N839AS

Part: SKIN — CRACKED (FUSELAGE) · airframe 33,947 hrs · 30,967 cycles

CRACK IN SKIN AT LT TRU DOOR AFT LATCH. R & R SKIN IAW SRM 51-40-11, 51-42-06-00, 51-42-10-00 AND REO 601R-53-11-2563, REO 601R-53-11-2572 AND DWG 600-33052. CLASSIFIED A MAJOR REPAIR.

Part: FITTING — CRACKED (LT MLG) · airframe 33,947 hrs · 30,967 cycles

LEFT MLG TRUNNION FITTING HAS TWO LOWER HOLES WITH CRACK INDICATIONS. REPAIRED IAW REO 601R-21-2002.

Part: HINGE — GOUGED (PAX DOOR) · airframe 33,932 hrs · 30,947 cycles

FOUND GOUGE DAMAGE ON DOOR SIDE OF ASD HINGE. BLENDED OUT GOUGE DAMAGE IAW SRM 51-12-00. MAJOR REPAIR.

Part: FITTING — CRACKED (LT WING) · airframe 33,947 hrs · 30,967 cycles

LEFT MLG TRUNNION FITTING HAS TWO LOWER HOLES WITH CRACK INDICATIONS. REPAIRED IAW REO 601R-57-21-2002 IAW NDTM PT6, 53-00-97.

Part: SKIN — DAMAGED (RT WING) · airframe 33,947 hrs · 30,966 cycles

RIGHT WING PLANK HAS TWO OVERSIZED HOLES. REPAIRED IAW REO 601R-57-21-2002 REV.P1.

Part: SKIN — DAMAGED (LT WING) · airframe 33,947 hrs · 30,966 cycles

LEFT WING PLANK HAS ONE OVERSIZED HOLE. REPAIRED IAW REO 601R-52-21-2002, REV P1.

Part: BULKHEAD — CRACKED · airframe 33,932 hrs · 30,947 cycles

REAR PRESSURE BULKHEAD WEB FWD FACE CRACKED ABOVE AFT CARGO DOOR TRACK AREA IS MARKED. COMPLIED WITH REO 601R-53-61-1541, REV D, DATED OCT 31, 2011 IAW NDTM PART 1 51-20-06 FOR BULKHEAD WEB.

Part: SIGN — INOPERATIVE (CABIN) · airframe 33,932 hrs · 30,947 cycles

SERVICE DOOR FAILED FUNCTIONAL TEST OF THE EXIT SIGN BETA LIGHT. REMOVED AND INSTALLED SERVICEABLE EXIT SIGN BETA LIGHT ON SERVICE DOOR IAW AMM 33-61-09-000-802, 33-51-09-400-802. FUNCTIONAL TEST GOOD OF SERVICE DOOR EXIT SIGN BETA LIGHT REF AMM TASK 33-51-09-720-801.

Part: FLOOR SUPPORT — CORRODED (BS 349-364) · airframe 33,947 hrs · 30,966 cycles

LT CABIN FLOOR SUPPORT CORRODED BS 349 TO 364. REPAIRED IAW SRM 51-21-06-00 AND REO 601R-53-00-530. MAJOR REPAIR.

Part: LIGHT — FAILED (CABIN) · airframe 33,932 hrs · 30,947 cycles

PAX DOOR FAILED FUNCTIONAL TEST OF THE EXIT SIGN BETA LIGHT. REMOVED AND INSTALLED SERVICEABLE BETA LIGHT EXIT SIGN ON PAX DOOR IAW AMM 33-51-09-000-801, 33-51-09-400-801.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 33,932 hrs · 30,947 cycles

ON LBL9 OTBD ANGLE CRACKED ON BS 280 FLOORBEAM, REMOVED CRACKED ANGLE IAW SRM 51-42-21-00. COMPLIED WITH REO 601R-53-11-926, REV B. IAW NDTM PART 1, 51-20-06. INSTALLED NEW ANGLE IAW SRM 51-42-21-00. COMPLIED WITH EC/TC REO 601R-53-11-926 01.

Part: FLOOR SUPPORT — CORRODED (BS 310-319) · airframe 33,932 hrs · 30,947 cycles

CORROSION ON FLOOR SUPPORT AROUND NUT PLATES AT RBL 45 FS 310 TO 319. REMOVED CORROSION IAW SRM 51-21-06-00. COMPLIED WITH REO 601R-53-00-530.

Part: HINGE — GOUGED (PAX DOOR) · airframe 33,932 hrs · 30,947 cycles

PASSENGER DOOR HINGE ON FUSELAGE HAS SEVERAL NICKS AND GOUGED. BLENDED OUT NICKS AND GOUGES ON PAX DOOR HINGE FUSELAGE SIDE AND ADDITIONAL GOUGE DAMAGE ON DOOR HINGE SIDE IAW SRM 51-12-00. RECEIVED AND COMPLIED WITH REO 601R-53-21-2464. MAJOR REPAIR

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 33,932 hrs · 30,947 cycles

CORROSION ON FLOOR SUPPORT. REMOVED FLOOR SUPPORT IAW SRM 51-42-06-01 AND INSTALLED IAW SRM 51-42-06 AND DWG 601R 31527. MAJOR REPAIR.

Part: CROSSBEAM — CORRODED (BS 349) · airframe 33,947 hrs · 30,966 cycles

CORROSION ON END OF CROSSBEAM AT BS 349.00, RBL 45. REMOVED CORROSION IAW SRM 51-21-06-00.

Part: BRACKET — CORRODED (FLOOR SUPPORT) · airframe 33,932 hrs · 30,947 cycles

CORROSION ON FLOOR SUPPORT. REMOVED FLOOR SUPPORT BRACKET IAW SRM 51-42-06-01. INSTALLED BRACKET IAW SRM 51-42-06, SRM 51-40-11 AND DWG 601R 31527. MAJOR REPAIR.

Part: FRAME — CORRODED (BS 394) · airframe 33,947 hrs · 30,966 cycles

FS 394 CORRODED ON FWD FACE APPROX RBL 3. REMOVED CORROSION IAW SRM 51-21-06.

Part: SEAT TRACK — DAMAGED (COCKPIT) · airframe 33,932 hrs · 30,947 cycles

SEAT TRACK HOLES ELONGATED. REMOVED INBD SEAT TRACK IAW SB601R-53-22, PART A. REWORKED SEAT TRACK FIG 1(1)(A)-(R). SEAT TRACK REMOVED IAW SB 60R-12-022, FIG 1 (1A) THRU (R AND INSTALLED IAW SB 601R-53-022. MAJOR REPAIR.

Part: SKIN — CRACKED (FUSELAGE) · airframe 33,947 hrs · 30,967 cycles

FOUND CRACK IN SKIN AT LT TRU DOOR AFT LATCH. R & R SKIN IAW SRM 51-42-06.

Part: SKIN — CRACKED (RT WING) · airframe 32,225 hrs · 29,198 cycles

CRACK .325" LONG FOUND AND CONFIRMED IAW HFEC INSPECTION AT RT WING BOTTOM AT WS 148.19. REPAIRED IAW EC/TC REO 601R-57-21-130 01 AND REO 601R-57-21-130, REV J.

Part: SKIN — CRACKED (RT WING) · airframe 32,225 hrs · 29,198 cycles

CRACK .325 LONG FOUND AND CONFIRMED IAW HFEC INSPECTION AT RT WING BOTTOM AT WS 148.19. STOP DRILLED CRACK TO .250" IAW REO 601R-57-21-138, REV A.

Part: LIGHT — UNKNOWN (CABIN) · airframe 32,157 hrs · 29,128 cycles

EMERGENCY LIGHTS WILL NOT TEST. DISCREPANCY NO LONGER EXISTS. IAW MCC, NO FURTHER ACTION IS REQUIRED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,084 hrs · 29,054 cycles

LEFT EMERGENCY LIGHT INOPERATIVE. R & R LT WING EMERGENCY LIGHT IAW AMM 33-51-21. OPS CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 30,494 hrs · 27,291 cycles

F/O FLASHLIGHT INOPERATIVE. R & R F/O FLASHLIGHT IAW AMM 25-61-02 CHECKED GOOD.

Part: LIGHT — MISWIRED (CABIN) · airframe 30,068 hrs · 26,827 cycles

LOWER OTBD EMERGENCY LIGHT ON F/A STATION DOES NOT WORK. FOUND WIRES SWAPPED BETWEEN EMERGENCY LIGHT DS9LY AND DS10LY PUT INPUT WIRES BACK TO THEIR CORRECT LOCATION IAW WDM 33-51-00. OPS TESTED GOOD.

Part: SEAT TRACK — CORRODED (BS 574) · airframe 30,053 hrs · 26,809 cycles

SEAT TRACK CORRODED. TRIMMED, FITTED AND INSRALLED SEAT TRACK IAW SRM 51-40-11 AND AMM 53-01-11-400-802 AT FS 574, RBL9.

Part: PRESSURE BLKHD — CRACKED · airframe 30,053 hrs · 26,809 cycles

REAR PRESSURE BULKHEAD FWD FACE IS CRACKED ABOVE LENTEL ATTACH POINT AREA. REPAIRED IAW REO 601R-53-61-1230 AND GREO 601R-53-61-1230 REV E.

Part: FLOORBEAM — CORRODED · airframe 30,053 hrs · 26,809 cycles

FLOORBEAM JUST AFT OF SERVICE DOOR CORRODED. HAND SANDED MINOR SURFACE CORROSION. REMOVED .001 OUT .053 THK IAW SRM 51-21-06 AND RESTORED FINISH IAW SRM 51-21-16. R & R FLOORBEAM ANGLE IAW SRM 51-42-21. REPAIR IS CLASSIFIED AS MINOR.

Part: SKIN — DENTED (BS 589 S21-22L) · airframe 30,062 hrs · 26,820 cycles

DENTS BELOW CARGO DOOR AT FS 589 S21-22L. INSTALLED REPAIR DOUBLER. SEALED, PAINTED & APPLIES CORROSION INHIBITER IAW SRM 53-00-31.

Part: FLOOR PANEL — CORRODED (BS 424-559) · airframe 30,053 hrs · 26,809 cycles

CORROSION FOUND AT PRESSURE FLOOR LT LBL 36, STR 17 OVERWING EXIT AND AFT AT FOLLOWING FS 424-559. REPAIRED IAW REO 601R-53-41-666.

Part: BRACKET — CORRODED (DOOR SILL) · airframe 30,053 hrs · 26,809 cycles

SURFACE CORROSION FOUND AT SERVICE DOOR SILL FRAME BRACKETS AT FS 320.0, 345.0 AND 348.0. REMOVED CORROSION AT SERVICE DOOR SILL FRAMES BRACKET IAW SRM 51-21-6. PERFORMED UT THICKNESS INSP OF BLEND AREA IAW MAC NDT INSP PROCEDURE UT-3 MIN MATERIAL REMAINING ON ANGLE IS .057". DRILLED NEW BRACKET AND INSTALLED IAW SRM 51-42-21.

Part: STIFFENER — CRACKED (BS 409) · airframe 30,053 hrs · 26,809 cycles

POSSIBLE CRACK ON STIFFENER LBL18.00 AT FS409.00+128 INDICATION IS AT THE VERY BOTTOM ON THE OTBD. COMPLY WITH EC/TC REO 601R-53-41-056. RT 161728 09/23/11 (LT) COMPLIED WITH EC/TC REO 601R-53-41-056 IAW REO 601R-53-51-056, REV-E. RII FOUND TO BE SATISFACTORY. (SDR CLOSED)

Part: PRESSURE BLKHD — CRACKED (FUSELAGE) · airframe 30,053 hrs · 26,809 cycles

REAR PRESSURE BULKHEAD FWD FACE IS CRACKED ABOVE LINTEL ATTACH POINT. REPAIRED IAW REO 601R-53-61-1230 AND REO 601R-53-61-4218.

Part: WEB — CORRODED (BS 585-605) · airframe 30,053 hrs · 26,809 cycles

WEB ON OTBD SIDE OF LBL 27 CORRODED BETWEEN FS 585-605. BLENDED IAW 51-12-00 AND FOUND TO BE OUT LIMITS IAW 53-00-00. REMOVED AND REPLACED WEB IAW SRM 51-40-06, 51-40-11, 51-42-06 AND SRM 51-42-21.

Part: LIGHT — CRACKED (CABIN) · airframe 30,053 hrs · 26,809 cycles

LEFT AISLE EMERGENCY EXIT LIGHT ASSY CRACKED. REMOVED AND REPLACED IAW AMM 33-51-01-01, REV A 161954 10-7-11.

Part: PRESSURE DECK — CORRODED (BS 424-559) · airframe 30,053 hrs · 26,809 cycles

CORROSION FOUND AT PRESSURE FLOOR FS 424-559 LBL 36, STR 17. REMOVED COSSOSION IAW SRM 51-21-06. PERFORMED UT THICKNESS INSPECTION IAW MAC NDT INSP PROCEDURE UT-3 MIN. MATERIAL REMAINING IS .071" WITHIN ALLOWABLE LIMITS OF REO 601R-53-41-666.

Part: PRESSURE BLKHD — CRACKED · airframe 30,053 hrs · 26,809 cycles

REAR PRESSURE BULKHEAD HAS A CRACK ABOVE LINTEL. REPAIRED.

Part: STIFFENER — CRACKED (BS 409) · airframe 30,053 hrs · 26,809 cycles

POSSIBLE CRACK ON STIFFENER, LBL 18.00 AT FS 409.00+128 INDICATION IS AT THE VERY BOTTOM ON THE OTBD. PERFORMED EDDY CURRENT INSPECTION IAW MAC NDT INSP PROCEDURE ET-2. STIFFENER CONFIRMED CRACKED AT BOTTOM, AFT, OTBD END OF POST. REPAIRED IAW REO 601R-53-41-056.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 30,053 hrs · 26,809 cycles

REAR PRESSURE BULKHEAD FWD FACE IS CRACKED ABOVE LINTEL ATTACH POINT AREA. REPAIRED IAW 601R-53-61-1230.

Part: SKIN — CORRODED (BS 559 S14A-15AL) · airframe 30,053 hrs · 26,809 cycles

LEFT EXTERIOR SKIN PANEL AT FS 559.00 + 64 AND BETWEEN STR 14A AND 15A HAS CORROSION. REMOVED CORROSION IAW SRM 51-21-06. TREATED, PRIMED AND PAINTED REPAIR AREA IAW SRM 51-21-11.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 30,053 hrs · 26,809 cycles

SEAT TRACK CORRODED. CORROSION REMOVAL WITHIN LIMITS IAW SRM 53-61-49.

Part: ISOLATOR — CRACKED (BULKHEAD) · airframe 30,053 hrs · 26,809 cycles

CARGO COMPARTMENT AFT PRESSURE BULKHEAD MOUNTING ISOLATOR CRACKED. R & R CRACKED ISOLATOR IAW SRM 51-40-11. MINOR REPAIR.

Part: FLOORBEAM — CORRODED · airframe 30,053 hrs · 26,809 cycles

FLOORBEAM CORRODED. REMOVED FLOORBEAM CAP IAW SRM 51-42-21. DRILL AND INSTALL NEW CAP IAW SRM 51-42-06 AND REO 601R-53-61-3778.

Part: SUPPORT BRACKET — CRACKED (WINDSHIELD) · airframe 30,053 hrs · 26,809 cycles

RT WINDSHIELD SIDE POST LOWER OTBD SUPPORT BRACKET CRACKED. REMOVED OLD SUPPORT BRACKET. LOCATED, DRILLED AND INSTALLED NEW SUPPORT BRACKET IAW SRM 51-42-21.

Part: PLACARD — MISSING (COCKPIT) · airframe 30,053 hrs · 26,809 cycles

COCKPIT EMERGENCY EXIT MISSING PLACARD. R & R PLACARD IAW AMM'S 11-20-00-000-801 & 11-10-03-400-801.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 29,803 hrs · 26,536 cycles

COPILOT FLASHLIGHT DOES NOT WORK. R & R F/O'S FLASHLIGHT IAW AMM 25-60-01.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 29,129 hrs · 25,799 cycles

CABIN CEILING EMERGENCY LIGHT 3 FROM FRONT INOP. RELAMPED CABIN CEILING EMERGENCY LIGHT 3RD FROM THE FRONT IAW CMM 33-22-89. OPS CK GOOD. RELAMPED CABIN CEILING EMERGENCY LIGHT 3RD FROM THE FRONT IAW CMM 33-22-89. OPS CHK GOOD.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 29,038 hrs · 25,697 cycles

EMERGENCY LIGHT COVER AT PX BOARDING DOOR IS MIISSING. REPLACED EMERGENCY LIGHT COVER AND PLACARD. OPS CHECK GOOD. (CLOSED)

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 28,856 hrs · 25,476 cycles

EMERGENCY LIGHT AT MAIN PAX DOOR ENTRANCE MISSING COVER. REPLACE MISSING EMERGENCY COVER AT MAIN DOOR ENTRANCE. REF AMM 33-51-19. (CLOSED)

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 28,817 hrs · 25,428 cycles

CAPT'S FLASHLIGHT IS BROKE. R & R CAPT'S PORTABLE FLASHLIGHT IAW AMM 25-61-00. OP'S CHECKED GOOD. R & R CAPT'S PORTABLE FLASHLIGHT IAW AMM 25-61-00. OP'S CHECKED GOOD.

Part: STEERING UNIT — FAILED (NLG) · airframe 28,743 hrs · 25,340 cycles

"STEERING INOP" CAUTION MESSAGE IN FLIGHT. RAN QRH BUT WAS UNABLE TO RESET OR EXTINGUISH MSG. (EMERGENCY DECLARED) R & R ECU IAW AMM 32-51-10. OPS CHECK GOOD.

Part: PDU — UNSERVICEABLE (TE FLAPS) · airframe 28,399 hrs · 24,919 cycles

FLAPS FAIL CAUTION MSG ON APPROACH AT 22 DEG (EMERGENCY DECLARED -- EMERGENCY VEHICLES WERE STANDING BY AS A PRECAUTION) COMPLIED WITH AD 2009-06-12. ACFT RETURNED TO SERVICE. CLEARED, PLACARD REMOVED. R & R FLAP PDU IAW AMM 27-52-01,OPS CK GOOD. (CLOSED)

Part: LIGHT — BROKEN (CABIN) · airframe 28,267 hrs · 24,774 cycles

F/A WARDROBE EMERGENCY LIGHT BASE BROKEN. REPLACED EMERGENCY LIGHT BASE IAW AMM 25-61-02 , OPS CHECK GOOD.

Part: DOOR — LACK OF LUBE (SERVICE) · airframe 27,242 hrs · 23,564 cycles

SERVICE DOOR COULD NOT BE OPENED FROM OUTSIDE HANDLE, JAMS HALF-WAY THROUGH TRAVEL. LUBED OUTER HANDLE IAW AMM 52-40-01. OPS GOOD.

Part: ANCHOR FITTING — OUT OF ADJUST (PAX DOOR) · airframe 27,010 hrs · 23,300 cycles

PAX DOOR HARD TO OPEN THEN MADE POPPING SOUNDS WHEN FINALLY OPENED. ADJUSTED PAX DOOR AFT ANCHOR FITTING IAW AMM 52-11-00.

Part: PRESSURE VALVE — OUT OF ADJUST (PAX DOOR) · airframe 26,976 hrs · 23,259 cycles

PAX DOOR HANDLE DIFFICULT TO OPEN. ADJUSTED AND TESTED PAX DOOR PRESSURE VALVE IAW AMM 52-11-15 OPS CK NORMAL.

Part: DOOR — STUCK (MAIN PAX) · airframe 26,931 hrs · 23,209 cycles

UPON REACHING GATE MAIN PAX DOOR WOULD NOT OPEN. AFTER SEVERAL ATTEMPS WE WERE ABLE TO OPEN DOOR. LUBE PAX DOOR HANDLE TRACKS, OPS CHECK GOOD, OK FOR SERVICE IAW AMM 52-10-00.

Part: CYLINDER — OUT OF RIG (MAIN PAX DOOR) · airframe 26,931 hrs · 23,209 cycles

CREW REPORTED PAX DOOR HARD TO OPEN. TROUBLESHOT PAX DOOR FOUND FWD GAS SPRING OUT OF RIG AND SUPPORT WHEEL DRAGGING ON DOOR FRAME. RIGGED PAX DOOR FWD GAS SPRING AND SUPPORT WHEEL IAW AMM 52-11-17 AND 52-11-13.

Part: DOOR — STUCK (MAIN PAX) · airframe 26,867 hrs · 23,130 cycles

F/A HAD TROUBLE OPENING PAX DOOR FROME INSIDE ACFT, SAYS HANDLE ONLY MOVES ABOUT HALFWAY. OPS CHECK GOOD IAW AMM 52-10-01.

Part: DOOR — STIFF (MAIN PAX) · airframe 26,842 hrs · 23,101 cycles

R & R PAX DOOR ASSY IAS AMM OF CHECK GOOD 52-11-03. (CLOSED)

Part: DOOR — STIFF (MAIN PAX) · airframe 26,842 hrs · 23,101 cycles

MAIN PASSENGER DOOR HANDLE DIFFICULT TO OPEN. REPEAT WRITE-UP.

Part: DOOR — STUCK (MAIN PAX) · airframe 26,800 hrs · 23,053 cycles

F/A REPORTS DIFFICULTY OPENING PAX DOOR.

Part: DOOR — STUCK (MAIN PAX) · airframe 26,771 hrs · 23,016 cycles

PAX CABIN DOOR WILL NOT OPEN FROM INSIDE. LEVER WILL ONLY RAISE 1/3 OF THE NORMAL TRAVEL. DOOR HAD TO BE OPEN FROM OUTSIDE TWICE.

Part: DOOR — STICKING (MAIN PAX) · airframe 26,756 hrs · 23,000 cycles

MAIN PAX DOOR STICKING DURING OPEN/CLOSING NOT OPERATING 1ST ATTEMPT.

Part: DOOR — STICKS (PAX DOOR) · airframe 26,742 hrs · 22,982 cycles

PASSENGER DOOR STICKS IN CLOSED POSITION.

Part: HANDLE — BINDING (PAX DOOR) · airframe 26,666 hrs · 22,898 cycles

F/A SAYS PAX DOOR INNER HANDLE IS DIFFICULT TO OPERATE WHEN OPENING THE DOOR.

Part: DOOR — BINDING (PAX DOOR) · airframe 26,666 hrs · 22,898 cycles

PASSENGER DOOR HARD TO OPEN FROM INSIDE.

Part: SEAT TRACK — CORRODED (BS 409) · airframe 26,545 hrs · 22,770 cycles

LEFT SEAT TRACKS (2 SECTIONS) FORWARD OF THE F.S. 409 ARE CORRODED. REMOVED AND REPLACED SEAT RAIL ON LEFT HAND SIDE AND INSTALLED LT SIDE SEAT TRACK AT FS 409+18.02 IAW AMM 53-07-11-04.

Part: SEAT TRACK — CORRODED (BS 409) · airframe 26,545 hrs · 22,770 cycles

RIGHT SEAT TRACKS (2 SECTIONS) FORWARD OF THE FS 409 CORRODED. REMOVED AND REPLACED NEW SEAT RAIL ON RIGHT SIDE AND INSTALLED RT SIDE SEAT TRACK AT FS 409+18.02 IAW AMM 53-01-11-04.

Part: FRAME — CORRODED (BS 319 S23L/R) · airframe 26,545 hrs · 22,770 cycles

FS319.00 BETWEEN ST23L AND 23R HAS CORROSION ON FWD AND AFT SIDES. REMOVED AND REPLACED DAMAGED FRAME SECTION AFT FS 319 BETWEEN STGR 23L AND 23RT. ALL WORK PERFORMED IAW SRM 53-21-15.

Part: STRUCTURE — CORRODED (BS 349) · airframe 26,545 hrs · 22,770 cycles

FS 349.00 FRAME BETWEEN ST23L AND 23R HAS CORROSION ON FWD AND AFT SIDES. REMOVED AND REPLACED IAW SRM 51-42-06.

Part: FRAME — CORRODED (BS 333) · airframe 26,545 hrs · 22,770 cycles

FS 333.00 BETWEEN ST23L AND 23R HAS CORROSION ON FWD AND AFT SIDES. REMOVED AND REPLACED DAMAGED FRAME SECTION AT FS 333 STGR 23L AND 23 RT. ALL WORK PERFORMED IAW SRM 53-21-15.

Part: CHANNEL — CRACKED (BS 409) · airframe 26,545 hrs · 22,770 cycles

AT FS 409+128 THE VERTICAL INBD U CHANNEL AT RBL 27 IS CRACKED IN THE AFT LOWER RADIUS AT EDGE. FABRICATED REPAIR ANGLE (-2) IN ANNEALED CONDITION IAW REO 601R-53-41-056. HEAT TREATED REPAIR ANGLE PER SRM 51-24-06. REMOVED FASTENERS IN REPAIR AREA PER REO 601R-53-41-056. TRIMED OUT CRACKED PORTION OF STIFFENER PER REO 601R-53-41-056. PERFORMED ET INSPECTION OF CUT LINE AT FS 409.00 + 128 , RBL27 IAW REO 601R-53-41-056 PER NDTM 51-20-06 NO DEFECTS NOTED. INSTALLED REPAIR ITEMS -2 AND -4 PER STEPS 7, 9, 10, 11 AND 12 OF REO 601R-53-41-056. APPLIED A023 PROTECTIVE COATING AND FILLET SEALED PER STEPS 8,AND 14 OF REO 601R-53-41-056.

Part: CHANNEL — CRACKED (BS 409) · airframe 26,545 hrs · 22,770 cycles

AT FS 409+128 THE INBD AND OTBD VERTICAL U CHANNELS AT BL 0 UPPER AFT REINFORCEMENT L ANGLES ARE CRACKED IN RADIUS. REMOVED AND REPLACED L ANGLES ON 409+128 INBD & OTBD POST BLO UPPER SIDE IAW SRM CH 51-42-06.

Part: CHANNEL — CRACKED (BS 409) · airframe 26,545 hrs · 22,770 cycles

AT FS 409+128 THE VERTICAL OTBD U CHANNEL AT RBL 18 IS CRACKED IN THE AFT LWR RADIUS AT EDGE. REPAIRED VERTICAL U CHANNEL AT FS 409+128 RBL18 IAW REO 601R-53-41-056.

Part: FRAME — CRACKED (BS 559) · airframe 26,545 hrs · 22,770 cycles

FRAME CAP ANGLE CRACKED IN RADIUS AT FS 559.00, LBL18. COMPLIED WITH N/R-00274. REPAIRED ON E/C REO 601R-53-41-260 W/O 132389.

Part: FLOORBEAM — CORRODED (BS 621) · airframe 26,545 hrs · 22,770 cycles

FLOORBEAM STRUCTURE AT FS621.0 AND BETWEEN LBL9.00 AND LBL 27.00 HAS CORROSION IN AREA OF NUTPLATES. BLENDED CORRODED AREA IAW SRM 51-12-00. DAMAGED AREA WAS FOUND TO BE .007 DEEP WITHIN ALLOWABLE DAMAGED LIMITS IAW SRM 53-61-43 AND 53-00-00 RESTORED FINISH AND REMOVED AND REPLACED N/P'S IAW SRM 51-21-00 AND 51-45-00.

Part: LIGHT — DAMAGED (CABIN) · airframe 26,545 hrs · 22,770 cycles

FLOOR EMERGENCY FLOOR TRACK LIGHT IS DAMAGED. REPAIRED IAW EO 600-33-0015.

Part: SKIN — CRACKED (LT WING) · airframe 26,545 hrs · 22,770 cycles

LT WING PLANK IS CRACKED AT THE AFT SPAR ON WS 148.019. REPAIRED LT WING PLANK AT THE AFT SPAR IAW EC/TC 600-57-134 C/W LK CK GOOD IAW CRJ 200 AMM 28-11-00.

Part: SIGN — CRACKED (EMERGENCY LIGHTS) · airframe 26,545 hrs · 22,770 cycles

EXIT PLASTIC SIGN ON FWD CABIN CEILING PANEL CRACKED. REMOVED AND REPLACED NEW EXIT PLASTIC SIGN ON FWD CABIN CEILING PANEL IAW AMM 33-51-14-04

Part: FRAME — CRACKED (BS 718) · airframe 26,545 hrs · 22,770 cycles

RT FS718.00 FRAME CRACKED BETWEEN STRINGERS 10 AND 11. REPAIRED BOTH LT & RT 718.00 FRAME PER S/B 601R-53-055.

Part: DOOR — BINDS (PAX DOOR) · airframe 26,429 hrs · 22,648 cycles

PAX DOOR DIFFICULT TO OPEN.

Part: DOOR — STUCK (MAIN PAX) · airframe 26,545 hrs · 22,770 cycles

UPON GATE RETURN PAX DOOR WOULD NOT OPEN. REPEAT WRITEUP.

Part: DOOR — BINDS (PAX DOOR) · airframe 26,429 hrs · 22,648 cycles

MAIN PAX DOOR DIFFICULT TO OPEN FROM INSIDE.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 25,616 hrs · 21,812 cycles

GEAR DISAGREE (NOSE GEAR DOWN) MSG IN FLT WITH NW STRNG INOP MSG. RETURNED TO ATL. NORMAL LANDING. RESET NWS, TAXIED TO GATE. EMERGENCY DECLARED.

Part: INTERCOSTAL — CRACKED (LT WING) · airframe 25,600 hrs · 21,800 cycles

INTERCOSTAL AT WS 130 ON LT WING HAS A CRACK.

Part: FLAP SYSTEM — FAILED (TE FLAPS) · airframe 25,229 hrs · 21,450 cycles

FLAPS FAIL AT ZERO ON TURN TO FINAL.

Part: DOOR — BINDS (PAX DOOR) · airframe 25,181 hrs · 21,406 cycles

PAX WILL NOT CLOSE. PAX DOOR POWER ASSIST SYSTEM.

Part: DOOR — STUCK (PAX DOOR) · airframe 24,560 hrs · 20,851 cycles

UNABLE TO OPEN PAX DOOR FROM OUTSIDE. -REPEAT-

Part: DOOR — STUCK (PAX DOOR) · airframe 24,560 hrs · 20,851 cycles

PAX DOOR STUCK CLOSED, WILL NOT OPEN FROM OUTSIDE.

Part: A/C PACK — SEIZED (RIGHT) · airframe 24,157 hrs · 20,493 cycles

AFTER LANDING DURING TAXI IN HAD A RT PACK HIGH TEMP CAUTION MESSAGE (FROM DEFECT 423741-1; STRONG SMELL IN CABIN AFTER TAKEOFF. SMELL RESEMBLED SMOKE AND STARTED DISSIPATING. CHECKED ALL SYSTEMS AND RETURNED FOR PRECAUTIONARY OVERWEIGHT LANDING. (AIR RETURN-RELATED TO DEFECT REPORT 423714-1). T/S FOUND RT PACK FROZEN. REMOVED AND REPLACED RT ACM IAW CRJ200 MM 21-51-10. OPS AND LEAK CHECK GOOD. (S)

Part: FLAP SYSTEM — FAILED (TE FLAPS) · airframe 23,217 hrs · 19,641 cycles

FLAP FAIL MSG WHEN SELECTING 8. FLAPS FAILED AT ZERO, EMERGENCY DECLARED, FLT 4218 CX.

Part: FLAP SYSTEM — FAILED (TE FLAPS) · airframe 23,196 hrs · 19,625 cycles

FLAPS FAIL AT ZERO DEGREE'S, FLT 4709 CX, FLT 4472 DEL 19 MINS.

Part: DOOR — UNKNOWN (MAIN PAX) · airframe 23,196 hrs · 19,625 cycles

PAX DOOR WILL NOT CLOSE PROPERLY.

Part: WARNING MESSAGE — ILLUMINATED (THRUST REVERSERS) · airframe 22,482 hrs · 19,015 cycles

R THRUST REVERSER UNLOCK MESSAGE IN FLIGHT EMER STOW BUTTON WAS USED, NO INDICATION CHANGE TOOK PLACE. EN ROUTE TO ATL A/C DIVERTED TO CVG DUE TO MTC. EMERGENCY DECLARED. THRUST REVERSER SYSTEMS.

Part: HANDLE — STICKS (PAX DOOR) · airframe 22,201 hrs · 18,774 cycles

MAIN CABIN DOOR DIFFICULT TO OPEN AND CLOSE, MAIN DOOR HANDLE IS STICKING.

Part: DOOR — STUCK · airframe 22,201 hrs · 18,774 cycles

MAIN ASD JAMMED SHUT.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 22,174 hrs · 18,753 cycles

LEFT BONDED SKIN DOUBLER AT 640 FRAME CRACKED.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 22,174 hrs · 18,753 cycles

ANGLE IS CRACKED AT FS 484 O/B OF RBL 27.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 22,174 hrs · 18,753 cycles

ANGLE IS CRACKED AT FS 484 O/B OF LBL 9.

Part: CONNECTOR — MISSING (CABIN) · airframe 22,174 hrs · 18,753 cycles

FLOOR EMERGENCY LIGHT BULLET CONNECTOR MISSING AT SERVICE DOOR ENTRY POSITION.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 22,174 hrs · 18,753 cycles

ANGLE IS CRACKED AT FS 484 O/B OF RBL 9.

Part: DOOR FRAME — CRACKED (PAX DOOR) · airframe 22,174 hrs · 18,753 cycles

PAX DOOR INNER FWD FRAME FS 320.10 IS CRACKED AT LOWER END. REMOVED REQUIRED FASTENERS FROM INNER SKIN & FS 338.00 FRAME IAW REO 601R-52-11-402 CUT AWAY DESIGNATED PORTION OF INNER SKIN IAW REO 601R-52-11-402. COMPLETED STEPS 1 & 2 OF RE0 601R-52-11-402. CUTLIINES REQUIRE LPI 13374 8-16-07. PERFORMED LPI ON PAX DOOR INNER FRAME REPAIR CUTLINES IAW REO 601R-52-11-402 AND NDTM 51-20-08. NO DEFECTS NOTED. TOUCHED UP CUTLINES IAW REO601R-52-11-402.OK TO INSTALL REPAIR ITEMS. INSTALL REPAIR ITEMS IAW REO601R-52-11-402 13374 8-21-07 .

Part: FITTING — CORRODED (HORIZ STAB) · airframe 22,174 hrs · 18,753 cycles

HORIZONTAL STAB ANTI-ROTATION FITTING CORRODED.

Part: PLACARD — MISSING (EMERGENCY EXIT) · airframe 22,174 hrs · 18,753 cycles

CREW ESCAPE HATCH MISSING EMERGENCY EXIT PUSH RELEASE TURN HANDLE TO OPEN PUSH EXIT IN PLACARD.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 22,174 hrs · 18,753 cycles

ANGLE IS CRACKED AT FS 484 O/B OF LBL 27.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 22,174 hrs · 18,753 cycles

ANGLE IS CRACKED AT FS 484 O/B OF RBL 27.

Part: CONNECTOR — MISSING (CABIN) · airframe 22,174 hrs · 18,753 cycles

FLOOR EMERGENCY LIGHT BULLET CONNECTOR MISSING AT AFT RIGHT OVERWING EXIT.

Part: DOOR FRAME — CRACKED (PAX DOOR) · airframe 22,174 hrs · 18,753 cycles

PAX DOOR INNER AFT FRAME FS 338.00 IS CRACKED AT LOWER END. REPAIRED IAW REO 601R-52-11-402.

Part: SKIN — CRACKED (FUSELAGE) · airframe 22,174 hrs · 18,753 cycles

RIGHT SIDE OF NLG DOOR CUTOUT HAS CRACK IN FUSLELAGE SKIN PROTRUDING OUT OF RIGHT RADIUS. REPAIRED RT FUSELAGE SKIN RADIUS AT FS 235 IAW BOMBARDIER REO 601R-53-11-048

Part: ATTACH BRACKET — CRACKED (RT WING) · airframe 22,174 hrs · 18,753 cycles

RIGHT WING I/B LEADING EDGE O/B ATTACH BRACKET CRACKED. REMOVED RIGHT WING I/B LEADING EDGE O/B ATTACH BRACKET. OK TO INSTALL SERVICEABLE RT WING I/B LEADING EDGE O/B ATTACH BRACKET P/N 600-12025-8. INSTALLED SERVICEABLE RT WING I/B LEADING EDGE O/B ATTACH BRACKET P/N 600-12025-8 IAW CRJ 200 AMM SECTION 20-21-0. SUPPLEMENTAL - SDR CLOSED 08/22/07.

Part: SKIN — CRACKED (FUSELAGE) · airframe 22,174 hrs · 18,753 cycles

LEFT SIDE OF NLG AFT DOOR CUTOUT HAS CRACK IN FUSELAGE SKIN PROTRUDING OUT OF LEFT RADIUS. 08-30-07 REPAIRED IAW REO 601R-53-11-048.

Part: DOOR — OPEN · airframe 21,744 hrs · 18,425 cycles

SERVICE DOOR OPENED WHILE AIRPLANE PARTIALLY PERSSURIZED. SERVICE DOOR WILL NOT CLOSE.

Part: ECU — OUT OF RIG (NLG STEERING) · airframe 21,508 hrs · 18,242 cycles

DURING CRUISE RECEIVED NOSEWHEEL STEERING INOP MSG ON EICAS FOLLOWED QRH BUT MSG DID NOT GO OUT WHEN NLG STEERING SWITCH RETURNED TO ARMED POS TURNED NLG STEERING BACK OFF AS PER QRH AND COORDINATED WITH MX AND FLT CONTROL TO RTB {A/C RETURNED TO ATL AFTER T/O} (EMERGENCY DECLARED} RERIGGED NOSE WHEEL STEERING ECU IAW CRJ 200 AMM 32-51-00 AND CRJ 200 AMM 32-51-20 OPS CHK GOOD. {SDR -CLOSED}

Part: STEERING SYS — MALFUNCTIONED (NLG) · airframe 21,469 hrs · 18,207 cycles

IN FLIGHT NOSE WHEEL STEERING INOP CAUTION MESSAGE. COMPLIED WITH QRH. CAUTION MESSAGE PERSISTED. LANDED WITH NOSE WHEEL STEERING INOP. EMERGENCY DECLARED.

Part: PUMP — FAILED (NR 2 HYD) · airframe 21,279 hrs · 18,059 cycles

NR 2 HYD ENGINE PUMP FAILED ON CLIMBOUT OF ATL, LOST NR 2 QUANTITY. A/C RETURNED TO ATL AFTER T/O. EMERGENCY EQUIPMENT AS PRECAUTION. FLTS 4178, 4654, 4217, 4744 CX.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 21,242 hrs · 18,028 cycles

F/O'S FLASHLIGHT INOP.

Part: SUPPORT BEAM — CRACKED (DOOR TRACK) · airframe 20,352 hrs · 17,363 cycles

CARGO DOOR TRACK SUPPORT BEAM AFT LOWER ANGLE IS CRACKED.

Part: STEP — BROKEN (AIRSTAIR) · airframe 19,915 hrs · 17,033 cycles

ASD LWR STEP BROKEN.

Part: HOUSING — BROKEN (EMERGENCY LIGHT) · airframe 19,528 hrs · 16,713 cycles

FOUND EMERGENCY EXIT LIGHT HOUSING BROKEN AND LOOSE.

Part: STEP — CRACKED (PAX DOOR)

DURING A GROUND INSPECTION IN MCN, THE PASSENGER DOOR BOTTOM STEP WAS FOUND TO BE BROKEN AT THE ATTACH POINT. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR BOTTOM STEP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: SHEAR TIE — CRACKED (BS 718)

DURING A C-CHECK IN MCN, THE AFT FUSELAGE FS 718 SHEAR CLIPS ABOVE AND BELOW STRINGER 10 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE AFT FUSELAGE FS 718 SHEAR CLIPS ABOVE AND BELOW STRINGER 10 IAW ASA EO 600-53-0067A. (M)

Part: FITTING — CRACKED (PAX DOOR)

DURING A C-CHECK IN MCN, THE FORWARD ANCHOR FITTING ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE IS REMOVING AND REPLACING THE FORWARD ANCHOR FITTING ON THE PASSENGER DOOR. (M)

Part: LIGHT — FAILED (CABIN)

DURING A C-CHECK IN MCN, THE EMERGENCY EXIT BETA LIGHT ON THE PASSENGER DOOR HANDLE FAILED THE TEST. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT BETA LIGHT ON THE PASSENGER DOOR HANDLE. OPERATIONAL CHECKS GOOD. (M)

Part: FINGER DOUBLER — CORRODED (BS 510-517)

DURING A C-CHECK IN MCN, THE FINGER DOUBLER AT FS 510 TO FS 517, RBL 34-44 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS SUBMITTING A DAMAGE REPORT TO BOMBARDIER FOR ISSUANCE OF AN REO TO DETERMINE THE APPROPRIATE CORRECTIVE ACTION. S/D - MAINTENANCE REMOVED THE CORROSION FROM THE FINGER DOUBLER AT FS 51- TO FS 517, RBL 34-44 BY COMPLYING WITH ASA EO 600-53-0313. (M)

Part: FITTING — CRACKED (BS 461)

DURING A C-CHECK, THE FITTING UNDER THE FLOOR AT FS 461, RBL 9 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE FITTING UNDER THE FLOOR AT FS 461, RBL 9. (K)

Part: FINGER DOUBLER — CORRODED (BS 523-559)

DURING A C-CHECK IN MCN, THE FINGER DOUBLER AT FS 523 TO FS 559, LBL 44 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS SUBMITTING A DAMAGE REPORT TO BOMBARDIER FOR ISSUANCE OF AN REO TO DETERMINE THE APPROPRIATE CORRECTIVE ACTION. S/D - MAINTENANCE REMOVED THE CORROSION FROM THE FINGER DOUBLER AT FS 523 TO FS 559, LBL 44 BY COMPLYING WITH ASA EO 600-53-0314. (M)

Part: DOUBLER — CORRODED (BS 508)

DURING A C-CHECK, THE DOUBLER AT FS 508, RBL 44 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS SUBMITTING A DAMAGE REPORT TO MFG FOR ISSUANCE OF AN REO TO DETERMINE THE APPROPRIATE CORRECTIVE ACTION. (K) S/D - MAINTENANCE REMOVED THE CORROSION FROM THE DOUBLER AT FS 508, RBL 44 BY COMPLYING WITH ASA EO 600-53-0313. (M)

Part: HANDLE — CRACKED (E/E BAY DOOR)

DURING A C-CHECK IN MCN, THE AVIONICS BAY DOOR HANDLE WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE AVIONICS BAY DOOR HANDLE. OPS CHECKS GOOD. (M)

Part: DOUBLER — CORRODED (BS 478)

DURING C-CHECK, THE DOUBLER AT FS 478, LBL 35-45 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS SUBMITTING A DAMAGE REPORT TO MFG FOR ISSUANCE OF AN REO TO DETERMINE THE APPROPRIATE CORRECTIVE ACTION. (K) S/D - MAINTENANCE REMOVED THE CORROSION FROM THE DOUBLER AT FS 476, LBL 35-45 BY COMPLYING WITH ASA EO 600-53-0314. (M)

Part: FINGER DOUBLER — CORRODED (BS 449)

DURING A C-CHECK IN MCN, THE FINGER DOUBLERS AT FS 449, LBL 44 AND RBL 44 WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS SUBMITTING A DAMAGE REPORT TO BOMBARDIER FOR ISSUANCE OF AN REO TO DETERMINE THE APPROPRIATE CORRECTIVE ACTION. (M) S/D - MAINTENANCE REMOVED THE CORROSION FROM THE FINGER DOUBLERS AT FS 449, LBL 44 AND RBL 44 BY COMPLYING WTH ASA EO 600-53-0314. (M)

Part: NUT PLATE — CORRODED (BS 530)

DURING A C-CHECK IN MCN, THE NUT PLATE AT FS 530, RBL 44 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS SUBMITTING A DAMAGE REPORT TO BOMBARDIER FOR ISSUANCE OF AN REO TO DETERMINE THE APPROPRIATE CORRECTIVE ACTION. S/D - MAINTENANCE REMOVED THE CORROSION FROM THE NUT PLATE AT FS 530, RBL 44 BY COMPLYING WITH ASA EO 600-53-0313. (M)

Part: FINGER DOUBLER — CORRODED (BS 540-544)

DURING A C-CHECK IN MCN, THE FINGER DOUBLER AT FS 540 TO FS 544, RBL 44 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS SUBMITTING A DAMAGE REPORT TO BOMBARDIER FOR ISSUANCE OF AN REO TO DETERMINE THE APPROPRIATE CORRECTIVE ACTION. S/D - MAINTENANCE REMOVED THE CORROSION FROM THE FINGER DOUBLER AT FS 540 TO FS 544, RBL 44 BY COMPLYING WITH ASA EO 600-53-0313. (M)

Part: FINGER DOUBLER — CORRODED (BS 461)

DURING A C-CHECK IN MCN, THE FINGER DOUBLER AT FS 461, RBL 44 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS SUBMITTING A DAMAGE REPORT TO BOMBARDIER FOR ISSUANCE OF AN REO TO DETERMINE THE APPROPRIATE CORRECTIVE ACTION. S/D - MAINTENANCE REMOVED THE CORROSION FROM THE FINGER DOUBLER AT FS 461, RBL 44, BY COMPLYING WITH ASA EO 600-53-0313. (M)

Part: DOUBLER — CORRODED (FS499-516)

DURING A C-CHECK, THE DOUBLERS AT FS 499 TO FS 516, LBL 44 WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS SUBMITTING A DAMAGE REPORT TO MFG FOR ISSUANCE OF AN REO TO DETERMNE THE APPROPRIATE CORRECTIVE ACTION. (K)

Part: FINGER DOUBLER — CORRODED (BS 439)

DURING C-CHECK, THE FINGER DOUBLERS AT FS439, LBL44, RBL44 WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS SUBMITTING A DAMAGE REPORT TO MFG FOR ISSUANCE OF AN REO TO DETERMINE THE APPROPRIATE CORRECTIVE ACTION. (K) S/D - MAINTENANCE REMOVED THE CORROSION FROM THE FINGER DOUBLERS AT FS 439, LBL 44 AND RBL 44 BY COMPLYING WITH ASA EO 600-53-0314. (M)

Part: FINGER DOUBLER — CORRODED (BS 484)

DURING A C-CHECK IN MCN, THE FINGER DOUBLERS AT FS 484, LBL 44 AND RBL 44 WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS SUBMITTING A DAMAGE REPORT. S/D - MAINTENANCE REMOVED THE CORROSION FROM THE FINGER DOUBLERS AT FS 484, LBL 44 AND RBL 44 BY COMPLYING WITH ASA EO 600-53-0314. (M)

Part: FINGER DOUBLER — CORRODED (BS 459)

DURING A C-CHECK, THE FINGER DOUBLER AT FS 459, LBL 44 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS SUBMITTING A DAMAGE REPORT TO BOMBARDIER FOR ISSUANCE OF AN REO TO DETERMINE THE APPROPRIATE CORRECTIVE ACTION. S/D - MAINTENANCE REMOVED THE CORROSION FROM THE FINGER DOUBLER AT FS 459, LBL 44 BY COMPLYING WITH ASA EO 600-53-0314. (M)

Part: SKIN — CORRODED (BS 453)

DURING A C-CHECK IN MCN, THE FUSELAGE SKIN AT FS 453, LBL 45 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS SUBMITTING A DAMAGE REPORT TO BOMBARDIER FOR ISSUANCE OF AN REO TO DETERMINE THE APPROPRIATE CORRECTIVE ACTION. S/D - MAINTENANCE REMOVED THE CORROSION FROM THE FUSELAGE SKIN AT FS 453, LBL 45 BY COMPLYING WITH ASA EO 600-53-0314. (M)

Part: DOUBLER — CORRODED (BS 422-446)

DURING A C-CHECK, THE DOUBLERS AT FS 422 TO FS446, RBL 34-44 WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS SUBMITTING A DAMAGE REPORT FOR ISSUANCE OF AN REO TO DETERMINE THE APPROPRIATE CORRECTIVE ACTION. (K) MAINTENANCE REMOVED THE CORROSION ON THE DOUBLERS AT FS 422 TO FS 446, RBL 34-44 BY COMPLYING WITH ASA EO 600-53-0313. (M)

Part: DOUBLER — CORRODED (BS 427)

DURING A C-CHECK, THE DOUBLERS AT FS 427, LBL 34-44 WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS SUBMITTING A DAMAGE REPORT FOR ISSUANCE OF AN REO TO DETERMINE THE APPROPRIATE CORRECTIVE ACTION. (K) S/D - MAINTENANCE REMOVED THE CORROSION ON THE DOUBLERS AT FS 427, LBL 34-44 BY COMPLYING WITH ASA EO 600-53-0314. (M)

Part: DOUBLER — CORRODED (BS 470)

DURING C-CHECK, THE DOUBLER AT FS 470, RBL 34-44 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS SUBMITTING A DAMAGE REPORT TO MFG FOR ISSUANCE OF AN REO TO DETERMINE THE APPROPRIATE CORRECTIVE ACTION. (K) S/D - MAINTENANCE REMOVED THE CORROSION FROM THE DOUBLER AT FS 470, RBL 34-44 BY COMPLYING WITH ASA EO 600-53-0313. (M)

Part: FINGER DOUBLER — CORRODED (BS 484)

DURING A C-CHECK IN MCN, THE FINGER DOUBLERS AT FS 484, LBL 44 AND RBL 44 WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS SUBMITTING A DAMAGE REPORT TO BOMBARDIER FOR ISSUANCE OF AN REO TO DETERMINE THE APPROPRIATE CORRECTIVE ACTION. (M)

Part: FINGER DOUBLER — CORRODED (BS 499-510)

DURING A C-CHECK IN MCN, THE FINGER DOUBLER AT FS 499 TO FS 510, RBL 44 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS SUBMITTING A DAMAGE REPORT TO BOMBARDIER FOR ISSUANCE OF AN REO TO DETERMINE THE APPROPRIATE CORRECTIVE ACTION. S/D - MAINTENANCE REMOVED THE CORROSION FROM THE FINGER DOUBLER AT FS 499 TO FS 510, RBL 44 COMPLYING WITH ASA EO 600-53-0313. (M)

Part: WEB — CORRODED (BS 559-574)

DURING A C-CHECK, THE LT FLOOR ATTACH WEB AT FS 559.80 TO 574 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE WILL DETERMNE THE APPROPRIATE REPAIR UPON FURTHER INSPECTION ON THE LT FLOOR WEB AT FS 559.80 TO FS 574.

Part: FLOOR SUPPORT — CORRODED (BS 559-605)

DURING C-CHECK, THE RT FLOOR SUPPORT WEB AT FS 559.112 TO FS 605 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED THE CORROSION ON THE RT FLOOR SUPPORT WEB AT FS 559.112 TO FS 605 BY COMPLYING WITH EO. (K)

Part: SUPPORT BEAM — CRACKED (ENGINE)

DURING A C-CHECK IN MCN, THE CENTER ENGINE SUPPORT BEAM WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE WILL REMOVE AND REPLACE THE CENTER ENGINE SUPPORT BEAM IAW EO`S 600-53-0078 AND 600-54-0009. (M)

Part: FLOOR SUPPORT — CRACKED (BS 280)

DURING A C-CHECK IN MCN, THE FLOOR SUPPORT ANGLE AT FS 280, LBL 9 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE FLOOR SUPPORT ANGLE AT FS 280, LBL 9 IAW ASA EO 600-53-0309. (M)

Part: FLOORBEAM — CRACKED (BS 584)

DURING A C-CHECK IN MCN, THE FLOORBEAM AT FS 584, LBL 9 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE FLOORBEAM AT S 584, LBL 9 IAW CRJ200 SRM 53-00-43. (M)

Part: FLOOR SUPPORT — CORRODED (BS 280)

DURING A C-CHECK IN MCN, THE FORWARD AND AFT FLOOR SUPPORT ANGLES AT FS 280 BETWEEN LBL 9 AND RBL 9 WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE FORWARD AND AFT FLOOR SUPPORT ANGLES AT FS 280 BETWEEN LBL 9 AND RBL 9 IAW ASA EO 600-53-0309. (M)

Part: FRAME — CRACKED (BS 280)

DURING A C-CHECK IN MCN, THE FS 280 FRAME AT LBL 10 AND RBL 10 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE FS 280 FRAME AT LBL 10 AND RBL 10 IAW ASA EO 600-53-0309. (M)

Part: FLOOR SUPPORT — CORRODED (FS 559-605)

DURING A C-CHECK, THE RT FLOOR SUPPORT WEB AT FS 559.112 TO FS 605 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE WILL DETERMNE THE APPROPRIATE REPAIR UPON FURTHER INSPECTION ON THE RT FLOOR SUPPORT WEB AT FS 559.112 TO FS 605. THIS MRR WILL REMAIN OPEN PENDING THE APPROPRIATE CORRECTIVE ACTION. (K)

Part: WEB — CORRODED (LT FLOOR ATTACH)

DURING A C-CHECK, THE LT FLOOR ATTACH WEB AT FS 559.80 TO FS 574 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED THE CORROSION ON THE LT FLOOR ATTACH WEB AT FS 559.80 TO FS 574 BY COMPLYING WITH EO. (K)

Part: DOOR FRAME — CRACKED (BS 320-338)

DURING A C-CHECK IN MCN, THE PASSENGER DOOR AFT OUTBOARD FRAME MEMBER LOWER END AT FS 320.10 AND FS 338 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE PASSENGER DOOR AFT OUTBOARD FRAME MEMBER LOWER END AT FS 320.10 AND FS 338 IAW BOMBARDIER REO NR 601R-52-11-402. (M)

Part: SUPPORT BEAM — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL 0 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL 0 IAW ASA EO 600-53-0072B. (M)

Part: STEP — BROKEN (PAX DOOR)

DURING A GROUND INSPECTION, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ASSEMBLY AND STEP RETRACTION ARM ON THE PASSENGER DOOR. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: SEAL — WORN (ACM DUCT)

DURING DESCENT INTO BNA FROM ATL, THE FLIGHT ATTENDANT NOTICED AN ODOR IN THE BACK OF THE CABIN FOLLOWED BY THE SYNOPTIC PAGE SHOWING THE RT PACK BEGINNING TO OVERTEMP. CREW TURNED OFF THE RT PACK AND THE ODOR SUBSEQUENTLY DISSIPATED. THE AIRCRAFT LANDED SAFELY IN BNA. UPON INSPECTION OF THE ACM, MAINTENANCE FOUND THE DUCT DETACHED FROM THE ACM. MAINTENANCE REMOVED AND REPLACED THE SEAL AND REATTACHED THE DUCT TO THE ACM. OPERATIONAL AND LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LIGHT — CRACKED (EMERGENCY EXIT)

DURING HANGAR MAINTENANCE IN MCN, THE EMERGENCY EXIT LIGHT AT THE SERVICE DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT AT THE SERVICE DOOR. (M)

Part: LIGHT — DAMAGED (CABIN)

DURING HANGAR MAINTENANCE IN MCN, THE EMERGENCY FLOODLIGHT BY THE PASSENGER DOOR WAS FOUND TO BE DAMAGED. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY FLOODLIGHT BY THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LIGHT — DEFECTIVE (CABIN)

DURING HANGAR MAINTENANCE, THE AFT MOST EMERGENCY CEILING LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT MOST EMERGENCY CEILING LIGHT ASSY. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: LIGHT — INOPERATIVE (CABIN)

DURING HANGAR MAINTENANCE IN BTR, THE EMERGENCY FLOOR TRACK LIGHTING AT ROW 5-8 WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY FLOOR TRACK LIGHTING AT ROW 5-8. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO COMPT)

DURING TAXI OUT FROM ATL-CRW, A SMOKE CARGO WARNING MESSAGE WAS RECEIVED AND THE NR 1 AND NR 2 FIRE BOTTLES DISCHARGED. THE CREW COMPLIED WITH QRH PROCEDURES AND PERFORMED AN EMERGENCY EVACUATION OF THE AIRCRAFT. ALL PASSENGERS WERE DEPLANED SAFELY THROUGH THE MAIN PAX DOOR. THERE WERE NO INJURIES AND NO AIRCRAFT DAMAGE. THE AIRCRAFT WAS INSPECTED AND RELEASED BY THE ATL FIRE SERVICES. MAINTENANCE ALSO INSPECTED THE AIRCRAFT AND IT WAS RETURNED TO THE GATE SAFELY. MAINTENANCE REMOVED AND REPLACED BOTH CARGO SMOKE DETECTORS AND ALSO REMOVED AND REPLACED THE NR 1 AND NR 2 FIRE BOTTLE CARTRIDGES. OPS CHECKS GOOD. NO DEFECTS WERE NOTED. AIRCRAFT OK FOR SERVICE. (M)

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

DURING A C-CHECK IN MCN, THE NR 1 EMERGENCY FLOOR LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 1 EMERGENCY FLOOR LIGHT LAMP. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: HINGE — CRACKED (PAX STEP)

DURING A C-CHECK IN THE MCN, THE PASSENGER DOOR TOP STEP HINGE WAS FOUND TO BE CRACKED. MAINTENANCE IS REMOVING AND REPLACING THE PASENGER DOOR TOP STEP HINGE. (M)

Part: INTERCOSTAL — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE INTERCOSTAL AT STRINGERS 13 AND 14 JUST FORWARD OF FS 625.30 ON THE LEFT SIDE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE INTERCOSTAL AT STRINGERS 13/14 JUST FORWARD OF FS 625.30 ON THE LEFT SIDE IAW REO 601R-53-61-105. (M)

Part: LIGHT — CRACKED (GALLEY)

DURING A C-CHECK IN MCN, THE EMERGENCY EXIT LIGHT LENS COVER ON THE LOWER SIDE VENT PANEL WAS FOUND TO BE CRACKED. MAINTENANCE IS REMOVING AND REPLACING THE EMERGENCY EXIT LIGHT ASSEMBLY ON THE LOWER SIDE VENT PANEL. (M)

Part: SKIN PANEL — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE NOSE LANDING GEAR CUT OUT ON BOTH AFT CORNERS AT FS 235 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE NOSE LANDING GEAR CUT OUT ON BOTH AFT CORNERS AT FS 235 IAW ASA EO 600-53-0122. (M)

Part: CLIP — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE CLIPS AT FS 484, RBL 27 AND LBL 27 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CLIPS AT FS 484, RBL 27 AND LBL 27 IAW ASA EO 600-53-0098. (M)

Part: SUPPORT ANGLE — CRACKED (FUSELAGE)

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

Part: STEP — CRACKED (PAX DOOR)

DURING A C-CHECK IN MCN, THE TOP STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REPAIRED THE TOP STEP ON THE PASSENGER DOOR IAW SRM 51-71-00. (M)

Part: STEP — CRACKED (PAX DOOR)

DURING A C-CHECK IN MCN, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REPAIRED THE BOTTOM STEP ON THE PASSENGER DOOR IAW SRM 51-74-00. (M)

Part: PLATE — CRACKED (FUSELAGE)

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

Part: CLIP — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE INBOARD CLIPS AT FS 280, LBL 9 AND RBL 9 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE INBOARD CLIPS AT FS 280, LBL 9 AND RBL 9 IAW SRM 51-42-21. (M)

Part: PROXIMITY SENSOR — OUT OF ADJUST (NLG)

DURING TAKEOFF FROM, THE NOSE GEAR WOULD NOT RETRACT. QRH PROCEDURES WERE COMPLIED WITH AND AN EMERGENCY WAS DECLARED. THE AIRCRAFT RETURNED, LANDING SAFELY. MAINTENANCE DISCOVERED THE NOSE GEAR S23 PROXIMITY SENSOR HITTING THE TARGET AND ADJUSTED THE SENSOR. MAINTENANCE ALSO PERFORMED FOUR GEAR SWINGS. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: PIN — BENT (PAX DOOR)

FLT 4160 - DURING A GROUND INSPECTION IN ATL, THE CREW REPORTED THE PASSENGER DOOR INSIDE HANDLE WOULD NOT LIFT AND THE DOOR WAS DIFFICULT TO OPEN SOMETIMES. MAINTENANCE STRAIGHTENED THE OUTER HANDLE PIN ON THE PASSENGER DOOR. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: FRAME — CRACKED (RT ENGINE)

DURING AN A-CHECK IN BTR, THE RIGHT ENGINE FRAME 640 BETWEEN STRINGERS 9 AND 12 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE RIGHT ENGINE FRAME 640 BETWEEN STRINGERS 9 AND 12 IAW ASA EO 600-53-0075. (M)

Part: LAMP — BURNED OUT (CABIN)

FLT 4480 - DURING A GROUND INSPECTION IN ATL, THE FLIGHT ATTENDANTS ANNUNCIATOR EMERGENCY BLUE LIGHT ON THE CEILING EMERGENCY EXIT SIGN WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FLIGHT ATTENDANTS ANNUNCIATOR EMERGENCY LIGHT LAMP ON THE CEILING EMERGENCY EXIT SIGN. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: B-NUT — LOOSE (LT ENGINE)

FLT 4476 - DURING CLIMB-OUT FROM ATL-HPN, THE LEFT ENGINE OIL PRESSURE DROPPED BELOW 25 PSI. THE CAPTAIN SHUT THE ENGINE DOWN AND THE AIRCRAFT RETURNED TO ATL. AN EMERGENCY LANDING WAS MADE SAFELY IN ATL. MAINTENANCE FOUND THE LEFT ENGINE 5 QUARTS LOW OF OIL AND THE B-NUT ON THE C-SUMP 4 O'CLOCK RETURN LINE LOOSE. MAINTENANCE TIGHTENED THE B-NUT ON THE RETURN LINE AND SERVICED THE LEFT ENGINE WITH 5 QUARTS OF OIL. OPERATIONAL AND LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: FRAME — CRACKED (STA 718)

DURNG 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 EO/REO/SRM.

Part: BEAM — CRACKED (ENG SUPPT BEAM)

DURING A HANGER INSPECTION, WHILE COMPLYING WITH EO, INSPECTION OF ENGINE SUPPORT BEAM CRACKS, A CRACK WAS DISCOVERED ON THE BEAM AT THE LEFT ACCESS PANEL FORWARD CORNER. MAINTENANCE REPAIRED THE CRACK IN THE ENGINE SUPPORT BEAM.

Part: CONTROL UNIT — INOPERATIVE (FUSELAGE)

FLT 4469 - DURING FLIGHT FROM YYZ TO ATL, CREW RECEIVED STAB TRIM AND MACH TRIM CAUTION MESSAGE ON RANDOM INTERVALS. CREW RESET SYSTEM, BUT MESSAGE WOULD START AGAIN. STAB AND MACH TRIM FAILED AGAIN UPON APPROACH. CREW DECLARED AN EMERGENCY AND LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED HSTCU. OPERTIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: CIRCUIT BREAKER — MALFUNCTIONED (COCKPIT)

FLT 4555 - DURING FLIGHT FROM YYZ-ATL, CREW RECEIVED A FLAP FAIL MESSAGE IN FLIGHT. CREW TURNED ON HYDRAULIC PUMPS. CREW DECLARED AN EMERGENCY AND DID A ZERO FLAP LANDING. AIRCRAFT LANDED SAFELY. MAINTENANCE RESET CIRCUIT BREAKERS B5, B8, BP-1 AND CBP-2. MAINTENANCE CYCLED FLAPS 12 TIMES. OPS CHECK WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M)