N449AW

Part: BULKHEAD WEB — CRACKED (AFT) · airframe 38,204 hrs · 37,521 cycles

1" CRACK DETECTED ON FWD FACE OF AFT PRESSURE BULKHEAD AT LBL 27.50. 36" ABOVE FLOOR LEVEL ***AIRCRAFT REMOVED FROM SERVICE*** REPAIRED CRACK OF FWD FACE OF AFT PRESSURE BULKHEAD AT LBL 27.50 36 INCHES ABOVE FLOOR LEVEL IAW BOMBARDIER REO 601R-53-61-1285 REV C

Part: SEAT TRACK — CORRODED (BS 559) · corrosion level 2 · airframe 38,204 hrs · 37,521 cycles

LBL 27 AT FS 559+65 TO FS 559+81 SEAT TRACK HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED SEAT TRACK AT LBL 27 AT FS 559+65 TO FS 559+81, IAW REO 601R-53-00-764 AND CRJ 200 SRM 51-42-20.

Part: BEAM — CORRODED (FS 559-605) · corrosion level 2 · airframe 38,204 hrs · 37,521 cycles

LBL 27 AT FS 559+20 TO FS 605 T CAP EXTRUSION HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED T CAP AT LBL 27 FS 559=20 TO FS 605, IAW DRAWING 601R35031.

Part: STRUCTURE — CORRODED (BS 559) · corrosion level 2 · airframe 38,204 hrs · 37,521 cycles

LBL 27 AT FS 559 +80 TO FS 559+120 T CAP EXTRUSION HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED T CAP EXTRUSION, LBL 27 AT FS 559 +80 TO FS 559+120, IAW DRAWING 601R35031 AND CRJ 200 SRM 51-42-20.

Part: WARNING MESSAGE — ILLUMINATED (DUCT) · airframe 37,269 hrs · 36,616 cycles

ON INITIAL CLIMB L 14TH DUCT WARNING MESSAGE DISPLAYED. WARNING DID NOT EXTINGUISH, PER THE QRH THE FLIGHT RETURNED TO EVV WITH NO FURTHER ISSUES.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 36,022 hrs · 35,387 cycles

IN CRUISE, RECEIVED L REV UNLOCKED CAUTION MESSAGE. PERFORMED IAC AND QRH, MESSAGE REMAINED. COMPLETED THE QRH, COORDINATED WITH DISPATCH, DECLARED AN EMERGENCY WITH ATC AND LANDED AT NEAREST AIRPORT PER QRH. REVERSER APPEARED TO BE IN STOWED POSITION. N1 REV ICON WAS AMBER.

Part: UNKNOWN — ODOR (COCKPIT & CABIN) · airframe 35,735 hrs · 35,113 cycles

FOLLOWING A FAILED START ATTEMPT OF THE APU IN FLIGHT AND A 2 MINUTE COOL DOWN AND A SUCCESSFUL START. THERE WAS A VERY STRONG ODOR OF FUEL IN THE COCKPIT AND CABIN. SHUT DOWN THE APU AND ODOR DISSIPATED. CW OPERATIONAL CHECK OF APU IAW AMM 49-10-00. OPS CHECK GOOD. BOTH PACKS ON APU AIR ONLY. NO UNUSUAL ODORS DETECTED. SUSPECT RESIDUAL FUEL FROM FAILED 1ST START ATTEMPT CLEARED AND NEXT APU START.

Part: SKIN — DAMAGED (TE FLAP) · airframe 35,079 hrs · 34,499 cycles

RIGHT INBOARD FLAP, LOWER SKIN DINGED AND PTTED. REMOVED AND REPLACED RT IB FLAP IB LOWER SKIN IAW SRM 51-42-13.

Part: SKIN — DAMAGED (TE FLAP) · airframe 35,079 hrs · 34,499 cycles

LEFT INBOARD FLAP LOWER IB SKIN DINGED AND PITTED. REMOVED AND REPLACED LH IB FLAP IB LOWER SKIN IAW SRM 51-42-13.

Part: SKIN — DENTED (FUSELAGE) · airframe 35,079 hrs · 34,499 cycles

DENT AT FS 589 BELOW CARGO DOOR REPAIRED. REPAIR DENT AT FS 589 BELOW CARGO DOOR IAW EA AWAC-CRJ253-00991 REV A DATE 07/11/2018.

Part: SKIN — CHAFED (RT AILERON) · airframe 35,079 hrs · 34,499 cycles

RT AILERON UPPER SKIN LEADING EDGE HAS SEVERAL CHAFED SPOTS. REMOVED AND REPLACED RT AILERON UPPER SKIN IAW SRM 51-42-22.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 35,079 hrs · 34,499 cycles

FLIGHT COMPARTMENT CENTER WINDSHIELD POST LT LOWER BRACKET CRACKED FROM LOWER RIVET TO EDGE OF BRACKET. REMOVED AND REPLACED CENTER POST LT LOWER BRACKET IAW SRM 51-42-21 AND 51-25-06.

Part: SKIN — CHAFED (TE FLAP VANE) · airframe 35,079 hrs · 34,499 cycles

RIGHT I/B FLAP VANE LEADING EDGE CHAFED AT WS 56.00. REPLACED RIGHT WING I/B FLAP VANE LEADING EDGE IAW SRM 51-42-13.

Part: BULKHEAD — DENTED (FUSELAGE) · airframe 35,079 hrs · 34,499 cycles

AFT PRESSURE BULKHEAD FWD SIDE HAS A DENT AT LBL22. REPAIRED AFT PRESSURE BULKHEAD IAW REO601R-53-61-6635 REV-A.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,079 hrs · 34,499 cycles

RIGHT SIDEWALL SEAT TRACK NR 6 CORRODED. REPLACED SEAT TRACK IAW AMM 53-01-11.

Part: BULKHEAD — DENTED (FUSELAGE) · airframe 35,079 hrs · 34,499 cycles

AFT PRESSURE BULKHEAD FWD SIDE HAS DENT AT LBL31. REPAIRED AFT PRESSURE BULKHEAD IAW REO601R-61-6635 REV-A.

Part: SKIN — CHAFED (TE FLAP VANE) · airframe 35,079 hrs · 34,499 cycles

RIGHT I/B FLAP VANE LEADING EDGE SKIN CHAFED. REPLACED RIGHT I/B FLAP VANE LEADING EDGE SKIN IAW SRM 51-42-13.

Part: RETAINER — CRACKED (LT PYLON) · airframe 35,079 hrs · 34,499 cycles

LEFT PYLON PNL 412DB HAS CRACKED SEAL RETAINER. REPAIRED SEAL RETAINER IAW SUPP 16-363.

Part: RETAINER — CRACKED (RT PYLON) · airframe 35,079 hrs · 34,499 cycles

RIGHT PYLON PNL 422BT SEAL RETAINER CRACKED. REPLACED SEAL RETAINER IAW SRM 54-63-01, 51-42-06, 51-40-11.

Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 34,340 hrs · 33,747 cycles

DURING A BULKHEAD INSPECTION, NDT REVEALED A ONE INCH CRACK BS 621, LBL 27.5, WL 132.

Part: DUCT — DETACHED (LT A/C PACK) · airframe 33,902 hrs · 33,281 cycles

TOILET SMOKE CAUTION MESSAGE ON PUSH BACK, APU ON 10TH STAGE BLEEDS CLOSED, ENGS OFF, F/A REPORTED SMOKE IN THE CABIN. FIRE BOTTLES ARMED. INSPECTED ACFT ELECTRICAL SYSTEMS AND PNEUMATIC SYSTEMS, NO SMOKE OR ODORS PRESENT. FOUND THE LEFT PACK DUCT BLOWN, REMOVED AND REPLACED PACK DUCT ASSY, OPS CHECKED GOOD IAW MM. R & R THE BELLOW ASSY ON APU INTAKE DUE TO SMOKE LIKE ODOR IN CABIN, PERFORMED OPS TEST AND OPS TESTED GOOD.

Part: PUMP — FAILED (HYD SYSTEM) · airframe 33,119 hrs · 32,530 cycles

AFTER TAKEOFF WITH GEAR SELECTOR UP, FOR MORE THAN 30 SECONDS RECEIVED GEAR DISAGREE WARNING MESSAGE. MAIN LANDING GEAR SHOWED WHITE HASH MARKS. NOSE GEAR SHOWED RED HASH MARKS. MESSAGE PERSISTED FOR MORE THAN 20 SECONDS. COMPLIED WITH QRH. TURNED ON HYD PUMP 2B, 3B WAS ALREADY ON FOR THE MEL. SELECTED EMERGENCY EXTENSION HANDLE. MAINS EXTENDED. NLG DID NOT EXTEND. SELECTED MLG DOWN, THEN NOSE SHOWED DOWN AND GREEN. SELECTED EMERGENCY EXTENSION HANDLE TO NORMAL AND NLG DOOR CLOSED. ALL MESSAGES EXTINGUISHED. R & R BOTH NR 3 ALTERNATING CURRENT MOTOR PUMP'S 3A AND 3B AND RESERVOIR.

Part: SWITCH — FAILED (BOOST PUMP) · airframe 33,026 hrs · 32,442 cycles

ACRID ODOR IN COCKPIT, (FAINT ELECTRICAL PLASTIC ODOR) APPROX. 10 MIN INTO FLIGHT, NOT NOTICEABLE OUTSIDE COCKPIT, NO ABNORMAL EICAS MESSAGES. DURING TROUBLESHOOTING, FOUND GROUND FAN INTERNAL WIRING HAD FRAYED AND MISSING SHIELDING ON INTERNAL WIRING. R & R GROUND FAN IAW AMM 21-24-19. OPS GOOD. REMOVED FLIGHT FAN FOR TROUBLESHOOTING OF ODOR. R & R THE FLIGHT FAN IAW AMM 21-24-19. CLEANED BUILD UP OF DUST IN LOOSE CENTER CONSOLE AND LEFT AND RIGHT PANEL CIRCUIT BREAKER PANEL NR 4 AND 3. FOUND PLASTIC BAG BEHIND FO'S SIDE 222CZ POSSIBLE COULD HAVE RUBBED ON FLIGHT COMPARTMENT SENSOR FAN ASSY CAUSING ODOR. PULLED PFDS FOR TROUBLESHOOTING. INSPETED AND CLEANED PFDS, NO FAULTS NOTED. R & R THE DISPLAY COOL FILTER IAW AMM 21-24-15. FOUND IMPROPERLY SEATED RT BOOST PUMP SWITCH AND BROKEN OFF LANYARD. NOTICED BURNED ELECTRICAL ODOR ON CAP AND SWITCH. R & R THE CAP AND SWITCH. OPS GOOD.

Part: SWITCH — NOT SEATED (FUEL SYSTEM) · airframe 33,026 hrs · 32,442 cycles

AFTER ROTATION EXPERIENCED FAINT ELECTRICAL, BURNT / OVERHEATED BRAKE ODOR. WENT AWAY, RETURNED AFTER 5-6 MIN AND AGAIN 20 MIN INTO FLIGHT. EACH TIME A LITTLE STRONGER ODOR. NO INOP FANS, LIGHTS OR ASSOCIATED MESSAGES. ODOR MAINLY IN COCKPIT. 2 TIMES ON APU BLEED, 3RD, TIME ON ENGINE BLEEDS. LANDING UNEVENTFUL AND UNDERWEIGHT. PULLED PFDS FOR T/S. INSPECTED AND CLEANED PFDS, NO FAULTS NOTED. R&R DISPLAY COOL FILTER IAW AMM 21-24-15. FOUND IMPROPERLY SEATED RT BOOST PUMP SWITCH AND BROKEN OFF LANYARD. NOTICED BURNT ELECTRICAL SMELL ON CAP AND SWITCH. R&R CAP AND SWITCH. OPS GOOD.

Part: B-NUT — LOOSE (APU) · airframe 32,917 hrs · 32,339 cycles

STRONG FUEL & EXHAUST ODOR COMING FROM BLEED AIR SYSTEM. STRONGER ODOR IN FLT DECK AND DURING FLT. THIS HAPPENS ON ENGINE AIR AS WELL AS ON APU AIR ONLY. FOUND THE MAIN FEED MANIFOLD CRACKED. FOUND BOTTOM B-NUT OF APU SOLENOID SHUTOFF VALVE LOOSE. SECURED THE B-NUT IAW AMM 49-31-05, LEAK AND OPS CHECKED GOOD. MAIN FEED MANIFOLD UNDER CARGO BAY FLOOR HAS A SPLIT AT THE FWD UPPER EDGE APPROX 10 INCHES LONG. REPLACED THE AC DISTRIBUTION MANIFOLD IAW AMM 21-22-01 LEAK AND OPS CHECKED GOOD.

Part: COALESCER BAG — ODOR (AC BAY) · airframe 32,911 hrs · 32,322 cycles

STRONG EXHAUST PETROLEUM ODOR COMING FROM BLEED AIR SYSTEM. STRONGER ON FLIGHT DECK. NO NOTICEABLE DIFFERENCE BETWEEN GATE AND CRUISE. R & R THE LT & RT COALESCER SOCKS ON AIR-CONDITIONING WATER SEPARATORS IAW SUP 14-192. OPS AIR-CONDITIONING SYSTEM. NO ODOR NOTED AT THIS TIME.

Part: APU — MALFUNCTIONED (APU BAY) · airframe 32,875 hrs · 32,296 cycles

APU FIRE MESSAGE, FOLLOWED BY APU AUTO SHUTDOWN. REMOVED AND REPLACED THE APU IAW TASK CARD , SUP 13-005 AND AMM 49-10. OPS AND LEAK CHECKED GOOD.

Part: HANDLE — UNSECURE (SERVICE DOOR) · airframe 32,401 hrs · 31,870 cycles

SERVICE DOOR HANDLE DOES NOT POP OUT FROM OUTSIDE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,316 hrs · 31,787 cycles

FLOOR LEVEL EMERGENCY LIGHTS DOES NOT ILLUMINATE FROM ROW 7 TO AFT OF ACFT.

Part: FLAP SYSTEM — FAILED · airframe 32,179 hrs · 31,666 cycles

FLAPS FAILED ON GO AROUND AT 20 DEGREES. COMING UP FROM 45 DEGREES. OVERSPEED CLACKER OCCURRED NEAR THE SAME TIME, AIR SPEED WAS 180 KIAS. COMPLIED WITH AWAC SUPP 98-018G TO STEP 12 A1. FLAPS FAILED ON CIRCUIT BREAKER RESET (CBP1-F4 AND CBP2-F4)

Part: APU — LEAKING · airframe 32,049 hrs · 31,544 cycles

SMOKE APPEARED IN THE FLIGHT DECK FROM AIR CONDITIONING VENTS, APU SHUTDOWN SHORTLY AFTERWARDS. LARGE PUDDLE OF OIL DRIPPING FROM AFT EQUIPMENT BAY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,044 hrs · 31,359 cycles

EMERGENCY LIGHTS FROM ROW 8 AFT DO NOT TURN ON.

Part: UNKNOWN — ODOR (CABIN) · airframe 31,823 hrs · 31,347 cycles

SMOKE APPEARANCE AND ELECTRICAL ODOR ROW 10 D/F AND 11 D/F AT CEILING LIGHTS WITH LIGHTS ON.

Part: YAW DAMPER — DEFECTIVE · airframe 31,675 hrs · 31,207 cycles

WHILE IN CRUISE, ACFT HAD UNCOMMANDED YAW TO LEFT. YAW DAMPERS REMAINED ENGAGED AT ALL TIMES. UNCOMMANDED YAW WAS INTERMITENT AND RANDOM IN NATURE. REQUEST INSPECTION. REMOVED AND INSTALLED NEW LINER ACUATOR YAW DAMPER IAW 22-22-01. OPS CHECKED GOOD IAW 22-22-01-710-802.

Part: UNKNOWN — MALFUNCTIONED (AUTOPILOT SYS) · airframe 31,441 hrs · 30,990 cycles

INTERMITTENT UNCOMMANDED YAW DURING CRUISE AND DECENT. YD2 DISENGAGED PRIOR TO APPROACH RE-ENGAGED ALTHOUGH YAW MOTION CONTINUED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,254 hrs · 30,807 cycles

CREW REPORTED THAT THE FLOOR LEVEL EMERGENCY LIGHTS DO NOT ILLUMINATE FROM ROW 8 AFT. FOUND DURING THE FIRST FLIGHT OF THE DAY ACCEPTANCE INSPECTION.

Part: PAN — CORRODED (SERVICE DOOR) · airframe 31,209 hrs · 30,767 cycles

SERVICE DOOR AFT LOWER PAN SEGMENT HAS CORROSION ON LOWER AND UPPER SURFACES. COMPLIED WITH TEMPORARY DISPOSITION FOR CORROSION DAMAGE ON LOWER AFT PAN OF SERVICE DOOR IAW REO 601R-52-41-238, REV DATED 06-21-2016.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,209 hrs · 30,767 cycles

UPON REMOVAL OF THE SPADE DOOR UPPER BUSHINGS, FOUND CORROSION UNDER RT SPADE DOOR FITTING.

Part: FRAME — CRACKED (FUSELAGE) · airframe 31,209 hrs · 30,767 cycles

FRAME CRACKED, FS 333 AND STR 1L.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,209 hrs · 30,767 cycles

UPON REMOVAL OF THE SPADE DOOR UPPER BUSHINGS, FOUND CORROSION UNDER LT SPADE DOOR FITTING.

Part: STRIKER — BENT (FUSELAGE) · airframe 31,209 hrs · 30,767 cycles

PASSENGER DOOR CUTOUT FWD EDGE AT UPPER LOCK LUG, LIP, SEAL STRIKER BENT.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,209 hrs · 30,767 cycles

CARGO PIT FLOOR AFT FITTING INBD FLANGE IS CORRODED AT FS 612.00, LBL9. REPAIRED CORROSION ON INBD AND OTBD FLANGES ON LBL9 CARGO BEAM AT FS 612, FS 615 IAW EA AWAC-CRJ253-00409, REV-A .

Part: SKIN — CRACKED (FUSELAGE) · airframe 31,209 hrs · 30,767 cycles

SKIN CRACKED RT AFT NLG SPADE DOOR CUTOUT AT FS 235.00, STR 26R. REPAIRED RT AFT NLG SPADE DOOR CUTOUT AT FS 235.00, STR 26R IAW GREO 601R-53-11-048, REV-D, DATED 06/10/2015.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,209 hrs · 30,767 cycles

FRAME 319.7, FWD SIDE JUST OTBD OT THE STR 23R INTERCOSTAL CORRODED, REPAIRED.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,209 hrs · 30,767 cycles

FRAME 333, ON THE FWD SIDE BETWEEN STR 23R AND 20R HAS CORROSION, REPAIRED.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 31,209 hrs · 30,767 cycles

RT OVERWING TO BODY PANEL SUPPORT AT FS 473.15 IS CRACKED, REPLACED.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,209 hrs · 30,767 cycles

FLOOR MEMBER BETWEEN RBL 27 TO RT SILL AND FS 589.00 IS CORRODED AROUND SCREW HOLES. REPLACED CARGO FLOOR MEMBER FROM RBL 27 TO RT SILL, FS 589.00 IAW SRM 51-40-11, 51-42-06.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 31,209 hrs · 30,767 cycles

RIGHT OVERWING TO BODY SUPPORT AT RT FS 508.00 CRACKED, REPLACED.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 31,209 hrs · 30,767 cycles

LEFT OVERWING TO FUSELAGE PANEL ATTACH STRUCTURE AT FS 470.00 IS CRACKED, REPLACED.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,209 hrs · 30,767 cycles

CARGO PIT FLOORBEAM, FLOOR SUPPORT FLANGE AT LBL27 IS CORRODED BETWEEN FS 559+112 TO FS 610.00. REPLACED CORRODED FLOORBEAM IAW SRM 51-40-11, 51-42-21, 51-42-06.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,209 hrs · 30,767 cycles

CARGO PIT FLOOR SUPPORT IS CORRODED AT FS 589.00 BETWEEN LBL9 TO 27. REPLACED CARGO FLOOR SUPPORT AT FS 589.00 BETWEEN LBL9 TO 27 IAW SRM 51-40-11, 51-42-06.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,209 hrs · 30,767 cycles

AFT FLOORBEAM FITTING AT LBL27 AND FS610.00 TO 621.00 HAS CORROSION ON FLANGE AND UNDER TEFLON CAP STRIP. REPAIRED CORROSION AT FS 610.00 TO 621.00, LBL27 CARGO FLOORBEAM REO 601R-53-61-4530, REV-A.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,209 hrs · 30,767 cycles

CARGO PIT FLOOR SUPPORT AT LBL 12 IS CORRODED BETWEEN FS 559+112 TO FS 574.00. REPLACED CORRODED FLOOR SUPPORT IN CARGO BAY FROM FS 559+112 TO FS 574.00, LBL12 IAW SRM 51-40-11, 51-42-06.

Part: TIE DOWN — CORRODED (CARGO BAY) · corrosion level 2 · airframe 31,209 hrs · 30,767 cycles

CARGO PIT TIE DOWNS ARE CORRODED AT LBL9, FS 574.00-605.00. REPLACED CARGO PIT TIE DOWNS AT LBL 9, FS 574.00- 605.00 IAW AMM 53-00-49.

Part: TIE DOWN — CORRODED (CARGO BAY) · corrosion level 2 · airframe 31,209 hrs · 30,767 cycles

CARGO PIT TIE DOWNS CORRODED BETWEEN FS 559+96 TO FS 559+112 AT LBL 27. REPLACED CARGO PIT TIE DOWNS BETWEEN FS 559+96 TO FS 559+112 T/A LBL 27 IAW AMM 53-00-49.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 31,209 hrs · 30,767 cycles

CARGO PIT SMALL TRACK IS CORRODED AT LBL9 BETWEEN FS 610.00 AND FS 616.00. REPLACED CARGO PIT SMALL TRACK AT LBL9, FS 610.00 TO FS 616.00 IAW AMM 53-00-49.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,209 hrs · 30,767 cycles

INTERCOSTAL FS 310 TO 319.7 AT STGR 20R IS CORRODED.

Part: SUPPORT BRACKET — CRACKED (AC BAY) · airframe 31,209 hrs · 30,767 cycles

AFT EQUIPMENT BAY, LT ACM SUPPORT BRACKET IS CRACKED. REPLACED LT ACM SUPPORT BRACKET IAW SRM 51-42-06, 51-42-21, 51-40-02.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 31,209 hrs · 30,767 cycles

STRINGER CLIP CRACKED AT STR 3L, FS 280.00. REPLACE STR CLIP AT STR3 L AND FS 280.00 IAW SRM 51-42-06, 51-42-21.

Part: BRACKET — CRACKED (RT MLG) · airframe 31,209 hrs · 30,767 cycles

RIGHT MLG BRAKE TRANSDUCER BRACKET IS CRACKED. REPLACED RT MLG TRANSDUCER BRACKET IAW SRM 51-42-06.

Part: CAP — LOOSE (CABIN) · airframe 31,031 hrs · 30,605 cycles

THE FWD END CAP OF THE EMER FLOOR TRACK LIGHTS IS LOOSE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,702 hrs · 30,299 cycles

REAR MOST FLOOR STRIP OF EMER LIGHT INOPERATIVE, RT SIDE FROM ROW 8 BACK.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 30,702 hrs · 30,299 cycles

DURING INSPECTION, FOUND LAST LAMP OF AFT SECTION OF FLOOR EMERGENCY LIGHT INOPERATIVE.

Part: FLAP SYSTEM — FAILED (TE FLAPS) · airframe 30,676 hrs · 30,273 cycles

FLIGHT 3746, FLAPS FAILED AT 20 DEGREES ON APPROACH. PERFORMED FLAP RESET IAW SUP 98-18G. FLAP FAIL MESSAGE REAPPEARED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,199 hrs · 29,831 cycles

EMERGENCY LIGHTS FROM ROW 5 - 8 & EMER FLOOD LIGHT BEHIND ROW 7F INOPERATIVE.

Part: UNKNOWN — ODOR · airframe 30,079 hrs · 29,712 cycles

STRONG FUEL SMELL FROM PACK AFTER LT ENG SHUT DOWN. RAN BOTH ENGS WITH APU, NO FUEL LEAKS NOTED. RAN PACKS ON BOTH ENG & APU BLEEDS, NO ODORS OR LEAKS NOTED. NO ODOR NOTED AFTER ENG SHUT DOWN IAW 36-10-00. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,382 hrs · 28,030 cycles

EMERGENCY FLOOR LIGHTING AFT OF ROW 8 INOPERATIVE.

Part: UNKNOWN — ODOR (CABIN) · airframe 26,586 hrs · 26,295 cycles

STRONG ELEC SMELL ROW 9 - 11 AT GATE.

Part: COWLING — DEPARTED (RT ENGINE) · airframe 26,496 hrs · 26,228 cycles

4042 ON DEPARTURE FROM DCA, AT APPROX 2000 FT, RWY 19, FELT ACFT SHUDDER SLIGHTLY. ACFT HANDLED NORMALLY ALL INDICATIONS WERE NORMAL. IN PHL DISCOVERED RT ENG UPPER CORE COWL WAS MISSING.

Part: BEARING — WORN (LT ELEVATOR) · airframe 26,492 hrs · 26,225 cycles

LT ELEVATOR NR 1 HINGE BEARING HAS AXIAL PLAY. R & R LT ELEVATOR NR 1 BEARING PN MS14102-6 IAW SUPPLEMENT NR 11-068 DATED DEC 16, 2011.

Part: BRACKET — DAMAGED (PAX DOOR) · airframe 26,491 hrs · 26,224 cycles

COMPLIED WITH CARD 4DMI17495 REPAIR PAX DOOR ASSIST MOTOR BRACKET. R & R PAX DOOR POWER ASSIST BRACKET WITH NEW SERVICEABLE BRACKET IAW SRM 51-42-06.

Part: PANEL — DAMAGED (PAX DOOR) · airframe 26,491 hrs · 26,224 cycles

COMPLIED WITH CARD 4DMI17423 REPAIR PAX DOOR AFT SIDE PANEL. REPAIRED PAX DOOR AFT SIDE PANEL IAW REO 601R 52-11-702 REV C.

Part: THRESHOLD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,491 hrs · 26,224 cycles

SERVICE DOOR THRESHOLD PLATE IS CORRODED AROUND HOLES. INSTALLED SERVICEABLE SERVICE DOOR THRESHOLD IAW 51-41-02.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,491 hrs · 26,224 cycles

54637-1000-0047 - PAX DOOR LWR SILL ANGLE IS CORRODED. REMOVED CORRODED LWR PAX DOOR SILL & INSTALLED NEW SERVICEABLE SILL IAW SRM 51-42-06, 51-42-13 & 51-42-21.

Part: FITTING — CRACKED (FUSELAGE) · airframe 26,491 hrs · 26,224 cycles

RT FS 484.00 CLIPS ARE CRACKED AT BL 27 - 36. R & R RT FS 484.00 CLIPS AT BL 27 & 36 IAW REO 601R-53-41-059 REV B.

Part: SKIN — CRACKED (FUSELAGE) · airframe 26,491 hrs · 26,224 cycles

54637-1000-0015 - EXT LWR FUSELAGE SKIN AT AFT NOSE WHEEL CUT OUT HAS CRACK ON LT RADIUS FS 235 & RT SIDE. REPAIRED FS 235 LT & RT SIDE CRACKS AT CUT OUT RADIUS IAW 601R-53-11-048.

Part: DRAG ANGLE — CRACKED (LT MLG WW) · airframe 26,491 hrs · 26,224 cycles

LT MLG WW DRAG ANGLE CRACKED. R & R LT MLG WW DRAG ANGLE IAW SRM 51-42-21 & 51-40-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,491 hrs · 26,224 cycles

NR 1 FLOOR SEAT RAILS AT LBL 9 & RBL 9 BOTH HAVE CORROSION. R & R SEAT RAIL NR 1 AT LBL 9 & RBL 9 IAW SRM 51-40-11 & 51-21-16.

Part: ATTACH ANGLE — CRACKED (RT WING) · airframe 26,491 hrs · 26,224 cycles

RT WING LE ATTACH ANGLE CRACKED UNDER 620ML. R & R WITH SERVICEABLE IAW SRM 51-41-02 & 51-40-11.

Part: FITTING — CRACKED (FUSELAGE) · airframe 26,491 hrs · 26,224 cycles

LT FS 484.00 CLIPS CRACKED BL 27.00 - 36.00. R & R INBD & OTBD 484.00 CLIPS IAW REO 601R 53-41-059 REV B.

Part: VANE — CHAFED (TE FLAP) · airframe 26,491 hrs · 26,224 cycles

LEFT INBD FLAP VANE LE IS CHAFED IN LOCATIONS FROM STOPS. R & R INBD HALF OF LE MID-SECTION IAW SRM 51-42-13. REPAIRED CHAFE AREAS ON INBD & OTBD SURFACES OF THE LT , INBD FLAP VANE LE IAW REO 601R-57-52-004.

Part: ATTACH BRACKET — CRACKED (HYDRAULIC BAY) · airframe 26,491 hrs · 26,224 cycles

NOSE HYD COMPARTMENT, UPPER HYD ACCUMULATOR, FWD ATTACH BRACKET IS CRACKED FWD LWR RADIUS. R & R CRACKED BRACKET IAW SRM 51-42-06, 51-41-02 & 51-41-04 AMM 20-24-00.

Part: FITTING — CRACKED (FUSELAGE) · airframe 26,491 hrs · 26,224 cycles

54637-2000-0077 - RBL 9 INBD & OTBD FLOOR SUPPORT BEAM CLIPS ARE CRACKED AT FS 280. REPAIRED RBL 9 INBD & OTBD FLOOR SUPPORT BEAM CLIPS IAW REO 601R -53-11-171 REV D.

Part: DRAG ANGLE — CRACKED (RT MLG WW) · airframe 26,491 hrs · 26,224 cycles

RT MLG WW DRAG ANGLE CRACKED. R & R RT MLG DRAG ANGLE IAW SRM 51-42-21 & 51-40-11.

Part: FITTING — CRACKED (FUSELAGE) · airframe 26,491 hrs · 26,224 cycles

LBL 9 INBD & OTBD FLOOR SUPPORT BEAM CLIPS ARE CRACKED AT FS 280. REPAIRED LBL 9 INBD & OTBD FLOOR SUPPORT BEAM CLIPS AT FS 280 IAW REO 601R-53-11-139 REV A.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 26,491 hrs · 26,224 cycles

COMPLIED WITH CARD 4DMI17497 REPAIR PAX DOOR STEP CHANNEL. REPAIRED PAX DOOR AFT DRAG ANGLE IAW REO 601R-52-11-53 REV A.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 26,491 hrs · 26,224 cycles

COMPLIED WITH CARD 4DMI16383 REPAIR. FUSELAGE SKIN AT FS 605 REO 601R-53-61-4588A. COMPLIED WITH PERMANENT REPAIR AT FUSELAGE SKIN FS 605 STRINGER 22L IAW REO 601R-53-61-5290.

Part: BULKHEAD — GOUGED (FUSELAGE) · airframe 26,491 hrs · 26,224 cycles

621 BULKHEAD HAS 2 GOUGED SPOTS, ONE LOCATED TOP RT BELOW CONNECTOR IDENTIFIER 2CP2RD, SECOND ONE LOCATED BOTTOM RT OTBD CORNER 4 INCHES ABOVE FLOOR LINE. BLENDED GOUGE SPOT ONE TO ALLOWABLE LIMITS IAW REO 601R-53-61-2155 REV A DATED 8-13-13. REPAIRED SECOND GOUGE SPOT IAW REO 601R-53-61-5289 DATED 6-10-14.

Part: CHANNEL — CHAFED (LT WING) · airframe 26,491 hrs · 26,224 cycles

LT WING UPPER TE HAS CHAFE NEAR WS 104.099 JUST OTBD OF INBD GND SPOILER ACTUATOR. R & R TE CHANNEL AT WS 104.099 WITH SERVICEABLE PART IAW SRM 51-40-11, 51-42-06 & 51-21-16.

Part: BRACKET — CRACKED (SERVCIE DOOR) · airframe 26,491 hrs · 26,224 cycles

SERVICE DOOR HANDLE PROXIMITY SENSOR BRACKET CRACKED. R & R WITH SERVICEABLE PART PN 601R38723-17 IAW SRM 51-40-11 & 51-41-02.

Part: BRACKET — CRACKED (LT MLG WW) · airframe 26,491 hrs · 26,224 cycles

LT MLG WW BRAKE TRANSDUCER BRACKET CRACKED. R & R LT MLG WW BRAKE TRANSDUCER BRACKET PN 601R75262-159 IAW SRM 51-40-11 & 51-42-06.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,491 hrs · 26,224 cycles

54637-2000-0068 - LT SIDE SEAT RAIL TRACK CORRODED AT FS 559+77. R & R AFT MOST LT SIDE SEAT RAIL TRACK SECTION WITH SERVICEABLE TRACK IAW REO 601R-53-00-055 REV A DATED NOV 18 2011.

Part: DOOR SILL — CRACKED (FUSELAGE) · airframe 26,491 hrs · 26,224 cycles

LT FLOOR SILL CRACKED AT CROSSBEAMS AT FS 589 & 605. REPAIRED LT FLOOR SILL IAW REO 601R-53-61-433 REV C DATED 2012-11-23.

Part: FLOOR SKIN — CRACKED (FUSELAGE) · airframe 26,491 hrs · 26,224 cycles

FWD AVIONICS BAY FLOOR SKIN CRACKED AT FS 193 ON LT SIDE. REPAIRED FLOOR SKIN IAW REO 601R-53-11-111 REV NC DATED 98-MAR-18.

Part: RVDT — MALFUNCTIONED (NLG STEERING) · airframe 26,015 hrs · 25,765 cycles

4004 AT CRUISE, IN FLT, RECEIVED STEERING INOPERABLE CAUTION MSG. COMPLIED WITH QRH & MSG DID NOT CLEAR. R & R RT RVDT IAW AMM 32-51-20, OPERATIONS CHECKED GOOD.

Part: RECEPTACLE — DAMAGED (EXTERNAL POWER) · airframe 25,587 hrs · 25,353 cycles

SUPPLIED AC POWER HOOKED UP, SPARKS WITH SMOKE ORIGINATED A TC POWER RECEPTACLE, REQUEST INSPECTION. INSPECTED AC POWER CONNECTOR IAW REO 601R-24-22-004, FOUND INSIDE PINS & RECEPTACLE DISCOLORED, PLACED ON MEL IAW REO 601R-25-22-004, SEE BLOCK 2 FOR MEL.

Part: COMPUTER — MALFUNCTIONED (FUEL SYSTEM) · airframe 22,138 hrs · 22,044 cycles

AT FL 230, IN LEVEL FLT, RECIEVED FUEL IMBALANCE CAUTION. RT TANK LOW. RT TANK QTY REDUCED TO ZERO, THEN SHOWED DASHES. CENTER TANK AND TOTAL FUEL QTY ALSO SHOWED DASHES. ON APPROACH, ALL INDICATIONS RETURNED TO NORMAL. CORRECTIVE ACTION TAKEN: PERFORMED BITE TEST OF FUEL COMPUTER. ALL RIGHT TANK PROBES SHOWING FAULTS. FOUND FUEL COMPUTER LOOSE ON MOUNT. RESEATED COMPUTER. BITE TEST OK PER AMM 28-41-16. OK FOR SERVICE.

Part: CONTROL CABLE — FAILED (THROTTLE) · airframe 21,925 hrs · 21,837 cycles

ON DESCENT, LT THRUST LEVER STUCK AT AROUND 82 PERCENT, N1. COMPLIED WITH QRH, SHUTDOWN NR 1 ENGINE IN FLIGHT, ALL ENGINE PARAMETERS NORMAL. R & R LT ENGINE THROTTLE CONTROL CABLE IAW AMM 76, OPS CHECKED GOOD.

Part: ATTACH BRACKET — CRACKED (FS 574) · airframe 21,594 hrs · 21,507 cycles

FWD CARGO DOOR SLIDER ATTACH BRACKET IS CRACKED. REMOVED UNSERVICEABLE SLIDER ATTACH BRACKET AND REPLACED WITH SERVICEABLE IAW SRM 51-41-11 & 51-42-06.

Part: FLOOR SUPPORT — CORRODED (FS 569-621) · corrosion level 2 · airframe 21,594 hrs · 21,507 cycles

FLOOR SUPPORT CAP CORRODED IN SEVERAL PLACES FROM FS 574 TO FS 621 LBL 27. R & R FLOOR SUPPORT CAP IAW SRM 57-61-43 & REO 61R-53-61-3778, REV A & REPAIRED CORROSION DAMAGE AROUND NUTPLATE HOLES ON INBD & OTBD SIDE OF LBL 27.0 AT FS 615 IAW REO 601R-53-61-4530.

Part: FLOOR SUPPORT — CORRODED (BS 569-610) · airframe 21,594 hrs · 21,507 cycles

FLOOR SUPPORT CAP BS 569-610 IS CORRODED. R & R FLOORBEAM CAP IAW SRM 51-42-21.

Part: CARGO TRACK — CORRODED (FS610-616) · airframe 21,594 hrs · 21,507 cycles

LAST SECTION OF CARGO TRACK ON LBL 9 JSUT FWD OF THE 621 BULKHEAD CORRODED. REPLACEED CARGO TRACK.

Part: TRUNNION — DAMAGED (MLG) · airframe 21,594 hrs · 21,507 cycles

DURING COLD WORKING OF MLG TRUNNION LOWER FLANGES, FOUND 2 TOTAL OVERSIZED HOLES 1 LT, 1 RT. COLD WORKED IAW REO 601R-57-21-1687.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 21,594 hrs · 21,507 cycles

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

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 21,594 hrs · 21,507 cycles

LEFT INBD FLAP VANE IS CHAFED. REPAIRED LT INBD FLAP VANE IAW ROE 601R-57-52-004, REV C AND SRM 51-12-00, 51-21-11, 51-25-06, 51-25-16 AND 51-25-26.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 21,594 hrs · 21,507 cycles

RT INBD FLAP VANE HAS 3 CHAFED SPOTS ON L/E. REPAIRED RT INBD FLAP VANE L/E IAW REO 601R-57-52-004, REV C AND SRM 51-12-00, 51-21-11, 51-25-06, 51-25-16, 51-25-26.

Part: ATTACH FITTING — CRACKED (FS 280) · airframe 21,594 hrs · 21,507 cycles

RBL 9 INBD ATTACH FITTING CRACKED AT FS 280. R & R CRACKED ATTACH FITTING IAW SRM 51-42-06 & 51-42-21.

Part: STRUCTURE — CHAFED (RT MLG DOOR) · airframe 21,594 hrs · 21,507 cycles

RT MLG DOOR L/E CHAFED. REMOVED UNSERVICEABLE FILLER AND REPLACED WITH SERVICEABLE FILLER IAW REO 601R-52-82-034.

Part: STRUCTURE — CHAFED (LT MLG DOOR) · airframe 21,594 hrs · 21,507 cycles

LT MLG DOOR CHAFED L/E CORNER BY DOOR BRUSH. REMOVED UNSERVICEABLE EXISTING FILLER AND REPLACED WITH SERVICEABLE FILLER IAW REO 61R-52-82-034, REV NC.

Part: THRESHOLD — CORRODED (FS 319-349) · airframe 21,594 hrs · 21,507 cycles

SERVICE DOOR THRESHOLD HAS CORROSION ON UPPER MOUNTING HOLES. REPLACED UNSERVICEABLE SERVICE DOOR THRESHOLD (BLENDED 0.062, 0.042" MATERIAL REMAINING WITH SERVICEABLE SERVICE DOOR THRESHOLD IAW SRM 53-00-00, FIG 102, SRM 51-40-11.

Part: WIRE HARNESS — DAMAGED (CARGO DOOR) · airframe 20,970 hrs · 20,853 cycles

PAX DOOR WARNING IN FLIGHT, FOLLOWED BY CARGO DOOR CAUTION. R & R CARGO DOOR HARNESS IAW AMM 52-70-02. OPS CKS GOOD.

Part: SKIN — DAMAGED (BS 193-202) · airframe 20,343 hrs · 20,173 cycles

DAMAGE TO FUSELAGE SKIN AT FS 202.75 BETWEEN STR 21L-23L. REPAIRED DAMAGED SKIN IAW REO 601R-53-11-2053.

Part: UNKNOWN — ODOR (CABIN) · airframe 19,820 hrs · 19,620 cycles

ELECTRICAL ODOR IN CABIN AROUND ROW 8 CEILING. INSPECTION OR AREA AND FOUND UNIT B116 EMITTING ODOR DISCONNECTED AND STOWED PLUGS REF LP 121785/1 FOR SIDEWALL LIGHTS AT ROW 7 MEL.

Part: BALLAST — BURNED (CABIN LIGHTS) · airframe 19,777 hrs · 19,573 cycles

BURNING ODOR IN CABIN BETWEEN ROWS 5-7. FOUND BALLAST ABOVE SEAT A/C BURNED (CTR AISLE LIGHT) R & R BALLAST IAW AMM 33-21-01. OPS CHECKED GOOD.

Part: DOOR — BINDING (MAIN PAX) · airframe 19,419 hrs · 19,182 cycles

INITIAL ATTEMPT TO OPEN PAX DOOR WAS UNSUCCESSFUL. UPON APPLICATION OF UNUSUALLY HIGH FORCE, DOOR OPENED. C/W OPS CHECK OF PAX DOOR. OPS CK NORMAL AT THIS TIME, REF AM 52-11-00.

Part: FAIRING — GOUGED (BS 529-559) · airframe 17,104 hrs · 16,778 cycles

LT STUB FAIRING GOUGED, LT FLAP STUD FAIRING WAS REPLACED WITH SERVICEABLE PN 601R31199-91.

Part: FITTING — GOUGED (LT WING TE FLAP) · airframe 17,104 hrs · 16,778 cycles

LT FLAP GUIDE FITTING PN 601R14526 IS CHAFED AND GOUGED. BLENDED LT OTBD FLAP GUIDE FITTING IAW REO 601R57-51-143 REV NC.

Part: BULKHEAD — DAMAGED (BS 280) · airframe 17,104 hrs · 16,778 cycles

AFT SIDE OF 280 BULKHEAD HAS 2 EA DENTES ON TR SIDE OF FLIGHT DECK ENTRY WAY. REPAIRED DAMAGED AREA ON RT SIDE, FS 280 BULKHEAD BY INCORPORATING REO 601R-53-11-1727, REV C.

Part: SKIN — PUNCTURED (RT WING SPOILER) · airframe 17,104 hrs · 16,778 cycles

RT WING FLIGHT SPOILER LOWER SURFACE DENTED/PUNCTURED REPAIRED IAW REO 601R-57-73-126.

Part: SKIN — CHAFED (LT WING AILERON) · airframe 17,104 hrs · 16,778 cycles

LT AILERON L/E PANEL 599CB HAS SIGNS OF CHAFING EVALUATED LT AILERON L/E PANEL 559CB. BLENDED MATERIAL THICKNESS FOUND TO BE WITHIN LIMITS IAW REO 601R-57-60-020.

Part: SKIN — CHAFED (LT WING AILERON) · airframe 17,104 hrs · 16,778 cycles

LT AILERON UPPER L/E SKIN CHAFED IN SEVERAL AREAS EVALUATED LT AILERON UPPER L/E SKIN BLENDED CHAFE AREA MATERIAL THICKNESS FOUND TO BE WITHIN LIMITS IAW REO 601R-57-60-013.

Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 17,104 hrs · 16,778 cycles

LT INBD FLAP VANE LOWER L/E SKIN CHAFED/GOUGED IN 3 PLACES JUST ABOVE ACTUATOR, DAMAGE COMING FROM BRIDGE BRACKET HARDWARE BEING TOO LONG (SCREWS TOO LONG) REPAIRED LT INBD FLAP VANE LOWER L/E SKIN IAW SRM 57-52-00, FIG 202.

Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 17,104 hrs · 16,778 cycles

LT INBD FLAP MOVEABLE VANE L/E SKIN CHAFED, 3 AREAS LOCATED INBD CTR AND OTBD. REPAIRED IAW B/A REO 601R-57-52-004, REV C.

Part: SKIN — CHAFED (LT WING) · airframe 17,104 hrs · 16,778 cycles

LT AILERON LOWER L/E SKIN CHAFED, EVALUATED LT AILERON LOWER L/E SKIN. BLENDED CHAFE AREAS MATERIALS THICKNESS FOUND TO BE WITHIN LIMITS IAW REO 601R-57-60-020.

Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 17,104 hrs · 16,778 cycles

LT INBD FLAP VANE LOWER L/E SKIN CHAFED AT FLAP STA 117.00 ABOVE OTBD ACTUATOR REPAIRED IAW SRM 57-52-00, FIG 202.

Part: SEAT TRACK — CORRODED (BS 559+32) · airframe 17,104 hrs · 16,778 cycles

RT AISLE SEAT TRACK IN LAV AREA CORRODED. R & R SEAT TRACK IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (BS 559-574) · airframe 17,104 hrs · 16,778 cycles

2 EA SECTIONS OF SEAT TRACKS IN CTR OF CARGO BAY CORRODED. R & R 2 EA, SEAT TRACKS.

Part: STRUCTURE — CRACKED (RT WING SPOILER) · airframe 17,104 hrs · 16,778 cycles

RT FLIGHT SPOILER UPPER METAL FLANGE SEAL BETWEEN THE PCU`S IS CRACKED. REMOVED RT FLIGHT SPOILER UPPER METAL FLANGE SEAL AND INSTALL NEW SEAL IAW SRM 51-42-06 AND 51-42-21.

Part: SKIN — DAMAGED (BS 625) · airframe 17,104 hrs · 16,778 cycles

DENT ON TOP FUSELAGE BETWEEN STR 0 AND BETWEEN FUSELAGE STATIONS 625 AND 640. REPAIRED DENT ON TOP FUSELAGE BETWEEN STR 0 & STR 11 AND FS 625 AND 640.

Part: STRIKER — CHAFED (BS 318) · airframe 17,104 hrs · 16,778 cycles

PAX DOOR SEAL STRIKER IN DOOR CUT OUT AREA IS CHAFED IN UPPER FWD AREA BY DOOOR LOCK PIN FITTING. REPAIRED IAW REO 601R-53-22-033 REV C, TYPE 1.

Part: SEAT TRACK — CORRODED (BS 559) · corrosion level 2 · airframe 17,104 hrs · 16,778 cycles

ALL 4 SECTIONS OF SEAT TRACK, THE 9B BULKHEAD ATTACHES TO CORRODED. R & R 4 EA SEAT TRACKS FROM FS 559.00+80 TO 559.00+96 AT LBL 27.0, LBL 9.0, & RBL 27.0 IAW AMM 53-01-11.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 17,104 hrs · 16,778 cycles

FLOOR SUPPORT CRACKED (AFT FACE) LBL 12 APPROX FS 280. REPAIR IAW 601R-53-11-138, REV NC AND 601R-53-11-1942.

Part: ATTACH FITTING — CRACKED (BS 484) · airframe 17,104 hrs · 16,778 cycles

RT FS 484 CLIPS ARE CRACKED RBL 27 & 36. REPAIR IAW REO 601R-53-41-059, REV A.

Part: RIB — CRACKED (LT WING) · airframe 17,104 hrs · 16,778 cycles

LT BATT RIB IN LT WW CRACKED. REPAIRED LT BATT RIB IN LT WW IAW REO 601R-57-51-046 REV B, DATED 2002-02-28.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 17,104 hrs · 16,778 cycles

RT FLAP VANE HAS 3 AREAS OF CHAFING OTBD AND MID CHAFING POINTS IN LIMITS OF REO 601R-57-52-004, REV C. REPLACED INBD L/E IAW SRM.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 17,104 hrs · 16,778 cycles

AFT DRAG ANGLE CRACKED ON PAX DOOR INCORPORATED REO 601R-52-11-082, REV A.

Part: RIB — CRACKED (RWS 53.6) · airframe 17,104 hrs · 16,778 cycles

RT BATT RIB IN RT WW CRACKS REPAIRED RT BATT RIB IN RT WW IAW B/A REO 601R-57-51-046, REV B.

Part: ANGLE — CRACKED (BS 625) · airframe 17,104 hrs · 16,778 cycles

STATION FRAME 625, OBLIQUE ANGLE CRACK APART 601R-35012-51 FABRICATED/ REPLACED ANGLE.

Part: ANGLE — CRACKED (BS 625) · airframe 17,104 hrs · 16,778 cycles

STATION FRAME BS 625 RT OBLIQUE, ANGLE CRACK PN 601-35012-52 FABRICATED/ REPLACED ANGLE.

Part: ATTACH FITTING — CORRODED (PAX DOOR) · corrosion level 2 · airframe 17,104 hrs · 16,778 cycles

CLIP IN AFT CORNER OF PAX DOOR HINGE HAS CORROSION. REMOVED AND REPLACED CLIP.

Part: PDU — MALFUNCTIONED (THRUST REVERSER) · airframe 16,966 hrs · 16,627 cycles

LEFT THRUST REVERSER UNLOCKED MESSAGE IN FLIGHT. DEACTIVATED LT THRUST REVERSER IAW AMM TASK 78-30-00-040802, R & R LT THRUST REVERSER PDU REF AMM 78-32-03, OPS CHECKED GOOD. REMOVED PLACARD AND REMOVED FROM MEL.

Part: CONNECTOR — BROKEN (ANTI SKID XDUCER) · airframe 16,335 hrs · 15,997 cycles

OTBD ANTI SKID CAUTION MSG ON T/O 120-150 KTS, MSG DISAPPEARED ON T/O. R & R BROKEN CONNECTOR PLUG CONNECTOR ON RT OTBD TRANSDUCER. OPS CHECKED IAW AMM 32-40.

Part: UNKNOWN — SMOKE (CABIN) · airframe 14,980 hrs · 14,055 cycles

AFTER TAKEOFF, SMELLED AND VISUALLY SAW SMOKE IN COCKPIT ENTERED FROM VENT LOUVERS. ODOR DISSIPATED AFTER APPROX 2 MIN. PERFORMED AIR RETURN AND LANDED AT 44,000 LBS, NORMAL LANDING. INSPECTED APU AND PACKS. NO DEFECTS FOUND. INSPECTED DE-ICE FLUID INGESTION INTO INLET OF APU OR PACKS. PERFORMED GROUND RUN AND TEST OF ENVIRONMENTAL SYSTEM WITH ENGINES AND APU BLEEDS. NO DEFECTS FOUND REF AMM 21-61-01.

Part: DOOR — CRACKED (RT TRU) · airframe 15,336 hrs · 14,979 cycles

FOUND DAMAGE TO RT TRU DOOR T/E AND FRAME FOR AFT EDGE OF DOOR TRU. DOOR HAS 2 CRACKS 1 IN APPROX 2" AND THE OTHER IS APPROX 4". FUSELAGE FOR ALL EDGE OF DOOR IS BENT DOWN APPROX 1/4", NO CRACKS NOTED. TRU DOOR HAS 2 CRACKS 1 IS APPROX 2" AND OTHER IS APPROX 4" CHANNEL FOR AFT EDGE OF DOOR ON FUSELAGE IS BENT DOWN APPROX 1/4" NO CRACKS NOTED AT THIS TIME SPEED TAPED T/E OF TRU DOOR REF WO 141293 FOR REMOVAL AND REPLACEMENT OF DOOR AND SEAL ANGLE. OK FOR SERVICE.

Part: HANDLE — STICKING (PAX DOOR) · airframe 14,645 hrs · 14,328 cycles

PAX DOOR HANDLE FROM INSIDE IS STICKING. REMOVED AND REPLACED ICE BREAKER CABLE IAW AMM 52-00-00, OPS CHECK GOOD. (K)

Part: HANDLE — STUCK (PAX DOOR) · airframe 14,159 hrs · 13,843 cycles

PASSENGER DOOR WILL NOT OPEN, HANDLE WILL TURN, LOCKS WILL ROTATE OFF PINS BUT HANDLE DOES NOT GO TO FULL OPEN POSITION.

Part: CONTROL UNIT — MALFUNCTIONED (ANTI SKID SYSTEM) · airframe 14,108 hrs · 13,797 cycles

ANTI-SKID OTBD MESSAGE ILLUMINATED AT 90 KNOTS, ABORTED TAKEOFF AT 102 KNOTS. BTMS TEMPERATURES READ 7,6,7,2. REMOVED AND REPLACED ANTI-SKID CONTROL UNIT IAW AMM 32-44-06. OPS CHECK GOOD REF 05-51-27. (K)

Part: PUMP — INOPERATIVE (HYD SYSTEM) · airframe 12,445 hrs · 12,223 cycles

HYD 2 LOW PRESSURE CAUTION MESSAGE IN FLIGHT, COMPLIED WITH QRH, ENGINE NR 2 RAN APPROXIMATELY 45 MINUTES WITH ZERO HYDRAULIC QUANTITY. FOUND PRESSURE LINE DISCONNECTED FROM PRESSURE MANIFOLD, RECONNECTED LINE. LEAK CHECKED GOOD. REMOVED AND REPLACED EDP NR 2 DUE TO EXCESSIVE CAVITATION IAW AMM 29-11-01 AND AWAC SUPP 06-029, OPS AND LEAK CHECK GOOD. FOUND SEVERAL DAMAGED FAIRLEADS. REPLACED DAMAGED FAIRLEADS IAW AMM 29-11. (A)

Part: STIFFENER — CRACKED (PAX DOOR) · airframe 11,796 hrs · 11,592 cycles

PAX DOOR AFT STIFFENER ON AFT WEB 601R3117745-7 CRACKED. PAX DOOR AFT STIFFENER ON AFT WEB REPLACED IAW SRM 51-42-06 & SRM 51-42-13. (A)

Part: SILL — CORRODED (BS 319-349) · corrosion level 1 · airframe 11,796 hrs · 11,592 cycles

SERVICE DOOR LOWER SILL PLATE CORRODED. CORROSION ON SERVICE DOOR LOWER SILL PLATE REMOVED IAW CRJ 200 SRM 51-21-06. (A)

Part: PANEL — CRACKED (PAX DOOR STAIR) · airframe 11,796 hrs · 11,592 cycles

PAX DOOR STAIR FWD SIDE PANEL IS CRACKED BETWEEN STEP NR 1 AND STEP NR 2. REPAIRED IAW REO 601R-52-11-702 REV A. (A)

Part: ATTACH FITTING — CORRODED (BS 615) · corrosion level 1 · airframe 11,796 hrs · 11,592 cycles

CARGO DOOR NET ATTCHMENT FITTING AT FS 615 LBL 40 CORRODED. CORROSION REMOVED IAW CRJ 200 SRM 51-21-06. (A)

Part: SILL — CORRODED (BS 579-621) · corrosion level 1 · airframe 11,796 hrs · 11,592 cycles

CARGO DOOR LOWER SILL FS 579-621 CORRODED. CORROSION REMOVED IAW CRJ 200 SRM 51-21-06. (A)

Part: FLOORBEAM — CRACKED (BS 280) · airframe 11,796 hrs · 11,592 cycles

CROSSBEAM AT PILOTS BULKHEAD CRACKED. CROSS BEAM REPAIRED IAW REO 601R-53-11-171 REV D SCHEME B. (A)

Part: ATTACH FITTING — CRACKED (BS 280) · airframe 11,796 hrs · 11,592 cycles

CROSSBEAM OF PILOTS BULKHEAD OUTBOARD CLIP CRACKED FS 280 LBL 9. CLIP AT CROSS BEAM OF PILOTS BULKHEAD FS 280, LBL 9 REPLACED IAW CRJ 200 SRM 51-42-06. (A)

Part: FLOORBEAM — CRACKED (BS 280) · airframe 11,796 hrs · 11,592 cycles

CROSSBEAM AT PILOTS BULKHEAD CRACKED. REPAIRED IAW REO 601R-53-11-171 REV D SCHEME B. (A)

Part: SUPPORT BRACKET — CRACKED (BS 531) · airframe 11,796 hrs · 11,592 cycles

HYDRAULIC SUPPORT BRACKET (P/N 601R75262-159) CRACKED IN LT MLG BAY. HYDRAULIC SUPPORT BRACKET REPLACED IN LT MLG BAY IAW REO 601R-53-42-007. (A)

Part: BRACKET — CRACKED (RT ENGINE) · airframe 11,796 hrs · 11,592 cycles

ON RT ENGINE INLET BRACKET FOUND CRACKED AT STATION XN155.845 NEAR 5 O`CLOCK POSITION (LOOKING FWD). RT ENGINE BRACKET AT STATION XN 138.845 NEAR 5 O’CLOCK POSITION (LOOKING FWD) REPLACED IAW CRJ 200 SRM 51-42-06 & SRM 51-42-13. (A)

Part: BULKHEAD — CRACKED (BS 202) · airframe 11,796 hrs · 11,592 cycles

FWD PRESSURE BULKHEAD AT FS 202, LBL 23.71, WL 69.00 IS CRACKED. FWD PRESSURE BULKHEAD AT FS 202.00, LBL 23.71 WL 69.00 REPAIRED IAW REO 601R-53-11-563. (A)

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 11,796 hrs · 11,592 cycles

HYDRAULIC SUPPORT BRACKET (P/N 601R75262-153) CRACKED IN RT MLG BAY. HYDRAULIC SUPPORT BRACKET IN RT MLG BAY IAW REO 601R-53-42-007. (A)

Part: SILL — CRACKED (BS 574) · airframe 11,796 hrs · 11,592 cycles

CARGO BAY FLOOR SILL FOUND CRACKED AT FS 574.00. CARGO BAY FLOOR SILL AT FS 574.00 REPAIRED IAW REO 601R-53-61-1741. (A)

Part: SILL — CORRODED (BS 310-349) · corrosion level 1 · airframe 11,796 hrs · 11,592 cycles

PAX DOOR LOWER SILL CORRODED FS 310.00 AND FS 349.00. CORROSION ON PAX DOOR LOWER SILL BLENDED IAW CRJ 200 SRM 51-21-06. (A)

Part: SHAFT — CORRODED (ESCAPE HATCH) · airframe 11,796 hrs · 11,592 cycles

CREW ESCAPE HATCH OUTER HANDLE SHAFT IS CORRODED. CREW ESCAPE HATCH OUTER HANDLE SHAFT REPLACED IAW CMM 52-22-03. (A)

Part: SUPPORT BRACKET — CRACKED (BS 718) · airframe 11,796 hrs · 11,592 cycles

NR 2 HYDRAULIC MANIFOLD SUPPORT BRACKET AT FS 718.00 RT CRACK FOUND IN AFT LOWER CORNER. NR 2 HYDRAULIC MANIFOLD SUPPORT BRACKET AT FS 718.00 RT REWORKED IAW REO 601R-53-62-031. (A)

Part: PUMP — FAILED (HYDRAULIC SYS) · airframe 12,068 hrs · 11,851 cycles

IN FLIGHT RECEIVED SPOILERONS FAULT STATUS MESSAGE AND INBOARD GROUND SPOILER FAULT STATUS MESSAGE. AFTER HYDRAULIC PUMP 2B REPLACEMENT REF MEL 182321/3 OPS TESTED SPOILER SYS PER AMM 27-60-00 NO DEFECTS NOTED. PERFORMED SYSTEM BITE ON SECU NR 1 AND NR 2 ALL SYSTEM PASS REF FIM 27-60-00. (S)

Part: BUSS — SHORTED (COCKPIT) · airframe 12,002 hrs · 11,790 cycles

RECIEVED MASTER CAUTIOIN AC SERVICE BUSS, RAN QRH AND CONTINUED IN ARI AND ON GROUND, MESSAGE IS INTERMITTENT, POSSIBLE ELECTRICAL ODOR IN COCKPIT, PULLED CIRCUIT BREAKER PANEL 2, S2. R&R ACFT SERVICE BUS SENSE RELAY K5XD REF WDM 24-50-00. OPS CHECK GOOD IAW 24-51-20.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 11,958 hrs · 11,750 cycles

FIRST OFFICERS WINDSHIELD SHATTERED (OUTER PANE) ON CLIMBOUT AT 9000 FT COMPLIED WITH QRH AND LANDED WITHOUT INCIDENT IN RDU. REMOVED AND REPLACED FIRST OFFICER`S WINDSHIELD IAW 56-11-01, OPS CHECK GOOD, LEAK CHECK GOOD. (A)

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 11,796 hrs · 11,592 cycles

INTERCOSTAL FS 484.0 WL 72.0, LBL 27.0 ANGLE IS CRACKED. CORRECTIVE ACTION IN PROGRESS. (A)

Part: INTERCOSTAL — CRACKED (BS 484) · airframe 11,796 hrs · 11,592 cycles

INTERCOSTAL AT FS 484.0, WL 72.0, RBL 36.0 IS CRACKED. INTERCOSTAL REPAIRED IAW REO 601-53-41-059. (A)

Part: INTERCOSTAL — CRACKED (BS 484) · airframe 11,796 hrs · 11,592 cycles

INTERCOSTAL AT FS 484.0, WL 72.0, LBL 36 IN CRACKED. INTERCOSTAL REPAIRED IAW REO 601R-53-41-059. (A)

Part: SUPPORT BRACKET — CRACKED (BS 529) · airframe 11,796 hrs · 11,592 cycles

HYDRAULIC SUPPORT BRACKET (P/N 601R75262-157) CRACKED IN RT MLG BAY. HYDRAULIC SUPPORT BRACKET REPLACED IN RT MLG BAY IAW REO 601R-53-42-007. (A)

Part: AHRS — MALFUNCTIONED (NR 1) · airframe 11,371 hrs · 11,185 cycles

COMPLETE NR 1 AHRS FAILURE IN FLIGHT. COMPLIED WITH QRH. NO ALTITUDE OR COMPASS INFORMATION. AFTER REVERSIONARY SLELECTION TO NR 2, ALL DISPLAY INFO WAS NORMAL ON CAPTAINS SIDE. (K)

Part: FLAP — FAILED (WING) · airframe 11,094 hrs · 10,908 cycles

FLAPS FAILED ON RETRACTION AFTER LANDING. RT FLAP INDICATES -0- DEGREES, LT FLAP INDICATES 22 DEGREES. C/W FLAP RESET, FLAP FAIL DID NOT CLEAR. FOUND FLAPS COVERED WITH ICE AND SNOW, PUT AC IN HANGAR TO THAW. PERFORMED RESET IAW AWAC SUPPLEMENT 98-018B AND PERFORMED OPS CK AND SYSTEM CHECK OF FLAPS IAW 27-50-00, OPS CHECK GOOD. NO FAULT CODES NOTED. (K)

Part: BALLAST — FAULTY (CABIN) · airframe 10,743 hrs · 10,568 cycles

ELECTRICAL SMOKE ODOR IN AREA OF ROW 3, AT GATE NO PASSENGERS ONBOARD. IDENTIFIED BAD BALLAST FOR 4DF CEILING LIGHT. REMOVED AND REPLACED CEILING LIGHT 4DF POWER UNIT/DIMMER (111B) IAW CRJ200 AMM 33-21-04. OPS CHECK GOOD. (M)

Part: SOLENOID — LEAKING (APU) · airframe 9,004 hrs · 8,841 cycles

FUEL LEAK AND RUNNING DOWN BELLY SURFACE UNDER TAIL. FOUND APU FUEL SOLENOID LEAKING DRAINING OUT FUSELAGE BELLY DRAIN. DEACTIVATED APU, NO LEAK NOTED, REMOVED AND REPLACED FUEL SOLENOID AND O-RING AT LOWER ELBOW FITTING IAW AMM 49-31, NO LEAKS NOTED. (K)

Part: FLAP SYSTEM — JAMMED (LT WING)

ON APPROACH INTO YOW, FLAPS FAIL CAS MESSAGE FAILED AT 0 DEGREES, COMPLIED WITH QRH. LANDED AT APPROXIMATELY 40,600 LBS, CREW DID NOT CALL IN DISCREPANCY. NO HES/RTO INSPECTION REQUIRED. INTERROGATED FECU, FECU SHOWS FLAP FAIL WAS DUE TO JAM ON LEFT WING. REMOVED AND REPLACED LT BPSU, OPS CHECK GOOD. INSPECTED FLAPS, NO EVIDENCE OF TWISTING OR SKEWING IAW AWAC SUPPLEMENT 98-018A. RESET FLAP CIRCUIT BREAKERS ONCE, MESSAGE CLEARED. FLAPS OPERATE NORMALLY. PLACED ON 72 HOUR FLAP WATCH. REF 164559/4 FOR DIL FECU INTERROGATION. BRAKE AND POS SENS UNIT P/N 855D100-11, S/N 2262. (M)

Part: INDICATOR — MALFUNCTIONED (COCKPIT)

DURING TAKEOFF STANDBY INDICATED AIRSPEED INDICATED 0 TO 80 KNOTS. ABORTED TAKEOFF. MAX BTMS READINGS WERE 4444 WEIGHT = 43,000 LBS IAS NR 1 AND NR 2 INDICATED NORMAL. REMOVED AND REPLACED STANDBY ALT/IAS IAW 34-12-01, PERFORMED PITOT STATIC LEAK CHECK, OPS CHECK GOOD IAW AMM 34-11-00. (M)

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS)

WHEN SELECTING FLAPS 30 DEGREES ON APPROACH, FLAP FAIL CAUTION MESSAGE ILLUMINATED, FLAPS REMAINED AT 20 DEGREES. LOCAL MAINTENANCE VISUAL INSPECTED FLAPS RESET C/B`S PER AMM SUPPLEMENT 98-018A, FLAPS OPERATE NORMALLY. PLACED ON 72 HOUR WATCH. (M)

Part: BPSU — FAULTY (T/E FLAP)

FLAPS FAILED AT ZERO DEGREES WHEN SELECTED ON APPROACH. CROSS REFERENCE: A6WA200740030 - FOUND EVIDENCE OF WATER IN RT NR 3 AND NR 4 FLEX DRIVE SHAFT, CLEANED FLEX DRIVE SHAFTS NR 3 AND NR 4. (K) WHEN SELECTING FLAPS FROM 8 DEGREES TO 20 DEGREES, A FLAP CAUTION MESSAGE OCCURRED IN FLIGHT. REMOVED AND REPLACED LT BRAKE AND POSITION SENSOR UNIT (BPSU). PERFORMED RIG AND OPS TEST, OPS TEST GOOD AT THIS TIME. (K)

Part: WINDSHIELD — CRACKED (COCKPIT)

FIRST OFFICERS WINDSCREEN IS CRACKED, FL220, CRUISE, WINDOW HEAT ON. REPLACED FIRST OFFICERS WINDSHIELD IAW CRJ AMM 56-10-00, OPS TEST GOOD. (M)

Part: CONNECTOR — DIRTY (PAX DOOR)

DOOR MOTOR CONTINUOUSLY RUNNING WITH DOOR SHUT. INSPECTED AND CLEANED PASSENGER DOOR ASSIST MOTOR CONNECTOR IAW CH 52. OPS CHECK GOOD AT THIS TIME.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

EMERGENCY FLOOR LIGHTING FORWARD SECTION DOES NOT ILLUMINATE. FOUND ELECTRICAL CONNECTIONS SWAPPED. RECONNECTED ELECTRICAL CONNECTIONS. TEST CARRIED OUT PER AMM 33-51-00-710-801 SATISFACTORILY. (M)

Part: SKIN — CORRODED (LT WING)

FOUND LEFT WING PLANK ACCESS CUTOUT FLANGE AT FUEL PANEL 540FB, HOLE NR 8 AT WS 139 HAS MINOR CORROSION APPROX .003 INCH DEEP ON 90 PERCENT OF CIRCUMSTANCE. REPAIRED THE LEFT WING LOWER PLANK PANEL CUTOUTS IAW BSC EO 601R-57-9567A. (M)

Part: SKIN — CORRODED (LT WING)

FOUND LEFT WING PLANK ACCESS CUTOUT FLANGE AT FUEL PANEL 510AB HOLE NR 2 AT WS 11.00 HAS MINOR CORROSION APPROX .002 INCH DEEP ON 60 PERCENT OF CIRCUMFERENCE. MAINTENANCE REPAIRED THE LEFT WING PLANK FUEL PANEL CUTOUT IAW BSC EO 601R-57-9567A. (M)

Part: FLOORBEAM — CRACKED (BS 621)

FOUND LEFT SIDE FS 621 FLOORBEAM ANGLE CRACKED APPROX 1.3 INCH LONG. MAINTENANCE REMOVED DAMAGED PORTION OF LT SIDE FS 621 FLOOR SUPPORT ANGLE REO 601R-53-61-117. IAW REO 601R-53-61-117 REV C. (M)

Part: FLOORBEAM — CRACKED (BS 621)

FOUND RIGHT SIDE FS 621 FLOORBEAM ANGLE CRACKS APPROX .7 INCH LONG. MAINTENANCE REMOVED DAMAGED PORTION OF RIGHT SIDE 621 FS FLOOR SUPPORT ANGLE IAW REO 601R-53-61-117 COMPLETED REPAIR OF RIGHT FS 621 ANGLE USING 2024 T3 .090 INCH P/N 601R53-61-117-2 AND 601R53-61-004-6 IAW REO 601R-53-61-117 REV C. (M)

Part: HANDLE — LACK OF LUBE (ESCAPE HATCH)

CREW ESCAPE HATCH OUTER HANDLE RELEASE BUTTON WON`T DEPLOY. CLEANED DIRT AND DEBRIS FROM RELEASE BUTTON AND OUTER HANDLE AND LUBED OUTER HANDLE AND RELEASE BUTTON. (M)

Part: ANGLE — CRACKED (BS 625)

FOUND FS 625 LEFT OBLIQUE ANGLE IS CRACKED APPROX .75 INCH. MAINTENANCE REPLACED FS 625 LT OBLIQUE ANGLE P/N 601-35012-51 WITH NEW IAW CRJ SRM 51-42-06. (M)

Part: GENERATOR — MALFUNCTIONED (NR 2)

GEN NR 2 OFFLINE 15 SECONDS AFTER TURNING IT ON, WILL NOT RESET. (M)

Part: CHECK VALVE — MALFUNCTIONED (LT ENGINE)

LEFT ENGINE OIL PRESSURE MASTER WARNING IN FLIGHT. REMOVED LEFT ENGINE OIL REPLENISHMENT CHECK VALVE. INSTALLED CHECK VALVE TAGGED REPAIR, P/N 2810044-101, S/N 972. ADDED 5 QUARTS TO LEFT ENGINE. OIL TANK SERVICED TO 5 1/2 FULL RED AMM 79-12-13. NO LEAKS NOTED. (M)

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 3,848 hrs · 3,980 cycles

UPON GEAR RETRACTION, NOSE DOOR END GEAR DISAGREE WARNING MESSAGE ILLUMINATED. CYCLED NLG WITH LINKS ATTACHED OPS CHECK GOOD OK FOR RETURN TO SERVICE IAW. (K)

Part: SKIN — GOUGED (FUSELAGE)

FOUND DENT/GOUGE IN LEFT SIDE AFT FUSELAGE SKIN AT FS 612, BETWEEN STRINGERS 24L AND 25L. MEASURES 2 INCH BY 1.8 INCH BY .040 INCH DEEP. PERFORMED A MAJOR REPAIR B4 CUTTING AWAY DAMAGED SKIN AND INSTALLING PN EXTERNAL DOUBLER IAW CRJ SRM 53-00-31 REPAIR NR 1. (M)

Part: INTERCOSTAL — CRACKED (FUSELAGE)

FOUND RIGHT SIDE FS 621-625.3 INTERCOSTAL AT STRINGER 14R IS CRACKED IN RADIUS .6 INCH LONG. REMOVED CRACKED INTERCOSTAL AND REPLACED WITH NEW INTERCOSTAL IAW CRJ200 SRM 51-42-06. (M)

Part: COMPUTER — MALFUNCTIONED (PITCH CONTROL) · airframe 3,160 hrs · 3,392 cycles

ON COMMAND OF AUTOPILOT DISENGAGEMENT, PITCH CONTROL DID NOT DISENGAGE FOR APPROX 5-10 SECONDS.