N924UP

Part: ROD — BROKEN (SPOILER) · airframe 49,127 hrs · 36,220 cycles

INSPECTION TYPE:PRD INBOARD SPOILER CASTING SUPPORT ROD BROKEN LT WING. INBOARD SPOILER LT WING CASTING SUPPORT ROD REPLACED.

Part: LIGHT — INOPERATIVE (CABIN)

INSPECTION TYPE:N/A, EMERGENCY EXIT LIGHT CAME ON IN FLIGHT INTERMITTENTLY. EMERGENCY LIGHT REPLACED PER MM 33-50, CHECKED OK.

Part: STRUCTURE — CRACKED (CARGO DOOR) · airframe 48,339 hrs · 35,505 cycles

INSPECTION TYPE:C&SI, SEVERAL CRACKS IN FWD CARGO DOOR. FWD CARGO DOOR REPLACED IAW MM 2-31-01.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 48,339 hrs · 35,505 cycles

INSPECTION TYPE:C&SI, FOLLOWING REWORK AT BS 1183 STR 15R TO 5R HOLES AT 10R HAVE EXCEEDED LIMITS AFTER CORROSION REMOVAL. REPAIR CARRIED OUT IAW SMRO EO 2000-026-006 & 2000-026-011 UPS ENGINEERING FILE NR 727-53-2269 & 727-53-2274.

Part: FITTING — CORRODED (FUSELAGE) · airframe 48,339 hrs · 35,505 cycles

INSPECTION TYPE:C+SI, AFTER REWORK OF BS 360 ON SMRO EO2000-026-001, TWO HOLES AT STR END FITTING 3L ARE REAMED UP TO MAX LIMITS AND STILL SHOW EVIDENCE OF CORROSION INSIDE SURFACE OF HOLES. HOLES REWORKED IAW SHANNON MROEO2000-026-010.UPS FILE NR 727-53-2273.

Part: ANGLE — CRACKED (CARGO DOOR) · airframe 48,339 hrs · 35,505 cycles

INSPECTION TYPE:C&SI, FWD CARGO DOOR BS 577 AFT ANGLE CRACKED AT HINGE ATTACHMENT FWD CARGO DOOR REPLACED REF NRC 175922 FOR REPLACEMENT.

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,339 hrs · 35,505 cycles

INSPECTION TYPE:C&SI, AFT CARGO DOOR HAS SUSPECT CRACKED FRAME AT STA 1072 BETWEEN NR 5 ST OPS. REMOVED AND REPLACED FRAME IAW SRM 53-30-2.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 48,339 hrs · 35,505 cycles

INSPECTION TYPE:C&SI, G-NET ATTACH POINT AT BS 365 BETWEEN STR 15L AND 16L HAS CRACKED ANGLE. INSTALLED NEW ANGLE AND CLIPS IAW SRM 51-30-02.

Part: BOLT — CRACKED (NR 2 ENGINE) · airframe 48,339 hrs · 35,505 cycles

INSPECTION TYPE:C&SI, ENGINE NR 2 CROSS STRUT AFT ATTACH BOLT FOUND CRACKED DURING NDI CHECK. BOLT REPLACED IAW MM 71-21-12.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 48,339 hrs · 35,505 cycles

INSPECTION TYPE:C&SI, SUSPECT CRACK TO HORIZ STIFFENER SUPPORT BRACKET AT BS 1183 RT AFT ENTRY UPPER DOOR CUTOUT. REPAIR CARRIED OUT IAW SRM 51-30-2.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 48,339 hrs · 35,505 cycles

INSPECTION TYPE:C&SI, FIRE WIRE BRACKET CRACKED AT BS 1010 LBL 45.5 LWR SURFACE OF FLOOR I T CARGO BAY. REPAIRED IAW SRM 51-40-3 FIG 1.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 48,339 hrs · 35,505 cycles

INSPECTION TYPE:C+SI, CORROSION ON LATERIAL SUPPORT ANGLE BS 850 LBL 6 AT DELTA BEAM. CORROSION ON SUPPORT ANGLE OUT OF LIMITS. NEW ANGLE FABRICATED IAW SRM 51-20-1. FASTENERS REMOVED IAW SRM 51-30-2. CORROSION REMOVED IAW SRM 51-10-6. REINSPECTED FOUND WITHIN LIMITS IAW SRM 53-10-1 FIG 1. NEW ANGLE AND FASTENERS REINSTALLED IAW SRM 51-30-2.

Part: BRACKET — CRACKED (NR 1 ENGINE) · airframe 48,339 hrs · 35,505 cycles

INSPECTION TYPE:C&SI, ENGINE NR 1 THRUST REVERSER O/B FAIRING MID SUPPORT BRACKET CRACKED. BRACKET REPLACED IAW MM 78-30-00.

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,339 hrs · 35,505 cycles

INSPECTION TYPE:C&SI, 2 SUSPECT CRACKS ON FRAME BS 277 ON RT SIDE OF CONTROL CABIN AT STR 15 AND 16. FRAME REPAIRED IAW SRM 51-40-2 FIG 1.

Part: HINGE — CORRODED (ELEVATOR) · airframe 48,339 hrs · 35,505 cycles

INSPECTION TYPE:C&SI, NR 5 BALANCE BAY HINGE HALF RT SIDE CORRODED BEYOND LIMITS (AFT HINGE HALF). REPLACED HINGE HALF AND HARDWARE IAW MM 27-30-21.

Part: STIFFENER — CORRODED (COCKPIT) · airframe 48,339 hrs · 35,505 cycles

INSPECTION TYPE:C&SI, CONTROL CABIN, HORIZ STIFFENER ON BS 251.6 IS CORRODED ON LT SIDE AT WL 220 APPROX. BRACKET REPLACED IAW SRM 51-20-01 & SRM 51-30-02.

Part: BEAM — CORRODED (FUSELAGE) · airframe 48,339 hrs · 35,505 cycles

INSPECTION TYPE:C&SI, FWD CARGO BAY CORROSION ON I BEAM LWR CHORD LWR SURFACE AT BS 500 BL 0. REPAIR CARRIED OUT IAW SMRO EO 2000-026-008 UPS ENGINEERING FILE 727-53-2271.

Part: SKIN — CRACKED (THRUST REVERSER) · airframe 48,339 hrs · 35,505 cycles

INSPECTION TYPE:C&S,I ENGINE NR 1 THRUST REVERSER UPPER DOOR INNER RAMP SKIN CRACKED. NOTE: CRACK COMING OUT FROM UNDER PREVIOUS PATCH REPAIR. REPAIR CARRIED OUT IAW SRM 78-30-01 FIG 205.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 48,339 hrs · 35,505 cycles

INSPECTION TYPE:C&SI, STR 10R AT BS 1105 HAS CRACK DUE TO CORROSION. REPAIR CARRIED OUT IAW SRM 51-40-4 FIG 1.

Part: BRACKET — CRACKED (NR 3 ENGINE) · airframe 48,339 hrs · 35,505 cycles

INSPECTION TYPE:C&SI, ENGINE NR 3 THRUST REVERSER O/B FAIRING MID SUPPORT BRACKET CRACKED. BRACKET REPLACED IAW MM 78-30-00.

Part: LINK ROD — CRACKED (LT MLG) · airframe 48,339 hrs · 35,505 cycles

INSPECTION TYPE:C+SI, CRACKED LINK AT LT MLG LINKAGE TO AIR GROUND SENSE. AIR GROUND SENSER LINK REPLACED IAW MM 20-80-01. FUNCTION CHECKED IAW MM 32-31-11 PG 501, FOUND SATISFACTORY.

Part: MOUNT — CORRODED (ANTENNA) · airframe 48,339 hrs · 35,505 cycles

INSPECTION TYPE:C+SI, CORROSION ON LWR ANTENNA SUPPORT BS 820 AT CENTER LINE. CORROSION REMOVED IAW SRM 51-10-6. FOUND TO BE OUT OF LIMITS. CORRODED ANGLE SUPPORT REMOVED IAW SRM 51-30-2. NEW ANGLE SUPPORT FABRICATED IAW SRM 51-20-1. ANGLE SUPPORT RE-INSTALLED IAW SRM 51-30-2.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 48,339 hrs · 35,505 cycles

INSPECTION TYPE:C&SI, CORROSION ON STR 24R AT BS 460. REPAIR CARRIED OUT IAW SRM 53-10-1 AND SRM 53-10-3.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 48,339 hrs · 35,505 cycles

INSPECTION TYPE:C+SI, BS 328 FLOORBEAM HAS SURFACE CORROSION AROUND FASTENERS ON TOP CAP, LBL30. CORROSION REMOVED IAW MM SRM 51-10-06. AREA FOUND TO BE OUT OF LIMITS IAW MM SRM 53-10-1 FIG 5 MAX 0.020 INCH. REPAIR CARRIED OUT IAW MM 53-10-8 FIG 7.

Part: FLANGE — CORRODED (NR 3 FLAP TRACK) · airframe 48,339 hrs · 35,505 cycles

INSPECTION TYPE:C&SI, NR 3 FLAP TRACK AFT ATTACH FLANGE AND HOLES CORRODED. REPAIR CARRIED OUT IAW SMRO EO 2000-02-004 UPS ENGINEERING FILE NR 727-57-2172.

Part: CARRIAGE — CORRODED (TE FLAP) · airframe 48,339 hrs · 35,505 cycles

INSPECTION TYPE:C&SI, NR 2 FLAP CARRIAGE SPINDLE THREADS CORRODED I/B DEADWEIGHT ROLLER HOLE CORRODED. REPLACED IAW OHM 57-58-01.

Part: BEAM — CRACKED (NR 8 SPOILER) · airframe 48,339 hrs · 35,505 cycles

INSPECTION TYPE:C&SI, CRACK FOUND AT NR 8 SPOILER SUPPORT BEAM I/B OF I/B HINGE. REPAIR CARRIED OUT IAW SMRO EO 2000-026-002 UPS ENGINEERING FILE NR 727-57-2169.

Part: FLANGE — CORRODED (NR 3 FLAP TRACK) · airframe 48,339 hrs · 35,505 cycles

INSPECTION TYPE:C&SI, NR 3 FLAP TRACK FWD ATTACH FLANGE UPPER SURFACE CENTRE HOLE AND O/B HOLE CORRODED. REPAIR CARRIED OUT IAW SMRO EO 2000-026-004 UPS ENGINEERING FILE NR 727-57-2172.

Part: PRESSURE PANEL — CRACKED (NLG WW) · airframe 48,339 hrs · 35,505 cycles

INSPECTION TYPE:C&SI, SUSPECT CRACK AT NOSE WHEEL WELL SIDEWALL AT RBL 23 AND STA 267 APPROX. REPAIR CARRIED OUT IAW SRM 51-40-2 FIG 1.

Part: MOUNT — CORRODED (NR 1 ENGINE) · airframe 48,339 hrs · 35,505 cycles

INSPECTION TYPE:C&SI, ENGINE NR 1 FWD MOUNT HOLES CORROSION IN BOTH I/B HOLES AND AFT O/B HOLE. REPAIR CARRIED OUT IAW EO B727-5440-11592-A APPENDIX A.

Part: BOLT — CORRODED (FUSELAGE) · airframe 48,339 hrs · 35,505 cycles

INSPECTION TYPE:C+SI, BS1183 TENSION BOLTS CORRODED ABOVE STR 8R. REMOVED SUFFICIENT BOLTS TO VERIFY CONDITION OF SPLICE. BOLTS REMOVED FROM STR 5R - 15R BOLTS FOUND CORRODED, OK ABOVE 5R AND OK BELOW 15R. HOLES REWORKED PER SMROEO2000-026-006 AND BOLTS REPLACED PER TABLE 4 OF SMRO EO2000-026-006. UPS FILE NR 727-53-2269.

Part: BRACKET — CRACKED (NR 4 SPOILER) · airframe 48,339 hrs · 35,505 cycles

INSPECTION TYPE:C&SI, LT WING T/E SUPPORT BRACKET CRACKED DIRECTLY AFT OF NR 4 SPOILER PANEL I/B HINGE. BRACKET REPLACED IAW SRM 51-30-02.

Part: BRACKET — CRACKED (SPOILER PANEL) · airframe 48,339 hrs · 35,505 cycles

INSPECTION TYPE:C&SI, LT WING, T/E SUPPORT BRACKET CRACKED 6 INCHES O/B OF NR 5 SPOILER PANEL I/B HINGE. BRACKET REPLACED IAW SRM 51-20-01 & SRM 51-30-02.

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,339 hrs · 35,505 cycles

INSPECTION TYPE:C+SI, SUSPECT CRACK ON VERTICAL CHORD AT BS 178 BULKHEAD TO SKIN ATTACH POINT, WL 200 APPROX, LT SIDE. NDT REQUIRED TO CONFIRM. CRACK CONFIRMED. POST CUT OUT IAW B727-NDTM PT6 51-00-00 FIG 4. CRACK FOUND TO BE REMOVED. T-SUPPORT AT STR 17 BS 183 CUT IAW SRM 51-10-00. T- SUPPORT RE-INSTALLED AND REPAIRED AT BS 178 REPAIRED IAW SRM 51-40-4 FIG 2.

Part: CARRIAGE — CORRODED (TE FLAP TRACK) · airframe 48,339 hrs · 35,505 cycles

INSPECTION TYPE:C&SI, NR 1 FLAP CARRIAGE SPINDLE BORE CORRODED. REPLACED CARRIAGE IAW MM 27-51-13.

Part: SKIN — CORRODED (FUSELAGE) · airframe 48,339 hrs · 35,505 cycles

INSPECTION TYPE:C+SI, LIGHT SURFACE CORROSION ON SKIN BS 1140 BETWEEN S3R & 4R. REPAIRED AREA IAW SRM 53-30-3 & UPS EO B727-5330-0509 APPEX 8.3 WEIGHT OF REPAIR 5.2 LBS. NOTE THIS IS A CAT B REPAIR AND REPAIR CRITICAL ROW ZERO TIMED.

Part: CARRIAGE — CORRODED (TE FLAP TRACK) · airframe 48,339 hrs · 35,505 cycles

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

Part: SPLICE PLATE — CRACKED (FUSELAGE) · airframe 48,339 hrs · 35,505 cycles

INSPECTION TYPE:C&SI, ON REMOVAL OF BS 930 SPLICE PLATE AT STR 14 CRACK FOUND IN LWR END OF FUSELAGE UPPER FRAME. REPAIR CARRIED OUT ON FRAME IAW SRM 53-10-4 FIG 1.

Part: SKIN — CORRODED (FUSELAGE) · airframe 48,339 hrs · 35,505 cycles

INSPECTION TYPE:C&SI, SUSPECT COROSSION BETWEEN FUSELAGE SKIN AND INTERNAL DOUBLER BS 1090 ABOVE STR 14 RT. REPAIR CARRIED OUT IAW SRM 53-30-3 FIG 3.

Part: BUTT JOINT — CORRODED (FUSELAGE) · airframe 48,339 hrs · 35,505 cycles

INSPECTION TYPE:C&SI, EVIDENCE OF CORROSION AT BS 1080 BUTT JOINT AFT EDGE (VIEWED INTERNALLY) BETWEEN S5R AND 2R. REPAIR CARRIED OUT IAW EO B727-5330-1177.

Part: BUTT JOINT — CORRODED (FUSELAGE) · airframe 48,339 hrs · 35,505 cycles

INSPECTION TYPE:C&SI, EVIDENCE OF CORROSION BS 1080 BUTT JOINT AFT EDGE BETWEEN S4L AND 2L. REPAIR CARRIED OUT IAW EO B727-5330-1177.

Part: BATTERY PACK — DISCHARGED (CABIN)

EMERGENCY EXIT LIGHT OVER COCKPIT DOOR AND ENTRANCE DOOR, GOT NO LIGHT WHEN TESTED BY CREW PRIOR TO DEPARTURE. REMOVED AND REPLACED BATTERY PACK. BATTERY REQUIRED CHARGING PRIOR TO INSTALLATION.

Part: FRAME — CRACKED (BS 930)

INSPECTION TYPE:C, BS 930 FRAME CRACK ON HORIZONTAL LEG OF FRAME AT FLOOR LEVEL. REPAIR TO FRAME CARRIED OUT IAW SMRO EO 99-30-003 UPS ENGINEERING FILE NR 727-53-2174.

Part: BEAM — CRACKED (BS 940)

INSPECTION TYPE:C, DURING REMOVAL TO FACILITATE REPLACEMENT OF BS 940 FITTING, FLAP ROLLER TRACK SUPPORT FOUND CRACKED IN THREE PLACES. BEAM ASSY REPLACED IAW SRM 51-30-2 AND OHM 20-50-01.

Part: BRACKET — CRACKED (BS 440)

INSPECTION TYPE:C, FLOOR SUPPORT BRACKET CRACKED AT BS 440 RT IN E & E BAY. BRACKET REPAIRED IAW SRM 51-40-3 FIG 1 AND REPROTECTED IAW SRM 51-10 -2.

Part: ANGLE — CRACKED (BS 560)

INSPECTION TYPE:C, ANGLE CRACKED ON AFT SIDE OF FRAME BS 560 STR 17 L. ANGLE REPLACED IAW SRM 51-40-03 FIG 1 & SRM 53-10-02.

Part: FITTING — MISDRILLED (BS 940)

INSPECTION TYPE:C, ON REMOVAL OF BS 940 LT FITTING 2 FASTENER HOLES THROUGH S18A AND FUSELAGE SKIN FOUND TO HAVE BEEN OVERSIZED AND OUT OF ED (AFT UPPER AT TACH BOLTS OF 940). INVESTIGATED AND REPAIR CARRIED OUT IAW SMRO EO 99-30-001 UPS ENGINEERING FILE NR 727-53-2170.

Part: T-EDGE — LIGHTNING STRIKE (RT ELEVATOR)

INSPECTION TYPE:C, LIGHTNING DISCHARGE DAMAGE RT ELEVATOR TIP T-EDGE AT BASE LWR SURFACE & STRUCTURE AT PREVIOUS REPAIR. REPAIR CARRIED OUT IAW SRM 55-20-3 FIG 3.

Part: SKIN — CRACKED (BS 203)

INSPECTION TYPE:C, CRACK ON SKIN BS 203 WL 219 RT. REPAIRED IAW SRM 53-30-3 FIG 3.

Part: SKIN — CRACKED (BS 251.6)

INSPECTION TYPE:C, CRACK IN SKIN BS 251.6 AT WL 215.5 RT SIDE. REPAIRED IAW SRM 53-30-3 FIG 3.

Part: SKIN — DENTED (RT TE FOREFLAP)

INSPECTION TYPE:C, DENT ON UPPER SURFACE OF RT O/B FORE FLAP UPPER SURFACE MID SPAN. REPAIRED IAW SRM 51-40-6 FIG 35.

Part: SKIN — DENTED (RT TE FOREFLAP)

INSPECTION TYPE:C DENT ON UPPER SURFACE OF RT O/B FORE FLAP UPPER SURFACE MID-SPAN. REPAIRED IAW SRM 51-40-6 FIG 35.

Part: BRACKET — CRACKED (TE MID FLAP)

INSPECTION TYPE:C ON INSP BRACKET FOUND CRACKED ON NR 1 FLAP TRACK MID FLAP FAIRING. REMOVED FAIRING TRACK FOR ACCESS IAW SRM 51-30-2. REMOVED CRACKED BRACKET IAW SRM 51-30-02. INSTALLED BRACKET IAW SRM 51-30-02. INSTALLED FLAP TRACK IAW SRM 51-30-02.

Part: FRAME — CRACKED (BS 783.95)

INSPECTION TYPE:C, DURING INSPECTION OF 783.95 L FRAME FOR CRACKS. CRACK FOUND EMINATING FROM SECOND FASTENER HOLE BELOW FLOOR. FRAME BS 783.95 LT REPAIRED IAW APPENDIX C OF EO B727-5310-5474- C AND SMRO EO 99-30-002 UPS ENGINEERING FILE NR 5310-2172.

Part: ANGLE — CORRODED (BS 950)

INSPECTION TYPE:C, SEPARATION DETECTED ON BS 950 FITTING BY NDT INSPECTION BETWEEN S 9 & S10 DOWNWARD. SPLICE ANGLE FOUND CORRODED NEW ANGLE FABRICATED IAW SRM 51-20-1.

Part: TRACK — CRACKED (TE FLAPS)

INSPECTION TYPE:C, NR 6 FLAP TRACK MID FAIRING O/B ROLLER TRACK CRACKED. TRACK REPLACED IAW SRM 51-30-2 AND DRG 65-21796.

Part: SKIN — NICKED (LT MLG DOOR)

INSPECTION TYPE:C LT LANDING GEAR DOOR OUTER SECTION HAS NICK ON OUTER SKIN -30 APPROX FROM FWD END. DAMAGED AREA CUT OUT AND REPAIR CARRIED OUT IAW SRM 52-80-02.

Part: FRAME — CRACKED (BS 825.95)

INSPECTION TYPE:C DURING INSPECTION OF BS 825.95 L FRAME A CRACK WAS FOUND EMINATING FROM 3RD FASTENER HOLE ABOVE FLOOR FRAME BS 825.95 LT. REPAIRED IAW APPENDIX C OF EO B727-5310-5474- C & SMRO EO 99-30-002 UPS ENGINEERING FILE NR 5310-2172.

Part: SKIN — DENTED (LT ELEV TAB)

INSPECTION TYPE:C SMALL DENT ON LWR SKIN OF LT ELEV TAB AT OUTBOARD END. REPAIRED IAW SRM 51-40-6 FIG 39.

Part: WEB — CRACKED (BS 1306)

INSPECTION TYPE:C, CRACK ON WEB AT RT SIDE OF AIRSTAIRS AT STA BS 1306 UPPER LIGHTENING HOLE. CRACK STOP DRILLED IAW SRM CH 51-10-2 AREA REPAIRED IAW SRM 51-40-2.

Part: WEB — CRACKED (BS 1306)

INSPECTION TYPE:C CRACK ON WEB AT LT SIDE OF AIRSTAIRS AT STA BS 1306 AT LWR LIGHTNING HOLE CRACK STOP DRILLED IAW SRM CH 51-10-2 . AREA REPAIRED IAW SRM 51-40-2.

Part: SKIN — LIGHTNING STRIKE (BS 259.5)

INSPECTION TYPE:C LIGHTNING STRIKE BS 259.5 BETWEEN S20R AND 21R. REPAIRED IAW SRM 53-30-03 FIG 20.

Part: BRACKET — CRACKED (NR 3 ENGINE)

INSPECTION TYPE:C, ENGINE NR 3 THRUST REV O/B FAIRING MID SUPPORT BRACKET CRACKED. REPLACED BRACKET IAW MM 78-30-00.

Part: SKIN — CRACKED (PAX DOORWAY)

INSPECTION TYPE:C, SUSPECT SKIN CRACK AT FWD ENTRY DOOR CUTOUT FWD UPPER CORNER. REPAIR CARRIED OUT IAW EO B727-5330-1460-C.

Part: BRACKET — CRACKED (NR 1 ENGINE)

INSPECTION TYPE:C, ENGINE NR 1 THRUST REV O/B FAIRING MID SUPPORT BRACKET CRACKED. REPLACED BRACKET IAW MM 78-30-00.

Part: SWITCH — FAILED (COCKPIT)

INSPECTION TYPE-N/A, EMERGENCY LIGHT COMES ON WHEN SWITCHED TO OFF POSITION AND POWER TURNED OFF. REMOVED AND REPLACED EMERGENCY LIGHTS ON/OFF ARM SW. EMERGENCY LIGHTS CK GOOD IAW WDM 33-51-01.

Part: LIGHT — LOOSE (COCKPIT)

COCKPIT EMERGENCY EXIT LIGHT FLICKERS IN THE ARMED POSITION. RE-SEATED COCKPIT EMERGENCY EXIT LIGHT ASSY INTO HOUSING. OPS CK OK, NO DEFECTS NOTED.

Part: WEB — CRACKED (BS 1381)

INSPECTION TYPE-C, CRACK ON WEB ABOVE NR 2 ENGINE HORIZONTAL FIREWALL RT SIDE AT BS 1381. NEW WEB FABRICATED AND INSTALLED IAW DRAWING 65-17555.

Part: WEB — CRACKED (BS 1381)

INSPECTION TYPE-C, CRACK ON WEB ABOVE NUMBER 2 ENGINE HORIZONTAL FIREWALL LT SIDE AT BS 1381. NEW WEB FABRICATED AND INSTALLED IAW DRAWING 65-17555.

Part: CLEVIS — CRACKED (LT ELEVATOR)

INSPECTION TYPE-C, LT ELEVATOR HAS CRACKED LUGS AT NR 3 HINGE POINT AT ES 66.5. REPAIR CARRIED OUT IAW SRS ENGINEERING ORDER 98-08-001, UPS FILE NUMBER 727-55-0366 AND BOEING SERVICE BULLETIN 727-55-53 REV 3FIGURE 6 AND DRAWING NUMBER 65-68883.

Part: FRAME — CRACKED (BS 360)

INSPECTION TYPE-C, FRAME CRACKED AT FWD RT ST 360 RIGHT HAND SIDE AT STRINGER 25 APPROX. FRAME REPAIRED IAW SRM 51-40-3.

Part: RIB — CRACKED (NR 4 LE SLAT)

INSPECTION TYPE-C, NR 4 LE SLAT CRACK ON RIB (THIRD FROM OUTBOARD). REPAIR CARRIED OUT IAW SRM 51-40-3 FIGURE 1.

Part: SKIN — CRACKED (WS 198)

INSPECTION TYPE-C, RIGHT HAND LE INNER SKIN CRACKED AT WS 198. INNER SKIN CUT OUT AND REPAIR CARRIED OUT IAW SRM 57-30-4.

Part: RIB — CRACKED (NR 4 LE SLAT)

INSPECTION TYPE-C, NR 4 LE SLAT CRACK ON RIB (THIRD FROM OUTBD). DAMAGED AREA BLENDOUT IAW SRM 51-40-01.

Part: CASTING — CORRODED (LT AILERON)

INSPECTION TYPE-C, LT AILERON TURNAROUND PULLEY CASTING HAS CORROSION ON LOWER SUPPORT LUG FOR TAB PULLEY. CASTING REPLACED IAW OHM 27-12-00.

Part: ROD END — WORN (NR 7 SPOILER)

INSPECTION TYPE-C, NR 7 GROUND SPOILER CASTING AND ACTUATOR ROD END HAS EXCESSIVE PLAY. REPLACED SPOILER CASTING IAW MM 27-62-81 AND REPLACED ACTUATOR ROD END IAW OHM 27-60-01.

Part: DOUBLER — CORRODED (NR 1 TANK)

INSPECTION TYPE-C, FUEL LEAK AT NR 1 TANK OVERWING REFUELING AREA ON INVESTIGATION, ADAPTER FILLER AND INTERNAL DOUBLER FOUND CORRODED. REPLACED CORRODED PARTS IAW DRAWING 65-19299.

Part: CASTING — WORN (NR 9 SPOILER)

INSPECTION TYPE-C, NR 9 GROUND SPOILER (ACTUATOR) CASTING HAS EXCESSIVE PLAY AT HINGE POINT. REPLACED ACTUATOR CASTING IAW MM 27-61-91.

Part: ROD END — WORN (NR 6 SPOILER)

INSPECTION TYPE-C, NR 6 GROUND SPOILER CASTING AND LINKAGE HAS EXCESSIVE PLAY. REPLACED WORN ACTUATOR CASTING LINKAGE ROD END AND BOLT IAW MM 27-6 2-81.

Part: FITTING — CRACKED (BS 740)

INSPECTION TYPE-C, BS 740 LT FUSELAGE FITTING HAS SEVERAL CRACKS ON OUTBD FLANGE BETWEEN S18L AND 23L. FITTING REPLACED IAW UPS ENGINEERING ORDER B727-5310-7477 AND SRS EO 98-08-002, REF UPS EO B727-5310-10332-A.

Part: FITTING — CRACKED (BS 740)

INSPECTION TYPE-C, BS 740 RT FUSELAGE FITTING HAS SEVERAL CRACKS ON OUTBD FLANGE BETWEEN S18R AND 23R. FITTING REPLACED IAW UPS ENGINEEIRNG ORDER B727-5310-7477 AND SRS ENGINEERING ORDER 98-08-003, REF UPS EO B727-5310-10331-A.

Part: STRINGER — CORRODED (BS 990)

INSPECTION TYPE-C, AFT CARGO COMPARTMENT CORROSION ON STRINGER 28L AT STA 990. FABRICATED AND INSTALLED REPAIR PER SRM 53-10-3, 51-30-2.

Part: ACTUATOR RIB — CRACKED (WS 286)

INSPECTION TYPE-C, LT NR 2 SLAT ACTUATOR RIB MOUNT ON O/B SIDE IS CRACKED. STOP DRILLED CRACK, FABRICATED REPAIR ANGLE PER SRM 57-50-2, 51-40-3, 51-30-1, 51-30-2, 51-10-1, 51-10-2.

Part: FRAME — CORRODED (BS 990)

INSPECTION TYPE-C, AFT CARGO PIT STRINGER 28L AFT SIDE FRAME CHORD AT STA 990 HAS STRINGER ATTACH HOLE THAT IS CORRODED. FABRICATED AND INSTALLED REPAIR PER SRM 51-40-3.

Part: SKIN — CRACKED (NR 4 LE SLAT)

INSPECTION TYPE-C, 1 INCH CRACK IN LT WING NR 4 SLAT INTERNAL NEXT TO LAST I/B RIB ON I/B SIDE AT BOTTOM IN RADIUS 6 INCHES O/B OF RIB. STOP DRILLED CRACK/ FAB AND INSTALLED REPAIR DOUBLER.

Part: CLIPS — CRACKED (BS 1070)

INSPECTION TYPE-C, STA 1070 STR TO FRAME CLIPS CRACKED AT STR'S 5L, 6L, 7L. REMOVED AND REPLACED CLIPS PER BOEING DWG NR 65-45313.

Part: CLIPS — CRACKED (BS 1070)

INSPECTION TYPE-C, STA 1070 STR TO FRAME CLIPS CRACKED AT STR'S 9R, 7R, 6R, 5R AND 4R. REMOVED AND REPAIRED CLIPS PER BOEING DWG NR 65-45313 AND SRM 51-30-2.

Part: CLIPS — CRACKED (BS 1050)

INSPECTION TYPE-C, STA 1050 STR TO FRAME CLIPS AT 6R, 7R AND 9R. REMOVED AND REPLACED CLIPS PER BOEING DWG NR 65-45313 AND SRM 51-30-2-1.

Part: WEB — CRACKED (NR 1 LE FLAP)

INSPECTION TYPE-C, THE NR 1 SLAT ACTUATOR I/B ATTACH WEB CRACKED. REMOVED WEB DAMAGE AND FABRICATED REPLACEMENT WEB PER SB 727-57-0130, INSTALLED REPLACEMENT WEB PER SB 727-57-0130 AND SRM 51-30-2.

Part: OVERHEAT LIGHT — ILLUMINATED (NR 2 ENGINE)

CREW REPORTED AT TOP OF CLIMB AS THRUST WAS REDUCED, THE NR 2 ENGINE OVERHEAT LIGHT ON OVERHEAD PANEL FLICKERED FOR FIVE SECONDS THEN WENT OUT. ALL ENGINE INDICATIONS NORMAL EXCEPT ON EVM, THE NR 2 ENG N1 WAS AT .5, WHILE NR 1 AND NR 3 WERE .24. AT THE TOP OF DESCENT DURING THRUST REDUCTION, THE NR 2 ENGINE OVERHEAT LIGHT CAME ON STEADY ILLUMINATING THE MASTER ENGINE OVHT LIGHT ON THE FWD PANEL. PER CHECK LIST, THE NR 2 ENGINE THROTTLE WAS CLOSED AND THE LIGHT WENT OUT. AFTER 3 MINUTES AT IDLE, ENGINE SHUT-DOWN CHECK LIST WAS PERFORMED. EMERGENCY WAS DECLARED, MAINTENANCE NOTIFIED, MRR FILED OPEN.

Part: WIRE — DAMAGED (NR 2 ENGINE)

SUPPLEMENTAL MRR: CREW REPORTED AT TOC AS THRUST WAS REDUCED, NR 2 ENG O/HEAT LIGHT ON OVERHEAD PANEL FLICKERED FOR 5 SECONDS AND WENT OUT. AT THE TOD DESCENT DURING THRUST REDUCTION, NR 2 ENG O/HEAT LIGHT CAME ON STEADY ILLUMINATING THE MASTER ENGINE O/HEAT LIGHT ON THE FWD PANEL. PER CHECK LIST, NR 2 ENGINE THROTTLE WAS CLOSED AND LIGHT WENT OUT. AFTER 3 MINUTES AT IDLE, ENG SHUT-DOWN CHECK LIST PERFORMED. EMERGENCY DECLARED. MAINTENANCE NOTIFIED. MAINTENANCE T/S SYS IAW MM 71-00-00 AND FOUND WIRE NR 9281-E9202-20 SHORTED TO GROUND ABOVE ENGINE MOUNT. REPAIRED WIRE INSULATION AND ISOLATED TO PREVENT FURTHER ABRASION. MX PERFORMED ENG O/HEAT SYS FUNCTIONAL TEST IAW AMM 75-41-00, NO DEFECTS NOTED.

Part: PACK — MALFUNCTIONED (LEFT)

ON CLIMB-OUT, CREW NOTICED BURNING SMELL ON CLIMB OUT LT COOLING DOOR AUTOMATICALLY OPENED. OPENED BOTH COOLING DOORS AND SMELL SUBSIDED. BOTH PACKS WERE OPERATED AT 115 DEGREES JUST ABOVE GREEN BAND. ON CLIMB-OUT, CPT NOTICED DPU FLAGS. RAN BOTH PACKS AND SELF-TEST ON EFIS. NO DEFECTS OR SMELLS NOTICED.

Part: CHORD — CORRODED (BS 1342)

WHILE IN C-CHECK, MAINTENANCE FOUND RT FRAME CHORD AT BS 1342, RBL 20 CORRODED. REMOVED AND REPLACED CHORD IAW EO B727-5530-4601.

Part: CHANNEL — CORRODED (WL 250)

WHILE IN C-CHECK, MAINTENANCE FOUND AFT CENTER CHANNEL AT WL 250 CORRODED. REMOVED AND REPLACED CHORD IAW EO B727-5530-4601.

Part: CHANNEL — CORRODED (BS 1342)

WHILE IN C-CHECK, MAINTENANCE FOUND LT CHANNEL AT BS 1342, LBL 18, WL 247 CORRODED. REMOVED AND REPLACED CHORD IAW EO B727-5530-4601.

Part: CHORD — CORRODED (BS 1342)

WHILE IN C-CHECK, MAINTENANCE FOUND LT FRAME CHORD AT BS 1342, LBL 20 CORRODED. REMOVED AND REPLACED CHORD IAW EO B727-5530-4601.

Part: CHORD — CORRODED (BS 1342)

WHILE IN C-CHECK, MAINTENANCE FOUND RT O/B CHORD AT BS 1342, RBL 30, WL 250 CORRODED. REMOVED AND REPLACED CHORD IAW EO B727-5530-4601.

Part: CHORD — CORRODED (BS 1342)

WHILE IN C-CHECK, MAINTENANCE FOUND FORWARD CENTER CHORD AT BS 1342 CORRODED. REMOVED AND REPLACED CHORD IAW EO B727-5530-4601.

Part: SKIN — CORRODED (BS 1243-1342)

WHILE IN C-CHECK, MAINTENANCE FOUND FUSELAGE SKIN GOUGED AND CORRODED BS 1243 TO 1342 BETWEEN STRINGERS 10R AND 14R. INSTALLED FABRICATED PARTS IAW SRM 63-30-2, 51-30-2.

Part: CHORD — CORRODED (BS 1342)

WHILE IN C-CHECK, MAINTENANCE FOUND LT O/B CHORD AT BS 1342, LBL 30, WL 250 CORRODED. REMOVED AND REPLACED CHORD IAW EO B727-5530-4601.

Part: BRACKET — CRACKED (CARGO DOOR)

WHILE IN C-CHECK, MAINTENANCE FOUND MAIN CARGO DOOR AFT LATCH ACTUATOR, FWD MOUNT BRACKET AND ATTACH ANGLE CRACKED. INSTALLED FABRICATED PARTS IAW SRM 51-30-1, 51-30-2.

Part: CHANNEL — CORRODED (BS 1342)

WHILE IN C-CHECK, MAINTENANCE FOUND RT CHANNEL AT BS 1342, RBL 18, WL 247 CORRODED. REMOVED AND REPLACED CHORD IAW EO B727-5530-4601.

Part: CHORD — CORRODED (BS 1342)

WHILE IN C-CHECK, MAINTENANCE FOUND RT FRAME CHORD AT BS 1342, RBL 24 CORRODED. REMOVED AND REPLACED CHORD IAW EO B727-5530-4601.

Part: CHORD — CORRODED (BS 1342)

WHILE IN C-CHECK, MAINTENANCE FOUND LT FRAME CHORD AT BS 1342, LBL 24 CORRODED. REMOVED AND REPLACED CHORD IAW EO B727-5530-4601.

Part: SWITCH — FAILED (RT MLG)

PILOT REPORTED RIGHT MAIN GEAR NO GREEN LIGHT. CYCLED GEAR, STILL NO LIGHT (GOOD TEST), 25 FLAPS, HORN (WARNING), RECEIVED GREEN LIGHT 25 SECONDS AFTER HANDLE WAS DOWN. MX REPLACED DOWNLOCK POSTION SWITCH IAW MM 32-61-22 AND REPLACED LANDING GEAR ELECTICAL MODULE IAW MM 32-09-111. PERFORMED GEAR SWING IAW MM 07-11-00, NO DEFECTS NOTED.