N940UP

Part: RECEPTACLE — DIRTY (LG MODULE BOX)

UPON GEAR RETRACTION 3 RED GEAR WARNING LIGHTS ILLUMINATED. GEAR DOORS OPERATED NORMAL. GEAR WAS EXTENDED. THREE GREEN GEAR LIGHTS ILLUMINATED AND THE NOSE GEAR RED LIGHT REMAINED ON. GEAR WAS RETRACTED AND THE 3 RED GEAR WARNING. REMOVED LANDING GEAR MODULE BOX, INSPECTED RECEPTABLE AND BACK OF BOX CLEANED W/CONTACT CLEANED ACCP TEST I/W 32-09-18 AND SWIFTY NOSE GEAR, I/W 32-33-00 FOUND EVERYTHING TO OPS CHECK NORMAL.

Part: SEAT TRACK — CORRODED (BS 560 LBL10-50) · airframe 58,465 hrs · 30,380 cycles

DURING REMOVAL OF FLOORBOARDS TO FACILITATE REPLACEMENT OF SEAT TRACK SECTION CORROSION FOUND ON FLOORBEAM UPPER CHORD AT BS 560 BETWEEN LBL 10 - LBL 50. CORROSION REMOVED IAW SRM 51-10-01. FOUND OUTSIDE LIMITS IAW SRM 51-10-1. HFEC CARRIED OUT ON BLENDED AREA IAW B 727-NDTM 51-00-00 PT6 FIG 4 , NO DEFECTS FOUND. AREA FLAP PEENED IAW SOPM 20-10-03. DOUBLER DERIVETED IAW SRM 51-30-02. FLOORBEAM CUT AS REQUIRES IAW SRM 53-10-08. FILLERS FABRICATED IAW SRM 51-20-01. SEAT TRACK RE-INSTALLED IAW SRM 51-30.

Part: RIB — CRACKED (L/E SLAT) · airframe 58,465 hrs · 30,380 cycles

INSPECTION TYPE:C NR 6 SLAT SUPPORT RIB CRACKED ABOUT 9 INCHES FROM SLAT I/B END. REMOVED DAMAGE IAW SRM 51-10-1. HFEC CARRIED OUT AROUND CUTOUT IAW B72 7NDTM 51-00-00 PT 6 FIG 4. SUPPORT RIB REPAIR DOUBLER FORMED IAW SRM 57--50-3. DOUBLER SHAPED AND DRILLED IAW SRM 57-50-3 AND 57-20-1. CAD PLATING CARRIED OUT IAW SOPM 20-42-10. REPROTECTED DOUBLER IAW SRM 51-1 0-2. INSTALLED DOUBLER IAW SRM 51-30-02.

Part: RIB — CRACKED (L/E SLAT) · airframe 58,465 hrs · 30,380 cycles

INSPECTION TYPE:C NR 6 SLAT SUPPORT RIB CRACKED, ABOUT 9 INCHES FROM THE SLAT O/B END. REMOVED DAMAGE IAW SRM 51-10-1. HFEC CARRIED OUT AROUND CUTOUT IAW B72 7NDTM 51-00-00 PT 6 FIG 4. REPAIR DOUBLER FORMED IAW SRM 57-50-3. DRILLED AND SHAPED DOUBLER IAW SRM 51-20-1. CAD PLATING CARRIED OUT IAW SO PM 20-42-10. REPROTECTED REPAIR ANGLE IAW SRM 51-10-2. INSTALLED ANGLE IAW SRM 51-30-02.

Part: RIB — CRACKED (NR 6 SLAT) · airframe 58,465 hrs · 30,380 cycles

NR 6 SLAT SUPPORT RIB CRACKED, ABOUT 9 INCHES FROM SLAT I/B END. REMOVED DAMAGE IAW SRM 51-10-01. HFEC CARRIED OUT AROUND CUTOUT IAW B7 27-NDTM 51-00-00 PT 6 FIG 4, NDF. REPAIR DOUBLER FORMED IAW SRM 57-50-3. NR 6 SLAT SUPPORT RIB CAD PLATING CARRIED OUT IAW SOPM 20-42-10. REPROTECTED DOUBLER IAW SRM 51-10-01. INSTALLED DOUBLER IAW SRM 51-30-0 2.

Part: BRACKET — CRACKED (NR 11 SPOILER) · airframe 58,465 hrs · 30,380 cycles

RIGHT WING T/E CAVITY NR 11 SPOILER I/B HINGE BRACKET ASSY, SUSPECT CRACK ON O/B BRACKET AT UPPER AFT CORNER. HFEC CARRIED OUT IAW B727-NDTM 51-00-00 PT6 FIG 4 CRACK CONFIRMED. REMOVED O/B HINGE BRACKET IAW SRM 51-30-02. FABRICATED BRACKET IAW SRM 51-20-01. REPROTECTED BRACKET IAW SRM 51-10-02. INSTALLED BRACKET IAW SRM 51-30-02. RETORQUED HINGE BOLTS IAW MM 27-61-01.

Part: SKIN — CORRODED (RT WING) · airframe 58,465 hrs · 30,380 cycles

INSPECTION TYPE:C CORROSION ON RT WING TIP UPPER SURFACE AT O/B TRAILING EDGE STATIC DISCHARGER. STATIC DISCHARGER REMOVED IAW SRM 51-30-02. CORROSION REMOVED IAW SRM 51-10-06 AND FOUND OUT OF LIMITS. HFEC CARRIED OUT ON BLENDED AREA IAW B727-NDTM 51-00-00 PT6 FIG 4 NDF. REPAIRED IAW AAAE EO 2006-037-002. REPLACED DISCHARGER IAW AAAE EO 2006-037-002. PAINTED REPAIRED AREA IAW MM 51-20-91.

Part: INTERCOSTAL — CRACKED (NR 3 SLAT) · airframe 58,465 hrs · 30,380 cycles

INSPECTION TYPE:C NR 3 SLAT AT O/B TRACK ATTACHMENT TO SLAT, CRACK ON INTERCOSTAL. FASTENERS REMOVED IAW SRM 51-30-02 AND CRACK CUTOUT IAW SRM 57-50-03. O/B SLAT TRACK DISPLACED AT FWD ATTACHMENT AREA IAW OHM 57-51-51. REPAIR DOUBLER FABRICATED IAW SRM 57-50-3. CAD PLATING CARRIED OUT IAW SOPM 20-42-10. REPAIR INSTALLED IAW SRM 57-50-3. FASTENERS INSTALLED IAW SRM 51-30-02. SLAT TRACK AND FWD ATTACHMENTS RE-INSTALLED IAW AMM 27-81.

Part: INTERCOSTAL — CRACKED (NR 3 SLAT) · airframe 58,465 hrs · 30,380 cycles

NR 3 SLAT AT O/B TRACK ATTACHMENT TO SLAT CRACK ON INTERCOSTAL. FASTENERS REMOVED IAW SRM 51-30-02 AND CRACK CUT OUT IAW SRM 57-50-03. REPAIR DOUBLER FABRICATED IAW SRM 57-50-03. CAD PLATING CARRIED IAW SO PM 20-42-10. REPAIR INSTALLED IAW SRM 57-50-03. FASTENERS INSTALLED IAW SRM 51-30-02. SYSTEM RETURNED TO SERVICE.

Part: FLANGE — CRACKED (BS 940) · airframe 58,465 hrs · 30,380 cycles

FOUND EVIDENCE OF CRACK ON LEFT BS 940 LOWER FWD FLANGE. FLANGE REPAIRED IAW AAAE EO 2006-037-007.

Part: BEARING — FAILED (MANUAL EXTENSION) · airframe 58,465 hrs · 30,380 cycles

NOSE WHEEL WILL NOT MANUALLY EXTEND. BEARINGS REPLACED IN CABLE DRUM IAW SOPM 20-50-03. DRUM REPLACED IAW MM 32-34-11. MANUAL EXTENSION SYSTEM ADJUSTED IAW MM 32-34-00. SYSTEM TESTED IAW AMM 32-34-00 AND RETURNED TO SERVICE.

Part: SLIDE — DEPLOYED (L1 DOOR)

INSPECTION TYPE:N/A UPON ARRIVAL TO AIRCRAFT PARKED ON RAMP, FOUND L1 DOOR OPEN AND FOUND ESCAPE SLIDE ON RAMP. REMOVED AND REPLACED SLIDE AND COMPARTMENT WITH SERVICEABLE UNITS IAW MM 25-60-14.

Part: ROD — BROKEN (COCKPIT WINDOW)

F/O SLIDING WINDOW (NR 2) LOCK RELEASE IS BROKEN. REPLACED OPEN WINDOW, RELEASE/LOCK ROD W/REF M/M 56-12-11-4 O/C GOOD W/REF MM 56-12-11-5.

Part: SHIM — LOOSE (RT WING)

RT WING O/B AILERON TAB DELAM DBLR LWR SURFACE. UPON INVESTIGATION FOUND DELAMINATION TO BE A SHIM THAT CAME LOOSE. STARTED REMOVAL OF AILERON BAL. TAB UP TO STEP D ON MM 27-10-19-4 REINSTALLED BOLTS IN TAB REDS AND INSTALLED COTTER PINS. RESECURED LOOSE SHAM PER MM 27-10-19-4

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT)

EMERGENCY EXIT LIGHTS OVER COCKPIT DOOR AND MAIN ENTRY DOOR ARE INOP. REPLACED EMERGENCY LIGHT BATTERY AS PER MM 33-50-90-2.

Part: FITTING — CRACKED (AFT CARGO BAY) · airframe 57,903 hrs · 29,936 cycles

INSPECTION TYPE:C SUSPECT CRACK ON CLEAT AT STR 28L ON FWD SIDE OF BS 1070 AFT CARGO BAY. HFEC CARRIED OUT IAW NDTM 51-00-00 FIG 4. RESULT CRACK CONFIRMED. REMOVED CRACKED CLEAT, FABRICATED AND INSTALLED NEW CLEAT IAW SRM 51-20-1.

Part: BRACKET — CRACKED (NR 5 FLAP TRACK) · airframe 57,903 hrs · 29,936 cycles

INSPECTION TYPE: C, NR 5 FLAP TRACK, FWD O/B FAIRING ATTACH ANGLE BRACKET IS CRACKED. BRACKET REPLACED IAW SRM 51-20-1.

Part: FITTING — CRACKED (AFT CARGO BAY) · airframe 57,903 hrs · 29,936 cycles

INSPECTION TYPE:C, SUSPECT CRACK ON CLEAT AT STR 29L ON FWD SIDE OF BS 1110 AFT CARGO BAY. HFEC CARRIED OUT IAW NDTM 51-00-00 FIG 4. CRACK CONFIRMED. REMOVED CRACKED CLEAT, FABRICATED AND INSTALLED NEW CLEAT IAW SRM 51-30-02.

Part: SKIN — CRACKED (NR 6 SLAT) · airframe 57,903 hrs · 29,936 cycles

INSPECTION TYPE: C, LE SLAT ACCESS PANEL (NR 6 SLAT) HAS 1/2 INCH CRACK ON SKIN. REPAIR CARRIED OUT IAW SRM 51-10-01, 51-40-02 AND 51-30-02.

Part: HINGE — CRACKED (LT OB AILERON) · airframe 57,903 hrs · 29,936 cycles

INSPECTION TYPE:C, LEFT O/B AILERON O/B BALANCE PANEL FWD IDLER HINGE CRACKED. HINGE REPLACED IAW 51-30-2.

Part: DOOR — CORRODED (TAIL SKI) · airframe 57,903 hrs · 29,936 cycles

INSPECTION TYPE:C, CORROSION FOUND AT TAIL SKID DOOR UPPER ATTACH POINTS BS 1183 S 28L + 28R. ON REMOVAL OF PANEL IT WAS FOUND TO BE CORRODED BEYOND LIMITS IAW 53-30-1. NEW PANEL FABRICATED IAW SRM 51-20-1. TAIL SKID MOUNTING CASTING SHOW SIGNS OF WEAR. NEW SUPPORT ANGLES FABRICATED IAW SRM 51-20-1 FIG 7.

Part: HOOK — CRACKED (NR 2 SLAT) · airframe 57,903 hrs · 29,936 cycles

INSPECTION TYPE:C SUSPECT CRACK ON NR 2 SLAT O/B HOOK UPPER FASTENER. HFEC CARRIED OUT IAW NDTM 51-00-00 FIG 4. RESULT - CRACK CONFIRMED. REPAIR CARRIED OUT IAW SRM 57-50-3 FIG 10.

Part: SUPPORT ANGLE — CRACKED (NR 4 FLAP TRACK) · airframe 57,903 hrs · 29,936 cycles

INSPECTION TYPE: C, NR 4 FLAP TRACK FAIRING SUPPORT ANGLE CRACKED AT O/B SIDE AT MLG BEAM. FAIRING SUPPORT ANGLE REPAIRED IAW SRM 51-20-1.

Part: RIB — CRACKED (NR 5 SLAT) · airframe 57,903 hrs · 29,936 cycles

INSPECTION TYPE:C NR 5 LE SLAT STRUCTURE HAS THREE RIBS CRACKED BETWEEN O/B TRACK AND O/B EDGE OF SLAT. REPAIRED CRACKED RIBS 3 PLACES AT NR 5 LE SLAT IAW SRM 57-50-03 FIG 9.

Part: RIB — CRACKED (NR 8 SLAT) · airframe 57,903 hrs · 29,936 cycles

INSPECTION TYPE: C, NR 8 LE SLAT STRUCTURE HAS CRACKED RIB JUST O/B OF ACTUATOR ATTACH POINT. REPAIR CARRIED OUT IAW SRM 57-50-03.

Part: STRUCTURE — CRACKED (FIREWALL) · airframe 57,903 hrs · 29,936 cycles

INSPECTION TYPE:C, SUSPECT CRACK ON LT CHORD ABOVE NR 2 ENGINE HORIZONTAL FIREWALL AT UPPER END OF CHORD. HFEC CARRIED OUT IAW NDTM PART 6 51-00-00, FIG 4. CRACK FOUND TO BE 5.0 INCH IN LENGTH. CHORD REMOVED AND NEW CHORD DRILLED OFF AND INSTALLED IAW SRM 51-30-02.

Part: SUPPORT ANGLE — CRACKED (NR 3 FLAP TRACK) · airframe 57,903 hrs · 29,936 cycles

INSPECTION TYPE: C, NR 3 FLAP TRACK FAIRING SUPPORT ANGLE CRACKED AT I/B AFT END. FAIRING SUPPORT ANGLE REPAIRED IAW SRM 51-20-01.

Part: SKIN — CORRODED (FUSELAGE) · airframe 57,903 hrs · 29,936 cycles

INSPECTION TYPE:C, AREA OF LITE SURFACE CORROSION ON SKIN BELOW S4L AT BS 1183. CORROSION FOUND TO BE RUNNING UNDER LAP. FURTHER RECTIFICATION CARRIED OUT IAW UPS EO B727-5330-0509.

Part: TAB — DELAMINATED (AILERON) · airframe 57,903 hrs · 29,936 cycles

INSPECTION TYPE: C, LT O/B AILERON TAB DELAMINATED AT UPPER I/B END. AILERON TAB REPAIRED IAW SRM 51-40-20.

Part: BUSHING — CORRODED (NR 1 ENG MOUNT) · airframe 57,903 hrs · 29,936 cycles

INSPECTION TYPE:C, ENGINE NR 1 FWD MOUNT FITTING HAS PITTING CORROSION IN ALL MOUNT HOLES. AFT O/B HOLE CORRODED BUSHING REMOVED IAW OHM 20-50-03. HFEC CARRIED OUT IAW NDTM 51-00-00 FIG 13, NO DEFECTS FOUND. REPAIRED IAW UPS EO B727-5440-11592-A.

Part: WEB — CRACKED (FUSELAGE) · airframe 579,032 hrs · 29,936 cycles

INSPECTION TYPE:C, RT VENTRAL STAIRWAY TORQUE BOX WEB SKIN CRACK EXTENDING BEYOND STOP DRILL HOLE ON FWD O/B END ADJACENT TO FUEL SHROUD HOLE & CRACK ON DOUBLER AT AFT SIDE BS 1263. REPAIR CARRIED OUT IAW EO B727-5310-1239-E.

Part: BUSHING — CORRODED (NR 3 ENG MOUNT) · airframe 57,903 hrs · 29,936 cycles

INSPECTION TYPE:C, ENGINE NR 3 FWD MOUNT FITTING HAS PITTING CORROSION IN BOTH O/B (LARGE) HOLES. FWD O/B HOLE BUSHING REMOVED OHM 20-50-03. HFEC CARRIED OUT IAW NDTM 51-00-00 FIG 13, NO DEFECTS FOUND. REPAIRED IAW UPS EO B727-5440-11592-A.

Part: PRESSURE PANEL — CRACKED (NLG WW) · airframe 57,903 hrs · 29,936 cycles

INSPECTION TYPE:C, NLG WHEEL WELL HAS 3 SUSPECT CRACKS AT RT AFT PRESSURE PANEL CUTOUT. TWO AT LWR FWD CORNER AND ONE NEAR UPPER AFT CORNER. REPAIR CARRIED OUT IAW AAAE EO 2005-001-004.

Part: DOOR — CORRODED (NLG) · airframe 57,903 hrs · 29,936 cycles

INSPECTION TYPE:C, NLG LT FWD DOOR HAS EVIDENCE OF CORROSION UNDER SEAL RETAINER. LT NLG DOOR REMOVED AND REPLACED IAW AMM 32-22-01.

Part: BRACKET — CRACKED (NR 1 KRUGER FLAP) · airframe 57,903 hrs · 29,936 cycles

INSPECTION TYPE:C, NR 1 KRUEGER FLAP TRUNNION BRACKET IS CRACKED ON O/B SIDE. BRACKET REPLACED IAW DRG 65-16275.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,903 hrs · 29,936 cycles

INSPECTION TYPE:C SUSPECT CORROSION BETWEEN SKIN AND INTERNAL STRUCTURE BS 294 BETWEEN S18R + S19R ON CLOSER INSPECTION CORROSION FOUND TO BE WELL WITHIN LIMITS IAW SRM 53-30-01. A SMALL CRACK WAS FOUND COMING FROM A FASTENER HOLE. AREA CUT OUT IAW SRM 53-30-03. HFEC CARRIED OUT, NO DEFECTS FOUND. REPAIR DOUBLER FABRICATED AND INSTALLED IAW 53-30-3.

Part: CASTING — CORRODED (NR 3 K-FLAP) · airframe 57,903 hrs · 29,936 cycles

INSPECTION TYPE:C, NR 3 KRUEGER FLAP INBOARD HINGE, FIXED LEADING EDGE CASTING HAS EVIDENCE OF INTERGRANULAR CORROSION. REPLACED AND INSTALLED NEW CASTING IAW DRG 64-8343.

Part: PANEL — DELAMINATED (NR 3 PYLON) · airframe 57,903 hrs · 29,936 cycles

INSPECTION TYPE:C, ENGINE NR 3 PYLON PANEL 5508 IS DELAMINATED INNER SURFACE FWD END. PANEL REPAIRED IAW MM 20-60-04.

Part: PANEL — DELAMINATED (NR 1 PYLON) · airframe 57,903 hrs · 29,936 cycles

INSPECTION TYPE:C, ENGINE NR 1 PYLON PANEL 5408 IS DELAMINATED INNER SURFACE FWD END. PANEL REPAIRED IAW SRM 51-40-20.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

FORWARD ENTRY EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK. OPS CHECK GOOD.

Part: VALVE — STUCK (O2 MASK)

CAPT O2 MASK HAS STUCK VALVE. REPLACED MASK ASSY, OPS CK NORMAL.

Part: CONTROL UNIT — MALFUNCTIONED (NR 3 ENG FIRE)

WHEN F/O TURNED OFF F/D ALTITUDE HOLD, RECEIVED AN INTERMITTENT FIRE WARNING. THE F/O TAPPED THE GLARE SHIELD AND THE FIRE WARNING LIGHT AND BELL CAME ON STEADY. ENGINE NR 3 WAS SHUTDOWN IAW PROCEDURES AND UNEVENTFUL. SIMULATED CREW ACTION BY TAPPING ON GLARE SHIELD-NO DEFECTS FOUND. CHECK RESISTANCE OF BOTH A AND B LOOPS-NO DEFECTS FOUND. RAN NR 3 ENG AND CHECKED DUCT LEAKS, NO DEFECTS FOUND. AS PRECAUTIONARY REMOVED AND REPLACED NR 3 ENG FIRE DETECTOR CONTROL UNIT. OPS CHECK GOOD. REF MM 26-11-21.

Part: A/C PACK — OVERTEMP (COCKPIT)

JUST AFTER T/O COCKPIT FILLED WITH FUMES, RIGHT PACK TEMP WAS 170'. TURNED OFF PAC FUMES STOPPED. ALL C/B'S CHECKED & IN PAC FAN OPS NORMAL. R/R 35 FT CONTROL VALVE PER AMM 21-51-42, OPS CHECK GOOD.

Part: BUSS TIE — CORRODED (RT I/B AILERON) · airframe 57,411 hrs · 29,491 cycles

INSPECTION TYPE: C&SI, RT I/B AILERON BUS QUADRANT CORRODED IN CABLE GROOVE. RIGHT I/B AILERON BUS QUADRANT REPLACED AS REQUIRED UP TO STEP D6 INCLUSIVE IAW MM 27-10-56.

Part: HINGE — CRACKED (O/B AIL IDLER) · airframe 57,411 hrs · 29,491 cycles

INSPECTION TYPE: C, LT O/B AILERON I/B BALANCE BAY FWD PANEL IDLER HINGE CRACKED & BROKEN. REPLACED LT O/B AILERON I/B BALANCE BAY FWD PANEL IDLER HINGE IAW MM 27-10-04 & ON REMOVAL OF HINGE, PIN FOUND TO BE DAMAGED, PIN REPLACED IAW MM 27-10-04.

Part: STIFFENER — CORRODED (FUSELAGE) · airframe 57,411 hrs · 29,491 cycles

INSPECTION TYPE:C CORROSION ON LT 870 MID SECTION ATTACHMENT TO BULKHEAD STIFFENER REPAIR CARRIED OUT IAW SRMO EO 2003-038-006 SRM 51-30-02, UPS EO B72 7-5310-3056 AND DRAWING 65C23231 UPS ENG. FILE NO. 727-53-20118

Part: SKIN — CRACKED (NR 3 RT WINDOW) · airframe 57,411 hrs · 29,491 cycles

INSPECTION TYPE: C, CRACKS IN SKIN FROM FASTENER HOLES AROUND NR 3 RT WINDOW CUTOUT FWD OF BS 259.5 AT S10R AREA. FASTENERS REMOVED AND DAMAGED AREA TRIMMED OUT IAW SRM 53-30-3 FIGUR E 29. REPAIR PARTS FABRICATED IAW SRM 53-30-3 FIG 29. REPAIR PARTS PARTIALLY INSTALLED IAW SRM 53-30-3. REMAINING FASTENERS INSTALLED IAW SRM 53-30-03 FIG 29.

Part: SILL — CRACKED (FUSELAGE) · airframe 57,411 hrs · 29,491 cycles

INSPECTION TYPE: C CRACKS ON LT SILL IN NLG WHEEL WELL AT FWD END AND THE 6TH RIVET FROM FWD. HFEC TO CONFIRM CRACK. CUTOUT MADE AND STOP DRILLED, REPAIRED IAW SRM 51-40-02.

Part: SKIN — CORRODED (FUSELAGE) · airframe 57,411 hrs · 29,491 cycles

INSPECTION TYPE: C SUSPECT CORROSION BS 605 STR 4R LFEC + HFEC CARRIED OUT, NDF. VISUAL INSPECTION SHOWS CORROSION AT STR 4 BS 521-BS740. DAMAGE REMOVED IAW SRM 53 30 03. REPAIR PARTS FABRICATED IAW SRM 53 30 03. REPAIR INSTALLED IAW SRM 53 30 03. REPAIR CARRIED OUT IAW EO B727 5330 0509.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 57,411 hrs · 29,491 cycles

INSPECTION TYPE: C SUSPECTED CORROSION AT BS 1180 STR. 20R REPAIR CARRIED OUT IAW SRM 51-10-06, SRM 53-30-01 & 53-30-02. NEW STRINGER ENDS INSTALLED, FASTENERS INSTALLED IAW SRM 51-30-02. LAP REFASTENED IAW UPS EO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,411 hrs · 29,491 cycles

INSPECTION TYPE:C SUSPECT CRACK AT MID GALLEY DOOR UPPER HINGE CUT OUT REPAIR CARRIED OUT IAW SRM 51-10-2. SKIN REPAIR CARRIED OUT IAW SMRO EO 2003-038-004 UPS ENGINEERING FILE NO. B727-5330-18961.

Part: HINGE — CRACKED (RT MLG DOOR) · airframe 57,411 hrs · 29,491 cycles

INSPECTION TYPE: C, RT MLG BODY DOOR HINGE UNDER SAFETY BAR HAS SUSPECT CRACK. HFEC INSP CARRIED OUT THE ABOVE AREA IAW B727 NDTM PT 6 51-00-00 FIG 4. RESULT: CRACK CONFIRMED. HINGE HALF REMOVED IAW SRM 51-30-02. NEW HINGE HALF FITTED IAW SRM 51-30-02.

Part: SKIN — CORRODED (RT WING) · airframe 57,411 hrs · 29,491 cycles

INSPECTION TYPE:C SUSPECT CORROSION ON FIXED L-EDGE SKIN UPPER AFT SURFACE AT 2 LOCATIONS LE STA 345 AND 340 APPROX RT. REPAIR CARRIED OUT IAW SMRO EO 2003-038-007. UPS ENGINEERING FILE NO. 727-57-20106

Part: CHANNEL — CRACKED (LT WING) · airframe 57,006 hrs · 29,107 cycles

INSPECTION TYPE:C+SI CHANNEL ON LT WING REAR SPAR O/B OF NR 1 SPOILER CRACKED.

Part: HOUSING — CRACKED (CARGO BAY) · airframe 57,006 hrs · 29,107 cycles

INSPECTION TYPE:C+SI ON CLEANING OF 9G NET FITTINGS, FLOOR MOUNTED HOUSINGS X2 WERE FOUND TO BE CRACKED. HOUSING REPLACED IAW SRM 51-30-02 AND DWG 65-49366.

Part: PIN — CORRODED (LT WING) · airframe 57,006 hrs · 29,107 cycles

INSPECTION TYPE:C+SI LEFT BS 740 TERMINAL PIN IS CORRODED IN AREA UNDERNEATH HEAD, AND PIN RETAINING BOLT HAS PITTING CORROSION. LEFT BS 740 TERMINAL PIN AND RETAINING BOLT REPLACED IAW MM 57-41-04.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 57,006 hrs · 29,107 cycles

INSPECTION TYPE:C+SI FLOOR SUPPORT UNDER THIRD CREW MANS TABLE IS CRACKED AT ANCHOR NUT HOLE AND HAS NUMEROUS AREAS OF LIGHT SURFACE CORROSION, FLOOR SUPPORT IS LOCATED JUST AFT OF F/O O2 MASK STORAGE BOX. FLOOR SUPPORT Z-BRACKET LOCATED BETWEEN BS 258-277 LONGITUDINALLY AT RBL 44 APPROX.

Part: CASTING — CRACKED (T/E FLAP) · airframe 57,006 hrs · 29,107 cycles

INSPECTION TYPE:C+SI LT ELEPHANTS EAR FWD CASTING CRACKED ON MOUNT LUG. CASTING REPLACED IAW DWG NO65-26786.

Part: SILL — CORRODED (COCKPIT) · airframe 57,006 hrs · 29,107 cycles

INSPECTION TYPE:C EVIDENCE OF CORROSION ON R3 WINDOW SILL IN CONTROL CABIN (IE) LWR EXTRUDED ANGLE.

Part: ATTACH FITTING — CORRODED (FLAP TRACK) · airframe 57,006 hrs · 29,107 cycles

INSPECTION TYPE:C+SI ON REMOVAL OF NR 5 FLAP TRACK FWD ATTACH FITTING, PITTING CORROSION FOUND IN UPPER HOLE COMMON TO SPECIAL STUD ON TRUNNION SUPPORT FITTING.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 57,006 hrs · 29,107 cycles

INSPECTION TYPE:C+SI EXFOLIATION CORROSION ON THE UPPER CHORD FLANGE OF FLOORBEAM AT BS 480 LBL 25 TO 45.

Part: LAP JOINT — CORRODED (FUSELAGE) · airframe 57,006 hrs · 29,107 cycles

INSPECTION TYPE:C+SI SURFACE CORROSION ON UPPER SKIN AT LAP JOINT BS 210 STR 24L IN LOWER NOSE COMPT. LAP JOINT DE-RIVETED, CORROSION REMOVED, AREA OUTSIDE LIMITS CUT OUT, REPAIR PARTS FAB'D, HFEC C/W AND NDF, REPAIR INSTALLED IAW SRM 53-30-3 FIG 14 AND SRM 53-30-4 FIG 1.

Part: FITTING — CORRODED (FUSELAGE) · airframe 57,006 hrs · 29,107 cycles

INSPECTION TYPE:C+SI EVIDENCE OF CORROSION ON SEAT TRACK SECTION BS 868 LBL 45.5, SEAT TRACK SUPPORT LINK. FITTING REMOVED SRM 51-30-02, NEW FITTING INSTALLED IAW SRM 51-30-02.

Part: FITTING — CORRODED (FUSELAGE) · airframe 57,006 hrs · 29,107 cycles

INSPECTION TYPE:C+SI FRAME TO STRINGER CLEAT CORRODED AT BS 420 STR 18L IN THE E+E BAY. AREA OF CORROSION APPROX .75 INCH BY .5 INCH AND EXTENDED THROUGH THE CLEAT. R&R IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 57,006 hrs · 29,107 cycles

INSPECTION TYPE:C+SI INTERCOSTAL BETWEEN FLOORBEAMS AT BS 320 RBL 55 APPROX IN THE E/E BAY IS CRACKED.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 57,006 hrs · 29,107 cycles

INSPECTION TYPE:C+SI SUPPORT TANG CRACKED ON DELTA BEAM BS 760 LT. CRACKED TANG TRIMMED FLUSH WITH DELTA BEAM LOWER CHORD. HFEC CARRIED OUT NDF. REPAIR CARRIED OUT IAW SMRO EO 2001-057-011.

Part: FLAP TRACK — CORRODED (T/E FLAP) · airframe 57,006 hrs · 29,107 cycles

INSPECTION TYPE:C+CI NR 5 FLAP TRACK PITTING CORROSION IN BORE AND COUTERBORE OF AFT RT HOLE ON FWD MOUNT PAD. TRACK REPLACED IAW MM 27-51-31.

Part: FITTING — CORRODED (RT WING) · airframe 57,006 hrs · 29,107 cycles

INSPECTION TYPE:C+SI RT WING NR 8 FLAP TRACK SUPPORT FITTING (WING FITTING) HAS PITTING CORROSION ON INBOARD FACE. CORROSION REMOVED BY MACHINING, NDT COMPLIED WITH AND NDF. FLAP PEENED AND CADPLATED IAW OHM.

Part: FLAP TRACK — CORRODED (T/E FLAP) · airframe 57,006 hrs · 29,107 cycles

INSPECTION TYPE:C+SI NR 7 FLAP TRACK, PITTING CORROSION ON FWD SUPPORT LUG BORE LT LUG. BUSHING REMOVED AND CORROSION REMOVED BY MACHINING. NDT COMPLIED WITH AND NDF. BUSHING FABRICATED, HEAT TREATED, CADPLATED, POST BAKED AND INSTALLED.

Part: FITTING — CORRODED (FLAP TRACK) · airframe 57,006 hrs · 29,107 cycles

INSPECTION TYPE:C+SI NR 7 FLAP TRACK WING SUPPORT FITTING HAS PITTING CORROSION ON INBOARD FACE OF LUG. CORROSION REMOVED, NDT COMPLIED WITH AND NDF. FLAP PEENED AND CADPLATED IAW OHM.

Part: FLAP TRACK — CORRODED (T/E FLAP) · airframe 57,006 hrs · 29,107 cycles

INSPECTION TYPE:C+SI NR 4 FLAP TRACK PITTING CORROSION ON BORE OF AFT LT HOLE ON MLG SUPPORT BEAM PAD. FLAP TRACK REPLACED.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 57,006 hrs · 29,107 cycles

INSPECTION TYPE:C+SI ON REMOVAL OF DAMAGED BRACKET, FWD LWR DOOR STOP FITTING FOUND DAMAGED AND DOOR CUTOUT FRAME CRACKED AT LWR FWD FASTENER FITTING HOLE AFT CARGO DOOR CUTOUT FWD FRAME.

Part: FLAP TRACK — CORRODED (T/E FLAP) · airframe 57,006 hrs · 29,107 cycles

INSPECTION TYPE:C+SI NR 4 FLAP TRACK PITTING CORROSION ON FACE OF LANDING GEAR ATTACH PAD. LANDING GEAR ATTACH PAD MACHINED IAW OHM 57-40-01. TRACK REPLACED IAW MM 27-51-31.

Part: FLAP TRACK — CORRODED (T/E FLAP) · airframe 57,006 hrs · 29,107 cycles

INSPECTION TYPE:C+SI NR 1 FLAP TRACK HAS PITTING CORROSION ON LT FWD SUPPORT LUG OUTER FACE. CORROSION REMOVED BY MACHINING IAW OHM 57-40-01. NDT COMPLIED WITH AND NDF IAW SOPM 20-20-01, FLAP PEENED IAW SOPM 20-10-03, STRESS RELIEVED IAW SOPM 20-10-02, CADPLATED IAW SOPM 20-42-10.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 57,006 hrs · 29,107 cycles

INSPECTION TYPE:C+SI SURFACE CORROSION ON THE LWR SURFACE OF SEAT TRACK UPPER FLANGE AT BS 350 LBL 45.

Part: FLAP TRACK — CORRODED (T/E FLAP) · airframe 57,006 hrs · 29,107 cycles

INSPECTION TYPE:C+SI NR 2 FLAP TRACK PITTING CORROSION ON FACE OF FWD MOUNT PAD.

Part: FLAP TRACK — CORRODED (T/E FLAP) · airframe 57,006 hrs · 29,107 cycles

INSPECTION TYPE:C+SI NR 5 FLAP TRACK PITTING CORROSION ON AUX SPAR ATTACH PAD. TRACK REPLACED.

Part: WEB — CRACKED (NR 2 NACELLE) · airframe 57,006 hrs · 29,107 cycles

INSPECTION TYPE:C+SI VERTICAL LT WEB CRACKED OVER ENGINE NR 2 HORIZONTAL FIREWALL AT BS 1376 APPROX. WEB REPLACED IAW DWG 65-17555.

Part: SUPPORT BRACKET — CORRODED (WING) · airframe 57,006 hrs · 29,107 cycles

INSPECTION TYPE:C+SI SUPPORT BRACKET FOR LT FWD END OF NR 4 FLAP TRACK HAS PITTING CORROSION IN BORE OF HOLE.

Part: FLAP TRACK — CORRODED (T/E FLAP) · airframe 57,006 hrs · 29,107 cycles

INSPECTION TYPE:C+SI NR 6 FLAP TRACK PITTING CORROSION ON FACE OF AUX SPAR PAD. CORROSION REMOVED BY MACHINING IAW OHM 57-40-01. NDT COMPLIED WITH NDF SOPM 20-20-01, FLAP PEENED IAW SOPM 20-10-03, STRESS RELIEVED IAW SOPM 20-10-02, CADPLATED IAW SOPM20-42-10.

Part: FLAP TRACK — CORRODED (T/E FLAP) · airframe 57,006 hrs · 29,107 cycles

INSPECTION TYPE:C+SI NR 5 FLAP TRACK, PITTING CORROSION IN BORE AND COUNTER BORE OF AFT LT HOLE ON FWD PAD. TRACK REPLACED IAW MM 27-51-31.

Part: FLAP TRACK — CORRODED (T/E FLAP) · airframe 57,006 hrs · 29,107 cycles

INSPECTION TYPE:C+SI NR 4 FLAP TRACK, PITTING CORROSION ON BORE OF HOLE C AND ON COUNTER BORE OF HOLE C. TRACKS REPLACED.

Part: BRACKET — CRACKED (T/E FLAP) · airframe 57,006 hrs · 29,107 cycles

INSPECTION TYPE:C+SI NR 4 FLAP TRACK CRACK IN FAIRING SUPPORT BRACKET FWD LT . BRACKET FABRICATED AND REPLACED IAW SRM.

Part: WEB — CRACKED (NR 2 NACELLE) · airframe 57,006 hrs · 29,107 cycles

INSPECTION TYPE:C+SI VERTICAL RT WEB CRACKED OVER ENGINE 2 HORIZONTAL FIREWALL AT BS 137 6 APPROX. WEB REPLACED IAW DWG 65-17555.

Part: FLAP TRACK — CORRODED (T/E FLAP) · airframe 57,006 hrs · 29,107 cycles

INSPECTION TYPE:C+SI NR 4 FLAP TRACK PITTING CORROSION ON AUX SPAR PAD. CORROSION ON PAD REMOVED BY MACHINING IAW OHM 57-40-01. TRACK REPLACED IAW 27-51-31.

Part: RIB — CRACKED (ELEVATOR) · airframe 57,006 hrs · 29,107 cycles

INSPECTION TYPE:C+SI CRACK IN ELEV SUPPORT RIB, O/B LWR AFT FLANGE AT ST 173.21 RT. RIB REPLACED.

Part: FLAP TRACK — CORRODED (T/E FLAP) · airframe 57,006 hrs · 29,107 cycles

INSPECTION TYPE:C+SI NR 8 FLAP TRACK, PITTING CORROSION ON OUTER FACE OF FWD SUPPORT LUG LT. CORROSION REMOVED BY MACHINING, NDT COMPLIED WITH NDF FLAP PEENED IAW OHE AND CADPLATED IAW OHM.

Part: FLAP TRACK — CORRODED (T/E FLAP) · airframe 57,006 hrs · 29,107 cycles

INSPECTION TYPE:C+S,I NR 3 FLAP TRACK PITTING CORROSION ON AUX SPAR ATTACH PAD.

Part: FLAP TRACK — CORRODED (L/E FLAP) · airframe 57,006 hrs · 29,107 cycles

INSPECTION TYPE:C+SI, NR 7 FLAP TRACK LOOSE BUSHING ON FWD SUPPORT LUG RT, LOOSE BUSHING REMOVED AND BORE FOUND CORRODED. PITTING CORROSION REMOVED BY MACHINING IAW SOPM 20-10-02. NDT C/W NDF. BUSHING FAB'D THEN HEAT TREATED, CADPLATED, POSTBAKED AND INSTALLED.

Part: FLAP TRACK — CORRODED (T/E FLAP) · airframe 57,006 hrs · 29,107 cycles

INSPECTION TYPE:C+SI PITTING CORROSION ON INNER FACE OF FWD SUPPORT LUG LT NR 7 FLAP TRACK. CORROSION REMOVED BY MACHINING NDT COMPLIED WITH AND NO DEFECTS WERE FOUND. FLAP PEENED AND CADPLATED IAW OHM.

Part: FLAP TRACK — CORRODED (T/E FLAP) · airframe 57,006 hrs · 29,107 cycles

INSPECTION TYPE:C+SI NR 8 FLAP TRACK, PITTING CORROSION FOUND ON INNER FACE OF FWD SUPPORT LUG LT. CORROSION REMOVED BY MACHINING, NDT COMPLIED WITH AND NDF. FLAP PEENED AND CADPLATED IAW OHM.

Part: CARRIAGE — CORRODED (T/E FLAP) · airframe 57,006 hrs · 29,107 cycles

INSPECTION TYPE:C+SI PITTING CORROSION IN FLT ROLLER BEARING MOUNT HOLES NR 1 FLAP CARRIAGE. CARRIAGE REPLACED IAW OHM 57-52-11.

Part: RIB — CRACKED (ELEVATOR) · airframe 57,006 hrs · 29,107 cycles

INSPECTION TYPE:C+SI CRACK IN ELEVATOR SUPPORT RIB AT ELEVATOR STA 17.20 LEFT I/B UPPER FLANGE. RIB REPLACED.

Part: CRANKSHAFT — CORRODED (AILERON) · airframe 57,006 hrs · 29,107 cycles

INSPECTION TYPE:C AILERON PCU INPUT CRANK IN LT WHEEL WELL IS BADLY CORRODED AROUND PIVOT BOLT. PCU INPUT CRANK REPLACED IAW OHM 27-40-00 & OHM 29-00-00.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,006 hrs · 29,107 cycles

INSPECTION TYPE:C+SI FRAME CRACKED AT BS 540 STR STR 18L ADJACENT TO MCD LATCH SUPPORT FITTING. DAMAGED AREA CUT OUT AND REPAIR PARTS FABRICATED, REPAIR PARTS INSTALLED.

Part: CARRIAGE — CORRODED (T/E FLAP) · airframe 57,006 hrs · 29,107 cycles

INSPECTION TYPE:C+SI NR 2 FLAP CARRIAGE HAS CORROSION INSIDE SPINDLE BORE CORROSION CONFINED TO SPINDLE BORE, NOT POSSIBLE TO MEASURE EXTENT. CARRIAGE REPLACED AS NO REPAIR POSSIBLE IAW 57-52-01.

Part: CARRIAGE — CORRODED (T/E FLAP) · airframe 57,006 hrs · 29,107 cycles

INSPECTION TYPE:C+SI CORROSION ON INNER BORE OF NR 8 FLAP CARRIAGE SPINDLE, AND ON END OF SPINDLE UNDER BEARING. CARRIAGE ASSY REPLACED IAW OHM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,006 hrs · 29,107 cycles

INSPECTION TYPE:C+SI FRAME CRACKED AT BS 487.1 AT STR 19L ADJACENT TO LATCH SUPPORT FITTINGS. CRACKED AREA CUT OUT, REPAIR PARTS FABRICATED, PARTS INSTALLED AND VERTICAL STIFFENER INSTALLED.

Part: SKIN — CORRODED (FUSELAGE) · airframe 57,006 hrs · 29,107 cycles

INSPECTION TYPE:C+SI RIVET HEAD POPPED AT STR 4R AT BS 710 APPROX. REPAIR CARRIED OUT IAW SRM.

Part: BUSHING — CORRODED (RT WING) · airframe 57,006 hrs · 29,107 cycles

INSPECTION TYPE:C+SI, RT WING REAR TERMINAL FORGING FWD BUSHING IS CORRODED. RETAINER REPLACED IAW MM 57-41-11, BUSHING REPLACED IAW OHM20-50-03.

Part: CARRIAGE — CORRODED (T/E FLAP) · airframe 57,006 hrs · 29,107 cycles

INSPECTION TYPE:C+SI CORROSION ON FLT ROLLER BEARING MOUNT HOLE NR 5 FLAP CARRIAGE. CARRIAGE ASSY REPLACED IAW OHM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,006 hrs · 29,107 cycles

INSPECTION TYPE:C+SI FRAME CRACKED AT BS 500 AT STR 18L ADJACENT TO LATCH SUPPORT FITTINGS. REPAIR PARTS FABRICATED AND DAMAGED AREA CUT OUT. REPAIR PARTS INSTALLED IAW SRM, VERTICAL STIFFENER INSTALLED.

Part: CARRIAGE — CORRODED (T/E FLAP) · airframe 57,006 hrs · 29,107 cycles

INSPECTION TYPE:C+SI CORROSION ON INNER SPINDLE BORE OF NR 7 FLAP CARRIAGE SPINDLE. REPLACED CARRIAGE ASSY IAW OHM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,006 hrs · 29,107 cycles

INSPECTION TYPE:C+SI FRAME CRACKED AT BS 580 ATR STR 18L, ADJACENT TO MCD LATCH SUPPORT FITTINGS. CRACKED AREA CUT OUT AND REPAIR PARTS FABRICATED, REPAIR PARTS INSTALLED.

Part: MOUNT — CORRODED (NR 3 ENGINE) · airframe 57,006 hrs · 29,107 cycles

INSPECTION TYPE:C+SI NR 3 ENGINE FWD MOUNT FWD OUTBOARD HOLE HAS PITTING CORROSION ON INSIDE OF BORE.

Part: MOUNT — CORRODED (NR 1 ENGINE) · airframe 57,006 hrs · 29,107 cycles

INSPECTION TYPE:C=SI NR 1 ENGINE FWD TRUNNION MOUNT AFT OUTBOARD HOLE HAS PITTING CORROSION IN BORE OF HOLE.

Part: SPAR — CORRODED (CENTER WING) · airframe 57,006 hrs · 29,107 cycles

INSPECTION TYPE:C+SI WING CENTER SECTION FRONT SPAR UPPER CHORD HAS CORROSION AT RT END OF CHORD AT RBL 55 APPROX. FOUND TO BE EXFOLIATED.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,006 hrs · 29,107 cycles

INSPECTION TYPE:C+SI SUSPECT CRACK IN MLG WW STRUCTURE AT BS 910 FWD FLANGE BELOW MLG CEILING. REPAIRED IAW EO B727-5310-1896B.

Part: FITTING — CORRODED (FUSELAGE) · airframe 57,006 hrs · 29,107 cycles

INSPECTION TYPE:C+SI VERTICAL FLANGE OF RT 740 FITTING AT I/B END HAS CORROSION. REPLACED FITTING IAW UPS EO B727-5310-7477 E AND DWG 65C13724.

Part: FITTING — CORRODED (FUSELAGE) · airframe 57,006 hrs · 29,107 cycles

INSPECTION TYPE:C+SI VERTICAL FLANGE OF LT 740 FITTING AT I/B END HAS CORROSION. LT 740 FITTING REPLACED IAW UPS EO B727-5310-7477E APPB AND DWG 65C 13724.

Part: UNKNOWN — ODOR (COCKPIT)

SMOKE ODOR IN FLT DECK AREA. RAN ALL 3 ENGINES AND OPERATED ALL PACKES AT FULL HOT AND COLD. COULD NOT DUPLICATE. OPERATED ALL NAV AND COMM EQUIPMENT. NO DEFECTS NOTED. OK TO CONTINUE SERVICE

Part: FIRE BOTTLE — LOW (CARGO BAY)

INSPECTION TYPE:N/A, PORTABLE CARGO COMP FIRE EXTINGUISHER BELOW LIMITS. REMOVED AND REPLACED FIRE BOTTLE.

Part: APU — OVERSERVICED (FUSELAGE)

INSPECTION TYPE:N/A, AFTER RUNNING PACK ON COCKPIT FILLED WITH SMOKE. SHUTDOWN PACK, SMOKE STARTED TO DISSIPATE. SMELLED LIKE BURNING OIL. *S/D* FOUND APU OVER SERVICED OPERATED PACK COOL AND HOT. NO PROBLEM NOTED.

Part: SUPPORT FITTING — CORRODED (LT WING) · airframe 57,006 hrs · 29,107 cycles

INSPECTION TYPE:C+SI LT WING SUPPORT BRACKET FOR NR 3 FLAP TRACK FWD END HAS PITTING CORROSION ON RT FACE OF LUG.

Part: BATTERY PACK — INOPERATIVE (CABIN)

INSPECTION TYPE:N/A, EMERGENCY EXIT LIGHTS (2) NEED NEW BATTERIES. INSTALLED NEW BATTERIES IN BOTH EMERGENCY EXIT LIGHTS, OPS CHECK GOOD.

Part: SKIN — CORRODED (FUSELAGE)

INSPECTION TYPE:C AFT FUSELAGE BS 1343 EXTERIOR SKIN LEFT CORNER OF AFT AIRSTAIR OPENING SURFACE CORROSION AND PULLING RIVETS. CUT OUT DAMAGED SECTION OF SKIN FROM BS 1343 - 1333. INSTALLED SKIN AND DOUBLER REPAIR, MATERIAL USED 7075-T6, 0.032, 28 X 10, IN ACCORDANCE WITH SRM 51-30-2 AND 51-40-2.

Part: LAP JOINT — CORRODED (FUSELAGE)

INSPECTION TYPE:C BULGING OF LONGITUDINAL SKIN LAP SPLICE AT STRINGER 4 RIGHT, BS 820 - 848. CUT OUT DAMAGE AT UPPER AND LOWER SKIN AREAS, STA 826 - 835 STR 4 RIGHT. INSTALLED FLUSH REPAIR AT SKIN LAP JOINT, MATERIAL USED FOR DOUBLER: 2024-T3, 0.071, 18 X 12. ACCOMPLISHED IN ACCORDANCE WITH SRM 53-3 0-3 FIGURE 6.

Part: SKIN — DENTED (HORIZ STAB)

RT HORIZNATAL STAB HAS DENTS WHICH ARE OUT OF LIMITS. REINSPECTED DENT AREA, DENT FOUND TO BE WITHIN LIMITS PER SRM 55-105 1.

Part: SKIN — DENTED (LE FLAP)

NR 1 SLAT HAS DENTS WHICH ARE OUT OF LIMITS. COMPLIED WITH EO B727-5740-1259.

Part: SKIN — CORRODED (RT AILERON)

INSPECTION TYPE-C, RT OUTBOARD AILERON HAS CORROSION ON LOWER SKIN AFT OF NR 2 HINGE AREA. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. REPLACED RT OUTBOARD AILERON IAW MM 27-10-31.

Part: FITTING — CORRODED (LT AILERON)

INSPECTION TYPE-C, LT WING I/B AILERON TURN-AROUND PULLEY FITTING AT PULLEY BOLT HOLE IS CORRODED. REMOVED CORRODED PULLEY FITTING, DRILLED UP NEW FITTING AND INSTALLED IAW MM 20-10-20, SRM 51-30-05, 51-30-02.

Part: FITTING — CRACKED (LT MLG)

INSPECTION TYPE-C, CRACK INDICATIONS NOTED LT MLG FWD TRUNNION BEARING SUPPORT FITTING. REMOVED AND REPLACED LT MLG TRUNNION BEARING SUPPORT FITTING IAW OHM 32-10-13. WHILE WORKING SUPPORT FITTING FOUND THE TRUNNION LINK TO BE CORRODED. REPLACED TRUNNION LINK IAW MM 32-11-01.

Part: TAB — DELAMINATED (RUDDER)

INSPECTION TYPE-C, UPPER RUDDER TAB DELAMINATED. REPAIRED UPPER RUDDER TAB IAW SRM 51-40-6.

Part: BEAM — CRACKED (PAX DOOR)

INSPECTION TYPE-C, WHILE WORKING NRC 715333 FOUND FED LOWER GATE BEAM CRACKED AFT SIDE I/B RADIUS. REMOVED AND REPLACED FED LOWER GATE BEAM IAW SRM 51-30-102, 51-30-2, AND 51-10-1.

Part: CASTING — CRACKED (PAX DOOR)

INSPECTION TYPE-C, UPON REMOVAL OF FWD ENTRY DOOR FOUND UPPER AND LOWER FUSELAGE TORQUE TUBE CASTINGS CRACKED. REPLACED CRACKED UPPER AND LOWER CASTINGS WITH NEW PARTS PER SRM 51-30-2 AND SRM 52-11-32.

Part: ANGLE — CRACKED (BS 620)

INSPECTION TYPE-C, WHILE WORKING INTERIOR 55 CUST ID 715443, DISCOVERED SUPPORT ANGLE AT BS 620 BELOW AFT CAM LATCH HOOK TO BE CRACKED WL 210. REMOVED, FABRICATED AND INSTALLED PER SRM 51-20-1, 51-10-2, 51-20-141.

Part: FITTING — CORRODED (WS 600)

INSPECTION TYPE-C, LT WING O/B AILERON LOCKOUT FITTING IS CORRODED UNDER LOCKOUT GEARBOX MOUNT BOLTS. REMOVED CORROSION AND FOUND OUT OF LIMITS AND REPLACED FITTING IAW SRM 51-30-2, 51-10-6, 27-10-121, 27-10-131.

Part: RETRACT MECH — LACK OF LUBE (NLG)

INSPECTION TYPE-N/A, ON INITIAL GEAR EXTENSION NOSE GEAR RED LIGHT ILLUMINATED AND NO GREEN NOSE GEAR LIGHT. FIRST RECYCLE GAVE SAME INDICATIONS, 2ND ATTEMPT CONDUCTED WITH CHECKLIST STEPS AND GREEN LIGHT ILLUM, THOUGH GREEN LIGHT WOULD DIMLY FLICKER. MANUAL EXTENSION. *S/D* LUBED NLG LOCKING MECHANISM, CLEANED SEQUENCE VALVE AND INDICATION C ANNON PLUGS, CK'D NOSE GEAR EXTENSION AND PERFORMED NOSE GEAR EXTENS ION AND RETRACTION ADJUSTMENT TEST WITH REFERENCE TO MM 32-33-00 PG 501. NOSE GEAR OPS CKS GOOD.

Part: LIGHT — INOPERATIVE (CREW ENTRY)

INSPECTION TYPE-N/A, EMERG EXIT LIGHT OVER CREW ENTRY DOOR IS INOP. REMOVED AND REPLACED 2 EMERG EXIT LIGHT BATTERIES, GRD CHECKS OK. P/N OFF/ON S106 LOT NR S106 DUE DATES 3-2-98.

Part: SKIN — CORRODED (BS 1123-1143)

INSPECTION TYPE-SV, STR 4R BETWEEN BS 1123 AND BS 1143, SKIN LAP HAD CORROSION BULGING EXCESSIVE SEALANT. REPAIRED IAW SRM 53-30-01.

Part: LIGHT — INOPERATIVE (COCKPIT)

COCKPIT EMERGENCY LIGHT INOPERATIVE. DEAD BATTERY. REMOVED AND REPLACED EMERERGENCY LIGHT ASSY IAW MM 256000. OPS CK NORMAL.

Part: LIGHT — INOPERATIVE (FLIGHT CABIN)

CREW EMERGENCY EXIT LIGHT INOPERATIVE. DEAD BATTERY. REMOVED AND REPLACED EMERGENCY EXIT LITE ASSY IAW M/M 25-60-00, OPS CHECK NORMAL.

Part: SKIN — CORROSION (STA 304)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED CORROSION ON SKIN AT STA 304 STR 14R, OUT OF LIMITS. REMOVED DAMAGED AREA IAW SRM 53-30-3. FABRICATED AND INSTALLED REPAIR IAW SRM 53-30-3 FIG 5.

Part: FLOOR BEAM — CORROSION (FS 640)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED FWD LOWER CARGO STA 640 BETWEEN LBL 44 TO 62. FLOOR BEAM UPPER FLANGE AFT SIDE HAS HEAVY EXFOLIATION CORROSION IN SEVERAL PLACES. REPAIRED DAMAGE AREA OF FLOOR BEAM LBL 8 TO LBL 62 IAW SRM 53-10-8 FIG 5, SRM 51-30-2.

Part: STRINGER — CORRODED (BS 455-460)

WHILE IN FOR D-CHECK, MAINTENANCE REPORTED STR 22L CORRODED FROM STA 440 TO STA 460 REMOVED BEYOND LIMITS. CORROSION REPAIRED AT STRINGER FROM STA 443-468 I.A.W. SRM 53-10-3.

Part: STRINGER — CORROSION (BS 1166-1183)

WHILE IN FOR D-CHECK, MAINTENANCE REPORTED LAP AT STA 1166-1183 AT STR 10R OUT OF LIMITS. REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS, AND INSTALLED REPAIR PER SRM 53-30-3 AND SRM 51-30-5.

Part: ATTACH CHANNEL — CRACKED (BS 312)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED FUS STA 312 STR 19R, STRINGER TO FRAME ATTACH CHANNEL IS CRACKED. REMOVED, FABRICATED AND INSTALLED ATTACH CHANNEL PER SRM 53-10-2 AND 51-30-2.

Part: SKIN — CORRODED (FS 1080)

WHILE IN FOR D-CHECK, MAINTENANCE REPORTED FUSELAGE SKIN UPPER LAP CORRODED BEYOND LIMITS AT STR 10R, FROM FS 1080-1122. REMOVED DAMAGE PER SRM 53-30-03 AND INSTALLED CONICAL WASHERS PER SRM 51-30-5 AND INSTALLED REPAIR PARTS PER SRM 51-30-5.

Part: STRINGER — CORROSION (FS 1160)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED CORROSION BEYOND LIMITS AT STR 22R FS 1160 REF N/R 429045 FOR CORROSION REMOVAL. CUT OUT WAS MADE FROM STA 1158 TO STA 1173 STR 22R. FABRICATED SPLICE SECTION PER SRM 53-10-3 FIG 1 AND INSTALLED PARTS PER SRM 51-30-2.

Part: STRINGER — CORROSION (BS 440)

WHILE IN FOR D-CHECK, MAINTENANCE REPORTED FS 420-440, STR 9L, HAS CORROSION UNDER EDGE OF LAP AND FS 440, STR 8L-10L HAS CORROSION UNDER CIRCUMFERENTIAL JOINT ON FORWARD SIDE. REPAIRED PER SRM 51-30-2, 51-10-6, 51-20-4 AND DWG NR 69-62161.

Part: SEAT TRACK — CORROSION (BS 929)

WHILE IN FOR D-CHECK, MAINTENANCE REPORTED MAIN CABIN SEAT TRACK AT RBL 62, BS 929 TO 932 HAS EXFOLIATION CORROSION. REMOVED DAMAGED SECTION OF TRACK, ALODINED AND PRIMED AND FASTENED PER SRM 51-10-2, 51-30-2, AND 53-10-5.

Part: INTERCOSTAL — CRACKED (BS 1148-1160)

WHILE IN FOR D-CHECK, MAINTENANCE REPORTED INTERCOSTAL CRACKED AT STA 1148-1166 AND STR 22R. REMOVED, FABRICATED, AND INSTALLED INTERCOSTAL PER SRM 53-10-2 AND SRM 53-30-2.

Part: FLOOR BEAM — CORRODED (FS 680)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED FS 680 RBL 3 TO 10, FLOOR BEAM UPPER FLANGE IS CORRODED BEYOND LIMITS. REMOVED DAMAGED SECTION FROM LBL 9 TO RBL 65.0 IAW SRM 53-10-8 FIG 5, REPAIRED IAW SRM 53-10-8 AND 51-30-3.

Part: STRINGER — CORRODED (BS 440-460)

WHILE IN FOR D-CHECK, MAINTENANCE REPORTED STA 440-460, STR 18L HAS CORROSION. REMOVED DAMAGED AREA AND INSTALLED REPAIR PARTS PER SRM 53-10-3 AND SRM 51-30-2.

Part: INTERCOSTAL — CORRODED (BS 294.5)

WHILE IN FOR D-CHECK, MAINTENANCE REPORTED INTERCOSTAL HAS CORROSION ABOVE LAV SERVICE PANEL TO FRAME 294.5 AND 518R. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT LATCH CHANNEL PER SRM 51-10-1 AND SRM 51-30-2.

Part: SKIN — CORROSION (BS 580)

WHILE IN FOR D-CHECK, MAINTENANCE REPORTED CORROSION ON SKIN BELOW FLOOR STA 580, STR 17R. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED DOUBLER PER BOEING SRM 51-40-2 AND 51-30-2.

Part: STRINGER — CORROSION (BS 1050)

WHILE IN FOR D-CHECK, MAINTENANCE REPORTED CORROSION ON STR 19L, STA 1050. CORROSION OUT OF LIMITS. INSTALLED REPAIR PARTS PER BOEING SRM 53-10-3. CORROSION REMOVED PER SRM 57-10-6.

Part: SHEAR TIE — CRACKED (BS 294.5)

WHILE IN FOR D-CHECK, MAINTENANCE REPORTED FUSELAGE FRAME SHEAR TIE IS CRACKED NEAR THE RADIUS UPPER END BETWEEN S20R AND S21R, BS 294.5. REMOVED DAMAGED AREA PER SRM 51-40-3. FABRICATED ANGLE AND REPAIRED PER SRM 51-30-2.

Part: FRAME CLIP — CRACKED (FS 328)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED FRAME CLIP CRACKED AT STA 328 STR 13R. CUT OUT DAMAGED FRAME SECTION IAW SRM 53-10-4, FABRICATED NEW FRAME/SPLICES IAW SRM 53-10-4 AND INSTALLED IAW SRM 53-10-4 AND 51-30-2.

Part: INTERCOSTAL — CRACKED (BS 304)

WHILE IN FOR D-CHECK, MAINTENANCE REPORTED CABIN FLOOR INTERCOSTAL UPPER OUTBOARD FLANGE HAS A 1.5 INCH CRACK AT RBL 44 AND BS 304 UNDER FORWARD LAV. REMOVED DAMAGED AREA PER SRM 51-40-3, FABRICATED AND INSTALLED FILLER AND REPAIR ANGLE PER SRM 51-10-2, 51-30-2, AND 51-40-3.

Part: ANGLE — CORRODED (BS 295.5-267)

WHILE IN FOR D-CHECK, MAINTENANCE REPORTED NLG LT TUNNEL, STA 295.5 TO STA 267 C/P SUB-FLOOR SUPPORT ANGLE HAS SEVERE CORROSION. REMOVED DAMAGED AREA, FABRICATED, AND INSTALLED T-ANGLE REPAIR PER BOEING SRM 51-40-2, 51-40-4, AND 51-30-2.

Part: STRINGER — CORRODED (BS 1030-1060)

WHILE IN FOR D-CHECK, MAINTENANCE REPORTED CORROSION ON STR 20R, STA 1030-1060. CUT OUT DAMAGED AREA PER SRM 53-10-3. REPLACED STR 20R FROM STA 1040-1060 AND INSTALLED SPLICE AT STA 1020-1030, STR 20R I.A.W. SRM 53-10-3, FIG. 4, AND SRM 51-30-2.

Part: SPLICE — CORROSION (BS 1070)

WHILE IN FOR D-CHECK, MAINTENANCE REPORTED CORROSION ON STR SPLICE 20L, STA 1070-1090. FABRICATED AND INSTALLED STR SECTION AND SPLICES PER BOEING SRM 53-10-3 AND 51-30-2.

Part: SKIN — CRACKED (BS 520)

WHILE IN FOR D-CHECK, MAINTENANCE REPORTED FS 520, STR 23R, LOWER FORWARD CARGO DOOR SKIN CRACKED. REMOVED DAMAGED AREA AND INSTALLED REPAIR PARTS I.A.W. DHC SK-940-271 AND SRM 51-30-2.

Part: FITTING — CORROSION (RT REAR SPAR)

WHILE IN FOR D-CHECK, MAINTENANCE REPORTED CORROSION AROUND BUSHING IN FITTING, FORWARD SIDE OF RT WING REAR SPAR FOR ATTACHMENT OF MLG SUPPORT BEAM. REMOVED AND REPAIRED FITTING NR 65-16290 PER BOEING DWG NR 65-16290 AND SRM 51-30-2.

Part: CLIP — CORRODED (BS 360)

WHILE IN FOR D-CHECK, MAINTENANCE REPORTED STRINGER CLIP AT BS 360 AND STRINGER 1 IS CORRODED. REMOVED AND REPLACED CLIP I.A.W. SRM 51-30-2.

Part: STIFFENER — CORROSION (WS 171)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED RT FRONT SPAR VERTICAL STIFFENER INB OF NR 3 TANK FUELING VALVE HAS CORROSION AT BONDING WIRE. REMOVED DAMAGED STIFFENER, FABRICATED REPLACEMENT STIFFENER IAW SRM 51-10-1 AND INSTALLED IAW SRM 51-30-2.

Part: SPAR — CRACKED (WS 304)

WHILE IN FOR D-CHECK, MAINTENANCE REPORTED RT WING REAR SPAR UPPER CHORD CRACKED AT W.S. 304 ABOVE MLG SUPPORT BEAM ATTACH FITTING. CUT OUT DAMAGE AREA, FABRICATED REPAIR PARTS PER BOEING DWG 65C21546, 65-16233 AND SRM 51-30-2.

Part: FITTING — CRACKED (MAIN CARGO DOOR)

WHILE IN FOR D-CHECK, MAINTENANCE REPORTED MAIN DOOR LATCH SUPPORT FITTING CRACKED B/S 560, REF N/R 428722. REMOVED AND REPLACED CARGO DOOR LATCH SUPPORT FITTING PER DHC SK-940-769 AND SRM 51-30-2.

Part: SWITCH MECH — MISSING (RT MLG DOOR)

CREW REPORTED, AFTER TAKEOFF, GEAR IN OFF POSITION, GEAR DOOR LIGHT ILLUMINATED, GEAR CYCLED LIGHT REMAINED ON, CONTACTED MAINTENANCE. REMAINDER OF FLIGHT FLOWN WITH GEAR HANDLE UP, LIGHT GIBSON WAS OFF. FOUND BUSHING, RT MAIN LANDING DOOR SWITCH MECHANISM MISSING. INSTALLED SAME PER 727-MM 32-62-11.

Part: ACT CONNECTOR — DIRTY (TAIL SKID)

CREW REPORTED, TAIL SKID WOULD NOT RETRACT. RECYCLED GEAR, TAIL SKIRT THEN CAME UP. CLEANED CONNECTION ON TAIL SKID ACTUATOR, CHECK OK IAW 32-71-01 PAGE 501.

Part: BATTERY — DISCHARGED (CABIN)

WHILE ON GROUND, MAINTENANCE FOUND EMERGENCY EXIT LIGHTS OVER THE FORWARD ENTRY DOOR INOP. MAINTENANCE REMOVED AND REPLACED FWD ENTRY DOOR EMERGENCY LIGHTING BATTERIES, OPS CK GOOD.

Part: EEL BATTERIES — DISCHARGED (CABIN)

WHILE ON GROUND, MAINTENANCE FOUND EMERGENCY LIGHTS OVER FLIGHT DECK AND FWD ENTRY DOOR INOP. REPLACED BATTERIES, OPS CHECK OK.

Part: CONTROL VALVE — MALFUNCTIONED (LANDING GEAR)

FELT RESTRICTION OF GEAR HANDLE DURING RETRACTION. CYCLED GEAR, SAME RESPONSE. REPLACED GEAR CONTROL VALVE.

Part: EEL BATTERY PACK — DISCHARGED (FLIGHT DECK)

MAINTENANCE REPORTED EMERGENCY EXIT LIGHTS INOP IN FLIGHT DECK. REPLACED BATTERY PACK PER MM 33-50-101. OPS CHECK OK.

Part: FRAME — CRACKED (GALLEY DOORWAY)

WHILE IN 'C' CHECK, MAINTENANCE FOUND MID GALLEY DOORWAY FORWARD UPPER FRAME SEGMENT CRACKED TOP I/B CORNER STA 636. INSTALLED REPAIR IAW SRM 51-10-1, 51-10-02, 51-30-2 AND MM 51-20-151.

Part: STRINGER — CRACK (BS 294.5)

WHILE IN 'C' CHECK, MAINT FOUND STR 15 AT BS 294.5 LEFT SIDE HAS A CRACK AT THE UPPER FLANGE ATTACH POINT LEFT SIDE. X-RAY NR 14-15 LEFT. INSTALLED REPAIR IAW EO 727-5310-1259F.

Part: FAILSAFE STRAP — CRACKED (BS 294)

WHILE IN 'C' CHECK, MAINTENANCE FOUND I/B AND O/B FAILSAFE STRAPS TO BE CRACKED AT BS 294, WL 215 APPROX. LBL 50. INSTALLED REPAIR IAW UPS FILE NR 727-53-1459.

Part: SKIN — CORRODED (PANEL 7204)

DURING 'C' CHECK, MAINTENANCE FOUND CORROSION AROUND FUEL CELL ACCESS CUT OUT FOR PANEL 7204. REPAIRED PER UPS ENGINEERING FILE NUMBER 727-57-1068, 727-57-1074.

Part: SKIN — CRACKED (FS 1155)

DURING 'C' CHECK, MAINTENANCE FOUND SKIN CRACKED AT STA 1155 BETWEEN STR 20-21L. FABRICATED AND INSTALLED REPAIR PER SRM 51-30-2, 51-30-8, 53-30-3.

Part: SKIN — CORRODED (PANEL 7608)

DURING 'C' CHECK, MAINTENANCE FOUND CORROSION AROUND FUEL CELL ACCESS CUT OUT FOR PANEL 7608. REPAIRED PER UPS ENGINEERING FILE NUMBER 727-57-1068, 727-57-1074.

Part: FLOOR SUPPORT — CORRODED (FS 756)

DURING 'C' CHECK, MAINTENANCE FOUND CORROSION ON FLOOR SUPPORT AT NUT PLATE AT STA 756, LBL 45-60. FABRICATED AND INSTALLED REPAIR PER SRM 53-10-1, 51-30-2.

Part: SKIN — CORRODED (PANEL 7610)

DURING 'C' CHECK, MAINTENANCE FOUND CORROSION AROUND FUEL CELL ACCESS CUT OUT FOR PANEL 7610. REPAIRED PER UPS ENGINEERING FILE NUMBER 727-57-1068, 727-57-1074.

Part: SKIN — CORRODED (PANEL 7602)

DURING 'C' CHECK, MAINTENANCE FOUND CORROSION AROUND FUEL CELL ACCESS CUT OUT FOR PANEL 7602. REPAIRED PER UPS ENGINEERING FILE NUMBER 727-57-1068, 727-57-1074.

Part: SKIN — CORRODED (PANEL 7606)

DURING 'C' CHECK, MAINTENANCE FOUND CORROSION AROUND FUEL CELL ACCESS CUT OUT FOR PANEL 7606. REPAIRED PER UPS ENGINEERING FILE NUMBER 727-57-1068, 727-57-1074.

Part: SKIN — CORRODED (PANEL 7208)

DURING 'C' CHECK, MAINTENANCE FOUND CORROSION AROUND FUEL CELL ACCESS CUT OUT FOR PANEL 7208. REPAIRED PER UPS ENGINEERING FILE NUMBER 727-57-1068, 727-57-1074.

Part: FLOOR SUPPORT — CORRODED (FS 848)

DURING 'C' CHECK, MAINTENANCE FOUND CORROSION ON FLOOR SUPPORT AT NUT PLATE AT STA 848, LBL 40, WL 208. FABRICATED AND INSTALLED REPAIR PER SRM 53-10-1, 51-30-2, 51-10-1.

Part: FRAME — CORRODED (FS 760)

DURING 'C' CHECK, MAINTENANCE FOUND CORROSION ON FRAME AT STA 760, LBL 65-70, WL 208. FABRICATED AND INSTALLED REPAIR PER SRM 51-10-2, 51-10-6, 51-30-2, AND UPS ENGINEERING FILE NUMBER 727-53-1456.

Part: SKIN — CORRODED (PANEL 7207)

DURING 'C' CHECK, MAINTENANCE FOUND CORROSION AROUND FUEL CELL ACCESS CUT OUT FOR PANEL 7207. REPAIRED PER UPS ENGINEERING FILE NUMBER 727-57-1068, 727-57-1074.

Part: SEAT TRACK — CORRODED (FS 780-820)

DURING 'C' CHECK, MAINTENANCE FOUND CORROSION ON SEAT TRACK AT STA 780-820, RBL 45, WL 208. REPLACED SEAT TRACK PER SRM 51-30-02, 51-10-1.

Part: SEAT TRACK — CORRODED (FS 756-852)

DURING 'C' CHECK, MAINTENANCE FOUND CORROSION ON SEAT TRACK AT STA 756-852, LBL 65. REPLACED SEAT TRACK PER SRM 51-30-02, 51-10-2, 51-20-4.

Part: SKIN — CORRODED (PANEL 7210)

DURING 'C' CHECK, MAINTENANCE FOUND CORROSION AROUND FUEL CELL ACCESS CUT OUT FOR PANEL 7210. REPAIRED PER UPS ENGINEERING FILE NUMBER 727-57-1068, 727-57-1074.

Part: SKIN — CORRODED (PANEL 7603)

DURING 'C' CHECK, MAINTENANCE FOUND CORROSION AROUND FUEL CELL ACCESS CUT OUT FOR PANEL 7603. REPAIRED PER UPS ENGINEERING FILE NUMBER 727-57-1068, 727-57-1074.

Part: LONG BEAM — CORROSION (FS 754-757)

WHILE IN 'C' CHECK, MAINTENANCE FOUND CORROSION AT STA 754-757 RBL 45.75 WL 203 ON LONGITUDINAL BEAM LOWER FLANGE. INSTALLED REPAIR IAW SRM 51-40-4, 51-30-2.

Part: TAB — DELAMINATION (RUDDER)

WHILE IN 'C' CHECK, MAINTENANCE FOUND UPPER RUDDER TAB UPPER CLOSURE WEB DELAMINATED. INSTALLED REPAIR IAW SRM 51-40-9 AND 51-30-2.

Part: TRANS BEAM — CORROSION (BS 1215)

WHILE IN 'C' CHECK, MAINTENANCE FOUND CORROSION ON LEFT UPPER TRANSVERSE BEAM (O/B) BS 1215 WL 174 LBL 17. INSTALLED REPAIR IAW SRM 51-30-2, 51-10-2 AND MM 51-20-151.

Part: FOREFLAP — DELAMINATION (RT TE FLAP)

WHILE IN 'C' CHECK, MAINTENANCE FOUND R/W O/B FOREFLAP I/B END HAS A PREVIOUS REPAIR DELAMINATING. INSTALLED REPAIR IAW SRM 51-40-06.

Part: WEB — CRACKED (AFT CARGO DOOR)

WHILE IN 'C' CHECK, MAINTENANCE FOUND CRACKED WEB ON AFT CARGO DOOR AT AFT HINGE ON BOTH FWD AND AFT SIDE OF HINGE ATTACHMENTS. INSTALLED REPAIR IAW SRM 51-30-2, 51-20-4, 51-30-5, AND MM 51-20-21, 51-20-151.

Part: VERTICAL STIFF — CORROSION (BS 1215)

WHILE IN 'C' CHECK, MAINTENANCE FOUND VERTICAL STIFFENER AT BS 1215 RBL 21 WL 173-169 TO BE CORRODED. INSTALLED REPAIR IAW 51-30-2.

Part: TRANS BEAM — CORROSION (BS 1215)

WHILE IN 'C' CHECK, MAINTENANCE FOUND FWD CORROSION ON LOWER TRANSVERSE BEAM BS 1215 RBL 21 LBL 21 WL 174. INSTALLED REPAIR IAW SRM 51-30-2, 51-20-2, 51-20-151.

Part: LINER — CRACK (FWD ENTRY DOOR)

WHILE IN 'C' CHECK, MAINTENANCE FOUND FORWARD ENTRY DOOR UPPER FORWARD LINER SUPPORT PAN L-ANGLE CRACKED. INSTALLED REPAIR IAW SRM 51-20-1, 51-10-2, 51-30-2.

Part: DOOR WAY — CRACKED (MID GALLEY)

WHILE IN 'C' CHECK, MAINTENANCE FOUND MID GALLEY DOOR WAY, UPPER FORWARD CORNER REVEAL CRACKED OUT OF FASTENER HOLE. INSTALLED REPAIR IAW SRM 51-10-1, 51-10-2, 51-30-2, AND MM 51-20-151.

Part: SKIN — CORROSION (BS 475-480)

WHILE IN 'C' CHECK, MAINTENANCE FOUND FASTENERS AT BS 475-480 LEAKING AND SKIN PILLOWING BETWEEN STR 7 AND 6L. INSTALLED REPAIR IAW SRM 53-30-3, 51-30-2, 51-10-6, 51-10-2, AND MM 51-20-00.

Part: TRANS BEAM — CORROSION (BS 1215)

WHILE IN 'C' CHECK, MAINTENANCE FOUND O/B UPPER TRANSVERSE BEAM INSIDE TORQUE BOX TO BE CORRODED BS 1215 RBL23 WL 174. INSTALLED REPAIR IAW SRM 51-30-2, 51-20-4.

Part: EXPANSION LINK — CORROSION (FS 740)

WHILE IN 'C' CHECK, MAINTENANCE FOUND FWD EXPANSION LINK ATTACH FITTING CORRODED STA 740 RBL 45 WL 207-201.

Part: WEB — CRACKED (AFT CARGO DOOR)

WHILE IN 'C' CHECK, MAINTENANCE FOUND CRACKED WEB ON AFT CARGO DOOR AT FWD HINGE ON FWD SIDE OF HINGE ATTACHMENT. INSTALLED REPAIR IAW SRM 51-30-5, 51-30-2 AND 51-20-4.

Part: TRANSVERSE BEAM — CORROSION (BS 1215)

WHILE IN 'C' CHECK, MAINTENANCE FOUND CORROSION ON LOWER TRANSVERSE BEAM BS 1215 RBL 21-23 WL 174. INSTALLED REPAIR IAW SRM 51-10-1, 51-10-2, 51-30-2, 51-20-4, AND MM 51-20-151.

Part: SEAT TRACK — CORROSION (FS 740-760)

WHILE IN C-CHECK MAINTENANCE, FOUND SEAT TRACK AT LBL 45 STA 740-760 CORRODED. INSTALLED REPAIR IAW SRM 51-10-01, 51-30-2, 51-10-02 AND MM 51-20-151.

Part: TE BEAM — CORROSION (HORIZ STAB)

WHILE IN C-CHECK MAINTENANCE, FOUND CORROSION ON RT HORIZIZONTAL STAB UPPER T/E BEAM, LOWER SURFACE OF FWD FLANGE AT APPROX STAB STA 118.00. INSTALLED REPAIR IAW SRM 51-30-2.

Part: CTR HINGE — CORROSION (RT AILERON)

WHILE IN C-CHECK MAINTENANCE, FOUND CENTER HINGE FOR T/E PANEL ON RT I/B AILERON PITTED AND CORRODED. INSTALLED REPAIR IAW SRM 20-20-01.

Part: SEAT TRACK — CORROSION (FS 756-852)

WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON SEAT TRACK STA 756-852, LBL 45, WL 208. INSTALLED REPAIR IAW SRM 51-10-2.

Part: SEAT TRACK — CORROSION (FS 756-852)

WHILE IN C-CHECK, MAINTENANCE FOUND SEAT TRACK HAS CORROSION AND PITTING STA 756-852, LB 25, WL 208. INSTALLED REPAIR IAW SRM 51-20-4 AND SRM 51-30-2.

Part: ANGLE — CORROSION (FS 740)

WHILE IN C-CHECK, MAINTENANCE FOUND CORRODED ANGLE THAT ATTACHES DELTA BEAM AND BS 740 WEB, AFT SIDE OF WEB, LBL 9 TO RBL 9. INSTALLED REPAIR IAW SRM 51-30-2 AND MM 20-10-05.

Part: EXPANSION LINK — CORROSION (FS 740-760)

WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON EXPANSION LINK LBL 45, STA 740-760. INSTALLED REPAIR IAW SRM 51-10-01 AND 51-30-2.

Part: TRACK — CORROSION (NR 6 FLAP)

WHILE IN C-CHECK MAINTENANCE, FOUND NR 6 FLAP TRACK HAS RUST EMITTING FROM SPOILER BEAM ATTACH POINT. INSTALLED REPAIR IAW OHM 57-40-01.