N465AW
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
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
RECEIVED GEAR DISAGREE WARNING MSG AFTER T/OFF CLIMBING THRU 5000'. MSG CLEARED AFTER A COUPLE SECONDS. GEAR WAS ALREADY UP/LOCKED WHEN MSG CAME ON. GEAR AND FLAP INDICATORS CAME ON BRIEFLY FOR APPROX 5 MINS AFTER GEAR DISAGREE MSG WARNING MSG MESSAGE. RECEIVED NO OTHER ASSOCIATED MSG'S. ACFT REMOVED FROM SERVICE. PERFORMED GVI OF GEAR, NO DISCREPANCIES FOUND. C/W M ACTION OF MEL 32-30-01, GEAR PINS INSTALLED FLAGS REMOVED. PERFORMED BITE CHECK OF PSEU IAW AMM 32-61-01. RECORDED FAULT CODE S21SHORT. REF 366179-4 AND 366180-1 FOR MEL'S. COLTON LOBITZ A/P 3849387 R&R PROX SENSOR PS1GA IAW AMM 32-61-05. OPS CHECK GOOD. PLACARD REMOVED. THIS CLEARS MEL
INFIGHTING REC'D "R COWL A/I" CAUTION WITH SWITCH SELECTED OFF. FOUND R COWL PRV POPPED ON POST FLIGHT. AIRCRAFT REMOVED FROM SERVICE R&R RH COWL PRESSURE RELIEF VALVE REF 30-2204. OPS CHECK GOOD
UPON DEPARTURE AND CLIMB OUT OF KDAY FLAP FAILED WITH INDICATION OF 0. CREW HAS ELECTED TO FLY ONTO KORD. CREW HAS DECLARED AN EMERGENCY FOR FLAP FAILURE. CREW IS SCHEDULED TO ARRIVE AT KORD AT 0838 CENTRAL TIME. AIRCRAFT REMOVED FROM SERVICE. R&R L BPSU IAW AMM 27-51-10 UP TO AND INCLUDING FLAP RIG. REF LP 353430-1 FOR FLEX SHAFT SAFETY AND PANEL INSTALLATION AND OPS CHECK DUE.
RECEIVED FLAP FAIL MESSAGE BEFORE DESCENT. AIRCRAFT REMOVED FROM SERVICE. T/S PER FIM 27-50 FIG 108, FECU #1 MOST PROBABLE FAULT #12 PRESENT. REPLACED THE FECU PER AMM 27-51-05, OPS CHECK GOOD. REMOVED PLACARD/MEL.
GEAR DISAGREE ON TAKE-OFF. WARNING MESSAGE APPEARED WITHIN 5 SECS OF SELECTION. NLG DID NOT MOVE. MLG RETRACTED NORMALLY. NOSE DOOR OPEN MESSAGE ALSO APPEARED. C/W QRH. RECEIVED THREE GREEN DOWN AND LOCKED. LANDING AT 46,500 LBS. BELOW LANDING WEIGHT. AIRCRAFT REMOVED FROM SERVICE. R & R NLG PROX SENSOR BRACKET. OPS CHECK GOOD.
AFT PRESSURE BULKHEAD FS621 IS MISSING ALL REINFORCEMENT ANGLES, AIRCRAFT REMOVED FROM SERVICE. INSTALLED REINFORCEMENT ANGLES TO AFT PRESSURE BULKHEAD FS621. PERFORMED HFEC WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW REO 601R-53-61-1240 REV (D).
PAX DOOR AFT PANEL DRAG ANGLE IS CRACKED AT PULLEY BRACKET AREA. AIRCRAFT REMOVED FROM SERVICE. REPAIRED DRAG ANGLE. PERFORMED HFEC WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW REO 601R-52-11-513 REV C.
CORROSION ON SERVICE DOOR LOWER SILL ANGLE P/N 601R38303-253 AT FS 310.0 AND RBL 43. AIRCRAFT REMOVED FROM SERVICE. REMOVED DAMAGE BY BLENDING SERVICE DOOR LOWER SILL ANGLE AT FS310.0 AND RBL 43. ORIGINAL MATERIAL THICKNESS 0.063. REMAINING THICKNESS 0.050 PERFORMED HFEC WITH NO INDICATIONS. RESTORED SURFACE FINISH. ALL WORK WITHIN LIMITS PERFORMED IAW EA AWAC-CRJ253-01941 REV A,
RIGHT HAND WING INBOARD FLAP INBOARD SIDE LOWER SKIN PN 601R4008 HAS CORROSION AND 5 GOUGES AT INBOARD WING STATION 50.498 - 79.062. ***********AIRCRAFT REMOVED FROM SERVICE**************** BLENDED OUT CORROSION IAW CRJ200 SRM 51-12-00 REV 39 AND SRM 51-21-06 REV 39. BLENDED GOUGE DAMAGES TO A SMOOTH CONTOUR. RESTORED SURFACE PROTECTIVE FINISH. ALL WORK WITHIN LIMITS PERFORMED IAW EA #: AWAC-CRJ257 - 01935 REV IR, DATED 12/19/2022. WORK PERFORMED UNDER AERSALE WORK ORDER 003813, CARD NO. 20079, TT: 39,454:52 TC: 38132.
CORROSION AND CRACK ON CABIN FLOORBEAM AT BS 621, LBL 27-43. AIRCRAFT REMOVED FROM SERVICE. BLENDED CORROSION, REMOVED AND REPLACED THE SECTION OF ANGLE. HFEC PERFORMED WITH NO INDICATIONS IAW NDT 51-20-06 REV 44 PART 1. RESTORED SURFACE FINISH. WORK WITHIN LIMITS WAS PERFORMED IAW SRM 53-00-00, REV 39, SRM 51-21-06, REV 39, SRM 53-61-43, REV 39, SRM 51-11-00, REV 39, SRM 51-21-11, REV 39, AND SRM 51-40-11. REV 39.
CORROSION ON CABIN FLOOR STRUCTURE SUPPORT P/N 601R38672-1 AT FS349.0 AND RBL19.0 TO RBL21. REMOVED CORROSION BY BLENDING CABIN FLOOR STRUCTURE SUPPORT. PERFORMED HFEC WITH NO INDICATIONS. RESTORED SURFACE PROTECTIVE FINISH. ALL WORK WITHIN LIMITS PERFORMED IAW ASAP EA CRJ253-01940 REV A,
LH WINGLET ATTACH STRUCTURE HAS ONE ELONGATED HOLE ON RIB AT WS404.08. REPAIRED LH WINGLET ATTACH STRUCTURE BY REPLACING RIB P AT WS404.08 AND WGLT3.25. INSTALLED FREEZE PLUG AND COUNTERBORED FREEZE PLUG. HFEC PERFORMED WITH NO INDICATIONS. RESTORED SURFACE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW REO 601R-57-31-1411 REV-.
CORROSION ON CABIN FLOOR STRUCTURE CROSSBEAM AT FS349.0 AND RBL19.0 TO RBL24. REMOVED CORROSION BY BLENDING CABIN FLOOR STRUCTURE CROSSBEAM P/N 601R32005-149 AT FS349.0 AND RBL19.0 TO RBL24. FABRICATED STRAP FROM 0.050ÿ½ ALUM. SHEET MATERIAL HEAT TREATED TO 7075-T6. STRAP DIMENSIONS L= 7.50ÿ½ X W= 0.080ÿ½. PERFORMED HFEC WITH NO INDICATIONS. RESTORED SURFACE PROTECTIVE FINISH. ALL WORK WITHIN LIMITS PERFORMED IAW ASAP EA #: AWAC-CRJ253-01938 REV IR,
CORROSION ON RT SEAT TRACK FROM BS 559 - 559+84, RBL 9. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION, PERFORMED HFEC WITH NO INDICATIONS IAW NDTM 51-20-06 PART 1, REV 44. RESTORED PROTECTIVE FINISH. WORK WITHIN LIMITS IAW AMM 53-01-11 REV 66, REPLACED THE SEAT TRACK IAW SRM 53-41-49 REV 39, SRM 53-31-49 REV 39, SRM 53-21-49 REV 39, SRM 53-51-49 REV 39, SRM 53-41-02 REV 39, SRM 53-40-11 REV 39, SRM 51-21-11 REV 39, SRM 51-26-00 REV 39, SRM 51-21-06 REV 39, SRM 51-25-06 REV 39 AND SRM 51-25-116 REV 39.
CORROSION ON CABIN FLOOR STRUCTURE SUPPORT ANGLE AT SERVICE DOOR FS349 AND RBL28 TO RBL42. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED ANGLE SUPPORT ANGLE AT SERVICE DOOR FS349 AND RBL28 TO RBL42. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW SRM 53-21-15 REV 39, SRM 53-00-00 REV 39, SRM 51-42-06 REV 39, SRM 51-42-20 REV 39.
CORROSION ON LEFT WING INBOARD FLAP LOWER SKIN FROM WS50.498- WS100.009. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED DAMAGED SECTION ON LEFT WING INBOARD FLAP LOWER SKIN FROM WS50.498 WS100.009. CUTOUT DIMENSIONS L= 29.700X W= 21.250. RESTORED SURFACE PROTECTIVE FINISH. PERFORMED HFEC WITH NO INDICATIONS. ALL WORK WITHIN LIMITS PERFORMED IAW EA AWAC-CRJ257-01943 REV IR,
CORROSION ON PAX DOOR FWD ANCHOR FITTING AT BS 310, WL 75. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED ON PAX DOOR FWD ANCHOR FITTING. RESTORED PROTECTIVE FINISH. WORK WITHIN LIMITS, PERFORMED IAW AMM 52-11-17-400-804, REV 66, ADJUSTMENT IAW AMM 52-11-17-820-802, REV 66.
CORROSION ON PAX DOOR AFT ANCHOR FITTING, PLATE AND COVER AT BS 349, WL 75. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED PAX DOOR AFT ANCHOR FITTING, PLATE, AND COVER. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW AMM 52-11-17-400-804, REV 66, ADJUSTMENT IAW AMM 52-11-17-820-802, REV 66.
RIGHT WINGLET ATTACH STRUCTURE HAS ONE ELONGATED HOLE ON RIB AND STRAP AT WS404.08. REPAIRED THE RT WINGLET ATTACH STRUCTURE BY REPLACING STRAP, INSTALLED FREEZE PLUG AND COUNTERBORED FREEZE PLUG. HFEC PERFORMED WITH NO INDICATIONS. RESTORED SURFACE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW REO 601R-57-31-1410 REV -.
CORROSION ON FLOOR STRUCTURE RH STRAP, BS 559, RBL 27 - 42. REMOVED AND INSTALLED FLOOR STRUCTURE RT STRAP WITH FABRICATED STRAP . RESTORED SURFACE FINISH. PERFORMED IAW SRM 53-00-00, REV 39, SRM 53-41-43 REV 39, SRM 51-40-11 REV 39, SRM 51-42-06 REV 39, SRM 51-24-21 REV 39 AND SRM 51-42-20 REV 39.
AT 3,000-3,500 FEET RH ENGINE OIL (PSI) FLUXUATION FROM 15 PSI TO 51 PSI, EVEN AT CRUISING POWER, C/W QRH, AIR RETURN. AIRCRAFT REMOVED FROM SERVICE. UPON FURTHER INSPECTION FOUND OIL TO BE LEAKING FROM SCAVENGER OIL FILTER HOUSING. FOUND OIL FILTER HOUSING CAP TO BE MISSING AN ORING. INSTALLED ORING IN REF AMM 79-21-05. NO LEAKS NOTED. NO DEFECTS AT THIS TIME. A/C PLACED ON DAILY OIL WATCH FOR LH ENGINE. DUE TO TAKING 10 PINTS OF OIL.
CRACKED ANGLE ON PASSENGER DOOR FORWARD SIDE WALL PANEL AT 2ND STEP. FS318 PAX DOOR P/N 601R31701-1 S/N 7896 ***AIRCRAFT REMOVED FROM SERVICE*** REPLACED PASSENGER DOOR FORWARD SIDE PANEL ANGLE P/N 601R-52-11-702-10 WITH FABRICATED ANGLE, FS318. RESTORED SURFACE FINISH. ALL WORK PERFORMED IAW REO 601R-52-11-702 REV E, DATED 2016-08-14.
TWO CRACKED ANGLES ON PASSENGER DOOR AFT SIDE WALL PANEL AT 2ND STEP. FS340. PAX DOOR P/N 601R31701-1 S/N 7896 ***AIRCRAFT REMOVED FROM SERVICE*** REPLACED PASSENGER DOOR FORWARD SIDE PANEL ANGLES P/N 601R-52-11-702-7 AND 601R-52-11-702-9 WITH FABRICATED ANGLE, FS340. RESTORED SURFACE FINISH. ALL WORK PERFORMED IAW REO 601R-52-11-702 REV E, DATED 2016-08-14.
LH WINGLET HAS 3 GOUGES AT INBOARD AND OUTBOARD LOWER FORWARD STRAPS, WS389. P/N 600-15108-7 AND P/N 600-15108-18. ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED 2 GOUGES AT LH LOWER FORWARD WINGLET OUTBOARD STRAP P/N 600-15108-7. DIMENSIONS 3.200ÿ½L X 2.00ÿ½W. PERFORMED HFEC WITH NO INDICATIONS. RESTORED SURFACE FINISH. ALL WORK WITHIN LIMITS AND PERFORMED IAW ASAP EA # AWAC-CRJ257-01637 REV A DATED 5/25/2021. BLENDED 1 GOUGE AT LH LOWER FORWARD WINGLET INBOARD STRAP P/N 600-15108-18. DIMENSIONS 1.600ÿ½L X 0.400ÿ½W. PERFORMED HFEC WITH NO INDICATIONS. RESTORED SURFACE FINISH. ALL WORK WITHIN LIMITS AND PERFORMED IAW ASAP EA # AWAC-CRJ257-01638 REV A DATED 5/25/2021.
CRACKED ANGLE ON PASSENGER DOOR FORWARD LOWER SIDE WALL PANEL AT LOWER STEP. FS318 PAX DOOR P/N 601R31701-1 S/N 7896 ***AIRCRAFT REMOVED FROM SERVICE*** REPLACED PASSENGER DOOR FORWARD LOWER SIDE WALL PANEL AT LOWER STEP, ANGLE P/N 601R-52-11-702-44, SHIM P/N 601R-52-11-702-43 AND TAPERED SHIM P/N 601R52-11-702-45 WITH FABRICATED PARTS, FS318. RESTORED SURFACE FINISH. PERFORMED HFEC WITH NO INDICATIONS. ALL WORK PERFORMED IAW REO 601R-52-11-702 REV E, DATED 2016-08-14
AFT FUSELAGE SKIN DENT FS 640.00 - 2ÿ½ LH STR 26 + 2ÿ½. ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED SKIN DENT AT AFT FUSELAGE FS640.00 - 2ÿ½ LH STR 26 +2ÿ½.DAMAGE MEASURES 0.550ÿ½L X 0.500ÿ½W X 0.008ÿ½D. PERFORMED HFEC WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW ASAP EA # AWAC-CRJ253-01636 REV A DATED 5/22/2021.
AFT FUSELAGE SKIN DENT FS 640.00 - 1ÿ½ LH STR 26 + 2ÿ½. ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED SKIN DENT AT AFT FUSELAGE FS640.00 - 1ÿ½ LH STR 26 +2ÿ½. DAMAGE MEASURES 1.200ÿ½L X 0.600ÿ½W X 0.023ÿ½D. PERFORMED HFEC WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW ASAP EA # AWAC-CRJ253-01636 REV A DATED 5/22/2021.
AFT FUSELAGE SKIN GOUGE FS 589.00 + 1ÿ½ RH STR 25 + 2ÿ½. ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED SKIN GOUGE FS 589.00 + 1 RH STR 25 + 2ÿ½. DAMAGE MEASURES 1.10ÿ½ L X 0.007ÿ½ W X 0.006ÿ½ D. PERFORMED HFEC WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW ASAP EA # AWAC-CRJ253-01639 REV IR DATED 5/24/2021.
AFT FUSELAGE SKIN DENT FS682.0 + 9ÿ½ RIGHT HAND STRINGER 24 + 2ÿ½. ***AIRCRAFT REMOVED FROM SERVICE*** HAND FORMED DENT AT FS682.0 + 9ÿ½ RIGHT HAND STRINGER 24 + 2ÿ½, DIMENSION0.700ÿ½L X 0.500ÿ½W X 0.050ÿ½W. DENT FOUND TO BE OUT OF LIMITS REF CRJ200 SRM 53-00-31. HFEC PERFORMED WITH NO INDICATIONS. RESTORED SURFACE FINISH. ALL WORK PERFORMED AND WITHIN LIMITS IAW ASAP EA # AWAC-CRJ253-1635 REV IR DATED 5/21/2021.
CRACK INDICATIONS (7 TOTAL) AT FS621.00 AFT PRESSURE WEB. CRACKS AT THE FOLLOWING LOCATIONS, WL 128.5 - 131.2, LBL 18.0, CRACK LENGTH 2.7"L, WL 113.5 - 114.2, LBL 9.50, CRACK LENGTH 0.7"L, 109.5 - 112.0, BL 0.0, CRACK LENGTH 2.5"L, WL 110.5 - 111.2, RBL 9.50, CRACK LENGTH 0.7"L, WL 128.5 - 129.0, RBL 18.0, CRACK LENGTH 0.5"L, WL 110.5 - 111.8, RBL 18.0, CRACK LENGTH 1.3"L, WL 109.5 - 110.0, RBL 27.5, CRACK LENGTH 0.5"L. ***AIRCRAFT REMOVED FROM SERVICE*** REPAIRED FS621.00 AFT PRESSURE WEB, PERFORMED HFEC WITH NO INDICATIONS, RESTORED PROTECTIVE FINISHES. ALL WORK WITHIN LIMITS WAS PERFORMED IAW REO 601R-53-61-1240 REV D, DATED 2016-10-31 AND REO 601R-53-61-7648 REV INITIAL ISSUE DATES 2021-06-03.
RECIEVED A STEERING INOPERATIVE CAUTION MESSAGE AFTER RETRACTING GEAR, COMPLIED WITH QRH, MESSAGE REMAINED, RETURNED TO DEPARTURE, LANDED NORMAL USING DIFFERENTIAL BREAKING. NO HYD SYST 3 MESSAGE, NO OTHER EICAS MESSAGES, NO STEERING ON TAXI AFTER LANDING. AIRCRAFT REMOVED FROM SERVICE, TROUBLESHOT AND FOUND THE LT RVDT HARD FAILURE. R & R THE LT STEERING RVDT IAW AMM 32-51. OPS CHECKED GOOD.
NOSE GEAR WOULD NOT RETRACT AFTER T/O. EICASE SHOWED NOSE GEAR DOWN AND NOSE GEAR OPEN INDICATIONS. RAN QRH. SELECTED GEAR DOWN. GEAR EXTENDED AND NORMAL LANDING.
FOUND INDICATION AT FS 409.00+128 OTBD RBL 18 POST AFT FLANGE RADIUS APPROX .250" LONG FSH FAILS NDT.
AC GROUND POWER RECEPTACLE STRUCTURE CRACKED @ MOUNT FASTENERS.
RT WALL SEAT TRACK IS CORRODED AT FS 409+128.
INDICATION NOTED AT FS621 REAR PRESSURE BULKHEAD FWD FACE AT BL0.00, WL 131 APROX 7.5" LONG AND 53% FULL SCREEN HEIGHT FAILING NDT.
LT WALL SEAT TRACK IS CORRODED AT VF.S.409+128.
INTERCOSTAL CORRODED BETWEEN F.S.349.00 AND F.S.364.00, STRG 26L AND 27.
RT F.S.484 CLIP IS CRACKED AT RBL27.
RT WALL SEAT TRACK IS CORRODED AT F.S.513.
RT WALL SEAT TRACK IS CORRODED AT F.S.513.
LT WING OUTBOARD FLAP FIXED VANE IS CHAFED AT W.S.274.
LT SIDEWALL SEAT TRACK IS CORRODED AT FS 529.00.
FOUND INDICATIONS AT FS409+128 BL 0 LT AND RT POSTS AFT FLANGE RADIUS APPROX. .500" LONG 100% FSH BOTH FAILS NDT.
FOUND INDICATIONS AT FS 409+128 B.L.0.00 LT AND RT POSTS AFT FLANGE RADIUS APPROX. .500" LONG 100% FSH BOTH FAIL NDT.
DURING TAKEOFF, THE FLAPS FAILED AT 3 DEGREES WHEN SELECTING FLAPS FROM 0 TO 8. RAN QRH, RETURNED TO DEPARTURE, EMERGENCY WAS DECLARED. AFTER LANDING FLAPS SYSTEM WAS SUCCESSFULLY RESET IAW 98-018G.
PAX DOOR MOTOR FOUND CRACKED IN THE LOWER VERTICAL STIFFENER. REMOVED AND REPLACED THE STIFFENER IAW SRM 51-42-06, AND 51-42-13.
4182 EMERGENCY PATH LIGHTING FROM ROW 5 TO 8 INOP. FOUND PIN PULLED OUT OF ENVIRONMENTAL SPLICE AT ROW 7. R&R'D PIN IAW ESPM 20-17, FUNCTION CHECK GOOD.
4231 EMERGENCY LIGHTS ROW 5 INOP ON FLOOR. PLACARDED & PLACED ON MEL. REMOVED & REPLACED EMERGENCY LIGHT STRIP ROW 5 IAW 33-51 & AWAC SUPP 16-371A. OPS CHECK GOOD.
FRAME BS 409+16 HAS CORROSION ON THE FWD AND AFT SIDE BETWEEN STRINGERS 26R AND 26L
FRAME BS 349 HAS CORROSION ON THE FWD AND AFT SIDE BETWEEN STRINGER 26L AND 26R.
LBL 27 AFT FITTING IS CORRODED AT OTBD NUTPLATE LOCATION AT BS 618.
FRAME BS 333 CRACKED AT STRINGER 2L.
STRINGER 3L CRACKED AT BS 379.
RIGHT INTERCOSTAL BRACKET CRACKED ON THE AFT REAR PRESSURE BULKHEAD AT BS 621. REPLACED INTERCOSTAL IAW SRM 51-41-21.
FLIGHT DECK FLOORBEAM CRACKED ON THE FWD SIDE OF BS 280, RBL9. REPLACED THE FLOORBEAM ANGLE IAW SRM 51-42-06, AND 51-42-21.
SEAL RETAINER CRACKED ON PANEL 422BT. REPAIRED THE SEAL RETAINER IAW SUP 16-363.
PAX DOOR EDGE MEMBER HAS A CRACK ON FWD END. REPAIRED IAW REO 601R-52-11-279, REV NC.
AT 31,000 FEET LOST 5% N1 ON RIGHT ENGINE WITH SLIGHT YAW. LASTED 2-3 SECONDS, THEN CONDITION CORRECTED ITSELF WITH NO INPUT FROM THE CREW. N1 WAS SET TO 85 % AT TIME OF ROLLBACK, AND SPEED SWITCHES WERE SELECTED ON. NO ABNORMAL CAUTIONS OR MESSAGES PRESENT DURING ROLLBACK. THE REST OF THE FLIGHT WAS UN-EVENTFUL, DECLARED EMERGENCY. DID NOT NOTICE FLUXUATION IN ANY OTHER SETTINGS OR PERAMETERS. DURING POWER ASSURANCE RUN AND ACCELERATION, DECELERATION CHECK NOTED AND AUDIBLE HISSING OR BLOWOFF NOISE FROM RIGHT ENGINE.
FLAPS FAIL DURING CLIMB OUT, AT FLT LEVEL 230, 280 KNOTS FLAPS AT 0 WITH NO MOVEMENT OR SELECTION TO FLAPS. COMPLIED WITH QRH, MESSAGE PERSISTED. DIVERTED AND DECLARED EMERGENCY. RESET FLAPS IAW FIM 27-50-00 AND SET FLAPS AT 20 DEGREES.
FLAP FAIL CAUTION MESSAGE DURING CRUISE CLIMB, FLAPS AT ZERO DEGREES, PERFORMED FLAP RESET PROCEDURE IAW SUPP 98-18G, BOX 12, FLAPS RESET. NOTED BY MAINTENANCE.
CARGO SMOKE WARNING OCCURRED AT GATE. RAMP VERIFIED SMOKE PRESENT IN CARGO BAY WHEN OPENING DOOR.
IN FLIGHT RECEIVED RT REV UNLOCK MSG. COMPLIED WITH QRH. DIVERTED & LANDED BELOW 47000 LBS & MAX BTMS WAS 4454. DEACTIVATED RT TR IAW SUP 15-046, M ACTION COMPLIED WITH. PERFORMED TR LUBE IAW SUPP 14-118A. OPERATIONS CHECKED GOOD AT THIS TIME. REMOVED PLACARD & FROM MEL.
FLIGHT NR 4026, IMMEDIATELY AT TAKEOFF, LOUD NOISE FROM FRONT OF ACFT, NO CAUTIONS, OR WARNINGS. ELEC SYNOPTIC SHOWED ADG DEPLOYED. ADG DEPLOYED AT APPROX 145 KNOTS, MAX OF 200 KNOTS ON RETURN. ADG DEPLOYED APPROX 14 MINUTES. PERFORMED VISUAL INSPECTION OF ADG STRUT & GEN HOUSING IAW SUPP 10-066. NO DEFECTS NOTED AT THIS TIME STOWED ADG IAW SUPP 16-015, IAW 253890 2 FOR ADG AUTO DEPLOY MEL & 253890 3 FOR NDT MEL.
FLIGHT 9365, 3848CXL 3951 CBP1 N5 & CBP2 H14 POPPED. ELEC BURNING SMELL IN COCKPIT & GALLEY. AHRS WAS INTERMITTENT THEN HARD FAIL. R & R AHRS COMPUTER. OPERATIONS CHECKED GOOD IAW AMM 34-21-01. CB DID NOT POP OR ELEC ODOR NOTED AT THIS TIME. SN OFF 3393 & SN ON 3253.
FLIGHT NR 3849, EMER FLOOR LIGHT STRIP INOPERATIVE AFT OF ROW 8.
HORIZONTAL STAB LT & RT OTBD PIVOT FITTING ON STAB IS GOUGED & SCORED.
LT UPPER OBLIQUE ANGLE ON SF621 BULKHEAD CRACKED.
BRACK TRANSDUCER BRACKET IN LT WW IS CRACKED.
FS 280 STRINGER 3L CLIPS ARE CRACKED.
UPPER CAP ON FS 280 FLOORBEAM IS CRACKED AT RBL 9 & 12.
WING STIFFENER IN RT WW AT WS 48 IS CRACKED.
OUTER CLIP CRACKED AT FS 280 LBL 9, BOTH CLIPS CRACKED AT LBL 9.
LEFT AFT FUSELAGE SKIN HAS PROTRUDING DENT AT FS 712.00.
55378-8000-0016 PAX DOOR AFT DRAG ANGLE IS CRACKED.
NOSE WW CUT OUT AFT RT CORNER IS CRACKED.
FS 202 BULKHEAD CRACKED APPROX 3" LONG AT CUT OUT FOR PARKING BRAKE CABLE.
PAX DOOR INNER HANDLE CRACKED.
LOWER SUPPORT ANGLE FOR CARGO COMPARTMENT CURTAIN HANGAR SUPPORT ON AFT END HAS A CRACK ON OTBD END.
SERVICE DOOR SEAL STRIKER GOUGED.
LEFT WINDSHIELD POST LOWER FITTING IS CRACKED.
RIGHT FS 484.00 CLIPS ARE CRACKED AT BL 27.00.
FLIGHT COMPARTMENT RT SIDE WINDOW POST LOWER FITTING IS CRACKED.
EMERGENCY LIGHT FLOOR TRACK COVER AT ROW 1C - D COMING OFF.
APU AUTOSHUTDOWN FLAME OUT. FIRST OFFICER FOUND METAL DEBRIS NEAR APU EXHAUST. INSPECTED & FOUND INTERNAL APU FAILURE, CLEANED & SECURED AREA. APU IS CONSIDERED INOPERABLE.
SKIN SURROUNDING PANEL 132AL HAS TWO PLACES THAT HAS SCREW BITE MARKS. BLENDED OUT DAMAGE ON RT FUSELAGE SKIN IAW REO 601R-53-11-2529, REV B.
SKIN HAS ONE SCREW HOLE THAT ELONGATED AT THE 12:00 POSITION. REPAIRED RT FUSELAGE SKIN IAW REO 601R-53-11-2529, REV B.
RUDDER RT LOWER FWD SKIN IS CRACKED AND DENTED. R & R SKIN.
SERVICE DOOR SWITCH MOUNT IS CRACKED. R & R MOUNT ON SERVICE DOOR IAW SRM 51-41-02 AND 51-42-21.
BULKHEAD TIE DOWNS AT 559+80 LBL 9 AND 27 AND RBL 9 AND 27 HAVE CORROSION. BLENDED OUT OF LIMITS, R & R.
APU AFT HEAT SHIELD HAS SIX SCREWS PULLED THRU. FABRICATE AND INSTALLED HEAT SHIELD IAW SRM 51-24-16, SRM 51-21-11,SRM 51-25-06 AND SRM 51-40-11.
RT AFT FS 280 BULKHEAD CHAFED. REPAIRED IAW REO 601R-53-11-1727. REV E.
DURING COLD WORKING OF MLG FOUND TWO OVERSIZED HOLES 1 ON LT & 1 ON RT LOWER MLG TRUNNION FLANGE. REPAIRED DISCREPANT HOLES ON LT & RT MLG TRUNNION FLANGE. IAW REO 601R-57-21-1963.
GOUGE ON UPPER T/E BRACKET ON RT PYLON L/E PANEL 421 AL IS OUT OF LIMITS DUE TO PROXIMITY TO FASTENER HOLE. R & R.
PAX DOOR LOWER SILL HAS MULTIPLE AREAS OF CORROSION FOUND TO BE OUT OF ALLOWABLE LIMITS. R & R PAX DOOR LOWER SILL IAW SRM.
VISOR PANEL NR 326 BL DISTORTED (BENT) CHAFED BEYOND LIMITS. REPLACED WITH SERVICEABLE VISOR PANEL.
LT FLIGHT SPOILER WING T/E SEAL IS CRACKED. R & R.
RT FLAP VANE L/E CRACKED. BLENDED 2 AREAS WITHIN LIMITS BLENDED INBD L/E OUT OF LIMITS CHANGED INBD L/E SKIN.
CHAFED L/E SKIN AT FLA STA 60.005 FOUND TO BE OUT OF LIMITS 040 MATERIAL LOSS ORIG THICK 050" REM MATERIAL 010" MAX ALLOWED 025" IAW REO 601R-57-52-004, REV C. R & R L/E SKIN IAW SRM 51-40-11 & SRM 51-42-13.
FWD LOWER SUPPORT BRACKET FOR CARGO BAY DOOR WAS CRACKED. R & R IAW SRM 51-42-06 & 51-41-02.
INNER SKIN CHAFED OUT OF LIMITS. REPLACED INNER SKIN.
ANGLE IS CRACKED. REMOVE UNSERVICEABLE ANGLES REPLACED WITH NEW IAW REO 601R-53-41-059, REV B.
CORROSION FOUND OUT OF LIMITS AT FS 574+10 LBL 9. R & R IAW SRM 53-61-49.
BRAKE PRESSURE TRANSDUCER BRACKET IN RT WHEEL WELL IS CRACKED. R & R RT BRAKE PRESSURE TRANSDUCER BRACKET, PN 601R75262-157 IAW SRM 51-42-06.
WHEN GEAR SELECTED TO DOWN NLG DOORS WERE OPENING AND CLOSING RAPIDLY LONGER THAN NORMAL TIME FOR GEAR TO INDICATE DOWN AND LOCKED. INTEROGATED PSEU, FOUND SENSOR S35 FAULT-NGD LK2 REF 237682/2 FOR MEL. REPLACED NLG DOWNLOCK TO PROX SENSOR HARNESS ASSY PER AMM 32-61-05. GEAR INDICATION SATISFACTORY AND OPS CHECK GOOD. REMOVED MEL REMOVAL PLACARD. RII I-165
ANTISKID CAUTION AT 75KTS, ABORTED TAKEOFF. BTMS MAX READINGS 2, 5, 5,7. HIGH ENERGY STOP INSPECTION NOT REQUIRED PER MXC. WHEN THROTTLES AT IDLE MESSAGE CLEARED AND RECEIVED MOMENTARY CONFIG SPOILERS WARNING. NO WARNING PRESENT NOW.
ANTISKID OUTBOARD CAUTION MESSAGE AT 30KTS. ABORTED TAKEOFF. BTMS MAX READING 3, 3, 3, 3. REMOVED AND REPLACED LEFT OUTBAORD ANTISKID HARNESS.
BURING ODOR NOTED AROUND ROWS 6-7. ALL OVERHEAD LIGHT ARE OFF. NO BURNING ODOR NOTED AROUND ROW 6-7. ACFT OK FOR SERVICE IAW AMM 25-20.
CORROSION ON LT CARGO FLOOR SILL BY CARGO DOOR. REMOVED, FABRICATED, AND INSTALLED NEW LT CARGO FLOOR SILL.
PAX DOOR FWD STEP RISER CRACKED. REPAIRED PAX DOOR, FWD STEP RISER AT 2ND STEP IAW REO 601R-52-11-702, REV E ZONE 2.
SEAT TRACKS AT LBL 9 & RBL 9 AT FS 539+112 IN CARGO BAY ARE CORRODED TABLE R & R SEAT TRACKS.
LT AIRLERON FLUTTER DAMPER SHEAR LINK ATTACH POINT ON AILERON IS CHAFED ON OTBD SIDE. REPAIRED DAMAGE IAW REO 601R-57-61-367 DAMAGE DEPTH .060.
HYD LINE BRACKET IN RT WHEEL WELL CRACKED. R & R HYD LINE BRACKET ON RT WHEEL WELL IAW SRM 51-42-06.
APU EXHAUST AFT HEAT SHIELD HAS LOOSE FASTENERS AND 2 EA PULLED THRU FASTENERS. REPAIRED APU AFT EXHAUST HEAT SHIELD IAW REO 601R-49-81-051.
PAX DOOR AFT DRAG ANGLE CRACKED. REMOVED CRACKED AFT DRAG ANGLE SECTION THEN INSTALLED NEW SERVICEABLE SECTION IAW REO 601R-52-11-513, REV A.
BOTH TUB FITTING CRACKED AT 460 AND RBL9. REMOVED UNSERVICEABLE FITTING AND INSTALLED SERVICEABLE FITTING IAW SRM 51-42-21.
RT MLG DOOR CHAFED 2EA PLACES. REPAIRED IAW REO`S 601R-52-82-102 & 601R-52-82-034.
FS 484, LBL 9 HAS A CRACKED BAT TUB FITTING IN AFT RADIUS. REMOVED UNSERVICEABLE FITTING AND INSTALLED SERVICEABLE FITTING IAW SRM 51-42-21.
PAX DOOR ASSIST MOTOR MOUNTING BRACKET CRACKED. REMOVED CRACKED POWER ASSIST MOTOR SUPPORT ANGLE, THEN INSTALLED NEW SERVICEABLE SUPPORT ANGLE, IAW SRM 51-40-11, 51-42-06.
FS 484, CLIP CRACKED AT RBL 36. REMOVED UNSERVICEABLE CLIP AND REPLACED WITH SERVICEABLE CLIP IAW REO 601R-53-41-059, REV B.
LT AILERON UPPER L/E SKIN CHAFED. REPAIR CHAFED AREA IAW REO 601R-57-60-013.
RT AILERON UPPER L/E SKIN CHAFED. REPAIR CHAFED AREA IAW REO 601R-57-60-013.
CRACKED INTERCOSTAL ADJACENT TO STRINGER 14 . REMOVED AND REPLACED IAW REO 601R-53-61-100.
PAX DOOR OUTER HANDLE CRACKED. REMOVED CRACKED OUTER HANDLE AND INSTALLED NEW SERVICEABLE OUTER HANDLE IAW EO E08/007/452, REV A.
LT ENGINE LOWER NOSE COWL THRUST REVERSER PDU ACCESS DOOR VENT LOUVER CRACKED. R & R VENT IAW SRM 51-42-13.
PITTING CORROSION ON NR 2 RT SIDE SEAT TRACK. R & R RT NR 2 SIDE SEAT TRACK.
AFTER T/O, FLAPS FAILED AT 20 DEGREES. COMPLIED WITH QRH. PERFORMED FLAP RESET PROCEDURE IAW SUPP 98-18D, BOX 12. FLAPS RESET. PLACARDED AND PLACED ON MEL. PERFORMED OPS TEST OF FLAPS SYS IAW AMM 27-51-05. ALL CHECKS GOOD, REMOVED FROM MEL. M/C REF 201889/1 FOR R & R OF FLAP CONTROL LEVER IAW AMM 27-51-01 ALL CHECKS GOOD. REF 201889/1 - R & R FLAP CONTROL LEVER OPS CK IAW 27-51-01. ALL CKS GOOD.
CRACK FOUND ON FS 280 RBL 9 INBD AND OTBD CLIP. 2 CLIP REPLACED IAW SRM 51-42-20 AND 51-42-06. (K)
CRACKS FOUND ON BRACKETS AT FS 280.00, LBL 9 INBD AND OTBD. BRACKET AT FS 280.00, LBL9 REPLACED IAW SRM 51-42-06 AND 51-42-20. (K)
CRACK FOUND ON PILOT BULKHEAD FS 280, RBL 9, LWR FLANGE. PILOT BULKHEAD REPAIR IAW REO 601R-53-11-171, REV D. (K)
CRACK ON PILOT BULKHEAD AFT ANGLE FS 280 LBL 9. REPAIRED IAW REO 601R-53-11-138. (K)
SCRATCH REPAIR ON FS 280 PILOT BULKHEAD RBL 9, WL 94.50 IAW REO 601R53-11-1706. (K)
CRACK FOUND ON PILOT BULKHEAD FS 280, LBL 9 LWR FLANGE (CRACK LENGTH .750). REPAIR ON PILOT BULKHEAD AT FS 280, LBL 9 LWR FLANGE CARRIED OUT IAW REO 601R-53-11-171. (K)
SERVICE DOOR THRESHOLD PLATE FOUND CORRODED OUT OF LIMIT. SERVICE DOOR THRESHOLD PLATE REPLACED IAW SRM 51-41-02. (K)
AFT PRESSURE BULKHEAD CRACKED AT LINTEL FITTING LOCATION. REPAIRED IAW REO 601R-53-61-1230. (K)
RT HYD MANIFOLD SUPPORT BRACKET IN AFT EQUIPMENT COMPT CRACKED (AFT LWR AREA) .20 INCH LONG RT HYD MANIFOLD SUPPORT BRACKET REPLACED IAW REO 601R-53-62-031, REV A. (K)
REPORTS NR 1 PACK SMELLS HOT IN AUTO AND MANUAL IN FLIGHT AND ON THE GROUND AND DUCT TEMP UNCONTROLLABLE. FOUND CONNECTOR PLUGS S3HG AND P9HG BROKEN, PLACED NR 1 PACK ON MEL AND PLACARDED. FOUND ACM SEIZED REMOVED AND REPLACED ACM IAW AMM 21-00. OPS CHECK GOOD. REMOVED PLACARD MEL. (K)
AFTER GEAR RETRACTION, GEAR STAYED IN DOWN POSITION, ASSOCIATED MESSAGES WERE INBD ANTISKID INOP AND PARK BRAKE SOV CAUTION MESSAGES. AFTER CYCLING GEAR, GEAR RETRACTED AND CYCLED NORMALLY. REMOVED AND REPLACED LANDING GEAR HANDLE IAW AMM 32-31-01. OPS CHECK GOOD. (K)
FLAPS FAILED AT 20 DEGREES WITH FLAPS FAIL CAUTION AFTER TAKEOFF. LANDED AT FLAPS 20 AFTER COMPLYING WITH QRH. COMPLIED WITH AWAC SUPP 98-018B RESET, FLAPS RESET OK. RESET.
FLAPS FAILED AT 30 DEGREES ON APPROACH, COMPLIED WITH QRH LANDED IN BUF. COMPLIED WITH RESET PROCEDURE IAW AWAC SUPPLEMENT 98-018B STEPS 1.3 AND 1.4 FLAPS SYSTEMS RESET OK. (A)
LT MLG DID NOT RETREAT AFTER TAKEOFF GEAR DISAGREE MSG C/W QRH RETURN TO LGA AT WS 39800 LBS. FOUND LT UPLOCK TARGET LOOSE AND OUT OF ADJUSTMENT. ADJUSTED TARGET FOR LT MLG UPLOCK. REF AMM 32-32-05. OPS TEST OF LANDING GEAR EXTENTION AND RETRACTION SYSTEM NORMAL. REMOVED FROM MEL.
INFLIGHT RECEIVED SPOILERON FAULT YELLOW CAUTION MESSAGE AND IB AND OB GROUND SPOILER FAULT STATUS MESSAGES. COMPLIED WITH QRH (FERRY TO PHL). INTERROGATED SECU NR 1 AND SECU NR 2 FAULT LOG FOUND CODE 13 (SECU 1 MODULE A) REMOVED AND REPLACED SECU NR 1 IAW 27-61-05. OPS CHECK GOOD IAW 27-61-00. (K)
UNUSUAL NOISE HEARD WHEN FIRST OFFICER YOKE TURNED. MORE NOTICEABLE WHEN TURNED RIGHT. ALSO NOTED THROUGH FLOOR ON CAPTAINS SIDE. RETORQUED FIRST OFFICERS YOKE REF SB CRJ-SL-27-045 REV A AND M 27-11-01. OPERATIONAL CHECK GOOD. (M)
FOUND LEFT FS 621 FLOOR SUPPORT ANGLE CRACKED. (M) MAINTENANCE REPAIRED IAW REO 601R-53-61-117. (M)
FOUND RIGHT FS 621 FLOOR SUPPORT ANGLE CRACKED. (M) MAINTENANCE REPAIRED IAW REO 601R-53-61-117. (M)
LT WING LOWER PLANK ACCESS HOLE NR 1 540BB HAS MINOR CORROSION IN NON-CRITICAL AREAS APPROX .003 INCH DEEP AND 5 INCH LONG IN (2) PLACES. (K) MAINTENANCE REPAIRED IAW REO 601R-57-21-030. (M)
RT WING IB FLAP LOWER SKIN GOUGED/DENTED APPROX 3 INCHES LONG X 3 INCHES WIDE X .205 INCH DEEP, ADJACENT TO RIB AT WS 74.8, APPROX 8 INCHES AFT OF LEADING EDGE OF FLAP. (K) MAINTENANCE REPAIRED FLAP LOWER SKIN IAW BSC EO 601R-57-12572. (M)
LT WING PLANK LOWER ACCESS HOLE NR 2 510AB HAS MINOR CORROSION IN NON-CRITICAL AREAS APPROX .005 DEEP AND 5 INCHES LONG. (K) MAINTENANCE REPAIRED IAW REO 601R-57-21-030. (M)
RT WING LOWER PLANK ACCESS HOLE NR 1 640BB HAS MINO CORROSION IN NON-CRITICAL AREAS APPPROX .003 DEEP AND 2.5 INCH LONG IN (2) PLACES. (K) MAINTENANCE REPAIRED IAW BSC REO 601R-57-21-030 REV F. (M)
RT 484 ANGLE IS CRACKED AT RBL 36 APPROX .25 INCH LONG. (K) MAINTENANCE REPAIRED ANGLE IAW BOMBARDIER REO 601R-53-41-059 REV A AND BOMBARDIER STANDARD REPAIR 601R-53-0030A. (M)
HYDRAULIC PRESSURE BRACKET IS CRACKED APPROX .1 INCH LONG IN RT MLG WHEEL WELL CEILING. (K) MAINTENANCE REMOVED AND REPLACED HAT CHANNEL P/N 601R75262-157 IAW CRJ 200 SRM 51-42-06. (M)
LT 484 ANGLE IS CRACKED AT LBL 36 APPROX .5 INCH LONG. (K) MAINTENANCE REPAIRED ANGLE IAW BOMBARDIER REO 601R-53-41-059 REV A AND BOMBARDIER STANDARD REPAIR 601R-53-0030A. (M)
LT 484 ANGLE IS CRACKED AT LBL 27 APPROX .5 INCHES LONG. (K) MAINTENANCE REPAIRED ANGLE IAW BOMBARDIER REO 601R-53-41-059 REV A AND BOMBARDIER STANDARD REPAIR 601R-53-0029B. (M)
RT 484 ANGLE IS CRACKED AT RBL 27 APPROX 1 INCH LONG. (K) MAINTENANCE REPAIRED ANGLE IAW BOMBARDIER REO 601R-53-41-059 REV A AND BOMBARDIER STANDARD REPAIR 601R-53-0029B. (M)
HYDRAULIC PRESSURE TRANSDUCER HAT CHANNEL CRACKED APPROX .1 LONG IN LT MLG WHEEL WELL CEILING. (K) MAINTENANCE REMOVED AND REPLACED HAT CHANNEL P/N 601R75262-159 IAW CRJ 200 SRM 51-42-06. (M)
RT OBLIQUE ANGLE AT STA 625.00 HAS A .5 INCH CRACKED IN RADIUS. (K) MAINTENANCE INSTALLED NEW ANGLE IAW CRJ SRM 51-42-06. (M)
LT OBLIQUE ANGLE AT STA 625 HAS .5 INCH CRACKED IN RADIUS. (K) MAINTENANCE INSTALLED NEW ANGLE CRJ SRM 51-42-06. (M)
FLAPS FAIL CAUTION MESSAGE INFLIGHT AFTER FLAP 8 TAKEOFF AFTER FLAP RETRACTION ALT, MOVED FLAP HANDLE TO ZERO, FLAPS STAYED AT 8. AIRSPEED 170 KTS OAT 21 DEGREES C. PERFORMED FLAPS FAIL CHECKLIST AND FLAPS 8 LANDING. TOUCHDOWN 164 KTS AT 100/MIN. COMPLIED WITH RESET PROCEDURE IAW AWAC SUPPLEMENT 98-018B STEPS 1.3 AND 1.4, FLAP SYSTEM RESET OK. AIRCRAFT GOOD FOR RETURN TO SERVICE. (M)
FLAPS FAIL CAUTION MESSAGE AND FLAPS FAIL AT 0 DEGREES. PERFORMED FLAP RESET PROCEDURE IAW AWAC SUPPLEMENT 98-018B STEPS 1.3 AND 1.4, FLAPS RESET. AIRCRAFT RELEASED FOR SERVICE, NO SDU LIGHTS ILLUMINATED AT THIS TIME. (M)
LEFT HYDRAULIC TRANSDUCER BRACKET, P/N 601R75262-159, CRACKED APPROXIMATELY .1 INCH LONG IN LEFT MLG WHEEL WELL CEILING. INSTALLED NEW BRACKET IAW CRJ SRM 51-42-06. (M)
PERFORMED AIR RETURN AFTER N1 FAN VIBRATION ON NR 2 ENGINE ASSOCIATED WITH AIRFRAME VIBRATION. VERTICAL DESCENT RATE LESS THAN 360 FPM AT TOUCHDOWN. LANDING WEIGHT 51,000 LBS. OVERWEIGHT LANDING INSPECTION NOT REQUIRED. RT ENGINE UPPER TRANSLATING COWL OPENED IN FLIGHT. REMOVED AND REINSTALLED ORIGINAL DAMAGED UPPER TRANSLATING COWL IAW CRJ AMM 71-11-01 AND REQUIRED REO FROM SHORTS FOR DAMAGE. COMPLIED WITH REQUIRED REO 601R-78-33-3528 REV WC20 FOR TAP TEST. APPLIED PAINT TO SCRATCH. APPLIED YELLOW DOT TO DENT. (M)
AFTER TAKEOFF WHILE RETRACTING FLAPS FROM 20 DEGREES. COMPLIED WITH QRH, FLAPS FAIL CAUTION MESSAGE ON ED1. COMPLIED WITH SUPPLEMENT 98-018A, NO FLAP TWISTING, SKEWING OR DEFORMATION NOTED. RESET CIRCUIT BREAKER ONCE, MESSAGE CLEARED, FLAPS OPERATE NORMALLY. (K)
ANTI-ICE DUCT MESSAGE WITH DUCT FAIL IN SWITCH LIGHT WITH WING ANTI-ICE LIGHT ON. COMPLIED WITH QRH, SELECTED 14TH STAGE BLEEDS AND WING ANTI-ICE OFF. MESSAGE CLEARED. WHEN 14TH STAGE BLEEDS SELECTED ON AND WING ANTI-ICE TO STANDBY, MESSAGE DID NOT REAPPEAR. REMOVED AND REPLACED SENSING ELEMENT A47WK REF AMM 36-21-04, OPS CHECK GOOD. (M)
MESSAGE DURING FLAP RETRACTION ON CLIMBOUT, FLAP FAIL AT ZERO. FOUND LT BRAKE POSITION SENSOR UNIT HARD FAILED. REPLACED BPSU IAW AMM 27-51-10. FLAPS CHECK GOOD. (K)
RT ENGINE OIL LOW PRESSURE ILLUMINATED EN ROUTE, WITH THROTTLE RETARDED, OIL PRESSURE DROPPED FROM 48 TO 28 PSI. ENGINE WAS SHUTDOWN MANUALLY. PERFORMED ENGINE OIL CONSUMPTION CHECK PER AWAC SUPPLEMENT 06-025. FOUND STARTER CARBON SEAL LEAKING. REMOVED AND REPLACED STARTER CARBON SEAL ERF AMM 72-60-00. OPS CHECK GOOD. (M)
FIRST OFFICERS FRONT WINDSCREEN SHATTERED, CRACKED AFTER TAKEOFF AND SHATTERED PRIOR TO 4000 FEET. HEAT WAS SELECTED ON. REMOVED AND REPLACED FIRST OFFICERS RT WINDSHIELD. OPS CHECK GOOD. (M)
FUSELAGE SKIN HAS SUSTAINED LIGHTNING STRIKE DAMAGE AT FS 654.5 BETWEEN STR 26R AND 27R. REPAIRED DAMAGED AREA BY INSTALLING AN EXTERNAL DOUBLER AT FS 654.5 BETWEEN STR 26R AND 27R IAW EO AND SRM. (K)
PASSENGER DOOR AFT SKIN DAMAGED AND INTERNAL STIFFENER CRACKED BELOW SKIN RIGHT STIFFENER CRACKED COMPLETELY IN HALF 1.5 INCH. INSTALLED REPAIR FILLER AND DOUBLE IAW BRAS EO 601R-52-7054A. (M)
CARGO DOOR SUPPORT BEAM MEMBER ANGLE, P/N 601R35050-109, CRACKED AT PRESSURE BULKHEAD FS 621, LBL 34.42. FABRICATED NEW CARGO DOOR SUPPORT BEAM ANGLE IAW CRJ200 SRM 51-30-06 AND BOMBARDIER DRAWING NR 601R35050, INSTALLED ANGLE IAW CRJ200SRM 51-42-21. (M)
DURING CLIMB-OUT, EXPERIENCED EXTREMELY LOUD NOISE FROM NOSE OF AIRCRAFT. RETURN TO FIELD. FOUND GROUND SERVICE DOOR OPEN. INSPECTED AND NO DAMAGE NOTED. CLOSED AND SECURED DOOR. NO FURTHER OCCURRENCES OR DEFECTS. (M)