N234FE

Part: RETAINER — BROKEN (GIRT BAR) · airframe 75,090 hrs · 47,705 cycles

GIRT BAR HOLDER ON L1 DOOR BROKEN. NEED PART RETAINER CLIP. R & R GIRT BAR RETAINER CLIP ON L1 DOOR IAW SMP. R & R GIRT BAR RETAINER CLIP ON L1 DOOR IAW SMP.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 74,655 hrs · 47,381 cycles

CREW ENTRY DOOR EMERGENCY SLIDE LIGHT INOPERATIVE. REPLACED EMERGENCY SLIDE LIGHT BATTERY PACK AND OPS CHECKED OK IAW MM 33-50-051. OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 74,636 hrs · 47,364 cycles

PERFORMED TRANSIT CHECK, CABIN EMERGENCY EXIT LIGHTS INOPERATIVE. R & R CABIN EMERGENCY EXIT LIGHT ASSY. OPS NORMAL IAW MM35-50-001-0-0. PREMATURE REMOVAL/INSTALLATION.

Part: FRAME — CORRODED (BS 1166 S27-29R) · corrosion level 2 · airframe 74,478 hrs · 47,204 cycles

AFT PIT FRAME IS CORRODED ON AFT SIDE BELOW FAIL SAFE CHORD AT BS 1166 BETWEEN S29R - S27R. REPLACED FRAME ASSY.

Part: SHEAR TIE — CORRODED (BS 1166 S28-29L) · corrosion level 2 · airframe 74,478 hrs · 47,204 cycles

AFT PIT SHEAR TIE IS CORRODED ON FWD SIDE AT BS 1166, BTWN S29L- S28L. REPLACED SHEAR TIE.

Part: SHEAR TIE — CORRODED (BS 1166 S29-30R) · corrosion level 2 · airframe 74,478 hrs · 47,204 cycles

AFT PIT SHEAR TIE IS CORRODED ON AFT SIDE AT BS 1166 BTWN S30 -S29R. REPLACED SHEAR TIE.

Part: TEE FITTING — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 74,478 hrs · 47,204 cycles

C2 DOOR LOWER INBD TEE FITTING CORRODED. REMOVED TEE FITTING IAW SRM 51-30-2, FABRICATED, LOCATED AND DRILLED NEW TEE FITTING IAW SRM 52-30-1 FIG 1, INSTALLED NEW TEE FITTING IAW SRM 51-30-2.

Part: FAILSAFE — CORRODED (BS 1166 S27-29L) · corrosion level 2 · airframe 74,478 hrs · 47,204 cycles

FAILSAFE CORRODED AT BS 1166 BTWN S27-29L. REMOVED FAILSAFE IAW SRM 51-30-2. FABRICATED NEW FAILSAFE IAW SRM 53-10-2 FIG 5 AND 51-20-1. INSTALLED NEW FAILSAFE IAW SRM 51-30-2 AND DWG 65-16349 REV T.

Part: ACCESS PANEL — GOUGED (LT WING TE FLAP) · airframe 74,478 hrs · 47,204 cycles

GOUGE - LT INBD FORE FLAP L/E ACCESS PANEL, UPPER SURFACE, APPROX FLAP CENTER LINE. REMOVED & REPLACED LT INBD FOREFLAP ASSY IAW MM 27-51-001-4. OPS CHECKED NORMAL IAW MM 27-51-000-5.

Part: SKIN — CORRODED (BS 700 S26L) · corrosion level 2 · airframe 74,478 hrs · 47,204 cycles

CORROSION ON SKIN BS 700 S26L. REPAIRED IAW EA 7-5330-152457.

Part: FRAME — CORRODED (BS 1166 S27-29L) · corrosion level 2 · airframe 74,478 hrs · 47,204 cycles

FRAME IS CORRODED ON AFT SIDE BELOW THE FAILSAFE CHORD AT BS 1166 BETWEEN S27-29L. REMOVED & REPLACED FRAME IAW DWG 65- 16349 AND SRM 51-30-2.

Part: SHEAR TIE — CORRODED (BS 720E S27L) · corrosion level 2 · airframe 74,478 hrs · 47,204 cycles

CORROSION ON SHEAR TIE 720E BETWEEN S27-28L. REMOVED SHEAR TIE IAW SRM 53-10-4 FIG 11. FABRICATED DOUBLER AND INSTALLED IAW SRM 53-10-4 FIG 11.

Part: STRINGER — CORRODED (BS 680-690 S27L) · corrosion level 2 · airframe 74,478 hrs · 47,204 cycles

AFT PIT S27L HAS ELONGATED FASTENER HOLES AND CORROSION BTWN BS 680 - BS 690. REMOVED DAMAGED STRINGER SECTION, FABRICATED STRINGER REPAIR PARTS & INSTALLED IAW SRM 53-10-3 FIG 1 & 51-30-2.

Part: STRINGER SPLICE — CORRODED · corrosion level 2 · airframe 74,478 hrs · 47,204 cycles

CORROSION STRINGER SPLICE 28L BS 680. REMOVED AND REPLACED IAW SRM 51-40-02.

Part: SHEAR TIE — CORRODED (BS 700 S25-26L) · corrosion level 2 · airframe 74,478 hrs · 47,204 cycles

CORROSION ON SHEAR TIE AT BS 700 BETWEEN S25-25L. REMOVED & REPLACED DAMAGED SHEAR TIE AT BS 700 BETWEEN STR 26L & 25L IAW DWG 69-43683, SRM 51-30-5, SRM 51-30-2.

Part: SHEAR TIE — CORRODED (BS 620 S28L) · corrosion level 2 · airframe 74,478 hrs · 47,204 cycles

CORROSION ON SHEAR TIE BS 620 S28L. CUT OUT DAMAGED SHEAR TIE FABRICATED NEW AND INSTALLED REPAIR IAW SRM 53-10-4 FIG 15.

Part: TORQUE BOX — DAMAGED (BS 1270) · airframe 74,478 hrs · 47,204 cycles

AFT AIRSTAIR AREA, RT TORQUE BOX INBD VERTICAL WEB HAS SMALL GOUGED AREA AT BS 1270. VERTICAL WEB ON RH TORQUE BOX RBL 20.5 STA 1253 TO 1283 REMOVED, FABRICATED NEW, AND INSTALLED.

Part: SHEAR TIE — CORRODED (BS 720D S28L) · corrosion level 2 · airframe 74,478 hrs · 47,204 cycles

CORROSION ON SHEAR TIE BS 720D AT S28L. REMOVED DAMAGED SHEAR TIE, FABRICATED AND INSTALLED NEW SHEAR TIE IAW SRM 53-10-4 FIG 15.

Part: SHEAR TIE — CORRODED (BS 620 S28 L&R) · corrosion level 2 · airframe 74,478 hrs · 47,204 cycles

CORROSION ON SHEAR TIE, BS 620 AT S28 L&R. CUT OUT DAMAGED SHEAR TIEI, FABRICATED REPAIR AND INSTALLED IAW SRM 53-10-4 FIG 15.

Part: SHEAR TIE — CORRODED (BS 640 S28 L&R) · corrosion level 2 · airframe 74,478 hrs · 47,204 cycles

CORROSION ON SHEAR TIE BS 640 S28 L&R. CUTOUT DAMAGED AREA, FABRICATED SHEAR TIE & RADIUS FILLER & INSTALLED IAW SRM 53-10-4 FIG 15.

Part: SKIN — CORRODED (BS 470) · corrosion level 2 · airframe 74,478 hrs · 47,204 cycles

CORROSION ON SKIN AROUND DOME NUTS AT BS 470 BL 0. FABRICATED & INSTALLED REPAIR DOUBLER IAW SRM 53-30-3 FIG 1, SRM 53-30-3 FIG 1.

Part: STRINGER — CORRODED (BS 700-720 S27L) · corrosion level 2 · airframe 74,478 hrs · 47,204 cycles

CORROSION ON STRINGER 27L BETWEEN FRAME 700-720. REMOVED DAMAGED STRINGER SECTION, FABRICATED & INSTALLED STRINGER REPAIR IAW SRM 53-10-3 FIG 1 & SRM 51-10-2.

Part: SHEAR TIE — CORRODED (BS 700 S28R) · corrosion level 2 · airframe 74,478 hrs · 47,204 cycles

CORROSION ON SHEAR TIE 700 AT S28R. FABRICATED AND INSTALLED NEW SHEAR TIE IAW SRM 53-10-4, FIG 11.

Part: SKIN — CORRODED (BS 700-720) · corrosion level 2 · airframe 74,478 hrs · 47,204 cycles

CORROSION ON SKIN AT DOMED NUTPLATES AT BS 700-720 BETWEEN S28L&R. DAMAGED SKIN REPAIRED PER EA 7-5530-152457.

Part: STRINGER — CORRODED (BS 680 S27L) · corrosion level 2 · airframe 74,478 hrs · 47,204 cycles

CORROSION ON STRINGER 27L BS 680. REPAIRED STRINGER SECTION FROM BS 670 - 690 ON NR N00838.

Part: SHEAR TIE — CORRODED (BS 720F S27-28L) · corrosion level 2 · airframe 74,478 hrs · 47,204 cycles

CORROSION ON SHEAR TIE 720F AT S27-28L. CUT OUT DAMAGE AREA, DIMENSION 1" X 6", FABRICATED SHEAR TIE AND INSTALLED IAW SRM 53-10-4 FIG 15.

Part: SHEAR TIE — CORRODED (BS 720 S27-28R) · corrosion level 2 · airframe 74,478 hrs · 47,204 cycles

CORROSION ON SHEAR TIE 720F AT S27-28R. CUT OUT DAMAGE AREA, FABRICATED AND. INSTALLED IAW SRM 53-10-4 FIG 15.

Part: STRINGER — CORRODED (BS 470 S28R) · corrosion level 2 · airframe 74,478 hrs · 47,204 cycles

CORROSION IN STRINGER 28R AT BS 470. REMOVED DAMAGED STRINGER SECTION FROM BS 460-490 IAW SRM 51-30-2. FABRICATED STRINGER SECTION IAW SRM 53-10-3 FIG 1. INSTALLED NEW STRINGER SECTION IAW SRM 53-10-3 FIG 1 AND 51-30-2.

Part: FRAME — CRACKED (BS 970 S26-27L) · corrosion level 2 · airframe 74,478 hrs · 47,204 cycles

FRAME AT BS 970 BETWEEN S26-27L CRACKED. REMOVED FRAME DAMAGED SECTION, FABRICATED NEW FRAME SECTION, SPLICES AND INSTALLED IAW SRM 51-40-3, FIG 1, SRM 53-10-2 FIG 5 & SRM 51-30-2.

Part: SHEAR TIE — CORRODED (BS 720F S28 L/R) · corrosion level 2 · airframe 74,478 hrs · 47,204 cycles

CORROSION ON SHEAR TIE 720F BETWEEN S28L-28R. CUTOUT DAMAGE AREA , FABRICATED SHEAR TIE AND, INSTALLED IAW SRM 53-10-4 FIG 15.

Part: SHEAR TIE — CORRODED (BS 950B S29-30L) · corrosion level 2 · airframe 74,478 hrs · 47,204 cycles

AFT CARGO BAY SHEAR TIE IS CORRODED ON FWD AND AFT SIDES AT BS 950B BETWEEN S29- 30L. REMOVED, FABRICATED NEW, AND INSTALLED SHEAR TIE IAW SRM 53-10-4 FIG 15.

Part: SKIN — CORRODED (BS 680 S28L/R) · corrosion level 2 · airframe 74,478 hrs · 47,204 cycles

CORRODED SKIN ON FRAME 680 BETWEEN STR 28R AND STR 28L. DAMAGED SKIN REPAIRED PER EA 7-5330-152457.

Part: STRINGER — CORRODED (BS 990-1010) · corrosion level 2 · airframe 74,478 hrs · 47,204 cycles

STRINGER 27L CORRODED BS 990-1010. REMOVED DAMAGED STRINGER SECTION. FABRICATED REPAIR PARTS (FILLER & SPLICE) & INSTALLED IAW SRM 53-10-3 FIG 1 & 51-30-2.

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 74,478 hrs · 47,204 cycles

AFT PIT SHEAR TIE CORRODED ON FWD SIDE AT BS 1070 BETWEEN S28R - S27R.

Part: STRINGER SPLICE — CORRODED (BS 990-1010 S27L) · airframe 74,478 hrs · 47,204 cycles

STRINGER 27L SPLICE IS CORRODED BETWEEN BS 990-1010. REMOVED DAMAGED STRINGER IAW SRM 51-30-2. FABRICATED & INSTALLED NEW STRINGER SPLICE IAW DWG 65-56249 & SRM 51-30-2.

Part: STRINGER — CORRODED (BS 1010-1030) · corrosion level 2 · airframe 74,478 hrs · 47,204 cycles

STRINGER 27L CORRODED BETWEEN BS 1010-1030. REMOVED DAMAGED STRINGER SECTION. FABRICATED STRINGER REPAIR PARTS & INSTALLED IAW SRM 53-10-3 FIG 1 & SRM 51-30-2.

Part: SHEAR TIE — CORRODED (BS 950B S28-29L) · corrosion level 2 · airframe 74,478 hrs · 47,204 cycles

SHEAR TIE CORRODED AT BS 950B S28-29L. REMOVED, FABRICATED, & INSTALLED SHEAR TIE SECTION IAW SRM 53-10-4 FIG 15.

Part: SHEAR TIE — CORRODED (BS 720B S28L) · corrosion level 2 · airframe 74,478 hrs · 47,204 cycles

CORROSION ON SHEAR TIE BS 720B AT S28L. CUT OUT DAMAGE SHEAR TIE SECTION IAW SRM 53-10-4 FIG 11. FABRICATED REPAIR IAW SRM 53-10-4 FIG 11. INSTALLED TIE IAW SRM 53-10-4 FIG 11 REV 103.

Part: SEAT TRACK — CORRODED (BS 848-870) · corrosion level 2 · airframe 74,478 hrs · 47,204 cycles

CORROSION ON SEAT TRACK AT LBL 25 BETWEEN BS 848 AND 870. REMOVED SEAT TRACK IAW SRM 51-30-2, FABRICATED, LOCATED AND DRILLED FLOATING SEAT TRACK & INSTALLED NEW SUPPORT SEAT TRACK & SUPPORT IAW DWG 53FX1497 REV S.

Part: ANGLE — CRACKED (BS 1273) · airframe 74,478 hrs · 47,204 cycles

AFT AIRSTAIR, RT LOWER TORQUE BOX, BS 1273 FWD SIDE ANGLE IS CRACKED. REMOVED & REPLACED ANGLE IAW DWG 65C13874 REV B.

Part: ANGLE — CRACKED (BS 1273) · airframe 74,478 hrs · 47,204 cycles

AFT AIRSTAIR, RT LOWER TORQUE BOX BS 1273 AFT SIDE ANGLE IS CRACKED. REMOVED & REPLACED ANGLE IAW DWG 65-17518.

Part: STRUCTURE — CORRODED (VERTICAL STAB) · corrosion level 2 · airframe 74,478 hrs · 47,204 cycles

VERT STAB INT. BS 1342 RT CORNER AT WL 259 AT LOWER WEB HAS EXFOLIATED CORROSION UNDER LEVELING COMPOUND. CUTOUT DAMAGED VERTICAL STAB LOWER CHORD, FABRICATED REPAIR PARTS & INSTALLED REPAIR AT VERTICAL STAB IAW FX WC 7-5530-7-2303 P6

Part: ANGLE — CRACKED (BS 1273) · airframe 74,478 hrs · 47,204 cycles

AFT AIRSTAIRS, RT LOWER TORQUE BOX, UPPER INBD ANGLE IS CRACKED AT BS 1273. REMOVED DAMAGED ANGLE, FABRICATED, AND INSTALLED IAW DWG 65C13874, REV B & SRM 51-30-2.

Part: SKIN — CORRODED (BS 480-500) · corrosion level 2 · airframe 74,478 hrs · 47,204 cycles

SKIN IS CORRODED BETWEEN BS 480-500 S28-27L. CUT-OUT DAMAGED SKIN AREA, FABRICATED & INSTALLED REPAIR DOUBLER IAW SRM 53-30-3 FIG 3A, SRM 51-30-2, & 51-30-5.

Part: SHEAR TIE — CORRODED (BS 700 S27-28L) · corrosion level 2 · airframe 74,478 hrs · 47,204 cycles

CARGO BAY HAS CORROSION ON SHEAR TIE AT BS 700 BETWEEN S27-28L REMOVED, FABRICATED, AND INSTALLED NEW SHEAR TIE IAW SRM 53-10-4, FIG 11.

Part: SHEAR TIE — CORRODED (BS 950A S28-29L) · corrosion level 2 · airframe 74,478 hrs · 47,204 cycles

SHEAR TIE CORRODED BS 950A BTWN S28-29L. CUT OUT DAMAGE IAW SRM 53-10-4 FIG 13. FABRICATED AND INSTALLED NEW SHEAR TIE IAW SRM 53-10-4 FIG 13.

Part: SHEAR TIE — CORRODED (BS 500 S27-28L) · corrosion level 2 · airframe 74,478 hrs · 47,204 cycles

CORROSION ON SHEAR TIE AT BS 500, BETWEEN STRINGER 28L AND 27L. REMOVED DAMAGED SHEAR TIE IAW SRM REV 103, 51-10-1 FABRICATED AND INSTALLED SHEAR TIE IAW SRM 53-10-4 FIG 15.

Part: SHEAR TIE — CORRODED (BS 1148 S29-30L) · corrosion level 2 · airframe 74,478 hrs · 47,204 cycles

SHEAR TIE IS CORRODED AT BS 1148, BETWEEN S30-S29L. REMOVED SHEAR TIE IAW SRM 51-30-2. FABRICATED NEW SHEAR TIE IAW DWG NR 65-16348. INSTALLED SHEAR TIE IAW SRM 51-30-2.

Part: STRINGER — PUNCTURED (BS 460-480 S28L) · corrosion level 2 · airframe 74,478 hrs · 47,204 cycles

STRINGER 28L OTBD FLANGE IS PUNCTURED BTWN BS 460-480. REMOVED, FABRICATED & INSTALLED STRINGER SECTION IAW SRM 53-10-3 FIG 1.

Part: STRINGER — CORRODED (BS 520-540 S28L) · corrosion level 2 · airframe 74,478 hrs · 47,204 cycles

STRINGER 28L IS CORRODED BETWEEN BS 520-540. REPAIRED STRINGER

Part: STRINGER — CORRODED (BS 490 S28L) · corrosion level 2 · airframe 74,478 hrs · 47,204 cycles

CORROSION ON STRINGER 28L AT BS 490.

Part: FRAME — CORRODED (BS 950A S28-29L) · corrosion level 2 · airframe 74,478 hrs · 47,204 cycles

FRAME CORRODED ON FWD SIDE BS 950A BETWEEN S29L-28L. REMOVED DAMAGED AREA IAW B727 SRM 51-40-3 FIG 1. FABRICATED REPAIR DOUBLER IAW SRM 51-40-3 FIG 1 AND 53-10-2 FIG 1. INSTALLED REPAIR DOUBLER IAW SRM 51-40-3 FIG 1.

Part: SHEAR TIE — CORRODED (BS 950A S29-30L) · corrosion level 2 · airframe 74,478 hrs · 47,204 cycles

SHEAR TIE CORRODED BS 950A BTWN S29-30L. CUT OUT DAMAGED SHEAR TIE IAW SRM 53-10-4 FIG 13. FABRICATED AND INSTALLED SHEAR TIE REPAIR IAW SRM 53-10-4 FIG 13.

Part: BULKHEAD — CORRODED (BS 950) · airframe 74,478 hrs · 47,204 cycles

AFT PIT, BS 950 BULKHEAD SHELF IS CORRODED ON UPPER SURFACE FROM LBL 30 TO RBL 12.

Part: STRINGER — CORRODED (BS 720A-720B S26) · corrosion level 2 · airframe 74,478 hrs · 47,204 cycles

STRINGER 26L CORRODED BETWEEN BS 720A-720B. CUTOUT DAMAGED SECTION OF THE STRINGER, APPROX CUTOUT DIM: 5". FABRICATED STRINGER FILLER AND STRINGER HAT SECTION REPAIR. INSTALLED REPAIR IAW SRM 53-10-1 FIG 1, SRM 53-10-3 FIG 1, SRM 51-10-2 AND SRM 51-30-2.

Part: STRINGER — CORRODED (BS 890 S18A LT) · corrosion level 2 · airframe 74,478 hrs · 47,204 cycles

CORROSION ON STRINGER 18A, LOWER SHELF AT BS 890, LBL 60. REMOVED DAMAGED STRINGER, FABRICATED NEW, AND INSTALLED IAW DWG 65-22419 & SRM 51-30-2.

Part: SKIN — CORRODED (BS 720A-720B) · corrosion level 2 · airframe 74,478 hrs · 47,204 cycles

FUSELAGE SKIN (LOWER) OF BS 720A TO 720B S26L, LAP SPLICE IS EXFOLIATED. CUTOUT DAMAGED SKIN, FABRICATED DOUBLER AND STRUCTURAL FILLER AND PARTS INSTALLED IAW SRM 53-30-3, FIG 5.

Part: STRINGER — CORRODED (BS 930 S18A LT) · corrosion level 2 · airframe 74,478 hrs · 47,204 cycles

CORROSION ON STRINGER 18A LOWER SHELF AT BS 930, LBL 60. REPAIR ACCOMPLISHED.

Part: SEAT TRACK — CORRODED (BS 760-848) · corrosion level 2 · airframe 74,478 hrs · 47,204 cycles

CORROSION ON SEAT TRACK AT LBL 25 BETWEEN FRAME 760 AND 848. FABRICATED SEAT TRACK IAW DRAWING 65-16279. INSTALLED NEW SEAT TRACK IAW SRM 51-30-2.

Part: SKIN — CORRODED (BS 720A S27-28L) · corrosion level 2 · airframe 74,478 hrs · 47,204 cycles

FWD CARGO BAY HAS CORROSION ON FUSELAGE SKIN NEAR BS 720A FRAME BETWEEN STR 27L AND 28L. REPAIRED.

Part: FLOORBEAM — CORRODED (BS 1070) · corrosion level 2 · airframe 74,478 hrs · 47,204 cycles

BS 1070 LOWER FLOORBEAM FLANGE HAS SURFACE CORROSION. REMOVED PREVIOUS REPAIR AT BS 1070 FLOORBEAM LOWER TEE CAP, CUTOUT FLOORBEAM LOWER TEE CAP SECTION BETWEEN LBL 69- RBL 69, FABRICATED FLOORBEAM LOWER TEE CAP REPAIR, SPLICES, AND STRAPS, LOCATED AND DRILLED REPAIR, TREATED AND PRIMED, INSTALLED FLOORBEAM LOWER TEE CAP REPAIR IAW EA 7-5310-152455.

Part: WEB — DAMAGED (TORQUE BOX) · airframe 74,478 hrs · 47,204 cycles

AFT AIRSTAIRS AREA RT SIDE FUSELAGE TORQUE BOX INBD VERTICAL WEB HAS DAMAGED AREA AT BS 1254. REMOVED DAMAGED VERTICAL WEB AT RT TORQUE BOX, RBL 20.5 STA 1253 TO 1283, FABRICATED NEW, AND INSTALLED NEW WEB AT RT TORQUE BOX IAW DWG 65C13874, REV B.

Part: STRINGER — CORRODED (BS 1030-1050) · corrosion level 2 · airframe 74,478 hrs · 47,204 cycles

BULGE EXTERIOR FUSELAGE STA 1050 - 1030 BETWEEN STR 26-27L. FOUND STRINGER CORRODED. ACCOMPLISHED STRINGER REPAIR.

Part: STRINGER SPLICE — CORRODED (BS 990-1010 S29R) · corrosion level 2 · airframe 74,478 hrs · 47,204 cycles

STRINGER SPLICE 29R HAS CORROSION BETWEEN BS 990-1010. REMOVED STRINGER SPLICE IAW SRM 51-30-2, LOCATED AND DRILLED NEW STRINGER SPLICE IAW DWG 65-56249. INSTALLED NEW STRINGER SPLICE IAW SRM 51-30-2, AND DWG NR 65-56249.

Part: SHEAR TIE — CORRODED (BS 1053 S26-27L) · corrosion level 2 · airframe 74,478 hrs · 47,204 cycles

BULGE EXTERIOR FUSELAGE STA 1053 BETWEEN STR 26 L TO STR 27L. FOUND SHEAR TIE CORRODED. REMOVED AND REPLACED SHEAR TIE IAW SRM 51-30-5 AND SRM 51-30-2.

Part: STRINGER — CORRODED (BS 490 S28L) · corrosion level 2 · airframe 74,478 hrs · 47,204 cycles

CORROSION ON STRINGER 28L AT BS 490. REMOVED DAMAGED STRINGER SECTION, FABRICATED NEW STRINGER SECTION, SPLICES AND INSTALLED IAW SRM 53-10-3 FIG 1 & SRM 51-30-2.

Part: STRINGER SPLICE — CORRODED (BS 950F-970 S28L) · corrosion level 2 · airframe 74,478 hrs · 47,204 cycles

STRINGER SPLICE 28L IS CORRODED BETWEEN BS 950F-970. REMOVED STRINGER SPLICE IAW SRM 51-30-2, FABRICATED NEW STRINGER SPLICE AND INSTALLED IAW SRM 53-10-3, FIG 1.

Part: STRINGER — CORRODED (BS 1148 S26R) · corrosion level 2 · airframe 74,478 hrs · 47,204 cycles

AFT PIT STRINGER 26R IS CORRODED WITH EXFOLIATION AT BS 1148. CUT OUT DAMAGED AREA AND FABRICATED FILLER, SPLICES AND TAPER SHIMS. INSTALLED REPAIR PARTS IAW SRM 53-10-3 FIG 1.

Part: STRINGER SPLICE — CORRODED (BS 950F S28L) · corrosion level 2 · airframe 74,478 hrs · 47,204 cycles

STRINGER SPLICE 28L, CORRODED AT BS 950F. ACCOMPLISHED REPAIR ON NR N00473.

Part: STRINGER — CORRODED (BS 1183-1166) · corrosion level 2 · airframe 74,478 hrs · 47,204 cycles

STRINGER 29L IS CORRODED BETWEEN BS 1183-1166. CUTOUT DAMAGED STRINGER SECTION, FABRICATED REPAIR FILLER & SPLICE, INSTALLED REPAIR IAW SRM 51-30-2, SRM 53-10-3 FIG 1, & SRM 51-10-2.

Part: SHEAR TIE — CORRODED (BS 720 S27-28R) · corrosion level 2 · airframe 74,478 hrs · 47,204 cycles

FWD CARGO COMPARTMENT SHEAR TIE CORRODED AT FRAME 720 BETWEEN S-27R AND S-28R. CUTOUT DAMAGED SHEAR TIE, FABRICATED NEW SHEAR TIE, & INSTALLED IAW SRM 53-10-4 FIG 11, SRM 53-10-2 FIG 3, SRM 51-30-2 & ER 2-37153-801.

Part: SHEAR TIE — CORRODED (BS 720 S27-28L) · corrosion level 2 · airframe 74,478 hrs · 47,204 cycles

FWD CARGO BAY HAS CORROSION ON SHEAR TIE AT BS 720 BETWEEN S27 AND 28L. REMOVED DAMAGED SHEAR TIE, FABRICATED NEW SHEAR TIE & INSTALLED IAW SRM 53-10-4 FIG 11, SRM 53-10-2 FIG 3 & SRM 51-30-2.

Part: SHEAR TIE — CORRODED (BS 1070 S27-28R) · corrosion level 2 · airframe 74,478 hrs · 47,204 cycles

AFT PIT SHEAR TIE CORRODED ON FWD SIDE AT BS 1070, BETWEEN S27-28R. REMOVED SHEAR TIE IAW SRM 51-30-02, LOCATED & DRILLED NEW SHEAR TIE IAW SRM 51-30-05. INSTALLED NEW SHEAR TIE IAW SRM 51-30-02.

Part: BATTERY — INOPERATIVE (SLIDE LIGHT) · airframe 74,454 hrs · 47,185 cycles

EMERGENCY ESCAPE SLIDE LIGHT (DOOR MOUNTED) INOPERATIVE. R & R EMERGENCY ESCAPE SLIDE LIGHT BATTERY, OPS CHECK GOOD IAW AMM 33-50-121-2-0.

Part: ACTUATOR — LEAKING (NR 3 LE FLAP) · airframe 74,283 hrs · 47,022 cycles

AFTER GEAR RETRACTION & DURING FLAP RETRACTION, TOTAL LOSS OF SYS A FLUID, COMPLIED WITH QRH & RETURNED TO DEPARTURE. AFTER BLOCK IN TO GATE, NOTED 1 GALLON OF FLUID REMAINING IN A SYS. R & R NR 3 L/E FLAP ACTUATOR IAW MM 27-81-022-4 AFTER UNIT FOUND TO BE LEAKING. ACFT OK FOR SERVICE.

Part: FRAME — DENTED (FUSELAGE) · airframe 66,899 hrs · 41,466 cycles

AFT CARGO BAY, FRAME DENTED, BETWEEN STR 26L & 25L AT BS 950C. REPAIRED IAW FED EX EA 7-5310-55240.

Part: FRAME — DENTED (FUSELAGE) · airframe 66,899 hrs · 41,466 cycles

AFT CARGO BAY FRAME DENTED, BS 990, BETWEEN STR 26L & 25L. REPAIRED IAW FED EX EA 7-5310-55245.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 66,899 hrs · 41,466 cycles

STATIC DISCHARGE DAMAGE AT BS 433 BETWEEN STR 20 AND 21 R/T. *S/D* REPAIRED IAW FED EX EA 7-5330-70631.

Part: FRAME — GOUGED (FUSELAGE) · corrosion level 2 · airframe 66,899 hrs · 41,466 cycles

FRAME GOUGED BS 1130 JUST BELOW STR 7L. REMOVED GOUGE ON FRAME AT BS 1130, JUST BELOW STRINGER 7L. ORIGINAL MATERIAL THICKNESS .071 INCH. REMOVED .050 INCH, DAMAGE OUT OF LIMITS PER SRM 53-10-1 FIG 1. REPAIRED DAMAGE IAW SRM 51-40-3.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,899 hrs · 41,466 cycles

CORROSION (C53-224-01,1) ON FLOORBEAM BS 340 RBL 12 WL 208 AT FASTENER HOLE. CORROSION ON FLOORBEAM BS 340, RBL 12, WL 208 AT FASTENER HOLE FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. REMOVED & REPLACED FLOORBEAM BS 340 FROM BL 0 - RBL 65 PER SR DWG SR 27-53-007.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,899 hrs · 41,466 cycles

STRINGER CORRODED AT BS 990 STR 28 LT. FOUND CORROSION ON STRINGER AT BS 990, STR 28 LT TO BE OUT OF LIMITS PER SRM 53-10- 1. REPAIRED STRINGER IAW SRM 53-10-3.

Part: STRINGER CLIP — DAMAGED (FUSELAGE) · airframe 66,899 hrs · 41,466 cycles

AFT CARGO BAY, MECHANICAL DAMAGE ON STRINGER CLIP, STR 25R, BS 1030. LOCATED & DRILLED HOLES ON NEW STRINGER CLIP AND REMOVED DAMAGE STRINGER CLIP AND INSTALLED NEW IAW SRM 51-30-2 AT BS 1030 25R STR.

Part: FRAME — DENTED (FUSELAGE) · airframe 66,899 hrs · 41,466 cycles

AFT CARGO BAY, FRAME DENTED, BS 1110, BETWEEN STR 26L & 25L. REPAIRED IAW FED EX EA 7-5310-55235

Part: FRAME — DAMAGED (FUSELAGE) · airframe 66,899 hrs · 41,466 cycles

FWD CARGO BAY TOP OF FRAME HAS MECHANICAL DAMAGE BS 580 BL 0 - RBL 4. REMOVED DAMAGE AREA OF BS 580 FRAME. FABRICATED REPAIR AND INSTALLED REPAIR IAW SRM 51-40-3.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,899 hrs · 41,466 cycles

CORROSION ON STR 27L, STA 580 AROUND FASTENER, FWD CARGO BAY. CORROSION ON STR 27 LT, STA 580 FWD CARGO BAY FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. REPAIRED AREA PER SRM 53-10-3, 51-30-2.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,899 hrs · 41,466 cycles

FOUND CORROSION ON SHEAR TIE AT BS 700 LBL 5 TO RBL 5. CUT AND REMOVED DAMAGE AREA OF SHEAR TIE BS 700 LBL 5 TO RBL 5. FABRICATED AND INSTALLED REPAIR IAW SRM 53-10-4 FIG 11.

Part: FRAME — DENTED (FUSELAGE) · airframe 66,899 hrs · 41,466 cycles

FWD CARGO BAY FRAME IS DENTED BS 700 BETWEEN STR 24L & 25L. REMOVED DAMAGE AREA OF FRAME. FABRICATED REPAIR AND INSTALLED REPAIR IAW SRM 51-40-3.

Part: SKIN — DENTED (FUSELAGE) · airframe 66,899 hrs · 41,466 cycles

DENT IN SKIN AT BS 1350 BELOW STR 6L. CUT OUT DAMAGED SKIN AT BS 1350 BELOW STR 6L AND INSTALLED REPAIR DOUBLER PER SRM 54-30-3.

Part: FRAME — DENTED (FUSELAGE) · airframe 66,899 hrs · 41,466 cycles

DENT IN FRAME, STA 580, BETWEEN STR 22L AND STR 24L. REMOVED DAMAGED SECTION ON FRAME 580 B/N STR 22L & STR 24L. APPROX. 1.5 INCHES PER SRM 53-40-3. FABRICATED REPAIR PART PER SRM 51-40-3. ALODINED, PRIMED & PAINTED PER SRM 51-10-2. INSTALLED PER SRM 51-30-2. FED EX EA 7-5310-70628A.

Part: FRAME — DENTED (FUSELAGE) · airframe 66,899 hrs · 41,466 cycles

AFT CARGO BAY, FRAME DENTED, BS 1070, BETWEEN STR 26L & 25L. REPAIRED I.A.W FED EX E.A. 7-5310-55239

Part: FRAME — DENTED (FUSELAGE) · airframe 66,899 hrs · 41,466 cycles

AFT CARGO BAY, FRAME DENTED, BS 1050, BETWEEN STR 26R & 25R. REPAIRED IAW FED EX EA 7-5310-55242

Part: FRAME — BENT (FUSELAGE) · airframe 66,899 hrs · 41,466 cycles

FRAME BENT AT BS 950C, STR 26 RT. REPAIRED IAW FED EX EA 7-5310-55240

Part: FRAME — DENTED (FUSELAGE) · airframe 66,899 hrs · 41,466 cycles

AFT CARGO BAY, FRAME DENTED, BS 970, BETWEEN STR 26L & 25L. REPAIRED IAW FED EX EA 7-5310-55243

Part: SKIN — GOUGED (FUSELAGE) · airframe 66,899 hrs · 41,466 cycles

FUSELAGE EXTERNAL SKIN HAS GOUGES AT BS 1149 BETWEEN STRINGER 6 & 7 LT. SKIN AT BS 1149 BETWEEN STR 6 & 7 LT WAS FOUND TO BE OUT OF LIMITS. CUT OUT DAMAGE & REPAIRED SKIN PER FED EX EA 7-5330-55232.

Part: FRAME — DENTED (FUSELAGE) · airframe 66,899 hrs · 41,466 cycles

DENT IN FRAME, STA 560, BETWEEN STR 23L AND STR 25L. REMOVED DAMAGE AREA OF BS 560 FRAME. FABRICATED REPAIR AND INSTALLED REPAIR IAW SRM 51-40-3, EA 7-5310-70628.

Part: FRAME — DENTED (FUSELAGE) · airframe 66,899 hrs · 41,466 cycles

DENT IN FRAME, STA 600, BETWEEN STR 23L AND STR 24L. REMOVED DAMAGE AREA OF BS 600 FRAME. FABRICATED REPAIR AND INSTALL REPAIR IAW SRM 51-40-3.

Part: FRAME — DENTED (FUSELAGE) · airframe 66,899 hrs · 41,466 cycles

AFT CARGO BAY, FRAME DENTED, BS 1030, BETWEEN STR 26L & 25L. REPAIRED IAW FED EX EA 7-5310-55236

Part: FRAME — DENTED (FUSELAGE) · airframe 66,899 hrs · 41,466 cycles

AFT CARGO BAY, FRAME DENTED, BS 1050, BETWEEN STR 26L & 25L. REPAIRED IAW FED EX EA 7-5310-55242

Part: BULKHEAD — PUNCTURED (FUSELAGE) · airframe 66,899 hrs · 41,466 cycles

WHILE WORKING FED EX WORK CARD, PUNCTURED BULKHEAD BS 227 LBL 21 WL 187. REPAIRED PUNCTURED BULKHEAD BS 227, LBL 21, WL 187 IAW SRM 51-40-2, 51-30-2 AND 51-10-2.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,899 hrs · 41,466 cycles

CORROSION ON STR 27L, STA 508, AROUND FASTENER, FWD CARGO BAY. REMOVED CORROSION ON STR 27L BS 508 AREA OF 1X1X.020 ORIG. 040. FOUND TO BE OUT OF LIMITS. CUT OUT DAMAGED SECTION OF STRINGER BS 490 - BS 510. FABRICATED, ALODINED, PRIMED, PAINTED AND INSTALLED REPAIR PARTS IAW SRM 53-10-1 AND 53-10-3 FIG 1.

Part: FRAME — DENTED (FUSELAGE) · airframe 66,899 hrs · 41,466 cycles

AFT CARGO BAY, FRAME DENTED, BS 950B, BETWEEN STR 26L & 25L. REPAIRED FRAME IAW FED EX EA 7-5310-55244

Part: FRAME — DENTED (FUSELAGE) · airframe 66,899 hrs · 41,466 cycles

AFT CARGO BAY, FRAME DENTED, BS 950F, BETWEEN STR 26L & 25L. REPAIRED IAW FED EX EA 7-5310-55238

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,899 hrs · 41,466 cycles

CRACKED SKIN AT BS 692, BL 0, WL 148. COMPLIED WITH FED EX EA 7-5330-70630 ON THE CRACKED SKIN AT B.S. 692, BL 0, WL 148.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,899 hrs · 41,466 cycles

CORROSION (C53-111-01, 3) AFT CARGO BAY, ON STR 25R, BS 1045. REMOVED CORROSION ON AFT CARGO BAY ON STR 25R BS 1045, 1 INCH X 2 INCHES. MAXIMUM MATERIAL LOST .040. ORIGINAL THICKNESS .071. OUT OF LIMITS. CUT OUT STRINGER FROM BS 1040 TO BS 1060. FABRICATED REPAIR STRINGER AND HAT SECTION. ALODINED, PRIMED, PAINTED AND INSTALLED IAW SRM 51-10-6, SRM 53-10-1, SRM 53-10-3, SRM 51-30-2 FED EX MM 51-20-151-7.

Part: FRAME — DENTED (FUSELAGE) · airframe 66,899 hrs · 41,466 cycles

AFT CARGO BAY, FRAME DENTED, BS 1090, BETWEEN STR 26L & 25L. REPAIRED IAW FED EX E.A. 7-5310-55241

Part: FAN — INOPERATIVE (AIR CONDITIONING) · airframe 66,105 hrs · 40,850 cycles

SHORTLY AFTER LVL OFF AT FLT LEVEL 280 THE NO EQUIP COOLING LIGHT ILLUM. QRH DIRECTED TO CHK / RESET EQUIP COOLING C/B. PULLED AND RESET THE C/B AND LIGHT REMAINED ON. QRH THEN DIRECTED TO SHUT OFF RADIO ALT, VHF, & DME - COMPLIED WITH CHK LIST AND LIGHT REMAINED ON. QRH DIRECTED LAND AT NEAREST SUITABLE AIRPORT - LANDED AT MCI 0201Z. FOUND BLOWER DISCHARGE DUCT MUFFLER/LINER SHIFTED AND BLOCKING HOLE FOR FLOW LIMIT NOZZLE. ALSO FOUND FLEX HOSE FOR FLOW LIMIT NOZZLE COLLAPSED. REMOVED AND REPLACED BLOWER FAN DUE TO FOD DAMAGE REF 727-200 AMM 21-58-011-4. REMOVED AND REPLACED BLOWER DISCHARGE DUCT & FLOW LIMITING NOZZLE FLEX HOSE REF 727-200 AMM 21-58-061-4. OPS CKS OK.

Part: WARNING LIGHT — FAILED (AIR CONDITIONER) · airframe 66,099 hrs · 40,844 cycles

EQUIPMENT COOLING LIGHT CAME ON IN FLIGHT. PULLED RADIO ALT CB VIA THE QRH AND LIGHT WENT OUT FOR A FEW MINUTES. LIGHT THEN CAME BACK ON STEADY. QHR SAID LAND, ASAP. ON RETURN TO MEMPHIS, LIGHT WENT OUT A COUPLE OF TIMES IN THE DESCENT BUT WAS ON MOST OF THE TIME. ADDITIONALLY WE ALL NOTICED A BURNING SMELL AFTER TAKE OFF THAT GRADUALLY DIMINISHED. FOUND LIGHT BULB BASE WORN AWAY. WITH BASE WORN AWAY THIS PUTS LIGHT IN THE PUSH-TO-TEST MODE. ALSO FOUND BURNT MARKS ON SIDE OF LIGHT LENSE FRAME WHICH COULD HAVE CAUSED SMELL. REPLACED LAMP AND CLEANED LENSE FRAME IAW SMP. TESTED AIRFLOW DETECTOR IAW 727 MM 21-58-031-4. EQUIP COOLING SYSTEM GROUND CKS, NORMAL.

Part: ARM — BENT (NLG ACTUATOR) · airframe 66,028 hrs · 40,790 cycles

RED "NOSE GEAR" UNSAFE LIGHT REMAINED DIMLY ILLUMINATED AFTER GEAR RETRACTION. COMPLIED WITH RED TAB PROCEDURES AND UPON RECYCLING GEAR, NOSE GEAR LIGHT AGAIN WENT FROM BRIGHT TO DIM AT THE SAME TIME. THE AMBER "NOSE GEAR DOOR" ANNUNICATOR LIGHT EXTINGUISHED ON S/O PANEL. FIVE MINUTES AFTER RECYCLING GEAR, RED LIGHT WENT FROM DIM TO OUT. FOUND THE THE NR 1 THROTTLE CLUTCH PACK HAS A SWITCH ACTUATOR ARM BENT. REMOVED AND REPLACED ACTUATOR ASSY FOR #1 ENG THROTTLE GEAR WARNING IN REF TO 727 MM 31- 26-011 AND OPS CKED IN REF TO 727 MM 31-26-000-5 NO PROBLEMS NOTED.

Part: OVERHEAT LOOP — OUT OF POSITION (A/C BAY) · airframe 65,418 hrs · 40,281 cycles

DURING CR FLT AT FL350 BOTH PACKS ON GOT A LWR AFT BODY OVERHEAT WARNING LIGHT. COMPL WITH RED TABS. WHEN R/PACK & ENG NR 3 BLEED AIR VLVS CLOSED, LIGHT WENT OUT WITH THROTTLE NR 3 REDUCTION. SYSTEM CK GOOD. LEFT RT PACK AND NR 3 BLEED SWITCHES CLOSED. REPEAT WRITEUP. REMOVED LT & RT AFT BODY DET LOOPS, LWR BODY DET LOOPS, AND K/ BEAM DET LOOP PER MM 26-14-001-2. FOUND R/AFT BODY LOOP TOUCHING AIR CLEANER PURGE VLV. ROUTED NEW LOOP AWAY FROM VALVE. TESTED NORM.

Part: OVERHEAT LOOP — FAULTY (FIRE PROTECTION) · airframe 65,414 hrs · 40,278 cycles

DURING CRUISE FLT AT FL330 WHEN POWER WAS REDUCED TO DESCEND, LOWER AFT BODY OVERHEAT LIGHT FLICKERED THEN CAME ON STEADY. COMPLIED WITH RED TAB PROCEDURES, LIGHT WENT OUT. SYSTEM TEST SATISFACTORY. MONITORED FOR REMAINDER OF FLIGHT. REMOVED AND REPLACED FIRE DETECTION UNIT PER M/M 26-14-00-5, OPS CHECK NORMAL. A/C OK TO CONTINUE SERVICE.

Part: OVERHEAT LOOP — FAULTY (A/C BAY) · airframe 65,392 hrs · 40,263 cycles

LOWER AFT BODY OVERHEAT LIGHT ILLUMINATED IN FLIGHT. TROUBLESHOT DOWN TO LEAK BETWEEN NR 3 BLEED & RT PACK VALVE. OPENED KEEL BEAM ACCESS IN RT W/W AND LEAK CHECKED WITH NR 3 ENGINE RUNNING NO LEAKS FOUND IN KEEL BEAM AREA, CARGO COMPARTMENT, OR AFT STAIRS AREA. ORDERED KEEL BEAM OVERHEAT DETECTOR PRECAUTIONARY. ALL OTHER OVERHEAT DETECTORS ARE IN STOCK AT GSO. FOUND GROUND IN M365 SECT 48 R OVERHEAT LOOP, REF AMM 26-14-000-1. REMOVED AND REPLACED SAME, OPS NORMAL PER AMM 26-14-001-2. SECURED AFT CARGO PANELS CLOSED PER SMP.

Part: DUCT — LEAKING (PNEUMATIC SYS) · airframe 65,375 hrs · 40,248 cycles

LOWER AFT BODY OVERHEAT LIGHT ILLUMINATED AFTER 1+10 FLIGHT TIME. DID RED TAB PROCEDURE. ISOLATED LEAK ON NR 3 ENG BETWEEN BLEED VALVE AND RIGHT PACK VALVE. FOUND STARTER DUCT LEAKING ON NR 3 ENG BLEED MANIFOLD. STARTER DUCT WAS MISALIGNED, REALIGNED STARTER DUCT TO BLEED ENG MANIFOLD & TIGHTENED CLAMPS. OPS CK NORMAL REF PER MM 36-10-000-1.

Part: SWITCH — FAULTY (NLG DOOR)

ON GEAR RETRACTION NOSE GEAR DOOR LIGHT SYS ON DIMLY. REMOVED AND REPLACED NOSE GEAR DOOR WARNING SWITCHES PER MM 32-62-011-4.

Part: DETECTOR — GROUNDED (NR 1 ENGINE)

LWR AFT BODY OVERHEAT LIGHT ILLUM. NR 1 ENG BLEED AND NR 2 ENG BLEED VALVE BOTH OPEN AND ILLUM. RAN NR 1 ENG WITH NR 1 BLEED OPEN, NO AIR LEAKS DETECTED. FOUND AFT BODY DETECTOR LOOP TOUCHING GROUND IN CLOSE PROXIMITY TO NR 1 BLEED DUCT. REPOSITIONED ELEMENT AND SYS WORK NORMAL.

Part: WARNING LIGHT — ILLUMINATED (NR 2 ENGINE)

NR 2 ENGINE LOW OIL PRESS/FILTER BYPASS ILLUM ON DEPARTURE. ENGINE SHUTDOWN FOR ABNORMALS. INSP MAIN ENG OIL FILTER, NO CONTAMINANTS FOUND PER MM 79-00-00. MANUAL INSP PER 79-00-518D OF P/W. OK TO CONTINUE SERVICE. INSP AT INTERVALS. REMOVED AND REPLACED NR 2 ENG OIL PRESSURE SWITCH PER MM 79-06-00. OPS CHECK GOOD.

Part: ACTUATOR — FAILED (NR 7 LE SLAT)

ON DEPARTURE DURING FLAP RETRACTION FROM 2 DEG TO 0 DEG, NR 7 SLAT WOULD NOT RETRACT. OPERATED SLAT/FLAPS NUMEROUS TIMES, OPS CHECKS GOOD. CHECKED NR 7 SLAT ACTUATOR FOR BYPASSING. CHECK OK, NO PLAY FOUND IN TRACKS OF ACTUATOR. OK FOR SERVICE. ALL WORK IAW B727 MM 27-80-00.

Part: POWER CONTROL — FAILED (RT ELEVATOR)

COMPLETE 'A' SYS HYD LOSS. GEAR CRANKED NORM AND ALT FLAPS OPER NORM. FOUND RT ELEV PWR CONTROL UNIT FIT BUSTED. REMOVED RT PWR CONTROL UNIT PER 727-200 MM 27-30-81. PWR CONTROL UNIT NEEDS INSTALL AND OPER CK. REMOVED AND REPLACED RIGHT ELEV PWR CONTROL PACK PER MM 27-30-081-4, OPER CK.

Part: FLOORBEAM — CORRODED (BS 1070)

CORROSION (C53-111-01,3) ON FLOORBEAM LOWER CHORD AT BS 1070, WL 200, LBL 40 TO RBL 48. *S/D* REMOVED AND REPLACED FLOORBEAM PER FEDEX EA 7-5310-45262A.

Part: FRAME — DENTED (BS 660)

THREE DENTS ON TOP FLANGE OF FRAME AT BS 660 BETWEEN STRS 23 AND 26R. *S/D* REMOVED DAMAGE FROM INNER FLANGE, FABRICATED AND INSTALLED REPAIR PARTS IAW FEDEX EA 7-5310-45287 AND SRM 51-40-2.

Part: FLOORBEAM — CORRODED (BS 1130)

CORROSION (C53-224-01,3) ON UPPER SURFACE OF UPPER CHORD BS 1130, RBL 47-49, WL 208. *S/D* REMOVED AND REPLACED CORROSION, FLAP PEENED AREA AND INSTALLED REPAIR STRAP PER FEDEX EA 7-5310-45275.

Part: FRAME — CORRODED (BS 1148)

CORROSION (C53-111-01,3) ON FRAME AT BS 1148, LBL 24 AND LBL 29, WL 161. *S/D* REMOVED AND REPLACED DAMAGE FROM FRAME, ACCOMPLISH SSI INSP AND FAB AND INSTALLED PARTS IAW FEDEX EA 7-5310-45290.

Part: FRAME — CORRODED (BS 1166)

CORROSION (C53-111-01,3) ON I/B FRAME FLANGE AT BS 1166, STR 17R. *S/D* REMOVED AND REPLACED FRAME PER FEDEX EA 7-5310-45249.

Part: BULKHEAD WEB — CRACKED (BS 1342)

WHILE WORKING W/C 7-5430-7-2303L1 PT 6 DISCOVERED CRACK IN THE BS 1342 BULKHEAD WEB AT WL 252, LBL 17. *S/D* REMOVED AND REPLACED BULKHEAD WEB PER IAW FEDEX EA 7-5310-45235.

Part: FRAME — CRACKED (BS 1010)

FOUND BS 1010 FRAME TO BE CRACKED AT RBL 18, WL 149. *S/D* REMOVED AND REPLACED FRAME PER IAW FEDEX EA 7-5310-45281.

Part: FLOORBEAM — CORRODED (BS 1090)

FOUND FLOORBEAM TO BE CORRODED AT BS 1090, RBL 45, WL 208. *S/D* REMOVED AND REPLACED UPPER FLANGE OF FLOORBEAM PER FEDEX EA 7-5310-45246.

Part: SKIN — CORRODED (BS 1115)

SKIN BULGING AT BS 1115 BETWEEN STR 26L AND 27L. *S/D* REMOVED AND REPLACED SKIN BULGE PER IAW FEDEX EA 7-5330-45222.

Part: FRAME — CORRODED (BS 1070)

NR 790 - CORROSION (C53-111-01(3)) ON FRAME AT BS 1070, STR 27R. REPAIRED FRAME AT BS 1070, STR 27R, IAW FEDEX SRM 51-40-3 FIG 1.

Part: FLOORBEAM — CORRODED (BS 1070)

NR 794 - CORROSION (C53-111-01(3)) ON FLOORBEAM LWR CHORD AT BS 1070, WL 200, LBL 40 - RBL 48. REMOVED AND REPLACED BS 1070 FLOORBEAM IAW FEDEX EA 7-5310-45262A.

Part: STRINGER — CORRODED (BS 950)

WHILE WORKING NR 802, FOUND CORROSION ON STRINGER 28R, BS 950E+1.

Part: BEAM — CRACKED (PASSENGER DOOR)

LT FWD ENTRY DOOR GATE BEAM CRACKED AT LOWER FORWARD STOP FITTING. ** S/D ** STOP DRILLED LT FWD ENTRY DOOR GATE BEAM AT LWR FWD STOP FITTING AND INSTALLED DOUBLER IAW FEDEX SR 27-52-015 STEP 1 THRU 10.

Part: SPLICE — CORRODED (BS 480)

UPON REMOVAL OF STR ON NR 303 FOUND CORROSION ON STR SPLICE STR 26L, BS 480. *S/D* REMOVED AND REPLACED STR SPLICE PER IAW FEDEX SRM 51-30-2.

Part: STRINGER — CORRODED (BS 1176)

CORROSION (C53-111-01, 3) ON STR 25R AT BS 1176. *S/D* REMOVED AND REPLACED 25R FROM BS 1158 TO 1183 IAW FEDEX SRM 53-10-3 FIG 1.

Part: STRINGER — CORRODED (BS 494)

CORROSION (C53-111-01,2) ON STRINGER 26L, BS 494. *S/D* REMOVED AND REPLACED STR 26L, BS 482-496 IAW FEDEX SRM 53-10-3 FIG 1.

Part: STRINGER — CORRODED (BS 990)

CORROSION (C53-111-01, 3) ON STR 27R AT BS 990. *S/D* REMOVED AND REPLACED STR 27R PER FEDEX EA 7-5310-45210A.

Part: BEAM — CORRODED (BS 264)

CORROSION (C53-221-01) ON FWD EDGE OF 25 G-BEAM BS 264, LBL 4 TO LBL 7, WL 208. *S/D* REMOVED AND REPLACED 25 G-BEAM, BS 264, LBL 8 TO RBL 21, WL 208 IAW FEDEX EA NR 7-5310-45212.

Part: WHEEL — MISSING (NR 1)

ON WALKAROUND, FOUND NR 1 TIRE MISSING FROM AXLE. *S/D* PERFORM VISUAL INSPECT OF LEFT MAIN GEAR, NO DEFECT NOTED. REPLACED LEFT O/B AXLE SLEEVE ASSY PER BOEING OVERHAUL MAN 32-12-01. PER HARD LAND INSP PHASE 1 PER M/M 51-51-61. REMOVED AND REPLACED NR 1 TIRE AND WHEEL ASSY PER M/M 32-45-01.

Part: CLAMP — LOOSE (NR 3 ANTI-ICE)

97-0132 LOWER AFT BODY OVERHEAT LIGHT ILLUMINATED AT FLIGHT LEVEL 250, AFTER TURNING OFF NR 2 BLEED VALVE, LIGHT EXTINGUISHED WITHIN 2 MINUTES. NR 1 AND NR 3 BLEED VALVE WERE OPEN WITH BOTH PACKS ON. CHECKED LOWER AFT BODY LOOPS IN AFT STAIRS, NR 2 ENGINE AREA, RAN ALL ENGINES. FOUND TWO CLAMPS LEAKING NR 3 THERMAL ANTI-ICE LINE BELOW LOOP. RETORQUED CLAMPS. LEAK STOPPED. OK FOR SERVICE.

Part: CLAMPS — LOOSE (NR 1 ENG STRUT)

ON CLIMBOUT, NR 1 ENGINE STRUT OVERHEAT LIGHT ILLUMINATED. NR 1 GENERATOR DRIVE OIL TEMPERATURE READ 130 IN TEMPERATURE. OVERHEAT LIGHT WENT OUT AFTER 1 MINUTE, SYSTEM TESTED GOOD NO FURTHER PROBLEMS. WING AND ENGINE ANTI-ICE WERE CLOSED. FOUND CLAMPS LOOSE AND LEAKING AT 13TH STAGE MODULATION VALVE, TIGHTENED SAME. ALSO, FOUND CONSTANT SPEED DRIVE OVER SERVICED DRAINED TO PROPER LEVEL ALL OK FOR SERVICE.

Part: RETRACT MECH — LACK OF LUBE (NLG)

ON GEAR EXTENSION NOSE GEAR REMAINED UNSAFE, GEAR WAS RECYCLED AND NO DOOR LIGHT FOR NOSE GEAR WAS NOTICED ON RETRACTION. GEAR WAS EXTENDED AGAIN WITH SAFE INDICATION ALL GEARS. GREASED, JACKED AND VISUALLY INSPECTED. OPERATED NOSE LANDING GEAR PER MAINTENANCE MANUAL 32-33-0, GEAR OPERATIONAL CHECKS NORMAL.