N481FE

Part: RETAINER — CRACKED (GIRT BAR) · airframe 46,421 hrs · 30,099 cycles

GIRT BAR RETAINING CLIP BROKEN. PART NEEDED. REPLACED CLIP.

Part: WIRE HARNESS — SPARKS (WINDOW HEAT) · airframe 46,209 hrs · 29,927 cycles

NOTICED SPARKS COMING FROM WINDSHIELD HEAT SUPPLY WIRE NEXT TO CAPTAIN'S MIKE CONNECTOR. FOLLOWED QRH, PULLED WINDSHIELD HEAT C/B. REMOVED AND REPLACED WINDOW AND WIRE HARNESS IAW MM 56-12-011-4.

Part: SWITCH — OUT OF ADJUST (PAX DOOR) · airframe 46,160 hrs · 29,876 cycles

ON A TEST FLIGHT, AFT ENTRY DOOR LIGHT ON S/O PANEL COMES ON AFTER A NORMAL LANDING. ADJUSTED AFT ENTRY DOOR SWITCH TO ACTUATE AT APPROX 5 DEG OF HANDLE TRAVEL AND PERFORMED SATISFACTORY. OPS CHECKED IAW AMM 52-70-001-5.

Part: HINGE FITTING — CRACKED (FUSELAGE) · airframe 46,155 hrs · 29,864 cycles

EXTERIOR FUSELAGE AFT MOST FUSELAGE MOUNTED MAIN CARGO DOOR HINGE SEGMENT HAS CORNER CRACKED SECOND LUG FWD OF AFT END VERIFIED WITH HFEC. REMOVED CRACKED HINGE IAW SRM 51-30-2. FABRICATED AND INSTALLED NEW HINGE IAW DWG 52FX1433 REV E AND SRM 51-30-2.

Part: FLOOR SUPPORT — DAMAGED (BS 1148-1138) · airframe 46,155 hrs · 29,864 cycles

MISDRILLED AND ELONGATED FASTENER HOLES IN FLOOR SUPPORT WEB BS 1148 TO 1183 BL0. AREA OUT OF LIMITS IAW SRM 53-10-1, FIG 1. REMOVED DAMAGED WEB, FABRICATED NEW AND INSTALLED IAW DWG 65-19606 AND SRM 51-30-2.

Part: STRINGER — CORRODED (BS 950E-950F) · corrosion level 2 · airframe 46,155 hrs · 29,864 cycles

CORROSION ON STRINGER 29L FROM BS 950E TO 950F. FABRICATED REPAIR STRAP AND SHIM IAW EA 7-5310-143984. INSTALLED REPAIR STRAP IAW EA 7-5310-143984 AND SRM 51-30-02 REV 103.

Part: SEAT TRACK — CORRODED (BS 740-757) · corrosion level 2 · airframe 46,155 hrs · 29,864 cycles

CORROSION AROUND FASTENER ON FLOATING SEAT TRACK SUPPORT ANGLE, BS 740 RBL 25. FOUND CORROSION OUT OF LIMITS IAW SRM 53-10-1, FIG 3. REMOVED DAMAGED SEAT TRACK IAW SRM 51-30-2 AMD MM 20-80-01-002. FABRICATED NEW SEAT TRACK SECTION IAW DWG 69-4121. INSTALLED SECTION IAW SRM 51-30-2 AND MM 20-80-01-002.

Part: SKIN — DENTED (BS 238) · airframe 46,155 hrs · 29,864 cycles

SKIN DENTED STA 238 ABOVE STR 24R. FOUND OUT OF LIMITS IAW SRM 53-30-1, FIG 1. CUT OUT DAMAGED AREA, FABRICATED REPAIR DOUBLER AND STRAP AND INSTALLED IAW SRM 53-30-3, FIG 1.

Part: SHEAR TIE — CORRODED (BS 950E) · corrosion level 2 · airframe 46,155 hrs · 29,864 cycles

CORROSION ON STUB FRAME SHEAR TIE AT BS 950E PLUS 4 INCHES, AFT SIDE, BETWEEN STRINGERS 29 AND 30R. REMOVED SHEAR TIE IAW SRM 51-30-02. FABRICATED NEW SHEAR TIE IAW DWG NR 65-56129 AND SRM 51-30-05 AND 51-20-1, FIG 7 & INSTALLED IAW SRM 51-30-02, REV 103.

Part: SEAT TRACK — CORRODED (BS 1130-1176) · corrosion level 2 · airframe 46,155 hrs · 29,864 cycles

CORROSION ON SEAT TRACK BS 1130-1176 BL 0. CORROSION OUT OF LIMITS IAW SRM 53-10-1 FIG 3. REMOVED DAMAGED SEAT TRACK SECTION, FABRICATED NEW SECTION AND INSTALLED IAW SRM 53-10-2 FIG 7A, SRM 51-30-2 AND DWG 53FX939, REV F.

Part: SEAT TRACK — CORRODED (BS 1118) · corrosion level 2 · airframe 46,155 hrs · 29,864 cycles

MAIN CABIN SEAT TRACK CORRODED ON INBD FLANGE AT BS 1118, RBL 24.75. REMOVED DAMAGED SEAT TRACK SECTION, FABRICATED A NEW SECTION AND INSTALLED IAW SRM 53-10-5, FIG 1.

Part: STRINGER — CORRODED (BS 700 S27L) · corrosion level 2 · airframe 46,155 hrs · 29,864 cycles

CORRODED STRINGER 27L BS 700. CUT OUT DAMAGED SECTION OF STRINGER IAW SRM 51-10-1. FABRICATED NEW STRINGER SECTION AND 2 EACH STRINGER SPLICES IAW SRM 53-10-03 FIG 1. INSTALLED REPAIR IAW SRM 51-30-02 FIG 1 REV 103.

Part: WEB — DAMAGED (BS 1323) · airframe 46,155 hrs · 29,864 cycles

FOUND ELONGATED FASTENER HOLES IN AFT LOWER TORQUE BOX WEB BS 1323, LBL 17.5. WEB REPLACED.

Part: SKIN — DAMAGED (BS 720A) · airframe 46,155 hrs · 29,864 cycles

EXTERIOR FUSELAGE BS 720A BELOW STR 15L HAS A PREVIOUS BLEND OUT. FOUND OUT OF LIMITS IAW IAW SRM 53-30-1 FIG 1, CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW SRM 53-30-3, FIG 3, SRM 53-30-2, FIG 2 AND SRM 51-30-2.

Part: SKIN — GOUGED (BS 720D) · airframe 46,155 hrs · 29,864 cycles

SKIN GOUGED BS 720D 10" STR 19L. REPAIRED IAW SRM 51-30-2, CUT OUT LOWER SKIN IAW SRM 53-30-3, FIG 5. FABRICATED NEW DOUBLER, STRUCTURAL FILLER AND FILLER IAW SRM 53-30-3, FIG 5. INSTALLED NEW DOUBLER, STRUCTURAL FILLER AND FILLER IAW SRM 53-30-3, FIG 5.

Part: SKIN — DENTED (BS 490) · airframe 46,155 hrs · 29,864 cycles

DENT IN SKIN BS 490 ABOVE STRINGER 25R. CUT OUT DAMAGED AREA ON FUSELAGE SKIN IAW SRM 53-30-3, FIG 1 AND 51-10-1. FABRICATED REPAIR DOUBLER IAW SRM 53-30-01, FIG 1. INSTALLED REPAIR DOUBLER IAW SRM 51-30-02.

Part: SEAT TRACK — CRACKED (BS 1130) · airframe 46,155 hrs · 29,864 cycles

CRACK ON SEAT TRACK SCALLOP BL 0 AT BS 1130. REMOVED DAMAGED SEAT TRACK IAW SRM 53-10-5, FIG 1. FABRICATED NEW SEAT TRACK AND INSTALLED IAW P-F SRM 53-10-5, FIG 1 AND SRM 53-10-5, FIG 1.

Part: WEB — CRACKED (AFT AIRSTAIR) · airframe 46,155 hrs · 29,864 cycles

AFT AIRSTAIR AREA CRACKS IN WEB AT LT LOWER TORQUE BOX, BS 1323. REMOVED AFT WEB AT LT LOWER TORQUE BOX AND ATTACH ANGLES IAW SRM 51-30-2. FABRICATED NEW WEB IAW DWG 65-17510. INSTALLED NEW WEB AND ATTACH ANGLES IAW SRM 51-30-2.

Part: WEB — CRACKED (AIRSTAIR) · airframe 46,155 hrs · 29,864 cycles

AFT AIRSTAIR AREA LT LOWER TORQUE BOX WEB IS CRACKED AT PNEUMATIC LINE, STAND OFF BRACKET BS 1223. REPAIRED IAW SRM 51-40-02

Part: DOOR — BINDING (COCKPIT) · airframe 45,913 hrs · 29,687 cycles

COCKPIT DOOR VERY DIFFICULT TO CLOSE. SUSPECT BENT DOOR FRAME. COCKPIT DOOR OPS CHECKED NORMAL IAW AMM CH 55-50-001-8-0. ACFT OK FOR SERVICE.

Part: BLEED VALVE — LACK OF LUBE (NR 2 ENGINE) · airframe 45,271 hrs · 29,182 cycles

WHILE CLIMBING THROGH FL305, NR 2 ENGINE, EXPERINCED ABOUT 5 COMPRESSOR STALLS. ENGING BEHAVED NORMALLY AFTER RETARDING NR 2 THRUST LEVER. ACFT WAS IN CLEAR AIR WITH ENGINE ANTI-ICE CLOSED. ABOUT 5 MINUTES EARLIER ACFT WAS IN MODERATE PRECIPITATION WITH ENGINE ANTI ICE OPEN. C/W INSPECTION ITEMS PER MM 71-00-000-6 FOR NR 2 ENGINE COMPRESSOR STALL. NO DEFECTS NOTED. ENG TURNS SMOOTH AND FREELY WITH NO UNUSUAL NOISES. LUBRICATED BLEED VALVES PER MOCC REQUEST, AND INSPECTED PS3 BLEED FILTER FOR DEBRIS, NONE NOTED, REF MM 75-30-00.

Part: GUSSET — CRACKED (TORQUE BOX) · airframe 44,955 hrs · 28,934 cycles

AFT AIRSTAIRS FLOOR WEB UPPER CHORD HAS CRACK INDICATION TORQUE BOX BS 1263. REMOVED TORQUE BOX WEB AND GUSSET AND 2 EA UPPER CHORDS AND REMOVED BOLT AT AFT AIRSTAIR IAW SRM 51-30-2. FABRICATED GUSSET IAW SRM 51-20-1. HEAT TREATED TO T6 IAW FAS ENGINEERING REPORT NR 2-37153-801 REV A. DRILLED AND TREATED AND PRIMED 2 EA CHORDS AND GUSSET IAW SRM 51-10-2 AND 51-30-5. INSTALLED PARTS IAW SRM 51-30-2. REINSTALLED TORQUE BOX WEB AND BOLT AT AFT AIRSTAIRS IAW SRM 51-30-2 AND SRM 53-10-2 FIG 6.

Part: RIB — CRACKED (NR 4 SLAT) · airframe 44,955 hrs · 28,934 cycles

NR 4 SLAT HAS 1 CRACKED RIB ON THE OTBD SIDE OF ACTUATOR FWD MOUNT. REMOVED ACCESS PANELS ON NR 4 SLAT IAW SRM 51-30-2. REMOVED (2) RIBS INBD AND OTBD FOR ACCESS & TWO (2) RIBS DAMAGED IAW SRM 51-30-2. LOCATED & DRILLED NEW RIBS INBD AND OTBD IAW SRM 51-30-5. INSTALLED NEW RIBS & RIBS FOR ACCESS IAW SRM 51-30-2. INSTALLED ACCESS PANELS IAW SRM 51-30-2.

Part: RIB — CRACKED (NR 2 SLAT) · airframe 44,955 hrs · 28,934 cycles

NR 2 SLAT HAS 2 CRACKED RIBS AT FWD MOUNT OF ACTUATOR. REMOVED CRACKED RIBS (2 EA) AT NR 2 SLAT & INSTALLED NEW RIBS INBD/OTBD IAW SRM 51-30-2, SRM 51-30-5, SRM 57-50-2 FIG 2, REV 102.

Part: SEAT TRACK — CORRODED (BS 870-910) · corrosion level 2 · airframe 44,955 hrs · 28,934 cycles

CORROSION RBL 45 SEAT TRACK STA 870 - 910 FWD END OF TRACK HAS LIFTED METAL IN CHANNEL AT STA 870. REMOVED DAMAGED SEAT TRACK IAW SRM 51-30-2. FABRICATED NEW SPLICES & SEAT TRACK IAW SRM 53-10-5 FIG 1. TREATED & PRIMED SEAT TRACK & SPLICES IAW SRM 51-30-2. INSTALLED NEW SEAT TRACK & SPLICES IAW SRM 51-30-2.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,955 hrs · 28,934 cycles

CORROSION SEAT TRACK MAIN CABIN BS 990 LBL 45. REMOVED SEAT TRACK SECTION, FABRICATED NEW SEAT TRACK IAW SRM 53-10-5 FIG 1, ALODINE & PRIME IAW SRM 51-10-2, INSTALLED NEW SEAT TRACK SECTION IAW SRM 51-30-2.

Part: SEAT TRACK — CORRODED (BS 950) · corrosion level 2 · airframe 44,955 hrs · 28,934 cycles

CORROSION RBL 45 SEAT TRACK FLANGES AND SPLICE HARDWARE STA 950. REMOVED CORROSION & FOUND TO BE OUT OF LIMITS IAW SRM 51-10-6, REMOVED SEAT TRACK SECTION BS 950 TO 1020 IAW SRM 51-30-2. FABRICATED NEW SEAT TRACK IAW SRM 53-10-5, TREATED AND PRIMED SEAT TRACK IAW SRM 51-10-2 AND DISPACED PRESSURE PANEL WEB IAW SRM 51-30-2 AND REINSTALLED PRESSURE PANEL & INSTALLED NEW SEAT TRACK & SPLICES IAW SRM 51-30-2.

Part: SHEAR TIE — CORRODED (BS 680 S28L/R) · corrosion level 2 · airframe 44,955 hrs · 28,934 cycles

CORRODED SHEAR TIE FWD PIT BS. 680 STR 28L TO 28R. CUT OUT DAMAGED AREA IAW EX SRM 51-10-1 REV 102 FABRICATED REPAIR DOUBLER AND SHEAR TIE IAW SRM 53-10-4 FIG 13 REV 102. FABRICATED RADIUS FILLER IAW SRM 53-10 -4 FIG 13 INSTALLED DOUBLER, SHEAR TIE AND RADIUS FILLER IAW SRM 51-30-2 REV 102.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,955 hrs · 28,934 cycles

CORROSION SEAT TRACK MAIN CABIN BS 610 TO BS 578 LBL 24 REMOVED CORRODED SEAT TRACK SECTION IAW SRM 51-30-2. FABRICATED NEW SEAT TRACK, ANGLE SPLICES, & STRAP SPLICE IAW SRM 53-10-5 FIG 1. TREATED AND PRIMED SEAT TRACK AND SPLICES IAW SRM 51-10-2. INSTALLED SEAT TRACK AND SPLICES IAW SRM 51-30-2.

Part: STRUCTURE — CRACKED (NR 7 SLAT) · airframe 44,955 hrs · 28,934 cycles

RT WING NR 7 SLAT INBD OF INBD STOP PAD CRACKED. REMOVED LOWER CHORD OF NR 7 SLAT IAW SRM REV 102 51-30-2. FABRICATED REPAIR IAW SRM 51-30-5, 57-50-2. INSTALLED IAW SRM REV 102, 51-30-2.

Part: SEAT TRACK — CORRODED (BS 510-540) · corrosion level 2 · airframe 44,955 hrs · 28,934 cycles

CORROSION SEAT TRACK BS 540 TO BS 510 LBL 45 REMOVED DAMAGED SEAT TRACK SECTION FROM BS 480-720A 10 IN LBL 45. FABRICATED NEW SEAT TRACK SECTION, ANGLE SPLICES AND STRAP SPLICE IAW SRM 53-10-5 FIG 1. TREATED AND PRIMED SEAT TRACK & SPLICES IAW SRM 51-10-2 AND INSTALLED NEW SEAT TRACK SECTION & SPLICES IAW SRM 51-30-2.

Part: SKIN — CRACKED (BS 526 S5R) · airframe 44,955 hrs · 28,934 cycles

EXTERIOR FUSELAGE BS 526 AT STR 5R HAS A LIGHTNING STRIKE REMOVED FASTENER IAW SRM 53-30-3 AND 51-30-2, HFEC INSPECTED AREA IAW NDTM 51-00-00, FIG 23 FIG 6, CRACK NOTED, CUT OUT DAMAGED AREA IAW SRM 53-30-3 FIG 3, FABRICATED DOUBLER REPAIR & FILLER IAW SRM 53-30-3 FIG 3 , TREATED AND PRIMED IAW SRM 51-10-2 INSTALLED REPAIR PARTS IAW SRM 51-30-2.

Part: WEB — CRACKED (BS 1303) · airframe 44,955 hrs · 28,934 cycles

AFT AIRSTAIRS RT TORQUE BOX WEB LIGHTENING HOLE IS CRACKED. CUT-OUT DAMAGE IAW SRM REV 102, 51-10-1. FABRICATED REPAIR DOUBLER IAW SRM 51-40-2 FIG 1, AND 53-10-2. INSTALLED REPAIR DOUBLER AT BS 1303 IAW SRM 51-30-2.

Part: WEB — CRACKED (AIRSTAIR) · airframe 44,955 hrs · 28,934 cycles

AFT AIRSTAIRS RT SIDE FLOOR WEB AT LIGHTENING HOLE HAS CRACK INDICATION AT BS 1334.0. CUT OUT DAMAGE ON RT FLOOR WEB AT LIGHTENING HOLE IN AFT AIRSTAIRS, 5 IAW SRM REV 102, 51-10-1. FABRICATED REPAIR DOUBLER IAW SRM 53-10-2 AND 51-40-2. INSTALLED REPAIR DOUBLER IAW SRM 51-30-2.

Part: SEAT TRACK — CORRODED (BS 620-680) · airframe 44,955 hrs · 28,934 cycles

CORROSION SEAT TRACK MAIN CABIN BS 680 TO BS 620, BL 0. REMOVED SEAT TRACK SECTION IAW SRM 51-30-2. FABRICATED NEW SECTION SEAT TRACK IAW SRM 53-10-5 REV 102 TREATED AND PRIMED SEAT TRACK & AREA IAW SRM 51-10-2. INSTALLED SEAT TRACK SECTION IAW SRM 51-30-2.

Part: FRAME — CRACKED (BS 640 S28L) · airframe 44,955 hrs · 28,934 cycles

FWD CARGO AREA, BS 640, STR 28L, CRACKED FRAME. CUT-OUT DAMAGE IN B640 FRAME AT STR. 28L, 1" X 1 1/4" IAW SRM REV 102, 51-10-1. FABRICATED REPAIR DOUBLER IAW SRM 51-40-3 FIG 1 AND 53-10-2 FIG 3. HEAT TREATED REPAIR DOUBLER TO -T6 CONDITION IAW FAS ENGINEERING REPORT 2-37153-801 REV A. INSTALLED DOUBLER ON FRAME IAW SRM 51-30-2 AND 51-40-3.

Part: SKIN — CRACKED (FUSELAGE) · airframe 44,955 hrs · 28,934 cycles

FWD GALLEY DOOR CUTOUT, LWR AFT CORNER CRACKED FROM FASTENER HOLE, SKIN: 0.40", BEAR STRAP: 0.15". STOP DRILLED CRACKS AT SKIN & BEAR STRAP, FABRICATED REPAIR DOUBLER, AND TRIPLER, TREATED & PRIMED AND INSTALLED REPAIR PARTS AT FWD GALLEY DOOR CUTOUT LWR AFT CORNER IAW SRM 51-10-1, SRM 51-10-2 & EO NR 7-5313-7-2304 PT 2.

Part: SEAT TRACK — CORRODED (BS 600-620) · airframe 44,955 hrs · 28,934 cycles

CORROSION SEAT TRACK BS 600 TO BS 620 RBL 24 MAIN CABIN. REMOVED SEAT TRACK. FABRICATED NEW SEAT TRACK IAW SRM 53-10-5 FIG 1 REV 102. TREATED AND PRIMED SEAT TRACK IAW SRM 51-10-2 AND INSTALLED SEAT TRACK IAW SRM 53-10-5 FIG 1 REV 102 & 51-30-2.

Part: SEAT TRACK — CORRODED (BS 720) · airframe 44,955 hrs · 28,934 cycles

CORROSION SEAT TRACK MAIN CABIN BS 720, 12 IN, RBL 45. WORK ACCOMPLISHED ON WO NR 00046937, NR N00775.

Part: SKIN — UNKNOWN (BS 440 S23R) · airframe 44,955 hrs · 28,934 cycles

FUSELAGE EXTERNAL REPAIR AT STA 440 STR 23R REQUIRES EVALUATION PER E.O. 7-5100-7- 5005 PT1. REMOVED EXISTING REPAIR DOUBLER AT STA 440 AND STR 23R IAW SRM REV 102 51-30-2. FABRICATED DOUBLER, SHIM AND FILLER IAW SRM 53-30-3 FIG 4. INSTALLED REPAIR DOUBLER, SHIM, AND FILLER IAW SRM 51-30- 2.

Part: FLOORBEAM — CRACKED (BS 400) · airframe 44,955 hrs · 28,934 cycles

CRACK INDICATION FLOORBEAM MAIN CABIN BS 400 LBL 8. CUTOUT DAMAGED AREA IAW DWG SR 27-53-034 REV "F". FABRICATED 2 ANGLE REPAIRS. 2 STRAPS, & 1 TEE IAW DWG SR 27-53-034 REV "F". TREATED AND PRIMED IAW SRM 51-10-2. INSTALLED ALL PARTS IAW SRM 51-30-2 & DWG SR 27-53-034 REV "F".

Part: SEAT TRACK — CORRODED (BS 848-870) · airframe 44,955 hrs · 28,934 cycles

CORROSION SHORT SECTION OF FLOATING SEAT TRACK LBL 25 STA 848.5 TO 870. REMOVED SHORT SEAT TRACK IAW SRM 51-30-2. FABRICATED NEW SEAT TRACK SECTION IAW SRM 53-10-5 FIG 1. ALODINED & PRIMED IAW SRM 51-10-2. INSTALLED IAW SRM 51-30-2.

Part: SEAT TRACK — CORRODED (BS 530-538) · airframe 44,955 hrs · 28,934 cycles

CORROSION SEAT TRACK MAIN CABIN BS 530, RBL 45 TO BS 538, RBL 45. REMOVED SEAT TRACK AT RBL 45 BETWEEN BS 480 TO BS 740. FABRICATED SEAT TRACK REPAIR IN 2 SECTIONS (1) FROM BS 480 TO BS 720B PLUS 10" (2) FROM BS 720B PLUS 10" TO BS 740 RBL 45. FABRICATED SEAT TRACK SPLICE REPAIR STRAP AND ANGLES, TREATED AND PRIMED NEW PARTS, AND INSTALLED NEW PARTS ALL IAW SRM 53-10-5 FIG 1, REV 102 AND SRM 51-30-2 AND SRM 51-10-2.

Part: FRAME — CRACKED (BS 620 S28R) · airframe 44,955 hrs · 28,934 cycles

FWD CARGO AREA, BS 620, STR 28R, CRACKED FRAME. CUT OUT DAMAGE IN FWD PIT ON STA 620 FRAME AT STR 28R, IAW SRM 51-10-1. FABRICATED REPAIR DOUBLER IAW SRM 51-40-3, FIG 1 AND 53-10-2 FIG 3. HEAT TREATED REPAIR DOUBLER TO T6 CONDITION IAW FAS ENG REPORT NR 2-37153-801 REV A. INSTALLED REPAIR DOUBLER ON BS 620 FRAME AT STR 28R IAW SRM 51-30-2, REV 102.

Part: SEAT TRACK — CORRODED (BS 1110-1070) · corrosion level 2 · airframe 44,955 hrs · 28,934 cycles

CORROSION SEAT TRACK 2 EA AREAS BS 1110 TO BS 1070 RBL 45. REMOVED SEAT TRACK SECTION FROM BS 1020 TO BS 1134 RBL 45 IAW B727 SRM 53-10-5 FIG 1 AND 51-30-2. FABRICATED NEW SEAT TRACK IAW SRM 53-10-5 FIG 1. TREATED AND PRIMED NEW SEAT TRACK IAW SRM 51-10-2. INSTALLED NEW SEAT TRACK SECTION IAW SRM 53-10-5 FIG 1 AND 51-30-2.

Part: SKIN — UNKNOWN (BS 178) · airframe 44,955 hrs · 28,934 cycles

REPAIR AT STA 178 STR 24L REQUIRES EVALUATION PER E.O. 7-5100-7-5005 PT1. REMOVED REPAIR DOUBLER AT STA 178, STR 24L IAW SRM 51-30-2. FABRICATED FILLER AND DOUBLER IAW SRM 53-30-3 FIG 3. INSTALLED DOUBLER AND FILLER IAW SRM 51-30-2 REV 102.

Part: SEAT TRACK — CORRODED (BS 390) · airframe 44,955 hrs · 28,934 cycles

CORROSION SEAT TRACK MAIN CABIN BS 390 RBL 45. REMOVED DAMAGED SEAT TRACK SECTION, FABRICATED NEW SEAT TRACK SECTION, LOWER SPLICE, & 2 ANGLES. TREATED AND PRIMED PARTS IAW SRM 51-10-2. INSTALLED NEW SEAT TRACK & SPLICES IAW SRM 51-30-2, SRM 53-10-5 FIG 1, SRM 51-30-5 & SRM 51-10-2.

Part: FRAME — CRACKED (BS 620 S28L) · airframe 44,955 hrs · 28,934 cycles

FORWARD CARGO AREA, BS 620, S28L, CRACKED FRAME. CUT OUT DAMAGED AREA IAW SRM 51-10-1. FABRICATED REPAIR DOUBLER IAW SRM 51-40-3 FIG 1 AND 53-10-2 FIG 3. HEAT TREATED REPAIR DOUBLER TO T6 CONDITION IAW FAS ENGINEERING REPORT NR 2-37153-801 REV A. INSTALLED REPAIR DOUBLER ON BS 620 FRAME AT S28L IAW SRM 51-30-2 AND 51-40-3 FIG 1.

Part: SKIN — DAMAGED (BS 640-660 S2-3L) · airframe 44,955 hrs · 28,934 cycles

MAIN CARGO AREA, BETWEEN STA 640-660, BETWEEN STR 2L-3L, PILOT HOLE NEXT TO FASTENER. CUT-OUT DAMAGED AREA AT MAIN CARGO DOOR AREA, FABRICATED FILLER DOUBLER AND TRIPLER AND INSTALLED REPAIR PARTS IAW SRM 53-30-3 FIG 1B.

Part: SPAR — CRACKED (NR 7 SPOILER) · airframe 44,955 hrs · 28,934 cycles

CRACK CHORD ANGLE FALSE SPAR AT NR 7 SPOILER ATTACH FITTING WBL 118 RT WING T/E. CUT OUT LT FALSE SPAR WEB AT NR 7 SPOILER ACTUATOR ATTACH FITTING AND ANGLE IAW DWG NR SR27-57-038 REV C. FABRICATED REPAIR ANGLES, CHORD, WEB, STRAP & WEB DOUBLER IAW DWG NR SR27-57-038. INSTALLED CHORD, ANGLES, STRAP, WEB DOUBLER IAW DWG NR SR27-57-038 REV C, AND SRM 51-30-2.

Part: SKIN — DENTED (HORIZONTAL STAB) · airframe 44,955 hrs · 28,934 cycles

HORIZ STAB RT SIDE L/E PANEL NR 9203 DAMAGED AT L/E OF PANEL. CUT OUT DAMAGE ON RT HORIZ STAB. L/E PANEL NR 9203, 6" X 7 3/8" IAW SRM 51-10-1, REV 102. FABRICATED FILLER AND DOUBLER, IAW SRM 55-10-3 FIG 2 AND 55-10-2 FIG 1 REV 102. INSTALLED FILLER AND DOUBLER IAW SRM 51-30-2 REV 102.

Part: SKIN — GOUGED (LT WING TE FLAP) · airframe 44,955 hrs · 28,934 cycles

LT OTBD FOREFLAP L/E IS GOUGED IN 2 PLACES ON PREVIOUS REPAIR- INBD END OF FOREFLAP. REMOVED PREVIOUS REPAIR AT LT OTBD FOREFLAP L/E IAW SRM 51-30-2. FABRICATED NEW REPAIR DOUBLER IAW SRM 57-50-2, FIG 4 AND 51-30-5. TREATED AND PRIMED DOUBLER IAW SRM 51-10-2. INSTALLED DOUBLER IAW SRM 51-30-2 REV 102.

Part: FRAME — CRACKED (BS 540 S21-22L) · airframe 44,955 hrs · 28,934 cycles

FWD CARGO AREA, STA 540, STR 21L-22L, CRACK ON LWR STUB FRAME EXTENSION RADIUS. REMOVED FASTENERS FOR ACCESS & REMOVED L/W FRAME EXTENSION IAW SRM 51-30-2. FABRICATED NEW FRAME AND HEATED TREATED TO T6 IAW ENGINEERING REPORT NR 2-37153-801 REV A, TREATED AND PRIME AREA & FRAME IAW SRM 51-10-2. INSTALLED FRAME EXTENSION IAW SRM 51-30-2.

Part: ROLLER — OUT OF ADJUST (TE FLAPS) · airframe 44,193 hrs · 28,393 cycles

ON DESCENT TO IAD AIRFRAME BUFFET AT 290 KNOTS 270FL FOLLOWED QRH AT 14,000 250 KTS NO BUFFET FELT. FLAPS 15 DEGREES LANDING ACCOMP FOR WING LEVEL NEED 1/2 UNIT OF TRIM RUDDER. CONTROL WHEEL SHOWED 35 DEGREES RIGHT WITH NO TRIM. OPS CHECK SPOILERS ALL DEPLOY EVENLY AND NO EVIDENCE OF FLUID BYPASS. WHILE TURNING CONTROL COLUMN WHEEL INSPECTED CABLES AND QUARDRUM: NO OBVIOUS DEFECTS FOUND. LOWERED FLAPS AND VISUALLY INSPECTED ROLLERS AND TRACK: ALL LOOKED OK. PHYSICALLY LIFTED ON FLAPS AND FOUND LEFT OUTBOARD AFT FLAP EXCESSIVE PLAY. ADJUSTED DEAD WEIGHT ROLLER ECCENTRIC AND OUTBOARD ROLLERS ECCENTRIC IAW MM 27-51-012-4. OPERATED FLAPS AND OPS CHECKED GOOD.

Part: FRAME — CRACKED (ZONE 800) · airframe 43,378 hrs · 27,803 cycles

GALLEY DOOR (R-1) CUTOUT UPPER FWD SIDE STATION 380 FRAME CRACKED ON FORWARD SIDE BETWEEN STR 7R AND 8R. REMOVED FASTENERS IN DAMAGED AREA, CUTOUT DAMAGE, NDT VERIFIED NO DEFECTS. FABRICATED STRAP AND FILLER, TREATED, PRIMED REPAIR PARTS. INSTALLED REPAIR PARTS REF EA NR 7-5310-113937, SRM 51-30-2.

Part: SHEAR TIE — CORRODED (BS 1010) · corrosion level 2 · airframe 43,378 hrs · 27,803 cycles

AFT PIT STA 1010 BUTT JOINT SPLICE SHEAR TIE CORRODED BETWEEN STR 27-28R BLENDED CORROSION, ORIGINAL MATERIAL THICKNESS WAS .075" BETWEEN 0.001" AND 0.017 IS THE MATERIAL LOSS. OUT OF LIMITS REF SRM 53-30-01 FIG 1. FABRICATED AND INSTALLED FILLER AND DOUBLER REF EA NR 7-5330-113263.

Part: WEB — CORRODED (ZONE 200) · corrosion level 2 · airframe 43,378 hrs · 27,803 cycles

MAIN DECK FLOOR SHEAR WEB AT BS 1165-1166 RBL 48" TO 49" WL 208 HAS CORROSION ON UPPER SURFACE. REMOVED CORROSION AND NDT AREA. REMOVED DAMAGED AREA INSTALLED DOUBLER AND FILLER PER SRM 51-40-02 FIGURE NR 1. REINSTALLED DISTURBED AREA PER MM 53-20-012-4, SRM 51-30-2 PG 13. MATERIAL VERIFIED PER SRM 51-40-2 FIG 1.

Part: WEB — CORRODED (BS 1165-1166) · corrosion level 2 · airframe 43,378 hrs · 27,803 cycles

MAIN DECK FLOOR SHEAR WEB AT BS 1165-1166 RBL 48" TO 49" WL 208 HAS CORROSION ON UPPER SURFACE. REMOVED CORROSION AND NDT AREA. REMOVED DAMAGED AREA INSTALLED DOUBLER AND FILLER PER SRM 51-40-02 FIGURE NR 1. REINSTALLED DISTURBED AREA PER MM 53-20-012-4, SRM 51-30-2 PG 13. MATERIAL VERIFIED PER SRM 51-40-2 FIG 1.

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 43,378 hrs · 27,803 cycles

AFT PIT STA 970 SHEAR TIE CORRODED BETWEEN STRINGER 25R-26R RBL 17-22 REMOVED CORRRODED SHEAR TIE. FAB`D REPAIR SHEAR TIE AND INSTALLED PER SRM 53-10- 4 FIG 11 PAGE 43 THR 45.

Part: PANEL — DELAMINATED (ZONE 600) · airframe 43,378 hrs · 27,803 cycles

RT WING OB TE PANEL 8855, LWR SKIN HAS LARGE AREA OF DISBOND IN CENTER OF PANEL. INSTALLED NEW PANEL IAW SRM 51-30-02 PG 1 AND PG 13-14.

Part: DEPRESSOR — GOUGED (CARGO DOOR) · airframe 43,378 hrs · 27,803 cycles

FWD LWR CARGO DOOR LOWER EDGE SEAL DEPRESSOR I/B SURFACE IS GOUGED IN 2 PLACES 26" AND 33" FROM AFT END OF DOOR. REPLACED SEAL DEPRESSOR IAW SRM 52-30-1.

Part: WEB — CRACKED (BS 1180) · airframe 43,378 hrs · 27,803 cycles

MAIN DECK ARCHED WEB AND ANGLE AT BS 1180 LBL38" WL 208 IS CRACKED. ABOVE SNRM WAS SOILED. FABRICATED NEW WEB, ANGLES AT BS 1180 LBL 38" WL 208 IAW B727 DWG 65-29567. TREATED AND PRIMED, INSTALLED IAW B727 SRM 51-10-2, 51-30-2.

Part: PANEL — CRACKED (ZONE 200) · airframe 43,378 hrs · 27,803 cycles

MAIN DECK ARCHED WEB BETWEEN BS 1176-1183 RBL 36" TO 47" HAS SEVERAL CRACKS AND SEPARATED COMPOSITE PATCH. REMOVED DAMAGED PART AND FABRICATED NEW FROM 2024-O .032 MATERIAL AND SENT FOR HEAT TREAT. TREATED AND PRIMED REF M/M 51-20-151-7. INSTALLED NEW PARTS REF SRM 51-30-2.

Part: PANEL — DELAMINATED (RT WING) · airframe 43,378 hrs · 27,803 cycles

RT WING O/B T/E PANEL 8855, LWR SKIN HAS LARGE AREA OF DISBOND IN CENTER OF PANEL. INSTALLED NEW PANEL IAW SRM 51-30-2 PG 1 & PG 13-14.

Part: KEELBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 43,378 hrs · 27,803 cycles

AFT PIT KEEL BEAM CHORD/STR 29L CORRODED STA 990-1010 REMOVED CORROSION. FOUND TO BE OUT OF LIMITS TREATED AND PRIMED BLENDED AREA REF SRM 51-10-2. FABBED REPAIR STRAP REF DWG SR 27-53-023. TREATED AND PRIMED REF SRM 51-10-2. INSTALLED REPAIR REF DWG SR 27-53-023.

Part: INTERCOSTAL — CORRODED (ZONE 100) · corrosion level 2 · airframe 43,378 hrs · 27,803 cycles

AFT PIT STA 970 STR 27R-28R INTERCOSTAL. REMOVED INTERCOSTAL REF SRM 51-30-2, REMOVED STIFFENERS REF SRM 51-30-2. FABRICATED AND HEAT TREATED NEW INTERCOSTAL REF WO 2007-07-027 PN 69-44880-12. TREATED AND PRIMED INTERCOSTAL REF SRM 51-10-2. INSTALLED NEW INTERCOSTAL REF SRM 51-30-2.

Part: SKIN — GOUGED (CARGO DOOR) · airframe 43,378 hrs · 27,803 cycles

FWD LWR CARGO DOOR INNER SKIN IS GOUGED 2 " FROM TOP 19 " FROM AFT EDGE. BLENDED DAMAGE PER SRM 51-10-1 PG 3-4 IT WAS OUT OF LIMITS PER SRM 52-00-2 PG 1 STEP 1B, REMOVED DOUBLER AND MANUFACTURED NEW DOUBLER OUT OF 7075-T6 .050. INSTALLED ON DOOR AND INSTALLED FIELD FASTENERS AROUND DAMAGED AREA PER SRM 52-00-3 FIG 3 AND SRM 51-30-2. TREATED AND PRIMED DOUBLER PER SRM 51-10-2 DOOR WAS REMOVED AND INSTALLED ON SNRM N00361.

Part: PANEL — CRACKED (ZONE 200) · airframe 43,378 hrs · 27,803 cycles

UPPER MAIN DECK STA. 1176-1183 RBL 27", ARCHED FLOOR WEB CLOSURE, INBD ANGLE IS DAMAGED. REMOVED DAMAGED ANGLE, FABRICATED NEW AND SENT FOR HEAT TREAT. TREATED AND PRIMED REF M/M 51-20-151-7. INSTALLED NEW ANGLE REF SRM 51-30-02.

Part: FRAME — CRACKED (ZONE 100) · airframe 43,378 hrs · 27,803 cycles

FWD CARGO PIT LT SIDE BS 600 STR 21L FRAME EXTENSION CRACKED ON O/B EDGE ABOVE STR 21L. REMOVED FRAME SPLICE REF SRM 51-30-02. FORMED NEW FRAME SPLICE USING .063 7075-O A 66693 PO NR 1008655 REF DWG 53FX1350 REV A. RECEIVED HEAT TREATED REPAIR SPLICE REF FORM 8130-3 FORM NR 2007-07-031 AND SNRM N00633. LOCATED DRILLED AND DEBURRED HOLES IN REPAIR PART REF SRM 51-30-02. INSTALLED REPAIR SPLICE IAW SRM 51-30-02 AND DWG NR 53FX1350.

Part: PLATE — CRACKED (ZONE 100) · airframe 43,378 hrs · 27,803 cycles

AFT CARGO PIT THRESHOLD PLATE IS CRACKED BY WELD. REPAIR ACCOMPLISHED ON N/R N00477, PER SR 27-53-025C.

Part: FRAME — CRACKED (ZONE 100) · airframe 43,378 hrs · 27,803 cycles

FWD CARGO PIT LT SIDE BS 600 STR 21L FRAME EXTENSION CRACKED ON O/B EDGE ABOVE STR 21L. REMOVED FRAME SPLICE REF SRM 51-30-2. FORMED NEW FRAME SPLICE USING .063 7075-O A66693 PO NR 1008655 REF DWG 53FX1350 REV A. RECEIVED HEAT TREATED REPAIR SPLICE REF FORM 8130-3 FORM NR 2007-07-031 AND SNRM N00633. LOCATED, DRILLED AND DEBURRED HOLES IN REPAIR PART REF SRM 51-30-02. INSTALLED REPAIR SPLICE IAW SRM 51-30-02 AND DWG # 53FX1350.

Part: ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 43,378 hrs · 27,803 cycles

AFT PIT FWD BULKHEAD BRACKET AT STA 950 WL 146 RBL 21-24 CORRODED. REPLACED ANGLE IAW SRM 53-10-1 THIS IS CLASSIFIED AS A MINOR REPAIR REF BAC65-58600, SRM 51-30-2.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 43,378 hrs · 27,803 cycles

FWD CARGO BAY STR S-28R I/B UPPER FLANGE IS CORRODED AT BS 530. REMOVED CORROSION. ORIGINAL MATERIAL THICKNESS WAS .063". REMAINING MATERIAL IS OUT OF LIMITS AT .043". FABBED, TREATED, AND PRIMED REPAIR PART, P/N BAC1498-132. INSTALLED REPAIR PART AND NUT SPACERS AFTER DAMAGE WAS REMOVED, REF SRM 51-10-6 AND SRM 53-10-3, PG 3-4B.

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 43,378 hrs · 27,803 cycles

AFT PIT SHEAR TIE CORRODED STA 950F BETWEEN STR 27 R-28R RBL 17 - 22 REMOVED CORROSION AT STA 950F, STR 27-28R, RBL 17-22, IAW SRM 53-10-1 PG 2, NDT FOR MATERIAL LOSS, ORIGINAL THICKNESS .063". REMAINING THICKNESS IS .058" . WITHIN 10% LIMIT IAW SRM 53-10-1 PG 1. TREATED AND PRIMED AFFECTED AREA SRM 51-10-2.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 43,378 hrs · 27,803 cycles

AFT PIT STRINGER 27R CORRODED FROM STA 1030-1060, BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS. REMOVED SHEAR TIE AND DAMAGED SECTION OF STRINGER. FABRICATED STRINGER REPAIR PARTS AND DRILLED TO FIT. TREATED AND PRIMED REPAIR PARTS. INSTALLED STRINGER REPAIR AT STA 1030-1060 STRINGER 27L AND REINSTALLED SHEAR TIE, REF SRM 53-10-1 AND SRM 51-30-2.

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 43,378 hrs · 27,803 cycles

FWD CARGO BAY INNER SKIN HAS CORROSION, BS 720C TO 720C 6 ", LBL 205" TO 5" WL 148.5. CUT OUT DAMAGE SKIN AT BS 720C TO 726C IAW B727 SRM 53-30-3.

Part: SKIN — GOUGED (ZONE 100) · airframe 43,378 hrs · 27,803 cycles

AFT FUSELAGE EXT SKIN BS 1208 STR S-23R SKIN IS GOUGED. INSTALLED REPAIR ON EXT SKIN, AFT FUSELAGE STA 1208 STR 23R REF B727 SRM 53-30-3, PG 6 FIG 1.

Part: LINER — CRACKED (HUSH KIT) · airframe 43,378 hrs · 27,803 cycles

NR 1 ENGINE HUSH KIT INNER LINER DISBONDED AND CRACKED AT 9 O'CLOCK POS. VERIFIED MATERIAL (INCONEL) REF. 78 -38-41 PREP FOR WELD REF 78-38-41, WELD WITH AMS 5837, A29984 INSPECT REF 78-38-41.

Part: SEAL DEPRESSOR — CRACKED (ZONE 500) · airframe 43,378 hrs · 27,803 cycles

LT WING TE PNL 8155 SEAL DEPRESSOR IS FRETTED, CRACKED ALONG INBD EDGE. REPLACED SEAL DEPRESSOR IAW SRM 51-30-2.

Part: RIB — CRACKED (ZONE 300) · airframe 43,378 hrs · 27,803 cycles

VERTICAL STABLIZER RIB NUMBER 2 LT OTBD CHORD CRACKED AT STRINGER 7. REMOVED DAMAGE, FABRICATED REPAIR PARTS, SENT TO HEAT TREAT, TRACKING NR 2007-06-203, DRILLED, TREATED, AND PRIMED REPAIR PARTS. INSTALLED REPAIR PARTS REF SRM 55-30-5 FIG 1.

Part: SKATE ANGLE — CRACKED (ZONE 600) · airframe 43,378 hrs · 27,803 cycles

RT WING AT NR 6 FLAP TRACK FWD FAIRING, I/B SKATE ANGLE IS CRACKED. REMOVED DAMAGE, FABRICATED NEW 2 REPAIR ANGLE AND INSTALLED 2 REF. REPAIR ANGLES, REF SRM 51-40-3 PG 1-6.

Part: FLAP — DELAMINATED (RT WING) · airframe 43,378 hrs · 27,803 cycles

RT WING, I/B FLAPS, AFT FLAP O/B END T/E IS DELAMINATED. REMOVED, REPAIRED, AND REINSTALLED RT WING I/B FLAP, AFT FLAP ASSY REF'S MM 27-51-002-4 AND SRM 51-40-20. THIS IS CLASSIFIED AS A MAJOR REPAIR. PLAY AND POSITION CHECK TO BE PERFORMED ON ROUTINE CARD W/C 76C017-00.

Part: WEDGE — DEBONDED (LT WING) · airframe 43,378 hrs · 27,803 cycles

LT I/B MID FLAP AFT WEDGE HAS DISBONDED JUST O/B OF THE AFT FLAP TRACK. REMOVED LT I/B AFT FLAP REF M/M 27-51-001-4 REPAIRED MID FLAP REF SRM 51-40-21 PARA 4D AND 4E AND SRM 51-40-20 PARA 7, 14, 15, 18, 20, 21, 22 LT I/B AFT FLAP ASSY INSTALLED ON SNRM N00328. COOK TICKET ATTACHED THIS IS CLASSIFIED AS A MAJOR REPAIR.

Part: FLAP — DELAMINATED (RT WING) · airframe 43,378 hrs · 27,803 cycles

RT WING, I/B FLAPS, AFT FLAP O/B END T/E IS DELAMINATED. REMOVED, REPAIRED, AND REINSTALLED RT WING I/B FLAP, AFT FLAP ASSY REF'S MM 27-51-002-4 AND SRM 51-40-20 THIS IS CLASSIFIED AS A MAJOR REPAIR. PLAY AND POSITION CHECK TO BE PERFORMED ON ROUTINE CARD W/C 76C017-00.

Part: RIB — CRACKED (RT WING) · airframe 43,378 hrs · 27,803 cycles

RT WING INBD L/E FORMER WEB CRACKED AT AFT UPPER AREA INBD SIDE. FORMER LOCATED AT O/B END OF NR 6 FLAP. FABRICATED REPAIR DOUBLER, ON RT WING INBD L/E FORMED WEB TREATED AND PRIMED, AND INSTALLED IAW B727 SRM 51-40-2 FIG 1, 51-10-2, 51-30-2, CLASSIFIED MINOR REPAIR.

Part: CHANNEL — CRACKED (ZONE 500) · airframe 43,378 hrs · 27,803 cycles

LEFT WING FIXED TRAILING PANEL SUPPORT BRACKETS, ARE CRACKED AT SUPPORT ROD. SUPPORT ROD ATTACHS TO, TWO PANELS LOCATED JUST INBD OF THE NR 2 SPOILER. REMOVED, LOCATED, DRILLED AND INSTALLED Z BRACKET LT WING T/E PANEL SUPPORT BRACKET INBD OF NR 2 SPOILER PER SRM 51-30-2.

Part: SKIN — DELAMINATED (KRUGER FLAP) · airframe 43,378 hrs · 27,803 cycles

LT WING, PNL JUST AFT OF NR 2 KRUGER FLAP IS DELAMED AROUND VENT. REPAIRED DELAMED ON LT WING PNL JUST AFT OF NR 2 KRUGER FLAP REF SRM 51-40-9 PG 9 PARA 7.

Part: SKIN — DAMAGED (ZONE 100) · airframe 43,378 hrs · 27,803 cycles

FWD CARGO BAY BS 720 13 STR S-23R FUSELAGE SKIN FASTENER HOLE DAMAGED. FABRICATED FILLER AND DOUBLER FOR FWD CARGO BAY BS 720 13" STR S-27R FUSELAGE SKIN REF SRM 53-30-03, 53-10-03, 53-30-02, SEALANT 51-20-04.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 43,378 hrs · 27,803 cycles

FWD CARGO BAY BS 720+10 TO 720+14, S27R FWD END OF ORIGINAL CUT STR UNDER SPLICE IS CORRODED. I/B AND OB SIDE REMOVED S27R SPLICE AT BS 720. REMOVED DAMAGE SECTION STR-27R, AFT OF SPLICE. REMOVED DAMAGE SKIN, FABRICATED NEW STRINGER SECTION SPLICE, TREATED AND PRIMED REPAIR PARTS AND SKIN. INSTALLED STRINGER AND SPLICE, REF SRM 51-30-02, SRM 51-10-01, SRM 53-10-03 PG 3, SRM 53-10-3 FIG 1 SHT 1-4, MM 51-20-021-7, MM 51-20-151-7.

Part: STRINGER — CRACKED (ZONE 100) · airframe 43,378 hrs · 27,803 cycles

FWD CARGO PIT STRINGER IS CRACKED AT RIVET IN LOWER CHANNEL BS 72 10, STR 27R. REMOVED STRINGER SPLICE AT BS 720 10". FABRICATED, LOCATED AND DRILLED AND DEBURRED NEW STRINGER SPLICE USING BAC1498-132 MATERIAL. TREATED AND PRIMED AND INSTALLED STRINGER AT BS720 10 REF SRM 51-30-2, 53-10-3 PG 9, FIG 1, MM 51-20-021-7, 51-20-151-7.

Part: BULKHEAD — CRACKED (ZONE 100) · airframe 43,378 hrs · 27,803 cycles

RT LOWER FUSELAGE AFT OF RT WHEEL WELL, FUSELAGE PANEL NR 3622 IS CRACKED AT INNER I/B AREA. REMOVED CRACK ON UNDER SIDE OF PANEL NR 3622 REF SRM 51-40-9 PARAGRAPHS 4A AND4E.

Part: WARNING LIGHT — ILLUMINATED (AIRSTAIR) · airframe 41,802 hrs · 26,639 cycles

ON DEPARTURE AFT AIRSTAIR LIGHT ILLUMINATED ON S/O PANEL, RETURNED TO MEM, LIGHT EXTINGUISHED ON TOUCHDOWN. ACN RELEASED FOR SERVICE PER MEL/CDL: 52-06-B CATEGORY: C EXPIRATION:

Part: ANGLE — DAMAGED (FUSELAGE) · airframe 41,264 hrs · 26,276 cycles

WHILE CLOSING AFT CARGO BAY THRESHOLD FOUND LOWER ANGLE AT BS 990 TO BE DAMAGED. REPAIRED DAMAGED AFT CARGO BAY THRESHOLD LOWER ANGLE BS 990 PER FED EX EA 7- 5310-86283.

Part: FITTING — CORRODED (VERTICAL STAB) · airframe 41,264 hrs · 26,276 cycles

VERTICAL FIN TENSION TIE RIB LEFT AFT VERT BOLT HOLE CORRODED A/C AND TENSION TIE SIDE. REPAIRED VERT FIN TENSION TIE RIB LT AFT VERT BOLT HOLE PER FED EX EA 7-5530-86280

Part: FITTING — CORRODED (VERTICAL STAB) · airframe 41,264 hrs · 26,276 cycles

CORROSION VERT STAB TENSION TIE AFT SHEER FITTING UPPER SURFACE. REPAIRED VERTICAL FIN TENSION TIE AFT SHEAR FITTING PER FED EX EA. 7-5530-86280.

Part: SHEAR TIE — TOOL DAMAGE (VERTICAL STAB) · airframe 41,264 hrs · 26,276 cycles

VERTICLE STAB TENSION TIE FWD SHEAR TIE FITTING HAS PREVIOUS TOOLING MARKS. REPAIRED PER EA 7-5530-86281.

Part: FITTING — CORRODED (VERTICAL STAB) · airframe 41,264 hrs · 26,276 cycles

VERTICAL STAB TENSION TIE RT AFT FITTING CORRODED. REPAIRED IAW EA 7-5530-86279.

Part: FITTING — CORRODED (VERTICAL STAB) · airframe 41,264 hrs · 26,276 cycles

VERTICAL STAB TENSION TIE LT AFT FITTING CORRODED. REPAIRED IAW EA 7-5530-86279.

Part: ATTACH FITTING — CORRODED (VERTICAL STAB) · airframe 41,264 hrs · 26,276 cycles

CORROSION VERTICAL STAB TENSION TIE RT FWD FITTING IS CORRODED. REPAIRED PER EA 7-5530-86277.

Part: ATTACH FITTING — CORRODED (VERTICAL STAB) · airframe 41,264 hrs · 26,276 cycles

CORROSION VERTICAL STAB TENSION TIE LT FWD FITTING IS CORRODED. REPAIRED PER EA 7-5530-86277.

Part: BEAM — CORRODED (LT MLG) · airframe 41,264 hrs · 26,276 cycles

CORROSION ON LT MLG BEAM LOWER SURFACE. REPAIRED PER EA 7-5710-86267.

Part: DOUBLER — DAMAGED (FUSELAGE) · airframe 41,264 hrs · 26,276 cycles

REPAIR AT EXTERNAL DOUBLER BS 990 TO BS 1000 BL 0 WL 148, 18 INCHES BY 18.5 INCHES NEEDS EVALUATION TO DETERMINE PER SRM OR APPROVED DATA. REPAIRED DOUBLER PER FED EX EA 7-5330-86271

Part: FITTING — DAMAGED (WING) · airframe 41,264 hrs · 26,276 cycles

WING FITTING REQUIRED RESLEEVING DUE TO BLENDED DAMAGE OUT OF LIMITS. SO, THE BODY FITTING ALSO NEED TO BE RESLEEVED. REPAIRED LT 740 WING TERMINAL FITTING PER FED EX EA 7-5710-86260.

Part: FITTING — DAMAGED (WING) · airframe 41,264 hrs · 26,276 cycles

BLENDED DAMAGE IN WING TERMINAL FITTING OUT OF LIMITS. REPAIRED LEFT WING BODY FITTING PER FED EX EA 7-5340-86266.

Part: SKIN — MISDRILLED (FUSELAGE) · airframe 41,264 hrs · 26,276 cycles

DRILL START IN FUSELAGE SKIN BELOW FWD GALLEY DOOR. REPAIRED DRILL START PER FED EX EA 7-5330-86265.

Part: INTAKE — CORRODED (APU) · airframe 41,264 hrs · 26,276 cycles

APU AIR INTAKE HOUSING HAS CORROSION ON MOUNTING FLANGE ALONG LOWER SIDE.

Part: FRAME — MISDRILLED (FUSELAGE) · airframe 41,264 hrs · 26,276 cycles

FOUND STUB FRAME BS 985 RT SIDE TO BE MISDRILLED AND CRACKED AT TWO SHEAR TIE LOCATIONS. REMOVED AND REPLACED STUB FRAME AT BS 985 PER SRM 51-30-02.

Part: SHEAR TIE — DAMAGED (FUSELAGE) · airframe 41,264 hrs · 26,276 cycles

REPAIR SHEAR TIE BS 380 BETWEEN STR 15L & 16L TO ACCOMPLISH 9G MOD. REPAIRED SHEAR TIE AT BS 380 BETWEEN STR 15L & 16L PER SRM 53-10-4.

Part: FLAP TRACK — CORRODED (TE FLAPS) · corrosion level 2 · airframe 41,264 hrs · 26,276 cycles

NR 1 FLAP TRACK FWD I/B ATTACH LUG CORRODED. REPLACED PER FED EX W/C 27X5707-03.

Part: SHEAR TIE — DAMAGED (FUSELAGE) · airframe 41,264 hrs · 26,276 cycles

REPAIR SHEAR TIE BS 380 BETWEEN STR 14L & 15L TO ACCOMPLISH 9G MOD. REPAIRED SHEAR TIE AT BS 380 BETWEEN STR 14L & 15L PER SRM 53-10-4.

Part: FLAP TRACK — CORRODED (TE FLAPS) · corrosion level 2 · airframe 41,264 hrs · 26,276 cycles

NR 3 FLAP TRACK AFT MOUNTING PAD CORRODED. REPLACED NR 3 FLAP TRACK PER FED EX W/C 27X5705-03.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 41,264 hrs · 26,276 cycles

WHILE WORKING BARRIER MOD FOUND STR 16 LT INTERCOSTAL CRACKED AT BS 354. REPAIRED PER SRM 51-40-3.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 41,264 hrs · 26,276 cycles

CORROSION SPOTS UNDER FLOORBEAM LOWER SURFACE AROUND NUT CLIP HOLES AT BS 1070 FROM LBL 42 TO RBL 21, WL 200 IN THE AFT CARGO BAY. BLENDED CORROSION ON LOWER SURFACE OF BS 1070 FLOORBEAM LOWER CHORD FROM RBL 21- LBL 42 WL 200, FOUND AREA RBL 21-LBL 4 TO BE WITHIN LIMITS PER SRM 53-10-1 FIG 4 AND AREA LBL 4.5- 42 TO BE OUT OF LIMITS PER SRM 53-10-1 FIG 4, REMOVED DAMAGED SECTION OF BS 1070 FLOORBEAM LBL 3-42 WL 200 FABRICATED REPAIR LWR CHORD FROM 60-3251, 7075T6511 EXT LOT 617089 AND INSTALLED REPAIR TO BS 1070 LWR CHORD FLOORBEAM RBL 3 - LBL 42 WL 200, ALL WORK ACCOMPLISHED PER FEDEX SR27-53-034E.

Part: SHEAR WEB — CORRODED (FUSELAGE) · airframe 41,264 hrs · 26,276 cycles

CORROSION ON SHEAR WEB WITH 100 PERCENT MATERIAL LOSS AT BS 1140-1145, LBL 57-62, WL 208. REPLACED SHEAR WEB PER SRM 51-40-2

Part: SKIN — CRACKED (PAX DOOR) · airframe 41,264 hrs · 26,276 cycles

N00261, MAIN ENTRY DOOR EXTERIOR SKIN SHOWS EVIDENCE OF A CRACK AT PREVIOUS REPAIR, 9 INCHES BELOW AFT SIDE OF DOOR HANDLE. INSTALLED REPAIR DOUBLER IAW SRM 52-00-3.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 41,264 hrs · 26,276 cycles

N01607, WHILE WORKING N00929, CORROSION ON SKIN BS 698, FOUND CRACK AND OVERSIZED FASTENER HOLE WITH LIMITED EDGE MARGIN ON SHEAR TIE BS 700 BETWEEN STR 28L AND STR 28R, WL 148. REMOVED AND REPLACED SHEAR TIE IAW SRM 53-10-4.

Part: STIFFENER — CRACKED (FUEL CELL) · airframe 41,264 hrs · 26,276 cycles

RIGHT WING INTERIOR FUEL CELL UPPER STIFFENER NR 10 IS CRACKED AT WS 686.5. REPAIRED FUEL CELL UPPER STIFFNER NR 10 AT WS 686.5 PER EA 7-5710-86251.

Part: STIFFENER — CRACKED (FUEL CELL) · airframe 41,264 hrs · 26,276 cycles

RIGHT WING INTERNAL FUEL CELL UPPER STIFFENER NR 9 IS CRACKED AT WS 656.5. REPAIRED PER E.A. 7-5710-86251.

Part: SKIN — DAMAGED (FUSLEAGE) · airframe 41,264 hrs · 26,276 cycles

N01530, REPAIR AT EXTERNAL DOUBLER BS 1195 BETWEEN STR 20R TO STR 22R 12 INCHES BY 9 INCHES NEEDS EVALUATION TO DETERMINE IAW SRM OR APPROVED DATA. REMOVED AND REPLACED DOUBLER IAW SRM 51-30-3 FIG 1.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 41,264 hrs · 26,276 cycles

N01608 WHILE WORKING N00929, CORROSION ON SKIN BS 698, FOUND CORROSION ON FRAME FORMED SHEAR TIE BS 700 BETWEEN STR 28L TO STR 28R, WL 148. REPAIRED SHEAR TIE PER SRM 53-10-4.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 41,264 hrs · 26,276 cycles

REPAIR AT EXTERNAL DOUBLER BS 300 TO BS 308, RBL 41, WL 170, 8 INCHES BY 6 INCHES NEED EVALUATION TO DETERMINE PER SRM OR APPROVED DATA. *S/D* INSTALLED REPAIR DOUBLER PER SRM 53-30-3.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 41,264 hrs · 26,276 cycles

REPAIR AT EXTERNAL DOUBLER BS 1304 TO BS 1320 BETWEEN STR 16R TO STR 18R, 16 INCHES BY 9 INCHES NEEDS EVALUATION TO DETERMINE PER SRM OR APPROVED DATA. *S/D* FOUND DOUBLER NOT TO BE DONE PER SRM, REPLACED DOUBLER PER SRM 53-30-3 FIG 3.

Part: SKIN — CORRODED (FUSELAGE) · airframe 41,264 hrs · 26,276 cycles

CORROSION ON SKIN BS 698 BETWEEN STRINGERS 28 LT & 28 RT. REPAIRED SKIN AT BS 698 BETWEEN STRINGERS 28 LT AND 29 RT PER SRM 53-30-3.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 41,264 hrs · 26,276 cycles

RIGHT HORIZONTAL STAB, INTERIOR RIB WEB CRACKED L/E STA 131, 2 INCHES FROM FWD EDGE ALONG TOP. *S/D* REPAIRED FRONT SPAR WEB, RIGHT STAB LEADING EDGE STA 131 PER SRM 55-10-4.

Part: DOOR FRAME — GOUGED (CARGO DOOR) · airframe 41,264 hrs · 26,276 cycles

MAIN CARGO DOOR AFT SIDE FRAME PREVIOUS REPAIR GOUGED 18 INCHES FROM BOTTOM OF DOOR. REMOVED AND REPLACED REPAIR ON MCD AFT SIDE FRAME PER SRM 51-20-1.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,264 hrs · 26,276 cycles

FRAME IS CRACKED AT BS 620, LBL 8, WL 157. REMOVED EXISTING REPAIR, FABRICATED DOUBLER, SHEAR TIE AND INSTALLED DOUBLER, AND SHEAR TIE. IAW SRM 53-10-4.

Part: WEB — CRACKED (FUSELAGE) · airframe 41,264 hrs · 26,276 cycles

BS 760, RBL 61, WL 206 FLOOR SUPPORT WEB IS CRACKED. *S/D* REPAIRED PER SRM 51-40-2.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 41,264 hrs · 26,276 cycles

CORROSION ON SHEAR TIE BS 950E, STR 26L. *S/D* REPAIRED PER SRM 53-10-4.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 41,264 hrs · 26,276 cycles

CORROSION ON SHEAR TIE, FWD SIDE, BS 1110, AT STR 28L AFT CARGO BAY. REPAIRED PER SRM 53-10-4 AND 51-30-2.

Part: FLOORBEAM — DAMAGED (FUSELAGE) · airframe 41,264 hrs · 26,276 cycles

BS 950, BL 59, WL 200, MECHANICAL DAMAGE ON LWR FLOORBEAM ANGLE. REPAIRED PER SRM 51-30-5, 51-30-6, 51-20-1

Part: STRINGER — CORRODED (FUSELAGE) · airframe 41,264 hrs · 26,276 cycles

BS 585 STR 24 LT IS DENTED AND GOUGED. REPAIRED STR 24 LT, BS 585 PER SRM 53-10-1, SRM 53-10-3 AND MM 51-20-151.

Part: SPLICE — CORRODED (STRINGER) · airframe 41,264 hrs · 26,276 cycles

CORROSION ON STRINGER SPLICE AT BS 678 STRINGER 28L. INSTALLED NEW STRINGER SPLICE AT BS 678, STR 28L IAW SRM 51-30-2 & SRM 51-10-2.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,264 hrs · 26,276 cycles

BS 480, STRINGER 26 RT IS CORRODED. REMOVED CORROSION, OUT OF LIMITS PER SRM, REPLACED STR 26 RT AT BS 480 TO BS 510, IAW SRM 53-10-3 AND 51-30-2.

Part: FRAME — CHAFED (FUSELAGE) · airframe 41,264 hrs · 26,276 cycles

BS 1148, STR 22 LT UPPER FRAME FLANGE IS CHAFED BY HYDRAULIC LINE. *S/D* REPAIRED EPR SRM 53-10-1, 51-40-3.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 41,264 hrs · 26,276 cycles

CORROSION OF SHEAR TIE FWD SIDE BS 1050, AT STR 27, AFT CARGO BAY. REPAIRED PER SRM 53-10-4.

Part: FRAME — DENTED (FUSELAGE) · airframe 41,264 hrs · 26,276 cycles

FRAME IS DENTED ON I/B FLANGE AT BS 500 BETWEEN STR'S 23 LT AND 25 LT. REMOVED DAMAGE ON FRAME BS 500 BETWEEN STR 23L AND 25L. FABRICATED DOUBLER, MATERIAL 7075-T6 0.63", LOT #181795 IAW SRM 51-40-3, ALODINED, PRIMED, INSTALLED PER SRM 51-20-2, MM 51-20-151-7, SRM 51-30-2

Part: STRINGER — DENTED (FUSELAGE) · airframe 41,264 hrs · 26,276 cycles

BS 592 STR 23 LT IS DENTED. REPAIRED PER SRM 53-10-3

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 41,264 hrs · 26,276 cycles

CORROSION ON SHEAR TIE BS 970 STR 29R -30R OUT OF LIMITS. REMOVED CORROSION FOUND TO BE OUT OF LIMITS PER SRM 53-10-1 REPARIED PER SRM 53-10-4

Part: FRAME — DENTED (FUSELAGE) · airframe 41,264 hrs · 26,276 cycles

FRAME IS DENTED ON I/B FLANGE AT BS 660 BETWEEN STR'S 23 LT AND 25 LT. REPAIRED PER SRM 51-40-3

Part: STRINGER CLIP — DAMAGED (FUSELAGE) · airframe 41,264 hrs · 26,276 cycles

MECHANICAL DAMAGE ON STRINGER CLIP AT BS 660, STR 13L. REPLACED PER SRM 51-30-2.

Part: FRAME — DENTED (FUSELAGE) · airframe 41,264 hrs · 26,276 cycles

FRAME IS DENTED ON I/B FLANGE AT BS 680 BETWEEN STR'S 23 LT AND 25 LT. REPAIRED PER SRM 51-40-3

Part: STRINGER — GOUGED (FUSELAGE) · airframe 41,264 hrs · 26,276 cycles

BS 592 STR 25 LT IS GOUGED. REPAIRED IAW SRM 53-10-3

Part: FRAME — DENTED (FUSELAGE) · airframe 41,264 hrs · 26,276 cycles

FRAME IS DENTED ON I/B FLANGE AT BS 560 BETWEEN STR'S 24 LT AND 25 LT. REPAIRED PER SRM 51-40-3, 51-10-2, MM 51-20-151-7 AND SRM 51-30-2

Part: STRINGER CLIP — MISDRILLED (FUSELAGE) · airframe 41,264 hrs · 26,276 cycles

BONUS HOLES IN STRINGER CLIP AT BS 970 STRINGER 7R. REPLACED EPR SRM 51-30-2.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 41,264 hrs · 26,276 cycles

BS 950 LBL 11, WL 208 CORROSION ON FLOORBEAM (OUT OF LIMITS). REPAIRED BS 950 FLOOR BEAM LBL 11 WL 208 FED EX EA 7-5310-86259.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 41,264 hrs · 26,276 cycles

CORROSION ON LOWER SIDE OF FLOORBEAM AT BS 1130, LBL 45 TO RBL 45, WL 200.

Part: STRINGER CLIP — DAMAGED (FUSELAGE) · airframe 41,264 hrs · 26,276 cycles

BONUS HOLES IN STRINGER CLIP AT BS 950F STR 7R. REPLACED PER SRM 51-30-2.

Part: DOOR FRAME — CRACKED (GALLEY DOOR) · airframe 41,264 hrs · 26,276 cycles

FWD GALLEY DOOR POSSIBLE CRACK IN DOOR FRAME NEXT TO LWR LATCH ROLLER. REMOVED AND REPLACED FWD SIDE FRAME OF DOOR IAW SRM 51-10-2, 51-00-4.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 41,264 hrs · 26,276 cycles

CORROSION SPOTS UNDER FLOORBEAM LOWER SURFACE AT BS 1130 LBL 43 TO RBL 52, WL 200 IN AFT CARGO BAY. FLOOR BEAM WILL BE REPLACED ON N01035, INTERIOR 5081 AT BS 1130, LBL 65 TO RBL 65 LOWER CHORD.

Part: FLOORBEAM — CORRODED (FUSLEAGE) · airframe 41,264 hrs · 26,276 cycles

CORROSION ON LOWER SIDE OF FLOORBEAM AT BS 1070, LBL 1 TO LBL 45, WL 200. WORK TO BE ACCOMPLISHED ON CUSTOMER CARD N01219

Part: STRINGER CLIP — DAMAGED (FUSELAGE) · airframe 41,264 hrs · 26,276 cycles

BONUS HOLES IN STRINGER CLIP AT BS 950C STR 7R. REPLACED PER SRM 51-30-2.

Part: STRINGER CLIP — MISDRILLED (FUSELAGE) · airframe 41,264 hrs · 26,276 cycles

BONUS HOLES IN STRINGER CLIP AT BS 950A STR 7L. REPLACED PER SRM 51-30-2

Part: STRINGER CLIP — MISDRILLED (FUSELAGE) · airframe 41,264 hrs · 26,276 cycles

BONUS HOLES IN STRINGER CLIP AT BS 950C STR 7L. REPLACED PER SRM 51-30-2

Part: STRINGER CLIP — DAMAGED (FUSELAGE) · airframe 41,264 hrs · 26,276 cycles

BONUS HOLES IN STRINGER CLIP AT BS 950A STR 7R. REPLACED PER SRM 51-30-2.

Part: STRINGER CLIP — MISDRILLED (FUSELAGE) · airframe 41,264 hrs · 26,276 cycles

BONUS HOLES IN STRINGER CLIP AT BS 950F STR 7L. REPLACED PER SRM 51-30-2

Part: STRINGER — TOOL DAMAGE (FUSELAGE) · airframe 41,264 hrs · 26,276 cycles

TOOLING DAMAGE AT BS 1010 STRINGER 7L IN STRINGER CLIP AND STRINGER SPLICE. REPAIRED PER SRM 53-10-2 (DUPLICATE ENTRY TO TRACKING NR 05-0336)

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,264 hrs · 26,276 cycles

BS 720D, RBL 4, WL 208 CORROSION ON FLOORBEAM. REPAIRED PER SRM 53-10-8

Part: SKIN — GOUGED (TE FLAPS) · airframe 41,264 hrs · 26,276 cycles

LT IB MID FLAP UPPER SURFACE IS GOUGED AT OB END 13 INCHES FROM LE. BLENDED GOUGE ON LT IB MIDFLAP OB END PER FEDEX EA 7-5710-86252

Part: STRINGER — TOOL DAMAGE (FUSELAGE) · airframe 41,264 hrs · 26,276 cycles

TOOLING DAMAGE AT BS 1010 STRINGER 7L IN STRINGER CLIP AND STRINGER SPLICE. REPAIRED PER SRM 53-10-2.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,264 hrs · 26,276 cycles

CORROSION IN STRINGER 26R, AFT OF BS 1148, AFT CARGO BAY.

Part: COALESCER BAG — CONTAMINATED (CABIN AIR) · airframe 40,335 hrs · 25,588 cycles

AT FL310, 1 HOUR AFTER LEVEL-OFF, THE ENTIRE CREW AND JUMPSEATER NOTICED AN OBVIOUS ODOR OF SMOKE. ACCOMPLISHED EMERGENCY DESCENT AND LANDING. NO FURTHER SMOKE DETECTED AFTER LANDING, NORMAL SHUTDOWN. FAINT SMELL AGAIN NOTED, SEEMED TO BE FROM C/B PANELS IN LEFT REAR OF COCKPIT. FIRE CREW ALSO NOTICED A FAINT ODOR. NO CARGO OR APU OR FIRE SMOKE OR FIRE WARNING WENT OFF. ODOR WAS STRONGEST BEHIND AND RIGHT OF F/O BEHIND ENGINEERS PANEL. RAN APU WITH BOTH PACKS, RAN ENGINES WITH BOTH PACK PER JRH CHAPTERS 5 & 7. SMELLED MORE LIKE DEICING FLUID, CHANGED OUT COALESCER BAG PER REF 21-55 -051-4, ODOR HAS DISSIPATED, OK FOR RETURN TO SERVICE.

Part: ACTUATOR — FAILED (KRUGER FLAPS) · airframe 40,327 hrs · 25,583 cycles

NR 3 KRUEGER FAILED TO EXTEND ON APPROACH TO KRST, C/W RED TABS DIVERT TO KMSP. REMOVED AND REPLACED THE NR 3 KRUEGER FLAP ACTUATOR AND THE L/E FLAP-SLAT POSITION CONTROL MODULE IAW MM 27-81-22 AND MM 27-82-031-4.

Part: TIRE — FAILED (MLG) · airframe 40,246 hrs · 25,526 cycles

SHORTLY AFTER TAXI OUT FROM OAK RAMP, HEARD A VERY LOUD BANG AND AIRCRAFT SHUDDERED SLIGHTLY. BROUGHT THE AIRCRAFT TO A SLOW STOP. ENGINE INDICATIONS NORMAL. REQUESTED FEDEX MX INSPECTION. BLOWN NR 3 TIRE NOTED BY MX. TOWED BACK TO RAMP.

Part: ENGINE — LEAKING (NR 1) · airframe 39,844 hrs · 25,218 cycles

AT FL 330 NR 1 OIL QTY WENT RAPIDLY TO ZERO. OIL PRESS DROPPED TO 30 PSI. ENGINE SHUTDOWN IAW RED TABS. REMOVED AND REPLACED NR 1 ENG ASSY AS PER WORK CARD 70T0001-01, A/C OK FOR SERVICE.

Part: CONTROL UNIT — FAULTY (E/E BAY) · airframe 39,700 hrs · 25,105 cycles

REPEAT WRITEUP. ENG NR 1 STRUT OVERHEAT LIGHT ILLUMINATED ON CLIMBOUT. COMPLIED WITH RED TABS AND LIGHT EXTINGUISHED WHEN NR 1 BLEED AIR SWITCH CLOSED AND LEFT, PACK TURNED OFF. REMAINED OFF FOR REST OF FLIGHT. INSPECTED NR 1 STRUT OVHT. DETECTOR SENSOR CONNECTORS NO DAMAGE NOTED, CLEANED CONNECTOR ENDS WITH CONTACT CLEANER. AFTER READING WIRING DIAGRHAM ENCH ENG. STRUT HAS A SEPARATE CONTROL UNIT INSIDE THE FIRE AND OVHT.DET. MODULE REMOVED AND REPLACED THE FIRE AND OVHT. DET. MODULE UNIT IAW MM 26-14-000-0 SYS OPS CK GOOD IAW MM 26-14-00-5.

Part: SHIM — BROKEN (STARTER DUCT)

02-46 #1 ENG STRUT OVERHEAT LIGHT ILLUM ON CLBOUT. R&R SHIM ON STARTER DUCT. OPS CK GOOD.

Part: FIRE WARNING — MALFUNCTIONED (COCKPIT)

ON TAKEOFF FIRE WARNING BELL CUTOUT LIGHTS ILLUMINATED. NEEDS BELL CUTOUT SWITCH. NO DEFECTS NOTED. AC OK TO CONTINUE.

Part: UNKNOWN — ODOR (COCKPIT)

01-190 AT FLT LEVEL 330 FLT CREW SMELLED ODOR IN COCKPIT. AIRCRAFT WAS DOWNLOADED & CANS CHECKED FOR ODOR. CHECK A/C PACKS, CND.

Part: STRUT — OVERHEATED (NR 1 ENGINE)

NR 1 ENG STRUT OVERHEAT LIGHT AT TAKEOFF ROTATION FOLLOWED RED TABS. *S/D* REMOVED AND REPLACED NR 1 STRUT LOOP. CK OK PER MM 26-14-001-2. NO LEAKS FOUND. OK FOR SERVICE.

Part: WARNING LIGHT — FALSE INDICATION (NR 1 ENGINE)

NR 1 ENGINE STRUT OVERHEAT LIGHT ILLUM AFT T/O. LIGHT WENT OUT AFT 2 MIN. SYS TEST GOOD. INSPECTED DUCTING AND OVERHEAT LOOP, NO DISCREPANCIES NOTED. TEST GOOD PER MM 26-14-000-5.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 37,031 hrs · 23,064 cycles

DURING ROUTINE INSPECTION, CRACK FOUND IN WEB FWD OF BS 1183 BULKHEAD, LBL 50 AT FLOOR LEVEL. REMOVED, FABRICATED AND INSTALLED PER IAW SRM 51-20-1 & SRM 51-30-2.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 37,031 hrs · 23,064 cycles

DURING ROUTINE INSPECTION, CRACK FOUND IN WEB AT FWD SIDE OF BS 1183 BULKHEAD, RBL 47 AT FLOOR LEVEL. REMOVED, FABRICATED AND INSTALLED PER IAW SRM 51-40-2 & SRM 51-30-2.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 37,031 hrs · 23,064 cycles

DURING ROUTINE INSPECTION, FOUND CRACK IN WEB FWD BS 1183 BULKHEAD, RBL 17 AT FLOOR LEVEL. REMOVED, FABRICATED, AND INSTALLED PER IAW SRM 51-20-1 & SRM 51-30-2.

Part: COMPRESSOR — STALLED (ENGINE)

UPON GEAR RETRACTION EXPERIENCED COMPRESSOR STALL ACCOMPANIED LOUD BANG/SHUDDER, DECREASE AND RECOVERY OF NR 2 EPR, LEFT PACK TRIPPED OFF ON AUTO PACK TRIP. COMPLIED WITH CTR ENG COMPRESSOR STALL CK FOR HIGH PWR STALL. INSPECTED ENG INLET AND EXHAUST AREAS, NO DAMAGE NOTED. NO PREVIOUS HISTORY OF STALL. SUSPECT CROSSWINDS. A/C OK FOR CONT SERVICE AS PER 727- 200 MM 71-00-000-6.

Part: CAP — MISSING (FLOW CONTROL)

00-48 CLIMBING TOWARD 10K CABIN DIFFERENTIAL PRESS WOULD NOT GO ABOVE 5 PSI, SWAPPING BLDS MADE NO DIFFERENCE. INSTALLED CAP GOING FROM RT FLOW CTRL VALVE TO HI-PRESS REG. VALVE. OPER CK GOOD. OK FOR SERVICE.

Part: ACCESSORY UNIT — MALFUNCTIONED (E & E COMPT)

99-206 - RT MLG RED LIGHT INTERMITTENT ON. CYCLED GEAR HANDLE FROM OFF TO UP AND GROUND LIGHT EXT. REMOVED AND REPLACED LANDING GEAR ELECTRONIC MODULE PER 727-200 MM 32-09-121-5.

Part: TRANSMITTER — MALFUNCTIONED (NR 3 ENGINE)

99-0012 - NR 3 ENG LOW OIL PRESS LIGHT ILLUM AFT T/O. ACCOMPLISH ABNORMAL CK LIST WHICH REQUIRE SHUTDOWN. FOUND BLEED AIR DUCT AT STARTER BLOWN. REMOVED AND REPLACED NR 3 OIL PRESSURE TRANSMITTER,SWITCH PER 727 MM 79-32-1,79-33-1. REMOVED AND REPLACED STARTER SUPPLY DUCT, FUEL HOSE ASSY PER MM 80-11-11, 77-00.

Part: BELLFRAME — CORRODED (BS 970)

AFT CARGO BELLFRAME LWR CHORD CORRODED AT BS 970, WL 138 O/B OF STR 29R, RBL 12. CUT OUT DAMAGED AREA AND REMOVED CORROSION PER SRM 51-10-6, INSTALLED SHEAR TIE REPAIR PER SRM 53-10-4.

Part: SKIN — CORRODED (BS 1055)

LOWER FUSELAGE, BS 1055, HEAVY CORROSION ON FUSE SKIN (BLOW OUT), JUST ABOVE STR 28R. *S/D* INSTALLED SKIN DOUBLER PER SRM 53-30-3.

Part: SKIN — CORRODED (BS 990)

LOWER FUSELAGE, BS 990 HEAVY CORROSION ON FUSE SKIN (BLOWOUT) AT STR 29R. *S/D* INSTALLED DOUBLER BS 990, STR 29R PER SRM 5.

Part: SKIN — CORRODED (BS 700)

NR 0427 7-5330-7-2352-P2 SKIN CORROSION BS 700 BETWEEN STR 28L AND 28R. REMOVED CORROSION TREATED AND PRIMED SKIN. INSTALLED EXTERNAL DOUBLER PER SRM 53-30-3 2024-T3 X .125.

Part: FRAME — CRACKED (BS 640)

NR 0248 NR 9115335 CRACK IN BELT FRAME AT FAST HOLE ABOVE STR 27R, BS 640. CUT OUT DAMAGED AREA INST 050 DOUBLER AND FILLER PER 51-40-3.

Part: STRINGER — CRACKED (BS 520)

NR 0849 71C208-02 STR 26L, BS 520 HAS CRACK PROPAGATING FROM STRINGER CLIP AFT I/B ATTACH HOLE. INSTALLED STRINGER REPAIR PER SRM 53-30-3, FIG 2.

Part: STRINGER — CORRODED (BS 700-720)

STR 27R CORRODED BETWEEN BS 700 AND BS 720. *S/D* REMOVED CORRODED SECTION AND INSTALLED NEW STR SECTION.

Part: DUCT — LEAKED (NR 3 ENGINE)

NR 3 ENGINE, FIRE WARNING INDICATION ON TAKEOFF ROLL. BOTH FIRE BOTTLES WERE DISCHARGED. FOUND 8TH STAGE DUCT NR 3 ENGINE BLOWN. REMOVED AND REPLACED DUCT AND BOTH FIRE BOTTLES, LEAK CHECKED GOOD. ENGINES RAN.

Part: OVERHEAT LOOP — OUT OF POSITION (LWR AFT FUS)

LOWER AFT BODY OVERHEAT LIGHT FLASHED ON AND OFF INTERMITTENTLY IN FLIGHT, BOTH PACKS ON BLEEDS 1 ENGINE 2 APU BLEED AND ENGINE 3 BLEED OPEN. LIGHT DOES NOT STAY ILLUMINATED LONG ENOUGH TO ISOLATE PROBLEM USING ABNORMAL CHECK LIST. ALSO, AFT CARGO SELECTED ON LOWER AFT BODY OVERHEAT COMPARTMENT SELECTOR SWITCH LOWER AFT BODY OVER HEAT LIGHT COMES ON INTERMITTENTLY. FOUND LOOP TOO CLOSE TO FLIGHT RECORDER CASING AND SEVERAL INSULATING GROMMETS IMPROPERLY INSTALLED. REPOSTIONED LOOP AND GROMMETS, CHECKED LOOP AT B-BELLY AFT BULKHEAD. RAN APU AND PACKS WITH AFT AIRSTAIR CLOSED TO CHECK FOR HEAT SENSITIVITY.

Part: OVERHEAT LOOP — OUT OF POSITION (LWR AFT FUS)

LWR AFT BODY OVERHEAT LIGHT BLINKED ON MOMENTARILY ONCE WHILE IN FLIGHT. REMOVED GILLINER PANELS LOWER AFT CARGO COMPARTMENT. INSPECTED SENSOR, FOUND NUMEROUS SPOTS SENSOR RUBBING METAL BRACKETS. REPOSITIONED SAME, REMOVED KEEL BEAM PANEL, INSPECTED SENSOR AND CHECKED GOOD. LEAK CHECK SYSTEM, MANY SMALL LEAKS AFT STAIR AREA. TIGHTEN CLAMPS RAN ENGINE AND APU NO LEAK NOTED. NO OVERHEAT NOTED, CLOSED ALL PANELS AND STILL NO OVERHEAT INDICATIONS NOTED.

Part: DOOR — REQ RIG (FWD ENTRY)

FWD ENTRY DOOR OPENED APPROX 3 0R 4 INCHES AFTER A/C WAS DEPRESSURIZED ON TAXI IN AT MEM. RIGGED DOOR IAW MM 52-11-01, PG 514 (3 A-D). REINSTALLED LINER AND SLIDE.