N8688C

Part: LIGHT — BROKEN (CABIN) · airframe 30,269 hrs · 28,146 cycles

FLOOR PATH LIGHTING STRIP COMING UP AT ROW 5C AND 0. REPLACED BROKEN FLOOR PATH LIGHT STRIP COVER I/A/W CRJ200 AMM CH 33-51-01. OPS CHECK GOOD.

Part: HOUSING — CRACKED (DOOR HANDLE) · airframe 29,954 hrs · 27,798 cycles

E/E BAY DOOR HANDLE HOUSING CRACKED. REMOVED AND REPLACED HOUSING ASSY PER CRJ 200 AMM 52-42-03.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 29,954 hrs · 27,798 cycles

RBL 9 SEAT TRACK #3 CORRODED. REMOVED AND REPLACED SEAT TRACK.

Part: REPAIR — GOUGED (SKIN) · airframe 29,954 hrs · 27,798 cycles

REPAIR DOUBLER AFT OF LOW PRESS. GROUND AIR DOOR GOUGED. REPAIRED DAMAGE PER REO 601R-53-61-7014.

Part: STRUCTURE — CRACKED (PAX DOOR) · airframe 29,954 hrs · 27,798 cycles

PAX DOOR EDGE MEMBER CRACKED AT PERVIOUS REPAIR. REPAIRED PER REO 601R-52-11-279.

Part: LANDING — CRACKED (AIR DOOR) · airframe 29,954 hrs · 27,798 cycles

AFT SIDE OF GROUND AIR DOOR LANDING CRACKED. REMOVED AND REPLACED LANDING.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 29,954 hrs · 27,798 cycles

SEAT RAIL RBL9 SECTION #4 HAS AREAS OF CORROSION. REMOVED AND REPLACED SEAT TRACK DUE TO CORROSION.

Part: DOUBLER — CRACKED (RT NACELLE) · airframe 29,954 hrs · 27,798 cycles

RH ENGINE UPPER CORE COWL 445AT UPPER FWD CORNER IS BENT AND CRACKED. INSTALLED DOUBLER DUE TO CRACKING.

Part: BEAM — CORRODED (BS 574-605) · airframe 29,954 hrs · 27,798 cycles

RBL 27 BEAM CAP FS 574-605 CORRODED. REMOVED AND REPLACED BEAM CAP.

Part: STIFFENER — CRACKED (LT EXHAUST) · airframe 29,954 hrs · 27,798 cycles

LH ENG EXHAUST FAIRING STIFFNER ANGLE RING CRACKED. REMOVED AND REPLACED STIFFNER DUE TO CRACK.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 29,954 hrs · 27,798 cycles

LH SIDE SEAT RAIL #3 CORRODED. REMOVED AND REPLACED SEAT RAIL

Part: PANEL — DAMAGED (NACELLE) · airframe 29,954 hrs · 27,798 cycles

PANEL 412DB DIVIDERS ARE KNIFE EDGED. REMOVED AND REPLACED KNIFE EDGED DIVIDERS

Part: PLATE — CRACKED (SERVICE DOOR) · airframe 29,954 hrs · 27,798 cycles

SERVICE DOOR PROTECTOR PLATE CRACKED AND CORRODED. REMOVED AND REPLACED PLATE.

Part: ANGLE — CRACKED (BS 193) · airframe 29,954 hrs · 27,798 cycles

ANGLE CLIP FS 193 CRACKED. REMOVED AND REPLACED CLIP PER SRM

Part: SEAT TRACK — CORRODED (CABIN) · airframe 29,954 hrs · 27,798 cycles

RH SIDE SEAT RAIL #7 CORRODED. REMOVED AND REPLACED SEAT RAIL.

Part: BEAM — CORRODED (BS 574-610) · airframe 29,954 hrs · 27,798 cycles

LBL 27 CORRODED FS 574-610. REMOVED AND REPLACED BEAM CAP

Part: DRAG ANGLE — CRACKED (RT MLG) · airframe 29,954 hrs · 27,798 cycles

RH MLG BAY, DRAG ANGLE CRACKED. REMOVED AND REPLACED DRAG ANGLE

Part: SEAT TRACK — CORRODED (CABIN) · airframe 29,954 hrs · 27,798 cycles

LH SIDE SEAT RAIL SECTION #2 HAS AREAS OF CORROSION. REMOVED AND REPLACED SEAT RAIL IAW CRJ 200 AMM 53-01-11

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 29,954 hrs · 27,798 cycles

L/H FLAP TOP SIDE HAS DENT IN MIDDLE CENTER. MEASURED AND EVUALATED DENT WITHIN LIMITS IAW CRJ 200 SRM 57-52-00 DENT ENTERED INTO DENT LOG FORM 908.9 AND MARKED WITH YELLOW DOT

Part: SEAT TRACK — CORRODED (CABIN) · airframe 29,954 hrs · 27,798 cycles

SEAT RAIL LBL9 SECTION #2 HAS AREAS OF CORROSION. REMOVED AND REPLACED SEAT TRACK IAW CRJ 200 AMM 53-01-11

Part: DRAG ANGLE — CRACKED (LT MLG WW) · airframe 29,954 hrs · 27,798 cycles

LH MLG BAY, DRAG ANGLE CRACKED. REMOVE AND REPLACED DRAG ANGLE DUE TO CRACK.

Part: ATTACH BRACKET — CRACKED (RT MLG WW) · airframe 29,954 hrs · 27,798 cycles

RH MLG BAY, BRAKE PRESSURE TRANSDUCER ATTACH BRACKET CRACKED. REMOVED AND REPLACED BRAKE PRESSURE ATTACH BRACKET

Part: PANEL — DAMAGED (NACELLE) · airframe 29,954 hrs · 27,798 cycles

PANEL 422DB DIVIDERS ARE KNIFE EDGED. REMOVED AND REPLACED DIVIDERS IAW CRJ 200 SRM 51-42-06

Part: SEAT TRACK — CORRODED (CABIN) · airframe 29,954 hrs · 27,798 cycles

RBL9 SEAT RAIL SECTION 1 HAS CORROSION. REMOVED CORROSION FOUND TO BE WITHIN LIMITS.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 29,954 hrs · 27,798 cycles

LH SIDE SEAT RAIL SECTION #6 HAS AREAS OF CORROSION. REMOVED AND REPLACED SEAT TRACK IAW CRJ 200 AMM 53-01-11.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 29,954 hrs · 27,798 cycles

LH SIDE SEAT RAIL SECTION #5 HAS AREAS OF CORROSION. REMOVED AND REPLACED SEAT TRACK IAW CRJ 200 AMM 53-01-11

Part: SEAT TRACK — CORRODED (CABIN) · airframe 29,954 hrs · 27,798 cycles

RBL9 SEAT RAIL SECTION 2 HAS CORROSION. REMOVED AND REPLACED SEAT RAIL

Part: RUB STRIP — CHAFED (NACELLE) · airframe 29,954 hrs · 27,798 cycles

COWL 432AT LE SEAL HAS CHAFING DAMAGE. REMOVED/REPLACED RUB STRIP IAW CMM 71-14-01 SRS091

Part: SEAT TRACK — CORRODED (BS 559) · airframe 29,954 hrs · 27,798 cycles

SEAT TRACK ON TOP OF RBL 27 HAS CORROSION BETWEEN FS 559+80 AND FS 559+96, IN THE CARGO BAY. REMOVED AND REPLACED SEAT TRACK IAW CRJ 200 AMM 53-00-49.

Part: SEAT TRACK — CORRODED (559-574) · airframe 29,954 hrs · 27,798 cycles

SEAT TRACK ON TOP OF LBL 9 HAS CORROSION BETWEEN FS 559+112 AND FS 574 IN THE CARGO BAY. REMOVED AND REPLACED SEAT TRACK IAW CRJ 200 AMM 53-00-49.

Part: SEAT TRACK — CORRODED (BS 559-574) · airframe 29,954 hrs · 27,798 cycles

SEAT TRACK ON TOP OF RBL 9 HAS CORROSION BETWEEN FS 559+112 AND FS 574 IN THE CARGO BAY. REMOVED AND REPLACED SEAT TRACK IAW CRJ 200 AMM 53-00-49

Part: SEAT TRACK — CORRODED (BS 621) · airframe 29,954 hrs · 27,798 cycles

SEAT TRACK ON TOP OF LBL 9 HAS CORROSON JUST FWD OF FS 621, IN THE CARGO BAY. REMOVED AND REPLACED SEAT TRACK IAW CRJ 200 AMM 53-00-49

Part: CARGO TRACK — CORRODED (BS 559) · airframe 29,954 hrs · 27,798 cycles

SEAT TRACK ON TOP OF RBL 9 HAS CORROSION JUST FWD OF FS559+80 AND FS559+96 IN THE CARGO BAY. REMOVED AND REPLACED SEAT TRACK

Part: RELAY — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 29,276 hrs · 27,085 cycles

EMERGENCY LIGHT SYSTEM INOP REMOVED AND REPLACED K1XD AC-ESSENTIAL BUS SENSE RELAY IAW CRJ 200 AMM 24-51-22 AND SLAVED IN PASSENGER SIGN/EMERGENCY LIGHT PANEL IAW CRJ 200 AMM 33-24-10.STILL NO HELP DEFECT REMAINS OPEN. INSTALLED ORIGINAL EME LIGHT PANEL BACK.

Part: STOWAGE BOX — LEAKING (COCKPIT) · airframe 28,792 hrs · 26,563 cycles

OBSERVERS O2 MASK BOX LEAKING FROM PRESS TO TEST MECHANISM. REMOVED AND REPLACED OBSERVERS O2 MASK STOWAGE BOX W/SERV ASSY IAW AMM 35-11-15-400-801, TA 001820. OPS AND LEAK CHECKS GOOD.

Part: SELECTOR VALVE — MALFUNCTIONED (NLG) · airframe 28,782 hrs · 26,551 cycles

ON FINAL FOR 21L INTO DTW SELECTED GEAR DOWN AT 220KTS, TO HELP SLOW DOWN AND CONFIGURE GOT NLG STEERNG INOP CAUTION. RETRACTED GEAR FOR G.A. AND GOT GEAR DISAGREE WARNING, MESSAGE CLRD, THE RAN QRH FOR STEERING INOP MESSAGE CLEARED. APPROACH AND LANDING UNEVENTFUL. PERFORMED DFDR DOWNLOAD IAW AMM 31-31-01 AND FILLED OUT GEAR DISAGREE DATA SHEET TS:001565B-R1. PER MOTR REQUEST, REMOVED AND REPLACED NOSE GEAR SELECTOR VALVE IAW AMM 32-33-10. PERFORMED FUNCTIONAL CHECK OF EXTENSION/RETRACTION SYSTEM IAW AMM 32-30-00. ALL CHECKS GOOD.

Part: UNKNOWN — MALFUNCTIONED (NLG) · airframe 28,615 hrs · 26,369 cycles

PER MEL 26-14-1A PON CLIMBOUT WE LEFT THE GEAR DOWN FOR 10-MINS. UPON GEAR RETRACTION THE MAIN GEAR CAME UP BUT NOSE GEAR DID NOT GEAR DISAGREE WARNING W/ NOSE GEAR SHOWING RED HASH MARKS. QRH COMPLIED WITH AND WOULD NOT ALLOW RE-CYCLE OF GEAR HANDLE WHEN GEAR HANDLE IS IN THE UP POSITION. INTERROGATED PSEU FOUND NLG UPLOCK "FAR" CODE. VERIFIED THE NLG UPLOCK SENSOR GASP WITHIN LIMITS IAW AMM 32-61-05. ALSO INSPECTED THE SENSOR AND TARGET FOR SECURITY WITH NO DEFECTS FOUND. PERFORMED SEVERAL LANDING GEAR EXT/RETR OPERATIONAL TEST SATISFACTORILY IAW AMM 32-30-00. SUSPECTED GEAR WAS RETRACTED WITH AIR SPEED GREATER THAN 200 KIS.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 28,564 hrs · 26,311 cycles

NR 4 EXTERIOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED NR 4 EXTERIOR EMERGENCY LIGHT IAW AMM 33-51-21 OPS CK GOOD.

Part: BATTERY PACK — INOPERATIVE (FLASHLIGHT) · airframe 28,390 hrs · 26,124 cycles

FOUND THE FIRST OFFICER`S FLASHLIGHT NOT WORKING. REMOVED AND REPLACED THE FLASHLIGHT BATTERY PACK IAW AMM 25-61-00. OPS CHECKED GOOD.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 28,099 hrs · 25,774 cycles

SIGNS & EMERGENCY LIGHTS WILL NOT TURN ON. REMOVED & REPLACED AN ELECTRICAL CONNECTOR IAW 20-17-10. OPS TEST IAW 33-51-00. OPS TESTED GOOD. ACFT OK FOR SERVICE.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 27,349 hrs · 24,967 cycles

EMERGENCY LIGHT INOPERATIVE AFTER EXIT ROW, PLUGED IN THE LIGHT ELECTRICAL CONNECTOR, REINSTALLED TOP FLOOR TRACK, AND OPS CHECKED NORMAL IAW AMM 33-51-01.

Part: LIGHT — INOPERATIVE (ROWS 9-12) · airframe 27,323 hrs · 24,942 cycles

FLOOR EMERGENCY LIGHTS INOPERATIVE ROW 9-12. R & R THE EMERGENCY LIGHT SECTION IAW AMM 33-51-01. OPS CHECKED GOOD. OK FOR SERVICE.

Part: LEVER — BROKEN (EXTINGUISHER) · airframe 26,490 hrs · 24,053 cycles

WARDROBE CLOSET PORTABLE FIRE EXTINGUISHER BOTTLES DISCHARGE LEVER BROKEN. R & R THE PORTABLE FIRE EXTINGUISHER BOTTLE IAW AMM 26-23-01.

Part: OXYGEN MASK — TORN · airframe 26,490 hrs · 24,053 cycles

PORTABLE OXYGEN BOTTLE HAS A TORN MASK. R & R THE OXYGEN MASK IAW AMM 35-31-01 OP CHECKED GOOD.

Part: OXYGEN BOX — NO TEST (COCKPIT) · airframe 25,997 hrs · 23,555 cycles

FIRST OFFICERS OXYGEN MASK DOES NOT TEST PRPOERLY PRESSING THE PRESS TO TEST BUTTON CONTINUALLY VENTS OXYGEN AND DOES NOT STOP WHILE BEING DEPRESSED. R & R THE OXYGEN BOX IAW AMM 35-11-15.OPS CHECKED GOOD.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 25,798 hrs · 23,354 cycles

EMERGENCY FLOOR TRACK LIGHTING FORWARD SECTION IS INOP. REMOVED AND REPLACED THE INVERTER AT BATTERY PACK 2 PER THE AMM 33-51-07. OPERATIONAL CHECK GOOD.

Part: SKIN — CORRODED (FUSELAGE) · airframe 24,970 hrs · 22,487 cycles

ACFT BELLY SKIN HAS CORROSION & PITTING ON THE INSIDE, ALL THE WAY AROUND THE FWD E & E BAY DOOR OPENING. REPAIRED LOWER SKIN FWD OF E & E BAY DOOR OPENING IAW EA CRJ253-04230 REV A.

Part: ATTACH BRACKET — CRACKED (RT PYLON) · airframe 24,970 hrs · 22,487 cycles

RIGHT PYLON UPPER STANG FAIRING ATTACH BRACKET CRACKED. R & R RT PYLON UPPER STANG FAIRING ATTACH BRACKET IAW SRM 51-42-06.

Part: SUPPORT — CORRODED · airframe 24,970 hrs · 22,487 cycles

AFTER BIRD DROPPING REMOVAL INSIDE PANEL OPENING 412EB, NOTED THAT THE INBD LOWER SUPPORT STRIP IS CORRODED. REPAIRED LOWER SUPPORT STRIP IAW EA CRJ 254-04297 REV A.

Part: HEAT SHIELD — CRACKED (RT EXHAUST) · airframe 24,970 hrs · 22,487 cycles

RIGHT EXHAUST FAIRING HEAT SHIELD CRACKED. REPAIRED EXHAUST FAIRING IAW CMM 78-11-00 REPAIR SR5027. WO 1012804 4000-0054 & SN 4571234.

Part: STIFFENER — CRACKED (NLG WW) · airframe 24,970 hrs · 22,487 cycles

LEFT SIDE WW STIFFENER IS DAMAGED 13" AFT OF LE OF NLG BAY. REPAIRED STIFFENER IAW EA CRJ253-04279 WO 1012803 1000 0100 SN 4570028.

Part: LOUVER — BENT (LT COWLING) · airframe 24,970 hrs · 22,487 cycles

LEFT ENG ACCESS PANEL 432AC HAS BENT LOUVERS. R & R LOUVERS IAW SRM 51-42-06.

Part: RUB STRIP — GOUGED (LT COWLING) · airframe 24,970 hrs · 22,487 cycles

TRAILING EDGE OF LT LOWER FAN COWL IS GOUGED. REMOVED TE RUB STRIP. INSTALLED NEW TE RUB STRIP IAW CMM 71-14-01 & SRM 51-42-06.

Part: STEP — CRACKED (FUSELAGE) · airframe 24,970 hrs · 22,487 cycles

PASSENGER DOOR STEP 832FT IS CRACKED. RECEIVED NEW STEP PN 601R31980-67 TN EO1343. WO 1012804 3000 0025 SN 4570889.

Part: ATTACH FITTING — CORRODED (FUSELAGE) · airframe 24,970 hrs · 22,487 cycles

FS 621.00 FLOOR ATTACH FITTING LBL 27 HAS A CORRODED FASTENER HOLE OTBD FLANGE. REPAIRED FS 621.00, LBL 27 FLANGE IAW EA CRJ 253-04252 REV A.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 24,970 hrs · 22,487 cycles

CARGO TIE DOWN TRACK LBL 9, FS 559.00+112 HAS CORROSION. R & R CARGO TIE DOWN TRACK IAW AMM 53-00-49-000-801 & 53-00-49-400-801.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 24,970 hrs · 22,487 cycles

WHILE REMOVING CORROSION ON LBL 27, FLOORBEAM AT FS 584 - 605, FOUND OTBD FLANGE TO BE CRACKED. R & R LBL 27 FLOORBEAM AT FS 584 - 605 IAW SRM 51-42-21 & SRM 51-42-06.

Part: SKIN — CRACKED (FUSELAGE) · airframe 24,970 hrs · 22,487 cycles

LEFT FWD FUSELAGE SKIN IS CRACKED AT AFT LATCH FOR PANEL 212AL. R & R SKIN WITH NEW SKIN IAW SRM 51-42-06.

Part: FRAME — CORRODED (FUSELAGE) · airframe 24,970 hrs · 22,487 cycles

FRAME 333 HAS CORROSION ON THE FWD & AFT SIDES, BETWEEN STRINGER 25L & 25R, IN THE E & E BAY. REMOVED CORROSION BY PERFORMING CUT OUT OF FRAME SECTION AT FS 333, FABRICATED & INSTALLED REPAIR PART IAW EA CRJ 253-04234.

Part: SKIN PANEL — CHAFED (RT AILERON) · airframe 24,970 hrs · 22,487 cycles

RIGHT WING AILERON LE ALL PANELS ARE CHAFED ON UPPER SURFACE. R & R LE PANELS IAW SRM 51-42-06.

Part: STRAP — CORRODED (FUSELAGE) · airframe 24,970 hrs · 22,487 cycles

FS 559.00 FLOOR STRAP RBL 27 TO RT FLOOR SILL HAS CORROSION. R & R UNSERVICEABLE FLOOR STRAP AT RBL 27 RT FLOOR SILL WITH A SERVICEABLE FLOOR STRAP AT RBL 27 IAW SRM 51-42-06.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 24,970 hrs · 22,487 cycles

RIGHT SIDE SEAT RAIL NR 6 FROM FS 499 - 544 HAS CORROSION. R & R RT SIDE SEAT RAIL IAW REO 601R-53-00-055 & AMM 53-01-11. WO 1012804 2700 0060, AN 4570942.

Part: SEAT TRACK — DENTED (FUSELAGE) · airframe 24,970 hrs · 22,487 cycles

SEAT RAIL BEAM LBL 9, FS 559.00+93, INBD FLANGE IS DENTED WITH A CREASE AT THE FASTENER HOLE. REPAIRED DAMAGE TO LBL 9, FS 559.00+93 INBD FLANGE IAW SRM 53-00-43 REPAIR 1.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 24,970 hrs · 22,487 cycles

SEAT RAIL BEAM RBL 9 OTBD FLANGE FS 559+48 - 559+80, HAS CORROSION. REPAIRED FLANGE IAW REO 601R-53-00-27 REV D. WO 1012804 1000 0057, SN 4571070.

Part: STRUCTURE — DAMAGED (APU BAY) · airframe 24,970 hrs · 22,487 cycles

APU ENCLOSURE BENT & DISTORTED AT DOOR MATING FLANGE. REPAIRED APU ENCLOSURE AT DOOR MATING FLANGE IAW REO 601R-49-11-071.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 24,970 hrs · 22,487 cycles

RIGHT FLOOR SILL FS 559.00 - 559.00+16 HAS CORROSION. REPAIRED RT FLOOR SILL FS 559 - 559+16 IAW EA CRJ253-04266 REV A.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 24,970 hrs · 22,487 cycles

RIGHT FLOOR SILL FS 563 - 621.00 HAS CORROSION AT FASTENER HOLES. R & R CORRODED RT FLOOR SILL AT FS 563 - 621, WITH A NEW RT FLOOR SILL IAW REO 601R-53-61-5376.

Part: RETAINING RING — CORRODED (LT WING) · airframe 24,970 hrs · 22,487 cycles

LEFT WING INSPECTION LIGHT RETAINER RING CORRODED. R & R BOND RETAINER RING IAW AMM 33-43-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 24,970 hrs · 22,487 cycles

COCKPIT FLOOR SUPPORT AT FS 280 IS CORRODED. R & R COCKPIT FLOOR SUPPORT AT FS 280 IAW SRM 51-42-06, SRM 51-40-11 & SRM 51-44-06.

Part: SKIN PANEL — CORRODED (LT WING) · airframe 24,970 hrs · 22,487 cycles

LEFT WING LE PANEL 530KL, INBD SIDE SKIN HAS CORROSION & PITTING AROUND PICCOLO TUBE MOUNTING FLANGE. R & R LT WING LE PANEL 530KL, INBD SIDE SKIN PN 601R12063-21 TAG B80867 IAW SRM 51-42-13, 51-42-06 & REO 601R-57-41-001 REV C.

Part: FITTING — CRACKED (FUSELAGE) · airframe 24,970 hrs · 22,487 cycles

ANGLE CLIP IS CRACKED JUST OTBD LBL 9 & AFT OF THE 280 BEAM, BELOW FLOOR. R & R CLIP IAW SRM 51-42-21.

Part: FITTING — CRACKED (FUSELAGE) · airframe 24,970 hrs · 22,487 cycles

ANGLE CLIP IS CRACKED JUST OTBD OF RBL 9 & AFT OF THE 280 BEAM, BELOW FLOOR. R & R CLIP IAW SRM 51-42-21.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 24,970 hrs · 22,487 cycles

RIGHT AISLE SEAT TRACK STICK 1 HAS CORROSION, IN CABIN. R & R RT AISLE SEAT TRACK STICK NR 1 IAW AMM 53-01-11-420-001 & REO 601R-53-00-485.

Part: FITTING — CRACKED (FUSELAGE) · airframe 24,970 hrs · 22,487 cycles

STRINGER 3L ANGLE CLIPS ARE BOTH CRACKED, JUST AFT OF FRAME 280, IN CABIN. R & R 3L ANGLE CLIPS WITH NEW CLIPS IAW SRM 51-42-06.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 24,970 hrs · 22,487 cycles

LEFT AISLE SEAT TRACK STICK 1 HAS CORROSION, IN CABIN. R & R FLOOR SEAT TRACK LT NR 1 IAW AMM 53-01-11-420-001 & REO 601R-53-00-485.

Part: HINGE — CRACKED (FUSELAGE) · airframe 24,970 hrs · 22,487 cycles

CARGO STEP PLATE ASSEMBLY HAS ALL 3 HINGES THAT ARE CRACKED. R & R HINGE IAW SRM 51-42-06.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 24,970 hrs · 22,487 cycles

LEFT SIDE SEAT RAIL NR 4 FROM 409.0+112 - 449.85 HAS CORROSION. R & R SEAT RAIL IAW AMM 53-01-11 & REO 601R-53-00-485.

Part: FITTING — CRACKED (FUSELAGE) · airframe 24,970 hrs · 22,487 cycles

ANGLE CLIP IS CRACKED JUST INBD OF LBL 9 & AFT OF THE 280 BEAM, BELOW FLOOR. R & R ANGLE CLIP WITH REPAIR CLIP IAW SRM 51-42-21 & 51-24-16.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 24,970 hrs · 22,487 cycles

FS 621 APB RT UPPER OBLIQUE ANGLE CRACKED. R & R RT OBLIQUE ANGLE WITH NEW ANGLE IAW SRM 51-42-21.

Part: STRAP — CORRODED (FUSELAGE) · airframe 24,970 hrs · 22,487 cycles

FS 589.0 FLOOR STRAP LBL 9 - 27 HAS CORROSION. R & R FLOOR STRIP WITH NEW STRIP IAW SRM 51-42-06.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 24,970 hrs · 22,487 cycles

RIGHT SIDE SEAT RAIL NR 3 FROM 409.0+16 - 409.0+112 HAS CORROSION. R & R SEAT RAIL IAW AMM 53-01-11.

Part: FITTING — CRACKED (FUSELAGE) · airframe 24,970 hrs · 22,487 cycles

ANGLE CLIP IS CRACKED JUST INBD OF RBL 9 & AFT OF THE 280 BEAM, BELOW FLOOR. R & R CRACKED ANGLE CLIP WITH FABRICATED REPAIR CLIP IAW SRM 51-24-21, SRM 51-42-21 & REO 601R53-11-926 REV B.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 24,970 hrs · 22,487 cycles

CARGO TIE DOWN TRACK LBL 9, FS 559.00+88 HAS CORROSION. REMOVED CARGO TIE DOWN IAW AMM 53-00-49. TIE DOWN WAS FOUND TO BE OUT OF LIMITS IAW 53-21-49. FABRICATED NEW CARGO TIE DOWN IAW REO 601R-53-00-485 & INSTALLED IAW REO 601R-53-00-485.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 24,970 hrs · 22,487 cycles

CARGO TIE DOWN TRACK RBL 9, FS 559.00+112 HAS CORROSION. REMOVED CARGO TIE DOWN IAW AMM 53-01-05. TIE DOWN FOUND TO BE OUT OF LIMITS IAW SRM 53-61-49. FABRICATED NEW CARGO TIE DOWN IAW REV 601R-53-00-485 & REINSTALLED IAW SMM 53-00-49.

Part: CONTROL CABLE — BROKEN (THROTTLE) · airframe 24,507 hrs · 22,029 cycles

LEFT ENGINE WOULD NOT GO TO IDLE IN FLIGHT WHEN COMMANDED TO BY LT THRUST LEVER. LEVER MOVED FREELY BUT LT ENGINE REMAINED AT CRUISE POWER. ADVANCING LT THRUST LEVER WOULD INCREASE THRUST BUT RETARDING IT WOULD NOT REDUCE IT. ACCOMPLISHED "THRUST LEVER STUCK/UNRESPONSIVE" PROCEDURES IN QRH AND SHUT ENGINE DOWN IN FLIGHT. FOUND PYLON ENGINE THROTTLE CONTROL CABLE BROKEN. R & R CABLE. IAW 76-11-09 ALL CHECKS GOOD, ACFT OK FOR SERVICE.

Part: CONTAINER — TORN (LIFE VEST) · airframe 23,843 hrs · 21,370 cycles

CAPTAIN LIFE VEST BAG TORN. R & R CAPTAIN LIFE VEST IAW AMM 25-61-03.

Part: FLASHLIGHT — DEFECTIVE (COCKPIT) · airframe 23,628 hrs · 21,154 cycles

CAPTAIN FLASHLIGHT, RED INDICATOR DOES NOT FLASH. R & R CAPTAIN FLASHLIGHT IAW AMM 25-61-04.

Part: BATTERY PACK — DISCHARGED (FLASHLIGHT) · airframe 23,510 hrs · 21,035 cycles

FLIGHT ATTENDANT FLASHLIGHT BLINKING LIGHT NOT BLINKING. REMOVED AND REPLACED BATTERY PACK. ALL CHECKS GOOD AT THIS TIME IAW AMM 25-60-00.

Part: LIFE VEST — UNSERVICEABLE (CABIN) · airframe 22,487 hrs · 20,060 cycles

FLIGHT ATTENDANT LIFE VEST HAS HOLES IN THE PACKAGING. REMOVED AND REPLACED FLIGHT ATTENDANT LIFE VEST IAW AMM 25-61-03.

Part: PIN — SEIZED (NLG) · airframe 22,474 hrs · 19,675 cycles

ON APPROACH ON FLIGHT 4038 RECEIVED GEAR DISAGREE WARNING MESSAGE. NOSE GEAR SHOWED UNSAFE. NOSE GEAR DID NOT COME DOWN. CREW PERFORMED A GO-AROUND. THEY FOLLOWED QRH FOR GEAR DISAGREE AND NOSE GEAR CAME DOWN. AIRCRAFT LANDED SAFELY AT GSP. FOUND NLG UPLOCK PIN SEIZED. ADJUSTED NLG UPLOCK PIN TO AMM LIMITS AND CHECKED NLG UPLOCK CLEARANCE CHECK IAW AMM 32-33-05. OPC EXTENSION AND RETRACTION SYSTEM IAW AMM 32-30-00. OP GOOD. COMPLIED WITH PA 05-018H SCENAIO 1 ,APPROVED. THIS CLEARS DM#73702. PLACARD REMOVED.

Part: FINGER DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,308 hrs · 19,870 cycles

RIGHT FLOOR LANDING AT BULKHEAD FROM FS 424 TO FS 559 FINGER DOUBLERS CORRODED. REPAIRED IAW BOMBARDIER REO 601R-53-41-666.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 22,308 hrs · 19,872 cycles

FS 202.75 PRESSURE BULKHEAD AT BL 23.75 HAS A CRACK AROUND THE BRAKE CABLE THRU HOLE. REPAIRED IAW BOMBARDIER REO 601R-53-11-563.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,308 hrs · 19,872 cycles

UPON REMOVAL OF RIGHT SEATS AT EMERGENCY EXIT FOUND SEAT TRACK AT EMERGENCY EXIT CORRODED. REMOVED AND REPLACED NR 5 EMERGENCY EXIT SEAT TRACK. REPAIRED IAW AMM 53-01-11.

Part: FITTING — CRACKED (FUSELAGE) · airframe 22,308 hrs · 19,872 cycles

CRACK AT FS 621 BULKHEAD LINTEL FITTING. REPAIRED IAW BOMBARDIER REO 601R-53-61-1230.

Part: CONTAINER — TORN (LIFE VEST) · airframe 22,199 hrs · 19,766 cycles

CAPTAIN'S AND FIRST OFFICER’S LIFE VEST BAG TORN. REMOVED AND REPLACED CAPTAIN'S AND FIRST OFFICER’S LIFE VEST IAW AMM 25-61-03.

Part: PROXIMITY SWITCH — OUT OF ADJUST (LT MLG) · airframe 21,411 hrs · 18,998 cycles

LT MAIN GEAR DISAGREE ON RETRACTION. FOUND PROX SEVERAL SWITCHES OUT OF ADJUSTMENT. ADJUSTED SWITCHES AND OPS CHECK GOOD.

Part: TRIM SWITCH — DIRTY (RUDDER) · airframe 21,372 hrs · 18,955 cycles

RUDDER TRIM STICKS. CLEANED RUDDER TRIM SWITCH CHECKS GOOD IAW AMM 27-20-00.

Part: HANDLE — DEFECTIVE (COCKPIT) · airframe 21,332 hrs · 18,916 cycles

FLAPS FAIL AT 45 DEGREES. FLAPS WILL NOT RESET. MAINTENANCE REPORTS FLAP HANDLE IS BAD.

Part: LIGHT — NOT SEATED (CABIN) · airframe 20,581 hrs · 18,181 cycles

EMERGENCY EXITS FLOOR TRACK ROW 8 INOP. RESEATED/RECONNECTED FLOOD EMERGENCY LIGHTS IAW AMM 33-50-10, NO FAULTS NOTED. OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,557 hrs · 18,157 cycles

EM LIGHTS ROW INOP RESEATED AND OPS CHECKED ROW 8 EM LIGHTS IAW WITH AMM 33-50-10. OK FOR SERVICE.

Part: CIRCUIT BREAKER — TRIPPED (COCKPIT) · airframe 20,434 hrs · 18,042 cycles

STAB TRIM CHANNEL 1 INOP STATUS MESSSAGE. RESET CB'S FOR STAB TRIM SYSTEM PER FIM 27-40-00. OPS CHECK GOOD.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 19,009 hrs · 16,712 cycles

CRACKED FS 559.00 BULKHEAD WEB FOUND CRACKED AND REQUIRES REPAIR. REPAIRED FS 559.00 BULKHEAD WEB IAW BOMBARDIER REO 601R-53-41-260 REV E AND BOMBARDIER REO 601R-53-41-609 REV B, DEVIATION "C" AND BSC EO'S 601R-53-20441A AND 601R-53-20447.

Part: SKIN — DENTED (TE FLAP) · airframe 18,415 hrs · 16,166 cycles

TWO DENTS WERE FOUND ON THE LEFT WING INBOARD FLAP UPPER SKIN. THE DAMAGES ARE LOCATED INBOARD OF WS = 121.5 AND APPROXIMATELY 4 INCHES FROM THE TRAILING EDGE FASTENER ROW. THE LARGER DENT MEASURES 1.86 INCHES BY 1.37 INCHES WITH A MAXIMUM DEPTH OF 0.020 INCH. A SMALL DENT MEASURING 0.66 INCH BY 0.25 INCH WITH A MAXIMUM DEPTH OF 0.004 INCH IS ADJACENT TO THE LARGER DISCREPANCY. TEMPORARY REPAIR IAW STS ENGINEERING EA 5-2010-216, FLY ON FOR 4500 FH, PERIODIC INSPECTIONS EVERY 600 FH, WITHIN WHICH TIME A PERMANENT REPAIR MUST BE ACCOMPLISHED IAW CRJ-200 SRM 57-52-00, REPAIR NR 2 - FLUSH REPAIR TO INBOARD FLAP SKIN OR REPAIR NR 3 - NON-FLUSH REPAIR TO INBOARD FLAP SKIN.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 17,488 hrs · 15,285 cycles

LEFT WING LOWER PLANK CORROSION AT FUEL PANEL 540FB AT WS 136.676 NR 8 HOLE ON EDGE OF CUTOUT MEASURED .007 INCH DEEP FORWARD AND .006 INCH DEEP IN AFT CRITICAL REGIONS. REPAIRED IAW BOMBARDIER REO 601R-57-21-030 REV H. REPAIR DEPTH IS .008 INCH FORWARD AND .007 INCH DEEP IN AFT CRITICAL REGION.

Part: SKIN — CORRODED (LT WIING) · corrosion level 2 · airframe 17,488 hrs · 15,285 cycles

LEFT WING LOWER PLANK AT WS 253.022 HOLE NR 13 EDGE OF ACCESS DOOR CUTOUT CORROSION FOUND .003 INCH DEEP. REPAIRED IAW BOMBARDIER REO 601R-57-21-030 REV H. REPAIR DEPTH IS .003 INCH.

Part: FLAP SYSTEM — UNKNOWN

FLAPS FAIL AT ZERO DEGREES WHEN SELECTED TO 20 DEGREES. RESET PER AD 2006-12-21, SET TO MONITORING FOR 72 HOURS.

Part: DRIVE SHAFT — DIRTY (T/E FLAP) · airframe 8,058 hrs · 7,151 cycles

FLAPS FAILED AT ZERO ON TAXI. RETURNED TO BLOCKS. REMOVED, CLEANED AND RELUBED RT FLAP SYSTEM FLEXIBLE DRIVE SHAFTS.

Part: FLAP — MALFUNCTIONED (WING) · airframe 8,058 hrs · 7,151 cycles

FLAPS FAILED AT ZERO ON DESCENT. FOLLOWED QRH, DECLARED EMERGENCY WITH UNEVENTFUL LANDING. SYSTEM RESET AND PLACED ON 72 HOUR WATCH PER AD 98-20-01.