N430AW

Part: NONE — CORRODED (AVIONICS DOOR) · corrosion level 2 · airframe 40,336 hrs · 38,944 cycles

FOUND PITTING AND EXFOLIATION CORROSION ON ALL 4 SEAL RETAINERS P/N CC670-38663-5, CC670-38675 ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED AND REPLACED ALL4 SEAL RETAINERS-3,CC670-38675-3,CC38662-5 FOR THE MAIN AVIONICS DOOR P/N 601R38346-83

Part: SEAT TRACK — CORRODED (FS 529) · corrosion level 2 · airframe 40,336 hrs · 38,944 cycles

RH SIDE SEAT RAIL-SEAT TRACK AT FS 529-FS 559 HAS MULTIPLE AREAS CORROSION. ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED CORROSION FROM RH SIDE SEAT RAIL SEAT TRACK IAW CRJ-200 SRM 51-21-06 AND 51-21-49, REPAIR WITHIN LIMITS

Part: SWITCH — MALFUNCTIONED (MACH STAB TRIM) · airframe 39,791 hrs · 38,370 cycles

MACH TRIM STAB TRIM CASS MESSAGES IN FLT. C/W QRH, MESSAGES REMAINED. OCCURRED DURING CRUISE AFTER NORMAL TAKE OFF. C/W QRH AND SET FLAPS TO 20. CONTROLS DIFFICULT TO MOVE BUT FELT SAFE TO PROCEED. LANDED WITHOUT ISSUES, SMOOTH LANDING BUT DID DECLARE AN EMERGENCY AS PRECAUTION BEFORE LANDING. AIRCRAFT REMOVED FROM SERVICE. R&R PITCH DISCONNECT SWITCH IAW AWAC SUP 10-048C OPS CHECKS GOOD.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 38,943 hrs · 37,463 cycles

AFT PRESSURE BULKHEAD IS CRACKED AT THE LINTEL FITTING. "AIRCRAFT REMOVED FROM SERVICE" REPAIRED AFT PRESSURE BULKHEAD AT LINTEL FITTING IAW REO 601R-53-61-1230 REV-F.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 38,943 hrs · 37,463 cycles

AFT PRESSURE BULKHEAD IS CRACKED AT THE TOP END OF THE CARGO DOOR TRACK. "AIRCRAFT REMOVED FROM SERVICE" REPAIRED AFT PRESSURE BULKHEAD IAW BOMBARDIER REO 601R-53-61-1541 REV. F.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 38,943 hrs · 37,463 cycles

AFT PRESSURE BULKHEAD IS CRACKED AT THE RBL 27.5 APPROX WL112 "AIRCRAFT REMOVED FROM SERVICE" REPAIRED CRACKED BULKHEAD IAW BOMBARDIER REO 601R53-61-1285 REV E

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 38,943 hrs · 37,463 cycles

AFT PRESURE BULKHEAD IS CRACKED AT BL O IN THE SPLICE WEB AT APPROXIMATELY WL 140. "AIRCRAFT REMOVED FROM SERVICE" REMOVED AND REPLACED SPLICE WEB IAW CRJ-200 SRM 51-42-06

Part: ANGLE — CRACKED (PAX DOOR) · airframe 38,943 hrs · 37,463 cycles

PASSENGER DOOR POWER ASSIST MOTOR MOUNT ANGLE IS CRACKED. "AIRCRAFT REMOVED FROM SERVICE" REMOVED AND REPLACED MOUNT ANGLE IAW CRJ200 SRM 51-42-06 & 51-42-13.

Part: WIRE HARNESS — DEFECTIVE (NLG STEERING) · airframe 38,610 hrs · 37,131 cycles

STEERING INOP CAUTION IN FLIGHT. QRH HAS US TURN NWS SWITCH OFF. MSG EXTINGUISHED. NO NWS ON GROUND REGARDLESS OF NWS SWITCH POSITION. AIRCRAFT REMOVED FROM SERVICE R&R NLG STEERING HARNESS IAW CMM 32-60-01-R3, OPS TEST GOOD IAW 32-51. REF MX WORK CARD #4 FOR GEAR SWING.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 36,865 hrs · 35,457 cycles

DURING FERRY FLIGHT FROM ORD TO MKE, CREW REPORTED: AFTER TAKEOFF FLAPS FAIL AND STAB AND MACH TRIM CAUTION MSGS. FLAPS FAIL AT 8 DEGREES. CW QRH. STAB AND MACH TRIM RESET OK. LANDING WEIGHT 36000, MAX BTMS 2112. CREW PERFORMED AND AIR RETURN TO ORD FOR FURTHER TROUBLESHOOTING/REPAIR.

Part: ANGLE — CRACKED (BS 280) · airframe 35,658 hrs · 34,274 cycles

ANGLE CRACKED AT BS 280, LBL9, AFT OF THE BEAM. REPLACED THE ANGLE IAW SRM 51-42-06, AND 51-42-21.

Part: INTERCOSTAL — CRACKED (BS 621) · airframe 35,397 hrs · 34,043 cycles

AFT PRESSURE BULKHEAD AFT FACE HAS A CRACKED INTERCOSTAL AT STRINGER 14L. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-42-21, AND SRM 51-42-06.

Part: PLATE — CRACKED (STEP) · airframe 35,397 hrs · 34,043 cycles

CARGO STEP PLATE IS CRACKED AND HAS BROKEN HINGE TANGS.

Part: RISER — CRACKED (PAX DOOR) · airframe 35,397 hrs · 34,043 cycles

PAX DOOR AFT RISER IS CRACKED BY LOWER FIXED STEP.

Part: STEP — CRACKED (PAX DOOR) · airframe 35,397 hrs · 34,043 cycles

PAX DOOR UPPER STAIR AFT WEB REPAIR ANGLE IS CRACKED. REPLACED THE REPAIR ANGLE IAW REO 601R-52-11-279 REV-NC.

Part: STEP — CRACKED (PAX DOOR) · airframe 35,397 hrs · 34,043 cycles

PAX DOOR UPPER STAIR WEB, FWD REPAIR ANGLE IS CRACKED. REPLACED THE REPAIR ANGLE IAW REO 601R-52-11-279 REV-NC.

Part: INTERCOSTAL — CRACKED (BS 621 BULKHEAD) · airframe 35,397 hrs · 34,043 cycles

AFT PRESSURE BULKHEAD AFT FACE HAS A CRACKED INTERCOSTAL AT STRINGER 13L. REPLACED THE INTERCOSTAL IAW SRM 51-42-00, AND 51-42-21.

Part: LANDING — CRACKED · airframe 35,397 hrs · 34,043 cycles

PANEL 446BL LANDING IS CRACKED. REPLACED LANDING IAW CMM 20-42-06.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,397 hrs · 34,043 cycles

FLOORBEAM LBL 9 BETWEEN FS 589 AND FS 605 CORRODED.

Part: ANGLE — CRACKED (BS 621-624) · airframe 35,397 hrs · 34,043 cycles

BS 621 TO 624, OBLIQUE ANGLE AT STRINGER 15R IS CRACKED. REPLACED THE OBLIQUE ANGLE IAW SRM 51-42-21.

Part: BRACKET — CRACKED (LT MLG WW) · airframe 35,397 hrs · 34,043 cycles

LT MLG WW BRAKE PRESSURE TRANSDUCER BRACKET CRACKED. REPLACED.

Part: BRACKET — CRACKED (RT MLG WW) · airframe 35,397 hrs · 34,043 cycles

RT MLG WW BRAKE PRESSURE TRANSDUCER HYD LINES BRACKET IS CRACKED. REPLACED.

Part: GUSSET — CRACKED (EQUIP RACK) · airframe 35,397 hrs · 34,043 cycles

RIGHT BS 719, GUSSET FOR THE NR 2 HYDRAULIC SYSTEM RACK IS CRACKED. REPLACED THE GUSSET IAW SRM 51-42-06.

Part: FITTING — CRACKED (FUSELAGE) · airframe 35,397 hrs · 34,043 cycles

FLOORBEAM CLIP AT FS 484 AND RBL 27 CRACKED. REPLACED.

Part: FITTING — CRACKED (FUSELAGE) · airframe 35,397 hrs · 34,043 cycles

FLOORBEAM CLIP AT FS 484 AND RBL 36 CRACKED. REPLACED.

Part: BRACKET — CRACKED · airframe 35,397 hrs · 34,043 cycles

RT MLG WW BRAKE PRESSURE TRANSDUCER BRACKET IS CRACKED. REPLACED.

Part: DRAG ANGLE — CRACKED (BS 349) · airframe 35,397 hrs · 34,043 cycles

PAX DOOR AFT RISER DRAG ANGLE IS CRACKED. REPAIRED THE DRAG ANGLE IAW REO601R-52-11-513 REV-B.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,397 hrs · 34,043 cycles

RT NR 4 FLOOR SEAT TRACK CORRODED. REPLACED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,397 hrs · 34,043 cycles

RT NR 1 FLOOR SEAT TRACK CORRODED. REPLACED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,397 hrs · 34,043 cycles

RT FLOOR NR 2 SEAT TRACK CORRODED. REPLACED.

Part: CHANNEL — CRACKED (EQUIP RACK) · airframe 35,397 hrs · 34,043 cycles

RIGHT HYDRAULIC SYSTEM, NR 2 EQUIPMENT RACK, C-CHANNEL CRACKED. REPAIRED CHANNEL IAW REO 601R-53-62-031 REV-A.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 35,397 hrs · 34,043 cycles

BATHTUB FLOOR SUPPORT FITTING AT FS 431 AND LBL 9 CRACKED. REPLACED BATHTUB FITTING AT FS 431 AND LBL 9 IAW SRM 51-42-06 AND 51-42-21.

Part: GUSSET — CRACKED (CRACKED) · airframe 35,397 hrs · 34,043 cycles

RIGHT SIDE HYDRAULIC SYSTEM, NR 2 EQUIPMENT RACK GUSSET IS CRACKED. REPLACED GUSSET AT BS 736, IAW SRM 51-42-06.

Part: BEAM — CRACKED (BS 409 BULKHEAD) · airframe 35,397 hrs · 34,043 cycles

BS 409+128 FWD BULKHEAD VERTICAL BEAM AT RBL18 IS CRACKED. REPAIRED VERTICAL BEAM IAW REO601R-53-41-056 REV-F.

Part: BEAM — CRACKED (BS 409) · airframe 35,397 hrs · 34,043 cycles

BS 409+128 VERTICAL BEAM AT RBL 27 HAS A VISUAL INDICATION OF A CRACK ON LOWER INBD SIDE. REPAIRED THE VERTICAL BEAM IAW REO 601R-53-41-056, REV-F.

Part: CHANNEL — CRACKED (CARGO DOOR) · airframe 35,397 hrs · 34,043 cycles

CARGO DOOR CAM TRACK SUPPORT LOWER CHANNEL AT FS 574 CRACKED. REPLACED.

Part: FRAME — CRACKED (BS 605) · airframe 35,397 hrs · 34,043 cycles

FRAME BS 605 FLANGE IS CRACKED AT STRINGER 9L. REPLACED THE FRAME SECTION IAW SRM 51-42-06, 51-42-21, AND REO 601R-53-61-6504, REV-.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 35,397 hrs · 34,043 cycles

LEFT INBD FLAP LOWER SKIN HAS MULTIPLE DENTS. REPLACES THE FLAP LOWER SKIN IAW SRM 51-42-13.

Part: FRAME — CHAFED (FUSELAGE) · airframe 35,397 hrs · 34,043 cycles

PERFORM PERMANENT REPAIR FS718, STR17R & STR 16R. PERFORMED PERMANENT REPAIR IAW EA CRJ253-00905 REV-IR.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 35,035 hrs · 33,670 cycles

EMERGENCY LIGHT WILL NOT ILLUMINATE PAST ROW 8. FOUND LOW VOLTAGE AT SFT CABLE. R & R THE NR 4 INVERTER IAW AMM 33-51-07, OPS CHECKED GOOD.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHTS) · airframe 34,801 hrs · 33,438 cycles

DURING PRE-FLIGHT ACCEPTANCE, CREW REPORTED THAT THE FLOOR EMERGENCY LIGHTING WILL NOT ILLUMINATE FROM ROW 9 AFT. SECURED THE CONNECTOR AT ROW 12 IAW AMM 33-51-00, OPS CHECKED GOOD.

Part: NONE — NONE · airframe 34,717 hrs · 31,439 cycles

4261 FLOOR PATH EMERGENCY LIGHTS WILL NOT ILLUMINATE FROM ROW 8 TO 13 CW OP TEST OF EMERG LIGHTS IAW AMM SUPP 16-374A AND VISUAL INSP IAW AMM 33-51-01 ACFT GOOD FOR SERVICE

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHTS) · airframe 34,645 hrs · 33,292 cycles

FLOOR EMERGENCY LIGHTS PAST ROW 8 WILL NOT ILLUMINATE. INSPECTED EMERGENCY LIGHTING AND FOUND CONNECTOR LOOSE AT ROW 12. SECURED THE CONNECTOR IAW AMM 33-51-00, OPS CHECKED GOOD.

Part: WIRE HARNESS — LOOSE (EMERGENCY LIGHTS) · airframe 34,608 hrs · 33,262 cycles

AFT HALF OF EMERERGENCY FLOOR LIGHTING DOES NOT ILLUMINATE. INSPECTED AND FOUND ROW 12 WIRE HARNESS ASSY LOOSE. ADJUSTED THE WIRE HARNESS, OPS CHECKED GOOD IAW AMM 33-51-00

Part: WIRE HARNESS — DEFECTIVE (CABIN) · airframe 34,580 hrs · 33,240 cycles

AFT FLOOR EMERGENCY LIGHT DO NOT TEST (ROW 8 AND AFT ). REMOVED AND REPLACED AFT HARNESS AND CONNECTIONS IAW AMM 33-50-00. OPS CHECK GOOD.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 34,343 hrs · 33,021 cycles

EMERGENCY LIGHT INOPERATIVE AFT OF ROW 9. INSPECTED THE EMERGENCY LIGHT AND FOUND A LOOSE CONNECTION. CONNECTED AND PERFORMED AN OPS CHECK IAW AMM 33-51-00, OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,072 hrs · 30,478 cycles

LAST SECTION OF EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE, ROW 9-12 REPORTED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,427 hrs · 31,210 cycles

LOWER LEVEL EMERGENCY EXIT LIGHTS OUT, FROM ROW 9 & AFT.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 32,427 hrs · 31,210 cycles

FLIGHT 3860. LOWER LEVEL EMERGENCY EXIT LIGHTS OUT, FROM ROW 9 & AFT. CONNECTED CONNECTOR ROW 12 & OPS CHECK IAW 12-032 & AMM 33-51-00.

Part: HANDLE — UNKNOWN (SERVICE DOOR) · airframe 32,406 hrs · 31,188 cycles

SERVICE DOOR OUTER HANDLE WILL NOT OPEN.

Part: HANDLE — LACK OF LUBE (SERVICE DOOR) · airframe 32,406 hrs · 31,188 cycles

SERVICE DOOR OUTER HANDLE WILL NOT OPEN. CLEANED AND LUBED SERVICE DOOR HANDLE PER AMM 52-41-02 OPS CHECKED GOOD AT THIS TIME.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,175 hrs · 30,978 cycles

EMERGENCY FLOOR TRACK LIGHT FROM ROW 1 TO 8 ILLUMINATED, ROW 8 AND HIGHER DO NOT ILLUMINATE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,032 hrs · 30,851 cycles

FLOOR LEVEL EMER LIGHTS ROW 8 & AFT WILL NOT ILLUMINATE.

Part: DOOR SEAL — DIRTY (SERVICE DOOR) · airframe 31,930 hrs · 30,757 cycles

GROUND CREW REPORTED THEY WERE UNABLE TO OPEN THE SERVICE DOOR FROM OUTSIDE THE ACFT. CLEANED & LUBED SERVICE DOOR AS REQUIRED. OPERATIONS CHECKED GOOD.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 31,899 hrs · 30,721 cycles

4070 RT REV UNLOCKED, AMBER CAUTION MSG IN FLT INTERMITTENTLY AT 12K FEET. IN DESCENT CAUTION WAS RECEIVED AGAIN & REMAINED FOR THE REST OF THE FLIGHT. NO YAWING MOTION.

Part: FAIRING — DEPARTED (RT EXHAUST) · airframe 31,698 hrs · 30,539 cycles

RIGHT ENG LOWER EXHAUST NOZZLE ATTACHING HARDWARE COVER, ON THE EXHAUST NOZZLE FAIRING, DEPARTED THE ACFT IN FLIGHT & CAUSED A 2 5/8 INCH CRACK IN THE EXHAUST NOZZLE FAIRING. R & R RT ENG EXHAUST NOZZLE FAIRING IAW AMM 78-11-01. OPERATIONS CHECKED GOOD.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,600 hrs · 30,441 cycles

FRAME 349 AFT SIDE, BETWEEN STRINGER 27 & 26L, AREA HAS CORROSION, R & R.

Part: FRAME — CHAFED (FUSELAGE) · airframe 31,600 hrs · 30,441 cycles

FRAME AT 718.00, BETWEEN STRINGER 17R & 16R IS CHAFED BY HYD PUMP BRAIDED LINE, TEMP REPAIRED.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 31,600 hrs · 30,441 cycles

LEFT FWD E & E BAY FLOOR AT FS 193 CRACKED, REPAIRED.

Part: SKIN — DAMAGED (LT WING) · airframe 31,600 hrs · 30,441 cycles

LT WING FUEL DRAIN NEXT TO BOOST PUMP ATTACH HOLES ARE OVAL, REPAIRED.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,600 hrs · 30,441 cycles

FRAME 333 AFT & FWD SIDES, BETWEEN STRINGER 23R & 22R CORRODED, REPLACED.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,600 hrs · 30,441 cycles

CARGO BEAM AT FS 616.00, RBL 27, INBD FLANGE HAS A CORRODED FASTENER HOLE, REPAIRED.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 31,600 hrs · 30,441 cycles

INTERCOSTAL C CHANNEL ON LT AFT SIDE OF AFT PRESS BULKHEAD AT STRINGER 14L IS CRACKED, REPAIRED.

Part: SKIN — GOUGED (RT AILERON) · airframe 31,600 hrs · 30,441 cycles

UPON REMOVAL OF PANEL 698LT, FOUND 3 LARGE GOUGES ON UPPER CTR LE OF RT AILERON.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 31,600 hrs · 30,441 cycles

FLIGHT DECK FLOOR LANDING ANGLE ON THE FWD SIDE OF 280 BEAM IS CRACKED AT BOTH LT & RT SIDES IN THE VERY FWD E & E BAY. R & R FLOOR LANDING ANGLE IAW SRM 51-42-06 & 51-42-21.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,600 hrs · 30,441 cycles

INTERCOSTAL JUST TO THE RT OF STRINGER 27 HAS CORROSION, BETWEEN FRAME 394.00 & 409.00, IN THE FWD E & E BAY. R & R CORRODED INTERCOSTAL WITH SERVICEABLE INTERCOSTAL IAW SRM 51-42-06 & 51-42-21.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,600 hrs · 30,441 cycles

INTERCOSTAL JUST LT OF STRINGER 27 HAS CORROSION, BETWEEN FRAMES 394.00 & 409.00 IN THE FWD E & E BAY. R & R CORRODED INTERCOSTAL IAW SRM 51-42-06 & 51-42-21.

Part: RETAINER — BENT (EMERGENCY EXIT) · airframe 29,491 hrs · 28,396 cycles

FLIGHT 4010. FLIGHT CREW REPORTED EVACUATION OF ACFT OUT OF ALL 4 EMERGENCY EXITS DUE TO SMOKE FROM PAX LUGGAGE UNDER SEAT 1DF. FLIGHT ATTENDANT USED FIRE EXTINGUISHER. CVR & FDR CB'S HAVE BEEN PULLED & COLLARED, CBP1 C9 & K2, CBP4 D7. IAW 282817 2 THRU 2828201 FOR ALL WORK PERFORMED FOUND BURN MARKS UNDER SEAT 1D & CTR AISLE AT ROW 2 CONTAINED TO CARPET ONLY. ALSO FOUND RT FOUND RT OVERWING EXIT SEAL RETAINER BENT. R & R FDR & CVR IAW 282820 2 ACFT OK FOR FERRY.

Part: TRUNNION — DAMAGED (MLG) · airframe 26,699 hrs · 25,705 cycles

DURING COLD WORKING OF THE MLG TRUNNION LOWER FLANGE, FOUND ONE EACH OVERSIZE HOLE ON THE RT SIDE. REPAIRED IAW REO 57-21-2131 DATED 2014-03-16.

Part: RIB — CRACKED (LT WING) · airframe 26,699 hrs · 25,705 cycles

LEFT MLG WW BATTERY RIB CRACKED. REPAIRED LT BATTERY RIB IAW REO 601R-57-51-046 REV B DATED 2002-02-28 REPAIR NR 2.

Part: THRESHOLD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,699 hrs · 25,705 cycles

SERVICE DOOR THRESHOLD PLATE CORRODED. R & R WITH SERVICEABLE PART PN 601R38957-19 IAW CRJ200 SRM 51-40-11 & 51-42-06.

Part: ANGLE — CRACKED (RT WING) · airframe 26,699 hrs · 25,705 cycles

RIGHT WING LE UPPER TRANSITION ANGLE UNDER PANEL 620ML CRACKED. R & R WITH SERVICEABLE PART PN 601R120371-30 IAW CRJ200 SRM 51-40-11 & 51-42-15.

Part: PANEL — CRACKED (PAX DOOR) · airframe 26,699 hrs · 25,705 cycles

PASSENGER DOOR STAIR SUPPORT FWD PANEL CRACKED AT LOWER CORNER OF UPPER STEP. REPAIRED IAW REO 601R-52-11-702 REV C DATED 2010-03-09 ZONE 2.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,699 hrs · 25,705 cycles

PASSENGER DOOR FWD HANDLE RECESS FITTING IN SILL AREA IS CORRODED. R & R WITH SERVICEABLE PART PN 601R31527-217 IAW CRJ 200 SRM 51-40-11 & 51-42-06.

Part: HANDLE — CRACKED (PAX DOOR) · airframe 26,699 hrs · 25,705 cycles

PASSENGER DOOR INNER HANDLE IS CRACKED AT THE ROLL PIN HOLE. REMOVED UNSERVICEABLE INNER DOOR HANDLE IAW CRJ 200 SRM 51-41-02. INSTALLED SERVICEABLE INNER DOOR HANDLE IAW CRJ 200 SRM 51-41-02.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,699 hrs · 25,705 cycles

PAX DOOR LOWER SILL CORRODED. REMOVED LOWER SILL & REPLACED WITH SERVICEABLE SILL IAW SRM 51-42-06 & 51-42-21.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,699 hrs · 25,705 cycles

CABIN FLOOR STRUCTURE RBL 9 SEAT TRACK FROM FS 559+100 TO 563 HAS CORROSION AROUND SCREWS & ONE EACH GOUGE. REMOVED OLD TRACK & FABRICATED NEW TRACK SECTION DRILL & COUNTERSINK NEW HOLES FOR INSTALLATION & INSTALLED IAW CRJ 200 SRM 51-40-11 & AMM 53-01-11.

Part: STEP — DAMAGED (PAX DOOR) · airframe 26,699 hrs · 25,705 cycles

COMPLIED WITH AWAC CARD 4DMI16423 REPAIR PAX DOOR LOWER AFT CORNER 601R-52-11-2144A. REPAIRED PAX DOOR AFT CORNER OF UPPER STEP IAW REO 601R-52-11-279 REV NC DATED 2001-10-18.

Part: PANEL — CRACKED (PAX DOOR) · airframe 26,699 hrs · 25,705 cycles

PASSENGER DOOR STAIR SUPPORT AFT SIDE PANEL CRACKED AT LIGHTNING HOLE UNDER GAS SHOCK SUPPORT. REPAIRED IAW REO 601R-52-11-702 REV C DATED 2010-03-09.

Part: WEB — CRACKED (ENTRY DOOR) · airframe 26,699 hrs · 25,705 cycles

MAIN ENTRY DOOR FWD WEB IS CRACKED IN LOWER CORNER OF RISER. REMOVED CRACK IAW SRM 51-12-00.

Part: DRAG ANGLE — CRACKED (RT MLG WW) · airframe 26,699 hrs · 25,705 cycles

RIGHT MLG WW DRAG ANGLE CRACKED. R & R WITH SERVICEABLE PART PN 600-10389-2 IAW CRJ200 SRM 51-40-11 & 51-42-21.

Part: DRAG ANGLE — CRACKED (RT MLG WW) · airframe 26,699 hrs · 25,705 cycles

RIGHT MLG WW DRAG ANGLE FWD ATTACH ANGLE CRACKED. R & R WITH SERVICEABLE PART IAW CRJ 200 SRM 51-40-11, 51-24-21 & 51-42-21.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 26,699 hrs · 25,705 cycles

LEFT FLOOR SEAT TRACK GOUGED AT FS 409+16. R & R TRACK SECTOR IAW CRJ 200 SRM 51-40-11 & AMM 53-01-11.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 26,699 hrs · 25,705 cycles

FLOOR BEAM INBD & OTBD ATTACH CLIPS AT LBL 9 & FS 280 ARE CRACKED. R & R CLIPS WITH SERVICEABLE PARTS IAW REO 601R-53-11-171 REV D DATED 13-FEB-07.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,699 hrs · 25,705 cycles

LEFT SIDE SEAT RAIL CORRODED FROM FS 546 TO 555+80. R & R LT SIDE SEAT RAIL WITH SERVICEABLE PART IAW CRJ 200 SRM 51-40-11 & AMM 53-01-11.

Part: SEAL — CRACKED (SPOILER) · airframe 26,699 hrs · 25,705 cycles

FLIGHT SPOILER SUPPORT INBD METAL SEAL ON RT WING TE IS CRACKED. R & R WITH SERVICEABLE PART PN 601R10226-132 IAW CRJ 200 SRM 51040-11 & 51-42-06.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 26,699 hrs · 25,705 cycles

FLOOR BEAM INBD & OTBD ATTACH CLIPS AT RBL 9 & FS 280 CRACKED. R & R CLIPS WITH SERVICEABLE PART IAW REO 601R-53-11-171 REV D DATED 13-FEB-07.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 26,699 hrs · 25,705 cycles

AIRCRAFT GND POWER PLUG SUPPORT STRUCTURE CRACKED. R & R WITH NEW SERVICEABLE SUPPORT STRUCTURE IAW SRM 51-42-13 & 51-42-21.

Part: FITTING — CRACKED (FUSELAGE) · airframe 26,699 hrs · 25,705 cycles

CLIPS CRACKED AT STRINGER 3L & FS 280. R & R INBD & OTBD CLIPS AT FS 280 ON STRINGER 3L IAW CRJ 200 SRM 51-40-11 & 51-42-06.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,699 hrs · 25,705 cycles

FLOOR SEAT TRACK CORRODED AT RBL 9 FROM FS 559+80 TO 559+94. R & R SEAT TRACK WITH SERVICEABLE PART IAW CRJ200 SRM 51-40-11.

Part: DRAG ANGLE — CRACKED (RT MLG WW) · airframe 26,699 hrs · 25,705 cycles

LG MLG WW DRAG ANGLE CRACKED AT AFT END. R & R ANGLE WITH SERVICEABLE PART IAW CRJ200 SRM 51-40-11 & 51-42-21.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,699 hrs · 25,705 cycles

RIGHT SIDE SEAT RAIL CORRODED FS 449 TO 499. R & R RT SIDE SEAT RAIL FS 449 - 499 WITH SERVICEABLE PART IAW CRJ200 SRM 51-40-11 & AMM 53-01-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,699 hrs · 25,705 cycles

RIGHT SIDE SEAT RAIL CORRODED FS 546 TO 559+80. R & R RT SIDE SEAT RAIL FS 546 TO 559+80 WITH SERVICEABLE PART IAW CRJ 200 SRM 51-40-11.

Part: FITTING — CRACKED (FUSELAGE) · airframe 26,699 hrs · 25,705 cycles

RIGHT BUTT LINE 27 CLIP AT FS 484 CRACKED. R & R WITH SERVICEABLE CLIP IAW CRJ200 SRM 51-40-11 & 51-42-21.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,699 hrs · 25,705 cycles

SEAT TRACK LBL 9 HAS CORROSION & WEAR MARKS AT FS 364. R & R SEAT TRACK ON LBL 9 FROM FS 364 TO 396 IAW CRJ 200 SRM 51-40-11 & AMM 53-01-11.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,699 hrs · 25,705 cycles

PAX DOOR LOWER SILL CORRODED. REMOVED CORRODED SILL & INSTALLED NEW SERVICEABLE SILL IAW SRM 51-42-06 & 51-42-21.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 26,699 hrs · 25,705 cycles

AIRCRAFT GND POWER PLUG MOUNT STRUCTURE CRACKED AT SCREW HOLE. R & R WITH SERVICEABLE PART PN 600-33283-33 IAW CRJ200 SRM 51-40-11, 51-42-13 & 51-42-21.

Part: SEAL — DAMAGED (E&E DOOR) · corrosion level 2 · airframe 26,699 hrs · 25,705 cycles

AVIONICS BAY DOOR SEAL IS WORN, TORN & SEAL RETAINER IS BENT& CORRODED. R & R WITH SERVICEABLE PARTS PN CC670-38662-5, CC670-38663-5, CC670-38674-3 & CC670-38675-3 IAW CRJ 200 SRM 51-40-11 & 51-42-06.

Part: TRIM SWITCH — FAULTY (COCKPIT) · airframe 26,652 hrs · 25,661 cycles

STAB TRIM RUNAWAY ON FINAL, AUTOPILOT WAS OFF, FLAPS WERE 30 DEGREES, USED CAPTAIN'S PITCH TRIM DISCONNECT. IAW REPLACED CAPTAIN`S YOKE STRAP TRIM SWITCH, OPERATIONS CHECKED GOOD IAW AMM 27-40-00.

Part: EJECTOR — BLOCKED (FUEL SYSTEM) · airframe 24,366 hrs · 23,438 cycles

AFTER TAKEOFF AT 1500 FEET RECEIVED L LOW FUEL PRESS, L EJECTOR CAUTION, ENGINE VIBRATIONS, ENGINE SURGE, NORMAL LANDING. ENGINE OPERATED NORMALLY AFTER LEVELING OFF. INSPECTED FUEL TANKS AND FOUND BLOCKAGE IN SCAVENGE EJECTOR. REMOVED BLOCKAGE. C/W OPS CHECK. NO DEFECTS NOTED.

Part: PUMP — MALFUNCTIONED (LT ENGINE) · airframe 24,366 hrs · 23,437 cycles

DURING CLIMBOUT, LOSS OF POWER ON LEFT ENGINE (LOW FUEL LOW PRESS MESSAGE) N2 DROP 15% WITH VIBRATION AND YAW TO LEFT (LT MAIN EJECTOR) MESSAGE, POWER UP, LOSS OF POWER 3X. SMOOTHED OUT (LOW FUEL, LOW PRESS ON LANDING). REMOVED AND REPLACED LEFT ENGINE FUEL PUMP AND FUEL CONTROL, FUEL PUMP SHAFT HAD EXCESS PLAY.

Part: OIL SYSTEM — OVERSERVICED (APU) · airframe 23,338 hrs · 22,417 cycles

AT FL 200 GOT APU OIL TEMP CASS MSG. COMPLIED WITH QRH, DIVERTED TO PIT. SHUTDOWN ON GROUND. INSPECTED APU OIL QUANTITY AND FOUND OIL LEVEL OVER-SERVICED. REMOVED EXCESS OIL AND SERVICED PROPERLY IAW AMM 49-90-00. OPS CHECKS GOOD.

Part: OIL SYSTEM — OVERSERVICED (APU) · airframe 23,338 hrs · 22,417 cycles

AT FL 200 GOT APU OIL TEMP CASS MSG. COMPLIED WITH QRH, DIVERTED TO PIT. SHUTDOWN ON GROUND. INSPECTED APU OIL QUANTITY AND FOUND OIL LEVEL OVER-SERVICED. REMOVED EXCESS OIL AND SERVICED PROPERLY IAW AMM 49-90-00. OPS CHECKS GOOD.

Part: SILL — CORRODED (BS 559-621) · airframe 21,882 hrs · 21,035 cycles

CARGO BAY LT FLOOR SILL HAS CORROSION AROUND NUTPLATES AND AREAS AS MARKED FS 559+80 TO FS 621. REMOVED UNSERVICEABLE CARGO BAY LT FLOOR SILL AND INSTALLED SERVICEABLE FLOOR SILL IAW REO 601R-53-61-690.

Part: FLOOR SUPPORT — CORRODED (CARGO BAY) · corrosion level 2 · airframe 21,882 hrs · 21,035 cycles

CARGO BAY FLOOR SUPPORT HAS CORROSION AROUND NUT PLATES. REMOVED DAMAGED FLOOR SILL, FABRICATED & INSTALLED NEW SERVICEABLE FLOOR SUPPORT IAW SRM 51-42-06.

Part: ANGLE — CRACKED (BS 605) · airframe 21,882 hrs · 21,035 cycles

FS 605, CARGO FLOOR SILL HAS CRACKED ANGLE FWD SIDE. R & R CRACKED ANGLE SRM 51-42-06.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 21,882 hrs · 21,035 cycles

LEFT INBD FLAP VANE L/E CHAFED IN 3 AREAS (FOUND INBD FWD RIG TO HAVE DOUBLER DRILLED HOLES) R & R LT INBD FLAP VANE INBD L/E PN 601R14303-53S & END RIB 601R14304-13 IAW SRM 51-40-11 AND 51-42-13.

Part: CARGO TRACK — CORRODED (BS 564) · corrosion level 2 · airframe 21,882 hrs · 21,035 cycles

CARGO TRACK AT RBL 9 & FS 564 HAD LEVEL 2 CORROSION. BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS. R & R WITH SERVICEABLE CARGO TRACK IAW AMM 53-01-11 & SRM 51-41-00.

Part: BULKHEAD — DAMAGED (FS 621) · airframe 21,882 hrs · 21,035 cycles

FS 621 BULKHEAD FWD FACE HAS 9 AREAS WITH OVERSIZED HOLES AND OR TOOLING MARKS WHERE BLANKET ATTACHES. BLENDED IN THE 9 AREAS WHERE TOOLING MARKS WERE MEASURED, FOUND TO BE WITHIN LIMITS IAW SRM 51-12-00 IAW REO 601R-53-61-2155 OVERSIZED HOLES WERE REPAIRED IAW REO 601R-53-61-4437, WHERE BLANKET ATTACHES.

Part: FLOOR SUPPORT — CORRODED (FS 589-621) · corrosion level 2 · airframe 21,882 hrs · 21,035 cycles

CARGO BAY FLOOR SUPPORT AT LBL27 INBD HAS CORROSION FS 589 TO FS 621. REMOVED AND INSTALLED SERVICEABLE FLOOR SUPPORT IAW REO 601R-53-61-3778, REV A.

Part: HINGE — BROKEN (LT STUB FAIRING) · airframe 21,882 hrs · 21,035 cycles

LEFT STUB FAIRING IS GOUGED AND HAS BROKEN HINGE. REPLACED UNSERVICEABLE LT STUB FAIRING WITH SERVICEABLE STUB FAIRING IAW SRM 51-42-06 AND SRM 51-40-11.

Part: ANGLE — CRACKED (FS 621) · airframe 21,882 hrs · 21,035 cycles

LT & RT OBLIQUE ANGLES CRACKED. REMOVED DAMAGED OBLIQUE ANGLES. FABRICATED NEW ANGLES & INSTALLE IAW REO 601R-53-61-100.

Part: TRACK — CRACKED (CARGO DOOR) · airframe 21,882 hrs · 21,035 cycles

CARGO DOOR FWD TRACK LWR ATTACH PLATE HAS CRACK FS 574, STA 16A LT. R & R WITH NEW SERVICEABLE BRACKET PN 601R35050-25 ON CARGO DOOR FWD TRACK LWR ATTACH POINT IAW SRM 51-40-11, 51-42-06.

Part: BULKHEAD — CHAFED (FS 280) · airframe 21,882 hrs · 21,035 cycles

RIGHT SIDE FS 280 BULKHEAD CHAFED AT LOWER INBD SIDES. REPAIRED CHAFED AREA IAW REO 601R-53-11-1727, REV E.

Part: TRANSFER SYS — MALFUNCTIONED (FUEL) · airframe 21,334 hrs · 20,459 cycles

NOTED INCREASING FUEL IMBALANCE IN FLIGHT, RECEIVED FUEL IMBALANCE CAUTION MESSAGE AND RAN QRH IT APPEARS THAT THE CENTER TANK WAS FEEDING INTO LT TANK ONLY, RT TANK STEADY DECLINED RT TRANSFER PUMP ON ENTIRE FLIGHT AND DID NOT APPEAR TO BE ADDING ANY FUEL TO RIDE IMBALANCE WHEN AS HIGH AS 1200 LBS.

Part: WIRE — BROKEN (MLG) · airframe 21,021 hrs · 20,326 cycles

TAKEOFF ABORTED AT 87 KNOTS FOR AS INBD CAUTION MESSAGE. MAX BREAK TEMPS WERE 7, 5, 3, 9 RESPECTIVELY. FWD BLUE AND WHITE WIRE BROKEN OFF AT SPLICE NEAR UPPER CONNECTOR PLUG ON RT INBD ANTI-SKID HARNESS SUB-ASSY. R & R INBD MLG ANTI-SKID HARNESS IAW SUP 09-062C. OPS CK GOOD. REMOVED PLACARD AND MEL.

Part: SKIN — DAMAGED (BS 265-280) · airframe 20,088 hrs · 19,155 cycles

FS 265.00-280.00, STR 27-26R, .0625 SKIN DAMAGE (NR 13). PERFORMED PERMANENT REPAIR OF LIGHTNING STRIKE DAMAGE BETWEEN FS 265 AND FS 280.00, STR 26R-STR 27 IAW REO 601R-53-00-115, REV A.

Part: SKIN — DAMAGED (BS 364) · airframe 20,088 hrs · 19,155 cycles

FS 364.00, STRINGER 27-26R, .3750 RIVET HEAD (NR 20). REMOVED DAMAGE RIVET NAS 1097 ADS AND INSTALLED NAS 1097AD6 RIVET AT FS 364.00, STRINGER 27-26R.

Part: HANDLE — DAMAGED (E/E DOOR HANDLE) · airframe 20,088 hrs · 19,155 cycles

TRANSFERRED FROM AWAC LOGPAGE WO 223126/168416, PG 3 0F 4 ITEM 64 AVIONICS DOOR HANDLE HAS VARIOUS BURN MARKS. BLENDED OUT DAMAGE TO SMOOTH CONTOUR, REMOVING BURN MARKS IN AVIONICS DOOR HANDLE.

Part: SKIN — DAMAGED (BS 394-409) · airframe 20,088 hrs · 19,155 cycles

FS 394-409, STRINGER 27-26R, .0625 SKIN DAMAGE NR 301. DRILLED OUT DAMAGE SPOT AT FS 394.00-409.00, STRINGER 27-26R AND INSTALLED NAS 1097AD4. RIVET IAW REO 601R-53-00-418, REV.

Part: SKIN — DAMAGED (BS 250) · airframe 20,088 hrs · 19,155 cycles

FS 250, STRINGER 20R-19R, .0312 SKIN DAMAGE NR 32, BLENDED OUT DAMAGE TO SMOOTH CONTOUR AT FS 250 STRINGER 20R-19R IAW REO 601R-53-00-410, REV.

Part: SKIN — DAMAGED (BS 379-394) · airframe 20,088 hrs · 19,155 cycles

FS 379-394 STRINGER 27-26R, .1250 SKIN DAMAGE. BLENDED AREAS ON RT AVIONICS DOOR CUT OUT IAW REO 601R-53-00-418, REV.

Part: SKIN — DAMAGED (BS 250-265) · airframe 20,088 hrs · 19,155 cycles

FS 250.00 TO FS 265.00, 27-26R SKIN DAMAGE. DRILL OUT DAMAGE AT FS 250.00 TO FS 265.00 27-26R AND INSTALLED NAS 1097 AD RIVET IAW REO 601R-53-00-418.

Part: SKIN — DAMAGED (BS 310-319) · airframe 20,088 hrs · 19,155 cycles

FS 310.00 TO 319.00, STRINGER 27-26R, .0625 DAMAGE. BLENDED DAMAGE AREA TO SMOOTH CONTOUR AT FS 310.00 TO 319.00, STRINGER 27-26R, WITH REMAINING MATERIAL OF .061 AREA WITHIN LIMITS IAW REO 601R-53-00-418, 601R-53-00-115.

Part: SKIN — DAMAGED (BS 280) · airframe 20,088 hrs · 19,155 cycles

FS280, STR 18R HAS .0625 RIVET HEAD DAMAGE. R & R RIVET IAW REO 601R-53-00-418.

Part: SKIN — DAMAGED (BS 280) · airframe 20,088 hrs · 19,155 cycles

FS 280, STR 17R-16R, .1250 RIVET HEAD DAMAGE. R & R RIVET IAW REO 601R-53-00-418.

Part: SKIN — DAMAGED (BS 250-265) · airframe 20,088 hrs · 19,155 cycles

DAMAGEDFS 250.00 TO FS 265.00, STRINGER 27-26R HAS SKIN DAMAGE. DRILL OUT DAMAGE AT FS 250.00 TO FS 265.00, STRINGER 27-26R AND INSTALLED NAS 1097AD RIVET IAW REO 601R-53-00-418.

Part: SKIN — DAMAGED (BS 364) · airframe 20,088 hrs · 19,155 cycles

FS 364, STR 27-26R HAS SKIN DAMAGE DRILLED OUT FS 364 DAMAGE. INSTALLED NAS 1097 RIVET IAW REO 601R-53-00-115, REV A.

Part: SKIN — DAMAGED (BS 250 S26-27R) · airframe 20,088 hrs · 191,555 cycles

FS 250.00, STRINGER 27-26R HAS .1250 SKIN DAMAGE (NR8). DRILLED OUT DAMAGE AT FS 250.00 TO 265.00, STRINGER 27-26R AND INSTALLED NAS 1097AD-4, RIVET IAW REO 601R-53-00-418.

Part: SKIN — DAMAGED (BS 265) · airframe 20,088 hrs · 19,155 cycles

LIGHTNING DAMAGE SKIN AT FS 265, STR 27 TO STR 26R STRIKE. REMOVED LIGHTNING STRIKE DAMAGE NR10 TO SMOOTH CONTOUR IAW REO 601R-53-00-418, REV.

Part: SKIN — DAMAGED (BS 265) · airframe 20,088 hrs · 19,155 cycles

SKIN DAMAGE AT FS 285 BTW 27 TO 26R. REMOVED LIGHTNING STRIKE DAMAGE NR 11 TO SMOOTH CONTOUR IAW REO 601R-53-00-418, REV.

Part: SKIN — DAMAGED (BS 250) · airframe 20,088 hrs · 19,155 cycles

LIGHTNING STRIKE DAMAGE ON FS 250 SKIN AT STR 27-26R. BLENDED DAMAGE TO SMOOTH CONTOUR AT FS 250-265 STRINGER 27-26R.

Part: SKIN — DAMAGED (AVIONICS DOOR) · airframe 20,088 hrs · 19,155 cycles

LIGHTING STRIKE DAMAGE ON AVIONICS DOOR AT STA 385 BETWEEN STR 27-26R. REPAIRED LIGHTNING STRIKE DAMAGE ON AVIONICS DOOR AT STA 385 BETWEEN STR 27-26R IAW REO 601R-52-42-042 REV -OE.

Part: SKIN — DAMAGED (AVIONICS DOOR) · airframe 20,088 hrs · 19,155 cycles

AVIONICS DOOR HAS LIGHTNING STRIKE DAMAGE 2 EA PLACES. REPAIRED LIGHTNING DAMAGE (2EA) PLACES ON AVIONICS DOOR SKIN.

Part: SKIN — DAMAGED (E/E BAY DOOR) · airframe 20,088 hrs · 19,155 cycles

FS 364-379, STRINGER 27-26R, .0625 AVIONICS DOOR DAMAGED (NR23). REPAIRED DAMAGE ON AVIONICS DOOR BETWEEN FS 364-379 AND STRINGERS 27R-26R IAW REO 601R-52-42-042, REV.

Part: STRUCTURE — DELAMINATED (AVIONICS DOOR) · airframe 20,088 hrs · 19,155 cycles

LIGHTNING STRIKE DAMAGE ON AVIONICS DOOR AT STA 389.5 BETWEEN 27-26R. REPAIRED LIGHTNING STRIKE DAMAGE ON AVIAONICS DOOR AT 389.5 BETWEEN 27-26R IAW REO 601R-52-42-042.

Part: SKIN — DAMAGED (AVIONICS DOOR) · airframe 20,088 hrs · 19,155 cycles

FS 364-379, STRINGER 27-26R, .3125 AVIONICS DOOR DAMAGE (NR 22). REPAIRED DAMAGE ON AVIONICS DOOR BETWEEN FS 364-379 AND STRINGERS 27-26R IAW REO 601R-52-42-042, REV.

Part: SKIN — DAMAGED (AVIONICS DOOR) · airframe 20,088 hrs · 19,155 cycles

LIGHTNING STRIKE DAMAGE ON AVIONICS DOOR AT STA 388.5 BETWEEN STR 27-26R. REPAIRED LIGHTING STRIKE DAMAGE ON AVIONICS DOOR AT STA 388.5 BETWEEN STR 27-26R IAW REO 601R-52-42-042, REV.

Part: SKIN — DAMAGED (AVIONICS DOOR) · airframe 20,088 hrs · 19,155 cycles

LIGHTNING STRIKE DAMAGE ON AVIONICS DOOR RIVET AT STA 390.5 BETWEEN STR 27-26R. REPLACED RIVET ON AVIONICS DOOR AT STA 390.5 BETWEEN STR 27-26R IAW REO 601R-52-42-042, REV.

Part: SKIN — DAMAGED (BS 559) · airframe 20,088 hrs · 19,155 cycles

FS559+48 AND FS559+64 AT STR 1L HAS 1 EA RIVET W/HEAD DAMAGE. REMOVED UNSERVICEABLE RIVET AND REPLACED WITH SERVICEABLE RIVET IAW REO 601R-53-00-115, REV A.

Part: SKIN — DAMAGED (BS 409) · airframe 20,088 hrs · 19,155 cycles

FS409+48 TO 409+64, STR 0 HAS DAMAGED RIVET HEAD. REMOVED UNSERVICEABLE RIVET AND REPLACED WITH SERVICEABLE RIVET IAW REO 601R-53-00-115, REV A.

Part: SKIN — DAMAGED (BS 559) · airframe 20,088 hrs · 19,155 cycles

FS 559+64-559+80, STR 1L HAS 1EA RIVET W/HEAD DAMAGE. REMOVED UNSERVICEABLE RIVET AND REPLACED WITH SERVICEABLE RIVET IAW REO 601R-53-00-115, REV A.

Part: SKIN — DAMAGED (BS 409) · airframe 20,088 hrs · 19,155 cycles

FS409+48, STR 1R HAS 1EA RIVET WITH HEAD DAMAGE. REMOVED UNSERVICEABLE RIVET AND REPLACED WITH SERVICEABLE RIVET IAW REO 601R-53-00-115, REV A.

Part: SKIN — DAMAGED (BS409) · airframe 20,088 hrs · 19,155 cycles

FS409+96-FS409+112,STR 0 HAS 1EA RIVET WITH HEAD DAMAGE. REMOVED UNSERVICEABLE RIVET AND REPLACED WITH SERVICEABLE RIVET IAW REO 601R-53-00-115, REV A.

Part: SKIN — DAMAGED (BS 280) · airframe 20,088 hrs · 19,155 cycles

FS 280 BETWEEN STR 0 AND STR 1R HAS 1EA RIVET W/LEAD DAMAGE. REMOVED UNSERVICEABLE RIVET AND REPLACED.

Part: RIVET — DAMAGED (BS 235-250) · airframe 20,088 hrs · 19,155 cycles

FS 235-250, S16R .0937, RIVET HEAD DAMAGE. REMOVED UNSERVICEABLE RIVET AND REPLACED WITH SERVICEABLE RIVET IAW REO 601R-53-00-115, REV A.

Part: SKIN — DAMAGED (BS 280) · airframe 20,088 hrs · 19,155 cycles

FS 280 BETWEEN STR 1L AND 2L HAS 1EA RIVET W/HEAD DAMAGE. REMOVED UNSERVICEABLE RIVET AND REPLACED WITH SERVICEABLE RIVET IAW REO 601R-53-00-115, REV A.

Part: SKIN — DAMAGED (BS 409) · airframe 20,088 hrs · 19,155 cycles

FS409+80-409+96 S 0 HAS 1 EA RIVET WITH HEAD DAMAGE. REMOVED UNSERVICEABLE RIVET AND REPLACED WITH SERVICEABLE RIVET IAW REO 601R-53-00-115, REV A.

Part: SKIN — DAMAGED (BS 280) · airframe 20,088 hrs · 19,155 cycles

FS 280 BETWEEN STR 1R AND 2R HAS 1EA RIVET W/LEAD DAMAGE. REMOVED UNSERVICEABLE RIVET AND REPLACED WITH SERVICEABLE RIVET IAW REO 601R-53-00-115, REV A.

Part: SKIN — DAMAGED (BS 310-319) · airframe 20,088 hrs · 19,155 cycles

FUSELAGE SKIN LIGHTNING STRIKE AT FS 310.00 TO 319.00, STR 27-26R-REF. ACFT SKIN DAMAGE LOCATION MARKED NR 18, C/W STEPS IB2/IB3 (A-G) OF REO 601R-53-00-115.

Part: SKIN — DAMAGED (BS 280-295) · airframe 20,088 hrs · 19,155 cycles

FS 280 TO FS 295, STR 27-26R, .0625 SKIN DAMAGE (NR16). PERFORMED PERMANENT REPAIR OF LIGHTNING STRIKE DAMAGE BETWEEN FS 280 AND FS 295, STR 27-26R IAW REO 601R-53-00-115, REV A.

Part: SKIN — DAMAGED (BS 235-280) · airframe 20,088 hrs · 19,155 cycles

FS 235 TO FS 250, STR 27-STR 26R HAS .0937 SKIN DAMAGE (NR5). PERFORMED PERMANENT REPAIR OF LIGHTNING STRIKE DAMAGE BETWEEN FS 235 TO FS 250, STR 26R-STR 27 IAW REO 601R-53-00-115, REV A.

Part: SKIN — DAMAGED (BS 280-295) · airframe 20,088 hrs · 19,155 cycles

FS 280 TO FS 295, STR 27-STR 26R HAS .0312 SKIN DAMAGE (NR 15). PERFORMED PERMANENT REPAIR OF LIGHTNING STRIKE DAMAGE BETWEEN FS 280 AND FS 295, STR 27-STR 26R IAW REO 601R-53-00-115, REV A.

Part: SKIN — DAMAGED (BS 235-250) · airframe 20,088 hrs · 19,155 cycles

FS 235 TO FS 250, STR 27-STR 26R HAS .0625 SKIN DAMAGE. PERFORMED PERMANENT REPAIR OF LIGHTNING STRIKE DAMAGE BETWEEN FS 235 TO FS 250, STR 26R-STR27 IAW REO 601R-53-00-115, REV A.

Part: SKIN — DAMAGED (BS 394-409) · airframe 20,088 hrs · 19,155 cycles

FS 394-409, STR 27, .0937 RIVET HEAD DAMAGED (NR29). R & R RIVET AT FS 400, STR 27 IAW REO 601R-53-00-115, REV A.

Part: SWITCH — MALFUNCTIONED (STAB TRIM) · airframe 17,952 hrs · 16,873 cycles

STAB TRIM (BOTH CHANNELS) AND MACH TRIM CAUTION MSG, C/W QRH AND WOULD NOT RESET. R & R F/O`S STAB TRIM DISCONNECT SWITCH IAW AMM 27-41-30. ALL OPS CKS GOOD AT THIS TIME.

Part: BRACKET — DAMAGED (LT MLG WW) · airframe 17,197 hrs · 16,084 cycles

R & R HYD TRANSDUCER BRACKET WITH SERVICEABLE BRACKET PN 601R75262-159 AT LT MLG WHEEL WELL IAW SRM 51-40-11, 51-21-11, 51-42-06, 51-22-00, 51-41-02, 51-25-16.

Part: TRACK — CHAFED (THRUST REVERSER) · airframe 17,197 hrs · 16,084 cycles

LT TR MAIN LOWER INBD TRACK CHAFED, REO 601R-78-34-2435.

Part: LUG — CHAFED (THRUST REVERSER) · airframe 17,197 hrs · 16,084 cycles

LT TR MAIN TRACK INBD LOWER LUG CHAFED REO 601R-78-34-2435 CARRIED OUT.

Part: LUG — CHAFED (THRUST REVERSER) · airframe 17,197 hrs · 16,084 cycles

LT TR MAIN TRACK LOWER OTBD LUG CHAFED REO 601R-78-34-2435 CARRIED OUT.

Part: BRACKET — CRACKED (BS 495) · airframe 17,197 hrs · 16,084 cycles

RT ENG SHUTOFF VALVE BRACKET IN FWD WW AREA BROKEN REMOVED, WELDED, REINSTALLED.

Part: FITTING — CRACKED (BS 484) · airframe 17,197 hrs · 16,084 cycles

LBL 18 CLIP BELOW PANEL 261 DLF IS CRACKED AT FS484. R & R DAMAGED CLIP IAW SRM 51-42-21 AND 51-42-06.

Part: RIB — CRACKED (RT WING) · airframe 17,197 hrs · 16,084 cycles

RT MLG WW BATT RIB CRACKED. REPAIRED RT MLG BATT RIB IAW REO 601R-57-51-046.

Part: FRAME — CRACKED (TAILPIPE FAIRING) · airframe 17,197 hrs · 16,084 cycles

RT TAIL PIPE FAIRING 2ND AFT INNNER FRAME CRACKED. REPAIRED RT EXHAUST NOZZLE FAIRING IAW BOMB CMM 78-11-00. REPAIR NR SRS042.

Part: SKIN — CHAFED (CARGO DOOR) · airframe 17,197 hrs · 16,084 cycles

CARGO DOOR OUTER SKIN IS CHAFED AT UPPER END. PERFORMED REO 601R-52-31-119.

Part: BULKHEAD — CRACKED (BS 202.75) · airframe 17,197 hrs · 16,084 cycles

FS 202.75 PRESSURE BULKHEAD CRACKED AT BRAKE CABLE PASS THRU. REPAIRED PRESSURE BULKHEAD FS 202.75 IAW REO 601R-53-11-563.

Part: HANDLE — CRACKED (PAX DOOR) · airframe 17,197 hrs · 16,084 cycles

PAX DOOR OUTER HANDLE CRACKED. R & R WITH NEW SERVICEABLE PART.

Part: SEAL — CHAFED (LT WING) · airframe 17,197 hrs · 16,084 cycles

LT FLAP FAIRING (HINGE) 592BB IB METAL SEAL IS CHAFED. REMOVED DAMAGED SEAL AND REPLACED WITH METAL SEAL SRM 51-12-00.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 17,197 hrs · 16,084 cycles

NR 2 HYD BRACKET (RETURN FILTER) REMOVED DAMAGED BRACKET AND INSTALLED SERVICEABLE BRACKET IAW SRM 51-42-06.

Part: SILL — CRACKED (CARGO DOORWAY) · airframe 17,197 hrs · 16,084 cycles

CARGO DOOR FLOOR SILL CRACKED AT FWD FLIP PLATE ANCHOR BOTTOM SIDE. REPAIRED CARGO DOOR FLOOR SILL IAW REO 601R-53-61-1741.

Part: NOSE COWL — GOUGED (LT ENGINE) · airframe 17,197 hrs · 16,084 cycles

LT LOWER NOSE COWL CHAFED AND GOUGED ON T/E. REMOVED DAMAGED T/E AND INSTALLED SERVICEABLE PN 228-50091-107 T/E IAW CMM 20-26-00, 20-42-061, 20-40-11, 71-14-01.

Part: SUPPORT — CHAFED (THRUST REVERSER) · airframe 17,197 hrs · 16,084 cycles

RT ENG INBD TRACK LUG SUPPORT IS CHAFED. CHAFE BLENDED IAW REO 601R-78-34-2435.

Part: FITTING — CRACKED (BS 280) · airframe 17,197 hrs · 16,084 cycles

FS280 CLIP IS CRACKED AT INBD SIDE OF RBL 9.0. R & R CLIP IAW SRM 51-42-21.

Part: SUPPORT — CHAFED (THRUST REVERSER) · airframe 17,197 hrs · 16,084 cycles

RT ENG LOWER OTBD TRACK LUG IS CHAFED. CHAFE BLENDED IAW REO 601R-78-34-2435.

Part: LUG — CHAFED (THRUST REVERSER) · airframe 17,197 hrs · 16,084 cycles

RT ENGINE LWR INBD T/R TRACK LUG IS CHAFED. CHAFE BLENDED IAW REO 601R-78-34-2435.

Part: ANGLE — CRACKED (BS 625) · airframe 17,197 hrs · 16,084 cycles

LT FS 625 OBLIQUE ANGLE CRACKED. R & R OBLIQUE ANGLE WITH SERVICEABLE PN 601-35012-51 IAW SRM 51-40-11.

Part: SUPPORT — CHAFED (THRUST REVERSER) · airframe 17,197 hrs · 16,084 cycles

RT ENG LOWER OTBD TR TRACK LUG SUPPORT IS CHAFED. CHAFE BLENDED IAW REO 601R-78-34-2435.

Part: TRACK — CHAFED (THRUST REVERSER) · airframe 17,197 hrs · 16,084 cycles

LT TR MAIN LOWER OTBD TRACK CHAFED REO 601R-78-2435 CARRIED OUT.

Part: COALESCER BAG — ODOR (LT A/C PACK)

AT FL230, TURNED TEMP UP ON LT PACK AND GOT A STRONG BURNED OIL ODOR IN COCKPIT DESCENDED AND TURNED LT PACK OFF, ODOR WENT AWAY. INSP ACM, OK COLOR NORMAL. OPERATED SYS AND OIL ODOR COMES BACK SOON AS LT PACK IS TURNED ON. REMOVED AND REPLACED LT PACK COALESCER IAW AMM 21-51-13. OPS CHECK GOOD, REMOVED. (K)

Part: HYDRAULIC LINE — DEFECTIVE (HYDRAULIC SYS) · airframe 14,932 hrs · 13,853 cycles

AT THE GATE: HY SYS NR 1 RESERVOIR SHOWS EMPTY, SMOKE COMING OUT OF APU BAY. REMOVED AND REPAIRED HYDR SYS TUBE ASSY PN 601R75286-85 IAW AMM 29-11-00 LEAK CHECK. (K)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 12,489 hrs · 11,512 cycles

EMERGENCY FLOOR LIGHTS ROW 6 AND 7 INOPERATIVE. (M)

Part: FLOOR SUPPORT — CORRODED (BS 574-621)

FS 574 TO 621 WL 73.50 RBL 9 FLOOR SUPPORT IS CORRODED. CORROSION REMOVED IAW SRM 51-21-06. (M)

Part: BEAM — CRACKED (BS 621)

AT FS 621, WL 114, LBL 27, BELOW BEAM ANGLE CRACKED. BEAM ANGLE REPLACED IAW SRM 51-24-21. (M)

Part: FLOOR SUPPORT — CORRODED (BS 285-310)

FOUND CORROSION EXISTS ON FLOOR SUPPORTS FS 285-310 WL 73.5 LBL 27 TO LBL 20. CORROSION ON FLOOR SUPPORTS REMOVED IAW SRM 51-21-06. (M)

Part: SILL — CORRODED (FUSELAGE)

AT FS 574 TO FS 621 WL 73.50 SILL PLATE CORRODED. BLENDED SILL PLATE IAW 51-21-06 SRM. (M)

Part: SILL — CRACKED (FUSELAGE)

AT FS 589 WL 73.5 CARGO SILL BESIDE RIVET CRACKED. REPAIRED CARGO SILL IAW REO 601R-53-61-43. (M)

Part: STRUCTURE — CORRODED (FUSELAGE)

AT FS 574 TO FS 621 WL 73.50 LBL 30.00 PLATE CORRODED. BLENDED PLATE IAW (51-21-06) SRM. (M)

Part: ANGLE — CRACKED (FUSELAGE)

AT INTERCOSTAL FS 484 RBL 27 AND 36, OUTBOARD AND INBOARD ANGLE CRACK. INTERCOSTAL REPAIRED IAW SRM 51-42-21 AND REO 601R-53-41-059 REV A. (M)

Part: CARGO TRACK — CRACKED (CARGO BAY)

FS 574 CHANNEL CARGO TRACK CRACKED LBL 40 WL 80. CHANNEL FOR CARGO TRACK REMOVED PER SRM 51-42-06, FABRICATED IAW SRM 51-24-21, 51-12-00 AND INSTALLED IAW SRM 51-42-06. (M)

Part: SUPPORT FITTING — CORRODED (FUSELAGE)

SUPPORT FITTING (MACHINED PLATE) RBL 9 FS 460 CRACK. SUPPORT FITTING REPLACED IAW CRJ 200 SRM 51-42-21. (M)

Part: HINGE — CRACKED (STOW PLATE)

CARGO STOW PLATE, FWD, MID AND AFT HINGES ARE CRACKED. CARGO STOW PLATE REPLACED IAW SRM 51-42-06. (M)

Part: STRUCTURE — CRACKED (PAX DOOR) · airframe 12,368 hrs · 11,402 cycles

FOUND CRACK EXIST ON PASSENGER DOOR EDGE MEMBER FORWARD. REPAIR ON PASSENGER DOOR EDGE CARRIED OUT IAW REO 601R-52-11-279. (M)

Part: ANGLE — CRACKED (FUSELAGE)

ANGLE AT FS 280 LBL 9 AND RBL 9 INBOARD AND OUTBOARD FOUND CRACK. ANGLES REPLACED IAW REO 601R-53-11-171 REV D. OUTBOARD ANGLE REPLACED IAW REO 601R-53-11-171 REV D, INBOARD ANGLE REPLACED IAW SRM 51-42-05 AND SRM 51-42-21. (M)

Part: PLATE — CRACKED (FUSELAGE) · airframe 12,368 hrs · 11,402 cycles

CARGO DOOR PLATE FOUND CRACKED. REPLACED CARGO DOOR PLATE IAW SRM 51-41-02. (M)

Part: BULKHEAD — CRACKED (FUSELAGE)

PILOTS BULKHEAD FS 280 RBL 9 FOUND CRACKED. BULKHEAD REPAIRED IAW REO 601R-53-11-171 REV D. (M)

Part: BULKHEAD — CRACKED (FUSELAGE)

PILOTS BULKHEAD FS 280 LBL 9 FOUND CRACKED. BULKHEAD REPAIR CARRIED OUT IAW REO 601R-53-11-171 REV D. (M)

Part: DIODE — FAILED (DC SYSTEM)

AFTER DEPARTURE DC EMERGENCY BUS CAUTION MESSAGE CAME ON AND OFF REPEATEDLY. COMPLIED WITH QRH. NO ASSOCIATED FAULT MESSAGES FOR SYSTEMS ASSOCIATED WITH DC EMERGENCY BUS APU BATTERY DIRECT FEED FLOWLINE REMAINED GREEN. REMOVED AND REPLACED DC EMERGENCY DIODE AND RELATED HARDWARE, OPS CHECK OF DC ELECTRICAL POWER NORMAL REF WDM 24-60-00. (M)

Part: FAIRING — LOOSE (FUSELAGE)

VERY NOTICEABLE RUMBLE AND VIBRATION COMING FROM NOSE AREA DURING CLIMB-OUT. ALTITUDE 12,000 TO 13,000 FT ASL, GEAR UP. LASTED APPROXIMATELY 30 SECONDS THEN DISAPPEARED. VIBRATION FELT THROUGH FLOOR AREA IN COCKPIT. FOUND BELLY FAIRING LOOSE. RESEALED IAW AMM 52-82-01, REF LOG PAGE 152396/4 FOR SEALING. ALSO REF 152397/2 AND 3 FOR RESIDUE REMOVAL AND ENGINE RUN. (M)

Part: SKIN — CRACKED (FUSELAGE)

LT FS640 SKIN DOUBLER FAILED NDT, FOUND CRACK .8 INCHES LONG. MAINTENANCE REPAIRED LT FS 640 SKIN DOUBLER BY CUTTING AWAY DAMAGED AREA OF SKIN DOUBLER. PERFORMED EDDY CURRENT INSPECTION, FABRICATED REPAIR PARTS AND INSTALLED IAW REO. (K)

Part: FLOOR SUPPORT — CRACKED (BS 621) · airframe 7,338 hrs · 6,490 cycles

RT FS 621 FLOOR SUPPORT ANGLE IS CRACKED 1.5 INCHES LONG. MAINTENANCE REPAIRED FS 621 FLOOR SUPPORT (RT) IAW REO. (K)

Part: SUPPORT ANGLE — CRACKED · airframe 7,338 hrs · 6,490 cycles

LT FS 621 FLOOR SUPPORT ANGLE IS CRACKED 1.5 INCH LONG, MAINTENANCE REPAIRED LT FS 621 FLOOR SUPPORT ANGLE IAW REO. (K)

Part: ANGLE — CRACKED (BS 925) · airframe 7,338 hrs · 6,490 cycles

RT FS 625 OBLIQUE ANGLE IS CRACKED MAINTENANCE REMOVED AND REPLACED RT FS 625, OBLIQUE ANGLE IAW SRM. (K)

Part: ANGLE — CRACKED (FUSELAGE) · airframe 7,338 hrs · 6,490 cycles

LT FS 625 OBLIQUE ANGLE IS CRACKED. MAINT REMOVED AND REPLACED LT FS 625, OBLIQUE ANGLE IAW SRM. (K)

Part: FUEL LINE — LEAKING · airframe 7,243 hrs · 6,392 cycles

STRONG FUEL SMELL IN CABIN. FOUND FUEL LEAK FROM THE APU DRAINS. PLACED APU ON MEL. REMOVED AND REPLACED APU FUEL LINE BETWEEN FUEL SOLENOID AND FUEL MAINIFOLD. LEAK CHECK GOOD. REMOVED OFF MEL. (K)

Part: A/C PACK — CONTAMINATED (LEFT) · airframe 6,664 hrs · 5,812 cycles

UPON CLEANING OIL RESIDUE FROM APU, FOUND LT PACK SMOKING SLIGHTLY FROM EXHAUST. FOUND OIL CAME FROM APU OIL COOLER RESIDUE. OPERATED LT PACK IAW AMM, NO FUMES OR SMOKE NOTED FROM AIR CONDITIONING SYSTEM OR EXHAUST. (K)

Part: SKIN — DENTED (FUSELAGE)

RIGHT SIDE FORWARD FUSELAGE DAMAGED BELOW CO-PILOTS WINDOW. COMPLIED WITH FLUSH REPAIR IAW BOMBARDIER, INC REO 601R-53-00-061 REV A AND BRAS EO 601R-53-6107C. (M)

Part: BUSHING — MIGRATED (RT MLG)

FOUND RIGHT MLG AFT TRUNNION BUSHING MIGRATED .35 INCH. REMOVED MIGRATED BUSHING. REAMED TRUNNION LUG BORE OT 1ST OVERSIZE AND INSTLALED 1ST OVERSIZED BUSHING, P/N 601R5721003-21 IAW BOMBARDIER REO 601R-57-21-003 REV B. (M)

Part: WINDSHIELD — CRACKED (COCKPIT)

FOUND RIGHT WINDSHIELD CRACKED RIGHT AFTER TAKEOFF. WINDSHEAR ENCOUNTERED DURING DEPARTURE ALSO, REMOVED AND REPLACED FIRST OFFICERS WINDSHIELD IAW AMM 56-11-01. (M)

Part: POWER SUPPLY — MALFUNCTIONED (COCKPIT)

APU LOAD CONTROL VALVE LIGHT, ISOLATION VALVE LIGHT, APU AVAILABLE LIGHT ALL INTERMITTENT, ELECTRICAL SMELL. REMOVED AND REPLACED BRIGHT/DIM POWER SUPPLY. (M)

Part: DOOR — OPEN (OXYGEN SERVICE)

AIR RETURN FOR LOUD WHISTLE AND STALL FAIL MESSAGE. INSPECTED AND FOUND OXYGEN SERVICE DOOR OPEN. SECURED DOOR. NO DAMAGE NOTED. OK FOR SERVICE. (M)

Part: CHAIN — FAILED (ELEVATOR TRIM)

AIR SHUTTLE 7451 - ELEVATOR TRIM STUCK APPROXIMATELY 50 MILES AFTER DEPARTURE. THE AIRCRAFT RETURNED TO THE GATE IN RAP. AFTER INSPECTION OF THE SYSTEM IT WAS FOUND THAT THE MASTER LINK ON THE ELEVATOR TRIM SERVO CHAIN HAD COME APART JAMMING THE ELEVATOR TRIM. FIX IS NOT COMPLETE AT THIS TIME. (M)

Part: SEQVLV — FAILED (NLG)

FLT 7456 - EN ROUTE DEN/RAP - ON DESCENT WHEN THE GEAR WAS SELECTEDDOWN, ALL BUT THE NOSE GEAR EXTENDED, AT WHICH TIME THE CREW NOTICED THATTHE NR 2 HYD SYSTEM PRESSURE AND QTY WAS ZERO. THE CREW THEN ALTERNATELYEXTENDED THE NOSE GEAR WITHOUT INCIDENT AND LANDED SAFELY. UPONINVESTIGATION IT WAS FOUND THAT THE NOSE LANDING GEAR DOOR SEQUENCE VALVESOLENOID HAD PARTIALLY SEPARATED SHEARING 2 OF 4 BOLTS ATTACHING SOLENOID TOVALVE BODY. THE SEQUENCE VALVE WAS REPLACED, HYDRAULIC SERVICED ALL CHECKEDNORMAL, A TEST FLT PERFORMED AND ACFT RETURNED TO SERVICE. (M)

Part: BOLTS — LOOSE (ELEVATOR CONTL)

DURING COMPLIANCE OF FCD 95-32, THREE BOLTS ON THE LEFT ELEVATOR OUTPUT LEVER WERE LOOSE. NO APPARENT VISUAL DAMAGE WAS FOUND TO THE OUPUT LEVER ASSY. THESE BOLTS WERE RETORQUED IAW DASH 8-300 MM 27-32-41, PAGE 201. (M)

Part: CONTROL CABLE — WORN (RT AILERON)

DURING INSPECTION, FOUND THAT THE RIGHT WING AILERON LOWER CABLE WAS WORN BY A PULLEY AT YW 190. IT SHOULD BE NOTED THAT THIS CONDITION IS NOT VISIBLE WITH THE GUST LOCK ENGAGED AND THE AILERONS IN NEUTRAL. THE CABLE WAS CHANGED ON FIELD AVIATION COMPANY WOR NR 21964 AT C-CHECK. (M)

Part: WARNING LIGHT — ILLUMINATED (NR 2 HYD SYSTEM)

IAD/JFK - FLT 6485 - DURING CLIMB AT 1500 HRS ON 2-4-95, THE NR 2 HYDRAULIC CAUTION LIGHT ILLUMINATED WHEN LANDING GEAR RETRACTED. AIRCRAFT RETURNED TO IAD WITH NO FURTHER INCIDENTS. MAINTENANCE OPENED DMI NR 05245 IAW MEL 29-3 ON THE HYDRAULIC WARNING SYSTEM. MAINTENANCE LATER CLEARED DMI NR 05245 ON 2-8-95 BY BLEEDING THE NR 2 HYDRAULIC SYSTEM. GROUND AND AIR OPS CHECKS GOOD. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X)

Part: HYDRAULIC PUMP — FAILURE (RT ENGINE)

FLT NR 6943 - SWF-IAD - DURING CLIMB-OUT DIVERTED TO SWF DUE TO THE NR 2 ENGINE HYDRAULIC PUMP ILLUMINATING UPON GEAR RETRACTION/EXTENSION. AN EMERGENCY WAS DECLARED, BUT AIRCRAFT RETURNED TO SWF WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED THE NR 2 ENGINE HYDRAULIC PUMP. PERFORMED GEAR SWING, OPS CHECK GOOD. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (Z)