N211FE

Part: SLIDE — UNSECURE (L1 DOOR) · airframe 27,996 hrs · 18,918 cycles

WHEN OPENING L1 DOOR FOR PREFLIGHT CHECK FOUND DOOR SLIDE LAYING ON FLOOR. REINSTALLED SLIDE ON L1 DOOR REF AMM 25-60-015-2. ACFT OK FOR SERVICE.

Part: SLIDE — DISLODGED (CABIN) · airframe 27,936 hrs · 18,886 cycles

FOUND ESCAPE SLIDE OUT OF COMPARTMENT AND UNPACKED, LAYING IN COURIER COMPARTMENT. INSTALLED SERVICABLE ESCAPE SLIDE IAW MM 25-60-015-2.

Part: WEB — DAMAGED (BS 328) · airframe 27,920 hrs · 18,863 cycles

L1 DOOR INTERIOR WEB DAMAGED, INSIDE SECOND LIGHTNING HOLE FROM BOTTOM NEAR CRNTER OF DOOR BS 328. DAMAGE OUT OF LIMITS IAW SRM 52-00-2. REMOVED WEB IAW SRM 51-30-2. FABRICATED NEW WEB IAW SRM 52-10-1 FIG 1, 51-30-5 AND 51-20-1 FIG7. INSTALLED REPAIR PARTS IAW SRM 51-30-2.

Part: SKIN — GOUGED (NR 7 SLAT) · airframe 27,920 hrs · 18,863 cycles

RT WING, NR 7 SLAT OTBD HOOK AREA HAS GOUGE ON T/E SKIN OTBD SIDE. REMOVED DAMAGED DOUBLER IAW SRM REV 103 51-30-2 FABRICATED DOUBLER AND INSTALLED IAW SRM 57-50-3 FIG 10.

Part: RIB — CRACKED (LT WING) · airframe 27,920 hrs · 18,863 cycles

LEFT WING NR 3 SLAT INBOARD ACTUATOR ATTACH RIB INSIDE SLAT IS CRACKED. REMOVED CRACKED RIB IAW SRM 51-30-2 REV 103. FABRRICATED NEW RIB IAW DRAWING 65-17294 AND SRM 51-20-1 FIG.7 INSTALLED NEW RIB IAW SRM 51-30-2

Part: RIB — CRACKED (NR 3 SLAT) · airframe 27,920 hrs · 18,863 cycles

LT WING NR 3 SLAT OTBD ACTUATOR ATTACH RIB INSIDE SLAT IS CRACKED. REMOVED RIB IAW SRM REV 103 51-30-2. FABRICATED NEW RIB IAW DWG 65-17294 AND SRM 51-20-1 FIG 7. INSTALLED NEW RIB IAW SRM 51-30-2 & 51-10-2.

Part: SEAT TRACK — CORRODED (BS 344) · airframe 27,920 hrs · 18,863 cycles

CORROSION ON SEAT TRACK FLANGE BS 344 LBL 25. REMOVED SEAT TRACK SECTION IAW SRM 51-30-2 REV 103. FABRICATED & INSTALLED SEAT TRACK SECTION IAW SRM 53-10-2 FIG. 7.

Part: STRINGER — CORRODED (BS 382 S4L) · airframe 27,920 hrs · 18,863 cycles

UPPER FUSELAGE INTERIOR, STRINGER 4L HAS CORROSION AT BS 682. REPLACED STRINGER SPLICE.

Part: SUPPORT — CORRODED (BS 661 S2L) · airframe 27,920 hrs · 18,863 cycles

UPPER FUSELAGE INTERIOR, MAIN CARGO DOOR UPPER SILL SUPPORT LOWER SURFACE HAS LIGHT SURFACE CORROSION AT BS 661, STRINGER 2L. REMOVED DAMAGED SILL SUPPORT IAW SRM 51-30-2. FABRICATED NEW SILL SUPPORT IAW SRM 53-10-2, FIG 3 AND 51-20-1, FIG 7. INSTALLED NEW SILL SUPPORT IAW SRM 51-30-2.

Part: STRINGER SPLICE — CORRODED (BS 678 S4L) · airframe 27,920 hrs · 18,863 cycles

UPPER FUSELAGE INTERIOR, STRINGER 4L HAS CORROSION AT BS 678 SPLICE. REMOVED SPLICE IAW SRM 51-30-2 REV 103. FORMED NEW SPLICE IAW SRM 53-10-2. INSTALLED NEW SPLICE IAW SRM 51-30-2

Part: SKIN — GOUGED (BS 520 S27L) · airframe 27,920 hrs · 18,863 cycles

EXTERIOR SURFACE GOUGE AT BS 520 AT S27L. CUT OUT DAMAGED AREA IAW SRM 53-30-3 REV 103 FIGURE 14. FABERICATED REPAIR DOUBLER, STRUCTURAL FILLER, AND FILLER IAW SRM 53-30-3 FIG 14. INSTALLED REPAIR PARTS IAW SRM 51-30-2.

Part: SKIN — CORRODED (BS 682-686) · airframe 27,920 hrs · 18,863 cycles

CORROSION ON INNER SKIN AT DRAIN VALVE, FWD. PIT BS 682 - 686, RBL 3.0. CUT OUT DAMAGED AREA IAW SRM REV.103, 53-30-3 FIG 3A. FABRICATED REPAIR DOUBLER AND FILLER AND INSTALLED IAW SRM 53-30-3 FIG 3A .

Part: STRINGER — CORRODED (BS 720 S4L) · airframe 27,920 hrs · 18,863 cycles

UPPER FUSELAGE INTERIOR, STRINGER 4 LT HAS CORROSION AT BS 720. CUT OUT DAMAGED AREA IAW SRM 53-10-3 REV 103 FIG 3. FABERICATED REPAIR PARTS IAW SRM 53-10-3 FIG 3. INSTALLED REPAIR PARTS IAW SRM 51-30-02.

Part: STRINGER — CORRODED (BS 720A S5L) · airframe 27,920 hrs · 18,863 cycles

UPPER FUSELAGE INTERIOR, STRINGER 5 LEFT HAS CORROSION AT BS 720A 3 INCHES. CUT OUT DAMAGED AREA IAW SRM REV.103 53-10-3 FIG3 FABRICATED REPAIR STARS AND FILLER IAW SRM 53-10-3 FIG 3 INSTALLED REPAIR PARTS IAW SRM 51-30-02 AND 53-10-3 FIG 3

Part: STRINGER — CORRODED (BS 702 S5L) · corrosion level 2 · airframe 27,920 hrs · 18,863 cycles

UPPER FUSELAGE INTERIOR STRINGER 5 LT HAS CORROSION AT BS 702. CUT OUT DAMAGED AREA IAW SRM 53-10-3 REV 103 FIG 3. FABRICATED STRAPS AND FILLER IAW SRM 53-10-3 FIG 3 INSTALLED REPAIR PARTS IAW SRM 51-30-02 AND 53-10-3 FIG 3.

Part: SKIN — GOUGED (BS 312) · airframe 27,920 hrs · 18,863 cycles

EXTERIOR FUSELAGE, 2 LONG GOUGES UNDER L-1 DOOR. CUTOUT DAMAGE AREA IAW SRM 53-30-3 REV 103 FIG 1. FABRICATED REPAIR DOUBLER AND FILLER IAW SRM 53-30-3 FIG 1. INSTALLED REPAIR FILLER AND DOUBLER IAW SRM 51-30-2 AND 53-30-3 FIG 1.

Part: ATTACH ANGLE — CRACKED (RT WING) · airframe 27,920 hrs · 18,863 cycles

RIGHT WING, NR 8 SPOILER ACTUATOR SUPPORT FITTING, HAS LOWER LT SIDE ATTACH ANGLE CRACKED AT WBL 120. REMOVED SECTION OF ATTACH ANGLE AND FABRICATED REPAIR PARTS IAW DWG SR27-57-038 REV C. INSTALLED ALL REPAIR PARTS IAW SRM 51-30-2 AND DWG SR27-57-038 REV C.

Part: STRUCTURE — CRACKED (RT WING TE FLAP) · airframe 27,920 hrs · 18,863 cycles

RT WING, INBD FLAP, MID FLAP AFT CHORD IS CRACKED AT 2 EA AREAS, NEAR THE MOST INBD HINGE AND ACTUATING ROD FOR AFT FLAP. CUT OUT DAMAGED AREA IAW SRM 51-40-4 FIG 1. FABRICATED REPAIR FILLER AND SPLICE ANGLE IAW SRM 41-40-4 FIG 1 AND 57-50-2 FIG 5. TREATED AND PRIMED AND INSTALLED REAPIR PARTS AT RH WING I/B FLAP MID FLAP AFT CHORD IAW SRM 51-40-4 FIG 1 AND 51-30-2.

Part: WEB — CRACKED (BS 1303) · airframe 27,920 hrs · 18,863 cycles

CRACK IN SIDE WEB AT LIGHTING HOLE LT SIDE AFT VENTRAL STAIR OPENING, BS 1303. CUTOUT DAMAGE AREA TORQUE BOX WEB IAW SRM 51-10-1, FIG 1. FABRICATED REPAIR DOUBLER IAW SRM 53-10-2, FIG 6 AND 51-40-2, FIG 1. INSTALLED REPAIR DOUBLER IAW SRM 51-40-2, FIG 1.

Part: WEB — CRACKED (TORQUE BOX) · airframe 27,920 hrs · 18,863 cycles

CRACK IN SIDE WEB AT LIGHTING HOLE RT SIDE AFT VENTRAL STAIRS BS 1239. CUT OUT DAMAGE AREA TORQUE BOX WEB IAW SRM 51-40-2 FIG 1. FABRICATED REPAIR DOUBLER IAW SRM 51-40-2 FIG 1 AND 53-10-2 FIG 6. INSTALLED REPAIR DOUBLER IAW SRM 51-40-2 FIG 1.

Part: SLIDE — DAMAGED (PAX DOOR) · airframe 27,906 hrs · 18,852 cycles

FWD ENTRY DOOR ESCAPE SLIDE, PART OF THE SLIDE DROOPING OUT OF CONTAINER. TROUBLESHOOTING. REMOVED ESCAPE SLIDE FROM ENCLOSURE. SECURED LOOSE ITEMS WITH EXISTING HOOK AND LOOP ON FLAPS. RE-INSTALLED ESCAPE SLIDE INTO ENCLOSURE IAW MM 25-60-015-2. OPS NORMAL.

Part: FITTING — INOPERATIVE (GIRT BAR) · airframe 27,843 hrs · 18,797 cycles

SLIDE FALLS OUT TOO EASILY. REPLACED GIRT BAR PLASTIC CLIPS.

Part: GEARBOX — LEAKING (NR 3 ENGINE) · airframe 27,092 hrs · 18,227 cycles

DURING CRUISE NR 3 LOW OIL FILTER BYPASS LITE ILLUMINATED. OIL PRESSURE INDICATED 28PSI QTY WAS 3.5 GALLONS AND TEMP WAS 95 DEG, OPERATED 2 MIN AT IDLE SHUTDOWN IAW RED TABS DID NOT LOOSE OIL QTY. ENGINE CONTINUED TO WINDMILL AFTER SHUTDOWN. R & R THE NR 3 ENGINE IAW THE FOLLOWING W/C'S 72T0002, 70T0001-03, 70T0301-03, 70T0004-03. OP'S AND LEAK CHECKS GOOD. PERFORMED MAX POWER RUN. ACCELERATION AND REVERSER CHECK IAW JRH.

Part: SWITCH — FAILED (HYD PRESSURE) · airframe 26,852 hrs · 18,071 cycles

AILERON SYS A ANNUNCIATOR LIGHT ON F/O PANEL CAME ON 30 AFTER LEVEL OFF, NO LOSS OF A SYS A HYD FLUID. REMOVED AND REPLACED AILERON "A" SYS HYD LOW PRESSURE WARNING SWITCH IAW AMM 27-10-144-4, OPS CHECKED GOOD.

Part: WARNING LIGHT — FALSE ACTIVATION (TAIL SKID) · airframe 26,421 hrs · 17,740 cycles

TAILSKID LIGHT REMAINED ON AFTER GEAR RETRACTION. CREW REPORTED THAT AFTER CYCLING GEAR THE SYSTEM WORKED NORMALLY AND ON APPROACH, SYSTEM FUNCTIONED NORMAL. INSPECTED SWITCH AT TAILSKID. NO DEFECTS FOUND. SUSPECT ICE IN BILLINGS CAUSED SWITCH TO STICK. LUBRICATED SWITCH, NO HISTORY FOR 90 DAYS, ACFT RELEASED FOR SERVICE.

Part: FITTING — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 25,992 hrs · 17,439 cycles

GENERATED BY EO 7-5510-7-5000, HORIZONTAL STAB RT HINGE FITTING O/B BUSHING BORE HAS CORROSION OVERSIZED LUG BORE TO 2.2244 INCH CORROSION REMOVED. HFEC INSPECTED BORE NO DEFECTS NOTED. FABRICATED OVERSIZE BUSHING, CAD PLATED BUSHING. INSTALLED OVERSIZE BUSHING IN LUG, IAW MM 55-10-051-8. THIS IS CLASSIFIED AS A MINOR REPAIR.

Part: SUPPORT ANGLE — CORRODED (FAIRING SUPPORT) · corrosion level 2 · airframe 25,992 hrs · 17,439 cycles

RT WHEEL WELL, LOWER FUSELAGE FAIRING SUPPORT FRAME HAS CORROSION, RBL 21, STA 950 FABRICATED TEE ANGLE FROM RT WHEEL WELL FUSELAGE FAIRING SUPPORT STA 950 REFB DWR 65-25550 AND CUSTOMER REQUEST, HEAT TREATED TRACKING NUMBER 2008-08-057. TREATED AND PRIMED, REF SRM 51-10-2 PG 1-7. INSTALLED REF SRM 51-30-2 PG 2,4-13. THIS IS CLASSIFIED AS A MINOR REPAIR.

Part: FAIRING — CRACKED (NR 5 FLAP TRACK) · airframe 25,992 hrs · 17,439 cycles

NR 5 FLAP TRACK MIDDLE FAIRING, AFT SKIN BENT/CRACKED. REMOVED DAMAGED SKIN, REF 51-30-2, PG 1-7. ORIGINAL SKIN AND REPLACEMENT BOTH IDENTIFIED AS 7075-T6, .040 REF 65-21795, REV E, PG 35 AND DWG 65-21795, AND A-TAG NR A27927. FABRICATED NEW SKIN, REF SRM 51-20-01, P 1-7. TREATED AND PRIMED REF SRM 51-10-2 P 1-27. INSTALLED SKIN REF 51-30-2, P 1-7. TOP COATED SKIN REF MM 51-20-151-PG 7. THIS IS CLASSIFIED AS A MINOR REPAIR.

Part: BRACKET — CRACKED (ZONE 100) · airframe 25,992 hrs · 17,439 cycles

AIRSTAIR COMPARTMENT LT BRACKET FOR FIRE LOOP SUPPORT IS CRACKED AT BULKHEAD STA 1183 NEAR FLOOR LEVEL. REMOVED OLD BRACKET REF SRM 51-30-02 P 1-7, IDENTIFIED MATERIALS REF DWR 65-27195 FRAME 1 SHEET 3 REV E ALSO A-TAG NR A03329. FABRICATED NEW BRACKET REF DWR 65-27195 PAGE 1. TREATED AND PRIMED BRACKET REF SRM 51-10-2 PG 1-27. INSTALLED BRACKET REF SRM 51-30-02 PG 1-7. THIS IS CLASSIFIED AS A MINOR REPAIR.

Part: BEAM — CORRODED (MLG WW) · corrosion level 2 · airframe 25,992 hrs · 17,439 cycles

LT MLG W/W UPPER BOX BEAM LOWER WEBS AFT OF STA 910 AND 930 HAVE CORROSION REMOVED FASTENERS FOR ACCESS. REMOVED CORROSION, ORIGINAL .080 REMAINING .070. REMOVED .010 OUT OF LIMITS, FABRICATED REPAIR DOUBLER 7075-O-100 HEAT TREAT T6. APPLIED ALODINE AND PRIMER, INSTALLED DOUBLER AND FASTENERS REMOVED FOR ACCESS. REF SRM 53-10-1 PG 1-6A, 53-10-1 PG 6B,C, 51-10-6 PG 1 AND 5. THIS IS CLASSIFIED AS A MINOR REPAIR.

Part: FAIRING — CRACKED (NR 6 FLAP TRACK) · airframe 25,992 hrs · 17,439 cycles

RT WING NR 6 FLAP TRANSMISSION FAIRING IS CRACKED AT CENTER ATTACH HOLE REMOVED FAIRING REF 51-30-2, PG 1-7 STOP DRILLED CRACKS REF 727 SRM 51-10-1 PG 13. NDT VERIFIED CRACK CONTAINMENT. NDT MANUAL PART 6, 51-00-00 FIG 23. ORIGINAL AND REPAIR MATERIAL IDENTIFIED REF SRM 57-20-2, PG 15 FIG 5 AND SRM 57-20-4, PG 7. WITH SRM 51-20-1, PG 13, ALSO A-TAG NR A84324. FABRICATED NEW REPAIR DOUBLER REF SRM 51-20-1 FIG 7. TREATED AND PRIMED REPAIR DOUBLER. REF SRM 51-10-2 PG 1 -27. INSTALLED DOUBLER REF SRM 51-30-2 PG 1-7, TOP COATED DOUBLER REF MM 51-20-151-7. REINSTALLED FAIRING REF SRM 51-30-0. THIS IS CLASSIFIED AS A MINOR REPAIR.

Part: ATTACH ANGLE — CRACKED (ZONE 600) · airframe 25,992 hrs · 17,439 cycles

RT WING, LOWER T/E PANEL BELOW NR 13 SPOILER ACTUATOR I/B ATTACH ANGLE CRACKED. REMOVED AND REPLACED CHANNEL REF SRM 51-30-5, SRM 51-30-2. THIS IS CLASSIFIED AS A MINOR REPAIR.

Part: ATTACH ANGLE — CRACKED (ZONE 600) · airframe 25,992 hrs · 17,439 cycles

RT WING LOWER T/E PANEL BELOW NR 13 SPOILER ACTUATOR O/B ATTACH ANGLE CRACKED. REMOVED AND REPLACED CHANNEL REF SRM 51-30-5, SRM 51-30-2. THIS IS CLASSIFIED AS A MINOR REPAIR.

Part: BRACKET — CRACKED (ZONE 100) · airframe 25,992 hrs · 17,439 cycles

FWD NOSE COMPARTMENT WEATHER RADAR MOUNT BRACKET CRACKED REMOVED WEATHER RADAR R/T. REPLACED MOUNT BRACKET, INSTALLED WEATHER RADAR R/T AND PERFORMED GOOD OPS CHECK REF SRM 51-30-02, AMM 34-41-041-4 AND AMM 34-41-000-5. THIS IS CLASSIFIED AS A MINOR REPAIR.

Part: ANGLE — CRACKED (ZONE 500) · airframe 25,992 hrs · 17,439 cycles

LEFT WING OB LE CAVITY, LE UPPER SKIN FORMED SUPPORT ANGLE CRACKED AT AFT END ABOVE TAI DUCT AT INBD END OF NR 4 SLAT WELL. REMOVED INTERCOSTAL AND DAMAGED SUPPORT ANGLE, FABRICATED NEW SUPPORT ANGLE, HEAT TREAT "T-3". TREAT AND PRIMED SUPPORT ANGLE, INSTALLED SUPPORT ANGLE AND INTERCOSTAL REF SRM 51-10-2, 51-30-2 P 2 AND 32, MM 51-20-151-7 PG 1. THIS IS CLASSIFIED AS A MINOR REPAIR.

Part: SUPPORT ANGLE — CRACKED (ZONE 600) · airframe 25,992 hrs · 17,439 cycles

RIGHT WING OB LE CAVITY, LE UPPER SKIN FORMED SUPPORT ANGLE CRACKED AT AFT END ABOVE TAI DUCT AT INBD END OF NR 5 SLAT WELL. REMOVED INTERCOSTAL AND SUPPORT ANGLE AT SLAT STA 260. FABRICATED NEW SUPPORT ANGLE. VERIFIED MATERIAL 2024 T-3, FAB'D WITH 2024-0, HEAT TREATED TO 2024 T-3. INSTALLED NEW SUPPORT ANGLE AND REINSTALLED INTERCOSTAL REF SRM 51-30-2 PG 2-3, DWR 69-16638. THIS IS CLASSIFIED AS A MINOR REPAIR.

Part: FRAME — CORRODED (WING TO BODY FRG) · corrosion level 2 · airframe 25,992 hrs · 17,439 cycles

LWR EXT FUSE BODY FRAME LWR CHORD IS CORRODED BS 351, LBL 17, WL 148-150. REMOVED CORROSION AT LWR EXT FUSE BODY FRAME LWR CHORD STA 351 LBL 17 - RBL 17, REF SRM 51-10-6 PG 1-5. MATERIAL LOSS 50 PERCENT, FOUND OUT OF LIMITS REF SRM 53-10-1 FIG 1. REMOVED AND REPLACED LWR CHORD (TEE ANGLE) REF BOEING DWR 65-16317, SRM 51-30-5 PG 1, 51-30-2 PG 2-5. THIS IS CLASSIFIED AS A MAJOR REPAIR.

Part: FLOORBEAM — CRACKED (ZONE 100) · airframe 25,992 hrs · 17,439 cycles

MAIN DECK FLOORBEAM INTERCOSTAL MID CHORD EXISTING REPAIR DOUBLER IS CRACKED BS 302, WL 207 FABRICATED NEW REPAIR ANGLE REF SRM 51-40-3 PG 1. TREATED AND PRIMED REF SRM 51-10-2 PG 1-9. INSTALLED ANGLE REF SRM 51-30-2 PGS 1-7. THIS IS CLASSIFIED AS A MINOR REPAIR.

Part: DUCT — CRACKED (ZONE 200) · airframe 25,992 hrs · 17,439 cycles

RT EXT FUSE NR 3 ENG FAN AIR EXH PORT ASSY IS FRETTED/CRACKED. REMOVED AND REPLACED FAN AIR EXH POT ASSY REF SRM 51-30-2 PG 1-32, REF MM 51-20-151-7 PG 1-5, REF MM 36-00-001-2 PG 1-4. THIS IS CLASSIFIED AS A MINOR REPAIR.

Part: ANGLE — CRACKED (ZONE 500) · airframe 25,992 hrs · 17,439 cycles

LT WING ROOT TE UPPER PNL IB OF NR 7 SPOILER HAS FRETTED/CRACKED IB SUPPORT ANGLE BS 950A, WBL 70. REPLACED SUPPORT ANGLES REF SRM 51-30-02 PG 1. THIS IS CLASSIFIED AS A MINOR REPAIR.

Part: FAIRING — CRACKED (WING TO BODY) · airframe 25,992 hrs · 17,439 cycles

PANEL RACK, WING BODY FAIRING 3517 AFT CORNER EXISTING COMPOSITE REPAIR IS CRACKED. REPAIRED PANEL 3517 REF SRM 51-40-9 STEP 7B(1)-7B(12) AND AMM 51-20-151-7. THIS IS CLASSIFIED AS A MINOR REPAIR

Part: DUCT — CRACKED (BLEED AIR) · airframe 25,992 hrs · 17,439 cycles

BLEED AIR EXH DUCT ON FUSELAGE ABOVE NR 1 ENG PYLON CRACKED AT AFT EDGE OF OPENING. REMOVED AND REPLACED BLEED AIR EXH DUCT ON FUSELAGE ABOVE NR 1 ENG PYLON. REF IPC 36-10-00-10 FIG 10, SRM 51-30-2 PG 13. THIS IS CLASSIFIED AS A MINOR REPAIR.

Part: BRACKET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 25,992 hrs · 17,439 cycles

CORROSION ON RT A/C BAY FWD COMPARTMENT LIGHT LENS RETAINER AND LIGHT MOUNT BRACKET. REPLACED FWD COMPARTMENT LIGHT, LENS RETAINER AND LIGHT MOUNT BRACKET. REFERENCE SWPM 20-84-10, PG 3-5; SRM 51-30-02 PG 2-3; BOEING DRW NR 66-14827-1/1. OPERATIONAL TEST OF LIGHT GOOD. THIS IS CLASSIFIED AS A MINOR REPAIR.

Part: BRACKET — CRACKED (L1 DOOR) · airframe 25,992 hrs · 17,439 cycles

L-1 GRAB ASSIST HANDLE MOUNT BRACKET CRACKED ON DOOR REPLACED FWD ENTRY DOOR ASSIST BRACKET REF: SRM 51-30-2 PG 13. THIS IS CLASSIFIED AS A MINOR REPAIR.

Part: FAIRING — CRACKED (NR 3 FLAP TRACK) · airframe 25,992 hrs · 17,439 cycles

LEFT WING INBD T/E LWR SURFACE, NR 3 FLAP TRACK FAIRING INBD ATTACH L- ANGLE CRACKED BETWEEN 2 FASTENERS, 12 INCHES FWD OF T/E PANELS AFT EDGE. REMOVED DAMAGED PORTION OF NR 3 FLAP TRACK FWD FAIRING INBD ATTACH L- ANGLE. FABRICATED FILLER AND DOUBLER, AND INSTALLED. REF SRM 51-40-03 FIG 1 AND BOEING DOC NR 65-28115. THIS IS CLASSIFIED AS A MINOR REPAIR.

Part: INTERCOSTAL — CRACKED (ZONE 100) · airframe 25,992 hrs · 17,439 cycles

MAIN DECK FLOORBEAM INTERCOSTAL UPPER CHORD IS BUCKLED/CRACKED BS 304-312, LBL 22. FABRICATED REPAIR ANGLE REF SRM 51-40-3 FIG 1. TREATED AND PRIMED REF SRM 51-10-2 PGS 1-9. INSTALLED REPAIR REF SRM 51-30-2 PG 1-7. THIS IS CLASSIFIED AS A MINOR REPAIR.

Part: FAIRING — CRACKED (LT WING TE FLAP) · airframe 25,992 hrs · 17,439 cycles

LEFT WING OB TE NR 2 FLAP TRANSMISSION JACKSCREW FAIRING ON INBD END OF MID FLAP HAS CRACK IN SIDE WEB 19 INCH AFT OF FWD END REMOVED CRACKED WEB. FABRICATED NEW WEB, P/N 65-28131-1. TREATED, PRIMED, AND PAINTED WEB. INSTALLED WEB REF SRM 51-30-2 PG 2-4/SRM 57-20-2 PG 15-17/SRM 51-20-1 PG 13/BOEING DWR NR 65-28131-1/SRM 51-10-2 PG 1-2/MM 51-20-151 PG 1. THIS IS CLASSIFIED AS A MINOR REPAIR.

Part: FAIRING — CRACKED (ZONE 500) · airframe 25,992 hrs · 17,439 cycles

LEFT WING INBD TE NR 3 FLAP TRANSMISSION JACKSCREW FAIRING ON O/B END OF MID FLAP IS CRACKED OUT OF FWD UPPER HOLE REMOVED FAIRING. NDT VERIFIED CRACK LOCATION. REMOVED DAMAGE AND INSTALLED REPAIR. REINSTALLED FAIRING TO MID FLAP REF SRM 51-30-2 PG 13/ NDT MAN PART 6 51-00-00, FIG 23/ SRM 57-20-4, FIG 1/SRM 51-30-4, FIG 1. THIS IS CLASSIFIED AS A MINOR REPAIR.

Part: INDICATOR — FAILED (COCKPIT) · airframe 24,294 hrs · 16,088 cycles

MOMENTARY SPEED FLAGS IN VIEW PRIOR TO TAKEOFF ON CAPT AND F/O ADI. ON TAKEOFF ROLL, AFTER INITIAL INCREASE OF AIRSPEED ON F/O AIRSPEED INDICATOR, GOT A FLAG IN THE AIRSPEED WINDOW. AFTER REJECT, FLAG WENT AWAY. REMOVED AND REPLACED F/O'S ELECTRIC AIRSPEED INDICATOR REF B727 MM 34-12-000-5. PERFORMED PITOT LEAK TEST REF B727 MM 34-12-000-5. ALL TESTS NORMAL. PREMATURE REMOVAL/INSTALLATION.

Part: BEAM — DAMAGED (BS 500) · airframe 23,466 hrs · 15,473 cycles

COMPLY WITH EA 7-5230-92344, DOORS, MAIN CARGO DOOR LOWER BEAM REPAIR AT BS 500.0. COMPLIED WITH EA 7-5230-92344 DOORS, MAIN CARGO DOOR LOWER BEAM REPAIR AT BS 500.

Part: CHANNEL — CORRODED (BS 1130-1148) · corrosion level 2 · airframe 23,466 hrs · 15,473 cycles

MCD FLOOR SUPPORT SEVERAL NUT PLATES CORRODED BETWEEN STA 1130 TO STA 1148, RBL 27 TO RBL 62. REMOVED CORRODED FLOOR SUPPORT IAW SRM 51-30-2-1, FOUND OUT OF LIMITS IAW SRM 52-10-1 FIG 1. RECEIVED NEW FLOOR SUPPORT ON TRAV NR T5/547544, MAT ID 60357/7075-T6511, BATCH NR 98R000924004. INSTALLED NEW FLOOR SUPPORT IAW SRM 51-30-2. INSTALLED NEW NUT PLATES IAW SRM 51-30-2. (MINOR REPAIR)

Part: FLOOR SUPPORT — CORRODED (BS 852) · corrosion level 2 · airframe 23,466 hrs · 15,473 cycles

MAIN DECK FLOOR SUPPORT AT STA 852 BETWEEN LBL 45.50 AND 62, CORROSION UNDER CLIP NUT HOLES AND MOUNT BOLT AT LBL 45.5. REMOVED CORROSION IAW SRM 51-10-6, FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1. REMOVED CHANNEL IAW 51-30-2. FABED NEW UPPER CAP USING MAT.2024T3 .016 BATCH 122431 IAW 51-20-1. FABED NEW CHANNEL ON TRAVELER TD/000219, INSTALLED CHANNEL IAW SRM 51-30-2. UPPER CAP INSTALLED IAW SRM 51-30-2.

Part: FLAP TRACK — CORRODED (TE FLAPS) · airframe 23,466 hrs · 15,473 cycles

NR 2 FLAP TRACK FWD MOUNT FITTING CORRODED AROUND BUSHINGS. REMOVED AND REPLACED NR 2 FLAP TRACK ASSY IAW MM 27-51-031-4.

Part: FLAP TRACK — CORRODED (NR 7 FLAP) · airframe 23,466 hrs · 15,473 cycles

RT WING O/B FLAP I/B TRACK NR 7 HAS SURFACE CORROSION AND SMALL CHAFINGS ON FACES AND ROLLERS SLIDING TRACKS. REMOVED AND REPLACED FLAP TRACK IAW MM 27-51-032-4.

Part: SKIN — CRACKED (BS 190) · airframe 23,466 hrs · 15,473 cycles

FUSELAGE SKIN IS DAMAGED, POSSIBLY CRACKED AT FS 190, AT APPROX 7 O'CLOCK POSITION, (NO STRINGERS IN THIS AREA.) MAJOR REPAIR PERFORMED HFEC IAW PTGNTM 51-00-00 CRACKED INDICATED AS MARKED. REMOVED DAMAGE IAW SRM 53-30-1FIG 1. FABRICATED REPAIR DOUBLER FROM 2024T3 .050 BATCH NR 950751 IAW SRM 53-30--1 FIG1 AND FILLER FROM 2024T3 .040 BATCH NR 957207 IAW SRM 53-30-1 FIG 1. INSTALLED REPAIR AND FILLER IAW SRM 53-30-1 FIG1. THIS IS ACATAGORY ""A"" REPAIR. PREP AND PAINTED IAW MM 51-20-151-7.

Part: FLAP TRACK — CORRODED (NR 6 FLAP) · airframe 23,466 hrs · 15,473 cycles

RT WING INBD FLAP OUTBD TRACK NR 6 HAS CORROSION, PITTING, AND CHAFING ON FACES AND ROLLERS SLIDING TRACKS. REPLACED NR 6 FLAP TRACK ASSY IAW MM 27-51-031-4.

Part: FLAP TRACK — CORRODED (RT WING) · airframe 23,466 hrs · 15,473 cycles

RT WING OUTBD FLAP, OUTBD TRACK HAS SURFACE CORROSION AND CHAFING ON FACES AND ROLLERS SLIDING TRACKS. REMOVED AND REPLACED NR 8 FLAP TRACK IAW MM 27-51-031-4.

Part: CASE — CRACKED (COMPRESSOR) · airframe 23,466 hrs · 15,473 cycles

NR 2 ENG RT FWD FAN FRAME CASE HAS SEVERAL CRACKS. DYE PENETRANT INSPECTION DONE IAW SOPM 20-20-02 FOUND 1EA CRACK AT 3 O'CLOCK POSITION. CRACK STILL WITHIN LIMITS IAW PW JT8D MM72-00-00. STOP DRILLED CRACK IAW PW JT8D MM 72-00-00. REINSPECT CASE EVERY 200 HRS PER MM 72-00-00 PG 662 B (1) (B).

Part: GUSSET — CRACKED (FWD CARGO DOOR) · airframe 23,466 hrs · 15,473 cycles

FWD CARGO DOOR AFT LOWER GUSSET IS CRACKED. REMOVED AND REPLACED GUSSET IAW SRM 51-30-2.

Part: GUSSET — CRACKED (FWD CARGO DOOR) · airframe 23,466 hrs · 15,473 cycles

FWD CARGO DOOR GUSSET IS CRACKED AFT SIDE 3RD BRKT FROM TOP OF DOOR. REMOVED AND REPLACED GUSSET IAW SRM 51-30-2.

Part: CONTROL VALVE — LACK OF LUBE (TE FLAP CONTROL) · airframe 23,268 hrs · 15,353 cycles

L/E DEVICES WOULD NOT RETRACT AT FLAPS 2 DEGREES. PERFORMED ADJUSTMENT AND TEST OF FLAP 2 DEG SWITCH AS PER M/M 27-82-021-2, OPS CK GOOD. INSPECTED PULLEYS ROD END GOING TO FLAP CONTROL VALVE AND LUBED AS NEEDED. FLAPS AND LEADING EDGE DEVICES GROUND CKS NORMAL. A/C OK TO CONTINUE.

Part: FLAP TRACK — BROKEN (TE FLAPS) · airframe 22,036 hrs · 14,451 cycles

OUTBOARD FLAPS STAYED AT 2 DEG WHEN FLAP HANDLE PUT TO 5 DEG. RAN QRH. LANDED UNEVENTFULLY. DECLARED AN EMERGENCY. IN WORK. RAN FLAPS TO 25 DEG. UPON VISUAL INSPECTION FOUND RIGHT OUTBD FOREFLAP BROKEN OFF OF FLAP TRACKS. EVALUATING DAMAGE AND PARTS AT THIS TIME. REMOVED AND REPLACED RIGHT O/B MIDFLAP AND I/B MIDFLAP TRACK, REMOVED AND REPLACED FOREFLAP.

Part: BEAM — DAMAGED (FUSELAGE) · airframe 20,544 hrs · 13,224 cycles

TWO HOLES WITH PILOT HOLES ADJACENT TO THEM AND 1 ELONGATED HOLE IN STUB BEAM WEB AT BS 783, WL 204-207, LBL 65. REMOVED AND REPLACED STUB BEAM PER EA 7-5310-65851.

Part: SKIN — CHAFED (FUSELAGE) · airframe 20,544 hrs · 13,224 cycles

SKIN IS CHAFED AT BS 475, 2 INCHES ABOVE STR 21R. REMOVED AND REPLACED SKIN PER SRM 53-30-3.

Part: FIRE LOOP — FAULTY (NR3 ENGINE)

PASS 12,000 FT GOT AN INTERMITTENT FIRE LIGHT ON THE NR 3 ENGINE. RECEIVED FIRE BELL MOMENTARILY. REPLACED LWR FIRE DETECTOR ELEMENT REF MM 26-11-012-4. OPS CK OK.

Part: CONTROL UNIT — MALFUNCTIONED (COCKPIT)

IN CLIMB GOT AN INTERMITTENT FIRE WARN LIGHT, A FIRE BELL, AND MASTER FIRE WARN LIGHT. REMOVED AND REPLACED FIRE DETECTION CONTROL UNIT AND RAN ALL 3 ENGINES PER IAW JRH CHPT 5. OPS CK GOOD. FIRE WARN TEST OK. REF EA 7-2610-56907.

Part: CONTROL UNIT — MALFUNCTIONED (COCKPIT)

DURING CLIMB, FIRE WARN MASTER LIGHT ON GLARESHIELD CAME ON. AIR TURNBACK. CK WIRE FROM FIRE DET CNTRL UNIT M819 PIN 14 OF D1478 FOR A GROUND. WIRE CK GOOD WITH FLUKE. SUSP FIRE DET CNTRL UNIT TO BE THE PROBLEM. REMOVED AND REPLACED ENG FIRE DETECTION UNIT PER EA 1-2610-56855 OPS CK GOOD. FOUND LEAK ON INLET SIDE OF FUEL HEAT AIR VALVE. REPLACED GASKETS PER B727 MM 73-14-011. OPS CK GOOD.

Part: WARNING LIGHT — FALSE ACTIVATION (COCKPIT)

NR 2 ENG FIRE WARN LIGHT/BELL. INSP ENG FIRE WARN ELEMENTS, FUEL HEATER, PLUMBING, AND BLD AIR DUCTS. NO DEFECTS NOTED. RAN NR 2 ENG PER JET RUN HDBK. COULD NOT DUPLICATE DISCREPANCY.

Part: TRANSCEIVER — INOPERATIVE (E/E BAY)

VHF RADIO PRODUCE CARRIER TONE THAT MADE IT IMPOSSIBLE TO COMMUNICATE WITH ATC ON MOST FREQ. REMOVED AND REPLACED NR 2 R/T INTO NR 2 SLOT. NR 2 IS NOW S/N 8304, NR 1 IS NOW B2157. PER IAW 727 MM 20-10-017 & 23-21-01.

Part: WARNING SYSTEM — ACTIVATED (NR 3 ENGINE)

00-14 - NR 3 ENGINE FIRE WARN LIGHT AND BELL CAME ON FOR AN INSTANT. PERF ADJ AND TEST PER MM 26-11-000-5, OPS CK NORM. RAN ENG TO T/O PWR 1.75 EPR FOR 15 MIN NO IND NOTED. OPS CK NORM. OK FOR SERVICE..

Part: FIRE LOOP — OUT OF POSITION (NR 3 ENGINE)

INTERMITTENT FIRE WARN LIGHT AND BELL ON NR 3 ENG. REPOSITIONED FIRE LOOP INSIDE NR 3 ENGINE COWLING. CLOSED ENGINE COWLING AND COMPLETED FIRE TEST, OPER NORM AS PER 727-200 MM SECTION 26.

Part: SKIN — DENTED (BS 1398)

NR 248 - DENT IN EXTERNAL SKIN AT BS 1398 2 ABOVE RAIN GUTTER ON LT SIDE. REPAIRED SKIN PER FEDEX EA 7-5430-47837.

Part: SKIN — DENTED (BS 1427)

DENT IN EXTERNAL SKIN AT BS 1427 6 O/B OF VERTICAL STABILIZER ON LT SIDE. *S/D* REPAIRED DENT, ALL WORK DONE IAW FEDEX EA NR 7-5430-47837.

Part: SKIN — DENTED (BS 1364)

NR 247 - DENT IN EXTERNAL SKIN AT BS 1364 3 ABOVE RAIN GUTTER ABOVE NR 2 ENGINE ON LT SIDE. REPAIRED SKIN PER FEDEX EA 7-5430-47837.

Part: WEB — CORRODED (BS 640)

NR 352 - WHILE CLOSING FLOOR BDS FOUND CORROSION ON WEB BS 640, WL 208, LBL 47.5 TO 50. REPAIRED WEB PER FEDEX SRM 51-40-2, FIG 1.

Part: CREASE BEAM — CRACKED (BS 740)

NR 315 - CRACK FROM FASTENER HOLE AT S-17L BS 740 (ON AFT SIDE OF FRAME). REPAIRED CRACK PER FEDEX EA NR 7-5310-47834.

Part: FRAME — CORRODED (BS 720)

CORROSION (C53-224-01,1) ON FRAME BS 720A, STR 2-3 RT. *S/D* REPAIRED FRAME IAW FEDEX SRM 53-10-4 FIG 1.

Part: FLOORBEAM — CORRODED (FUSELAGE)

NR 346 CORROSION (C53-224-01(1)) AROUND NUT CLIP HOLES BS 344 FLOORBEAM UPPER CHORD AT LBL 13 AND RBL 10-12, WL 208. ** S/D ** REPAIRED PER IAW FEDEX SRM 53-10-8, 51-30-2, 51-10-2.

Part: FRAME — CORRODED (BS 720)

CORROSION ON FRAME BS 720E, STR 2 LT TO STR 4 RT OUT OF LIMITS. *S/D* REMOVED CORRODED SECTION, FAB AND INSTALLED REPAIR PARTS IAW FEDEX SRM 53-10-4 FIG 1.

Part: FRAME — CORRODED (BS 720)

CORROSION ON FRAME AT BS 720D BETWEEN STR 4L AND STR 4R OUT OF LIMITS. *S/D* REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR PARTS IAW FEDEX SRM 53-10-4 FIG 1 STR 5L TO STR 3R.

Part: SKIN — CHAFED (BS 720)

CHAFING ON EXTERIOR SKIN BS 720D+14 S19R. *S/D* REPAIRED EXT SKIN IAW FEDEX SRM 53-30-3.

Part: FRAME — CORRODED (BS 720)

CORROSION (C53-244-01, 1) ON FRAME BS 720C, STR 4 LT - STR 5 RT. *S/D* REPAIRED FRAME IAW FEDEX SRM 53-10-4 FIG 1.

Part: SKIN — CHAFED (FUSELAGE)

NR 593 CHAFFING ON EXTERIOR SKIN BS 720D + 14 S19L. ** S/D ** REPAIRED SKIN PER IAW FEDEX SRM 53-30-3.

Part: FIRE BELL — SOUNDED (CARGO COMPT)

AT FLT LEVEL 270, ENG FIRE WARNING BELL SOUNDED AND EXT 2 TIMES. FIRE WARNING MAIN CARGO SMOKE AND GROUND FAULT DET SYS CHECKED GOOD. CONNECTORS CHECKED AND CLEANED ON FIRE AND OVHT DET MODULE. ENG FIRE WARNING TEST PER MM 26-11-001-5. SYS CHECKED SERVICEABLE.

Part: TORSION LINKS — SCRATCHED (NLG)

A SEVERE VIBRATION OCCURRED WHEN LEFT RUDDER WAS APPLIED TO TURN LEFT OFF THE RUNWAY. A/C WAS STOPPED IMMED AND EMERGENCY EQUIP WAS CALLED OUT. REMOVED AND REPLACED BOTH UPPER AND LOWER NOSE GEAR TORSION LINKS AS PER MM 32-21-21. INSTALLED NG ELECTRICAL HARNESS, NOSE WHEEL STEERING CTRL ROD PER MM 32-21-51 PG 401, MM 32-20-01.

Part: PACK — ODOR (RIGHT)

AFTER TURNING ON R/PACK, HAD AN ACRID, SMOKEY SMELL TO COCKPIT. PACK TEMP APPROX 50C DUCT TEMP BELOW 20C. DUCT PRESS APPROX 32 PSI. TURNED PACK OFF FOR REMAINDER OF FLT. SMELL SUBSIDED. RAN ENG PER CHAPTER 5 OF 727 JET RUN HANDBOOK. PERF'D OPS CK OF R/PACK PER 727 MM CHAP 21 W/O NOTICEABLE ODOR OR SMOKEY SMELL OBSERVED. WILL REQ NO ACTION. OK TO CONTINUE.

Part: RETRACT MECH — MALFUNCTIONED (NLG DOORS)

NOSE GEAR DOOR WARNING LIGHT ON SECOND OFFICER'S PANEL AND RED DOOR WARNING LIGHT ON FRONT PANEL REMAINED ON AFTER GEAR RETRACTION. THE ABNORMAL PROCEDURE WAS ATTEMPTED. DURING RECYCLE, DOORS OPERATED NORMAL BUT LIGHT REMAINED ON DURING RETRACTION. ALSO, LOUD RUMBLING NOISE LIKE DOORS WERE OPEN WAS EVIDENT THROUGHOUT FLIGHT. REPEAT WRITE-UP, DEFERRED LIGHT PER MEL 32-1 EXP 2-25-95 CAT C CONT NR 0215039, NOSE GEAR DOOR WARNING SYSTEM INOP. NOSE STRUT WAS FOUND FLAT AGAIN AFTER RESERVICING STRUT. RECHECKED NOSE GEAR DOORS PER MM 32-21, NO DEFECTS NOTED. SWUNG GEAR SEVERAL TIMES WITH NO DEFECTS.

Part: RIB — CRACKED (BS 760)

WHILE WORKING INSP CARD 7-5710-7-2308H PT 1 NOTED CRACK INDICATIONS IN THE FWD UPPER AND LOWER HOLES OF THE 70.5 CHORD BS 760 RT. CRACK INDICATIONS IN THE FWD UPPER ARE IN THE 1 AND 6 O'CLOCK POSITION, LWR FWD HOLE IN 2 O'CLOCK POSITION. TRIMMED OUT CRACKED FWD UPPER AND LOWER HOLES IN THE RIB CHORD ONLY 760 RBL 70.5 WL 206 IAW EWO 95-3292. ACCOMPLISHED ALL WORK DONE ON 70.5 IAW FEDEX PREVENTIVE MOD EA 7-5710-26723.

Part: CHORD — CRACKED (BS 760)

NOTED CRACK INDICATIONS LT 70.5 BS 760 WHILE PERFORMING INSPECTION CARD NR 7-5710-7-2308H PT1, CRACK LOCATIONS ARE THE FWD UPPER HOLE AT 11 AND 5 O'CLOCK POSITION L/B LOOKING I/B. CRACK INDICATION ARE IN THE T-CHORD, PLUS CHORD. ACCOMPLISHED CRACK CONTAINMENT BY REAMING HOLES UP TO .278 AND ACCOMPLIHSED INSTALLATION OF SMALL REPAIR PER SB 727-57-0112 AT BS 760 LBL 70.5 WL 204.

Part: FRAME — CRACKED (BS 660)

CRACK IN LOWER LOBE FRAME BS 660, RBL 2, WL 154. CUT OUT DAMAGED AREA AT BS 660, BL ZERO - RBL 5, WL 154. FABRICATED REPAIR PARTS OUT OF 7075T6.050 MATERIAL, AND INSTALLED WET WITH SEAL AS PER FEDEX SRM 53-10-2 AND 51-40-3.