N686BR

Part: BULKHEAD WEB — CHAFED (BS 621) · airframe 30,849 hrs · 30,288 cycles

FOUND REAR PRESSURE BULKHEAD WEB HAS 5 CHAFED AREA WL 103, LBL 27.50, LBL 18.00, RBL 18.00, RBL 27.50 AND RBL 36.20 .200" LONG BY .200" WIDE .003 DEEP. REPAIRED CHAFED AREAS OF REAR PRESSURE BULKHEAD WEB, IAW BOMBARDIER REO 601R-53-61-2155, REV A.

Part: FLOOR SUPPORT — CORRODED (BS 409-559) · airframe 30,849 hrs · 30,288 cycles

FLOOR BEAM BETWEEN FS 409+119 AND FS 559 IS CORRODED AT NUMEROUS LOCATIONS AT RBL 9. CONTINUATION FROM OP NR 106 FLOORBEAM BETWEEN FS 409+115 AND FS 559 IS CORRODED AT NUMEROUS LOCATIONS AT RBL 9. REPAIRED FLOOR BEAM BETWEEN FS 409+118 TO FS 559 (9) RBL 9, IAW MHIRJ REO 601R-53-41-27.

Part: ATTACH ANGLE — CORRODED (BS 280 FLOORBEAM) · airframe 30,849 hrs · 30,288 cycles

FS 280 FLOOR BEAM ATTACH CLIP AT LBL 9 OUTBOARD POSITION IS CRACKED. REMOVED AND REPLACED FLOOR BEAM CLIP P/N 601R31113-57, IAW CRJ 200 SRM51-40-11. OPERATIONS TEST GOOD.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 30,849 hrs · 30,288 cycles

FS 280 CROSSBEAM IS CRACKED IN RADIUS OF LOWER FLANGE APPROX 2" LONG AT RBL 9. REMOVED & REPAIRED FS 280 CROSSBEAM, IAW BOMBARDIER REO 601R-53-11-926 REV-B, 2006/05/10.

Part: SEAT TRACK — CORRODED (BS 394-409) · airframe 30,849 hrs · 30,288 cycles

FLOOR SEAT TRACK SEGMENT BETWEEN FS 394 AND 409+128 AT LBL 9 IS CORRODED. REMOVED AND REPLACED CORRODED SEAT TRACK BETWEEN FS 394 AND 409+128 AT LBL 9, IAW CRJ 200 AMM 53-01-11-000/400-802 AND SRM 51-40-11.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 30,849 hrs · 30,288 cycles

CARGO FLOOR TRACK IS CORRODED (QTY 2) RBL 9 FS 559+86 AND RBL 29 FS 559+80. REPLACED SEAT TRACK SEGMENTS IN AFT CARGO AREA AT RBL 9.0 FS 559+86 AND RBL 29 FS 559+80, IAW CRJ 200 AMM 53-01-11-400-802, NO DEFECTS NOTED.

Part: SUPPORT — CORRODED (BS 621) · airframe 30,849 hrs · 30,288 cycles

CARGO BLOWOUT DIAPHRAGM FWD OF FS 621 IS DISPLACED. REMOVED AND REPLACED CARGO BLOWOUT DIAPHRAGM FWD OF FS 621 BULKHEAD, IAW CRJ 200 AMM 53-61-17-000-801 AND SRM 51-41-02.

Part: DOUBLER — CORRODED (BS 310) · airframe 30,849 hrs · 30,288 cycles

GALLEY FLOOR MOUNT DOUBLER AFT OF FS 310 AT RBL 9 IS CORRODED. REMOVED AND REPLACED GALLEY FLOOR MOUNT DOUBLER, IAW CRJ 200 SRM 51-42-06 & 51-40-11.

Part: FLOORBEAM — CRACKED (BS 484) · airframe 30,849 hrs · 30,288 cycles

FS 484 ANGLES CRACKED AT RBL 27 AND RBL 36. REMOVED & REPLACED RBL 27-36 CLIPS FS 484, IAW CRJ 200 SRM 51-42-21 & REO 601R-53-41-059 REV C2020/3/11.

Part: DIAPHRAGM — CORRODED (BS 621) · airframe 30,849 hrs · 30,288 cycles

CARGO BLOWOUT DIAPHRAGM FWD OF FS 621 IS DISPLACED. REMOVED AND REPLACED CARGO BLOWOUT DIAPHRAGM FWD OF FS 621 BULKHEAD, IAW CRJ 200 AMM 53-61-17-000-801 AND SRM 51-41-02.

Part: FLOORBEAM — CRACKED (BS 484) · airframe 30,849 hrs · 30,288 cycles

FS 484 ANGLES CRACKED AT RBL 27 AND RBL 36. REMOVED & REPLACED RBL 27-36 CLIPS FS 484, IAW CRJ 200 SRM 51-42-21 & REO 601R-53-41-059 REV C2020/3/11.

Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 30,849 hrs · 30,288 cycles

FOUND REAR PRESSURE BULKHEAD WEB HAS MULTIPLE INDICATIONS NOTED AT LBL 36.20 WL 78.0 1.0 INCH LONG 60% FSH FAILED NDT INSPECTION. REPAIRED DAMAGED AREA OF FS 621.00 REAR PRESSURE BULKHEAD WEB, IAW REO 601R-53-61-1285 REV E DATED 2016-10-31.

Part: STIFFENER — CRACKED (BS 621) · airframe 30,849 hrs · 30,288 cycles

WHILE PERFORMING A REPAIR TO FS 621 BULKHEAD AT LBL 36.20 WL 79.0 FOUND STIFFNER CRACKED. LOCATED, DRILLED, & INSTALLED NEW STIFFNER P/N 601R36008-51, IAW CRJ 200 SRM 51-40-11-00-51-42-06-00.

Part: SEAT TRACK — CORRODED (BS 364-394) · airframe 30,849 hrs · 30,288 cycles

FLOOR SEAT TRACK SEGMENT BETWEEN FS 364 AND FS 394 AT RBL 9 IS CORRODED. REMOVED AND REPLACED FLOOR SEAT TRACK SEGMENT BETWEEN FS 364 AND FS 394 AT RBL 9, IAW CRJ200 AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 394-409) · airframe 30,849 hrs · 30,288 cycles

FLOOR SEAT TRACK SEGMENT BETWEEN FS 394 AND FS 409+128 AT RBL 9 IS CORRODED. REMOVED AND REPLACED FLOOR SEAT FS 394 & FS 409 OF RBL 9, IAW CRJ 200 AMM 53-01-11-400-802.

Part: CARGO TRACK — CORRODED (BS 574) · airframe 30,849 hrs · 30,288 cycles

CARGO FLOOR TRACK IS CORRODED FS 574, LBL 9.0. REMOVED AND REPLACED FLOOR TRACK AT LBL 9 FS 574 P/N 601R38779-5, IAW CRJ200 AMM 53-01-11-400-802. "

Part: SEAT TRACK — CORRODED (BS 364-394) · airframe 30,849 hrs · 30,288 cycles

FLOOR SEAT TRACK SEGMENT BETWEEN FS 364 AND FS 394 AT LBL 9 IS CORRODED. REMOVED AND REPLACED FLOOR SEAT TRACK SEGMENT BETWEEN FS 364 AND FS 394 AT LBL 9, IAW CRJ 200 AMM 53-01-11-400-802.

Part: ANGLE — CRACKED (BS 621) · airframe 30,849 hrs · 30,288 cycles

LT AND RT OBLIQUE ANGLES ARE CRACKED AT STRINGER 14L AFT SIDE OF FS 621 BULKHEAD. REMOVED AND REPLACED LT & RT OBLIQUE ANGLES AFT SIDE OF FS 621 BULKHEAD AT STRINGERS 14L & 16R, IAW CRJ 200 SRM 51-82-21.

Part: ANGLE — CRACKED (BS 621) · airframe 30,849 hrs · 30,288 cycles

AFT CARGO SURROUND UPPER BEAM MEMBER LOWER ANGLE THAT ATTACHES TO THE FS 621 BULKHEAD IS CRACKED. REMOVED AND INSTALLED NEW DRILLED UP ANGLE IN CARGO SURROUND UPPER BEAM, IAW BOMBARDIER CRJ 200 SRM 51-42-21.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 28,736 hrs · 28,025 cycles

LBL 27 OB FLOOR LANDING HAS CORROSION SPOTS BETWEEN FS 559+96 THRU FS 574. REPAIRED DAMAGE PER REO 601R-53-00-027.

Part: WEB — CRACKED (FUSELAGE) · airframe 28,736 hrs · 28,025 cycles

FWD. ACCY. COMPT. FLOOR WEB HAS A CRACK OUTOARD OF HYD. SYS-2 ACCUMULATOR GAUGE. PERFORMED DOUBLER REPAIR ON FWD ACCY, COMP. FLOOR WEB IAW REO 601R-53-11-081. OP'S AND LEAK CHECK GOOD PER AMM 32-43-17-400-801 STEP 3B.

Part: RISER — CORRODED (PAX DOOR) · airframe 28,736 hrs · 28,025 cycles

WHILE WORKING MID STEP CORROSION FOUND AFT RISER ATTACH FLANGE AT NUT PLATE CORRODED OFF. REPAIRED AFT RISER ATTACH FLANGE IAW EA 252-08690 REV A OPS CK OF PAX DOOR COUNTER BALANCE GOOD IAW AMM 52-11-17-710-802.

Part: ANGLE — CRACKED (COCKPIT) · airframe 28,736 hrs · 28,025 cycles

FLT DECK FWD WINDSHIELD CENTER POST LT LOWER ANGLE FITTING IS CRACKED. REMOVED CRACKED FITTING AND INSTALLED NEW FITTING IAW SRM 51-42-21.

Part: ANGLE — CRACKED (COCKPIT) · airframe 28,736 hrs · 28,025 cycles

FLT DECK FWD WINDSHIELD CENTER POST R/H LOWER ANGLE FITTING IS CRACKED. REMOVED CRACKED FITTING AND INSTALLED NEW FITTING IAW SRM 51-42-21.

Part: CHANNEL — CRACKED · airframe 28,736 hrs · 28,025 cycles

PNL 422DB SEAL CHANNEL IS CRACKED. REMOVED/REPLACED CRACKED SEAL CHANNEL WITH NEW PNL 422DB IAW SRM 51-42-06.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 28,736 hrs · 28,025 cycles

SEAT TRACK ON TOP OF LBL 9 HAS CORROSION BETWEEN FS 559+80 AND FS 559+96, IN THE CARGO BAY. REMOVED/REPLACED WITH NEW SEAT TRACK IAW AMM 53-00-49.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 28,736 hrs · 28,025 cycles

SEAT TRACK ON TOP OF LBL 9 HAS CORROSION BETWEEN FS 559+112 AND FS 574, IN THE CARGO BAY. REMOVED/REPLACED WITH NEW SEAT TRACK IAW AMM 53-00-49.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 28,736 hrs · 28,025 cycles

SEAT TRACK ON TOP OF RBL 9 HAS CORROSION BETWEEN FS 559+112 AND FS 574, IN THE CARGO BAY. REMOVED/REPLACED WITH NEW SEAT TRACK IAW AMM 53-00-49.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 28,736 hrs · 28,025 cycles

SEAT TRACK ON TOP OF LBL 9 HAS CORROSION JUST FWD OF FS 621, IN THE CARGO BAY. REMOVED/REPLACED WITH NEW SEAT TRACK IAW AMM 53-00-49.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 28,736 hrs · 28,025 cycles

SEAT TRACK ON TOP OF LBL 27 HAS CORROSION BETWEEN FS 559+80 AND FS 559+96, IN THE CARGO BAY. REMOVED/REPLACED WITH NEW SEAT TRACK IAW AMM 53-00-49.

Part: DOOR SILL — CRACKED (FUSELAGE) · airframe 28,736 hrs · 28,025 cycles

WHILE WORKING AFT CARGO LT FLOOR SILL LBL 36 FOUND CRACK IN FLOOR SILL FS 589. REPAIRED AFT CARGO AT FLOOR SILL LBL 36 & FS 589 IAW REO 601R-53-61-433.

Part: BULKHEAD WEB — DAMAGED (BS 621) · airframe 28,453 hrs · 27,713 cycles

DURING COMPLIANCE OF SDI RPB FWD FACE (TC 53-280-607) NOTED RPB SUSTAINED 5 LINER HARDWARE STRIKES @ LBL27.5, 18,+ RBL 18,27.5,36.2 ALL IN A LINE HORIZONTAL. APPROX 29.75". ALSO NOTED 5 RIVIT HEAD STRIKES @LBL 36.2,27.5,18 + RBL 27.5, 36.2. ALL IN A LINE HORIZONTAL APPROX 13" UP BLENDED OUT SURFACE DAMAGE ON AFT BULK HEAD WEB IAW BOMBARDIER REV #A 601R-53-61-2155. REPLACED DAMAGE RIVITS IAW CRJ 200 SRM 51-42-06. SEE CONTINUATION CARD #114971 FOR DETAILS

Part: OXYGEN MASK — UNSECURE (COCKPIT) · airframe 27,777 hrs · 27,008 cycles

WHEN F/O TESTED O2 MASK, VALVE STUCK AND QTY DROPPED TO 1540. RE-SECURED F/O O2 MASK IAW AMM 35-11-15. SERVICED CREW O2 IAW AMM 12-16-35. OPS CHECKS GOOD.

Part: OXYGEN MASK — LEAKING (FIRST OFFICER'S) · airframe 27,111 hrs · 26,294 cycles

FIRST OFFICER`S SIDE OXYGEN MASK WAS LEAKING WHEN IN EMERGENCY MODE IT IS A FASTER LEAK. REMOVED AND REPLACED FIRST OFFICER`S OXYGEN MASK IAW AMM 35-11-12. ALL CHECKED GOOD IAW AMM 35-10-00, AND AMM 23-51-00. NO LEAKS NOTED. ACFT OK FOR SERVICE.

Part: CONTROL HANDLE — MALFUNCTIONED (MLG) · airframe 26,778 hrs · 25,945 cycles

AFTER TAKE OFF, RECIEVED AN ANTI-SKID INBD & PARK BRAKE SOV MESSAGES, LANDING GEAR HANDLE WAS IN THE UP POSITION BUT GEAR NEVER CAME UP. THREE GREEN INDICATIONS FROM GEAR. FOLLOWED QRH. MESSAGE WENT AWAY. ON GEAR HANDLE GOING IN THE DOWN POSITION. NO GEAR DISAGREE MESSAGE RECEIVED. R & R THE LANDING CONTROL HANDLE IAW AMM 32-31-01. OPS TESTED NORMAL.

Part: SMOKE DETECTOR — INOPERATIVE (LAVATORY) · airframe 25,862 hrs · 24,936 cycles

LAVATORY SMOKE DETECTOR INOPERATIVE. REMOVED AND REPLACED LAVATORY SMOKE DETECTOR IAW AMM 26-16-01. OPS CHECKED GOOD.

Part: CONTROL HANDLE — INOPERATIVE (MLG) · airframe 25,587 hrs · 24,637 cycles

AFTER TAKEOFF, LANDING GEAR FAILED TO RETRACT WHEN SELECTED UP. ANTI-SKID INBOARD AND PARKING BRAKE SOV CAUTION MESSAGES, WHILE THE GEAR HANDLE WAS UP. GEAR DISAGREE MASTER WARNING DID NOT GO OFF. R & R LANDING GEAR CONTROL HANDLE IAW AMM 32-31-01. OPS CHECKED GOOD.

Part: LEG ASSY — BENT (PAX DOOR) · airframe 25,369 hrs · 24,409 cycles

DOOR ASSIST FOR MAIN DOOR DOES NOT WORK, ALSO DOOR WILL NOT OPEN FROM INSIDE. OPERATED DOOR ASSIST IAW AMM 52-11-08 AND FOUND TO OPERATE NORMALLY. INSPECTED PAX DOOR AND FOUND SUPPORT LEG ASSY BENT AND STRIKES FUSELAGE WHEN DOOR RETRACTED. R&R SUPPORT LEG ASSY IAW AMM 52-11-13. DOOR LOCKS AND UNLOCKS AND OPENS NORMALLY AT THIS TIME. ACFT OK FOR SERVICE AT THIS TIME. P/N ON, OFF- 601R317092-1, NO S/N'S. P/N ON/OFF-NAS322C11-0151, NO S/N'S.

Part: STOWAGE BOX — INOPERATIVE (OXYGEN MASK) · airframe 25,285 hrs · 24,325 cycles

OBSERVERS OXYGEN MASK DOES NOT TEST. REPLACED THE OXYGEN MASK STOWAGE BOX IAW AMM 35-11-15, OPS CHECKED GOOD.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 25,277 hrs · 24,316 cycles

LT LOWER EXIT LIGHT AT ESCAPE HATCH IS INOP. R/R EXIT LIGHT PN 6020-6 IAW 33-51-00, DID NOT FIX. R&R EMERGENCY LIGHT INVERTER IAW AMM 33-51-07, OPS CK GOOD.

Part: EXTINGUISHER — UNSERVICEABLE · airframe 25,277 hrs · 24,316 cycles

HALON FIRE EXTINGUISHER MISSING DISCHARGE HOSE. REMOVED UNSERVICEABLE HALON FIRE EXTINGUISHER AND INSTALLED SERVICEABLE HALON FIRE EXTINGUISHER IAW JOB CARD 26-900-700 P/N ON/OFF: 100-9750 S/N: F002305C S/N OFF:000671C

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,863 hrs · 27,862 cycles

LEFT OVER WING EMERGENCY EXIT INTERIOR LOWER LIGHT INOP. REMOVED AND REPLACED LEFT OVER WING EMERGENCY EXIT INTERIOR LOWER LIGHT IAW AMM 33-51-10.

Part: SEAT TRACK — CORRODED (BS 499-559) · airframe 24,643 hrs · 23,569 cycles

RIGHT SIDE SEAT TRACK CORRODED BS 499 - 559+80. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11-000-802 AND 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 409-449) · airframe 24,643 hrs · 23,569 cycles

RIGHT SEAT TRACK CORRODED BS 409.00+112 - 449.00+85. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11-000-802, AND AMM 53-01-11-400-802.

Part: CARGO TRACK — CORRODED (BS 583) · airframe 24,643 hrs · 23,569 cycles

CARGO TRACK LBL 9, BS 583 CORRODED. REMOVED AND REPLACED IAW SRM 51-41-04.

Part: SEAT TRACK — CORRODED (BS 449-499) · airframe 24,643 hrs · 23,569 cycles

RIGHT SIDE SEAT TRACK CORRODED BS 449.00+85 - 499. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11-000-802, AND AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 409-559) · airframe 24,643 hrs · 23,569 cycles

LEFT SEAT TRACK CORRODED LBL 9, BS 409+128 - 559+32. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11-000-802, AND AMM 53-01-11-400-802.

Part: ANGLE — CORRODED (DOOR SILL) · airframe 24,643 hrs · 23,569 cycles

PAX DOOR LOWER SILL ANGLE CORRODED AT SEVERAL AREAS. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00. REMOVED AND REPLACED THE ANGLE IAW SRM 51-42-06, 51-41-13 AND 51-42-21, SRM 51-40-11, AND 51-42-13. MAJOR REPAIR.

Part: CARGO TRACK — CORRODED (BS 621) · airframe 24,643 hrs · 23,569 cycles

CARGO TRACK FITTING AT LBL 27, BS 621 IS CORRODED. REMOVED AND REPLACED THE CARGO TRACK IAW SRM 51-42-21, SRM 51-40-11, SRM 51-42-22, AND REO 601R-53-61-3778. MAJOR REPAIR.

Part: FLOOR SUPPORT — CORRODED (BS 409) · airframe 24,643 hrs · 23,569 cycles

RBL 9 FLOOR SUPPORT CAP 409+6 - 409+118 CORRODED.

Part: ANGLE — CORRODED · airframe 24,643 hrs · 23,569 cycles

SERVICE DOOR LOWER SILL ANGLE CORRODED FWD AND AFT SECTIONS. REMOVED AND REPLACED IAW SRM 57-42-71, SRM 51-40-11, SRM 51-42-21, AND DWG 601R38-303. MAJOR REPAIR.

Part: CARGO TRACK — CORRODED (BS 559) · airframe 24,643 hrs · 23,569 cycles

CARGO TRACK LBL 27 BS 559+78 - 559+99. REMOVED AND REPLACED THE CARGO TRACK IAW AMM 53-00-49-000-801, AND AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 24,643 hrs · 23,569 cycles

LBL 9 SEAT TRACK BS 559+85 - 559+94 CORRODED AT SEVERAL AREAS. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801, AND AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 499-548) · airframe 24,643 hrs · 23,569 cycles

LEFT SEAT TRACK CORRODED BS 499 - 548. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11-000-802, AND AMM 53-01-11-400-802.

Part: PLATE — CORRODED (BS 574-621) · airframe 24,643 hrs · 23,569 cycles

CARGO DOOR LOWER SILL PLATE HAS CORROSION BETWEEN BS 574 - 621. BLENDED AREAS ARE WITHIN ALLOWABLE LIMITS IAW REO 601R-53-00-526.

Part: CARGO TRACK — CORRODED (BS 559) · airframe 24,643 hrs · 23,569 cycles

CARGO TRACK RBL 27 BS 559+47 - 559+39 CORRODED. REMOVED AND REPLACED THE CARGO TRACK IAW AMM 53-00-49-000-801, AND AMM 53-00-49-400-801.

Part: CARGO TRACK — CORRODED (BS 591) · airframe 24,643 hrs · 23,569 cycles

CARGO TRACK LBL 9, BS 591 CORRODED. REMOVED AND REPLACED IAW SRM 51-41-04.

Part: SEAT TRACK — CORRODED (BS 449-499) · airframe 24,643 hrs · 23,569 cycles

LEFT SEAT TRACK CORRODED BS 449.85 - 499. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11-000-802, AND AMM 53-01-11-400-802.

Part: FLOOR SUPPORT — CORRODED (BS 598-618) · airframe 24,643 hrs · 23,569 cycles

FLOOR SUPPORT BS 598.5 - 618.5 CORRODED. BLENDED CORROSION IAW SRM 51-21-06. FOUND TO BE OUT OF LIMITS IAW REO 601R-53-00-005. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-11, ECTC REO 601R-53-61-3778 REV A, SRM 601R-53-61-3778, AND SRM 51-42-21.

Part: SEAT TRACK — CORRODED (BS 409) · airframe 24,643 hrs · 23,569 cycles

RT SIDE SEAT TRACK CORRODED BS 409+16 - 409+112. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11-000-802, AND AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 24,643 hrs · 23,569 cycles

CARGO TRACK LBL 27, BS 559+120 CORRODED. REMOVED AND REPLACED IAW SRM 51-41-04.

Part: INTERCOSTAL — CRACKED (BS 621) · airframe 24,643 hrs · 23,569 cycles

BS 621 INTERCOSTAL IS CRACKED. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-42-21, 51-42-06, AND 51-42-21, 51-42-06.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 24,643 hrs · 23,569 cycles

LBL 9 SEAT TRACK BS 559+85 - 559+94 CORRODED SEVERAL AREAS. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801, AND AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 339-409) · airframe 24,643 hrs · 23,569 cycles

LBL 9 SEAT TRACK BS 339.5 - 409+126 CORRODED SEVERAL AREAS. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11-000-802 AND 53-01-11-400-802.

Part: FLOORBEAM — CORRODED (BS 349) · airframe 24,643 hrs · 23,569 cycles

CABIN FLOORBEAM BS 349 CORRODED RBL 42. REPAIRED IAW REO 601R-53-21-27-35.

Part: SEAT TRACK — CORRODED (BS 409-449) · airframe 24,643 hrs · 23,569 cycles

LT SIDE SEAT TRACK CORRODED BS 409+112 - 449.85. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11-00-802, AND AMM 53-01-11-400-802.

Part: FLOOR SUPPORT — CORRODED (BS 409) · airframe 24,643 hrs · 23,569 cycles

LBL 9 FLOOR SUPPORT CAP 409+6 - 409+118. INSTALLED REPAIR IAW REO 601R-53-31-877.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 24,643 hrs · 23,569 cycles

RBL 9 SEAT TRACK BS 559+4 - 559+85 CORRODED SEVERAL AREAS. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11-000-802 AND 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 544-559) · airframe 24,643 hrs · 23,569 cycles

RIGHT SIDE SEAT TRACK CORRODED BS 544 - 559+80. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11-000-802 AND AMM 53-01-11-400-802.

Part: INTERCOSTAL — CRACKED (BS 621) · airframe 24,643 hrs · 23,569 cycles

BS 621 INTERCOSTAL IS CRACKED. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-42-21, 51-42-06.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 24,643 hrs · 23,569 cycles

RBL 9 SEAT TRACK BS 559+85 - 559+94 CORRODED AT SEVERAL AREAS. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801, AND AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 24,643 hrs · 23,569 cycles

LBL 9 SEAT TRACK BS 559+4 - 559+81 CORRODED AT SEVERAL AREAS. REMEOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11-000-802, AND AMM 53-01-11-400-802.

Part: FRAME — CORRODED (BS 605) · airframe 24,643 hrs · 23,569 cycles

FRAME BS 605 FWD & AFT FACE HAS CORROSION BETWEEN STRINGERS 25R-19L. REMOVED CORROSION IAW SRM 51-21-06 AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00 FIG 101 & 102. REMOVED AND REPLACED THE FRAME IAW SRM 51-42-06, 51-42-21, AND DRAWING 601R 36026.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 24,643 hrs · 23,569 cycles

CARGO TRACK AT LBL 27 BS 559+103 CORRODED. REMOVED AND REPLACED IAW SRM 51-41-04.

Part: INTERCOSTAL — CRACKED (BS 621) · airframe 24,643 hrs · 23,569 cycles

BS 621 INTERCOSTAL IS CRACKED. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-42-21, AND 51-42-06.

Part: SEAT TRACK — CORRODED (BS 339-409) · airframe 24,643 hrs · 23,569 cycles

RBL 9 SEAT TRACK BS 339.5-409+126 CORRODED SEVERAL AREAS. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11-000-802 AND 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 364-409) · airframe 24,643 hrs · 23,569 cycles

LT SIDE SEAT TRACK CORRODED BS 364 - 409.00+16. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11-802, AND 53-01-11-400-802.

Part: FLOOR SUPPORT — CORRODED (BS 349-364) · airframe 24,643 hrs · 23,569 cycles

RIGHT CABIN FLOOR SUPPORT CORROODED BS 349 - 364. FOUND TO BE OUT OF LIMITS IAW GREO 601R-53-00-530. REPAIRED THE FLOOR SUPPORT IAW REO 601R-53-21-326 REV A.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 24,643 hrs · 23,569 cycles

CARGO TRACK AT LBL 27, BS 559+112 CORRODED. REMOVED AND REPLACED IAW SRM 51-47-04.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 24,643 hrs · 23,569 cycles

RBL 9 SEAT TRACK BS 559+110 - 559+122 CORRODED SEVERAL AREAS. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801, AND AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 409-559) · airframe 24,643 hrs · 23,569 cycles

RIGHT SEAT TRACK CORRODED RBL 9, BS 409+128 - 559+32. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11-000-802, AND AMM 53-01-11-400-802.

Part: CARGO TRACK — CORRODED (BS 612-616) · airframe 24,643 hrs · 23,569 cycles

CARGO TRACK SEGMENT LBL 9 BS 612-616 CORRODED. REMOVED AND REPLACED THE CARGO TRACK IAW AMM 53-01-49-000-801, AND AMM 53-01-11-400-802.

Part: PLATE — CORRODED (BS 310-319) · airframe 24,643 hrs · 23,569 cycles

RT FWD FLOOR PLATE BETWEEN BS 310 - 319.70 CORRODED. REMOVED AND REPLACED THE PLATE IAW SRM 51-42-06 AND 51-42-15.

Part: SEAT TRACK — CORRODED (BS 364-399) · airframe 24,643 hrs · 23,569 cycles

LBL 9 SEAT TRACK BS 364-399.5 CORRODED AT SEVERAL AREAS. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11-000-802 AND 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 364-399) · airframe 24,643 hrs · 23,569 cycles

RBL 9 SEAT TRACK BS 364-399.5 CORRODED AT SEVERAL AREAS. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11-000-802, AND AMM 53-01-11-400-802.

Part: BULKHEAD — CRACKED (BS 621) · airframe 24,643 hrs · 23,569 cycles

REAR PRESSURE BULKHEAD FORWARD FACE IS CRACKED ABOVE CARGO DOOR AFT TRACK AREA. REPAIRED IAW REO 601R-53-61-5772.

Part: DOOR SILL — CRACKED (CARGO DOORWAY) · airframe 24,643 hrs · 23,569 cycles

CARGO DOOR LOWER SILL PLATE CRACKED AT BS 605. REPAIRED IAW REO 601R-61-433 AND REO 601R-53-61-433 REV C.

Part: HINGE — GOUGED (PAX DOOR) · airframe 24,643 hrs · 23,569 cycles

PASSENGER DOOR HINGE AFT LUG IS GOUGED. REPAIRED THE HINGE IAW ECTC REO 601R-52-11-1347 AND REO 601R-52-11-1347. MAJOR REPAIR.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 24,643 hrs · 23,569 cycles

FLOORBEAM ANGLE CRACKED AT BS 280, RBL 9. REMOVED AND REPLACED THE FLOORBEAM ANGLE IAW SRM 51-42-06 & 51-42-21.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 24,643 hrs · 23,569 cycles

FLOORBEAM ANGLE CRACKED AT BS 280, LBL9. REMOVED AND REPLACED THE FLOORBEAM ANGLE IAW SRM 51-42-06, & 51-42-21.

Part: DOOR — LACK OF LUBE (EMERGENCY EXIT) · airframe 24,643 hrs · 23,569 cycles

RIGHT OVERWING EMERGENCY EXIT FAILS PULL TEST. LUBRICATED THE OVERWING EXIT IAW AMM 12-20-52-640-802 AND 52-21-00-720-801. OPS CHECKED GOOD.

Part: SEAT TRACK — CORRODED (BS 544-559) · airframe 24,620 hrs · 23,545 cycles

LEFT SIDE WALL SEAT TRACK CORRODED BETWEEN FS 544.00 TO FS 559.00+80. R & R LT SIDE WALL SEAT TRACK BETWEEN FS 544.00 TO FS 559.00+80 IAW SRM 53-01-11.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 22,414 hrs · 21,285 cycles

EMERGENCY LIGHTS WILL NOT COME ON. EMERGENCY LIGHT CHARGED NORMALLY AND OPS CHECKED GOOD IAW AMM 33-51-00. NO FURTHER DEFECTS NOTED. ACFT OK OF SERVICE.

Part: ENGINE — SHUTDOWN (RIGHT) · airframe 22,376 hrs · 21,247 cycles

RIGHT ENGINE SHUTDOWN IN FLIGHT DURING CRUISE AT FL 300. ATTEMPED TWO STARTS, NO HELP. ACFT DIVERTED. EMERGENCY DECLARED. RIGHT ENGINE ASSY REPLACED, ALL OPS & FUNCTIONAL TEST GOOD, NO DEFECTS NOTED AT THIS TIME.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 20,820 hrs · 19,644 cycles

CENTER EXTERIOR EMERGENCY LIGHTS INOPERATIVE. R & R NR 2 BATTERY PACK IAW AMM 33-51-04. OPS CHECKED GOOD.

Part: FITTING — CORRODED (PAX DOOR) · airframe 20,594 hrs · 19,415 cycles

FOUND ANCHOR FITTING TO HAVE CORROSION. REMOVED FWD PAX DOOR ANCHOR FITTING IAW AMM 52-11-17-04-02, T/R 52-297. INSTALLED NEW ANCHOR FITTING IAW AMM 52-11-17-04-02.

Part: FITTING — CORRODED (PAX DOOR) · airframe 20,600 hrs · 19,420 cycles

FOUND ANCHOR FITTING CORRODED. REMOVED FWD PAX DOOR ANCHOR FITTING IAW AMM 52-11-17-04-02, INSTALLED NEW ANCHOR FITTING IAW AMM 52-11-17-04-02 .

Part: ANGLE — CORRODED (PAX DOOR) · airframe 20,634 hrs · 19,447 cycles

TWO L ANGLES AT HINGE SIDE OF PAX DOOR CORRODED. R & R TWO L ANGLES.

Part: FLOOR SUPPORT — CORRODED (BS 574-589) · airframe 20,634 hrs · 19,447 cycles

CORROSION FOUND ON FLOOR SUPPORT BETWEEN FS 574 & 589. REMOVED CORROSION IAW SRM 51-21-06.

Part: FLOOR SUPPORT — CORRODED (BS 559) · airframe 20,634 hrs · 19,447 cycles

CORROSION FOUND ON FLOOR SUPPORT BETWEEN FS 559+80 & 559+112) REMOVED CORROSION IAW SRM 51-21-06. NO DAMAGE LIMITS IS GIVEN IN SRM 53-51-43 FOR THE FLOOR SUPPORT ASSY.

Part: ANGLE — BROKEN (PRESSURE BLKHD) · airframe 20,593 hrs · 19,411 cycles

IN AEB ON LT SIDE PRESSURE BULKHEAD FS 621, THERE IS A BROKEN ANGLE AT APPROX STRINGER 14. REMOVED BROKEN CLIP LOCATED DRILLED INSTALLED AND RESTORED FINISH TO NEW CLIP PN 601-35-021-51 AS NEEDED REF: SRM 51-42-21, 51-40-11, 51-25-06 AND SRM 51-25-16.

Part: CARGO TRACK — CORRODED (BS 605-621) · airframe 20,594 hrs · 19,415 cycles

CORROSION FOUND ON CARGO TRACK BETWEEN FS 605 & 621. REMOVED CORROSION IAW SRM 51-21-6.

Part: ANGLE — CRACKED (BS 484) · airframe 20,634 hrs · 19,447 cycles

LT SIDE FS 484 PRESSURE FLOOR INTERCOSTAL ANGLE CRACKED, OTBD. REPLACED ANGLE IAW REO 601R-53-41-039.

Part: FLOOR SUPPORT — CRACKED (BS 484) · airframe 20,634 hrs · 19,447 cycles

RT SIDE PRESSURE FLOOR SUPPORT FS 484 CRACKED. REPLACED FLOOR SUPPORT IAW REO 601R-53-41-039.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 20,346 hrs · 19,145 cycles

NR 1 CEILING EMERGENCY FLOOD LIGHT INOPERATIVE. REPLACED LAMP IAW AMM 33-51-16.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 19,893 hrs · 18,679 cycles

PAX DOOR AFT DRAG ANGLE, CRACKED. UPON FURTHER INVESTIGATION FOUND PREVIOUS REPAIR IAW REO 601R-52-11-513, REV A. R & R -1 REPAIR ANGLE REF REO 601R-52-11-513, REV A.

Part: PROXIMITY SENSOR — OUT OF RIG (NLG) · airframe 19,737 hrs · 18,518 cycles

GEAR DISAGREE MESSAGE AFTER TAKEOFF, NOSE GEAR DOWN, MAIN GEAR UP. ACFT RETURN. EMERGENCY DECLARED. FOUND NLG EXTENDED/CENTERED PROXIMITY SENSOR (S23) OUT OF RIG WHEN ACFT IS IN CONFIG, RIGGED S23 IAW AMM 32-61-05, PERFORMED NUMEROUS GEAR SWINGS IAW AMM 32-30-00-720-801, OPS CHECK GOOD AT THIS TIME. SDR CLOSED.

Part: HOUSING — CRACKED (EMERGENCY LIGHT) · airframe 19,646 hrs · 18,424 cycles

GALLEY FLOOR EMERGENCY FLOOD LIGHT HOUSING CRACKED. R & R GALLEY FLOOR EMERGENCY FLOOD LIGHT HOUSING IAW AMM 33-51-19. OPS CHECKED GOOD.

Part: BULB — BURNED OUT (CONTROL PANEL) · airframe 19,058 hrs · 17,783 cycles

LIGHT BULB ON EMERGENCY LIGHTS PANEL INOPERATIVE. R & R EMERGENCY LIGHTS OFF PBA LIGHT BULBS IAW ESPM 20-24-00. NO FURTHER DEFECTS NOTED, ACFT OK FOR SERVICE.

Part: OIL SYSTEM — OVERSERVICED (ENGINE) · airframe 18,618 hrs · 17,323 cycles

ROUGH AFTER TAKEOFF, CABIN FILLED WITH SMOKE. ENOUGH SMOKE TO FILL UP TO COCKPIT. SMOKE TANLET MESSAGE ILLUMINATED. ACFT RETURNED TO DEPARTURE, EMERGENCY DECLARED. FOUND BOTH ENGINES OVERSERVICED WITH OIL DRAINED EXCESSIVE OIL FROM BOTH OIL TANKS. SERVICED BOTH ENGINES TO THE FULL MARK. R & R BOTH ACM COALESCER BAGS IAW AMM 21-15-13, OPS TESTED GOOD, RAN ENGINES AT T/O POWER IAW AMM 71-00-00, NO DEFECTS NOTED.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 18,574 hrs · 17,269 cycles

RED F/A LIGHT AT EMERGENCY EXIT ROW OTS. R & R EMERGENCY EXIT BULB IAW AMM 33-51-14. OP'S CHECKED IAW AMM 33-51-00-710-801. NO DEFECTS NOTED

Part: FITTING — CRACKED (HYD SYSTEM) · airframe 17,807 hrs · 16,442 cycles

AT 28,000 DETECTED BURNING RUBBER IN COCKPIT AND CABIN FOR APPROXIMATELY 30 SECONDS. DIDN'T REPEAT. R & R CRACKED 90 DEGREE ELBOW FITTING BETWEEN NR 1 EDP RETURN FLEXIBLE LINE AND CRES LINE IAW AMM 20-22-01. NO HYDRAULIC LEAKS AND NEW CHARGER OPERATES NORMALLY.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 17,082 hrs · 15,645 cycles

CEILING EMERGENCY LIGHT INOP AT 10CD. RELAMPED CEILING EMERGENCY LIGHT AT 10CD AS REQUIRED. OPS CK GOOD IAW AMM 33-51-00. RELAMPED CEILING EMERGENCY LIGHT AT 10CD AS REQUIRED. OPS CHK GOOD IAW AMM 33-51-00.

Part: LENS — MISSING (LIGHT) · airframe 15,849 hrs · 14,222 cycles

FLOOD LIGHT LENS MISSING AT FLOOR LEVEL ON FWD BULKHEAD AT ASD. R & R FLOOD LIGHT ASSY IAW AMM 33-51-19. (CLOSED)

Part: VALVE — FAILED (NLG) · airframe 15,771 hrs · 14,138 cycles

UPON T/O & RETRACTING GEAR NOSE GEAR DOORS WOULD NOT CLOSE. RECEIVED NOSE GEAR OPEN MASTER WANING . CYCLED GEAR ONCE. LANDED UNDER 47. DOOR REMAINED OPEN ALL THE WAY INTO THE GATE. ACFT RETURNED TO DEPARTURE AFTER T/O -- EMERGENCY EQUIPMENT STANDING BY AS A PRECAUTION. R & R NOSE GEAR DOOR SELECTOR VALVE IAW AMM 32-22-20. OPS CHECK AND LEAK CHECK GOOD. NO FURTHER DEFECTS NOTED. OK FOR SERVICE. (CLOSED)

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 15,761 hrs · 14,128 cycles

EMERGENCY BATTERY PACK NR2 IS DEAD. R & R SERVICEABLE PART IAW AMM 33-1-04-000-801 AND 33-51-04-400-801. OPS CHECK OF PACK GOOD. (CLOSED)

Part: BULKHEAD — CRACKED (BS 202.75) · airframe 15,748 hrs · 14,109 cycles

INDICATION OF CRACK APPROX .7" LONG AT 202.75 BULKHEAD AT PARKING BRAKE C BALE CUTOUT. C/W WITH EC/TC REO 601R-53-11-563 AND REO 601R-53-11-563.

Part: ATTACH FITTING — CRACKED (BS 484) · airframe 15,748 hrs · 14,109 cycles

CLIP CRACKED AT TOP IN 2 PLACES AT OTBD OF RBL 27.0 & FS 484.0. R & R CLIP IAW SRM 51-42-06. (CLOSED)

Part: INTERCOSTAL — CRACKED (BS 484) · airframe 15,748 hrs · 14,109 cycles

INTERCOSTAL CRACKED AT TOP & 1 RIVET HEAD SHEARED OFF AT LBL 36.0 & FS 484.0. REPAIR TO THE INTERCOSTAL AT F.S. 484 LBL 36, IS COMPLETED IAW REO 601R-53-41-059 AND MEETS WITH ALL THEIR REQUIREMENTS.

Part: INTERCOSTAL — CRACKED (BS 484) · airframe 15,748 hrs · 14,109 cycles

INTERCOSTAL CRACKED AT RBL 36.0 & FS 484.0. COMPLIED WITH STEPS 1 & 2 OF REO 601R-53-41-059. PERFORMED EDDY CURRENT INSP ON CUTLINE EDGES OF INTERCOSTAL AT RBL 36.0 FS 484.0. NO INDICATIONS FOUND AT THIS TIME, REPORT ATTACHED IAW STEP 3 OF REO 601R-53-41-059 AND NDTM PART 51-20-06. TOUCH UP EDGES IS REQ'D. TOUCHED UP EDGES AS REQUIRED IAW STEP 4 OF REO 601R-53-41-059. COMPLIED WITH STEPS 5 THRU 14 OF REO 601R-53-41-059. REPAIR TO THE INTERCOSTALS AT FS 484 BETWEEN BL27.00 AND BL36.00 IS COMPLETED IAW REO 601R-53-41-059 AND MEETS WITH ALL THEIR REQUIREMENTS.

Part: ATTACH FITTING — CRACKED (BS 484) · airframe 15,748 hrs · 14,109 cycles

SUPPORT CLIP CRACKED AT TOP BETWEEN OTBD OF LBL 22.0 & INTERCOSTAL AT FS 484.0. REMOVED CLIP IAW SRM 51-42-06. CLIP NEEDS DRILLED & INSTALLED. DRILLED NEW SERVICEABLE SUPPORT CLIP FOR INTERCOSTAL AT FS 484, LBL 27 SIDE IAW SRM 51-40-11. INSTALLED CLIP IAW SRM 51-42-06 AND 51-42-21. (CLOSED)

Part: ANGLE — CRACKED (BS 559) · airframe 15,748 hrs · 14,109 cycles

CAP ANGLE AT FS 559.0 RBL 18 HAS A INDICATION IN THE RADIUS 50 PERCENT FSH APPROX .2" LONG. FAILED NDT INSP. REPAIRED FS 559 BULKHEAD AND CAP ANGLES FROM LBL 27 TO RBL 27 IAW REO 601R-53-41-260 REV.D. COMPLIED WITH EC/TC REO 601R-53-41-260 IAW REO 601R-53-41-260 REV.D.

Part: BULKHEAD — CRACKED (AFT) · airframe 15,748 hrs · 14,109 cycles

REAR PRESSURE BULKHEAD WEB AFT SIDE RT FS 621 TO 625 ANGLE, STR 14 IS CRACK. REMOVED ANGLE PN 601-35012-52 IAW SRM 51-42-21, PG 19. AFTER REMOVING ANGEL, FOUND ELONGATED HOLES IN INTERCOSTAL. WAITING ENGINEERING DISPOSITION. INSTALLED NEW ANGLE PN 601-35012-52 ON REAR PRESSURE BULKHEAD WEB AFT SIDE RT FS 621 TO 625 IAW SRM 51-42-06. C/W ASA EC/TC, REO 601R-53-61-3791.

Part: SEAT TRACK — CORRODED (BS 559-567) · airframe 15,748 hrs · 14,109 cycles

CARGO COMPARTMENT FLOOR SEAT RAILS AT LBL 27 BETWEEN FS 559+80 AND FS 567.00 ARE CORRODED. REMOVED 3 CORRODED ANCHOR PLATES FROM FS 559+80 TO FS 567 LBL 27 AND INSTALLED NEW ANCHOR PLATES IAW AMM 20-21-00-910-807. REMOVED BULKHEAD HOLD DOWN BRACKET AND TRACK SEGMENT. INSTALLED NEW TRACK SEGMENT AND BULKHEAD FITTING AT LBL 27 FS 567 IAW AMM 20-21-00-910-801.

Part: ANCHOR FITTING — CRACKED (PAX DOOR) · airframe 15,748 hrs · 14,109 cycles

PASSENGER DOOR AFT ANCHOR FITTING IS CRACKED AND FWD AND AFT SWIVEL LEVERS HAVE ELONGATED HOLES. R & R PAX DOOR AFT ANCHOR FITTING AND FWD AND AFT SWIVEL LEVER IAW AMM TASK 52-11-17-000-804 AND 52-11-17-400-804. DUE ADJUSTMENT OF PAX DOOR COUNTER BALANCE SYSTEM. PERFORMED THE ADJUSTMENT OF THE PAX DOOR COUNTER BALANCE IAW AMM 52-11-17-820-802. NO DEFECTS NOTED AT THIS TIME.

Part: CARGO TRACK — CORRODED (BS 559-569) · airframe 15,748 hrs · 14,109 cycles

CARGO COMPARTMENT FLOOR CARGO RAILS AT RBL 9 BETWEEN FS 559+91 AND FS 569.00 ARE CORRODED. R & R SEAT RAILS AT STA RBL 9 BETWEEN FS 559+91 AND 569.00. WORK PERFORMED IAW 51-41-02.

Part: FLOOR SUPPORT — CORRODED (BS 559-617) · airframe 15,748 hrs · 14,109 cycles

CARGO COMPARTMENT FLOOR STRUT RAILS AT LBL 9 BETWEEN F.S. 559+91 AND F.S. 617 ARE CORRODED. REMOVED RAILS 601238663-21 2 EA AND 601R31032-51 IAW SRM 51-41-02. REMOVED 2 FWD RAILS BY REMOVING SCREWS. INSTALLED FWD RAIL SEGMENT AT FS 559+91 AND 2 HOLD DOWN CLIPS. ALL WORK IAW AMM 20-21-00-910-801. TEMP INSTALLED 2 AFT SEAT RAIL SEGMENTS. AFT SEAT RAIL SEGMENTS NEED INSTALLATION. REINSTALLED 2 AFT SEAT RAIL SEGMENTS AT LBL 9 BETWEEN FS 559+91 AND FS 617 IAW SRM 51-41-09 AND 51-41-04.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 15,748 hrs · 14,109 cycles

CARGO COMPARTMENT FLOOR SEAT RAIL AT RBL 27 BETWEEN FS 559+80 AND FS 559+96 IS CORRODED. REMOVED CARGO SEAT RAIL SEGMENT AT RBL 27 BETWEEN F.S. 559+80 AND F.S. 559+96. INSTALLED NEW SEAT RAIL SEGMENT IAW AMM 20-21-00-910-801.

Part: FLOOR SUPPORT — CORRODED (BS 568-621) · airframe 15,748 hrs · 14,109 cycles

FOUND LBL 27 FLOORBEAM CAP BETWEEN FS 568.00 AND FS 621.00 CORRODED BEYOND LIMITS. REMOVED FLOORBEAM CAP FROM FS 568.00 TO FS 621.00 AND LBL 27. ALL HOLES FOUND TO BE SERVICEABLE IN ACFT STRUCTURE IAW SRM 51-42-06 AND 51-42-21. LOCATE AND INSTALL NEW FLOORBEAM CAP. LOCATED AND DRILLED NEW SERVICEABLE FLOORBEAM CAP PN 601R35031-263 IAW SRM 51-40-11. INSTALLED FLOORBEAM CAP. INSTALLED NEW SERVICEABLE FLOORBEAM CAP AT LBL 27 IAW REO 601R-53-61-3778. QUANTITY 3 RIVNUTS REQ INSTALLATION, COMPLIED WITH ASA EC/TC REO 601R-53-61-3778.

Part: MOTOR — MALFUNCTIONED (DOOR ASSIST SYS) · airframe 15,744 hrs · 14,106 cycles

PAX DOOR JAMMED WILL NOT OPEN ( PASSENGER DOOR POWER ASSIST SYS ) R & R PAX DOOR ASSIST MOTOR IAW AMM 52-11-08. DEFER CLEARED. PLACARD REMOVED.

Part: SWITCH — FAILED (EMERGENCY LIGHTS) · airframe 15,402 hrs · 13,710 cycles

AFTER COMPLETED SHUTDOWN CHECK TO THE LINE NOTICED EMERGENCY LIGHTS ON WHITE STATUS MSG. EMERGENCY LIGHTS SWITCH IS IN ARM POSITION. R & R EMERGENCY LIGHT SWITCH AT F/A PANEL IAW AMM 20-41-00. OPS CHECK GOOD NO FURTHER DEFECT NOTED.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 15,220 hrs · 13,488 cycles

AFT CABIN CEILING EMERGENCY FLOOD LIGHT INOP. (RESOLVED ON W/O: 156512 TASKCARD: N/R-00002 ) RELAMPED AFT CABIN CEILING EMERGENCY FLOOD LIGHT. OPS CHECK GOOD. RELAMPED AFT CABIN CEILING EMERGENCY FLOOD LIGHT. OPS CHECK GOOD. (CLOSED)

Part: PUMP — OVERTEMP (HYD SYSTEM) · airframe 15,129 hrs · 13,375 cycles

NOSE OPEN/ DISAGREE MSG AFTER TAKEOFF. (ACFT RETURNED AFTER T/O -- EMERGENCY DECLARED) RFER TO AFDL NR 535842-3 FOR WORK ACCOMPLISHED. R & R 3B HYD PUMP, OPS CHECK GOOD. (CLOSED)

Part: PLACARD — SEPARATED (CABIN) · airframe 14,849 hrs · 13,063 cycles

EXIT PLACARD STICKER FELL OFF PASSENGER BOARDING DOOR. REPLACED MISSING EXIT PLACARD IAW AMM 11-30-02. OK FOR SERVICE.

Part: A/C PACK — SMOKE · airframe 14,527 hrs · 12,682 cycles

UPON SWITCHING BLEEDS TO APU ON LANDING FWA GOT SMOKE IN COCKPIT AND CABIN AND SET OFF LAV SMOKE DETECTOR, SHUTOFF BOTH PACKS AND SMOKE DISSAPATED.

Part: UNKNOWN — SMOKE (CABIN) · airframe 14,527 hrs · 12,682 cycles

AFTER SWITCHING BLEEDS FROM ENG'S TO APU IMMEDIATLY STARTED GETTING SMOKE IN COCKPIT & CABIN. SET OFF LAV SMOKE ALARM. SWITCHED BLEEDS BACK SMOKE WENT AWAY NOTHING ABNORMAL ON ECS SYNOPTIC PAGE.

Part: UNKNOWN — WARNING LIGHT · airframe 14,022 hrs · 12,125 cycles

STALL FAIL AFTER ROTATION. EMERENCY DECLARED--ENROUTE, ACFT DIVERTED DUE TO MX.

Part: APU — MALFUNCTIONED (APU BAY) · airframe 13,687 hrs · 11,785 cycles

DURING SINGLE ENGINE TAXI FOR TAKEOFF RECEIVED "APU OVERTEMP WARNING". GATE RETURN, EMERGENCY DECLARED. FIRE TRUCKS ESCORTED A/C BACK TO GATE. FLT 5348 DEL 60 MINS. AUXILIARY POWER UNIT APU - INTAKE DOOR DEACTIVATED CLOSED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,175 hrs · 11,311 cycles

CEILING EMERGENCY LIGHT 3RD FROM FRONT INOP.

Part: WEB — CRACKED (PAX DOOR)

PAX DOOR AFT WEB IS CRACKED IN ZONE 3. REPAIRED PAX DOOR AFT WEB IAW BOMBARDIER REO 601R-52-11-702. SEAL AND PAINT REQUESTED STEP 11. SEALED AND PAINTED REPAIRED AREA ON PAX DOOR AFT WEB IAW BOMBARDIER REO 601R-52-11-702 STEP 11. COMPLIED WITH ALL STEPS OF AS EC/TC REO 601R-52-11-702. (S)

Part: WEB — CRACKED (PAX DOOR)

PAX DOOR FWD WEB IS CRACKED IN ZONE 2 & 3. REPAIRED PAX DOOR FWD WEB IAW BOMBARDIER REO 601R-52-11-702. SEAL AND PAINT REQUESTED STEP 11. SEALED AND PAINTED REPAIR AREA ON PAX DOOR FWD WEB IAW BOMBARDIER REO 601R-52-11-702 STEP 11. COMPLIED WITH ALL STEPS OF ASA EC/TC REO 601R-52-11-702. (S)

Part: ATTACH FITTING — CRACKED (BS 280)

ANGLE CLIPS AT FS 280 LBL 9 AREA CRACKED AT THE INBD AND OTBD POSITIONS. REMOVED INBD & OTBD DAMAGED CLIPS FROM LBL 9 AND REPLACED WITH NEW SERVICEABLE CLIPS IAW CRJ 200 SRM 51-42-06. REMOVED ALTERNATE LANDING GEAR PULLEY BRACKET FROM FS 280 BEAM IAW CRJ 200 AMM 20-21-00-910-801. CABLE BLOCKS WERE PLACED FWD OF FS 280 PULLEY AND AT FS 292 BEAM. REINSTALLED SAME SERVICEABLE BRACKET FOR MLG ALTERNATE EXTENSION AT FS 280 IAW CRJ 200 AMM 20-21-00-910-801. CABLE BLOCKS AT FWD SIDE OF FS 280 AND AT FS 292 WERE REMOVED. OPS CHECK FOR ALTERNATE MLG EXTENSION DUE. COMPLIED WITH THE MLG OPS TEST OF THE MANUAL RELEASE SYSTEM IAW 32-34-00-710-801. THE MANUAL RELEASE SYSTEM CHECKS GOOD AT THIS TIME. ASA RII COMPLIED 5300002. (S)

Part: BULKHEAD — DAMAGED

REAR PRESSURE BULKHEAD WEB THAT SURROUNDS LINTEL ATTACHMENT FITTING HAS AN INDICATION NOTED APPROX 1 INCH IN LENGTH AND 60 PERCENT FULL SCREEN HEIGHT. FAILED NDT INSPECTION. REPAIRED AFT PRESSURE BULKHEAD WEB AND LINTEL FITTING IAW ASA EC/ET REO 601R-53-61-1230. ASA RII COMPLIED WITH 5300002. (S)

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 11,027 hrs · 9,356 cycles

DURING CRUISE AT FL 310, THE STAB TRIM AND MACH TRIM FAIL MESSAGES DISPLAYED ON EDI. RAN QRH PROBLEM PERSISTED. ALSO ACCOMPANYING MSG AP PITCH TRIM MSG. RAN QRH, AP PITCH TRIM MSG PERSISTED UNTIL A/P DISCONNECTED. FLT 4563 DEL 41 MINS. EMERGENCY DECLARED.

Part: DOOR — BINDS (ASD) · airframe 10,628 hrs · 9,018 cycles

STATION REPORTS DIFFICULTY CLOSING ASD.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 8,884 hrs · 7,594 cycles

F/O`S FLASHLIGHT BATTERIES INOP.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 8,190 hrs · 7,072 cycles

CAPTAIN`S FLASHLIGHT INOP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 7,810 hrs · 6,799 cycles

RIGHT FWD EXT EMERGENCY EXIT LIGHT INOP.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 7,619 hrs · 6,661 cycles

FIVE MINUTES AFTER 10TH STAGE BLEEDS WERE SWITCHED TO APU, NOTED AN OILY SMELL IN COCKPIT. LEFT PACK SHOWED ONLY 8 PSI. SHUTDOWN LEFT PACK. SMELL WENT AWAY. NO SMELL IN CABIN.

Part: CONTROL UNIT — FAILED (NLG STEERING) · airframe 6,705 hrs · 5,932 cycles

NOSE WHEEL STEERING WENT LEFT THEN RIGHT ON TAKEOFF ROLL. REPLACED LEFT RVDT, CHECKED NOSE WHEEL STEERING RIGGING; HIGH SPEED TAXI TEST CHECK GOOD.

Part: WARNING LIGHT — FALSE ACTIVATION (SPOILERS)

UPON TAKEOFF, RECEIVED LOW SPEED ABORT. CREW CLEARED SPOILER FAULT, AND DID ANOTHER UNEVENTFUL TAKEOFF.