N470ZW
Registered owner: CSI AVIATION INC, TX (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
Maintenance disclosures
DURING CRUISE AT 30,000FT FOR FLIGHT 6024 CAE-ORD, THE FLIGHT CREW REPORTED A LOSS OF ELECTRICAL POWER. THE FLIGHT CREW DECLARED AN EMERGENCY AND IS RETURNING TO CAE. THIS FLIGHT IS STILL ENROUTE. SHORTLY AFTER LEVEL OFF AT CRUSE RECEIVED GEN 2 FAIL AND AC 2 AUTO XFER FAIL CAUTIONS. C/W QRH AND RETURNED TO CAE. ONLY BUSS 1 AND ESS BUS BEING POWERED. ADG DID NOT DEPLOY. AIRCRAFT REMOVED FROM SERVICE SERVICED #2 IDG IAW AWA SUPP 16-364A. C/W OPS TEST OF #2 IDG IAW AMM 24-11-00. C/W FUNCTIONAL TEST OF AC POWER TRANSFER CIRCUIT IAW AMM 24-20-00. ALL TESTS GOOD.
FLAP FAIL AT ZERO IN CRUISE AIRCRAFT REMOVED FROM SERVICE R+R LH BPSU IAW SUPP 04-048B. OPS CHECK GOOD. REMOVED PLACARD + REMOVED FROM MEL. P/N 855D100-15 S/N OFF 2363 S/N ON 2480 KSG
WHILE EXTENDING FLAP TO 8 DEG ON APPROACH, RCVD "FLAP FAIL" CAUTION MESSAGE. PERFORMED FLAP RESET PROCEDURE IAW AWAC SUPPLEMENT 98-18IBOX 12. FLAPS RESET. PLACARED AND PLACED ON MEL ***** AIRCRAFT REMOVED FROM SERVICE ***** R/R LFT BPSU OPS CHECK GOOD AT THIS TIME. REF AMM 27-51-10 REMOVED PLACARDE AND REMOVED FROM MEL PN OFF: 855D100-15 PN ON: 855D100-15 SN OFF: 1809 SN ON: 2363
RECEIVED FLAP FAIL CAUTION AT FL 230 IN CRUISE. COMPLETED AND COMPLETED WITH QRH BTMS READ 6,5,4,6 PERFORMED FLAP RESET PROCEDURE IAW AWAC SUPPLMENT 98-018I BOX 12 FLAPS RESET PLACARDED AND PLACED ON MEL ***** AIRCRAFT REMOVED FROM SERVICE R & R FECU/ ADJUSTED BOTH BPSU POSTION. REMOVE PLACARD AND REMOVE FROM MEL.
UPON DESCENT FROM CRUISE, FLAPS FAIL AT 0 DEGREES C/W QRH. FLAP HANDLE WAS NOT TOUCHED. AIRCRAFT REMOVED FROM SERVICE. ADJUSTED FLAP FECU POTENTIOMETERS IAW AMM 27-51-10 SUBTASK 27-51-10-830/008, REF 353376-3 FOR TS PER AWAC SUPP 98-018I. OPS CK GOOD.
AT FL240, RECEIVED FLAPS FAIL CAUTION MESSAGE. FLAPS AT 0 DEGREES. BTMS TEMPS 4,3,4 AND 7. PERFORMED FLAP RESET PROCEDURE IAW AWAC SUPPLEMENT 98-18I, BOX 12. FLAPS RESET. PLACARDED AND PLACED ON MEL. AIRCRAFT REMOVED FROM SERVICE. FLAPS PLACED ON MEL AND JOB-CARD SCHEDULED TO INTERROGATE FECU FOR FAULT CODES AND TROUBLESHOOT PER CRJ200 FIM. FECU 5-8 OUT OF ADJUSTMENT . REF 353376-2 FOR CORRECTIVE, REF 353376-4 FOR FECU FAULT LOG CODES
AFTER TAKE OFF RECEIVED NWS CAUTION MSG AND WOW INPUT. MSGS APPEARED APROX 6 SECONDS AFTER GEAR SELECTION. C/W QRH MGS PERSISTED, DURRING APPROCH; WITH GEAR UP AND FLAPS AT 0, MSGS CLEARED. AIRCRAFT REMOVED FROM SERVICE. PERFORMED NLG PROX SENSOR ADJUSTMNETS AND NOSE WHEEL STEERING OP CHECK IAW AWA SUP 12-029E FROM SUB TASK 32-61-05-980-019AW THRU CLOSE OUT. ALL OPS CHECK GOOD. R&R NLG WOW #2 AND SENSOR/EXTENDED PROX SENSOR HARNESS.
30 SECONDS AFTER TAKE-OFF, RECEIVED NWS INOP CAUTION MESSAGE. C/W QRH. MESSAGE DID NOT CLEAR. AIRCRAFT REMOVED FROM SERVICE. REF WO 334202 WC #9 FOR CORRECTIVE ACTION. R & R RVTD WO 334202: INSTALLED AND RIGGED LT NWS RVDT PER AMM SUP 15-177A AND RIGGED PER AMM 32-51-20, VOLTAGE VALUES AND OPERATIONAL CHECK GOOD AT THIS TIME
AFTER T/O RECEIVED HAD NOSE DOOR AND GEAR DISAGREE WARNING MSG RAN QRH ALL GEAR WAS EXTENDED. MSG APPEARED APROX 5 SECONDS OF HANDLE MOVEMENT. LANDING WEIGHT 44,000LBS. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED NLG CENTERED/EXTENDED BRACKET IAW AMM 32-21-01 R&R NLG PROX SENSOR CENTERED/EXT HARNESS IAW AMM 32-61-25 ADJUSTED NLG CENTERED/PROX SENSOR IAW AMM 32-61-05 REMOVED GEAR PINS IAW AMM 10-11-01 C/W LDG EXT/RET IAW AMM 32-30-00. OPS CK GOOD
DURING CLIMB OUT RT ENG ITT SPIKED TO 980 PLUS DEGREES SOUND (BANG) AND VIBRATION HEARD, RT FUEL LOW PRESSURE CAUTION MSG RECEIVED C/W QRH RH ENGINE UNRESPONSIVE. CONT LOG PAGE 363235/1 SELECTED IDLE, INDICATIONS AS FOLLOWS, N1 28 %, ITT 750 DEG C, N2 57 %, AFTER LANDING SHUT ENGINE DOWN, LANDING WEIGHT 47800 LBS, NORMAL LANDING. REF WO 332590 FOR REMOVAL AND REPLACEMENT OF RH ENG. NO INSPECT FOR REQUIRED FOR OVERWEIGHT LANDING PER AWA SUPP 16-306D.
AT 12K FT RECEIVED MLG BAY OVERHEAT MESSAGE. C/W QRH MESSAGE REMAINED. BTMS READ 1'S. GEAR WAS DOWN. ALL TEMP INDICATIONS NORMAL. *******AIRCRAFT REMOVED FROM SERVICE*********** REF 352283-1 FOR CORRECTIVE ACTION R+R WHEEL BINS. R+R BOTH WHEEL BINS, OPS CHECK GOOD REF AMM 53-83 REMOVED PLACARD AND FROM MEL.
9883 - OXY LO PRESS AT 1180 PSI NEED REPLENISHED. AIRCRAFT REMOVED FROM SERVICE. SERVICED CREW O2 TO 1820 PSI. IAW AWAC SUP 09-053E
TOOLING MARKS ON LH FS424.00 ****AIRCRAFT REMOVED FROM SERVICE******* BLENDED TOOL MARKINGS ON LH SKIRT DOUBLER PN 601R31145 -323 AT FS424.00 UNDER ACCESS PANEL WING TO FUSELAGE FRAME ATTACHMENT FWD 161CL. PERFORMED HFEC WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW CRJ200 SRM 51-11-00, SRM 51-12-00, SRM 51-25-06, SRM 51-25-16, SRM 51-26-00, SRM 53-41-45 REV 39, AND EA#: AWAC-CRJ253-01990 DATE ISSUED 5/15/2023 REV IR. WORK PERFORMED UNDER AERSALE WORK ORDER 003911, CARD NO.20066, TT: 38,125:30 TC: 36,944.
CORROSION ON FLOOR SILL PN601R31132-58 AT FS409.00+80 TO FS 409.00+112 AND RBL42. ***** AC REMOVED FROM SERVICE ***** P1 - L= 3.40IN X W= 0.600IN X D= 0.003IN FS409.00+96 P2 - L= 0.700IN X W= 0.700INX D= 0.002IN FS409.00+98 P3 - L= 1.900IN X W= 1.200IN X D= 0.013IN FS409.00+103 P4 - L= 1.800N X W= 0.900IN X D= 0.003IN FS409.00+112 REMOVED CORROSION AT FLOOR SILL SUPPORT LOCATION P1-P4 BETWEEN FS409.00+80 TO FS409.00+112 AND RBL42. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW CRJ200 SRM 51-21-00 REV 39, SRM 51-21-11 REV 39, SRM 51- 21-16 REV 39, SRM 51-26-00 REV 39, SRM 53-31-43 REV 39, AND SRM 53-00-00 REV 39 AND AWAC-CRJ253-01982 REV WORK PERFORMED UNDER AERSALE WORK ORDER 003911, CARD NO.20136, TT: 38,125:30 TC: 36,944.
HORIZONTAL AND VERTICAL STAB PIVOT BUSHINGS ARE WORN BEYOND LIMITS. ******AIRCRAFT REMOVED FROM SERVICE****** HORIZONTAL AND VERTICAL STAB PIVOT BUSHINGS ARE WORN BEYOND LIMITS. P1A- L=2.00IN X W 0.1968IN X D=0.001IN P1B- L=2.00IN X W 0.3543IN X D=0.002IN. P1C- L=2.00IN X W 0.1968IN X D=0.001IN P2A- L=3.50N X W 0.275IN X D=0.003IN P2B L=3.50N X W 0.393IN X D=0.002IN P2C- L=3.50IN X W 0.157IN X D=0.001IN P2D- L=3.50IN X W 0.118IN X D=0.001IN P3C-L0.590IN X W=0.625INXD 0.0026IN EVALUATED DAMAGE FOUND BUSHINGS TO BE OUT OF LIMITS. INSTALLED NEW LH AND RH PIVOTS PN 600-2107-3. PERFORMED HFEC WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW MHIRJ REO 601R-55-11- 744 REV-- DATED 2023/05/08 AND CRJ SRM 51-11-00 REV 39. WORK PERFORMED UNDER AERSALE WORK ORDER 003911 CARD NO.20153, TT: 38,125:30 TC: 36,944
CORROSION ON LH FLOOR SILL P/N: 601R31133-47 AND P/N: 601R31133-77 AT FS 574.00+ 12 TO FS 605+12 AND LBL42. CRACK 0.300ÿ½L X 0.010ÿ½W ON L/H FLOOR LANDING PLATE P/N: 601R35001-63 AT FS 605.00 AND LBL 42. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION AT FLOOR SILL SUPPORT LOCATION P1-P13 BETWEEN FS574.00+12 TO FS605+12 AND LBL42 IAW BOMBARDIER GREO 601R-53-00-526 REV (--) DATED 22 MAY 2013. RESTORED PROTECTIVE FINISH. PREFORMED EDGE BLEND REMOVING CRACK AT LBL 42 IAW ASAP EA # AWAC-CRJ253-01985 DATE 6/3/2023 REV B. ALL WORK WITHIN LIMITS WAS PERFORMED IAW CRJ200 SRM 51-21-00 REV 39, SRM 51-21-11 REV 39, SRM 51-21-16 REV 39, SRM 51-26-00 REV 39, SRM 53-31-43 REV 39, AND SRM 53-00-00 REV 39. WORK PERFORMED UNDER WORK ORDER 003911.
CORROSION ON FLOOR SILL STRAP P/N 601R31025-29 AT FS280.00 AND LBL 9 TO RBL9. ***** AC REMOVED FROM SERVICE ***** BLENDED CORROSION ON 3 AREAS AT FS280.00 RBL9 TO LBL9. P1-L=2.5IN X W=1.5IN X D=0.036 P2-L=4IN X W=1IN X D=0.037 P3-L=3ININ X W=1.5 X D=0.037 REPLACED FLOOR SILL STRAP WITH A NEW FABRICATED STRAP P/N 600-34017-351 AT FS280.00 AND LBL9 AND RBL 9. NEW REPAIRED PARTS SPLICE ANGLE PN 601R-53-11-136-3/4 AT LBL12.5 AND RBL 12.5, FILLER ANGLE PN 601R53-11-136-1 BTW LBL 12.5 AND RBL 12.5, AND ANGLE SUPPORT PN 600-34017-3515 BTW LBL9 AND RBL 9. REPLACED CRACKED CLIP ANGLES ON 3 AREAS LBL 9 OB PN 601R3113 -57, RBL 9 IB PN 601R31113-58 AND RBL 9 OB PN 601R31113-58. PREFORMED HFEC WITH NO INDICATIONS RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW MHIRJ REO601R-53-11- 136 REV A DATE 2007/11/01, CRJ200 SRM 53-11-19 REV 39, SRM 51- 26-00 REV 39, SRM 51-26-06 REV 39, SRM 51-11-00 REV 39, SRM 51 -42-06 REV 39, SRM 51-42-21 REV 39, SRM51-42-20 REV 39, SRM 51 -42-10 REV 39, AND SRM 53-00-00 REV 39. WORK PERFORMED UNDER AERSALE WORK ORDER 003911, CARD NO. 20137, N470ZW TT: 38,125: 30 TC: 36,944.
SEAT TRACK PN 20276-288-0-0 AT FS349.00ÿ½ FS599.00+112 LHS HAS CORROSION AT NUMEROUS LOCATIONS. ***** AC REMOVED FROM SERVICE ***** BLENDED CORROSION ON SEAT TRACK PN 20276-288-0-0 AT FS349.00 ÿ½ FS599.00+112 LH PN 20276-144-0-0. DIMENSIONS P1 L= 63IN X W= 1.250IN X D= 0. 010IN P2-L=94IN X W=1.250 X D=0.13 P3-L=56IN X W=1.250IN X D=0. 015. PREFORMED HFEC WITH NO INDICATIONS. ALL WORK WITH IN LIMITS WAS PERFORMED IAW CRJ200 SUPPLEMENT NO.13-074 DATE 8/14/2013, SRM 53-41-49 REV 39, SRM 53-21-49 REV 39, SRM 53- 01-11 REV 39, SRM 53-00-49 REV 39, SRM 51-25-06 REV 39, SRM 51-25-16 REV 39, SRM 51-21-11 REV 39SRM 51-26-00 REV 39, SRM 53-01-11REV 39, AND SRM 51-40-11 REV 39WORK PERFORMED UNDER AERSALE WORK ORDER 003911, CARD NO. 20133, N470ZW TT: 38,125: 30 TC: 36,944.
CORROSION ON FLOOR SILL P/N 601R31145 AT FS449.85 TO FS461.50 AND LBL41-LBL42 ******AIRCRAFT REMOVED FROM SERVICE******* CORROSION ON FLOOR SILL P/N 601R31145 AT FS449.85 TO FS461.50 AND LBL41-LBL42 P11-L=1.300IN X W=1.200IN X D=0.002 P12-L=1.00IN X W=0.700IN X D=0.003 BLENDED CORROSION ON 2 AREAS ON LH FLOOR SILL AT FS449.85 TO FS461.50 AND LBL41-LBL42.PREFORMED HFEC WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW MHIRJ REO 601R-53-41-3169 REVÿ½DATE 2023/05/27. WORK PERFORMED UNDER AERSALE WORK ORDER 003911 CARD NO.20183, TT: 38,125:30 TC: 36,944
CORROSION ON CABIN FLOOR SILL RH AT FS484.00+2 TO FS484.00 +5 AND RBL 42. AIRCRAFT REMOVED FROM SERVICE. BLENDED 4 AREAS OF CORROSION ON FLOOR SILL RH AT FS484.00+2 TO FS484.00+9 AND RBL 42. P10-L=1.200IN X W=0.800IN X D=0.003 P11-L=2.00IN X W=1.00IN X D=0.006 P12-L=1.100IN X W=1.000IN X D=0.006 P13-L=1.350IN X W=1.100IN X D=0.002 ORIGINAL THICKNESS 00.80 REMAINING THICKNESS .078 MATERIAL LOSS .002. PERFORMED HFEC WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW ASAP EA# AWAC-CRJ253-01983 DATE 5/31/2023 REV A. WORK PERFORMED UNDER AERSALE WORK ORDER 003911 CARD NO.20163, TT: 38,125:30 TC: 36,944
CORROSION ON CABIN FLOOR SILL LH AT FS461.50+6 TO FS473.15+5 AND LBL36. AIRCRAFT REMOVED FROM SERVICE. BLENDED 4 AREAS OF CORROSION ON LH FLOOR SILL AT FS513.00 TO FS529.00 AND LBL 36-38. P14-L=1.100IN X W=0.600IN X D=0.002 P15-L=1.200IN X W=0.700IN X D=0.002 P16-L=3.500IN X W=1.700IN X D=0.002 P18-L=0.800IN X W=1.200IN X D=0.002 ORIGINAL THICKNESS 00.80 REMAINING THICKNESS .078 MATERIAL LOSS .002. PERFORMED HFEC WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH . ALL WORK WITHIN LIMITS WAS PERFORMED IAW ASAP EA# AWAC-CRJ253-01987 DATE 5/27/2023 REV A. WORK PERFORMED UNDER AERSALE WORK ORDER 003911 CARD NO.20166, TT: 38,125:30 TC: 36,944
CORROSION ON CABIN FLOOR SILL LH AT FS513.00 TO FS529.00 AND LBL36-38. AIRCRAFT REMOVED FROM SERVICE. BLENDED 4 AREAS OF CORROSION ON LH FLOOR SILL AT FS513.00 TO FS529.00 AND LBL 36-38. P24-L=0.600IN X W=0.400IN X D=0.002 P25-L=1.700IN X W=0.700IN X D=0.002 P26-L=0.800IN X W=0.700IN X D=0.002 P27-L=0.600IN X W=0.400IN X D=0.002 ORIGINAL THICKNESS 00.80 REMAINING THICKNESS .078 MATERIAL LOSS .002. PERFORMED HFEC WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH . ALL WORK WITHIN LIMITS WAS PERFORMED IAW MHIRJ REO 601R-53-41-3163 DATE 5/11/2023 WORK PERFORMED UNDER AERSALE WORK ORDER 003911 CARD NO.20164, TT: 38,125:30 TC: 36,944
TWO FLANGES UNDERFLOOR PANEL 271ALF AT FS559.00+16 BLO 0 ARE NOT INSTALLED. AIRCRAFT REMOVED FROM SERVICE. DURING EVALUATION FOUND 13 OVERSIZED HOLE EFFECTING RBL 9 BL 0 AND LBL 9 ON FLOOR BEAM FLANGES AND INSTALLED NEW FLANGES PN 6010R31025-23 AND PN 601R31025-99. PERFORMED HFEC WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW MHIRJ REO 601R-53-41-3162 REV A DATED 2023/05/08 AND CRJ SRM 51-42-06 REV 39. WORK PERFORMED UNDER AERSALE WORK ORDER 003911 CARD NO.20144, TT: 38,125:30 TC: 36,944
CORROSION ON CABIN FLOOR SILL LH AT FS424.00 TO FS424.00+4 AND LBL35-38. *****AIRCRAFT REMOVED FROM SERVICE********* BLENDED 4 AREAS OF CORROSION ON LH FLOOR SILL AT F424.00 TO FS424.00+4 AND LBL 35-38. P2-L=1.800IN X W=1.400IN X D=0.002 P3-L=0.700IN X W=0.500IN X D=0.002 P4-L=1.800IN X W=0.800IN X D=0.200 P5-L=1.600IN X W=0.800IN X D=0.200 ORIGINAL THICKNESS 00.80 REMAINING THICKNESS .078 MATERIAL LOSS .002. PERFORMED HFEC WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH . ALL WORK WITHIN LIMITS WAS PERFORMED IAW ASAP EA# AWAC-CRJ 253-01986 REV A DATE 5/27/2023. WORK PERFORMED UNDER AERSALE WORK ORDER 003911 CARD NO.20164, TT: 38,125:30 TC: 36,944
CORROSION ON CABIN FLOOR SILL LH AT FS473.15 AND LBL36. *******AIRCRAFT REMOVED FROM SERVICE******* REMOVED CORROSION ON LH FLOOR SILL AT F473.15AND LBL 36. P16-L=3.500IN X W=1.700IN X D=.002 ORIGINAL THICKNESS 00.80 REMAINING THICKNESS .078 MATERIAL LOSS .002. PERFORMED HFEC WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH . ALL WORK WITHIN LIMITS WAS PERFORMED IAW ASAP EA# AWAC-CRJ 253-01988 REV A DATE 5/27/2023. WORK PERFORMED UNDER AERSALE WORK ORDER 009311, CARD NO.20167, TT: 38,125:30 TC: 36,944
CORROSION ON PASSENGER DOOR LOWER SILL BRACKETS P/N 601R31527-217 STG17L. ***** AC REMOVED FROM SERVICE ***** EVALUATED BLENDED AREA AT PASSENGER DOOR LOWER SILL BRACKETS P/N 601R31527-217 AT FS310.00+4 TO FS333+9 STG17L FOUND TO BE OUT OF LIMITS. REPLACED TWO BRACKETS TO PASSENGER DOOR SILL AT FS310.00+4 TO FS333+9 STG17L.PERFORMED HFEC WITH NO INDICATIONS. RESTORED SURFACE FINISH. ALL WORK WITHIN LIMITS PERFORMED IAW SRM 51-40-11 REV 39, SRM 51-42-06 REV 39, SRM 51-21-06 REV 39SRM51-42-06 REV 39, SRM 53-00-00 REV 39 AND SRM 53-21-23 REV 39. WORK PERFORMED UNDER AERSALE WORK ORDER 003911, CARD NO.20114, TT: 38,125:30 TC: 36,944
CORROSION ON RH FLOOR SILL STRAP PN# 601R3113-102 AT FS559. +112 TO FS621.00 RBL 42. ***** AC REMOVED FROM SERVICE ***** REPLACED FLOOR SILL WITH A NEW SILL P/N601R31133-102 AT FS559.00+80 TO FS559.00_112.RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW CRJ200 SRM 51-21-11 REV 39, SRM 51-25-06 REV 39, SRM 51-25-16 REV 39, SRM 51-42 -06 REV 39, SRM 51-40-11 REV 39, SRM 51-42-20 REV 39 SRM53- 00-00 REV 39, AND SRM 53-51-43 REV 39. WORK PERFORMED UNDER AERSALE WORK ORDER 003911, CARD NO.20140, TT: 38,125:30 TC: 36,944. PROGRESSES
CLIMBING THROUGH FL210, RECEIVED CABIN ALT CAUTION MESSAGE. BEGAN QRH, RECEIVED CABIN ALT WARNING MESSAGE. CW IAC/QRH, DIVERTED TO FWA. CABIN ALT INDICATION WAS RISING WHEN CATION MESSAGE WAS DISPLAYED. *****AIRCRAFT REMOVED FROM SERVICE******* DUE TO EXTENSIVE CABIN PRESSURE ISSUES AND SEVERAL CPAM FAIL MESSAGES WITH CPAM S/N 1524A ISNTALLED. R&R CPAP IAW AMM 21-23. OPS CHECK GOOD LEAK CHECK GOOD.
FLOOR SEAT RAIL HAS 4 EA AREAS OF CORROSION BETWEEN FS 574 TO FS 615 AND RBL 27. *************AIRCRAFT REMOVED FROM SERVICE************************* BLENDED 4 EA AREAS OF CORROSION IAW CRJ200 SRM 51-21-06 REV 39. EVALUATED BLEND AREAS AND FOUND AREAS P1 TO P3 NOT WITHIN ALLOWABLE LIMITS AND AREA P4 WITHIN ALLOWABLE LIMITS IAW CRJ200 53-61-43 REV 39 AND CRJ200 SRM 53-00-00 REV 39. REMOVED AND REPLACED FLOOR SEAT RAIL P/N: 601R35031-263 FROM FS 565 TO FS 613 AT RBL 27 IAW CRJ200 SRM 51-42-06 REV 39 AND CRJ200 SRM 51-42-20 REV 39. WORK ACCOMPLISHED ON AERSALE WO #003911 CARD #20141 CARD ID #1884445. TT: 38,125:30 TC: 36,944
STAB TRIM / MACH TRIM MESSAGE APPROX 7000 - 8000 FEET. APPROX 200 KNOTS. THEY WOULD NOT RE-ENGAGE. MULTIPLE ATTEMPTS. AUTO-PILOT NOT ENGAGED. ******AIRCRAFT REMOVED FROM SERVICE********* R/R FO PITCH TRIM DISCONNECT SWITCH IAW AMM SUP 10-048D. OPS CHECK GOOD
AILERON TRIM SLIGHTLY OUT OF ZERO R WING DOWN. WILL NOT RESPOND TO L WING DOWN TRIM SWITCH MOVEMENTS. POSITIONED TO ZERO P2-F7 COLLARD C/B P2-F7. PLACARDED AND PLACED ON MEL. ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED AND REPLACED AILERON/RUDDER TRIM PANEL PER AMM 27-12-10. OPS CHECK GOOD AT THIS TIME. REMOVED PLACARD, THIS REMOVES ITEM FROM MEL. P/N: 601R51226-23, S/N OFF: AW0156, S/N ON: AW0142 ARW
DURING APPROACH, THE CREW RECEIVED A FLAP FAILURE MESSAGE. CREW ELECTED TO GO AROUND, COORDINATE WITH DISPATCH & DECLARED AN EMERGENCY. CREW COMMUNICATED WITH F/A AND PAX, RETURNED & LANDED WITHOUT FURTHER INCIDENT. FLAPS FAILED AT 20 DEG ON APPROACH WHEN 30 DEG SELECTED. PERFORMED FLAP RESET PROCEDURE IAW AWAC SUP 98-18I BOX 12 FLAPS RESET. AIRCRAFT REMOVED FROM SERVICE. R&R FLAP HANDLE /GAURD IAW AMM 27-51-01. OPS CHECK GOOD. FAULT NO LONGER EXISTS.
RECEIVED ANTI-ICE DUCT WARNING MESSAGE IN FLIGHT. RIGHT FUSELAGE DUCT INDICATED. C/W QRH, MESSAGE PERSISTS. ***AIRCRAFT REMOVED FROM SERVICE*** R&R AFT EQUIPMENT BAY FUSELAGE AIR BLEED LEAK SENSING ELEMENT A46WK IAW AMM 36-21-04 OPS CHECK GOOD.
PILOT REPORTS APU FAILED TO START ON DESCENT FAILED TO LIGHT. AFTER 2ND ATTEMPT THERE WAS A STRONG FUEL SMELL IN AIRCRAFT. FUEL SMELL WENT AWAY AFTER THEY SHUT IT DOWN. FOUND COALESCER TO BE CONTAMINATED DUE TO APU START FAILURE. C/W AWAC SUP 09-037C. APU OPS CHECK GOOD AT THIS TIME. NO FURTHER ODORS AT THIS TIME. TROUBLESHOT, FOUND APU FUEL CONTROL TO BE FEEDING FUEL TOO MUCH. R&R APU FUEL CONTROL IAW 49-30-31, OPS CHECK GOOD. REMOVED PLACARD REMOVED FROM MEL. SN OFF 23327 SN ON 26453 LEF R&R APU FUEL SOLENOID IAW AMM CH 49-30, OPS CHECK GOOD. SN OFF 2076 SN ON T#2567 LEF
L1 DOOR HINGE LUGS FROM FWD #2, #9, #19, #30, #32, #36, #39, #46, #50, #52, HAVE GOUGES. AIRCRAFT REMOVED FROM SERVICE BLENDED LUGS #2,#9,#19,#30,#32,#36,#39,#46,#50,#52,IAW SRM 51-12-00, REV.37, AFTER BLENDING REMAINING MATERIAL THICKNESS IS AS FOLLOWS, LOG#2 .114", LOG#9 .102" LUG#19 .101" LUG#30 .117" LUG#32 .117 LUG#36 .116 LUG# 39 .116 LUG#46 .113 LUG#50 .117 LUG#52 .117, ALL LUGS ARE IN SERVICE LIMITS IAW REO 601R-52-11-1347 PERFORMED HFEC ON ALL BLENDED LUGS IAW NDTM P1 51-20-06 REV. 41 NO CRACKS FOUND
L/H I/B FLAP VANE L/E BETWEEN FLAP STA 69.631-FLAP STA 79.257 HAS GOUGE DAMAGE. AIRCRAFT REMOVED FROM SERVICE CUT OUT DAMAGED SKIN ON L/H I/B FLAP VANE AT FLAP STA 77.5 . CUTOUT DIMENSIONS ARE 1.3"W X .7"L . FABRICATED FLAP VANE INSERT AND VANE BUTT STRAP FROM 2024-T3 .050" REF CRJ 200 SRM 57-52-00 AND SRM 51-24-16 REV 37 LOCATED AND DRILLED HOLES AND COMMON TO THE VANE INSERT, BUTTSTRAPS, AND L/H I/B FLAP VANE AT FLAP STA 77.5 REF CRJ 200 SRM 57-52-00 REV 37 SRM 51-40-11-11. INSTALLED REPAIR PARTS ON L/H I/B FLAP VANE AT FLPA STA 77.5 REF CRJ-200 SRM 57-52-00 AND 51-42-13 REV 37.
SERVICE DOOR FITTING BELOW HANDLE HAS A CRACK. AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED SERVICE DOOR FITTING P/N 601R38723-17 REF CRJ 200 AMM 52-41-03 REV 60 AND CRJ 200 SRM 51-42-20 REV 37.
CRACK WAS DISCOVERED IN THE AFT PRESSURE BULKHEAD FS621, LB 27.50, 103.50 WL DURING SCHEDULED SDI OF THE AFT PRESSURE BULKHEAD. CRACK WAS REPAIRED PER REO 601R-53-61-1285.
GEAR DISAGREE WARNING ON APPROACH. RIGHT GEAR UNSAFE. C/W QRH MSG REMAINS. CYCLED GEAR, RT MLG CAME DOWN AND LOCKED. REMOVED AND REPLACED MAIN LANDING GEAR RUN AROUND BYPASS VALVE IAW AMM 32-32-20. COMPLIED WITH FUNCTIONAL TEST OF MAIN LANDING GEAR EXTENSION AND RETRACTION SYSTEM IAW TASK 32-30-00-720-801 AND OPS OF MANUAL RELEASE SYSTEM IAW TASK 32-34-00-710-801. CYCLED GEAR 12 TIMES, OPS AND LEAK CHECK GOOD.
CABIN EMERGENCY LIGHTS 2 AND 4 IN CEILING NOT LIGHTING. REPLACED NR 4 EMERGENCY LIGHTS BATTERY PACK IAW AMM 33-51-04, OPS CHECK OKAY.
ABORTED TAKEOFF BECAUSE A/C WOULD NOT STEER, FULL HARD LEFT. ON TAXI IN TILLER WOULD NOT SELF CENTER, LOW SPEED ABORT BTMS OK REMOVED AND REPLACED THE TILLER IAW AMM 32-51-01. OPS CHECKED GOOD.
LEFT FLOOR SILL CORRODED FROM FS 559+80 TO 621.00, LBL42. REPAIRED SILL IAW REO 601R-53-00-526.
1015032-1000-0010 - ANGLE AT L/H LONGERON 24 ABOVE CENTER WING FWD OF FS 473.15 IS CRACKED. REMOVED AND REPLACED ANGLE AT L/H LONGERON 24 ABOVE CENTER WING IAW CRJ200 SRM 51-42-06, 51-42-21.
ANGLE AT LT LONGERON 24 ABOVE CENTER WING FWD OF FS 473.15 IS CRACKED. REMOVED AND REPLACED ANGLE AT LT LONGERON 24 ABOVE CENTER WING IAW SRM 51-42-06, 51-42-21.
ANGLE AT RT LONGERON 24 ABOVE CENTER WING FWD OF FS473.15 IS CRACKED. REMOVED AND REPLACED ANGLE IAW SRM 51-42-06, 51-42-21.
SYSTEM 1 AC PUMP CASE DRAIN FILTER BRACKET IS CRACKED. REMOVED AND REPLACED BRACKET IAW SRM 51-42-06.
SYSTEM 2 HYD CASE DRAIN FILTER FRAME SUPPORT BRACKET HAS A 1" CRACK. REMOVED AND REPLACED BRACKET IAW SRM 51-42-06.
RIGHT WINDSHIELD HEAT ARCING, WINDOW CRACKED, INCIDENT OCCURED CLIMBING THRU 20,000 FT. OBSERVED ARCING, NO ODOR. SELECTED OFF. LANDED. R & R THE WINDSHIELD IAW AMM 56-11-01, OPS & LEAK CHECK GOOD.
F/A REPORTS STRONG ELECTRICAL BURNING ODOR IN VICINITY OF ROW 7 AND ROW 8, NO PASSENGERS ON BOARD AT TIME OF DISCOVERY. DID NOT NOTICE ANY VISIBLE OR AUDIBLE ARCING/SPARKING. INSPECTED AND VERIFIED BALLAST B113 CAUSED FLUORESCENT CEILING LIGHTS AT ROW 5AC TO OVERHEAT AND DAMAGE CEILING PANEL. INSPECTED CEILING LIGHTS. R&R TWO BALLAST AT 5AC TWO BULBS AT 5AC AND BULBS AT 3FD. OP CK GOOD IAW AMM 33-21-01 AND 33-21-710-001
AFTER TAKEOFF AT 7000 FT, NOTICED ACFT WAS NOT PRESSURIZING ON PRESSURE CONTROLLER NR 1. SWITCHED TO PRESSURE CONTROLLER 2, CABIN ALTITUDE CLIMBING AT SAME RATE AS ACFT. SWITCHED TO MANUAL, NO AFFECT. AIR RETURN, LANDED AT 44,000 LBS GROSS.
AILERONS PAUSE AT FULL DEFLECTION, BOTH CONTROLS & THEY SEEM TIGHT. RECEIVED AILERON TRIM FLAG ON PFD INFLIGHT & AT TIMES AUTOPILOT TURN WOULD CAUSE HESITATION & THEN A JERK MOVEMENT OF CONTROL YOKE.
ON TAKEOFF ROLL RECEIVED ANTI-SKID OTBD CAUTION MSG, ABORTED TAKEOFF. BTMS WAS 4-4-3-1, ABORTED UNDER 40 KNOTS.
SERVICE DOOR WILL NOT OPEN FROM OUTSIDE. REPEAT WITH SOME HISTORY. CLEANED & LUBRICATED. OPERATIONS CHECKED GOOD OF THE SERVICE DOOR OUTER HANDLE IAW AMM 52-41-03.
SERVICE DOOR OUTER HANDLE WILL NOT POP OUT. REMOVED PAINT OVERSPRAY & LUBED DEVICE DOOR OUTER HANDLE IAW SUPP 11-029B. SERVICE DOOR OUTER HANDLE OPERATIONS CHECKED GOOD IAW AMM 52-41-03.
MAIN PAX DOOR WOULD NOT OPEN WHEN ACFT ARRIVED AT THE GATE. CLEANED DEBRIS & DIRT FROM PAX DOOR CHUTE BOLTS. PAX DOOR OPERATES GOOD IAW AMM52-11-02.
WHILE PERFORMING GREO 601R-57-31-330 TO THE RT WINGLET TIP FAIRING, STRUCTURE UNDER FAIRING FOUND TO BE CRACKED & HAS ELONGATED HOLES. REPAIRED RT WINGLET TIP FAIRING & WINGLET RIB IAW REO 601R-57-31-1252 REV, DATED 2015 12 17.
LEFT AILERON OTBD LOWER LE CHAFED. R & R PANEL IAW SRM 51-42-06.
SKIN AT FWD L1 DOOR HINGE PIN, COVER IS GOUGED. REPAIRED IAW EA 40-2015-275.
PASSENGER DOOR ASSIST MOTOR FWD MOUNT, RACKED LOWER SIDE. R & R PAX DOOR ASSIST MOTOR FWD MOUNT WITH NEW MOUNT IAW SRM 51-42-06.
RIGHT SIDE HYD EQUIP RACK GUSSET & STANDOFF FOR NR 2 HYD PRESS LINE ARE DAMAGED. R & R GUSSET & STANDOFF IAW SRM 51-42-06.
PASSENGER DOOR AFT DRAG ANGLE CRACKED. R & R PREVIOUSLY REPAIRED -1 SECTION ON PAX DOOR, AFT DRAG ANGLE IAW REO 601R-52-11-513 REV B DATED 2015 07 05.
LEFT SIDE FS 625.00 CHANNEL TO FRAME CRACKED AT STRINGER 13L. R & R INTERCOSTAL CHANNEL, LT SIDE FS 625.00 TO FRAME AT STRINGER 13L IAW SRM 51-42-21.
INNER STIFFENER BROKE LOOSE FROM BOTTOM OF APU ENCLOSURE. REPAIRED THE STIFFENER IAW REO 601R-49-11-071 REV C DATED NOV 22 2004.
MID CABIN OVERHEAD EMER LIGHTS FAILED OPERATIONS CHECK. R & R EMER EXIT SIGN CHARGER CONTROL UNIT IAW AMM 33-51-05. OPERATIONS CHECKED GOOD IAW AMM 33-51-04.
DECK SKIN INSIDE LT FWD EQUIPMENT COMPARTMENT AT FS 193.00, FRAME IS CRACKED. REPAIRED DAMAGED DECK SKIN IN LT FWD EQUIPMENT COMPARTMENT IAW REO 601R5311-081-NC-2.
IN THE AFT EQUIP BAY, RT SIDE HYD EQUIP RACK U CHANNEL, WHERE NR 2 HYD RETURN MANIFOLD ATTACHES, IS CRACKED AT LOWER AFT CORNER. REPAIRED NR 2 HYD RETURN MANIFOLD ATTACH BRACKET IAW REO 601R-53-62-031 REV A DATED 13 JAN 2007.
SEAT TRACK HAS CORROSION ON RBL 9, BETWEEN FS 559+112 & FS 574.00 IN THE CARGO BAY. REPAIRED SEAT TRACK ON RBL 9, BETWEEN FS 559+112 & FS 574.00 IAW AMM 53-01-11 & REO 601R-53-00-485.
SEAT TRACK HAS CORROSION ON LBL 9, BETWEEN FS 559+112 & FS 574.00 IN THE CARGO BAY. R & R TRACK IAW AMM 53-00-49.
SEAT TRACK HAS CORROSION ON RBL 9, BETWEEN FS 559+80 & FS 559+96 IN THE CARGO BAY. REPAIRED SEAT TRACK ON RBL 9, BETWEEN FS 559+80 & FS 559+96 IAW REO 601R-53-00-485 & AMM 53-01-11.
LEFT SIDE FS 621 TO FS 625 CLIP, INTERCOSTAL TO FRAME, AT STRINGER 14L IS CRACKED. REMOVED CRACKED CLIP & INSTALLED REPLACEMENT CLIP IAW SRM 51-42-21 & REO 601R-53-61-100 REV A DATE 2008 0123.
SERVICE DOOR THRESHOLD CORRODED. RECEIVED NEW SERVICE DOOR THRESHOLD, PN 601R38957-31 & INSTALLED IAW SRM 51-40-11, 51-45-00 & 51-42-06.
FLOOR STRAP BETWEEN RBL 27 & THE RT FLOOR SILL HAS CORROSION AT FS 559.00 IN THE CABIN. R & R FLOOR STRAP WITH SHOP FABRICATED STRAP IAW SRM 51-42-06 & 51-42-10.
CARGO NET TIE DOWN FITTING HAS CORROSION ON LBL 9, BETWEEN FS 574.00 & FS 589.00. R & R TIE DOWN FITTING IAW AMM 53-49-000-801.
CARGO TIE DOWN FITTING HAS CORROSION ON LBL 9, BETWEEN FS 589.00 & FS 605.00. R & R TIE DOWN FITTING IAW AMM 53-00-49-000-801.
FLOOR STRAP, BETWEEN LBL 27 & THE LT FLOOR SILL HAS CORROSION AT FS 559.00 IN THE CABIN. R & R FLOOR STRAP IAW SRM 51-42-06 & 51-23-00.
LEFT SIDE FS 625 CHANNEL ATTACHED TO FRAME AT STRINGER 14L IS CRACKED. REMOVED CRACKED CHANNEL & INSTALLED REPLACEMENT CHANNEL LT FS 625 AT SIDE STRINGER 14L IAW SRM 51-42-06, 51-42-21 & 51-40-11.
BEAM 280 IS CRACKED AT THE LOWER ANGLE, JUST OTBD OF LBL 9 & PULLEY BRACKET FOR THE MLG MANUAL RELEASE CABLE. REPAIRED LOWER ANGLE JUST OTBD OF LBL 9 AT 280.0 BEAM IAW 601R-53-11-171.
LEFT AISLE SEAT TRACK HAS CORROSION AT FS 394.00. R & R SEAT TRACK IAW AMM 53-01-11.
BEAM 280 IS CRACKED AT THE LOWER ANGLE, JUST OTBD OF RBL 9. REPAIRED LOWER ANGLE AT FS 280.00 BEAM, OTBD OF RBL 9 IAW REO 601R-53-00-171.
T FITTING ON FRAME 319.70 IS CORRODED, JUST INBD OF THE SERVICE DOOR OPENING AT WS 73.50. R & R FITTING IAW SRM 51-42-21.
INBOARD & OUTBOARD CLIPS AT FS 280.0 & STRINGER 3L ARE CRACKED. R & R INBD & OTBD CLIPS AT FS 280.0, STRINGER 3L IAW SRM 51-42-06 & 51-42-21.
IN CRUISE FLIGHT RECEIVED ANTI-ICE DUCT WARNING MSG. COMPLIED WITH QRH, CLOSED 14TH STAGE BLEED AIR VLV & MSG PERSISTED. RT FUSELAGE SHOWING RED. AIR DEVERT TO ORF, EMERGENCY DECLARED, NORMAL LANDING. R & R SENSING ELEMENT A46WK IAW AMM 36-21-04, OPERATIONS CHECKED GOOD.
PASSENGER DOOR AFT SEAL STRIKER REPAIR IS DAMAGED & BENT. REPLACED DAMAGED TO PAX DOOR AFT SEAL STRIKER IAW REO 601R-53-22-033 TYPE 1 REPAIR.
EXTERNAL POWER RECEPTACLE MOUNT IS CRACKED. R & R EXTERNAL POWER RECEPTACLE MOUNT IAW CRJ 200 AMM 24-41-03, SRM 51-42-21, 51-42-13 & 51-42-06.
CORROSION FOUND ON STRINGER 26L UNDER NLG WW LT SPADE DOOR FITTING. PERFORMED REPAIR OF EA 15-201-496.
PASSENGER DOOR OUTER HANDLE CRACKED. R & R OUTER HANDLE IAW AMM 52-11-03.
PASSENGER DOOR LOWER SILL CORRODED. R & R IAW SRM 51-42-06.
DURING THE COLD WORKING OF THE MLG TRUNNION LOWER FLANGES FOUND ONE OVERSIZED HOLE ON THE RT SIDE. COMPLIED WITH REO 601R-52-21-2039 REN.
DENT IN EXT SKIN AT FS 265 - FS 280 BETWEEN STRINGER 24R - 23R. PERFORMED PERMANENT REPAIR REO 601R-53-11-2580 REV A, DRESSED DENT BACK TO AERODYNAMIC LIMITS.
CARGO DOOR FLOOR SILL FROM FS 574 TO FS 621 HAS CORROSION AROUND SEVERAL NUTPLATE HOLES. BLENDED CORROSION, FOUND OUT OF LIMITS IAW CRJ 200 SRM TR 5327. REMOVED UNSERVICEABLE FLOOR SILL THEN INSTALLED A SERVICEABLE FLOOR SILL.
RIGHT MLG WW AFT BRACKET FOR BRAKE PRESS VOLUMETRIC FUSE BRACKET CRACKED. R & R RT MLG WW VOLUMETRIC FUSE BRACKET.
RIGHT MLG DRAG ANGLE COMMON TO BATT RIB IS CRACKED. R & R CRACKED ANGLE WITH NEW SERVICEABLE ANGLE IAW CRJ 200 SRM 51-42-21.
RIGHT MLG WW AFT VOLUMETRIC FUSE BRACKET CRACKED. R & R WITH SERVICEABLE VOLUMETRIC FUSE BRACKET.
RIGHT MLG WW FWD BRACKET TRANSDUCER CRACKED. R & R TRANSDUCER BRACKET ON RT MLG WW FWD.
LEFT MLG WW FWD BRACKET FOR VOLUMETRIC FUSES CRACKED. REMOVED, FABRICATED & REINSTALLED,
PRESSURE TRANSDUCER BRACKET CRACKED, R & R.
ANGLE AT FS 484 LBL 36 IS CRACKED. REMOVED, FABRICATED & INSTALLED NEW ANGLE.
CENTER WINDSHIELD POST LOWER LT POST BRACKET CRACKED, R & R.
CRACKED AT FS 484 END OTBD OF RBL 27 & INBD OF RBL 36 EACH ANGLES. REMOVED UNSERVICEABLE TWO EACH ANGLE, FABRICATED & INSTALLED SERVICEABLE TWO EACH 484 CLIPS.
GEAR DISAGREE WARNING DURING GEAR RETRACTION NLG SHOWED UNSAFE ALONG WITH NWS INOP CAUTION MESSAGE AND NOSE DOOR WARNING AND AURAL WARNING MANUAL EXTENSION USED M/C-ACARS DATA SHOWS THE NLG LEFT THE DOWN LOCK BUT NEVER REACHED. NWS OPS CHECK GOOD AT THIS TIME, NO NWS INOP CAUTION MSG NOTED. REF ADJUSTED NLG WOW PROX SENSORS PS13GA AND PS4GA IAW 32-61-05.
UNABLE TO OPEN SERVICE DOOR FROM OUTSIDE, HANDLE POPS OUT BUT WILL NOT TURN. INSPECTED AND LUBED SERVICE DOOR, MOVED ACFT FWD AND BACK. DOOR IS STILL DIFFICULT TO OPEN AND CLOSE FROM THE OUTSIDE IAW AMM 52-11-00. R & R SERVICE DOOR SEAL, OPS AND LEAK CHECKED GOOD. ACFT OK FOR SERVICE.
ABNORMAL LEFT TURN OF CONTROL WHEEL DURING FLIGHT OPS. ALL TRIMS CENTERED. INSPECTED AUTOPILOT CONTROL CABLE TENSION 4 FOUND OUT OF LIMITS, ADJUSTED AUTOPILOT CONTROL CABLE TO BE WITHIN LIMITS.
CORROSION ON MAIN AVIONICS COMPARTMENT DOOR SEAL RETAINER. R & R SEAL RETAINER.
RT UPPER NOSE T/E SEAL CHAFED. REPAIRED SRS 090+SRS 094 IAW CMM 71-14-01.
LEFT BATTERY RIB IS CRACKED. REPAIRED RIB IAW REO 601R-57-51-046, REV B.
UNDER CARGO FLOOR PANEL 281LLF THE STRUCTURE SURROUNDING THE NUT PLATES IS SHOWING SIGNS OF CORROSION. REMOVED UNSERVICEABLE LBL 27 FLOOR SUPPORT, FABRICATED AND INSTALLED SERVICEABLE LBL 27 FLOOR SUPPORT IAW REO 601R-53-61-3778, REV A.
CORROSION LT & RT SEAT TRACK NR 1. R & R LT AND RT SEAT TRACKS IAW SRM 51-40-11, AMM 53-01-11-020-002.
FUSELAGE FAIRING CHAFING AT INBD WING ROOT BEHIND STUB FAIRING ON LT SIDE. REPAIRED IAW REO 601R-53-41-610.
NLG W/W OUTER SKIN CUT OUT AT RBL 6.0 CRACKED IN RADIUS. REPAIRED NLG CUTOUT CRACK ON OUTER SKIN AT RBL 6 IAW REO 601R-53-11-048.
AFT NECESSARY COMPARTMENT REAR PRESSURE BULKHEAD LT ANGLE CRACKED STA 621 TO 625. R & R AFT ACCESSORY COMPARTMENT REAR PRESSURE BULKHEAD LT OBLIQUE ANGLE IAW SRM 51-42-06, 51-40-11, & 51-42-21.
AFT ACCESSORY COMPARTMENT REAR PRESSURE BULKHEAD RT OBLIQUE ANGLE CRACKED STA 621 TO 625. R & R AFT ACCESSORY COMPARTMENT REAR PRESSUE BULKHEAD RT OBLIQUE ANGLE IAW SRM 51-42-06, 51-42-21.
RT INBD FLAP VANE CHAFED IN 3 AREAS ON L/E BLENDED OTBD & CNT CHAFED AREAS, NDT INSPECTED, ALODINED, PRIMED, TOP COATED & TEFLON IAW REO 601R-57-52-004. REMOVED INBD L/E SKIN AND INSTALLED NEW SKIN PN 601R14303-54 & IAW SRM 51-42-13, 51-40-11, 51-23-00, 51-25-16.
FS 202 BULKHEAD CRACKED AT PARKING BRAKE CABLE. REPAIRED CRACKED AREA AT PARKING BRAKE CABLE FITTING AREA ON BULKHEAD IAW REO 601R-53-11-563, TYPE II.
RT AILERON PANEL 449BB CHAFED. REPAIRED CHAFED AREA ON RT AILERON PANEL 699BB IAW REO 601R-57-60-020.
PAX DOOR STAIR STRUCTURE IS CARACKED 3RD STEP FWD CORNER. REPAIRED PAX DOOR STAIRS 3RD STEP ON FWD SIDE IAW SRM 52-00-00.
RT AILERON CHAFED ON UPPER EDGE L/E SKIN 4 PLACES MARKED. REPAIRED CHAFED AREA ON RT AILERON UPPER L/E SKIN IAW REO 601R-57-60-013.
HORZONTAL STAB TRIM ACTUATOR PIVOT STRUCTURE DAMAGED ON LT OTBD FACE. BLENDED DAMAGED AREA NDT INSPECTION PRIMED IAW REO 601R-55-31-220.
HORZONTAL STAB PIVOT FITTING DAMAGED ON LT INBD FWD FACE. BLENDED DAMAGED AREA NDT INSPECTION FLAP PEENED, ALODINED, PRIMED IAW REO 601R-55-11-392.
APU EXHAUST AFT HEATSHIELD HAS 1 PULLED THRU SCREW AND 1 LOOSE SCREW. REPAIRED APU EXHAUST AFT HEATSHIELD IAW REO 601R-49-81-051.
SHEARED RIVET HEAD ON OTBD BATHTUB FITTING AT LBL 9. REPLACED RIVET IAW SRM 51-42-06.
FLOORBEAM AT 280 CRACKED. REPAIRED FLOORBEAM IAW REO 601R-53-11-138.
NR 4 TIRE BLEW OUT ON ROTATION, IMMEDIATELY AFTER RECEIVED A SKID OTBD INOPERATIVE CAUTION MSG AND RT OTBD BTMS INOP. R & R NR 4 MLG WHEEL ASSY IAW 32-41-01.
PAX DOOR WOULD NOT OPEN DUE TO POWER ASST CABLE CATCHING DOOR FRAME. C/W M ACTION. PLACARDED AND PLACED ON MEL. R & R PAX DOOR MOTOR.
ELECTRICAL ODOR EVIDENT ROW 5 RT SIDE, LIGHT WERE ON AT THE TIME. INSPECTED CEILING AND SIDEWALL LIGHT BALLAST AT AND AROUND ROW 5, C/W OPS CK OF CEILING AND SIDEWALL LIGHTS, NO DEFECTS NOTED IAW AMM.
RECEIVED AILERON TRIM CAUTION FLAG ON EVERY TURN INITIATED TO THE LT WITH AUTOPILOT ON IN CRUISE FLIGHT. DURING TURNS MADE TO THE LT ACFT ROLLS VIOLENTLY TO THE LT TO ABOUT 30 DEGREES. ACFT CONTROLS FEEL HEAVY IN FLIGHT. MAINT WORK CARD NR 8 FOR R & R OF THE RT AILERON NR 2 SYS PCU SAFETY WIRE IAW AMM 27-11. OPS CK GOOD AT THIS TIME. (K)
RT ENGINE FAN CASE, P2T2 SENSOR LINE OTBD BRACKET CRACKED RT ENGINE FAN CASE P2T2, SENSOR LINE OTBD BRACKET REPLACED IAW SHORTS CMM 20-42-06. (K)
RT ENGINE TAILPIPE FAIRING FIRELOOP COVER FWD BRACKET RT ENGINE TAILPIPE FAIRING FIRELOOP COVER FWD BRACKET REPLACED IAW SHORTS CMM 20-42-06. (K)
PAX DOOR STAIRCASE AFT SIDE PANEL CRACKED BETWEEN STAIR NR 4 AND NR 5 (CRACK LENGTH .200") PAX DOOR STAIRCASE AFT SIDE BTW STAIR NR 4 AND NR 5 PERFORMED IAW REO 601R-52-11-702, REV A. (K)
LT PYLON PANEL 412DB FOUND WITH SEAL RETAINER CRACKED, LT PYLON PANEL 412DB SEAL RETAINER REPLACED IAW SRM 51-42-06. (K)
CARGO DOOR FLOOR SILL AT FS 574.00 CRACKED. CARGO DOOR FLOOR SILL AT FS 574.00. REPAIRED IAW REO 601R-53-61-1741 REV ORIGINAL. (K)
MAIN AVIONIC BAY TEFLON FITTINGS GUIDES CRACKED QTY (1) RT FWD AND QTY (1) LT AFT. MAIN AVIONIC BAY TEFLON FITTINGS GUIDES REPAIRED IAW MODSUM IS 601R 53-20-0001, REV A. (K)
AFT PRESSURE BULKHEAD WEB AT THE LINTEL LOCATION IS CRACKED FS 621.00, LBL 46.00, WL 110.00 AFT PRESSURE BULKHEAD WEB AT THE LINTEL LOCATION REPAIRED IAW REO 601R-53-61-1230, REV D. (K)
UPON SELECTION OR GEAR UP RECEIVED GEAR DISAGREE AFTER 30 SEC WOW INPUT CAUTION WOW OUTPUT STATUS MSG, WOW INPUT CAUTION, WOW INPUT STATUS MSG, NOSE GEAR DIDN`T RETRACT, MAIN GEAR RETRACTED NORMAL. C/W QRH RECEIVED 3 GREEN INDICATION. GEAR DISAGREE CLEARED. BOTH WOW MESSAGES REMAINED ON UNTIL TOUCHDOWN. FOUND NLG AND LT MLG STRUT EXTENSIONS LOW. SERVICED NOSE AND LT MLG STRUTS IAW AMM 12-12-32 PERFORMED FUNCTIONAL TEST OF LANDING GEAR EXTENSION AND RETRACTION IAW AMM 32-30-00, CHECKS GOOD. (K)
193765/3 - AT FL 290 RT 14TH DUCT MSG WARNING REMAINED WITH RT 14TH STAGE SOV CLOSED. REMOVED AND REPLACED RT PYLON ELEMENT "A58WK" IAW AMM 36-21-01, OPS CHECK GOOD, AND LEAK CHECKED 14TH STAGE DUCTING AND PRSOV, NO LEAKS NOTED. (K)
UPON LANDING, LT MLG COLLAPSED; AIRCRAFT DEPARTED RUNWAY TO THE LT SIDE, CVR AND FDR CIRCUIT BREAKERS HAVE BEEN PULLED, NO FIRE INDICATIONS RECEIVED. (K)
RT MLG DOOR L/E INNER SKIN GOUGE RT MLG DOOR REPAIRED IAW REO 601R-52-82-034. (K)
FOUND CARGO DOOR HOUSING CRACK. (M) CARGO DOOR HOUSING REPLACED IAW CRJ SRM 51-42-21. (K)
SCRATCH ON LT WING UPPER PLANK AT WS 162-49. (M) SCRATCH REWORKED IAW REO 601R-57-21-887. (K)
FOUND PAX DOOR AFT DRAG ANGLE CRACK, LENGTH 1 INCH. (M) PAX DOOR AFT DRAG ANGLE REPAIRED IAW REO 601R-52-11-513, REV A. (K)
FOUND LT MLG DOOR GOUGED AT LOWER FORWARD CORNER LOADING EDGE. (M) DAMAGED REPLACED IAW REO 601R-52-82-034.
FOUND FLOOR SUPPORTS IN CARGO COMPARTMENT AT FS 621 RBL 38 CRACKED. REPAIRED IAW CRJ 200 REO 601R-53-61-117 REV C. (M)
FOUND CRACK ON SUPPORT BRACKET AT LOWER ROLLER CARGO DOOR TRACK IS 574 WL 82. REMOVED AT LOWER ROLLER TRACK CARGO DOOR IAW CRJ 200 SRM 51-42-06. BRACKET FABRICATED IAW CRJ 200 SRM 51-24-21, BRACKET INSTALLED IAW SRM 51-42-06. (M)
WEAR MARK ON OUTBOARD FLAP ALIGNMENT FITTING LT SIDE OUT OF LIMIT IAW REO 601R-57-51-143, .060 INCH DEPTH. REPLACED IAW SRM 51-42-06 AND 51-42-20. OPS CHECK C/O IAW CRJ 200 AMM 27-54-00-710-801. (M)
FOUND RIGHT OUTBOARD FLAP ALIGNMENT FITTING GOUGE AT WS 170, WEAR DEPTH .060 INCH. OUT OF LIMIT IAW REO 601R-57-51-143. FLAP ALIGNMENT FITTING REPLACED IAW SRM 51-42-06 AND 51-42-20. OPS CHECK C/O IAW CRJ 200 AMM 27-54-00-710-801. (M)
FOUND PAX DOOR OUTER HANDLE CRACKED. REPLACED IAW AMM 52-11-03-400-802. (M)
FOUND INTERCOSTAL ANGLES AT FS 484 RBL 36 AND RBL 27 ARE CRACKED. REPAIRED IAW REO 601R-53-059 REV A. (M)
FOUND INTERCOSTAL ANGLES AT FS 484 LBL 36 AND LBL 27 ARE CRACKED. REPAIRED IAW REO 601R-53-41-059 REV A. (M)
FOUND RIGHT OUTBOARD FLAP MID HINGE FAIRING, INBOARD GUIDE CRACKED. REPAIRED IAW SRM 51-24-16, 51-21-16, 51-25-16. (M)
PASSENGER DOOR WILL NOT OPEN. (DISCOVERED AT GATE, WHEN TRYING TO DEPLANE PASSENGERS). PERFORMED OPERATIONAL CHECK OF PASSENGER DOOR, COULD NOT DUPLICATE MALFUNCTION IAW AMM 52-11-00. (K)
ABORTED TAKEOFF AT 110 KNOTS. FLIGHT CONTROLS FELT UNRESPONSIVE IN ROLL, CONTROL YOKE FULL LT DEFLECTION, AIRCRAFT STILL WANTED TO ROLL RT. MAX BTMS = 5, TOW =40,800. INSPECTED AILERON RUDDER, ELEVATOR FLAPS, SPOILERONS, STAB TRIM, RUDDER TRIM AND AILERON TRIM FOR TRAVEL AND OPERATION. CHECKED HYDRAULIC FLUID LEVELS AND ALL CIRCUIT BREAKERS IN-CHECK GOOD. ALL FLIGHT COTROLS OPERATE NORMAL. (K)
LAV SMOKE WARNING IN FLIGHT, COMPLIED WITH QRH, F/A REPORTS LAV SMOKE WARNING AND F/A REPORTS TEMPERATURE WARM IN CABIN, PACK AIR OUTPUT IN COCKPIT SMELLS OF DIRTY SOCKS. REMOVED AND REPLACED SMOKE DETECTOR, (CHANGING BOTH COALESCER BAGS). (K)
ON CLIMB-OUT AT 20,000 FEET, NOTICED LOUD SQUEALING FROM PAX DOOR, VERIFIED LIGHT COMING THROUGH PAX DOOR SEAL, RETURN TO PHL, LANDING WEIGHT WAS 46,900 LBS. FOUND SEALANT ON STRIKER SEAL REPAIR FORWARD AND AFT STRIKER CHIPPED. REAPPLIED AS PER REO 60R-53-22-033.
FOUND FUSELAGE SKIN DAMAGE CONSISTS OF DENTS MEASURING 3/32 AND 1/16 DEEP WITH NO CREASES OR BREAKS IN SKIN. MAINTENANCE INSTALLED NON-FLUSH EXTERNAL REPAIR FS 589-605, STRINGER 24L-27L IAW BOMBARDIER SERVICES CORP EO 601R-53-9765. (M)
EN ROUTE AT 24,000 FEET, LEFT WINDSHIELD SHATTERED, NO PRESSURIZATION LOSS NOTED. COMPLIED WITH QRH. REMOVED AND REPLACED LEFT WINDSHIELD IAW 56-11-01, OPS AND PRESSURIZATION CHECK GOOD. (M)
LT SIDE FS621.00 TO 625.30 INTERCOSTAL AT STR 14L IS CRACKED NEAR RADIUS APPROX 1.1 INCH LONG. REMOVED AND REPLACED INTERCOSTAL, PN 601-35012-51, IAW REO (UNREADABLE). (K)
LEFT PACK HIGH PRESSURE CAS MESSAGE. PERFORMED OPERATIONAL CHECK OF LEFT PACK IAW AMM 21-60-00. OPS CHECK NORMALLY OF ENGINE BLEED/APU BLEED. NO FURTHER MAINTENANCE REQUIRED. (M)
FOUND LEFT PACK HIGH PRESSURE CAS MESSAGE. (M)