N425AW

Part: HINGE FITTING — UNKNOWN (RH WING TRAILING) · airframe 43,912 hrs · 42,141 cycles

FOUND I/B BUSHING LUG BORE OF O/B FITTING FOR RH WING SIDE AILERON ATTACH POINT TO BE PREVIOUSLY OVERSIZED. ***** AC REMOVED FROM SERVICE ***** REPAIRED IAW BOMBARDIER REO 601R-57-51-05 REV NC DATED AUG 09, 1995, AND MHIRJ REO 601R-57-51-1011 REV-- DATED 2023-04-18

Part: ANGLE — CRACKED (PAX DOOR) · airframe 43,912 hrs · 42,141 cycles

PAX DOOR INNER ANGLE AT PRESSURE RELEASE DOOR IS CRACKED. *********AIRCRAFT REMOVED FROM SERVICE************ REMOVED CRACKED ANGLE, LOCATED DRILLED AND INSTALLED NEW SERVICEABLE ANGLE PN 601R318072-1 IAW CRJ 200 SRM 51-40-11 AND 51-42-06

Part: INTERCOSTAL — CORRODED (PAX DOOR) · corrosion level 2 · airframe 43,912 hrs · 42,141 cycles

PAX DOOR MID INTERCOSTAL DD6 IS CORRODED. ***** AC REMOVED FROM SERVICE ***** LOCATE, DRILLED AND INSTALLED SERVICEABLE INTERCOSTAL DD6 MID P/N 601R318057-1 IAW CRJ 200 SRM 51-40-11, 51-42-06, AND 51-42-21.

Part: FRAME — CORRODED (PAX DOOR) · corrosion level 2 · airframe 43,912 hrs · 42,141 cycles

PAX DOOR FRAME 313.56 BETWEEN DD4 AND DD5 IS CORRODED. ***** AC REMOVED FROM SERVICE ***** LOCATED AND DRILLED NEW PAX DOOR FRAME AT F/S 313.56 IAW CRJ 200 SRM 51-40-11 , INSTALLED NEW FRAME P/N 601R318086-1 IAW CRJ 200 SRM 51-42-06

Part: INTERCOSTAL — CORRODED (PAX DOOR) · corrosion level 2 · airframe 43,912 hrs · 42,141 cycles

PAX DOOR INTERCOSTAL DD7 FWD IS CORRODED. ***** AC REMOVED FROM SERVICE ***** LOCATED, DRILLED AND INSTALLED SERVICEABLE DD7A FWD INTERCOSTAL IAW CRJ 200 SRM 51-40-11 AND 51-46-06.

Part: HINGE — CORRODED (PAX DOOR) · corrosion level 2 · airframe 43,912 hrs · 42,141 cycles

Ï¿½PAX DOOR LOWER FOLDING STEP HINGE THAT ATTACHES TO THE PAX DOOR SILL HAS EXFOLIATION IN 2 PLACES. ***** AC REMOVED FROM SERVICE ***** INSTALLED NEW HINGE ON TOP STEP P/N (601R31980-41) IAW CRJ200 51-41-02

Part: CLEAT — CORRODED (PAX DOOR) · corrosion level 2 · airframe 43,912 hrs · 42,141 cycles

PAX DOOR INTERCOSTAL DD4 IS CORRODED. ***** AC REMOVED FROM SERVICE ***** LOCATED, DRILLED, AND INSTALLED SERVICEABLE DD4 FWD CLEAT P/N 600-31902-269 IAW CRJ 200 SRM 51-40-11 AND 51-42-06.

Part: SEAT TRACK — CORRODED (LBL9 FS559+4) · corrosion level 2 · airframe 43,912 hrs · 42,141 cycles

Ï¿½LBL9 SEAT TRACK FS559+4 - FS559+86 SEGMENT IS CORRODED. ***** AC REMOVED FROM SERVICE ***** INSTALLED NEW SEAT TRACK P/N 601R31032-9S LOCATED, DRILLED, AND INSTALLED AT LBL9 BETWEEN FS559+4 AND FS559+86 IAW CRJ-200 SRM 51-40-11 AND AMM 53-00-49-400-801

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 43,912 hrs · 42,141 cycles

PAX DOOR AFT DRAG ANGLE IS CRACKED IN PREVIOUS REPAIR. ***** AC REMOVED FROM SERVICE ***** LOCATED, DRILLED AND INSTALLED NEW SERVICEABLE DRAG ANGLE PN 601R31772-5S ONTO AFT WEB IAW CRJ 200 SRM 51-40-11 AND 51-42-06.

Part: FORMER — CORRODED (PAX DOOR) · corrosion level 2 · airframe 43,912 hrs · 42,141 cycles

PAX DOOR FWD FORMER F.S.311.75 BETWEEN DD5 AND DD4 IS CORRODED. ***** AC REMOVED FROM SERVICE ***** LOCATED, DRILLED, AND INSTALLED SERVICEABLE PAX DOOR FWD FORMER P/N 601R318031-5 IAW CRJ 200 SRM 51-40-11, 51-42-06, AND 51-42-21.

Part: FLOORBEAM — CORRODED (LBL27 FS569 - FS) · corrosion level 2 · airframe 43,912 hrs · 42,141 cycles

LBL27 FLOOR BEAM IS CORRODED BETWEEN FS569 AND FS621. ******AIRCRAFT REMOVED FROM SERVICE******** INSTALLED LBL27 FLOOR BEAM BETWEEN FS569 AND FS621 IAW CRJ-200 SRM 51-42-21, 51-42-34, AND REO 601R-53-61-3778 REV -B DATED: 2016-1

Part: CAP — CORRODED (LBL9 FS589) · corrosion level 2 · airframe 43,912 hrs · 42,141 cycles

3 EA. TOP PLATES CORRODED ON FLOOR BEAM AT FS589 BETWEEN LBL9 AND RBL9 *********AIRCRAFT REMOVED FROM SERVICE********* UPON INVESTIGATION FOUND DAMAGE TO BOTH LBL9 AND RBL 9 TO BE WITHIN LIMITS. LBL9 CAP SPLICE: LOWEST REMAINING 0.076". ORIGINAL THICKNESS WAS 0.080", 0.004" REM

Part: DIAPHRAGM — CORRODED (FS.621) · corrosion level 2 · airframe 43,912 hrs · 42,141 cycles

JUST FWD. OF F.S.621 @ FWD. FLOOR BEAM (PRESSURE DIAPRAM AREA) TOP BEAM CAP IS CORRODED (AS MARKED) UNDER 281CLF ********AIRCRAFT REMOVED FROM SERVICE*********** DIAPHRAGM ASSEMBLY REQUIRES REPLACEMENT RECEIVED LOCATED AND DRILLED NEW SERVICEABLE DIAPHRAGM ASSEMBLY P/N 601R35235-61 IAW CRJ-200 SRM 51-41-02 AND 51-40-11

Part: BUSHING — UNKNOWN (RH WINGSIDE) · airframe 43,912 hrs · 42,141 cycles

FOUND I/B BUSHING LUG BORE OF O/B FITTING FOR RH WINGSIDE AILERON ATTACH POINT TO BE PREVIOUSLY OVERSIZED. ***** AC REMOVED FROM SERVICE ***** COMPLIED WITH MHIRJ REO 601R-57-51-1011 REV -- DATED 2023-04-18.

Part: TRACK — CORRODED (FS559+86-FS 559+) · corrosion level 2 · airframe 43,912 hrs · 42,141 cycles

LBL9 SEAT TRACK FS559+86 - FS559+96 SEGMENT IS CORRODED. ******AIRCRAFT REMOVED FROM SERVICE******** INSTALLED NEW SERVICEABLE SEAT TRACK AT LBL9 FS 559+86 TO 559+96 IAW CRJ200 AMM 53-01-11-400-802.

Part: TRACK — CORRODED (FS 559+78 - 559+) · corrosion level 2 · airframe 43,912 hrs · 42,141 cycles

RBL27 SEAT TRACK FS559+78 - FS559+96 SEGMENT IS CORRODED. ********AIRCRAFT REMOVED FROM SERVICE******* INSTALLED NEW SERVICEABLE SEAT TRACK AT RBL27, FS559+78 TO FS 559+96 IAW CRJ200 AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (RBL 9) · corrosion level 2 · airframe 43,912 hrs · 42,141 cycles

RBL9 SEAT TRACK FS559+4 - FS559+86 SEGMENT IS CORRODED. ******AIRCRAFT REMOVED FROM SERVICE******* EVALUATED CORROSION AND FOUND TO BE BEYOND ALLOWABLE DAMAGE LIMITS, IAW CRJ200 SRM 53-21-49. RBL 9 FS 559+4 TO 559+86 SEAT TRACK REQUIRE REPLACEMEN

Part: SEAT TRACK — CORRODED (FS559+86 - 96) · corrosion level 2 · airframe 43,912 hrs · 42,141 cycles

RBL9 SEAT TRACK FS559+86 - FS559+96 SEGMENT IS CORRODED. *******AIRCRAFT REMOVED FROM SERVICE******** REMOVED UNSERVICEABLE CARGO TIE DOWN TRACK, FIT, & DRILLED FROM P/N 20276-288-0-0A, PAINTED AND INSTALLED NEW SECTION IAW BOMBARDIER REO# 601R-53-00-485, REV-D, DATED 2018-01-29, AND CRJ200 SRM 51-40-11, 51-24-36, & AMM 53-01-11-000-802, & 53-01-11-400-802.

Part: UNKNOWN — UNKNOWN · airframe 43,843 hrs · 42,068 cycles

AFTER CLEARING RUNWAY FOR ABORTED TAKE-OFF, TOWER INFORMED US THE LH ENGINE WAS SMOKING. ALL LH ENG INDICATIONS WERE "0". PERFORMED ENG SHUT DOWN. NO LH ENGINE FIRE INDICATION IN THE COCKPIT. FIRE BOTTLES DISCHARGED. PAX EVACUATED THROUGH MAIN CABIN DOOR. PASSENGERS REPORTED SMOKE SMELL IN CABIN, BUT NO VISIBLE SMOKE. SMOKE WAS VISIBLE FROM ENGINE EXHASUT PIPE AND BYPASS. AIRCRAFT REMOVED FROM THE SERVICE CHECKED RIG AT LH ENGINE THROTTLE GEAR BOX FOUND WORN DOWN. DOUBLE SPLINES REPLACED & RERIGGED ARM. REF AMM 76-11-17. RERIGGED FCU ARM REF AMM 76-10-00 LH ENGINE. RERIGGED ENTIRE LH ENGINE AND PYLON CHECKS GOOD. R&R BOTH ROD ENDS ON PUSH PULL ROD FROM THROTTLE GEAR BOX TO FCU (LH ENGINE). REF POWER PLANT BUILD UP MANUAL 71-00-03. REPLACED PUSH PULL ROD AND ENDS RECLOCKED ARM ON THROTTLE GEAR BOX ADJUSTED HR THROTTLE CONTROL INCLUDING MICRO STOP TO FIT REF AMM 76-10-20. REPLACED AND ADJUSTED RH UPPER CORE COWL IAW SUPP 14-187A AND AMM 71-12-01. R&R TR OUTER CASCADE & LOWER CENTER 845 ASSY REF AMM TASK 78-33-01. R&R RH ENGINE STARTER IAW AIR WIS SUP 14-043A. R&R CANNON PLUG. R&R UPPER COWL.

Part: NONE — NONE · airframe 42,958 hrs · 41,214 cycles

***SUPPLEMENTAL INFORMATION *****L REV UNLOCKED CAUTION MESSAGE ON DEPARTURE. IACS AND QRH C/W. YELLOW REV ICON. L REVRESER APPEARS PHYSICALLY STOWED. ***AIRCRAFT REMOVED FROM SERVICE ***** LFT TR DEACTIVATED PER AWAC SUP 15-046D. THE TR WAS FOUND TO BE IN THE STOWED POSITION, NO PDU ADJUSTMENT NECESSARY. REF 339091/3 FOR MEL VODZAK, NICHOLAS A&P 3563655 TROUBLESHOOT LEFT TR PER AWA SUPP 13-037A. NO DEFECTS FOUND AT THIS TIME. LUBRICATED LEFT TR SLIDER BLOCKS, TRACKS, AND BALLSCREW ACTUATORS PER AWA SUPP 14-118A AND AWA SUPP 12-128.

Part: NONE — NONE · airframe 42,067 hrs · 40,373 cycles

IN CRUISE RECEIVED IAS COMP ON FLAG ON CAPT PFD. CW QRH MESSAGE CLEARED AFTER SELECTING AIR DATA COMPUTER TO #2 PER QRH. ***AIRCRAFT REMOVED FROM SERVICE*** R&R #1 ADC IAW AMM 34-13-01 AND SUP 17-010A. ALL OPS AND FUNC TEST GOOD

Part: FRAME — CORRODED (FS 333) · corrosion level 2 · airframe 41,478 hrs · 39,789 cycles

FWD FACE OF FRAME AT FS 333.0 CORRODED BETWEEN STR 21R TO 24R. ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED AND REPLACED FRAME AT FS 333.0 BETWEEN STR 17R TO 22R IAW CRJ-200 SRM 51-42-06 AND 51-42-21

Part: FRAME — CORRODED (FS 605) · corrosion level 2 · airframe 41,478 hrs · 39,789 cycles

FWD AND AFT FACE, AND LWR LEG OF FRAME AT FS 605.00 CORROSION BETWEEN STR 26R AND 23R ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED CORROSION FROM FWD AND AFT FACE OF FRAME AT FS 605.00 BETWEEN STR 26R AND 23R IAW CRJ-200 SRM 51-21-06. ORIGINAL THICKNESS .050, THICKNESS REMAINING .047 FOUND TO BE WITHIN LIMITS IAW CRJ-200 SRM 53-00-00. TREATED, PRIMED PAINTED AND TOPCOATED IAW CRJ-200 SRM 51-25-01

Part: FRAME — CORRODED (FS 589) · corrosion level 2 · airframe 41,478 hrs · 39,789 cycles

AFT FACE OF FRAME AT FS 589.0 SEVERAL SPOTS OF CORROSION BETWEEN STR 25R AND 27. ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED CORROSION FROM AFT FACE AT FS 589.0 BETWEEN STR 25R AND 27R IAW CRJ-200 SRM 51-21-06. ORIGINAL THICKNESS .050, THICKNESS REMAINING .048, FOUND TO BE WITHIN LIMITS IAW CRJ-200 SRM 53-00-00. TREATED, PRIMED AND TOP COATED IAW CRJ-200 SRM 51-25-01

Part: WASHER — CORRODED (BS 544-549) · corrosion level 2 · airframe 41,478 hrs · 39,789 cycles

LH AND RH GEAR WELLS PASS THROUGH AT FS 544-549 HAS CORROSION REQUIRES FURTHER EVAL UPON FURTHER INVESTIGATION FOUND WASHERS TO BE CORRODED, REMOVED AND REPLACED WASHERSIAW CRJ-200 SRM 51-41-02 ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED AND REPLACED WASHERS IAW CRJ-200 SRM 51-42-02

Part: CONTROL UNIT — MALFUNCTIONED (FLAP SYSTEM) · airframe 40,817 hrs · 39,109 cycles

DURING APPROACH SELECTED FLAPS 8 THEN RECEIVED FLAPS FAIL CAUTION MSG FLIGHT CONTROL SYSNOPTIC PAGE SHOWED FLAPS AT 0 DEGREES,COMPLIED WITH QRD CK LIST. NORAML LANDING,SMOTH TOUCHDOWN, BPMS READING SHOWED 5-5-4-4. PERFORMED FLAP RESET PROCEDURE IAW AWAC SOP 98-18I BOX 12. FLAPS RESET. PLACARDED AND PLACED ON MEL. ***AIRCRAFT REMOVED FROM SERVICE*** INVESTIGATED AND FOUND FECU TO BE MOST PROBABLE PER FIM SUP 98-018I R&RD FECU IAW AMM 27-50 OPS CHECKS GOOD, NO FURTHER DEFECTS NOTED

Part: BPSU — MALFUNCTIONED (FLAP SYS) · airframe 40,223 hrs · 38,469 cycles

RECIEVED FLAPS FAIL CAUTION MESSAGE DURING THE APPROACH. FLAPS FAILED AT ZERO DEGREES. COMPLIED WITH QRH. LANDED AT FLAPS ZERO. PERFORMED FLAP RESET PROCEDURE IAW 98-18I BOX 12. FLAPS RESET. AIRCRAFT REMOVED FROM SERVICE. RIGGED THE LT AND RT FLAP BPSU IAW AMM 27-51-10. OPS CHECKD GOOD.

Part: STRUT — MALFUNCTIONED (NLG) · airframe 39,296 hrs · 37,553 cycles

SUPPLIMENTAL INFORMATION, AFTER T/O, ON LANDING GEAR UP, WE RECIEVED A GEAR DISAGREE AND NOSE DOOR OPEN WARNING MESSAGES WITH WOW INPUT CAUTION MESSAGE. AIRCRAFT REMOVED FROM SERVICE. SERVICED NLG SHOCK STUT IAW AMM 12-12-32-610-803.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,240 hrs · 37,503 cycles

R/H FLOOR SILL HAS CORROSION ON THE UPPER AND LOWER SURFACES AT NUT PLATE LOCATIONS BETWEEN FS559+80 AND 621 REMOVED AND REPLACED R/H FLOOR SILL @ FS559+80 IAW CRJ-200 SRM 51-42-06 AND 51-22-21

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,240 hrs · 37,503 cycles

R/H FLOOR SILL HAS CORROSION ON THE UPPER AND LOWER SURFACES AT NUT PLATE LOCATIONS BETWEEN FS559+80 AND 621 AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED R/H FLOOR SILL @ FS559+80 IAW CRJ-206 00 SRM 51-42-AND 51-22-21

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,240 hrs · 37,503 cycles

SERVICE DOOR LOWER SILL ANGLE CORRODED AIRCRAFT REMOVED FROM SERVICE REPLACED LOWER SILL ANGLE IAW CRJ200 SRM 51-42-06, 53-00-00.

Part: POST — CRACKED (FUSELAGE) · airframe 39,240 hrs · 37,503 cycles

FS409+128 POST AT LEFT BL18 IS CRACKED IN THE O/B RADIUS. AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED FS409+128 POST IAW REO 601R-53-41-889 REV-D.

Part: BRACKET — CRACKED (BS 449) · airframe 39,240 hrs · 37,503 cycles

FS 449 RBL 47 FAIRING BRACKET IS CRACKED. AIRCRAFT GROUNDED REMOVED AND REPLACED BRACKET IAW CRJ-200 SRM 51-42-06.

Part: FRAME — CORRODED (BS 513) · corrosion level 2 · airframe 39,240 hrs · 37,503 cycles

FS 513 MACHINED FRAME HAS CORROSION AT STR 5R. REPAIRED FRAME SECTOR AT FS 513.0 STR 5R IAW EA AWAC-CRJ253-01360

Part: SKIN — DENTED (RT SPOILER) · airframe 39,240 hrs · 37,503 cycles

RT WING I/B GRND SPOILER HAS DENT ON BOTTOM SURFACE. REPAIRED RT WING I/B GRND SPOILER BOTTOM SURFACE IAW AWAC-CRJ257-01361 REV IR DATE 10/26/2019

Part: SKIN — DAMAGED (SPOILER) · airframe 39,240 hrs · 37,503 cycles

RT WING I/B GRND SPOILER HAS ROCK CHIP DAMAGE ON BOTTOM SURFACE. REPAIRED RT WING I/B GRND SPOILER BOTTOM SURFACE IAW AWAC-CRJ257-01361 REV IR DATE 10/26/2019

Part: VANE — CHAFED (LT WING LE FLAP) · airframe 39,240 hrs · 37,503 cycles

LEFT I/B VANE L/E CHAFFED IN 3 PLACES. REMOVED AND REPLACED LEFT MIDDLE FLAP VANE L/E IAW CRJ-200 SRM 51-42-10. BLENDED LEFT I/B AND O/B TO SMOOTH CONTOUR. FOUND TO BE WITHIN LIMITS IAW REO 601R-57-52-004.

Part: POST — CORRODED (BS 409) · corrosion level 2 · airframe 39,240 hrs · 37,503 cycles

INBOARD POST AT FS 409+128 LBL 18 HAS CORROSION. REPLACED

Part: STIFFENER — CRACKED (BS 621 BULKHEAD) · airframe 39,240 hrs · 37,503 cycles

LOWER 621 BULKHEAD STIFFENER AT LBL 36 CRACKED. REPLACED

Part: ANGLE — CRACKED (BS 605) · airframe 39,240 hrs · 37,503 cycles

FS 605 CLIP UNDERNEATH THE CARGO DOOR SILL AT STR 17L IS CRACKED. REMOVED AND INSTALLED NEW CLIP UNDER CARGO DOOR SILL AT STR 17L FS 605 IAW CRJ 200 SRM 51-42-21

Part: ANGLE — CRACKED (CARGO DOOR) · airframe 39,240 hrs · 37,503 cycles

LOWER AFT ANGLE 601R35050-109 FOR CARGO DOOR BEAM CRACKED. REMOVED AND REPLACED LOWER AFT ANGLE P/N 601R35050-109 IAW CRJ 200 SRM 53-61-23

Part: BRACKET — CRACKED (BS 461) · airframe 39,240 hrs · 37,503 cycles

F.S. 461 RBL 47 FAIRING BRACKET IS CRACKED. REMOVED AND REPLACED BRACKET IAW CRJ200 SRM 51-42-06

Part: BRACKET — CRACKED (BS 449) · airframe 39,240 hrs · 37,503 cycles

FS 449 LBL FAIRING BRACKET CRACKED. REPLACED

Part: DOOR SILL — CRACKED (BS 589) · airframe 39,240 hrs · 37,503 cycles

CARGO DOOR SILL AT FS 589 AT INBOARD RIVET IS CRACKED. REMOVED DAMAGED AREA IAW BOMB. REO 601R-53-61-433 REV C

Part: BRACKET — CRACKED (BS 469) · airframe 39,240 hrs · 37,503 cycles

FS 469 RBL 47 FAIRING BRACKET IS CRACKED. REPLACED

Part: RETAINER — CRACKED (HORIZONTAL STAB) · airframe 39,240 hrs · 37,503 cycles

PANEL 422DB SEAL RETAINER IS CRACKED. REMOVED AND REPLACED SEAL RETAINER IAW CRJ 200 SRM 51-42-06

Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE) · airframe 38,313 hrs · 36,598 cycles

THE CREW ADVISED DISPATCH THAT THE AIRCRAFT WAS UNABLE TO PRESSURIZE AND WAS LEVELING OFF AT 10,000. CREW COMPLIED WITH QRH AND SWITCHED TO CONTROLLER 2 AND MANUAL MODE; NEITHER CORRECTED THE ISSUE. THE FLIGHT BURNED OFF FUEL AND RETURNED TO CAE. RTN-CABIN W/N PRESSURIZE REC'D CABIN ALT CAUTION MSG RAN CABIN ALT QRH CABIN WOULD SILL NOT PRESSURIZE DELTA P REMAINED AT.1 ENTIRE TIME SWAPPED CONTROLLERS AND TRIED MANUAL, AIRCRAFT WOULD STILL NOT PRESSURIZE. NO ASSOCIATED MSG'S.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 38,182 hrs · 36,471 cycles

LT AND RT WING A-ICE CAUTION ON CLIMB OUT POWER AT T/O THRUST. C/W QRH MSG'S LEARED. WITH A-ICE IN STANDBY MODE. ON APROACH RECEIVED LT AND RT WING A-ICE CAUTION IN STANDBY MODE. WITH POWER GREATER THAN 85 PERCENT N2 UNABLE TO CLEAR MESSAGE BY INCREASING POWER, GREEN A-ICE ON MSG WAS INTERMITTENT. DIVERTED DUE TO ICING CONDITIONS.

Part: FORMER — CRACKED (PAX DOOR) · airframe 35,584 hrs · 33,841 cycles

PAX DOOR AFT FORMER CRACKED AT POWER ASSIST MOTOR PULLEY LOCATION.

Part: SKIN — DENTED (BS 173-196) · airframe 35,584 hrs · 33,841 cycles

FWD RT SKIN PANEL BETWEEN BS 169 TO 172.60 / WL 79 TO 90 IS DENTED

Part: SKIN — DENTED (BS 169-175) · airframe 35,584 hrs · 33,841 cycles

LH EXTERIOR SKIN BETWEEN BS 169 TO 175 DENTED.

Part: SKIN — DENTED (BS 169-193) · airframe 35,584 hrs · 33,841 cycles

FWD SKIN PANEL BETWEEN BS 169 TO 193, LBL 9 TO RBL 9 IS DENTED

Part: BRACKET — CRACKED (BS 621) · airframe 35,584 hrs · 33,841 cycles

CRACKED BRACKET AT BS 621, RBL40. REPLACED THE BRACKET IAW SRM 51-42-06, AND 51-24-21.

Part: STIFFENER — CRACKED (LT ENG TAILPIPE) · airframe 35,584 hrs · 33,841 cycles

LEFT ENGINE TAIL PIPE FAIRING FIRST STIFFENER ANGLE IS CRACKED. REPAIRED IAW CMM 78-11-00, REPAIR SRS042.

Part: ANGLE — CRACKED (BS 280 FLOORBEAM) · airframe 35,584 hrs · 33,841 cycles

FWD ANGLE ON THE BS 280 FLOORBEAM CRACKED. REPLACED THE ANGLE IAW SRM 51-42-06, 51-40-11, AND REO 601R-53-11-136, REV-A.

Part: TEE FITTING — CORRODED (BS 319) · corrosion level 2 · airframe 35,584 hrs · 33,841 cycles

TEE FITTING AT BS 319, RBL 43 IS EXFOLIATED. REPLACED THE TEE FITTING IAW SRM 51-42-06, AND 51-42-21.

Part: ANGLE — CRACKED (BS 280) · airframe 35,584 hrs · 33,841 cycles

ATTACH ANGLE CRACKED AT BS 280, LBL 8. REPLACED THE ANGLE IAW REO 601R-53-11-170, REV-D.

Part: ATTACH ANGLE — CRACKED (BS 280) · airframe 35,584 hrs · 33,841 cycles

CRACKED ATTACH ANGLE AT BS 280, RBL 10. REPLACED ANGLE IAW REO 601R-53-11-136, REV-A.

Part: CLEAT — CORRODED (BS 315) · corrosion level 2 · airframe 35,584 hrs · 33,841 cycles

MAIN CABIN HINGE CUT OUT CLEAT CORRODED AT BS 315, LBL 39. REPLACED CLEAT IAW SRM 51-42-06, AND 53-21-23.

Part: ATTACH ANGLE — CRACKED (BS 280) · airframe 35,584 hrs · 33,841 cycles

CRACKED ATTACH ANGLE AT BS 280, RBL 8. REPLACED THE ATTACH ANGLE IAW REO 601R-53-11-171, REV D.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 35,584 hrs · 33,841 cycles

BS 280 FLOORBEAM CORRODED AT RBL 9 TO LBL 9. REPLACED THE FLOORBEAM IAW REO 601R-53-11-136 REV-A.

Part: BRACKET — CORRODED (MAIN CABIN) · corrosion level 2 · airframe 35,584 hrs · 33,841 cycles

MAIN CABIN FLOOR HINGE CUT OUT BRACKET CORRODED. REPLACED THE BRACKET IAW SRM 51-42-06.

Part: BULKHEAD — GOUGED (BS 621) · airframe 35,584 hrs · 33,841 cycles

AFT PRESSURE BULKHEAD BS 621 FWD FACE HAS A GOUGE ON PREVIOUS REPAIR DOUBLER AT RBL 18. REPLACED THE DOUBLER IAW REO 601R-53-61-1285 REV-E.

Part: WARNING MESSAGE — FALSE ACTIVATION (MLG) · airframe 35,478 hrs · 33,736 cycles

PROXIMITY SYS CHANNEL CAUTION MESSAGE AT CRUISE FL 270. COMPLIED WITH QRH. UNABLE TO STOW MANUAL GEAR RELEASE. GEAR ARE PINNED. BTMS NORMAL. REMOVED AND REPLACED PSEU IAW AMM 32-61-01, OPS CHECKED GOOD, STOWED LANDING GEAR MANUAL RELEASE HANDLE IAW AMM 32-34-00, REMOVED GEAR PINS AS REQUIRED.

Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 35,042 hrs · 33,312 cycles

BS 621 BULKHEAD HAS CRACKS AT RBL 27 / WL 91, RBL 18 / 103, RBL 9.5 / WL 83 & 103 AND BL 0 / WL 124-133

Part: INDICATION SYS — MALFUNCTIONED (FUEL SYSTEM) · airframe 32,984 hrs · 31,786 cycles

FUEL CH 1 & 2 CAUTION MESSAGE IN FLIGHT. ALL FUEL QUANTITIES SHOWED DASHES. DIVERTED TO SWF. MESSAGES WENT AWAY MINUTES LATER AND FUEL QUANTITIES RETURNED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,557 hrs · 31,970 cycles

FLIGHT 4019, EMERGENCY LIGHTS FROM ROWS 1 AND 2 WILL NOT ILLUMINATE. REMOVED AND REPLACED EMERGENCY FLEX LIGHT STRIP AT ROW 1 AND 2 IAW AMM 33-51-01. OPS CHECKED GOOD.

Part: WIRE — EXPOSED (CABIN) · airframe 32,479 hrs · 30,954 cycles

WIRE PROTRUDING FROM EMER FLOOR TRACK LIGHT NEAR SEAT 1D.

Part: WIRE — BROKEN (CABIN) · airframe 31,982 hrs · 30,471 cycles

FRONT SECTION OF FLOOR EMER TRACK LIGHTING TORN UP, ON CALL FOUND WIRES PULLED UP & BROKEN.

Part: INTERCOSTAL — GOUGED (FUSELAGE) · airframe 31,717 hrs · 30,218 cycles

INTERCOSTAL AT FS 449.85, FWD OF OVERWING EXIT, UPPER STOP PAD IS GOUGED, R & R.

Part: SKIN PANEL — DAMAGED (FUSELAGE) · airframe 31,717 hrs · 30,218 cycles

AFT LOWER FUSELAGE SKIN AREA FS 586 TO 600, BETWEEN STRINGER 21R & 26R IS DENTED & HAS PARTIALLY BLENDED GOUGES.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,717 hrs · 30,218 cycles

INTERCOSTAL BETWEEN FRAMES AT FS 364 & 349, ON STRINGER 26L HAS CORROSION, IN THE FWD E & E BAY.

Part: STRAP — CRACKED (LT WING) · airframe 31,717 hrs · 30,218 cycles

LEFT WING LOWER SKIN STEEL STRAP, MLG TRUNNION RIB, DURING X-RAY INSPECTION SHOWED EVIDENCE OF A CRACK.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 31,717 hrs · 30,218 cycles

INTERCOSTAL BETWEEN FRAMES 364 - 349 & STRINGER 27 - 26L HAS CORROSION IN THE FWD E & E BAY, REPAIRED.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,717 hrs · 30,218 cycles

STRINGER 27 HAS CORROSION, BETWEEN FRAMES 349 & 333, IN THE FWD E & E BAY. R & R.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,717 hrs · 30,218 cycles

CARGO FLOORBEAM, FS 589.00 - 621.00 & LBL 24, CORRODED AROUND SCREW HOLES, REPAIRED.

Part: SKIN — DENTED (RUDDER) · airframe 31,717 hrs · 30,218 cycles

SMALL DENT ON LT SIDE OF RUDDER. REPAIRED DENT ON LT SIDE OF RUDDER IAW EA 40-2015-185.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,717 hrs · 30,218 cycles

STRINGER 27 HAS CORROSION, BETWEEN FRAMES 333 & 319.70, IN THE FWD E & E BAY. REPAIRED BY REMOVING DAMAGED STRINGER 27 & INSTALLING REPLACEMENT STRINGER 27, BETWEEN FS 280 & 346 IAW SRM 51-21-06, 53-00-00, 51-41-02, 51-42-06, 51-42-21, TR 53-51, 51-21-11, 51-25-06, 51-25-16, 53-21-17, TR 51-29 & AMM 20-21-00, 52-42-00, 57-70-08, 20-22-01 & 22-12-01.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 31,717 hrs · 30,218 cycles

INTERCOSTAL BETWEEN FRAMES 364 THROUGH STRINGER 27 - 26R HAS CORROSION, IN THE E & E BAY. REMOVED & REINSTALLED. PRIMARY STRUCTURE, GUSSET & INTERCOSTAL REMOVED FOR ACCESS & THEN REINSTALLED ORIGINAL PARTS.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 31,717 hrs · 30,218 cycles

PASSENGER DOOR AFT DRAG ANGLE CRACKED, R & R.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,717 hrs · 30,218 cycles

CARGO DOOR LOWER SILL HAS LIGHT CORROSION.

Part: ANGLE — DAMAGED (FUSELAGE) · airframe 31,717 hrs · 30,218 cycles

SERVICE DOOR LOWER SILL, UPPER ANGLE HAS 3 ELONGATED CLIP NUT HOLES AT FWD END. R & R SERVICE DOOR LOWER SILL UPPER ANGLE IAW SRM 51-42-13 & APPLIED TOUCH UP TOP COAT TO FASTENERS IAW SRM 51-25-16.

Part: ATTACH BRACKET — CRACKED (FUSELAGE) · airframe 31,717 hrs · 30,218 cycles

ACFT POWER RECEPTACLE ATTACH BRACKET IS CRACKED. R & R DISCREPANT ACFT POWER RECEPTACLE ATTACH BRACKET IAW SRM 51-42-06 & 51-42-13.

Part: MOUNT — CRACKED (RT WING) · airframe 31,717 hrs · 30,218 cycles

RIGHT WING FUEL SINGLE POINT MOUNT CRACKED. REMOVED CRACKED RT WING FUEL SINGLE POINT MOUNT & INSTALLED REPLACEMENT MOUNT, PN 600-62441-1, IAW SRM 51-42-06 & 51-42-02.

Part: TORQUE BOX — CRACKED (THRUST REVERSER) · airframe 31,717 hrs · 30,218 cycles

RIGHT ENG TORQUE BOX CRACKED AT 8 O CLOCK AM PANEL MOUNT. REPAIRED RT ENG TORQUE BOX IAW REO 601R-78-30-2553 REV A DATED 26 MAY 2004.

Part: SKIN — CHAFED (RT MLG) · airframe 31,717 hrs · 30,218 cycles

RIGHT MLG DOOR INNER SKIN CHAFED. R & R RT LG DOOR INNER SKIN IAW SRM 51-42-13 & 51-42-22.

Part: THRESHOLD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,717 hrs · 30,218 cycles

SERVICE DOOR THRESHOLD CORRODED, R & R.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,717 hrs · 30,218 cycles

RIGHT SIDEWALL SEAT TRACK NR 6 IS CHAFED & HAS AREAS OF CORROSION. R & R.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,717 hrs · 30,218 cycles

RIGHT AISLE SEAT TRACK NR 2 STICK HAS CORROSION. REPLACED IAW SRM 51-41-02 & AMM 53-01-11.

Part: SUPPORT ANGLE — CRACKED (PAX DOOR) · airframe 31,717 hrs · 30,218 cycles

PASSENGER DOOR LATCH CAM COVER SUPPORT ANGLE CRACKED, REPLACED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,717 hrs · 30,218 cycles

RIGHT AISLE SEAT TRACK STICK 1 CORRODED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 31,717 hrs · 30,218 cycles

LEFT AISLE SEAT TRACK STICK 1 HAS CORROSION IN CABIN. R & R LT AISLE SEAT TRACK STICK 1 IAW MM 53-01-11.

Part: A/C PACK — ODOR (LEFT) · airframe 28,689 hrs · 27,302 cycles

ON AIR EXCHANGE FROM APU TO ENGINE, HEARD A POP AND SMELLED AN ODOR WHICH DISSIPATED IMMEDIATELY. LIMITED AIR FLOW BOTH PACKS ON APU. LT PACK TEMP INCREASES ON APU. INSPECTED APU DUCTS & BOTH PACKS IN AFT EQUIPMENT BAY. RAN PACKS & NOTICED ODOR FROM LT PACK. RT PACK OPS CHECKED GOOD. R & R ACM WATER SEPARATOR & PRSOV. OPS CHECKED GOOD.

Part: POST — CRACKED (BS 409) · airframe 26,730 hrs · 25,410 cycles

FS 409+128 VERT POST AT RBL 27 IS CRACKED AT LWR EDGE. REPAIRED POST IAW B/A REO 601R-53-41-056, REV F.

Part: ATTACH FITTING — CRACKED (LT WING) · airframe 26,730 hrs · 25,410 cycles

LEFT T/E ATTACH FITTING AT WS 264.00 IS CRACKED. REMOVED CRACKED FITTING AT WS 264.00 AND INSTALLED NEW SERVICEABLE FITTING, PN 601R10836-3 IAW SRM 51-42-06, 51-42-21.

Part: SUPPORT — LOOSE (HANDRAIL) · airframe 26,730 hrs · 25,410 cycles

FWD HAND RAIL SUPPORT HAS LOOSE FASTENERS. R & R WITH NEW PARTS UPPER TUBE, UPPER TUBE FITTING, LOWER TUBE IAW SRM 51-40-11.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 26,730 hrs · 25,410 cycles

RIGHT INBD FLAP VANE L/E IS CHAFED THREE LOCATIONS. BLENDED AREAS, REWORKED UNSERVICEABLE & REPLACED WITH SERVICEABLE.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,730 hrs · 25,410 cycles

SERVICE DOOR LOWER SILL CORRODED. REPLACED .

Part: FITTING — BROKEN · airframe 26,730 hrs · 25,410 cycles

ATTACH FITTING BROKEN UNDER VISOR PANEL LT 326CL. FABRICATED & REPLACED IAW SRM 51-24-16.

Part: TRUNNION — DAMAGED (RT MLG) · airframe 26,730 hrs · 25,410 cycles

ONE OVERSIZED HOLE ON RT LOWER MLG TRUNNION FLANGE. REPAIRED DISCREPANT HOLE ON RT LWR MLG TRUNNION FLANGE REO 601R-57-21-1999.

Part: POST — CRACKED (BS 409) · airframe 26,730 hrs · 25,410 cycles

FS 409+128, VERT POST AT LBL 27 IS CRACKED AT LOWER EDGE. REPAIRED IAW REO 601R-53-41-056, REV F.

Part: RETAINER — CORRODED (E/E BAY DOOR) · corrosion level 2 · airframe 26,730 hrs · 25,410 cycles

MAIN AVIONICS DOOR SEAL RETAINER CORRODED. REPLACED WITH NEW SERVICEABLE SEAL RETAINERS.

Part: BRACKET — CRACKED (RT MLG WW) · airframe 26,730 hrs · 25,410 cycles

RIGHT MLG WHEEL WELL BRAKE TRANSDUCER BRACKET CRACKED. R & R BRACKET.

Part: ANGLE — CORRODED (DOOR FRAME) · airframe 26,730 hrs · 25,410 cycles

PASSENGER DOOR CUT OUT LOWER ANGLE CORRODED. REPLACED ANGLE.

Part: RIB — CRACKED · airframe 26,730 hrs · 25,410 cycles

BAT RIB DRAG ANGLE CRACKED, R & R.

Part: RIB — CRACKED (RT WING) · airframe 26,730 hrs · 25,410 cycles

RIGHT DRAG ANGLE AT INBD BATTERY RIB WAS CRACKED. REPLACED RT DRAG ANGLE AT INBD BATTERY RIB.

Part: ANGLE — CRACKED (BS 484) · airframe 26,730 hrs · 25,410 cycles

ANGLE AT FS 484, RBL 27 - 33 CRACKED. REPLACED ANGLE IAW REO 601R-53-41-059.

Part: RETAINER — DENTED (CARGO DOOR) · airframe 26,730 hrs · 25,410 cycles

CARGO DOOR LOWER SEAL RETAINER HAS 3 EA DENTS. R & R WITH NEW PN IAW SRM 51-42-06.

Part: SEAL — TORN (JET PIPE) · airframe 26,730 hrs · 25,410 cycles

LT JET PIPE FAIRING UPPER LOWER SEALS ARE TORN. R & R UPPER & LOWER SEALS IAW CMM 78-11-00, SRS 070.

Part: SUPPORT ANGLE — CRACKED (BS 280) · airframe 26,730 hrs · 25,410 cycles

FS 280 FLOOR SUPPORT ANGLE INBD AND OTBD OF LBL 9 ARE CRACKED. REPLACED.

Part: STRUCTURE — CRACKED (RT WING) · airframe 26,730 hrs · 25,410 cycles

RIGHT WING L/E AT WS 139 TO 149 IS CRACKED AT WS149. R & R WITH NEW SERVICEABLE EDGING.

Part: SILL — CRACKED (BS 280) · airframe 26,730 hrs · 25,410 cycles

PASSENGER DOOR UPPER SILL LINTEL CRACKED AT FS 280, BULKHEAD. R & R.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 26,730 hrs · 25,410 cycles

PASSENGER DOOR POWER ASSIST MOTOR MOUNT BRACKET CRACKED. REPLACED PART.

Part: SKIN — CORRODED (BS 473) · airframe 26,730 hrs · 25,410 cycles

LIGHT SURFACE CORROSION FS 473.15 ON SKIN. REMOVED CORROSION TREATED PRIMED & TOP COATED.

Part: ANGLE — CORRODED (BS 461-499) · airframe 26,730 hrs · 25,410 cycles

WEB ANGLE BETWEEN FS 461-499 HAS LIGHT SURFACE CORROSION. REMOVE CORROSION, TREAT, PRIME, AND PAINT.

Part: HANDLE — CRACKED (CARGO DOOR) · airframe 26,730 hrs · 25,410 cycles

CARGO DOOR EXTERNAL HANDLE CRACKED FWD END. R & R HANDLE IAW SRM 51-41-11, 51-42-21.

Part: ANGLE — CRACKED (BS 280) · airframe 26,730 hrs · 25,410 cycles

OUTBOARD ANGLE ON FS 280, RBL 9 IS CRACKED. REPLACED.

Part: STRINGER — CORRODED (BS 589) · airframe 26,730 hrs · 25,410 cycles

STRINGER 26L CORRODED AT AFT SIDE OF FS 589.00. BLENDED LIGHT SURFACE CORROSION ALODINED, PRIMED, TOP COATED.

Part: STRUCTURE — CHAFED (NOSE COWL) · airframe 26,730 hrs · 25,410 cycles

RT UPPER NOSE COWL T/E STRIP CHAFED IN MULTIPLE AREAS ACROSS ENTIRE LENGTH. R & R EDGE STRIP IAW CMM 71-14-01, SRS070.

Part: SEAT TRACK — CORRODED (BS 559-574) · airframe 26,730 hrs · 25,410 cycles

SEAT TRACK BETWEEN FS 559+112 AND FS 574 AT LBL 9 CORRODED. R & R SEAT TRACK.

Part: SEAL — TORN (JET PIPE) · airframe 26,730 hrs · 25,410 cycles

RT JET PIPE FAIRING L/E SEAL UPPER AND LOWER ARE TORN. REMOVED AND INSTALLED NEW UPPER & LOWER SEALS IAW CMM 78-11-00, SRS 070.

Part: BULKHEAD — GOUGED (BS 621) · airframe 26,166 hrs · 24,864 cycles

GOUGES ON EXISTING REPAIR DOUBLER FS 621.0 PRESSURE BULKHEAD 0.009" MAX D LBL 28.5 X WL 126.0. REO 601R-53-61-4928, REV A.

Part: BULKHEAD — DENTED (BS 621) · airframe 26,166 hrs · 24,864 cycles

GOUGES & DENTS ON EXISTING REPAIR DOUBLER FS 621.00 PRESSURE BULKHEAD LBL 49.2 X WL 101.33 & WL 101.5 LBL 44.4 X WL 103.65 MAX D 0.038" 0.053" & 0.053 RESPECTIVELY. REO 601R-53-61-4925 PRELIMINARY P1 ISSUED.

Part: COMPUTER — FAILED (FUEL SYSTEM) · airframe 25,232 hrs · 23,982 cycles

AT CRUISE FUEL CHANNEL 1/2 CAUTION MSG AND XFLOW STATUS MSG CLEARED, (THIS WAS ON MEL) FOLLOWED BY THE FUEL CHANNEL 1/2 CAUTION MSG CLEARING (AFTER 3 SECONDS) THEN THE FUEL CHANNEL 1 FAIL STATUS MSG ILLUMINATED AND SMOKE WAS SMELLED AT ROW 9. REMOVED AND REPLACED FUEL SYSTEM COMPUTER IAW AMM 28-41-16 OP CL GOOD, A/C OK FOR SERVICE.

Part: BALLAST — DEFECTIVE (CABIN) · airframe 24,481 hrs · 23,249 cycles

STRONG ELECTRICAL / PLASTIC ODOR ROW 10. REF W/O 191295. REMOVED AND REPLACED PAX SIDEWALL LIGHTS 9, 10 & 11 AND BALLAST FOR EACH. OPS CHECK GOOD. RAN FOR 1 HOUR WITH NO SMELL.

Part: A/C PACK — MALFUNCTIONED · airframe 23,976 hrs · 22,741 cycles

WITH LEFT PACK ON, ENGINE BLEED, PACK SHUTS OFF WHEN THROTTLES ADVANCED TO 75 PERCENT.

Part: UNKNOWN — ODOR (CARGO BAY) · airframe 23,960 hrs · 22,725 cycles

RAMP REPORTED BURNING ODOR IN CARGO COMPARTMENT. INSPECTED CARGO FIRE PROTECTION, CARGO FAN AND CARGO LIGHTS AND AFT EQUIPMENT BAY. UNABLE TO DUPLICATE AT THIS TIME.

Part: UNKNOWN — ODOR (CARGO BAY) · airframe 23,960 hrs · 22,725 cycles

AT GATE, RAMP REPORTS BURNING ODOR IN CARGO COMPARTMENT. INSPECTED CARGO FIRE PROTECTION, CARGO FAN, CARGO LIGHTS, BOTH PAX AND AFT EQUIPEMENT BAY. UNABLE TO DUPLICATE AT THIS TIME.

Part: ANGLE — CORRODED (PAX DOOR) · corrosion level 2 · airframe 22,173 hrs · 20,837 cycles

PAX DOOR PANEL 832ET HAS MINOR CHAFE DAMAGE AND SURFACE CORROSION ON ANGLE. REMOVED CORROSION AND MINOR CHAFING IAW SRM 51-21-06. FOUND OUT OF LIMITS.

Part: RISER — CRACKED (PAX DOOR) · airframe 22,173 hrs · 20,837 cycles

PAX DOOR AFT STOP RISER IS CRACKED IN 2 PLACES UNDER STEP PANELS 832DT AND 832CT. REPAIRED CRACKS IAW REO 601R-52-11-702, REV C.

Part: GUIDE — OUT OF POSITION (LT WING TE FLAP) · airframe 22,173 hrs · 20,837 cycles

LEFT OTBD FLAP CENTER HINGE ARM OTBD FAIRING GUIDE IS CHAFING THE BUTTE DOOR ACTUATOR. R & R FAIRING GUIDE BRACKET LT OTBD FLAP CENTER HINGE OTBD SIDE WITH SERVICEABLE PART IAW SRM 51-42-06, 51-40-06 AND 51-24-21.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 22,173 hrs · 20,837 cycles

RIGHT INBD FLAP VANE CHAFED 3 PLACES BLENDED AND SMOOTHED CHAFING WO IAW REO601R-57-52-004.

Part: DOUBLER — CHAFED (RT NACELLE) · airframe 22,173 hrs · 20,837 cycles

RT LOWER CORE COWL EXTERNAL DOUBLER CHAFED AROUND FWD LATCHES. BLENDED CHAFING AROUND RT CORE COWL EXTERNAL DOUBLER IAW CMM 71-12-01-300-822 AOL.

Part: DOOR — CHAFED (RT MLG) · airframe 22,173 hrs · 20,837 cycles

RT MLG DOOR INBD EDGE CHAFED, REMOVED CHAFED FILLER, FABRICATED NEW FILLER IAW REO 601R-52-82-034 AND INSTALLED.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 22,173 hrs · 20,837 cycles

LEFT INBD FLAP VANE CHAFED 3 PLACES BLENDED AND SMOOTHED CHAFING IAW REO 601R-57-52-004.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 22,173 hrs · 20,837 cycles

PAX DOOR AFT DRAG ANGLE CRACKED JUST AFT OF POWER ASSIST CABLE PULLEY BRACKET. REMOVED DAMAGED DRAG ANGLE AND REPAIRED WITH SERVICEABLE DRAG ANGLE IAW REO 601R-52-11-513.

Part: SHIELD — CHAFED (RT MLG DOOR) · airframe 22,173 hrs · 20,837 cycles

RT MLG WHEEL SPLASH SHIELD CHAFED. FABRICATED AND INSTALLED NEW RT MLG WHEEL SPLASH SHIELD IAW SRM 51-24-21 AND SRM 51-41-20.

Part: DOOR — CHAFED (LT MLG) · airframe 22,173 hrs · 20,837 cycles

LT MLG DOOR INBD L/E CHAFED. REMOVED CHAFED FILLERS, FABRICATED NEW FILLERS IAW REO 601R-52-82-034 AND REO 601R-52-82-102 AND INSTALLED.

Part: ANGLE — DAMAGED (BS 559) · airframe 22,173 hrs · 20,837 cycles

FS 559 LOWER CAP ANGLE REQUIRES REINFORCEMENT IAW REO 601R-53-41-1816. REPAIRED CAP ANGLE IAW REO 601R-53-41-1116.

Part: RIB — CRACKED (LT WING) · airframe 22,173 hrs · 20,837 cycles

LT MLG WHEEL WELL BATTERY RIB IS CRACKED. REPAIRED LT BATT RIB IAW REO 601R-57-51-046.

Part: BUSHING — CORRODED (HINGE FITTING) · corrosion level 1 · airframe 17,275 hrs · 15,754 cycles

LT WING INBD AND OTBD AILERON HINGE FITTING PLATES AND BUSHINGS ARE CORRODED. LT WING INBD AND OTBD AILERON HINGE FITTING PLATES AND BUSHINGS ARE REPLACED IAW AMM 20-11-00-910-801 AND AMM 20-26-00-910-803 AND SRM 51-42-06. (K)

Part: ANGLE — CRACKED (BS 559) · airframe 17,275 hrs · 15,754 cycles

PRESSURE BULKHEAD CAP ANGLE IS CRACKED IN THE RADIUS FS 559.00, RBL 20.0 CRACK LENGTH IS .250" PRESSURE BULKHEAD CAP ANGLE REPAIRED AT FS 559, RBL 10 IAW REEO 601R-53-41-260, REV C, SCHEME D. (K)

Part: SKIN — CORRODED (RT WING) · corrosion level 1 · airframe 17,275 hrs · 15,754 cycles

CORROSION FOUND ON FUEL ACCESS DOOR CUT-OUT 640DB. REPAIR PERFORMED ON FUEL ACCESS DOOR DUT-OUT 640DB IAW REO 601R-57-21-030, REV "G" AND AWAC E06/021/457, REV "A". (K)

Part: STIFFENER — GOUGED (RT TAILPIPE) · airframe 17,275 hrs · 15,754 cycles

RT ENGINE TAIL PIPE EXHAUST FAIRING, STIFFENER GOUGED ADJACENT TO ACCESS PANEL AT 6 O`CLOCK POSITION ACCESS PANEL STIFFENER IAW CMM 78-11-00-300-818-A01, REPAIR SRS 084. (K)

Part: SHIM — CORRODED (KICK PLATE) · corrosion level 2 · airframe 17,275 hrs · 15,754 cycles

SERVICE DOOR KICK PLATE SHIM IS CORRODED. SERVICE DOOR KICK PLATE SHIM REPLACED IAW AMM 20-21-00-910-801. (K)

Part: BULKHEAD — CRACKED (BS 280) · airframe 17,275 hrs · 15,754 cycles

CRACK FOUND (2X) ON AFT ANGLE OF PILOT BULKHEAD AT FS 280.00, RBL 9.0 AND LBL 9.0. REPAIR PERFORMED ON PILOT BULKHEAD AT FS 280.00, RBL 9.0 AND LBL 9.00 WL 73.10 IAW REO 601R-53-11-136 REV "A". (K)

Part: ATTACH FITTING — CRACKED (BS 484) · airframe 17,275 hrs · 15,754 cycles

CRACK FOUND ON INTERCOSTAL CLIP AT FS 484.00, RBL 27.00 AND RBL 36.00 (CRACK ARE NR1 .50", NR2 .50") CLIP AT FS 484.00, RBL 36.00 REPLACED IAW SRM 51-42-06 AND 51-42-21, REMAINING CLIP TO BE REPLACED AT FS 484.00, RBL 27.00, TRANSFERRED MWC 140147-225. (K)

Part: PANEL — CRACKED (PAX DOOR) · airframe 17,275 hrs · 15,754 cycles

PAX DOOR, AFT PANEL CRACKED IN ZONE 3, REF REO 601R-52-11-702. REPAIR PERFORMED ON PAX DOOR AFT SIDE PANEL ZONE 3 IAW REO 601R-52-11-702 A 1-3, REV A. (K)

Part: BULKHEAD — CRACKED (BS 202) · airframe 172,785 hrs · 15,754 cycles

CRACK FOUND ON FWD PRESSURE BULKHEAD AT FS 202.75, LBL 23.71 AT PARKING BRAKE. REPAIR C/OUT ON FWD PRESSURE BULKHEAD AT FS 202.75, LBL 23.71 AT PARKING BRAKE LOCATION IAW REO 601R-53-11-1763, REV "NC". (K)

Part: SKIN — GOUGED (LT MLG DOOR) · airframe 17,275 hrs · 15,754 cycles

LT MLG DOOR GOUGED AT FWD LOWER CORNER .500" X 2" .040 DEEP REPAIR PERFORMED ON LT MLG DOOR SKIN IAW REO 601R52-82-034 NC. (K)

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 17,275 hrs · 15,754 cycles

PAX DOOR, AFT DRAG ANGLE CRACKED. PAX DOOR AFT DRAG ANGLE REPLACED IAW 601R-52-11-513, REV A. (K)

Part: SUPPORT BRACKET — CRACKED (HYD MANIFOLD) · airframe 17,275 hrs · 15,754 cycles

CRACK FOUND ON RT HYD MANIFOLD SUPPORT BRACKET AT FS 718. RT HYD MANIFOLD SUPPORT BRACKET AT FS 718, REPAIRED IAW REO 53-62-031 REV A. (K)

Part: SKIN — GOUGED (LT WING) · airframe 17,275 hrs · 15,754 cycles

LT WING LWR SKIN GOUGED AFT OF FUEL PANEL 540EB. LT WING LWR SKIN GOUGE BLENDED IAW SRM 51-12-00. NDT C/OUT - NO CRACK FOUND. (K)

Part: SILL — CRACKED (FUSELAGE) · airframe 17,275 hrs · 15,754 cycles

CARGO DOOR CUTOUT, LWR SILL CRACKED AT STOW FLAP BRAKET LOCATION (LENGTH .500"). REPAIRED IAW REO 53-61-174, REV NC AT CARGO DOOR SILL AT STOW FLAP BRACKET. (K)

Part: SKIN — CRACKED (BS 235) · airframe 17,275 hrs · 15,754 cycles

NLG SKIN CUT-OUT CRACK REPAIRED IAW REO 601R-53-11-048, REV C AT FS 235, RBL 6.0. REPAIRED IAW REO 601-53-11-048 REV C FS 235, RBL 6.0. (K)

Part: FITTING — WORN (LT WING) · airframe 17,275 hrs · 15,754 cycles

LT WING OTBD FLAP ALIGNMENT FITTING 601R10156 FOUND ROLLER WEAR DAMAGE LT WING OTBD FLAP ALIGNMENT FITTING 601R10156. REPAIRED IAW REO 601R-57-51-143, REV NC. (K)

Part: FLOOR SUPPORT — CORRODED (BS 605-621) · corrosion level 1 · airframe 17,275 hrs · 15,754 cycles

CORROSION FOUND ON FLOOR STRUCTURE BTWN FS 605.00 AND 621.00, RBL 45.00 ON FLOOR STRUCTURE BTWN FS 605.00 AND FS 621.00 AT RBL 45.00 CORROSION REPAIRED IAW SRM 51-21-06. (K)

Part: SKIN — CORRODED (LT WING) · corrosion level 1 · airframe 17,275 hrs · 15,754 cycles

LT WING CORROSION FOUND ON FUEL ACCESS DOOR CUT OUT 540EB. ON LT WING, ON FUEL TANK ACCESS DOOR CUT-OUT 540EB CORROSION REPAIRED IAW REO 601R57-21-030, REV G. (K)

Part: SKIN — CORRODED (LT WING) · corrosion level 1 · airframe 17,275 hrs · 15,754 cycles

LT WING CORROSION FOUND ON FUEL ACCESS DOOR CUT-OUT 550GB. ON LT WING, ON FUEL TANK ACCESS DOOR CUT-OUT 550GB CORROSION REPAIRED IAW REO 601R-57-21-030, REV G. (K)

Part: SKIN — CORRODED (RT WING) · airframe 17,275 hrs · 15,754 cycles

CORROSION FOUND ON FUEL ACCESS DOOR CUT-OUT 650BB. CORRODION ON FUEL ACCESS DOOR CUT-OUT 650BB REPAIRED IAW REO 601R-57-21-030, REV G AND EO E06/012/457 REV "A". (K)

Part: BULKHEAD — CRACKED (BS 280)

CRACK FOUND ON PILOT BULKHEAD AT FS 280.00, LBL 9.0 (CRACK LENGTH .400). REPAIRED PERFORMED ON PILOT BULKHEAD AT FS 280.00, LBL 9.0 IAW REO 601R-53-11-171 "SCHEME A", REV D.

Part: SKIN — CORRODED (RT WING) · corrosion level 1 · airframe 17,275 hrs · 15,754 cycles

CORROSION FOUND ON FUEL ACCESS DOOR CUT-OUT 650DB. CORROSION REMOVED ON FUEL ACCESS DOOR CUT-OUT 650DB IAW REO 601R-57-21-030, REV "G" AND EO E06/021/457, REV "A".

Part: SKIN — CORRODED (RT WING) · airframe 17,275 hrs · 15,754 cycles

CORROSION FOUND ON FUEL ACCESS DOOR CUT-OUT 650CB CORROSION REMOVED ON FUEL ACCESS DOOR CUT-OUT 650CB IAW REO 601R-57-21-030, REV G. (K)

Part: SKIN — CORRODED (RT WING) · corrosion level 1 · airframe 17,275 hrs · 15,754 cycles

CORROSION FOUND ON FUEL ACCESS DOOR CUT-OUT 640BB ON FUEL TANK ACCESS DOOR CUT-OUT 640BB CORROSION REPAIRED IAW REO 601R-57-21-030, REV "G" AND EO E06/021/457, REV "A". (K)

Part: SKIN — CORRODED (RT WING) · corrosion level 1 · airframe 17,275 hrs · 15,754 cycles

CORROSION FOUND ON FUEL ACCESS DOOR CUT-OUT 640AB. CORROSION REMOVED ON FUEL ACCESS DOOR CUT-OUT 640AB IAW REO 601R-57-21-030, REV G. EO. E06/021/457, REV A. (K)

Part: SKIN — CORRODED (LT WING) · corrosion level 1 · airframe 17,275 hrs · 15,754 cycles

CORRODION FOUND ON FUEL TANK ACCESS DOOR CUT-OUT 510AB. ON FUEL TANK ACCESS DOOR CUT-OUT 510AB CORROSION REPAIRED IAW REO 601R-57-21-030 REV G AND EO E06/021/457, REV "A". (K)

Part: FITTING — CRACKED (FLOORBEAM) · airframe 17,275 hrs · 15,754 cycles

CRACK FOUND ON FLOORBEAM FITTING FS 461, RBL 9.00 OTBD. FLOORBEAM FITTING AT FS 461.00, RBL 9.00 OTBD REPLACED IAW SRM 51-42-21. (K)

Part: SKIN — CORRODED (LT WING) · corrosion level 1 · airframe 17,275 hrs · 15,754 cycles

CORROSION FOUND ON FUEL ACCESS DOOR CUT-OUT 510BB. CORROSION REMOVED ON FUEL ACCESS DOOR CUT-OUT 510BB IAW REO 601R-57-21-030, REV "G" AND EO E06/021/457, REV "A". (K)

Part: BULKHEAD — CRACKED (BS 621) · airframe 17,275 hrs · 15,754 cycles

AFT PRESSURE BULKHEAD AT FS 621.00 CRACK AT LINTEL. AFT PRESSURE BULKHEAD AT LINTEL LOCATION REPAIRD IAW REO 601R-53-61-1230, REV D. (K)

Part: SKIN — CORRODED (LT WING) · corrosion level 1 · airframe 17,275 hrs · 15,754 cycles

CORROSION FOUND ON FUEL ACCESS DOOR CUT-OUT 550CB. CORROSION REMOVED ON FUEL ACCESS DOOR CUT-OUT 550CB IAW REO 601R-57-21-030, REV "G" AND EO E06/021/457, REV "A". (K)

Part: SKIN — CORRODED (LT WING) · corrosion level 1 · airframe 17,275 hrs · 15,754 cycles

CORROSION FOUND ON FUEL ACCESS DOOR CUT-OUT 550DB. CORROSION REMOVED ON FUEL ACCESS DOOR CUT-OUT 550DB IAW REO 601R-57-21-060, REV G. (K)

Part: SKIN — CORRODED (LT WING) · corrosion level 1 · airframe 17,275 hrs · 15,754 cycles

CORROSION FOUND ON FUEL ACCESS DOOR CUT-OUT 540DB. CORROSION ON FUEL ACCESS DOOR CUT-OUT 540DB REMOVED IAW REO 601R-57-21-030, REV "G" AND EO E06/021/457, REV A. (K)

Part: STRUCTURE — CRACKED (DOOR STAIR) · airframe 17,275 hrs · 15,754 cycles

REPAIR CRACKS ON PASSENGER DOOR STAIR, TOP AFT CORNER OF EDGE MEMBER. REPAIR PERFORMED ON PASSENGER DOOR STAIR, TOP AFT CORNER OF EDGE MEMBER IAW REO 601R-52-11-27. (K)

Part: FITTING — WORN (RT WING) · airframe 17,275 hrs · 15,754 cycles

RT WING OTBD FLAP ALIGNMENT FITTING 601R10156 FOUND WITH ROLLER WEAR DAMAGE. RT WING, OTBD FLAP ALIGNMENT FITTING, REPAIRED IAW REO 601R57-51-149, REV NC. (K)

Part: BULKHEAD — CRACKED (BS 280) · airframe 17,275 hrs · 15,754 cycles

CRACK FOUND ON PILOT BULKHEAD AT FS 280.00, RBL 9.0 (LENGTH 2.250"). PILOT BULKHEAD AT FS 280.00, RBL 9.00 REPAIRED AND PERFORMED IAW REO 601R-53-11-171, REV "D". (K)

Part: BULKHEAD — DAMAGED (BS 621) · airframe 17,275 hrs · 15,754 cycles

AFT PRESSURE BULKHEAD FS 621, LBL 27.50, LB 130.00 ABOVE CARGO DOOR TRACK REPAIRED IAW REO 601R-53-61-1541, REV B. (K)

Part: SILL — CRACKED (BS 589-605) · airframe 17,275 hrs · 15,754 cycles

CARGO DOOR SILL CRACKED AT FS 589.00 AND FS 605.00. CARGO DOOR SILL REPAIRED IAW REO 601R-53-61-433. (K)

Part: FIRE BOTTLE — DISCHARGED (CARGO BAY) · airframe 16,236 hrs · 14,746 cycles

CARGO BOTTLE LOW MESSAGE IN FLIGHT. COMPLIED WITH QRH, DIVERTED, MESSAGE OUT ON LANDING. REMOVED AND REPLACED LT CARGO FIRE EXTINGUISHER BOTTLE A2HL IAW AMM 26-25-01. OPS CHECK GOOD AT THIS TIME. (K)

Part: WARNING LIGHT — ILLUMINATED (MLG) · airframe 15,015 hrs · 13,614 cycles

ON GEAR EXTENSION AND RETRACTION RECEIVED ANTI-SKID OB CAUTION MESSAGE. COMPLIED WITH QRH. EMERGENCY LANDING DECLARED. BRAKE SYSTEM OPS CHECK GOOD IAW 32-43-00710-801. (K)

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 14,233 hrs · 12,891 cycles

FLAPS FAILED AT ZERO IN FLIGHT. BRAKE TEMPS WERE IN NORMAL RANGE AT LANDING. COMPLIED WITH RESET PROCEDURE IAW AWAC SUPP 98-018B STEPS 1.3 AND 1.4 FLAPS SYSTEM RESET OK. AIRCRAFT RELEASED FOR SERVICE. (A)

Part: FUEL LINE — LEAKING (FUEL SYSTEM) · airframe 13,375 hrs · 12,053 cycles

FUEL LEAKING FROM DRAIN UNDER AFT FUSELAGE. REMOVED AND REPLACED FUEL LINE ASSY IAW 28-20-01. (K)

Part: SELECTOR VALVE — FAILED (NLG)

ON DEPARTURE, SELECTED GEAR LEVER UP. RECEIVED TRIPLE CHIME AND DISAGREE AURAL MESSAGE. GOT GEAR DISAGREE NOSE GEAR DOOR WARN MESSAGES AND WOW INPUT AND NWS INOPERATIVE CAUTION MESSAGES. EXECUTED QRH IN THAT ORDER, HAD 3 GEAR DOWN LOCKED INDICATIONS. REMOVED AND REPLACED NLG SELECTOR VALVE, SWING OF NLG CHECKS GOOD IAW AMM 32-33-10. (K)

Part: WIRE HARNESS — DAMAGED (NR 1 FIRE DETECT)

ON TAKEOFF ROLL, THRUST LEVER ADVANCEMENT GOT LEFT JET OVERHEAT FAIL CAS MESSAGE. ABORTED TAKEOFF AT 10 KNOTS, MAX BTMS READING IS 4, TAKEOFF WEIGHT 44,300 LBS. REMOVED AND REPLACED ENGINE NR 1 FIRE DETECTION HARNESS PER AMM 26-11-07. OPS CHECK GOOD. (M)

Part: SKIN — DAMAGED (FUSELAGE)

RT KIDNEY PANEL CUTOUT AT FWD FUSELAGE HAS ONE ELONGATED HOLE. MAINTENANCE REPAIRED IAW REO 601R-53-11-162. (M)

Part: PANEL — DAMAGED (FUSELAGE)

FOUND RIGHT KIDNEY PANEL CUTOUT AT FORWARD FUSELAGE HAS ONE ELONGATED HOLE. (M)

Part: ATTACH FITTING — CRACKED (FS 280)

FOUND FS 280 LBL 9 OUTBOARD CLIP CRACKED. SUP - MAINTENANCE REPLACED CLIP IAW SRM 51-42-13, 51-42-21 AND BSC SRM 601R-57-0057A. (M)

Part: ATTACH FITTING — CRACKED (FS 280)

FOUND FS 280 RBL 9 OUTBOARD CLIP CRACKED. SUP - MAINTENANCE REPLACED CLIP IAW SRM 51-42-06 AND BSC SRM 601R-53-0057A. (M)

Part: ANGLE — CRACKED (FS 559)

FOUND FS 559 LBL 9 VERTICAL POST AT OUTBOARD LEG IS CRACKED AT BOTTOM RIVET. SUP - MAINTENANCE REPAIRED POST OUTBOARD LEG AT LBL 9, FS 559 IAW REO 601R-53-41-057 REV A. (M)

Part: ATTACH FITTING — CRACKED (FS 280)

FOUND FS 280 LBL 9 INBOARD CLIP CRACKED. SUP - MAINTENANCE REPLACED CLIP IAW SRM 51-42-06 AND 51-42-21. (M)

Part: ATTACH FITTING — CRACKED (FS 280)

FOUND FS 280 RBL 9 INBOARD CLIP CRACKED. SUP - MAINTENANCE REPLACED CLIP IAW SRM 51-42-06 AND 51-42-21. (M)

Part: CHANNEL — CRACKED (CARGO DOOR)

CARGO DOOR FORWARD TRACK BOTTOM CHANNEL, P/N 601R35050-25 IS CRACKED. MAINTENANCE REMOVED AND INSTALLED SERVICEABLE CHANNEL P/N 601R35050-25 IAW CRJ 200 SRM 51-42-06. (M)

Part: BRACKET — CRACKED (FUSELAGE)

BRAKE TRANSDUCER BRACKET IN LT MLG WHEEL WELL IS CRACKED. MAINTENANCE REMOVED AND INSTALLED SERVICEABLE BRACKET P/N 601R75262-159 IAW CRJ 200 SRM 51-41-04, AND 51-42-06. (M)

Part: SUPPORT BRACKET — CRACKED (FUSELAGE)

EXTERNAL POWER RECEPTACLE SUPPORT BRACKET, P/N 600-33283-33, IS CRACKED AT RECEPTACLE FORWARD OUTBOARD ATTACH MEDT BOLT HOLE. CRACK IS APPROX .6 INCHES LONG. (M)

Part: BULKHEAD — CRACKED (BS 202)

FS 202.75 FORWARD PRESSURE BULKHEAD IS CRACKED LT SIDE AT WL 65, APPROX LBL 28, FITTING FOR RT INBOARD BRAKE NR 3 HYD LINE. CRACK IS APPROX 1.3 INCHES LONG. SUP - MAINTENANCE REPAIRED CRACK BY TRIMMING OUT DAMAGE AND INSTALLING FILLER AND DOUBLE IAW BSC EO 601R-53-13065. (M)

Part: BULKHEAD — CRACKED (BS 202)

FS 202.75 FORWARD PRESSURE BULKHEAD IS CRACKED LT SIDE AT WL 65, APPROX LBL 28, FITTING FOR RT INBOARD BRAKE NR 3 HYD LINE. CRACK IS APPROX 1.3 INCH LONG. (M)

Part: BRACKET — CRACKED (FUSELAGE)

EXTERNAL POWER RECEPTACLE SUPPORT BRACKET, P/N 600-33283-33, IS CRACKED AT RECEPTACLE FORWARD OUTBOARD ATTACH MEDT BOLT HOLE. CRACK IS APPROX .5 INCHES LONG. SUP - MAINTENANCE REMOVED AND INSTALLED SERVICEABLE SUPPORT BRACKET P/N 600-33283-33 IAW CRJ 200 SRM 51-42-06 AND 51-42-21. (M)

Part: TARGET — LOOSE (LT MLG)

AFTER TAKEOFF ON GEAR RETRACTION LEFT MLG INDICATED INTRANSIT, LT MLG NEVER SHOWED UP AND LOCKED. GEAR DISAGREE CAS MESSAGE 28 SECONDS. COMPLIED WITH QRH, PULLED EMERGENCY GEAR EXT HANDLE, GEAR CAME DOWN, 3 GREEN ALL DOWN AND LOCKED. FOUND LEFT MLG UPLOCK TARGET EXCESSIVELY LOOSE. RESECURED TARGET, OPS CHECK GOOD PER AMM 32-60. (M)

Part: CONTROL CABLE — FRAYED (AILERONS) · airframe 7,894 hrs · 6,769 cycles

SPOILERON FAULT, AILERON FEELS ROUGH WHEN TURNED TO THE RIGHT. AC HAS FRAYED AILERON CABLES DUE TO INCORRECT INSTALLATION, REPLACED CABLES.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 7,535 hrs · 6,455 cycles

PASSENGER DOOR DRAG ANGLE IS CRACKED 1.0 INCH IN RADIUS ABOVE POWER ASSIST CABLE SUPPORT PULLEY BRACKET. MAINTENANCE REPAIRED PAX DOOR ANGLE IAW MDG REO. (K)

Part: ANGLE — CRACKED (BS 484)

RIGHT FS 484 AT RBL 36 ANGLE CRACKED. MAINTENANCE REPAIRED CRACKED ANGLE BY REMOVING CRACKS FLANGE AND INSTALLING A REPAIR FLANGE BRAS AND REO. (M)

Part: FLOOR SUPPORT — CRACKED (BS 621)

LT FS 621 FLOOR SUPPORT ANGLE CRACKED. MAINTENANCE LT FS 621.00, FLOOR SUPPORT ANGLE IAW REO. (M)

Part: ANGLE — CRACKED (BS 484)

FOUND LT FS 484 AT LBL 36 ANGLE CRACKED. MAINTENANCE REPAIRED CRACKED ANGLE BY REMOVEING CRACKED FLANGE AND INSTALLING REPAIRED FLANGE IAW SRM AND REO. (M)

Part: FLOORBEAM — CRACKED (BS 621)

RIGHT FS 621 FLOORBEAM ANGLE CRACKED. REPAIRED RT FS 621.00 FLOOR SUPPORT ANGLE IAW REO. (M)

Part: INTERCOSTAL — CRACKED (FS 621-625.3)

FOUND RT SIDE FS 621 TO 625.3 INTERCOSTAL AT STRINGER 142 IS CRACKED NEAR RADIUS APPROX .80 INCH LONG. MAINTENANCE REMOVED CRACKED INTERCOSTAL AND INSTALLED NEW INTERCOSTAL IAW SRM. (M)

Part: PIN — DAMAGED (NLG CAM LOCK)

AIR RETURN GEAR DISAGREE MASTER WARNING, PERFORMED QRH LIFT OFF POSITIVE CLIMB AT 160 KNOTS 0004Z NOSE GEAR DID NOT RETRACT, IT REMAINED DOWN ENTIRE TIME. REPACKED NOSE GEAR AND INSTALLED NEW CAM LOCKING PINS. OPS AND LEAK CHECK GOOD AND SWING SATISFACTORY. ALL OK FOR SERVICE. REF CRJ MM 32-20-04 AND 32-33-00. (M)

Part: ANGLE — CRACKED (FUSELAGE)

MAINTENANCE WORK CARD NR 14, FOUND THE RIGHT OBLIQUE ANGLE IS CRACKED AT FS 625.3 ADJACENT TO STRINGER 14R AT WATERLINE 95. (M)

Part: WARNING LIGHT — FALSE ACTIVATION (CARGO SMOKE) · airframe 3,876 hrs · 3,296 cycles

SMOKE CARGO WARNING WHILE TAXIING. RETURN TO GATE. CARGO PIT CHECK FOR SMOKE, NONE NOTED. NO ODOR NOTED. COMPLIED WITH OPS TEST OF CARGO SMOKE DETECTION SYSTEM. IAW MM 26-15-00. OPS CHECK GOOD.

Part: WARNING LIGHT — ILLUMINATED (CARGO SMOKE) · airframe 3,856 hrs

SMOKE CARGO WARNING MESSAGE DURING TAXI. COMPLIED WITH IMMEDIATE ACTION CHECKLIST QRH. CARGO BOTTLE LOW CAUTION MESSAGE. MESSAGE SMOKE CARGO EXTINGUISHED. REMOVED AND REPLACED BOTH FIRE BOTTLES AND SQUIBS IAW MM. REMOVED FROM MEL AND PLACARD. REMOVED AND REPLACED CARGO SMOKE DETECTOR. INSIDE SMOKE DETECTOR WAS DIRTY CAUSING INTERMITTENT ALARMS. CLEANED INSIDE DETECTOR. (M)