N448AW

Part: WINDSHIELD — CRACKED (COCKPIT RT) · airframe 37,715 hrs · 36,422 cycles

FIRST OFFICER'S WINDSHIELD CRACKED AT APPROXIMATELY 7,500 FEET. PRIOR TO CRACKING WE GOT A RIGHT WINDSHIELD HEAT CAUTION. AIRCRAFT REMOVED FROM SERVICE. R & R RT WINDSHIELD, IAW AMM 56-11-01. OPS CHECK GOOD. S/N OFF: 14139H5917 S/N ON: 19284H9352.

Part: UNKNOWN — MALFUNCTIONED (AC BAY) · airframe 37,282 hrs · 36,009 cycles

AFTER TAKEOFF WHEN SWITCHING RH PACK TO 10TH STAGE AIR RECEIVED A RH PACK HIGH PRESSURE CAUTION, WITH THE LEFT PACK ALREADY ON MEL. CREW COMPLETED QRH AND PERFORMED AN AIR RETURN TO IAD. AIRCRAFT REMOVED FROM SERVICE PERFORMED OPS CHECK OF RH PACK WITH APU BLEADS AND ENGINE BLEEDS SWITCHING BACK AND FORTH PER AMM 21-51-00 AND 71-00-00 OPS CHECKED GOOD NO DEFECTS NOTED FER NARRATIVE FROM FLIGHT CREW. PRIOR TO THE FLIGHT WE DISCUSSED THE MEL FOR THE LEFT PACK INOP AND REVIEWED THE PROCEDURE IN APPENDIX (B) FOR TRANSFERRING THE RIGHT PACK TO THE RIGHT ENGINE 10TH STAGE BLEED AFTER TAKEOFF. I ALSO EXPLAINED TO MY FO WHEN AND HOW WE WOULD ACCOMPLISH THIS PROCEDURE IN ORDER TO AVOID A PACK OVER PRESSURE SITUATION. DESPITE THIS MY FO TRANSFERRED THE BLEEDS AFTER TAKE OFF BEFORE I HAD AN OPPORTUNITY TO TO REDUCE THE N1 TO 60%. THIS IMMEDIATELY CAUSED A PACK HI PRESSURE AND AUTOMATIC SHUT DOWN OF THE RIGHT PACK. WE SUBSEQUENTLY RAN THE THE QRH BUT WERE UNABLE TO RESTORE THE OPERATION OF THE RIGHT PACK. CONSEQUENTLY WE HAD TO RUN ADDITIONAL QRH. PROCEDURES AND CONDUCT AN AIR RETURN AND UNPRESSURIZED LANDING. THIS WAS MY FOÏ¿½S FIRST TIME OPERATING WITH A SINGLE PACK AND PERFORMING THE PROCEDURE IN APPENDIX (B). I THINK HE SIMPLY FORGOT THAT WE WERE SINGLE PACK AND TRANSFERRED THE BLEEDS OUT OF HABIT.

Part: WARNING MESSAGE — FALSE ACTIVATION (MLG) · airframe 35,553 hrs · 34,381 cycles

AFTER TAKEOFF RECEIVED GEAR DISAGREE WARNING, NLG INDICATED RED. HYD P UMP 3A ON MEL. DISAGREE NEVER CLEARED. CW QRH. INDICATED GREEN. UNEVEN TFUL LANDING. DISAGREE AT APROX 28 SECONDS AFTER GEAR SELECTION. DID N OT MOVE GEAR HANDLE WITHIN 30 SECONDS. MANUAL RELEASE WAS USED. AIRCRAFT WAS EXPERIENCING TURBULENCE. HYD SYSTEM PRESSURE WAS NORMAL. #3B AN D 2B PUMPS WERE IN AUTO. NO EMERGENCY DECLARED. NO ASSOCIATED EICAS MS GS.

Part: TRIM SYSTEM — FROZEN (RUDDER) · airframe 35,527 hrs · 34,351 cycles

ON FINAL APPROACH REC'D UNCOMMANDED YAW, CONTINUED TO LANDING WHEN IN FLARE TRIED TO APPLY RT RUDDER, RT RUDDER WAS FROZEN. A/P WAS DISENGAGED. RUDDER TRIM OPERATES NORMALLY, NO ASSOCIATED MSG'S RUDDER POSITION INDICATION FLUXES LT/RT OF CENTER.

Part: BPCU — MALFUNCTIONED (TE FLAPS) · airframe 34,899 hrs · 33,752 cycles

RECEIVED FLAPS FAIL CAUTION MESSAGE DURING CLIMB THROUGH FL 210. FLAPS HAD BEEN SET TO ZERO SINCE LEAVING PATTERN ALTITUDE. NO OTHER ISSUES. DIVERTED BACK TO ORD. SUSPECT RH BPSU

Part: BPSU — MALFUNCTIONED (TE FLAPS) · airframe 34,899 hrs · 33,752 cycles

RECIEVED FLAPS FAIL CAUTION MESSAGE IMMEDIATELY FOLLOWING INITIAL DESCENT FROM FL 300. RAN QRH. LANDED FLAPS ZERO DEGREES. NO OTHER ISSUES NOTED. LANDING WAS UNEVENTFUL. PERFORMED FLAP RESET PROCEDURE IAW AWA SUPP. 98-018G BOX 12. FLAPS RESET. PLACARDED AND PLACED ON MEL. COMPLETED INSTALLATION OF RH BPSU IAW AMM 27-51-10-420-013, PERFORMED RIGGING OF RH BPSU IAW AMM 27-51-10, OPS CHECK GOOD, NO MESSAGES PRESENT AT THIS TIME

Part: PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,836 hrs · 33,686 cycles

SERVICE DOOR THRESHOLD COVER PLATE CORRODED, R&R.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 34,836 hrs · 33,686 cycles

LT FLOOR SEAT TRACK CORRODED BETWEEN FS 409+128 AND FS 559.00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 34,836 hrs · 33,686 cycles

L/H WALL SEAT TRACK CORRODED AT FS 409+128

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 34,836 hrs · 33,686 cycles

RT FLOOR SEAT TRACK CORRODED BETWEEN FS 349 AND FS 379.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,836 hrs · 33,686 cycles

LT FLOOR SEAT TRACK CORRODED BETWEEN FS 349 AND FS 379, R&R.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 34,836 hrs · 33,686 cycles

LT FLOOR SEAT TRACK CORRODED BETWEEN FS 379 AND 409+128.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 34,836 hrs · 33,686 cycles

LT WALL SEAT TRACK CORRODED BETWEEN FS 409+16 AND FS 409+112.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 34,836 hrs · 33,686 cycles

LT WALL SEAT TRACK CORRODED BETWEEN FS 449.85 AND FS 499.00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 34,836 hrs · 33,686 cycles

RT WALL SEAT TRACK CORRODED BETWEEN FS 449.85 AND FS 499.00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 34,836 hrs · 33,686 cycles

RT FLOOR TRACK CORRODED BETWEEN FS 379.00 AND FS 409+128. R&R.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 34,836 hrs · 33,686 cycles

RT WALL SEAT TRACK CORRODED BETWEEN FS 409+16 AND FS 409+112.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,836 hrs · 33,686 cycles

RT WALL SEAT TRACK CORRODED BETWEEN FS 544 AND FS 559+16.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 34,836 hrs · 33,686 cycles

LT WALL SEAT TRACK CORRODED BETWEEN FS 544.00 AND FS 559+80.

Part: FIRE BOTTLE — LOW (CARGO BAY) · airframe 34,466 hrs · 33,319 cycles

CARGO BOTTLE LOW CAUTION MSG. CW QRH. DIVERTED TO DAY REMOVED AND REPLACED LT CARGO FIRE BOTTLE IAW AMM SUP 10-099A. OPS CHECKED GOOD.

Part: FIRE BOTTLE — LOW (CARGO BAY) · airframe 34,466 hrs · 33,319 cycles

CARGO BOTTLE LOW CAUTION MSG. CW QRH. DIVERTED TO DAY REMOVED AND REPLACED LT CARGO FIRE BOTTLE IAW AMM SUP 10-099A OPS CHECKED GOOD.

Part: WIRE HARNESS — DAMAGED (NLG SENSOR) · airframe 33,542 hrs · 32,344 cycles

DURING CLIMB OUT, RECEIVED A GEAR DISAGREE THROUGH 17000 FT. NLG SHOWED YELLOW HASH. COMPLIED WITH QRH. MESSAGE CLEARED ON ITS OWN. DIVERTED. ON APPROACH SELECTED GEAR DOWN, HEARD CLICKING NOISE FROM THE NOSE GEAR. GEAR INDICATED DOWN AND LOCKED. R & R THE NR 2 NLG DOWN LOCK HARNESS IAW AMM 32-61-25. PERFORMED A GEAR SWING OF THE NLG. ALL GEAR INDICATIONS GOOD. PERFORMED AN OPS CHECK OF THE PROXIMITY SENSOR SYSTEM IAW AMM 32-61-00. OPS CHECKED GOOD.

Part: SENSOR — OUT OF LIMITS (MLG) · airframe 33,426 hrs · 32,237 cycles

GEAR DISAGREE DURING CLIMB. COMPLIED WITH THE QRH. MESSAGE CLEARED AND REAPPEARED MULTIPLE TIMES. THEN CLEARED COMPLETELY. NLG SHOWED AMBER. DURING DESCENT GEAR EXTENDED NORMALLY. LANDED AT NEAREST SUITABLE AIRPORT IAW QRH. FOUND NLG DOWNLOCK SENSOR OUT OF LIMITS. ADJUSTED THE DOWNLOCK SENSOR IAW AMM 32-61. GEAR RETRACTION TESTED GOOD.

Part: LIGHT — INOPERATIVE (ROW 8) · airframe 32,278 hrs · 31,172 cycles

EMERGENCY FLOOR LIGHT INOPERATIVE BEHIND ROW 8

Part: CIRCUIT BREAKER — TRIPPED (AC BUSS) · airframe 31,835 hrs · 30,777 cycles

FLT 3978. IN FLIGHT AC ESSENTIAL FEED CIRCUIT BREAKER TRIPPED. CIRCUIT BREAKER PANEL 1 C2 ASSOCIATED AC ESS SWITCH ILLUMINATED COMPLIED WITH QRH. GEN 1 WILL NOT RESET. RESET CIRCUIT BREAKER ON PANEL 1 C2 PERFORMED OPS CHECK OF AC BUSS 1 SYSTEM OPS CHECK GOOD IAW AMM 24-20-00

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,687 hrs · 30,641 cycles

AFT SECTION FLOOR EMERGENCY LIGHTS INOP. ROWS 9 -12.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,658 hrs · 30,613 cycles

EMERGENCY LIGHT DO NOT WORK STARTING AT ROW 8 TO BACK OF PLANE. R&R EMERGENCY FLOOR TRACK LIGHTS AT ROW 12 IAW AMM 33-51-01. OPS CHECK GOOD.

Part: BALLAST — INOPERATIVE (CABIN) · airframe 31,445 hrs · 30,423 cycles

FLIGHT 4041.ODOR IN CABIN SIMILAR TO ELECTRICAL OVERHEAT. STRONGEST MID CABIN. LT SIDE ROW 9 SIDE WALL LIGHT INOPERATIVE. INSPECTED AND FOUND LIGHT BALLAST INOPERATIVE AT SEAT 1CA. REMOVED AND REPLACED BALLAST AND SIDEWALL LIGHT BULB OPS CHECK OK. NO ODOR IN CABIN

Part: SHROUD — CRACKED (RT WING) · airframe 31,201 hrs · 30,198 cycles

RIGHT OTBD L/E SHROUD IS DENTED AND CRACKED AT WS 342-350.

Part: DOUBLER — CHAFED (FUSELAGE) · airframe 31,201 hrs · 30,198 cycles

NLG DOOR CUTOUT, RT DOUBLER AT FS 206 IS CHAFED.

Part: SKIN — CHAFED (RT AILERON) · airframe 31,201 hrs · 30,198 cycles

RIGHT AILERON UPPER L/E SKIN CHAFED AT AREAS ALONG ENTIRE LENGTH, REPLACED.

Part: SKIN — CHAFED (TE FLAP VANE) · airframe 31,201 hrs · 30,198 cycles

RIGHT INBD FLAP VANE L/E IS CHAFED OTBD OF ACCESS PANEL 684ET.

Part: RIB — BENT (TE FLAP) · airframe 31,201 hrs · 30,198 cycles

RIGHT INBD FLAP RIB AT WS 106.352 BENT, REPLACED.

Part: SKIN — CHAFED (TE FLAP VANE) · airframe 31,201 hrs · 30,198 cycles

RIGHT INBD FLAP VANE L/E IS CHAFED JUST INBD OF ACCESS PANEL 684DT.

Part: WEB — CRACKED (FUSELAGE) · airframe 31,201 hrs · 30,198 cycles

WEB BELOW PILOTS WINDSHIELD SIDE POST SUPPORT IS CRACKED.

Part: FITTING — CRACKED (COCKPIT) · airframe 31,201 hrs · 30,198 cycles

LEFT PILOT SIDE LOWER WINDSHIELD CLIP, 202.00 CENTER POST IS CRACKED. REPLACED CLIP AT 202.00, CENTER POST, PILOTS SIDE LOWER WINDSHIELD IAW SRM 51-42-21, 51-40-11.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 31,201 hrs · 30,198 cycles

FS 280 FLOOR ANGLE CRACKED AT MLG ALT EXTENSION CABLE PULLEY LOCATION.

Part: SKIN — GOUGED (TE FLAP) · airframe 31,201 hrs · 30,198 cycles

RT INBD FLAP HAS DEEP GOUGE ON LOWER SKIN AT INBD AFT CORNER. REPAIRED RT INBD FLAP LOWER INBD SKIN IAW SRM 57-20-00, REPAIR NR 3.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,201 hrs · 30,198 cycles

FLOOR LANDING ANGLE BETWEEN LBL27 AND THE LT FLOOR SILL HAS CORROSION AND BARE METAL AT FS 621.00 IN THE CARGO BAY. REPLACED FLOOR ANGLE AT FS 621.00, LBL27 TO LT FLOOR SILL IAW SRM 51-40-11, 51-42-06, 51-42-20.

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 31,201 hrs · 30,198 cycles

FS 621 BULKHEAD WEB FWD FACE HAS 1 EA BARE BLENDED AREA AT SCREW HOLE, LOCATED AT APPROXIMATELY WL 103, LBL 45, NEAR LINTEL REPAIR AREA, REPAIRED.

Part: ANGLE — CRACKED (FUSELAGE) · corrosion level 2 · airframe 31,201 hrs · 30,198 cycles

FLIGHT DECK FLOOR LANDING ANGLE ON THE FWD SIDE OF BEAM 280.00 IS CRACKED AND CORRODED ON THE BOTTOM SIDE BETWEEN LBL9 AND RBL9 IN THE VERY FWD ELECTRONIC EQUIPMENT BAY. REPLACED FLIGHT DECK FLOOR LANDING FORWARD ANGLE AT FS 280.00 BETWEEN LBL9 AND RBL9 IAW SRM 51-40-11, 51-42-06, 51-42-21.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,201 hrs · 30,198 cycles

STRINGER 26L IS CORRODED UNDER THE FOOTPRINT OF THE NLG SPADE DOOR HINGE FITTING FOOTPRINT.

Part: SKIN — CRACKED (FUSELAGE) · airframe 31,201 hrs · 30,198 cycles

FWD LOWER FUSELAGE SKIN IS CRACKED AT THE NLG WHEEL WELL CUTOUT RT AFT CORNER. REPAIRED FUSELAGE SKIN AT THE NLG DOOR CUTOUT RT AFT CORNER IAW REO 601R-53-11-048, REV-D, 601R-53-11-2940, REV.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,201 hrs · 30,198 cycles

FRAME 409+16 HAS CORROSION ON BOTH THE FWD AND AFT SIDES BETWEEN STR 26L AND 26R IN THE FWD ELECTRONIC EQUIPMENT BAY. REPAIRED FRAME 409+16 IAW SRM 53-00-15.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,201 hrs · 30,198 cycles

RIGHT AISLE SEAT TRACK STICK 3 HAS CORROSION BETWEEN FS 409+128 TO FS 559 IN CABIN.

Part: FITTING — CRACKED (FUSELAGE) · airframe 31,201 hrs · 30,198 cycles

RIGHT SIDE LOWER WINDSHIELD CENTER POST CLIP CRACKED.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,201 hrs · 34,023 cycles

FLOOR LANDING ANGLE AT FS 621.00 HAS CORROSION AND BARE METAL BETWEEN RBL 27 AND RT SILL IN THE CARGO BAY. REPLACED DAMAGED SECTION OF FLOOR LANDING AT FS 621.00, BETWEEN RBL 27 AND RT SILL IAW REO601R-53-61-117, REV-C.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,763 hrs · 29,795 cycles

EMERGENCY FLOOR LIGHTING AT ROWS 6 - 8 INOPERATIVE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,763 hrs · 29,795 cycles

EMERGENCY FLOOR LIGHTING ROW 1 INOPERATIVE.

Part: SIGN — UNSECURE (CABIN) · airframe 29,397 hrs · 28,494 cycles

EXIT SIGN ON BULKHEAD AT SEAT 1A-C FELL OFF.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,177 hrs · 28,278 cycles

EMERGENCY FLOOR TRACK LIGHTS, ROWS 6 - 8 ARE INOPERATIVE. PLACARDED & PLACED ON MEL. MC-REF 254233 3.

Part: UNKNOWN — MALFUNCTIONED (AUTOPILOT SYS) · airframe 34,120 hrs · 31,988 cycles

RECEIVED FLAPS DEGRADED MSG IN CRUISE. PITCH OSCILLATION IN CRUISE WITH AUTO PILOT ON, PITCH OSCILLATION STOPPED WITH AUTO PILOT OFF. DURING PITCH OSCILLATION THE FLAPS INDICATED UNCOMMANDED MOVEMENT FROM 0-8 DEGREES, THEN BACK, THEN 0-2 DEGREES, THIS STOPPED WHEN AUTO PILOT WAS SELECTED OFF. VERIFIED ON FLIGHT CONTROL SYNOPTIC PAGE.

Part: CAP — MISSING (CABIN) · airframe 28,952 hrs · 28,051 cycles

FLIGHT 3885, 3826 FLOOR TRACK LIGHTS FWD END CAP MISSING & 1ST COVER STRIP IS NOT SECURE. R & R EMER FLOOR TRACK LIGHTS COVER & END CAP IAW AMM 33-51-01 AT ROW 1D. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,870 hrs · 27,967 cycles

EMERGENCY LIGHTS NEXT TO ROW 6 - 7 & EXIT SIGN ON RT EMER EXIT WILL NOT ILLUMINATE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,460 hrs · 27,571 cycles

FLIGHT 3970, EMER FLOOR LIGHTS ROW 5 - 7, DO NOT ILLUMINATE. COULD NOT DUPLICATE, AS PRECAUTIONARY R & R INVERTER PS3LY. OPERATIONS CHECKED.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 28,323 hrs · 27,439 cycles

REAR MOST CEILING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE BULB.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,836 hrs · 26,967 cycles

FLOOR TRACK EMER LIGHTS AT ROW 6 - 7 & IDENTIFIER BELOW RT OVERWING EXIT INOPERATIVE.

Part: LIGHT — BROKEN (CABIN) · airframe 27,107 hrs · 26,280 cycles

EMERGENCY LIGHTS AT ROW 1 OVERLAY IS BROKEN.

Part: LIGHT — INOPERATIVE (ROW 6-8) · airframe 27,185 hrs · 26,352 cycles

EMERGENCY LIGHT INOPERATIVE RT ROW 6 - 8 & SIGN AT EXIT ROW 8 INOPERATIVE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,827 hrs · 26,023 cycles

EMERGENCY FLOOR LIGHTS AT ROW 6 AND SIDEWALL EMERGENCY LIGHT AT ROW 8 ARE OUT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,827 hrs · 26,023 cycles

EMER FLOOR LIGHTS AT ROW 6 SIDEWALL EMER LIGHT AT ROW 8 OUT. ROWS 6 - 8 LIGHTS WERE OUT.

Part: HEAT EXCHANGER — DAMAGED (AC BAY) · airframe 26,507 hrs · 25,737 cycles

WHILE LEVEL FL240, CABIN ALTITUDE BEGAN TO CLIMB, UNABLE TO MAINTAIN PRESSURIZATION. RT PACK & RT 10TH STAGE PRESS APPEARED NORMAL, NO AIRFLOW FROM VENTS. DECLARED AN EMER, PERFORMED QRH, LEVELED AT 10,000 FT UNPRESSURIZED. INSP ALL DUCTING & PRESS LINES IN AFT EQUIP BAY. FOUND RT DUAL HEAT EXCHANGER DUCT BLOWN OFF & FLANGE DAMAGED. REMOVED DAMAGED HEAT EXCHANGER IAW AMM 21-51-07. REPLACED RT HEAT EXCHANGER & DUCT IAW AMM 21-51-07, WORK ORDER WC 22. OPERATIONS CHECK & LEAK CHECK. SN OFF 200304092 & SN ON 200209170.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 26,470 hrs · 25,702 cycles

PAX DOOR AFT DRAG ANGLE CRACKED JUST ABOVE PULLEY.

Part: STIFFENER — CRACKED (RT WING) · airframe 26,470 hrs · 25,702 cycles

STIFFENER IN RT WW AT APPROX WS 47 IS CRACKED IN 2 PLACES.

Part: SKIN — DAMAGED (LT AILERON) · airframe 26,470 hrs · 25,702 cycles

COMPLIED WITH AWAC CARD 4DMI17327 REPAIR LT OTBD FLAP LOWER SKIN.

Part: ANGLE — CRACKED (VERTICAL STAB) · airframe 26,470 hrs · 25,702 cycles

RT VERTICAL STAB INBD FARING MOUNT ANGLE CRACKED AFT OF HSTAB LE LOWER SIDE.

Part: CAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,470 hrs · 25,702 cycles

FLOOR CAP AT LBL 27 & FS 589 CORRODED AROUND SCREW HOLES.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 26,470 hrs · 25,702 cycles

INBD & OTBD STRINGER CLIPS CRACKED AT FS 280 & STRINGER 3L.

Part: FITTING — CRACKED (FUSELAGE) · airframe 26,470 hrs · 25,702 cycles

PRESS FLOOR SUPPORT BEAM AT RBL 27 ATTACH CLIP TO INTERCOSTAL AT FS 484 IS CRACKED.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 26,470 hrs · 25,702 cycles

AEB FS 621 TO 625 LT UPPER OBLIQUE ANGLE CRACKED.

Part: PLATE — CRACKED (RT EXHAUST) · airframe 26,470 hrs · 25,702 cycles

RT ENG EXHAUST FAIRING ACCESS PANEL 446BB CUT OUT SUPPORT PLATE CRACKED.

Part: MOUNT BRACKET — CRACKED (FUSELAGE) · airframe 26,470 hrs · 25,702 cycles

HYD SYS 2 FILTER MOUNT BRACKET CRACKED.

Part: FITTING — CRACKED (FUSELAGE) · airframe 26,470 hrs · 25,702 cycles

LBL 9 & FS 280 FLOORBEAM INBD & OTBD CLIPS ARE CRACKED.

Part: BULKHEAD — GOUGED (FUSELAGE) · airframe 26,470 hrs · 25,702 cycles

FWD FACE OF FS 621 PRESS BULKHEAD GOUGED BY SCREW AT LBL 13, 3 INCHES ABOVE FLOOR.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 26,470 hrs · 25,702 cycles

RT SIDE SEAT RAIL TRACK GOUGED AT FS 428.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,470 hrs · 25,702 cycles

RBL 9 FLOOR SEAT RAIL TRACK CORRODED FROM FS 559+55 TO 559+85.

Part: FITTING — CRACKED (FUSELAGE) · airframe 26,470 hrs · 25,702 cycles

INBD & OTBD FLOORBEAM CLIPS AT RBL 9 & FS 280 ARE CRACKED.

Part: FITTING — CRACKED (FUSELAGE) · airframe 26,470 hrs · 25,702 cycles

PRESS FLOOR SUPPORT BEAM LBL 27 & LBL 36 CLIPS TO INTERCOSTAL AT FS 484 IS CRACKED.

Part: FITTING — CRACKED (COCKPIT) · airframe 26,470 hrs · 25,702 cycles

CO-PILOTS WINDSHIELD OTBD POST LOWER OTBD CLIP IS CRACKED.

Part: HOUSING — SCORED (SERVICE DOOR) · airframe 26,470 hrs · 25,702 cycles

SERVICE DOOR HANDLE HOUSING SCORED ON INNER SURFACE.

Part: SKIN — CRACKED (FUSELAGE) · airframe 26,470 hrs · 25,702 cycles

FUSELAGE SKIN CRACKED AT AFT LT CORNER OF NLG WW CUT OUT.

Part: DOUBLER — CRACKED (LT EXHAUST) · airframe 26,470 hrs · 25,702 cycles

LEFT EXHAUST FAIRING LOWER MOUNT BOLT ACCESS CUT OUT DOUBLER CRACKED.

Part: PROXIMITY SENSOR — OUT OF ADJUST (PAX DOOR) · airframe 21,548 hrs · 20,960 cycles

PAX DOOR WARNING IN FLIGHT AT 7 PSID. C/W QRH, WITNESS MARKS APPEARED NORMAL. ADJUSTED PAX DOOR CAN 1 PROXIMITY SENSOR IAW AMM 52-70-04. OPS CHECKED GOOD.

Part: ANGLE — CORRODED (FS 310-349) · corrosion level 2 · airframe 21,580 hrs · 20,958 cycles

PAX DOOR LOWER SURROUND STRUCTURE ANGLE BETWEEN FS 310.00 & FS 349.00 AT WL 73 CORRODED. R & R PAX DOOR LOWER SURROUND STRUCTURE ANGLE BETWEEN FS 310.00 AND FS 349.00 AT WL 73 IAW SRM 51-42-06 & 51-42-21.

Part: HINGE FITTING — GOUGED (RT WING TE FLAP) · airframe 21,580 hrs · 20,958 cycles

RIGHT OTBD FLAP, OTBD FORWARD HINGE BOX HAS A GOUGE BEHIND THE FORWARD INBD FLAP HINGE BOX FAIRING ATTACH POINT. BLENDED AND ROTO PEENED RT OTBD FLAP, OTBD FWD HINGE BOX IAW REO 601R-57-21-1715 SRM 51-40-11, 51-12-00, 51-28-11, 51-25-06, 51-25-16, 51-24-11.

Part: HINGE FITTING — GOUGED (LT WING TE FLAP) · airframe 21,580 hrs · 20,958 cycles

LT OTBD FLAP, OTBD HINGE BOX IS GOUGED BY FAIRING ATTACHMENT FASTENER INBD FWD LT OTBD FLAP OTBD HINGE BOX BLENDED AND SHOT PEENED IAW REO 601R-57-21-1715, SRM 51-25-16, 51-12-00, 51-40-11, 51-24-11, 51-21-11, 51-25-06.

Part: RETAINER — DAMAGED (CARGO DOOR SEAL) · airframe 21,580 hrs · 20,958 cycles

CARGO DOOR SEAL RETAINER DAMAGED. REMOVED DAMAGED CARGO DOOR SEAL RETAINER AND REPLACED WITH NEW SERVICEABLE IAW SRM 51-42-06.

Part: SUPPORT BRACKET — CRACKED (RT EXHAUST DUCT) · airframe 21,580 hrs · 20,958 cycles

RT JETPIPE UPPER CORE COWL STANG ROD SUPPORT BRACKET ASSY MISSING RIVET AND STIFFENER AT XN214 CRACKED. R & R STIFFENER IAW CMM 78-11-00, SRS 042.

Part: SUPPORT BRACKET — CRACKED (CARGO DOOR) · airframe 21,580 hrs · 20,958 cycles

CARGO DOOR LOWER FWD SUPPORT BRACKET IS CRACKED. REMOVED CRACKED CARGO DOOR LOWER FWD SUPPORT BRACKET INSTALLED NEW SERVICEABLE CARGO DOOR LOWER FORWARD BRACKET IAW SRM 51-42-06.

Part: MOUNT BRACKET — CRACKED (PAX DOOR) · airframe 21,580 hrs · 20,958 cycles

PAX DOOR POWER ASSIST MOTOR MOUNTING BRACKET IS CRACKED. REMOVED CRACKED MOUNTING BRACKET THEN INSTALLED NEW SERVICEABLE BRACKET PN 601R317745-7 IAW SRM 51-42-06.

Part: HANDLE — CRACKED (PAX DOOR) · airframe 21,580 hrs · 20,958 cycles

PAX DOOR EXTERIOR OPEN HANDLE IS CRACKED. REMOVED CRACKED OUTER HANDLE FROM PAX DOOR AND INSTALLED NEW SERVICEABLE OUTER HANDLE IAW AMM 52-11-03.

Part: HANDLE — CRACKED (CARGO DOOR) · airframe 21,580 hrs · 20,958 cycles

CARGO DOOR HANDLE CRACKED ON FLANGE. REMOVED DAMAGED HANDLE ASSY AND REPLACED WITH NEW SERVICEABLE HANDLE ASSY, PN H3415-31 IAW SRM 51-42-01, 51-42-21 AND AMM 52-31-03.

Part: HINGE — DAMAGED (PAX DOOR) · airframe 21,580 hrs · 20,958 cycles

PAX DOOR FUSELAGE HINGE HALF HAS DAMAGE FROM ROLL PIN COMPLIED WITH REO 601R-52-11-1347.

Part: ATTACH ANGLE — CRACKED (BS 334) · airframe 21,580 hrs · 20,958 cycles

PAX DOOR LATCH CAM COVER PLATE AFT ATTACH ANGLE IS CRACKED. R & R PAX DOOR LATCH CAM COVER PLATE AFT ATTACH ANGLE IAW SRM 51-41-02.

Part: HINGE — CHAFED (PAX DOOR) · airframe 21,580 hrs · 20,958 cycles

PAX DOOR HINGE HAS CHAFED LUGS. COMPLIED WITH REO 601R-52-11-1347.

Part: BULKHEAD — DAMAGED (FS 280) · airframe 21,580 hrs · 20,958 cycles

RT AFT SIDE OF 280 BULKHEAD HAS DAMAGE ON PREVIOUS REPAIR FROM CONTACT WITH GALLEY STORAGE DOOR. BLENDED OUT MINOR SURFACE DAMAGE AND RESTORED PROTECTIVE FINISH IAW SRM 51-12-00, 51-21-11, 51-25-06, 51-25-16.

Part: BRACKET — CRACKED (FS 529) · corrosion level 2 · airframe 21,580 hrs · 20,958 cycles

LT MLG WHEEL WELL PRESSURE TRANSDUCER MOUNT BRACKET CRACKED. R & R CRACKED BRACKET ON LT MLG WW WITH NEW IAW SR 51-42-06 AND 51-40-11.

Part: SEAT TRACK — CORRODED (FS 568-559) · airframe 21,580 hrs · 20,958 cycles

CORROSION FOUND ON CARGO TRACKS AT LBL 9 & RBL 9 AT FS 568-559+110. R & R CARGO TRACKS WITH SERVICEABLE IAW AMM 53-01-11.

Part: DOOR — CHAFED (APU BAY) · airframe 21,580 hrs · 20,958 cycles

APU ENCLOSURE DOOR HAS CHAFE ON INSIDE. REMOVED CHAFE DAMAGE ON APU ENCLOSURE DOOR IAW REO 601R-49-11-070, REV B.

Part: MOUNT BRACKET — CRACKED (FS 529) · airframe 21,580 hrs · 20,958 cycles

RT MLG WW PRESSURE TRANSDUCER MOUNT BRACKET CRACKED. R & R CRACKED BRACKET IN RT MLG WW PRESSURE TRANSDUCER MOUNT BRACKET WITH NEW SERVICEABLE PN 601R75262-157 IAW SRM 51-42-06, 51-40-11, 51-25-06.

Part: ATTACH BRACKET — CRACKED (FS 175) · airframe 21,580 hrs · 20,958 cycles

HYDRAULIC NR 3 BRAKE ACCUMULATOR BRACKET FWD CRACKED. R & R 3 ATTACH BRACKET IAW SRM 51-42-21.

Part: TRUNNION — DAMAGED (LT MLG) · airframe 21,580 hrs · 20,958 cycles

FOUND OVERSIZE HOLE IN LT MLG LOWER TRUNNION FLANGE AFT MOST HOLE IN DOUBLER WHILE PERFORMING COLD WORKING. REPAIRED 1 EA DISCREPANT HOLE IN LT LOWER MLG TRUNNION FLANGE IAW REO 601R-57-21-1714, REV 2012 7/14.

Part: DOOR — CRACKED (APU BAY) · airframe 21,580 hrs · 20,958 cycles

APU ENCLOSURE DOOR HAS MULTIPLE CRACKS. REPAIRED CRACKS ON APU DOOR, 3 EA, IAW REO 601R-49-11-070, REV B.

Part: POST — CRACKED (FS 409+128) · airframe 21,580 hrs · 20,958 cycles

RBL 27 POST AT FS 409+128 CRACKED ON LOWER END. COMPLIED WITH REO 601R-53-41-056, REV F.

Part: THRESHOLD — CORRODED (FS 310-349) · airframe 21,580 hrs · 20,958 cycles

SERVICE DOOR THRESHOLD HAS SEVERAL CORRODED FASTENER HOLES AND CRACKED. REMOVED UNSERVICEABLE SERVICE DOOR THRESHOLD AND REPLACED WITH SERVICEABLE SERVICE DOOR THRESHOLD IAW SRM 51-41-00.

Part: O-RING — MISSING (IDG CARBON SEAL) · airframe 18,496 hrs · 17,726 cycles

LT ENG LOW OIL PRESS INDICATION. OIL PRESSURE AT 37 PSI. CW, QRH, REDUCED TO IDLE. OIL PRESSURE DROPPED TO 35 PSI. OIL PRESSURE 27-31 PSI TIL SHORT FINAL THEN DROPPED TO 25 PSI. JUST PRIOR LDG AND 20 PSI JUST AFTER LDG. SHUTDOWN ENGINE AFTER LANDING. FOUND MISSING O-RING TO LEFT ENG IDG CARBON SEAL. REPLACED CARBON SEAL O`RING IAW SUPP 05 018D. CONSUMED 0 OIL ON ENG CONSUMPTION RUN. IDLE SPEED CHECK OK.

Part: SKIN — GOUGED (RT WING SPOILER) · airframe 17,578 hrs · 16,772 cycles

TOP OF RT FLIGHT SPOILER AT CTR T/E IS GOUGED. REPAIRED RT FLIGHT SPOILER UPPER SKIN BETWEEN SPOILER STA 195.3603 AND SPOILER STA 204.3603 IAW REO 601R-57-73-133.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 17,578 hrs · 16,772 cycles

FS 202 BULKHEAD CRACKED AROUND BRAKE PUSH-PULL ROD. REPAIRED BULKHEAD AT FS 202.00 BY FULLY INCORPORATING REO 601R-53-11-2009.

Part: SKIN — CHAFED (LT WING AILERON) · airframe 17,578 hrs · 16,772 cycles

LT AILERON UPPER L/E IS CHAFED. REPAIRED AREAS AILERON STA 302-304 AILERON 309-321 AND AILERON STA 360-345 IAW REO 601R-57-60-013, NC.

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 17,578 hrs · 16,772 cycles

FOUND MISLOCATED FUEL QTY CONNECTOR PLUG HOLE ON RT 559 REPAIR. REPAIRED MISLOCATED FUEL QTY CONNECTOR PLUG HOLE ON RT 559 IAW DEVIATION REO 601R-53-41-1303.

Part: SKIN — CRACKED (PAX DOOR) · airframe 17,578 hrs · 16,672 cycles

AFT PAX DOOR AIRSTAIR SKIN CRACKED UNDER STEP 832DT. REPAIRED AFT SKIN UNDER STEP 832DT IAW REO 601R-52-11-702, REV C.

Part: FITTING — CHAFED (RT WING TE FLAP) · airframe 17,578 hrs · 16,772 cycles

RT OTBD FLAP INBD ROLLER GUIDE FITTING CHAFED. BLENDED OUT DAMAGE IAW SRM 51-12-00, EDDY CURRENT INSPECTION IAW NDTM 51-20-06. ROTO PEEN REWORKED AREA SRM 51-24-11.

Part: SIDEWALL PANEL — CRACKED (FUSELAGE) · airframe 17,578 hrs · 16,772 cycles

AFT STAIR SIDEWALL CRACKED ABOVE PANEL 832FR. REPAIRED AFT STAIR PANEL SIDEWALL ABOVE 832FR IAW REO 601R-52-11-702, REV C.

Part: FITTING — CHAFED (RT WING TE FLAP) · airframe 17,578 hrs · 16,772 cycles

RT OTBD FLAP INBD ROLLER FITTING BENEATH ROLLER CHAFED. BLENDED OUT CHAFED AREA IAW SRM 51-12-00, EDDY CURRENT INSPECT IAW NDTM 51-20-06, ROTOPEEN IAW SRM 51-24-11.

Part: TRACK — CHAFED (THRUST REVERSER) · airframe 17,578 hrs · 16,772 cycles

RT THRUST REVERSER UPPER PYLON TRACK CHAFED. BLENDED OUT CHAFE AREA TO SMOOTH CONTOUR IAW SRM 51-12-00, NOT EXCEDING REPORTED DEPTH EDDY CURRENT INSPECTED, RESTORED FINISH IAW CMM 20-21-11.

Part: FITTING — CHAFED (LT WING TE FLAP) · airframe 17,578 hrs · 16,772 cycles

LT OTBD FLAP INBD ROLLER FITTING BENEATH ROLLER IS CHAFED. BLENDED OUT DAMAGE TO A SMOOTH CONTOUR IAW SRM 51-12-00, EDDY CURRENT INSPECTED IAW 51-20-06 SHOT PEEN IAW SRM 51-24-11. RESTORED PROCTINO FINISH IAW SRM 51-21-16.

Part: SKIN — CHAFED (FLAP VANE) · airframe 17,578 hrs · 16,772 cycles

RT INBD FLAP, FLAP VANE SKIN L/E CHAFED AT INBD CTR OTBD ENDS BLENDED CTR AND OTBD LOCATIONS ARE WITHIN LIMITS, INBD VANE L/E LOCATION REPLACED L/E SKIN COMPLETING WORK IAW REO 601R-57-52-004, REV C, SRM 51-42-13.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 17,578 hrs · 16,772 cycles

PAX DOOR AFT DRAG ANGLE CRACKED ON PREVIOUS REPAIR. REPAIRED AFT DRAG ANGLE IAW REO 601R-52-11-513, REV A.

Part: PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 17,578 hrs · 16,772 cycles

FUEL C/O FOR PNL 550CB REQUIRE AWAC E06/021/457 CURRENT REV TO BE C/W INDICATION FOUND ON AFT OTBD SIDE. REPAIRED FUEL PANEL C/O PNL 550CB IAW REO 601R-57-21-030 REV H, AT APT OTBD SIDE DETAIL III.

Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 17,578 hrs · 16,772 cycles

LT INBD FLAP VANE L/E INBD CTR AND OTBD CHAFED. REPAIR LT INBD FLAP VANE SKIN AT FLAP STA 137.012 AND BETWEEN FLAP STA 98.509 AND 108.135 IAW REO 601R-57-52-004, REV C. R & R LT INBD FLAP VANE INBD L/E SIN IAW SRM 51-42-13.

Part: RIB — CRACKED (LT WING) · airframe 17,578 hrs · 16,772 cycles

LT WING BATT RIB IS CRACKED. REPAIRED LT WING BATT RIB AT WS 53.60 IAW REO 601R-57-51-046, REV B, REPAIR NR 2.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 17,578 hrs · 16,772 cycles

RT OBLIQUE ANGLE AT FS 625.00 IS CRACKED. R & R RT OBLIQUE ANGLE IAW REO 601R-53-61-100.

Part: BULKHEAD — CHAFED (FUSELAGE) · airframe 17,578 hrs · 16,772 cycles

FS 280, RBL 9 APPROX 18" FROM FLOOR ON BACKSIDE OF BULKHEAD HAS 2 AREAS OF CHAFING. REPAIRED FS 280 BULKHEAD AT RBL 11.0 BETWEEN STR 13A & 14A REO 601R-53-11-1727, REV D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 17,578 hrs · 16,772 cycles

LBL9 INBD CLIP FS 280 CRACKED. R & R CLIP AT FS 280, INBD SIDE OF LBL 9.0 IAW SRM 51-42-21.

Part: PLATE — CHAFED (LT WING TE FLAP) · airframe 17,578 hrs · 16,772 cycles

LT INBD FLAP INBD AFT LUG PLATE HAS CHAFE DAMAGE WS 80.50. REPAIRED IAW REO 601R-57-52-1536, TYPE I.

Part: PLATE — CHAFED (RT WING TE FLAP) · airframe 17,578 hrs · 16,772 cycles

RT INBD FLAP INBD OF LUG PLATE HAS CHAFE DAMAGE WS 80.50. REPAIRED IAW REO 601R-57-52-1536, TYPE I.

Part: BEARING — OUT OF TOLERANCE (RUDDER) · airframe 17,578 hrs · 16,772 cycles

REPLACE MIDDLE (UPPER & LOWER) RUDDER HINGE BEARINGS ON ACFT WITH RUDDER PN 601R22014-1. R & R BEARINGS.

Part: ANTI-ICE SYSTEM — WARNING MESSAGE · airframe 15,726 hrs · 14,806 cycles

ANTI ICE DUCT WARNING ON TAKE OFF SYNOPTIC PAGE INDICATES LEFT FUSELAGE, MESSAGE DID NOT CLEAR WHEN 14TH STAGE AIR SELECTED OFF. C/A IN PROGRESS.

Part: THRESHOLD — CORRODED (BS 319-349) · corrosion level 2 · airframe 13,620 hrs · 12,697 cycles

SERVICE DOOR THRESHOLD CORRODED. CORROSION REMOVED IAW SRM 51-21-06 AND FOUND OUT OF LIMITS IAW SRM 53-00-00. SERVICE DOOR THRESHOLD PLATE REPLACED IAW CRJ 200 51-41-02. (K)

Part: FLOORBEAM — CRACKED (BS 280) · airframe 13,620 hrs · 12,697 cycles

AFT FLOORBEAM ANGLE AT LBL 9.00, FS 280.00 FOUND CRACKED AFT FLOOR ANGLE AT LBL 9.0, FS 280. REPAIRED IAW REO 601R-53-11-136 REV A. (K)

Part: FLOORBEAM — CRACKED (BS 280) · airframe 13,620 hrs · 12,697 cycles

OTBD CLIP CRACKED AT FS 280.00, LBL 9.0, OTBD CLIP AT FS 280.00 AND LBL 9.00. REPLACED IAW SRM 51-52-21. (K)

Part: FLOORBEAM — CRACKED (BS 484) · airframe 13,620 hrs · 12,697 cycles

PREVIOUS REPAIR, ANGLE AND CLIP CRACKED AT FS 480.00, LBL 27.00 AND LBL 36.00. AND ANGLE AND CLIP ARE REPLACED IAW SRM 51-42-21. (K)

Part: BEAM — CRACKED (CARGO DOORWAY) · airframe 13,620 hrs · 12,697 cycles

CARGO DOOR UPPER BEAM LOWER ANGLE AT FS 621.00 (PRESSURE BULKHEAD) CRACKED. CARGO DOOR UPPER BEAM LOWER ANGLE AT FS 621 (BULKHEAD PRESSURE) REPLACED IAW SRM 51-42-21. (K)

Part: STRUCTURE — CRACKED (PAX DOOR) · airframe 13,620 hrs · 12,697 cycles

PAX DOOR EDGE MEMBER FWD CORNER CRACK, CRACK LENGTH .400 CUT OUT PERFORMED ON PAX DOOR EDGE MEMBER IAW REO 601R-52-11-279. EDDY CURRENT PERFORMED ON CUT-OUT IAW REO 601R-52-11-279. REPAIR PERFORMED ON PAX DOOR EDGE MEMBER FWD CORNER IAW REO 52-11-279. (K)

Part: FLOORBEAM — CRACKED (BS 484) · airframe 1,360 hrs · 12,697 cycles

PREVIOUSLY REPAIRED ANGLE AND CLIP CRACKED AT F/S 484, RBL 27 AND RBL 36.0 (REF REO 53-41-059 REV A) FABRICATED ANGLE AND CLIP AND INSTALLED. (K)

Part: SILL — CRACKED (BS 574) · airframe 13,620 hrs · 12,697 cycles

LT FLOOR SILL CRACKED AT FS 574.00 UNDER STOP BRACKET. LT FLOOR SILL CRACK AT FS 574 UNDER STOP BRACKET REPAIR IAW REO 601R-53-61-1741. (K)

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 13,620 hrs · 12,697 cycles

PAX DOOR AFT DRAG ANGLE CRACKED, CRACK LENGTH .800, REPAIR TO PAX DOOR AFT DRAG ANGLE CARRIED OUT IAW REO 601R-52-11-513, REV A. (K)

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 13,620 hrs · 12,697 cycles

AFT FLOOR ANGLE AT RBL 9.0, FS 280.00. FOUND CRACKED AFT FLOOR ANGLE AT RBL 9.0, FS 280.0. REPAIRED IAW REO 601R 53-11-136, REV A. (K)

Part: FLOORBEAM — CRACKED (BS 280) · airframe 13,620 hrs · 12,697 cycles

INBD CLIP FOUND CRACKED, FS 280, RBL 9.0. INBD CLIP REPLACED AT FS 280.0, RBL 9.0 IAW SRM 51-42. (K)

Part: ELEMENT — MALFUNCTIONED (LT NACELLE) · airframe 12,570 hrs · 11,685 cycles

LT 14TH DUCT WARNING MESSAGE EN ROUTE. COMPLIED WITH QRH. R&R LT PYLON 14TH STAGE SENSE ELEMENT IAW 36-21-00. OPS CHECK GOOD.

Part: BPSU — MALFUNCTIONED (TE FLAPS) · airframe 12,444 hrs · 11,563 cycles

FLAP FAIL ON TAXI OUT AFTER SHORT TURN. ATTEMPT TO RESET PER FIM DID NOT CLEAR MESSAGE. FLAPS AT ZERO. LT BPSU REPLACED IAW AMM 27-51-10-400-801. RIGGING CARRIED OUT AND OPS CHECK CARRIED OUT IAW 27-51-10-220-802. OPS CHECK GOOD. OK FOR SERVICE.

Part: PDU — FAILED (TE FLAPS) · airframe 12,438 hrs · 11,555 cycles

FLAPS FAIL AT 20 DEGREES ON APPROACH. R&R FLAP PDU PER AMM 27-53-01, OPS CHECK GOOD.

Part: FLAP — MALFUNCTIONED (WING) · airframe 12,416 hrs · 11,537 cycles

FLAPS FAIL AT 30 DEGREES ON APPROACH REF PREVIOUS WRITE UP. COMPLIED WITH FLAP RESET PROCEDURE IAW AWAC SUPP 98-018B STEPS 1.3 AND 1.4 FLAP SYSTEM RESET OK.

Part: FLAP SYSTEM — FAILED (TE FLAPS) · airframe 12,400 hrs · 11,520 cycles

FLAPS FAIL AT ZERO DURING APPROACH. FOUND REPEAT LT BPSU, FECU, WIRING FAULT CODES. CONTINUITY RESISTANCE & MEGGER CHECKED LT BPSU WIRING. NO FAULTS FOUND. REPLACED FECU PER AMM CH 27-50. OPS CHECK AND RIG CHECKS GOOD.

Part: SENSOR — FAILED (TE FLAPS) · airframe 12,322 hrs · 11,438 cycles

FLAPS FAIL MESSAGE FROM 30 TO 45 ON LANDING. FLAPS FAILED AT 30 DEGREES. REMOVED AND REPLACED LT BRAKE POSITION SENSOR UNIT PER AMM 27-54-01, OPS AND RIG CHECK GOOD. (S)

Part: FLAP SYSTEM — FAILED (TE FLAPS) · airframe 12,314 hrs · 11,431 cycles

FLAPS FAILED AT ZERO AFTER TAKEOFF. DID NOT LAND OVERWEIGHT. CORRECTIVE ACTION IN PROGRESS. (A)

Part: FLAP SYSTEM — FAILED (TE FLAPS) · airframe 12,314 hrs · 11,431 cycles

FLAP FAIL CAS MESSAGE ILLUMINATED AT 100FT AGL WITH FLAPS AT 45 DEGREES, MESSAGE ILLUMINATED APPROXIMATELY 1 MINUTE AFTER FLAPS INDICATED AT 45 DEGREES. C/W AWAC SUPP 98-018B RESET C/B`S INTERROGATED FECU, RAN FLAP SYS NO DEFECTS NOTED AT THIS TIME.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 11,473 hrs · 10,632 cycles

ON DESCENT CAPTAINS WINDSHIELD CRACKED. COMPLIED WITH QRH, CYCLED HEAT `OFF`, THEN `ON` THEN BACK `OFF`, AFTER RECEIVING LT WINDSHIELD HEAT CAS MESSAGE. REMOVED AND REPLACED CAPTAINS WINDSHIELD IAW AMM 56-11-01. (M)

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 11,066 hrs · 10,230 cycles

IDG NR 1 CAUTION MESSAGE ON TAKEOFF, TAKEOFF ABORTED AT LESS THAN 80 KNOTS. (K)

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 8,982 hrs · 8,217 cycles

FLAPS FAIL IN FLIGHT WHEN FLAPS 8 DEGREES SELECTED, FLAPS FAILED AT 0 DEGREES. VISUALLY INSPECTED EACH OB FLAP NO EVIDENCE OF TWISTING, SKEWING OR ABNORMAL DEFORMATION NOTED. OB FLAP POSITION INDICATION ARE NOT OUTSIDE GO RANGE. FLAP FAIL MESSAGE NOT ILLUMINATED, FLAPS OPS NORMAL, IAW AWAC SUPP 98-018B. (K)

Part: RELAY — DAMAGED (ADG) · airframe 865 hrs · 7,916 cycles

ON AC SYNOPTIC PAGE, ADG BUSS DISPLAYED IN WHITE. AC1 AND AC2 BUSS SHOW WHITE LINES TO ESS BUSS, ESS BUSS IS GREEN. REMOVED AND REPLACED ADG ESSENTIAL TRANSFER CONTACTOR (KX2D). PERFORMED OPS CHECK, OPS CHECK GOOD. REF AMM 24-51-31. (K)

Part: SPAR — MISDRILLED (WING)

WHILE PERFORMING E03/062/457 MODIFICATION LT AND RT WING REAR SPARS, A FASTENER HOLE WAS MISDRILLED. HOLE DIAMETER .213 INCH AT TRAILING EDGE WS 129, 2 INCHES IB OF JACKING PAD POINT ON RT WING. (M) MAINTENANCE REAMED HOLE TO ACCOMMODATE .25 INCH HOLE TO BE COLD WORKED AND INSTALLED HST11A68 HI-LITE IAW BSC EO 601R-57-10936. (K)

Part: STRUCTURE — DAMAGED (WING)

FOUND NR 15 HOLE AT WS 148 LHS IS ELONGATED TO .230 INCH. (M) MAINTENANCE REPAIRED BY CLEANING UP HOLE AND INSTALLING FREEZE PLUG IAW EO 601R57-10925A. (K)

Part: ANGLE — CRACKED (RT FS484)

FOUND FS 484 ANGLE IS CRACKED AT RBL 36. (M) MAINTENANCE REPLACED ANGLE IAW REO 601R-53-41-059. (K)

Part: ANGLE — CRACKED (FUSELAGE)

FOUND FS 484 ANGLE IS CRACKED AT LBL 36. (M) MAINTENANCE REPLACED ANGLE IAW REO 601R-53-41-059. (K)

Part: FITTING — CRACKED (RT IB, OB) · airframe 8,623 hrs · 7,884 cycles

FS 280.00 CLIPS ARE CRACKED .2500 INCH IN UPPER RADIUS IB AND OB RBL 9. (K) MAINTENANCE REMOVED AND REPLACED FS 280 CLIPS IB AND OB OF RBL 9 MFG STANDARD REPAIR NR 601R-53-0057A, STEPS 1 THRU 4. (K)

Part: FITTING — CRACKED (LT IB, OB FUSELA) · airframe 8,623 hrs · 7,884 cycles

FS 280.00 CLIPS ARE CRACKED .2500 INCH IN UPPER RADIUS IB AND OB OF LBL 9. (K) MAINTENANCE REMOVED AND REPLACED FS 280 CLIPS IB AND OB OF LBL 9 IAW MFG STANDARD REPAIR NR 601R-53-0057A STEPS 1 THRU 4. (K)

Part: ANGLE — CRACKED (LT, RT, FS625) · airframe 8,623 hrs · 7,884 cycles

LT AND RT FS 625.00 OBLIQUE ANGLES ARE CRACKED .5 INCH LONG ON AFT RADIUS. (K) MAINTENANCE DRILLED OFF, REMOVED CRACKED OBLIQUE ANGLES LT AND RT FS 625 DRILLED UP, ALODINED AND INSTALLED ANGLES PN 601-35012-51 (LT AND 601-35012-529 (RT). OBLIQUE ANGLES INSTALLED WET USING PR1422BY2 SEALANT AND MS2D470AD-5 AND -6 SOLID RIVETS, PRIMED AND PAINTED. (K)

Part: BRACKET — CRACKED (RT MLG BAY) · airframe 8,623 hrs · 7,884 cycles

HYDRAULIC TRANSDUCER HAT CHANNEL APPROX .1 INCH LONG RT MLG WHEEL WELL CEILING. (K) MAINTENANCE INSTALLED NEW HAT CHANNEL IAW SRM 51-42-06. (K)

Part: BRACKET — CRACKED (LT MLG BAY) · airframe 8,623 hrs · 7,884 cycles

HYDRAULIC TRANSDUCER HAT CHANNEL CRACKED APPROX .1 INCH LONG LT MLG WHEEL WELL CEILING. (K) MAINTENANCE INSTALLED NEW HAT CHANNEL IAW SRM 51-42-06. (K)

Part: SKIN — DENTED (TE FLAP)

INBOARD LEFT FLAP LOWER SKIN HAS DENT WITH GOUGE LOCATED 3.75 INCH FROM INBOARD EDGE AND 8.5 INCH FORWARD OF T/E MEASURES 2 INCHES BY 2 INCHES BY .098 INCH DEEP. REPAIRED LEFT INBOARD FLAP LOWER SKIN BY INSTALLING EXTERNAL DOUBLER IAW BSC EO 601R-57-9969. (M)

Part: BUSHING — MIGRATED (RT MLG)

RIGHT AFT MAIN LANDING GEAR TRUNNION BUSHING IS MIGRATED .041 INCH, AT WS 66. (M)

Part: FLOOR SUPPORT — CRACKED (FUSELAGE)

FLOOR SUPPORT ANGLE AT FS 621, LBL 36, WL 73 IS CRACKED, APPROXIMATELY .25 INCH. (M)

Part: BUSHING — MIGRATED (LT MLG)

LEFT AFT MAIN LANDING GEAR TRUNNION BUSHING IS MIGRATED .050 INCH AT WS 66. (M)

Part: ANGLE — CRACKED (FUSELAGE)

RT FS 621 ANGLE HAS A .5 INCH CRACK ON OUTBOARD RADIUS. S/D - REPAIRED CRACKED RT FS 621 ANGLE BY CUTTING AWAY DAMAGED AREA AND INSTALLING REPAIR ANGLE AND STRAP IAW BOMBARDIER REO 601R-53-61-117 REV C. (M)

Part: WINDSHIELD — FAILED (COCKPIT)

CAPTAINS FORWARD WINDSHIELD SHATTERED IN FLIGHT. REMOVED AND REPLACED WINDSHIELD. (M)

Part: CONTROLLER — INTERMITTENT (FIRE DETECTOR)

INTERMITTENT RT ENGINE FIRE FAIL CAS INDICATION INFLIGHT AT ONE TIME FOR 3 SECONDS ENGINE FIRE CAS MESSAGE. REMOVED AND REPLACED FIRE DETECTION CONTROLLER. (M)