N973EV

Part: WIRE HARNESS — DAMAGED (NLG STEERING) · airframe 21,344 hrs · 19,319 cycles

RECEIVED NWS INOPERATIVE MESSAGE IN FLT, PERFORMED QRH WOULD NOT RESET. EMERGENCY DECLARED. R & R NOSE LANDING GEAR STEERING HARNESS IAW AMM 32-61-25, OPS CHECKED GOOD.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 20,567 hrs · 18,479 cycles

FS 280 INBD & OTBD CLIPS ARE CRACKED AT LBL 9 AND RBL 9. THIS REPAIR IS CLASSIFIED AS A MINOR REPAIR IAW ASA SOP 5702. (CLOSED)

Part: ANGLE — CORRODED (BS 280) · airframe 20,565 hrs · 18,477 cycles

FS 280.00 FWD J ANGLE CORRODED. REMOVED MINOR SURFACE CORROSION IAW SRM 51-21-06.

Part: ANGLE — CRACKED (BS 280) · airframe 20,565 hrs · 18,477 cycles

FS 280.00 UPPER ANGLE OTBD OF LBL 9 CRACKED AND FS 280.00 WEB CORRODED. REPAIRED IAW REO 601R-53-11-926 REV B.

Part: POST — CRACKED (BS 409) · airframe 20,565 hrs · 18,477 cycles

FOUND FS 409+128 VERTICAL POST BL 0.0 LT AND RT SIDES HAS INDICATIONS NOTED AT WL 69.0 AFT FLANGE RADIUS APPROX .3" IN LENGTH 80 PERCENT FSH. BOTH FAILED NDT INSPECTION. REMOVED POST ASSY IAW SRM 51-42-06. INSTALLED POST ASSY IAW SRM 51-42-06 AND REO 601R-53-41-889, REV A.

Part: BULKHEAD WEB — FAILED · airframe 20,565 hrs · 18,477 cycles

FOUND REAR PRESSURE BULKHEAD WEB THAT SURROUNDS THE LINTEL ATTACHMENT FITTING HAS INDICATION NOTED APPROX 1" IN LEGNTH 100 PERCENT FSH FAILED NDT INSPECTION. REPAIRED IAW EC/TC REO 601R-53-61-1230.

Part: ISOLATOR — BROKEN (BULKHEAD) · airframe 20,565 hrs · 18,477 cycles

REAR PRESSURE BULKHEAD FWD FACE HAS 6 BROKEN ISOLATORS. INSTALLED NEW SERVICEABLE ISOLATORS PN SL2337-3 IAW SRM 51-42-13. REPAIR CLASSIFIED AS MINOR IAW SOP 5702.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 20,565 hrs · 18,477 cycles

FS 280.00 INBD AND OTBD FLOORBEAM ANGLE CRACKED AT LBL 9 AND RBL 9. REMOVED IAW SRM 51-42-06 AND 51-42-21. INSTALLED IAW SRM 51-42-21.

Part: FLOORBEAM — CORRODED (BS 349) · airframe 20,565 hrs · 18,477 cycles

CABIN FLOORBEAM AT FS 349.00 BETWEEN RBL 27 AND RBL 45 IS CORRODED AT SEVERAL LOCATIONS ALONG ENTIRE LENGTH. REPAIRED IAW SRM 51-42-10, 51-21-06, IAW 53-00-00 AND 53-21-15. MINOR REPAIR.

Part: FLOORBEAM — CORRODED (BS 349) · airframe 20,565 hrs · 18,477 cycles

CABIN FLOORBEAM AT FS 349.00 CORRODED AT OTBD END RBL 45. BLENDED MINOR CORROSION, REMOVING .005" D MAX DAMAGE .058" REMAINING WITHIN LIMITS IAW SRM 51-21-06 IAW 53-00-00 AND 53-21-15.

Part: CABLE — WORN (THROTTLE) · airframe 20,567 hrs · 18,479 cycles

RT ENG THROTTLE CABLE AT FS 461.00 OUTER COATING IS TORN. REO 601R-76-11-006 AND MET ALL REQUIREMENTS OF REO 60R-76-11-006. RIGGING OF THE THROTTLE CONTROLS DUE IAW AMM 76-10-00-830-801. PERFORMED RIGGING OF THE THROTTLE CONTROLS IAW AMM 76-10-00-830-801. CHECKS GOOD AT THIS TIME. FUNCTION TEST OF THROTTLE CONTROLS DUE IAW AMM 76-10-00-720-805. ACCOMPLISHED FUNCTIONAL TEST OF THE RT ENG THROTTLE CONTROL IAW AMM 76-10-00-720-805. TEST GOOD. FRICTION TEST OF THROTTLE LEVER DUE IAW AMM 76-10-00-720-802. ACCOMPLISHED FRICTION TEST OF THE RT ENG THROTTLE CONTROL IAW AMM 76-10-00-720-802 AND MFG RIL 2068. TEST GOOD. BACKLASH TEST OF THROTTLE CONTROL DUE IAW AMM 76-10-00-720-803. PERFORMRED BACKLASH TEST OF THE THROTTLE CONTROL IAW AMM 76-10-00-720-803. CKS GOOD AT THIS TIME. DISCONNECTED RT ENGINE THROTTLE CABLE AT THE PYLON IAW AMM 76-11-09-000-80. RECONNECTED RT ENGINE THROTTLE CABLE AT THE PYLON IAW AMM 76-11-09-400-801.

Part: SILL — CORRODED (BS 349-364) · airframe 20,565 hrs · 18,477 cycles

RT CABIN FLOOR SILL CORRODED FROM FS 349.00 TO FS 364.00. CLEANED AREA IAW SRM 51-26-00, REMOVED MINOR CORROSION FROM SURFACE APPROX .003" DEEP MATERAL AFTER BLENDING .060" IAW SRM 51-21-06. ORIGINAL THICKNESS .063 WITHIN LIMITS OF SRM 53-00-00. RESTORED ALODINE AND PAINT FINISH IAW SRM 51-21-11 AND 200 51-25-16. MINOR REPAIR.

Part: ANGLE — CRACKED (BS 484) · airframe 20,565 hrs · 18,477 cycles

FS 484.00 LT ANGLE AT LBL 36.0 IS CRACKED. REPAIRED IAW REO 601R-53-41-059.

Part: ANGLE — CRACKED (BS 484) · airframe 20,565 hrs · 18,477 cycles

FS 484.00 RT, ANGLE AT RBL 27 IS CRACKED. R & R ANGLE IAW SRM 51-40-11, 51-42-06.

Part: CARGO TRACK — CORRODED (BS 559) · airframe 20,565 hrs · 18,477 cycles

CARGO TRACK AT LBL 9, BETWEEN FS 559.00+80 AND 559.00+96 CORRODED. REMOVED AND REPLACED CARGO TRACK IAW SRM 51-40-11& AMM TASK 53-01-11-400-802. MINOR REPAIR.

Part: PANEL — BENT (FUSELAGE) · airframe 20,567 hrs · 18,479 cycles

GROUND AIR CONDITIONING PANEL 172BR FWD & AFT LANDINGS ARE BENT. REMOVED SEALANT FROM REWORK AREAS IAW SRM 51-23-00. REF LINE ITEM 5 FOR APPLICATION OF SEALANT. C/W STEP 1 OF REO 601R-53-61-4105. STEP 2 OF REO 601R-53-61-4105 NEED C/W. C/W STEP 2 OF REO 601R-53-61-4105. PERFORMED EDDY CURRENT OF FWD AND AFT DOOR LANDING REPAIRS IAW NDTM 51-20-26. NO INDICATIONS NOTED AT THIS TIME.

Part: ARM — GOUGED (TE FLAP) · airframe 20,567 hrs · 18,479 cycles

LT OTBD FLAP INBD HINGE ARM HAS 3 GOUGES ON OTBD SIDE WHERE HINGE ARM ATTACHES TO HINGE BOX APPROX .005" DEEP. REPAIRED 3 GOUGES ON LT OTBD FLAP INBD HINGE ARM IAW WITH REO 601R-57-54-197, STEPS 1-5 .005 MATERIAL MAX REMOVED. REO 601R-57-54-194 HAS BEEN ACCOMPLISHED AND ALL STEPS HAVE BEEN DOCUMENTED AND SIGNED FOR ON A NON-ROUTINE WORKCARD. ALL RII'S HAVE BEEN ACCOMPLISHED BY A TRAINED, QUALIFIED AND AUTHORIZED RII INSPECTOR, GMM 3-3 PROCEDURES, PRIOR TO THE ACFT BEING RELEASED TO SERVICE.

Part: ANGLE — CRACKED (BS 621-625) · airframe 20,565 hrs · 18,477 cycles

AFT EQUIPMENT COMPARTMENT FS 621 TO 625 OBLIQUE ANGLES ARE CRACKED LT & RT SIDES. REPLACED LT AND RT OBLIQUE ANGLES IAW SRM 51-42-06 AND 51-40-11. THIS REPAIR IS CLASSIFIED AS A MINOR REPAIR IAW SOP 5702.

Part: SILL — CORRODED (FUSELAGE) · airframe 20,592 hrs · 18,504 cycles

PAX DOOR LOWER SILL CORRODED AROUND PROXIMITY SWITCH AND GROUND STUD. . REMOVED PAX DOOR LOWER SILL ASSY FOR REPLACEMENT IAW SRM 51-42-06 AND 51-42-21. DRILLED AND LOCATED NEW PART 601R-31527-221 IAW SRM 51-40-11 AND 51-40-06. INSTALLED NEW PAX DOOR LOWER SILL ANGLE PN 601R-31527-221 IAW SRM 51-41-02, 51-42-06 AND 51-42-21.

Part: SILL — CORRODED (BS 310-349) · airframe 20,565 hrs · 18,477 cycles

SERVICE DOOR CUTOUT LOWER SILL IS CORRODED FROM FS 310 TO FS 349. REMOVED CORRODED SERVICE DOOR SILL ANGLE ASSY IAW SRM 51-42-13, 51-42-06, 51-42-10,, AND 51-42-21. INSTALLED NEW SERVICE DOOR SILL ANGLE ASSY IAW SRM 51-42-34, 51-42-21, AND 51-42-36, AND 51-42-06.

Part: SILL — CORRODED (FUSELAGE) · airframe 20,565 hrs · 18,477 cycles

PAX DOOR LOWER SILL UPPER ANGLE CORRODED AROUND RIVETS ATTACHING LIGHTNING PROTECTION MOUNTING CLIPS. AFTER FURTHER INVESTIGATION FOUND PROTECTOR LEAD CONNECTION ANGLE TO BE CORRODED ONLY, ANGLE IS IN SERVICEABLE CONDITION WITH NO CORROSION EVIDENT WHATSOEVER. ANGLE WAS CLEANED IAW SRM 51-26-00. FASTENERS WERE REPLACED IAW SRM 51-42-11 AND 51-42-13. MINOR REPAIR.

Part: INVERTER — UNSERVICEABLE (EMERGENCY LIGHTS) · airframe 20,471 hrs · 18,369 cycles

RT EMERGENCY EXIT, FLOOR LEVER EXIT SIGN INOPERATIVE. REMOVED AND REPLACED NR3 INVERTER IAW AMM 33-51-07.

Part: LIGHT — INOPERATIVE (RT OVERWING) · airframe 20,134 hrs · 17,992 cycles

LOWER EXIT SIGN FOR RT OVERWING EMERGENCY EXIT DOOR INOP. R & R RT OVERWING EMERGENCY EXIT DOOR LOWER EXIT LIGHT IAW AMM 33-51-09. OPS CHECK GOOD. NO FURTHER DEFECTS FOUND AT THIS TIME. R & R RT OVER WING EMERGENCY EXIT DOOR LOWER EXIT LIGHT IAW AMM 33-51-09. OPS CHECK GOOD. NO FURTHER DEFECTS FOUND AT THIS TIME.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 20,046 hrs · 17,894 cycles

NR 1 LT EXTERIOR EMERGENCY LIGHT INOP. RELAMPED NR 1 LT EXTERIOR EMERGENCY LIGHT IAW AMM 33-51-21, OP'S CHECK GOOD. RELAMPED NR 1 LT EXTERIOR EMERGENCY LIGHT IAW AMM 33-51-21, OP'S CHECK GOOD.

Part: PLACARD — DETERIORATED (MAIN CABIN) · airframe 19,740 hrs · 17,545 cycles

EXIT PLACARD ON MAIN CABIN DOOR WORN ( NON-REQUIRED PLACARDS ). R & R EXIT PLACARD IAW AMM 11-30-00. (CLOSED)

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 18,967 hrs · 16,628 cycles

AFT CABIN CEILING EMERGENCY LIGHT INOP. RELAMPED AFT CABIN CEILING LIGHT IAW AMM 33-51-16. OPS CHECK GOOD. RELAMPED AFT CABIN CEILING LIGHT IAW AMM 33-51-16. OPS CHECK GOOD.

Part: COALESCER BAG — ODOR (A/C BAY) · airframe 18,168 hrs · 15,700 cycles

STRONG ODOR FROM PACKS. R & R COALESTER SOCKS IAW AMM 21-51-13 OP CK GOOD. ACFT OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,444 hrs · 14,894 cycles

NR 4 CEILING EMERGENCY LIGHT INOPERATIVE.

Part: LIGHT — INOPERATIVE (EMERGENCY EXIT) · airframe 17,247 hrs · 14,687 cycles

RT OVERWING EMERGENCY EXIT LWR EMERGENCY LIGHT, INOPERATIVE.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 16,704 hrs · 14,140 cycles

LEFT BONDED SKIN DOUBLER CRACKED AT FS 640.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 16,704 hrs · 14,140 cycles

RIGHT FLOOR SUPPORT STRUT LOCATED AT FS559.0 NEEDS NDT FOR SUSPECTED CRACK. FOUND RIGHT FLOOR SUPPORT STRUT CRACKED. REMOVED AND REINSTALLED COMPONENTS NECESSARY TO PERFORM THE REPAIR. PERFORMED EDDY CURRENT INSPECTION OF CAP ANGLE AT RBL 9.00 FS 559 IAW NDTM 51-20-06. WORK DONE IAW AMM 21-22-01 PROCEDURE 2.F.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 16,704 hrs · 14,140 cycles

WHILE PERFORMING EC/TC AWL2 53-41-201 FS 559.00, RECEIVED A SUSPECT INDICATION UNDER BEAM AT LBL 18 FRAME CAP ANGLE RADIUS. PERFORMED EDDY CURRENT INSPECTION OF INDICATION AT 559 UNDER BEAM AT LBL 18 IAW NDTM 51-20-06. REMOVED AND REINSTALLED REQUIRED COMPONENTS FOR REPAIR. ALL OPS CHECKS COMPLIED WITH SATISFACTORY AT THIS TIME.

Part: FITTING — CRACKED (FUSELAGE) · airframe 16,704 hrs · 14,140 cycles

CLIP CRACKED AT FS589 AND CARGO DOOR SILL (UNDER DOOR SILL AT FRAME). WORK COMPLETED IN ACCORDANCE WITH IAW SRM 51-42-06, 51-42-21 AND 41-42-15. INSTALLED INTERCOSTAL IAW SRM 51-42-21. COMPLETELY INSTALLED CARGO DOOR SILL IAW SRM 51-41-02. INSTALLED CARGO DOOR BOTTOM FWD LATCH IAW SRM 51-41-02. REPLACED CLIP AND CARGO DOOR SILL WITH NEW CLIP FABRICATED PER REO 601R-53-61-3190, INSTALLED IAW SRM 51-42-06, 51-42-21 AND 51-42-15.

Part: ISOLATOR — BROKEN (BULKHEAD) · airframe 16,704 hrs · 14,140 cycles

2 EA ISOLATORS BROKEN ON FWD SIDE OF AFT PRESSURE BULKHEAD(MARKED)

Part: INTERCOSTAL — CRACKED (PAX DOOR) · airframe 16,704 hrs · 14,140 cycles

AFT SIDE PAX DOOR 318 INTERCOSTAL IS CRACKED.

Part: SENSOR — FAILED (TE FLAP) · airframe 16,461 hrs · 13,897 cycles

FLAP FAIL ON TAKEOFF FLAPS STUCK ON 8FT. EMERGENCY DECLARED, A/C RETURNED TO ATL AFTER T/O. THIS SDR WILL REMAIN OPEN PENDING MTC DETERMINATION OF AN APPROPRIATE CORRECTIVE ACTION. FLT 5108 DEL 38 MINS. SKEW DETECTION SYSTEM. REMOVED AND REPLACED LT NR 3 AND 4 SKEW SENSOR IAW CRJ 200 AMM 27-51-15 OPS CHECK GOOD DEFER CLEARED.

Part: HANDLE — CRACKED (ASD) · airframe 16,260 hrs · 13,714 cycles

ASD HANDLE IS CRACKED.

Part: SPRING STRUT — DEFECTIVE (PAX DOOR)

MAIN DOOR IS NOT LOCKING CLOSE. REMOVED AND REPLACED FWD PAX DOOR GAS SPRING STRUT IAW AMM 52-11-14. OPS CHECK GOOD, ACFT OK FOR SERVICE. (K)

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 12,590 hrs · 10,558 cycles

F/O SIDE FLASHLIGHT INOP.

Part: STRUCTURE — CRACKED (BS 461) · airframe 12,494 hrs · 10,487 cycles

CRACK FOUND ON FLOOR STRUCTURE AT FS 461.00 LBL 9 AND RBL 9.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 12,494 hrs · 10,487 cycles

CLIP CRACKED AT FS 484 LBL 36 UNDER FLOOR.

Part: SILL — CORRODED (FUSELAGE) · airframe 12,494 hrs · 10,487 cycles

CORROSION ON FWD AND AFT BRACKET OF PASSENGER DOOR FLOOR SILL NEAR HINGE ATTACHMENT POINTS.

Part: FLOORBEAM — CORRODED (BS 349) · airframe 12,494 hrs · 10,487 cycles

CORROSION FOUND ON TOP OF BEAM BETWEEN LBL 27 TO 40 FS 349.00.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 12,494 hrs · 10,487 cycles

INTERCOSTAL CRACK BETWEEN FS 621 TO 625 LT AND RT.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 12,494 hrs · 10,487 cycles

PREVIOUSLY REPAIRED FLOOR ANGLE CRACKED AT FS 621 LT AND RT. [06-21-07] REPAIRED IAW REO 601R-53-61-117 REV:C.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 12,494 hrs · 10,487 cycles

CRACK FOUND AT FS 280.00 FLOOR ANGLE IN LOWER FLANGE AT LBL 9.0. [06-21-07] REPAIR CARRIED OUT IAW REO 601R-53-11-171 REV C.

Part: SILL — CORRODED (FUSELAGE) · airframe 12,494 hrs · 10,487 cycles

SERVICE DOOR LOWER SILL PLATE CORRODED. REFERTO EXELTECH W/O YUL000617 NRTC 200-24 FOR ALL WORK ACCOMPLISHED. SUPPLEMENTAL - SDR CLOSED 06/15/07.

Part: SILL — CORRODED (FUSELAGE) · airframe 12,494 hrs · 10,487 cycles

LEFT FLOOR SILL CORRODED BETWEEN FS 574 TO FS 621.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 12,494 hrs · 10,487 cycles

ANGLE CRACKED AT FS 621 CARGO DOOR SURROUND STRUCTURE SUPPORT MEMBER. REFER TO EXELTECH W/O YUL000617 NRTC 200-25 FOR ALL WORK ACCOMPLISHED. SUPPLEMENTAL - SDR CLOSED 06/15/07.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 11,393 hrs · 9,662 cycles

RIGHT EXTERIOR EMERGENCY OVERWING FORWARD LIGHT INOP.

Part: CONNECTOR — BROKEN (EMERGENCY LIGHTS) · airframe 11,360 hrs · 9,636 cycles

FLOOR TRACK LIGHT EMERGENCY AT THE END HAS BROKEN CONNECTOR.

Part: FRAME — CRACKED (BS 640) · airframe 11,360 hrs · 9,636 cycles

LT FS 640.00 DOUBLER CRACKED. REFER TO W/C 1003 FOR CORRECTIVE ACTION. SEE PART C OF SB 601R-53-061. VS813 12-20-06.

Part: PLACARD — MISSING (CABIN) · airframe 11,360 hrs · 9,636 cycles

PAX DOOR EXIT PLACARD MISSING.

Part: TANK — LEAKING (LT WING) · airframe 11,106 hrs · 9,431 cycles

FUEL LEAKING FROM LT WING FUEL TANK IN FLT. EN ROUTE TO ATL A/C DIVERTED TO PIT DUE TO MTC. REMOVED AND INSPECTED FUEL CAP AND O-RING. NO DEFECTS NOTED. CLEANED O-RING AND MATING SERVICE. RESEATED CAP LEAK CHECKS GOOD ON GROUND. SP 680 CLEARED IN ATL. VERIFIED WITH MTC CONTROL. (CLOSED 11/09/06)

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 10,269 hrs · 8,775 cycles

EMERGENCY EXIT EXTERIOR LIGHT OUT OF SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 9,960 hrs · 8,531 cycles

SERVICE DOOR EMERGENCY EXIT SIGN HAS SEVERAL LIGHTS INOP.

Part: ANCHOR FITTING — CRACKED (AIR STAIR DOOR) · airframe 9,893 hrs · 8,481 cycles

ASD AFT ANCHOR FITTING CRACKED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 9,547 hrs · 8,203 cycles

FLOOR EMERGENGY TRACK LIGHTING INOP AT SEAT 10CD.

Part: UNKNOWN — UNKNOWN (TE FLAPS)

DURING CLIMB OUT, AT APPROXIMATELY 5,000 FT, THE CREW RECEIVED A FLAPS FAIL MESSAGE WITH A FLAP DETENT AT ZERO AND THE FLAPS SHOWING 8 DEGREES. THE CREW COMPLIED WITH THE QRH AND THE EMERGENCY VEHICLES WERE DISPATCHED. THE AIRCRAFT RETURNED TO DEPARTURE WHERE IT LANDED SAFELY. MAINTENANCE COMPLIED WITH EO AND AMM WITH NO DEFECTS NOTED. OERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: FLASHLIGHT — INOPERATIVE (COCKPIT)

DURING A GROUND INSPECTION, THE CAPTAIN`S COCKPIT FLASHLIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED TH CAPTAIN`S COCKPIT FLASHLIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)