N826AS

Part: BLADES — DAMAGED (TURBINE SECTION) · airframe 36,227 hrs · 32,039 cycles

RT ENGINE FLAMED OUT ON DESCENT AT 4000 & 250 KIAS. ATTEMPTED RELIGHT UNSUCCESSFUL. COMPLIED WITH WITH AREA C BOROSCOPE INSPECTION IAW MANUAL 72-00-00. FOUND DAMAGE BLADES ON STAGE 6 T/E. R & R RT ENGINE IAW AMM 71-00-00. OP'S AND LEAK CHECK GOOD.

Part: WIRE — SHORTED (EMERGENCY LIGHT) · airframe 35,121 hrs · 31,069 cycles

EMERGENCY LIGHTS COME ON IN ARM POSTION. FOUND WIRE LQ1AZZ SHORTED IAW ESPM 20-12-01. INSTALLED SPLICE ON WIRE LQ1AZZ IAW ESPM 20-16-00. PERFORMED OPS TEST OF SERVICE LIGHTS IAW AMM 33-31-00-710-801. OPS CHECKED GOOD.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 35,121 hrs · 31,069 cycles

EMERGENCY LIGHTS AT PAX DOOR INOPERATIVE. EMERGENCY LIGHT HAS A CONNECTOR DAMAGED. INSTALLED NEW PIN AND CONNECTOR ONTO WIRE OF EMERGENCY LIGHT IAW ESPM 20-11-00, 20-12-00-20-17-10.

Part: STRUCTURE — CORRODED (PAX DOOR) · airframe 35,121 hrs · 31,069 cycles

PAX DOOR AFT BOTTOM CORNER CORRODED. REMOVED PAX DOOR AFT BOTTOM CORNER (2 PART) IAW SRM 51-42-06. INSTALLED NEW ASD AFT BOTTOM CORNER (2 PART) IAW SRM 51-42-06 DWG NR 600-31998. REPAIR CLASSIFIED AS MAJOR.

Part: STRUCTURE — CORRODED (PAX DOOR) · airframe 35,119 hrs · 31,068 cycles

PAX DOOR FWD BOTTOM CORNER CORRODED. REMOVED FWD BOTTOM CORNER (2 PART) IAW SRM 51-42-06. INSTALLED NEW ASD FWD BOTTOM CORNER IAW SRM 51-42-06, 51-42-21. REPAIR CLASSIFIED AS MAJOR.

Part: FLOOR SUPPORT — CORRODED (BS 409-559) · airframe 35,119 hrs · 31,068 cycles

DURING REINSPECTION IAW EO 600-53-216/01 ADDITIONAL CORROSION ON LT FLOOR SUPPORT FROM FS 409 + 128 - FS 559.00 WAS FOUND. REMOVED CORROSION IAW SRM 51-21-06 35. FOUND TO BE OUT OF LIMITS IAW GREO 601R-53-41-666. COMPLIED WITH REO 601R-53-41-666 AND REO 601R-53-41-1625.

Part: FLOOR SUPPORT — CORRODED (BS 409-559) · airframe 35,119 hrs · 31,068 cycles

DURING REINSPECTION IAW EO 600-53-216/01 FOUND ADDITIONAL CORROSION ON FLOOR SUPPORT FROM FS 409 + 128 TO FS 559.0 ON RT SIDE. REMOVED CORROSION IAW SRM 51-21-06, 33 AREAS. FOUND TO BE OUT OF LIMITS OF GREO 601R-53-41-666. COMPLIED WITH REO 601R-53-41-1624 AND REO 601R-53-41-1674.

Part: ISOLATOR — BROKEN (AFT BULKHEAD) · airframe 35,119 hrs · 31,068 cycles

TWO ISOLATORS BROKEN ON AFT BULKHEAD. REMOVED AND REPLACED ISOLATORS IAW SRM 51-42-13.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 35,119 hrs · 31,068 cycles

PAX DOOR AFT DRAG ANGLE CRACKED AT RIVET. REPAIRED IAW GREO 601R-52-11-513. COMPLIED WITH EC/TC REO 601R-52-11-513.

Part: FLAP SYSTEM — UNKNOWN · airframe 33,944 hrs · 30,055 cycles

FLAPS FAIL AT ZERO WHEN SELECTING FLAPS AT EIGHT. EMERGENCY DECLARED . COMPLIED WITH AD 2009-06-12. PERFORMED TROUBLESHOOTING IAW FIM 27-50-00. FOUND NO FAULTS LOGGED IN FECU AND MDC. PERFORMED OPS TEST OF FLAPS. NO DEFECTS NOTED AND OP'S CHECKED GOOD IAW AMM 27-54-00.

Part: WARNING MESSAGE — FALSE ACTIVATION (HYD TEMP) · airframe 33,645 hrs · 29,803 cycles

AT FL 290, RECEIVED A HYD NR 2 HIGH TEMP CAUTION MESSAGE. COMPLIED WITH QRH AN LANDED AT NEAREST SUITABLE AIRPORT. EMERGENCY DECLARED. COULD NOT DUPLICATE COMPLAINT, PERFORMED FUNCTIONAL TEST OF HYD SYS 2 TEMP INDICATION IAW AMM 29-10-00-720-802. NO FURTHER DEFECTS NOTED, ALSO RAN ENGINE AT POWER SETTING IAW AMM 71-00-00, COULD NOT DUPLICATE.

Part: BPSU — OUT OF ADJUST (TE FLAPS) · airframe 33,642 hrs · 29,800 cycles

FLAP FAIL AT ZERO DEGREES. EMERGENCY DECLARED. RIGGED LT AND RT BPSU, IAW AMM 27-51-01, PERFORMED ADJUSTMENT TEST OF FECU IAW AMM 27-51-05-05. OPS CHECKED GOOD, ACFT OK FOR SERVICE.

Part: DETECTOR — FAILED (FLAP SKEW) · airframe 33,472 hrs · 29,650 cycles

FLAPS FAILED AT 0 DEGREES DURING CRUISE ALT NORMAL LANDING. EMERGENCY DECLARED. R & R SKEW DETECTION UNIT IAW AMM 27-51-15.

Part: PUMP — FAILED (HYD SYSTEM) · airframe 33,431 hrs · 29,614 cycles

CLIMBING OUT OF SAV RECEIVED HYD 2 HI TEMP. FOLLOWED QRH TEMP CONTINUED TO CLIMB ABOVE 135 DEGREES C. DIVERTED, IAW QRH. EMERGENCY DECLARED. R & R NR 2 ENGINE DRIVEN HYD PUMP IAW AMM 29-11-01. OPS AND LEAK CHECKS GOOD.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 33,254 hrs · 29,453 cycles

EMERGENCY LIGHTS LEFT IN ON POSTION OVERNIGHT AND DISCHARGED THE BATTERIES, EMERGENCY LIGHTS NOW INOP. OPS CHECKED GOOD IAW AMM 33-51-00.

Part: COOLING DUCT — DISCONNECTED · airframe 32,692 hrs · 28,912 cycles

COOL CAUTION MESSAGE DISPLAYED SHORTLY AFTER T/O, RAN QRH PRECEDURE, MESSAGE PERSISTED, ED T-4 EACH DISLAYED OVERHEAT AND ALL MESSAGE EXTINGUISHED. ( ACFT DIVERTED -- EMERGENCY DECLARED AS A PRECAUTION) CONNECTED THE SUPPLY DUCT TO PLENUM WITH CLAMP IAW AMM-21-24-22 INSPECTED DISPLAY COOL FILTERS AND LOW FLOW DETECTOR IAW AMM-21-24-07 INSPECTED ALL CRT'S. CLEARED AND PERFORMED OPS TEST OF PFD'S MFD'S IAW AMM 34-25-00 NO DEFECTS NOTED.

Part: DOOR — BINDING (MAIN PAX) · airframe 32,092 hrs · 28,394 cycles

PAX DOOR WILL NOT OPEN FROM OUTSIDE. OPS CHECK PAX DOOR SEVERAL TIMES IAW AMM 52-11-00. OPS CHECK GOOD NO FURTHER DEFECTS FOUND.

Part: LATCH — BINDING (PAX DOOR) · airframe 31,527 hrs · 27,909 cycles

F/A STATES THAT MAIN CABIN DOOR LATCH WOULD NOT ACTUATE THE FIRST FEW TIMES TRIED TO OPEN THE DOOR UPON ARRIVAL. OPERATED PAX DOOR SEVERAL TIMES NO DEFECTS NOTED, OPS CHECKED GOOD IAW AMM 52-11-00.

Part: HANDLE — DAMAGED (PAX DOOR) · airframe 31,434 hrs · 27,825 cycles

MAIN DOOR WILL NOT OPEN. RESECURED PAX DOOR INSIDE HANDLE STRAP IAW AMM 52-11-02. OPS CHECK GOOD AT THIS TIME. (CLOSED)

Part: DOOR — LACK OF LUBE (MAIN PAX) · airframe 31,434 hrs · 27,825 cycles

MAIN DOOR CATCHES WHEN TRYING TO OPEN FROM OUTSIDE. PERFORMED LUBRICATION OF PAX DOOR IAW AMM 12-20-52. OPS CHECK GOOD AT THIS TIME. (CLOSED)

Part: HANDLE — OUT OF RIG (PAX DOOR) · airframe 31,191 hrs · 27,597 cycles

PAX DOOR HANDLE IS VERY HARD TO OPEN AND STOW. APPEARS TO BE IMPROPERLY RIGGED. REMOVED PAX DOOR ACCESS PANELS. REMOVED CLOSING PLATE UNDER BOTTOM FOLDING STOP IAW AMM 52-11-23-820-801, STEP 3.A.2. REMOVED PAX DOOR STAIR PANELS IAW AMM 52-11-04-000-808 AND 52-11-04-000-810. INSTALLED PAX DOOR STAIR PANELS IAW MM 52-11-04-400-807 AND 52-11-04-400-810. OPS CHECKS GOOD. PERFORMED PAX DOOR ADJUSTMENT, SYS TEST AND OPS TEST IAW AMM 52-11-03-710-801, 52-11-00-730-802 AND 52-11-03-710-801. OPS CHECKS GOOD AT THIS TIME.

Part: LIGHT — BROKEN (CABIN)

FLOOR EMERGENCY FLOOD LIGHT ON WARDROBE IS BROKEN. REPLACED EMERGENCY FLOOR LIGHT ON LOWER WARDROBE ASSY IAW AMM 33-51-19-400-801. OPS CHECKED GOOD IAW AMM 35-51-00-710-801.

Part: SKIN — CORRODED (BS 559-574)

CORROSION ON BELLY SKIN AROUND FASTENERS STA 559+112 TO FS 574 BETWEEN STR 23R-24L.

Part: FRAME — CORRODED (BS 333) · airframe 31,174 hrs · 27,580 cycles

FS 333, FRAME IN BELLY IS CORRODED. PRIMED AND PAINTED REPAIR AREA IAW SRM 51-25-01. THIS REPAIR REQUIRES MAJOR/MINOR CLASSIFICATION IAW ASA SOP 5702. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW ASA SOP 5702. APPLIED CORROSION INHIBITOR TO BARE AREAS IAW AMM 51-25-56-390-802.

Part: SKIN — CORRODED (BS 559-574) · airframe 31,174 hrs · 27,580 cycles

CORROSION ON BELLY SKIN AROUND FASTENERS STA 559+112 TO 574 BETWEEN STR 23R-24L. DOUBLER INSTALLED IAW REO 601R-53-61-3943

Part: BEAM — CRACKED (FUSELAGE) · airframe 31,174 hrs · 27,580 cycles

ON THE ECU SUPPORT FRAME THE OTBD FWD BEAM ASSY IS CRACKED, PN 601R95156-66, AND THE INBD BEAM ASSY IS GOUGED. REMOVED INBD BEAM ASSY, PN 601R95155-76, IAW SRM 51-42-06. INSTALLED NEW SERVICEABLE INBD BEAM, PN 601R95155-82 AND ANGLE, 601R95156-63 IAW SRM 51-42-06, 51-42-21, 51-41-04, DWG 601R95100. REMOVED OTBD FWD BEAM, PN 601R95-156-66, IAW SRM 51-42-06. INSTALLED NEW BEAM, PN 601R95-156-70, IAW SRM 51-42-06. THIS REPAIR IS CLASSIFIED AS A MINOR REPAIR.

Part: INTERCOSTAL — CORRODED (BS 559) · airframe 31,174 hrs · 27,580 cycles

INTERCOSTAL CAP AT FS 559.00+80 BETWEEN RBL 9, 27 & FLOOR SUPPORT IS CORRODED. R & R INTERCOSTAL CAP AT FS 559.00+80 BETWEEN RBL 27 & RBL 9 FLOOR SUPPORT IAW SRM 51-42-06 & SRM 521-42-15. THIS REPAIR IS CLASSIFIED AS A MINOR REPAIR IAW ASA SOP 5702. (CLOSED)

Part: SKIN — CRACKED (BS 235) · airframe 31,174 hrs · 27,580 cycles

FUSELAGE SKIN IS CRACKED AT FS 235, LT SIDE BL 6.0, RT SIDE HAS BEEN PREVIOUSLY REPAIRED USING REO 601R-53-11-048. REPAIRED IAW REO 601R-53-11-2038.

Part: INTERCOSTAL — CRACKED (CARGO BAY) · airframe 31,174 hrs · 27,580 cycles

CARGO TIE DOWN PAN AFT LOCATION HAS OTBD, AFT END CRACKED AT FASTENER HOLE ON INTERCOSTAL. R & R INTERCOSTAL, 601R35031-205, IAW SRM 51-42-06. (CLOSED)

Part: ANGLE — CRACKED (DOOR SILL) · airframe 31,174 hrs · 27,580 cycles

ANGLE UNDER CARGO SUPPORT SILL CRACKED. R & R ANGLE WITH SERVICEABLE ANGLE IAW SRM 51-42-21. THIS REPAIR IS CLASSIFIED AS A MINOR REPAIR IAW ASA SOP 5702.

Part: STRINGER — CORRODED (BS 336-338) · airframe 31,174 hrs · 27,580 cycles

STRINGER 26 RT HEAVILY CORRODED/PITTED AROUND RIVETS APPROX 1/2" 0 0.035" DEEP A FS 336 & 338. INSTALLED NEW STRINGER SEGMENT IAW SRM 53-00-03.

Part: SKIN — CORRODED (BS 559-574) · airframe 31,174 hrs · 27,580 cycles

CORROSION ON BELLY SKIN AROUND FASTENERS STA 559+112 TO 574, BETWEEN STR 23R-24L. REMOVED CORROSION FROM BELLY SKIN IAW SRM 51-21-06. FOUND TO BE WITHIN LIMITS IAW SRM 53-00-31 3C.

Part: POST — CRACKED (BS 409) · airframe 31,174 hrs · 27,580 cycles

FOUND FS 409+128 VERTICAL POST RBL 18.0 INBD SIDE HAS INDICATION NOTED APPROX .2" IN LENGTH 55 PERCENT FSH AT WL 69.0 AFT FLANGE RADIUS. FAILED NDT INSP. REMOVED VERTICAL POST IAW SRM 51-42-06. INSTALLED NEW POST IAW SRM 51-42-06 AND 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 REVISION A.

Part: FRAME — CORRODED (BS 333) · airframe 31,174 hrs · 27,580 cycles

FS 333, FRAME IN BELLY IS CORRODED. REMOVED CORRODED FRAME FROM FS 333 IAW SRM 51-42-06 AND 51-742-21. LOCATED AND DRILLED NEW FS 333 FRAME PIN 601R32004-55 AND INSTALLED IAW SRM 51-40-11, 51-42-21 & 51-42-06.

Part: FLOOR SUPPORT — CORRODED (BS 574-621) · airframe 31,174 hrs · 27,580 cycles

FLOORBEAM CAP AT RBL 27, FS 621 TO 574 IS CORRODED. BLENDED CORROSION ON FLOORBEAM CAP LBL 27 IAW REO 601R-53-60-005, REV A AND FOUND TO BE OUT OF LIMITS IAW REO 601R-53-00-005. REMOVED FLOORBEAM CAP IAW SRM 51-42-06. LOCATED AND DRILLED NEW CAP IAW SRM 51-40-11. INSTALLED IN FLOORBEAM CAP IAW REO 601R-53-61-3941 AND SRM 51-41-04 AND 51-42-21.

Part: SILL — CORRODED (FUSELAGE) · airframe 31,174 hrs · 27,580 cycles

CARGO DOOR CUTOUT FLOOR SUPPORT SILL IS CORRODED. REPLACED CARGO DOOR SILL PLATE IAW REO 601R-53-61-1574 & REO 601R-53-61-1574.

Part: FLOOR SUPPORT — CORRODED (BS 559-621) · airframe 31,174 hrs · 27,580 cycles

RT CARGO FLOOR SUPPORT FROM FS 621 TO 559+112 IS CORRODED. REMOVED MINOR CORROSION FROM RT FLOOR SUPPORT IAW SRM 51-21-06 APPROX .001 - .002. MATERIAL REMOVED WITHIN LIMITS. REPAIR IS CLASSIFIED AS A MINOR.

Part: INTERCOSTAL — CORRODED (BS 589) · airframe 31,174 hrs · 27,580 cycles

INTERCOSTAL CAP AT FS 589 BETWEEN RBL 9 AND 27 IS CORRODED. REMOVED MINOR CORROSION ON INTERCOSTAL CAP, MAT LOSS .006 IAW SRM 51-21-06, 51-21-11 & 51-25-16. REPAIR CLASSIFIED AS A MINOR REPAIR.

Part: INTERCOSTAL — CORRODED (BS 589) · airframe 31,174 hrs · 27,580 cycles

INTERCOSTAL CAP AT FS 589 BETWEEN LBL 9 AND 27 IS CORRODED. REMOVED MINOR CORROSION ON INTERCOSTAL CAP AT FS 589 BETWEEN RBL & LBL 9 MAT LOSS .006 IAW SRM 51-21-06, 51-21-11 & 51-25-15. REPAIR CLASSIFIED AS A MINOR.

Part: SILL — CORRODED (BS 589) · airframe 31,174 hrs · 27,580 cycles

INTERCOSTAL CAP AT FS 589 BETWEEN RBL 27 AND FLOOR SUPPORT SILL IS CORRODED. REMOVED MINOR CORROSION ON INTERCOSTAL CAP, MAT LOSS .006 IAW SRM 51-21-06, 51-21-11 & 51-25-16. REPAIR CLASSIFIED AS A MINOR.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 31,174 hrs · 27,580 cycles

LT AND RT FWD SEAT TRACK SEGMENTS ARE CORRODED. REMOVED 1 EA LT & RT FWD FLOOR SEAT TRACK SEGMENTS DUE TO CORROSION IAW AMM 53-01-11-000-802, STEPS 3B1-3B3. INSTALLED NEW LT & RT FWD FLOOR SEAT TRACK SEGMENTS IAW AMM 53-01-11-420-001, STEPS 3B1-3B8.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 31,174 hrs · 27,580 cycles

CARGO SEAT TRACK AT RBL 9 FS 559+112 AND 559+80 IS CORRODED. R & R SEAT TRACK SEGMENT IAW AMM 20-21-00-910-801.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 31,174 hrs · 27,580 cycles

CARGO SEAT TRACK AT RBL 27, FS 559+80 IS CORRODED. INSTALLED NEW CARGO TRACK IAW AMM 53-01-11-400-802.

Part: INTERCOSTAL — CORRODED (BS 589) · airframe 31,174 hrs · 27,580 cycles

INTERCOSTAL CAP AT FS 589 BETWEEN RBL AND LBL 9 IS CORRODED. BLENDED CORROSION ON FLOORBEAM IAW REO 601R-53-60-005, REV A AND FOUND TO BE OUT OF LIMITS REO 601R-53-00-005. REMOVED FLOORBEAM CAP FROM IAW SRM 51-42-06. LOCATED AND DRILLED NEW FLOORBEAM CAP IAW SRM 51-40-11. INSTALLED IN FLOORBEAM CAP IAW REO 601R-53-61-3941 AND SRM 51-41-04 AND 51-42-21.

Part: FLOOR SUPPORT — CORRODED (BS 574-621) · airframe 31,174 hrs · 27,580 cycles

FLOORBEAM CAP AT RBL 9 FS 621 TO FS 574 IS CORRODED. BLENDED CORROSION OF FLOORBEAM CAP IAW REO 601R-53-00-005. FOUND TO BE OUT OF LIMITS. REMOVED FLOORBEAM CAP IAW SRM 51-42-06. LOCATED AND DRILLED NEW FLOORBEAM CAP IAW SRM 51-40-11. INSTALLED NEW SERVICEABLE FLOORBEAM CAP IAW REO 601R-53-61-3941 AND SRM 51-41-02.

Part: SEAT TRACK — CORRODED (BS 574-621) · airframe 31,174 hrs · 27,580 cycles

CARGO SEAT TRACK AT LBL 9 FS 621, FS 574 AND FS 559+80 IS CORRODED. REMOVED MINOR CORROSION ON INTERCOSTAL CAP, MAT LOSS .006 IAW SRM 51-21-06, 51-21-11 & 51-25-15. REPAIR CLASSIFIED AS A MINOR.

Part: ISOLATOR — CRACKED (BS 621 BULKHEAD) · airframe 31,174 hrs · 27,580 cycles

FS 621, PRESS BULKHEAD HAS CRACKED ISOLATORS AT RBL 27 (1), LBL 18 (2), LBL 27. REMOVED ISOLATOR MOUNTS. R & R ISOLATOR BRACKETS PN SL2337-3. REINSTALLED ISOLATOR MOUNTS IAW SRM 51-42-06 AND 51-23-00. PRIME TOUCHED UP ISOLATORS ASSY IAW SRM 51-25-06. THIS REPAIR IS CLASSIFIED AS A MINOR REPAIR IAW ASA SOP 5702.

Part: FRAME — CRACKED (BS 718) · airframe 31,174 hrs · 27,580 cycles

LT AND RT 718 FRAMES ARE CRACKED BEHIND THE ACM'S. REF MWC CO 7210411, JOB 8721046, OPS 17 AND 18.

Part: FLOORBEAM — CORRODED (BS 621) · airframe 30,167 hrs · 26,701 cycles

CARGO BAY UNDER FLOOR , FLOORBEAM AT LBL 27.00 HAS CORROSION AT MULTIPLE NUTPLATES JUST OF FS 621.00. RELAMPED AFT CABIN CEILING LIGHT IAW AMM 33-51-16. OPS CHECK GOOD.

Part: COVER — CRACKED (EMERGENCY LIGHT) · airframe 30,167 hrs · 26,701 cycles

EMERGENCY LIGHT STRIPS CRACKED AT SEAT LOCATION APPOX 11AB, 11DC, 13AB, 8AB, 5AB, 5DC AND CABIN ENTRY THRESHOLD LT SIDE. REPLACED COVER OVER LIGHT STRIPS APPROX AT SEAT LOCATIONS 11AB, 11DC, 13AB, 8AB, 5AB, 5DC IAW AMM REF 33-51-01-400-806.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 29,136 hrs · 25,732 cycles

CABIN EMERGENCY LIGHTS WILL NOT ILLUMINATE. PLACED EMERGENCY LIGHT SWITCH IN ARMED POSITION AND CHARGED EMERGENCY LIGHT BATTERY. OPS CHECKED GOOD IAW AMM 33-51-00

Part: BULB — BURNED OUT (FLASHLIGHT) · airframe 28,396 hrs · 24,946 cycles

BULB IN F/O FLASHLIGHT BURNED OUT.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 28,010 hrs · 24,528 cycles

GEAR DISAGREE POSTED WHEN SELECTED DOWN FOR LANDING. COMPLIED WITH QRH NOSE GEAR, EMERGENCY DECLARED.

Part: SIGN — BROKEN (PAX DOOR) · airframe 26,501 hrs · 23,051 cycles

PAX DOOR EXIT SIGN BROKE.

Part: PLATE — BROKEN (CABIN) · airframe 26,427 hrs · 22,986 cycles

JOB 8721025 OPERATION 118 WARDROBE EMERGENCY EXIT FLOOR LEVEL FLOOR LIGHT BASE PLATE BROKEN.

Part: SEAL — LACK OF LUBE (EMERGENCY EXIT)

JOB 8721021 OPERATION 170 RT OVERWING EMERGENCY EXIT FAILED TO OPEN AT 30 10 LBF. RESOLVED ON W/0 98649 TASKCARD NR 00220. C/A CLEANED AND APPLIED DC33 TO SEAL AND PINS ON RT OVERWING EMER EXIT. PERFORMED FUNC TEST OF EXIT IAW CRJ 200 AMM 52-21-00-720-801. FOUND HANDLE OPERATING WITHIN LIMITS AT THIS TIME. ASARII C/W 5300014

Part: SEAL — LACK OF LUBE (EMERGENCY EXIT)

JOB 8721021 OPERATION 169 LT OVERWING EMERGENCY EXIT FAILED TO OPEN AT 30 10 LBF. RESOLVED ON W/O 98649 TASKCARD NR 00219. C/A CLEANED AND APPLIED LUBE DC33 TO SEAL AND PINS ON LT OVERWING EMER EXIT. PERFORMED FUNC TEST OF EXIT IAW CRJ 200 AMM 52-21-00-720-801. FOUND HANDLE OPERATING WITHIN LIMITS AT THIS TIME. ASA RII C/W 53000

Part: COVER — BROKEN (CABIN)

JOB 8721021 OPERATION 105 LT WINDSCREEN EXIT SIGN COVER IS BROKEN ON CORNER. RESOLVED ON W/O 98649 TASKCARD NR 00131. C/A R&R EXIT SIGN COVER ON LT WINDSCREEN IAW CRJ 200 AMM 33-51-13-400-801.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 26,307 hrs · 22,873 cycles

LT EXTERIOR AFT EMERGENCY LIGHT INOPERATIVE. RELAMP LT AFT EMERGENCY EXTERIOR LIGHT IAW 33-51-21. (S)

Part: LIGHT — BROKEN (CABIN) · airframe 25,718 hrs · 22,347 cycles

ENTRANCE EMERGENCY LIGHT BASE BROKEN (RESOLVED ON W/O: 89597 TASKCARD: N/R-00002) R/R ENTRANCE EMERGENCY LIGHT ASSY IAW CRJ 200 AMM 33-51. OP CK GOOD.--[SDR CLOSED](B)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,731 hrs · 21,524 cycles

NR 1 EMERGENCY LIGHT BATTERY WILL NOT TURN ON LIGHTS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,731 hrs · 21,524 cycles

NR 4 EMERGENCY LIGHT BATTERY WILL NOT TURN ON LIGHTS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,731 hrs · 21,524 cycles

NR 2 EMERGENCY LIGHT BATTERY WILL NOT TURN ON LIGHTS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,731 hrs · 21,524 cycles

NR 3 EMERGENCY LIGHT BATTERY WILL NOT TURN ON LIGHTS.

Part: INTERCOSTAL — CRACKED (BS 484) · airframe 24,731 hrs · 21,524 cycles

FOUND LT SIDE FS 484 INTERCOSTAL INBD CLIP CRACKED.

Part: LIGHT — BROKEN (EMERGENCY EXIT) · airframe 24,731 hrs · 21,524 cycles

F/A STATION EXIT LIGHT ASSY IS CRACKED AND BROKEN.

Part: SKIN — CRACKED (ENGINE SUPPORT) · airframe 24,731 hrs · 21,524 cycles

ENGINE SUPPORT BOX BEAM UPPER SKIN HAS 17/32 INCH CRACK AT AFT CENTER SECTION JUST I/B OF RBL 9.500 SEE AFDL 311351 ITEM 2.

Part: PLACARD — WORN (PAX DOOR) · airframe 24,731 hrs · 21,524 cycles

PAX DOOR STEP "EXIT" PLACARD IS WORN.

Part: COVER — LOOSE (CABIN) · airframe 24,533 hrs · 21,360 cycles

EMERGENCY TRACK LIGHTING COVER LOOSE AT ROW 1 AND END CAP MISSING. FLT 4630 DEL 28 MINS.

Part: STRIP — LOOSE (CABIN) · airframe 24,045 hrs · 20,953 cycles

EMERGENCY LIGHT STRIP LOOSE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,855 hrs · 20,066 cycles

LEFT SIDE EMERGENCY LIGHT AND RT SIDE WING INSPECTION LIGHT OUT.

Part: DOOR — STIFF (MAIN PAX) · airframe 21,785 hrs · 19,242 cycles

PAX DOOR HARD TO SECURE.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 21,599 hrs · 19,095 cycles

FOUND CORROSION ON CABIN FLOOR SEAT TRACKS FROM FS 349.00 TO FS 559.00.

Part: BULKHEAD — CRACKED (BS 202) · airframe 21,599 hrs · 19,095 cycles

PRESSURE BULKHEAD FUS STA 202.75 CRACKED AT PARKING BRAKE CABLE 11 O'CLOCK VIEW LOOKING AFT (RESOLVED ON W/O: 33166 TASKCARD: N/R-00311 ) PERFORMED EDDY CURRENT INSPECTION OF PRESSURE BULKHEAD AT F.S. 202.75, PARKING BRAKE CABLE, I/A/W CRJ 200 NDTM 51-20-06. BULKHEAD IS CRACKED AT 11 O'CLOCK AND 7 O'CLOCK POSITION LOOKING AFT. INFO ONLY---FOUND CRACK AT 1100 POSITION TO END .150 FROM ADDED FASTNER IN EXISTING REPAIR. REQUEST ENGINNERING ASSISTANCE. REMOVED AFT DOUBLER PER SRM 51-42-06. FABRICATED NEW DOUBLER FROM 2024T3 .063". DRILLED AND STARTED TRIMMING DOUBLER. PER REO 601R-53-11-1048. REMOVED DAMAGED AREA PER REO 601R-53-11-1048. PERFORMED EDDY CURRENT INSPECTION OF CUT LINE ON PRESSURE BULKHEAD AT F

Part: FLOORBEAM — CORRODED (BS 349) · airframe 21,598 hrs · 19,094 cycles

FLOORBEAM AT FUS STA 349, OB OF RBL 27 HAS CORROSION UNDER NUTPLATES (MARKED).

Part: FLOORBEAM — CORRODED (BS 349) · airframe 21,598 hrs · 19,094 cycles

FUS STA 349, OB OF LBL 27 HAS CORROSION ON ANGLE, AFT SIDE OF FLOORBEAM.

Part: PRESSURE PANEL — CORRODED (LT WING) · airframe 21,598 hrs · 19,094 cycles

LT OVER WING PRESSURE FLOOR HAS LIGHT SURFACE CORROSION. AT MARKED AREAS FUS STA 473 AND 529. BLENDED ( WITHIN LIMTS ) LT OVER WING PRESSURE FLOOR (.002 REMOVED).PER CRJ 200 SRM 51-41-43 LT OVER WING PRESSURE FLOOR ALODINED PRIMED PAINTEDAND DYNATRUALED.PER CRJ200 SRM 51-25-00. JOB COMPLETED (CLOSED)

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 21,598 hrs · 19,094 cycles

CORROSION FOUND UNDER ANGLE AT ASD THRESHOLD FLOORBEAM .

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 21,598 hrs · 19,094 cycles

LT FUS 484 IB CLIP IS CRACKED.

Part: HANDLE — CRACKED (ESCAPE HATCH) · airframe 21,598 hrs · 19,094 cycles

CREW ESCAPE HANDLE CRACKED AT BASE. PERFORMED EDDY CURRENT INSPECTION OF BASE ON CREW ESCAPE HATCH, FOR THE HANDLE, I/A/W CRJ 200 NDTM 51-20-06. NO DEFECTS NOTED. (CLOSED)

Part: FLOORBEAM — CRACKED (BS 280) · airframe 21,598 hrs · 19,094 cycles

FS 280 AFT FLOORBEAM ANGLE CRACKED OB OF LT AND RT BL9. REMOVED FWD FLOOR SUPPORT ANGLE, CUT-OUT AFT FLOOR SUPPORT ANGLE AND DAMAGED SECTION OF WEB REF REO 601R-53-11-926. TRIMMED -5 AFT ANGLE TO SIZE FABRICATED -13 SHIM AND LOCATED HOLES IAW REO 601R-53-11-926.PERFORMED EDDY CURRENT INSPECTION OF CUT OUT AREA PER REO # 601R-53-11-926 IAW CRJ 2OO NDTM PART 1. 51-20-06. NO DEFECTS NOTED. DRILLED AND TRIMMED NEW AFT ANGLE ALL WRK DONE REQUEST OK TO INSTALL IAW REO601R-53-11-926 DK 7022603. BEGAN INSTALLATION AFT ANGLE ON 280 FRAME ALL WORK DONE IAW REO 601R-53-11-926 DK 7022603COMPLETED INSTALLATION OF AFT 280 ANGLE MINUS 2 NUT PLATES ALL WORK DONE IAW REP 61R-53-11-926 DK 7022603. INSTALLED LT AND RT.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 21,598 hrs · 19,094 cycles

FLOOR SUPPORT AFT OF AFT CUT-OUT CUP CORRODED RESOLVED ON W/O: 33166 TASKCARD: N/R-00193 ) CORROSION FOUND TO WITHIN ALLOWABLE DAMAGE LIMITS, REMOVED CORROSION IAW SRM 51-21-06 SG7020421 ALODINED, PRIMED REPAIRED AREA IAW SRM 51-25-16 SG7020421. PAINTED REPAIR AREA AT STA 349 TRANSVERSE BEAM IAW SRM 51-25-00. JOB COMPLETE (8/14/06-SUPPLEMENTAL - SDR CLOSED)

Part: SKIN — CRACKED (WS 148R) · airframe 21,598 hrs · 19,094 cycles

RT WING LOWER AFT SIDE CRACKED AT WS148.018 ADJACENT TO JACKING PAD.

Part: FLOORBEAM — CRACKED (BS 310) · airframe 21,598 hrs · 19,094 cycles

FLOORBEAM UPPER ANGLE CRACKED FWD OB CORNER (UNDERSIDE) (RESOLVED ON W/O: 33166 TASKCARD: N/R-00190 ). PERFORMED EDDY CURRENT INSPECTION OF FLOORBEAM ANGLE AT F.S. 310 IAW CRJ 200 NDTM 51-20-06. NO DEFECTS NOTED ON FLOOR SUPPORT ANGLE THAT IS ATTACHED TO FLOORBEAM STRINGER P/N 601R31527-221. (SDR CLOSED)

Part: ANGLE — CRACKED (CARGO DOORWAY) · airframe 21,598 hrs · 19,094 cycles

CARGO DOOR SURROUND UPPER MEMBER BEAM AFT LOWER ANGLE CRACKED. REMOVED LOWER ANGLE ON UPPER MEMBER BEAM ON CARGO DOOR TRACK IAW CRJ 200 SRM 51-42-10. REINSTALLED FIRE BLOCK MATERIAL AS NEEDED. I/A/W SRM 51-42-00. (MPC 20041). FABRICATED NEW ANGLE FROM 2024- T3 .040". PER EO 600-53-0346. (MPC 20041). COMPLIED WITH LPI OF FABRICATED ANGLES IAW NDTM 51-20-08. NO DEFECTS AT THIS TIME. GM19494 8/17/06. TREATED PRIMED AND PAINTED NEW ANGLE, IDENTIFIED WITH P/N 601R35050-109ASA, INSTALLED NEW ANGLE AS NEEDED I/A/W SRM 51-42-00. (MPC 20041). (CLOSED)

Part: ANGLE — CORRODED (FUSELAGE) · airframe 21,598 hrs · 19,094 cycles

FS 280, ANGLE AT FLT STA ENTRANCE CORRODED. REMOVED FWD FLOOR SUPPORT ANGLE, CUT-OUT AFT FLOOR SUPPORT ANGLE,AND DAMAGED SECTION OF WEB REF REO 601R-53-11-926. DRILLED NEW FWD ANGLE AND REQUEST OK TO INSTALL ALL WORK DONE IAW 601R-53-11-926 DK7022603. INSTALLED CAM LOCKS RECEPTICALS ON FWD ANGLE AND BEGAN INSTALLTION ON 280 FRAME ALL WORK DONE IAW CRJ200 SRM 51-42-06 DK 7022603.COMPLETED INSTALLING FWD ANGLE MINUS 2 CAM LOCK RECEPTICALS ALL WORK DONE IAW CRJ 200 SRM 51-42-06 DK 7022603.INSTALLED EMERGENCY GEAR EXTENSION PULLY BRACKET AND 2 CAM LOCK RECEPTICALS IAW CRJ 200 SRM 51-42-00 AND EC REO 601R-53-11-926 SG7020421 JOB COMPLETE COMPLIED WITH RII INSPECTION IAW SP607 FOR FS280 ANGLE REPAIR (CLOSED)

Part: BULKHEAD — CRACKED (BS 280) · airframe 21,598 hrs · 19,094 cycles

FS280 BULKHEAD WEB CRACKED LT SIDE AT EMER GEAR EXT. PULLEY BRACKET LBL9. REMOVED DAMAGED SECTION OF WEB REF REO 601R-53-11-926.TRIMMED -3 WEB FILLER, -1 WEB SPLICE, AND -2 WEB SPLICE TO SIZE IAW REO 601R-53-11-926. PERFORMED EDDY CURRENT INSPECTION OF CUT OUT AREA PER REO 601R-53-11-926 IAW CRJ 2OO NDTM PART 1. 51-20-06. NO DEFECTS NOTED. LOCATED HOLES IN -1 WEB SPLICE, -2 WEB SPLICE AND -3 WEB FILLER IAW REO 601R-53-11-926. FINISHED LOCATING AND DRILLING HOLES IN WEB SPLICES -1.-2., FABRICATED AND DRILLED -9,-10 UPPER WEB SPLICE,--11. AND 12 SHIMS, -7,- AFT SPLICE ANGLE AND BENT UP -8 SPLICE ANGLE. ALL WORK DONE IAW REO 601R-53-11-926 DK 7022603. PREFORMED FINAL TRIM AND DRILL ON -7,-8 ANGLE SPLICES AND

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,870 hrs · 18,483 cycles

FOUND CEILING EMERGENCY LIGHT 1 EA, INOP.

Part: STEP — DAMAGED (AFT SERVICE DOOR) · airframe 20,849 hrs · 18,468 cycles

ASD BOTTOM STEP SEPARATED AT ATTACHED STAY ROD BRACKET TO STEP COMPOSITE.

Part: FLASHLIGHT — DISCHARGED (COCKPIT)

DURING A GROUND INSPECTION, THE CAPTAIN`S AND FIRST OFFICERS FLASHLIGHTS WERE FOUND TO BE DIM. MAINTENANCE REMOVED AND REPLACED THE CAPTAIN`S AND FO`S FLASHLIGHTS. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: LAMP — BURNED OUT (EMERGENCY LIGHT)

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

Part: HANDLE — LACK OF LUBE (FUSELAGE)

DURING A GROUND INSPECTION, THE PASSENGER DOOR WAS DIFFICULT TO OPEN. MAINTENANCE LUBRICATED THE PASSENGER DOOR HANDLE ROLLER CAM. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: LIGHT — INOPERATIVE (CABIN)

DURING A GROUND INSPECTION IN ATL, FIVE SECTIONS OF EMERGENCY FLOOR LIGHTS WERE FOUND TO BE INOPERATIVE. (M)

Part: WIRE — SHORTED (EMERGENCY LIGHT)

FLT 4408 - DURING A GROUND INSPECTION IN ATL, FIVE SECTIONS OF EMERGENCY FLOOR LIGHTS WERE FOUND TO BE INOPERATIVE. UPON INSPECTION MAINTENANCE FOUND ONE SECTION OF EMERGENCY FLOOR LIGHTS SHORTED OUT CAUSING ALL FIVE SECTIONS TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE SHORTED OUT EMERGENCY FLOOR LIGHT STRIP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: MECHANISM — BINDING (PAX DOOR)

DURING A GROUND INSPECTION IN ATL, THE PASSENGER DOOR WAS FOUND HARD TO CLOSE. MAINTENANCE ADJUSTED THE LATCH MECHANISM ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: CONNECTOR — DAMAGED (CABIN)

DURING OVERNIGHT MAINTENANCE IN SHV, THE FORWARD EMERGENCY FLOOR LIGHT STRIP WAS FOUND TO BE INOPERATIVE. MAINTENANCE FOUND AND REPAIRED A LOOSE CONNECTION TO THE FORWARD EMERGENCY FLOOR LIGHT STRIP. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: SKIN — CRACKED (FUSELAGE)

DURING A C-CHECK, THE RT AFT CORNER OF THE NLG CUTOUT WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE RT FUSELAGE SKIN RADIUS AT FS 235 IAW EO. (K)

Part: PRESSURE BLKHD — CRACKED (FUSELAGE)

DURING A C-CHECK, THE FORWARD PRESSURE BULKHEAD IN THE HYDRAULIC BAY AT FS 202.75, BL23.71 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE FORWARD PRESSURE BULKHEAD IN THE HYDRAULIC BAY AT FS 202.75, BL 23.71 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE FORWARD PRESSURE BULKHEAD IN THE HYDRAULIC BAY AT FS 202.75, BL 23.71 IAW REO. (K)

Part: CLIP — CRACKED (FUSELAGE)

DURING A C-CHECK, THE LT UPPER SURFACE OF THE PRESSURE FLOOR, FS 484 BRACKET ON THE IB AND OB WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE LT IB FS 484, LBL 27 CLIP IAW EO. (K)

Part: SILL — CORRODED (FUSELAGE)

DURING A C-CHECK, THE CARGO COMPARTMENT DOOR SILL PLATE WAS FOUND TO BE CORRODD, CHAFED AND CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE CARGO COMPARTMENT DOOR SILL PLATE IAW SRM. (K)

Part: DOUBLER — CRACKED (FUSELAGE)

DURING C-CHECK, THE PASSENGER DOOR FRAME DOUBLER AT THE AFT AREA UPPER IB OF THE UPPER AFT SEAL WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE PASSENGER DOOR FRAME DOUBLER AND OUTER SKIN IAW EO. (K)

Part: LIGHT — DAMAGED (CABIN)

DURING A C-CHECK, THE EMERGENCY EXIT LIGHT COVER AND BASE BY THE SERVICE DOOR WAS FOUND DAMAGED. MAINTENANCE IS REMOVING AND REPLACING THE EMERGENCY EXIT LIGHT ASSEMBLY BY THE SERVICE DOOR. (K)

Part: STEP — CRACKED (PAX DOOR)

DURING A C-CHECK, THE LOWER STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE IS REMOVING AND REPLACING THE LOWER STEP ON THE PASSENGER DOOR. (K)

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

FLT 9950 - DURING HANGAR MAINTENANCE IN BTR, THE SECOND FROM AFT EMERGENCY CEILING LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE SECOND FROM AFT EMERGENCY CEILING LIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT)

FLT 9950 - DURING HANGAR MAINTENANCE IN BTR, THE EMERGENCY FLOOR TRACK LIGHT AT ROW 10 C-D WAS FOUND TO BE INOPERATIVE. MAINTENANCE RECONNECTED THE EMERGENCY FLOOR TRACK LIGHTING AT ROW 10 C/D. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: STEP — CRACKED (PAX DOOR)

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

Part: LIGHT — BROKEN (PAX DOOR)

FLT 4415 - DURING A GROUND INSPECTION IN ATL, THE PASSENGER DOOR EMERGENCY EXIT LIGHT WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR EMERGENCY EXIT LIGHT ASSEMBLY. OPS CEHCKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: ENGINE — FAILED (LEFT)

DURING CLIMB-OUT FROM CHS-DFW, AT APPROXIMATELY 21,000 FT THE CREW RECEIVED A LOW OIL PRESSURR WARNING ON THE LT ENGINE. BEFORE THE CREW COULD BEGIN INITIATING QRH PROCEDURES, OIL PRESSURE ON THE LT ENGINE DROPPED RAPIDLY AND SUBSEQUENTLY SHUT ITSELF DOWN, FOLLOWED BY A STRONG YAW TO THE LT. AN EMERGENCY WAS DECLARED WITH THE AIRCRAFT DIVERTING TO ATL, LANDING SAFELY. MAINTENANCE REMOVED AND REPLACED THE LEFT ENGINE. OPS AND LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: ANGLE — CRACKED (FUSELAGE)

DURING HANGAR MAINTENANCE AT CKB, THE FLOOR SUPPORT ANGLE ON THE LEFT AND RIGHT SIDES AT FS 621, WL 73, RBL AND LBL 40 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE FLOOR SUPPORT ANGLE ON THE LEFT AND RIGHT SIDES AT FS 621, WL 73, RBL AND LBL 50 IAW ASA EO 600-53-0105. (M)

Part: DOUBLER — CRACKED (FUSELAGE)

DURING HANGAR MAINTENANCE AT CKB, THE DOUBLER IN THE RADIUS AT FRAME FS 640 BETWEEN STRINGERS 9 AND 12 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPLACED THE DOUBLER IN THE RADIUS AT FRAME FS 640 BETWEEN STRINGERS 9 AND 12 IAW ASA EO 600-53-0075. (M)

Part: FLOORBEAM — CRACKED (FUSELAGE)

DUIRNG HANGAR MAINTENANCE AT CKB, THE FLOORBEAM ON THE PILOTS BULKHEAD AT FS 280, LBL AND RBL 9 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRD THE FLOORBEAM ON THE PILOTS BULKHEAD AT FS 280, LBL AND RBL 9 IAW ASA EO 600-53-0090. (M)

Part: DOUBLER — CRACKED (FUSELAGE)

DURING HANGAR MAINTENANCE AT CKB, THE LEFT AND RIGHT SIDE INTERNAL DOUBLER AT FS 640 BETWEEN STRINGERS 10 L/R AND 11 L/R WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE LEFT AND RIGHT SIDE INTERNAL DOBLER AT FS 640 BETEEN STRINGERS 10 L/R AND 11 L/R IAW ASA EO 600-53-0107 AND ASA EO 600-53-0109. (M)

Part: SUPPORT BEAM — CRACKED (FUSELAGE)

DURING HANGAR MAINTENANCE AT CKB, THE LEFT AND RIGHT ENGINE SUPPORT BEAM LOWER WEB AT BL 36.20 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE LEFT AND RIGHT ENGINE SUPPORT BEAM LOWER WEB AT BL 36.20 IAW ASA EO 600-53-0073. (M)

Part: DOUBLER — CRACKED (FUSELAGE)

DURING HANGAR MAINTENANCE AT CKB, THE FRAME DOUBLER AT FS 640 BETWEEN STRINGERS 9 AND 12 ON THE LEFT SIDE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPLACED THE FRAME DOUBLER AT FS 640 BETWEEN STRINGERS 9 AND 12 ON THE LEFT SIDE IAW ASA EO 600-53-0075. (M)

Part: ANGLE — CORRODED (FUSELAGE)

DURING HANGAR MAINTENANCE AT CKB, THE CHANNEL AT FS 280 BETWEEN RBL AND LBL 9 WAS FOND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CHANNEL ANGLE IAW SRM 51-42-13. (M)

Part: FRAME — CRACKED (FUSELAGE)

DURING HANGAR MAINTENANCE AT CKB, THE FRAME SECTOR AT FS 640 ON THE RIGHT SIDE BELOW STRINGER 9R WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE FRAME SECTOR AT FS 640 ON THE RIGHT SIDE BELOW STRINGER 9R IAW ASA EO 600-53-0075. (M)

Part: FRAME — CRACKED (FUSELAGE)

DURING HANGAR MAINTENANCE AT CKB, THE FRAME SECTOR AT FS 640 BELOW STRINGER 9 ON THE LT SIDE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE FRAME SECTOR AT FS 640 BELOW STRINGER 9 ON THE LT SIDE IAW ASA EO 600-53-0075. (M)

Part: INTERCOSTAL — CRACKED (FUSELAGE)

DURING HANGAR MAINTENANCE AT CKB, THE FLOOR SUPPORT INTERCOSTAL AT FS 484, LBL AND RBL 36 AT THE ATTACH FLANGE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FLOOR SUPPORT INTERCOSTAL AT FS 484, LBL AND RBL 36 AT THE ATTACH FLANGE IAW ASA EO 600-53-0098. (M)

Part: SUPPORT — BROKEN (PAX DOOR)

FLT 4571 - DURING A GROUND INSPECTION IN ATL, THE PASSENGER DOOR BOTTOM STAIR SUPPORT PANEL ASSEMLBY WAS FOUND TO BE BROKEN BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR BOTTOM STAIR SUPPORT PANEL ASSEMBLY. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: POWER SUPPLY — INOPERATIVE (CABIN)

DURING HANGER INSPECTION, THE OVERHEAD LIGHTED EMERGENCY EXIT SIGN AT ROW 8 WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 2 EMERGENCY POWER SUPPLY. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE.

Part: ELEMENT — DEFECTIVE (LT ENGINE)

DURING CLIMB-OUT OF MCO, WITH THE GEAR UP THE CAPTAIN RECEIVED A 14TH STAGE DUCT WARNING ON THE LEFT ENGINE. AN EMERGENCY WAS DECLARED AND AIRCRAFT RETURNED TO MCO AND LANDED SAFELY. MAINTENANCE FOUND THE ROOT CAUSE OF THIS OCCURRENCE TO BE A DEFECTIVE 14TH STAGE SENSING ELEMENT. MAINTENANCE REMOVED AND REPLACED THE SENSING ELEMENT. THE 14TH STAGE BLEED AIR DUCT WAS REPLACED DUE TO CHAFING DAMAGE CAUSED BY THE DEFECTIVE ELEMENT. THE 14TH STAGE ANTI-ICE CHECK VALVE AS WELL AS THE VALVE COUPLING AND BOOT WERE REPLACED AS A PRECAUTION. (M)

Part: CARBON SEAL — LEAKING (RT ENGINE)

FLT 4698 - WHILE CLIMBING THROUGH FL270 FROM ATL-SWF, THE CAPTAIN REPORTED RECEIVING A RIGHT ENGINE OIL PRESSURE MESSAGE FOLLOWED BY AN AURAL WARNING. THE OIL PRESSURE WAS FLUCTUATING BETWEEN 30 AND 49 PSI. THE CAPTAIN SECURED THE RIGHT ENGINE AND RETURNED TO LAND SAFELY IN ATL. MAINTENANCE PERFORMED AN OIL CONSUMPTION RUN. AN OIL LEAK WAS DISCOVERED AT THE NR 7 CARBON SEAL AREA. MAINTENANCE REMOVED AND REPLACED THE NR 7 CARBON SEAL AND THE 4 AND 6 POSITIONS SCAVENGE TUBE PACKINGS. LEAK AND OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BEAM — CRACKED (FUSELAGE)

DURING C-CHECK INSPECTION IN MCN, WHILE COMPLYING WITH ASA EO600-63-0043, VISUAL INSPECTION OF THE ENGINE SUPPORT BEAMS, BOTH SIDES WERE FOUND TO HAVE A CRACK. MAINTENANCE COMPLETED STEPS 1-5 OF REO 601R-53-61-358 WHICH IS ANOTHER TEMPORARY REPAIR TO THE ENGINE SUPPORT BEAM. (M)

Part: ENGINE — FAILED (NR 2)

FLT 4543 - IN CRUISE, FL350, IN SMOOTH AIR AND CLEAR OF CLOUDS, THE AIRCRAFT SUDDENLY SHOOK AND VIBRATED MOMENTARILY AS THE RIGHT ENGINE FAILED. CREW FOLLOWED QRH PROCEDURES, DECLARED AND EMERGENCY, AND DIVERTED TO RIC WHERE THEY LANDED SAFELY. MAINTENANCE REPLACED THE ENGINE FUEL CONTROL AND PUMP. MAINTENANCE ALSO PERFORMED N2 COMPRESSOR AND HOT SECTION BOROSCOPE INSPECTIONS AND ENGINE RUNS. THE FDR WAS REMOVED AND SENT TO GE FOR INVESTIGATION. THE DFDR DATE REVEALED A MOMENATRY FUEL FLOW INTERRUPTION. THE CAUSE OF THE FUEL INTERRUPTION IS UNKNOWN. TEAR DOWN AND TESTS OF THE FUEL CONTROL AND FUEL PUMP WERE NORMAL. NO CONTAMINATION WAS FOUND. (M)

Part: POWER SUPPLY — INOPERATIVE (CABIN)

ATL - FLT 4674 - PRE-FLIGHT - CREW REPORTED THE FORWARD FLOOR TRACK EMERGENCY LIGHTS WERE INOPERATIVE. ATL MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT POWER SUPPLY. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RELEASED FOR FURTHER SERVICE. (X)