N685BR

Part: FLOORBEAM — CRACKED (BS 280) · airframe 32,013 hrs · 30,434 cycles

FS280 LBL9, I/B CLIP IS CRACKED. REMOVED CRACKED ANGLE AND INSTALLED NEW ANGLE(FABRICATED) IAW CRJ200 SRM 51-24-16 AND RESTORED TO ORIG FINISH IAW CRJ 200 SRM 51-21-11, 51-25-16, 51-25-06

Part: FLOORBEAM — CORRODED (BS 280) · airframe 32,013 hrs · 30,434 cycles

FS280 HAS CORROSION AT AFT ANGLE. REMOVED CORRODED AFT ANGLE AND REPLACED WITH NEW ANGLE. IAW CRJ 200 SRM 51-42-21 AND 51-42-06 AND RESTORES TO ORIG FINISH IAW CRJ 200 SRM 53-00-00

Part: FLOORBEAM — CRACKED (BS 280) · airframe 32,013 hrs · 30,434 cycles

FS280 RBL9, I/B, O/B CLIPS CRACKED AT FWD AND AFT FLOOR. REMOVED CRACKED CLIPS AND REPLACED WITH NEW FABRICATED CLIPS. IAW 53-21-43 AND 51-24-16

Part: RIB — CRACKED (LT WING) · airframe 32,013 hrs · 30,434 cycles

BATT RIB IS CRACKED ABOVE THE UPPER RIVET AT L/H WS 53.60. REPAIRED BATT RIB IAW BOMBA REO 601R-57-51-046 REV B REPAIR TYPE 2

Part: RIB — CRACKED (RT WING) · airframe 32,013 hrs · 30,434 cycles

BATT RIB IS CRACKED ABOVE THE UPPER RIVET AT R/H WS 53.60. REPAIRED BATT RIB IAW BOMBA REO 601R-57-51-046 REV B REPAIR TYPE 2

Part: FRAME — CORRODED (BS 605) · airframe 32,013 hrs · 30,434 cycles

FS605 FRAME CORRODED UNDER CARGO FLOOR PANEL 281 DLF. REMOVED CORROSION ON FRAME 605 AND FOUNT TO BE OUT OF LIMITS IAW CRJ200 SRM53-00-00 REPAIRED FS605 FRAME UNDER CARGO FLOOR PANEL 281 DLF IAW EA#CRJ253-11320

Part: HANDLE — FAILED (MLG) · airframe 29,991 hrs · 28,142 cycles

AFTER TAKEOFF THE LANDING GEAR WON`T RETRACT WITH THE LANDING GEAR LEVER IN THE UP POSITION. SHORTLY AFTER PARK BRAKE SOV? AND A/SKID INBD? CAUTION MESSAGES. RETURNED TO FIELD. (FLT#3500) REMOVED AND REPLACED LANDING GEAR CONTROL HANDLE ASSEMBLY IAW AMM. PERFORMED MULTIPLE SUCCESSFUL FUNCTIONAL TESTS OF THE EXTENSION AND RETRACTION SYSTEM IAW AMM. FUNCTIONAL TEST GOOD. NO FURTHER DEFECTS NOTED.

Part: CONTROL HANDLE — FAILED (MLG) · airframe 29,983 hrs · 28,135 cycles

AFTER TAKEOFF. ANTI SKI INBOARD CAUTION; PARKING BRAKE SOV CAUTION, AND A GEAR DISAGREE WARNING MESSAGE. AFTER RUNNING THE QRH, THE GEAR RETRACTED. (FLT#3951) REMOVED AND REPLACED LANDING GEAR HANDLE ASSY IAW AMM. OPS CHECK GOOD NO FURTHER FAULTS FOUND A/C OK FOR SERVICE.

Part: ACCUMULATOR — FAILED (HYD SYSTEM) · airframe 29,960 hrs · 28,110 cycles

AFTER TAKEOFF GEAR DISAGREE MESSAGE. BEFORE WE COULD RUN THE QRH, THE CHECKLIST MESSAGE WENT AWAY AND GEAR CAME UP AND LOCKED. (FLT#3997) REMOVED AND REPLACED HYDRAULIC 3 ACCUMULATOR IAW AMM. EXTENSION/RETRACTION TESTS GOOD IAW AMM.

Part: HYDRAULIC SYSTEM — CONTAMINATED (NR 3) · airframe 29,891 hrs · 28,041 cycles

UPON TAKEOFF RECEIVED A HYD 3 LO PRESS CAUTION MESSAGE FOLLOWED BY A GEAR DISAGREE WARNING MESSAGE WITH THE LANDING GEAR HANDLE SELECTED IN THE €ŒUP€? POSITION. COMPLIED WITH QRH AND RETURNED TO FIELD FOR A NORMAL LANDING. (FLT 4981) CLOSED INSPECTED AND FOUND NR 3 HYDRAULIC SYSTEM AT 100%. AFTER PURGING AIR FROM NR 3 HYDRAULIC SYSTEM FOUND LEVEL TO BE AT 40%. SERVICED NR 3 HYDRAULIC SYSTEM REFERENCE IAW AMM. PERFORMED OPS CHECK OF GEAR EXTENTION/RETRACTION SYSTEM IAW AMM. OPS CHECK GOOD. PERFORMED OPS CHECK OF NR 3 HYDRAULIC SYSTEM PRESSURE INDICATIONS IAW AMM. OPS CHECK GOOD.

Part: LANDING GEAR — WARNING LIGHT · airframe 29,323 hrs · 27,412 cycles

GEAR DISAGREE WARNING MESSAGE DURING GO AROUND ON APPROACH, INITIATED AFTER MICROBURSTS ON THE FIELD. GEAR WAS NEVER SELECTED UP AND NOTICED THIS AT 230KTS, AFTER WHICH GEAR HANDLE WAS SELECTED UP, CAUSING THE MESSAGE. GEAR RETRACTED AS AIRPLANE SLOWED THROUGH APPROXIMATELY 220 KTS. (FLT#4705) CLOSED PERFORMED SEVERAL OPS CHECKS OF THE LANDING GEAR EXTENSION AND RETRACTION IAW AMM. COULD NOT DUPLICATE. OPS CHECK GOOD AT THIS TIME.

Part: NOT REPORTED — DENTED (FUSELAGE) · airframe 29,049 hrs · 27,114 cycles

DENT AT FS559.00+16 BETWEEN STRINGERS 15R AND 16R. (C-CHECK) RO: 08/01/2018 DRESSED DENT DAMAGE BACK TO ORIGINAL CONTOUR IAW REO.

Part: SKIN — DENTED (FUSELAGE) · airframe 29,049 hrs · 27,114 cycles

DENT AT FS409.00+18.5 STR24L ON EXTERIOR SKIN. (C-CHECK) RO: 08/01/2018 REPAIRED DENT AT FS409.00+18.5 STR 24L IAW SRM. ALL CHECKS GOOD.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 29,049 hrs · 27,114 cycles

PASSENGER DOOR INTERCOSTAL DD6 HAS CORROSION BETWEEN FS338 AND FS347. (C-CHECK) RO: 08/01/2018 REMOVED AND REPLACED PAX DOOR INTERCOSTAL DD6 IAW SRM. PRESSURE LEAK CHK GOOD.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 29,049 hrs · 27,114 cycles

PASSENGER DOOR INTERCOSTAL DD7 HAS CORROSION BETWEEN FS338 AND FS347. (C-CHECK) RO: 08/01/2018 REMOVED AND REPLACED PASSENGER DOOR INTERCOSTAL DD7 BETWEEN FS338 AND FS347 IAW SRM. ALL CHECKS GOOD.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 29,049 hrs · 27,114 cycles

PASSENGER DOOR INTERCOSTAL DD7 HAS CORROSION BETWEEN FS311 AND FS320. (C-CHECK) RO: 08/01/2018 REMOVED AND REPLACED PAX DOOR INTERCOSTAL DD7 IAW SRM. PRESSURE LEAK CHECK GOOD.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 29,049 hrs · 27,114 cycles

PASSENGER DOOR INTERCOSTAL DD4 HAS CORROSION BETWEEN FS320 AND FS338. (C-CHECK) RO: 08/01/2018 REMOVED & REPLACED PAX DOOR INTERCOSTAL DD4 IAW SRM. PRESSURE LEAK CHECK GOOD.

Part: VANE — CHAFED (TE FLAP) · airframe 29,049 hrs · 27,114 cycles

REPLACE THE RT INBD FLAP CENTER VANE CAP. (C-CHECK) RO: 08/01/2018 REPLACED RT INBD FLAP CENTER VANE CAP WITH NEW PART IAW SRM.

Part: SKIN — DENTED (TE FLAP) · airframe 29,049 hrs · 27,114 cycles

RIGHT WING INBOARD FLAP, DENT ON LOWER SKIN NEAR TRAILING EDGE APPROXIMATE WS72.00. (C-CHECK) RO: 08/01/2018 REPAIRED THE RIGHT HAND INBOARD FLAP LOWER SKIN AT WS 72.00 IAW SRM.

Part: VANE — CHAFED (TE FLAP) · airframe 29,049 hrs · 27,114 cycles

RT SIDE INBOARD FLAP( VANE) HAS CHAFING WEAR AT INBOARD, CENTER, AND OUTBOARD LEADING EDGE SECTION OF FLAP VANE. (C-CHECK) RO: 08/01/2018 REMOVED DAMAGE FROM INBD FLAP VANE CAPS IAW REO.

Part: SKIN — CHAFED (RT AILERON) · airframe 29,049 hrs · 27,114 cycles

RIGHT AILERON, BOTH LOWER SKIN SHROUDS ARE CHAFED. AILERON STATIONS 323.843, 329.875 & 370.031, 375.857. (C-CHECK) RO: 08/01/2018 REMOVED AND REPLACED RT AILERON LOWER SHROUDS (INB AND OUTB) IAW SRM.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 29,049 hrs · 27,114 cycles

PASSENGER DOOR CORROSION ON THE DD6 INTERCOSTAL. (C-CHECK) RO: 08/01/2018 REMOVED AND REPLACED PASSENGER DOOR INTERCOSTAL DD6 IAW SRM. ALL CHECKS GOOD.

Part: DOWNLOCK SENSOR — FAILED (NLG) · airframe 28,203 hrs · 26,192 cycles

RECEIVED NOSE DOOR WARNING ALONG WITH GEAR DISAGREE. COMPLIED WITH QRH ALL THREE GEAR DOWN AND GREEN. RETURNED TO FIELD. DID NOT DECLARE EMERGENCY. (FLT 4584) REMOVED AND REPLACED THE NLG DOWNLOCK NR 2 SENSOR AND HARNESS ASSY IAW AMM. REMOVED AND REPLACED THE NLG SHOCK STRUT ASSY IAW AMM. SYSTEM OPS CHECK AND LEAK CHECK GOOD.

Part: SKIN — DENTED (BS 672) · airframe 25,737 hrs · 23,453 cycles

FUSELAGE DENT AFT OF 10TH STAGE GROUND BLEED AIR SUPPLY DOOR AT BS 672 AND STRINGER 20L. COLD WORKED AND HAND DRESSED OUT DENT BACK TO ORIGINAL CONTOUR IAW EA.

Part: FLOOR SUPPORT — CORRODED (BS 349-356) · airframe 25,737 hrs · 23,453 cycles

RT FLOOR SUPPORT AFT OF BS 349 HAS EVIDENCE OF CORROSION BS 349 TO 356. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM AND REO.

Part: FLOOR SUPPORT — CORRODED (BS 559-621) · airframe 25,737 hrs · 23,453 cycles

LEFT CARGO FLOOR EDGE MEMBER HAS CORROSION AT THE NUT-PLATE LOCATIONS FROM BS 621 TO 559+80. REPLACED IAW REO.

Part: ANGLE — CORRODED (PAX DOOR SILL) · airframe 25,737 hrs · 23,453 cycles

PASSENGER DOOR LOWER SILL LONGERON VERTICAL LEG HAS EVIDENCE OF CORROSION AROUND SEVERAL NUT PLATE AND GROUND STUD LOCATIONS. REPLACED PAX DOOR SILL FLOOR SUPPORT ANGLE IAW SRM. ALL OP CHECKED GOOD.

Part: WEB — CORRODED (PAX DOOR STAIR) · airframe 25,737 hrs · 23,453 cycles

PAX DOOR, THE AFT FIXED STAIR WEB/PANEL HAS SEVERAL SPOTS OF CORROSION. REPAIRED THE STAIR WEB IAW EA.

Part: WEB — CORRODED (PAX DOOR STAIR) · airframe 25,737 hrs · 23,453 cycles

PAX DOOR, THE FWD FIXED STAIR WEB PANEL HAS SEVERAL SPOTS OF CORROSION. REPAIRED THE PAX DOOR WEB IAW STS EA.

Part: FCU — UNKNOWN (LT ENGINE) · airframe 22,146 hrs · 19,811 cycles

LEFT ENGINE SHUTDOWN ON DESCENT. COMPLIED WITH QRH AND LANDED NORMALLY. R & R LEFT ENGINE FUEL PUMP AND FUEL CONTROL. LEAK AND OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,866 hrs · 19,540 cycles

LEFT LOWER EMERGENCY EXIT LIGHT INOPERATIVE. R & R LT LOWER EMERGENCY EXIT LIGHT AND INVERTER IAW AMM.

Part: WEB — CRACKED · airframe 21,834 hrs · 19,506 cycles

VISUAL INSPECTION OF THE ESB, LOWER WEB, CRACK FOUND AT LBL 11.0 AFT EDGE CRACK IS GOING THROUGH RIVET. C-CHECK, COMPLIED WITH PERMANENT REPAIR FOR CRACK ON ESB LOWER WEB AT LBL 11.0, AFT EDGE, IAW REO.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 21,834 hrs · 19,506 cycles

RT SEAT TRACK AT RBL 9, BS 559 +3 TO 559 +85 CORRODED. C-CHECK, R & R SEAT TRACK IAW AMM.

Part: SEAT TRACK — CORRODED (BS 559-570) · airframe 21,834 hrs · 19,506 cycles

RT SEAT TRACK AT RBL 9 BS 559 + 109 -- 570 CORRODED. C-CHECK, R & R SEAT TRACK IAW AMM.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 21,834 hrs · 19,506 cycles

RIGHT SEAT TRACK AT RBL 9 BS 559 + 85 - 559 + 96 HAS CORROSION. C-CHECK R & R SEAT TRACK IAW AMM.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 21,834 hrs · 19,506 cycles

LEFT SEAT TRACK AT LBL 9 BS 559 + 109 - 570 CORRODED. R & R SEAT TRACK IAW AMM.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 21,834 hrs · 19,506 cycles

LEFT SEAT TRACK AT LBL 9, BS 559 + 85 - 559 + 96 CORRODED. R & R SEAT TRACK IAW AMM.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 21,834 hrs · 19,506 cycles

RT SEAT TRACK AT RBL 27 BS 559 + 78 - 559 + 96 CORRODED. C-CHECK R & R SEAT TRACK IAW AMM.

Part: SKIN — CORRODED (LT WING) · airframe 21,834 hrs · 19,506 cycles

LEFT WING PLANK THRU FUEL ACCESS PANEL 540BB, PITTING CORROSION SOME AREAS. BLENDED DAMAGED AREA AND REMOVED CORROSION IAW REO.

Part: HINGE — GOUGED (PAX DOOR) · airframe 21,834 hrs · 19,506 cycles

PAX DOOR HINGE, FUSELAGE SIDE, HAS GOUGE ON HINGE LUG, 7TH BACK FROM FRONT. C-CHECK, REPAIRED PAX DOOR HINGE, FUSELAGE SIDE HINGE LUG, 7TH BACK FROM FRONT IAW REO.

Part: CONNECTING ROD — GOUGED (LT MLG DOOR) · airframe 21,834 hrs · 19,506 cycles

LEFT MLG DOOR CONNECTING ROD, THE INBD END AT THE HEIM BALL, THE FWD SIDE IS GOUGED. C-CHECK, REPAIRED GOUGING DAMAGE ON LT MLG DOOR CONNECTING ROD IAW REO.

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 21,834 hrs · 19,506 cycles

FLAP VANE SKIN, RT SIDE HAS CHAFING MARK AT L/E INBD SIDE. C-CHECK, REPAIRED FLAP VANE SKIN, RT SIDE, IAW SRM AND REO.

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 21,834 hrs · 19,506 cycles

FLAP VANE SKIN, RT SIDE HAS CHAFING MARK AT L/E OTBD SIDE. C-CHECK, REPAIRED FLAP VANE SKIN, RT SIDE, IAW SRM AND REO.

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 21,834 hrs · 19,506 cycles

FLAP VANE SKIN, RT SIDE HAS CHAFING MARK AT L/E CENTER SIDE. C-CHECK, REPAIRED FLAP VANE SKIN, RT SIDE, IAW SRM AND REO.

Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 21,834 hrs · 19,506 cycles

LEFT INBD FLAP. FLAP VANE HAS CHAFING ON INBD SECTION OF VANE L/E. C-CHECK, BLENDED CHAFE ON FLAP VANE INBD SIDE, IAW REO.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 21,834 hrs · 19,506 cycles

LEFT SIDE INBD FLAP. FLAP VANE HAS CHAFING AT CENTER OF VANE. C-CHECK, R & R LEFT SIDE INBD FLAP VANE CENTER SKIN IAW REO AND SRM.

Part: SKIN — CHAFED (LT WING AILERON) · airframe 21,834 hrs · 19,506 cycles

LEFT AILERON LOWER OTBD FIXED PANEL CHAFED. C-CHECK, REPAIRED LT LOWER FIXED AILERON OTBD PANEL IAW STS EA.

Part: SKIN — CHAFED (LT WING AILERON) · airframe 21,834 hrs · 19,506 cycles

LT AILERON LOWER L/E PANEL 599BB CHAFED. C-CHECK, REPAIRED LT AILERON LOWER L/E PANEL 599BB IAW STS EA.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 21,834 hrs · 19,506 cycles

LEFT INBD FLAP, FLAP VANE HAS CHAFING ON FLAP VANE OTBD SIDE OF VANE. C-CHECK, BLENDED CHAFE ON FLAP VANE OTBD SIDE, IAW REO.

Part: DOOR SILL — CORRODED (SERVICE DOOR) · airframe 21,834 hrs · 19,506 cycles

THE SERVICE DOOR SILL PLATE ASSY HAS EVIDENCE OF CORROSION AROUND EACH OF THE LOWER FASTENER HOLES AND HAS 1, SEIZED DOME NUT. C-CHECK, REPLACED SERVICE DOOR SILL PLATE IAW SRM.

Part: BEAM — CRACKED (BS 559) · airframe 21,567 hrs · 19,234 cycles

FOUND A CRACK AT WEB BEAM LBL 9.0 ON BS 559. C-CHECK COMPLIED WITH STRUCTURAL REPAIRS AS REQUIRED IAW REO.

Part: CONNECTOR — LOOSE (CABIN) · airframe 20,450 hrs · 18,167 cycles

EMERGENCY LIGHT AT 8D INOPERATIVE. FLT#4696 RESECURRED LOOSE CONNECTION ONTO SEAT 8D FLOOR LEVEL E-EXIT SIGN.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 19,198 hrs · 16,936 cycles

RIGHT SIDE EMERGENCY EXIT OVERWING LOWER LIGHT DOES NOT ILLUMINATE. (FLT 4776) REMOVED AND REPLACED THE NR 3 ECBP INVERTER AND THE LIGHT ASSEMBLY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,903 hrs · 16,647 cycles

NR 2 EMERGENCY OVERHEAD BURNED OUT. (FLT 4663) RELAMPED EMERGENCY LIGHT.

Part: PROXIMITY SENSOR — OUT OF ADJUST (RT MLG) · airframe 18,404 hrs · 16,136 cycles

GEAR DISAGREE WARNING MESSAGE ON RETRACTION. (FLT 7775) ADJUSTED TARGET/PROXIMITY SENSOR ON RIGHT MLG UPLOCK IN REFERENCE TO CRJ 200 AMM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 18,323 hrs · 16,060 cycles

FS 280.00 UPPER FLOOR SUPPORT ANGLE CRACKED BY SUPPORT STRUT AND LBL 9.0 AND RBL 9.0. (C-CHECK) REPAIRED FS 280.00 UPPER FLOOR SUPPORT ANGLE FROM LBL 9.0 TO RBL 9.0 PER REO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 18,323 hrs · 16,060 cycles

FS 621 BULKHEAD WEB AT AFT CARGO DOOR TRACK HAS A CRACK. (C-CHECK) REPAIRED PER REO.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 18,323 hrs · 16,060 cycles

TOP OF FLOORBEAM AT FS 349.00 NEAR SERVICE DOOR HAS CORROSION. (C-CHECK) REPAIRED IN REFERENCE TO REO.

Part: DOOR — CORRODED (E&E BAY) · airframe 18,323 hrs · 16,060 cycles

CORROSION ON FORWARD SEAL SURFACE OF FORWARD EMERGENCY BAY DOOR. (C-CHECK) REPAIRED PER REO.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,286 hrs · 16,029 cycles

AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4728) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,250 hrs · 15,998 cycles

1ST OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4765) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,754 hrs · 15,533 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4718) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,437 hrs · 15,208 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4494) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,828 hrs · 14,616 cycles

LAST OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4621) RELAMPED EMERGENCY LIGHT.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 15,950 hrs · 13,803 cycles

PAX DOOR AFT DRAG ANGLE CRACKED AT PULLEY BRACKET. REMOVED DAMAGED SECTION OF AFT DRAG ANGLE AND SPLICED IN A NEW SECTION IAW REO 670-52-11-513, REV A.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 15,037 hrs · 12,965 cycles

BULKHEAD WEB CRACKED AROUND LINTEL ATTACH FITTING AT FS 621, LBL 38, WL 106-103. CUT OUT DAMAGE AND INSTALLED REPAIR DOUBLER PER REO 601R-53-61-1230.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 13,232 hrs · 11,279 cycles

FWD PRESSURE BULKHEAD CRACKED AT PARKING BRAKE CABLE CUTOUT. CUT OUT DAMAGE AND INSTALLED REPAIR DOUBLER PER REO 601R-53-11-563 AND EA 10-5311-02795.

Part: SKIN — CRACKED (PAX DOOR) · airframe 11,383 hrs · 9,881 cycles

PAX DOOR INNER SKIN IS DAMAGED AT DOOR DATUM 6, FS329.5. REPAIRED IAW EA 10-5210-02377.

Part: ACTUATOR — FAULTY (T/E FLAP) · airframe 9,783 hrs · 8,574 cycles

FLIGHT 5696 - FLAPS FAILED ON TAKEOFF UPON RETRACTION, FAILED AT 18 DEGREES. AIRCRAFT RETURNED BACK TO DSM AND LANDED SAFELY. REMOVED AND REPLACED LEFT O/B FLAP O/B ACTUATOR.

Part: ACTUATOR — FAULTY (T/E FLAP) · airframe 9,783 hrs · 8,574 cycles

FLIGHT 5696 - FLAPS FAILED ON TAKEOFF UPON RETRACTION, FAILED AT 18 DEGREES. AIRCRAFT RETURNED BACK TO DSM AND LANDED SAFELY. REMOVED AND REPLACED LEFT I/B FLAP I/B ACTUATOR.

Part: ACTUATOR — FAULTY (T/E FLAP) · airframe 9,783 hrs · 8,574 cycles

FLIGHT 5696 - FLAPS FAILED ON TAKEOFF UPON RETRACTION, FAILED AT 18 DEGREES. AIRCRAFT RETURNED BACK TO DSM AND LANDED SAFELY. REMOVED AND REPLACED LEFT I/B FLAP O/B ACTUATOR.

Part: ACTUATOR — FAULTY (T/E FLAP) · airframe 9,783 hrs · 8,574 cycles

FLIGHT 5696 - FLAPS FAILED ON TAKEOFF UPON RETRACTION, FAILED AT 18 DEGREES. AIRCRAFT RETURNED TO DSM AND LANDED SAFELY. REMOVED AND REPLACED LEFT O/B FLAP I/B ACTUATOR.

Part: ACTUATOR — FAULTY (T/E FLAP) · airframe 9,665 hrs · 8,479 cycles

FLIGHT 5681 - RECEIVED FLAP FAIL CAUTION MESSAGE. DECLARED EMERGENCY, ABORTED APPROACH, THEN LANDED CVG WITHOUT INCIDENT. REPLACED RIGHT SIDE NR 2 FLAP ACTUATOR. NO FURTHER DEFECTS.

Part: ACTUATOR — FAULTY (T/E FLAP) · airframe 9,665 hrs · 8,479 cycles

FLIGHT 5681 - RECEIVED FLAP FAIL CAUTION MESSAGE. DECLARED EMERGENCY, ABORTED APPROACH, THEN LANDED CVG WITHOUT INCIDENT. REPLACED RIGHT SIDE NR 1 FLAP ACTUATOR. NO FURTHER DEFECTS.

Part: ACTUATOR — FAULTY (T/E FLAP) · airframe 9,665 hrs · 8,479 cycles

FLIGHT 5681 - RECEIVED FLAP FAIL CAUTION MESSAGE. DECLARED EMERGENCY, ABORTED APPROACH, THEN LANDED CVG WITHOUT INCIDENT. REPLACED RIGHT SIDE NR 4 FLAP ACTUATOR. NO FURTHER DEFECTS.

Part: ACTUATOR — FAULTY (T/E FLAP) · airframe 9,665 hrs · 8,479 cycles

FLIGHT 5681 - RECEIVED FLAP FAIL CAUTION MESSAGE. DECLARED EMERGENCY, ABORTED APPROACH, THEN LANDED CVG WITHOUT INCIDENT. REPLACED RIGHT SIDE NR 3 FLAP ACTUATOR. NO FURTHER DEFECTS.

Part: FLAP — MALFUNCTIONED (WING) · airframe 9,660 hrs · 8,478 cycles

FLIGHT 5199 - RECEIVED FLAP FAIL CAUTION MESSAGE. DECLARED EMERGENCY, ABORTED APPROACH, THEN LANDED MSP WITHOUT INCIDENT. COMPLIED WITH SI-2-2710002. PERFORMED FLAP REJUVE ON RIGHT SIDE. NO FURTHER DEFECTS.

Part: SMOKE DETECTOR — NONE (LAVATORY) · airframe 8,274 hrs · 7,373 cycles

FLIGHT 5037 - RECEIVED LAV SMOKE WARNING. RETURNED TO ATL. LANDED WITHOUT INCIDENT. INSPECTED LAV AND PERFORMED OPS CHECK OF LAV SMOKE DETECTOR. NO FURTHER DEFECTS.

Part: SWITCH — DIRTY (STAB TRIM) · airframe 7,765 hrs · 7,001 cycles

FLIGHT 5266 - ON CLIMBOUT STAB AND MACH TRIM ABNORMAL MESSAGES. RAN QRH, NO CHANGE. AIRCRAFT RETURNED BACK TO RIC AND LANDED SAFELY. CLEANED STAB TRIM DISCONNECT SWITCHES ON BOTH YOKE ASSEMBLIES. OPS CHECK GOOD AT THIS TIME.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 7,729 hrs · 6,970 cycles

FLIGHT 5564 - FLAPS FAIL CAUTION MESSAGE WHEN SELECTED FROM ZERO DEGREES ON APPROACH. A/C LANDED SAFELY. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3 (A, B, C). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES.

Part: UNKNOWN — MALFUNCTIONED (E/E BAY DOOR) · airframe 7,329 hrs · 6,639 cycles

FLIGHT 5123 - DURING TAKEOFF ROLL BELOW 10 KTS AVIONICS BAY DOOR INDICATION. ABORTED TAKEOFF AND RETURNED TO GATE. VERIFIED DOOR CLOSED, LOCKED AND LATCHED, TRANSFERRED TO DMI LIST PER 52-70-02.

Part: TRANSDUCER — INTERMITTENT (NR 1 MACH)

ADC1 FAIL, MACH TRIM DISENGAGE INTERMITTENT ON CLIMBOUT. MX REMOVED & REPLACED NR 1 MACH TRANSDUCER. PERFORMED PITOT/STATIC CHECK.

Part: BULB — BURNED OUT (EMERGENCY LIGHT)

DURING INSPECTION THE LEFT HAND OVERWING EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 2,932 hrs · 2,536 cycles

DURING INSPECTION THE EMERGENCY FLOOR LIGHTING WAS FOUND INOPERATIVE. THE LIGHT STRIP WAS FOUND INOPERATIVE AND REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RETURNED TO SERVICE.

Part: INVERTER — FAULTY (CABIN)

DURING MAINTENANCE INSPECTION, NUMEROUS EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED INVERTER, AN OPERATIONAL CHECK WAS SATISFACTORY AND AIRCRAFT WAS RELEASED FOR SERVICE.

Part: LINE — FAILED (HYDRAULIC SYSTEM)

HYDRAULIC PRESSURE SENT TO ZERO IN-FLIGHT. AIRCRAFT RETURNED TO AIRPORT SAFELY. MAINTENANCE FOUND RESERVOIR EMPTY DUE TO MASSIVE LEAK AT RT FLAP ACTUATOR LINES. NEW LINES INSTALLED. RIGHT HYDRAULIC PUMP FAILED TO PRODUCE PRESSURE. REPLACED PUMP AND FILTER. OPS CHECK OK. HOSES FAILED DUE TO AGE. LOCATED IN AREA IMPOSSIBLE TO INSPECT PROPERLY. PUMP FAILED DUE TO FLUID STARVATION.