N404AW

Part: APU — FIRE · airframe 39,862 hrs · 36,281 cycles

AFTER TRANSFER OF BLEED TO APU AUTO SHUTDOWN, FUELER REPORTED LOTS OF SMOKE & FIRE COMING FROM APU EXHAUST.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,974 hrs · 27,940 cycles

ROW F & AFT EMER FLOOR TRACK LIGHTS INOPERATIVE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 39,228 hrs · 35,654 cycles

REAR 1/3RD OF FLOOR LEVEL EMER LIGHTS ARE INOPERATIVE.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 39,182 hrs · 35,612 cycles

FS 409+128 BULKHEAD VERTICAL BEAM AT LBL 27.0, OTBD STIFFENER CRACKED AT BOTTOM FASTENER HOLE. REPAIRED IAW GREO 601R53-41-056.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 39,182 hrs · 35,612 cycles

FS409.00+128 BULKHEAD VERTICAL BEAM AT RBL 27.0, INBD STIFFENER CRACKED AT BOTTOM FASTENER HOLE. REPAIRED IAW GREO 601R-53-41-056.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 39,182 hrs · 35,612 cycles

1012024 1000-0002 FS 409.00+128 BULKHEAD VERTICAL BEAM STIFFENER AT LBL 27.0, INBD STIFFENER CRACKED AT BOTTOM FASTENER HOLE. REPAIRED IAW GREO 601R-53-41-056.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 39,137 hrs · 35,570 cycles

THREE LIGHT BULBS BURNED OUT ON MID CABIN EMERGENCY LIGHTS ON CEILING. R & R 3 LIGHT BULBS IN MID CABIN EMERGENCY EXIT IAW AMM 33-51-14. OPERATIONS CHECKED GOOD.

Part: BULB — ABNORMAL (CABIN LIGHTS) · airframe 39,137 hrs · 35,570 cycles

FLIGHT 3892, ONE BULB BURNED OUT ON CEILING LIGHT BY LAVATORY DOOR. R & R THE BULB IAW AMM 33-51-16. OS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 39,137 hrs · 35,570 cycles

ONE BULB BURNED OUT ONBOARD CEILING LIGHT BY LAVATORY DOOR. R & R NUMBER 4 CEILING EMERGENCY LIGHT BULB IAW AMM 33-51-16. OPERATIONS CHECKED GOOD.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 37,972 hrs · 34,436 cycles

RECEIVED NWS INOPERATIVE MSG ENROUTE. COMPLIED WITH QRH, MSG REMAINED.

Part: LIGHT — INOPERATIVE (ROWS 6-8) · airframe 37,451 hrs · 33,961 cycles

FLIGHT ATTENDANT REPORTED EMERGENCY LIGHTS ROW 6 - 8 AND LOWER EMER EXIT SIGN RT SIDE INOPERATIVE.

Part: BALLAST — DEFECTIVE (CABIN) · airframe 36,168 hrs · 32,783 cycles

BURNING WIRE SMELL FROM OVERHEAD BIN ROW 10 RT SIDE. INSPECTED OVERHEAD BIN & FOUND BALLAST AT OVERHEAD BIN ROW 10 D/F INOPERATIVE WITH BURNT SMELL. R & R BALLAST AT OVERHEAD BIN ROW 10 D/F IAW SUPP 13-096, OPERATIONS CHECKED GOOD.

Part: HEATER — SHORTED (GALLEY) · airframe 35,976 hrs · 32,590 cycles

STRONG BURNING RUBBER ODOR INFLIGHT, LOCALIZED TO GALLEY & FIRST COUPLE ROWS OF CABIN. NO SMOKE NOTED & NO ELECTRICAL ISSUES NOTED. GALLEY HEAT & POTABLE WATER SYS ON. PULLED BREAKERS FOR POTABLE WATER & GALLEY HEAT & ODOR DISPERSED. FOUND GALLEY LINE HEATER GROUNDED OUT & BURNING INSULATION NO DAMAGE NOTED TO ACFT SKIN OR STRUCTURE SAFTIED LINE HEATER & BREAKER IAW 278322 3 FOR MEL.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,927 hrs · 32,549 cycles

FLOOR SUPPORT ANGLE AT PAX DOOR THRESHOLD CORRODED AT FS 310 TO 349. R & R FLOOR SUPPORT ANGLE AT PAX DOOR SILL F 310 - 349 WITH SERVICEABLE PN 601R31527-221 IAW CRJ200 SRM 51-40-11 & 51-42-21.

Part: HANDLE — CRACKED (CARGO DOOR) · airframe 35,927 hrs · 32,549 cycles

CARGO DOOR OUTER HANDLE CRACKED. R & R CARGO DOOR HANDLE ASSEMBLY IAW CRJ200 SRM 51-21-11, 51-42-21 & 51-40-11.

Part: PANEL — CORRODED (CARGO BAY) · corrosion level 2 · airframe 35,927 hrs · 32,549 cycles

LOWER ATTACH POINT ON CARGO BAY PANEL 282AR CORRODED. R & R WITH NEW SERVICEABLE PANEL.

Part: HINGE — CORRODED (PAX DOOR) · corrosion level 2 · airframe 35,927 hrs · 32,549 cycles

PAX DOOR UPPER FOLDING STEP HINGE CORRODED THROUGH. R & R PAX DOOR UPPER FOLDING STOP HINGE IAW CRJ 200 AMM 52-11-14, PN 601R-31980-41.

Part: SKIN — CRACKED (RIGHT) · airframe 35,927 hrs · 32,549 cycles

RIGHT JET PIPE HAS 3 CRACKS IN SKIN AROUND COMBUSTOR DRAIN. REPAIRED CRACKS IAW STS EA 15-2014-050.

Part: STEP — CORRODED (PAX DOOR) · corrosion level 2 · airframe 35,927 hrs · 32,549 cycles

PAX DOOR STEP PANEL 832 FT IS DELAMINATED FROM CORROSION. R & R PAX DOOR STEP PANEL 832 FT WITH SERVICEABLE PN 601R31980-59 IAW CRJ200 SRM 51-41-02.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,927 hrs · 32,549 cycles

RIVETS CORRODED AT FS 349, LBL 9 - LBL 27. REMOVED CORROSION IAW CRJ 200 SRM 51-21-06, 53-00-00 & 51-21-11. R & R WINDSCREEN FITTING.

Part: BRACKET — CORRODED (PAX DOOR) · corrosion level 2 · airframe 35,927 hrs · 32,549 cycles

PAX DOOR AFT HANDRAIL SUPPORT STOW CUP BRACKET CORRODED. R & R AFT HANDRAIL SUPPORT BRACKET IAW CRJ SRM 51-40-11, 51-42-10.

Part: RIB — CORRODED (LT WING) · corrosion level 2 · airframe 35,927 hrs · 32,549 cycles

LT OTBD LE, INBD RIB IS CORRODED. R & R INBD RIB ON LT OTBD LE PN 601R12063-21 IAW CRJ 200 SRM 51-40-11 & 51-42-13.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,927 hrs · 32,549 cycles

FLOOR SUPPORT BEAM AT 349.00 CORRODED. R & R FLOOR SUPPORT BEAM IAW CRJ200 51-42-13 & 51-42-06.

Part: DRAG ANGLE — CRACKED (RT MLG DOOR) · airframe 35,927 hrs · 32,549 cycles

RT MLG DRAG ANGLE COMMON TO BATTERY RIB IS CRACKED. REMOVED & INSTALLED RT MLG DOOR DRAG ANGLE, STIFFENER PN 600-10389-2 IAW CRJ 200 SRM 51-42-21.

Part: DRAG ANGLE — CRACKED (LT MLG WW) · airframe 35,927 hrs · 32,549 cycles

BATTERY RIB DRAG ANGLE CRACKED IN LT MLG WW. R & R WITH SERVICEABLE PART, PN 600-10389-1 IAW CRJ 200 SRM 51-40-11 & 51-42-21.

Part: HINGE — GOUGED (PAX DOOR) · corrosion level 2 · airframe 35,927 hrs · 32,549 cycles

PAX DOOR UPPER FOLDING STEP HINGE HAS NUMEROUS GOUGES AT EACH STEP, SIDE HINGE HALF PIN LOBE & UPPER STEP CLOSING PLATE CORRODED BEYOND LIMITS. R & R TWO EACH HINGES ON PAX DOOR UPPER FOLDING STEP WITH NEW SERVICEABLE HINGES PN 601R31980-41 & 600-31980-103S & UPPER STEP CLOSING PLATE WITH SERVICEABLE PART IAW SRM 51-40-11 & 51-41-02.

Part: RIB — CRACKED (RT WING) · airframe 35,927 hrs · 32,549 cycles

RIGHT MLG BATTERY RIB IS CRACKED. REPAIRED RT MLG BATTERY RIB IAW REO 601R 57-51-046 REV B DATED 2002-02-28 REPAIR NR 2.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 35,927 hrs · 32,549 cycles

NLG CUTOUT AFT RT CORNER CRACKED. REPAIRED NLG CUTOUT RT CORNER IAW REO 601R-53-11-048.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 35,927 hrs · 32,549 cycles

LT OBLIQUE ANGLE AT FS 621 - 625 & STRINGER 14L IS CRACKED. R & R WITH SERVICEABLE PART, PN 601-35012-51 IAW SRM 51-40-11 & 51-42-21.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 35,927 hrs · 32,549 cycles

RIGHT OBLIQUE ANGLE FS 621 - 625 AT STRINGER 14R IS CRACKED. R & R RT OBLIQUE ANGLE WITH SERVICEABLE PART PN 601-35012-52 IAW CRJ 200 SRM 51-40-11 & 51-42-21.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,927 hrs · 32,549 cycles

LT FLOOR SEAT TRACK CORRODED AT FS 364 & LBL 9. R & R WITH SERVICEABLE PART IAW SRM 51-40-11 & AMM 53-01-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,927 hrs · 32,549 cycles

RT FLOOR SEAT TRACK AT RBL 9 HAS CORROSION AT FS 364. R & R WITH SERVICEABLE PART IAW SRM 51-40-11 & AMM 53-01-11.

Part: FITTING — CRACKED (FUSELAGE) · airframe 35,927 hrs · 32,549 cycles

FLOORBEAM LBL 9 OTBD CLIP AT FS 280 IS CRACKED. R & R CLIP WITH SERVICEABLE PART IAW 601R-53-11-171 REV D DATED 13-FEB-07.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 35,927 hrs · 32,594 cycles

CARGO COMPARTMENT SEAT TRACKS CORRODED AT LBL & RBL 9, FS 559+112, LBL & RBL 27 AT FS 559+85. R & R THREE TRACKS AT RBL 9, FS 559+112, LBL & RBL 27 AT FS 559+85 WITH SERVICEABLE PARTS IAW SRM 51-40-11.

Part: STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,927 hrs · 32,549 cycles

FLOOR SUPPORT STRAP AT FS 559 & LBL 38 CORRODED. R & R WITH SERVICEABLE PART IAW SRM 51-40-11 & 51-42-06.

Part: AUTOPILOT SYS — MALFUNCTIONED (COCKPIT) · airframe 35,369 hrs · 32,028 cycles

3925DLY NON COMMANDED YAW MOTION TO THE RT AT FL290 SAT 46C ON FLIGHT DIRECTOR NR 2 FOR APPROXIMATELY 2 SECONDS. YAW DAMPER REMAINED ENGAGED, NO FURTHER OCCURRENCES. INTEGRATED FCC & REPORTS CUT R OCCURRENCE, IAW FIM 22-22, ACTION REQUIRED IS NONE. PERFORMED OPERATIONS CHECK OF YAW DAMPER IAW AMM 22-22-01, OPERATIONS CHECKED GOOD.

Part: ADG — MALFUNCTIONED · airframe 350,026 hrs · 31,685 cycles

DURING TAKEOFF, WOW, ADG DEPLOYED. DEACTIVATED ADG AUTO DEPLOY IAW AMM 24-23-22, RESTOWED ADG IAW AMM 24-23-22.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 32,263 hrs · 28,977 cycles

STRONG ELECTRICAL BURNING ODOR DETECTED IN COCKPIT AND GALLEY AREA. SEEMS STRONGER WITH COCKPIT DOOR CLOSED. TROUBLESHOT PACK SYSTEM TO FULL HOT, FULL COLD FOR 30 MIN, RAN ALL INTERIOR LIGHTS ON BRIGHT FOR 30 MIN WITH PAX DOOR AND COCKPIT DOOR CLOSED, NO ELECTRICAL ODOR NOTED. R & R ADDRESSING PANEL FOR POSSIBLE WATER DAMAGE. OPS CHECKED GOOD IAW AMM 23-31-01, OPS CHECKED DISPLAY COOL FAN SYS, CHECKED GOOD.

Part: BRACKET — CRACKED (FS 574) · airframe 31,087 hrs · 27,848 cycles

FWD UPPER CARGO DOOR TRACK ROLLER BRACKET CRACKED. R & R WITH SERVICEABLE IAW REO 601R-52-31-179.

Part: ROLLER — CRACKED (CARGO DOOR) · airframe 31,087 hrs · 27,848 cycles

FWD UPPER CARGO DOOR TRACK ROLLER BRACKET CRACKED. R & R WITH SERVICEABLE PN CC670-38706-3 IAW REO 601R-52-31-179.

Part: TRUNNION — DAMAGED (WS 675.75) · airframe 31,087 hrs · 27,848 cycles

DURING COLD WORKING OF THE MLG TRUNNION LOWER FLANGED, FOUND FOUR PREVIOUSLY OVERSIZED HOLES RT REPAIRED IAW REO 601R-57-21-1607.

Part: SILL — CORRODED (BS 574-621) · corrosion level 2 · airframe 31,087 hrs · 27,848 cycles

CARGO DOOR SILL CORRODED AROUND NUT PLATE HOLES FS 574-621. R & R CARGO DOOR SILL FS 574-621 IAW SRM 51-40-11, 51-42-06, & REO 601R-53-690, REV D.

Part: HINGE FITTING — CRACKED (WS 65.75) · airframe 31,087 hrs · 27,848 cycles

NDT INDICATED A CRACK AT THE AFT HOLE OF THE AFT HINGE FITTING LOCATION. REPAIRED IAW REO 601R-57-21-1608.

Part: FRAME — CORRODED (BS 349) · airframe 31,087 hrs · 27,848 cycles

CORROSION ON RIB AT STA 349 IN AVIONICS BAY BILGE AREA ( FWD SIDE) R & R LOWER FRAME SECTION AT FS 349, STR 34L-24 PN 601R32005-69 IAW SRM 51-42-06, 51-42-21 & 51-40-11.

Part: FRAME — CORRODED (BS 319) · corrosion level 2 · airframe 31,087 hrs · 27,848 cycles

CORROSION ON RIB AT STA 319 IN AVIONICS BAY BILGE AREA (FWD & AFT SIDE). R & R LOWER FRAME SECTION AT BS 319 S24L-24R IAW SRM 51-42-06, 51-42-21, 51-40-11.

Part: FLOORBEAM — CRACKED (FS 484.0) · airframe 31,087 hrs · 27,848 cycles

LEFT FS 484, BL27 INBD CLIP IS CRACKED. R & R CLIP IAW REO 601R-53-41-059, REV B.

Part: FRAME — CORRODED (BS 333) · corrosion level 2 · airframe 31,087 hrs · 27,848 cycles

CORROSION ON RIB AT STA 333 IN AVIONICS BAY BILGE AREA (FWD AND AFT SIDE) R 7 R FRAME SECTION PN 601R32004-55 IAW SRM 51-42-06, 51-42-21, 51-40-11.

Part: SILL — CORRODED (BS 319-349) · corrosion level 2 · airframe 31,087 hrs · 27,848 cycles

SERVICE DOOR SILL AREA HAS CORROSION. R & R SERVICE DOOR SILL ANGLE IAW SRM 51-42-06, 51-42-21. R & R SERVICE DOOR STEP PLATE IAW AMM 25-33-01.

Part: FLOORBEAM — CRACKED (FS 621) · airframe 31,087 hrs · 27,848 cycles

FLOORBEAM BS 621 CRACKED. REPAIRED FLOORBEAM IAW REO 601R-53-61-117, REV C.

Part: FLOOR SUPPORT — CORRODED (FS 574-621) · airframe 31,087 hrs · 27,848 cycles

LBL 9 FLOOR SUPPORT CORRODED AROUND NUT PLATE HOLES FROM FS 574 TO 621. R & R FLOOR SUPPORT.

Part: FLOOR SUPPORT — CORRODED (FS 574-621) · airframe 31,087 hrs · 27,848 cycles

LBL 27, FLOOR SUPPORT CORRODED AROUND NUT PLATE HOLES. R & R FLOOR SUPPORT.

Part: SUPPORT ANGLE — CRACKED (RT WING) · airframe 31,087 hrs · 27,848 cycles

UPPER ANGLE SUPPORT FOR PICCOLO TUBE TRANSITION DUCT BETWEEN L/E 520JL AND 530JL IS CRACKED. REMOVED, FABRICATE4D AND INSTALLED IAW FORM 412, SRM 51-41-29, 51-41-02, 51-42-06, 51-42-15, 51-24-16, 51-21-11, 51-25-06.

Part: SUPPORT ANGLE — CRACKED (WING) · airframe 31,087 hrs · 27,848 cycles

UPPER SUPPORT ANGLE FOR PICCOLO TUBES TRANSITION 620JL AND 630JL IS CRACKED. REMOVED UPPER SUPPORT ANGLE, FABRICATED AND INSTALLED IAW FORM 412, SRM`S 51-41-21, 51-41-02, 51-42-15, 51-24-16, 51-21-11, 51-25-06.

Part: NUT PLATE — DAMAGED (FS 158.71) · airframe 31,087 hrs · 27,848 cycles

MISDRILLED HOLE, DRILLED BESIDE NUTPLATE & UPPER NAV LIGHT TRANSFORMER REPAIR IAW REO 601R-55-32-299.

Part: BEAM — WORN (FLAP VANE) · airframe 31,087 hrs · 27,848 cycles

RIGHT INBD FLAP VANE ACTUATOR SLIDING BEAM HAS WEAR DAMAGE. REPAIRED WEAR DAMAGE IAW REO 601R-57-52-1864.

Part: BEAM — WORN (FLAP VANE) · airframe 31,087 hrs · 27,848 cycles

LEFT INBD FLAP VANE ACTUATOR OTBD AND CENTER SLIDING BEAM HAS WEAR. REPAIRED WEAR IAW REO 601R-57-52-1863.

Part: FLOORBEAM — CRACKED (FS 589) · airframe 31,087 hrs · 27,848 cycles

FLOORBEAM CAP IS CRACKED AT BS 589 UNDER CARGO DOOR SILL FLOOR SILL. REMOVED DAMAGED SECTION OF FLOORBEAM CAP, LOCATED, DRILLED AND INSTALLED NEW REPAIR SECTION IAW REO 601R-53-61-4419, REV.

Part: ATTACH FITTING — CRACKED (FS 589) · airframe 31,087 hrs · 27,848 cycles

ATTACH FITTING ON RIB AT BS 589 TO CARGO DOOR SILL CRACKED. REMOVED, FABRICATED AND INSTALLED NEW ATTACH FITTING IAW SRM 51-40-11, 51-42-21.

Part: DRAG ANGLE — CRACKED (AFT PAX DOOR) · airframe 31,087 hrs · 27,848 cycles

PAX DOOR AFT DRAG ANGLE APPEARS CRACKED IN AREA BY POWER ASSIST MOTOR CABLE PULLEY SUPPORT BRACKET. REMOVED CRACKED SECTION OF AFT DRAG ANGLE THEN INSTALLED NEW SECTION IAW REO 601R-52-11-513, REV.

Part: INTERCOSTAL — CRACKED (PAX DOOR) · airframe 31,087 hrs · 27,848 cycles

INTERCOSTAL APPEARS CRACKED IN PAX DOOR, UNDER PANEL 832NR. REMOVED CRACKED INTERCOSTAL ON AFT PAX DOOR UNDER PANEL 832BR, & INSTALLED NEW INTERCOSTAL.

Part: ANGLE — CHAFED (NACELLE) · airframe 31,087 hrs · 27,848 cycles

ANGLE ON L/E PANEL NR 421AL CHAFED. REMOVED ANGLE & INSTALLED SERVICEABLE ANGLE IAW SRM 51-42-06.

Part: RIB — DAMAGED (DOOR) · airframe 31,087 hrs · 27,848 cycles

AEB ENTRY DOOR HAS SUPPORT FRAMEWORK DAMAGED ( UNDER STRUCTURE). REPAIRED AEB ENTRY DOOR BY REMOVING DAMAGED RIB, DUPLICATED NEW RIB OF NEW MATERIAL AND INSTALLED SRM 51-24-16, 51-42-06.

Part: FLOOR PANEL — CRACKED (AVIONICS BAY) · airframe 31,087 hrs · 27,848 cycles

CRACK IN AVIONICS BAY FLOOR. REPAIRED CRACK IAW REO 601R-53-11-245, REV B.

Part: HEAT SHIELD — CRACKED (APU BAY) · airframe 31,087 hrs · 27,848 cycles

APU FWD HEAT SHIELD CRACKED AT 6 O`CLOCK POSITION. REPAIRED CRACK IAW REO 601R-49-81-003, REV B.

Part: STIFFENER — BROKEN (APU DOOR) · airframe 31,087 hrs · 27,848 cycles

APU ENCLOSURE DOOR HAS BROKEN WELD ON TOP STIFFENER AT AFT SIDE. REPAIRED CRACKS BY WELDING IAW REO 601R-49-11-070, REV A.

Part: BRACKET — CRACKED (FS 144-210) · airframe 31,087 hrs · 27,848 cycles

HYD ACCUMULATOR TOP, FWD, OTBD BRACKET CRACKED IN LT LOWER NOSE COMPARTMENT. REMOVED AND REPLACED BRACKET IAW SRM 51-42-06, 51-40-11, AND SRM 51-42-21.

Part: SEAT BACK — CRACKED (COCKPIT) · airframe 31,087 hrs · 27,848 cycles

CO-PILOT BACK REST PANEL FOUND TO BE CRACKED "UNDER METAL SHROUD". REMOVED CO-PILOT BACKREST PANEL AND INSTALLED SERVICEABLE BACKREST PANEL PN 1B3003-5R IAW SRM 51-42-13.

Part: ATTACH FITTING — CRACKED (FS 484.0) · airframe 31,087 hrs · 27,848 cycles

LEFT INTERCOSTAL CLIP OTBD OF LBL27 FS 484.0 IS CRACKED. REMOVED & REPLACED CLIP.

Part: FLOORBEAM — CRACKED (FS 280) · airframe 31,087 hrs · 27,848 cycles

OTBD FS 280 FLOORBEAM CRACKED RBL 9 CRACKED. FLOORBEAM REMOVED, FABRICATED, AND INSTALLED IAW REO 601R-53-11-171, REV D.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 31,087 hrs · 27,848 cycles

LT UPPER OBLIQUE ANGLE IS CRACKED. REMOVED CRACKED LT UPPER OBLIQUE ANGLE. INSTALLED NEW SERVICEABLE ANGLE.

Part: HOSE — LEAKING (HYD SYSTEM) · airframe 30,076 hrs · 26,803 cycles

HYD 2 LOW PRESSURE ACCOMPANIED BY COMPLETE FLUID LOSS. LARGE POOL OF FLUID UNDER NR 2 ENG. ENGINE OPERATING LESS THAN 1 MINUTE AFTER FLUID LOSS. R & R HYD NR 2 RESERVOIR ASSY IAW AMM 29-11-32 AND R & R PUMP IAW AMM 29-11-03. NO FIX. R & R PRESSURE HOSE ASSY AND CLAMP IAW AMM 29-11-52. OPS & LEAK CHECKED GOOD.

Part: BRACKET — CRACKED (NLG DOOR) · airframe 27,693 hrs · 24,287 cycles

SUSPECT CRACK NLG DOOR BRACKET FOR ACTUATOR. PERFORMED EDDY CURRENT INSP IAW AWAC NDT MANUAL. CONFIRMED NLG DOOR BRACKET IS CRACKED.

Part: OIL COOLER — CLOGGED (APU) · airframe 27,349 hrs · 23,924 cycles

APU OIL TEMP CAUTION MSG ILLUMINATED IN FLT C/W QRH. FOUND APU OIL COOLER PLUGGED, R & R COOLER IAW AMM 49-91-07 LEAK AND OPS CHECK GOOD.

Part: SKIN — CRACKED (PAX DOOR) · airframe 26,845 hrs · 23,375 cycles

PAX DOOR INNER SKIN IS CRACKED, RT SIDE JUST ABOVE LOWER TORQUE TUBE AT BASE OF THE STEP REPAIRED IAW REO 601R-52-11-1796, REV A.

Part: DOOR FRAME — CRACKED (BS 338) · airframe 26,845 hrs · 23,375 cycles

PAX DOOR FRAME AT FS 338 IS CRACKED AT BOTTOM OF STEPS REPAIRED IAW REO 601R-52-11-1793 AND REO 601R-52-11-402, REV H.

Part: HYDRAULIC SYSTEM — LOW (NR 1) · airframe 26,988 hrs · 23,523 cycles

AT CRUISE, HYD NR1 LO PRESS CAUTION, CW QRH PRESSURE WENT TO ZERO, DIVERTED. REPLACED FLEXIBLE PRESSURE LINE IN LT PYLON IAW AMM 29-11-01. LEAK CHECK GOOD AT THIS TIME.

Part: ANGLE — CORRODED (PAX DOOR) · corrosion level 3 · airframe 26,845 hrs · 23,375 cycles

AFTER REMOVAL OF FOAM RESIN DRAINAGE RAMP IN LWR PAX DOOR FOUND AFT LWR CORNER PIECE CORRODED. REMOVED DAMAGED CORNER AND REPLACED WITH NEW SERVICEABLE PART.

Part: LINE — LEAKING (APU FUEL) · airframe 26,972 hrs · 23,504 cycles

EXCESSIVE FUEL ODOR DETECTED IN COCKPIT AND CABIN WHILE ON APU BLEEDS. NOTED FUEL INSIDE APU C AREA WHEN APU IS OPERATED. CLEANED FUEL. R & R APU FUEL CONTROL FUEL LINE IAW AMM 49-30-01. OPS AND LEAK CHECKS GOOD AT THIS TIME. REMOVED FROM MEL.

Part: ANGLE — CRACKED (BS 280) · airframe 26,845 hrs · 23,375 cycles

CLIP AT FS 280 RBL 9 IS CRACKED. R & R CLIP WITH NEW REO 601R-53-11-926 REV B DATED 5/10/2006.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 26,845 hrs · 23,375 cycles

FS 280 UPPER CAP CRACKED AT RBL 10.0 AND LBL 10.0. R & R CLIP IAW SRM PROCEDURES AND REO 601R-53-11-926, REV B DABE 5/10/2006.

Part: BRACKET — CORRODED (BS 559+16) · corrosion level 2 · airframe 26,845 hrs · 23,375 cycles

SMALL GREEN LIGHT ASSY AND MOUNTING BRACKET IN LAV SERVICE AREA ARE CORRODED. REMOVED UNSERVICEABLE BRACKET AND REPLACED SERVICEABLE BRACKET P/N 601R520701-55 IN LAV SERVICE AREA IAW SRM 51-41-02 A, AMM 38-31-15-000-801.

Part: BULKHEAD — CORRODED (BS 280) · corrosion level 2 · airframe 26,845 hrs · 23,375 cycles

AFT SIDE OF THE FS 280 BULKHEAD IS CORRODED AT THE BASE ON THE RT OF THE COCKPIT ENTRANCE. REPAIRED REO 601R-53-11-926 REV B DATE 05/10/06.

Part: SKIN — CRACKED (RT WING) · airframe 26,845 hrs · 22,375 cycles

RT L/E 620JL INNER SHROUD CRACKED AT ACCESS PANEL 620CZ OTBD MATING SURFACE R & R INNER SHROUD INSTALLED IAW SRM 51-42-13 & 51-42-06.

Part: SKIN — CHAFED (RT AILERON) · airframe 26,845 hrs · 23,375 cycles

RT AILERON L/E UPPER SURFACE IS CHAFED. REPAIR DAMAGE ON RT AILERON L/E UPPER SURFACE IAW REO 601R-57-60-013, REV NC 2000-11-20 AND REO 601R-57-60-073, REV A 2010-4-22.

Part: SEAL — CRACKED (THRUST REVERSER) · airframe 26,845 hrs · 23,375 cycles

LT T/R METAL SEAL CRACKED. R & R SEAL IAW SHORTS CMM 78-30-00, REPAIR NR SRS 077.

Part: ATTACH FITTING — CHAFED (BS 473.15) · airframe 26,845 hrs · 23,375 cycles

RT WING ATTACH FITTING HAS CHAFING DAMAGE OF FWD END OF FITTING. FS 473.15 TO BE REPAIRED BY REO 601R-57-21-1274.

Part: BULKHEAD — CRACKED (BS 559) · airframe 26,845 hrs · 23,375 cycles

FS 559.00 BULKHEAD JUST OTBD OF RBL9 AND APPROX WL 58.70 HAS CRACK INDICATION REO 601R-53-41-260, REV D. DATED 9/17/09 AND REO 601R-53-41-609, REV B, DATED 12/18/09 DEVIATION E.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 26,845 hrs · 23,375 cycles

CRACKED ANGLE FS 484, RBL 28. (ANGLE LOCATED ON FLOOR SUPPORT INTERCOSTAL OTBD END AT RBL 28) REPAIRED IAW REO 601R-53-41-059.

Part: ANGLE — CRACKED (BS 484) · airframe 26,845 hrs · 23,375 cycles

CRACKED ANGLE FS 484, RBL 36. REPAIRED IAW REO 601R-53-41-059.

Part: ANGLE — CRACKED (BS 484) · airframe 26,845 hrs · 13,375 cycles

CRACKED ANGLE AT FS 484.0, LBL 36. REPAIR IAW GREO 601R-53-41-059.

Part: ANGLE — CRACKED (BS 625) · airframe 26,845 hrs · 23,375 cycles

RT 625, OBLIQUE ANGLE CRACKED. DUPLICATE AND REPLACE IAW SRM PROCEDURES 51-42-21.

Part: SKIN — CRACKED (BS 235) · airframe 26,845 hrs · 23,375 cycles

FUSELAGE SKIN CRACKED AT AFT LT CORNER OF NLG WHEEL WELL CUT OUT. REPAIR IAW REO 601R-53-11-048.

Part: ANTENNA — ERRATIC (GLIDE SLOPE) · airframe 24,441 hrs · 20,972 cycles

NAV 1 AND NAV 2 INDICATED ERRATIC GLIDE SLOPE INDICATIONS FOLLOWED BY ERRONEOUS INDICATION AND GLIDE SLOPE FLAG WHILE OTHER ACFT RECEIVED NAV-AID RECEPTION. REMOVED AND REPLACED GLIDE SLOPE ANTENNA IAW AMM 34-51-11. OPS CHECK GOOD. (K)

Part: STARTER — MALFUNCTIONED (APU) · airframe 23,943 hrs · 20,485 cycles

DURING APU START EGT 715, RPM 6 FLAMES REPORTED SHOOTING OUT OF THE EXHAUST CM ACTION C/W PLACED ON MEL. R&R APU STARTER PER AMM 49-41-07. OPS CHECK GOOD. APU PARAMETERS NORMAL. REMOVED FROM MEL. PLACARD REMOVED.

Part: SKIN — CRACKED (RT WING LE)

RIGHT WING L/E AT WS 185.95 QTY 1 L/E SCREW HOLE IS CRACKED IN THE L/E EXTERIOR SKIN AND EDGING. (M) REPLACED IAW REO 601R-57-41-510. (A)

Part: ANGLE — CRACKED (RT WING) · airframe 22,254 hrs · 18,863 cycles

RIGHT WING, L/E EDGE 630JL, ANGLE CRACKED AT WS 149.58. (M) ANGLE REPLACED IAW SRM 51-41-02.

Part: SILL — CORRODED (FUSELAGE) · airframe 22,254 hrs · 18,863 cycles

CARGO DOOR AREA, LOWER SILL PLATE IS CORRODED. CORROSION REMOVED IAW SRM 51-21-06. (M)

Part: BULKHEAD — CRACKED (BS 202) · airframe 22,254 hrs · 18,863 cycles

CRACK EXIST ON FORWARD PRESSURE BULKHEAD F/S 202.75 BL 45, WL 69, 684 AROUND PARKING BRAKE (.250 LONG). (M) FWD PRESSURE BULKHEAD REPAIRED IAW REO 601R5311536. (P)

Part: SNUBBER — CRACKED (THRUST REVERSER) · airframe 22,254 hrs · 18,863 cycles

NR 1 T/R ACTUATOR AT 2 O`CLOCK POSITION SNUBBER AND SNUBBER COVER FOUND CRACKED AND BRACKET. (K) REPLACED SNUBBER AND SNUBBER COVER IAW SRM 51-42-06.

Part: SNUBBER — CRACKED (THRUST REVERSER) · airframe 22,254 hrs · 18,863 cycles

T/R ACTUATOR AT 1 O`CLOCK POSITION, SNUBBER AND SNUBBER COVER FOUND CRACKED. (K) REPLACED IAW SRM 51-42-06.

Part: STRUCTURE — MISSING (RUDDER) · airframe 22,254 hrs · 18,863 cycles

RUDDER LOWER CLOSURE RIB CLOTH MISSING. (M) RUDDER LOWER CLOSURE RIB DIAPHRAGMS REPAIR IAW 601R-55-41-018.

Part: PLATE — CRACKED (BS 589) · airframe 22,254 hrs · 18,863 cycles

CARGO DOOR FLOOR LANDING PLATE CRACKED AT FS 589. (M) CARGO DOOR FLOOR LANDING PLATE REPAIRED IAW REO 601R-53-61-433. (A)

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 22,254 hrs · 18,863 cycles

CRACK FOUND AT FS 484 LBL 36 WL 73. CRACK REPAIRED AT FS 484 LBL 36 WL 73.00 IAW REO 601R-53-41-059 REV A. (A)

Part: STRUCTURE — CORRODED (PAX DOOR) · airframe 22,254 hrs · 18,863 cycles

CORROSION EXIST ON FORWARD CLEAT AND AFT CLEAT OF PAX DOOR BETWEEN FS 313 AND FS 346. (M) CORROSION REMOVED ON BOTH CLEATS IAW SRM. (A)

Part: STRUCTURE — CRACKED (PAX DOOR) · airframe 22,254 hrs · 18,863 cycles

REPAIR CRACK IN PAX DOOR AT AFT EDGE MEMBER. (M)

Part: SILL — CRACKED (BS 575) · airframe 22,254 hrs · 18,863 cycles

CARGO BAY FLOOR SILL CRACKED AT FS 575. (M) REPAIR PERFORMED ON CARGO DOOR SURROUND LOWER SILL AT FS 575 IAW REO 601R-53-61-1741. (A)

Part: STRUCTURE — CRACKED (PAX DOOR) · airframe 22,254 hrs · 18,863 cycles

REPAIR CRACK IN PAX DOOR AT AFT EDGE MEMBER. PAX DOOR AT AFT EDGE MEMBER REPAIRED IAW CRJ 200 REO 601R-52-11-279. (A)

Part: STRUCTURE — MISSING (RUDDER) · airframe 22,254 hrs · 18,863 cycles

RUDDER UPPER CLOSING RIB CLOTH MISSING. (M) REPAIRED IAW REO 601R-55-41-037 REV A.

Part: DIAPHRAGM — MISSING (STAB DRAG ANGLE) · airframe 22,254 hrs · 18,863 cycles

STABILIZER DRAG ANGLE DIAPHRAGM CLOTH MISSING. (M) REPAIRED IAW REO 601R-55-32-075 REV E.

Part: BRACKET — CRACKED (LT WING) · airframe 22,254 hrs · 18,863 cycles

ANGLE BRACKET FOUND CRACK ON LT WING WS 148.019, CRACK LENGTH .500. (M) NEW ANGLE BRACKET INSTALLED IAW 51-41-02 QND SRM 51-41-04 (A)

Part: BRACKET — CRACKED (LT WING) · airframe 22,254 hrs · 18,863 cycles

ON LEFT WING ANGLE BRACKET FOUND CRACK, CRACK LENGTH .900. (M) REPLACED ON LEFT WING AT WS 149.58 IAW SRM 51-41-02 AND SRM 51-41-04 (A)

Part: FLOOR SUPPORT — CORRODED (BS 319) · airframe 22,254 hrs · 18,863 cycles

CORROSION FOUND AT SERVICE DOOR FORWARD LOWER FRAME TO FLOOR SUPPORT BRACKET, FS 319. (M) SUPPORT BRACKET REPLACED IAW SRM 51-42-21.

Part: FLOOR SUPPORT — CORRODED (BS 319-349) · corrosion level 2 · airframe 22,254 hrs · 18,863 cycles

FLOOR SUPPORT ANGLE BTW FS 319.70 AND FS 349.0 IB OF SERVICE DOOR, BTW RBL 27.00, FOUND CORRODED. (K) FLOOR SUPPORT FABRICATED WITH FORMED ANGLE RAW MATERIAL P/N S6144-14 IAW SRM 51-24-21 AND INSTALL IAW SRM 51-42-06.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 22,115 hrs · 18,729 cycles

FLAPS FAIL CAS MESSAGE AFTER LANDING WHEN FLAPS SELECTED TO ZERO POSITION, FLAPS READ 45 DEGREES LT, 45 DEGREES RT. (M)

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 22,128 hrs · 18,742 cycles

FLAPS FAIL CAS MESSAGE AFTER LANDING WHEN FLAPS SELECTED TO ZERO FLAPS READ ZERO ON FLIGHT CONTROL PAGE. COMPLIED WITH RESET PROCEDURE IAW AWAC SUPP 98-018B STEPS 1.3 AND 1.4, FLAPS RESET AIRCRAFT RELEASED FOR SERVICE. (M)

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 21,626 hrs · 18,272 cycles

CRACK FOUND ON AFT PRESSURE BULKHEAD FWD FACE IN LINTEL FITTING ARE FS 621.00 LT. REPAIR PERFORMED ON AFT PRESSURE BULKHEAD FWD FACE IN LINTER FITTING AREA AT FS 621.00 LT IAW REO 601R-53-61-1230, REV C. (K)

Part: PROXIMITY SWITCH — MALFUNCTIONED (PAX DOOR)

CLIMBING THRU 14,000 FT GOT PAX DOOR LATCH CAUTION MESSAGE, FOLLOWED BY PAX DOOR (RED) WARNING MESSAGE, COMPLIED WITH QRH NO PRESSURIZATION PROBLEM NOTED. NO ABNORMAL NOISE OR ALIGNMENT INDICATION NOTED. DIVERTED, RED WARNING MESSAGE CLEARED BELOW 16,000 FT, AND PAX DOOR LATCH MESSAGE RETURNED ALL MESSAGES OUT BELOW 3,000 FT. LANDING WEIGHT 45,400 LBS. SEE CROSS REFERENCE SDR A6WA200740095. (REMOVED AND REPLACED PS5MB AND PS6MB, OPS CHECK GOOD). (K)

Part: PROXIMITY SWITCH — DEFECTIVE (PAX DOOR)

INFLIGHT, PAX DOOR WARNING MESSAGE. COMPLIED WITH QRH CHECKLIST, LANDED AT 46,000. REMOVED AND REPLACED PS5MB AND PS6MB PROXIMITY SWITCHES IAW AMM 52-70-04. OPS CHECK OF PASSENGER DOOR GOOD. PSEU FOUND NO FAULTS. (K)

Part: PROXIMITY SENSOR — FALSE INDICATION (PAX DOOR)

PASSENGER DOOR LATCH CAUTION MESSAGE IN FLIGHT, COMPLIED WITH QRH. REMOVED AND REPLACED PASSENGER DOOR PROXIMITY SWITCH IAW CRJ AMM 5270-04, SYSTEM OPS CHECK GOOD. (M)

Part: SENSOR — DIRTY (PAX DOOR)

PASSENGER DOOR LATCH MESSAGE, FOLLOWED BY RED PASSENGER DOOR MESSAGE COMPLIED WITH QRH. PRESSURIZATION NORMAL AND POSSIBLE OVERWEIGHT LANDING AT 48,600 LBS. FOUND "$47 FAR" AND"$46 FAR" IN PSEU. CLEARED DEBRIS FOR LATCH SENSOR PASSENGER DOOR WARNING SYSTEM, OPS CHECK GOOD AT THIS TIME. PSI`D AIRCRAFT. PASSENGER INDICATES GOOD RED 52-70-04. (M)

Part: MANIFOLD — INOPERATIVE (NLG NWS SERVO) · airframe 18,871 hrs · 15,663 cycles

STEERING INOP DURING TAXI. REMOVED AND REPLACED NOSEWHEEL STEERING SERVO MANIFOLD AMM. OPS AND LEAK CHECK GOOD. (K)

Part: HANDLE — OUT OF ADJUST (PAX DOOR)

PASSENGER DOOR WILL NOT OPEN FROM INSIDE, OPS OPENED FROM OUTSIDE. CLEANED AND ADJUSTED PASSENGER DOOR HANDLE IAW AMM 52, LUBED AS REQUIRED, OPS CHECK GOOD. (M)

Part: HANDLE — LACK OF LUBE (PAX DOOR)

FOUND PASSENGER DOOR HANDLE HARD TO OPEN FROM INSIDE. CLEANED AND LUBED INNER AND OUTER PASSENGER DOOR HANDLE IAW AMM 52-10-00, OPS CHECK GOOD. (M)

Part: FIRE BOTTLE — DISCHARGED (LT/RT)

ENGINE FIRE BOTTLES NR 1 AND NR 2 WERE FOUND DISCHARGED AT THE GATE. REMOVED AND REPLACED FIRE BOTTLES. (M)

Part: ANGLE — CRACKED (FUSELAGE) · airframe 14,208 hrs · 14,187 cycles

FS 484 ANGLE CRACKED AT LBL 27.0 APPROX .75 INCH LONG. (K) MAINTENANCE REPAIRED CRACKED ANGLE AT LBL 27 FS 484 BY REMOVING AND REPLACING ANGLE IAW BSC STANDARD REPAIR 601R-53-0029A. (M)

Part: SKIN — DENTED (TE FLAP) · airframe 14,208 hrs · 14,187 cycles

RT IB FLAP HAS A SMALL DENT ON BOTTOM OF FLAP AT WS 65.75 .5 INCH LONG X .2500 INCH WIDE X .006 DEEP. (K) MAINTENANCE REPAIRED DENT ON BOTTOM OF FLAP AT WS 65.75 BY CUTTING OUT DAMAGE, FABRICATED REPAIR DOUBLER, PERFORMED EDDY CURRENT INSPECTION AND INSTALLED DOUBLER IAW CRJ200 SRM 57-52-00 REPAIR NR 3. (M)

Part: PLATE — CRACKED (FUSELAGE) · airframe 14,208 hrs · 14,187 cycles

CARGO BAY ENTRANCE HAS A CRACKED FLOOR SILL PLATE AT FS 605 AND WL 97.50, LBL 45 APPROX .2500 INCH LONG. (K)

Part: SKIN — CORRODED (WING) · corrosion level 1 · airframe 14,208 hrs · 14,187 cycles

RT WING LOWER PLANK FUEL ACCESS PANEL 640BB CUT-OUT HAS MINOR CORROSION AT THE IB RADIUS AND THE FWD MID EDGE WHICH IS IN THE CRITICAL REGION. (K) MAINTENANCE REPAIRED MINOR CORROSION ON FUEL TANK ACCESS PANEL (640BB) CUTOUT (IN CRITICAL AREA) BY BLENDING OUT DAMAGE, PERFORMING EDDY CURRENT INSPECTION, SHOT PEENED REWORKED AREA, AND REAPPLYING PROACTIVE COATING IAW BOMBARDIER REO 601R-57-21-030 REV D. (M)

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 1 · airframe 14,208 hrs · 14,187 cycles

LT WING LOWER PLANK FUEL TANK ACCESS PANEL 110AB CUT-OUT HAS MINOR CORROSION AT IB RADIUS. NOT IN CRITICAL REGION. (K) REPAIRED FUEL TANK ACCESS PANEL 510AB CUTOUT IAW BOMBARDIER REO 601R-57-21-030 REV D. (M)

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 1 · airframe 14,208 hrs · 14,187 cycles

LT WING PLANK LOWER FUEL ACCESS PANEL 540BB CUT-OUT HAS MINOR CORROSION AT C/B RADIUS NOT IN CRITICAL REGION. (K) MAINTENANCE REPAIRED MINOR CORROSION ON FUEL ACCESS PANEL (540BB) CUTOUT BY BLENDING OUT DAMAGE, PERFORMING EDDY CURRENT INSPECTION, SHOT PEENED REWORKED AREA, AND RE-APPLYING PROTECTIVE COATING, IAW BOMBARDIER REO 601R-57-21-030 REV D. (M)

Part: INTERCOSTAL — CRACKED (BS 621-625)

FOUND LEFT SIDE FS 621 TO FS 625.3 INTERCOSTAL AT STRINGER 14L IS CRACKED NEAR RADIUS APPROXIMATELY .80 INCH LONG. MAINTENANCE AFTER FURTHER INVESTIGATION FOUND INTERCOSTAL NOT TO BE CRACKED, ONLY DEFECT IN PAINT. (M)

Part: A/C PACK — SMOKE (RIGHT) · airframe 15,512 hrs · 12,428 cycles

RT PACK HIGH TEMP MESSAGE, PACK SHUTDOWN, SMOKE IN CABIN AND COCKPIT. (K)

Part: CONNECTOR — CONTAMINATED (CABIN COOLING) · airframe 14,894 hrs · 11,882 cycles

OVERBOARD COOL CAUTION AND IB COOL STATUS MESSAGE. INSPECTED DOOR AND FOUND CONNECTOR INSIDE DOOR WET. CLEANED AND DRIED CONNECTOR PLUG. OPS CHECK GOOD. (K)

Part: SEAL — FAILED (NLG STRUT) · airframe 14,484 hrs · 11,533 cycles

AFTER TAKEOFF, RECEIVED RED NOSE DOOR GEAR MESSAGE AND RED GEAR DISAGREE MESSAGE. REMOVED AND REPLACED NOSE LANDING GEAR STRUT SEALS. RESERVICED NLG STRUT, OPS CHECK GOOD. (K)

Part: SPLICE — WRONG PART (EMERGENCY LIGHT) · airframe 13,999 hrs · 11,102 cycles

FLOOR TRACK LIGHTING HAS WRONG SPLICES AT ROW NR 12. REMOVED AND REPLACED SPLICES AT ROW NR 12 IAW CRJ 200 WIRING MANUAL 20-17-10.

Part: SPLICE — BROKEN (EMERGENCY LIGHT) · airframe 13,999 hrs · 11,102 cycles

FLOOR TRACK LIGHTING HAS A BROKEN SPLICE AT ROW NR 8. REMOVED AND REPLACED SPLICE AT ROW NR 8 IAW CRJ 200 WIRING MANUAL 20-17-10.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 13,972 hrs · 11,079 cycles

FS 280, LBL9 OB ANGLE PN 601R31113-57 IS CRACKED IN RADIUS AT WL 73. REMOVED AND REPLACED ANGLE WITH PRE-FABBED ANGLE IAW REO 601R-53-11-171 REV A AND BRAS EO 601R-53-5547.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 13,972 hrs · 11,079 cycles

FS280 UNDER FLOORBEAM AT LBL 12 AND WL 69 LOWER FLANGE IS CRACKED. CUT AWAY DAMAGED SECTION OF FLOOR ANGLE, PERFORMED LPI TO ENSURE NO CRACKS EXIST. FAB REPAIR ANGLE AND FILLER FROM S-6144-3, S-6144-13 AND INSTALLED WET USING SOLID RIVETS AND LOCK FASTENERS. IAW REO 601R-53-11-171 REV A AND BRAS EO 6012-53-5547.

Part: PLATE — CORRODED (SERVICE DOOR) · airframe 14,024 hrs · 11,133 cycles

SERVICE DOOR RAMP PLATE, PN 601R38957-19, CORRODED AROUND OPENINGS AND FASTENER HOLES. REPLACED RAMP PLATE WITH NEW RAMP PLATE IAW SRM 51-41-02.

Part: PLATE — CORRODED (SERVICE DOOR) · airframe 3,972 hrs

SERVICE DOOR RAMP PLATE, PN 601R38957-19, CORRODED AROUND OPENINGS AND FASTENER HOLES. REPLACED RAMP PLATE WITH NEW RAMP PLATE IAW SRM 51-41.02.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 13,972 hrs · 11,079 cycles

FS 280 UNDER FLOORBEAM AT RBL 12 AND WL 69 LOWER FLANGE IS CRACKED. CUT AWAY DAMAGED SECTION OF FLOOR ANGLE, PERFORMED LPI TO ENSURE NO CRACKS EXIST. FABRICATED REPAIR ANGLE AND FILLER FROM S-6744-3 AND S6744-13 AND INSTALLED WET USING SOLID RIVETS AND LOCK FASTENERS. ALL WORK DONE IAW REO 601R-53-11-131 REV A AND EO 601R-53-5547.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 13,972 hrs · 11,079 cycles

FS 280, RBL 9 IB ANGLE PN 601R3113-58 IS CRACKED IN RADIUS AT WLK 73. REMOVED AND REPLACED ANGLE WITH NEW ANGLE PN 601R3113-58 IAW SRM 51-42-06 AND 51-42-21.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 13,972 hrs · 11,079 cycles

FS 280, RBL 9 OB ANGLE PN 601R31113-58 IS CRACKED IN RADIUS AT WL73. REMOVED AND REPLACED ANGLE WITH PRE-FABBED ANGLE IAW REO 601R53-11-171 REV A AND BRAS EO 601R-53-5447 AND M.

Part: STRUCTURE — DAMAGED (PUMP SUPPORT) · airframe 14,024 hrs · 11,133 cycles

LT BOOST PUMP CANISTER SATELLITE HOLE AFT SIDE LBL 11.18 FAILED EDDY CURRENT INSPECTION. INDICATION NOTED ON OB SIDE OF HOLE. REPAIRED SATELLITE HOLE BY REAMING THE HOLE TO .4150 AND INSTALLING A FREEZE PLUG. (OD EO 601R-57-21-526).

Part: RIB — CRACKED (RT WING) · airframe 13,972 hrs · 11,079 cycles

RT WS 53.60 BATT RIB ASSY IS CRACKED, 1 INCH LONG IN AFT UPPER RADIUS. REPAIRED BATT RIB ASSY BY CUTTING OUT DAMAGED SECTION. FABBED REPAIR ANGLE FROM S6144-0 AND FILLER FROM 7075T62 P.O. NR 35850, INSTALLED REPAIR PARTS WET USING SOLID RIVETS AND HI-LIGHT FASTENERS. ALL WORK DONE IAW REO 601R-57-51-046, REV B AND EO 601R-57-5541.

Part: RIB — CRACKED (WING) · airframe 13,972 hrs · 11,079 cycles

BATT RIB ASSY IS CRACKED 1.2500 INCH LONG IN AFT UPPER RADIUS. CORRECTIVE ACTION IN PROGRESS.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 13,972 hrs · 11,079 cycles

INTERCOSTAL AT FS 484 LT SIDE IS CRACKED NEAR RADIUS OF ATTACHMENT FLANGE AT LBL36. CUT AWAY DAMAGED ATTACHMENT ANGLE. PERFORMED LPI TO ENSURE NO CRACKS EXIST, FAB REPLACEMENT ANGLE FROM 6144-14 AND INSTALLED USING SOLID RIVETS AND HI-LITE FASTENERS. ALL WORK DONE IAW REO 601R53-41-059, REV A AND BRAS. STANDARD REPAIR 601R5.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 13,972 hrs · 11,079 cycles

INTERCOSTAL LT SIDE IS CRACKED NEAR RADIUS OF ATTACHMENT FLANGE AT LBL 36. CUT AWAY DAMAGED ATTACHMENT ANGLE. PERFORMED LPI TO ENSURE NO CRACKS EXIT, FAB REPLACEMENT ANGLE FROM 6144-14 AND INSTALLED USING SOLID RIVETS AND HI-LITE FASTENERS. ALL WORK DONE IAW REO 601R-53-41-059, REV A AND BRAS STANDARD REPAIR 601R5.

Part: ACTUATOR — FAILED (MACH TRIM)

MACH AND STAB TRIM FAIL. REMOVED AND REPLACED HST ACTUATOR IAW AMM 27-42-01. (M)

Part: GENERATOR — FAILED (NR 2)

NR 2 GENERATOR FAILED DURNG TAKEOFF. SERVICED NR 2 IDG IAW AMM 12-13-24. RAN ENGINE TO POWER. OPS CHECK GOOD. (M)

Part: DUCT — DAMAGED (CABIN AIR)

PASSING THROUGH 10K FEET NOTICED LACK OF AIRFLOW. SWITCHED TO APU AIR. NO HELP PASSING THROUGH 22K FEET. RECEIVED 'CABIN HI ALT' MESSAGE. PERFORMED EMERGENCY DESCENT. DECLARED EMERGENCY AND RETURNED TO ORD. REMOVED AND REPLACED DUCT. REMOVED AND REPLACED CHECK VALVE (P/N 92E20-3) AND WATER SEPARATOR, P/N 601R95251-15. (M)

Part: SKIN — LIGHTNING STRIKE (FUSELAGE) · airframe 12,312 hrs · 9,692 cycles

RIVET ON RT FUSELAGE SKIN AT FS 265.00 BETWEEN STRINGERS 22 AND 23 HAS LIGHTNING DAMAGE THAT EXTENDS BEYOND COUNTERSINK HOLE IN SKIN. (ADDTNL INFO-WO 59971 MWC 22) REMOVED FASTENER, ENLARGED FASTENER HOLE TO A NOMINAL .1875 DIAMETER, PERFORMED EDDY CURRENT TO ENSURE NO CRACKS EXISTED AND DAMAGE WAS REMOVED, INSTALLED FASTENER NAS1097AD6 WET USING PR1422B1/2 IAW WVAC EO 601R-53-4578.

Part: SKIN — LIGHTNING STRIKE (FUSELAGE)

RIVET ON RIGHT FUSELAGE SKIN AT FS 265 BETWEEN STRINGERS 22 AND 23 HAS LIGHTNING DAMAGE THAT EXTENDS BEYOND COUNTERSINK HOLE IN SKIN. REMOVED FASTENER, ENLARGED FASTENER HOLE TO A NOMINAL .1875 INCH DIAMETER, PERFORMED EDDY CURRENT TO ENSURE NO CRACKS EXISTED AND DAMAGE WAS REMOVED. INSTALLED FASTENER NAS1097AD6 WET USING PR1422B1/2 IAW WVAC EO 601R-53-4578. (M)

Part: CONTROL UNIT — FAILED (SPOILER)

CAPTAINS SIDE PILOTS 'ROLL' LIGHT ILLUMINATED WITH ASSOCIATED ADVISORY MESSAGE ON ED2 ON ARRIVING IN GATE. MESSAGE CLEARED WITH SECU BITE TEST. PERFORMED SYSTEM TEST AND FOUND INTERNAL SECU (SPOILER ELECT CONTROL UNIT) FAILURE. REPLACED NR 1 SECU IAW AMM. OPS CHECK GOOD. (M)

Part: CONTROLLER — FAILED (RT WINDOW) · airframe 10,440 hrs · 8,030 cycles

RT WINDOW HEAT CAUTION MESSAGE REMOVED AND REPLACED WINDOW HEAT CONTROLLER IAW AMM 30-41-01. OPS CHECK GOOD A THIS TIME.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE)

FOUND SUPPORT ANGLES AT FS 484 RIGHT SIDE OF CABIN FLOOR LEVEL ARE CRACKED. CUT AWAY CRACKED FLANGE AND REMOVED INBOARD ANGLE FABRICATED ANGLES. INSTALLED REPAIR IAW WVAC EO 601R-53-37281. (M)

Part: BRACKET — DAMAGED (FUSELAGE)

HYDRAULIC BRACKET AT FS 656 RT SIDE AT STRINGER 9 HAS AN ELONGATED THRU HOLE AT HYDRAULIC PRESSURE LINE REMOVED BRACKET, REPAIRED, AND REINSTALLED. PERFORMED NDT WITH NO INDICATIONS NOTED.

Part: BRACKET — DAMAGED (FUSELAGE)

HYDRAULIC BRACKET AT FS 656 LT SIDE AT STRINGER 9 HAS AN ELONGATED THRU HOLE AT HYDRAULIC PRESSURE LINE REMOVED, REPAIRED, AND INSTALLED BRACKET. NDT PERFORMED, NO INDICATIONS NOTED.

Part: FRAME — CRACKED (FUSELAGE)

FS FRAME 718 IS CRACKED .25 INCHES AT TOP RIVET HOLE AT STRINGER 11 LT SIDE, INCORPORATED MFG REO 601R-53-61-193 REV A.

Part: ANGLE — CRACKED (FUSELAGE)

OBLIQUE ANGLE AT FS 625 LT SIDE IS CRACKED ONE INCH IN RADIUS. REMOVED AND REPLACED CRACKED OBLIQUE ANGLE AT FS 625 LT SIDE WITH NEW.

Part: ANGLE — CRACKED (FUSELAGE)

OBLIQUE ANGLE AT FS 625 RT SIDE IS CRACKED 1 INCH IN RADIUS REMOVED AND REPLACED CRACKED OBLIQUE ANGLE AT FS 625 RIGHT SIDE.

Part: ACCESS PANEL — DAMAGED (FUSELAGE)

RT BOOST PUMP ACCESS HOLE HAS FAILED FASTENER HOLE AT 1:00 O`CLOCK POSITION PERFORMED REPAIRS NR 1 AND NR 2 OF REO 601R-57-21-169 BY OPENING UP HOLE. FABRICATING BUSHING AND INSTALLING BUSHING.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE)

FOUND FLOOR SUPPORT STRUCTURE AT FS 621 CRACKED AT LEFT AND RIGHT SIDES COMPLIED WITH REO 601R-53-61-004 REV B. (M)

Part: FLOOR SUPPORT — CRACKED (FUSELAGE)

FOUND FLOOR SUPPORT STRUCTURE AT FS 621, CRACKED AT LEFT AND RIGHT SIDES COMPLIED WITH REO 601R-53-6-004 REV B. (M)

Part: WARNING SYSTEM — FALSE INDICATION (COCKPIT)

PAX DOOR OUTER HANDLE CAUTION MESSAGE AT 17,000 FT AIRCRAFT ALTITUDE. 100 CABIN ALTITUDE DIFF PRESS 6.3 MESSAGE DISAPPEARS WHEN DOOR WAS OPENED AT THE GATE.

Part: HANDLE — OUT OF POSITION (PAX DOOR) · airframe 8,555 hrs · 6,531 cycles

PAX DOOR OUTER HANDLE MESSAGE ON CLIMB OUT (12,000 FT) INNER STOW HANDLE WILL NOT STOW CORRECTLY. MESSAGE WENT AWAY WHEN PRESS ON GROUND. ON CALL MAINTENANCE INSPECTED DOOR AND SURROUNDING AREA, NO DEFECTS. PRESSURIZED AIRCRAFT. NO OBVIOUS DEFECTS, CYCLED DOOR OPEN AND CLOSED SEVERAL TIMES DOOR OPS NORMAL.

Part: CONTROLLER — FAILED (COCKPIT)

CAPTAINS SIDE WINDOW HEAT FAIL, RETURN TO DENVER. MAINTENANCE REMOVED AND REPLACED LEFT SIDE WINDSHIELD HEAT CONTROLLER. OPS CHECK GOOD. (M)