N936UP

Part: LIGHT — MALFUNCTIONED (COCKPIT)

INSPECTION TYPE: N/A EMERGENCY EXIT LIGHT ILLUMINATED IN FLIGHT COULD NOT RESET. STAYED ON. ACCOMPLISHED EMERGENCY LIGHTING ADJUSTMENT/TEST IAW MM 33-50-01-5. SYSTEM CHECKS GOOD. UNABLE TO DUPLICATE PROBLEM.

Part: SHEAR TIE — CRACKED (FS 441 S26L) · airframe 48,258 hrs · 31,358 cycles

INSPECTION TYPE:SV SHEAR TIE CRACKED AT STA 441 STR 26L. REMOVED CRACKED SHEAR TIE AT STA 441 STR 26L IAW SRM 51-30-02, FABRICATED AND INSTALLED SHEAR TIE AT STA 441 STR 26L IAW DWG 6913293 AND SRM 51-30-02.

Part: CONNECTOR — INOPERATIVE (NAV ANTENNA)

IN FLIGHT, CAPTAIN'S VOR/FLAG INDICATED RED. STATIONS SELECTED ALL ALONG FLIGHT WITH NO GOOD INDICATION ON EASI. TAE NAV 1 DENTS WERE GOOD, DME AND RMI NEEDLES MATCHED FO'S INDICATIONS. NORMAL AND OVERRIDE WERE ALSO SELECTED ON RADIO CONTROL. DIVERSION. REMOVED AND REINSTALLED NR 1 NAV ANT COAX CONNECTOR IN E/E LAMP, OPS CK PER MM 34-31-22.

Part: MOUNT — CORRODED (NR 3 ENGINE) · airframe 40,018 hrs · 31,168 cycles

INSPECTION TYPE:C NR 3 PYLON FWD ENGINE MOUNT, AFT O/B HOLE HAS PITTING CORROSION IN BORE OF HOLE. REPAIRED IAW EO B727-5440-11592-A.

Part: SKIN — CORRODED (BS 1080-1139) · airframe 40,018 hrs · 31,168 cycles

INSPECTION TYPE:C EVIDENCE OF FRETTING FOUND AT BS 1080 TO 1139.5 FROM STR 24L TO STR 26 L ON THE SKIN. SKIN REPLACMENT REQUIRED AT THIS LOCATION, CARRIED OUT IAW AAAE EO NR 2006-003-001 - UPS REF NR B727-5330-23687-A.

Part: MOUNT — CORRODED (NR 3 PYLON) · airframe 40,018 hrs · 31,168 cycles

INSPECTION TYPE:C NR 3 PYLON FWD MOUNT, FWD I/B HOLE HAS PITTING CORROSION. REPAIRED IAW EO B727-5440-11592-A.

Part: MOUNT — CORRODED (NR 3 ENG) · airframe 40,018 hrs · 31,168 cycles

INSPECTION TYPE:C NR 3 PYLON FWD ENGINE MOUNT, FWD O/B HOLE PITTING CORROSION IN BORE OF HOLE. REPAIR CARRIED OUT IAW EO B727-5440-11592-A.

Part: MOUNT — CORRODED (NR 1 ENGINE) · airframe 40,018 hrs · 31,168 cycles

INSPECTION TYPE:A ENG NR 1 PYLON FWD ENGINE MOUNT, AFT O/B HOLE PITTING CORROSION IN BORE OF HOLE. REPAIRED IAW EO B727-5440-11592-A.

Part: MOUNT — CORRODED (NR 1 ENGINE) · airframe 40,018 hrs · 31,168 cycles

INSPECTION TYPE:C NR 1 PYLON FWD ENGINE MOUNT FWD O/B HOLE, HAS PITTING CORROSION IN BORE OF HOLE. REPAIRED IAW EO B727-5440-11592-A.

Part: FLOORBEAM — CORRODED (BS360 - LBL67) · airframe 40,018 hrs · 31,168 cycles

INSPECTION TYPE:C ON REMOVAL OF FLOORBOARD AT BS 360 EVIDENCE OF CORROSION FOUND. UPPER CHORD OF FLOORBEAM REMOVED BETWEEN RBL 12 AND LBL 67 AT BS 360. REPAIR CARRIED OUT IAW SRM NR 53-10-5.

Part: BEAM — CORRODED (BS 740) · airframe 40,018 hrs · 31,168 cycles

INSPECTION TYPE:C CORROSION FOUND ON RT FWD FACE OF HORIZONTAL BEAM ATTACH POINT TO BS 740 FITTING. REPLACED HORIZONTAL BEAM IAW SRM NR 51-30-2 AND DRW NO.65-15927.

Part: ANGLE — CORRODED (BS 1428 R/H FUSE) · airframe 48,018 hrs · 31,168 cycles

INSPECTION TYPE-C RT FUSE ABOVE NR 2 ENG AT THE ANGLE BETWEEN FUSE AND VERT STAB HAS LIGHT SURFACE CORROSION AT BS1428 TO 1464. DAMAGED ANGLE REMOVED AND REPLACEMENT ANGLE FABRICATED IAW DRW. NR QF5314263. REPLACEMENT ANGLE INSTALLED IAW SRM51-30-02 AND DRW. QF531 4001.

Part: MOUNT — CORRODED (NR 1 ENGINE) · airframe 40,018 hrs · 31,168 cycles

INSPECTION TYPE:C NR 1 PYLON FWD ENGINE MOUNT, FWD I/B HOLE, PITTING CORROSION IN THE BORE OF HOLE. REPAIRED IAW EO B727-5440-11592-A.

Part: OXYGEN MASK — INOPERATIVE (COCKPIT)

CREW PREFLIGHT - F/O O2 MASK WOULD NOT TRANSMIT. REMOVED AND REPLACED F/O'S 02 MASK ASSY. OPS CKS GOOD IAW MM 35-11-00.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 47,543 hrs · 30,806 cycles

INSPECTION TYPE: C, DURING INSPECTION OF SKIN REPAIR, AT 1334 LT SIDE AFT AIRSTAIRS, SKIN ATTACH ANGLE FOUND CORRODED. REPLACED ATTACH ANGLE IAW SRM 51-10-01.

Part: SUPPORT BRACKET — CRACKED (NR 5 FLAP TRACK) · airframe 47,543 hrs · 30,806 cycles

INSPECTION TYPE: C, SUPPORT BRACKET FOR NR 5 FWD FLAP TRACK FAIRING FOUND CRACKED ON O/B SIDE OF NR 5 FLAP TRACK. SUPPORT BRACKET REMOVED IAW SRM 51-30-02, NEW ANGLE FABRICATED IAW SRM 51-20-01, ANGLE PROTECTED IAW SRM 51-10-01, ANGLE INSTALLED ON FLAP TRACK IAW SRM 51-30-02.

Part: STRAP — CORRODED (FLOOR PANEL) · airframe 47,543 hrs · 30,806 cycles

INSPECTION TYPE: C ON INSP FLOOR PANEL SPLICE STRAP FOUND BADLY CORRODED AT BS 520 BETWEEN RBL 24 AND LBL 24. SPLICE STRAP REPLACED IAW SRM 51-20-01

Part: LIGHT — DEFECTIVE (COCKPIT) · airframe 47,543 hrs · 30,806 cycles

INSPECTION TYPE: C-COCKPIT EMERGENCY LIGHT DOES NOT ILLUMINATE WITH SWITCH ON P5 PANEL TO ON. LIGHT ASSEMBLY FOUND DEFECTIVE IAW WDM 33-51-01. LIGHT ASSY REPLACED IAW MM 33-50-01. FUNCTION CHECKED OK.

Part: CASTING — CRACKED (NR 7 FLAP TRACK) · airframe 47,543 hrs · 30,806 cycles

INSPECTION TYPE: C, CRACK ON NR 7 FLAP TRACK CASTING ON VERTICAL FLANGE SECOND FROM I/B. HFEC CARRIED OUT - CRACKS CONFIRMED AND ENDS MARKED. STOP DRILLED CRACKS IAW SRM 51-10-1. OUTSIDE LIMITS PER SRM 51-10-6. CASTING REPLACED AND INSTALLED IAW DRG 65-16201.

Part: STIFFENER — CORRODED (MLG WW) · airframe 47,543 hrs · 30,806 cycles

INSPECTION TYPE: C, HORIZONTAL STIFFNER CORRODED AFT OF APU EXHAUST PORT ON LOWER SURFACE OF UPPER PANEL AT 2 LOCATIONS. CORROSION FOUND TO BE OUTSIDE LIMITS. STIFFNER REMOVED IAW SRM 51-30-02. NEW STIFFNER INSTALLED IAW DRG 65-21655.

Part: SKIN — CORRODED (FUSELAGE) · airframe 47,543 hrs · 30,806 cycles

INSPECTION TYPE:C, SUSPECT CORROSION BS 1340 BETWEEN STR 8L AND 9L DAMAGED SKIN REMOVED FROM BS 1323 TO BS 1342, FROM FIN TO STR 10L IAW SRM 51-10-6 AND REPAIRED IAW AAAE EO 2004-077-007. REF UPS FILE 727-53-20160.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 47,543 hrs · 30,806 cycles

INSPECTION TYPE: C, CRACK ON DOUBLER RT SIDE BS 1444 APPROX. CRACK CUT OUT IAW SRM 51-40-02. HFEC CARRIED OUT IAW NDT MANUAL 51- 00-00 PT 6 FIG 4. NO DEFECTS FOUND. REPAIR DOUBLER FABRICATED IAW SRM 51-40-02 AND INSTALLED IAW SRM 51-30-02.

Part: SPAR — CORRODED (LT WING) · airframe 47,543 hrs · 30,806 cycles

INSPECTION TYPE: C, CRACK INDICATION AT WS 205 ON LT UPPER CHORD REAR SPAR. REPAIR CARRIED OUT IAW AAAE EO 2004-077-005. REF UPS EO B727-5710-20995.

Part: SKIN — DEBONDED (LT OB MIDFLAP) · airframe 47,543 hrs · 30,806 cycles

INSPECTION TYPE:C LT OB MIDFLAP T-EDGE WEDGE UPPER SKIN DISBOND 45 INCHES IB OF OB EDGE. DAMAGE REPAIRED IAW SRM 51-40-5

Part: LAP JOINT — CORRODED (FUSELAGE) · airframe 47,543 hrs · 30,806 cycles

INSPECTION TYPE: C, SUSPECT CORROSION AT LAP JOINT S19L BETWEEN BS 390 AND BS 441, CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 51-30-02. REPAIR CARRIED OUT IAW AAAE 2004-077-006 AND UPS EO B727-5330-21003-A.

Part: SKIN — CORRODED (FUSELAGE) · airframe 47,543 hrs · 30,806 cycles

INSPECTION TYPE: C, SUSPECT CORROSION BETWEEN SKIN AND INTERNAL STRUCTURE BS 217 STR 25L. AREA PAINT STRIPPED IAW MM 51-20-15. TRIMMED CORRODED AREA IAW SRM 53-30-03 AND REPAIRED AREA IAW SRM 53-30-3 FIG. 3.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,543 hrs · 30,806 cycles

C-CRACKS ON CENTER POST OF COCKPIT WINDOWS, NR 1 LT AND NR 1 RT, LOWER IB CORNERS. HFEC CARRIED OUT AND CRACKS CONFIRMED. CRACKED SKIN REPLACED IAW AAAE EO 2004-077-004 AND UPS FILE NR 727-53-20157.

Part: LIGHT — INOPERATIVE (CABIN)

INSPECTION TYPE:PFLT EMERGENCY EXIT LIGHT FOR CABIN INOP. REMOVED AND REPLACED CABIN EMERGENCY LIGHTING FIXTURE PER MM 33-50. OPS CHECKS NORMAL AT THIS TIME.

Part: LIGHT — INOPERATIVE (CABIN)

INSPECTION TYPE:PFLT CABIN DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED CABIN DOOR, EMERGENCY EXIT LIGHT OPS CHECKS NORMAL AT THIS TIME PER MM 33-50.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT)

INSPECTION TYPE: ASV, EMERGENCY EXIT LIGHTS INOPERATIVE IN COCKPIT AND FORWARD ENTRY REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY. OPS CKS GOOD.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 47,122 hrs · 30,408 cycles

INSPECTION TYPE: C&SI, CORROSION ON FLOORBEAM TOP CAP BS 950 LBL 50. REPAIR CARRIED OUT IAW SRM EO 2003-008-022. UPS ENGINEERING FILE 7 27-53-20100.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 47,122 hrs · 30,408 cycles

INSPECTION TYPE: C&SI, ON REMOVAL OF WINDOW FRAME TO FACILITATE BS 870 FITTING REPLACEMENT CORROSION FOUND ON FLANGE OF WINDOW FRAMES, FRAME AT BS 880 AT LWR AFT CENTER. CORROSION BLENDED OUT IAW SRM 51-10-6 & AREA OF DAMAGE FOUND OUTSIDE LIMITS IAW SRM 56-20-1. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 56-20-03 FIG 1.

Part: PAD — CORRODED (#6 FLAP TRACK) · airframe 47,122 hrs · 30,408 cycles

INSPECTION TYPE:C&SI #6 FLAP TRACK AFT ATTACH POINT LWR PAD ON R/H FALSE SPAR HAVE EVIDEN CE OF CORROSION REMOVED PAD IAW SRM 51-30-02. ON REMOVAL OF CORROAION, CORROSION FOU ND TO BE OUTSIDE LIMITS IAW SRM 51-10-1. REPLACED PAD IAW SRM 51-30- 02

Part: STIFFENER — CRACKED (#6 FLAP TRACK) · airframe 47,122 hrs · 30,408 cycles

INSPECTION TYPE:C&SI #6 FLAP TRACK AFT O/B ATTACH POINT VERTICAL STIFFENER ON R/H FALSE S PAR CRACKED STIFFENER REMOVED IAW SRM 51-30-2. STIFFENER REPLACED IAW SRM 51-30 -02 & DRAWING 65-16216

Part: YOKE — CRACKED (TAILSKID) · airframe 47,122 hrs · 30,408 cycles

INSPECTION TYPE: C&SI, DURING REMOVAL OF TAILSKID ACTUATOR FITTING, TAILSKID YOKE ASSY FOUND CRACKED. TAILSKID YOKE ASSY REPLACED IAW MM 32-71-41.

Part: FITTING — CRACKED (TAILSKID TRUNN) · airframe 47,122 hrs · 30,408 cycles

INSPECTION TYPE: C&SI, DURING REMOVAL OF UPPER AIRSTAIR THREADS IT WAS NOTED THAT THE TAILSKID ACTUATOR FITTING (RT SIDE) WAS CRACKED (TRUNNION FITTING). TAILSKID TRUNNION FITTING REMOVED & REPLACED IAW SRM 51-10-01 & DRG 65-25992.

Part: SKIN — CORRODED (BS 856-860 WBL70) · airframe 47,122 hrs · 30,408 cycles

INSPECTION TYPE:C&SI EVIDENCE OF CORROSION BETWEEN WING CENTER SECTION UPPER SKIN & SKIN UPPER SPLICE @ BS 856 - 860 I/B OF WBL 70.5 RIGHT REPAIR CARRIED OUT IAW SRM 51-10-1, 51-10-2, 51-30-02 & SMRO EO 2003 -008-018 UPS ENGINEERING FILE NO B727-5730-18440-A

Part: STIFFENER — CORRODED (FUSELAGE) · airframe 47,122 hrs · 30,408 cycles

INSPECTION TYPE: C&SI, CORROSION ON INTERNAL SIDE OF NLG LT SIDE WALL AT BS 285 (FWD OF VERTICAL STIFFENER) LWR END CORROSION FOUND AT BS 280 & 285 BETWEEN STIFFENER AND SKIN. SKIN CUTOUT MADE AT VERT STIFFENER TO REMOVE CORROSION IAW SRM 51-10-6. DOUBLER FABRICATED IAW SRM 51-40-2. FILLERS FABRICATED IAW SRM 51-40-2. INSTALLED IAW SRM 51-40-2.

Part: STIFFENER — CORRODED (NLG) · airframe 47,122 hrs · 30,408 cycles

INSPECTION TYPE: C+SI, VERT STIFFENER HAS INTERGRANULAR CORROSION AT BS 343 APPROX AT NLG CUTOUT LT VERT WEB. INSTALLED NEW STIFFENER IAW SRM 51-30-02.

Part: CASTING — CORRODED (LT O/B AILERON) · airframe 47,122 hrs · 30,408 cycles

INSPECTION TYPE: C&SI, LT O/B AILERON TAB FIRST & SECOND FROM O/B HINGE CASTINGS HAVE PITTING CORROSION. HINGE CASTINGS REPLACED IAW MM 27-10-19.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 47,122 hrs · 30,408 cycles

INSPECTION TYPE:C&SI CABIN SEAT TRACK AT STA 650 TO 680 HAS CORROSION ON O/B FLANGE OF T RACK LBL 45.5. CORROSION REMOVED IAW SRM 53-10-1 OUT OF LIMITS. SEAT TRACK SECTION REMOVED BETWEEN BS 650-740 LBL 45.5 IAW SRM 51-30-2. NEW SECTION OF SEAT TRACK FABRICATED, PROTECTED PRIMED AND FITTED IAW SRM 53-10-5 & 51-30-2 & CPT 2061.

Part: SEAT TRACK — CORRODED (BS 344 & 480) · airframe 47,122 hrs · 30,408 cycles

INSPECTION TYPE:C&SI CORROSION ON SEAT TRACK LBL 42.84 BETWEEN BS 344 & 480 SEAT TRACK REMOVED IAW SRM 51-30-2. NEW SEAT TRACK FABRICATED IAW S RM 51-20-1. NEW SEAT TRACK REPROECTED IAW SRM 51-10-2.NEW SEAT TRACK INSTALLED IAW SRM 51-30-2

Part: CARRIAGE — CORRODED (R/H WING WBL 348) · airframe 47,122 hrs · 30,408 cycles

INSPECTION TYPE:C+SI NO.7 FLAP TRACK CARRIAGE HAS PITTING COROSION ON BEARING MOUNT HOLE. FLAP TRACK CARRIAGE REPLACED IAW SB 27-112.

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,122 hrs · 30,408 cycles

INSPECTION TYPE: C&SI, SUB FRAME AT BS 920 RT HAS SMALL CRACK AT STR 15. SUB FRAME AT BS 920 RT REPAIRED IAW SRM 51-40-03.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 47,122 hrs · 30,408 cycles

INSPECTION TYPE: C&SI, CORROSION ON FLOORBEAM TOP CAP BS 344 RBL 24.75 TO 24.75 LBL. CORROSION REMOVED IAW SRM 51-10-6 DEPTH OF BLEND-OUTS MEASURED AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-01 IN SEVERAL AREAS. FLOORBEAM TOP CHORD REPLACED IAW BOEING DRAWING 65-16316 WITH REF TO SRM 53-10-2 & 51-30-2.

Part: FITTING — CRACKED (BS 870 L/H) · airframe 47,122 hrs · 30,408 cycles

INSPECTION TYPE:C&SI L/H 870 FITTING HAS 2 CRACKS FWD OF CENT. LINE IN 1ST ROW OF FASTENE RS (HOLES 3 & 4) AND 1 CRACK IN AFT OF BUTT LINE 1ST ROW 3RD FASTENE R FROM TOP FITTING REPLACEMENT CARRIED OUT IAW UPS EO B727-5310-3056 APPENDIX E

Part: HINGE — CORRODED (AILERON) · airframe 47,122 hrs · 30,408 cycles

INSPECTION TYPE: C+SI, LT WING O/B AILERON BEARING HINGES (4 OFF) CORRODED. LEFT O/B AILERON REPLACED IAW MM 27-10-14.

Part: FLAP TRACK — CORRODED (NR 5 FLAP) · airframe 47,122 hrs · 30,408 cycles

INSPECTION TYPE: C&SI, NR 5 FLAP TRACK HAS CORROSION ON MOUNT HOLES C, E, F & CORROSION ON MOUNT PADS A & B. REFER TO SMRO EO 2003-008-008 & UPS EO B727-5742-0651-K FOR DETAILED SIGNOFF & RECTIFICATION. UPS ENGINEERING FILE B727-540-18418-B.

Part: CARRIAGE — CORRODED (#5 FLAP TRACK) · airframe 47,122 hrs · 30,408 cycles

INSPECTION TYPE:C&SI ON REMOVAL OF SEALANT FROM THE INNER BORE OF SPINDLE ON FLAP TRACK C ARRIAGE #5 EXCESSIVE CORROSION IS EVIDENT #5 FLAP TRACK CARRIAGE REPLACED IAW OHM 57-58-02

Part: ATTACH FITTING — CORRODED (NR 2 FLAP TRACK) · airframe 47,122 hrs · 30,408 cycles

INSPECTION TYPE: C&SI, ON INSPECTION OF NR 2 FLAP TRACK CORROSION FOUND ON FWD MOUNT LUG FACES A, B, C & D AND IN FWD LUG BOREHOLES A & B. REPAIR CARRIED OUT IAW SRMO EO'S 2003-008-001 & SMRO 2003-008-014. UPS ENGINEERING FILE NR 727-57-20096.

Part: FLAP TRACK — CORRODED (NR 3) · airframe 47,122 hrs · 30,408 cycles

INSPECTION TYPE: C&S, NR 3 FLAP TRACK HAS SURFACE CORROSION IN THE FOLLOWING AREAS, INSIDE HOLE D, INSIDE HOLE E, INSIDE HOLE F, INSIDE HOLE G & FLAP AFT PAD (B). REPAIR CARRIED OUT IAW SRMO EO 2003-008-006 & 2003-008-012 UPS ENGINEERING FILE NR 727-57-20094.

Part: AILERON — CORRODED (O/B R/H) · airframe 47,122 hrs · 30,408 cycles

INSPECTION TYPE:C&SI CORROSION ON O/B R/H AILERON HINGES 2, 3 & 4 ON INVESTIGATION OF HINGE ASSYS, HINGES FOUND TO BE CORRODED BEYOND ALLOWABLE LIMITS IAW SRM 57-50-11. INSTALLED REPLACEMENT AILERON IAW MM 27-10-14. REF. NRC 632179 FOR AILERON RIGGING & OUSTANDING STEP S

Part: CARRIAGE — CORRODED (R/H WING WBL203) · airframe 47,122 hrs · 30,408 cycles

INSPECTION TYPE:C+SI ON REMOVAL OF SEALANT FROM THE INNER BORE OF NO.6 FLAP TRACK CARRIAG E SPINDLE,EXCESSIVE CORROSION IS EVIDENT. NO.6 FLAP TRACK CARRIAGE REPLACED IAW OHM 57-58-02.

Part: FLAP TRACK — CRACKED (#6) · airframe 47,122 hrs · 30,408 cycles

INSPECTION TYPE:C&SI #6 FLAP TRACK HAS SUSPECT CRACK FROM HOLE F ON SPOILER SUPPORT BEAM PAD REPLACED #6 FLAP TRACK IAW MM 27-51-31

Part: ATTACH FITTING — CORRODED (NR 7 FLAP TRACK) · airframe 47,122 hrs · 30,408 cycles

INSPECTION TYPE: C&SI, NR 7 FLAP TRACK HAS SURFACE CORROSION ON FWD MOUNT LUG FACES A & D AND IN FWD LUG BOREHOLES. REPAIR CARRIED OUT IAW SRMO EO'S 2002-008-002 & 2003-008-011. UPS ENGINEERING FILE NR 727-57-20093.

Part: FITTING — CRACKED (940) · airframe 47,122 hrs · 30,408 cycles

INSPECTION TYPE:C&SI 2 SUSPECT CRACKS ON R/H AFT UPPER 940 FLOORBEAM ATTACH FLANGE CRACKS OUT OF LIMITS FITTING REPLACED IAW UPS EO B727-5310-4501

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 47,122 hrs · 30,408 cycles

INSPECTION TYPE: C&SI, SUSPECT CRACK AT AFT END OF BEAD IN RIGHT MLG CEILING AT BS 940 RBL 58 APPROX. REPAIRED IN CONJUNCTION WITH 940 FITTING REPLACEMENT REF NRC 631320.

Part: RIB — CORRODED (LT WING) · airframe 47,122 hrs · 30,408 cycles

INSPECTION TYPE: C&SI, LEFT WING, L/E CAVITY SUPPORT RIB CORRODED AT FSS 250 ADJACENT TO WIRING P-CLIP. REMOVED RIB IAW SRM 51-30-02, FOUND TO BE OUTSIDE LIMITS IAW SRM 51-10-01. REPLACED EXTRUDED TEE TO RIB IAW SRM 51-30-02. INSTALLED RIB IAW SRM 51-30-02.

Part: PANEL — DELAMINATED (#10 SPOILER) · airframe 47,122 hrs · 30,408 cycles

INSPECTION TYPE:C&SI DELAM ON R/H WING TE PANEL UPPER FWD OF NO 10 SPOILER PANEL REPAIRED IAW SRM 51-40-5

Part: SKIN — CORRODED (FUSELAGE) · airframe 47,122 hrs · 30,408 cycles

INSPECTION TYPE: C&SI, AREA OF LIGHT SURFACE CORROSION ON SKIN ABOVE ENG NR 2 PYLON RT SIDE AT BS 1363 AT RT COWL HINGE LINE. FASTENERS REMOVED FROM SKIN & GUTTER IAW SRM 51-30-02. NEW PANEL MADE IAW SRM 54-10-2 & 51-10-1. NEW PANEL ALODINED & PRIMED IAW SRM 51-10-2. RAIN GUTTER INSTALLED IAW SRM 51-30-02.

Part: SKIN — CORRODED (BS 1183 S9 & 10) · airframe 47,122 hrs · 30,408 cycles

INSPECTION TYPE:C&SI SKIN BULGING JUST FWD OF 1183 AND BETWEEN STR 9R & 10R AREA FOUND CORRODED OUTSIDE LIMITS IAW SRM 51-30-01. DAMAGED AREA CU T OUT IAW SRM 51-30-3 AT STR. 9.REMOVED CORROSION IAW SRM 51-20-01 F OUND WITHIN LIMITS IAW SRM 53-30-01. STRINGER TIE REMOVED IAW SRM 51 -10-2. NEW FILLER & DOUBLER FABRICATED IAW SRM 53-30-3. REPAIR INSTA LLED IAW SRM 53-30-3

Part: PRESSURE PANEL — CRACKED (NLG WW) · airframe 47,122 hrs · 30,408 cycles

INSPECTION TYPE: C&SI, AIR LEAK COMING FROM WHAT APPEARS TO BE CRACK IN PRESSURE WEB IN NOSE W/W LEFT SIDE MIDWAY ON LT SIDE WALL. CRACKED AREA CUT OUT IAW SRM 51-40-2. DOUBLER & FILLER FABRICATED IAW SRM 51-40-2. HFEC C/O ON CUTOUT ON THE ABOVE AREA IAW NDTM 51-00-00 PT 6. - NDF. REPAIR PARTS INSTALLED IAW SRM 51-40-2.

Part: SKIN — CRACKED (NOSE W/W L/H) · airframe 47,122 hrs · 30,408 cycles

INSPECTION TYPE:C&SI AIR LEAK COMING FROM WHAT APPEARS TO BE CRACK IN SKIN OF NOSE W/W L/ H SIDE ABOVE DECAL FOR STRUT SERVICING. CRACKED AREA CUTOUT IAW SRM 51-40-2 DOUBLER, FILLER & SHIM FABRICATE D IAW SRM 51-40-2.. HFEC C/O AROUND CUTOU ON THE AREA - NO DEFECTS F OUND. REPAIR PARTS INSTALLED IAW SRM 51-40-2

Part: FLANGE — CRACKED (LT MLG WW) · airframe 47,122 hrs · 30,408 cycles

INSPECTION TYPE: C&SI, LEFT MAIN WHEEL WELL BS 930 FITTING SUSPECT CRACK ON I/B VERTICAL FLANGE. REPAIR CARRIED OUT IAW SRM 51-30-02, 51-40-04, 53-10-3, 53-10-4, 51- 10-02 & 51-40-3 & DRAWINGS 65-16336 & 65C15732.

Part: SUPPORT FITTING — CRACKED (CARGO DOOR) · airframe 47,122 hrs · 30,408 cycles

INSPECTION TYPE: C&SI, CRACK FOUND AT CLEAT BETWEEN MCD SUPPORT FITTING AND FRAME AT STA 540 WL 207 CRACK START AT RIVET TO EDGE OF CLEAT .375 INCH. REPAIR CARRIED OUT IAW SRM 51-40-3.

Part: SUPPORT FITTING — CRACKED (FUSELAGE)

INSPECTION TYPE:HFEC REFERENCE D211423 VERTICAL SUPPORT FITTINGS AT BS 930 BETWEEN STRINGERS 14 AND 18A HAS APPROX 5 INCHES CRACK (LEFT HAND SIDE). CLEANED AREA PERFORMED HFEC INSP PER B727 NDT MANUAL PART 6-51-00-00 FIG 4 ON BS 930 FITTING LT SIDE CRACK DOES NOT EXTEND ABOVE W/L 201.4. PREVIOUS REPAIR INSTALLED PER EO B727-5310-2611 APPLIED CORROSION INHIBITING COMPOUND THIS CLEARS DMI D211423.

Part: WARNING LIGHT — ILLUMINATED (COCKPIT)

INSPECTION TYPE:N/A, RT MLG DOOR WARNING ILLUM. OK TO FLY ON REVENUE TO CAE FROM PHL AS PER EO B727-1245B-DISSUED. A/C MUST FLY WITH GEAR HANDLE IN UP POSITION AT ALL TIMES NO FURTHER ACTION IS REQUIRED.

Part: DOOR — INOPERATIVE (MLG)

INSPECTION TYPE:N/A, UPON PLACING GEAR HANDLE IN OFF POSITION AFTER T/O RED DOOR LIGHT ON FROM PANEL AND RIGHT MAIN GEAR DOOR LIGHT ON S/O PANEL ILLUMINATED. GEAR WAS CYCLED, SAME INDICATIONS AGAIN OCURRED WHEN GEAR HANDLE WAS PLACED IN OFF POSITION. *S/D* OK TO FLY ON REVENUE TO CAE FROM PHL AS PER EO B727-1245B-DISSUED D. A/C MUST FLY WITH GEAR HANDLE IN UP POSITION AT ALL TIMES. NO FURTHER ACTION IS REQUIRED.

Part: SWITCH — MALFUNCTIONED (LE FLAPS)

INSPECTION TYPE:N/A - AIR TURNBACK, UNABLE TO RETRACT FLAPS PAST 2 DEGREES. REMOVED AND REPLACED NR 2 FLAP SWITCH.

Part: SKIN — CRACKED (HORIZONTAL STAB)

INSPECTION TYPE:N/A SMALL CRACK ON LT HORIZANTAL LEADING EDGE VERIFIED CRACK WITH HFEC REPAIRED CRACK PER SRM 55-10-3. THIS EXTERNAL DOUBLER MUST BE REPLACED WITH A FLUSH REPAIR PER SRM 5501003, FIG 2 NO LATER THAN NEXT C CHECK.

Part: SKIN — CRACKED (FUSELAGE)

INSPECTION TYPE:N/A CRACK FOUND AFT LOWER FUSELAGE SIDE JUST IN FRONT OF AIRSTAIRS STOP DRILLED CRACK PER EO B727-5330-12732-A. PERFORMED HFGC NO CRACKS BEYOND STOP DRILL PERMANENT REPAIR WITHIN 15 DAYS. RCQC 15650

Part: O2 REGULATOR — INOPERATIVE (COCKPIT)

F/O 02 REGULATOR INOP. REPLACED F/O REGULATOR AND MASK.

Part: SWITCH — OUT OF ADJUST (MLG)

INSPECTION TYPE:N/A, AFTER GEAR RETRACTION, RED DOORS LIGHT REMAINED ILLUMINATED, CYCLED GEAR, LIGHT WENT OUT. PERFORMED ADJ/TEST OF LANDING GEAR DOOR WARNING SWITCHES PER AMM 32- 62-11 PG 501. ALL INDICATORS LIGHTS CK GOOD PER MM REFERENCE.

Part: LIGHT — INOP (PAX DOOR)

INSPECTION TYPE:N/A, EMERGENCY EXIT LIGHT OVER FORWARD ENTRY DOOR INOP. REPLACED BATTERIES, OPS CKS OK.

Part: LIGHT — INOP (FLIGHT DECK)

INSPECTION TYPE:N/A COCKPIT ENTRY DOOR EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERIES, LIGHTS OPS CK OK.

Part: BULB — FAILED (COCKPIT)

INSPECTION TYPE-N/A, EMER EXIT LIGHT ABOVE COCKPIT ENTRY DOOR VERY WEAK. RELAMPED, OPS CHECKS OK.

Part: BEARING — CORRODED (RT MLG)

INSPECTION TYPE:C FWD RT MLG TRUNNION BEARING (FWD) AND SUPPORT CORRODED. BEARING AND SUPPORT REPLACED IAW MM 32-11-51 AND 32-11-72.

Part: FRAME — CRACKED (FRAME 760.95)

INSPECTION TYPE-C, CRACK FOUND EMINATING FROM FASTENER HOLE ON FRAME 760.95 RT OVERSIZE HOLE. FRAME 760.95 RT REPAIRED IAW APPENDIX C OF EO B727-5310-5474.

Part: SUPPORT — CORRODED (RT TE FLAP)

INSPECTION TYPE:C SUPPORT ASSY CORRODED FOR RT I/B FLAP I/B TRACK AT ATTACH HOLE FOR MLG FITTING BOLT. SUPPORT ASSY REPLACED IAW MM 32-11-51.

Part: BRACKET — CRACKED (RT ELEVATOR)

INSPECTION TYPE-C, RT ELEVATOR AT REAR SPAR AND ELEV STA 66.5 BRACKET CRACKED. REPLACED BRACKET IAW DRAWING NR 69-19144 AND DRAWING NR 65-25635.

Part: SUPPORT ROD — SHEARED (NR 8 SPOILER)

INSPECTION TYPE:C NR 8 SPOILER I/B HINGE SUPPORT ROD SHEARED. SUPPORT ROD REMOVED AND REPLACED IAW MM SRM 51-30-2.

Part: FITTING — CORRODED (WS 224.5)

INSPECTION TYPE-C, CORROSION FOUND ON RT LANDING GEAR SUPPPORT FITTING ON WING REAR SPAR STA 224.5. FITTING REPLACED IAW DRAWING 65-84405.

Part: BRACKET — CRACKED (NR 3 ENGINE)

INSPECTION TYPE:C ENGINE NR 3 ENGINE CONTROLS DRUM INSTALLATION, SUPPORT BRACKET HAS SUSPECT CRACK. REPAIRED BRACKET, REINSTALLED AS PER MM CHP 76-11-21.

Part: CHANNEL — CRACKED (BS 351-2)

INSPECTION TYPE-C, SUSPECT CRACK AT BS 351-2 LOCK ACTUATOR SUPPORT CHANNEL LT SIDE UPPER BOLT HOLE. REPLACED CHANNEL IAW DRAWING NR 69-19122.

Part: FITTING — CORRODED (BS 870)

INSPECTION TYPE-C, CORROSION ON 870 FRAME RT AT FLOORBEAM ATTACH RBL 62.5. FITTING REPLACED IAW EO B727-5310-3056.

Part: FRAME — CRACKED (BS 910)

INSPECTION TYPE-C, SUSPECT CRACK OUTBOARD FLANGE RADIUS BS 910 LT BETWEEN STRINGER 18A SILL AND WHEEL WELL CEILING LT WHEEL WELL. REPAIR CARRIED OUT IAW SRM ADDENDUM EO B727-5310-1896.

Part: CASTING — CORRODED (LT AILERON)

INSPECTION TYPE:C ON REMOVAL OF LT INB AILERON TURNAROUND PULLEY, PULLEY CASTING FOUND CORRODED AT LWR LUG. REPLACED LT I/B TURNAROUND CASTING IAW SRM 51-30-02 AND MM 20-10-20.

Part: FLANGE — CRACKED (BS 910)

INSPECTION TYPE-C, SUSPECT CRACK O/B FLANGE RADIUS BS 910 RT BETWEEN STR 18A SILL AND W/WELL CEILING IN RT W/WELL. REPAIR CARRIED OUT IAW SRM ADDENDUM EO B 727-5310-1896.

Part: FRAME — DAMAGED (BS 848.95)

INSPECTION TYPE-C, DURING INSP OF FRAME 848.95 LT FOURTH FASTENER HOLE ABOVE FLOOR FOUND TO BE .3125 WITH MECHANICAL DAMAGE AFTER MAX OVERSIZE. FRAME 848.95 LT REPAIRED IAW APPENDIX C OF EO B727-5310-5474.

Part: SEAT TRACK — BROKEN (BS 870)

INSPECTION TYPE:C SEAT TRACK FLANGE BROKEN AT BS 870 RBL 24.75. SEAT TRACK SECTION REPLACED IAW SRM 53-10-5 FIG 1.

Part: SKIN — CORRODED (BS 1180)

INSPECTION TYPE-C, LIGHT SURFACE CORROSION ON SKIN BS 1180 BETWEEN S6L AND S7L. CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-30-1. REPAIRED IAW SRM 53-30-3 FIG 9.

Part: SKIN — CORROSION (BS 1130)

INSPECTION TYPE:C SUSPECT CORROSION BETWEEN SKIN AND INTERNAL STRUCTURE BS 1130 JUST ABOVE STR 4 R. REPAIR CARRIED OUT IAW SRM 53-30-3 FIG 5.

Part: WEB — CRACKED (BS 1376)

INSPECTION TYPE:C WEB OVER NR 2 ENGINE CRACKED AT BS 1376 RT. NEW WEB FABRICATED AND INSTALLLED IAW DRAWING 65-17555.

Part: SKIN — CORRODED (BS 310)

INSPECTION TYPE-C, SUSPECT CORROSION BETWEEN SKIN AND INTERNAL STRUCTURE BS 310 BETWEEN STR 9L AND S8L. REPAIR CARRIED OUT IAW SRS EO 98-30-003 AND 98-30-003 REVISION 1, REFERENCE UPS ENGINEERING FILE NUMBER 5330-2084.

Part: SKIN — CORRODED (BS 1850)

INSPECTION TYPE-C, LIGHT SURFACE CORROSION ON SKIN BS 1850 ABOVE NR 2 ENGINE RT COWL AFT HINGE POINT. SKIN REPAIRED AT BS 1850 RT PER SRM 54-30-2 FIG 4.

Part: SEAT TRACK — CORRODED (BS 344)

INSPECTION TYPE-C, WHILE INSPECTION UNDER FWD LAV LOWER FLANGE OF SEAT TRACK AT BS 34.4 RBL 24.75 FOUND CORRODED SECTION OF SEAT TRACK. REPLACED BS 344 TO 400 RBL 24.75 TRACK FABRICATED FROM EXTRUSION BAC1520-1432 IAW SRM 53-10-5 FIG 1.

Part: FLANGE — CRACKED (BS 913-5)

INSPECTION TYPE-C, SUSPECT CRACK O/B FLANGE RADIUS OF BS 913-5 BETWEEN STR 18A SILL AND W/WELL CEILING LT W/WELL. REPAIR CARRIED OUT IAW SRS EO B727-5310-1896.

Part: PANEL — CORRODED (LT HORIZ STAB)

INSPECTION TYPE:C CORROSION ON LT HORIZ STAB LE PANEL NR 9103 INBD END. CUT OUT DAMAGED AREA IAW SRM 55-10-3 (FIG 2). CARRIED OUT REPAIR IAW SRM 55-10-3 (FIG 2).

Part: SUPPORT — CRACKED (NR 5 SPOILER)

INSPECTION TYPE:C SUPPORT CHANNEL FOR NR 5 SPOILER PANEL INB DOWNSTOP CASTING CRACKED. NR 5 SPOILER CHANNEL REPLACED IAW SRM 51-30-02.

Part: SKIN — CORRODED (BS 1075)

INSPECTION TYPE-C, SUSPECT CORROSION BETWEEN SKIN AND INTERNAL STRUCTURE BS 1075 S18R AREA AT BS 1071 TO BS 1080 STR 18R TO STR 19R. REPAIRED PER SRS EO 98-30-001 ENGINEERING FILE NR 5330-2085.

Part: STRINGER — CORRODED (BS 850-870)

INSPECTION TYPE-C, CORROSION ON LOWER FLANGE OF STRINGER 18A LEFT HAND BETWEEN BS 870 AND 850. REPAIR CARRIED OUT IAW SRS EO 98-30-004, REF UPS ENGINEERING FILE NUMBER 727-53-2086.

Part: SKIN — CORRODED (BS 380)

INSPECTION TYPE-C, CORROSION BETWEEN SKIN AND INTERNAL STRUCTURE BS 380 S20R. REPAIR CARRIED OUT IAW SRM 53-30-3.

Part: SKIN — CORRODED (BS 380)

INSPECTION TYPE:C SUSPECT CORROSION BETWEEN SKIN AND INTERNAL STRUCTURE BS 380 S20R. REPAIR CARRIED OUT IAW SRM 53-30-3 FIG 1.

Part: QUADRANT — CRACKED (SPOILER)

INSPECTION TYPE:C NR 1 SPOILER QUADRANT IS CRACKED AT CABLE GUARD. NR 11 SPOILER QUADRANT REPLACED IAW 27-61-81 MM.

Part: CONTROL CABLE — DAMAGED (SPOILER)

INSPECTION TYPE-N/A, A/C ROLLS NOTICEABLY TO THE LEFT WHEN SPEED BRAKES EXTENDED 15-20 DEGREES AT 250 KTS. REPLACED SPOILER CABLE WSAZ AND RIGGED PER MM 27-61-31, OPS CKS GOOD.

Part: LIGHT — INOPERATIVE (CABIN)

INSPECTION TYPE-N/A, REPEAT GRIP, UPON ROTATION EMER EXIT LIGHT FELL FROM SOCKET ABOVE MAIN CABIN ENTRANCE. REFER TO LOG PAGE 966096, ITEM NR 1 WILL NOT REMAIN SECURE IN SOCKET. LIGHT INOP UPON INSP. REPAIR FOR CYCLE IAW EO B727-3350-8620-A.

Part: LIGHT — NOT SECURE (CABIN)

INSPECTION TYPE-N/A, UPON ENTERING EMERGENCY EXIT LIGHT ABOVE MAIN ENTRY DOOR FOUND LAYING ON FLOOR. EXIT LIGHT DOES NOT LATCH SECURELY IN BRACKET. REINSTALLED EMERGENCY EXIT LIGHT COVER, OPS CK NORMAL.

Part: AIR DISTRIBUTION — ODOR (COCKPIT)

INSPECTION TYPE-N/A, SMELLED ON CLIMBOUT A SMOKE SMELL FROM EYELET ON S/O PANEL RAN A/C SMOKE CHECKLIST AND WENT ON O2 MASKS DURING THE FLIGHT THE SMELL CAME AND WENT SEVERAL TIMES. OPERATED BOTH PACKS WITH NR 1 AND 3 ENGS AND WITH APU RAN GASPER FAN CK'D FWD AND AFT EE COMPS CK'D ACM OIL RAN PACKS AND GASPER FAN FOR 5 HOURS. NO ABNORMAL ODOR OR SMOKE NOTED.

Part: HINGE — CORRODED (CARGO DOOR)

INSPECTION TYPE-C, AFTER FURTHER INVESTIGATION FOUND THE FWD AND AFT MAIN CARGO DOOR HINGES CORRODED ON CUSTOMER CARD ID NR 625571. REMOVED CORRODED HINGES, PROCURED NEW HINGES AND INSTALLED IAW SRM 51-10-1, SRM 51-30-2, MM 52-34-01 AND MM 51-20-151.

Part: SKIN — DELAMINATED (RT TE AFT FLAP)

INSPECTION TYPE-C, RIGHT WING INBOARD AFT FLAP TRAILING EDGE IS DELAMINATED 11.5 INCHES INBOARD FROM THE OUTBOARD END. REMOVED DAMAGED AREA, REPAIRED PER SRM 51-40-6.

Part: FLAP — DELAMINATED (RT TE FLAP)

INSPECTION TYPE:C, R/W I/B AFT FLAP IS DISBONDED IN 2 PLACES AT THE 38 AND 86 FROM I/B END. REPAIRED AFT FLAP IAW SRM 51-40-6.

Part: FLAP — DELAMINATED (RT TE FLAP)

INSPECTION TYPE:C, RIGHT WING INBOARD AFT FLAP TRAILING EDGE IS DELAMINTATED 11.5 INCHES INBOARD FROM THE OUTBOARD END. REPAIRED IAW SRM 51-40-6.

Part: STIFFENER — CORRODED (BS 336)

INSPECTION TYPE-C, CORROSION (C53-111-03-1B) ON STIFFENER BS 336 RBL 15 WL 181. FOUND CORROSION TO BE OUT OF LIMITS PER SRM 53-10-1. REMOVED AND REPLACED STIFFENER IAW SRM 51-20-1, 51-30-5 AND MM 51-20-151.

Part: LUG — CORRODED (NR 6 LE FLAP)

INSPECTION TYPE:C, NR 6 K-FLAP O/B ATTACH LUG IS CORRODED AT MOUNT BOLT HOLES ON O/B SIDE. REMOVED AND REPLACED NR 6 K-FLAP IAW MM 27-80-01.

Part: SKIN — GOUGE (RUDDER)

INSPECTION TYPE:C, UPPER RUDDER EXTERNAL SKIN PANEL AT LEFT RUDDER STA 242.137 TO 271.323 HAS DEEP GOUGE. REMOVED DAMAGED SKIN PANEL, DRILLED UP NEW PANEL COUNTERSUNK AND INSTALLED NEW SKIN PANEL IAW SRM 51-30-2.

Part: UPPER BEAM — CORRODED (CARGO DOOR)

INSPECTION TYPE:C, UPON REMOVAL OF MAIN CARGO DOOR, FOUND UPPER BEAM CORRODED. CORROSION REMOVAL WAS OUT OF LIMITS. REMOVED MAIN CARGO DOOR UPPER BEAM, FABRICATED NEW UPPER BEAM AND INSTALLED NEW BEAM PER SRM 51-10-1, 51-10-2, 51-30-2.

Part: SPOILER — DELAMINATED (NR 1)

INSPECTION TYPE:C, NR 1 SPOILER IS SEVERELY DELAMINATED. REMOVED AND REPLACED NR 1 SPOILER PER MM 27-61-01, 27-61-01 27-61-00.

Part: CASTING — CORRODED (CARGO DOOR)

INSPECTION TYPE:C, UPON REMOVAL OF MAIN CARGO DOOR, FOUND FWD UPPER PRESSURE SEAL CORNER CASTING CORRODED. CASTING WAS CORRODED BEYOND LIMITS. REPLACED CASTING WITH NEW PART IAW SRM 51-10-1, 51-30-5, MM 51-20-31.

Part: CASTING — CORRODED (CARGO DOOR)

INSPECTION TYPE:C, UPON REMOVAL OF MAIN CARGO DOOR, FOUND UPPER AFT PRESS SEAL CORNER CASTING CORRODED. CASTING WAS CORRODED BEYOND LIMITS. REMOVED AND REPLACED CORNER CASTING PER SRM 51-20-31, 51-30-2, 51-30-5, 51-10-1.

Part: LIGHT — INOPERATIVE (PAX DOOR)

LEFT LIGHT BULB OF EMERGENCY EXIT LIGHT OVER FORWARD ENTRY DOOR INOPERABLE. (RELAMPED NO HELP). REMOVED AND REPLACED FORWARD ENTRY DOOR EXIT LIGHT ASSY. OPS CHECKS GOOD.

Part: BATTERIES — DISCHARGED (COCKPIT)

INSPECTION TYPE-N/A, COCKPIT AND FOREWARD DOOR EMERGENCY EXIT LIGHTS INOP. INSTALLED NEW BATTERIES IN COCKPIT AND FOREWARD DOOR EMERGENCY EXIT LIGHTS, OPS CHECK GOOD.

Part: UPLOCK HOOK — CORRODED (LT MLG)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND LT UPLOCK HOOK HAS EXCESSIVE PLAY. FOUND UPLOCK CORRODED. REMOVED UPLOCK ASSY AND REPLACED WITH NEW PART PER MM 32-32-51, 32-32-61, 32-32-0.

Part: SPAR — CORROSION (VERT STAB)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON VERTICAL FIN REAR SPAR CHORD, RUDDER STA 223-STA 238 WHERE PANEL 9515 MATES LT SIDE. REMOVED AND INSTALLED FABRICATED PARTS. WORK DONE IAW E.O. B727-5530-7482A.

Part: SHEAR TIE — CORRODED (VERT STAB)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION (C55-395-10-00-01) ON BOTH LT AND RT FWD SHEAR TIES INSIDE VERTICAL FIN TUNNEL AT FIN STA 87.0 UPPER END OF RIBS NR 5. MECHANICALLY REMOVED CORROSION. REWORK OUT-OF-LIMITS IAW SRM 55-50-00. REMOVED AND REPLACED SHEAR TIES IAW SRM 51-30-2.

Part: FLOOR BEAM — CORRODED (BS 420)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION (C53-224-01.05-01) ON FLOOR BEAM STA 420 RBL 45-65 WL 208 LWR SIDE OF UPPER CHORD. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. REPAIRED IAW UPS E.O. B727-5310-7455A.

Part: SKIN — CORRODED (BS 272-275)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION (53-221-01.00-01) ON SKIN AT BS 272-275, LBL 56, WL 209-213. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS, TRIMMED OUT DAMAGED AREA, FABED REPAIR DOUBLER, FINAL REPAIR PER SRM 53-30-1, 53-30-2, 51-10-2, 51-30-2.

Part: FLOOR BEAM — CORRODED (BS 420)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION (C53-224-01.05-01) ON BEAM STA 420 LBL 0 TO LBL 24 AND LBL 45 - LBL 65 WL 208 LWR SIDE OF UPPER CHORD. REMOVED CORROSION ON UPPER CHORD OF FLOOR BEAM. FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. REMOVED AND REPLACED UPPER CHORD OF FLOOR BEAM PER UPS EO B727-5310-7455A.

Part: FLOOR BEAM — CORRODED (BS 328)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON FL BEAM STA 328, LBL 33 WL 208, ALSO, HAS MECH. DAMAGE LBL 54 WL 208. REPAIRED FL BEAM PER 727 SRM 53-10-08, FIG 7.

Part: RIB — CORRODED (HORIZ STAB)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION IN BORE FOR BOTTOM BUSHING AND OUTBOARD FACE ON UPPER THRUST RIB LUG FOR LWR SPLICE BEAM AT APPROX. RUDDER STA 128.765 LT. REMOVED CORROSION AND OVERSIZE BORE, INSTALL OVERSIZED BUSHING IAW TRAMCO EWO 95-3072.

Part: WEB — CRACKED (BS 600)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND SUPPORT WEB TO BE CRACKED AT BS 600, LBL 7, WL 300. REPAIRED AREA PER E.O. B727-53-1683.

Part: SHEAR TIE — CORROSION (VERT STAB)

WHILE ON GROUND, MAINTENANCE FOUND CORROSION ON BOTH LT AND RT VERTICAL STABILIZER SHEAR TIES, AT FWD END OF RIB NR 9 AT FIN STA 180.6 INSIDE VERTICAL FIN TUNNEL. REMOVED AND REPLACED LT AND RT SHEAR TIES IAW 727 SRM 51-30-2.

Part: MID SPAR — CRACKED (VERT FIN)

WHILE ON GROUND, MAINTENANCE FOUND RT VERT FIN MID SPAR UPPER FLANGE HAS BROKEN FASTENER HOLE. REMOVED DAMAGE, FABRICATED, INSTALLED REPAIR ANGLES PER SRM 51-30-2 UPS EO 727-55-0303.

Part: STIFFENER — CRACKED (FSS 475)

WHILE ON GROUND, MAINTENANCE FOUND VERTICAL STIFFENER AT FSS 475, ON THE I/B SIDE OF NR 6 SLAT I/B TRACK IS CRACKED. REMOVED AND REPLACED STIFFENER AT FSS 475, I/B SIDE NR 6 SLAT I/B TRACK IAW SRM 51-30-2.

Part: FITTING — CORRODED (LT AILERON)

WHILE ON GROUND, MAINTENANCE FOUND CORROSION LT WING O/B AILERON LOCKOUT FITTING HAS CORROSION PITS IN LOWER SURFACE NEXT TO BELL CRANK. REPLACED FITTING IAW SRM 51-30-2, MM 27-10-131, 27-10-121.

Part: RIB — CORRODED (RUD STA 128)

WHILE ON GROUND, MAINTENANCE FOUND CORROSION IN BORE FOR BOTTOM BUSHING AND O/B FACE ON UPPER THRUST RIB LUG FOR LOWER SPLICE BEAM, AT APPROX RUDDER STA 128 TO 765 LT. REMOVED CORROSION AND OVERSIZE BORE, INSTALLED OVERSIZED BUSHING IAW EO 727-55-0302.

Part: FITTING — CORROSION (LT AILERON)

WHILE ON GROUND, MAINTENANCE FOUND CORROSION LT WING I/B AILERON TURNAROUND FITTING. REPLACED FITTING IAW SRM 51-30-2.

Part: SPAR — CORRODED (FSS 200)

WHILE ON GROUND, MAINTENANCE FOUND CORROSION ON RT WING L/E LOWER FRONT SPAR CHORD AT FSS 200. MECHANICALLY REMOVED CORROSION, REWORK OUT OF LIMITS IAW SRM 57-10, FRONT SPAR LOWER CHORD REPAIRED IAW UPS EO 727-57-1642.

Part: SHEAR TIE — CORROSION (VERT STAB)

WHILE ON GROUND, MAINTENANCE FOUND CORROSION ON VERTICAL FIN SHEAR TIE FITTING, AT FIN STA 204 LT SIDE FORWARD END OF RIB NR 10 INSIDE TUNNEL, FOUND WHILE WORKING TAIL 227 CI 360676. REMOVED SHEAR TIE FITTING AT FIN STA 204 LT SIDE. REPLACED SHEAR TIE IAW WRM 51-30-2.

Part: FLAP — CORRODED (NR 3 LE FLAP)

WHILE ON GROUND, MAINTENANCE REPLACED NR 3 K-FLAP, DUE TO CONDITION AND CORROSION. REMOVED AND REPLACED NR 3 K-FLAP IAW MM 27-81-01.

Part: SPAR — CORRODED (WS 571)

WHILE ON GROUND, MAINTENANCE FOUND CORROSION ON INDICATIONS ON UPPER REAR SPAR ON LT WING AT WS 571. REMOVED CORROSION IAW 57-10-1, REPAIRED SPAR IAW SRM 57-10-6.

Part: FLOORBEAM — CORRODED (BS 600)

WHILE ON GROUND, MAINTENANCE FOUND CORROSION FWD CARGO BAY IN THE NUTPLATE HOLES, LOWER FLANGE OF THE 600 FLOORBEAM LBL 16 RLB 58 WL 201. REPAIRED BS 600 FLOORBEAM IAW UPS EO B727-5310-7463-A. CORROSION REWORK WAS OUT OF LIMTS IAW SRM 53-10-1.

Part: SPAR — CORRODED (VERT STAB)

WHILE ON GROUND, MAINTENANCE FOUND CORROSION ON LT SIDE VERTICAL FIN FRONT SPAR FROM FIN STA 108.8 TO 6.372. CORROSION OUT OF LIMITS, REPAIRED LT SPAR CHORD IAW UPS EO B727-5530-7473-A.

Part: FITTING — CRACKED (RUDDER)

WHILE ON GROUND, MAINTENANCE FOUND UPPER RUDDER CENTER RUDDER HINGE SUPPORT FITTING IS CRACKED AT RUD STA 212 TO 208. REMOVED UPPER RUDDER, INSTALLED REPLACEMENT RUDDER IAW MM 27-20-01.

Part: FITTING — CRACKED (RUDDER)

WHILE ON GROUND, MAINTENANCE FOUND LOWER RUDDER CENTER RUDDER HINGE SUPPORT FITTING IS CRACKED AT RUD STA 178 LT SIDE 3RD FASTENER FROM TOP. REMOVED RUDDER, INSTALLED SERVICEABLE RUDDER IAW MM 27-20-01.

Part: STIFFENER — CRACKED (FSS 480)

WHILE ON GROUND, MAINTENANCE FOUND VERTICAL STIFFENER AT FSS 480, ON O/B SIDE OF NR 6 SLAT I/B TRACK IS CRACKED. REMOVED AND REPLACED CRACKED STIFFENER IAW SRM 51-30-2 AT FSS 480.

Part: SKIN — DELAMINATED (HORIZ STAB)

WHILE ON GROUND, MAINTENANCE FOUND DAMAGE AROUND FASTENERS AT APPROX STAB STA 32.08 TO 44.00 ON LT HORIZONTAL STAB UPPER SURFACE. REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS AND INSTALLED IAW EO B727-5510-7485-A.

Part: FLOORBEAM — CORRODED (BS 328)

WHILE ON GROUND, MAINTENANCE FOUND CORROSION ON FLOORBEAM STA 328 LBL 33 WL 208 AND MECHANICAL DAMAGE LBL 54 WL 208. REPAIRED IAW SRM 53-10-8 AND B727-53-1686.

Part: SKIN — CORROSION (BS 272-275)

WHILE ON GROUND, MAINTENANCE FOUND CORROSION ON SKIN AT BS 272 TO 275, LBL 56 WL 209 TO 213. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. TRIMMED OUT DAMAGE AREA, FABRICATED REPAIR DOUBLER, FINAL REPAIR PER SRM 53-30-1, 53-30-2, 51-10-2, 51-30-2, EO B727-5330-7453A.

Part: SHEAR TIE — CORROSION (VERT STAB)

WHILE ON GROUND, MAINTENANCE FOUND CORROSION ON RT VERTICAL STABILIZER SHEAR TIE FITTING, AT FIN STA 204 INSIDE VERTICAL FIN TUNNEL. REMOVED AND REPLACED FITTING ON RT VERTICAL STAB AT FIN STA 204 IAW SRM 51-30-2.

Part: PRESSURE PANELS — CORRODED (NR 3120-3121)

WHILE ON GROUND, MAINTENANCE FOUND CORROSION ON PANELS BETWEEN GASKET SEAL ON PRESSURE PANELS 3120 AND 3121. REMOVED AND REPLACED PANELS IAW SRM 51-30-2.

Part: SPAR — CORRODED (VERT STAB)

WHILE ON GROUND, MAINTENANCE FOUND CORROSION ON RT SIDE VERT FIN UPPER FLANGE ON FRONT SPAR ENTIRE LENGTH STA 6.372 TO 180.6. CORROSION OUT OF LIMITS, REPAIRED RT SPAR CHORD IAW UPS EO B727-5530-7473-A.

Part: SPAR — CORRODED (LT HORIZ STAB)

WHILE ON GROUND, MAINTENANCE FOUND CORROSION BETWEEN LT HORIZONTAL STAB UPPER REAR SPAR CHORD AND SKIN AT STAB STA 215. REMOVED REAR SPAR CHORD, INSTALLED NEW SPAR CHORD AND FABRICATED RELATED PARTS, INSTALLATION PER SRM 51-30-02 SRM 51-21-31, 51-31-31, 55-10-3, EO B727-8510-7484-A/727-55-0300.

Part: FLOOR BEAM — CORRODED (BS 328)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON THE FLOOR BEAM AT STA 328, LBL 33 WL 208. ALSO, HAS MECHANICAL DAMAGE LBL 54, WL 208. MAINTENANCE REPAIRED THE FLOOR BEAM IAW SRM 53-10-8, FIGURE 7.

Part: FLOOR BEAM — CORROSION (BS 420)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON BEAM STA 420 LBL 0 TO LBL 24 AND LBL 45 - LBL 65, WL 208 LOWER SIDE OF UPPER CHORD. MAINTENANCE REMOVED CORROSION ON UPPER CHORD OF FLOOR BEAM, FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1. MAINTENANCE REMOVED AND REPLACED UPPER CHORD OF FLOOR BEAM PER UPS EO B727-5310-7455A.

Part: RIB — CORROSION (EMPENNAGE)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON BORE FOR BOTTOM BUSHING AND O/B FACE ON UPPER THRUST RIB LUG FOR LOWER SPLICE BEAM AT APPROX RUDDER STA 128.765 LT. MAINTENANCE REMOVED CORROSION AND OVERSIZE BORE, INSTALLED OVERSIZED BUSHING IAW TRAMCO EWO 95-3072.

Part: UPLOCK HOOK — CORRODED (LT MLG)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND THE LT UPLOCK HOOK HAS EXCESSIVE PLAY. MAINTENANCE FOUND THE UPLOCK TO BE CORRODED, REMOVED UPLOCK ASSY AND REPLACED WITH NEW PART IAW MM 32-32-51, 32-32-61, 32-32-0.

Part: SKIN — CORRODED (BS 272-275)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON SKIN AT BS 272-275, LBL 56, WL 209-213. MAINTENANCE REMOVED THE CORROSION, WAS FOUND TO BE OUT OF LIMITS, TRIMMED OUT DAMAGED AREA, FABRICATED REPAIR DOUBLER, PERFORMED FINAL REPAIR IAW SRM 53-30-1, 53-30-2, 51-10-2, 51-30-2.

Part: WEB — CRACKED (BS 600)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND SUPPORT WEB TO BE CRACKED AT BS 600, LBL 7, WL 300. MAINTENANCE REPAIRED AREA IAW EO B727-53-1683.

Part: FLOOR BEAM — CORROSION (BS 420)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON FLOOR BEAM AT STA 420 RBL 45-65, WL 208 LOWER SIDE OF UPPER CHORD. MAINTENANCE REMOVED THE CORROSION, FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. MAINTENANCE REPAIRED IAW UPS EO B727-5310-7455A.

Part: FITTING — CORROSION (LT LOWER)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION LT LOWER SPLICE BEAM UPPER AND LOWER SHEAR FITTINGS. REPLACED PER SRM 51-30-2, MM 51-20-21, 51-20-00, 51-20-21.

Part: FLOORBEAM — CORROSION (BS 400)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION (C53-224-01.05-01), ON FLOORBEAM STA 400 RBL 25 TO RBL 60 WL 208, LOWER SIDE OF UPPER CHORD. REMOVED CORROSION, FOUND OUT OF LIMIT, REMOVED DAMAGE AREA, FABRICATED T-CHORD. FINAL INSTALLATION PER SRM 53-10-8, 53-30-2, 51-10-6 AND 53-10-1.

Part: TRUNION FITTING — CORRODED (LT MLG)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON INNER SURFACE OF ATTACH FITTING, AROUND HOLES WHERE BEARING SUPPORT MATES, FWD TRUNNION. REPLACED TRUNNION FITTING PER SRM 51-30-2, 51-10-2, 51-20-4.

Part: TRUNNION FTGS — CORRODED (NLG)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND LEFT AND RIGHT NOSE LANDING GEAR TRUNNION FITTINGS CORRODED BEYOND LIMITS. REMOVED AND REPLACED LEFT AND RIGHT NLG TRUNNION FITTINGS AND STIFFENERS IAW UPS EO B727-5310-3954B AND BOEING REPAIR DRAWING 65-88189.

Part: STRINGER — CORRODED (BS 618-164)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION (C53-224-01-68-01), ON AND AROUND FASTENERS ON STRINGER 4R STA 618 TO 624. REPAIRED STRINGER PER SRM 53-10-1, 53-10-3, 51-10-2, 53-10-4, 51-30-2 AND MM 51-20-151.

Part: FITTING — CORROSION (TIE RIB)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON AFT VERTICAL BOLT HOLE FLANGE LOWER SURFACE ON TENSION TIE RIB. REMOVED CORROSION AND INSTALLED DNW BUSHINGS PER 51-10-6.

Part: FITTING — CORROSION (TIE RIB)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION IN AFT VERTICAL BOLT HOLES, AT TENSION TIE SHEAR FITTING. REMOVED CORROSION, REMOVED AND REPLACED BUSHINGS PER SRM 51-10-6 EO 727-55-0294.

Part: CORE — CONTAMINATED (NR 12 SPOILER)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND NR 12 SPOILER HAS WATER CONTAMINATION INTERNAL. REPAIRED SPOILER PER SRM 51-40-06.

Part: SKIN — CORRODED (NR 2 LE FLAP)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND AND REPLACED NR 2 K-FLAP DUE TO CONDITION AND CORROSION. THE NR 2 K-FLAP WAS FOUND TO BE CORRODED OUT OF LIMITS. REPLACED NR 2 K-FLAP PER MM 27-81-01.

Part: TE WEDGE — CORRODED (RT TE MIDFLAP)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND RT WING, I/B MIDFLAP T/E WEDGE SPAR CORROSION. REPLACED RT WING, I/B MIDFLAP T/E WEDGE PER SRM 51-10-1, 51-30-2.

Part: RIB — CRACKED (NR 4 LE SLAT)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND NR 4 SLAT RIB CRACKED AT SLAT STA 48.25. REPAIRED RIB IAW 727 SRM 57-50-3. STOP DRILLED CRACK AND INSTALLED REPAIR DOUBLER.

Part: FLOOR — CRACKED (RT DOGHOUSE)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND UPON REMOVAL OF LT AND RT DOGHOUSE FLOORS, BOTH LT AND RT HAND FLOORS HAVE NUMEROUS CRACKS. INSTALLED FABRICATED FLOOR REPAIRS PER SRM 51-20-1, 51-40-2, 51-30-2.

Part: SILL — CORROSION (CARGO DOOR)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON MAIN CARGO DOOR INTERNAL THRESHOLD STA 620 LBL 67 WL 208 LOWER SIDE OF SHEAR WEB. BLENDED OUT CORROSION, INSTALLED NUTPLATE DOUBLER IAW EO 727-53-1675.

Part: FLOORBEAM — CORRODED (BS 560)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION FORWARD CARGO BAY IN NUTPLATE HOLES IN THE LOWER FLANGE OF THE 560 FLOORBEAM RBL 5 TO RBL 58 WL 201. BLENDED CORROSION IAW 727-53-1669.

Part: FLOORBEAM — CORRODED (BS 1130)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION AROUND NUTPLATE HOLES BS 1130, RBL 25 TO 45 WL 208, FLOORBEAM JUST FORWARD OF PRESSURE WEB. BLENDED OUT CORROSION IAW 727 SRM 51-10-6.

Part: CORE — CONTAMINATED (NR 14 SPOILER)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND NR 14 SPOILER HAS WATER CONTAMINATION INTERNAL AND CORE DAMAGE. REPAIRED SPOILER PER SRM 51-40-6.

Part: FLOORBEAM — CORRODED (BS 640)

WHILE IN FOR SI CHECK MAINTENANCE FOUND CORROSION (C53-224-06.00-01) ON BEAM UNDER NUT PLATE AT BS 640, LBL 47, WL 208. REMOVED CORROSION BY BLENDING, FABRICATED STRAP AND DOUBLER FINAL REPAIRS PER SRM 51-10-6, 51-10-2, 51-10-1 AND EO 727-53-1668.

Part: BOLT — CRACKED (NR 5 LE SLAT)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND NR 5 SLAT IS CRACKED AT O/B GUIDE HOOK, UPPER ATTACH BOLT. REPAIRED NR 5 SLAT PER SRM 57-50-03.

Part: PANEL — CONTAMINATED (NR 8 SPOILER)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND NR 8 SPOILER HAS WATER CONTAMINATION. REPLACED NR 8 SPOILER PANEL WITH NEW PANEL PER MM 27-62-01.

Part: CHORD — CRACKED (BS 740)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION AND CRACKS ON 740 CHORD RBL 45 WL 200. REMOVED CORROSION AND REPAIRED PER EO B727-5710-7409A.

Part: FLOORBEAM — CORRODED (BS 680)

WHILE IN FOR SI CHECK MAINTENANCE FOUND CORROSION ON UPPER CHORD OF FLOOR BEAM BS 680, RBL 10, 16, 59. TRIMMED OUT UPPER CHORD FROM RBL 12 TO RBL 70 AND SPLICED IN NEW CHORD SECTION IAW 727 SRM 53-10-8.

Part: STRINGER — CORRODED (BS 323)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION (C53-224-01.00-01), STR 4L STA 323, 344 TO 348. REPAIR WAS MADE.

Part: FLAP — CORRODED (NR 5 LE FLAP)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON NR 5 K-FLAP. REPLACED NR 5 K-FLAP PER MM 27-81-01.

Part: FLOORBEAM — CORROSION (BS 380)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION (C53-224-01.05-01), ON FLOORBEAM AROUND NUTPLATE HOLES LOWER AFT SIDE OF UPPER CHORD STA 380 RBL 55 TO 58 WL 208. REPAIRED FLOORBEAM PER UPS EO B727-5310-7415-A.

Part: RIB — CRACKED (ELEV STA 50.05)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND LT HORIZ STAB NR 2 T/E SUPPORT RIB, AT ELEV STA 50.05 IS CRACKED ON LOWER SURFACE. REPLACED CRACKED SUPPORT RIB PER SRM 51-30-2, 51-30-5, 51-10-2.

Part: SUPPORT — CORRODED (LT TE MIDFLAP)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND LT WING I/B MIDFLAP I/B ACTUATING CABLE PULLEY GOUGED. PULLEY SUPPORT FITTING ASSY CORRODED EXTENSIVELY. REPLACED PULLEY SUPPORT ASSY IAW OHM 20-50-03, 57-52-01.

Part: STRINGER — CORRODED (BS 990-1050)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION AND BARE METAL ON STRINGER 6 LT, STA 990 - 1050. REMOVED DAMAGED SECTION OF STRINGER AND SPLICED IN A NEW SECTION IAW SRM 53-10-3 BETWEEN BS 990 - 1050.

Part: FRAME — CORRODED (BS 344)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION (C53-224-01.00-01) ON FRAME 344 BETWEEN STRINGER 1 TO STRINGER 8R. REPAIRED 344 FRAME IAW SRM 51-40-3.

Part: WEB — CORROSION (BS 350)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION (C53-111-01.00-01) AT BS 350 ON THE WEB AFT SIDE LBL 61 WL 181 TO 188. REPAIRED IAW SRM 53-10-1, 51-10-6, 51-40-2.

Part: BLKHD ANGLE — CORROSION (BS 227.8)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION (C53-111-01.00-01) STA 227.8 LBL 40 WL 186 AFT SIDE OF BULKHEAD, SUPPORT ANGLE CORRODED BEYOND LIMITS. REMOVED CORRODED AREA, INSTALLED REPAIR PER SRM 51-40-4.

Part: FLOOR BEAM — CORROSION (BS 640)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION (C53224-01.00-1) ON FLOOR BEAM, FLOORBOARD HOLES BS 640, RBL 32, 37, 41, 49, WL 208. REMOVED CORROSION, FOUND OUT OF LIMITS, CUT DAMAGE CHORD SECTION, FABRICATED CHORD SECTION. FINAL INSTALLATION PER SRM 53-10-1, 51-30-2.

Part: CHORD — CORRODED (BS 1110)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION BS 1110, WL 199 BL 0 ON THE STABILIZATION STRAP (CHORD) AROUND THE NUT PLATES. REMOVED CORROSION PER SRM 53-10-1. REMOVED DAMAGED SECTION, FABRICATED REPLACEMENT CHORD AND INSTALLED PER SRM 51-30-2 AND SRM 51-10-1.

Part: STRINGER — CORRODED (BS 1110-1130)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION (C53-224-01.00-03) ON STRINGER 1 STA 1110-1130. CORROSION MECHANICALLY REMOVED IAW SRM 51-10-6. REPAIRED STR 1 STA 1110-1130 IAW SRM 53-10-3.

Part: RIB — CRACKED (NR 5 TE SLAT)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND CRACKED RIB ON NR 5 SLAT 23 INCHES FROM O/B END (4TH RIB FROM O/B END, MARKED). REMOVED AND REPLACED 4TH RIB FROM O/B END OF NR 5 SLAT IAW SRM 51-30-2, 51-30-5.

Part: FRAME — CRACKED (BS 804)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND FRAME CRACKED AT STRINGER TO FRAME ATTACH POINT BS 804 STRINGER 14 RT. REPAIRED FRAME PER SRM 51-40-3.

Part: RIB — CRACKED (NR 3 LE SLAT)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND NR 3 SLAT, RIB JUST I/B OF TAI T-DUCT, CRACKED AT FWD CORNER. REMOVED AND REPLACED NR 3 SLAT RIB JUST I/B OF TAI T-DUCT IAW SRM 51-10-1, 51-30-2.

Part: RIB — CRACKED (NR 5 LE SLAT)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND CRACKED RIB IN NR 5 SLAT 8 INCHES FROM I/B END (3RD RIB IN FROM I/B END MARKED). REPLACED RIB IAW SRM 51-30-2.

Part: STRINGER — CORROSION (BS 990-1050)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION AND BARE METAL ON STRINGER 4 LT STA 990 - 1050. CUT OUT DAMAGED SECTION OF STRINGER BETWEEN BS 990 - 1050 AND SPLICED IN NEW SECTION IAW SRM 53-10-3.

Part: STRINGER — CORRODED (BS 990-1050)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION AND BARE METAL ON STRINGER 5 LT STA 990 - 1050. CUT OUT DAMAGED SECTION OF STRINGER BETWEEN BS 990 - 1050 AND SPLICED IN A NEW SECTION IAW SRM 53-10-3.

Part: FRAME — CORRODED (BS 420)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION BS 420 STR 23R ON TOP AND FWD SIDE OF FRAME. FABRICATED AND INSTALLED REPAIR DOUBLER TO FRAME IAW 727 SRM 51-40-3.

Part: FLOOR BEAM — CORRODED (BS 344)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION (C53-224-01.05-01) ON FLOOR BEAM STA 344 LBL 60-RBL 60 WL 208. MECHANICALLY REMOVED CORROSION IAW SRM 51-10-6. REPAIRED FLOOR BEAM IAW SRM5 1-30-2, 51-10-2, 53-10-8.

Part: CLIP — CORROSION (BS 400)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION (C53-111-01.00-01) BS 400 STR 19L ON STRINGER CLIP. REPLACED CLIP IAW SRM 51-10-6, 51-30-2 SRM 51-20-4.

Part: WEB — CRACKED (NR 4 LE SLAT)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND NR 4 SLAT RIB CRACKED AT SLAT STA 7.25. REMOVED AND REPLACED NR 4 SLAT RIB AT SLAT STA 7.25 IAW SRM 51-10-1, 51-30-2.

Part: FRAME — CORRODED (BS 227.8)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION (C53-221-01.03-01) ON BACKSIDE OF WEB AT BS 227.8 LBL 41 WL 224. MECHANICALLY REMOVED CORROSION IAW SRM 51-10-6. REPAIRED WEB FRAME IAW SRM 51-40-2.

Part: FLOOR BEAM — CORRODED (FUSELAGE)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND CUT OUT DAMAGED PORTION OF FLOOR BEAM. FABRICATED NEW TOP CHORD AND INSTALLED. ALL WORK DONE IAW SRM 51-30-2, 51-40-2 AND 51-40-4.

Part: FRAME — CORROSION (BS 574-580)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION (C53-224-01.00-01) ON MCD SHEAR WEB AT STA 574 TO 580 WL 208, LBL 60. REMOVED DAMAGED AREA, FABRICATED DOUBLER AND FILLER. FINAL INSTALLATION PER SRM 51-10-2, 51-10-6, 53-10-11, 51-40-2, 51-30-2.

Part: SKIN — CORROSION (BS 1070-1080)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION (C53-224-01.06-03) ON INTERIOR SKIN STA 1070-1090 STR 10-14 RT FROM UNDER WINDOW CASTING AND REPAIR DOUBLERS. REPLACED WINDOW FRAME PER SRM 51-10-1, 51-10-2, 51-10-6, 51-30-2, 53-10-4 AND 51-20-4.

Part: STRINGER — CORROSION (BS 660-680)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION (C53-224-0.1-08-01) ON STR 6L STA 660-680. REPAIRED IAW SRM 53-10-3, 51-10-2, 51-10-3.

Part: FLAP — CRACKED (RT TE MID FLAP)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND RT WING O/B MID-FLAP TO HAVE CRACKS AND CORROSION THROUGHOUT FLAP. MID-FLAP WAS REPLACED PER MM 27-51-11.

Part: SKIN — CORRODED (BS 829)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION (C53-224-01.01-02) ON SKIN AND LAP AT BS 829 STR 4 RT (ACCESS REQUIRED). MECHANICALLY REMOVED CORROSION IAW SRM 53-10-1. REPAIRED SKIN LAP IAW SMR 53-30-3.

Part: STRINGER — CORRODED (BS 680-700)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON STR 6R FROM ST 680 - 700. CUT OUT DAMAGED SECTION OF STRINGER AND SPLICED IN NEW SECTION IAW 727 SRM 53-10-3.

Part: SPAR — CORRODED (RT HORIZ STAB)

WHILE IN FOR SI CHECK MAINTENANCE FOUND AND REPLACED RT STAB UPPER FRONT SPAR CHORD DUE TO CORROSION AND CRACKS. INSTALLED NEW FRONT SPAR CHORD PER SRM 51-30-2.

Part: STRINGER — CRACKED (WS 629)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND LEFT WING STRINGER NR 4 IS CRACKED AT WS 629.0. STOP DRILLED CRACK, INSTALL REPAIR KIT PER E.O. B727-5710-0314F.

Part: STRINGER — CRACKED (WS 656.5)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND LT WING UPPER STRINGER 14 AT WS 656-5 IS CRACKED. CUT OUT DAMAGE AREA. ALSO, STOP DRILL FINISH INSTALLATION OF KIT PER E.O. B727-5710-0314.

Part: STRINGER — CORRODED (BS 1130-1180)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON STRINGER 3 LT STA 1130 - 1180. REPAIRED STRINGER PER SRM 53-10-3.

Part: FRAME — CORROSION (BS 350)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION (C53-111-01.00-01) BS 350 STR 22L ON AFT SIDE OF FRAME. REPAIRED FRAME IAW SRM 51-10-6, 53-10-1, 53-30-2, 51-40-2.

Part: TRIM TAB — DELAMINATED (RT AILERON)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND RT WING I/B AILERON TAB IS DELAMINATED AT T/E (MARKED). REPLACED RT WING AILERON TAB IAW SRM 51-80.

Part: RIB — CRACKED (LT HORIZ STAB)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND LOWER LT HORIZONTAL STAB RIB CHORD HAS A CRACK AT STA STA 8.00 (MARKED AT FRONT SPAR WEB). REMOVED AND REPLACED RIB CHORD AT LT STAB STA 8.00 PER SRM 51-10-1 AND SRM 51-30-2.

Part: FITTING — CORROSION (NR 2 LE FLAP)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON UPPER FWD SIDE OF NR 2 K-FLAP OUTBOARD MOUNTING LUG WHILE WORKING NR 360298 (WINGS 203). REMOVED AND REPLACED NR 2 K-FLAP OUTBOARD MOUNTING FITTING PER SRM 51-30-2 AND MM 27-81-01.

Part: SKIN — DAMAGED (BS 460-464)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND DISHED FASTENERS 4 EA AT BS460 - 464 519R (NOTE: ACCOMPLISHED NDI INSPECTION OF LAP PER E.O. B727-5330-0509. FOUND MATERIAL LOSS AT BS 461 - 476). ACCOMPLISHED REPAIR PER E.O. B727-5330-0509 AND SRM 53-30-3.

Part: BLKHD ANGLE — CORRODED (BS 227.8)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION (C53-111-01.00-01) STA 227.8 RBL 38 WL 199 AFT SIDE OF BULKHEAD ON SUPPORT ANGLE. REMOVED CORROSION MECHANICALLY IAW SRM 53-10-1. REMOVED AND REPLACED ANGLE (STIFFENER) IAW SRM 51-30-2, 51-10-1.

Part: RIB CHORD — CORRODED (RT HORIZ STAB)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON THE RIGHT HAND HORIZONTAL STABILIZER, INBOARD UPPER CLOSURE WEB CHORD FROM APPROXIMATELY 11.5 TO 24.75 AFT OF HORIZONTAL STABILIZER FRONT SPAR. MAINTENANCE REMOVED, FABRICATED AND REPLACED THE CHORD IAW SRM.

Part: DOUBLER — CORRODED (BS 307.5)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON THE DOUBLER AT STATION 307.5 TO STA 316, LBL 12.5 WL 181 TO 169. MAINTENANCE REMOVED TRIPLER AND REMOVED CORROSION ON TRIPLER. CORROSION FOUND BEYOND LIMITS, FABRICATED NEW DOUBLER AND TRIPLER, FINAL INSTALLATION PER SRM 51-10-6, 51-30-2, 51-20-4, MM 51-20-0 AND UPS 727-53-1671.

Part: RIB — CORRODED (HORIZ STAB)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON THE HORIZONTAL STABILIZER RIGHT HAND INBOARD CLOSURE WEB, INSIDE ACCESS HOLE 9223 AREA, FWD WEB UPPER END WHERE THE WEB ATTACHING BRACKET IS MOUNTED AND EXTENDING 16 INCHES FWD. MAINTENANCE REMOVED, FABRICATED AND INSTALLED NEW CLOSURE WEB IAW SRM.

Part: FRAME — CORRODED (BS 360)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON THE FASTENER HOLES, COMMON TO FRAME AT STATION 360 LBL 48 WL 165, BS 360 LBL 45 WL 165, BS 360 LBL 35 WL 158 AND BS 360 RBL 21 WL 151. MAINTENANCE REPAIRED PER UPS EO 727-53-1667.

Part: FITTING — CRACKED (NR 3 FLAP TRACK)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND A CRACK IN THE TRACK ATTACH POINT, LEFT WING NR 3 FLAP TRACK INBOARD AFT ATTACH FITTING AT SPOILER SUPPORT BEAM. MAINTENANCE REMOVED THE CRACKED ATTACH FITTING, INSTALLED A NEW ATTACH FITTING PER SRM 51-30-2, MM 27-51-31.

Part: LOWER FRAME — CORRODED (LT OVERWING EXIT)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON THE LOWER SEAL OF THE LEFT HAND AFT OVERWING EXIT HATCH. MAINTENANCE REMOVED THE LOWER AFT FRAME AND SEAL FORMERS, INSTALLED NEW FRAME AND SEAL FORMER. INSTALLATION IAW SRM 51-30-2, 53-30-01, AND 52-20-1.

Part: INTERCOSTAL — CORRODED (BS 277-294)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON THE INTERCOSTAL AT STA 277 TO 294 WL 208. MAINTENANCE REPLACED THE DAMAGED AREA IAW SRM 51-30-2, 51-10-2, 51-10-6 AND 51-20-6.

Part: STIFFENER — CORRODED (HORIZ STAB)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON THE HORIZONTAL STABILIZER RIGHT INBOARD CLOSURE WEB INSIDE ACCESS PANEL 9205 AREA AT UPPER END OF WEB WHERE AFT INTERSPAR WEB ATTACHING BRACKET IS MOUNTED. MAINTENANCE FABRICATED NEW STIFFENER AND INSTALLED IAW SRM 51-30-2 AND 55-10-1.

Part: INTERCOSTAL — CORRODED (BS 803)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION AROUND THE NUT PLATES AT STATION 803, RBL 6 AND WL 148. MAINTENANCE REMOVED THE DAMAGED AREA, FABRICATED NEW INTERCOSTAL AND INSTALLED IAW SRM 53-10-1, 51-10-6 AND 51-30-2.

Part: STIFFENER — CORRODED (HORIZ STAB)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON THE RIGHT HORIZONTAL STABILIZER AFT INTERSPAR WEB INBOARD ATTACHING BRACKET INSIDE ACCESS PANEL AREA 9206. MAINTENANCE FABRICATED NEW STIFFENER AND INSTALLED IAW SRM 51-30-2 AND 55-10-1.

Part: BEAM — CORRODED (HORIZ STAB TE)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON THE LEFT HORIZONTAL TRAILING EDGE BEAM EXTERIOR SURFACE AT STAB STATION 225.54 AND 182.5. MAINTENANCE CUTOUT THE DAMAGED SECTION AND SPLICED IN NEW SECTION IAW SRM 55-10-6.

Part: FLOOR BEAM — CORRODED (BS 500)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON THE FLOOR BEAM AROUND THE NUTPLATE HOLE FORWARD LOWER SIDE OF THE UPPER CHORD ON THE FLOOR BEAM AT STATION 500, LBL 55 - 57 AND WL 208. MAINTENANCE REPAIRED THE FLOOR BEAM IAW SRM 53-10-8.

Part: CHORD — CORRODED (BS 324)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON THE UPPER NOSE CHORD AT STATION 324, 340, 346, RBL 14.5 AND WL 166. MAINTENANCE REPLACED THE CHORD IAW SRM 51-10-2, 51-10-6, 51-30-2, 53-10-1 AND 51-20-4.

Part: STIFFENER — CRACKED (HORIZ STAB)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND A CRACK IN THE LEFT HORIZONTAL STABILIZER WEB STIFFENER AT STAB STATION 73 ON THE UPPER SIDE OF THE STIFFENER. MAINTENANCE REMOVED THE CRACKED STIFFENER AND REPLACED WITH NEW IAW SRM 57-30-2.

Part: STRINGERS — CORRODED (BS 277-294)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION IN VARIOUS SPOTS ON STRINGER 5, 6, 7, 8 AT STATION 277 - 294, LBL 29 - 47 AND WL 268 - 287. MAINTENANCE REPLACED STRINGERS 7 AND 8L ON UPS EO 5310-1259F, STRINGERS 5 AND 6L WERE REMOVED AND REPLACED IAW SRM.

Part: SPLICE — CORRODED (BS 380)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON THE TOP OF FRAME AT STATION 380 AND STRINGER 26R - 25R. MAINTENANCE REPLACED THE FRAME SPLICE IAW SRM 53-10-1, 53-10- 2 AND 51-10-6.

Part: STIFFENER — CRACKED (HORIZ STAB)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND A CRACK IN THE LEFT HORIZONTAL STABILIZER WEB STIFFENER AT STAB STATION 64 ON THE UPPER SIDE OF STIFFENER. MAINTENANCE REMOVED THE CRACKED STIFFENER AND REPLACED WITH NEW PER SRM 57-30-2.

Part: SKIN — DELAMINATED (TR TE FORE FLAP)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND DELAMINATION ON UPPER SURFACE RUB STRIP OF THE RIGHT WING INBOARD FORE FLAP. MAINTENANCE REPAIRED THE DAMAGED AREA IAW SRM 51-40-6.

Part: STRINGER — CORRODED (BS 1130)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION AND BARE METAL ON STRINGER 5L AND STATION 1130 - 1180. MAINTENANCE CUT OUT DAMAGED AREA, FABRICATED, AND INSTALLED PER SRM 53-10-3, 53-10-2, 51-30-3, 51-10-2 AND 51-10-6.

Part: STRINGER — CRACKED (BS 294.5)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND A CRACK IN STRINGER 16 AT STATION 294.5, LBL 59 AND WL 217. MAINTENANCE REMOVED AND REPLACED PART OF THE STRINGER IAW UPS EO B727-5310-1259F.

Part: STRINGER — CORRODED (BS 1110)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON STRINGER 7L STATION 1110 - 1176. MAINTENANCE REMOVED THE DAMAGED AREA, FABRICATED REPAIR PARTS, AND INSTALLED IAW SRM 53-10-3 AND SRM 51-30-2.

Part: SPAR WEB — CORRODED (LT WING)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON THE LEFT WING FRONT SPAR CENTER TANK ACCESS DOOR CUTOUT ON THE OUTER SURFACE. MAINTENANCE REMOVED THE DAMAGED AREA, REPAIRED AND INSTALLED PER SRM 57-30-3 AND UPS EO 727-57-1630.

Part: CHORD — CORRODED (BS 334)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON THE UPPER NOSE CHORD AT STATION 334 AND 335 AND LBL 14.5. MAINTENANCE REPLACED THE CHORD IAW SRM 51-10-2, 51-10-6, 51-30-2. 53-10-1 AND MM 51-20-4.

Part: RIB — CRACKED (NR 6 LE SLAT)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND A CRACK IN THE RIB OF THE NR 6 SLAT ATTACH ROD END ATTACH POINT. MAINTENANCE REMOVED THE CRACKED RIB AND REPLACED WITH A NEW RIB IAW SRM 51-30-2, 51-30-8 AND 51-30-5.

Part: STIFFENER — CRACKED (HORIZ STAB)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND A CRACK ON THE LEFT HORIZONTAL STABLIZER WEB STIFFENER AT STATION 54 ON THE UPPER SIDE OF THE STIFFENER. MAINTENANCE REMOVED THE CRACKED STIFFENER AND REPLACED WITH NEW IAW SRM 57-30-2.

Part: STRINGER — CORRODED (BS 1110)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION AND BARE METAL ON STRINGER 4R AT STATION 1110 - 1180. MAINTENANCE REMOVED THE DAMAGED AREA, FABRICATED AND INSTALLED IAW SRM 53-10-1, 53-10-2, 51-10-6, 53-10-3, 51-30-2.

Part: SPAR CHORD — CRACKED (LT HORIZ STAB)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND A CRACK IN THE LEFT HAND HORIZONTAL STABILIZER LOWER AFT SPAR CHORD AT STAB STATION 170. MAINTENANCE STOP DRILLED THE CRACK, NDT VERIFIED CONTAINMENT, FABRICATED REPAIR ANGLE DOUBLER.

Part: BLKHD SUPPORT — CORRODED (BS 680)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON THE FORWARD CARGO BAY AT THE HORIZONTAL ANGLE OF THE 680 BULKHEAD SUPPORT, LBL 13 RBL 17 AND WL 198. MAINTENANCE REPLACED THE SUPPORT IAW SRM 51-20-1, 51-30-5 AND 51-30-2.

Part: SILL — CORRODED (BS 304)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON THE MOPSILL AT STATION 304 TO 344, RBL 61 AND WL 208. MAINTENANCE REMOVED THE CORROSION, FABRICATED REPAIR PARTS AND INSTALLED PER SRM 53-10-1, 53-10-2 AND 51-30-2.

Part: TE WEDGE — DELAMINATED (LT TE MIDFLAP)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND DELAMINATION ON THE LEFT WING OUTBOARD MIDFLAP TRAILING EDGE WEDGE. MAINTENANCE REMOVED THE DAMAGED AREA, FABRICATED GLASS REPAIR AND INSTALLED IAW SRM 51-40-6.

Part: TE WEDGE — DELAMINATED (LT TE MIDFLAP)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND DELAMINATION ON THE INBOARD END UPPER SURFACE OF THE TRAILING EDGE WEDGE, ON THE LEFT WING INBOARD MIDFLAP. MAINTENANCE REMOVED THE DAMAGED AREA, APPLIED FIBERGLASS AND COMPLETED THE REPAIR PER SRM 51-40-6.

Part: SKIN — DELAMINATED (RT TE AFT FLAP)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND DELAMINATION ON THE UPPER SURFACE OF THE RIGHT WING INBOARD AFT FLAP. MAINTENANCE REMOVED THE DAMAGED AREA, APPLIED FIBERGLASS AND COMPLETED REPAIR PER SRM 51-40-6.

Part: SKIN — DELAMINATED (RT TE AFT FLAP)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND DELAMINATION AND MULTIPLE DENTS ALONG THE LOWER SURFACE OF THE RIGHT WING INBOARD AFT FLAP. MAINTENANCE REMOVED THE DAMAGED AREA, APPLIED FIBERGLASS AND COMPLETED REPAIRS PER SRM 51-40-6.

Part: TE WEDGE — DELAMINATED (RT TE MIDFLAP)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND DELAMINATION ON THE RIGHT WING INBOARD MIDFLAP TRAILING EDGE WEDGE, AT THE UPPER SURFACE NR 3 AFT FLAP CARRIAGE AND LOWER SURFACE AT THE NR 4. MAINTENANCE REPLACED THE TRAILING EDGE WEDGE.

Part: TE SKIN — DELAMINATED (RT TE MIDFLAP)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND DELAMINATION ON THE RIGHT WING INBOARD MIDFLAP UPPER AND LOWER TRAILING EDGE SURFACES, AT NR 1 AFT FLAP CARRIAGES. MAINTENANCE REPLACED THE TRAILING EDGE WEB.

Part: SKIN — DELAMINATED (LT TE AFT FLAP)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND DELAMINATION ON THE LEFT WING OUTBOARD AFT FLAP UPPER SURFACE CENTER. MAINTENANCE REMOVED THE DAMAGED AREA, FABRICATED FIBERGLASS REPAIR AND INSTALLED PER SRM 51-40-6.

Part: DOUBLER — DELAMINATED (RT TE FOREFLAP)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND DELAMINATION AT THE SEAM DOUBLER ON THE RIGHT WING INBOARD FOREFLAP LOWER SURFACE. MAINTENANCE REMOVED THE DAMAGED AREAS, APPLIED FIBERGLASS AND COMPLETED THE REPAIR PER SRM 51-51-11, 51-40-6.

Part: SKIN — DELAMINATED (RT TE FOREFLAP)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND DELAMINATION IN THE RIGHT WING INBOARD FOREFLAP ALONG THE LEADING EDGE INBOARD END LOWER SURFACE. MAINTENANCE REMOVED THE DAMAGED AREA, APPLIED FIBERGLASS AND COMPLETED REPAIR PER MM 51-20-151, 51-40-6.

Part: WEB — CRACKED (BS 1217)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND A CRACK EMANATING FROM THE LIGHTENING HOLE OF THE LEFT HAND AIRSTAIR WEB AT STATION 1217 AND WL 184. MAINTENANCE REPAIRED THE DAMAGE PER SRM 51-40-2.

Part: CLIP — CORRODED (BS 1166)

WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON THE STRINGER CLIP AT STATION 1166 AND STRINGER 22R. MAINTENANCE REMOVED THE STRINGER CLIP, FABRICATED NEW STRINGER AND INSTALLED PER SRM 51-20-1 AND 51-30-2.

Part: LOCK ASSY — LACK OF LUBE (NLG)

PILOT REPORTED, NOSE GEAR FAILED TO EXTEND ON FINAL, CYCLED GEAR PER AOM AND GEAR OPERATED NORMAL. CLEANEDAND INSPECTED UPLOCK ASSY, LUBRICATED PER MM 12-21-11.

Part: CRT — FAILED (LT FLIGHT DECK)

PILOT REPORTED, SMOKE IN FLIGHT DECK ON INBOUND LEG TO PHL. CAPT'S UPPER CRT IS SUSPECT DO TO SCREEN BLANKED AFTER FUMES AND SMOKE, NOTICED BY FLIGHT CREW. REPLACED CRT ON CAPTAIN'S SIDE.