N417AW

Part: WARNING MESSAGE — FALSE INDICATION (TE FLAPS) · airframe 45,995 hrs · 44,531 cycles

6030 - FLAPS FAIL CAUTION MESSAGE SHOWING 0 DEGREES AT CRUISE. FLAP HANDLE POSTION WAS AT 0 DEGREES. PERFORMED FLAP RESET PROCEDURE IAW AWAC SUPPLEMENT 98-18IBOX 12. FLAPS RESET. PLACARDED AND PLACED ON MEL. AIRCRAFT REMOVED FROM SERVICE. PERFORMED TROUBLESHOOTING IN REF WITH FIM 27-50-00. NO FAULTS FOUND AT THIS TIME, PERFORMED OPS TEST OF FLAPS, BPSU'S AND FECU SYSTEMS, IAW FIM 27-50-00. OPS TEST GOOD. REMOVED PLACARD AND REMOVED FROM MEL.

Part: UNKNOWN — CRACKED (UNKNOWN) · airframe 44,376 hrs · 42,619 cycles

RH DETAILED INSPECTION OF LOWER WING PLANK SPLICE JOINTS AT BL45.0 WS65.75 AND WS148.0 CONFIRMED 2ND LAYER DEFECT INDICATIONS IN FWD 2 FASTENER LOCATIONS PROCEEDING TOWARD AFT ROW OF FASTENERS. APPROXIMATELY .250". *****AIRCRAFT REMOVED FROM SERVICE******** HAD MHI MOBILE REPAIR TEAM TO PERFORM REPAIR OF THE WING SPLICE JOINT IN COMPLIANCE WITH SB 601R-57-044D AND REO 601R-57-21-3790.

Part: FRAME SPLICE — CORRODED (BS 349 S22-23R) · corrosion level 2 · airframe 43,833 hrs · 42,005 cycles

FRAME SPLICE LOCATED AT FS 394 BETWEEN STRG 22R AND STRG 23R IS CORRODED. ****AIRCRAFT REMOVED FROM SERVICE******* REPAIRED FRAME SPLICE LOCATED AT FS 394 BETWEEN STRG 22R AND STRG 23R

Part: FLOOR SUPPORT — CORRODED (BS 280-409) · corrosion level 2 · airframe 43,833 hrs · 42,005 cycles

PAX DOOR AFT LOWER SILL IS CORRODE ***** AC REMOVED FROM SERVICE ***** REPAIRED PAX DOOR AFT LOWER SILL REF REO 601R-53-21-3596 REV -- DATED 2023-01-19

Part: DRAIN — CRACKED (LT WING) · airframe 43,833 hrs · 42,005 cycles

L/H AFT WING DRAIN BY BOOST PUMP ATTACHMENT HOLES ARE CRACKED INSIDE HOLES **** AC REMOVED FROM SERVICE ***** REPAIRED L/H AFT WING DRAIN BY BOOST PUMP ATTACHMENT HOLES REF REO 601R-57-21-3679 REV-- 2023-01-13

Part: FLOOR SUPPORT — CORRODED (BS 559-621) · corrosion level 2 · airframe 43,833 hrs · 42,005 cycles

L/H FLOOR SILL HAS CORROSION BETWEEN FS 559+80 TO FS621. AIRCRAFT REMOVED FROM SERVICE. REPLACED THE FLOOR SILL

Part: FLOORBEAM — CORRODED (FS589-FS605) · corrosion level 2 · airframe 43,833 hrs · 42,005 cycles

LBL 27 FLOOR BEAM HAS SPOTS OF CORROSION APPROX. LOCATION FS605-FS589 *************AIRCRAFT REMOVED FROM SERVICE********* REMOVED AND REPLACED NEW FLOOR BEAM CAP FROM SUPPORT STRUCTURE AT LBL27.00 BETWEEN FS559.00+112 - FS621.00 PER CRJ-200 SRM 51-42-21, CRJ-200 SRM 51

Part: FLOORBEAM — CORRODED (FS 559+80) · corrosion level 2 · airframe 43,833 hrs · 42,005 cycles

RBL 27 FLOOR BEAM HAS SPOTS OF CORROSION APPROX. LOCATION FS559+80 ********AIRCRAFT REMOVED FROM SERVICE********* REMOVED AND REPLACED FLOOR BEAM SECTION RBL27 FS559-FS574 REF CRJ-200-SRM 51-42-21, CRJ-200-SRM 51-42-06, DWG 601R 31026 REV F, AND COMPLIED WITH ALL STEPS OF REO 601R-53-51-641, REV --, 2023-01-10.

Part: FLOOR SKIN — CORRODED (FS 559+80 TO FS) · corrosion level 2 · airframe 43,833 hrs · 42,005 cycles

R/H SIDE FLOOR SILL HAS AREAS OF CORROSION FROM FS 559+80 TO FS 621.0 *******AIRCRAFT REMOVED FROM SERVICE******** BLEND AND RESTORE FINISH

Part: ANTI-ICE SYSTEM — FALSE INDICATION · airframe 42,657 hrs · 40,882 cycles

ON CLIMB IN CLEAR CLOUDS RECEIVED WING ANTI-ICE DUCT WARNING MESSAGE. ANTI-ICE WAS OFF WHEN OCCURRED. ANTI-ICE SYNOPTICS SHOWED RED LEADING EDGE OF LEFT WING ***AIRCRAFT REMOVED FROM SERVICE*** MX IN PROGRESS

Part: FLOOR SUPPORT — CORRODED (FS 559) · corrosion level 2 · airframe 41,283 hrs · 39,483 cycles

FS559.00 FLOOR SUPPORT CORRODED BEYOND LIMITS ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED AND REPLACED FLOOR SUPPORT AF FS559.00

Part: FLOOR SUPPORT — CORRODED (FS 559) · corrosion level 2 · airframe 41,283 hrs · 39,483 cycles

FLOOR SUPPORT L/H AT FS559.O CORRODED BEYOND LIMITS ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED AND REPLACED FLOOR SUPPORT L/H AT FS559.O

Part: SKIN — DENTED (FUSELAGE) · airframe 41,283 hrs · 39,483 cycles

DENT IN SKIN B/T FS640.0 AND FS672.20, B/T STR 26R AND STR 27R ***AIRCRAFT REMOVED FROM SERVICE*** REPAIRED DENT IN SKIN B/T 640.0 AND 672.20, B/T STR 26R AND STR 27R IAW EA#AWAC-CRJ253-01550

Part: STRUCTURE — CORRODED (FS 310) · corrosion level 2 · airframe 41,283 hrs · 39,483 cycles

CORROSION FOUND ON FS 310 B/T STR 26L AND STR 26R ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED AND REPLACED FS 310 LOWER SECTION AT FS 310.0 BETWEEN STR 26L AND 26R

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 40,939 hrs · 39,112 cycles

CAPTAIN`S WINDSHIELD CRACKED AT FL320. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED CAPTAIN`S WINDSHIELD, IN REFERENCE TO 56-11-01 & IAW AWAC SUPP 09-047A.

Part: PRESSURE SWITCH — MALFUNCTIONED (ANTI-ICE SYS) · airframe 40,186 hrs · 38,405 cycles

SUPPLIMENTAL INFORMATION, AFTER DEPARTURE RECEIVED RIGHT WING ANTI ICE CAUTION MESSAGE WITH STANDBY MODE. RESET ANTI ICE AND RECEIVED CAUTION MESSAGE AFTER 1 MIN 30 SECONDS. AIRCRAFT REMOVED FROM SERVICE. R/R RIGHT HAND ANTI ICE PRESSURE SWITCH IAW AMM 30-10 OPS CHECK GOOD.

Part: WARNING MESSAGE — ILLUMINATED (TE FLAPS) · airframe 39,499 hrs · 37,737 cycles

AFTER TAKE-OFF , THE CREW RECEIVED A FLAP FAIL AT APPROX. 8 DEGREES. FLIGHT CONTINUED AND DECLARED AN EMERGENCY. RECEIVED FLAPS FAIL CAUTION MSG AT APROX 20,000 FEET FLAPS AT ZERO. PERFORMED FLAP RESET PROCEEDURE IAW SUP 98-18G BOX 12. FLAPS RESET.

Part: HINGE — GOUGED (PAX DOOR) · airframe 38,831 hrs · 37,106 cycles

PASSENGER DOOR HINGE HALF ON FUSELAGE SIDE AFT LUG IS GOUGED. REPLACED HINGE HALF IAW CRJ200 SRM 53-21-23, REO 601R-53-21-656 REV-A.

Part: ATTACH ANGLE — CRACKED (NOT REPORTED) · airframe 38,831 hrs · 37,106 cycles

AC POWER CONTROL UNIT LOWER ATTACH ANGLE IS CRACKED. REPLACED

Part: MOUNT — CRACKED (DOOR ASIST MOTOR) · airframe 38,831 hrs · 37,106 cycles

PAX DOOR ASSIST MOTOR OUTBD MOUNT IS CRACKED AT LOWER RADIUS. REPLACED

Part: FLOORBEAM — CRACKED (BS 280) · airframe 38,831 hrs · 37,106 cycles

FS 280 BEAM AFT ANGLE IS CRACKED AT LBL 9 AND RBL 9. REPAIRED

Part: FRAME — CRACKED (BS 333) · airframe 38,831 hrs · 37,106 cycles

FS 333 FRAME STR 3L TO STR 0 IS CRACKED STARTING AT TOOLING HOLE. REPLACED

Part: BEAM — WORN (CARGO DOOR) · airframe 38,831 hrs · 37,106 cycles

CARGO DOOR LOWER O/B BEAM MEMBER 601R35050-64 HAS WEAR FROM ASSIST CABLE. REPLACED CARGO DOOR BEAM MEMBER IAW SRM51-42-06, 51-42-21.

Part: FLOORBEAM — CORRODED (BS 280) · corrosion level 2 · airframe 38,831 hrs · 37,106 cycles

FS280.00 BEAM CORRODED FROM LBL9 TO RBL9. REPAIRED BEAM IAW REO 601R-53-11-926 REV-B.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 38,831 hrs · 37,106 cycles

FS280.00 BEAM FWD ANGLE CRACKED AT LBL 9 AND RBL9.

Part: BRACKET — CRACKED (BS 621) · airframe 38,831 hrs · 37,106 cycles

CARGO DOOR AFT BALANCE SPRING ASSY MOUNT BRACKET IS CRACKED. REPLACED BRACKET IAW CRJ200 SRM 51-24-21, 51-42-06.

Part: FLOOR PANEL — CRACKED (FWD E/E BAY) · airframe 38,831 hrs · 37,106 cycles

FWD EQUIPMENT COMPARTMENT TRU DECK CRACKED AT FS193.00, LBL30. REPAIRED TRU DECK IAW REO 601R-53-11-081 REV-NC.

Part: ANGLE — CRACKED (BS 574) · airframe 38,831 hrs · 37,106 cycles

CARGO DOOR BEAM FWD ATTACH ANGLE CRACKED. REPLACED ANGLE IAW CRJ200 SRM 51-42-21, 51-40-11, TR51-42.

Part: STIFFENER — CRACKED (RT EXHAUST) · airframe 38,831 hrs · 37,106 cycles

RIGHT EXHAUST NOZZLE FAIRING HAS A CRACKED STIFFENER THIRD FROM THE FWD END. REPLACED STIFFENER IAW CMM 21-42-06.

Part: BRACKET — CRACKED (RT MLG WW) · airframe 38,831 hrs · 37,106 cycles

RIGHT MLG WHEEL WELL HYDRAULIC LINE Z BRACKET CRACKED. REPLACE BRACKET IAW SRM 51-42-06.

Part: LANDING — CRACKED (FUSELAGE) · airframe 38,831 hrs · 37,106 cycles

LT TRU PANEL LAND CRACKED AT AFT DOOR LATCH CUTOUT. REPAIRED.

Part: POST — CRACKED (BS 202.75) · airframe 38,831 hrs · 37,106 cycles

NLG WHEEL WELL FS 202.75 RBL 9 VERTICAL POST UPPER CLIP CRACKED. REPLACED

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 38,831 hrs · 37,106 cycles

PAX DOOR AFT DRAG ANGLE CRACKED. REPAIRED.

Part: FITTING — CRACKED (COCKPIT) · airframe 38,831 hrs · 37,106 cycles

WINDSHIELD PILOT SIDE POST OUTBD FITTING CRACKED. REPLACED.

Part: FITTING — CRACKED (COCKPIT) · airframe 38,831 hrs · 37,106 cycles

WINDSHIELD CO-PILOT SIDE POST OUTBD CLIP CRACKED. REPLACED.

Part: BRACKET — CRACKED (RT MLG WW) · airframe 38,831 hrs · 37,106 cycles

RT MLG WHEEL WELL TRANSDUCER HAT BRACKET CRACKED. REPLACED.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 38,831 hrs · 37,106 cycles

FS 509 LBL 47 FAIRING BRACKET CRACKED. REPLACED.

Part: BRACKET — CRACKED (PAX DOOR) · airframe 38,831 hrs · 37,106 cycles

PASSENGER DOOR LOWER BRACKET PULLEY MOUNT CRACKED. REPLACED.

Part: FITTING — CRACKED (BS 461) · airframe 38,831 hrs · 37,106 cycles

BATHTUB FITTING AT RBL 9 FS 461 IS CRACKED. REPLACED

Part: FRAME — CRACKED (FUSELAGE) · airframe 38,831 hrs · 37,106 cycles

FS 605 FRAME AT STR 9L CRACKED. REPAIRED.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 38,831 hrs · 37,106 cycles

FS 469, LBL FAIRING SUPPORT BRACKET CRACKED. REPLACED BRACKET IAW SRM 51-42-06.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 38,831 hrs · 37,106 cycles

FS 461.5 FAIRING BRACKET AT LBL 47 CRACKED. REPLACED BRACKET IAW SRM 51-42-06.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 38,831 hrs · 37,106 cycles

FS449.85, LBL FAIRING BRACKET CRACKED. REPLACED BRACKET IAW SRM 51-42-06.

Part: CHANNEL — CRACKED (CARGO BAY) · airframe 38,831 hrs · 37,106 cycles

FWD CARGO DOOR TRACK LOWER U-CHANNEL CRACKED. REPLACED.

Part: SUPPORT BRACKET — CRACKED (BS 477) · airframe 38,831 hrs · 37,106 cycles

FS477, RBL47 FAIRING SUPPORT BRACKET CRACKED. REPLACED BRACKET IAW CRJ200 SRM 51-42-06.

Part: SUPPORT BRACKET — CRACKED (BS 469) · airframe 38,831 hrs · 37,106 cycles

FS469, RBL47 FAIRING SUPPORT BRACKET CRACKED. REPLACED BRACKET IAW CRJ 200 SRM 51-42-06.

Part: SUPPORT BRACKET — CRACKED (BS 449.85) · airframe 38,831 hrs · 37,106 cycles

FS449.85, RBL 47 FAIRING SUPPORT BRACKET CRACKED. REPLACED BRACKET IAW CRJ200 SRM 51-42-06.

Part: ANGLE — CRACKED (BS 280) · airframe 38,831 hrs · 37,106 cycles

FS280, STR 3L I/B AND O/B CLIPS CRACKED. REPLACED CLIPS IAW CRJ 200 SRM 51-42-06, 51-42-21.

Part: ATTACH BRACKET — CRACKED (RT WING) · airframe 38,831 hrs · 37,106 cycles

RIGHT WING MID L/E I/B ATTACH BRACKET IS CRACKED. REPLACED BRACKET IAW CRJ 200 SRM 51-41-02.

Part: WIRE — DAMAGED (CONNECTOR) · airframe 36,890 hrs · 35,117 cycles

4199 4225 APU AUTO SHUTDOWN. IMMEDIATELY AFTER SHUTDOWN A STRONG SMELL OF FUEL IN CABIN AND COCKPIT. F/O OBS FUEL DRIPPING AND SMOKE COMING OUT APU DOOR. NO FIRE WARNING PRESENT. INTERROGATED APU ECU FOUND CODES 154,155 AND LRU FUEL SOLENOID.FLAGGED. FOUND FUEL SOLENOID AND CANNON PLUG LOOSE, TIGHTENED SOLENOID HARDWARE AND CLEANED AND TIGHTENED PLUG. R&R COALESCER SOCKS IAW SUPPLEMENT 14-192 PERFORMED CLEARING OF CONTAMINATED DUCTING IAW AMM SUPPLEMENT 09-037A NO REMAINING FUEL SMELL NOTED. APU NO FIX REF 302554 BLOCK 2 FOR MEL R&R FUEL SOLENOID IAW AMM 49-31-05. NO FIX FOUND BROKEN WIRE ON CANNON PLUG. REPAIRED WIRE IAW ESPM OPS CHECK GOOD. REMOVED PLACARD AND FROM MEL.

Part: CONNECTOR — DAMAGED (APU) · airframe 36,343 hrs · 34,621 cycles

APU AUTO SHUTDOWN AT GATE. EXHAUST ODOR IN FLIGHT DECK. SMOKE SEEN FROM APU EXHAUST. REMOVED AND REPLACED APU FUEL SOLENOID VALVE IAW AMM 49-31-05 AND SUP 10-023A. REMOVED AND REPLACED APU FUEL SOLENOID CONNECTOR PLUG IAW ESPM 20-17-35, OPS AND LEAK CHECKED GOOD.

Part: COALESCER BAG — ODOR (LT & RT) · airframe 35,571 hrs · 33,904 cycles

STRONG FUEL ODOR IN COCKPIT AND CABIN WITH PACKS ON. R & R THE LT AND RT COALESCER SOCKS IAW 14-192. NO ODOR NOTED.

Part: ACCESS PANEL — DAMAGED (RT HORIZ STAB) · airframe 35,569 hrs · 33,903 cycles

PANEL 342 AB HAS 1 BLOWN OUT FASTENER HOLE. REPAIRED PANEL 342AB IAW EA AWAC-CRJ255-00643 DATED 2-27-2017 REV-IR. PRIORITY 2 REQUIRED.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,569 hrs · 33,903 cycles

LBL27 SEAT TRACK O/B FLANGE HAS CORROSION AT FS560 AND FS565.

Part: STRUCTURE — CHAFED (FUSELAGE) · airframe 35,569 hrs · 33,903 cycles

WHILE ACCOMPLISHING AWAC JOB CARD 4EOAWA20075-E16/011/453 SECTION 1 ITEM 5, FOUND CHAFE TO EXCEED LIMITS ON LT APRON, REQUIRES REPAIR.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,569 hrs · 33,903 cycles

LBL27 FLOORBEAM ATTACHMENT TO REAR PRESSURE BULKHEAD HAS CORROSION ON UPPER SURFACE.

Part: PANEL — DAMAGED (RT WING) · airframe 35,569 hrs · 33,903 cycles

PANEL 684AB HAS 1 BLOWN OUT FASTENER HOLE.

Part: ATTACH BRACKET — CRACKED (VERTICAL STAB) · airframe 35,569 hrs · 33,903 cycles

LEFT LOWER VISOR FORWARD ATTACH BRACKET CRACKED. REMOVED AND REPLACED THE LOWER VISOR ATTACH BRACKET IAW SRM 51-42-21,.

Part: DEPRESSOR — GOUGED (BS 342) · airframe 35,569 hrs · 33,903 cycles

SERVICE DOOR SURROUND LOWER DEPRESSOR GOUGED AT AFT SPIGOT FITTING. REMOVED AND REPLACED LOWER DEPRESSOR IAW SRM 51-42-02.

Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 35,569 hrs · 33,903 cycles

LEFT INBD FLAP VANE L/E SKIN CHAFED IN THREE LOCATIONS. REPAIRED THE FLAP VANE SKIN IAW REO601R-57-52-009 AND REPLACED CENTER SKIN IAW SRM 51-42-10, 51-25-16, 51-25-06, AND 51-21-11.

Part: ATTACH BRACKET — CRACKED (LT WING) · airframe 35,569 hrs · 33,903 cycles

LH WING INBD LEADING EDGE OUTBOARD ATTACH BRACKET IS CRACKED

Part: FITTING — CRACKED (WINDSHIELD) · airframe 35,569 hrs · 33,903 cycles

FLIGHT DECK WINDSHIELD CENTER POST LOWER LEFT FITTING IS CRACKED. NDT HAS VERIFIED

Part: FLOOR SUPPORT — CORRODED (BS 574-621) · corrosion level 2 · airframe 35,569 hrs · 33,903 cycles

LBL 27 FLOOR SUPPORT CAP HAS CORROSION ON OTBD FLANGE BETWEEN BS 589 AND 621

Part: FITTING — CRACKED (WINDSHIELD) · airframe 35,569 hrs · 33,903 cycles

FLIGHT DECK WINDSHIELD CENTER POST LOWER RIGHT FITTING IS CRACKED. NDT HAS VERIFIED

Part: WEB — CRACKED (BS 588) · airframe 35,569 hrs · 33,903 cycles

INBD WEB OF LBL 27 FLOORBEAM HAS A CRACKED FASTENER HOLE AT BS 588

Part: STIFFENER — CRACKED (EXHAUST) · airframe 35,569 hrs · 33,903 cycles

RIGHT EXHAUST FAIRING SECONND STIFFENER IS CRACKED

Part: SEAT TRACK — CORRODED (BS 364-394) · corrosion level 2 · airframe 35,569 hrs · 33,903 cycles

LEFT AISLE SEAT TRACK HAS CORROSION BETWEEN BS 364 AND 394, IN CABIN.

Part: WIRE — CUT (EMERGENCY LIGHT) · airframe 34,947 hrs · 33,323 cycles

FLIGHT 3922. EMERGENCY LIGHT WIRE CUT AT ROW 13. REPAIRED THE WIRE AT ROW 13 IAW ESPM 20-16-00, OPS CHECKED GOOD.

Part: POWER UNIT — FAILED (CABIN) · airframe 34,789 hrs · 33,173 cycles

REQUEST INSPECTION FOR POSSIBLE ELECTRIC SMELL AT ROW 11 AND 12. REMOVED AND REPLACED POWER UNIT/DIMMER ABOVE ROWS 12DF. OPS CHECK GOOD IAW AMM 33-21-00.

Part: CONNECTOR — BROKEN (CABIN) · airframe 34,731 hrs · 33,123 cycles

FLIGHT 9898. EMERGENCY FLOOR TRACK LIGHTING INOP ROW 8 AND AFT REPAIRED BROKEN CONNECTOR PER ESPM 20-17-10, OPS CHECK GOOD.

Part: LIGHT — OBSTRUCTED (CABIN)

BACK 2 ROWS ON FLOOR TRACK LIGHTS STRIP OBSCURED.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 33,942 hrs · 32,391 cycles

RECEIVED PROXIMITY SYSTEM FAULT MSG INFLIGHT ON GEAR EXTENTION. RECEIVED INBD ANTI-SKID CAUTION MSG BTMS 3, 3, 3, 2.

Part: WIRE HARNESS — DAMAGED (CARGO DOOR) · airframe 33,878 hrs · 32,339 cycles

AFTER TAKEOFF RECEIVED PAX DOOR WARNING, ALSO SERVICE & CARGO DOOR CAUTION. PRESSURIZATION NORMAL, LANDED UNDERWEIGHT. R & R CARGO DOOR HARNESS IAW AMM 52-70-02 & RE-RACKED PSEU & OPS CHECK IAW AMM 32-61-01, SERVICE DOOR & CARGO DOOR CAUTION MESSAGE STILL REMAIN, IAW 2880711 FOR FURTHER MX. R & R PSEU IAW AMM 3261-01. OPS CHECKED GOOD, NO OTHER DEFECTS NOTED.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 33,878 hrs · 32,339 cycles

AFTER TAKEOFF RECEIVED PASSENGER DOOR WARNING ALSO SERVICE AND CARGO DOOR CAUTION. PRESSURIZATION NORMAL, LANDED UNDERWEIGHT.

Part: LIGHT — BROKEN (CABIN) · airframe 33,306 hrs · 31,798 cycles

FLIGHT 3852, EMERGENCY LIGHT BROKEN FROM ROW 9 BACK. END CAP BROKEN OFF & WIRING EXPOSED.

Part: GEARBOX — BINDING (THROTTLE CONTROL) · airframe 33,045 hrs · 31,558 cycles

LEFT THRUST LEVER BINDS IN FLIGHT, BOTH ADDING & REDUCING THRUST. R & R LT THROTTLE CONTROL GEARBOX IAW AMM 76-11-17. OPERATIONS CHECKED GOOD AT THIS TIME, RII COMPLIED WITH.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT)

HYD 2 LOW PRESS MSG ON CLIMB OUT. HYD SYS READS 10%. HYD PUMP 2A OPERATED FOR MORE THAN 30 MINUTES.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,134 hrs · 30,672 cycles

FLIGHT 3757, EMER ROW 2 - 5 FLOOR TRACK LIGHTS INOPERATIVE. R & R EMER ROW 2 - 5 RIBBON CONNECTION FLOOR TRACK LIGHT STRIP IAW SUP 13-022 IN ESPM.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 30,794 hrs · 29,408 cycles

PASSENGER DOOR STEP AFT SUPPORT DRAG ANGLE CRACKED.

Part: DOOR SILL — CRACKED (FUSELAGE) · airframe 30,794 hrs · 29,408 cycles

FLOOR SILL AT LBL 27 FS 605 IS CRACKED.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 30,794 hrs · 29,408 cycles

RIGHT HYD MANIFOLD ASSEMBLY SUPPORT IS CRACKED IN AFT LOWER RADIUS.

Part: RIB — CRACKED (LT WING) · airframe 30,794 hrs · 29,408 cycles

LEFT MLG WW BATTERY RIB IS CRACKED.

Part: MOUNT — CRACKED (LT MLG WW) · airframe 30,794 hrs · 29,408 cycles

LEFT WW NR 3 HYD RESERVOIR AFT MOUNT CRACKED.

Part: ANGLE — CRACKED (LT WING) · airframe 30,794 hrs · 29,408 cycles

LEFT WING CTR LE INBD MOUNT ANGLE ON WING IS CRACKED AT BOTTOM.

Part: MOUNT FITTING — CRACKED (DOOR) · airframe 30,794 hrs · 29,408 cycles

AUXILIARY DOOR HANDLE MECHANISM SUPPORT MOUNT FITTING CRACKED DURING REPLACEMENT OF OUTER HANDLE ASSEMBLY.

Part: DRAG ANGLE — CRACKED (LT WING) · airframe 30,794 hrs · 29,408 cycles

DRAG ANGLE ADJACENT TO LT BATTERY RIB IS CRACKED.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 30,794 hrs · 29,408 cycles

CARGO SEAT TRACKS ARE CORRODED AT LBL 9, FS 574 - 559+112, LBL 9, FS 559+86-559+96, LBL 27, FS 559+112 & AT RBL 9 574-559+112.

Part: MOUNT — CRACKED (RT WING) · airframe 30,794 hrs · 29,408 cycles

RIGHT WING LE MOUNT NEAR WS 149.58 IS CRACKED.

Part: DRAG ANGLE — CRACKED (RT WING) · airframe 30,794 hrs · 29,408 cycles

DRAG ANGLE ADJACENT TO RT BATTERY RIB IS CRACKED.

Part: MOUNT BRACKET — CRACKED (LT MLG WW) · airframe 30,794 hrs · 29,408 cycles

LEFT WW BRAKE PRESS TRANSDUCER MOUNT IS CRACKED.

Part: ATTACH BRACKET — CRACKED (LT WING) · airframe 30,794 hrs · 29,408 cycles

LT WING LE ATTACHMENT BRACKET NEAR WS 148 IS CRACKED.

Part: FITTING — CRACKED (FUSELAGE) · airframe 30,794 hrs · 29,408 cycles

CLIP CRACKED AT FS 484 RBL 36.

Part: FITTING — CRACKED (FUSELAGE) · airframe 30,794 hrs · 29,408 cycles

CLIPS AT FS 484, LBL 27 & LBL 36 ARE CRACKED.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,794 hrs · 29,408 cycles

SERVICE DOOR LOWER SILL HAS CORROSION.

Part: MOUNT BRACKET — CRACKED (FUSELAGE) · airframe 30,794 hrs · 29,408 cycles

ACFT GND POWER RECEPT MOUNT BRACKET CRACKED.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,794 hrs · 29,408 cycles

CORROSION ON FLOOR SUPPORT STRUCTURE, FS 349, LBL 30 - 40.

Part: TERMINAL BLOCK — FIRE (COCKPIT) · airframe 30,337 hrs · 29,001 cycles

CAPTAINS WINDSHIELD LOWER LT TERMINAL BLOCK STARTED ON FIRE. SHUT OFF WINDSHIELD HEAT, FIRE STOPPED.

Part: ADG — UNWANTED DEPLOY · airframe 29,730 hrs · 28,409 cycles

AFTER TO ADG INADVERTENTLY DEPLOYED. LDG WT 45,700. COMPLIED WITH INSPECTION OF DRY ADG IAW AWAC SUP 10-066. STOWED ADG IAW AMM 24-23-01. COMPLIED WITH M ACTION OF MEL 24-23-01. SEE 272119 1,2 FOR MELS.

Part: A/C PACK — MALFUNCTIONED (AC BAY) · airframe 29,288 hrs · 28,001 cycles

ON SHORT FINAL RECEIVED BURNING SMELL, LT PACK TEMP CLIMBED RAPIDLY. TURNED PACK OFF & SMELL WENT AWAY. PACK TEMP WAS UNCONTROLLABLE. PLACARD & PLACED ON MEL.

Part: SCREW — LOOSE (WINDSHIELD) · airframe 29,225 hrs · 27,939 cycles

PUFF OF SMOKE, 5 SECOND DURATION, FROM RT BOTTOM WINDSHIELD AREA & ACRID ELEC SMELL AT 28,000 FT. SMOKE & SMELL IMMEDIATELY DISSIPATED. RT WINDSHIELD HEAT BLOCK TOO HOT TO TOUCH UNTIL DECENT. NO OTHER INDICATIONS. FOUND TOP SCREW ON LOWER RT WINDSHIELD TERMINAL BLOCK LOOSE. SECURED SCREW AS REQUIRED & CHECKED RESISTANCE IAW SUPP 07-030A. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: FLAP — FAILED (WING) · airframe 28,149 hrs · 26,908 cycles

4097 ON APPROACH, FLAP FAILED AT ZERO, OAT 27. PERFORMED FLAP RESET PROCEDURE IAW AMM SUPP 98-18F, BOX 12. FLAPS RESET, PLACARD PLACE DON MEL.

Part: STOP FITTING — GOUGED (CARGO DOOR) · airframe 26,130 hrs · 24,945 cycles

GOUGED AREA FOUND AT AFT LOWER SIDE OF CARGO DOOR STOP FITTING. BLEND & PERFORM PASSIVITY APPLICATION IAW REO 601R-52-31-206.

Part: STOP FITTING — CRACKED (WING) · airframe 26,130 hrs · 24,945 cycles

BUTE DOOR STOP ON PANEL 694 I/B FOUND TO BE CRACKED AND MISSING. REMOVED AND REPLACED CRACKED BUTE DOOR STOP IAW CRJ 200 SRMS 51-40-11, 51-42-06, 51-42-28.

Part: SPLICE — DAMAGED (LT WING) · airframe 26,130 hrs · 24,945 cycles

LEFT OR LEADING EDGE 530 O/B SPLICE HAS OVERSIZED (ELONGATED) SCREW HOLES. REMOVED AND REPLACED CH O/B LEADING O/B SPLICE.

Part: SEAT TRACK — CHAFED (FUSELAGE) · airframe 26,130 hrs · 24,945 cycles

CHAFE FOUND ON RT SIDE SEAT TRACK NEAR FS 522. BLEND & RESTORE FINISH IAW REO 601R-53-41-1663.

Part: MOUNT BRACKET — CRACKED (BRAKE ACCUM) · airframe 26,130 hrs · 24,945 cycles

FORWARD MOUNTING BRACKET FOR UPPER BRAKE ACCUMULATOR IS CRACKED. REMOVED AND REPLACED CRACKED BRACKET WITH NEW AND SERVICEABLE BRACKET (/N 601R75250-25) IAW CRJ 200 SRMS 51-40-11 & 51-42-21.

Part: VANE — CHAFED (TE FLAP) · airframe 26,130 hrs · 24,945 cycles

LEFT I/B FLAP VANE IS CHAFED FROM ALL 3 STOPS. REMOVED AND REPLACED I/B LEADING EDGE FLAP VANE & REPAIRED CTR & O/B VANES IAW REO 601R-57-52-004.

Part: STRIKER — GROOVED (FUSELAGE) · airframe 26,130 hrs · 24,945 cycles

PAX DOOR UPPER CENTER DOOR STRIKER ON FUSELAGE IS GROOVED. REMOVED AND REPLACED ARRESTER WITH NEW AND SERVICEABLE ARRESTER (P/N 601R31222-1) IAW CRJ 200 SRM 51-41-02.

Part: SHROUD — CHAFED (RT WING) · airframe 26,130 hrs · 24,945 cycles

RIGHT WING INBOARD L/E INNER SPAR INNER SHROUD IS CHAFED 2 LOCATIONS. REMOVED CHAFED SHROUD. LOCATED DRILLED AND INSTALLED NEW SERVICEABLE SHROUD P/N 600-12030-40) IAW CRJ 200 SMS 51-40-11, 51-41-02.

Part: PLATE — CORRODED (FUSELAGE) · airframe 26,130 hrs · 24,945 cycles

CORROSION FOUND ON GALLEY MOUNTING PLATE AT FS 318.00. REMOVE & REPLACE GALLEY MOUNTING PLATE IAW CRJ 200 SRM.

Part: FITTING — CORRODED (LT MLG) · corrosion level 2 · airframe 26,130 hrs · 24,945 cycles

UPON REMOVAL OF LEFT MLG SIDE STAY PIN FROM THE SIDE STAY FITTING FOUND CORROSION IN THE BORE OF THE FITTING. SENT TO BOMBARDIER FOR EVAL AND REPAIR PROCESSES.

Part: TRANSCOWL — GOUGED (THRUST REVERSER) · airframe 26,130 hrs · 24,945 cycles

TRANS COWL 444AT IS GOUGED ON OUTER SIDE. REPAIRED TRANS COWL IAW REO 601R-78-33-4010.

Part: BRACKET — TORN (MCU) · airframe 26,130 hrs · 24,945 cycles

BRACKET FOR MCU SAFETY CABLE IS TORN WHERE CABLE GOES THRU HOLE. REMOVED UNSERVICEABLE MCU BRACKET, FABRICATED, AND INSTALLED SERVICEABLE MCU BRACKET IAW CRJ 200 SRM 51-24-16/51-40-11/51-42-06.

Part: BRACKET — CORRODED (LAV SERVICE) · airframe 26,130 hrs · 24,945 cycles

LAV SERVICE DOOR, LED LIGHT BRACKET IS CORRODED. REMOVED UNSERVICEABLE BRACKET AND INSTALLED SERVICEABLE BRACKET IAW CRJ 200 SRM 51-42-06.

Part: FITTING — CHAFED (TE FLAP) · airframe 26,130 hrs · 24,945 cycles

CHAFE FOUND ON ALIGNMENT FITTING OF RIGHT O/B FLAP. BLEND, MEASURE & RESTORE FINISH IAW REO 601R-57-51-143.

Part: INTERCOSTAL — CRACKED (PAX DOOR) · airframe 26,130 hrs · 24,945 cycles

PAX DOOR INTERCOSTAL ON PANEL 832BR IS CRACKED. REMOVED & REPLACED INTERCOSTAL.

Part: STEP — CORRODED (PAX DOOR) · corrosion level 2 · airframe 26,130 hrs · 24,945 cycles

UPPER PAX DOOR STEP 832 ET HAS CORROSION ON UPPER AND CENTER HINGES. REMOVE AND REPLACE HINGES.

Part: LUG — GOUGED (PAX DOOR) · airframe 26,130 hrs · 24,945 cycles

PAX DOOR AFT HINGE LUG IS GOUGED. REPAIRED PAX DOOR AFT HINGE LUG IAW BOMBARDIER REO 601R-52-11-1347.

Part: SHROUD — CHAFED (RT AILERON) · airframe 26,130 hrs · 24,945 cycles

RIGHT AILERON UPPER FWD SHROUDS ARE CHAFED. BLENDED CHAFE IAW REO 601R-57-60-013.

Part: SILL — CORRODED (FUSELAGE) · airframe 26,130 hrs · 24,945 cycles

UNDER LEFT CARGO BAY FLOOR PANELS 271FLF & 281KLF HAVE CORROSION AROUND O/B NUT PLATES (FLOOR SILL). REMOVED CORROSION ON LEFT CARGO FLOOR SILL 559+48 -559+112 IAW REO 601R-53-51-221 REV.

Part: FLAP — CHAFED (LT WING) · airframe 26,130 hrs · 24,945 cycles

CHAFED AREA FOUND ON LEFT O/B FLAP NEAR I/B ROLLER BEARING. BLEND, MEASURE, RESTORE FINISH IAW REO 601R-57-53-968.

Part: FITTING — CHAFED (TE FLAP) · airframe 26,130 hrs · 24,945 cycles

RIGHT O/B FLAP ROLLER GUIDE FITTING CHAFED. BLEND, MEASURE & RESTORE TO ORIG FINISH IAW REO 601R-57-53-969.

Part: FITTING — CRACKED (FUSELAGE) · airframe 26,130 hrs · 24,945 cycles

RBL 9 O/B CLIP AT FS 280 IS CRACKED. REMOVED UNSERVICEABLE RBL 9 O/B 280 CLIP, FABRICATED AND INSTALLED SERVICEABLE RBL 9 O/B FS 280 CLIP AND RESTORED FINISH IAW CRJ 200 SRM 51-42-06/51-42-21/51-40-11.

Part: TRUNNION — DAMAGED (MLG) · airframe 26,130 hrs · 24,945 cycles

DURING COLDWORKING PROCESS FOUND 1 OVERSIZED HOLE ON LEFT & 1 EACH OVERSIZED HOLE ON RIGHT MLG LOWER TRUNNION FLANGES. REPAIRED OVERSIZED HOLES ON LEFT & RIGHT LOWER MLG TRUNNION FLANGES IAW BOMBARDIER REO 601R-57-21-1866 REV A.

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 26,130 hrs · 24,945 cycles

RIGHT BULKHEAD AT FS 280 CHAFED AND DENTED AT FLIGHT DECK ENTRANCE. REPAIRED IAW CRJ REO 601R-53-11-1727.

Part: SKIN — CHAFED (TE FLAP) · airframe 26,130 hrs · 24,945 cycles

L/E SKIN ON RIGHT I/B FLAP VANE CHAFED & FOUND TO BE OUT OF ALLOWABLE LIMITS AT FLA STA 60.005. REMOVE & REPLACE L/E SKIN ON RIGHT I/B FLAP VANE IAW SRM 51-40-11 & SRM 51-42-13.

Part: SILL — CORRODED (FUSELAGE) · airframe 26,130 hrs · 24,945 cycles

PAX DOOR LOWER SILL HAS CORROSION. REMOVED CORRODED SILL, FABRICATED, AND INSTALLED NEW SERVICEABLE SILL IAW CRJ 200 SRM 51-24-21, 51-40-11, 51-42-06.

Part: SKIN — CRACKED (TAILPIPE) · airframe 26,130 hrs · 24,945 cycles

RIGHT ENGINE TAILPIPE INNER SKIN IS CRACKED NEAR THE 8 O`CLOCK POSITION. INSTALLED REPAIR DOUBLE IAW CRJ 200 SMM 78-11-00-300-801.

Part: PLATE — CRACKED (FUSELAGE) · airframe 26,130 hrs · 24,945 cycles

STIFFENER PLATE FWD SIDE CARGO DOOR CUTOUT JUST BELOW BOTTOM STOP FITTING IS CRACKED. REMOVED & REPLACED WITH NEW STIFFENER PLATE.

Part: FITTING — CRACKED (FUSELAGE) · airframe 26,130 hrs · 24,945 cycles

LBL 9 I/B AND O/B CLIPS AT FS 280 ARE CRACKED. REMOVED UNSERVICEABLE I/B O/B CLIPS AND INSTALLED SERVICEABLE I/B AND O/B CLIPS IAW REO 601R-53-11-136 REV A CRJ 200 SRM 51-40-11/51-21-11/51-402-21.

Part: SKIN — CRACKED (TAILPIPE) · airframe 26,130 hrs · 24,945 cycles

RIGHT ENGINE TAIL PIPE INNER SKIN IS CRACKED NEAR THE 11 O`CLOCK ACCESS PANEL. INSTALLED REPAIR DOUBLER IAW CRJ 200 CMM 78-11.

Part: SEAT TRACK — DAMAGED (BS 409) · airframe 26,130 hrs · 24,945 cycles

LEFT SEAT TRACK HAS DAMAGE NEAR FS 409 + 128. BLENDED DAMAGED AREA FOUND TO BE WITHIN LIMITS.

Part: HINGE — SCRATCHED (PAX DOOR) · airframe 26,130 hrs · 24,945 cycles

SCRATCH ON PAX DOOR HINGE AFT LUG LAND. BLEND SCRATCH IAW CRJ REO 601R-53-21-814.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 26,130 hrs · 24,945 cycles

AFT EQUIPMENT BAY DOOR CUTOUT, RIGHT SIDE AT FS 700 SUPPORT ANGLE CRACKED. REMOVED AND FAB SERVICEABLE ANGLE PER SRM.

Part: BPSU — FAILED (TE FLAP) · airframe 26,003 hrs · 24,821 cycles

FLAP FAIL ZERO DEG ON VECTORS TO APPROACH, PERFORMED FLAP RESET PROCEDURE IAW AWAC SUP 98-18E BOX 12 FLAPS RESET PLACARD AND PLACED ON MEL. REMOVED AND REPLACED RIGHT BPSU. OPS AND LEAK CHECK GOOD IAW AMM 27-51-10. REMOVED PLACARD REMOVED FROM MEL.

Part: SENSOR — CONTAMINATED (TE FLAP) · airframe 25,870 hrs · 24,693 cycles

DESCENDING INTO BTV, FLAPS FAIL ZERO, PERFORMED FLAP RESET PROCEDURE IAW AWAC SUPP 98-18E BOX 12. FLAPS RESET. CHECK FECU CODES, POSSIBLE CKP TECHNIQUE PROBLEM. FOUND EXCESSIVE GREASE BUILD UP ON RIGHT DPSU'S CLEANED DPSU AND LUBED IAW AMM 27 51 10. PERFORMED OP CHECK OF FLAP IAW AMM 27 54 00 OP CHECK GOOD. REMOVE PLACARD/MEL.

Part: CONTROL UNIT — FAILED (TE FLAPS) · airframe 24,991 hrs · 23,818 cycles

FLAPS FAIL MESSAGE AT 8 DEGREES ON TAKEOFF. PERFORMED FLAP RESET PROCEDURE IAW AWAC SUP 98-18E BOX 12. FLAPS RESET. INSPECTED WIRING FROM FECU TO R BPSU, COMPLIED WITH TORQUE CHECK OF ALL FLAP ACTUATORS, R & R FECU IAW AMM 27-51-05. OPS CHECK GOOD AT THIS TIME. REMOVED PLACARD AND MEL.

Part: FLAP SYSTEM — FAILED (TE FLAPS) · airframe 24,895 hrs · 23,724 cycles

FLAP FAIL AT 15 DEGREES AFTER TAKEOFF. RETURNED TO LAND AT 46600 LBS. FPM DESCENT RATE AT TOUCHDOWN APPROX 400 FPM. PERFORMED FLAP RESET PROCEDURE IAW SUP 98-18E, BOX 12. FLAPS RESET. REF TO MX WO 189963 FOR ACCOMPLISHED JOB. R & R RT BPSU. OPS CHECK GOOD AT THIS TIME IAW AMM 27-54-00.

Part: FLAP SYSTEM — FAILED · airframe 24,549 hrs · 23,380 cycles

FLAP FAIL AT 12 DEGREES, COMPLIED WITH QRH, PERFORMED RESET IAW SUPPLEMENT 98-18E BOX 12, FLAPS RESET.

Part: BPSU — FAILED (TE FLAPS) · airframe 24,437 hrs · 23,266 cycles

FLAPS FAILED AFTER TAKE OFF AT 15 DEG ON ED1 AND FLT CONTROL SYNOPTIC PAFE READS 14 DEG-RAN QRH. RETURNED TO DEPARTURE FOR LANDING, PERFORMED FLAP RESET PROCEDURES IAW AWAC SUPP 98-18E, BOX 12, R & R BPSU REF AMM 27-51-10. OPS CHECKED AND RIG CHECKED GOOD.

Part: SELECTOR VALVE — FAILED (NLG) · airframe 23,126 hrs · 21,906 cycles

DURING GEAR RETRACTION, LOUD CLUNKING NOISE FROM NLG AREA, NOISE WENT AWAY AFTER GEAR AND FLAPS RETRACTED. NOISE RETURNED AGAIN WHEN FLAPS SELECTED TO 8 DEGREES. R & R NLG DOOR SELECTOR VALVE REF AMM 32-22-20. OPS AND LEAK CK GOOD. SN OFF 1794, SN ON 1178, PC 32-20-152 CLM.

Part: SHUTOFF VALVE — INOPERATIVE (BLEED SYS) · airframe 22,404 hrs · 21,123 cycles

DURING SINGLE PACK OPS, WHEN SELECTING BLEED TRANSFER TO ENGINE AIR, LT PACK SHUTS OFF. PERFORMED AIR RETURN, BTMS READS 3-3-3-3. R & R LT PACK VALVE IAW AMM 21-51-43. OPS CK GOOD AT THIS TIME.

Part: PLATE — CORRODED (BS 319.7-349) · corrosion level 2 · airframe 21,606 hrs · 20,234 cycles

SERVICE DOOR THRESHOLD PLATE CORRODED. REPLACED UNSERVICEABLE SERVICE DOOR THRESHOLD PLATE WITH SERVICEABLE PLATE PN 601R38957-19S IAW AMM 20-21-00-944-001 ON NON ROUTINE 0024, ZONE 1000.

Part: POST — CRACKED (BS 409) · airframe 21,606 hrs · 20,234 cycles

RBL 27.00 POST CRACKED INBD BOTTOM AT 409.00+123. REPAIRED RBL 27 INBD POS AND LWR CAP ANGLE IAW REO 601R-53-41-056, REV E AND 601R-53-41-1392.

Part: BRACKET — GOUGED (PAX DOOR) · airframe 21,606 hrs · 20,234 cycles

FUSELAGE PAX DOOR CUT OUT AFT PULL IN LEVER GUIDE BRACKET GOUGED. R & R PULL IN LEVER GUIDE BRACKET IAW SRM 51-42-21 AND 51-40-11.

Part: SKIN — CHAFED (RT WING) · airframe 21,606 hrs · 20,234 cycles

BUTTE DOOR 694PB INNER SKIN CHAFED. R & R BUTTE DOOR 694PB SKIN IAW SRM 51-42-06.

Part: HEAT SHIELD — DETACHED (APU) · airframe 21,606 hrs · 20,234 cycles

APU AFT HEATSHIELD HAS FASTENERS PULLED THRU REPAIRED IAW REO 601R-49-81-147, 601R-49-81-051.

Part: SKIN — CHAFED (RUDDER) · airframe 21,606 hrs · 20,234 cycles

RUDDER L/E CHAFED RT SIDE BLENDED CHAFING OUT IAW SRM 51-12-00.

Part: SKIN — CHAFED (LT MLG DOOR) · airframe 21,606 hrs · 20,234 cycles

LT MLG DOOR FWD EDGE CHAFED 2 EA PLACES. FABRICATED FILLER AND DOUBLER INSTALLED IAW REO 601R-52-82-034 AND REO 601R-52-82-102.

Part: DOOR — CRACKED (APU BAY) · airframe 21,606 hrs · 20,234 cycles

APU ENCLOSURE DOOR 311B2 CRACK AT WELD TOP OF STIFFENER. REPAIRED APU ENCLOSURE DOOR 311B2 AND IAW REO 601R-49-11-070.

Part: STRUCTURE — CRACKED (THRUST REVERSER) · airframe 21,606 hrs · 20,234 cycles

LT T/R UPPER INBD CASCADE CRACKED. REPAIRED LT T/R UPPER INBD CASCADE IAW PROCESS SPECIFICATION 1, DWG AW78-30-0711-04.

Part: HEAT SHIELD — CRACKED (APU) · airframe 21,606 hrs · 20,234 cycles

APU EXHAUST HEATSHIELD CRACKED AT 6 O`CLOCK POSITION. REPAIRED APU EXHAUST HEATSHIELD IAW REO 601R-49-81-003, REV B.

Part: SKIN — CHAFED (RT MLG DOOR) · airframe 21,606 hrs · 20,234 cycles

RT MLG DOOR FWD EDGE CHAFED IN 2 EA PLACES PREVIOUS REPAIRS. R & R LOWER FILLER IAW REO 601R-52-82-034.

Part: INTERCOSTAL — CRACKED (PAX DOOR) · airframe 21,606 hrs · 20,234 cycles

PAX DOOR INTERCOSTAL UNDER PANEL 832BR IS CRACKED. REMOVED CRACKED INTERCOSTAL THEN INSTALLED NEW SERVICEABLE INTERCOSTAL PN 601R-31902-318 AND IAW SRM 51-41-06.

Part: FRAME — CRACKED (BS 409) · airframe 21,606 hrs · 20,234 cycles

LBL 18.00 POST CRACKED OTBD BOTTOM AT FS 409+128. REPAIRED IAW REO 601R-53-41-056, REV E.

Part: FRAME — CRACKED (BS 409) · airframe 21,606 hrs · 20,234 cycles

RBL 18.00 POST CRACKED OTBD BOTTOM AT FS 409.00+128. REPAIRED IAW REO 601R-53-41-056, REV E.

Part: RIB — CRACKED (RT WING) · airframe 21,606 hrs · 20,234 cycles

RT BATT RIB IS CRACKED. REPAIRED RT BATT RIB IAW REO 601R-57-51-046, REV B.

Part: SEAT TRACK — CORRODED (BS 559) · corrosion level 2 · airframe 21,606 hrs · 20,234 cycles

SEAT TRACK TIE DOWN CORRODED RBL 9.00, FS 669+112 CARGO BAY PARTS. REMOVED UNSERVICEABLE SEAT TRACK FROM RBL 9.00, FS 559+112 AND INSTALLED SERVICEABLE SEAT TRACK IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 21,606 hrs · 20,234 cycles

SEAT TIE DOWN TRACK CORRODED LBL 9.00, FS 559+112 CARGO BAY AREA. REMOVED UNSERVICEABLE SEAT TRACK FROM LBL 9.00, FS 559+112 AND INSTALLED SERVICEABLE SEAT TRACK IAW AMM 53-01-11.

Part: ANGLE — CORRODED (PAX DOOR) · corrosion level 2 · airframe 21,606 hrs · 20,234 cycles

CORROSION ON ANGLE CLIPS AT FS 320.10 AND FS 338.00. REMOVED CORRODED CLIPS AT FS 320.10 AND FS 338.00 AND INSTALLED NEW SERVICEABLE CLIPS IAW SRM 51-42-06.

Part: SILL — CORRODED (BS 574) · corrosion level 1 · airframe 21,606 hrs · 20,234 cycles

LT CARGO BAY FLOOR SILL CORRODED AND CRACKED. REMOVED CORROSION AT LT CARGO BAY FLOOR SILL AND CUT OUT CRACK IAW SRM 51-21-06 AND REO 601R-53-61-433, REV B.

Part: PRESSURE BLKHD — CRACKED (BS 202.75) · airframe 21,606 hrs · 20,234 cycles

FWD PRESSURE BULKHEAD IS CRACKED AROUND THE PARKING BRAKE CABLE. REPAIRED FS 202.75 BULKHEAD AT LBL 23.71, LW 69.684 IAW REO 601R-53-11-563.

Part: SEAT TRACK — CORRODED (BS 621) · airframe 21,606 hrs · 20,234 cycles

SEAT TRACK TIE DOWN CORRODED LBL 9.00, FS 621. REMOVED SERVICEABLE SEAT TRACK FROM LBL 9.00, FS 621 AND INSTALLED SERVICEABLE SEAT TRACK IAW AMM 53-01-11.

Part: PANEL — GOUGED (LT WING AILERON) · airframe 21,606 hrs · 20,234 cycles

LOWER LT AILERON SHROUD PANELS 599AB AND 599CB CHAFED. REPAIRED LOWER LT AILERON SHROUD PANELS 599AB AND 599CB IAW REO 601R-57-60-020.

Part: PANEL — GOUGED (LT WING AILERON) · airframe 21,606 hrs · 20,234 cycles

LOWER LT AILERON SHROUD PANEL 599BB GOUGED. REPAIRED LOWER LT SHROUD PANEL 599BB IAW REO 601R-57-60-020.

Part: SEAT TRACK — CORRODED (BS 574) · corrosion level 2 · airframe 21,606 hrs · 20,234 cycles

SEAT TRACK TIE DOWN CORRODED RBL 9.00, FS 574 CARGO BAY AREA. REMOVED UNSERVICEABLE SEAT TRACK FROM RBL 9, FS 574 AND INSTALLED SERVICEABLE SEAT TRACK IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (BS 574) · corrosion level 2 · airframe 21,606 hrs · 20,234 cycles

SEAT TRACK CORRODED LBL 9.00, FS 574 CARGO BAY AREA. REMOVED UNSERVICEABLE SEAT TRACK FROM LBL 9, FS 574 INSTALLED SERVICEABLE SEAT TRACK IAW AMM 53-01-11.

Part: TRIM PANEL — MALFUNCTIONED (COCKPIT) · airframe 21,554 hrs · 20,183 cycles

FLT 3755, LOG 212249/1, DLY 3594, RUDDER TRIM KNOB STUCK IN FLIGHT MOMENTARILY WITH LT RUDDER TRIM INPUT. TRIM TENDS TO RUN-AWAY WITHOUT CORRECTION. R & R RUDDER/ AILERON TRIM PANEL REF AMM 27-22-00. OPS CKS GOOD.

Part: PRESSURE BLKHD — CRACKED (BS 559) · airframe 20,156 hrs · 18,709 cycles

FS 559, RBL 9.0 INBD SIDE CRACKED AT BOTTOM EDGE FROM LOWEST FASTENER INCORPORATED REO 601R-53-41-260 REV D DATED 09/17/09 ALONG WITH REO 601R-53-41-609 REV B DEVIATION E DATED 12/18/09.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 17,135 hrs · 15,674 cycles

MWC 135144-2 - AFT PRESSURE BULKHEAD CRACKED AT FS 621.00 LT, LINTEL ASSY AREA. AFT PRESSURE BULKHEAD CRACK AT FS 621.00 LT AT LINTEL ASSY REPAIRED IAW REO 601R-53-61-1230, REV D. (K)

Part: INLET — CRACKED (APU) · airframe 17,135 hrs · 15,674 cycles

(AT GATE) 199793/1 - EXCESSIVE SMOKE FROM APU INLET AFTER APU SHUTDOWN FOR 3(?) MINUTES FIRE WARNING FOR SPLIT SEC AND THEN SILENCED ITSELF. INSPECTED APU INLET AND EXHAUST, PULLED APU COVER AND INSPECTED AREA NO DEFECTS NOTED. INSPECTED FIRE LOOPS, NO DEFECTS NOTED. (REMOVED AND REPLACED APU ASSY). (K)

Part: INTERCOSTAL — CRACKED (BS 484) · airframe 16,960 hrs · 15,516 cycles

MWC 134852-187 - FS 484, RBL 27.00 AND RBL 36 CLIP AND INTERCOSTAL FOUND CRACKED. FS 484, RBL 27.00 AND RBL 36 CLIP AND INTERCOSTAL REPAIRED IAW REO 601R-53-41-059, REV "A". (K)

Part: ATTACH FITTING — CRACKED (BS 280)

MWC 134852-144 - FS 280.00, RBL 9.0, INBD CLIP OF PILOT BULKHEAD FOUND CRACKED. CLIP AT FS 280.00, RBL 9.0 INBD. REMOVED AND REPLACED IAW SRM 51-42-21 AND 51-42-06. (K)

Part: RETAINER — CORRODED (E/E BAY DOOR) · corrosion level 2 · airframe 16,960 hrs · 15,516 cycles

MWC 134852-112 - AVIONIC DOOR SEAL RETAINERS FOUND CORRODED. SEAL RETAINER REMOVED AND REPLACED IAW SRM 51-42-06. (K)

Part: RETAINER — CORRODED (E/E BAY DOOR) · corrosion level 2 · airframe 16,960 hrs · 15,516 cycles

AVIONIC DOOR SEAL RETAINERS FOUND CORRODED. SEAL RETAINER REMOVED AND REPLACED IAW SRM 51-42-06. (K)

Part: PROXIMITY SENSOR — OUT OF ADJUST (MLG) · airframe 14,630 hrs · 13,268 cycles

GEAR DISAGREE WARNING MESSAGE ILLUMINATED AFTER RETRACTION. REF WO 122814 ADJUSTED NLG OLEO CENTERED/EXTENDED PROX SENSOR IAW AMM 32-61-05. OPS CHECK GOOD. (K)

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 14,465 hrs · 13,107 cycles

FLAP FAILED MESSAGE, FLAP FAILED AT ZERO. COMPLIED WITH RESET PROCEDURE IAW AWAC SUPP 98-018B STEPS 1.3 AND 1.4, FLAP SYSTEM RESET. OK. (M)

Part: WARNING LIGHT — FALSE ACTIVATION · airframe 14,417 hrs · 13,056 cycles

STAB AND MACH TRIM CAUTION IN FLIGHT. AUTOPILOT PITCH TRIM MESSAGE IN FLIGHT. PERFORMED OPS CHECK OF STAB SYSTEM, NO FAULTS NOTED. INTERROGATED HSTCU REF 27-41-00, NO FAULTS NOTED. (M)

Part: RUDDER — MALFUNCTIONED · airframe 14,242 hrs · 12,889 cycles

UNCOMMANDED FULL RT RUDDER AT HIGH ALTITUDE CLIMB 280 KNOTS WITH YAW DAMPER ENGAGED, STEPPED ON RUDDER TO CORRECT AND TRIMMED BACK IN POSITION, PROCEEDED NORMALLY. (K)

Part: COMPUTER — MALFUNCTIONED (AHRS)

AFTER TAKEOFF, ROLL AND PITCH INDICATION ON CAPTAINS F/O ATTITUDE INDICATOR CAME ON, FOLLOWED QRH AND RETURNED TO MKE CAPTS PITCH PLUS 7 DEGREES OVER FIRST OFFICER BANK 5-10 DEGREE. REPLACED CAPTAINS AHRS COMPUTER IAW CRJ AM 34-21-01. OPS TEST FOUND SATISFACTORY, FOUND SERVICEABLE. (M)

Part: BRACKET — CRACKED (BS 349) · airframe 12,260 hrs · 10,956 cycles

PAX DOOR ASSIST MOTOR BRACKET (PN 601R317743-7) CRACKED AT BOTTOM END APPROX. 12 INCHES LONG. (K)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 1 · airframe 12,660 hrs · 10,956 cycles

RT FWD FLOOR SUPPORT ANGLE (PN 601R31148-79) BETWEEN FS 310.00 AND FS319.70 CORRODED ON AFT END. REMOVED AND REPLACED SUPPORT (PN 601R31148-79) IAW SRM 51-23-00, SRM 51-42-06 AND DRWG 601R31148. (K)

Part: SKIN — CORRODED (RWS 95) · airframe 12,260 hrs · 10,956 cycles

RT WING PLANK AT ACCESS HOLE 640DB HAS CORROSION ON LOWER IB SIDE MEASURES APPROX .5 X .25 X .002 IN NON-CRITICAL AREA. REPAIRS ACCOMPLISHED IAW EO E06/021/457. (K)

Part: BRACKET — CORRODED (FUSELAGE) · corrosion level 2

FOUND SERVICE DOOR SURROUND STRUCTURE LOWER SILL JOINT BRACKET (P/N 601R38335-1, CORRODED AT FS 318.70 WL 73 STRINGER 18. (M) REMOVED AND REPLACED BRACKET (PN 601R383355-1) IAW SRM 51-40-11 AND BSC EO 601R53-11628. (K)

Part: BRACKET — CRACKED (FUSELAGE) · airframe 12,260 hrs · 10,956 cycles

RT HYDRAULIC TRANSDUCER BRACKET (PN 601R75262-157) CRACKED APPROX .2 INCH LONG IN RT MLG WHEEL WELL CEILING. INSTALLED NEW BRACKET IAW SRM 51-42-06. (K)

Part: SUPPORT BRACKET — CRACKED (RT MLG WW)

RT HYDRAULIC TRANSDUCER LINE SUPPORT BRACKET, P/N 601R75262-153, CRACKED APPROX .1 INCH LONG IN RT MLG WHEEL WELL CEILING. (M) INSTALLED NEW BRACKET IAW SRM 51-42-06. (K)

Part: FITTING — CRACKED (FUSELAGE)

OUTBOARD FLOOR SUPPORT BEAM CLIP AT FS 280, RBL 9.0 IS CRACKED IN RADIUS APPROX .1 INCH LONG. (M) REPAIRED FS280 CLIP IAW BSC SR 601R530557A.

Part: BRACKET — CRACKED (LT MLG BAY)

LT HYDRAULIC TRANSDUCER BRACKET, P/N 601R75262-159) CRACKED APPROX .1 INCH LONG IN LT MLG WHEEL WELL CEILING. (M) MAINTENANCE INSTALLED NEW BRACKET IAW SRM 51-42-06. (K)

Part: FITTING — CRACKED (FUSELAGE)

INBOARD FLOOR SUPPORT BEAM CLIP AT FS 280, LBL 9.0 IS CRACKED IN RADIUS APPROX .2 INCH LONG. (M) REPAIRED FS280 CLIP IAW BSC SR 601R530057A. (K)

Part: FITTING — CRACKED (FUSELAGE)

OUTBOARD FLOOR SUPPORT BEAM CLIP AT FS 280, LBL 9.0 IS CRACKED IN RADIUS APPROX .4 INCH LONG. (M) REPAIRED FS 280 CLIP IAW BSC SR 601R530057A. (K)

Part: PCU — MALFUNCTIONED (RT SPOILER) · airframe 12,169 hrs · 10,873 cycles

VIBRATION NOTED AT 10,000 FT AIRSPEED 310 KNOTS, SLOWED TO 260 KNOTS, VIBRATION STOPPED. GEAR WAS UP. REMOVED AND REPLACED RT SPOILER PCU REF AMM 27-62-01, OPS CHECK GOOD AT THIS TIME. REMOVED SPOILER PCU SER NO MAL 5041, PN 270007, TSN: 11492 CSN: 10286. SPOILER PCU SER NO MAL 5155, PN 270007, TSN: 12169, CSN: 10873. (K)

Part: SILL — CORRODED (FUSELAGE) · corrosion level 1

CARGO DOOR SILL PLATE HAS MINOR SURFACE CORROSION IN AREA OF NUTPLATES FROM FS 574 TO 621. (M) REPAIRED CARGO DOOR SILL PLATE IAW SRM 51-21-01 AND 51-25-01. (K)

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 12,040 hrs · 10,740 cycles

WHEN SELECTING FLAPS FROM 8 DEGREES TO 20 DEGREES, A FLAP CAUTION MESSAGE OCCURRED IN FLIGHT. (K)

Part: MICROPHONE — INTERMITTENT (OXYGEN MASK)

CAPTAINS OXYGEN MASK MIC INTERMITTENT. REMOVED AND REPLACED CAPTAINS OXYGEN MASK IAW 35-10-00, OPS CHECK GOOD. (M)

Part: IDG — FAULTY (NR 1 ENGINE) · airframe 8,737 hrs · 7,541 cycles

ON TAKEOFF ROLL IDG NR 1 FAULT FOLLOWED GEN NR 1 FAULT ABORTED 40 KNOTS BTMS INDICATION 2,2,22 LIGHT BREAKING. SERVICED IDG NR 1 IAW AMM. COMPLIED WITH ENGINE RUN. OPS CHECK GOOD. NOT LEAKS NOTED IAW AMM. NO HIGH ENERGY STOP INSPECTION REQUIRED. (K)

Part: FLOOR SUPPORT — CRACKED (FUSELAGE)

RIGHT FS 621 FLOOR SUPPORT ANGLE IS CRACKED. PERFORMED A MAJOR REPAIR BY REMOVING DAMAGED ANGLE AND INSTALLING A REPAIR ANGLE IAE BOMBARDIER, INC REO 601R-53-61-117 REV C. (M)

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 7,530 hrs · 6,410 cycles

MWC 135 RT FS621 FLOOR SUPPORT ANGLE IS CRACKED. REPAIRED BY REMOVING SECTION OF DAMAGED ANGLE, FABRICATING AND INSTALLING REPAIR ANGES IAW MFG REO. (K)

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 7,530 hrs · 6,410 cycles

MWC 134 LT FS 621 FLOOR SUPPORT ANGLE IS CRACKED. REPAIRED BY REMOVING DAMAGED SECTION OF ANGLE, FABRICATING AND INSTALLING REPAIR ANGLES IAW MFG REO. (K)

Part: SKIN — CHAFED (RT WING)

RIGHT LOWER WING PLANK UNDER PANEL 650HB IS CHAFED IN TWO AREAS. INBOARD AREA CHAFED .050 INCH WIDE 6 INCHES LONG APPROX .002 INCH DEEP. OUTBOARD AREA CHAFED .050 INCH WIDE 4 INCHES LONG APPROX .001 INCH DEEP. FORWARD CENTER IS AT STARTING STAGES OF CORROSION .5 INCH LONG .1 INCH WIDE. REPAIRED BY BLENDING OUT DAMAGE, PERFORMING NDT, ROTO-PEENED RE-WORKED AREA IAW BOMBARDIER INC REO 601R-57-21-030 REVD. (M)

Part: BUSHING — MIGRATED (RT MLG TRUNION)

RIGHT MAIN LANDING GEAR AFT TRUNNION BUSHING MIGRATED .012 INCH. REMOVED MIGRATED BUSHING AND INSTALLED 2ND OVERSIZE BUSHING P/N 601R5721003-2003-23, P/N 601R5721003-23 IAW BOMBARDIER INC REO 601R-57-21-003 REV B. (M)

Part: SKIN — CORRODED (LT WING)

LEFT LOWER WING PLANK IS CORRODED UNDER PANEL 550AB, OUTBOARD EDGE 1 INCH LONG BY .100 WIDE BY .002 DEEP. (M)

Part: SKIN PANEL — CORRODED (LT WING)

LT LOWER WING PLANK IS CORRODED UNDER PANEL 550FB, INBOARD SIDE 3 INCH LONG BY .100 WIDE BY .002 INCH DEEP, FORWARD SIDE .200 INCH LONG BY .100 INCH WIDE BY .002 INCH DEEP. S/D - REPAIRED LEFT WING LOWER PLANK FUEL TANK ACCESS DOOR CUTOUT FOR PANEL 550 FB IAW BOMBARDIER, INC REO 601R-57-21-030 REV D.(M)

Part: SKIN — CORRODED (LT WING)

LEFT LOWER WING PLANK IS CORRODED AROUND ENTIRE CIRCUMFERENCE UNDER PANEL 510AB, .100 INCH S BY .002 INCH DEEP. (M)

Part: SKIN PANEL — CORRODED (LT WING)

LEFT LOWER WING PLANK IS CORRODED UNDER PANEL 550HB AT FORWARD CENTER EDGE .600 INCH LONG BY .100 INCH WIDE BY .002 INCH DEEP, INBOARD EDGE 4 INCHES LONG BY .050 INCH WIDE BY .003 INCH DEEP, OUTBOARD SIDE 4.5 INCH LONG BY .025 INCH WIDE BY .003 INCH DEEP. S/D - REPAIRED LT WING LOWER PLANK FUEL TANK ACCESS DOOR CUTOUT FOR PANEL S SCH B IAW BOMBARDIER, INC REO 601R-57-21-030. (M)

Part: SKIN — CORRODED (LT WING)

LEFT LOWER WING PLANK IS CORRODED UNDER PANEL 540BB, FORWARD INBOARD EDGE 4 INCH LONG BY .100 INCH WIDE BY .002 INCH DEEP, AFT EDGE .050 INCH LONG BY .100 INCH WIDE BY .002 INCH DEEP. (M)

Part: SKIN — CORRODED (LT WING)

LEFT LOWER WING PLANK IS CORRODED UNDER PANEL 660CB, AFT INBOARD EDGE .400 INCH LONG BY .100 INCH WIDE BY .002 INCH DEEP. (M)

Part: CLIP — CRACKED (FUSELAGE)

FOUND CRACK ON CLIP AT FS 280 RIGHT SIDE APPROX .5 INCH IN LENGTH AT TOP CORNER IN. REMOVED AND REPLACED RT FS 280 CLIP IAW CRJ SPM 51-42-06 FOR SOLID RIVETS AND 51-45-21 FOR HILITES. (M)

Part: DRAG ANGLE — CRACKED (PAX DOOR)

DOOR AFT DRAG ANGLE CRACKED .7 INCHES LONG AT SUPPORT CABLE PULLEY. (M)

Part: IDG — MALFUNCTIONED (NR 2) · airframe 6,319 hrs · 5,371 cycles

GEN NR 2 FAIL CASS MESSAGE FOLLOWED BY GEN 1 CASS MESSAGE. GEN NR 1 AND 2 RESET OPS NORMALLY. APU WAS RUNNING AND GEN OPS NORMALLY. SERVICED BOTH IDG IAW AMM 12-13-24. OPS CHECK GOOD. OK FOR SERVICE. NO LEAKS NOTED. NR 1 ENG 11 PUMPS AND NR 2 ENGINE 25 PUMPS.

Part: WARNING LIGHT — ILLUMINATED (BLEED AIR DUCT) · airframe 3,697 hrs · 3,097 cycles

LEFT 14TH STAGE BLEED AIR DUCT WARNING INFLIGHT COMPLIED WITH QRH MESSAGE WENT OUT AND THEN CAME BACK 10 MINUTES. WITH ENGINE SHUTDOWN MESSAGE PERSISTED ON GROUND. REMOVED AND REPLACED LT PYLON SENSING ELEMENT A59WK IAW AMM 36-21-04. OPS CHECK GOOD. (M)

Part: WARNING LIGHT — ILLUMINATED (ENGINE BLEED) · airframe 3,697 hrs · 3,096 cycles

RECEIVED LT 14TH STAGE DUCT MESSAGE, COMPLIED WITH QRH. MESSAGE CLEARED WITH THRUST LEVER RETARDED. INSPECTED LEFT 14TH STAGE DUCT BLEED AIR SYSTEM IAW MM 36-12-04. NO FAULTS FOUND. RAN ENGINES TO POWER, NO FAULTS NOTED. OK FOR SERVICE.

Part: IDG — MALFUNCTIONED (NR 2)

IDG CAUTION APPEARED ON TAKEOFF ROLL. COMPLIED WITH 'CM' ACTION PLACARDED AND PLACED ON MEL. RESET NR 2 IDG DISCONNECT MECHANISM. SERVICED IDG AS REQUIRED, OPS CHECK GOOD. REMOVED FROM MEL. (M)

Part: TIRE — FAILED (MLG) · airframe 2,844 hrs · 2,302 cycles

UPON LANDING, MKE, NR 3 MLG TIRE BLEW CAUSING DAMAGE TO RIGHT INBOARD FLAP REPLACED RIGHT INBOARD FLAP IAW AMM. RIGGED FLAP IAW AMM. OPS CHECK GOOD.

Part: IDG — LACK OF LUBE (NR 2 ENGINE)

ABORTED TAKEOFF IDG NR 2 CAUTION MESSAGE. MAINTENANCE SERVICED NR 2 IDG. (M)

Part: CONTROL UNIT — MALFUNCTIONED (TE FLAPS)

FLAPS FAIL ON APPROACH AT ZERO. C/W QRH, RESET FLAP CONTROL NR 1 C/B PER MECHANIC CONTROL, FLAPS NOW RUN AT HALF SPEED - NORMAL LANDING. MAINTENANCE RESET FLAPS PER AWAC SUPPLEMENT 98-18 FLAPS OPERATE AT NORMAL SPEED.

Part: FCU — MALFUNCTIONED (TE FLAPS)

FLAP FAIL IN FLIGHT, FOLLOWED QRH AND MECHANIC PROCEDURES, CAS MESSAGE WENT OUT. MAINTENANCE INTERROGATED FCU, RESET FCU, RAN FLAPS OP CHECK OK C/W AWAC SUPPLEMENT 98-18, AMM 27-50.

Part: JACKSCREW — FROZEN (ELEV TRIM)

ELEVATOR TRIMS BINDS IN THE MIDDLE OF THE TAKEOFF RANGE, TO COMPLETELY NOSE UP RANGE IN FLIGHT. REMOVED AND REPLACED LEFT AND RIGHT ELEVATOR TRIM JACKSCREWS. SUBMITTER STATES, SUSPECT FREEZING OF JACKSCREWS IN FLIGHT, DUE TO WATER COMING OUT OF WEEP HOLES AFTER REMOVAL. SUBMITTER STATES, THESE ARE THE LATEST MOD FROM DHC. LEFT TRIM CABLE IN TAIL CONE FOUND CHAFED. ALSO, REMOVED AND REPLACED CABLE. AIRCRAFT RETURNED TO SERVICE. (M)

Part: AIR DISTR — ODOR (CABIN)

AIRCRAFT FILLED WITH STRONG FUEL ODOR AND BELIEVED TO BE COMING FROM APU BAY AREA. RAN APU BLEED NOTED NO FUEL SMELL OR ABNORMAL ODOR, SUSPECT APU BLEED OPERATION WITH RIGHT ENGINE RUNNING IN FEATHER. AIRCRAFT RETURNED TO SERVICE.

Part: CONTROL UNIT — OUT OF ADJUST (COCKPIT)

FLT NR 6345 - IAD-LGA - ABORTED THE APPROACH DUE TO THE LEFT MAIN GREEN PRIMARY INDICATION NOT ILLUMINATING. SECONDARY INDICATION CHECKED GOOD. AIRCRAFT LANDED WITH NO FURTHER INCIDENCE. MAINTENANCE FOUND THE LIGHT LENS ASSEMBLY INTERFERING WITH THE LAMP. (Z)

Part: FUEL FILTER — DIRTY (NR 2 ENG)

FLT NR 6529 - IAD-LGA - THE NR 2 FUEL FILTER BYPASS CONTAMINATION LIGHT ILLUMINATED IN FLIGHT. AIRCRAFT RETURNED TO IAD WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED NR 2 ENGINE HIGH PRESSURE FUEL FILTER. OPS CHECKED GOOD. AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. (W)