N836AS

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 33,490 hrs · 29,255 cycles

EMERGENCY EXIT LIGHT BY MAIN CABIN DOOR, COVER IS BROKEN. INSTALLED COVER IAW AMM 33-50-00. OK FOR SERVICE.

Part: ROD — DAMAGED (SERVICE DOOR) · airframe 32,982 hrs · 28,780 cycles

SERVICE DOOR IS DIFFICULT TO OPEN ESPECIALLY FROM OUTSIDE THE ACFT. FOUND SERVICE DOOR INTERNAL STABILIZER ROD DAMAGED. REPLACED & RIGGED STABILIZER ROD IAW MM 52-41-00. SDR CLOSED.

Part: LATCH — LACK OF LUBE (SERVICE DOOR) · airframe 32,868 hrs · 28,672 cycles

UNABLE TO OPEN GALLEY SERVICE DOOR FROM OUTSIDE - OPENS FINE FROM THE INSIDE. CLEANED SILL AND LUBED LATCHES AND HANDLE. CHECKED OPS IAW AMM 52-41-00. OPS CK OK. SDR CLOSED.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 32,769 hrs · 28,586 cycles

LEFT EMERGENCY EXIT FLOOR LEVEL EXIT SIGN INOPERATIVE. R & R NR 2 INVERTER IAW AMM 33-51-07. OP CHECKED GOOD.

Part: A/C PACK — ODOR (LEFT) · airframe 32,545 hrs · 28,386 cycles

IN CRUISE FLT, AT 260, LEFT PACK HIGH TEMP MESSAGE. SMELLED OVERHEAT ODOR FROM LT PACK. PERFORMED OPS CHECK ON LT PACK IAW AMM 21-51-00. OPS CHECKED GOOD. NO FURTHER DEFECTS AT THIS TIME.

Part: INVERTER — UNSERVICEABLE (EMERGENCY LIGHT) · airframe 32,335 hrs · 28,189 cycles

RT EMERGENCY EXIT LOWER EMERGENCY LIGHT INOPERATIVE. R & R NR 3 EMERGENCY LIGHT INVERTER ASSY IAW AMM-33-51-07,OPS CHECKED GOOD ACFT OK FOR SERVICE.

Part: LANDING GEAR — MALFUNCTIONED (NOSE) · airframe 31,248 hrs · 27,196 cycles

GEAR DISAGREE MASTER WARNING, NLG WOULD NOT RETRACT. ACFT RETURNED AFTER T/O AND EMERGENCY DECLARED. PERFORMED LANDING GEAR EXTENSION AND RETRACTION FUNCTIONAL TEST IAW AMM 32-30-00. OP'S CHECKED GOOD.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 31,232 hrs · 27,184 cycles

FLASHLIGHT DIM. INSTALLED NEW BATTERIES IAW AMM 25-60-00.

Part: PROXIMITY SWITCH — OUT OF RIG (MLG) · airframe 31,216 hrs · 27,169 cycles

ACFT RETURNED AFTER TAKE OFF DUE TO A GEAR DISAGREE WARNING MESSAGE FOR NOSE GEAR. DECLARED AN EMERGENCY, FOLLOWED QRH AND LANDED UNEVENTFUL. RIGGED NLG UPLOCK PROXIMITY SWITCH PS3GA IAW AMM 32-33-05. COMPLIED WITH SEVERAL GEAR SWINGS. OPS CHECKED GOOD.

Part: PROXIMITY SENSOR — OUT OF ADJUST (NLG) · airframe 31,144 hrs · 27,095 cycles

AFTER T/O GEAR DISAGREE MASTER WARNING , QRH C/W EMERGENCY DECLARE DEVERSIONARY LAND, SYS WAS ABLE TO DOWN LOCK BUT NOT UP LOCK , SYS DID TURN GREEN FOR DOWNLOCK. ACFT DIVERTED, EMERGENCY DECLARED. ADJUSTED NLG OLEO CENTERED/EXTENDED PROXIMITY SENSOR BACK INTO LIMITS IAW AMM 32-61-05 AND PERFORMED FUNCTIONAL TEST OF MLG EXTEN/ RETRAC SYS IAW AMM 32-30-00. OPS CHECKED GOOD.

Part: LANDING GEAR — MALFUNCTIONED (NOSE) · airframe 31,137 hrs · 27,088 cycles

GEAR DISAGREE WARNING MSG IN FLIGHT. NOSEWHEEL WOULD NOT RETRACT FOLLOWED QRH CHECKLIST. EMERGENCY RELEASE HANDLE PULLED. PERFORMED OPS TEST, SWUNG GEAR 10 TIMES, NO DEFECTS NOTED IAW AMM 32-30-00-720-801.

Part: UPLOCK — FAILED (NLG) · airframe 31,109 hrs · 27,059 cycles

UPON GEAR RETRACTION, RECEIVED A NOSE WHEEL DISAGREE & WOULD NOT RETRACT. ACFT RETURNED TO DEPARTURE & EMERGENCY DECLARED. R & R NLG UPLOCK ASSY IAW AMM 32-33-05 AND PERFORMED NLG SWING RETRACTION IAW AMM 32-33-00. OPS CHECKED GOOD. ACFT RETURNED TO SERVICE.

Part: MECHANISM — LACK OF LUBE (SERVICE DOOR) · airframe 31,059 hrs · 27,008 cycles

SERVICE DOOR DIFFICULT TO OPEN AND CLOSE. LUBED SERVICE DOOR ROD AND BEARINGS IAW AMM 12-20-52. OPS CHECKED GOOD.

Part: CONTROLLER — FAILED (ANTI ICE TEMP) · airframe 30,927 hrs · 26,884 cycles

WING OVERHEAT MESSAGE C/W QRH EMERGENCY PROCEDURES. MESAGE REMAINED ON. R & R WING ANTI ICE TEMP CONTROLER IAW AMM 30-12-19. RESEALED LT WING STAND BY THERMAL SWITCHES IAW AMM 30-12-16.

Part: MOTOR — FAILED (PAX DOOR) · airframe 30,476 hrs · 26,494 cycles

PAX DOOR WILL NOT OPEN. REMOVED AND REPLACED PAX DOOR MOTOR ASSY IAW AMM 52-11-08. OPS CHECKED GOOD NO FURTHER DEFECTS FOUND.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 30,099 hrs · 26,184 cycles

F/A FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED F/A FLASHLIGHT IAW AMM 25-61-00.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 30,072 hrs · 26,157 cycles

EXTERIOR EMERGENCY LIGHT (7) SEVEN, LOCATED BELOW THE PASSENGER WINDOW AT FS 491.50L IS INOP. R & R THE BULB AT THE EXTERIOR EMERGENCY LIGHT (NR 7) IAW MM 33-51-21-000-801/400-801. PERFORMED THE OPS TEST OF THE EMERGENCY LIGHTS IAW MM 33-51-00-710-801. NO DEFECTS NOTED AT THIS TIME.

Part: FRAME SPLICE — CRACKED (BS 718 S20R) · airframe 30,068 hrs · 26,151 cycles

FRAME SPLICE AT FS 718, STR 20R IS CRACKED. LOCATED AND INSTALLED SERVICEABLE FRAME SPLICE AT FS 718, STR 20R IAW SRM 51-42-06. THIS REPAIR REQUIRES MAJOR/MINOR CLASSIFICATION IAW ASA SOP 5702. THIS REPAIR IS CLASSIFIED AS A MINOR REPAIR IAW ASA SOP 5702.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 30,068 hrs · 26,151 cycles

FOUND REAR PRESSURE BULKHEAD WEB HAS INDICATION NOTED AT WL 130, LBL 27.50, APPROX .3" IN LENGTH 1005 FSH, FAILED NDT INSPECTION. REPAIRED IAW REO 601R-53-61-1541.

Part: SEAT TRACK — CORRODED (BS 364-409) · airframe 30,068 hrs · 26,151 cycles

RIGHT FLOOR SEAT RAILS FORM FS 364.00 TO FS 409.00+128, RBL 9.0 ARE CORRODED. REPAIRED IAW REO 601R-53-00-412.

Part: POST — CRACKED (BS 409) · airframe 30,068 hrs · 26,151 cycles

VERTICAL POST AT FS 409+128, WL 69.00, RBL 18.00 HAS 2 INDICATIONS: (1) ON THE OTBD POST, (1) ON THE INBD POST. BOTH IN THE AFT RADIUS. FAILED NDT INSPECTION. REMOVED VERT POST IAW SRM 51-42-06. LOCATED, DRILLED AND ASSEMBLED VERT POST IAW SRM 51-42-06 AND 51-42-22. INSTALLED IAW SRM 51-42-22.

Part: FLOOR SUPPORT — CORRODED (BS 280) · airframe 30,068 hrs · 26,151 cycles

FS 280, FWD ANGLE BETWEEN LBL 9 AND RBL 9 IS CORRODED. REFER CO 7263111, REO 601R-53-11-926 W/O 198723 STEP 77 FOR INSTALLATION OF FS 280 FWD FLOOR SUPPORT ANGLE.

Part: SKIN — CORRODED (BS 559) · airframe 30,068 hrs · 26,151 cycles

FUSELAGE SKIN AT FS 559+93 STRG 23R HAS A SMALL AREA OF CORROSION AROUND A RIVET. REMOVED CORROSION IAW SRM 51-21-06. BLEND IS WITHIN ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-31. TREAT, PRIME AND PAINT BLEND AREA.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 30,068 hrs · 26,151 cycles

PILOTS WINDSHIELD POST LOWER ATTACHMENT ANGLE CRACKED. INSTALLED NEW ANGLE IAW SRM 51-42-21.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 30,068 hrs · 26,151 cycles

FS 280.00 OTBD OF LBL 9.0 CLIP IS CRACKED. REPAIRED IAW REO 601R-53-11-926 W/O 198723 STEP 82.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 30,068 hrs · 26,151 cycles

FS 280 FLOORBEAM AFT CAP ANGLE IS CORRODED BETWEEN RBL 9 AND LBL 9. REPAIRED FS 280 FLOORBEAM IAW REO 601R-53-11-926, REV B.

Part: SEAT TRACK — CORRODED (BS 621) · airframe 30,068 hrs · 26,151 cycles

LBL 9 AFT SEAT TRACK AT FS 621.00 CORRODED. R & R AT FS 621.00, LBL 9 SEAT RACK PN 601R31632-51 IAW AMM 20-21-00. (CLOSED)

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 30,068 hrs · 26,151 cycles

CO-PILOT WINDSHIELD POST LOWER ATTACHMENT ANGLE CRACKED. R & R WINDSHIELD POST LOWER ATTACHMENT ANGLE WITH NEW PART IAW SRM 51-40-11 AND SRM 51-42-21. REPAIR CLASSIFIED AS MINOR.

Part: PLACARD — WORN (CABIN) · airframe 30,068 hrs · 26,151 cycles

EXIT INDICATORS AT THE OVERWING EXITS ARE WORN, ALL 4 PIECES. TO BE INSTALLED UNDER FLUSH COVER, NOT ON TOP. REMOVED AND INSTALLED SERVICEABLE MARKERS IAW AMM 11-30-00-000-801 & 11-30-00-400-801.

Part: POST — CRACKED (BS 409) · airframe 30,068 hrs · 26,151 cycles

LBL 27 INBD POST CRACKED AT FS 409+128 AT S20L. REPAIRED IAW REO 601R-53-41-056 IAW REO 601R-53-41-056

Part: LIGHT — UNSERVICEABLE (SERVICE DOOR) · airframe 30,068 hrs · 26,151 cycles

SERVICE DOOR BETA LIGHT FAILED FUNCTIONAL TEST. REMOVED AND INSTALLED SERVICEABLE BETA EXIT LIGHT ON SERVICE DOOR IAW AMM 33-51-09-400-802. SERVICE DOOR BETA LIGHT REQ'S A FUNCTIONAL TEST IAW AMM 33-51-09-720-801. PERFORMED FUNC TEST OF SERVICE DOOR HANDLE BETA LIGHT IAW AMM 33-51-04-720-801, NO DEFECTS NOTED.

Part: FRAME — CRACKED (BS 718 S11-12L) · airframe 30,068 hrs · 26,151 cycles

LEFT BS 718 FRAME IS CRACKED AT S11-12L. REPLACED FRAME IAW SRM 51-42-06, 51-42-21.

Part: STRUCTURE — CORRODED (BS 559) · airframe 30,068 hrs · 26,151 cycles

FS 559.00+105 STR 23R HAS A SMALL AREA OF CORROSION AROUND RIVET" IN DIA. REMOVED LIGHT SURFACE CORROSION IAW SRM 51-21-06. WITHIN ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-31.

Part: SEAT TRACK — CORRODED (BS 364-409) · airframe 30,068 hrs · 26,151 cycles

RIGHT FWD FLOOR SEAT TRACK FROM FS 364.00 TO FS 409.00+128 RBL 9.0 ARE CORRODED. R & R RT FWD FLOOR SEAT TRACK IAW AMM 53-01-11-000-802 & 53-01-11-400-802.

Part: STIFFENER — CHAFED (BS 621 BULKHEAD) · airframe 30,068 hrs · 26,151 cycles

621 BULKHEAD VERTICAL STIFFENER AT BL 0 IS CHAFED APPROX 1" L X .5" W X .005 ABOVE ESB. BLENDED AREA ON FS 621 BL 0.02 MEMBER IAW REO 601R-53-61-1523. PERFORMED EDDY CURRENT INSP ON THE NEWLY BLENDED AREA OF THE VERTICAL STIFFENER AT FS 621, BL0.0. NO INDICATIONS FOUND AT THIS TIME IAW ITEM 4 OF REO 601R-53-61-1523 AND NDTM PART 1, 51-20-06. TREATED & RESTORED FINISH TO REPAIRED AREA ON 621 BULKHEAD VERT STIFFENER AT BL 0 IAW REO 610R-53-61-1523, STEP 3. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702.

Part: LANDING GEAR — SMOKE · airframe 29,665 hrs · 25,792 cycles

TOWER REPORTED SMOKE COMING FROM MLG AFTER LANDING, DURING TAXI IN. VISUALLY INSPECTED LT AND RT MLG, TIRES, AND BRAKE ASSY'S FOR DEFECTS AND LEAKS IAW AMM CH 32-10-00. NO DEFECTS FOUND.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 28,510 hrs · 24,815 cycles

OVERHEAD EMERGENCY LIGHTS INOP. R & R NR 4 BATTERY PACK IAW AMM 33-51-04. OPS CK GOOD. R & R NR 4 BATTERY PACK IAW AMM 33-51-04, OPS CK GOOD.

Part: WINDOW — ARCED (COCKPIT) · airframe 27,683 hrs · 24,076 cycles

F/O'S SIDE WINDOW ARCING (ACFT RETURNED AFTER T/O -- EMERGENCY DECLARED AS A PRECAUTION] R & R FO'S SIDE WINDOW IAW AMM 56-12-01. LEAK AND OP'S CHECK GOOD. ACFT OK FOR SERVICE.

Part: FLOOR SUPPORT — CORRODED (CARGO BAY) · airframe 25,730 hrs · 22,152 cycles

FLOOR SUPPORT CORRODED UNDER INBD SIDE OF PANEL 281LLF IN CARGO BAY. REPAIRED IAW EC/TC REO 601R-53-61-3145 IAW REO 601R-53-61-3145 REV B.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 25,730 hrs · 22,152 cycles

FOUND SEAT TRACK CORRODED CARGO AREA BETWEEN PANELS 281ELF AND 281KLF.

Part: ANCHOR FITTING — CRACKED (PAX DOOR) · airframe 25,730 hrs · 22,152 cycles

ASD AFT ANCHOR FITTING CRACKED. COMPLIED WITH ITEM 4 SUBTASK 52-11-17-400-803 CLOSE OUT STEPS C,D,E,F,G AND H. JOB COMPLETE.

Part: CARGO TRACK — CORRODED (BS 574) · airframe 25,730 hrs · 22,152 cycles

ADVANCED CORROSION ON LT AND RT CARGO TIE DOWN TRACKS AT FS 574, RBL 9 AND LBL 9.

Part: FRAME — CORRODED (BS 349 S25L/R) · airframe 25,730 hrs · 22,152 cycles

CORROSION DAMAGE AT FS 349.00 FRAME IN MAIN AVIONICS BAY STGR 25 LT TO STGR 25 RT.

Part: FRAME — CORRODED (BS 364 S25L/R) · airframe 25,730 hrs · 22,152 cycles

CORROSION DAMAGE AT FS 364.00 FRAME IN MAIN AVIONICS BAY STGR 25 LT TO STGR 25 RT.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 25,730 hrs · 22,152 cycles

LEFT SIDE SEAT RAILS OTBD SIDE CORRODED AS MARKED THROUGHOUT CABIN.

Part: SEAT TRACK — CORRODED · airframe 25,729 hrs · 22,152 cycles

LT SIDE SEAT RAIL CORRODED AND GOUGED. CORROSION REMOVED ON SEAT RAIL, FOUND WITHIN LIMITS IAW SRM 53-21-49.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 25,730 hrs · 22,152 cycles

ADVANCED CORROSION ON SEAT TRACK RBL 9 AFT OF SEAT POSITION 11CD, MARKED IN RED.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 25,205 hrs · 21,660 cycles

INTERCOSTAL CRACK AT FS484 LBL 36.

Part: HANDLE — CRACKED (PAX DOOR) · airframe 24,708 hrs · 21,180 cycles

PAX DOOR INNER HANDLE HAS CRACK.

Part: SERVICE DOOR — MALFUNCTIONED · airframe 24,494 hrs · 20,978 cycles

SERVICE DOOR WILL NOT CLOSE FROM INSIDE. DOOR OPS OK PER 52-40-01.

Part: DOOR — INOPERATIVE (SERVICE) · airframe 24,397 hrs · 20,891 cycles

SERVICE DOOR WILL NOT CLOSE. OPS CHECKED SERVICE DOOR PER 52-40-01. CHECKS GOOD. (S)

Part: PDU — MALFUNCTIONED (TE FLAPS) · airframe 24,153 hrs · 20,652 cycles

FLAPS FAIL AT 25 WHEN SELECTING FLAPS TO 30 FROM 20. EMERGENCY VEHICLES WERE ON STANDBY AS A PRECAUTION (SKEW DETECTION SYSTEM). REMOVED AND REPLACED FLAP POWER DRIVE UNIT IAW AMM 27-52-01. FLAPS OPERATE NORMALLY AT ALL SELECTED POSITIONS.

Part: DOOR — STUCK (SERVICE) · airframe 24,066 hrs · 20,578 cycles

SERVICE DOOR WON’T CLOSE. SERVICE DOOR OPS CHECK GOOD IAW CRJ 200 AMM 52-40-01. ACFT OK FOR SERVICE. (S)

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 2,378,821 hrs · 20,331 cycles

LT MIDDLE EXTERIOR EMERGENCY LIGHT INOP RELAMPED LT MIDDLE EXTERIOR EMERGENCY LIGHT PER CRJ 200 AMM 33-51-21. (B)

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 23,513 hrs · 20,092 cycles

LEFT AFT MOST EXTERNAL EMERGENCY LIGHT INOP.

Part: LIGHT — BROKEN (CABIN) · airframe 23,204 hrs · 19,830 cycles

FLOOR LEVEL LIGHT BY PAX DOOR BROKEN.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 21,699 hrs · 18,605 cycles

PAX DOOR EXTERIOR EMERGENCY LIGHT WILL NOT ILLUMINATE.

Part: ATTACH ANGLE — CRACKED (RT WING) · airframe 21,679 hrs · 18,587 cycles

RIGHT WING MIDDLE LEADING EDGE I/B ATTACH ANGLE CRACKED.

Part: BRACKET — CRACKED (LT WING) · airframe 21,679 hrs · 18,587 cycles

LEFT WING I/B LEADING EDGE O/B BRACKET CRACKED.

Part: FITTING — CRACKED (FUSELAGE) · airframe 21,679 hrs · 18,587 cycles

CRACK FOUND ON CLIP AT FS 484 LBL 9.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 21,679 hrs · 18,587 cycles

RIGHT 640 SKIN BONDED BUTT STRAP DOUBLER IS CRACKED. [07-23-07] COMPLIED WITH EC/TC REO 601R-53-61-506.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 21,679 hrs · 18,587 cycles

SEAT TRACK ON FLOOR UNDER OVERHEAD BIN 11CD SHOWS SIGNS OF CORROSION. [07-23-07] REPAIRED IAW; 53-21-49, 51-12-00, AND 51-21-06.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 21,679 hrs · 18,587 cycles

SEAT TRACK ON FLOOR UNDER OVERHEAD BIN 1 AB SHOWS SIGNS OF CORROSION TO FWD SECTION OF TRACK. [SUP 05-24-07] REMOVED AND REPLACED SEAT TRACK P/N 601R-31032-15 IAW CRJ 200 AMM 53-01-11.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 21,679 hrs · 18,587 cycles

LEFT 640 SKIN BONDED BUTT STRAP DOUBLERS CRACKED. [07-23-07] COMPLIED WITH EC/TC REO 601R-53-61-506.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 21,679 hrs · 18,587 cycles

CRACK FOUND AT FS 484 AT RBL 27 OUTBOARD ON INTERCOSTAL. REMOVED CRACKED ANGLE AT FS 484 AT RBL 27 O/B INTERCOSTAL IAW REO 601R-53-41-059. INSTALLED NEWLY MANUFACTURED CLIP. (.063, 2024-T3, PO 9345-1) IAW REO 601R-53-41-059. SUPPLEMENTAL - SDR CLOSED 05/22/07.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 21,679 hrs · 18,587 cycles

INTERCOSTAL CRACKED AT FS 484, LBL 27 OUTBOARD.

Part: PLACARD — WORN (COCKPIT) · airframe 21,679 hrs · 18,587 cycles

CREW ESCAPE HATCH 3 EXTERIOR PLACARDS WORN. THE RED ARROW FOR DIRECTIONS, OPEN & EMERGENCY EXIT, PUSH TO RELEASE AND TURN TO OPEN PLACARDS. [07-23-07] REMOVED AND REPLACED THREE (3) LISTED EXTERIOR PLACARDS ON CREW ESCAPE HATCH IAW CRJ 200 AMM 11-20-00.

Part: DOOR — NO TEST (EMERGENCY EXIT) · airframe 21,679 hrs · 18,587 cycles

RIGHT OVERWING EMERGENCY EXIT DOOR FAILED FUNCTIONAL TEST. REFER TO TASK 000-52-830-104. REPAIRED IAW; AMM 12-20-52, AND AMM 52-21-00.

Part: DOOR — NO TEST (EMERGENCY EXIT) · airframe 21,679 hrs · 18,587 cycles

LEFT OVERWING EMERGENCY EXIT DOOR FAILED FUNCTIONAL TEST. REFER TO TASK 000-52-830-104. [07-23-07] REPAIRED IAW; AMM 12-20-52, AND AMM 52-21-00.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,421 hrs · 18,385 cycles

AFT FOUR FLOOR LEVEL EMERGENCY LIGHTS INOP.

Part: CARGO TRACK — CRACKED (FUSELAGE) · airframe 20,484 hrs · 17,696 cycles

CARGO TRACK SUPPORT BEAM AFT LOWER ANGLE CRACKED.

Part: STEERING SYS — INOPERATIVE (NLG) · airframe 20,378 hrs · 17,603 cycles

STEERING INOP CAUTION MSG JUST AFTER TAKEOFF, EMERGENCY TRUCKS ROLLED AS A PRECAUTION.

Part: HUMIDIFIER — ODOR (CABIN) · airframe 19,158 hrs · 16,636 cycles

BURNING SMELL FROM AIR VENTS DURING CLIMB AND APPROACH. THE SMELL IS CHEMICAL AND TOXIC, FLT 4228 DEL 47 MINS.

Part: CONNECTOR — LOOSE (CABIN)

DURING A GROUND INSPECTION, THE EMERGENCY FLOOR LIGHTS, FROM ROW 1-4, WERE FOUND TO BE INOPERATIVE. MAINTENANCE FOUND AND SECURED A LOOSE CONNECTOR ON THE EMERGENCY FLOOR LIGHTS, FROM ROW 1-4. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: CONNECTOR — LOOSE (CABIN)

DURING A GROUND INSPECTION, THE EMERGENCY FLOOR LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE FOUND AND RESECURED A LOOSE CONNECTOR ON THE EMERGENCY FLOOR LIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: LAMP — BURNED OUT (FUSELAGE)

DURING A GROUND INSPECTION, THE LT AFT EXTERIOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE LT AFT EXTERIOR EMERGENCY LIGHT ASSEMBLY. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: ODOR — DETECTED (CABIN)

DURING CLIMB OUT FROM DEPARTURE, WHEN TRANSFERRING TO BLEEDS, AN OIL ODOR WAS NOTICED FOR APPROXIMATELY FIVE MINUTES. THE AIRCRAFT LANDED SAFELY. MAINTENANCE PERFORMED OPERATIONAL CHECKS WITH NO DEFECTS NOTED. AIRCRAFT OK FOR SERVICE. (K)

Part: WARNING LIGHT — FALSE INDICATION (PAX DOOR)

DURING CLIMB-OUT FROM OMA-ATL, AT APPROXIMATELY 8,000 FEET, THE CREW RECEIVED A PASSENGER DOOR LATCH CAUTION MESSAGE. THE CREW COMPLIED WITH THE QRH, WHEN AT APPROXIMATELY 18,500 FEET, A PASSENGER DOOR WARNING MESSAGE WAS RECEIVED. THE CREW DECLARED AN EMERGENCY AND DIVERTED TO MCI, WHERE IT LANDED SAFELY. MAINTENANCE PRESSURIZED THE AIRCRAFT TO 5 DELTA P WITH NO DEFECTS NOTED. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT)

DURING A C-CHECK IN MCN, THE NR 2 POWER SUPPLY WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 2 POWER SUPPLY. OPERATIONAL CHECKS GOOD. (M)

Part: LENS — CRACKED (EMERGENCY LIGHT)

DURING A C-CHECK IN MCN, THE EXIT LIGHT LENS, ABOVE THE SERVICE DOOR, WAS FOUND TO BE CRACKED. MAINTENANCE WILL REMOVE AND REPLACE THE EXIT LIGHT LENS, ABOVE THE SERVICE DOOR. (M)

Part: SEAT TRACK — CORRODED (BS 559)

DURING A C-CHECK IN MCN, THE CARGO COMPARTMENT FORWARD BULKHEAD SEAT TRACK AT FS 559 PLUS 112, RBL 9 AND RBL 27 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CARGO COMPARTMENT FORWARD BULKHEAD SEAT TRACK AT FS 559 PLUS 112, RBL 9 AND RBL 27 IAW CRJ200 AMM 53-00-11. (M)

Part: HANDLE — CORRODED (ESCAPE HATCH)

DURING A C-CHECK IN MCN, THE CREW ESCAPE HATCH HANDLE WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CREW ESCAPE HATCH HANDLE IAW CRJ200 MM 52-22-03. (M)

Part: FLOOR PANEL — CORRODED (BS 473)

DURING A C-CHECK IN MCN, THE PRESSURE FLOOR SKIN AT FS 473.15, LBL 36 WAS FOUND TO BE CORRODED BEYOND LIMITS. (M)

Part: FLOORBEAM — CORRODED (BS 280)

DURING A C-CHECK IN MCN, THE FS 280 FLOOR SUPPORT BEAM ANGLE, BETWEEN LBL 9 AND RBL 9, WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE WILL REPAIR THE FS 280 FLOOR SUPPORT BEAM ANGLE, BETWEEN LBL 9 AND RBL 9, IAW BOMBARDIER REO 601R-53-11-926. (M)

Part: BULKHEAD — CRACKED (BS 202)

DURING A C-CHECK IN MCN, THE FORWARD PRESSURE BULKHEAD, FS 202.75, AT BL 23.71, WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE WILL REPAIR THE FORWARD PRESSURE BULKHEAD FS 202.75, AT BL 23.71, IAW ASA EO 600-53-0217. (M)

Part: FLOORBEAM — CRACKED (BS 280)

DURING A C-CHECK IN MCN, THE FS 280 AND LBL 9 FLOOR SUPPORT BEAM, ON THE INBOARD RIVET OF FLOOR SUPPORT LEG, WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE WILL REPAIR THE FS 280 AND LBL 9 FLOOR SUPPORT BEAM, ON THE INBOARD RIVET OF THE FLOOR SUPPORT LEG, IAW BOMBARDIER REO 601R-53-11-926. (M)

Part: FRAME — CRACKED (FS 718)

DURING A C-CHECK IN MCN, THE LEFT AND RIGHT FS 718 FRAME, AT STRINGER 10-12, WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE WILL REPAIR THE LEFT AND RIGHT FS 718 FRAME, AT STRINGER 10-12, IAW ASA EO 600-53-0067A. (M)

Part: LIGHT — CRACKED (CABIN)

DURING A C-CHECK IN MCN, THE EMERGENCY EXIT LIGHT, NEAR THE SERVICE DOOR, WAS FOUND TO HAVE A CRACKED LENS COVER. MAINTENANCE WILL REMOVE AND REPLACE THE EMERGENCY EXIT LIGHT ASSEMBLY. (M)

Part: LINKAGE — OUT OF ADJUST (PAX DOOR HANDLE)

FLT 4307 - DURING A GROUND INSPECTION IN ATL, THE FLIGHT ATTENDANT NEEDED ASSISTANCE TO LOCK PASSENGER DOOR. MAINTENANCE ADJUSTED THE PASSENGER DOOR HANDLE LINKAGE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

DURING A GROUND INSPECTION IN SHV, EMERGENCY FLOODLIGHT AND THE EMERGENCY EXIT LIGHT, NEAR THE SERVICE DOOR, WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMPS IN THE EMERGENCY FLOOD LIGHT AND THE EMERGENCY EXIT LIGHT NEAR THE SERVICE DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: CABLE — BINDING (FUSELAGE)

DURING A GROUND INSPECTION, THE PASSENGER DOOR WOULD NOT OPEN OR LOCK AND TH DOOR ASSIST MOTOR WOULD NOT OPERATE THE DOOR ALL THE WAY. MAINTENANCE FOUND THE DOOR ASSIST CABLE WRAPPED AROUND THE DOOR HINGE AND REMOVED IT FROM AROUND THE HINGE. OPERATIONAL HECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: COALESCER BAG — ODOR (RT A/C PACK)

FLT 4518 - DURING CLIMB-OUT FROM SHV-ATL, THE CREW NOTICED AN OILY ODOR POSSIBLY FROM THE AIR CONDITIONING PACKS. THE FLIGHT CONTINUED AND THE AIRCRAFT LANDED SAFELY IN ATL. MAINTENANCE REMOVED AND REPLACED THE LEFT AND RIGHT COALESCER BAGS. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: FIRE LOOP — DEFECTIVE (RT ENGINE)

DURING CRUISE, CREW RECEIVED RT ENGINE FIRE FAIL CAUTION MESSAGE WARNING. WHEN COMPLYING WITH THE QRH, FIRE LOOP-A WAS SELECTED AND FIRE WARNING RECEIVED. QRH COMPLIED WITH AND LOOP-B SELECTED. ACFT LANDED SAFELY. MX CLEARED DEFERRED FIRE LOOP BY REMOVING AND REPLACING RT ENGINE FIRE LOOP-A. OPS CHECKS GOOD. ACFT OK FOR SERVICE. (M)

Part: STEP — BROKEN (PAX DOOR)

DURING A GROUND INSPECTON, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPS CHECK GOOD. AC OK FOR SERVICE. (K)

Part: LIGHT — INOPERATIVE (CABIN)

DURING HANGAR MAINTENANCE IN MCN, THE EMERGENCY FLOODLIGHT AT THE PASSENGER DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY FLOODLIGHT ASSEMBLY AT THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. (M)

Part: ANCHOR FITTING — CRACKED (PAX DOOR)

DURING HANGAR MAINTENANCE IN MCN, THE FORWARD ANCHOR FITTING ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE FORWARD ANCHOR FITTING ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. (M)

Part: STEP — CRACKED (PAX DOOR)

DURING AN A-CHECK IN BTR, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR IAW CRJ200 AMM 52-10-00. (M)

Part: BRACKET — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE AFT INTERCOSTAL BRACKET AT FS 484, RBL 36 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE AFT INTERCOSTAL BRACKET AT FS 484, RBL 26 IAW ASA EO 600-0098. (M)

Part: CLIP — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE CLIPS AT FS 280, LBL 9 AND RBL 9 INBOARD AND OUTBOARD WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE CLIPS AT FS 280, LBL 9 AND RBL 9 INBOARD AND OUTBOARD. (M)

Part: FLOOR SUPPORT — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE CARGO COMPARTMENT ANGLE UNDER THE FLOORBOARD AT THE LEFT SIDE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE CARGO COMPARTMENT ANGLE UNDER THE FLOORBOARD. (M)

Part: SILL — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE CARGO DOOR SILL WAS FOUND CORRODED AND CRACKED ON THE FORWARD EDGE BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE CARGO DOOR SILL. (M)

Part: RIB — CRACKED (LT WING)

DURING A C-CHECK IN MCN, THE LEFT WING BATT RIB ASSEMBLY AT WS 53.60 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LEFT WING BATTERY RIB ASSEMBLY AT WS 53.60 IAW ASA EO 600-57-039A. (M)

Part: BRACKET — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE AFT EQUIPMENT BAY RAM AIR INLET SPIDER DUCT BRACKET WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE AFT EQUIPMENT BAY RAM AIR INLET SPIDER DUCT BRACKET. (M)

Part: FLOOR SUPPORT — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE LEFT AND RIGHT CARGO COMPARTMENT FLOOR SUPPORT ANGLES AT FS 621, LBL 27 AND RBL 27 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LEFT AND RIGHT CARGO COMPARTMENT FLOOR SUPPORT ANGLES AT FS 621, LBL 27 AND RBL 27 IAW ASA EO 600-53-0105. (M)

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

FLT 4324 - DURING A GROUND INSPECTION IN DFW, AN EMERGENCY CEILING LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED AN EMERGENCY CEILING LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: STEP — CRACKED (PAX DOOR)

DURING HANGAR MAINTENANCE IN MCN, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT)

DURING HANGAR MAINTENANCE, THE EMERGENCY FLOOR LIGHTING FROM ROW 6 C/D AFT WAS FOUND TO BE INOPERATIVE. MAINTENANCE RECONNECTED THE EMERGENCY FLOOR LIGHTS AT ROW 6 C/D AFT. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: ANCHOR — CRACKED (PAX DOOR)

DURING HANGAR MAINTENANCE IN MCN, THE AFT ANCHOR ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFT ANCHOR ON THE PASSENGER DOOR. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: ENGINE — MALFUNCTIONED (LEFT)

DURING CLIMB-OUT AT APPROXIMATELY 6,500 FT THE CREW RECEIVED A RED FLAG ON THE LT INTERSTAGE TURBINE TEMPERATURE GAUGE OF APPROXIMATELY 886 DEGREES. THE CREW REDUCED POWER SLIGHTLY ON THE LT ENGINE WITH THE TEMPERATURE RETURNING TO NORMAL, THEN INCREASED POWER SLIGHTLY AND THE RED FLAG RE-OCCURRED INCLUDING A SLIGHT VIBRATION. QRH PROCEDURES WERE COMPLIED WITH AND THE CREW SHUT DOWN THE LEFT ENGINE. AN EMERGENCY WAS DECLARED AND EMERGENCY EQUIPMENT REQUESTED. THE AIRCRAFT RETURNED TO ATL, LANDING SAFELY. MAINTENANCE REMOVED AND REPLACED THE LEFT ENGINE. OPERAITONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: HOSE — LEAKING (ENG DRIVEN PUMP)

DURING FLIGHT, AIRCRAFT LOST ALL HYDRAULIC FLUID IN THE NR 1 SYSTEM. AIRCRAFT DIVERTED AND LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE ENGINE DRIVEN PUMP PRESSURE LINE AND ALSO REMOVED AND REPLACED THE ENGINE DRIVEN HYDRAULIC PUMP ITSELF. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE.

Part: WIRE — DAMAGED (CABIN)

DURING GROUND INSPECTION IN DFW, THE AFT SECTION OF EMERGENCY FLOOR LIGHTING WAS FOUND INOPERATIVE. MAINTENANCE INSPECTED AND DISCOVERED WIRE DS29LY-1 NEEDED REPAIR. MAINTENANCE REPAIRED THE WIRE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DURING GROUND INSPECTION IN ATL, THE EMERGENCY LIGHT STRIP AT ROW 6 WAS FOUND TO BE INOPERATIVE. MAINTENANCE RESECURED THE FLOOR LIGHTING STRIP AT ROW 6. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

DURING C-CHECK INSPECTION IN BNA, THE LEFT NR 2 SEAT TRACK OUTBOARD FLOOR BOARD FLANGE, AT A CLIP NUT FASTENER HOLE JUST FORWARD OF FRAME 17, WAS FOUND CORRODED BEYOND ALLOWABLE LIMITS. MAINTENANCE REPAIRED CORROSION IAW ASA EO72-53-0119. THIS EO REFERENCE FAA FORM 8110-3, REPORT NR 01-286, WHICH INCLUDES REPAIR SPECIFICATIONS. (M)

Part: LIGHT — INTERMITTENT (CABIN)

FLT 4431 - DURING GROUND INSPECTION IN ATL, THE EMERGENCY FLOOR LIGHTS WORKED INTERMITTENTLY BETWEEN ROWS 5 AND 8. MAINTENANCE INSPECTED AND PERFORMED EMERGENCY FLOOR LIGHTING OPERATIONAL CHECKS. ALL LIGHTS WERE OPERATIONAL AT THAT TIME. NO DEFECTS WERE NOTED. AIRCRAFT OK FOR SERVICE. (M)

Part: ENGINE — LACK OF LUBE (RT)

FLT 4757 - EN ROUTE FROM ATL TO DSM, THERE WAS A LOSS OF OIL PRESSURE ON THE RIGHT ENGINE. THE ENGINE ROLLED BACK AND THE PILOT SECURED IT. AIRCRAFT DIVERTED AND LANDED SAFELY IN EVV. ON GROUND, THE CREW REPORTED THE CHIP DETECTOR LIGHT ILLUMINATED. MAINTENANCE DETERMINED THE ENGINE HAD NO OIL AND THE CHIP DETECTOR WAS COVERED. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DURING INSPECTION, FOUND EMERGENCY LIGHTS AFTER ROW 8, INOPERATIVE.MAINTENANCE ADJUSTED LIGHTS. OPERATIONAL CHECKS WERE GOOD. AC RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN)

DURING INSPECTION, CREW FOUND EMERGENCY FLOOR LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED POWER STRIP IN THE SECOND SECTION OF THE FLOOR. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: WINDSHIELD — CRACKED (LT COCKPIT)

ATL/PFN - FLT 4706 - CLIMBING THROUGH 6,000 FEET, LEFT WINDSHIELD SHATTERED. CREW DECLARED AN EMERGENCY AND RETURNED TO ATL WHERE LANDING WAS MADE SAFELY AND WITHOUT FURTHER INCIDENT. (X)