N981EV

Part: LIGHT — INOPERATIVE (OVERWING EXIT) · airframe 30,900 hrs · 29,816 cycles

RH OVERWING EMERGENCY EXIT LIGHT AT FLOOR LEVEL INOP REPLACED RH OVERWING EMERGENCY EXIT LIGHT PN 6020-5 AT FLOOR LEVEL IAW CRJ-200 AMM 33-51-10. EMERGENCY LIGHTS OPS CHECKS GOOD IAW CRJ-200 AMM 33-51-10.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 30,668 hrs · 29,582 cycles

DURING MORNING WAKE UP FOUND EMERGENCY EXIT SIGN IN MID CABIN FACING FORWARD INOP R&R EMRGENCY LIGH BATTERY PACK #2 IAW AMM 33-51-04. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED AT THIS TIME.

Part: BULKHEAD WEB — DENTED (BS 621) · airframe 29,634 hrs · 28,476 cycles

FS 621 REAR PRESSURE BULKHEAD WEB FWD FACE HAS 2 TOOLING MARKS .1"" ROUND BY .002 DEEP AT LBL 42 AND RBL 42 WL76. REPAIRED AREA IAW REO 601R-53-61-7003 AND GREO 601R-53-61-2155.

Part: FLOOR SUPPORT — CORRODED (BS 529-544) · airframe 29,634 hrs · 28,476 cycles

MULTIPLE CORROSION BETWEEN FS 529.00 TO 544 BETWEEN 2 PREVIOUS REPAIRS IB FLOOR BOARD FLANGE RBL 9. REPAIRED CORROSION BETWEEN FS 529 TO 544 IAW REO 601R-53-41-2495 REV IR DATED 2019-06-19 AND SRM 53-41-43, 53-00-00 INBD FLOOR BOARD FLANGE CONTINUED ON CO 77681119 JOB 87768111 OP317 MOERSCH, DANIEL 7166

Part: FLOOR SUPPORT — CORRODED (BS 449-473) · airframe 29,634 hrs · 28,476 cycles

MULTIPLE CORR BETWEEN FS 449.85 TO 473.15 IB FLOOR BOARD FLANGE RBL 9. FOUND CORROSION OUT OF LIMITS IAW REO 601R-53-00-005. REPAIRED AREA BTW FS 449.85 TO 473.15 IB FLOOR BOARD FLANGE RBL 9 IAW REO 6010R-53-41-2498 REV IR DATED 2019-06-20 MOERSCH, DANIEL 712

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 29,634 hrs · 28,476 cycles

LH OB FLAP BOTTOM SKIN DENTED BETWEEN WS 280.66 AND FS 273 APPROX 6"" WIDE BY 4"" HIGH BY .050 DEEP. REPAIRED LH OB FLAP LOWER SKIN IAW ENDEAVOR EA 257-09206.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 29,634 hrs · 28,476 cycles

WIRE BROKEN FOR WARDROBE EMERGENCY LIGHT. INSTALLED SERVICEABLE CONTACT ON WARDROBE EMERGENCY LIGHT AND INSTALLED CONTACT IN SPLICE CONNECTOR IAW CRJ 200 ESPM 20-17-10 OPS CHECK GOOD IAW CRJ 200 AMM 33-51-00-710-801.

Part: FLOOR SUPPORT — CORRODED (BS 513-544) · airframe 29,634 hrs · 28,476 cycles

MULTIPLE CORR BETWEEN FS 513 TO FS 544 OB FLOOR BOARD FLABGE RBL9. REPAIRED CORROSION DAMAGE ON RBL 9 BETWEEN FS 513 AND FS 544 IAW BOMBARDIER REO 601R-53-41-2495 REV IR DATED 2019-06-19 OB FLOOR BOARD FLANGE.

Part: FRAME — CORRODED (BS 333) · airframe 29,634 hrs · 28,476 cycles

FRAME 333 IS CORRODED AT STR 22R. REMOVED AND REPLACED FS 333 FRAME SECTOR BETWEEN STR 18 AND 23R IAW CRJ 200 SRM 51-42-06 AND 51-42-21

Part: FRAME — CORRODED (BS 574) · airframe 29,634 hrs · 28,476 cycles

FS 574.00 FRAME CORRODED ON FWD SIDE BETWEEN STRINGER 25L AND 25R. REPLACED FS 574 LOWER FRAME SECTION P/N 601R36024-61 IAW CRJ 200 SRM 51-42-06, 51-42-21, AND 51-40-11 TR#51-42

Part: FRAME — CORRODED (BS 589) · airframe 29,634 hrs · 28,476 cycles

FS 589 FRAME CORRODED ON FWD AND AFT SIDES BETWEEN STRINGERS 22L AND 23R. REPLACED FS 589 FRAME IAW SRM 51-42-21, 51-42-06,51-40-11 TR 51-42 51-23-00, 51-21-16, 51-25-00, AND 51-21-11

Part: PLATE — CORRODED (BS 310) · airframe 29,634 hrs · 28,476 cycles

WARDROBE AFT INBD AND OB MOUNT BOLT PLATES CORRODED AT FS 310 LBL 18 AND LBL 36. REMOVED AND REPLACED WARDROBE AFT IB AND OB MOUNT BOLT PLATES IAW SRM 51-42, 51-42-06, AND 51-42-13.

Part: VERTICAL BEAM — CRACKED (BS 409) · airframe 29,634 hrs · 28,476 cycles

FS409.00 + 128 VERTICAL BEAM AT LBL27 SHOWS VISUAL SIGNS OF A CRACK OF A CRACK ON INBD BOTTOM SIDE. THIS ENTRY ICLUDES WORK CONTINUATION CARD JOB 87768111 OP312 REPAIRED LBL27 POST AT FS409+128 IAW BOMBARDIER GREO 601R53-41-056. WVAC EMP STAMP 769

Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 29,634 hrs · 28,476 cycles

FOUND REAR PRESSURE BULKHEAD WEB HAS INDICATIONS NOTED AT BL0 WL112 4 INCHES LONG 100% FSH FAILED NDT INSPECTION. INCLUDES WORK CONTINUATION CARD JOB 877681115 OP70 REPAIRED BULKHEAD IAW BOMBARDIOER GREO 601R-53-61-1285. WVAC EMP STAMP 769

Part: FLOORBEAM — CRACKED (BS 460) · airframe 29,634 hrs · 28,476 cycles

RH FS460 FLOOR SUPPORT FITTING CRACKED AT OUTBOARD SIDE OF RBL9. REMOVED AND REPLACED FS480 FLOOR FITTING ON OUTBOARD SIDE OF RBL9 IAW SRM 51-42-21.

Part: SUPPORT ANGLE — CORRODED (BS 319) · airframe 29,634 hrs · 28,476 cycles

SERVICE DOOR LOWER SILL ANGLE SUPPORT ANGLE CORRODED AT FS319. REPLACED ANGLE IAW SRM 51-42-06 AND 51-42-21.

Part: FLOOR SUPPORT — CORRODED (BS 424-439) · airframe 29,634 hrs · 28,476 cycles

MULTIPLE CORR BETWEEN FS 424 TO FS 439 OUTBD FLOOR BOARD FLANGE RBL9. FOUND CORROSION OUT OF LIMITS IAW REO 601R-53-00-005. REPAIRED AREA BETWEEN FS 424 TO FS 439 O/B FLOOR BOARD FLANGE RBL9 IAW REO 601R-53-41-2499 REV -- DATED 2019-06-20.

Part: FLOOR SUPPORT — CORRODED (BS 409-439) · airframe 29,634 hrs · 28,476 cycles

MULTIPLE CORR BETWEEN FS 409+128 TO FS 439 LBL9 INBD FLOOR BOARD FLANGE. FOUND CORROSION OUT OF LIMITS IAW REO 601R-53-00-005. REPAIRED CORROSION IAW REO 601R-53-41-2490 REV-- .

Part: FLOOR SUPPORT — CORRODED (BS 424-439) · airframe 29,634 hrs · 28,476 cycles

CORROSION AT BS 424 TO 439, LBL9 OUTBD FLOOR SUPPORT. FOUND DAMAGE OUT OF LIMITS IAW REO 601R-53-00-005. REPAIRED AREA IAW REO 601R-53-41-2490 REV--.

Part: STRAP — CORRODED (BS 559 FLOORBEAM) · airframe 29,634 hrs · 28,476 cycles

RH F.S. 559 FLOOR SUPPORT STRAP CORRODED BETWEEN RBL27 AND RBL 42. LOCATED AND DRILLED NEW SERVICEABLE STRAP P/N 601R31025-29 IAW SRM 51-40-11, INSTALLED NEW SERVICEABLE STRAP IAW SRM 51-42-06 AND SRM 51-42-13

Part: CARGO TRACK — CORRODED (BS 605-621) · airframe 29,634 hrs · 28,476 cycles

CARGO COMPARTMENT BAGGAGE RAIL CORRODED BETWEEN FS 605 AND FS 621 LBL 9.0. REMOVED AND REPLACED WITH SERVICEABLE TRACK P/N 601R31032-51 IAW CRJ 200 AMM 53-00-49-400-801 & 53-00-49-000-801. REMOVED TAPE.WVAC 712

Part: ATTACH ANGLE — CRACKED (BS 280 BULKHEAD) · airframe 29,634 hrs · 28,476 cycles

STRINGER 3L UPPER ATTACH ANGLE CRACKED JUST AFT OF FS 280 BULKHEAD. REMOVED AND REPLACED STRINGER 3L CRACKED ATTACH ANGLE JUST AFT OF FS 280 BULKHEAD WITH NEW SERVICEABLE ATTACH ANGLE PN 600-31057-19 IAW CRJ 200 SRM 51-42-06 AND 51-40-11 TR 51-42

Part: BRACKET — CORRODED (BS 333) · airframe 29,634 hrs · 28,476 cycles

CORRODED CLIP ON INTERCOSTAL BETWEEN FS 319-FS333 AT STR 23. INSTALLED A NEW BRACKET IAW SRM 51-42-06 AND SNIEO 601R44010-501.

Part: FLOORBEAM — CRACKED (BS 484) · airframe 29,634 hrs · 28,476 cycles

LH FS 484.00 FLOOR SUPPORT INTERCOSTAL ANGLE CRACKED AT LBL 27. REMOVED AND REPLACED LH FS 484.00 INTERCOSTAL ANGLE AT LBL 27 IAW CRJ200 SRM 51-42-21. REMOVED TAPE. WVAC 712.

Part: FLOOR SUPPORT — CRACKED (BS 484) · airframe 29,634 hrs · 28,476 cycles

RH FS 484.00 FLOOR SUPPORT INTERCOSTAL ANGLE CRACKED AT RBL 27. REMOVED AND REPLACED RH FS 484.00 INTERCOSTAL ANGLE AT RBL 27 SRM 51-42-21.

Part: STRINGER — CRACKED (BS 379) · airframe 29,634 hrs · 28,476 cycles

STRINGER 3L CRACKED AT F.S. 379. REPAIRED STRINGER 3L IAW EA 253-09203.

Part: FRAME — CORRODED (BS 605) · airframe 29,634 hrs · 28,476 cycles

CARGO BAY FS605 FRAME CORRODED FROM STRINGER 23R TO STRINGER 21R. REFERENCE CONTINUATION CARD 87768111 OP 304. REMOVED, LOCATED DRILLED AND INSTALLED NEW SERVICEABLE FS 605 LWR FRAME SEGMENT IAW CRJ 200 SRM 51-42-06, 51-42-21,51-40-11,51-12-16,51-25-00 AND 51-21-11 AND AMM 38-32-01-400-802. OPS CHECK GOOD

Part: FRAME — CRACKED (BS 333) · airframe 29,634 hrs · 28,476 cycles

F.S.333 FRAME CRACKED ABOVE PAX DOOR CUT OUT BETWEEN STRINGER 0 AND 1L1.MARKED WITH TAPE.2. REMOVED CRACKED FS 333 FRAME ABOVE PAX DOOR CUT OUT IAW CRJ200 SRM 51-42-06 & 51-42-21.3NOT USED. 4)PAINT, SEALANT,AND CIC REQUIRED5)DISPLACED WIRE BUNDLE FROM JB1 TO FS 349 STR1-2.6)DISPLAPLACED LWR GEN CONTROL UNIT BY REMOVING 4 EA SCREWS. - "1)TAPE REMOVED2)INSTALLED NEW SERVICEABLE FS 333 FRAME ABOVE PAX DOOR CUT OUT PN 601R32004-41 IAW CRJ 200 SRM 51-42-214)SEALED REPAIR IAW CRJ200 AMM 51-23-00-390-804 AND PAINTED REPAIR IAW CRJ 200 SRM 51-25-16 APPLIED CIC TO REPAIR IAW CRJ 200 MM 51-25-56-390-802WVAC712 5)ROUTED GEN 1 WIRE HARNESS BACK IAW CRJ 200 ESPM 20-12-00. WVAC 769 6) MOUNTED LOWER GCU IAW CRJ 200 AMM 24-11-07-400-801. WVAC 769

Part: FLOORBEAM — CRACKED (BS 280) · airframe 29,634 hrs · 28,476 cycles

FS 280 FLOOR SUPPORT BEAM PREVIOUS REPAIR CLIPS CRACKED INBD AND OB. LOCATED, DRILLED, AND INSTALLED I/B AND O/B FS 280.00 CLIPS PN 601R3113-57 AT LBL 9.0 IAW CRJ 200 SRM 51-42-21, 51-40-11, TR 51-42 AND RE-MOVED TAPE. WVAC 712

Part: FLOOR SUPPORT — CORRODED (BS 319) · airframe 29,634 hrs · 28,476 cycles

RIGHT FLOOR SILL HAS CORROSION UNDER AFT END OF SILL, FS 319, RBL 42. REMOVED AND REINSTALLED NEW PLATE ASSY#601R31148-79 TO RBL 42-FS 319 IAW SRM 51-42-21 AND SRM 51-42-06.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 29,634 hrs · 28,476 cycles

FS 280 BEAM UPPER J-ANGLE PREVIOUS REPAIR ANGLE CRACKED OUTBD OF RBL 9. INSTALLED NEW ANGLE P/N 601R-53-137-6 AT FS 280 IAW CRJ 200 SRM 51-42-06.WVAC 769

Part: FLOORBEAM — CRACKED (BS 280) · airframe 29,634 hrs · 28,476 cycles

FS 280 BEAM UPPER J-ANGLE CRACKED APPROX. 4""LONG OUTBD OF LBL9. REPAIRED FS 280 BEAM UPPER J-ANGLE AT LBL 9 IAW BOMBARDIER REO 601R-5311-138 REV A DATED 2010-11-10.

Part: BULKHEAD WEB — CHAFED (BS 621) · airframe 29,634 hrs · 28,476 cycles

FS 621 REAR PRESSURE BULKHEAD WEB FWD FACE HAS DAMAGE AT LBL9,18,36,AND RBL9,18,36 WL 103. REPAIRED IAW GREO 601R-53-61-2155.

Part: FITTING — CRACKED (WINDOW POST) · airframe 29,634 hrs · 28,476 cycles

PILOT WINDSHIELD SIDE POST LOWER AFT FITTING CRACKED. DRILLED UP AND INSTALLED NEW SERVICEABLE PILOT WINDSHIELD SIDE POST LOWER AFT FITTING P/N 601R33235-35 IAW TR#51-42-51-40-11-000 AND 51-42-21-100.

Part: FITTING — CRACKED (WINDOW POST) · airframe 29,634 hrs · 28,476 cycles

CO-PILOT WINDSHIELD SIDE POST LOWER AFT FITTING CRACKED. REMOVED AND INSTALLED NEW SERVICEABLE COPILOT WINDSHIELD SIDE POST LOWER AFT FITTING IAW SRM 51-40-11 AND 51-42-21.

Part: WINDOW POST — CRACKED (COCKPIT) · airframe 29,634 hrs · 28,476 cycles

WINDSHIELD CENTER POST BOTTOM LH AND RH FITTINGS CRACKED. REMOVED AND REPLACED DAMAGED WINDSHIELD CENTER POST FITTINGS IAW SRM 51-40-11 TR 51-42 AND 51-42-21.

Part: FLOORBEAM — CORRODED (BS 559) · airframe 29,634 hrs · 28,476 cycles

RT FLOOR BEAM CAP CORRODED AT FS 559 INBD SIDE OF RBL9. REPAIRED AREA IAW REO 601R-53-41-2483.

Part: STRAP — CORRODED (BS 559 FLOORBEAM) · airframe 29,634 hrs · 28,476 cycles

LH FS 559 FLOOR SUPPORT STRAP CORRODED BETWEEN LBL27 AND LBL42. LOCATED AND DRILLED NEW SERVICEABLE STRAP PN 601R31025-291AW IAW SRM 51-40-11, INSTALLED NEW SERVICEABLE STRAP IAW CRJ 200 SRM 51-42-06 AND SRM 51-42-13.

Part: FLOORBEAM — CORRODED (BS 621) · airframe 29,634 hrs · 28,476 cycles

LH FLOOR SUPPORT ANGLE ATTACHED TO FS 621 PRESSURE BULKHEAD CORRODED BETWEEN LBL27 AND LBL42. REPAIRED IAW BOMBARDIER REO 601R-53-61-7009.

Part: STIFFENER — CRACKED (BS 621 BULKHEAD) · airframe 29,634 hrs · 28,476 cycles

FOUND REAPR PRESSURE BULKHEAD Z-MEMBER BL0.0 WL 112 HAS INDICATION NOTED 2 INCHES LONG 60% FSH FAILED NDT INSPECTION. (FROM CONTINUATION CARD OP69) REPAIRED IAW BOMBARDIER GREO 601R-53-61-1285 REV E.

Part: BRACKET — CRACKED (NLG WW) · airframe 29,634 hrs · 28,476 cycles

RIGHT NLG WHEEL WELL HYD TRANSDUCER BRACKET CRACKED. REMOVED ADN REPLACED RH TRANSDUCER BRACKET PN 601R75262-157 IAW CRJ 200 SRM 51-40-11 & 51-42-06

Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 29,634 hrs · 28,476 cycles

FOUND REAR PRESSURE BULKHEAD WEB HAS INDICATIONS NOTED AT RBL 27.50 WL 99 3 INCHES LONG 60% FSH FAILED NDT INSPECTION. REPAIRED IAW GREO 601R-53-61-1285 REV E.

Part: HANDLE — CRACKED (E/E BAY DOOR) · airframe 29,634 hrs · 28,476 cycles

FOUND MAIN AVIONICS DOOR HANDLE HOUSING HAS INDICATIONS NOTED AROUND ENTIRE BASE OF SHAFT HOUSING FAILED NDT 100% FSH. REMOVED AND REPLACED MAIN AVIONICS DOOR HANDLE ASSY IAW CRJ 200 SRM 51-42-41.

Part: BRACKET — CRACKED (OIL LINE) · airframe 29,634 hrs · 28,476 cycles

AFT EQUIPMENT COMPARTMENT HYD. SYSTEM #2 PRESSURE AND RETURN FILTER BRACKET IS CRACKED AT THE AFT BOTTOM CORNER. REMOVED AND REPLACED SYSTEM #2 HYD PRERSSURE AND RETURN FILTER BRACKET INTERCOSTAL IAW CRJ 200 SRM 51-42-06, 51-42-21, 51-45-00, 51-40-11. LEAK OPS AND BOND CHECK GOOD

Part: NOT REPORTED — MALFUNCTIONED (NR 2 ENGINE) · airframe 28,368 hrs · 27,114 cycles

DURING ENGINE START OF THE NUMBER 2 ENGINE THERE WAS NO LIGHT OFF. SHORTLY THERE AFTER THE GROUND CREW INFORMED US SMOKE AND A LITTLE BIT OF FLAMES WERE COMING OUT OF THE ENGINE. REMOVED FUEL CONTROL UNIT IAW AMM 73-21-01. BREAKERS PULLED + COLLARED CBP-1 M2, M3, M4, M5. REQUEST NO ELECTRICAL POWER. AICRAFT NOT AIRWORTHY, WORK ON GOING INSTALLED MAIN FUEL CONTROL IAW AMM 73-21-01. LEAK CHECK GOOD IAW 71-00-00. REMOVED FUEL PUMP IAW AMM 73-11-01. INSTALLED FUEL PUMP IAW AMM 73-11-01. LEAK CHECK GOOD IAW AMM 71-00-00.

Part: SDU — FAULTED (TE FLAPS) · airframe 27,938 hrs · 26,640 cycles

FLAPS FAILED CAUTION AT FLAPS 12, FAILED ON RETRACTION IN FLIGHT, FLAP HANDLE AT 8, EICAS AT 12 BETWEEN 150 - 200 KTS, 2-3 MINUTE FLIGHT TIME. PERFORMED A FLAP FAIL RESET, RESET SUCCESSFUL. PERFORMED TROUBLESHOOTING IAW FIM 27-50-00, REV 54 IAW AD 2009-06-12, PARAGRAPH H, 6, I, AND TD 00100-R6 FIM TECHNICAL SUPPLEMENT. R & R THE SDU . PERFORMED TORQUE CHECK IAW AML 3352937-2.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 27,238 hrs · 25,901 cycles

EMERGENCY LIGHT ON OVERHEAD PANEL INOPERATIVE. REMOVED AND REPLACE THE BULBS IAW AMM 31-11-00. OPS CHECKED GOOD.

Part: STRUT — MALFUNCTIONED (NLG) · airframe 26,871 hrs · 25,513 cycles

NOSE GEAR DID NOT RETRACT AFTER TAKE OFF. MASTER WARNING MESSAGES, GEAR DISAGREE AND NOSE GEAR DOOR RAN QRH AND RETURNED TO DEPARTURE. R & R THE NOSE LANDING GEAR SHOCK STRUT. RIGGED & OPS CHECKED GOOD. GEAR DISAGREE OPS CHECK PERFORMED IAW AMM 32-30-00. OPS CHECKED GOOD.

Part: APU — FAILED · airframe 26,657 hrs · 25,289 cycles

APU AUTO SHUTDOWN, APU FAULT CAUTION MESSAGE. ABOUT TO PUSH APU SHUT DOWN, RAMP SAID APU HAD FIRE AND SMOKE COMING OUT OF IT. APU WENT FROM 100% TO 0% IN A SECOND. CONTINUE FROM ABOVE ABOUT TO PUSH, SMELLED SMOKE IN THE COCKPIT ALONG WITH A VIBRATION. RAMP TOLD US THERE WAS FIRE AND SMOKE COMING FROM THE APU. REMOVED ELECTRICS FROM APU AND BLEED AIR SECURED APU. NO FIRE INDICATION ON EICAS. PERFORMED INSPECTION OF APU INLET IAW AMM 49-14-01, NO DEFECTS NOTED. PERFORMED DETAIL INSP OF INSPECTION OF THE APU INTAKE DOOR IAW 49-14-01, NO DEFECTS NOTED. CHECK APU DUCTS, TURBINE HOUSING AND GVI OF APU IAW AMM 49-20-00, NO DEFECTS NOTED. REMOVED AND REPLACED THE APU IAW 200-49-10-00. OPS CHECKED GOOD.

Part: OXYGEN MASK — LEAKING (FLIGHT DECK) · airframe 26,237 hrs · 24,845 cycles

CAPTAIN'S OXYGEN MASK HEAD HARNESS LEAKS WHEN TESTED. REPLACED THE OXYGEN MASK IAW 35-11-12-000/400-801. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,180 hrs · 24,787 cycles

LT EMERGENCY LIGHT BEHIND OVERWING EXIT IS OUT. REPLACED BULB IN LT AFT OVERWING EXIT LIGHT IAW AMM TASK 33-51-21-400-801 OPS CK GOOD.

Part: THERMAL SWITCH — FAILED (LT WING) · airframe 25,814 hrs · 24,382 cycles

LEFT WING OVERHEAT WARNING MESSAGE. REMOVED AND REPLACED LEFT WING OVERHEAT SENSORS AMM 30-12-14, OPS CHECKED GOOD. REMOVED AND REPLACED ALL 5 LT WING SENSORS UNDER WING L/E PANEL BTW WS 78.39-86.45 IAW AMM 30-12-12. LEFT WING LEADING EDGE DAMAGE DUE TO ANTI ICE OVERHEAT. REMOVED DAMAGED LT WING CENTER L/E ASSY 530JL. DRILLED UP AND COUNTER SUNK NEW L/E ASSY 530JL. INSTALLED AND ADJUSTED PICCOLO TUBE IN NEW WING L/E ASSY. INSTALLED LT WING CENTER L/E PANEL IAW AMM 57-41-01, SRM 51-40-11. LT WING CENTER L/E ASSY 530JL P/N 601R12044-5 S/N ASAP-3079.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 25,548 hrs · 24,078 cycles

PAX DOOR AFT DRAG ANGLE CRACKED. COMPLIED WITH ECTC REO 601R-52-11-513. AIRCRAFT APPROVED FOR RETURN TO SERVICE.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 25,548 hrs · 24,078 cycles

LBL 27 SEAT TRACK FROM BS 559+80 TO 559+96 IS CORRODED OUT OF LIMITS. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801 AND 53-00-49-400-801.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 25,548 hrs · 24,078 cycles

FLOORBEAM LBL 9 CORRODED. MAINTENANCE REMOVED AND REPLACED BEAM IAW REO 601R-53-51-291. AIRCRAFT APPROVED FOR RETURN TO SERVICE.

Part: SEAT TRACK — CORRODED (BS 394-409) · corrosion level 2 · airframe 25,548 hrs · 24,078 cycles

SEAT TRACK LBL 9 BS 394 - 409+128 HAS CORROSION. REPAIRED IAW ECTC/REO 601R-53-00-485 AND GENERIC REO 601R-53-00-485 REV B. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-00-11-000-802, 53-00-11-400-802. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SEAT TRACK — CORRODED (BS 559) · corrosion level 2 · airframe 25,548 hrs · 24,078 cycles

RBL 9 SEAT TRACK CORRODED OUT OF LIMITS. REMOVED AND REPLACED THE SEAT TRACK IAW ECTC REO 601R-53-00-485. AIRCRAFT APPROVED FOR RETURN TO SERVICE.

Part: SEAT TRACK — CORRODED (BS 559) · corrosion level 2 · airframe 25,548 hrs · 24,078 cycles

SEAT TRACK LBL 9 CORRODED OUT OF LIMITS. MAINTENANCE REMOVED AND REPLACED SEAT TRACK IAW ECTC REO 601R-53-00-485. AIRCRAFT APPROVED FOR RETURN TO SERVICE.

Part: SEAT TRACK — CORRODED (BS 409-559) · airframe 25,548 hrs · 24,078 cycles

DURING C CHECK, FOUND THE RT SEAT TRACK CORRODED AT RBL 9 BETWEEN BS 409+128 - 559. COMPLIED WITH ECTC REO 601R-53-00-485, GREO 601R-53-00-485 REV B, AND AMM 53-01-11-000-802.

Part: FLOOR SUPPORT — CORRODED (BS 409) · airframe 25,548 hrs · 24,078 cycles

DURING CARE MOD FOUND THE FLOOR SUPPORTCORRODED, RBL 9 BETWEEN BS 409 - 409+128. R & R THE FLOOR SUPPORT IAW REO 601R-53-51-885 REV 0 AND ECTC REO 601R-53-51-885 REV 0

Part: SEAT TRACK — CORRODED (BS 394-409) · airframe 25,548 hrs · 24,078 cycles

DURING C CHECK, FOUND SEAT TRACK CORRODED LBL 9 BETWEEN BS 394 - 409+128. R & R THE SEAT RACK IAW AMM 53-00-11-000-802 & 53-00-11-400-802.

Part: SEAT TRACK — CORRODED (BS 409-559) · airframe 25,548 hrs · 24,078 cycles

DURING C CHECK, FOUND SEAT TRACK CORRODED. R & R THE SEAT TRACK IAW AMM 53-00-11-000-802 & 53-00-11-400-802. 00-485 REV B.

Part: WEB — DAMAGED (BS 559) · airframe 25,548 hrs · 24,078 cycles

DURING C CHECK, DAMAGED BEAM WEB @ BS 559+16 - 559+32. C/W ECTC SNIEO 601R31119 S02.

Part: CROSSBEAM — CORRODED (BS 559) · airframe 25,548 hrs · 24,078 cycles

DURING C CHECK, FOUND CROSSBEAM CORRODED BS 559+48, RBL42. C/W ECTC REO 601R-53-51-292.

Part: FLOORBEAM — CORRODED (BS 559) · airframe 25,548 hrs · 24,078 cycles

CORROSION ON FLOORBEAM AT BS 559+48, RBL42. MAINTENANCE COMPLIED WITH ECTC REO 601R-53-51-292

Part: FLOOR SUPPORT — CORRODED (BS 409-559) · airframe 25,548 hrs · 24,078 cycles

DURING C CHECK FOUND CARGO BAY DOOR FLOOR SUPPORT CORRODED. REMOVED CORROSION AND REPAIRED IAW REO 601R-53-00-526 AND ECTC REO 601R-53-00-526.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 25,548 hrs · 24,078 cycles

DURING C CHECK, FOUND SEAT TRACK CORRODED. R & R THE SEAT TRACK IAW AMM 53-00-49-000-801 AND 53-00-49-400-801.

Part: FLOOR SUPPORT — CORRODED (BS 574-621) · airframe 25,548 hrs · 24,078 cycles

DURING C CHECK FOUND FLOOR SUPPORT CORRODED LBL 27 BETWEEN BS 574 - 621. R & R THE FLOOR SUPPORT IAW SRM 51-40-11, REO 601R-53-61-3778, AND ECTC REO 601R-53-61-3778.

Part: FLOOR SUPPORT — CORRODED (BS 559-574) · airframe 25,548 hrs · 24,078 cycles

DURING C CHECK, FOUND THE FLOOR SUPPORT CORRODED BS 559+16 - 574. C/W ECTC REO 601R-53-51-291.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 25,548 hrs · 24,078 cycles

DURING C CHECK FOUND LT FLOOR SILL CORRODED BETWEEN FS559+16 - FS559+64. MTC C/W ECTC REO 601R-53-00-526 AND GREO 601R-53-00-526 DATED 05-22-13.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 25,548 hrs · 24,078 cycles

DURING C CHECK, FOUND SEAT TRACK CORRODED BS 559 - 559+85. R & R THE SEAT TRACK, C/W ECTC REO 601R-53-00-485.

Part: FLOOR SUPPORT — CORRODED (BS 394) · airframe 25,548 hrs · 24,078 cycles

DURING C CHECK FOUND RT FLOOR SUPPORT CORRODED BS 394. REPAIRED FLOOR SUPPORT BETWEEN BS 280 & 409+128 IAW ECTC REO 601R-53-00-530 REV A.

Part: CROSSBEAM — CRACKED (BS 280) · airframe 25,548 hrs · 24,078 cycles

DURING C CHECK, FOUND CCROSSBEAM CRACKED NEAR RBL 9, BS 280. COMPLIED WITH ECTC REO 601R-53-11-171 AND 601R-53-11-137.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 25,548 hrs · 24,078 cycles

MAC - DURING C CHECK FOUND LT FLOOR SILL CORRODED AT FS 409+16. MTC REPAIRED FLOOR SILL BETWEEN FS 280 & FS 409+128 IAW REO 601R-53-530 REV A.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 24,716 hrs · 23,230 cycles

GALLEY EMERGENCY LIGHT INOPERATIVE. R & R THE WIRE SPLICES FOR LY5C22 AND LY6C22 IAW ESPM 20-16-00. OPS CHECK GOOD.

Part: BULKHEAD — CRACKED (BS 621) · airframe 24,675 hrs · 23,191 cycles

AFT PRESSURE BULKHEAD FOUND CRACKED AT LBL 27.50. REPAIRED IAW REO 601R-53-61-1541, REV F.

Part: ISOLATOR — CRACKED (BS 621 BULKHEAD) · airframe 24,675 hrs · 23,191 cycles

13 ISOLATORS CRACKED OR BROKEN OFF OF THE LINER STANDOFFS ON THE FWD SIDE OF REAR PRESSURE BULKHEAD. REMOVED DAMAGED ISOLATORS AND REPLACED WITH NEW ISOLATORS IAW SRM 51-42-13.

Part: OVERHEAT LOOP — MALFUNCTIONED (LT ENGINE) · airframe 23,861 hrs · 22,384 cycles

LEFT 14TH DUCT WARNING MESSAGE IN FLIGHT. ACFT DIVERTED. MESSAGE REMAINED ON AFTER QRH PROCDEDURE. MESSAGE ALSO REMAINED ON AFTER SHUTDOWN AT GATE. EMERGENCY ACTIONS. R & R 14TH STAGE PYLON LOOP A59WK IAW AMM 36-21-00, OPS CHECKED GOOD IAW 36-21-00-710-801. NO DEFECTS NOTED.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 22,861 hrs · 21,415 cycles

EMERGENCY LIGHTS WILL NOT STAY ON FOR MORE THAN A FEW SECONDS. ENERGIZED EMERGENCY POWER PACKS FOR 30 MINUTES PERFORMED TEST OF EMEGENCY LIGHTS IAW AMM 33-51-00. OPS CHECKED GOOD. ACFT OK FOR SERVICE.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 22,544 hrs · 21,077 cycles

LEFT AFT EMERENCY LIGHT INOPERATIVE ON EXTERIOR OF ACFT. R & R BULB IAW AMM 33-51-21. OPS CHECKED GOOD. ACFT OK FOR SERVICE.

Part: BULKHEAD — CRACKED (BS 202) · airframe 22,205 hrs · 20,736 cycles

BS 202 BULKHEAD CRACKED. REPAIRED IAW REO 601R-53-11-563, REV C. MAJOR REPAIR IAW GMM 5-3.

Part: BULKHEAD — CRACKED (BS 205) · airframe 22,211 hrs · 20,742 cycles

TWO .2500 FT CRACKED ON BULKHEAD AT FS 202.75 AT PARKING BRAKE CABLE ENTRY/EXIT POINT. FS 202.75 BULKHEAD CRACKS COMPLETED, ACFT RETURN TO SERVICE.

Part: DOOR FRAME — CRACKED (EMERGENCY EXIT) · airframe 21,436 hrs · 19,940 cycles

CREW ESCAPE HATCH SURROUND FRAME AT FS 276.00 HAS .02 INCH CRACK. REPAIRED IAW EO CL600-2B19-53-I00276/P1.

Part: INTERCOSTAL — CRACKED (BS 621-625.3) · airframe 21,450 hrs · 19,958 cycles

FS 621-625.3 INTERCOSTAL, CRACKED IN CORNER RADIUS OF THE AFT END APPROX .5 INCH L. REMOVED INTERCOSTAL IAW SRM 51-42-06, 51-42-21. LOCATED, DRILLED AND INSTALLED NEW INTERCOSTAL IAW SRM 51-40-11.

Part: INTERCOSTAL — CRACKED (BS 621-625) · airframe 21,436 hrs · 19,940 cycles

FS 621-625.3 INTERCOSTAL, IS CRACKED IN CORNER RADIUS OF THE AFT END APPROX .5" L. REPAIRED IAW SRM 51-42-06, 51-42-21, 51-40-11.

Part: ANGLE — CRACKED (BS 625) · airframe 21,436 hrs · 19,940 cycles

LT AND RT FS 625 UPPER OBLIQUE ANGLES ARE CRACKED. REMOVED CRACKED LT & RT FS 625 UPPER OBLIQUE ANGLES LOCATED, DRILLED & INSTALLED NEW LT & RT FS 625 UPPER OBLIQUE ANGLES IAW SRM 51-40-11, 51-42-21 & 51-42-06.

Part: POST — CRACKED (BS 409) · airframe 21,436 hrs · 19,940 cycles

FOUND FS 409.00+128, RBL 18 INBD AND OTBD VERT POSTS HAVE INDICATIONS NOTED IN AFT FLANGE RADII AT WL 69. BOTH APPROX .300" LONG X 50 PERCENT FSH. FAILED NDT INSPECTION. REMOVED POST IAW SRM 51-42-06. LOCATED & DRILLED NEW SERVICEABLE POSTS PN 601R32208-32S & 601R32208-156 IAW SRM 51-40-11. RIVETED POSTS TOGETHER IAW SRM 51-42-06. INSTALLED POSTS IAW SRM 51-42-06 & REO 601R-53-41-889.

Part: POST — CRACKED (BS 409) · airframe 21,436 hrs · 19,940 cycles

FOUND FS 409.00+128 LBL 18 OTBD VERTICAL POST HAS INDICATION NOTED AT TOP FASTENER (COMMON WITH BULKHEAD) AT WL 69 APPROX .250" LONG X 60 PERCENT FSH. FAILED NDT INSPECTION. REMOVED 409.00+128 VERTICAL POST ASSY AT LBL 18 IAW SRM 51-42-06. COMPLIED WITH EC/TC REO 601R-53-41-889 AND MET ALL THE REQUIREMENTS OF REO 601R-53-41-889, REV A.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 21,436 hrs · 19,940 cycles

RT FLOOR SUPPORT CRACKED AT UPPER END. REMOVED DAMAGED RT FLOOR SUPPORT AT RBL 27 IAW SRM 51-42-21 AND REPLACED WITH A NEW IAW SRM 51-42-21.

Part: FLOORBEAM — CRACKED (BS 484) · airframe 21,436 hrs · 19,940 cycles

FLOORBEAM FS 484.00, BETWEEN LBL 27 AND LBL 36, IS CRACKED AT UPPER END. REPAIRED FLOORBEAM IAW REO 601R-53-41-059.

Part: STRUCTURE — CORRODED (RT WING) · airframe 21,450 hrs · 19,958 cycles

RIGHT BOOST PUMP CUTOUT LAND SURFACE AND VERTICAL SURFACE HAVE CORROSION INDICATIONS AROUND CIRCUMFERENCE, 50 PERCENT FULL SCREEN HEIGHT. FAILED NDT. REPAIRED IAW REO 601R-57-21-1930.

Part: STRUT — CHAFED (RT MLG) · airframe 21,436 hrs · 19,940 cycles

RT MLG DOOR STRUT ATTACH LUG ON DOOR CHAFED ON AFT SIDE APPROX .020" DEEP. COMPLIED WITH EC/TC REO 601R-52-82-143 IAW REO 601R-52-143.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 20,063 hrs · 18,513 cycles

F/A FLASHLIGHT INOPERATIVE. R & R FLASHLIGHT BATTERIES, IAW AMM 25-61-00. OPS CHECKED GOOD.

Part: FRAME — CRACKED (PAX DOOR) · airframe 19,227 hrs · 17,577 cycles

FWD SIDE OF AIR STAIR DOOR CRACKED. ON FURTHER INVESTIGATION FOUND CRACK AT PAX DOOR FWD EDGE MEMBER TO BE WITH IN LIMITS OF REO 601R-52-11-1360 REV B, FIG 6, ZONE 5. MAX ALLOWABLE CRACK IS 1.250 " CRACK MEASURES .850 MCO DEFECT 382853 CREATED AND M318.

Part: STRUCTURE — CRACKED (PAX DOOR) · airframe 19,227 hrs · 17,577 cycles

AFT SIDE OF AIR STAIR DOOR, CRACKED. PERFORMED OPS CHECK OF PASSENGER DOORS IAW AMM 52-11-04. REPAIRED IAW REO 601R-52-11-279.

Part: STRUCTURE — CRACKED (PAX DOOR) · airframe 19,223 hrs · 17,573 cycles

DURING ROUTINE INSPECTION OF PAX DOOR, FWD DOOR EDGE MEMBER WAS FOUND TO BE CRACKED UNDER TOP FOLDING STEP. (OPEN)

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 19,138 hrs · 17,480 cycles

F/A REPORTS LIGHTS ON MID-CABIN, OVERHEAD EXIT SIGN DO NOT ILLUMINATE TO INDICATE AN INTERCOM-CALL, CREWMEMBER INTERPHONE SYS: INTERPHONE ALERTING FUNCTION: MID CABIN F/A CALL LIGHTS (COCKPIT, LAVATORY, CABIN). R & R MID CABIN EMERGENCY EXIT SIGN. OPS CHECKED OK IAW AMM 33-24-01. REF 33-24-01.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 16,954 hrs · 15,027 cycles

SECOND AFT EMERGENCY CEILING LIGHT IS INOPERATIVE. R & R EMERGENCY CEILING LIGHT BULB IAW AMM 33-51-16. OP'S CHECKED GOOD.

Part: SKIN — CRACKED (ELEVATOR) · airframe 16,616 hrs · 14,645 cycles

JOB 8776835 OPERATION 176/RT ELEV UPPER L/E OF SKIN IS CRACKED AT ES 26.520 IN 2 PLACES. CRACKS ARE APPROX .250 LONG. RESOLVED ON W/O: 177349 TASKCARD: N/R-00570 ) C/W STEPS 1-15 OF ASA EC/TC 601R-55-21-298, BOMBARDIER AEROSPACE REO NR 601R-55-21-298. REQUIRES FIT CHECK, STEP 16. FIT CHECK GOOD AT THIS TIME IAW BOMBARDIER AEROSPACE REO 601R-55-21-288 STEP 16. BOMBARDIER REO 601R-55-21-298 REV 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 PER ASA GMM 3-3 PROCEDURES. PRIOR TO THE A/C BEING RETURNED TO SERVICE. ASA RII C/W: 5300177"

Part: FITTING — CORRODED (BS 610-621) · airframe 16,570 hrs · 14,591 cycles

RBL 27 FITTING BETWEEN FS 610-FS 621 HAS CORROSION AROUND NUTPLATE ON OTBD SIDE THAT IS BEYOND LIMITS OF REO 601R-53-00-005A. REMOVED FITTING IAW SRM 51-42-06 AND SRM 51-42-21. INSTALLED NEW FITTING IAW SRM 51-42-06 AND SRM 51-42-21.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 16,570 hrs · 14,591 cycles

PAX DOOR AFT DRAG ANGLE CRACKED .75" IN LENGTH AT THE DOOR ASSIST MOTOR MOUNT LOCATION. REMOVED DAMAGED DRAG ANGLE AND REPAIRED IAW ASA EC/TC 601R-52-11-513. PAINTED REPAIR IAW EC/TC 601R-52-11-513, STEP 12. COMPLIED WITH EC/TC REO 601R-52-11-513.

Part: SEAT TRACK — CORRODED (BS 610-621) · airframe 16,570 hrs · 14,591 cycles

SEAT RAIL BEAM CAP FITTING AT FS 610-621, LBL 27 HAS CORROSION AROUND NUTPLATE HOLE. (OPEN)

Part: SEAT TRACK — CORRODED (BS 579-610) · airframe 16,570 hrs · 14,591 cycles

SEAT RAIL BEAM CAP AT FS 610-579 HAS CORROSION AT 5EA LOCATIONS. (OPEN)

Part: PLACARD — WORN (CABIN) · airframe 16,570 hrs · 14,591 cycles

PAX DOOR "EXIT", "OPEN" & DIRECTIONAL PLACARDS WORN. (OPEN)

Part: STRUCTURE — CORRODED (BS 559-621) · airframe 16,570 hrs · 14,591 cycles

MINOR CORROSION AROUND VARIOUS NUTPLATE HOLES ON RBL 36 FROM FS 621 TO 559+96. USING NR40 DRILL BIT, REMOVED NUTPLATES FROM THRESHOLD. REMOVED LIGHT CORROSION ON THE SURFACE IAW SRM 41-21-06 3A(1)B(1)(2)(3)(4)(5). REINSTALLED NEW SERVICEABLE NUTPLATES IAW SRM 51-42-15.

Part: FLOOR SUPPORT — CORRODED (BS 574-621) · airframe 16,570 hrs · 14,591 cycles

EVIDENCE OF CORROSION ON FLOOR SUPPORT AROUND NUTPLATES AT RBL 27, FS 574-FS 621. (OPEN)

Part: SEAT TRACK — CORRODED (CARGO BAY) · airframe 16,570 hrs · 14,591 cycles

ALL 7 CARGO SEAT TRACKS HAVE CORROSION. REMOVED DISCREPANT CARGO SEAT TRACKS AND INSTALLED NEW SERVICEABLE SEAT TRACKS IAW SRM 51-41-04. (CLOSED)

Part: BEAM — CORRODED (BS 585) · airframe 16,570 hrs · 14,591 cycles

TRANSVERSE BEAM CAP BETWEEN LBL 9 AND LBL 27 AT APPROX FS 585 HAS MINOR CORROSION. TRANSVERSE BEAM CAP CORROSION UPON INVESTIGATION IS OVER THE LIMIT. REQUIRES REPLACEMENT AND INSTALLATION. REMOVED AND DRILLED NEW BEAM CAP IAW SRM 51-42-06 AND SRM 51-42-21. NEW SERVICEABLE PLATE REQUIRES INSTALL. INSTALLED NEW SERVICEABLE PLATE IAW SRM 51-42-06 & SRM 51-42-21. NEW PLATE WAS DRILLED UP IAW SRM 51-40-11. (CLOSED)

Part: ISOLATOR — CRACKED (BULKHEAD) · airframe 16,570 hrs · 14,591 cycles

BULKHEAD ISOLATOR AT LBL 27 IS CRACKED (UPPER ISOLATOR). (OPEN)

Part: FLOOR SUPPORT — CORRODED (BS 574-621) · airframe 16,570 hrs · 14,591 cycles

EVIDENCE OF MINOR CORROSION AROUND THE NUTPLATE HOLES ON FLOORBEAM CAP LBL 27 FROM FS 574 TO FS 621.00. DURING CLEANING OF CORROSION AROUND NUTPLATE HOLES ON FLOORBEAM CAP LBL 27 FROM FS 574 TO FS 621 FOUND CORROSION TO BE BEYOND. REPAIRABLE LIMITS REF 8776831, OPS 367 AND 368. (CLOSED)

Part: BULKHEAD — CRACKED (BS 559) · airframe 16,570 hrs · 14,591 cycles

FOUND FS 559, RT BULKHEAD WEB HAS INDICATION NOTED APPROX .2" IN LENGTH 50 PERCENT FSH AT WL 54.10 OTBD OF RBL 9.0. FAILED NDT INSP. REPAIRED FS 559 PRESSURE BULKHEAD WEB AND CAP ANGLES FROM LBL 27 TO RBL 27 IAW REO 601R-53-41-260 REV E, STEPS 1 THROUGH 4.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 16,405 hrs · 14,400 cycles

NR3 CEILING EMERGENCY LIGHT INOP. RELAMPED NR 3 CABIN CEILING EMERGENCY LIGHT. OPS CHECK GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 15,962 hrs · 13,867 cycles

RT FUSELAGE EXTERIOR OVERWING NR 3 EMERGENCY LIGHT INOP. RELAMPED RT SIDE EXTERIOR NR 3 EMERGENCY EXIT LIGHT IAW AMM 33-51-21 OPS CHECK GOOD. RELAMPED RT SIDE EXTERIOR NR 3 EMERGENCY EXIT LIGHT IAW AMM 33-51-21 OPS CHECK GOOD.

Part: BULB — INOPERATIVE (EMEGENCY LIGHT) · airframe 15,304 hrs · 13,094 cycles

RT NR 3 EXTERIOR EMERGENCY LIGHT INOP. R & R LIGHT BULB. OPS CHECK GOOD AT THIS TIME. WORK PERFORMED IAW AMM 33-51-21.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,165 hrs · 12,947 cycles

ZONES NR 3 EMERGENCY LIGHTS INOP.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 15,165 hrs · 12,947 cycles

ZONE NR 4 EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,524 hrs · 12,253 cycles

LEFT FWD SIDE EMERGENCY LIGHT INOP.

Part: DETECTION SYS — DEFECTIVE (TE FLAP) · airframe 14,193 hrs · 11,929 cycles

FLAPS FAIL AT 0 WHILE CLIMBING OUT AT FLT LEVEL 230, EMERGENCY DECLARED. SKEW DETECTION SYSTEM.

Part: FLAP — MALFUNCTIONED (WING) · airframe 13,619 hrs · 11,372 cycles

CLIMBING THROUGH 16,000 FT AT 290 KNOTS RECEIVED HIGH SPEED AURAL WARNING CLACKER FOLLOWED IMMEDIATELY BY FLAPS FAIL AT 0 DEGREES. RAN QRH, LANDED AT 100 FPM WITH LANDING WEIGHT OF 37,000 LBS. EMERGENCY DECLARED, EN ROUTE TO GSP. A/C DIVERTED TO ATL DUE TO MTC.

Part: WARNING SYSTEM — ACTIVATED (TE FLAP) · airframe 13,636 hrs · 11,387 cycles

AT 17000 FT AND 280 KNOTS RECEIVED OVERSPEED CLACKER AURAL WARNING FOLLOWED IMMEDIATELY BY FLAPS FAIL CAUTION MSG AT DETENT O, AC WAS WELL BELOW OVERSPEED CONDITION. EMERGENCY EQUIPMENT REQUESTED AS A SAFETY PRECAUTION.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 13,603 hrs · 11,359 cycles

FLAPS FAIL CAUTION MSG ILLUM IN FLT AT 0 AT 17000. EMERGENCY DECLARED. A/C RETURNED TO ATL AFTER T/O. FLT 5399 DEL 156 MINS.

Part: DETECTION SYS — FAILED (TE FLAP) · airframe 13,546 hrs · 11,304 cycles

FLT 5609, FLAPS FAIL AT 0 WHEN SELECTED TO 8. EMERGENCY DECLARED. SKEW DETECTION SYSTEM. INSTALLED SKEW DETECTION PANEL IAW AMM 27-51-15 OPS CHECK GOOD DEFER CLEARED PLACARD REMOVED.

Part: BATTERY — DISCHARGED (CABIN) · airframe 13,516 hrs · 11,273 cycles

NR 3 EMERGENCY LIGHTING BATTERY HAS NO CHARGE.

Part: SIGN — INOPERATIVE (CABIN) · airframe 12,684 hrs · 10,516 cycles

EMERGENCY EXIT SIGNS ON WARDROBE GALLEY TRIM PANEL AND SERVICE DOOR TRIM PANEL FAILED OPERATION TEST.

Part: FLOOR SUPPORT — CRACKED (BS 484) · airframe 12,684 hrs · 10,516 cycles

RT FS 484 FLOOR SUPPORT INTERCOSTAL ANGLE CRACKED RBL 27.

Part: BEAM — CRACKED (BS 559) · airframe 12,684 hrs · 10,516 cycles

VERTICAL BEAM AT BS 559 RBL 9 CRACKED .05. OPEN

Part: LIGHT — INOPERATIVE (CABIN) · airframe 9,628 hrs · 8,009 cycles

FLOOR EMERGENCY LIGHTS FROM ROW 1CD TO ROW 6CD INOP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 9,003 hrs · 7,561 cycles

RIGHT OVERWING EMERGENCY EXIT LIGHT INOP.

Part: WARNING LIGHT — ILLUMINATED (THRUST REVERSER) · airframe 8,759 hrs · 7,380 cycles

RT REV UNLOCK MSG IN FLT. EN ROUTE TO ATL, A/C DIVERTED TO TYS DUE TO MTC. EMERGENCY DECLARED. REPLACED RT ENG T/R PDU. OPS CHECK GOOD. DML CLEARED PLACARD REMOVED. 3 MAN HRS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 8,556 hrs · 7,226 cycles

FLOOR LEVEL EMERGENCY LIGHT STRIP ROW 2 TO 5 INOP. FLTS 4229,4915 CX.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHT) · airframe 8,282 hrs · 7,019 cycles

SEAT 8AB LOWER EMERGENCY EXIT SIGN IS INOP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 8,282 hrs · 7,019 cycles

CABIN FWD EMERGENCY TRACK LIGHTING IS INOP.

Part: STRINGER CLIP — CRACKED (BS 484) · airframe 7,995 hrs · 6,782 cycles

LEFT FUSELAGE STA 484 O/B CLIP CRACKED (O/B OF LBL 27).

Part: FLOOR SUPPORT — CRACKED (BS 621) · airframe 7,995 hrs · 6,782 cycles

FS 621.00 FLOOR SUPPORT ANGLE IS CRACKED RT SIDE AT AFT PRESSURE BULKHEAD (MARKED) PER MTC. REPAIRED IAW REO 601R-53-61-117. (CLOSED)

Part: FLOOR SUPPORT — CRACKED (BS 621) · airframe 7,995 hrs · 6,782 cycles

FS 621.00 FLOOR SUPPORT ANGLE IS CRACKED LT SIDE AT AFT PRESSURE BULKHEAD (MARKED) PER MTC. REPAIRED IAW REO 601R-53-61-117. (CLOSED)

Part: ATTACH FITTING — CRACKED (BS 625) · airframe 7,995 hrs · 6,782 cycles

RIGHT FS 625 CLIP IS CRACKED. REMOVED AND REPLACED RT FS 625.00 INTERCOSTAL PER SRM 51-42-21. (CLOSED)

Part: ATTACH FITTING — CRACKED (BS 625) · airframe 7,995 hrs · 6,782 cycles

LEFT FS 625 CLIP IS CRACKED. REMOVED AND REPLACED LT FS 625.00 INTERCOSTAL PER SRM 51-42-21. (CLOSED)

Part: BEAM — CRACKED (FUSELAGE) · airframe 7,995 hrs · 6,782 cycles

BOX BEAM LOWER WEB CRACKED AT FWD INBOARD PNL OPENING COMING FROM N/P RIVET AT ACCESS PNL 312DZ. FINISHED INSTALLING FASTNERS IN 366 WEB REPAIR PER REO 601R-53-61-366. (CLOSED)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 7,500 hrs · 6,394 cycles

RT MID OVERWING EMERGENCY LIGHT INOP.

Part: OIL SYSTEM — MALFUNCTIONED (NR 1 ENGINE) · airframe 6,945 hrs · 5,941 cycles

JUST AFTER T/O NR 1 ENGINE OIL PRESSURE BEGAN RAPIDLY FLUCTUATING. RECEIVED TRIPLE CHIME AND EICAS MSG (LT ENG OIL PRESS) 3 TIMES. FLUCTUATIONS WERE BETWEEN 25 AND 44 PSI. RAN QRH FOR OIL PRESSURE LEFT NR1 ENGINE AT IDLE AND LANDED. A/C RETURNED TO ATL AFTER T/O. FLTS 4310 (X2) CX, AN EMERGENCY WAS DECLARED.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT)

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

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT)

DURING A GROUND INSPECTION, THE AFT EMERGENCY FLOOR TRACK LIGHT STRIP WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR4 INVERTER. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: CONNECTOR — DISCONNECTED (CABIN)

DURING A GROUND INSPECTION, THE CENTER AISLE EMERGENCY LIGHT STRIP WAS FOUND TO BE DISCONNECTED AT THE AFT POSITION. MAINTENANCE RECONNECTED THE CENTER AISLE EMERGENCY LIGHT STRIP AT THE AFT POSITION. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)