N801AY

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 27,911 hrs · 25,771 cycles

RIGHT SIDE FLOOR SEAT TRACK , "STICK - 2 " GOUGED AND CORRODED. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-01-11.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 27,911 hrs · 25,771 cycles

RT OVERWING SUPPORT BRACKET IS CRACKED ON BOTH SIDES OF BRACKET NEAR FS409+128. SEE STREAMER. REMOVED CRACKED BRACKET IAW SRM 51-72-86. FABRICATED NEW BRACKET IAW SRM 51-24-36. APPLIED FINISH IAW SRM 51-25.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 27,720 hrs · 25,450 cycles

RT SIDEWALL SEAT TRACK STICK 6 HAS CORROSION SPOTS, IN THE CABIN. REMOVED AND REPLACED RT SIDEWALL SEAT TRACK STICK 6 IAW AMM 53-01-11.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 27,532 hrs · 25,375 cycles

F/A EMER FLASHLIGHT OUT OF SERVICE. REPLACED FWD F.A. FLASH LIGHT BATTERY AS REQUIRED. OPS TEST GOOD. REF: AMM 25-61-00.

Part: APU — SEIZED · airframe 27,294 hrs · 25,113 cycles

APU AUTO SHUTDOWN WITH NO INDICATIONS OTHER THAN A BAD ODOR. R & R THE APU IAW 200-49-10-00. PERFORMED A LEAK CHECK AND OPS CHECK, BOTH CHECKS WERE GOOD. ACFT OK FOR SERVICE.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 27,169 hrs · 24,971 cycles

FOUND A CRACK IN THE REAR PRESSURE BULKHEAD WEB FACE AT THE MACHINED FITTING IB 0.25" L. COMPLETED REPAIR TO REAR PRESSURE BULKHEAD NEAR LINTLE AREA FITTING AT FS 621 IAW REO 601R-53-61-1230 REV F. NDT COMPLIED WITH.

Part: PBE — UNSERVICEABLE (CABIN) · airframe 26,996 hrs · 24,786 cycles

DURING INSPECTION NOTED WARDROBE PBE PACKAGE HAS LOST VACUUM SEAL. REMOVED & REPLACED WARDROBE PBE IAW AMM CH 35-30-00. P/N OFF/ON: MR-10042N. NO S/N OFF/ON.

Part: PBE — DAMAGED (COCKPIT) · airframe 26,073 hrs · 23,725 cycles

COCKPIT PBE HAS LOST VACUUM ON PACKAGE. REMOVED AND REPLACED COCKPIT PBE IAW AMM 35-30-00.

Part: ELEMENT — INOPERATIVE (RT FIRE LOOP) · airframe 28,686 hrs · 23,307 cycles

RT 14TH STAGE BLEED WARNING AT FL 280 PERFORMED QRHM MESSAGE DID NOT GO OUT, CLOSED 4 14TH STAGE BLEED, OPENED ISOLATION VALVE REDUCED RT THRUST TO IDLE. LANDED FLAPS 20. R & R PYLON SENSING ELEMENT ON RT SIDE LOOP A58WK IAW AMM 36-21-04. OPS CHECKED GOOD.

Part: ACTUATOR — INOPERATIVE (TE FLAP) · airframe 25,217 hrs · 22,821 cycles

FLAP FAIL OCCURRED IN FLIGHT APPROX 40 MIN INTO FLIGHT WHILE SELECTING FLAPS FROM 30 TO 45 FLAPS STOPPED AT 36 AIRSPEED 160KTS OAT 12C FOLLOWED QRH SELECTED FLAPS TO 30 LEFT AND RT FLAPS REMAINED AT 36. UNDER DIRECTION OF MOC PERFORMED FLAP FAIL RESET IAW FIM RESET PROCEDURES FLAP FAIL MESSAGE EXTINGUISHED DEFERRED FLAP SYSTEM IAW MEL 27-50-00. PERFORMED 5 CONSECUTIVE FLAP CYCLES - FLAP SYSTEM CHECK OK AT THIS TIME AND ALL INDICATIONS NORMAL ENT MM2 PLACARD INSTALLED MOC NOTIFIED 4488. PERFORMED TROUBLESHOOTING PER FIM REV 25 IAW AD 2009-06-12 PARAGRAPH (H)(6)(I) AMOC LOG 16-81 DATED 12/14/2016 AND TS 001100R4 FIM TECHNICAL SUPPLEMENT. ALL 8 FLAP ACTUATORS REPLACED DUE TO JAM CODES. REF 409 601821 FOR DETAILS.

Part: BULB — INOPERATIVE (EXIT SIGN) · airframe 25,004 hrs · 22,589 cycles

PAX CALL SIGN LIGHT FRONT SIDE MID CABIN EXIT SIGN OUT. R & R THE BULB IAW AMM 33-51-14. OPS CHECKED GOOD. OK FOR SERVICE

Part: FLAP SYSTEM — INOPERATIVE · airframe 24,878 hrs · 22,457 cycles

FLAPS FAIL CAUTION MESSAGE AT 3500FT MSL, 200KT, GEAR DOWN PERFORMED TROUBLESHOOTING IAW FIM REV. 52. REPLACED THE RT OTBD FLAP ACTUATOR , RT BPSU, AND RT NR 5 FLEX DRIVE SHAFT DUE TO UNUSUAL NOISE IAW AMM 27-53-10, 27-51-10, ,AND 2753-05.

Part: STRUT — DEFECTIVE (NLG) · airframe 24,269 hrs · 21,837 cycles

ON T/O AT "GEAR UP" NOSE DOOR OPEN WARNING, RAN QRH. PUT GEAR DOWN, ALL GREEN. DEFERRED LANDING GEAR RETRACTION SYS. NOTIFIED PINS SAFTIED AND INSTALLED MMO2 UPDATED FLAGS REMOVED. R&R NLG DRESSED ASSY IAW JOB CARD 200-32-21-02. OPS + FUNCTIONAL CHEC K GOOD AT THIS TIME. R&R BOTH LEFT AND RIGHT NLG WHEEL AND TIRE ASSY IAW AMM 32-42-01 IB/OB WHEEL SPACERS VERIFIED INSTALLED OK FOR SVC AND PER JOB CARD 200-32-4 2-01

Part: OXYGEN BOTTLE — DAMAGED (PORTABLE) · airframe 24,153 hrs · 21,713 cycles

PORTABLE OXYGEN BOTTLE KNOB BROKEN OFF. REPLACED THE OXYGEN BOTTLE IAW AMM 35-30-00

Part: BULKHEAD — GOUGED (FUSELAGE) · airframe 23,899 hrs · 21,454 cycles

GOUGE ON AFT PRESSURE BULKHEAD FS 621, LBL 17.5 30" ABOVE FLOOR WENT OUT OF LIMITS AND REQUIRES REPAIR. REPAIRED APB LBL 17.5 30" ABOVE FLOOR IAW REO 601R-53-61-1285, REV D. PERFORMED OPS TEST, OPS TEST GOOD IAW AMM 74-30-400-801, STEP 4D.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 23,899 hrs · 21,454 cycles

LT FLOOR SILL FROM FS 621-559+112 IS CORRODED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS FROM STA 596-598. ALL OTHER AREAS IN LIMITS IAW REO 601R-53-00-526, REPAIRED FLOORSILL STA 596-598 IAW EA CRJ253-04611, REV IR.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 23,899 hrs · 21,454 cycles

FLOORBEAM AT LBL 27 AND FS 610 AND 559+112 HAS CORROSION ON BOTH INBD AND OTBD LANDINGS. R & R FLOORBEAM, CAP, LBL27, FROM FS 559+112-FS 610 IAW SRM 51-42-21, & SRM 51-42-24.

Part: BULKHEAD — GOUGED (FUSELAGE) · airframe 23,899 hrs · 21,454 cycles

GOUGE ON AFT PRESSURE BULKHEAD FS 621, LBL 27, 30" ABOVE FLOOR, OUT OF LIMITS AND REQUIRES REPAIR. REPAIRED FS 621 AFT PRESSURE BULKHEAD AT LBL27, 30" ABOVE FLOOR IAW REO 601R-53-61-1285, REV D.

Part: DOOR — OBSTRUCTED (EMERGENCY EXIT) · airframe 23,899 hrs · 21,454 cycles

RIGHT OVERWING EMERGENCY DOOR WILL NOT OPEN AT ALL. NEEDS EVALUATION. UPON FURTHER EVALUATION FOUND PROBLEM TO BE EXCESSIVE PAINT BUILD UP, OPENED DOOR AND PERFORMED OPS TEST, OPS TEST GOOD IAW AMM 52-21-00-710-801.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 23,899 hrs · 21,454 cycles

621 REAR PRESSURE BULKHEAD FORWARD SIDE IS CRACKED AT TOP OF CARGO DOOR TRACK. REPAIRED 621 REAR PRESSURE BULKHEAD FORWARD SIDE AT TOP OF CARGO DOOR TRACK IAW REO 601R-53-61-1541, REV F.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 23,899 hrs · 21,454 cycles

IN MAIN CABIN SIDEWALL SEAT RAILS ON LEFT SIDE NR 5-7 ARE CORRODED AND GOUGED IN MULTIPLE AREAS. R & R LT SIDE SEAT RAILS NR 5 TO NR 7 IAW AMM 53-01-11, PAR 2A AND PAR 3A.

Part: FRAME — CRACKED (FUSELAGE) · airframe 23,899 hrs · 21,454 cycles

FS 333, FRAME IS CRACKED ADJACENT TO STR 1L. REPAIRED CRACK IN FS 333 AT STR 1L IAW REO 601R-53-21-2740.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 23,899 hrs · 21,454 cycles

LEFT FLOOR SEAT TRACK NR 1 HAS MULTIPLE AREAS OF CORROSION AND GOUGES. R & R SEAT TRACK NR 1 IAW AMM 53-01-11-000-802 & 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 23,899 hrs · 21,454 cycles

LEFT FLOOR SEAT TRACK NR 2 HAS MULTIPLE AREAS OF CORROSION AND GOUGES. R & R LT FLOOR SEAT TRACK NR 2 IAW AMM 53-01-11.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 23,899 hrs · 21,454 cycles

PASSENGER DOOR AFT DRAG ANGLE CRACKED AT PULLEY BRACKET. R & R EXISTING PASSENGER DOOR AFT DRAG ANGLE REPAIR IAW REO 601R-52-11-513.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 23,899 hrs · 21,454 cycles

LEFT FLOOR SEAT TRACK STICK, NR 5 HAS CORROSION. R & R LT FLOOR SEAT TRACK NR 5 IAW AMM 53-01-11.

Part: BRACKET — CRACKED (PAX DOOR) · airframe 23,899 hrs · 21,454 cycles

PASSENGER DOOR POWER ASSIST MOTOR LOWER MOUNT BRACKET CRACKED. R & R PASSENGER DOOR POWER ASSIST MOTOR LOWER MOUNT BRACKET IAW SRM 51-42-06.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 23,899 hrs · 21,454 cycles

IN MAIN CABIN SIDEWALL SEAT RAILS ON LT SIDE OF NR 1-4 ARE CORRODED AND GOUGED IN MULTIPLE AREAS. R & R SEAT RAILS LT SIDE SEAT TRACK'S 1, 2, 3, 4, STA 349.00, FS 461.00 IAW AMM 53-01-11.

Part: FITTING — CRACKED (FUSELAGE) · airframe 23,899 hrs · 21,454 cycles

COPILOTS SIDE POST LOWER OTBD CLIP IS CRACKED. R & R CO-PILOTS SIDE POST LOWER OTBD CLIP IAW SRM 51-42-21.

Part: FITTING — CRACKED (FUSELAGE) · airframe 23,899 hrs · 21,454 cycles

PILOT`S SIDE POST OTBD LOWER CLIP IS CRACKED. R & R PILOTS SIDE POST LOWER OTBD CLIP IAW SRM 51-42-21.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 23,899 hrs · 21,454 cycles

IN MAIN CABIN SIDEWALL SEAT RAILS ON RT SIDE NR 5-7 ARE CORRODED AND GOUGED IN MULTIPLE AREAS. R & R RT SIDEWALL SEAT TRACKS NR 5-7 IAW AMM 53-01-11 AND REO 601R-53-00-485.

Part: FITTING — CRACKED (FUSELAGE) · airframe 23,899 hrs · 21,454 cycles

FS 484.88, CLIP RBL 27 IS CRACKED. R & R -9 CLIP AT STA 484.88, RBL27 IAW SRM 51-42-21 AND REO 601R-53-41-059.

Part: FITTING — CRACKED (FUSELAGE) · airframe 23,899 hrs · 21,454 cycles

FS 484.88, CLIP RBL 36 IS CRACKED. R & R -2 CLIP AT STA 484.88, RBL36 IAW SRM 51-42-21 AND REO 601R-53-41-059.

Part: DOUBLER — GOUGED (FUSELAGE) · airframe 23,899 hrs · 21,454 cycles

APB AT RBL 27 HAS GOUGE ON PREVIOUS REPAIR. R & R WEB DOUBLER IAW REO NR 601R-53-61-1285.

Part: DOUBLER — GOUGED (FUSELAGE) · airframe 23,899 hrs · 21,454 cycles

APB AT RBL 36 HAS GOUGE ON PREVIOUS REPAIR. R & R WEB DOUBLER IAW REO NR: 601R-53-61-1285.

Part: VANE — INOPERATIVE (AOA) · airframe 23,836 hrs · 21,383 cycles

AIR RETURN TO DEPARTURE DUE TO STALL FAIL INDICATION. EMERGENCY WAS DECLARED BY CREW. FLIGHT HAS LANDED AND TAXIING TO AMA PAINT HANGAR. REPLACED AOA VANE.

Part: PROXIMITY SENSOR — FAULTY (NLG) · airframe 23,246 hrs · 20,785 cycles

GEAR DISAGREE DURING GEAR RETRACTION AFTER TAKEOFF. DEFER LG SYS IAW MEL 32-30-01 GEAR PINS ARE INSTALLED. R & R CENTERING PROXIMITY SENSOR BRACKET IAW CMM 32-20-04. GEARS SWING OPERATIONS CHECKED GOOD IAW AMM 32-30-00. R & R THE NLG WOW NR 2 & CENTERING HARNESS IAW AMM 32-61-25. OPERATIONS CHECKED GOOD. SERVICED NLG STRUT IAW JC 12-710-002. PERFORMED GEAR EXT & RET SYS IAW AMM 32-30-00-720-801, NO DEFECTS NOTED. OPERATIONS CHECK GOOD THIS CLEARS MEL 3263296-1, MM02 UPDATED, PLACARD REMOVED, MOC 51364 NOTIFIED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,140 hrs · 20,679 cycles

EMERGENCY EXIT FLOODLIGHT ABOVE SEAT 2C INOPERATIVE. DEFERRED FWD CEILING EMER FLOODLIGHT IAW MEL 33-51-11 CONTROL NR 326325-2, PLACARD INSTALLED. OK FOR SERVICE. R & R EMER OVERHEAD LIGHT BULB AT ROW 2 WITH NEW UNIT IAW AMM 33-51-16-960-801.

Part: SENSING ELEMENT — DEFECTIVE (NR 1 PYLON) · airframe 22,991 hrs · 20,528 cycles

14TH STAGE BLEED ISSUE. FLIGHT IS RETURNING WITH AFFECTED NR 1 ENG AT IDLE POWER. EMER WAS DECLARED IN FLIGHT. LANDING & TAXI TO THE GATE WAS NORMAL. LT 14TH DUCT WARNING MSG WHILE IN FLIGHT. QRH PROCEDURE COMPLIED WITH. REPLACED PYLON SENSE ELEMENT A59WK IAW AMM 36-21-04. COMPLETED OPERATIONS TEST IAW AMM 36-21-10. ALL CHECKED GOOD.

Part: UNKNOWN — ODOR (COCKPIT & CABIN) · airframe 22,367 hrs · 19,891 cycles

APU DID NOT START IN FLIGHT ON DESCENT DOOR OPENS & STARTER ENGAGED BUT NO LIGHT OFF. WE SHUTDOWN APU, WAITED & ATTEMPTED AGAIN, THIS TIME APU APPEARED TO START NORMALLY. AFTER ABOUT 20 SECONDS A VERY STRONG ODOR OF JET A WAS NOTICED IN THE COCKPIT & CABIN. PERFORMED OPERATIONS CHECK OF APU IAW AMM 49-10-00. OPERATIONS GOOD, OK FOR SVC.

Part: WIRE HARNESS — DEFECTIVE (NLG) · airframe 22,283 hrs · 19,815 cycles

UPON GEAR RETRACTION MASTER WARNING CAME ON WITH MSG NOSE DOOR OPEN GEAR DISAGREE WITH GEAR HANDLE UP NOSE GEAR INDICATING DN GREEN. LT & RT MLG INDICATING WHITE & UP ACCOMPLISHED EP 12-2 & EP 12-8 GEAR INDICATIONS NORMAL WITH HANDLE DOWN. COMPLIED WITH TROUBLESHOOTING 001565. R & R NLG HARNESS. REPLACED PROC SENSOR BRACKET & ADJUSTED NOSE GEAR TOW BAR COLLAR REFERENCE NON-ROUTINE CONTINUATION CARDS FOR DETAILS.

Part: GLOWSTRIP — LOOSE (CABIN) · airframe 21,358 hrs · 18,821 cycles

EMERGENCY LIGHTING STRIP ON FLOOR SEPARATING FROM FLOOR. SECURED EMER PHOTO LUMINESCENT FLOOR STRIP LIGHTING ROW 1AB - 2AB IAW AMM 33-51-01.

Part: STIFFENER — CHAFED (FUSELAGE) · airframe 21,137 hrs · 18,600 cycles

FOUND CHAFE DAMAGE TO THE FS 621.00 BULKHEAD VERTICAL STIFFENER AT BL 0. THE CHAFE MEASURES .800 X .063 DEEP ON THE CORNER OF THE OUTER FLANGE & .014 DEEP ON THE WEB. REPAIRED IAW EA CRJ253-02896.

Part: FIRST AID KIT — UNSERVICEABLE (CABIN) · airframe 20,185 hrs · 17,667 cycles

FIRST AID KIT NOT SEALED. INVENTORY SHOWS MISSING ITEMS. R & R FIRST AID KID IAW AMM 25-61-06.

Part: OIL SYSTEM — LEAKING (APU) · airframe 19,749 hrs · 17,241 cycles

OIL DISCHARGE FROM PACK EXHAUST. ODOR IN COCKPIT DURING CLIMB. OIL COMING FROM APU OIL COOLER AIR INLET.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 19,574 hrs · 17,072 cycles

GALLEY EMERGENCY EXIT LIGHT INOPERATIVE. R & R BATTERY PACK IAW 33-51-04. OPS CHECKED GOOD.

Part: LIGHT — BROKEN (CABIN) · airframe 19,177 hrs · 16,683 cycles

LIGHT BASE FOR EMERGENCY EXIT SIGN BROKEN NEXT TO SERVICE DOOR. R & R LIGHT BASE NEXT TO SERVICE DOOR IAW CMM 33-21-34. OPS CHECKED GOOD.

Part: FITTING — CRACKED (FUSELAGE) · airframe 18,957 hrs · 16,454 cycles

BATHTUB FITTING AT FS461, RBL 9 CRACKED 0.50" LONG. R & R IAW SRM 51-42-21, 51-40-11, 51-25-16, 51-21-11.

Part: SKIN — DAMAGED (WING) · corrosion level 2 · airframe 18,957 hrs · 16,454 cycles

FUEL PANEL 5650EB ACCESS HOLE AT WS 253.022 HAS NICKS ON FWD INNER SIDE 0.010" DEEP IN NON-CRITICAL REGION. REPAIRED IAW REO 601R-57-21-030.

Part: SKIN — DAMAGED (WING) · corrosion level 2 · airframe 18,957 hrs · 16,454 cycles

FUEL PANEL 550CB ACCESS HOLE AT WS 209.040 HAS NICKS ON FWD INNER SIDE 0.010" DEEP IN NON-CRITICAL REGION. REPAIRED IAW REO 601R-57-21-030.

Part: SKIN — DAMAGED (WING) · corrosion level 2 · airframe 18,957 hrs · 16,454 cycles

FUEL PANEL 510AB ACCESS HOLE LANDING CORRODED AT WS12.245 IN NON-CRITICAL REGION. REPAIRED IAW REO 601R-57-21-030.

Part: FITTING — CRACKED (FUSELAGE) · airframe 18,957 hrs · 16,454 cycles

BATHTUB FITTING AT FS461, LBL9 CRACKED 0.75" LONG. R & R IAW SRM 51-42-11.

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 18,957 hrs · 16,454 cycles

FORWARD FACE OF FS621 BULKHEAD HAS MULTIPLE SCREW SHANK NICKS ON SKIN AND RIVET HEADS 0.007" DEEP. REPAIRED IAW REO 601R-53-61-2155.

Part: BEAM — CRACKED (FUSELAGE) · airframe 18,957 hrs · 16,454 cycles

FS409+128 LOWER VERTICAL BEAM RBL27 CRACKED AT RIVET HEAD. REPAIRED IAW REO 601R-53-41-056.

Part: SELECTOR VALVE — FAULTY (NLG) · airframe 18,874 hrs · 16,371 cycles

GEAR DISAGREE WARNING MESSAGE ON LANDING 2500 AGL 180 KTS, RAN QRH, CYCLED GEAR TWICE HAD TO PULL MANUAL EXTENSION. NOSE GEAR CAME DOWN AND SHOWED DOWN AND LOCKED ON TOUCHDOWN RATE OF DESCENT WAS 100 FPM. REMOVED AND REPLACED NOSE LANDING GEAR SELECTOR VALVE IAW CRJ 200 AMM 32-33-10. OPERATIONS CHECKS GOOD.

Part: LIFE VEST — UNSERVICEABLE (CABIN) · airframe 18,404 hrs · 15,933 cycles

(2) INFANT LIFE VESTS BAGS TORN. REMOVED & REPLACED 2 INFANT LIFE VEST IAW PA 25-096A.

Part: THERMOCOUPLE — DEFECTIVE (RT ENGINE) · airframe 18,404 hrs · 15,933 cycles

ON FLIGHT 4005 (MEM TO IND) JUST AFTER TAKEOFF DURING CLIMBOUT, RT ENGINE ITT SPIKED INTO THE RED, INDICATING 998 DEGREES. AIRCRAFT PERFORMED AN AIR RETURN BACK TO MEM AND ITT CONTINUED TO FLUCTUATE FROM NEAR NORMAL TO 998 DEGREES, AT ALL POWER SETTINGS, UNTIL ENGINE WAS SHUT DOWN AFTER LANDING. RIGHT ENGINE MISCOMP CAUTION MESSAGE. REMOVED AND REPLACED THE THERMOCOUPLE ASSEMBLY IAW AMM 71-11-05. OPS CHECK GOOD.

Part: HINGE — WORN (FUSELAGE) · airframe 184,147 hrs · 15,687 cycles

IN HEAVY CHECK FOUND PASSENGER DOOR HINGE WORN (FUSELAGE SIDE). REMOVED AND REPLACED PAX DOOR HINGE HALF ON FUSELAGE SIDE IAW CRJ 200 SRM 53-21-23.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 18,134 hrs · 15,675 cycles

CRACK FOUND IN FS 559 SEMI-PRESSURE BULKHEAD CAP ANGLES AT RBL 18 AND LBL 18. REPAIRED IAW BOMBARDIER REO 601R-53-41-260, 601R-53-41-609, 601R-53-41-1645.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 18,134 hrs · 15,675 cycles

FS 280 LOWER WEB FLOOR ANGLE IS CRACKED OUTBOARD OF RBL 9, WL 70. REPAIRED IAW BOMBARDIER REO 601R-53-11-171.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 18,134 hrs · 15,675 cycles

FS 280 FLOOR LANDING ANGLE IS CRACKED AT LBL 9, WL 73.5. REPAIRED IAW BOMBARDIER REO 601R-53-11-136.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 18,134 hrs · 15,675 cycles

FS 280 FLOOR LANDING ANGLE IS CRACKED AT RBL 9, WL 73.5. REPAIRED IAW BOMBARDIER REO 601R-53-11-136.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 18,134 hrs · 15,675 cycles

FS 280 LOWER WEB FLOOR ANGLE IS CRACKED OUTBOARD OF LBL 9, NEXT TO ALTERNATE EXT PULLEY MOUNT BRACKET AT WL 70. REPAIRED IAW BOMBARDIER REO 601R-53-11-171.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 18,134 hrs · 15,675 cycles

CAP ANGLES OF SEMI PRESSURE BULKHEAD AT FS 559 FOUND CRACKED AT LBL 18 AND RBL 18. REPAIRED IAW BOMBARDIER REOS 601R-53-41-260, 601R-53-41-609, AND 601R-5341-1645 AND PA 53-025B.

Part: BATTERY PACK — DISCHARGED (FLASHLIGHT) · airframe 18,011 hrs · 15,556 cycles

FLIGHT ATTENDANT FLASHLIGHT INOPERABLE. REPLACED FLIGHT ATTENDANT FLASHLIGHT BATTERY PACK IAW CMM 25-60-02. CHECKS NORMAL AND CLEARS DM#74437 PLACARD REMOVED.

Part: COALESCER BAG — DIRTY (AC BAY) · airframe 17,971 hrs · 15,510 cycles

CREW PERFORMED ATB TO DTW (ON FLIGHT 4125 SCHEDULED TO FLY DTW TO CVG) DUE TO LAV SMOKE TOILET AT 1500' AGL BUT NO VISIBLE SMOKE. THE CREW RAN THE QRH AND DECLARED AN EMERGENCY. LANDING WEIGHT WAS 47,300 AND THE AIRCRAFT LANDED WITH NO ISSUES. COMPLIED WITH WORKSCOPE FOR SMOKE IN THE CABIN. FOUND THE COALESCER SOILED. REMOVED AND REPLACED COALESCER SOCKS IAW AMM 21-51-13. CHECKS GOOD ON APU. COMPLIED WITH WORKSCOPE FOR SMOKE IN THE CABIN. NO FURTHER DEFECTS NOTED. PERFORMED HIGH POWER ENGINE RUN WITH ECS SELECTED TO ENGINE BLEEDS & APU BLEEDS. NO SMOKE NOTED OR INDICATED. OK FOR SERVICE.

Part: FILTER — DAMAGED (ENGINE OIL) · airframe 17,750 hrs · 15,279 cycles

IN FLIGHT AT ABOUT 4000 GOT A MASTER WARNING FOR ENGINE OIL PRESSURE ON THE NR 2 RIGHT ENGINE. PERFORMED THE QRH ENGINE INDICATION AT IDLE THE MASTER WARNING WENT OUT AND OIL PRESSURE WAS IN THE GREEN AT 29 PSI. IF THE POWER WAS INCREASED YOU WOULD GET THE MAS INSPECTED MAG CHIP DETECTOR IAW AMM 79-21-09. INSPECTED AND REPLACED OIL FILTER IAW AMM 79-21-05. FOUND O-RING MISSING FROM EDP PLUG. INSTALLED PLUG AND O-RING IAW AMM/MEL 29-11-00. PERFORMED ENG RUN. NO OIL LEAK NOTED. SERVICED RT ENG WITH 208 OZ IAW AMM 12-13-79. OK FOR SERVICE.

Part: GEARBOX — FAILED (THROTTLE LEVER) · airframe 16,946 hrs · 14,474 cycles

LEFT THRUST REVERSER INOPERATIVE. REPLACED THROTTLE GEAR BOX .

Part: ACCUMULATOR — DAMAGED (BRAKE SYSTEM) · airframe 16,510 hrs · 14,053 cycles

AIR RETURN FOR LOUD VIBRATING RUMBLING NOISE AROUND AND BELOW F/O`S FEET CLIMBOUT AT 10,500FT TO 11,000FT LASTED FOR 20 SECS. ACCOMPLISHED VIBRATION WORKSCOPE AND FOUND NR 2 BRAKE ACCUMULATOR AND GAUGE BLOWN OUT WITH HYDRAULIC FLUID IN TRU AND BRAKE VALVE COMPARTMENT. REMOVED AND REPLACED NR 2 SYSTEM BRAKE ACCUMULATOR AND GAUGE. OP`S AND LEAK CK`S GOOD. REF AMM 32-43-16,32-43-17. NO OTHER DEFECTS NOTED.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 14,088 hrs · 11,745 cycles

FS 202.75 PRESSURE BULKHEAD IS CRACKED AT BRAKE CABLE PASS-THRU HOLE. REPAIRED 202.75 PRESSURE BULKHEAD IAW REO 601R-53-11-563 AND BSC STANDARD REPAIR 601R-53-0101A.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 14,088 hrs · 11,745 cycles

LIGHTNING STRIKE DAMAGE AT FS 449.00, STRINGER 2R. PERFORMED A MAJOR REPAIR TO FUSELAGE SKIN AT FS 449.00 STR 2R BY FABRICATING A FILLER, DOUBLER AND TRIPLER, AND INSTALLED THE REPAIR PARTS IAW BOMBARDIER SERVICES CORPORATION ENGINEERING ORDER NO: 601R-53-20037.

Part: PRESSURE PANEL — DAMAGED (FUSELAGE) · airframe 14,088 hrs · 11,745 cycles

FOUND DOUBLE DRILLED HOLE IN PRESSURE FLOOR AT FS 523.00 AT RBL 27.00. PERFORMED A MAJOR REPAIR TO DAMAGED HOLE ON PRESSURE FLOOR AT FS 523.00 RBL 27.00 IAW BOMBARDIER SERVICES CORPORATION ENGINEERING ORDER NO: 601R-53-20026.

Part: SKIN — DENTED (FUSELAGE) · airframe 14,088 hrs · 11,745 cycles

CREASED DENT AT LOWER CARGO DOOR OPENING WAS FOUND MEASURING 5.6" X 1.75" W X 0.081 DEEP BETWEEN FRAMES 589 -605 STR 18-19L. PERFORMED A MAJOR REPAIR TO DAMAGED FUSELAGE SKIN BETWEEN FS 589-605 STR 17-19L IAW BOMBARDIER SERVICES CORPORATION ENGINEERING ORDER NO: 601R-53-20038.

Part: BULKHEAD — CHAFED (FUSELAGE) · airframe 14,088 hrs · 11,745 cycles

FS 621.00 PRESSURE BULKHEAD IS CHAFED 0.018 INCH DEEP AT RBL 36.20 AND WL 105.00. PERFORMED A MAJOR REPAIR AT FS 621.00 ON PRESSURE BULKHEAD AT RBL 36.20 AND WL 105.00 BY MANUFACTURING DOUBLERS, FILLER, AND INSTALLING REPAIR PARTS IAW REO 601R-53-61-1285 REV B.

Part: SKIN — DENTED (RT WING SPOILER) · airframe 14,035 hrs · 11,703 cycles

A SINGLE INDENTATION WAS FOUND ON THE RT WING OTBD GROUND SPOILER UPPER SURFACE. THE DAMAGE IS RECORDED AS 0.049 INCH DIAMETER AND A MAXIMUM DEPTH OF 0.006 INCH AND IS LOCATED 3.7 INCHES AFT OF THE L/E AND 7.68 INCHES FROM THE OTBD EDGE. TEMPORARY REPAIR IAW STS EA 5-2010-291. AT THE NEXT C CHECK MX INTERVAL, NOT TO EXCEED 5,000 FLIGHT HOURS, REPAIR THE GROUND SPOILER UPPER SKIN INDENTATION IAW SRM 51-72-00; METAL HONEYCOMB REPAIRS.

Part: STEP — PUNCTURED (PAX DOOR) · airframe 13,620 hrs · 11,307 cycles

PUNCTURE IN THE PASSENGER STEP SURFACE WAS FOUND ON THE SECOND STEP FROM THE TOP (WITH DOOR IN OPEN POSITION). THE PENETRATION MEASURES APPROX 0.50 INCH DIAMETER AND IS LOCATED AT THE INBD EDGE OF THE STEP 4.75 INCHES FWD OF THE AFT EDGE. A VISUAL CHECK FROM THE STAIR ASSY INTERIOR FOUND NO DAMAGE TO ADJACENT STRUCTURE. TEMPORARY REPAIR IAW STS ENGINEERING EA 5-2010-180 FLY ON FOR 1000 FH, WITHIN WHICH TIME A REPLACEMENT OF THE DAMAGED DOOR TREAD MUST BE PERFORMED.

Part: WIRE HARNESS — FAULTY (NLG) · airframe 11,759 hrs · 9,554 cycles

WOW INPUT CAUTION MSG CYCLED FIVE TIMES ON AND OFF AFTER GEAR RETRACTION. REMOVED AND REPLACED NLG ELECTRICAL HARNESS IAW AMM 32-61-25. OPS CHECK NORMAL, OK FOR SERVICE.

Part: CONTROL SYSTEM — FAILED (TE FLAPS)

(REF NR: 05-087) FLAPS FAILED ON APPROACH, QRH FOLLOWED UNEVENTFUL LANDING. RESET FLAPS AND PLACED SYSTEM ON 72 HOUR WATCH IAW AD 98-20-01. (K)