N606AW

Part: BRACKET — IMPROPER (LT ELEVATOR)

LEFT ELEVATOR NR 2 HINGE 'A' FRAME TOP MOUNTING BOLT HAS AN IMPROPER SAFETY BRACKET, POORLY MANUFACTURED. REPLACED WITH NWE PART NR HC551B0098-000. (M)

Part: SKIN — DAMAGED (T/E FLAP)

DAMAGED RIGHT OUTBOARD FLAP TAB BOTTOM SKIN BETWEEN RIBS 21-22. REPAIR IAW BAE FAX BARA/AVR/6530/03-DC. (M)

Part: STRINGER — CORRODED (FUSELAGE)

FOUND STRINGER 33 LEFT BETWEEN FRAME 34 AND 35 CORRODED BEYOND LIMITS OF SRM 53-00-00-101. REV AVMAX NON-ROUTINE 1204 FOR REPAIR. REPAIRED STRINGER IAW SRM 53-00-12 FIG 207. (M)

Part: STRINGER — CORRODED (FUSELAGE)

FOUND STRINGER 33 RIGHT BETWEEN FRAME 34 AND 35 CORRODED BEYOND LIMITS OF SRM 53-00-00-101 AVMAX NON-ROUTINE 2289 FOR REPAIR. REPAIRED STRINGER IAW BAE SRM 53-00-12 FIG 207. (M)

Part: STRUCTURE — DAMAGED (LT WING TE FLAP)

DAMAGED BUSHING BORES AT LT WING FLAP STRUCTURE AT TRACK 2. MAINTENANCE REQUESTED REPAIR FROM BAE REF AVMAX FAX NR 1655-6060005. (M)

Part: DOOR FRAME — GOUGED (FUSELAGE)

AFT CARGO DOOR OUTSIDE DOOR SURROUND GOUGED AT TOP AFT RADIUS MAINTENANCE REQUESTED REPAIR FROM BAE REF AVMAX FAX NR 1655-6060004. (M)

Part: STRUCTURE — CRACKED (FUSELAGE)

FOUND CRACK AT RIVET LOCATION JUST AFT OF FRAME 29 STRINGER 13 LT. MAINTENANCE REQUESTED REPAIR FROM BAE REF AVMAX FAX NR 1655-6060002. (M)

Part: SKIN — DAMAGED (CARGO DOOR)

DAMAGE EXTERNAL SKIN TO THE FORWARD CARGO DOOR MAINTENANCE REQUESTED REPAIR FROM BAE REF AVMAX FAX NR 1655-6060001. (M)

Part: FRAME — CORRODED (FUSELAGE)

FOUND CORROSION ON FRAME 18 MAINTENANCE REQUESTED REPAIR FROM BAE REF AVMAX FAX NR 1655-6060003. (M)

Part: A/C PACK — SMOKE

PACKS EMITTING SMOKE INTO CABIN MAINTENANCE REMOVED AND REPLACED APU, PERFORMED PACK BURNOUT IAW AWAC SUPP 96.31. (M)

Part: CLAMP — OUT OF POSITION (MLG ACTUATOR)

DAMAGE TO THE MAIN LANDING GEAR BAY SKIN AT FRAME 29 LEFT SIDE AS CAUSED BY DOWN LOCK ACTUATOR CLAMP. MAINTENANCE DAMAGE BLENDED OUT IAW SRM 51-10-2. (M)

Part: WEB — DAMAGED (FUSELAGE) · airframe 30,332 hrs · 44,568 cycles

DAMAGE TO WEBS ABOVE AND BELOW FORWARD PASSENGER DOOR DAMPER CAN. MAINTENANCE REMOVED AND REPLACED DAMPER CAN LOWER AND UPPER WED ASSEMBLIES IAW BAE 146 SRM.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 30,332 hrs · 44,568 cycles

LONGERON ON THE RT SIDE, AT THE TOP OF SERVICE DOOR AFT OF FRAME 19 AT THE FRAME HAS A CRACK. MAINTENANCE FOUND CLEAT OF DIAPHRAM CRACKED AND REPAIRED BY PATCHING IAW BAE SRM 51-71-11 AND FOUND SERVICEABLE.

Part: FRAME — CRACKED (FUSELAGE) · airframe 30,332 hrs · 44,568 cycles

FOUND SEVERE CORROSION AND CRACKING ON THE AFT SIDE OF FRAME 18, ON THE I/B FRAME FLANGE 8 INCHES ABOVE FLOOR LEVEL AND 4 INCHES TO 8 INCHES BELOW FLOOR LEVEL. MAINTENANCE C/W PARTIAL FRAME REPLACEMENT OF FRAME 18 LT IAW RIL HC537H9453 & BAE FAX REF BARA/AVR/5277/01.

Part: BRAKE — FAILED (MLG)

FLT 5545 - ORD-MLI - AFTER CHOCKS WERE PULLED. AIRCRAFT STARTED ROLLING FORWARD, BRAKING DID NOT STOP AIRCRAFT. AIRCRAFT HIT TERMINAL BLDG. AIRCRAFT REMOVED FROM SERVICE FOR REPAIR. (M)

Part: STRINGER — DENTED (FUSELAGE)

HAT STRINGER ON AFT WALL OF APU BOX IS DENTED. REPLACED HAT STRINGER ON AFT APU FIREWALL IAW BAE FAXES BARA/AVR/1885/98 AND DWC/RJ0002-98. (M)

Part: CABLES — CORRODED (ELEVATOR)

LEFT AND RIGHT MAIN ELEVATOR CONTROL CABLES ARE CORRODED AT VERTICAL STABILIZER REAR SPAR PULLEYS. REMOVED AND REPLACED ALL FOUR MAIN ELEVATOR CONTROL CABLES FROM REAR PRESS BULKHEAD TO CABLE COMPENSATORS, ADJUSTED IAW MM. W/C GENERATED FOR FUNCTION ALL TEST. (M)

Part: FLOORBEAM — CRACKED (FRAME 37)

FOUND CRACK IN FLOORBEAM AT FRAME NR 37 UNDER FLOOR PANEL 241DF IN CENTER ON FWD SIDE OF BEAM ABOUT 8 INCHES LONG AND 1 INCH FROM TOP OF BEAM. REMOVED CRACKED AREA OF FRAME 37 AND REPAIRED IAW BAE DRAWING NR HC538H9219 AND BAE FAX REF RJO778-98 DATED 11/2/98. (M)

Part: DIAPHRAGM — CRACKED (NLG WW)

NLG ACTUATOR AT UPPER ATTACHMENT POINT DIAPHRAGM IS CRACKED IN THE WEB AND BOSS. REPORTED TO BAE RDO. REF W/C 7025 FOR CORRECTIVE ACTION, DIAPHRAGM REPLACEMENT.

Part: DIAPHRAGM — CRACKED (NLG WW)

NOSE SIDEWALL DIAPHRAGM REMOVED FOR CRACKED ACTUATOR ATTACH POINT. REPLACED NLG LEFT DIAPHRAGM PER BAE FAX REF NR JEN/RJO0505-98. GEN W/C FOR 60 CYC DV INSPECTIONS AND 2000 AND OR 10 MONTH REPLACEMENT. (M)

Part: CONTROL CABLE — CORRODED (ELEVATOR TRIM)

ELEVATOR TRIM CABLE BETWEEN SCREWJACKS HAS SIGNS OF CORRISON AT CENTER PULLEY. ALSO, CENTER PULLEY BEARING WORN. REMOVED AND REPLACED CENTER PULLEY AND TRIM CABLE BETWEEN SCREWJACKS. ADJUSTED TENSION IAW MM 27-32-00. REF W/C 3055 FOR FUNCTIONAL TEST. (M)

Part: ENGINE — FAILED (NR 1)

NR 1 EGINE FAILE AND FIRE IN FLIGHT. REMOVED AND REPLACED NR 1 ENGINE ASSY IAW BAE 146 MM ANS AWAC GMM ENG CHANGE CHECKLIST VOLUME II SEC B CHAP 72, COMPLIED WITH ALL REQ'D ENGINE GROUND RUNS. ALL PARAMETERS FOUND SATISFACTORY. (M)

Part: ENGINE — FAILED (NR 1)

NR 1 ENGINE FAIL/SAFE AND FIRE INFLIGHT. REMOVED AND REPLACED NR 1 ENGINE ASSY IAW BAE 146 MM AND AWAC GMM ENGINE CHANGE CHECKLIST VOLUME II SEC B CHAP 72. COMPLIED WITH ALL REQUIRED ENGINE GROUND RUNS. ALL PARAMETERS FOUND SATISFACTORY. (M)

Part: POPPET VALVE — FAILED (NR 4 ENGINE)

NR 4 ENGINE READS 7 PERCENT BELOW N1 REF AT 904 DEGREES TGT, ABORTED TAKEOFF AT LESS THAN 60 KTS, RETURNED TO GATE AT DEN. REPLACED FCU POPPET VALVE ASY. ENGINE STILL LOW ON POWER. (M)

Part: GENERATOR — FAILED (APU)

DEN - FLT 587 - APU GENERATOR WENT OFF-LINE AND WOULD NOT RESET. FAILURE ACCOMPANIED BY ELECTRICAL SMELL WHEN APU AIR IS USED. INSPECTED APU, OIL LEVELS OK. INSPECTED MAG PLUG AND FILTERS, NO CONTAMINATION NOTED. STARTED APU, APU GEN OPS NORMALLY UNDER LOAD. NO ELECTRICAL SMELLS NOTED.

Part: SPOILER LIGHT — ILLUMINATED (LEFT)

DEN - FLT 655 - AFTER TAKEOFF GEAR RETRACTED, SPOILER LOCK-UP LIGHT ILLUMINATED ALONG WITH MAIN SPOILER FAULT LIGHT. RETURNED FOR LANDING. UPON GEAR DOWN, MAIN SPOILER FAULT LIGHT EXTINGUISHED, LEFT SPOILER GLARESHIELD LIGHTS ILLUMINATED. C/W FAULT ISO CHART 32-09-00, PAGE 138, FIG 110. NO FAULTS FOUND, C/W LIFT SPOILER SYSTEM ANNUNCIATOR CIRCUIT OPS CHECK IAW 27-61-00, PG 503, PARA 2C. CANNOT DUPLICATE, OPS CHECKS GOOD.

Part: SLIDE — DAMAGED (CABIN)

LEFT FORWARD EVACUATION SLIDE PACK-BOARD STRUCTURE WAS TORN AND SLIDE PARTIALLY PULLED FROM DOOR. REPLACED SLIDE.

Part: RELAY — FAILED (LANDING GEAR)

UNABLE TO RAISE GEAR UNLESS OVERRIDE IS SELECTED. GEAR SELECTED DOWN NORMAL EXTENSION. REMOVED AND REPLACED RELAY GF4 SYSTEM CHECKS GOOD. (M)

Part: ANGLE — CRACKED (CABIN)

MACHINED ANGLE ATTACHED TO SEAT RAIL 5 INCHES AFT OF FRAME 28 TO 6 INCHES AFT OF FRAME 29 LEFT OUTBOARD CRACKED. REPLACED ANGLE, REF FAX FOR HI-LOKS IN LIEU OF SP157 FAX NR DJR/RJ1282-96. (M)

Part: SKIN — CHAFED (LT TE FLAP)

REF FAX JM/RJ0927-6 DATED 8/14/96, LT FLAP TAB UPPER SKIN CHAFES AT RIBS 19 AND 21, FORWARD OF THE SPOILER RIB STRIP. REQUIRE REPAIR BY 34682 TCA. AWAC FAX LM185-96 REFERS. REPAIRED IAW AVRO REPAIR DRAWING HC579H9080, HC579H9074 AND FAX REP NR JM/RJ1109-96.

Part: SUPPORT — CRACKED (CABIN)

CABIN FLOOR SUPPORT AT FRAME 20A CRACKED AT CENTER GUSSET PLATE. REPAIRED FRAME 20A FLOOR SUPPORT IAW AVRO FAX REF NR DJR/R J1269-96.

Part: SEAT RAIL — CORRODED (CABIN)

FORWARD VESTIBULE FRAME 18 RIGHT INBOARD SEAT RAIL CORRODED IN SEVERAL SPOTS, REF SRM 53-00-32 PAGE 203 AND 51-31-11 PAGE 22. REPAIRED FORWARD VESTIBLE RT INBOARD SEAT RAIL BY SPLICING NEW RAIL IN PLACE PER SRM 53-00-32 PAGES 202, 203, 204. SPLICED PLACE WAS 20.75 INCH LONG AND SPLICED AT FORWARD END OF RAIL.

Part: FLOORBEAM — CRACKED (CABIN)

CRACK INDICATIONS FOUND ON THREE PRESSURE FLOORBEAMS OVER FRAME NR 32 LEFT SIDE. VERIFIED WITH ET INSPECTION. REPAIRED 3 CRACKS AT FRAME 32 IAW AVRO REPAIR DRAWING HC536H9211 AND FAX REF NR DJR/RJ1228-96 AND DJR/RJ1209-96.

Part: FLOORBEAM — CRACKED (FRAME 29)

ELEVEN CRACK INDICATIONS ON FORWARD END OF PRESSURE FLOORBEAMS AT FRAME 29. CRACKED BEAMS ARE NR 2, 3, 4, 5, 6, 7, 9, 13, 15, 19 AND 20 NUMBERED L TO RT. REPAIRED 11 CRACKS AT FRAME 29 IAW AVRO REPAIR DRAWING HC536H9211 AND FAX REP NR DJR/RJ1228-96 AND DJR/RJ1209-96.

Part: RIB — CHAFED (NR 1 FLAP TRACK)

RIB ABOVE LEFT NR 1 FLAP TRACK IS CHAFED WHERE IT CONTACTS ACCESS PANEL 285FT. BLENDED AND REPROTECTED THE CHAFE MARK ON THE SIDE OF RIB 2 TRAILING EDGE EXTENSION PER FAX DJR/RJ1243-96 DATED OCT 31, 1996 AND SRM 51-20-11. GENERATED W/C TO C/W A DV INSPECTION IN 4000 FLTS.

Part: FLAP TRACK — WORN (LT TE FLAP)

NR 1 FLAP TRACK LEFT SIDE HAS .020 INCH WEAR ON SIDE OF LOWER AND UPPER RAILS, FROM SLIPPER PLATES. BLENDED THE OUTBOARD SIDE OF THE LEFT NR 1 FLAP TRACK UPPER AND LOWER RAILS PER FAX DJR/RJ1243-96, DATED OCT 31, 1996.

Part: BOLTS — TOO LONG (WING/FUSELAGE)

FUSELAGE BOLT LOOSE AT RIGHT WING FORWARD SPAR. CHECK TORQUE ON THREE OTHER IN THAT SAME ROW. REPLACED 2 BOLTS FOUND TO BE TOO LONG. CHECK TORQUE ON REMAINING 3, CHECK OK. WITCOBOND 2 REPLACEMENT BOLTS, HOLES WITHIN LIMITS. AFT OF FR 26 WING TO FUSELAGE CLOSING ANGLE. (

Part: CABLES — CORRODED (LT/RT AILERONS)

LEFT AND RIGHT AILERON INTERCONNECT CABLES COVER SLEEVES ARE WORN IN TWO AT CABLE GUIDES. REMOVED AND REPLACED LEFT AND RIGHT AILERON INTERCONNECT CABLES IAW AMM W/C GENERATED FOR FUNCTIONAL CHECKS. REF W/C 2365. (M)

Part: ANGLES — BROKEN (FUSELAGE)

AFT CARGO BAY AT FRAME NR 35, RT BELLY TIE DOWN AREA, SURROUND PLATE BENT AND ANGLES TO FRAME BROKEN. ALSO, MISSING RIVETS IN FRAME. STRAIGHTEN PLATE AND REPLACED ANGLE AND REPLACED RIVETS.

Part: CABLES — CORRODED (AILERONS)

PERFORMED AILERON INTERCONNECT CABLE CHECK. FOUND AILERON INTERCONNECT CABLES CORRODED AT WING ROOT PULLEYS. REMOVED AND REPLACED IAW AMM GENERATED W/C FOR FUNCTIONAL CHECK.

Part: FLAP TRACKS — WORN (LT TE FLAPS)

LEFT WING NR 2 FLAPTRACK WEARMARKS LOWER RAIL OUTBOARD EDGE FRM SLIP P/PLATE. WEARMARKS 94) BOTH SIDES TOP OF LOWER RAIL FROM ROLLERS AND 1, UPPER RAIL OUTBOARD EDGE FROM SIDE ROLL. COMPLIED WITH BLENDING OF WEARMARKS ON UPPER OUTBOARD RAIL AND BOTH SIDES ON TOP OF LOWER RAIL IAW SRM 57-20-41. BLENDED LOWER RAIL EDGES AND SHIMMED THE RUB PADS OF THE LOWER CARRIAGE PER FAX DJR/1200-96.

Part: BLKHD STIFFENERS — CRACKED (FUSELAGE)

PERFORMED ET AT FRAME 29 BULKHEAD TO C/W EO E95/003/653 ITEM NR 3. FOUND CRACKS AT STIFFENER STATION 36.62, 31.13, 25.94 LEFT AND 36.62, 31.13, 25.94 RT. REPAIR STIFFENERS IAW EO E95/005/654. END OF CRACKS MARKED WITH GREASE PENCIL. REPAIRED FRAME 29 STIFFENERS AT LT AND RT STATIONS 25.94, 31.13, 36.62 IAW EO E95/005/653 ORIG ISSUE AND AVRO FAXES DJR/RJ1199-96 AND DJ/RJ059.

Part: RAIL — CORRODED (AIRSTAIR)

FORWARD VESTIBULE INBOARD AIRSTAIR RAIL NEEDS TO BE REPLACED DUE TO CORROSION. RAIL IS REMOVED. REPLACED FORWARD INBOARD AIRSTAIR RAIL.

Part: SUPPORT — CORRODED (FUSELAGE)

FRAME 20 LEFT SIDE FLOOR SUPPORT BEAM HAS CORROSION WHERE BOTH FORWARD AIRSTAIR RAILS ATTACH. NEEDS TO BE CLEANED AND MEASURED FOR DEPTH. REPAIR OR REPAINT AS NECESSARY (ONLY ONE SIGNIFICANT SPOT W/A DEPTH MAX AT .029 INCH). REPAIRED IAW FAX DJR/RJ1197-96.

Part: BOLTS — FAILED (LT SPOILER)

LEFT WING INBOARD LIFT SPOILER JACK BOLTS, FORWARD AND AFT, FAILED NDT. INSTALLED NEW FORWARD AND AFT JACK BOLTS ON LEFT INBOARD LIFT SPOILER.

Part: BLKHD DOUBLER — CRACKED (BS 47.2)

IN HYD BAY AT FRAME 29 BULKHEAD, THE TWO MOST OUTBOARD STIFFENERS LEFT AND RIGHT WERE FOUND TO HAVE CRACKED DOUBLERS AT BOTTOM BOLT HOLE. THESE STIFFENERS ARE NOT COVERED IN EO E95/003/653, STATION 47.20 LT/RT, END OF CRACKS MARKED WITH GREASE PENCIL. REPLACED LT AND RT FRAME 29 DOUBLERS AT STIFFENER STATION 47.20 IAW BAE STRUCTURAL REPAIR MANUAL AND AVRO FAX NR DJR/RJ1201-96.

Part: HI-LOK — SHEARED (FUSELAGE)

SIGHTING ATTACHMENT ON (BELLY) LONGERON FITTING OF FRAME NR 29 HAS HI-LOK SHEARED. REPLACED BROKEN HI-LOK IAW BAE 146MM (SAME PART AS ORIGINAL). (M)

Part: RAIL — CORRODED (REAR AIRSTAIR)

REAR AIRSTAIR, INBOARD RAIL CORRODED NEEDS TO BE REPLACED. REMOVED AND REPLACED AFT INBOARD AIRSTAIR RAIL. (M)

Part: ANGLE — CRACKED (PAX DOOR)

FORWARD PASSENGER DOOR HAS TWO CRACKED ANGLE BRACKETS AT THE BOTTOM OF BOX STRUCTURE FOR DOOR MECHANISM. REPLACED CRACKED AREAS PER SRM. ANGLES MADE PER SRM. REMOVED STRUCTURE INSPECTED AND NO OTHER DAMAGE NOTED.

Part: CABLES — RUSTED (RIGHT AILERON)

RIGHT AILERON CONTROL CABLES ARE RUSTED AT WING ROOT CABLE PULLEYS. INSTALLED RIGHT AILERON CONTROL CABLES IAW AMM W/C GENERATED FOR REQUIRED CHECKS AND SAFTIES.

Part: BOLT — FAILED (CTR SPOILER)

FORWARD BOLT OF JACK ON MIDDLE LIFT SPOILER FAIL NDT LEFT WING. REMOVED AND REPLACED FORWARD BOLT OF JACK ON MIDDLE LIFT SPOILER LEFT WING. (M)

Part: BOLTS — CRACKED (RT SPOILER)

RIGHT WING OUTBOARD LIFT SPOILER INBOARD HINGE BOLT SHOWS CRACK INDICATION. RIGHT WING, REMOVED AND REPLACED BOLT TO LIFT SPOILER INBOARD HINGE OF OUTBOARD SPOILER.

Part: STEP — CORRODED (FWD AIRSTAIR)

FORWARD AIR STAIR ASSEMBLY NR 2 STEP CORRODED. REPLACED STEP ASSEMBLY.

Part: BOLT — BAD (COCKPIT)

RIGHT FORWARD RESTRAINT LINK BOLT FOUND TO BE BAD ON MAG PART INSPECTION. DRILLED NEW BOLT FOR COTTER PIN AND INSTALLED IN RIGHT FORWARD RESTRAINT LINK. (M)

Part: BOLT — CORRODED (RT SPOILER)

RIGHT WING OUTBOARD LIFT SPOILER MIDDLE HINGE BOLT HAS CORROSION AND CRACK INDICATION. REMOVED AND REPLACED BOLT, RIGHT WING OUTBOARD LIFT SPOILER MIDDLE HINGE. (M)

Part: BOLT — DAMAGED (NR 2 TE FLAP)

RIGHT NR 2 FLAP TRACK FLAP TO CARRIAGE, BOLT APPEARS TO HAVE RECEIVED A LIGHTENING STRIKE,DUE TO PITS NEAR THREADED AREA. INSTALLED NEW BOLT IN NR 2, RIGHT FLAP TO CARRIAGE HOUSING. (M)

Part: FRAME — CORRODED (E/E COMPT)

LIGHT SURFACE CORROSION ON FRAME 15 FLOOR SUPPORT BEAM BY LEFT AFT CORNER OF AVIONICS BAY ACCESS OPENING. REMOVED MINOR SURFACE CORROSION, CLEANED, TREATED AND REPAINTED. (M)

Part: BOLT — CRACKED (NR 4 ENGINE)

NR 4 ENGINE YOKE TO PYLON, DURING UT INSPECTION OF TOP LEFT BOLT P/N HC712H0041-000 CRACK INDICATION. REMOVED BOLT FOR MT, VERIFICATION REQUIRED. REMOVED BOLT, BOLT FAILED MAGNETIC PARTICLE INSPECTION. REPLACED AND INSTALLED IAW BAE 146 MM.

Part: BOLT — FAILED (NR 1 ENGINE)

NR 1 ENGINE YOKE TO PYLON. DURING INSPECTION OF BOLTS FOUND CRACK INDICATIONS ON BOTTOM RT IN THREAD RUNOUT AREA. REMOVED BOTTOM RT BOLT FOR MAGNETIC PARTICLE VERIFICATION SSI 54-00-123. REMOVED ABOVE BOLT, BOLT FAILED MAGNECTIC PARTICLE INSPECTION REPLACED AND INSTALLED IAW BAE 146 MM.

Part: RIVETS — CORRODED (DOOR SILL)

RIGHT FORWARD SILL PLATE AFT INBOARD ATTACHMENT HOLES HAVE CORRODED RIVETS THAT NEED TO BE REPLACED. REPLACED RIVETS. (M)

Part: BOLT — OUT OF POSITION (NR 3 TE FLAP)

LEFT WING NR 3 FLAP TRACK CARRIAGE TO FLAP BOLT, MAGNEFLUXED OK, BUT INNER BOLT HAS SLID OUT OF POSITION AND FIRST THREADS NEED DRESSED-OUT. RESEALED AND RESE CURED INNER FAIL/SAFE BOLT. DRESSED-OUT OUT THREADS AS REQUIRED.

Part: BULKHEAD RIVETS — MIS INSTALLED (REAR PRESS DOME)

FORWARD SIDE OF REAR PRESSURE DOME , 2 RIVETS NEED SHIMS AT HORIZONTAL STIFFENERS TO CENTER RING AS MARKED. DRILLED OUT 2 RIVETS MADE SHIM FROM SHEET METAL, INSTALLED SHIM AND 2 RIVETS. (M)

Part: SILL — CORRODED (PAX DOOR)

LEFT REAR PASS DOOR SILL PLATE CORRODED THROUGH. REMOVED OLD SILL PLATE AND INSTALLED NEW SILL PLATE FROM STOCK, FORWARD HALF ONLY. REINSTALLED FORWARD GIRT BAR BRACKET. (M)

Part: BRACKETS — CRACKED (FUSELAGE)

LOW FREQUENCY RUMBLE ON A/C AIR FRAME BETWEEN 270-285 KTS. CAN BE BOTH FELT AND HEARD. FLIGHT CONTROLS NORMAL. CORRECTIVE ACTION: FOUND FIVE CRACKED BRACKETS ON PANEL 281CT, REM AND REP ALL 5 BRACKETS.

Part: COMPRESSOR — STALLED (NR 2 ENGINE)

ASE - FLT 650 - WHILE APPLYING TAKEOFF POWER, NR 2 ENGINE POPPED AND SHUT DOWN. DEN MX LOCKED DOWN ENGINE AND WILL 3-ENGINE FERRY TO ATW. REMOVED AND REPLACED ENGINE.

Part: MOUNTING PAD — SEPARATED (NR 4 GEARBOX)

MKE - FLT 548 - NR 4 ENGINE OIL LEAK. FOUND STARTER MOUNTING PAD SEPARATING FROM ACCESSORY GEARBOX. THREE-ENGINE FERRY TO ATW FOR GEARBOX CHANGE. REMOVED AND REPLACED STARTER MOTOR.

Part: CONTACTS — DIRTY (CABIN)

EMERGENCY LIGHT ABOVE FWD PAX DOOR INOP, ON TEST. CLEANED CONTACTS ON LIGHT ASSY.

Part: ENGINE — FAILED (NR 2)

DEN - FLT 604 - NR 2 ENGINE FAILED IN-FLIGHT, NR 1 BOTTLE BLOWN. ENGINE CHECK LIST C/W. REMOVED AND REPLACED NR 2 ENGINE IAW MM, PAGE 28412/3 FOR REMOVAL AND REPLACMEENT OF BOTTLE. S/N OFF, LF-05220. S/N ON LF-05076.

Part: SLIDE — FAILED CHECK (NR 3)

THE NR 3 EMERGENCY SLIDE FAILED THE POWER PACK EFFICIENCY CHECK. REPLACED THE SLIDE.

Part: BOLT — LOOSE (RT SPOILER)

ATW - FLT 309 - DURING EN ROUTE CLIMB WITH TMS TGT SYNC SELECTED, THE CPT AND FO FELT A PRONOUNCED AIRFRAME VIBRATION ON COCKPIT FLOOR AND COCKPIT SEATS. NO VIBRATION WAS FELT IN CONTROL YOKE. REMOVED AND REPLACED LOCKING PLATE ON RT WING MIDDLE SPOILER HINGE BOLT. (LOOSE BOLT CAUSED PLAY IN SPOILER HINGE.) OPS CHECK SATISFACTORY.

Part: POSITION TRANS — FAILED (AIR BRAKES)

UNCOMMANDED AIRBRAKE OPERATION. CREW COMPLIED WITH 'M' MEL PULLED AND COLLORED CIRCUIT BREAKER. REMOVED AND REPLACED AIRBRAKE FEEDBACK POSITION POTENTIOMETER IAW AC MM. OP CHECK SATISFACTORY. MEL 27-60-1 REM.

Part: VALVE — FAILED (AIR BRAKES)

UNCOMMANDED OPENING OF THE AIRBRAKE ON APPROACH INTO ORD. COMPLIED WITH M ACTION OF THE MEL. REMOVED AND REPLACED AIR BRAKE VALVE IAW MM. OPS CHECK OK. REMOVED FROM MEL.

Part: AIRSPEED IND — MALFUNCTIONED (LEFT)

ATW - FLT 300 - CAPTAIN'S AIRSPEED INDICATOR READ ZERO ON TAKEOFF ROLL AT 80 KNOT SPEED CHECK, FIRST OFFICER'S WAS OK. ABORTED TAKEOFF AND RETURNED TO THE GATE. ATW MAINTENANCE PUMPED UP PITOT SYSTEM AND AIRSPEED READ NORMAL, MAINTENANCE CTL DECIDED TO REPLACE INDICATOR AS A PRECAUTION. ABORTED SECOND TAKEOFF WITH SAME PROBLEM, SWAPPED AIRCRAFT.

Part: PBE MASK — MALFUNCTION (FWD CABIN)

FORWARD CABIN PBE MASK RED IND SHOWING. REMOVED AND REPLACED PBE ASSY. (W)