N918UP

Part: CONTROL VALVE — FAILED (FIRE EXTINGUISH)

NR 2 ENGINE FIRE EXTINGUISHING SELECTOR CONTROL VALVE FAILED TO OPEN DURING ROUTINE TESTING IAW UPS ROUTINE TASK CARD TC 2-221-12. THE VALVE SOLENOID HOUSING WAS NOTED AS BEING CORRODED. (K)

Part: STRINGER — CORRODED (STR 24R BS725) · airframe 49,800 hrs · 51,186 cycles

INSPECTION TYPE:C STRINGER 24 RT FOUND CORRODED AT BS 725. PLEASE INVESTIGATE DAMAGE FOUND TO BE BEYOND LIMITS IAW SRM 53-10-3. DAMAGED SECTION OF STRINGER 24R CUT OUT AND REMOVED. AREA REPAIRED IAW 53-10-3 FIG 1 DETAIL 1 PAGE 4B.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 49,800 hrs · 51,186 cycles

INSPECTION TYPE:C AFT CARGO DOOR CRACK ON INNER SKIN SECOND INSPECTION HOLE FWD EDGE AT BOTTOM. REMOVE FASTENER AND CHECK DEPTH OF CRACK TO DETERMINE REPAIR. HFEC CARRIED OUT AND CRACK FOUND CONTAINED WITHIN FASTENER HOLE. REPAIRED IAW SRM 51-40-02.

Part: INTERCOSTAL — CRACKED (BS660 STR 29R) · airframe 49,800 hrs · 51,186 cycles

INSPECTION TYPE:C STA 660, ST 29R REPAIR TO INTERCOSTAL IS CRACKED. PLEASE REPAIR IAW SRM. REPAIR BRACKET FABRICATED IAW SRM 51-20-071 FIG 7. REPAIR BRACKET REPLACED IAW SRM 51-30-02.

Part: LINK — CRACKED (RT MLG UPLOCK) · airframe 49,800 hrs · 51,186 cycles

INSPECTION TYPE:C RT MLG UPLOCK FWD SUPPORT LINKS CRACKED. REPLACE LINKS. RT MLG UPLOCK FWD SUPPORT LINKS REPLACED IAW MM 20-80-01.

Part: SKIN — CORRODED (BS360 STR 22L) · airframe 49,800 hrs · 51,186 cycles

EVIDENCE OF CORROSION AT BS 360 STR 22L AT FWD END OF STR AT AFT FACE OF FRAME. PLEASE INVESTIGATE AND RECTIFY. CORROSION BLENDED OUT IAW SRM 51-10-06. CORROSION FOUND TO BE OUTSIDE LIMITS IAW SRM 51-10-1. REPAIR STRAP FABRICATED IAW SRM 51-20-1 FIG 7. MATERIAL P/N 7055T6 0.063". REPAIR STRAP INSTALLED IAW SRM 51-30-02.

Part: SPAR — CORRODED (BS 870 BRL 36) · airframe 49,800 hrs · 51,186 cycles

AREA OF SUSPECT CORROSION ON WING CENTER SECTION REAR SPAR LWR CHORD BS 870 RBL36 DUE TO 2 POPPED FASTENER HEADS. PLEASE INVESTIGATE AND RECTIFY AS NECESSARY. AS PER BOEING INSTRUCTIONS THE LWR CHORD WAS REPLACED. NEW CHORD WAS CUT AT RBL 9.5. REPAIR SPLICE ANGLES AND STRAPS INSTALLED IAW SRM51-30-02 AND DWG 65C21566. WCS REPAIR OF WEB CARRIED OUT IAW BOEING REPAIR AND A AAE EO 2005-093-013. UPS AUTHORIZATION NR B727-5710-23321-A.

Part: SKIN — CORRODED (BS 441 STR 8L) · airframe 49,800 hrs · 51,186 cycles

INSPECTION TYPE:C NDT INSPECTION HAS INDICATION OF MATERIAL LOSS AT BS 441 FWD OF CENTER LINE AT STR 8L, INVESTIGATE. CORROSION FOUND BETWEEN SKIN AND DOUBLER. CORROSION REMOVED AND FOUND BE WITHIN LIMITS, AREA REPROTECTED IAW SRM 51-30-02.

Part: TRUNNION — CRACKED (RT MLG) · airframe 49,800 hrs · 51,186 cycles

RT TRUNNION ATTACH FITTING HAS CRACK AT OB FLANGE HOLE E RUNNING UP APPROX 2.5 INCHES. REMOVE AND REPLACE FITTING. RT TRUNNION FITTING FOUND CRACKED OUTSIDE REPAIRABLE LIMITS IN UPS EO B727-5740-20666C. REPLACED IAW UPS AUTHORIZATION B727-5740-23046-B.

Part: SKIN — CORRODED (BS 852-1011) · airframe 49,800 hrs · 51,186 cycles

SURFACE CORROSION ON LAP JOINT BETWEEN S-4L AND 5L AT LOCATIONS BETWEEN BS 852 AND 1011. CORROSION REMOVED IAW SRM 51-10-2 (.002") AND FOUND WITHIN LIMITS IAW SRM 51-20-4.

Part: SUPPORT — CORRODED (RT MLG TRUNNION) · airframe 49,800 hrs · 51,186 cycles

INSPECTION TYPE:C RT MLG TRUNNION BUTTERFLY FITTING HAS CORROSION. PLS REPLACE. SUPPORT REPLACED IAW DRW 65-19296.

Part: BUSHING — CRACKED (NR 3 AFT MOUNT) · airframe 49,800 hrs · 51,186 cycles

INSPECTION TYPE:C ENGINE NR 3 AFT MOUNT FITTING HAS CORROSION ON INNER SURFACE OF UPPER USHING. REPLACE BUSHING. REPLACED BUSHING IAW OHM 20-50-03.

Part: MOUNT — CORRODED (NR 3 ENGINE) · airframe 49,800 hrs · 51,186 cycles

INSPECTION TYPE:C ENGINE NR 3 FWD MOUNT FITTING HAS PITTING CORROSION ON BOTH OUTBOARD HOLES. REPAIR. REPAIRED IAW EO B727-5540-11592-A.

Part: SKIN — CORRODED (BS 521-515) · airframe 49,800 hrs · 51,186 cycles

AREA OF SUSPECT CORROSION ON CROWN SKIN BS 521 TO BS 515 BETWEEN STR 2L AND 3L. PLEASE PAINT STRIP AREA, REMOVE FASTENERS IF REQUIRED, REINSPECT AND RECTIFY AS NECESSARY. REPAIRED IAW UPS AUTHORIZATION B727-5330-23323-A

Part: SUPPORT FITTING — CRACKED · airframe 49,800 hrs · 51,186 cycles

RT WING FRONT SPAR TO BODY FITTING HAS SUSPECT CRACK ON OUTBD SIDE OF BOTTLE PIN. FITTING REPLACED IAW DWG 65C13724 AND UPS EO B727-5310-7477.

Part: SKIN — CRACKED (FWD DOOR STR 7L) · airframe 49,800 hrs · 51,186 cycles

INSPECTION TYPE:C SUSPECT SKIN CRACKS AT UPPER FWD CORNER OF FWD ENTRY DOOR CUT OUT BETWEEN STR 7L AND 8L. PLEASE CARRY OUT NDI AND RECTIFY AS NECESSARY IAW SRM ADDENDUM. HFEC CARRIED OUT IAW NDTM 51-00-00 PT6 FIG 4. TWO CRACKS FOUND. DAMAGE REMOVED IAW EO B727-5330-1460-D. HFEC CARRIED OUT ON ALL EXISTING REMOVED FASTENERS, HOLES AND AROUND CUT OUT IAW NDTM 51-00-00PT6 FIG 4 AND 16. NO DEFECTS FOUND. NEW HOLES PITCH IN DOUBLER IAW EO B727-5330-1460D D.

Part: TRUNNION — CRACKED (LH MLG) · airframe 49,800 hrs · 51,186 cycles

LT MLG SUPPORT FITTING HAS CRACK INDICATION IN HOLE B & C ON INB FLANGE AND HOLES E IN COUNTERSINKS. REPAIR AND REPLACE FITTING LT MLG TRUNNION REMOVED AND FOUND CRACKED OUTSIDE REPAIRABLE LIMITS IN UPS EO B727-5740-20666C. TRUNNION REPAIRED IAW UPS AUTHORIZATION B727 -5740-23046-B.

Part: SKIN — CRACKED (BS235 STR16L&17L) · airframe 49,800 hrs · 51,186 cycles

INSPECTION TYPE:C NDT INDICATES 2 CRACKS EMINATING FROM FASTENERS " BS235.8 STR16L-17L. PLEASE REPAIR IAW SRM 53-30-3 FIG 3. FASTENERS REMOVED FROM AFFECTED AREA IAW SRM 51-80-02. AFFECTED AREA CUTOUT IAW SRM 53-30-3. HFEC CARRIED OUT AROUND CUTOUT AND ON REMOVED FASTENERS IAW NDTM 51-00-00PT6 FIG 4 AND FIG 16. NO DEFECTS FOUND. REPAIR DOUBLER AND FILLER FABRICATED IAW SRM 53-30-3 FIG 1. PRIMED REPAIR DOUBLER AND FILLER AND INSTALLED IAW SRM 53-30-3 FIG 1.

Part: SKIN — CRACKED (MID GALLEY DOOR) · airframe 49,800 hrs · 51,186 cycles

FOUND SKIN CRACK AT FASTENER HOLE IN MID GALLEY DOOR CUT OUT, UPPER FWD CORNER. PLEASE CONFIRM WITH NDI AND RECTIFY AS NECESSARY HFEC CARRIED OUT ON FASTENER HOLES COMMON TO REPAIR IAW 727NDTM 51-00- 00 PT6 FIG 16. THREE CRACKS FOUND. REPAIR CARRIED OUT IAW UPS EO AUTHORIZATION NUMBER B727-5330-2320-A

Part: LIGHT — INOPERATIVE (COCKPIT)

BOTH EMERGENCY EXIT LIGHTS ARE INOPERATIVE. REPLACED BATTERIES, OPS CHECK'S NORMAL.

Part: WARNING LIGHT — ILLUMINATED (SMOKE DETECTION)

INSPECTION TYPE:N/A LOWER CARGO MX LIGHT ILLUMINATED INFLIGHT, MAINT. CODES DISPLAYED; A3398. SYSTEM TEST NORMAL PER MM 26-18-00. TESTED SEVERAL TIMES DURING LAYOVER PERIOD WITH NO DEFECTS NOTED AT THIS TIME DI 268782 CLOSED

Part: LIGHT — INOPERATIVE (EVAC SLIDE)

EVACUATION SLIDE ILLUMINATION LIGHT IS INOPERATIVE. REF TO WDM 33-50-02, EVACUATION SLIDE ILLUMINATION LIGHT IS ONLY A PROVISION.

Part: CONTROL UNIT — MALFUNCTIONED (RUDDER)

WITH RUDDER TRIMMED TO ZERO 12 DEGREE LEFT AILERON REQUIRED TO HOLD WINGS LEVEL DEPLOYING SPEED BRAKE SLIGHTLY FIXES PROBLEM. INSPECTED SPOILERS NO DEFECTS FOUND INSPECTED FLIGHT CONTROLS GEN MX PRACTICES 27-00-00 PAGE 201, 203 NO DEFECT FOUND HOWEVER SUSPECT FUEL INBALANCE READING SAME DIP STICKS DIFFER BY TWO INCHES FURTHER T/S REQUIRED REFERENCE D222078.

Part: BATTERY — DISCHARGED (CABIN)

INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS EXTINGUISH SHORTLY AFTER TURNED ON. REPLACED BATT IN FWD AFT EMERG LIGHT ASSY OPS CHECKS GOOD.

Part: STRINGER — CORRODED (FUSELAGE)

INSPECTION TYPE: C, FWD CARGO COMPT BETWEEN STA 680 AND 660, LT SIDE STRINGER 24, CORROSION. CUT OUT SECTION AT BAD STRINGER AREA STA 680 TO STA 660 LT STRINGER 24 INSTALLED REPAIR AS PER B727 SRM 53-10-3 FIG 1 SIDE OF STRINGER DOUBLER REPAIR 11 1/4 INCHES.

Part: KEELBEAM — CRACKED (FUSELAGE)

INSPECTION TYPE:C, RT SIDE OF KEELBEAM APU CUT OUT FWD END HAS A DOUBLER CRACKED AT BS 874 NEXT TO HORIZONTAL STIFFENER. REMOVED OLD DOUBLER REPAIR OF KEEL BEAM AREA AND INSTALLED NEW DOUBLER REPAIR AT SAME AREA BS 874 AS PER B727 SRM 51-10-01.

Part: WEB — CRACKED (WING BOX)

INSPECTION TYPE:C LOWER F.S. AT WING CENTER SECTION APROX BETWEEN BS 800 TO 810 AND LBL 13 WEB IS CORRODED. REMOVE WEB AT LWR FUSELAGE CENTER SECTION BETWEEN BS 800 TO BS 810 LBL 13 WEB AS PER B727 SRM 51-30-2. REPLACED DAMAGED WEB LOWER CENTER WING AT BS 800 TO 810 LBL 13 WEB AS PER B727 SRM 51-30-2.

Part: WEB — CRACKED (WING BOX)

INSPECTION TYPE:C LOWER F.S. AT WING CENTER SECTION APROX 770 AND LBL 13 WEB IS CORRODED. REMOVED WEB AT LOWER FUSELAGE CENTER SECTION AT BS 770 AND LBL13 WEB AS PER B727 SRM 51-30-02. REPLACED DAMAGE WEB LOWER CENTER WING AT BS 770 AND LBL 13 WEB AS PER B 727 SRM 51-30-2.

Part: WEB — CRACKED (WING BOX)

INSPECTION TYPE:C LOWER F.S. AT WING CENTER SECTION BETWEEN BS 775 TO BS 800 AND RBL 13 WEBS CRACKED AND CORRODED. REMOVE WEB AT LWR FUSELAGE CENTER SECTION BETWEEN 767 TO 830 RBL13 AS PER B727 SRM 51-30-02 REMEOVED AND REPLACED DAMAGE WEB LOWER CENTER WING SECTION BS 775 TO 800 RBL 13 AS PER SRM 51-30-02.

Part: SEAT TRACK — GOUGED (FUSELAGE)

INSPECTION TYPE: C, MAIN CARGO DECK FUSELAGE STATION 1130 LBL 45 SEAT TRACK TONGUES ARE NICKED AND GOUGED REPLACED DAMAGED SECTION OF SEAT TRACK FROM BS 1110 TO STA 1130 LBL 45

Part: PRESSURE PANEL — CRACKED (NLG WW)

INSPECTION TYPE: C, NOSE WHEEL WELL RT SIDE CRACKED AT BS 286.5 TO BS 294.5 WL 160 LOOKING FROM INSIDE TUNNEL. CUT OUT DAMAGE AREA, NDT CUT OUT, AND INSTALLED DOUBLER REPAIR AS PER B727 SRM 51-40-2 FIG.1

Part: PULLEY — WORN (TE FLAPS)

INSPECTION TYPE:N/A, ATB DURING FLAP RETRACTION OUTBOARD FLAPS WENT TO 2 DEGREES, MATCHED FL AND LE, INBOARD FLAPS JAMMED AT R-5 DEGREES L-15 DEGREES. REMOVED AND REPLACED LEFT INBOARD FLAP TRANSMITTER CABLE AND PULLEY PER MM 27-52-02. OPS CK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN)

INSPECTION TYPE:N/A, EMERGENCY EXIT LIGHT INOP. REPLACED LIGHT ASSEMBLE AND BATTERIES OPS CK GOOD.

Part: BATTERY PACK — INOPERATIVE (CABIN)

EMERGENCY LIGHT FWD ENTRY DOOR INOPERATIVE. R/R EMERGENCY LIGHT AND BATTERY PACK. OPS CHECKED GOOD. P/N 10-00067 -9 SN ON 1315 SN OFF 900

Part: LIGHT — INOPERATIVE (CABIN)

EMERGENCY LIGHT AT MAIN ENTRANCE DOOR IS INOPRATIVE. R/R EXIT LIGHT BATTERY ALL OPS CHECKS GOOD

Part: LIGHT — FAILED (CABIN)

INSPECTION TYPE:N/A, REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSY (P/N 10-0067-7) (S/N 20261) OFF, REF IPC 33-50-00-20-15. REMOVED EMERGENCY EXIT LIGHT ASSY, OPS CHECK GOOD.

Part: LIGHT — INOP (CABIN)

INSPECTION TYPE:N/A, BORROWED PART INSTALLED IN EMERGENCY EXIT LIGHT L1 POSITION. REMOVED AND REPLACED EMERGENCY EXIT LIGHT IN L1 POSITION (P/N 10-0067-9) ON, (P/N 10- 0067-7) OFF, (S/N 2151) ON, (S/N 20261) OFF.

Part: BATTERY PACK — DISCHARGED (COCKPIT)

INSPECTION TYPE:N/A, COCKPIT EMERGENCY LIGHTS ABOVE DOOR INOP, FAILED TO TEST. REMOVED UNIT FROM A/C, PUT BATTERIES ON CHARGE, REINSTALLED BATTS IN A/C AND OPS OK.

Part: LIGHT — INOPERATIVE (FLT DECK DOOR)

INSPECTION TYPE-N/A, EMER EXIT LIGHT OVER FLIGHT DECK DOOR WILL NOT STAY IN IT'S ELECTRICAL SOCKET CAUSING IT TO STAY ON IN FLIGHT. REINSTALLED EMER EXIT LIGHT PROPERLY UNTILL LATCHES ENGAGED, EMER EXIT LIGHT, OPS CHECK GOOD.

Part: BATTERIES — DISCHARGED (FLIGHT DECK)

INSPECTION TYPE-N/A, EMER EXIT LIGHT OVER FLIGHT DECK DOOR INOP. REPLACED WITH NEW BATTERIES, LIGHT OPS CHECKED OK.

Part: LIGHT — INOPERATIVE (CABIN)

INSPECTION TYPE-N/A, EMERGENCY EXIT LIGHTS DO NOT TURN ON WITH SWITCH IN ON POSITION. REPLACED BATT ON EMERGENCY EXIT LIGHT, OPS CKS NORMAL.

Part: LIGHT — INOPERATIVE (COCKPIT)

EMERGENCY EXIT LIGHT IN COCKPIT IS NOT SECURE AND CAME ON DURING LANDING ROLL OUT. RESECURED, OPS CHECKED GOOD.

Part: SHEAR WEB — CORRODED (BS 1131)

INSPECTION TYPE-C, SHEAR WEB STA 1131 RBL 62 WL 208 HAS CORROSION AT NUTPLATE HOLE. CORROSION REMOVAL WAS OUT OF LIMITS. REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS, INSTALLED ALL WORK DONE IAW EO NR 727-53-1851 AND TRAMCO EWO 97-2020.

Part: SUPPORT FITTING — CRACKED (NR 3 SPOILER)

INSPECTION TYPE-C, NR 3 SPOILER SUPPORT FITTING ATTACH ANGLE IS CRACKED AT LOWER I/B ATTACH BOLT HOLE. REMOVED CRACKED NR 3 SPOILER SUPPORT FITTING ATTACH ANGLE. REPLACED PER SRM 51-30-2, MM 27-61-81, 27-61-0.

Part: SKIN — CRACKED (LT TE FOREFLAP)

INSPECTION TYPE-C, LT WING I/B FOREFLAP L/E SKIN CRACKED FWD OF DEFLECTOR DOOR I/B END. REMOVED AND INSTALLED SERVICEABLE FOREFLAP, WORK DONE IAW MM 27-51-01.

Part: ANGLE — CORRODED (BS 178)

INSPECTION TYPE-C, CORROSION FOUND ON RT LOWER L-ANGLE RBL 24 BS 178 WL 207. FOUND CORROSION TO BE OUT OF LIMITS PER SRM 53-10-1. REPLACED L-ANGLE PER SRM 51-40-4, 53-10-2, 51-10-1, 51-10-6, 51-30-2.

Part: HINGE — CORRODED (NR 5 LE FLAP)

INSPECTION TYPE-C, NR 5 K-FLAP CENTER HINGE FITTING HAS SEVERAL SPOTS OF CORROSION. REMOVED AND INSTALLED NEW HINGE ASSY, WORK DONE IAW SRM 51-30-2, 51-30-5, 51-30-8, 51-10-2, 51-20-04, MM 27-87-01.

Part: RIB — CRACKED (NR 3 LE SLAT)

INSPECTION TYPE-C, NR 3 SLAT 1ST RIB I/B OF ACTUATOR ROD END CRACKED. REPLACED WITH NEW SLAT ASSY, WORK DONE IAW MM 27-81-11.

Part: FITTING — CORROSION (BS 1073)

INSPECTION TYPE-C, CORROSION ON FAIRING ATTACH FITTING AT BS 1073 STR 19L. FABRICATED NEW FITTING AND INSTALLED, WORK DONE IAW 53-10-1, 51-10-2, 51-10-1 AND MM 51-20-151.

Part: POS SWITCH — FAILED (NLG)

CREW REPORTED ON FINAL, THE GREEN NOSE GEAR LIGHT SUDDENLY WENT OUT AND THE GEAR HORN CAME ON. GEAR WAS CYCLED AND ALL THREE GEAR LIGHTS ILLUMINATED AGAIN. MAINTENANCE REMOVED AND REPLACED THE NOSE GEAR POSITION SWITCH AND THE NOSE GEAR LOCK SWITCH IAW MM 32-61-21.

Part: SPAR — CORRODED (WS 740)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION LOWER FRONT SPAR CHORD AT STA 740 WL 167 LBL 37. REPLACED IAW SRM 51-30-2.

Part: STIFFENER — CRACKED (WS 594)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND CRACKED VERTICAL STIFFENER AT FS 594 ON L/W L/E. REPLACED IAW SRM 51-30-2, 51-20-4, 51-10-2.

Part: STIFFENER — CRACKED (WS 553)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND CRACKED VERTICAL STIFFENER AT FS 553 ON L/W L/E. REPLACED IAW SRM 51-30-2, M/M 36-00-01.

Part: RIB — CRACKED (WING)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND CRACKED RIB ON SLAT TRACK ON O/B SIDE. REPLACED IAW SRM 57-51-31 AND 51-30-2.

Part: STIFFENER — CRACKED (WS 598)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND CRACKED VERTICAL STIFFENER AT FS 598 ON L/W L/E. REPLACED IAW SRM 51-30-2, 51-20-4, 51-10-2.

Part: STRINGER — CORRODED (BS 484)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON STRINGER FLANGE AT BS 484, STR 24 LT WL 157. REPAIRED IAW SRM 53-10-6, 53-10-3, 51-30-2.

Part: CORE — DAMAGED (NR 1 SPOILER)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND NR 1 SPOILER CORE DAMAGED AND CONTAMINATED. REPLACED IAW M/M 27-61-01.

Part: FLOORBEAMS — CORRODED (BS 580)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION AROUND NUTPLATES ON FLOORBEAMS AT BS 580, RBL 49 TO 59, WL 201. REPAIRED IAW B727-5310-7176-A, SRM 53-10-1.

Part: STRAP — CORRODED (BS 1025-1148)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON BL 0 STABILIZER STRAP BS 1025 TO 1148 AROUND NUTPLATES. REPLACED IAW SRM 51-30-8, 51-30-2, 51-20-4, 51-10-6, 51-10-2, 51-10-1.

Part: CORE — DAMAGED (NR 7 SPOILER)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND NR 7 SPOILER CORE DAMAGED AND CONTAMINATED. REPLACED IAW M/M 27-62-01.

Part: SPOILER — DAMAGED (WING)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND NR 3 SPOILER CORE DAMAGED AND CONTAMINATED. REPLACED IAW M/M 27-61-01.

Part: ANGLE — CRACKED (WS 100)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND CRACKED ON I/B ATTACH ANGLE AT BOTTOM OF TWO HOLES IN RIGHT WING AT WL 208 FS 100.0. REPAIRED IAW SRM 51-30-2.

Part: CORE — DAMAGED (NR 2 SPOILER)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND NR 2 SPOILER CORE DAMAGED AND CONTAMINATED. REPLACED IAW M/M 27-61-01.

Part: FLOORBEAM — CORRODED (BS 64)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON FLOORBEAM AT STA 64.0 LBL 30 WL 208. REPLACED IAW EO B727-5310-7190.

Part: RIB — CORRODED (NR 4 LE SLAT)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND NR 4 SLAT O/B TRACK I/B RIB AND FITTING CORRODED. REPLACED IAW SRM 51-10-1, 51-30-2.

Part: CORE — DAMAGED (NR 13 SPOILER)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND NR 13 SPOILER CORE DAMAGED AND CONTAMINATED. REPLACED IAW M/M 27-62-01.

Part: ANGLE — CORRODED (BS 600)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION AROUND NUTPLATES ON FLOORBEAM ANGLE AT BS 600 RBL 49 TO 59 WL 201. REPAIRED IAW SRM 53-10-1, 51-10-2, M/M 51-20-121, 51-30-2.

Part: STRAP — CORRODED (BS 519-660)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON STRAP AT BS 519 TO 660, BL 0, WL 201 AROUND NUTPLATE HOLES ON LOWER SIDE. ALSO, AT LBL 2, RBL 2 AT BS 612 TO 628. REPLACED IAW EO B727-5310-7178-A.

Part: CREASE BEAM — CORRODED (BS 1130)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON CREASE BEAM AT BS 1130 WL 208 RBL 64. REPLACED IAW SRM 53-10-1, 51-30-2, 51-20-4.

Part: RIB — CORRODED (NR 5 LE SLAT)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND NR 5 SLAT O/B TRACK O/B RIB CORRODED. REPLACED IAW SRM 51-30-2, 51-10-1.

Part: K-FLAP — CORRODED (NR 1)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND NR 1 K-FLAP CORRODED. REPLACED IAW M/M 27-81-01.

Part: SIDE LOAD BEAM — CORRODED (BS 740)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON SIDE LOAD BEAM AT STA 740 WL 170 LBL 34 TO RBL 34. REPAIRED IAW 727-53-1628.

Part: SPOILER — DAMAGED (NR 5 SPOILER)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND NR 5 SPOILER CORE DAMAGED AND CONTAMINATED. REPLACED IAW M/M 27-61-01.

Part: FRAME — CORRODED (BS 344)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON SIDE OF FRAME AT BS 344 STR 22 RT, WL 177. REPAIRED IAW SRM 51-40-3.

Part: STRINGER — CORRODED (BS 620)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON STRINGER 21R AT BS 620. REPLACED IAW SRM 53-10-3.

Part: ATTACH LUG — CORRODED (NR 3 LE FLAP)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND NR 3 K-FLAP CORROSION ON I/B ATTACH LUG. REPLACED IAW M/M 27-81-01.

Part: FLOORBEAM — CORRODED (BS 1050)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON FLOORBEAM LOWER CHORD AT BS 1050 WL 199 LBL 31 TO RBL 45. REPLACED IAW SRM 51-30-2 AND EO B727-5310-7183-A.

Part: RIB — CRACKED (NR 1 LE SLAT)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND CRACKED RIB ON NR 1 SLAT ON LT SIDE NR 5 RIB FROM END. REPLACED IAW OHM 57-51-31, SRM 51-30-2.

Part: ATTACH LUG — CORRODED (NR 5 LE FLAP)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND NR 5 K-FLAP CORROSION ON O/B ATTACH LUG. REPLACED IAW M/M 27-81-01.

Part: BULKHEAD — CRACKED (BS 950)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND CRACK IN BS 950 BULKHEAD AT LBL 15 WL 175. REPAIRED IAW SRM 53-10-9.

Part: EXPANSION LINK — CORRODED (BS 740)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON EXPANSION LINK BUSING HOLE AT RBL 13 BS 740 WL 165. REPAIRED IAW SRM 51-30-2.

Part: SKIN — CORRODED (BS 689)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON SKIN AT BS 689 STR 19 RT. REPAIRED IAW EO B727-5330-0509.

Part: FLOORBEAM — CORRODED (BS 380)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION UNDER NUTPLATE STA 380 RBL 48 WL 208 AND LBL 45 TO 62.5 WL 208. REPAIRED IAW SRM 53-10-1, 53-10-8.

Part: FAILSAFE — CORRODED (FS 480)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON UNDERSIDE OF FAILSAFE 480, STR 25 LT WL 160. REPAIRED IAW SRM 51-40-3.

Part: FRAME — CORRODED (BS 1050)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION IN AFT CARGO BAY BS 1050 STR 26R WL 160, TOP OF FRAME AROUND 2 NUTPLATES. REPAIRED IAW SRM 51-40-3.

Part: FLOORBEAM — CORRODED (BS 277)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION AROUND NUTPLATES ON FLOORBEAM AT STA 277 WL 208 RBL 15 TO 40. REPAIRED IAW SRM 53-10-1, 51-40-4.

Part: INTERCOSTAL — CORROSION (FS 259)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON INTERCOSTAL AT STA 259 TO 277 WL 208 LBL 11. REPAIRED IAW SRM 51-30-2, 51-10-1.

Part: RIB — CRACKED (WS 171.5)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CRACKED UPPER RIB CHORD AT FWD VENT BOX FWD FLANGE 7 INCHES AFT OF FRONT SPAR ON LEFT WING AT STA 171.5. REPAIRED IAW SRM 51-40-04.

Part: FLOORBEAM — CORROSION (FS 740)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON FLOORBEAM UNDERSIDE OF UPPER CHORD AT STA 740, BL 0-LBL 25, WL 208.5. REPAIRED IAW SRM 53-10-1, 51-30-5, 51-30-2, 51-10-1.

Part: FRAME — CORROSION (BS 640)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION AROUND FASTENER HOLES ON TOP OF FRAME AT BS 640 BETWEEN STR 22 TO 21RT. REPAIRED IAW SRM 51-40-3, 53-10-2, 53-10-1, 53-10-2.

Part: SEAT TRACK — CORROSION (FS 344-360)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON SEAT TRACK FLANGE AT STA 344 TO 360 LBL 62 WL 208. REPAIRED IAW SRM 53-10-5.

Part: RIB — CRACKED (NR 5 LE SLAT)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CRACKED RIGHT WING NR 5 SLAT ACTUATOR O/B RIB AT FWD END OF SLAT ACTUATOR ROD END ATTACHING RIB. REPLACED IAW SRM 51-10-1.

Part: FLOORBEAM — CORROSION (FS 640)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON FLOORBEAM STA 640, RBL 29 TO 60, WL 208, AFT SIDE OF UPPER CHORD. REPAIRED IAW SRM 51-30-2, 51-10-8.

Part: FLOORBEAM — CORROSION (FS 900)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON FLOORBEAM LOWER FLANGE AND SUPPORT STRAP AT STA 900 LBL 25 TO LBL 60 WL 200 AFT SIDE. REPAIRED IAW SRM 53-10-1, 53-10-8, 51-30-2, 51-10-1.

Part: T-CHORD — CRACKED (VERT STAB)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CRACK ON T-CHORD FOR PANEL 9707 ON VERTICAL FIN AT FIN STA 225.6 RT SIDE. REPAIRED IAW SRM 51-30-2.

Part: FLOORBEAM — CORRODED (FS 910)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON FLOORBEAM LOWER FLANGE FWD SIDE AT STA 910 WL 200 RBL 25-RBL 55. REPAIRED IAW SRM 51-30-2, 51-10-2, 51-20-4, 53-10-8.

Part: CLIP — CORROSION (FS 954)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON STRINGER TO FORGING ATTACH CLIP IN AFT BAY AT BS 954, WL 154 STR 25L. REPAIRED IAW SRM 51-10-1, 53-10-2, 51-10-6, 51-30-5, 51-30-2, M/M 51-10-151.

Part: FLOORBEAM — CORROSION (FS 1090)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON FLOORBEAM ON FWD SIDE OF UPPER CHORD AROUND NUTPLATE HOLE AT STA 1090 LBL 60 WL 208. REPAIRED IAW SRM 53-10-1.

Part: STRINGER — CRACKED (FS 400)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CRACK ON STRINGER 15R AT BS 400. REPAIRED IAW SRM 53-10-3.

Part: INTERCOSTAL — CORROSION (FS 256)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON INTERCOSTAL AT STA 256 TO 277 WL 208 RBL 15. REPAIRED IAW SRM 51-10-4, 51-30-2, M/M 32-34-71.

Part: SEAT TRACK — CORROSION (FS 344)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION SEAT TRACK AT STA 344 RBL 25 WL 208. REPAIRED IAW SRM 53-10-1, 53-10-5.

Part: SEAT TRACK — CORROSION (FS 678)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION SEAT TRACK FLANGE AT STA 678 RBL 24 WL 208. REPAIRED IAW SRM 51-30-2, 51-10-1, 51-10-6, 53-10-1.

Part: WEB — CRACKED (FUSELAGE)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CRACK EMITTING FROM FASTENER HOLE IN WEB AT STA 259.5 WL 192.5 LBL 21. REPAIRED IAW SRM 53-10-02, 51-30-2, 51-40-02.

Part: FLOORBEAM — CORRODED (FS 312/328)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION AROUND NUTPLATE HOLES ON FLOORBEAMS AT STA 312 AND 328, BL 0 TO LBL 60, WL 208. REPAIRED IAW SRM 51-10-2, 51-20-4, 53-10-8, 53-10-1, M/M 51-20-151.

Part: FRAME — CORROSION (CARGO COMPT)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON WEB UPPER SIDE AND END FRAME OF AFT CARGO FLOOR. REPAIRED IAW SRM 51-20-3, 51-40-2, 51-10-1.

Part: FLOOR BEAM — CORROSION (BS 344)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION AROUND NUTPLATE HOLES ON TOP FLANGE OF FLOOR BEAM STA 344, RBL 52 - LBL 46, WL 208. REPAIRED IAW SRM 51-30-2, 53-10-8, 51-10-6.

Part: STIFFENER — CRACKED (RT ELEVATOR)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND CRACKED LOWER SKIN STIFFENER ON RT ELEVATOR AT ELEV STA 17.2 INSIDE ACCESS PANEL 9406 APPROX 5.25 INCHES AFT OF FRONT SPAR CHORD. REPAIRED IAW SRM 51-20-2, 51-30-2, 51-20-1, 55-20-2.

Part: FLOOR BEAM — CORRODED (BS 306-312)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON CREASE BEAM BS 306-312 RBL 56, WL 208 AT FLOORBOARD FASTENER HOLES. REPAIRED IAW SRM 51-40-3.

Part: STRINGER — CORRODED (BS 488)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON TOP STRINGER FLANGE AT BS 488, STR 24 LT WL 165. REPAIRED IAW SRM 53-10-3, 51-30-2, M/M 51-20-151.

Part: BEAM — CORRODED (BS 760-850)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION AROUND SEVERAL NUTPLATE HOLES ON UNDERSIDE LONGITUDINAL BEAM AT BS 760-850, RBL 45, WL 208. REPAIRED IAW SRM 51-10-1, 53-10-1, 53-10-2.

Part: CLIP — CRACKED (FS 1010)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND CRACKED STRINGER CLIPS STA 1010 STR 6, 8 RT. REPLACED IAW SRM 51-30-2.

Part: INTERCOSTAL — CORROSION (BS 304-344)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION AROUND NUTPLATE HOLES ON INTERCOSTAL STA 304-344, LBL 30, WL 208. REPAIRED IAW SRM 51-30-2, 53-10-1, 51-10-2, M/M 51-20-15.

Part: WEB — CORRODED (BS 870)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON TOP EDGE OF STA 870 WHEELWELL WEB RBL 0-65 WL 178. REPAIRED IAW SRM 53-10-9, 51-30-2.

Part: ANGLE — CORRODED (FUSELAGE)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON INTERCOSTAL AND SUPPORT ANGLE BETWEEN END FRAME AND NR 1 TRANSVERSE BEAM 15 INCHES FWD OF AFT EDGE. REPAIRED IAW SRM 53-10-1, 51-30-2, 51-10-6.

Part: FRAME — CORRODED (FS 1130)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON FRAME AT STA 1130, STR 8-10, RT SIDE. REPAIRED IAW SRM 51-40-3, 53-10-1, 51-10-2, M/M 51-20-151.

Part: WEB — CRACKED (BS 348-360)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND CRACK ON HORIZ. WEB BETWEEN FRAME AT 348 TO 360, LT WL 216. REPAIRED IAW SRM 51-10-07, M/M 51-20-151, SRM 51-40-2.

Part: STIFFENER — CORRODED (BS 320)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON STIFFENER ON SIDE PANEL OF NOSE GEAR WHEELWELL (INSIDE DOG HOUSE) BS 320, RBL 14, WL 182. REPLACED IAW SRM 51-10-1, 51-30-2, 51-20-4.

Part: RETAINER — CRACKED (TE FLAPS)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND CRACKED L/W O/B MID-FLAP AFT LOWER CHORD AND ATTACHED BULB SEAL RETAINER 21 INCHES FROM O/B END. REPAIRED IAW SRM 51-10-1, 51-30-2.

Part: STATIC WICK — CORRODED (ELEVATOR)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON ELEVATOR O/B STATIC WICK BASE. REPAIRED IAW SRM 55-20-3, M/M 51-20-21, 51-20-31, 51-20-13, 23-61-00.

Part: FRAME — CRACKED (FS 340)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND CRACK ON FLANGE OF FRAME AT BS 340, BETWEEN STR 11 AND STR 12R BEHIND SIDE WALL SUPPORT. REPAIRED IAW SRM 51-40-3, 51-10-2, 51-30-2.

Part: BEAM — CORRODED (BS 760-850)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION AROUND SEVERAL NUTPLATE HOLES ON UNDERSIDE LONGITUDINAL BEAM AT BS 760-850, LBL 25, WL 208. REPAIRED IAW SRM 53-10-1, 51-10-6, 51-10-2, M/M 51-20-00.

Part: BEAM — CORRODED (BS 760-850)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION AROUND SEVERAL NUTPLATE HOLES ON UNDERSIDE LONGITUDINAL BEAM AT BS 760-850, LBL 45, WL 208. REPAIRED IAW SRM 53-10-1, 51-10-6, 51-10-2, M/M 51-20-00.

Part: SEAT TRACK — CORRODED (BS 472-480)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORRODED SEAT TRACK STRAPS STA 472-480, LBL 45, WL 208. REPLACED IAW SRM 51-30-2, M/M 51-20-151.

Part: CLIP — CRACKED (BS 1070)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND CRACKED STRINGER CLIPS STA 1070 STR 5, 8 RT. REPLACED IAW SRM 51-30-2, 51-10-1.

Part: FOREFLAP — DELAMINATED (LT WING)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND DELAMINATION OF LT I/B FOREFLAP UNDER RUB STRIP ON I/B END. REPAIRED IAW M/M 51-51-11.

Part: SKIN — CORROSION (BS 420)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION AROUND NUTPLATE HOLES STA 420, LBL 45 TO 62.5, WL 208. REPAIRED IAW SRM 53-10-8.

Part: STIFFENER — CORRODED (BS 302)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON STIFFENER AT BS 302, WL 180, ON TOP OF PANEL OF NOSE GEAR WELL RBL 3. REPLACED IAW SRM 51-30-2, 51-30-5.

Part: INTERCOSTAL — CORRODED (FS 240-250)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON INTERCOSTAL AT B.S. 240-250, RT WL 185, RBL 42. REPAIRED IAW SRM 51-20-01, 20-43-03, 20-44-04, 51-30-2.

Part: STUB BEAM — CORRODED (BS 762)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION AROUND FASTENER HOLES ON STUB BEAM AT BS 762, LBL 55 UNDERSIDE WL 207. REPAIRED IAW SRM 51-40-4.

Part: FLOOR BEAM — CORRODED (BS 680)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION FLOOR BEAM STA 680, RBL 37-60, WL 208 UPPER AND LOWER SIDE OF UPPER CHORD.

Part: TAB — DELAMINATED (RUDDER)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND DELAMINATION OF UPPER RUDDER TAB (SEVEN AREAS), CORE CONTAMINATED WITH WATER. REPAIRED IAW SRM 51-40-6, M/M 51-20-151.

Part: WARN LIGHTS — MALFUNCTION (FLIGHT DECK)

PILOT REPORTED LEFT MAIN GEAR DOOR INDICATED NOT UP AND LOCKED ON FLIGHT DECK GEAR PANEL. LIGHT EXTINGUISHED ON F/E PANEL. CHECKLIST WAS C/W AND THE GEAR WAS EXTENDED AND RETRACTED. BOTH LIGHTS DID NOT GO OUT. CLEANED LEFT GEAR DOOR SWITCH AND CHECKED SECURITY, FOUND OK. OPS CHECKED OK.