N407AW

Part: HANDLE — LACK OF LUBE (SERVICE DOOR) · airframe 35,558 hrs · 33,221 cycles

SERVICE DOOR UNABLE TO BE OPENED FROM OUTSIDE. LUBED OUTER HANDLE & HANDLE RELEASE PIN AS REQUIRED. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: STRIP — MISSING (CABIN) · airframe 35,542 hrs · 33,205 cycles

EMERGENCY FLOOR TRACK LIGHTING MISSING AMBER STRIP AT SEAT 1DF & MISSING END CAP.

Part: DIMMER — DEFECTIVE (CABIN) · airframe 35,082 hrs · 32,768 cycles

FLIGHT 3825, ODOR OF ELEC BURNING IN CABIN AREA MID TO FWD. R & R BOTH POWER UNIT DIMMERS AT ROW 2D - F IAW AMM 33-21-04. OPS CHECKED GOOD. INSPECTED WIRING FOR POWER UNIT DIMMERS, NO FAULT FOUND, NO ELEC BURNING ODOR NOTED.

Part: DIMMER — FAULTY (CABIN) · airframe 35,057 hrs · 32,742 cycles

FLIGHT 3961STRONG ELECT BURNING SMELL AT ROW 3 IN CABIN. PER CREW, LIGHTING IS SUFFICIENT FOR DAY TIME FLIGHTS. ON CALL IDENTIFIED BALLAST ROW 3. PLACARDED & PLACED ON MEL. R & R 3 AC CEILING & SIDE WALL LIGHT POWER DIMMER UNITS IAW AMM 33-21-10 & 33-21-09. OPERATIONS CHECKED GOOD, REMOVED PLACARD.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 34,148 hrs · 31,844 cycles

FLAP FAIL AT 30 DEGREES IN FLIGHT. PERFORMED FLAP RESET PROCEDURE IAW AWAC, FLAPS RESET. PLACARD & PLACED ON MEL. TROUBLE SHOT IAW FIM 27-50-00 & AWAC SUP 98-018F, NO SDU LIGHTS. RECORDED FECU FAULT LOG & EVENT CIRCUMSTANCES LOG. FECU PASSED GND MX TEST. NOTED NO FLAP TWIST. FLAP CONTROL LEVEL FAULTS & CODES 19CI & 19C2 INDICATED A FALSE LEVER FAULT. FECU NR 7 TEST & FLAPS OPERATIONS NORMAL.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,206 hrs · 30,961 cycles

FORWARD AFT FACE OF FRAME 333 IS CORRODED.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,206 hrs · 30,961 cycles

FORWARD & AFT FACE FRAME 295 IS CORRODED.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,206 hrs · 30,961 cycles

CARGO BAY FLOORBEAM LBL 27 AT FS 589 TO FS 621 IS CORRODED AROUND SCREW HOLES.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 33,206 hrs · 30,961 cycles

WIND SHIELD CTR POST ON RT LOWER ATTACH FITTING CRACKED.

Part: SKIN — DENTED (TE FLAP) · airframe 33,206 hrs · 30,961 cycles

RIGHT INBD FLAP LOWER OTBD EXTERIOR SKIN DENTED.

Part: FITTING — CRACKED (FUSELAGE) · airframe 33,206 hrs · 30,961 cycles

FLOOR SUPPORT BEAM HAS CRACKED CLIP AT FS 280, RBL 9 INBD CLIP.

Part: FITTING — CRACKED (FUSELAGE) · airframe 33,206 hrs · 30,961 cycles

LEFT FS 484 CLIP CRACKED.

Part: SKIN PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,206 hrs · 30,961 cycles

EXTERIOR LOWER SKIN PANEL HAS CORROSION ON LOWER SURFACE AT FS 599+116 STRINGER 26L.

Part: ATTACH BRACKET — CRACKED (LT WING) · airframe 33,206 hrs · 30,961 cycles

LEFT WING LE ATTACH BRACKETS ARE CRACKED AT WS 139 & WS 149.

Part: FITTING — CRACKED (FUSELAGE) · airframe 33,206 hrs · 30,961 cycles

CLIP CRACKED FS 280 FLOORBEAM RBL10.

Part: MOUNT BRACKET — CRACKED (HYDRAULIC BAY) · airframe 33,206 hrs · 30,961 cycles

NUMBER 3 HYD BRAKE ACCUMULATOR FWD MOUNTING BRACKET CRACKED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,206 hrs · 30,961 cycles

LEFT NR 2 SEAT TRACK HAS FOUR EACH AREAS OF CORROSION FS 394 - 409+128.

Part: BRACKET — CRACKED (LT MLG DOOR) · airframe 33,206 hrs · 30,961 cycles

LEFT MLG DOOR ROLLER BRACKET CRACKED.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,206 hrs · 30,961 cycles

FUSELAGE SKIN UNDER LOWER T CAS ANTENNA IS CORRODED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,206 hrs · 30,961 cycles

LEFT NR 3 FLOOR SEAT TRACK GOUGED & CORRODED.

Part: MOUNT BRACKET — CRACKED (FUSELAGE) · airframe 33,206 hrs · 30,961 cycles

CARGO DOOR LOWER FWD TRACK MOUNT BRACKET CRACKED.

Part: HANDLE — CRACKED (PAX DOOR) · airframe 33,206 hrs · 30,961 cycles

PASSENGER DOOR INNER HANDLE CRACKED.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 33,206 hrs · 30,961 cycles

INBOARD & OUTBOARD TIE CLIPS AT STRINGER 3L & FS 280 ARE CRACKED.

Part: BEAM — CRACKED (FUSELAGE) · airframe 33,206 hrs · 30,961 cycles

FS 409+128 VERTICAL BEAM AT RBL 18 IS CRACKED ON LOWER END.

Part: DRAG ANGLE — CRACKED (RT WING) · airframe 33,206 hrs · 30,961 cycles

RIGHT DRAG ANGLE COMMON TO BATTERY RIB CRACKED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,206 hrs · 30,961 cycles

RIGHT SEAT TRACK CORRODED BETWEEN FS 364 - FS 394.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,206 hrs · 30,961 cycles

RIGHT FLOOR SEAT TRACK CORRODED FROM FS 424 - FS 559.

Part: SKIN — CRACKED (FUSELAGE) · airframe 33,206 hrs · 30,961 cycles

FUSELAGE SKIN CRACKED AT AFT RT CORNER OF NLG WW.

Part: FLOOR PANEL — CRACKED (E&E BAY) · airframe 33,206 hrs · 30,961 cycles

FORWARD EQUIPMENT COMPARTMENT FLOOR SKIN CRACKED ON LT SIDE AT FS 193.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,206 hrs · 30,961 cycles

RIGHT SEAT TRACK CORRODED BETWEEN FS 394 - FS 409+128.

Part: BULKHEAD — CHAFED (FUSELAGE) · airframe 33,206 hrs · 30,961 cycles

AFT SIDE OF FS 280 BULKHEAD CHAFED AT RBL 9 AT WL 86.L.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,206 hrs · 30,961 cycles

FLOOR SUPPORT FITTING AT FS 319 BELOW SERVICE DOOR IS CORRODED.

Part: CROSSBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,206 hrs · 30,961 cycles

FLOOR SUPPORT CROSSBEAM AT FRAME FS 349 CORRODED.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 33,206 hrs · 30,961 cycles

FLOORBEAM WEB CRACKED AT LBL 10 OTBD & FS 280 FROM LOWER OTBD PULLEY BRACKET ATTACHMENT BOLT HOLE.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 33,206 hrs · 30,961 cycles

CARGO BAY TIE DOWN TRACK CORRODED, RBL 9 FROM FS 559+80 TO 559+112.

Part: SKIN — DENTED (FUSELAGE) · airframe 33,206 hrs · 30,961 cycles

COMPLIED WITH CARD 4DMI17806 REPAIR DENTS FS 179 STRINGER 26 & 24.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,206 hrs · 30,961 cycles

LEFT FLOOR SEAT TRACK CORRODED FS 364 - 394.

Part: FITTING — CRACKED (FUSELAGE) · airframe 33,206 hrs · 30,961 cycles

CARGO DOOR SUPPORT BEAM LOWER CLIP AT FS 621 BULKHEAD CRACKED.

Part: SEAL — CRACKED (LT SPOILER) · airframe 33,206 hrs · 30,961 cycles

LEFT SPOILERON CTR SPRING SEAL CRACKED.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 33,206 hrs · 30,961 cycles

AFT TIE CLIP STRINGER 3L TO FS 280 CRACKED.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,206 hrs · 30,961 cycles

FRAME CORRODED AT FS 349 BETWEEN STRINGERS 25L & 25R.

Part: ACTUATOR — FAULTY (YAW DAMPER) · airframe 31,734 hrs · 29,550 cycles

DURING CLIMB ACFT YAWED UNCOMMANDED. COMPLIED WITH QRH, DISCONNECTED YAW DAMPERS & YAWING PERSISTED. FD NR 2 WAS ENGAGED. ACFT RETURNED TO PHL, EMERGENCY DECLARED. LANDED AT 46,900 LBS, NORMAL LANDING. IAW WO 212612 WC 5 FOR TROUBLESHOOTING & WORK PERFORMED. R & R YAW DAMPER LINEAR ACTUATOR, OPERATIONS CHECKED GOOD.

Part: RIB — GOUGED (NACELLE) · airframe 28,315 hrs · 26,221 cycles

LOWER CORE COWL 445AB HAS 1 EA GOUGE ON 2 INNER RIBS AND NUMEROUS SMALL GOUGES AND DENTS ON INNER SKIN. C/W REO 601R-71-12-4129 BY HAND BLENDING MINOR CHAFING CUTTING OUT DAMAGE AND FILLING WITH STRUCTURAL ADHESIVE. FABRICATED 3 EA DOUBLERS FOR OUT OF LIMITS.

Part: SILL — CORRODED (PAX DOORWAY) · airframe 28,315 hrs · 26,221 cycles

PAX DOOR SILL HAS CORROSION. FOUND CORROSION TO BE 100 PERCENT MATERIAL LOSS. REMOVED, FABRICATED, AND INSTALLED NEW SERVICEABLE SILL IAW SRM 51-42-06, 51-42-13, 51-42-21 AND 51-24-16.

Part: ROLLER — CHAFED (LT WING TE FLAP) · airframe 28,315 hrs · 26,221 cycles

LEFT OTBD FLAP ROLLER FITTING CHAFED. PERFORMED REPAIR OF LT OTBD FLAP INBD ROLLER FITTING IAW REO 601R-57-53-943.

Part: LEVER — CHAFED (PAX DOOR) · airframe 28,315 hrs · 26,221 cycles

PAX DOOR FWD PULL IN LEVER IS CHAFING THE PAX DOOR STRUCTURE. REPAIRED STRUCTURE IAW REO 601R-52-2058.

Part: DOOR — CHAFED (RT MLG) · airframe 28,315 hrs · 26,221 cycles

RIGHT MLG DOOR CHAFED ON LOWER L/E. REPLACED FILLER ON LOWER L/E ON RIGHT MLG DOOR IAW REO 601R-52-82-034.

Part: FAIRING — CHAFED (RT WING TE FLAP) · airframe 28,315 hrs · 26,221 cycles

RT FLAP STUB FAIRING HAS CHAFING AND A DENT AFT END ASSEMBLED REPLACEMENT SERVICEABLE RT STUB FAIRING IAW SRM 51-40-11 AND 51-42-06.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 28,315 hrs · 26,221 cycles

THREE CARGO TRACKS ON LBL AND RBL 9 HAS CORROSION IN CARGO AREA. REMOVED AND INSTALLED SERVICEABLE CARGO TRACKS IAW AMM 53-01-11.

Part: POST — GOUGED (AFT BULKHEAD) · airframe 28,315 hrs · 26,221 cycles

AFT PRESSURE BULKHEAD CENTER POST IS GOUGED AT TOP. REPAIRED AFT PRESSURE BULKHEAD CENTER POST FS 621 TO DEPTH. .055 AND FOUND TO BE WITHIN ALLOWABLE LIMITS IAW REO 601R-53-61-4636.

Part: SEAT TRACK — GOUGED (BS 409) · airframe 28,315 hrs · 26,221 cycles

RT SIDE SEAT TRACK NR 3 GOUGED BEYOND LIMITS. R & R SEAT TRACK SECTION.

Part: ATTACH BRACKET — CRACKED (PAX DOOR) · airframe 28,315 hrs · 26,221 cycles

PAX DOOR LATCH CAM TORQUE TUBE CLOSE OUT PANEL AFT ATTACHMENT BRACKET FWD .5 IS CRACKED. REMOVED CRACKED FWD BRACKET .5 LOCATED AND DRILLED NEW BRACKET, INSTALLED NUTPLATES ON BRACKET, INSTALLED NEW SERVICEABLE BRACKET ASSY IAW SRM 51-42-02, 51-40-11, 51-42-06 AND 51-45-00.

Part: STRUCTURE — CORRODED (PAX DOOR) · airframe 28,315 hrs · 26,221 cycles

TOP OF PAX DOOR STAIR STRUCTURE HAS CORROSION. REMOVED OLD PAX DOOR EDGE MEMBER DUE THE CRACKS FOUND WHILE CLEANING CORROSION FABRICATED NEW EDGE MEMBER IAW SRMS 51-24-19, 51-42-06, 51-42-13.

Part: DOOR — LACK OF LUBE (MAIN PAX) · airframe 28,241 hrs · 26,149 cycles

MAIN CABIN DOOR WILL NOT OPEN FROM OUTSIDE. INSPECTED AND FOUND LOCKING PINS TO BE DRY. LUBED, ROLLERS AND LOCKING PINS IAW REF AMM 52-11-00. OPS CHECKS WITH CREW 5 TIMES. OPS CHECK GOOD.

Part: WIRE HARNESS — DAMAGED (NR 2 ENGINE) · airframe 27,847 hrs · 25,735 cycles

DURING RON INSPECTION OF STARTER OIL, DISCOVERED THAT SEVERAL WIRE HARNESS COVERS WERE MELTED AND THERE WERE CARBON DEPOSITS ON THE ENG. SUSPECT POSSIBLE ENG FIRE. FOUND B-NUT ON THE FUEL FILTER OUTLET LOOSE AND LEAKING FUEL. ALL DAMAGE FOUND TO BE LIMITED IN NATURE AND DELT WITH INDIVIDUALLY ON WCS WITHIN THE WO IAW AMM 72-00-00-200-801, SPECIAL INSPECTION. REMOVED AND REPLACED NR 2 ENGINE REF CORE COWL HARNESS REF AMM TASK 71-50-00-000-804 AND 71-50-00-400-804.

Part: SELECTOR VALVE — MALFUNCTIONED (NLG) · airframe 27,263 hrs · 25,174 cycles

AFTER SELECTING GEAR HANDLE UP, BOTH MLG RETRACTED, NLG DID NOT. RECEIVED GEAR DISAGREE AND NOSE DOOR OPEN WARNING MESSAGE. QRH- LANDED WITHOUT INCIDENT. REF WO 183218 FOR R & R OF NLG SELECTOR VALVE AND NLG PRIORITY VALVE REF AMM 32-3. OPS AND LEAK CK GOOD.

Part: ACTUATOR — FAILED (RT MLG) · airframe 26,915 hrs · 24,796 cycles

AFTER TAKE OFF DURING GEAR RETRACTION, RECEIVED GEAR DISAGREE GEAR UP CAUTION MESSAGE FOR APPROX 10 SECONDS WITH RT MLG RED HASH MARKS, THEN CLEARED. R & R RT MLG SIDE STAY ACTUATOR IAW AMM 32-32-01 & SUPP 11-015. OPS AND LEAK CHECKED GOOD.

Part: OIL SYSTEM — LEAKING (RT ENGINE) · airframe 25,768 hrs · 23,590 cycles

AT ALTITUDE, RECEIVED RT ENGINE OIL WARNING MESSAGE. (FL30.0 APPROX 80 PERCENT N1) RETARDED THROTTLE TO 76 PERCENT N1 WARNING EXTINGUISHED, PRESSURE READ 33 PSI. AFTER 5 MIN WARNING RETURNED. AT THROTTLE IDLE PRESSURE INDICATED 30 PSI. INDICATION FLUXUATED 5 PERCENT AT ALLN1 SPEEDS. ALL OTHER ENGINE INDICATIONS NORMAL. INSPECTED AND FOUND SIGNIFICANT AMOUNT OF OIL LEAKING FROM ENG. FOURN RT ENG SCAVENGE PUMP OIL FILTER HSG O-RING MISSING, INSTALLED O-RING M83248-1-136. SERVICED 7 QTS OF OIL. VERIFIED OIL REPLENISHMENT, SYS OPS NORMAL.

Part: WARNING LIGHT — ILLUMINATED · airframe 24,262 hrs · 22,022 cycles

DC EMERGENCY BUSS CAUTION MESSAGE ENROUTE. FOUND CBP1-R7 POSER SENSE TO BE POPPED. RESET BREAKER MESSAGES CLEARED. C/W OPS CHECK OF LT AND RT FIRE EXT IAW AMM 26-11-00, APU EXT IAW AMM 26-12-11, AND RT FUEL SOV IAW AMM 28-21-36, BATT DIRECT FEED IAW AMM 24-32-01, APU BATT DIRECT SERVICE IAW AMM 24-32-02. OPS CHECK GOOD.

Part: FLAP TRACK — WORN (LT WING) · airframe 23,771 hrs · 21,516 cycles

LT OTBD FLAP OTBD VANE TRUCK IS NEARLY FLUSH WITH VANE SKIN. REQUIRES BUTTE DOOR RIGGING AFTER REPAIR. R & R LT OTBD FLAP VANE OTBD TRACK PN 601R14502-1, IAW REO 601R-57-53-016.

Part: SKIN — CHAFED (RT MLG DOOR) · airframe 23,771 hrs · 21,516 cycles

RT MLG DOOR HAS CHAFE DAMAGE AT FWD AND AFT LOWER INBD EDGES COMPLIED WITH REO 601R-52-82-033, REV A, REO 601R-52-82-034, REV NC, REO 601R-52-82-290 REV NC TO REPAIR CHAFE DAMAGE.

Part: DOOR FRAME — CRACKED (PAX DOOR) · airframe 23,771 hrs · 21,516 cycles

AFT FRAME ON PAX DOOR AT DATUM NR1 IS CRACKED. REPAIRED IAW REO 601R-52-11-402.

Part: SKIN — DAMAGED (BS 644) · airframe 23,771 hrs · 21,516 cycles

DENT ON TOP OF FUSELAGE AT STA 644. REPAIRED DENT WITH LAP PATCH. REPAIR IAW REO 601R-53-61-3805.

Part: INTERCOSTAL — CRACKED (PAX DOOR) · airframe 23,771 hrs · 21,516 cycles

INTERCOSTAL IN UPR REAR CORNER ON PAX DOOR IS CRACKED. R & R IAW SRM 51-42-06.

Part: ATTACH FITTING — CORRODED (BS 340) · corrosion level 2 · airframe 23,771 hrs · 21,516 cycles

FWD AND AFT DOOR HANDRAIL CLEATS UNDER FLOOR PANEL 213 CLF HAVE CORROSION. R & R AFT UNSERVICEABLE CLEAT AND IAW SRM 51-42-06 & REPAIRED FWD SERVICEABLE CLEAT IAW SRM 53-00-00.

Part: BRACKET — CRACKED (BS 672) · airframe 23,771 hrs · 21,516 cycles

NR 2 HYD RETURN MANIFOLD BRACKET IN AFT EQUIPMENT BAY CRACKED. REPAIRED NR2 HYD RETURN MANIFOLD BRACKET IAW REO 601R-53-62-031.

Part: SEAT TRACK — CORRODED (BS 349-439) · corrosion level 2 · airframe 23,771 hrs · 21,516 cycles

LT NR1 AND NR2 FROM FWD CABIN FLOOR SEAT TRACKS HAVE CORROSION. REMOVED UNSERVICEABLE SEAT TRACK LT NR1 AND LT NR2 AND REPALCED BY SERVICEABLE SEAT TRACK PN NK6-2075 IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (BS 559) · corrosion level 1 · airframe 23,771 hrs · 21,516 cycles

SEAT TRACK RAIL STA 559+80, RBL 9, PN 601R387779-13 CORROSION ON ATTACH HOLES FOR SEAT RAIL AND ON FLANGES. R & R WITH NEW SECTION OF SEAT TRACK.

Part: ATTACH ANGLE — CRACKED (BS 280) · airframe 23,771 hrs · 21,516 cycles

51847-1000-0026 F/S 280, 9.0 OTBD FLOORBEAM ATTACH ANGLE IS CRACKED, FABRICATED, LOCATED AND INSTALLED NEW SERVICEABLE CLIP ANGLE.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 23,771 hrs · 21,516 cycles

FS 280 FLOOR SUPPORT ON OTBD SIDE OF LBL 9 IS CRACKED. REMOVED DAMAGED AREA FABRICATED AND INSTALLED NEW SERVICEABLE ANGLE SUPPORT.

Part: ATTACH FITTING — CRACKED (BS 280) · airframe 23,771 hrs · 21,516 cycles

51847-1000-0025-FS 280, RBL 9, INBD FLOORBEAM ATTACK CLIP IS CRACKED. REMOVED DAMAGED CLIP FABRICATED AND INSTALLED NEW SERVICEABLE CLIP.

Part: ATTACH FITTING — CRACKED (BS 280) · airframe 23,771 hrs · 21,516 cycles

51847-1000-0022-280 F/S, LBLB 9.0, INBD FLOOR BEAM ATTACH CLIP IS CRACKED. REMOVED DAMAGED CLIP, FABRICATED NEW SERVICE CLIP AND INSTALLED.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 23,771 hrs · 21,516 cycles

FS 280 FLOOR SUPPORT ANGLE HAS CORROSION UNDER FLIGHT DECK CTR FLOOR PANEL. REMOVED CORRODED SUPPORT ANGLE FABRICATED AND INSTALLED NEW SERVICEABLE SUPPORT ANGLE AT FS 280.

Part: ATTACH FITTING — CRACKED (BS 484) · airframe 23,771 hrs · 21,516 cycles

RT FS 484 CLIP AND INTERCOSTAL CLIP ON OTBD SIDE OF RBL 27 CRACKED C/W REO 601R-53-41-059.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 23,771 hrs · 21,516 cycles

NR 4 AND NR 5 SEAT TRACK FLOOR CORRODED. REMOVED UNSERVICEABLE SEAT TRACKS LT NR 4, LT NR 5 ON FLOOR CABIN AND REPLACED SERVICEABLE SEAT TRACKS. PN 126-2075 IAW AMM.

Part: DOOR — CHAFED (BS 544) · airframe 23,771 hrs · 21,516 cycles

LT MLG DOOR HAS CHAFE DAMAGE ON LWR INBD L/E. R & R DAMAGED FILLER IAW REO 601R-52-82-034.

Part: RIB — CRACKED (RT WING) · airframe 23,771 hrs · 21,516 cycles

RT BATT RIB IS CRACKED. REPAIR IAW REO 601R-57-51-046, REV B, REPAIR NR 3.

Part: BULKHEAD — CRACKED (BS 202) · airframe 23,771 hrs · 21,516 cycles

SKIN AT FS 202.0, WHERE PARKING CABLE PASSES THROUGH TO FWD HYD COMPARTMENT IS CRACKED. REPAIRED FS 202 BULKHEAD SKIN IAW REO 601R-53-11-1969 REV A DATED 2010-09-06.

Part: RIB — CRACKED (LT WING) · airframe 23,771 hrs · 21,516 cycles

LT BATT RIB CRACKED AT WS 53.60. REPAIRED LT BATT RIB IAW REO 601R-57-51-046, REV B.

Part: BULKHEAD — CRACKED (BS 559) · airframe 22,102 hrs · 19,788 cycles

FOUND FS BULKHEAD WEB TO HAVE 2 INDICATIONS NOTED. RT SIDE (1) OTBD OF RBL 9, WL 58.70, APPROX .2" L 50 PERCENT FSH, (2) RT SIDE INBD OF RBL 18 WL59.10 APPROX .3"L 50 PERCENT FSH, FS 559 LT CAP ANGLE INDICATION .3" L 80 PERCENT FSH. ALL FAILED NDT. PERFORMED A MAJOR REPAIR TO FS 559 BULKHEAD WEB AND CAP ANGLES BY COMPLYING WITH REO`S 601R-53-41-260 AND 601R-53-41-609. (K)

Part: MOTOR — MALFUNCTIONED (DOOR ASSIST) · airframe 21,025 hrs · 18,731 cycles

PASSENGER DOOR WILL NOT OPEN 1 FOOT. REMOVED AND REPLACED PAX DOOR ASSIST MOTOR AND FUSELAGE DOOR JAM MOTOR ASSIST ATTACH POINT EYE BOLT IAW AMM 52-11-08. OPS CHECKS GOOD. (K)

Part: ACTUATOR — MALFUNCTIONED (MLG) · airframe 20,156 hrs · 17,902 cycles

REQUEST INSP OF LANDING GEAR DUE TO YEAR DISAGREE MESSAGE INFLIGHT. REMOVED AND REPLACED RT SIDESTAY ACTUATOR. (K)

Part: LANDING GEAR — MALFUNCTIONED (LT MLG) · airframe 19,806 hrs · 17,582 cycles

LT MLG DID NOT EXTEND ON LANDING.

Part: WARNING LIGHT — FALSE ACTIVATION (CABIN PRESSURE) · airframe 19,027 hrs · 16,823 cycles

RECEIVED CABIN ALTITUDE MASTER WARNING MESSAGE IN FLIGHT AIRCRAFT ALTITUDE 12,000FT CABIN ALTITUDE 10,200FT, PRESSURIZATION WORKED IN NORMAL MODE. REF LOG 186158/1-COMPLIED WITH OPS CHECK OF CABIN PRESSURIZATION IN MANUAL MODE IAW AMM 21-31-00, OPS CHECK AND LEAK CHECK GOOD ON THE GROUND. (A)

Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE) · airframe 19,028 hrs · 16,822 cycles

ACFT WOULD NOT PRESSURIZE AFTER TAKEOFF, SWITCHED CONTROLLERS, TRIED MANUAL NO ABNORMAL INDICATION. DURING TROUBLESHOOTING OF ACFT PRESSURIZATION SYS FOUND CABIN PRESSURE TUBE ASSY B NOT CROSS THREADED. R&R CABIN PRESS TUBE ASSY IAW MM 21-31-00 REF W/C 9 FOR LEAK CHECK.

Part: CONTROLLER — INTERMITTENT (CABIN PRESSURE) · airframe 18,439 hrs · 16,253 cycles

CABIN ALT CAUTION MESSAGE, RAN QRH AUTO 1&2 CONTROLLER INTERMITTENT AND MANUAL INOPERATIVE. REMOVED DEBRIS FROM EJECTOR JET PUMP. INSPECTED BOTH OUTFLOW VALVES. PER RELIABILITY AS PRECAUTIONARY REPLACED NR 1 CPC PER AMM 21-31-16. OPS CHECK GOOD. REMOVED PLACARD AND MEL.

Part: WINDSHIELD — FAILED (COCKPIT) · airframe 18,391 hrs · 16,203 cycles

CAPTAIN WINDSHIELD SHATTERED IN FLIGHT AT FL 260. R & R CAPT WINDSHIELD IAW AMM 56-11-01. OPS CHECK GOOD. NO LEAKS.

Part: REGULATOR — MALFUNCTIONED (CABIN PRESSURE) · airframe 18,348 hrs · 16,162 cycles

AIRCRAFT DID NOT PRESSURIZE AFTER TAKEOFF, CABIN RATE OF CLIMB MATCHED AIRCRAFT RATE OF CLIMB. NO EICAS MESSAGE RECEIVED. PLACED BOTH AUTOPRESSURE CONTROLLERS ON MEL. REMOVED AND REPLACED AUTOPRESSURE REGULATOR IAW AMM21-31-07. (K)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,029 hrs · 15,853 cycles

FLOOR LEVEL EMERGENCY LIGHTING ADJACENT TO ROW 1, ORANGE SEGMENT FWD INOPERATIVE. (K)

Part: WARNING SYSTEM — MALFUNCTIONED (THRUST REVERSER) · airframe 17,658 hrs · 15,495 cycles

LT REVERSER UNLOCKED MESSAGE IN FLIGHT. REACTIVATED LT THRUST REVERSER PERFORMED FUNCTIONAL TEST IAW 78-30-00. CHECKS NORMAL THIS TIME PLACARD AND MEL REMOVED. (K)

Part: DRAIN — CONTAMINATED (AIRSPEED)

ABORTED TAKEOFF BELOW 80 KNOTS DUE TO FAILED STANDBY AIRSPEED INDICATOR 0 KNOTS. ALL BRAKE TEMPERATURES INDICATE NORMAL. FOUND WATER IN P3 DRAIN. PERFORMED P3 CONTAMINATION REMOVAL PER AMM 34-11-00. PERFORMED LEAK TEST OF P3 PER AMM 34-11-00-790-803 TEST OK. (M)

Part: CONTROL PANEL — MALFUNCTIONED (STAB TRIM)

STAB TRIM/MACH TRIM CAUTION MESSAGE IN FLIGHT. STAB TRIM STUCK AT 4.4 DEGREES. FLAPS AT 20 WHEN FAILURE OCCURRED, BOTH CHANNELS. REMOVED AND REPLACED STAB/MACH TRIM PANEL ASSEMBLY IAW AMM 27-40-00. (M)

Part: A/C PACK — UNKNOWN (RIGHT)

RIGHT PACK HIGH TEMP CAUTION MESSAGE ON THE GROUND. COMPLIED WITH QRH, HAD SLIGHT ODOR OF SMOKE APPARENT AND SLIGHT HAZE. (M) [07-31-07] INSPECTED RT PACK, NO DAMAGE NOTED, OIL SERVICE OK. OBSERVED CREW OPERATE LT PACK, NO SIGNS OF SMOKE OR HAZE. (K)

Part: ACTUATOR — OUT OF RIG (NLG DOOR)

UNUSUAL REPETITIVE NOISE AFTER GEAR RETRACTION. NOISE PERSISTED UNTIL GEAR EXTENSION, REPETITIVE PUMPING. TROUBLESHOOTING REVEALED R-NOSE DOOR ACTUATOR OUT OF RIG. (M)

Part: COALESCER BAG — DIRTY (LT & RT)

SMOKE TOILET CAUTION MESSAGE DURING CLIMB-OUT. COMPLIED WITH QRH, AIR RETURN TO PHL. NO OVERWEIGHT LANDING 41,000 LBS, NO VISUAL SMOKE IN LAV OR CABIN. INSPECTED LAV, FOUND SMOKE DETECTOR OK. PERFORMED OPS CHECK IAW AMM 26-16-01-710-801. NO DEFECTS NOTED. REMOVED AND REPLACED LEFT AND RIGHT COALESCER BAGS IAW AMM 21-51-13. OPS CHECK GOOD. NO SMOKE NOTED. (M)

Part: REGULATOR VALVE — MALFUNCTIONED (RT ENGINE)

SMOKE TOILET CAUTION MESSAGE ON TAKEOFF CLIMB, COMPLIED WITH QRH, AIR RETURNED TO PHL NO OVERWEIGHT LANDING WTW 41,000 LBS. NO VISUAL SMOKE IN LAV OR CABIN. (M) REMOVED AND REPLACED PRESS REGULATING VALVE ASSY ON RT ENG IAW AMM 25-31-05. PERFORMED COMP WASH AND POWER RUNS NO SMELLS NOTED AND NO SMOKE NOTED THROUGH ALL POWER RANGES, OK FOR SERVICE. (K)

Part: BEAM — CRACKED (FUSELAGE)

FOUND LEFT FS 409 PLUS 128 INBOARD VERTICAL BEAM LBL 27 HAS A .25 INCH CRACK AT BOTTOM RADIUS. MAINTENANCE REPAIRED BULKHEAD AT FS 409 PLUS 128 POST AT BL 27, LT IAW REO 601R-53-41-056 REV D. (M)

Part: PANEL — CORRODED (RT WING)

FOUND RIGHT WING PLANK ACCESS HOLE BETWEEN BL 0.00 AND WS 12.245 FUEL PANEL 610AB HAS MINOR CORROSION AT INBOARD RADIUS. MAINTENANCE BLENDED MINOR CORROSION, PERFORMED EDDY CURRENT, ROTOPEENED, SANDED AND APPLIED FINISH IAW REO 601R-57-21-030. (M)

Part: FITTING — CRACKED (FUSELAGE)

FOUND RIGHT FS 280 RBL 9.0 INBOARD AND OUTBOARD FLOOR SUPPORT CLIPS CRACKED. MAINTENANCE REMOVED AND REPLACED FLOOR SUPPORT CLIPS AT FS 280 RBL 9 INBOARD AND OUTBOARD POSITIONS IAW CRJ SRM 51-40-11, 51-42-21 AND BSC SB 601R-53-0057A. (M)

Part: FITTING — CRACKED (FUSELAGE)

FOUND LEFT FS 280 LBL 9 INBOARD AND OUTBOARD FLOOR SUPPORT CLIPS CRACKED. MAINTENANCE REPLACED AND REPLACED FLOOR SUPPORT CLIPS AT FS 280 LBL INBOARD AND OUTBOARD POSITIONS IAW SRM 51-40-11, 51-42--21 AND BSC SB 601R-53-0057A. (M)

Part: INTERCOSTAL — CRACKED (FUSELAGE)

FOUND LEFT SIDE FS 621 TO FS 625 INTERCOSTAL AT STRINGER 14L IS CRACKED NEAR RADIUS APPROX .6 INCH LONG. MAINTENANCE REMOVED AND INSTALLED NEW INTERCOSTAL/CLIP IAW CRJ 200 SRM 51-42-06. (M)

Part: WARNING LIGHT — ILLUMINATED (STALL WARNING)

RECEIVED EFIS COMP MON ABOVE 80 KNOTS IAS MESSAGE V1, AFTER TAKEOFF RECEIVED STALL FAIL CAUTION 800 FT EXTREMELY LOUD NOISE COCKPIT. RETURNED FOR LANDING. FOUND OXYGEN SERVICE DOOR OPEN. SECURED DOOR, NO DAMAGE FOUND. INSPECTED RVSM CRITICAL AREA NO DEFECTS FOUND. INTERROGATED MDC, NO FAULTS FOUND. SPC COMPLIED WITH FUNCTIONAL CHECK OF STALL PROTECTION SYSTEM. TEST OK IAW CRJ200 AMM. (M)

Part: WINDOW — CRACKED (COCKPIT) · airframe 12,487 hrs · 10,533 cycles

FO SIDE WINDOW CRACKED DURING DESCENT AT 24,000 FT DIFFERENTIAL PRESSURE NOTED AT 7.2 PRESSURE NORMAL CONTINUED DESCENT IAW QRH FOR UNPRESSURIZED FLIGHT AS PRECAUTION. REMOVED AND REPLACED FO SIDE WINDOW. PRESURIZED CABIN. LEAK CHECK GOOD. WINDOW HEAT OPS CHECK GOOD. (K)

Part: SKIN — GOUGED (FUSELAGE)

FOUND SKIN GOUGED AT PANEL B2AL ATTACH SCREW AT 1 O'CLOCK POSITION. BLENDED AREA, PERFORMED EDDY CURRENT AND TREATED BARE MATERIAL. (M)

Part: CLIP — CRACKED (FUSELAGE)

THE LEFT AND RIGHT INTERCOSTAL ATTACH ANGLES/CLIPS ARE CRACKED .25 INCH AT LBL 27 AND RBL 27, FS 484, WL 73. (M) REMOVED CRACKED ANGLES AT FS 484, RBL 27 AND LBL 27. INSTALLED NEW ANGLES, IAW SRM AND BRAS STD REP. (K)

Part: ANGLE — CRACKED (FUSELAGE) · airframe 10,891 hrs · 9,231 cycles

RT FS 625 OBLIQUE ANGLE CRACKED IN RADIUS .3750 INCH LONG. REMOVED CRACKED ANGLE, INSTALLED NEW ANGLE IAW SRM. (K)

Part: LINK — DISCONNECTED (NLG STEERING)

NOSE GEAR OPEN GEAR DISAGREE, WOW YELLOW MESSAGE AFTER TAKEOFF AND GEAR RETRACTION, NOSE GEAR INDICATED DOWN. INSPECTED NOSE GEAR FOUND STEERING LINK DISCONNECTED, RECONNECTED STEERING LINKAGE, NO FURTHER DEFECTS NOTED. AIRCRAFT OK FOR SERVICE. (M)

Part: BRACKET — CRACKED (FUSELAGE) · airframe 7,446 hrs · 6,182 cycles

FS 625 AT STR 14R, FUSELAGE TO HORIZONTAL INTERCOSTAL CONNECTING CLEAT HAS A CRACK AT THE FORWARD RADIUS. REPLACED CLEAT WITH PN S6144-4 IAW EO 601R-53-4181. NEW BRACKET (CLEAT) INSTALLED REF CRJ SRM 51-42-06 AND 51-42-21.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE)

THE LEFT AND RIGHT CARGO FLOOR SUPPORT STRUCTURE IS CRACKED AT AFT PRESSURE BULKHEAD FS 621, WL 73.5 AND LBL 40 AND RBL 40. REPAIR IAW REO 601R-53-611-117 REV A. (M)

Part: ANGLE — CRACKED (FUSELAGE)

FOUND FS 625 RIGHT UPPER OBLIQUE ANGLE, STRINGER 14 IS CRACKED APPROXIMATELY 2 INCHES. REMOVED AND REPLACED OBLIQUE ANGLE IAW CRJ 200 SRM 51-42-06. (M)

Part: ANGLE — CRACKED (FUSELAGE)

FOUND FS 625 RIGHT UPPER OBLIQUE ANGLE, P/N 601-35012-52, AT STRINGER 14 IS CRACKED APPROX 2 INCHES. (M)

Part: ANGLE — CRACKED (FUSELAGE)

FOUND STRINGER 14 OBLIQUE ANGLE P/N 601-35012-51 IS CRACKED APPROXIMATELY 2 INCHES. REMOVED AND REPLACED OBLIQUE ANGLE IAW CRJ 200 SRM 51-42-06. (M)

Part: ANGLE — CRACKED (FUSELAGE)

FOUND LEFT FS 625 STRINGER 14 OBLIQUE ANGLE, P/N 601-35012-51, IS CRACKED APPROX 2 INCHES. (M)

Part: SWITCH — DIRTY (PAX DOOR)

PASSENGER DOOR OUTER HANDLE WARNING CAME ON DURING CLIMB THROUGH 17K FEET. CLEANED SWITCH, CYCLED DOOR, OPS CHECK GOOD.

Part: FLAP — MALFUNCTIONED (WING) · airframe 3,109 hrs · 2,748 cycles

FLAPS FAIL CAS ON APPROACH, LANDED AT FLAPS ZERO. MAINTENANCE C/W AWAC SUPPLEMENT 98-18 IN AMM CHAPTER 27, NO CODED FAILS IN LAST 72 HOURS, SYSTEM RESET.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 2,965 hrs · 2,636 cycles

FLAP FAIL CAS MESSAGE ON APPROACH. MAINTENANCE C/W AWAC SUPPLEMENT 98-18 OPS GOOD ECU CODES, JAM, RBPSU, PDU DIFF.