N194FE

Part: ENGINE — LEAKING (NR 3) · airframe 66,589 hrs · 48,628 cycles

LOST OF OIL QUANTITY AND PRESSURE IN NR 3 ENG. SHUTDOWN PER CHECK LIST AND LANDED. INSPECTED CHIP DETECTORS, AND FILTER FOUND TO BE CLEAN. FOUND OIL PUDDLED IN TAILPIPE, NO EVIDENCE OF OIL IN COLD STREAM AREA. SERVICED ENG OIL AND MOTORED. OIL QTY DROPPED STEADILY TO 0 AND OIL RAN FROM TAILPIPE. OIL COMING FROM ENG CORE. PER CREW REPORT AND ENG M/M 72-00 P 518D PROBABLE ENG CHANGE. ENGINE REPLACED.

Part: DRIVE MOTOR — FAILED (RT MLG WW)

AT FLIGHT LEVEL 350 BOTH SYSTEM-A PRESSURE LIGHTS FLICKERED. SYSTEM-A PRESSURE WENT TO 0 EXECUTED LOSS HYDRAULIC CHECK LIST. SYSTEM-A FLUID SHUTOFFS WERE CLOSED AT 0410. REMOVED AND REPLACED OUTBOARD FLAP DRIVE MOTOR, OPERATIONAL CHECKS IN ACCORDANCE WITH MAINTENANCE MANUAL 27-51-62. OPERATIONAL CHECKS NORMAL, NO LEAKS NOTED.

Part: CABLE — DISLODGED (AFT CARGO DOOR)

AFT CARGO DOOR WARNING LIGHT ON SECOND OFFICER'S PANEL ILLUMINATED DURING CLIMBOUT PASSING 2,600 FEET. RETURN TO FIELD TO TROUBLESHOOT. FOUND CABLE STUCK IN DOOR JAMB. OPENED AND CLOSED DOOR, ALL LIGHTS WENT OUT.

Part: RADOME — CHIPPED (BS 175)

WHILE WORKING CARD 71C102-01, FOUND RADOME TO BE MISALIGNED AT BS 178 ALLOWING RADOME TO CATCH DOUBLER WHICH CRACKED DOUBLER AND CHIPPED RADOME WL 285, LBL 4. REPAIRED RADOME WL 285 LBL 4, PER SRM 53-50-4 AND REPAIRED SKIN DOUBLER AT BS 178 WL 235 LBL 4 PER EA 7-5310-27737.

Part: SKIN — CRACKED (BS 423)

WHILE PERFORMING PRESSURIZATION DISCOVERED CRACK IN EXTERIOR SKIN BS 423, JUST BELOW STR 23 RT. REPAIRED EXTERIOR SKIN IAW SRM 53-30-3 FIG 2.

Part: SPAR CHORD — CORROSION (BS 870)

CORROSION (C53-132-02) ON THE WING CENTER SECTION REAR LOWER CHORD, STA 870 LBL 20 TO 26 WL 140. REMOVED AND REPLACED LOWER CHORD PER FEDEX EA 7-5710-27481.

Part: BULLNOSE — CORROSION (NR 4 LE FLAP)

CORROSION (097-562-01-2) NR 4 K-FLAP BULLNOSE O/B BONDING JUMPER, UPPER ATTACH POINT. REMOVED CORROSION PER FEDEX SRM 57-50-03 AND 27-57-010.

Part: SHEAR WEB — CORRODED (BS 1174)

CORROSION EMANATING FROM UNDER NUTPLATES ON BOTTOM SIDE OF SHEAR WEB AT BS 1174 RBL 6 TO LBL 20 WL 208. FABRICATED NEW WEB AND INSTALLED PER SRM 53-10-1.

Part: DOOR FRAME — GOUGED (BS 310)

FWD ENTRY DOOR LATCH ROLLER RUBS ON DOOR STRUCTURE. REMOVED AND REPLACED FWD SIDE FRAME SRM 53-10-1.

Part: SPAR CHORD — CORROSION (BS 870)

CORROSION (C53-132-02) ON THE WING CENTER SECTION REAR UPPER SPAR CHORD, STA 870 LBL 30 RBL 30 WL 174. REMOVED AND REPLACED UPPER CHORD PER FEDEX EA 7-5710-27481.

Part: SHEAR TIE — DAMAGED (BS 600)

MECH DAMAGE ON SHEAR TIE AT BS 600 BETWEEN STR 16 AND 17R. REMOVED AND REPLACED SHEAR TIE SRM 53-10-1.

Part: SKIN — CREASED (BS 366)

BS 366 STR 20R THERE IS A CREASE IN SKIN. REPAIRED CREASE PER FEDEX SRM 53-03-3.

Part: FITTING — CORRODED (BS 1342)

CORROSION (C53-137-01) BS 1342 RBL 17 STR 5R ON FITTING ANGLE. REMOVED CORRODED TERMINAL FITTING AND INSTALLED NEW RT SPAR TERMINAL FITTING ON VERTICAL STABILIZER AT BS 1342 IAW BOEING SB 727-55-088.

Part: FITTING — CORRODED (BS 360)

CORROSION ON STR 20L FITTING BS 360 TO 367. REMOVED AND REPLACED CORRODED FITTING PER SB 727-53-0209.

Part: INTERCOSTAL — DENTED (BS 1055)

DENTED INTERCOSTAL BS 1055 BETWEEN STR 23L TO 25L LBL 36 TO 48 WL 156. REMOVED AND REPLACED OUT OF LIMITS INTERCOSTAL PER FEDEX SRM 53-10-1.

Part: FITTING — CORRODED (BS 1342)

CORROSION (C53-137-01) BS 1342 LBL 17 STR 5L ON FITTING ANGLE. REMOVED AND REPLACED FITTING ON VERTICAL STABILIZER AT BS 1342 LBL 17 AT STR 5L PER SB 727-55-00.

Part: MID SPAR — WORN (VERT STAB)

VERTICAL FIN MID SPAR, STR 7 AND PANEL SUPPORT HAS WORN FASTENER HOLE AT FIN STA 225.707 RT. REPAIRED PER FEDEX EA 7-5510-27728.

Part: FITTING — CORRODED (BS 360)

CORROSION 26L BS 360 FITTING. REPLACED STR TIE FITTING AT STR 26L, BS 360 AND MADE STR REPAIR ON STR 26L FROM BS 360 TO 390. DAMAGE ON THAT PORTION OF STR WAS FOUND TO BE OUT OF LIMITS AS PER FEDEX SRM 53-10-1 FEDEX SRM 53-10-3.

Part: STRINGER — DAMAGED (BS 560)

MECH DAMAGE ON STR 25L BS 560 WL 154. REPAIRED DAMAGED STR AT BS 560 STR 25L WL 154 PER FEDEX EA 7-5310-27491.

Part: BLKHD SUPPORT — CORRODED (BS 1342)

REMOVED VERTICAL CHORD TO ACCESS TERMINAL FITTING AND DISCOVERED CORROSION ON BULKHEAD SUPPORT CHANNEL, BS 1342 WL 238 TO 246 RBL 24. REMOVED AND REPLACED BS 1342 BULKHEAD SUPPORT CHANNEL OF BS 1342 RBL 24 WL 193 TO 258.

Part: STIFFENER — CRACKED (BS 740)

WHILE WORKING 7-5310-7-3367B PT 1, DISCOVERED A CRACK IN THE FWD PRESSURE PAN STIFFENER AT BS 740 WL 208 LT. ALSO, FOUND FWD PRESSURE PAN DAMAGED, FABRICATED NEW STIFFENER AND RIVETED TOGETHER NEW PAN. ALL WORK ACCOMPLISHED PER FEDEX SRM 51-20-1 AND BOEING DRAWING NR 65-38294.

Part: CHORD — CORROSION (BS 1342)

AREA OF CORROSION ON BS 1342 CHORD UPPER FWD RT FLANGE RBL 20. REMOVED AND REPLACED UPPER CHORD IAW FEDEX DRAWING 65-17508.

Part: DOUBLER — CRACKED (BS 178)

WHILE WORKING CARD NR 71C102-01, FOUND RADOME TO BE MISALIGNED AT BS 178, ALLOWING RADOME TO CATCH DOUBLER WHICH CRACKED DOUBLER AND CHIPPED RADOME WL 235 LBL 4. *S/D* REPLACED RADOME WL 235, LBL 4 PER FEDEX SRM 53-50-4 AND REPAIRED SKIN DOUBLER BS 178, WL 235, LBL 4 PER FEDEX EA 7-5310-27737.

Part: SKIN — CORRODED (BS 1142-1148)

WHILE WORKING NR0007, FOUND CORROSION IN UPPER SKIN LAP BS 1142 TO 1148 STR 26R. REPAIRED SKIN PER SRM 53-30-3 AND SB 727-53-0072.

Part: CHORD — CORRODED (BS 1176)

CORROSION (C53-224-08), ON BS 1176 CHORD AT LBL 20 AND RBL 65 WL 208. REMOVED AND REPLACED 1176 CHORD PER 51-30-2.

Part: SKIN — GOUGED (BS 590-620)

THREE GOUGES IN SKIN AT BS 590 TO 620, BETWEEN STR 21 TO 22R. REPAIRED 3 GOUGES IN THE SKIN AT BS 590 TO 620, BETWEEN STR 21 TO 22R PER FEDEX SRM 53-30-3.

Part: SHEAR TIE — CRACKED (BS 1166)

SHEAR TIE IS CRACKED AT FASTENER HOLE, BS 1166 BETWEEN STR 25 TO 26R. REPAIRED CRACKED SHEAR TIE PER FEDEX SRM 53-10-4 FIG 14.

Part: SKIN — CORRODED (BS 227.8)

BULGING AROUND FASTENERS ON EXTERIOR SKIN BS 227.8 RBL TO LBL 5. REPAIRED BULGING SKIN AT BS 227.8 RBL TO LBL 5 AS PER FEDEX SRM 53-30-3.

Part: SPAR CHORD — CORROSION (BS 870)

CORROSION (C53-132-02) ON THE WING CENTER SECTION REAR UPPER SPAR CHORD, STA 870 LBL 30 RBL 30 WL 174. *S/D* REMOVED AND REPLACED UPPER CHORD PER FEDEX EA 7-5710-27481.

Part: THRESHOLD WEB — CORRODED (BS 527)

CORROSION (C53-111-01-1) ON DOOR THRESHOLD VERTICAL WEB, BS 527 RBL 22 WL 156. REMOVED, FABRICATED AND INSTALLED VERTICAL AND HORIZONTAL WEB PER SRM 53-10-1.

Part: VERT MID SPAR — WORN (FS 225.707)

VERTICAL FIN MID SPAR, STR 7 AND PANEL SUPPORT HAS WORN FASTENER HOLE AT FIN STA 225.707 LEFTSIDE. *S/D* REPAIRED PER FEDEX EA 75510-27728.

Part: MID SPAR — WORN (VERT STAB)

VERTICAL FIN MID SPAR, STR 7 AND PANEL SUPPORT HAS WORN FASTENER HOLE AT FIN STA 225.707 LT. REPAIRED PER FEDEX EA 7-5510-27728.

Part: FAIL-SAFE — CORRODED (BS 380)

CORROSION (53-111-01-1) ON THE FAIL-SAFE AT BS 380 STR 26L WL 150 AROUND I/B FASTENER HOLE. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PARTS PER SRM 51-40-3.

Part: STRAP — CORRODED (BS 520)

CORROSION (C53-111-01-2), ON FWD CARGO BAY THRESHOLD STRAP, BS 520 RBL 24 WL 156. REMOVED AND REPLACED THE FWD CARGO BAY THRESHOLD STRAP BS 500 TO 580 RBL 24 WL 156.

Part: INTERCOSTAL — DENTED (BS 1055)

DENTED INTERCOSTAL BS 1055 BETWEEN STR 23 TO 25L LBL 36 TO 48 WL 156. *S/D* REMOVED AND REPLACED OUT OF LIMITS INTERCOSTEL PER FEDEX SRM 53-10-1.

Part: FLOOR BEAM — CORRODED (BS 600)

CORROSION (C53-111-01, -2) ON LOWER FLANGE OF FLOORBEAM IN NUTPLATE HOLES AT BS 600 LBL 20 TO RBL 26 WL 200. REMOVED CORRODED AREA FROM LBL 17 TO RT SKIN. FABRICATED AND INSTALLED REPAIR PARTS PER FEDEX SRM 53-10-8 FIG 2.

Part: FLOOR BEAM — DOUBLE DRILLED (BS 580)

WHILE WORKING NR0308 FOUND HOLE IN RADIUS OF FLOOR BEAM LOWER CHORD BS 580 BL 0 WL 200. *S/D* REPAIRED FLOOR BEAM PER SRM 53-10-8.

Part: SHEAR WEB — CORRODED (BS 1173)

CORROSION (C53-224-02), ON SHEAR WEB AT BS 1173 RBL 27 WL 208. REPAIRED SHEAR WEB PER SRM 51-40-2.

Part: BLKHD WEB — CORROSION (BS 870)

ON REMOVAL OF THE REAR, UPPER AND LOWER SPAR CHORDS, FOUND 870 BULKHEAD WEB HAS CORROSION, LBL TO RBL 70 WL 174 TO 140. REMOVED AND REPLACED 870 BULKHEAD WEB.

Part: FLOORBEAM — DOUBLE DRILLED (BS 540)

WHILE WORKING CARD NR0683, FOUND BS 540 FLOORBEAM BL 0 WL 208 TO HAVE DOUBLE HOLE. REPAIRED FLOORBEAM AT BS 540 BL 0 WL 208 IAW FEDEX SRM 53-10-8.

Part: SKIN — GOUGED (BS 945)

GOUGE IN EXTERIOR SKIN BS 945 STR 9R. REMOVED DAMAGED SKIN, BS 945 STR 9R. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FEDEX SRM 53-30-3.

Part: BLKHD WEB — CUT (BS 950)

WHILE WORKING NR0788, FOUND A CUT IN 950 BULKHEAD VERTICAL WEB BL 0 WL 208 AFT SIDE. REPAIRED CUT IN 950 BULKHEAD VERTICAL WEB AT BL 0 WL 208 AFT SIDE PER FEDEX SRM 53-10-9 FIG 2.

Part: FLOORBEAM — DOUBLE DRILLED (BS 580)

WHILE WORKING CARD NR0683, FOUND BS 580 FLOORBEAM BL 0 WL 208 TO HAVE DOUBLE HOLE. REPAIRED DOUBLE HOLE PER FEDEX SRM 53-10-8.

Part: CHANNEL — CORROSION (BS 1057-1110)

CORROSION (C53-111-01, -3), ON NR 2 CARGO DOORWAY C-CHANNEL BS 1057 TO 1110 RBL 27 WL 147. REMOVED AND REPLACED C-CHANNEL AT DOORWAY.

Part: FLOORBEAM — CORRODED (BS 1110)

CORROSION (C53-111-01, -3), ON LOWER CHORD OF 1110 FLOORBEAM WL 200 LBL 2 TO 30 AT NUTPLATE HOLES. REMOVED AND REPLACED CORRODED LOWER CHORD OF BS 1110 FLOORBEAM AT WL 200 RBL 4 TO LBL 19.75 WITH FABRICATED REPAIR PARTS PER SRM 53-10-8 FIG 2.

Part: STRINGER — DAMAGE (BS 560)

MECHANICAL DAMAGE ON STR 25L BS 560, WL 154. *S/D* REPAIRED DAMAGE STRINGER AT BS 560, STR 25L WL 154 PER FEDEX EA 7-5310-27491.

Part: STRINGER — CORROSION (BS 930)

CORROSION (C53-224-01, -2), ON STR 9R BS 930 PLUS 7 RT AREA IS OUT OF LIMITS. REPAIRED STR 9R IAW FEDEX SRM 53-10-3.

Part: FRAME — CRACKED (BS 580)

THE FRAME AT BS 580 IS CRACKED ON I/B FLANGE AT RBL 67 WL 210. THE FRAME AT BS 580 RBL 67 WL 210 WAS FOUND TO BE DAMAGED BEYOND LIMITS PER FEDEX SRM 53-10-1. REPAIRED FRAME PER FEDEX SRM 51-40-3.

Part: WEB — CORROSION (BS 294-355)

CORROSION ON WEB AT BS 294.5 TO 355 RBL 10 TO 35 WL 169. CORROSION FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED WEB PER SRM 51-40-02.

Part: FLOORBEAM — DOUBLE DRILLED (BS 500)

DOUBLE HOLE IN FLOORBEAM BS 500 BL 0 WL 208.1. REPAIRED DOUBLER HOLE AT BS 500 BL 0 WL 208 IAW FEDEX SRM 53-10-8.

Part: FLOORBEAM — DOUBLE DRILLED (BS 600)

WHILE WORKING CARD NR0683, FOUND BS 600 FLOORBEAM BL 0 WL 208 TO HAVE DOUBLE HOLE. REPAIRED FLOORBEAM BS 600 BL 0 WL 208 IAW FEDEX SRM 53-10-8.

Part: SKIN — CORROSIOIN (FUSELAGE)

BS 1110 STR 26, THERE IS BULGE IN SKIN TRIPLER DAMAGED OUT OF LIMITS. REPLACED BONDED DOUBLER AT BS 1148 TO 1166 STR 25 TO 26R. REPLACED BONDED TRIPLER FROM BS 1108 TO 1130 STR 25 TO 26R. REPAIRED REMAINING DEBONDED SKIN USING FIXED PATTERN PER FEDEX SRM 53-30-4, FROM BS 1110 TO 1183.

Part: FLOORBEAM — CORROSION (BS 640)

CORROSION (C53-111-01, -2), ON LOWER FLANGE OF FLOORBEAM BS 640 RBL 23 TO 26.7 WL 200. REMOVED CORROSION ON LOWER FLANGE OF FLOORBEAM IN NUTPLATE HOLES AT BS 640 LBL 20 TO RBL 26 WL 200. FOUND TO BE OUT OF LIMITS AT RBL 23 TO RBL 26.5, REPAIRED IT AS PER FEDEX SRM 53-10-8.

Part: WEB — CORRODED (BS 303-309)

CORROSION (C53-111-01-1), ON DOGHOUSE WEB STA 303 TO 309 LT LBL 15 WL 177. REMOVED CORROSION FOUND MATERIAL LOSS WAS WITHIN LIMITS PER SRM 53-10-1. TREATED AREA, PRIMED AND REINSTALLED FASTENERS.

Part: HINGE RIB — CRACKED (RT ELEVATOR)

RT ELEVATOR HINGE RIB AT HORIZONTAL STAB STATION 136.50 IS CRACKED ON THE I/B UPPER FLANGE. REMOVED AND REPLACED ELEVATOR HINGE RIB PER SRM 27-30-0.

Part: FITTING — CORRODED (BS 360)

CORROSION (C53-111-01-1) STR 26L FITTING BS 360. REPAIRED STRINGER TE FITTING AT S26L, BS 360 AND MADE STRINGER REPAIR ON S26L FROM BS 360 TO 390, DAMAGE ON THAT PORTION OF STRINGER FOUND TO BE OUT OF LIMITS PER SRM 53-10-1 AND SRM 53-10-3.

Part: FITTING — CORRODED (BS 360-367)

CORROSION ON STR 20L FITTING BS 360 TO 367. REMOVED AND REPLACED CORRODED FITTING PER SB 727-53-0209.

Part: SKIN — GOUGED (BS 945)

GOUGE IN EXTERIOR SKIN BS 945 STR 9R.

Part: FLOORBEAM — CORRODED (BS 540)

CORROSION AT BS 540 FLOORBEAM LOWER CHORD FROM LBL 16 TO RBL 28 WL 200. REPAIRED LOWER CHORD OF FLOORBEAM AT BS 540 WL 200 FROM LBL 16 TO RBL 28 IAW FEDEX SRM 53-10-08.

Part: SKIN — GOUGE (BS 640-650)

GOUGES IN SKIN AT BS 590 TO 620 BETWEEN STR 21 TO 22R. *S/D* REPAIRED 3 GOUGES IN THE SKIN AT BS 590 TO 620 BETWEEN STR 21 TO 22 RT PER FEDEX SRM 53-30-3.

Part: SKIN — GOUGED (BS 945)

GOUGE IN EXTERIOR SKIN BS 945 STR 9R. REMOVED DAMAGED SKIN, BS 945, STR 9 RT FABRICATED AND INSTALLED REPAIR DOUBLER IAW FEDEX SRM 53-30-3.

Part: LT FITTING — CORRODED (BS 1342)

CORROSION (C53-137-01) BS 1342 LBL 17 STR 5L ON FITTING ANGLE. REMOVED AND REPLACED FITTING AT 1342, LBL 17 AT S5L PER.

Part: FITTING — CORRODED (BS 360)

CORROSION ON STR 26R FITTING BS 360. REMOVED T-FITTING BS 360 STR 26R, INSTALLED NEW T-FITTING AT BS 360 STR 26R.

Part: STRINGER — GOUGED (BS 640)

WHILE WORKING NR0429, FOUND GOUGE ON STR NR 3 BS 640 RT. REPAIRED STR NR 3 BS 640 IAW FEDEX SRM 53-10-3.

Part: SUPPORT — CRACKED (BS 1362)

WHILE WORKING NR0122, FOUND RIB SUPPORT WEB TO BE CRACKED AT THREE FASTENER LOCATIONS BS 1362 WL 281 RBL 11. REMOVED AND REPLACED WEB BS 1362 WL 181 RBL 11.

Part: WEB — MECH DAMAGE (BS 560-580)

MECHANICAL DAMAGE AND MISDRILLED HOLES IN WEB AT BS 560 TO 580 LBL 41 WL 200. REMOVED DAMAGE, FABRICATED REPAIR PARTS AND INSTALLED PER SRM 51-40-2.

Part: FLOOR BEAM — CORRODED (BS 620)

CORROSION (C53-111-01, -2) ON LOWER FLANGE OF FLOORBEAM IN NUTPLATE HOLES AT BS 620 LBL 20 TO RBL 26 WL 200. *S/D* REPAIRED FLOOR BS 620, LBL 20 TO RBL 26, WL 200 IAW FEDEX SRM 53-10-8.

Part: WEB — CRACKED (BS 1362)

WHILE WORKING NR0122, FOUND RIB SUPPORT WEB TO BE CRACKED AT 3 FASTENER LOCATIONS BS 1662 WL 281 RBL 11.

Part: SHEAR TIE — CORRODED (BS 970)

CORROSION (C53-111-01, 3) ON SHEAR TIE AT BS 970 RBL 10 WL 138.5. REMOVED AND REPLACED SHEAR TIE AT BS 970 RBL 10 WL 138.5.

Part: FLOORBEAM — DOUBLE DRILLED (BS 970)

WHILE WORKING NR0754, FOUND DOUBLE HOLE IN BS 970 FLOORBEAM AT BL 0 WL 208. REMOVED DAMAGE, FABRICATED REPAIR PARTS AND INSTALLED PER SRM 53-10-8.

Part: NOSE CHORD — CORROSION (NLG WW)

CORROSION (C53-111-01) ON UPPER NOSE CHORD, BS 312 TO 324 RBL 15 WL 169. REMOVED AND REPLACED UPPER NOSE CHORD STA 294.5 TO 355 RBL 15 WL 169 IAW BAC DRAWING NR 65-18415. WEB TO BE INSTALLED ON NR0834 AT STA 294.5 TO 355 RBL 15 TO 25 WL 169.

Part: STRINGER — CORRODED (BS 680-700)

MECH DAMAGE ON STR NR 3 BS 680 TO 700 LT. REMOVED MECH DAMAGE ON STR NR 3 BS 680 TO 700 LT, FOUND TO BE OUT OF LIMITS PER FEDEX SRM 53-10-1. REMOVED DAMAGED SECTION OF STR BS 670 TO 710, FABRICATED REPAIR PARTS AND INSTALLED PER FEDEX SRM 53-10-3 FIG 3.

Part: FLOORBEAM — DOUBLE DRILLED (BS 560)

WHILE WORKING CARD NR0683, FOUND BS 560 FLOORBEAM BL 0 WL 208 TO HAVE 3 DOUBLE HOLES. REPAIRED FLOORBEAM AT BS 560 BL 0 WL 208 IAW FEDEX SRM 53-10-8, (P/N BAC 1505-100617).

Part: SKIN — CREASE (BS 365-390)

LARGE CREASE IN EXTERIOR SKIN BS 365 TO 390 STR 23R. REMOVED DAMAGE, FABRICATED REPAIR PARTS AND INSTALLED PER SRM 53-30-3.

Part: FLOORBEAM — CORRODED (BS 620)

CORROSION (C53-111-01, 2) ON LOWER FLANGE OF FLOORBEAM IN NUTPLATE HOLES AT BS 620 LBL 20 TO RBL 26 WL 200. REPAIRED FLOORBEAM BS 620 LBL 20 TO RBL 26 WL 200 IAW FEDEX SRM 53-10-8.

Part: FLOORBEAM — DOUBLE DRILLED (BS 1010)

WHILE WORKING NRO754, FOUND DOUBLE HOLE IN BS 1010 FLOORBEAM AT BL 0 WL 208. REPAIRED FLOORBEAM BS 1010 BL 0 WL 208 IAW FEDEX SRM 53-10-8.

Part: HINGE FITTING — ELONGATED HOLES (LT AILERON)

O/B LT WING AILERON HINGE FITTING MOST I/B ON AILERON SIDE BOLT HOLES ARE ELONGATED. REMOVED AND REPLACED O/B LT WING AILERON I/B HINGE FITTING. REINSTALLED AND TORQUED ATTACH BOLTS IAW FEDEX MM 27-10-31.

Part: WEB — CRACK (BS 520)

CRACK IN WEB AT BS 520 WL 198 RBL 58. *S/D* REMOVED AND FABRICATED NEW WEB AND INSTALLED THE WEB AT BS 500 TO 580, RBL 58, WL 198 AS PER BOEING DRAWING 65-19309.

Part: CHORD — CORRODED (BS 1176)

CORROSION (C53-224-08) ON BS 1176 CHORD AT LBL 20 AND RBL 65 WL 208. REMOVED AND REPLACED BS 1176 CHORD PER SRM 51-30-2.

Part: FLOOR BEAM — DOUBLE DRILLED (BS 1010)

WHILE WORKING NR0754, FOUND DOUBLE HOLE IN BS 1010 FLOOR BEAM AT BL 0 WL 208. *S/D* REMOVED DAMAGED, FABRICATED REPAIR PARTS AND INSTALLED PER SRM 53-10-8.

Part: FITTING — CORRODED (BS 360)

CORROSION ON STR 26R FITTING BS 360. REMOVED T-FITTING AT BS 360, STR 26R, INSTALLED NEW T-FITTING AT BS 360 STR 26R PER SRM 53-10-1 AND SRM 53-10-3.

Part: WEB — CORROSIOIN (BS 294-355)

CORROSION ON WEB AT BS 294.5 TO 355 RBL 10 TO 35 WL 169. CORROSION FOUND TO BE OUT OF LIMITS. *S/D* REMOVED AND REPLACED WEB PER SRM 51-40-02.

Part: FLOORBEAM — DOUBLE DRILLED (BS 990)

WHILE WORKING NR0754, FOUND DOUBLE HOLE IN BS 990 FLOORBEAM AT BL 0 WL 208. REMOVED DAMAGE, FABRICATED REPAIR PARTS AND INSTALLED PER SRM 53-10-8.

Part: RT FITTING — CORRODED (BS 1342)

CORROSION (C53-137-01) BS 1342 RBL 17 STR 5R ON FITTING ANGLE. REMOVED CORROSION TERMINAL FITTING AND INSTALLED NEW RT SPAR FITTING AT BS 1342 IAW BOEING SB 727-55-088.

Part: FLOOR BEAM — DOUBLE HOLE (BS 500)

DOUBLE HOLE IN FLOORBEAM BS 500 BL 0 WL 208.1. *S/D* REPAIRED DOUBLE HOLE AT BS 500, BL 0 WL 208.1 IAW FEDEX SRM 57-10-8.

Part: CHORD — CORRODED (BS 1342)

AREA OF CORROSION ON BS 1342 CHORD UPPER FWD RT FLANGE RBL 20. *S/D* REMOVED AND REPLACED UPPER CHORD IAW FEDEX DRAWING 65-17508.

Part: HINGE RIB — CRACKED (RT ELEVATOR)

RT ELEVATOR HINGE RIB AT HORIZONTAL STAB STATION 136.50 IS CRACKED ON THE I/B UPPER FLANGE. *S/D* REMOVED AND REPLACED ELEVATOR HINGE RIB SRM 27-30-0.

Part: STRINGER CLIP — CRACKED (BS 420)

DAMAGED STR CLIP BS 420 STR NR 4 LT. REMOVED AND REPLACED DAMAGED STR CLIP AT BS 420 STR 4 LT.

Part: THRESHOLD WEB — CORROSION (BS 527)

CORROSION (C53-111-01-2) ON DOOR THRESHOLD VERTICAL WEB AT BS 527 RBL 22 WL 156. WILL REQUIRE PARTIAL REMOVAL OF HORIZONTAL WEB AND STRAP. *S/D* REMOVED, FABRICATED AND INSTALLED VERTICAL AND HORIZONTAL WEB PER SRM 53-10-1.

Part: SHEAR WEB — CORRODED (BS 1173)

WHILE WORKING CARD NR 0583, FOUND BS 540 FLOOR BEAM, BL 0 WL 208 TO HAVE DOUBLE HOLE. *S/D* REPAIRED FLOOR BEAM AT BS 540, BL 0, WL 208 IAW FEDEX SRM 53-10-8.

Part: SKIN PANEL — CORROSION (BS 1108-1130)

BS 1110 STR 26 THERE IS BULGE IN SKIN TRIPLER DAMAGED OUT OF LIMITS. *S/D* REPLACED BONDED DOUBLER AT BS 1148 TO 1166 STR 25 TO 26 RIGHT. REPLACED BONDED TRIPLER FROM BS 1108 TO 1130 STR 25R TO 26R. REPAIRED REMAINING DEBONDED SKIN USING FIXED PATTERN PER FEDEX SRM 53-30-4 FROM BS 1110 TO 1183.

Part: NOSE CHORD — CORROSION (BS 312-324)

CORROSION (C53-111-01) ON UPPER NOSE CHORD BS 312 TO 324 RBL 15 WL 169. *S/D* REMOVED AND REPLACED UPPER NOSE CHORDS 294.5 TO BS 355 RBL 15 WL 169 IAW DRAWING NR 65-18415. WEB TO BE INSTALLED ON NR 0834 AT BS 294.5.

Part: CLIP — CORRODED (BS 380)

CORROSION (C53-111-01-1), STRINGER CLIP STR 24L BS 380. REMOVED AND REPLACED STR CLIP AT STR 24L BS 380.

Part: TE WEDGE — DELAMINATED (LT AILERON)

LT WING O/B AILERON T/E WEDGE HAS AN AREA OF DELAMINATION ON I/B LOWER SURFACE 6 INCHES BY 4 INCHES. REPAIRED LT WING O/B AILERON T/E WEDGE PER FEDEX SRM 51-80-04 SRM 51-40-06.

Part: SKIN — GOUGE (BS 688)

GOUGE IN SKIN AT STA 688 RBL 30 BETWEEN STR 24 AND 25R. REPAIRED GOUGE IN SKIN AT STA 688 RBL 30 BETWEEN STR 24 AND 25R IAW FEDEX SRM 53-30-3, 53-30-1.

Part: SKIN — CREASE (BS 365-390)

LARGE CREASE IN EXTERIOR SKIN BS 365 TO 390 STR 23R.

Part: SKIN — DELAMINATED (LT TE AFT FLAP)

LT WING O/B AFT FLAP HAS A 6 INCH BY 3 INCH DELAMINATED DENT ON LOWER SURFACE 30 INCHES FROM I/B END. REPAIRED DELAMINATION PER SRM 51-40-6.

Part: SHEAR WEB — CORRODED (BS 1173)

CORROSION (C53-224-01) ON SHEAR WEB AT BS 1173 RBL 27 WL 208. *S/D* REPAIRED SHEAR WEB PER SRM 51-40-2.

Part: SHEAR WEB — CORRODED (BS 1173)

CORROSION ON NOSE WHEEL WELL VERTICAL WEB BS 303 TO 309, WL 177, LBL 15 ON SHEAR WEB AT BS 1173 RBL 27 WL 208. *S/D* REMOVED CORROSION FOUND MATERIAL LOSS WAS WITHIN LIMITS PER SRM 53-10. TREATED AREA, PRIMED AND REINSTALLED FASTENERS REMOVED.

Part: FLOOR BEAM — CORROSION (BS 600)

CORROSION (C53-111-01, -2) ON LOWER FLANGE OF FLOOR BEAM IN NUTPLATE HOLES AT BS 600 LBL 20 TO RBL 26 WL 200. *S/D* REMOVED AND CORRODED AREA FROM LBL 17 TO RT SKIN FABRICATED AND INSTALLED REPAIR PARTS PER FDE SRM 53-10-18 FIG 2.

Part: FRAME — DENTED (BS 1090)

DENT IN FRAME BS 1090 BETWEEN STR 23 TO 24L LBL 47 WL 169. REMOVED DAMAGE, FABRICATED REPAIR ANGLE AND INSTALLED PER SRM 51-40-3.

Part: FLOOR BEAM — CORRODED (BS 640)

CORROSION (C53-111-01, -2) ON LOWER FLANGE OF FLOOR BEAM AT BS 640 LBL 23 TO RBL 26.7 WL 200. *(S/D)* REMOVED AND CORRODED ON LOWER FLANGE OF FLOOR BEAM IN NUTPLATE HOLES AT BS 640 LBL 23 TO RBL 26.7 WL 200. REPAIR PARTS PER FDE SRM 53-10-8.

Part: STRINGER — GOUGE (BS 400)

GOUGE IN STR BS 400 STR 16R. REPAIRED GOUGE IN STR BS 400 STR 16R PER FEDEX SRM 53-10-03 FIG 2.

Part: FLOOR BEAM — DOUBLE HOLE (BS 580)

WHILE WORKING CARD NR 0685, FOUND BS 580 FLOOR BEAM, BL 0 WL 208 TO HAVE DOUBLE HOLE. *S/D* REPAIRED DOUBLE HOLE PER SRM 53-10-8 SRM 53-10-8.

Part: FLOORBEAM — MISDRILLED (BS 990)

WHILE WORKING NR0754, FOUND DOUBLE HOLE IN BS 990 FLOORBEAM AT BL 0 WL 208.

Part: SHEAR WEB — CORRODED (BS 1174)

CORROSION EMANATING FROM UNDER NUTPLATES ON BOTTOM SIDE OF SHEAR WEB AT BS 1174 RBL 5, LBL 20 WL 208. *S/D* FABRICATED NEW WEB AND INSTALLED PER SRM 53-10-1.

Part: FLOORBEAM — MISDRILLED (BS 970)

WHILE WORKING NR0754, FOUND DOUBLE HOLE IN BS 970 FLOORBEAM AT BL 0 WL 208.

Part: FLOOR BEAM — DOUBLE DRILLED (BS 600)

WHILE WORKING CARD NR 0683, FOUND BS 600 FLOOR BEAM, BL 0 WL 208 TO HAVE DOUBLE HOLE. *S/D* REPAIRED FLOOR BEAM BS 600, BL 0, WL 208 IAW FEDEX SRM 53-10-8, HOLE PER SRM 53-10-8.

Part: STRINGER — GOUGED (BS 640)

WHILE WORKING NR0429, FOUND GOUGE ON STR NR 3 BS 640 RT.

Part: WEB — MECH DAMAGE (BS 560-580)

MECHANICAL DAMAGE AND MISDRILLED HOLES IN WEB AT BS 560 TO 580 LBL 41 WL 200.

Part: FRAME — CRACKED (BS 580)

THE FRAME AT BS 580 IS CRACKED ON I/B FLANGE AT RBL 67, WL 210. *S/D* THE FRAME AT BS 580, RBL 67, WL 210, WAS FOUND TO BE DAMAGED BEYOND LIMITS PER SRM 53-10-1. REPAIRED FRAME PER FEDEX SRM 51-40-3.

Part: TIE WEDGE — DELAMINATED (RT TE MIDFLAP)

RT WING I/B MIDFLAP TIE WEDGE HAS AN AREA OF DELAMINATION ON O/B END 12 INCHES BY 3 INCHES. REPAIRED DELAMINATION PER SRM 51-40-6.

Part: FRAME — DENTED (BS 1010)

DENT IN FRAME AT BS 1010 LBL 39 WL 153. FABRICATED PART AND REPAIRED FROM PER SRM 51-40-03.

Part: FRAME — DENTED (BS 1050)

DENT IN FRAME BS 1050 BETWEEN STR 25 TO 26L LBL 30 WL 153. REPAIRED DENT IN FRAME AT BS 1050 BETWEEN STR 25 TO 26L LBL 30 WL 153 PER FEDEX SRM 51-40-3 FIG 1.

Part: CHANNEL — CORROSION (BS 1157-1110)

CORROSION (C-53-111-01, -3) ON NR 2 CARGO DOORWAY C-CHANNEL BS 1057 TO 1110 RBL 27, WL 147. *S/D* REMOVED AND REPLACED C-CHANNEL AT DOORWAY.

Part: BONDING STRAP — CORROSION (NR 4 LE FLAP)

CORROSION (097-562-01-2) NR 4 RT FLAP BULLNOSE OB BONDING JUMPER UPPER ATTACH POINT AND TOOLING MARKS BS 950A, STR 7 RT AFT SIDE OF FRAME. *S/D* REMOVED CORROSION PER FEDEX SRM 57-50-3 AND 27-57-010.

Part: TIE WEDGE — DELAMINATED (RT TE MIDFLAP)

RT WING I/B MIDFLAP TIE WEDGE HAS AN AREA OF DELAMINATION ON O/B END 12 INCHES BY 3 INCHES.

Part: FLOORBEAM — CORRODED (BS 540)

CORROSION AT BS 540 FLOORBEAM LOWER CHORD FROM LBL 16 TO RBL 28 WL 200.

Part: SHEAR TIE — CORRODED (BS 970)

CORROSION (C53-111-01,3) ON SHEAR TIE AT BS 970 RBL 10.

Part: SKIN — CORROSION (BS 1080-1110)

CORROSION (C53-100-01-4), BS 1080 TO 1110 STR 26 LT AND RT. ALSO, DEEP GOUGES ON EXTERIOR SKIN. MECHANICALLY REMOVED CORROSION FROM EXTERIOR SKIN, BS 1080 TO 1110 STR 26 LT AND RT. FOUND A 1.5 INCH BY 1.5 INCH AREA AT STR 27L BS 1090 TO BE OUT OF LIMITS PER FEDEX SRM 53-30-1. ALL OTHER AREAS TO BE WITHIN LIMITS. REPAIRED SKIN AT BS 1091 STR 27L PER FEDEX SRM 53-30-3.

Part: SHEAR TIE — DAMAGED (BS 600)

MECHANISM DAMAGE ON SHEAR TIE AT BS 600 BETWEEN STR 16 TO 17R.

Part: FLOOR BEAM — CORRODED (BS 1110)

CORROSION (C53-111-01, -3) ON LOWER CHORD OF 1110 FLOOR BEAM WL 200 LBL 2 TO 30 AT NUTPLATE HOLES. *S/D* REMOVED AND REPLACED CORRODED LOWER CHORD AT BS 1110 FLOOR BEAM AT WL 200, RBL TO LBL 19.75 WITH FABRICATED REPAIR PARTS PER SRM 53-10-8 FIG 2 PER FEDEX EA 75310-27491.

Part: FRAME — GOUGE (BS 310)

FWD ENTRY DOOR LATCH ROLLER RIBS ON DOOR STRUCTURE. *S/D* REMOVED AND REPLACED FORWARD SIDE FRAME PER SRM 53-10-1.

Part: SKIN — DELAMINATION (LT TE AFT FLAP)

LEFT WING I/B AFT FLAP HAS AREA OF DELAMINATION ON I/B UPPER AND LOWER SKIN 18 INCHES BY 18 INCHES. REPAIRED DELAMINATION PER SRM 51-40-06.

Part: SKIN — CREASED (BS 366)

BS 366 STR 20R THERE IS A CREASE IN SKIN. *S/D* REPAIRED CREASE PER FEDEX SRM 53-03-3.

Part: SKIN — CREASE (BS 1120)

BS 1120 BETWEEN STR 17 TO 19L, THERE IS A CREASE IN SKIN. REMOVED DAMAGE, FABRICATED REPAIR PARTS AND REPAIRED PER SRM 53-30-3.