N925UP

Part: UPLOCK — FAILED (NLG)

INSPECTION TYPE:N/A NOSE LANDING GEAR TOOK 4 CYCLES TO EXTEND MANUAL EXTENSION WAS NO HE LP. *S/D* REF WDM 32-64-01 REMOVED AND REPLACED WIRE BETWEEN S96 & S93. REMOVED AND ADJUSTED CORRECTLY. REMOVED AND REPLACED NLG LOCK ACT W/REF 32-33-11, PERFORMED NLG MANUAL EXT W/REF 32-34-00. REMOVED AND REPLACED NLG LOCK SW W/REF MM 32-61-21, ALL ITEM R/R OPS CHECK AND LEAK CHECK GOOD. NLG SWING AND MANUAL EXTENSION NORMAL, OK TO CONTINUE.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 49,004 hrs · 36,346 cycles

INSPECTION TYPE:C, ON REMOVAL OF ATTACH BRACKET FASTENERS CORROSION FOUND ON STR 24L AT BS 740. STRINGER REPAIRED IAW SRM 53-10-3 FIG 1.

Part: BOLT — CRACKED (NR 3 ENGINE) · airframe 49,004 hrs · 36,346 cycles

INSPECTION TYPE:C, ENG NR 3 AFT LOWER CRANE BEAM SHOULDER BOLT FAILED NDI DUE CRACK COMING FROM SPLIT PIN HOLE. ALSO, CAD PLATING DAMAGED. NR 3 ENG AFT CRANE BEAM LOWER SHOULDER BOLT REPLACED IAW MM 71-21-03.

Part: ANGLE — CORRODED (RT WING) · airframe 49,004 hrs · 36,346 cycles

INSPECTION TYPE:C, CRACK ON ANGLE BETWEEN SKIN AND RIB IN RIGHT WING L/E CAVITY AT O/B END OF NR 6 L/E FLAP. REPLACED ANGLE AND INSTALLED FASTENERS IAW SRM 51-30-02 AND BOLTS IAW OHM 20-50-01.

Part: WEB — CRACKED (CARGO BAY) · airframe 49,004 hrs · 36,346 cycles

INSPECTION TYPE:C, AFT CARGO DOOR HINGE FWD WEB CRACKED AT INNER CORNER. FABRICATED WEB IAW DRW 69-19170. AFT CARGO DOOR FWD HINGE FWD WEB REPLACED IAW DRAWING 65-18625.

Part: BOLT — CRACKED (NR 1 ENGINE) · airframe 49,004 hrs · 36,346 cycles

INSPECTION TYPE:C, ENG NR 1 AFT UPPER CRANE BEAM SHOULDER BOLT FAILED NDI DUE CRACK COMING FROM SPLIT PIN HOLE. ALSO, CAD PLATING DAMAGED. NR 1 ENG AFT CRANE BEAM UPPER SHOULDER BOLT REPLACED IAW MM 71-21-03.

Part: BOLT — CRACKED (NR 2 ENGINE) · airframe 49,004 hrs · 36,346 cycles

INSPECTION TYPE:C, ENG NR 2 LEFT ADAPTER FITTING SWING LINK BOLT FAILED NDI DUE CRACK IN THREADS. REPLACED BOLT IAW MM 71-21-12.

Part: BOLT — CRACKED (NR 2 ENGINE) · airframe 49,004 hrs · 36,346 cycles

INSPECTION TYPE:C, ENG NR 2 LEFT ADAPTER FITTING SUSPENSION LINK UPPER ADAPTER FITTING DUE CRACK IN TREADS. REPLACED BOLT IAW MM 71-21-12.

Part: BOLT — CRACKED (NR 1 ENGINE) · airframe 49,004 hrs · 36,346 cycles

INSPECTION TYPE:C, ENG NR 1 AFT LOWER CRANE BEAM SHOULDER BOLT FAILED NDI DUE CRACK COMING FROM SPLIT PIN HOLE. ALSO, CAD PLATING DAMAGED. NR 1 ENG AFT CRANE BEAM LOWER SHOULDER BOLT REPLACED IAW MM 71-21-03.

Part: BOLT — CRACKED (NR 1 ENGINE) · airframe 49,004 hrs · 36,346 cycles

INSPECTION TYPE:C, ENG NR 1 FWD UPPER CRANE BEAM SHOULDER BOLT FAILED NDI DUE CRACK COMING FROM SPLIT PIN HOLE. ALSO, CAD PLATING DAMAGED. ENG NR 1 FWD CRANE BEAM UPPER SHOULDER BOLT REPLACED IAW MM 71-21-03.

Part: BOLT — CRACKED (NR 2 ENGINE) · airframe 49,004 hrs · 36,346 cycles

INSPECTION TYPE:C, ENG NR 2 RIGHT ADAPTER FITTING CONE BOLT ATTACH BOLT FAILED NDI DUE CRACK IN THREADS. REPLACED BOLT IAW MM 71-21-22.

Part: WEB — CRACKED (CARGO BAY) · airframe 49,004 hrs · 36,346 cycles

INSPECTION TYPE:C, AFT CARGO DOOR AFT HINGE FWD WEB CRACKED AT UPPER CORNER. AFT CARGO DOOR AFT HINGE FWD WEB REPLACED IAW DRW 65-18625.

Part: BOLT — CRACKED (NR 3 ENGINE) · airframe 49,004 hrs · 36,346 cycles

INSPECTION TYPE:C, ENG NR 3 FWD LOWER CRANE BEAM SHOULDER BOLT FAILED NDI DUE CRACK COMING FROM SPLIT PIN HOLE. ALSO, CAD PLATING DAMAGED. NR 3 ENG FWD CRANE BEAM LOWER SHOULDER BOLT REPLACED IAW MM 71-21-03.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 49,004 hrs · 36,346 cycles

INSPECTION TYPE:C EVIDENCE OF CORROSION UNDER RIVET HEAD ON BS 870 BULKHEAD I DOWN FROM PRES DECK, 42 INCHES RIGHT OF KEEL BEAM (RT WHEEL WELL). HFEC INSP OF THE CUTOUT PERIPHERY C/O NDF BULKHEAD REPAIRED IAW SRM 53-10-9 FIG 4.

Part: FIREWALL — CRACKED (NR 2 ENGINE) · airframe 49,004 hrs · 36,346 cycles

INSPECTION TYPE:C, SUSPECT CRACK ON WEB OVER ENGINE NR 2 HORIZONTAL FIRE WALL BS 1376 RT. HFEC C/O, CRACK CONFIRMED. FABRICATED AND INSTALLED WEB IAW DRAWING 657555.

Part: RIB — CRACKED (NR 4 SLAT) · airframe 49,004 hrs · 36,346 cycles

INSPECTION TYPE:C, NR 4 L/E SLAT 2 RIBS CRACKED OUTBOARD OF OUTBOARD TRACK. RIBS REPAIRED IAW SRM 57-50-3 FIG 9 & SRM 51-30-2.

Part: BOLT — CRACKED (NR 2 ENGINE) · airframe 49,004 hrs · 36,346 cycles

INSPECTION TYPE:C, ENG NR 2 FWD MOUNT CROSS STRUT AFT ATTACH BOLT FAILED NDI DUE BOLT CRACKED. NR 2 ENG FWD MOUNT CROSS STRUT AFT ATTACH BOLT REPLACED PER MM 71-21-1 2.

Part: BOLT — CRACKED (NR 2 ENGINE) · airframe 49,004 hrs · 36,346 cycles

INSPECTION TYPE:C, ENGINE NR 2 FWD LEFT CONE BOLT HOUSING ATTACHMENT BOLTS, AFT UPPER BOLT FAILED NDI DUE BOLT CRACKED. ENG NR 2 FWD LEFT CONE BOLT HOUSING ATTACH BOLTS AFT UPPER REPLACED IAW MM 71-21-12.

Part: SKIN — CORRODED (FUSELAGE) · airframe 49,004 hrs · 36,346 cycles

INSPECTION TYPE:C, SUSPECT CORROSION BETWEEN SKIN AND INTERNAL STRUCTURE BS 1020 S17L. HFEC INSP C/O ON HOLES IN ABOVE AREA. NO DEFECT FOUND. CORROSION REMOVED IAW SRM 51-10-06 FROM SKIN AND FROM CUSP ANGLE SKIN CUTOUT BS 1020 S17L. REPAIRED AREA IAW SRM 53-30-3 FIG 3. NOTE THIS IS A CAT A REPAIR AND HAS BEEN ZERO TIMED. CUSP ANGLE REPAIRED IAW SRM 51-40-3.

Part: SKIN — CORRODED (FUSELAGE) · airframe 49,004 hrs · 36,346 cycles

INSPECTION TYPE:C, SUSPECT CORROSION BETWEEN SKIN AND STRUCTURE BS 1178 BETWEEN S7R & 9R. FASTENERS REMOVED, CORROSION FOUND TO BE OUT OF LIMITS. REMOVED DAMAGED SKIN BETWEEN BS 1183 - 1165 RT S7R - S9R IAW SRM 53-30-3. NDT INSP C/O. NO DEFECT FOUND. REPAIRED AREA IAW SRM 53-30-3 FIG 3 A.

Part: APU — OVERSERVICED (AFT)

INSPECTION TYPE:N/A, APU FIELD RELAY TRIPPED FLIGHT DECK FILLED WITH SMOKE. FOUND APU OVERSERVICED WITH OIL. RESERVICED APU PACKS, RUN ALL AND OPS CHECK NORMAL WITH NO SMOKE.

Part: BULB — FAILED (COCKPIT)

DURING ASE, COCKPIT EMERGENCY EXIT IND ONE FILAMENT INOP. RELAMPED EMERGENCY EXIT LIGHT IN COCKPIT FROM AIRCRAFT SPARE STOWAGE.

Part: SPAR — CRACKED (LT WING)

INSPECTION TYPE:N/A, LT WING AFT FALSE SPAR LWR. CAP CRACKED BELOW I/B GROUND SPOILER ACTUATOR SUPPORT BRACKET AT TERMINATING END. DAMAGE APROX 1.25 INCHES IN LENGTH. *S/D* REPAIRED CRACK PER UPS EO B727-5750-11867-A, PARA 6A. CRACK STOP DRILLED IAW SRM 51-10-1 D-178976 ASSIGNED TO CREATE MPI FOR INSPECTION.

Part: LIGHT — LOOSE (FLIGHT DECK)

INSPECTION TYPE:N/A, DURING TAKEOFF THE FLIGHT DECK EMERGENCY LIGHT FELL OFF MOUNT. REINSTALLED EMERGENCY EXIT LIGHT ASSY, OPS CHECKS NORMAL.

Part: OUT FLOW VALVE — STUCK (RIGHT)

INSPECTION TYPE:SI, AIR TURNBACK AT 1945UTC DUE TO UNSATISFACTORY AIRCRAFT PRESSURIZATION. WHEN CLIMB THRUST SET, CARGO HEAT O'FLOW VALVE CLOSED, FULL MANUAL INCRASE ON MANUAL CONTROLLER. AIRCRAFT WAS ONLY ABLE TO MAINTAIN A CABIN ALTITUDE OF 8,000 AND DIFFERENTIAL OF 7 PSID. HAD FLIGHT CONTINUED, CABIN ALTITUDE WOULD HAVE EXCEEDED 10,000 2-3MTS. TROUBLESHOT SYSTEM PER MM, FOUND RT OUTFLOW VALVE TO BE STUCK OPEN DUE TO INSULATION BLANKET STUCK IN VALVE. REMOVED BLANKET AND PERFORMED PRESSURE CONTROL SYSTEM TEST PER MM 21-30-01. NO DEFECTS NOTED.

Part: AIRSTAIR — OUT OF ADJUST (AFT FUSELAGE)

INSPECTION TYPE:SI, AFT AIRSTAIR LIGHT ILLUMINATED IN FLT. VISUAL INSPECTION OF STAIR AREA SHOWED FLEXING OF DOOR ARMS INDICATIVE OF UNLOCK CONDITION. DOOR LIGHT WENT OUT WITH INITAIL FLAP SELECTION TO 2 DEGREES (POSSIBLE AIRFLOW CHANGE ON DOOR/STAIR AREA). FOUND AFT AIRSTAIR POSITION PROXIMITY SWITCH TO BE OUT OF ADJUSTMENT. ADJUSTED SWITCH PER MM 52-70-01 PARA E PAGE 508. FUNCTIONALLY TESTED PER MM 52-70-01 PARA 2 PG 509, NO FURTHER DISCREPANCIES NOTED.

Part: CONNECTOR — DIRTY (NLG)

INSPECTION TYPE:SI, AIR TURNBACK AT 0100 UTC UPON GEAR RETRACTION, GEAR LEVER WOULD NOT MOVE PAST OFF POSITION. ALSO, I/B ANTISKID RELEASE REMAINED ON IN FLIGHT WITH GEAR HANDLE IN DOWN/IN POSITION. REMOVED, CLEANED CONNECTOR AND RE-INSTALLED ANTISKID CONTROL BOX. REMOVED AND REPLACED NLG SAFETY SWITCH PER 727 MM 32-09-211. PERFORMED OPERATION CHECK OF ANTISKID SYS CHECK GOOD PER 32-42-00. FUNCTIONAL TESTED GEAR SAFETY SENSOR (SWITCH) GOOD PER 32-21-11. ADJUSTED AND RIGGED NLG PISTON POSITION CABLES PER 727 MM 32-51-00.

Part: TRACK — CORRODED (TE FLAP)

INSPECTION TYPE:SI (CORROSION C57-581-06.00-04) ON NR 6 FLAP TRACK AT SPOILER BEAM PAD. CORROSION ON SPOILER BEAM PAD IS OUT OF LIMITS IAW SRM 57-40-02. FLAP TRACK WAS REPLACED ON CID 888728.

Part: FLOORBEAM — CORRODED (BS 312)

INSPECTION TYPE:SI, CORROSION ON STRAP ON FLOORBEAM UPPER CHORD LOWER SIDE BS 312, BL 0, WL 208. REPAIR TO BE ACCOMPLISHED ON CUSTOMER ID 888989.

Part: FITTING — CORRODED (TE FLAP)

INSPECTION TYPE:SI, CORROSION ON NR 7 FLAP TRACK FWD ATTACH FITTING. FITTING WAS REWORKED ON NRC NR 888956 AND REINSTALLED ON NRC NR 888744.

Part: FITTING — CORRODED (TE FLAP)

INSPECTION TYPE:SI, CORROSION ON NR 8 FLAP TRACK FWD ATTACH FITTING. REWORKED FITTING PER ER 99-5226.

Part: CHORD — CORRODED (FUSELAGE)

INSPECTION TYPE:SI, 740 UPPER CHORD CORRODED RBL 65-70 WL 202. REMOVED AND REPLACED CHORD SEGMENT RBL 53-55 TO RIGHT O/B END.

Part: SKIN — CORRODED (BS 873-877)

INSPECTION TYPE:SI, INTERIOR FUSELAGE SKIN AT STA 873-877 RT WL 261 ALONG EDGE OF 5-10R IS CORRODED. BLENDED CORROSION ON LOWER SKIN, HFEC FASTENER HOLES, FLAT PEENED THE BLENDED AREA. ALODINED AND PRIMED BLENDED AREA, FABRICATED REPAIR DOUBLER AND REPAIR FILLER, ALODINED AND PRIMED REPAIR PARTS AND INSTALLED.

Part: SKIN — CORRODED (BS 870)

INSPECTION TYPE:SI, CORROSION (C57-174-01-1B) ON INTERNAL 870 SKIN AT UPPER SPAR CHORD BS 870, RBL 61-64. REMOVED CORROSION PER SRM 57-30-1, FLAP PEENED AREA PER ER NR 99-5258, ALODINED AND PRIMED PER ER NR 99-5258.

Part: FLOORBEAM — CORRODED (BS 312)

INSPECTION TYPE:SI CORROSION ON FLOORBEAM BS 312, LBL 3.5, WL 208. REMOVED AND REPLACED UPPER CHORD SEGMENT PER SRM 53-10-8 FIG 9.

Part: STRINGER — CORRODED (BS 806)

INSPECTION TYPE:SI, CORROSION AT BS 806 STR 2 FOUND TO BE OUT OF LIMITS. REPAIRED SRM 53-10-3.

Part: STRINGER — CRACKED (BS 500)

INSPECTION TYPE:SI CRACKS AROUND UPPER FASTENER ON STR 16R COMMON TO BS 500 FRAME. REPAIRED PER SRM 53-10-3.

Part: SEAT TRACK — CORRODED (BS 740)

INSPECTION TYPE:SI CORROSION C53-224-01.05-01, ON FLANGE OF SEAT TRACK BS 740, LBL 25, WL 208, CUT OUT DAMAGED SECTION DUE TO THE EXTENT OF CORROSION. FABRICATED REPAIR PARTS (SEAT TRACK AND STRAPS). ALODINE, PRIMED AND INSTALLED REPAIR PARTS PER SRM 53-10-5 AND 51-30-2.

Part: STRINGER — CORRODED (BS 851)

INSPECTION TYPE:SI BS 851 STR 2 RT FOUND TO BE OUT OF LIMITS. REPAIRED PER SRM 53-10-3 CPCP.

Part: DOUBLER — CORRODED (BS 870)

INSPECTION TYPE:SI WHILE WORKING NRC 888366 (FUSE 123) LT 870 ACCESS COVER (PANEL) DOUBLER RING IS CORRODED LBL 58, BS 870, WL 180. AFTER THE CORROSION REMOVAL, THE DOUBLER RING WENT BEYOND THE SRM LIMITS. REMOVED DOUBLER RING AND FABRICATED A NEW ONE. ALODINED AND PRIMED AND INSTALLED DOUBLER RING PER SRM 51-10-2, 51-10-3 AND 51-30-2.

Part: STRINGER — CRACKED (BS 400)

INSPECTION TYPE:SI CRACKS AROUND UPPER AND LOWER FASTENERS IN STRINGER 15R COMMON TO BS 400 FRAME. REPAIRED PER SRM 53-10-3.

Part: SHEAR TIE — CRACKED (BS 400)

INSPECTION TYPE:SI CRACKED SHEAR TIE AT BS 400 BETWEEN STR 14R AND STR 15R. REPLACED PER SRM 51-30-2.

Part: FLOORBEAM — CORRODED (BS 344)

INSPECTION TYPE:S,I WHILE WORKING CARD 888501 DISCOVERED CORROSION ON FLOORBEAM BS 344 RBL 16-25 WL 208. REPAIR FLOORBEAM PER SRM 51-30-2 SRM 53-10-08.

Part: STRINGER — CRACKED (BS 400)

INSPECTION TYPE:SI, CRACKS AROUND FASTENERS IN STR 5R COMMON TO FRAME AT BS 400. REMOVED AND REPLACED STRINGER SEGMENT FROM BS 380-440 PER SRM 53-10-3 FIGURE 3.

Part: STRINGER — CRACKED (BS 655)

INSPECTION TYPE:SI CRACK IN STR 10L, BS 655, REMOVED DAMAGED SECTION OF STRINGER 10L AT BS 655. FABRICATED REPAIR PARTS. ALODINED, PRIMED, AND INSTALLED REPAIR PARTS PER SRM 51-40-4 AND 51-30-2.

Part: CARRIAGE — CORRODED (NR 3 TE FLAP)

INSPECTION TYPE:SI, CORROSION (C57-581-04.00-03) NR 3 FLAP CARRIAGE. REMOVED AND REPLACED NR 3 FLAP CARRIAGE IAW MM 27-57-21.

Part: STRUCTURE — CRACKED (BS 400)

INSPECTION TYPE:SI, CRACK AROUND UPPER FASTENER IN STR 7 RT COMMON TO BS 400 FRAME. REMOVED CRACKED SECTIONS AT STRINGER 7 RT, BS 400. FABRICATED REPAIR PARTS FOR THE STRINGER AND FRAME. ALODINED, PRIMED AND INSTALLED REPAIR PARTS PER SRM 53-10-3 AND 53-10-4.

Part: SEAT TRACK — CORRODED (BS 344)

INSPECTION TYPE:SI WHILE WORKING CARD NR 888993 FOUND SEAT TRACK AT BS 344 RBL 22 WL 208 TO BE CORRODED ON LWR SURFACE. REPLACED SECTION OF SEAT TRACK FROM BS 344-390 RBL 25 WL 208 PER SRM 51-30-2.

Part: STRINGER — CORRODED (BS 484)

INSPECTION TYPE:D CORROSION (C53-224-01-04-01) ON STR 7 BS 484. REMOVED CORRODED STR 7 FROM BS 480-508, FABRICATED NEW PART OF INSTALLED PER SRM 53-10-3.

Part: STIFFENER — CORRODED (BS 320)

INSPECTION TYPE:SI, CORROSION ON STIFFENER BS 320 RBL 15 WL 170-175. REMOVED AND REPLACED STIFFENER PER SRM 51-30-2.

Part: STIFFENER — CORRODED (BS 336)

INSPECTION TYPE:SI, CORROSION (C53-111-01.05-01) ON STIFFENER ATTACH ANGLE BS 336 LBL 15 WL 170. REMOVED ATTACH ANGLE, FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. FABRICATED PER SRM 51-20-1, INSTALLED ATTACH ANGLE PER SRM 51-30-2.

Part: FITTING — CORRODED (TE FLAP TRACK)

INSPECTION TYPE:SI, CORROSION (C57-581.06.00-04) ON NR 7 FLAP TRACK FWD FITTING. REPAIRED PER ER 99-5216.

Part: ANGLE — CORRODED (BS 320)

INSPECTION TYPE:SI, CORROSION (C53-111-01.05-01) ON STIFFENER ATTACH ANGLE BS 320 LBL 15 WL 170. CORROSION FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. FABRICATED AND INSTALLED NEW ANGLE PER SRM 51-20-1 AND SRM 51-30-2.

Part: TRACK — CORRODED (TE FLAP)

INSPECTION TYPE:SI, CORROSION (C57-581.06.00-04) ON NR 8 FLAP TRACK FWD ATTACH FITTING. REPAIRED PER ER 99-5226.

Part: FITTING — CORRODED (TE FLAP)

INSPECTION TYPE:SI, CORROSION (C57-581-06.00-04) NR 5 FLAP TRACK FWD ATTACH FITTING. REPLACED FITTING BEYOND ECONOMICAL REPAIR PER ESR NR 16, ON NRC 888880.

Part: FLOORBEAM — CORRODED (BS 846-842)

INSPECTION TYPE:SI, CORROSION (C53-224-01.05-02) ON FLOORBEAM UPPER CHORD BS 846 THRU 842, LBL 44, WL 208. REPAIRED ER 99-5239.

Part: CARRIAGE — CORRODED (TE FLAP)

INSPECTION TYPE:SI, CORROSION (C57-581-04.00-04) ON NR 7 FLAP CARRIAGE UPPER SURFACE O/B SIDE. REMOVED AND REPLACED CARRIAGE INSTALLATION ON TC C57-581-04-4D.

Part: SEAT TRACK — CORRODED (BS 775-780)

INSPECTION TYPE:SI CORROSION C53-224-01.05-02 MAIN DECK SEAT TRACK BS 775-780 LBL 60 WL 208 O/B FLANGE. REMOVED AND REPLACED SEAT TRACK FROM BS 760-848 WL 208 LBL 60 PER SRM 53-10-1.

Part: TRACK — CORRODED (TE FLAP)

INSPECTION TYPE:SI, CORROSION (C57-581-06.00-04) ON NR 7 FLAP TRACK AT FWD ATTACH LUG AND INSIDE BARREL NUT HOLE. REPAIRED PER ER 99-5243.

Part: FITTING — CORRODED (TE FLAP)

INSPECTION TYPE:SI, CORROSION (C57-581-06.00-04) ON NR 5 FLAP TRACK FWD ATTACH FITTING. REMOVED AND REPLACED SUPPORT ASSY.

Part: FRAME — CORRODED (BS 780)

INSPECTION TYPE:SI CORROSION (C53-224-01.00-02) MAIN DECK FRAME OUTBOARD TOP SURFACE BS 780 STR 8R-STR1. FOUND CORROSION OUT OF LIMITS PER SRM 53-10-01 BETWEEN STRINGERS 4 AND 5. REMOVED DAMAGED AREA AND INSTALLED STANDARD FRAME REPAIR PER SRM 53-10-4 PG 9 AND SRM 53-10-4 FIG 2.

Part: TRACK — CORRODED (TE FLAP)

INSPECTION TYPE:SI, CORROSION (C57-581-06.00-04) ON NR 7 FLAP TRACK AT FWD ATTACH LUG AND INSIDE BARREL NUT HOLE. REPAIRED ON CUSTOMER ID 888950.

Part: STRINGER — CORRODED (BS 740-870)

INSPECTION TYPE:SI, CORROSION (C53-224-01.00-02) MAIN DECK STR 2R BS 740 TO 870 ALONG BOTH FLANGES ON BOTH SURFACES. REPAIR ON NRC 888518 AND 888519.

Part: STRINGER — CORRODED (BS 1094)

INSPECTION TYPE:SI, CORROSION ON STRINGER 3R BS 1094 .375 BY .375. REPAIRED PER SRM 53-10-3 FIG 2.

Part: TRANSMITTER — MALFUNCTIONED (RT TE FLAP)

ON APPROACH SELECTED FLAPS, 2 INBD FLAPS REMAINED AT 0 USED ALT FLAP PROCEDURE PER AOM AND QRH FLAPS EXTENED DECLARED EMERG AND MADE NORMAL LANDING. REMOVED AND REPLACED RT IB FLAP TRANSMITTER PER MM 27-52-02 OPS OK, P/N ON/OFF 2514-10 S/N ON1-4340 SN OFF NSN.

Part: LINE — FAILED (B HYD SYST)

INSPECTION TYPE-N/A, HYD SYS 'B' FAILURE INFLIGHT BOTH PUMP LIGHTS ILLUMINATED QUANTITY WENT TO 0, PRESSURE WENT TO 0. FOUND BROKEN HYD LINE IN HYD BAY. REMOVED AND REPLACED HYD LINE (P/N 65-17849-4061) CHANGED CASE DRAIN FILTERS, PUMPS OK. SERVICED NO LEAKS NOTED PER M-M 29-12-21.

Part: CLIP — CRACKED (BS 1070)

INSPECTION TYPE-C, BS 1070 AT STR 6L AND 5L STRINGER TO FRAME CLIPS CRACKED. REMOVED, FABRICATED AND INSTALLED NEW CLIPS IAW BAC DWG 65-45313 AND SRM 51-30-2.

Part: STIFFENER — CRACKED (RT WING)

INSPECTION TYPE-C, RT WING NR 5 SLAT AT ACTUATOR ROD MOUNT STIFFENER IS CRACKED IN RADIUS. REPAIRED IAW SRM 51-40-03 AND SRM 51-30-02.

Part: CLIP — CRACKED (BS 1070)

INSPECTION TYPE-C, BS 1070 STR 6R STRINGER TO FRAME CLIP CRACKED. REMOVED, FABRICATED AND INSTALLED NEW CLIP IAW DWG 65-45313 AND SRM 51-30-2.

Part: SPAR CHORD — CRACKED (RT AILERON)

INSPECTION TYPE-C, RT O/B AILERON UPPER SPAR CHORD IS CRACKED, JUST O/B OF THE CENTER I/B HINGE. FABBED AND INSTALLED REPLACEMENT PART IAW SRM 57-30-02 AND 51-30-2.

Part: RIBS — CRACKED (RT WING)

INSPECTION TYPE-C, RT WING NR 5 SLAT, OUTBD AND INBD ACTUATOR ATTACH RIBS ARE CRACKED. REMOVED RIBS AND FABRICATED REPLACEMENT RIBS IAW DWG 65-17276 AND INSTALLED IAW SRM 51-30-02.

Part: FRAME — BULGED (BS 990)

INSPECTION TYPE-C, LT FUSELAGE IS BULGED AT FRAME BS 990 BETWEEN S17 AND S18L. REMOVED DAMAGED AREA, TREATED AND PRIMED, INSTALLED REPAIR AND REINSTALLED FAIRING ATTCH FITTING.

Part: VERT STIFFENER — CRACKED (LT WING)

INSPECTION TYPE-C, LT WINGS L/E NR 2 SLAT I/B TRACK O/B MOUNT VERTICAL STIFFENER ANGLE IS CRACKED AT THE BOTTOM. REMOVED, FABRICATED AND INSTALLED STIFFENER ANGLE PER DWG 65-16200 SHT 1 AND 8 AND SRM 51-30-2.

Part: VERT STIFFENER — CRACKED (LT WING)

INSPECTION TYPE-C, LT WING NR 3 SLAT O/B TRACK, O/B MOUNT VERTICAL STIFFENER ANGLE IS CRACKED AT BOTTOM. REMOVED DAMAGED STIFFENER, FAB AND INSTALLED REPLACEMENT STIFFENER SEALED DOME FASTENERS.

Part: VERT STIFFENER — CRACKED (LT WING)

INSPECTION TYPE-C, LT WING L/E, NR 3 SLAT I/B TRACK, O/B MOUNT VERTICAL STIFFENER ANGLE IS CRACKED AT BOTTOM. REMOVED, FABRICATED AND INSTALLED REPLACEMENT ANGLE IAW 65-16200 AND SRM 51-30-02.

Part: CHANNEL — CORRODED (BS 303-348)

INSPECTION TYPE-C, U-CHANNEL DIRECTLY BELOW THE LAV DOOR IS CORRODED. REMOVED DAMAGED U-CHANNEL IAW SRM 51-10-01. FABRICATED U-CHANNEL IAW SRM 53-10-01 AND INSTALLED IAW SRM 51-10-01.

Part: WEB — CRACKED (BS 1270)

INSPECTION TYPE-C, AFT TORQUE BOX UPPER WEB AT BS 1270 IS CRACKED AT FASTENER IN THE INBD CHORD. REMOVED DAMAGED AREA, INSTALLED FILLER AND DOUBLER.

Part: SEAL RETAINER — CORRODED (NLG DOOR)

INSPECTION TYPE-C, LT AFT NLG DOOR SEAL RETAINER CORRODED. REPLACED LT AFT NLG DOOR SEAL RETAINER PER SRM 51-30-02.

Part: SEAL RETAINER — CORRODED (NLG DOOR)

INSPECTION TYPE-C, RT AFT NLG DOOR SEAL RETAINER CORRODED. REPLACED RT AFT NLG DOOR SEAL RETAINER PER SRM 51-30-2.

Part: CONNECTOR — WET (AFT STAIRS)

ON CLIMB-OUT FROM PHL, NR 1 ENGINE STRUT OVERHEAT LIGHT BEGAN FLICKERING. LIGHT BECAME STEADY UPON LEVEL OFF AT FL 280. ACCOMPLISHED ENGINE STRUT OVERHEAT QF CHECKLIST. LIGHT WENT OUT WHEN NR 1 THROTTLE RETARDED TO NEAR IDLE. AFTER ABOUT 5 MINS, LIGHT RE-ILLUMINATED. ACCOMPLISHED REMAINDER OF CHECKLIST AND SHUTDOWN NR 1 ENGINE IAW CHECKLIST. FOUND WATER IN PLUG, CLEANED. PUT PLUG IN AFT STAIRWELL BACK TOGETHER PER M/M 20-11-13, SEALED PLUG, NO LEAKS NOTED ON ENGINE RUN-UP, NO FLICKERING OF OVERHEAT LIGHT FOR NR 1 ENGINE. OK FOR SERVICE.

Part: ACTUATOR — LEAKING (NR 5 LE FLAP)

CREW REPORTED AIR TURN BACK DUE TO A SYS HYDRAULIC FAILURE. TURN BACK AT 0457 Z, QUANTITY WENT TO ZERO. NR 5 KRUGER FLAP ACT. LEAKING, AWAITING PARTS FOR REPAIR.

Part: UPLOCK SW — OUT OF POSITION (NLG)

CREW REPORTED AFTER TAKEOFF, NOSE GEAR WOULD NOT RETRACT IN ACC WITH ADM PROCEDURES. THE GEAR WAS CYCLED AND IT STILL WOULD NOT RETRACT, BTB ACCOMPLISHED. RESEATED UPLOCK CHECK SWITCH ON CANNON PLUG PIN.

Part: COALESCER BAGS — DIRTY (A/C PACK)

WHILE IN JACKSON, MS, A BURNING SMELL OCCURRED ON TAKEOFF ROLL. MAINTENANCE CHANGED LT AND RT WATER SEPARATOR COALESCERS PER MM 21-51-34.

Part: RIB — CRACKED (BS 760.95)

WHILE IN NAPLES FOR C-MAINTENANCE, FOUND ON WING RIB UPPER CHORD AT BS 760.95. REPAIRED IAW EO B727-5710-1271.

Part: RIB — CRACKED (BS 760.95)

WHILE IN NAPLES FOR C-MAINTENANCE, FOUND CRACKS ON WING RIB UPPER CHORD AT BS 760.95. REPAIRED IAW EO B727-5710-1271.

Part: RIB — CRACKED (BS 758.5)

WHILE IN NAPLES FOR C-MAINTENANCE, FOUND CRACK ON VERTICAL FLANGE OF RIB CHORD AT BS 758.5, RT SIDE. REPAIRED IAW B727-55710-1271.

Part: CHORD — CORRODED (VERT STAB)

WHILE IN NAPLES FOR C-CHECK, MAINTENANCE FOUND CORROSION ON INNER CHORD LT SIDE AT B.S. 1342. REPLACED IAW SRM 51-30-2, E.O. B727-5530-4601B.

Part: CHORD — CORRODED (VERT STAB)

WHILE IN NAPLES FOR C-CHECK, MAINTENANCE FOUND CORROSION ON LOWER CHORD RT SIDE AT B.S. 1342. REPLACED IAW SRM 51-30-2, E.O. B727-5530-4601B.

Part: ANGLE — CRACKED (FS 1370)

WHILE IN NAPLES FOR C-CHECK, MAINTENANCE FOUND CRACKED ANGLE AT B.S. 1370, RT SIDE WL 259.5 INSTALLED FABRICATED PARTS IAW SRM 54-10-2, 51-10-2.

Part: CHORD — CORRODED (VERT STAB)

WHILE IN NAPLES FOR C-CHECK, MAINTENANCE FOUND CORROSION ON LOWER CHORD LT SIDE AT B.S. 1342. REPLACED IAW SRM 51-30-2, E.O. B727-5530-4601B.

Part: ANGLE — CRACKED (FS 1370)

WHILE IN NAPLES FOR C-CHECK, MAINTENANCE FOUND CRACKED ANGLE AT B.S. 1370, LT SIDE WL 254.5. INSTALLED FABRICATED PARTS IAW SRM 54-10-2, 51-10-2.

Part: CHORD — CORRODED (VERT STAB)

WHILE IN NAPLES FOR C-CHECK, MAINTENANCE FOUND CORROSION ON INNER UPPER CHORD LT SIDE AT B.S. 1342. REPLACED IAW SRM 51-30-2, E.O. B727-5530-4601B.

Part: FITTING — CORRODED (FS 1342)

WHILE IN NAPLES FOR C-CHECK, MAINTENANCE FOUND CORROSION ON CHORD FITTING AT STA 1342 RT SIDE. REPLACED IAW B727-5330-4601B AND SRM 51-30-2.

Part: CHANNEL — CORRODED (BS 1342)

WHILE IN NAPLES FOR C-CHECK, MAINTENANCE FOUND CORROSION ON CHANNEL AT STA. 1342 LT SIDE. REPLACED IAW SRM 51-30-2, E.O. B727-5330-4501B.

Part: FITTING — CORRODED (FS 1362)

WHILE IN NAPLES FOR C-CHECK, MAINTENANCE FOUND CORROSION ON CHORD FITTING AT STA 1362 RT SIDE. REPLACED IAW B727-5330-4601B AND SRM 51-30-2.

Part: FITTING — CORRODED (BS 1362)

WHILE IN NAPLES FOR C-CHECK, MAINTENANCE FOUND CORROSION ON CENTER CHORD FITTING AT STA 1362. REPLACED IAW B727-5330-4601B AND SRM 51-30-2.

Part: CHORD — CORRODED (FUSELAGE)

WHILE IN NAPLES FOR C-CHECK, MAINTENANCE FOUND CORROSION ON O/B CHORD FITTING AT STA 1362 LT SIDE. REPLACED IAW B727-5330-4601B AND SRM 51-30-2.