N8974C

Part: SOLENOID VALVE — INOPERATIVE (FUEL SYSTEM) · airframe 25,732 hrs · 25,489 cycles

CREW REPORTED A FUEL ODOR WITH THE NR 1 PACK ON, IN THE COCKPIT. FOUND FUEL SOLENOILD VALVE ON APU LEAKING. REPLACED THE SOLENOID VALVE IAW AMM 49-31-05. OPS AND LEAK CHECKED GOOD. R & R APU FUEL CONTROL IAW AMM 49-31-01. OPS & LEAK CHECKED GOOD.

Part: BULKHEAD — CHAFED (FUSELAGE) · airframe 25,209 hrs · 24,907 cycles

FS621 RPB WEB AHS 4 EA CHAFES FROM BAGGAGE LINEAR SCREWS AT WL103 RBL18, 27, AND 36 + WL76 LBL 23. C/W REPAIR TO 621RPB CHAFES IAW BSC REO 601R-53-61-2155 REV A DATED 2013-08-13. NO DEFECTS NOTED. WVAC

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 25,209 hrs · 24,907 cycles

L/H SIDEWALL SEAT RAIL IS CORRODED AT F.S. 499 TO F.S. 544. REMOVED UNSERVICEABLE LH SIDEWALL SEAT RAIL AT FS 499-544 FABRICATED AND INSTALLED NEW SEAT RAIL IAW REO 601R-53-00-055 REV C. WVAC STAMP

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 25,209 hrs · 24,907 cycles

ONE CRACK INDICATION NOTED IN FS 621 RPB WEB AT ""HEEL LINE AREA"" OF LBL 27 VERT POST ""Z"" MEMBER AT WL 130.5 - WL 131 (TOP OF CARGO DOOR TRACK) BY 100% FSH. FAILED NDT INSP. REPAIRED FS621 BULKHEAD IAW REO 601R-53-61-1541 REV F DATED 2014/11/12. WVAC

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 25,209 hrs · 24,907 cycles

THE SERVICE DOOR LOWER FLOOR SUPPORT ANGLE IS CORRODED REPLACED MOUNTING ANGLE P/N 601R38303-253 IAW CRJ 200 SRM 51-42-36, 51-42-11, 51-42-21 AND 51-42-06. WVAC STAMP

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 25,209 hrs · 24,907 cycles

L/H SIDEWALL SEAT RAIL CORRODED FROM F.S. 409+16 TO F.S. 409+112. REMOVED AND REPLACED L/H SIDEWALL SEAT RAIL @ 409+16.0 TO 409+112 IAW BSC REO 601R-53-00-485 DATED 2018-01-29 REV D. WVAC STAMP

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 25,209 hrs · 24,907 cycles

FS 349 TRANSVERSE BEAM CAP IS CORRODED AT RBL 40 AROUND OUTBOARD WINDSCREEN MOUNT. REPLACED CORRODED ANGLE AND REINSTALLED RELATED STRUCTURAL PARTS IAW CRJ 200 SRM 51-42-21, CRJ 200 SRM 51-42-13 AND CRJ 200 SRM 51-42-06. WVAC STAMP

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 25,209 hrs · 24,907 cycles

L/H FLOOR SEAT RAIL CORRODED & GOUGED FROM F.S. 394 - F.S. 409+128 INSTALLED NEW SEAT RAIL F.S. 394 - 409.128 LBL 9 P/N 601R31032-21 IAW BOMBARDIER CRJ 200 AMM 53-01-11-400-802. WVAC STAMP EMP# 717 MTC.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 25,209 hrs · 24,907 cycles

RH FLOOR SEAT RAIL IS CORRODED & GOUGED AT FS 394 TO FS 409+128. ISNTALLED NEW SEAT RAIL FS 394 - 409+128 RBL 9 P/N 601R31032-21 IAW BOMBARDIER CRJ 200 AMM 53-01-11-400-802. WVAC STAMP EMP# 717 MTC.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 25,209 hrs · 24,907 cycles

R/H FLOOR SEAT RAIL CORRODED/GOUGED AT F.S. 364-394. INSTALLED NEW SEAT RAIL F.S. 364-394 RBL 9 P/N 601R31032-15 IAW BOMBARDIER CRJ 200 AMM 53-01-11-400-802. WVAC STAMP

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,209 hrs · 24,907 cycles

EMERGENCY LIGHT CENTER OF CABIN CEILING LIGHT INOP LOCATION: (F) CEILING EMERGENCY FLOOD LT #2 (REF: AMM 33-51-00-13)PG.13). REMOVED AND INSTALLED NEW SERVICEABLE EMERGENCY LIGHT IAW CRJ 200 AMM 33-51-16-000-801 AND 33-51-16-400-801. OPS TEST GOOD. WVAC EMP #571017

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 23,138 hrs · 22,730 cycles

EXTERIOR EMERGENCY LIGHT 4 INOP RELAMPED EXTERIOR EMERGENCY LIGHT 4 REF CRJ200 AMM 33-51-21. OPS CHECK GOOD

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 22,745 hrs · 22,289 cycles

FA FLASHLIGHT INOP. REMOVED AND REPLACED FA FLASHLIGHT IAW AMM 25-61-02. OPS CHECK GOOD.

Part: OXYGEN MASK — LEAKING (FIRST OFFICER'S) · airframe 22,183 hrs · 21,679 cycles

ENROUTE, SUSPECT FIRST OFFICER 02 MASK LEAKINE OR SOV NOT CLOSING. R & R THE FIRST OFFICER`S OXYGEN FULL FACE MASK, OPS CHECKED GOOD IAW AMM 35-11-12.

Part: YAW DAMPER — MALFUNCTIONED · airframe 22,020 hrs · 21,508 cycles

CREW DECLARED EMERGENCY, LEFT WIND FUEL CROSSFLOW RAN CONTINOUSLY AND IMBALANCE GREW TO 600LBS WITH LT WING LIGHT, UPON LEVEL OFF IMBALANCE BEGAN TO CORRECT AND RETURNED TO A BALANCED STATE. UNCOMMANDED YAW MOTION AT FL330, DESCENDED TO 270 AND YAW STILL PRESENT EVEN WITH AUTOPILOT OFF AND TRIMMED FOR STRAIGHT FLIGHT. COMPLIED WITH QRH AND UNCOMMANDED YAW STOPPED. NO EICAS MESSAGES NOTED DURING FLIGHT. REPLACED THE LINEAR ACTUATOR AND PERFORMED OPS CHECK OF ACUTATORS WERE GOOD, CABLE TENSION GOOD, FUEL CROSSFEED CHECKED GOOD, REPLACED THE RUDDER POSITION TRANSMITTER AND OPS CHECKED GOOD.

Part: SHEAR TIE — DAMAGED (BS 267) · airframe 22,020 hrs · 21,508 cycles

FRAME BS 267 MISSING END OF THE SHEAR TIE. REPAIRED THE SHEAR TIE IAW EA 253-06779

Part: FRAME — DAMAGED (BS 208) · airframe 22,020 hrs · 21,508 cycles

UPPER LEFT BS 208 FRAME WAS FOUND DAMAGED. REMOVED AND REPLACED THE FRAME.

Part: ANGLE — CRACKED (BS 280) · airframe 22,020 hrs · 21,508 cycles

STRINGER 3L, INBD AND OTBD ANGLES ARE CRACKED. JUST AFT OF BS 280. REMOVED AND REPLACED THE ANGLES IAW SRM 51-42-06, SRM 51-42-21, AND SRM 51-40-11.

Part: WEB — CRACKED (PAX DOOR) · airframe 22,020 hrs · 21,508 cycles

AFT WEB AT STEP 1 IS CRACKED ON THE PAX DOOR. CUTOUT THE DAMAGE AND INSTALLED A REPAIR IAW REO 601R-52-11-702, OPS CHECKED GOOD IAW AMM 52-11-17-710-802.

Part: BRACKET — CRACKED (RT NACELLE) · airframe 22,020 hrs · 21,508 cycles

RIGHT PYLON UPPER STANG FAIRING FWD BRACKET CRACKED. REMOVED AND REPLACED THE BRACKET IAW CMM 20-42-06.

Part: SUPPORT BRACKET — CRACKED (BS 449) · airframe 22,020 hrs · 21,508 cycles

RIGHT OVERWING SUPPORT BRACKET AT BS 449.85 IS CRACKED. REMOVED AND REPLACED THE SUPPORT BRACKET IAW SRM 51-42-06.

Part: BRACKET — CRACKED (BS 210) · airframe 22,020 hrs · 21,508 cycles

FLIGHT DECK PILOT SIDE ANGLE BRACKET IS CRACKED NEAR WINDOW SILL BY BS 210. REMOVED AND REPLACED BRACKET IAW SRM 51-42-21.

Part: FRAME — CRACKED (FUSELAGE) · airframe 22,020 hrs · 21,508 cycles

FRAME 333 IS CRACKED JUST I/B OF STR 1L, IN THE CABIN. REPAIRED FRAME 333, I/B OF STR 1L IAW EA CRJ-253-06709.

Part: ATTACH BRACKET — CRACKED (LT WING) · airframe 22,020 hrs · 21,508 cycles

LT WING CTR L/E PANEL INBD ATTACH BRKT CRACKED AT ANTI-ICE TRANS DUCT MOUNT. REMOVED AND REPLACED LT WING CTR L/E PANEL INBD ATTACH BRKT IAW SRM 51-41-00.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 22,020 hrs · 21,508 cycles

INTERCOSTAL BETWEEN LBL27 AND LT SILL AT FS 484.0 INBD CLIP IS CRACKED. REMOVED AND REPLACED INBOARD LT ANGLE(CLIP) FS484 WITH NEW ANGLE IAW REO 601R-53-41-059 REV B.

Part: DOOR TRACK — CHAFED (CARGO) · airframe 21,132 hrs · 20,554 cycles

WHILE PERFORMING A 12 MONTH INSPECTION OF CARGO DOOR FITTINGS, DISCOVERED THE FORWARD CARGO DOOR BALANCE SPRING ASSEMBLY CABLE OUT OF POSITION, CAUSING A CHAFFING CONDITION ON THE UPPER CARGO DOOR TRACK CROSS MEMBER IN TWO LOCATIONS. REFERENCE E.O. CRJ253-05936 FOR REPAIR INFORMATION AND ILLUSTRATIONS

Part: BUTTON — BROKEN (OXYGEN BOX) · airframe 21,123 hrs · 20,546 cycles

OBSERVER`S OXYGEN BOX HAS A BROKEN PUSH TO TEST BUTTON. PUSH TO TEST IS INOPERATIVE. REPLACED THE OBSERVER`S OXYGEN MASK BOX IAW AMM 35-11-15. OPS & LEAK CHECKED GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 20,283 hrs · 19,660 cycles

RIGHT AFT EXTERIOR EMERGENCY LIGHT INOP. RELAMPED EMERGENCY LIGHT, OPS CKS GOOD IAW AMM 33-51-00. P/N ON/OFF - 1317

Part: DOOR — UNKNOWN (MAIN PAX) · airframe 19,355 hrs · 18,700 cycles

MAIN CABIN DOOR WILL NOT SECURE CLOSED. PASSENGER DOOR OUTLINED IN RED WITH PASSENGER DOOR OUTER HANDLE MESSAGE ON DOORS SYNOPTIC PAGE. AS IS UNABLE TO LOCK THE STOW AND SECURE HANDLE FROM INSIDE THE AIRCRAFT. PERFORMED VI OF PAX LATCH MECHANISM, DOOR CLOSED AND OPERATED NORMALY IAW AMM 52-11-21 NO DEFECTS NOTED, PERFORMED OPS TEST OF THE PAX DOOR ASSIST MOTOR IAW AMM 52-11-08 OPS CHECK GOOD.

Part: BPSU — INOPERATIVE (TE FLAP SYSTEM) · airframe 19,234 hrs · 18,571 cycles

FLAPS FAIL CAUTION DURING FINAL, FAILED AT 30 AND AIRSPEED AT 160-165. REMOVED AND REPLACED THE LEFT AND RIGHT BPSU IAW MTR.

Part: BPSU — FAILED (TE FLAPS) · airframe 19,233 hrs · 18,570 cycles

FLAPS FAIL CAUTION IN FLIGHT, FL 260. OCCURED WHILE FLAPS STOPPPED EICAS PFLAP POSITION INDICATES 0, FLAPS AT O. AIRSPEED 300KNTS/. 74 MACH 45 MINS INTO FLIGHT OAT SAT -22/TAT 5. FOUND RT BPSU SHORTED INTERNALLY. REMOVED AND REPLACED IAW AMM 27-51-10. ALL RIGGING AND OPERATIONAL CHECKS GOOD. DURING RIGGING FECU FAIL. REMOVED AND REPLACED FECU IAW AMM 27-51-05. ALL RIGGING, OPERATIONAL AND FUNCTIONAL CHECKKS GOOD.

Part: BPSU — INOPERATIVE (TE FLAP SYSTEM) · airframe 19,227 hrs · 18,564 cycles

FLAPS FAILED AT 8 DEGREES AFTER DEPARTURE. R & R THE RT BPSU IAW AMM 27-51-10, AND FECU IAW AMM 27-51-05. OPS CHECKED AND RIGGING GOOD.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 19,090 hrs · 18,416 cycles

FORWARD FLIGHT ATTENDANT FLASHLIGHT NOT BLINKING. R & R FLIGHT ATTENDANT FLASHLIGHT BATTERY IAW AMM 25-61-02. OPERATIONS CHECKED NORMAL.

Part: HANDLE — OUT OF ADJUST (PAX DOOR) · airframe 19,067 hrs · 18,392 cycles

MAIN CABIN DOOR NOT CLOSING PROPERLY. ADJUSTED OUTER HANDLE DETENT & PUSHROD IAW NRWC 520650.

Part: STRUCTURE — GOUGED (FUSELAGE) · airframe 19,040 hrs · 18,364 cycles

WHILE PERFORMING INCOMING DAMAGE PERMANENT REPAIR TO WATCH ITEM 53336, CUSTOMER CARD 628814 FOUND FURTHER DAMAGE. FOUR EACH GOUGES AT FS 589.00 - 596.00, BETWEEN STRINGER 21R & 22R. REPAIRED FS 589 - 596, BETWEEN STRINGER 21R & 22R IAW EA CRJ253-04343.

Part: STRUCTURE — DENTED (FUSELAGE) · airframe 19,040 hrs · 18,364 cycles

WHILE PERFORMING CUSTOMER TASK CARD W533337, A DENT AT FS 592, BETWEEN STRINGERS 25R & 26R COULD NOT BE RE-CONTOURED & REQUIRES REPAIR. PERFORMED CUT OUT OF DAMAGE & FABRICATED & INSTALLED REPAIR DOUBLER IAW EA CRJ253-04341.

Part: ANGLE — CRACKED (STANG FAIRING) · airframe 19,040 hrs · 18,364 cycles

LEFT ENG UPPER STANG FAIRING FWD Z ANGLE CRACKED. R & R UPPER STANG FAIRING FWD Z ANGLE IAW CMM 20-42-06.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 19,040 hrs · 18,364 cycles

FS 559 PRESS BULKHEAD CAP ANGLE IS CRACKED IN RADIUS AT LBL 18. REPAIRED CAP ANGLE AT 559 IAW EO P53025

Part: POST — CRACKED (FUSELAGE) · airframe 19,040 hrs · 18,364 cycles

VERTICAL POST STATION 409.0+128, BL 0.00, CRACKED RT SIDE IN RADIUS OF C CHANNEL. REMOVED CRACKED ANGLE & INSTALLED NEW ANGLE IAW REO 601R-53-41-2030 DATED 5 13 16 IAW SB 601R-53-083 REV C.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 19,040 hrs · 18,364 cycles

RIGHT ACM RACK, Z ANGLE CRACKED. R & R UNSERVICEABLE Z ANGLE WITH A SERVICEABLE Z ANGLE IAW SRM 51-42-06 & 51-41-21.

Part: SUPPORT BRACKET — CRACKED (CARGO DOOR) · airframe 19,040 hrs · 18,364 cycles

BAGGAGE DOOR LOWER FWD RAIL SUPPORT BRACKET IS CRACKED. R & R UNSERVICEABLE FWD RAIL SUPPORT BRACKET WITH A SERVICEABLE FWD RAIL SUPPORT BRACKET IAW SRM 51-42-06 & 51-41-02.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 19,040 hrs · 18,364 cycles

IN MAIN CABIN RIGHT SEAT RAIL HAS MULTIPLE AREAS OF CORROSION & GOUGES, STATION 409+128 - 559+112. R & R SEAT TRACKS ON RT SIDE 4 - 7, STATION 409+128 - 559+112 IAW AMM 53-01-11-000-802 & 53-01-11-400-802.

Part: RUB STRIP — CHAFED (NR 1 COWLING) · airframe 19,040 hrs · 18,364 cycles

NUMBER 1 ENG UPPER FAN COWL RUB STRIP IS CHAFED. R & R NR 1 ENG UPPER FAN COWL RUB STRIP IAW CMM 71-14-01.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 19,040 hrs · 18,364 cycles

CABIN, RT SIDE SEAT RAIL HAS MULTIPLE AREAS OF CORROSION FROM FS 364 - 409+128. R & R SEAT TRACK IAW AMM 53-01-11-000-802 & 53-01-11-420-001-2A, PN 601R38312-31 TAG B 83648.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 19,040 hrs · 18,364 cycles

INTERCOSTAL IS CRACKED AFT OF AFT PRESS BULKHEAD, AT FS 621, STRINGER 15L. R & R AFT CARGO UNSERVICEABLE INTERCOSTAL WITH A SERVICEABLE INTERCOSTAL IAW SRM 51-42-06, 51-42-21 & 51-24-21.

Part: RING — CHAFED (NR 1 COWLING) · airframe 19,040 hrs · 18,364 cycles

NUMBER 1 ENG UPPER CORE COWL AFT EDGE IS CHAFED IN SEVERAL AREAS. REPLACED CLOSURE RING IAW SRM 51-42-06, 51-42-07 & CMM 71-12-01 TASK 71-12-01-320-820-A01 STEPS 21 A - F, H - J), IPL SEQ 71-12-01-01-380 AAR AP-52.

Part: GUIDE — CHAFED (TE FLAP) · airframe 19,040 hrs · 18,364 cycles

RIGHT WING INBD FLAP, INBD HINGE ARM INBD FAIRING GUIDE IS CHAFED. R & R GUIDE IAW SRM 51-42-06.

Part: GUIDE — CHAFED (TE FLAP) · airframe 19,040 hrs · 18,364 cycles

RIGHT WING INBD FLAP OTBD HINGE ARM INBD FAIRING GUIDE IS CHAFED. R & R GUIDE IAW SRM 51-42-06.

Part: GUIDE — CHAFED (TE FLAP) · airframe 19,040 hrs · 18,364 cycles

RIGHT WING OTBD FLAP CTR HINGE ARM INBD FAIRING GUIDE IS CHAFED. R & R OTBD FAIRING GUIDE IAW SRM 51-42-06 & 51-42-10.

Part: COALESCER BAG — DIRTY (AC BAY) · airframe 18,501 hrs · 17,850 cycles

STRONG OILY ODOR WHEN PACK TEMP RISES ABOVE 20 C. REPLACED WATER SEPARATOR COALESCE BAGS 1 & 2 IAW AMM 21-51-13. COMPLIED WITH OPERATION CHECK IAW AMM 21-51-00, NO OILY ODOR DETECTED. OK FOR SERVICE. OPERATIONS CHECKED GOOD.

Part: CABLE — UNKNOWN (CABIN DOOR) · airframe 17,790 hrs · 17,123 cycles

MAIN CABIN DOOR IS VERY DIFFICULT TO OPEN & CLOSE. R & R ICE BREAK CABLE ON PAX DOOR PRESS RELIEF DOOR IAW AMM 52-11-15. OPERATIONS CHECKED GOOD.

Part: STOWAGE BOX — LEAKING (CREW O2) · airframe 17,724 hrs · 17,055 cycles

OBSERVED O2 LEAK ON STATUS PAGE OXYGEN QTY INDICATOR. TROUBLE SHOT PILOT O2 MASK STOWAGE BOX WAS LEAKING O2, ,AT 50 PSI IN 10 MINS. R & R CREW MASK STOWAGE BOX IAW AMM 35-11-15. OK FOR SERVICE.

Part: RELAY — FAILED (CABIN DOOR) · airframe 17,578 hrs · 16,893 cycles

MAIN CABIN DOOR ASSIST MOTOR DOES NOT SHUT OFF AFTER DOOR IS CLOSED. DEFERRED CABIN DOOR ASSIST SYS IAW MEL 52-11-11. COMPLETED MX PROCEDURES, COMPLIED WITH DDG 52-11-11 ENTERED INTO MEL & MM02, MXC NOTIFIED TB. R & R RELAY K1MB FROM JB2 IAW CMM 24-00-02. PERFORMED ADJUSTMENT TEST OF JB2 IAW AMM 24-01-02. PERFORMED OPERATIONS CHECK OF PAX DOOR POWER ASSIST IAW AMM 52-11-08. ALL CHECKED GOOD. THIS CLEARS DM 001328. OK FOR SERVICE.

Part: UNKNOWN — MALFUNCTIONED (PAX DOOR) · airframe 17,363 hrs · 16,655 cycles

PAX DOOR DROPPED HARD ON OPEN INFO IAW F/A. R & R PAX DOOR ASSIST MOTOR IAW AMM 52-11-08. DID NOT FIX. DOOR STILL FALLS TOO FAST. LOGPAGE 3217923 FOR ADDITIONAL WRITEUP.

Part: FLAP — FAILED (WING) · airframe 17,277 hrs · 16,560 cycles

FLAPS FAILED. RESET FLAP CONTROL CB'S IAW FIM RESET MC NOTIFIED D F. OPERATIONS CHECKED GOOD.

Part: PBE — UNSERVICEABLE (COCKPIT) · airframe 17,243 hrs · 16,525 cycles

COCKPIT PBE HUMIDITY INDICATOR NOT BLUE. R & R PBE IAW AMM 25-60-00. OK FOR SERVICE.

Part: FITTING — CRACKED (FUSELAGE) · airframe 16,216 hrs · 15,511 cycles

FS 621 BULKHEAD LT LINTEL FITTING CRACKED. REPAIRED IAW REO 601R-53-61-1230.

Part: SKIN — CRACKED (FUSELAGE) · airframe 16,216 hrs · 15,511 cycles

FUSELAGE SKIN CRACKED 1/2 INCHES AT FS 235, RBL 6. REPAIRED IAW REO 601R-53-11-048.

Part: RIB — CRACKED (LT WING) · airframe 16,216 hrs · 15,511 cycles

LEFT MLG BATTERY RIB CRACKED & HAS PREVIOUS REPAIR AT WS 53.6. REPAIRED IAW REO 601R-57-51-684.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 16,216 hrs · 15,511 cycles

SEVERAL LOCATIONS ON CARGO DOOR FLOOR SILL CORRODED. REPAIRED IAW REO 601R-53-61-690 & 601R-53-00-526.

Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 16,216 hrs · 15,511 cycles

LEFT ELEVATOR AT ES 65 UPPER SKIN DAMAGE AROUND POP RIVET. REPAIRED IAW SRM 55-20-00 FIGURE 204 SHEET 5.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 16,216 hrs · 15,511 cycles

FORWARD PRESS BULKHEAD AT FS 202 CRACKED AT PARKING BRAKE CABLE PASS THROUGH HOLE. REPAIRED IAW REO 601R-53-11-536.

Part: FIRE BOTTLE — UNSERVICEABLE (CABIN) · airframe 14,533 hrs · 13,840 cycles

F/A NOTED AFT WATER FIRE EXTINGUISHER SEAL BROKEN. REPLACED FIRE EXTINGUISHER WITH SERVICABLE EXTINGUISHER IAW AMM 26-23-01.

Part: FITTING — CRACKED (FUSELAGE) · airframe 14,475 hrs · 13,779 cycles

REMOVED AND REPLACED CRACKED OUTBOARD CLIP AT S-13R BETWEEN FS 621 AND FS 625 IAW SRM 51-42-06.

Part: FITTING — CRACKED (FUSELAGE) · airframe 14,475 hrs · 13,779 cycles

REMOVED AS REPLACED CRACKED OUTBOARD CLIP AT S-15R BETWEEN FS 621 AND FS 625 IAW SRM 51-42-06.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,081 hrs · 13,407 cycles

EMERGENCY EXIT ROW LIGHT BULB OUT. REPLACED EMERGENCY ROW BULB IAW AMM 33-51-1.

Part: LIFE VEST — UNSERVICEABLE (COCKPIT) · airframe 13,355 hrs · 12,713 cycles

LIFE VEST HAS HOLE IN BAG "CAPTAINS". REMOVED AND REPLACED CAPTAINS LIFE VEST AMM 25-61-03.

Part: CONTROL PANEL — DIRTY (AILERON TRIM) · airframe 13,087 hrs · 12,436 cycles

AILERON TRIM STUCK IN LEFT POSTION. CLEANED CONTROL PANEL TRIM CENTERED. PERFORMED OPS CHECK OF AILERON TRIM SWITCH IAW AMM 27-12-00. OPS CHECKED GOOD.

Part: STRUCTURE — CRACKED (BS 280) · airframe 12,851 hrs · 15,192 cycles

LBL9 FS 280 LWR FLANGE CRACKED. REPAIRED LWR FLANGE LBL9 FS 280 IAW REO 601R-53-11-271.

Part: STRUCTURE — CRACKED (BS 280) · airframe 12,851 hrs · 15,192 cycles

RBL 9 FS 280 LOWER FLANGE CRACKED. REPAIRED LWR FLANGE RBL9 FS 28D IAW REO NR 601R-53-11-171 REF.

Part: ANGLE — CRACKED (BS 280) · airframe 12,851 hrs · 15,192 cycles

RT 280 RBL 9 CORNER ANGLE CRACKED. REMOVED AND REPLACED CRACKED ANGLE IAW SRM 51-4206 AND 51-42-21. HST101AC-5-2 B72140, B0203013-08 B03442, MS20470AD5-6 B46967 AAR SM-10.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 12,851 hrs · 15,192 cycles

LT INBOARD FLAP VANE OUTBOARD LEADING EDGE IS CHAFED. REMOVED AND INSTALLED NEW FLAP VANE IAW SRM 51-42-13.

Part: SEAT TRACK — CHAFED · airframe 12,851 hrs · 15,192 cycles

LT SIDE SEAT TRACK NR 5 IS CHAFED IN A FEW AREAS. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-01-11. MAJOR REPAIR.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 12,851 hrs · 15,192 cycles

RT INBOARD FLAP VANE INBOARD END LEADING EDGE IS CHAFED. REPLACED FLAP INBOARD END LEADING EDGE PANEL IAW SRM 51-42-13.

Part: SEAT TRACK — CORRODED · airframe 12,851 hrs · 15,192 cycles

RT SEAT TRACK CORRODED. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-01-11. MAJOR REPAIR.

Part: SEAT TRACK — CHAFED · airframe 12,851 hrs · 15,192 cycles

RT SIDE SEAT TRACK NR 6 CHAFED. REMOVED AND REPLACED 6 SEAT TRACK IAW AMM 53-01-11.

Part: SEAT TRACK — CHAFED · airframe 12,851 hrs · 15,192 cycles

SEAT TRACK NR 3 CHAFED. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-01-11.

Part: SEAT TRACK — CHAFED · airframe 12,851 hrs · 15,192 cycles

RT SIDE SEAT TRACK NR 4 CHAFED. REMOVED AND REPLACED SEAT TRACK IAW AMM 52-01-11.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 12,851 hrs · 12,192 cycles

LT WINDSCREEN EXIT LIGHT LENS BROKEN. REMOVED BROKEN EXIT LIGHT LENS AND INSTALLED SERVICEABLE EXIT LENS ON LT WINDSCREEN IAW AMM 33-51-13 P/N BF5-0390-901.

Part: PROXIMITY SENSOR — OUT OF ADJUST (NLG) · airframe 12,552 hrs · 11,853 cycles

NOSE WHEEL DID NOT RETRACT AFTER TAKEOFF, HAD NOSE GEAR DISAGREE WHEN GEAR SELECTED UP AND NOSE DOOR OPEN. FOLLOWED NON-NORMAL CHECKLIST. ADJUSTED NLG PROX SENSOR PS14GA PER 32-61-05 AMM. OPS CHECK GOOD.

Part: SKIN — DAMAGED (LT WING TE FLAP) · airframe 11,109 hrs · 10,199 cycles

DURING POST FLIGHT, NOTED A SEPARATION BETWEEN UNDER SIDE OF FLAP SURFACE AND T/E ON LT INBD FLAP ABOVE MAIN GEAR. APPEARS TO HAVE SOME RED PLASTIC PROTRUDING FROM GAP. REO 601R-57-52-1702, REV A- STEP 6; FILL GAP BETWEEN T/E STRUCTURE & LWR SKIN W/AERODYNAMIC SEALANT IAW SRM 51-12. APPLIED AERODYNAMIC FILLER IAW SRM 51-20-00 & 601R-57-52-1702, REMOVED FROM MM02 MXC NOTIFIED NR 4632. PERFORMED EDDY CURRENT ON LT INBD FLAP T/E. NO DAMAGE NOTED AT THIS TIME IAW NDTM 51-20-06. REPAIR COMPLETED

Part: LIGHT — LOOSE (CABIN) · airframe 10,617 hrs · 9,649 cycles

F/A REPORTS PLASTIC STRIP ON FLOOR BY SEATS 1BC & 2BC IS LOOSE. REPLACED EMERGENCY FLOOR TRACK LIGHT STRIP PN PL22-300LH00 AT SEATS 1DC & 2DC (RT CABIN).

Part: DOOR — BROKEN (CABIN) · airframe 9,334 hrs · 8,261 cycles

EXIT SIGN AT KNEE LEVEL BY BOARDING DOOR BROKEN. REPLACED LIGHT ASSY P/N BR9279-013, OPS CHECKS GOOD IAW AMM 33-51-10.

Part: TERMINAL — OUT OF POSITION (FIRE LOOP) · airframe 7,287 hrs · 6,073 cycles

L JET OVHT FAIL CAUTION MESSAGE FLASHED ON AND OFF AFTER PASSING FL300 FOR APPROX 10 MIN. COMPLETED THE EMERGENCY CHECKLIST AND LIGHT CAUTION CONTINUED. REMOVED EXHAUST NOZZLE FAIRING, INSPECTED BOTH A AND B JETPIPE LOOPS. FOUND TERMINAL LUG CHAFING ON ENGINE COWL. REPOSITIONED TERMINAL TUG AS REQUIRED. RE-INSTALLED SAME EXHAUST NOZZLE FAIRING PER AMM 78-11-01. PERFORMED INSULATION RESISTANCE CHECK, LOOPS CHECK GOOD PER CMM 26-11-67. OPS NORMAL PER AMM 78-11-00.

Part: UNKNOWN — ODOR · airframe 5,557 hrs · 4,397 cycles

DURING APPROACH NOTICED STRONG FUEL SMELL WHEN APU AIR SELECTED. INSPECTED APU AND COMPLETED RUNS WITH NO SMELL NOTED.

Part: FLAP SYSTEM — UNKNOWN

FLAPS FAIL ON APPROACH.

Part: FLAP SYSTEM — UNKNOWN · airframe 2,984 hrs · 2,230 cycles

FLAP FAIL, SECOND OCCURRENCE WITHIN 72 HOURS

Part: UNKNOWN — UNKNOWN (TE FLAPS)

FLAPS FAIL AT ZERO DEGREES. RESET FLAPS AND MONITOR FOR 72 HRS PER AD2006-12-21.