N494FE

Part: COWLING — DAMAGED (NR 3 NACELLE) · airframe 42,381 hrs · 28,172 cycles

DAMAGE BOTTOM NR 3 NOSE COWL. REMOVED AND REPLACED NR 3 ENGINE NOSE COWL IAW MM 71-10-021-4. OPS AND LEAK CHECKS GOOD IAW MM 71-00-000-1.

Part: SUPPORT FITTING — CRACKED (BS 620) · airframe 42,381 hrs · 28,172 cycles

CRACKED FITTING (SUPPORT) BS 620, MAIN CARGO DOOR CUT OUT. REMOVED CRACKED FITTING AT BS 620 MAIN CARGO DOOR CUTOUT & INSTALLED NEW FITTING IAW SRM 51-30-2 & SRM 51-30-5.

Part: SKIN — DAMAGED (LT WING TE FLAP) · airframe 42,381 hrs · 28,172 cycles

LEFT IB FLAP AFT IS DAMAGED OB TE. REMOVED LT IB AFT FLAP IAW MM 27-51-002-4, AND REMOVED DAMAGE 10" X 3" IAW SRM 51-40-20, AND FABRICATED REPAIR CORE IAW SRM 51-40-20. BONDED CORE IAW SRM 51-40-20 AND FABRICATED DOUBLER 12" X 5" IAW SRM 51-40-20, BONDED DOUBLER IAW SRM 51-40-20, AND CLEANED SEALED AND PRIMED IAW SRM 51-40- 20. REINSTALLED LT IB AFT FLAP AND ACCOMPLISHED ADJ/OPS CHECK IAW MM 27-51-005-4.

Part: SKIN — GOUGED (BS 1203 S20-22R) · airframe 42,381 hrs · 28,172 cycles

GOUGE ON EXISTING DOUBLER EXTERIOR FUSELAGE BS 1203 BETWEEN STR 20R - 22R. REMOVED EXISTING DOUBLER REPAIR IAW SRM 51-30-2 AND FABRICATED NEW DOUBLER REPAIR FROM 2024T3 .050 DIM: 11 3/4" X 7 3/4" IAW SRM 53-30-3 FIG 26. INSTALLED DOUBLER REPAIR IAW SRM 51-30-2.

Part: SILL — MISINSTALLED (ZONE 200) · airframe 42,381 hrs · 28,172 cycles

NO EDGE DISTANCE BETWEEN PILOT HOLES AND FASTENER HOLES ON CTR SILL. REMOVED MCD CENTER UPPER SILL IAW SRM, REV 103, 51-30-2. LOCATED AND DRILLED NEW SILL IAW SRM 51-30-5. INSTALLED NEW SILL IAW SRM 51-30-2.

Part: SILL — DAMAGED (BS 620) · airframe 42,381 hrs · 28,172 cycles

NUMEROUS DRILLED HOLES IN FRAME BS 620 RADIUS WHERE NUT-PLATES ARE INSTALLED STR 5L TO 9L ( 7 EA.) REMOVED BS 620 FRAME SECTION FROM STRINGER 2L TO 14L IAW SRM, REV 103, 51-30-2. LOCATED DRILLED AND DEBURRED NEW FRAME SECTION IAW EA NR 7-5330-135584. INSTALLED BS 620 FRAME SECTION FROM STRINGER 2L TO 14L IAW EA NR 7- 5330-135584.

Part: SKIN — DAMAGED (ZONE 100) · airframe 42,381 hrs · 28,172 cycles

NO EDGE DISTANCE AT FASTENER HOLES (3 EA) MCD CUTOUT SKIN BS 582 - BS 559 STR 3L. REPAIRED NO EDGE DISTANCE CONDITION IAW EA 7-5330-135589.

Part: SKIN — DAMAGED (ZONE 100) · airframe 42,381 hrs · 28,172 cycles

DOUBLE DRILLED HOLES MCD CUT-OUT SKIN BS 610 - BS 602, STR 3L. CUTOUT DAMAGED SKIN AREAS, FABRICATED REPAIR DOUBLERS & FILLERS & INSTALLED REPAIR PARTS AT MCD CUTOUT INNER SKIN IAW EA 7-5330-135586.

Part: FRAME — DAMAGED (ZONE 100) · airframe 42,381 hrs · 28,172 cycles

NUMEROUS DRILLED HOLES IN FRAME BS 480 RADIUS WHERE NUT-PLATES ARE INSTALLED STR 6L- 9L. ( 7 EA ) REMOVED DAMAGED FRAME, LOCATED & DRILLED NEW FRAME & INSTALLED NEW FRAME IAW SRM 51-30-2 & EA 7-5310-135585.

Part: SKIN — GOUGED (CARGO DOOR) · airframe 42,381 hrs · 28,172 cycles

MAIN CARGO DOOR AFT FRAME INNER SKIN IS GOUGED IN NUMEROUS PLACES, BS 620. REMOVED MAIN CARGO DOOR AFT INNER SKIN, FABRICATED NEW SKIN & INSTALLED NEW SKIN IAW SRM 51-10-2, SRM 51-30-2 & HAYES INTERNATIONAL DWG NO. 53FX1551.

Part: FRAME — CORRODED (BS 990 S26-27R) · corrosion level 2 · airframe 42,381 hrs · 28,172 cycles

AFT PIT, FRAME 990, AFT SIDE SURFACE HAS CORROSION BETWEEN 26R AND 27R. CUT OUT DAMAGE ON BS 990 FRAME BETWEEN STRINGER 26R AND 27R IAW SRM, REV 103, 51-40-4 FIG 2. FABRICATED FILLER, & DOUBLERS IAW SRM 51-40-4 FIG 2. INSTALLED DOUBLERS AND FILLER IAW SRM 51-40-4 FIG 2.

Part: RIB — CRACKED (NR 3 SLAT) · airframe 42,381 hrs · 28,172 cycles

NUMBER 3 SLAT RIBS CRACKED - I/B AND O/B SIDE AT ACTUATOR ROD END ATTACH POINT. REMOVED NR 3 SLAT ACTUATOR I/B AND O/B RIBS IAW SRM 51-30-2. FABRICATED 1 RIB IAW SRM 51-20-1 FIG 7 USING 2024-0, .040" X 8" X 16". INSTALLED INBD AND OUTBD RIB IAW SRM 51-30-2, REV 103.

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 42,381 hrs · 28,172 cycles

SURFACE CORROSION ON FORWARD AND AFT SIDES OF STUB FRAME WEB, STATION 950E PLUS 4", STRINGER 29 - 28R REMOVED STUB FRAME AT STATION 950E PLUS 4", STRINGER 29 - 28R IAW SRM, REV 103, 51-30-2. FABRICATED NEW FRAME USING 7075-0, .040" X 21 3/4" X 7" IAW SRM 51-20-1 FIG 7. INSTALLED FRAME IAW SRM 51-30-2.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 42,381 hrs · 28,172 cycles

TWO POPPED RIVETS EXTERIOR FUSELAGE BS 1015 STRINGER 28R. REMOVED SECTION OF STRINGER 25 3/4" IN LENGTH AT BS 1015, STRINGER 28R IAW SRM, REV 103, 53-10-3, FIG 1 DETAIL 1. FABRICATED 2 STRINGER SECTIONS USING BAC1498-147, 7075-T6, 11" AND 14 3/4" LONG AND 2 SPLICES USING BAC1498-131, 7075-T6, 12" LONG EACH IAW SRM 53-10-3 FIG 1 DETAIL 1. INSTALLED STRINGER AND SPLICE SECTIONS IAW SRM 53-10-3, FIG 1, DETAIL 1.

Part: FITTING — CRACKED (BS 460 S3-4L) · airframe 42,381 hrs · 28,172 cycles

MCD UPPER SILL FITTING BS 460 FWD SIDE BETWEEN STR 3L AND 4L CRACKED. REMOVED AND REPLACED MCD UPPER SILL FITTING IAW SRM REV 103, 51-30-5 AND 51-30-2.

Part: FRAME — GOUGED (BS 480) · airframe 42,381 hrs · 28,172 cycles

MAIN CARGO DOOR FWD FRAME INNER SKIN IS GOUGED IN NUMEROUS PLACES BS 480. REMOVED DAMAGED FWD INNER SKIN , FABRICATED NEW INNER SKIN & INSTALLED NEW SKIN AT CUTOUT FWD IAW SRM 51-30-5, SRM 51-30-2, & DWG NR 53FX1551.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 42,381 hrs · 28,172 cycles

CORROSION MAIN CABIN FLOORBEAM TOP TEE CAP BS. 380 RBL 45 TO RBL 61 CUTOUT AREA DAMAGE, DIM: 2 1/2" X 1" IAW SRM 53-10-8. FABRICATED TWO REPAIR ANGLES FROM 7075TO HEAT TREATED TO T6 CONDITION IAW FAS ENGINEERING REPORT 2-37153-801 REV A DIM: 5 1/2" X 2 5/8" & 10 1/2" X 2 3/8". FABRICATED ONE FILLER IAW SRM 53-10-8 FIG 2 AND INSTALLED REPAIR PARTS & STIFFNER IAW SRM 51-30-2.

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 42,381 hrs · 28,172 cycles

SURFACE CORROSION BS 970 SHEAR TIE, STRINGER 29R - 27R. CUT OUT DAMAGED SHEAR TIES ON BS 970 FRAME BETWEEN STRINGER 29R AND 27R, 2" X 6 1/2" (QTY 2) IAW SRM 53-10-4 FIG 13. FABRICATED SHEAR TIE USING 7075-0, .071" X 4 1/2" X 7 1/2" AND DOUBLER USING 7075-T6, .071" X 7 1/2' X 3 3/8" AND RADIUS FILLER USING 7075-T6, .071" X 6 1/2" X 1" BETWEEN 28R AND 29R. FABRICATED SHEAR TIE USING 7075-0, .071" X 8 1/8" X 4 1/2" AND DOUBLER USING 7075-T6 .071" X 6 1/2" X 3 1/2" BETWEEN STRINGER 27R AND 28R IAW SRM 53-10-4 FIG 13. INSTALLED REPAIR DOUBLERS AND SHEAR TIES IAW SRM 53-10-4 FIG 13, REV 103.

Part: STRINGER — CORRODED (BS 950C-950F) · airframe 42,381 hrs · 28,172 cycles

CORROSION INSIDE CHANNEL OF STR 30, BS 950C TO 950F. REMOVED CORROSION IN CHANNEL OF STRINGER IAW SRM, REV 103, 51-10-6. COMPLIED WITH UT THICKNESS IAW NDTM PT 4, 51-00-00, FIG 2, AND MAPPED DAMAGE LOCATION IAW EA 7-5330-135588. ENGINEERING ANALYSIS FOUND NO REPAIR NECESSARY IAW EA 7-5330-135588. TREATED AND PRIMED AREA IAW SRM 51-10-2.

Part: SEAT TRACK — CORRODED (BS 950F-970) · corrosion level 2 · airframe 42,381 hrs · 28,172 cycles

CORROSION SEAT TRACK IB FLANGE, RBL 25 STA. 950F-970 REMOVED OUT OF LIMITS SEAT TRACK IAW SRM 51-30-2. FABRICATED NEW SEAT TRACK FROM BAC 1520-792-7178T6, DIM: 80" AND TWO ANGLES FROM BAC 1503-100122-7178T6, DIM: 13 1/8" X 2 1/2" 2 EA. IAW SRM 53-10-5 FIG 1. INSTALLED NEW SEAT TRACK & ANGLES IAW SRM 51-30-2.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 42,381 hrs · 28,172 cycles

CORROSION SEAT TRACK FLANGE MAIN CABIN BS 690 LBL 25 REMOVED SEAT TRACK FROM STA 690 TO 740 LBL 25, FABRICATED SEAT TRACK FROM BAC1520-792-7178-T6511 IAW SRM 53-10-5 FIG 1. INSTALLED SEAT TRACK IAW SRM 51-30-2.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 42,381 hrs · 28,172 cycles

CORROSION SEAT TRACK FLANGE MAIN CABIN BS 760.95 - 850 LBL 45. REMOVED DAMAGED SEAT TRACK FROM BS 740 TO BS 850 AND FABRICATED NEW SEAT TRACK SECTION FROM MATERIAL BAC 1520-14667178T6 DIM: 15 7/8" AND INSTALLED NEW PART IAW SRM 51-10-2, SRM 51-30-2 & DWG. NR 65-16279.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 42,381 hrs · 28,172 cycles

CABIN BS 760 -825 LBL 24 SEAT TRACK, IB FLANGE, HAS CORROSION. REMOVED DAMAGED SECTION OF SEAT TRACK AND BEAM SECTION. FABRICATED NEW BEAM SECTION USING BAC1506-1108 7075T-6 DIMS 96" AND SEAT TRACK SECTION USING BAC1520-841 DIMS 95 1/8" AND INSTALLED IAW DWG 65-16279, DWG 65-16278, SRM 51-30-5 AND SRM 51-30-2.

Part: SHEAR TIE — CORRODED (ZONE 200) · corrosion level 2 · airframe 42,381 hrs · 28,172 cycles

CORROSION ON SHEAR TIE AT BS 700 BETWEEN STRINGERS 28L AND 27L. REMOVED DAMAGED SHEAR TIE IAW SRM, REV 103, 53-10-4 FIG 13. FABRICATED SHEAR TIE USING 7075-T6, .050" X 6" X 7/8" AND DOUBLER USING 7075-T6, .050" X 7 5/8" X 3 5/8" IAW SRM 53-10-4 FIG 13. INSTALLED SHEAR TIE AND DOUBLER IAW SRM 53-10-4 FIG 13.

Part: HINGE — LOOSE (CARGO DOOR) · airframe 42,381 hrs · 28,172 cycles

MCD FWD HINGE SECTION HAS EXCESSIVE MOVEMENT AT HINGE AND PIN AREA. REMOVED UPPER HINGE SECTION, LOCATED & DRILLED NEW HINGE ASSY & INSTALLED NEW UPPER HINGE ASSY IAW SRM 51-30-2, SRM 51-30-8, SRM 51-10-2 & DWG NR 52FX1433.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 42,381 hrs · 28,172 cycles

CORROSION FLOORBEAM, TOP MAIN CABIN FRONT OF 9G BARRIER. CUTOUT DAMAGED AREA, FABRICATED REPAIR ANGLES & FILLER & INSTALLED FLOORBEAM. REPAIR AT BS 344 IAW SRM 53-10-8, FIG 9, SRM 51-10-2, SRM 51-30-2.

Part: HINGE — LOOSE (CARGO DOOR) · airframe 42,381 hrs · 28,172 cycles

AFT HINGE SECTION HAS EXCESSIVE MOVEMENT AT HINGE AND PIN AREA. REMOVED MCD LOWER HINGE ASSY, LOCATED & DRILLED NEW HINGE ASSY & INSTALLED NEW LOWER HINGE ASSY IAW SRM 51-30-2, SRM 51-10-2, & DWG B27-53-070 B & DWG NR 52-487 & 52FX1433.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 42,381 hrs · 28,172 cycles

CORROSION FLANGE SEAT TRACK MAIN CABIN BS 480 - BS 690, LBL 25. REMOVED DAMAGE SEAT TRACK SECTION, FABRICATED NEW SEAT TRACK SECTION AT LBL 25 BS 480-610, INSTALLED NEW SEAT TRACK SECTION IAW SRM 53-10-5 FIG 1 & SRM 51-30-2 & P-F SRM 53-10-2.

Part: SEAT TRACK — CORRODED (BS 480-610) · corrosion level 2 · airframe 42,381 hrs · 28,172 cycles

CORROSION SEAT TRACK MAIN CABIN BS 480 - BS 610, BL 0. REMOVED SEAT TRACK SECTION IAW SRM, REV 103, 51-30-2. FABRICATED REPLACEMENT SEAT TRACK SECTION USING BAC1520-792, 7178-T6511, 130" IN LENGTH IAW SRM 53-10-5 FIG 1 AND IAW P-F SRM 53-10-2 FIG 7A. INSTALLED SEAT TRACK IAW SRM 51-30-2.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 42,381 hrs · 28,172 cycles

CORROSION ON SEAT TRACK RBL 25, STA 1130 - 1183. REMOVED CORRODED SEAT TRACK SECTION IAW SRM 51-30-2. FABRICATED NEW SEAT TRACK SECTION IAW DWG NR 53FX976 AND INSTALLED NEW SEAT TRACK SECTION IAW SRM 51-30-2.

Part: BULKHEAD — CRACKED (BS 1183) · airframe 42,381 hrs · 28,172 cycles

CRACK COMING FROM RIVET HEAD BS 1183, BULKHEAD LBL 58 BETWEEN STR 18R TO 19R LEVEL. CUTOUT CRACKED AREA, FABRICATED REPAIR DOUBLER & FILLER & INSTALLED REPAIR PARTS AT BS 1183 LBL 58 IAW SRM 51-30-2, SRM 51-10-2 & EA 7-5310-135579.

Part: SEAT TRACK — CORRODED (BS 950) · corrosion level 2 · airframe 42,381 hrs · 28,172 cycles

CORROSION ON SEAT TRACK AT STA 950, 10", PRODUCTION SPLICE, RBL 45. REMOVED CORRODED SEAT TRACK IAW SRM 51-30-2 AND FABRICATED NEW SEAT TRACK FROM PN BAC1520-7927178T6511, DIM: 91" IAW SRM 53-10-5 FIG 1 REV 103. INSTALLED NEW SEAT TRACK IAW SRM 51-30-2. REMOVED CORRODED SPLICE AND FABRICATED NEW SPLICE FROM PN BAC 1503-1001227178-T6511 DIM: 14" AND INSTALLED ALL IAW SRM 53-10-5 FIG 1, SRM 51-30-2.

Part: SKIN — CRACKED (ZONE 200) · airframe 42,381 hrs · 28,172 cycles

MCD CUTOUT UPPER SILL BS 605 & 615 HAS UPPER FLANGE WITH CRACK INDICATION AT (2 EA) RIVET HOLES. REMOVED DAMAGED MCD UPPER SILL, LOCATED & DRILLED NEW AFT SILL & INSTALLED NEW SILL UPPER SILL BEAM IAW EA 7-5310-135582.

Part: SKIN — CRACKED (ZONE 200) · airframe 42,381 hrs · 28,172 cycles

MCD CUTOUT UPPER SILL BS 485, 487, & 495 SILL UPPER FLANGE HAS CRACK INDICATION AT 3 EA RIVET HOLES. REMOVED DAMAGED MCD UPPER SILL, LOCATED & DRILLED NEW SILL & INSTALLED NEW SILL BEAM IAW EA 7-5310-135582.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 42,280 hrs · 28,087 cycles

R1 WINDOW ARCED AND CRACKED AT FL350 DURING CRUISE. OUTER PANE CRACKED, NO PRESSURIZATION LOSS. R & R R1 WINDSHIELD IAW AMM 56-11-011-4. ALSO MOVED WINDOW WIRING LEAD TO TRANSFORMER TAP TERMINAL 26, IAW AMM 30-41-042-5. OK FOR SERVICE. (CLOSED)

Part: SWITCH — FAILED (MLG) · airframe 41,360 hrs · 27,345 cycles

"NOSE GEAR DOWN AND LOCKED LIGHT" AND NOSE GEAR UNSAFE LIGHT" ILLUMINATED WHEN LANDING GEAR HANDLE WAS MOVED TO OFF POSITION FOLLOWING GEAR RETRACTION. BOTH LIGHTS THEN REMAINED ILLUMINATED WHEN LANDING GEAR HANDLE WAS MOVED TO "UP" POSITION. JACKED ACFT IAW MM 07-11-000-2 AND RETRACTED NOSE GEAR AND FOUND S92 CONTROL LEVER POSITION SWITCH INTERMITTENT. REMOVED AND REPLACED SWITCH IAW MM 32-61-012-4. SWITCH OPS CHECKS GOOD PER SAME.

Part: FRAME — DAMAGED (ZONE 100) · airframe 41,141 hrs · 27,171 cycles

SCREW MARKS ON FRAME 1110 AT STR 27R AND 27L UNDER TIE DOWN POINTS.

Part: SKIN — DENTED (NR 1 SLAT) · airframe 41,141 hrs · 27,171 cycles

NR 1 SLAT UPPER SURFACE HAS ONE DENT AT WS 760.

Part: KEELBEAM — CRACKED (ZONE 100) · airframe 41,141 hrs · 27,171 cycles

RT WHEEL WELL INBD SIDE ON 870 BULKHEAD AND KEEL BEAM CHORD CRACKED. REMOVED AND REPLACED RT WHEEL WELL BS 870 BULKHEAD CHORD WITH NEW CHORD PO NR 819337 IAW B727 SRM 51-30-5 AND SRM 51-30-2.

Part: SKIN — CRACKED (RT WING TE FLAP) · airframe 41,141 hrs · 27,171 cycles

RT O/B FOREFLAP O/B L/E CRACKED. HFEC INSPECTED RT OB FOREFLAP IAW NDTM PT 6 51-00-00 FIG 23 ONE CRACK NOTED ENDS MARKED. STOP DRILLED CRACK DIMS .250 IAW SRM 51-10-1. HFEC INSPECTED STOP DRILL IAW NDTM PT 6 51-00-00 FIG 23 CRACK TERMINATES IN STOP DRILL HOLE. FABRICATED REPAIR USING 2024-T3 .063 PO NR 9006699 DIMS 5 INCH BY 5 INCH IAW SRM 57-50-2 FIG 4, 57-50-4 FIG 7, 51-30-5 AND 51-30-8. TREATED AND PRIMED IAW SRM 51-10-2. INSTALLED REPAIR IAW SRM 57-50-4 FIG 7.

Part: SKIN — CRACKED (LT WING TE FLAP) · airframe 41,141 hrs · 27,171 cycles

LT O/B FOREFLAP O/B L/E CRACKED. HFEC INSPECTED LT OB FOREFLAP IAW NDTM PT 6 51-00-00 FIG 23 ONE CRACK NOTED ENDS MARKED. STOP DRILLED CRACK IAW SRM 51-10-1 DIMS .250. HFEC INSPECTED STOP DRILL IAW NDTM 51-00-00-FIG 23 CRACK TERMINATES IN STOP DRILL HOLE. FABRICATED REPAIR USING 2024-T3 .063 PO NR 9006699 DIMS 3 1/2 INCH BY 4 INCH IAW SRM 57-50-2 FIG 4, 57-50-4 FIG 7, 51-30-5, 51-30- 8. TREATED AND PRIMED REPAIR IAW SRM 51-10-2. INSTALLED REPAIR IAW SRM 57-50-4 FIG 7.

Part: BULKHEAD — CRACKED (ZONE 100) · airframe 41,141 hrs · 27,171 cycles

CRACK IN RIGHT WHEEL WELL 870 BULKHEAD BOTTOM SIDE OF APU BLEED VALVE DUCT CUTOUT. FABRICATED REPAIR DOUBLER IAW SRM 53-10-9, & FILLER, INSTALLED REPAIR PARTS IAW SRM 53-10-9 FIG 5.

Part: SKIN — DENTED (ZONE 100) · airframe 41,141 hrs · 27,171 cycles

LT FWD FUSELAGE STA 190 STR 27L REPAIR DOUBLER HAS SKIN BULGES AND DENTS. CUTOUT DAMAGED AREA DIMS 1 1/4 INCH BY 1 1/2 INCH IAW SRM 53-10-3 FIG 5. FABRICATED DOUBLER REPAIR USING 2024-T3 .050 PO NR 9006288 DIMS 10 1/2 INCH BY 13 1/2 INCH AND FILLER USING 2024-T3 .040 PO NR 9007107 DIMS 1 1/4 INCH BY 1 1/2 INCH IAW SRM 53-30-2 FIG 1, 53-30-3 FIG 3. TREATED AND PRIMED IAW SRM 51-10-2. INSTALLED REPAIR PARTS IAW SRM 51-30-2.

Part: SKIN — DENTED (ZONE 100) · airframe 41,141 hrs · 27,171 cycles

DENT IN LEFT FWD FUSELAGE STA 545 ABOVE STR 24L (RVSM AREA). REPAIRED DENT IAW EA 7-5330-116991.

Part: ANGLE — CRACKED (RT WING) · airframe 41,141 hrs · 27,171 cycles

RT WING L/E STA 90 VERTICAL ANGLE CRACKED LWR SIDE. FABRICATED REPAIR ANGLE FILLER FROM 7075-T6 .050 PO NR 9007294 DIMS 7 INCH BY 2 1/2 INCH, FILLER 2 INCH BY 1 INCH. INSTALLED REPAIR PARTS AT RT WING LE STA 90 IAW SRM 51-40-3 FIG 1, SRM 57-20-2 FIG 1 AND SRM 51-30-2.

Part: BOLT — DAMAGED (FUEL CONTROL) · airframe 41,141 hrs · 27,171 cycles

NR 3 ENGINE STARTER CONTROL ROD INBD OF ENGINE, NUT HAS NO THREADS SHOWING AND SPRING CLIP NOT BENT OVER BOLT HEAD. PROPERLY INSTALLED NR 3 ENG START CONTROL ROD (UPPER) BOLT AND ATTACHING HARDWARE IAW FX MM 76-11-021-2.

Part: STRINGER — CORRODED (ZONE 100) · airframe 41,141 hrs · 27,171 cycles

SKIN BULGE JUST FWD OF STATION 1010 STR 27L. REMOVED FASTENERS FROM AFFECTED AREA IAW SRM 51-30-2, CUTOUT STRINGER SECTION (DIM 10 1/4" LONG) IAW B727 SRM 53-10-3 FIG 1, REMOVED EXISTING SPLICE IAW SRM 51-30-2, FABRICATED REPAIR PARTS IAW SRM 51-10-2, CLEANED SKIN AND NO CORROSION NOTED, INSTALLED REPAIR PARTS IAW SRM 51-30-2 AND 53-10-3 FIG1.

Part: CONTROL CABLE — TWISTED (ZONE 500) · airframe 41,141 hrs · 27,171 cycles

OUTBOARD FLAP TRANSMITTER CABLE TWISTED AROUND (2 EACH) LT WING SPOILER CABLES. RE-ROUTED LT O/B FLAP TRANSMITTER CABLE WHICH WAS WRAPPED AROUND 2 EACH SPOILER CABLES IAW MM 27-52-013-4. NO DEFECTS NOTED TO SPOILER OR FLAP TRANSMITTER CABLE. OPS CHECK GOOD IAW MM 27-51-000-5 AND 27-61-000-5.

Part: NUT — MISSING (THROTTLE) · airframe 41,141 hrs · 27,171 cycles

MISSING NUT ON BOLT SECURING NR 3 ENGINE THROTTLE CONTROL ROD INBD OF ENGINE. REMOVED AND REPLACED NUT, BOLT AND LOCK IAW FX B727 76-12-000-5.

Part: BRACKET — CHAFED (BS 305 S3-4R) · airframe 41,141 hrs · 27,171 cycles

STATION 305 BETWEEN STR'S 3R AND 4R WHERE COCKPIT BULKHEAD ATTACHES TO INTERCOSTAL, BRACKET CHAFFING THROUGH INTERCOSTAL. REMOVED INTERCOASTAL WEB IAW SRM 51-30-2. FABRICATED WEB IAW B727 SRM 51-10-3, 51-30-5, AND 53-10-2. TREATED AND PRIMED IAW SRM 51-10-2. INSTALLED NEW INTERCOASTAL IAW SRM 51-30-2.

Part: STRINGER — DAMAGED (ZONE 200) · airframe 41,141 hrs · 27,171 cycles

STATION 344 STR 11R STRINGER TIE MIS-DRILLED AND HAS A FASTENER WITH ZERO EDGE DISTANCE. INSTALLED FRAME REPAIR, FILLER AND STRINGER CLIP IAW SRM 51-30-2, 53-10-4 FIG 1, 53-10-2 FIG 3 AND 51-20-1.

Part: KEELBEAM — CRACKED (ZONE 100) · airframe 41,141 hrs · 27,171 cycles

LEFT MAIN LANDING GEAR WHEEL WELL KEEL BEAM CHORD CRACKED AT STA 872.

Part: WEB — CRACKED (LT WING) · airframe 41,141 hrs · 27,171 cycles

CRACK ON LEFT WING TRAILING EDGE WEB JUST OUTBOARD OF NR 7 SPOILER FITTING. CUT-OUT DAMAGED AREA, FABRICATED NEW DOUBLER, FABRICATED WEB, & INSTALLED REPAIR PARTS IAW SRM 51-30-2, AND DRAWING SR27-57-038.

Part: SKIN — DENTED (ZONE 200) · airframe 41,141 hrs · 27,171 cycles

EXTERIOR FUSELAGE STA 300 JUST FWD OF L1 DOOR HAS A BULGE IN SKIN STR 9L. 9L REWORKED DENT TO ORIGINAL CONTOUR IAW SRM 51-40-1. HFEC INSPECTED DENT IAW NDTM 51-00-00 FIG 23 PART 6. NO DEFECTS NOTED. TREATED AND PRIMED AREA IAW SRM 51-10-2.

Part: KEELBEAM — CRACKED (ZONE 100) · airframe 41,141 hrs · 27,171 cycles

LT MAIN LANDING GEAR WHEEL WELL KEEL BEAM CHORD CRACKED AT STA 872. TRIMMED OUT DAMAGED AREA. FABRICATED REPAIR DOUBLER, INSTALLED DOUBLER IAW SB727-53-0208 AND EA 7-5310-116992.

Part: DOUBLER — FAILED (ZONE 200) · airframe 41,141 hrs · 27,171 cycles

FUSELAGE SKIN DOUBLER IN FRONT OF L1/R1 WINDSHIELDS TORN AWAY AT L/E, BODY STA 178 AT TOP OF NOSE RADOME. REMOVED AND REPLACED TORN SKIN DOUBLER AT BS 178 IN FRONT OF L1 AND R1 WINDOWS. NEW SKIN PART NUMBER 65-45800Y218 PO 819342 IAW SRM 51-30-5 AND SRM 51-30-5.

Part: SKIN — CHAFED (ZONE 100) · airframe 39,210 hrs · 25,640 cycles

RIGHT FUSELAGE IS CHAFED AT LANDING FACE FOR WING TO BODY FAIRING, FWD OF LANDING LIGHT. REMOVED DAMAGE, FABRICATED, ALODINED, PRIMED AND INSTALLED FUSELAGE SKIN REPAIR FROM STA 720D TO 720E BETWEEN STRINGERS 18R TO 20R ALL IAW FX B727-200 SRM 53-30-3 FIG 14, 51-30-2 AND 51-10-2.

Part: STRINGER — CORRODED (ZONE 100) · airframe 39,210 hrs · 25,640 cycles

STA 950A TO 950B STRINGER 29 LEFT HAS CORROSION. REMOVED DAMAGE, FABRICATED, ALODINED, PRIMED AND INSTALLED REPAIR AT STA 950A TO 950B ON STRINGER 29L ALL IAW FX SRZ SR27-53-023A FIG 7 AND B727 SRM 51-30-2, 51-10-2.

Part: FRAME — CORRODED (ZONE 100) · airframe 39,210 hrs · 25,640 cycles

FOUND FRAME AT STA 950E AND STRINGER 29L IS CORRODED. REMOVED DAMAGE, FABRICATED, ALODINED, PRIMED AND INSTALLED FRAME REPAIR AT STA 950E BETWEEN S28L AND S29L ALL IAW FX B727 SRM'S 53-10-4 FIG 12, 53-10-1, 53-10-2, 51-30-2, 51-10-6 AND 51-10-2, SNRM N00986.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 39,210 hrs · 25,640 cycles

FWD PIT BS 700 AT STRINGER 28L CORROSION ON STRINGER AND WEB. CORRECTIVE ACTION: REMOVED DAMAGE,LOCATED, DRILLED AND INSTALLED NEW STRINGER AT STA 700 TO 720 AND S28L ALL IAW FX B727 SRM'S 53-10-3 FIG1,51-30-2 AND 53-10-1.

Part: FRAME — CORRODED (ZONE 100) · airframe 39,210 hrs · 25,640 cycles

FRAME STA 950F STRINGER 29L, CORROSION. REMOVED DAMAGE, FABRICATED, ALODINED, PRIMED AND INSTALLED FRAME REPAIR STA 950F AT S29L ALL IA FX B727 SRM'S 53-10-4 FIG 12,53-10-1,53-10-2 AND 51-10-2 SNRM N00990.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 39,210 hrs · 25,640 cycles

FWD PIT MAIN CABIN FLOORBEAM LOWER SIDE HAS CORROSION AROUND NUT PLATES STA 720 BETWEEN LBL 50 AND RBL 50. REMOVED DAMAGE, FABRICATED, ALODINED, PRIMED AND INSTALLED FLOORBEAM REPAIR STA 720 FROM LBL 50 TO RBL 50 ALL IAW FX SRM DRAWING SR27-53-034.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 39,210 hrs · 25,640 cycles

AFT PIT FLOORBEAM LOWER CHORD SEVERAL AREAS CORRODED BS 1070 AT LBL 26. REMOVED DAMAGE, FABRICATED, HEAT TREATED, ALODINED, PRIMED AND INSTALLED FLOORBEAM REPAIR TO STA BS 1070 BETWEEN RBL 54 AND LBL 26 ALL IAW FX SRZ SR27-53-034E REPAIR NR 8, B727 SRM'S 51-30-2,51-10-2 AND TPS 1003 REV A.

Part: SKIN — LIGHTNING STRIKE · airframe 39,210 hrs · 25,640 cycles

NOSE AREA FUSELAGE EXTERNAL SKIN HAS SEVERAL LIGHTNING STRIKES BETWEEN BS178 AND 203.8 BETWEEN STRINGERS 24 TO 26 LT. REMOVED DAMAGE, FABRICATED, ALODINED, PRIMED AND INSTALLED. FUS SKIN REPAIR STA 178 TO 203 BETWEEN STRINGERS 26LAND 24L ALL IAW FX B727 SRM'S 53-30-3 FIG'S 3 AND 13, 53-30-1,53-30-2,51-30-2 AND 51-10-2. SNRM N00680.

Part: FRAME — CORRODED (ZONE 200) · airframe 39,210 hrs · 25,640 cycles

FRAME AT STA 950C 4 INCHES RT OF CENTER LINE IS CORRODED. REMOVED DAMAGE, FABRICATED, ALODINED, PRIMED AND INSTALLED FRAME REPAIR AT STA 950C LBL 4 TO RBL 4 ALL IAW FX B727 SRM 53-10-4 FIG12,51-30-2,53-10-1, 53-10-2 AND 51-10-2.

Part: SHEAR TIE — CORRODED (ZONE 100) · airframe 39,210 hrs · 25,640 cycles

FWD PIT SHEAR TIE STA 700 BETWEEN STRINGER 28L AND 27L IS CORRODED. REMOVED AND REPLACED WITH NEW SHEAR TIE AT STA 700 BETWEEN S28L AND 27L IAW SRM B727 51-30-5 AND 51-30-2. SNRM N01051.

Part: SKIN — CORRODED (FUSELAGE) · airframe 39,210 hrs · 25,640 cycles

FUS SKIN AT FWD PIT STA 700-720A BETWEEN STRINGER 27L AND 28L IS CORRODED. REMOVED DAMAGE, FABRICATED, ALODINED , PRIMED AND INSTALLED FUS SKIN REPAIR STA 700-720A FROM STRINGER 27L TO 28L ALL IAW SRM'S 53-30-1 FIG1,53-30-3 FIG3,51-30-2 AND 51-10-2. SNRM N01050.

Part: SKIN — CORRODED (ZONE 100) · airframe 39,210 hrs · 25,640 cycles

FWD PIT STA 680 FROM STRINGER 27R TO 28R SKIN IS CORRODED. FABRICATED, ALODINED, PRIMED AND INSTALLED FUS SKIN REPAIR AT STA BS 680-690 AND STRINGER 27R TO 28R ALL IAW FX SRM'S 53-30-3 FIG 3, 53-30-1, 53-30-2,51-30-2 AND 51-10-2. SNRM N01070.

Part: STRINGER — CORRODED (ZONE 100) · airframe 39,210 hrs · 25,640 cycles

FWD PIT AT STA 490 STRINGER 26L HAS CORROSION AT SPLICE. REMOVED, FABRICATED, ALODINED, PRIMED AND INSTALLED STRINGER 26L REPAIR AT STA 490 ALL IAW FX B727 SRM REF'S 53-10-3 FIG 1, 51-10-6, 51-10-2 AND 51-30-2.

Part: SKIN — GOUGED (ZONE 100) · airframe 39,210 hrs · 25,640 cycles

FUSELAGE EXTERIOR SKIN HAS 1 INCH GOUGE AT STA 380 AND STRINGER 15L. FABRICATED, ALODINED, PRIMED AND INSTALLED FUS EXTERIOR DOUBLER AT STA 380 AND S15L ALL IAW FX B727 SRM REF'S 53-30-3 FIG 3A, 53-30-2, 53-10-1 AND 51-10-2.

Part: SHEAR TIE — DAMAGED (FUSELAGE) · airframe 38,386 hrs · 24,988 cycles

SHEAR TIE AT BS 380 AT STR 16 NEEDS TO BE REPAIRED TO ACCOMPLISH 9G RIGID BARRIER MOD. *S/D* REPAIRED PER SRM 54-10-4.

Part: SHEAR TIE — DAMAGED (FUSELAGE) · airframe 38,386 hrs · 24,988 cycles

SHEAR TIE AT BS 380, STR 14 NEEDS TO BE REPAIRED TO ACCOMPLISH 9G BARRIER MOD. *S/D* REPAIRED PER SRM 53-10-4.

Part: PROXIMITY SWITCH — MALFUNCTIONED (RT MLG) · airframe 37,239 hrs · 24,097 cycles

RIGHT GEAR GREEN AND UNSAFE LIGHT REMAIN ILLUMINATED AFTER T/O WITH GEAR HANDLE UP. FOLLOWED QRF AND CYCLED GEAR WITH SAME RESULTS. LOWERED GEAR AND LANDED UNEVENTFULLY.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 36,997 hrs · 23,886 cycles

DAMAGED FASTENER HOLES ON FRAME AT BS 1110, LBL 22, WL 152. CUT OUT MATERIAL FROM FRAME THAT HAD DAMAGED FASTENERS HOLES AT BS 1110, LBL 22, WL 152. FABRICATED REPAIR FROM HFAB53-FR-011, AND INSTALLED ALL IAW SRM 53-10-1, 51- 40-3, 51-30-5, 51-30-2, AND 51-10-2, FED-EX E.A. 7-5310-54912.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 36,997 hrs · 23,886 cycles

DAMAGED FASTENER HOLE ON FRAME AT BS 1070, LBL 22, WL 152. DAMAGED FASTENER HOLES ON FRAME AT BS 1070, LBL-22, WL-152 FOUND TO BE OUT OF LIMITS PER SRM 53-10-1, CUT OUT DAMAGED MATERIAL AND REPAIRED IAW SRM5 1-40-3, FED- EX EA 7-5310-54913.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 36,997 hrs · 23,886 cycles

ELONGATED FASTENER HOLE AT B/S 1070, 1050, 1110, LBL-22, WL-152. REPAIRED FRAME AT B.S. 1070, 1050, 1110, LBL 22 (WL 152) IAW SRM 51-40-3 AND EA 7-5310-54911.

Part: FLOORBEAM — BULGED (FUSELAGE) · corrosion level 2 · airframe 36,997 hrs · 23,886 cycles

PLATE ON 25G BEAM UNDER FE'S SEAT BULGED. ACCESSED FLOOR PANELS; REMOVED 25G BEAM; REPLACED WITH NEW PART; PER SRM 51-30- 2; REINSTALLED ACCESSED GROUP.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,997 hrs · 23,886 cycles

CORROSION ON SHEAR TIE AFT SIDE BS 1130, BETWEEN STR 29 AND 28 LT. REMOVED CORROSION ON SHEAR TIE AFT SIDE 2.20 X 1.80 X .007 INCH MAX, IAW SRM 51-10-6. ORIGINAL MATERIAL .050, OUT OF LIMITS IAW SRM 53-10-1 FIG 1. FABRICATED REPAIR SHEAR TIE OF 7075 T6 .050 LOT 504450 PER SRM 51-10-3, SRM 51-20-1, SRM 51-30-5, ALODINED PER SRM 51-10-2 PAR 3 G. PRIMED, PAINTED AND INSTALLED IAW FED-EX MM 51-20-151-7 SEC 5-8 AND SRM 51-30-2 SEC 4.

Part: STRUCTURE — WORN (PYLON-BODY) · airframe 36,997 hrs · 23,886 cycles

NR 2 ENGINE LT FWD COWL FWD FUSELAGE MATING SURFACE WORN THROUGH AT BS 1350.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,997 hrs · 23,886 cycles

CORROSION ON FRAME SHEAR TIE AND FUSE SKIN AT BS 720C LBL 12, WL 150. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. REPAIRED SHEAR TIE PER SRM, 51-30-2, 51-10-1, 53-10-1, 51-10-2, 51-10-3.

Part: SKIN — GOUGED (FUSELAGE) · airframe 36,997 hrs · 23,886 cycles

SKIN GOUGED IN 3 PLACES BS 384 BELOW STR 24L. REPAIRED SKIN BS 384 BELOW STR 25L IAW SRM 53-30-3 DETAIL 1.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,997 hrs · 23,886 cycles

CORROSION ON SHEAR TIE AFT SIDE BS 1130, BETWEEN STR 29 AND 28 LT. REMOVED CORROSION ON SHEAR TIE AFT SIDE 2.20 X 1.80 X .007 INCH MAX, IAW SRM 51-10-6. ORIGINAL MATERIAL .050, OUT OF LIMITS IAW SRM 53-10-1 FIG 1. FABRICATED REPAIR SHEAR TIE OF 7075 T6 .050 LOT 504450 PER SRM 51-10-3, SRM 51-20-1, SRM 51-30-5, ALODINED PER SRM 51-10-2 PAR 3G, PRIMED, PAINTED AND INSTALLED IAW FED-EX MM 51-20-151-7 SEC 5-8 AND SRM 51-30-2 SEC 4.

Part: SKIN — WORN (NR 2 NACELLE) · airframe 36,997 hrs · 23,886 cycles

NR 2 ENGINE LT FWD COWL FWD FUSELAGE MATING SURFACE WORN THROUGH AT BS 1350. FOUND AREA ON 1350 RING CHORD TO HAVE 100 PERCENT MATERIAL LOSS AND CRACKED OUT OF LIMITS. REMOVED 1350 RING CHORD. DRILLED UP AND INSTALLED NEW 1350 CHORD IAW SRM 51-30-2, 51-30-5.

Part: CONTROL UNIT — FALSE INDICATION (E&E BAY) · airframe 36,815 hrs · 23,734 cycles

AT FL 190 AND CLIMBING (310 KIAS) THE FIRE WARNING BELL & MASTER FIRE LIGHT WENT OFF CONTINUOUSLY WITH NO OTHER INDICATIONS. THE BELL WOULD ONLY SILENCE WHEN ANY SILENCING BUTTON WAS HELD IN. BELL AND LIGHT WENT OUT ON DESCENT, CAME BACK ON AS AIRCRAFT BLOCKED IN. BELL AND LIGHT WERE STILL ON UPON ACFT ARRIVAL, CONNECTED EXTERNAL PWR, DURING DEBRIEF WITH CREW, EXTERNAL PWR DROPPED OFF-STARTED APU, APPLIED PWR AND THE BELL AND LIGHT DID NOT COME BACK ON. COULD NOT GET THE PROBLEM TO DUPLICATE. T/S TO FIRE AND OVERHEAT DETECT OR ACCESSORY BOX IN E/E. REMOVED AND REPLACED FIRE DETECTOR BOX PER SMP'S. FIRE SYSTEM TEST NORMAL PER JRH CHAPTER 5 .

Part: SWITCH — LACK OF LUBE (LT MLG) · airframe 36,197 hrs · 23,242 cycles

LEFT MAIN GEAR DOOR INDICATED UNSAFE WHEN GEAR WAS LOWERED. CYCLED GEAR AND DOOR LIGHT WENT OUT PER NORMAL OPS. CLEANED AND LUBED LEFT MAIN LANDING GEAR DOOR SWITCH CHECKED ADJUSTMENT AND TEST PER MM. OPERATED DOORS SEVERAL TIMES AND OPS CHECKED GOOD.

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 36,194 hrs · 23,239 cycles

LEFT GEAR DOOR LIGHT REMAINED ILLUMINATED ON TAKEOFF. LIGHT STAYED ON AFTER CYCLING GEAR IAW RED TABS. OPERATED LEFT LANDING GEAR DOOR SEVERAL TIMES. DOOR INDICATION OPS GOOD AT THIS TIME.

Part: WARNING LIGHT — ILLUMINATED (LT MLG)

AFTER T/O, MAIN GEAR DOOR LIGHT ILLUM. INSPECTED AND CYCLED LT GEAR DOOR CHECK OK. DEFER PER MEL 32-01.

Part: SENSOR — INOPERATIVE (NR 2 ENGINE)

DURING PREFLT INSP FOUND NR 2 FIRE WARN FIRE WALL INOP. FOUND 2 FIRE WALL FIRE LOOP CUT AND NR 6 BLD PLUMBING FROM FIRE WALL BLOWN OUT AND HEAT SHIELD DAMAGED AROUND DUCTING. *S/D* REMOVED AND REPLACED NR 2 ENG SENSOR / RESPONDER ON WORK RELEASE 26-10/4135. REMOVED AND REPLACED NR 2 ENG THERMAL ANTI-ICE DUCT, LWR LEFT FIREWALL PER MM 36-00-001-2, 727 SRM 54-10-3.

Part: TRANSMITTER — READS LOW (COCKPIT)

NR 2 ENGINE WAS CK DURING TAKEOFF/CLIMBOUT. FIVE MIN INTO FLT OIL PRESS FELL TO 40 PSI RAN CK LIST AT IDLE OIL PRESS WAS 30. SHUTDOWN AND RETURN TO ARN. OIL PRESS TRANSMITTER REPLACED PER MM 79-32-1.

Part: DOWN LOCK SW — FAILED (TAIL SKID)

TAIL SKID LIGHT ON AFTER TAKEOFF. RECYCLE GEAR, NO SUCCESS. *S/D* REMOVED AND REPLACED DOWN LOCK SWITCH S662 NR MS25011-1 PER MM 32-71-101. CK ADJUSTMENT OF SWITCH S663 PER MM 32-71-91. CYCLED TAIL SKID, COULD NOT DUP PROBLEM.

Part: CONNECTOR — DIRTY (NR 3 STRUT)

DURING CLIMB WITH ENG ANTI-ICE ON, ENG NR 3 STRUT OVERHEAT LIGHT ILLUM. ALL ITEM IN EMERGENCY CHECKLIST ACCOMP. LIGHT WENT OUT AND REMAINED OUT WHEN THRUST WAS RESTORED. REPEAT WRITEUP. CONNECTION TO STRUT OVERHEAT DETECTOR REMOVED. CLEANED AND REFITTED. CLAMP CONNECTION IN STRUT AREA RETIGHTENED AS REQUIRE. GROUND RUN CARRIED OUT. SYS FUNCTION CKS SATISFACTORY.

Part: CLAMP — LEAKING (NR 3 ENGINE)

NR 3 ENG STRUT OVERHEAT LIGHT CAME ON WITH RT PK AND NR 3 BLD ON. PER CK LIST TURN NR 3 BLD OFF LIGHT WENT OUT. AFTER THROTTLE UP LIGHT DID NOT COME BACK ON. FOUND ONE OF THE NR 3 ENG BLD VALVE CLAMP LEAK. REMOVED AND REPLACED NR 3 ENG BLD VALVE CLAMP. RAN NR 3 ENG PER JET RUN HANDBOOK. NO LEAK FOUND.

Part: CLAMPS — DISCONNECTED (NR 3 ENGINE)

98-242 - APPROX 6 INTO FLT AT FL 330, NR 3 ENG STRUT OVERHEAT LIGHT ILLUM. CONFIG WAS BOTH PKS ON NR 2 AND NR 3 ENG BLDS OPEN, ENG ANTI-ICE CLOSED. RAN RED TAB PROCEDURES. ENG EXTINGUISH WITH NR 3 BLD CLOSED AND 3 ENG RETARD TO 65 PERCENT N1. RESTORE ENG. LIGHT REMAIN EXTINGUISH REMAINDER OF FLT. FOUND CLAMP DISCONNECT BETWEEN PRECOOLER AND BLD AIR DUCT TO FIRE WALL RECONNECT CLAMP AND RAN ENG PER JET RUN HDBK. NO LEAKS FND. SYS CK OK PER MM 26-14-1.

Part: SWITCH — FAILED (NR 3 LE FLAP)

98-0080 CDG - AFTER TAKEOFF DURING FLAP RETRACTION TO 0 HAD FAILURE NR 3 LED FAILED TO RETRACT. PERFORMED APPROPRIATE CHECK LIST WITH NO RESOLUTION OF PROBLEM. DUMPED FUEL TO MAXIMUM LAND WEIGHT. NORMAL LANDING AT CDG. INSTALLED JUMPER CABLE ON NR 3 LEADING EDGE FLAP POSITION SWITCH AS PER MAINTENANCE MANUAL 27-82-0. OPERATION OF FLAPS AND SLATS PERFORMED, ALL INDICATION NORMAL. NR 3 LEADING EDGE FLAP POSITION INDICATION SWITCH REPLACED PER MAINTENANCE MANUAL 27-82-1 ADJUSTMENT AND TEST PER SAME. ALL INDICATIONS NORMAL.

Part: RETRACT IND — MALFUNCTION (LE FLAPS)

LEADING EDGE DEVICE AMBER LIGHT ON AT 2 DURING FLAP RETRACTION NUMBER 3 AND 4 LEADING EDGE DEVICE INDICATOR LIGHTS SHOWED AMBER. RECYCLED 2 TIMES IN FLIGHT, NO CHANGE. LEADING EDGE DEVICES WERE OK AT 5/15/25/30 ON FLAP RETRACTION. CYCLED SLATS AND FLAPS FOR SEVERAL TIMES ALL INDICATIONS WERE NORMAL. VISUAL INSPECTED SLAT AND FLAPS FOR CONDITION, NO OBSTRUCTIONS FOUND.

Part: INDICATION — MALFUNCTION (LANDING GEAR)

CDG: 97-0149 ON INITIAL GEAR EXTENSION HAD RED NOSE GEAR LIGHT NO GREEN. PER RED TABS RECYCLED, ON SECOND ATTEMPT NOSE GEAR INDICATED DOWN AND LOCKED. PERFORMED NOSE GEAR SWING SEVERAL TIMES. INDICATION IS NORMAL CHECKED NOSE GEAR WHEEL WELL FOUND OK. INSPECTED SWITCHES AND WIRES FOR INTEGRITY FOUND ALL NORMAL. AIRCRAFT OK FOR SERVICE.

Part: SKIN — CORRODED (BS 720)

BS 720 O/B SIDE OF STR 28 RT, FUSELAGE SKIN IS BULGING. CUT OUT DAMAGE AREA 1 INCH BY 2 INCH AND INSTALLED DOUBLER PER SRM 51-0-6.

Part: SHEAR TIE — CORRODED (BS 590)

AFT LEG OF SHEAR TIE ON BELL FRAME STA 590 IS DEEPLY CORRORED BETWEEN STR 26 TO 27L. CORROSION WAS FOUND BEYOND LIMITS. REMOVED SHEAR TIE AND REPLACES WITH SERVICEABLE SHEAR TIE PER SRM 51-10-1.

Part: STRINGER — CORROSION (FS 720)

FORWARD CARGO STA 720, STR 28R, HAS CORROSION ON STRINGER. REPLACED CORRODED STRINGER PER SRM 53-10-3 WITH NEW STRINGER, 3 FEET, AND SPLICE.