N972EV

Part: ENGINE — MALFUNCTIONED (RIGHT) · airframe 24,633 hrs · 22,274 cycles

RT ENGINE VIBRATION, ITT SPIKE, AND LOOSE OF POWER AT ROTATION. FOLLOWED QRH AND RETURNED FOR LANDING. EMERGENCY DECLARED, ACFT RETURNED. R & R NR 2 ENGINE.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 23,920 hrs · 21,536 cycles

NR 3 CABIN CEILING EMERGENCY FLOOD LIGHT INOP. RELAMPED NR 3 CABIN EMERGENCY FLOOD LIGHT IAW AMM 33-51-16, OPS CHECKED GOOD.

Part: CONTROL UNIT — FAILED (TE FLAPS) · airframe 23,832 hrs · 21,452 cycles

FLAPS FAILED AT ZERO DEGREES, PRECEDED BY FLAPS HALF SPEED IN ROUTE. EMERGENCY DECLARED. R & R FECU IAW AMM 27-51-05. FLAPS OPS TESTED GOOD IAW AMM 27-54-00. NO FURTHER DEFECTS NOTED.

Part: ENGINE — FAILED (LEFT) · airframe 23,427 hrs · 21,004 cycles

LEFT ENGINE FAILED ON DESCENT, ATTEMPTED ONE RESTART, WOULD NOT RESTART. COMPLIED WITH WO 246732, LEFT ENGINE CHANGE. ACFT RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT) · airframe 23,351 hrs · 20,927 cycles

EMERGENCY LIGHTS DO NOT COME ON. FOUND F/A EMERGENCY LIGHT SWITCH IN THE ON POSITION. RECHARGED BATTERIES USING WITH A/C ELEC SYSTEM. SYSTEM RESET. IAW MCC, NO FURTHER ACTION REQUIRED AT THIS TIME.

Part: CHARGER — MALFUNCTIONED (EMERGENCY LIGHT) · airframe 23,052 hrs · 20,584 cycles

LEFT OVERWING EMERGENCY LIGHT IS ON ALL THE TIME. FOUND NR 2 BATTERY CHARGER DEFECTIVE AND BLEEDING THROUGH TO THE LT O/W EMERGENCY LIGHT. REPLACED THE NR 2 CHARGER ASSY IAW AMM TASKS 33-51-05-000-801 AND 33-51-05-400-801. TESTED GOOD IAW AMM TASK 33-51-04-740-801.

Part: FLOORBEAM — CORRODED (BS 349) · airframe 23,067 hrs · 20,601 cycles

FLOORBEAM AT FS 349.00 RT SIDE OF FUSELAGE RBL 36.0 IS CORRODED BEYOND LIMITS. REPAIRED IAW SRM.

Part: BULKHEAD WEB — CRACKED (AFT) · airframe 23,052 hrs · 20,584 cycles

FOUND REAR PRESSURE BULKHEAD WEB HAS A CRACK INDICATION NOTED AT LBL 27.50, WL 130 APPROX .3 INCHES IN LENGTH 100 PERCENT FSH, FAILED NDT INSPECTION. REPAIRED IAW REO 601R-53-61-1541.

Part: SEAT TRACK — CORRODED (BS 364) · airframe 23,052 hrs · 20,584 cycles

CABIN FLOOR FWD SEAT TRACK AT RBL 9 CORRODED AT FS 364.00. REMOVED CORRODED SEAT TRACK AND INSTALLED NEW SERVICEABLE SEAT RAIL IAW AMM TASKS 53-01-11-000-802 AND 53-01-11-400-802.

Part: INTERCOSTAL — CRACKED (BS 621-625) · airframe 23,052 hrs · 20,584 cycles

FS 621.00 TO FS 625.00 INTERCOSTAL ANGLE CRACKED AT RBL 45 AND LBL 45 AT STR 14 WL 97.5. REMOVED INTERCOSTAL ANGLE. INSTALLED INTERCOSTAL ANGLE IAW SRM 51-42-21.

Part: BRACKET — BROKEN (BS 621 BULKHEAD) · airframe 23,052 hrs · 20,584 cycles

BROKEN ISOLATOR BRACKET ON FWD SIDE OF FS 621 BULKHEAD. R & R ISOLATOR IAW SRM 51-42-06.

Part: FLOOR SUPPORT — CORRODED (BS 310-319.7) · airframe 23,052 hrs · 20,584 cycles

CABIN FLOOR SUPPORT AND SILL PLATE RT SIDE BETWEEN FS 310.00 AND FS 319.70 IS CORRODED AT RBL 42.0. REMOVED CABIN FLOOR SUPPORT AND SILL PLATE IAW SRM 51-42-06 AND 51-42-21. DRILLED & LOCATED NEW SERVICEABLE FLOOR SUPPORT 601R31148-79 AND ANGLE 601R3669-49 IAW SRM 51-42-06 AND 51-42-21. INSTALLED NEW FLOOR SUPPORT AND SILL PLATE ANGLE ON RT SIDE BETWEEN FS 310.00 AND FS 319 IAW SRM 51-42-06 AND 51-42-21.

Part: ATTACH FITTING — CORRODED (BS 319.7) · airframe 23,052 hrs · 20,584 cycles

SERVICE DOOR SILL PLATE ANGLE ATTACHMENT FITTING AT FS 319.70 IS CORRODED. REPLACED SILL PLATE ANGLE 601R3669-49.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 23,052 hrs · 20,584 cycles

FS 280.00 FWD AND AFT "J" ANGLES ARE CORRODED BETWEEN LBL 9 AND RBL 9. (SDR OPEN)

Part: FLOORBEAM — CORRODED (BS 349) · airframe 23,052 hrs · 20,584 cycles

FLOORBEAM SUPPORT STRUCTURE AT FS 349.00 RT SIDE OF FUSELAGE, RBL 36.0 IS CORRODED BEYOND LIMITS. (OPEN)

Part: NUT — MISSING (TOILET SEAT) · airframe 23,052 hrs · 20,584 cycles

PANEL 272 BRW LAVATORY SEAT HINGE MISSING NUT & MISSING 3 STUDS & HARDWARE. INSTALLED SERVICEABLE TOILET SEAT NUT IAW CMM 25-40-01. INSTALLED SERVICEABLE BALL STUDS 3 EA AND HARDWARE IAW CMM 25-40-01.

Part: ANGLE — CORRODED (DOOR SILL) · airframe 23,052 hrs · 20,584 cycles

SERVICE DOOR LOWER SILL ANGLE CORRODED. REMOVED SERVICE DOOR SILL ANGLE ASSY IAW SRM 51-42-06 & 51-42-21. DRILLED & LOCATED NEW SERVICEABLE ANGLE IAW SRM 51-42-06 & 51-42-21. INSTALLED SERVICE DOOR LOWER SILL ANGLE IAW SRM 51-42-06, 51-41-21 & 51-42-36.

Part: FLOORBEAM — CORRODED (BS 349) · airframe 23,052 hrs · 20,584 cycles

REMOVED FLOORBEAM CAP ANGLE OTBD SIDE OF FLOORBOARD SUPPORT STRUCTURE OF FS 349.00. RBL 36. REINSTALLED FLOORBEAM STRUCTURE AT FS 349, RBL 36.0 IAW SRM 51-42-06 AND 51-42-21.

Part: ANGLE — CRACKED (BS 280) · airframe 23,052 hrs · 20,584 cycles

FS 280.00 ANGLE OTBD OF RBL 9 IS CRACKED. LOCATED FASTENER HOLES IN NEW FS 280, RBL 9.0 OTBD ANGLE. INSTALLED ANGLE IAW SRM 51-42-06 & 51-42-21.

Part: ANGLE — CORRODED · airframe 23,052 hrs · 20,584 cycles

ANGLE CORRODED. REPAIRED IAW REO 601R-53-11-136.

Part: FLOORBEAM — CRACKED (BS 484) · airframe 23,052 hrs · 20,584 cycles

RT FS 484.00 FLOORBEAM REPAIR ANGLE AT RBL 36.0 IS CRACKED. REPAIRED FLOORBEAM ANGLE IAW REO 601R-53-41-059.

Part: SUPPORT — CRACKED (E/E BAY) · airframe 23,052 hrs · 20,584 cycles

AFT EQUIPMENT COMPARTMENT, RT HEAT EXCHANGER SUPPORT STRUCTURE UNDER ACM CROSSBEAM ANGLE CRACKED. FIT, DRILLED & INSTALLED NEW BEAM, IAW SRM 51-42-06, 51-40-11.

Part: ECU — FAILED (TE FLAPS) · airframe 21,763 hrs · 19,151 cycles

FLAPS FAIL CAUTION MESSAGE, FLAPS AT 0 DEGREES, 12000' IN CLIMB, 290KTS. (DECLARED EMERGENCY AS A PRECAUTION) COMPLIED WITH EC/TC AD 2009-06-12 AND RESET FECU IAW FIM 27-51-05. SYS OPS CK GOOD AT THIS TIME. (CLOSED)

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 21,350 hrs · 18,703 cycles

EMERGENCY LIGHTS WILL NOT GO OUT. CYCLED SWITCH SEVERAL TIMES, OPS CK GOOD IAW AMM 200 33-51-00. (CLOSED)

Part: SENSOR — OUT OF ADJUST (NLG) · airframe 21,234 hrs · 18,575 cycles

GEAR DISAGREE JUST AFTER T/O NOSE GEAR REMAINED DOWN & GREEN, MAINS RETRACTED AS NORMAL. EMER DECLARED, RETURNED TO DEPARTURE. (ACFT RETURNED TO DEPARTURE AFTER T/O -- DECLARED EMERGENCY) ADJUSTED NLG (WOFW) SENSORS IAW AMM 32-61-05. OPS CHECK GOOD. (CLOSED)

Part: PLACARD — DETERIORATED (CABIN) · airframe 21,221 hrs · 18,553 cycles

PLACARD ABOVE DOOR OPENING IN FRONT ENTRY WAY IS BLANK. REPLACED MISSING PLACARD IAW SUPPLIMENT 11-30-00.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 20,976 hrs · 18,272 cycles

NR7 LT AFT EXTERIOR EMERGENCY LIGHT INOP. RELAMPED NR7 LT AFT EXTERIOR EMERGENCY LIGHT IAW AMM 33-51-21, OPS CHECK GOOD. RELAMPED NR7 LT AFT EXTERIOR EMERGENCY LIGHT IAW AMM 33-51-21, OPS CHECK GOOD.

Part: BLEED AIR SYS — ODOR (ENGINE) · airframe 20,843 hrs · 18,111 cycles

ON APPROACH, HAD A BURNING ODOR IN FRONT OF ACFT. SWAPED BLEEDS TO APU ODOR WAS DIMINISHED IMMEDIATELY. C/W OPS CHECK OF BOTH ENGINES IAW AMM 71-00-00. OPS CK GOOD. NO DEFECTS NOTED. (CLOSED)

Part: WIRE — MISINSTALLED (EMERGENCY LIGHTS) · airframe 20,008 hrs · 17,136 cycles

GALLEY EMERGENCY "EXIT" LIGHT SIGNS INOP. FOUND SVC DOOR PROX. EXIT SIGN AND SVC DOOR EXIT SIGN WIRES SWAPPED. INSTALLED CORRECTLY IAW AMM 33-61-05. OPS CK GOOD.

Part: LIGHT — BROKEN (CABIN) · airframe 19,903 hrs · 17,021 cycles

FLOOD LIGHT, FLOOR LEVEL EMERGENCY AT PAX DOOR DOOR BROKEN. FLT 5156, DEL 26 MINS. R & R LIGHT BACKING HSG IAW AMM 33-51-19. (CLOSED)

Part: CARGO TRACK — CORRODED (FUSELAGE) · airframe 19,867 hrs · 16,975 cycles

NR 4 FLOOR TRACK IN AFT CARGO AREA HAS SPOTS OF CORROSION. R & R NR 4 FLOOR TRACK CORRODED SECTION IAW AMM 53-01-11. (CLOSED)

Part: ATTACH FITTING — CRACKED (BS 280) · airframe 19,867 hrs · 16,975 cycles

BS 280 FRAME CLIP AT RBL9 IS CRACKED. REMOVED CRACKED FRAME CLIP & REPLACED WITH NEW AT STA 280, RBL 9, IAW SRM 53-21-43.

Part: BRACKET — CRACKED (BS 625.30 S14L) · airframe 19,867 hrs · 16,975 cycles

ANGLE BRACKET CRACKED AT FS625.30 AND S14L. R & R ANGLE BRACKET AT FS 625.30 & STR 14L IAW SRM 51-40-11.

Part: CARGO TRACK — CORRODED (FUSELAGE) · airframe 19,867 hrs · 16,975 cycles

NR 2 FLOOR TRACK PUCS IN AFT CARGO AREA HAS SPOTS OF CORROSION. R & R BULKHEAD ATTACH FITTING IAW AMM 53-01-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 19,867 hrs · 16,975 cycles

NR 1 FLOOR TRACK IN AFT CARGO AREA HAS SPOTS OF CORROSION. R & R NR 1 FLOOR TRACK CORRODED SECTION IAW AMM 53-01-11. (SDR CLOSED)

Part: CARGO TRACK — CORRODED (FUSELAGE) · airframe 19,867 hrs · 16,975 cycles

NR 1 FLOOR TRACK PUCS IN AFT CARGO AREA HAS SPOTS OF CORROSION. R & R PUCKS IAW SRM 51-40-00.

Part: FRAME — CRACKED (BS 718 S10-11R) · airframe 19,867 hrs · 16,975 cycles

STA 718 BETWEEN STR 10 AND 11 RT, FRAME FLANGE IS CRACKED. REPAIR TO BE C/W ON CARD S/B 601R-53-055.

Part: CARGO TRACK — CORRODED (FUSELAGE) · airframe 19,867 hrs · 16,975 cycles

NR 3 FLOOR TRACK IN AFT CARGO AREA HAS SPOTS OF CORROSION. R & R CORRODED SECTIONS OF NR 3 CARGO FLOOR TRACK IAW AMM 53-01-11. (CLOSED)

Part: CARGO TRACK — CORRODED (FUSELAGE) · airframe 19,867 hrs · 16,975 cycles

NR 2 FLOOR TRACK IN AFT CARGO AREA HAS SPOTS OF CORROSION. R & R CORRODED SECTIONS OF NR 2 CARGO FLOOR TRACK IAW AMM 53-01-11. (CLOSED)

Part: ATTACH FITTING — CRACKED (BS 280) · airframe 19,867 hrs · 16,975 cycles

BS 280 FRAME CLIP AT LBL9 IS CRACKED. REMOVED CRACKED FRAME CLIP & REPLACED WITH NEW AT STA 280, LBL 9 IAW SRM 53-21-43.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 19,867 hrs · 16,975 cycles

REAR PRESSURE BULKHEAD IS CRACKED AT LINTEL FITTING. ACCOMPLISHED LINTEL FITTING/ AFT PRESSURE BULKHEAD REPAIR IAW PL601R-53-61-1230, C/W RII OF REAR PRESSURE BULKHEAD LINTEL FITTING.

Part: ATTACH ANGLE — CRACKED (PAX DOOR) · airframe 19,867 hrs · 16,975 cycles

PAX DOOR ATTACH ANGLE CRACKED AT BELL CRANK. HFEL INSP VERIFIED ONLY PAINT CRACKED, NO EXISTING CRACK IN ANGLE IAW NDTM PT. 6, 51-20-06.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 19,864 hrs · 16,972 cycles

SEVERAL LIGHTS FROM NR 3 EMERGENCY BATTERY PACK NOT FUNCTIONING . R & R NR 3 EMERGENCY BATTERY PACK IAW AMM 33-51-04. OPS CHECK GOOD. R & R NR 3 EMERGENCY BATTERY PACK IAW AMM 33-51-04. OPS CHECK GOOD.

Part: SENSING ELEMENT — FAILED (ANTI ICE SYS) · airframe 19,682 hrs · 16,772 cycles

ANTI ICE DUCT WARNING ILLUMINATED IN FLIGHT. (EMERGENCY DECLARED). REMOVED AND REPLACED SENSING ELEMENT A40WK IN RT WHEEL BIN IAW AMM 36-21-04. OPS CK GOOD.

Part: PLACARD — MISSING (CABIN) · airframe 19,503 hrs · 16,569 cycles

EXIT SIGN ON BOARDING STAIRS MISSING.

Part: THRUST REVERSER — WARNING LIGHT (LEFT) · airframe 19,013 hrs · 16,043 cycles

L REV UNLOCKED CAUTION MSG AFTER T/O NO CHANGE NOTICIED IN ACFT PERFORMANCE [EMERGENCY DECLARED -- ACFT RETURNED TO DEPARTURE AFTER T/O]( THRUST REVERSER SYSTEMS ).

Part: LIGHT — UNKNOWN (CABIN) · airframe 18,497 hrs · 15,513 cycles

FLOOR LEVEL EMERGENCY FLOODLIGHT REQUIRES REPLACEMENT.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 16,462 hrs · 13,616 cycles

LT WING AFT EMERGENCY LIGHT INOPERATIVE. RELAMPED LT WING AFT EMERGENCY LIGHT IAW CRJ200 AMM 33-51-21. OP CHECKED GOOD AT THIS TIME. (S)

Part: FITTING — CRACKED (FUSELAGE) · airframe 15,914 hrs · 13,127 cycles

AAR - FS 280 CLIP CRACKED I/B OF RBL 36.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 15,914 hrs · 13,127 cycles

FS 280 SUPPORT ANGLE FOR FLOORBOARD 221ALF (FLIGHT DECK FLOORBOARD) CRACKED AT RBL 9. REMOVED ANGLE IAW SRM 51-42-06. LOCATED HOLES IN NEW SERVICEABLE SUPPORT ANGLE IAW SRM 51-42-06. OK TO INSTALL. INSTALLED NEW SERVICEABLE ANGLE IAW SRM 51-42-06. FILLET SEALED AND TOPCOATED SUPPORT ANGLE IAW SRM 51-25-16 AND 51-23-00. OPS CHECK GOOD IAW MM 32-34-00.

Part: STRUCTURE — CRACKED (PAX DOOR) · airframe 15,914 hrs · 13,127 cycles

PAX DOOR AFT EDGE MEMBER CRACKED UNDER STEP 832ET. REMOVED DAMAGED AREA OF PAX DOOR AFT EDGE MEMBER PER: REO 601R-52-11-279. C/W HFEC INSP OF PAX DOOR AFT MEMBER, IAW NDTM 51-20-06 AND REO 601R-52-11-279. NO DEFECTS NOTED. COMPLIED WITH REPAIR OF PAX DOOR AFT EDGE MEMBER AS REQUIRED, IN ACCORDANCE WITH REO 601R-52-11-279. COMPLIED WITH EC/TC EO 600-52-43.

Part: FITTING — CRACKED (FUSELAGE) · airframe 15,914 hrs · 13,127 cycles

AAR - FS 280 CLIP CRACKED O/B OF RBL 9.

Part: FITTING — CRACKED (FUSELAGE) · airframe 15,914 hrs · 13,127 cycles

AAR - FS 280 CLIP CRACKED O/B OF LBL 9.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 15,914 hrs · 13,127 cycles

AAR - CRACK ON FS 280.0 UPPER ANGLE AT APPROX LBL 13.0 AT RIVET 13333.

Part: FITTING — CRACKED (FUSELAGE) · airframe 15,914 hrs · 13,127 cycles

AAR - CLIP CRACKED O/B SIDE OF LBL 27 AT FS 484.

Part: FITTING — CRACKED (FUSELAGE) · airframe 15,914 hrs · 13,127 cycles

AAR - CLIP CRACKED O/B SIDE OF LBL 27 AT FS 484.

Part: FITTING — CRACKED (FUSELAGE) · airframe 15,914 hrs · 13,127 cycles

AAR - FS 280 CLIP CRACKED I/B OF LBL 9.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 15,914 hrs · 13,127 cycles

RIGHT OBLIQUE ANGLE BRACKET IN WEB IS CRACKED. REMOVED RT OBLIQUE ANGLE, DISCARDED. DUPLICATED NEW ANGLE, LOCATED HOLES, DEBURRED, ALODINED, PRIMED/TOPCOAT AND INSTALLED WET WITH LOCK FASTENER PINS, TOPCOAT APPLIED, REWORK ACCAMPLISHED IAW SRM 53-61-17, 51-21-11, 51-42-21, 51-25-06, 51-25-16, AND 51-23-00. NEW ANGLE P/N S6144A33

Part: ANGLE — CRACKED (FUSELAGE) · airframe 15,914 hrs · 13,127 cycles

LT OBLIQUE ANGLE BRACKET IN WEB IS CRACKED. REMOVED LT OBLIQUE ANGLE, DISCARDED. DUPLICATED NEW ANGLE, LOCATED HOLES, DEBURRED, ALODINED, PRIMED/TOPCOAT AND INSTALLED NEW ANGLE WET WITH LOCK FASTENER PINS, TOPCOAT APPLIED, ALL REWORK ACCOMPLISHED IAW SRM 53-61-17, 51-12-11, 51-42-21, 51-25-06, 51-25-16, 51-23-00. NEW ANGLE P/N S6144A33.

Part: CHANNEL — CRACKED (CARGO DOOR) · airframe 15,914 hrs · 13,127 cycles

CARGO DOOR FWD TRACK, LOWER U-CHANNEL CRACKED. DRILLED OUT CRACKED LOWER U-CHANNEL LOCATED IN THE CARGO BAY. IDENTIFIED MATERIAL IAW SRM 53-61-23 AND MADE A SERVICEABLE PART (DUPLICATE) IAW SRM 51-24-21. ALODINED AND PRIMED DUPLICATED PART IAW SRM 51-25-06. APPLIED TOPCOAT IAW 51-25-16. INSTALLED SERVICEABLE DUPLICATED PART IAW SRM 51-42-060.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,862 hrs · 13,064 cycles

RIGHT SIDE EXT EMERGENCY LIGHT HAS LIGHT BULB INOP.

Part: SELECTOR KNOB — BROKEN (STBY ALTIMETER) · airframe 15,674 hrs · 12,925 cycles

DURING CLIMB THRU FL 180 THE STBY ALTIMETER SELECT KNOB BROKE, KNOB WILL ONLY ROTATE COUNTER CLOCKWISE. EMERGENCY DECLARED. A/C RETURNED TO ATL AFTER T/O.

Part: DOOR — STIFF · airframe 14,753 hrs · 12,177 cycles

F/A REPORTS SERVICE DOOR HARD TO OPERATE.

Part: COVER — OUT OF POSITION (CABIN) · airframe 14,672 hrs · 12,104 cycles

EMERGENCY EXIT ROW LIGHT COVER AT ROW 8 FELL OFF.

Part: WARNING MESSAGE — MULTIPLE FAIL · airframe 12,297 hrs · 10,284 cycles

UPON GEAR UP RECEIVED NOSE GEAR /DOOR RED WARNING MESSAGE, ALSO A CAUTION HYD 3A LOW PRESS MESSAGE ON FOURTH ATTEMPT. QRH COMPLIED WITH, GEAR CAME UP AND LOCKED UNDER NORMAL CONDITIONS GEAR UP TOOK APPROX 15-20 SEC. A/C RETURNED TO ATL AFTER T/O (EMERGENCY DECLARED).

Part: LIGHT — INOPERATIVE (LT WING) · airframe 11,702 hrs · 9,792 cycles

LT OVERWING EMERGENCY LIGHT INOP.

Part: CLIP — CRACKED (FUSELAGE) · airframe 11,433 hrs · 9,587 cycles

FOUND CLIP CRACKED ON TOP OF BOX BEAM, FS 639 BELOW STR 9.

Part: FLOOR SUPPORT — CORRODED (BS 300-310) · airframe 11,434 hrs · 9,587 cycles

CORROSION ON FLOOR SUPPORT AND DOUBLER AT FS 300 TO 310 - RBL 44. REMOVED DOUBLER AND CLIP AT FS310 RBL44 FOM PER SRM 51-42-06. BLENDED LIGHT CORROSION ON DOUBLER 0.003 DEEP AND FLOOR SUPPORT 0.002 PER SRM 51-12-00 BOTH ARE WITHIN ALLOWABLE DAMAGE LIMITS PER SRM 51-00-00 SG7020421 ALODINED, PRIMED, AND PAINTED ALL BLENDED AREAS PER SRM 51-21-16 AND REINSTALLED DOUBLER AND CLIP PER SRM 51-42-00 SG7020421.(CLOSED)

Part: CLIP — CRACKED (FUSELAGE) · airframe 11,434 hrs · 9,587 cycles

FS 280 CLIP CRACKED AT RBL 9 IB.

Part: HANDLE — CRACKED (AVIONICS BAY) · airframe 11,434 hrs · 9,587 cycles

AVIONICS BAY OUTER HANDLE APPEARS CRACKED.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 11,434 hrs · 9,587 cycles

LT SIDE FS 484 INTERCOSTAL CRACKED (MARKED)

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 11,434 hrs · 9,587 cycles

LT SIDE FS 484 INTERCOSTAL CRACKED (MARKED).

Part: ANGLE — CRACKED (FUSELAGE) · airframe 11,434 hrs · 9,587 cycles

LT SIDE FS 621 FLOOR ANGLE CRACKED (MARKED) (RESOLVED ON W/O: 25161 TASKCARD: N/R-00244 ) REMOVE DAMAGED PORTION OF -239 ANGLE, DRILLED UP NEW -1 ANGLE AND -5 STRAP IAW REO 601R-53-61-117 05-19-06 FINISHED DRILLING AND TRIMMING -5 ANGLE ALODINED, PRIMED , AND PAINTED -5 ANGLE IAW SRM 51-00-00 5-23-06 INSTALLED ANGLES, -1, -3, AND -5 ON 621 FLOOR SUPPORT ANGLE ON LT HAND SIDE IAW REO 601R-53-61-117 05-23-0 RII REQUIREMENTS SATISFACTORY PER ASA SP 607 (SUPPLEMENTAL SDR 5/23/2006) (SDR CLOSED)

Part: BEAM — CRACKED · airframe 11,434 hrs · 9,587 cycles

SUSPECT POSSIBLE CRACK ON CENTER BOX BEAM UNDER FIRE LOOP CLIP.

Part: RIB — CRACKED · airframe 11,434 hrs · 9,587 cycles

RT BATT RIB CRACKED IN RT W/W. C/W REPAIR ON RT BATT RIB IAW REO601R-57-51-046 (CLOSED).

Part: DOUBLER — CRACKED (FUSELAGE FRAME) · airframe 11,434 hrs · 9,587 cycles

RT FUS STA 640 FRAME DOUBLER APPERS CRACKED IN AREA OF BOX BEAM. C/W RT FUSELAGE STA 640 FRAME REPAIR IAW EO600-53-0081C. (CLOSED)

Part: RIB — CRACKED (LT WW) · airframe 11,434 hrs · 9,587 cycles

LT BATT RIB CRACKED IN LT W/W. C/W LT BATT RIB REPAIR IAW REO 601R57-51-046.

Part: CONTROL UNIT — MALFUNCTIONED (SPOILER)

DURING CLIMB OUT, THE CREW RECEIVED A GROUND SPOILER CAUTION MESSAGE, FOLLOWED BY THE AIRCRAFT ROLLING AND YAWING TO THE LT. THE FLIGHT CONTROL SYNOPTIC PAGE INDICATED THAT THE LT IB GROUND SPOILER HAD FULLY DEPLOYED. THE CREW COMPLIED WITH THE QRH, DECLARED AN EMERGENCY, AND DIVERTED, WHERE IT LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE NR 2 SSCU. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: LIGHT — INOPERATIVE (CABIN)

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

Part: SECU — MALFUNCTIONED (SPOILER)

DURING APPROACH FROM IAH-ATL, AT APPROXIMATELY 3,500 FEET THE CREW RECEIVED AN AMBER CAUTION GND SPOILER DEPLOY MESSAGE. THE FLIGHT CONTROL SYNOPTIC PAGE INDICATED THE LEFT WING INBOARD GROUND LIFT DUMPING SPOILER HAD FULLY DEPLOYED. THE CREW COMPLIED WITH THE QRH AND THE SPOILER CONTINUED TO INDICATE FULL DEFLECTION. THE CREW DECLARED AN EMERGENCY AND THE EMERGENCY VEHICLES WERE DISPATCHED. THE AIRCRAFT LANDED SAFELY IN ATL. MAINTENANCE REMOVED AND REPLACED THE NR 1 SECU. OPERATIONAL CHECK GOOD. AIRCRAFT OK FOR SERVICE. (M)