N447CA

Part: WEB — CRACKED (BS 559) · airframe 22,681 hrs · 20,895 cycles

CRACK INDICATION NOTED AT FS 559, RBL 9, WL 58.70 ON WEB APPROX .10 IN LENGTH 53 PERCENT FSH, FAILED NDT. C/W EC/TC REO 601R-53-41-260 & REO 601R-53-41-260, REV E DATED 8/24/2010 AS WRITTEN. C/W EC/TC REO 601R-53-41-609 02 AND MET ALL THE REQUIREMENTS OF REO 601R-53-41-609 REV B SHT 3-11 ARE AT REV A OF REO FOR DEVIATION E. FOR TENSIONING OF AILERON CABLES ADDRESSED IN ITEM NR2. RII FOUND TO BE SATISFACTORY. (SDR CLOSED)

Part: BULKHEAD WEB — CRACKED · airframe 22,673 hrs · 20,887 cycles

FOUND REAR PRESSURE BULKHEAD WEB HS INDICATION NOTED AT LBL 27.50, WL 130 APPROX .5" IN LENGTH 100 PERCENT FSH FAILED NDT INSPECTION. LEAK CHECK OF AIR CONDITIONING SYS DUE IAW AMM TASK 21-51-00-790-801. PERFORMED LEAK CHECK OF AIR CONDITIONING SYS LT PACK DISCHARGE DUCT IAW MM 21-51-00-770-801. NO LEAKS NOTED.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 22,665 hrs · 20,877 cycles

FOUND REAR PRESSURE BULKHEAD WEB HAS CRACK INDICATION NOTED AT LBL 27.50, WL 130 APPROX .5" IN LENGTH 100 PERCENT FSH FAILED NDT INSPECTION.

Part: ISOLATOR — BROKEN (BULKHEAD) · airframe 22,668 hrs · 20,880 cycles

PRESSURE BULKHEAD IN CARGO BAY HAS 3 BROKEN ISOLATORS. REMOVED CARGO COVER CAP PN LXA5028A FROM FS 565 TO FS 621 117.50 FOR ACCESS. INSTALLED RT CARGO SIDEWALL CAP PN LXA5028A IAW AMM TASK 25-52-01-400-801. OK TO INSTALL. R & R BROKEN PRESSURE BULKHEAD ISOLATORS IAW SRM 51-42-13, PN SL2337-3. THIS REPAIR REQUIRES MAJOR/MINOR CLASSIFICATION IAW ASA SOP 5702. THIS REPAIR IS CLASSIFIED AS A MINOR REPAIR IAW ASA SOP 5702. (SDR CLOSED)

Part: WEB — CRACKED (BS 559) · airframe 22,665 hrs · 20,877 cycles

CRACK INDICATION NOTED AT FS 559, RBL 9, WL 58.70 ON WEB APPROX 10 IN LENGTH 53 PERCENT FULL SCREEN HEIGHT. FAILED NDT.

Part: GROUND WIRE — UNSECURE (EMERGENCY LIGHT) · airframe 22,461 hrs · 20,672 cycles

RT FORWARD PART OF CABIN EMERGENCY FLOOR LIGHT NOT ATTACHED TO GROUND. SECURED NEW FLOOR LIGHT TRACK COVER IAW AMM 33-51-01, CKS GOOD. (SDR CLOSED)

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 22,085 hrs · 20,267 cycles

FUSELAGE LT 2ND FROM FRONT EXTERNAL EMERGENCY LIGHT INOP. RELAMPED FUSELAGE LT 2ND FROM FRONT EXTERNAL EMERGENCY LIGHT IAW AMM 33-51-21. RELAMPED FUSELAGE LT 2ND FROM FRONT EXTERNAL EMERGENCY LIGHT IAW AMM 33-51-21.

Part: DOOR — BINDING (MAIN PAX) · airframe 21,912 hrs · 20,081 cycles

CABIN DOOR JAMMING UP DURING OPENING AND CLOSING, MAY CAUSE PROBLEM IN THE EVENT ON EVACUATION. INSPECTED MAIN CABIN DOOR LINKAGES AND ROD ENDS FOR DEFECTS, NO DEFECTS NOTED. GREASED CABIN DOOR LATCH FITTINGS IN REFERANCE TO AMM 12-20-52. OPERATED DOOR, OPS CHECKED GOOD ALSO HAD F/A OPERATE DOOR.

Part: DOOR — BINDING (MAIN PAX) · airframe 21,779 hrs · 19,952 cycles

MAIN CABIN DOOR IS STICKING SHUT AND IS DIFFICULT TO OPEN. PERFORMED OPS TEST ON PAX DOOR IAW AMM 52-11-00. (CLOSED)

Part: DOOR — BINDING · airframe 21,759 hrs · 19,931 cycles

F/A HAS TROUBLE OPENING DOOR. PERFORMED OPERATION TEST ON PAX DOOR IAW AMM 52-11-00.

Part: DOOR — BINDING (MAIN PAX) · airframe 21,727 hrs · 19,895 cycles

PASSENGER DOOR DIFFICULT TO OPEN. PERFORMED PASSENGER DOOR INSPECTION. CHECK IAW IAW AMM 52-11-00. NO DEFECTS NOTED. (CLOSED)

Part: DOOR — BINDING (MAIN PAX) · airframe 20,538 hrs · 18,612 cycles

ARRIVING AT GATE, F/A COULD NOT OPEN PASSENGER DOOR. RAMP ALSO COULD NOT OPEN PASSENGER DOOR. OPENED DOOR AND OPS CHECKED GOOD IAW AMM 52-11-01, MX READY. (CLOSED)

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 20,216 hrs · 18,254 cycles

RT WING EMERGENCY LIGHT INOP. R & R RT WING EMERGENCY LIGHT BULB IAW AMM 33-51-21. OPS CHECK GOOD , NO DEFECTS NOTED AT THIS TIME.

Part: POST — CRACKED (BS 409) · airframe 19,686 hrs · 17,662 cycles

TWO INDICATIONS FOUND DURING INSP OF FS 409.0+128 VERTICAL POST AT RBL 18.0 1 ON I/B CHANNEL APPROX .312" LONG 100% FSH, 1 ON O/B CHANNEL APPROX .20" LONG 70% FSH FAILED NDT INSP. REMOVED VERTICAL POST AT F.S. 409+128 RBL 18 IAW SRM 51-42-06, 51-41-02. DRILLED/LOCATED NEW POST TOP ACFT IAW SRM 51-42-06. INSTALLED I/B AND O/B VERTICAL POSTS IAW SRM 51-42-06, 51-41-02 AND C/W EC/TC REO 601R-53-41-889 AND MET ALL THE REQUIREMENTS OF REO 601-R53-41-889 REV A. PRIMED, PAINTED, SEALED, AND APPLIED CORROSION INHIBITOR IAW SRM 51-25-06, 51-25-16, 51-23-00, AND 51-21-11.

Part: DOOR — BINDING (MAIN PAX) · airframe 19,594 hrs · 17,558 cycles

F/A REPORTS THE PAX DOOR IS DIFFICULT TO OPEN/CLOSE. PERFORMED OPS CK OF PAX DOOR. NO FAULTS FOUND AT THIS TIME OK FOR SERVICE IAW AMM 52-11-00. (CLOSED)

Part: LIGHT — INOPERATIVE (EMERGENCY EXIT) · airframe 19,444 hrs · 17,380 cycles

RT WING EMERGENCY EXIT (2) LIGHTS INOP FWD OF OVERWING EXIT. REPLACED BULBS (2) CK OK IAW AMM 53-12-10.

Part: SMOKE DETECTOR — DIRTY (LAVATORY) · airframe 19,285 hrs · 17,201 cycles

SMOKE TOILET CAUTION MESSAGE SHORTLY AFTER TAKEOFF. COMPLIED WITH QRH. NO SMOKE OR FIRE FOUND. CAUTION MESSAGE DISSAPPEARED AFTER 5 MINUTES. REMOVED DUST PARTICLES FROM LAVATORY SMOKE DETECTOR OPS CK GOOD IAW AMM 26-10-00

Part: WARNING MESSAGE — FALSE ACTIVATION (LAVTORY SMOKE) · airframe 19,074 hrs · 16,984 cycles

SMOKE TOILET ON DEPARTER (ACFT RETURNED TO DEPARTURE AFTER T/O -- EMERGENCY DECLARED AS A PRECAUTION) ( LAVATORY SMOKE DETECTION SYS ). PERFORMED OPS CK IAW AMM 26-16-01 OPS CK GOOD MEL CLEARED PLACARD REMOVED.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHT) · airframe 18,887 hrs · 16,771 cycles

EMERGENCY EXIT SIGN ON SIDE WARDROBE INOP.

Part: ATTACH FITTING — CRACKED (BS 625) · airframe 18,849 hrs · 16,730 cycles

RT FS 625 CLIP CRACKED.

Part: ATTACH FITTING — CRACKED (BS 625) · airframe 18,849 hrs · 16,730 cycles

LT FS 625 CLIP CRACKED. REMOVED AND REPLACED LT FS 625 IAW SRM 51-42-21. FOR WORK ACCOMPLISHED.

Part: FLOORBEAM — CRACKED (BS 589) · airframe 18,849 hrs · 16,730 cycles

FLOORBEAM CLIP AT FS 589 AND CARGO DOOR SILL CRACKED. REMOVED AND REPLACED CLIP AT FS 589 UNDER CARGO DOOR SILL IAW SRM 51-42-06 AND 51-42-21.

Part: SUPPORT BEAM — DAMAGED (CARGO DOOR) · airframe 18,849 hrs · 16,730 cycles

CARGO DOOR SUPPORT BEAM DAMAGED. REMOVED AND REPLACED CARGO DOOR SUPPORT BEAM AFT LWR CLIP IAW SRM 51-42-21.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 18,849 hrs · 16,730 cycles

SEAT TRACK CORRODED AT FS 559+95 AT LBL9.

Part: FRAME — CRACKED (BS 621) · airframe 18,849 hrs · 16,730 cycles

RT FS 621 FRAME CRACKED AT FLOOR SILL. WORK ACCOMPLISHED IAW EC/TC REO 601R-53-61-117 ON W/O 137143.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 18,849 hrs · 16,730 cycles

FS 280.00 TRANSVERSE FLOORBEAM CRACKED AT THE RT FLOORBEAM MEMBER AT RBL-9 AT LWR FLANGE RADIUS. CUT OUT DAMAGED AREA AND REMOVED EXISTING FASTENERS IN REPAIR AREA. REMOVED EXISTING -5 CLIP AT FS280 RBL 9 PER REO 601R-53-11-171. PERFORMED ET INSP FOLLOWED BY FPI OF CUTLINE IAW NDTM 51-20-06/08. RECEIVED CRACK INDICATION AT LOWER CUTLINE AROUND THE LWR FASTNER HOLES. STARTED FABRICATING NEW -5 CLIP FROM S 6144-14 BATCH 1085294 AND -4 REPAIR ANGLE FROM 7075-T6 .050 BATCH 1066537 IAW REO 601R-53-11-171. FINISHED FABRICATING -5 CLIP AND REPAIR ANGLE AND FABRICATED -6 FILLER AND -8 FILLER PER REO 601R-53-11-171. OPENED CUT OUT IAW SCHEME B REO 601R-53-11-171. PERFORMED ET INSP OF CUTLINE FS 280, RBL 9.0 IAW REO 601R-53-11-171 IAW NDTM 51-20-06 NO DEFECTS NOTED. PERFORMED LPI OF -8 FILLER IAW NDTM 51-20-08. NO DEFECTS NOTED. PARTIALLY INSTALLED -4 DOUBLER, -8 FILLER IS COMPLETELY INSTALLED WORK DONE IAW SRM 51-42-06 AND REO 601R-53-11-171. INSTALLED REMAINING FASTENERS (HI LITES) IN REPAIR IAW REO 601R-53-11-171 AND SRM 51-42-21. APPLIED A023 FINISH AND CIC IAW SRM 51-21-16. WORK COMPLETE.

Part: FLOOR SUPPORT — CORRODED (BS 567-621) · airframe 18,849 hrs · 16,730 cycles

FLOOR SUPPORT HAS MINOR CORROSION AT LBL 27 FROM FS 567 TO 621 AS MARKED.

Part: SEAT TRACK — CORRODED (BS 621) · airframe 18,849 hrs · 16,730 cycles

SEAT TRACK CORRODED JUST FWD OF FS 621 AT LBL 9. REMOVED AND REPLACED SECTION OF SEAT TRACK JUST FWD OF FS 621 AT LBL 9 IAW SRM 51-40-00.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 18,849 hrs · 16,730 cycles

FS 280.00 TRANSVERSE FLOOR BEAM CLIP JUST OTBD OF RBL-9 IS CRACKED. REMOVED AND REPLACED OTBD CLIP AT RBL 9, SRM 51-40-11 AND 51-42-21.

Part: FRAME — CRACKED (BS 559) · airframe 18,849 hrs · 16,730 cycles

FRAME CAP ANGLE CRACKED IN RADIUS AT FS559.00, LBL9.00 AND LBL18.00.

Part: FRAME — CORRODED (BS 349) · airframe 18,849 hrs · 16,730 cycles

CORROSION FOUND AT F.S. 349 FRAME, BL 0. REMOVED LIGHT SURFACE CORROSION AT FS 349 FRAME, BL 0 DAMAGE FOUND TO BE WITHIN LIMITS IAW SRM 53-21-15. REMOVED AND REINSTALLED 4 EA RIVETS FROM REMOVAL OF CORROSION. RESTORED A023 FINISH IAW SRM 51-21-06, 51-21-11.

Part: SEAT TRACK — CORRODED (BS 339) · airframe 18,849 hrs · 16,730 cycles

LT AND RT FWD FLOOR SHORT SEAT TRACKS ARE CORRODED. REMOVED AND INSTALLED NEW LT AND RT FLOOR SHORT SEAT TRACKS AT FS 339.50 AMM 53-01-11.

Part: LENS — CRACKED (EMERGENCY LIGHT)

EMERGENCY LIGHT ASSY AT SERVICE DOOR BELOW GALLEY IS CRACKED. REMOVED AND REPLACE EMERGENCY LIGHT LENS COVER AT SERVICE DOOR BELOW GALLEY IAW AMM 33-51-10-000-801 AND 33-51-10-400-801 WPW 7015097 10/30/09 END [SUPPLEMENTAL -- SDR CLOSED]

Part: FEEDER CABLE — INOPERATIVE (EMERGENCY LIGHTS) · airframe 18,849 hrs · 16,730 cycles

EMERGENCY FLOOR LIGHTING STRIP BETWEEN SEAT 12CD AND LAV DOOR IS INOP. REMOVED AND REPLACED POWER CABLE ON EMERGENCY FLOOR LIGHT TRACK BETWEEN SEAT 12CD AND LAV IAW AMM 33-51-01 THEN COMPLIED WITH OPS TEST OF EMERGENCY FLOOR LIGHT TRACK IAW AMM 33-51-00-710-801. NO OTHER DEFECTS FOUND.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,832 hrs · 15,696 cycles

RT FWD EMERGENCY LIGHT INOP.

Part: ANTI-SKID SYS — MALFUNCTIONED (LANDING GEAR) · airframe 17,737 hrs · 15,603 cycles

ON TAKEOFF AND CLIMBOUT RVD MULTIPLE INTERMITTENT ANTI-SKID OUTBOARD CAUTION MSGS. EMERGENCY DECLARED. A/C RETURNED TO ATL AFTER T/O.

Part: DRAG ANGLE — CRACKED (ASD) · airframe 1 hrs · 1 cycles

ASD AFT DRAG ANGLE CRACKED AT THE MOTOR PULLEY.

Part: BPSU — FAULTY (TE FLAPS) · airframe 16,714 hrs · 14,748 cycles

RECEIVED FLAP FAIL ON APPROACH. DECLARED EMERGENCY, ABORTED APPROACH, LANDED WITHOUT INCIDENT. REPLACED RT BPSU. NO FURTHER DEFECTS. (S)

Part: BPSU — FAILED (TE FLAPS) · airframe 16,708 hrs · 14,744 cycles

FLAPS FAIL CAUTION MSG RECEIVED WHEN FLAPS SELECTED TO 45 DEG ON APPROACH. ACFT LANDED SAFELY. REMOVED AND REPLACED RT BPSU. (S)

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 15,502 hrs · 13,806 cycles

UPON EDDY CURRENT INSPECTION FOUND AFT PRESSURE BULKHEAD CRACKED AROUND LINTEL ATTACHMENT FITTING. REPAIRED PRESSURE BULKHEAD WEB FS 621.0 LINTEL INSTALLATION IAW REO 601R-53-61-1230.

Part: ATTACH BRACKET — CRACKED (FUSELAGE) · airframe 15,507 hrs · 13,806 cycles

DURING HMV3 INSPECTION FOUND LONGITUDINAL FLOORBEAM ATTACH BRACKETS CRACKED AT AFT SIDE. REMOVED AND REPLACED DAMAGED BRACKETS.

Part: WINDOW — CRACKED (COCKPIT) · airframe 15,129 hrs · 13,515 cycles

FLIGHT 5129 - PILOT SIDE WINDOW ARCED AND THEN CRACKED. DECLARED EMERGENCY, DIVERTED TO SYR, LANDED WITHOUT INCIDENT. REPLACED PILOT SIDE WINDOW. NO FURTHER DEFECTS.

Part: GCU — MALFUNCTIONED · airframe 13,767 hrs · 12,448 cycles

ADG DEPLOYED ON WEIGHT OFF GEAR, A/C RETURNED TO ABE AND LANDED SAFELY. REPLACED THE ADG GCU.

Part: WIRE HARNESS — FAULTY (LANDING GEAR) · airframe 13,130 hrs · 11,945 cycles

FLIGHT 5290 - DURING TAKEOFF ROLL RECEIVED AN ANTI-SKID CAUTION MESSAGE, ABORTED TAKEOFF AND RETURNED TO THE GATE. REPLACED THE NR 3 SEGMENTED WIRING HARNESS ON WHEEL SPEED TRANSDUCER.

Part: ELEMENT — FAULTY (HEAT SENSOR) · airframe 12,926 hrs · 11,780 cycles

FLIGHT 5559 - EN ROUTE CVG-CHA RECEIVED A RIGHT FUSELAGE ANTI-ICE DUCT WARNING MESSAGE, FLIGHT RETURNED TO CVG. REPLACED HEAT SENSING ELEMENT IN THE RIGHT WHEEL WELL.

Part: WARNING MESSAGE — FALSE INDICATION (ANTI-ICE DUCT) · airframe 11,946 hrs · 10,825 cycles

FLIGHT 5623 - EN ROUTE CVG-CHA, RECEIVED AN ANTI-ICE DUCT WARNING MESSAGE, FLIGHT DIVERTED TO MEM. PERFORMED AN INSPECTION OF THE 14TH STAGE BLEED LINES AND LOOPS, NO DEFECTS NOTED. PERFORMED GROUND RUNS AND AN OPERATIONAL CHECK OF THE ANTI-ICE SYSTEM. DISCREPANCY COULD NOT BE DUPLICATED BY MAINTENANCE.

Part: WARNING LIGHT — ILLUMINATED (ANTI-ICE SYSTEM) · airframe 11,396 hrs · 10,283 cycles

FLIGHT 5348 - ANTI-ICE DUCT WARNING. OPERATIONAL CHECK OF SYSTEM WAS SATISFACTORY.

Part: WARNING LIGHT — ILLUMINATED (TE FLAPS) · airframe 10,646 hrs · 9,629 cycles

FLIGHT 5651- DURING TAXI OUT RECEIVED A FLAP FAIL CAUTION MESSAGE. FLIGHT RETURNED TO GATE. COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE FIRST EVENT MAINTENANCE ACTION, PARAGRAPH (B) 1, 2, 3 (A, B, C AND E). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES.

Part: PUMP — MALFUNCTIONED (HYD SYSTEM) · airframe 7,933 hrs · 7,224 cycles

FLIGHT 5821 GEAR DISAGREE WARNING. REPLACED THE 3A HYDRAULIC PUMP.

Part: COALESCER BAG — DIRTY (CABIN AIR) · airframe 3,776 hrs · 3,832 cycles

FLIGHT 5297 VISABLE SMOKE IN CABIN CLEANED THE ACM WATER SERPERTOR BAGS. GROUND RAN SYSTEM, NO ODOR NOTED.

Part: INTEGRATED · airframe 2,225 hrs · 2,263 cycles

INTEGRATED DRIVE GENERATOR CAUITON MESSAGE DURING TAKE OFF.SERVICED LTH LEFT ENGINE INTEGRATED DRIVE GENERATOR TO PROPER OIL LEVEL.

Part: CONNECTOR · airframe 1,731 hrs · 1,796 cycles

FLIGHT 6006 LEFT ENGINE OIL PRESSURE INDICATED ZERO DURING T/O.REPAIRED LOOSE WIRING AT PRESSURE TRANSDUCER.

Part: CABLE — DEFECTIVE (CABIN) · airframe 834 hrs · 902 cycles

FLIGHT 5504 FORWARD 1/3 OF EMERGENCY FLOOR PATH LIGHTING IS INOP.REPLACED FLOOR LIGHTING CONNECTOR CABLE.