N432FE

Part: COUPLING — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,036 hrs · 19,588 cycles

FOUND CORROSION AT COUPLING, C 70, P 37RT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,036 hrs · 19,588 cycles

FOUND CORROSION AF FITTING C 54.2, P 45-46 RT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,036 hrs · 19,588 cycles

FOUND CORROSION AF FITTING C 54.2, P 45-46 RT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.

Part: COUPLING — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,036 hrs · 19,588 cycles

FOUND CORROSION AT COUPLING, C 65, P 56 LT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.

Part: COUPLING — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,036 hrs · 19,588 cycles

CORROSION FOUND AT COUPLING AT C 65, P 57 RT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 46,036 hrs · 19,588 cycles

FOUND CORROSION ON STRINGER P 54 RT, C 68-69 STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201.

Part: COUPLING — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,036 hrs · 19,588 cycles

FOUND CORROSION AT COUPLING P 53LT, C 55/58 REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.

Part: PLATE — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,036 hrs · 19,588 cycles

FOUND CORROSION AT GROUND VALVE PLATE C 24-25 , P52-55 LT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.

Part: COUPLING — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,036 hrs · 19,588 cycles

FOUND CORROSION AT COUPLING, C 65, P 56 LT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.

Part: ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,036 hrs · 19,588 cycles

CORROSION FOUND ON REINFORCING ANGLE AT C38-39, P 48 LT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.

Part: COUPLING — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,036 hrs · 19,588 cycles

CORROSION FOUND AT COUPLING AT C 26/32, P 45 RT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.

Part: COUPLING — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,036 hrs · 19,588 cycles

FOUND CORROSION ON COUPLING P 50 RH, C 69. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.

Part: COUPLING — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,036 hrs · 19,588 cycles

FOUND CORROSION AT COUPLING P 55RH, C 65. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.

Part: COUPLING — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,036 hrs · 19,588 cycles

CORROSION FOUND AT COUPLING AT C 65, P 55 RT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,032 hrs · 19,586 cycles

FOUND CORROSION AT CROSSBEAM C 67, C66. CROSSBEAM REPAIR PERFORMED IAW SRM 53-10-15 FIG 207 .

Part: SKIN — DAMAGED (ZONE 600) · airframe 46,032 hrs · 19,586 cycles

DURING FUNCTION PHASE, THE RT INBOARD FLAP TRAILING EDGE WAS DAMAGED REPAIR PERFORMED IAW SRM 57-53-12 PARA 13 (FIG 209).

Part: SPAR — CORRODED (RT ELEVATOR) · corrosion level 2 · airframe 46,032 hrs · 19,586 cycles

CORROSION FOUND ON RT ELEVATOR FRONT SPAR WEB NEAR RIB 2A AROUND ONE BONDING POINT REPAIR PERFORMED BY BLENDOUT UNTIL CORROSION REMOVAL IAW EA 6-5520-79603 AND RAS/CASA/3692/2004 ISS A.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,032 hrs · 19,586 cycles

FOUND CORROSION ON STRINGER P 57 LT, C 69-70 OUT OF LIMIT. STRINGER REPAIR PERFORMED SRM 53-10-14 FIG 201.

Part: RIB — CORRODED (ZONE 600) · corrosion level 2 · airframe 46,032 hrs · 19,586 cycles

FOUND ON RT MLG FWD LUG INNER BORE RIB 5 THE BUSHING TO BE OUT OF ROUND, AFTER REMOVAL OF BUSHING FOUND CORROSION ON THE LUG REPAIR PERFORMED BY CORROSION REMOVAL AND REAM UP THE HOLE IAW DRAWING R572-49121, APPROVED BY EA 6-5751-8106 AND RAS/BAE/0979/2004 ISS A.

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,032 hrs · 19,586 cycles

FOUND CORROSION AT RUN OUT FITTING AT P 44, C16A-17A LT. REPAIR PERFORMED BY REPLACEMENT OF RUNOUT FITTING IAW DRAWING R536-10440.

Part: SKIN PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,031 hrs · 19,585 cycles

CORROSION FOUND ON INTERNAL SKIN C-37-38, P55LT-55RT DOUBLER REPAIR PERFORMED IAW SRM 53-10-12 FIG 221 AND 203.

Part: BEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,032 hrs · 19,586 cycles

CORROSION FOUND ON LOWER SILL BEAM OF AFT CARGO DOOR AT C59A. REPAIR PREFORMED BY TRIM OUT THE AFFECTED AREA AND FABRICATE A STRAP IAW EA 6-5310-79580 AND RAS/DATLS/0001970/2004 ISS A.

Part: FITTING — WORN (ZONE 600) · airframe 46,032 hrs · 19,586 cycles

AT RT SPIGOT FITTING FWD OUTBOARD SIDE FOUND WEAR MARKS REPAIR PERFORMED BY BLEND OUT TO SMOOTH CONTOUR IAW EA 6-5720-79605 AND RAS/BAE/0818/2004 ISS A.

Part: PANEL — CORRODED (ZONE 400) · airframe 46,032 hrs · 19,586 cycles

FOUND CRACK ON PYLON NR 2 AT RIB 8 INBOARD AND OUTBOARD SIDE AT PANEL (ABOUT 8MM) DOUBLER REPAIR ON SIDEWALL PANELS PERFORMED IAW SRM 5451-31 FIG 201.

Part: ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,032 hrs · 19,586 cycles

FOUND CORROSION AFT PRESSURE BULKHEAD CIRCUMFERENTIAL STRAP, INNER RIM ANGLE AND FRAME COUPLING AT C80/82, P25LH TO 36RH. REPAIR PERFORMED BY CUT OUT OF DAMAGED PARTS, REINSTALLING NEW PARTS IAW DRAWING R539-70603, APPROVED BY 6-5318-79562 AND RAS/DAHAM/4018245/2004 ISS A.

Part: SKIN — WORN (ZONE 400) · airframe 46,032 hrs · 19,586 cycles

FOUND ON PYLON NR 1 AT RIB 8 INBOARD AND OUTBOARD SIDE THE HOLE FOR SUPPORT WORN DOUBLER REPAIR PERFORMED IAW SRM 54-51-31 FIG 201.

Part: FLANGE — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,032 hrs · 19,586 cycles

CORROSION FOUND ON UPPER FLANGE C25. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10

Part: SKIN — DELAMINATED (ZONE 500) · airframe 46,032 hrs · 19,586 cycles

FOUND ON LT INBOARD FLAP LOWER SKIN AT TRAILING EDGE, RIB 3-4, DELAMINATION. IN THIS AREA FOUND ON UPPER SKIN AN OLD DOUBLER INSTALLED. REPAIR PERFORMED BY REMOVAL OF THE OLD REPAIR ON UPPER SKIN AND RENEW THE REPAIR ON LOWER AND UPPER SURFACE IAW SRM 57-52-12 FIG 204.

Part: SKIN PANEL — DENTED (ZONE 200) · airframe 46,032 hrs · 19,586 cycles

FOUND DENT ON SKIN C 94-95, P3-4 RT OUT OF LIMIT. DOUBLER REPAIR PERFORMED IAW SRM 53-19-12 FIG 201.

Part: SKIN PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,032 hrs · 19,586 cycles

CORROSION FOUND ON SKIN PANEL C78/80, P 45-50 RT, IN SERVICE PANEL AREA. REPAIR PERFORMED BY BLEND OUT UNTIL CORROSION REMOVAL AND REPLACING THE TOILET SERVICE DOOR WITH COVER A539-809076-200 IAW EA 6-5330-79575 AND RAS/DATLS/0001961/2004 ISS A.

Part: SKIN PANEL — WORN (ZONE 600) · airframe 46,032 hrs · 19,586 cycles

ELONGATED HOLES FOUND ON RT WING TO PYLON HYDRAULIC FITTING RIB 8 REPAIR PERFORMED BY REAM UP AND BUSH INSTALLATION IAW DRAWING R572-49184, APPROVED BY EA 6-5720-79595 AND RAS/BAE/0931/2004 ISS A.

Part: FLANGE — DAMAGED (ZONE 100) · airframe 46,032 hrs · 19,586 cycles

FOUR MISDRILLED HOLES AT UPPER FLANGE (BEAM) AT C 33 LT. SPLICE REPAIR PERFORMED IAW SRM 53-10-15 FIG 207.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,031 hrs · 19,585 cycles

FOUND CORROSION AT STRINGER P 37 RT, C37 STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201.

Part: SKIN — CORRODED (ZONE 500) · corrosion level 2 · airframe 46,032 hrs · 19,586 cycles

DURING REMOVAL OF BOLT 642, NOTED IN SB A310-57-2028 FOUND CORROSION INSIDE THE FITTING BORE, LT WING AREA OF RIB 5 REPAIR PERFORMED BY OVERSIZING THE HOLE IAW EA 6-5721-81050 AND RAS/BAE/0928/2004 ISS A.

Part: FLANGE — DAMAGED (ZONE 100) · airframe 46,032 hrs · 19,586 cycles

TWO MISDRILLED HOLES AT UPPER FLANGE (BEAM) AT C 33 LT. SPLICE REPAIR PERFORMED IAW SRM 53-10-15 FIG 207.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,032 hrs · 19,586 cycles

FOUND CORROSION ON STRINGER P50 AT C80, LT. STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201.

Part: SPLICE — CRACKED (ZONE 100) · corrosion level 2 · airframe 46,032 hrs · 19,586 cycles

FOUND CORROSION AT SPLICE C20, P46 RT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.

Part: RIB — CORRODED (ZONE 500) · corrosion level 2 · airframe 46,032 hrs · 19,586 cycles

FOUND ON LT MLG FWD LUG INNER BORE RIB 5 THE BUSHING TO BE OUT OF ROUND, AFTER REMOVAL OF BUSHING FOUND CORROSION ON THE LUG REPAIR PERFORMED BY CORROSION REMOVAL AND REAM UP THE HOLE IAW DRAWING R572-49121, APPROVED BY EA 6-5751-8106 AND RAS/BAE/0979/2004 ISS A.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,032 hrs · 19,586 cycles

FOUND CORROSION ON STRINGER CONNECTION AT C80, P 38 LT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,032 hrs · 19,586 cycles

CORROSION FOUND AT STRINGER P38, C79-80. STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201

Part: BEAM — CRACKED (ZONE 200) · airframe 46,032 hrs · 19,586 cycles

FOUND CRACK ON LONGITUDINBAL BEAM C 74-76, P 11 LT/RT, (LT: 8MM, RT 15MM). REPAIR PERFORMED BY INSTALLING REPAIR ANGLES IAW SRM 53-181-18 FIG 204.

Part: FRAME — CORRODED (ZONE 200) · corrosion level 2 · airframe 46,032 hrs · 19,586 cycles

FOUND CORROSION AT MILLING FRAME C60, P 22RT REPAIR PERFORMED BY BLEND OUT CORROSION IAW RAS/DATLS/0001942/2004.

Part: ATTACH FITTING — CHAFED (ZONE 400) · airframe 46,032 hrs · 19,586 cycles

FOUND CHAFING MARKS, ENLARGED HOLES AND NOT CORRECT INSTALLED BUSHINGS AT PYLON NR 2 PYLON TO WING ATTACH FITTING LUGS AT RIB 12. REPAIR PERFORMED BY OVERSIZING THE BORES AND INSTALLING NEW REPAIR BUSHS IAW DRAWING R571-40283, APPROVED BY EA 6-5450-81064 AND RAS /BAE/0929/2004 ISS A.

Part: VANE — DENTED (ZONE 500) · airframe 46,032 hrs · 19,586 cycles

FOUND DENT ON LT INBOARD FLAP VANE NOSE SKIN, RIB 7-8 REPAIR PERFORMED BY CUTTING THE DAMAGED AREA AND INSTALLING A NEW SKIN WITH INNER STRAPS IAW EA 6-5752-81059 AND RAS/DABRE/7004146/2004 ISS A.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,032 hrs · 19,586 cycles

FOUND CORROSION ON STRINGER P 56 RT, C 64-65 OUT OF LIMIT STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201.

Part: SPLICE — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,032 hrs · 19,586 cycles

FOUND CORROSION AT SPLICE C20, P50 RT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.

Part: SKIN PANEL — WORN (ZONE 500) · airframe 46,032 hrs · 19,586 cycles

FOUND ELONGATED HOLES ON LT WING TO PYLON HYDRAULIC FITTING HOLES RIB 8 REPAIR PERFORMED BY REAM UP AND INSTALL BUSHINGS IAW DRAWING R572-49184 , APPROVED BY EA 6-5720-79594 AND RAS/BAE/0931/2004 ISS A.

Part: LONGERON — CORRODED (ZONE 200) · corrosion level 2 · airframe 46,015 hrs · 19,578 cycles

LONGERON BETWEEN C12A AND 15A, Y 1959 HEAVY CORRODED SPLICE REPAIR PERFORMED IAW SRM 53-12-15 FIG 207.

Part: LONGERON — CORRODED (ZONE 200) · corrosion level 2 · airframe 46,018 hrs · 19,579 cycles

LONGERON C12A-15A, Y-1959 HEAVY CORRODED REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,018 hrs · 19,579 cycles

FOUND CORROSION AT Y-Z LATCH SUPPORT FITTING OF FRAME C 25A RT REPAIR PERFORMED IAW SRM 53-13-13 FIG 203.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,018 hrs · 19,579 cycles

CORROSION ON STRINGER P52, 53, 55 RT, C 65-66 OUT OF LIMIT STRINGER REPAIR PERORMED IAW SRM 53-10-14 FIG 201.

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,018 hrs · 19,579 cycles

FOUND CORROSION AT FRAME 20A, P45 RT OUT OF LIMIT REPAIR PERORMED IAW SRM 53-13-13 FIG 202.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,021 hrs · 19,580 cycles

FOUND CORROSION ON CLIP AT C 71, P57-56RT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,018 hrs · 19,579 cycles

CORROSION FOUND ON STRINGER P 52 LT, C 60-61 STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,018 hrs · 19,579 cycles

CORROSION FOUND AT P 56 RT, C 69 OUT OF LIMIT. STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 46,018 hrs · 19,579 cycles

FOUND SEAT TRACK C15A-19, Y-953 HEAVY CORRODED. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,018 hrs · 19,579 cycles

FOUND CORROSION AT INTERNAL SKIN C17-18, P49 RH- P51 LT. REPAIR PERFORMED BY BLEND OUT THE CORROSION IAW SRM 53-12-12 FIG 104 AND RAS 031331/01/2004 ISS A, APPROVED BY EA 6-5330-79577.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,018 hrs · 19,579 cycles

CORROSION FOUND AT C64-65, P 44 LT. STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201.

Part: SKIN PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,018 hrs · 19,579 cycles

CORROSION FOUND ON INNER SKIN C 64-71, P56 LT-56 RT DOUBLER REPAIR PERFORMED AT C 66, P56 LT-56RT IAW RAS/DAHAM/4018310/2004 ISS A AND AT C 69, P56LT-56RT IAW RAS/DAHAM/4018309/2004 ISS A AND SMOOTH BLEND OUT OF CORROSION BETWEEN C 64-71, P 56 LT-56RT IAW RAS/DAHAM/4018287/2004 ISS D. APPROVED BY EA 6-5330-79574.

Part: SKIN PANEL — NONE (ZONE 100) · airframe 46,018 hrs · 19,579 cycles

OLD SKIN DOUBLER REPAIR AT C 34, BETWEEN P 54 LT-P54 RT NOT COMPATIBLE TO P TO F CONVERSION DOUBLER REPAIR RENEWED IAW EA 6-5314-79564 AND RAS/DABRE/7003949/2004 ISS A AND RAS/DABRE/7004007/2004 ISS A.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,018 hrs · 19,579 cycles

CORROSION FOUND AT C55/58-59, STRINGER P 50 LT. STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201.

Part: SKIN PANEL — FAILED (ZONE 100) · airframe 46,015 hrs · 19,578 cycles

OLD EXTERNAL SKIN DOUBLER C 33, P37-39 LT NOT COMPATIBLE WITH P TO F CONVERSION. REPAIR PERFORMED BY RENEWING THE DOUBLER REPAIR IAW RAS/DABRE/7004007/2004 ISS A AND DRAWING R737B1150.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,018 hrs · 19,579 cycles

CORROSION FOUND ON STRINGER P 56, AT C68 OUT OF LIMIT. STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 46,018 hrs · 19,579 cycles

FOUND SEAT TRACK C15-19 Y-1959 HEAVY CORRODED. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.

Part: LONGERON — CORRODED (ZONE 200) · corrosion level 2 · airframe 46,018 hrs · 19,579 cycles

LONGERON C11-15A, Y 1456 HEAVY CORRODED. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.

Part: BEAM — CORRODED (PAX DOOR) · corrosion level 2 · airframe 46,015 hrs · 19,578 cycles

CORROSION ON FWD PAX DOOR 31 LT AT BEAM NR 1 OUT OF LIMIT REPAIR PERFORMED IAW SRM 52-11-00 FIG 213, APPROVED BY EA 6-5210-79568.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,018 hrs · 19,579 cycles

CORROSION FOUND ON STRINGER P53, 54, 55 AT C59 OUT OF LIMIT. STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201.

Part: STRUCTURE — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,018 hrs · 19,579 cycles

CORROSION FOUND ON CONNECTING SECTION, C 55/58-59, P 50 LT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 46,015 hrs · 19,578 cycles

CORROSION FOUND AT SEATTRACK C15A0-19, Y 1959 REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,018 hrs · 19,579 cycles

CORROSION FOUND AT C64, P 52 LT. STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 46,018 hrs · 19,579 cycles

SEAT TRACK C15A-19, Y-1552 HEAVY CORRODED. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,018 hrs · 19,579 cycles

CORROSION AT STRINGER P 48, C38.2-39 OUT OF LIMIT. STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,018 hrs · 19,579 cycles

CORROSION ON FLOORBEAM C70 RT OUT OF LIMIT. SPLICE REPAIR PERFORMED IAW SRM 53-10-15 FIG 207.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,018 hrs · 19,579 cycles

CORROSION FOUND AT C67-69, P 56 AND P56 RT. STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,018 hrs · 19,579 cycles

CORROSION FOUND ON STRINGER P44 RT AT C54.2 OUT OF LIMIT. STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201.

Part: FRAME — CRACKED (NR 1 PYLON) · airframe 45,828 hrs · 19,472 cycles

PYLON NR 1 AT AFT T/E LOWER SECTION LOWER FARING INNER INNER (A)-FRAME UPPER AND LOWER PORTION SUPPORT HAS CRACK BETWEEN RIB 19 AND 20 AND VISIBLE THRU OPEN ACCESS NR 474CR AND LIGHTING HOLE REMOVED AND REPLACED A FRAME IAW SRM 51-40-21.

Part: SILL — CORRODED (CARGO DOORWAY) · corrosion level 2 · airframe 45,828 hrs · 19,472 cycles

AFT CARGO COMPARTMENT AFT LOWER CORNER SILL EXFOLIATED AROUND NR 7 ECCENTRIC DOOR FRAME FITTING REMOVED AND REPLACED DOOR SILL BEAM P/N 539-70189-000 RT IAW 51-32-11-5 AND DWG 17/E53970189 REV A. PERFORMED AFT CARGO DOOR TEST AND ADJUSTMENT TEST STEP 3E ,1 AND 9 IAW AMM 52-32-11-5 CHECK GOOD. WARNING SWITCH OPS CHECKS GOOD IAW AMM 52-71 11-5 CARRY OUT OPERATIONAL OPS CHECKS GOOD IAW AMM 52-71-11-5.

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 45,828 hrs · 19,472 cycles

FOUND FRAME CORRODED. COMPLY WITH EA 6-5310-110742 FUSELAGE MAINFRAME FR 63 RIGHT CORROSION REPAIR COMPLIED WITH EA 6-5310-110742 FUSELAGE, MAINFRAME, FR 63 RIGHT CORROSION REPAIR AND SPLICE AT STR NR 39.

Part: ATTACH FITTING — CORRODED (ZONE 300) · corrosion level 2 · airframe 45,828 hrs · 19,472 cycles

VERT STAB REAR SPAR RT UPPER MOST HINGE ATTACH FITTING HAS CORROSION. REMOVED HINGE FITTING IAW SRM 51-40-21. LOCATED AND DRILLED NEW FITTING IAW SRM 51-40- 44. INSTALLED NEW FITTING IAW SRM 51-40-21. INSTALLED NEW STRINGER CLIPS 1/2 AT RIB 25 IAW N/R S00021 AND EA 6-5530-110749.

Part: ATTACH FITTING — CORRODED (ZONE 300) · corrosion level 2 · airframe 45,828 hrs · 19,472 cycles

VERT STAB REAR SPAR RT UPPER MOST HINGE ATTACH FITTING HAS CORROSION. REMOVED HINGE FITTING IAW SRM 51-40-21. LOCATED AND DRILLED NEW FITTING IAW SRM 51-40-44. INSTALLED NEW FITTING IAW SRM 51-40-21. INSTALLED NEW STRINGER CLIPS 1 AND 2 AT RIB25 IAW N/R S00021 AND EA 6-5530-110749.

Part: STIFFENER — CRACKED (NR 1 PYLON) · airframe 45,828 hrs · 19,472 cycles

ENG NR 1 AFT LOWER PYLON INNER COMPARTMENT AT FLOOR AREA,RIB NR 14 "C"-CHANNEL SUPPORT HAS A CRACK VISIBLE THRU OPEN ACCESS NR 473 AL. REMOVED AND REPLACED STIFFENER IAW SRM 51-40-21 AND 51-40-00.

Part: FAIRING — DELAMINATED (LT WING) · airframe 45,828 hrs · 19,472 cycles

LEFT NR 3 FLAP TRACK MOVABLE FAIRING HAS TWO AREAS OF DELAMINATED. REMOVED DAMAGE AND BONDED REPAIR PLIES PER SRM 57-20-35 AND PAINTED PER SRM 51-75-10.

Part: BRACKET — GOUGED (THRUST REVERSER) · airframe 45,828 hrs · 19,472 cycles

EXHAUST NR 1 ENGINE LT T/R, FWD LATCH MOUNT BRACKET GOUGED. COMPLIED WITH EA NR 6-7830-110747 EXHAUST NR 1 ENGINE LT TR-FWD LATCH MOUNT BRACKET GOUGED. COMPLIED WITH EA NR 6-7830-110747 EXHAUST NR 1 ENGINE LT TR, FWD LATCH MOUNT BRACKET GOUGED.

Part: BRACKET — GOUGED (THRUST REVERSER) · airframe 45,828 hrs · 19,472 cycles

NR 2 ENGINE LT T/R FWD LATCH MOUNT BRACKET GOUGED. COMPLIED WITH EA NR 6-7830-110748 EXHAUST, NR 2 ENGINE LT TR FWD LATCH MOUNT BRACKET GOUGED. COMPLIED WITH EA NR 6-7830-110747 EXHAUST, NR 1 ENGINE LT TR-FWD LATCH MOUNT BRACKET GOUGED.

Part: DOOR — DELAMINATED (RT MLG) · airframe 45,828 hrs · 19,472 cycles

RT GEAR DOOR EXTERIOR SURFACE HAS AN AREA OF DELAMINATION APPROX 6" IN DIAMETER IN THE CENTER OF THE COMPOSITE FAIRING, AREA MARKED. REMOVED DAMAGE SKIN IAW SRM 51-77-10. CLEANED AND PREPPED DAMAGE AREA IAW SRM 51- 70-10 MIXED RESIN, FABBED REPAIR PLIES, MIXED BONDING RESIN AND BONDED PLIES IAW SRM 51-7710. APPLIED PRIMER IAW SRM 51-77-10 AND PAINTED REPAIR AREA IAW SRM 51-75-10.

Part: SKIN — DELAMINATED (RT ELEVATOR) · airframe 45,828 hrs · 19,472 cycles

RT ELEV L/E 3" FROM I/B EDGE HAS DELAM. REMOVED RT ELEV I/B TIP IAW MM 55-24-11-4. REPAIRED TIP IAW SRM 55-24-11,RE-INSTALLED TIP IAW MM 55-24-11-4.

Part: SKIN — DELAMINATED (LT ELEVATOR) · airframe 45,828 hrs · 19,472 cycles

LT ELEVATOR L/E 3" FROM I/B EDGE HAS DELAMINATED. REMOVED AND INSTALLED LT ELEVATOR I/B TIP IAW MM 55-24-11-4. REPAIRED TIP IAW SRM 55-24-11.

Part: PANEL — CRACKED (LT WING) · airframe 45,828 hrs · 19,472 cycles

LEFT WING LEADING EDGE LOWER SURFACE ACCESS PANEL 524 EB LAND AREA HAS CRACK LENGTH 1.300 IN WS 1403. FABRICATED DOUBLERS FROM 6061-T6 .063 AND 6061-T6 .071C IAW SRM 57-41-12, SRM 51-71-30, SRM 51-71-40. LOCATED AND DRILLED IAW SRM 51-40-44. INSTALLED DOUBLERS IAW SRM 51-40-21.

Part: BRACKET — CRACKED (NR 1 PYLON) · airframe 45,828 hrs · 19,472 cycles

PYLON NR 1 AT AFT T/E LOWER SECTION LOWER FAIRING INNER "A" FRAME SUPPORT BRACKET HAS A CRACK (APPROX 3" LONG) VISIBLE THRU OPEN ACCESS NR 474DR AND BETWEEN RIB 20-21 THRU LIGHTENING HOLE. REMOVED AND REPLACED WEB IAW SRM 51-40-21. LOCATED AND DRILLED IAW SRM 51-40- 44, FABBED WEB ON MAE TRAVELER NR T7/678060.

Part: FAIRING — CRACKED (NR 1 PYLON) · airframe 45,828 hrs · 19,472 cycles

NR 1 PYLON TO NACELLE FILLET FAIRING IS CRACKED LENGTH 2.5 IN LT SIDE STA 683/RIB6. INSTALLED NEW FILLET FAIRING IAW SRM 51-40-21.

Part: SKIN — DENTED (FUSELAGE) · airframe 45,828 hrs · 19,472 cycles

LOWER EXTERNAL FUSELAGE SKIN HAS DENT BETWEEN FR 67 TO FR68 STRG 53R TO STRG 54R APPROX 4" REPAIRED IAW SRM 53-10-12 FIG. 225

Part: SKIN — DENTED (FUSELAGE) · airframe 45,828 hrs · 19,472 cycles

LOWER EXTERNAL FUSELAGE SKIN HAS CREASE BETWEEN FR 66 TO FR 67 AND STGR 52R TO STGR 54R APPROX 6 IN CREASE ON FUSELAGE SKIN FOUND TO BE OUT OF LIMIT IAW SRM 53-10-12 FIG 110. REMOVED DAMAGED AREA IAW SRM 53-10-12, FABBED DOUBLER REPAIR MATERIAL/2024-T3 .100C BATCH NR 251819 IAW SRM 53-10-12 FIG 226, 224 SRM 53-17-12 FIG 3 SHEET 8. INSTALLED DOUBLER REPAIR IAW SRM 53-10-12 FIG 226.

Part: INDICATOR — MALFUNCTIONED (AIRSPEED) · airframe 43,583 hrs · 18,290 cycles

REJECTED TAKE OFF, CAPT'S AIRSPEED READ 100 KTS, FO STILL BELOW 80. REJECT NORMAL. PUMPED UP BOTH FO AND CAPT AIRSPEED WITH TEST BOX. FO LAGGED BEHIND CAPT. REMOVED AND REPLACED ADC 2 PER AMM 34-11-34-4. TESTED FO AIRSPEED INDICATOR WITH TEST BOX PER AMM 34-13-00-0. OPS CHECKS NORMAL. BLEW OUT FO PITOT SYSTEM WITH DRY NITROGEN PER AMM 34-10-00-3. NO DEBRIS FOUND. AIRCRAFT OK FOR SERVICE. PREMATURE REMOVAL/INSTALLATION .