Meridian Air Group, Inc.

Part: HINGE — WORN (LT MLG DOOR) · airframe 77,006 hrs · 90,940 cycles

LT MLG OUTBOARD FLYING DOOR. THE ARTICULATING DOOR HINGE HAS A FAIR AMOUNT OF MOVEMENT VERTICALLY. REMOVED, LOCATED AND DRILLED WORN HINGE SECTION AND INSTALLED HINGE SECTION AND FLYING DOOR.

Part: RIB — TORN (WING) · airframe 77,006 hrs · 90,940 cycles

AFT END OF XCW 42 RIBS IS TORN ABOUT MIDWAY UPPER WEB. FABRICATED FILLER AND REPAIRED DOUBLER, LOCATED AND DRILLED FILLER AND DOUBLER, INSTALLED FILLER AND DOUBLER.

Part: INTERCOSTAL — GOUGED (FUSELAGE) · airframe 77,006 hrs · 90,940 cycles

AFT CARGO COMPARTMENT INTERCOSTAL AT LONGERON 29 RIGHT HAS GOUGES ALONG AFT END AT STATION 785. REMOVED INTERCOSTAL, DRILLED UP AND INSTALLED NEW INTERCOSTAL.

Part: INTERCOSTAL — DAMAGED (FUSELAGE) · airframe 77,006 hrs · 90,940 cycles

INTERCOSTAL AT FRAME STATION 340 BETWEEN LONGERON 28 AND 29 DAMAGED. REMOVED INTERCOSTAL, FIT AND DRILLED UP AND INSTALLED NEW INTERCOSTAL.

Part: LONGERON — DAMAGED (FUSELAGE) · airframe 77,006 hrs · 90,940 cycles

AFT CARGO LONGERON 29 RIGHT HAS ELONGATED HOLES TWO EACH STATION 785 FRAME LOCATION. FABRICATED AND INSTALLED SECTION OF LONGERON. REMOVED AND INSTALLED SHOVEL CLIP.

Part: FRAME — CRACKED (FUSELAGE) · airframe 77,006 hrs · 90,940 cycles

FASTENER HOLES AT FRAME STATION 785 AND LONGERON 22 LEFT IS CRACKED. FABRICATED, LOCATED AND DRILLED AND INSTALLED FRAME SPLICE. REMOVED AND INSTALLED SHEAR TIE.

Part: SPLICE — DAMAGED (WING) · airframe 77,006 hrs · 90,940 cycles

FASTENER HOLES DAMAGED IN CENTER TANK ON STRINGER 17 AFT SPLICE PLATE APPROXIMATELY 1 INCH LEFT OF STATION 0 BULKHEAD. SPOTFACED HOLE TO REMOVE DAMAGE, FABRICATED AND INSTALLED FASTENERS IN STRAP.

Part: CLIP — CRACKED (CENTER TANK) · airframe 77,006 hrs · 90,940 cycles

CENTER TANK FORWARD SPAR ACCESS WEB 8 EACH INSULATION ATTACH CLIPS REQUIRE REMOVAL TO FACILITATE OTHER MAINTENANCE. REMOVED AND INSPECTED CLIPS, FABRICATED AND INSTALLED CLIPS.

Part: INTERCOSTAL — DAMAGED (FUSELAGE) · airframe 77,006 hrs · 90,940 cycles

INTERCOSTAL AT FRAME STATION 332 BETWEEN LONGERON 28 AND 29 DAMAGED. REMOVED INTERCOSTAL, FABRICATED FIT AND DRILLED CLIPS AND INTERCOSTAL, INSTALLED INTERCOSTAL AND CLIP.

Part: INTERCOSTAL — DAMAGED (FUSELAGE) · airframe 77,006 hrs · 90,940 cycles

AT STATION 766 LONGERON 29 RIGHT INTERCOSTAL FORWARD ATTACH CLIP HAS ELONGATED HOLE. REMOVED ATTACH CLIP, FABRICATED AND INSTALLED CLIP.

Part: INTERCOSTAL — DAMAGED (FUSELAGE) · airframe 77,006 hrs · 90,940 cycles

REMOVED INTERCOSTAL FROM STATION 785 TO 800 AT LONGERON 29 RIGHT TO FACILITATE MAINTENANCE. FOUND ELONGATED HOLES. LOCATED AND DRILLED INTERCOSTAL, INSTALLED INTERCOSTAL.

Part: SHEAR TIE — DAMAGED (FUSELAGE) · airframe 77,006 hrs · 90,940 cycles

REMOVED SHEAR TIE AT STATION 785 FROM LONGERON 21 LEFT TO 27 LEFT TO FACILITATE MAINTENANCE. SHEAR TIE HAS SEVERAL ELONGATED HOLES, LOCATED AND DRILLED AND INSTALLED SHEAR TIE.

Part: ATTACH ANGLE — DAMAGED (VERTICAL STAB) · airframe 77,006 hrs · 90,940 cycles

STATION 930 FRAME AT THE RIGHT DORSAL FIN ATTACH ANGLE HAS A FASTENER PULLING THROUGH. REMOVED 2 HI-LOKS FROM RIGHT SIDE, REAMED 2 HOLES, FABRICATED AND INSTALLED SLEEVE BUSHING.

Part: ATTACH ANGLE — DAMAGED (VERTICAL STAB) · airframe 77,006 hrs · 90,940 cycles

STATION 930 AT THE LEFT DORSAL FIN ATTACH ANGLE HAS TWO FASTENERS PULLING THROUGH. REMOVED 2 HI-LOKS, FABRICATED AND INSTALLED SLEEVE BUSHINGS.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 77,006 hrs · 90,940 cycles

FORWARD CARGO COMPARTMENT LOWER DOOR JAMB HAS SEVERAL AREAS OF MODERATE CORROSION STATION 312 TO 370. REMOVED DAMAGED SECTION FIT, DRILLED SECTION AND INSTALLED NEW SECTION.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 77,006 hrs · 90,940 cycles

FORWARD CARGO COMPARTMENT FLOOR SUPPORT AT STATION 218 HAS SEVERAL AREAS LIGHT CORROSION LONGERON 30 TO 28 RIGHT DOT 469. HEAT TREATED 2 DOUBLERS, LOCATED AND DRILLED DOUBLER, INSTALLED REPAIR DOUBLER, LOCATING AND DRILLED REMAINING FLOOR LINING, INSTALLED 2 NUT PLATES.

Part: FITTING — CORRODED (RT WING) · airframe 77,006 hrs · 90,940 cycles

RIGHT WING XCW 58 LOWER WING TEE REQUIRES REPAIR OR REPLACEMENT DUE TO CORROSION REMOVAL. REMOVED WING TEE, RECEIVED NEW WING TEE, LOCATED AND DRILLED AND INSTALLED WING TEE.

Part: INTERCOSTAL — DAMAGED (FUSELAGE) · airframe 77,006 hrs · 90,940 cycles

INTERCOSTAL AT LONGERON 29 BETWEEN FRAME STATION 313 AND 370 HAS A LARGE HOLE ON UPPER AFT END. REMOVED AND INSTALLED INTERCOSTAL.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,006 hrs · 90,940 cycles

NOSE SKIN HAS 4 POSSIBLE CRACKS AT STATION 76.6, 18 INCHES LEFT OF CENTER AREA NEEDS TO BE STRIPPED AND VERIFIED. VERIFIED CRACKS LOCATED AND DRILLED PILOT HOLES AND FABRICATED DOUBLER.

Part: INTERCOSTAL — DAMAGED (FUSELAGE) · airframe 77,006 hrs · 90,940 cycles

INTERCOSTAL AT FRAME STATION 320 BETWEEN LONGERON 28 AND LONGERON 29 DAMAGED. FIT AND DRILLED INTERCOSTAL, REMOVED AND INSTALLED INTERCOSTAL.

Part: SHEAR TIE — DAMAGED (FUSELAGE) · airframe 77,006 hrs · 90,940 cycles

AT FRAME STATION 786 FRAME TO SKIN SHEAR TIE HAS NUMEROUS ELONGATED HOLES FROM LONGERON 30 TO 27 LEFT. LOCATED AND DRILLED SHEAR TIE, REMOVED AND INSTALLED SHEAR TIE.

Part: INTERCOSTAL — DAMAGED (FUSELAGE) · airframe 77,006 hrs · 90,940 cycles

INTERCOSTAL AT FRAME STATION 360 BETWEEN LONGERON 29 DAMAGED. FIT AND DRILLED INTERCOSTAL REMOVED AND INSTALLED INTERCOSTAL.

Part: INTERCOSTAL — DAMAGED (FUSELAGE) · airframe 77,006 hrs · 90,940 cycles

INTERCOSTAL AT FRAME STATION BETWEEN LONGERON 28 AND 29 DAMAGED. FIT AND DRILLED INTERCOSTAL REMOVED AND INSTALLED INTERCOSTAL.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 77,006 hrs · 90,940 cycles

FORWARD CARGO COMPARTMENT HAS LIGHT CORROSION ON INTERCOSTAL AT STA 218-237 BETWEEN LONGERON 28R-27R. DRILLED UP NEW INTERCOSTAL, REMOVED AND INSTALLED INTERCOSTAL.

Part: INTERCOSTAL — CRACKED (CARGO DOOR) · airframe 77,006 hrs · 90,940 cycles

FORWARD CARGO DOOR HAS A CRACKED INTERCOSTAL OUTBOARD OF LOWER AFT STOP FITTINGS BELOW BEAM 1. LOCATED AND DRILLED INTERCOSTAL. REMOVED AND INSTALLED INTERCOSTAL.

Part: CONNECTOR — FAULTY (LT ENGINE) · airframe 76,783 hrs · 90,783 cycles

LEFT ENGINE OIL TEMPERATURE IS PEGGED. PRESSURE AND QUANTITY IS NORMAL PER QRH. ENGINE NOT SHUT DOWN WITHIN 15 MINUTE LIMIT WHEN AIRCRAFT LANDED AT MILWAUKEE. FUEL TEMPERATURE ALSO DID NOT INCREASE. REPAIRED AND REPLACED LEFT ENGINE OIL TEMPERATURE CONNECTOR AND TEMPERATURE BULB.

Part: ENGINE — MALFUNCTIONED (LEFT) · airframe 75,914 hrs · 90,188 cycles

AT CRUISE ALT LEFT ENGINE MASTER CAUTION, LEFT ENGINE OIL PRESSURE LOW ANNUNCIATOR ON. LEFT ENGINE OIL PRESSURE IS ZERO. LEFT OIL TEMP IS 20 DEGREES CELSIUS AND QUANTITY IS 17-18 QUARTS. SHUT DOWN BY SELECTION. REMOVED AND REPLACED ENGINE.

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

PASSENGER DOOR HANDLE HOUSING CRACKED. REMOVED AND REPLACED HOUSING.

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: 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: 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: 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: 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: 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: 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: 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: 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: 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: 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: 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.