N424AW

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,663 hrs · 37,035 cycles

SERVICE DOOR CUTOUT LOWER SILL ANGLE IS CORRODED.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,663 hrs · 37,035 cycles

PAX DOOR LOWER SILL ANGLE IS CORRODED AROUND CUTOUT FOR THE PROX SENSOR I/B SIDE.

Part: POST — CRACKED (FUSELAGE) · airframe 38,662 hrs · 37,035 cycles

FS 409+128 LBL 18 VERT POST HAS CRACK INDICATION NOTED IN THE AFT FLANGE RADIUS AT WL 69 I/B SIDE .250 LONG O/B SIDE .500 LONG. BOTH GREATER THAT 50%FSH BOTH FAILED NDT INSP>

Part: POST — CRACKED (FUSELAGE) · airframe 38,662 hrs · 37,035 cycles

FS 409+128, LBL 18 VERT POST HAS CRACK INDICATIONS NOTED IN THE AFT FLANGE REDIUS AT WL 69 I/B SIDE .250 LONG, O/B SIDE .500 LONG. BOTH GREATER TAHN 50% FSH BOTH FAILED NDT ISP.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,663 hrs · 37,035 cycles

LBL27 CARGO FLOORBEAM HAS CORROSION AROUND ONE NUTPLATE HOLE AT FS559+ 114.

Part: SEAT TRACK — CORRODED (BS 574-608) · corrosion level 2 · airframe 38,662 hrs · 37,035 cycles

CARGO LBL 27 SEAT RAIL BEAM IS CORRODED AROUND NUTPLATES OB FLANGE F.S. 574.00 TO F.S. 608.00.

Part: WEB — CRACKED (PAX DOOR) · airframe 38,662 hrs · 37,035 cycles

PASSENGER DOOR AFT WEB HAS AN INDICATION NOTED AT FOOTPRINT OF O/B STIFFENER FOR POWER ASSIST MOTOR. 0.250" LONG BY 50%FSH, FAILED NDT.

Part: POST — CRACKED (FUSELAGE) · airframe 38,663 hrs · 37,035 cycles

FS409+128 RBL18 VERT POST HAS CRACK INDICATIONS NOTED IN THE AFT FLANGE RADIUS AT WL69. I/B SIDE .250" LONG, O/B SIDE .600" LONG, BOTH GREATER THAN 50% FSH. FAILED NDT INSPECTION.

Part: POST — CRACKED (FUSELAGE) · airframe 38,663 hrs · 37,035 cycles

FS409+128 RBL18 VERT POST HAS CRACK INDICATIONS NOTED IN THE AFT FLANGE RADIUS AT WL69. I/B SIDE .250" LONG, O/B SIDE .600" LONG, BOTH GREATER THAN 50 % FSH. FAILED NDT INSPECTION.

Part: POST — CRACKED (FUSELAGE) · airframe 38,663 hrs · 37,035 cycles

FS409+128 BL0 POST HAS CRACK INDICATIONS NOTED IN THE AFT FLANGE RADIUS AT WL69. LT SIDE .600" LONG, R/H SIDE .300" LONG. BOTH GREATER THAN 50% FSH, BOTH FAILED NDT INSPECTION.

Part: POST — CRACKED (FUSELAGE) · airframe 38,663 hrs · 37,035 cycles

FS409+128 BL0 POST HAS CRACK INDICATIONS NOTED IN THE AFT FLANGE RADIUS AT WL69. LT SIDE .600" LONG, RT SIDE .300" LONG. BOTH GREATER THAN 50% FSH. BOTH FAILED NDT INSPECTION.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 38,663 hrs · 37,035 cycles

FOUND REAR PRESSURE BULKHEAD WEB HAS 7 AREAS WITH MULTIPLE INDICATIONS NOTED. 1) LBL 18, WL 129 - 132.5, 60% FSH, 2) LBL 9.5, WL 131 - 133, 50% FSH, 3) RBL 18, WL 131 - 134.5, 50% FSH, 4) RBL 27.5, WL 129.5 - 131, 70% FSH, 5) RBL 27.5, WL 114 - 85.5, 60% FSH, 6) RBL 9.5, WL 110 - 109, 80% FSH, AND 7) LBL 27.5, WL 110 -97, 60% FSH. ALL 7 AREAS FAILED NDT INSPECTION.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 38,662 hrs · 37,035 cycles

PASSENGER DOOR AFT DRAG ANGLE IS CRACKED IN PREVIOUS REPAIR.

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 38,662 hrs · 37,035 cycles

RH INBD FLAP LOWER SKIN HAS A DENT ON O/B T/E APPROX 10 INCHES FROM THE O/B END OF FLAP

Part: PLATE — CORRODED (BS 319-349) · corrosion level 2 · airframe 38,662 hrs · 37,035 cycles

SERVICE DOOR STEP PLATE IS CORRODED.

Part: SMOKE DETECTOR — OUT OF POSITION (LAVATORY) · airframe 37,944 hrs · 36,341 cycles

SMOKE TOILET CAUTION AND AURAL TONE RECEIVED ON FINAL AT 2600 FT. AFTER LANDING, INSPECTION CREW NOTICED SMOKE DETECTOR WAS NOT FLUSH WITH BULKHEAD.

Part: WARNING MESSAGE — ILLUMINATED (ANTI-SKID SYSTEM) · airframe 37,716 hrs · 36,122 cycles

AT LIFT OFF RECEIVED IB ANTISKID CAUTION MSG. MSG CLEARED AFTER G EAR RETRACTION. MSG RETURNED AFTER GEAR EXTENSION ON TOUCHDOWN AND CLEAR AGAIN ON TAXI IN.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 37,295 hrs · 35,715 cycles

AFTER T/O AND SELECTING GEAR LEVER IP, RECEIVED GEAR DISAGREE. NOSE GEAR DID NOT SHOW RETRACTED. C/W QRH. OPERATED MANUAL RELEASE AND SELECTED HANDLE DOWN. GEAR SHOWED 3 GREEN. RETURNED TO MKE. LANDING WEIGHT LESS THAN 46,000 LBS.

Part: ACTUATOR — FAILED (TE FLAPS) · airframe 35,221 hrs · 33,618 cycles

FLAPS FAILED AT 27 DEGREES DURING APPROACH. EMERGENCY DECLARED. REMOVED AND REPLACED THE LT FLAP ACTUATOR IAW AMM27-53-05. OPS CHECKED GOOD.

Part: HINGE — CRACKED (PAX DOOR) · airframe 35,146 hrs · 33,549 cycles

PAX DOOR OUTER HANDLE FLAP HINGE FWD DOOR HINGE IS BROKEN. REPLACED PAX DOOR OUTER HANDLE FLAP HINGE ASSY IAW SRM 51-42-06.

Part: ATTACH BRACKET — CRACKED (COCKPIT) · airframe 35,146 hrs · 33,549 cycles

FLIGHT DECK CENTER WINDSHIELD POST LOWER ATTACH BRACKET CRACKED. REPLACED BRACKET IAW SRM 51-41-21.

Part: ATTACH BRACKET — CRACKED (COCKPIT) · airframe 35,146 hrs · 33,549 cycles

CENTER WINDSHIELD POST LOWER ATTACH BRACKET LT SIDE IS CRACKED. REPLACED BRACKET IAW SRM 51-41-21.

Part: LANDING — CRACKED (AIR DOOR) · airframe 35,146 hrs · 33,549 cycles

GROUND AIR DOOR AFT LANDING IS CRACKED

Part: FRAME — CORRODED (BS 394) · corrosion level 2 · airframe 35,146 hrs · 33,549 cycles

FRAME BS 394 CORRODED ON AFT SIDE BETWEEN STRINGER 26L AND 26R. REPAIRED THE FRAME IAW 17-156.

Part: BULKHEAD — CRACKED (BS 621) · airframe 34,656 hrs · 33,089 cycles

CRACKS FOUND ON AFT PRESSURE BULKHEAD AT LBL 36.2, WL 79.5, LBL .5, WL 127 - 132.5, LBL .5, WL107 - 115, AND LBL .5, WL 100.5 - 104.5.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHTS) · airframe 34,181 hrs · 32,636 cycles

EMERGENCY LIGHTS INOPERATIVE ROW 8 AND AFT. PERFORMED OPS CHECK ON EMERGENCY SYSTEM AND FOUND LOOSE CONNECTOR ON FLOOR LIGHT, SECURED THE CONNECTOR AND PERFORMED OPS CHECK, OPS CHECKED GOOD IAW AMM 33-50-00.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,961 hrs · 31,507 cycles

FLOOR EMERGENCY LIGHTS, ROW 8 AND AFT WILL NOT ILLUMINATE.

Part: ENGINE — MALFUNCTIONED (LEFT) · airframe 31,197 hrs · 29,843 cycles

RECEIVED VIBRATION & HEARD LOUD BANG, THEN SAW N1 & N2 ON LT ENG DECREASING & ITT RISING UNTIL IT EXCEEDED 900 DEG C. PULLED LT ENG BACK TO IDLE UNTIL SHUTDOWN, CHECKLIST COULD BE COMPLETED. N1 & N2 CONTINUED TO ROTATION, ITT WENT TO ALMOST ZERO. VIBRATION STILL EVIDENT IN AIRFRAME & IN THRUST LEVERS. DIVERTED, LANDING WEIGHT 43000. BTMS READING 6645, LANDING WAS SMOOTH. INSPECTED LT ENG NO EXTERNAL DAMAGE NOTED. R & R ENG.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,976 hrs · 29,617 cycles

FLIGHT 3996, EMER FLOOR LIGHTS INOPERATIVE BETWEEN ROWS 6 - 8. REMOVED LIGHT STRIP ROW 6 - 8. INSPECTED CONNECTORS, NO DEFECTS. REINSTALLED FLOOR STRIP, LIGHTS STILL INOPERATIVE, SEE 266879 3 FOR MEL.

Part: CONNECTOR — LOOSE (CABIN) · airframe 32,406 hrs · 30,657 cycles

FLIGHT 3874 EMERGENCY PATH LIGHTING, ROWS 7 - 9 & LOWER EXIT SIGN WINDOW EXIT RIGHT SIDE INOPERATIVE. FOUND CONNECTOR LOOSE ON FLOOR TRACK LIGHTING ROW 9. CONNECTED WIRING IAW AMM 33-51-01. OPERATIONS CHECKED GOOD.

Part: SUPPORT — CRACKED (PAX DOOR) · airframe 37,676 hrs · 29,409 cycles

PAX DOOR SUPPORT WHEEL LEG IS CRACKED.

Part: ANGLE — UNKNOWN (FUSELAGE) · airframe 37,676 hrs · 29,409 cycles

REPAIR & REINFORCEMENT FOR FS LOWER CAP ANGLES BL 9.00 & 18.00 LT & 7 RT.

Part: FITTING — CRACKED (FUSELAGE) · airframe 37,676 hrs · 29,534 cycles

LBL 280 & RBL 9 INBD & OTBD CLIPS CRACKED.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 37,676 hrs · 29,409 cycles

PAX DOOR AFT DRAG ANGLE CRACKED FWD OF POWER ASSIST YOKE.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 37,676 hrs · 29,409 cycles

LEFT WINDSHIELD SIDE POST SUPPORT LOWER OTBD MOUNT ANGLE IS CRACKED.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 37,676 hrs · 29,409 cycles

RIGHT SIDE FS 621 - 625 OBLIQUE ANGLE AFT OF 621 BULKHEAD AT STRINGER 14R CRACKED.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 37,676 hrs · 29,409 cycles

STRINGER 3L ATTACHED CLIPS AT FS 280.00 BULKHEAD CRACKED.

Part: ATTACH BRACKET — CRACKED (FUSELAGE) · airframe 37,676 hrs · 29,409 cycles

LEFT LOWER NOSE COMPARTMENT FWD ATTACH BRACKET FOR UPPER HYD ACCUMULATOR IS CRACKED.

Part: SEAT TRACK — CHAFED (FUSELAGE) · corrosion level 2 · airframe 37,676 hrs · 29,409 cycles

LT & RT SEAT TRACK AT FS 364 - 409 HAS CORROSION.

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 30,985 hrs · 29,534 cycles

FS 559.00 LOWER BULKHEAD HAS A GOUGE & CRACK AT LBL 18.00.

Part: ENGINE — MALFUNCTIONED (RIGHT) · airframe 30,504 hrs · 29,175 cycles

RT ENGINE INDICATING 125 - 127 PSI IN CLIMB OUT & CRUISE. REDUCED THRUST TO 80% N1 & 86% N2 OIL PRESS PSI. INDICATES 86 PSI AT IDLE ON GROUND. REPLACED RT ENGINE. ALL CHECKED GOOD.

Part: UNKNOWN — ODOR (CABIN) · airframe 28,924 hrs · 27,661 cycles

ELECTRICAL BURNING SMELL EMANATING FROM CEILING AREA AROUND ROWS 5 & 6.

Part: CONTROL UNIT — FAULTY (FIRE WARNING) · airframe 26,999 hrs · 25,805 cycles

INFLIGHT RECEIVED MULTIPLE RT FIRE FAIL CAUTION MESSAGES & RECEIVED 1 RT ENG FIRE RED WARNING MESSAGE, ALL MESSAGES LASTED FOR 2 - 3 SEC. R & R FIRE OVERHEAT CONTROL UNIT IAW AMM 26-10-01, OPERATIONS CHECKED GOOD.

Part: STOP — DAMAGED (CARGO DOOR) · airframe 26,247 hrs · 25,101 cycles

FWD UPPER CARGO DOOR STOP HAS ENLARGED HOLE. REPLACED PART.

Part: ANGLE — CRACKED · airframe 26,247 hrs · 25,101 cycles

ANGLE AT RBL 9 INBD IS CRACKED. REPLACED WITH SERVICEABLE ANGLE.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 26,247 hrs · 25,101 cycles

RAM AIR INTAKE MOUNT BRACKET CRACKED. R & R IAW SRM.

Part: HINGE FITTING — DAMAGED (RUDDER) · airframe 26,247 hrs · 25,101 cycles

RUDDER CENTER HINGE UPPER & LOWER FITTING BEARING TOLERANCE OUT OF LIMITS. R & R HINGE FITTING.

Part: HANDLE — CRACKED (PAX DOOR) · airframe 26,247 hrs · 25,101 cycles

PAX DOOR OUTER HANDLE IS CRACKED. R & R IAW EO E08/007/452, REV B.

Part: HINGE FITTING — DAMAGED (LT WING LE FLAP) · airframe 26,247 hrs · 25,101 cycles

LEFT OTBD FLAP HINGE BOXES AT 178.00, 220.00 AND 264.00 HAS TOOL DAMAGE. BLENDED AND REMOVED DAMAGE.

Part: HINGE — DAMAGED (RWS 220) · airframe 26,247 hrs · 25,101 cycles

RT HINGE BOX AT WS 220 HAS TOOLING MARKS. BLENDED AND REMOVED DAMAGE ON RT HINGE BOX.

Part: TRUNNION — DAMAGED (RT WING MLG) · airframe 26,247 hrs · 25,101 cycles

DURING COLDWORK PROCESS FOUND 1 EA OVERSIZED HOLE ON RT LWR WING MLG TRUNNION STEEL STRAP ON WING PLANK. ACCOMPLISHED REAM AND COLD WORK OF FASTENER HOLE AND INSTALLED IAW REO 601R-57-21-1982.

Part: SEAT TRACK — CORRODED (CABIN) · corrosion level 2 · airframe 26,247 hrs · 25,101 cycles

SEAT TRACK, FS 409-559.64, CORRODED. REMOVED CORRODED SEAT TRACK AND REPLACED WITH NEW SEAT TRACK IAW AMM 53-01-11, 53-01-11-04.

Part: SEAT TRACK — CORRODED (BS 364-439) · corrosion level 2 · airframe 26,247 hrs · 25,101 cycles

SEAT TRACK FS 364-439 HAS CORROSION. REMOVED SEAT TRACK & REPLACED WITH NEW SERVICEABLE SEAT TRACK IAW SRM 53-21-49.

Part: DAMPENER — CRACKED (HORIZONTAL STAB) · airframe 26,247 hrs · 25,101 cycles

LT HORIZONTAL STABILIZER INBD FLUTTER DAMPNER LIGHTING HOLE IS CRACKED. CARRIED OUT EA 15-2013-352.

Part: MOUNT — CRACKED (RT MLG WW) · airframe 26,247 hrs · 25,101 cycles

MOUNT BRACKET CRACKED IN RT W/W. REPLACED BRACKET WITH SERVICEABLE PART.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 26,247 hrs · 25,101 cycles

RT INBD FLAP VANE L/E CHAFED. BLENDED CHAFED AREAS FOUND OTBD L/E TO BE WITHIN LIMITS AND INBD AND MIDDLE OTBD L/E'S TO BE OUT OF LIMITS. R & R INBD AND MIDDLE OTBD L/E'S AND REINSTALLED OTBD L/E ORIGINAL FINISH.

Part: DRAG ANGLE — CRACKED (LT MLG WW) · airframe 26,247 hrs · 25,101 cycles

LT MLG WELL BATTERY RIB DRAG ANGLE CRACKED AT AFT END, R & R.

Part: FLOOR SUPPORT — CORRODED (BS BS 569-590) · airframe 26,247 hrs · 25,101 cycles

FLOOR SUPPORT LBL27, FS 569 - 590 HAS CORROSION AT FASTENER HOLE LOCATIONS. REMOVED DAMAGED PART AND INSTALLED IAW REO 601R-53-61-3778, SRM 51-42-21, 51-42-06.

Part: STRUCTURE — CRACKED (RT WING) · airframe 26,247 hrs · 25,101 cycles

RT WING L/E UPPER EDGING IS CRACKED ON OTBD SIDE. REMOVED UNSERVICEABLE EDGING & FABRICATED AND INSTALLED NEW SERVICEABLE EDGING.

Part: FLOOR SUPPORT — CORRODED (BS 589-621) · corrosion level 2 · airframe 26,247 hrs · 25,101 cycles

CARGO DOOR FLOOR SUPPORT HAS CORROSION AT NUT PLATES AND FASTENER HOLE LOCATIONS. REMOVED CORRODED SECTION AND SPLICED IN NEW SECTION IAW REO 601R-53-61-690, REV D.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 26,247 hrs · 25,101 cycles

LT INBD FLAP VANE L/E SKIN CHAFED. R & R IAW SRM 51-42-13.

Part: DRAG ANGLE — CRACKED · airframe 26,247 hrs · 25,101 cycles

CRACKED DRAG ANGLE. R & R DRAG ANGLE.

Part: MOUNT — CRACKED (HYD FILTER) · airframe 26,247 hrs · 25,101 cycles

HYD SYS NR 2 RETURN FILTER MOUNT IS CRACKED AT LOWER AFT CORNER NEAR FS 718 RT. REPAIRED IAW REO 601R-53-62-031, REV A.

Part: ANGLE — CRACKED (BS 484) · airframe 26,247 hrs · 25,101 cycles

ANGLE AT RBL 36 AT AFT FS 484 IS CRACKED. REMOVED CRACKED ANGLE, FABRICATED AND INSTALLED SERVICEABLE ANGLE IAW REO 601R-53-41-059, REV B.

Part: ANGLE — CRACKED (BS 484) · airframe 26,247 hrs · 25,101 cycles

ANGLE CRACKED AT FS 484, RBL 27, OTBD. REMOVED CRACKED ANGLE, FABRICATED AND INSTALLED SERVICEABLE ANGLE IAW SRM TR 53-30.

Part: STEP — CORRODED (PAX DOOR) · corrosion level 2 · airframe 26,247 hrs · 25,101 cycles

PAX DOOR TOP STEP PANEL 832ET CORRODED. REMOVED CORRODED MEMBER FROM STEP PANEL 832ET IAW SRM 51-42-06, FABRICATED REPAIR IAW SRM 51-24-16, INSTALLED REPAIR IAW SRM 51-42-06.

Part: STRUCTURE — CHAFED (BS 498-510) · airframe 21,687 hrs · 20,528 cycles

LOWER FUSELAGE UNDER EACH END OF FAIRING 193AB FWD WHEEL WELL HAS CHAFING DAMAGE. REPAIRED (BLEND) IAW REO 601R-57-21-880, REV C.

Part: RIB — CRACKED (RT WING) · airframe 21,687 hrs · 20,528 cycles

RT BATT RIB CRACKED. REPAIRED IAW REO 601R-57-51-552.

Part: STRUCTURE — CHAFED (MLG DOOR) · airframe 21,687 hrs · 20,528 cycles

RIGHT MLG DOOR L/E LOWER CORNER CHAFED. REPAIRED IAW REO 601R-52-82-016.

Part: POST — CRACKED (BS 409) · airframe 21,687 hrs · 20,528 cycles

LBL 18 OTBD SIDE OF POST AT FS 409.0 +128 CRACKED IN LOWER RADIUS. REPAIRED CRACK IAW REO 601R-53-41-056.

Part: BRACKET — CRACKED (PAX DOOR) · airframe 21,687 hrs · 20,528 cycles

PAX DOOR ASSIST MOTOR MOUNTING BRACKET CRACKED. R & R BRACKT IAW SRM 51-42-06.

Part: RIB — CRACKED (WS 53.60) · airframe 21,687 hrs · 20,528 cycles

LEFT BATTERY RIB CRACKED REPAIR IAW REO 601R-57-51-046.

Part: SILL — DENTED (PAX DOOR)

ADX PAX DOOR SILL DENTED ABOVE UPPER ROLLER. REPAIRED AFT PAX DOOR SILL IAW REO 601R-53-22-033.

Part: SPLICE — DAMAGED (HORIZONTAL STAB) · airframe 54,687 hrs · 20,528 cycles

2EA SCREWS HAVE HEADS DRILLED OFF AND STUCK IN NUTPLATES UNDER LT HORIZ STAB TIP. REMOVED UNSERVICEABLE SPLICE ON LT HORIZ STAB TIP AND INSTALLED SERVICEABLE STAB TIP IAW SRM 51-45-00 SRM 51-42-13 AND SRM 51-12-11.

Part: ANGLE — CRACKED (PAX DOOR HANDLE) · airframe 21,687 hrs · 20,528 cycles

CRACKED INNER ANGLE ON PAX DOOR HANDLE MOUNTING ASSY. REMOVED CRACKED INNER HANDLE THEN FABRICATED AND INSTALLED NEW ANGLE ON PAX DOOR HANLE MOUNTING ASSY.

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 21,687 hrs · 20,528 cycles

RT INBD FLAP VANE CHAFED IN 3 AREAS. REPAIRED IAW REO 601R-57-52-004.

Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 21,687 hrs · 20,528 cycles

LT FLAP VANE CHAFED IN 3 AREAS. REPAIRED IAW REO 601R-57-52-004.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 1 · airframe 21,687 hrs · 20,528 cycles

FUEL PANEL 650AB INBD FWD HAS CORROSION, COMPLIED WITH E06/021/452 AND REO 601R/57-21-030 TO BLEND AND REPAIR AREA.

Part: VENT — CHAFED (PAX DOOR) · airframe 21,687 hrs · 20,528 cycles

PAX DOOR VENT FLAP CHAFED FROM ICE BREAK CABLE. REPAIRED PAX DOOR VENT DOOR CHAFING IAW B/A REP 601R-52-11-1040.

Part: PANEL — CRACKED (PAX DOOR) · airframe 21,687 hrs · 20,528 cycles

PAX DOOR FWD STAIR SIDE PANEL CRACKED AT TOP OF 2ND STEP RISER CUTOUT CRACKED AREA THEN FABRICATED NEW SECTION THEN INSTALLED IAW SRM 601R-52-11-702, REV C.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 21,687 hrs · 20,528 cycles

PAX DOOR AFT DRAG ANGLE CRACKED AT PULLEY BRACKET MOUNT. REMOVED CRACKED SECTION OF AFT DRAG AND THEN INSTALLED NEW SERVICEABLE SECTION IAW REO 601R-52-11-513, REV A.

Part: HINGE — GOUGED (PAX DOOR) · airframe 21,687 hrs · 20,528 cycles

PASSENGER DOOR PIANO HINGE IN FUSELAGE SIDE IS GOUGED JUST AFT OF AFT LUB. BLENDED GOUGE IAW REO 601R-53-21-814 TYPE IV.

Part: PANEL — CHAFED (RT AILERON) · airframe 21,687 hrs · 20,528 cycles

RIGHT AILERON ACCESS PANEL 699CB IS CHAFED BY RUB SEAL. BLEND CHAFING IAW REO 601R-57-60-020.

Part: SKIN — CHAFED (RT AILERON) · airframe 21,687 hrs · 20,528 cycles

RIGHT AILERON L/E PANELS 699AB AND 699BB HAS CHAFING DAMAGE. BLENDED CHAFING IAW REO 601R-57-60-00.

Part: PANEL — MISSING (THRUST REVERSER) · airframe 20,916 hrs · 19,709 cycles

LT ENGINE LOWER STANG PANEL MISSING. PERFORMED EDDY CURRENT INSP ON LT LOWER STANG PANEL BRACKETS IAW NDTM PART 6-53-00-096, FOUND NO DEFECTS. INSTALLED LOWER ENGINE STANG PANEL.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 19,143 hrs · 17,826 cycles

REPAIR FUSELAGE DAMAGE BELOW CARGO DOOR. REPAIRED DAMAGE IAW REO 601R-53-61-3739.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 19,143 hrs · 17,826 cycles

EVALUATE DAMAGE BELOW CARGO DOOR. REPAIRED DAMAGE IAW REO 601R-53-61-3742.

Part: WIRE — BROKEN (STAB) · airframe 18,860 hrs · 17,534 cycles

STAB TRIM/ MACH TRIM DISENGAGED IN FLIGHT, COULD NOT RESET. CHANNEL A AND B OF HSTCU FAULT. COPILOTS DISCONNECT SWITCH FOUND BROKEN WIRE. REPAIRED WIRE IAW AMM 27-41-30. OPS CHECK GOOD.

Part: SENSING ELEMENT — DEFECTIVE (BLEED AIR SYS) · airframe 18,572 hrs · 17,238 cycles

ANTI-ICE DUCT WARNING MSG RECEIVED DURING FLIGHT WITH WING ANTI-ICE SELECTED ON SYNOPTIC SHOWED LT FUSE RED, ON GROUND. R & R FUSELAGE SENSING ELEMENT A15WK IAW AMM 36-21-04, PERFORMED OPS IAW 36-21-00. OPS CK GOOD.

Part: FLOOR SUPPORT — DAMAGED (BS 280-295) · airframe 17,031 hrs · 15,705 cycles

FLOOR SUPPORT FOUND WITH ELONGATED HOLE BTWN FS 280 AND FS 295 AT LBL 9. BEAM BTWN FS 280 TO FS 295 AT LBL 9 REPLACED IAW SRM 51-42-06. (K)

Part: A/C PACK — SMOKE (LEFT) · airframe 17,135 hrs · 15,815 cycles

(AT GATE) LT PACK STARTED RISING IN TEMP, WENT TO MANUAL AND CONTINUED RISING, SMOKE STARTED TO ENTER CABIN, SMOKE CLEARED WHEN PACK SELECTED OFF. MEL`D LT PACK. DRAINED AND SERVICED LT ACM IAW AMM 21-51-10, R &R LT COALSCER BAG OPS GOOD, REMOVED FROM MEL. (K)

Part: FRAME — CRACKED (BS 559) · airframe 17,031 hrs · 15,705 cycles

PRESSURE BULKHEAD LWR FRAME CAP ANGLE IS CRACKED IN THE RADIUS. FS 559.00, RBL 18. CRACK LENGTH .450 INCH PRESSURE BULKHEAD FS 559 LWR FRAME CAP REPAIRED IAW REO 601R-53-41-1046 (DEVIATION OF REO 601R53-41-260, REV C).

Part: ANGLE — CRACKED (BS 280) · airframe 17,031 hrs · 15,705 cycles

UPPER FWD ANGLE FS 280. LBL 9.5, WL 72.8 PREVIOUS REPAIR CRACKED LENGTH .500 INCH. UPPER FWD ANGLE AT FS 280 AND WL 72.8. REPLACED IAW SRM 51-42-06 AND 51-42-21. (K)

Part: FRAME — CRACKED (BS 559) · airframe 17,031 hrs · 15,705 cycles

PRESSURE BULKHEAD LWR FRAME CAP ANGLE IS CRACKED IN THE RADIUS FS 559, LBL 18.00, CRACK LENGTH IS .350 INCH. PRESSURE BULKHEAD LWR FRAME CAP LBL 18 ANGLE REPAIRED IAW REO 601R-53-41-260, REV C. (K)

Part: FRAME — CRACKED (BS 559) · airframe 17,031 hrs · 15,705 cycles

PRESSURE BULKHEAD LWR FRAME CAP ANGLE IS CRACKED IN THE RADIUS FS 559, LBL 18.00, CRACK LENGTH IS .350 INCH. PRESSURE BULKHEAD LOWER FRAME CAP LBL 18 ANGLE REPAIRED IAW REO 601R-53-41-260, REV C. (K)

Part: ATTACH FITTING — GOUGED (MLG DOOR) · airframe 17,031 hrs · 15,705 cycles

GOUGE ON RT MLG DOOR ATTACHED FITTING. GOUGE ON RT MLG DOOR ATTACHED FITTING REPAIRED IAW REO 601R-52-82-248. (K)

Part: FLOOR PANEL — CORRODED (CARGO BAY) · corrosion level 1 · airframe 17,031 hrs · 15,705 cycles

CORROSION ON 3 PLATES OF CARGO FLOOR STRUCTURE BTWN FS 574 TO FS 621 AND BTWN LBL 27 TO LT SILL. CORROSION REMOVED ON 3 PLATES IAW SRM 51-21-06. (K)

Part: FRAME — CORRODED (BS 349) · corrosion level 1 · airframe 17,031 hrs · 15,705 cycles

CORRODION ON FRAME FS 349 OUTER FLANGE BETWEEN STRINGER 26L AND 27. CORROSION REMOVED ON FRAME FS 349 IAW SRM 51-21-06. (K)

Part: PLATE — GOUGED (RT WING TE FLAP) · airframe 17,031 hrs · 15,705 cycles

RT WING INBD FLAP, INBD AFT HINGE LUG PLATES FOUND GOUGED (INBD .014 INCH DEEP, OTBD .007 INCH DEEP) LUG PLATES REPAIRED IAW REO 601R-57-52-1488. (K)

Part: FRAME — CORRODED (BS 349) · corrosion level 1 · airframe 17,031 hrs · 15,705 cycles

CORROSION ON FRAME FS 349.00 OUTER FLANGE BETWEEN STRINGER 26L AND STRINGER 27. CORROSION REMOVED ON FRAME FS 349.00 OUTER FLANGE BETWEEN STR 26L AND 27 IAW SRM 51-21-06. (K)

Part: ANGLE — CRACKED (BS 280) · airframe 17,031 hrs · 15,705 cycles

UPPER AFT ANGLE FS 280, LBL 11.00, WL 72.800 CRACKED. CRACK LENGTH .7 INCH REPAIRED IAW REO 601R-53-11-138 AND 601R-53-1774 AND SRM 53-51-59. (K)

Part: DOOR — CORRODED (SERVICE) · corrosion level 1 · airframe 17,031 hrs · 15,705 cycles

SERVICE DOOR, LOWER SECTION CORRODED NEAR FWD SPIGOT AND NEAR LOWER SPLICE, CORROSION REMOVED IAW SRM 51-21-06. (K)

Part: ANGLE — DAMAGED (BS 280) · airframe 17,031 hrs · 15,705 cycles

AT UPPER AFT ANGLE FS 280.00, LBL 11.00, WL 72.800, REPAIR PERFORMED IAW REO 601R-53-11-138, REV NC. (K)

Part: SILL — CORRODED (BS 574-621) · corrosion level 1 · airframe 17,031 hrs · 15,705 cycles

CORROSION FOUND ON LOWER FLOOR SILLS OF CARGO DOOR FS 574 TO FS 621. CORROSION REMOVED IAW SRM 51-21-06. (K)

Part: FLOORBEAM — CRACKED (BS 484) · airframe 17,031 hrs · 14,705 cycles

CLIP CRACKED AT FS 484.00 AND RBL 27.00 UNDER FLOOR CLIP FABRICATED AT FS484.00 AND RBL 27.00 UNDER FLOOR IAW SRM 51-24-21. NEW CLIP INSTALLED IAW REO 601R-53-41-059 REV A, RESTORE FINISH IAW SRM 51-21-16. (K)

Part: BULKHEAD — CRACKED (BS 621) · airframe 17,031 hrs · 15,705 cycles

AFT PRESSURE BULKHEAD WEB IS CRACKED ABOVE THE CARGO DOOR TRACK AT FS 621.00, LBL 27.50, WL 130.00 CRACK LENGTH IS .250 INCH. REPAIR ON AFT PRESSURE BULKHEAD WEB ABOVE CARGO DOOR TRACK IAW REO 601R-53-16-1541, REV B. (K)

Part: SILL — CORRODED (BS 574-621) · corrosion level 1 · airframe 17,031 hrs · 15,705 cycles

CORROSION FOUND ON LWR FLOOR SILLS OF CARGO DOOR FS 574 TO FS 621, CORROSION REMOVED IAW SRM 51-21-06. (K)

Part: INTERCOSTAL — CORRODED (BS 349-364) · corrosion level 1 · airframe 17,031 hrs · 15,705 cycles

CORROSION ON INTERCOSTAL BETWEEN FS 349.00 TO 364.00 AND BETWEEN STRINGER 26R TO 27 CORROSION ON INTERCOSTAL BETWEEN FS 349.00 TO 364.00 AND BETWEEN STRINGER 26R TO 27 REMOVED IAW SRM 51-21-06. (K)

Part: SKIN — GOUGED (RT WING) · airframe 17,031 hrs · 15,705 cycles

RT WING LWR PLANK FUEL TANK ACCESS DOOR CUTOUT 650EB EDGE OF FLANGE FOUND GOUGED. (DEPTH .012 INCH) NONE CRITICAL REGION. ACCESS DOOR CUTOUT 650EB REPAIRED IAW REO 601R-57-21-030, REV G. NON CRITICAL REGION. (K)

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 1 · airframe 17,031 hrs · 15,705 cycles

CORROSION FOUND AROUND FUEL ACCESS PANEL CUTOUT 640CB. (NON CRITICAL REGION) CORROSION REMOVED AROUND FUEL ACCESS PANEL CUT OUT 640CB (NON CRITICAL REGION) IAW REO 601R-57-21-030 REV G AND EO NR E06/021/457 REV A. (K)

Part: SKIN — CORRODED (RT WING) · corrosion level 1 · airframe 17,031 hrs · 15,705 cycles

CORROSION FOUND AROUND FUEL ACCESS PANEL CUT OUT 640DB (CRITICAL REGION). CORROSION REMOVED AROUND (CRITICAL REGION) FUEL ACCESS PANEL (640DB) IAW EO E06/021/457 AND REO 601R-57-21-030, REF G. (K)

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 17,031 hrs · 15,705 cycles

RT INBD FLAP VANE L/E FOUND CHAFED (3 AREAS) RT INBD FLAP VANE L/E REPAIRED IAW REO 601R-57-52-004, REV C. (K)

Part: BRACKET — CRACKED (FLAP FAIRING) · airframe 17,031 hrs · 15,705 cycles

BRACKET HOLDING RT WING, FLAP STUB FAIRING CRACK AT W/S 48.00 CRACK LENGTH .300 INCH BRACKET AT RT WING W/S 48.00 REPLACED IAW SRM 51-42-21. (K)

Part: FLOORBEAM — CRACKED (BS 484) · airframe 17,031 hrs · 15,705 cycles

FLOORBEAM FS 484.00, LBL 27.00 AND 36.00 FOUND CRACKED. FLOORBEAM AT FS 484.00, LBL 27.00 AND 36.00. REPAIRED IAW REO 601R-53-41-059, REV A. ANGLES FABRICATED FROM MATERIAL S6144A14. (K)

Part: BRACKET — GOUGED (LT WING TE FLAP) · airframe 17,031 hrs · 15,705 cycles

BRACKET HOLDING LT WING, FLAP STUP FAIRING GOUGED AT W/S 48.00 BRACKET REPLACED IAW SRM 51-42-21. (K)

Part: STRUCTURE — GOUGED (LT MLG WW) · airframe 17,031 hrs · 15,705 cycles

IN LT WHEEL WELL, SCREW HOLE OF CONNECTOR J189 GOUGED. SCREW HOLE OF CONNECTOR J189 REPAIRED IAW REO 601R-53-41-1040. (K)

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 17,031 hrs · 15,705 cycles

L/E LT INBD FLAP VANE CHAFED IN 3 PLACES. L/E OF LT INBD FLAP VANE. REPAIRED IAW REO 601R-57-52-004, REV C. (K)

Part: BULKHEAD — CRACKED (BS 280) · airframe 17,031 hrs · 15,705 cycles

RT PILOTS BULKHEAD FS 280.00, RBL 9.0 CRACKED (LOWER CROSSBEAM SECTION) RT PILOT BULKHEAD FS 280.00, RBL 9.0, REPAIRED C/O IAW REO 601R-53-11-171, REV D. (K)

Part: BULKHEAD — CRACKED (BS 202)

FS 202.75 AT LBL 23.71, PRESSURE BULKHEAD CRACKED AT PARKING BRAKE LOCATION 3 CRACKS: 1.00 INCH, 1.00 INCH, .500 INCH. REPAIR IAW REO 601R-53-11-1738 AND 601R-53-11-563. (K)

Part: PRESSURE BLKHD — CRACKED (BS 202) · airframe 17,031 hrs · 15,705 cycles

FS 202.75 AT LBL 23.71 PRESSURE BULKHEAD CRACKED AT PARKING BRAKE LOCATION, 3 CRACKS, 1.00 INCH, 1.00 INCH, .500 INCH. REPAIR IAW REO 601R-53-11-1738 AND 601R-53-11-563. (K)

Part: BULKHEAD — CRACKED (BS 280) · airframe 17,031 hrs · 15,705 cycles

RIGHT PILOTS BULKHEAD FS 280.00, RBL 9.0 CRACKED (LOWER CROSSBEAM SECTION) RT PILOT BULKHEAD FS 280.00, RBL 9.0 REPAIRED C/O IAW REO 601R-53-11-171, REV D. (K)

Part: BULKHEAD — CRACKED (BS 280) · airframe 17,031 hrs · 15,705 cycles

LEFT PILOTS BULKHEAD FS 280, LBL 9 CRACKED (LOWER CROSSBEAM SECTION) LENGTH .900 FT LT PILOTS BULKHEAD FS 280, LBL 9 REPAIRED IAW REO 601R53-11-171. (K)

Part: SWITCH — MALFUNCTIONED · airframe 13,552 hrs · 12,404 cycles

CAPTAIN ROLL SELECT SWITCH GREEN AND YELLOW LIGHTS INSPECTION WHEN SELECTED DO NOT RECEIVE "PILOT ROLL COMMAND" EICAS MESSAGE. FIRST OFFICERS ROLL SELECT SWITCH OPERATES NORMAL. (M)

Part: WARNING LIGHT — ILLUMINATED (AOA HEAT) · airframe 13,469 hrs · 12,356 cycles

RT AOA HEAT CAUTION MESSAGE ILLUMINATED IMMEDIATELY AFTER TAKEOFF. COMPLIED WITH QRH, MESSAGE DID NOT EXTINGUISH. PERFORMED AIR RETURN TO DEPARTURE. LANDED AT 46,900 LBS, BRAKE TEMPS 3-3-5-5. (K)

Part: BRACKET — CRACKED (RT MLG BAY)

RIGHT MLG WHEEL WELL HYDAULIC SUPPORT BRACKETS ARE CRACKED BETWEEN RBL 18 AND RBL 27. SUP - MAINTENANCE REMOVED AND REPLACED CRACKED BRACKETS AT RBL 18 TO RBL 27 IAW SRM 51-42-06. (M)

Part: BULKHEAD — CRACKED (BS 202)

FORWARD PRESSURE BULKHEAD AT FS 202.75 LOWER LT CORNER SKIN IS CRACKED AROUND BULKHEAD FITTING FOR RT INBOARD BRAKE LINE. MAINTENANCE CUT AWAY DAMAGED SECTION OF WEB AND INSTALLED REPAIR DOUBLE IAW BSC EO 601R-53-12837. (M)

Part: BULKHEAD — CRACKED (FUSELAGE)

REAR PRESSURE BULKHEAD WEB THAT SURROUNDS THE LINTEL ATTACHMENT FITTING HAS AN INDICATION NOTED APPROX .3 INCHES IN LENGTH FAILED NDT. MAINTENANCE REWORKED LINTEL INSTALLED BY CUTTING AWAY DAMAGED SECTION OF WEB AND INSTALLED REPAIR DOUBLER AND ANGLE IAW BOMBARDIER REO 601R-53-61-1230 REV D. (M)

Part: ANGLE — CRACKED (CARGO DOOR)

FOUND CARGO DOOR SUPPORT BEAM LOWER ANGLE TO REAR PRESSURE BULKHEAD CRACKED. SUP - REPLACED ANGLE IAW SRM 51-40-11 AND 51-42-21. (M)

Part: STEP — CRACKED (PAX DOOR)

PASSENGER DOOR TOP STEP EDGE MEMBER CRACKED. SUP - MAINTENANCE REPAIRED IAW REO NR 601R-52-11-279. (M)

Part: SKIN — CRACKED (PAX DOOR)

PASSENGER DOOR FORWARD SKIN IS CRACKED AT STEP 832CT. SUP - MAINTENANCCE REPAIRED IAW BSC EO 601R-52-12944. (M)

Part: SKIN — CRACKED (PAX DOOR)

PAX DOOR AFT STAIR SKIN CRACKED IN CORNER BETWEEN FIXED STEP AND MID STEP 832CT. SUP - MAINTENANCE REPAIRED AFT STAIR SKIN PANEL IAW REO 601R-52-11-702. (M)

Part: SKIN — CORRODED (RT WING)

RT LOWER WING PLANK ACCESS HOLE 650AB HAS MINOR PITTING CORROSION IN NON-CRITICAL AREA OUTBOARD SIDE OF CUTOUT ON LANDING. CORROSION AREA IS APPROX 2.5 INCHES IN LENGTH AND .2 INCHES WIDE CORROSION PITTING IS APPROX .004 INCH BY .006 INCH BY .008 INCH DEEP. MAINTENANCE PERFORMED A MAJOR REPAIR BY BLENDING MINOR PITTING CORROSION AFT RT LOWER WING PLANK ACCESS HOLE 650AB, WS 163, HOLE NR 9 IAW BOMBARDIER REO 601R-57-21-030 REV F. (M)

Part: BRACKET — CRACKED (LT MLG BAY)

LT MLG WHEEL WELL HYDRAULIC SUPPORT BRACKET BETWEEN LBL 18 AND LBL 27 IS CRACKED. SUP - MAINTENANCE REMOVED AND REPLACED CRACKED BRACKET IAW CRJ 200 SRM 51-42-06 DAMAGED WAS APPROX .5 INCH LONG. (M)

Part: FLOORBEAM — CRACKED (BS 484)

FOUND FS 484 FLOOR SUPPORT BEAM INTERCOSTAL ANGLE AT RBL 36 IS CRACKED. MAINTENANCE REPAIRED CRACKED ANGLE BY REMOVING CRACKED ANGLE AND FABRICATED NEW ANGLE AND INSTALLED SERVICEABLE ANGLE IAW BSC STANDARD REPAIR 601R-53-0030A AND REO 601R-53-41-059 REV A. (M)

Part: FLOORBEAM — CRACKED (BS 460)

FOUND FS 460 FLOORBEAM ANGLE AT RBL 9 IS CRACKED. MAINTENANCE REPAIRED FS 460 FLOORBEAM ANGLE AT RBL 9 BY REMOVING DAMAGED ANGLE AND INSTALLING NEW ANGLE IAW CRJ 200 SRM 51-42-06, 51-42-20, 51-42-21 AND BSC EO 601R-53-12916. (M)

Part: FLOORBEAM — CRACKED (BS 484)

FOUND FS 484 FLOORBEAM ANGLE AT LBL 36 IS CRACKED. MAINTENANCE REPAIRED ANGLE BY REMOVING CRACKED ANGLE, FABRICATING NEW ANGLE AND INSTALLING SERVICEABLE ANGLE IAW BSC STANDARD REPAIR 601R-53-0030A AND REO 601R-53-41-059 REV A. (M)

Part: STRINGER CLIP — CRACKED (BS 280)

FOUND FS 280 INBOARD AND OUTBOARD CLIPS AT RBL 9.0 ARE CRACKED. MAINTENANCE REMOVED AND REPLACED TWO 280 CLIPS IAW CRJ 200 SRM 51-42-21 AND 51-42-06. (M)

Part: STRINGER CLIP — CRACKED (BS 280)

FOUND FS 280 INBOARD AND OUTBOARD STRINGER CLIP AT LBL 9 ARE CRACKED. MAINTENANCE REMOVED AND REPLACED 280 STRINGER CLIP IAW CRJ 200 SRM 51-42-21 AND 51-42-06. (M)

Part: ANGLE — CRACKED (BS 621) · airframe 7,428 hrs · 6,525 cycles

LT FS621.0 FLOOR SUPPORT ANGLE HAS A 1 INCH CRACK. MAINTENANCE CUT OUT AND REMOVED DAMAGED ANGLE AT FS 621 LT FITTED AND DRILLED NEW ANGLES AND STRAP AND INSTALLED IAW REO. (K)

Part: FLOORBEAM — CRACKED (BS 621) · airframe 7,428 hrs · 6,525 cycles

RT FS 621.0 FLOOR SUPPORT ANGLE HAS A 1 INCH CRACK. CUT OUT AND REMOVED DAMAGED ANGLE. FITTED AND DRILLED UP NEW ANGLE AND STRAP, COUNTER SUNK HOLES. TREATED ALL REPAIR PARTS. INSTALLED PARTS AND PAINTED IAW REO. (K)

Part: INTERCOSTAL — CRACKED (BS 621-625.3)

LT FS 621-625.3 INTERCOSTAL AT STRINGER 14L IS CRACKED NEAR RADIUS APPROX 1 INCH LONG. (M)

Part: INTERCOSTAL — CRACKED (BS 621-625.3) · airframe 7,428 hrs · 6,525 cycles

RT FS621-625.3 INTERCOSTAL AT STR 14R IS CRACKED NEAR RADIUS APPROX 1.2 INCHES LONG. REMOVED CRACKED INTERCOSTAL AND INSTALLED NEW INTERCOSTAL IAW SRM. (K)

Part: FLANGE — CRACKED (BS 484) · airframe 7,656 hrs · 7,428 cycles

MWC 138, UNDERFLOOR INTERCOSTAL ATTACHED FLANGE IS CRACKED AT LBL 36, BS 484, WL73. REPAIRED UNDERFLOOR INTERCOSTAL AT LBL 36 IAW 601R-53-41-059 AND 601R-53-0030 BY CUTTING OUT CRACKED ANGLE AND INSTALLING REPAIR ANGLE. (K)

Part: HANDLE — FAILED (MLG)

LANDING GEAR DIDN'T RETRACT WHEN SELECTED UP. ANTI-SKID INBOARD AND PBSOV MESSAGE ILLUMINATED WITH GEAR SELECTED UP. REMOVED AND REPLACED LANDING GEAR CONTROL HANDLE IAW 32-30-00 JACKED AIRCRAFT, COMPLIED WITH GEAR SWING. NO DISCREPANCIES NOTED. OK FOR SERVICE. (M)

Part: TRIM SWITCH — STICKS (COCKPIT)

UNCOMMANDED STAB TRIM RUNAWAY. AUTOPILOT OFF, FIRST OFFICER FLYING. PILOT TRIM CLACKER OVERODE, OPS OK. FOUND FIRST OFFICERS TRIM SWITCH STICKING. REMOVED AND REPLACED SWITCH IAW 27-41-05. OPS CHECK GOOD. (M)

Part: BUSHING — LOOSE (LT MLG TRUNNION) · airframe 3,904 hrs · 3,406 cycles

LT MLG AFT TRUNNION BUSHING IS MIGRATED .058. REMOVED AND REPLACED LEFT MLG AFT TRUNNION BUSHING USING FIRST OVERSIZE BUSHING P/N 601R-5721003-21 IAW CRJ SB 601R-32-054 REV B PART B STEP 3A-3E. (M)

Part: BUSHING — LOOSE (LT MLG TRUNNION)

THE LEFT MLG AFT TRUNNION BUSHING IS MIGRATED .058. REMOVED MIGRATED BUSHING. REAMED TRUNNION BORE TO 1ST OVERSIZE AND INSTALLED 1ST OVERSIZE BUSHING P/N 601R5721003-21 IAW SERVICE BULLETIN 601R-32-054 REV B PART B STEP 3A THROUGH 3E. (M)

Part: CARBON SEAL — LEAKING (RT ENGINE)

IN FLIGHT RIGHT ENGINE OIL PRESSURE WARNING LIGHT ILLUMINATED. OIL PRESSURE FLUCTUATING BETWEEN 20-30 PSI. COMPLIED WITH QRH. ALL OTHER ENGINE INDICATIONS NORMAL. LANDED WITH RT ENGINE AT IDLE AT MCI. INSPECTED AND FOUND OIL COMING FROM GANG DRAIN. R & R ACCESS B AND F CARBON SEAL IAW GE 34 RJ SEI ENG MM. GROUND RAN ENGINE, NO LEAKS NOTED. (M)

Part: FIRE BOTTLE — DISCHARGED (NR 1 ENGINE)

FOUND FIRE BOTTLE EMPTY, REMOVED BOTTLE REMOVED AND REPLACED NR 1 ENGINE FIRE EXTINGUISHER CONTAINER IAW AMM 26-21-07. OPS CHECK GOOD. (M)

Part: BOTTLE — DISCHARGED (NR 2 FIRE)

ENGINE FIRE NR 2 LOW LOW PSI CAS MESSAGE. REMOVED AND REPLACED ENGINE NR 2 FIRE BOTTLE IAW 26-20, PERFORMED OPS TEST OF BOTTLE/SYSTEM. (M)

Part: BPSU — FAILED (T/E FLAP)

FLAP FAIL CAS MESSAGE FLAP FAIL AT ZERO DEGREES. NO FLAP LANDING. COMPLIED WITH QRH. REPLACED LEFT BPSU. OPS CHECK GOOD. (M)

Part: DOOR — LACK OF LUBE (PAX DOOR)

PASSENGER ENTRY DOOR JAMBED CLOSED. MAINTENANCE LUBED LOWER DOOR CAMS AND REPOSITIONED AIRCRAFT TO RELIEVE DOOR FRAME STRESS.