N417AW
Registered owner: UMB BANK NA TRUSTEE, UT (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
Maintenance disclosures
L COWL ANTI ICE CAUTION LIGHT IN FLIGHT. DIVERTED TO PIA. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED RIGHT ENGINE COWL ANTI-ICE VALVE PER AWA AMM SUPP 10-094.OPS CHECK GOOD. PERFORMED OPERATIONAL TEST OF THE ENGINE COWL AND ANTI-ICE SYSTEM PER AMM 30-22-00. OPS CHECKED GOOD. PN OFF: 300013000-003 S/N OFF: 2091 PN ON: 5399-00-1 SN ON: 1484B SMG
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.
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.
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
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
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
L/H FLOOR SILL HAS CORROSION BETWEEN FS 559+80 TO FS621. AIRCRAFT REMOVED FROM SERVICE. REPLACED THE FLOOR SILL
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.
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
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
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
FLOOR SUPPORT L/H AT FS559.O CORRODED BEYOND LIMITS ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED AND REPLACED FLOOR SUPPORT L/H AT FS559.O
FS559.00 FLOOR SUPPORT CORRODED BEYOND LIMITS ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED AND REPLACED FLOOR SUPPORT AF FS559.00
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
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
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.
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.
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.
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.
AC POWER CONTROL UNIT LOWER ATTACH ANGLE IS CRACKED. REPLACED
FS 280 BEAM AFT ANGLE IS CRACKED AT LBL 9 AND RBL 9. REPAIRED
PAX DOOR ASSIST MOTOR OUTBD MOUNT IS CRACKED AT LOWER RADIUS. REPLACED
FS 333 FRAME STR 3L TO STR 0 IS CRACKED STARTING AT TOOLING HOLE. REPLACED
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.
FS280.00 BEAM CORRODED FROM LBL9 TO RBL9. REPAIRED BEAM IAW REO 601R-53-11-926 REV-B.
FS280.00 BEAM FWD ANGLE CRACKED AT LBL 9 AND RBL9.
CARGO DOOR AFT BALANCE SPRING ASSY MOUNT BRACKET IS CRACKED. REPLACED BRACKET IAW CRJ200 SRM 51-24-21, 51-42-06.
FWD EQUIPMENT COMPARTMENT TRU DECK CRACKED AT FS193.00, LBL30. REPAIRED TRU DECK IAW REO 601R-53-11-081 REV-NC.
CARGO DOOR BEAM FWD ATTACH ANGLE CRACKED. REPLACED ANGLE IAW CRJ200 SRM 51-42-21, 51-40-11, TR51-42.
RIGHT EXHAUST NOZZLE FAIRING HAS A CRACKED STIFFENER THIRD FROM THE FWD END. REPLACED STIFFENER IAW CMM 21-42-06.
RIGHT MLG WHEEL WELL HYDRAULIC LINE Z BRACKET CRACKED. REPLACE BRACKET IAW SRM 51-42-06.
NLG WHEEL WELL FS 202.75 RBL 9 VERTICAL POST UPPER CLIP CRACKED. REPLACED
LT TRU PANEL LAND CRACKED AT AFT DOOR LATCH CUTOUT. REPAIRED.
FS 509 LBL 47 FAIRING BRACKET CRACKED. REPLACED.
WINDSHIELD PILOT SIDE POST OUTBD FITTING CRACKED. REPLACED.
BATHTUB FITTING AT RBL 9 FS 461 IS CRACKED. REPLACED
RT MLG WHEEL WELL TRANSDUCER HAT BRACKET CRACKED. REPLACED.
WINDSHIELD CO-PILOT SIDE POST OUTBD CLIP CRACKED. REPLACED.
PASSENGER DOOR LOWER BRACKET PULLEY MOUNT CRACKED. REPLACED.
PAX DOOR AFT DRAG ANGLE CRACKED. REPAIRED.
FS 469, LBL FAIRING SUPPORT BRACKET CRACKED. REPLACED BRACKET IAW SRM 51-42-06.
FS 461.5 FAIRING BRACKET AT LBL 47 CRACKED. REPLACED BRACKET IAW SRM 51-42-06.
FS449.85, LBL FAIRING BRACKET CRACKED. REPLACED BRACKET IAW SRM 51-42-06.
FS 605 FRAME AT STR 9L CRACKED. REPAIRED.
FWD CARGO DOOR TRACK LOWER U-CHANNEL CRACKED. REPLACED.
FS477, RBL47 FAIRING SUPPORT BRACKET CRACKED. REPLACED BRACKET IAW CRJ200 SRM 51-42-06.
FS449.85, RBL 47 FAIRING SUPPORT BRACKET CRACKED. REPLACED BRACKET IAW CRJ200 SRM 51-42-06.
FS469, RBL47 FAIRING SUPPORT BRACKET CRACKED. REPLACED BRACKET IAW CRJ 200 SRM 51-42-06.
FS280, STR 3L I/B AND O/B CLIPS CRACKED. REPLACED CLIPS IAW CRJ 200 SRM 51-42-06, 51-42-21.
RIGHT WING MID L/E I/B ATTACH BRACKET IS CRACKED. REPLACED BRACKET IAW CRJ 200 SRM 51-41-02.
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.
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.
STRONG FUEL ODOR IN COCKPIT AND CABIN WITH PACKS ON. R & R THE LT AND RT COALESCER SOCKS IAW 14-192. NO ODOR NOTED.
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.
LBL27 SEAT TRACK O/B FLANGE HAS CORROSION AT FS560 AND FS565.
PANEL 684AB HAS 1 BLOWN OUT FASTENER HOLE.
WHILE ACCOMPLISHING AWAC JOB CARD 4EOAWA20075-E16/011/453 SECTION 1 ITEM 5, FOUND CHAFE TO EXCEED LIMITS ON LT APRON, REQUIRES REPAIR.
LBL27 FLOORBEAM ATTACHMENT TO REAR PRESSURE BULKHEAD HAS CORROSION ON UPPER SURFACE.
SERVICE DOOR SURROUND LOWER DEPRESSOR GOUGED AT AFT SPIGOT FITTING. REMOVED AND REPLACED LOWER DEPRESSOR IAW SRM 51-42-02.
LEFT LOWER VISOR FORWARD ATTACH BRACKET CRACKED. REMOVED AND REPLACED THE LOWER VISOR ATTACH BRACKET IAW SRM 51-42-21,.
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.
LH WING INBD LEADING EDGE OUTBOARD ATTACH BRACKET IS CRACKED
FLIGHT DECK WINDSHIELD CENTER POST LOWER LEFT FITTING IS CRACKED. NDT HAS VERIFIED
FLIGHT DECK WINDSHIELD CENTER POST LOWER RIGHT FITTING IS CRACKED. NDT HAS VERIFIED
LBL 27 FLOOR SUPPORT CAP HAS CORROSION ON OTBD FLANGE BETWEEN BS 589 AND 621
INBD WEB OF LBL 27 FLOORBEAM HAS A CRACKED FASTENER HOLE AT BS 588
RIGHT EXHAUST FAIRING SECONND STIFFENER IS CRACKED
LEFT AISLE SEAT TRACK HAS CORROSION BETWEEN BS 364 AND 394, IN CABIN.
FLIGHT 3922. EMERGENCY LIGHT WIRE CUT AT ROW 13. REPAIRED THE WIRE AT ROW 13 IAW ESPM 20-16-00, OPS CHECKED GOOD.
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.
FLIGHT 9898. EMERGENCY FLOOR TRACK LIGHTING INOP ROW 8 AND AFT REPAIRED BROKEN CONNECTOR PER ESPM 20-17-10, OPS CHECK GOOD.
BACK 2 ROWS ON FLOOR TRACK LIGHTS STRIP OBSCURED.
RECEIVED PROXIMITY SYSTEM FAULT MSG INFLIGHT ON GEAR EXTENTION. RECEIVED INBD ANTI-SKID CAUTION MSG BTMS 3, 3, 3, 2.
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.
AFTER TAKEOFF RECEIVED PASSENGER DOOR WARNING ALSO SERVICE AND CARGO DOOR CAUTION. PRESSURIZATION NORMAL, LANDED UNDERWEIGHT.
FLIGHT 3852, EMERGENCY LIGHT BROKEN FROM ROW 9 BACK. END CAP BROKEN OFF & WIRING EXPOSED.
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.
HYD 2 LOW PRESS MSG ON CLIMB OUT. HYD SYS READS 10%. HYD PUMP 2A OPERATED FOR MORE THAN 30 MINUTES.
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.
LEFT WW NR 3 HYD RESERVOIR AFT MOUNT CRACKED.
LEFT WING CTR LE INBD MOUNT ANGLE ON WING IS CRACKED AT BOTTOM.
FLOOR SILL AT LBL 27 FS 605 IS CRACKED.
LEFT MLG WW BATTERY RIB IS CRACKED.
RIGHT HYD MANIFOLD ASSEMBLY SUPPORT IS CRACKED IN AFT LOWER RADIUS.
PASSENGER DOOR STEP AFT SUPPORT DRAG ANGLE CRACKED.
AUXILIARY DOOR HANDLE MECHANISM SUPPORT MOUNT FITTING CRACKED DURING REPLACEMENT OF OUTER HANDLE ASSEMBLY.
RIGHT WING LE MOUNT NEAR WS 149.58 IS CRACKED.
LEFT WW BRAKE PRESS TRANSDUCER MOUNT IS CRACKED.
DRAG ANGLE ADJACENT TO LT BATTERY RIB IS CRACKED.
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.
DRAG ANGLE ADJACENT TO RT BATTERY RIB IS CRACKED.
LT WING LE ATTACHMENT BRACKET NEAR WS 148 IS CRACKED.
CLIP CRACKED AT FS 484 RBL 36.
CLIPS AT FS 484, LBL 27 & LBL 36 ARE CRACKED.
ACFT GND POWER RECEPT MOUNT BRACKET CRACKED.
SERVICE DOOR LOWER SILL HAS CORROSION.
CORROSION ON FLOOR SUPPORT STRUCTURE, FS 349, LBL 30 - 40.
CAPTAINS WINDSHIELD LOWER LT TERMINAL BLOCK STARTED ON FIRE. SHUT OFF WINDSHIELD HEAT, FIRE STOPPED.
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.
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.
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.
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.
LEFT OR LEADING EDGE 530 O/B SPLICE HAS OVERSIZED (ELONGATED) SCREW HOLES. REMOVED AND REPLACED CH O/B LEADING O/B SPLICE.
GOUGED AREA FOUND AT AFT LOWER SIDE OF CARGO DOOR STOP FITTING. BLEND & PERFORM PASSIVITY APPLICATION IAW REO 601R-52-31-206.
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.
CHAFE FOUND ON RT SIDE SEAT TRACK NEAR FS 522. BLEND & RESTORE FINISH IAW REO 601R-53-41-1663.
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.
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.
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.
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.
TRANS COWL 444AT IS GOUGED ON OUTER SIDE. REPAIRED TRANS COWL IAW REO 601R-78-33-4010.
CORROSION FOUND ON GALLEY MOUNTING PLATE AT FS 318.00. REMOVE & REPLACE GALLEY MOUNTING PLATE IAW CRJ 200 SRM.
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.
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.
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.
PAX DOOR INTERCOSTAL ON PANEL 832BR IS CRACKED. REMOVED & REPLACED INTERCOSTAL.
PAX DOOR AFT HINGE LUG IS GOUGED. REPAIRED PAX DOOR AFT HINGE LUG IAW BOMBARDIER REO 601R-52-11-1347.
LAV SERVICE DOOR, LED LIGHT BRACKET IS CORRODED. REMOVED UNSERVICEABLE BRACKET AND INSTALLED SERVICEABLE BRACKET IAW CRJ 200 SRM 51-42-06.
RIGHT AILERON UPPER FWD SHROUDS ARE CHAFED. BLENDED CHAFE IAW REO 601R-57-60-013.
CHAFED AREA FOUND ON LEFT O/B FLAP NEAR I/B ROLLER BEARING. BLEND, MEASURE, RESTORE FINISH IAW REO 601R-57-53-968.
RIGHT O/B FLAP ROLLER GUIDE FITTING CHAFED. BLEND, MEASURE & RESTORE TO ORIG FINISH IAW REO 601R-57-53-969.
CHAFE FOUND ON ALIGNMENT FITTING OF RIGHT O/B FLAP. BLEND, MEASURE & RESTORE FINISH IAW REO 601R-57-51-143.
UPPER PAX DOOR STEP 832 ET HAS CORROSION ON UPPER AND CENTER HINGES. REMOVE AND REPLACE HINGES.
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.
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.
RIGHT BULKHEAD AT FS 280 CHAFED AND DENTED AT FLIGHT DECK ENTRANCE. REPAIRED IAW CRJ REO 601R-53-11-1727.
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.
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.
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.
RIGHT ENGINE TAIL PIPE INNER SKIN IS CRACKED NEAR THE 11 O`CLOCK ACCESS PANEL. INSTALLED REPAIR DOUBLER IAW CRJ 200 CMM 78-11.
STIFFENER PLATE FWD SIDE CARGO DOOR CUTOUT JUST BELOW BOTTOM STOP FITTING IS CRACKED. REMOVED & REPLACED WITH NEW STIFFENER PLATE.
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.
SCRATCH ON PAX DOOR HINGE AFT LUG LAND. BLEND SCRATCH IAW CRJ REO 601R-53-21-814.
LEFT SEAT TRACK HAS DAMAGE NEAR FS 409 + 128. BLENDED DAMAGED AREA FOUND TO BE WITHIN LIMITS.
AFT EQUIPMENT BAY DOOR CUTOUT, RIGHT SIDE AT FS 700 SUPPORT ANGLE CRACKED. REMOVED AND FAB SERVICEABLE ANGLE PER SRM.
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.
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.
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.
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.
FLAP FAIL AT 12 DEGREES, COMPLIED WITH QRH, PERFORMED RESET IAW SUPPLEMENT 98-18E BOX 12, FLAPS RESET.
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.
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.
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.
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.
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.
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.
BUTTE DOOR 694PB INNER SKIN CHAFED. R & R BUTTE DOOR 694PB SKIN IAW SRM 51-42-06.
APU AFT HEATSHIELD HAS FASTENERS PULLED THRU REPAIRED IAW REO 601R-49-81-147, 601R-49-81-051.
RUDDER L/E CHAFED RT SIDE BLENDED CHAFING OUT IAW SRM 51-12-00.
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.
APU ENCLOSURE DOOR 311B2 CRACK AT WELD TOP OF STIFFENER. REPAIRED APU ENCLOSURE DOOR 311B2 AND IAW REO 601R-49-11-070.
APU EXHAUST HEATSHIELD CRACKED AT 6 O`CLOCK POSITION. REPAIRED APU EXHAUST HEATSHIELD IAW REO 601R-49-81-003, REV B.
LT T/R UPPER INBD CASCADE CRACKED. REPAIRED LT T/R UPPER INBD CASCADE IAW PROCESS SPECIFICATION 1, DWG AW78-30-0711-04.
RT MLG DOOR FWD EDGE CHAFED IN 2 EA PLACES PREVIOUS REPAIRS. R & R LOWER FILLER IAW REO 601R-52-82-034.
RBL 18.00 POST CRACKED OTBD BOTTOM AT FS 409.00+128. REPAIRED IAW REO 601R-53-41-056, REV E.
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.
LBL 18.00 POST CRACKED OTBD BOTTOM AT FS 409+128. REPAIRED IAW REO 601R-53-41-056, REV E.
RT BATT RIB IS CRACKED. REPAIRED RT BATT RIB IAW REO 601R-57-51-046, REV B.
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.
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.
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.
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.
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.
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.
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.
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.
LOWER LT AILERON SHROUD PANELS 599AB AND 599CB CHAFED. REPAIRED LOWER LT AILERON SHROUD PANELS 599AB AND 599CB IAW REO 601R-57-60-020.
LOWER LT AILERON SHROUD PANEL 599BB GOUGED. REPAIRED LOWER LT SHROUD PANEL 599BB IAW REO 601R-57-60-020.
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.
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.
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)
(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)
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)
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)
MWC 134852-112 - AVIONIC DOOR SEAL RETAINERS FOUND CORRODED. SEAL RETAINER REMOVED AND REPLACED IAW SRM 51-42-06. (K)
AVIONIC DOOR SEAL RETAINERS FOUND CORRODED. SEAL RETAINER REMOVED AND REPLACED IAW SRM 51-42-06. (K)
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)
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)
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)
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)
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)
PAX DOOR ASSIST MOTOR BRACKET (PN 601R317743-7) CRACKED AT BOTTOM END APPROX. 12 INCHES LONG. (K)
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)
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)
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)
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)
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)
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)
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.
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)
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)
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)
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)
WHEN SELECTING FLAPS FROM 8 DEGREES TO 20 DEGREES, A FLAP CAUTION MESSAGE OCCURRED IN FLIGHT. (K)
CAPTAINS OXYGEN MASK MIC INTERMITTENT. REMOVED AND REPLACED CAPTAINS OXYGEN MASK IAW 35-10-00, OPS CHECK GOOD. (M)
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)
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)
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)
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)
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)
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)
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)
LEFT LOWER WING PLANK IS CORRODED AROUND ENTIRE CIRCUMFERENCE UNDER PANEL 510AB, .100 INCH S BY .002 INCH DEEP. (M)
LEFT LOWER WING PLANK IS CORRODED UNDER PANEL 660CB, AFT INBOARD EDGE .400 INCH LONG BY .100 INCH WIDE BY .002 INCH DEEP. (M)
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)
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)
LEFT LOWER WING PLANK IS CORRODED UNDER PANEL 550AB, OUTBOARD EDGE 1 INCH LONG BY .100 WIDE BY .002 DEEP. (M)
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)
DOOR AFT DRAG ANGLE CRACKED .7 INCHES LONG AT SUPPORT CABLE PULLEY. (M)
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.
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)
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.
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)
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.
ABORTED TAKEOFF IDG NR 2 CAUTION MESSAGE. MAINTENANCE SERVICED NR 2 IDG. (M)
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.
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.
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)
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.
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)
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)