N293UE

ATA 5210

Part: CHANNELS — CRACKED (PAX DOOR)

ATW - FORWARD PASSENGER LT DOOR HAS 2 L-CHANNELS CRACKED AT BOTTOM OF THE DOOR HANDLE BOX STRUCTURE. CRACKS WERE CONFIRMED WITH EDDY CURRENT INSP. CORRECTIVE ACTION: REMOVED BOTH ANGLE BRACKETS. BENT NEW ANGLES AND INSTALLED IAW BAE 146 SRM CHAPTERS 51 AND 52 ON FORWARD PASSENGER DOOR JUST BELOW DOOR HANDLE BOX 52-11-11 DETAIL (E). SEE ADDITIONAL WC'S NR 2280 AND 2281.

ATA 5313

Part: LONGERON — CHAFED (FUSELAGE)

ATW - RT MOST UPPER AIRBRAKE HINGE MOUNTING LONGERON ASSY HAS BEEN CHAFED BY THE AIRBRAKE ACTUATOR TO A DEPTH OF .040 INCH. CORRECTIVE ACTION: REPAIRED CHAFED AREA IAW BAE FAX DJR/RJ063096 AND BAE SRM CHAPTER 51-00-00 STANDARD PRACTICES AND PROCEDURES.

ATA 5320

Part: GUSSET — BROKEN (FUSELAGE)

ATW - GUSSET PLATE FOR RT AIRBRAKE TOP HINGE LONGERON TO AFT WEB BROKE AFT AT LONGERON. CORRECTIVE ACTION: FABRICATED GUSSET IAW ASSY ON BAE R.I.L. NR HC539H0229 AND INSTALLED PER 51-00-00 OF THE SRM.

ATA 5313

Part: LONGERON — DAMAGED (FUSELAGE)

ATW - FORWARD PASSENGER DOOR FUSELAGE UPPER LONGERON AFT OF FUSELAGE FR NR 14 HAS DRILL MARK BOTTOM SURFACE APPROXIMATELY .018 INCH DEEP. PART NEEDS TO BE MADE, CHECKED, ALODINED, NOTED FOR CRACKS. CORRECTIVE ACTION: REC'D FAX JM/RJ0624-96 DAI/1011/55 ALLOWING REPAIR PIECE MADE/INSTALLED. MADE REPAIR PER FAX. PART HEAT TREATED AND CHECKED FOR T-81 CONDITION. ALODINED AND PAINTED PART. DRESSED AREA. NDT'D, NO CRACKS.

ATA 5320

Part: BRACKET — CRACKED (FUSELAGE)

ATW - BRACKET ATTACHED TO THE FRAME CAP OF FRAME 45 AT 12 O'CLOCK POSITION THAT HAS THE LT PACK VALVE DUCTING ATTACHED HAS A RIVET ALMOST SHEARED OFF AND CRACKED. CORRECTIVE ACTION: REPLACED BRACKET IAW AVRO FAX REF DJR/RJ0630-96 AND DRAWING HC361J0137.

ATA 5320

Part: SUPPORT — CRACKED (CARGO COMPT)

ATW - FORWARD CARGO BAY; FLOOR SUPPORT CRACKED FORWARD END. MARKED. NEAR TIE-DOWN RING. REF IPC 53-21-05-30T. CORRECTIVE ACTION: REPAIRED INTERCOSTAL.

ATA 5320

Part: ANGLE — CRACKED (CARGO COMPT)

ATW - FORWARD CARGO BAY; FLOOR SUPPORT ANGLE CRACKED NEAR TIE-DOWN RING (OTBD). MARKED. CORRECTIVE ACTION: REPALCED ANGLE.

ATA 5320

Part: ANGLE — CRACKED (CARGO COMPT)

ATW - FORWARD CARGO BAY SUPPORT FOR FORWARD OTBD TIE-DOWN CRACKED AT BOTH ENDS. REF IPC 53-21-05-30T (MARKED). CORRECTIVE ACTION: REPLACED ANGLE.

ATA 5753

Part: BOLT — FAILED (NR 6 TE FLAP)

ATW - RT FLAP TAB HINGE NR 6 BOLT/PIN FAILED NDT. CORRECTIVE ACTION: REMOVED AND REPLACED NR 6 RT FLAP TAB HINGE BOLT.

ATA 5753

Part: BOLT — FAILED (NR 3 TE FLAP)

LT FLAP TAB HINGE NR 3 BOLT/PIN FAILED NDT. CORRECTIVE ACTION: REPLACED NR 3 HINGE BOLT.

ATA 5330

Part: SKIN — DAMAGED (LT MLG)

ATW - PERMANENT REPAIR TO BE C/W ON LT FORWARD MLG FAIRING ZONE 725 AND DIAPHRAM DUE IN 1800 CYCLES AT 16005 CYC PER AW FAX'S LM/100-95, LM/101-95, LM/102-95 AND BAE FAX JM/RJ1321-95 =1=HC535H0040-200U, SKIN. CORRECTIVE ACTION: REPLACE LT FORWARD MLG FAIRING SKIN PANEL, DIAPHRAM AND CAMLOC ATTACH BRACKET JUST FORWARD OF PANEL 725BB.

ATA 2710

Part: CABLES — OUT OF ADJUST (AILERON)

ATW - AILERON INTERCONNECT CABLES WORN AT THE RIGHT SIDE FUSELAGE PRESSURE SEALS. CORRECTIVE ACTION: REMOVED AND REPLACED AND ADJUSTED INTERCONNECT CABLES IAW BAE MM 27-11-44 AND 00. GENERATED W/C TO C/W AILERON CONTROLS CK.

ATA 5330

Part: SKIN — DENTED (FUSELAGE)

ATW - C/W A PERMANENT REPAIR TO DENT IN RT FUSELAGE LOCATED 6 INCHES FORWARD OF FRAME 21 AND 51 INCHES BELOW SKIN LAP JOINT. REPORTED CLASS 'A' DAMAGE X=1.812 INCH, D=.032 INCH. CORRECTIVE ACTION: REPAIRED IAW SRM 53-00-12, PAGES 206-208, AND AVRO FAX REF JM/RJ606-96. SCANNED AREA AFTER DAMAGE WAS REMOVED USING ET PER AWAC NDT SPEC TO ASSURE IT IS CRACK FREE. NO INDICATIONS NOTED AT THIS TIME, 5-20-96.

ATA 5400

Part: RIB — CRACKED (NR 2 PYLON)

ATW - NR 2 PYLON CENTER BOX BETWEEN RIBS 4 AND 5 HAS A CRACK ON THE LOWER FLANGE OF RIB NR 5 THAT IS APPROXIMATELY .4375 INCH LONG. CORRECTIVE ACTION: NR 2 PYLON RIB NR 5 CRACK HAS BEEN REPORTED TO AVRO RDO AND IS ACCEPTABLE FOR SERVICE PER RIL HC546H9018. GENERATED W/C FOR REINSP.

ATA 5320

Part: STIFFENERS — CRACKED (BS 25.94)

ATW - REF EO E95/003/653 ORIG ITEM 3 . TWO CRACKED STIFFENERS FOUND AT POSITIONS 25.94 ON RT SIDE AND AT POSITION 25.94 ON LT SIDE. C/W EO E95/005/653 ORIG FOR REPAIR. CORRECTIVE ACTION: C/W EO E95/005/653, 2/6/95. INSTALLATION OF REPAIR STIFFENERS, POSITIONS 25.94 LT AND RT SIDES. PERFORMED ET AND POSITIONS 25.94 LT AND RT AROUND CUTLINE AFT. DAMAGE REMOVED PER NOTE '1' OF DRAWING AW-53-20-9506-06.

ATA 5400

Part: RIB — CRACKED (NR 2 PYLON)

ATW - NR 2 PYLON CENTER BOX BETWEEN RIBS 3 AND 4 HAS A CRACK ON THE LOWER FLANGE OF RIB NR 4 THAT IS APPROXIMATELY .4375 INCH LONG. CORRECTIVE ACTION: NR 2 PYLON RIB NR 4 CRACK HAS BEEN REPORTED TO AVRO RDO AND IS ACCEPTABLE FOR SERVICE PER RIL HC546H9018. GENERATED W/C FOR REINSP.

ATA 5400

Part: RIB — CRACKED (NR 4 PYLON)

ATW - NR 4 PYLON CENTERBOX BETWEEN RIBS 3 AND 4 HAS A CRACK IN LOWER FLANGE OF RIB 4 THAT IS APPROXIMATELY .3125 INCH LONG HAS BEEN REPORTED TO AVRO BAE RDO AND IS ACCEPTABLE FOR SERVICE PER RIL HC546H9018. GENERATED W/C FOR REINSP.

ATA 5400

Part: RIB — CRACKED (NR 3 PYLON)

NR 3 PYLON CENTER BOX BETWEEN RIBS 3 AND 4 HAS A CRACK IN LOWER FLANGE OF RIB 4 THAT IS APPROXIMATELY .25 INCH LONG. CORRECTIVE ACTION: NR 3 PYLON RIB 4 LOWER FLANGE APPROXIMATELY .25 INCH CRACK HAS BEEN REPORTED TO AVRO/RDO AND IS ACCEPTABLE FOR SERVICE PER RIL HC54R6H9018. GENERATED W/C FOR REINSP.

ATA 5320

Part: ANGLE — CRACKED (CARGO COMPT)

ATW - FREIGHT ANGLE AT FRAME 36 REAR CARGO BAY IS CRACKED AND CORRODED. CORRECTIVE ACTION: REMOVED AND REPLACED CRACKED AND CORRODED FREIGHT ANGLE LOCATED AT FRAME 36 IN REAR CARGO BAY.