N843AS

Part: SUPPORT ANGLE — CRACKED (BS 621 BULKHEAD) · airframe 35,666 hrs · 32,390 cycles

BS 621 BULKHEAD, CARGO DOOR SUPPORT MEMBER. LOWER ATTACHMENT ANGLE IS CRACKED. R & R SUPPORT ANGLE WITH NEW SERVICEABLE PART IAW SRM 51-42-21.

Part: ISOLATOR — CRACKED (BS 621 BULKHEAT) · airframe 35,666 hrs · 32,390 cycles

BS 621 FWD FACE OF BULKHEAD NUMEROUS ISOLATOR MOUNTS CRACKED AND/OR BROKEN. REPLACED ISOLATORS WITH NEW IAW SRM 51-42-06.

Part: LIGHT — DAMAGED (CABIN) · airframe 35,339 hrs · 32,067 cycles

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

Part: TRUNNION — CRACKED (LT MLG) · airframe 34,328 hrs · 31,076 cycles

LEFT MLG TRUNNION HAS ONE CRACKED FASTENER HOLE. RECEIVED AND COMPLIED WITH REO 601R-57-21-2099 AND EC/TC REO 601R-57-21-2099. REPAIR CLASSIFIED AS MAJOR.

Part: SKIN — CORRODED (RT WING) · airframe 34,328 hrs · 31,076 cycles

ACCESS PANEL RT WING 640BB HAS CORROSION AROUND LAND. COMPLIED WITH REO 601R-57-21-030 AND ECTC EO 600-57-81. REPAIR CLASSIFIED AS MAJOR.

Part: SKIN — CORRODED (WING) · airframe 34,328 hrs · 31,076 cycles

ACCESS PANEL 540BB HAS PITTING AROUND THE FLANGE. COMPLIED WITH REO 601R-57-21-030 AND EC/TC EO 600-57-81. REPAIR CLASSIFIED AS MAJOR.

Part: ACCESS PANEL — CORRODED (WING) · airframe 34,328 hrs · 31,076 cycles

ACCESS PANEL 650CB CORRODED. COMPLIED WITH REO 601R-57-21-030 AND ECTC EO 600-57-81. REPAIR CLASSIFIED AS MAJOR.

Part: BULKHEAD — CRACKED · airframe 34,328 hrs · 31,076 cycles

CRACK INDICATION ON REAR PRESSURE BULKHEAD FORWARD FACE BELOW WL 120.43 AT BL 0. COMPLIED WITH ECTC REO601R-53-61-1285 AND MET ALL THE REQUIREMENTS OF REO 601R-53-61-1285, REV D.

Part: SEAT TRACK — CORRODED (BS 409-559) · airframe 34,328 hrs · 31,076 cycles

SEAT TRACK CORRODED FS 409+128-559, RBL 9. COMPLIED WITH REO 601R-53-00-485, REMOVED AND REPLACED SEAT TRACK IAW AMM 53-01-11, TASK 53-01-11-000-802 AND AMM 53-01-11-400-801.

Part: ATTACH ANGLE — CRACKED (BS 280) · airframe 34,328 hrs · 31,076 cycles

BS 280 BULKHEAD TO LBL 9 FLOOR ATTACH ANGLE CRACKED OTBD SIDE. REMOVED ATTACH ANGLE IAW SRM 51-42-20. INSTALLED FABRICATED NEW ATTACH ANGLE IAW REO 601R-53-11-926. COMPLIED WITH REO 601R-53-11-926, REV B IAW NDTM PART 1, 51-20-06. REPAIR CLASSIFIED AS MAJOR.

Part: SEAT TRACK — CORRODED (BS 364-394) · airframe 34,328 hrs · 31,076 cycles

SEAT TRACK CORRODED, FS 364-394, LBL 9.0. R & R SEAT TRACK IAW AMM 53-01-11-000-802 & 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 364-394) · airframe 34,328 hrs · 31,076 cycles

SEAT TRACK CORRODED FS 364-394, RBL 9. R & R SEAT TRACK IAW AMM 53-01-11-000-802, & 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 394-409) · airframe 34,328 hrs · 31,076 cycles

SEAT TRACK CORRODED FS 394-409+128, RBL 9. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-01-11, TASK 53-01-11-000-802 AND 53-01-11-400-802.

Part: CARGO TRACK — CORRODED (BS 559) · airframe 34,328 hrs · 31,076 cycles

CARGO TRACK CORRODED FS 559+80, LBL 27.5. REMOVED AND REPLACED CARGO TRACK IAW AMM 53-01-11, TASK 53-01-11-000-802, & 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 394-409) · airframe 34,328 hrs · 31,076 cycles

SEAT TRACK CORRODED FS 394-409+128, LBL 9. R & R SEAT TRACK IAW AMM 53-01-11-000-802 & 01-11-400-802.

Part: HINGE — DENTED (PAX DOOR) · airframe 34,328 hrs · 31,076 cycles

PASSENGER DOOR HINGE HALF DENTED BETWEEN RIVET 7 AND 11 AND INCLUDE DOOR FRAME UNDER SEAL RETAINER. REPAIRED IAW SRM 52-00-00 AND SRM 51-42-06. REPAIR CLASSIFIED AS MAJOR.

Part: INTERCOSTAL — CRACKED (CARGO DOOR) · airframe 34,328 hrs · 31,076 cycles

CARGO DOOR LOWER AFT CORNER INTERCOSTAL CRACKED. REMOVED INTERCOSTAL IAW SRM 51-42-06-000. INSTALLED INTERCOSTAL & FASTENERS IAW SRM DWG 601R3507. REPAIR CLASSIFIED AS MAJOR.

Part: HINGE — GOUGED (PAX DOOR) · airframe 34,328 hrs · 31,076 cycles

HINGE SEGEMENT, PASSENGER DOOR LUGS HAS GOUGE DAMAGE. R & R HINGE IAW SUPPLEMENT ASA 52-11-26. COMPLIED WITH ECTC EO600-52-0146. REPAIR CLASSIFIED AS MAJOR.

Part: HINGE — GOUGED (FUSELAGE) · airframe 34,328 hrs · 31,076 cycles

HINGE SEGEMENT HALF ON FUSELAGE SIDE HAS GOUGED LUGS. REPAIRED IAW REO 601R-53-21-814. REPAIR CLASSIFIED AS MAJOR.

Part: LIGHT — WRONG PART (CABIN) · airframe 33,833 hrs · 30,566 cycles

CABIN FLOOR EMERGENCY LIGHT INCORRECT FOR THIS ACFT. R & R PAX CABIN EMERGENCY LIGHT IAW AMM 33-51-01 01.

Part: SKIN — DENTED (BS 310) · airframe 33,735 hrs · 30,466 cycles

DENT ON FUSELAGE AT FS 310 AND STGR 16L CAUSED BY CONTACT WITH FWD LOWER PAX DOOR LATCH PIN. REPAIRED IAW GREO 601R-53-21-160, REV B. CLASSIFIED AS MAJOR REPAIR IAW GMM 5-3.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 32,142 hrs · 28,834 cycles

LIGHTED EMERGENCY EXIT SIGN ON THE LOWER WARDROBE INOPERATIVE. R & R THE LIGHTED EMERGENCY EXIT SIGN IAW AMM 33-51-10. OPS CHECKED GOOD.

Part: PUSHROD — OUT OF ADJUST (PAX DOOR) · airframe 31,863 hrs · 28,541 cycles

PAX DOOR SOMETIMES WILL NOT OPEN. ADJUSTED PUSH ROD ON LATCH CAM TORQUE-TUBE MECHANISM IAW AMM 52-11-23. SDR CLOSED.

Part: WIRE — MISROUTED (PAX DOOR) · airframe 31,850 hrs · 28,526 cycles

ON GATE RETURN, COULD NOT OPEN PAX DOOR. WIRING ON P55MB AND P56MB WAS FOUND HOOKED OVER THE CAM ON PAX DOOR TORQUE TUBE . REPAIRED. PERFORMED OPS TEST OF PAX DOOR IAW AMM 52-11-00. NO DEFECT NOTED.

Part: FRAME — CORRODED (BS 333) · airframe 30,508 hrs · 27,064 cycles

FS 333.00 FRAME CORRODED AT LOWER SIDE NEAR STRINGER 26L. REPAIRED IAW REO 601R-53-21-2264.

Part: SKIN — CRACKED (RT WING) · airframe 30,508 hrs · 27,064 cycles

RT WING PLANK CRACKED OTBD OF RT JACK PAD. REWORKED AREA IAW REO 601R-57-21-130 REV J.

Part: ANGLE — CORRODED (THRESHOLD) · airframe 30,508 hrs · 27,064 cycles

SERVICE DOOR AFT LOWER CORNER AND TEE CAP AT FS 349.50 CORRODED. REMOVED DAMAGE IAW REO 601R-53-21-2263. COMPLIED NDTM PART 1, 51-20-06. NO INDICATIONS NOTED. INSTALLED NEW SERVICEABLE ANGLE AND FITTING AT FS 349.00 IAW SRM 51-42-06-00 AND 51-42-21-00.

Part: FRAME — CORRODED (BS 333 S26L) · airframe 30,508 hrs · 27,064 cycles

BS 333 FRAME CORRODED AT LOWER SIDE NEAR STRINGER 26L. REMOVED CORROSION IAW SRM 51-21-06-00. PERFORMED UT THICKINESS INSPECTION IAW MAC NDT PROCEDURES UT-3. MIN MATERIAL REMAINING IS .045" ORIGINAL IS .050" MATERIAL REMOVED IS.005". ALODINED AREA, WET SHOT RIVETS, PRIMED, PAINTED AREA IAW REO 601R-53-21-2264, ECTC 601R-53-21-2264.

Part: SILL — CORRODED (SERVICE DOOR) · airframe 30,508 hrs · 27,064 cycles

SERVICE DOOR SILL CORRODED AROUND BOTH FWD AND AFT STOP FITTINGS. REMOVED SERVICE DOOR SILL DUE TO CORROSION BE BEYOND LIMITS IAW SRM 31-42-21 AND 51-42-06. INSTALLED NEW SERVICEBLE SERVICE DOOR SILL IAW SRM 51-42-21 AND 51-42-06.

Part: STRUCTURE — CORRODED (SERVICE DOOR) · airframe 30,508 hrs · 27,064 cycles

SERVICE DOOR AFT LOWER CORNER AND TEE CAP AT FS 349.50 ON CORRODED. REMOVED CORROSION IAW SRM 51-21-06 FOUND TO BE BEYOND LIMITS. REMOVED FITTING AND ANGLE, IAW SRM 51-42-06 AND 51-42-21.

Part: RIB — CRACKED (RT WING) · airframe 30,508 hrs · 27,064 cycles

RIGHT WING AFT SPAR SUPPORT RIB AT WS 149.58 CRACKED. PERFORMED EDDY CURRENT INSPECTION IAW MAC NDT INSPECTION PROCEDURE ET-2 AREA IS CONFIRMED CRACKED. REPAIRED IAW REO 601R-57-21-130, REV J, REPAIR OPTION 2.

Part: BUSHING — CORRODED (HORIZONTAL STAB) · airframe 30,508 hrs · 27,064 cycles

LEFT SIDE HORIZONTAL TO VERTICAL ATTACHMENT POINT BUSHING CORRODED ON VERTICAL. REMOVED THE HORISONTAL STABLIZER IAW AMM 55-10-00-000-801. REPAIRED BUSHING, INSTALLED ORIGINAL HORIZONTAL STABLIZER IAW AMM 55-10-00-400-801.

Part: HOUSING — BROKEN (EMERGENCY LIGHT) · airframe 30,508 hrs · 27,064 cycles

CEILING EMERGENCY LIGHT HOUSING BROKEN AT FLOOD LIGHT 1, FS 405.00. R & R EMERGENCY LIGHT ASSY WITH NEW LIGHT ASSY IAW AMM 33-51-16-000-801 & 33-51-16-400-801.

Part: SEAT BELT — UNSERVICEABLE (CABIN) · airframe 30,508 hrs · 27,064 cycles

SEATS 1A AND 1B SEAT BELT TAGS UNREADABLE. R & R SEAT BELTS FOR PAX SEATS 1A&1B IAW CMM 25-25-82.

Part: LIGHT — DAMAGED (CABIN) · airframe 30,508 hrs · 27,064 cycles

EMERGENCY LIGHT STAINED BEYOND 10 PERCENT OF 48 INCH LENGTH. (4.75) AT SEATS 1&2 ABCD. R & R LIGHT IAW AMM SUPPLEMENT 33-51-00 AND 33-51-01-000-806, 33-51-01-400-806. OP CHECKED GOOD.

Part: FITTING — CRACKED (MLG) · airframe 29,603 hrs · 26,034 cycles

LT MLG MAIN FITTING HAS A CRACK INDICATION ON OTBD SIDE OF AFT BOLT HOLE AREA. REMOVED LT MLG ASSY IAW AMM 32-11-00. R & R MAIN FITTING ASSY IAW CMM 32-10-15. REINSTALLED SERVICABLE LT MLG ASSY IAW AMM 32-11-00. OPS AND LEAK CHECK GOOD IAW AMM 32-11-00.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 28,219 hrs · 24,467 cycles

CAPTAIN'S FLASHLIGHT INOP. REPLACED BATTERIES IN FLASHLIGHT, OPS TEST GOOD IAW CRJ 200 AMM 25-61-00.

Part: THRUST REVERSER — UNKNOWN (LEFT) · airframe 27,950 hrs · 24,139 cycles

LT ENGINE THRUST REVERSER ECAIS MESSAGE AND REV N1 WARNING INFLIGHT. COMPLIED WITH QRH 1-12 NO OTHER ABNORMALITIES NOTED. (ACFT RETURNED TO DEPARTURE AFTER T/O -- TOWER DECLARED EMERGENCY) PERFORMED OPS TEST OF THE THRUST REVERSER SYS IAW AMM 78-30-00. OPS CK GOOD. NO DEFECTS NOTED. PLACARD REMOVED, DEFER CLEARED.

Part: DOOR — BINDING (MAIN PAX) · airframe 27,701 hrs · 23,839 cycles

PAX DOOR HARD TO OPEN, OUTER HANDLE HARD TO DEPLOY. COMPLIED WITH OPS CHECK OF PAX DOOR IAW AMM 52-11-00. OPS CHECKED GOOD IAW AMM. OK FOR SERVICE.

Part: PLATE — CRACKED (BS 589) · airframe 26,722 hrs · 22,717 cycles

CARGO FLOOR LANDING PLATE IS CRACKED AT FS 589 AT INBD FLOORBEAM RIVET. C/W EC/TC REO 601R-53-61-433 AND MET ALL THE REQUIREMENTS OF REO 601R-53-61-433.

Part: SILL — CORRODED (BS 574-621) · airframe 26,722 hrs · 22,717 cycles

CARGO DOOR SILL PLATE HAS CORROSION AROUND NUTPLATE HOLES FROM FS 574.00 TO FS 621.00. REMOVED 5 OLD DAMAGED INSERTS. INSTALLED 5 NEW SERVICEABLE INSERTS FROM LAV THRESHOLD IAW CMM 53-10-04 PART D STEPS 1-13, USING EY3010A/B ADHESIVE PO W1011.

Part: SKIN — CRACKED (RT WING) · airframe 26,722 hrs · 22,717 cycles

RT WING FUEL DRAIN HOLE AT APPROX WS 50.00 HAS A 60 PERCENT FSH HFEC INDICATION NOTED 0.100" LONG APPROX 0125" OTBD OF DRAIN HOLE. INDICATION MARKED ON ACFT. FAILS NDT INSP AT THIS TIME. COMPLIED WITH EC/TC REO 601R-57-21-1230 AND REO 601R-57-21-1230.

Part: BEAM — CRACKED (BS 409 BULKHEAD) · airframe 26,722 hrs · 22,717 cycles

FS 409+128 BULKHEAD LBL 18.00 VERTICAL BEAM CRACKED ON C/B SIDE BY LOWER ATTACH FASTENER. REMOVED VERT BEAM IAW SRM 51-42-06 ST 1 AND 11. INSTALLED NEW SERVICEABLE O/B VERTICAL BEAM TO THE BEAM ASSEMBLY IAW SRM 51-42-06 1 AND 9. INSTALLED VERT BEAM IAW REO 601R-53-41-889. COMPLIED WITH EC/TC REO 601R-53-41-889 AND MET ALL THE REQUIREMENTS OF REO 601R-53-41-889.

Part: SILL — CORRODED (BS 559-621) · airframe 26,722 hrs · 22,717 cycles

FS 559.00+80 - FS 621.00 RT FLOOR SILL HAS CORROSION. REMOVED NUTPLATES FROM RT CARGO SILL PLATE IAW SRM 51-42-15 STEP 10 AND 51-42-10 FIGURE 4. REMOVED CORROSION FROM RT CARGO SILL IAW SRM 51-21-06 STEP 3. INSTALLED NEW NUTPLATES IAW SRM 51-45-00 STEP 9 AND 51-42-15 STEP 6. RT CARGO FLOOR SILL HAS CORROSION REMAINING. REMOVED CARGO FLOOR SILL IAW SRM 51-42-06 AND 51-42-21. INSTALLED DOUBLERS AND NUTPLATES IAW SRM 51-42-06. INSTALLED GROMMETS IAW SRM 51-22-00. INSTALLED CABLE SUPPORT IAW SRM 51-42-13. INSTALLED SERVICEABLE CARGO SILL PLATE IAW SRM 51-42-21 AND SRM 51-42-06. APPLIED PROTECTIVE TOPCOAT IAW SRM 51-25-16.

Part: FLOOR SUPPORT — CORRODED (BS 567-621) · airframe 26,722 hrs · 22,717 cycles

FS 567.00-FS 621.00 LBL 27 HAS CORROSION AROUND NUTPLATE HOLES ON FLOOR SUPPORT CAP. REMOVED FLOOR BEAM CAP IAW SRM 51-42-06 STEP 11 AND 51-42-21 STEP 11 AND LOCATED AND DRILLED NEW FLOOR BEAM CAP IAW SRM 51-40-11 AND INSTALLED FLOOR PANEL NUTPLATES IAW SRM 51-45-00. INSTALLED FLOOR BEAM CAP IAW REO 601R-53-61-3400 AND SRM 51-42-21, 51-42-34 AND 51-42-22. COMPLIED WITH EC/TC REO 601R-53-61-3400 IN ACCORDANCE WITH REO 601R-53-61-3400 REV.D.

Part: POST — CRACKED (BS 409) · airframe 26,722 hrs · 22,717 cycles

FOUND FS 409.0+128 VERTICAL POST RBL 18.00 INBD AND OTBD SIDES HAVE INDICATIONS NOTED AFT FLANGE RADIUS WL 69 APPROX .2" IN LEGNTH 60 PERCENT FSH AND 70 PERCENT FSH FAILED NDT INSP. REMOVED 409+128 INBD & OTBD RBL 18 POSTS IAW SRM 51-42-06 STEP 11 A & B 1-6. OBTAINED SERVICEABLE PARTS. DRILLED AND LOCATED HOLES IAW SRM 51-42-06 STEP 7A-B. RIVETED POSTS TOGETHER IAW SRM 51-42-06 STEP 9A AND FIG 8. INSTALLED RBL 18 INBD AND OTBD POSTS AT FS 409+128 IAW SRM 51-42-06 FIG 1 SHEET 1 AND REO 9601R-53-41-889. C/W EC/TC REO 601R-53-41-889 AND MET ALL THE REQUIREMENTS OF REO 601R-53-41-889.

Part: FLOORBEAM — CORRODED (BS 621) · airframe 26,722 hrs · 22,717 cycles

FS 621, LBL 27 FLOOR SUPPORT UPPER FITTING HAS CORROSION AROUND RIVET HOLE. REMOVED CORRODED FLOOR SUPPORT FITTING IAW SRM 51-42-22 PG 21 ITEM 11A. INSTALLED NEW FLOOR SUPPORT FITTING IAW SRM 51-42-22 PG 17 ITEMS 9A THROUGH 9C(1), 51-41-02 PG 5 ITEM 3A THROUGH PG 6 ITEM 3B(1)(H).

Part: FLOORBEAM — CORRODED (BS 559) · airframe 26,722 hrs · 22,717 cycles

FLOOR SUPPORT ANGLE HAS CORROSION AROUND NUTPLATE HOLES FS 559.00+80 RBL 27 TO RBL 36. REMOVED LIGHT CORROSION FROM FLOOR SUPPORT ANGLE IAW SRM 51-21-06 1A, 3A AND B1-2, 4 AND 5, FOUND TO BE WITHIN LIMITS IAW SRM 53-00-00 1A-B FIGURE 102. STARTING THICKNESS OF FLOOR SUPPORT .100", REMOVED .010" MATERIAL, WITHIN LIMITS AS NOTED IN STEP 1 IAW SRM 53-00-00 1A-B. INSTALLED MYLAR TAPE ON FLOOR SUPPORT ANGLE IAW SRM 51-27-19.

Part: FLOORBEAM — CORRODED (BS 559) · airframe 26,722 hrs · 22,717 cycles

FLOOR SUPPORT ANGLE HAS CORROSION AROUND NUTPLATE HOLES AT FS 559.00 BETWEEN LBL 9 AND LBL 27. FOUND CORROSION TO BE BEYOND LIMITS. REMOVED FLOOR SUPPORT ANGLE CAP IAW SRM 51-42-06 STEP 11 AND 51-42-29 STEP 11. INSTALLED NEW SERVICEABLE FLOOR SUPPORT ANGLE CAP IAW SRM 51-42-06 STEPS 1 AND 9. PAINTED IAW SRM 51-25-01.

Part: FLOORBEAM — CORRODED (BS 589) · airframe 26,722 hrs · 22,717 cycles

FLOOR SUPPORT ANGLE HAS CORROSION AROUND NUTPLATE HOLES AT FS 589 BETWEEN RBL 9 AND RBL 27. REMOVED CORRODED (BEYOND LIMITS) FLOOR SUPPORT ANGLE CAP IAW SRM 51-42-06 STEP 11 AND 51-42-21 STEP 11. INSTALLED NEW ANGLE IAW SRM 51-42-06. INSTALLED NEW SERVICEABLE FLOOR SUPPORT ANGLE CAP IAW SRM 51-42-21 AND SRM 51-42-06.

Part: CARGO TRACK — CORRODED (BS 559) · airframe 26,722 hrs · 22,717 cycles

BAGGAGE RAIL AT FS 559+112 LBL 9 CORRODED. REMOVED CORRODED BAGGAGE RAIL AT FS 559+112 LBL 9. LOCATED AND DRILLED NEW SERVICEABLE RAIL. INSTALLED RAIL IAW SRM 51-41-02 STEPS 1A, 2B1, C1A2A, 3A2A-D.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 26,722 hrs · 22,717 cycles

FLOOR SEAT TRACK SEGMENT CORRODED FS 559+80 RBL 9. REMOVED CORRODED FLOOR SEAT TRACK SEGMENT FS 559+80 RBL 9 BY REMOVING 9 COUNTERSUNK SCREWS. INSTALLED NEW FLOOR SEAT TRACK SEGMENT FS 559+80 RBL 9 IAW SRM 51-40-11, PG 8 ITEMS 6A THROUGH 6B(1), 51-41-02 PG 1 ITEM 2A THROUGH PG 3 ITEM 2C(2)(A), PG 5 ITEM 3A THROUGH 3A(2)(D) AND 51-25-06 PG 3 ITEM 5A THROUGH PG 4-5B(6).

Part: PLATE — CORRODED (BS 559-567) · airframe 26,722 hrs · 22,717 cycles

2 EA ANCHOR PLATES CORRODED AT LBL 27 BETWEEN FS 559+90 AND FS 567. REMOVED AND REPLACED 2EA ANCHOR PLATES AT LBL 27 BETWEEN F.S. 509+90 AND F.S. 567.00 IAW SRM 51-41-00 AND 51-41-04 STEP 3.

Part: CARGO TRACK — CORRODED (BS 559) · airframe 26,722 hrs · 22,717 cycles

BAGGAGE RAIL AT FS 559+112 RBL 9 CORRODED. REMOVED CORRODED FLOOR CARGO TRACK SEGMENT FS 559+112 RBL 9 BY REMOVING 11 SCREWS. INSTALLED NEW FLOOR CARGO TRACK SEGMENT IAW SRM 51-40-11 PG 8 ITEMS 6A THROUGH 6B(1), 51-41-02 PG 1 ITEM 2A THROUGH PG 3 ITEM 2C2(A), PG 5 ITEMS 3A THROUGH 3A(2)(D) AND 51-25-06 PG 3 ITEM 5A THROUGH PG 4 ITEM 5B(6).

Part: PLATE — CORRODED (BS 574-605) · airframe 26,722 hrs · 22,717 cycles

2 EA ANCHOR PLATES CORRODED AT LBL 9 BETWEEN FS 574 AND FS 605. RECEIVED TWO NEW SERVICEABLE ANCHOR PLATES. REMOVED AND INSTALLED TWO NEW SERVICEABLE ANCHOR PLATES IAW SRM 51-41-02.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 26,722 hrs · 22,717 cycles

FLOOR TRACK SEGMENT CORRODED AT FS 559+80 LBL 9. REMOVED CORRODED FLOOR SEAT TRACK SEGMENT FS 559+80 RBL 9 BY REMOVING 9 COUNTERSUNK SCREWS. INSTALLED NEW FLOOR SEAT TRACK SEGMENT IAW SRM 51-40-11, PG 8 ITEMS 6A THROUGH 6B(1), 51-41-02 PG 1 ITEM 2A THROUGH PG 3 ITEM 2C(2)(A), PG 5 ITEM 3A THROUGH 3A(2)(D) AND 51-25-06 PG 3 ITEM 5A THROUGH PG 4-5B(6).

Part: CARGO TRACK — CORRODED (BS 621) · airframe 26,722 hrs · 22,717 cycles

BAGGAGE RAIL AT FS 621 ON LBL 9 CORRODED. REMOVED CORRODED BAGGAGE RAIL AT FS 621 LBL 9 & INSTALLED NEW RAIL (SERVICEABLE) IAW SRM 51-41-00.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 26,722 hrs · 22,717 cycles

FLOOR SEAT TRACK SEGMENT CORRODED FS 559+80 RBL 27. REMOVED CORRODED SEAT TRACK FROM FS 559+80 RBL 27 IAW SRM 51-41-00. LOCATED & DRILLED NEW SERVICEABLE SEAT TRACK AT FS 559+80 RBL 27. INSTALLED SEAT TRACK P/N 601R387799 PO 112139 WITH SCREW P/N NAS517-3-4 PO 110856 IAW SRM 51-41-02 STEPS 1A, 2B(1), C1(A), 2(A), 3A2 (A-D).

Part: SILL — CORRODED (BS 559) · airframe 26,722 hrs · 22,717 cycles

FS 559.00+80 - FS 559.00+95.01 LT FLOOR SILL HAS CORROSION. REMOVED 9 EA NUTPLATES FROM LT FLOOR SILL IAW SRM 51-45-00 STEP 8 AND 51-42-10 FIG 4 AND REMOVED CORROSION IAW SRM 51-21-06 STEP 3E. REMOVED APPROX .003 MAX. TREATED & PRIMED AREA IAW SRM 51-21-11 STEP D & 51-25-06 AND INSTALLED NUTPLATES IAW SRM 51-45-00 STEP 9 & 51-42-15 STEP 6. APPLIED TOPCOAT TO TREATED AREAS IAW SRM 51-25-16 STEPS 3, 4 AND 5. INSPECTED AREA AND FOUND TO BE WITHIN LIMITS PER SRM 53-00-00 FIG 102.

Part: SILL — CORRODED (BS 409-559) · airframe 26,722 hrs · 22,717 cycles

PRESSURE FLOOR SILL FROM FS 409.00+128 TO FS 559.00 OTBD OF LBL 36 HAS SEVERAL AREAS OF CORROSION. CLEANED AND STRIPPED PAINT TO ACCESS CORROSION IAW AMM 51-26-00-150-803. C/W REO 601R-53-41-666 REV O.

Part: SILL — CORRODED (BS 409-559) · airframe 26,722 hrs · 22,717 cycles

PRESSURE FLOOR SILL FROM FS 409.00+128 TO FS 559.00 OTBD RBL 36 HAS SEVERAL AREAS OF CORROSION. CLEANED AND STRIPPED PAINT FOR ACCESS TO CORROSION IAW AMM 51-26-00-150-803. C/W EC/TC REO 601R-53-41-1163 AND REO 601R-53-41-1163 REV NC.

Part: PLACARD — MISSING (ESCAPE HATCH) · airframe 26,722 hrs · 22,717 cycles

CREW ESCAPE HATCH EXTERIOR SKIN MISSING ALL PLACARDS. REPLACED SILKSCREEN IAW AMM 11-10-03-400-801.

Part: BULKHEAD — CRACKED (BS 621) · airframe 26,722 hrs · 22,717 cycles

FS 621.00 PRESSURE BULKHEAD WEB HAS A 40 PERCENT FSH INDICATION NOTED .50" LONG AT LBL 36.20 WL 78.50 INDICAITON MARKED ON ACFT. FAILS NDT INSP AT THIS TIME. COMPLIED WITH EC/TC REO 601R-53-61-1285 AND PROCESSED M-93 WEIGHT CHANGE FORM AS REQUIRED. COMPLIED WITH EC/TC REO 601R-53-61-1285 AND PROCESSED M-93 WEIGHT CHANGE FORM AS REQUIRED.

Part: BULKHEAD — CRACKED (BS 621) · airframe 26,722 hrs · 22,717 cycles

FS 621.00 PRESSURE BULKHEAD WEB HAS AN 80 PERCENT FSH INDICATION NOTED APPROX 1.0" LONG AT LBL 27.50 WL 131.00 EXTENDING FROM THE UPPER VB CORNER OF THE AFT CARGO DOOR TRACK. AREA MARKED ON ACFT. FAILS NDT INSP AT THIS TIME. C/W EC/TC REO 601R-53-61-1541.

Part: BULKHEAD — CRACKED (BS 621) · airframe 26,722 hrs · 22,717 cycles

FS 621.00 PRESSURE BULKHEAD WEB HAS 2 INDICATIONS NOTED AT RBL 18.00 HEEL LINE. 1, 3.50" LONG INTERMITTENT 50 PERCENT FSH AT WL 108.50 & 2) 0.25" LONG 40 PERCENT FSH AT WL 133.00. AREAS MARKED ON ACFT. FAILS NDT INSPECTION AT THIS TIME. C/W EC/TC REO 601R-53-61-1285 AND PROCESSED M-93 WEIGHT CHANGE FORM AS REQUIRED. ACFT REQUIRES PRESSURIZATION CHECK. ASA EC/TC REO 601R-53-61-3525 REQUIRES COMPLIANCE. C/W EC/TC REO 601R-53-61-3525 AND REO 601R-53-61-3525

Part: ANGLE — CRACKED (BS 625) · airframe 26,722 hrs · 22,717 cycles

RT MID FS 625 OBLIQUE ANGLE IS CRACKED AT BL 45, STR R14 WL 97.5. R & R RT MID FS 625 OBLIQUE ANGLE IAW SRM 51-42-21. PAINTED OBLIQUE ANGLE IAW SRM 51-25-16.

Part: PLACARD — PEELING (PAX DOOR) · airframe 26,722 hrs · 22,717 cycles

PAX DOOR "EXIT" PLACARD IS PEELING. REMOVED PAX DOOR EXIT PLACARD IAW AMM 11-20-00-000-801. INSTALLED NEW PAX DOOR EXIT PLACARD IAW AMM 11-20-00-400-801.

Part: ANGLE — CRACKED (BS 625) · airframe 26,722 hrs · 22,717 cycles

LT MID FS 625 OBLIQUE ANGLE IS CRACKED AT BL 45, STR LT WL 97.5. R & R LT MID FS 625 OBLIQUE ANGLE IAW SRM 51-42-21. PAINTED OBLIQUE ANGLE IAW SRM 51-25-16.

Part: HANDLE — OUT OF ADJUST (PAX DOOR) · airframe 26,722 hrs · 22,717 cycles

PAX DOOR INNER HANDLE FAILED PULL TEST. ADJUSTED THE PAX DOOR FWD SPIGOT FITTING BY REMOVING .010 SHIM FROM UNDER SERRATED PLATE IAW MM 52-11-00-730-802, STEP 3A (23)(1)1-5 AND 18-62. PERFORMED PAX DOOR INNER HANDLE PULL TEST IAW MM 52-11-23-720-801 STEPS 3A(18)(A)(B)(C) AND FOUND INNER HANDLE PULL TO BE WITHIN LIMITS AND GOOD AT THIS TIME.

Part: PLACARD — WORN (CABIN) · airframe 26,340 hrs · 22,306 cycles

EXIT PLACARD ON PAX DOOR IS WORN AND NOT READABLE. F/A REPORTS "EXIT" DECAL ON MAIN AIRSTAIR DOOR NEEDS TO BE REPLACED.

Part: DOOR — STUCK (MAIN PAX) · airframe 26,201 hrs · 22,153 cycles

PAX DOOR GETS STUCK IN CLOSED POSITION, WILL NOT OPEN FROM INNER HANDLE.

Part: FRAME — CRACKED (BS 718 S11-12L) · airframe 26,190 hrs · 22,139 cycles

F.S. 718 LT FRAME HAS A PREVIOUS REPAIR BETWEEN STR 11L AND 12L THAT IS CRACKED. FRAME HOLES ALSO WILL NOT ALIGN WITH S/B 601R-53-055-01 ATTACH FITTINGS. REMOVED LT FS 718.00 FRAMED IAW SRM 51-42-06. INSTALLED NEW FRAME IAW SRM 51-42-06.

Part: FRAME — CRACKED (BS 718) · airframe 26,190 hrs · 22,139 cycles

FS 718 RT FRAME HAS A PREVIOUS REPAIR BETWEEN STR 11R AND 12R THAT IS CRACKED. FRAME HOLES ALSO WILL NOT ALIGN WITH S/B 601R-53-055-01 ATTACH FITTINGS. REMOVED FRAME IAW SRM 51-42-06. INSTALLED NEW FRAME IAW SRM 51-42-06.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 26,171 hrs · 22,118 cycles

WORKING APU DOOR POS UNKNOWN PER DML 478158-3

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 25,378 hrs · 21,329 cycles

IN FLIGHT RECEIVED SPOILERON CAUTION AND FLIGHT SPOILER CAUTION MESSAGE AND I/B GROUND SPOILER FAULT STATUS MESSAGE. EMERGENCY DECLARED.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 25,298 hrs · 21,253 cycles

DURING FLIGHT REC'D SPOILERON, FLT SPLRS, + GND SPLR DEPLOY. CAUTION MSGS COMPLIED WITH QRH GROUND SPOILERS WERE NOT DEPLOYED. EMERGENCY DECLARED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,839 hrs · 20,836 cycles

LT SIDE AFT EMERGENCY LIGHT IS INOP.

Part: STEP — CRACKED (ASD) · airframe 24,798 hrs · 20,796 cycles

ASD LOWER COMPOSITE STEP IS CRACKED ON THE FWD SIDE.

Part: BPSU — MALFUNCTIONED (T/E FLAP) · airframe 24,097 hrs · 20,136 cycles

FLAPS FAILED AT 20 DEGREES AND WOULD NOT RETRACT AFTER DEPARTURE. ENROUTE TO ATL A/C DIVERTED TO CAE DUE TO MTC. EMERGENCY VEHICLES ROLLED AS A PRECAUTION. R&R LT BPSU IAW CRJ-200 M/M 27-51-10. OPS CK GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 23,697 hrs · 19,788 cycles

LT SIDE OF FUSELAGE EXTERNAL AFT EMERGENCY LIGHT INOP. RELAMP LT SIDE OF FUSELAGE EXTERNAL AFT EMERGENCY LIGHT IAW AMM 33-51-21. OPS CHECK GOOD. (B)

Part: FCU — MALFUNCTIONED (TE FLAPS) · airframe 23,608 hrs · 19,700 cycles

FLAPS FAIL EICAS CAUTION MSG WHEN FLAPS SELECTED FROM 20 TO 30. FLT 4343 CX. REMOVED AND REPLACED FECU IAW CRJ200 AMM 27-51-05, OPS CHECK GOOD.

Part: LIGHT — BROKEN (CABIN) · airframe 22,749 hrs · 18,964 cycles

AAR-2150 - FLOOR EMERGENCY FLOOR LIGHT ON WARDROBE IS BROKEN.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 22,740 hrs · 18,957 cycles

RIGHT FS 640 BONDED SKIN DOUBLER CRACKED. REPAIRED RT 640.00 BONDED SKIN DOUBLER IAW REO 601R-53-61-506.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 22,740 hrs · 18,957 cycles

LEFT FS 640 BONDED SKIN DOUBLER WAS FOUND TO HAVE TWO CRACKS AS MARKED. COMPLIED WITH EC/TC REO 601R-53-61-2492.

Part: SIGN — INOPERATIVE (CABIN) · airframe 22,740 hrs · 18,957 cycles

AAR - LIGHTED FLOOR LEVEL EXIT SIGN AT LEFT OVERWING EXIT DID NOT LIGHT DURING OPS CHECK OF NR 4 CHARGER ASSEMBLY. UPON FURTHER REVIEW OF INSERTS ON FLOOR PANEL 271ELF FOUND INSERT TO BE LOOSE AND NOT DAMAGE REBONDED SAME SERVICEABLE INSERT IAW CMM REPAIR.

Part: FITTING — CRACKED (FUSELAGE) · airframe 22,740 hrs · 18,957 cycles

AAR - CLIP CRACKED O/B OF RBL 27.

Part: FITTING — CRACKED (FUSELAGE) · airframe 22,740 hrs · 18,957 cycles

AAR - CLIP CRACKED I/B OF RBL 36.

Part: FITTING — CRACKED (FUSELAGE) · airframe 22,740 hrs · 18,957 cycles

AAR - CLIP CRACKED O/B OF LBL 27.

Part: ANGLE — CRACKED (BS 625) · airframe 22,740 hrs · 18,957 cycles

RIGHT FS 625 OBLIQUE ANGLE IS CRACKED. REMOVED CRACKED RIGHT FS 625 OBLIQUE ANGLE. LOCATED NEW OBLIQUE ANGLE P/N 601-35012-52, IAW CRJ SRM 51-40-11. OK TO INSTALL. INSTALLED OBLIQUE ANGLE IAW CRJ SRM 51-42-21 AND REO 601R-53-61-985. OK TO TOP COAT FASTENERS FINISH A023. APPLIED FINISH A023 TO FASTENERS IAW CRJ SRM 51-21-16. SUPPLEMENTAL SDR CLOSED 1/23/08.

Part: HANDLE — DAMAGED (PAX DOOR) · airframe 22,361 hrs · 18,657 cycles

MAIN CABIN DOOR OUTER HANDLE WOULD NOT STOW FROM INSIDE OF A/C, HAD TO GET GROUND PERSONEL TO CLOSE FROM OUTSIDE. THAT STILL TOOK SEVERAL ATTEMPTS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,171 hrs · 17,702 cycles

SEVERAL EMERGENCY LIGHTS INOP.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 21,140 hrs · 17,679 cycles

NR 3 POWER PACK FOR EMERGENCY LIGHTS INOP.

Part: SIGN — NO TEST (EMERGENCY LIGHTS) · airframe 21,136 hrs · 17,675 cycles

OVERHEAD EMERGENCY EXIT SIGN DID NOT ILLUMINATE DURING TEST.

Part: SIGN — INOPERATIVE (CABIN) · airframe 21,126 hrs · 17,668 cycles

EMERGENCY EXIT SIGN AT ROW 8 WILL NOT ILLUMINATE.

Part: SIGN — INOPERATIVE (CABIN) · airframe 21,110 hrs · 17,658 cycles

EMERGENCY EXIT SIGN IN CENTER CABIN ROOF, FACING FWD, INOP.

Part: BULKHEAD — CRACKED (BS 621) · airframe 20,182 hrs · 16,950 cycles

FUSELAGE STATION 621 AFT PRESSURE BULKHEAD IS CRACKED BY UPPER CARGO DOOR CUTOUT STIFFENER ATTACH POINT. CRACK APPROX 0.025 IN LENGTH MARKED.

Part: WARNING MESSAGE — ILLUMINATED (COCKPIT) · airframe 20,046 hrs · 16,858 cycles

ON GEAR EXTENSION RECEIVED -GEAR DISAGREE WARNING MSG-. FOLLOWED QRH PROCEDURE AND ALL GEAR INDICATED DOWN AND LOCK. FLTS 4189, 4800 CX.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,622 hrs · 16,550 cycles

EMERGENCY LIGHTS INOP.

Part: CAUTION MESSAGE — ILLUMINATED (TE FLAPS) · airframe 19,281 hrs · 16,296 cycles

RECEIVED FLAP FAIL CAUTION MSG ON APPROACH INTO ATL, FLAPS WERE SET TO 8 DEG SPEED 210 KTS 5000 FT, (EMERGENCY DECLARED). FLTS 4106,4229 CX.

Part: STEP — BROKEN (PX DOOR) · airframe 18,411 hrs · 15,582 cycles

BOTTOM ASD STEP IS BROKEN.

Part: STRUCTURE — CORRODED (BS 349)

DURING A C-CHECK, THE FS 349 ATTACHMENT, LBL 36, WAS FOUND TO BE CORRODED. AFTER MAINTENANCE BLENDER, ALODINED, AND PRIMED THE FS 349 ATTACHMENT, LBL 36, IT WAS FOUND TO BE WITHIN ACCEPTABLE LIMITS IAW SRM. (K)

Part: ELEVATOR — CORRODED (EMPENNANGE)

DURING C-CHECK, THE RT ELEVATOR, AT THE FRONT SPAR AT RIB 1, WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE RT ELEVATOR, AT THE FRONT SPAR AT RIB 1 IAW AMM. (K)

Part: INTERCOSTAL — CRACKED (FUSELAGE)

DURING A C-CHECK, THE LT SIDE LOWER FS 625 CLIP WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LT FS 625 INTERCOSTAL IAW SRM. (K)

Part: SEAT TRACK — CORRODED (FUSELAGE)

DURING C-CHECK, THE LT FLOOR SEAT TRACK, AT FS 364 TO FS 394, WAS FOUND TO BE CORRODED AND DAMAGED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LT SEAT TRACK, AT FS 364 TO FS 394, IAW AMM. (K)

Part: ISOLATOR — BROKEN (FUSELAGE)

DURING C-CHECK, THE AFT PRESSURE BULKHEAD HAS BROKEN NUT PLATE ISOLATORS AT LBL9, RBL9, AND RBL36. THIS MRR WILL REMAIN OPEN PENDING MAINTENANCE DETERMINATION OF AN APPROPRIATE CORRECTIVE ACTION. (K)

Part: PLATE — CORRODED (FUSELAGE)

DURING A C-CHECK, THE PASSENGER DOOR HORIZONTAL PLATE, AT FS358, LBL 45, WAS FOUND TO BE CORRODED. THIS MRR WILL REMAIN OPEN PENDING MAINTENANCES DETERMINATION OF AN APPROPRIATE CORRECTIVE ACTION. (K)

Part: FLOORBEAM — CRACKED (FUSELAGE)

DURING C-CHECK, THE FS280 BEAM, AT RBL 9, WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE FS 280 BEAM, AT RBL 9, IAW REO. (K)

Part: PANEL — CORRODED (FUSELAGE)

DURING A C-CHECK, THE FLOOR PANEL 221ALF, RT ATTACH ANGLE WAS FOUND TO BE CORRODED BEYOND LIMITS. THIS MRR WILL REMAIN OPEN PENDING MAINTENANCES DETERMINATION OF AN APPROPRIATE CORRECTIVE ACTION. (K)

Part: ATTACH ANGLE — CORRODED

DURING A C-CHECK, THE FLOOR PANEL 221ALF, LT ATTACH ANGLE, WAS FOUND TO BE CORRODED BEYOND LIMITS. THIS MRR WILL REMAIN OPEN PENDING MAINTENANCES DETERMINATION OF AN APPROPRIATE CORRECTIVE ACTION. (K)

Part: ANGLE — CORRODED (FUSE FLOOR PANEL)

DURING A C-CHECK, THE FLOOR PANEL AFT ATTACH ANGLE, FS 280, WAS FOUND TO BE CORRODED. THIS MRR WILL REMAIN OPEN PENDING MAINTENANCES DETERMINATION OF AN APPROPRIATE CORRECTIVE ACTION. (K)

Part: CLIP — CRACKED (FS654)

DURING AC-CHECK, THE CLIP ON THE FORWARD FACE 654 WAS FOUND TO BE CRACKED. THIS MRR WILL REMAIN OPEN PENDING MAINTENANCES DETERMNATION OF AN APPROPRIATE CORRECTIVE ACTION. (K)

Part: DOUBLER — CORRODED (FUSELAGE)

DURING AC-CHECK, THE RT PRESSURE FLOOR OB SILL DOUBLER, FROM FS 409+128 TO FS 559, WAS FOUND TO BE CORRODED IN SEVERAL PLACES. THIS MRR WILL REMAIN OPEN PENDING MAINTENANCES DETERMINATION OF AN APPROPRIATE CORRECTIVE ACTION. (K)

Part: FLOORBEAM — CORRODED (FUSELAGE)

DURING A C-CHECK, THE FS 349 HORIZONTAL FLOORBEAM, LBL 36, WAS FOUND TO BE CORRODED. THIS MRR WILL REMAIN OPEN PENDING MAINT DETERMINATION OF AN APPROPRIATE CORRECTIVE ACTION. (K)

Part: ATTACH BRACKET — CORRODED (FUSELAGE)

DURING A C-CHECK, THE FS 349 ATTACHMENT, LBL 36, WAS FOUND TO BE CORRODED. AFTER MAINTENANCE BLENDED, ALODINED, AND PRIMED THE FS 349 ATTACHMENT, LBL 36, IT WAS FOUND TO BE WITHIN ACCEPTABLE LIMITS IAW SRM. (K)

Part: HANDLE — CORRODED (FUSELAGE)

DURING A C-CHECK, THE CREW ESCAPE HATCH DOOR HANDLE WAS FOUND TO HAVE CORROSION INSIDE THE HANDLE. MAINTENANCE REMOVED AND REPLACED THE CREW ESCAPE HATCH DOOR HANLE IAW CMM. (K)

Part: SKIN — CORRODED (FUSELAGE)

DURING C-CHECK, THE MIDDLE FUSELAGE AREA FROM FS 409.00+112 TO FS559.00, ON THE LT SIDE, WAS FOUND TO BE CORRODED. THIS MRR WILL REMAIN OPEN PENDING MAINTENANCES DETERMINATION OF AN APPROPRIATE CORRECTIVE ACTION. (K)

Part: PLATE — CRACKED (FUSELAGE)

DURING A C-CHECK, THE FORWARD HYDRAULIC ACCESS BAY, AROUND THE BRAKE CABLE HOLE, AT APPROXIAMATELY THE 7 OCLOCK POSITION, WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE FORWARD HYDRAULIC ACCESS BAY, AROUND THE BRAKE CABLE, AT APPROXIMATELY THE 7 OCLOCK POSITION IAW REO. (K)

Part: FLOORBEAM — CORRODED (FUSELAGE)

DURING A C-CHECK, THE FS 280 FLOORBEAM, BETWEEN LBL 9 AND RBL 9, FRONT STRINGER, WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REPAIRED THE FS 280 FLOORBEAM, BETWEEN LBL 9 AND RBL 9, FRONT STRINGER IAW REO. (K)

Part: LENS — CRACKED (CABIN)

DURING A C-CHECK, THE EMERGENCY EXIT LIGHT COVER, NEAR THE GALLEY, WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT COVER, NEAR THE GALLEY. (K)

Part: DOUBLER — CRACKED (FUSELAGE)

DURING A C-CHECK, THE RT FS 640 DOUBLER WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE RT FS 640 DOUBLER IAW SRM. (K)

Part: DOUBLER — CRACKED (FUSELAGE)

DURING C-CHECK, THE LT FS 640 DOUBLER WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LT FS 640 DOUBLER IAW SRM. (K)

Part: SERVO VALVE — MALFUNCTIONED (STEERING SYS)

DURING APPROACH, AT APPROXIMATELY 1,500 FT, THE CREW RECEIVED A STEERING INOPERATIVE MESSAGE. THE CREW COMPLIED WITH THE QRH AND REQUESTED THAT THE EMERGENCY VEHICLES BE DISPATCHED. THE AIRCRAFT LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE HYDRAULIC MANIFOLD AND THE HYDRAULIC SERVO VALVE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: STRUT — MALFUNCTIONED (STEERING SYS)

DURING APPROACH, AT APPROXIMATELY 1,500 FT, THE CREW RECEIVED A STEERING INOP MESSAGE. THE CREW COMPLIED WITH THE QRH AND REQUESTED THAT THE EMERGENCY VEHICLES BE DISPATCHED. THE AIRCRAFT LANDED SAFELY. (K)

Part: MANIFOLD — MALFUNCTIONED (HYD SYS)

DURING APPROACH, AT APPROXIMATELY 1,500 FT, THE CREW RECEIVED A STEERING INOPERATIVE MESSAGE. THE CREW COMPLIED WITH THE QRH AND REQUESTED THAT THE EMERGENCY VEHICLES BE DISPATCHED. THE AIRCRAFT LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE HYDRAULIC MAINIFOLD AND THE HYDRAULIC SERVO VALVE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICES. (K)

Part: TRANSDUCER — MALFUNCTIONED (HYDRAULIC SYS)

DURING CRUISE FROM MLI-ATL, THE CREW RECEIVED AN EICAS HYDRAULIC READOUT OF 1600 PSI WITH A SMALL LOSS OF HYDRAULIC QUANTITY ON SYSTEM NR 1. A MASTER CAUTION `OB GND SPLR` WAS ALSO RECEIVED. THE TOWER ELECTED TO DISPATCH EMERGENCY VEHCILES, AND THE AIRCRAFT DIVERTED INTO BNA, WHERE IT LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE PRESSURE TRANSDUCER IAW CRJ200 AMM 29-31-01. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: ODOR — DETECTED (UNKNOWN)

FLT 4523 - DURING CLIMB-OUT FROM BWI-ATL, AT APPROXIMATELY 15,000 FEET, THE F/O NOTICED AN ELECTRIC SMOKE ODOR COMING FROM THE FLOOR NEAR THE F/O`S FEET. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED INTO IAD, WHERE IT LANDED SAFELY. MAINTENANCE INSPECTED ALL LIGHT FIXTURES, WIRES, AND COMPONENTS IN THE COCKPIT, AVIONICS BAY, AND THE AFT EQUIPMENT BAY. NO DEFECTS WERE NOTED. BOTH ENGINES AND AIR CONDITION SYSTEMS WERE RAN FOR 45 MINUTES WITH NO DEFECTS NOTED. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LIGHT — SHORTED (CABIN)

DURING A GROUND INSPECTION, THE FORWARD SECTION OF EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED AN EMERGENCY FLOOR LIGHT STRIP IN THE FORWARD SECTION. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: LAMP — BURNED OUT (EMERGENCY LIGHT)

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

Part: SUPPORT BEAM — CRACKED (CENTER ENGINE)

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

Part: LAMP — BURNED OUT (EMERGENCY LIGHT)

FLT 4512 - DURING HANGAR MAINTENANCE IN BTR, THE LOWER LEFT EMERGENCY FLOOD LIGHT NEAR THE PASSENGER DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LOWER LEFT EMERGENCY FLOOR LIGHT LAMP NEAR THE PASSENGER DOOR. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: CONNECTOR — INOPERATIVE (EMERGENCY LIGHT)

DURING HANGAR MAINTENANCE IN BTR, THE EMERGENCY FLOOR LIGHTING AT ROW 7-C/D WAS FOUND TO BE INOPERATIVE. MAINTENANCE RESECURED THE ELECTRICAL CONNECTOR ON THE EMERGENCY FLOOR LIGHT TRACK AT ROW 7-C/D. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

DURING A GROUND INSPECTION IN MGM, THE RIGHT FORWARD OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE RIGHT FORWARD OVERWING EMERGENCY LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: BRACKET — CRACKED (FUSELAGE)

DURING HANGAR MAINTENANCE IN MCN, THE LEFT AND RIGHT ANGLE BRACKETS BELOW THE ENGINE SUPPORT BEAM WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LEFT AND RIGHT ANGLE BRACKETS BELOW THE ENGINE SUPPORT BEAM IAW SRM 51-00. (M)

Part: WINDSHIELD — CRACKED (COCKPIT)

FLT 4843 - DURING TAXI INTO DFW, THE CAPTAINS LEFT WINDSHIELD WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE CRACKED WINDSHIELD. PRESSURE AND OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LIGHT — INOPERATIVE (EXTERIOR)

FLT 4505 - DURING A SCHEDULED INSPECTION IN XNA, THE RIGHT EXTERNAL EMERGENCY LIGHT IN THE NR 2 POSITION WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BURNED OUT EXTERNAL EMERGENCY LIGHT BULB. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: SMOKE — DETECTED (CABIN)

APPROXIMATELY TWO MINUTES AFTER TAKEOFF, THE CAPTAIN RECEIVED A SMOKE TOILET MESSAGE. THE FLIGHT ATTENDANT CALLED APPROXIMATELY THREE SECONDS LATER TO REPORT THE SMELL OF SMOKE BUT NO ACTUAL SMOKE IN THE CABIN. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED FOR SAFE BUT OVERWEIGHT LANDING. MAINTENANCE PERFORMED THE OVERWEIGHT LANDING INSPECTION, AND NO DEFECTS WERE NOTED. MAINTENANCE INSPECTED THE AIRCRAFT RUNNING BOTH ENGINES AS WELL AS BOTH AIR CONDITIONER PACKS, BUT THE DISCREPANCY WAS NOT DUPLICATED. THERE WAS NO EVIDENCE OF FIRE, SMOKE, OR HEAT NOTED AT THAT TIME. AIRCRAFT RETURNED TO SERVICE.

Part: BULB — BURNED OUT (CABIN)

FLT 4787 - DURING A SCHEDULED INSPECTION IN XNA, THE AFT CEILING EMERGENCY FLOOD LIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BURNED OUT CEILING EMERGENCY LIGHT BULB. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LINE — LEAKING (RT ENGINE)

ON TAKEOFF FROM ATL, AT 1500 FEET, CAPTAIN NOTED RIGHT ENGINE OIL PRESSURE WAS AT 32 PSI AND FLUCTUATING. THE CAPTAIN THEN RECEIVED A RIGHT ENGINE OIL PRESSURE WARNING. THE ENGINE WAS SECURED, AND AN EMERGENCY WAS DECLARED. AIRCRAFT LANDED SAFELY IN ATL. MAINTENANCE INSPECTED AND FOUND THE B AND C SUMP LINES LEAKING. MAINTENANCE REMOVED AND REPLACED THE B AND C FITTING O-RINGS AND TIGHTENED THE OIL LINES AT THE OIL PUMP. THE ENGINE WAS RUN FOR FIVE MINUTES AT 85 PERCENT WITH NO LEAKS. AIRCRAFT RETURNED TO SERVICE. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DURING GROUND INSPECTION IN TOL, CREW REPORTED FLOOR LEVEL EMERGENCY TRACK LIGHTING INOPERATIVE AT ROWS 1-6. MAINTENANCE REMOVED AND REPLACED THE CABLE FLOOR TRACK LIGHTING ASSEMBLY AT ROWS 1-6. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: BEARING — FAILED (RT ENGINE)

DURING FLIGHT FROM AUS TO ATL, CREW RECEIVED A NR 2 ENGINE 'LOW OIL PRESS' LIGHT. CREW SHUT DOWN RIGHT ENGNIE FOLLOWING QRH AND DECLARED AN EMERGENCY. AIRCRAFT DIVERTED TO JAN AND LANDED SAFELY. MAINTENANCE PERFORMED MAGNETIC CHIP DETECTOR INSPECTION AS PER CRJ AMM 72-00-00 AND DETERMINED THE NR 2 ENGINE TO BE OUT OF LIMITS. MAINTENANCE REMOVED AND REPLACED THE RIGHT ENGINE. TEARDOWN REPORT FROM LUFTHANSA STATE THE ENGINE FAILURE WAS DUE TO A PTO DUPLEX BEARING FAILURE. THE BEARING CAGE WAS DAMAGED AND SOME BEARING BALLS WERE MISSING. (M)

Part: ENGINE — FAILED (NR 2)

FLT 4742 - DURING FLIGHT FROM AUS TO ATL, CREW RECEIVED A NR 2 ENGINE 'LOW OIL PRESSURE' LIGHT. CREW SHUT DOWN RIGHT ENGINE FOLLOWING QRH AND DECLARED AN EMERGENCY. AIRCRAFT DIVERTED TO JAN AND LANDED SAFELY. MAINTENANCE PERFORMED MAGNETIC CHIP DETECTOR INSPECTION AS PER CRJ AMM 72-00-00 AND DETERMINED THE NR 2 ENGINE TO BE OUT OF LIMITS. MAINTENANCE REMOVED AND REPLACED THE RIGHT ENGINE. (M)