N8976E

Part: VERTICAL BEAM — CRACKED (BS 559) · airframe 24,489 hrs · 24,258 cycles

FOUND VERTICAL POST RBL 9.0 AT FS 559 CRACKED FROM LOWER IB SIDE UP TO HALF WAY TO SECOND RIVET ON ANGLE. REPAIRED VERTICAL POST RBL 9.0 AT FS559 IAW REO 601R-53-41-2584 AND REO 601R-53-41-057. THIS IS A MAJOR REPAIR

Part: PISTON — FAULTY (NLG) · airframe 22,861 hrs · 22,532 cycles

DURING INITIAL CLIMB ONCE THE GEAR HANDLE WAS PUT IN THE UP POSITION WE RECEIVED 3 EICAS MESSAGES. ""NOSE DOOR OPEN"" WARNING, ""GEAR DISAGREE"" WARNING, ""WOW INPUT"" CAUTION MESSAGE, ""WOW OUTPUT FAIL"" STATUS MESSAGE. THE MAIN GEARS BOTH SHOWED A DOWN INDICATION ON THE EDI AND THE NOSE GEAR SHOWED AN UP INDICATION. REMOVED & REPLACED NLG PISTON AXLE ASSY IAW JOB CARDS 200-32-21-20 & EO P32064. PERFORMED MULTIPLE GEAR RETRACTIONS/ EXTENSIONS IAW AMM 32-30-00, OPS CHECK GOOD. A/C OK FOR SERVICE.

Part: FLANGE — CRACKED (AC DOOR) · airframe 22,700 hrs · 22,362 cycles

GROUND AIR CONDITIONING DOOR FLANGE / LANDING BENT AT AFT DOOR CUTOUT. REMOVED BENT ANGLES AND REPLACED WITH NEW ANGLES IAW SRM 51-42-06. LEAK CHECKED GROUND AIRCONDITIONING DOOR FLANGE LANDING, LEAK CHECK GOOD IAW AMM 21-20-03-420-003.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 22,700 hrs · 22,362 cycles

EMERGENCY BATTERY PACK 3 FAILS TO LIGHT MID CABIN FWD FACING CEILING EXIT SIGN. REMOVED, REPLACED BATTERY PACK 3 IAW AMM 33-51-04. OP CHECK OF EMERGENCY LIGHT BATTERY PACK GOOD IAW AMM 33-51-04-740-801.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 22,700 hrs · 22,362 cycles

AFT PRESSURE BULKHEAD IS CRACKED AT THE UPPER END OF THE CARGO DOOR TRACK. REPAIRED AFT PRESSURE BULKHEAD AT UNDER UPPER END OF CARGO DOOR TRACK IAW REO 601R-53-61-1541. OPS CK OF THE CARGO DOOR IAW AMM 52-31-00-710-801, 52-70-02-710-801.

Part: FRAME — CRACKED (FUSELAGE) · airframe 22,700 hrs · 22,362 cycles

FRAME 559+96 CRACKED AT STR 21R. REPAIRED FRAME IAW SRM 53-00-15.

Part: FRAME — CORRODED (FUSELAGE) · airframe 22,700 hrs · 22,362 cycles

FS333.00 CIRCUMFERENCIAL FRAME HAS CORROSION AT SKIN ATTACHMENT FLANGES BTWN STR 25L AND 26R. REPAIRED DAMAGED SECTION OF FRAME AT STA 333 PER EA CRJ253-07515 IAW SEM 51-42-06 AND 51-42-21. OPS CHECK ACCOMPLISHED.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 22,700 hrs · 22,362 cycles

AT FS280.00 UPPER FUSELAGE STR 3 HAS CRACK. REMOVED CRACKED O/B ANGLE CLIP AND INSTALLED NEW ANGLE CLIP AT STGR 3L FS280 IAW SRM 51-42-06 AND 51-42-21 NDT VERIFIED NO CRACK IN LONGERON STGR 3L.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 22,700 hrs · 22,362 cycles

ANGLE CLIP ON THE I/B SIDE OF STR 3L IS CRACKED, JUST AFT OF FRAME 280, IN THE CABIN. REMOVED CRACKED I/B ANGLE CLIP AND INSTALLED NEW ANGLE CLIP AT STR 3L FS280 IAW SRM 51-42-06 AND 51-42-21.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 22,700 hrs · 22,362 cycles

LEFT NR 2 SIDE SEAT TRACK HAS CORROSION. R&R LT NR 2 SIDE SEAT TRACK IAW AMM 53-01-11.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 22,388 hrs · 22,015 cycles

TWO BULBS INOPERATIVE FOR THE EMERGENCY LIGHTS. R & R IAW 33-51-03. CHECKED GOOD.

Part: SEAL — BROKEN (FLASHLIGHT) · airframe 22,388 hrs · 22,015 cycles

FLIGHT ATTENDANT FLASHLIGHT SEAL WAS BROKEN. R & R THE SEAL IAW CMM 25-60-02.

Part: OXYGEN MASK — LEAKING (FIRST OFFICER'S) · airframe 22,358 hrs · 21,980 cycles

FIRST OFFICER`S OXYGEN MASK HARNESS WAS LEAKING. REMOVED AND REPLACED THE OXYGEN MASK IAW AMM 35-11-12. OPS CHECKED GOOD. NO DEFECTS NOTED.

Part: WEB — CRACKED · airframe 22,051 hrs · 21,623 cycles

DURING COMPLIANCE OF TC 53-160-635, A .625" CRACK ON IB LOWER ANGLE/ FLANGE OF WEB RBL 27.00, FS 406.00+128, STGR 22 WAS NOTED. THIS IS A MAJOR REPAIR*DAMAGE REPAIRED IAW REO 601R-41-056. REF NR 653459 FOR REPAIR DETAILS.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 21,562 hrs · 21,111 cycles

FA FLASHLIGHT NOT WORKING R&R FA EMERG FLASHLIGHT IAW AMM 25-61-00.OPS CHECK GOOD. AC GOOD FOR SERVICE

Part: LIGHT — BURNED OUT (CABIN) · airframe 21,399 hrs · 20,925 cycles

PAX ENTRY FLOOR LEVEL EMERGENCY FLOODLIGHT COVER DEGRADED + LAMP BURNT. R&R FLOOR LEVEL EMERGENCY FLOOD LIGHT COVER + RE-LAMPED IAW AMM 33-51-19. OPS CHECK GOOD. P/N BC5-0393-103 / PN 6100928V17023.

Part: COVER — CRACKED (DOOR HANDLE) · airframe 21,292 hrs · 20,790 cycles

LH EMERGENCY EXIT DOOR HANDLE COVER CRACKED. REMOVED AND REPLACED THE DOOR HANDLE COVER IAW 25-26-17.

Part: FITTING — OUT OF ADJUST (PASSENGER DOOR) · airframe 19,993 hrs · 19,416 cycles

DOOR TOP WITNESS MARKS DONT LINE UP, DOOR WONT OPEN. PERFORMED ADJUSTMENT TEST OF FWD & AFT SPIGOT FITTINGS IAW 52-11-00. ALL CHECKS GOOD, SEE NRCCS 103246, 103247 & 103248 FOR DETAILS OF WORK PERFORMED.

Part: OXYGEN MASK — LEAKING (COCKPIT) · airframe 19,861 hrs · 19,284 cycles

CAPTAIN`S OXYGEN MASK LEAKS. R & R THE OXYGEN BOX IAW AMM 35-11-15. LEAK CHECKED GOOD. OK FOR SERVICE. SWAPPED THE CAPTAIN`S OXYGEN MASK INTO OBSERVERS SEAT. R & R OBSERVER`S OXYGEN MASK IAW AMM 35-11-12. OBSERVERS SEAT OK FOR SERVICE.

Part: BATTERY PACK — INOPERATIVE (FLASHLIGHT) · airframe 19,420 hrs · 18,831 cycles

FA FLASHLIGHT INOPERATIVE. R & R THE FLASHLIGHT BATTERY IAW AMM 25-61-00

Part: STRIKER — CRACKED (FUSELAGE) · airframe 19,014 hrs · 18,429 cycles

FWD SIDE PAX DOOR SEAL STRIKER AT FS 310.00 IS SEVERELY CRACKED. REPAIRED PASSENGER DOOR FWD SEAL RETAINER IAW REO 601R-53-22-033, TYPE 4.

Part: RETAINER — DAMAGED (PAX DOOR) · airframe 19,014 hrs · 18,429 cycles

PAX DOOR LOWER SEAL RETAINER IS WAVY WITH MULTIPLE BENDS THROUGHOUT RETAINER. LOCATED, DRILLED AND INSTALLED NEW SERVICEABLE SEAL RETAINER, PN:601R318722-1 IAW SRM 51-40-11 AND REO: 601R-52-11-915, REV DATED 01/04/06.

Part: ROD — OUT OF ADJUST (PAX DOOR) · airframe 19,000 hrs · 18,416 cycles

MAIN CABIN DOOR WILL NOT CLOSE FULLY. ADJUSTED PUSH ROD ON MAIN PAX DOOR LATCH CAM TORQUE TUBE IAW AMM 52-11-23. OPERATIONS CHECK OF PAX DOOR NORMAL IAW AMM.

Part: TORQUE TUBE — DIRTY (CABIN DOOR) · airframe 18,927 hrs · 18,327 cycles

MAIN CABIN DOOR DIFFICULT TO CLOSE. CLEANED EXCESSIVELY TORQUE TUBE SYS. OPERATIONS CHECKED BY MX & FA TO SATISFACTION. OPERATIONS CHECKED IAW AMM 52-11-02. NO DISCREPANCIES AFTER SEVERAL OPERATION CHECKS.

Part: DOOR — DIRTY (CABIN) · airframe 18,808 hrs · 18,191 cycles

PASSENGER DOOR HARD TO CLOSE. CLEANED DIRTY & EXCESS OF GREASE. OPERATIONS CHECK OF PAX DOOR GOOD IAW AMM 52-11-00.

Part: CABLE — OUT OF POSITION (CABIN DOOR) · airframe 18,795 hrs · 18,179 cycles

FLIGHT ATTENDANT REPORTS MAIN CABIN DOOR STICKY TO GET TO CLOSE. CHECKED & CLEARED DEBRIS & REPOSITIONED ICE BREAK CABLE. OPERATIONS CHECKED GOOD IAW AMM 52-11-01.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 18,725 hrs · 18,110 cycles

RIGHT FLOOR SILL HAS CORROSION AROUND SCREW HOLES, BETWEEN FS 559+84 TO 560.0 005. R & R RT FLOOR SILL FS 559+84 - 560 WITH SERVICEABLE PART IAW EA NOCRJ253-04167 REV 1R DATED 03 22 16 & SRM 51-40-11, 51-42-06 & 51-42-21.

Part: SUPPORT CHANNEL — CHAFED (CARGO DOOR) · airframe 18,725 hrs · 18,110 cycles

CARGO DOOR PULLEY SUPPORT CHANNEL IS CHAFED STATION 574, 43 INCHES ABOVE FLOOR. R & R CARGO DOOR PULLEY SUPPORT CHANNEL IAW SRM 51-42-06 & 51-42-21.

Part: STEP — CORRODED (PAX DOOR) · airframe 18,725 hrs · 18,110 cycles

PANEL RACK PAX DOOR STEP 832DT HAS CORROSION FRONT & BACK SIDES. RECEIVED SERVICEABLE STEP INSTALLATION. COMPLIED WITH ON WO 1012732 8000 0043.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 18,725 hrs · 18,110 cycles

FS 621.00 LT STRINGER 16L, INTERCOSTAL IS CRACKED. R & R INTERCOSTAL IAW SRM 51-42-21.

Part: STEP — CORRODED (PAX DOOR) · airframe 18,725 hrs · 18,110 cycles

PANEL RACK PAX DOOR STEP 832AT HAS CORROSION FRONT & BACK SIDES. R & R PAX DOOR STEP 832AT SKIN IAW SRM 51-42-06.

Part: ATTACH BRACKET — CRACKED (PAX DOOR) · airframe 18,725 hrs · 18,110 cycles

PASSENGER DOOR ASSIST MOTOR, ATTACH BRACKET CRACKED AT LOWER RADIUS. R & R PAX DOOR ASSIST MOTOR ATTACH BRACKET IAW SRM 51-42-06 & SRM 51-40-11.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 18,725 hrs · 18,110 cycles

FS 621.00 LT STRINGER 14L INTERCOSTAL IS CRACKED. R & R INTERCOSTAL IAW SRM 51-42-21.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 18,725 hrs · 18,110 cycles

RIGHT SEAT TRACK 2 IS CORRODED & GOUGED IN MULTIPLE AREAS. R & R RT NR 2 SEAT TRACK IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 18,725 hrs · 18,110 cycles

LEFT SEAT TRACK 2 IS CORRODED & GOUGED IN MULTIPLE AREAS. R & R LT NR 2 SEAT TRACK IAW AMM 53-01-11.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 18,725 hrs · 18,110 cycles

FS 621.00 LT STRINGER 15L INTERCOSTAL IS CRACKED. R & R INTERCOSTAL IAW SRM 51-42-21.

Part: BULKHEAD — GOUGED (FUSELAGE) · airframe 18,725 hrs · 18,110 cycles

AFT PRESS BULKHEAD FWD FACE HAS 9 SCREW GOUGES, APPROX 29" ABOVE THE FLOOR. AFT PRESS BULKHEAD GOUGES REMOVED & FOUND TO BE WITHIN LIMITS IAW REO 601R-53-61-2155 REV A. ONE EACH AREA FOUND OUT OF LIMITS. DAMAGE CUT OUT & REPAIRED IAW REO 601R-53-61-1285 REV D. DAMAGED AREAS TREATED PRIMED IAW SRM TR51-36 & SRM TR51-39.

Part: MOUNT BRACKET — CRACKED (FUSELAGE) · airframe 18,725 hrs · 18,110 cycles

NUMBER 1HYD ACM PUMP CASE DRAIN FILTER MOUNT BRACKET IS CRACKED. R & R PUMP CASE DRAIN FILLER MOUNT BRACKET IAW SRM 51-42-06 & 51-24-24.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 18,725 hrs · 18,110 cycles

FS 484.00 CLIP LBL 36 IS CRACKED. REPAIRED SECTION OF INTERCOSTAL AT FS 484, LBL 36 IAW REO 601R-53-41-059 REVISION B.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 18,725 hrs · 18,110 cycles

FLOOR SEAT TRACK LBL 9, NR 3 CORRODED & GOUGED MULTIPLE AREAS. R & R FLOOR SEAT TRACK LBL 9, NR 3 IAW AMM 53-01-11-020-002B & AMM 53-01-11-420-001B.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 18,725 hrs · 18,110 cycles

FLOOR SEAT TRACK RBL 9, NR 3 IS CORRODED & GOUGED MULTIPLE AREAS. R & R FLOOR SEAT TRACK RBL 9 NR 3 IAW AMM STEP 2B, 3B 53-01-11.

Part: SUPPORT CHANNEL — BENT (FUSELAGE) · airframe 18,725 hrs · 18,110 cycles

CARGO DOOR FWD TRACK SUPPORT CHANNEL IS BENT IN MULTIPLE AREAS. FORMED BENDED SURFACE IAW SRM 51-24-21 & RE-STORED TO FINISH IAW SRM 51-25-16.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 18,725 hrs · 18,110 cycles

LEFT SIDE NR 6 SEAT RAIL HAS CORROSION AT FS 520. R & R LT NR 6 SEAT RAIL IAW AMM 53-01-11-400-802.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 18,725 hrs · 18,110 cycles

FS 202 BULKHEAD CRACKED AROUND PARKING BRAKE CABLE PASS THROUGH HOLE. REMOVED CRACK BY PERFORMING CUT OUT OF DAMAGE & FABRICATING & INSTALLING ALL REPAIR PARTS IAW REO 601R-53-11-563.

Part: FITTING — CRACKED (COCKPIT) · airframe 18,725 hrs · 18,110 cycles

FLIGHT DECK LT WINDOW SIDE POST LOWER FITTING IS CRACKED. R & R LT WINDOW SIDE POST LOWER FITTING IAW SRM 51-42-21 & SRM 51-40-11.

Part: FITTING — CRACKED (COCKPIT) · airframe 18,725 hrs · 18,110 cycles

FLIGHT DECK RT WINDOW SIDE POST LOWER FITTING IS CRACKED. R & R RT WINDOW SIDE POST LOWER FITTING IAW SRM 51-42-21 & SRM 51-40-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 18,725 hrs · 18,110 cycles

FLOOR SUPPORT BETWEEN LBL 27 & LT SILL IS CORRODED AT FS 559.0. R & R FLOOR SUPPORT STRAP IAW SRM 51-40-11 & 51-42-06.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 18,725 hrs · 18,110 cycles

LEFT SIDE NR 4 SEAT RAIL HAS CORROSION AT FS 428. R & R LT 4 SEAT RAIL IAW AMM 53-01-11-020-002 STEP 3A & 53-01-11-420-001 STEP 2A.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 18,725 hrs · 18,110 cycles

LEFT SEAT TRACK 1 IS CORRODED & GOUGED IN MULTIPLE AREAS. R & R LT SEAT TRACK 1 IAW AMM 53-01-11-420-001 & TASK 53-01-11-000-802.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 18,725 hrs · 18,110 cycles

RIGHT SEAT TRACK 1 IS CORRODED & GOUGED IN MULTIPLE AREAS. REMOVED CORRODED SEAT TRACK FROM RB 19 NR 1 POSITION & INSTALLED SERVICEABLE SEAT TRACK IAW AMM 53-01-11-400-802.

Part: FITTING — CRACKED (FUSELAGE) · airframe 18,725 hrs · 18,110 cycles

FS 461.00 BATH TUB FITTING IS CRACKED RBL 9. R & R BATH TUB FITTING FS 461.00, RBL 9 IAW SRM 51-40-01 & SRM 51-42-20.

Part: FITTING — CRACKED (FUSELAGE) · airframe 18,725 hrs · 18,110 cycles

FS 484.00 CLIP RBL 27 OTBD IS CRACKED. R & R CLIP AT FS 484, RBL 27 IAW REO 601R-53-41-059.

Part: FITTING — CRACKED (FUSELAGE) · airframe 18,725 hrs · 18,110 cycles

FS 484.00 CLIP LBL 27 OTBD IS CRACKED. R & R CLIP AT FS 484, LBL 27 IAW REO 53-41-059.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 18,725 hrs · 18,110 cycles

REAR PRESS BULKHEAD HAS A CRACK AT THE UPPER INBD EDGE OF THE LINTEL FITTING. REPAIRED REAR PRESS BULKHEAD AT LISTED FITTING IAW REO 601R-53-61-1230 REV F.

Part: GLOWSTRIP — BROKEN (CABIN) · airframe 18,166 hrs · 17,568 cycles

LEFT FLOOR AISLE EMER EXIT LIGHT, 3RD FROM FRONT BROKE. R & R EMER PHOTO LUMINESCENT MARKING LIGHT IAW AMM 33-51-01.

Part: LATCH — BROKEN (COCKPIT DOOR) · airframe 17,699 hrs · 17,078 cycles

FLIGHT DECK DOOR HOLD OPEN LATCH BROKEN. R & R FLIGHT DECK DOOR HOLD OPEN LATCH IAW AMM 25-31-01.

Part: DOOR — LACK OF LUBE (CABIN) · airframe 17,358 hrs · 16,728 cycles

MAIN CABIN DOOR HANDLE STICKS JUST BELOW THE FULL UP POSITION, PREVENTING DOOR FROM OPENING. PERFORMED LUBRICATION OF THE PAX DOOR IAW AMM 12-20-52. OPERATIONS CHECKED GOOD IAW AMM 52-11-00.

Part: LIGHT — DAMAGED (CABIN) · airframe 17,225 hrs · 16,584 cycles

RIGHT EMERGENCY AISLE LIGHT HAD DAMAGE AFT OF EXIT, PHOTO LUMINESCENT EMERGENCY FLOOR LIGHT. R & R PHOTO LUMINENSCENT MARKING LIGHT AFT OF EMERGENCY EXIT IAW AMM 33-51-01.

Part: SEAL — MISSING (FIRE BOTTLE) · airframe 17,078 hrs · 16,420 cycles

COCKPIT FIRE EXTINGUISHER SEAL MISSING. INSTALLED ANTI-TEMPERING SEAL ON FIRE EXTINGUISHER IAW MM 26-23-01.

Part: OXYGEN MASK — MISINSTALLED (COCKPIT) · airframe 23,222 hrs · 20,601 cycles

OBSERVER`S 02 MASK INSTALLED UPSIDE DOWN. CORRECTLY INSTALLED OBSERVER`S 02 STOWAGE BOX IAW AMM 35-11-15. OK FOR SERVICE.

Part: SEAL — MISSING (FLASHLIGHT) · airframe 16,565 hrs · 15,921 cycles

FLIGHT ATTENDANT FLASHLIGHT SEAL MISSING. RE-SEALED FLIGHT ATTENDANT FLASHLIGHT STRAP IAW AMM 25-60-00.

Part: WEB — DAMAGED (NLG WW) · airframe 15,716 hrs · 16,362 cycles

THE NLG WW UPPER WEB & CHANNELS DAMAGED. REPAIRED IAW EA CRJ253-02788.

Part: SPAR CAP — GOUGED (RT WING) · airframe 15,787 hrs · 15,154 cycles

RIGHT WING AFT SPAR LOWER CAP AT WS 143 IS GOUGED AT AFT EDGE 0.5 INCHES X 0.125 INCHES X 0.115 INCHES DEEP. REPAIRED IAW REO 601R57-21-2139.

Part: LIFE VEST — DAMAGED (COCKPIT) · airframe 15,762 hrs · 15,122 cycles

FIRST OFFICER'S LIFE VEST IS DAMAGED. R & R THE CO-PILOTS LIFE VEST IAW AMM 25-61-03.

Part: COVER — MISSING (CABIN) · airframe 15,671 hrs · 15,034 cycles

FLIGHT ATTENDANT`S CALL LIGHT COVER ON EMERGENCY EXIT SIGN MISSING. INSTALLED FLIGHT ATTENDANT`S CALL LIGHT COVER IAW AMM 33-51-14.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 15,602 hrs · 14,968 cycles

OIL PRESS GAUGE SHOWING ZERO INBOUND ABE. QRH FOLLOWED, ENG. WAS SHUT DOWN. EMERGENCY WAS DECLARED. FLT LANDED WITHOUT INCIDENT & TAXIED TO GATE.

Part: WIRE — CHAFED (CHART LIGHT) · airframe 15,217 hrs · 14,593 cycles

F/O'S YOLK CLIP STARTED SMOKING. FOUND F/O CHART LIGHT WIRES CHAFED AND RHEOSTAT SHORTED. R & R F/O CHART LIGHT ASSY IAW AMM 33-13-13. NO FURTHER DEFECTS FOUND. OPS CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 13,849 hrs · 13,248 cycles

FLIGHT ATTENDANT FLASHLIGHT FLIGHT ATTENDANT REPORTS INOPERABLE. REMOVED AND REPLACED FLASHLIGHT STRAP IAW AMM 25-61-01. OPS CHECK FLASHLIGHT GOOD AT THIS TIME IAW AMM 25-61-01. OK FOR SERVICE.

Part: LIFE VEST — UNSERVICEABLE (COCKPIT) · airframe 13,635 hrs · 13,039 cycles

CAPTAIN LIFE VEST BAG TORN. REMOVED AND REPLACED CAPTAIN LIFE VEST IAW AMM 25-60-03.

Part: LIGHT — BROKEN (COCKPIT) · airframe 13,629 hrs · 13,033 cycles

EMERGENCY EXIT LIGHT ASSEMBLY ON FRONT WINDSCREEN IS BROKEN. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSY IAW AMM 33-51-10.

Part: LIFE VEST — UNSERVICEABLE (COCKPIT) · airframe 13,493 hrs · 12,896 cycles

OBSERVER LIFE VEST BAG TORN. REMOVED AND REPLACED OBSERVERS LIFE VEST IN ACCORDANCE WITH AMM 25-61-03.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 13,164 hrs · 12,572 cycles

FS 280 UPPER AFT ANGLE CRACKED AT RBL 9/LBL 9 AND 4 CLIPS CRACKED. REPAIRED IAW BOMBARDIER REO 601R-53-11-136A.

Part: WEB — CRACKED (FUSELAGE) · airframe 13,164 hrs · 12,572 cycles

FS 280 LOWER WEB CRACKED JUST OUTBOARD OF LBL/RBL 9. REPAIRED IAW BOMBARDIER REO 601R-53-11-171D.

Part: BULKHEAD — CHAFED (FUSELAGE) · airframe 13,164 hrs · 12,572 cycles

FS 621 PRESSURE BULKHEAD CHAFED 9 PLACES ABOVE WL 73.5 0.005" - 0.009" DEEP. REPAIRED IAW BOMBARDIER REO 601R-53-61-2155.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 12,870 hrs · 12,279 cycles

PASSENGER DOOR AFT DRAG ANGLE CRACKED. REPAIRED PASSENGER DOOR AFT DRAG ANGLE IAW REO 601R-52-11-513.

Part: CONTROL HANDLE — MALFUNCTIONED (MLG) · airframe 12,167 hrs · 11,463 cycles

ON TAKEOFF, WHEN THE LANDING GEAR HANDLE WAS SELECTED UP, 1 ANTI SKID INBD, 2 PARKING BRAKE SOV CAUTION MESSAGES ANNUNCIATED. LANDING GEAR, ALL 3 REMAINED DOWN. ON APPROACH, BACK TO DEPARTURE, WHEN LANDING GEAR HANDLE SELECTED DOWN, CAUTION WENT AWAY. REPLACED LDG CONTROL HANDLE IAW AMM 32-31-01. FUNCTIONAL TEST GOOD REF MM 409, NR 401370 FOR DETAILS.

Part: CONTROL HANDLE — MALFUNCTIONED (MLG) · airframe 12,139 hrs · 11,428 cycles

SHORTLY AFTER TAKEOFF, AFTER SELECTING LANDING GEAR UP, RECEIVED "A SKID INBD" CAUTION AND "PARK BRAKE SOV" CAUTION DISPLAYED. LANDING GEAR REMAINED DOWN. RAN THE NON-NORMAL CHECKLIST. WHEN SELECTING LANDING GEAR HANDLE DOWN CAUTIONS WENT AWAY. PERFORMED CONTINUITY CHECKS OF LANDING GEAR HANDLE. NO DEFECTS FOUND. PERFORMED EXTENSION RETRACTION CHECKS IAW AMM 32-30-00. COULD NOT DUPLICATE FAULT. NOTED DI11 OFF CODE LATCHED ON PSEU (LANDING GEAR HANDLE/WIRING TO PSEU). REPLACED LANDING GEAR CONTROL HANDLE, IAW AMM 32-31-01. ALL CHECKS GOOD AT THIS TIME. ACFT OK FOR SERVICE. CLEARED PSEU MEMORY. ALSO REF FIM 32-60-00, BLOCK 6.

Part: PCU — FAILED (RUDDER) · airframe 12,118 hrs · 11,401 cycles

ON GROUND AFTER LANDING "HYD 1 LO PRESS" ILLUMINATED FOLLOWED NON NORMAL CHECKLIST. HYD FLUID NR 1 WAS EMPTY HYD, SYSTEM PRESSURE HAD SOME PRESSURE WHEN WE PULLED UP HYD PAGE ON EICAS AND BLED DOWN TO 0PSI. SHUTDOWN ENGINE NR 1 PUMP RAN FOR LESS THAN 30 SEC WITH PRESSURE. NOT SURE HOW LONG ENGINE RAN NO FLUID BUT ENGINE WAS SHUTDOWN WITHIN ABOUT 5 MINUTES OF RECIEVING THE CAUTION FOR THE "HYD 1 LOW PRESS. FOUND RUDDER PCU NR 1 FAILED REMOVED & REPLACED IAW AMM 27-23-01 OPS CHECKS GOOD AT THIS TIME

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 10,108 hrs · 9,062 cycles

NOTED EXTERIOR EMERGENCY LIGHT 1 INOP. RELAMPED EXTERIOR EMERGENCY LIGHT 1 IAW AMM 33-51-21 OP CHECKED IAW TASK 33-51-00-710-801.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 9,844 hrs · 8,766 cycles

DURING JOB CARD 33-900-001 EMERGENCY LIGHT FOR AIRSTAIR DOOR EXTERIOR IS INOP. REPLACED AIRSTAIR EXTERNAL EMERGENCY EXIT LAMP IAW AMM 33-51-21 P/N ON/OFF 1317. OPS CHECK GOOD.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 9,464 hrs · 8,382 cycles

DURING HEAVY CHECK THE LT INBD FLAP PN 601R14002-1, SN SB/RJ/1013 WAS FOUND TO HAVE A DENT IN THE LOWER SKIN AT WS 68.138, 19.125" FROM THE T/E AND MEASURES 1.313" X 1.125" X 0.055" DEEP. DENT ON LT INBD FLAP WITHIN LIMITS TO REPAIR IAW SRM 57-52-00, PERFORMED HFEC OF DENT AND CUTOUT DAMAGED AREA. IAW NDTM PART 6 5 3-00 AND PERFORMED COMPLETE REPAIR IAW SRM 57-52-00-02-03 REPAIR NR3 AND EO NR C57057 & PAINTED TOPCOAT IAW SRM 51-25-01 FURTHER DETAILS SEE CONT CARDS 072777 & 072796.

Part: OIL SYSTEM — OVERSERVICED (APU)

WHILE APPROACHING KFAR AT 8000 FT CREW SWITCHED TO APU BLEEDS. THEN OBSERVED A LAV SMOKE INDICATION, AND PUFFS OF SMOKE IN COCKPIT AND CABIN. CREW WENT THROUGH THE NON-NORMAL CHECKLIST AND INFORMED ATC OF AN EMERGENCY SITUATION. EMERGENCY EQUIPMENT WAS DISPATCHED. FLIGHT LANDED WITHOUT INCIDENT. ARFF CREWS UPON OPENING CARGO BAY OBSERVED SMOKE IN CARGO BAY. APU INOP, CAUSES SMOKE THROUGH BLEED WHEN USED. CHECKED OIL LEVEL FOUND TO BE OVERSERVICED, RAN A/C TO GET PROPER OIL LEVEL CHECK AND DUPLICATED PROBLEM. CHECKED OIL AGAIN AND FOUND TO BE OVERSERVICED, REMOVED OIL TO PROPER LEVEL AND RAN A/C AGAIN. NO DEFECTS NOTED WITH PACKS ON AND OFF.