N947UP

Part: SLIDE — OUT OF LIMITS (COCKPIT)

EMERGENCY ESCAPE SLIDE PRESSURE IS BELOW LIMITS. REMOVED EMERGENCY ESCAPE SLIDE PER MM 25-60-15.

Part: BRACKET — CRACKED (BULKHEAD) · airframe 64,253 hrs · 47,110 cycles

INSPECTION TYPE: C, ON REMOVAL OF SECTION OF BULKHEAD AT BS 178, SUPPORT BRACKET FOR PNEUMATIC BOTTLE FOUND CRACKED. REMOVED SUPPORT BRACKET FOR PNEUMATIC BRAKE BOTTLE IAW SRM 51-30-2. FABRICATED SUPPORT BRACKET IAW DRW60-6962 AND SRM 51-20-1 FIG 7, INSTALLED NEW FAB'D SUPPORT BRACKET FOR PNEUMATIC BRAKE BOTTLE IAW SRM 51-2 30-2.

Part: FRAME — CORRODED (NR 2 TANK) · airframe 64,253 hrs · 47,110 cycles

INSPECTION TYPE: C, EVIDENCE OF CORROSION ON CENTER SECTION OF NR 2 TANK UPPER CHORD AT RBL 63.5 APPROX. ON INVESTIGATION CORROSION WAS FOUND TO BE EXTENSIVE. UPPER CHORD FWD SPAR CENTER SECTION REMOVED PER SRM 51-30-2, NEW CHORD SECTION CUT TO ACC INSTL IAW DRG LOR-444. REPAIR & INSTALATION CARRIED OUT IAW AAAE EO 2004-068-007.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 64,253 hrs · 47,110 cycles

INSPECTION TYPE: C, DURING REMOVAL OF BS 740 FITTING (LEFT) THE INTERCOSTAL LOCATED BETWEEN STR 20 & STR 21 FOUND TO BE CRACKED. FABRICATED NEW INTERCOSTAL IAW SRM 51-20-1 FIG 7. INSTALLED INTERCOSTAL IAW SRM 51-30-02 AND EO B727-5310-7477-E.

Part: PANEL — DEBONDED (LT WING SPOILER) · airframe 64,253 hrs · 47,110 cycles

INSPECTION TYPE: C, NR 5 SPOILER PANEL DISBOND (MINOR) LWR I/B SURFACE AT I/B CORNER FWD DOUBLER. ON INVESTIGATION FURTHER DISBOND FOUND ON UPPER SURFACE. SPOILER REPAIRED IAW SRM 51-40-20. NR 5 SPOILER PANEL ADJ/TEST CARRIED OUT PER MM 27-61-00/501 PARA 6H THROUGH 6M, 6O, 6P & Q.

Part: FAIRING — CRACKED (NR 7 FLAP TRACK) · airframe 64,253 hrs · 47,110 cycles

INSPECTION TYPE: C, 7 FLAP TRACK SAILBOAT FAIRING HAS SUSPECT CRACK TO OUTER SKIN AT RIB ATTACH POINT (INDICATED ON SKIN). HFEC CONFIRMED CRACK AND MARKED END. REPAIR CARRIED OUT IAW SRM 51-40-02 FIG 1.

Part: SKIN — DEBONDED (LT WING TE FLAP) · airframe 64,253 hrs · 47,110 cycles

INSPECTION TYPE: C, LEFT I/B FOREFLAP I/B END & UPPER SURFACE HAS DISBOND. REPAIRED IAW SRM 51-40-20. DURING OPS CHECKS THE O/B END WAS CONTACTING THE MIDFLAP AND BINDING. FOREFLAP RESKIMMED BUT DID NOT SOLVE PROBLEM. INSTALLED FOREFLAP REMOVED FROM A/C N945UP FOR TROUBLESHOOTING PER NRC 725261, NO BINDING EXPERIENCED.

Part: SEAT TRACK — CORRODED (COCKPIT) · airframe 64,253 hrs · 47,110 cycles

INSPECTION TYPE: C, O/B SEAT TRACK SECTION FWD OF BS 740 LEFT SIDE CORRODED AT BS 740 & 751 ON HORIZONTAL FLANGE AND FWD END OF FLANGE FOUND BENDED BEYOND CLEANUP LIMITS. SEAT TRACK FABRICATED IAW SRM 51-20-01 & SRM 53-10-02. SEAT TRACK ALODINED AND PRIMED IAW SRM 51-10-02. SEAT TRACK INSTALLED IAW SRM 51-30-02.

Part: FRAME — CRACKED (NLG) · airframe 64,253 hrs · 47,110 cycles

INSPECTION TYPE: C, FRAME CRACKED AT BS 323 AT LOWER LOBE WALKWAY LEVEL, LEFT SIDE OF LOWER NOSE COMPARTMENT PRESSURE WEB AND FRAME REMOVED IAW SRM 51-30-2. REPLACEMENT FRAME FABRICATED IAW SRM 51-20-1. FRAME REPROTECTED IAW 51-10-02. FRAME CUT AND INSTALLED IAW SRM 51-30-2. REPAIR SPLICE FABRICATED IAW 51- 40-3 FIG 1. SPLICE PROTECTED IAW 51-10-02 AND INSTALLED IAW SRM 51- 30-2. FASTENERS INSTALLED IAW SRM 51-30-2.

Part: SKIN — CORRODED (FUSELAGE) · airframe 64,253 hrs · 47,110 cycles

INSPECTION TYPE:C, CORROSION ON SKIN NEXT TO FASTENER BS 470 S19R. FASTENER REMOVED FROM SUSPECT AREA IAW SRM 51-30-02. CORROSION FOUND TO BE OUTSIDE LIMITS IAW SRM 53-30-1. CORRODED SKIN TRIMMED OUT IAW SRM 53-30-3 FIG 14. AFTER TRIM OUT CORROSION FOUND ON LOWER SKIN, CORROSION REMOVED IAW SRM 51-10-06. LOWER SKIN TRIMMED IAW SRM 53-30-3, REPAIR DOUBLERS FABRICATED AND INSTALLED IAW SRM 53-30-3.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,253 hrs · 47,110 cycles

INSPECTION TYPE: C, SUSPECT CRACK ON FWD RADIUS OF WING ANTI-ICE SCANNING LIGHT ON LT SIDE AT BS 680-700 APPROX & BETWEEN STR 14-15 LT. HFEC CARRIED OUT AND CRACK CONFIRMED AND END MARKED. REPAIR CARRIED OUT IAW AAAE EO 2004-068-001R1.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,253 hrs · 47,110 cycles

INSPECTION TYPE:C, SUSPECT CRACK ON SKIN AT BS 253 S9R, AFT OF NR 3 RT COCKPIT WINDOW CUTOUT. HFEC CARRIED OUT ON THE ABOVE AREA IAW NDT MANUAL 51-00-00 PT 6 FIG 4. FASTENERS REMOVED IAW SRM 51-30-02. DAMAGED AREA REMOVED AND CUT LINE TRIMMED IAW SRM 53-30-3 FIG 29. FABRICATED EXTERNAL DOUBLER AND FILLER PARTS IAW SRM 53-30-3 FIG 29. INSTALLED REPAIR AND FASTENERS IAW SRM 51-30-02 AND 53-30-3 FIG 29.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,253 hrs · 47,110 cycles

INSPECTION TYPE:C, SUSPECT CRACK ON SKIN AT BS 253 S9L AFT OF NR 3 LT COCKPIT WINDOW CUTOUT. HFEC CARRIED OUT, CRACK CONFIRMED AND END MARKED. REPAIR CARRIED OUT IAW SRM 53-30-3 FIGURE 29.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 64,253 hrs · 47,110 cycles

INSPECTION TYPE:C, INSPECT CRACK ON BS 1183 BULKHEAD, SUSPECT CRACK IS LOCATED ON AFT SIDE OF BULKHEAD, WL 175 APPROX LBL 20. HFEC INSPECTION CARRIED OUT & CRACKS CONFIRMED AND ENDS MARKED. FASTENERS REMOVED AND CRACKS TRIMMED OUT IAW SRM 51-10-6, REPAIR CARRIED OUT IAW AAAE EO 2004-068-003 R1.

Part: BULKHEAD — CRACKED (FUSLEAGE) · airframe 64,253 hrs · 47,110 cycles

INSPECTION TYPE: C, CRACK ON FWD PRESSURE BULKHEAD AT WL 198 RBL 02. HFEC CARRIED, CRACK CONFIRMED AND END MARKED. REPAIR CARRIED OUT USING REPAIR KIT 65C36289-1. REPAIR CARRIED OUT IAW DRG 65C36289 & SRM 51-30-02.

Part: STOP FITTING — CRACKED (FWD CARGO DOOR) · airframe 64,253 hrs · 47,110 cycles

INSPECTION TYPE: C, FWD CARGO DOOR CUTOUT, NR 4 FWD STOP PAD IS CRACKED. STOP PAD LOCATED ON FWD EDGE FRAME OF DOOR CUTOUT IN FUSELAGE, REPAIR IN IAW EO B727-5230-0032 NOT SUITABLE FOR THIS STOP FITTING. REPLACEMENT OF STOP FITTING CARRIED OUT IAW BOEING DRW 65-20723 AND SRM 51-30-02. FWD CARGO DOOR RIG GAPS CHECKED AND FOUND SATISFACTORY IAW 52-31-01.

Part: DOOR — CRACKED (THRUST REVERSER) · airframe 64,253 hrs · 47,110 cycles

INSPECTION TYPE: C, ENGINE NR 1 THRUST REVERSER UPPER DOOR, INNER LWR SKIN HAS SUSPECT CRACK AT OUTBOARD TOP CORNER. HFEC INSPECTION CARRIED OUT IAW B727 NDTM PART 6 51-00-00 FIG 4. CRACK CONFIRMED AND MARKED. CRACK REMOVED IAW SRM 78-30-01. HFEC INSPECTION CARRIED OUT. NO DEFECTS FOUND. REPAIR DOUBLER FABRICATED IAW SRM SUPP 78-30-01. DYE PENETRANT INSPECTION CARRIED OUT. NO DEFECTS FOUND.

Part: DOOR FRAME — CRACKED (AFT CARGO BAY) · airframe 64,253 hrs · 47,110 cycles

INSPECTION TYPE:C, SUSPECT CRACK ON AFT CARGO DOOR FRAME SKIN FLANGE RADIUS OF NR 3 FWD STOP FITTING (REF DETAIL I FIGURE 1 FLANGE 1 OF EO SECTION B-B). HFEC CONFIRMED CRACK AND MARKED END. REMOVED CARGO DOOR BALANCE MECHANISM IAW MM 52-31-53. REMOVED AFT CARGO DOOR FRAME IAW SRM 51-30-02. FRAMES INSTALLED IAW DRG 65C16422 & SRM 51-30-2. CARGO DOOR BALANCE MECHANISM REFITTED IAW MM 52-31-53.

Part: SKIN — CRACKED (AFT CARGO DOOR) · airframe 64,253 hrs · 47,110 cycles

INSPECTION TYPE:C SUSPECT CRACK AFT CARGO DOOR FRAME SKIN FLANGE RADIUS OF NR 2 FWD STOP FITTING (FWD), REF FIG 1 FLAG NOTE 1 OF EO SECTION B-B DISPLACED DOOR SEAL IAW MM 51-30-00. HFEC CARRIED OUT IAW NDT MANUAL 51-00-00 FIG 4. RESULT: CRACK CONFIRMED ENDS MARKED. DUE TO CLOSE PROXIMITY OF CRACKS, THE FRAMES WILL BE REPLACED. FRAMES ORDERED. REMOVED AFT CARGO DOOR FRAME IAW 51-30-02. FRAME INSTALLED ON AFT CARGO DOOR IAW DRW 65C16422. OPERATIONAL AND LEAK CHECK OF DOOR C/W.

Part: WEB — CRACKED (NR 2 ENG SUPPORT) · airframe 64,253 hrs · 47,110 cycles

INSPECTION TYPE:C, CENTER ENGINE SUPPORT STRUCTURE, WEB CRACKED ON RT SIDE AT BS 1387. WEB REMOVED IAW SRM 51-30-02. WEB FABRICATED PER DRAWING 65-17555. WEB INSTALLED PER DRAWING 65-17555.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 64,253 hrs · 47,110 cycles

INSPECTION TYPE: C, RIGHT WING O/B AFT FLAP HONEYCOMB FILLER DELAMINATED AT I/B END. AFT FLAP FITTINGS REMOVED FROM UNSERVICEABLE FLAP AND FITTED TO REPLACEMENT AFT FLAP IAW OHM 20-50-01 AND OHM 57-52-11. FLAP ASSY REPLACED IAW MM 27-51-12 AFT FLAP ADJUSTED IAW MM 27-51-12 PARA 5 SUB PARA 4A-G. INCLUSIVE ECCENTRIC ROLLERS ADJUSTED AS REQUIRED & SATISFIED IAW MM 27-51-00.

Part: SKIN — CRACKED (LT WING TE FLAP) · airframe 64,253 hrs · 47,110 cycles

INSPECTION TYPE: C, CRACK ON I/B MID FLAP LOWER T/E SKIN AT I/B AFT FLAP ACTUATING ROD CUTOUT O/B AFT CORNER (LT). HFEC CONFIRMED CRACK AND MARKED END. DAMAGED AREA TRIMMED OUT IAW SRM 51-10-1. REPAIR CARRIED OUT IAW AAAE EO 2004-068-006.

Part: WEB — CRACKED (TORQUE BOX) · airframe 64,253 hrs · 47,110 cycles

INSPECTION TYPE:C, CRACK EVIDENT AT LIGHTENING HOLE IN THE AFT ENTRY STAIRS AREA. CRACK LOCATED AT B-STA 1263 APPROX, LEFT SIDE OF TORQUE BOX VERTICAL WEB JUST OUTSIDE DOUBLER OF PREVIOUS REPAIR. CRACK STOP DRILLED PER SRM 51-10-1. HFEC INSPECTION CARRIED OUT AROUND STOP DRILL HOLE IAW B727 NDT M 51-00-00 FIG K. RESULT WAS THE CRACK WAS CONTAINED WITHIN STOP DRILL. AREA TRIMMED OUT WITHIN LIMITS IAW SRM 51-10-1. REMOVED DOUBLER FROM PREVIOUS REPAIR AND REPAIRED LIGHTENING HOLE IAW SRM 51-40-2.

Part: YOKE — MALFUNCTIONED (COCKPIT) · 47,110 cycles

INSPECTION TYPE: C, PERFORM A GVI OF CAPT & F/O CONTROL YOKES & ATTACHED LINKAGE, PAYING ATTENTION TO CORROSION, BINDING OR LOOSENESS OF BEARINGS. ROTATE EACH CONTROL WHEEL FULL TRAVEL LEFT & RIGHT CHECKING FOR ANY STIFFENESS, BINDING OR RATCHETING OF MOVEMENT. OPERATE AILERON TRIM FULL TRAVEL IN EACH DIRECTION CHECKING FOR BINDING & FRICTION. GVI CARRIED OUT IAW UPS GMM 4-3-1. FOUND SATISFACTORY. BACKLASH ON CAPT'S CONTROL WHEEL ADJUSTED IAW OHM27-16-01 STEP 12P502 & RATCHETING FOUND REMOVED. AILERON TRIM & CENTERING SPRINGS REPLACED & ADJUSTED TO MAX. LIMIT PER OHM 27-11-01. ALL PULLEYS & LINKAGES LUBED IAW MM. TRIM SYS CHECKED & NO LAGGING FOUND. CONTROL COLUMNS RECONN.

Part: LONGERON — CRACKED (NR 2 ENGINE COWL) · airframe 64,253 hrs · 47,110 cycles

INSPECTION TYPE:C, ENGINE NR 2 LT FWD COWL UPPER LONGERON IS CRACKED AT ALIGNMENT PLATE. REMOVED LT FWD COWL UPPER LONGERON IAW SRM 51-30-02. FABRICATED NEW LONGERON PER DRAWING QF7122130-1AND SRM 54-10-06. INSTALLED NEW LONGERON IAW SRM 57-30-02.

Part: SKIN — DEBONDED (AILERON TAB) · airframe 64,253 hrs · 47,110 cycles

INSPECTION TYPE:C, LEFT I/B AILERON TAB DISBOND AT AFT I/B CORNER O/B END. AILERON TAB REPAIRED IAW SRM 51-40-20.

Part: ROD — CRACKED (RT IB AILERON)

INSPECTION TYPE: C, RIGHT INBOARD AILERON TAB SUSPECT CRACK ON TAB ACTUATING ROD AT AFT END. HFEC CARRIED OUT IAW NDT MANUAL 51-00-00 PT 6 FIG 4, CRACKS CONFIRMED. ACTUATING ROD REMOVED IAW 27-10-01. REPLACED AFT END OF ROD IAW SRM 51-30-02. REINSTALLED ACTUATING ROD IAW MM 27-10-01.

Part: SKIN — DELAMINATED (RT AILERON TAB)

INSPECTION TYPE: C, RIGHT OUTBOARD AILERON TAB DELAMINATED ON UPPER SKIN AT INBOARD END AND OUTBOARD END. AILERON TAB REMOVED IAW MM 27-10-19. DAMAGE REPAIRED IAW SRM 51-40-20, AILERON TAB REINSTALLED IAW MM 27-10-19.

Part: WEB — CRACKED (NR 2 KRUGER FLAP) · airframe 64,253 hrs · 47,110 cycles

INSPECTION TYPE:C, NR 2 KRUEGER FLAP ACTUATOR TRUNNION SUPPORT BOX LT WEB CRACKED. REMOVED LT WEB TO FACILITATE IN FABRICATION OF NEW ONE IAW SRM 51-30- 02. FABRICATED NEW LT WEB IAW DRAWING 65-16269 AND INSTALLED ON NR 2 KRUEGER FLAP ACTUATOR TRUNNION SUPPORT BOX LT IAW DRAWING 65-162 69.

Part: WEB — CRACKED (NR 6 KRUGER FLAP) · airframe 64,253 hrs · 47,110 cycles

INSPECTION TYPE: C, NR 6 KRUEGER FLAP ACTUATOR TRUNNION SUPPORT BOX L + R WEB CRACKED. REMOVED NR 6 KRUEGER FLAP ACTUATOR IAW MM 27-81-22. REMOVED BOTH CRACKED WEBS FOR FABRICATION IAW SRM 51-30-02. FABRICATED LT & RT WEBS AS PER DRAWING 65-16275. INSTALLED FABRICATED LT & RT WEBS IAW SRM 51-30-02 AND DRAWING 65-16275.

Part: ANGLE — CRACKED (FUSELAGE)

INSPECTION TYPE:C, SUSPECT CRACK ON ANGLE ON O/B SIDE OF LOWER LEG OF BS 870 FITTING IN LT MWW. CRACK FOUND IN ANGLE, ANGLE REMOVED IAW SRM 51-30-2. NEW ANGLE FABRICATED AND FITTED IAW SRM 51-20-1, SRM 51-30-2 AND DRG 65-16330.

Part: SUPPORT FITTING — CRACKED (MCD LATCH)

INSPECTION TYPE:C MAIN CARGO DOOR LATCH SUPPORT FITTING @ BS 612-90 FOUND CRACKED DURI NG INSPECTION FITTING REMOVED I.A.W. SRM 51-30-03 FITTING REPLACED I.A.W. EO B727-5310-0437

Part: SKIN — CRACKED (THURST REVERSER) · airframe 63,836 hrs · 46,760 cycles

INSPECTION TYPE: C, SUSPECT CRACK ON NR 3 ENG TR LWR DOOR INNER UPPER SKIN. NDT PERFORMED AND TWO CRACKS DETECTED AND ENDS MARKED. CRACKED ENDS TERMINATED BY STOP DRILLING WITH .1875 INCH HOLE DIAMETER SRM SUPP 78-30-01 FIG 201 PARA 2. DAMAGED RAMP SKIN REPAIR CARRIED OUT SRM SUPP 78-30-0 1 FIG 201 PARA 3 TO 6.

Part: DOUBLER — CORRODED (BS1180 S6L) · airframe 63,836 hrs · 46,760 cycles

INSPECTION TYPE:C SMALL AREA OF EXFOLIATION CORROSION FOUND ON FUSELAGE SKIN BS1180 JU ST ABOVE STR.6L REPAIR FILLER AND NEW DOUBLER TO INCORPORATE NEW AND EXISTING REPAIR FABRICATED IAW SRM 53-30-03 FIG.3A. REPAIR PARTS INSTALLED IAW SRM 53-30-03.

Part: FITTING — CRACKED (TAIL SKID) · airframe 63,836 hrs · 46,760 cycles

INSPECTION TYPE:C, RT UPPER TERMINAL FITTING IN TAIL SKID BAY CRACKED. REMOVED RT UPPER TERMINAL FITTING IAW SRM 51-30-02. NEW FITTING INSTALLED IAW DRAWING 65-25992.

Part: FITTING — CRACKED (TAIL SKID BAY) · airframe 63,836 hrs · 46,760 cycles

INSPECTION TYPE:C R/H LWR. TERMINAL FITTING IN TAIL SKID BAY CRACKED. REMOVED FITTING IAW SRM 51-30-02. FABRICATED NEW FITTING IAW DRAWING NO.65-85208 INSTALLED FABRICATED FITTING IAW DRAWING NO.65-25992

Part: SKIN — CORRODED (FUSELAGE) · airframe 63,836 hrs · 46,760 cycles

INSPECTION TYPE:C NDT HAVE MATERIAL LOSS INDICATION OF 15-20 PERCENT ON FUSELAGE SKIN FWD OF BUTT JOINT 360, STR 25R TO 27R. FASTENERS REMOVED FROM ABOVE AREA IAW SRM 51-30-2. TO FACILITATE CORROSION CLEAN UP EXISTING DOUBLER ABOVE STR 25R DE-RIVETED BETWEEN BS 328 AND BS 360 IAW SRM 51-30-2. NEW DOUBLER FABRICATED IAW BOEING DRG 65-18420. NEW DOUBLER FASTENED IAW SRM 51-30-2 AND BOEING DRG 65-18420.

Part: FITTING — CRACKED (TAIL SKID BAY) · airframe 63,836 hrs · 46,760 cycles

INSPECTION TYPE:C, LT LOWER TERMINAL FITTING IN TAIL SKID BAY CRACKED. REMOVED LWR TERMINAL FITTING IAW SRM 51-30-02. NEW FITTING INSTALLED IAW DRAWING 65-25992.

Part: RIB — CRACKED (BS870 S9 TO S12) · airframe 63,836 hrs · 46,760 cycles

INSPECTION TYPE:C DURING EDDY CURRENT INSP.OF R/H BS870 FORGING 2 CRACKS WERE FOUND ON FWD INTEGRAL RIB AT S11. REF EO.B727-5310-3057 APPDX.D FOR PARTIAL REPLACEMENT OF TERMINAL F ITTING S9 TO S12 AND APPDX.C STEP 1.

Part: FITTING — DAMAGED (FUSELAGE) · airframe 63,836 hrs · 46,760 cycles

INSPECTION TYPE: C, TO FACILITATE REPAIR TO BE 870 RT FITTING REMOVE FASTENERS X 20 BELOW PROPOSED CUT LINE AT S12 AND CARRY OUT NDT ON OPEN HOLES. FASTENERS REMOVED BELOW PROPOSED CUT LINE IAW SRM 51-30-02. FASTENER HOLE NDT INSP IAW NDTM H6 51-00-00 FIG 16 WITH NDF. FASTENER INSTALLATION IAW SMRO EO2003-005-003 + UPS EO B727-5310-182 54-A.

Part: WEB — CRACKED (NOSE WW L/H SIDE)

INSPECTION TYPE:C NLG WHEEL EWLL. L/H SIDE WALL AREA HAS CRACK APPROX. BS244 BELOW ACCESS PANEL 3122. REMOVED FASTENERS ON NLG L/H WHEEL WELL L/H SIDE WEB AREA APPROX BS 244 BELOW ACCESS PANEL 3122 AS PER SRM 51-30-02. CUT OUT DAMAGE AREA AS PER B727 SRM 51-40-02 APPROX 1"X3.5" HFEC PERFORMANCE AS PER B727 TPG 51-00-00 FIG 4. DOUBLER REPAIR INSTALLED AS PER B727 SRM 52-40-02.

Part: WEB — CRACKED (NLG WW BS 240)

INSPECTION TYPE:C NLG WHEEL WELL R/H SIDEWALL AREA HSA CRACK APPROX BS 240 BELOW ACCESS PANEL 3122. REMOVED FASTENERS AT R/H SIDE BS 240 CUT OUT DAMAGE AREA AS PER B727 SRM 51-40-02. PERFORMANCE NDT INSP AS PER B727 NDT 51-00-00 FIG 4. FOUND NO CRACK. INSTALLED REPAIR AT NOSE LANDING GEAR R/H WEB AREA BS 240 BELOW ACCESS PANEL AS PER B727 SRM 51-40-2.

Part: WEB — CRACKED (NLG WW BS 250)

INSPECTION TYPE:C NLG WHEEL WELL L/H SIDE WEB AREA HAS CRACK APPROX BS 250 BELOW ACCESS PANEL 3122 REMOVED FASTENERS ON NLG WHEEL WELL L/H SIDE WEB AREA APPROX BS250 BELOW ACCESS PANEL 3122 AS PER B727 SRM 51-30-2. CUT OUT DAMAGE AREA AS PER B727 SRM 51-40-2. PERFORMANCE HFEC INSP AS PER B727 NDT 31-00-00 FIG 4, NO CRACK FOUND. INSTALLED BOUBLER REPAIR AS PER B727 SRM 51-40-02.

Part: WEB — CRACKED (BS 1180)

INSPECTION TYPE:C MAIN CABIN LEFT AFT LAV, BS 1180 OUTBOARD FLOOR WEB CRACK. REMOVED AND REPLACED FLOOR WEB (DITCHING PANEL) AT BS 1180 LBL 55 REF B727 SRM 51-10-01 AND 51-30-02 MATERIAL USED 2024 T3/.020" ALUMINUM.

Part: DOOR — WILL NOT TEST (OXYGEN SYSTEM)

INSPECTION TYPE:N/A FWD FLIGHT ATTENDANT O2 DOOR WOULD NOT DEPLOY. PERFORMED E.O.727-3520-14476-A OPS CK FWD FLT ATTENDANTS O2 MASK DOOR DROP CK. OPS CKS GOOD

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE:N/A, EMERGENCY LIGHT IN LT GALLEY NEEDS BATTERY. INSTALLED NEW BATTERY PACK FOR LT GALLEY, OPS CHECKED GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE:N/A, EMERGENCY LIGHT NEED BATTERY PACK ROW 2 L AISLE LIGHT. INSTALLED NEW BATTERY ROW L AISLE.

Part: SKIN — DELAMINATED (LT WING)

INSPECTION TYPE:W/E LT WING UPPER T/E FIXED WING PANEL FWD OF GROUND SPOILERS, UPPER SKIN DELAMINATED (P/N 65-21655-475) REF IPC 57-30-00 FIG 10 ITEM 735 FOR LOCATION. REMOVED ICE AND WATER, PERFORMED A DETAILED INSPECTION (SRM 51-00-6) USING NDT TAP TEST. PANEL WAS DETERMINED TO BE NOT DELAMINATED.

Part: OXYGEN MASK — BROKEN (COCKPIT)

INSPECTION TYPE:PFLT, 2ND OBSERVERS 02 MASK HANGER IS BROKEN. *S/D* REMOVED AND REPLACED MASK HOLDER.

Part: DOOR — INOPERATIVE (MLG)

INSPECTION TYPE:N/A LANDING GEAR IN UP POSITION. REF WAN 547040. ***SUPPLEMENTAL***ACCOMPLISHED WAN 547040. PERFORMED A GENERAL CK OF NLG DOORS FOR SECURITY AND POSITION. NO FAULTS FOUND.

Part: DOUBLER — CORRODED (FUSELAGE)

INSPECTION TYPE:EO EVIDENCE OF CORROSION PRESENT AT LAP SEAM 4 RIGHT FROM BS950 TO BS 1080. INSTALLED REPAIR DOUBLER AT STR 4 RIGHT, BS 1053-1065 IN ACCORDANCE WITH SRM 53-30-3 FIG 5. REPLACED ALSO SECTION OF BONDED TEAR STRAP STR 3-5 RIGHT, STA 1070 IAW SRM 53-30-4.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE:N/A, GPU RAN OUT OF GAS, EMERGENCY EXIT LIGHTS LEFT IN ARMED POSITION. ALL EMERGENCY EXIT LIGHT BATTERIES DEAD. REMOVED AND REPLACED EMERGENCY EXIT BATTERY. OPS CK NORMAL.

Part: BATTERY PACK — INOPERATIVE (GALLEY)

INSPECTION TYPE:P/F, EMERGENCY EXIT LIGHT AT GALLEY CEILING AFT INOP. REMOVED AND REPLACED BATTERY PACK. OPS CK NORMAL.

Part: BATTERY PACK — INOPERATIVE (GALLEY)

INSPECTION TYPE:P/F, EMERGENCY EXIT LIGHT AT GALLEY RT SIDE INOP. REMOVED AND REPLACED BATTERY PACK. OPS CK NORMAL.

Part: BATTERY PACK — INOPERATIVE (GALLEY)

INSPECTION TYPE:P/F, EMERGENCY EXIT LIGHT AT GALLEY CEILING FWD INOP. REMOVED AND REPLACED BATTERY PACK. OPS CK NORMAL.

Part: SIGN — INOPERATIVE (CABIN)

RT GALLEY DOOR EMERGENCY EXIT SIGN INOPERATIVE. R&R IAW MM CH 33 50 00. OPS CK NORMAL.

Part: LIGHT — INOPERATIVE (OVERWING)

LT OVERWING EXIT & OVERHEAD EXIT SIGN INOPERATIVE. R&R BOTH IAW MM CH 33 50 00 OPS CK NORMAL.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,069 hrs · 45,519 cycles

INSPECTION TYPE:SI CRACKS NOTED IN FASTENER HOLES OF MAIN CARGO DOOR CUTOUT AT FORE AND AFT HINGES ATTACH HOLES AT STR 3, BS 487.5, 610.25 (OUTER HOLES) 611.75 (OUTER HOLE) 613, 614 AS IDENTIFIED IN 727 NDT PT 6, 53-10-27 FIG NR 16 SHEETS 2 AND 3. REPLACED CROWN SKIN ASSY (P/N 65-42370-52) PER BFG ER 99-6465.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,069 hrs · 45,519 cycles

INSPECTION TYPE:SI CRACK NOTED STR 3L AND BS 480 FWD MCD FRAME WHILE DOING INSPECTION. REPAIRED 480 FRAME AT OUTBOARD FLANGE RADIUS AT STR 3L.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,069 hrs · 45,519 cycles

INSPECTION TYPE:SI CRACK NOTED STR 3L AND BS 480 FWD MCD FRAME WHILE DOING INSPECTION. REPAIRED BS 480 FRAME (PN 65-40223-1) AT O/B FLANGE RADIUS AT STR 3L PER BFG ER 99-6456A.

Part: LAP JOINT — CORRODED (FUSELAGE SKIN) · airframe 62,069 hrs · 45,519 cycles

INSPECTION TYPE:SI, UPON ACCESSING AND REMOVAL OF UPPER SKIN DISCOVERED SKIN LAP AT STR 4 RT CORRODED. REMOVED CORROSION ON UPPER SKIN LAP AT STR 4R AND REPAIRED PER BFG ER 99-6465.

Part: LAP JOINT — CORRODED (FUSELAGE SKIN) · airframe 62,069 hrs · 45,519 cycles

INSPECTION TYPE:SI, WHEN ACCESSING AND REMOVAL OF UPPER CROWN SKIN DISCOVERED STR 4R SKIN LAP CORRODED BS 480 TO 740. REMOVED CORROISON ON UPPER SKIN LAP AT STR 4R AND REPAIRED PER ER 99-6465.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,069 hrs · 45,519 cycles

INSPECTION TYPE:SI WHILE NDI ACCESSED HOLES COMMON TO REMOVED CROWN SKIN, DISCOVERED CRACK IN BS 480 FRAME LBL 60 STR 10L AFT ROW. REPAIRED PER ER 99-6617 UNDER UPS FILE 727-53-2248.

Part: FITTING — CRACKED (FUSELAGE) · airframe 62,069 hrs · 45,519 cycles

INSPECTION TYPE:SI, CRACKS NOTED IN FASTENER HOLES OF MAIN CARGO DOOR CUTOUT AT FWD AND AFT HINGE ATTACH HOLES AT STR 3, BS 482.5, 610.25, 611.75, 613, 614 AS IDENTIFIED IN 727 NDI, PT 6, 53-10-27, FIG NR 16 SHEET 2 AND 3. REPLACED CROWN SKIN ASSY AND FREEZE PLUGGED DISCREPENT HOLES.

Part: FRAME — CRACKED (BS 1110)

INSPECTION TYPE:SI, CRACK FOUND WITH HFEC AT AFT CARGO DOOR CUT-OUT AFT FRAME WEB, UPPER DOORSTOP CUT-OUT AT WL 183.5, RBL 64, BS 1110. CRACK GOES FROM CENTER OF CUT-OUT OUTBD INTO RADIUS UNDER STRAP. REPAIRED FRAME PER SRM 51-40-02 AND DWG 65-20729.

Part: SKIN — CORRODED (BS 1183)

INSPECTION TYPE:SI CORROSION (C53-100-01.02-06) PILLOWING SKIN AT BS 1183 LBL 30. REPAIR PER ER NR 99-6454 (727-53-2214).

Part: STRINGER — CRACKED (BS 490 - 550)

INSPECTION TYPE:SI CRACKED FASTENER HOLES IN STR 1 BETWEEN BS 490 AND BS 540. REMOVED STRINGER 1 FROM BS 490 TO BS 550. FABRICATED NEW STRINGER AND REPAIR PARTS AND INSTALLED PER SRM 53-10-2 SRM 51-30-2, SRM 53-10-1 SRM 53-10-3.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,069 hrs · 45,519 cycles

INSPECTION TYPE:SI ACCESSED HOLES COMMON TO REMOVED CROWN SKIN, DISCOVERED CRACK IN BS 480 FRAME LBL 60 STR 10L AFT ROW. REPAIRED BS 480 FRAME PER ER 99-6617, UNDER UPS FILE NUMBER 727-53-2248.

Part: STRINGER — CRACKED (BS 490 - 540)

INSPECTION TYPE:SI CRACKED FASTENER HOLES IN STR 3 RT BETWEEN BS 490 AND BS 540. CUT OUT DAMAGED STRINGER FROM BS 490 TO BS 550, STR 3 RT. FABRICATED NEW STRINGER COLD FORMED NEW STRINGER AT JOGGLED AREAS AND FABRICATED STRINGER REPAIR SPLICES ALODINED PRIMED AND INSTALLED ALL PARTS IAW SRM 5 3-10-3, SRM 51-30-2, SRM 51-10-2.

Part: FITTING — CRACKED (BS 1183)

INSPECTION TYPE:SI, THE STR 29L BATH TUB FITTING COMMON TO BS 1183 IS CRACKED (INBD FITTING). FITTING WAS REPLACED PER SRM 51-30-2 AND MM 53-11-0.

Part: FLOORBEAM — CORRODED (BS 328)

INSPECTION TYPE:SI, CORROSION (C53-224-01.05-01) ON FLOORBEAM BS 328 LBL 20 WL 208. REPLACED FLOORBEAM FROM LBL 21 TO RBL 16, BS 328 WL 208 PER SRM 53-10-8.

Part: SKIN — CORRODED (BS 259.5)

INSPECTION TYPE:SI, LFEC INSP EXHIBITS GREATER THAN 10 PERCENT MATERIAL LOSS AT BS 259.5 STR 23L TO STR 24L FWD SIDE OF SPLICE. REPAIRED SKIN AT 259.5 STR 23L TO STR 24L IAW UPS EO B727-5310-1371E APP 8.5 AND DWG 69-62161.

Part: ANGLE — CORRODED (BS 351)

INSPECTION TYPE:SI, CORRODED FLOOR SUPPORT STRUCTURE BS 351, RBL W 168.5. REMOVED, FABRICATED AND INSTALLED MISC ANGLES AND WEBS PER SRM 51-40-2.

Part: FLOORBEAM — CORRODED (BS 1044 - 1050)

INSPECTION TYPE:SI, CORRODED FLOORBEAM AT BS 1044-1050, LBL 2, WL 148.5. CORROSION CLEAN UP BEYOND ACCEPTABLE LIMITS. REMOVED, FABRICATED, AND REPLACED FLOORBEAM SEGMENT FROM BS 950-1050 SRM 53-10-5 FIG 4.

Part: FLOORBEAM — CORRODED (BS 1050 - 1044)

INSPECTION TYPE:SI, CORRODED FLOORBEAM AT BS 1050-1044 RBL 9 WL 148.5. CORROSION CLEAN UP BEYOND ACCEPTABLE LIMITS. REMOVED, FABRICATED AND REPLACED FLOORBEAM SEGMENT FROM BS 950-1050 PER SRM 53-10-5 FIG 4.

Part: HINGE — CORRODED (RUDDER)

INSPECTION TYPE:SI, UPPER RUDDER, UPPER RUDDER TAB HINGE IS LOOSE AND CORRODED ON INNER HINGE CLEVIS. REMOVED AND REPLACED UPPER RUDDER, UPPER HINGE PER MM 27-20-11.

Part: FRAME — CRACKED (CARGO DOOR)

INSPECTION TYPE:SI, FWD LWR CARGO DOOR CUTOUT AFT DOOR FRAME WEB AT LWR STOP PAD FITTING CRACKED. REPAIRED PER SRM 51-40-2 AND SRM 51-30-2.

Part: STIFFENER — CORRODED (BS 294.5)

INSPECTION TYPE:SI, CORROSION AT BS 294.5, LBL 10.5 NOSE WHEEL UPPER LEFT CORNER ON STIFFENER. FABRICATED STIFFENER AND REPLACED PER SRM 51-20-1, SRM 51-30-2.

Part: SEAT TRACK — CORRODED (BS 538)

INSPECTION TYPE:SI, CORROSION AT FWD CARGO BAY SEAT TRACK BS 538 RBL 14 WL 148.5. REMOVED AND REPLACED SEAT TRACK BS STA 480-588, RLB 14 PER SRM 53-10-5.

Part: FLOORBEAM — CORRODED (BS 312)

INSPECTION TYPE:SI, CORROSION (C53-224-01.05-01) ON FLOORBEAM AT UNDERSIDE OF THE AFT UPPER FLANGE, BS 312, RBL 11, WL 208. REPLACED FLOORBEAM FROM RBL 1 TO RBL 65, BS 312, WL 208 PER SRM 53-10-8.

Part: SEAT TRACK — CORRODED (BS 343)

INSPECTION TYPE:SI, CORROSION (C53-224-01.00-01) ON SEAT TRACK, BS 343, LBL 24 WL 208. REPLACED SEAT TRACK AT BS 344-480, LBL 24, WL 208 PER SRM 51-10-6, 53-10-1, 51-30-2.

Part: WEB — CRACKED (BS 277)

INSPECTION TYPE:SI, WEB CRACKED AT BS 277 STRINGER 16 RT SIDE. REPAIRED PER SRM 51-40-2 FIG 1 PG 2.

Part: FLOORBEAM — CORRODED (BS 312)

INSPECTION TYPE:SI, CORROSION ON FLOORBEAM BS 312, WL 200, RBL 60. REPAIRED CORRODED FLOORBEAM BS 312, WL 220, RBL 60, IAW SRM 53-10-08.

Part: FLOORBEAM — CORRODED (BS 720)

INSPECTION TYPE:SI, CORROSION ON FLOORBEAM AT BS 720, RBL 46 TO RBL 50 WL 208. REMOVED AREA OF CORROSION IN A AREA OF 1.0 X 1.0 AND 1.0 X .75, REMOVED MAX .141 FROM ORIG OF .151 FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. REMOVED UPPER SECTION OF FLOORBEAM FROM BS 720 RBL 0 TO RBL 70. FABRICATED NEW SECTION AND REPAIR SPLICES FILLERS. INSTALLED ALL PER SRM 53-10-8, 51-30-5, 51-30-6, 51-30-2.

Part: FLAPTRACK — CORRODED (WING)

INSPECTION TYPE:SI, LT WING O/B FLAP NR 2 MIDFLAP CARRIAGE HAD RUST INSIDE. REPLACED THE NR 2 FLAP CARRIAGE WITH A NEW ASSY.

Part: STRINGER — CORRODED (BS 760 - 848)

INSPECTION TYPE:SI, CORROSION (C53-224-01.00-01) MAIN DECK LONGITUDINAL BEAM BS 760-848 LBL 45 WL 208 RT FLANGE SEVERAL PLACES. REPAIRED PER SRM 51-10-2, 51-30-2.

Part: SILL — CORRODED (BS 312 - 344)

INSPECTION TYPE:SI, CORROSION (C53-224-01.00-01) ON MOP SILL ANGLE BS 312 BS 344 LBL 58 WL 208. REMOVED, REPLACED MOP SILL PER SRM 51-30-2, 53-10-1.

Part: SEAT TRACK — CORRODED (BS 780)

INSPECTION TYPE:SI, MAIN DECK SEAT TRACK HAS CORROSION ON TOP OF TRACK, BS 760 AND BS 780 RBL 63 WL 208. REMOVED CORRODED SEAT TRACK, FABRICATED AND INSTALLED NEW SEAT TRACK PER SRM 53-10-1, SRM 51-30-5, SRM 51-10-2 AND SRM 51-30-2.

Part: FRAME — CORRODED (BS 620)

INSPECTION TYPE:SI WHILE ACCESSING MCD FOR NDT, FOUND CORROSION UNDER SEAL DEPRESSOR BS 620 LT ABOVE SPLICE WL 268 ON FRAME. REPAIRED CORRODED FRAME IAW ER-6435A.

Part: BATTERY PACK — DISCHARGED (LT EMER EXIT)

2 EXIT LIGHTS IN OVER HEAD INOP LEFT WING EMERGENCY LIGHT INOP. REMOVED AND REPLACED BATTERY PACK. OPS CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (AFT AIRSTAIR)

AFT AIRSTAIR EMERGENCY LIGHT INOP. REMOVED AND REPLACED BATTERY PACK.

Part: BATTERY PACK — DISCHARGED (CABIN)

EMERGENCY LIGHT ABOVE AFT WORK STATION VERY DIM. REMOVED AND REPLACED BATTERY PACK. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (ROW 19)

ROW 19 EMER LIGHT INOP. REMOVED AND REPLACED BATTERY PACK. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (GALLEY)

EMERGENCY LIGHT AT GALLEY SERVICE DOOR INOP. REMOVED AND REPLACED BATTERY PACK.

Part: ACTUATOR — FAILED (FLIGHT SPOILERS)

INSPECTION TYPE:N/A, ON HIGH SPEED CLIMB PROFILE 340 FLTS A/C REQUIRED 10 DEG RIGHT AILERON INPUT. A/C TRIMMED IAW AOM PROCEDURE. LEFT RUDDER TRIM 1/4 TURN AILERON TRIM 1/2 TURN. A/C LANDED FLAPS 30 AT 140 KNOTS WITH 20 DEG RIGHT AILERON REQUIRED TO KEEP WINGS LEVEL. EMERGENCY DECLARED DUE TO INCREASED LANDING SPEED. *S/D* REMOVED AND REPLACED NR 1, 2 AND 3 FLIGHT SPOILER ACT PER MM 27 -61-81, PERFORMED LEAK CHECK AND ADJUSTED ALL CHECKS GOOD.

Part: BATTERY PACK — DISCHARGED (ROW 9)

ROW 9 FLOOR LIGHT INOP. REMOVED AND REPLACED BATTERY PACK. OPS CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN)

LEFT ENTRY DOOR, FORWARD SIDEWALL EXIT IDENTIFIER INOP. REMOVED AND REPLACD BATTERY PACK. OPS CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (ROW 17)

ROW 17 FLOOR LIGHT INOP. REMOVED AND REPLACED BATTERY PACK. OPS CK, GOOD.

Part: BATTERY PACK — DISCHARGED (PASSENGER DOOR)

EMERGENCY EXIT MARKER LIGHT ASSY ABOVE FWD ENTRY DOOR FAILED TEST PER TASK CARD 7-1 STEP 1B (1) E. STEADY GREEN LIGHT FAILED TO ILLUMINATE. REMOVED AND REPLACED BATT PACK, OPS CHECK GOOD IAW T/C 7-1 STEP 1B (1)E P/N ON/OFF 96-2-1019.

Part: LIGHT — INOP (VENTRAL STAIR)

EMERG VENTRAL STAIR PATH LIGHT INOP. T/S FOUND CONTINUITY ON WIRE FROM PINS 11 BUT FOUND NOTHING ON PINS 12 OR 13 DEFERED ITEM PER MEL33-16-02.

Part: BATTERY PACK — DISCHARGED (CARGO COMPT)

REPLACE EMERGENCY LIGHT RECEIVER BATTERIES. REMOVED AND REPLACED BATTERIES AS REQ'D A/C IN CARGO CONFIG.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE-N/A, ROWS 4, 9, 11, 13, 15, 17, 19 EMERG EXIT LIGHTS INOP. REMOVED AND REPLACED BATT PACKS AS ABOVE, OPS CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (PAX DOOR)

INSPECTION TYPE-N/A, FWD ENTRY EEL INOP TOP AND BOTTOM. REMOVED AND REPLACED EEL BATT PACKS AS ABOVE, OPS CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE-N/A, REAR EXIT EEL INOP. REMOVED AND REPLACED BATT PACK, OPS CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE-N/A, GALLEY EEL INOP. REMOVED AND REPLACED GALLEY EXIT EMERG LIGHT BATT PACK, OPS CHECK GOOD.

Part: LIGHT — INOP (CABIN)

INSPECTION TYPE-N/A, EMER EXIT LIGHTS INOP. REMOVED AND REPLACED LIGHT ASSY, OPERATION CK GOOD (P/N 96-3-1010) (S/N 1015) ON, (S/N 1004).

Part: SMOKE DETECTOR — MALFUNCTIONED (LAVATORY)

INSPECTION TYPE-N/A, SMOKE DETECTOR WENT OFF IN FLIGHT, NO SMOKE DETECTED. DEACTIVATED UNIT AND RESET RIGHT AFT LAV, REPEAT WRITE UP 3. RIGHT AVE LAVATORY SMOKE DETECTOR INOP, DEFERRED PER MEL 26-17 M160233 ASSIGNED.

Part: SKIN — CORRODED (BS 305)

INSPECTION TYPE:C CORROSION ON EXTERNAL SKIN BETWEEN STR 24L AND 26L BS 305. REMOVED AND REPLACED FUSELAGE SKIN PANEL BS 227 TO 360 IAW SRM 51-30-02, 51-20-1, 51-50-1, 51-50-4 BFGOODRICH ENGINEERING REPAIR 98-2513.

Part: FITTING — CRACKED (NR 6 SPOILER)

INSPECTION TYPE:C NR 6 SPOILER SUPPORT HINGE FITTING CRACKED AT UPPER HORIZONTAL LUG AFT SIDE O/B SIDE. REMOVED NR 6 SUPPORT HINGE FITTING (SPOILER) IAW SRM 51-30-5, MM 57-42-75.

Part: SKIN — CORRODED (BS 1179)

INSPECTION TYPE:C, CORROSION (C53-100-01.00-05) ON SKIN BS 1179, LBL 60, WL 250. REMOVED DAMAGED AREA AND INSTALLED FILLER AND REPAIR DOUBLER PER UPS SRM 53-30-3, FIG 3A, AND 51-30-2.

Part: SKIN — CORRODED (BS 1372)

INSPECTION TYPE-C, CORROSION AND PILLOWING SKIN ABOVE NR 2 ENGINE FAIRING BS 1372 RBL 30 WL 250. REMOVED AND REPLACED SKIN PANEL AND REPAIRED DAMAGED FWD SKIN IAW SRM 53-30-03.

Part: RIB — CRACKED (WS 686)

INSPECTION TYPE:C FLOURSCENT PEN INSPECTION EXHIBITS CRACKS IN WS 686 RIB LOWER FLANGE RADUIS AT STR 6 LOWER ATTACH HOLE (LEFT WING). REMOVED AND REPLACED CRACKED RIB AT LEFT WS 686 PER SRM 51-30-2 AND EO B727-5710-1325H.

Part: SKIN — CRACKED (NR 4 LE SLAT)

INSPECTION TYPE:C, CRACK GROWING PAST STOP DRILL HOLE IN NR 4 SLAT, I/B TRACK, O/B SIDE OF SKIN SUPPORT ANGLE. STOP DRILLED END OF CRACK, NDT VERIFIED CONTAINMENT, RE-INSTALLED EXISTING REPAIR IAW SRM 57-50-3.

Part: FITTING — CORROSION (NLG)

INSPECTION TYPE:C CORROSION IN BEARING BORE OF LT NLG TRUNNION SUPPORT FITTING. BORE LT NLG TRUNNION FITTING BORE IAW SRM 53-40-1.

Part: RIB — CRACKED (NR 4 LE SLAT)

INSPECTION TYPE:C, CRACK GROWING PAST STOP DRILL HOLD IN NR 4 SLAT I/B END RIB. REMOVED CRACKED RIB AND REPLACED WITH NEW ITEM PER SRM 51-30-2 AND SRM 20-50-01.

Part: SKIN — CORRODED (BS 1130-1145)

INSPECTION TYPE:C, CORROSION (C53-100-01.01-05) AND POPPED RIVET HEAD ON SKIN LAP LEFT SIDE OF NR 2 ENGINE INLET BS 1130-1145, LBL 20-30, WL 290. CORROSION FOUND TO BE OUT OF LIMITS PER SRM 53-30-1 IN AND AREA OF 8 BY 8. DAMAGED SKIN REMOVED AND A STANDARD SKIN LAP REPAIR ACCOMPLISHED PER SRM 53-30-3, SRM 51-10-2, MM 51-20-13 AND SRM 51-30-2.

Part: BATT PACK — DISCHARGED (CABIN)

INSPECTION TYPE-N/A, EMERGENCY EXIT LIGHT AT AFT ATTENDANT PANEL UPPER POSITION INOP. REMOVED AND REPLACED EMERGENCY BATTERY PACK AT AFT ATTENDANT POSITION.

Part: OVERHEAT LOOP — OUT OF POSITION (NR 1 ENGINE)

INSPECTION TYPE-N/A, ON TAKEOFF ENG 1 STRUT OVERHEAT LIGHT ILLUMINATED. PER CHECK LIST, NR 1 THRUST LEVER RETARDED TO IDLE AND LIGHT WENT OUT. WHEN THRUST LEVER ADVANCED AGAIN, LIGHT RE-ILLUMINATED. LEFT THRUST IN IDLE AND RETURNED TO JAX. REMOVED NR 1 STRUT PANELS AND PERFORMED ENG RUN, NO LEAKS. CHECK WIRING AND SENSE LINE INSTALLATION. FOUND OVERHEAT LOOP RUBBING ON BRACKET. MOVED LOOP, RERAN ENGINE NR 1, NO LIGHT. REINSTALLED STRUT PANELS, OK TO CONTINUE FLIGHT.

Part: BATTERY PACK — DISCHARGED (CABIN)

GALLEY FWD EMERGENCY EXIT LIGHT GLOWS DIM. REMOVED AND REPLACED BATTERY PACK.

Part: LIGHT — INOPERATIVE (CABIN)

INSPECTION TYPE-N/A, GALLEY DOOR EMERGENCY EXIT LIGHT DIM. REMOVED AND REPLACED EXIT LIGHT BATTERY, OPS CK'D GOOD ON EMERGENCY LIGHT TEST.

Part: OXY MASKS — DEPLOYED (CABIN)

INSPECTION TYPE-N/A, ALL PAX O2 MASKS DEPLOYED REPACKED ALL O2 MASKS AS REQUIRED IAW 35-20-00 DUE TO INADVERTANT DEPLOYMENT, NO OTHER DEFECTS NOTED.

Part: LIGHT — INOPERATIVE (COCKPIT)

INSPECTION TYPE: MOD COCKPIT EMERGENCY. ENTRANCE LIGHT INOP. REPLACED ALL 3 CONTROL MODULES EMERGENCY LIGHTS. OPS CHECKED GOOD IAW PEMC DRAWING 015-00357.

Part: STRUT FITTING — CORRODED (RT FUSELAGE)

INSPECTION TYPE-C, RT SIDE FUSELAGE TO WING STRUT FITTING, WBL 40 RT FWD LWR SPAR CHORD IS HEAVILY CORRODED. REMOVED, FABRICATED AND INSTALLED STRUT FITTING IAW DWG 65-21799 AND SRM 51-30-2.

Part: SHEAR TIE — CORRODED (BS 351.2)

INSPECTION TYPE-C, SHEAR TIE AT STA 351.2, STR 22R WAS FOUND TO BE CORRODED BEYOND LIMITS. CUT OUT DAMAGED SECTION OF SHEAR TIE AT BS 351.2, STR 22R, FABRICATED AND INSTALLED REPAIR IAW SRM 53-10-2 AND 51-40-3.

Part: STIFFENER — CORRODED (CTR WING SPAR)

INSPECTION TYPE-C, CENTER WING FRONT LWR SPAR STIFFENER LBL 42 HAS HEAVY CORROSION. REMOVED, FABRICATED AND INSTALLED REPLACEMENT STIFFENER IAW DWG 65-16281 AND SRM 51-30-2.

Part: SPAR CHORD — CORRODED (CTR WING)

INSPECTION TYPE-C, CENTER WING TANK FWD LOWER SPAR CHORD SEVERELY CORRODED FROM LBL 26 TO LBL 40 REF N/R 588971. REMOVED AND REPLACED SPAR CHORD IAW SRM 51-30-2, 51-30-10, 51-30-1.

Part: FRAME — CRACKED (BS 1050)

INSPECTION TYPE-C, AFT PIT BS 1050 APPROX RBL 3, THE FRAME APPEARS CRACKED IN THE RADIUS OF THE UPPER FLANGE. CUT OUT DAMAGED AREA AS REQUIRED, FABRICATED PARTS AND INSTALLED IAW SRM 51-40-3.

Part: CHORD — CRACKED (VERTICAL STAB)

INSPECTION TYPE-C, VERTICAL STAB RT LOWER TORQUE BOX CHORD CORRODED AND CRACKED. REMOVED DAMAGED SECTION OF CHORD, FABRICATED AND INSTALLED REPAIR PARTS IAW DHC SK947-123 AND SRM 51-30-2 REF ENGINEERING FLIE NR 727-55-0338.

Part: FLOORBEAM — CORRODED (BS 344)

INSPECTION TYPE-C, FLOORBEAM STA 344 RBL 18 UPPER CHORD FWD FLANGE CORRODED BEYOND LIMITS. REMOVED DAMAGED SECTION OF CHORD, FABRICATED AND INSTALLED REPAIR SECTION USING EXISTING SPLICE IAW SRM 51-30-2, 51-40-2.

Part: SKIN — CORRODED (BS 1096-1112)

INSPECTION TYPE-C, FUSELAGE SKIN AND INTERNAL DOUBLER BS 1096 TO 1112 STR 18R TO 20R CORRODED BEYOND LIMITS ON UPS NRC 588666. FABRICATED REPAIR SKINS AND SPLICE DOUBLER IAW SK 974-957. INSTALLED REPAIR SKINS AND DOUBLER IAW DHC SK 947-957 REF ENGINEERING FILE NR 727-53-1841.

Part: SHEAR TIE — CORRODED (BS 351.2)

INSPECTION TYPE-C, FRAME 351.2 EXFOLIATED ABOVE STR 25R, DETERMINED TO BE ON SHEAR TIE AND NOT ON FRAME. REMOVED DISCREPANT AREA, FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 51-40-2, 53-10-2 AND 51-30-2.

Part: FRAME — CRACKED (BS 1070)

INSPECTION TYPE-SP, FRAME CRACKED AT BS 1070 ABOVE AFT CARGO DOOR AT FWD HINGE ATTACH POINT. STOP DRILLED CRACK, REPAIRED PER SRM 53-10-4 FIG 6.

Part: INTERCOSTAL — CRACKED (NR2 ENG FIREWALL)

INSPECTION TYPE-SP, CRACK ACROSS 2 RIVET HOLES ON FLANGE OF HORIZONTAL INTERCOSTAL ON NR 2 ENG FIREWALL 4TH FWD FROM REAR ENG MT. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PARTS PER SRM 54-10-3 FIG 2 AND 54-10-3 FIG 1.

Part: STRINGER — CRACKED (BS 1050)

INSPECTION TYPE-SP, BS 1050 STR 16 HAS 2 CRACKS AND STR 17, 1 CRACK THROUGH FUSELAGE SKIN. REMOVED AND REPLACED DISCREPANT SKIN AND DOUBLER. FABRICATED REPLACEMENT PARTS PER UPS SRM 53-30-3 FIG 12 53-30-2, 51-40-05 SKIN REPLACEMENT FROM STA 1020 TO 1080 FROM STR 14R TO 20R.

Part: LIGHT — INOPERATIVE (COCKPIT)

COCKPIT EMERGENCY EXIT LIGHT INOP. REPLACED LIGHT ASSY, OP CHECKS GOOD (P/N 10-0067-9), OFF (S/N 19703), ON (S/N 26798).

Part: LIGHT — INOPERATIVE (COCKPIT)

INSPECTION TYPE: EMERGENCY EXIT LIGHT FAILED TO TEST. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSY.

Part: ANTI-ICE TUBE — BROKEN (NR 2 ENGINE)

CREW REPORTED, NR 2 FIRE WARN LIGHT AND BELL WITH CLIMB THRUST, CLIMBING TO ALTITUDE OUT OF ROA. ENGINE NR 2 SHUTDOWN AT 0927Z PER CHECKLIST, FIRE LIGHT WENT OUT AND ALL ENGINE INDICATIONS NORMAL. ENGINE HEAT WAS ON IN THE ICING CONDITIONS. REMOVED AND REPLACED BROKEN LT REAR A/I TUBE ASSY. REMOVED AND REPLACED CRACKED HIGH PRESSURE SUPPLY WYE DUCT. ALL IAW MM 75-10, LEAK CHECK GOOD.

Part: FRAME — CRACKED (BS 930)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND 2 CRACKS ON FRAME AT B.S. 930, RBL 64 AND 67, WL 199 RT WHEELWELL. REPAIRED IAW E.O. B727-5310-7167-A.

Part: CHORD — CORRODED (BS 340-348)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON LT UPPER NOSE CHORD BS 340 TO 348, LBL 15, WL 170. REPAIRED IAW SRM 53-10-1, 51-10-1, 51-30-5, 51-20-4, 51-30-2.

Part: EXPANSION LINK — CORRODED (FS 740-780)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON EXPANSION LINK AT STA 740 TO 760 AT RBL 25, WL 208. REPAIRED IAW SRM 53-10-1, 51-30-8, OHM 20-50-03, 20-50-02, 20-50-1.

Part: SKIN — DELAMINATED (NR 9 SPOILER)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND DELAMINATED SPOILER AT UPPER I/B CORNER, 4 INCH BY 4.5 INCH ON THE NR 9. REPAIRED IAW SRM 51-40-06.

Part: WEB — CRACKED (FS 294-312)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CRACKED WEB AT STA 294 TO 312, RBL 40, WL 207. REPAIRED IAW SRM 51-30-2, 51-20-1, M/M 51-20-151.

Part: SKIN — DELAMINATED (NR 5 SPOILER)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND DELAMINATED SPOILER AT UPPER I/B CORNER 4 INCH BY 4.5 INCH ON THE NR 5. REPAIRED IAW SRM 51-40-06.

Part: SUPPORT — CORRODED (FS 302-312)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON FLOOR SUPPORT STA 302 TO 312. REPAIRED IAW SRM 51-10-6, 51-30-6, 51-20-1, 51-30-5, 51-30-02.

Part: FLAP — DELAMINATED (RT TE AFT FLAP)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND DELAMINATION OF I/B RT AFT FLAP ON THE O/B CORNER. REPAIRED IAW SRM 51-40-6, M/M 51-20-151.