N443AW

Part: POWER SUPPLY — INOPERATIVE (TE FLAP SYS) · airframe 38,851 hrs · 37,475 cycles

FLAPS FAIL AT ZERO DEGREES ON APROACH WHEN SELECTED FROM 0 TO 8, FLAPS DID NOT MOVE. LANDING WEIGHT APROX 45000 LBS, SMOOTH UNEVENTFUL LANDING, MAX BTMS 7556. AIRCRAFT REMOVED FROM SERVICE. REF WO 307503 MX WC 2-19 FOR TBS AND CORRECTIVES (LH AND RH BPSU WERE SWAPPED PER MHI ACTION PLAN AND FAULT FOLLOWED TO RH SIDE RH BPSU WAS REPLACED AND OPS CK GOOD) RII ACCOMPLISHED ON WO 307503

Part: FLAP SYSTEM — FAILED (TE FLAPS) · airframe 38,842 hrs · 37,466 cycles

REF 347659-2 AFTER TAKEOFF, REC FLAP FAIL CAUTION MSG DURING FLAP RETRACTION FROM FLAPS 8 TO FLAPS 0. CW AWA SUP 98-018I RESET FAILED WHEN MOVING HANDLE FROM 8 TO 0 TO BEGIN 5 FLAP CYCLES ***AIRCRAFT REMOVED FROM SERVICE*** MX IN PROGRESS

Part: FLAP SYSTEM — MALFUNCTIONED · airframe 38,818 hrs · 37,438 cycles

FLAP FAIL AT 0, FLAPS ALREADY ON MEL, FN 3917 EMERGENCY DECLARED BY CREW. AS THEY TURNED ONTO AN EXTENDED FINAL INTO ORD, FO FLYING, WENT UNDER 180, SELECTED FLAPS TO 8 & RECEIVED A FLAP MASTER CAUTION, FLAPS NEVER MOVED OUT OF 0. RAN QRH & DECLARED EMERGENCY. SELECTED 10 CENTER. APPROACH FINE, LANDING NORMAL, HIGHEST BTMS READING WAS 8. REMOVED FROM SERVICE. TROUBLESHOT IAW FIM 27-50-00. FOUND POTENTIOMETERS 6+7 OUT OF LIMITS IAW AMM 27-51-10. RIGGED IAW AMM 27-51-10. POTENTIOMETERS FELL OUT OF RIG AFTER OPS CHECK OF FLAPS. R & R FECU IAW AMM 27-51-05. OPS CHECKED GOOD. NO FAULTS FOUND.

Part: FLAP SYSTEM — MALFUNCTIONED · airframe 38,816 hrs · 37,434 cycles

DURING APPROACH AND FLAPS SET TO ZERO, RECIEVED A FLAPS FAIL CAUTION. 44 PASSENGERS, FO WAS FLYING, NO OBSERVERS. CAPTAIN STATED DURING DEBRIEF THAT IT WAS A NORMAL ILS APPROACH AT 10 CENTER AND 210 KIAS. LOWERED GEAR AT 200 KIAS. CAPTURED GLIDESLOPE AT 170 KIAS. SET FLAPS TO 8 AND HEARD A "DING" FLAPS STAYED AT ZERO. CREW ASKED FOR A "GO AROUND" AND HAD WAS ABLE TO LAND ON THE LONGEST RUNWAY AVAILABLE. IT WAS A NORMAL LANDING AT 10 LEFT. CREW REQUESTED FOR EMERGENCY RESPONSE AND THE FA WAS BRIEFED. PA ANNOUNCMENT TO THE PASSENGERS WAS MADE. IT WAS A NORMAL TAXI AND THE JET BRIDGE WAS USED. EMERGENCY VEHICLE DID FOLLOW THE A/C TO THE GATE. THERE WAS NO KNOWN INJURIES, A/C, OR PROPERTY DAMAGE NOTED. NO ADVERSE REACTON FROM THE PASSENGERS. THE CREW HAD NO REG OR SAFETY CONCERNS. REF. 347655/2, "FLAP FAIL @ ZERO ON APPROACH. SMOOTH LANDING, BRAKE TEMP IS NORMAL. PERFORMED FLAP RESET PROCEDURE IAW WAC SUP 98-18I BOX 12. FLAPS RESET. PLACARDED AND PLACED ON MEL"---- MEL WAS REAPPLIED AND HAD 6 CYCLES REMAINING. PLANNING HAS THE A/C SCHEDULED FOR OVERNIGHT MX IN ATW TONIGHT (17JULY21). ***AIRCRAFT REMOVED FROM SERVICE*** MX IN PROGRESS

Part: CONTROL UNIT — MALFUNCTIONED (TE FLAPS) · airframe 38,813 hrs · 37,430 cycles

DURING THE APPROACH TO KORD, THE FLIGHT CREW EXPERIENCED A FLAP FAILURE AND DISCONTINUED THE APPROACH. THE CREW COMPLETED REQUIRED CHECKLISTS, DECLARED AN EMERGENCY WITH ATC, COMMUNICATED WITH THE FLIGHT ATTENDANT, PASSENGERS AND DISPATCH THEN RETURNED AND LANDED AT KORD WITHOUT FURTHER INCIDENT. FLAP RESET WAS PERFORMED SUCCESSFULLY ON THE GROUND AND SYSTEM WAS PLACED ON MEL. AIRCRAFT REMOVED FROM SERVICE, DURING T/S NOTED THE FECU'S DISPLAY WAS INTERMITTENTLY FLASHING. REPLACED THE FECU IAW AMM 27-51-05, OPS CHECK GOOD. REMOVED PLACARD

Part: FLAP SYSTEM — STUCK · airframe 38,696 hrs · 37,316 cycles

AFTER SELECTING FLAPS ZERO AFTER TAKEOFF, RECEIVED FLAPS FAIL CAUTION MESSAGE. FLAPS STUCK AT 3 DEG LEFT & 4 DEG RIGHT. IAS AT TIME OF FLAP FAIL WAS 200 KTS, OAT OF 27 DEG C, & TIME NOTED IN AIR WAS 1 MINUTE. (BLOCK 2) PERFORMED FLAP RESET PROCEDURE IAW SUPP 98-018I BOX 12. FLAPS RESET. PLACARDED AND PLACED ON MEL. MEL CANNOT BE APPLIED DUE TO PREVIOUS WRITE UPS. REF BLOC THREE FOR NEW DISCREPANCY A/C FERRY OUT OF PNS TO MKE- FLT # 3172 AIRCRAFT REMOVED FROM SERVICE. LEFT AND RIGHT BPSU REQUIRED RIGGING. RIGGED LEFT AND RIGHT BPSU IAW AMM 27-51-10 OPS CHECKS GOOD.

Part: BPSU — FAILED (TE FLAP SYSTEM) · airframe 38,690 hrs · 37,313 cycles

AT FL 300 AND MACH . FLAPS FAILED AT ZERO. AIRCRAFT REMOVED FROM SERVICE. LEFT BPSU REPLACED, OPS CHECK GOOD.

Part: BPSU — FAILED (TE FLAP SYSTEM) · airframe 38,687 hrs · 37,310 cycles

FL 240 RECEIVED FLAPS FAIL CAUTION MSG C/W QRH FLAPS FAILED AT 0 DEGREES. DECLARED AN EMERGENCY AND LANDED WITH NO ISSUES IN IAD. C/W FIM RESET IAW AWAC SUP 98-18I BOX 12 FLAP RESET, AND PLACED ON MEL AIRCRAFT REMOVED FROM SERVICE. R&R LFT BPSU IAW AMM27-51-10 OPS CHECKS GOOD REMOVE PLACARD AND REMOVE FROM MEL. RII I-278

Part: SKIN — DENTED (RT WING) · airframe 37,632 hrs · 36,157 cycles

PERFORM PERMANENT REPAIR TO R/H L/E BETWEEN WS 226 TO WS 242 THAT MEASURES 2.0"L X 2.5" W X .037"D. "AIRCRAFT REMOVED FROM SERVICE" DENT AT WS 242 REFORMED TO ORIGINAL CONTOUR AND HFEC WITH NO CRACK INDICATIONS. REF ASAP EA# AWAC-CRJ257-01476 REV IR DTD 03/14/20.

Part: DOUBLER — CORRODED (CLOSET) · corrosion level 2 · airframe 37,632 hrs · 36,157 cycles

SUPPLEMENTAL, CLOSET ASSY HAS CORROSION ON LWR SILL BY MOUNT POINT. AIRCRAFT REMOVED FROM SERVICE. MANUFACTURED PART ITEMS 55 & 75 AND REPLACED ITEMS 35 AND 65. REF ASAP EA AWAC-CRJ225-01480 REV IR DTD 3/21/20.

Part: CABLE — FRAYED (PAX DOOR) · airframe 37,632 hrs · 36,157 cycles

L1 DOOR MAIN PAX DOOR POWER ASSIST CABLE IS FRAYED. "AIRCRAFT REMOVED FROM SERVICE" REMOVED AND REPLACED L1 MAIN PAX DOOR POWER ASSIST CABLE REF CRJ-200 AMM 52-11-00

Part: SKIN — DENTED (FUSELAGE) · airframe 37,632 hrs · 36,157 cycles

PERFORM REPAIR TO L/H FUSELAGE SKIN BETWEEN FRAMES FS 544 TO FS 559 & S9L TO S10L FOR 1-OFF DENT THAT MEASURES 2.4"L X .5"W X .128"D. "AIRCRAFT REMOVED FROM SERVICE" CUTOUT DAMAGED AREA. HFEC PERFORMED AROUND CUTOUT. REPAIR DOUBLER FABRICATED FROM 2024-T3 0.063" AND INSTALLED REF ASAP EA# AWAC-CRJ253-01468 REV IR DTD 03/25/2020

Part: VANE — CRACKED (THRUST REVERSER) · airframe 37,632 hrs · 36,157 cycles

#2 ENGINE THRUST REVERSER CASCADE AT 12 O'CLOCK POSITION HAS A CRACKED VANE. "AIRCRAFT REMOVED FROM SERVICE" REMOVED AND REPLACED 12 O'CLOCK POS CASCADE ON #2 ENG REF CRJ 299 AMM 78-33-01. REV 60

Part: BRACKET — DAMAGED (NLG WW) · airframe 37,570 hrs · 36,101 cycles

AFTER T/O SELECTED GEAR UP GOT GEAR DISAGREE AND NOSE DOOR OPEN (W) MS GS AND NOSE GEAR WOULD NOT RETRACT. RAN QRH FOR NOSE DOOR OPEN ALL (W) MSGS DISAPPEARED AIRCRAFT REMOVED FROM SERVICE INSPECTED NLG DOORS, NO DEFECTS NOTED, NO HYD LEAKS NOTED. INTERROGATED PSEU RCVD CODES DI14 DOWN ON, DI15 DOWN ON,S23DOWN FAR, S22DOWN FAR, S30DOWN FAR, S31DOWN FAR, S32DOWN FAR, S21DOWN NEAR, S35DOWN NEAR. GEAR WAS PINNED IN DOWN POSITION AND PLACED ON MEL. FOUND TOW GUARD COLLAR SLIPPED AND DAMAGED CENTER PROX SWITCH BRACKET COMPLY WITH THE WORK INSTRUCTONS OF EO E19/016/432 ORG R/R'D NLG CENTERED/EXTENDED PROX SENSOR SUPPORT BRACKET PER AMM 32-61-05 SET SENSOR GAP PER AMM 32-61-05 PEROFMRED RETRACTION EXTENSION FUNCTIONAL TEST OF LANDING GEAR IAW TASK 32-30-00 OPS CK GOOD

Part: BPSU — MALFUNCTIONED (TE FLAP) · airframe 37,154 hrs · 35,687 cycles

SHORTLY AFTER DEPARTURE, THE FLIGHT CREW RECEIVED A FLAP FAIL CAUTION MESSAGE. THE CREW DECLARED AN EMERGENCY AND RETURNED TO KORD WITHOUT FURTHER INCIDENT. FLAPS FAIL CAS MSG MOVING FLAP LEVERS FROM 8 TO 0 AFTER TAKE OFF PERFROMED FLAP FAIL RESET PROCEDURES IAW SUP 98-186G BOX 12. FLAPS RESET PLACARDED AND PLACED ON MEL. AIRCRAFT REMOVED FROM SERVICE. R/R LT BPSU IAW AMM 27-51. OP CHECK GOOD. REMOVED PLACARD AND REMOVED FROM MEL. S/N OFF 1702A S/N ON 2297.

Part: PITOT LINE — CONTAMINATED (PITOT\STATIC SYS) · airframe 37,100 hrs · 35,622 cycles

DURING CLIMB OUT IN MODERATE ICING RECEIVED IAS AND ALT YELLOW BOX MSG"S ON BOTH PFD'S AND OTHER ASSOCIATED MSG'S. NO PITOT OR STATIC HEAT FAILURES. COULD NOT ISOLATE EITHER ADC, BOTH APPEARED INOP. RECEIVED ADC TEMP DISAGREE CAUTION AFTER 10 MIN. ALL MSG'S CLEARED AFTER LEAVING ICING CONDITIONS AND ALL INDICATIONS MATCHED AND APPEARED NORMAL APPROXIMATELY 8 MILES OUT ON APPROACH. THE CREW DECLARED AN EMERGENCY AND AIR RETURNED TO SBN AIRCRAFT REMOVED FROM SERVICE COMPLIED WITH AWAC SUPP. 17-077B, THE INSPECTION FOR UN-RELIABLE AIR DATA, FOUND AND PURGED CONTAMINATION IN #2 ADC PITOT-LINE AND P1, P2, S1 AND S2 DRAIN VALVES IAW AWAC SUPP. 18-167 AND REMOVAL AND REPLACEMENT OF #2 ADC IAW AMM 34. OPS AND LEAK CHECK GOOD IAW SUPP. 17-010. S/N OFF 10CLH S/N ON H4LF JLC

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 35,707 hrs · 34,295 cycles

LEFT WINDSHIELD ARCED AT FL 280 CW QRH. APPEARS TO BE CRACKED. LH WINDSCREEN MIDDLE PANE IS CRACKED ALMOST FULL WIDTH

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 35,164 hrs · 33,748 cycles

OUT OF 15,000FT IN DECENT RECEIVED DYD 1 LO PRESS CAUTION C/W QRH PROBLEM DID NOT RESOLVE. PRESSURE WENT FROM 1800PSI TO 500PSI IN 2 MINUTES. TURNED ACMP OFF, PUMP RAN FOR APPROX 3 MINUTES. EDP RAN FOR APPROX 15 MINUTES AT LO PRESS.

Part: WARNING MESSAGE — ILLUMINATED · airframe 34,968 hrs · 33,611 cycles

4826 WHILE TRANSFERING BLEEDS TO THE ENGINES AFTER T/O CHECKLIST RECEIV ED LH PACK HI PRESSURE CAUTION MSG. CW QRH PROCEEDURE. MSG REMAINED. ON CLIMB WITH LG ENGINE AT BELOW 60% N1 RECEIVED LH PACK OVERPRESSURERE DUCED LH ENGINE TO 57% N1 AND CYCLED PACK SW. MSG REMAINED. RETURNED TO CAK CW LEAK CHECK OF LH PACK IAW AMM 21-51-00. CW OPS CHECK OF LH PACK IAW AMM 21-51-00. OPS AND LEAK CHECK GOOD.

Part: LATCH — CRACKED (LRU DOOR) · airframe 34,310 hrs · 32,961 cycles

LEFT LRU DOOR AFT LATCH STRUCTURE IS CRACKED.

Part: BULKHEAD — CRACKED (BS 621) · airframe 34,310 hrs · 32,961 cycles

AFT PRESSURE BULKHEAD ABOVE AFT CARGO DOOR TRACK AT UPPER END IS CRACKED .

Part: FITTING — CRACKED (BS 461) · airframe 34,310 hrs · 32,961 cycles

BATH TUB FITTING AT BS 461, OTBD SIDE OF LBL 9 IS CRACKED.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 34,310 hrs · 32,961 cycles

PAX DOOR HAD A CRACKED AFT DRAG ANGLE.

Part: HINGE — CRACKED (PAX DOOR STEP) · airframe 34,310 hrs · 32,961 cycles

PAX DOOR LOWER FOLDING STEP HINGE CRACKED.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 34,310 hrs · 32,961 cycles

LEFT INBD FLAP LOWER SKIN DENTED AT FLAP STATION 54.5 APPROXIMATELY 4 INCHES FROM TRAILING EDGE.

Part: BRACKET — CRACKED (BS 529) · airframe 34,310 hrs · 32,961 cycles

RIGHT MLG WHEEL WELL PRESSURE TRANSDUCER BRACKET IS CRACKED. REPLACED THE BRACKET IAW SRM 51-42-06.

Part: RETAINER — CRACKED (PLYON PANEL SEAL) · airframe 34,310 hrs · 32,961 cycles

L/H PYLON PANEL 412BT SEAL RETAINER CRACKED. REPAIRED THE SEAL RETAINER IAW SUPP 16-363.

Part: RETAINER — CRACKED (PANEL SEAL) · airframe 34,310 hrs · 32,961 cycles

LEFT LOWER PYLON PANEL 412DB SEAL RETAINER IS CRACKED. REPAIRED THE SEAL RETAINER IAW 16-363.

Part: ANGLE — DAMAGED (BS 280-295) · airframe 34,310 hrs · 32,961 cycles

ANGLE DAMAGED AT BS 280 TO 295, STRINGERS 2L TO 4L, REPAIRED IAW REO 601R31522.

Part: ANTI-ICE VALVE — DEFECTIVE (LT COWLING) · airframe 34,022 hrs · 32,650 cycles

CLIMBOUT RECEIVED LEFT COWL ANTI-ICE CAUTION MESSAGE WITH COWL ANTI-ICE SELECTED OFF. C/W QRH MESSAGE CLEARED AT 84% N2. RETURNED FOR A NORMAL LANDING UNDER LANDING WEIGHT.

Part: ACTUATOR — MALFUNCTIONED (YAW DAMPER) · airframe 33,732 hrs · 32,321 cycles

UNCOMMANDED YAW, ONCE DURING CLIMB AND ONCE IN CRUISE. SLIGHT YAW AND NO CROSSWIND OR TAILWIND NOTICED. NO MESSAGE POSTED, AUTOPILOT ENGAGED. REMOVED AND REPLACED LEFT YAW DAMPER LINEAR ACTUATOR IAW AMM 22-22-01. OPS CHECKED GOOD.

Part: B-NUT — LEAKING (APU) · airframe 32,469 hrs · 31,142 cycles

DURING DESCENT WITH APU OFF AND BOTH PACKS SELECTED TO AUTO, CREW REPORTED STRONG FUEL ODOR IN CABIN AND COCKPIT. PERFORMED VISUAL INSPECTION OF AFT EQUIPMENT BAY AIR CONDITIONING DUCTS, NO DEFECTS NOTED. FOUND A B-NUT FITTING ON APU FUEL CONTROL UNIT LEAKING WHEN APU WAS RUNNING. SHUT OFF APU, NO LEAKS NOTED. CLEANED SPILL AND PERFORMED OPS CHECK OF AIR CONDITIONING SYSTEM WITH ENGINES RUNNING WITH CREW ASSISTANCE. NO FUEL ODOR NOTED FROM PACKS, SYSTEM CHECKS GOOD IAW AMM 2151-00.

Part: UNKNOWN — ODOR (CABIN) · airframe 32,320 hrs · 31,006 cycles

EXHAUST SMELL AND SMOKE IN CABIN WITH BOTH PACKS ON AND APU RUNNING.

Part: SKIN — DAMAGED (BS 559-574) · airframe 32,181 hrs · 30,874 cycles

FUSELAGE SKIN DAMAGED AT BS 559+112 TO 574, STRINGERS 14 TO 16R.

Part: STRINGER — DAMAGED (BS 559-574) · airframe 32,181 hrs · 30,874 cycles

STRINGER 15R DAMAGED BETWEEN BS 559+112 AND 574

Part: INVERTER — INOPERATIVE (CABIN) · airframe 31,570 hrs · 30,315 cycles

FLIGHT NUMBER 4041. EMERGENCY LIGHTS BETWEEN ROWS 5D AND 8D, AND EMERGENCY EXIT ROW 8F LOWER GREEN EXIT SIDEWALL SIGN NOT ILLUMINATING. R & R THE NR 3 INVERTER IAW AMM 33-51-07. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,485 hrs · 30,235 cycles

FLIGHT 3862. LEFT LOWER EXIT LIGHT ROW 8 INOPERATIVE. FLOOR LIGHT ROWS 2-5 INOPERATIVE CYCLED EMERG LIGHT SWITCH. EMERGENCY LIGHTS OPS CHECK GOOD IAW AMM 33-51

Part: HEAT EXCHANGER — UNSERVICEABLE (LT ENGINE) · airframe 31,271 hrs · 30,024 cycles

ON CLIMBOUT, RECEIVED HIGH OIL TEMP OF 151, FLASHING YELLOW, CW QRH OIL TEMP AGAIN CLIMBED IN TO CAUTION RANGE, FOLLOWED QRH PROCEDURES, ACCOMPLISHED SINGLE ENGINE PROCEDURES, OIL TEMP AND PRESSURE CLIMBING PRIOR TO ENGINE SHUTDOWN, OIL PRESSURE NEVER EXCEEDED 70 PSI. R & R LT ENGINE HEAT EXCHANGER IAW AMM 79-21-07, OPS CHECK GOOD, LEAK CHECK GOOD.

Part: SPAR — DAMAGED (RT HORIZ STAB) · airframe 30,746 hrs · 29,540 cycles

REPAIR RT HORIZONTAL STAB AT RIB 9. TEMP REPAIR COMPLIED WITH IAW REO 601R-55-11-519. PERFORM PERMANENT REPAIR.

Part: SKIN — DAMAGED (RT HORIZ STAB) · airframe 30,746 hrs · 29,540 cycles

REPAIR RT HORIZONTAL STAB, LOWER SKIN TEMP REPAIR IAW REO 601R-55-11-520. PERFORM PERMANENT REPAIR AS REQUIRED.

Part: SUPPORT ANGLE — CRACKED (NLG WW) · airframe 30,746 hrs · 29,540 cycles

RBL 9 IN NLG WW HAS A CRACKED SUPPORT ANGLE TOP OF RBL 9 POST. REPLACED ANGLE AT RBL 9 & FS 202.75 IN NLG BAY IAW SRM 51-42-06.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,746 hrs · 29,540 cycles

SEAT RAIL BEAM, LBL 27 INBD & OTBD FLANGE, FS 574.00 - 605.00, HAS CORROSION.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,746 hrs · 29,540 cycles

SEAT RAIL LBL 27 OTBD FLANGE HAS CORROSION AFT OF FS 559+112.

Part: FITTING — CRACKED (FUSELAGE) · airframe 30,746 hrs · 29,540 cycles

CLIP FS 605.00 UNDER CARGO DOOR SILL CRACKED.

Part: FRAME — CRACKED (FUSELAGE) · airframe 30,746 hrs · 29,540 cycles

FS 333.00 FRAME CRACKED INBD OF PAX DOOR UPPER SILL.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 30,746 hrs · 29,540 cycles

RIGHT WINDSHIELD SIDE POST LOWER OTBD ANGLE CLIP IS CRACKED IN FLIGHT DECK.

Part: SKIN — CHAFED (RUDDER) · airframe 30,746 hrs · 29,540 cycles

BOTH SIDES OF RUDDER LE ARE HEAVILY CHAFED.

Part: SUPPORT BRACKET — CRACKED (PAX DOOR) · airframe 30,746 hrs · 29,540 cycles

PASSENGER ENTRY DOOR SUPPORT WHEEL BRACKET CRACKED.

Part: STRAP — DAMAGED (FUSELAGE) · airframe 30,746 hrs · 29,540 cycles

INSTALLED NEW FUEL PRESS BOX, REQUIRED STRAP REPLACEMENT.

Part: FITTING — CRACKED (FUSELAGE) · airframe 30,746 hrs · 29,540 cycles

CLIP ON THE INBD SIDE OF STRINGER 3L AT FS 280.00 IS CRACKED, REPLACED.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 30,746 hrs · 29,540 cycles

STRINGER 3L AT FS 280 IS CRACKED, REPLACED.

Part: ATTACH BRACKET — CRACKED (FUSELAGE) · airframe 30,746 hrs · 29,540 cycles

RIGHT OVERWING TO FUSELAGE CLOSEOUT PANEL ATTACHMENT STRUCTURE, FS 461.00 IS CRACKED. REPLACED PANEL SUPPORT ATTACHMENT IAW SRM 51-24-21, 51-40-11, 51-42-06 & 53-82-83.

Part: STOP FITTING — CRACKED (RT SPOILER) · airframe 30,746 hrs · 29,540 cycles

RIGHT WING FLIGHT SPOILER INBD SPRING STOP IS CRACKED. REPLACED RT WING FLIGHT SPOILER INBD SPRING STOP IAW SRM 51-42-06 & 51-42-21.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 30,746 hrs · 29,540 cycles

RIGHT OVERWING TO FUSELAGE CLOSE OUT PANEL ATTACHMENT STRUCTURE FS 449.85 IS CRACKED. REPLACED RT OVERWING TO FUSELAGE CLOSE OUT PANEL ATTACHMENT STRUCTURE ANGLE IAW SRM 51-42-06.

Part: ATTACH FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,746 hrs · 29,540 cycles

SEAT RAIL BEAM ATTACH FITTING FS 621.00 & LBL 9 HAS CORROSION. REPAIRED FLOORBEAM ATTACH FITTING IAW EA AWAC-CRJ253-00363.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 30,746 hrs · 29,540 cycles

FRAME 235 IS CRACKED JUST UNDER THE LT WINDSHIELD SIDE POST SUPPORT IN THE FLIGHT DECK. REPLACED POST SUPPORT UNDER LT WINDSHIELD IAW SRM 51-42-06 & 51-42-21.

Part: ATTACH FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,746 hrs · 29,540 cycles

RBL 9 & FS 621.00 SEAT RAIL ATTACHMENT FITTING HAS CORROSION. REPAIRED RBL 9 & FS 621.00 FLOORBEAM IAW EA AWAC-CRJ253-00364.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 30,746 hrs · 29,540 cycles

REPAIR FILLER ON THE AFT PRESS BULKHEAD, FWD SIDE, HAS SEVERAL SCRIBE MARKS ON IT & IS SUSPECTED TO BE CRACKED, LOCATED AROUND LINTEL FITTING AT FS 621.00, LBL45, WL 113.33 IN THE CARGO BAY. REPAIRED CRACKED EXISTING LINTEL REPAIR WEB FILLER IAW REO 601R-53-61-5701 REV A DATED 2016 05 03.

Part: SKIN — GOUGED (FUSELAGE) · airframe 30,746 hrs · 29,540 cycles

UPON REMOVAL OF RT STUB FAIRING FOUND DEEP GOUGE IN THE RT APRON SKIN. REPAIRED APRON SKIN IAW REO 601R-53-41-610 REV DATED 2007 10 29.

Part: ATTACH BRACKET — CRACKED (FUSELAGE) · airframe 30,746 hrs · 29,540 cycles

RIGHT OVERWING TO FUSELAGE CLOSEOUT PANEL ATTACHMENT STRUCTURE, FS 469.15 IS CRACKED. REPLACED ATTACHMENT BRACKET AT FS 469.15 IAW SRM 51-24-21, 51-40-11, 51-42-06, 51-41-02 & 53-82-83.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 30,746 hrs · 29,540 cycles

AFT PRESS BULKHEAD INTERCOSTAL AT FS 621.00 & STRINGER 14L IS CRACKED. REPLACED INTERCOSTAL ON AFT PRESS BULKHEAD IAW SRM 51-42-21 & 51-41-06.

Part: SUPPORT ANGLE — CRACKED (RT WING) · airframe 30,746 hrs · 29,540 cycles

UPPER OTBD CORNER OF PICOLO TUBE SUPPORT AT RT WS 143.89 IS CRACKED. REPLACED SUPPORT ANGLE IAW SRM 51-41-02, 51-40-11 & 51-42-15.

Part: STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,746 hrs · 29,540 cycles

FS 559.00 FLOOR STRAP, LBL 36 TO LT SILL HAS CORROSION. REPLACED FS 559.00 FLOOR STRAP, AT LBL36 TO LT SILL IAW SRM 51-42-06.

Part: FITTING — CRACKED (FUSELAGE) · airframe 30,746 hrs · 29,540 cycles

LEFT WINDSHIELD SIDE POST LOWER OTBD ANGLE CLIP IS CRACKED. REPLACED ANGLE CLIP IAW SRM 51-42-21.

Part: ANGLE — CRACKED (LT WING) · airframe 30,746 hrs · 29,540 cycles

UPPER ANGLE UNDER PANEL 520ML IS CRACKED. REPLACED UPPER ANGLE UNDER PANEL 520ML IAW SRM 51-42-15 & 51-41-02.

Part: STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,746 hrs · 29,540 cycles

FLOOR STRAP AT FS 559 HAS CORROSION, BETWEEN RBL 27 & THE RT FLOOR SILL IN CABIN. REPLACED FLOOR STRAP AT FS 559, BETWEEN RBL 27 & THE RT FLOOR SILL IAW SRM 51-42-06.

Part: MOUNT BRACKET — CORRODED (SERVICE DOOR) · corrosion level 2 · airframe 30,746 hrs · 29,540 cycles

SERVICE DOOR INNER HANDLE MICRO SWITCH MOUNT BRACKET IS CORRODED. REPLACED SERVICE DOOR INNER HANDLE MICRO SWITCH MOUNT BRACKET IAW SRM 51-42-21 & 51-41-02.

Part: STIFFENER — CRACKED (RT FAIRING) · airframe 30,746 hrs · 29,540 cycles

RIGHT JET PIPE FAIRING HAS A CRACK AT THE 9 O'CLOCK POSITION OF THE SECOND STIFFENER FROM THE FRONT. REPAIRED RT JET PIPE FAIRING IAW CMM 78-11-00 TASK 78-11-00-300-810-A01.

Part: RELIEF VALVE — FAULTY (ANTI-ICE SYS) · airframe 30,166 hrs · 29,023 cycles

LEFT COWL, ANTI-ICE FAILED OPEN, COMPLIED WITH QRH, VLV WOULD ONLY CLOSE WHEN LT 14TH STAGE BLEED SOV WAS CLOSED. DIVERTED BACK DUE TO ICING CONDITIONS. COWL ANTI-ICE VLV IAW AMM 30-22-01. OPERATIONS CHECKED GOOD. R & R LT PRESS RELIEF VLV IAW AMM 30-22-04. OPERATIONS CHECKED GOOD.

Part: PSEU — FAULTED (LANDING GEAR) · airframe 29,659 hrs · 28,538 cycles

FLIGHT 3902, AT 31000 FEET RECEIVED NOSE DOOR OPEN WARNING & AURAL MSG. COMPLIED WITH QRH. ALSO RECEIVED PARKING BRAKE SOV & ANTI-SKID INBD CAUTION MSGS, & PROX SYS FAULT WHITE STATUS SGS, HEARD & FELT NOSE DOOR OPEN AT ABOUT 245 KNOTS INDICATED. PSEU HAS A 03 FAIL CODE. R & R PSEU IAW AMM 32-61-01. ALL CHECKED GOOD.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 28,023 hrs · 26,931 cycles

RECEIVED STEERING INOPERATIVE & WOW INPUT CAUTION MSG'S ON DEPARTURE. COMPLIED WITH QRH, MSG REMAINS. HAPPENED DURING GEAR RETRACTION.

Part: TRIM SYSTEM — MALFUNCTIONED (STAB) · airframe 27,993 hrs · 26,841 cycles

STAB TRIM MOVING WITHOUT PILOT INPUT.

Part: LINE — LOOSE (LT ENGINE) · airframe 25,930 hrs · 24,941 cycles

PRECAUTIONARY ENG SHUTDOWN OF LT ENG FOR OIL PRESS INDICATION. PRESS INDICATION 22 PSI UPON ENG SHUTDOWN. ENG SHUTDOWN FOR 15 MIN WITH POSITIVE OIL PRESS. SERVICED ENG OIL LT 16.25 PTS, INSPECTED FOUND LOOSE OIL SUPPLY LINE. TORQUED TO 75 FT LBS IAW AMM 79-11-01, INSPECTED MASTER CHIP DETECTOR, NO PARTICLES FOUND IAW 79-21-09. MOTORED ENG NO LEAKS NOTED. RAN ENGS NO LEAKS NOTED. PERFORMED ENG LT CHIP DETECTOR TASK, NO FAULTS FOUND.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 25,899 hrs · 24,908 cycles

PAX DOOR AFT DRAG ANGLE CRACKED NEAR POWER ASSIST MOTOR CABLE CUT OUT. REPAIRED PAX DOOR AFT DRAG ANGLE IAW REO 601R-52-11-513 REV A DATED 09 MAR 05.

Part: SPLICE — CRACKED (RT EXHAUST) · airframe 25,899 hrs · 24,908 cycles

RIGHT EXHAUST NOZZLE SPLICE CRACKED. REMOVED CRACKED SPLICE & INSTALLED SERVICEABLE SPLICE IAW SRM 51-21-11, 51-40-11 & 51-42-06 SPLICE.

Part: BRACKET — CRACKED (LT ENGINE) · airframe 25,899 hrs · 24,908 cycles

LEFT ENG LOWER FAN CASE BRACKET CRACKED. R & R WITH NEW SERVICEABLE BRACKET IAW REO 601R-71-61-3941 REV A.

Part: RETAINER — CORRODED (E&E DOOR) · corrosion level 2 · airframe 25,899 hrs · 24,908 cycles

AVIONICS DOOR SEAL RETAINER CORRODED. R & R SEAL RETAINERS PN CC670-38674-3, CC670-38663-5, CC670-38662-5 & CC670-38675-3 IAW SRM 51-40-11 & 51-42-06.

Part: FITTING — CRACKED (FUSELAGE) · airframe 25,899 hrs · 24,908 cycles

CRACKED CLIP AT FS 484, RBL 27 & RBL36. REMOVED CRACKED CLIPS 2 EACH AT FS 484, RBL 27 & 36 & INSTALLED SERVICEABLE CLIPS IAW SRM 51-23-00, 51-25-06, 51-25-16, 51-42-06, 51-21-11 & 51-42-21.

Part: WEB — CRACKED (PAX DOOR) · airframe 25,899 hrs · 24,908 cycles

PAX DOOR AFT WEB AT UPPER STEP NR 2 IS CRACKED. REPAIRED PAX DOOR AT WEB IAW REO 601R-52-11-702 REV C DATED 2010-03-09.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 25,899 hrs · 24,908 cycles

NUMBER 2 HYD MANIFOLD SUPPORT INTERCOSTAL CRACKED. REPAIRED BRACKET IAW 601R-53-62-031 REV A DATED 13-JAN-2007.

Part: SUPPORT BRACKET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 25,899 hrs · 24,908 cycles

THREE SUPPORT BRACKETS THAT HOLD THE DECOMPRESSION EQUALIZER DIAPHRAGMS ARE CORRODED. R & R BRACKETS WITH NEW SERVICEABLE BRACKETS IAW SRM 51-40-11 & 51-42-06.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 25,899 hrs · 24,908 cycles

LOWER U BRACKET CRACKED AT RIVET FS 574.00. R & R U BRACKET WITH NEW SERVICEABLE BRACKET IAW SRM 51-42-06 & 51-41-00.

Part: THRESHOLD — CRACKED (FUSELAGE) · airframe 25,899 hrs · 24,908 cycles

CARGO BAY THRESHOLD IS CRACKED & CHAFED. R & R WITH NEW SERVICEABLE THRESHOLD IAW SRM 51-40-11.

Part: MOUNT BRACKET — CRACKED (LT MLG WW) · airframe 25,899 hrs · 24,908 cycles

LEFT MLG BRAKE VOLUMETRIC FUSE TRANSDUCER MOUNT BRACKET IS CRACKED. REMOVED CRACKED LT MLG BRAKE VOLUMETRIC FUSE TRANSDUCER MOUNT BRACKET & INSTALLED NEW SERVICEABLE BRACKET IAW SRM 51-40-06.

Part: MOUNT BRACKET — CRACKED (RT MLG WW) · airframe 25,899 hrs · 24,908 cycles

RIGHT MLG BRAKE VOLUMETRIC FUSE TRANSDUCER MOUNT BRACKET IS CRACKED. REMOVED UNSERVICEABLE BRACKET & INSTALLED NEW BRACKET IAW SRM 51-40-11 & 51-42-06.

Part: FITTING — CRACKED (FUSELAGE) · airframe 25,899 hrs · 24,908 cycles

FS 280 RBL 9 INBD & OTBD FLOOR SUPPORT BEAM CLIPS ARE CRACKED. REMOVED UNSERVICEABLE CLIPS & INSTALLED SERVICEABLE CLIPS IAW REO 601R-53-11-171REV D.

Part: ANGLE — CRACKED (BS 484) · airframe 25,899 hrs · 24,908 cycles

LEFT SIDE FS 484 ANGLE IS CRACKED. R & R ANGLE WITH NEW SERVICEABLE IAW REO 601R-53-41-059 REV B.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 25,899 hrs · 24,908 cycles

LEFT INTERCOSTAL ANGLE IS CRACKED AT FS 621 BULKHEAD STRINGER 14L. REMOVED CRACKED LT OBLIQUE ANGLE & INSTALLED NEW SERVICEABLE ANGLE IAW SRM 51-42-21.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 25,899 hrs · 24,908 cycles

RIGHT FLOOR SILL CORROSION BEYOND LIMITS AT FS 559+87. REPAIRED RT FLOOR SILL AT FS 559+87 IAW EA 15-2014-081.

Part: BEAM — CRACKED (FUSELAGE) · airframe 25,899 hrs · 24,908 cycles

VERTICAL BEAM AT FS 409+128 HAS CRACK ON LOWER OTBD SIDE. REPAIRED BEAM AT FS 409+128 LBL 18 IAW REO 601R-53-41-056 REV F.

Part: TRUNNION — DAMAGED (RT MLG) · airframe 25,899 hrs · 24,908 cycles

DURING COLD WORKING OF RT MLG TRUNNION LOWER FLANGE, FOUND 4 OVER SIZED HOLES. REPAIRED RT MLG TRUNNION FLANGE AT WS 65.75 BETWEEN RS & AUX SPAR IAW REO 601R-57-21-2154.

Part: SKIN — CRACKED (FUSELAGE) · airframe 25,899 hrs · 24,908 cycles

FUSELAGE SKIN CRACKED ON LT & RT AFT CORNERS OF THE NLG WW. REPAIRED LT & RT AFT CORNERS OF NLG WW IAW REO 601R-53-11-048 REV C DATED 2008-10-01.

Part: RIB — CRACKED (RT WING) · airframe 25,899 hrs · 24,908 cycles

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

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 25,899 hrs · 24,908 cycles

CARGO DOOR BRACING BETWEEN FWD & AFT TRACKS HAS CRACKED ATTACH CLIP AT AFT LOWER CLIP WHERE IT ATTACHES TO FS 621 BULKHEAD. INSTALLED NEW SERVICEABLE ATTACH CLIP AT 621 BULKHEAD LOWER CARGO DOOR IAW SRM 51-42-21.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 25,899 hrs · 24,908 cycles

FRAME AT FS 349 IS CORRODED, BETWEEN STRINGER 26L & 27. R & R FS 349 FRAME PN 601R32005-69 & INTERCOSTAL BETWEEN 349 & 364 RT OF STRINGER 27 PN 601R31049-120 IAW SRM 51-40-11, 51-42-06 & 51-42-21.

Part: RING — CRACKED (TAIL PIPE) · airframe 25,899 hrs · 24,908 cycles

RIGHT TAIL PIPE FAIRING SECOND RING CRACKED. REPAIRED SECOND RING IAW CMM 78-11-00.

Part: UPLOCK — MALFUNCTIONED (RT MLG) · airframe 25,631 hrs · 24,659 cycles

AFTER TAKEOFF, GEAR SELECTED UP, RECEIVED GEAR DISAGREE MASTER WARNING FOR RT MLG & RT MLG SHOWED RED DASHES, APPROXIMATELY 5 SECONDS AFTER GEAR HANDLE UP, MANUAL RELEASE WAS USED. COMPLIED WITH QRH, LANDING WAS NORMAL, BRAKING WAS NORMAL & LANDED AT APPROXIMATELY 46800. COMPLIED WITH MEL 32-30-01 IAW 270423 2 FOR MEL.. R & R RT MLG UPLOCK IAW AWAC SUPP 08-067 & AMM 32-32-05, OPERATIONS CHECKED GOOD, REMOVED MEL & PLACARD SN OFF DCL351 96 & SN ON NGL0313/98.

Part: UNKNOWN — MALFUNCTIONED (RT MLG) · airframe 25,167 hrs · 24,202 cycles

3850, AFTER TO RECEIVED GEAR DISAGREE MESSAGE & RT GEAR SHOWED RED HASHES APPROXIMATELY 30 SECONDS AFTER GEAR WAS SELECTED UP. COMPLIED WITH QRH WITH GEAR HANDLE STILL SELECTED UP PULLED GEAR MANUAL RELEASE HANDLE. AT THAT TIME RECEIVED PARK BRAKE SOV, NOSE DOOR & INBD ANTISKID MESSAGES. UPON SELECTION OF GEAR HANDLE DOWN & MANUAL RELEASE LEVER TO NORMAL IAW THE QRH ALL MESSAGES CLEARED NAD ALL 3 GEAR INDICATED DOWN & LOCKED. LANDED WITHOUT INCIDENT. ACFT WT AT LANDING 47500, LANDING WAS SMOOTH. IAW 248038 2,3 RT MLG DID NOT RETRACT FULLY. COMPLIED WITH M ACTION PLACARD & PLACED LG RETRACTION SYS ON MEL MC RT GEAR NEVER MADE IT UP INTO THE LOCK FROM THE INDICATIONS.

Part: PITOT SYSTEM — CONTAMINATED (COCKPIT) · airframe 23,765 hrs · 22,824 cycles

ON T/O STBY AIRSPEED DID NOT MOVE FROM 0. ABORTED T/O AT 75KTS BTMS READS 6-4-4-5. PURGED P3 & S3 IAW AMM 34-11-00 OPS CHECK & LEAK CHECK GOOD.

Part: CONTACTOR — DEFECTIVE (ELECTRICAL SYS) · airframe 23,331 hrs · 22,394 cycles

AT CRUISE RECEIVED A/C ESS BUS CAUTION MSG MOMENTARY, CB PANEL 1 CB C2 POPPED A/C ESS BUS XFER TO AC BUSS 2 ALONG WITH A/C ESS ALTERNATE STAT MSG. AFTER 5 MINS RECEIVED A/C ESS BUS CAUTION AGAIN WITH CB PNL 2 CB C2 POPPED. REMOVED AND REPLACED UTIL BUS CONTACTOR 1 IAW AMM 24-51-23 AND AWAC SUPP 09-023 OPS CHECK GOOD.

Part: MOUNT BRACKET — CRACKED (PAX DOOR) · airframe 21,249 hrs · 20,396 cycles

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

Part: SKIN — CRACKED (CARGO DOOR) · airframe 21,249 hrs · 20,396 cycles

CARGO DOOR EXTERIOR SKIN CRACKED, FWD OF THE CARGO DOOR HANDLE CUT OUT. R & R CARGO DOOR HANDLE HSG ASSY. PN H3415-31.

Part: FLOOR SUPPORT — CORRODED (FS 618) · airframe 21,249 hrs · 20,396 cycles

FS 618, LBL 18, FLOOR SUPPORT CORRODED AROUND THE NUT PLATES CUT AWAY DAMAGED AREA AND INSTALLED SERVICEABLE. REPAIR IAW REO 601R-53-61-4468, REV.

Part: SKIN — CHAFED (LT NACELLE) · airframe 21,249 hrs · 20,396 cycles

LEFT UPPER CORE COWL HAS A CHAFED AREA, FWD LOWER CORNER CHAFE MARK IS APPROX 10" LONG. REPAIRED LT CORE COWL IAW REO 601R-71-12-4106.

Part: ATTACH BRACKET — CRACKED (FS 169) · airframe 21,249 hrs · 20,396 cycles

FWD ATTACH BRACKET CRACKED FOR UPPER BRAKE ACCUULATOR IN NOSE HYD COMP. REMOVED UNSERVICEABLE BRACKET AND INSTALLED SERVICEABLE BRACKET IAW SRM 51-42-21.

Part: FRAME — DAMAGED (FS 280) · airframe 21,249 hrs · 20,396 cycles

RT AFT SIDE FS 280 HAS DAMAGE FROM COMPARTMENT DOOR MAKING CONTACT WHEN OPENED IAW REO 601R-53-11-1727, REV E.

Part: CARGO TRACK — CORRODED (FS 559) · airframe 21,249 hrs · 20,396 cycles

CARGO TIE DOWN TRACK CORRODED AT FS 559+88 LBL 18. R & R TRACK.

Part: CARGO TRACK — CORRODED (FS 559) · airframe 21,249 hrs · 20,396 cycles

CARGO TIE DOWN TRACK CORRODED AT FS 559+88, RBL9. R & R CARGO TRACK.

Part: CARGO TRACK — CORRODED (FS 559) · airframe 21,249 hrs · 20,396 cycles

CARGO TIE DOWN TRACK CORRODED AT FS 559+88, LBL 18. R & R CARGO TRACK.

Part: FLOOR SUPPORT — CORRODED (FS 574-621) · corrosion level 2 · airframe 21,249 hrs · 20,396 cycles

CARGO BAY FLOOR SUPPORT CORROSION ON TOP AND UNDERNEATH FS 574 TO 621 AROUND NUT PLATES UPPER AND LOWER SURFACE. BLENDED AREAS ON FLOOR SUPPORT FOUND AREAS TO BE OUT OF LIMITS IAW SRM 53-00-00. REMOVED DAMAGE FLOOR SUPPORT AND REPLACED WITH SERVICEABLE FLOOR SUPPORT IAW REO 601R-53-61-640, REV D.

Part: CARGO TRACK — CORRODED (FS 559+88) · airframe 21,249 hrs · 20,396 cycles

CARGO TIE DOWN TRACK IS CORRODED AT FS 559+88, RBL 9. R & R TRACK.

Part: PANEL — CRACKED (PAX DOOR) · airframe 21,249 hrs · 20,396 cycles

PAX DOOR AFT SIDE PANEL CRACKED BETWEEN STEPS 3 & 4. INCORPORATED REPAIR TO PAX DOOR AFT SIDE PANEL ZONE 3. REPAIR TYPE II OF REO 601R-52-11-702, REV C, 2010-03-09.

Part: CARGO TRACK — CORRODED (FS 559) · airframe 21,249 hrs · 20,396 cycles

CARGO TRACK 559+88 CORRODED. R & R CARGO TIE DOWN TRACK IAW SRM 51-41-00, SRM 51-40-00, SRM 51-40-11, AMM 53-01-11.

Part: ANGLE — CRACKED (FS 484) · airframe 21,249 hrs · 20,396 cycles

LEFT FS 484.00, BL 27.0 CLIP CRACKED. REPAIRED LT FS 484.0, BL 27.0 CLIP BY INCOROPORATING REO 601R-53-41-059.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 21,249 hrs · 20,396 cycles

LEFT INBD FLAP VANE EDGE IS CRACKED IN 3 PLACES. REPAIRED OTBD AND MID CHAFED AREAS IAW REO 601R-57-52-004, REV C. REMOVED UNSERVICEABLE INBD SKIN AND INSTALLED SERVICEABLE INBD SKIN IAW SRM 51-42-13.

Part: SMOKE DETECTOR — FALSE ACTIVATION (CARGO BAY) · airframe 21,090 hrs · 20,237 cycles

CARGO SMOKE WARNING CAME ON JUST BEFORE V1. ABORTED TAKE OFF AT APPROX 120 KTS MAX BTMS READINGS 8,5, 4, 4. CARGO SMOKE WARNING EXTINGUISHED 10-20 SECONDS LATER. R & R FWD AND AFT SMOKE DETECTORS IN CARGO BAY IAW AMM 26-10-10. OPS CHECKED GOOD AT THIS TIME. HIGH ENERGY STOP INSPECTION NOT REQUIRED IAW AMM 05-51-27.

Part: PROXIMITY SWITCH — OUT OF ADJUST (PAX DOOR) · airframe 21,064 hrs · 20,209 cycles

CLIMBING THROUGH 12000 FT, PAX DOOR OUTER HANDLE CAUTION MESSAGE ILLUMINATED, COMPLIED WITH QRH, MESSAGE PERSISTED, UPON ARRIVAL DOOR COULD NOT BE OPENED FROM OUTSIDE ACFT. PERMORMED ADJUSTMENT OF PAX DOOR PROX SWITCH PS2MB IAW AMM 527004, OPS CHECKED GOOD.

Part: BPSU — FAILED (TE FLAPS) · airframe 20,556 hrs · 19,665 cycles

FLAP FAILED MESSAGE WHEN SELECTING FLAPS 20-30. COMPLIED WITH QRH AND LANDED UNEVENTFULLY. FOUND REPEAT SKEW DETECT SENSOR FAULTS ASSOCIATED JAMB AND RT BPSU CODES IN FECU IAW FIM 27-50. REPLACED RT WING BPSU IAW AMM 27-51. OPS CHECKED GOOD.

Part: DETECTION SYS — FALSE ACTIVATION (CARGO SMOKE) · airframe 20,547 hrs · 19,655 cycles

AFTER TAKEOFF, RECEIVED A CARGO SMOKE WARNING FOR APPORX 2 SECONDS. WARNING CLEARED AND DID NOT RETURN FOR REMAINDER OF FLIGHT. COMPLIED WITH OPS TEST OF CARGO SMOKE DETECTION SYS IAW 26-15-00. NO DEFECTS NOTED, OPS CHECKED GOOD.

Part: PROXIMITY SENSOR — FAILED (TE FLAPS) · airframe 20,486 hrs · 19,587 cycles

DURING ILS APPROACH, FLAPS FAILED AT 20 DEGREES WHEN FLAP LEVER SELECTED TO 30 DEGREES. PERFORMED QRH AND LANDED. DECLARED EMERGENCY LANDING, LANDING UNEVENTFUL. R & R PROXIMITY SENSORS, RH3 AND RH4.

Part: COUNTERBALANCE — OUT OF RIG (PAX DOOR) · airframe 19,653 hrs · 18,722 cycles

PAX DOOR HARD TO OPEN. PLACARDED AND PLACED ON MEL. TIGHTENED LWR LATCH FITTING, RIGGED COUNTER BALANCE, REPLACED PAX DOOR ACTUATOR.

Part: ANGLE — CRACKED (RT A/C PACK) · airframe 17,618 hrs · 16,590 cycles

RT PACK HAS CRACKED CLIP CROSS BEAM TO ORDER DUAL BYPASS VALVE MOUNT. REPLACED NR 2 PAC ANGLE CLIP AT CORSS BEAM (PN 601R95159-43).

Part: CROSSBEAM — CRACKED (AFT EQUIP BAY) · airframe 17,618 hrs · 16,590 cycles

LT PACK CROSSBEAM CRACKED OTBD END BELOW ACM REPLACED NR 1 PACK CROSSBEAM ATTACHING FRAME.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 17,618 hrs · 16,590 cycles

LT PACK ATTACHMENT CLIP CRACKED THRU FROM CROSS BEAM TO INNER SUPPORT FOR DUEL BYPASS VALVES. REPLACED NR1 PACK ANGLE CLIP AT CROSS BEAM (PN 601R59159-43).

Part: DOOR — BINDING (MAIN PAX) · airframe 17,018 hrs · 15,959 cycles

AT GATE - UNABLE TO OPEN MAIN CABIN DOOR FROM INSIDE. C/A IN PROGRESS.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 16,805 hrs · 15,739 cycles

AFT EQUIPMENT BAY RT SIDE AT FS 700 HAS A SUPPORT CLIP THAT IS CRACKED, THE TOP RIVET JUST BELOW PULLEY SHELF. R & R CLIP IAW SRM 51-42-06.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 1 · airframe 16,805 hrs · 15,739 cycles

RT NR 4 SEAT TRACK JUST FWD OF EMERGENCY EXIT. REMOVED MINOR CORROSION IAW SRM 55-41-49.

Part: FITTING — CORRODED (HORIZ STAB) · corrosion level 2 · airframe 16,805 hrs · 15,739 cycles

ANTI-ROTATION FITTING- 600-21073-7 HORIZ STABILIZER PIVOT PIN CORROSION WITH PITTING IN PIN NOTCHES. REPLACED ANTI AND ROTATION FITTING.

Part: FITTING — CHAFED (LT WING TE FLAP) · airframe 16,805 hrs · 15,739 cycles

LT OTBD FLAP ALIGNMENT ROLLER FITTING ON FLAP IS CHAFED REO 601R-57-53-794.

Part: FITTING — CHAFED (LT WING) · airframe 16,805 hrs · 15,739 cycles

LT OTBD ALIGNMENT FITTING ON WING IS CHAFED, REO 601R-57-51-143.

Part: SKIN — CHAFED (RUDDER) · airframe 16,805 hrs · 15,739 cycles

RUDDER L/E HAS CHAFE DAMAGE ALONG LENGTH OF RUDDER RT SIDE BLENDED RUDDER L/E BETWEEN 98.75 AND 151.508 AND FOUND TO BE SERVICEABLE IAW SRM 55-40-00. AREA BETWEEN 40.458 AND 81.50. R & R IAW SRM 51-42-06.

Part: SKIN — CHAFED (RUDDER) · airframe 16,805 hrs · 15,739 cycles

RUDDER L/E HAS CHAFING DAMAGE ON LT SIDE ALONG LENGTH OF RUDDER R & R CHAFED L/E IAW SRM 51-42-06.

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 16,805 hrs · 15,739 cycles

RT WING INBD FLAP VANE SKIN CHAFED FROM 11B STRAP R & R INBD FLAP SKIN IAW SRM 51-42-10.

Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 16,805 hrs · 15,739 cycles

LT INBD FLAP VANE CHAFED IN 3 AREAS ON L/E VANE REPAIRED DAMAGE IAW REO 601R-57-52-004, REV C.

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 16,805 hrs · 15,739 cycles

RT WING INBD FLAP VANE SKIN HAS CHAFING FROM OTBD STOP REPAIRED DAMAGE IAW REO 601R-51-52-004, REV C.

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 16,805 hrs · 15,739 cycles

RT WING INBD FLAP VANE SKIN CHAFING FROM CENTER STOP. REMOVED DAMAGE WITH MATERIAL LOSS OF .006" WITHIN LIMITS IAW REO 601R-57-52-004, REV C.

Part: FRAME — MISINSTALLED (BS 640) · airframe 16,805 hrs · 15,739 cycles

EO E06/012/453. ENGINE SUPPORT BEAM PREVIOUSLY REINFORCED BY DETACHING THE BEAM FROM FS 640. DAMAGE ASSESSMENT SENT TO MFG FOR REO. EXISTING DAMAGE - LARGE HOLE 0.264", BETWEEN STRINGER 9R AND STR 10R, FOUND WHILE PERFORMING SB A601-53-059. ENGINE BEAM DISCONNECT.

Part: FITTING — CRACKED (FUSELAGE) · corrosion level 1 · airframe 16,805 hrs · 15,739 cycles

(2 EA) ANGLE CLIPS AT FS 319.00 AND (2 EA) ANGLE CLIPS AT FS 338.00 CORRODED. FABRICATED NEW ANGLES OUT OF 7075 0.063 AND INSTALLED.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 16,805 hrs · 15,739 cycles

DURING VISUAL INSPECTION FOUND LBL 9 ANGLE OTBD SIDE CRACKED FROM BOTTOM RIVET TO EDGE OF ANGLE. REPAIRED BY INCORP OF REO`S 601R-53-41-260, REV D & 601R-53-41-609, REV B.

Part: ENGINE — SMOKE (RIGHT) · airframe 16,970 hrs · 15,910 cycles

NOTICEABLE SMOKE DISCHARGE FROM TAILPIPE OF RT ENGINE. APPROX 2 MINUTES AFTER ENGINE SHUTDOWN. RAN ENGINE SEVERAL TIMES, 10 MINUTES APART. SHUTDOWN ENGINE, WAITED 2 MINUTES. NO NOTABLE SMOKE DISCHARGE FROM TAIL PIPE. OPS CHECKS GOOD IAW AMM 72-00-00. ADDED 2 PTS OF OIL TO RT AND LT ENGINES.

Part: CONTROL UNIT — MALFUNCTIONED (TE FLAPS) · airframe 15,135 hrs · 14,073 cycles

FLAP FAIL AT 3000 FT INBOUND TO HPN DIVERTED. PERFORMED FLAP RESET PROCEEDURE IAW SUP 98-18C-AMOC BOX 6. FLAPS RESET. ACFT RELEASED FOR SERVICE. FLAP FAIL DEFERAL IAW MEL 27-50-01. PLACARDED AND PLACED ON MEL REF 206261/1 FLAP FAIL DEFERAL IAW MEL 27-50-01. PLACARDED AND PLACED ON MEL REF 206261/2. REMOVED AND REPLACED FECU DUE TO FAULT CODE 33BC BITE TEST FAILURE IAW AMM 27-51-05, REMOVED FROM MEL. (K)

Part: PDU — MALFUNCTIONED (TE FLAP) · airframe 14,145 hrs · 13,106 cycles

FLAPS FAIL AT ZERO AFTER TAKEOFF. REMOVED AND REPAIRED LT BPSU, NO HELP, RIGGED FLAPS, CHANGED PDU OPS CK GOOD. FLAP SYS OPS CK GOOD. (K)

Part: ACTUATOR — FAILED (TE FLAPS) · airframe 13,948 hrs · 12,915 cycles

ON APPROACH, FLAPS FAIL CAUTION MSG. FLAPS STUCK AT ZERO DEGREES. C/W QRH, AIR DIVERSION. LANDED OK, NORMAL BRAKING. REMOVED AND REPLACED FLAP ACTUATORS.

Part: ACTUATOR — FAILED (TE FLAPS) · airframe 13,948 hrs · 12,915 cycles

LOG 196278/2 - ON APPROACH, FLAPS FAIL CAUTION MSG. FLAPS STUCK AT ZERO DEGREES. C/W QRH, AIR DIVERSION. LANDED OK, NORMAL BRAKING. REMOVED AND REPLACED FLAP ACTUATORS. LH1 PN 852D100-21, SN 4867 (10,780 FH), LH2 PN 852D10021, SN 6782 (3,250 FH), LH3 PN 601R93103-19, SN 3982 (3250 FH), RH2 PN 852D10019, SN 4418 (10530 FH), RH3 PN 853D100-20, SN 2429 (12,559 FH), RH4 PN 854D11-20, SN 3805 (3250 FH).

Part: ACTUATOR — FAILED (TE FLAP)

LOG 196278/2 - ON APPROACH, FLAPS FAIL CAUTION MSG. FLAPS STUCK AT ZERO DEGREES. C/W QRH, AIR DIVERSION. LANDED OK, NORMAL BRAKING. REMOVED AND REPLACED FLAP ACTUATORS.

Part: ACTUATOR — FAILED (TE FLAP) · airframe 13,948 hrs · 12,915 cycles

LOG 196278/2 - ON APPROACH, FLAPS FAIL CAUTION MSG. FLAPS STUCK AT ZERO DEGREES. C/W QRH, AIR DIVERSION. LANDED OK, NORMAL BRAKING. REMOVED AND REPLACED FLAP ACTUATORS.

Part: ACTUATOR — FAILED (TE FLAPS)

LOG 196278/2 - ON APPROACH, FLAPS FAIL CAUTION MSG. FLAPS STUCK AT ZERO DEGREES. C/W QRH, AIR DIVERSION. LANDED OK, NORMAL BRAKING. REMOVED AND REPLACED FLAP ACTUATORS.

Part: ACTUATOR — FAILED (TE FLAP) · airframe 13,948 hrs · 12,915 cycles

LOG 196278/2 - ON APPROACH, FLAPS FAIL CAUTION MSG. FLAPS STUCK AT ZERO DEGREES. C/W QRH, AIR DIVERSION. LANDED OK, NORMAL BRAKING. REMOVED AND REPLACED FLAP ACTUATORS. LH1 PN 852D100-21, SN 4867 (10,780 FH), LH2 PN 852D10021, SN 6782 (3,250 FH), LH3 PN 601R93103-19, SN 3982 (3250 FH), RH2 PN 852D10019, SN 4418 (10530 FH), RH3 PN 853D100-20, SN 2429 (12,559 FH), RH4 PN 854D11-20, SN 3805 (3250 FH).

Part: LANDING GEAR — UNKNOWN (NLG & MLG) · airframe 13,189 hrs · 12,209 cycles

ON GEAR RETRACTION, GEAR DISAGREE WARNING MESSAGE. SUSPECT NOSE GEAR FAULT. LANDED AT 41,000 LBS AND BRAKING WAS NORMAL. SERVICED MLG AND NLG IAW AMM 12-12-32, PERFORMED GEAR EXTENSION AND RETRACTION CHECK AS REQUIRED. OPS CHECK GOOD. (K)

Part: BULKHEAD — CRACKED (BS 621) · airframe 12,177 hrs · 11,224 cycles

REAR PRESSURE BULKHEAD WEB CRACK FS 621 LBL 45 BTWN WL 106.17 AND WL (LINTEL ATTACHMENT FITTING). REAR PRESSURE BULKHEAD WEB FS 621 LBL 45 BTWN WL 106.17 AND WL 113.33 REPAIRED IAW REO 601R-53-61-1230 REV D.

Part: PLATE — CORRODED (BS 574-621) · corrosion level 1 · airframe 12,177 hrs · 11,224 cycles

CORROSION ON FLOOR LANDING PLATE AROUND NUT PLATES HOLES BTWN FS 574 TO FS 621 AND AT LBL 44. CORROSION REMOVED ON FLOOR LANDING PLATE AROUND NUT PLATES HOLES BTWN FS 574 TO FS 621 AND AT LBL 44 IAW SRM 51-21-06.

Part: BULKHEAD — DENTED (BS 280) · airframe 12,177 hrs · 11,224 cycles

DENT EXIST ON FLIGHT COMPARTMENT BULKHEAD FS 280 RBL 9 WL 93.0 FLIGHT COMPARTMENT BULKHEAD REPAIRED IAW REO 601R-53-11-1376.

Part: CHANNEL — CRACKED (BS 574) · airframe 12,177 hrs · 11,224 cycles

CHANNEL CRACK AT FS 574 FWD TRACK OF CARGO DOOR. CRACKED CHANNEL REPLACED IAW SRM 51-42-06.

Part: HINGE — CRACKED (CARGO DOOR) · airframe 12,177 hrs · 11,224 cycles

CARGO DOOR STEP PLATE ONE HINGE CRACKED (FWD). CARGO DOOR STEP PLATE ONE HINGE (FWD) REPLACED IAW SRM 51-42-06. .

Part: INTERCOSTAL — CRACKED (BS 484) · airframe 12,177 hrs · 11,224 cycles

CRACK FOUND AT FS 484 LBL 36 WL 72. (M) INTERCOSTAL REPAIRED AT FS 484, LBL 36, WL 72 IAW REO 601R-53-41-059 REV A.

Part: INTERCOSTAL — CRACKED (BS 484) · airframe 12,177 hrs · 11,224 cycles

CRACK FOUND AT FS 484 RBL 36 WL 72. - - INTERCOSTAL REPAIRED AT FS 484, RBL 36, WL 72 IAW REO 601R-53-41-059 REV A. (S)

Part: BRACKET — CRACKED (BS 621) · airframe 12,177 hrs · 11,224 cycles

BRACKET CRACKED ON BULKHEAD AT FS 621 WL 107 (CRACK LENGTH .500") BRACKET FABRICATED AS PER SAMPLE AND REPLACED AT FS 621 WL 107 IAW SRM 51-42-21.

Part: STRUCTURE — CRACKED (BS 325-334) · airframe 12,177 hrs · 11,224 cycles

CRACK EXIST ON PASSENGER DOOR EDGE MEMBER. PAX DOOR CRACKS REPAIRED IAW REO 601R-52-11-279.

Part: FLOORBEAM — CRACKED (BS 605) · airframe 12,177 hrs · 11,224 cycles

FLOOR LANDING PLATE CRACKED AT FS 605, LBL 43. DAMAGE CUTOUT, NDT PERFORMED ON CUTOUT, REDUNDANT HOLE PLUGGED IAW REO 601R-53-61-433.

Part: SILL — CRACKED (BS 574) · airframe 12,177 hrs · 11,224 cycles

CARGO BAY FLOOR SILL CRACKED APPROX .200 IN AT FS 574. REPAIRED IAW CRJ 200 REO 601R-53-61-1741. (M)

Part: PLATE — CRACKED (BS 605) · airframe 12,177 hrs · 11,224 cycles

FLOOR LANDING PLATE CRACKED AT FS 605, LBL 42. - - DAMAGE CUTOUT, NDT PERFORMED ON CUTOUT, REDUNDANT HOLE PLUGGED IAW REO 601R-53-61-433. .

Part: FRAME — CRACKED (BS 280) · airframe 12,177 hrs · 11,224 cycles

CRACK FOUND ON FRAME FS 280 RBL 9 WL 73. FRAME AT FS 280, RBL 9, WL 73 REPAIRED IAW RWO 601R-53-11-171 REV "D" SCHEME "B". .

Part: FRAME — CRACKED (BS 280) · airframe 12,177 hrs · 11,224 cycles

CRACK FOUND ON FRAME 280, LBL 9 WL 73.00. - - FRAME AT FS 280 LBL 9 WL 73.00 REPAIRED IAW REO 601R-53-11-171 REV "D" SCHEME B. .

Part: BULKHEAD — CRACKED (BS 202) · airframe 12,177 hrs · 11,224 cycles

CRACK FOUND ON PRESSURE BULKHEAD FS 202.75 LBL 23.71 AROUND PARKING BRAKE. CRACK PRESSURE BULKHEAD REPAIRED IAW REO 601R-53-11-563.

Part: FLAP SYSTEM — FAILED (TE FLAPS)

WHILE IN FLIGHT, FLAPS FAILED AT ZERO WHILE ATTEMPTING TO EXTEND. LANDED FLAPS AT ZERO. NORMAL BRAKING ACTION. BRAKE TEMPS READ 5, 5, 5, 6. RESET PER AMM SUPPLEMENT 98-018A. PLACED ON 72 FLAP WATCH. (M) COMPLIED WITH AMM SUPPLEMENT 98-018A, NO FURTHER INCIDENT. (K)

Part: FLAP SYSTEM — UNKNOWN (TE FLAPS)

FLAPS FAIL YELLOW CAUTION MESSAGE IN FLIGHT. LANDED AT FLAPS ZERO. (M)

Part: PSEU — UNKNOWN (DOOR WARNING)

SERVICE DOOR CAUTION MESSAGE IN FLIGHT. CAME ON AT ABOUT 1000 AGL, THEN EXTINGUISHED, AND CAME ON AGAIN AT ABOUT 5 TO 7000 FEET INDICATED MSL. INSPECTED SERVICE DOOR, NO DAMAGE OR DEFECTS NOTED. PRESSURIZED AIRCRAFT TO 4.0 PSI, NO FAULTS FOUND. INTERCHANGED PSEU AND FOUND CODE D122 REF CRJ MM 52-70-01. (M)

Part: SWITCH — MALFUNCTIONED (TRIM ACTUATOR)

STAB TRIM 1 AND 2 DISENGAGED INFLIGHT DURING MANUAL TRIM ACTUATIONS. REMOVED AND REPLACED CAPT TRIM DISCONNECT SWITCH AFTER TESTING IAW AWAC SUPPLEMENT NR 05-029. WORK PERFORMED IAW CRJ AMM 27-4, OPS CHECK GOOD. (M)

Part: SOLENOID VALVE — MALFUNCTIONED (NLG)

ON DEPARTURE FROM BNA FLT 3818, STEERING INOPERATIVE CAUTION MESSAGE ILLUMINATED, COMPLIED WITH QRH, NO FURTHER ACTION. EMERGENCY LANDING DECLARED BY CREW. REMOVED AND REPLACED NOSEWHEEL STEERING SELECTOR VALVE IAW CRJ AMM 32-51-25. OPS AND LEAK CHECK GOOD. PERFORMED GEAR SWING IAW AMM 32-30-00, OPS CHECK GOOD. (M)

Part: ANCHOR — CRACKED (PAX DOOR)

PAX DOOR AFT CABLE ANCHOR ASSY, P/N 601R380741-3 IS CRACKED, APPROX 1.5 INCH IN LENGTH. REMOVED AND REPLACED AFT COUNTERBALANCE ASSY ANCHOR FITTING WITH NEW P/N 601R31976-1, IAW CRJ-200 AMM 52-11-17 AND SB 601R-52-116 REV C. (M)

Part: DRAG ANGLE — CRACKED (FUSELAGE)

PAX DOOR AFT DRAG ANGLE CRACKED AT PULLEY BRACKET APPROX 7 INCHES LONG. REPAIRED PAX DOOR AFT DRAG ANGLE IAW BOMBARDIER REO 601R-52-11-513 REV A. (M)

Part: RIB — CRACKED (LWS 53)

FOUND LT WS 53.60 BATT RIB ASSEMBLY HAS A .5 INCH CRACK AT TOP CORNER. REPAIRED BATTERY RIB BY REMOVING DAMAGED AREA AND INSTALLING REPAIR ANGLE DOUBLE AND FILLER IAW BOMBARDIER REO 601R-57-51-046 REV B. (M)

Part: INTERCOSTAL — CRACKED (BS 621-625 S14L)

FOUND LEFT SIDE FS 621 TO FS 625.3 INTERCOSTAL AT STRINGER 14L IS CRACKED NEAR RADIUS APPROX 1.0 INCH LONG. REMOVED AND INSTALLED NEW LEFT INTERCOSTAL, P/N 601-35012-51, AT FS 621 TO 625.3, STRINGER 14L, IAW CRJ-200 SRM 51-42-06. (M)

Part: INTERCOSTAL — CRACKED (FUSELAGE)

FOUND RT SIDE FS 621 TO FS 625.3 INTERCOSTAL AT STRINGER 14R IS CRACKED NEAR RADIUS APPROX 1.1 INCH LONG. REMOVED AND INSTALLED NEW INTERCOSTAL P/N 601-35012-52 AT FS 621 TO FS 625.3, STRINGER 14R, IAW CRJ-200 SRM 51-42-06. (M)

Part: LINE — CHAFED (APU FUEL SYS)

SMELL STRONG FUEL ODOR IN CABIN. REMOVED AND REPLACED CHAFED LINE FROM FUEL SOLENOID TO APU BURNER CAN. REMOVED AND REPLACED AIR PACK COALESCER SOCKS, RAN ENGINES AIRCRAFT OK FOR SERVICE. (M)

Part: FLOORBEAM — CRACKED (FUSELAGE)

THE LT AND RT SIDE UNDER FLOORBEAM STRUCTURE IS CRACKED AT FSL73, LBL40 AND RBL40. REMOVED CRACKED AREA AND INSTALLED REPAIR PARTS IAW REO.

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY)

SMOKE TOILET CAS MESSAGE ON TAXI, COMPLIED WITH QRH. FIRE DEPARTMENT INSPECTED LAV, NO EVIDENCE OF SMOKE OR FIRE. INSTALLED SMOKE DETECTOR AFT LAV, TESTED OK. REMOVED FROM MEL. (M)

Part: ENGINE — MALFUNCTIONED (NR 2)

ABORTED TAKEOFF, 140 KNOTS NR 2 ENGINE N2 DROPPED OFF TO APPROX 50-60 PERCENT. ON TAKEOFF ROLL, BRAKE MAX TEMPS WERE 11, 9, 7, 8 ABORTED TAKEOFF, TAKEOFF AT 1655Z MARKED FDR AT 1704Z. PERFORMED ACCELERATION/DECELERATION CHECKS AND POWER ASSURANCE CHECKS, NO DEFECTS NOTED. COULD NOT DUPLICATE. INSPECTED TIRES AND BRAKES AS PER AMM 05-51-29, OK FOR SERVICE. (M)