N482FE

Part: SHUTOFF VALVE — MALFUNCTIONED (LT A/C PACK) · airframe 46,527 hrs · 30,083 cycles

CLIMBOUT, HAD LESS THAN 2 PSID AT 10,000 MGL, LT AIR MIX VALVE WOULD NOT WORK, LT PACK WOULD NOT PRODUCE ANY AIR FOR PRESSURIZATION ON ENG 1 OR 2 BLEED. PRESSURIZED ACFT USING BOTH PACKS, EQUIPMENT COOLING AIR SHUTOFF VALVE DID NOT CLOSE BY 3 PSID. WRENCHED VALVE CLOSED AND PRESSURIZED ACFT TO 6.5 PSID USING GROUND AIR SOURCE. REPLACED COOLING AIR VALVE IAW MM 21-58-021-4. PRESSURIZED ACFT USING ENGINE BLEEDS 1 & 3 TO 7.5 PSID. ACFT MAINTAINED CURRENT CABIN ALTITUDE WITH 1 & 3 ENGINES AT IDLE AND SUPPLYING PNEUMATICS. BOTH PACK MIX VALVES WORKED NORMALLY DURING TEST. REPLACED LT FWD PACK SHUTOFF VALVE IAW MM 21-55-071-4, REQUIRES OPS AND LEAK CHECK.

Part: STRINGER — CORRODED (BS 720F-740 S27L) · corrosion level 2 · airframe 46,346 hrs · 29,925 cycles

CORROSION ON STRINGER 27L AT BS 720F TO 740. CUT OUT DAMAGED AREA OF STRINGER 27L AT BS 720F PLUS 9 INCHES IAW SRM 53-10-3 FIG 1. FABRICATED STRINGER SECTION FILLER AND SPLICE IAW SRM REV 103, 53-10-3 FIG 1 AND 53-10-2. INSTALLED STRINGER REPAIR IAW SRM 51-30-2 AND 53-10-3 FIG 1

Part: STRINGER — CORRODED (BS 720F S27R) · corrosion level 2 · airframe 46,346 hrs · 29,925 cycles

CORROSION ON STRINGER 27R AT BS 720F, PLUS 15 INCHES. CORROSION OUT OF LIMITS IAW SRM 53-10-1 FIG 7. CUT OUT DAMAGED AREA IAW SRM 53-10-3 FIG 1. FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 53-10-3 FIG 1 AND SRM 53-10-2 FIG 9.

Part: STRINGER SPLICE — CORRODED (BS 950 S27L) · corrosion level 2 · airframe 46,346 hrs · 29,925 cycles

CORROSION ON STRINGER SPLICE AT BS 950, STRINGER 27 LEFT. REMOVED DAMAGED SPLICE IAW SRM 51-30-2. FABRICATED SPLICE IAW SRM 51-20-1, REV 103, FIG 7 AND DWG 66-2521. INSTALLED SPLICE IAW SRM 51-30-2.

Part: STRINGER — DAMAGED (BS 570 S28L) · airframe 46,346 hrs · 29,925 cycles

FORWARD CARGO BAY WIRE BUNDLE STAND-OFF BRACKET BROKEN OFF AT BS 570, LBL 15. CUT OUT SECTION OF STRINGER 28L AT BS 570, 3 INCHES LONG IAW SRM 53-10-3 FIG 1. FABRICATED FILLER AND STRINGER REPAIR SECTION IAW SRM 53-10-3 FIG 1 REV 103. INSTALLED FILLER AND STRINGER REPAIR SECTION IAW SRM 53-10-3 FIG 1.

Part: SHEAR TIE — CORRODED (BS 970 S28-29L) · airframe 46,346 hrs · 29,925 cycles

CORROSION ON SHEAR TIE AT BS 970, BETWEEN STRINGER 28 AND 29 LEFT. CUT OUT SHEAR TIE IAW SRM 53-10-4 REV 103 FIG 15. FABRICATED SHEAR TIE REPAIR IAW SRM 53-10-4 FIG 15. INSTALLED IAW SRM 51-30-2.

Part: SHEAR TIE — CORRODED (BS 1050 S29-30R) · corrosion level 2 · airframe 46,346 hrs · 29,925 cycles

CORROSION ON SHEAR TIE AT BS 1050, BETWEEN STRINGER 30 AND 29R. CUT OUT DAMAGED AREA OF BS 1050 SHEAR TIE IAW SRM 53-10-4 FIG 15. FABRICATED SHEAR TIE REPAIR ANGLE IAW SRM 53-10-4 FIG 15 REV 103. INSTALLED REPAIR IAW SRM 51-30-2 AND 53-10-4 FIG 15.

Part: SHEAR TIE — CORRODED (BS 970 S29-30L) · corrosion level 2 · airframe 46,346 hrs · 29,925 cycles

CORROSION ON SHEAR TIE AT BS 970, BETWEEN STRINGER 29 AND 30 LEFT. REMOVED SECTION OF SHEAR TIE IAW SRM 53-10-4, FIG 15. FABRICATED SHEAR TIE REPAIR ANGLE IAW SRM 53-10-4 REV 103, FIG 15 AND 51-20-1 FIG 7 AND INSTALLED IAW SRM 51-30-2.

Part: STRINGER — CORRODED (BS 1050 S30) · corrosion level 2 · airframe 46,346 hrs · 29,925 cycles

CORROSION ON STRINGER 30, BS 1050. CUT OUT DAMAGED PORTION OF STRINGER 30 IAW B727 SRM 51-10-1 AND 53-10-3 FIG 1. FABRICATED STRINGER SECTION AND TWO SPLICES IAW SRM REV 103, 53-10-3 FIG 1. INSTALLED STRINGER REPAIR SECTION AND TWO SPLICES IAW SRM 53-10-3 FIG 1.

Part: STRINGER — CORRODED (BS 625 S27R) · corrosion level 2 · airframe 46,346 hrs · 29,925 cycles

CORROSION ON STRINGER 27R AT BS 625. REMOVED DAMAGED PORTION OF STRINGER IAW SRM 53-10-3 FIG 1 AND 51-10-1. FABRICATED STRINGER REPAIR SECTION IAW SRM 53-10-3 FIG 1. INSTALLED STRINGER REPAIR PARTS IAW SRM 51-30-2 REV 103 AND SRM 53-10-3 FIG 1.

Part: SHEAR TIE — CORRODED (BS 1010 S29-30R) · corrosion level 2 · airframe 46,346 hrs · 29,925 cycles

CORROSION ON SHEAR TIE AT BS 1010, BETWEEN STRINGER 30 AND 29R. CUT OUT DAMAGED SHEAR TIE 1" X 6" IAW SRM 53-10-4 FIG 15 REV 103. FABRICATED SHEAR TIE REPAIR ANGLE IAW SRM 53-10-2 FIG 5 AND 53-10-4 FIG 15. INSTALLED SHEAR TIE REPAIR ANGLE IAW SRM 53-10-4 FIG 15.

Part: SHEAR TIE — CORRODED (BS 950B S29-30L) · corrosion level 2 · airframe 46,346 hrs · 29,925 cycles

CORROSION ON SHEAR TIE AT BS 950B, BETWEEN STRINGER 30 AND 29L. CUT OUT DAMAGED AREA SHEAR TIE IAW SRM 53-10-4 REV 103, FIG 15. FABRICATED SHEAR TIE REPAIR ANGLE IAW SRM 51-20-1 FIG 7 AND 53-10-4 FIG 15 AND 53-10-2 FIG 5. INSTALLED SHEAR TIE REPAIR ANGLE IAW SRM 51-30-2 AND 53-10-4 FIG 15

Part: SKIN — DAMAGED (BS 1170 S27R) · airframe 46,346 hrs · 29,925 cycles

DAMAGED AND SHEARED FASTENERS STA 1170, STR 27R. CUT OUT DAMAGED SKIN AREA IAW SRM 53-30-3 FIG 24. FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 53-30-3 FIG 24 AND SRM 53-30-2 FIG 2.

Part: FRAME — WORN (BS 1030) · airframe 46,346 hrs · 29,925 cycles

AFT CARGO BAY, ELONGATED FASTENER HOLE IN UPPER FLANGE OF FRAME AT BS 1030, LBL 25. CUT OUT DAMAGED AREA OF FRAME 1/2" X7/8" IAW SRM REV 103 51-40-3 FIG 1. FABRICATED REPAIR DOUBLER FROM 7075-0,.063"X 14"X 4 1/2" IAW SRM 51-40-3 AND SRM 51-30-5 INSTALLED DOUBLER IAW SRM 51-30-2 REV 3

Part: INTERCOSTAL — BENT (E/E BAY) · airframe 46,346 hrs · 29,925 cycles

MAIN E/E BAY HATCH INTERIOR ENTRY AREA RT SIDE INTERCOSTAL BENT, FASTENER HEADS GOUGED BS 440, FROM CATCHING ON HATCH DURING OPERATION. REPAIRED DOUBLER IAW SRM 51-30-02, FABRICATED DOUBLER IAW SRM 51-40-2 FIG 1 AND 53-10-2 FIG 3 INSTALLED REPAIR IAW SRM 51-30-02

Part: BRACKET — CRACKED (L1 DOOR) · airframe 46,346 hrs · 29,925 cycles

L1 DOOR CUTOUT, STR 15L, SMALL BRACKET ATTACHED TO FORWARD DOOR STOP FITTING CRACKED, VIEWED FROM BOTTOM. REMOVED CRACKED BRACKET, FABRICATED AND INSTALLED NEW BRACKET IAW DWG 50-7946 REV K AND SRM 51-30-2.

Part: SKIN — GOUGED (BS 1087) · airframe 46,346 hrs · 29,925 cycles

SKIN GOUGED AND DENTED STA 1087 STR 24R. CUT OUT DAMAGED AREA IAW SRM 51-10-1 AND 53-30-3 FIG 3 FABRICATED REPAIR DOUBLER AND FILLER IAW SRM 53-30-3 FIG 3 AND 53-30-2 FIG 2 INSTALLED REPAIR DOUBLER AND FILLER IAW SRM 51-30-02

Part: WEB — CRACKED (BS 1227) · airframe 46,346 hrs · 29,925 cycles

AFT AIR STAIR AREA FWD LT LIGHTNING HOLE CRACKED, BS 1227. CUT OUT DAMAGED AREA OF L/H AFT TORQUE BOX VERTICAL WEB STA 1227, FABRICATED, AND INSTALLED REPAIR DOUBLER IAW B727 SRM 53-10-2 FIG 6 AND 51-40-2 FIG 1

Part: OIL SYSTEM — LEAKING (NR 1 ENGINE) · airframe 46,039 hrs · 29,683 cycles

NR 1 ENGINE LOST OIL QTY AND PRESSURE AT FL 320. ENGINE WINDMILLED FOR 30 MINS, OIL PRESSURE WAS ZERO. REMOVED AND REPLACED THE ENGINE

Part: SWITCH — INOPERATIVE (LE FLAPS) · airframe 45,806 hrs · 29,499 cycles

DURING FLAP RETRACTION FROM 5 DEG TO 2 DEG THE NR1 L/E FLAP IN TRANSIT LIGHT AND L/E FLAP YELLOW LIGHT REMAINED ILLUMINATED. NO ASSYEMETRY NOTED IN FLIGHT CONTROLS. NR 1 L/E FLAP, IAW MM REF 27-82-000-1, NO HELP. NEED POSITION SWITCH. PHL U TRIED JUMPER OF NR 1 L/E FLAP SWITCH NO HELP. R & R NR1 L/E FLAP POSITION INDICATING SWITCH IAW AMM 27-82-00. 1-4 SYS CK`S NORMAL. (CLOSED)

Part: SLIDE — LOW PRESSURE · airframe 45,524 hrs · 29,285 cycles

ESCAPE SLIDE READS 2300 WHICH IS UNDER THE LIMIT FOR THIS TEMP. R & R EMERGENCY ESCAPE SLIDE IAW MM 25-60-015-2. OPS NORMAL.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 45,223 hrs · 29,051 cycles

RIGHT EMERGENCY EXTERIOR SLIDE LIGHT INOPERATIVE. REMOVED AND REPLACED EMER EXIT LIGHT POWER SUPPLY AND TESTED IAW AMM 33-50-051-2-0. OPS CHECKS GOOD. OK FOR SERVICE.

Part: SWITCH — FAILED (SLATS) · airframe 45,192 hrs · 29,029 cycles

NR 6 LED FAILED TO RETRECT. NR 6 SLAT EXTEND LIGHT ON SO'S PANEL REMAINS ON AT ALL FLAP POSITIONS. WITH THE NR 6 SLAT CONNECTOR PLUG DISCONNECTED THE EXTEND LIGHT WILL EXTINGUISH. WITH THE JUMPER WIRE INSTALLED THE RETRACT REMAINS ON AT ALL FLAP SETTINGS AGAIN. REPLACED THE NR 6 L/E SLAT EXTEND SWITCH IAW MM 27-82-011-4-0. OPS CHECK GOOD. OK TO CONTINUE. (CLOSED)

Part: HOSE — LEAKING (HYD SYSTEM) · airframe 45,035 hrs · 28,924 cycles

CLIMBING THRU 16,000 FT NOTICED SYS A HYD QTY WAS ZERO, SHORTLY AFTER SYS PRESSURE WENT TO ZERO & BOTH LOW PRESSURE LIGHTS CAME ON. PERFORMED STABILIZER & QRH SYS A LEAK OR LOSS CHECKLIST, PERFORMED MANUAL GEAR EXTENTION & ALT MASTER FLAP EXTENTION. LANDED 16R AFW. TROUBLESHOT & FOUND PRESSURE HOSE FOR LOWER RUDDER PACK HAD A HOLE FROM CHAFING ON BRACKET JUST ABOVE LWR RUDDER PACK, R & R BOTH PRESSURE & RETURN HYD LINES FOR LWR RUDDER PACK, R & R NR 1 ENG SYSTEM A ENGINE DRIVEN HYD PUMP PER M/M 29-11-033-4 R & R NR 1 ENG SYS A HYD PUMP CASE DRAIN FILTER PER MM 29-11-041-2 R & R ENG SYS A ENG DRIVEN HYDPUMP PER MM 29-11-033-4, R & R NR 2 ENG SYSTEM A HYD PUMP CASE DRAIN FILTER PER MM 29- 11-041-2 & R & R SYSTEM A HYD RETURN FILTER PER M/M 29-11-102-2 LEAK & OPS CHECK PER MM 29-11-033-4 NO LEAKS NOTED RAN ENG PER J.R.H OPS CHECK NORMAL NR 1 & 2 ENG HYD PUMPS 3000 PSI NO LEAKS. LEAKED CHECK LOWER RUDDER HYD PRESSURE & RETURN LINES NO LEAKS A/C OK TO CONTINUE SERVICE. LEAK CHECKED NR 1 & 2 ENG CASE DRAIN FILTER HOUSING NO LEAKS.

Part: INDICATOR — INOPERATIVE (FUEL QTY) · airframe 44,967 hrs · 28,863 cycles

AIRCRAFT VERY DIFFICULT TO TRIM PROPERLY. REQUIRED OVER 2 UNITS OF LEFT AILERON TRIM, AND OVER 1 UNIT OF L RUDDER TRIM. NR 1 FUEL TANK GAUGE INOP, WAS FUELED TO A KNOWN QTY. A FUEL IMBALANCE COULD HAVE BEEN PART OF THE PROBLEM THOUGH WE COULD NOT TELL. WHEN ACFT ARRIVED AT SGF, NR 1 FUEL QTY INDICATOR WAS DEFERRED AND THE TANK WAS EMPTY, COMPARED TO NR 3 TANK, WHICH HAD A QTY OF 5900 LBS RESULTING IN A FUEL IMBALANCE OF APPROX 5900 LBS AND TRIM PROBLEM. A/C OK FOR SERVICE.

Part: RIB — CRACKED (NR 8 SLAT) · airframe 44,911 hrs · 28,829 cycles

NR 8 SLAT SECOND RIB FROM INBD END IS CRACKED WING STA 355.4. REMOVED DAMAGED RIB, INSTALLED NEW RIB PN 65-17321-4 IAW SRM 51-30-2.

Part: FRAME — CORRODED (BS 990 S29R) · corrosion level 2 · airframe 44,911 hrs · 28,829 cycles

AFT CARGO STATION 990 STUB FRAME CORRODED AT STR 29R. CUT OUT DAMAGED AREA IAW SRM 53-10-4 FIG 15 AND 51-10-1. FABRICATED DOUBLER, ANGLE AND SHIM IAW SRM 53-10-4 FIG 15. INSTALLED REAIR PARTS IAW SRM 51-30-2.

Part: WEB — CRACKED (TORQUE BOX) · airframe 44,911 hrs · 28,829 cycles

CRACK NOTED - RIGHT HAND LOWER TORQUE BOX WEB, RBL 20.5 AT BS 1223. UPPER LIGHTING HOLE, FORWARD OF PREVIOUS REPAIR RIVET LINE. REMOVED PREVIOUS REPAIR DOUBLER AT BS 1223, RBL 20.5 IAW SRM 51-30-2. ROUTED OUT DAMAGED AREA IAW SRM 51-10-1. FABRICATED NEW REPAIR DOUBLER IAW SRM 51-40-2 AND 53-10-2. TREATED AND PRIMED DOUBLER IAW SRM 51-10-2. INSTALLED DOUBLER IAW SRM 51-30-2, REV. 102.

Part: SHEAR TIE — CORRODED (BS 1110 S27L) · corrosion level 2 · airframe 44,911 hrs · 28,829 cycles

AFT CARGO STATION 1110, STRINGER 27L, SHEAR TIE CORRODED. REMOVED SHEAR TIE TEE ANGLE AT BS 1110, STR 27L IAW SRM, REV 102, 51-30-2. FABRICATED REPLACEMENT SHEAR TIE FROM PM60-5632, 7075-T6511, 4.5" LONG IAW DRAWING NR. 65-16346 REV P. INSTALLED SHEAR TIE IAW SRM 51-30-2.

Part: FLOORBEAM — DAMAGED (BS 1110) · airframe 44,911 hrs · 28,829 cycles

ELONGATED HOLE MAIN CABIN FLOOR BEAM BS 1110 LBL 45. CUT OUT DAMAGED AREA IAW SRM 53-10-8 FIG 8. FABRICATED 2 ANGLE REPAIRS. IAW SRM 53-10-8 FIG. 8. FABRICATED 2 SHIMS. IAW SRM 53-10-8. FABRICATED CHANNEL. FABRICATED FILLER IAW SRM 53-10-8, 51-10-3, AND 51-20-1. HEAT TREATED REPAIR ANGLES TO T6 CONDITION IAW FASI ER 2-37153-801 REV A. INSTALLED ANGLES AND PARTS REPAIR IAW SRM 53-10-8 FIG 8.

Part: FLOORBEAM — CORRODED (BS 1070) · corrosion level 2 · airframe 44,911 hrs · 28,829 cycles

AFT CARGO STATION 1070, BOTTOM OF FLOORBEAM, CORROSION AROUND SCREW HOLES. RBL 12-45. CUT OUT 2 DAMAGED AREAS IAW SRM 53-10-8 FIG 8. FABRICATED 2 REPAIR ANGLES AND 2 FILLERS IAW SRM 53-10-8 FIG 8. HEAT TREATED ANGLES TO T6 CONDITION IAW FASI ER 2-37153-801 REV A. INSTALLED REPAIR PARTS IAW SRM 51-30-2.

Part: SKIN — DAMAGED (LOWER FUSELAGE) · airframe 44,911 hrs · 28,829 cycles

EVALUATE TRIM OUT EXTERIOR FUSELAGE LAP SEAM BS 178 STR 18R CUT OUT DAMAGE ON UPPER SKIN 2" X 2 1/8" AND REMOVED FASTENERS COMMON TO REPAIR DOUBLER IAW EA 7-5330-135526, FABRICATED REPAIR PARTS, DOUBLER AND FILLER USING 2024-T3, 0.071" PO NR 9009068 DIMENSION S 7 1/8" X 6 5/8" IAW EA NR 7-5330- 135526 FIG 1 AND INSTALLED DOUBLER AND FILLER REPAIR IAW SRM 51-30-2, REV 102, AND EA NR 7-5330-135526 FIG 1. FABRICATED FILLER FROM .063" X 7 1/2" X 5 1/8", PO NR 9009134, 2024-T3.

Part: SKIN — CHAFED (LT ELEVATOR) · airframe 44,911 hrs · 28,829 cycles

LT ELEVATOR INSIDE NR 5 BALANCE BAY, GOUGE ON UPPER PANEL, OTBD END. REMOVED DAMAGE BY STOP DRILLING GOUGE ON UPPER PANEL INSIDE NR 5 BALANCE BAY FOR LT ELEVATOR IAW SRM 51-10-1, REV 102. COMPLIED WITH HFEC INSP IAW NDTM 51-00-00, FIGURE 23, WITH NO DEFECTS NOTED. FABRICATED REPAIR DOUBLER USING 2024-T3, .032" X 4 3/4" X 6" IAW SRM 55-20-3 FIGURE. INSTALLED DOUBLER IAW SRM 55-20-3 FIG 3.

Part: FLOORBEAM — CORRODED (BS 560) · corrosion level 2 · airframe 44,911 hrs · 28,829 cycles

CORROSION FLOORBEAM MAIN CABIN BS 560, LBL10 CUT-OUT DAMAGED AREA IAW SRM 53-10-8 FIG 3, FABRICATED CHORD FAB 2 EA SUPPORT ANGLES, FAB 2 EA REINFORCEMENT STRAP IAW SRM 53-10-8 FIG REV 102, INSTALLED FLOORBEAM REPAIR AT BS 560 LBL 10 IAW SRM 51-30-2 REV 102.

Part: SKIN — CRACKED (INBD FOREFLAP) · airframe 44,911 hrs · 28,829 cycles

RT INBD FORE FLAP, STA 224, CRACK ON THE SKIN, L/E, FWD OF ATTACH FITTING. CUT OUT DAMAGED AREA IAW SRM 57-50-4 FIG 1. FABRICATED DOUBLER AND FILLER IAW SRM 57-50-4 FIG 1. INSTALLED DOUBLER AND FILLER IAW SRM 51-30-2.

Part: ANGLE — CRACKED (BS 1263) · airframe 44,911 hrs · 28,829 cycles

AFT AIRSTAIRS RT LOWER TORQUE BOX TEE ANGLE CRACKED AT BS 1263, AFT SIDE. REMOVED RT LOWER TORQUE BOX TEE ANGLE IAW SRM, REV 102, 51-30-2. LOCATED, DRILLED AND DEBURRED HOLES ON NEW TEE ANGLE IAW SRM 51-30-5. INSTALLED NEW TEE ANGLE IAW SRM 51-30-2.

Part: FLOORBEAM — CORRODED (BS 328) · airframe 44,911 hrs · 28,829 cycles

FWD LAV AREA - CORROSION ON FLOOR SUPPORT ANGLE AT BS 328 FROM BL 0 TO LBL 55, UPPER AND LOWER SURFACES. CUT OUT DAMAGED AREA APPROX DIM 2" IAW SRM 53-10-8 FIG 9. FABRICATED REPAIR FLOORBEAM. FABRICATED ANGLES 2. FABRICATED 2 ANGLES IAW SRM 53-10-8 FIG 9. INSTALLED REPAIR PARTS ON FLOORBEAM IAW SRM 53-10-8 FIG 9.

Part: STRUCTURE — CRACKED (LT WING TE FLAP) · airframe 44,911 hrs · 28,829 cycles

LT INBD MID FLAP LOWER AFT CLOSE OUT CHORD WBL 106 IS CRACKED AT ACT ROD CUTOUT. CUT OUT DAMAGED SECTION DIM 47 1/4 " LONG IAW SRM 51-40-4 FIG 1. FABRICATED LOWER CHORD AND SPLICE IAW SRM 51-40-4 FIG 4. LOCATED AND DRILLED HOLES IAW SRM 51-30-5. INSTALLED LOWER CHORD IAW SRM 51-30-2.

Part: SEAT TRACK — CORRODED (BS 690-720E) · airframe 44,911 hrs · 28,829 cycles

CORROSION SEAT TRACK NUMEROUS AREAS MAIN CABIN BS 690 TO BS 720E 10 INCHES, RBL 45. REMOVED SEAT TRACK SECTION IAW SRM 51-30-2. FABRICATED NEW SEAT TRACK, FABRICATED ANGLE SPLICES AND STRAP SPLICES IAW SRM 53-10-5 FIG 1. TREATED AND PRIMED REPAIR PARTS IAW SRM 51-10-2. INSTALLED REPAIR PARTS IAW SRM 51-30-2.

Part: DOOR FRAME — CRACKED (RT OVERWING EXIT) · airframe 44,911 hrs · 28,829 cycles

BS 783, RT OVERWING FRAME, STR 17R, CRACK ORIGINATING FROM FASTENER HOLE. STOP DRILLED CRACK, FABRICATED REPAIR ANGLE, STRAP, SPLICE ANGLE, NEW CHANNEL, AND INSTALLED REPAIR PARTS IAW SRM 51-10-1, SRM 51-30-2, SRM 51-30-5, SRM 51-10-2, ER NR 2-37153-0801 REV A, MFG DWG NR 65C36280 AND EO 7-5310-7-3367 B4 TA4.

Part: WEB — CRACKED (BS 1223) · airframe 44,911 hrs · 28,829 cycles

AFT AIRSTAIR RT LOWER TORQUE BOX WEB IS CRACKED AT LOWER LIGHTING HOLE BS1223. STOP DRILLED CRACK AT RT LOWER LIGHTING HOLE IAW SRM 51-10-1 AND 51-40-2 FIG 1. HFEC INSP IAW NDTM PT6 51-00-00 FIG 23 VERIFIED CRACK ENDS AT STOP DRILL. FABRICATED NEW DOUBLER IAW SRM 53-10-2 FIG 6 AND 51-40-2 FIG 1. INSTALLED NEW DOUBLER IAW SRM 51-30-2 AND 51-40-2 FIG. 1, REV 102.

Part: SUPPORT ANGLE — CRACKED (BS 1263) · airframe 44,911 hrs · 28,829 cycles

AFT AIRSTAIR RT LOWER TORQUE BOX, SUPPORT ANGLE IS CRACKED AT FASTENER, BS 1263, ON AFT SIDE. REMOVED RT LOWER TORQUE BOX SUPPORT ANGLE IAW SRM, REV 102, 51-30-2. FORMED SUPPORT ANGLE IAW DWG NR 65-17517. HEAT TREATED GUSSET TO T-6 CONDITION IAW ENGINEERING REPORT NR 2-37153-801 REV A. INSTALLED GUSSET IAW SRM, REV. 102, 51-30-2 AND DWG NR 65-17517 REV F.

Part: SUPPORT ANGLE — CRACKED (BS 1263) · airframe 44,911 hrs · 28,829 cycles

AFT AIRSTAIR RT LOWER TORQUE BOX, SUPPORT ANGLE HAS CRACK INDICATION AND WORKING FASTENERS. BS 1263, FWD SIDE. REMOVED RT TORQUE BOX WEB DOUBLER FROM BS1243 TO 1283 IAW SRM, REV 102, 51-30-2. CUT WEB AT BS 1263 IAW SRM 51-10-1. REMOVED RT LOWER TORQUE BOX ANGLE IAW SRM 51-30-2. LOCATED, DRILLED AND DEBURRED HOLES IN NEW ANGLE IAW SRM 51-30-5. INSTALLED NEW ANGLE, TORQUE BOX WEB AND DOUBLER IAW SRM 51-30-2.

Part: WEB — CRACKED (BS 1243) · airframe 44,911 hrs · 28,829 cycles

AFT AIRSTAIR RT LOWER TORQUE BOX WEB IS CRACKED AT UPPER LIGHTING HOLE BS 1243. STOP DRILLED CRACK AT LOWER RIGHT LIGHTING HOLE IAW SRM 51-10-1 AND 51-40-2. COMPLIED WITH HFEC INSPECTION IAW NDTM PT6 51-00-00, FIG. 23, AND VERIFIED CRACK ENDS AT STOP DRILL. FABRICATED NEW DOUBLER, IAW SRM 51-40-2 AND 53-10-2 FIG. 6. INSTALLED NEW DOUBLER IAW SRM 51-30-2 AND 51-40-2 FIG. 1, REV 102.

Part: FLOORBEAM — CORRODED (BS 1070) · corrosion level 2 · airframe 44,911 hrs · 28,829 cycles

AFT CARGO, BL 0 FLOORBEAM REPAIR, SCREW HOLES CORRODED, 3EA AT RBL5, STA 1070. REMOVED FLOORBEAM REPAIR LOWER STRAP IAW SRM 51-30-2. FABRICATED NEW STRAP IAW SRM 53-10-8 FIG 2. TREATED AND PRIMED NEW STRAP IAW SRM 51-10-2 INSTALLED NEW STRAP IAW SRM 53-10-8 FIG 2 REV 102.

Part: SUPPORT ANGLE — CRACKED (BS 1250) · airframe 44,911 hrs · 28,829 cycles

AFT AIRSTAIR LT LOWER TORQUE BOX, SUPPORT ANGLE IS CRACKED AT RIVET, BS 1250. REMOVED SUPPORT ANGLE FROM AFT AIRSTAIR LT LOWER TORQUE BOX AT BS 1250 IAW SRM, REV 102, 51-30-2. FABRICATED SUPPORT ANGLE IAW DWG NR 65-17516 AND BAC 1517-1457. INSTALLED SUPPORT ANGLE IAW SRM 51-30-2 AND DWG NR 65-17516.

Part: STRINGER — CORRODED (BS 1170 S26R) · corrosion level 2 · airframe 44,911 hrs · 28,829 cycles

AFT CARGO ATA 1170, STR 26R CORRODED. REMOVED DAMAGED SECTION OF STRINGER IAW SRM 51-10-1, REV. 102. FABRICATED STRINGER AND SPLICE IAW SRM 53-10-3 FIG. 1 DETAIL 1. INSTALLED STRINGER SECTIONS AND SPLICE IAW SRM 53-10-3 FIG. 1, DETAIL 1 AND 51-30-2.

Part: SILL — DAMAGED (BS 520 S2L) · airframe 44,911 hrs · 28,829 cycles

DOUBLE DRILLED HOLES FOUND MCD UPPER FWD INBD SILL BS 520 STR 2L. R & R MAIN CARGO DOOR FWD IB SILL AT BS 442055 TO BS 570.5 IAW DWG NR 53FX1475, SRM 51-30-5, SRM 51-10-2, AND SRM 51-30-2.

Part: WEB — DAMAGED (BS 1260) · airframe 44,911 hrs · 28,829 cycles

AFT AIRSTAIRS RT LOWER TORQUE BOX WEB, LIGHTING HOLE ROUTE OUT IS GREATER THAN .100 INCH, BS 1230. FABRICATED NEW DOUBLER IAW SRM 53-10-2, FIG 6 AND 51-40-2 FIG 1. INSTALLED NEW DOUBLER IAW SRM 51-30-2 AND 51-40- 2 FIG 1, REV 102.

Part: STRINGER — CORRODED (BS 1030 S26R) · corrosion level 2 · airframe 44,911 hrs · 28,829 cycles

AFT CARGO STA 1030, STR 26R CORRODED. REMOVED 2" SECTION OF DAMAGED STRINGER AND FABRICATED FILLER AND STRINGER REPAIR SPLICE IAW SRM 53-10-2 FIGURE 9 AND 53-10-3 FIGURE 1 DETAIL 1. INSTALLED SPLICE AND FILLER IAW SRM 51-30-2, REV. 102.

Part: SKIN — GOUGED (ZONE 100) · airframe 44,911 hrs · 28,829 cycles

EVALUATE EXTERNAL SKIN REPAIR BS 360, STR 17L, DIM: 25 1/2 X 20 IAW EO 7-5100-7-5005, PT1. REMOVED PREVIOUS REPAIR DOUBLER, HFEC AND AND UT INSP IAW NDTM 51-00-00 AND FOUND SKIN GOUGED, CUT OUT DAMAGED AREA IAW SRM 51-10-1, HFEC INSPECTED. CUTOUT AND HOLES WITH NO DEFECTS NOTED IAW NDTM 51-00-00, FABRICATED SKIN USING 2024T-3 .050 30" X 44" PO NR 2907450 AND FILLER USING 2024T-3 .032 30" X 44" PO NR 9007927 AND SPLICE USING 2024T-3 .063 8.5" X 44" PO NR 9009208 IAW SRM 53-30-3 FIG 12, FABICATED DOUBLER USING 2024T-3 .080 28.75" X 27.25" PO NR 9008686 AND 2 EACH FILLERS USING 2024T- 3 .071 10" X 7.75" PO NR 9008655, 1 FILLER 1" ROUND USING 2024T-3 .071 PO NR 9008655 AND INSTALLED ALL PARTS IAW EA 7-5330-135528.

Part: ATTACH BRACKET — CRACKED (LT WING) · airframe 44,911 hrs · 28,829 cycles

LT WING L/E CAVITY, BOTH INBD AND OTBD NR 1 SLAT ACTUATOR ATTACH BRACKETS HAVE INSIDE PLATES CRACKED. REMOVED INBOARD AND OUTBOARD ATTACH BRACKETS IAW SRM, REV 102, 51-30- 2. FABRICATED 2 ATTACH BRACKETS FOR NR 1 SLAT ACTUATOR, IAW SRM 51-20-1 FIGURE 7 AND 51-10-3. INSTALLED NEW BRACKETS IAW SRM 51-30-2.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,911 hrs · 28,829 cycles

CORROSION AND CRACKED SEAT TRACK MAIN CABIN BS 510-690 LBL 25. REMOVED SEAT TRACK SECTION, FABRICATED NEW SEAT TRACK SPLICE REPAIR AND DRILLED AND LOCATED SEAT TRACK, INSTALLED SEAT TRACK, INSTALLED SEAT TRACK SPLICE REPAIR IAW SRM 51-30-2, 51-30-5, 53-10-5 FIG 1.

Part: SEAT TRACK — CRACKED (ZONE 100) · airframe 44,911 hrs · 28,829 cycles

CRACKED SEAT TRACK MAIN CABIN BS 950D RBL 25. REMOVED SEAT TRACK AND SPLICE, FABRICATED SEAT TRACK REPAIR AND SPLICE REPAIR. INSTALLED IAW SRM 53-10-2, FIG 7A AND SRM 53-10-5 FIG 1, 51-30-5, 51-30-2. TREATED AND PRIMED REPAIR PARTS PRIOR TO INSTALLATION IAW SRM 51-10-2.

Part: HINGE FITTING — CRACKED (CARGO DOOR) · airframe 44,911 hrs · 28,829 cycles

CRACK & GOUGED LOBE MCD HINGE SUPPORT FUSELAGE SIDE FWD NR 1. REMOVED DAMAGED HINGE SECTIONS, FABRICATED NEW HINGE SECTIONS USING 5212791. PO NR 29146119 DIMS 45.75" AND 20.1250" AND INSTALLED IAW DWG 52FX1433 REV E.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,911 hrs · 28,829 cycles

CORROSION SEAT TRACK BS 690-530 LBL 45. REMOVED SEAT TRACK IAW SRM 51-30-2. FABRICATED SEAT TRACK IAW SRM 53-10-5 FIG 1 FABRICATED 2 SEAT TRACK SPLICES IAW SRM 53-10-5 FIG 1 LOCATED AND DRILLED SEAT TRACK IAW SRM 51-30-5. INSTALLED SEAT TRACK AND SPLICES IAW SRM 51-30-2.

Part: SEAT TRACK — CRACKED (ZONE 100) · airframe 44,911 hrs · 28,829 cycles

CRACK SEAT TRACK MAIN CABIN BS 950D BL 0. REMOVED SECTION SEAT TRACK IAW SRM 51-30-2, FABRICATED NEW SECTION SEAT TRACK, & STRAPS IAW SRM 53-10-5, FIG 1. TREATED AND PRIMED NEW PARTS IAW SRM 51-10-2 AND INSTALLED NEW REPAIR PARTS IAW SRM 51-30-2.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,911 hrs · 28,829 cycles

CORROSION SEAT TRACK BS 600-BS 720 BL 0. REMOVED SEAT TRACK SECTION IAW SRM 51-30-2. FABRICATED SEAT TRACK IAW SRM 53-10-5 FIG 1. INSTALLED SEAT TRACK IAW SRM 51-30-2.

Part: HINGE BRACKET — WORN (CARGO DOOR) · airframe 44,911 hrs · 28,829 cycles

EXCESSIVE PLAY 6 EA HINGE SUPPORT ASSY MCD FUSELAGE ATTACHMENT TOP AFT NR 7. REMOVED DAMAGED HINGE SECTION UPPER AND LOWER, FABRICATED NEW HINGE SECTIONS. UPPER AND LOWER, INSTALLED NEW HINGE SECTIONS AT MAIN CARGO DOOR AFT SIDE. UPPER AND LOWER IAW MM 51-30-2, DWG NR 52FX1433 REV E., MM 20-80-001-2 AND 52-34-000-4.

Part: FLOORBEAM — CORRODED (BS 1110) · corrosion level 2 · airframe 44,911 hrs · 28,829 cycles

CORROSION FLOORBEAM MAIN CABIN BS 1110, RBL12. CUTOUT DAMAGED FLOORBEAM DIM: 1.9" X 2" IAW SRM 53-10-8, FIG 3 FABRICATED FLOORBEAM REPAIR, SUPPORT ANGLE, AND STRAP IAW SRM 53-10-3 FIG 3. TREATED AND PRIMED REPAIR PARTS IAW SRM 51-10-2. INSTALLED REPAIR PARTS AT BS 1110 RBL 12 IAW SRM 51-30-2 & SRM 53-10-8, FIG 3.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,911 hrs · 28,829 cycles

CORROSION AND CRACKED SEAT TRACK MAIN CABIN FLOOR BS 950 PLUS 10" IN - BS 950D. REMOVED SECTION SEAT TRACK IAW SRM 51-30-2. FABRICATED SEAT TRACK, STRAP AND 2 ANGLES IAW SRM 53-10-5 FIG 1. TREATED AND PRIMED NEW REPAIR PARTS IAW SRM 51-10-2 AND INSTALLED REPAIR PARTS IAW SRM 51-30-2 & SRM 53-10-5 FIG 1.

Part: SILL — CRACKED (BS 490 S3-4L) · airframe 44,911 hrs · 28,829 cycles

MAIN CARGO DOOR UPPER SILL, STA 490, BETWEEN STR 3L AND 4L. CRACKS ORIGINATING FROM 2 FASTENER HOLES. R & R UPPER OTBD SILL AT BS 442.65 TO BS 570.5 AND REPAIRED ADDITIONAL OPEN HOLES IN SKIN IAW EA 7-5310-135527 AND SRM 51-10-1, 51-30-2, 51-30-5 AND 51-10-2.

Part: SKIN — GOUGED (NR 7 SLAT) · airframe 44,911 hrs · 28,829 cycles

RT WING NR 7 SLAT T/E BOTTOM SIDE GOUGED INBD OF SLAT HOOK WS 639. BLENDED OUT GOUGE AT NR 7 SLAT T/E WS 639, FOUND BLEND OUT OF LIMITS, FABRICATED REPAIR DOUBLER & INSTALLED REPAIR DOUBLER IAW SRM 51-30-2, SRM 57-50-1 FIG 2, SRM 57-50-3 FIG 10 & SRM 51-10-2.

Part: SHEAR TIE — CORRODED (BS 720A) · corrosion level 2 · airframe 44,911 hrs · 28,829 cycles

FWD PIT - CORROSION ON SHEAR TIE AT BS 720A, FWD SIDE, BETWEEN STRINGERS 28R AND 27R. REMOVED DAMAGED SECTION OF SHEAR TIE 1"X5 7/8" IAW SRM 51-10-1. FABRICATED SHEAR TIE FROM 7075-T6, .063" X 2 1/4"X 5 7/8" IAW B727 SRM 53-10-4 FIG 15 AND 53-10-2 FIG 3. INSTALLED SHEAR TIE IAW SRM 51-30-2, BETWEEN STR 27RT-28RT AT BS 720A REV 102.

Part: SHEAR TIE — CORRODED (BS 540 S28L/R) · airframe 44,911 hrs · 28,829 cycles

FWD PIT - CORROSION ON SHEAR TIE AT BS 540, BETWEEN STRINGERS 28L AND 28R. REMOVED CORROSION IAW SRM, REV 102, 51-10-6. UT INSPECTED AREA IAW NDTM 51-00-00, FIGURE 3, PART 4. ORIGINAL THICKNESS OF .046", MATERIAL LOSS OF .001", MATERIAL REMAINING .045". AREA FOUND TO BE WITHIN LIMITS IAW SRM 53-10-1.

Part: STRUCTURE — CRACKED (NR 5 SLAT) · airframe 44,911 hrs · 28,829 cycles

RT WING NR 5 SLAT T/E CRACKED, WS 400. ROUTED OUT DAMAGED EDGE AT RT WING NR 5 SLAT T/E IAW SRM 51-10-1, COMPLIED WITH HFEC INSP IAW NDTM 51-00-00 WITH NO CRACK NOTED, AREA FOUND TO BE WITHIN LIMITS IAW DWG SR27-57-046 AND SRM 57-50-1.

Part: SKIN — CRACKED (NR 8 SLAT) · airframe 44,911 hrs · 28,829 cycles

RT WING NR 8 SLAT OTBD STOP PAD INBD SIDE SKIN CRACKED IN RADIUS OF SLAT SKIN, SLAT STA 760. REMOVED LOWER CHORD FROM NR 8 SLAT IAW SRM, REV 102, 51-30-2. FABRICATED NEW LOWER CHORD IAW SRM 57-50-2 FIG. 2, AND 51-30-5. INSTALLED LOWER CHORD IAW SRM 51-30-2.

Part: ANGLE — CRACKED (RT WING) · airframe 44,911 hrs · 28,829 cycles

CRACKED CHORD ANGLE, RT WING FALSE SPAR AT NR 8 SPOILER ACTUATOR ATTACH FITTING. REMOVED DAMAGE BY CUTTING OUT WEB AND CHORD IAW FED EX B727 DRAWING NUMBER SR27-57-038 REV C. FABRICATED 2 REPAIR ANGLES, LOWER CHORD, DOUBLER , STRAP, WEB, & 2 RADIUS FILLERS IAW DRAWING NUMBER SR27-57-038 REV C. INSTALLED RADIUS FILLERS, CHORD, SPLICE ANGLES, DOUBLER, STRAP AND WEB IAW DRAWING NUMBER SR27-57-038 REV C.

Part: COMPRESSOR — STALLED (NR 1 ENGINE) · airframe 44,896 hrs · 28,819 cycles

CLIMBING THROUGH 16,000 FT VERY LOUD "THUMP" WITH ASSOCIATED AIRFRAME SHUDDER. COMPLIED WITH QRH ENGINE COMPRESSOR STALL/LIMIT/SURGE AND RETURNED TO DEPARTURE. DID A WALK AROUND OF AFT. NO AIRFRAME DAMAGED NOTED. ALL CONTROL SURFACES ACCOUNTED FOR. R & R NR 1 ENG ASSY LEAK AND OPS CKS NORMAL.

Part: BULKHEAD — CRACKED (ZONE 100) · airframe 44,325 hrs · 28,334 cycles

NOSE LANDING BULKHEAD STA NR 351.2 HAS 3 CRACKS MIGRATING FROM 1 FASTENER HOLE ATTACHING THE NOSE GEAR LOCK ACTUATOR FITTING TO BULKHEAD. TRIMMED CRACKS, INSTALLED REPAIR DOUBLER FABRICATED FROM 7075 T6 0.100.BATCH NR 1338161.

Part: ACTUATOR — MALFUNCTIONED (NLG) · airframe 44,325 hrs · 28,334 cycles

AFTER PLACING LANDING GEAR LEVER IN DOWN POSITION NOSE GEAR RED LIGHT REMAINED ON AND GREEN NOSE GEAR LIGHT DID NOT COME ON. DID A MANUAL GEAR EXTENSION AND GOT PROPER DOWN AND LOCKED INDICATION. FOUND NLG LOCK HYD ACTUATOR FITTING CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-30-2 AND SRM 51-10-1 PARA 9A. PERFORMED OPS CHECK AND LEAK CHECK IAW MM 32-33-011-4. PERFORMED NLG STEERING OPS CHECK IAW MM 32-51-000-5. REMOVED AND REPLACED NLG LOCK ACTUATOR AND REMOVED AND REPLACED NLG LOCK ACTUATOR SPRING BUNGEE. REMOVED AND REPLACED EXTENSION AND RETRACTION HYD TUBES. MINOR REPAIR.

Part: MUFFLER — FOD (COOLING DUCT) · airframe 44,269 hrs · 28,293 cycles

NO EQUIP COOLING LIGHT ILLUMINATED AT FL180 ON CLIMB-OUT. QRH COMPLIED WITH EQUIP COOLING CIRCUIT BREAKERS PULLED FOR 15 SECONDS & RESET. LIGHT WENT OUT & REMAINED OUT FOR ABOUT 2 MINS THEN RE-ILLUMINATED. CB PULL IAW QRH. LIGHT EXTINGUISHED DURING APPROACH. REMOVED EQUIPMENT COOLING SYSTEM FLOW STRAIGHTNER AND MUFFLER. FOUND INSIDE INSULATION LOOSE & BLOCKING AIR EXIT. R & R FLOW STRAIGHTNER & MUFFLER IAW MM 21-58-061-4. PER MTSI WRI 21-26/1509. R & R FLOW CONTROL VALVE IAW MM 21-58-021-4. GROUND PRESSURIZED ACFT IAW JRH, WHEN FLOW CONTROL VALVE CLOSED EQUIP COOLING LIGHT REMAINED OFF. EQUIP COOLING SYS GROUND OP'S CKD GOOD PER MM 21-58-021-4, 21-58-061-4, 21-58-000-0. ACFT OK FOR SERVICE.

Part: BLOWER — FAILED (EQUIP COOLING) · airframe 44,269 hrs · 28,293 cycles

EQUIPMENT COOLING LIGHT ILLUMINATED INFLIGHT, APPROX ABOVE 18K FEET. RAN CHECKLIST. COMPLIED WITH PROCEDURE TO PULL APPROPRIATE CIRCUIT BREAKERS. REPEAT WRITEUP, LIGHT WENT OUT ON SHORT FINAL. REMOVED AND REPLACED COOLING BLOWER IAW MM 21-58-011-4, OPS CHECK GOOD. REMOVED AND REPLACED BLOWER SHUT-OFF RELAY IAW SMP. REMOVED AND REPLACED DIFFERENTIAL PRESSURE SWITCH IAW MM 21-58-051-4. STILL REQS ADJ/TEST IAW 21-58-00-5 PARAGRAPH 3 IAW TSI. AVIONICS IS GOING TO DO TEST.

Part: WARNING HORN — FALSE ACTIVATION (COCKPIT) · airframe 41,556 hrs · 26,231 cycles

DURING T/O ROLL AT APPROX 65 KIAS (ON CAPT'S A/S IND) THE MACH A/S WARN CLACKER SOUNDED. REJECTED T/O AND COMPLIED WITH RTO CHECKLIST IN QRH. RETURNED TO GATE. PERFORMED MACH AIRSPEED WARN CHECKS IAW 727-200 M/M 34-14-002-5, BOTH NR 1 AND NR 2 OVERSPEED WARNING SYS CKD WITHIN M/M LIMITS AND PITOT/STATIC SYS. LEAK CKD GOOD. CKD BOTH SYSTEMS AT REQUIRED ALTITUDES AND AT SEA LEVEL AND FIELD ELEVATION AT KMEM, NO ABNORMALITIES NOTED WITH EITHER SYSTEM. UNABLE TO DUPLICATE DISCREPANCY. A/C IS OK FOR SERVICE.

Part: ENGINE — MALFUNCTIONED (NR 3) · airframe 41,311 hrs · 26,070 cycles

AFTER 20 MINUTES AT CRUISE, NR 3 OIL PRESSURE READ 34 PSI. WENT TO QRH, RETARDED THROTTLE AND OIL TEMP ROSE TO 120 C. ALL OTHER INDICATIORS WERE GOOD. SHUT ENGINE DOWN IAW QRH, DIVERTED TO CVG.

Part: ENGINE — MALFUNCTIONED (NR 3) · airframe 41,309 hrs · 26,069 cycles

ON CLIMBOUT NR 3 ENG OIL PRESS WENT TO 30PSI AND OIL T EMP WENT TO 130C. SHUT DOWN ENG NR 3 IAW QRH AND RETURNED TO MEMPHIS. ACCOMP ENG WINDMILLING CK AND R&R OIL FILTER PER M/M 72-00-00, PG 531. RAN ENG AND OPS CKS GOOD AT IDLE. ADJ OIL PRESS RELIEF VALVE PER M/M 79-34-01. TOOK ACFT TO HIGHPOWER AND ALL OPS CK'D GOOD.

Part: TRANSMISSION — DAMAGED (TE FLAPS) · airframe 40,984 hrs · 25,855 cycles

AFTER T/O UPON FLAP RETRACTION ASSYMETRICAL FLAPS ON INBOARD FLAPS RAN RED TABS AND RETURNED TO PVD. RT INBRD TRAILING EDGE FLAP INBRD JACK SCREW GEARBOX DAMAGED AND PULLED APART WHERE JACK SCREW ENTERS GEARBOX AT REAR SPAR. FACT 08AUG05 19:08 PVD R R&R'D RT INBD FLAP, INBD FLAP TRANSMISSION ASSY IAW 27-51-041-4. ALSO, R&R'D RT IB AILERON AND TAB ASSY PER MM 27-10-001-2, PGS 1-3.

Part: SPAR — CORRODED (RT WING) · airframe 40,915 hrs · 25,798 cycles

CORROSION ON RT WING FUEL CELL FWD SPAR WEB FWD FACE AROUND CUTOUT 7540R. *S/D* REPAIRED RIGHT WING FUEL CELL FWD SPAR WEB FACE AROUND PANEL 7540 PER FED EX EA 7-5710-86300.

Part: ATTACH ANGLE — DAMAGED (NR 2 SPOILER) · airframe 40,915 hrs · 25,798 cycles

NR 2 SPOILER ACTUATOR LWR ATTACH ANGLE HOLES ARE ELONGATED. *S/D* REPLACED NR 2 SPOILER ACTUATOR SUPPORT FITTING PER SRM 51-30-2.

Part: FRAME — DAMAGED (FUSEAGE) · airframe 40,915 hrs · 25,798 cycles

WHILE WORKING N01404 FOUND HOLES IN FRAME AT BS 520 RBL 65 WL 201 DAMAGE. *S/D* REMOVED AND REPLACED BS 520 FRAME SEGMENT STR 13R TO 25R, FOUND TO BE A MAJOR REPAIR PER SRM 51-30-5 AND 51-30-2.

Part: FLAP TRACK — CORRODED (NR 3) · airframe 40,915 hrs · 25,798 cycles

NR 3 FLAP TRACK HAS CORROSION EMINATING FROM AFT ATTACH AREA. REPLACED NR 3 FLAP TRACK PER MM 27-51-031-4

Part: FRAME — DAMAGED (FUSELAGE) · airframe 40,915 hrs · 25,798 cycles

N01425 BS 360, STR 2R BS 360 S2R FRAME IS DAMAGED AT TOOLING HOLE. REPAIRED FRAME PER SRM 51-40-3

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 40,915 hrs · 25,798 cycles

UPPER FUSELAGE, STA 440, STR 6L, STRINGER TO FRAME CLIP CRACKED. *S/D* REPLACED CLIP PER SRM 51-30-2.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 40,915 hrs · 25,798 cycles

UPPER FUSELAGE, STA 440, STR 1R, STR TO FRAME CLIP DAMAGED. *S/D* REPLACED CLIP PER SRM 51-30-2.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 40,915 hrs · 25,798 cycles

UPPER FUSELAGE, STA 440, STR 0, STR TO FRAME CLIP DAMAGED. *S/D* REPLACED CLIP PER SRM 51-30-2.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 40,915 hrs · 25,798 cycles

UPPER FUSELAGE STA 360, MULTIPLE OPEN HOLES IN CIRCUM FRAME, FROM BL 0 TO STR 5L. *S/D* REPAIRED MULTIPLE OPEN HOLES IAW SRM 51-40-3 AND 51-30-02.

Part: SKATE ANGLE — CHAFED (LT MLG TRUNNION) · airframe 40,915 hrs · 25,798 cycles

LEFT MLG FWD TRUNNION SKATE ANGLE CHAFED ON LWR WING SURFACE (I/B). REPAIRED PER FED EX EA 7-5710-86301.

Part: BEAM — DAMAGED (HORZIONTAL STAB) · airframe 40,915 hrs · 25,798 cycles

RT HORIZ STAB, LOWER TRAILING EDGE BEAM DAMAGED WITH LOOSE FASTENERS AT I/B RUB PLATE. REPAIRED IAW FED EX EA 7-5510-86315.

Part: TIE — CORRODED (VERTICAL STAB) · airframe 40,915 hrs · 25,798 cycles

VERTICAL FIN TENSION TIE RT FWD VERTICAL BOLT HOLE IN TENSION TIE & SHEAR FITTING HAS CORROSION. REPAIRED TENSION TIE PER FED EX EA 7-5530-86296.

Part: TIE — CORRODED (VERTICAL STAB) · airframe 40,915 hrs · 25,798 cycles

CORROSION, VERTICAL FIN TENSION TIE RIGHT FWD BOLT HOLE HAS CORROSION ON FACE OF TENSION TIE LUGS UNDER NUT & BOLT HEAD SIDE. REPAIRED TENSION TIE PER FED EX EA 7-5530-86296.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 40,915 hrs · 25,798 cycles

EVALUATE 15 INCH BY 20 INCH EXTERNAL DOUBLER AT BS 656-672 STR 28L-28R, WL 148. REMOVED AND REPLACED DOUBLER PER SRM 53-30-3.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 40,915 hrs · 25,798 cycles

CORROSION ON INTERCOSTAL, BS 259 - 277, LBL 7.5, WL 208. REMOVED AND REPLACED INTERCOSTAL PER SRM 51-30-2.

Part: BEAM — CORRODED (FUSELAGE) · airframe 40,915 hrs · 25,798 cycles

A 9G FITTING CORRODED, BS 266, LBL 5, WL 208. REMOVED AND REPLACED G-BEAM PER SRM 51-30-2.

Part: SKIN — DENTED (CARGO DOOR) · airframe 40,915 hrs · 25,798 cycles

FWD LOWER CARGO DOOR, EXTERIOR SKIN HAS A DENT, 16 INCHES DOWN FROM TOP, 35 INCHES AFT FROM FWD EDGE. REPAIRED DOOR PER SRM 52-00-3

Part: FLOORBEAM — MISDRILLED (FUSELAGE) · airframe 40,915 hrs · 25,798 cycles

UPPER LOBE INTERIOR, STA 520, RBL 43, TOP OF FLOORBEAM HAS DOUBLE DRILLED HOLES. REPAIRED BS 520 UPPER CHORD PER FED-EX EA 7-5310-86321.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 40,915 hrs · 25,798 cycles

STRINGER CLIP CRACKED AT BS 825 STR 7R. *S/D* REPLACED STRINGER CLIP PER SRM 51-30-2.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 40,915 hrs · 25,798 cycles

N01344 CREASE IN EXTERNAL SKIN AT BS 1124 STRINGER 20 LT, JUST BELOW SKIN LAP REPAIRED SKIN PER SRM 53-30-3

Part: FLOORBEAM — CORRODED (FUSLEAGE) · airframe 40,915 hrs · 25,798 cycles

AFT CARGO, STA 1130 FLOORBEAM LWR CHORD CORRODED AT NUT CLIP LOCATIONS LBL 60 TO RBL 60 (C53-113-01, 2). *S/D* REPAIRED FLOORBEAM PER SRM 53-10-8.

Part: STRINGER — CRACKED (LT WING) · airframe 40,915 hrs · 25,798 cycles

LT WING UPPER STR 9 CRACKED AT WS 656.50. REPAIRED STRINGER PER FED EX EA 7-5710-86294

Part: STRINGER — CRACKED (RT WING) · airframe 40,915 hrs · 25,798 cycles

RT WING UPPER STR 10 CRACKED AT WS 686.5 REPAIRED STRINGER PER FED EX EA 7-5710-86294.

Part: STRINGER — CRACKED (RT WING) · airframe 40,915 hrs · 25,798 cycles

RT WING UPPER STR 9 CRACKED AT WS 656.5. REPAIRED STRINGER PER FED EX EA 7-5710-86294.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 40,915 hrs · 25,798 cycles

FWD CARGO BAY FRAME IS CREASED BS 660, STR 24L. REPAIRED FRAME AT BS 660, STR 24L PER SRM 51-40-3

Part: FRAME — DAMAGED (FUSELAGE) · airframe 40,915 hrs · 25,798 cycles

FWD CARGO BAY FRAME IS CREASED BS 680, STR 24L TO 25L. REPAIRED FRAME AT BS 680 STR 24L-25L PER SRM 51-40-3.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 40,915 hrs · 25,798 cycles

FWD CARGO BAY FRAME IS CREASED AT BS 560 STR 24L TO 25L. REPAIRED FRAME PER SRM 51-40-3.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 40,915 hrs · 25,798 cycles

FWD CARGO BAY FRAME IS CREASED BS 600, STR 24L TO 25L. *S/D* REPAIRED FRAME PER SRM 51-40-3 AT BS 600 STR 24L-25L.

Part: SKIN — CRACKED (FUSELAGE) · airframe 40,915 hrs · 25,798 cycles

CRACK IN SKIN AT BODY STATION 1053 STR 28L.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 40,915 hrs · 25,798 cycles

DAMAGED AIRCRAFT ON RIGHT SIDE WHILE REMOVING BALLAST BARREL'S AT B.S. 420-426 STR 18. REPAIRED SKIN PER FED EX EA 7-5330-86306.

Part: SKIN — DENTED (FUSELAGE) · airframe 40,915 hrs · 25,798 cycles

DENT IN SKIN AT BS 1348, STR 14L. REPLACED SKIN PANEL PER SRM 51-30-2.

Part: SKIN — DENTED (FUSELAGE) · airframe 40,915 hrs · 25,798 cycles

DENT IN SKIN, BS 1348, STR 23L. REMOVED DAMAGED SKIN & REPLACED DAMAGE SKIN BS 1342-1352 WL 190.3 - 259.5. ALL WORK DONE IAW SRM 51-10-1, 51-30-2, 51-30-5, 51-30-8, 51-10-2 & M/M 51-20-013-7

Part: STRINGER — CRACKED (FUSELAGE) · airframe 40,915 hrs · 25,798 cycles

FOUND CRACK IN STR 24L BS 560. REPAIRED STRINGER PER SRM 53-10-3.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 40,915 hrs · 25,798 cycles

CORROSION AT FLOORBEAM FASTENER HOLES BS 720 RBL 50 LBL 50, WL 200. REPAIRED FLOORBEAM PER SRM 53-10-8.

Part: SKIN — DENTED (FUSELAGE) · airframe 40,915 hrs · 25,798 cycles

DENT IN SKIN BS 1348, STR 22L. REPLACED SKIN PANEL PER SRM 51-30-2.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 40,915 hrs · 25,798 cycles

UPPER LOBE INTERIOR, STR 950A, LBL 10-22 TOP OF FLOORBEAM CORRODED. REPAIRED FLOORBEAM PER SRM 53-10-8.

Part: SKIN — DENTED (FUSELAGE) · airframe 40,915 hrs · 25,798 cycles

DENT IN SKIN BS 1347, STR 7L. REPLACED SKIN PANEL PER SRM 51-30-2.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 40,915 hrs · 25,798 cycles

FWD CARGO BAY FRAME IS CREASED AT BS 580 STR 25L. REPAIRED FRAME PER SRM 51-40-3

Part: FRAME — DAMAGED (FUSELAGE) · airframe 40,915 hrs · 25,798 cycles

FWD CARGO BAY IS CREASED BS 580 STR 24L - 25L. FOUND LEAK IN AC BAY 3 AT THE TRIM AIR PRESSURE REGULATOR VALVE ROTATED CLAMP AND REPLACED FILTER SEAL LEAK CHECKS GOOD NOW, REPLACED SENSE LOOP IN THE AC BAY AS A PRECAUTION ALL WORK DONE IAW SMP. RAN NR 3 ENGINE AND PERFORMED NR 3 PNEUMATIC SYSTEM TEST IAW JRH 7-3. ALL CHECKS NORMAL. OK FOR SERVICE.

Part: CONTROLLER — SMOKE (FLT DIRECTOR) · airframe 40,668 hrs · 25,609 cycles

AFTER TAKEOFF WHEN GEAR HANDLE WAS RAISED, SMOKE WAS OBSERVED COMING FROM UNDER INSTRUMENT PANEL AT CENTER. SMOKE WAS A PURPLISH COLOR WITH AN ACRID SMELL INDICATING ELECTRICAL ORIGIN. ALSO NOTED FLT DIR- 2, AC C/B POPPED. SMOKE STOPPED AFTER APPROX 1 MIN. BUT SMELL STILL NOTICEABLE IN COCKPIT DURING APPROACH / LANDING AND AFTER BLOCK IN. PER CREW DEBRIEF, SMOKE WAS COMING FROM FLIGHT DIRECTOR MODE CONTROLLER. REPLACED FLIGHT DIRECTOR MODE CONTROLLER. VERIFIED STRONG BURN SMELL FROM CONTROLLER WHEN REMOVED.

Part: TRANSCEIVER — FAILED (ZONE 100) · airframe 39,091 hrs · 24,381 cycles

WEATHER RADAR INDICATOR DISPLAYS A FAIL MESSAGE IN WX, MAP & TEST MODES. REMOVED AND REPLACED RADAR TRANSCEIVER PART 622-1532-101, S/N 4416 (ON) PART 622-5132-120, S/N 4511(OFF), OP'S CHECK GOOD IAW M/M 34-41-041-4.

Part: MOTOR — LEAKING (TE FLAPS)

HYDRAULIC SYS "A" QUANTITY LOSS IN FLIGHT. R&R OUTBOARD FLAP HYDRAULIC DRIVE MOTOR PER MM 27-51-062-4.

Part: SENSOR — FAULTY (AFT AIRSTAIR)

LWF AFT BODY WARN LIGHT ILLUM. REMOVED AND REPLACED 6 O/H SENSORS IN AFT AIRSTAIR. REPLACED D1306 CONNECTOR.

Part: MODULE — MALFUNCTIONED (OVERHEAT DETECT)

LWR AFT BODY O/H LIGHT ON AT TOP OF CLIMB WITH ENG ANTI-ICE ON. LIGHT EXTING AFT CLOSING ANTI-ICE AND PWR REDUCTION AT LEVEL OFF. *S/D* REMOVED AND REPLACED SERVICEABLE MODULE ASSY, CONTROLLER PER MM 26-14-000-1.

Part: DETECTOR — FAILED (FIRE PROTECTION)

LWR AFT BODY OVERHEAT ILLUM. REMOVED AND REPLACED OVERHEAT DETECTOR PER MM 20-10-017-2. RAN ENG 1, 2 & 3 PER IAW 727 JRH. LWR AFT BODY OVERHEAT LIGHT DID NOT ILLUM.

Part: WARNING LIGHT — ILLUMINATED (COCKPIT)

LWR AFT BODY OVERHEAT LIGHT CAME ON. AFT TURN RIGHT PACK OFF, SYS TEST OK AND FLT CONT ON ONE PACK. RUNNING 3 ENG AND BOTH AC PACKS ON INSP PNEU DUCTS ON AFT BODY COMP AND KEEL BEAM AREA. NO LEAKS NOTED. INSP SENSING ELEMENT BY PROXIMITY TO PNEU DUCT. NO FAULT FOUND. AC OK FOR SERVICE.

Part: VALVE — FAULTY (HEATER)

00-351 NR 2 DUCT OVERHEAT LIGHT ILLUM. R&R NR 2 THERMOSTATIC CONTROL VALVE PER MM 30-21-012. R&R FLOOR PANEL PER MM 53-20-012-4.

Part: CONNECTOR — FAULTY (OVERHEAT DETECT)

00-341 LWR AFT BODY OVERHEAT LIGHT, NR 2 & 1 ENGINE BLEED CLOSED. ** S/D ** R&R WIRE, CONNECTOR PER WIRING PRACTICE MANUAL 20-62-14. OPS CK OK.

Part: DUCT — INOPERATIVE (AFT BODY)

00-321 LWR AFT BODY OVERHEAT LIGHT ILLUM IN FLT AT ALTITUDE, LIGHT EXTING WHEN REDUCED NR 2 THROTTLE AND NEVER REILLUMINATED, EVEN AT CLIMB POWER. INSPECTED KEELBEAM AREA AND FOUND RIGHT PNEUMATIC DUCT BROKEN **S/D** R&R PER WORK CARD 49T0501 & MM 49-10-001. OPS CK GOOD

Part: WARNING LIGHT — ILLUMINATED (AFT BODY)

LWR AFT BODY OVERHEAT LIGHT CAME ON DURING CR. SWITCHING BLEEDS TO 1 AND 3 EXTINGUISHED. INSP ALL LOOPS DETECTOR, OK. NO FAULT FOUND.

Part: DETECTOR — FAILED (LT PACK OVERHEAT)

LWR AFT BODY OVERHEAT LIGHT ILLUM. RED TABS FOLLOWED, LIGHT WENT OUT AFT 1 & 2 BLD TURN OFF WITH LEFT PACK OPERATED ON RT NR 1 PACK MONITORED. *S/D* REPLACED OVERHEAT LOOPS M322 & M365 (AFT AIRSTAIRS SECTION 48) PER BOEING 727 MM 26-14-11. AC GOOD FOR SERVICE.

Part: WARNING LIGHT — ILLUMINATED (COCKPIT)

AT CR LWR AFT BODY HEAT LIGHT ON. *S/D* TIGHTENED CLAMPS VISUALLY INSP ALL DUCTS FOR LEAKS. NONE FOUND. OK FOR SERVICE.

Part: DUCT — RUPTURED (AIRSTAIRS)

DURING CR LWR AFT BODY OVHT LIGHT BEGAN FLASHING. THROTTLE RETARDED AND LIGHT EXTINGUISHED. TIGHTENED AND SECURED CLAMPS. INSTALLED CANNED DUCT ASSY PER MM 26-14-000-1, 36-00-001-2. AC OK FOR SERVICE.

Part: WARNING SYSTEM — OVERHEATED (LWR BODY OVERHT)

LWR AFT BODY OVERHEAT LIGHT ILLUM DURING FLT. RAN CKLIST AND ISOLATED IT TO THE NR 1 ENG BLEED SYS. INSP PNEUMATIC SYS AND CARGO COMPT FOR LEAKS, AFT BODY OVHT SENSING ELEMENT, NO LEAK NOTED. NO FAULT FOUND.

Part: WARNING LIGHT — ILLUMINATED (COCKPIT)

LWR AFT OVERHEAT WARN LIGHT CAME ON DURING FLT. LIGHT WENT OUT AFT CLOSING LEFT ENGINE 2/APU BLEED SWITCH. RAN ALL 3 ENGINES AT HI POWER FOR 20 MIN, BUT COULD NOT DUPLICATE. REF PER 727 JET RUN HANDBOOK.

Part: ACTUATOR — FAILED (RT MLG DOOR)

REPEAT, GEAR RETRACT BROUGHT GEAR HANDLE TO OFF AND RED DOOR LIGHT CAME ON. RT GEAR DOOR ON 2ND OFF PANEL, CYCLED ONCE AND LIGHT REMAINED ON. LEFT GEAR HANDLE UP AS PER RED TABS WITH HANDLE IN OFF POS. ALSO, THERE WAS NOISE AND SLIGHT VIBRATION. *S/D* REMOVED AND REPLACED RMG WHEEL WEEL DOOR ACTUATOR PER MM 32-32-0814, OPER CK OK.

Part: WIRE — FAILED (RETRACT MECH)

LANDING GEAR HANDLE WOULD NOT COME UP. APPROPRIATE CHECK LISTS FOLLOWED WITH NEGATIVE RESULTS. LOG BOOK ENTRY REQUIRED. *S/D* REPAIRED SPLICE ON WIRE W526-206-22B PER FED-EX WPM 20-30-12. FUNCTIONAL CHECKED GOOD PER FED-EX M/M 32-31-11.

Part: SHEAR WEB — CORRODED (BS 1175)

CORROSION (C53-224-04) ON TOP AND BOTTOM OF SHEAR WEB AT BS 1175, RBL 1 TO 15, WL 208. *S/D* REMOVED AND REPLACED DAMAGED SHEAR WEB, BS 1140 TO 1176, RBL 20 TO LBL 20, WL 208 IAW FED-EX SRM 51-30-2, 51-20-1.

Part: CHORD — CORRODED (BS 1176)

CORROSION (C53-224-08) ON 1176 REINFORCEMENT CHORD AT BS 1176, RBL 7, WL 208. *S/D* REMOVED AND REPLACED REINFORCEMENT CHORD AT BS 1176, RBL 65 TO LBL 65, WL 208 PER FED-EX SRM 51-30-2 AND BOEING DRAWING NR 65-19606.

Part: SHEAR WEB — CORRODED (BS 1176)

UPON REMOVAL OF 1176 REINFORCEMENT CHORD ON NR 0094, DISCOVERED CORROSION ON SHEAR WEB AT BS 1176, RBL 32, WL 208. *S/D* REMOVED AND REPLACED SHEAR WEB FROM BS 1171 TO 1177, RBL 16 TO RBL 44 PER FED-EX SRM 51-40-2.

Part: AIR GRD SENSOR — DEFECTIVE (LT MLG WW)

ON TAKEOFF, GEAR HANDLE WOULD NOT RAISE ABOVE OFF POSITION, HAD 3 GREEN INDICATION, TAIL SKID AND 3 RED LIGHT. WHEN FLAPS RAISED FROM 5 TO 2, HAD INTERMITTENT HORN. FLAPS RETURNED TO 5 AND GEAR HANDLE DOWN WITH RESULTING 3 GREEN LIGHTS. CHECKLIST PROCEDURES FOR LEVER LATCH FAILURE FOLLOWED. LANDED OK AT MEMPHIS. FOUND AIR SENSE SENSOR IN LEFT HAND WHEEL WELL BAD. REPLACED SENSOR, REPLACED LANDING GEAR ACCESSORY UNIT BAD. REPLACED SOLENDID PRECAUTIONARY. SYSTEM CHECK NORMAL OK TO CONTINUE.

Part: ENGINE — OIL LOSS (NR 3)

AT APPROXIMATELY FLIGHT LEVEL 220, NR 3 LOW OIL PRESSURE/FILTER BYPASS LIGHT FLASHED ON AND OFF. CONFIRMING LOW PRESSURE ZERO QUANTITY AND RED LINE OIL TEMPERATURE. ENGINE WAS SHUT DOWN, LANDING ACCOMPLISHED DFW. REPLACED NR 3 ENGINE PER WORK CARDS 70T0001, 70T0003, 70T0301, AND C/W FEC-M-0485 ENGINE RUN FORM, ALL OPS AND LEAK CKS GOOD.

Part: FLOORBEAM — CORROSION (BS 400)

CORROSION ON MAIN CABIN FLOORBEAM STA 400 AT RBL 24, FOUND WHEN FLOOR TRACK WAS REMOVED. ROUTED OUT DAMAGED AREA, INSTALLED DOUBLER WITH INTERCOSTAL PER 53-10-5.

Part: SUPPORT — CORRODED (BS 480)

STR 26R IS CORRODED AT STA 480. REMOVED SECTION OF FLOOR SUPPORT RT STA 480 TO 495 FOM. REMOVED CORRODED STR 26R SPLICE AT STA 480, TREATED WITH ALODINE 1200 PER SRM 51-10-2, DRILLED NEW SPLICE, ALODINE 1200 TREATED, PRIMED. ALL FASTENERS THROUGH THE SKIN INSTALLED WET. FINISHED INSTALLATION OFSPLICE PER 51-30-1, INSTALLED FLOOR SUPPORT.

Part: DOOR FRAME — CORRODED (BS 450)

LEVELING COMPOUND AFT OF E AND E DOOR CUTOUT AFT FRAME IS LOOSE. REMOVED LEVELING COMPOUND CORROSION FOUND ON DOOR CUTOUT FRAME. FRAME AT BS 450 REMOVED AND REPLACED WITH NEW FRAME PER SRM 51-10-1.

Part: FLOORBEAM — CORRODED (FS 344)

CORROSION ON MAIN CABIN FLOORBEAM STA 344 RBL 24 TO LBL 65.REMOVED CORROSION PER SRM 51-20-6 CORROSION REMOVAL BEYOND LIMITS. INSTALLED SPLICE REPAIR ON TEE CHORD IAW ATTACHED JOB PROGRESS FROM SRM 51-10-1 AND 51-40-4 PAGE 942.

Part: SKIN — CORRODED (BS 720)

FWR CARGO STA 720 BLO LEVELING COMPOUND SEPARATING FROM SKIN. REMOVED LEVELING COMPOUND AND REMOVED CORROSION PER SRM 87-10-6, TREATED PER SRM 59-10 MATERIAL REMOVED BEYOND LIMITS. INSTALLED DOUBLER REPAIR PER SRM 53-30-3 PAGE 519.

Part: FLOORBEAM — CORRODED (BS 480)

CORROSION ON FLOORBEAM AT STA 480 UNDER NR 5 SEAT TRACK. REMOVED CORROSION AS PER SRM 51-20-11, CORROSION REMOVED BEYOND LIMITS. INSTALLED DOUBLER PER EA 7-5310-25380 8/4/95.

Part: FLOORBEAM — CORRODED (BS 344)

CORROSION ON UNDERSIDE OF TOP FLANGE OF FLOORBEAM STA 344, AROUND NUT CLIPS FROM BLL 12 TO BLR 12. REMOVED CORROSION, REMOVED AND REPLACED TOP TEE CHORD AND INSTALLED SPLICE REPAIR ON TEE CHORD IAW ATTACHED JOB PROGRESS FORM 51-10-1 OF SRM, 51-40-4 FIG 1 OF SRM.

Part: ANGLE — CORRODED (BS 227.5)

CORROSION ON BOTH THE VERTICAL AND HORIZONTAL INTERNAL FLANGES OF THE BS 227.5 LOWER CHORD ANGLE. THE CORROSION IS LOCATED JUST TO THE LEFT OF BL 0. FABRICATED REPAIR DOUBLER PER ESO11782, 8-8-95 AND EA 7-5310-25381, 8-4-95.

Part: FLOORBEAM — CORRODED (BS 620)

FWD CARGO STA 620L BOTTOMSIDE OF MAIN CARGO FLOORBEAM LBL 48 CORROSION AROUND NUTPLATE. REMOVED NUTPLATE AS PER SRM 51-10-1. REMOVED CORROSION AS PER SRM 51-10-6, CORROSION REMOVED APPROX 50 PERCENT MATERIAL REMAINING. INSTALLED DOUBLERPER EA 7-5310-25380 8/4/98.

Part: ANGLE — CORRODED (BS 227.5)

CORROSION ON BOTH VERTICAL AND HORIZANTAL INTERNAL FLANGES AT BS 227.5 LOWER CHORD ANGLE. CORROSION IS LOCATED JUST TOTHE LEFT OF BLLO. FABRICATED REPAIR DOUBLER PER EA 7-5310-25381 8/4/95.

Part: FLOORBEAM — CORRODED (BS 530)

CORROSION ON FLOORBEAM STA 530 BETWEEN 5 AND 6 SEAT TRACKS.CORROSION WAS CUT OUT OF UPPER AFT FLANGE OF BEAM. DOUBLERS, REPAIR ANGLES AND FILLER WERE INSTALLED PER ESO 11782 DATE 8-03-95 REF NR1127.

Part: TAB HINGES — BROKEN (RUDDER)

A/C HAS A HEAVY YAW VIBRATION AND FLOOR VIBRATION ABOVE .72M AT FL 350. AT FL 280 VIBRATION STARTS AT .62M SPEEDBRAKES, CLIMB, DESCENTS AND TURNS HAVE NO EFFECT ON VIBRATION OR YAW. AIRCRAFT WAS FLOWN AT 62M AND FL280 FROM DAY-MEM. REMOVED LOWER TAB. FOUND BROKE TAB HINGES AND ATTACH HARDWARE WORN AND BROKEN. REPLACED LOWER TAB HINGES IAW MM 27-20-11. REPLACED LOWER TAB IAW MM 27-20-11 AND 27-20-00. OPS CHECK GOOD.