N835AS

Part: BRACKET — BENT (NLG) · airframe 36,500 hrs · 31,962 cycles

NOSE GEAR DISAGREE WARNING MESSAGE FOLLOWED BY NOSE DOOR OPEN WARNING RAN CHECKLIST FOR AND PULLED MANUAL GEAR RELEASE RETURNED FAR NORMAL LANDING . ACFT RETURNED TO DEPARTURE AFTER T/O, EMERGENCY ACTIONS. FOUND NLG CENTERED, EXTENDED PROXIMITY SENSOR BRACKET BENT. R & R NLG CENTERED/EXTENDED PROX SENSOR BRACKET IAW CRJ 200 AMM 32-21-01. PERFORMED ADJUSTMENT OF NLG CENTERED, EXTENDED PROXIMITY SENSOR (PS14GA) IAW AMM 32-61-05. PERFORMED FUNCTIONAL TEST OF THE LANDING GEAR EXTENSION, RETRACTION SYSTEM IAW AMM 32-30-00. OPS CHECK GOOD. NO DEFECTS NOTED.

Part: LIGHT — DAMAGED (CABIN) · airframe 36,412 hrs · 31,880 cycles

PAX DOOR FLOOR LEVEL FLOOD LIGHT ASSY DAMAGED. R & R PAX DOOR FLOOR LEVEL FLOOD LIGHT ASSY IAW AMM 33-51-19. OPS CHECKED GOOD, NO FURTHER DEFECTS NOTED AT THIS TIME.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 35,594 hrs · 31,138 cycles

AFT CABIN EMERGENCY CEILING LIGHT IS INOPERATIVE. R & R BULB IAW AMM 33-51-16. OP'S CHECKED GOOD.

Part: FLOOR SUPPORT — CORRODED (BS 579.5-621) · airframe 34,537 hrs · 30,163 cycles

FLOOR SUPPORT AT CARGO DOOR AREA IS CORRODED. REMOVED FLOOR SUPPORT AT LANDING FROM FS 579.5 TO 621 IAW SRM 51-42-06 AND 51-42-21.

Part: FLOOR SUPPORT — CORRODED (BS 310) · airframe 34,537 hrs · 30,163 cycles

FLOOR SUPPORT AT FS 310 LBL 42 HAS CORROSION. REPAIRED IAW EO CL600-2B19-53-I00192.

Part: FLOOR SUPPORT — CORRODED (BS 559) · airframe 34,537 hrs · 30,163 cycles

FS 559+132 - 559+48 LT FLOOR SUPPORT HAS CORROSION AROUND NUTPLATE HOLES. REPAIRED IAW REO CL600-2B19-53-I00194.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 34,537 hrs · 30,163 cycles

FS 280, LBL 9 INBD AND OTBD ANGLES CRACKED. REMOVED DAMAGED IAW SRM 51-42-21. FABRICATED AND INSTALLED ANGLES IAW REO 601R-53-11-926, REV B.

Part: POST — CRACKED (BS 409) · airframe 34,537 hrs · 30,163 cycles

INDICATION NOTED AT FS 409+128 WL 69.0 LBL 18 OTBD CHANNEL IN RADIUS APPROX .10 L 50 PERCENT FULL SCREEN HEIGHT. LBL 18 OTBD CHANNEL FAILED NDT. REMOVED POST AT LBL 18 STA 409+128 IAW SRM 51-42-06. DRILLED UP AND INSTALLED NEW POSTS PN 601R32208-156 AND 601R32208-315 IAW SRM 51-42-06 AND REO 601R-53-41-889 AND SRM 51-40-11.

Part: FLOOR SUPPORT — CORRODED (BS 559) · airframe 34,537 hrs · 30,163 cycles

FS 559+48 - 559+80 LT FLOOR SUPPORT HAS CORROSION. REPAIRED IAW EO CL600-2B19-53-I00194.

Part: FLOOR SUPPORT — CORRODED (BS 349) · airframe 34,537 hrs · 30,163 cycles

RT FLOOR SUPPORT JUST AFT OF FS 349 HAS CORROSION AROUND NUTPLATE HOLE. REPAIRED IAW EO CL600-2B19-53-I00186.

Part: ANGLE — CRACKED (BS 621) · airframe 34,537 hrs · 30,163 cycles

BS 621 BULKHEAD INTERCOSTAL CLIP AT STGR 16L IS CRACKED APPROX 1.5L. REMOVED 621 BULKHEAD CLIP AT STGR 16L IAW SRM 5-42-06 AND 51-42-21. LOCATED AND DRILLED NEW INTERCOSTAL CLIP IAW SRM 51-40-11. INSTALLED NEW CLIP AT FS 621 STGR 16L IAW SRM 51-42-06 AND 51-42-21.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 34,537 hrs · 30,163 cycles

CARGO DOOR INNER SKIN CRACKED AT THE UPPER FWD STOP BRACKET IN 2 PLACES. REMOVED DAMAGED DOOR FRAME SECTION AND CUT AWAY CHANNEL AND CAP ANGLE IAW BSC PRELIMINARY EO CL600-2B19-52-I00176. FABRICATED & INSTALLED REPAIR PARTS FOR CARGO DOOR FRAME REPAIR AND C/W FINAL BSC EO CL600-2B19-52-L00176.

Part: FLOOR SUPPORT — CORRODED (BS 559) · airframe 34,537 hrs · 30,163 cycles

RT FLOOR SUPPORT FS 559+116 - 599+32 HAS CORROSION. REPAIRED IAW CL600-2B19-53-I00193A.

Part: FLOORBEAM — CORRODED (BS 574) · airframe 34,537 hrs · 30,163 cycles

FLOORBEAM AT FS 574 BETWEEN RBL 18 & RBL 27 IS CORRODED. R & R FLOORBEAM CAP IAW SRM 51-42-06.

Part: ANGLE — CRACKED (BS 621) · airframe 34,537 hrs · 30,163 cycles

621 BULKHEAD INTERCOSTAL CLIP AT S14L IS CRACKED APPROX 1.5L. REMOVED 621 BULKHEAD INTERCOSTAL CLIP AT STGR 14L IAW SRM 51-42-06, 51-42-21. INSTALLED NEW SERVICEABLE 621 BULKHEAD INTERCOSTAL CLIP AT STR 14L IAW SRM 51-42-06 AND 51-42-21.

Part: ANGLE — CRACKED (FLOOR SUPPORT) · airframe 34,537 hrs · 30,163 cycles

RT 484, RBL 27 FLOOR SUPPORT CRACKED. R & R FLOOR SUPPORT ANGLE IAW SRM 51-40-11 AND 51-42-21.

Part: ANGLE — CRACKED (BS 621) · airframe 34,537 hrs · 30,163 cycles

BS 621 BULKHEAD INTERCOSTAL CLIP AT S13L IS CRACKED APPROX 1.5L. REMOVED 621 BULKHEAD INTERCOSTAL CLIP AT STGR 13L IAW SRM 51-42-06 AND SRM 51-42-21. LOCATED AND DRILLED NEW INTERCOSTAL IAW SRM 51-40-11 AND INSTALLED IAW SRM 51-42-21 AND SRM 51-42-06.

Part: FLOOR SUPPORT — CORRODED (BS 349) · airframe 34,537 hrs · 30,163 cycles

FLOOR SUPPORT ANGLE AT FS 349 LBL 42 HAS CORROSION. REPAIRED IAW EO CL600-2B19-53-I00191.

Part: FLOOR SUPPORT — CORRODED (BS 559-321) · airframe 34,537 hrs · 30,163 cycles

RT CARGO FLOOR SUPPORT FROM FS 621 TO 559+180 HAS MULTIPLE AREAS OF CORROSION. REPAIRED IAW EO CL600-2B19-53-I00196.

Part: GLOWSTRIP — MISSING (CABIN) · airframe 34,352 hrs · 29,989 cycles

FWD CABIN PHOTOLUMINESCENT ISLE END MARKERS ARE MISSING. INSTALLED FWD CABIN PHOTOLUMINESCENT AISLE END MARKERS IAW AMM 33-51-01.

Part: LIGHT — MALFUNCTIONED · airframe 31,333 hrs · 27,307 cycles

EMERGENCY LIGHTS ON REGARDLESS OF SWITCH POSITION. PERFORMED OPS CHECK OF EMERGENCY LIGHTS IN REF WITH AMM 33-51-00. OPS CHECK GOOD. NO DEFECTS NOTED.

Part: BATTERY PACK — UNSERVICEABLE (EMERGENCY LIGHT) · airframe 30,788 hrs · 26,787 cycles

REFER TO DMIL 767423 "EXTERIOR EMERGENCY LIGHT INOP". R & R NR 3 EMERGENCY LIGHT BATTERY PACK IAW AMM 33-51-04. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED. DMIL 767423 IS CLEARED. PLACARD REMOVED.

Part: BATTERY PACK — UNSERVICEABLE (EMERGENCY LIGHTS) · airframe 30,788 hrs · 26,787 cycles

EXIT SIGN IN MIDDLE CABIN WILL NOT ILLUMINATE (CABIN EMERGENCY LIGHTS ). R & R NR 3 EMERGENCY LIGHT BATTERY PACK IAW AMM 33-51-04. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED. DMIL 767422 IS CLEARED. PLACARD REMOVED.

Part: BATTERY PACK — UNSERVICEABLE (EMERGENCY LIGHT) · airframe 30,788 hrs · 26,787 cycles

NR2 EMERGENCY LIGHT OVER THE WING DOES NOT ILLUMINATE. EXTERIOR EMERGENCY LIGHTS - ACFT NOT OPERATED AT NIGHT. R & R NR3 EMERGENCY LIGHT BATTERY PACK IAW AMM 33-51-04. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED. DMIL 767423 IS CLEARED. PLACARD REMOVED.

Part: BATTERY PACK — UNSERVICEABLE (EMERGENCY LIGHT) · airframe 30,788 hrs · 26,787 cycles

REFER TO DMIL 767422 "MIDDLE EMERGENCY CABIN SIGN INOP." R & R NR 3 EMERGENCY LIGHT BATTERY PACK IAW AMM 33-51-04. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED. DMIL 767422 IS CLEARED. PLACARD REMOVED.

Part: DOOR — BINDING (MAIN PAX) · airframe 30,721 hrs · 26,729 cycles

MAIN PASSENGER DOOR DIFFICULT TO OPEN. PERFORMED OPERATIONAL CHECK OF MAIN PASSENGER DOOR IAW AMM 52-11-02. OPS CHECKED GOOD.

Part: HANDLE — BINDING (PAX DOOR) · airframe 30,535 hrs · 26,558 cycles

HAD DIFFICULT STOWING DOOR OUTER HANDLE LEAVING GPS AND DOOR WAS DIFFICULT TO OPEN. PERFORMED OPS CHECK OF PASSANGER DOOR IAW AMM 52-10-00. OPS CHECK GOOD. NO DEFECTS NOTED.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 30,479 hrs · 26,509 cycles

EMERGENCY LIGHT COVER BROKEN. REPLACED PAX ENTRY EMERGENCY LIGHT COVER AS REQUIRED.

Part: DOOR — BINDING (PAX) · airframe 30,418 hrs · 26,453 cycles

PAX DOOR HARD TO OPEN. FOUND EXCESSIVE AMOUNTS OF GREASE ON PAX DOOR SEAL , CLEANED AND RE-LUBBED AS REQUIRED. PERFORMED VISUAL AND FUNCTIONAL CHECK OF PAX DOOR , NO DEFECTS NOTED PAX DOOR OP CHECKS GOOD IAW AMM 52-11-00. DEFER CLEARED PLACARD REMOVED. (CLOSED)

Part: DOOR — BINDING (MAIN PAX) · airframe 30,418 hrs · 26,453 cycles

PAX DOOR GET STUCK CLOSED. LUBRICATED DOOR STRIKERS AND ROLLERS, OPS CHECKED GOOD 5 TIMES WITHOUT FAULT IAW AMM 52-11-00.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 30,413 hrs · 26,448 cycles

EMERGENCY LIGHT UNDER ARROW BY MAIN CABIN DOOR AND LENS BROKE BASE. REPLACED LIGHT COVER.

Part: SEAL — CONTAMINATED (PAX DOOR) · airframe 30,413 hrs · 26,448 cycles

F/A STATES THAT DOOR HANDLE WILL NOT COME UP TO OPEN DOOR. (DOORS AND OVERWING EMERGENCY EXITS) FOUND EXCESSIVE AMOUNTS OF GREASE ON PAX DOOR SEAL, CLEANED AND RE-LUBED AS REQUIRED. PERFORMED VISUAL AND FUNCTIONAL CHECK OF PAX DOOR , NO DEFECTS NOTED. IAW AMM 52-11-00, PAX DOOR OPS CHECKS GOOD. DEFER CLEARED , PLACARD REMOVED.

Part: DOOR — BINDING (MAIN PAX) · airframe 30,326 hrs · 26,371 cycles

CABIN DOOR WILL NOT OPEN FROM INSIDE ACFT, UNLESS ASSISTED BY GROUND CREW. SAW THE GROUND CREW PUSH THE VENT FLAP TO GET DOOR OPEN. OPS CHECK AND LUBRICATE CABIN DOOR WITH REF TO AMM 52-11-00. OPS CHECK GOOD. ACFT OK FOR SERVICE.

Part: STRUCTURE — CORRODED (BS 364 S25L/R) · airframe 29,654 hrs · 25,775 cycles

FUSELAGE FS 364.00 HAS CORROSION FROM STGR 25L TO 25R.

Part: FRAME — CORRODED (BS 364) · airframe 29,654 hrs · 25,775 cycles

FUSELAGE FS 364.00 HAS CORROSION FROM STR 25L TO 25R. REMOVED LIGHT CORROSION IAW SRM 51-21-06, STEPS 3B1 THROUGH 5. FOUND TO BE WITHIN LIMITS IAW SRM 53-21-15 AND 53-00-00.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 29,654 hrs · 25,775 cycles

EMERGENCY LIGHTING WIRE BROKE OFF ON PANEL 232BZ. REPLACED EMERGENCY LIGHT IAW 33-51-10-400-801. OPS TESTED GOOD.

Part: SUPPORT ANGLE — CORRODED (BS 349) · airframe 29,654 hrs · 25,775 cycles

SUPPORT ANGLE ON FS 349.00, RBL 38.00 CORRODED. INSTALLED NEW SERVICEABLE SUPPORT ANGLE PN 601R38783-13 IAW SRM 51-42-06, 51-42-21 & 51-42-13. REPAIR REQUIRES MAJOR/MINOR CLASSIFICATION IAW SOP 5702. THIS REPAIR IS CLASSIFIED AS A MINOR REPAIR IAW SOP 5702. (CLOSED)

Part: FRAME — CORRODED (BS 349) · airframe 29,654 hrs · 25,775 cycles

FRAME FS 349.00 HAS CORROSION FROM STR 25L TO STR 25R. INSTALLED 6 EA SAME NUTPLATES ON DRAIN MAST NUTPLATES. INSPECTED AND FOUND TO BE IN SERVICEABLE CONDITION IAW SRM 51-42-06 AND 51-45-00. REINSTALLED SAME SERVICEABLE INTERCOSTAL AT STR 25L IAW SRM 51-42-06. TREATED, PRIMED AND PAINTED REPAIRED AREA IAW SRM 51-25-16. APPLIED CORROSION PREVENTATIVE TO REPAIR IAW SRM 51-21-11.

Part: FLOOR PANEL — CORRODED (BS 409-559) · airframe 29,654 hrs · 25,775 cycles

UPPER SURFACE OF PRESSURE FLOOR SKIN HAS SEVERAL AREAS OF CORROSION FROM FS 409+128 TO FS 559 ON RBL 36 TO RBL 47. REPAIRED IAW REO 601R-53-41-1354.

Part: ANGLE — CORRODED (PAX DOOR) · airframe 29,654 hrs · 25,775 cycles

PAX DOOR LOWER ANGLE CORRODED AT LWR ENTRANCE SURROUND. REMOVED CORRODED ANGLE IAW SRM CH 51-42-06, 51-42-10 AND CH 51-42-21. LOCATED, DRILLED, SEALED, INSTALLED AND PAINTED NEW SILL ANGLE IAW SRM 51-40-11, 51-23-00, 51-42-11, 51-42-21 AND 51-25-21. REPAIR IS CLASSIFIED AS MINOR.

Part: FLOOR PANEL — CORRODED (BS 409-559) · airframe 29,654 hrs · 25,775 cycles

UPPER SURFACE OF PRESSURE FLOOR SKIN HAS SEVERAL AREAS OF CORROSION FROM FS 409+128 TO FS 559 ON RBL 36 TO RBL 47. REPAIRED IAW REO 601R-53-41-1353.

Part: ANGLE — CRACKED (BS 280) · airframe 29,654 hrs · 25,775 cycles

FS 280.090, RBL 9.0, OTBD ANGLE IS CRACKED. REMOVED CRACK ANGLE IAW SRM 51-42-21. FABRICATED AND INSTALLED ANGLE IAW REO 601R-53-11-638, REV A, STEP 4.

Part: STRUCTURE — CORRODED (BS 333 S25L/R) · airframe 29,654 hrs · 25,775 cycles

FUSELAGE FS 333.00 HAS CORROSION FROM STR 25L TO STR 25R.

Part: SEAT TRACK — CORRODED · airframe 29,654 hrs · 25,775 cycles

CORRODED SEAT TRACKS IN CARGO BAY AT FS 559+112, RBL 9 AND RBL 27. REMOVED OLD SEAT TRACKS AND INSTALLED NEW SERVICEABLE SEAT TRACK PN 601R38779-13 AT FS 559+112, RBL 9 AND PN 601R38779-9 AT FS 559+112, RBL 27 IAW SRM 51-40-11, 51-41-00. THIS REPAIR IS CLASSIFIED AS A MINOR REPAIR IAW SOP 5702.

Part: BRACKET — CORRODED (FUSELAGE) · airframe 29,654 hrs · 25,775 cycles

PAX DOOR SURROUND STRUCTURE AFT BRACKET HAS CORROSION. LOCATED FASTENER HOLES IN NEW BRACKETS FOR AFT PAX DOOR SURROUND STRUCTURE IAW SRM CH 51-45-00 AND CH 51-40-11. INSTALL NEW BRACKET. INSTALLED THE PAX DOOR AFT CUP BRACKET IAW THE SRM 51-42-06 & 51-42-11, 51-23-00, 51-25-21. ALSO, FOUND THE UPPER CLEAT ON THE CUP BRACKET IS CORRODED AND REQUIRES REPLACEMENT. LOCATED, DRILLED, SEALED AND INSTALLED A NEW CLEAT PN 601R31527-137 IAW THE SRM 51-42-06, 51-23-00, 51-25-21, 51-40-11. THIS REPAIR IS CLASSIFIED AS A MINOR REPAIR IAW SOP 5702.

Part: SILL — CORRODED (FUSELAGE) · airframe 29,658 hrs · 25,781 cycles

SERVICE DOOR LOWER SILL HAS CORROSION. INSTALLED FWD & AFT SERVICE DOOR SILL PLATE LATCHES IAW AMM 20-24-00-910-803 AND 20-24-00-910-806.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 29,654 hrs · 25,775 cycles

CARGO BAY SEAT TRACK CORRODED AT FS 559+112, LBL 9 AND LBL 27. REMOVED OLD SEAT TRACKS AND INSTALLED NEW SERVICEABLE SEAT TRACKS, PN 601R38779-13 AT FS 559+112, LBL 9 AND PN 601R38779-9 AT FS 559+112 LBL 27 IAW SRM 51-40, 57-41-00. THIS REPAIR IS CLASSIFIED AS A MINOR REPAIR IAW SOP 5702.

Part: SEAT TRACK — CORRODED (BS 574) · airframe 29,654 hrs · 25,775 cycles

CARGO BAY SEAT TRACK CORRODED AT FS 574, LBL 9. REMOVED OLD SEAT TRACK AND INSTALLED NEW SERVICEABLE SEAT TRACK PN 601R38779-5 AT FS 574 LBL 9 IAW SRM 51-40-11, 51-41-00. THIS REPAIR REQUIRES MAJOR/MINOR CLASSIFICATION IAW ASA SOP 5702. THIS REPAIR IS CLASSIFIED AS A MINOR REPAIR IAW SOP 5702. (CLOSED)

Part: SUPPORT BEAM — CRACKED (BS 621) · airframe 29,654 hrs · 25,775 cycles

CARGO DOOR SUPPORT BEAM ANGLE CRACKED AT FS 621.00. R & R BRACKET, PN 601R35050-109 AT CARGO DOOR SUPPORT BEAM AND FS 621 BULKHEAD IAW SRM 51-40-11, 51-42-21. THIS REPAIR REQUIRES MAJOR/MINOR CLASSIFICATION IAW ASA SOP 5702. THIS REPAIR IS CLASSIFIED AS A MINOR REPAIR IAW SOP 5702. (CLOSED)

Part: FLOORBEAM — CRACKED (BS 280) · airframe 29,654 hrs · 25,775 cycles

CABIN FLOOR SUPPORT STRUCTURE FS 280.00 AND LBL 9.0 CLIP IS CRACKED. REMOVED CRACKED FLOORBEAM IAW SRM 51-42-21. FABRICATED REPAIRE IAW REO 601R-53-11-638 REV A, STEP 4. INSTALLED REPAIR IAW REO 601R-53-11638 STEP 11.

Part: SEAT TRACK — CORRODED (BS 574) · airframe 29,654 hrs · 25,775 cycles

CARGO BAY SEAT TRACK CORRODED AT FS 574, RBL 9. REMOVED OLD SEAT TRACK AND INSTALLED NEW SERVICEABLE SEAT TRACK PN 601R38779-49 IAW SRM 51-40-11, 51-41-00 AT FS 574 RBL 9. THIS REPAIR REQUIRES MAJOR/MINOR CLASSIFICATION IAW SOP 5702. THIS REPAIR IS CLASSIFIED AS A MINOR REPAIR IAW SOP 5702. (CLOSED)

Part: FRAME — CORRODED (BS 349) · airframe 29,654 hrs · 25,775 cycles

FRAME FS 349 HAS CORROSION FROM STR25L TO STR 25R. REMOVED CORROSION FROM FS 349 IAW SRM 51-21-06. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00. REMOVED AND INSTALLED NEW LOWER FRAME SECTOR AT FS 349.00 IAW SRM 51-42-06, 51-42-21.

Part: FRAME — CORRODED (BS 319.7) · airframe 29,654 hrs · 25,775 cycles

FUSELAGE FS 319.70 HAS CORROSION FROM STR 25L TO STR 25R. REMOVED CORROSION IAW SRM 51-21-06. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00. R & R FRAME 319.70 IAW SRM 51-42-06 & 51-42-21.

Part: FRAME — CORRODED (BS 364) · airframe 29,654 hrs · 25,775 cycles

FRAME FS 364.00 HAS CORROSION FROM STR 25L TO 25R. REPAIRED IAW SRM 51-42-06

Part: POST — CRACKED (BS 409) · airframe 29,654 hrs · 25,775 cycles

FOUND FS 409.0+128, VERT POST BL 0.0 LT & RT SIDES HAVE INDICATIONS NOTED APPROX .2" IN LENGTH 60 PERCENT AT WL 69.0 AFT FLANGE RADIUS. BOTH FAILED NDT INSP. REMOVED VERTICAL POST IAW SRM 51-42-22 AND 51-42-21. INSTALLED NEW POST AND ANGLES IAW REO 601R-53-41-889, STEP 2 AND WITH REO 601R-53-41-1357, STEPS 1-12, AND SRM 51-42-06.

Part: FRAME — CORRODED (BS 333) · airframe 29,654 hrs · 25,775 cycles

FRAME F.S. 333 HAS CORROSION FROM STR 25L TO STR 25R. REMOVED CORROSION IAW SRM 51-21-06. AREA FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00. R & R LOWER FRAME SECTOR IAW SRM 51-42-06, 51-42-21.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 29,654 hrs · 25,775 cycles

LT/ RT FWD TWO SECTIONS OF FLOOR SEAT TRACK ARE CORRODED IN CABIN. REPLACED SEAT TRACKS IAW MM 53-01-11-000-802 & 53-01-11-400-802.

Part: ANGLE — CRACKED (BS 484) · airframe 29,654 hrs · 25,775 cycles

ANGLE AT FS 484, LBL 27 IS CRACKED. (PREVIOUS REPAIR). R & R ANGLE AT FS 484, LBL 27 IAW SRM 51-42-21. THIS REPAIR REQUIRES MAJOR/MINOR CLASSIFICATION IAW SOP 5702. THIS REPAIR IS CLASSIFIED AS A MINOR REPAIR IAW SOP 5702.

Part: ATTACH FITTING — CRACKED (BS 484) · airframe 29,654 hrs · 25,775 cycles

REPAIR AT RBL 36, FS 484 CLIP IS CRACKED. REMOVED & INSTALLED NEW SERVICEABLE FABRICATED FITTING IAW SRM 51-42-21.

Part: SIGN — NO TEST (CABIN) · airframe 29,654 hrs · 25,775 cycles

PAX DOOR BETA LIGHT EXIT SIGN FAILED FUNCTIONAL TEST LIGHT DIM. REPLACED PAX DOOR BETA LIGHT IAW MM 33-51-09-400-801. PERFORMED FUNCTIONAL TEST IAW 33-51-09-720-801 AMM. CHECKED GOOD.

Part: SIGN — NO TEST (CABIN) · airframe 29,654 hrs · 25,775 cycles

SERVICE DOOR BETA LIGHT "EXIT SIGN" FAILS FUNCTIONAL TEST LIGHT TO DIM. REPLACED SERVICE DOOR BETA LIGHT SIGN IAW AMM TASK 33-51-09-400-802. FUNCTIONALLY TESTED GOOD AT THIS TIME.

Part: FLAP SYSTEM — UNKNOWN (TE FLAPS) · airframe 29,583 hrs · 25,705 cycles

FLAP FAIL MESSAGE- FLAP FAIL AT 0. EMERGENCY DECLARED. COULD NOT DUPLICATE FAULT. MCO CLEARED. ACFT OK FOR SERVICE.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 29,127 hrs · 25,272 cycles

F/A FLASHLIGHT INOP. R & R BATTERIES IAW AMM 25-60-00. OPS CK GOOD. (CLOSED)

Part: LINKAGE — OUT OF ADJUST (PAX DOOR) · airframe 28,242 hrs · 24,511 cycles

PAX DOOR IS HARD TO OPEN & CLOSE. ADJUSTED OUTER DOOR HANDLE LINKAGE IAW AMM 52-11-03. OPS CHECKED GOOD NO FURTHER DEFECTS NOTED. (CLOSED)

Part: UNKNOWN — SMOKE (CABIN) · airframe 28,033 hrs · 24,326 cycles

FLT U:7135--PASSENGERS IN 10 A&B COMPLAINED OF SMOKE ON SHORT FINAL (EMERGENCY DECLARED - TRUCKS STANDING BY AS A PRECAUTION) PERFORMED SYS CKS AND INSP OF BOTH ENG'S BOTH PACK SYS AND APU NO FAULTS FOUND NO LEAKS NO SMOKE OR SMELL. LT & RT PACK ACM SERVICED GOOD BOTH LT & RT ENG'S TOOK NO OIL APU SERVICED GOOD. ALL SYS OP CK GOOD IAW AMM 21-00-00, 49-00-00, AND 71-00-00. (CLOSED)

Part: BPSU — FAILED (TE FLAPS) · airframe 27,787 hrs · 24,102 cycles

FLAP FAIL AT 0 DEG ON APPROACH. (EMERGENCY DECLARED). R & R LT BPSU ASSY IAW AMM-27-51-10. PERFORMED RIGGING TEST AND POSITION TEST IAW 27-51-10-830-801. OPS CHECKS GOOD NO DEFECTS NOTED C/W AD 2009-06-12. MCO CLEARED. (CLOSED)

Part: WINDOW — ARCED (COCKPIT) · airframe 27,903 hrs · 24,207 cycles

RT MOST WINDOW SPARKED DURING FLIGHT. R & R RT SIDE WINDOW IAW AMM 56-12-01 , OPS CHECKS GOOD . LEAK CHECK GOOD IAW AMM 21-32-00-863-801 . NO FURTHER DEFECTS NOTED . OK FOR SERVICE.

Part: CONNECTOR — FIRE (WINDSHIELD HEAT) · airframe 26,977 hrs · 23,328 cycles

IN DESCENT THRU 23K FT GOT LOUD BANG, FLAMES AND SMOKE FROM LT WINDSHIELD LWR PWR CONNECTOR. TURNED OFF LT W/S HEAT AND SMOKE AND FLAME STOPPED. EMERGENCY DECLARED.

Part: STEERING SYS — INOPERATIVE (NLG) · airframe 26,938 hrs · 23,284 cycles

"STEERING INOP" CAUTION MSG DURING FLIGHT CLEARED ITSELF AFTER LANDING NOSE WHEEL STEERING WORKED NORMAL DURING TAXI. TOWER DECLARED EMERGENCY -- FIRE TRUCKS REQ'D AS A PRECAUTION.

Part: DOOR — BINDING (CABIN) · airframe 26,237 hrs · 22,549 cycles

PAX DOOR WAS DIFFICULT TO OPEN.

Part: DOOR — STUCK (CABIN) · airframe 26,190 hrs · 22,507 cycles

MAIN PAX DOOR LATCH STUCK. F/A COULD NOT OPEN AT THE GATE. ALSO ON TAXI IN WE RECIEVED A "PAX DOOR" CAUTION MSG FOR 10 SEC OR SO.

Part: DOOR — STIFF (MAIN PAX) · airframe 25,952 hrs · 22,277 cycles

MAIN DOOR SOMETIMES DIFFICULT TO OPEN.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 25,768 hrs · 22,101 cycles

CHANNEL FOUND CRACKED AFT FS 554 LT SIDE MAIN UNDERCARRIAGE UPLOCK AND APRON ASSY. REMOVED CHANNEL AND FABRICATED NEW CHANNEL PER SAMPLE AND DRAWING PL601R31058. INSTALLED CHANNEL IAW 51-12-06.

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 25,768 hrs · 22,101 cycles

FS 621.00 BULKHEAD HAS A 75 PERCENT FSH INDICATION NOTED IN THE WEB AT LBL 9.50 WL 132.5. INDICATIONS IS 0.2 INCH LONG. FAILS NDT INSPECTION AT THIS TIME. REPAIR F.S. 621 BULKHEAD AT LBL 95.0 WL 132.5 IAW REO 601R-53-61-1285 AND 601R-53-61-3099.

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 25,768 hrs · 22,101 cycles

QTY 3 EDDY CURRENT INDICATIONS FOUND DURING THE INSP OF FS 559.00 SEMI-PRESSURE BULKHEAD WEB AND CAP ANGLE. SIZES AND LOCATIONS AS LISTED WEB AT RBL 18 WL 59.10 HAS 1005 FSH INDICATION 1.5 INCH LONG, CAP ANGLE AT RBL 18 HAS 80 PERCENT FSH INDICATION APPROX .2 INCH LONG, CAP ANGLE AT LBL 18 HAS 100 FSH INDICATION APPROX .5 INCH LONG, FAILS NDT INSP AT THIS TIME. COMPLIED WITH REPAIR OF BULKHEAD WEB AND POSTS IAW REO 601R-53-41-260. COMPLIED WITH EC/TC REO 601R-53-41-260.

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 25,768 hrs · 22,101 cycles

FS 621.00 BULKHEAD HAS A 100 PERCENT FSH EDDY CURRENT INDICATION, APPROX 0.1 INCH LONG IN THE WEB SURROUNDING THE LINTEL FITTING. FAILS NDT INSPECTION AT THIS TIME. INDICATION EXTENDS FROM TOP OF FITTING. REPAIR PER EC/TC REO 601R-53-61-1230 HAS BEEN COMPLETED AND THE REPAIR COMPLIES WITH THE REQUIREMENTS OF EC/TC AND REO 601R-53-61-1230 REV.D.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 25,768 hrs · 22,101 cycles

FS 625 OBLIQUE ANGLE IS CRACKED AT STR 14R. REMOVED AND REPLACED OBLIQUE ANGLE IAW SRM 51-42-21.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 25,768 hrs · 22,101 cycles

THE RT UPPER FS 625.0 INTERCOSTAL IS CRACKED.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 25,768 hrs · 22,101 cycles

PRESSURE BULKHEAD HAS A CRACKED ISOLATOR BRACKET AT RBL 36 WL 97.50 ON FWD SIDE OF BULKHEAD.

Part: FITTING — CRACKED (FUSELAGE) · airframe 25,472 hrs · 21,833 cycles

CLIP ON INTERCOSTAL CRACKED ON UPPER 2ND FS 484.0 LBL 27.

Part: ACTUATOR — MALFUNCTIONED (THRUST REVERSER) · airframe 24,959 hrs · 21,352 cycles

IN FLIGHT RETURN, RT THRUST REV UNLOCK MSG AT 22000FT, UNCOMMANDED YAW. RT ENGINE SHUTDOWN IN FLIGHT. EMERGENCY DECLARED. A/C RETURNED TO ATL AFTER T/O. REMOVED AND REPLACED BALL SCREW ACTUATOR IAW AMM 78-3201, OPS CHECK GOOD. CLEARED, PLACARD REMOVED.

Part: HANDLE — OUT OF POSITION (DOOR) · airframe 24,910 hrs · 21,301 cycles

FLIGHT ATTENDANT CLOSED DOOR, PLUNGER PULLED OUT, INNER HANDLE CAME OUT. GATE RETURN.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

RT SIDE FUSELAGE AFT EMERGENCY EXTERIOR LIGHT INOP. RELAMPED AFT EMERGENCY LIGHT AT RT EXTERIOR SIDE OF FUSELAGE IAW CRJ 200 AMM 33-51-21. OPS CHECK GOOD. (A)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 2,401,254 hrs · 20,477 cycles

EMERGENCY LIGHTS DO NOT WORK. FLT 4691 DEL 36 MINS REMOVED AND REPLACED BATTERY PACKS, IAW AMM 33-51-01. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,889 hrs · 20,370 cycles

F/A REPORTS SOME FLOOR LEVEL EMERGENCY LIGHTING IS INOP. FLT 4906 DEL 21 MINS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,814 hrs · 20,306 cycles

OVERWING EMERGENCY LIGHT INOP.

Part: PUMP — LEAKING (HYDRAULIC SYS) · airframe 23,655 hrs · 20,174 cycles

REMOVAL OF HYDRAULIC PUMP, LEAKING. EMERGENCY DECLARED. FLT 4915 DEL 68 MINS.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 23,626 hrs · 20,148 cycles

EMERGENCY LIGHT ON RIGHT FUSELAGE AFT IS INOP.

Part: DOOR — BINDING (SERVICE DOOR) · airframe 22,431 hrs · 19,101 cycles

SERVICE DOOR WILL NOT OPEN FROM OUTSIDE. FLT 4605 DEL 91 MINS.

Part: DOOR — STUCK (SERVICE DOOR) · airframe 22,358 hrs · 19,045 cycles

SERVICE DOOR WILL NOT OPERATE FROM THE OUTSIDE.

Part: WARNING SYSTEM — ACTIVATED (PAX DOOR) · airframe 22,318 hrs · 19,011 cycles

PAX DOOR HANDLE MSG. EN ROUTE TO MLI A/C DIVERTED TO CHA DUE TO MTC. EMERGENCY DECLARED.

Part: HANDLE — BROKEN (PAX DOOR) · airframe 22,001 hrs · 18,775 cycles

STATION REPORTING THE PAX DOOR OUTER HANDLE BROKEN OFF WHILE CLOSING DOOR.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,828 hrs · 18,638 cycles

RIGHT EMERGENCY OVERWING MIDDLE EXT LIGHT INOP.

Part: DOUBLER — CORRODED (BS 640) · airframe 21,594 hrs · 18,460 cycles

FOUND RT FS 640 INNER BONDED SKIN DOUBLER CRACKED AT STR 9. COMPLIED WITH EC/TC ASA REO 601R-53-61-506. RII-5001388.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 21,594 hrs · 18,460 cycles

LEFT FS 640 INNER BONDED SKIN DOULBER CRACKED AT STR 9. COMPLIED WITH EC/TC ASA RE 601R-53-61-506. RII-5001388.

Part: ATTACH ANGLE — CRACKED (BS 621) · airframe 21,594 hrs · 18,460 cycles

FOUND 2 NTERCOSTAL CLIPS CRACKED LT AFT 621 BULKHEAD BETWEEN FS 621.00 AND 625.00.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 21,594 hrs · 18,460 cycles

RIGHT OBLIQUE ANGLE CRACKED AFT 621 BULKHEAD.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 21,594 hrs · 18,460 cycles

RIGHT I/B INTERCOSTAL LOCATED AT FS 484 AND RBL 27, IS CRACKED.

Part: STRUCTURE — CRACKED (PAX DOOR) · airframe 21,594 hrs · 18,460 cycles

PAX DOOR CRACK AT FS 320.010 ABOVE DATUM 1. [SUP 05-09-07] REPAIRED PAX DOOR FWD FRAME AT FS 320.010 IAW ASA EO REO 601R-52-11-402.

Part: STRUCTURE — CRACKED (PAX DOOR) · airframe 21,594 hrs · 18,460 cycles

PAX DOOR CRACK AT FS 338.00 ABOVE DATUM 1. [SUP 4-24-07] COMPLIED WITH REPAIR TO PAX DOOR AFT FRAME MEMBER AT FS 338.00 IAW ASA REO 601R-52-11-402.

Part: ANCHOR FITTING — CRACKED (PAX DOOR) · airframe 21,594 hrs · 18,460 cycles

PAX DOOR AFT ANCHOR FITTING CRACKED. [SUP 05-09-07] INSTALLED SERVICEABLE BASE PLATE P/N 600-38061-6 1EA AND SERVICEABLE ANCHOR FITTING P/N 601R38074-51SB01

Part: CAUTION MESSAGE — ILLUMINATED · airframe 20,588 hrs · 17,722 cycles

UPON TAKEOFF IN ATL, GEAR SELECTED UP LT & RT MAIN CAME UP AND CENTER STAYED DOWN, GOT NOSE DOOR OPEN MASTER CAUTION WARNING FOLLOWED BY A GEAR DISAGREE WARNING. PUT GEAR DOWN LANDING ATL. AIRCRAFT RETURNED TO ATL AFTER T/O. FLT 4564 CX AND ON 11/16/06 FLT 4322 CX.

Part: STEP — CRACKED (AIR STAIR DOOR) · airframe 19,373 hrs · 16,795 cycles

ASD BOTTOM STEP CRACKED.

Part: PRESSURE SWITCH — INOPERATIVE (NLG STEERING)

DURING CLIMB-OUT FROM ATL-TYS, THE CREW RECEIVED A STEERING INOPERATIVE CAUTION MESSAGE. THE QRH WAS COMPLIED WITH AND THE CREW DECLARED AN EMERGENCY. THE EMERGENCY VEHICLES WERE DISPATCHED, AND THE AIRCRAFT RETURNED TO ATL WHERE IT LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE NOSE WHEEL STEERING PRESSURE SWITCH. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: ELECTRICAL SYS — MALFUNCTIONED (COCKPIT)

FLT 4738 - DURING CRUISE FROM CVG-CLE, THE AC ESS BUS FELL OFFLINE AND WAS RESET IN THE AIR. THE FLIGHT ATTENDANT ALSO REPORTED AN ELECTRICAL BURNING ODOR. THE FLIGHT CONTINUED TO CLE, WHERE IT LANDED SAFELY. MAINTENANCE RESET AC ESS BUS, INSPECTED AND RETORQUED AC ESS BUS RELAY. AIRCRAFT POWERED UP SEVERAL TIMES WITH NO DEFECTS NOTED. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: INTERCOSTAL — CRACKED (BS 280)

DURING A C-CHECK IN MCN, THE FS 280 INTERCOSTAL, AT RBL 9, WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE WILL REMOVE AND REPLACE THE FS 280 INTERCOSTAL, AT RBL 9, IAW REO 601R-53-11-638. (M)

Part: SIGN — INOPERATIVE (EMERGENCY EXIT)

DURING A C-CHECK IN MCN, THE PASSENGER DOOR EMERGENCY EXIT SIGN, ON THE LOWER FORWARD CLOSET, WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR EMERGENCY EXIT SIGN, LOCATED ON THE LOWER FORWARD CLOSET. OPS CHECKS GOOD. (M)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DURING A C-CHECK IN MCN, THE SERVICE DOOR EMERGENCY LIGHT, MOUNTED ON THE GALLEY, WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 1 EMERGENCY LIGHT BATTERY PACK. OPS CHECKS GOOD. (M)

Part: SEAT TRACK — CORRODED (BS 513)

DURING A C-CHECK IN MCN, THE UPPER LEFT SEAT TRACK, AT FS 513, AS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE UPPER LEFT SEAT TRACK AT FS 513. (M)

Part: SEAT TRACK — CORRODED (BS 559)

DURING A C-CHECK IN MCN, THE AFT CARGO COMPARTMENT SEAT TRACK, AT FS 559 PLUS 112, WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE WILL REMOVE AND REPLACED THE AFT CARGO COMPARTMENT SEAT TRACK, FROM FS 559 PLUS 112. (M)

Part: SEAT TRACK — CORRODED (BS 559)

DURING A C-CHECK IN MCN, THE LEFT UPPER SEAT TRACK, AT FS 559 PLUS 64, WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE WILL REMOVE AND REPLACED THE LEFT UPPER SEAT TRACK, AT FS 559 PLUS 64. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

DURING A C-CHECK IN MCN, THE RIGHT SIDE SEAT RAIL, FROM THE FRONT TO THE REAR, WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE WILL REMOVE AND REPLACE THE RIGHT SIDE SEAT RAIL, FROM THE FRONT TO REAR. (M)

Part: SEAT TRACK — CORRODED (BS 364)

DURING A C-CHECK IN MCN, THE LEFT INBOARD SEAT TRACK, AT FS 364, WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE WILL REMOVE AND REPLACE THE LEFT INBOARD SEAT TRACK, AT FS 364. (M)

Part: SEAT TRACK — CORRODED (BS 473)

DURING A C-CHECK IN MCN, THE LEFT UPPER SEAT TRACK, AT FS 473.15, WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE WILL REMOVE AND REPLACE THE LEFT UPPER SEAT TRACK, AT FS 473.15. (M)

Part: SEAT TRACK — CORRODED (BS 364)

DURING A C-CHECK IN MCN, THE RIGHT INBOARD SEAT TRACK, AT FS 364, WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE WILL REMOVE AND REPLACE THE RIGHT INBOARD SEAT TRACK, AT FS 364. (M)

Part: HANDLE — CRACKED (ESCAPE HATCH)

DURING A C-CHECK IN MCN, THE CREW EMERGENCY ESCAPE HATCH HANDLE WAS FOUND TO POSSIBLY BE CRACKED. S/D - MAINTENANCE INSPECTED THE CREW EMERGENCY ESCAPE HATCH HANDLE. NO DEFECTS NOTED. (M)

Part: PLACARD — WORN (CABIN)

DURING A C-CHECK IN MCN, THE EMERGENCY ESCAPE PLACARD ON THE PILOT`S ESCAPE HATCH WAS FOUND TO BE WORN. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY ESCAPE PLACARD ON THE PILOT`S ESCAPE HATCH. (M)

Part: DOUBLER — CORRODED (BS 449-529)

DURING A C-CHECK IN MCN, THE LEFT SIDE DOUBLERS, FROM 449-529, BL 45 ON THE PRESSURE FLOOR WERE FOUND TO BE CORRODED. MAINTENANCE IS SUBMITTING A DAMAGE REPORT TO BOMBARDIER TO DETERMINE THE APPROPRIATE CORRECTIVE ACTION. AFTER MAINTENANCE BLENDED, ALODINED, AND PRIMED THE LEFT SIDE DOUBLERS, FROM 449-529, BL 45, IAW REO 601R-53-41-359, FOUND TO BE WITHIN LIMITS. (M)

Part: ANGLE — CRACKED (BS 559)

DURING A C-CHECK IN MCN, THE FLOORBEAM SUPPORT ANGLE, AT FS 559 PLUS 112, LBL 9 WAS SUSPECTED OF BEING CRACKED BEYOND LIMITS. S/D - MAINTENANCE PERFORMED AN INSPECTION ON THE FLOORBEAM SUPPORT ANGLE, AT FS 559 PLUS 112, LBL 9 WITH NO DEFECTS FOUND. (M)

Part: DOUBLER — CORRODED (BS 449-559)

DURING A C-CHECK IN MCN, THE RIGHT SIDE DOUBLERS, FROM 449-559, ON THE PRESSURE FLOOR WERE FOUND TO BE CORRODED. MAINTENANCE IS SUBMITTING A DAMAGE REPORT TO BOMBARDIER TO DETERMINE THE APPROPRIATE CORRECTIVE ACTION. AFTER MAINTENANCE BLENDED, ALODINED, AND PRIMED THE RIGHT SIDE DOUBLERS, FROM FS 449-559, IAW REO 601R-53-41-359, FOUND TO BE WITHIN LIMITS. (M)

Part: CLIP — CRACKED (BS 484)

DURING A C-CHECK IN MCN, THE LEFT OUTBOARD FS 484 CLIP WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LEFT OUTBOARD FS 484 CLIP IAW BOMBARDIER REO 601R-53-41-059. (M)

Part: STRINGER CLIP — CRACKED (BS 339)

DURING A C-CHECK IN MCN, A POSSIBLE CRACK IN THE CLIP AT FS 339, STRINGER 15 RIGHT JUST ABOVE THE SEAT TRACK WAS FOUND. MAINTENANCE PERFORMED AN EDDY CURRENT INSPECTION OF CLIP AT FS 339.00, STRINGER 15 RT. NO DEFECTS WERE NOTED. (M)

Part: SILL — CORRODED (BS 559)

DURING A C-CHECK IN MCN, THE RIGHT SILL PLATE AT FS 559 PLUS 48 FLOOR LEVEL WAS FOUND TO BE CORRODED. S/D - MAINTENANCE REPAIRED THE RHS SILL PLATE, AT FS 559 PLUS 48, IAW BOMBARDIER REO 601R-53-51-036. (M)

Part: DUCT — CORRODED (BS 559)

DURING A C-CHECK IN MCN, FOUND CORROSION AROUND THE INLET DUCT AT FS 559 PLUS 96 RT. AFTER MAINTENANCE BLENDED, ALODINED, AND PRIMED THE INLET DUCT AT FS 559 PLUS 96 RT, IAW REO 601R-53-41-037, IT WAS FOUND TO BE WITHIN LIMITS. (M)

Part: SILL — CORRODED (BS 559-621)

DURING A C-CHECK IN MCN, SEVERAL NUT PLATES AND THE SILL AREA FLOOR LEVEL UNDER THE LAVATORY POTABLE WATER TANK BETWEEN FS 559.64-621 RT WERE FOUND TO BE CORRODED. S/D - MAINTENANCE REPAIRED THE RHS FLOOR SILL, AT FS 559.64-621, IAW BOMBARDIER REO 601R-53-51-036. (M)

Part: SKIN — CORRODED (FUSELAGE)

DURING A C-CHECK, THE INNER BELLY SKIN AFT OF THE LAVATORY FAN BELOW RBL 27 WAS FOUND TO BE CORRODED. S/D - MAINTENANCE REPAIRED THE INNER BELLY SKIN, AFT OF THE LAVATORY, BELOW RBL 27, IAW BOMARDIER REO 601R-53-41-037. (M)

Part: NUT PLATE — CORRODED (BS 559)

DURING A C-CHECK IN MCN, CORROSION WAS FOUND ON THE CARGO SILL NUT PLATE AFT OF THE LAVATORY AT FS 559 +80 RT. MAINTENANCE REMOVED AND REPLACED CORRODED NUT PLATES ON CARGO SILL RT SIDE AFT OF LAV 559+80 IAW SRM 51-00-00 (CLOSED)

Part: CARGO TRACK — CORRODED (CARGO BAY)

DURING A C-CHECK IN MCN, CORROSION WAS FOUND ON THE TIE DOWN FITTINGS AND TIE DOWN TRACKS. AFTER MAINTENANCE REMOVED CORROSION ON THE TIE DOWN FITTINGS AND THE TIE DOWN TRACKS, THEY WERE FOUND TO BE WITHIN LIMITS. (M)

Part: FLOORBEAM — CORRODED (BS 559-621)

DURING A C-CHECK IN MCN, THE FLOORBEAM CAP AT FS 559 PLUS 112 THRU 621.00, LBL 27 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE FLOOREAM CAP AT FS 559 PLUS 112 THROUGH 621.00, LBL 27. (M)

Part: ANGLE — CORRODED (BS 280)

DURING A C-CHECK, THE FORWARD AND AFT FLOOR SUPPORT ANGLES, AT FS 280 BETWEEN LBL 9 AND RBL 9, WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE WILL REMOVED AND REPAIR THE FORWARD AND AFT FLOOR SUPPORT ANGLES, AT FS 280 BETWEEN LBL 9 AND RBL 9, IAW REO 601R-53-11-638. (M)

Part: BEAM — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE CENTER BOX BEAM WAS SUSPECTED OF BEING CRACKED UNDER THE CLIP. MAINTENANCE WILL REPAIR THE CENTER BOX BEAM IAW ASA EO 600-53-0072B. (M)

Part: SKIN — CRACKED (NLG DOOR)

DURING A C-CHECK IN MCN, THE RADIUS OF FUSELAGE SKIN FORWARD OF THE NOSE LANDING GEAR DOOR WAS SUSPECTED OF BEING CRACKED BEYOND LIMITS. S/D - MAINTENANCE REPAIRED THE FUSELAGE SKIN RADIUS RH AND LHS, AT FS 235, IAW ASA EO 600-53-0122. (M)

Part: CLIP — CRACKED (BS 280)

DURING A C-CHECK IN MCN, THE FS 280, LBL 9 AND RBL 9 INBOARD CLIPS WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE WILL REMOVE AND REPLACED THE FS 280, LBL 9 AND RBL 9 INBOARD CLIPS IAW REO 601R-53-11-638. (M)

Part: RIB — CRACKED (RT WING)

DURING A C-CHECK IN MCN, THE RIGHT BATT RIB ASSEMBLY AT WS 53.60 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE WILL REPAIR THE RIGHT BATTERY RIB ASSEMBLY AT WS 53.60 IAW ASA EO 600-57-0039B. (M)

Part: CLIP — CRACKED (BS 280)

DURING A C-CHECK IN MCN, THE FS 280 LBL 9 AND RBL 9 OUTBOARD CLIPS WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE FS 280, LBL 9 AND RBL 9 OUTBOARD CLIPS IAW BOMBARDIER REO 601R-53-11-638. (M)

Part: FRAME — CRACKED (BS 718)

DURING A C-CHECK IN MCN, THE LEFT FS 718 FRAME REPAIR WAS FOUND TO POSSIBLY BE CRACKED. S/D - MAINTENANCE INSTALLED A NEW 718 DOUBLER AND A NEW REPAIR DOUBLER IAW BOMBARDIER REO601R-53-61-243. (M)

Part: PLACARD — PEELING (CABIN)

DURING A C-CHECK IN MCN, THE EMERGENCY EXIT PLACARD NEAR THE FLIGHT ATTENDANTS SEAT WAS FOUND TO BE PEELING. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT PLACARD NEAR THE FLIGHT ATTENDANTS SEAT. (M)

Part: BPSU — MALFUNCTIONED (T/E FLAP)

FLT 4381 - DURING CRUISE FROM FWA-ATL, AT APPROXIMATELY 28,000 FEET, THE CREW BELIEVED THE AIRCRAFT WAS STRUCK BY LIGHTNING AND THEN SEVERAL MORE TIMES DURING DESCENT FOR APPROACH INTO ATL. UPON APPROACH, THE CREW SELECTED THE FLAPS TO EIGHT DEGREES AND THEN TO TWENTY DEGREES WHICH WAS FOLLOWED BY AN AMBER FLAPS FAIL MESSAGE ON EICAS WITH AN INDICATION OF ZERO DEGREES FLAPS. THE QRH WAS COMPLIED WITH AND AN EMERGENCY WAS ALSO DECLARED. THE AIRCRAFT LANDED SAFELY IN ATL. MAINTENANCE INSPECTED THE AIRCRAFT FOR LIGHTNING STRIKES WITH NO EVIDENCE FOUND. MAINTENANCE ALSO REMOVED AND REPLACED THE RIGHT BRAKE POSITION SENSOR UNIT (BPSU). OPS AND RIG CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: STEP — CRACKED (PAX DOOR)

DURING HANGAR MAINTENANCE IN MCN, THE PASSENGER DOOR TOP STEP WAS FOUND CRACKED AT THE OUTBOARD FORWARD AND AFT CORNERS. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR TOP STEP. OPERATIONAL CHECKS GOOD. (M)

Part: SMOKE — DETECTED (CABIN)

FLT 4355 - DURING APPROACH INTO CVG FROM BNA, AFTER SWITCHING THE BLEEDS FROM THE ENGINES TO THE AUXILIARY POWER UNIT, THE CREW SMELLED AND SAW VISIBLE SIGNS OF SMOKE FOLLOWED BY A LAV SMOKE WARNING MESSAGE. THE AIRCRAFT LANDED SAFELY IN CVG. MAINTENANCE HAD THE FLIGHT CREW RUN THE ENGINES AND PERFORM A FUNCTIONAL CHECK OF THE PACKS. NO DEFECTS WERE NOTED. MAINTENANCE INSPECTED THE LEFT AND RIGHT AIR CYCLE MACHINES FOR OIL, INSPECTED THE DUCTING, AUXILIARY POWER UNIT AND AFT EQUIPMENT BAY FOR INDICATIONS OF SMOKE. NO OIL WAS FOUND AND NO DEFECTS WERE NOTED. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LAMP — BURNED OUT (EMERGENCY LIGHT)

DURING OVERNIGHT SERVICE, THE EMERGENCY LIGHT AT THE PASSENGER DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT LAMP AT THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: TIRE — BLOWN (MLG)

DURING CRUISE, THE CREW WAS ADVISED BY TOWER THE AIRCRAFT MAY HAVE EXPERIENCED A TIRE BLOWING ON THE RT SIDE UPON TAKEOFF. AN EMERGENCY WAS DECLARED AND EMERGENCY VEHICLES WERE REQUESTED TO BE ON STANDBY AS A PRECAUTION. THE AIRCRAFT LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE RT OB TIRE ASSY AS A RESULT OF THE BLOWN TIRE AND ALSO RT IB TIRE ASSY AS REQUIRED. IN ADDITION, MAINTENANCE REPLACED THE RT MAIN GEAR HARNESS ASSY AND SEVERAL RT ENGINE FAN BLADES WHICH WERE DAMAGED FROM TIRE FOD. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE.

Part: HANDLE — STIFF (PAX DOOR)

DURING A GROUND INSPECTION IN DFW, THE PASSENGER DOOR WAS DIFFICULT TO OPEN AND CLOSE. MAINTENANCE ADJUSTED THE PASSENGER DOOR HANDLE LINKAGE. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: HANDLE — BINDING (PAX DOOR)

DURING A GROUND INSPECTION IN DFW, THE PASSENGER DOOR WAS DIFFICULT TO CLOSE. THE DOOR LATCH AND HANDLE WERE VERY STIFF. MAINTENANCE CLEANED AND LUBRICATED THE PASSENGER DOOR HANDLE AND THE LOWER BEARING ASSEMBLY P/N MS21151-8. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: BPSU — MALFUNCTIONED (RT WING TE FLAP)

DURING APPROACH INTO TLH FROM DFW, THE FLAPS FAILED WHEN SELECTED TO TWENTY DEGREES. THE QRH WAS COMPLIED WITH AND EMERGENCY VEHICLES WERE REQUESTED TO BE ON STANDBY AS A PRECAUTION. THE AIRCRAFT LANDED SAFELY IN TLH. MAINTENANCE RE-RIGGED THE RIGHT INBOARD AND OUTBOARD FLAPS AND ALSO REMOVED AND REPLACED THE RIGHT BRAKE POSITION SENSOR UNIT (BPSU). OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: FCU — MALFUNCTIONED (TE FLAPS)

DURING CLIMB-OUT FROM DFW-SHV, AT APPROXIMATELY 14,000 FEET AND 290 KTS THE CREW RECEIVED A FLAPS FAIL MESSAGE. THE QRH WAS COMPLIED WITH AND THE AIRCRAFT RETURNED TO DFW. EMERGENCY VEHICLES WERE REQUESTED AS A PRECAUTIONARY MEASURE. THE AIRCRAFT LANDED SAFELY IN DFW. MAINTENANCE REMOVED AND REPLACED THE FLAPS ELECTRONIC CONTROL UNIT (FECU). OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: DOOR — BINDING (MAIN PAX)

DURING A GROUND INSPECTION, THE PASSENGER DOOR WAS DIFFICULT TO OPEN. MAINTENANCE LUBRICATED THE PASSENGER DOOR. OPERATIONAL CHEKS GOOD. AIRCRAFT OK FOR SERVICE. (ASOA04340)

Part: DOOR — BINDING (MAIN PAX)

DURING A GROUND INSPECTION, THE PASSENGER DOOR WAS DIFFICULT TO OPEN. MAINTENANCE LUBRICATED THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE.

Part: CLIP — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE CLIPS AT FS 484, LBL 28 AND RBL 36 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CLIPS AT FS 484, LBL 28 AND RBL 36 IAW ASA EO 600-53-0098. (M)

Part: CLIP — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE OUTBOARD CLIP AT FS 484, RBL 27 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE OUTBOARD CLIP AND INTERCOSTAL AT FS 484, RBL 27, IAW ASA EO 600-53-0098. (M)

Part: SILL — CRACKED (FUSELAGE)

DURNG A C-CHECK IN MCN, THE CARGO DOOR FLOOR SILL PLATE AT FS 562.72-589 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CARGO DOOR FLOOR SILL PLATE AT FS 562.72-589 IAW ASA EO 600-53-0095. (M)

Part: FLOOR SUPPORT — CRACKED (FUSELAGE)

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

Part: LIGHT — DAMAGED (CABIN)

DURING A C-CHECK IN MCN, THE EMERGENCY FLOOR LEVEL FLOOR LIGHT COVER ON THE AFT WALL BY THE PASSENGER DOOR WAS FOUND DAMAGED. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY FLOOR LEVEL FLOOD LIGHT ASSEMBLY ON THE AFT WALL BY THE PASSENGER DOOR. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LIGHT — DAMAGED (GALLEY)

DURING A C-CHECK IN MCN, THE EMERGENCY EXIT SIGN COVER BY THE SERVICE DOOR WAS FOUND DAMAGED. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT SIGN ASSEMBLY BY THE SERVICE DOOR. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: SKIN PANEL — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE NOSE LANDING GEAR DOOR FUSELAGE SKIN RADIUS AFT AREA LHS AT FS 235 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE NOSE LANDING GEAR DOOR FUSELAGE SKIN RADIUS AFT AREA LHS AT FS 235 IAW ASA EO 600-53-0122. (M)

Part: LIGHT — INOPERATIVE (PAX DOOR)

DURING AN A-CHECK IN MCN, THE EMERGENCY LIGHT ON THE PASSENGER DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT ASSEMBLY ON THE PASSENGER DOOR. OPERATIONAL CEHCKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LAMP — BURNED OUT (EMERGENCY LIGHT)

DURING A GROUND INSPECTION, THE AFT OVERHEAD EMERGENCY CEILING LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT OVERHEAD EMERGENCY CEILING LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

DURING A HANGAR INSPECTION IN BTR, THE SECOND FROM THE FRONT EMERGENCY CEILING LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE SECOND FROM THE FRONT EMERGENCY CEILING LIGHT LAMP. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LIGHT — INOPERATIVE (EXTERIOR)

FLT 4242 - DURING HANGAR INSPECTION IN BTR, THE RIGHT EXTERIOR EMERGENCY LIGHT FORWARD OF THE EMERGENCY EXIT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE RIGHT EXTERIOR EMERGENCY LIGHT LAMP FORWARD OF THE EMERGENCY EXIT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: STEP — CRACKED (PAX DOOR)

DURING A GROUND INSPECTION IN ATL, THE PASSENGER DOOR BOTTOM STEP WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR BOTTOM STEP. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LIGHT — INOPERATIVE (CABIN)

FLT 4681 - DURING A GROUND INSPECTION IN ATL, THE RIGHT SIDE FLOOR EMERENCY LIGHT STRIPS FROM THE SERVICE DOOR TO ROW EIGHT WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE RIGHT SIDE FLOOR EMERGENCY LIGHT STRIPS FROM THE SERVICE DOOR TO ROW EIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: CLIP — CRACKED (FUSELAGE)

DURING HANGAR MAINTENANCE IN SHV, THE FLOORBEAM CLIPS AT BULKHEAD FS 280, LBL AND RBL 9 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE PERFORMED A TEMPORARY REPAIR BY STOP DRILLING THE ENDS OF THE CRACKS OF THE FLOORBEAM CLIPS AT BULKHEAD FS 280, LBL AND RBL 9 IAW ASA EO 600-53-0100. (M)

Part: ELBOW — LEAKING (FUEL LINE)

FLT 4481 - DURING CRUISE FROM LEX-ATL AT APPROX 26,000 FEET, WHEN THE CREW INCREASED THE COCKPIT TEMPERATURE TO 43 DEGREES CELSIUS A FUEL SMELL OCCURRED. THE SMELL DIMINISHED BUT REMAINED NOTICEABLE WHEN THE CREW DECREASED THE TEMPERATURE TO 3 DEGREES CELSIUS. THE AIRCRAFT LANDED SAFELY IN ATL. MAINTENANCE REMOVED AND REPLACED THE AUXILIARY POWER UNIT FUEL LINE ELBOW. OPERATIONAL AND LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: FRAME — CRACKED (FUSELAGE)

DURING HANGER MAINTENANCE, A CRACK WAS DISCOVERED IN FRAME STATION 718 BETWEEN STRINGERS 10 AND 12 ON THE LEFT AND RIGHT SIDES. MAINTENANCE REPAIRED THE CRACKED FRAME IAW SRM.

Part: BEAM — CRACKED (SUPPORT BEAM)

DURING HANGER MAINTENANCE, CRACKS WERE FOUND ON THE ENGINE SUPPORT BEAM AT BL 36.20 ON BOTH SIDES. MAINTENANCE REPAIRED THE CRACKED ENGINE SUPPORT BEAM IAW REO. THIS REO GIVES REPAIR SPECIFICATIONS FOR THE ENGINE SUPPORT BEAM CRACK ON AIRCRAFT AS WELL AS OUTLINES A THRESHOLD OF CYCLES FOR THE PERMANENT REPAIR AND FOLLOW UP NDI INSPECTIONS. AIRCRAFT OK FOR SERVICE.

Part: ENGINE — FAILED (LEFT)

ON APPROACH, DESCENDING THROUGH 9,000 FEET, THE LT ENGINE OIL LOW PRESSURE WARNING LIGHT ILLUMINATED. THE OIL PRESSURE MOMENTARILY FLUCTUATED BACK TO THE GREEN ARC, BUT THEN DROPPED DOWN TO ZERO PSI. THE CAPTAIN COMPLETED THE ENGINE OIL PRESSURE CHECKLIST, WHICH INCLUDES THE SECURING OF THE ENGINE, FOLLOWED BY THE SINGLE ENGINE CHECKLIST. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED SAFELY. MAINTENANCE FOUND THE GEARBOX BOROSCOPE CRANK PAD COVER OFF. AFTER DOWN LOADING THE DIGITAL FLIGHT DATA RECORDER, MAINTENANCE LEARNED THE LEFT ENGINE RAN FOR 2.5 MINUTES WITH NO OIL PRESSURE. MAINTENANCE REMOVED AND REPLACED THE LT ENGINE. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN)

DURING GROUND INSPECTION IN ATL, MAINTENANCE DISCOVERED LEFT OVERWING EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED LEFT OVERWING EMERGENCY LIGHT BULB. OPS CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: WINDSHIELD — CRACKED (COCKPIT)

FLT 4696 - DURING TAXI IN ON FLIGHT FROM ATL TO SWF, CAPTAIN''S SIDE WINDSHIELD CRACKED. MAINTENANCE REMOVED AND REPLACED CAPTAIN''S SIDE WINDSHIELD. OPERATIONAL AND CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: WINDSHIELD — CRACKED (COCKPIT)

FLT 4738 - DURING FLIGHT FROM ATL-ICT, CAPTAIN''S WINDSHIELD CRACKED. MAINTENANCE REMOVED AND REPLACED CAPTAIN''S WINDSHIELD. OPS AND LEAK CHECK WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: LENS — MISSING (EXTERIOR)

OUTSTATION GPT - FLT 4672 - CREW REPORTED THE EXTERIOR EMERGENCY FLOOD LIGHT LENS IS MISSING. AIRCRAFT WAS FERRIED TO ATL FOR REPAIR. ATL MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSY. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RELEASED FOR FURTHER SERVICE. (X)