N463AW
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
FLAPS FAILED CAUTION MSG ON APPROACH. FLAPS FAILED AT ZERO DEG. C/W FIM RESET, RESET FAILED. AIRCRAFT REMOVED FROM SERVICE. INSPECTED FLAP SKEW DETECTOR IAW FIM 27-50-00. FAULTS NOTED FOR FECU POWER 1 AND 2 AND LH OUTBD PANEL SKEW L4 AND L3. DEACTIVATED SKEW SYSTEM IAW AWA SUP 06-080A INSPECTED FLAPS NO SKEW NOTED. FLAPS OPS CHECK GOOD. MX WC#4 REACTIVATED SKEW DETECTION SYSTEM IAW SUPP 06-076A OPS CHECK OF THE SDS AND FLAPS GOOD. REF 338986/3 R&R BRAKE UNIT MOTOR.
LEFT OVERWING EXIT WILL NOT OPEN FREELY. AIRCRAFT REMOVED FROM SERVICE. PERFORMED OPS CHECK OF OVERWING EMGERGENCY EXIT IAW AMM 52-21-00. PERFORMED OPS CHECK OF OVERWING EMGERGENCY EXIT IAW AMM 52-21-00. DOOR OPENS AND CLOSES FREELY, COMPLIED WITH CM ACTION OF MEL 25-70-20-16. TAPE APPLIED TO SIDEWALL PANEL REFERENCE 369579/3 FOR MEL
GEAR DISAGREE ON RETRACTING GEAR AT 220 KTS. AT FLAPS 0, HYD PUMPS IN AUTO 3B TO ON. MESSAGES ENCOUNTERED DURRING GO AROUND. (MOC NOTE GO AROUND WAS FOR UNSTABLE APPROCH) *****AIRCRAFT REMOVED FROM SERVICE******** CW M ACTION FOR MEL 32-30-01 REF 359659/3 FOR MEL CLEANED P3GA SENSOR AND TARGET, PERFORMED MULTILPLE EXTENSION AND RETRACTION CHECKS IAW AMM 32-30-00-05. COULD NOT DUPLICATE FAULT. OPS CHECK GOOD. NO INPUT ERROR WITH GEAR UP. REMOVED PLACARD AND FROM MEL.
AFTER TAKE-OFF, AFTER SELECTING GEAR UP, GOT GEAR DISAGREE WITH NOSE GEAR SHOWING DOWN. COMPLETED QRH TO EXTEND GEAR, GEAR SHOWED DOWN WITH THREE GREEN. NOSE GEAR INDICATION REMAINED GREEN WHOLE FLIGHT. HYD QTY, PRESSURE AND TEMPS NORMAL.AIRCRAFT REMOVED FROM SERVICE. COMPLIED WITH M ACTION FOR MEL 32-30-01. REF 358892-3 FOR MEL. REF MX WORKORDER 325114 MX WORK CARDS 1&2 FOR ALL WORK PERFORMED, REMOVED PLACARD AND FROM MEL. R&R #2 NLG HARNESS
RECEIVED GEAR DISAGREE WARNING MESSAGE AFTER TAKE-OFF AND NOSE DOOR OPEN WARNING MESSAGE. FLAPS AT 8. RECEIVED 3 GREEN AFTER SELECTING GEAR DOWN WITH MANUAL RELEASE HANDLE AND GEAR LEVER PER QRH. AIRCRAFT REMOVED FROM SERVICE. R & R BENT NLG CENTERING PROX SENSOR BRACKET IAW CMM 32-20. OPS CHECK GOOD. REMOVED PLACARD AND MEL
ON SHORT FINAL FA REPORTED SMOKE/SMELL FROM ROW 8CD. CHEMICAL SMELL LASTED FOR ABOUT 5MINS AFTER LANDING TO OPENING THE PAX DOOR AIRCRAFT REMOVED FROM SERVICE. INSPECTED CABIN. ALL OVERHEAD AND SIDEWALL LIGHTING OPS NORMAL. INSPECTED AND CLEANED TEMP SENSOR/FAN UNIT FOR CABIN TEMP CONTROL. C/W AWA SUPP 09-037D. NO ODORS PRESENT. NO OTHER DEFECTS NOTED.
ON-TAKE OFF AFTER GEAR RETRACTION RECEIVED NOSE DOOR OPEN AND GEAR DISAGREE MASTER WARNING APPROXIMATELY 6 SECONDS AFTER SELECTING GEAR UP. (BLK 2) NOSE LANDING GEAR SHOWED RED ON EICAS MANUAL RELEASE WAS USED. DID NOT ENCOUNTER ICING OR TURBULENCE HYD PUMPS TEMP & PRESSURE WERE NORMAL EMERGENCY DECLARED AND NORMAL LANDING. *********AIRCRAFT REMOVED FROM SERVICE******* MEL IN WORK
DURING INCORPORATION OF REO 601R-53-61-1240 REPAIR AND MODIFICATION TO THE FS621.00 PRESSURE BULKHEAD WEB, FOUND EXISTING DOUBLER PN 601R-53-61-5768-1 INSTALLED AT FS621.00 AND LBL9.50 TO LBL27.50, WL74 TO WL87.4. *****AIRCRAFT REMOVED FROM THE SERVICE******** REMOVED EXISTING DOUBLER PN 601R-53-61-5768-1 AT FS621.00 AND LBL9.50 TO LBL27.50, WL74 TO WL87.4. INSTALLED NEW DOUBLER PN 601R-53-61-1240. IN SERVICE DEVIATION INSPECTION REQUIREMENTS TO GENERIC REO 601R-53-61-1240 REV D. ALL WORK WITHIN LIMITS WAS PERFORMED IAW MHIRJ REO 601R-53-61-7944 REV (--) DATED 2023-02-16 AND MHIRJ REO 601R-53-61-1240 REV D, DATED 2016-10-31. WORK PERFORMED UNDER AERSALE WORK ORDER 003822, CARD NO. 00506 CARD ID # 1797163. N463AW TT: 39,233:25 TC: 37,967.
DENT TO FORWARD FUSELAGE SKIN FS280.0 TO FS310.0 AND STR 11-14 RHS. ****AIRCRAFT REMOVED FROM SERVICE******* PERFORMED A PERMANENT REPAIR FOR TEMPORARY REO 601R-53-21-3568 TO A DENT TO FORWARD FUSELAGE SKIN FS280.0 TO FS310.0 AND STR 11-14 RHS. FABRICATED DOUBLER PN 601R-53-21-3594-1 FOR REPAIR TO THE INTERNAL FUSELAGE SKIN. CUTOUT DAMAGE DIMENSIONS L= 1.950ÿ½ X W = 1.950ÿ½. FABRICATED DOUBLER DIMENSIONS L = 10.700ÿ½ X W = 8.900ÿ½ FROM 0.025ÿ½ CLAD ALUMINUM. PERFORMED HFEC WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW REO 601R-53-21-3594 REV (--) DATED 2023-02-06. WORK PERFORMED UNDER AERSALE WORK ORDER 003822, CARD NO. 50009, TT: 39,235:25 TC: 37,967.
ONE DENT ON FORWARD FUSELAGE SKIN PN 601R31022-61 AT FS310.00-FS319.00 AND STR 25L - STR 26L. DENT DIMENSIONS: D4- L = 0.825ÿ½ X W = 0.800ÿ½ X D = 0.008ÿ½, FS310.00+9 ORIGINAL MATERIAL THICKNESS 0.063ÿ½. ****AIRCRAFT REMOVED FROM SERVICE****** VERIFIED NO LOOSE OR PULLED FASTENERS IN AREA SURROUNDING DENT AND FREE OF CREASES. PERFORMED HFEC WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW ASAP EA #: AWAC-CRJ253-01945 REV IR, DATED 1/13/2023. WORK PERFORMED UNDER AERSALE WO # 003822, CARD NO. 20003, CARD ID # 1794968. N463AW TT: 39,235:25 TC: 37,967
THREE DENTS ON FORWARD FUSELAGE SKIN PN 601R31022-61 AT FS280.00-FS295.00 AND STR 25L - STR 26L. DENT DIMENSIONS: D1- L = 0.250ÿ½ X W = 0.200ÿ½ X D = 0.004ÿ½, FS280.00+13 D2- L = 0.400ÿ½ X W = 0.325ÿ½ X D = 0.007ÿ½, FS280.00+14 D3- L = 0.350ÿ½ X W = 0.300ÿ½ X D = 0.006ÿ½, FS280.00+12 ORIGINAL MATERIAL THICKNESS 0.063ÿ½. *******AIRCRAFT REMOVED FROM SERVICE***** VERIFIED NO LOOSE OR PULLED FASTENERS IN AREA SURROUNDING DENT AND FREE OF CREASES. PERFORMED HFEC WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW ASAP EA #: AWAC-CRJ253-01945 REV IR, DATED 1/13/2023. WORK PERFORMED UNDER AERSALE WO # 003822, CARD NO. 20002, CARD ID # 1794967. N463AW TT: 39,235:25 TC: 37,967
PAX DOOR AFT PANEL DRAG ANGLE IS CRACKED AT PULLEY BRACKET AREA AT FS339.50. AIRCRAFT REMOVED FROM SERVICE. REPAIRED DRAG ANGLE WITH FABRICATION OF NEW ANGLE, DIMENSIONS L= 21.500ÿ½ W= 1.600ÿ½. PERFORMED HFEC WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW REO 601R-52-11-513 REV (C) DATED 2020-10-22.
CORROSION ON CABIN FLOOR SEAT TRACK PN 601R35031-263 AT FS559.00 TO FS621.00 AND RBL27.0. ***** AC REMOVED FROM SERVICE ***** CORROSION EXCEEDED SRM LIMITS AND REMOVED AND REPLACED CABIN FLOOR SEAT TRACK PN 601R35031-263 AT FS559.00 TO FS621.00 AND RBL27.0. SEAT TRACK LENGTH 41.00ÿ½. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW CRJ200 SRM 51-26-00 REV 39, SRM 51-11-00 REV 39, SRM 53-61-43 REV 39, SRM 51-12-00 REV 39, SRM 51-40-11 REV 39, SRM 51-25-06 REV 39, SRM 51-25-16 REV 39, SRM 51-42-36 REV 39, SRM 51-42-21 REV 39, SRM 51-41-02 REV 39 AND CRJ200 AMM 53-01-01 REV 66. WORK PERFORMED UNDER AERSALE WORK ORDER 003822, CARD NO. 20232, TT: 39,235:25 TC: 37,967.
TWO DENTS ON FORWARD FUSELAGE SKIN PN 601R31022-61 AT FS319.00-FS333.00 AND STR 25L - STR 26L. DENT DIMENSIONS: D5- L = 0.600ÿ½ X W = 0.600ÿ½ X D = 0.009ÿ½, FS280.00+13 D6- L = 0.600ÿ½ X W = 0.500ÿ½ X D = 0.008ÿ½, FS280.00+14 ORIGINAL MATERIAL THICKNESS 0.063ÿ½. ******AIRCRAFT REMOVED FROM SERVICE********* VERIFIED NO LOOSE OR PULLED FASTENERS IN AREA SURROUNDING DENT AND FREE OF CREASES. PERFORMED HFEC WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW ASAP EA #: AWAC-CRJ253-01945 REV IR, DATED 1/13/2023. WORK PERFORMED UNDER AERSALE WO # 003822, CARD NO. 20004, CARD ID # 1794971. N463AW TT: 39,235:25 TC: 37,967
WEAR DAMAGE TO THE FUSELAGE EXTERNAL SKIN PN 601R35004-405 AT FS682.00 - FS700.00 AND STR 15R. ********AIRCRAFT REMOVED FROM SERVICE*********** BLENDED WEAR DAMAGE TO THE FUSELAGE EXTERNAL SKIN PN 601R35004-405 AT FS682.00 - FS700.00 AND STR 15R. DIMENSIONS L = 5.300ÿ½ X W = 2.400ÿ½ X D = 0.013ÿ½. PERFORMED HFEC WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW ASAP EA # AWAC-CRJ253-01953 REV IR DATED 2/9/2023. WORK PERFORMED UNDER AERSALE WORK ORDER 003822, CARD NO. 20306, CARD ID # 1820142. N463AW TT: 39,235:25 TC: 37,967
NOSE GEAR DISAGREE MESSAGE APPEARED AFTER LANDING GEAR WAS MOVED TO UP POSITION. RAN QRH, MESSAGE PERSIST. MANUALLY DEPLOY GEAR AND MESSAGE CLEARED. NOSE DOOR OPEN WARNING MESSAGE APPEARED AFTER GEAR DISAGREE MESSAGE WAS DISPLAYED. NO GEAR BOXES WERE RED, ONLY WHITE. ONCE GEAR WAS DEPLOYED, ALL BOXES GREEN AND LOCKED. MESSAGE APPEARED AT 150KTS. EMERGENCY LANDING WAS DECLARED. ***AIRCRAFT REMOVED FROM SERVICE **** ADJUSTED PS14GA( NLG OLEO PROX SENSOR) IAW AMM 32-61-05 OPS CK GOOD
****SUPPLEMENTAL INFORMATION**** FLAPS FAIL CAUTION MESSAGE IN CRUISE AT FL 300. QRH COMPLETED. PERFORMED FLAP RESET PROCEDURE IAW AWAC SUPPLEMENT 98-18I BOX 12. FLAPS RESET, PLACARDED AND PLACED ON MEL AIRCRAFT REMOVED FROM SERVICEPERFORMED FLAP RESET PROCEDURE IAW AWAC SUPPLEMENT 98-18I BOX 12. FLAPS RESET, PLACARDED AND PLACED ON MEL AIRCRAFT REMOVED FROM SERVICE ****AIRCRAFT REMOVED FROM SERVICE*** NOTED
RECEIVED FLAPS FAIL CAUTION MESSAGE AFTER INTIAL DECENT. C/W QRH & PROCEDED TO LAND AT DESTINATION. FLAPS WERE AT ZERO POSITION. PERFORMED FLAP RESET PROCEDURE IAW SUP 98-18I BOX 12. FLAPS RESET. CAPTAIN WAS THE FLYING PILOT. DURING DECENT AT 5,000 FT & FLAPS SET AT ZERO RECEIVED A FLAPS FAIL. CREW FOLLOWED QRH & DECLARED AN EMERGENCY. LANDING WAS NORMAL. . NO DAMAGE TO A/C OR INJURIES TO PASSENGERS NOTED. ***AIRCRAFT REMOVED FROM SERVICE*** T/S PER FIM 27-50, LH BPSU OUT OF RIG AT ZERO DEGREE POSITION. RIGGED LH BPSU PER AMM 27-51, OPS CHECK GOOD.
FO'S FRONT WINDSHIELD IS CRACKED, OUTER PLY. ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED FO WINDSHIELD AND COMPLETED INSTALLATION UP TO SUBTASK 56-11-01-430-007, STEP D. REF 348762/1 FOR COMPLETION OF TASKS P/N: NP139321-18, S/N OFF: 1107H5903, S/N ON: 21208H3450 ARW
AFTER TAXIING INTO GATE, UNABLE TO OPEN MAIN CABIN DOOR FROM INSIDE OR OUTSIDE. ***AIRCRAFT REMOVED FROM SERVICE*** CLEANED, INSPECTED, AND LUBED PAX DOOR SEAL IAW AWAC SUP 19-152A. OPS CHECK GOOD AT THIS TIME. OPERATED FROM INSIDE AND OUTSIDE, OPENED AND CLOSED SMOOTHLY.
BOTTOM LEADING EDGE OF RIGHT AILERON SKIN CHAFING. REMOVED AND REPLACED RT AILERON LOWER CENTER LEADING EDGE SKIN IAW SRM 51-42-06 AND 51-42-21.
RT HYDRAULIC MANIFOLD SUPPORT BRACKET AFT LOWER CORNER CRACKED. REMOVED AND REPLACED RT HYDRAULIC MANIFOLD SUPPORT BRACKET IAW REO 601R 53-62-031 REV A.
FLOOR SEAT TRACK #4 ON RBL9 HAS CORROSION. REMOVED AND REPLACED FLOOR SEAT TRACK #4 RBL 9 IAW SUPPLEMENT 19-254.
INTERCOSTAL WHICH BUTTS UP TO AIRCARFT SKIN ON AFT SIDE OF 621 BULKHEAD AT STRINGER 14L APPEARS CRACKED. REMOVED AND REPLACED STRINGER 14L INTERCOSTAL IAW SRM 51-42-06 AND 51-42-21.
409+128 VERTICAL POST AT RBL 18 IS CRACKED ON RIGHT SIDE AT AFT INBOARD ANGLE AT 6TH FASTENER FROM TOP. REMOVED AND REPLACED VERTICAL POST ASSEMBLY AT FS 409+128 AT RBL 18 IAW GREO 601R-53-41-889 REV D.
RT FLOOR SILL HAS CORROSION BETWEEN FS 559+80 AND FS 589 ON UPPER AND LOWER SURFACES. REMOVED AND REPLACED RT FLOOR SILL AT WL 73.50 AND FS 559+87 TO 559+118 IAW SRM 51-42-21 AND 51-42-06.
FUEL ACCESS CUTOUT 510AB SHOWS SIGNS OF FRETTING. REPAIRED FUEL ACCESS CUTOUT 510AB IAW EA# AWAC-CRJ257-01318 REVA.
EVIDENCE OF CORROSION ON PAX DOOR INTERCOSTAL THAT IS ABOVE LATCH MECH BOX. REMOVED AND REPLACED INTERCOSTAL IAW SRM 51-42-06, 51-42-21 AND 51-42-13.
AFTER REMOVAL OF CARGO BAY DOOR TRACK SUPPORT BEAM BRACKET ON 621 FWD SIDE CRACKED IN TWO PLACES. REMOVED AND REPLACED CARGO DOOR BEAM BRACKET IAW SRM 51-42-21 AND SRM T/R 51-42.
PERFORM PERMANENT REPAIR FOR CARGO BAY DOOR TRACK SUPPORT BEAM. REPLACED CARGO DOOR SUPPORT BEAM IAW SRM 51-42-20. THIS COMPLIES WITH DMI 22614.
RIGHT INBOARD FLAP VANE, INBOARD SKIN HAS CHAFING. REPLACED RIGHT I/B FLAP VANE I/B LEADING EDGE IAW SRM 51-42-13.
PAX DOOR INNER SKIN CRACKED AT DOOR DATUM 6, FS335. REPAIRED PAX DOOR INNER SKIN IAW SUPP. 19-248.
RIGHT FLOOR SEAT TRACK #3 CORRODED. REPLACED SEAT TRACK IAW AMM 53-01-11.
RIGHT FLOOR SEAT TRACK #5 CORRODED. REPLACED SEAT TRACK #5 IAW AMM 53-01-11.
RIGHT MLG BAY VOLUMETRIC FUSE BRACKET, LINE BRACKET CRACKED. REPLACED BRACKET IAW SRM 51-42-06.
FS469.00, LBL45 FAIRING SUPPORT ATTACH BRACKET CRACKED. REPLACED BRACKET IAW CRJ 200 SRM 51-42-06.
FS461.00, RBL45 FAIRING ATTACH BRACKET CRACKED. REPLACED BRACKET IAW SRM 51-42-06.
FS 202.75 IN NLG WHEEL WELL RBL9 POST UPPER CLIP IS CRACKED. REPLACED CLIP IAW SRM 51-42-06.
FS449.00,LBL 45 FAIRING ATTACH BRACKET CRACKED. REPLACED BRACKET IAW SRM 51-42-06.
SERVICE DOOR LOWER SILL THRESHOLD CORRODED. REPLACED SERVICE DOOR LOWER SILL THRESHOLD IAW CRJ200 SRM TR 51-42.
FS469.00, RBL 45 FAIRING ATTACH BRACKET IS CRACKED. REMOVED AND REPLACED FS469.00, RBL 45 FAIRING ATTACH BRACKET IAW SRM 51-42-06.
INTERCOSTAL ON AFT SIDE OF 621 BULKHEAD AT STR 15L IS CRACKED. REPLACED INTERCOSTAL IAW SRM 51-42-06, 51-42-21.
FS235.00, STR 26L NLG CUT OUT IS CRACKED. REPAIRED NLG CUT OUT IAW REO 601R-53-11-101 REV-E.
INTERCOSTAL AT FS621.00 STR 16L IS CRACKED ON AFT SIDE OF BULKHEAD. REPLACED INTERCOSTAL IAW CRJ 200 SRM 51-42-06, 51-42-21.
FS 235 STR 26R NLG CUTOUT HAS A CRACK INDICATION REPAIR ACCOMPLISHED ON AAR N/R WO 1017605 1000/0005
CARGO FLOOR TRACK CORRODED AT 559+78 TO 559+95, LBL27. OUT OF LIMITS PER SRM 53-21-49, REPLACED TRACK IAW AMM 53-01-11.
FS 193,LBL30 TRU WEB IS CRACKED. REPAIRED WEB IAW REO 601R-53-11-111 REV-NC.
LEFT SIDEWALL SEAT TRACK NR 5 CORRODED. OUT OF LIMITS PER REO 601R-53-00-055 REV-C REPAIR B. REPLACED LEFT SIDEWALL SEAT TRACK 5 IAW AMM 53-01-11.
409+128 VERTICAL POST AT BL 0 IS CRACKED ON BOTH RIGHT AND LEFT SIDES AT AFT ANGLE, 6TH FASTENER FROM TOP. REPLACED ANGLES ON THE VERTICAL POST IAW SRM 51-42-06 AND REO 601R-53-41-889 REV-D.
FS 484, LBL36 I/B CLIP CRACKED. REPLACED CLIP IAW REO 601R-53-41-059 REV-B.
FS 484.00, LBL 27 O/B CLIP IS CRACKED. REPLACED CLIP IAW REO 601R-53-41-059REV-B.
VERTICAL POST AT FS 409-128, RBL18 CORRODED ON O/B AFT FLANGE. DAMAGE OUT OF LIMITS. POST WILL BE REPLACED ON W/O 1017605-1000-0035.
LEFT TRU DOOR AFT LATCH HAS CRACK IN RADIUS. REPAIRED CRACK IAW AWAC SUPP. 19-016B.
FOUND CHAFING DAMAGE TO OUTER SKIN OF PREVIOUS REPAIR PER GREO 601R-53-61-1285E
DURING CLIMB OUT, ACFT DID NOT PRESSURIZE. RETURNED TO DEPARTURE. FOUND OVERBOARD EXHAUST SHUT OFF VALVE IN THE INCORRECT POSITION, PERFORMED 14-259. EXHAUST VALVE IN THE CLOSED POS.
PAX DOOR FWD RISER IS EXFOLIATED AT THIRD STEP
CORROSION UNDER THE LEFT UPPER DOOR FITTING FOR NLG SPADE DOOR
ANGLE IS CORRODED. LOCATED ON THE OB SIDE OF INTERCOSTAL ON STRINGER 23R AND FOWARD SIDE OF FRAME 333 IN THE FWD E&E BAY.
CRACK ON FRAME BS 333 ABOVE PASSENGER DOOR.
PAX DOOR LOWER SILL CORRODED
PAX DOOR PIANO HINGE ON FUSELAGE SIDE MOST AFT LUG LANDING IS GOUGED
CARGO TRACK RBL 9 & FASTNERS CORRODED FROM BS 559+88 TO 559+96
RIGHT SEAT TRACK NR 6 FROM BS 449 TO 544 HAS CORROSION.
CARGO TRACK LBL 9 CORRODED AT BS 559+88
CARGO TRACK LBL 9 AND FASTENERS CORRODED FROM BS 559+112 TO 574
PAX DOOR ASSIST MOTOR LOWER BRACKET IS CRACKED.
PAX DOOR AFT RISER IS CRACKED.
FS 280 FWD FLOORBEAM ANGLE BETWEEN LBL 12 AND RBL 12 WAS CRACKED.
CLIP AT BS 280 AT STRINGER 3R CRACKED. REPLACED THE ATTACH ANGLE.
1014186-1000-0014 - 280 BEAM IS CRACKED AT THE LOWER SIDE NEXT TO THE MLG MANUAL RELEASE CABLE PULLEY BRACKET, O/B OF LBL9. REPAIRED 280 BEAM AT LOWER SIDE O/B OF LBL9 IAW REO 601R-53-11-171 REV-D.
STRINGER 23R IS CORRODED AT BS 333. REMOVED AND REPLACED THE STRINGER IAW SRM 51-42-06, AND 53-00-03.
SPLICE PLATE ON THE AFT SIDE OF FRAME BS 349 IS CORRODED BETWEEN STRINGERS 22 AND 24R. REPAIRED SPLICE PLATE IAW EA AWAC-CRJ253-00665 REV-IR.
NUMBER 2 HYD SYS RT AILERON PCU LINK FOUND TO BE CRACKED OPEN 1/4 INCH ON THE TOP SIDE OF THE LINK, ON AILERON END. LINK ASSEMBLY WAS REPLACED & SISTER LINK REPLACED ALSO, LT SIDE LINKS INSPECTED. ACFT ALREADY WAS OUT OF SERVICE FOR RON MX.
UPON LANDING, EXPERIENCED ABNORMAL YAW MOTION WITH THRUST REVERSERS DEPLOYED, LT ENG SLOWER TO SPOOL THAN RT ENG. ACCOMPLISHED THRUST REVERSER OPERATIONS CHECK IAW AMM 71-00-00-710-806. OPERATIONS CHECKED GOOD, NO DEFECTS NOTED. PERFORMED CHECK IAW FIM 73-20-00. R & R LT PCU, RIG & LEAK CHECKED GOOD.
DURING CLIMB OUT, SLIGHT OILY & BURNING SMELL. SMELL WENT AWAY AT CRUISE POWER, BUT EFFECTS OF BURNING EYES & NOSE REMAINED. FILM NOTED ON INSIDE OF WINDOW, SMELL NOTICED WITH APU OFF. R & R WATER SEPARATOR COALESCE SOCKS IAW SUPP 14-192. PERFORMED CLEARING OF DUCTING OF APU. PERFORMED CLEARING OF ENG WITH APU OFF. NO SMELL NOTED AT THIS TIME. OPERATIONS CHECK IAW SUPP 09-037A. COMPLIED WITH ENG OIL SERVICE IAW AMM 12-13-74, .25 & .25 PTS ADDED. COMPLIED WITH APU INSPECTION IAW AMM 49-11-01, OIL LEVEL GOOD NO LEAKS NOTED. INSPECTED COCKPIT WINDOWS, NO FILM NOTED.
FLIGHT 3857, BATTERY MASTER LEFT ON, DISPLAY ED1 SHOWING DISPLAY HI TEMP WARNING ON SCREEN. ELEC OVERHEAT ODOR IN COCKPIT. ALLOWED MAIN BATTERY TO CHARGE. PERFORMED MASTER BATTERY OPERATIONS CHECK IAW AMM 24-31-01. OPERATIONS CHECKED GOOD, NO ODOR NOTED IN COCKPIT AT THIS TIME.
EXIT SIGN IN ENTRYWAY LOWER BULKHEAD INOPERATIVE. R & R THE SIGN IAW AMM 33-51-10. OPS CHECKED GOOD.
FLIGHT 3766, RECEIVED APU FAULT & APU LOW OIL PRESS CAUTION MSG. AT GATE APU AUTO SHUTDOWN, SMELL OF BURNT OIL IN COCKPIT. COMPLIED WITH CM ACTION PLACARDED & PLACED ON MEL.
FS 280 STRINGER 3 CLIP CRACKED.
CARGO BAY FLOORBEAM HAS CORROSION AT LBL FS 603.00.
PAX DOOR AFT DRAG ANGLE IS CRACKED.
RBL 9 INBD & OTBD CLIPS CRACKED.
LEFT ENG TAIL PIPE FAIRING HAS A CRACK IN NR 2 STIFFENER.
RIGHT WING ROOT DRAG ANGLE ADJACENT TO BATTERY RIB IS CRACKED.
LEFT AFT FUSELAGE SKIN DENTED AT FS 700.
CARGO COMPARTMENT FWD ROLLER GUIDE, LOWER SUPPORT BRACKET HAS A CRACK ON ART SIDE.
RIGHT INBD 484 CLIP IS CRACKED.
LT INBD 484 CLIP IS CRACKED.
PAX FLOORBEAM SUPPORT FITTING AT LBL 9, FS 461 IS CRACKED.
LEFT HORIZONTAL STAB ACCESS PANEL 332AB HAS AN ELONGATED HOLE.
LEFT WINDSHIELD POST OTBD LOWER CLIP CRACKED.
LT & RT OBLIQUE ANGLES CRACKED.
AFT FUSELAGE SKIN HAS TWO PROTRUDING DENTS.
PASSENGER DOOR EXIT LIGHT COVER BROKEN. SECURED COVER WITH TAPE IAW M ACTION IAW 280805 3 FOR MEL. PAX DOOR FLOOR EMER FLOODLIGHT ON LOWER WARDROBE COVER BROKEN. COMPLIED WITH M ACTION. PLACARDED & PLACED ON MEL.
LEFT FWD GALLEY BULKHEAD & RT FUSELAGE ABOVE WING INSPECTION, LT EMER LIGHTS INOPERATIVE.
WHILE AIRBORNE, APU EXPERIENCED A HUNG START. START ABORTED & RE-ATTEMPTED. SECOND START ATTEMPT WAS SUCCESSFUL BUT A STRONG FUEL SMELL ENTERED THE CABIN THEN DISSIPATED.
AFTER TAKEOFF, RECEIVED PITOT BASE HEAT, LEFT AOA HEAT, LT STATIC HEAT, LT PITOT HEAT. COMPLIED WITH QRH. MESSAGES PERSISTED. COMPLIED WITH FIM RESET. MESSAGES CLEARED.
REPAIR LT HORZ STAB NUTPLATES 601R-55-11-375A, UNDER TIP FAIRING LT SIDE RIB NR 9. REPAIRED IAW REO 601R-55-11-465, REV A.
CARGO DOOR HANDLE HOUSING GOUGED AND FOUND TO BE CRACKED. R & R HANDLE, PN H3415-31 IAW SRM 51-40-11 & 51-42-21.
NOSE HYD COMPARTMENT FWD UPPER ACCUMULATOR O/B BRACKET IS CRACKED. REMOVED AND REPLACED BRACKET IAW SRM 51-42-21.
TOP CENTER OUTER SKIN ON CARGO DOOR IS GOUGED/CHAFED. REPAIRED IAW REO 601R-52-31-213.
PAX DOOR INNER SKIN AT PANEL 832AL IS CRACKED AT OTBD NUTPLATE. REMOVED DAMAGED AND INSTALLED 1 EA DOUBLER AND 2 EA FILLERS IAW REO 601R-52-11-2165.
LEFT T/R BLOCKER DOOR NR 8, INBD LUG BROKEN. R & R PN 228-50758-857 IAW CMM 78-30-04, SRS 087.
LEFT OTBD FLAP, OTBD HINGE HAS FOD DAMAGE ON HINGE BOX AND HINGE ARM. REPAIRED IAW REO 601R-57-21-1938, REV A.
RIGHT OTDB GROUND SPOILER DENTED ON UPPER SURFACE. WITHIN ALLOWABLE LIMITS IAW REO 601R-57-72-214.
PAX DOOR AFT DRAG ANGLE CRACKED. REMOVED AND INSTALLED NEW SERVICEABLE DRAG ANGLE IAW SRM 51-42-06, 51-40-11, 51-25-06, 51-25-16.
PRESSURE TRANSDUCER BRACKET IN LEFT WHEEL WELL IS CRACKED. R & R LEFT PRESSURE TRANSDUCER BRACKET.
LEFT MLG DOOR AFT EDGE IS CHAFED. REPAIRED LEFT MLG DOOR AFT EDGE IAW REO 601R--52-82-367, REV.
WHILE PERFORMING COLD WORKING OF LOWER FLANGE OF MLG TRUNNION FITTING FOUND 1 EA OVERSIZED HOLE ON RT SIDE AND 2 EA OVERSIZED HOLES ON LT SIDE. REPAIRED IAW REO 601R-57-21-1932, REV A.
RIGHT BATT RIB IN THE RT WHEEL WELL IS CRACKED. PERFORMED DOUBLER REPAIR IAW REO 601R-57-51-046.
CREW ESCAPE HATCH LT HINGE ARM IS CHAFED. BLENDED OUT CHAFE DAMAGE IAW REO 601R-52-22-030.
SPOILER OTBD SPRING SEAL IS CRACKED. R & R CRACKED SEAL IAW SRM.
PRESSURE TRANSDUCER BRACKET IN RT WHEEL WELL IS CRACKED, PN 601R75262-157, REV K, R & R.
RIGHT INBD FLAP VANE CHAFED WHERE IT HITS INBD STOP. R & R WITH NEW SERVICEABLE PN 601R14303-545 IAW SRM 51-42-13.
LEFT INBD FLAP VANE CHAFED WHERE IT HITS THE INBD STRIP. REMOVED UNSERVICEABLE LT INBD FLAP VANE INBD L/E LOCATED DRILLED AND INSTALLED NEW SERVICEABLE LT INBD FLAP VANE INBD L/E IAW SRM 51-40-11, 51-42-13, O/N 601R14303-535.
INTERCOSTAL ATTACH ANGLE CRACKED AT RBL 27 AND FS 484. REPLACED ATTACH ANGLE.
CORROSION ON TOP OF FLOOR SUPPORT STRUCTURE RBL 36 AND FS 559. REMOVED CORROSION ON RT FLOOR SILL AT 359 IAW REO 601R-53-41-666, REV C. REMOVED UNSERVICEABLE STRAP AT FS 559, RBL 27 TO RBL 36. FABRICATED AND INSTALLED NEW SERVICEABLE STRAP.
CARGO DOOR NET SUPPORT UPPER AFT MOUNTING CLIP IS CRACKED. REMOVED UNSERVICEABLE CLIP AND INSTALLED SERVICEABLE CLIP ON CARGO DOOR NET SUPPORT IAW SRM 51-42-21, 53-61-23 AND 51-24-16.
RIGHT WINDSHIELD HEAT CAUTION MESSAGE ON TAXI OUT. INSPECTED AND CLEANED RT WINDSHIELD, PERFORMED OPS CHECK IAW AMM 30-41-00, OPS CHECKED GOOD, ACFT OK FOR SERVICE.
LEFT JET OVERHEAT FAIL CAUTION INTERMITTENT IN FLIGHT THREE DING AUDIO AND RED. FOUND ALL FOUR JET PIPE CONECTIONS CHAFING ON LOWER COWL INSTALLED NEW TERM ENDS AND ROUTED AWAY FROM COWL. OPS CHECK GOOD OF LT JET PIPE AT THIS TIME IAW AMM 26-11-04. REMOVED PLACARD AND FROM MEL.
LT LOWER CORE COWL HAS 4 CHAFED AREAS. REPAIRED IAW REO 601R-71-12-4064.
LT HORIZ TIP FAIRING HAS SEVERAL UNSERVICEABLE NUT PLATES. REPAIRED LT NUT PLATES ON HORIZ TIP FAIRING ATTACH IAW REO 601R-55-11-375.
CARGO DOOR HAS DEEP CHAFE IN THE TOP CENTER OF SKIN. REPAIRED REO 601R-53-31-157 DAMAGE DEPTH .037.
GALLEY DOOR HANDLE CUT OUT GOUGED ON AFT SIDE REPAIRED IAW REO 601R-52-41-182.
LT LWR CORE COWL INNER SKIN HAD 3 DENTS OUT OF LIMITS. CUT AWAY DAMAGE C/W, REO 601R-71-12-4064 AND CMM 71-12-01. REPAIR NR SRS 095 AND SRS 021.
LT MLG DOOR CHAFING AT FWD CORNER. C/W REO 601R-52-82-034 AND SRM 52-82-00.
LT THRUST REVERSER LOWER OTBD TRACK AND LUG ARE CHAFED. REPAIRED DAMAGE IAW REO 601R-78-34-2435, REV E.
RT AILERON LOWER L/E IS CHAFED. BLENDED OUT CHAFING DAMAGE ON RT AILERON LOWER L/E AND RESTORED TO ORIGINAL FINISH (ALODINE, PRIME AND PAINT) IAW REO 601R-57-60-020.
RT AILERON UPPER L/E IS CHAFED. BLENDED OUT CHAFING DAMAGE ON RT AILERON UPPER L/E AND RESTORED TO ORIGINAL FINISH IAW REO 601R-57-60-013.
APU LINE ON ACTUATOR ATTACH BRACKETS ARE CRACKED. REMOVED UNSERVICEABLE ATTACH BRACKET, LOCATED AND DRILLED AND INSTALLED IAW SRM 51-42-06 AND 51-40-11.
FS 461.0 BATHTUB FITTING CRACKED, RBL 9.0 JUST BELOW FLOOR. REMOVED UNSERVICEABLE BATHTUB FITTING ON RBL 9.0, FS 461.0. LOCATED AND DRILLED SERVICEABLE BATHTUB FITTING AND INSTALLED AIW SRM 51-42-21 & 51-42-06.
LT UPPER PYLON TRACK PN 228-50200-809 GOUGE 0.4" X 0.4" MAX DEPTH 0.070" BLENDED AND APPLIED PROTECTIVE TREATMENT IAW REO 601R-78-30-4069.
PAX DOOR SEAL RETAINER IS GOUGED ON THE TOP EDGE NEXT TO SENSOR TARGET. R & R TOP EDGE PAX DOOR SEAL RETAINER IAW CRJ.
RT AND LT OBLIQUES ARE CRACKED. REMOVED UNSERVICEABLE RT AND LT OBLIQUES AND REPLACED WITH SERVICEABLE PN 601-35012-51 AND 601-35012-52 IAW SRM 51-42-06 AND REO 601R-53-61-422.
BULKHEAD DAMAGED AT FS 621.00. REPAIRED BULKHEAD WEB AT FS 621.00, RBL 9.0 BY INCORPORATING PERMANENT REPAIR IAW REO 601R-53-61-1285, REV B.
INTERCOSTAL UNDER PAX DOOR PANEL 832BR IS CRACKED. R & R INTERCOSTAL UNDER PAX DOOR PANEL PANEL 832BR IAW SRM 51-42-06 & 51-42-21.
CLIPS ARE CRACKED AT RBL 9.0, OTBD AND INBD, LBL 9.0 INBD. R & R CLIPS RBL 9.0 OTBD AND INBD AND LBL 9.0 INBD IAW SRM 51-42-06 AND REO 601R-53-21-064, REV NC.
LT WING PANEL 559AB HAS CHAFING BLENDED AREA AND FOUND TO BE WITHIN SERVICEABLE LIMITS (MAX MATERIAL REMOVED .004" IAW REO 601R-57-60-020.
LT WING PANEL 599AB HAS CHAFING BLENDED AREA AND FOUND TO BE WITHIN SERVICEABLE LIMITS ( MAX MATERIAL REMOVED .004" IAW REO 601R-57-60-020.
LT AILERON UPPER L/E CHAFED. BLENDED OUT DAMAGE AND FOUND TO BE WITHIN SERVICEABLE LIMITS, MAX MATERIAL LOSS 0.010" IAW REO 601R-57-60-013.
LT AILERON LOWER CENTER AND OTBD L/E HAS CHAFING, BLENDED OUT DAMAGE AND FOUND TO BE WITHIN SERVICEABLE LIMITS, MAX MATERIAL LOSS .005" IAW REO 601R-57-60-020.
LT AILERON LOWER CENTER AND OTBD L/E HAS CHAFING BLENDED OUT DAMAGE AND FOUND TO BE WITHIN SERVICEABLE LIMITS, MAX MATERIAL LOSS .005" IAW REO 601R-57-60-020.
LT AILERON UPPER SKIN L/E CHAFED ON INBD AND OTBD END. REPAIRED LT AILERON UPPER SKIN L/E. INBD AND OTBD END IAW REO 601R-57-60-013.
LT AILERON UPPER SKIN L/E CHAFED AND INBD AND OTBD END. REPLACED LT AILERON UPPER SKIN L/E, INBD AND OTBD END IAW REO 601R-57-60-013.
LT UPPER NOSE COWL T/E SEAL CHAFED. R & R LT UPPER NOSE COWL SEAL IAW CMM 71-14-01.
FWD CLIP AT FS 320.10 ON LOWER END OF PAX DOOR IS CORRODED. R & R FWD CLIP AT FS 320.10 ON LOWER END OF PAX DOOR IAW SRM 51-42-06 & 51-42-21.
CARGO DOOR HANDLE CUT OUT IS GOUGED. BLENDED GOUGE IN CARGO DOOR HANDLE CUT OUT TO A SMOOTH CONTOUR. DID NOT EXCEED DIMENSIONS STATED IN REO 601R-52-31-086 IAW SRM 51-12-00.
LT WINDSHIELD CRACK BEGINNING AT WINDSHIELD HEATING ELEMENT. R & R LT WINDSHIELD IAW AMM 56-11-01 & OPS TEST IAW AMM 30-41-01.
SMOKE TOILET CAUTION MSG DURING APPROACH TO LAND WITH BLEED AIR TRANSFER TO APU. BURING SMELL WAS NOTICED. TRANSFERRED BLEEDS BACK TO ENG AND SMELL DISSAPATED, C/W QRH. VERVIED ODOR IS COMING FROM APU. REF 210866/3 FOR MEL OF APU.
PRIOR TO T/O, APU AUTO SHUTDOWN DUE TO DEICING. APU RESTARTED PACKED NORMALLY. CABIN FILLED MIST. CLEARED WITHOUT ANY ACTION. CLEANED APU ENCLOSURE AND CONTAMINATION DUCTING IAW SUPPLEMENT 09-37A NO ODORS OR MIST NOTICE.
ON GROUND AFTER APU START AND BLEED TRANSFER FUEL ODOR FROM PACKS USING APU BLEED AIR PACKS WERE OK, O ENG. INSPECTED APU, NO OBVIOUS FUEL LEAKAGE WITH APU RUNNING, RAN PACKS OFF ENG BLEED AIR, NO ODOR NOTED, COMPLIED WITH CM ACTION, PLACED APU ON MEL.
DURING CRUISE FLT RECEIVED UNCOMMANDED FLT SPOILER DEPLOY CAUTION MSG WITH FLT SPOILER HANDLE IN STOWED POSITION. HAD A LIGHT BUFFET ASSOCIATED WITH CAUTION MSG. REF QRH NO FURTHER PILOT ACTION REQUIRED. FLT SPOILER DEPLOY CAUTION MSG APPEARED 3 TIMES. R & R RT FLIGHT SPOILER OTBD PCU IAW AMM 27-62-01. CHECKS GOOD NO LEAKS NOTED.
DURING CRUISE FLIGHT ACFT ROLLED LT UNCOMMANDED AND A FEW SECONDS LATER RECEIVED FLIGHT SPOILER DEPLOY CAUTION MESSAGE. REF QRH. FLIGHT SPOILER HANDLE WAS FULLY STOWED. CAUTION MESSAGE APPEARED AND DISSAPPEARED SEVERAL TIMES. ALSO RECEIVED INTERMITTENT CAS MIS-COMPARE MESSAGE. FLIGHT SPOILER FAULT MESSAGE STAYED ON THE ENTIRE TIME UNTIL ACFT TAXIED INTO GATE AND FLIGHT SPOILER FAULT DISAPPEARED. REMOVED AND REPLACED SECU NR 2 IAW 27-61-05, OPS CHECK IAW 27-61-00. OPS CHECK GOOD. (K)
PILOTS BULKHEAD WEB IS GOUGED. PILOTS BULKHEAD WEB REPAIRED IAW REO 601R-53-11-1677. (K)
AFT PRESSURE BULKHEAD WEB IS CRACKED AT FS 621.00, LBL 27.50, WL 130.00, ABOVE THE CARGO DOOR TRACK. AFT PRESSURE BULKHEAD WEB AT FS 621.00, LBL 27.50, WL 130.00. REPAIRED IAW REO 601R-53-61-1541, REB B. (K)
REWORK RT AND LT UPPER AND LOWER PYLON TO FUSELAGE FITTINGS IN ORDER TO ELIMINATE LOW EDGE DISTANCE AND FOULING CONDITION WITH THE THROTTLE CABLE. RT AND LT UPPER AND LOWER PYLON TO FUSELAGE FITTINGS TRIMMED IAW SB A601R-53-059, REV F PART C AND MODUSM TC 601R17262 DISPOSITION 9. (K)
UPPER FLOOR ANGLE IS CRACKED AT FS 28000, LBL 9.00, WL 73.00. UPPER FLOOR ANGLE AT FS280.00, LBL 9.00, WL 73.00. REPAIRED IAW REO 601R-53-11-138. (K)
CARGO DOOR FWD RAIL LWR SUPPORT CRACKED. CARGO DOOR FWD RAIL LWR SUPPORT CHANNEL REPLACED IAW SRM 51-42-06. (K)
CLIP AT FS 484.00, LBL 27.00, WL 72.00 IS CRACKED. CLIP AT FS 484.00, LBL 27.00, WL 72.00. REPLACED IAW SRM 51-42-20. (K)
FLIGHT COMPARTMENT BULKHEAD CROSSBEAM F/S 280, RBL 9, WL 72.00 CRACKED (CRACK LENGTH .500) FLIGHT COMPARTMENT BULKHEAD CROSSBEAM F/S 280, RBL 9, WL 72.00 REPAIR CARRIED OUT IAW REO 601R-53-11-171, REV D. (K)
INTERCOSTAL AT F/S 484.00, LBL 36.0, WL 72.0 IS CRACKED. CRACK LENGTH IS .450" INTERCOSTAL AT F/S 484.00, LBL 36.0, WL 72.0 REPAIRED IAW REO 601R-53-41-059 REV. A. (K)
INTERCOSTAL AT F/S 484.00, RBL 36.00, WL 72.00 IS CRACKED. (CRACK LENGTH IS .250") INTERCOSTAL AT F/S 484.00, RBL 36.00, WL 72.00 REPAIRED IAW REO 601R-53-41-059, REV A. (K)
CLIP AT FS 484.00, RBL 27.00, WL 72.00 IS CRACKED. CLIP AT FS 484.00, RBL 27.00, WL 72.00. REPLACED IAW SRM 51-42-06 AND 51-42-20. (K)
PASSENGER DOOR STAIR AFT DRAG ANGLE FOUND CRACKED AT PULLEY BRACKET LOCATION. PAX DOOR STAIR ASSY AFT DRAG ANGLE REPAIRED IAW REO 601R-52-11-513 REV A. (K)
PASSENGER DOOR STAIRS FWD STAIRS FWD SIDE PANEL CRACKED IN ZONE NR 2 (REF REO 601R-52-11-702, REV A). PAX DOOR STAIR ASSY FWD PANEL REPAIRED IAW REO 601R-52-11-702, REV A. (K)
PASSENGER DOOR STAIRS AFT SIDE PANEL FOUND CRACKED IN ZONE 2 AND ZONE 3 (REF: REO 601R-52-11-702, REV A) PAX DOOR STAIR ASSY AFT SIDE PANEL REPAIRED IAW REO 601R-52-11-702, REV A. (K)
CRACK FOUND ON FWD PRESSURE BULKHEAD FS 202.75, LBL 23.71, CRACK LENGTH IS .500. FWD PRESSURE BULKHEAD REPAIRED IAW REO 601R-53-11-563. (K)
APU ENCLOSURE IS CRACKED. APU ENCLOSURE REPAIRED IAW REO 601R-49-11-071. (K)
PAX DOOR HANDLE FOUND CRACKED AT 4 PLACES. PAX DOOR HANDLE REPLACED IAW AMM 52-11-03-400-802. (K)
PASSENGER DOOR EDGE MEMBER FOUND CRACKED ON AFT SECTION. PAX DOOR EDGE MEMBER REPAIRED IAW REO 601R-52-11-279. (K)
CREW EMERGENCY HATCH OUT HANDLE CAN`T EJECT. CORROSION FOUND ON OUTER HANDLE SHAFT. CREW EMERGENCY HATCH OUTER HANDLE REPLACED IAW AMM TASK 52-22-03-400-801. (K)
AFT PRESSURE BULKHEAD WEB AT FS 621.00, LBL 45.00, WL 110.00, IS CRACKED AT THE LINTEL INSTALLATION. AFT PRESSURE BULKHEAD AT FS 621.00, LBL 45.00, WL 110.00. REPAIRED IAW REO 601R-53-61-1230, REV D. (K)
14TH DUCT O/H, C/W QRH RED LENG TO IDLET MSG WENT AWAY AND REAPPEARED 5 MINUTES LATER. LANDING WEIGHT 49,000, BTMS 6-5-5-6. REMOVED AND REPLACED LT PYLON 14TH STAGE LENS ELEMENT A59WK IAW AMM 36-21-04. OPS AND LEAK CHECK NORMAL. (K)
DISPLAY COOL CAUTION MSG IN FLIGHT, C/W`D QRH, AT FLT LEVEL 270. REMOVED AND REPLACED FAN NR 1 IAW AMM 21-24-19, OPS CHECK GOOD. (K)
SMOKE IN COCKPIT WHEN FO TURNED FLOODLIGHT ON. TURNED OFF FLOODLIGHT AND SMOKE WENT AWAY.
INFLIGHT, RT N2 GAUGE READS ZERO APPROXIMATELY 30 MINUTES INTO FLIGHT. CLEANED BLUE HARNESS CONNECTOR W8P2 AT RT ALTERNATOR IAW 73-21-13 AND AWAC SUPP 06-003, OPS CHECK GOOD. (K)
(2) EA CRACKED ANGLES AT FS 280.0, RBL 9.0. MAINTENANCE REMOVED AND REPLACED ANGLES AT FS 280.00, RBL 9 IAW SRM AND BSC SR 601R-53-0057A. (K)
2 EA, CRACKED ANGLES AT FS 280, LBL 9.0. MAINTENANCE REMOVED AND REPLACED ANGLES AT FS280, LBL 9 CRJ 200, SRM 51-42-21 AND BSC SR 601R-53-0057A. (K)
FS 484.0 LT LBL 27.0, WL 71.0 TO 73.5 ANGLE CRACKED. MAINTENANCE REMOVED AND REPLACED CRACKED ANGLE AT FS 484.00, LBL 27.0 IAW REO 601R53-41-059. (K)
LT FLOOR SUPPORT STRUCTURE IS CRACKED AT FS 621.00. MAINTENANCE REPAIRED FLOOR SUPPORT BY CUTTING OUT DAMAGED ANGLE, FABBING REPAIR PARTS AND INSTALLING IAW REO 601R53-61-717, REV C AND BSC EO 601R-53-12256. (K)
RT FLOOR SUPPORT STRUCTURE IS CRACKED AT FS 621.00. MAINTENANCE REPAIRED RT FS 621 IAW REO 601R53-61-117 REV C. (K)
PAX DOOR AFT DRAG ANGLE CRACKED APROX .7 INCH LONG IN AREA OF PULLEY BRACKET. MAINTENANCE CUT AWAY CRACKED SECTION OF DRAG ANGLE AND INSTALLED REPAIR ANGLE IAW REO 601R52-11-513, REV A. (K)
LT SIDE FS 621.00 TO FS 625.30 INTERCOSTAL AT STR 14L IS CRACKED NEAR RADIUS APPROX 1.1 INCH LONG. MAINTENANCE REMOVED AND REPLACED LT SIDE FS 621.00 TO 625.00 INTERCOSTAL AT STR 14L IAW CRJ 200, SRM 51-42-06. (K)
RT SIDE FS 621.00 TO 625.30 INTERCOSTAL AT STR 14R IS CRACKED NEAR RADIUS APPROX 1.0 INCH LONG. MAINTENANCE REMOVED AND REPLACED RT SIDE FS621.00 TO 625..00 INTERCOSTAL AT STR 14 R IAW CRJ 200 SRM 51-42-06. (K)
DURING APPROACH SPOILERONS CAUTION AND OUTBOARD GROUND SPOILERS CAUTION MESSAGE ILLUMINATED, COMPLIED WITH QRH, PREFORMED FLAP 20 DEGREES LANDING. PERFORMED FUNCTION TEST OF SPOILER IAW AMM 27-61-00. OPS CHECK GOOD AT THIS TIME. (M)
FOUND DENT IN LEFT SKIN FROM FS 235 TO FS 265 BETWEEN STRINGER 17L AND STRINGER 19L. REPAIRED DENT IN FUSELAGE SKIN FROM FS 235 TO FS 265 BETWEEN STRINGER 17L AND STRINGER 19L IAW BRAS EO 601R-53-5788A. (M)
DENT ON LT SKIN FROM FS 193, 00 TP FS 202.75 BETWEEN STR 18L AND STR 20L. REPAIRED DENT IN FUSELAGE SKIN FROM FS 193.00 TO FS 202.75 BETWEEN STR 18L AND 20L IAW BRAS EO. (K)
THE RIGHT FUSELAGE SKIN WAS DAMAGED WHEN THE SERVICE DOOR WAS OPENED WHILE PRESSURIZED. PERFORMED A MAJOR REPAIR TO RIGHT SIDE OF FUSELAGE SKIN AT FS 298.5 BETWEEN STRINGERS 13R AND 14R USING STANDARD SHOP PRACTICES. FABRICATED STIFFENER FROM 2024-T3 .063 INCH TO EXTEND BETWEEN TWO STRINGERS UNDER THE DENTED AREA IAW BRAS EO 601R-53-4835. (M)
THE RIGHT FUSELAGE SKIN WAS DAMAGED WHEN THE SERVICE DOOR WAS OPENED WHILE PRESSURIZED. FUSELAGE SKIN WAS DENTED BETWEEN STRINGERS 13/14 APPROX 3.5 INCHES AFT OF FS 295 AND DENTED WITH A CREASE BETWEEN STRINGERS 16/17 AT FS 295. TRIMMED OUT SKIN PANEL AND FRAME FLANGE. ALL CRACKS REMOVED. REPAIRED FRAME FLANGE BY FABRICATING REPAIR ANGLE. ALL WORK DONE IAW BRAS EO 601R-53-4835. (M)
FORWARD SERVICE DOOR JAMMED. TWO DENTS FORWARD OF RT FORWARD SERVICE DOOR. DENTS OUT OF LIMITS. COMPLIED WITH REPAIR BRAS EO 601R-53-4835 STEPS 1, 2, 3, 4 AND 5. PERFORMED REPAIR OF SERVICE DOOR STRINGER 16/17 OF FIG 245 AND STRINGER 13/14 FIG 295. (M)