N420AW
Registered owner: CSI AVIATION INC, TX (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| AIR WISCONSIN AIRLINES CORPORATION | Operator | 2025-02-01 – 2025-02-01 | Operator named in NTSB report |
| AIR WISCONSIN AIRLINES LLC (A6WA) | Operator | 2025-02-01 – 2025-02-01 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
AFTER ADDING TAKEOFF THRUST AND RELEASING BRAKES AIRCRAFT PULLED VERY HARD TO THE LEFT, ABORTED TAKE OFF. TAXIED OFF RUNWAY NO ISSUES AT NORMAL TAXI SPEED. BRAKE TEMPS NORMAL NO ABNORMAL MESSAGES AND NWS OPERATED NORMALLY. ALL OTHER INDICATIONS NORMAL. AIRCRAFT REMOVED FROM SERVICE. T/S PER FIM 32-50-02-01 FOR LATERAL DEVIATION AND FOUND LOOSE CONNECTOR ON LH FEEDBACK RVDT. RIG CHECKED RVDT IAW 32-51-02 AND CHECK IS GOOD. TAXI CHECK IS GOOD, NO ABNORMALITIES
FLAPS FAIL CAUTION MSG AT 20* FLAPS ON APPROACH. PERFORMED FLAP RESET PROCEDURE IAW AWAC SUP 98-18I BOX 12. FLAPS RESET. PLACARDED AND PLACED ON MEL. ACARS: A/C FLT DEP DST TIME ALT N420AW 6068 LEX PHL 1642Z 1756 STATE MINS IAS OAT FLAPS FAIL HALF AIR 00115 174 16 19 YES NO ***** AIRCRAFT REMOVED FROM SERVICE ***** R&R FLAP CONTROL LEVER IAW AMM SUPP 09-038A. OPS CHECK GOOD. REMOVED PLACARD AND REMOVED FROM MEL. PN:7-45500-1 SN OFF:0434 SN ON:0497 RAH
ABORTED TAKE OF DUE TO LACK OF RUDDER RESPONSE LESS THAN 60 KTS FO'S LEG. PRESSURIZED ALL 3 HYD SYSTEMS, VISUALLY VERIFIED FULL DEFLECTION OF RUDDER TRAVEL FROM BOTH CA AND FO RUDDER PEDALS. EICAS INDICATION AGREES. AIRCRAFT REMOVED FROM SERVICE. PERFORMED VIS INSP ON MLG TIRE IAW AMM 32-41-01 AND NLG TIRE IAW AMM 32-42-01, NO DEFECTS NOTED. PERFORMED OPS CHECK OF BRAKE SYS IAW AMM 32-43-00, OPS CHECK GOOD. PERFORMED OPS CHECK OF RUDDER CONTROL SYS IAW AMM 27-21-00. OPS CHECK GOOD. PERFORMED OPS CEHCK OF NWS STEERING
GEAR DISAGRE ON WARNING NLG DOWN MLG UP C/W QRH MANUAL EXT GEAR DOWN ALL AND LOCKED NORMAL LANDING. 6 SEC AND MANUL RELEASE WAS USED. HYD WAS IN AUTO. EMERGENCY DECLARED, 180 KNTS SPEED. NO OVERWEIGHT LDG. AIRCRAFT REMOVED FROM SERVICE. R/R NOSE LANDING GEAR PROX SENSOR BRACKET IAW AMM 32-61 OPS CHECK GOOD. GOOD TO CONTINUE SERVICE.
IN CRUISE, RECEIVED FLAPS FAIL CAUTION. BTMS INDICATIONS DID NOT EXCEED 10. PERFORMED FLAP RESET PROCEDURE IAW AWAC SUP 98-018I, BOX 12. FLAPS RESET. PLACARDED AND PLACED ON MEL. FLAPS FAILED AGAIN APPROX 5 MINUTES AFTER RESET. AIRCRAFT REMOVED FROM SERVICE. R&R RIGHT HAND BPSU IAW AMM 27-51-10, OPS CHECK GOOD.
ON DEPARTURE RECIEVED STEERING INOP CAUTION FOLLOWED BY WOW INPUT CAUTION AND WOW OUT PUT FAIL STATUS MSGS. RAN QRH. CYCLED NWS, MSG PERSISTED. WHEN EXTENDING GEAR ALL MSGS CLEARED. AIRCRAFT REMOVED FROM SERVICE. C/W FAULT ISOLATION OF STERING INOP MSG REF CRJ-200 FIM 32-50-01 REV 62 ADJUSTED NLG W/OFF/W SENSORS IN REF CRJ-200 AMM 32-61-05-000-805 AND 32-61-05-400-805 REV 66, & C/W OPS TESTS REF CRJ-200 AMM 32-30-00-710-802, 32-61-00-710-801 AND 32-51-00-710-801 REV 66 ALL TESTS GOOD AND NO STEERING INOP MSG SHOWN.
SKIN DIMPLED AROUND 4 RIVETS ON FRAME FS379.00 BETWEEN STGR23LL AND STGR22L ***** AC REMOVED FROM SERVICE ***** REPAIRED FRAME AT FS 379 BETWEEN STRG23L AND STRG22L REF REO 601R-53-21-3628 REV -- DATED 2023-04-21
CORROSION FOUND ON PAX DOOR FORMER AT FS320.00 FROM DD5-UPPER FORMER AT HINGE. ***** AC REMOVED FROM SERVICE ***** INSTALL FORMER AT FS 320.00 BETWEEN DD5 DATUM AND UPPER FORMER AT HINGE REF CRJ200 SRM 51-42-06, CRJ200 SRM 51-42-21 AND DWG 601R31702 REV: -N
FRAME AT FS 319 HAS CORROSION REF CRJ-200 SRM 51-42-06 AND SRM 51-42-21 AND DWG 601R32003 REV P ***** AC REMOVED FROM SERVICE ***** REPLACE FRAME AT FS 319 REF
L/H PRESSURE FLOOR SILL PANEL FROM FS409+128 TO FS559 HAS MULTIPLE AREAS OF CORROSION . ***** AC HAS BEEN REMOVED FROM SERVICE ***** REPAIRED L/H PRESSURE FLOOR SILL PANEL FROM FS409+128 TO FS 559 REF REO 601R-53-41-666 REV -- DATED 27-MAY-2008 AND REO 601R-53-41-3151 REV -- DATED 2023-04-15
INTERCOSTAL AT STGR21L BETWEEN FS349-FS333 HAS CORROSION ***** AC REMOVED FROM SERVICE ***** INSTALLED NEW INTERCOSTAL FROM STGR 21 LH BETWEEN FS 333.00 AND FS 349.0 REF CRJ200 SRM 51-42-06 AND CRJ200 SRM 51-42-21 AND DWG 601R31527 REV AM
R/H PRESSURE FLOOR SILL PANEL FROM FS409+128 TO FS559 HAS MULTIPLE AREAS OF CORROSION ***** AC REMOVED FROM SERVICE ***** REPAIRE R/H PRESSURE FLOOR SILL REF REO 601R-53-41-3149 REV A DATED 2023-04-14
REMOVE EXISTING REPAIR TO COMPLY WITH PERMANENT REPAIR AT THE REQUEST OF THE CUSTOMER ***** AC REMOVED FROM SERVICE ***** REPAIRED FRAME SECTION AT FS276 REF REO 601R-53-11-3859 REV -- DATED 2023-04-19
CORROSION ON FRAME FS364.00 AND STRG23L ***** AC REMOVED FROM SERVICE ***** REPLACED FRAME SECTION REF REO 601R-53-21-3626 REV -- DATED 2023-04-19
FRAME AT FS 333 HAS CORROSION STGR23L-25R ********AIRCRAFT REMOVED FROM SERVICE******** REPLACED FRAME AT FS333 REF CRJ-200-SRM 51-42-06,CRJ-200-SRM 51-42-21, AND DRAWING 601R32004 REV M
CORROSION FOUND ON PAX DOOR CLEAT AT FS338.00 AND UPPER FORMER AT HINGE *********AIRCRAFT REMOVED FROM SERVICE******* INSTALLED NEW PAX DOOR CLEAT AT FS338.00 REF DWG 601R31702 REV-N CRJ 200 SRM 51-42-10
PAX DOOR FWD FORMER HAS CORROSION BETWEEN DD6-DD5 *********AIRCRAFT REMOVED FROM SERVICE******* REPLACED NEW PAX DOOR FWD FORMER REF DRAWING 601R31702 REV N
PERFORM PERMANENT REPAIR FOR LH INBOARD FLAP INNER DOUBLER. ********AIRCRAFT REMOVED FROM SERVICE******* REPAIRED L/H INBOARD FLAP UPPER SKIN REF REO 601R-57-52-2482 REV -- DATED 2023-04-12
CORROSION FOUND ON PAX DOOR INTERCOSTAL AT DD4 BETWEEN FS 338.00 FS349.00 *********AIRCRAFT REMOVED FROM SERVICE********* INSTALLED A NEW PAX DOOR INTERCOSTAL FS338.00-FS349.00. REF DWG 601R31702 REV-N AND CRJ 200 SRM 51-42-06
CORROSION FOUND ON PAX DOOR CLEAT AT FS313.56 DD4. *****AIRCRAFT REMOVED FROM SERVICE********* INSTALLED NEW CLEAT AT FS 313.56 DD4 REF CRJ-200-SRM 51-42-06 AND DRAWING 601R31702 REV N
PRESSURE FLOOR SKIN HAS 2EA DENTS BETWEEN LBL 9-BL0 FS499 *******AIRCRAFT REMOVED FROM SERVICE***** REPAIRED PRESSURE FLOOR SKIN REF REO 601R-53-41-3147 REV -- DATED 2023-04-07
"ÿ½PASSENGER DOOR HINGE ON FUSELAGE LUGS FAILED THE CHECK WITH THE NO/GO GAUGE ***** AC REMOVED FROM SERVICE ***** REPLACED PAX DOOR HINGE ,BOMBARDIER DWG 601R31527 REV AM AND REO 601R-53-21-656 REV A DATED 2017/03/06"
PAX DOOR AFT FORMER HAS CORROSION BETWEEN DD6-DD5 ***** AC REMOVED FROM SERVICE ***** REPLACED AFT PAX DOOR FORMER REF DWG 601R31702 REV N
FRAME AT FS 310 HAS CORROSION STRG26L-26R. AC REMOVED FROM SERVICE. INSTALLED NEW LOWER FRAME SECTOR TO THE LOWER SKIN @ FS310 REF CRJ-200 SRM 51-42-06 AND DWG 601R32002 REV.AC.
CORROSION FOUND ON PAX DOOR INTERCOSTAL AT DD6 BETWEEN FS 320-FS 338.00 *******AIRCRAFT REMOVED FROM SERVICE******** REPLACE INTERCOSTAL ON PAX DOOR DD6 REF CRJ-200-SRM 51-42-06,CRJ-200-SRM 51-42-21
FWD CARGO DOOR BOX SPRING FRAME SUPPORT STRUCTURE CRACKED. *******AIRCRAFT REMOVED FROM SERVICE****** REPLACED FWD CARGO DOOR BOX SPRING FRAME SUPPORT STRUCTURE BRACKET REF SRM 51-42-06
CORROSION FOUND ON PAX DOOR INTERCOSTAL AT DD5 BETWEEN FS 338.00 TO FS 349.00 ******AIRCRAFT REMOVED FROM SERVICE******** REPLACED PAX DOOR INTERCOSTAL AT DD5 BETWEEN FS 338.00 TO FS 349.00 REF DWG 601R31702 REV-N
FS484.00 BETWEEN RBL 27-36, FLIGHT CONTROL CABLE ROLLER GUIDE ASSY, INBOARD ATTACH ANGLE CRACKED(MARKED) *****AIRCRAFT REMOVED FROM SERVICE*********** REPLACED CLIP REF SRM51-42-21 AND DWRG 601R31171 REV - E
FS 484.00 BETWEEN LBL 27-36 FLIGHT CONTROL CABLE ROLLER GUIDE ASSY ,INBOARD ATTACH ANGLE ********AIRCRAFT REMOVED FROM SERVICE******* REPLACE CLIP 484 CLIP REF DRAWING 601R31171 REV E , AND CRJ-200 SRM 51-42-21
COLLINS 4200 FMS. KEYS ON KEYBOARD ARE WORE OUT AND WHEN YOU TYPE THE KEYS REPEATS THE SAME NUMBER OR LETTER, 2 TO 3 TIMES. COMPANY REFUSES TO FIX THEM. IMO THIS IS A SAFETY OF FLIGHT ISSUE. ALL AIRCRAFT IN FLEET HAVE THIS PROBLEM. 405-471AW
ON TAKE-OFF REC'D RT ENG OIL WARNING MESSAGE. MESSAGE WAS INTERMITTENT. OIL PSI FLUCTUATED BETWEEN 25 AND 35 PSI. OIL TEMP WAS NORMAL. MESSAGE WAS LESS INTERMITTENT WITH REDUCED POWER. EVENT DESCRIPTION: EN ROUTE, THE #2 ENGINE OIL PRESSURE BEGAN TO FLUCTUATE. AFTER REVIEWING THE QRH AND COORDINATING WITH DISPATCH, THE FLIGHT CREW HAS DECLARED AN EMERGENCY ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED AND REPLACED THE OIL PRESURE TRANDSUCER O-RING AND INSTALLED MISSING TEFLON BACKER RINGS ON RIGHT ENGINE. IAW AMM 79-31-05, OPS CHECK AND LEAK CHECKS
3885 RT WING A-ICE CAUTION MSG USING STANDBY. EN ROUTE, THE FLIGHT EXPERIENCED A RIGHT WING ANTI ICE CAUTION MESSAGE. IN THE INTEREST OF SAFETY, TO AVOID ICING CONDITIONS, THE CREW AND DISPATCHER HAVE AGREED TO DIVERT TO DAY. NO EMERGENCY DECLARED AND THE FLIGHT LANDED IN DAY. WRITE UP WAS "RT WING A-ICE CAUTION MSG USING STANDBY." ***AIRCRAFT REMOVED FROM SERVICE*** R&R ANTI ICE PANEL IAW AMM 30-12-21 OPS CHECK GOOD IN BOTH STBY AND NORMAL MODE. REMOVED PLACARD REMOVED FROM MEL
LH SIDE RAIL BETWEEN FS 449 TO 499 IS OUT OF LIMITS DUE TO HEAVY CORROSION. REMOVED AND REPLACED LH SIDE RAIL
LEFT WINDSHIELD CRACKED IN FLIGHT DURING CLIMB OUT. AIR RETURN TO IAD. AIRCRAFT REMOVED FROM SERVICE. R & R CA WINDSHIELD PER AMM 56-11-01 SEE LP 307033/1 FOR SEALANT CURE CHECK AND 307033/2 FOR OPS CHECK/LEAK CHECK OF WINDSHIELD HEAT P/N OFF:NP139321-13,S/N OFF:10293H5106 ; P/N ON:NP139321-17,S/N ON:20017H0070. MPM
EVENT DESCRIPTION: CREW REPORTED CRACKED WINDSHIELD EN ROUTE TO MKE. FLIGHT DIVERTED TO DAY AND DECLARED AN EMERGENCY. FLIGHT IS A REPOSITION WITH ZW MECHANICS ON BOARD, REF 307026/4: AT FLT 300 OBSERVED ARCING ON F/O' WINDSCREEN TURNED F/O WINDSHIELD HEAT OFF 5 SECONDS LATER F/O WINDSCREEN SHATTERED. SWITCH WAS IN LOW POSITION, REF 307027/1: WHILE PERFORMING QRH FOR A CRACKED WINDSHIELD MAN ALT SWITCH STUCK IN UP POSITION AND WOULD NOT GO TO NEUTRAL POSITION. RECEIVED CABIN ALT WARNING AND THE PASSENGER MASKS AUTO DEPLOYED. AFTER LANDING FOUND F/A'S MASK (CONT IN BLOCK 2) ROWS 5 CD AND 6AB HANGING LOWER THAN OTHERS. AIRCRAFT REMOVED FROM SERVICE. R & R FO WINDSHIELD, IAW AMM 56-11-01. OPERATIONS AND LEAK CHECK GOOD.
STEERING INOPERABLE MESSAGE AT CRUISE FL 290. CW QRH MESSAGE PERSISTED, AFTER SELECTING GEAR DOWN CYCLED STEERING OFF ON MESSAGE RETURNED. EMERGENCY DECLARED. CYCLED SW AGAIN AT 500 FT MESSAGE CLEARED. STEERING APPEARED NORM AFTER LANDING. TAXI TO GATE UNDER OWN POWER. AIRCRAFT REMOVED FROM SERVICE. R & R NOSE STEERING HARNESS, REF AMM 32-61-25. OPERATIONS CHECK GOOD NO MESSAGE DURING TAXI.
RECEIVED R AOA HEAT CAUTION MESSAGE IN-FLIGHT. C/W QRH MESSAGE PERSISTED. AIRCRAFT REMOVED FROM SERVICE. C/W FIM RESET MESSAGE CLEARED.
FLAP FAIL CAUTION MESSAGE DURING CRUISE AT 280 KNOTS, C/W QRH. DECLARED EMERGENCY AND SELECTED LONGEST RUNWAY. AIRCRAFT REMOVED FROM SERVICE. RESET AND PLACED ON MEL FOR 10 CYCLES.
FLAP WERE MEL'D AT ORD AND RESET. EN ROUTE TO CID THEY FAILED AGAIN. FLIGHT WILL CONTINUE TO CID. THE CAPTAIN INDICATED THAT DURING DESCENT TO KCID THE FLIGHT CREW RECEIVED A FLAPS FAIL CAUTION MESSAGE. THE CREW COMPLETED THE APPROPRIATE CHECKLISTS, ADVISED THE F/A AND PASSENGERS AND DECLARED AN EMERGENCY AND LANDED WITHOUT FURTHER INCIDENT. AIRCRAFT REMOVED FROM SERVICE. T/S IAW FIM 27-50-00 FIG 107 BASED ON FECU CODES INCLUDED ON RECORD OF FECU FAULT LOG, CONTENTS INCLUDED IN WORK PACK. CW HARNESS INTEGRITY TEST FROM RT BPSU TO CONNECTOR 2P5CE NO FAULT FOUND REMOVED & REPLACED RT BPSU, IAW AMM 27-51-10. OPS CHECK GOOD.
UPON GEAR EXTENSION RECIVED GEAR DISAGREE NOSE SHOWED UNSAFE PERFORMED EMERGENCY GEAR EXTENSION PER QRH. MESSAGE OCCURED 6 SECONDS AFTER SELECTION, NO OTHER ASSOSIATED EICAS MESSAGES.
AIRCRAFT SKIN HAS TWO PROTRUDING DENTS BETWEEN FS 621-640 AND IN BETWEEN STRINGERS 25L AND 26L. REPAIRED SKIN BETWEEN FS 621-640 BETWEEN STRINGER 25L AND 26L IAW EA# AWAC-CRJ253-01271.
BRACKET BETWEEN TH INBD LE AND CENTER LE CRACKED. REPLACED
CORE COWL 435AT UPPER SKIN AFT I/B CORNER CRACKED. REPAIRED CORE COWL IAW CMM71-12-01.
CARGO DOOR BEAM GROOVED AT AFT END OF BEAM DUE TO CARGO DOOR SPRING CABLE. REPLACED CARGO DOOR BEAM MEMBER IAW CRJ200 SRM 51-42-06, 51-42-21.
PAX DOOR LOWER SILL FWD CLEAT CORRODED. REPLACED CLEAT IAW CRJ200 SRM 51-42-06, 51-42-10, 51-42-12.
PAX DOOR AFT LOWER CLEAT CORRODED. REPLACED CLEAT IAW CRJ 200 SRM 51-42-06, 51-42-10, 51-42-12.
CENTER WINDSHIELD POST LOWER FITTING CRACKED LH SIDE IN RADIUS. REPLACED.
RH INBD FLAP VANE LE CENTER SKIN IS CHAFFED. REPLACED
LEFT INBD FLAP VANE MIDDLE LE CHAFED. REPLACED.
RH INBD FLAP VANE LE OUTBD SKIN IS CHAFFED. REPLACED
FS 559+78 TO 559+95 RBL 27 CARGO TRACK CORRODED. REPLACED
FS 559+86 TO 559+95 LBL 9 CARGO TRACK CORRODED. REPLACED
NOSE GEAR SPADE DOOR CUTOUT AFT R/H CORNER IS CRACKED. REPAIRED CUTOUT SKIN IAW REO 601R-53-11-048 REV-D.
L/H O/B FLAP, CENTER HINGE ARM I/B FAIRING GUIDE IS CHAFED. REPLACED FAIRING GUIDE IAW CRJ200 SRM 51-42-06.
RIGHT I/B FLAP VANE, L/E I/B SKIN IS CHAFED. REPLACE RIGHT I/B FLAP VANE I/B L/E SKIN IAW SRM 51-42-13.
LT WHEEL WELL VOLUMETRIC FUSE BRACKET IS CRACKED. REMOVED AND REPLACED CRACKED LT BRACKET IN WHEEL WELL IAW SRM TR 51-42 AND 51-42-06.
FS 559 LBL 28 TO LBL 42 PRESSURE FLOOR STRAP HAS CORROSION. REMOVED AND REPLACED FS 559 LBL 28 TO LBL 42 PRESSURE FLOOR STRAP IAW SRM 51-42-06.
RH WHEEL WELL VOLUMETRIC FUSE BRACKET CRACKED REMOVED AND REPLACED RH WHEEL WELL FUSE BRACKET IAW SRM 51-40-11 (TR51-42), 51-42-06
PASSENGER DOOR AFT DRAG ANGLE CRACKED NEAR PULLEY BRACKET REPAIRED PAX DOOR AFT DRAG ANGLE IAW BOMBARDIER REO# 601R-52-11-513
SERVICE DOOR SURROUND STRUCTURE FS 319 RBL 43 WL 71 T-BRACKET IS EXFOLIATED. REPLACED.
TRU PANEL LAND AT LATCH CRACKED. REPAIRED.
ON CLIMBOUT RECEIVED PAX DOOR OUTER HANDLE CAUTION WHICH CONTINUOUSLY REPEATED IN FLIGHT. ON LANDING ROLLOUT RECEIVED PAX DOOR WARNING MESSAGE. PERFORMED OPS TEST OF PAX DOOR WARNING SYSTEM IAW AMM 52-70-04, OPS CHECK GOOD. R&R PS1MB IAW AMM 52-70-04-04. OPS CK GOOD.
PROXIMITY SYSTEM FAULT CAUTION MESSAGE DURING FLIGHT, COMPLIED WITH QRH, INBOARD & OUTBOARD ANTI-SKID MESSAGES STILL PRESENT. INTERROGATED PSEU FOUND CODE NO COMM. R & R THE PSEU IAW AMM 32-61-01 OPS CHECKED GOOD.
DURING RON MAINTENANCE, THE AFT OVERWING EMERGENCY EXIT WERE FOUND TO BE INOPERATIVE BOTH RIGHT AND LEFT SIDE. REMOVED AND REPLACED NR 4 BATTERY PACK IAW AMM 33-51-01. OPS CHECKED GOOD.
BS 333 FRAME HAS CORROSION OTBD OF STRINGER 23R.
LBL 9 FLOOR SUPPORT HAS CORROSION AROUND NUTPLATE LOCATIONS BETWEEN BS 605 AND BS 621.
LBL 9 OTBD FLOOR SUPPORT WEB BETWEEN BS 574 AND 589 HAS 1EA ELONGATED FASTENER HOLES.
RBL 27 FLOOR SUPPORT HAS CORROSION AT NUTPLATE LOCATION BETWEEN BS 605 AND 621.
FRAME FS 605 CORRODED BETWEEN STRINGERS 25L AND 26R
FS 280 FWD FLOORBEAM ANGLE CRACKED, LBL 9 AND RBL 9.
BS 280, RBL 9, INBD ANGLE CRACKED
BS 280, LBL 9 INBD ANGLE CRACKED.
CARGO BAY FLOORBEAM WEB BUCKLED AT FS 605.00, LBL9. REPLACED THE WEB IAW SRM 51-42-021.
OTBD AND INBD ATTACH ANGLES CRACKED AT BS 280, STRINGER 3L. REPLACED INBD AND OTBD ATTACH ANGLES IAW IAW SRM 51-42-06, AND 51-42-21.
RIGHT INBD FLAP UPPER SKIN IS DENTED ON INBD END. REPAIRED THE RT INBD FLAP UPPER SKIN DENTED IAW SRM 57-52-00, REPAIR 3.
CABIN FLOORBEAM CORRODED AT FS 280.00 BETWEEN RBL 12 AND LBL 12. REPLACED THE FLOORBEAM IAW REO 601R-53-11-136 REV-A.
RIGHT SEAT TRACK NR 1CORRODED FROM BS 364 TO 397, RBL 9. REMOVED AND REPLACED THE SEAT TRACK IAW CRJ200 AMM 53-01-11.
LEFT SEAT TRACK CORRODED AT BS 364 TO 397, LBL 9. REPLACED THE SEAT TRACK IAW AMM 53-01-11.
DURING FLIGHT, APU DID NOT START ON FIRST ATTEMPT, STARTED ON SECOND ATTEMPT. AFTER TRANSFER OF 10TH STAGE BLEED THERE WAS A STRONG FUEL AND FUMES ODOR. SHUTDOWN APU, ODOR CLEARED AFTER SEVERAL MINUTES.
RECEIVED FLAP FAIL CAUTION MSG IN CRUISE FLIGHT. EICAS SHOWS FLAPS FAILED AT 0 DEGREES. C/W CIRCUIT BREAKER RESET IAW SUPPORT 98-018G, MSG DID NOT CLEAR.
SERVICE DOOR WILL NOT OPEN FROM INSIDE OR OUTSIDE. OUTER HANDLE WILL NOT DEPLOY, MEL'D ON 299684/4.
WING OVERHEAT WARNING ON TAKEOFF ROLL. ABORTED TAKEOFF AT 110 KTS. MAX BTMS READS 4545, ACARS REPORTS LT WING DUCT OVERHEAT. WING & COWL ANTI-ICE WERE ON & MSG CLEARED AFTER THROTTLES RETARDED. COMPLIED WITH CM ACTION PLACARDED & PLACED ON MEL. R & R LT 14TH STAGE MODULATING VLV IAW AMM 30-12-04. OPERATIONS CHECKED GOOD, REMOVED PLACARD & FROM MEL.
AT FL190, RECEIVED PAX DOOR RED WARNING MSG, ACCOMPANIED BY INCREASED NOISE FROM MAIN PAX DOOR. COMPLIED WITH QRH, PRESS NORMAL, WITNESS MARKS ARE ALIGNED BUT LOCK INDICATOR SHOWS UNSAFE. TROUBLE SHOT DOOR IAW AMM 52-11-00. ADJUSTED LOCK INDICATOR, LUBED LATCHES, CHECKED FOR CODES, NOTE NOTED. PERFORMED BITE TEST, NO DEFECTS NOTED AT THIS TIME. INSPECTED DOOR TO FUSELAGE HARNESS, NO DEFECTS NOTED.
AT APROX 90 KTS ON TAKEOFF ROLL RECEIVED A SINGLE CHANNEL ANTI-SKID MSG, MSG WENT AWAY ONCE AIRBORNE.
RIGHT FLOOR SILL UPPER SURFACE IN CARGO AREA HAS CORROSION AT MULTIPLE LOCATIONS.
PAX DOOR EXTERNAL HANDLE IS CRACKED.
RIGHT BOOST PUMP CANISTER DRAIN VLV AFT ATTACHMENT HOLE HAS NDT DEFECT INDICATION OVER 90%.
CREW ESCAPE HATCH LT & RT HINGE CUT OUTS FRAME ON CRACK.
PAX DOOR LOWER SILL & FLOORBOARD ANGLE CORRODED.
GND RECEPTACLE MOUNT BRACKET CRACKED AT SCREW HOLES.
LBL 27 FLOORBEAM IN CARGO AREA HAS CORROSION AT TOP AT MULTIPLE LOCATIONS FROM FS 559+112 TO 621.00.
PAX DOOR AFT DRAG ANGLE IS CRACKED BY POWER ASSIST MOTOR.
ANGLE CRACKED ON RT WING LE ABOVE TRANSITION DUCT.
PAX DOOR INNER HANDLE CRACKED AT KNOB.
PAX DOOR AFT CAM FITTING CHAFED.
AVIONICS COMPONENTS SUPPORT PLATES BELOW THE LT & RT FLIGHT DECK ARE CRACKED.
NUTPLATES FOR ADF ANTENNA CORRODED.
PAX DOOR AFT ANCHOR FITTING COVER PLATE IS CRACKED.
LT ENG UPPER CORE COWL INBD FWD EDGE GOUGED & CRACKED.
PAX DOOR FWD & AFT CLEATS ARE CORRODED.
FS 409+128 & RBL 9 VERTICAL POST CRACKED AT OTBD LOWER RADIUS.
FS 409+128 & LBL 18.00 VERTICAL POST IS CRACKED AT LOWER RADIUS.
THREE EACH CARGO TIE DOWNS AT LBL 27 FLOORBEAM FROM FS 559+96 TO 574.00 HAVE CORROSION.
FLOOR SUPPORT STRUCTURE CLIP AT FS 484.00, RBL 27 IS CRACKED AT UPPER RADIUS.
LT WINDSHIELD SIDE SUPPORT AFT BRACKET AT WINDOW SILL LEVEL IS CRACKED.
LEFT WING FWD FACE OF FWD SPAR, INBD MOUNTING BRACKET FOR LE PANEL 530 JL, HAS A CRACK ON UPPER END.
HYD LINE SUPPORT BRACKET CRACKED IN RT WW JUST FWD OF BRAKE PRESS TRANSDUCER.
FS 621.00 BULKHEAD INTERCOSTAL AT STRINGER 14R IS CRACKED.
IN FLIGHT ELEVATOR CONTROL INCREASE INPUTS NEEDED FOR ELEVATOR MOVEMENT, ELEVATOR FEELS HEAVY ON TAXI IN.
EMERGENCY EXIT SIGN AT SERVICE DOOR & AT CEILING AT ROW 8 INTERMITTENTLY FLASHING ON & OFF.
CANX LAVATORY SMOKE DETECTOR GOING OFF AT GATE RT PACK SPIKED AT 120 DEGREES.
CARGO BAY DOOR HANDLE HOUSING CRACKED. R & R CARGO DOOR HANDLE HOUSING.
CARGO DOOR THRESHOLD SILL HAS TWO CRACKS AT FS 589 - 605 FROM EDGE TO FASTENER HOLES. REPAIRED SILL IAW REO 601R-53-61-433, REV C.
FLOORBEAM BS 280 RBL 9 OTBD ANGLE IS CRACKED. R & R ANGLE IAW SRM 51-42-26.
RT SIDE SEAT TRACK CORRODED BS 559. BLENDED & RESTORED FINISH IAW REO 601R-53-00-533.
RT SIDE SEAT TRACK CORRODED. BLENDED & RESTORED FINISH IAW REO 601R-53-00-533.
RT SIDE SEAT TRACK CORRODED. BLENDED & RESTORED FINISH IAW REO 601R-53-00-533.
LT SIDE SEAT RAIL CORRODED. BLENDED & RESTORED FINISH IAW REO 601R-53-00-533.
LT SIDE SEAT TRACK CORRODED BS 559+13 TO +26. BLENDED & RESTORED FINISH IAW REO 601R-53-00-533.
RT WALL SEAT TRACK CORRODED. BLENDED & RESTORED FINISH IAW REO 601R-53-00-533.
LT SIDE SEAT TRACK CORRODED. BLEND & RESTORE FINISH IAW REO 601R-53-00-533.
LEFT WALL SEAT TRACK CORRODED. BLENDED & RESTORED FINISH IAW REO 601R-53-00-533.
CORROSION AT FASTENER HOLE LOCATIONS ENTIRE LENGTH OF FLOOR SUPPORT CAP FS 569 - 621, LBL27. REMOVED, DUPLICATED AND INSTALLED REPLACEMENT FLOOR SUPPORT CAP SRM 51-45-00, 51-42-15, 51-25-06, 51-25-11, 51-40-11, 51-41-00, 51-42-06, 51-42-22,51-42-34, AND REO 601R-53-61-3778, REV A.
LEFT WING CENTER TRANSITION DUCT BRACKET IS CRACKED. R & R CRACKED ANGLE AND INSTALLED NEW SERVICEABLE ANGLE, PN 601R120371-27.
SERVICE DOOR THRESHOLD FRAME IS CORRODED IN SEVERAL PLACES. REMOVED CORRODED THRESHOLD FRAME AND REPLACE WITH NEW THRESHOLD FRAME.
RIGHT EXHAUST NOZZLE FAIRING IS CRACKED BY PANEL 446BR. REPAIRED EXHAUST NOZZLE FAIRING IAW REO 601R-78-11-4006, REV C.
ANGLE IS CRACKED AT FS 589, REMOVED & REPLACED.
LT MLG WHEEL WELL DRAG ANGLE COMMON TO INBD BATT RIB IS CRACKED. R & R IAW SRM.
FUSELAGE SKIN DAMAGED BETWEEN FS605 AND FS621 BETWEEN STRINGERS 21-22R. REPAIRED SKIN IAW REO 601R-53-61-4922.
RIGHT MLG WHEEL WELL DRAG ANGLE COMMON TO INBD BATT RIB IS CRACKED. R & R IAW SRM.
RIGHT LOWER CORE COWL HAS GOUGE ON THE SECOND STIFFENER FROM T/E. BLENDED OUT GOUGES IAW CMM 20-12-00.
SKIN AT BS 409 S24-25L DENTED. COMPLIED WITH PERMANENT REPAIR IAW REO 601R-53-31-795.
CORROSION BEYOND LIMITS ON SEAT TRACK FROM FS 559-559+80, RBL 9. R & R IAW AMM 53-01-11.
CRACKED OBLIQUE ANGLE LT UPPER AT FS 621. R & R LT UPPER OBLIQUE ANGLE IAW SRM 51-40-11 & SRM 51-42-21.
RT JET PIPE FIRE LOOP COVER ASSY CRACKED, . REMOVED CRACKED FIRE LOOP COVER ASSY. INSTALLED SERVICEABLE FIRE LOOP COVER ASSY.
RT NR 2 HYD MANIFOLD SUPPORT BRACKET IS CRACKED. REMOVED DAMAGE AND INSTALLED FABRICATED ANGLE.
LT INBD FLAP VANE L/E AT 60.005 CHAFED. FOUND TO BE OUT OF LIMITS. R & R L/E SKIN IAW SRM 51-40-11 & SRM 51-42-13.
CARGO TRACK AT FS 559+95, RBL 9 IS CORRODED. REMOVED CORRODED CARGO TRACK, FABRICATED & INSTALLED NEW CARGO TRACK.
CARGO TRACK AT FS 574 - 615, LBL 9 ARE CORRODED. R & R WITH NEW SERVICEABLE.
CARGO TRACK AT BS 564, LBL 9 ARE CORRODED AT FASTENER LOCATORS. R & R WITH DUPLICATED TRACKS.
RT WHEEL WELL THE RT BRAKE TRANSDUCER MOUNT BRACKET IS CRACKED, R & R.
ON TAKEOFF CAPT AIRSPEED IND 80 KNOTS, F/O IND 60 KNOTS ABORTED TAKEOFF. PURGED MAIN PITOT STATIC SYSTEM, RAN PITOT STATIC LEAK CHECK. OPS CHECK GOOD IAW 34-11-00.
ON TAKE OFF ROLL, RECEIVED IDG 1 CAUTION MESSAGE. SERVICED NR 1 IDG WITH 11 PUMPS IAW AMM 12-23-01. RAN NR 1 ENGINE. OPS CHECKED GOOD.
AILERON TRIM MOVES LT AND RT UNCOMMANDED WITH A/P ON OR OFF 3-5 DEGREES EACH WAY. R & R AILERON CONTROL PANEL IAW AMM 27-12-10. OPS CK NORMAL.
GEAR DISAGREE WARNING AFTER TAKE OFF. NR 1 AND 2 HYD NORMAL, NR 3 HYD HAD 90 PERCENT AND 3200 PSI. LOUD THUMPING AND SHAKING. ALL RETURNED TO NORMAL ONCE GEAR DOWN IAW QRH. R & R LANDING GEAR PRIORITY VALVE.
FS 202.75 HAS CRACK IN BULKHEAD AT PARKING BRAKE CABLE. REPAIRED BULKHEAD AT FS 202.75 IAW REO 601R-53-11-563, REV A.
SERVICE DOOR OUTER HANDLE CUTOUT GOUGED. REPAIRED SERVICE DOOR OUTER HANDLE CUTOUT IAW REO 601R-52-41-184.
RT TOP FLOOR SILL AFT OF 9G HAS CORROSION. BLENDED CORRODED AREAS ON RT FLOOR SILL AFT OF 9G IAW REO 601R-53-51-158.
BATTERY RIB CRACKED IN RT MLG W/W. WORKED REPAIR IAW REO 601R-57-51-540.
LT WING PANEL C/O 550AB HAS INDICATION OF CORROSION INBD. WORKED IAW EO E06/012/457 & REO 601R-57-21-030.
CENTER VERTICAL STIFFENER ON AFT SIDE OF APB GOUGED AND CHAFED BY ISOLATION GAUGE. BLENDED DAMAGED AREA, PERFORMED LPI, ALODINED, PRIMED, AND TOP COATED IAW REO 601R-53-61-4129.
RT LOWER CORE COWL INNER SKIN GOUGED. REPAIRED GOUGE IAW CMM 71-12-01 AND REO 601R-71-12-4073.
RT OBLIQUE ANGLE IS CRACKED. REMOVED UNSERVICEABLE RT OBLIQUE ANGLE AND INSTALLED SERVICEABLE RT OBLIQUE ANGLE PN 601-35012-52 IAW SRM 51-42-06, 51-40-11, 51-42-21, 51-23-00, 51-25-16 AND REO 601R-53-61-985.
FS 484.0 CLIP CRACKED LBL 27.0. R & R CLIP IAW REO 601R-53-41-059.
RT INBD (FLAP) VANE WHERE IT CONTACTS RUBBER STOPS. BLENDED CHAFED AREA IAW REO 601R-57-52-004 ALSO NDT.
LT INBD VANE (FLAP) WHERE IT CONTACTS RUBBER STOPS. BLENDED CHAFED AREA IAW REO 601R-57-52-004, ALSO NDT.
FOUND 5 AREAS OF MINOR TO SEMI-MODERATE CHAFING ON RT AILERON UPPER SKIN L/E BLENDED AND SMOOTHED. ALL SERVICEABLE CHAFING AREAS IAW REO 57-60-013 RETURNED FINISH TO A023.
LT AILERON UPPER AND LOWER L/E HAS CHAFE MARKS. BLENDED GOUGES, TREATED AND RESTORED FINISH IAW REO 601R-57-60-020, 601R-57-60-013.
AFTER TAKEOFF, GEN 1 CAUTION MESSAGE CAME ON WITH RESET CAUTION MESSAGE WENT OUT REQUEST INSPECTION GEN 1 (GEN 2 ON MEL). R & R GEN NR 1 IAW AMM 24-11-01, OPS CHECKS GOOD, LEAK CK GOOD.
REPAIR FUSELAGE SKIN LIGHTNING DAMAGE SITE NR 8, 0.018 INCHES DEEP X 0.075 DIA LOCATED .021 INCHES BELOW STR 24L AND 4.179 INCHES OF FS 409+32. FUSLAGE SKIN LIGHTNING AT STR 24L TO FS 409.32. REPAIRED IAW REO 601R-53-31-675. (K)
CORROSION ON FLOOR SUPPORT AT FS 574-621 LB 27 AROUND NUT PLATE HOLES. CORROSION ON FLOOR SUPPORT BTWN FS 574-621, LBL 27 REPAIRED IAW REO 601R53-61-3313. (K)
LOWER CAP ANGLE ON PRESSURE BULKHEAD FS 559, RT SIDE CRACKED. LOWER CAP ANGLE PRESSURE BULKHEAD FS 559, RT SIDE REPAIRED IAW REO 601R-53-41-1045, 601R-53-41-1045, REV, 601R-53-41-260, REV C. (K)
AFT PRESSURE BULKHEAD WEB IS CRACKED. AFT PRESSURE BULKHEAD WEB REPAIRED IAW REO 601R-53-61-1541, REV B. (K)
PASSENGER DOOR EDGE MEMBER CRACKED ON THE AFT SIDE PASSENGER DOOR EDGE MEMBER REPAIRED IAW SRM 51-42-13 AND 51-24-16. (K)
CROSSBEAM WEB FS 280.00, BTW RBL 9 TO LBL 9WL 72.00 IS CORRODED. CROSSBEAM WEB FS 280.00 BTW RBL 9 TO LBL 9.00, WL 72.00. REPAIRED IAW REO 601R-53-11-926, REV B. (K)
AFT PRESSURE BULKHEAD WEB AT FS 621, LBL 36.2 AND WL 111 CRACKED. AFT PRESSURE BULKHEAD BEB AT FS 621, LBL 36.2 AND WL 111 REPAIRED IAW REO 601R-53-61-3306. (K)
FS 621 AFT SIDE OF REAR PRESSURE BULKHEAD, LT STR 14 CLIP CRACKED. CLIP FABRICATED AND REPLACED AT FS 621 AFT SIDE OF REAR PRESSURE BULKHEAD, LT SIDE STR 14 IAW REO 601R-53-61-100, REV A. (K)
UNDER FLOOR FS 484, RBL 27 CLIP CRACKED. UNDER FLOOR FS 484, RBL 27 CLIP, REPLACED IAW SRM 51-21-42. (K)
PASSENGER DOOR STAIR AFT DRAG ANGLE CRACKED. AFT DRAG ANGLE REPAIR CARRIED OUT IAW REO 601R-52-11-513. (K)
UNDER FLOOR FS 484.00 LBL 36 CLIP CRACKED. UNDER FLOOR CLIP AT FS 484.00, LBL 36 REPAIRED IAW REO 601R-53-41-059, REV A. (K)
UNDER FLOOR FS484, RBL 36 CLIP CRACKED. UNDER FLOOR FS 484, RBL 36 CLIP REPAIRED IAW REO 601R-53-41-059, REV A. (K)
MWC 136498-2 - AFT PRESSURE BLKHD WEB AT FS 621 AT THE LINTEL ASSY INSTALLATION IS CRACKED. REPAIR ON AFT PRESSURE BULKHEAD WEB AT F/S 621.00 AT THE LINTEL ASSY INSTL. PERFORMED IAW REO 601R-53-61-1230, REV D. (K)
TRU 1 FAN INOPERATIVE. (M)
FS 589 TO FS 621 WL 73.50 LBL 27 FLOOR SUPPORT CORRODED. FLOOR SUPPORT CORROSION REMOVED IAW SRM 51-21-06. (M)
SKIN UNDER PAX DOOR AFT DRAG ANGLE IS CRACKED AT 3RD FASTENER DOWN APPROX .5 INCH LONG. (K) MAINTENANCE REPAIRED AFT DRAG ANGLE IAW EO 601R-52-12354. (M)
AFT PAX DOOR DRAG ANGLE (PN 601R31772-5) IS CRACKED AT PREVIOUS REPAIR APPROX .5 INCH LONG. (K) MAINTENANCE REMOVED AND REPLACED DRAG ANGLE ON AFT PAX DOOR IAW REO 601R-52-11-513. (M)
CREW ESCAPE HATCH EXTERNAL HANDLE WILL NOT DEPLOY. CLEANED AND LUBRICATED HANDLE IAW CRJ200 AMM 12-20-52-640-803. OPERATES NORMAL. (M)
HYDRAULIC PRESSURE TRANSDUCER BRACKET (PN 601R75262-157) CRACKED APPROX .2 INCH LONG IN RT MLG WHEEL WELL CEILING. (K) MAINTENANCE REMOVED DAMAGED BRACKET AND INSTALLED SERVICEABLE BRACKET IAW CRJ 200 SRM 51-42-06. (M)
HYDRAULIC LINE Z-BRACKET (PN 601R75262-153) CRACKED APPROX .1 INCH LONG IN RT MLG WHEEL WELL CEILING. (K) MAINTENANCE REMOVED DAMAGED BRACKET AND INSTALLED SERVICEABLE BRACKET IAW CRJ 200 SRM 51-42-06. (M)
PASSENGER DOOR ASSIST MOTOR MOUNT BRACKET (PN 601R317743-7) CRACKED APPROX .2 INCH LONG AT BOTTOM OF BRACKET. (K) MAINTENANCE REMOVED AND REPLACED BRACKET IAW CRJ200 SRM 51-42-06. (M)
CARGO DOOR FWD ROLLER TRACK U-CHANNEL (PN 601R35050-25) CRACKED APPROX .2 INCH LONG AT BOTTOM OF TRACK. (K) MAINTENANCE REMOVED AND REPLACED U-CHANNEL IAW CRJ 200 SRM 51-42-06. (M)
HYDRAULIC PRESSURE TRANSDUCER BRACKET (PN 601R75262-159) CRACKED APPROX .2 INCH LONG IN LT MLG WHEEL WELL CEILING. (K) MAINTENANCE REMOVED AND REPLACED BRACKET IAW CRJ 200 SRM 51-42-13. (M)
FS 409.0+128 VERTICAL BEAM AT RBL 27 CRACKED APPROX.2 INCH LONG ON IB SIDE AT BOTTOM RIVET. (K) MAINTENANCE REMOVED DAMAGE FABRICATED AND INSTALLED REPAIR PARTS IAW BOMBARDIER REO 601R-53-41-056 REV E AND BSC EO 601R-53-12516. (M)
FLOOR EDGE MEMBER CRACKED AT FS 574.00. (K) MAINTENANCE REMOVED AND REPLACED DAMAGED PART IAW REO 601R-53-61-1574. (M)
LT FS 484 FLOOR SUPPORT INTERCOSTAL ANGLE AT LBL 27 CRACKED APPROX .2 INCH LONG. (K) MAINTENANCE REPAIRED FS 484, LBL 27 ANGLE IAW BOMBARDIER STANDARD REPAIR 601R-53-0029B. (M)
FLOOR EDGE MEMBER CRACKED AT FS 589.00. (K) MAINTENANCE REMOVED DAMAGED AND INSTALLED REPAIR IAW REO 601R-53-61-1574 REV A. (M)
RT FS 484 FLOOR SUPPORT INTERCOSTAL ANGLE AT RBL 27 CRACKED APPROX .2 INCH LONG. (K) MAINTENANCE REMOVED AND REPLACED ANGLE IAW CRJ 200 SRM 51-42-06 AND 51-42-21. (M)
RT FS 484 FLOOR SUPPORT INTERCOSTAL AT RBL 36 CRACKED APPROX .2 INCH LONG. MAINTENANCE REPAIRED IAW REO 601R-53-41-059 AND EO 601R-53-003A. (M)
RT FS 460 FLOOR SUPPORT FITTING (PN 600-31068) AT OB SIDE OF RBL 9 CRACKED APPROX 1.5 INCHES LONG. (K) MAINTENANCE REMOVED AND REPLACED FITTING P/N 600-31068-19 IAW CRJ 200 SRM 51-42-13, 51-42-21, AND 51-23-00. (M)
FOUND FS 280 RBL 9 INBOARD CLIP, P/N 601R31113-58 IS CRACKED. MAINTENANCE REMOVED AND REPLACED ANGLE IAW CRJ 200 SRM 51-42-13 ABD BSC SR 601R-53-0057A. (M)
FS 280 RBL 9 CLIP P/N 601R31113-58 (OUTBD) IS CRACKED .25 INCH. MAINTENANCE REMOVED AND REPLACED ANGLE IAW CRJ 200 SRM 51-42-13 AND BSC SR 601R-53-0057A. (M)
LT FS 484 FLOOR SUPPORT INTERCOSTAL AT LBL 36 CRACKED APPROX .2 INCH LONG. MAINTENANCE REMOVED FLANGE FABRICATED AND INSTALLED ANGLE IAW BSC SR 601R-53-0030A AND BOMBARDIER REO 601R-53-41-059 REV A. (M)
RT FS 621-FS 625 INTERCOSTAL ANGLE (PN 601-35012-52) CRACKED APPROX .2 INCH LONG IN AFT EQUIPMENT BAY. (K) MAINTENANCE REMOVED AND REPLACED ANGLE IAW CRJ 200 SRM 51-42-06, 51-42-21 AND BOMBARDIER REO 601R-53-61-422 REV NC. (M)
LT FS 621- 625 INTERCOSTAL ANGLE (PN 601-35012-51) CRACKED APPROX .3 INCH LONG IN AFT EQUIPMENT BAY. (K) MAINTENANCE REMOVED AND REPLACED ANGLE IAW CRJ 200 SRM 51-42-06, 51-42-21 AND BOMBARDIER REO 601R-53-61-422 REV C. (M)
RT NOSE SKIN PANEL PN 600-33052-141 IS DENTED 3 INCHES LONG BY 2 INCHES WIDE BY 0.100 DEEP BETWEEN FS 169.00 AND FS 174.00. S/D - MAINTENANCE REMOVED AND REPLACED SKIN PANEL P/N 600-33052-141 BETWEEN FS 169.00 AND 174 IAW CRJ 200 SRM 51-42-06. (K)
RT NOSE SKIN PANEL PN 600-33010-27 IS DENTED 5 INCH LONG X 4 INCHES WIDE X 0.125 INCHES DEEP FROM FS 169.00 TO FS 193.00. S/D - MAINTENANCE REMOVED AND REPLACED SKIN PANEL P/N 600-33010-27, IAW CRJ 200 SRM 51-42-06 AND BSC EO 601R-53-11942. (K)
STAB TRIM AND MACH TRIM CAUTION INFLIGHT NEITHER CHANNEL 1 AND 2 WOULD RE-ENGAGE COMPLIED WITH QRH. REMOVED AND REPLACED STAB TRIM AND MACH TRIM CONTROL PANEL IAW CRJ AMM 27-41-25, OPS CHECK GOOD. (M)
SHORTLY AFTER TAKEOFF, ENGINE NR 2 FAN VIBE WENT TO 3.3 TWO, YELLOW RANGE. COMPLIED WITH QRH, ENGINE WAS SHUTDOWN AND AIRCRAFT RETURNED TO ELM. CLEANED INLET AREA, REPLACED BLADES 1, 2, 4, 5, 6, 14, 16, 18, 19, 29 AND REPLACED SPACER ON STATOR ASCEND AT 10 O`CLOCK COMPRESSOR DAMAGE VTR .3 ON TAKEOFF AIRCRAFT RETURNED TO SERVICE. (M)
ANTI-ICE DUCT WARNING CASS IN FLIGHT RIGHT WING INDICATED RED ON SYNOPTIC PAGE. COMPLIED QRH, WARNING EXTINGUISHED. REMOVED AND REPLACED RIGHT BLEED LEAK CONTROL UNIT IAW 36-31-10. PERFORMED OPS CHECK OF ANTI-ICE CONTROL AND INDICATION, OPS CHECK GOOD IAW 30-30-00. (M)
(TIRE BLOWN OUT ON LANDING) LT IB TIRE NEEDS TO BE REPLACED. THRUST REVERSER USED IAW FOM BRAKE TEMPS AND GATE WAS 4,1,4,4. REMOVED AND REPLACED MLG NR2 WHEEL ASSEMBLY IAW AMM. (K)
STAB TRIM AND MACH TRIM MESSAGE APPEARED DURING CLIMB. COMPLIED WITH QRH, MESSAGE PERSISTED. REMOVED AND REPLACED HSTCU PN 7060-9, IAW AMM. OPS CHECK GOOD.
CONFIG SPOILER MESSAGE ON TAKEOFF. ABORTED TAKEOFF AT 120 KNOTS. BRAKE TEMPS 5, 6 AND 7. AIRCRAFT WEIGHT 50,900 LBS. ADJUSTED GAP ON LEFT INBOARD GROUND SPOILER NR 4 TO WITHIN LIMITS IAW AMM 27-60-00-220-801. (M)
DURING TAKEOFF ROLL 70 KNOTS IDG NR FAIL, GEN NR 2 OFF APPEARED MODERATE BREAKING BTMS READOUT 4, 5,6,7 FOUND NR 2 IDG OIL LEVEL LOW SERVICED NR 2 IDG RAN ENGINE NO LEAKS NOTED OPS CHECK GOOD IAW MM. PERFORMED RTO INSPECTION. (K)
HORIZONTAL STABILIZER FORWARD STEADY FITTING HAS 3 LOOSE MOUNT BOLTS ON LT SIDE OF FITTING. REMOVED BOLTS, VISUALLY INSPECTED HARDWARE AND HOLES, REINSTALLED BOLTS AND TORQUED IAW AMM. (K)
PASSENGER DOOR STAIR AFT DRAG ANGLE IS CRACKED, .5 INCH LONG IN RADIUS (ADJACENT TO MOUNT FOR PASSENGER DOR ASSIST CABLE PULLEY). REMOVED DAMAGED SECTION OF ANGLE, FABRICATED REPAIR ANGLE AND INSTALLED ANGLE IAW REO. (K)
NESTED ANGLE ON FWD WEB OF ENGINE BEAM HAS A DEEP GOUGE IN RADIUS APPROX .300 INCH LONG X .075 INCH WIDE AND .050 DEEP. REMOVED DAMAGED SECTION OF NESTING ANGLE. FABRICATED AND INSTALLED REPAIR PARTS IAW EO. (K)
RT WING LOWER PLANK FUEL TANK ACCESS DOOR CUTOUT FOR PANEL 640BB HAS FRETTING DAMAGE. 2 INCH LONG X .125 INCH WIDE. REPAIRED BY BLENDING AND TREATING DAMAGED AREA IAW REO. (K)
RT LOWER WING PLANK AT WS 45, FUEL ACCESS PANEL 640BB CUT OUT, RAS FRETTING DAMAGE 2 INCH LONG X .175 INCH WIDE. (K)
FS 280, RBL 9, IB ATTACH CLIP CRACKED. REPLACED ANGLE IAW SRM AND EO. (K)
FS700, LBL 9 IB ATTACH CLIP CRACKED. REPLACED ANGLE IAW CRM AND EO. (K)
FS 280, LBL 9, IB ATTACH CLIP CRACKED. REPLACED ANGLE IAW SRM AND EO. (K)
FS 280, RBL 9, OB ATTACH CLIP CRACKED. (K) REPLACED ANGLE P/N 601R31113-58 IAW CRJ SRM 51-42-06 AND BRAS EO 601R-53-6888. (M)
FS 280, LBL 9, OB ATTACH CLIP CRACKED. (K) REPLACED ANGLE P/N 601R31113-58 IAW CRJ CRM 51-42-06 AND BRAS EO 601R-53-6888. (M)
PROTRUDING DENT AT FS 679, BETWEEN STR 23 AND STR 24, RT MEASURES .5 INCH X .020 INCH DEEP. PERFORMED REPAIR TO FUSELAGE SKIN FROM FS 672 TO 682 BETWEEN STRING STR 23 AND 24 BY CUTTING OUT DAMAGED AREA, PERFORMED NDT OF CUT LINE FAB AND DOUBLER AND INSTALLED IAW SRM. (K)
RT FS 625, OBLIQUE ANGLE IS CRACKED. REMOVED CRACKED OBLIQUE ANGLE AND REPLACED WITH NOW IAW SRM. (K)
WO 84084, MWC 131, RT SIDE UNDERFLOOR SUPPORT STRUCTURE IS CRACKED 1.0 INCH AT FS 621, RBL 40, WL 73. REPAIRED BY REMOVING DAMAGED SECTION OF ANGLE, FABRICATING AND INSTALLING REPAIR ANGLES IAW REO. (K)
ABORTED TAKEOFF DUE TO CONFIG TRIM WARNING. ABORTED AT 60 KNOTS, RUDDER IN GREEN BAND, WILL TRAVEL TO LEFT BUT NOT TO THE RIGHT. REMOVED AND REPLACED RUDDER TRIM CONTROL PANEL, IAW AMM 27-10-01, OPS CHECK GOOD. (M)
FLOOR ANGLE AT FS 621, LEFT SIDE, NEXT TO CARGO DOOR IS CRACKED. REPAIR IAW BOMBARDIER REO 601R-53-61-117. SEALED AND PAINTED IAW BOMBARDIER REO 601-53-61-117. PRESSURIZED AIRCRAFT IAW AMM 21-32-00-863-801. NO LEAKS NOTED. (M)
AFTER ROTATION SMELLED SOMETHING HOT, APU EGT ABOVE RED LINE, APU SHUTDOWN AND TRANSFERRED BLEEDS TO ENGINE. SMOKEY ODOR DISAPPEARED. REMOVED APU SEIZED. REMOVED AND REPLACED APU. NO FURTHER INCIDENT. (M)