N461FE

Part: SPLICE — CORRODED (BS 1178) · corrosion level 2 · airframe 39,189 hrs · 27,373 cycles

AFT PIT STR -30 APPROX STA 1178 EXFOLIATED. REMOVED AND REPLACED SPLICE IAW 51-30-2.

Part: SKIN — CRACKED (LT WINGTIP) · airframe 39,189 hrs · 27,373 cycles

LEFT WING SMALL CRACK AND DENT IN WING TIP L/E ADJACENT TO O/B END. REMOVED AND REPALCED WING TIP SKIN PNL IAW SRM 51-30-2, P/N 65-16209-4. PAINTED SKIN IAW MM 51-20-151-7.

Part: SKIN — CRACKED (LT WING) · airframe 39,189 hrs · 27,373 cycles

LEFT WING L/E CRACKED ABOVE NR 3 SLAT O/B TRACK. REPAIRED CRACKED ON LEFT WING ABOVE NR 3 SLAT O/B TRACK IAW SRM 57-30-4 FIG 11.

Part: CARGO TRACK — CORRODED (BS 950 LBL 63) · airframe 39,189 hrs · 27,373 cycles

MAIN CABIN STA 950 AT LBL 63 HAS AREA OF CORROSION AROUND TIE DOWN. FAB NEW TIE DOWN ON TRAVELER T7/670839. REMOVED AND REPLACED TIE DOWN IAW SRM 51-30-2.

Part: SEAT TRACK — CORRODED (BS 870-960) · airframe 39,189 hrs · 27,373 cycles

MAIN CABIN SEAT TRACK STA 870-960 RBL 45 HAS SEVERAL AREA'S OF CORROSION. REMOVED SEAT TRACK AND FLOATING TRACK IAW SRM 51-30-2. FABRICATED NEW SEAT TRACK FROM MAE TRAVELER T7/667877, MATERIAL 60-6549/24, BATCH NR 866725. INSTALLED NEW SEAT TRACK AND FLOATING TRACK IAW 51-30-2.

Part: PANEL — DELAMINATED (NR 1 KRUEGER) · airframe 39,189 hrs · 27,373 cycles

LEFT WING LWR SURFACE L/E PNL DELAMINATING AFT OF NR 1 KRUEGER FLAP. REMOVED DAMAGE AND BONDED REPAIR PLIES PER SRM 51-40-9. PAINTED PER MM 51-20-151-7.

Part: BEAM — CRACKED (HORIZONTAL ZONE) · airframe 39,189 hrs · 27,373 cycles

LT HORIZONTAL STAB T/E LWR BEAM BESIDE NR 5 RIB FROM I/B HAS CRACK. REPAIRED LT HORIZONTAL STAB LWR BEAM IAW SRM 55-10-6 FIG 1. PREPPED AND PAINTED. REPAIRED AREA IAW AMM 51-20-151-7.

Part: FLOORBEAM — CORRODED (BS 680) · airframe 39,189 hrs · 27,373 cycles

CABIN FLOORBEAM FS 680,BL-0 TO RBL 24.75 CORRODED ON UPPER SURFACE. REMOVED CORROSION IAW SRM 51-10-06, ORIGINAL MATERIAL IS .125" MATERIAL LOSS IS .011", MATERIAL REMAINING IS .114", IT IS OUT OF LIMIT IAW SRM P TO F 63-10-1. REMOVED DAMAGED IAW SRM 53-10-08. RECEIVED ANGLES FABRICATED ON MAE TRAVELER T7/669483 AND T7/669482. FABRICATED STRAPS FROM MAT ID 7075-T6 .50 AND 7075-T6 .080 IAW SRM 53-10-8. LOCATE AND DRILLED PARTS IAW SRM 53-10--8 FIG 3. TREATED AND PRIMED REPAIR PARTS IAW SRM 51-10-02. INSTALLED REPAIR PARTS IAW SRM 51-30-2.

Part: STRINGER — CORRODED (BS 1183 S25R) · corrosion level 2 · airframe 39,189 hrs · 27,373 cycles

AFT PIT S-25R AND TENSION TIE AT 1183 STA EXFOLIATED. REMOVED STR AND TENSION TIE, FABED NEW PARTS IAW SRM 53-10-3, FIG 1, DETAIL 2. INSTALLED TENSION TIE AND STRINGER REPAIR PARTS IAW SRM 53-30-2,AND 53-10-3.

Part: FLOORBEAM — CORRODED (BS 620) · airframe 39,189 hrs · 27,373 cycles

CABIN FLOORBEAM UPPER SURFACE HAS CORROSION, FS 620, LBL 24.75, TO RBL 24.75. REMOVED CORROSION IAW SRM 51-10-6. FABRICATED REPAIR PARTS ON MAE TRAV NR T7/669488,T7/669489, AND T7/668025 AND INSTALLED REPAIR PARTS IAW SRM 51-30-2. MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (BS 720A) · airframe 39,189 hrs · 27,373 cycles

CABIN FLOORBEAM FS 720A, RBL 24.75 TO BL -0, HAS CORROSION ON UPPER SURFACE. REMOVED CORROSION, REMOVED FLOORBEAM DAMAGE IAW SRZ 27-53-034. FABED NEW ANGLES AND FILLER REPAIR IAW SRZ 27-53-034. INSTALLED REPAIR PARTS IAW SRM 51-30-2. MINOR REPAIR.

Part: FLOORBEAM — CORRODED (BS 720D) · airframe 39,189 hrs · 27,373 cycles

CABIN FLOORBEAM HAS CORROSION ON UPPER SURFACE FS 720D, LBL 24.75 TO LBL 65. REMOVED CORROSION, REMOVED DAMAGE PORTION SR 27-53-034. FABED NEW PARTS PER SR 27-53-034. INSTALLED NEW ANGLES AND NEW FILLER REPAIR IAW SRM 51-30-2.

Part: SKIN — MISREPAIRED (STA 232) · airframe 39,189 hrs · 27,373 cycles

EXTERNAL DOUBLER AT STA 232-243.5 STR 24R DOES NOT COMPLY WITH FAA APPROVED DATA. REPAIRED AREA AT STA 232-243.5, STR 24R IAW SRM 53-30-3 FIG 14 SH 7.

Part: SKIN — MISREPAIRED (FUSELAGE) · airframe 39,189 hrs · 27,373 cycles

EXTERNAL DOUBLER AT STA 392- 408, STR 14L, DOES NOT COMPLY WITH FAA APPROVED DATA. REMOVED REPAIR, FAB`D NEW FILLER DOUBLER MAT 2024-T3, 0.080, BATCH 1228717, IAW SRM 53-30-3. INSTALLED REPAIR FILLER DOUBLER IAW SRM 53-30-3.

Part: WEB — CRACKED (RT WING) · airframe 39,189 hrs · 27,373 cycles

R/M/G WEB CRACKED AT NR 8 SPOILER MOUNT AFT OF GEAR. REMOVED AND REPLACED WEB IAW SRM 51-40-2, AND SRM 51-30-2. REMOVED AND REPLACED EXTERNAL DOUBLER IAW SRM 51-20-1, FIG 7, AND SRM 51-30-2.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 39,189 hrs · 27,373 cycles

FOUND CABIN FLOORBEAM UPPER SURFACE HAS CORROSION, FS 580, RBL 24.75, TO RBL 45.5. REWORKED IAW FEDEX EA 7-5310-102028.

Part: SKIN — MISREPAIRED (BS 298-307) · airframe 39,189 hrs · 27,373 cycles

REPAIR AT STA 298-307, STR 21R TO 23R DOES NOT COMPLY WITH FAA APPROVE DATA. REMOVED REPAIR, FAB`D NEW REPAIR DOUBLER IAW SRM 53-30-3, FIG 3, TABLE 1, MAT 2024-T3, .063C, AND INSTALLED REPAIR DOUBLER IAW SRM 53-30-3, FIG 3.

Part: INTERCOSTAL — CORRODED (BS 348-360) · airframe 39,189 hrs · 27,373 cycles

FOUND INTERCOSTAL CORRODED FS 348 TO 360, AT STR 12L. REMOVED CORRODED, CHECKED AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1, FIG 1, SHEET 2. FAB`D NEW FILLER AND DOUBLER FROM 7075-T6, .040C BATCH 1120917, AND 7075-T6, .050C BATCH 761741 IAW SRM 51-40-2, FIG 1, PAGE 1-6. INSTALLED FILLER AND DOUBLER IAW SRM 51-40-2, FIG 1, PG 1-6.

Part: SKIN — CORRODED (BS 1166) · airframe 39,189 hrs · 27,373 cycles

AFT CARGO FWD OF STA 1166, FROM LBL 6 TO RBL 2, HAS CORROSION ON SKIN. REMOVED CORROSION IAW SRM 51-10-6, UT INSP PER NTM 51-00-00, PT4, MAT THICKNESS BEFORE .125 AFTER REWORK .118, FOUND TO BE WITH IN LIMITS IAW SRM 53-10-1, FIG 1, DETAIL I. TREATED AND PRIMED AREA IAW SRM 51-10-2. PREPPED AND PAINTED AREA IAW MM 51-20-151-7.

Part: INTERCOSTAL — CORRODED (BS 348-360) · airframe 39,189 hrs · 27,373 cycles

INTERCOSTAL CORRODED FS 348 TO 360 AT STR 9L. REMOVED CORROSION, CHECKED LIMITS, IAW SRM 53-104-1, FIG 1, SHEET 2. FAB`D NEW FILLER AND DOUBLER FROM 7075-T6, .040C BATCH 1107917 AND 7075-T6, .050C BATCH 76174. IAW SRM 51-40-2, FIG 1. INSTALLED FILLER AND DOUBLER IAW SRM 51-40-2, FIG 1, PG 1-6.

Part: ANGLE — CRACKED (BS 1100) · airframe 39,189 hrs · 27,373 cycles

MAIN CABIN UPPER LOBE STA 1100, "LEFT AND 1" RIGHT OF STR 1, HAS 2EA RIVETS WITH CRACKS AROUND RIVETS. REPAIRED DAMAGED AREA IAW SRM 53-30-3, FIG 3, AND SB 727-53A0204. REPAIRED DAMAGED SKATE ANGLE IAW SRM 51-40-9. PREPPED AND PAINTED AREA IAW AMM 51-20-151-7.

Part: SKIN — CORRODED (BS 950D-950E) · airframe 39,189 hrs · 27,373 cycles

AFT BAG BIN FUSE SKIN CORRODED ADJACENT TO STR 29L BETWEEN FS 950D TO 950E. CUT OUT DAMAGE, FABRICATED REPAIR PLATE AND FILLER FROM MAT 2024-T3. TREATED AND PRIMED IAW SRM 51-10-2 AND INSTALLED REPAIR IAW SRM 53-30-3, FIG 3. MAJOR REPAIR.

Part: SKIN — MISREPAIRED (BS 1087-1096) · airframe 39,189 hrs · 27,373 cycles

EXTERNAL DOUBLER LOCATED AT STA 1087- 1096, STR 22R - 23R, DOES NOT COMPLY WITH FAA APPROVED DATA. REMOVED EXISTING REPAIR, FABRICATED NEW REPAIR DOUBLER AND FILLER FROM MAT 2024-T3, .071. TREATED AND PRIMED IAW SRM 51-10-2. INSTALLED REPAIR DOUBLER AND FILLER IAW SRM 53-30-3, FIG 1. MAJOR REPAIR.

Part: WARNING LIGHT — FALSE INDICATION (APU FIRE HANDLE) · airframe 37,668 hrs · 26,141 cycles

DURING CLIMBOUT AT FL 220 HAD INTERMITTENT MASTER FIRE WARNING LIGHT AND TESTED ENGINE AND CARGO FIRE SYSTEMS, ALL TESTED OK. DURING CRUISE AT 330 ABOUT 30 MINS LATER, APU FIRE LIGHT ILLUMINATED. NO WARNING BELL JUST THE LIGHT IN THE HANDLE. RAN RED TABS PULLED FIRE HANDLE AND PUSHED DISCHARGE BUTTON. (OPEN)

Part: FRAME — DAMAGED (FUSELAGE) · airframe 37,029 hrs · 25,639 cycles

WHILE COMPLING WITH EA 7-5310-64946 A F/U FOUND FRAME REPAIR NOT TO BE DONE IAW SRM AT BS 680 STR 24R NEED TO COMPLY WITH EA 7-5310-55392 ** SD ** COMING REPAIRED IAW EA 7-5310-55392.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 37,029 hrs · 25,639 cycles

CORROSION ON SHEAR TIE BS 950F BETWEEN STRS 29R AND 28R. REPAIRED SHEAR TIE BS 950F BETWEEN STRS 29R AND 28R PER SRM 53-10-4 FIG 15.

Part: SKIN — CORRODED (FUSELAGE) · airframe 37,029 hrs · 25,639 cycles

CORROSION ON INNER SKIN BS 720C LBL 5 WL 136. BLENDED CORROSION ON INNER SKIN AT BS 720C BL 0 AND ON SHEARTIE BS 720C RBL 5 - LBL5 W/L 136. BOTH AREAS FOUND TO BE OUT OF LIMITS PER SRM 53-10-1 FIG 1 AND 53-30-1 FIG 1. FABRICATED REPLACEMENT SHEARTIE BAC1490-2785, 707556X.050 INCH NR 563248. INSTALLED REPAIR BS 720C RBL5 - LBL 5 PER SRM 53-10-4, FIG 15. REMOVED DAMAGED SECTION OF INTERSKIN, FABRICATED REPAIR PLATE 2024T3X.125 NR 525155 AND INSTALLED REPAIR BS 720C BL 0 W/L 136 PER SRM 53-30-3 FIG 1.

Part: THERMOSTAT — INOPERATIVE (ANTI-ICE SYS) · airframe 36,294 hrs · 25,094 cycles

PASSING THROUGH 7500 FT ANTI ICE DUCT OVERHEAT NR 2 LIGHT ILLUMINATED. TEMP WAS FULL HOT 250 DEG C, THEN EXTINGUISHED SHORTLY AFTER (30 SEC) NR 2 LOWER AFT BODY OVERHEAT LIGHT ILLUMINATED. DUCT OVERHEAT LIGHT ILLUMINATED ONCE AGAIN AFTER LANDING. REMOVED AND REPLACED NR 2 ENG THERMOSTATIC VALVE PER MM 30-21-021-4. RAN ENGINES AT HIGH PWR ANTI-ICE TEMP INDICATION WAS AT 219 DEG C; WELL BELOW 490 DEG C THRESHOLD PER MM 30-21-001-0 WHICH ILLUMINATES THE OVERHEAT LIGHT.

Part: FLAP — LOOSE (WING) · airframe 35,364 hrs · 24,297 cycles

AIRFRAME BUFFET OCCURRED DURING CLIMB OUT AT .65 MACH, SLOWING THE AIRCRAFT DECREASED THE BUFFET. NO BUFFET AT .58 MACH. INSPECTED FLAPS AND AILERONS FOR SECURITY. FOUND THE RT OUTBD AFT FLAP HAD EXCESSIVE PLAY. DROPPED FLAPS AND CHECKED THE AFT FLAP AFT ROLLER ECCENTRIC MEASUREMENT. FOUND ALL OF THEM OUT OF LIMITS. ADJUSTED ALL RT OUTBD AFT FLAP ECCENTRICS PER M/M 27-51-012-4. CYCLED FLAPS SEVERAL TIMES. OPS CHECK IS NORMAL. ALSO FOUND RT OUTBD FLAP, OUTBD JACKSCREW FAIRING SLIGHTLY LOOSE. SECURED ALL MOUNT BOLTS PER M/M 27-51-023-4.

Part: SKIN — CORRODED (FUSELAGE)

CORROSION AT INNER SKIN SURFACE AT BS 470, WL 138, BL 0, COMMON TO ANTENNA MOUNT AREA.

Part: FLOORBEAM — CORRODED (FUSELAGE)

CORROSION ON FLOORBEAM AT BS 890, LBL 50-52, WL 201 AFT SIDE OF LWR FLANGE UPPER SIDE.

Part: SPAR — CHAFED (VERTICAL STAB) · airframe 35,189 hrs · 24,161 cycles

VERT FIN MID SPAR IS CHAFED AT STA 228 RIGHT HAND SIDE. REMOVED AND REPLACED VERT FIN MID SPAR PER EA 7-5510-64975.

Part: SPAR — CHAFED (VERTICAL STAB) · airframe 35,189 hrs · 24,161 cycles

VERT FIN MID SPAR IS CHAFED AT STA 228, LEFT HAND SIDE. REMOVED AND REPLACED VERT FIN PER EA 7-5510-64976.

Part: FRAME — CHAFED (FUSELAGE) · airframe 35,189 hrs · 24,161 cycles

CHAFING ON FRAME FROM HYDRAULIC LINE AT BS 560, STR 4R.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 35,189 hrs · 24,161 cycles

CORROSION ON UPPER FLANGE OF FLOORBEAM BS 1050, LBL 19, WL 208.

Part: FRAME — DENTED (FUSELAGE) · airframe 35,298 hrs · 24,224 cycles

FRAME DENTED BS 680, STR 24R.

Part: FRAME — DENTED (FUSELAGE) · airframe 35,189 hrs · 24,161 cycles

FRAME DENTED BS 500, STR 24 - 25L.

Part: KEELBEAM — CRACKED (FUSELAGE)

RT WHEEL WELL KEELBEAM FWD VERTICAL CHORD IS CRACKED BETWEEN TWO FASTENERS.

Part: KEELBEAM — CRACKED (FUSELAGE)

RIGHT WHEEL WELL KEELBEAM FWD VERTICAL CHORD IS CRACKED BETWEEN TWO FASTENERS. R & R KEELBEAM PER SRM 51-30-2.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 35,189 hrs · 24,161 cycles

CORROSION ON FLOORBEAM LWR FLANGE BS 900, LBL 54-68, WL 208 (C53-224-01, 2).

Part: STRINGER — CRACKED (FUSELAGE) · airframe 35,189 hrs · 24,161 cycles

CRACKED STR WITH 4 OPEN HOLES BS 640, STR 27 LT. REMOVED AND REPLACED STRINGER PER SRM 53-10-3 FIG 1.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 35,189 hrs · 24,161 cycles

HOLE IN L-ANGLE CRACKED AT BS 783.

Part: STRAP — CRACKED (FUSELAGE) · airframe 35,189 hrs · 24,161 cycles

LAST HOLE IN REINFORCEMENT STRAP CRACKED. REMOVED AND REPLACED STRAP PER SRM 51-30- 5, 51-10-2.

Part: SKIN — CHAFED (PYLON) · airframe 35,189 hrs · 24,161 cycles

SKIN CHAFED AT BS 1352 AT NR 2 ENG RT RAIN GUTTER 15 INCHES BELOW NR 3 PYLON T/E AND RAIN GUTTER. REMOVED AND REPLACED PER EA 7-5410-64955 & SRM 54-30-3.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 35,189 hrs · 24,161 cycles

CORROSION ON TOP OF FLOORBEAM BS 360, RBL 6. REMOVED AND REPLACED FLOORBEAM PER SRM 53-10-8 FIG 3.

Part: DUCT — LEAKING (A/C BAY)

LWR BODY O/H LIGHT ILLUM. REMOVED AND REPLACED NR 2 PACK DUCT. LEAK CHECK GOOD.

Part: CONTROL UNIT — FAULTY (E&E COMPARTMENT)

01-268 DUR FLT WITH ENG ANTI-ICE OPEN LWR AFT BODY O/H LIGHT ILLUM. R&R FIRE DET O/H DETECTOR PER MM 20-10-017-2. TEST GOOD.

Part: CONNECTOR

01-258 DUR CRUISE LWR AFT BODY O/H LIGHT ILLUM. R&R CONNECTOR D1304 OF R/H STAIRWELL ELEMENT M365 PER IAW 727-2 MM CH 20 SYS.

Part: VALVE — FAILED (AIR STAIR)

01-218 LWR AFT BODY OVERHEAT LIGHT ILLUM. ACCOMPLISH RED TAB PROC. LIGHT WENT OUT FOLLOWING CLOSING #3 BLD AIR VALVE. LEAK BETWEEN #3 BLD AIR VALVE & RH PACK VALVE. R&R LEFT PURGE VALVE PER MM 36-13-011. OPS CK GOOD.

Part: WARNING LIGHT — ILLUMINATED (OVERHEAT SYS)

LWR AFT BODY OVERHEAT LIGHT ILLUM DURING CLIMBOUT. LIGHT WENT OUT WHEN NR 3 BLD VALVE AND RIGHT PACK TURN OFF PER RED TABS. RAN 2 AND 3 ENG PER JET RUN HANDBOOK CND. NO HISTORY NOTED. OK FOR SERVICE.

Part: CONTROL UNIT — FAILED (OVERHEAT DETECT)

IN CR LWR AFT BODY OVERHEAT LIGHT ILLUM. PERFORMED RED TABS. REMOVED AND REPLACED OVERHEAT DETECTION CONTROL UNIT PER MM 26-12-011-05. SYSTEM CHECK NORMAL.

Part: CONTROL UNIT — FAULTY (NR 3 ENGINE)

LWR AFT BODY O/H LIGHT CAME ON. TURN OFF R/PACK AND NR 3 ENG BLD AND O/H LIGHT WENT OUT. REMOVED AND REPLACED CONTROL UNIT PER 727-200 MM 26-14-000-1. RAN A/C ENG 3 PER JET RUN HDBK. NO O/H LIGHT. OPS CK GOOD.

Part: CLAMP — LOOSE (BLEED AIR)

AFT LEVEL OFF LWR AFT BODY O/H LIGHT ILLUM, RED TAB PROC UTILIZED AND LIGHT EXT. SECURED CLAMP AT PURGE BLD LINE ON NR 1 ENG BLD AIR CLEANER, NO LEAKS NOTED. PERF O/H DETECT ADJUST AND TEST AND OPS CK NORM PER B727 MM 26-14-000-5.

Part: ADI — FAULTY (CONTROL CABIN)

00-332 DURING T/O 1ST OFFICER ADI HAD RED GYRO FLAG APPEAR. ADI WENT TO 2 DEG NOSE DOWN WHEN AC WAS AT 15 DEG. CIRCUIT BREAKERS ALL IN. R&R NR 2 ADI PER MM 34-62-011. OPS CK GOOD.

Part: UPLOCK BRACKET — SHEARED (MLG)

AFT T/O & RAISING GEAR HANDLE RED LEFT GEAR UNSAFE LIGHT REMAIN ILLUM. CONTINUED FLT AND MONITORED LIGHT IN ACCORD WITH RED TAB PROC. *S/D* REMOVED AND REPLACED LEFT MAIN GEAR UPLOCK PER MM 32-32-51. OPS CK GOOD.

Part: SKIN — DAMAGED (BS 1031)

OUTER SKIN SCRATCHED BS 1031 FROM STR 29L TO STR 29R. *S/D* REPAIRED SKIN PER FEDEX SRM 53-30-3 FIG 3.

Part: SKIN — DENTED (BS 406)

DENT IN EXTERNAL SKIN BS 406, STR 17L. *S/D* CUT OUT DAMAGE AND REPAIRED SKIN PER FEDEX SRM 53-30-3 FIG 3.

Part: SKIN — CORRODED (BS 817)

NR 598 - CORROSION (C53-224-05) ON UPPER LEVEL CELL SKIN BS 817, LBL 12, WL 195. REMOVED CORROSION PER FEDEX SRM 51-10-6. REPLACED FASTENERS PER FEDEX SRM 51-30-2 AND FEDEX EA NR 7-5730-47895 AND PERF LEAK CK MM 28-11-00, CK GOOD.

Part: ANGLE — CORRODED (BS 294.5)

CORROSION (C53-100-01,1) ON UPPER PORTION OF HORIZONTAL L ANGLE AT BS 294.5, RBL 11 IN NLG W/W. *S/D* REMOVED AND REPLACED IAW FEDEX SRM 51-30-2 & FEDEX DRAWING 65-18415.

Part: SKIN — LIGHTNING STRIKE (BS 400)

LIGHTNING STRIKE FASTENER HOLE BS 400, 3 INCHES BELOW STR 21 L. *S/D* REMOVED AND REPLACED PER FEDEX SRM 53-30-3 FIG 13A.

Part: ANGLE — CORRODED (BS 294.5)

CORROSION (C53-100-01,1) ON LWR END OF VERTICAL L ANGLE AT BS 294.5, LBL 23 IN NLG W/W TORQUE BOX. *S/D* REMOVED AND REPLACED PER FEDEX SRM 51-40-4.

Part: SEAT TRACK — CORRODED (BS 1030)

SEAT TRACK AT BS 1030 TO BS 1030+11, LBL 45, WL 208 WAS CORRODED. *S/D* REMOVED FLOOR PNLS BS 990-1110, LBL 45-65, BS 997-1068 LBL 25-45, PER FEDEX 727 SRM 51-30-2 & 51-20-4.

Part: INTERCOSTAL — CORRODED (BS 740)

CORROSION EMANATING FROM FWD END OF DELTA BOX BS 740 FRAME LBL 4 & LBL 9, WL 148. *S/D* REMOVED AND REPLACED INTERCOSTAL PER FEDEX 57-30-2, 57-20-4 SRM & FEDEX DRAWING NR 65-23555.

Part: STATIC LINE — MALFUNCTION (LT COCKPIT)

RIGHT AFTER TAKEOFF WINDSHEAR WARNING WENT OFF AND CAPTAINS INSTRUMENTS (AIRSPEED AND ALTIMETER) STARTED READING ERRONEOUSLY. ABOUT ONE MINUTE LATER GOT A SECOND WINDSHEAR WARNING. AT 4000 CAPTAINS ALTIMETER READ 1100 AND AIRSPEED INDICATOR WAS PEGGED AT BOTTOM. *S/D* REMOVED AND REPLACED STATIC LINE ON CAPT IVSI AND PERFORMED FULL RANGE LEAKAGE TEST PER MAINTENANCE MANUAL 34-11-0. NO LEAKS NOTED AND ALL IND NORMAL. REMOVED AND REPLACED GPWS COMPUTER AND TESTED PER MAINTENANCE MANUAL 34-52-00. OPERATIONAL TEST NORMAL.

Part: AIR DATA COMP — INOPERATIVE (E/E COMP)

DURING TAKEOFF ROLL AT 80 KNOTS CHECK, AIRSPEEDS CHECKED OK THEN CAPTAIN'S DECREASED TOWARDS 0. CAPTAIN'S ALTIMETER FROZE AT 1500 FT AND STAYED THERE THROUGHOUT FLIGHT. TRIED AUXILIARY STATIC SOURCE. NO CHANGE TO CAPTAIN'S AIRSPEED OR ALTITUDE. NO FLAGS ON CAPTAIN'S ALTIMETER. *S/D* REMOVED AND REPLACED DIGITAL AIR DATA COMPUTER AND TESTED SYSTEM PER MAINTENANCE MANUAL 34-12-0. ALL TESTS AND CHECKS NORMAL. NO FAULTS NOTED. AIRCRAFT DOWN GRADED TO CHECK CAT II A AND B.

Part: OVERHEAT LIGHT — MALFUNCTION (NR 1 STRUT)

WHILE CONDUCTING THE PRESSURIZATION DISCREPANCY SHEET THE NR 1 STRUT OVERHEAT LIGHT BEGAN TO FLICKER. NR 1 BLEED OFF, LEFT PACK OFF, NR 2 BLEED CLOSED, NR 3 BLEED AND RIGHT PACK ON. RAN ALL 3 ENGINES, AND APU AND PACKS, UNABLE TO DUPLICATE. SYSTEM FUNCTIONAL CHECK OK PER MAINTENANCE MANUAL 26-14-0.

Part: FLOORBEAM — CORRODED (BS 360)

HEAVY EXFOLIATION CORROSION ON 360 FLOORBEAM AT LBL 4 TO RBL 2. CUTOUT DAMAGED AREA AND INSTALLED DOUBLER PER SRM 53-10-8 PG 18.

Part: FRAME — DENTED (BS 500)

FRAME DENTED BETWEEN STR 24R AND 25R BS 500. CUTOUT DAMAGE AND INSTALLED DOUBLER PER SRM 53-40-3.

Part: FRAME — DENTED (BS 560)

FWD CARGO BS 560 BETWEEN STR 24 LT AND 22 LT FRAME DENTED. INSTALLED DOUBLER AT BS 560 BELL FRAME STR 24 LT TO 22 LT PER SRM 53-40-3.

Part: FRAME — DENTED (BS 600)

FWD CARGO FRAME DENTED AT BS 600 BETWEEN STR 23 LT AND 25 LT. INSTALLED DOUBLER AT BELL FRAME BS 600 BETWEEN STR 23 LT AND 25 LT PER SRM 53-40-3.

Part: GEAR SWITCH — OUT OF ADJUST (LT MLG)

LEFT MAIN GEAR LIGHT REMAINED ON AFTER RAISING GEAR LEVER. EXTINGISHED AFTER MOVING GEAR LEVER TO OFF. *S/D* SWITCHES ADJUSTED - (NR0007) AND OPS CHECKED NORMAL PER M/M 32-32-0.

Part: DUCT — FAILED (LT PACK)

LOWER AFT BODY OVERHEAT LIGHT CAME ON 40 MINUTES INTO FLIGHT. LIGHT WENT OUT AFTER SECURING LEFT PACK AND NR 1 AND NR 2 BLEED. THE LEAK IS BETWEEN THE BLEED VALVE AND THE PACK VALVE AS PER RED TABS. *S/D* REPAIRED DUCTS IN KEEL BEAM AND AFT CARGO AREAS. DUCTS REPAIRED AND LEAKED CK'D ON NR 0712, 0713, 0714 AND 0715. INSTALLED AND SAND ON SAME NR'S. REPAIRED DUCTS PER BOHM 36-10-01.

Part: ACCESSORY UNIT — MALFUNCTION (LT MLG)

97-0148 IN FLT AFTER RAISING THE GEAR, LT MAIN IND UNSAFE RED. LEFT GEAR LIGHT ON. AFTER RECYCLING 2 TIMES THE LIGHT WENT OUT. HANDLE RETURNED TO OFF POSITION AND ALL LIGHTS REMAINED OFF. ALL OTHER DOOR LIGHTS INDICATED NORMAL OPERATION. REMOVED LANDING GEAR ACCESSORY UNIT TO CHECK FOR MOISTURE. CLEANED CONNECTOR. REINSTALLED ACCESSORY UNIT. ALSO, CLEANED TARGET SENSOR ON LIMIT UPLOCK. TESTED LANDING GEAR ACCESSORY UNIT AS PER MAINTENANCE MANUAL 32-09-121. OPERATIONAL CHECK GOOD.

Part: OVERHEAT LIGHT — ILLUMINATED (LOWER BODY)

DURING CLIMBOUT AT FLIGHT LEVEL 200, THE LOWER AFT BODY OVERHEAT LIGHT ILLUMINATED. COMPLIED WITH ABNORMAL CHECKLIST. LOWER AFT BODY OVERHEAT LIGHT EXTINGUISHED WITH LEFT PACK OFF AND NR 1 THROTTLE RETARDED. CHECKED AFT STAIRS AREA, NO LEAKS. REMOVED AFT FORWARD LEFT CARGO LINER AND CHECKED BEHIND LINER FOR LEAKS, NONE NOTED. RAN NR 1 ENGINE AND LEFT PACK, NO DEFECTS FOUND. REINSTALLED LINER.

Part: OVERHEAT SENSOR — OUT OF POSITION (AFT BODY)

97-0125 REPEAT ITEM (SEE AIRCRAFT MAINTENANCE LOG # 51863). LOWER AFT BODY LIGHT ILLUMINATED DURING CLIMB. FOLLOWED CHECK LIST PROCEDURE. SHUTDOWN LEFT PACK AND ENGINE NR 2 BLEED VALVE RETARDED NR 1 THROTTLE AND LIGHT WENT OUT. RESTORED NR 1 THROTTLE AND LIGHT REMAINED OUT FOR REMAINDER OF FLIGHT. REPOSITIONED ELEMENT IN AFT BODY AREA PER MAINTENANCE MANUAL 26-14-0. CHECKED WITH ENGINE RUNNING. CHECKS OK. NO LEAKS NOTED.

Part: MODULE — MALFUNCTIONED (COCKPIT)

LEFT GEAR INDICATED UNSAFE AFTER NORMAL GEAR EXTENSION, NO GREEN LIGHT. COMPLIED WITH RED TAB PROCEDURES, STILL NO GREEN LIGHT, BUT POINTER WAS IN GREEN BAND. ON FINAL APPROACH APPROXIMATELY 160 KTS GREEN LIGHT ILLUMINATED RECYCLED GEAR TRIED NEGATIVE G, BUT UNSUCCESSFUL. REMOVED AND REPLACED LEFT HAND MAIN GEAR DOWNLOCK SENSOR AS PER MAINTENANCE MANUAL 32-61-91, NO HELP. FOUND LANDING GEAR INSTRUMENT MODULE PANEL BAD. ORDERED SAME, REMOVED AND REPLACED LANDING GEAR INSTRUMENT MODULE, SYSTEM OPERATIONAL AND FUNCTIONS NORMAL.

Part: SMOKE DETECTOR — MALFUNCTIONED (NR 2 CARGO)

NR 2 CARGO SMOKE LIGHT AND BELL CAME ON FOR 5 SECONDS, THEN OFF. AFTER 2 MINUTES BOTH CAME ON AGAIN FOR 5 SECONDS, THEN OFF AGAIN ON FINAL APPROACH. REMOVED AND REPLACED NR 2 CARGO SMOKE DETECTOR AND OPS CK NORMAL.

Part: SHEAR TIE — CORROSION (BS 950)

CORROSION ON SHEAR TIE AND FRAME AT BS 950 RBL 10 TO 15 WL 150. REPLACED AFTER CUT OUT, PER FEDEX SRM 53-10-4.