N900ME

Part: CONTROL CABLE — OUT OF RIG (LANDING GEAR) · airframe 74,660 hrs · 89,373 cycles

UNABLE TO RAISE LANDING GEAR AFTER TAKE OFF UNABLE TO TURN NOSE WHEEL AND NO AUTO PRESSURIZATION INITIALLY BUT IT STARTED WORKING 15 MINUTES INTO FLIGHT. RIGGED GROUND SENSING CABLES.

Part: OIL CAP — UNSECURE (RT ENGINE) · airframe 74,275 hrs · 89,129 cycles

RIGHT ENGINE OIL QUANTITY DROPPED TO 4.5 QUARTS ALL OTHER INDICATIONS NORMAL. MAINTENANCE SERVICED ENGINE OIL AND RESECURED OIL CAP.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 74,186 hrs · 89,071 cycles

INTERCOSTAL AT STATION 817 AND LONGERON 3 LEFT IS CRACKED ON LOWER FLANGE. FABRICATED AND INSTALLED DOUBLER REPAIR.

Part: PAN — CHAFED (CARGO DOOR) · airframe 74,186 hrs · 89,071 cycles

FORWARD CARGO DOOR PAN, AFT SIDE MODERATELY CHAFED ON RADIUS, NEXT TO DOOR LATCH. FABRICATED AND INSTALLED DOUBLER.

Part: FRAME — CHAFED (FUSELAGE) · airframe 74,186 hrs · 89,071 cycles

FRAME IS CHAFED ON FORWARD SIDE IN AFT ACCCESSORY AT STATION 860 BETWEEN LONGERONS LEFT 5 AND LEFT 6. FABRICATED AND INSTALLED FRAME REPAIR PARTS.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 74,186 hrs · 89,071 cycles

LEFT SIDE AFT PRESSURE BULKHEAD SIDE STATION Z=34, 6 INCHES OUTBOARD OF DOOR CUTOUT FINGER DOUBLER IS CRACKED AROUND Z-RIVETS. ALSO AT STATION 40 FINGER DOUBLER HAS CRACK AROUND 1 RIVET. FABRICATED AND INSTALLED FINGER DOUBLER.

Part: HOUSING — CRACKED (PAX DOOR) · airframe 73,079 hrs · 88,324 cycles

PASSENGER DOOR HANDLE HOUSING CRACKED. REMOVED AND REPLACED HOUSING.

Part: INTERCOSTAL — CRACKED (DOOR) · airframe 73,079 hrs · 88,324 cycles

PASSENGER DOOR INTERCOSTAL IS CRACKED IN THE FLANGE AT HANDLE ASSY. REMOVED AND REPLACED INTERCOSTAL.

Part: RECEIVER — INOPERATIVE (NAVIGATION)

MKE - FLT 132 - THE NR 2 NAVIGATIONAL RECEIVER IS INOPERATIVE ON VOR FREQUENCIES. REMOVED AND REPLACED NR 2 NAVIGATIONAL RECEIVER. (M)

Part: FITTING — DAMAGED (CARGO BAY) · airframe 71,598 hrs · 87,302 cycles

AFT CARGO COMPARTMENT FITTINGS FOR AFT CARGO DOOR HAVE ELONGATED HOLES WHERE CARGO DOOR HINGE THRU-BOLT GOES. FABRICATED AND INSTALLED BUSHING PLATES.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 71,598 hrs · 87,302 cycles

CORROSION ON BOTTOM SIDE OF NR 4 SEAT TRACK AROUND FASTENER HOLES AT STATIONS 255 TO 264. FABRICATED AND INSTALLED SEAT TRACK SPLICE.

Part: SKIN — PUNCTURED (FUSELAGE) · airframe 71,598 hrs · 87,302 cycles

FUSELAGE SKIN HAS PUNCTURE ON RIGHT SIDE, STATION 897. FABRICATED AND INSTALLED REPAIR DOUBLER.

Part: SKIN — CANNING (LT ELEVATOR) · airframe 71,598 hrs · 87,302 cycles

LEFT ELEVATOR TOP SKIN IS OIL CANNING AT STATION XHS 170. FABRICATED AND INSTALLED SKIN.

Part: DOUBLER — MISINSTALLED (RT BUTE DOOR) · airframe 71,598 hrs · 87,302 cycles

RIGHT INBOARD BUTE DOOR INBOARD RECEPTICAL BRACKET HAS NUT PLATES. INSTALLED WHERE CAMLOC RECEPTICALS SHOULD BE. FABRICATED AND INSTALLED SKIN DOUBLER, REPAIR ANGLE, AND INTERNAL DOUBLER.

Part: STRUCTURE — CRACKED (LT PYLON) · airframe 71,598 hrs · 87,302 cycles

LEFT ENGINE PYLON BOX AREA DIVIDER CRACKED THRU RIVET HOLES AFT OF THE AFT SPAR BOTTOM ATTACH AREA. STOP DRILLED CRACK. FABRICATED AND INSTALLED REPAIR ANGLES.

Part: SEAT TRACK — DAMAGED (COCKPIT) · airframe 71,598 hrs · 87,302 cycles

FIRST OFFICER I/B SEAT TRACK HOLES ELONGATED BEYOND .375 INCHES. FABRICATED AND INSTALLED DOUBLER. FABRICATED AND INSTALLED SEAT TRACK.

Part: SKIN — DAMAGED (SERVICE DOOR) · airframe 71,598 hrs · 87,302 cycles

GALLEY SERVICE DOOR HAS AN EXTERNAL SKIN DING BETWEEN NUMBER 3 AND 4 BEAM, 3 INCHES INBOARD OF VERTICAL INTERCOSTAL. FABRICATED AND INSTALLED REPAIR DOUBLER.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 71,598 hrs · 87,302 cycles

STRINGER 19 HAS CORROSION ON LOWER FORWARD FLANGE AT STATION 101. DRILLED AND INSTALLED NEW STRINGER SECTION 19 AND SPLICES.

Part: FRAME — CHAFED (RT PYLON) · airframe 71,598 hrs · 87,302 cycles

RIGHT PYLON HAS A CHAFED FRAME LOCATED AFT OF HYDRAULIC FLEX LINES. FABRICATED AND INSTALLED REPAIR DOUBLER.

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 71,598 hrs · 87,302 cycles

STATION 817 LOWER BULKHEAD WEB HAS SEVERAL TOOL MARKS ON THE FORWARD SIDE OUTBOARD OF LONGERON 27 RIGHT TO LONGERON 27 LEFT. FABRICATED AND INSTALLED DOUBLERS.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 71,598 hrs · 87,302 cycles

CABIN SUBFLOOR HAS AREAS OF LIGHT CORROSION AND BARE METAL BETWEEN STATION 275 TO 294 ADJACENT TO LONGERON 181 RIGHT. FABRICATED AND INSTALLED REPAIR PARTS AND BRACKET.

Part: NUT PLATE — CRACKED (RT PYLON) · airframe 71,598 hrs · 87,302 cycles

RIGHT PYLON TRAILING EDGE ATTACH STRUCTURE IS CRACKED AT FORWARD INBOARD NUT PLATE ON TOP SIDE. FABRICATED AND INSTALLED NEW ANGLE.

Part: ANGLE — ELONGATED (LT WING) · airframe 71,598 hrs · 87,302 cycles

ELONGATED HOLE ON AFT SPAR ATTACH ANGLE LEFT WING STATION XRS 161.7. FABRICATED AND INSTALLED REPAIR ANGLES. INSTALLED, FABRICATED REPAIR DOUBLER.

Part: ACCESS PANEL — CHAFED (RT WING) · airframe 71,598 hrs · 87,302 cycles

RIGHT WING MIDDLE BUTE DOOR I/B EDGE IS CHAFED. FABRICATED AND INSTALLED FILLER AND DOUBLER.

Part: CHANNEL — CHAFED (BULKHEAD) · airframe 71,598 hrs · 87,302 cycles

AFT PRESSURE BULKHEAD DOOR ZEE CHANNEL IS CHAFED IN THE AFT LOWER RIGHT CORNER. REMOVED AND REPLACED ZEE.

Part: SKIN — MISDRILLED (FUSELAGE) · airframe 71,598 hrs · 87,302 cycles

SKIN SECTION BETWEEN CANTED STATIONS 942 AND 953 JUST OUTBOARD OF RIGHT VENTRAL STAIRWAY DOOR JAMB HAS MISDRILLED HOLES. FABRICATED AND INSTALLED NEW SKIN SELECTION.

Part: ACCESS PANEL — PUNCTURED (LT WING) · airframe 71,598 hrs · 87,302 cycles

PUNCTURE IN UPPER FORWARD BUTE DOOR, LEFT WING APPROXIMATELY XTE 293. FABRICATED AND INSTALLED A DOUBLER.

Part: SPAR — DAMAGED (LT WING) · airframe 71,598 hrs · 87,302 cycles

OUT OF ROUND HOLE ON SPAR AT STATION XRS 383 LEFT WING LOWER TANG. FABRICATED AND INSTALLED REPAIR SPLICE, ANGLE, CUTOUT FILLERS, SHIMS, AND RADIUS FILLERS.

Part: BULKHEAD — CORRODED (CARGO BAY) · airframe 71,598 hrs · 87,302 cycles

AFT CARGO BULKHEAD WEB STATION 817 CORRODED. REMOVED LONGERON 25 RIGHT TO LONGERON 25 LEFT. FABRICATED AND INSTALLED NEW WEB.

Part: BATTERY PACK — INOPERATIVE (FUSELAGE) · airframe 71,598 hrs · 87,302 cycles

DURING THE EMERGENCY LIGHTS SYSTEM TEST THE LEFT NACELLE LIGHT DID NOT TURN ON. REMOVED AND REPLACED LEFT EMERGENCY BATTERY PACK.

Part: FITTING — CRACKED (VENTRAL DOOR) · airframe 71,598 hrs · 87,302 cycles

AFT VENTRAL DOOR HAS CRACKS IN THE PAN, FITTING, AND ATTACH ANGLE INSIDE AT UPPER INNER DOOR STOP. MAINTENANCE FABRICATED AND INSTALLED PAN, TEE, AND ANGLE.

Part: CLIP — DAMAGED (RT WING) · airframe 71,598 hrs · 87,302 cycles

REMOVED ALL LOWER SHEAR TIES FROM STATION 23 TO STATION 11 AT RIGHT WING STATION XRS69. REMOVED TO FACILITATE OTHER MAINTENANCE AND FOUND THREE SHEAR TIE CLIPS OUT OF LIMITS. MAINTENANCE FABRICATED AND INSTALLED NEW SHEAR TIE CLIPS.

Part: PAN — DAMAGED (SERVICE DOOR) · airframe 71,598 hrs · 87,302 cycles

GALLEY DOOR INNER PAN, LOWER FORWARD CORNER, INTERIOR SURFACE HAS 3 AREAS OF TOOLING MARKS. BLENDED OUT AREAS, FABRICATED AND INSTALLED PAN.

Part: DOOR — CRACKED (RT WING) · airframe 71,598 hrs · 87,302 cycles

RIGHT WING CENTER BUTE DOOR INBOARD AFT ATTACH HOLE CRACKED. FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER.

Part: ANGLE — DAMAGED (DOOR JAMB) · airframe 71,598 hrs · 87,302 cycles

VENTRAL STAIRWAY DOOR JAMB SPLICE ANGLE AT STATION 908 RIGHT HAS SHORT E.D. ON SEVERAL FASTENER HOLES. REMOVED SPLICE ANGLE AND INSTALLED DOUBLER/SPLICE ANGLE.

Part: PANEL — BOWED (LT ELEVATOR) · airframe 71,598 hrs · 87,302 cycles

LEFT ELEVATOR TRAILING EDGE PANEL IS BOWED. DRILLED AND INSTALLED NEW CLOSEOUT CHANNEL.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 71,598 hrs · 45,841 cycles

FUSELAGE SKIN DRAIN HOLE IS ENLARGED FROM .25 TO .5 INCHES STATION 902 AT VENTRAL STAIR CUTOUT JAMB LEFT SIDE. FABRICATED AND INSTALLED NEW DOUBLER.

Part: STIFFENER — CRACKED (BULKHEAD DOOR) · airframe 71,598 hrs · 87,302 cycles

AFT PRESSURE BULKHEAD DOOR HAS 2 STIFFENERS CRACKED AND 1 CHAFED AT TOPSIDE OF DOOR. FABRICATED AND INSTALLED NEW STIFFENERS.

Part: ANGLE — DAMAGED (BULKHEAD) · airframe 71,598 hrs · 87,302 cycles

TOOL MARKS ON LOWER PART OF AFT PRESSURE BULKHEAD DOOR SILL IN SEAL AREA. FABRICATED AND INSTALLED ZEE.

Part: SKIN — CHAFED (AIRSTAIR) · airframe 71,598 hrs · 87,302 cycles

AFT VENTRAL STAIRWAY CHAFED ON BOTH LEFT AND RIGHT OUTBOARD EDGES. FABRICATED AND INSTALLED SKIN.

Part: RIB — CRACKED (LT ELEVATOR) · airframe 71,598 hrs · 87,302 cycles

LEFT ELEVATOR RIB AT STATION 180 IS CRACKED AT THE TRAILING EDGE. FABRICATED AND INSTALLED REPAIR.

Part: SKIN — CORRODED (FUSELAGE) · airframe 71,598 hrs · 87,302 cycles

AREAS OF LITE CORROSION ON OUTER BELLY OF FUSELAGE SKIN AT STATION 642 TO 645. FABRICATED AND INSTALLED NEW SKIN.

Part: PANEL — DELAMINATED (RT WING) · airframe 71,598 hrs · 87,302 cycles

RIGHT WING T/E OUTBOARD PANEL IS DELAMINATED. FABRICATED AND INSTALLED NEW PANEL.

Part: STRUCTURE — CHAFED (CARGO DOOR) · airframe 71,598 hrs · 87,302 cycles

FORWARD CARGO DOOR IS CHAFED AROUND LIGHTENING HOLE EDGE, BELOW FORWARD HINGE ARM. FABRICATED AND INSTALLED NEW REPAIR DOUBLER.

Part: PAN — CHAFED (CARGO DOOR) · airframe 71,598 hrs · 87,302 cycles

FORWARD CARGO DOOR HAS CHAFING AROUND AFT HINGE SPRING ATTACH HOLE ON INNER PAN. FABRICATED AND INSTALLED REPAIR DOUBLER.

Part: PAN — MISDRILLED (SERVICE DOOR) · airframe 71,598 hrs · 87,302 cycles

GALLEY DOOR INNER PAN DOUBLER ON LOWER EDGE HAS 8 MISDRILLED HOLES. FABRICATED AND INSTALLED INNER SKIN DOUBLER.

Part: PANEL — DELAMINATED (LT WING) · airframe 71,598 hrs · 87,302 cycles

LEFT WING TRAILING EDGE IS DELAMINATED STATION 445. TRIMMED, DRILLED, AND COUNTERSUNK PANEL.

Part: SKIN — CHAFED (CARGO DOOR) · airframe 71,598 hrs · 87,302 cycles

FORWARD CARGO DOOR EXTERIOR PAINT IS CHAFED THROUGH ON OUTER SKIN. FABRICATED AND INSTALLED NEW SKIN.

Part: PANEL — DELAMINATED (LT WING) · airframe 71,598 hrs · 87,302 cycles

BOTTOM INBOARD CORNER OF LEFT OUTBOARD UPPER TRAILING EDGE HAS AN AREA OF DELAMINATION ON LEFT WING. MAINTENANCE DRILLED AND TRIMMED TRAILING EDGE PANEL.

Part: RIB — CRACKED (SEVICE DOOR) · airframe 71,598 hrs · 87,302 cycles

GALLEY DOOR NR 2 RIB AT FORWARD EDGE HAS ADDITIONAL CRACK IN PREVIOUS REPAIR AREA. FABRICATED AND INSTALLED NEW RIB.

Part: STIFFENER — MISDRILLED (PRESSURE BULKHEAD) · airframe 71,598 hrs · 87,302 cycles

AFT PRESSURE BULKHEAD TEE HAS A HOLE DRILLED THRU THE VERTICAL LEG AT STATION 817 APPROXIMATELY .5 INCH UP FROM RADIUS. FABRICATED AND INSTALLED REPAIR DOUBLERS.

Part: DOUBLER — DAMAGED (COCKPIT) · airframe 71,598 hrs · 87,302 cycles

A DOUBLER TEMPORARY REPAIR IN COCKPIT NEEDS TO BE REPLACED. REMOVED AND REPLACED DOUBLER.

Part: PAN — GOUGED (SERVICE DOOR) · airframe 71,598 hrs · 87,302 cycles

GALLEY DOOR OUTER PAN LOWER EDGE HAS SEVERAL SMALL NICKS AND GOUGES. FABRICATED AND INSTALLED NEW OUTER PAN.

Part: CHANNEL — CORRODED (KEELBEAM) · airframe 71,598 hrs · 87,302 cycles

LIGHT AREAS OF CORROSION, AT STATION 635 - 642 ON KEEL Z CHANNEL, RT SIDE. FABRICTED AND INSTALLED NEW Z CHANNEL.

Part: FITTING — CORRODED (KEELBEAM) · airframe 71,598 hrs · 87,302 cycles

KEEL RT HINGE CORRODED AT STATION 640 LT SIDE BETWEEN LONGERON 29 AND MAIN BEAM. FABRICATED AND INSTALLED NEW KEEL FITTING.

Part: FLOORBOARD — CRACKED (LAVATORY) · airframe 71,598 hrs · 87,302 cycles

FLOOR PANEL BETWEEN AFT LAVATORIES, HAS RIVET HEADS SHEARED OFF, CRACKS, AND A DOUBLE DRILLED HOLE. FABRICATED AND INSTALLED REPAIR DOUBLERS AND 5 EACH HAT CHANNELS.

Part: FITTING — CRACKED (RT WING) · airframe 71,598 hrs · 87,302 cycles

DURING UT TEST, CRACK INDICATION NOTED AT FORWARD SIDE OF THREE BOLT HOLES OF RT TRAPEZOIDAL PANEL LOWER SUPPORT FITTING. FABRICATED AND INSTALLED REPAIR ANGLES.

Part: STRINGER — CORRODED (RT WING) · airframe 60,253 hrs · 35,661 cycles

RIGHT WING INTERNAL, STRINGER 11 AFT LOWER LEG HAS A CORROSION SPOT AT STATION 77. FABRICATED AND INSTALLED BUSHING.

Part: PAN — CHAFED (CARGO DOOR) · airframe 60,253 hrs · 35,661 cycles

CHAFING ON OUTER PAN AROUND SEVERAL DOOR STOPS ON FORWARD CARGO DOOR. FABRICATED AND INSTALLED OUTER PAN.

Part: PAN — NICKED (CARGO DOOR) · airframe 71,598 hrs · 87,302 cycles

FORWARD CARGO DOOR INNER PAN IS NICKED ON INSIDE SURFACE JUST ABOVE NR 4 BEAM. FABRICATED AND INSTALLED NEW INNER PAN.

Part: LONGERON — DAMAGED (FUSELAGE) · airframe 60,253 hrs · 35,661 cycles

LONGERON 1 HAS TOOL MARKS BETWEEN STATION 180 - 200. FABRICATED AND INSTALLED LONGERON SPLICES.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 60,253 hrs · 35,661 cycles

KEEL AREA STRINGERS AT STATION 642 - 553 HAVE MODERATE CORROSION INBOARD OF LONGERON 29 LEFT AND RIGHT. FABRICATED AND INSTALLED STRINGERS.

Part: CLIP — CRACKED (RIGHT WING) · airframe 71,598 hrs · 87,302 cycles

RIGHT WING STATION XRS 111.5 SHEAR CLIP HAS A CRACK AT AFT FLANGE. FABRICATED AND INSTALLED CLIP.

Part: STRINGER — CORRODED (RIGHT WING) · airframe 71,598 hrs · 87,302 cycles

RIGHT WING INTERIOR, STRINGER 18 HAS MODERATE CORROSION SPOT FORWARD LOWER LEG STATION XRS 62. FABRICATED AND INSTALLED STRINGER.

Part: INTERCOSTAL — CHAFED (FUSELAGE) · airframe 71,598 hrs · 87,302 cycles

CABIN FLOORBEAM INTERCOSTAL AT STATION 375 AND AIRCRAFT CENTERLINE IS CHAFED. FABRICATED AND INSTALLED 2 ANGLE REPAIRS.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 71,598 hrs · 87,302 cycles

LOWER LEFT ANGLE FOR STATION 816 AT JACK PAD AREA HAS CORROSION. FABRICATED AND INSTALLED NEW ANGLE.

Part: STRINGER — CORRODED (RIGHT WING) · airframe 71,598 hrs · 87,302 cycles

RIGHT WING INTERIOR, STRINGER 19 FORWARD LOWER LEG HAS CORROSION AROUND TWO RIVETS STATION 56. FABRICATED AND INSTALLED NEW STRINGER SECTION.

Part: INTERCOSTAL — DAMAGED (FUSELAGE) · airframe 71,598 hrs · 87,302 cycles

STATION 160 INTERCOSTAL UNDER SUB FLOOR HAS 1 OVERSIZE HOLE WHERE INTERCOSTAL INTERSECTS STATION 160 FLOORBEAM. FABRICATED AND INSTALLED REPAIR DOUBLERS.

Part: INTERCOSTAL — INADEQUATE (FUSELAGE) · airframe 71,598 hrs · 87,302 cycles

IN ORDER TO ACCOMODATE LONGERON SPLICE IN AREA, INTERCOSTAL BETWEEN STATIONS 168 AND 180 REQUIRES REPLACEMENT. FABRICATED AND INSTALLED INTERCOSTAL.

Part: PAN — MISDRILLED (CARGO DOOR) · airframe 71,598 hrs · 87,302 cycles

FORWARD CARGO DOOR INNER PAN HAS A DOUBLE DRILLED HOLE AT LOWER FORWARD END. FABRICATED AND INSTALLED DOUBLER.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 71,598 hrs · 87,302 cycles

CRACK ON LEFT SUB FLOOR NEAR LIGHTENING HOLE AT STATION 642 INSIDE CABIN. FABRICATED AND INSTALLED DOUBLER.

Part: PAN — MISDRILLED (CARGO DOOR) · airframe 71,598 hrs · 87,302 cycles

SIX MISDRILLED HOLES THRU INNER PAN LOCATED ABOVE LOWER, CENTER INTERCOSTAL ON AFT CARGO DOOR. FABRICATED AND INSTALLED NEW REPAIR DOUBLERS AND RIVETS.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 71,598 hrs · 87,302 cycles

SUB FLOOR IS CRACKED OUTBOARD OF NR 4 SEAT TRACK AT STATION 756. FABRICATED AND INSTALLED DOUBLER.

Part: SKIN — DAMAGED (APU BAY) · airframe 71,598 hrs · 87,302 cycles

APU DOG HOUSE, RIGHT SIDE SKIN MANY FASTENER HOLES ARE WORN AND DISFIGURED AND HOLES ARE TOO LARGE. FABRICATED AND INSTALLED DOUBLER.

Part: SKIN — DENTED (FUSELAGE) · airframe 71,598 hrs · 87,302 cycles

DENT ON EXTERIOR UPPER FUSELAGE SKIN AT STATION 987 ABOUT 17 INCHES LEFT OF CENTER. FABRICATED AND INSTALLED DOUBLER REPAIR.

Part: STRINGER — CORRODED (RIGHT WING) · airframe 71,598 hrs · 87,302 cycles

RIGHT WING INTERIOR, STRINGER 20 FORWARD LOWER LEG HAS MODERATE CORROSION AT STATION XRS 56 TO 63. FABRICATED AND INSTALLED NEW STRINGER.

Part: SKIN — CORRODED (E/E BAY DOOR) · airframe 71,598 hrs · 87,302 cycles

MODERATE CORROSION AROUND BN'S ON UPPER FORWARD EDGE OF E & E DOOR SKIN. FABRICATED AND INSTALLED DOUBLER.

Part: STRINGER — CORRODED (RIGHT WING) · airframe 71,598 hrs · 87,302 cycles

RIGHT WING INTERIOR, STRINGER 21, FORWARD LOWER LEG HAS HEAVY CORROSION AT STATION XRS 59. FABRICATED AND INSTALLED NEW STRINGER AND SPLICES.

Part: STRINGER — CORRODED (RIGHT WING) · airframe 71,598 hrs · 87,302 cycles

RIGHT WING INTERIOR, STRINGER 22 FORWARD LOWER LEG TO VERTICAL HAS MODERATE CORROSION IN THE RADIUS STATION XRS 77.5. FABRICATED AND INSTALLED STRINGER.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 71,598 hrs · 87,302 cycles

CORROSION ON BOTTOM SIDE OF FASTENER HOLE ON NR 4 SEAT TRACK AT STATION 615. FABRICATED AND INSTALLED REPAIR PARTS.

Part: SKIN — DENTED (TE FLAP) · airframe 71,598 hrs · 87,302 cycles

LEFT FLAP AFT FLAP PANEL SKIN HAS 3 DEEP DENTS. FABRICATED AND INSTALLED NEW SKIN.

Part: FITTING — PLUGGED (CARGO DOOR) · airframe 71,598 hrs · 87,302 cycles

FORWARD CARGO DOOR NR 2 BEAM FORWARD END FITTING HAS A PLUG IN THE RADIUS. FABRICATED AND INSTALLED NEW FITTING.

Part: FLOORBOARD — CHAFED (CABIN) · airframe 71,598 hrs · 87,302 cycles

CABIN FLOOR PANEL E-13 HAS AREAS OF BARE METAL AND MISSING CHAFE STRIPS. FABRICATED AND INSTALLED FLOORBOARD.

Part: SHEAR TIE — GOUGED (FUSELAGE) · airframe 71,598 hrs · 87,302 cycles

STATION 786 SHEAR TIE HAS A GOUGE BETWEEN LONGERON 6 AND 7 LEFT. FABRICATED AND INSTALLED REPAIR DOUBLER.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 71,598 hrs · 87,302 cycles

GOUGES AROUND FLOORBOARD FASTENER HOLES TOP OF NR 4 SEAT TRACK AT STATION 661 TO 681. FABRICATED AND INSTALLED REPAIR PARTS.

Part: INTERCOSTAL — MISMANUFACTURED (CARGO DOOR) · airframe 71,598 hrs · 87,302 cycles

REPAIR INSTALLED ON FORWARD CARGO DOOR INTERCOSTAL ABOVE BEAM NR 1, 2ND FROM FORWARD IS NOT PER SRM REQUIREMENTS. FABRICATED AND INSTALLED INTERCOSTAL.

Part: FLOORBOARD — CHAFED (CABIN) · airframe 71,598 hrs · 87,302 cycles

CABIN FLOOR PANEL C-7 HAS A CHAFED AREA. MAINTENANCE REPAIRED DAMAGED AREA.

Part: STRINGER CLIP — CRACKED (RIGHT WING) · airframe 71,598 hrs · 87,302 cycles

RIGHT WING STRINGER 11, STATION XRS 111.5 OUTBOARD CLIP IS CRACKED. FABRICATED AND INSTALLED NEW CLIP.

Part: FLOORBOARD — CORRODED (LAVATORY) · airframe 71,598 hrs · 87,302 cycles

FLOOR PANEL BETWEEN AFT LAVATORYS HAS NUMEROUS AREAS OF LIGHT CORROSION, CHAFES, AND MISSING PAINT. FABRICATED AND INSTALLED REPAIR DOUBLER.

Part: ANGLE — MISDRILLED (CARGO DOOR) · airframe 71,598 hrs · 87,302 cycles

FORWARD CARGO DOOR LOWER ANGLE HAS DOUBLE DRILLED HOLES AT FORWARD END. FABRICATED AND INSTALLED ANGLE REPAIR.

Part: FRAME — NICKED (FUSELAGE) · airframe 71,598 hrs · 87,302 cycles

FORWARD ACCESS STATION 47 FRAME HAS 2 SPOTS WITH NICKS APROXIMATELY 6 AND 12 INCHES LEFT OF CENTER ON FORWARD SIDE. FABRICATED AND INSTALLED TWO DOUBLERS.

Part: FLOORBOARD — FLAKING (CABIN) · airframe 71,598 hrs · 87,302 cycles

CABIN FLOORBOARD FOR STATION 160 TO 200 RIGHT OF CENTER BEAM 45 TO 55 INCHES HAS LAMINATE FLAKING UP. MAINTENANCE REPAIRED DAMAGED AREA IAW SRM 51-70.

Part: FLOORBOARD — FLAKING (CABIN) · airframe 71,598 hrs · 87,302 cycles

CABIN FLOOR PANEL, FOR STATION 160 TO 200, IN FRONT OF PAX DOOR HAS LAMINATE FLAKING AND A HOLE WITH INSUFFICIENT EDGE DISTANCE. REPAIRED DAMAGED AREAS IAW SRM 51-70.

Part: SKIN — DISENGAGED (WING) · airframe 71,598 hrs · 87,302 cycles

OUT OF ROUND HOLE AT STATION XRS 214 AND 184 LEFT WING FORWARD LOWER SKIN. FABRICATED AND INSTALLED PLUG.

Part: LONGERON — MISDRILLED (FUSELAGE) · airframe 71,598 hrs · 87,302 cycles

LONGERON 16 AND 17 HAVE A MISDRILLED HOLE AT STATION 737. FABRICATED AND INSTALLED NEW LONGERON.

Part: SUPPORT BRACKET — DENTED (CARGO) · airframe 71,598 hrs · 87,302 cycles

AFT CARGO RIGHT HAND SUPPORT STRUT AT STATION 680 IS DENTED. FABRICATED AND INSTALLED NEW STRUT SUPPORT.

Part: FLOORBEAM — CHAFED (FUSELAGE) · airframe 71,598 hrs · 87,302 cycles

CABIN FLOORBEAM HAS CHAFES AT STATION 484 INBOARD OF LEFT HAND INBOARD SEAT TRACK. FABRICATED AND INSTALLED REPAIR ANGLE AND WEAR STRIPS.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 71,598 hrs · 87,302 cycles

CABIN SUB FLOOR HAS SEVERAL AREAS OF LIGHT CORROSION BETWEEN STATION 408 - 427 ADJACENT TO LONGERON 18 RIGHT. FABRICATED AND INSTALLED REPAIRS.

Part: SKIN — DENTED (FUSELAGE) · airframe 71,598 hrs · 87,302 cycles

DENT ON EXTERIOR FUSELAGE SKIN AT STATION 266, JUST BELOW LONGERON 19 LEFT. FABRICATED AND INSTALLED DOUBLER.

Part: SKIN — DENTED (ELEVATOR) · airframe 71,598 hrs · 87,302 cycles

LEFT HAND ELEVATOR BOTTOM SKIN HAS SEVERAL DENTS AT STATION XHS 60. FABRICATED AND INSTALLED NEW SKIN.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 71,598 hrs · 87,302 cycles

LONGERON 2 LEFT IS CRACKED AT STATION 623. FABRICATED AND INSTALLED REPAIR PARTS.

Part: INTERCOSTAL — MISDRILLED (CARGO DOOR) · airframe 71,598 hrs · 87,302 cycles

FORWARD CARGO DOOR INTERCOSTAL FORWARD OF AFT HINGE HAS DOUBLE DRILLED HOLES AT UPPER END. FABRICATED AND INSTALLED NEW INTERCOSTAL.

Part: INTERCOSTAL — DAMAGED (CARGO DOOR) · airframe 71,598 hrs · 87,302 cycles

FOUND ELONGATED HOLES IN AFT CARGO DOOR INTERCOSTAL WEB. MAINTENANCE FABRICATED AND INSTALLED INTERCOSTAL.

Part: DOOR — CHAFED (RIGHT WING) · airframe 71,598 hrs · 87,302 cycles

RIGHT WING OUTBOARD BUTE DOOR IS CHAFED AT INBOARD END AT AFT FASTENER, INNER SURFACE. FABRICATED AND INSTALLED DOUBLER.

Part: SKIN — GOUGED (FUSELAGE) · airframe 71,598 hrs · 87,302 cycles

FUSELAGE SKIN EXTERIOR HAS A GOUGE AT STATION 101 BELOW ELECTRICAL POWER PLUG OPENING. FABRICATED AND INSTALLED DOUBLER AND FILLER.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 71,598 hrs · 87,302 cycles

SUB FLOOR HAS SEVERAL SPOTS OF LIGHT CORROSION BETWEEN CENTER OF A/C TO FLOOR SUPPORT FORWARD OF NR 1 SEAT TRACK BETWEEN STATION 160 - 200. FABRICATED AND INSTALLED NEW SUBFLOOR.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 71,598 hrs · 87,302 cycles

REMOVED GALLEY DRAIN PAN TO FOM AND FOUND GALLEY SUB FLOOR OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR DOUBLER.

Part: PAN — CHAFED (CARGO DOOR) · airframe 71,598 hrs · 87,302 cycles

AFT CARGO DOOR INNER AND OUTER PANS HAVE NUMEROUS CHAFES ALONG BOTTOM EDGE. FABRICATED AND INSTALLED ANGLES.

Part: SPAR — MISDRILLED (LT WING) · airframe 71,598 hrs · 87,302 cycles

DOUBLE DRILLED HOLE AT STATION XRS 189 LEFT WING FORWARD UPPER SPAR. FABRICATED AND INSTALLED PLUG.

Part: FLOORBOARD — CRACKED (CABIN) · airframe 71,598 hrs · 87,302 cycles

CABIN FLOOR PANEL E13 HAS NUMEROUS CHAFE MARKS AROUND BOLT HOLES BOTTOM SIDE, AND A DENT WITH A CRACK ON TOP CENTER. FABRICATED AND INSTALLED NEW FLOORBOARD.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,598 hrs · 87,302 cycles

SUB SURFACE CRACK INDICATION ON EXTERNAL SKIN LOWER FORWARD CORNER OF FORWARD CARGO COMPARTMENT OPENING. FABRICATED AND INSTALLED DOUBLER AND FILLERS.

Part: INTERCOSTAL — DENTED (FUSELAGE) · airframe 71,598 hrs · 87,302 cycles

FLOORBEAM INTERCOSTAL AT STATION 375 AND FUSELAGE CENTERLINE IS DENTED AND CHAFED. MAINTENANCE FABRICATED AND INSTALLED INTERCOSTAL.

Part: FLOORBOARD — GOUGED (CABIN) · airframe 71,598 hrs · 87,302 cycles

GOUGES AROUND FLOORBOARD FASTENER HOLES TOP OF NR 2 SEAT TRACK FROM STATION 718 TO 786. FABRICATED AND INSTALLED REPAIRED TRACK.

Part: INTERCOSTAL — CHAFED (CARGO DOOR) · airframe 71,598 hrs · 87,302 cycles

FORWARD CARGO DOOR AFT INTERCOSTAL BY DOOR HINGE IS CHAFED ON AFT SIDE. FABRICATED AND INSTALLED NEW INTERCOSTAL.

Part: WEB — CRACKED (VENTRAL DOOR) · airframe 71,598 hrs · 87,302 cycles

AFT VENTRAL DOOR JAMB WEB IS CRACKED ON RIGHT SIDE APPROX 1 FOOT BELOW UPPER CORNER. FABRICATED AND INSTALLED NEW DOUBLER.

Part: FRAME — GOUGED (FUSELAGE) · airframe 71,598 hrs · 87,302 cycles

FRAME 737 IS GOUGED AT LONGERON 17 LEFT. FABRICATED AND INSTALLED ANGLE.

Part: SKIN — DENTED (FUSELAGE) · airframe 71,598 hrs · 87,302 cycles

EXTERIOR SKIN DENTS AT STATION 235 & 247 BETWEEN LONGERON 17 & 18 LEFT. FABRICATED AND INSTALLED REPAIR DOUBLER.

Part: PAN — CHAFED (CARGO DOOR) · airframe 71,598 hrs · 87,302 cycles

AFT CARGO DOOR INNER PAN IS CHAFED AT SCREW HOLES WHERE SEAL ATTACH. FABRICATED AND INSTALLED REPAIR STRAPS AND NEW INNER PAN.

Part: SKIN — DENTED (AILERON) · airframe 71,598 hrs · 87,302 cycles

RIGHT AILERON HAS A DENT ON LOWER SURFACE, 4 INCHES FROM OUTBOARD END. FABRICATED AND INSTALLED REPAIR DOUBLER.

Part: PANEL — BULGED (RIGHT WING) · airframe 71,598 hrs · 87,302 cycles

RIGHT WING PANEL HAS A BULGE. FABRICATED AND INSTALLED NEW PANEL.

Part: FLOORBOARD — PUNCTURED (COCKPIT) · airframe 71,598 hrs · 87,302 cycles

CAPTAIN FLOORBOARD AROUND YOLK IS PUNCTURED AT INBOARD AFT CORNER. FABRICATED AND INSTALLED NEW DOUBLER.

Part: FINGER DOUBLER — CRACKED (LEFT ELEVATOR) · airframe 71,598 hrs · 87,302 cycles

FINGER DOUBLER SPLICE IS REMOVED FROM LEFT HAND ELEVATOR LOWER INBOARD SKIN TO FOM. FABRICATED AND INSTALLED NEW DOUBLER.

Part: BULKHEAD — GOUGED (FUSELAGE) · airframe 71,598 hrs · 87,302 cycles

STATION 786 BULKHEAD HAS SEVERAL GOUGES IN AFT SIDE OF WEB BETWEEN LONGERON 8-9 LEFT. FABRICATED AND INSTALLED DOUBLER.

Part: LONGERON — CHAFED (FUSELAGE) · airframe 71,598 hrs · 87,302 cycles

LONGERON 8 LEFT IS CHAFED AT STATION 709. FABRICATED AND INSTALLED REPAIR LONGERON AND SPLICE.

Part: SKIN — GOUGED (FUSELAGE) · airframe 71,598 hrs · 87,302 cycles

GOUGE ON EXTERIOR SKIN LEFT HAND SIDE AT STATION 216, LONGERON 18 LEFT. FABRICATED AND INSTALLED REPAIR DOUBLER.

Part: FLOORBOARD — DENTED (COCKPIT) · airframe 71,598 hrs · 87,302 cycles

COCKPIT FLOORBOARD BEHIND CENTER PEDESTAL IS DENTED. FABRICATED AND INSTALLED NEW DOUBLER.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 71,598 hrs · 87,302 cycles

THE INTERNAL SURFACE OF FUSELAGE SKIN HAS DRILL MARKS AT STATION 699 UNDER LONGERON 3R AND 6R. FABRICATED AND INSTALLED FINGER DOUBLER AND FILLER.

Part: SKIN — DENTED (FUSELAGE) · airframe 71,598 hrs · 87,302 cycles

EXTERIOR SKIN DENTED AT STATION 231 AT LONGERONS 18 AND 19 LEFT. FABRICATED AND INSTALLED DOUBLER.

Part: FLOOR SUPPORT — CRACKED (CABIN) · airframe 71,598 hrs · 87,302 cycles

CABIN SUB FLOOR HAS A CRACK UNDER SEAT TRACK NR 4 AT STATION 256. FABRICATED AND INSTALLED REPAIR DOUBLER.

Part: ANGLE — DAMAGED (RUDDER) · airframe 71,598 hrs · 87,302 cycles

FOUND ELONGATED FASTENER HOLES ON NUMBER 21 RIB SUPPORT ANGLE ON LEADING EDGE OF RUDDER. MAINTENANCE INSTALLED REPAIR TEE.

Part: SKIN — DENTED (FUSELAGE) · airframe 71,598 hrs · 87,302 cycles

FUSE SKIN DENT AT STATION 233 BELOW LONGERON 16 RIGHT IS A CLASS 1B. FABRICATED AND INSTALLED REPAIR DOUBLER.

Part: SKIN — SCRATCHED (CARGO DOOR) · airframe 71,598 hrs · 87,302 cycles

AFT CARGO DOOR OUTER SKIN HAS NUMEROUS SCRATCHES ACROSS BEAM 3 INCHES FROM FWD TO AFT SIDE. FABRICATED AND INSTALLED NEW SKIN PANEL.

Part: SKIN — GOUGED (VERTICAL STAB) · airframe 71,598 hrs · 87,302 cycles

VERTICAL SKIN IS GOUGED FROM RIGHT LOWER HORIZONTAL TO VERTICAL FAIRING. FABRICATED AND INSTALLED NEW SKIN PANEL.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 71,598 hrs · 87,302 cycles

TOOL MARK ON FRAME 294 AT LONGERON 16R. FABRICATED AND INSTALLED REPAIR PLATE.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 71,598 hrs · 87,302 cycles

INTERCOSTAL AT STATION 557 LONGERON 10R IS CRACKED. FABRICATED AND INSTALLED DOUBLER.

Part: SUPPORT BRACKET — DAMAGED (FUSELAGE) · airframe 71,598 hrs · 87,302 cycles

STATION 38, BOTTOM RIGHT SIDE OF PRESSURE PANEL, TWO MODERATE TOOL MARKS. FABRICATED AND INSTALLED DOUBLER REPAIR.

Part: LONGERON — NICKED (FUSELAGE) · airframe 71,598 hrs · 87,302 cycles

LONGERON 16 LEFT HAS NICKS IN FRAME ATTACH LEGS AT STATION 661. FABRICATED AND INSTALLED NEW LONGERON.

Part: FLOORBOARD — CRACKED (CABIN) · airframe 71,598 hrs · 87,302 cycles

CABIN FLOOR PANEL F-5 HAS CRACKS, PUNCTURES, AND DAMAGED FIBERGLASS SUPPORT CHANNELS. FABRICATED AND INSTALLED DOUBLERS.

Part: FLOORBOARD — DAMAGED (CABIN) · airframe 71,598 hrs · 87,302 cycles

CABIN FLOOR PANEL C-4 HAS FIBERGLASS SPLITTING WHERE RIVETS ATTACH EXPANSION JOINT. REPAIRED DAMAGED AREA''S IAW SRM 51-70-1 PARAGRAPH 7.

Part: FLOORBOARD — DAMAGED (CABIN) · airframe 71,598 hrs · 87,302 cycles

CABIN FLOOR PANEL C-3 HAS FIBERGLASS DAMAGE ON OVERLAPPED TONGUE. REPAIRED PANEL C-3 IAW SRM 51-70.

Part: FLOORBOARD — CHAFED (CABIN) · airframe 71,598 hrs · 87,302 cycles

CABIN FLOOR PANEL E-8 HAS CHAFED AREA AND IS MISSING CHAFE. FABRICATED AND INSTALLED NEW FLOOR PANEL.

Part: FLOORBEAM — MISDRILLED (FUSELAGE) · airframe 71,598 hrs · 87,302 cycles

STATION 160 FLOORBEAM HAS 3 NUT PLATE HOLES THAT ARE ELONGATED AT X=-18 + X=-29 + X=-47. FABRICATED AND INSTALLED NEW FLOORBEAM AND SPLICES.

Part: FLOORBOARD — DAMAGED (CABIN) · airframe 71,598 hrs · 87,302 cycles

CABIN FLOOR PANEL D-6 IS SPLITTING ON OVERLAPPING TONGUE. REPAIRED DAMAGED AREA IAW SRM 51-70-1.

Part: LONGERON — CHAFED (FUSELAGE) · airframe 71,598 hrs · 87,302 cycles

LONGERON 17, 16, AND 15 RIGHT ARE CHAFED BEYOND LIMITS AT STATION 661 PER SRM 53-01. FABRICATED AND INSTALLED NEW LONGERONS.

Part: FLOORBOARD — CRACKED (CABIN) · airframe 71,598 hrs · 87,302 cycles

CABIN FLOOR PANEL B-1 AND F-4 HAS A CRACK AND MISSING CHAFE. FABRICATED AND INSTALLED NEW CHAFE STRIP AND DOUBLER.

Part: FLOORBOARD — PUNCTURED (CABIN) · airframe 71,598 hrs · 87,302 cycles

CABIN FLOOR PANEL E-8 IS PUNCTURED AND HAS SEVERAL CRACKS. FABRICATED AND INSTALLED NEW FLOORBOARD PANEL.

Part: INTERCOSTAL — GOUGED (CARGO DOOR) · airframe 71,598 hrs · 87,302 cycles

FORWARD CARGO DOOR HAS GOUGE ON INTERCOSTAL ABOVE BEAM NR 1 AT FORWARD CORNER. FABRICATED AND INSTALLED NEW INTERCOSTAL.

Part: FLOORBOARD — CORRODED (CABIN) · airframe 71,598 hrs · 87,302 cycles

CABIN FLOORPANEL F-1 HAS AREAS OF BAREMETAL, WIDESPREAD LIGHT TO MODERATE CORROSION, AND DAMAGED FIBERGLASS SUPPORT CHANNEL. FABRICATED AND INSTALLED FLOORBOARD.

Part: FRAME — MISDRILLED (FUSELAGE) · airframe 71,598 hrs · 87,302 cycles

HOLES ARE DOUBLE DRILLED IN FRAME AT STATION 332 LONGERON 4 LEFT. MAINTENANCE FABRICATED AND INSTALLED REPAIR ANGLE, PLATE, AND FILLER.

Part: LONGERON — MISDRILLED (FUSELAGE) · airframe 71,598 hrs · 87,302 cycles

LONGERON 9 RIGHT HAS SEVERAL DAMAGED HOLES ON UPPER FLANGE BETWEEN STATION 313 - 332. FABRICATED AND INSTALLED NEW LONGERON SPLICES AND INTERCOSTAL.

Part: FLOORBOARD — CRACKED (CABIN) · airframe 71,598 hrs · 87,302 cycles

CABIN FLOOR PANEL E-1 IS CRACKED, PUNCTURED, AND HAS CORNERS CRACKED OUT. FABRICATED AND INSTALLED NEW FLOORBOARD.

Part: FLOORBOARD — PUNCTURED (CABIN) · airframe 71,598 hrs · 87,302 cycles

CABIN FLOOR PANEL B-3 HAS AREAS OF BAREMETAL AND IS PUNCTURED. FABRICATED AND INSTALLED REPAIR DOUBLER.

Part: FLOORBOARD — MISDRILLED (CABIN) · airframe 71,598 hrs · 87,302 cycles

CABIN FLOORPANEL B-7 HAS AREAS OF METAL, CHAFES, AND DOUBLE DRILLED HOLES. FABRICATED AND INSTALLED NEW FLOORBOARD.

Part: DOUBLER — CHAFED (FUSELAGE) · airframe 71,598 hrs · 87,302 cycles

NOSE LANDING GEAR WHEEL WELL PRESSURE PANEL CHAFED ABOVE RIGHT HAND NOSE WHEEL SPIN BRAKE ASSMEBLY STATION 67. FABRICATED AND INSTALLED DOUBLER REPAIR.

Part: FLOORBOARD — CHAFED (CABIN) · airframe 71,598 hrs · 87,302 cycles

CABIN FLOOR PANEL D-1 HAS A CHAFED AREA AND HAS BEEN PARTIALLY DRILLED INTO. REPAIRED DAMAGED AREA IAW SRM 51-70-1.

Part: FLOORBOARD — CRACKED (COCKPIT) · airframe 71,598 hrs · 87,302 cycles

COCKPIT CENTER FLOOR PANEL ASSY CRACKED IN SEVERAL PLACES. REPAIRED COCKPIT CENTER FLOORPANEL IAW DC-9 SRM 51-70-1.

Part: FITTING — CRACKED (CARGO DOOR) · airframe 71,598 hrs · 87,302 cycles

AFT CARGO DOOR NR 2 FORWARD INTERNAL BEAM FITTING CRACKED. FABRICATED AND INSTALLED NEW FITTING.

Part: FLOORBOARD — CRACKED (CABIN) · airframe 71,598 hrs · 87,302 cycles

CABIN FLOORBOARD B-1 HAS A FASTENER HOLE THAT IS CRACKED AT FLOORBOARD CORNER. FABRICATED AND INSTALLED DOUBLER.

Part: FLOORBOARD — DAMAGED (CABIN) · airframe 71,598 hrs · 87,302 cycles

CABIN FLOOR PANEL F-7 HAS DAMAGED FIBERGLASS SUPPORT CHANNELS AND SUPPORT CHANNEL ATTACH RIVETS HAVE INSUFFICIENT EDGE DISTANCE. FABRICATED AND INSTALLED FIBERGLASS SUPPORT CHANNELS.

Part: FLOORBOARD — DENTED (CABIN) · airframe 71,598 hrs · 87,302 cycles

CABIN FLOORPANEL B-6 HAS A DENT AND NUMEROUS CRACKS ON SKIN AND SUPPORT CHANNELS. FABRICATED AND INSTALLED NEW PANEL.

Part: INTERCOSTAL — MISDRILLED (FUSELAGE) · airframe 71,598 hrs · 87,302 cycles

HOLE IS DOUBLE DRILLED IN INTERCOSTAL AT LONGERON 9 RIGHT STATION 331. FABRICATED AND INSTALLED INTERCOSTAL AND DOUBLER.

Part: PANEL — CHAFED (NLG WW) · airframe 71,598 hrs · 87,302 cycles

NLG WHEELWELL PRESSURE PANEL CHAFED ABOVE LT NOSE WHEEL SPIN BRAKE ASSY. FABRICATED AND INSTALLED DOUBLER REPAIR.

Part: FLOORBOARD — CHAFED (CABIN) · airframe 71,598 hrs · 87,302 cycles

CABIN FLOOR PANEL A-3 HAS AREAS OF BAREMETAL AND A CHAFED AREA. FABRICATED AND INSTALLED DOUBLER.

Part: FLOORBOARD — CRACKED (CABIN) · airframe 71,598 hrs · 87,302 cycles

CABIN FLOOR PANEL A-5 HAS CRACKS AND DAMAGED FIBERGLASS SUPPORT CHANNEL. FABRICATED AND INSTALLED DOUBLER.

Part: LONGERON — DAMAGED (FUSELAGE) · airframe 71,598 hrs · 87,302 cycles

LONGERON 10 RIGHT AT STATION 710 HAS SEVERAL TOOLING MARKS. FABRICATED AND INSTALLED NEW SECTION OF LONGERON AND REPAIR SPLICE.

Part: FLOORBOARD — MISDRILLED (CABIN) · airframe 71,598 hrs · 87,302 cycles

CABIN FLOOR PANEL C-6 HAS BEEN PARTIALLY DRILLED INTO. REPAIRED HOLE IN PANEL C-6 IAW SRM 51-70-1.

Part: FLOORBOARD — CRACKED (CABIN) · airframe 71,598 hrs · 87,302 cycles

CRACK ON OUTBOARD EDGE OF FLOOR PANEL A-5. FABRICATED AND INSTALLED DOUBLER.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 71,598 hrs · 87,302 cycles

INTERCOSTAL IS CRACKED AND DEFORMED AT STATION 330 LONGERON 8 LEFT. FABRICATED AND INSTALLED REPAIR DOUBLER.

Part: FLOORBOARD — CRACKED (CABIN) · airframe 71,598 hrs · 87,302 cycles

CABIN FLOOR PANEL B-2 HAS AREAS OF BAREMETAL, AND A SECTION CRACKED OUT FROM ATTACHMENT HOLE. FABRICATED AND INSTALLED DOUBLER.

Part: FLOORBOARD — MISDRILLED (CABIN) · airframe 71,598 hrs · 87,302 cycles

CABIN FLOOR PANEL E-9 HAS DOUBLE DRILLED HOLES AND OPEN FASTENER HOLES. FABRICATED AND INSTALLED NEW REPAIR DOUBLERS.

Part: INTERCOSTAL — MISDRILLED (FUSELAGE) · airframe 71,598 hrs · 87,302 cycles

INTERCOSTAL AT LONGERON 10R AT STATION 708 HAS DOUBLE DRILLED HOLES. FABRICATED AND INSTALLED DOUBLER.

Part: FLOORBOARD — CRACKED (CABIN) · airframe 71,598 hrs · 87,302 cycles

CABIN FLOOR PANEL A-1 HAS CRACKS, CHAFES AND A PUNCTURE. FABRICATED AND INSTALLED REPLACEMENT FILLER AND DOUBLER PLATES.

Part: FLOORBOARD — CHAFED (CABIN) · airframe 71,598 hrs · 87,302 cycles

CABIN FLOOR PANEL A-2 HAS CHAFED AREAS AND CRACKS. FABRICATED AND INSTALLED DOUBLER.

Part: FLOORBOARD — DAMAGED (CABIN) · airframe 71,598 hrs · 87,302 cycles

CABIN FLOORPANEL C-5 HAS A HOLE WITH INSUFFICIENT EDGE DISTANCE. REPAIRED DAMAGED AREA IAW SRM 51-70-1.

Part: FLOORBOARD — MISDRILLED (CABIN) · airframe 71,598 hrs · 87,302 cycles

CABIN FLOOR PANEL B-9 HAS AREAS OF BAREMETAL, HOLES WITH INSUFFICIENT EDGE DISTANCE, AND MISSING CHAFE STRIP. FABRICATED AND INSTALLED REPAIR DOUBLER.

Part: FLOORBOARD — CRACKED (CABIN) · airframe 71,598 hrs · 87,302 cycles

CABIN FLOOR PANEL E-5 HAS AREAS OF BAREMETAL, A CRACK, AND A CHAFE. FABRICATED AND INSTALLED NEW DOUBLER.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 71,598 hrs · 87,302 cycles

EVIDENCE OF TOOLING DAMAGE EXITS ON FRAME 661 AT LONGERON 17L, 16L, AND 15L UNDER SHEAR CLIPS. FABRICATED AND INSTALLED NEW FRAME.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 71,598 hrs · 87,302 cycles

INTERCOSTAL CRACKED AT STATION 150 FWD OF SERVICE DOOR AT APPROXIMATELY LONGERON 13 RIGHT. FABRICATED AND INSTALLED NEW INTERCOSTAL.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 71,598 hrs · 87,302 cycles

AFT PRESSURE BULKHEAD STAIR SUPPORT CHANNEL IS CRACKED. FABRICATED AND INSTALLED REPAIR ANGLE.

Part: LONGERON — CHAFED (FUSELAGE) · airframe 71,598 hrs · 87,302 cycles

LONGERON 28 RIGHT IS CHAFED ALONG LEFT LEG BETWEEN STATION 165 - 175. FABRICATED AND INSTALLED NEW LONGERON AREA AND SPLICE.

Part: WEB — DAMAGED (FUSELAGE) · airframe 71,598 hrs · 87,302 cycles

FOUR HOLES DRILLED IN STEEL STRAP AT FRAME 312 LONGERON 29 RIGHT ON DOOR JAMB WEB. FABRICATED AND INSTALLED NEW GUSSET.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 71,598 hrs · 87,302 cycles

INTERCOSTAL AT LONGERON 28R BETWEEN STATION 160 TO 180 HAS LIGHT CORROSION. FABRICATED AND INSTALLED NEW INTERCOSTAL.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 71,598 hrs · 87,302 cycles

TOOLING DAMAGE ON FRAME 661 AT LONGERON 17R, 16R, AND 15R. FABRICATED AND INSTALLED NEW FRAME SECTION AND REPAIR SPLICES.

Part: INTERCOSTAL — DAMAGED (FUSELAGE) · airframe 71,598 hrs · 87,302 cycles

INTERCOSTAL HAS AN ELONGATED HOLE AT LONGERON 16 STATION 642 - 661. FABRICATED AND INSTALLED NEW INTERCOSTAL.

Part: STIFFENER — CRACKED (SERVICE DOOR) · airframe 71,598 hrs · 87,302 cycles

GALLEY DOOR LONGERON STIFFENER BETWEEN NR 3 AND NR 4 RIBS IS CRACKED. FABRICATED AND INSTALLED NEW LONGERON.

Part: INTERCOSTAL — BENT (FUSELAGE) · airframe 36,628 hrs · 28,428 cycles

INTERCOSTAL BENT ABOVE LONGERON 29 LEFT BETWEEN STATION 699 AND 718. FABRICATED AND INSTALLED NEW INTERCOSTAL.

Part: INTERCOSTAL — MISDRILLED (FUSELAGE) · airframe 71,598 hrs · 87,302 cycles

FIGURE 8 HOLE IN AFT PIT INTERCOSTAL BETWEEN LONGERON 28R & 27R AND STATION 800 AND 817. FABRICATED AND INSTALLED INTERCOSTAL AND BRACKET.

Part: CHANNEL — CORRODED (FLOOR SUPPORT) · airframe 71,598 hrs · 87,302 cycles

FLOOR SUPPORT J CHANNEL HAS HEAVY CORROSION AROUND SCREW HOLE AT STATION 195 CENTER OF AIRCRAFT. FABRICATED AND INSTALLED NEW J-CHANNEL.

Part: DOOR FRAME — CORRODED (CARGO DOOR) · airframe 71,598 hrs · 87,302 cycles

AFT CARGO LOWER DOOR JAMB HAS NUMEROUS LIGHT TO MODERATE CORROSION FROM STATION 718 TO 758. FABRICATED AND INSTALLED REPAIR SPLICES.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 71,598 hrs · 87,302 cycles

SUB FLOOR HAS SEVERAL SPOTS OF LIGHT CORROSION BETWEEN STATION 160 - 200. FABRICATED AND INSTALLED NEW SUB FLOOR.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 71,598 hrs · 87,302 cycles

CABIN SUB FLOOR IS CRACKED AT STATION 500. FABRICATED AND INSTALLED REPAIR DOUBLER.

Part: CHANNEL — CORRODED (FLOOR SUPPORT) · airframe 71,598 hrs · 87,302 cycles

FLOOR SUPPORT AT STATION 200 HAS LIGHT CORROSION AND LOWER SURFACE OUTBOARD OF NR 4 SEAT TRACK. FABRICATED AND INSTALLED NEW J-CHANNEL.

Part: FRAME — CHAFED (FUSLEAG) · airframe 71,598 hrs · 87,302 cycles

FRAME 680 IS CHAFED AT LONGERON 16R. FABRICATED AND INSTALLED FRAME.

Part: SKIN — DENTED (FUSELAGE) · airframe 71,598 hrs · 87,302 cycles

DENT ON RIGHT HAND EXTERIOR SKIN AT STATION 83.55 ABOUT 33 INCHES FROM NOSE GEAR DOOR. FABRICATED AND INSTALLED DOUBLER.

Part: DOUBLER — SCRATCHED (FUSELAGE) · airframe 71,598 hrs · 87,302 cycles

DEEP SCRATCHES ARE PRESENT IN STRAP UNDER LONG 9 RT AT STATION 220. FABRICATED AND INSTALLED DOUBLER.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 71,598 hrs · 87,302 cycles

LONGERON 7L IS CRACKED AT STATION 623. FABRICATED AND INSTALLED REPAIR SPLICE.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 71,598 hrs · 87,302 cycles

LONGERON 1 IS CRACKED AT STATION 566. DRILLED AND INSTALLED NEW LONGERON AREA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 71,598 hrs · 87,302 cycles

SUB FLOOR HAS SEVERAL AREAS OF CORROSION AND CRACKS AT STATION 206, 24 INCHES RIGHT OF CENTER. FABRICATED AND INSTALLED DOUBLER.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 71,598 hrs · 87,302 cycles

CABIN BEAM AND ATTACH ANGLE HAS AREAS OF LIGHT CORROSION AT STA 237. FABRICATED AND INSTALLED NEW ANGLE.

Part: FLOORBEAM — MISMANUFACTURED (FUSELAGE) · airframe 71,598 hrs · 87,302 cycles

TWO ACCESS HOLES NEED TO BE CUT IN FLOOR MEMBRANE BETWEEN STATIONS 604 - 623 AND STATIONS 623 - 642 ON THE RIGHT HAND SIDE. CUT OUT ACCESS HOLES AND FABRICATED REPAIR DOUBLERS WERE INSTALLED.

Part: INTERCOSTAL — CRACKED (CARGO DOOR) · airframe 71,598 hrs · 87,302 cycles

FORWARD CARGO COMPARTMENT DOOR JAMB UPPER AFT CORNER HAS 2 CRACKS ON INTERCOSTAL. MAINTENANCE FABRICATED AND INSTALLED INTERCOSTAL.

Part: SEAT TRACK — MISDRILLED (FUSELAGE) · airframe 71,598 hrs · 87,302 cycles

NR 1 SEAT TRACK HAS A MISDRILLED HOLE AT STATION 200. FABRICATED AND INSTALLED NEW SEAT TRACK.

Part: SKIN — DENTED (FUSELAGE) · airframe 71,598 hrs · 87,302 cycles

DENT ON EXTERIOR FUSELAGE SKIN AT STATION 218 JUST BELOW LONGERON 17 LEFT. FABRICATED AND INSTALLED REPAIR DOUBLER.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 71,598 hrs · 87,302 cycles

SUB FLOOR CRACKED STATION 237 LEFT OF NR 1 SEAT TRACK. FABRICATED AND INSTALLED SEAT TRACK.

Part: FRAME — MISDRILLED (FUSELAGE) · airframe 71,598 hrs · 87,302 cycles

STATION 294 FORMER FROM L18R - L21R HAS SEVERAL HOLES WITH SHORT EDGE DISTANCE. FABRICATED AND INSTALLED NEW FORMER.

Part: LONGERON — GOUGED (FUSELAGE) · airframe 71,598 hrs · 87,302 cycles

LONGERON L17L HAS A DEEP GOUGE AT STATION 661 UNDER THE FRAME. FABRICATED AND INSTALLED NEW LONGERON.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 71,598 hrs · 87,302 cycles

FOUND J-CHANNEL AT STATION 150 - 170 RIGHT OF GALLEY DRAIN TO FOM. FABRICATED AND INSTALLED NEW J-CHANNEL.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 71,598 hrs · 87,302 cycles

SUB FLOOR IS CRACKED AT STATION 785, 3 INCHES INBOARD OF RIGHT CUSP. FABRICATED AND INSTALLED DOUBLER.

Part: CHANNEL — CORRODED (FLOOR SUPPORT) · airframe 71,598 hrs · 87,302 cycles

FLOOR SUPPORT J-CHANNEL BETWEEN NR 3 AND NR 4 SEAT TRACK HAS LIGHT CORROSION ON UPPER AND LOWER SURFACE AT STATION 200. FABRICATED AND INSTALLED J-CHANNEL.

Part: WEB — CRACKED (FUSELAGE) · airframe 71,598 hrs · 87,302 cycles

CRACKED WEB AT STATION 838 JUST FORWARD OF AFT PRESSURE BULKHEAD RBL 18 TO RBL 25 JUST BELOW FLOOR LEVEL. FABRICATED AND INSTALLED NEW WEB.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 71,598 hrs · 87,302 cycles

LONGERON HAS A CRACKED FASTENER HOLE UNDER LONGERON SPLICE AT STATION 689 L8L. FABRICATED AND INSTALLED NEW LONGERON AND SPLICE.

Part: FRAME — DENTED (FUSELAGE) · airframe 71,598 hrs · 87,302 cycles

AFT SIDE OF FRAME 294 IS DENTED ABOVE LONGERON 20 RIGHT. FABRICATED AND INSTALLED FRAME, SPLICE, AND SHEAR TIE.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 71,598 hrs · 87,302 cycles

LONGERON 9R IS CRACKED AT STATION 642. FABRICATED AND INSTALLED NEW LONGERON AREA AND SPLICE.

Part: SKIN — DENTED (FUSELAGE) · airframe 71,598 hrs · 87,302 cycles

RIGHT HAND EXTERIOR SKIN AT STATION 110 TO 108 HAS A DENT ABOUT 2 INCHES BELOW LONGERON 20. FABRICATED AND INSTALLED REPAIR DOUBLER.

Part: DOOR FRAME — CRACKED (CARGO DOOR) · airframe 71,598 hrs · 87,302 cycles

AFT CARGO DOOR JAMB HAS A CRACK IN LOWER FORWARD CORNER. FABRICATED AND INSTALLED NEW DOUBLER.

Part: FLOORBEAM — CHAFED (FUSELAGE) · airframe 71,598 hrs · 87,302 cycles

TWO HOLES CHAFED THROUGH SUB FLOOR FORWARD OF STATION 160. FABRICATED AND INSTALLED DOUBLER.

Part: CHANNEL — CORRODED (CENTERLINE) · airframe 71,598 hrs · 87,302 cycles

REMOVED J-CHANNEL AT STATION 160 CENTERLINE TO RIGHT FUSELAGE TO FOM. FABRICATED AND INSTALLED NEW J-CHANNEL.

Part: INTERCOSTAL — DAMAGED (FUSELAGE) · airframe 71,598 hrs · 87,302 cycles

INTERCOSTAL BETWEEN STATION 256 AND 275 AT LONGERON 6R HAS A HOLE PUNCHED IN IT AT STATION 261. FABRICATED AND INSTALLED INTERCOSTAL.

Part: CHANNEL — CORRODED (FLOOR SUPPORT) · airframe 71,598 hrs · 87,302 cycles

FLOOR SUPPORT J-CHANNEL FWD OF NR 4 SEAT TRACK HAS LIGHT TO MODERATE CORROSION ON UPPER SURFACE AND AROUND SCREW HOLES ON LOWER SURFACE BETWEEN STATION 160 - 200. FABRICATED AND INSTALLED NEW J-CHANNEL.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 71,598 hrs · 87,302 cycles

FLOOR SUPPORT J-CHANNEL BETWEEN CENTER AND NR 3 SEAT TRACK HAS LIGHT CORROSION AROUND FASTENER HOLES UPPER AND LOWER SURFACE AT STATION 200. FABRICATED AND INSTALLED NEW J-CHANNEL.

Part: LONGERON — MISDRILLED (FUSELAGE) · airframe 71,598 hrs · 87,302 cycles

ONE HOLE IS EGGSHAPED AT LONGERON 15R STATION 726.5. FABRICATED AND INSTALLED LONGERON AND SPLICE.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 71,598 hrs · 87,302 cycles

NR 4 SEAT TRACK HAS LIGHT CORROSION AT STATION 200. FABRICATED AND INSTALLED NEW SEAT TRACK AND SPLICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 71,598 hrs · 87,302 cycles

SUB FLOOR HAS A SPOT OF HEAVY CORROSION AT STATION 160. FABRICATED AND INSTALLED DOUBLER.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 71,598 hrs · 87,302 cycles

INTERCOSTAL AT L17L STATION 661 - 680 HAS MODERATE CORROSION ON OUTER FLANGE. FABRICATED AND INSTALLED NEW INTERCOSTAL.

Part: LONGERON — MISDRILLED (FUSELAGE) · airframe 71,598 hrs · 87,302 cycles

LONG 16L HAS 2 MISDRILLED HOLES AT STATION 802 AFT ATTACH FASTENERS. FABRICATED AND INSTALLED NEW LONGERON AND SPLICE.

Part: SKIN — DENTED (FUSELAGE) · airframe 71,598 hrs · 87,302 cycles

DENT ON EXTERIOR FUSELAGE SKIN AT STATION 222 JUST BELOW LONGERON 16 LEFT. FABRICATED AND INSTALLED REPAIR DOUBLER.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 71,598 hrs · 87,302 cycles

NR 3 SEAT TRACK HAS LIGHT CORROSION BETWEEN STATION 200 - 238 UPPER AND LOWER SURFACE. FABRICATED AND INSTALLED SEAT TRACK.

Part: SKIN — MISDRILLED (FUSELAGE) · airframe 71,598 hrs · 87,302 cycles

MISDRILLED FASTENER HOLE ON EXTERNAL SKIN AT STATION 459 AT LONGERON 18 LEFT. FABRICATED AND INSTALLED DOUBLER.

Part: INTERCOSTAL — BUCKLED (FLOOR SUPPORT) · airframe 71,598 hrs · 87,302 cycles

AFT CARGO CENTER CEILING FLOOR SUPPORT BETWEEN STATION 737 - 758 IS BUCKLED. FABRICATED AND INSTALLED NEW INTERCOSTAL.

Part: FLOORBEAM — MISMANUFACTURED (FUSELAGE) · airframe 71,598 hrs · 87,302 cycles

FLOOR MEMBRANE NEEDS TO HAVE 2 ACCESS HOLES CUT IN FLOOR MEMBRANE AT STATION 604 - 623 AND 623 - 642, LEFT SIDE. FABRICATED AND INSTALLED REPAIR DOUBLERS.

Part: FRAME — CRACKED (FUSELAGE) · airframe 71,598 hrs · 87,302 cycles

FRAME 680 IS DENTED AND CRACKED AT LONGERON 15L AND 16L. FABRICATED AND INSTALLED NEW SPLICE AND FRAME.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 71,598 hrs · 87,302 cycles

FOUND CORROSION ON ANGLE BRACKETS AND LONGERONS CRACKED ON FRAME AT STATION 880 LONGERON 2L AND 2R. MTC INSTALLED NEW LONGERON AND ANGLES.

Part: INTERCOSTAL — CRACKED (CARGO DOOR) · airframe 71,598 hrs · 87,302 cycles

FORWARD CARGO COMPARTMENT DOOR JAMB UPPER AFT CORNER HAS 2 CRACKS ON INTERCOSTAL. FABRICATED AND INSTALLED NEW INTERCOSTAL.

Part: INTERCOSTAL — BENT (FUSELAGE) · airframe 71,598 hrs · 87,302 cycles

INTERCOSTAL BENT ABOVE LONGERON 29R BETWEEN STATION 680 AND 699. FABRICATED AND INSTALLED NEW INTERCOSTAL.

Part: SKIN — CRACKED (SUBFLOOR)

SUB FLOOR SKIN IS CRACKED AT STATION 785. FABRICATED AND INSTALLED REPAIR DOUBLER.

Part: LIGHT — FAILED (FUSELAGE)

RIGHT OVERWING EMERGENCY EXIT LIGHT IS INOPERATIVE. MAINTENANCE TROUBLESHOT AND REPAIRED GROUND FROM LIGHT BRACKET TO AIRFRAME.

Part: BATTERY PACK — DISCHARGED (CARGO COMPT)

RIGHT OVERWING EMERGENCY EXIT LIGHT DOES NOT ILLUMINATE DURING TEST. MAINTENANCE CHARGED EMERGENCY EXIT LIGHT BATTERY PACK.

Part: BEAM — MISDRILLED (COCKPIT)

THE WEB BEAM AN DOUBLER BETWEEN CAPTAINS AND SLIDING CLEARVIEW WINDOW HAS A FIGURE 8 HOLE THROUGH ON FASTENER. MAINTENANCE REMOVED AND REPLACED BEAM AND FABRICATED AND INSTALLED DOUBLER TEMPORARY REPAIR.

Part: SLIDE — LOOSE (GALLEY DOORWAY)

THE GALLEY SLIDE WAS FOUND LOOSE. MTC REINSTALLED GALLEY SLIDE.

Part: SKIN — DAMAGED (RT HORIZ STAB)

MKE - RIGHT HORIZONTAL STABILIZER HAS BLEND OUTS ON LEADING EDGE AT XFS 163.375 XFS 200.00 AND XFS 232.00 TO XH 209.125. MTC FABRICATED AND INSTALLED DOUBLER REPAIR. (X)

Part: SEAT TRACK — WORN (COCKPIT)

MKE - FOUND ELONGATED HOLES ON CAPTAIN'S RIGHT AFT SEAT TRACK. MTC FABRICATED AND INSTALLED NEW SEAT TRACK. (X)

Part: BEAM — CRACKED (PASSENGER DOOR)

MKE - FOUND CRACK ON FORWARD PASSENGER DOOR DOUBLER ON TOP SIDE OF NR 1 BEAM. MTC FABRICATED AND INSTALLED DOUBLER REPAIR. (X)

Part: SKIN — CRACKED (PAX DOORWAY)

A .5 INCH CRACK EMANATING FROM FORWARD ENTRY DOOR CUTOUT UPPER DOOR STOP SCREW HOLE. INSTALLED REPAIR IAW SRM 53-30-0 FIGURE TYPE 11 REFERENCE TELEX NUMBER M-7200-98-05166.

Part: BATTERY PACK — DISCHARGED (RT OVERWING)

FOUND RIGHT OVERWING EMERGENCY EXIT DOOR LIGHT INOPERATIVE. MTC REMOVED AND REPLACED BATTERY PACK.

Part: COVER — LOOSE (PAX DOOR)

THE FORWARD ENTRANCE SLIDE COVER FELL OFF. MTC REINSTALLED FORWARD ENTRANCE SLIDE COVER.

Part: LIGHT — DIM (CABIN)

THE PORTABLE EMERGENCY LIGHT FOUND DIM. MAINTENANCE INSTALLED SERVICEABLE PORTABLE EMERGENCY LIGHT.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

THE EMERGENCY LIGHTS AT LAST ROW OF SEATS CEILING REMAINED ON WHEN POWER TURNED OFF. MTC REMOVED AND REPLACED POWER SUPPLY.

Part: CLIP — DAMAGED (WS 69)

REMOVED CLIP FROM LEFT HAND WING AT STATION 69 STRINGER 11 TO FACILITATE OTHER MAINTENANCE. MTC FABRICATED AND INSTALLED STRINGER CLIP.

Part: CLIP — CRACKED (WS 111)

FOUND CRACKED LEFT WING RIB 111 MOST AFT LOWER SHEAR CLIP. MTC FABRICATED AND INSTALLED SHEAR CLIP.

Part: ANGLE — CRACKED (LT WING)

FOUND A 2 INCH CRACK AND CORROSION ON LEFT HAND WING BETWEEN XRS 69 AND 91 AT STRINGER 11. MTC FABRICATED AND INSTALLED REPAIR SPLICE ANGLES.

Part: TEE — CRACKED (LT WING)

FOUND CRACK ON LEFT WING LOWER TEE OUTBOARD LOWER LEG AT STATION 58. MTC REMOVED AND REPLACED TEE.

Part: DOUBLER — DAMAGED (BS 256)

REMOVED TCAS ANTENNA AND DOUBLER STATION 256 FRAME SHEAR CLIP FASTENERS IN SKIN LAP AT STATION 229, L27 LEFTHAND TO L28 RIGHT HAND TO FACILITATE OTHER MAINTENANCE. MTC REINSTALLED ANTENNA DOUBLER AND SHEAR CLIP.

Part: BULKHEAD DOOR — CRACKED (AFT PRESS BLKHD)

FOUND CRACK ON VENTRAL DOOR JAMB UPPER RIGHT CORNER. MTC REPAIRED WITH 5 DOUBLERS.

Part: SPLICE — CRACKED (BS 237)

FOUND CRACK ON FORWARD CARGO LONGERON 2L AT STATION 237 ON LEFT VERTICAL LEG. MTC FABRICATED AND INSTALLED LONGERON AND SPLICE.

Part: STRAP — MISINSTALLED (AFT PRESS BLKHD)

THE AFT VENTRAL DOOR JAMB UPPER LEFT AND RIGHT CORNER STRAPS HAVE BEEN TRIMMED INCORRECTLY. MTC FABRICATED AND INSTALLED STRAPS.

Part: STRINGER — CORROSION (WS 67)

FOUND CORROSION ON LEFT WING STRINGER 12 AFT LEG AT STATION XRS 67. MTC FABRICATED AND INSTALLED REPAIR ANGLE.

Part: LONGERON — CRACKED (BS 786)

FOUND CRACK ON LONGERON 17R AT STATION 786 ATTACH BOLTS. MAINTENANCE REMOVED LONGERON SECTION FABRICATED AND INSTALLED NEW SECTION.

Part: LANYARD — FRAYED (GALLEY DOOR)

GALLEY SERVICE DOOR EVACUATION SLIDE GIRT BAR LANYARD FRAYED. FABRICATED AND INSTALLED GIRT BAR LANYARD.

Part: SLIDE — DEPLOYED (PAX DOOR)

THE FORWARD ENTRANCE DOOR SLIDE FELL OUT OF DOOR WHEN OPENED. MTC INSTALLED FORWARD ENTRANCE DOOR SLIDE.

Part: DE-ICE SYST — MISWIRED (LT WINDSHIELD)

CAPTAINS WINDSHIELD DEVELOPED ICE ON IT IMPAIRING VISIBILITY. MTC SWAPPED WIRES AT THE WINDSHIELD TEMP SENSOR AND RESET THE TRIPPED CIRCUIT BREAKER.

Part: FUEL PRESS SW — DEFECTIVE (RT ENGINE)

IN CLIMBOUT, THE RT FUEL INLET PRESS LOW LIGHT CAME ON AND COULD NOT BE PUT OUT WITH EITHER RT PUMPS OR LT BOOST PUMPS WITH THE FUEL CROSSFEED OPEN. MTC REMOVED AND REPLACED RT ENGINE FUEL PRESS SWITCH.

Part: DOOR — CRACKED (PAX DOOR)

DURING C-CHECK, FOUND CRACK ON FORWARD PAX DOOR UPPER AFT CORNER. REPAIRED IAW SRM 51-10-3 AND SRM 52-05.

Part: SKIN — CRACKED (PAX DOOR)

DURING C-CHECK, FOUND CRACK ON FORWARD PAX DOOR BEAM NR 1 AFT END. REPAIRED IAW SRM 52-05-05 FIG 31.

Part: SKIN — CRACKED (LT MLG DOOR)

DURING C-CHECK, FOUND CRACK ON LEFT MLG INBOARD DOOR SKIN. REPAIRED IAW DC9 SRM 52-05 PAGE 25.

Part: SLIDE — DEFECTIVE (GALLEY DOOR)

DURING TRANS CHECK, FOUND EMERG GALLEY SLIDE PRESS LOW. MTC REMOVED AND REPLACED SLIDE.

Part: SLIDE — PROTRUDING (GALLEY DOOR)

DURING TC, FOUND GALLEY EMERG SLIDE PROTRUDING BEHIND PLASTIC COVER. MTC REMOVED AND INSTALLED SLIDE IAW DAC MM 25-62-0.

Part: DOOR PAN — CRACKED (CARGO DOOR)

DURING C-CHECK, FWD CARGO DOOR PAN AFT SIDE CRACKED. MAINT REPAIRED IAW SB 52-89 R6 DACO DRW 5934104.

Part: OIL SYSTEM — BLOW BY (APU)

CREW REPORTS, SMOKEY SMELL IN CABIN. MAINT RAN APU AND CYCLE MACHS, NO SMELL NOTED. SUSPECT OIL BLOW FROM APU.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

DURING A-CHECK, FOUND SEVERAL EMER POWER CEILING LIGHTS INOP IN AFT CABIN. REPLACED BATTERY POWER SUPPLY, OPS CHECK GOOD.

Part: SKIN — DENTED (BS 40/55)

DURING TOWING, THE A/C RECEIVED SKIN DAMAGE WHEN COMING IN CONTACT WITH TOWING UNIT. TWO DENTS AT STA 40 AND 55 ABOVE LT NOSE GEAR DOOR. INSTALLED REPAIRS IAW SRM 53-01 FIG 4, SHT 3.

Part: SKIN — CRACKED (FS 737/786)

AFT FUS UPPER SKIN CRACKS, FS 786, LONG 7L, 1 INCH AND .75 INCH IN LENGTH, ONE AT FS 737, LONG 7L, .75 INCH IN LENGTH. REPAIRED CRACKS IAW DC9 SRM 53-04, FIG 38.

Part: SKIN — CRACKED (FS 859)

DURING C-CHECK, FOUND SKIN CRACK AT FS 859, .25 INCH IN LENGTH EMANATING FROM FASTENER HOLE LONGERON 13R. INSTALLED DOUBLER REPAIR IAW SRM 53-01, FIG 2 SHEET 3.

Part: ESCAPE ROPE — DEPLOYED (FLT COMPT)

PILOT REPORTS, UPON LANDING IN MKE THE F/O'S ESCAPE ROPE DEPLOYED AND UNRAVELED. MAINTENANCE RESECURED ESCAPE ROPE.

Part: SLIDE COVER — FELL OFF (PAX DOOR)

CREW REPORTS FORWARD ENTRANCE DOOR SLIDE COVER FELL OFF. RESECURED DOOR SLIDE COVER.

Part: MEGAPHONE — INOP (AFT CABIN)

CREW REPORTS, A/C MEGAPHONE INOP. MAINTENANCE REMOVED AND REPLACED MEGAPHONE AND RETURNED A/C TO SERVICE.

Part: FRAME — CORRODED (BS 786)

DURING CORROSION TASK INSPECTION OF AFT CARGO BAY, FOUND LIGHT CORROSION TO AFT FACE OF FRAME BETWEEN LONGERON 39R AND 29L, STA 786. MAINTENANCE INSTALLED REPAIR DOUBLER IAW SRM 53-03, AIRCRAFT RETURNED TO SERVICE.

Part: SKIN — CHAFED (VERT STAB)

DURING CORROSION TASK INSPECTION OF VERTICAL STABILIZER, FOUND THE LEFT HAND FORWARD SKIN CHAFED UNDER HORIZONTAL STABILIZER FAIRING. MAINTENANCE REMOVED AND REPLACED SKIN IAW 55-01 PG 1, AIRCRAFT RETURNED TO SERVICE.

Part: SWITCH WASHER — LOOSE (RT MLG)

PILOT REPORTS, ON CLIMBOUT THE RIGHT GEAR RED UNSAFE LIGHT WOULD NOT EXTINGUISH, PERFORMED QRH PROCEDURES, RETURNED TO MKE. MAINTENANCE FOUND RIGHT UPLATCH SWITCH STRIKER WASHER LOOSE, STRIKER HAD JUMPED WASHER. SECURED WASHER, OPS CHECK GOOD. RETURNED A/C TO SERVICE.

Part: EEL SIGN — DETACHED (FWD GALLEY)

THE EMERGENCY EXIT LIGHT SIGN CAME OFF THE WALL, NEXT TO THE FWD GALLEY SERVICE DOOR. MAINTENANCE INSTALLED NEW SIGN. OPS CHECK GOOD AND RETURNED A/C TO SERVICE.

Part: SKIN — CRACKED (CARGO DOOR)

DURING ROUTINE INSPECTION, THE AFT CARGO DOOR SKIN WAS FOUND CRACKED ON LOWER EDGE. MAINTENANCE INSTALLED REPAIR DOUBLER IAW SRM 52-05 FIG 4. RETURNED A/C TO SERVICE.

Part: SKIN — CRACKED (CARGO DOOR)

DURING ROUTINE INSPECTION, THE FWD CARGO DOOR SKIN WAS FOUND CRACKED ON LOWER FWD CORNER. MAINTENANCE INSTALLED REPAIR DOUBLER IAW 52-05 FIG 4. RETURNED A/C TO SERVICE.

Part: SLIDE COVER — FELL OFF (PAX DOOR)

CREW REPORTS, EVACUATION SLIDE COVER FELL OFF OF MAIN ENTRANCE DOOR. MAINTENANCE RE-INSTALLED EVACUATION SLIDE COVER. RETURNED A/C TO SERVICE.

Part: DOOR JAMB — CRACKED (FWD ENT DOOR)

DURING ROUTINE INSPECTION IT WAS FOUND THAT FWD PAX ENTRANCE DOOR JAMB HAD A 1.25 INCH CRACK AT UPPER FWD CORNER. REPAIRED DOOR JAMB IAW SRM 53-05, FIG, 26. RETURNED A/C TO SERVICE.

Part: WATER LINE — DISCONNECTED (FWD BAG COMPT)

PILOT REPORTED STIFF AILERONS IN FLIGHT. MECHANICS FOUND LINE FOR WATER SYSTEM DISCONNECTED WHICH CAUSED WATER TO DRAIN INTO WHEEL WELLS FORMING ICE ON AILERON PULLEY CLUSTERS. REMOVED ICE FROM PULLEYS. INSPECTED CABLES AND PERFOMRED OPS CHECK. RETURNED A/C TO SERVICE.

Part: EVAC SLIDE — DETACHED (PAX DOOR)

PILOT REPORTS MAIN ENTRANCE DOOR EVACUATION SLIDE FELL OFF. MECHANICS RESECURED EVACUATION SLIDE AND RETURNED A/C TO SERVICE.

Part: EVAC SLIDE — FELL OFF DOR (PAX DOOR)

DURING ROUTINE MAINTENANCE, THE PAX DOOR EMERGENCY SLIDE FELL OUT. RESECURED EMERGENCY SLIDE IN DOOR SLIDE HOLDER. RETURNED A/C TO SERVICE.