N954UP

Part: BATTERY — INOPERATIVE (EMERGENCY EXIT)

EXIT LIGHT OVER COCKPIT DOOR INOP. REMOVED AND REPLACED LIGHT ASSY AND BATTERIES. OPS CK GOOD PER AMM 33-50-01-5.

Part: TAB — CORRODED (RT AILERON) · airframe 62,079 hrs · 53,369 cycles

INSPECTION TYPE:C, I/B RIGHT AILERON TAB HINGE CASTINGS ARE CORRODED AND SUSPECT CRACK ON AILERON REAR SPAR. REMOVED AILERON IAW AMM 27-10-00, REMOVED HINGES & SPAR IAW SRM 51-3 -30-02. SPAR REPAIRED IAW SRM 57-30-2 FIG 7 & SRM 51-40-02 FIG 1. NEW HINGES INSTALLED IAW SRM 51-30-2 AND DWG 65-21765. WEIGHT OF REPAIR .051LB ARM 20.75 INCHS. INSTALLED TAB HINGES IAW SRM 51-30-02 AND INSTALLED TAB IAW MM 27-10-05.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 62,074 hrs · 53,369 cycles

INSPECTION TYPE: C, ON REMOVAL OF INTERCOSTAL TO FACILITATE RIGHT FITTING REPLACEMENT AT BS 740, A CRACK WAS FOUND. REPLACED INTERCOSTAL WEB IAW SRM 51-20-04.

Part: WEB — CRACKED (FUSELAGE) · airframe 62,074 hrs · 53,369 cycles

INSPECTION TYPE:C, BS 740 LOWER WEB RBL 35, WL 160 SUSPECT CRACK IN THIS LOCATION. HFEC CARRIED OUT IAW NDTM 51-00-00, CRACK CONFIRMED WITHIN FASTENER HOLE. REPAIR CARRIED OUT IAW SRM 53-10-9 FIG 4.

Part: WEB — CRACKED (BS BL 35 WL1) · airframe 62,074 hrs · 53,369 cycles

INSPECTION TYPE-C BS 740 LOWER WEB RT BL 35 WL160 APPROX SUSPECT CRACK IN THIS LOCATION. HFEC CARRIED OUT ON ABOVE AREA IAW NDTM 51-00-00 PT 6 FIG 4 CRACKS CONTAINED WITHIN FASTENER HOLE. REPAIR PARTS FABRICATED IAW SRM 53-10-09. REPROTECTED REP PARTS AND DAMAGED AREA IAW SRM 51-10-02. SEALANT APPLIED IAW SRM 51-20-04.

Part: DOOR — CRACKED (RT WING MLG) · airframe 62,074 hrs · 53,369 cycles

INSPECTION TYPE:C, BRACKET CRACKED ON WING DOOR FWD OF HINGE CASTING. STOP DRILLED CRACK IAW SRM 51-10-01. HFEC CARRIED OUT AROUND STOP DRILLED AREA IAW B727 NDTM 51-00-00 PT 6 FIG 4. CRACK CONTAINED WITHIN STOP DRILLED AREA. REPAIRED IAW SRM 51-20-01.

Part: SKIN — CORRODED (RT OB AILERON) · airframe 62,074 hrs · 53,369 cycles

INSPECTION TYPE-C RT OB AILERON HAS PITTING CORROSION ON CONTROL ROD ATTACH CASTING. AILERON REPLACED IAW MM 27-10-14.

Part: SKIN — CRACKED (LT WING) · airframe 62,074 hrs · 53,369 cycles

INSPECTION TYPE: C, SUSPECT CRACK AT FWD UPPER CORNER OF LEFT WING ICE LIGHT CUTOUT. HFEC CARRIED OUT ON ABOVE AREA IAW B727 NDTM 51-00-00 PT 6 FIG 4, CRACKS CONFIRMED, ENDS MARKED. DOUBLER AND FILLER INSTALLED IAW SRM 53-30-03. WEIGHT OF REPAIR 2.37 LBS.

Part: BRACKET — CRACKED (FWD CARGO DOOR) · airframe 62,074 hrs · 53,369 cycles

INSPECTION TYPE: C, FWD CARGO DOOR BRACKETS CRACKED AT UPPER AFT HINGE ATTACH POINT. REMOVED BRACKETS IAW 51-30-02. NEW BRACKETS FABRICATED IAW BOEING DRAWING 69-18203. NEW BRACKETS INSTALLED IAW 51-30-02.

Part: FITTING — CORRODED (WING CENTER SECT) · airframe 62,074 hrs · 53,369 cycles

INSPECTION TYPE:C DURING REMOVAL OF RIGHT 740 FITTING CORROSION FOUND ON CENTER WING SECTION FRONT SPAR UPPER CHORD AT RBBL 65-70 APPROX CORROSION REMOVED IAW SRM 51-10-06. REPAIR ANGLES FABRICATED IAW SRM 53-30-03. HFEC CARRIED OUT ON ABOVE AREA IAW B727-NDTM 51-00-00 PT 6 FIG 4, NO DEFECTS FOUND.

Part: FITTING — CORRODED (LT OB AILERON) · airframe 62,074 hrs · 53,369 cycles

INSPECTION TYPE:C, LEFT O/B AILERON TAB MAST FITTINGS HAVE PITTING CORROSION AROUND BUSHINGS. ON INVESTIGATION LEFT O/B AILERON TAB FITTINGS FOUND TO BE OUTSIDE LIMITS. LEFT O/B AILERON TAB REPLACED IAW 27-10-19.

Part: HINGE — CORRODED (RT IB AILERON) · airframe 62,074 hrs · 53,369 cycles

INSPECTION TYPE-C RT IB AILERON TAB HINGE CASTINGS ARE CORRODED AND SUSPECT CRACK ON AILERON REAR SPAR. REPLACED REAR SPAR IAW SRM 51-30-02. NEW TAB HINGES INSTALLED IAW SRM 51-30-02

Part: PRESSURE PANEL — CRACKED (NLGWW) · airframe 62,074 hrs · 53,369 cycles

INSPECTION TYPE: C, CRACK FOUND ON NWW LEFT SIDEWALL JUST BELOW LEFT AFT SIDE PRESSURE PANEL. HFEC CARRIED OUT IAW B727 NDTM 51-00-00 PT 6 FIG 4, CRACK CONFIRMED, ENDS MARKED. STOP DRILLED CRACKS IAW SRM 51-10-01. HFEC CARRIED OUT AROUND STOP DRILLED AREAS IAW B727 NDTM 51-00-00 PT 6 FIG 4. CRACKS CONTAINED WITHIN STOP DRILLED AREA. REPAIRED IAW SRM 51-40-02.

Part: TERMINAL — CRACKED (TAIL SKID BAY) · airframe 62,074 hrs · 53,369 cycles

INSPECTION TYPE: C, TAIL SKID BAY STABILIZING LINKS UPPER AND LOWER LEFT AFT TERMINALS CRACKED AND LOWER AFT RIGHT TERMINAL CRACKED. INSTALLED NEW UPPER AND LOWER LEFT AFT TERMINALS ON TAILSKID BAY, FABRICATED LOWER AFT RIGHT TERMINAL AND FITTED IAW SRM 51-30-2.

Part: FITTING — CRACKED (FUSELAGE) · airframe 62,074 hrs · 53,369 cycles

INSPECTION TYPE:C, TO GAIN ACCESS FOR NDT PLEASE REMOVE FASTENERS BETWEEN STR 23 & 24 BS 740 FITTING RIGHT. REMOVED FASTENERS IAW SRM 51-30-02. HFEC CARRIED OUT ON ABOVE AREA IAW B727 NDTM 51-00-00 PT6 FIG 4, CRACK CONFIRMED, ENDS MARKED. REF UPS EO B727-5310-7477-E FOR FITTING REPLACEMENT.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 62,074 hrs · 53,369 cycles

INSPECTION TYPE:C, BS 178 BULKHEAD: EVIDENCE OF CRACK ON FWD FACE AT RBL 10 WL 235.1 EMANATING FROM FASTENER HOLE. HFEC CARRIED OUT IAW NDTM 51-00-00 FIG 4. CRACK CONFIRMED AND ENDS MARKED. CUT OUT DAMAGED AREA IAW SRM 53-10-9. HFEC CARRIED OUT, NO DEFECTS FOUND. REPAIR DOUBLER INSTALLED IAW SRM 53-10-9.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 62,074 hrs · 53,369 cycles

INSPECTION TYPE: C, SKIN BULGING AT BS 1307-1315 STR 8L. FOUND BULGING WAS CAUSED BY CORROSION ON STRINGER EXTRUSION. CORROSION REMOVED AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1. REPAIR DOUBLER INSTALLED IAW SRM 53-30-3.

Part: LIGHT — INOPERATIVE (CREW ENTRY)

INSPECTION TYPE:N/A, CREW ENTRY EMERGENCY LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM 33-50-67, OPS CHECK GOOD.

Part: FAN — INOPERATIVE (CABIN COOLING)

DURING CLIMB ACRID ODOR NOTED IN COCKPIT. CREW TURNED OFF GASPER FAN, ODOR WENT AWAY. GASPAR FAN DEACTIVATED AND PLACED ON MEL M286609 & MEL CLOSED ON LP 212332. REPLACED GASPER FAN PER B727 MM CH 21-23-22, GASPER FAN OPS CHECK NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY EXIT)

INSPECTION TYPE:N/A COCKPIT EMERGENCY EXIT LIGHT HAS 1 LAMP INOP. RELAMPED AS REQUIRED, OPS CHECKS GOOD IAW M/M 33-50-01.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 61,567 hrs · 52,963 cycles

INSPECTION TYPE: C, ON REMOVAL OF BLIND FASTENER STRINGER FOUND DAMAGED (CRACKED) AT FUSELAGE HOLE STRINGER 26L AT BS 320. CRACK CONTAINED IAW SRM 53-10-3. HFEC INSP CARRIED OUT ON THE ABOVE AREA IAW B727 NDTM PT 6 51-00-00 FIG 4 &16 RESULT. NO DEFECTS FOUND CRACK CONTAINED. REPAIR CARRIED OUT IAW SRM 53-10-3.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 61,567 hrs · 52,963 cycles

INSPECTION TYPE: C, 2 SUSPECT CRACKS AT SHEAR STRAPS AT LBBL 20 BETWEEN BS 294 & BS 328 2 REPAIRS. FABRICATED NEW SHEAR TIES IAW SRM 51-20-1. REPAIRED SHEAR TIES IAW SRM 51-40-3. INSTALLED NEW SHEAR TIES IAW SRM 51-30-2.

Part: ANGLE — CRACKED (NR 6 SLAT) · airframe 61,567 hrs · 52,963 cycles

INSPECTION TYPE: C, NR 6 SLAT, O/B TRACK TO SLAT ATTACH ANGLE IS CRACKED. ANGLE FABRICATED IAW SRM 51-20-01. ANGLE INSTALLED IAW SRM 51-20-02.

Part: BRACKET — CRACKED (NR 3 SLAT) · airframe 61,567 hrs · 52,963 cycles

INSPECTION TYPE: C, NR 3 SLAT, STRUCTURE SUPPORT ANGLE IS CRACKED JUST I/B OF WHERE ACTUATOR EYE END ATTACHES TO SLAT. BRACKET REMOVED IAW SRM 51-30-02. BRACKET FABRICATED IAW SRM 51-20-01. BRACKET INSTALLED IAW SRM 57-50-03 & SRM 51-30-02.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,567 hrs · 52,963 cycles

INSPECTION TYPE:C SUSPECT CRACK AT FWD ENTRY DOOR CUTOUT AT FWD UPPER CORNER AS MARKED. HFEC INSP CARRIED OUT IAW B727 NDTM PT 6 51-00-00 FIG 4. RESULT CRACK CONFIRMED. REPAIR CARRIED OUT IAW UPS EO B727-5330-1460-D. REPAIR AT FWD ENTRY DOOR REPAINTED IAW MM 51-20-91.

Part: SUPPORT BRACKET — CRACKED (WX RADAR SYS) · airframe 61,567 hrs · 52,963 cycles

INSPECTION TYPE: C, WEATHER RADAR TX MOUNTING PLATE, SUPPORT BRACKET AFT LEFT SIDE IS CRACKED. REPAIR CARRIED OUT IAW SRM 51-40-2 FIG 1 SHEET 1.

Part: SKIN — CORRODED (LT ELEVATOR) · airframe 61,567 hrs · 52,963 cycles

INSPECTION TYPE: C, LT ELEV UPPER SURFACE, CORROSION BENEATH I/B & 2ND FROM I/B STATIC DISCHARGE BASES. DISCHARGE BASE REMOVED IAW SRM 51-30-02 ON 2ND FROM I/B STATIC BASE. CORROSION REMOVED AND FOUND TO BE OUTSIDE OF LIMITS IAW SRM 55-20-1. REPAIRS CARRIED OUT IAW SRM 55-20-3 FIG 2. STATIC DISCHARGERS INSTALLED IAW MM 23-61-00. TEST CARRIED OUT PER MM 23-61-00, FOUND TO BE SATISFACTORY.

Part: STOP — CRACKED (PAX DOORWAY) · airframe 61,567 hrs · 52,963 cycles

INSPECTION TYPE: C, AFT NR 1 DOOR STOP ON FWD DOOR HAS A SUSPECT CRACK. HFEC INSP CARRIED OUT ON AFT NR 1 DOOR STOP ON FWD DOOR IAW B727 NDTM PT 6 51-00-00 FIG 4. RESULT - CRACK CONFIRMED. AFT NR 1 DOOR STOP FITTING REPAIRED IAW EO B727-5230-0032-N APPX C REFERENCE NRC 674885.

Part: WASHER — MISSING (PRESSURE PANEL) · airframe 61,567 hrs · 52,963 cycles

INSPECTION TYPE: C, AIR LEAK AT NWW PRESSURE PANEL, RT FWD PANEL. PANEL REMOVED IAW MM 20-80-01. FIBRE WASHERS FOUND TO BE MISSING & REPLACED IAW IPC 25-53-00. ON FURTHER INVESTIGATION CRACK FOUND ON NWW SIDE WALL. AREA CUT OUT IAW SRM 51-40-2. REPAIRED AREA IAW SRM 51-40-2. LEAK CHECKED REPAIR AREA AND PANEL IAW MM 21-30-01. NO LEAKS FOUND.

Part: LIGHT — INOPERATIVE (CABIN)

EMERGENCY EXIT LIGHT AT CREW ENTRY DOOR INOPERATIVE. PERFORMED ADJ/TEST OF EMERGENCY LIGHTS IAW MM 33-50-01. OPS CHECK GOOD. NO DEFECTS NOTED.

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,381 hrs · 40,253 cycles

INSPECTION TYPE: C&SI, FUSELAGE FAIRING NR 3431, AFT FORMED SECTION HAS HEAVY CORROSION UNDER FLOATING ANCHOR NUTS REMOVED FASTENERS ON FRAME IAW SRM 51-30-02. CORRODED SECTION OF FRAME FOUND TO BE OUTSIDE LIMITS IAW SRM 51-10-01 FIG 1 & CORRODED SECT ION OF FRAME REMOVED IAW SRM 51-10-06 REPAIRED FRAME IAW SRM 51-40-3

Part: ANGLE — CRACKED (AFT CARGO DOOR) · airframe 52,381 hrs · 40,253 cycles

INSPECTION TYPE: C&SI, CRACK ON ANGLE AFT CARGO DOOR INTERIOR, JUST ABOVE FWD DOOR STOP FITTING REMOVED CRACKED ANGLE, AFTER DE-RIVETING AREA IAW SRM 51-30-2 FABRIC ATED NEW ANGLE IAW SRM 51-20-1 FIG 7. INSTALLED NEW ANGLE & REPAIRED IAW SRM 51-40-3

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 52,381 hrs · 40,253 cycles

INSPECTION TYPE: C&SI, SEAT TRACK CRACKED AT O/B FLANGE, RBL 45.5 BETWEEN BS 780 - BS 804 REPLACED SEAT TRACK IAW DRAWING NR 65-41980

Part: FLAP TRACK — CORRODED (WING) · airframe 52,381 hrs · 40,253 cycles

INSPECTION TYPE: C&SI, NR 7 FLAP TRACK - LIGHT SURFACE CORROSION IN HORIZ. HOLES I & J. NR 2 FLAP TRACK INSTALLED IN NR 7 FLAP TRACK POS. IAW MM 27-51-31

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 52,381 hrs · 40,253 cycles

INSPECTION TYPE: C&SI, SUSPECT CORROSION UNDER 2 STRIP PANELS EITHER SIDE OF FEEL COMPUTER BOTH PANELS HAVE SUSPECT BULGES IN AREAS AROUND FASTENERS TO FACILITATE ACCESS LT & RT PANELS NT 9703 & 9704 REMOVED IAW SR M 51-30-5 REMOVED LT & RT TEE SUPPORTS IAW SRM 51-30-2 LT & RT T-CHORD SUPPORTS REPLACED IAW DRAWING 65-72786

Part: WIRE — DAMAGED (CABIN)

INSPECTION TYPE:PFLT EMERGENCY EXIT LIGHT ABOVE FORWARD ENTRY DOOR INOP. NO POWER TO PINS 1 AND 5 FOR CHARGING, CORRECTED WIRING PER WDM 33-5 1-01. REPLACED BATTERIES PER MM 33-51-01 PAGE 201.

Part: SKIN — CORRODED (BS259.5 STR10RT)

INSPECTION TYPE:C CIRCUMFERENTIAL 259.5 EXHIBIT MATERIAL LOSS OF 10% AT STR 10RT. REMOVED FASTENERS & CUT OUT DAMAGE SKIN AS PER DRW 69-62161, SIVE OF CUT OUT 3.5" X 4.25". INSTALLED DOUBLER REPAIR AS PER EO B727-5310 -1371 APPENDIX E. DOUBLER SIZE 8" X 6".

Part: SKIN — CORRODED (BS441 STR18R-22R)

INSPECTION TYPE:C FUSELAGE CIRCUMFERENTIAL 441 EXHIBIT 10% MATERIAL LOSS STINGER 20R THRU STRINGER 22R. REMOVED FASTENERS FROM REPAIR AREA, CUT OUT CORROSION ON FUSELAGE SK IN BS 441 FROM STR 18R TO STR 22R IAW EO B727-5310-1371. SIZE OF CUT OUT 4.5" X 34.5". INSTALLED REPAIR AT FUSELAGE SKIN BS 441 FWD SKIN OUT FROM STR 18R TO STR22R AS PER EOB727-5310-1371. R&R EXISTING DO UBLER AFT SKIN BUTT STA 441 LAP SEAM AS PER B727 SRM 53-30-3.

Part: SKIN — CORRODED (BS640-660 6LT)

INSPECTION TYPE:C FUSELAGE SKIN MISSING RIVET HEAD AT LAP JOINT 6LT AND SOME OTHER RIV ETS ARE DISHED BS 640 TO 660. REMOVED RIVETS AT FUSELAGE SKIN LAP JOINT 6LT FROM FS640 TO 660 AND FOUND CORROSION ON LOWER SKIN FS 650 OUT OF LIMITS. CUT OUT DAMAGED AREA AT FS 650 STR60 IAW SRM 53-30-3, SIZE OF CUT OUT 5" X 3". INST ALLED DOUBLER REPAIR IAW BOEING COMPANY SERVICE ENG. UPS MIA-02-000- 1H & SRM53-30-3.

Part: CONTROL UNIT — FAULTY (SMOKE DETECTION)

INSPECTION TYPE:PFLT D/D M220970 LOWER AFT CARGO SMOKE DETECTOR. SUP SYS INOP. INSTALLED CONTROL UNIT IAW MM 26-18-04. REQUIRES ADJ/TEST KSM 55919 PERFORMED SMOKE DETECTOR / CONFIG MODULE ADJ/TEST MM 26-18-01 AND LOWER CARGO COMP SMOKE DETECTION ADJ/TEST MM 26-18-00. NO DEFECTS NOTED. OK FOR SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE:N/A, EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERY PACKS, OPS NORMAL.

Part: SWITCH — FAILED (LE FLAPS)

INSPECTION TYPE:N/A PILOT REPORT NR 2 L/E FLAP DISAGREE LIGHT ILLUM (RFD) REPEAT ITEM - NR 2 LED AMBER FLAP LIGHT ILLUM TECH RECOMMENDS:REPLACE NR 2 LEADING EDGE FLAP SWITCH(PREVIOUS SWITCH WAS REPLACED IN RFD ON 12/27 WAS BAD FROM STOCK NEW SWITCH & ACTUATING ARM INSTALLED LED INDICATIONS ON FWD PANEL & F/E ALL FUNCTION CORRECTLY AT THIS TIME MEL CLEARED

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,542 hrs · 51,932 cycles

INSPECTION TYPE: C+SI. DURING INSPECTION OF SECTION 41 RT SKIN. 13 FASTENER HOLES HAVE CRACKED INDICATIONS. HFEC INSP. C/O IN SECT.41 AREA IAW B727 NDT MANUAL D6-48875,PT6,SUB 51-00-00 FIG16 ON ACCESSED HOLES.RESULT NDF. HFEC INSP C/O IAW B727 NDT MANUAL,PT6,51-00-00,FIG4. AROUND CRACKED SKIN CUTOUTS. NDF. REPAIRED IAW SRM 53-30-3 FIG3. AND UPS.EO.B727-5330-0795 SECT41 RT SKIN BS 255 - 225, WL 234 - 207.5.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 60,542 hrs · 51,932 cycles

INSPECTION TYPE: C+SI, WHILE REPLACING REINFORCEMENT FRAME, SUPPORT BRACKET FOUND CRACKED. FABRICATED NEW BRACKET IAW SSRM 51-20-01. INSTALLED BRACKET IAW SRM 51-30-2

Part: GIMBAL PIN — CORRODED (JACKSCREW) · airframe 60,542 hrs · 51,932 cycles

INSPECTION TYPE: C+SI, HORIZONTAL STABILIZER JACKSCREW-GIMBLE ASSY HAS CORROSION IN BORE AND PIN OUTER SURFACE. REPLACE GIMBLE ASSY IAW MM 51-10-01 AND ACTUATOR PINS IAW MM 51-10-0 1

Part: RIB — CRACKED (NR 8 FLAP) · airframe 60,542 hrs · 51,932 cycles

INSPECTION TYPE: C+SI. NR 8 FLAP TRACK SECOND RIB FROM FWD END, CRACKED ON MID FAIRING. RIB REPLACED IAW DRAWING NR 65-21796.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 60,542 hrs · 51,932 cycles

INSPECTION TYPE: C+SI, WHILE RECTIFING CORROSION ON FLOORBOARD, TRANSVERSE FLOORBEAM AT BS 1183, FOUND TO BE CORRODED. CORROSION REMOVED IAW SRM 51-10-6. CORROSION FOUND TO BE OUTSIDE LIMITS AND REINFORCED CHORD REPLACED IAW DRW #65-19606.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 60,542 hrs · 51,932 cycles

INSPECTION TYPE: C+SI, ON REMOVAL OF CORRODED BOLT BS 740 FRONT SPAR BULKHEAD LINK & SEAT TRACK FOUND CORRODED. LINK & SEAT TRACK REPLACED IAW SRM 51-10-01 & SRM 51-30-02 BS740-BS7 60.

Part: CARRIAGE — CORRODED (TE FLAP) · airframe 60,542 hrs · 51,932 cycles

INSPECTION TYPE:C+SI, NR 2 FLAP TRACK SPINDLE BORE CORRODED. REPLACED FLAP TRACK CARRIAGE IAW 27-51-13 & OHM 57-52-11.

Part: CARRIAGE — CORRODED (TE FLAP) · airframe 60,542 hrs · 51,932 cycles

INSPECTION TYPE:C+SI, NR 1 FLAP TRACK CARRIAGE SPINDLE BORE CORRODED (INSIDE BORE.) NR 1 CARRIAGE REPLACED IAW MM 27-51-13.

Part: SUPPORT FITTING — CORRODED (VERTICAL STAB) · airframe 60,542 hrs · 51,932 cycles

INSPECTION TYPE: C+SI, RT STABILIZER HINGE BEARING OB SUPPORT LUG SHOWS CORROSION INDICATION DURING HFEC INSPECTION. CORROSION REMOVED AND LUG REWORKED, COMPLETED IAW EO B727-5510-2284 APPEX B.P6 3-7 (F)-(J).HFEC INSP C/O IAW B727 NDT MANUAL,PT6,51-00-0 0.FIG4 ON OB LUG BORE.NDF.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 60,542 hrs · 51,932 cycles

INSPECTION TYPE: C+SI, CORROSION ON SEAT TRACK BS 560-600 LBL/RBL0. SEAT TRACK REPLACED IAW SRM 51-10-01 AND INSTALLED IAW SRM 51-30-02.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 60,542 hrs · 51,932 cycles

INSPECTION TYPE: C+SI, FRAME LEG CRACKED AT ATTACHMENT TO SKIN BETWEEN STR 17L - STR 18L AT BS 1110. HFEC INSP C/O ON 7 CSK HOLES AT ABOVE LOCATION IAW B727 NDT MANUAL D6-48875.PT6,SUBJECT 53-30-00 FIG 3. FRAME LEG REPAIRED IAW SRM 53-10- 4 FIG11.RESULT NDF.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 60,542 hrs · 51,932 cycles

INSPECTION TYPE: C+SI, SURFACE CORROSION ON FLOORBEAM BS 344 LBL & RBL 0. HFEC C/O IN AREA OF BLEND CORROSION/CUTOUT IAW B727 NDT MANUAL PT6, 51-00-00 ,FIG4 .NDF. CORROSION REMOVED IAW SRM 51-10-06. FLOORBEAM REPA IRED IAW SRM 53-10-08 FIG7.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 60,542 hrs · 51,932 cycles

INSPECTION TYPE: C+SI, CORROSION ON FLOORBEAM, BS640 BETWEEN RBL 24.75 - 45.5 (CABIN) HFEC C/O IAW B727 NDT MANUAL PT6 51-00-00 FIG4 AROUND CUTOUT.NDF. FLOORBEAM REPAIRED IAW SRM 53-10-8 FIG 5.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 60,542 hrs · 51,932 cycles

INSPECTION TYPE: C+SI, CORROSION ON FLOORBEAM BS 640 BETWEEN RBL 24.75 & 45.5. HFEC C/O IAW B727 NDT MANUAL PT6 51-00-00 FIG4 AROUND CUTOUT.NDF.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 60,542 hrs · 51,932 cycles

INSPECTION TYPE:C+SI CORROSION ON STRINGER 21R AT BS 390 IN E/E BAY. CORROSION REMOVED IAW SRM 51-10-6 AND STRINER REPAIRED IAW SRM 53-10-3 F IG2.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 60,542 hrs · 51,932 cycles

INSPECTION TYPE:C+SI FLOOR SUPPORT IN E/E BAY AT BS 380 ABOVE STR 25R IS CRACKED. REPAIRED SUPPORT IAW SRM.51-20-1,SRM.51-30-1

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 60,542 hrs · 51,932 cycles

INSPECTION TYPE:C+SI INTERCOSTAL UNDER LAVATORY DOOR AND PARTITION CORRODED (FWD TOILET) INTERCOSTAL REPLACED IAW SRM 53-10-02 AND SRM 51-10-1

Part: PIN — CORRODED (BOTTLE) · airframe 60,542 hrs · 51,932 cycles

INSPECTION TYPE:C+SI RT BS 740 BOTTLE PIN CORRODED. BOTTLE PIN REMOVED AND REPLACED ***CPCP***

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 60,542 hrs · 51,932 cycles

INSPECTION TYPE: C+SI, CORROSION ON FLOORBEAM BS 680 BETWEEN BL 0 & RBL 24.75. HFEC C/O IAW B727 NDT MANUAL PT6,51-00-00FIG4 AROUND TRIM AREA. NDF. FLOORBEAM REPAIR IAW SRM 53-10-08 FIG5.

Part: SPAR — CRACKED (HORIZONTAL STAB) · airframe 60,542 hrs · 51,932 cycles

INSPECTION TYPE:C+SI LT HOROZONTAL STAB, FRONT SPAR LOWER CHORD CRACKED @ LE STA 236 - 248. HFEC C/O IAW B727 NDT MANUAL, PT6, 51-00-00, FIG 4. CRACK ENDS MARKED BEFORE REPAIR AND POST DAMAGE REMOVAL. NO DEFECTS FOUND. REPAIR C/O IAW SRM 55-10-5

Part: SKIN — CRACKED (THRUST REVERSER) · airframe 60,542 hrs · 51,932 cycles

INSPECTION TYPE: C+SI. ENGINE NR 1 THRUST REVERSER LOWER DOOR INNER SKIN CRACKED AT MID SECTION . DYE PENETRANT INSPECTION CARRIED OUT TO LOCATE ENDS IAW B727 SOP D6- 51702, SECTION 20-20-02. RESULTS; ENDS MARKED & STOP DRILLED. CRACK FOUND TO BE CONTAINED WITHIN STOP DRILL HOLES. REPAIR CARRIED OUT IAW SRM CHP.78-30-01.FIG 201.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 60,542 hrs · 51,932 cycles

INSPECTION TYPE:C+SI SUSPECT CRACK ON BS 178 BULKHEAD LT STR 17L. HFEC INSPECTION CARRIED OUT IAW B727-NDT MANUAL, PT6,51-00-00,FIG4. CRACK CONFIRMED ON BS 178 BULKHEAD LT ANGLE, AT STR 17L. CRACK CUT OUT IAW SRM 51-40-3 FIG1 .HFEC INSP C/O IAW B727 NDT MANUAL,PT6,51-00-00, FIG4 AFTER DAMAGE REMOVED. NO DEFECT FOUND.

Part: SLEEVE — CORRODED (FUSELAGE) · airframe 60,542 hrs · 51,932 cycles

INSPECTION TYPE:C+SI BS 740 RT FITTING SLEEVE CORRODED. RT BS 740 FITTING SLEEVE REPLACED IAW.DRW 65C13724 ***CPCP***

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 60,542 hrs · 51,932 cycles

INSPECTION TYPE: C+SI. LOWER FWD CARGO HOLD CRACKED ON CARGO DOOR FRAME AT BS 570 BETWEEN STR 21 RT & 22 RT. HFEC INSP CARRIED OUT IAW B727 NDT MANUAL, PT6, 51-00-00, FIG 4. TOTAL OF 6 CRACKS FOUND. CRACK ENDS MARKED. FRAME REPAIRED IAW SRM 53-10-4 FIG 10 AND SRM 51-30-2.

Part: SPOILER PANEL — CONTAMINATED (WING) · airframe 60,542 hrs · 51,932 cycles

INSPECTION TYPE: C+SI. X-RAY INSPECTION HAS SHOWN THAT NR 13 SPOILER PANEL HAS SOME MOISTURE CONTAMINATION. NR 13 SPOILER PANEL REMOVED IAW MM 27-61-01. NR 13 SPOILER PANEL INSTALLED IAW MM 27-61-01.

Part: FRAME — TORN (FUSELAGE) · airframe 60,542 hrs · 51,932 cycles

INSPECTION TYPE:C+SI. SMALL TEAR IN FRAME BS620 @ STR 5 & 6 RT (CABIN). HFEC INSP CARRIED OUT IAW B727 NDT MANUAL, PT6, 51-00-00, FIG4. POST DAMAGE REMOVAL. NDF. DAMAGED AREA BLENDED OUT IAW SRM 51-10-01 AND FRAME REPAIRED IAW SRM 53-10-04.FIG2.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 60,542 hrs · 51,932 cycles

INSPECTION TYPE: C&SI, CRACK ON CLEAT BETWEEN MAIN CARGO DOOR SILL & FRAME IN LWR FWD CARGO HOLD AT STA BS 500 REPAIRED PER SRM 51-40-2 FIG 1

Part: BEAM — CRACKED (RT WING) · airframe 60,542 hrs · 51,932 cycles

INSPECTION TYPE: C+SI. RT WING CRACKED ON SPOILER NR 8 SUPPORT BEAM AT IB HINGE. HFEC INSP C/O ON NR 8 SPOILER IB SUPPORT BEAM & HINGE IAW B727-NDT MANUAL PT6 SUBJECT 51-00-00 FIG16 & 4.RESULT NDF. REPAIR C/O IAW EO 2000-022-005 UPS FILE NR 727-57-2163.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,542 hrs · 51,932 cycles

INSPECTION TYPE:C+SI DURING HFEC INSP. OF SECTION 41 FUSELAGE SKIN, 2 FASTENER HOLES CRACKED, FOUND AT BS.203.8 BETWEEN WL207.5 AND WL234 RT. REPAIRED IAW SRM 53-30-3 FIG3 PER EO B727-5330-0795 BS203.8 WL207.5 TO WL234 RT.

Part: ATTACH ANGLE — CORRODED (NR 5 FLAP TRACK) · airframe 60,542 hrs · 51,932 cycles

INSPECTION TYPE: C+SI, NR 5 FLAP TRACK AFT ATTACH FLANGE UPPER SURFACE CORRODED. MACHINED AFT ATTACH FLANGE UPPER SURFACE IAW SOPM 20-10-02. REF SMRO EO2000-022-007 FOR REPAIR .UPS FILE NO.5740-2167.

Part: SKIN — CORRODED (FUSELAGE) · airframe 60,542 hrs · 51,932 cycles

INSPECTION TYPE:C+SI SUSPECTED CORROSION BETWEEN FUSELAGE SKIN AND INTERNAL DOUBLER BS 1140, BETWEEN STR 3 AND 4 RT. LFEC FOUND CORROSION. AREA DERIVETED IAW SRM 51-30-2 BS 1183 & 1110. EO.B727-5330-0509.APPX8.3 C/O

Part: FITTING — CORRODED (LT AILERON) · airframe 60,542 hrs · 51,932 cycles

INSPECTION TYPE:C+SI. LT OB AILERON 2 ND HINGE SUPPORT FITTING FROM IB IS BADLY CORRODED REPLACED FITTING IAW DRW NR 65-21708

Part: FITTING — CORRODED (LT WING) · airframe 60,542 hrs · 51,932 cycles

INSPECTION TYPE: C+SI. LT OB AILERON, IB END FITTING IS BADLY CORRODED AROUND ATTACH LUG FOR AILERON OPERATING ROD. REPLACED AILERON CASTING IAW DRW 65-21766.

Part: SPAR — PUNCTURED (AILERON) · airframe 60,542 hrs · 51,932 cycles

INSPECTION TYPE: C+SI. LT IB AILERON REAR SPAR IS PUNCTURED. REMOVED AILERON AND TAB IAW MM 27-10-01. REPAIR CARRIED OUT IAW SRM 5 1-40-2 FIG 1.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,542 hrs · 51,932 cycles

INSPECTION TYPE: C+SI. FASTENER HEAD MISSING & TWO OTHER FASTENERS HEADS DISHED AT BS 730 STR 14RT. REMOVED ALL FASTENERS ALONG LAP JOINT IAW SRM 52-30-2. HFEC ON COUNTER SINK IAW B727 MANUAL D6-48875. PT6. SUB 53-30-00 FIG 3 ON STR 14 RT BETWEEN BS 677 & BS 740 NOT INC. SKIN REPAIR. NDF.

Part: ATTACH ANGLE — CORRODED (NR 5 FLAP TRACK) · airframe 60,542 hrs · 51,932 cycles

INSPECTION TYPE: C+SI, NR 5 FLAP TRACK FWD ATTACH FLANGE UPPER SURFACE CORRODED. MACHINED FWD ATTACH FLANGE UPPER SURFACE IAW SOPM 20-10-02 AND OHM 57 -40-01. SMRO EO.2000-022-007.UPS FILE NO.5740-2167.

Part: FLAP TRACK — CORRODED (TE FLAP) · airframe 60,542 hrs · 51,932 cycles

INSPECTION TYPE: C+SI, NR 3 FLAP TRACK FWD ATTACH LUG CORRODED. MACHINED AREA TO REMOVE CORROSION. MPI C/O ON THE FWD ATTACH LUGS IAW B727 SOP D6-51702 CHP 20-20-01.NDF. REF SMRO EO.2000-022-006 FOR REP AIR UPS FILE NR .727-57-2164.

Part: FLAP TRACK — CORRODED (TE FLAP) · airframe 60,542 hrs · 51,932 cycles

INSPECTION TYPE: C+SI, NR 3 FLAP TRACK AFT FLANGE UPPER SURFACE & HOLES CORRODED INSIDE BORES & LWR SURFACES. MACHINED AREA TO REMOVE CORROSION. REPAIR CARRIED OUT IAW SMRO EO.200 022-004.UPS FILE NO727-57-2165.

Part: FITTING — CRACKED (NR 3 TE FLAP) · airframe 60,542 hrs · 51,932 cycles

INSPECTION TYPE:C+SI. NR 3 FLAP TRANSMISSION MOUNT FITTING IS CRACKED NR 3 FLAP TRANSMISSION REMOVED IAW MM 27-51-41. CASTING REPLACED BOEING DRAWING 65-16201. REFITTED NR 3 FLAP TRANSMISSION ASSY IAW MM.27-51-41.

Part: SKIN — CHAFED (THRUST REVERSER) · airframe 60,542 hrs · 51,932 cycles

INSPECTION TYPE: C+SI. ENGINE NR 3 TRUST REVERSER LOWER DOOR INNER SKIN WORN DUE CHAFING OF SEAL. REPAIR CARRIED OUT IAW SRM CHP.78-30-01 FIG 202.

Part: SKIN — CHAFED (THRUST REVERSER) · airframe 60,542 hrs · 51,932 cycles

INSPECTION TYPE: C+SI. ENGINE NR 1 TRUST REVERSER LOWER DOOR INNER SKIN WORN DUE CHAFING OF SEAL. REPAIR CARRIED OUT IAW SRM CHP 78-30-01 FIG202

Part: ANGLE — CRACKED (NR 2 ENGINE AREA) · airframe 60,542 hrs · 51,932 cycles

INSPECTION TYPE:C+SI ENGINE NR 2 AFT MOUNT SUPPORT RIB RIGHT CHORD INSIDE THE VERTICAL FIN HAS CRACKED SUPPORT ANGLE APPROX 17 INCHS FROM TOP OF CHORD. REPLACED CRACKED ANGLE IAW DRAWING NO.65-17553

Part: CARRIAGE — CORRODED (TE FLAP) · airframe 60,542 hrs · 51,932 cycles

INSPECTION TYPE:C+SI, NR 5 FLAP CARRIAGE SPINDLE OUTER SURFACE CORRODED UNDER FWD THRUST WASHER. REPLACED CARRIAGE.

Part: CARRIAGE — CORRODED (NR 3 TE FLAP) · airframe 60,542 hrs · 51,932 cycles

INSPECTION TYPE:C+SI NR 3 FLAPTRACK CARRIAGE SPINDLE BORE CORRODED (INTERNALLY) CARRAGE REPLACED. ***CPCP***

Part: CARRIAGE — CORRODED (TE FLAP) · airframe 60,542 hrs · 51,932 cycles

INSPECTION TYPE:C+SI, NR 7 FLAP CARRIAGE SPINDLE BORE CORRODED (INTERNALLY). REPLACED FLAP TRACK CARRIAGE IAW MM 27-51-13+OHMJ57-52-11.

Part: CARRIAGE — CORRODED (NR 6 FLAP) · airframe 60,542 hrs · 51,932 cycles

INSPECTION TYPE:C+SI NR 6 FLAP CARRIAGE SPINDLE BORE CORRODED (INTERNALLY) REPLACE NR 6 FLAP CARRIAGE.

Part: CARRIAGE — CORRODED (TE FLAP) · airframe 60,542 hrs · 51,932 cycles

INSPECTION TYPE:C+SI, NR 8 FLAP CARRIAGE SPINDLE BORE CORRODED. REPLACED CARRIAGE ASSY IAW MM 27-51-13.

Part: CARRIAGE — CORRODED (TE FLAP) · airframe 60,542 hrs · 51,932 cycles

INSPECTION TYPE:C+SI, NR 4 FLAP TRACK CARRIAGE SPINDLE BORE CORRODED. REPLACED CARRIAGE.

Part: FLAP TRACK — CRACKED (WING) · airframe 60,542 hrs · 51,932 cycles

INSPECTION TYPE:C+SI, NR 1 FLAP TRACK SUSPECT CRACK AT SPACER BLOCK FAIRING GUIDE BLOCK FWD HOLE. HFEC INSP CARRIED OUT IAW B727 NDT MANUAL, PART 6,51-00-00, FIG 4. CRACK CONFIRMED ON NR 1 FLAP TRACK SPACER BLOCK FAIRING GUIDE BLOCK FWD HOLE. TRACK REPLACED IAW MM 27-51-31.

Part: SUPPORT BRACKET — CRACKED (THRUST REVERSER) · airframe 60,542 hrs · 51,932 cycles

INSPECTION TYPE: C+SI. ENGINE NR 3 THRUST REVERSER OUTBOARD FAIRING MID SUPPORT BRACKET CRACKED. BRACKET REPLACED IAW MM.78-30-00

Part: SUPPORT BRACKET — CRACKED (THRUST REVERSER) · airframe 60,542 hrs · 51,932 cycles

INSPECTION TYPE: C+SI. ENGINE NR 1 THRUST REVERSER FAIRING MID SUPPORT BRACKET CRACKED. REPLACE BRACKET.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 60,542 hrs · 51,932 cycles

INSPECTION TYPE:C+SI LT 18A HAS SUSPECTED CRACK AT BS940 LOWER FWD ATTACHMENT BOLT. HFEC INSP CARRIED OUT IAW B727 NDT MANUAL,PT6,51-00-00,FIG4. CRACK CONFIRMED ON S18A LT BS 940 LT AND FUSELAGE SKIN FOUND CRACKED IN TWO PLACES AT THIS POSITION (BS940 LT STR 18A) CRACKS IN SKIN TRIMMED OUT IAW SRM 51-10-06.REPAIR C/O IAW SMRO. EO2000-022-003.UPS FILE NR 727-53-2263.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 60,542 hrs · 51,932 cycles

INSPECTION TYPE:C+SI SUSPECT CRACK IN MAIN CARGO DOOR SKIN AT FORWARD PRESSURE RELIEF DOOR UPPER FORWARD CUTOUT. HFEC INSP C/O IAW B727 NDT MANUAL,PT6,51-00-00,FIG4. CRACK CONFIRMED ON MAIN CARGO DDOOR AT FWD PRESSURE RELIEF DOOR FWD UPPER CORNER.REPAIR TO MCD SKIN C/O IAW SRM 52-00-03,IAW FIG3. NOTE THIS IS CATEGORY A TYPE REPAIR.HFEC INSP C/O IAW B727 NDT MANUAL,PT6,51-00-00,FIG4.POST DAMA GE REMOVED-NDF

Part: JACKSCREW — CORRODED (NLG) · airframe 60,542 hrs · 51,932 cycles

INSPECTION TYPE:C+SI NLG MANUAL EXTENSION JACK CORRODED JACKSCREW REMOVED AND REPLACED IAW MM 32-34-11. NLG MANUAL EXTENSION ADJUSTED IAW MM 3234-00

Part: ANGLE — CORRODED (FUSELAGE) · airframe 60,542 hrs · 51,932 cycles

INSPECTION TYPE: C+SI, CORROSION ON PULLEY SUPPORT BRACKET FOR NLG STEERING CABLES. WEB ANGLE FOUND CORRODED. ON REMOVAL OF PULLEY SUPPORT BRACKET, BRACKET FOUND TO BE O.K. AT BS 312L. PRESSURE WEB ANGLE FOUND TO BE CORRODED BEYOND LIMITS. REPLACED ANGLE IAW SRM 51-30-2 & DRW 65-18915. DYE PEN INSP C/O ON NEW WEB AN GLE IAW B727 NDT MANUAL SOP D6-51702 SECT 20-20-02.RESULT NDF.

Part: OUTFLOW VALVE — LEAKING (FUSELAGE) · airframe 60,542 hrs · 51,932 cycles

INSPECTION TYPE: C+SI, LT OUTFLOW VALVE LEAKING ON PRESSURIZATION. BOTH OUTFLOW VALVES REPLACED DUE PRESSURIZATION PROBLEM. REMOVED VALVE IAW MM21-30-52.

Part: SKIN — CORRODED (BS 913)

INSPECTION TYPE:C, UPPER FUSELAGE SKIN HAS BULGE AND SKIN CRACKED AT BS 913 AND STR 4 LT. CUT OUT DAMAGED AREA, REMOVED CORROSION, INSTALLED DOUBLER REPAIR FROM STATION 810 TO 930 STRINGER 4 LT AS PER UPS EO B727-5330-0509 AND B727 SRM 53-30-3 FIG 5.

Part: SKIN — DEBONDED (RUDDER)

INSPECTION TYPE:C, LOWER RUDDER, RT SIDE, CORNER OF SKIN PANEL DEBONDED WITH CORROSION. INSTALLED FIBERGLASS REPAIR OVERLAY AT LOWER RUDDER RT SIDE SD PER B727 SRM 51-40-8.

Part: LINKAGE — CRACKED (NR 4 LE FLAP)

INSPECTION TYPE:N/A, NR 4 L/E FLAP O/B BULL-NOSE LINKAGE WHERE IT ATTACHES TO WING CRAC KED AND CORRODED. INSTALLED NEW LUG AT NR 4 KRUEGER FLAP BULLNOSE LINKAGE WITH REF TO SRM 51- 30-2. CHECKS GOOD.

Part: LINKAGE — CRACKED (NR 5 LE FLAP)

INSPECTION TYPE:N/A, NR 5 LEADING EDGE I/B FLAP BULL-NOSE LINKAGE WHERE IT ATTACHES TO THE WING CRACKED AND CORRODED. INSTALLED NEW LUG AT NR 5 KRUEGER FLAP BULLNOSE LINKAGE WITH REF TO SRM 51- 30-2. CHECKS GOOD.

Part: LIGHT — MALFUNCTIONED (CABIN)

EMERGENCY EXIT LIGHT IN COCKPIT DOES NOT COME ON OR IS VERY DIM WHEN EMERGENCY EXIT LIGHT SWITCH SET TO ON. HOWEVER, WHEN SWITCH BEHIND EXIT LIGHT PLASTIC PANEL IS SET TO ON, LIGHT COMES ON BRIGHT. REMOVED AND REPLACED PORTABLE EMERGENCY EXIT LIGHT ASSY PER MM 33-5 0-01. OPS GOOD.

Part: BULB — FAILED (COCKPIT)

INSPECTION TYPE-N/A, EMER EXIT LIGHTS UNARMED LIGHT DOES NOT PRESS TO TEST OR ILLUMINATE AT ALL. CHANGE BULB, NO HELP. ARMED/UNARMED LIGHT, RELAMPED WITH A 1864 BULB AND OPS CHECKED SERVICEABLE.

Part: BULB — FAILED (CABIN)

INSPECTION TYPE-N/A, EMER EXIT LIGHTS UNARMED LIGHT DOES NOT PRESS TO TEST OR ILLUMINATE AT ALL. ARMED/UNARMED LIGHT RELAMPED WITH A 1684 BULB AND OPS CHECKED SERVICEABLE.

Part: BATTERY — DISCHARGED (CABIN)

ENTRY DOOR EMER EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY, OPS CHECK OK.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE-N/A, BOTH EMERGENCY LIGHTS OUT AT COCKPIT DOOR AND L1 DOOR. REMOVED AND REPLACED BATTERY PACK FOR COCKPIT DOOR AND L1 DOOR, OPS CHECK GOOD.

Part: HYD CHECK VLV — MALFUNCTIONED (APU COMPT)

INSPECTION TYPE:N/A, HEAVY SMOKE IN COCKPIT SHORTLY AFTER TAKEOFF, BEFORE GEAR RETRACTION. ALL A/C PACK INDICATIONS NORMAL. AIR TURNBACK TO JAX. *S/D* FOUND SMOKE FUMES TO BE SYDROL. FOUND LOOSE FITTING DRIPPING ONTO PACK (L), TIGHTENED FITTING, RUN ENGS, FUMES STILL PRESENT. REMOVED AND REPLACED 3 CHK VALVES AND PRESS REGULATOR IN HYD RES PRESS SYS.

Part: LIGHT — INOPERATIVE (COCKPIT)

EMERGENCY EXIT LIGHT OVER CREW ENTRANCE DOOR DOES NOT TEST. INSTALLED NEW BATTERIES, SYS OPS NORMAL.

Part: INTERCOSTAL — CRACKED (BS 303.5)

INSPECTION TYPE-C, INTERCOSTAL AT STR 10L STA 303.5 IS CRACKED APPOX 1.5 INCH LENTH. FABRICATED, AND INSTALLED REPLACEMENT ANGLE PER DWG 65-17684 AND SRM 51-30-2.

Part: ANGLE — CRACKED (NR 3 LE SLAT)

INSPECTION TYPE-C, NR 3 SLAT INBD TRACK INBD VERTICAL SUPPORT ANGLE IS CRACKED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT ANGLE IAW SRM 51-30-2, 51-10-1.

Part: ANGLE — CRACKED (BS 1345)

INSPECTION C-CHECK, RT SKIN SUPPORT ANGLE IS CRACKED FS 1345. CUT OUT DAMAGED AREA FROM STA 1342 TO 1365. FABRICATED ANGLE AND DOUBLER AND INSTALLED IAW SRM 51-40-3 AND 51-30-2.

Part: ANGLES — CRACKED (NR 6 LE FLAP)

INSPECTION TYPE-C, RT WING NR 6 SLAT I/B TRACK BOTH I/B AND O/B VERT MOUNT ANGLE STIFFENERS ARE CRACKED AT LWR END. REMOVED, FABRICATED AND INSTALLED ANGLES IAW SRM 57-10-2, 51-30-2.

Part: ANGLE — CRACKED (NR 5 LE FLAP)

INSPECTION TYPE-C, RT WING L/E NR 5 K-FLAP ACTUATOR I/B SUPPORT ANGLE IS CRACKED AT UPPER AND LWR ENDS. FABRICATED AND INSTALLED REPLACEMENT ANGLE IAW SRM 51-10-1 AND 51-30-2.

Part: BULKHEAD FORGING — CORRODED (BS 870)

INSPECTION TYPE-C, BS 870 BULKHEAD FORGING IS CORRODED BEYOND LIMITS. REMOVED CORRODED FLANGE, FABRICATED AND INSTALLED REPAIR PARTS PER SRM 53-10-9 FIG 6.

Part: STRINGER — CORRODED (BS 304-312)

INSPECTION TYPE-C, STR 20R AT STA 304 TO 312 EXFOLIATED CORROSION OUT OF LIMITS. CUT OUT DAMAGED STR STA 304 TO 312, FABRICATED AND INSTALLED STRINGER REPAIR PER SRM 53-10-3, 51-30-2.

Part: INTERCOSTAL — CORRODED (BS 312)

INSPECTION TYPE-C, CORROSION FOUND TO BE OUT OF LIMITS ON INTERCOSTAL ATTACHED TO STRINGER AT FS 312 STR 18 APPROX 12 INCHES BELOW FLOORBEAM. REF N/R 490324 REMOVED, FABRICATED AND INSTALLED INTERCOSTAL PER BOEING DWG 69-22183 AND SRM 51-10-2, 51-30-2.

Part: SKIN — CRACKED (BS 1060)

INSPECTION TYPE-C, A .5625 INCH CRACK IN EXTERIOR SKIN AT LOWER AFT CARGO DOOR CUT OUT UPPER FWD CORNER, TERMINATES AT FASTENER HOLE. REPAIRED IAW DHC SK-954-616 REV A REF ENRG FILE NR B727-53-1850.

Part: WINDOW FRAME — CRACKED (BS 740)

INSPECTION TYPE-C, CRACK AT RT WINDOW FORGING INNER SURFACE AT BS 740 AND 760 FWD FRAME. REMOVED AND REPLACED WINDOW FRAME FORGING PER SRM 51-30-2 AND DWG 65-19581.

Part: WEB — CRACKED (RT MLG WW)

INSPECTION TYPE-C, RT MLG WW UPPER PRESSURE WEB CRACKED AT AFT O/B CORNER AT APPROX RBL 70. FABRICATED AND INSTALLED REPAIR IAW DHC SK-954-586 REF UPS ENRG FILE NR B727-53-1849.

Part: SEAT TRACK — CORRODED (BS 760-850)

INSPECTION TYPE-C, SEAT TRACK BS 760 TO 850 IS SEVERELY CORRODED. REMOVED AND REPLACED SEAT TRACK PER SRM 51-30-2 AND 51-10-1.

Part: ANGLE — CRACKED (BS 1342)

INSPECTION C-CHECK, LT SKIN SUPPORT ANGLE IS CRACKED FS 1345. REMOVED DAMAGED ANGLE, FABRICATED REPLACEMENT ANGLE AND DOUBLER AND INSTALLED IAW SRM 51-40-3 AND 51-30-2.

Part: INTERCOSTAL — CRACKED (BS 1367)

INSPECTION C-CHECK, LT INTERCOSTAL IS CRACKED BS 1367 FIN STA 22.5. CUT OUT DAMAGED AREA, FABRICATED DOUBLER AND INSTALLED PER SRM 51-40-3 AND 51-30-02.

Part: TORQUE BOX — CORRODED (BS 1342)

INSPECTION TYPE: C. VERTICAL FIN TORQUE BOX RT HORIZONTAL CHORD BS 1342 FIN STA ZERO IS CORRODED BEYOND LIMITS. CUT OUT DAMAGED AREA, FABRICATED REPAIR PARTS, TREATED, PRIMED AND INSTALLED PER DHC SK-954-576 REF. ENRG FILE NR 727-55-0339.

Part: SKIN — GOUGED (BS 623)

INSPECTION C-CHECK, AT STA 623 LT LAP SPLICE STR 14L GOUGE FOUND TO BE OUT OF LIMITS. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED FILLER AND DOUBLER IAW DHC SK-954-569 REV I.R. REF. UPS ENRG. FILE NR B727-53-1848 AND SRM 53-30-3.

Part: SPAR — CORRODED (VERT STAB)

INSPECTION TYPE: C. LT VERTICAL FIN SPAR CHORD IS CORRODED BEYOND LIMITS FIN. STA. 22.5. CUT OUT DAMAGE AND REPAIRED IAW BOEING DWG. 65-68408 AND SRM 51-30-2.

Part: INTERSPAR SKIN — CORRODED (BS 1342)

INSPECTION TYPE: C B.S. 1342 LT INTERSPAR SKIN IS CORRODED BEYOND LIMITS AT TERMINAL FITTING. CUTOUT DAMAGE, FABRICATED REPAIR PART AND INSTALLED PER DHC SK 954-578 REF. ENGINEERING FILE NR 727-55-0340.

Part: SPAR CHORD — CORRODED (VERT STAB)

INSPECTION C-CHECK, RT VERTICAL FIN SPAR CHORD IS CORRODED BEYOND LIMITS AT FIN STA 22.5. CUT OUT DAMAGE ON CHORD AND REPAIRED IAW BOEING DWG 65-68408 AND SRM 51-30-2.

Part: INTERCOSTAL — CRACKED (VERT STAB)

INSPECTION C-CHECK, INTERCOSTAL IS CRACKED RT SIDE FIN STA 22.5 B.S.1367. CUT OUT DAMAGED AREA, FABRICATED DOUBLER AND INSTALLED IAW SRM 51-40-3 AND 51-30-02.

Part: SHEAR TIE — MIS LOCATED (BS 1303)

INSPECTION TYPE: C. SHEAR TIE BS 1303 BETWEEN STRS 13R AND 14R HAS FASTENER HOLES WITH IMPROPER PITCH AND SHORTED. REMOVED SHEAR TIE, FABRICATED AND INSTALLED PER SRM 53-10-2, 51-10-1, AND 51-10-2.

Part: FITTING — CORROSION (NR 5 LE FLAP)

INSPECTION TYPE-C, RT WING L/E NR 5 K-FLAP ACTUATOR HINGE SUPPORT CASTING HAS HEAVY CORROSION. REMOVED AND REPLACED HINGE FITTING (P/N 65-18532-8) PER DWG NR 65-18532 AND SRM 51-30-2 AND DWG NR 65-16269.

Part: CHANNEL — CRACKED (CARGO DOORWAY)

INSPECTION TYPE-C, FWD LWR CARGO DOOR FRAME IS CRACKED AT AFT HINGE ARM FWD OF UPPER AFT STOP. REMOVED AND REPLACED CHANNEL (P/N 65-18620-7) PER SRM 51-30-2.

Part: CHORD — WORN (NR 2 ENGINE)

INSPECTION TYPE: C. NR 2 ENGINE RING CHORD IS SEVERLY WORN AND CHAFED. REMOVED NR 2 ENGINE'S OLD CHORD AND INSTALLED A NEW CHORD PER SRM 51-30-2.

Part: FRAME — RUSTED (BS 1342)

INSPECTION TYPE: C B.S. 1342 RT HD FRAME CHORD RBL 20 P/N 69-15405 IS SEVERELY RUSTED. REMOVED AND REPLACED CHORD IAW UPS E.O. B727-5530-4601-B.

Part: FRAME — RUSTED (BS 1342)

INSPECTION TYPE: C. B.S. 1342 RT HD LOWER FRAME CHORD RBL 24 P/N 65-17508-6 IS SEVERELY RUSTED. REMOVED AND REPLACED LOWER FRAME CHORD IAW UPS EO B727-5530-4601-B.

Part: CHORD — RUSTED (BS 1342)

INSPECTION TYPE: C. B/S 1342 RT HD OUTBOARD CHORD RBL 30 WL 250 P/N 19532-2 IS SEVERELY RUSTED. REMOVED AND REPLACED OUTBOARD CHORD IAW UPS EO B727-5530-4601-B.

Part: CHANNEL — RUSTED (BS 1342)

INSPECTION TYPE: C. B.S. 1342 LT SIDE AT LBL 18 WL 247 CHANNEL P/N 65-22551-1 IS SEVERELY RUSTED. REMOVED AND REPLACED CHANNEL WITH P/N 65-93155-567 IAW UPS E.O. B727-5530-4601-B, AND SRM 51-10-1, AND 51-30-2.

Part: FRAME — RUSTED (BS 1342)

INSPECTION TYPE: C. BS 1342 LT LOWER FRAME CHORD AT LBL 24 P/N 65-17508-5 IS SEVERELY RUSTED. REMOVED AND REPLACED FRAME CHORD WITH P/N 65-17508-223 IAW SRM 51-10-1, 51-30-2, AND UPS E.O. B727-5530-4601-B.

Part: CHANNEL — RUSTED (BS 1342)

INSPECTION TYPE: C. BS 1342 AFT CENTER CHANNEL W.L. 250 P/N 65-22551-7 IS SEVERELY RUSTED. REMOVED AND REPLACED CHANNEL IAW SRM 51-10-1, 51-30-2, AND UPS E.O. B727-5530-4601-B.

Part: CHANNEL — RUSTED (BS 1342)

BS 1342 RT HD CHANNEL RBL 18 WL 247, P/N 65-22551-2, IS SEVERELY RUSTED. REMOVED AND REPLACED CHANNEL WITH P/N 65-93155-67 IAW SRM 51-30-2, AND UPS EO B727-5530-4601-B.

Part: LIGHT — INOPERATIVE (COCKPIT)

INSPECTION TYPE-N/A, EMERGENCY LIGHTS INOP IN COCKPIT. REPLACED LIGHT ASSY PER 33-50-00, OPS CK NORMAL.

Part: OVERHEAT DETECT — DEFECTIVE (NR 1 ENGINE)

INSPECTION TYPE NA, NR 1 ENG FIRE DETECTION GROUND FAULT LIGHT STEADY IN FLIGHT, FIRE WARNING BELL SOUNDED. GROUND FAULT WAS EXTINGUISHED. REMOVED AND REPLACED NR 1 ENG FIRE OVERHEAT DETECTOR, OPS CHK GOOD PER M/M 26-11-00.

Part: BEARING — FAILED (TE FLAPS)

INSPECTION TYPE: DURING FLAP EXT FROM 5 DEG TO 15 DEG, ONLY O/B T/E FLAPS INDICATED 15 DEG, I/B FLAPS SHOWED 5 DEG. ATTEMPTED AGAIN WITH NO CHANGE. DECLARED AN EMERGENCY AND LANDED UNEVENTFUL AT SDF. FOUND RT ELEPHANT EAR LOCKED UP, PARTIALLY REMOVED SAME. REPLACED ELEPHANT EAR FWD BEARING.

Part: UPPER CHORD — CORROSION (WS 870)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON 870 UPPER CHORD, LBL 35 AND RBL 25 WL 190. REMOVED AND REPLACED IAW EO B727-5710-7412A.

Part: BRACKET — CRACKED (BS 344)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND BROKEN CHANNEL SUPPORT BRACKET, STA 344 RBL 53 WL 207, UNDER HAT CHANNEL. REMOVED AND REPLACED CRACKED HAT CHANNEL SUPPORT BRACKET PER SRM 51-30-2, 51-20-1, 51-10-02 AND 51-20-04.

Part: TE WEDGE — CORRODED (RT AILERON)

WHILE IN FOR C CHECK MAINTENANCE FOUND RT WING OUTBOARD AILERON TRAILING EDGE WEDGE HAS WATER CONTAMINATION, IS CORRODED AND HAS A PREVIOUS REPAIR IS DELAMINATED. REMOVED AND INSTALLED NEW WEDGE IAW SRM 51-80-1, 51-80-4, 51-80-6 MM 27-10-41 ANS SRM 51-30-2.

Part: SPAR CHORD — CORROSION (WS 228)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON RT LOWER BEAM SPAR CHORD HORIZONTAL FLANGE AT WING STA 228. REMOVED CORROSION AND FOUND OT OF LIMITS. CUT OUT DAMAGE AREA OF SPAR CHORD AND SHEAR TIE, FABRICATED REPAIRS AND INSTALLED PER SRM 51-30-10, 51-30-2, E.O. B727-5710-7434-A.

Part: HINGE FITTING — CORRODED (NR 9 SPOILER)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND NR 9 SPOILER SUPPORT FITTING IS CORRODED. REMOVED AND INSTALLED NEW FITTING WORK DONE IAW SRM 51-30-2 AND MM 27-51-131 AND MM 27-62-91.

Part: TRUNNION FITTING — CORRODED (NLG)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND, AFTER REMOVING NOSE LANDING GEAR ON CARD 364793, BOTH RT AND LT NOSE TRUNNION FITTINGS CORRODED BEYOND LIMITS. REMOVED AND INSTALLED NEW FITTINGS. WORK DONE IAW SRM 51-10-2, 51-10-6, 53-10-1, 51-20-1, 51-30-5, 51-30-5, MM 32-33-0 AND E.O. B727-5310-3954B.

Part: BULKHEAD — CRACKED (BS 1183)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND, WHILE WORKING FUSELAGE 13/CL2-115-01, A 3 INCH CRACK ON THE 1183 BULKHEAD, RBL 8, WL 181 - 2L 178. INSTALLED REPAIRS IAW E.O. B727-5311-0635B.

Part: SPAR CHORD — CORRODED (WS 180-184)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION (C57-581-03.00E-01) LT WING LOWER SPAR CHORD IS CORRODED AT WS 180 TO 184 IN HEEL OF CHORD. REMOVED CORROSION, FOUND TO BE BEYOND LIMITS, REPAIRED PER UPS E.O. B727-5710-7411-A.

Part: SKIN — CRACKED (WS 190-224.5)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND RT WING UPPER SKIN HAS CORROSION AND AN 8 INCH CRACK FROM RWS 190 TO 224.5 AT AFT SPAR. CUTOUT DAMAGED SKIN, FABRICATED, INSTALLED REPAIR DOUBLERS, PER UPS E.O. B727-5730-7416.

Part: SPAR CHORD — CORRODED (WS 130-224.5)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION (C57-581-03.00E-02) RT WING UPPER SPAR CHORD IS CORRODED FROM WS 130 TO 224.5 AND GOING UNDER TRUNNION FITTING. REMOVED AND REPAIRED RT WING SPAR CHORD IAW UPS E.O. B727-5710-7410-A.

Part: RIB — CRACKED (NR 1 ELEVATOR)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND LT NR 1 ELEVATOR HINGE SUPPORT RIB CRACKED IN THREE PLACES ON UPPER CHORD. REMOVED AND INSTALLED NEW SUPPORT RIB. WORK DONE IAW SRM 51-30-2 MM 27-20-1, MM 27-30-05, MM 27-30-81, MM 27-30-61, MM 27-30-00.

Part: SPAR WEB — CORRODED (BS 870)

WHILE IN FOR C-CHECK, MAINTENANCE REMOVED CENTER CELL REAR SPAR WEB FOR ACCESS OF 870 TENSION STRAP. AFTER WEB REMOVAL, FOUND CORROSION ON WEB TO BE OUT OF LIMITS PER SRM 57-10-1. REPLACED BS 870 WEB PER SRM 51-30-2, 51-10-1, 51-10-2, 51-10-6, 51-30-5, 51-20-4 AND MM 51-20-151.

Part: STRINGER — CORROSION (WS 226-230)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON NR 1 STRINGER (LOWER) RWS 226-230, LOCATED ON TOP SIDE OF BOTTOM HORIZONTAL LEG OUT OF LIMITS. REMOVED AND REPLACED STRINGER PER E.O. 757-57-1641. UPON REMOVAL OF STRINGER, FOUND DAMGED SHEAR TIE AND ANGLE. REMOVED AND REPLACED SHEAR TIE AND ANGLE IAW SRM 51-30-2.

Part: SLAT — CORROSION (NR 5 LE FLAP)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND NR 5 K-FLAP ATTACH LUGS ARE CORRODED AT LUG MOUNT BOLTS OUT OF LIMITS. REMOVED AND REPLACED NR 5 K-FLAP PER MM 27-81-1 AND MM 27-81-00.

Part: CHORD — CORROSION (BS 870)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION (SSID W-1A) ON EXTERIOR OF LOWER CHORD AT BS 870 RBL 41. WHILE REMOVING WEB, FOUND CORROSION ON LOWER SIDE OF CHORD BEYOND LIMITS. REPLACED LOWER CHORD. WORK DONE IAW E.O. B727-5710-7413-A.

Part: CHORD — CORROSION (BS 740)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON LOWER CHORD BS 740 LBL 10 TO LBL 13 WL 165. REMOVED AND REPLACED BS 740 LOWER CHORD PER UPS E.O. B727-5710-7431 AND SRM 51-30-2, 51-20-4.

Part: SKIN — CORRODED (BS 870)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND, WHILE ACCESSING 870 PRESSURE SEAL RETAINER, CORROSION UPPER SIDE OF TOP SKIN STA 870, LBL 45-65, WL 190. REMOVED CORROSION, REPAIRED SKIN PER USP E.O. 727-57-1648.

Part: LOAD BEAM — CORRODED (BS 740)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON SIDE LOAD BEAM STA 740, RBL 40 TO LBL 40, WL 170. REMOVED BEAM CHORD AND REPLACED WITH NEW CHORD IAW 727 SRM 51-10-2, 51-10-6, 51-30-2.

Part: BRACKET — CORRODED (BS 740)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON DELTA BEAM FORWARD ATTACH ANGLE BS 740 LBL 6 TO RBL 6, WL 155. REMOVED ANGLE, FABRICATED NEW ANGLE AND INSTALLED IAW 727 SRM 51-10-01, 51-10-2, 53-10-1, 51-30-2.

Part: UPPER SKIN — CORRODED (BS 868-870)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON THE THE BOTTOM SIDE OF UPPER SKIN AT STATION 868 TO 870, RBL 63 LBL 63. MAINTENANCE COMPLIED WITH UPS EO 727-57-1648.

Part: SKIN — CORRODED (BS 870)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON THE ON THE UPPER SIDE OF THE TOP SKIN AT STATION 870, RBL 45 TO 65 WL 190. MAINTENANCE BLENDED OUT THE CORROSION, FLAP PEENED AREA IAW OHM, TREATED AND INSTALLED REPAIR STRAP IAW UPS EO 727-57-1648.

Part: FRAME — CRACKED (FWD ENTRY DOOR)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND A CRACK IN THE FORWARD FRAME ON THE FORWARD ENTRY DOOR AT THE LOWER FORWARD CORNER. MAINTENANCE REMOVED AND REPLACED THE FORWARD ENTRY DOOR FORWARD FRAME PER SRM 51-10-1 AND 51-20-1.

Part: GATE BEAM — CRACKED (FWD ENTRY DOOR)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND A CRACK IN THE FORWARD ENTRY DOOR UPPER GATE BEAM IN THE OUTBOARD RADIUS. MAINTENANCE REMOVED AND REPLACED THE FORWARD ENTRY DOOR UPPER GATE BEAM PER SRM 51-10-2, 51-30-2, 51-20-4, 51-10-1, 51-20-1 AND MM 51-20-151.

Part: FRAME — CRACKED (FWD ENTRY DOOR)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND A CRACK IN THE FORWARD ENTRY DOOR AFT FRAME AT THE LOWER AFT CORNER. MAINTENANCE REMOVED AND REPLACED THE FORWARD ENTRY DOOR AFT FRAME PER SRM 51-10-2, 51-30-2, 51-20-4, 51-10-1 AND 51-20-1.

Part: FITTING — CORRODED (RT AILERON)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON THE RIGHT WING OUTBOARD AILERON, OUTBOARD CENTER BEARING SUPPORT FITTING ON THE AILERON. MAINTENANCE REMOVED AND INSTALLED NEW FITTING IAW SRM 51-30-2.

Part: SEAL DEPRESSOR — CRACKED (FWD ENTRY DOOR)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND A CRACK IN THE FORWARD ENTRY DOORWAY SEAL DEPRESSOR BELOW LOWER HINGE CUTOUT. MAINTENANCE REMOVED THE OLD SEAL DEPRESSOR, FABRICATED NEW SEAL DEPRESSOR AND INSTALLED PER SRM 51-10-2, 51-10-1 AND 51-30-2.

Part: BOLTS — SHEARED (NR 3 FLAP TRACK)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND THE NR 3 FLAP TRACK SPOILER BEAM BOLTS WERE SHEARED. MAINTENANCE REMOVED AND INSTALLED NEW BOLTS, FABRICATED NEW SHIM AND INSTALLED. ALL WORK DONE IAW MM 27-51-31-AND 51-30-2.

Part: FITTING — CORRODED (RT AILERON)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON THE RIGHT WING OUTBOARD AILERON, OUTBOARD BEARING SUPPORT FITTING ON THE AILERON. MAINTENANCE REMOVED AND INSTALLED A NEW FITTING IAW SRM 51-10-1 AND 51-30-2.

Part: GATE — CORRODED (FWD ENTRY DOOR)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION IN THE FORWARD ENTRY DOOR LOWER GATE AT CENTER ROD ATTACHING POINT. MAINTENANCE REMOVED AND REPLACED THE FWD ENTRY DOOR LOWER GATE PER SRM 51-10-2, 51-30-2, 51-20-4, 51-10-1 AND 51-20-1 AND MM 51-20-151.

Part: SKIN — DELAMINATED (LT TE FOREFLAP)

WHILE IN C-CHECK, MAINTENANCE FOUND DELAMINATION ON THE UPPER SURFACE AND LOWER SURFACE OF THE LEFT WING INBOARD FORE FLAP. MAINTENANCE REPAIRED THE UPPER AND LOWER SURFACES OF THE LEFT WING INBOARD FORE FLAP IAW SRM 51-40-6.

Part: GATE BEAM — CRACKED (PAX DOOR)

WHILE IN C-CHECK, MAINTENANCE FOUND A CRACK IN THE FORWARD ENTRY DOOR LOWER GATE BEAM AT THE LOWER AFT CORNER. MAINTENANCE REMOVED AND REPLACED THE CRACKED LOWER GATE BEAM AND SECURED WITH FASTENERS IAW SRM 51-30-2 AND SRM 51-10-1.

Part: ANGLE — CRACKED (NR 3 SKATE)

WHILE IN C-CHECK, MAINTENANCE FOUND A CRACK IN THE NR 3 SKATE ANGLE IN 2 PLACES ON INBOARD SIDE. MAINTENANCE STOP DRILLED THE CRACK NDI VERIFIED AND INSTALLED DOUBLER IAW SRM 51-40-2.

Part: CHORD — CORRODED (BS 294.5)

WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON THE LEFT MID-CHORD AT STATION 294.5 - 312, LBL 15 AND WL 170. MAINTENANCE REMOVED CORROSION BEYOND LIMITS, REMOVED AND REPLACED THE CHORD, FINAL INSTALLATION PER SRM 51-30-2, 53-10-1 AND 56-40-00.

Part: DOUBLER — CORRODED (BS 875)

WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON THE ACCESS PANEL DOUBLER AT STATION 875, LBL 55 AND WL 165. MAINTENANCE REMOVED THE CORRODED DOUBLER, FABRICATED A NEW DOUBLER, AND INSTALLED PER SRM 51-10-2, 51-30-5 AND 51-30-2.

Part: TE WEDGE — DELAMINATED (RT TE MIDFLAP)

WHILE IN C-CHECK, MAINTENANCE FOUND DELAMINATION ON THE LOWER SKIN ON THE RIGHT WING OUTBOARD MID-FLAP TRAILING EDGE WEDGE. MAINTENANCE REMOVED THE DAMAGED AREA, CLEANED AND REPAIRED AREA PER SRM 51-40-6.

Part: TE WEDGE — DELAMINATED (LT TE MIDFLAP)

WHILE IN C-CHECK, MAINTENANCE FOUND DELAMINATION ON THE UPPER SURFACE OF THE LEFT WING OUTBOARD MID-FLAP TRAILING EDGE WEDGE. MAINTENANCE REPAIRED THE LEFT WING OUTBOARD MID-FLAP TRAILING EDGE WEDGE IAW SRM 51-40-6.

Part: SKIN — DELAMINATED (NR 5 SPOILER)

WHILE IN C-CHECK, MAINTENANCE FOUND DELAMINATION ON THE NR 5 SPOILER AT THE FORWARD OUTBOARD CORNER ON BOTH UPPER AND LOWER SKINS. MAINTENANCE REPLACED SPOILER IAW UPS NRC 364863.

Part: FITTING — PITTED (BS 870)

WHILE IN C-CHECK, MAINTENANCE FOUND THE AILERON PCU MOUNT FITTING PITTED AT THE ATTACH POINTS AND CONTROL LINKAGES. MAINTENANCE REMOVED THE DAMAGED FITTING, INSTALLED NEW FITTING ONTO AIRCRAFT AND INSTALLED CABLES AND TORQUE TUBES PER MM 27-10-91.

Part: TE WEDGE — DELAMINATED (RT TE MIDFLAP)

WHILE IN C-CHECK, MAINTENANCE FOUND DELAMINATION ON THE UPPER SURFACE AND LOWER SURFACE OF THE RIGHT WING INBOARD MID-FLAP TRAILING EDGE WEDGE. MAINTENANCE REPAIRED THE RIGHT WING INBOARD MID-FLAP TRAILING EDGE WEDGE IAW SRM 51-40-6.

Part: TE WEDGE — DELAMINATED (RT TE FORE FLAP)

WHILE IN C-CHECK, MAINTENANCE FOUND DELAMINATION ON THE LOWER SURFACE OF THE RIGHT WING OUTBOARD FORE FLAP. MAINTENANCE REMOVED THE CORROSION AND TRAILING EDGE WEDGE, REPAIRED THE CORE AND INSTALLED NEW WEDGE PER SRM 51-40-6.

Part: TE WEDGE — DELAMINATED (LT TE MIDFLAP)

WHILE IN C-CHECK, MAINTENANCE FOUND DELAMINATION ON THE UPPER SURFACE AND LOWER SURFACE OF THE LEFT WING INBOARD MID-FLAP TRAILING EDGE WEDGE. MAINTENANCE REMOVED THE DAMAGED SKIN ON THE UPPER AND LOWER SKINS, FINAL REPAIRS PER SRM 51-40-6.

Part: SKIN — DELAMINATED (LT TE FLAP)

WHILE ON GROUND MAINTENANCE FOUND DELAMINATION OF LT I/B T/E FLAP. REPAIRED IAW EO B727-5750-3081.