N408AW

Part: NONE — NONE · airframe 43,348 hrs · 41,355 cycles

RIGHT ENGINE OIL PRESSURE WENT TO 0 PSI DURING DECENT PLUS RIGHT ENGINE PRESSURE WARN. RAN QRH. RIGHT ENGINE FAILED SHORTLY AFTER WHILE RUNNING SINGLE ENGINE QRH. AFTER OIL WARNING, RAN QRH, AFTER APPROXIMATELY 3 MINUTES ENGINE SHUT DOWN WITH VIBE ON OWN ****AIRCRAFT REMOVED FROM SERVICE *****

Part: WIRE HARNESS — DAMAGED (NLG) · airframe 41,756 hrs · 39,778 cycles

APPROX 6 SEC AFTER SELECTING GEAR UP RECEIVED GEAR DISAGREE AND NOSE DOOR MSGS WITH ASSOCIATED AURAL WARNINGS. HYD TEMP AND QTY AND PRESURE WERE NORMAL. CW QRH. TURNED ON 2B AND 3B ACMPS- NO CHNAGE. PULLED EMERG GEAR RELEASE PER QRH AND SELECTED GEAR HANDLE DOWN. GEAR EXTENDED AND LOCKED DOWN. LANDING WEIGHT 46700 LBS. ***AIRCRAFT REMOVED FROM SERVICE*** C/W M ACTION ON MEL 32-30-01 LANDING GEAR RETRACTIONS SYSTEM PLACARDED AND PLACED ON MEL; REMOVED AND REPLACED NLG CENTERING SENSOR BRACKET IN REF TO CMM 32-20-04R15 REMOVED AND REPLACED NLG #2 WOW HARNESS IAW AMM SUPP 12-029E OPS TEST GOOD REF ALSO DAY WO 302588. REMOVED PLACARD & REMOVED FROM MEL

Part: RVDT — OUT OF RIG (NLG STEERING) · airframe 41,752 hrs · 39,773 cycles

STEEERING INOP CAUTION MSG IN FLT. RESET SW FROM ARMED TO OFF TO ARMED PER QRH MSG REMAINED. GEAR WAS UP. EXTENDED GEAR ANDED WITHOUT INCIDENT ATTEMPTED SW RESET AGAIN NO FIX. TAXIED TO GATE WITH BRAKES AND THROTTLES. CW FIM FAULT RESET WITH CB RESET NO FIX. STEERR INOP MSG REAPEARS AND THERE IS NO AUDIBLE CLUNK WITH #3 HYD PRESURED ***AIRCRAFT REMOVED FROM SERVICE*** INSP AND FOUND RH RVDT OUT OF RIG, R&R RH RVDT IAW AMM 32-50 OPS CHECK GOOD.

Part: SKIN — DAMAGED (HORIZONTAL STAB) · airframe 40,114 hrs · 38,143 cycles

LEFT H-STAB UPPER SKIN AFT EDGE IS BENT AND HAS A FASTENER PULLED THROUGH THE SKIN AT BL 72.0. REPAIRED

Part: SUPPORT FITTING — WORN (LT WING TE FLAP) · airframe 40,114 hrs · 38,143 cycles

LH OB FLAP OB VANE SUPPORT FITTING IS WORN. REPLACED

Part: SKIN — GOUGED (BS 559) · airframe 40,114 hrs · 38,143 cycles

FUSELAGE OUTER SKIN AT FS 559+112 BETWEEN STR 11 AND 12 R HAS A SCRIBE LINE NEAR RIVET. REPAIRED.

Part: ANGLE — CORRODED (BS 310-349) · corrosion level 2 · airframe 40,114 hrs · 38,143 cycles

PAX DOOR SURROUND STRUCTURE LOWER SILL ANGLE CORRODED. REPLACED.

Part: FRAME — CRACKED (BS 333) · airframe 40,114 hrs · 38,143 cycles

FS 333 FRAME CRACKED AT STRINGER 1R REPAIRED

Part: SKIN PANEL — CRACKED (FUSELAGE) · airframe 40,114 hrs · 38,143 cycles

LEFT TRU SKIN PNL CRACKED AT THE AFT LATCH. REPAIRED SKIN IAW SUPP. 19-016B.

Part: SUPPORT FITTING — WORN (LT WING TE FLAP) · airframe 40,114 hrs · 38,143 cycles

LH OB FLAP CTR VANE SUPPORT FITTING IS WORN. REPLACED.

Part: SKIN — CRACKED (FUSELAGE) · airframe 40,114 hrs · 38,143 cycles

RIGHT TRU SKIN PANEL HAS A CRACK ON AFT LATCH. REPAIRED SKIN IAW AWAC SUPP. 19-226.

Part: SEAT TRACK — CORRODED (BS 399-409) · corrosion level 2 · airframe 40,114 hrs · 38,143 cycles

RH FLOOR SEAT TRACK STICK 2 CORRODED. REPLACED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,114 hrs · 38,143 cycles

LT FLOOR SEAT TRACK #2 HAS CORROSION. REMOVED AND REPLACED LT FLOOR SEAT TRACK STICK 2 IAW AMM 53-01-11.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,114 hrs · 38,143 cycles

FRAME 605.00 CORRODED AT STR 21L TO 21R. REPLACED LOWER FRAME 605.00 IAW SRM 51-42-06, 51-42-21.

Part: PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 40,114 hrs · 38,143 cycles

RIGHT WING PNL 640AT FRETTED. REPLACED PNL 640AT IAW SRM 51-24-36, TR 51-42.

Part: PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 40,114 hrs · 38,143 cycles

RIGHT WING PNL 640CT FRETTED. REPLACED PNL 640CT IAW SRM 51-24-36 & TR 51-42.

Part: PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 40,114 hrs · 38,143 cycles

LEFT WING PNL 540CT FRETTED. REPLACED PNL 540CT IAW SRM TR 51-42, 51-24-36.

Part: PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 40,114 hrs · 38,143 cycles

RIGHT WING PNL 640BT FRETTED. REPLACED PNL 640BT IAW SRM 51-24-36, TR 51-42.

Part: PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 40,114 hrs · 38,143 cycles

LEFT WING PNL 540AT FRETTED. REPLACED PANEL 540AT IAW SRM 51-24-36, TR 51-42.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,114 hrs · 38,143 cycles

RIGHT FLOOR SILL CORRODED AT FS 562.00 TO 595.00. REPAIRED FLOOR SILL IAW EA# AWAC-CRJ 253-01295 AND AWAC-CRJ253-01296.

Part: ATTACH ANGLE — CRACKED (CARGO DOOR) · airframe 40,114 hrs · 38,143 cycles

CARGO DOOR BEAM MEMBER FWD LOWER ATTACH ANGLE CRACKED. REPLACED ANGLE IAW SRM 51-42-21.

Part: ATTACH BRACKET — CRACKED (FUSELAGE) · airframe 40,114 hrs · 38,143 cycles

A/C POWER SERVICE PANEL LOWER ATTACH BRACKET IS CRACKED. REPLACED BRACKET IAW SRM 51-42-06.

Part: CROSSBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,114 hrs · 38,143 cycles

FS 349 CROSSBEAM CORRODED AT RBL43. REPAIRED FS349 CROSSBEAM IAW REO601R-53-21-2745 REV--.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 40,114 hrs · 38,143 cycles

REAR PRESSURE BULKHEAD STR 14L OBLIQUE ANGLE IS CRACKED. REPLACED ANGLE IAW SRM 51-42-21.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 40,114 hrs · 38,143 cycles

LEFT WINDSHIELD SIDE LOWER SIDE POST ATTACH FITTING CRACKED. REPLACED FITTING IAW SRM 51-42-21.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 40,114 hrs · 38,143 cycles

RIGHT WINDSHIELD SIDE POST LOWER ATTACH FITTING CRACKED. REPLACED FITTING IAW SRM 51-42-21.

Part: CHANNEL — CRACKED (CARGO DOOR) · airframe 40,114 hrs · 38,143 cycles

CARGO DOOR FWD TRACK LOWER U CHANNEL IS CRACKED. REPLACED CHANNEL IAW SRM 515-42-06.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 40,114 hrs · 38,143 cycles

AFT CARGO FLOOR TRACK AT FS559+86 TO FS 559+95 LBL9 CORRODED. REPLACED FITTING IAW SRM 51-42-21.

Part: SKIN — CRACKED (RT WING) · airframe 40,114 hrs · 38,143 cycles

RT WING T/E PANEL 594PB LANDING IS CRACKED AND GOUGED. REPAIRED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,114 hrs · 38,143 cycles

LT SIDEWALL SEAT RAIL STICK 1 CORRODED. REPLACED.

Part: RECEPTACLE — CORRODED (CABIN) · corrosion level 2 · airframe 40,114 hrs · 38,143 cycles

PAX DOOR LOWER SILL ANGLE AFT RECESSED CANNON PLUG RECEPTACLE STRUCTURE CORRODED. REPLACED.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,114 hrs · 38,143 cycles

PASSENGER DOOR LOWER SILL ANGLE CORRODED. REPLACED PAX DOOR LOWER SILL ANGLE IAW SRM 51-42-06.

Part: CLEAT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,114 hrs · 38,143 cycles

PASSENGER DOOR LOWER SILL FWD CLEAT CORRODED. REPLACED CLEAT IAW SRM 51-42-06, 53-21-23.

Part: RECEPTACLE — CORRODED (CABIN) · corrosion level 2 · airframe 40,114 hrs · 38,143 cycles

PAX DOOR LOWER SILL ANGLE FORWARD RECESSED CONNECTOR RECEPTACLE STRUCTURE CORRODED. REPLACED.

Part: POST — CRACKED (FUSELAGE) · airframe 40,114 hrs · 38,143 cycles

FS409+128 VERTICAL POST AT BL0 IS CRACKED IN THE AFT RADIUS ON THE RIGHT HAND SIDE OF POST, WL64.

Part: SKIN — CHAFED (TE FLAP VANE) · airframe 40,114 hrs · 38,143 cycles

LEFT HAND I/B FLAP VANE CENTER LEADING EDGE CHAFED. REPLACED CENTER LEADING EDGE IAW SRM 51-42-13.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,114 hrs · 38,143 cycles

LT FLOOR SEAT TRACK STICK 1 HAS CORROSION. REPLACED.

Part: ATTACH BRACKET — CRACKED (FAIRING) · airframe 40,114 hrs · 38,143 cycles

FS 469 RBL 47 FAIRING ATTACH BRACKET CRACKED. REPLACED.

Part: ATTACH BRACKET — CRACKED (FAIRING) · airframe 40,114 hrs · 38,143 cycles

FS 449.85 RBL 47 FAIRING ATTACH BRACKET CRACKED. REPLACED.

Part: ATTACH BRACKET — CRACKED (FUSELAGE) · airframe 40,114 hrs · 38,143 cycles

FS 461 RBL 47 ATTACH BRACKET CRACKED. REPLACED.

Part: ATTACH BRACKET — CRACKED (FAIRING) · airframe 40,114 hrs · 38,143 cycles

FS 449.85 LBL 47 FAIRING ATTACH BRACKET CRACKED. REPLACED.

Part: ATTACH BRACKET — CRACKED (FAIRING) · airframe 40,114 hrs · 38,143 cycles

FS 469 LBL 47 FAIRING ATTACH BRACKET CRACKED. REPLACED.

Part: ATTACH BRACKET — CRACKED (FAIRING) · airframe 40,114 hrs · 38,143 cycles

FS 477 LBL 47 FAIRING ATTACH BRACKET CRACKED. REPLACED.

Part: STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,114 hrs · 38,143 cycles

PRESSURE FLOOR SUPPORT STRAP CORRODED. REPLACED FLOOR SUPPORT STRAP IAW SRM 53-41-43. 51-42-06.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,114 hrs · 38,143 cycles

LEFT FLOOR SEAT TRACK #4 CORRODED. REPLACED LEFT FLOOR SEAT TRACK #4 IAW SRM 51-40-11, TR51-42 AND AMM 53-01-11.

Part: FITTING — CRACKED (FUSELAGE) · airframe 40,114 hrs · 38,143 cycles

FS484.00, LBL27, O/B CLIP IS CRACKED. REPAIRED CLIP IAW SRM 51-42-21 AND REO 601R-53-41-059 REV-B.

Part: FITTING — CRACKED (FUSELAGE) · airframe 40,114 hrs · 38,143 cycles

FS484.00, RBL 27, O/B CLIP IS CRACKED. REPLACED CLIP IAW SRM 51-42-21 AND REO 601R-52-41-059 REV-B.

Part: WARNING MESSAGE — ILLUMINATED (NLG) · airframe 40,078 hrs · 38,109 cycles

AFTER TAKEOFF AND AFTER GEAR SELECTED UP RECEIVED GEAR DISAGREE WARNING MESSAGE. GEAR INDICATIONS SHOWED NOSE GEAR DOWN AND MAINS UP. NOSE DOOR OPEN WARNING MESSAGE ALSO DISPLAYED. FOLLOWED QRH PROCEEDURE WITH EMERGENCY GEAR EXTENSIONHANDLE PULLED. LANDED UNEVENTFUL

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 39,681 hrs · 37,723 cycles

CRACK ON AFT PRESSURE BULKHEAD FWD FACE FS 621 WL 101 LBL 27.5.

Part: STRUT — NOT REPORTED (NLG) · airframe 37,693 hrs · 35,744 cycles

ON GEAR RETRACTION RECEIVED GEAR DISAGREE WARNING, NOSE DOOR WARNING, AND WOW INPUT CAUTION. NOSE GEAR DOWN AND LOCKED INDICATION. R&R NLG SHOCK STRUT ASSY IAW AMM 32-21 & MX TASK CM SUPP 12-072, OPS, LEAK AND RIG CHECK GOOD.

Part: STRUT — DEFECTIVE (NLG) · airframe 37,693 hrs · 35,744 cycles

ON GEAR RETRACTION RECEIVED GEAR DISAGREE WARNING, NOSE DOOR WARNING, AND WOW INPUT CAUTION. NOSE GEAR DOWN AND LOCKED INDICATION. R&R NLG SHOCK STRUT ASSY IAW AMM 32-21 & MX TASK CM SUPP 12-072, OPS, LEAK AND RIG CHECK GOOD.

Part: STRUT — LOW (NLG) · airframe 37,673 hrs · 35,727 cycles

RECEIVED GEAR DISAGREE WARNING AFTER T/O. LT AND RT MLG SHOWED UP, NLG DOWN AFTER GEAR HANDLE SELECTED UP. ALSO RECEIVED STEERING INOP CAUTION, WOW INPUT, NOSE DOOR WARNING, AND WOW OUTPUT FAIL STATUS. C/W QRH, MANUALLY EXTENDED GEAR. MANUAL RELEASE HANDLE WOULD NOT STOW. RECEIVED THREE GREEN AND RETURNED TO ORD. AFTER CLEARING RUNWAY RECEIVED HYD 3 HIGH TEMP. SELECTED 3A AND 3B OFF. TEMPS RETURNED TO NORMAL. INSPECTED ALL PROX SENSORS, WIRING AND BRACKETS NO DEFECTS NOTED. C/W NLG STRUT OIL/NITROGEN SERVICE IAW AMM 12-12-32. PERFORMED GEAR SWING.

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 36,919 hrs · 34,936 cycles

RT WING INBD FLAP LOWER SKIN HAS TWO DENTS IN THE INBD LOWER CORNER.

Part: SHROUD — CRACKED (RT WING) · airframe 36,919 hrs · 34,936 cycles

RIGHT WING OTBD SHROUD CRACKED ON OTBD LEADING EDGE. REPLACED THE SHROUD IAW SRM 51-40-11, AND 51-42-13.

Part: FITTING — CRACKED · airframe 36,919 hrs · 34,936 cycles

WINDSCREEN CENTER POST LOWER RT FITTING IS CRACKED. REPLACED FITTING IAW SRM 51-42-21.

Part: CARGO TRACK — CORRODED (BS 559) · corrosion level 2 · airframe 36,919 hrs · 34,936 cycles

1014536-1600-0016 - CARGO TRACK CORRODED AT BS 559+112, RBL 9

Part: ANGLE — CRACKED (BS 621 BULKHEAD) · airframe 36,919 hrs · 34,936 cycles

AFT ACCESSORY COMPARTMENT, REAR PRESSURE BULKHEAD AT BS 621 LBL 36.2, THIRD INTERCOSTAL ANGLE FROM THE TOP IS CRACKED

Part: FLOOR SUPPORT — CORRODED (BS 574-621) · corrosion level 2 · airframe 36,919 hrs · 34,936 cycles

AFT CARGO FLOOR SUPPORT CORRODED AT BS 574 TO 621.00, LBL 47. REPLACED THE FLOOR SUPPORT IAW SRM 51-42-06, AND REO 601R-53-61-593, REV-A,

Part: HANDLE — LACK OF LUBE (SERVICE DOOR) · airframe 32,297 hrs · 30,586 cycles

SERVICE DOOR OUTER HANDLE WILL NOT OPEN. LUBED & CLEANED IAW SUPP 10-054C SERVICE DOOR OUTER HANDLE. OPERATIONS CHECKED GOOD. ADDITIONAL CORRECTIVE ACTION. R & R SERVICE DOOR HANDLE ASSEMBLY IAW AMM 52. OPERATIONS CHECKED GOOD SN OFF 0649 & SN ON 0806 DMB.

Part: HANDLE — STUCK (SERVICE DOOR) · airframe 34,594 hrs · 32,794 cycles

SERVICE DOOR WILL NOT OPEN FROM OUTSIDE, HANDLE WILL NOT COME OUT.

Part: HOUSING — DAMAGED (SERVICE DOOR) · airframe 34,546 hrs · 32,746 cycles

SERVICE DOOR OUTER HANDLE WILL NOT RELEASE. PLACARDED & PLACED ON MEL. REPAIRED HANDLE HOUSING IAW CMM 52-41-03. ADJUSTED HANDLE TENSION IAW AMM 52-41-03. ALL CHECKED GOOD REMOVED PLACARD & MEL.

Part: HANDLE — DIRTY (SERVICE DOOR) · airframe 33,092 hrs · 31,380 cycles

SERVICE DOOR WILL NOT OPEN FROM OUTSIDE. CLEANED & LUBRICATED SERVICE DOOR OUTER HANDLE IAW SUPP 11-029B. OPERATIONS CHECKED GOOD. OUTER HANDLE FUNCTIONS NORMALLY, NO DEFECTS.

Part: ATTACH ANGLE — CRACKED (LT WING) · airframe 32,300 hrs · 30,588 cycles

LT CTR LE ATTACH ANGLE & OVER SUPPORT AT TRANSITION SPLICE CRACKED IN RADIUS.

Part: SKIN — CHAFED (RT AILERON) · airframe 32,300 hrs · 30,588 cycles

RIGHT AILERON UPPER LE SKIN CHAFED.

Part: FRAME — CORRODED (BS 333) · corrosion level 2 · airframe 32,300 hrs · 30,588 cycles

FWD & AFT SIDES OF FRAME AT FS 333.00 & STRINGER 24L TO 24R CORRODED.

Part: POST — CRACKED (FUSELAGE) · airframe 32,300 hrs · 30,588 cycles

FS 409+128 BULKHEAD VERTICAL POST AT RBL 27 IS CRACKED AT LOWER END RADIUS.

Part: BRACKET — CRACKED (CARGO DOOR) · airframe 32,300 hrs · 30,588 cycles

BRACKET ON BOTTOM OF CARGO DOOR FWD TRACK IS CRACKED.

Part: FITTING — CRACKED (FUSELAGE) · airframe 32,300 hrs · 30,588 cycles

FS 280.00, STRINGER 3L, CLIPS & SUPPORT CLIP ARE CRACKED.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,300 hrs · 30,588 cycles

SERVICE DOOR FLOOR SILL CORRODED.

Part: SPOILER — CHAFED (RT WING) · airframe 32,300 hrs · 30,588 cycles

RT FLIGHT SPOILER CHAFED AT LE NEAR CTR HINGE.

Part: MOUNT — CHAFED (RT ENGINE) · airframe 32,300 hrs · 30,588 cycles

RT ENG REAR MOUNT FLANGE CHAFED ON OTBD SIDE FROM CORE COWL.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 32,300 hrs · 30,588 cycles

RT OBLIQUE ANGLE INTERCOSTAL CRACKED FS 621 - 625.

Part: DOUBLER — CHAFED (FUSELAGE) · airframe 32,300 hrs · 30,588 cycles

PREVIOUS REPAIR DOUBLER ON RT FS 280 BULKHEAD CHAFED.

Part: FITTING — CRACKED (FUSELAGE) · airframe 32,300 hrs · 30,588 cycles

LEFT FS 484 CLIP CRACKED AT BL 36.

Part: SKIN — DENTED (FUSELAGE) · airframe 32,300 hrs · 30,588 cycles

AFT LOWER FUSELAGE SKIN HAS A PROTRUDING DENT FWD OF FS 682.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,300 hrs · 30,588 cycles

RIGHT FLOOR SILL CORRODED AT FS 319.

Part: FRAME — CHAFED (FUSELAGE) · airframe 32,300 hrs · 30,588 cycles

FRAME FS 559+48 NEXT TO STRINGER 7R HAS CHAFE DAMAGE.

Part: CLEAT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,300 hrs · 30,588 cycles

PAX DOOR FLOOR SILL CLEATS CORRODED, AFT CLEAT BEYOND LIMITS.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 31,885 hrs · 30,174 cycles

EMERGENCY LIGHTS INOPERATIVE FROM ROW 2 - 5 & LT OVERWING. R & R NR 2 INVERTER IAW AMM 33-51-07. OPS CHECKED GOOD.

Part: SENSOR — ICED (NLG STEERING) · airframe 31,768 hrs · 30,062 cycles

AFTER TAKEOFF RECEIVED WOW INPUT FOLLOWED BY NLG STEERING INOPERATIVE CAUTION MSG. MSG APPEARED APPROX 28 SEC AFTER GEAR RETRACTION, NORMAL EXTENSION & DECLARED AN EMER. QRH DIDN'T CLEAR IMMEDIATE. CLEARED ON ITS OWN AFTER A FEW MIN. INTERROGATED PSEU & FOUND CODE S11FAR, FOUND PROX SENSOR PS4GA COATED WITH ICE. REMOVED ICE FROM SENSOR & PERFORMED BITE CHECK OF PSEU IAW AMM 32-61-00, NO FAULTS FOUND. PERFORMED OPS CHECK OF NWS IAW AMM 32-51. OPS CHECKED GOOD.

Part: WARNING MESSAGE — ILLUMINATED (NLG) · airframe 31,653 hrs · 29,955 cycles

AFTER TAKEOFF WHEN GEAR WAS RETRACTED, NLG DISAGREE MSG DISPLAYED AFTER 28 SECS.

Part: LIGHT — ODOR (CABIN) · airframe 28,017 hrs · 26,395 cycles

LEFT 14TH DUCT FAILS DUCT TEST. ANIT-ICE PAGE SHOWS DARK-DUCT FROM LEFT VALVE TO LEFT COWL. TEST CAUSES STRONG BURNING ODOR. TROUBLESHOT AND FOUND CONNECTOR P83WK WIRE DISCONNECTED, R&R'D CONNECTOR P83WK PER ESPM 20-17-11 AND PERFORMED OPS CK PER AMM 36-21-00, OPS CHECKED GOOD. FOUND STRONG BURNING ODOR COMING FROM ABOVE SEATS 2 AND 3. FOUND BULBS TO BE OLD AND OVERHEATING CAUSING CEILING PANEL TO PRODUCE ODOR. REMOVED BULBS FROM ABOVE ROWS 2 AND 3.

Part: CONNECTOR — DAMAGED (ANTI ICE SYS) · airframe 28,017 hrs · 26,395 cycles

LEFT 14TH DUCT FAILS DUCT TEST. ANIT-ICE PAGE SHOWS DARK-DUCT FROM LEFT VALVE TO LEFT COWL. TEST CAUSES STRONG BURNING ODOR. TROUBLESHOT AND FOUND CONNECTOR P83WK WIRE DISCONNECTED, R & R CONNECTOR P83WK PER ESPM 20-17-11 AND PERFORMED OPS CK PER AMM 36-21-00, OPS CHECKED GOOD. TROUBLESHOT AND FOUND STRONG BURNING ODOR COMING FROM ABOVE SEATS 2 AND 3. FOUND BULBS TO BE OLD AND OVERHEATING CAUSING CEILING PANEL TO PRODUCE ODOR. REMOVED BULBS FROM ABOVE ROWS 2 AND 3.

Part: PANEL — DAMAGED (TE FLAP) · airframe 27,977 hrs · 26,352 cycles

LEFT FLAP PANEL 584AB HAS 1 EA ELONGATED FASTENER HOLE TOP RB CORNER. REMOVED ELONGATED HOLE AND INSTALLED FREEZE PLUG, PN 05-2013-056 IAW SRM 57-52-00-02.

Part: SKIN — DAMAGED (RT ELEVATOR) · airframe 27,977 hrs · 26,352 cycles

RT ELEVATOR UPPER L/E IS BENT UP IN THREE PLACES OVER HINGE AND HORIZONAL STAB AERODYNAMIC SEAL DAMAGED. REPAIRED ELEVATOR L/E IAW REO 601R-55-21-112. REPAIRED HORIZ STAB AERODYNAMICAL SEAL IAW REO 601R-55-12-531.

Part: FLOOR SUPPORT — CORRODED (BS 569-621) · airframe 27,977 hrs · 26,352 cycles

CARGO BAY FLOOR SUPPORT CAP AT LBL 27 BS 569-621 IS CORRODED AROUND FASTENER HOLE LOCATIONS. REMOVE DAMAGED CAP AND INSTALLED DUPLICATED FLOOR SUPPORT CAP IAW SRM 51-42-06, 51-42-21, 51-25-16, 51-25-06, 51-40-11, & 51-21-11.

Part: FRAME — CHAFED (BS 718) · airframe 27,977 hrs · 26,352 cycles

LEFT BS 718 BETWEEN S16-17L FRAME WAS CHAFED BY ACMP RETURN LINE. REMOVED DAMAGED AREA OF FRAME AND INSTALLED A REPAIR DOUBLER IAW EA 24-2013-190.

Part: DRAG BRACE — CRACKED (LT MLG) · airframe 27,977 hrs · 26,352 cycles

LT MLG DRAG BRACE ON T/B BATT RIB IS CRACKED. REPLACE PART.

Part: ANGLE — CRACKED (RT WING) · airframe 27,977 hrs · 26,352 cycles

RIGHT WING L/E ANGLE AT WS 148 CRACKED UPPER OUTBD CORNER. R & R IAW SRM 51-24-16 & 51-42-06.

Part: SKIN — CHAFED (RT AILERON) · airframe 27,977 hrs · 26,352 cycles

RIGHT AILERION UPPER SHROUND SKIN IS CHAFED BEYOND REPAIRABLE. REMOVED AND INSTALLED NEW SERVICEABLE SKIN IAW SRM 51-25-06, 51-25-16, 51-23-00, 51-40-11, 51-42-06, 51-42-13 AND STS EA 15-2013-330 & SUP 13-055.

Part: SKIN — CHAFED (TE FLAP) · airframe 27,977 hrs · 26,352 cycles

TE FLAP SKIN PANEL 594PB CHAFED. R & R SKIN IAW SRM 51-40-11 AND 51-42-06.

Part: SEAL — GOUGED (EXAHAUST) · airframe 27,977 hrs · 26,352 cycles

RT JET PIPE FAIRING UPPER SEAL WORN AND STIFFENER GOUGED WITH HOLE PUNCTURE. R & R SEAL AND STIFFENER IAW CMM 78-11-00, SRS 0910,78-11-00, SRS 070, 20-40-11, 20-42-06, 20-23-00, 20-25-06.

Part: STEP — CORRODED (BS 307-349) · corrosion level 2 · airframe 27,977 hrs · 26,352 cycles

PAX DOOR TOP STEP NR 832 ET HAS CORROSION AROUND ALL FASTENER HOLE LOCATIONS OF HINGE ASSY. REPLACED CORRODED HINGE ASSY OF PAX DOOR STEP NR 832ET IAW SRM 51-40-11.

Part: CLEAT — CORRODED (PAX DOOR) · corrosion level 2 · airframe 27,977 hrs · 26,352 cycles

PAX DOOR CLEAT CORRODED. R & R CLEAT & BRACKET IAW SRM 51-21-06 & 51-42-06.

Part: FLOOR SUPPORT — CORRODED (BS 559) · corrosion level 2 · airframe 27,977 hrs · 26,352 cycles

RIGHT FLOOR SUPPORT IS CORRODED AT FS 559+92 TO UNALLOWABLE LIMITS. R & R FLOOR SUPPORT.

Part: STIFFENER — CRACKED (RT WING) · airframe 27,977 hrs · 26,352 cycles

RIGHT MLG UPPER WING SKIN STIFFENER IS CRACKED. R & R WITH NEW PN 600-10389-2 IAW SRM 51-21-11, 51-25-06, 51-25-16, 51-42-11, 51-42-21.

Part: VANE — CHAFED (TE FLAP) · airframe 27,977 hrs · 26,352 cycles

CHAFE TO L/T INBD FLAP VANE UPPER SKIN T/E AT WS 55.49. BLENDED IAW REO 601R-57-52-2028.

Part: MOUNT — CRACKED (BS 529) · airframe 27,977 hrs · 26,352 cycles

RIGHT BRAKE HYD FUSE MOUNT IS CRACKED IN THE RT WHEEL WELL. REMOVED UNSERVICEABLE FUSE MOUNT AND REPLACED WITH NEW SERVICEABLE RT FUSE MOUNT IAW SRM 51-42-06.

Part: CARGO TRACK — CORRODED (BS 559) · corrosion level 2 · airframe 27,977 hrs · 26,352 cycles

CARGO TRACK IS CORRODED AT RBL 27 AT BS 559+86 TO 559+96. R & R CARGO TRACK IAW SRM 51-41-02 AND 51-40-11.

Part: MOUNT BRACKET — BENT (BS 700-705) · airframe 27,977 hrs · 26,352 cycles

NR 2 HYD ECO BOTTLE MOUNT IS BENT AND CRACKED ON UPPER FWD R/B CORNER. REMOVE, DUPLICATE AND INSTALL MOUNT WEB BRACKET.

Part: SEAT TRACK — CORRODED (BS 409) · corrosion level 2 · airframe 27,977 hrs · 26,352 cycles

CORROSION ON LT SEAT TRACK FS 409+48. R & R SEAT TRACK IAW 51-41-02.

Part: ANGLE — CRACKED (BS 621-625) · airframe 27,977 hrs · 26,352 cycles

LT ANGLE IS CRACKED. R & R.

Part: ANGLE — CRACKED (BS 621-625) · airframe 27,977 hrs · 26,352 cycles

RT ANGLE IS CRACKED, R & R.

Part: CARGO TRACK — CORRODED (BS 559-574) · corrosion level 2 · airframe 27,977 hrs · 26,352 cycles

CARGO TRACK IS CORRODED AT RBL9 AND BS 559+112 TO 574. R & R WITH SERVICEABLE CARGO TRACK.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 27,977 hrs · 26,352 cycles

RIGHT INBD FLAP VANE L/E HAS CHAFE DAMAGE AT R/B, OTBD AND MID OTBD EDGES. R & R MID OTBD AND R/B L/E BLENDED OTBD L/E TO SMOOTH CONTOUR.

Part: SEAT TRACK — CORRODED (BS 506) · corrosion level 2 · airframe 27,977 hrs · 26,352 cycles

CORROSION ON RT SEAT TRACK AT BS 506. REPLACED SEAT TRACK FROM 409+128 - 559.

Part: SEAT TRACK — CORRODED (BS 559) · corrosion level 2 · airframe 27,977 hrs · 26,352 cycles

EXFOILATION CORROSION ON SEAT TRACK AT FS 559+40 .025 DEEP. REPLACED SEAT TRACK.

Part: CARGO TRACK — CORRODED (BS 5559) · corrosion level 2 · airframe 27,977 hrs · 26,352 cycles

CARGO TRACK, CORRODED AT RBL 9 AND BS 559+86 TO 559+96. REPLACED UNSERVICEABLE CARGO TRACK WITH SERVICEABLE CARGO TRACK.

Part: CARGO TRACK — CORRODED (BS 559-574) · airframe 27,977 hrs · 26,352 cycles

CARGO TRACK HAS CORROSION AT LBL9 AND BS 559+112 TO 574, REMOVED AND REPLACED CARGO TRACK.

Part: ANGLE — CRACKED (BS 484) · airframe 27,977 hrs · 26,352 cycles

RT INBD ANGLE IS CRACKED AT 484 LBL 27. R & R IAW SRM AND REO.

Part: STIFFENER — CRACKED (JET PIPE) · airframe 27,977 hrs · 26,352 cycles

RT JETPIPE 1ST STIFFENER CRACKED AT 9 O`CLOCK POSITION. REPAIRED IAW AMM 78-11-00, REPAIR SRS 042.

Part: SUPPORT — CRACKED (PAX DOOR ASSIST) · airframe 27,977 hrs · 26,352 cycles

PAX DOOR ASSIST MOTOR SUPPORT CRACKED. R & R CRACKED SUPPORT WITH PN 601R317745-7 IAW SRM 51-42-06.

Part: BRACKET — CRACKED (BS 589) · airframe 27,977 hrs · 26,352 cycles

ANGLE BRACKET IS CRACKED UNDER LT FLOOR SUPPORT AT FS 589. R & R.

Part: CARGO TRACK — CORRODED (BS 559-568) · corrosion level 2 · airframe 27,977 hrs · 26,352 cycles

CARGO TRACK CORRODED AT LBL 27 AND FS 559+104, 559+112 AND FS 568. REMOVED AND REPLACED CARGO TRACK IAW SRN 51-21-06, 53-51-49, 51-41-02, 53-61-49 AND AMM 20-21-00.

Part: TIE DOWN — CORRODED (BS 584-600) · corrosion level 2 · airframe 27,977 hrs · 26,352 cycles

CARGO TIE DOWN CORRODED AT LBL 9 AND BS 584 - 600. REMOVED AND REPLACED TIE DOWN IAW SRM 51-21-06, 53-61-49, 51-41-02 AND AMM 20-21-00.

Part: SEAT TRACK — CORRODED (BS 611-616) · corrosion level 2 · airframe 27,977 hrs · 26,352 cycles

CARGO TRACK IS CORRODED AT LBL 9 AND BS 611 TO 616. REMOVED AND REPLACED CARGO TRACK IAW SRM 51-21-06, 53-61-49, 51-41-02 AND AMM 20-21-00.

Part: STRUCTURE — DAMAGED (LEFT NACELLE) · airframe 24,759 hrs · 23,215 cycles

CLIMBING THRU FL140, LT ENG OBSERVED MOMENTARY OVERSPEED OF N1. NORM ENG INDICATIONS OBSERVED. UPON DECENT LEFT ENGINE THRUST LEVER STUCK AND UNABLE TO REDUCE N1 BELOW 81 PERCENT. COMPLIED WITH QRH, THRUST LEVER JAM PROCEDURE AND SHUTDOWN LEFT ENGINE INFLIGHT. COMPLIED WITH SINGLE ENGINE PROCEDURE QRH AND PERFORMED SINGLE ENGINE, FLAPS 20 LANDING. NOTED DAMAGE TO LT ENGINE. ON POST FLIGHT WALK AROUND NOTED LEFT ENGINE UPPER COWLING DAMAGE. OPEN

Part: LINK — SHEARED (LT ELEVATOR PCU) · airframe 24,924 hrs · 23,384 cycles

LEFT ELEVATOR PCU LINK TO PCU ROD END, SHEARED LOWER PIN. CONDITION FOUND DURING "A" CHECK FOUND 2 PCU`S WITH SAME PROBLEM. NR 10K, NR 2 FAILED, NR 3 ON (INBD) HEAD SHEARED, BUT PCU STILL FUNCTION HAD NOT FAILED COMPLETELY.

Part: SHUTOFF VALVE — MALFUNCTIONED (FUEL TRANFER) · airframe 23,432 hrs · 21,798 cycles

AFTER LEVELING OFF, NOTICED INCREASING FUEL IMBALANCE BETWEEN LT AND RT WINGS. RT TRANSFER SOV HAD FAILED TO OPEN, LT TRANSFER SOV WAS OPERATING. AUTO TRANSFLOW ATTEMPTED TO REFILL RT WING FROM LT WING, BUT COULDN`T ELIMINATE IMBALANCE SYNOPTIC PAGE SHOWS RT TRANSFLOW EJECTOR PUMP "WHITE" AND VALVE CLOSED. R & R RT FUEL TRANSFER SHUTOFF VALVE IAW AMM 28-13-43. OPS TESTED GOOD.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 23,433 hrs · 21,798 cycles

RT INBD FLAP VANE ON TOP INBD SIDE AT T/E IS CHAFED. BLENDED CHAFE IAW REO 601R-57-52-1768. DID NOT EXCEED MAXIMUM ALLOWABLE DEPTH TOOL USED AAR 1743 CAL DATE 04/20/12.

Part: THRESHOLD — CORRODED (SERVICE DOOR) · corrosion level 2 · airframe 23,433 hrs · 21,798 cycles

SERVICE DOOR THRESHOLD CORRODED ON BOTTOM SIDE AROUND SCREWS LOCATED AND DRILLED SERVICEABLE THRESHOLD P/N 601R-38957-19 IAW SRM 51-40-11 INSTALLED IAW CMM 25-33-01.

Part: BUSHING — CORRODED (HORIZONTAL STAB) · airframe 23,433 hrs · 21,798 cycles

LEFT HORIZONTAL STABILIZER BUSHING CORRODED. R & R HORIZONTAL STAB BUSHING IAW SB 601R-55-007.

Part: STRINGER — CHAFED (BS 718-736 S12L) · airframe 23,433 hrs · 21,798 cycles

LT STRINGER NEX TO LT OIL REPLENISH TUBE CHAFED. REPAIRED LT STRINGER 12 NEXT TO LT OIL REPLENISH TUBE BY INCORPORATING SRM STRINGER. REPAIR CHAPTER 53-00-03, FIG 202, SHEET G.

Part: CLEAT — ERODED (PAX DOOR) · airframe 23,433 hrs · 21,798 cycles

PAX DOOR FWD AND AFT CLEATS CORRODED. REPAIRED PAX DOOR AFT CLEAT BY DUPLICATING AND INSTALLING REPAIRED PAX DOOR FWD CLEAT AND INSTALLED IAW SRM 53-00-00 & SRM 51-42-06.

Part: TORQUE BOX — DAMAGED (THRUST REVERSER) · airframe 23,433 hrs · 21,798 cycles

RT THRUST REVERSER TORQUE BOX HAS NUMEROUS DAMAGED AREAS, REO 78-30-4072.

Part: BRACKET — CRACKED (BS 718) · airframe 23,433 hrs · 21,798 cycles

NR 2 HYD MANIFOLD BRACKET CRACKED. REPAIRED IAW REO 601R-53-62-031, REV A.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 23,433 hrs · 21,798 cycles

CLIP AT FS 280 FLOORBEAM APPROX RBL 9 IS CRACKED. R & R CLIPS (INBD & OTBD) IAW REO 601R-53-11-171, REV D.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 23,433 hrs · 21,798 cycles

CLIP AT FS 280 FLOORBEAM APPROX LBL 9 IS CRACKED. R & R LBL9 CLIPS ( INBD AND OTBD) IAW REO 601R-53-11-171, REV D.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 23,433 hrs · 21,798 cycles

FS 280 FLOORBEAM CRACKED AT APPROX LBL12 BY MLG AFT RELEASE CABLES PULLEY SUPPORT ATTACH BOLT. REPAIR IAW REO 601R-53-11-136, REV A.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 23,433 hrs · 21,798 cycles

FS 280 FLOORBEAM CRACKED APPROX RBL 12. REPAIRED FLOORBEAM IAW REO 601R-53-11-171, REV D.

Part: FLOORBEAM — CORRODED (BS 280) · corrosion level 2 · airframe 23,433 hrs · 21,798 cycles

TOP ON FLOORBEAM AT FS280 HAS HEAVY CORROSION ACROSS UPPER SURFACE AT FLT DECK ENTRY WAY. R & R FWD FLOORBEAM ANGLE IAW SRM 51-42-06.

Part: SKIN — CHAFED (LT MLG DOOR) · airframe 23,433 hrs · 21,798 cycles

CHAFING AT LT MLG DOOR L/E CHANGED -3 .100" IAW REO 601R-52-82-016.

Part: FAIRING — CHAFED · airframe 23,433 hrs · 21,798 cycles

CHAFING DAMAGE ON OTBD ENDS OF FAIRING 193AB ON LOWER SKIN UNDER FAIRING MATING SURFACES. REPAIRED DAMAGE IAW REO 601R-57-21-880, REV C, ZONE A.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 23,433 hrs · 21,798 cycles

LT INBD FLAP VANE ON TOP INBD SKIDE OF T/E CHAFED. REPAIRED IAW REO 601R-57-52-1765.

Part: STRUCTURE — CHAFED (NOSE COWL) · airframe 23,433 hrs · 21,798 cycles

LEFT LWR NOSE COWL T/E STRIP CHAFED. R & R T/E STRIP PN 228-50081-107 IAW CMM 71-14-01.

Part: RETAINER — CORRODED (E/E DOOR) · corrosion level 2 · airframe 23,433 hrs · 21,798 cycles

MAIN AVIONICS COMPARTMENT DOOR SEAL RETAINER CORRODED. R & R DOOR SEAL RETAINER IAW SRM 51-42-06.

Part: SEAT TRACK — CORRODED (BS 473.15-529) · airframe 23,433 hrs · 21,798 cycles

RT NR1 FLOOR SEAT TRACK CORRODED. R & R RT NR1 FLOOR SEAT TRACK.

Part: SEAT TRACK — CORRODED (BS 473.15-529) · corrosion level 2 · airframe 23,433 hrs · 21,798 cycles

LT NR1 FLOOR SEAT TRACK CORRODED. R & R LT NR1 FLOOR SEAT TRACK.

Part: SEAT TRACK — CORRODED (BS 529) · corrosion level 2 · airframe 23,433 hrs · 21,798 cycles

RT NR 2 SEAT TRACK CORRODED. R & R RT NR 2 SEAT TRACK.

Part: SILL — CORRODED (BS409) · corrosion level 2 · airframe 23,433 hrs · 21,798 cycles

SEVERAL; AREAS PF CORROSION, LT FLOOR SILL FROM FS 409+128 TO FS 559.00. REMOVED CORROSION FROM LT FLOOR SILL (7 AREAS) FROM FS 409+128 TO FS 559.00.

Part: HANDLE — CRACKED (PAX DOOR) · airframe 23,433 hrs · 21,798 cycles

PAX DOOR ESTERNAL HANDLE IS CRACKED. REMOVED UNSERVICEABLE PAX DOOR EXTERNAL HANDLE AND INSTALLED SERVICEABLE PAX DOOR EXTERNAL HANDLE IAW AMM 52-11-03 AND EO EO08/007/452.

Part: HINGE FITTING — CHAFED (AFT PAX DOOR) · airframe 23,433 hrs · 21,798 cycles

PAX DOOR AFT HINGE LUG ON FUSELAGE SIDE HAS CHAFING DAMAGE IN 2 PLACES. REPAIRED PAX DOOR AFT HINGE LUG ON FUSELAGE SIDE IAW DOOR SRM 51-12-00 AND REO 601R-53-21-814.

Part: HINGE FITTING — CHAFED (AFT PAX DOOR) · airframe 23,433 hrs · 21,798 cycles

AFT HINGE LUG ON PAX DOOR HAS CHAFING DAMAGE FROM HINGE PIN. REPAIRED AFT HINGE LUG ON PAX DOOR IAW SRM 51-12-00 AND REO 601R-52-11-1347.

Part: FLOORBEAM — CRACKED (BS 484.0) · airframe 23,433 hrs · 21,798 cycles

FLOORBEAM CRACKED AT FS484.0, LBL27.0. R & R FLOORBEAM TEE IAW REO 601R-53-41-059.

Part: BRACKET — CRACKED (BS 574) · airframe 23,433 hrs · 21,798 cycles

U BRACKET AT FS 574 CRACKED AT LOWER EDGE AROUND RIVET, 2 PLACES. R & R U BRACKET WITH SERVICEABLE PART.

Part: CARBON SEAL — FAILED (NR 2 ENGINE) · airframe 23,288 hrs · 21,641 cycles

ON POST FLT WALK AROUND FOUND SMOKE COMING FROM NR 2 JET PIPE AND STRONG ODOR. R & R OF NR 7 CARBON SEAL. OPS AND LEAK CHECK GOOD. REF EMM 72-00-00, SEP 38.

Part: PDU — MALFUNCTIONED (THRUST REVERSER) · airframe 21,880 hrs · 20,139 cycles

WHILE CLIMBING THRU FLIGHT LEVEL 255. RECEIVED R-REV UNLOCK CAUTION MESSAGE. BOTH REVERSER DISARM AT THE TIME MESSAGE RECEIVED. MESSAGE PERSISTED UNTIL ENGINE SHUTDOWN AT GATE C/W QRH. DIVERTED. R & R RT T/R PDU IAW AMM 78-32-03. OPS CHECKED GOOD, REMOVED PLACARD AND MEL, R & REINSTALLED UPPER AND LOWER NOSE COWLS ON RT ENGINE IAW AWAC SUP 07-015 AND 07-016. RII I-145.

Part: ANGLE — CRACKED (BS 559) · airframe 19,148 hrs · 17,294 cycles

PRESSURE BULKHEAD AT FS 559.0, LBL 18.0 CRACK AT CAP ANGLE LOCATION PRESSURE BULKHEAD AT FS 559, LBL 18.0. REPAIRED IAW REO 601R-53-41-260, REV D. (K)

Part: ANGLE — CRACKED (BS 559) · airframe 19,148 hrs · 17,294 cycles

PRESSURE BULKHEAD AT FS 559, RBL 18.0 CRACKED AT CAP ANGLE LOCATION. PRESSURE BULKHEAD AT FS 559, RBL 18.0 REPAIRED IAW REO 601R-53-41-260 REV D AND REO 601R-53-41-609, REV A. (K)

Part: ATTACH FITTING — CRACKED (BS 621) · airframe 19,148 hrs · 17,294 cycles

AT REAR PRESSURE BULKHEAD IN AFT COMPARTMENT, INTERCOSTAL CLIP BTW FS 621 AND FS 625, ADJACENT TO STR 14R CRACK AT REAR PRESSURE BULKHEAD IN AFT COMPARTMENT, INTERCOSTAL CLIP BTW FS 621 AND 625. ADJACENT TO STR 14R REPLACED IAW SRM 51-21-42 AND REO 601R-53-61-422. (K)

Part: ATTACH FITTING — CRACKED (BS 621 S14L) · airframe 19,148 hrs · 17,294 cycles

AT REAR PRESSURE BULKHEAD, IN AFT COMPARTMENT, INTERCOSTAL CLIP AT FS 621, ADJACENT TO STR 14L CRACK AT REAR PRESSURE BULKHEAD, IN AFT COMPT, INTERCOSTAL CLIP AT FS 621 ADJACENT TO STR 14L, REPLACE IAW SRM 57-42-21 AND REO 601R-53-61-422. (K)

Part: HANDLE — CRACKED (CARGO DOOR) · airframe 19,148 hrs · 17,294 cycles

CARGO DOOR HANDLE HOUSING CRACK. (UPPER 1.00, LOWER .500) CARGO DOOR HANDLE HSG REPLACED IAW SRM 51-42-21 AND DWG 601R35027. (K)

Part: FLOORBEAM — CRACKED (BS 461.5) · airframe 19,148 hrs · 17,294 cycles

FLOORBEAM FITTING CRACKED AT FS 461.5, RBL 9.0, OTBD SIDE FLOORBEAM FITTING AT FS 461.5, RBL 9.0 OTBD SIDE REPLACED IAW SRM 51-42-06 AND SRM 51-42-21. (K)

Part: BULKHEAD — CRACKED (BS 202.75) · airframe 19,148 hrs · 17,294 cycles

FWD PRESSURE BULKHEAD FS 202.75, LBL 23.71, WL 69.7, CRACKED AT PARKING BRAKE LINE LOCATION (CRACK LENGTH 1.500") FWD PRESSURE BULKHEAD FS 202.75, LBL 23.71, WL 69.7. REPAIRED AT PARKING BRAKE IAW REO 601R-53-11-563. (K)

Part: SILL — CRACKED (BS 574) · airframe 19,148 hrs · 17,294 cycles

CARGO DOOR FLOOR SILL FS 574.00 LBL 45.00 CRACKED. CARGO DOOR FLOOR SILL FS 574.00, LBL 45 REPAIRED IAW REO 601R-53-61-1741. (K)

Part: PLATE — CRACKED (BS 589) · airframe 19,148 hrs · 17,294 cycles

CARGO DOOR FLOOR LANDING PLATE CRACKED FS 589.00, LBL 45.00. CARGO DOOR FLOOR LANDING PLATE REPAIRED IAW REO 601R-53-61-433 REV NC AND REO 601R-53-61-3403. (K)

Part: ATTACH FITTING — CRACKED (BS 484) · airframe 19,148 hrs · 17,294 cycles

INTERCOSTAL CLIP CRACKED AT FS 484, LBL 27.0. INTERCOSTAL CLIP AT FS 484, LBL 27.0. REPLACED IAW REO 601R-53-41-059, REV B. (STEP 8 TO 14). (K)

Part: CONTROL HANDLE — MALFUNCTIONED (MLG) · airframe 17,111 hrs · 15,283 cycles

LOG 197305/3 AFTER TAKEOFF LANDING GEAR DID NOT COME UP WHEN SELECTED UP. LANDING GEAR LIGHT REMAINED GREEN. ALSO GOT INBD ANTI-SKID CAUTION AND PARKING BRAKE SHUT OFF VALVE CAUTION. CLEARED WHEN GEAR SELECTED DOWN. INTERROGATED PSEU AND FOUND DI 11 OFF FAULT CODE. R&R LANDING GEAR CONTROL HANDLE IAW AMM 32-31-01. OPS CHECK GOOD AT THIS TIME.

Part: WEB — CRACKED (PAX DOOR)

PAX DOOR FORWARD WEB SKIN IS CRACKED IN RADIUS BETWEEN STEP 832CT AND FIXED STEP. MAINTENANCE CUT AWAY DAMAGED SKIN AND INSTALLED REPAIR DOUBLER AND ANGLES IAW BOMBARDIER REO 601R-52-11-702 REV A AND BSC EO 601R-52-13284. (M)

Part: SKIN — CORRODED (LT WING)

LT LOWER WING PLANK HAS MINOR PITTING DAMAGE IN A NON-CRITICAL AREA .001-.002 DEEP AT WING ACCESS PANEL 540BB. MAINTENANCE REPAIRED LT LOWER WING PLANK IAW BOMBARDIER REO 601R-57-21-030 REV F. (M)

Part: SKIN — CORRODED (RT WING)

MINOR PITTING ON RIGHT LOWER WING PLANK WS 54.897 ACCESS PANEL 640BB IN NON-CRITICAL AREA. MAINTENANCE REPAIRED IAW BOMBARDIER REO 601R-57-21-030. (M)

Part: SKIN — CORRODED (LT WING)

LT LOWER WING PLANK AT ACCESS PANEL 540 CB HAS MINOR PITTING DAMAGE IN NON-CRITICAL AREA, .001-.002 INCH DEEP. MAINTENANCE REPAIRED LT LOWER WING PLANK PER BOMBARDIER REO 601R-57-21-030 REV F. (M)

Part: SKIN — CORRODED (LT WING)

MINOR PITTING DAMAGE LT LOWER WING PLANK WS 188.040 FUEL ACCESS PANEL 550BB IN NON-CRITICAL AREA .001 INCH -.002 INCH DEEP. MAINTENANCE REPAIRED IAW BOMBARDIER REO 601R-57-21-030. (M)

Part: SKIN — CORRODED (RT WING)

MINOR PITTING DAMAGE RT LOWER WING PLANK WAS 12.245 ACCESS PANEL 610AB, .001 INCH-.002 INCH DEEP IN CRITICAL AND NON-CRITICAL AREAS. MAINTENANCE REPAIRED IAW BOMBARDIER REO 601R-57-21-030 REV F. (M)

Part: SKIN — CRACKED (PAX DOOR)

PAX DOOR AFT STAIRS SKIN IS CRACKED BETWEEN PANEL 832CT AND 832DT STEPS, CRACK IS .250 LONG. MAINTENANCE CUT AWAY DAMAGED SKIN AND INSTALLED REPAIR DOUBLER AND ANGLES IAW BOMBARDIER REO 601R-52-11-702 REV A. (M)

Part: ATTACH FITTING — CRACKED (BS 280)

FOUND FS 280 RBL 9 OUTBOARD ATTACH CLIP IS CRACKED. 10-24-07 MAINTENANCE REMOVED AND REPLACED LCIP P/N 601R31113-58 IAW CRJ SRM 51-42-06, 51-42-21. (M)

Part: ATTACH FITTING — CRACKED (BS 280)

FOUND FS 280 LBL 9 INBOARD CLIP CRACKED. 10-24-07 MAINTENANCE REMOVED AND REPLACED CLIP P/N 601R31113-57 IAW CRJ SRM 51-42-06, 51-42-21. (M)

Part: ATTACH FITTING — CRACKED (BS 280)

FOUND FS 280 LBL 9 OUTBOARD ATTACH CLIP CRACKED. 10-24-07 MAINTENANCE REMOVED AND REPLACED CLIP P/N 601R31113-57, IAW CRJ SRM 51-42-06, 51-42-21. (M)

Part: ATTACH FITTING — CRACKED (BS 280)

FOUNF FS 280 RBL 9 INBOARD CLIP CRACKED. 10-24-07 MAINTENANCE REMOVED AND REPLACED CLIP P/N 601R31113-58 IAW CRJ SRM 51-42-06, 51-42-21. (M)

Part: CARGO TRACK — CRACKED (FUSELAGE)

FOUND CARGO DOOR FORWARD TRACK LOWER AT CHANNEL CRACKED. 10-24-07 MAINTENANCE REPLACED C-CHANNEL IAW CRJ SRM 51-42-06. (M)

Part: DRAG ANGLE — CRACKED (PAX DOOR)

PAX DOOR AFT DRAG ANGLE CRACKED APPROX 1 INCH AT DOOR ASSIST CABLE PULLEY IN RADIUS OF ANGLE. MAINTENANCE REPAIRED ANGLE IAW BOMBARDIER AERO SPACE REO 601R-52-11-513. (M)

Part: SKIN — CRACKED (PAX DOOR)

PAX DOOR AFT STAIR SIDE SKIN CRACKED APPROX .70 INCH BETWEEN MID UPPER STEP AND MID STEP. MAINTENANCE CUT AWAY DAMAGED SKIN AND INSTALLED REPAIR DOUBLER AND ANGLES IAW BOMBARDIER REO 601R-52-11-702 REV A. (M)

Part: HANDLE — FAILED (ESCAPE HATCH) · airframe 14,291 hrs · 12,558 cycles

WO 114147, MWC 144, CREW ESCAPE HATCH OUTER HANDLE WILL NOT OPEN. REMOVED AND REPLACED CREW ESCAPE HATCH OUTSIDE HANDLE IAW CMM 52-22-03, FUNCTIONAL TEST OF OUTSIDE HANDLE GOOD IAW CMM 52-22-03. (K)

Part: WIRE — DAMAGED (LANDING GEAR) · airframe 12,942 hrs · 11,274 cycles

PROXIMITY SYSTEM FAULT WHITE STATUS MESSAGE. INSTALLED NEW WIRES FROM P4MB TO PROXIMITY SWITCH S38. WIRES INSTALLED WERE RED AND BLUE IAW WDM 20-12-00. OPS CHECK GOOD. (K)

Part: SKIN — DENTED (RUDDER)

TEMPORARY DISPOSITION FOR THE DENTS TO RUDDER SKIN BETWEEN RS 108.25 AND RS 113.98. MAINTENANCE REPAIRED RUDDER BY CUTTING AWAY DAMAGE AND INSTALLING NON FLUSH DOUBLER IAW CRJ200 SRM 55-40-00. (M)

Part: RADOME — NONE (FUSELAGE) · airframe 9,730 hrs · 8,173 cycles

REQUEST BIRD STRIKE INSPECTION. REMOVED AND REPLACED RADOME DUE TO BIRD STRIKE IAW AMM 53-81-01. PERFORMED BIRDSTRIKE AMM 05-51-25. NO FURTHER DAMAGE AND NO ENGINE INGESTION FOUND. (K)

Part: A/C PACK — LEAKING (RIGHT) · airframe 8,911 hrs · 7,450 cycles

CABIN FILLED WITH SMOKE WHILE AT GATE WITH ENGINES OFF, APU AND BOTH PACKS RUNNING. INSPECTED AFT EQUIPMENT BAY AND FOUND AIR LEAK RT PACK WATER SEPARATOR PIPE. NO EVIDENCE OF SMOKE WITH APU AND BOTH PACK ON. (K)

Part: STRUT — DISCHARGED (NLG)

AFTER ROTATION AND GEAR UP RECEIVED SEVERAL MESSAGES NOSE DOOR, GEAR DISAGREE, WOW INPUT AND STEERING INOP. FOLLOWED QRH PROCEDURES LANDED WITH NOSE STEERING INOPERATIVE. SERVICED NLG STRUT IAW CRJ AMM 12-12-32B REFERENCE AWAC W/O NR 77064 FOR DETAILS OF WORK PERFORMED KMCBICK 6735 CRSWVER835K. (M)

Part: DCU — MALFUNCTIONED (NR 2)

AFTER ROTATION AND GEAR UP RECEIVED SEVERAL M/C'S AND WINDSHEAR NOSE GEAR DOOR, DISAGREE AND STEERING INOPERATIVE FOLLOWED QRH RETURNED TO CKB WITHOUT INCIDENT. POWERED DOWN AC REMOVED AND RERACKED NR 2 DCU, OPS IAW CRJ AMM 31-41-04. OPS GOOD, NOTE GROSS AT LOG 36200, NO OVERWEIGHT INSPECTION REQUIRED. (M)

Part: SKIN — DENTED (LT T/E FLAP) · airframe 7,532 hrs · 6,229 cycles

FLAP LOWER SKIN DENTED AT WS NEAR T/E. DENT MEASURES 2 INCHES ROUND BY .085 INCH DEEP. INSTALLED EXTERNAL REPAIR TO LT IB FLAP LOWER SKIN AT WS 106, 5 INCHES FROM T/E IAW REO.

Part: ANGLE — CRACKED · airframe 7,532 hrs · 6,229 cycles

LT FS 484.00 AT LBL 36 ANGLE CRACKED.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 7,532 hrs · 6,229 cycles

RT FS 621 FLOOR SUPPORT ANGLE CRACKED.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 7,532 hrs · 6,229 cycles

RT FS 621.00, FLOOR SUPPORT ANGLE CRACKED. REMOVED DAMAGED PORTION OF ANGLE AND INSTALLED REPAIR ANGLE IAW REO.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 7,532 hrs · 6,229 cycles

RT FS 621 FLOOR SUPPORT ANGLE CRACKED.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 7,532 hrs · 6,229 cycles

LT FS 621 FLOOR SUPPORT ANGLE CRACKED.

Part: ANGLE — CRACKED (FUSELAGE)

FOUND RIGHT FS 484 AT RBL 36 ANGLE CRACKED. REPAIRED RIGHT FS 484 AT RBL 36 ANGLE IAW BOMBARDIER REO 601R-53-41-059 REV A. (M)

Part: ANGLE — CRACKED (FUSELAGE) · airframe 7,532 hrs · 6,229 cycles

RT FS 625.00 OBLIQUE ANGLE CRACKED.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 7,532 hrs · 6,229 cycles

LT FS 621.00 FLOOR SUPPORT ANGLE CRACKED.

Part: ANGLE — CRACKED (FUSELAGE)

FOUND LEFT FS 625 OBLIQUE ANGLE CRACKED. REPLACED ANGLE P/N 601-35012-51 IAW CRJ SRM 51-42-06. (M)

Part: ANGLE — CRACKED (FUSELAGE) · airframe 7,532 hrs · 6,229 cycles

RT FS 625.00 OBLIQUE ANGLE CRACKED. REPLACED ANGLE P/N 601-35012-12 IAW CRJ SRM 51-42-06. (M)

Part: ANGLE — CRACKED (FUSELAGE) · airframe 7,532 hrs · 6,229 cycles

RT FS 625.00 OBLIQUE ANGLE CRACKED. REMOVED CRACKED OBLIQUE ANGLE AT FS 625 RT SIDE AND REPLACED WITH NEW SERVICEABLE ANGLE PN 601-35012-52 IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE)

FOUND LEFT FS 484 AT LBL 36 ANGLE CRACKED. REPAIRED LEFT FS 484 AT LBL 36 IAW BOMBARDIER REO 601R-53-41-059 REV A. (M)

Part: SKIN — CORRODED (LT WING) · airframe 7,532 hrs · 6,229 cycles

LT WING LOWER PANEL FUEL TANK ACCESS DOOR CUT-OUT AT WS 12.245 HAS NUMEROUS AREAS OF PITTING/ FRETTING LOCATED ON FAYING SURFACE AND RADIUS AREAS. DEPTH LESS THAN .015 INCH. REPAIRED ACCESS DOOR CUTOUT AT WS 12/245 IAW BOMBARDIER REO 601R-57-21-030 REV C. (M)

Part: RIB — CRACKED (RT WING WW)

FOUND RIGHT MLG WHEEL WELL BATT RIB IS CRACKED 1.5 INCHES LONG IN UPPER AFT RADIUS. REPAIRED RIGHT MLG BATTERY RIB IAW CRJ BOMBARDIER REO 601R-57-51-046 REV B. (M)

Part: HANDLE — LACK OF LUBE (ESCAPE HATCH) · airframe 7,532 hrs · 6,229 cycles

CREW ESCAPE HATCH, OUTER HANDLE FROZE IN POSITION, WILL NOT DEPLOY. LUBRICATED OUTER HANDLE ASSEMBLY ON CREW ESCAPE HATCH. FOUND TO BE IN GOOD WORKING ORDER IAW CRJ AMM 12-20-52-640-803. (M)

Part: VANE — WORN (TE FLAPS) · airframe 7,532 hrs · 6,229 cycles

LT OB FLAP - VANE FITTING AT WS 296.073 IS WORN BEYOND LIMITS. COMPLY WITH MFG REO.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 7,532 hrs · 6,229 cycles

LT FS 625.00 OBLIQUE ANGLE CRACKED.

Part: APU — SMOKE (APU BAY)

SMOKE FROM APU, SHUTDOWN APU AND BLEW BOTTLE. REMOVED AND REPLACED APU FIRE EXTINGUSHER IAW AMM 26-22-07. OPS CHECK GOOD. PERFORMED OPS CHECK OF APU, NO DEFECTS NOTED. (M)

Part: WIRE — OUT OF POSITION (OVERHEAT SYS)

BLEED AIR DUCT MASTER WARNING WOULD COME ON INTERMITTENTLY AND REPEATEDLY IN FILGHT 31,000 FEET. COMPLIED WITH QRH MSS EXTINGUISHING 55 PERCENT N1 LEFT ENGINE. STRAIGHTENED WIRE AT 14TH STAGE BLEED AIR DUCT AND TIGHTENED CLAMP AT AIR SWITCH. RAN ENGINE, OPERATIONAL CHECK GOOD. (M)

Part: STRIKER — DAMAGED (PAX DOORFRAME)

PREVIOUS PASSENGER DOOR SEALS STRIKER REPAIR IS DAMAGED, FS 310. REPAIRED DAMAGED AREA IAW BOMBARDIER INC REO 601R-52-11-008 REV B. (M)

Part: ADG — FAILED (ELECTRICAL)

MAINTENANCE CHECK REQUIRED FOR INFLIGHT ADG DEPLOYMENT FUNCTION. ADG TEST FAILED. REMOVED AND REPLACED ADG, (S/N OFF: 0611, S/N ON: 0238) TEST FLIGHT OF ADG TEST SATISFACTORY. ADG COMPONENT REPAIR SHOP TEAR-DOWN FINDINGS, NO FAULT FOUND (NFF).