N499FE

Part: WIRE — BROKEN (KRUEGER FLAP) · airframe 52,414 hrs · 43,354 cycles

DURING FLAP RETRACTION AT FLAPS 2 DEG UNSAFE LED INDICATION FOR NR 5 LED. COMPLIED WITH QRH, DIVERTED TO INDY. T/S AND FOUND BURNT/BROKEN WIRE AT WIRE LOOM AFT OF NR 5 KRUEGER FLAP SWITCH ASSY. REPAIRED BROKEN WIRE REF B-727-200 SWP'S CH 20. SYSTEM OPERATES NORMALLY AT THIS TIME. OK FOR SERVICE.

Part: FITTING — BROKEN (LT WING) · airframe 52,096 hrs · 43,075 cycles

LEFT MLG LOWER TRAILING EDGE PANEL ATTACH BRACKET COMMON TO THE NR 7 SPOILER ACTUATOR FITTING IS BROKEN. REPAIRED L/H T/E CHORD PER FED-EX E.A. 7-5710-91398.

Part: STRUCTURE — CHAFED (NACELLE) · airframe 52,096 hrs · 43,075 cycles

NR 2 ENGINE BS 1342, MATING SURFACE FOR RT FWD COWL CHAFED, WORN TO KNIFE EDGE AT 5:30 TO 6:00 O'CLOCK POSITION. REPLACED 1342 CHORD PER SRM 51-30-2.

Part: RIB — CRACKED (TE FLAP) · airframe 52,096 hrs · 43,075 cycles

R/W I/B MID FLAP TE RIB IS CRACKED AT IB AFT FLAP PUSHROD CUT OUT. REMOVED CRACKED SECTION & INSTALLED NEW SECTION IAW SRM 51-40-4.

Part: STOP FITTING — GOUGED (CARGO DOOR) · airframe 52,096 hrs · 43,075 cycles

FWD CARGO BAY DOOR, FWD LOWER DOOR STOP FITTING IS GOUGED. INSTALLED NEW FWD CARGO DOOR FWD LWR DOOR STOP FITTING PER SRM 51-30-2.

Part: KEELBEAM — CORRODED (BS 905E) · airframe 52,096 hrs · 43,075 cycles

STA 950E 2 STR 29R CORROSION ON STR FLANGE. REPAIRED STRINGER AT BS 950E 2, 29R PER FED EX EA 7-5310-91393

Part: STOP FITTING — GOUGED (CARGO DOOR) · airframe 52,096 hrs · 43,075 cycles

FWD CARGO BAY DOOR, AFT LOWER DOOR STOP FITTING IS GOUGED. INSTALLED NEW FWD CARGO DOOR, AFT LWR DOOR STOP FITTING PER SRM 51-30-2.

Part: INTERCOSTAL — CORRODED (LT MLG WW) · airframe 52,096 hrs · 43,075 cycles

WHILE PERFORMING BUYBACK OF UPLOCK OF THE LT MLG WW, FOUND INTERCOSTAL CORRODED ON THE UPPER SURFACE, BS 900 TO BS 905, LBL 68, 12 BELOW CEILING. REPLACED INTERCOSTAL IN LT MLG WW, BS 900-905, LBL 68 PER SRM 51-.30-2.

Part: STIFFENER — CORRODED (BS 870) · corrosion level 2 · airframe 52,096 hrs · 43,075 cycles

CORROSION, C53-100-01, FOUND HORIZONTAL STIFFENER CORRODED AT CLAMP STANDOFF, BS 870, WL 198 LBL 8. REPLACED STIFFENER AT BS 870, LBL 6 WL 198 PER SRM 51-30-2.

Part: FRAME — DENTED (CARGO DOOR) · airframe 52,096 hrs · 43,075 cycles

FWD CARGO BAY DOOR LOWER CHORD IS DENTED AND CHAFED FROM CENTER TO AFT CORNER. REMOVED AND REPLACED LOWER CENTER CHORD IAW SRM 51-30-2.

Part: STOP FITTING — GOUGED (CARGO DOOR) · airframe 52,096 hrs · 43,075 cycles

N00460 FWD CARGO BAY DOOR, FWD 2ND UP FROM BOTTOM STOP FITTING IS GOUGED. INSTALLED NEW FWD CARGO DOOR, FWD 2ND UP FROM THE BOTTOM DOOR STOP FITTING PER SRM 51-30-2.

Part: FAILSAFE — CORRODED (BS 1148 FRAME) · corrosion level 2 · airframe 52,096 hrs · 43,075 cycles

STA 1148 LBL 12 CORROSION ON BULK CARGO FRAME FAILSAFE CHORD. REPLACED STIFFENER AT BS 1148 LBL 12 PER 51-40-4.

Part: FITTING — CORRODED (DOOR HANDLE) · airframe 52,096 hrs · 43,075 cycles

LEFT FWD EMERGENCY ESCAPE DOOR, ACCESS HANDLE CLOSURE FRAME CORRODED. REPLACED LT FWD EMERGENCY ESCAPE DOOR ACCESS HANDLE CLOSURE FITTING PER SRM 51-30-2.

Part: HANDLE — CORRODED (ESCAPE DOOR) · airframe 52,096 hrs · 43,075 cycles

RT FWD EMERGENCY ESCAPE DOOR, ACCESS HANDLE CLOSURE FRAME IS CORRODED. REPLACED RT FORWARD EMERGENCY ESCAPE DOOR ACCESS HANDLE CLOSURE FITTING PER SRM 51-30-2.

Part: STRINGER CLIP — CRACKED (BS 1110) · airframe 52,096 hrs · 43,075 cycles

STA 1110 STR 28R STRINGER CLIP CRACKED. REPLACED STRINGER CLIP AT B.S. 1110 STR 28R PER SRM 51-30-2.

Part: FRAME — DAMAGED (BS 950F) · airframe 52,096 hrs · 43,075 cycles

MAIN CARGO BAY, MECHANICAL DAMAGE TO FRAME BS 950F BETWEEN STRINGER 4 LT AND 5 LT. REPAIRED FRAME AT BS 950F BETWEEN STR 4L & 5L PER SRM 53-10-4

Part: FLOORBEAM — CORRODED (BS 1148) · airframe 52,096 hrs · 43,075 cycles

REMOVAL OF BL 0 TENSION STRAP ON FED EX CARD, FOUND CORROSION ON LWR FLANGE OF FLOORBEAM AT B/S 1148, WL 200 BL 0. REPAIRED FLOORBEAM AT B.S. 1148, BL0, WL 200 PER SRM 53-10-8.

Part: FLOORBEAM — CORRODED (BS 950) · airframe 52,096 hrs · 43,075 cycles

CORROSION AT BS 950 LBL 48-53 WL 207 AT UNDERSIDE OF FLOORBEAM . ALL WORK ACCOMPLISHED IAW FED EX EA 7-5310-91391.

Part: FRAME — CORRODED (BS 1166) · corrosion level 2 · airframe 52,096 hrs · 43,075 cycles

CORROSION, STA 1166 RBL 20 TO LBL 20 CORROSION ON BULK CARGO FRAME UPPER FLANGE. REPAIRED FRAME AT BS 1166 RBL 20 TO LBL 20 PER SRM 51-40-3

Part: FLOORBEAM — CORRODED (BS 950) · airframe 52,096 hrs · 43,075 cycles

CORROSION AT FLOORBEAM BS 950 RBL 48-54 WL 208 AT NUT PLATE HOLES. REPAIRED FLOORBEAM PER FED EX EA 7-5310-91395.

Part: SKIN — MISSING (CARGO DOOR) · airframe 52,096 hrs · 43,075 cycles

MAIN CARGO DOOR LOWER AFT CORNER HAS A PIECE OF EXTERIOR SKIN MISSING. REPAIRED MAIN CARGO DOOR SKIN PER FED EX EA 7-5230-93692A

Part: FLOORBEAM — CORRODED (BS 560) · airframe 52,096 hrs · 43,075 cycles

CORROSION ON TOP FLOORBEAM BS 560 BL 0 TO RBL 50 AROUND NUT PLATES HOLES. REPAIRED FLOORBEAM IAW SRM 53-10-1.

Part: KEELBEAM — CRACKED (BS 805) · airframe 52,096 hrs · 43,075 cycles

FOUND CRACK IN THE DELTA KEELBEAM LWR FLANGE AT B/S 805 RBL 6 WL 148. REPAIRED DELTA KEELBEAM, BS 805, RBL6, WL 148 PER FED-EX EA 7-5310-91384.

Part: SKIN — MISREPAIRED (BS 385-396) · airframe 52,096 hrs · 43,075 cycles

EXISTING REPAIR BS 385 TO 396 STR 26L TO 27L 11"L X 7.5W. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPLACED REPAIR AT BS 385 TO 396, STR 26L-27L PER SRM 53-30-3.

Part: FRAME — DENTED (BS 660) · airframe 52,096 hrs · 43,075 cycles

DENT IN FRAME BETWEEN STR 24R-25R BS 660. REPAIRED DENT IN FRAME AT B.S. 660, STR 24R-25R PER SRM 51-40-3.

Part: FRAME — DENTED (BS 660) · airframe 52,096 hrs · 43,075 cycles

DENT IN FRAME AT BS 660 STR 24L. REPAIRED DENT IN FRAME AT B.S. 660 STR 24L PER SRM 51-40-3.

Part: FRAME — DENTED (BS 560) · airframe 52,096 hrs · 43,075 cycles

FORWARD CARGO BAY, FRAME IS DENTED ON IB FLANGE AT BS 560 BETWEEN STRINGER 24 LT AND 25 LT. REPAIRED FWD CARGO BAY FRAME AT BS 560 BETWEEN STR 24LT & 25LT PER SRM 51-40-3.

Part: FRAME — DENTED (BS 520) · airframe 52,096 hrs · 43,075 cycles

FWD CARGO BAY, FRAME IS DENTED ON IB FLANGE AT BS 520 BETWEEN STR 22 LT AND 25 LT. REPAIRED PER SRM 53-10-1, 51-30-2, 51-40-3 FIG 1 MAJOR REPAIR.

Part: FRAME — DENTED (BS 520) · airframe 52,096 hrs · 43,075 cycles

FORWARD CARGO BAY, FRAME IS DENTED ON IB FLANGE AT BS 520 BETWEEN STRINGER 24 RT AND 26RT. REPAIRED FRAME AT B.S. 520 STR 24R & 26R PER SRM 51-40-3.

Part: FRAME — CORRODED (BS 660) · airframe 52,096 hrs · 43,075 cycles

CORROSION, FWD CARGO BAY (C53-111-01(2)) ON FRAME BS 660 BETWEEN BL 0 AND STRINGER 38RT (ON FWD SIDE OF FRAME). REPAIRED FRAME AT BS 660 BETWEEN BL0 AND STR 28RT IAW SRM 51-40-2.

Part: FRAME — DENTED (BS 680) · airframe 52,096 hrs · 43,075 cycles

FORWARD CARGO BAY, FRAME IS DENTED ON IB FLANGE AT BS 680 STRINGER 25 RT. REPAIRED FRAME AT BS 680 STR 25R PER SRM 51-40-3.

Part: FRAME — DENTED (BS 1050) · airframe 52,096 hrs · 43,075 cycles

FRAME DENTED AT BS 1050, BELOW STR 26R. REPAIRED FRAME AT B.S. 1050 BELOW STR 26R PER SRM 51-40-3.

Part: FRAME — DENTED (BS 1070) · airframe 52,096 hrs · 43,075 cycles

FRAME DENTED AT BS 1070, JUST BELOW STR 25R. REPAIRED FRAME AT B.S. 1070, STR 25R PER SRM 51-40-3.

Part: FRAME — DENTED (BS 970) · airframe 52,096 hrs · 43,075 cycles

FRAME DENTED AT BS 970, ABOVE STR 26L. REPAIRED PER SRM 53-10-1.

Part: FRAME — DENTED (BS 990) · airframe 52,096 hrs · 43,075 cycles

FRAME DENTED AT BS 990, BELOW STR 25L. REPAIRED FRAM AT BS 990 STR 25L PER SRM 51-40-3.

Part: BEAM — CORRODED (BS 760-848) · airframe 52,096 hrs · 43,075 cycles

CORROSION ON TOP LONGITUDINAL BEAM BS 760 TO 848.95 LBL 25 WL 208. REPAIRED PER SRM 53-10-1, 53-10-2.

Part: FLOORBEAM — CORRODED (BS 1148) · airframe 52,096 hrs · 43,075 cycles

UPON REMOVAL OF BL "0" TENSION STRAP ON FEDEX CARD, FOUND CORROSION ON LOWER FLANGE OF FLOORBEAM AT BS 1148, WL200, BL'0'. REPAIRED FLOORBEAM AT B.S. 1148, BLO, WL 200 PER SRM 53-10-8.

Part: FRAME — DENTED (BS 1130) · airframe 52,096 hrs · 43,075 cycles

FRAME DENTED AT BS 1130, STR 26L. REPAIRED FRAME AT BS 1130 STR 26L PER SRM 51-40-3

Part: FRAME — DENTED (BS 950B) · airframe 52,096 hrs · 43,075 cycles

AFT CARGO BAY, BS 950B FRAME BETWEEN STR 25R AND STR 26R HAS A DENT. REPAIRED FRAME AT BS 950B STR 26R PER SRM 51-40-3.

Part: SHEAR TIE — CORRODED (BS 950B) · airframe 52,096 hrs · 43,075 cycles

AFT CARGO BAY, SHEAR TIE IS CORRODED AT BS 950B, RBL9, WL138. REPAIRED AFT CARGO BAY, SHEAR TIE AT BS 950B, RBL 9 WL 138 IAW SRM 51-10-2, 53-10-4.

Part: FRAME — DENTED (BS 1050) · airframe 52,096 hrs · 43,075 cycles

FRAME DENTED IN 2 PLACES AT BS 1050, STR 23L AND 25L. REPAIRED FRAME AT BS 1050 STR 23L & 25L PER SRM 51-40-3.

Part: FRAME — DENTED (BS 1130) · airframe 52,096 hrs · 43,075 cycles

FRAME DENTED AT BS 1130, STR 26L. REPAIRED FRAME AT BS 1130 STR. 26L PER SRM 51-40-3.

Part: KEELBEAM — DAMAGED (BS 740) · airframe 52,096 hrs · 43,075 cycles

LT AC BAY, BS 740 TO 800 KEELBEAM LWR WEB, 4 LIGHTNING HOLES HAVE OUT OF ROUND HOLES AND ARE MISSING STRESS BEVELS. REPAIRED LOWER KEELBEAM WEB PER SRM 51-40-2.

Part: FRAME — DENTED (BS 950C) · airframe 52,096 hrs · 43,075 cycles

AFT CARGO BAY, FRAME IS DENTED AT BS 950C BETWEEN STR 25R AND STR 26R. REPAIRED FRAME AT BS 950C, STR 25R-26R PER SRM 51-40-3.

Part: KEELBEAM — CRACKED (BS 873) · airframe 52,096 hrs · 43,075 cycles

CRACK IN KEEL BEAM UPPER FLANGE AT FASTENER LOCATION ON STA 873 LBL 6. REPAIRED KEEL BEAM PER EA 7-5310-91372.

Part: STRINGER — CORRODED (BS 506.5) · airframe 52,096 hrs · 43,075 cycles

CORROSION, FORWARD CARGO BAY ON STRINGER 25 RT BS 506.5. REPAIRED STRINGER AT BS 506.5 STRINGER 25R PER SRM 53-10-3.

Part: FLOORBEAM — CORRODED (BS 1110) · airframe 52,096 hrs · 43,075 cycles

CORROSION, STA 1110 BL 0, CORROSION ON MAIN DECK FLOORBEAM LOWER CHORD. REPAIR FLOOR BEAM LOWER CHORD PER SRM 53-10-8, FIG 2.

Part: SHEAR TIE — CORRODED (BS 720) · airframe 52,096 hrs · 43,075 cycles

CORROSION, FORWARD CARGO BAY ON SHEAR TIE BETWEEN STRINGER 27 LT AND STRINGER 28 LT BS 720 (FWD SIDE OF FRAME). REPAIRED SHEAR TIE AT B.S. 720 BETWEEN STR 27L & 28L PER SRM 53-10-4.

Part: SPLICE — CORRODED (STRINGER) · airframe 52,096 hrs · 43,075 cycles

CORROSION, FORWARD CARGO BAY ON STRINGER SPLICE 26 RT BS 680 (FWD I/B SIDE). REMOVED CORROSION ON STR SPLICE FOUND TO BE WITHIN LIMITS ALL WORK DONE IAW SRM 51-10-6, 53-10-01, 51-30-2.

Part: SHEAR TIE — CORRODED (BS 720) · airframe 52,096 hrs · 43,075 cycles

CORROSION, FORWARD CARGO BAY ON SHEAR TIE BETWEEN STRINGER 28 RT AND STRINGER 28 LT BS 720 (FWD SIDE OF FRAME). FOUND TO BE OUT OF LIMITS IAW 51-10-1. REMOVED & REPLACED IAW 53-40-4 & 51-20-2.

Part: INDICATOR — FALSE INDICATION (MLG) · airframe 50,349 hrs · 41,661 cycles

ON DEPARTURE WHEN THE GEAR HANDLE WAS PUT UP THE GEAR CAME UP NORMAL THE RED GEAR DOOR LIGHT STAYED ON, GREEN GEAR LIGHTS OFF AND S/O PANEL ALL LIGHTS SHOWED NORMAL. CYCLE GEAR ONCE SAME INDICATION. PULLED GEAR INDICATION CB'S AND RECYCLED GEAR NORMAL INDICATION RECYCLE GEAR AGAIN AND NORMAL INDICATION AGAIN. DURING THE FLIGHT, A/C FLEW NORMAL AS IF GEAR AND DOORS WERE UP IVEN WHEN DOOR LIGHT REMAINED ON.

Part: POSITION SWITCH — FAILED (L/E FLAP)

WHILE RETRACT FLAPS NR 4 L/E DEVICE WOULD NOT RETRACT WHEN FLAPS MOVED FROM 5 DEG TO 2 DEG. DUMP FUEL. COULD NOT DUPLICATE. AS PRECAUTIONARY REMOVED AND REPLACED NR 4 L/E FLAP POSITION SWITCH REF B727-200 MM 27-82-001-4. REMOVED AND REPLACED CONTROL MODULE AT S/O''''S STATION MM 27-82-031-4. PERF OPS OF FLAPS NUMEROUS TIMES, OPS NORMAL.

Part: CONNECTOR — FAULTY (L/E FLAP)

NR 4 LEAD EDGE FLAP WOULD NOT RETRACT WHEN FLAPS MOVED FROM 5 DEG TO 2 DEG. *S/D* REPLACED PLUG OPS CK GOOD. CHANGED CANNON PLUG D904 IAW WDM 27-81-02. RAN NR 1 ENG PER 727 JRH CK LWDT WING LEAD EDGE DISTRIBUTION MANIFOLD FOR LEAKS PER MM 30-13-000-5. NONE FOUND.

Part: WARNING LIGHT — ILLUMINATED (APU FIRE DETECT)

APU FIRE WARN LIGHT CAME ON IN FLT. AC RELEASE PER SERVICE PER MEL/CDL. RAN APU IAW JET RUN HANDBOOK AND NO DISCREPANCIES NOTED.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 48,230 hrs · 39,858 cycles

DURING ROUTINE INSP, NR 4 SEAT TRACK FOUND CORRODED BEYOND LIMITS FROM BS 480 - 580. REMOVED DAMAGED, FAB, AND INSTALLED PER IAW SRM 53-10-5.

Part: WEB — CRACKED (FUSELAGE) · airframe 48,230 hrs · 39,858 cycles

DURING ROUTINE INSP, THE ANGLE AND WEB JUST FWD OF BS 1183 FOUND CRACKED. REMOVED WEB AND ANGLE, FAB PER IAW SRM 51-20-1, 51-30-2.

Part: RIB — CRACKED (NR 4 SLAT) · airframe 48,230 hrs · 39,858 cycles

DURING ROUTINE INSP, NR 4 SLAT RIB FOUND CRACKED JUST O/B OF THE I/B TRACK. CUT OUT DAMAGED AREA, FAB DOUBLER AND FILLER, AND INSTALLED REPAIR PER IAW SRM 57-50-3.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 48,230 hrs · 39,858 cycles

DURING ROUTINE INSP, TWO STR TIE CLIPS WERE FOUND CRACKED AT BS 950D AT STR 2L AND 4L. REMOVED AND REPLACED PER IAW SRM 51-30-2.

Part: SPLICE — CRACKED (STRINGER) · airframe 48,230 hrs · 39,858 cycles

DURING ROUTINE INSP, STRINGER SPLICE AT BS 483 - 488 ON STR 3R FOUND CRACKED. REMOVED DAMAGE, INSTALLED PER IAW SRM 5-30-2.

Part: FLOOR SUPPORT — CRACKED (COCKPIT) · airframe 48,230 hrs · 39,858 cycles

DURING ROUTINE INSP, COCKPIT FLOOR STRUCTURE FOUND CRACKED BS 284, LBL 7. REMOVED AND REPLACED, FAB PER IAW SRM 51-20-1 & 51-30-2.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 48,230 hrs · 39,858 cycles

DURING ROUTINE INSP, NR 3 SEAT TRACK FOUND CORRODED BEYOND LIMITS FROM BS 540 - 700. REMOVED, REPLACED AND FAB PER IAW SRM 53-10-5.

Part: SKIN — CRACKED (MLG DOOR) · airframe 48,230 hrs · 39,858 cycles

DURING ROUTINE INSP, LEFT MAIN LAND GEAR DOOR INNER SKIN FOUND CRACKED. CUT OUT DAMAGED AREA, FAB DOUBLER AND FILLER, AND INSTALL PER IAW SRM 51-40-2.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 48,230 hrs · 39,858 cycles

DURING ROUTINE INSP, COCKPIT DOORWAY THRESHOLD BS 302 FOUND CORRODED AND CRACKED. REMOVED DAMAGE, FAB AND INSTALLED PER SRM 51-20-1, 51-30-2.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 48,230 hrs · 39,858 cycles

DURING ROUTINE INSP, ATTACH ANGLE AT BS 720F FROM STR 28L TO 28R FOUND CRACKED. REMOVED, REPLACED AND FAB PER IAW SRM 51-20-1 AND 51-30-2.

Part: ANGLE — CRACKED (WING LE) · airframe 48,230 hrs · 39,858 cycles

DURING ROUTINE INSP, THE ANGLE AT RIGHT WING LEAD EDGE WEB JUST O/B OF THE BOTTLE BOLT, FOUND CRACKED. REMOVED AND REPLACED ANGLE PER IAW SRM 51-30-2.

Part: PANEL — CORRODED (CARGO BAY) · airframe 48,230 hrs · 39,858 cycles

DURING ROUTINE INSP, RIGHT TRANSITION PANEL AT BS 540, STR 27R FOUND CORRODED IN FWD BAG BIN. REMOVED, FAB AND INSTALLED PER IAW SRM 51-20-1 AND SRM 51-30-2.

Part: INTERCOSTAL — CRACKED (CABIN) · airframe 48,230 hrs · 39,858 cycles

DURING ROUTINE INSP, CABIN FLOOR INTERCOSTAL BS 312, LBL 32 FOUND CRACKED. REMOVED DAMAGED, FAB, AND INSTALLED PER IAW SRM 51-20-1, 51-30-2.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 48,230 hrs · 39,858 cycles

DURING ROUTINE INSP, INTERCOSTAL AT BS 277 - 294, LBL 14 IN COCKPIT FLOOR STRUCTURE FOUND CORRODED BEYOND LIMITS. CUT OUT DAMAGED AREA, FAB, REMOVED AND REPLACED PER 51-40-3.

Part: WEB — CRACKED (RT WING LE) · airframe 48,230 hrs · 39,858 cycles

DURING ROUTINE INSP, 4 CRACKS WERE FOUND IN RT WING LEAD EDGE WEB JUST O/B OF BOTTLE BOLT. STOP DRILLED CRACKS, FAB DOUBLERS AND INSTALLED REPAIR PER IAW SRM 51-40-2.

Part: RIB — CORRODED (VERTICAL STAB) · airframe 48,230 hrs · 39,858 cycles

DURING ROUTINE INSP, VERTICAL FIN TENSION TIE RIB BUSHING FOUND CORRODED AT LEFT AFT HORIZONTAL BOLT. REMOVED AND REPLACED VERTICAL FIN TENSION TIE RIB BUSHING PER IAW BOEING OHM 20-50-03.

Part: ACTUATOR — FAILED (NR 6 LE FLAP)

WHILE RETRACTING FLAPS AFTER T/O, NR 6 LED FAILED TO RETRACT. TRIED LOWERING FLAPS TO 2 DEG AND THEN RETRACTING BACK TO FULLY UP POSITION AND NR 6 LED STILL FAILED TO RETRACT. REMOVED AND REPLACED NR 6 SLAT ACT IAW MM 27-81-32, OPS CK NORMAL.

Part: RIB — CRACKED (BS 1283)

RIB CRACKED AT BS 1283 AT 7 O'CLOCK POSITION ON S-DUCT. *S/D* REPAIRED RIB AT BS 1283 AT 7 O'CLOCK POSITION ON 5 DUCT IAW FED-EX SRM 54-10-3.

Part: PANEL — MISSING (NR 7 LE SLAT)

NR 7 LEADING EDGE SLAT ACTUATOR DOOR MISSING. * S/D* REPLACED AND ADJUSTED NR 7 SLAT ACTUATOR DOOR PER MAINTENANCE MANUAL 27-81-32, OPERATIONAL CHECK NORMAL.

Part: RECEIVER — FAILED (E/E COMP)

97-0142, NR 2 VOR FAILED IN FLIGHT (NO IDENT ON VHF NAV NR 2 ANY STATION). REMOVED AND REPLACED NR 2 VOR/ILS RECEIVER PER MAINTENANCE MANUAL 34-31-21, OPERATIONAL CHECKED GOOD.

Part: FIRE DETECTION — FAILED (NR 1 ENGINE)

97-0097 13 MINS INTO FLT, ENG NR 1 FIRE DETECTION FAULT IND LIGHT ILLUMINATED WITH NO OTHER FIRE INDICATIONS. IAW RED TABS, FOUND LOOP A FAULTY AND COMPLETED REMAINDER OF FLT IN LOOP B. REPEAT GRIPE AGAIN. AC RELEASED FOR SERV PER MEL/COL:26-6B CATEGORY: C EXP 06JUN97 NO TIME-DEF, PER MEL 26-6(B) NR 1 ENG A LOOP INOP. ON INSPECT OF WIRING, FOUND WIRE HARNESS BINDING AT UPR FWD INBD COWLING ATTACH. REMOVED ELBOW ANTI-ICING AIR TUBE R/FRONT TO FACILITATE MX RELOCATED WIRE BUNDLE TO CLR ALL ENG AND COWLING STRUCTURES. REINSTALLED ELBOW WITH NEW GASKET. SECURED COWL CLOSED. TESTED PER M/M 26-11-02. RAN ENG TO CK A PUMP DEPRESS ON AND OK. NO FAULTS OCCURRED. AC REL FOR SERVICE.

Part: FIRE DETECTOR — FAILED (NR 1 ENGINE)

97-0094, NR 1 ENGINE FIRE LIGHT BELL AND DETECTOR FAULT LIGHT ILLUMINATED IN FLIGHT FOR 5 SECONDS. DETECTOR SYSTEM WAS IN LOOP-A AS PER MINIMUM EQUIPMENT LIST. LOOP-B FAILED TEST, NO OTHER ABNORMAL ENGINE INDICATIONS. REMOVED AND REPLACED FIRE DETECTOR ELEMENT AND ENGINE FIRE CONTROL UNIT. OPERATIONAL CHECK OF FIRE DETECTOR CHECKED GOOD. ALSO, CHECKED PNEUMATIC LEAKS, NONE NOTED.

Part: SOLENOID — FAILED (LDG GEAR HANDLE)

AFTER TAKEOFF FROM PHL, LANDING GEAR LEVER FAILED TO RAISE PASS THE OFF POSITION. THE LANDING GEAR LEVER LATCH FAILED TO RELEASE. CHECKLIST WAS ACCOMPLISHED. LANDING GEAR WAS SUBSEQUENTLY RETRACTED USING THE LANDING GEAR LEVER LATCH TRIGGER. SWAPPED LANDING GEAR ACCESSORY MODULE, NO HELP. REINSTALLED ORIGINAL BOX. REPLACED R92 LANDING GEAR SAFETY RELAY (OVERHEAT), NO HELP. FOUND NO POWER GOING TO LEVER LATCH SOLENOID (LANDING GEAR HANDLE), WITH LEVER LATCH CIRCUIT BREAKER PULLED. CHANGED LEVER LATCH SOLENOID. GEAR HANDLE CHECKED BY DISCONNECTING WALKING BEAM. OK FOR SERVICE.

Part: SKIN — CORROSION (BS 680-740)

CORROSION FWD BAY, ON AND UNDER BONDED DOUBLER AT BL 0, BS 720-726 AT VARIOUS BODY STAT, IT IS DISBONDED, ALSO, (ACCESS IS REQUIRED). REMOVED AND REPLACED BELLY SKIN FROM BS 680-740, STR 26 LT AND RT ALL WORK DOWN IAW FEDEX EA 7-5300-25764 AND DRAWING NR 65-54577.

Part: SKIN — DENTED (BS 650)

EA 7-5330-25397 CORRECTIONS FOR DENT IN FUSELAGE SKIN/CARGO DOOR DOUBLER (LOGBOOK ENTRY REQUIRED) MACH NR 53-30/686. REMOVED DAMAGED STR 24L, RECONTOURED DENT, INSPECTED FOR CRACKS NONE FOUND. FABRICATED STR AND DOUBLER REPAIR AND INSTALLED REPAIR PARTS AT BS 650, STR 23-24L PER SRM 53-10-3, 53-30-3, 51-40-1 AND FEDEX EA 7-5310-25787. INSPECTION SCUFF MARK AT BS 490, STR 23L. BLENDED AREA, INSPECTED AT CRACKS, NONE FOUND. NO FURTHER ACTION REQUIRED AT BS 490, STR 23L PER SRM 53-30-1.

Part: FAIL-SAFE CHORD — CORRODED (BS 740)

CORROSION FWD BAY ON TOP SIDE OF BS 740 FAIL-SAFE CHORD LBL 9 TO LBL 14. ALSO, 4 FASTENERS UNDERSIDE, 2 AT STR 27L AND 2 AT STR 27R, ACCESS IS REQUIRED. REMOVED CORROSION ON FAIL-SAFE CHORD BS 740 FROM LBL 18 RBL 16, FOUND CORROSION TO BE OUT OF LIMITS PER FEDEX SRM 53-10-1. FABRICATED REPAIR PARTS, DRILLED, ALODINED, PRIMED AND INSTALLED IAW FEDEX EA 7-5310-25785.

Part: GUSSET — CORROSION (BS 740)

CORROSION FWD BAY ON PRESS GUSSET AT BS 740 AT KEEL BEAM, STR 28R WL 145. REMOVED CORROSION FROM PRESS GUSSET AT BS 740 STR 28R AND FOUND OUT OF LIMITS PER FEDEX SRM 53-10-1. REMOVED GUSSET AND INSTALLED NEW GUSSET, BS 740 STR 28R. FUNCTIONAL CHECK PER MM FEDEX 21-56-0, 28-22-0 AND 27-82-31.

Part: SPLICE — CORRODED (BS 680)

CORROSION (71C209-02), ON STR SPLICE BS 680 STR 27R WL 148. CORROSION FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED STR SPLICE AT BS 680 STR 27R WL 148 IAW SRM 53-10-1.

Part: STRINGER — CORROSION (BS 680)

CORROSION ON STR 27L AT VARIOUS LOCATIONS FROM BS 680 TO 740 WL 145. REMOVED CORROSION ON STR 27L FROM BS 680 TO 740 AND FOUND OUT OF LIMITS PER FEDEX SRM 53-10-1. REMOVED STR 27L FROM BS 680 TO 740 AND INSTALLED NEW STR 27L FROM 680 TO 740.

Part: SHEAR TIE — CORROSION (BS 680)

CORROSION (71C209-02), ON SHEAR TIE BS 680 STR 25 TO 26R WL 150. REMOVED CORROSION FROM SHEAR TIE BS 680 STR 25 TO 26R AND FOUND OUT OF LIMITS PER FEDEX SRM 53-10-1. REMOVED SHEAR TIE AND INSTALLED NEW SHEAR TIE AT BS 680 STR 25 TO 26R.

Part: SHEAR TIE — CORROSION (BS 680)

CORROSION (71C209-02), ON SHEAR TIE BS 680 STR 26 TO 27R WL 148. REMOVED CORROSION FROM SHEAR TIE BS 680 STR 26 TO 27R AND FOUND OUT OF LIMITS PER FEDEX SRM 53-10-1. REMOVED SHEAR TIE AND INSTALLED NEW SHEAR TIE AT BS 680 STR 26 TO 27R.

Part: FRAME — CORRODED (BS 720)

CORROSION FWD BAY, BS 720E WL 150 RBL 4, 6 AND 11, LBL 5, 7 AND 13 ON BILGE FRAME. REMOVED CORROSION AND FOUND TO BE BEYOND LIMITS PER FEDEX SRM 53-10-1, REMOVED CORRODED FRAME.

Part: KEEL BEAM — CORRODED (BS 720-740)

CORROSION 71C209-02, ON KEEL BEAM BS 720 TO 740 STR 28L. REMOVED KEEL BEAM AT STR 28L BS 720 TO 740 AND REPLACED WITH KEEL BEAM.

Part: SHEAR TIE — CORRODED (BS 720)

CORROSION IN FWD BAY, BS 720C STR 27 TO 28L WL 148 ON THE SHEAR TIE. REMOVED CORRODED SHEAR TIE BS 720C STR 27 TO 28L WL 148 AND REPAIRED PER FEDEX SRM 53-10-4. SHEAR TIE WAS FOUND TO BE OUT OF LIMITS PER FEDEX SRM 53-10-1.

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

FOUND CORROSION, MECHANICAL DAMAGES IN SEAT TRACK AT BS 690 TO 740 WL 208.5 LBL 25. REMOVED CORRODED SEAT TRACK FROM BS 690 TO 740 WL 208.5 LBL 25. INSTALLED FABRICATED SEAT TRACK FROM BS 690 TO 740 WL 208.5 LBL 25.

Part: SEAT TRACK — CORRODED (BS 381-406)

FOUND MECHANICAL DAMAGE ON SEAT TRACK AT BS 381 WL 208.5 RBL 63. ACCOMPLISHED SEAT TRACK REPAIR AT BS 381 TO 406 WL 208.5 RBL 63, PER SRM 53-10-5. REMOVED DAMAGED WEBS AND MOPSILL BS 360 TO 440 WL 208 RBL 64 TO 70. FAB NEW WEBS AND INSTALLED NEW MOPSILL PER FEDEX DRAWING 65-56153.

Part: SHEAR TIE — CORRODED (BS 720)

CORROSION, FWD BAY FOUND WHILE WORKING FUSELAGE 159 NR 460 SHEAR TIES FROM FRAME AT BS 720F WL 149 AND 150, BETWEEN STR 27 TO 28L ON 720 FRAME. FOUND CORROSION TO BE OUT OF LIMITS AND REPAIRED SHEAR TIE AT BS 720F STR 27 TO 28L IAW SRM 53-10-4.

Part: SHEAR TIE — CORRODED (BS 720)

CORROSION IN FWD BAY, BS 720R STR 26 TO 27R WL 148 ON THE SHEAR TIE. FOUND CORROSION TO BE OUT OF LIMITS. REMOVED AND REPLACED SHEAR TIE IAW SRM 53-10-4 FIG 15.

Part: SHEAR TIE — CORRODED (BS 700)

CORROSION IN FWD BAY, BS 700 STR 28 LT AND RT WL 148 ON THE SHEAR TIE. REPLACED SHEAR TIE AT BS 700 STR 28 LT AND RT WL 148 PER FEDEX SRM 53-10-4. THE CORROSION REMOVED WAS FOUND TO BE OUT OF LIMITS PER FEDEX SRM 53-10-1.

Part: SHEAR TIE — CORRODED (BS 720)

CORROSION FWD BAY, BS 720B STR 28 LT AND RT WL 148 ON SHEAR TIE. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS, BS 720B STR 28 LT AND RT WL 148 PER FEDEX 53-10-3. FABRICATED SHEAR TIE AND INSTALLED PER FEDEX 53-10-4 SRM.

Part: STRINGER — CORRODED (BS 740)

CORROSION FWD BAY ON STR 27R BS 740 ACCESS IS REQUIRED, FWD BAY STR 27R BS 680 TO 740. REMOVED AND REPLACED WITH NEW STR, CORROSION WAS FOUND TO BE OUT OF LIMITS PER FEDEX SRM 53-10-1.

Part: CHORD — DAMAGED (HORIZ STAB)

RT LOWER T/E CHORD, HORIZONTAL STAB, 3 RUBSTRIP FASTENERS HAVE PULLED THROUGH BETWEEN ELEVATOR STATIONS. REPAIRED LOWER T/E CHORD IAW FEDEX EA 7-5510-25695.

Part: SHEAR TIE — CORRODED (BS 720)

CORROSION IN FWD BAY, BS 720B STR 27 AND 28R WL 148 ON THE SHEAR TIE. CORROSION FOUND TO BE OUT OF LIMITS. REPAIRED SHEAR TIE AT BS 720B STR 27 TO 28R WL 148 IAW SRM 53-10-4.

Part: SHEAR TIE — CORRODED (BS 720)

CORROSION IN FWD BAY, BS 720C STR 28 LT AND RT WL 148 ON THE SHEAR TIE. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS PER FEDEX SRM 53-10-1. REMOVED DAMAGED SHEAR TIE AT BS 720C STR 28 LT AND RT WL 148, FABRICATED REPAIR PART AND INSTALLED PER FEDEX SRM 53-10-4.

Part: INTERCOSTAL — CORRODED (BS 700-720)

CORROSION IN FWD BAY, BS 700 TO 720 STR 28L WL 148 ON THE INTERCOSTAL WEB. INTERCOSTAL WEB CORRODED BEYOND LIMITS IAW FEDEX SRM 53-10-1. REMOVED AND REPLACED INTERCOSTAL, BS 700 TO 720 STR 28L WL 148.

Part: STRINGER — CORRODED (BS 680-723)

CORROSION FOUND WHILE WORKING NR 0460 ON STR 28R BS 680 TO 723 WL 145. REMOVED CORROSION ON STR 28R BS 680 TO 723 WL 145, FOUND TO BE OUT OF LIMITS PER FEDEX SRM 53-10-1. REPLACED STR PER FEDEX SRM 51-10-1.

Part: INTERCOSTAL — CORRODED (BS 680-700)

CORROSION FOUND WHILE WORKING NR 0460 ON INTERCOSTAL BS 680 TO 700 RBL 13.5 WL 145. REMOVED INTERCOSTAL BETWEEN BS 680 TO 700 RBL 13.5 WL 145, WORK DONE PER FEDEX SRM 51-30-2. DAMAGE WAS FOUND TO BE OUT OF LIMITS PER FEDEX SRM 53-10-1.

Part: SHEAR TIE — CORRODED (BS 720)

CORROSION IN FWD BAY, BS 720C STR 27 TO 28R WL 148 ON THE SHEAR TIE. CORROSION FOUND TO BE OUT LIMITS. REMOVED AND REPAIRED DAMAGED SHEAR TIE PER SRM 53-10-4.

Part: KEEL BEAM — CORRODED (BS 920)

CORROSION FWD BAY ON KEEL BEAM AROUND BUCKTAILS AT CRACKED PAINT, BS 920C TO 720E IN BILGE ACCESS IS REQUIRED, RT KEEL BEAM. REMOVED KEEL BEAM BS 720 TO 740, STR 28R AND REPLACED WITH NEW KEEL BEAM.

Part: SHEAR TIE — CORROSION (BS 720)

CORROSION IN FWD BAY, BS 720B STR 27 TO 28L WL 148 ON THE SHEAR TIE. REMOVED CORRODED SHEAR TIE, BS 720B STR 27 TO 28L AND REPAIRED PER FEDEX SRM 53-10-4.

Part: SHEAR TIE — CORROSION (BS 720)

CORROSION FWD BAY BS 720C STR 25R AND 26R WL 148 ON THE SHEAR TIE. REMOVED AND REPLACED SHEAR TIE AT BS 720C STR 25 TO 26R WL 148, ALDOINED, PRIMED, AND PAINTED. CORROSION ON SHEAR TIE WAS FOUND TO BE OUT OF LIMITS PER FEDEX SRM 53-10-1.

Part: SKIN — DENTED (BS 1173-1176)

DENT IN SKIN BS 1173 TO 1176 BETWEEN STR 16 AND 17R, .5 BY .5 BY .045 OUT OF LIMITS PER SRM. DENT WAS FOUND TO BE OUT OF LIMITS. CUTOUT DAMAGED SKIN AND REPAIRED IAW SRM 53-30-3.

Part: SPLICE — CORRODED (BS 680)

CORROSION FOUND WHILE WORKING NR 0460 ON STR SPLICE AT BS 680 AT STR 28R WL 145. CORROSION FOUND TO BE OUT OF LIMITS, REMOVED OLD STR SPLICE AND REPLACED WITH NEW STR SPLICE AT BS 680 STR 28R.

Part: BONDING JUMPER — CORRODED (NR 3 LE FLAP)

CORROSION (75C002-00), NR 3 K-FLAP TO BULLNOSE I/B BONDING JUMPER LOWER ATTACH POINT. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. REPAIRED NR 3 K-FLAP IAW EA 7-5710-25636 SR 27-57-010.

Part: SPLICE — CORRODED (BS 680)

CORROSION (71C209-02), ON STR TERMINATION SPLICE STR 27L BS 680. CORROSION FOUND TO BE OUT OF LIMITS, REMOVED STR SPLICE AT BS 680 STR 27L.

Part: INTERCOSTAL — CORRODED (BS 740)

CORROSION FWD BAY ON PRESS GUSSET AT BS 740 BL 0 WL 145, BETWEEN KEEL BEAMS. DISCOVERED WHILE WORKING FUSELAGE 00188 NR 0561. PRESS GUSSET AT BS 740 BL 0 WL 145 FOUND TO BE CORRODED BEYOND LIMITS, PER FEDEX SRM 55-10-1. REMOVED AND REPLACED PRESS GUSSET PER FEDEX SRM 51-30-2.

Part: FRAME — DENTED (BS 700)

FWD BAY FRAME DENTED AT BS 700 BETWEEN STR 25 AND 22R. REMOVED DAMAGED PART OF FRAME AT BS 700 BETWEEN STR 22 AND 25R. INSTALLED REPAIR DOUBLER IAW FEDEX SRM 51-40-3.

Part: SHEAR TIE — CORROSION (BS 700)

CORROSION FWD BAY BS 700 STR 27 TO 28R ON THE SHEAR TIE. REMOVED DAMAGED SHEAR TIE AND INSTALLED FABRICATED SHEAR TIE. FOUND SHEAR TIE CORRODED OUT OF LIMITS PER FEDEX SRM 53-10-1.

Part: SHEAR TIE — CORROSION (BS 720)

CORROSION FWD BAY BS 720C STR 26 TO 27R WL 148 ON THE SHEAR TIE. FOUND SHEAR TIE BS 720C STR 26 TO 27R WL 148 CORRODED BEYOND LIMITS PER FEDEX SR 727 53-10-1. REMOVED AND REPLACED SHEAR TIE.

Part: WEB — CORROSION (BS 344)

CORROSION ON WEB AT BS 344 WL 207 AND 208 RBL 6 LBL 46 AFT AND FWD SIDE, FOUND WHILE WORKING NR 0827 AFTER REMOVAL OF FLOORBEAM. REMOVED CORROSION ON WEB AT BS 344 WL 207 AND 208 RBL 6 LBL 46 AFT AND FWD SIDE, FOUND TO BE OUT OF LIMITS AT LBL 27-43. FABRICATED AND INSTALLED DOUBLER PER SRM FEDEX 51-40-2 AT LBL 27-43.

Part: STR CLIP — CORROSION (BS 660)

CORROSION FWD BAY ON STR CLIP AT BS 660 STR 26R ON BILGE. REMOVED STR CLIP AT BS 660 STR 26R AND FOUND CORROSION OUT OF LIMITS PER FEDEX SRM 53-10-1. INSTALLED FAB STR CLIP AT BS 660 STR 26R.

Part: FRAME — DENTED (BS 500)

FWD BAY DENTED AT BS 500 BETWEEN STR 26 TO 22R. REPAIRED DENTED FRAME AT BS 500 STR 26 TO 22R, PER FEDEX SRM 51-40-2.

Part: STIFFENER — CORROSION (BS 740)

CORROSION FWD BAY ON VERTICAL STIFFENER AT BS 740 BL 0 WL 150. REMOVED CORRODED STIFFENER AND REPLACED NEW STIFFENER BS 740 BL 0 WL 150.

Part: STRINGER CLIP — CORROSION (BS 720)

CORROSION FWD BAY ON STR CLIP AT BS 720C AT STR 26L. REMOVED CLIP TO ACCESS AREA, FOUND CORROSION ON CLIP. DRILLED FAB CLIP ALODINED, PRIMED AND FASTENED INTO PLACE. CORROSION ON STR CLIP FOUND TO BE OUT OF LIMITS PER FEDEX SRM 53-10-1 STR 26L BS 720C.

Part: SHEAR TIE — CORROSION (BS 720)

CORROSION IN FWD BAY BS 720A STR 27 TO 28R WL 148 ON THE SHEAR TIE. REMOVED CORRODED SHEAR TIE BS 720A STR 27 TO 28R WL 148. FABRICATED, DRILLED, ALODINED, PRIMED, PAINTED AND INSTALLED SHEAR TIE PER FEDEX SRM 53-10-4.

Part: TE WEDGE — DENTED (RT AILERON)

RT WING O/B AILERON WEDGE HAS CREASED DENT ON UPPER SURFACE AND 2 DISBONDS ON T/E. REPAIRED RT WING O/B AILERON WEDGE IAW FEDEX SRM 51-40-6 AND 51-40-10.

Part: STRINGER CLIP — CORROSION (BS 660)

CORROSION FWD BAY ON STR CLIP AT BS 660 AT STR 26L. ACCESSED AREA, REMOVED CLIP AND CLEANED AREA. DRILLED FAB CLIP DEBURRED AND ALODINED AREA. PAINTED AREA, CLIP AND FASTENED INTO PLACE. CORROSION ON STR CLIP FOUND OUT OF LIMIT PER FEDEX SRM 53-10-1.

Part: STRINGER — CORRODED (BS 1111)

CORROSION STR 4R BS 1111. THE CORROSION WAS FOUND TO BE OUT OF LIMITS. INSTALLED CHANNEL REPAIR AT BS 1111 STR 4L IAW SRM 53-10-3 AND 53-10-1.

Part: SEAT TRACK — CORROSION (BS 720)

FOUND CORROSION IN SEAT TRACK AT BS 720 TO 720F WL 208.5 BL 0. REMOVED CORRODED SEAT TRACK AND INSTALLED NEW FABRICATED SEAT TRACK AT BS 720 TO 720F WL 208.5 BL 0.

Part: FLOORBEAM — CORROSION (BS 344)

FOUND CORROSION IN FLOORBEAM AT BS 344 WL 208.5 RBL 4 LBL 51. REMOVED DAMAGED PORTION OF FLOORBEAM AND INSTALLED REPAIR PARTS AT BS 344 WL 208 RBL 10 LBL 70, PER FEDEX DRAWING SR 27-53-007.

Part: STRINGER CLIP — CORRODED (BS 720)

CORROSION FWD BAY ON STR CLIP AT BS 720C AND 720B AT STR 26R. FOUND CORROSION TO BE OUT OF LIMITS. REMOVED AND REPLACED STR CLIP AT BS 720C AND 720B AT STR 26R.

Part: SKIN — CORROSION (BS 580-600)

WHILE WORKING NR 0448, FOUND CORROSION ON SKIN UNDER INTERCOSTAL AND LEVELING COMPOUND BS 580 TO 600 LBL 7 WL 147.5. FOUND CORROSION TO BE OUT OF LIMITS. REMOVED AND REPLACED SKIN AT BS 580 TO 600 LBL 7 WL 147.5 IAW SRM 53-30-3.

Part: STRINGER — CORROSION (BS 680-720)

CORROSION FOUND WHILE WORKING NR 0450 ON STR 28L BS 680 TO 720 WL 145. CORROSION FOUND TO BE OUT OF LIMITS PER FEDEX SRM 53-10-1. REMOVED AND REPLACED STR 28L BS 680 TO 720 PLUS 3 WL 145.

Part: SHEAR TIE — CORROSION (BS 720)

CORROSION FWD BAY BS 720B STR 26 TO 27R WL 148 ON THE SHEAR TIE. FOUND SHEAR TIE STA 720B STR 26 TO 27R WL 148 CORRODED BEYOND LIMITS PER FEDEX SRM 727 53-10-1. REMOVED AND REPLACED NEW SHEAR TIE.

Part: SKIN SUPPORT — CORRODED (BS 740)

FWD BAY, FOUND CORROSION WHILE WORKING NR O858 FUSELAGE 00117 SKIN SUPPORT (P/N 69-43695-1), OF BS 740 WL 145 TO 150 BETWEEN STR 28 AND 27L. CORROSION WAS FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED SKIN SUPPORT IAW SRM 51-10-1, 53-10-1.

Part: SEAT TRACK — CORROSION (BS 344-480)

FOUND CORROSION IN SEAT TRACK AT BS 344 TO 480 WL 208.5 BL 0. REMOVED CORROSION FROM SEAT TRACK BS 347 TO 415 BL 0 AND IT WAS FOUND TO BE WITHIN LIMITS IAW FEDEX SRM 53-10-1. ALODINE AND PRIMED SEAT TRACK BS 347 TO 415 BL 0. ACCOMPLISHED SEAT TRACK REPAIR FROM BS 450 TO 480 IAW FEDEX SRM 53-10-5.

Part: WEB — CRACKED (VERTICAL STAB)

1303 WEB IN BAY NR 1 AT VERTICAL FIN IS CRACKED LT LOWER CORNER. REPAIRED CRACK AT 1303 WEB IN BAY NR 1 OF VERTICAL FIN LT LOWER CORNER, PER FEDEX DRAWING SR 27-53-015.

Part: WEB — CRACKED (VERTICAL FIN)

1303 WEB IN BAY NR 1 IN VERTICAL FIN IS CRACKED LT LWR CORNER. REPAIRED CRACK IN 1303 WEB IN BAY NR 1 OF VERTICAL FIN LT LOWER CORNER, PER FEDEX DRAWING SR 27-53-015.

Part: SEAT TRACK — CORROSION (BS 344-480)

FOUND CORROSION IN SEAT TRACK AT BS 344 AND 480 WL 208.5 BL 0. REMOVED CORROSION FROM SEAT TRACK BS 347 TO 415 BL 0 AND FOUND TO BE WITHIN LIMITS IAW FEDEX SRM 53-10-1. ALODINE AND PRIMED SEAT TRACK BS 347 TO 415 BL 0. ACCOMPLISHED SEAT TRACK REPAIR FROM BS 450 TO 480, IAW FEDEX SRM 53-10-5.

Part: FRAME — GOUGED (BS 720)

FWD FRAME DENTED AND GOUGED ON TOP BS 720C AT STR 23 TO 24R. GOUGE FOUND TO BE OUT OF LIMITS. REMOVED DAMAGE AND REPAIRED FRAME AT BS 720C STR 23 TO 24R, PER SRM 51-40-3.

Part: SKIN SUPPORT — CORRODED (BS 740)

CORROSION FWD BAY FOUND WHILE WORKING NR 0338 FUSELAGE 00117 SKIN SUPPORT AT BS 740 WL 145 TO 150 BETWEEN STR 28 TO 27L. CORROSION WAS FOUND TO BE OUT OF LIMITS. REMOVED OLD SKIN SUPPORT AND REPLACED WITH NEW SKIN SUPPORT IAW SRM 51-10-1, 53-10-1.

Part: SKIN — CORROSION (BS 420)

WHILE WORKING CARD NR 7-3520-7-3313A PT 2, COCKPIT 00017. REMOVED STR 20R FOR OXYGEN MOD AND FOUND CORROSION ON SKIN AT BS 420 UNDER STR 20R, OUT OF LIMITS PER FEDEX SRM 53-30-1. REPAIRED DAMAGED SKIN PER FEDEX SRM 53-10-3 FIG 4.

Part: FRAME — GOUGED (BS 720)

FWD, FRAME DENTED AND GOUGED ON TOP BS 720C AT STR 23 TO 24R. GOUGE FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED DAMAGED FRAME AT BS 720C STR 23 TO 24R, PER SRM 51-40-3.

Part: FRAME — DENTED (BS 600)

FWD BAY, FRAME DENTED ON TOP AT BS 600 BETWEEN STR 26 TO 23L. ALSO FACTORY SPLICE IS DENTED. REPAIRED FRAME AT BS 600 BETWEEN STR 26 TO 23L PER FEDEX SRM 51-40-3.

Part: CLIP — CORRODED (BS 1166)

CORROSION STR CLIP BS 1166 STR 15L. REMOVED CORRODED STR CLIP AT BS 1166 STR 15L AND INSTALLED NEW STR CLIP AT BS 1166 STR 15L IAW FEDEX SRM 51-30-2.

Part: FRAME — DENTED (BS 720)

FWD BAY, FRAME DENTED AT BS 720C BETWEEN STR 25 TO 24L. REPAIRED DENTED FRAME AT BS 720C BETWEEN STR 24 TO 25L PER FEDEX SRM 51-40-3.

Part: CLIP — CORRODED (BS 1166)

CORROSION STR CLIP BS 1166 STR 15L. REMOVED CORRODED STR CLIP AT BS 1166 STR 15L AND INSTALLED NEW STR CLIP, IAW FEDEX SRM 51-30-2.

Part: FRAME — DENTED (BS 720)

FWD BAY, FRAME DENTED AT BS 720C BETWEEN STR 25 TO 24L. REPAIRED DENTED FRAME AT BS 720C BETWEEN STR 24 TO 25L PER FEDEX SRM 51-40-3.

Part: SEAT TRACK — CORROSION (BS 480-600)

FOUND CORROSION IN SEAT TRACK AT BS 480 TO 600 WL 208.5 BL 0. REMOVED CORRODED SEAT TRACK AT BS 480 TO 600 WL 208.5 BL 0. FABRICATED NEW SEAT TRACK AND INSTALLED AT BS 480 TO 600 WL 208.5 BL 0, REF FEDEX SRM 53-10-5.

Part: FRAME — DENTED (BS 600)

FWD BAY, FRAME DENTED ON TOP AT BS 600 BETWEEN STR 26 TO 23L. ALSO, FACTORY SPLICE IS DENTED. REPAIRED FRAME AT BS 600 BETWEEN STR 26 TO 23L PER FEDEX SRM 51-40-3.

Part: SEAT TRACK — CORROSION (BS 480-600)

FOUND CORROSION IN SEAT TRACK AT BS 480 TO 600 WL 208.5 BL 0. REMOVED CORRODED SEAT TRACK AT BS 480 TO 600 BL 0 WL 208.5. FABRICATED NEW SEAT TRACK AND INSTALLED AT BS 480 TO 600 BL 0 WL 208.5, REF FEDEX SRM 53-10-5.

Part: FRAME — DENTED (BS 680)

FWD BAY, FRAME DENTED AT BS 680 BETWEEN STR 25 AND 23R. REPAIRED FRAME AT BS 680 BETWEEN STR 25 AND 23R, PER SRM 51-40-3 FEDEX.

Part: FRAME — DENTED (BS 660)

FWD BAY, FRAME DENTED ON TOP BS 660 BETWEEN STR 25 AND 22L. ALSO, FACTORY SPLICE IS DENTED. REPAIRED FRAME AT BS 660 BETWEEN STR 25 AND 22L, IAW FEDEX SRM 51-10-3.

Part: SKIN — DAMAGED (BS 1333)

FASTENERS AT BS 1333 ON SKIN HAS 11 PULLED THROUGH FASTENER WL 257, LT SIDE ON SKIN EDGE. REMOVED DAMAGED SKIN AT BS 1333 WL 257 LT, FABRICATED DOUBLER, FILLER AND TAPERED SHIM, SCOTCH BRITE, ALODINE AND PRIMED. INSTALLED AS PER FEDEX 54-30-3, 51-20-1.

Part: STRINGER — CRACKED (BS 404)

FOUND CRACK STRINGER AT BS 404 STR 2R. ACCOMPLISHED STR REPAIR AT BS 404 STR 2R PER FEDEX SRM 53-10-3.

Part: SKIN — DENTED (BS 1243)

DENT WITH CREASE FOUND IN SKIN AT BS 1243 WL 143 ON RIGHT SIDE OF A/C BETWEEN STR 22R AND 23R.

Part: DELTA BEAM WEB — CORRODED (BS 790)

IN THE LOWER A/C BAY AT BS 790 RBL 5 WL 148 THERE IS CORROSION ON THE DELTA BEAM WEB. REMOVED DAMAGED SECTION. FABRICATED REPAIR DOUBLER & FILLER PER FEDEX SRM 51-40-02. INSTALLED DOUBLER & FILLER PER FEDEX SRM 51-30-02. APPLIED SKYDROL RESISTANT FINISH & APPLIED 2PS 3 TO CLEANED AREAS, ON DELTA BEAM WEB.

Part: SWITCH — FAILED (NR 1 LE FLAP)

AFTER T/O, DURING FLAP RETRACTION, GOT STEADY AMBER LEADING EDGE FLAP LIGHT AT 2 DEG. CHECKED S/O PANEL, IT SHOWED NR 1 FLAP STILL EXTENDED CYCLED FLAPS, NO HELP. RETURNED TO AIRPORT AND LANDED UNEVENTFULLY. REPLACED NR 1 L/E FLAP SWITCH. CHECKS OK PER MM 27-82-404.