N428AW

Part: SKIN — DENTED (FS654.50 TO FS67) · airframe 43,408 hrs · 42,237 cycles

4 DENTS ON EXTERIOR LOWER SKIN AT FS 672.20 AND STRINGER 27. CUST W/O: 332319 JOB CARD: 453-900-501 EXTERIOR LOWER SKIN AT FS559.0 +112 - S755.0 AIRCRAFT REMOVED FROM SERVICE. PERFORMED HAND DRESS ON 4 EA DENTED AREAS (P1 TO P4) TO REFORM SKIN TO ORIGINAL CONTOUR AND RESTORED PROTECTIVE FINISHES AT FUSELAGE SKIN BETWEEN FS 654.50 AND FS 672.20 AND BETWEEN STR 26R TO STR 26L IAW ASAP EA# AWAC-CRJ253-02022 DATED 12/7/23 REV IR.

Part: TIRE — FLAT (MLG) · airframe 41,872 hrs · 40,571 cycles

AFTER TO FROM KIND FELT A VIBRATION AND NOTICED #3 BTMS SHOWED LINES AND NO DIGITS. IND REPORTED TIRE DEBRIS ON RUNWAY. #4 BTMS READ 2. LANDED WITH OUT INCIDENT. CFR REPORTS #3 TIRE FLAT #4 TIRE SUPPORTING THE AC. TAXIED TO GATE WITHOUT INCIDENT ***AIRCRAFT REMOVED FROM SERVICE ***** R & R #3 MLG TIRE IN REFERENCE TO AWAC SUPP 12-015I. COMPLIED WITH M061 INSTRUCTIONS, THE SPACER AND WASHER WERE RETAINED FROM THE REMOVED WHEEL ASSEMBLY AND USED ON THE INSTALLED WHEEL ASSEMBLY.

Part: ANTI-ICE VALVE — MALFUNCTIONED (RT ENGINE) · airframe 39,522 hrs · 38,148 cycles

RT ENGINE ANTI ICE CAUTION MESSAGE IN FLIGHT WITH SYSTEM OFF. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED RT ENGINE COWL ANTI-ICE SHUT OFF VALVE, IAW AWAC SUP 10-094. OPERATIONS AND LEAK CHECK GOOD.

Part: SKIN — DENTED (BS 589-621) · airframe 38,611 hrs · 37,201 cycles

REF ROUTINE 1018039-1000-0062. 4DMI21302. REPAIR FS589-FS621, STR22L -STR23L, 601R-53-61-6304B. AIRCRAFT REMOVED FROM SERVICE REPAIRED LOWER FUSELAGE SKIN FS589-FS621, STR 21L - STR25R IAW BOMBARDIER REO 601R-53-61-7269 REV.-- DATED 1/28/2020

Part: STIFFENER — CRACKED (BS 409) · airframe 38,611 hrs · 37,201 cycles

CRACK AT 409+128, LBL27, INBOARD SIDE AT BOTTOM FASTENER HOLES. AIRCRAFT REMOVED FROM SERVICE REPAIRED CRACKED STIFFENER IAW REO 601R-53-41-056 REV. F.

Part: STIFFENER — CRACKED (BS 409) · airframe 38,611 hrs · 37,201 cycles

CRACK LOCATED AT 409+128 18R ON LOWER END OF STRUT AIRCRAFT REMOVED FROM SERVICE REPAIRED POST AT FS 409+128 RBL 18 IAW REO 601R-53-41-889 REV D 601R-53-41-056 REV F AND 601R-53-41-2679 REV---.

Part: DRAG ANGLE — MISINSTALLED (BS 310) · airframe 38,611 hrs · 37,201 cycles

AFT WEB AND DRAG ANGLE HAS IMPROPERLY INSTALLED FASTENERS PN PAX DOOR AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED AFT WEB AND DRAG ANGLE IAW SRM 51-42-13 AND SRM 51-42-06

Part: POST — CRACKED (BS 409) · airframe 38,611 hrs · 37,201 cycles

FOUND A CRACK LOCATED AT 409+128, LBL 18, ON THE LOWER END OF STRUT. AIRCRAFT REMOVED FROM SERVICE. REPAIRED THE POST STRUT IAW REO 601R-53-41, 56, REV E.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,611 hrs · 37,201 cycles

INTERCOSTAL JUST TO THE LEFT OF STRINGER 27 HAS CORROSION SPOTS BETWEEN FRAMES 364 AND 349, IN FWD E&E BAY. ORIGINAL MATERIAL .080, MATERIAL LOSS .009, .071 REMAINING. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED INTERCOSTAL IAW SRM 51-42-06 AND 51-42-21.

Part: SKIN — CHAFED (LT AILERON) · airframe 38,611 hrs · 37,201 cycles

LEFT WING AILERON LOWER AND UPPER SURFACE LEADING EDGES ARE CHAFED. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED LEFT AILERON UPPER LEADING EDGE IAW SRM 51-40-11, TR51-42, 51-42-06 AND SUPPLEMENT 13-055B. BLENDED LOWER LE AND FOUND TO BE WITHIN LIMITS IAW SRM 57-60-00.

Part: ANGLE — CRACKED (RT WING) · airframe 38,611 hrs · 37,201 cycles

O/B ANGLE P/N 600-12045-12, ON RIGHT WING AT PANEL 620ML, IS CRACKED. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED ANGLE IAW SRM 51-41-02.

Part: ATTACH BRACKET — CRACKED (BS 621) · airframe 38,611 hrs · 37,201 cycles

CARGO DOOR AFT SPRING BOX ATTACH BRACKET WAS CRACKED. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED CARGO DOOR AFT SPRING BOX ATTACH BRACKET IAW CRJ 200 SRM 51-42-06

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,611 hrs · 37,201 cycles

FLOOR SUPPORT AT FS589 BETWEEN RIGHT FLOOR SILL AND RBL27 HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED FLOOR SUPPORT CAP STRIP IAW SRM 51-42-06 AND 51-42-15.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,611 hrs · 37,201 cycles

FLOOR SUPPORT STRUCTURE IS CORRODED AT FS559+64-559+80, RBL9. AIRCRAFT REMOVED FROM SERVICE REPAIRED FLOOR STRUCTURE IAW SRM 53-00-43.

Part: SPAR — CRACKED (LT ELEVATOR) · airframe 38,661 hrs · 37,201 cycles

LEFT ELEVATOR LOWER SURFACE 334DB ACCESS PANEL LANDING SPAR FLANGE CRACKED. AIRCRAFT REMOVED FROM SERVICE. REPAIRED LEFT ELEVATOR LOWER SPAR FLANGE IAW REO 601R-55-21-529 REV --.

Part: SKIN — DENTED (TE FLAP) · airframe 38,611 hrs · 37,201 cycles

LEFT WING INBOARD FLAP, OUTBOARD END HAS DENT. (OUTBOARD AND BELOW OF THE OUTBOARD FLAP ARM) AIRCRAFT REMOVED FROM SERVICE REPAIRED LEFT WING INBOARD FLAP OUTBOARD END LOWER SKIN IAW REO 601R-57-52-1544.

Part: THRESHOLD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,611 hrs · 37,201 cycles

SERVICE DOOR THRESHOLD HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE LOCATED, DRILLED AND REPLACED THRESHOLD IAW CRJ SRM 51-42-06 & TR51-4.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 38,611 hrs · 37,201 cycles

RPB AT FS 621 STRG 14 OBLIQUE ANGLE IS CRACKED AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED RPB OBLIQUE ANGLE AT FS 621 BSTRG 14

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 38,611 hrs · 37,201 cycles

STIFFENER P/N 601R36008-51 ON AFT SIDE OF 621 BULKHEAD, LBL 40, IS CRACKED. AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED STIFFENER IAW CRJ SRM 51-42-06.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 38,611 hrs · 37,201 cycles

REAR PRESSURE BULKHEAD STGR 14 OBLIQUE ANGLE IS CRACKED. REMOVED FROM SERVICE REMOVED AND REPLACED REAR PRESURE BULKHEAD STGR 14 OBLIQUE ANGLE IAW CRJ-200 SRM 51-42-21

Part: SUPPORT — CORRODED (LT MLG DOOR) · corrosion level 2 · airframe 38,611 hrs · 37,201 cycles

L/H MLG AFT LUG INTERIOR CORRODED AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED DAMAGED SUPPORT ON LH MLG DOOR IAW CRJ-200 SRM 51-42-28

Part: SUPPORT BRACKET — CRACKED (LT MLG WW) · airframe 38,611 hrs · 37,201 cycles

BRAKE PRESSURE TRANSDUCER SUPPORT BRACKET CRACKED AT FS530, LH MLG WHEEL WELL. AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED BRAKE PRESSURE TRANSDUCER SUPPORT BRACKET AT FS530 IAW CRJ200 SRM 51-42-06

Part: ATTACH ANGLE — CRACKED (CARGO DOOR) · airframe 38,611 hrs · 37,201 cycles

FWD LOWER CARGO DOOR BEAM ATTACH ANGLE CRACKED AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED CRACKED ANGLE IAW CRJ 200 SRM 51-42-21

Part: ATTACH ANGLE — CRACKED (CARGO DOOR) · airframe 38,611 hrs · 37,201 cycles

AFT LOWER CARGO DOOR BEAM ATTACH ANGLE CRACKED AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED CRACKED ANGLE IAW 51-42-21

Part: FITTING — CRACKED (COCKPIT) · airframe 38,611 hrs · 37,201 cycles

R/H LOWER WINDSHIELD SIDE POST JOINT TO SILL FITTING CRACKED ON AFT SIDE AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED R/H LOWER WINDSHIELD SIDE POST JOINT TO SILL FITTING IAW CRJ-200 SRM 51-42-21

Part: BRACKET — CRACKED (BS 529) · airframe 38,611 hrs · 37,201 cycles

BRAKE PRESURE TRANSDUCER BRACKET IN R/H MLG WHEEL WELL AT FS529 IS CRACKED AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED BRAKE PRESSURE TRANSDUCER BRACKET IAW CRJ200 SRM 51-42-06

Part: LIGHT — BROKEN (CABIN) · airframe 36,244 hrs · 34,954 cycles

FLOOR LEVEL EMERGENCY FLOODLIGHT BROKEN AT THE PAX DOOR. R&R FLOODLIGHT, OPS CHECK GOOD IAW 33-51-19.

Part: VALVE — STICKING (CABIN PRESSURE) · airframe 35,206 hrs · 33,918 cycles

CLIMBING TO FL 200, PRESSURIZATION WAS NORMAL. ABOVE FL 220 CABIN ALTITUDE CLIMBED AT AN EXCESSIVE RATE. DURING CRUISE AT FL 290, CABIN ALTITUDE 7300 AND A DELTA P OF 7300 FT. WHEN STARTING DECENT AND REDUCING ENGINE POWER CABIN ALTITUDE CLIMBED AT A RATE OF 1500 FT PER MINUTE. RECEIVED A CABIN ALT CAUTION AND WARNING. CABIN ALTITUDE REACHED 10,300 FT WITH A DELTA P OF 1.7. COMPLIED WITH QRH AND PERFORMED EMERGENCY DECENT. FOUND LOW PRESSURE CABIN AIR SUPPLY CHECK VALVE FORWARD SECTION DOES NOT SEAT AND AFT SECTION STICKS IN FULLY OPEN POSITION.

Part: WARNING MESSAGE — ILLUMINATED (ANTI ICE) · airframe 35,190 hrs · 33,900 cycles

RECIEVED AN ANTI-ICE DUCT WARNING MESSAGE IN FLT. LEFT WING LEADING EDGE RED ON SYNOPTIC PAGE. OCCURED ON APPROACH. THROTTLE MID RANGE. INDICATIONS INITIALLY CLEARED WHEN ANTI-ICE SELECTED TO OFF THEN TO STANDBY. MESSAGE INDICATION RECURRED AFTER SEVERAL MINUTES WHILE IN STBY. DIVERTED. AND LANDED.

Part: SKIN — DENTED (BS 589-621) · airframe 35,175 hrs · 33,886 cycles

SKIN DENTED AT BS 589 TO 621, STRINGERS 22 - 23L

Part: ANGLE — CRACKED (FUSELAGE) · airframe 35,175 hrs · 33,886 cycles

RT UPPER OBLIQUE ANGLE CRACKED ON AFT PRESSURE BULKHEAD. REPLACED.

Part: BRACKET — CRACKED (COCKPIT) · airframe 35,175 hrs · 33,886 cycles

LT LOWER CENTER WINDSHIELD POST BRACKET IS CRACKED. REPLACED BRACKET IAW SRM 51-42-21.

Part: BRACKET — CRACKED (BS 235) · airframe 35,175 hrs · 33,886 cycles

LEFT LOWER CENTER WINDSHIELD POST BRACKET CRACKED. REPLACED THE BRACKET.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 35,175 hrs · 33,886 cycles

LT UPPER OBLIQUE ANGLE CRACKED AT FS 621.00, STR 14L. REPLACED ANGLE IAW SRM 51-42-21, 51-40-11.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,175 hrs · 33,886 cycles

FLOOR SUPPORT DOUBLER CORRODED AT FS 313.00, LBL20. REPLACED DOUBLER IAW SRM 51-21-06, 51-42-13, 51-24-36, 51-40-11.

Part: SKIN — CORRODED (TE FLAP) · corrosion level 2 · airframe 35,175 hrs · 33,886 cycles

LT I/B FLAP SKIN CORRODED. REPLACED LT I/B LOWER SKIN IAW SRM 51-42-10, 51-42-13.

Part: GUIDE — CRACKED · airframe 35,175 hrs · 33,886 cycles

PANEL 422BT GUIDES ARE CRACKED. REPLACED GUIDES IAW CMM 20-42-06.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 35,175 hrs · 33,886 cycles

FLOOR SUPPORT ANGLE CRACKED AT FS 280.00, RBL11. REPLACED ANGLE IAW REO 601R-53-11-171 REV-D.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 35,175 hrs · 33,886 cycles

FLOOR SUPPORT ANGLE CRACKED AT FS280.00, RBL8. REPLACED ANGLE IAW REO601R-53-11-171 REV-D.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 35,175 hrs · 33,886 cycles

FLOOR SUPPORT ANGLE CRACKED AT FS280.00, LBL8. REPLACED ANGLE IAW REO601R-53-11-171 REV-D.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 35,175 hrs · 33,886 cycles

FLOOR SUPPORT ANGLE CRACKED AT FS 280.00, LBL11. REPLACED ANGLE IAW REO601R-53-11-171 REV-D.

Part: FLOOR SUPPORT — CRACKED (CARGO BAY) · airframe 35,175 hrs · 33,886 cycles

AFT CARGO DOOR OPENING FLOOR SUPPORT HAS CRACK. REPAIRED THE FLOOR SUPPORT.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,175 hrs · 33,886 cycles

FLOOR MOUNT DOUBLER CORRODED FOR GALLEY AT FS317.00. REPLACED DOUBLER IAW SRM 51-24-36, 51-42-06.

Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 35,175 hrs · 33,886 cycles

LEFT INBOARD FLAP VANE SKIN CHAFED AT WS 56.30. REPLACED SKIN IAW SRM 51-42-13.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,175 hrs · 33,886 cycles

GALLEY FLOOR SUPPORT DOUBLER CORRODED FROM FS 297.00, RBL5. REPLACED DOUBLER IAW SRM 51-24-36, 51-42-06, 51-42-13.

Part: SKIN — CHAFED (TE FLAP VANE) · airframe 35,175 hrs · 33,886 cycles

LT INBOARD FLAP VANE SKIN CHAFED AT W56.30. REPLACED SKIN IAW SRM 51-42-13.

Part: RVDT — FAILED (NLG STEERING) · airframe 34,582 hrs · 33,307 cycles

DURING CRUISE AT FL 320, RECEVED A STEERING INOPERATIVE CAUTION MESSAGE. COMPLIED WITH QRH. MESSAGE PERSISTED. DECLARED EMERGENCY. REPLACED THE LT NWS RVDT IAW 15-177A, CHECKED GOOD AFTER TAXI TEST.

Part: WIRE HARNESS — DAMAGED (NLG STEERING) · airframe 34,580 hrs · 33,306 cycles

STEERING INOPERATIVE CAUTION MESSAGE IN FLIGHT. COMPLIED WITH QRH, MESSAGE PERSISTS. DECLARED EMERGENCY. R & R NLG ELECTRICAL STEERING HARNESS IAW 12-029D. OPS CHECKED GOOD, NO MESSAGE.

Part: TARGET — LOOSE (RT PROX SENSOR) · airframe 34,348 hrs · 33,083 cycles

GEAR DISAGREE AFTER TAKEOFF. RT MLG UNSAFE. COMPLIED WITH QRH. MANUALLY EXTENDED GEAR. EMERGENCY DECLARED, AIR RETURN. FOUND ACARS DATA POINTS TO RT MLG UPLOCK. INSPECTED AND FOUND RT MLG UPLOCK PROXIMITY SENSOR PS7GA TARGET LOOSE. TORQUED AND SAFETIED THE TARGET, AND CHECKED CLEARANCE IAW AMM 32-61-05. SENSOR TO TARGET CLEARANCE IS WITHIN LIMITS. SWUNG GEAR MULTIPLE TIMES IAW AMM 32-30-00. OPS CHECKED GOOD.

Part: PUMP — NOT REPORTED (HYDRAULIC SYS) · airframe 34,347 hrs · 33,080 cycles

AFTER TAKEOFF RECEIVED GEAR DISAGREES WARNING MESSAGE. EICAS SHOWED RT MLG UNSAFE. R&R HYD PUMP 3A IAW AMM 29-12-03. CW GEAR RETRACTION NO DEFECTS.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,099 hrs · 30,041 cycles

FRAME 310 HAS CORROSION ON BOTH THE FWD & AFT SIDES, BETWEEN STRINGER 23R - 21R, REPLACED.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 31,099 hrs · 30,041 cycles

CARGO TIE DOWN TRACK AT LBL 9 AT FS 559+112 IS CORRODED, REPLACED.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 31,099 hrs · 30,041 cycles

CARGO TIE DOWN TRACK AT RBL 9 AT FS 559+112, IS CORRODED, REPLACED.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 31,099 hrs · 30,041 cycles

CARGO TIE DOWN TRACK AT RBL 27 AT FS 559+80, IS CORRODED.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 31,099 hrs · 30,041 cycles

CARGO TIE DOWN TRACK AT LBL 9, AT FS 621.00 IS CORRODED, REPLACED.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 31,099 hrs · 30,041 cycles

CARGO TIE DOWN TRACK AT RBL 9, AT FS 559+80 IS CORRODED, REPLACED.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,099 hrs · 30,041 cycles

POTABLE WATER DRAIN MAST U SHAPED DOUBLER HAS CORROSION, BETWEEN FRAMES 349 - 333 & STRINGER 25R - 24R, IN THE FWD E & E BAY. R & R UNSERVICEABLE U SHAPED DOUBLER FOR GALLEY DRAIN MAST IAW SRM 51-11-20, 51-24-21, 51-21-11, 51-25-06, 51-25-16, 51-40-11 & 51-42-06.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,099 hrs · 30,041 cycles

FLOOR SUPPORT BEAM CAP AT FS 349.00, BETWEEN RBL 27 & 36, CORRODED AT FASTENERS. R & R FASTENERS AT FLOOR SUPPORT BEAM CAP FS 349.00, RBL 27 - 36 IAW SRM 51-42-10. REMOVED & INSTALLED NEW AFT FLOOR SUPPORT ANGLE AT FS 349.00, RBL 27 - 36 IAW SRM 51-42-06. REINSTALLED MOUNT FITTING IAW SRM 51-42-21.

Part: WEB — CRACKED (ENTRY DOOR) · airframe 31,099 hrs · 30,041 cycles

MAIN ENTRY DOOR, FWD WEB IS CRACKED ON CORNER TOP STEP RISER.. REPAIRED MAIN ENTRY DOOR FWD WEB IAW REO 601R-52-11-702.

Part: CARGO TRACK — CORRODED (CARGO TRACK) · corrosion level 2 · airframe 31,099 hrs · 30,041 cycles

CARGO TIE DOWN TRACK AT RBL 27, FS 559+96 IS CORRODED. R & R CARGO TIE DOWN TRACK AT RBL 27 & FS 559+96 IAW AMM 53-01-11 & REO 601R-53-00-485.

Part: FITTING — CRACKED (FUSELAGE) · airframe 31,099 hrs · 30,041 cycles

RIGHT SIDE FLOORBEAM, OTBD CLIP AT FS 484.0 & RBL 27 IS CRACKED. R & R CRACKED CLIP AT FS 494 & RBL 27 IAW SRM 51-42-06 & 51-42-21.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,099 hrs · 30,041 cycles

LOWER FWD ANGLE FITTING SUPPORT FOR THE O2 BOTTLE HAS CORROSION, LOCATED ON THE OTBD SIDE OF INTERCOSTAL ON STRINGER 23R, BETWEEN FRAME 333 & 319.7 IN THE FWD E & E BAY. R & R UNSERVICEABLE LOWER FWD SUPPORT BRACKET FOR O2 MOUNT INTERCOSTAL IAW SRM 51-11-20, 51-24-21, 51-21-11, 51-25-06, 51-25-16 & 51-42-15.

Part: ATTACH BRACKET — CRACKED (FUSELAGE) · airframe 31,099 hrs · 30,041 cycles

BRAKE ACCUMULATOR FWD OTBD ATTACHMENT BRACKET IS CRACKED. R & R BRAKE ACCUMULATOR FWD OTBD ATTACHMENT BRACKET IAW SRM 51-42-21.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,099 hrs · 30,041 cycles

LBL 27 FLOOR RAIL BEAM, FS 574.0 TO 621.0, INBD & OTBD FLANGE HAS CORROSION AT FASTENER HOLES. REPAIRED FLOOR RAIL BEAM IAW EA 40-2015-281 & SUPPLEMENT 15-316.

Part: TIE DOWN — CORRODED (CARGO BAY) · corrosion level 2 · airframe 31,099 hrs · 30,041 cycles

CARGO TIE DOWN FITTING AT LBL 27, FS 567 IS CORRODED.

Part: TIE DOWN — CORRODED (CARGO BAY) · corrosion level 2 · airframe 31,099 hrs · 30,041 cycles

CARGO TIE FITTING AT LBL 27, FS 558 IS CORRODED.

Part: TIE DOWN — CORRODED (CARGO BAY) · corrosion level 2 · airframe 31,099 hrs · 30,041 cycles

CARGO TIE DOWN FITTING AT LBL 9, FS 584 IS CORRODED.

Part: TIE DOWN — CORRODED (CARGO BAY) · corrosion level 2 · airframe 31,099 hrs · 30,041 cycles

CARGO TIE DOWN FITTING AT LBL 9, FS 599 IS CORRODED.

Part: TIE DOWN — CORRODED (CARGO BAY) · corrosion level 2 · airframe 31,099 hrs · 30,041 cycles

CARGO TIE DOWN FITTING AT LBL 27, FS 550 IS CORRODED.

Part: RECEPTACLE — LEAKING (FUEL SYSTEM) · airframe 30,791 hrs · 29,760 cycles

REQUEST INSPECTION FOR FUEL LEAK ON BELLY OF ACFT NEAR WHEEL WELLS. INSPECTED ACFT & FOUND BOTH AFT RECEPTACLES ON OVERWING GRAVITY FUEL PANEL FULL OF FUEL. DE-FUELED ACFT DOWN TO 5040 POUNDS & LEAK HAS STOPPED. R & R BOTH AFT RECEPTACLES ON CTR TANK GRAVITY FULL COVER IAW SRM 51-23-02. NO LEAKS NOTED AT THIS TIME.

Part: ROLL PIN — BROKEN (SERVICE DOOR) · airframe 30,615 hrs · 29,595 cycles

SERVICE DOOR LATCH, RELEASE HANDLE LOOSE, WILL NOT RELEASE SERVICE DOOR. INSPECTED & FOUND ROLL PIN IN DOOR LATCH HANDLE BROKEN. SERVICE DOOR CLOSES & WITNESS MARKS LINE UP REF 254681 1 FOR MEL. R & R ROLL PIN IN THE OPEN LOCK CATCH ON SERVICE DOOR IAW CMM 52-41-10. OPERATIONS CHECKED GOOD. THIS CLEARS MEL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,609 hrs · 29,589 cycles

ORANGE ON FLOOR LIGHT STRIP, EMER EXIT ROW 1, ORANGE OVERLAY MISSING. INSPECTED & FOUND ROW 1 OVERLAY MISSING & ROW 1 IS INOPERATIVE. NO VISIBLE DAMAGE FROM TOP OF LIGHT STRIP IAW 254681 2 FOR MEL.

Part: INDICATOR — READS LOW (COCKPIT) · airframe 39,228 hrs · 35,654 cycles

STANDBY AIRSPEED INDICATOR READS ZERO, ABORTED TAKEOFF AT 75 KTS.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 29,900 hrs · 28,275 cycles

FLIGHT 3815, RECEIVED A FLAP FAIL CAUTION MESSAGE DURING APPROACH. FLAPS FAILED AT 30 DEG. COMPLIED WITH QRH. BTMS 3, 5, 3 & 3 DECLARED AN EMERGENCY AND PERFORMED FLAP RESET PROCEDURE IAW 98-018G BOX 12. FLAPS RESET.

Part: TIRE — BLOWN (NLG) · airframe 29,742 hrs · 28,711 cycles

FLIGHT 3736, OBSERVED VIBRATION ON TAKEOFF, UPON LANDING DISCOVERED RT NLG TIRE BLOWN. NO GEAR DISAGREE MSGS. NO ENG FLUCTUATIONS OBSERVED. NO THRUST REVERSER'S WERE USED ON LANDING. BRAKE TEMPS SHOWED 3, 2, 2, 3. VIBRATION PRESENT ON LANDING ROLL OUT. PERFORMED TIRE BURST INSPECTION IAW AMM 05-51-29, NO DAMAGE TO WINGS, ENGS, NLG BAY, & FLAPS. REF 253516 2 FOR DAMAGE FOUND ON SPADE DOOR. REF 253516 3 FOR TIRE DAMAGE. NO FOD DAMAGE NOTED AROUND ENG NACELLES OF FLIGHT CONTROLS.

Part: CAP — MISSING (EMERGENCY LIGHT) · airframe 29,467 hrs · 28,440 cycles

FLIGHT 3777. END CAP MISSING ON FWD END OF EMERGENCY TRACK LIGHTING. INSTALLED FWD END CAP ON EMERGENCY TRACK LIGHTING. OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (ROW 8) · airframe 29,090 hrs · 28,081 cycles

EMERGENCY LIGHT DOES NOT ILLUMINATE AFT OF ROW 8.

Part: CONTROL ROD — MISRIGGED (LT ENGINE) · airframe 26,345 hrs · 25,507 cycles

AFTER TOUCH DOWN & STOWING T/R RECEIVED LT ENG OIL PRESS MASTER WARNING. OIL PRESS READ 2PSI & ENG SHUT ITS SELF-DOWN ON ITS OWN. COMPLIED WITH QRH, DECLARED EMERGENCY & REQUESTED SPECIAL SERVICE VEHICLES INSPECT AC & ESCORT TO GATE. FOUND THROTTLE CONTROL CABLE MISS RIGGED ON LT ENG. ADJUSTED THROTTLE CONTROL ROD TO PROPER DIMENSIONS IAW AMM 76-10-00. OPERATIONS CHECKED GOOD, LOW OIL PRESS DUE TO ENG SHUT DOWN.

Part: SUPPORT ANGLE — CRACKED (PAX DOOR) · airframe 26,189 hrs · 25,363 cycles

CRACK IN THE 4TH STEP SUPPORT ANGLE AFT SIDE OF PAX DOOR. REMOVED CRACK & INSTALLED REPAIR ANGLE & DOUBLER IAW CRJ 200 REO 601R-852-11-702 REV C.

Part: FITTING — CRACKED (FUSELAGE) · airframe 26,189 hrs · 25,363 cycles

FUSELAGE STATION 484 FLOOR SUPPORT BEAM CLIP AT LBL 36 IS CRACKED. R & R CLIP IAW REO 601R-53-41-059 REV B.

Part: ANGLE — CRACKED (LT WING) · airframe 26,189 hrs · 25,363 cycles

LEFT WING OTBD LE CRACKED AT OTBD END OF SHROUD ANGLE. R & R ANGLE PN 601R12076-7 IAW CRJ 200 SRM 51-42-06 & 51-42-13.

Part: SILL — CORRODED (FUSELAGE) · airframe 26,189 hrs · 25,363 cycles

IN ACCORDANCE WITH WORK ORDER 54253/2000/0054 PART WAS MODIFIED WITHOUT ENGINEERING APPROVAL. PAX DOOR SILL FLOOR SUPPORT ANGLE HAS CORROSION ADJACENT TO AFT PAX DOOR CLEAT AT FS 342. REMOVED THE UNSERVICEABLE FLOOR SILL & INSTALLED A SERVICEABLE FLOOR SILL IAW CRJ 200 SRM 51-42-21,51-42-06, 51-42-15, 51-45-00.

Part: SKIN — DENTED (TE FLAP) · airframe 26,189 hrs · 25,363 cycles

RIGHT INBD FLAP LOWER SKIN DENTED AT WS 120.00, ADJACENT TO PREVIOUS DOUBLER REPAIR. REPAIR DENTED AREA IAW EA 15-2013-520.

Part: TRUNNION — DAMAGED (LT MLG) · airframe 26,189 hrs · 25,363 cycles

DURING COLD WORKING OF THE MLG TRUNNION FASTENER HOLES, FOUND ONE EACH OVERSIZED HOLE ON LT LOWER FLANGE. REWORKED OVERSIZED FASTENER HOLE ON LT MLG TRUNNION FLANGE IAW REO 601R-57-21-2060 REV.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,189 hrs · 25,363 cycles

LEFT SIDE SEAT RAIL FROM FS 449.85 - 499 IS BADLY CORRODED ALONG ENTIRE LOWER INNER SURFACE OF RAIL. R & R SEAT RAIL.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 26,189 hrs · 25,363 cycles

RIGHT MLG BRAKE PRESS TRANSDUCER FWD & AFT BRACKETS ARE CRACKED, R & R.

Part: TRUNNION — DAMAGED (RT MLG) · airframe 26,189 hrs · 25,363 cycles

DURING COLD WORKING OF THE MLG TRUNNION FASTENER HOLES, FOUND ONE EACH OVERSIZED HOLE ON RT LOWER FLANGE. REWORKED OVERSIZED FASTENER HOLE ON RT MLG TRUNNION FLANGE IAW REO 601R-57-21-2060 REV.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 26,189 hrs · 25,363 cycles

LEFT MLG BRAKE PRESS TRANSDUCER BRACKET. R & R BRACKET.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 26,189 hrs · 25,363 cycles

NUMBER 1 HYD RETURN FILTER BRACKET CRACKED. REMOVED UNSERVICEABLE BRACKET IAW CRJ 200 SRM 51-42-06 & INSTALLED A SERVICEABLE BRACKET IAW CRJ 200 SRM 51-42-06.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,189 hrs · 25,363 cycles

PASSENGER SEAT TRACKS HAVE CORROSION AT RBL 9 & LBL 9 FS 368. REMOVED UNSERVICEABLE SEAT TRACKS SEGMENTS LBL 9 & RBL 9, FS 369. FABRICATED & INSTALLED NEW SERVICEABLE SEAT TRACK SECTIONS IAW REO 601R-53-00-485 IAW CRJ 200 SRM 53-21-?.

Part: HINGE BRACKET — CRACKED (RT AILERON) · airframe 26,189 hrs · 25,363 cycles

RIGHT AILERON CTR HINGE, CTR SAFETY PLATE BETWEEN HINGE BOLTS IS CRACKED & BENT. R & R A SERVICEABLE RT AILERON CTR HINGE BRACKET.

Part: BRACKET — CRACKED (PAX DOOR) · corrosion level 2 · airframe 26,189 hrs · 25,363 cycles

BRACKETS TWO EACH CORRODED BEYOND LIMITS AT PAX DOOR, CLEATS TWO EACH CORRODED BEYOND LIMITS AT PAX DOOR. REPLACED TWO EACH BRACKETS & TWO EACH CLEATS AT PAX DOOR.

Part: DRAG ANGLE — CRACKED (RT WING) · airframe 26,189 hrs · 25,363 cycles

RIGHT MLG DRAG ANGLE COMMON TO BATT RIB CRACKED. REPLACED RT MLG DRAG ANGLE IAW CRJ SRM 51-42-21.

Part: STRUCTURE — CRACKED (PAX DOOR) · airframe 26,189 hrs · 25,363 cycles

PASSENGER DOOR EDGE MEMBER IS CRACKED AT THE AFT EDGE UNDER RIVET ROW. REPAIRED CRACKED PAX DOOR EDGE MEMBER IAW REO 601R-52-11-229.

Part: HOUSING — CRACKED (CARGO DOOR) · airframe 26,189 hrs · 25,363 cycles

CARGO BAY OUTER HANDLE HOUSING IS CRACKED. REPLACED CARGO BAY OUTER HANDLE HOUSING.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 26,189 hrs · 25,363 cycles

LEFT HEAT EXCHANGER AFT INBD SUPPORT ROD HAS CRACKED CLIP. R & R SUPPORT ROD CLIP.

Part: RIB — CRACKED (RT WING) · airframe 26,189 hrs · 25,363 cycles

RIGHT MLG BATT RIB CRACKED. REPAIR IAW CRJ REO 601R-57-51-046.

Part: SKIN — DENTED (FUSELAGE) · airframe 26,189 hrs · 25,363 cycles

PROTRUDING DENT 3.2 INCHES LONG X 2.1 INCHES WIDE X .053 INCHES DEEP WITH .160 X .090 GOUGE CTR OF DENT. REPAIRED IAW STS EA 15-2013-518.

Part: DRAG ANGLE — WORN (LT MLG) · airframe 26,189 hrs · 25,363 cycles

LEFT MLG DRAG ANGLE. R & R ANGLE IAW CRJ SRM 51-42-21.

Part: FITTING — CRACKED (FUSELAGE) · airframe 26,189 hrs · 25,363 cycles

INBOARD CLIPS CRACKED AT FS 280.00 RBL 9 & LBL 9. FABRICATED, DRILLED, LOCATED & INSTALLED SERVICEABLE INBD RBL 9 & LBL 9 280 CLIPS.

Part: RETAINER — CORRODED (E&E DOOR) · corrosion level 2 · airframe 26,189 hrs · 25,363 cycles

AVIONICS BAY DOOR SEAL RETAINER HAS CORROSION. R & R AVIONICS BAY DOOR SEAL RETAINERS IAW CRJ 200 SRM 51-42-06 & 51-42-13.

Part: SUPPORT — CRACKED (PAX DOOR) · airframe 26,189 hrs · 25,363 cycles

PASSENGER DOOR LOWER STEP SUPPORT SKIN FWD & AFT BRACKETS ARE CRACKED. REPAIRED IAW STS EA 15-2013-509.

Part: NUT PLATE — DAMAGED (BS 409) · airframe 21,727 hrs · 20,927 cycles

NUTPLATE FOR LOWER VHF-2 ANTENNA IS DAMAGED AND UNSERVICEABLE. REPAIRED VHF-2 ANTENNA NUTPLATE AND MOUNTING HOLE IAW REO 601R-53-21-2265, REV A.

Part: HINGE FITTING — CHAFED (LT WING TE FLAP) · airframe 21,847 hrs · 21,065 cycles

LT INBD FLAP INBD FLAP HINGE BOX IS CHAFING LWR INBD BRACKET. R & R LT INBD FLAP INBD FLAP HINGE BOX INBD BRACKET.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 21,847 hrs · 21,065 cycles

PAX DOOR AFT DRAG ANGLE CRACKED ABOVE POWER ASSIST PULLEY BRACKET. R & R PAX DOOR AFT DRAG ANGLE SECTION IAW SRM 51-42-06.

Part: MOUNT BRACKET — CRACKED (PAX DOOR) · airframe 21,847 hrs · 21,065 cycles

PAX DOOR POWER ASSIST MOTOR MOUNT BRACKET CRACKED REMOVED DAMAGED MOUNT BRACKET AND INSTALLED NEW SERVICEABLE PAX DOOR POWER ASSIST MOTOR MOUNT BRACKET IAW SRM 51-42-06.

Part: TIE DOWN — CORRODED (FS 559) · corrosion level 2 · airframe 21,847 hrs · 21,065 cycles

CARGO BAY TIE DOWN TRACKS AT LBL 9 & RBL 9 HAVE CORRODED HARDWARE SCREWS AT FS 559+112 INSTALLED SERVICEABLE (2) CARGO TIE DOWN TRACKS IAW SRM 51-42-02.

Part: SKIN — DAMAGED (RT NACELLE) · airframe 21,847 hrs · 21,065 cycles

RT UPPER CORE COWL HAS SCRATCHES ON OUTER SKIN. REPAIRED RT UPPER CORE COWL OUTER SKIN ON OTBD SIDE IAW CMM 71-12-01, REPAIR SRS 021.

Part: HINGE FITTING — GOUGED (RT AILERON) · airframe 21,847 hrs · 21,065 cycles

RT AILERON INBD/CNTR HINGE LUG GOUGED. REMOVED GOUGE IAW REO 601R-57-51-573.

Part: HANDLE — CRACKED (PAX DOOR) · airframe 21,727 hrs · 20,927 cycles

PAX DOOR OUTER HANDLE SPRING DOOR CRACKED. R & R PAX DOOR OUTER HANDLE SPRING DOOR IAW SRM 51-42-06.

Part: STRIKER — DAMAGED (PAX DOOR) · airframe 21,847 hrs · 21,065 cycles

PAX DOOR CUT OUT AFT SEAL STRIKER DAMAGE. REPAIRED IAW REO 601R-53-22-033, REV C.

Part: ATTACH BRACKET — CRACKED (BS 718) · airframe 21,847 hrs · 21,065 cycles

AFT EQUIPMENT COMPARTMENT, RT NR 2 HYD SYS RETURN FILTER ATTACH BRACKET IS CRACKED AFT LOWER CORNER. REPAIRED ATTACH BRACKET IAW REO 601R-53-62-031, REV A.

Part: DOOR — CRACKED (PAX DOOR HANDLE) · airframe 21,847 hrs · 21,065 cycles

PAX DOOR OUTER HANDLE SPRING DOOR CRACKED. R & R PAX DOOR OUTER HANDLE SPRING DOOR IAW SRM 51-42-06.

Part: SEAL — DAMAGED (FS 663.4) · airframe 21,847 hrs · 21,065 cycles

PANEL 412BT HAS CHAFING ON EXTERIOR SIDE HAS CRACKED SEAL RETAINER WITH DAMAGED SEAL. REPLACED SEAL RETAINER BLENDED EXTERIOR SIDE OF PANELS.

Part: ANGLE — CRACKED (FS 484) · airframe 21,847 hrs · 21,065 cycles

INBD ANGLE ON LBL 27 AT FS 484 CRACKED. COMPLIED WITH REO 601R-53-41-059, REV B.

Part: SKIN — CHAFED (LT NACELLE) · airframe 21,847 hrs · 21,065 cycles

LT LOWER CORE COWL OUTER SKIN CHAFED FROM LOCKER DOOR COMPLIED WITH CMM. REPAIR SRS 104428.

Part: SKIN — CHAFED (RT NACELLE) · airframe 21,847 hrs · 21,065 cycles

RT LOWER CORE COWL OUTER SKIN CHAFED FROM BLOCKER DOOR. COMPLIED WITH CMM REPAIR SRS 104C.

Part: DUCT — DISCONNECTED (LT A/C PACK)

ON APPROACH, SMELLED ELECTRICAL ODOR IN COCKPIT. ODOR DID NOT APPEAR TO BE COMING FROM GASPERS. ODOR NOT PRESENT IN CABIN AREA. OPERATED ALL ELECTRICAL CONSUMERS AND LIGHTS WHILE OPERATING ENGINES WITH ACMS. ISOLATED ELECTRICAL ODOR PRESENT REF 220998/2 FOR MEL. INSPECTED LT PACK ASSY FOUND Y-DUCT DISCONNECTED AND CRACKED. R & R LT PACK DISCHARGE Y DUCT IAW AMM 21-51-15 ALONG WITH CLEANING LT COALSCER BAG IAW AMM 21-51-13 LEAK AND OPS CHECK GOOD, NO UNUSUAL NOTED, CLEARED MEL.

Part: PRESSURE BLKHD — PUNCTURED (BS 621) · airframe 19,925 hrs · 18,980 cycles

AFT PRESSURE BULKHEAD AT FS 621 IS PUNCTURED ON LOWER LT SIDE. REPAIRED PUNCTURE ON LOWER LT SIDE OF FS 621 BULKHEAD IAW REO 601R-53-61-4035.

Part: PRESSURE BLKHD — CHAFED (BS 621) · airframe 19,925 hrs · 18,980 cycles

AFT PRESSURE BULKHEAD AT FS 621 ON FWD SIDE HAS 4 CHAFED AREAS ALONG LOWER SIDE OF BULKHEAD AT RBL 41.70, LBL 32.00, RBL 22.50 AND RBL 32.00.

Part: PRESSURE BLKHD — DENTED (BS 621) · airframe 19,925 hrs · 18,980 cycles

AFT PRESSURE BULKHEAD AT 621 LT FWD SIDE IS DENTED ON LWR LT SIDE. REPAIRED DENT ON LOWER LT SIDE OF FS 621 BULKHEAD IAW REO 601R-53-61-4035.

Part: CONTROL UNIT — INOPERATIVE (NLG STEERING) · airframe 19,053 hrs · 18,081 cycles

AFTER TAKEOFF, RECEIVED STEERING INOP CAUTION MESSAGE COMPLIED WITH QRH UNABLE TO RESET. R & R STEERING HANDWHEEL CONTROL UNIT, IAW AMM 32-51-01. OPS CK GOOD.

Part: SWITCH — INOPERATIVE (THRUST REVERSER) · airframe 18,598 hrs · 17,590 cycles

DURING CLIMB OUT AND AFTER THRUST REVERSER WAS DISARMED, RECEIVED GREEN THRUST REVER SER ICON IN LT N1 GUAGE, NO ABNORMAL THRUST INDICATION THRUST LEVER SETTING WERE NOTED. R & R LT T/R DEPLOY SWITCH IAW AMM 78-37-01. OPS CK OK. LT T/R SYSTEM GOOD AT THIS TIME. REMOVED PLACARD AND MEL.

Part: SWITCH — DEFECTIVE (THRUST REVERSER) · airframe 18,643 hrs · 17,640 cycles

DURING CLIMB OUT AND AFTER T/R WAS DISARMED RECEIVED GREEN THRUST REVERSER ICON IN LT N1 GUAGE, NO ABNORMAL THRUST INDICATION THRUST LEVER SETTING WERE NOTED. R & R LT T/R DEPLOY SWITCH IAW AMM 78-37-01. OPS CHECK OK. LT T/R SYS GOOD AT THIS TIME. REMOVED PLACARD AND MEL.

Part: DOOR — BINDING (MAIN PAX) · airframe 18,112 hrs · 17,071 cycles

F/A REPORTS PAX DOOR DIFFICULT TO OPEN. DOOR HANDLE MOTION FROM STOWED TO OPEN POSITION IS DIFFICULT AND NOT SMOOTH. C/W OPS TEST OF PAX DOOR IAW AMM 52-11-00710-801. NO DEFECT NOTED.

Part: ATTACH BRACKET — CRACKED (LT WING TE FLAP) · airframe 17,063 hrs · 15,949 cycles

LT WING BUTE 594JB ATTACH BRACKET BROKEN. REMOVED BROKEN BRACKET & REPLACED WITH NEW BRACKET PN 600-10196-15.

Part: HANDLE — CRACKED (PAX DOOR) · airframe 17,063 hrs · 15,949 cycles

PAX DOOR OUTER HANDLE IS CRACKED ON AFT OTBD SIDE. R & R PAX DOOR OUTER HANDLE ASSY PN 601R31704-9 IAW AMM 52-11-03.

Part: ATTACH FITTING — CHAFED (RT WING) · airframe 17,063 hrs · 15,949 cycles

RT OTBD FLAP ALIGNMENT ROLLER ATTACH FITTING IS CHAFED. BLENDED CHAFE SMOOTH IAW REO 601R-57-53-779.

Part: BRACKET — CRACKED (PAX DOOR) · airframe 17,063 hrs · 15,949 cycles

FOUND CRACKED UPON VISUAL INSPECTION, NEW BRACKET MFG AND INSTALLED IAW SRM 51-42-06.

Part: MOUNT — CRACKED (PRECOOLER) · airframe 17,063 hrs · 15,949 cycles

SUPPORT MOUNT FOR LT PRECOOLER TO BELLOW FOUND TO BE CRACKED W/O 51539, W/C 3000-0038. R & R BRACKET IAW CRJ 200-51-24-21.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 17,063 hrs · 15,949 cycles

INBD CLIP AT FS 280, INBD OF RBL 9.0 APPEARS TO BE CRACKED. REMOVED CRACKED CLIP AND INSTALLED SERVICEABLE CLIP IAW REO 601R-53-11-171.

Part: ATTACH FITTING — CORRODED (BS 311.75) · airframe 17,063 hrs · 15,949 cycles

PAX DOOR DRAINAGE RAMP AREA HAS 4 EA CORRODED CLIPS. R & R DUPLICATED PARTS.

Part: PANEL — CRACKED (COCKPIT) · airframe 17,063 hrs · 15,949 cycles

FLIGHT DECK PANEL 222DZ MAP POCKET IS CRACKED. R & R MAP POCKET ON PNL 222DZ, PN 601R422517 IAW SRM 51-42-06.

Part: ANGLE — CRACKED (PAX DOOR HANDLE) · airframe 17,063 hrs · 15,949 cycles

PAX DOOR INNER HANDLE MOUNTING ASSY IS CRACKED. DUPLICATED PART (REMOVED CRACKED ANGLE ON INNER HANDLE ASSY AND FABRICATED NEW ANGLE IAW SRM 51-42-06, 51-25-16, 51-25-06.

Part: STRUCTURE — CRACKED (LT PYLON) · airframe 17,063 hrs · 15,949 cycles

PYLON PANEL 412BT SEPARATOR CLIP IS CRACKED. R & R SEPARATOR CLIP PN 601-37003-183 IAW SRM 51-42-06.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 17,063 hrs · 15,949 cycles

INBD FS 280, CLIP ON LBL 9.0 APPEARS TO BE CRACKED. REMOVED CRACKED CLIP ON INBD SIDE OF LBL 9.0 AT FS 280 AND INSTALLED SERVICEABLE CLIP IAW REO 601R-53-11-171.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 17,063 hrs · 15,949 cycles

FLOORBEAM ANGLE AT FS 280 OTBD OF RBL 9.0 CRACKED. REPAIRED ANGLE IAW REO 601R-53-11-136.

Part: RIB — CRACKED (LT WING) · airframe 17,063 hrs · 15,949 cycles

BATT RIB CRACKED IN LT MLG WW REPAIRED LT BATT RIB IAW 601R-57-51-046.

Part: ANGLE — CRACKED (BS 625) · airframe 17,063 hrs · 15,949 cycles

RT OBLIQUE ANGLE IN AFT EQUIPMENT BAY CRACKED. REMOVED RT OBLIQUE ANGLE PN 601-35012-52, DISCARD INSTALLED NEW ANGLE PN 601-35012-52, IAW SRM 51-42-21, 51-40-11, 51-21-16.

Part: ANGLE — CRACKED (BS 625) · airframe 17,063 hrs · 15,949 cycles

LT OBLIQUE ANGLE IN AFT EQUIPMENT BAY CRACKED. REMOVED CRACKED LT OBLIQUE ANGLE, INSTALLED NEW SERVICEABLE LT OBLIQUE ANGLE PN 601-35012-51, IAW SRM 51-42-21, 51-40-11, 51-21-16.

Part: SILL — CRACKED (BS 574) · airframe 17,063 hrs · 15,949 cycles

CARGO DOOR FLOOR SILL CRACKED UNDER FWD FOLDING SKID PLATE ANCHOR AT FASTENERS. REPAIRED CARGO DOOR FLOOR SILL CRACKS BY INCORPORATION OF REO 601R-53-61-1741.

Part: SUPPORT — CRACKED (CARGO DOORWAY) · airframe 17,063 hrs · 15,949 cycles

FWD LOWER CARGO DOOR CAM TRACK SUPPORT ASSY IS BENT AND CRACKED. REMOVED CRACKED CHANNEL FABRICATED NEW CHANNEL AND INSTALLED.

Part: ATTACH FITTING — CRACKED (BS 484) · airframe 17,063 hrs · 15,949 cycles

CLIP CRACKED, R & R DAMAGED CLIP ON RT INBD 484 INTERCOSTAL IAW SRM 51-24-21, 51-42-06, 51-42-21.

Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 16,729 hrs · 15,618 cycles

FS 621.00, PRESSURE BULKHEAD WEB FOUND CRACKED AT UPPER END OF AFT CARGO TRACK LBL 27.50, WL 130.00. PRESSURE BULKHEAD WEB AT FS 621.00, LBL 27.50, WL 130.00. REPAIRED IAW REO 601R-53-61-1541, REV B. (K)

Part: BULKHEAD — CRACKED (BS 621) · airframe 16,729 hrs · 15,618 cycles

FS 621.00, AFT PRESSURE BULKHEAD FOUND CRACKED AT LINTEL FITTING AREA W/L 110.00. REPAIR PERFORMED ON AFT PRESSURE BULKHEAD AT FS 621.00, W/L 110.00 IAW REO 601R-53-61-1230, REV D. (K)

Part: A/C PACK — SMOKE (RIGHT) · airframe 15,380 hrs · 14,300 cycles

RT PACK HIGH TEMP CAUTION MESSAGE ALONG WITH ODOR OF SMOKE. PLACED ON MEL AND PLACARDED. REMOVED AND REPLACED RT ACM IAW AMM 21-51-10. OPS CHECK GOOD. REMOVED PLACARD AND REMOVED FROM MEL. (K)

Part: UNKNOWN — ODOR (CABIN) · airframe 13,636 hrs · 12,616 cycles

SUSPICIOUS ODOR IN FRONT OF CABIN, APPEARS ELECTRICAL IN NATURE. DETERMINED ELECTRICAL ODOR COMING FROM POWER UNIT/DIMMER CEILING LIGHTS B101. REMOVED AND REPLACED CEILING LIGHTS POWER UNIT DIMMER B101 IAW AMM 33-20-04, REMOVED AND REPLACED SIDEWALL LIGHTS DIMMER B102 IAW 33-21-10, REMOVED AND REPLACED CEILING LIGHT POWER RELAY IAW AMM 33-21-06, REMOVED AND REPLACED SIDEWALL LIGHTS POWER RELAY IAW AMM 33-21-12. OPS CHECK GOOD. (S)

Part: ENGINE — BIRD INGESTION (LEFT) · airframe 12,912 hrs · 11,927 cycles

LARGE BIRD INGESTED, LEFT ENGINE AT 1000 AGL DURING TAKEOFF FROM PHL, GEAR EXTENDED PERFORMED AIR RETURN TO PHL, LANDED AT 43,700 LBS. C/W BIRDSTRIKE INSP REF AMM 05-51-25 REF W/O 123145 FOR AW WORK FOUND.

Part: FLAP SYSTEM — FAILED (TE FLAPS) · airframe 12,597 hrs · 11,622 cycles

AFTER LANDING, ON TAXI, FLAPS FAILED CAS MESSAGE (45 DEGREES) PERFORMED RESET IAW SUPPLEMENT 98-018B. DURING TEST FLAPS FAILED AT 20 DEGREES. (K)

Part: FRAME — DENTED (FUSELAGE) · airframe 12,325 hrs · 11,362 cycles

FRAME DENTED OVER LIMITS AT FS 700.00 BTW STR 22L TO STR 23L. FRAME SELECTOR REPLACED AT FS 700.00 BTW STR 22L TO 23L SRM 51-42-06. (K)

Part: SEPARATOR — CORRODED (LT PYLON) · airframe 12,325 hrs · 11,362 cycles

QTY 1 SEPARATOR HAS FRETTING ON LT PYLON ACCESS PANEL 421DB. (K)

Part: SEPARATOR — DAMAGED (LT PYLON) · airframe 12,325 hrs · 11,362 cycles

QTY 1 SEPARATOR HAS FRETTING ON LT PYLON ACCESS PANEL 412DB. QTY (1) SEPARATOR REPLACED ON LT PYLON ACCESS PANEL 412DB IAW SRM 51-42-06. (K)

Part: BRACKET — UNKNOWN (RT NACELLE) · airframe 12,325 hrs · 11,362 cycles

RT ENGINE UPPER CORE COWL STA ROD PIN AND BRACKET (SPRING CLIP) FOUND. RT ENGINE UPPER CORE COWL STAY ROD PIN REPLACED AND BRACKET (SPRING CLIP) REPLACED IAW SRM 51-42-06. (K)

Part: FRAME — DENTED (BS 700 S22-23L) · airframe 12,325 hrs · 11,362 cycles

DENT EXIST ON SKIN FS 700 STR L 22 TO L 23. REMOVED FRAME IAW REO 601R-53-61-2482. NEW FRAME INSTALLED IAW SRM 51-42-06. (K)

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 12,325 hrs · 11,362 cycles

CRACK FOUND ON FLOOR STRUCTURE ON FS 280, LBL 9. DAMAGE ON FLOOR STRUCTURE AT FS 280, LBL 9 REPAIRED IAW REO 601R-53-11-171. (K)

Part: FITTING — GOUGED (FUSELAGE) · airframe 12,325 hrs · 11,362 cycles

PAX DOOR SURROUND STRUCTURE CAM FITTING GOUGE ON FS 349, STR 5L. REPLACED IWA SRM 51-42-21. (K)

Part: BRACKET — GOUGED (FUSELAGE) · airframe 12,325 hrs · 11,362 cycles

PAX DOOR SURROUND STRUCTURE ROLLER BRACKET GOUGED ON FS 349, STR 6L. SURROUND STRUCTURE NEW ROLLER BRACKET INSTALLED ON PAX DOOR AT FS 349, STR 6 IAW SRM 51-41-04. (K)

Part: SUPPORT ANGLE — CRACKED (HEAT EXCHANGER) · airframe 12,325 hrs · 11,362 cycles

ANGLE CRACK ON RT HEAT EXCHANGE SUPPORT STRUCTURE BTW FS 700 AND FS 718. ANGLE REPLACED ON RT HEAT EXCHANGER SUPPORT STRUCTURE BTW BS 700 AND BS 718 IAW SRM 51-24-16 AND SRM 51-42-06. (K)

Part: BULKHEAD — GOUGED (FUSELAGE) · airframe 12,325 hrs · 11,362 cycles

GOUGE FOUND ON AFT OF FLIGHT COMPARTMENT BULKHEAD RBL9, WL 97.50 (.250 X 300). (K)

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 12,325 hrs · 11,362 cycles

CRACK EXIST ON INTERCOSTAL LBL 27 AND LBL 36, FS 484. BRACKET REPLACED ON INTERCOSTAL LBL 27 AND LBL 36, FS 484. (K)

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 12,325 hrs · 11,362 cycles

FRETTING FOUND ON AFT OF FLIGHT COMPARTMENT OF BULKHEAD RBL 9, WL 97.50 (250 X 300) .002 DEEP. FRETTING REMOVED IAW SRM 51-12-00. SURFACE FINISH APPLY IAW SRM 51-25-16. (K)

Part: FLOORBEAM — CRACKED (FUSELAGE)

ANGLE CRACK ON IB SIDE OF FLOORBEAM AT FS 280, RBL 9. NEW ANGLE INSTALLED ON IB SIDE OF FLOORBEAM AT FS 280, RBL 9, SRM 51-42-20. (K)

Part: ANGLE — CRACKED (LT PYLON) · airframe 12,325 hrs · 11,362 cycles

ONE ANGLE IS CRACKED ON LT PYLON ACCESS PANEL 412BT. ANGLE ON LT PYLON ACCESS PANEL 412BT, REPLACED IAW SRM 51-42-06. (K)

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 12,325 hrs · 11,362 cycles

CRACK ON FLOOR SUPPORT STRUCTURE FS 280, RBL 9. REPAIRED IAW REO 61R-53-11-171, REV D. (K)

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 12,325 hrs · 11,362 cycles

FS621.0 AT REAR PRESSURE BULKHEAD AND CARGO DOOR STRUCTURE JUNCTION, ONE CLIP CRACKED. LT FS 621.00 AT REAR PRESSURE BULKHEAD AND CARGO DOOR STRUCTURE INTERCOSTAL QTY (1) ONE CLIP REPLACED IAW SRM 51-24-16 AND SRM 51-42-21. (K)

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 12,325 hrs · 11,362 cycles

CRACK EXIST ON INTERCOSTAL RBL 27, FS 484. BRACKET ON INTERCOSTAL RBL 27, FS 484, REPLACED IAW SRM 51-42-06. (K)

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 12,325 hrs · 11,362 cycles

CRACK EXIST ON FLOOR SUPPORT STRUCTURE FS621, LBL 41. CRACK REMOVED ON FLOOR SUPPORT STRUCTURE FS 621, LBL 41 IAW REO 601R-53-61-117. (K)

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 12,325 hrs · 11,362 cycles

BTW FS 621.00 AT RT STR 14 STRINGER CLIP CRACKED. NEW STRINGER CLIP INSTALLED IAW SRM 51-42-20. (K)

Part: BRACKET — GOUGED (CARGO BAY) · airframe 12,325 hrs · 11,362 cycles

BRACKET ASSY FWD AND AFT OF CARGO STEP PLATE FOUND GOUGED. BRACKET ASSY FWD AND AFT ON CARGO STEP PLATE REPLACED IAW SRM 51-42-21. (K)

Part: NOSE COWL — WORN (LT ENGINE) · airframe 12,325 hrs · 11,362 cycles

LT ENGINE UPPER NOSE COWL (432AT) AFT CORNER WORN THIN. REPLACED ON LT ENG UPPER NOSE COWL (432AT) AFT CORNER IAW CMM 71-14-01-300-814-A01. (K)

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 12,325 hrs · 11,362 cycles

CRACK SUSPECTED ON LT FWD PRESSURE BULKHEAD FS 202.75 AT PARKING BRAKE FITTING CUTOUT. REPAIR PERFORMED ON FWD PRESSURE BULKHEAD FS 202.75 AT PARKING BRAKE CUTOUT IAW REO 601R-53-11-563. (K)

Part: NOSE COWL — WORN (LT ENGINE) · airframe 12,325 hrs · 11,362 cycles

LT ENGINE LOWER NOSE COWL (432AB) AFT CORNER WORN THIN.. (K)

Part: SUPPORT BRACKET — CRACKED (LT MLG WW) · airframe 12,325 hrs · 11,362 cycles

MLG BAY LT HYDRAULIC SUPPORT BRACKET FOUND CRACKED. MLG BAY LT NEW HYDRAULIC SUPPORT BRACKET INSTALLED IAW SRM 51-42-06. (K)

Part: HANDLE — CRACKED (E&E DOOR) · airframe 12,325 hrs · 11,362 cycles

HANDLE ASSY CRACKED ON AVIONIC BAY DOOR. HANDLE ASSY REPLACED ON AVIONIC BAY ACCESS DOOR IAW SRM 51-42-06 IAW AMM 52-41-03-400-801. (K)

Part: SUPPORT FITTING — DAMAGED (LT HANDRAIL) · airframe 12,325 hrs · 11,362 cycles

LT HANDRAIL SUPPORT FITTING CHAFED AND BENT ON PAX DOOR. REPLACED LT HANDRAIL SUPPORT FITTING ON PAX DOOR. (K)

Part: HINGE — DAMAGED (PAX DOOR) · airframe 12,325 hrs · 11,362 cycles

PASSENGER DOOR VERTICAL FOLDING STEP HINGE REPLACED IAW SRM 51-42-06. (K)

Part: ADC — MALFUNCTIONED (NR 2)

AIR RETURN, AFTER TAKEOFF RECEIVED AIRSPEED, ALTITUDE, HEADING MESSAGES ON PFD2, COMPLIED WITH QRH FOR EACH AS WELL AS ADC FAILURE. REPLACED NR 2 ADC USING AMM 34-13-01. PERFORMED OPS CHECK OF ADC NR 2 USING AMM 34-13-01-710-801 CHECK GOOD. PERFORMED FUNCTIONAL CHECK OF PITOT/STATIC SYSTEM USING AMM 34-11-00-720-801, CHECKS GOOD. (M)

Part: CONNECTOR — DEFECTIVE (WEATHER RADAR) · airframe 10,181 hrs · 9,244 cycles

CIRCUIT BREAKER PANEL 1, K3 POPPED (WEATHER RADAR RT). REMOVED AND REPLACED RADAR ANTENNA ELEC CONNECTOR AND WEATHER RADAR ANTENNA IAW AMM 34-41-01. REMOVED AND REPLACED WEATHER RADAR CONTROL PANEL IAW 34-41-04, RAN OPS CHECK OF WEATHER RADAR IAW AMM 34-41-00. OPS GOOD. NO NOTICE OF LIGHTNING STRIKE DAMAGE. (K)

Part: SENSOR — MALFUNCTIONED (TE FLAPS)

FLAP FAIL CAUTION MESSAGE INFLIGHT, FAILED AT ZERO. PERFORMED EXTERNAL VISUAL INSPECTION OF EACH OUTBOARD FLAP, NO EVIDENCE OF TWISTING, SQUEEZING OR ABNORMAL DEFORMATIONS, RESET. UPON INSPECTION OF THE FECU FOUND LEFT BPSU SENSOR FAULT ERROR CODES. REMOVED AND REPLACED LT BPSU. BRAKE AND POS SENSOR UNIT P/N 855D10011, S/N 1878. (M)

Part: UNKNOWN — UNKNOWN (TE FLAPS) · airframe 9,548 hrs · 8,615 cycles

CLIMBING OUT AT 5000 FT FLAPS AT ZERO, FLAP FAIL AMBER CAUTION CAS MESSAGE, CW QRH. PERFORMED ZERO FLAP LANDING, APPLIED BRAKES AT 80 KNOTS, MAX BTMS READING WAS 3. NORMAL LANDING WEIGHT. PERFORMED INSPECTION IAW AWAC SUPPLEMENT 98-18, NO EVIDENCE OF TWISTING OR SKEWING OR ABNROMAL DEFORMATION OF FLAPS. RESET THE FLAP SYSTEM, TEST GOOD. RESET THE FLAP SYSTEM, TEST GOOD. (K)

Part: PITOT TUBE — FOD (RIGHT) · airframe 9,430 hrs · 8,497 cycles

SMOKE ODOR IN COCKPIT AFTER ENGINE SHUTDOWN AND LEAVING AIRCRAFT CHECKLIST WITH BATTERY MASTER ON. INSPECTED PITOT SYS FOUND FOD IN RT PITOT TUBE REMOVED AND REPLACED RT PITOT TUBE RUN PITOT STATIC LEAK CHECK, NO LEAKS FOUND, SYSTEM CHECKS NORMAL. (K)

Part: WINDOW — FAILED (COCKPIT) · airframe 9,389 hrs · 8,462 cycles

F/O WINDOW SHATTERED. REMOVED AND REPLACED F/O SIDE WINDOW IAW AMM. OPS CHECK AND LEAK CHECK GOOD. (K)

Part: SKIN — GOUGED (BS 643 S23-24)

FOUND GOUGED DENT AT FS 643 APPROX 6 INCHES LONG BETWEEN STRINGER 23 AND STRINGER 24. (M)

Part: SKIN — PUNCTURED (BS 640)

AIRCRAFT FUSELAGE PUNCTURED BY BELT LOADER AT FS 640.00 BETWEEN STRINGERS 23L AND 24L. (M)

Part: SKIN — GROUND DAMAGE (BS 605)

FOUND FUSELAGE DAMAGED BY BELT LOADER UNDER CARGO DOOR BETWEEN FS 605.00 AND FS 621.00 AND STR 22L TO STR 0 CL. MAINTENANCE PERFORMED MAJOR REPAIR TO FS 605 AND FS 621 AT STRINGER 22L TO STRINGER 25L IAW BOMBARDIER SERVICES CORPORATION EO 601R-53-9415. (M)

Part: SENSOR — FAILED (LT PACK) · airframe 7,893 hrs · 7,017 cycles

WHILE RUNNING LT PACK IN AUTO MODE AT FULL COLD DUCT TEMP EXCEEDED 100 C, SMOKE IN COCKPIT, SHUT OFF PACK AND SMOKE CLEARED. CM ACTION C/W PLACARDED AND PLACED ON MEL. REMOVED AND REPLACED LT PACK TEMP SENSOR (RT4HB) OPS CHECK GOOD. REMOVED FROM MEL AND PLACARD. IAW AMM, NO DEFECTS NOTED. (K)

Part: ACM — SMOKE (LT ACM) · airframe 7,873 hrs · 6,996 cycles

SMOKE IN COCKPIT AND CABIN ON GROUND AT GATE. REMOVED AND REPLACED LT AIR CYCLE MACHINE, OPS CHECK GOOD IAW AMM, THIS CLEARS MEL, PLACARD REMOVED. (K)

Part: FLOOR SUPPORT — CRACKED (RT SIDE,FS621) · airframe 7,386 hrs · 6,515 cycles

CARGO FLOOR SUPPORT RT SIDE AT FS 621 CRACKED .50 INCH LONG. MAINTENANCE REPAIRED CARGO FLOOR SUPPORT AT FS 621.00 RT SIDE IAW REO. (K)

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 7,386 hrs · 6,515 cycles

FS 484 INTERCOSTAL ANGLE AT LBL 36 IS CRACKED. MAINTENANCE REPAIRED FS 484 INTERCOSTAL ANGLE AT LBL36 IAW REO. (K)

Part: ANGLE — CRACKED (FUSELAGE) · airframe 7,386 hrs · 6,515 cycles

FS 484 INTERCOSTAL ANGLE AT RBL 36 IS CRACKED. MAINTENANCE REPAIRED FS 484 INTERCOSTAL ANGLE AT RBL 36 IAW REO. (K)

Part: SKIN — CORRODED (RT WING)

FOUND RIGHT WING PLANK HOLE NR 11 HAS CORROSION AT OUTBOARD SIDE 2 INCHES LONG BY .002 INCH - .003 INCH DEEP. NOT IN CRITICAL AREA. MAINTENANCE REPAIRED RIGHT WING PLANK ACCESS HOLE AT WS 209.040 HOLE NR 11 IAW BOMBARDIER REO 601R-57-21-030 REV D. (M)

Part: SKIN — CORRODED (FUSELAGE)

FOUND RIGHT WING HOLE NR 1 HAS CORROSION ON THE INBOARD SIDE 2 INCHES LONG BY .003 INCH - .005 INCH DEEP AND AT OUTBOARD AFT SIDE 1.3 INCH LONG BY .003 INCH - .005 INCH DEEP. NOT IN CRITICAL AREA. MAINTENANCE REPAIRED RIGHT WING PLANK ACCESS HOLE AT WS 54.897 HOLE NR 1 IAW BOMBARDIER REO 601R-57-21-030 REV D. (M)

Part: STRUCTURE — CORRODED (RT WING) · airframe 7,386 hrs · 6,515 cycles

RT WING PLANK HOLE NR 14 HAS CORROSION AT IB SIDE 8 INCH L X .002 INCH-.003 INCH DEEP AND AT OB SIDE 5 INCH L X .001 INCH-.002 INCH D. NOT IN CRITICAL AREA. MAINTENANCE REPAIRED RT WING PLANK ACCESS HOLE AT WS 274.319 HOLE NR 14 IAW REO. (K)

Part: SKIN — CORRODED (RT WING) · airframe 7,386 hrs · 6,515 cycles

RT WING PLANK HOLE NR 15 HAS CORRODION AT IB AFT SIDE 4 INCHES L X .002 INCH-.003 INCH D AND IB FWD SIDE 1.5 INCH L X .001 INCH - .002 INCH D AND AT OB SIDE 1 INCH L X .002 INCH-.003 INCH D. NOT IN CRITICAL AREA. MAINTENANCE REPAIRED RT WING PLANK ACCESS HOLE AT WS 294.048 HOLE NR 15 IAW REO. (K)

Part: SKIN — CORRODED (RT WING)

FOUND RIGHT WING PLANK HOLE NR 12 HAS CORROSION AT INBOARD SIDE 7 INCHES LONG BY .005 INCH - .005 INCH DEEP AND AT OUTBOARD SIDE 6 INCHES LONG BY .003 INCH - .5 INCH DEEP. NOT IN CRITICAL AREA. MAINTENANCE REPAIRED RIGHT WING PLANK ACCESS HOLE AT WS 230.415 HOLE NR 12 IAW BOMBARDIER REO 601R-57-21-030 REV D. (M)

Part: SKIN — CORRODED (RT WING) · airframe 7,386 hrs · 6,515 cycles

RT WING PLANK HOLE NR 16 HAS CORROSION AROUND ENTIRE OPENING .003 INCH-.005D IN CRITICAL AREA. MAINTENANCE REPAIRED RT WING PLANK ACCESS HOLE AT WS 303.861 HOLE NR 16 IAW REO. (K)

Part: CLIP — CRACKED (FUSELAGE) · airframe 7,386 hrs · 6,515 cycles

FS 280 FLOOR BEAM CLIP IB SIDE RBL 9 IS CRACKED NEAR RADIUS APPROX .50 INCHES. MAINTENANCE REMOVED AND REPLACED ANGLE PN 601R3111358 IAW SRM. (K)

Part: FITTING — WORN (RT WING) · airframe 7,386 hrs · 6,515 cycles

RT OB FLAP, OB ROLLER GUIDE ON FIXED VANE IS WORN TO MINIMUM LIMITS. MAINTENANCE REMOVED AND REPLACED FLAP FITTING IAW REO. (K)

Part: CLIP — CRACKED (FUSELAGE) · airframe 7,386 hrs · 6,515 cycles

FS 280 FLOORBEAM CLIP OB SIDE RBL 9 IS CRACKED REAR RADIUS APPROX .50 INCH. MAINTENANCE REMOVED AND REPLACED BRACKET PN 601R31113-58 IAW SRM. (K)

Part: CLIP — CRACKED (FUSELAGE)

FS 280 FLOORBEAM CLIP IB SIDE LBL 9 IS CRACKED NEAR RADIUS APPROX .50 INCH. MAINTENANCE INSTALLED NEW CLIP AT IB SIDE LBL9 IAW SRM. (K)

Part: CLIP — CRACKED (FUSELAGE) · airframe 7,386 hrs · 6,515 cycles

FS 280 FLOORBEAM CLIP OB SIDE LBL 9 IS CRACKED NEAR RADIUS APPROX .50 INCH. MAINTENANCE INSTALLED NEW CLIP OB SIDE LBL 9 IAW SRM. (K)

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 7,386 hrs · 6,515 cycles

RT FS 621 TO FS 625 INTERCOSTAL ANGLE (OBLIQUE) CRACKED APPROX 1 INCH LONG. MAINTENANCE REMOVED AND REPLACED RT FS 621.0 TO 625.3 INTERCOSTAL, PN 601-35012-52, IAW SRM. (K)

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 7,386 hrs · 6,515 cycles

LT FS 621 TO FS 625 INTERCOSTAL ANGLE (OBLIQUE) CRACKED APPROX 1 INCH LONG. MAITENANCE REMOVED AND REPLACED LT FS 621.0 TO 625.3 INTERCOSTAL, PN 601-35012-51, IAW SRM. (K)

Part: BUSHING — MIGRATED (MLG TRUNNION)

FOUND RIGHT MLG TRUNNION BUSHING IS MIGRATING .032 INCH. PERFORMED A MAJOR REPAIR BY REMOVING MIGRATED BUSHING AND INSTALLING 1ST OVERSIZE BUSHING P/N 601R5721003-21 IAW BOMBARDIER REO 601R-57-21-003 REV B. (M)

Part: BUSHING — MIGRATED (MLG TRUNNION)

FOUND LEFT MLG AFT TRUNNION BUSHING IS MIGRATED .003 INCH. PERFORMED A MAJOR REPAIR BY REMOVING MIGRATED BUSHING AND INSTALLING 1ST OVERSIZE BUSHING P/N 601R5721003-21 IAW BOMBARDIER REO 601R-57-21-003 REV B. (M)

Part: HANDLE — FROZEN (EMERGENCY DOOR)

SERVICE/EMERGENCY DOOR EXTERIOR HANDLE IS FROZEN IN PLACE. REQUIRES LUBRICATION. LUBRICATED SERVICE/EMERGENCY DOOR EXTERIOR HANDLE IAW CRS 200 AMM SUBTASK 12-20-52-640-023 STEPS 3 AND 10. HANDLE IS NO LONGER STICKING. (M)

Part: PUMP — FAILED (HYD SYSTEM)

GEAR UP DISAGREE MESSAGE AFTER TAKEOFF 60 SECONDS. THREE HYDRAULIC PUMP FAILED LANDING GEAR SWING TIME TEST. REMOVED AND REPLACED 3A HYDRAULIC PUMP IAW 29-12093. OPS AND LEAK CHECK GOOD. LANDING GEAR SWING TEST GOOD IAW AMM 32-20-00. (M)

Part: RELIEF VALVE — INOPERATIVE (HYD SYSTEM)

NOSE GEAR DISAGREE INFLIGHT AFTER TAKEOFF, COMPLIED WITH QRH. HYDRAULIC 3 HIGH TEMP ON GROUND. COMPLIED WITH QRH. REMOVED AND REPLACED PRESSURE MANIFOLD RELIEF VALVE PER AMM 29-12-07. LEAK CHECK GOOD. PERFORMED MULTIPLE GEAR SWINGS IAW 32-30-00. REMOVED AND REPLACED 3B PUMP IAW AMM 29-12-03. OPS CHECK GOOD. (M)