N235FE

Part: BULKHEAD WEB — MISINSTALLED (ZONE 100) · airframe 74,865 hrs · 47,295 cycles

BS 1183 BULKHEAD WEB HAS INSUFFICIENT FASTENER SPACING AT LBL 12. REPAIRED ON NR N00736 AND EA 7-5310-143956.

Part: SEAT TRACK — CORRODED (BS 950D) · corrosion level 2 · airframe 74,865 hrs · 47,295 cycles

SEAT TRACK IS CORRODED AT BS 950D, RBL 25. REMOVED SEAT TRACK SECTION RBL 25 FROM BS 950 PLUS 10" TO BS 950F PLUS 10" IAW SRM 53-10-5 , FABRICATED NEW SEAT TRACK SECTION FROM 7178T6 IAW SRM 53-10-2, FIG 7 & SRM 51-30-2. INSTALLED NEW SEAT TRACK SECTION IAW SRM 51-30-2.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 74,865 hrs · 47,295 cycles

LT INBD MID FLAP L/E AREA HAS DENT AT WBL 95, WS 194. FOUND OUT OF LIMITS IAW SRM 57-50-1, FIG 3, CUT-OUT DAMAGE AND FABRICATED REPAIR DOUBLER AND FILLER IAW SRM 57-50-4, FIG 2 & 57-50-2, FIG 3, INSTALLED REPAIR FILLER AND DOUBLER AT LT INBD MID FLAPS L/E SKIN AT WBL 95, WS 194 IAW SRM 57-50-4, FIG 2 & 51-30-2 & EA 7-5750-143960.

Part: SKIN — GOUGED (BS 620-640) · airframe 74,865 hrs · 47,295 cycles

SKIN GOUGED SEVERAL PLACES AROUND CARGO DOORWAY BS 620 TO 640, STR 5L TO 16L. REPAIRED IAW SRM 51-30-2 & EA 7-5330-143955 .

Part: SKIN — DENTED (AIRSTAIR DOOR) · airframe 74,865 hrs · 47,295 cycles

AFT AIRSTAIR SKIN HAS DENT ON RT SIDE BS 1296. CUT OUT DAMAGED AREA IAW SRM 52-10-2, FIG 3. FABRICATED DOUBLER AND FILLER IAW SRM 52-10-2, FIG 3 INSTALLED REPAIR DOUBLER AND FILLER IAW SRM 52-10-2, FIG 3.

Part: SKIN — DENTED (AIRSTAIR DOOR) · airframe 74,865 hrs · 47,295 cycles

AFT AIRSTAIR SKIN HAS DENT ON RT SIDE BS 1283. CUT OUT DAMAGED AREA IAW SRM 52-10-2, FIG 3. FABRICATED DOUBLER AND FILLER IAW SRM 52-10-2, FIG 3. INSTALLED REPAIR PARTS IAW SRM 52-10-2, FIG 3.

Part: SKIN — DENTED (AFT AIR STAIR DO) · airframe 74,865 hrs · 47,295 cycles

AFT AIRSTAIR SKIN HAS PROTRUDING DENT ON RT SIDE BS1323 CUT OUT DAMAGED AREA AT AFT AIRSTAIR SKIN, RT SIDE BS 1323 IAW SRM 52-10-2, FIG 3. FABRICATED DOUBLER REPAIR IAW SRM 52-10-2, FIG 3 AND 52-10-1, FIG 3. INSTALLED DOUBLER REPAIR IAW SRM 52-10-2, FIG 3.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 74,865 hrs · 47,295 cycles

LEFT WING OTBD MIDFLAP HAS A DENT ON LOWER SURFACE OF L/E, 15" FROM OTBD END OF FLAP. CUTOUT DAMAGED AREA IAW SRM 57-50-4, FIG 2. FABRICATED DOUBLER AND FILLER IAW SRM 57-50-4, FIG 2. INSTALLED DOUBLER, FILLER AND FASTENERS IAW SRM 57-50-4, FIG 2 & EA 7-5750-143958.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 74,865 hrs · 47,295 cycles

LEFT INBD T/E MIDFLAP TOP AREA INBD SIDE HAS THREE DENTS. FOUND OUT OF LIMITS IAW SRM 57-50-1, FIG 3, CUT-OUT DAMAGE AND FABRICATED REPAIR DOUBLER AND FILLER IAW SRM 57-50-4, FIG 2 & 57-50-2, FIG 3, INSTALLED REPAIR FILLER AND DOUBLER AT LT INBD MID FLAPS L/E SKIN AT WBL 95, WS 240 IAW SRM 57-50-4, FIG 2 & 51-30-2 & EA 7-5750-143960.

Part: SHEAR TIE — CORRODED (BS 1148) · corrosion level 2 · airframe 74,865 hrs · 47,295 cycles

AFT CARGO PIT BILGE SHEAR TIE CORRODED BS 1148, LBL 2. REMOVED CORROSION IAW B727 SRM 51-10-6, C/W U.T. THICKNESS IAW SRM NDTM PT 4, 51-00-00 FIG 2. ORIGINAL: .063, REMAINING .043, MATERIAL LOS .020, FOUND OUT OF LIMITS IAW SRM 53-10-1 FIG 1. CUTOUT DAMAGE AREA DIM: 4" X 1" IAW SRM 53-10-4 FIG 15, FORMED REPAIR ANGLE IAW 53-10-4 FIG 15 & 51-20-1 FIG 7 ( DIM: 4" X 3"), HEAT TREATD TO T6 IAW FAS ENGINEERING REPORT 2-37153-001 REV A. TREATED AND PRIMED IAW SRM 51-10-2 & INSTALLED IAW SRM 51-30-2.

Part: BULKHEAD WEB — DAMAGED (BS 1183) · airframe 74,865 hrs · 47,295 cycles

FOUND AFT AIRSTAIR UPPER HORIZ SUPPORT ANGLE FASTENERS WITH NO ED AT BS 1183 BULKHEAD JUST BELOW THE AFT ENTRY DOOR DURING ACCESS TO VERT BEAM REPAIR. REMOVED SUPPORT WEB, FABRICATED NEW WEB, TREATED & PRIMED AND INSTALLED IAW SRM 51-30-2, SRM 51-10-2, & EA 7-5310-143956, SECTION 2. TRIMMED OUT DAMAGE HORIZ CHORD ANGLE, NDT INSPECTED AREA, FABRICATED REPAIR PARTS, TREATED & PRIMED & INSTALLED AT AFT AIRSTAIRS UPPER HORIZ SUPPORT ANGLE BS 1183 BULKHEAD IAW SRM 51-30-2, SRM 51-10-2 AND EA 7-5310-143956, FUSELAGE AD 98-11-03R1, BS 1183 BULKHEAD WEB WITH INSUFFICENT FASTENER SPACING AT LBL 12, SECTION 3.

Part: SEAT TRACK — CORRODED (BS 760-849) · corrosion level 2 · airframe 74,865 hrs · 47,295 cycles

CORROSION ON SEAT TRACK FLANGE BS 760-849 LBL 45. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 53-10-1, FIG 8, REMOVED SEAT TRACK SECTION AND SUPPORT IAW SRM 53-30-2, FABRICATED NEW SUPPORT IAW SRM 53-10-2, FIG 7 & SRM 51-30-5, INSTALLED NEW SUPPORT AND SEAT TRACK IAW SRM 51-30-2.

Part: VERTICAL BEAM — DAMAGED (BS 1183) · airframe 74,865 hrs · 47,295 cycles

FOUND FASTENERS WITH SHORT EDGE DISTANCE AT BS 1183 BULKHEAD VERTICAL BEAM LBL 26.83 AFTER PAINT AND CORROSION REMOVAL. ACCOMPLISHED REPAIR IAW EA 7-5310-143956. ORIGINAL SUBMISSION 12/01/2011

Part: SKIN — DENTED (BS 1348) · airframe 74,865 hrs · 47,295 cycles

LT SIDE OF FUSELAGE DENTED AT BS 1348, STRINGER 23L TO 26L. CUT OUT DAMAGED AREA IAW SRM 54-30-3 FIG 7. FABRICATED DOUBLER REPAIR IAW SRM 54-30-3 FIG 7 AND 54-30-2 FIG 4. TREATED AND PRIMED DOUBLER IAW SRM 51-10-2. INSTALLED COUNTERSINK WASHERS IAW SRM 51-30-8. INSTALLED DOUBLER REPAIR IAW SRM 54-30-3 FIG 7 REV 103.

Part: VERTICAL BEAM — CORRODED (BS 1183) · airframe 74,865 hrs · 47,295 cycles

AFT PIT, STA 1183 BULKHEAD LBL 26.8 VERTICAL BEAM CHORD HAS CORROSION. REMOVED CORROSION FROM VERTICAL BEAM IAW SRM 51-10-6 & EA 7-5310-143956, ORIGINAL THICKNESS .200 MATERIAL REMAINING .174, FOUND MATERIAL LOSS OF .026 TO BE WITHIN LIMIT IAW EA 7-5310-143956, SECTION 6, TREATED AND PRIMED AREA IAW SRM 51-10-2.

Part: SKIN — GOUGED (RT WING TE FLAP) · airframe 74,865 hrs · 47,295 cycles

RIGHT WING OTBD FOREFLAP L/E SKIN GOUGED IN 2 PLACES ABOVE NR 7 FLAP CARRIAGE. REPAIRED IAW SRM 57-50-2, FIG 4 & SRM 57-50-4, FIG 1 & EA 7-5750-143963.

Part: VERTICAL BEAM — CORRODED (BS 1183) · corrosion level 2 · airframe 74,865 hrs · 47,295 cycles

AFT PIT, BS 1183 BULKHEAD VERTICAL BEAM AT BL 0 HAS CORROSION AT BOTTOM. CUTOUT DAMAGE AREA IAW SRM 51-40-2, FIG 2. FABRICATED REPAIR PARTS IAW SRM 51-40-2, FIG 2. INSTALLED REPAIR PARTS 3 EA PLATES & STRUCTURAL FILLERS IAW SRM 51-40-4, FIG 2.

Part: VERTICAL BEAM — CORRODED (BS 1183) · corrosion level 2 · airframe 74,865 hrs · 47,295 cycles

AFT PIT, BS 1183 BULKHEAD RBL 26.8 VERTICAL BEAM CHORD HAS CORROSION AT FORWARD SIDE. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 53-10-1, FIG 1, CUTOUT DAMAGE AND FABRICATED REPAIR FILLER (1 EA) AND 3 EA. REPAIR ANGLES IAW SRM 51-40-4, FIG 2 & SRM 53-10-2, FIG 5, TREATED AND PRIMED AND INSTALLED REPAIR PARTS AT AFT PIT BS 1183 BULKHEAD RBL 17 VERTICAL BEAM CHORD IAW SRM 51-30-2, SRM 51-10-2, & SRM 51-40-4, FIG 2.

Part: SKIN — DAMAGED (LT WING TE FLAP) · airframe 74,865 hrs · 47,295 cycles

LEFT TE FLAP LE HAS LARGE CREASED AREA TOP SIDE. REMOVED DAMAGE AREA SKIN AND CORE ON LT INBD T/E L/E, FABRICATED, HOT BONDED CORE AND DOUBLER REPAIRS, CLEANED, SEALED, & FINISHED IAW SRM 51-40-20 & EA 7-5750-143964.

Part: SHEAR TIE — CORRODED (BS 700) · corrosion level 2 · airframe 74,865 hrs · 47,295 cycles

CORROSION ON SHEAR TIE AT AFT SIDE OF BS 700, BETWEEN STRINGER 27L AND 28L. REMOVED DAMAGED SHEAR TIE IAW SRM 51-30-2. FABRICATED SHEAR TIE IAW SRM 53-10-4 FIG 15. INSTALLED NEW SHEAR TIE IAW SRM 53-10-4 FIG 15.

Part: STRINGER — CORRODED (BS 1020 S30L) · corrosion level 2 · airframe 74,865 hrs · 47,295 cycles

CORROSION ON STRINGER 30L BS 1020. CUT OUT DAMAGED STRINGER 46 INCHES IN LENGTH IAW SRM 53-10-3 FIG 1. FABRICATED STRINGER REPAIR HATS AND SPLICES IAW SRM 53-10-3 FIG 1, AND 53-10-2 FIG 9. INSTALLED REPAIR HATS AND SPLICES IAW SRM 53-10-3 FIG 1 AND 51-30-2.

Part: SEAT TRACK — CORRODED (BS 849-870) · corrosion level 2 · airframe 74,865 hrs · 47,295 cycles

CORROSION ON SEAT TRACK BS 849 - 870, RBL 25. REMOVED SEAT TRACK SECTION, REMOVED CORROSION, AREA FOUND TO BE OUT OF LIMITS, FABRICATED NEW SEAT TRACK SECTION, TREATED AND PRIMED, INSTALLED IAW SRM 51-30-2, 51-10-6, 53-10-1 FIG 1, 53-10-2 FIG 7.

Part: SHEAR TIE — DAMAGED (BS 950E S28-29R) · airframe 74,865 hrs · 47,295 cycles

AFT CARGO BAY BILGE AREA, SHEAR TIE DAMAGED BS 950E BETWEEN S28-29R. REMOVED SHEAR TIE IAW SRM 51-30-02. FABRICATED NEW SHEAR TIE IAW SRM 53-10-4 FIG 15. INSTALLED NEW SHEAR TIE IAW SRM 51-30-02 AND 53-10-4 FIG 15.

Part: SHEAR TIE — CORRODED (BS 720E S27-28L) · corrosion level 2 · airframe 74,865 hrs · 47,295 cycles

CORROSION ON SHEAR TIE AT BS 720E BETWEEN STRINGER 27L AND 28L. REMOVED, FABRICATED AND INSTALLED SHEAR TIE IAW SRM 53-10-4 FIG 13 .

Part: STRUCTURE — CRACKED (RT WING TE FLAP) · airframe 74,865 hrs · 47,295 cycles

RT WING INBD MID FLAP T/E CHORD CRACKED AT INBD FLAP CONTROL DRUM, WBL 100. REMOVED MID FLAP T/E CHORD IAW SRM 51-30-2. LOCATED AND DRILLED NEW CHORD IAW SRM 57-50-2, FIG 5 AND INSTALLED NEW CHORD SECTION, USED PREVIOUS REPAIR IAW SRM 57-50-2, FIG 5 & EA 7-5750-143959.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 74,865 hrs · 47,295 cycles

CORROSION ON SEAT TRACK FLANGE SPLICE BS 849 - 870, LBL 45. REMOVED CORROSION, AREA FOUND TO BE OUT OF LIMITS. FABRICATED NEW SEAT TRACK SECTION, TREATED AND PRIMED AND INSTALLED IAW SRM 51-30-2, 53-10-1, 51-10-6, 53-10-02 FIG 7 AND 51-10-2.

Part: STRINGER — CORRODED (BS 720F-740) · corrosion level 2 · airframe 74,865 hrs · 47,295 cycles

STRINGER 26L BS 720F-740 CORRODED. CUT OUT DAMAGED AREA IAW B727 SRM 53-10-3 FIG 1. FABRICATED REPAIR PARTS IAW SRM 53-10-3 FIG 1 AND 53-10-2 FIG 9. INSTALLED REPAIR PARTS IAW SRM 51-30-2 AND 53-10-3 FIG 1

Part: STRINGER — CORRODED (BS 720F-740) · corrosion level 2 · airframe 74,865 hrs · 47,295 cycles

STRINGER 26R CORRODED BETWEEN BS 720F - 740. CUT OUT DAMAGED STRINGER IAW SRM 53-10-3, FIG 1. FABRICATED REPAIR PARTS IAW SRM 53-10-3, FIG 1 AND 53-10-2, FIG 9 INSTALLED REPAIR PARTS IAW SRM 53-10-3, FIG 1 AND 51-30-02.

Part: SHEAR TIE — CORRODED (BS 720C) · corrosion level 2 · airframe 74,865 hrs · 47,295 cycles

CORROSION ON SHEAR TIE AT BS 720C, BETWEEN STRINGER 27-28L. REMOVED DAMAGED SHEAR TIE IAW SRM 51-30-2 FABRICATED NEW SHEAR TIE AND INSTALLED IAW SRM 53-10-4 FIG 13.

Part: LATCH — OUT OF ADJUST (PAX DOOR) · airframe 74,736 hrs · 47,197 cycles

MAIN ENTRY DOOR POPPED OPEN ON LANDING. FOUND DOOR LATCH ARM HAS SOFT UNLATCHING. PERFORMED FORWARD ENTRY DOOR - ADJUSTMENT/TEST IAW MM 52-11-001-5, PARAGRAPH 3 & 4. DOOR OPS CHECK GOOD. FINAL CLOSED.

Part: SLIDE — DISLODGED (PAX DOOR) · airframe 74,731 hrs · 47,193 cycles

RAFT FELL OUT OF MAIN ENTRY DOOR COMPARTMENT IN FLIGHT, R & R MAIN SLIDE RAFT IAW MM 25-60-015-2-0.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 74,715 hrs · 47,176 cycles

15 INCHES BELOW THE OUTFLOW VALVE, NEAR STA 1183, 2 EACH FASTENER HEADS SHEARED OFF AND NUMEROUS OTHERS AROUND THEM ARE CRACKED. REPAIRED AREA BY COMPLING WITH EA 7-5330-152417 (SEQ 9, WO 00052855). NO OTHER ACTION REQUIRED.

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 74,715 hrs · 47,176 cycles

FOUND CORROSION IN THE SKIN AT BS 1167-1181 STR 27R. COMPLIED WITH EA 7-5330-152417 BY TRIMING OUT THE SUBJECT SKIN AND INSTALLED A REPAIR DOULBER AND STRUCTURAL FILLER.

Part: TIE — CORRODED (VERTICAL STAB) · airframe 67,894 hrs · 42,042 cycles

CORROSION VERTICAL STAB TENSION TIE RT FWD VERTICAL BOLT HOLE AIRCRAFT AND TENSION TIE. *S/D* REPAIRED PER EA 7-5530-86241.

Part: SHEAR TIE — DAMAGED (FUSELAGE) · airframe 67,894 hrs · 42,042 cycles

REPAIR SHEAR TIE AT BS 380 BETWEEN STR 15 AND 16 LT TO COMPLY WITH FED EX EO 7-5340-5002 P1. *S/D* REPAIRED PER SRM 51-20-1, 51-20-4, 51-30-2.

Part: TIE — CORRODED (VERTICAL STAB) · airframe 67,894 hrs · 42,042 cycles

CORROSION VERTICAL STAB TENSION TIE RT AFT VERTICAL BOLT HOLE AIRCRAFT AND TENSION TIE. *S/D* REPAIRED PER EA 7-5530-86241.

Part: TIE — CORRODED (VERTICAL STAB) · airframe 67,894 hrs · 42,042 cycles

CORROSION VERTICAL STAB TENSION TIE LT FWD VERTICAL BOLT HOLE AIRCRAFT AND TENSION TIE. *S/D* REPAIRED PER EA 7-5530-86241.

Part: TIE — CORRODED (VERTICAL STAB) · airframe 67,894 hrs · 42,042 cycles

CORROSION VERTICAL STAB TENSION TIE LT AFT VERTICAL BOLT HOLE AIRCRAFT AND TENSION TIE. *S/D* REPAIRED PER EA 7-5530-86241.

Part: SHEAR TIE — DAMAGED (FUSELAGE) · airframe 67,894 hrs · 42,042 cycles

REPAIR SHEAR TIE AT BS 380 BETWEEN STR 14 AND 15 TO COMPLY WITH FED EX EO 7-5340-7--5002 P1. REPAIRED PER SRM 51-20-1, 51-20-4, 51-30-2.

Part: SKIN — GOUGED (FUSELAGE) · airframe 67,894 hrs · 42,042 cycles

WHILE WORKING ROUTINE CARD 7-5330-2342 P1 FOUND GOUGE IN FUSELAGE SKIN CROWN AREA BS 1061 BETWEEN STR 1R & 2R, 35 INCHES FWD OF S-DUCT HOUSING L/E. *S/D* GOUGE FOUND TO BE OUT OF LIMITS, REPAIRED AREA PER SRM 53-30-3.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 67,894 hrs · 42,042 cycles

STR 27R BS 735 WL 145 IS CRACKED. REPAIRED PER SRM 53-10-3.

Part: BULKHEAD — CORRODED (FUSLEAGE) · airframe 67,894 hrs · 42,042 cycles

BS 740 RBL 8 WL 148 CORROSION AFT SIDE OF BULKHEAD. FOUND CORROSION OUT OF LIMITS PER SRM 53-10-1 REPLACED SUPPORT DOUBLER PER EA 7-5310-86238 AND SRM 51-30-2, 51-10-2 & 51-40-2.

Part: STRINGER CLIP — GOUGED (FUSELAGE) · airframe 67,894 hrs · 42,042 cycles

GOUGE ON LOWER SURFACE OF STR 6L, STRINGER SPLICE BS 951. REPLACED PER SRM 51-30-2 AND 53-10-1

Part: STRINGER — CRACKED (VERTICAL STAB) · airframe 67,894 hrs · 42,042 cycles

STRINGER CRACKED IN VERTICAL FIN AT VERT FIN STA 110.4 STRINGER 7 LEFT. *S/D* REPAIRED PER SRM 55-30-4.

Part: FRAME — DENTED (FUSELAGE) · airframe 67,894 hrs · 42,042 cycles

BS 680, LBL 35, WL 162, DENT ON FRAME. REPAIRED PER SRM 51-40-3.

Part: FRAME — DENTED (FUSELAGE) · airframe 67,894 hrs · 42,042 cycles

BS 500, RBL 35, WL 161 DENT ON FRAME. REPAIRED PER SRM 53-10-1, 51-40-3

Part: STRINGER — CRACKED (VERTICAL STAB) · airframe 67,894 hrs · 42,042 cycles

STRINGER CRACKED IN VERTICAL FIN AT FIN STA 180.6 STRINGER 3 LEFT. *S/D* FABRICATED AND INSTALLED REPAIR PARTS PER SRM 55-30-4 FIG 1.

Part: FRAME — DENTED (FUSELAGE) · airframe 67,894 hrs · 42,042 cycles

BS 1030 STR 25L FRAME DENTED. REPAIRED PER SRM 51-40-3.

Part: FRAME — DENTED (FUSELAGE) · airframe 67,894 hrs · 42,042 cycles

BS 720A, LBL 34, WL 167 DENT ON FRAME. REPAIRED FRAME BS 702A, LBL 36 PER SRM 53-10-1.

Part: FRAME — DENTED (FUSELAGE) · airframe 67,894 hrs · 42,042 cycles

BS 1030, STR 25R FRAME IS DENTED. REPAIRED PER SRM 51-40-3.

Part: FRAME — DENTED (FUSELAGE) · airframe 67,894 hrs · 42,042 cycles

FRAME HAS TWO DENTS WITHIN 10 INCHES OF EACH OTHER BS 1110 BELOW STR 25R AND AT STR 26R. REPAIRED PER SRM 53-40-2

Part: FRAME — DENTED (FUSELAGE) · airframe 67,894 hrs · 42,042 cycles

DENT IN FRAME BS 1070 JUST BELOW STR 25R. REPAIRED PER SRM 53-10-2

Part: FRAME — DENTED (FUSELAGE) · airframe 67,894 hrs · 42,042 cycles

BS 720, RBL 39, STR 24, WL 163 FRAME DENTED. REPAIRED FRAME AT BS 720, STR 24, RBL 39, WL 163 PER SRM 51-40-3.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 67,894 hrs · 42,042 cycles

MAIN CARGO DOOR CUTOUT DOUBLER, FASTENER HOLE DOUBLE DRILLED, BS 675 STR 26L. REPAIRED PER SRM 53-10-3.

Part: FLOORBEAM — DAMAGED (FUSELAGE) · airframe 67,894 hrs · 42,042 cycles

REPAIR ON FLOORBEAM UPPER CORD BS 344, WL 208, LBL 20.5 TO RBL 70, 90.5 INCHES LONG NEEDS EVALUATION TO DETERMINE PER SRM OR APPROVED DATA . REMOVED AND REPLACED FLOORBEAM UPPER CHORD BS 344, WL 208, LBL 65 TO RBL 65 IAW SRM 51-30-2 & 53-10-8

Part: SKIN — DAMAGED (RUDDER) · airframe 67,894 hrs · 42,042 cycles

SHARP CREASE ON LOWER RUDDER, LEFT HAND SIDE TOWARDS THE BOTTOM. REPLACED LOWER RUDDER PER MM 27-20-001.

Part: STRINGER — CORRODED (FUSLEAGE) · airframe 67,894 hrs · 42,042 cycles

BS 640, RBL 15 WL 154 CORROSION ON STRINGER. REPAIRED PER SRM 53-10-3

Part: STRINGER — CORRODED (FUSELAGE) · airframe 67,894 hrs · 42,042 cycles

BS 720D PLUS 18, STR 23R STRINGER CORROSION. REMOVED & FABRICATED NEW STRINGER AND 2 HAT CHANNELS SRM 53-10-2, 51-30-2.

Part: STRINGER — CORRODED (N/A) · airframe 67,894 hrs · 42,042 cycles

BS 720E PLUS 12 - BS, STR 23R CORROSION. CORROSION 100 PERCENT IN MATERIAL REMOVED AND REPLACED STRINGER PER SRM 53-10-2 AND 51-10-2.

Part: SKIN — GOUGED (FUSELAGE) · airframe 67,894 hrs · 42,042 cycles

EXTERNAL SKIN GOUGED AT LAP SPLICE, BS 337, RT SIDE, 21 INCHES O/B OF NOSE WHEEL WELL CUTOUT. *S/D* REPAIRED SKIN DAMAGE PER SRM 53-30-3.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 67,894 hrs · 42,042 cycles

BS 675, STR 27R CORROSION ON STRINGER. *S/D* REPAIRED PER SRM 53-10-3.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 67,894 hrs · 42,042 cycles

BS 720F, STR 23R STRINGER CORROSION (C53-111-01). *S/D* CORROSION 100 PERCENT IN MATERIAL REMOVED AND REPLACED STRINGER PER SRM 53-10-2 & 51-30-2.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 67,894 hrs · 42,042 cycles

BS 720A, RBL 25, WL 153 SHEAR TIE CORROSION. REPAIRED PER SRM 53-10-4.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 67,894 hrs · 42,042 cycles

CORROSION ON CREASE BEAM BS 450, RBL 60, WL 208. *S/D* REPAIRED IAW SRM 53-10-1.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 67,894 hrs · 42,042 cycles

BS 720C, STR 28L - STR 27L CORROSION ON SHEAR TIE. *S/D* REPAIRED SHEAR TIE PER SRM 53-10-4.

Part: KEELBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,894 hrs · 42,042 cycles

BS 950A+8 RBL 8 CORROSION ON KEELBEAM. REPAIRED PER FED EX SR DRAWING NR SR27-53-023 REV A

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,894 hrs · 42,042 cycles

BS 1148 CORROSION ON SHEAR TIE AND SKIN BS 1148 BETWEEN STRINGERS 28R & 29R. REMOVED CORROSION SHEAR TIE FOUND TO BE OUT OF LIMITS PER SRM 53-10-1 REPAIRED PER SRM 53-10-04.

Part: PROBE — CONTAMINATED (NR 1 ENGINE) · airframe 66,971 hrs · 41,313 cycles

DURING T/O, NR 1 ENG INDICATED LOW N1 RPM (APPROX 80 PERCENT) WHEN STD EPR SET. ABORTED T/O AT APPROX 90 KTS, 138400 LBS, 600 FT PA, -3 DEGREES C. RAN ALL APPROPRIATE CHECKLISTS AND AFTER COORDINATION WITH GROUND CONTROL RAN UP NR 1 ENG. DURING RUN-UP NR 1 ENG RAN NORMAL. DUE TO CREW INFO ABOVE, A/C DID MAKE POWER ON 2ND ATTEMPT. A/C SAT TODAY IN FREEZING RAIN. SUSPECT ICE ON EPR PROBE. INSPECTED INLET AND EXHAUST FOR ICE DAMAGE, NONE FOUND. CREW RUN ENGINE AGAIN TO VERIFY N1 GAUGE IS WORKING CORRECTLY. ALL INDICATIONS NORMAL ON ENG RUN. REQUIRED BRAKE COOLING TIME WAS ACCOMPLISHED. A/C OK TO CONTINUE.

Part: INDICATOR — FAULTY (MLG)

AFT GEAR EXT AND THREE GREEN LIGHT ALL RED GEAR UNSAFE LIGHTS REMAIN ILLUM. RECYCLED GEAR AND GOT NORMAL IND AFT 2ND ATTEMPT. *S/D* REMOVED FOR ACCESS P/S LINES, RECONNECTED AND LEAK CK GOOD PER B727-200 MM 34-11-000-5.

Part: SLAT — FAILED (FLAP/SLAT SYSTEM)

ON FLAP RETRACT AFT T/O AT FLAP 2 DEG POS LED FAILED TO RETRACT. RED TAB PROC WOULD NOT CORRECT PROBLEM. *S/D* PERF OPS CK OF FLAPS AND LEAD EDGE CK GOOD PER B727-200 MM 27-82-000-0.

Part: ACCESSORY UNIT — INOPERATIVE (E/E BAY)

UPON LWR LAND GEAR GOT 3 GREEN AND RED NOSE GEAR RED LEFT GEAR, DOORS AND TAIL SKID LIGHT. RECYCLED GEAR UP. OK BACK DOWN WITH PROPER 3 GREEN IND. REMOVED AND REPLACED ELECTRONIC MODULE, PERF ADJUSTMENT/TEST PER MM 32-09-122. OPS CK OK.

Part: SWITCH — INOPERATIVE (MLG CONTROL)

ON LANDING GEAR EXT, LEFT MAIN AND NOSE GEAR RED UNSAFE LIGHTS ILLUM. REMOVED AND REPLACED CONTROL LEVER POSITION SWITCH. OPS CHECK NORM. CLEANED LEVER SO IT SLIDES EASIER INTO THE DOWNLOCK DETENT REF 727 MM 32-61-012-4.

Part: ACCESSORY UNIT — INOPERATIVE (E/E BAY)

ON GEAR EXT ALL 3 RED GEAR LIGHT REMAIN ILLUM. REMOVED AND REPLACED LAND ACCESSORY UNIT. PERF MM 32-09-122. CK OPS, CK. NO FAULTS FOUND ON GROUND. AC OK TO DEPART.

Part: FLOORBEAM — CORRODED (FUSELAGE)

NR 1156 WHILE WORKING CLOSE CARD FND CORROSION ON FLOORBEAM LOWER FLANGE AT BS 1130, RBL 5, WL 201 UNDER NUTCLIP. ** S/D ** R&R PER FEDEX SRM 53-10-1, 51-30-2, EA# 7-5310-50036A.

Part: SHEAR TIE — CORRODED (FUSELAGE)

CORROSION (C53-111-01) ON SHEAR TIE BS 950B, LBL 11, WL 138. *S/D* REMOVED AND REPLACED PER IAW FEDEX SRM 53-10-4, FIG 13, & FEDEX EA 7-5310-56037.

Part: SHEAR TIE — CORRODED (FUSELAGE)

CORROSION (C53-111-01) ON FWD AND AFT SIDE OF SHEAR TIE AT BS 970 JUST O/B OF STR 29L, WL 138. MARKED, IN AFT CARGO BAY. *S/D* REMOVED AND REPLACED PER IAW FEDEX SRM 53-10-4 FIG 13, FEDEX EA 7-5310-50037.

Part: SHEAR TIE — CORRODED (FUSELAGE)

CORROSION (C53-111-01) ON SHEAR TIE BS 950B, RBL 18, WL 138. *S/D* REMOVED AND REPLACED PER IAW FEDEX SRM 51-10-01, 51-30-03.

Part: FRAME — DAMAGED (FUSELAGE)

FOUND MECHANICAL DAMAGE TO FRAME BS 1110, STR 27 LT. *S/D* REMOVED AND REPLACED PER IAW FEDEX SRM 51-40-3, 7075T6.063 M NR 269280.

Part: STRINGER — CRACKED (FUSELAGE)

CRACKED STRINGER BS 343, STR 5R AT LAV WALL ATTACHMENT BRACKET.

Part: SPLICE — CORRODED (FUSELAGE)

CORROSION (C53-111-01) BS 1070 BETWEEN STR 24-25R ON FRAME SPLICE (MARKED).

Part: SKIN — DENTED (FUSELAGE)

EXTERIOR SECTION 48 DENT ON SKIN BS 1310, 19 INCHES ABOVE NR 3 ENGINE PYLON.

Part: SKIN — DENTED (FUSELAGE)

SKIN IS DENTED AT BS 1345, RBL 36, WL 224.

Part: FLOORBEAM — CORRODED (FUSELAGE)

CORROSION ON UPPER CHORD OF FLOORBEAM AT BS 1130, LBL 18.5, WL 208 (C53-224-01). *S/D* REMOVED AND REPLACED PER FEDEX 51-30-2, 51-20-4 SRM & FEDEX EA 7-5310-50036.

Part: FLOORBEAM — CORRODED (FUSELAGE)

CORROSION ON FLOORBEAM AT BS 1030, RBL 15, WL 208 (C53-224-01).

Part: STRINGER — CORRODED (FUSLEAGE)

CORROSION (C53-111-01) ON EXT SERVICE PAN AND STR BETWEEN BS 1070 - 1090, STR 23R (MARKED).

Part: SHEAR TIE — CORRODED (FUSELAGE)

CORROSION (C53-111-01) ON SHEAR TIE 950A, LBL 4, WL 108. *S/D* REMOVED AND REPLACED PER IAW FEDEX EA 7-5310-50037.

Part: FRAME — CRACKED (FUSELAGE)

FRAME CRACKED AT BS 660, RBL 33, WL 158.

Part: FRAME — DENTED (FUSELAGE)

BS 600 FRAME DENTED BETWEEN STR 221-24L.

Part: SHEAR TIE — CORRODED (FUSELAGE)

CORROSION (C53-111-01) ON SHEAR TIE 950B, LBL 18, WL 138. *S/D* FAB & INSTALLED PER IAW FED SRM 53-10-1, 53-10-04, 51-40-3 & FEDEX EA 7-5310-50037.

Part: FRAME — DENTED (FUSELAGE)

BS 580 FRAME DENTED IN 2 SPOTS AT STR 22L. *S/D* CUT OUT DAMAGE PER FEDEX SRM 51-40-03.

Part: SHEAR TIE — CORRODED (FUSELAGE)

CORROSION (C53-111-01) ON SHEAR TIE 950C, LBL 11, WL 138. *S/D* REPAIR IAW FEDEX SRM 53-10-4 FIG 13 & ER 00-5085.

Part: STRAP — CORRODED (FUSELAGE)

CORROSION (C53-224-01,2) AROUND FASTENERS RBL 45, BS 760, WL 206. *S/D* REMOVED AND REPLACED NEW STRAP PER FEDEX SRM 51-30-02.

Part: FLOORBEAM — CORRODED (FUSELAGE)

CORROSION AT FASTENER HOLES ON UPPPER CHORD OF FLOORBEAM BS 1050, RBL 35, WL 208 (C53-224-01). *S/D* REMOVED AND REPLACED PER IAW FEDEX SRM 53-10-8 FIG 8.

Part: KEELBEAM — CORRODED (FUSELAGE)

CORROSION ON KEEL BEAM BS 950F+16, RBL 6, WL 138. *S/D* REMOVED AND BLENDED, INSTALLED REPAIR STRAP PER FEDEX DG 27-53-023 & EA 7-5310-50017.

Part: SKIN — CORRODED (FUSELAGE)

FUSELAGE SKIN CORRODED AT BS 470 AT ATC ANTENNA MOUNTING LOCATON. *S/D* REMOVED DAMAGED SKIN PER FEDEX SRM 53-30-3 FIG 1.

Part: STRINGER — CORRODED (FUSELAGE)

CORROSION (C53-224-01, 2) CORROSION ON STRINGER 8 LT AT BS 783 TO 825. *S/D* ALODINED, PAINTED AND REPAIR PARTS PER IAW FEDEX 51-20-151, 51-30-2 & 53-10-3.

Part: SKIN — DENTED (FUSELAGE)

WHILE WORKING EO 7-5310-7-2301 C2 PT 1 FOUND DENT IN SKIN AT BS 1346, WL 200, LBL 36. *S/D* CUT OUT DAMAGE AREA AND FAB, ALODINED AND PRIMED PER FEDEX SRM 54-30-3 2024T3.

Part: SKIN — DENTED (FUSELAGE)

SKIN IS DENTED AT LT SKIN PANEL AT BS 1342, WL 235. *S/D* REWORKED DENT IAW FEDEX SRM 51-40-1, WITHIN LIMITS PER 53-30-1.

Part: SKIN — CORRODED (FUSELAGE)

OUTER SKIN BULGING AND POPPED FASTENER HEADS BS 950F+13, STR 28L. ** S/D ** R&R DAMAGE PER FEDEX SRM 53-10-3 FIG 1.

Part: INTERCOSTAL — CORRODED (FUSELAGE)

NR 1025 CORROSION ON INTERCOSTAL FLOOR SUPPORT AT BS 1105, RBL 11.5, WL 208 ( C53-224-01). ** S/D ** FAB, ALODINED & PRIMED INSTALL PER FEDEX SRM 51-10-1, 51-30-5, 51-30-6 AND 51-10-2.

Part: SEAT TRACK — CORRODED (BS 740 - 690)

CORROSION C53-224-01 ON SEAT TRACK BS 740-690, RBL 45, WL 208.

Part: FLOORBEAM — CORRODED (FUSELAGE)

CORROSION ON UPPER CHORD OF FLOORBEAM AT BS 1110, LBL 4 TO LBL 11, WL 208 (C53-224-01). ** S/D ** R&R DAMAGE AREA PER IAW FEDEX SRM 53-10-08.

Part: FLOORBEAM — CORRODED (FUSELAGE)

CORROSION (71C709-02) OF MAIN DECK FLOOR SUPPORT BEAM BETWEEN BS 1100 TO BS 1130, RBL 12, WL 208. VARIOUS LOCATIONS MARKED. *S/D* REMOVED AND REPLACED PER FEDEX SRM 51-10-6, 51-10-2, 51-20-1, 53-10-2.

Part: SKIN — CHAFED (BS 720D+13)

SKIN CHAFFED AT BS 720D PLUS 13 AT STR 20R.

Part: SKIN — CHAFED (BS 720D+12.5)

NR 300 - SKIN CHAFED AT BS 720D+12.5 AT STR 19 LT. REMOVED AND REPLACED PER FEDEX SRM 53-30-3 FIG 14. FILLET SEALED PER FEDEX SRM 51-20-4.

Part: SKIN — GOUGED (FUSELAGE)

EXTERIOR SECTION 48, HAS A GOUGE IN SKIN ATBS 1327 21 INCHES ABOVE AFT AIRSTAIR RT CUTOUT & DENT EXTEND APPROX 6 IN. AFT ** S/D ** REMOVED DAMAGE & FAB PER FEDEX SRM 53-30-3 FIG 1 & 53-30-1.

Part: STRINGER — CORRODED (FUSELAE)

CORROSION (C53-113-01(1)) ON STRINGER AT RBL 15, WL 150, BS 674. ** S/D ** R&R PER FEDEX SRM 53-10-1, 53-10-3.

Part: ACTUATOR — FAILED (LE SLAT)

99-186 - 'A' SYSTEM HYDRAULIC QUANTITY FELL TO ZERO. PRESSURE OK AT 3000 PSI. COMPLIED WITH LOSS OF 'A' SYSTEM RED TABLS. REMOVED AND REPLACED TWO WING PANELS AT LT NR 4 SLAT ACTUATOR. REMOVED AND REPLACED NR 4 LEADING EDGE SLAT ACTUATOR PER BOEING MM 27-81-32-4.

Part: SWITCH — INOP (LANDING GEAR)

99-184 - 1ST ATTEMPT TO LWR MLG RECEIVED LEFT AND NOSE UNSAFE IND, 2ND ATTEMPT ALL 3 MLG IND DOWN AND LOCKED. REMOVED AND REPLACED NOSE GEAR, LMG DOWN LOCK SENSOR,32-61-91, POSITION SWITCH PER MM 32-61-71.

Part: ADC — FAILED (E & E COMP)

98-246 ON CLIMB-OUT, LOST CAPT AIRSPEED CAPT ALT, GPWS, ALT ALERTER, TRANSPONDER NR 1, & MODE C IN BOTH TRANSPONDER & AUTOPILOT. REMOVED AND REPLACED DADC PER BOEING 727 MM CHAPTER 34-12-11. OPER CKS NORM. AUTOPILOT DOWNGRADED TO CK CAT 2 STATUS. A/C DOWNGRADED TO NOT CAT 2 STATUS.

Part: SWITCH — DIRTY (AFT AIRSTAIRS)

AFT AIRSTAIR LIGHT ILLUMINATED AT ROTATION AND STAYED LIGHTED. OPENED AFT AIRSTAIR, CLEANED SW, CYCLED STAIRS. OPS CK NORMAL.

Part: ACTUATOR — FAILED (NR 2 LE SLAT)

97-0256 AFTER TAKEOFF FLAPS WERE RETRACTED TO 0 DEG AND AMBER LE FLAPS LIGHT REMAINED ILLUMINATED ON FORWARD INSTRUMENT PANEL. S/O PANEL CONFIRMED NR 2 SLAT EXTEND. CYCLED FLAPS SEVERAL TIMES BOTH LIGHTS WOULD GO OUT MOMENTARY AND THEN REILLUMINATED. REF OIL NR 27-80-2061. REMOVED AND REPLACED NR 2 SLAT ACTUATOR PER M/M REF 27-81-32.

Part: DOUBLER — CRACKED (BS 1330)

CRACK IN HAT SECTION OF STR 13L AT BS 1330. STOP DRILLED CRACK AND INSTALLED 7075T-6 .063 DOUBLER.

Part: STRINGER — CORRODED (BS 730-734)

BS 730 TO 734 ON STRINGER 28 LT CORRODED. REMOVED CORROSION, TREATED AND PRIMED STRINGER. INSTALLED .050 7075T-6 STRAP PER EA 7-5310-29227.