N453AW

Part: ADG — UNWANTED DEPLOY · airframe 37,755 hrs · 36,943 cycles

ADG DEPLOYED IN FLIGHT AT APPROX 280 KTS. ADG WAS DEPLOYED FOR 72 MINS. AC ESSENTIAL BUS WAS NEVER DE-POWERED. AIRCRAFT REMOVED FROM SERVICE. COMPLIED WITH SUP 16-172, TROUBLESHOT, PER FIM 24-23-00, NO FAULT FOUND. PERFORMED SPECIAL VISUAL INSPECTION OF ADG, IAW AMM 24-23-01 AND AWAC SUP 10-066A. NO DAMAGE FOUND, REF PAGE 319685/3 FOR MEL OF NDT PENETRANT INSPECTION OF ADG.

Part: SEAT TRACK — CORRODED (BS 559) · corrosion level 2 · airframe 37,753 hrs · 36,942 cycles

LBL 9 AT FS 559+80 SEAT TRACK AFT SECTION 6" STRIP HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED SEAT TRACK AT FS 559 AT LBL 9, IAW REO 601R-53-00-764.

Part: TIMER — CORRODED (TOILET) · corrosion level 2 · airframe 37,753 hrs · 36,942 cycles

TOILET TIMER HAS CORROSION ON HOUSING AT ATTACH POINTS. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED TIMER, IAW AMM25-41-00-04.

Part: SEAT TRACK — CORRODED (BS 429-570) · corrosion level 2 · airframe 37,753 hrs · 36,942 cycles

NR-N RBL 9 SEAT TRACK AT FS 429 THROUGH FS 570 HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED SEAT TRACK AT FS 429-FS 570 AT RBL 9, IAW REO 601R-53-00-764.

Part: SPAR — CRACKED (RT WING) · airframe 37,753 hrs · 36,942 cycles

RIGHT WING LOWER EDGE OF REAR SPAR AT WS 62.5 SUSPECTED CRACK/CORROSION INDICATION DETECTED DURING NDT INSPECTION. AIRCRAFT REMOVED FROM SERVICE. DAMAGE WAS REMOVED BY BLENDING WITH A MINIMUM REMAINING THICKNESS OF .235" NDT EVALUATION SHOW NO CRACK EXIST. REPAIR IS IAW EA#AWAC-CRJ257-01511.

Part: UNKNOWN — UNKNOWN (MLG) · airframe 35,528 hrs · 34,725 cycles

DURING CLIMB AFTER DEPARTURE, THE FLIGHT CREW NOTED THE LANDING GEAR TOOK AN ABNORMALLY LONG TIME TO RETRACT. THE CREW EVALUATED THE SITUATION AND ELECTED TO RETURN TO KIAD. THE CREW DECLARED AN EMERGENCY AND COORDINATED WITH DISPATCH. THE FLIGHT HELD TO BURN FUEL BEFORE RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. PARK BRAKE SOV & A/SKID INBD CAUTION MSG APPEARED WHEN GEAR HANDLE SELECTIED TO UP. GEAR REMAINED DOWN FOR 4 MIN. LANDING GEAR MOVED TO RETRACTED/UP INDICATION & ALL ABNORMAL INDICATION/MSGS DISAPPEARED. HYD TEMP,PRES,QTY INDICATIONS NORMAL. EMERGENCY DECLARED.

Part: DOOR SEAL — DEFECTIVE (SERVICE DOOR) · airframe 34,785 hrs · 34,005 cycles

FOLLOWING HEAVY CHECK MAINTENANCE DURING CLIMB OUT CREW HEARD A LOUD POP THEN CABIN BEGAN TO DEPRESSURIZE. CREW COMPLIED WITH QRH AND REDUCED ALTITUDE AND DIVERTED BACK TO OKC FOR INSPECTION. FOUND SERVICE DOOR SEAL WITH NO VENT HOLES, CUT HOLES IN SEAL IAW AMM 52-41-07, PRESSURE CHECK GOOD

Part: LANDING — CRACKED (BS 169-193) · airframe 34,783 hrs · 34,003 cycles

LEFT TRU DOOR LANDING AFT LATCH AREA HAS CRACK. REPLACED LH TRU DOOR LANDING IAW AWAC SUPPLEMENT 17-280

Part: SKIN — CRACKED (RT WING) · airframe 34,783 hrs · 34,003 cycles

RT OB WING LE HAS 2 CRACKED EDGING BY RIVETS. REPLACED RT OB WING LE EDGING IAW SRM 51-42-13.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,783 hrs · 34,003 cycles

FLOORBEAM CORRODED AT FS 559+86, RBL9. REPAIRED FLOORBEAM IAW SRM 53-00-43.

Part: SKIN — CRACKED (FUSELAGE) · airframe 34,783 hrs · 34,003 cycles

AFT NLG DOOR CUT OUT, AFT RIGHT CORNER FUSELAGE SKIN IS CRACKED. REPAIRED NLG AFT DOOR CUT OUT FUSELAGE SKIN IAW REO 601R-53-11-0048 REV-D.

Part: SKIN — CHAFED (TE FLAP VANE) · airframe 34,783 hrs · 34,003 cycles

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

Part: TORQUE BOX — CRACKED (THRUST REVERSER) · airframe 34,783 hrs · 34,003 cycles

NR 1 T/R AFT TORQUE BOX CRACKED AT THE 7 O'CLOCK POSITION. REPAIRED T/R TORQUE BOX AT THE 7O'CLOCK POSITION IAW REO 601R-78-30-2616 REV-NC.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 34,783 hrs · 34,003 cycles

ENGINE SUPPORT BEAM LT LOWER FUSELAGE ATTACH ANGLE CRACKED. REPLACED ANGLE IAW SRM 51-42-21.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 34,783 hrs · 34,003 cycles

PAX DOOR AFT DRAG ANGLE CRACKED AT PULLEY BRACKET. REPAIRED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,783 hrs · 34,003 cycles

RIGHT FLOOR SEAT TRACK NR 1 CORRODED. REPLACED SEAT TRACK IAW AMM 53-01-11.

Part: FITTING — CRACKED (FUSELAGE) · airframe 34,783 hrs · 34,003 cycles

AFT PRESSURE BULKHEAD CLIP CRACKED AT FS 625.00, STR 15L. REPLACED CLIP IAW SRM TR51-42, 51-42-21.

Part: FITTING — CRACKED (FUSELAGE) · airframe 34,783 hrs · 34,003 cycles

AFT PRESSURE BULKHEAD CLIP CRACKED AT FS 625.00, STR 15R. REPLACED CLIP IAW SRM TR51-42, 51-42-21.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 34,783 hrs · 34,003 cycles

AFT PRESSURE BULKHEAD HAS 2 CRACKS AT BL 0.0, WL 110. REPAIRED BULKHEAD IAW REO 601R-53-61-1285 REV-E.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 34,783 hrs · 34,003 cycles

AFT PRESSURE BULKHEAD HAS 2 CRACKS AT FS621.00, BL0.0, WL 132.0. REPAIRED BULKHEAD IAW REO601R-53-61-1285 REV-E.

Part: TORQUE BOX — CRACKED (THRUST REVERSER) · airframe 34,783 hrs · 34,003 cycles

NR 1 THRUST REVERSER TORQUE BOX IS CRACKED AT THE 5 O'CLOCK POSITION. REPAIRED NR 1 T/R TORQUE BOX IAW REO601R-78-30-2616 REV-NC.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 34,783 hrs · 34,003 cycles

VERTICAL POST AT FS409+128 AND BL 0.0, WL 69.0 IS CRACKED IN THE RIGHT AFT RADIUS. VERTICAL POST FOUND TO NOT BE CRACKED, REINFORCEMENT ANGLE WAS CRACKED. REPLACED REINFORCEMENT ANGLE IAW SRM TR51-42, 51-42-06, REO 601R-53-41889 REV-C.

Part: RETAINER — CRACKED (PYLON) · airframe 34,783 hrs · 34,003 cycles

PYLON PANEL 412BT SEAL RETAINER CRACKED. REPLACED SEAL RETAINER IAW SRM 51-42-06.

Part: RETAINER — CRACKED (PYLON) · airframe 34,783 hrs · 34,003 cycles

PYLON PANEL 422BT SEAL RETAINER CRACKED. REPLACED SEAL RETAINER IAW SRM 51-42-06.

Part: FITTING — CRACKED (FUSELAGE) · airframe 34,783 hrs · 34,003 cycles

FS 484.00 OUTBOARD CLIP CRACKED AT LBL27. REPLACED CLIP IAW CRJ200 SRM 51-42-06, 51-42-21, 51-24-36, TR 51-42.

Part: STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,783 hrs · 34,003 cycles

FLOOR SUPPORT STRAP CORRODED AT FS559.00, RBL29 TO RBL43. REPAIRED STRAP IAW EA AWAC-CRJ253-01045 REV-IR.

Part: UNKNOWN — UNKNOWN (FLT CONTROLS) · airframe 33,975 hrs · 33,252 cycles

DURING DESCENT, AN UNCOMMANDED YAW AND ROLL OCCURED AT 16000 FT. RAN QRH FOR THE UNCOMMANDED YAW MOTION AND DISCONNECTED YAW DAMPERS. YAW CONTINUED ALL THE WAY TO TOUCH DOWN. INTERMITTENT LEFT AND RIGHT DUTCH ROLL.

Part: LIGHT — CONTAMINATED (ROWS 2-5) · airframe 33,043 hrs · 32,338 cycles

DURING PRE-FLIGHT ACCEPTANCE CHECK, CREW FOUND THAT THE EMERGENCY LIGHTS FROM ROWS 2-5 WERE INOPERATIVE INSPECTED AND FOUND WATER IN THE LIGHT. REMOVED WATER AND INSTALLED. SYSTEM OPS CHECKED GOOD IAW 16-374A.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 32,454 hrs · 31,782 cycles

EMERGENCY FLOOR LIGHTING ROW 9 AND AFT NOT ILLUMINATING. R&R NR 4 EMERGENCY LIGHT INVERTER IAW AMM 33-51. OPS CHECK GOOD AT THIS TIME.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 32,446 hrs · 31,767 cycles

FLOOR EMERGENCY LIGHTS FROM ROW 9 TO AFT NOT WORKING. R & R THE BATTERY PACK AT POSITION 4 IAW AMM 33-51-04. OPS CHECKED GOOD.

Part: UNKNOWN — ODOR (CABIN) · airframe 31,669 hrs · 31,042 cycles

CREW REPORTED THAT AT FLIGHT LEVEL 16,000 A STRONG ODOR OF EXHAUST FUMES, CABIN PRESSURE WAS NORMAL, APU WAS OFF, PACKS WERE RUNNING ON ENGINES AND SET TO AUTO, ODOR WAS PRESENT IN COCKPIT ONLY, FA COULD NOT ODOR ANYTHING ABNORMAL IN THE CABIN.

Part: PLUG — MIGRATED (PRESSURE PANEL) · airframe 31,287 hrs · 30,681 cycles

DURING CUSTOMER WALK, FOUND 3 FREEZE PLUGS PUSHING IN ON FWD PRESSURE PNL 132AL.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,287 hrs · 30,681 cycles

RT FLOOR SILL CORRODED BETWEEN FS 559+48 AND 559+112 RBL 43.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,287 hrs · 30,681 cycles

PAX DOOR SILL FLOOR SUPPORT ANGLE CORRODED AROUND NUTPLATES.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 31,287 hrs · 30,681 cycles

FUSELAGE EXTERNAL SKIN HAS LIGHTNING STRIKE DAMAGE ON SKIN AND STRINGER AT FS 248-265 S14L.

Part: FRAME — CRACKED (FUSELAGE) · airframe 31,287 hrs · 30,681 cycles

FRAME 333 IS CRACKED JUST I/B OF STR 1L.

Part: SKIN — DENTED (TE FLAP) · airframe 31,287 hrs · 30,681 cycles

LEFT I/B FLAP HAS DENT ON LOWER SURFACE AT WS 56.30. REPLACED DAMAGED SECTION OF LOWER LT I/B FLAP SKIN FROM WS 64.00 TO I/B CORNER IAW REO 601R-57-52-1544.

Part: BRACKET — CRACKED (WINDOW POST) · airframe 31,287 hrs · 30,681 cycles

PILOT WINDSHIELD LWR INBD BRACKET AT CENTER POST IS CRACKED.

Part: INTERCOSTAL — CRACKED (BS 621 BULKHEAD) · airframe 31,287 hrs · 30,681 cycles

BS 621 BULKHEAD INTERCOSTAL ANGLE STRINGER 13L IS CRACKED

Part: INTERCOSTAL — CRACKED (BS 621 BULKHEAD) · airframe 31,287 hrs · 30,681 cycles

BS 621 BULKHEAD INTERCOSTAL ANGLE STRINGER 14L IS CRACKED

Part: ANGLE — CRACKED (BS 621 BULKHEAD) · airframe 31,287 hrs · 30,681 cycles

BS 621 BULKHEAD INTERCOSTAL ANGLE STRINGER 15L IS CRACKED

Part: DOOR SILL — CRACKED (CARGO DOORWAY) · airframe 31,287 hrs · 30,681 cycles

CARGO DOOR SILL PLATE CRACKED AT FS 589 FROM I/B FASTENER TO EDGE OF PART.

Part: ATTACH ANGLE — CRACKED (WINDSHIELD POST) · airframe 31,287 hrs · 30,681 cycles

LEFT WINDSHIELD SIDE POST OTBD ATTACH ANGLE CRACKED.

Part: ANGLE — CRACKED (WINDOW POST) · airframe 31,287 hrs · 30,681 cycles

RIGHT WINDSHIELD SIDE POST OTBD ATTACH ANGLE CRACKED.

Part: FLOORBEAM — CRACKED (BS 484) · airframe 31,287 hrs · 30,681 cycles

FLOORBEAM RBL 27, OTBB ANGLE IS CRACKED AT BS 484.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 31,072 hrs · 30,478 cycles

FLIGHT 4069, LAST SECTION OF EMERGENCY LIGHTS INOPERATIVE. ROWS 9-12. R & R INVERTER IAW AMM, OP CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,754 hrs · 30,176 cycles

FLIGHT 4018. FLOOR EMERGENCY LIGHTS INOPERATIVE BEHIND ROW 8.

Part: CONNECTOR — DETACHED (EMERGENCY LIGHTS) · airframe 30,911 hrs · 30,326 cycles

FLIGHT 3822. EMERGENCY LIGHTS AFT OF ROW 8 INOPERATIVE. RECONNECTED EMERGENCY LIGHT STRIP FROM STRIP AT ROW 8F.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 30,472 hrs · 29,908 cycles

COMPLIED WITH PERMANENT REPAIR TO FS 621 PRESS BULKHEAD AT LBL 27.5, WL 131, REPAIRED.

Part: UNKNOWN — MALFUNCTIONED (CABIN) · airframe 29,583 hrs · 29,065 cycles

3758 EMERGENCY FLOOR LIGHT AT PAX DOOR EXIT COMES ON, THEN GOES OUT WHEN TURNED ON.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,577 hrs · 29,060 cycles

EMERGENCY LIGHTS AFT OF ROW 8 DO NOT ILLUMINATE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,946 hrs · 28,448 cycles

EMERGENCY LIGHTS AFT OF ROW 12 WILL NOT ILLUMINATE, APPROXIMATELY 10 INCHES IN LENGTH. R & R THE EMERGENCY LIGHT IAW AMM 33-51-01 & SUPP 12-032. OPS CHECKED GOOD.

Part: A/C PACK — SHUTDOWN (LEFT) · airframe 28,458 hrs · 27,980 cycles

DURING CLIMB, LOST LEFT A/C PACK. COMPLIED WITH QRH, PACK DID NOT COME BACK ON. COMPLIED WITH EMERGENCY DESCENT. INSPECTED NR 1 PACK DUCTS IN APU BAY. NO FAULTS FOUND. COMPLIED WITH OPS CHECK. PACK OPS GOOD USING APU AIR OR ENGINE AIR AT LOW & HIGH POWER.

Part: CAP — MISSING (EMERGENCY LIGHTS) · airframe 27,958 hrs · 27,508 cycles

FLIGHT 3846 FLOOR TRACK LIGHTING FWD END CAP MISSING. REPLACE FLOOR TRACK LIGHTING FWD END CAP IAW SUPP 13-022.

Part: COVER — CRACKED (EMERGENCY LIGHT)

EMERGENCY LIGHT COVER AT ROW 2 DETACHED AND CRACKED. REPLACED THE EMERGENCY LIGHT COVER AT ROW 1 - 3. OPS CHECKED GOOD.

Part: SKIN — CHAFED (LT AILERON) · airframe 26,726 hrs · 26,313 cycles

LEFT AILERON UPPER OTBD LE HAS DEEP CHAFING.

Part: SKIN — DENTED (TE FLAP) · airframe 26,726 hrs · 26,313 cycles

LEFT INBD FLAP HAS A DENT & NICK ON THE BOTTOM SKIN SURFACE AT INBD FWD CORNER AT FS 53.50.

Part: PANEL — CRACKED (PAX DOOR) · airframe 26,726 hrs · 26,313 cycles

PASSENGER DOOR AFT STAIR PANEL CRACKED 2 PLACES.

Part: PANEL — CRACKED (PAX DOOR) · airframe 26,726 hrs · 26,313 cycles

PASSENGER DOOR STEP FWD & AFT PANELS HAVE CRACKS IN RADIUS AT 1ST TO 2ND STEPS.

Part: PANEL — CRACKED (PAX DOOR) · airframe 26,726 hrs · 26,313 cycles

PASSENGER DOOR FWD STAIR SUPPORT PANEL CRACKED AT 3RD & 4TH RISERS.

Part: SKIN — DAMAGED (RT ELEVATOR) · airframe 26,726 hrs · 26,313 cycles

RIGHT ELEVATOR TE HAS LIGHTNING STRIKE BURN ES 77.68.

Part: SUPPORT BRACKET — GOUGED (LAVATORY) · airframe 26,726 hrs · 26,313 cycles

LAVATORY WATER TANK CARGO COMPARTMENT LINER HAS TWO GOUGED SUPPORT BRACKETS.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,726 hrs · 26,313 cycles

LEFT SIDE SEAT RAIL HAS CORROSION AT FS 559 + 40.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 26,726 hrs · 26,313 cycles

AFT SIDE OF 621 BULKHEAD HAS CRACKED OBLIQUE ANGLE AT STRINGER 14R.

Part: TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,726 hrs · 26,313 cycles

FOUR EACH 9G TIE DOWN TRACK AT FS 559 + 96 & LBL 27 & RBL 27.

Part: TIE DOWN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,726 hrs · 26,313 cycles

ONE EACH TIE DOWN AT FS 559 + 112 HAS CORROSION.

Part: SKIN — CHAFED (TE FLAP VANE) · airframe 26,726 hrs · 26,313 cycles

LEFT WING INBD FLAP VANE LE HAS THREE EACH GOUGES FROM THE STOPS INBD, OTBD & CTR.

Part: BRACKET — CRACKED (LT MLG WW) · airframe 26,726 hrs · 26,313 cycles

LT WW TRANSDUCER BRACKET IS CRACKED.

Part: MOUNT BRACKET — CRACKED (PAX DOOR) · airframe 26,726 hrs · 26,313 cycles

PASSENGER DOOR ASSIST MOTOR MOUNT BRACKET CRACKED.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 26,726 hrs · 26,313 cycles

OBLIQUE ANGLE CRACKED AT STRINGER 14 FS 625.

Part: FITTING — CRACKED (FUSELAGE) · airframe 26,726 hrs · 26,313 cycles

FS 484 INTERCOSTAL CLIP AT LBL 27 CRACKED.

Part: BRACKET — CRACKED (RT MLG WW) · airframe 26,726 hrs · 26,313 cycles

RT WW TRANSDUCER BRACKET IS CRACKED.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 26,726 hrs · 26,313 cycles

GND POWER RECEPTACLE BRACKET IS CRACKED AT SCREW HOLE.

Part: BRACKET — CRACKED (RT MLG WW) · airframe 26,726 hrs · 26,313 cycles

RT WW TRANSDUCER BRACKET IS CRACKED.

Part: SKIN — CHAFED (TE FLAP VANE) · airframe 26,726 hrs · 26,313 cycles

RIGHT INBD FLAP VANE LE SKIN CHAFED FROM STOP, CTR SKIN BEYOND LIMITS.

Part: RIB — CRACKED (RT WING) · airframe 26,726 hrs · 26,313 cycles

RIGHT MLG WW BATTERY RIB CRACKED.

Part: RIB — CRACKED (LT WING) · airframe 26,726 hrs · 26,313 cycles

LEFT MLG WW BATTERY RIB CRACKED.

Part: BULKHEAD — CHAFED (FUSELAGE) · airframe 26,726 hrs · 26,313 cycles

FS 280 BULKHEAD AFT SIDE WEB CHAFED RT SIDE 20 INCHES ABOVE FLOOR.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 26,726 hrs · 26,313 cycles

INBD & OTBD FLOORBEAM ATTACH CLIPS CRACKED, LBL & RBL 9 AT FS 280.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,726 hrs · 26,313 cycles

LOWER FRAME SECTION AT FS 605 CORRODED BEYOND LIMITS.

Part: FITTING — LOOSE (APU) · airframe 25,660 hrs · 25,320 cycles

STRONG FUEL SMELL IN CABIN & FUEL LEAK COMING FROM APU DRAIN LINE. FOUND FUEL LEAK ON FITTINGS ON FUEL SOLENOID VLV COMING INTO FCU. TIGHTENED FITTING IAW AMM 49-31-05. OPERATIONS CHECKED GOOD, AIRED OUT CABIN, FUEL SMELL WENT AWAY. VERIFIED PACK AIR, PACK AIR GOOD WITH NO FUEL SMELL.

Part: FLAP — MALFUNCTIONED (WING) · airframe 25,118 hrs · 24,809 cycles

RECEIVED FLAPS FAIL CAS MSG WHEN SETTING FLAPS TO 30 ON APPROACH, FLAPS INDICATED 30. RAN QRH & LANDED. PERFORMED FLAP RESET PROCEDURE IAW AWAC SUPP 99-18F BOX 12. FLAPS RESET, PLACARDED & PLACED ON MEL.

Part: SEALANT — MISSING (FAIRING) · airframe 24,420 hrs · 24,133 cycles

AIRFRAME VIBRATION ABOVE 250 KTS. ENGINE INDICATIONS NORMAL NO ISSUES WITH FLIGHT CONTROLS. FOUND SEALANT MISSING FROM BELLY FAIRING FORWARD OF MLG IN THE CENTER OF THE ACFT APPLIED SEALANT TO BELLY FAIRING PANEL 193AB L/E REF AMM 51-23-00.

Part: WINDOW — CRACKED (COCKPIT) · airframe 23,098 hrs · 22,849 cycles

FO'S SIDE WINDOW CRACKED IN FLT AT 12,000FT ON DESCENT-CRACKS APPEARS AT LOWER LEFT CORNER. REMOVED AND REPLACED F/O'S SIDE WINDOW. OK FOR CONTINUED SERVICE.

Part: LIGHT — LOOSE (GALLEY) · airframe 22,287 hrs · 22,031 cycles

STRONG ELECTRICAL BURNING OR MELTING PLASTIC ODOR IN COCKPIT IMMEDIATELY AFTER LANDING GOES AWAY AFTER 5 MINUTES. INSPECTED AND FOUND TOP GALLEY SERVICE LIGHT BULB LOOSE IN CARRIER CAUSING INTERMITTENT SHORT. REMOVED BULB, OK TO CONTINUE ON MEL 33-21-01 REF 247119/3.

Part: DUCT — LOOSE (BLEED AIR) · airframe 21,313 hrs · 21,080 cycles

FLT 453. RIGHT 14TH DUCT WARNING MESSAGE IN FLIGHT AS 12,000 FT WITH ANTI-ICE OFF. COMPLIED WITH QRH & MESSAGE PERSISTS. A/I PAGE SHOWS RED AT "T" BETWEEN 14TH STAGE SHUTOFF VALVE AND THE WING & COWL SHUTOFF VALVES. PERFORMED OPS TEST OF FIRE LOOPS. NO FAULTS FOUND. OPS CHECKED GOOD. FOUND LOOSE 14TH STAGE DUCTING BOOT 2" BELOW FIRE LOOP. RESECURED AND LEAK CHECKED IAW SUPPLEMENT 99-016. NO LEAKS FOUND.

Part: DOWNLOCK SENSOR — OUT OF ADJUST (MLG) · airframe 20,168 hrs · 19,907 cycles

AFTER SELECTING GEAR LEVER UP, RECEIVED INBD ANTI-SKID CAUTION MESSAGE, SHORTLY FOLLOWED BY DISAGREE WARNING. RT MLG INDICATED DOWN AND GREEN FOR SHORT PERIOD, THEN GEAR RETRACTED AND MESSAGES CLEARED. MESSAGES CLEARED. MESSAGES WERE PRESENT FOR APPROX 5 SECONDS. RESET LT AND RT MLG DOWNLOCK PROXIMITY SENSORS. ADJUSTED RT MLG DOWNLOCK AND WOW SENSORS AND NLG UPLOCK SENSOR. COMPLETED MULTIPLE GEAR SWINGS. INDICATIONS NORMAL AT THIS TIME.

Part: ACTUATOR — INOPERATIVE (NLG)

NOSE DOOR OPEN MESSAGE ILLUMINATED FOR 30-45 SECONDS AFTER GEAR WAS UP AND LOCKED, CW QRH. EXTENDED GEAR. MESSAGE CLEARED WHILE GEAR WAS EXTENDING. MESSAGE RETURNED WHEN GEAR DOWN AND LOCKED. R & R NLG DOOR ACTUATOR IAW AMM 32-22-10.

Part: PROXIMITY SWITCH — OUT OF ADJUST (NLG) · airframe 19,610 hrs · 19,335 cycles

NOSE DOOR OPEN WARNING MESSAGE AT 15000 FT. MESSAGE REMAINED AFTER GEAR EXTENSION. ADJUSTED LT AND RT NLG DOOR FWD PROXIMITY SWITCHES IAW AMM 32-61-05. PERFORMED EXTENSION/RETRACTION CHECK IAW AMM 32-30-00.

Part: WIRE HARNESS — UNKNOWN (NLG UPLOCK) · airframe 19,359 hrs · 19,093 cycles

DURING CLIMBOUT AT 10,000 FT, RECEIVED GEAR DISAGREE AURAL AND WARNING MESSAGE. UNABLE TO DUPLICATE PROBLEM, PERFORMED RIG CHECK OF NLG UPLOCK, WITHIN LIMITS, SUSPECT NLG UPLOCK HARNESS. R & R UPLOCK PS3GA IAW AMM 326105, OPS CK GOOD AT THIS TIME.

Part: ACM — FAILED (LEFT) · airframe 18,037 hrs · 17,678 cycles

HEAVY SMOKE IN ACFT AFTER LANDING. SHUT OFF PACKS- DISSIPATED. R & R LT ACM, OPS CK OK. REF AMM 21-51-10-04. THIS CLEARS MEL AND PLACARD REMOVED.

Part: FITTING — LEAKING (HYD SYSTEM) · airframe 17,232 hrs · 16,800 cycles

ON TAKEOFF, NR2 MAIN TIRE BURST AS REPORTED BY CREW, ACFT RETURNED TO DEPARTURE, CREW REPORTED TO MX CONTROL, DID NOT LAND OVERWEIGHT. REF W/O 160575 FOR ALL WORK PERFORMED. FOUND NR2 BRAKE DISCONECT FITTING LEAKING. R & R FITTING AND NR1 AND NR2 TIRE AND BRAKE.

Part: HANDLE — CRACKED (PAX DOOR) · airframe 17,173 hrs · 16,739 cycles

PAX DOOR OUTER HANDLE CRACKED. REMOVED CRACKED OUTER HANDLE INSTALLED NEW SERVICEABLE HANDLE IAW AMM 52-11-03, COMPLIED WITH OPS CHECK IAW AMM 52-11-03-710-502. NO DEFECTS NOTED.

Part: BULKHEAD — CHAFED (BS 621) · airframe 17,173 hrs · 16,739 cycles

AFT PRESSURE BULKHEAD FWD SKIN HAS CHAFE AT FS 621.00 BETWEEN LBL 36.20 AND LBL 27.50. REPAIRED FWD FACE OF FS 621.00 BULKHEAD IAW REO 601R-53-61-3865.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,173 hrs · 16,739 cycles

NR1 FLOOR SEAT TRACK ON RBL9 IS CORRODED. REMOVED UNSERVICEABLE NR1 FLOOR SEAT TRACK AT RBL9 DUPLICATED SEAT TRACK FROM BULK PN N126-2075, INSTALLED SEAT TRACK IAW SRM 51-41-02 & AMM 53-01-11.

Part: HOUSING — CHAFED (DOOR HANDLE) · airframe 17,173 hrs · 16,739 cycles

CARGO DOOR HANDLE CUT OUT IS CHAFED IN 3 PLACES. REPAIRED CHAFED DAMAGE ON CARGO DOOR HANDLE 3 PLACES CUT OUT IAW REO 601R-52-31-141.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 17,173 hrs · 16,739 cycles

LT INBD FLAP VANE HAS CHAFING DAMAGE ON L/E IN 3 PLACES. REPAIRED CHAFE DAMAGE ON LT INBD FLAP VANE L/E IAW REO 601R-57-52-004.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,173 hrs · 16,739 cycles

NR1 FLOOR SEAT TRACK ON LBL9 HAS CORROSION. REMOVED UNSERVICEABLE FLOOR SEAT TRACK AT LBL9, DUPLICATED SEAT TRACK USING BULK PN N126-2075, INSTALLED SEAT TRACK IAW SRM 51-41-02 & AMM 53-01-11.

Part: RIB — CRACKED (RT WING) · airframe 17,173 hrs · 16,739 cycles

RT BATT RIB CRACKED. REPAIRED BATT RIB ASSY, AT WS 53.60 IAW REO 601R-57-51-046, REV B, REPAIR NR 3.

Part: ANGLE — CRACKED (BS 559)

FOUND INBD CAP ANGLE AY FS559 & RBL 9 CRACKED. REPAIRED CRACKED CAP ANGLE AT FS 559 & RBL 9 BY FULL INCORPORATION OF REO 601R-53-41-260, REV E. INCLUDING DEVIATION REO 601R-53-41-609, REV B DEVIATION E TO THE FS 559 PRESSURE BULKHEAD LT & RT SIDES FROM LBL 27 TO RBL 27.

Part: SHAFT — DENTED (LT WING TE FLAP) · airframe 17,173 hrs · 16,739 cycles

LT INBD VANE ACTUATOR SHAFT DENTED FROM ROLLERS. EXCESSIVELY BLENDED ACTUATOR SHAFT FOUND TO BE WITHIN LIMITS IAW BA REO 601R-57-52-1640.

Part: FITTING — CHAFED (ROLLER GUIDE) · airframe 17,173 hrs · 16,739 cycles

LT OTBD FLAP ALIGNMENT GUIDE ROLLER FITTING HAS CHAFING DAMAGE BLENDED OUT CHAFED DAMAGE IAW B/A REO 601R-57-53-835 AND SRM 51-12-00.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 17,173 hrs · 16,739 cycles

INBD FLOORBEAM CLIP ON LBL 9 AT FS 280 IS CRACKED. R & R PN 601R31113-57 AT OTBD LBL FS 280 IAW SRM 51-42-21.

Part: PRESSURE PANEL — GOUGED (BS 210) · airframe 17,173 hrs · 16,739 cycles

RT FUSELAGE PRESSURE PANEL CUT OUT HAS TOOLING MARKS AROUND A HOLE LOCATED AT THE 3 O`CLOCK POSITION. BLENDED OUT TOOL MARKS AROUND A HOLE LOCATED AT THE 3 O`CLOCK POSITION ON RT PRESSURE PANEL (132AL) OPENING IAW REO 601R-53-11-2002.

Part: ANGLE — CRACKED (BS 625) · airframe 17,173 hrs · 16,739 cycles

RT FS 625 OBLIQUE ANGLE IS CRACKED. REMOVED UNSERVICEABLE OBLIQUE ANGLE FROM RT FS 625 AND INSTALLED SERVICEABLE ANGLE IAW SRM 51-42-21 AND REO 601R-53-61-985.

Part: SKIN — CHAFED (LT MLG DOOR) · airframe 17,173 hrs · 16,739 cycles

LT MLG LOWER L/E CHAFING DAMAGE. REPAIRED LT MLG LOWER L/E IAW REO 601R-52-82-034 NC.

Part: FITTING — CRACKED (BS 461) · airframe 17,173 hrs · 16,739 cycles

BATHTUB FITTING AT RBL9, FS 461 CRACKED PN 600-31068-19. REPLACED BATHTUB FITTING WITH SERVICEABLE FITTING IAW SRM 51-42-21, 51-42-06.

Part: ATTACH FITTING — CRACKED (BS 484) · airframe 17,173 hrs · 16,739 cycles

LT OTBD 484.00 CLIP CRACKED. FATRICATED CLIP AND INSTALLED SERVICEABLE CLIP IAW REO 601R-53-41-059, REV B.

Part: ANGLE — CRACKED (BS 625) · airframe 17,173 hrs · 16,739 cycles

LT FS 625 OBLIQUE ANGLE IS CRACKED. REMOVED UNSERVICEABLE OBLIQUE ANGLE FROM LT FS 625 AND INSTALLED SERVICEABLE ANGLE IAW SRM 51-42-21 AND REO 601R-53-61-985.

Part: SKIN — CHAFED (BS 559+26) · airframe 17,173 hrs · 16,739 cycles

SKIN ON FUSELAGE AT RT STUB FAIRING IS CHAFED. REPAIRED DAMAGE AREA IAW REO 601R-53-41-341, REV C.

Part: SKIN — CHAFED (LT WING AILERON) · airframe 17,173 hrs · 16,739 cycles

ENTIRE TOP SIDE OF LT AILERON L/E IS CHAFED. REPAIRED THE CHAFED ON ENTIRE TOP SIDE OF LT AILERON L/E IAW MFG 601R-57-60-013 REV NC.

Part: INTERCOSTAL — CRACKED (PAX DOOR) · airframe 17,173 hrs · 16,739 cycles

UPPER AFT INTERCOSTAL ON PAX DOOR IS CRACKED. REPLACED CRACKED INTERCOSTAL DOUBLER WITH NEW SERVICEABLE PN 601R318094-2, IAW SRM 51-40-11, 51-42-06.

Part: CONNECTOR — CONTAMINATED (TE FLAPS SYS) · airframe 15,395 hrs · 14,867 cycles

ON ARRIVAL THE FLAPS FAILED AT 20 DEGREES WHEN ATTEMPTED TO SELECT 30 DEGREES. INITIATED A GO-AROUND AND COMPLIED WITH THE QRH THEN MADE A 20 DEGREE FLAP LANDING. AN EMERGENCY WAS DECLARED. AS PART OF FLAP FAIL TROUBLESHOOTING: MEGOHM CKD TRANSDUCER CIRCUIT FOR THE LT AND RT BPSU WIRING HARNESSES. NO FAULTS FOUND AT THIS TIME. FOUND FLUID IN LT BPSU CONNECTOR PLUG. CLEANED AND REAPPLIED SUPER CORR B. ALSO CLEANED RT BPSU CONNECTOR PLUG AND APPLIED SUPER CORR B. CKD BOTH FLAP POSITION TRANSMITTER CONNECTOR PLUGS AND NO DEFECTS NOTED. ALSO CLEANED CONNECTOR NR 1 P5CE AT STA 559 IAW FIM 27-50-00, ITEM 20, PG 136.

Part: ECU — MALFUNCTIONED (APU) · airframe 14,012 hrs · 13,539 cycles

TROUBLESHOT APU ECU. FAULT CODES INDICATED INTERNAL ECU FAULT. REMOVED AND REPLACED ECU IAW AMM 49-61-01. OPS CHECKS GOOD. FUEL ODOR DISSIPATED AFTER APU AND PACKS WERE OPERATED. (K)

Part: GROUND WIRE — DAMAGED (NR 2 IDG) · airframe 13,555 hrs · 13,077 cycles

GENERATOR 2 AND IDG CAUTION MESSAGE ON CLIMB-OUT, COMPLIED WITH QRH. SERVICED NR IDG IAW 12-12-24, REPAIRED RT ENGINE IDG TEMP BULB GROUND WIRE (P22EZ) IAW ESPM 20. CONNECTED IDG NR 2 IAW AMM 24-11-01. OPS CHECK GOOD AT THIS TIME. IDG NR 2 TOOK 13 PUMPS. (K)

Part: CONTROLLER — MALFUNCTIONED (WINDSHIELD HEAT) · airframe 13,538 hrs · 13,057 cycles

190224/2 - LT WINDSHIELD HEAT CAUTION LIGHT ON EICAS AND WILL NOT RESET. RETURNED TO DEPARTURE. REMOVED AND REPLACED LT WINDSHIELD TEMP CONTROLLER IAW AMM 30-41 & PLACED LT WINDSHIELD ON BACKUP SENSOR IAW AMM 30-41. OPS CHECK GOOD. (K)

Part: APU — SEIZED (APU BAY) · airframe 13,497 hrs · 13,019 cycles

DETECTED STRONG ACRID ELECTRICAL BURNING SMELL FOLLOWED APU AUTO SHUTDOWN, GROUND SUPERVISOR EXCESS SMOKE FROM APU EXHAUST AFTER APU SHUTDOWN. F/A REPORTED POP PRIOR TO APU SHUTDOWN. FOUND APU SEIZED APU DOOR IS CLOSED, NO SMELL OF ANY KIND EVIDENT WITH APU. REMOVED AND REPLACED APU IAW AMM 49-10-00. OPS CHECK GOOD AT THIS TIME. (K)

Part: ENGINE — SEIZED (APU) · airframe 13,406 hrs · 12,931 cycles

190219/1 - (AT GATE) DETECTED STRONG ACRID ELECTRICAL BURNING ODOR FOLLOWED BY APU AUTO SHUTDOWN, GRND SUPERVISOR EXCESS SMOKE FROM APU EXHAUST AFTER APU SHUTDOWN. FA REPORTED POP PRIOR TO APU. FOUND APU SEIZED, APU DOOR IS CLOSED NO SMELL OF ANY KIND EVIDENT WITH APU. REMOVED AND REPLACED APU IAW AMM 49-10-00. OPS CHECK GOOD AT THIS TIME. (K)

Part: BULKHEAD — CRACKED (BS 202) · airframe 13,376 hrs · 12,901 cycles

MWC 133218-23 FWD PRESSURE BULKHEAD AT FS202.75 FOUND CRACKED AT PARKING BRAKE LOCATION. CUTOUT PERFORMED ON CRACKED PORTION OF FWD BULKHEAD, EDDY CURRENT PERFORMED ON CUTOUT IAW REO 601R-53-11-563. REPAIR PERFORMED IAW REO601R-53-11-563. (K)

Part: SUPPORT BRACKET — CRACKED (MLG WW) · airframe 13,376 hrs · 12,901 cycles

HYD SUPPORT BRACKET IN LT SIDE MLG BAY FOUND CRACKED. HYD SUPPORT BRACKET IN LT MLG BAY REPLACED IAW SRM 51-42-06. (K)

Part: ATTACH FITTING — CRACKED (BS 484) · airframe 13,376 hrs · 12,901 cycles

MWC 133218 - ATTACH FITTING CRACKED AT INTERCOSTAL F/S 484.0 RBL 27.0 UNDER FLOOR STRUCTURE. FITTING REPLACED AT INTERCOSTAL FS 484.0, RBL 27.0 IAW CRJ 200 SRM 51-42-10, 51-42-21. (K)

Part: SILL — CRACKED (BS 574) · airframe 13,376 hrs · 12,901 cycles

CRACK FOUND ON CARGO DOOR LOWER SILL, FS 574 (CRACK LENGTH .400 INCH). REPAIRED ON CARGO DOOR LOWER SILL PERFORMED IAW REO 601R-53-61-1741. (K)

Part: PANEL — CRACKED (PAX DOOR) · airframe 13,376 hrs · 12,901 cycles

PAX DOOR AFT SIDE PANEL CRACKED IN ZONE Z (CRACK LENGTH .500) REF REO 601R-52-11-702, REV A. REPAIR ON AFT SIDE PANEL OF PAX DOOR PERFORMED IAW REO 601R-52-11-702, REV A. (K)

Part: PANEL — CRACKED (PAX DOOR) · airframe 13,376 hrs · 12,901 cycles

PAX DOOR FWD SIDE PANEL CRACKED IN ZONE 2 (CRACK LENGTH .460) REF REO 601R-52-702, REV A. REPAIR ON FWD FWD SIDE OF PAX DOOR PANEL PERFORMED IAW REO 601R-52-11-702, REV A. (K)

Part: BULKHEAD — CRACKED (BS 280) · airframe 13,376 hrs · 12,901 cycles

CRACK FOUND ON PILOT BULKHEAD FS 280, RBL 9 (CRACK LENGTHIS .500). REPAIR TO PILOTS BULKHEAD FS 280, RBL 9 DONE IAW REO 601R-53-11-171, REV D. (K)

Part: FLOORBEAM — CRACKED (BS 280) · airframe 13,376 hrs · 12,901 cycles

CRACK FOUND ON CLIP FS 280, RBL 9 (CRACK LENGTH IS .500) CLIP FS 280.00 RBL 9 FABRICATED IAW SRM 52-24-16 AND INSTALLED IAW SRM 51-42-06 AND 51-42-21. (K)

Part: STRUCTURE — CRACKED (PAX DOOR) · airframe 13,376 hrs · 12,901 cycles

PASSENGER DOOR EDGE MEMBER AFT SIDE FOUND CRACKED. (CRACK LENGTH .500) REPAIR PAX DOOR EDGE MEMBER IAW REO 601R-52-11-279. (K)

Part: BULKHEAD — CRACKED (BS 280) · airframe 13,376 hrs · 12,901 cycles

CRACK FOUND ON AFT ANGLE OF PILOT BULKHEAD FS 280, LBL 9 CRACK LENGTH IS .500. REPAIR ON ANGLE OF PILOT BULKHEAD FS 28000, LBL 9 C/O IAW REO 601R-53-11-138. (K)

Part: FLOORBEAM — CRACKED (BS 280) · airframe 13,376 hrs · 12,901 cycles

CRACK FOUND ON CLIPS FS 280, LBL 9 (2 CRACKS, LENGTH IS .500) CLIP CHANGED ON FS 280.00, LBL 9 IAW SRM 51-42-06 AND 51-42-21. (K)

Part: BULKHEAD — CRACKED (BS 621) · airframe 13,376 hrs · 12,901 cycles

AFT PRESSURE BULKHEAD AT F/S 621.00 FOUND CRACKED AT LINTEL FITTING LOCATION. REPAIR TO AFT PRESSURE BULKHEAD AT FS 621.00 CARRIED OUT IAW REO 601R-53-61-1230, REV D. (K)

Part: PRIORITY VALVE — FAILED (NLG) · airframe 13,359 hrs · 12,884 cycles

AFTER T/O GEAR DISAGREE WITH NOSE GEAR SHOWING NOT STOWED C/W QRH RETURN TO DEPARTURE (APPROX 15 SECONDS AFTER SELECTING GEAR UP WARNING CAME ON.) FOUND PRIORITY VALVE FAILING TEST REF 32-30-00, REMOVED AND REPLACED NLG PRIORITY VALVE IAW AMM 32-33-15, OPS CHECK GOOD. (K)

Part: STRUT — FAILED (NLG) · airframe 13,356 hrs · 12,880 cycles

AFTER T/O GEAR DISAGREE AND NLG DOOR OPER WARNING MSG APPEARED AT ACCELLERATION ALTITUDE MSGS CLEARED AND NOSE GEAR RETRACTED NORMALLY. BOTH MAINS UP AND LOCKED. INTERROGATED PSCU FOUND CODES SHOWING NLG DIDN`T EXTEND. REPACKED NLG SHOCK STRUT REF AMM 32-21-30 LEAK CHECK GOOD. (K)

Part: BLOCKER DOOR — MISSING (THRUST REVERSER) · airframe 13,286 hrs · 12,814 cycles

LT THRUST REVERSER BLOCKER DOOR NR 8 MISSING. REMOVED AND REPLACED LT ENGINE THRUST REVERSER BLOCKER DOOR NR 8, SPRING BOX SUPPORT AND LOCK ASSY AND LT DIVERTER FAIRING ASSY IAW AMM REF 78-33-21 AND CMM 78-30-00, THRUST REVERSER CK OK IAW AMM 71-00-00-710-806. (K)

Part: CONTROL SYSTEM — MALFUNCTIONED (RUDDER) · airframe 11,080 hrs · 10,678 cycles

ON TAKEOFF ROLL, FULL RUDDER DEFLECTION UNABLE TO MAINTAIN CENTERLINE. ABORTED TAKEOFF AT APPROXIMATELY 60 KNOTS, MAX BTMS READING = 2. CROSSWING ABOUT 10 KNOTS. OPS CHECK OF NWS IAW 32-51-00. OP CHECK GOOD. PERFORMED OPS CHECK OF RUDDER CONTROL SYSTEM IAW 27-21-00. PERFORMED OPS CHECK OF SPOILER SYSTEM IAW 27-61-00, OPS CHECK GOOD. PERFORMED OPS CHECK OF AILERON SYSTEM IAW 27-11-00. AIRCRAFT OK FOR SERVICE. (M)

Part: STRUT — UNDERSERVICED (NLG) · airframe 10,961 hrs · 10,565 cycles

ON TAKEOFF RECEIVED NWS INOP AND GEAR DISAGREE, COMPLIED WITH QRH. GEAR DISAGREE ILLUMINATED APPROX 30 SECS. AFTER GEAR UP SELECTION. RETURNED FOR LANDING, LANDING WEIGHT= 41,000 LBS., MAX BTMS=2,2,2,2. SERVICE NOSE GEAR STRUT IAW 12-12-32 OPS CHECK GOOD, GEAR SWING GOOD. (K)

Part: FILTER — INOPERATIVE (RT A/C PACK) · airframe 10,385 hrs · 10,003 cycles

RT PACK HIGH PRESS CAUTION MESSAGE ON TAKEOFF ROLL, ABORTED TAKEOFF AT APPROXIMATELY 20 KNOTS, BTMS READINGS=2,2,1,2. REMOVED AND REPLACED RT ENGINE PRESSURE REGULATING SHUTOFF VALVE FILTER, REF AMM 21-51-43 AND AWAC SUPPLEMENT 06-039. (K)

Part: CONTROL UNIT — MALFUNCTIONED (STAB)

STAB CHANNEL 1 DIS-ENGAGED NUMEROUS TIMES IN FLIGHT. REMOVED AND REPLACED MCU IAW 27-42-05, OPS CHECK GOOD. (M)

Part: ELEMENT — MALFUNCTIONED (LT PYLON)

LT 14TH DUCT MESSAGE INTERMITTENT, INFLIGHT. COMPLIED WITH QRH. REMOVED AND REPLACED LEFT PYLON SENSING ELEMENT IAW AMM 36-21-04. TEST GOOD AT THIS TIME. (M)

Part: FLAP SYSTEM — UNKNOWN (TE FLAPS)

ON APPROACH INTO LGA, FLAP FAIL CAUTION ILLUMINATED FLAPS AT 30 DEGREES, COMPLIED WITH Q2RH. TOUCHDOWN AT 138 KNOTS, LANDING WEIGHT = 45,020 MAX BTMS READING = 6, 5, 6, 6. PERFORMED FLAP RESET PROCEDURE IAW AWAC SUPPLEMENT 98-018B STEPS 1.3 AND 1.4, FLAPS RESET. AIRCRAFT RELEASED FOR SERVICE. LANDING WEIGHT AND BTMS IN LIMITS, NO FURTHER ACTION REQUIRED. (M)

Part: SHUTOFF VALVE — MALFUNCTIONED (LT A/C PACK)

LT PACK OVERPRESSURE ON CLIMB-OUT OF 5000 FT, RESET PACK UPON CLIMBING LT PACK OVERTEMP MESSAGE. AIR RETURN TO ORF. LANDING WEIGHT = 41,300. MAX BTMS = 4. REMOVED AND REPLACED LT PRSOV IAW 21-51-43, OPS AND LEAK CHECK GOOD. AIRCRAFT LANDING WEIGHT WITHIN LIMITS, NO FURTHER ACTION REQUIRED. (M)

Part: SKIN — CORRODED (RT WING) · corrosion level 1 · airframe 8,508 hrs · 8,165 cycles

RT WING PLANK ACCESS HOLE NR6 HAS MINOR PITTING IN CRITICAL AND NOT CRITICAL AREAS. MAINTENANCE REPAIRED RT WING PLANK ACCESS HOLE NR6 UNDER FUEL ACCESS PANEL 640 DB IAW REO 601R-57-21-030 REV D AND AWAC E06/021-457. (K)

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 8,508 hrs · 8,165 cycles

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

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 8,508 hrs · 8,165 cycles

FLOOR SUPPORT ANGLE AT FS 621 IS CRACKED (RT). MAINTENANCE REPAIRED RT FLOOR SUPPORT ANGLE IAW REO 601R-53-61-117, REV C. (K)

Part: FLOORBEAM — CRACKED (BS 621) · airframe 8,508 hrs · 8,165 cycles

FLOOR SUPPORT ANGLE AT FS621.0 IS CRACKED (LT) MAINTENANCE REPAIRED LT FS621 FLOOR SUPPORT ANGLE IAW REO 601R-53-61-117, REV C. (K)

Part: INTERCOSTAL — CRACKED (BS 84) · airframe 8,508 hrs · 8,165 cycles

INTERCOSTAL CRACKED AT FS484.0, RBL 36.0. MAINTENANCE CUT AWAY DAMAGED FLANGE AND INSTALLED REPAIR ANGLE IAW BSC SR 601-53-0030A AND REO 601R-53-41-059, REV A. (K)

Part: INTERCOSTAL — CRACKED (BS 484) · airframe 8,508 hrs · 8,165 cycles

INTERCOSTAL CRACKED AT FS484.0, LBL 36.0. MAINTENANCE CUT AWAY DAMAGED FLANGE AND INSTALLED REPAIR ANGLE IAW BSC SR 601R-53-0030A AND REO 601R-53-41-059, REV A. (K)

Part: INTERCOSTAL — CRACKED (FS 621-625 S14R) · airframe 8,508 hrs · 8,165 cycles

RT SIDE FS 621.00 TO FS 625.30 INTERCOSTAL AT STR 14R IS CRACKED NEAR RADIUS APPROX 1.2 INCH LONG. MAINTENANCE REPLACED INTERCOSTAL PN 601-35012-52 IAW SRM 51-42-06. (K)

Part: INTERCOSTAL — CRACKED (FS 621-625 S14L) · airframe 8,508 hrs · 8,165 cycles

LT SIDE FS 621.00 TO FS 625.30 INTERCOSTAL AT STR 14L IS CRACKED NEAR RADIUS APPROX 1.2 INCH LONG. MAINTENANCE REMOVED AND REPLACED LT INTERCOSTAL PN 601-35012-51 IAW SRM 51-42-06. (K)

Part: FLAP SYSTEM — UNKNOWN (TE FLAPS)

FLAPS FAILED AT 30 DEGREES, FOLLOWED QRH, COMPLIED WITH LANDING REQUIREMENT FOR LANDING FLAPS 30. RESET FLAPS C-B PER AMM SUPP 98-018A, PLACED ON 72 HOURS FLAP WATCH. (M)

Part: COALESCER BAG — CONTAMINATED (RIGHT)

SMOKE TOILET MESSAGE INFLIGHT. COMPLIED WITH QRH. FLIGHT ATTENDANT REPORTS HAZE IN CABIN. SMOKE NO LONGER PRESENT. RESET C/B, TESTED TOILET SMOKE DETECTORS, SYSTEM CHECK GOOD. TROUBLESHOT AND FOUND PACK NR 2 ACM DEFECTIVE. NR 2 ACM OIL CHECKED NORMAL. REPLACED RIGHT WATER SEPARATOR SOC GROUND RAN ECS PACK NR 2 AND ACM CHECKS NORMAL. NO SMOKE VISIBLE. (M)

Part: WARNING LIGHT — ILLUMINATED (AILERON TRIM)

ABORTED TAKEOFF AT 49,400 LBS AT 95 KNOTS FOR CONFIG WARNING, BRAKING ACTION MEDIUM. NO BRAKE WARNINGS RECEIVED. COMPLIED WITH RTO INSPECTION IAW 05-51-27. NO DEFECTS NOTED. AILERON TRIM WAS RESET TO ZERO. SHOWED RIGHT WING UP DURING TAKEOFF. (M)