 7-5330-98634.

Part: SKIN — MISMANUFACTURED (BS 479) · airframe 39,969 hrs · 27,046 cycles

BS 479 STR 4L-5L SKIN HAS HOLES WITH LESS THAN 4D FASTENER SPACING. REMOVED DAMAGED SECTION OF SKIN BS 680 STR 4L TO 10L AND REPAIRED PER FED EX EA 7- 5330-98633.

Part: SKIN — UNKNOWN (BS 950-1009) · airframe 39,969 hrs · 27,046 cycles

AFT CARGO BAY SKIN REQUIRES REPLACEMENT FROM BS 950 TO BS 1009, STR 26 LT TO STR 26 RT. *S/D* REMOVED AND INSTALLED AFT CARGO BAY SKIN FROM BS 950 - BS 1009, STR 26L-26R IAW EA 7-5310-96541.

Part: STRINGER — CORRODED (BS 720C-720D) · airframe 39,969 hrs · 27,046 cycles

CORROSION ON STR 3 RT, BS 720C-720D. REPAIRED STR 3 RIGHT, BS 720C-720D PER SRM 53-10-3 FIG 3.

Part: STRINGER — CORRODED (BS 720C) · airframe 39,969 hrs · 27,046 cycles

CORROSION ON STR 4 RT AT BS 720C PLUS 10. REPAIRED STRINGER 4 RIGHT AT BS 720C PLUS 10 PER SRM 53-10-3 FIG 3.

Part: SHEAR TIE — CORRODED (BS 950E) · airframe 39,969 hrs · 27,046 cycles

CORROSION ON SHEAR TIE AT BS 950E STR 26 LT. *S/D* REMOVED, FABRICATED AND INSTALLED A NEW SHEAR TIE IAW SRM 51-30-2, 53-10-1 AND 53-10-4.

Part: SKIN — DAMAGED · airframe 39,969 hrs · 27,046 cycles

N01351, BS 660 LBL 25 TEAR STRAP HAS OPEN HOLES. LAP HAS 2 OPEN HOLES AT LBL . COMPLIED WITH FED EX EA 7-5330-98570

Part: LAP JOINT — MISDRILLED (FUSELAGE) · airframe 39,969 hrs · 27,046 cycles

N01349, BS 620 LBL 26 STR 4L LAP HAS HOLES WITH LESS THAN 4D FASTENER SPACING.

Part: FRAME — MISDRILLED (FUSELAGE) · airframe 39,969 hrs · 27,046 cycles

N01348, BS 620 LBL 26 BOTH FRAME HALVES HAVE DRILL STARTS COMMON TO OEM SKIN. COMPLIED WITH FED EX EA 7-5310-98573.

Part: FRAME — DAMAGED (BS 491) · airframe 39,969 hrs · 27,046 cycles

BS 491 LBL 22 2 EA FASTENER HOLES IN STUB FRAME HAVE LESS THAN 4D SPACING. AFT HOLE HAS LESS THAN 2D EDGE MARGIN (HOLE SIZES .312, SPACING .736, EDGE MARGIN .350).

Part: SILL — DAMAGED (BS 595) · airframe 39,969 hrs · 27,046 cycles

BS 595.4 LBL 24 MCD CUTOUT O/B SILL HAS AN OPEN HOLE WITH NO FASTENER SPACING TO HINGE BOLT HOLE. COMPLIED WITH FED EX EA 7-5310-98577.

Part: FRAME — TOOL DAMAGE (BS 460) · airframe 39,969 hrs · 27,046 cycles

BS 460 STR 3L FWD FRAME SEGMENT HAS DRILL START. REPAIRED PER FED EX EA 7-5330-98634.

Part: TEAR STRAP — MISDRILLED · airframe 39,969 hrs · 27,046 cycles

FASTENER HOLES IN TEAR STRAP HAVE SHORT SPACING AND EDGE MARGIN B.S. 640, LBL 25. REPAIRED TEAR STRAP AT BS 640 LBL 25 PER FED-EX EA 7-5330-98635.

Part: FRAME — DAMAGED (BS 496) · airframe 39,969 hrs · 27,046 cycles

BS 496 LBL 22 2 EA FASTENER HOLES IN STUB FRAME HAVE LESS THAN 4D SPACING. FWD HOLE HAS LESS THAN 2D EDGE MARGIN. (HOLE SIZES .312, SPACING .750, EDGE MARGIN .415).

Part: ANGLE — MISDRILLED · airframe 39,969 hrs · 27,046 cycles

N01357 BS 480 STR 2R ATTACH ANGLE HAS 2 EA DRILL STARTS. FABRICATED NEW STRINGER ATTACH ANGLE PER SRM 51-10-2, 51-10-3, 51-30-2, 51-30-5.

Part: FRAME — DAMAGED (BS 488) · airframe 39,969 hrs · 27,046 cycles

FASTENER HOLES IN STUB FRAME HAVE SHORT SPACING AND EDGE MARGINS ON FWD HOLE IS LESS THAN 2D BS 488 LBL 22.

Part: SKIN — DAMAGED (BS 480) · airframe 39,969 hrs · 27,046 cycles

BS 480 STR 4L-4R SKIN HAS NUMEROUS OPEN AND FIGURE 8 HOLES AT ORIGINAL CIRCUMFERENTIAL SPLICE. SKIN IS OIL CANNED AT BS 440-480 STR 2L-2R. REPAIRED PER EA 7-5330-99478A.

Part: SILL — MISDRILLED · airframe 39,969 hrs · 27,046 cycles

BS 568 LBL22-24 MCD CUTOUT OB SILL UPPER SURFACE HAS 2 FASTENER HOLES WITH NO EDGE MARGIN. COMPLIED WITH FED EX EA 7-5310-98587.

Part: FRAME — DAMAGED (BS 601) · airframe 39,969 hrs · 27,046 cycles

FASTENER HOLES IN STUB FRAME HAVE SHORT SPACING AND EDGE MARGIN BS 601 LBL 22.

Part: FRAME — DAMAGED (BS 609) · airframe 39,969 hrs · 27,046 cycles

FASTENER HOLES IN STUB FRAME HAVE SHORT SPACING AND EDGE MARGIN BS 609 LBL 22. *S/D* WORK ACCOMPLISHED.

Part: SILL — MISDRILLED · airframe 39,969 hrs · 27,046 cycles

N01355, BS 617 LBL 22-24 MCD CUTOUT OB SILL UPPER SURFACE AFT OB HOLE HAS LESS THAN 2D EDGE MARGIN. (FASTENER HOLE SIZE .375 EDGE MARGIN .485) COMPLIED WITH FED EX EA 7-5310-98586.

Part: SILL — MISDRILLED (FUSELAGE) · airframe 39,969 hrs · 27,046 cycles

BS 480-620 MCD CUTOUT OB SILL UPPER SURFACE HAS SEVERAL OPEN HOLES. COMPLIED WITH FED EX EA 7-5310-98574.

Part: FRAME — MISMANUFACTURED · airframe 39,969 hrs · 27,046 cycles

N01345 FASTENER HOLES IN STUB FRAME HAVE SHORT SPACING AND EDGE MARGIN BS 611.5, LBL 22.

Part: FRAME — DAMAGED (BS 499) · airframe 39,969 hrs · 27,046 cycles

FASTENER HOLES IN STUB FRAME HAVE SHORT SPACING AND EDGE MARGIN BS 499 LBL 22.

Part: FRAME — MISDRILLED · airframe 39,969 hrs · 27,046 cycles

N01352, BS 640 LBL 25 FRAME HAS A DRILL START COMMON TO OEM SKIN. COMPLIED WITH FED EX EA 7-5310-98575.

Part: FRAME — MISDRILLED · airframe 39,969 hrs · 27,046 cycles

N01356, BS 620 LBL 23 FWD FRAME SEGMENT HINGE HOLE HAS LESS THAN 2D EDGE MARGIN. (HINGE HOLE SIZE .375 EDGE MARGIN .500).

Part: SKIN — DAMAGED (BS 492-500) · airframe 39,969 hrs · 27,046 cycles

BS 492- BS 500, RBL 15, WL 150, STR 27R GRAVEL DAMAGE COMMON TO BELLY SKIN BS 492 TO BS 500, STR 27R. *S/D* REPAIRED DAMAGE ON SKIN BS 492 - BS 500 RBL 15 WL 150 STR 27R IAW SRM 53-30-3.

Part: FRAME — CORRODED (BS 740) · airframe 39,969 hrs · 27,046 cycles

CORROSION ON AFT HORIZONTAL FLANGE OF BS 740 FRAME BETWEEN STR 1 AND 2 LT. REPAIRED HORIZONTAL FLANGE OF BS 740 FRAME BETWEEN STR 1L AND 2L IAW EA 7-5310- 96551.

Part: FRAME — DAMAGED (BS 604) · airframe 39,969 hrs · 27,046 cycles

FASTENER HOLES IN STUB FRAME HAVE SHORT SPACING AND EDGE MARGIN BS 604, LBL 22.

Part: FLOORBEAM — GOUGED (BS 880) · airframe 39,969 hrs · 27,046 cycles

FOUND GOUGED AFT SIDE OF BS 880 FLOORBEAM AT RBL 47 WL 204. REPAIRED PER FED EX E.A. 7-5310-96540.

Part: MOUNT — CORRODED (NR 1 ENGINE) · airframe 39,969 hrs · 27,046 cycles

NR 1 ENGINE FWD PYLON FITTING HAS CORROSION ON VERTICAL FLANGE. REPAIRED NR 1 ENGINE PYLON FITTING IAW FED EX EA 7-5410-96738.

Part: MOUNT — CORRODED (NR 3 ENGINE) · airframe 39,969 hrs · 27,046 cycles

NR 3 ENGINE FWD PYLON FITTING HAS CORROSION ON VERTICAL FLANGE. REPAIRED NR 3 ENGINE PYLON FITTING IAW FED EX EA 7-5410-96738.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 39,969 hrs · 27,046 cycles

N00235 GRAVEL DAMAGE BS 620-720 STR 25L -20R. REMOVED GRAVEL DAMAGE BS 620-720 STR 25L-20R COMMON TO SKIN WITHIN LIMITS PER SRM 53-30-1 DETAIL 1 AND FIG 2.

Part: SHEAR TIE — CORRODED (BS 970) · airframe 39,969 hrs · 27,046 cycles

BS 970 STR 29L-30 TIE HAS CORROSION. REMOVED SHEAR TIE AT BS 970 STR 29L-30 AND REPLACED WITH NEW SHEAR TIE PER SRM 53-10-4.

Part: SHEAR TIE — CRACKED (BS 950F) · airframe 39,969 hrs · 27,046 cycles

N01277 BS 950F LBL 12 WL 140 SHEAR TIE CRACKED. REMOVED AND REPLACED SHEAR TIE IAW SRM 53-10-4, AND SRM 51-30-09.

Part: SHEAR TIE — CORRODED (BS 950A) · airframe 39,969 hrs · 27,046 cycles

N01273 BS 950A S28-29R RBL10-15 SHEAR TIE HAS CORROSION. REMOVED AND REPLACED IAW SRM 51-30-2.

Part: SHEAR TIE — CORRODED (BS 970) · airframe 39,969 hrs · 27,046 cycles

SHEAR TIE REPAIR STRAP BS 970 STR 29 L WL 148 HAS CORROSION. *S/D* REMOVED SHEAR TIE AT BS 970 STR 29L WL 148 AND INSTALLED NEW SHEAR TIE PER SRM 53-10-4.

Part: SKIN — BULGED (BS 255) · airframe 39,969 hrs · 27,046 cycles

BS 255, STR 24-25 L, 2" CREASED BULGE IN THE SKIN. REPAIRED FUSELAGE SKIN AT BS 255 STR 24-25 L/TAS PER FED EX EA 7-5330-91428.

Part: FRAME — DAMAGED (BS 560) · airframe 39,969 hrs · 27,046 cycles

FRAME IS CREASED AT BS 560, LBL 10, WL 148.5. REPAIRED FRAME PER SRM 54-40-3 FIG 1.

Part: FRAME — DAMAGED (BS660, STR6) · airframe 39,969 hrs · 27,046 cycles

RT FUSELAGE INTERNAL FRAME REPAIR DOUBLER 12 INCHES BY 2.5 INCHES, LOCATED AT BS 660, STRINGER 6 REQUIRES EVALUATION TO DETERMINE IF THE REPAIR IS MAJOR OR MINOR AND IF REPAIR IS IAW APPROVED DATA. REPAIRED FRAME DOUBLER BS 660 STR 6 SRM 53-10-4.

Part: REPAIR — NONE (FSUELAGE) · airframe 39,969 hrs · 27,046 cycles

RT FUSELAGE SKIN REPAIR DOUBLER, 14" BY 7" LOCATED AT BS 1223-1243 REQUIRES EVALUATION TO DETERMINE IF THE REPAIR IS MAJOR OR MINOR AND IF REPAIR IS IN ACCORDANCE WITH FAA APPROVED DATA. REPAIRED SKIN DOUBLER PER SRM 53-30-3 FIG 1.

Part: SHEAR TIE — CORRODED (BS 1010) · corrosion level 2 · airframe 39,969 hrs · 27,046 cycles

FOUND CORROSION ON SHEAR TIE AT BS 1010 RBL 3 WL 148. REPAIRED SHEAR TIE AT BS 1010 RBL 3 WL 148 IAW SRM 53-10-4 FIG 15.

Part: LAP JOINT — DAMAGED (BS 660) · airframe 39,969 hrs · 27,046 cycles

FOUND DOUBLER HOLE AT MCD LAP SEAM LOWER ROW BS 660 S27L. REPAIRED PER FED EX EA 7-5330-95993A.

Part: SEAL DEPRESSOR — CHAFED (CARGO DOOR) · airframe 39,969 hrs · 27,046 cycles

LOWER FWD CARGO DOOR, LOWER DOOR FRAME IS CHAFED. REMOVED AND REPLACED LWR FWD CARGO DOOR FRAME PER SRM 51-30-2.

Part: RIB — GOUGED (ELEVATOR) · airframe 39,969 hrs · 27,046 cycles

WHILE WORKING CARD NR N00763 FOUND RT NR 5 ELEVATOR HINGE, SUPPORT RIB L/E GOUGED. REPAIRED RIB PER FED EX EA 7-5510-91427.

Part: STRINGER — CORRODED (BS 950-1009) · airframe 39,969 hrs · 27,046 cycles

STR 28L BS 950-1009 HAS SEVERAL AREAS OF CORROSION. REMOVED DAMAGED STRINGER 28L FROM BS 950-1009 AND REPLACED PER SRM 53-10-3 FIG 1 AND SRM 51-30-02

Part: SKIN — BULGED (BS206,STR24-24L) · airframe 39,969 hrs · 27,046 cycles

N00204 BS 206, STR 24-24L, 2 INCH CREASED BULGE IN THE SKIN. REPAIRED FUSELAGE SKIN AT BS 206, STR 24L-25L AS PER FED EX EA 7-5310-91431

Part: FRAME — CORRODED (FUSELAGE) · airframe 39,969 hrs · 27,046 cycles

N01022, CORROSION (C53-113-01(2)) ON LOWER CHORD AROUND NUTPLATE HOLE BS 1130 RBL 24 WL 201. REMOVED CORROSION ON LOWER CHORD BS 1130 RBL 24, WL 201, FOUND TO BE OUT OF LIMITS, REPAIRED LOWER CHORD IAW SRM 53-10-8 FIG 10.

Part: FLAP TRACK — CORRODED (NR3 FLAP) · airframe 39,969 hrs · 27,046 cycles

N01126 LT WING IB FLAP OB FLAP TRACK CORRODED ON AFT ATTACH POINT. ** SD ** COMING REPLACED FLAP TRACK IAW W/C 27X5705-03

Part: INTERCOSTAL — CRACKED (BS 950B) · airframe 39,969 hrs · 27,046 cycles

INTERCOSTAL CRACKED BS 950B-2, STR 29R WL 155. REPAIRED IAW SRM 51-40-2.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 39,969 hrs · 27,046 cycles

UPON REMOVAL OF REPAIR ON AFT AIRSTAIR (FEDEX CARD 30956, N01070) FOUND CHORD TO BE DAMAGED. REPAIRED CHORD PER SRM 51-30-2.

Part: REPAIR — UNKNOWN (AIRSTAIR DOOR) · airframe 39,969 hrs · 27,046 cycles

TEMPORARY REPAIR INSTALLED ON AIR STAIR DOOR EXTERNAL ON AIR STAIR DOOR EXTERNAL SKIN LT FWD CORNER. REPAIRED DOOR PER SRM 51-30-2.

Part: SKIN — DENTED (CARGO DOOR) · airframe 39,969 hrs · 27,046 cycles

GOODRICH RESPONSIBILITY. FOUND WHILE WORKING N00409, DENTED FWD CARGO DOOR SKIN 4.5" AFT FROM FWD EDGE AND 3" UP FROM LOWER EDGE. REPAIRED PER SRM 52-00-3.

Part: FRAME — DENTED (BS 950C) · airframe 39,969 hrs · 27,046 cycles

AFT CARGO COMPARTMENT, DENT IN FRAME BS 950C RBL 36 WL 152. REMOVED DENT DAMAGE AREA, FABRICATED REPAIR PART AND INSTALLED IAW SRM 51-40-3.

Part: SKIN — CHAFED (CARGO DOOR) · airframe 39,969 hrs · 27,046 cycles

LOWER AFT CARGO DOOR OUTER SKIN IS CHAFED ALONG FAIRING RUB STRIP. REPAIRED LOWER AFT CARGO DOOR OUTER SKIN PER 52-00-3 FIG 4.

Part: STRINGER CLIP — DAMAGED (BS 950C) · airframe 39,969 hrs · 27,046 cycles

MECHANICAL DAMAGE TO STRINGER CLIP BS 950C STRINGER 5 RT. REPAIRED STRINGER CLIP PER SRM 53-10-1, 51-30-2.

Part: SKIN — DENTED (BS 1170) · airframe 39,969 hrs · 27,046 cycles

N00222 BS 1170 STR. 23-24L DENT IN SKIN ** SD ** COMING DENT ON SKIN WAS FOUND TO BE OUT OF LIMITS, REPAIRED DENT ON SKIN AT BS 1170, STR 23L-24L, IAW SRM 53-30-3.

Part: WEB — GOUGED (BS 341) · airframe 39,969 hrs · 27,046 cycles

FOUND L-1 DOOR CUTOUT UPPER WEB IS GOUGED STA 341, WL 282, LBL 50. REPAIRED L1 DOOR CUTOUT UPPER WEB PER SRM 53-10-1.

Part: SKIN — DENTED (BS 423) · airframe 39,969 hrs · 27,046 cycles

FOUND BS 423, STR 22-23L, CREASED DENT IN SKIN. REPAIRED SKIN AT BS 423, STR 22-23L PER SRM 53-30-3.

Part: CREASE BEAM — MISDRILLED (BS 848-870) · airframe 39,969 hrs · 27,046 cycles

CREASE BEAM IB CHORD HAS DOUBLE HOLES BS 848-870 RBL 63 WL 208. REPAIRED CREASE BEAM I/B CHORD AT BS 848-870 RBL 63, WL 208 PER SRM 51-30-2.

Part: FRAME — DENTED (BS 500) · airframe 39,969 hrs · 27,046 cycles

FRAME DENT AT BS 500, ABOVE STR 23L. TRIMED DAMAGE, FABRICATED AND INSTALLED DOUBLER PER SRM 51-40-3.

Part: FRAME — DENTED (BS 560) · airframe 39,969 hrs · 27,046 cycles

FOUND FRAME DENT AT BS 560 ABOVE STR 24L. REPAIRED FRAME AT BS 560 STR 24L IAW SRM 51-40-3.

Part: SHEAR TIE — CORRODED (BS 1090) · airframe 39,969 hrs · 27,046 cycles

EXERNAL FUSELAGE SKIN PILLOWING AROUND SHEAR TIE FASTENERS AT BS 1090, STR 28 - 29 LEFT. REMOVED SHIM BETWEEN SHEAR TIE & FUSELAGE SKIN AT BS 1090 STR 28-29L FABRICATED NEW SHIM & INSTALLED PER SRM 51-10-2, 51-30-2.

Part: FLOORBEAM — DAMAGED (BS 740) · airframe 39,969 hrs · 27,046 cycles

FOUND DOUBLE HOLE IN FLOORBEAM BS 740 LBL 47 WL 208. REPAIRED PER FED EX EA 7-5810-91429.

Part: SKIN — CORRODED (BS 1051) · airframe 39,969 hrs · 27,046 cycles

EXTERNAL FUSELAGE SKIN PILLOWING AROUND FASTENER HEADS AT BS 1051, STR 29 LEFT. SUSPECT CORRODED STRINGER. REMOVED CORROSION FOUND OUT OF LIMITS. REMOVED AREA OF DAMAGE, FABRICATED REPAIR DOUBLER AND FILLER AND ISNTALLED, IAW SRM 53-30-3.

Part: FRAME — DENTED (BS 990) · airframe 39,969 hrs · 27,046 cycles

AFT CARGO COMPARTMENT, FRAME IS DENTED BS 990 LBL 29 WL 150. REPAIRED FRAME, BS 990, LBL 29, WL 150 PER SRM 51-40-3.

Part: FRAME — DENTED (BS 950B) · airframe 39,969 hrs · 27,046 cycles

AFT CARGO COMPARTMENT, FRAME IS DENTED BS 950B LBL 27 WL 148. REPAIRED FRAME PER SRM 51-40-3.

Part: STRINGER — CORRODED (BS 1050) · airframe 39,969 hrs · 27,046 cycles

CORROSION (C53-111-01) AFT CARGO COMPARTMENT ON STR 29 STA 1050. REPAIRED STR 30 BS 1050 PER SRM 53-10-3.

Part: KEELBEAM — CORRODED (BS 950C-950F) · airframe 39,969 hrs · 27,046 cycles

STR 29L KEEL BEAM BS 950C TO 950D WL 148 HAS CORROSION (C53-113-01).

Part: FRAME — DENTED (BS 1010) · airframe 39,969 hrs · 27,046 cycles

AFT CARGO COMPARTMENT, FRAME IS DENTED BS 1010 LBL 27 TO LBL 30 WL 150 TO WL 153. DENT IN FRAME FOUND TO BE OUT OF LIMITS, CUT OUT DAMAGE FABRICATED DOUBLER, ALODIEND & PRIMED, INSTALLED FASTENERS IN REPAIR SRM 51-30-2.

Part: SKIN — BENT (PAX DOOR) · airframe 39,969 hrs · 27,046 cycles

FOUND FORWARD ENTRY DOOR, UPPER AFT CORNER SKIN IS BENT OUTWARDS. REPAIRED FORWARD ENTRY DOOR UPPER AFT CORNER SKIN PER SRM 52-00-3.

Part: STRINGER — CORRODED (BS 310-317) · airframe 39,969 hrs · 27,046 cycles

FOUND CORROSION ON STRINGER 21R BS 310-317. FOUND CORROSION ON STR 21R BS 310-317 TO BE OUT OF LIMITS. REMOVED CORRODED PORTION OF STR. REPAIRED STRINGER IAW SRM 53-10-3 FIG 1.

Part: RADAR — MALFUNCTIONED (WX SYSTEM) · airframe 39,698 hrs · 26,835 cycles

ON CLIMB-OUT, TURNING RADAR ON AND GOT A FAIL LT ALONG WITH SPOKING IN ALL RANGES. TURNED OFF, PULLED AND RESET CB'S, SAMETHING WHEN RADAR TURNED ON. REMOVED AND REPLACED WEATHER RADAR R/T. SYS OPS CKD NORMAL. REF B727-200 MM 34-41-41.

Part: BEAM — CORRODED (FUSELAGE) · airframe 39,566 hrs · 26,731 cycles

CORROSION ON LONGITUDIONAL BEAM BS 740 - 840 RBL 45. REPLACED LONGITUDINAL BEAM PER SRM 51-30-2.

Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,678 hrs · 25,256 cycles

LT WHEEL WELL HAS CORROSION AT STRINGER 18A CHANNEL BS 939 & 912 UPR SURFACE. REMOVED AND REPLACED SILL CHANNEL BS 870-940, LBL 65, WL 190 AT STR 18A PER SRM 51- 30-5, 51-30-2.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,678 hrs · 25,256 cycles

WHILE WORKING FED EX NRC N00312, FOUND CORROSION ON WEB AT LBL 10, BS 1146-1166, WL 146. REMOVED CORRODED WEB AND REPAIRED PER SRM 51-30-5, 51-30-2.

Part: KEELBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,678 hrs · 25,256 cycles

CORROSION (C53-113-01) ON STR 29L KEEL BEAM O/B FLANGE FROM STA 950D TO 950E. REMOVED CORROSION ON STR 19L KEEL BEAM O/B FLANGE FROM BS 950D TO 950E FOUND TO BE OUT OF LIMITS IAW SRM 51-10-3. INSTALLED REPAIR STRAP ON STR 29L KEEL BEAM IAW FED EX DRAWING SR 27-53-023A.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,678 hrs · 25,256 cycles

WHILE WORKING FED EX NRC N00312 FOUND CORROSION ON WEB AT RBL 6, BS 1146-1166, WL 146. CORROSION FOUND TO BE OUT OF LIMITS. REPAIRED WEB PER SRM 51-30-2.

Part: SKIN — DENTED (FUSELAGE) · airframe 37,678 hrs · 25,256 cycles

DENT IN EXTERNAL FUSE SKIN AT BS 1105 BETWEEN STR 28 LEFT AND 29. FOUND DENT ON EXTERNAL FUSE SKIN AT BS 1105 BETWEEN STR 28 LEFT AND 29 TO BE OUT OF LIMITS. CUT OUT DAMAGED SKIN. FABRICATED REPAIR DOUBLER FOR SKIN. CUT OUT AT BS 1105 BETWEEN STR. 28 LEFT AND 29. ALODINED, PRIMED & INSTALLED IAW SRM 53-30-3.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,678 hrs · 25,256 cycles

WHILE WORKING FUSELAGE 5081, N00285, FOUND SHEAR TIE TO BE CORRODED OUT OF LIMITS BS 620, WL 138, LBL 3.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,678 hrs · 25,256 cycles

CORROSION (C53-113-01, 2) ON FRAME + SHEAR TIE FWD AND AFT SIDES BS 1166 WL 146 LBL 12. CORROSION ON FRAME AND SHEAR TIE FOUND TO BE OUT OF LIMITS PER SRM 51-30-2. CUT OUT SECTION SHEAR TIE. FABRICATED REPAIR PARTS FROM BAC 1490-2738 7075 T6 LOT 487559 7075 T6 .100 LOT 381963 PER SRM 53-10-4 FIG B. ALODINE AND PRIMED PER SRM 51-10-2. INSTALLED FASTENERS COMMON TO REPAIR AREA.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,678 hrs · 25,256 cycles

CORROSION BS 1166 RBL 15 WL 146 ON FRAME, FWD & AFT SIDES. REPAIRED FRAME AT BS 1166, RBL 3 - RBL 15, WL 146 PER SRM 53-10-1.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,678 hrs · 25,256 cycles

CORROSION ON SHEAR TIE STA 950E BETWEEN STR 29R AND 30R. CORROSION FOUND TO BE OUT OF LIMITS. REPAIRED SHEAR TIE PER SRM 53-10-4, 53-10-1, 51- 10-6.

Part: OXYGEN BOTTLE — DEFECTIVE (FWD & AFT)

AFT APPROX 90 MIN OF FLIGHT OXYGEN PRESSURE WENT TO 100 PSI. ALL MASK IND WENT TO ORANGE. *S/D* REMOVED AND REPLACED BOTH FWD AND AFT NR 2 BOTTLES PER 727-200 MM 12-15-011-2 PAR 2. LEAK CK GOOD PER MM 35-00-000-2.

Part: GENERATOR — INOP (AC SYSTEM)

DURING CLIMB LOST NR 1 GEN AND BUS ACCOMPLISHED ELECTRICAL SYS MALFUNCTION CKLIST AND GENERATOR FIELD/GENERATOR BREAKER TRIP CK LIST AND CSD DISC. REMOVED AND REPLACED NR 1 GENERATOR CONTROL UNIT AND VOLTAGE REGULATOR. REMOVED AND REPLACED NR 2 VOLTAGE REGULATOR, ALL CK GOOD.

Part: SKIN — CORRODED (BS 950)

CORROSION ON SKIN AND STRINGER 28L, BS 950E+12 TO 950F+6. CUT OUT CORRODED STR SECTION. INSTALLED STRINGER REPAIR PER SRM 53-10-3. CUT OUT CORRODED SKIN, INSTALLED EXTERNAL REPAIR PER SRM 53-30-3.

Part: SKIN — CORRODED (BS 1120-1126)

FUSELAGE BS 1120 TO 1126 SKIN CORROSION UNDER STR 29 LEFT. CUT OUT DAMAGED SKIN AND INSTALLED EXTERNAL DOUBLER PER SRM 53-30-3 FIG 3.

Part: ANNUNCIATOR — INOPERATIVE (CARGO DOOR)

PASSING 1000 FT ON T/O, THE MAIN CARGO DOOR WARNING LIGHT CAME ON. AIRCRAFT RELEASED FOR SERVICE PER MEL/CDL: 52-4A CATEGORY: A EXPIRATION: 29-JAN-98. MAIN CARGO DOOR ANNUNCIATOR LIGHT INOP. MAIN CARGO DOOR IS CLOSED AND LOCKED PRIOR TO EACH BLOCK OUT OK TO CONTINUE CAT A EXP 29 JAN 98 CONTROL NR 29169 CARGO DOOR VERIFIED CLOSED AND LOCKED.

Part: HYD TUBE — FAILED (A HYD SYST)

HYD SYS 'A' LOSS ON DESCENT INTO TYS. ** (S/D) ** REMOVED AND REPLACED NR 1 ENG TO 'A' SYS MODULE PRESSURE TUBE ASSY. SERVICED HYD - AND RAN NR 1 ENG. OPS AND LEAK CHECKS GOOD.

Part: ACTUATOR — FAILED (TAIL SKID)

AFTER T/O, THE LANDING GEAR HAD TO BE RECYCLED TO EXTINGUISH THE TAIL SKID LIGHT. DURING THE SECOND ATTEMPT IT TOOK 10 SECONDS FOR THE LIGHT TO GO OUT. REPLACED TAIL SKID ACTUATOR PER MM 32-71-12 AND ADJ PER MM 32-71-01, GROUND CHECKS OK.

Part: FLOORBEAM — CORRODED (BS 380)

FLOORBEAM AT STA 380 RBL 47 WL 208.1 HAS CORROSION, CORROSION REMOVED FOUND OUT OF LIMITS. CUT OUT CORRODED SECTION OF FLOORBEAM AND INSTALLED FLOORBEAM PER SRM 53-10-8.

Part: SUPPORT — CORRODED (BS 1035)

MAIN CARGO, FLOOR BOARD SUPPORT CORRODED AT STA 1035 AT 12 RBL. INSTALLED NEW PART PER SRM 51-10-1.

Part: FLOORBEAM — CORRODED (BS 380)

FLOORBEAM AT STA 380 RBL 47 WL 208.1 HAS CORROSION. CORROSION REMOVED FOUND OUT OF LIMITS. CUT OUT CORRODED SECTION OF FLOORBEAM AND INSTALLED FLOORBEAM PER SRM 53-10-8.

Part: RIB — CRACKED (BS 760)

STA 760 RT RIB CHORD, HFEC INDICATES CRACKS TOP AND BOTTOM FWD HOLE. INSTALLED REPAIR PER BOEING DRAWING 65-68492-18.

Part: FLOORBEAM — CORRODED (BS 344)

CABIN FLOORBEAM UPPER CHORD LWR SURFACE CORRODED AROUND SCREW HOLE STA 344 LBL 25.5 RBL 20. SPLICED IN NEW SECTION PER FEDEX DRAWING SR 27-53-007. REMOVED CORROSION OUTSIDE OF SPLICE SECTION PER SRM 51-10-6.

Part: FLOORBEAM — CORRODED (BS 344)

CORROSION ON FLOORBEAM STA 344 BL O LBL 22.5. CORROSION BEYOND LIMITS, REMOVED T-CHORD FROM LBL 2 TO 32 SPLICED IN NEW SECTION PER FEDEX DRAWING SR 27-53-007.

Part: ANGLE — CRACKED (BS 750-760)

LT FLOOR BOARD CHORD ANGLE AT 750 TO 760 LBL 62 IS CRACKED. REMOVED CRACKED CHORD ANGLE, REPLACED LT 760 CHORD ANGLE PER SRM 51-10-1.

Part: FLOORBEAM — CRACKED (BS 344)

CABIN FLOORBEAM UPPER AFT CHORD CRACKED AT SCREW HOLE STA 344 LBL 25. REMOVED CRACKED SECTION OF CHORD. SPLICED IN NEW SECTION OF CHORD PER FEDEX DRAWING NR SRM 27-53-007.

Part: FRAME — CRACKED (BS 640)

FORWARD LOWER CARGO FUSE FRAME STA 640 CRACKED AT RBL 8 FLOOR STR ATTACH. STOP DRILLED ENDS OF CRACK, CONFIRMED CRACK ENDS AT STOP DRILL WITH DYE PENETRANT. INSTALLED REPAIR DOUBLER PER SRM 51-40-3.

Part: FLOOR BEAM — CORRODED (BS 1070)

AFT LOWER CARGO FLOOR BEAM LOWER FWD FLANGE CORRODED BEYOND SRM LIMITS STA 1070, RBL 12. REMOVED CORROSION AND INSTALLED DOUBLER PER SRM 51-10-6.

Part: STRAP — CORRODED (BS 1070)

AFT LOWER CARGO FLOOR BEAM STABILIZER STRAP CORRODED BEYOND SKIN LIMITS STA 1070, RBL 24. DOUBLER INSTALLED PER SRM 51-40-3.

Part: SKIN — CORRODED (BS 965)

STA 965 STR 30L FASTENER HEAD PULLED AND SKIN BULGING SUSPECT CORROSION. CUT OUT CORROSION STA 965 STR 30L AND INSTALLED FILLER AND DOUBLER PER SRM 53-30-3 PG 11.

Part: FLOOR BEAM — CORRODED (BS 380)

FLOOR BEAM AT STA 380, RBL 47, WL 208.1, HAS CORROSION. CORROSION REMOVED AND FOUND TO BE OUT OF LIMITS .086 INCH. SHOULD BE .100 INCH.

Part: FRAME — CRACKED (BS 680)

STA 680 ABOVE STR 6R FRAME CRACKED AT RIVET. ROUTED OUT CRACK, INSTALLED REPAIR DOUBLER PER SRM 51-40-3.

Part: FRAME — CRACKED (BS 680)

STA 680 ABOVE STR 6R FRAME CRACKED AT RIVET.

Part: CLIP — CRACKED (BS 440)

CRACK FOUND IN STR CLIP BS 440 STR 2R. REMOVED FASTENERS FROM CRACKED STR CLIP AT BS 440 STR 2R. THEN INSTALLED NEW STR CLIP IAW FEDEX SRM 51-30-2.