N941UP

Part: BATTERY — INOPERATIVE (COCKPIT)

WITH EMERGENCY EXIT SWITCH ON, COCKPIT AND MAIN ENTRY DOOR LIGHTS DO NOT COME ON REPLACED BATERIES

Part: BULKHEAD — CRACKED (THRUST REVERSER) · airframe 568,314 hrs · 44,735 cycles

ENGINE NR 3 THRUST REVERSER AFT BULKHEAD CRACKED AT 11 O`CLOCK POS. REPAIRED IAW SRM 51-40-2 AND SRM 51-30-2.

Part: SEAT TRACK — BROKEN · airframe 568,314 hrs · 44,735 cycles

SEAT TRACK HORIZ FLANGE UPPER, BROKEN AT BS870 RBL 24.75. REPAIRED IAW UPS EO 727-53-20184.

Part: SUPPORT ANGLE — CRACKED (NR 1 LE SLAT) · airframe 568,314 hrs · 44,735 cycles

LE SLAT CRACKED ON SUPPORT ANGLE BENEATH TELESCOPIC DUCT, REPAIR. REPAIRED IAW SRM 51-40-3 AND SRM 57-50-2 FIG 2.

Part: SKIN — CORRODED (BS 290) · airframe 56,831 hrs · 44,735 cycles

LIGHT SURFACE CORROSION FOUND ON FUSELAGE SKIN BS 290 STR 6L TO 7L. SURFACE CORROSION BLENDED AND FOUND O/S LIMITS. SKIN CUT AND EXTENSIVE CORROSION FOUND ON INNER SURFACE AND DISBOND BETWEEN SKIN AND DOUBLER. FABRICATED NEW SKIN IAW SRM 51-20-01 FOR BS 277-360 S4L AND S10L. RE AIR CARRIED OUT IAW UPS EO B727-5330-22625.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 568,314 hrs · 44,735 cycles

ON REMOVAL OF FLOOR PANEL OUTSIDE FWD LAV, INTERCOSTAL FOUND CORRODED. LOCATION BETWEEN BS312-328 LBL 29. REPLACED INTERCOSTAL IAW SRM 53-10-02 AND 53-30-2.

Part: SHEAR WEB — CORRODED (MCD SILL) · airframe 568,314 hrs · 44,735 cycles

NUMEROUS AREAS OF LIGHT SURFACE CORROSION ON MAIN CARGO DOOR SILL SHEAR WEB IN UPPER SURFACE AREAS OF CORROSION CLEANED AND REPROTECTED. WITHIN LIMITS PER SRM 51-1 0-6.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 568,314 hrs · 44,735 cycles

REPLACE UPPER CHORD OF FLOORBEAM BS 344 FROM LBL 12 RBL 30 IAW SRM DUE CORROSION. REPLACED UPPER CHORD IAW SRM 53-10-8.

Part: SUPPORT — CORRODED · airframe 568,314 hrs · 44,735 cycles

FWD LAV SUPPORT TOP HAT EXTRUSION IS CORRODED AT BS 328RBL 13. REPLACED FWD LAV SUPPORT/TOP HAT IAW SRM 51-20-1 FIG 7.

Part: FITTING — CORRODED · airframe 568,314 hrs · 4,735 cycles

RT MLG W/W, BS 870 FITTING HAS EVIDENCE OF CORROSION AT LOWER O/B FLANGE. REPAIRED IAW UPS EO 727-53-20186. (M)

Part: REGULATOR — LEAKING (COCKPIT OXYGEN)

INSPECTION TYPE:N/A CREW OXYGEN SYSTEM LEAKING AT REGULATOR DIRECTLY ABOVE BOTTLE. REMOVED AND REPLACED CREW 02 PRESS REDUCING REGULATOR PER MM 35-11-21. LEAK AND OPS CHECK GOOD.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT)

FOUND EMERGENCY LIGHT SWITCH IN ON POSITION, BATTERIES DISCHARGED. REPLACED BATTERIES, NOW OPS GOOD.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 50,850 hrs · 39,757 cycles

INSPECTION TYPE: C, BROKEN BRACKET AT BS 1223 LBL 36 AFT AIRSTAIRS EQUIP AREA. REMOVED BROKEN BRACKET IAW OHM 20-50-01. BRACKET FABRICATED IAW SRM 51-20-01 AND INSTALLED IAW SRM 51-30-02.

Part: YOKE — CORRODED (LT MLG) · airframe 50,850 hrs · 39,757 cycles

INSPECTION TYPE: C, ON REMOVAL & BREAKDOWN OF LT SWING LINK, YOKE ASSY FOUND TO BE CORRODED. REPLACED SWING YOKE SUPPORT LT MLG SWING LINK IAW MM 57-15-01.

Part: FLAP TRACK — CRACKED (NR 7 FLAP) · airframe 50,850 hrs · 39,757 cycles

INSPECTION TYPE: C, NR 7 FLAP TRACK FAIRING I/B TRACK CRACKED. REPLACED TRACK IAW DRW 65-21796 & SRM 51-30-02.

Part: WEB — CRACKED (KRUGER FLAP) · airframe 50,850 hrs · 39,757 cycles

INSPECTION TYPE: C, NR 1 KRUEGER FLAP ACTUATOR TRUNNION CAP SUPPORT WEB I/B & O/B CRACKED. NR 1 K-FLAP ACTUATOR REMOVED PER MM 27-81-22. FABRICATED TRUNNION CAP SUPPORT WEB IAW SRM 51-20-1. INSTALLED 31 K-FLAP ACTUATOR TRUNNION SUPPORT CAP WEB PER BOEING DRAWING 65-16269. INSTALLED NR 1 K-FLAP ACTUATOR IAW MM 27-81-22.

Part: BRACKET — CRACKED (THRUST REVERSER) · airframe 50,850 hrs · 39,757 cycles

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

Part: SKIN — CRACKED (RT ELEVATOR) · airframe 50,850 hrs · 39,757 cycles

INSPECTION TYPE: C, X-RAY INSPECTION OF RIGHT ELEVATOR SHOWS 2 CRACK INDICATIONS ON BEADED SKIN, PREVIOUSLY STOP DRILLED ON PANEL ELEVATOR STA 136.5 TO 173.21. REPAIR CARRIED OUT IAW SRM 51-30-02, 55-20-3, 51-40-5, 55-20-3, 51-30 -026, 51-10-02 & DRG 65-25638.

Part: SKIN — CRACKED (RT ELEVATOR) · airframe 56,172 hrs · 44,234 cycles

INSPECTION TYPE: C, X-RAY INSPECTION OF RT ELEVATOR SHOWS 2 CRACK INDICATIONS ON BEADED SKIN, PREVIOUSLY STOP DRILLED ON PANEL ELEV STA 136.5 TO 173.21. HFEC CARRIED OUT. CRACKS CONTAINED WITHIN STOP DRILLED HOLES. REPAIR DOUBLERS FABRICATED IAW SRM 55-20-3. BONDED TO PANEL IAW SRM 51-40-5. REPAIRS RIVETED IAW SRM 55-20-3 FIG 3 AND SRM 51-30-026. RT ELEV BALANCE CALCULATED IAW SRM 51-80-07.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 50,850 hrs · 39,757 cycles

INSPECTION TYPE:C, CORROSION ON SEAT TRACK AT BEARSTRAP LOCK PIN LOCATION, BS 950 RBL 4 5.5. FABRICATED AND INSTALLED NEW SEAT TRACK SECTION IAW SRM 53-10-5. REPAIR CARRIED OUT IAW SRM EO 2004-017-001 UPS ENGINEERING FILE 727-53-20136.

Part: FITTING — CRACKED (TAIL SKID BAY) · airframe 50,850 hrs · 39,757 cycles

INSPECTION TYPE:C, RIGHT LWR TERMINAL FITTING IN TAIL SKID BAY CRACKED. RIGHT LWR TERMINAL FITTING REPLACED IAW DWG 65-25992.

Part: WEB — CRACKED (KRUGER FLAP) · airframe 50,850 hrs · 39,757 cycles

INSPECTION TYPE: C, CRACKS ON NR 5 K-FLAP ACTUATOR I/B & O/B TRUNNION CAPS SUPPORT WEBS AT UPPER & LWR CORNERS. NR 5 K-FLAP ACTUATOR REMOVED PER MM 27-81-22. FABRICATED TRUNNION CAPS SUPPORT WEBS IAW SRM 51-20-1 & DRG 65-16269. INSTALLED TRUNNION CAPS SUPPORT WEB PER BOEING DRG 65-16249. INSTALLED NR 5 K-FLAP ACTUATOR IAW MM 27-81-22.

Part: FITTING — CRACKED (TAIL SKID BAY) · airframe 50,850 hrs · 39,757 cycles

INSPECTION TYPE: C, LEFT UPPER TERMINAL FITTING IN TAIL SKID BAY CRACKED. LEFT UPPER TERMINAL FITTING IN TAIL SKID BAY REPLACED IAW DWG 65-2 5992.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,850 hrs · 39,757 cycles

INSPECTION TYPE: C, FUSELAGE SKIN CRACKED AT BS 1354 RT. REPAIRED IAW SRM 51-40-2 FIG 1.

Part: CASTING — CORRODED (I/B RT AILERON) · airframe 50,850 hrs · 39,757 cycles

INSPECTION TYPE: C, SURFACE CORROSION ON I/B RIGHT AILERON TAB HINGE BEARING SUPPORT CASTINGS (BOTH O/B AND MIDDLE CASTINGS). REMOVED I/B AILERON IAW MM 27-10-01. REPLACED CORRODED TAB HINGE SUPPORT CASTINGS IAW SRM 51-30-2. NO WEIGHT CHANGE OCCURRED TO AILERON DURING CASTING REPLACEMENT.

Part: SHOCK ABSORBER — CRACKED (TAIL SKID) · airframe 50,850 hrs · 39,757 cycles

INSPECTION TYPE: C, TAIL SKID ABSORBER FOUND TO BE CRACKED. REPLACED TAIL SKIN ABSORBER IAW MM 32-71-41 & OHM 32-71-04.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,850 hrs · 39,757 cycles

INSPECTION TYPE: C, SUSPECT CRACK INDICATION AT BS 243.7 WL 216.5. AREA PAINT STRIPPED IAW MM 51-20-01. HFEC INSPECTION CARRIED OUT AT THE ABOVE AREA IAW B727 NDTM PT 6 51-00-00. RESULT: CRACK CONFIRMED AND END MARKED. REPAIR CARRIED OUT IAW SRM 53-30-3 FIG 3.

Part: FITTING — CRACKED (FUSELAGE) · airframe 56,172 hrs · 44,234 cycles

INSPECTION TYPE: C, SUSPECTED CRACK FOUND ON BS 940 FITTING LEFT ON FWD UPPER FLANGE. FITTING REPLACED IAW EO B727-5310-4501 AND DRW 65C15732.

Part: FIRE DETECTOR — WILL NOT TEST (CARGO BAY)

LOWER CARGO FIRE MX LIGHT ON. CODES A7418A, A9051A 26-18-02 SYSTEM OK. TESTED AND RESET LOWER CARGO SMOKE DETECTOR SYSTEM IAW MM 26-18-02 SYSTEM OK.

Part: CHECK VALVE — CONTAMINATED (HYD SYSTEM)

INSPECTION TYPE:N/A AT APPROX 3000 FT CREW NOTICED SMOKE IN COCKPIT DID AN AIR TURNBACK TO DEC. REMOVED AND REPLACED THE A-SYSTEM AIR PRESUURE REGULATOR IAW M/M 2912. FOUND EVIDENCE OF HYDRAULIC FLUID IN RES AIR PRESSURE CHECK VALVE ASSY RNR ALL 3 CHECK VALVES PERFORMED LEAK CK RAN ALL ENGINES WITH 2 PACKS, NO FAULTS NOTED RNR WATER SEPARATOR BAGS PRECAUTIONARY.

Part: CHECK VALVE — LEAKING (HYD SYSTEM)

INSPECTION TYPE: N/A SMOKE IN COCKPIT - ATB. A/C LANDED WITHOUT INCIDENT. T/S IN PROGRESS. REMOVED AND REPLACED THE A SYS AIR PRESSURE REGULATOR IAW MM 2912. FOUND EVIDENCE OF HYD FLUID IN THE RES AIR PRESS CHECK VALVE ASSY. REMOVED AND REPLACED ALL 3 CHECK VALVES PERFORMED LK CHECK AND RAN ALL 3 ENGINES APPROX 10 MINS 2 PACKS ON NO DEFECTS FOUND.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,486 hrs · 43,683 cycles

INSPECTION TYPE:C DURING INSTALLATION OF REPAIR PARTS TO LOWER SECTION OF BS 930 FITTING, CRACKS FOUND ON AFT HORIZONTAL FLANGE AT WL 201. FRAME REPLACED IAW DWG 65-16336 AND SRM 51-30-3. FRAME REPAIR IAW SRM 53-10-4 FIG 1 FRAME REINFORCING ANGLE REPAIRED IAW SRM 51-40-4 FIG 1.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 55,486 hrs · 43,683 cycles

INSPECTION TYPE:C NLG RT PRESSURE WEB HAS SUSPECT CRACK AT BS 286 4 INCHES FROM SILL. HFEC CARRIED OUT IAW NDT MAN PT6 51-00-00 FIG 4 CRACK CONFIRMED AND ENDS MARKED. DAMAGE REMOVED IAW SRM 51-10-01. HFEC INSPECT CUTOUT TO CONFRM DAMAGE REMOVAL. REPAIRED IAW SRM 51-40-02 FIG 1.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 55,486 hrs · 43,683 cycles

INSPECTION TYPE:C SUSPECT CRACK IN NOSE WHEEL WELL RT PRESSURE WEB BS 258. HFEC CONFIRMS CRACKS IAW 727 NDT MAN PT6 51-00-00 FIG 4. DAMAGE AREA REMOVED IAW SRM 51-10-01. HFEC CARRIED OUT AND CONFIRMS DAMAGE REMOVAL. REPAIR CARRIED OUT IAW SRM 51-40-02 FIGURE 1.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 55,486 hrs · 43,683 cycles

INSPECTION TYPE:C SUSPECT CRACK AT BS 246, NLG WHEEL WELL RT PRESSURE WEB 6 INCHES ABOVE SILL CHORD. HFEC IAW NDT MAN 51-00-00 PT 6 FIG 4 CRACK CONFIRMED, DAMAGE CUTOUT IAW SRM 51-10-01, HFEC IAW NDT MAN 51-00-00 PT 6 FIG 4 NDF. REPAIR CARRIED OUT IAW SRM 51-40-02 FIGURE 1.

Part: CONTROL QUADRANT — CORRODED (AILERON) · airframe 55,486 hrs · 43,683 cycles

INSPECTION TYPE:C LT I/B AILERON BUS QUADRANT FOUND TO HAVE CORROSION ON BEARING SEAT ON REMOVAL OF BEARINGS. REMOVED LOWER QUADRANT IAW MM 27-10-56, QUADRANT REPLACED IAW MM 27-10-56.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 55,486 hrs · 43,683 cycles

INSPECTION TYPE:C CRACK INDICATION FOUND IN RIGHT WALL OF NOSE WHEEL WELL LOCATED AT B S 264.5 APPROX 7 INCHES FROM CEILING CRACK IS APPROX 2 INCHES LONG. HFEC INSPECT IAW NDT MAN PT6 51-00-00 FIG 4, CRACK CONFIRMED AND ENDS MARKED. DAMAGE REMOVED IAW SRM 51-10-01, HFEC CARRIED OUT ON CUTOUT NDF. REPAIR CARRIED OUT IAW SRM 51-40-02 FIG 1

Part: BRACKET — CORRODED (WS192) · airframe 55,486 hrs · 43,683 cycles

INSPECTION TYPE:C R/H WING REAR SPAR LWR CHORD T BRACKET CORRODED WS 192 TO GAIN ACCESS #2 TANK FRONT SPAR PANELS REMOVED. NEW BRACKET INSTAL LED IOAW BOEING DWG 65-16201, WING PANELS CLOSED.

Part: STRAP — CORRODED (FUSELAGE) · airframe 55,486 hrs · 43,683 cycles

INSPECTION TYPE:C TEAR STRAP DISBONDED AT BS 640 BETWEEN S4R AND S5R. DURING REPAIR IAW SRM CORROSION NOTED BETWEEN FAYING SURFACES. TEAR STRAP REMOVED IAW SRM 51-30-02, CORROSION FOUND OUTSIDE LIMITS, NEW TEAR STRAP FABRICATED IAW SRM 53-30-04 PARA 2C METHOD V AND INSTALLED.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 55,486 hrs · 43,683 cycles

INSPECTION TYPE:C NOSE WHEEL WELL RT SIDE WALL WEB HAS SUSPECT CRACK 3 INCHES ABOVE SILL AT BS 243 APPROX. HFEC CARRIED AND CONFIRMS CRACKS. DAMAGE REMOVED IAW SRM 51-10-01, HFEC C/W ON CUTOUT NDF. REPAIRED IAW SRM 51-40-02 FIGURE 1.

Part: WEB — CRACKED (R/H WING) · airframe 55,486 hrs · 43,683 cycles

INSPECTION TYPE:C CRACK ON WEB ABOVE NO5 L/E FLAP I/B CORNER. CRACK STOP DRILLED IAW 727 SRM 51-10-01 NDT CARRIED OUTIAW NDT MAN 5 1-00-00 PT 6 FIG 4, CRACK CONTAINED. REPAIR CARRIED OUT IAW SRM REF 51-40-02.

Part: WEB — CRACKED (BS 285) · airframe 55,486 hrs · 43,683 cycles

INSPECTION TYPE:C NOSE WHEEL WELL L/H SIDEWALL WEB HAS SUSPECT CRACK AROUND RIVETS @ B S 285, 3" ABOVE SILL WEB REPAIRED IAW SRM 51-40-2 FIG 1

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,486 hrs · 43,683 cycles

INSPECTION TYPE:C CRACK CONFIRMED AT MID GALLEY DOOR LWR HINGE LWR CUTOUT. CRACK CONTAINED WITH STOP DRILL CONFIRMED BY NDT HFEC. REPAIR DOUBLER FABRICATED IAW UPS EO B727-5330-1036 AND BOEING DWG 65-73484.

Part: ANGLE — CRACKED (BS 870 S18A WEB) · airframe 55,486 hrs · 43,683 cycles

INSPECTION TYPE:C LEFT MLG WHEEL WELL, ATTACH ANGLE LOCATED BETWEEN FITTING BS 870 & S TR. 18A WEB IS CRACKED REPLACED ANGLE IAW SRM 51-30-2

Part: WEB — CRACKED (FUSELAGE) · airframe 55,486 hrs · 43,683 cycles

INSPECTION TYPE:C LT LIGHTNING HOLE, FOURTH AFT UPPER HOLE ON LT AIRSTAIR WELL SIDE WALL IS CRACKED AT 5 O'CLOCK POSITION. CRACK STOP DRILLED IAW SRM 51-10-01 & REPAIR CARRIED OUT IAW SRM 51-40-02.

Part: ATTACH FITTING — CRACKED (SPOILER) · airframe 55,486 hrs · 43,683 cycles

INSPECTION TYPE:C NR 13 SPOILER SUPPORT CASTING O/B CASTING ATTACH BRACKET IS CRACKED AT LOWER ATTACH HOLE. REMOVED NR 13 SPOILER AND FWD ATTACH CASTING IAW MM 27-62-01, REPLACED O/B SUPPORT CASTING IAW DWG 65-17351 AND 65-16201, AND SRM 51-30-20. REINSTALLED SPOILER AND SPOILER SUPPORT IAW MM 27-61-01, 27-61-81.

Part: WEB — CRACKED (FUSELAGE) · airframe 55,486 hrs · 43,683 cycles

INSPECTION TYPE:C RT LIGHTNING HOLE SECOND AFT UPPER HOLE ON STAIRWELL SIDE WALL AT 7 O'CLOCK POSITION IS CRACKED. CRACK STOP DRILLED IAW SRM 51-10-01, REPAIRED IAW SRM 51-40-02.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 55,486 hrs · 43,683 cycles

INSPECTION TYPE:C SUSPECT CRACK INDICATION FOUND IN NOSE WHEEL WELL SIDEWALL AT BS 276 RT SIDE 3 INCH INDICATION IS LOCATED 24 INCHES FROM NWW CEILING. DAMAGE REMOVED IAW SRM 51-10-1 REPAIRED AREA IAW SRM 51-40-02 FIG 1.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 55,486 hrs · 43,683 cycles

INSPECTION TYPE:C LWR FWD CARGO HOLD DOOR CRACK ON INNER SKIN ADJACENT TO LWR TORQUE UBE AT LIGHTNING HOLE. REPAIR CARRIED OUT IAW SRM 51-40-2 FIG 1.

Part: BRACKET — CRACKED (DOOR PULL HANDLE) · airframe 55,486 hrs · 43,683 cycles

INSPECTION TYPE:C DOOR PULL HANDLE SUPPORT BRACKET REPAIR CARRIED OUT IAW SRM 51-30-3

Part: BUTT JOINT — CORRODED (BS 441) · airframe 55,486 hrs · 43,683 cycles

INSPECTION TYPE:C SUSPECT CORROSION FOUND AT BUTT JOINT BS 441, AREA DERIVETED BETWEEN S17 AND S21 R. COROSION FOUND OUTSIDE LIMITS BETWEEN 18R AND 21R IAW SRM 53-30-01. REPAIRED IAW UPS EO B727-5310- 1371 APPENDIX E.

Part: HOUSING — CRACKED (RT WING) · airframe 55,486 hrs · 43,683 cycles

INSPECTION TYPE:C FUEL LEAKING FROM NR 3 TANK O/B BOOST PUMP CAVITY. FUEL LEAK TRACED TO BOOST PUMP HOUSING FWD I/B AREA AT ATTACH FLANGE, SEALANT REMOVED FROM SUSPECT AREA IAW SRM 51-20-4, SUSPECT CRACKS FOUND ON BOOST PUMP ATTACH FLANGE, HFEC CONFIRMS CRACKS. CRACKED BOOST PUMP HOUSING FLANGE CUTOUT IAW SRM 51-10-01. HFEC PERFORMED ON CUTOUT NDF. HOUSING REPAIRED IAW SRM 57-10-3, SEALED IAW SRM 51-20-04.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 54,591 hrs · 43,038 cycles

INSPECTION TYPE:C+SI, DURING REPAIR TO CORRODED STRINGER 24R AT BS 463 FASTENER HOLE SIZES AT ENDS OF FRAME TO SKIN WERE FOUND TO BE EXCESSIVE BS 460 BETWEEN S2 4R AND S25R. CARRIED OUT REPAIR IAW SRM 53-10-4.

Part: BULKHEAD — CHAFED (FUSELAGE) · airframe 54,591 hrs · 43,038 cycles

INSPECTION TYPE:C+SI, OPERATING HANDLE FOR AIRSTAIRS PUMP HAS CHAFED AFT PRESSURE BULKHEAD. REPAIRED IAW SMRO EO 2001-006-019.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 54,591 hrs · 43,038 cycles

INSPECTION TYPE:C+SI, SPLICE FITTING AT BS 1040 (REAR CARGO COMPT) CORRODED AND CRACKED. REPLACED FITTING IAW SRM 51-30-2.

Part: PRESSURE PANEL — CRACKED (NLG WW) · airframe 54,591 hrs · 43,038 cycles

INSPECTION TYPE:C+SI, NOSE WHEEL WALKWAY AREA PRESSURE PANEL CRACKED AT UPPER SIDE BS 309 LBL 4. CARRIED OUT REPAIR IAW SRM 51-20-1.

Part: FASTENER — CORRODED (FRAME) · airframe 54,591 hrs · 43,038 cycles

INSPECTION TYPE:C+SI, BOLTS FOUND CORRODED AT BS 360 BETWEEN STR 24-26L AND 24-26R. HOLES REWORKED IAW SMRO EO 2001-006-020.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 54,591 hrs · 43,038 cycles

INSPECTION TYPE:C+SI, CORROSION ON STRINGER 25R BS 463. REPLACED STRINGER IAW SRM 53-10-3.

Part: PANEL — CORRODED (LT ELEVATOR) · airframe 54,591 hrs · 43,038 cycles

INSPECTION TYPE:C+SI, NR 5 BALANCE BAY HINGE LT ELEVATOR HAS SLIGHT SURFACE CORROSION. BALANCE PANEL REPLACED IAW MM 27-30-21.

Part: STIFFENER — CORRODED (WING) · airframe 54,591 hrs · 43,038 cycles

INSPECTION TYPE:C+SI, WHILE REMOVING CORROSION FROM NR 3 FLAP TRACK TO AUX SPAR MOUNT HOLES THE STIFFENER ABOVE MOUNT RIVETED TO THE AUX SPAR WAS FOUND TO HAVE EXCESSIVE CORROSION IN BARREL NUT HOLE. STIFFENER REPLACED IAW SRM 51-30-00 AND DRAWING 65-16216.

Part: SPAR — CORRODED (LT WING) · airframe 54,591 hrs · 43,038 cycles

INSPECTION TYPE:C+SI, AFTER REMOVING A STIFFENER LOCATED AT FWD SIDE OF LT AUX SPAR, THE UPPER CHORD OF THE AUX SPAR WAS FOUND TO HAVE CORROSION IN A 2 INCH SECTION AROUND WS 277. UPPER CHORD REPAIRED IAW SRM 51-10-01.

Part: ATTACH FITTING — CRACKED (FLAP) · airframe 54,591 hrs · 43,038 cycles

INSPECTION TYPE:C+SI, RT WING - CRACK AT NR 7 FLAP TRACK ATTACH AREA O/B FASTENER ROW, THIRD HOLE FROM FRONT. REPAIR CARRIED OUT IAW SRM 51-30-5 & SMRO WO 2001-006-013 UPS ENGINEERING FILE NR B727-5730-14010-A.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 54,591 hrs · 43,038 cycles

INSPECTION TYPE:C+SI, INTERCOSTAL T-PROFILE HAS CRACK AT ATTACH POINT BS 1183 VERT BEAM LBL 17.8 WL 283. T-PIECE REPLACED IAW SRM 51-30-2, FABRICATED IAW BOEING DWG 65C34406.

Part: STIFFENER — CORRODED (CENTER WING) · airframe 54,591 hrs · 43,038 cycles

INSPECTION TYPE:C+SI, ON REMOVAL OF CENTER SECTION REAR SPAR UPPER CHORD SEVERAL STIFFENERS FOUND DAMAGED AND CORRODED. REPLACED STIFFENERS IAW 51-30-02 AND DWG 65C21531.

Part: BOLT — CRACKED (NR 6 ROLLER) · airframe 54,591 hrs · 43,038 cycles

INSPECTION TYPE:C+SI, DURING MAG PARTICLE INSP DEAD WEIGHT ROLLER BOLT NR 6 FOUND CRACKED. BOLT REPLACED IAW MM 27-51-03.

Part: BRACKET — CORRODED (SPOILER) · airframe 54,591 hrs · 43,038 cycles

INSPECTION TYPE:C+SI, LT WING NR 5 SPOILER INBD BRACKET SUPPORT RIVETED TO AUX SPAR HAS A NUMBER OF POPPED RIVET HEADS. BRACKET FOUND CORRODED THEREFORE BRACKET REPLACED.

Part: PIN — CRACKED (LT HORIZ STAB) · airframe 54,591 hrs · 43,038 cycles

INSPECTION TYPE:C+SI, LT OUTER HORIZ STAB HINGE PIN CRACKED. REPLACED PIN IAW MM 55-10-01.

Part: SPAR — CORRODED (WING) · airframe 54,591 hrs · 43,038 cycles

INSPECTION TYPE:C+SI, CORROSION FOUND ON REAR SPAR UPPER CHORD OUT OF LIMITS. CHORD REPLACED IAW BOEING DRG 65C21531 AND SMRO EO 2001-006-004 UPS ENGINEERING FILE NR B727-5710-4094-A.

Part: ANGLE — CRACKED (RT MLG) · airframe 54,591 hrs · 43,038 cycles

INSPECTION TYPE:C+SI, RT MLG DOOR ACTUATOR REACTION SUPPORT STRUCTURE 2 ANGLES CRACKED. REPLACED IAW SRM 51-30-2.

Part: INTERCOSTAL — CRACKED (RT MLG) · airframe 54,591 hrs · 43,038 cycles

INSPECTION TYPE:C+S, RT MLG FWD CUTOUT INTERCOSTAL CRACKED AT MLG DOOR MANUAL RELEASE HANDLE. REPAIR CARRIED OUT IAW SRM 51-40-03.

Part: CONTROL VALVE — CORRODED (TE FLAP) · airframe 54,591 hrs · 43,038 cycles

INSPECTION TYPE:C+SI, CORROSION ON T/E FLAP INPUT QUADRANT ABOVE FLAP CONTROL VALVE. REPAIR CARRIED OUT IAW MM 27-51-00 & MM 27-51-51.

Part: FRAME — CRACKED (RT MLG WW) · airframe 54,591 hrs · 43,038 cycles

INSPECTION TYPE:C+SI, RT BS 910 CRACKED IN MAIN LANDING GEAR WHEEL WELL. REPAIRED IAW DRAWING NR 65C27194.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 54,591 hrs · 43,038 cycles

INSPECTION TYPE:C+SI, CORROSION ON FLOORBEAM TOP CAP BS 344 BETWEEN LBL 10 & RBL 14. FLOORBEAM REPAIRED IAW SRM 53-10-8.

Part: FRAME — CORRODED (FUSELAGE) · airframe 54,591 hrs · 43,038 cycles

INSPECTION TYPE:C+SI, FWD CARGO BAY, EVIDENCE OF CORROSION ON BS 520 AFT FACE AT LOWER FORWARD AREA ADJACENT TO DOOR OPEN CLOSE SWITCH. REPAIRED IAW SRM 51-10-06.

Part: SUPPORT FITTING — WORN (SPOILER) · airframe 54,591 hrs · 43,038 cycles

INSPECTION TYPE:C+SI, INBOARD SUPPORT ARM FOR NR 7 SPOILER IS LOOSE AND HAS WEAR, WHERE SUPPORT ARM CONNECTS TO MAIN LANDING GEAR BEAM. BUSHING INSTALLED IAW SMRO EO 2001-006-018.

Part: FRAME — CRACKED (LT MLG WW) · airframe 54,591 hrs · 43,038 cycles

INSPECTION TYPE:C+SI, LT 910 FRAME CRACKED IN MAIN LANDING GEAR WELL. REPAIRED IAW EO B727-5319-1896-B.

Part: BRACKET — CRACKED (LT ELEVATOR) · airframe 54,591 hrs · 43,038 cycles

INSPECTION TYPE:C+SI, LT ELEV POSITION SENSOR BRACKET ON FRONT SPAR CRACKED. REPLACED IAW MM 20-80-01.

Part: SUPPORT FITTING — CORRODED (SPOILER) · airframe 54,591 hrs · 43,038 cycles

INSPECTION TYPE:C+SI, EVIDENCE OF SURFACE CORROSION ON NR 13 SPOILER ACTUATOR SUPPORT CASTING AND LIGHT SURFACE CORROSION ON O/B RIB ATTACHED TO SUPPORT CASTING. REPAIR CARRIED OUT IAW MM 27-61-81 & MM 27-61-81.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,591 hrs · 43,038 cycles

INSPECTION TYPE:C+SI, SUSPECT CRACK ON UPPER CHORD AT BS 740 AT LBL 60 APP. REPAIRED IAW SRM 51-30-02.

Part: FLANGE — CRACKED (FUSELAGE) · airframe 54,591 hrs · 43,038 cycles

INSPECTION TYPE:C+SI, DURING INSP 2 DISCREPANT HOLES WERE FOUND ON AFT O/B FLANGE OF BS 950 LT SIDE FITTING (1 CRACK) (1 HOLE CORRODED). REPAIR CARRIED OUT IAW SMRO EO 2001-006-003 UPS ENGINEERING FILE NR 727-57-20006.

Part: STRUCTURE — CORRODED (WING) · airframe 54,591 hrs · 43,038 cycles

INSPECTION TYPE:C+SI, X-RAY REPORT - SUSPECT CORROSION ON WING CENTER SECTION AT WBL 70.5 UPPER LT AREA AT BS 870. REPAIR CARRIED OUT IAW SRM 51-30-2 BOEING DWG 69-13965 & SMRO EO 200 1-006-015, UPS ENGINEERING FILE NR 727-57-20009.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 54,591 hrs · 43,038 cycles

INSPECTION TYPE:C+SI, UPPER CHORD OF INTERCOSTAL BETWEEN BS 1148 & BS 1156 CRACKED. REPLACED UPPER CHORD OF INTERCOSTAL IAW SRM 51-20-2.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 54,591 hrs · 43,038 cycles

INSPECTION TYPE:C+SI, CORROSION FOUND ON FLOORBEAM TOP CAP BS 950 RBL 55. REPAIRED IAW SMRO EO 2001-006-017.

Part: PIN — CORRODED (RT WING) · airframe 54,591 hrs · 43,038 cycles

INSPECTION TYPE:C+SI, RIGHT BS 740 BOTTLE PIN CORRODED. BOTTLE PIN REPLACED IAW MM 57-41-01.

Part: FITTING — CORRODED (RT WING) · airframe 54,591 hrs · 43,038 cycles

INSPECTION TYPE:C+SI, NR 7 FLAP TRACK ATTACH FITTING ON LWR SURFACE OF RT WING HAS LIGHT SURFACE CORROSION ON INBD FACE OF FITTING. CORROSION REMOVED IAW OHM REF EO SMRO 2001-006-008 FOR DETAILS.

Part: FLAP TRACK — CORRODED (WING) · airframe 54,591 hrs · 43,038 cycles

INSPECTION TYPE:C+SI, NR 5 FLAP TRACK HAS EVIDENCE OF CORROSION TO INBD LUG AT FWD ATTACH POINT. CORROSION REMOVED AND REWORKED IAW OHM 57-40-01.

Part: STRUCTURE — CRACKED (WING CNTR BOX) · airframe 54,591 hrs · 43,038 cycles

INSPECTION TYPE:C+SI, X-RAY REPORTS SUSPECT CRACKS AND CORROSION IN WING CENTER SECTION AT WBL 70.5 UPPER RT AREA AT BS 870. REPAIRED IAW SMRO EO 2001-006-016.

Part: WEB — CRACKED (AFT CARGO BAY) · airframe 54,591 hrs · 43,038 cycles

INSPECTION TYPE:C+SI, CRACK IN AFT CARGO HOLD CLOSURE WEB FWD OF DOOR CUTOUT. WEB REPAIRED IAW SRM 51-40-02 PRIMER APPLIED TO WEB IAW SRM 51-20-15.

Part: CASTING — CORRODED (SPOILER) · airframe 54,591 hrs · 43,038 cycles

INSPECTION TYPE:C+SI, LT WING T/E, NR 1 SPOILER, O/B END SUPPORT CASTING IS CORRODED. REPAIR CARRIED OUT IAW SRM 51-30-2.

Part: ATTACH FITTING — CORRODED (LT WING) · airframe 54,591 hrs · 43,038 cycles

INSPECTION TYPE:C+SI, NR 1 FLAP TRACK ATTACH FITTING ON LWR SURFACE OF WING HAS LIGHT SURFACE CORROSION ON INBOARD SIDE AND OUTBOARD SIDE. REWORKED IAW SMRO EO 2001-006-006.

Part: FLAP TRACK — CORRODED (LT WING) · airframe 54,591 hrs · 43,038 cycles

INSPECTION TYPE:C+SI, NR 7 FLAP TRACK, FWD ATTACH LUGS HAS HEAVY SURFACE CORROSION FOUND ON BOTH LUGS ON BOTH INBD AND OTBD THRUST FACES BORE HAS ALSO GOT SIGNS OF CORROSION. CORROSION REMOVED BY MACHINING AND BUSHINGS INSTALLED AS REQUIRED.

Part: LINK — CORRODED (NR4 KRUEGER FLAP) · airframe 54,591 hrs · 43,038 cycles

INSPECTION TYPE:C+SI, NR 4 KRUEGER FLAP O/B LINK CORRODED AT O/B SIDE. REPLACED LINK IAW OHM 20-50-01.

Part: ATTACH FITTING — CORRODED (FLAP) · airframe 54,591 hrs · 43,038 cycles

INSPECTION TYPE:C+SI, NR 1 FLAP TRACK EVIDENCE OF HEAVY CORROSION FOUND ON FWD ATTACH LUGS, ON BOTH INBD AND OUTBD THRUST FACES. ALSO, BORE HAS SIGNS OF LITE SURFACE CORROSION. REWORKED IAW SMRO EO 2001-006-006.

Part: FLAP TRACK — CORRODED (WING) · airframe 54,591 hrs · 43,038 cycles

INSPECTION TYPE:C+SI, NR 7 FLAP TRACK, AFT MOUNT OTBD HOLE DAMAGED DUE TO CORROSION. REWORKED IAW OHM 57-40-01.

Part: CARRIAGE — CORRODED (NR 3 FLAP) · airframe 54,591 hrs · 43,038 cycles

INSPECTION TYPE:C+SI, NR 3 FLAP CARRIAGE HAS CORROSION IN SPINDLE BORE. NR 3 FLAP CARRIAGE REPLACED IAW MM 27-51-03.

Part: LINK — CORRODED (NR7 SPOILER) · airframe 54,591 hrs · 43,038 cycles

INSPECTION TYPE:C+SI, SURFACE CORROSION ON NR 7 SPOILER ACTUATING LINKAGE. LINKAGE REPLACED IAW MM 27-61-01.

Part: CARRIAGE — CORRODED (T/E FLAP) · airframe 54,591 hrs · 43,038 cycles

INSPECTION TYPE:C+SI, NR 5 FLAP CARRIAGE HAS CORROSION IN SPINDLE BORE. REPLACED CARRIAGE IAW MM 27-51-03.

Part: BOLT — CORRODED (NR7 SPOILER) · airframe 54,591 hrs · 43,038 cycles

INSPECTION TYPE:C+SI, NR 7 SPOILER ACTUATING LINKAGE BOLT CORRODED. REPLACED BOLT AND LINKAGE IAW MM 27-61-01.

Part: CARRIAGE — CORRODED (FLAP) · airframe 54,591 hrs · 43,038 cycles

INSPECTION TYPE:C+SI, NR 6 FLAP CARRIAGE HAS CORROSION INSIDE SPINDLE BORE. NR 6 FLAP CARRIAGE REPLACED IAW MM 27-51-13.

Part: CARRIAGE — CORRODED (LT FLAP) · airframe 54,591 hrs · 43,038 cycles

INSPECTION TYPE:C+SI, NR 2 CARRIAGE ON LEFT O/B FLAP HAS CORROSION IN SPINDLE BORE. REPLACED CARRIAGE IAW MM 27-51-13.

Part: LINK — CORRODED (NR6 SPOILER) · airframe 54,591 hrs · 43,038 cycles

INSPECTION TYPE:C+SI, SURFACE CORROSION ON NR 6 SPOILER ACTUATING LINKAGE. REPLACED ACTUATOR LINKAGE IAW MM 27-61-01.

Part: PRESSURE PANEL — CRACKED (MLG WW) · airframe 54,591 hrs · 43,038 cycles

INSPECTION TYPE:C+SI, CRACK IN LT MLG WHEEL WELL PRESSURE FLOOR AT 930 AFT REINFORCING BEAM AT LBL 54. REPAIRED IAW B727-5310-0460 APPENDIX C.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 54,591 hrs · 43,038 cycles

INSPECTION TYPE:C+SI, CRACK IN LT WHEEL WELL PRESSURE FLOOR AT BS 940 AFT REINFORCING BEAM AT LBL 30. REPAIRED IAW EOB727-5310-0460 APPENDIX C.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 54,591 hrs · 43,038 cycles

INSPECTION TYPE:C+SI, CRACK IN RT MLG WHEEL WELL PRESSURE WEB AT BS 930 FWD REINFORCING BEAM AT RBL 44. CRACK STOP DRILLED IAW SRM 51-10-1 AND EO APPENDIX C, REPAIRED IAW EO B727-5310-0460.

Part: FRAME — CRACKED (ENTRY DOOR) · airframe 54,591 hrs · 43,038 cycles

INSPECTION TYPE:C+SI, CRACK IN TOP FRAME (AFT) OF FWD ENTRY DOOR TOP FRAME. REPLACED IAW SRM 51-30-2 WITH REFERENCE TO BOEING DWG 50 -7954.

Part: BEAM — CRACKED (FUSELAGE) · airframe 54,591 hrs · 43,038 cycles

INSPECTION TYPE:C+SI, APB 1183 VERT BEAM AT LBL 26.83 HAS A CRACK RUNNING FROM FLANGE LIGHTENING HOLE AT WL 258. REPAIRED PER APPENDIX D OF EO B727-5311-0651 & BOEING DRWG 65C34406.

Part: INDICATOR — INOPERATIVE (NR 1 ENG FIRE)

INSPECTION TYPE:PFLT, NR 1 ENG A FIRE LIGHT WILL NOT TEST. ACCOMPLISH WAN 558661/REF DMI M 208397, NR 1 ENGINE B LOOP FIRE TEST INOP, TECH RECOMMENDS CHECK RESISTANCE BETWEEN PINS E AND G RESISTANCE CHECKED BETWEEN PINS E AND G, FOUND TO BE WITHIN LIMITS IAW MM 26-11-02. SYSTEM OPS CHECK, PERFORMED FOUND SATIS. THIS CLOSES DMI 208397.

Part: BATTERY — INOPERATIVE (CABIN)

INSPECTION TYPE:PFLT EMERGENCY LIGHTS WILL NOT TEST. BATTERY CHARGED.

Part: INDICATOR — FAILED (HORIZON)

INSPECTION TYPE:N/A, DURING FLIGHT F/O EADI SCREEN WENT BLANK FOR APPROX 5 SEC FOLLOWED BY LOUD POP SOUND AND SPARKS VISIBLE DROPPING BEHIND PANEL AT F/O RUDDER PEDDLES. EADI SCREEN RETURNED TO NORMAL AND ACURID SMELL OF SMOKE IN COCKPIT FOLLOWED. PULLED EADI AND EHSI C/B''S ON F/O SIDE AS PRECAUTIONARY. INSPECTED AND NO SIGNS OF BURNING, ARCHING, DAMAGE. REMOVED AND REPLACED F/O''S EADI, EHSI AND NR 2 DPUA AS PRECAUTIONARY.

Part: SKIN — CRACKED (RT WING TIP)

FOUND CRACK ON BOTTOM SIDE OF RIGHT WING TIP. REMOVED AND REPLACED RT WING TIP P/N ON 65-72719-108 S/N ON 1910.

Part: BRACKET — CRACKED (BS 970)

INSPECTION TYPE:C, AFT CARGO BAY, ANGLE BRACKET CRACKED AT BS 970 LBL 20 ATTACHING INTERCOSTAL TO FRAME. FABRICATED REPAIR ANGLE IAW SRM 51-20-01. RE-INSTALLED BRACKET IAW SRM 51-30-2.

Part: CHANNEL — CORRODED (BS 570)

INSPECTION TYPE:C, LIGHT SURFACE CORROSION ON FLOOR SUPPORT CHANNEL BS 570 RBL 10. CORROSION REMOVED AND FOUND TO BE BEYOND LIMITS IAW 53-10-1, CHANNEL REPAIRED IAW SRM 53-10-5 FIG 4.

Part: HINGE — CRACKED (CARGO DOOR)

INSPECTION TYPE:C, FWD HINGE ON AFT CARGO DOOR CRACKED. NEW HINGE INSTALLED IAW MM 52-31-101.

Part: FLOORBEAM — CORRODED (BS 1130)

INSPECTION TYPE:C, FLOORBEAM LWR CHORD BS 1130 RBL 20-24 HAD CORROSION. CORROSION REMOVED IAW SRM 51-10-6 FIG 3, FOUND OUT OF LIMITS. AREA TRIMMED TO REMOVE CORROSION IAW SRM 51-10-6 FIG 3. REF SMRO EO 99-24-004 R1 UPS ENGINEERING FILE NR 727-53-2161.

Part: SKIN — CRACKED (NR 3 LE FLAP)

INSPECTION TYPE:C, NR 3 L/E FLAP ANTI-ICE SKIN CRACKED AT UPPER FASTENER 2ND SKIN PANEL I/B OF ACTUATOR. REPAIRED IAW EO B727-5750-3082.

Part: STRINGER — CRACKED (BS 938)

INSPECTION TYPE:C, CRACK AT STRINGER 18A LT BS 938. CARRIED OUT REPAIR TO DAMAGED STR IAW SMRO EO 99-24-006 UPS ENGINEERING FILE NR 727-53-2161.

Part: SKIN — CRACKED (NR 3 LE FLAP)

INSPECTION TYPE:C, NR 3 LE FLAP ANTI-ICE SKIN CRACKED AT MIDDLE O/B FASTENER 2ND SKIN PANEL I/B OF ACTUATOR. REPAIRED IAW EO B727-5750-3082.

Part: SKIN — CRACKED (RT ELEVATOR)

INSPECTION TYPE:C, RT ELEVATOR CRACK ON SKIN BONDED STIFFENER AT STA 204. CRACK STOP DRILLED IAW SRM 51-10-1, REPAIRED IAW EO 99-24-002 UPS ENGINEERING FILE NR 727-55-0397.

Part: SKIN — CRACKED (RT TE FOREFLAP)

INSPECTION TYPE:C, RT INBOARD FORE FLAP, CRACK AND CHAFING AT I/B LEADING EDGE, AREA FORWARD OF FOREFLAP INBOARD ATTACHMENT POINT. REPAIR CARRIED OUT IAW SRM 57-50-4.

Part: SKIN — CRACKED (BS 1303)

INSPECTION TYPE:C, CRACK ON BOX SKIN, LT SIDE OF AIRSTAIRS AT LIGHTENING HOLE AT STA 1303. REPAIRED IAW 51-40-2.

Part: SKIN — CRACKED (BS 1263-1273)

INSPECTION TYPE:C, CRACK ON STRUCTURE UNDER AIRSTAIRS ACTUATOR STA 1263 TO STA 1273. CRACK STOP DRILLED IAW 51-10-1. REPAIRED IAW EOB727-5310-1239E SECTION 3.

Part: BULKHEAD FORGING — CORRODED (BS 740)

INSPECTION TYPE:C, CORROSION ON LT BS 740 BULKHEAD FORGING BETWEEN STR 23L AND STR 24L. FITTING REPLACED IAW EO B727-5310-7477-E.

Part: BULKHEAD FORGING — CORRODED (BS 740)

INSPECTION TYPE:C, CORROSION ON RT SIDE BS 740 BULKHEAD FORGING BETWEEN STR 23R AND STR 24R. FITTING REPLACED IAW UPS EO B727-5310-7477-E & SRS EO 99-24-003 ENGINEERING FILE NR 727-53-2159.

Part: LIGHT — INOP (COCKPIT)

EMERGENCY LIGHT AT FWD ENTRY DOOR AND COCKPIT INOP. BATTERIES REPLACED, OP CHECKS OK IAW MM 33-50-00.

Part: TRACK — CRACKED (TE FLAP)

INSPECTION TYPE-AD, FLAP TRACK NR 8 CRACKED AT TIP. FLAP TRACK REPLACED IAW MM 57-51-31.

Part: FLAP TRACK — CRACKED (TE FLAP)

INSPECTION TYPE-N/A, FLAP TRACK NR 8 CRACKED AT TIP. ALL FERRY FLIGHT PROCEDURES HAVE BEEN ACCOMPL. ISSUED DMI NR 167087. FLAP TRACK REPLACED AND DMI NR 167087 WAS CLEARED.

Part: LIGHT — INOP (PAX DOOR)

INSPECTION TYPE-N/A, EXIT LIGHT OVER FWD ENTRY DOOR INOP. REPLACED EMERGENCY EXIT LIGHT ASSY, OPS CKD OK.

Part: FITTING — CORRODED (RT MLG)

INSPECTION TYPE-C, FITTING IN REAR SPAR OF RIGHT HAND WING FOR ATTACHING RT MLG FWD TRUNNION BEARING SUPPORT HAS EVIDENCE OF CORROSION. BEARING SUPPORT FITTING ATTACH FITTING REPLACED PER DRAWING 65-19297.

Part: FITTING — CORRODED (RT MLG)

INSPECTION TYPE-C, RIGHT HAND MLG FWD TRUNNION BEARING SUPPORT FITTING HAS CORROSION ON INNER AND OUTER LUGS THAT CONTACT REAR SPAR FITTING BEARING. SUPPORT FITTING REPLACED IAW MM 32-11-51.

Part: TRUNNION FITTING — CORRODED (NLG)

INSPECTION TYPE-C, CORROSION ON TRUNNION FITTING ON RIGHT HAND SIDE FOR NOSE LANDING GEAR. CORROSION REMOVED AND AREA REPROTECTED PER SRM 53-40-1 FIG 2.

Part: FITTING — CORRODED (WS 224.5)

INSPECTION TYPE-C, EXCESSIVE CORROSION ON NR 4 FLAP TRACK, WING ATTACH FITTING. BUSHING MANUFACTURED AND THEN INSTALLED PER OHM 57-40-01. FITTING THEN REINSTALLED PER OHM 20-50-01.

Part: FITTING — CORRODED (NLG)

INSPECTION TYPE-C, CORROSION ON LEFT HAND TRUNNION FITTING FOR NOSE LANDING GEAR. CORROSION REMOVED AND AREA REPROTECTED PER SRM 53-40-1 FIG 2.

Part: FITTING — CORRODED (LT MLG)

INSPECTION TYPE-C, CORROSION ON LEFT HAND FWD TRUNNION BEARING SUPPORT ATTACH FITTING ON REAR SPAR. BEARING SUPPORT FITTING REPLACED IAW DRAWING 65-19297.

Part: FITTING — CORRODED (WS 224.5)

INSPECTION TYPE-C, EXCESSIVE CORROSION ON NR 5 FLAP TRACK ON WING ATTACH FITTING. BUSHING MANUFACTURED AND THEN INSTALLED PER OHM 57-40-01. FITTING THEN REINSTALLED PER OHM 20-50-01.

Part: FITTING — CORRODED (RT AILERON)

INSPECTION TYPE:C, RIGHT OUTBOARD AILERON PUSHROD ATTACH FITTING ON AILERON HAS SURFACE CORROSION AROUND LUG HOLES, FITTING REPLACED IAW DRAWING 65-21766.

Part: WEB — CRACKED (BS 1381.5)

INSPECTION TYPE:C, CRACK ON WEB ABOVE NR 2 ENGINE HORIZONTAL FIREWALL, RT SIDE AT STATION 1381.5. WEB FABRICATED AND FITTED IAW DRAWING 65-17555.

Part: SKIN — CRACKED (BS 1245)

INSPECTION TYPE:C, CRACK ON SKIN, AFT ENTRY STAIRS CENTER LINE APPROX BS 1245. REPAIR CARRIED OUT IAW SRM 53-10-2 FIGURE 3.

Part: FRAME — CRACKED (CARGO DOOR)

INSPECTION TYPE-B, SUSPECT CRACK ON AFT DOOR FRAME INBOARD RADIUS AT NR 1 FWD DOOR STOP. FRAME WAS REPLACED IAW DWG 65-18625 USING FRAME 65-18625-86.

Part: FRAME — CRACKED (CARGO DOOR)

INSPECTION TYPE-B SUSPECT CRACK ON AFT CARGO DOOR FRAME OUTBOARD RADIUS AT NR 5 AFT DOOR STOP. FRAME REPLACED IAW DRAWING 658625 USING FRAME 65-18625-99.

Part: RIB — CRACKED (WS 760)

INSPECTION TYPE-C, A PREVIOUS REPAIR WAS DISCOVERED TO THE RBL 70.5 RIB CHORD AT 135 760. HOWEVER, A CRACK HAD PROGRESSED SINCE THE ORIGINAL REPAIR INSTALLATION. REPAIR PER CARRIED OUT PER SB727-53-0112 (UPS EO 7275710-1271) WITH DEVIATIONS OUTLINED IN SRS EO 96-30-016.

Part: BODY JOINT — CORRODED (BS 360)

INSPECTION TYPE-C, BOLTS IN PRODUCTION JOINT AT BS 360 FOUND CORRODED DURING STRUCTURAL SAMPLE BELOW STR 21L AND 21R. BOLTS REPLACED AS REQUIRED BETWEEN STR 21L AND 21R AT BS 360 AND TORQUED IAW MM 553-11-00 PG 601, CRACK IN HOLE AT BS 360 O/B OF STR 28R REPAIRED IAW SRS EO 96-30-005.

Part: VERT STRINGER — CRACKED (WS 686.5)

INSPECTION TYPE-C, VERT STRINGER FOUND CRACKED AT STR 13 TO 14 AT WS 686.5 LT. REPAIRED PER UPS EO B727-5710-0314-F.

Part: RIBS — CRACKED (WS 656.5L)

INSPECTION TYPE-C, TWO HYDROPRESSED RIBS WERE FOUND CRACKED. CRACKED RIBS REPLACED WITH BUILT-UP RIBS, PER ABOVE EO O/S FASTENERS INSTALLED PER SRS EO 96-30-012.

Part: SKIN — CORRODED (BS 1183-1080)

INSPECTION TYPE-C, CORROSION AND DISBOND ON FUSELAGE SKIN AND DOUBLER BS 1183 TO 1080 BETWEEN S20R AND 26R. SKIN PANEL DERIVETED IAW SRM 51-30-02. SKIN PANEL AND DOUBLER INSPECTED USING LFEC IAW B727 NDT MANUAL, PART 6 51-00-00 FIG 5, MATERIAL LOSS OF 10 TO 30 PERCENT INDICATED ALONG LENGTH INSPECTED. DOUBLER FOUND TO BE BOTH CORRODED AND DISBONDED SKIN PANEL REPAIRED IAW SRS EO 96-30-13.

Part: CLAMP RINGS — CORRODED (LT/RT FUEL DOORS)

INSPECTION TYPE-C, FRETTING SURFACE CORROION ON LT AND RT WING FUEL TANK DOOR CLAMP RINGS. FUEL TANK DOOR CLAMP RINGS REPLACED IAW MM 28-11.

Part: STRINGER — CORRODED (BS 460-480)

INSPECTION TYPE-D, STR 21R BS 460 TO 480. REPAIRED PER SRM 53-10-3.

Part: DOUBLER — CRACKED (PAX DOOR CUTOUT)

INSPECTION TYPE-C, FWD ENTRY DOOR CUTOUT HAS DOUBLER CRACK AT TOP FWD CORNER. REPAIR CARRIED OUT IAW EO B727-5330-1460 APPENDIX OPTION 1.

Part: FRAME — CORRODED (BS 600)

INSPECTION TYPE-C, CORROSION ON FRAME BS 600 ADJACENT TO STR 26L. CORROSION REMOVED AND FOUND TO BE OUT OF LIMITS IAW SRM 51-10-01. FRAME REPAIRED IAW SRM 53-10-4 FIG 1.

Part: SKIN — CORRODED (LT AILERON)

INSPECTION TYPE-C, LT O/B AILERON HAS SKIN BULGE ON TOP SKIN I/B END. RIVETS REMOVED FROM AILERON SKIN I/B END IAW SRM 51-30-2, AILERON HINGE ASSM FOUND CORRODED. REPLACED HINGE ASSM IAW DWG 65-2176 AILERON RIGGED IAW 27-10-00.

Part: SHEAR TIE — CORRODED (BS 328)

INSPECTION TYPE-D, SHEAR TIE CORRODED AND CRACKED ON ST 22L AT BS 328 LT SIDE. SHEAR TIE REPLACED SRM 53-10-2.

Part: WEB — CRACKED (BS 292)

INSPECTION TYPE-C, CRACK IN NOSE WHEEL WELL WEB, BS 292 RBL 30 WL 180 APPROX. HFEC CARRIED OUT TO CONFIRM CONTAINMENT OF CRACK BY STOPDRILL IAW B727 NDT MANUAL PART 6, 51-00-00 FIG 4, NO DEFECTS FOUND. REPAIR TO WEB IN NOSE WHEEL WELL CARRIED OUT IAW SRS EO 96-30-002.

Part: SKIN — CORRODED (BS 1085)

INSPECTION TYPE-C, CORROSION ON FUSELAGE SKIN BS 1085 BETWEEN STR 12L AND BL AREA PAINT STRIPPED IAW MM 51-20-1, AREA REINSPECTED FOUND TO BE CORRODED AND DAMAGED. SKIN AT BS 1080 TO 1160 BETWEEN S10L & S14L DERIVETED IAW SRM 51-30-2, SKIN PANEL REPAIRED IAW SRS EO 96-30-004.

Part: BOTTLE PIN — CORRODED (LT WING)

INSPECTION TYPE-C, SLIGHT SURFACE CORROSION ON INNER SURFACE OF LT REAR BOTTLE PIN. NEW BOTTLE PIN INSTALLED IAW MM 57-41-01.

Part: SKIN — DELAMINATION (BS 1090-1110)

INSPECTION TYPE-C, DELAMINATION AT BS 1090 TO 1110 BETWEEN STR 11 AND 12 RT SIDE. FOKKER BOND INSP CARRIED OUT ON TWO SUSPECT AREAS OF METAL TO METAL DISBOND IAW B727 NDT MANUAL PART 4 51-40-00 FIG 1. BOTH AREAS INDICATE DISBONDING SKIN PANEL AND DOUBLER INSPECTED. SKIN PANEL REPAIRED IAW SRS EO 96-30-008.

Part: SKIN — CORRODED (BS 1183)

INSPECTION TYPE-C, CORROSION BETWEEN FUSELAGE SKIN AND FRAME AT BS 1183 BETWEEN 58L AND 59L. AREA PAINT STRIPPED IAW MM 51-20-1, FASTENERS REMOVED IAW SRM 51-30- 2, AREA BETWEEN BS 1183 AND 1166 BETWEEN 510L AND 58L INSPECTED IAW B7 27 NDT MANUAL 51-00-00 FIG 5. INTERNAL FOUND DISBONDED WITH SURFACE CORROSION ON BOTH SKIN AND DOUBLER. AREA REPAIRED IAW SRS EO 96-30-010.

Part: SKIN — CORRODED (BS 1183)

INSPECTION TYPE-C, CORROSION BETWEEN FUSELAGE SKIN AND S17L, BS 1183. REMOVED SKIN PANEL, REPAIRED IAW SRS EO 96-30-015.

Part: BATTERY — DISCHARGED (CABIN)

WHILE ON THE GROUND IN CGN, MAINTENANCE FOUND EMERGENCY LIGHT DOES NOT COME ON WHEN SWITCHED TO ON. MAINTENANCE REPLACED THE BATTERIES, FUNCTIONAL CHECKS GOOD.

Part: KEEL WEB — CORRODED (BS 788-828)

WHILE IN SHANNON, IRELAND FOR C-CHECK, MAINTENANCE FOUND CORROSION ON RT KEEL BEAM WEB AT BS 790-828 (INNER AND OUTER). OUTER WEB REPAIRED PER SRM 51-40-2, FIGURE 1. INNER WEB REPAIRED PER SRS E.O. 95-10-001.

Part: SEAT TRACK — CRACKED (BS 500-520)

WHILE IN SHANNON, IRELAND FOR C-CHECK, MAINTENANCE FOUND CRACKED SEAT TRACK BBL 45.5 LT, BS 500 THROUGH BS 520. SEAT TRACK REPLACED PER SRM 53-10-5, FIG. 7.

Part: CONE BOLT — GOUGED (NR 2 ENG)

WHILE IN SHANNON, IRELAND FOR C-CHECK, MAINTENANCE FOUND NR 2 ENGINE, LT FWD MOUNT CONE BOLT NOT SITTING PROPERLY. NEW CONE BOLT INSTALLED AND INSPECTION CARRIED OUT PER E.O. 95-10-003.

Part: SKIN — CORRODED (BS 1080)

WHILE IN SHANNON, IRELAND FOR C-CHECK, MAINTENANCE FOUND BULGE ON BUTT JOINT BS 1080 STR 16 RT. REPAIRED PER SRM 53-30-3 - FIGURE 3.A.J. SHEET 3.