N754EV

Part: CONNECTOR — UNSECURE (SMOKE DETECTOR) · airframe 36,037 hrs · 26,349 cycles

SMOKE AFT LAV WARNING MESSAGE ON APPROACH AT 7000 FT MSL. RAN QRH HALF OF QRH FOR SMOKE AFT LAV, MESSAGE PERSISTED. NO SIGN OF SMOKE OR FUMES. TROUBLESHOT AFT LAV WARNING MESSAGE, PER SERVICE LETTER, NO DEFECTS NOTED. CONTINUED TROUBLESHOOTING AFT LAV WARNING, PER CRJ700 FIM. SUSPECT AFT LAV SMOKE DETECTOR DEFECTIVE. FOUND AFT LAV SMOKE DECTECTOR ELECTRICAL CONNECTOR NOT PROPERLY SECURED. REMOVED AND REPLACED AFT LAV SMOKE DETECTOR, PER CRJ 700 AMM. OPERATIONS CHECK GOOD. PERFORMED ENG RUNS WITH BLEED IN ALL POSSIBLE CONFIGURATIONS, PER CRJ 700 AMM AND PERFORMED OPERATIONAL TEST OF AIR CONDITION DISTRIBUTION SYSTEM ON APU AND ENGINE BLEEDS, PER CRJ 700 AMM. OPERATIONS CHECK GOOD.

Part: FAIRING — CHAFED (PAX DOOR HINGE) · airframe 36,032 hrs · 26,347 cycles

PAX DOOR HINGE FAIRING 141AL IS CHAFING ON DOOR SKIN. C-CHECK RO 12/24/2020. REMOVED DAMAGED PANEL 141AL AND INSTALLED NEW SERVICEABLE PANEL, IAW CRJ-700 AMM.

Part: INTERCOSTAL — CORRODED (ZONE 100) · airframe 36,032 hrs · 26,347 cycles

INTERCOSTAL FROM FS 310.00 TO 333.00 AT STRINGER 21L IS CORRODED. C-CHECK RO 12/24/2020. REMOVED AND REPLACED INTERCOSTAL FROM FS 310.00 TO 333.00 AT STRINGER 21L, IAW CRJ-700 SRM. REF ATTACHED TASK CARD AND M-337 FOR RII TASKS. NO CHANGE TO WEIGHT AND BALANCE.

Part: FRAME — CORRODED (ZONE 100) · airframe 36,032 hrs · 26,347 cycles

FRAME SECTION AT FS 319.00 FROM STRINGER 18L-21L IS CORRODED. C-CHECK RO 12/24/2020. REMOVED AND REPLACED FRAME SECTION AT 319.00 FROM STRINGER 18L-21L, IAW CRJ-700 SRM. REF ATTACHED TASK CARD AND M-337. NO CHANGE TO WEIGHT AND BALANCE. PRESSURE CHECK GOOD, IAW CRJ 700 AMM.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 36,032 hrs · 26,347 cycles

FLOOR SUPPORT ANGLE FROM FS 310.00 TO 333.00 AT LBL 27 IS CORRODED. C-CHECK RO 12/24/2020. REMOVED AND REPLACED FLOOR SUPPORT ANGLE FROM FS 310.00 TO 333.00 AT LBL 27, IAW CRJ-700 SRM.

Part: INTERCOSTAL — CORRODED (ZONE 100) · airframe 36,032 hrs · 26,347 cycles

INTERCOSTAL BETWEEN FS 319.00 AND FS 349.00 AT STRINGER 20R FOUND TO BE CORRODED. C-CHECK RO 12/24/2020. REMOVED CORRODED INTERCOSTAL AND INSTALLED NEW SERVICEABLE INTERCOSTAL, IAW CRJ-700 SRM. COMPLETED ATTACHED SKY CARD AND M-337. NO CHANGE TO WEIGHT AND BALANCE.

Part: FRAME — CORRODED (ZONE 200) · airframe 36,032 hrs · 26,347 cycles

RT FRAME SECTION AT FS 333.00 FOUND TO BE HEAVILY CORRODED. C-CHECK RO 12/24/2020. REMOVED CORRODED RT FRAME SECTION AT FS 333.00 AND INSTALLED NEW SERVICEABLE FRAME SECTION, IAW CRJ-700 SRM. COMPLIED WITH ATTACHED TASK CARD AND M-337. NO CHANGE TO WEIGHT AND BALANCE.

Part: STRINGER CLIP — CORRODED (ZONE 200) · airframe 36,032 hrs · 26,347 cycles

FOUND CORRODED CLIP AT STRGR 18L BETWEEN FS 280-FS 295. C-CHECK RO 12/24/2020. REMOVED AND REPLACED CLIP AT STRGR 18L BETWEEN FS 280-FS295, IAW CRJ700 SRM AND PAINTED AND APPLIED CIC, IAW CRJ 700 SRM.

Part: LUG — DAMAGED (LT AILERON) · airframe 36,032 hrs · 26,347 cycles

LT AILERON LUG NR 1 FOUND TO HAVE DAMAGE OUT OF LIMITS FOR REPAIR, AILERON REQUIRES REPLACEMENT. C-CHECK RO 12/24/2020. RECEIVED NEW SERVICEABLE AILERON, REF CAMP 21674471 FOR REMOVAL AND INSTALLATION.

Part: PANEL — CHAFED (RT WING) · airframe 36,032 hrs · 26,347 cycles

RT INBOARD FLAP VANE ACCESS PANEL 684ET IS A DEEP CHAFING ON LEADING EDGE. C-CHECK RO 12/24/2020. RECEIVED SERVICABLE RT INBOARD FLAP VANE PANEL 684ET, REFERENCE MASTER PANEL BOOK CO 10173820 JOB 91017380 OP REF BINDER CAMP CP 21674491 FOR REMOVAL AND INSTALLATION. REFERENCE CONTINUATION FOR WORK PERFORMED.

Part: STRINGER — CORRODED (ZONE 200) · airframe 36,032 hrs · 26,347 cycles

STR 23L BETWEEN FS 1015-FS 1031 CORROSION. C-CHECK RO 12/24/2020. REMOVED AND REPLACED STR 23L BETWEEN FS 1015-FS 1031, IAW CRJ 700 SRM & SKY CARD NO WEIGHT CHANGE NO INSPECTION REQUIREMENTS FORM 337 IS ATTACHED.

Part: LAP JOINT — CORRODED (ZONE 100) · airframe 36,032 hrs · 26,347 cycles

CORROSION FOUND AT AT STR 21L AT FS 333.00 ON CIRCUMFERENTIAL JOINT. C-CHECK RO 12/24/2020. REPAIRED CORROSION AT STR 21L AT FS 333.00 CIRCUMFERENTIAL JOINT, IAW MHIRJ REO & SKY CARD NOTE DTA REQUIREMENTS WILL BE PROVIDED WITHIN 12 MONTHS. NO WIEGHT CHANGES FORM 337 IS ATTACHED, REF CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.

Part: ANGLE — CORRODED (ZONE 100) · airframe 36,032 hrs · 26,347 cycles

WHILE ACCESSING FOUND CIRCUMFERENTIAL JOINT ANGLE WITH CORROSION. C-CHECK RO 12/24/2020. REMOVED AND REPLACED CIRCUMFERENTIAL JOINT ANGLE, IAW CRJ 700 SRM & SKY CARD. NO WEIGHT CHANGES FORM 337 IS ATTACHED. REF ATTACHED CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.

Part: STRINGER — CORRODED (ZONE 100) · airframe 36,032 hrs · 26,347 cycles

CORROSION FOUND ON STR 20L BETWEEN FS 319 AND FS 333. C-CHECK RO 12/24/2020. REMOVED CORRODED STRINGER 20L BETWEEN FS 319.00 AND 333.00 AND INSTALLED NEW SERVICEABLE STRINGER, IAW CRJ-700 SRM. REF ATTACHED TASK CARD AND M-337. NO CHANGE TO WEIGHT AND BALANCE.

Part: STRINGER — CORRODED (ZONE 200) · airframe 36,032 hrs · 26,347 cycles

STR 19L FROM FS 338 TO FS 342 CORRORED. C-CHECK RO 12/24/2020. REMOVED AND REPLACED STR 19L FROM FS 338 TO FS 342, IAW CRJ700 SRM & SKY CARD NO WEIGHT CHANGES FORM 337 IS ATTACHED.

Part: HINGE — GOUGED (PAX DOOR) · airframe 36,032 hrs · 26,347 cycles

PAX DOOR HINGE (DOOR SIDE) LUGS NR 1, 2, 3, 4, 5, 6, 7, 8, 9, 13, 14, 15, 19, 20, 25, AND 26 ARE GOUGED. C-CHECK RO 12/24/2020. REMOVED DAMAGE BY COMPLYING WITH REPAIR TYPE 1 OF REO. COMPLETED AND ATTACHED M-337 AND SKY CARD. NO WEIGHT CHANGE. REFERENCE CONTINUATION CARD AND ATTACHED SKY CARD FOR WORK PERFORMED.

Part: WINDOW — CRAZED (GALLEY DOOR) · airframe 36,032 hrs · 26,347 cycles

GALLEY DOOR WINDOW IS BADLEY CRAZED. C-CHECK RO 12/24/2020. REMOVED AND REPLACED GALLEY SERVICE DOOR WINDOW, IAW CRJ-700 AMM.

Part: SKIN — CHAFED (CARGO DOOR) · airframe 36,032 hrs · 26,347 cycles

CARGO DOOR OUTER SKIN HAS TWO CHAFES ON UPPER EDGE OF DOOR. C-CHECK RO 12/24/2020. REPAIRED CARGO OUTER DOOR CHAFES, IAW REO. COMPLETED TASK CARD AND ATTACHED FORM 337. NO WEIGHT CHANGE. REFERENCE CONTINUATION CARD FOR WORK PERFORMED.

Part: SEAT TRACK — CORRODED (MAIN CABIN) · airframe 36,032 hrs · 26,347 cycles

LBL 9 CABIN FLOOR SEAT TRACK FROM FS 485.00 TO FS 581.00 IS CORRODED. C-CHECK RO 12/24/2020. REMOVED CORRODED SEAT TRACK AT LBL 9 FS 485.00 TO FS 517.00 AND INSTALLED NEW SEAT TRACK, IAW CRJ-700 AMM.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 36,032 hrs · 26,347 cycles

RBL 9 CABIN FLOOR SEAT TRACK FROM FS 485.00 TO FS 581.00 IS CORRODED. C-CHECK RO 12/24/2020. REMOVED AND REPLACED RBL 9 CABIN FLOOR SEAT TRACK FROM FS 485.00 TO FS 581.00, IAW CRJ 700 AMM. REF ATTACHED CONTIUATION CARD FOR DETAILS OF WORK PERFORMED.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 36,032 hrs · 26,347 cycles

CABIN SIDE SEAT RAIL RT BETWEEN FS 714.00 TO FS 761.85 IS CORRODED. C-CHECK RO 12/24/2020. REMOVED RT SIDE SEAT RAIL AT FS 714.00 TO 761.85 AND INSTALLED NEW SERVICEABLE SEAT TRACK, IAW CRJ-200 AMM.

Part: STRINGER — CORRODED (ZONE 200) · airframe 36,032 hrs · 26,347 cycles

RT STRINGER 20 R IS CORRODED AT FS 347.00. C-CHECK RO 12/24/2020. REMOVED AND REPLACED RT STRINGER 20R AT FS 347.00, IAW CRJ 700 SRM AND SKY CARD NOTE NO WEIGHT CHANGES AND FORM 337 IS ATTACHED. REF CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.

Part: ANGLE — CORRODED (ZONE 200) · airframe 36,032 hrs · 26,347 cycles

FS 280 FWD J ANGLE IS CORRODED FROM BL 9.04 LT AND BL 9.04 RT SIDE. C-CHECK RO 12/24/2020. INSTALLED SERVICABLE J ANGLE AT FS 280 FROM LBL 9.04 TO RBL 9.04, IAW CRJ 700 SRM. REFERENCE CONTINUATION CARD FOR WORK PERFORMED.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 36,032 hrs · 26,347 cycles

CABIN SIDE SEAT RAIL LT FROM FS 379.00 TO FS 512.00 IS CORRODED. C-CHECK RO 12/24/2020. INSTALLED SERVICEABLE CABIN SIDE SEAT RAIL LT FROM FS 379.00 TO FS 512.00, IAW CRJ 700 AMM. REFERENCE CONTINUATION CARD FOR WORK PERFORMED.

Part: INTERCOSTAL — CORRODED (ZONE 200) · airframe 36,032 hrs · 26,347 cycles

INTERCOSTAL FROM FS 310.00 TO FS 349.00 AND AFT ATTACHMENT CLIP IS CORRODED LOCATED AT STR 20R. C-CHECK RO 12/24/2020. REMOVED AND REPLACED INTERCOSTAL FROM FS 310.00 TO FS 349.00 AND AFT ATTACHMENT CLIP AT STR 20R, IAW CRJ 700 SRM AND SKY CARD. REF ATTACHED CONTINUATION CARD FOR DETAILS OF WORK PERFORMED. NO WEIGHT CHANGES AND FORM M-337 IS ATTACHED.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 36,032 hrs · 26,347 cycles

CABIN SIDE SEAT RAIL LHS BETWEEN FS 512 & FS 570 IS CORRODED. C-CHECK RO 12/24/2020. AMM INSTALLED SERVICEABLE CABIN SIDE SEAT RAIL LT BETWEEN FS 512 AND FS 570, IAW CRJ 700 AMM. REFERENCE CONTINUATION CARD FOR WORK PEERFORMED.

Part: SUPPORT CHANNEL — CORRODED (CABIN) · airframe 36,032 hrs · 26,347 cycles

CABIN SIDE SEAT TRACK SUPPORT CHANNEL IS CORRODED FROM FS 785.15 TO FS 797.00. C-CHECK RO 12/24/2020. REMOVED AND REPLACED CABIN SIDE SEAT TRACK SUPPORT CHANNEL FROM FS 785.15 TO FS 797.00, IAW CRJ 700 AMM.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 36,032 hrs · 26,347 cycles

INTERCOSTAL AT STR 21L FROM FS 310.00 TO FS 349.00 IS HEAVILY CORRODED. C-CHECK RO 12/24/2020. REMOVED AND REPLACED INTERCOSTAL FROM FS 333-349 AT STRINGER 21L, IAW CRJ-700 SRM. REF ATTACHED SKY CARD AND M-337. NO WEIGHT CHANGES.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 36,032 hrs · 26,347 cycles

CABIN SIDE SEAT RAIL BETWEEN FS 785.15 AND FS 797.00 IS CORRODED. C-CHECK RO 12/24/2020. REMOVED AND REPLACED RT CABIN SIDE SEAT RAIL BETWEEN FS 785.15-FS 847 +6", IAW CRJ700 AMM.

Part: LINK — CORRODED (LT WING AILERON) · airframe 36,032 hrs · 26,347 cycles

BOTH LT WING AILERON PCU OUTPUT LINKS AND HARDWARE ARE CORRODED. C-CHECK RO 12/24/2020. REMOVED AND REPLACED LT AILERON PCU OUTPUT LINK AND HARDWARE, IAW CRJ700 AMM. OPERATIONS TEST GOOD.

Part: LINK — CORRODED (RT WING AILERON) · airframe 36,032 hrs · 26,347 cycles

BOTH RT WING AILERON PCU OUTPUT LINK AND HARDWARE ARE CORRODED. C-CHECK RO 12/24/2020. REPLACED THE RIGHT AILERON PCU OUTPUT LINKS AND HARDWARES, IAW CRJ-700 AMM TASK.

Part: SKIN — CHAFED (LT AILERON) · airframe 36,032 hrs · 26,347 cycles

LT AILERON LOWER HINGE LINE SKIN IS CHAFED BETWEEN WS 348 AND WS 353 APPROXIMATELY .750IN WIDE X .020 DEEP. C-CHECK RO 12/24/2020. RECEIVED NEW SERVICEABLE AILERON PN: CC670-13000-1 SN: 7678, REF CAMP 21674471 FOR INSTALL.

Part: SKIN — CORRODED (ZONE 100) · airframe 36,032 hrs · 26,347 cycles

FUSELAGE SKIN AT STR 27, FS 978-982 HAS AREA WITH A CHAFE FROM A SCREW, AN AREA OF CORROSION AROUND THAT SCREW AND AN AREA EXTENDING FROM THAT CORROSION WITH MISSING PAINT THAT HAS BEEN POORLY BLENDED AND TREATED. C-CHECK RO 12/24/2020. REPAIRED FUSELAGE SKIN AT STR 27 FS 978-982 CHAFE WITH AREA OF CORROSION AROUND THAT SCREW AND BEYOND, IAW BOMBARDIER REO & SKY CARD INSPECTION DUE IN 40000 FLIGHT CYCLES FROM NOW AT 66347 FLIGHT CYCLES WITH A REPEAT EVERY 40000 FLIGHT CYCLES. WEIGHT CHANGE IS AFFECTED FORM 337 IS ATTACHED.

Part: SKIN — CHAFED (LT AILERON) · airframe 36,032 hrs · 26,347 cycles

LT AILERON UPPER HINGE LINE SKIN IS CHAFED BETWEEN WS 282 AND WS 353 APPROXIMATELY .250IN WIDE X .020IN DEEP. C-CHECK RO 12/24/2020. RECEIVED NEW SERVICEABLE AILERON PN: CC670-13000-1 SN: 7678, REF CAMP 21674471 FOR INSTALL.

Part: DOOR SILL — CORRODED (ZONE 100) · airframe 36,032 hrs · 26,347 cycles

AFT CARGO DOOR SILL HAS CORROSION IN MULTIPLE PLACES. C-CHECK RO 12/24/2020. REMOVED AND REPLACED AFT CARGO DOOR SILL, IAW MHIRJ REO AND CRJ 700 SRM & SKY CARD NO WEIGHT CHANGE AND FORM M337 IS ATTACHED. REF ATTACHED CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.

Part: BRACKET — CORRODED (ZONE 200) · airframe 36,032 hrs · 26,347 cycles

BRACKET CORRODED AT STRINGER 19L AND FS 1031.00. C-CHECK RO 12/24/2020. REMOVED AND REPLACED STRINGER CLIP AT STRINGER 19L AT FS 1031, IAW CRJ 700 SRM.

Part: BOLT — CORRODED (BPSU MOUNT) · airframe 36,032 hrs · 26,347 cycles

RT FLAP BPSU MOUNTING HARDWARE IS CORRODED. C-CHECK RO 12/24/2020. REMOVED AND REPLACED RT FLAP BPSU CORRODED HARDWARE WITH NEW SERVICEABLE HARDWARE, IAW CRJ 700 AMM. OPERATIONS AND RIG CHECKS GOOD. REFERENCE CONTINUATION CARD FOR WORK PERFORMED.

Part: TORQUE TUBE — CORRODED (RT WING FLAPS) · airframe 36,032 hrs · 26,347 cycles

RT INBOARD FLAP TORQUE TUBE CARRIER BEARING AT WS 97.45 IS CORRODED. C-CHECK RO 12/24/2020. REMOVED AND INSTALLED NEW SERVICEABLE RT INBOARD FLAP TORQUE TUBE, IAW SKYWEST TASK CARDS. REFERENCE TASK CARDS FOR WORK PERFORMED.

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 36,032 hrs · 26,347 cycles

RT INBOARD FLAP LOWER SKIN IS CHAFED AROUND PERIMETER OF INBOARD FAIRING. C-CHECK RO 12/24/2020. REPAIRED RT INBOARD FLAP LOWER SKIN CHAFE BY DOING A SKIN SPLICE REPAIR, IAW CRJ700 SRM. COMPLETED TASK CARD AND ATTACHED FORM M-337. WEIGHT CHANGE +3.83 LBS, ARM 847.00 AND MOMENT +3244 IN LB. SEE CONTIINUATION CARD FOR DETAILS OF WORK PERFORMED.

Part: BRACKET — CORRODED (ZONE 200) · airframe 36,032 hrs · 26,347 cycles

BRACKET CORRODED AT STRINGER 19L AND FS 1015.00. C-CHECK RO 12/24/2020. REMOVED CORRODED STRINGER CLIP AT FS 1015.00 STRINGER 19L AND INSTALLED NEW SERVICEABLE CLIP, IAW CRJ-700 SRM. NOTE CLIP WAS FABRICATED, REF ATTACHED CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.

Part: MOUNT — CORRODED (FLAP BPSU) · airframe 36,032 hrs · 26,347 cycles

LT FLAP BPSU MOUNTING HARDWARE IS CORRODED. C-CHECK RO 12/24/2020. REMOVED AND REPLACED SIEZED AND CORRODED LT FLAP BPSU MOUNTING HARDWARE, IAW CRJ 700 AMM.

Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 36,032 hrs · 26,347 cycles

LT INBOARD FLAP LOWER SKIN IS CHAFED AROUND PERIMETER OF INBOARD HINGE FAIRING. C-CHECK RO 12/24/2020. REPAIRED LT INBOARD FLAP LOWER SKIN CHAFE BY DOING A SKIN SPLICE REPAIR, IAW CRJ700 SRM. COMPLETED TASK CARD AND ATTACHED FORM M-337. WEIGHT CHANGE +3.83 LBS, ARM 847.00 AND MOMENT +3244 IN LB. SEE CONTIINUATION CARD FOR DETAILS OF WORK PERFORMED.

Part: PANEL — CHAFED (FUSELAGE) · airframe 36,032 hrs · 26,347 cycles

PANEL 684 BB IS CHAFFED AROUND HINGE FAIRING CONTACT. C-CHECK RO 12/24/2020. RECIEVED NEW SERVICEABLE PANEL 684BB, SEE CONTINUATION FOR WORK PERFORMED. REF CAMP 21674491 FOR INSTALL OF PANEL.

Part: PANEL — CHAFED (LT WING) · airframe 36,032 hrs · 26,347 cycles

PANEL 584 BB IS CHAFED AROUND FAIRING CONTACT. C-CHECK RO 12/24/2020. RECEIVED NEW SERVICEABLE PANEL 584BB, REF ATTACHED CONTINUATION FOR WORK PERFORMED. REF CAMP 21674490 FOR INSTALL OF PANEL.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 36,032 hrs · 26,347 cycles

LT OUTBOARD FLAP VANE LEADING EDGE HAS VERTICLE CHAFE ON LOWER LEADING EDGE SURFACE AT WS 266. C-CHECK RO 12/24/2020. REMOVED DAMAGED LT OUTBOARD FLAP SKIN PANEL AND INSTALLED NEW PANEL, IAW CRJ-700 SRM. COMPLETED ATTACHED TASK CARD AND M-337. NO CHANGE TO WEIGHT AND BALANCE.

Part: SKIN — DAMAGED (ZONE 100) · airframe 36,032 hrs · 26,347 cycles

COMPLY WITH SCHEDULED MAINTENANCE CODE: RA53479-670-53-00-045 754EV FS256 ON STR23R-PR1. COMPLIED WITH TEMPORARY REPAIR, PER REO BLENDED DAMAGED SKIN AS REQUIRED AT FS 256 ON STR 23R. REPAIR IS VALID UNTIL NEXT HEAVY MAINTENANCE CHECK OR FOR 8000 FLIGHT HOURS MAXIMUM (WHICHEVER COMES FIRST). PART NUMBER: -, SERIAL NUMBER: 10173, POSITION: C-CHECK RO 12/24/2020. COMPLIED WITH PERMANANT REPAIR AT FS 256 ON STR 23R, IAW MHIRJ REO AND SKY CARD NOTE REPAIR WILL HAVE ADDITIONAL INSPECITON REQUIREMENTS TO BE COMPLETED WITHIN 12 MONTHS. NO WEIGHT CHANGE AND FORM 337 IS ATTACHED.

Part: WARNING MESSAGE — FALSE ACTIVATION (NLG STEERING) · airframe 34,764 hrs · 25,322 cycles

AFTER TAKE OFF RECEIVED STEERING IN-OP CAUTION MESSAGE, RAN QRH, RETURNED TO FIELD AND LANDED. LANDED WITHOUT NWS. FLIGHT 3126 CLOSED THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 20065245 WITH THE FOLLOWING CORRECTIVE ACTION: "FOUND B1 CODE 007460 NGDL DISAGREE. THIS MESSAGE IS RELATED TO AND CAUSED BY THE GEAR DISSAGREE. SEE ML 20065246 FOR GEAR DISAGREE CORRECTIVE ACTIONS. NWS OPS CHECKS GOOD AT THIS TIME REFERENCING AMM."

Part: STRUT — COLLAPSED (NLG) · airframe 34,764 hrs · 25,322 cycles

RECEIVED GEAR DISAGREE AFTER SELECTING GEAR HANDLE UP. AFTER SELECTING GEAR DOWN, WAITED A LONGER THAN NORMAL FOR 3 GREEN DOWN AND LOCKED INDICATIONS. DECLARED AN EMERGENCY AND LANDED. FLIGHT 3126 CLOSED "UPON INSPECTION OF AIRCRAFT FOUND NLG SHOCK STRUT FULLY COMPRESSED. PERFORMED NLG PISTON/AXLE STRUT SEAL REPACK REFERENCING AMM. PERFOMED FULL SERVICING (OIL AND NITROGEN) OF THE NLG SHOCK STRUT WITH AIRCRAFT ON JACKS REFERENCING AMM. LEAK CHECK GOOD. PERFORMED OPS CHECK OF THE LANDING GEAR EXTENSION AND RETRACTION SYSTEM REFERENCING AMM. OPS CHECK GOOD FOUND NO FAULTS OR DEFECTS AT THIS TIME. OK FOR SERVICE."

Part: VALVE — FAILED (E/E COOLING) · airframe 34,616 hrs · 25,192 cycles

AIRCRAFT WAS NOT PRESSURIZING AT ALTITUDE FLIGHT # 3044 CLOSEDFOUND AVIONICS COOLING GROUND VALVE OPEN UPON ARRIVAL TO STATION. SEE ID 311953 FOR REACTIVATION OF AVIONICS GROUND COOLING VALVE AND ID 311954 FOR CORRECTIVE ACTION FOR SERVICE DOOR INDICATION DEFERRAL. AIRCRAFT PRESSURE CHECKS GOOD ON THE GROUND,

Part: ENGINE — MALFUNCTIONED (LEFT) · airframe 33,892 hrs · 24,557 cycles

AFT LAV SMOKE WARNING MESSAGE ON ROTATE. RETURN TO FIELD. (FLT#3136) FO: 05/13/2019 CLOSED REMOVED AND REPLACED LEFT ENGINE IAW AMM.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 33,539 hrs · 24,266 cycles

SMOKE AFT LAV MASTER WARNING MESSAGE DURING CLIMB. SMELL WAS NOTICED FROM THE FLIGHT DECK, FA REPORTED NO SIGN OF SMOKE IN THE LAV. RETURNED TO FIELD. (FLT#3291) FO: 03/06/2019 CLOSED REMOVED AND REPLACED AFT LAV SMOKE DETECTOR IAW AMM. OPS CHECK GOOD AT THIS TIME.

Part: STRIKER — GOUGED (FUSELAGE) · 24,170 cycles

PAX DOOR LOWER SEAL STRIKER HAS SEVERAL GOUGES ALONG UPPER EDGE. (C-CHECK) RO: 01/26/2019 PERFORMED PERMANENT REPAIR IAW REO. PRESSURE LEAK CHECK GOOD AT THIS TIME.

Part: FRAME — DAMAGED (FUSELAGE) · 24,170 cycles

REPAIR MID SECTOR FRAME AT FS 517 AND STR 25L IN FWD CARGO BAY. (C-CHECK) RO: 01/26/2019 PERFORMED REPAIR OF MID SECTOR FRAME AT FS 517 AND STR 25L IN FWD CARGO BAY IAW REO. LEAK CHECK OF REPAIRED AREA GOOD AT THIS TIME.

Part: PLATE — CORRODED (FUSELAGE) · 24,170 cycles

FWD CARGO LOWER SURROUND SILL PLATE HAS CORROSION AROUND SEVERAL FASTENERS. (C-CHECK) RO: 01/26/2019 REMOVED CORROSION FROM FWD CARGO LOWER SURROUND SILL PLATE, IAW REO.

Part: DOOR SILL — GOUGED (FUSELAGE) · 24,170 cycles

FWD BAG BAY DOOR SILL HAS A GOUGE/NICK ON THE EDGE COMMON TO UPPER FLANGE AND WEB OF SILL 4" AFT OF FWD EDGE. (C-CHECK) RO: 01/26/2019 BLENDED DAMAGE, FWD BAG BAY DOOR SURROUND STRUCTURE EDGE OF SILL AND INNER SKIN, IAW SRM AND REO.

Part: PLATE — CORRODED (FUSELAGE) · 24,170 cycles

FWD LOWER EXTERNAL JOINT PLATE AT FS533 OF FWD CARGO DOOR ENTRANCE HAS LIGHT CORROSION AT SEVERAL PLACES. (C-CHECK) RO: 01/26/2019 REMOVED CORROSION ON FWD LOWER EXTERNAL JOINT PLATE AT FS533 IAW REO.

Part: PLATE — CORRODED (FUSELAGE) · 24,170 cycles

FWD CARGO DOOR LOWER SURROUND PLATE CORRODED AT FWD AND AFT DOOR HINGES. (C-CHECK) RO: 01/26/2019 REMOVED CORROSION ON FWD CARGO DOOR LOWER SURROUND PLATE AND AFT DOOR HINGES IAW REO.

Part: FRAME — CORRODED (FUSELAGE) · 24,170 cycles

FS 265.00 FRAME LOWER FLANGE CORRODED FROM APPROXIMATELY 7" TO THE LEFT TO 5" TO THE RIGHT OF THE NLG JACK FITTING SUPPORTS. (C-CHECK) RO: 01/26/2019 INSTALLED NEW FS 265.00 FRAME ANGLE IAW SRM. PERFORMED LEAK CHECK OF FASTENERS IAW AMM. LEAK CHECK GOOD.

Part: STRINGER — CORRODED (FUSELAGE) · 24,170 cycles

CORROSION ON STR 24L BETWEEN FS 517.00 AND FS 533.00. (C-CHECK) RO: 01/26/2019 REMOVED AND REPLACED STR 24L BETWEEN FS 517 AND FS 533 IAW SRM. PRESSURE CHECK GOOD.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · 24,170 cycles

DD6 CENTER INTERCOSTAL MIDDLE CLIP P/N 600-31902-269 CORRODED. (C-CHECK) RO: 01/26/2019 REMOVED AND REPLACED WITH NEW PART IAW SRM.

Part: RETAINER — CORRODED (E&E DOOR) · 24,170 cycles

AVIONICS BAY DOOR“ ALL 4 SEAL RETAINERS HAVE EVIDENCE OF CORROSION. (C-CHECK) RO: 01/26/2019 REMOVED AND REPLACED ALL 4 SEAL RETAINERS, P/N'S CC670-38662-5, CC670-38663-5, CC670-38674-3 AND CC670-38675-3, IAW SRM.

Part: FIREWALL — CRACKED (NR 1 PYLON) · airframe 33,164 hrs · 23,984 cycles

NR 1 PYLON FIREWALL WEB CRACKED IN SEVERAL PLACES AROUND HYDRAULIC FITTING. REPAIRED IAW EC/TC SNIEO MM670-37150 S03.

Part: UNKNOWN — ODOR (CABIN) · airframe 32,949 hrs · 23,810 cycles

DURING BOARDING THE CABIN STARTED TO FILL UP WITH A SMOKEY HAZE. ALSO HAD A VERY STRONG ODOR. NOT A BURNING SMELL. INSPECTED PSU'S NEAR ROW 4 WHERE SMELL IS LOCALIZED. NO EVIDENCE OF FIRE OR BURNING. ALSO INSPECTED RIGHT ACM IAW AMM 21-50-00. NO DEFECTS NOTED. SMOKEY HAZE IS CLEARED UP. HAZE BELIEVED TO BE FROM CONDENSATION SINCE PACKS WERE RECENTLY JUST TURNED ON. SWEET /CHEMICAL LIKE SMELL REMAINS ONLY STRONG AROUND ROW 4. NO C/B POPPED, ALL LIGHTS AND SEAT PWR OPERATIONAL. NO DEFECTS NOTED.

Part: ENGINE — FAILED (RIGHT) · airframe 32,007 hrs · 23,050 cycles

PILOT REPORTED THE RT ENGINE FAILED AFTER TAKEOFF. SECURED THE ENGINE AND LANDED. MX REMOVED AND REPLACED THE RIGHT ENGINE. ACFT APPROVED FOR RETURN TO SERVICE.

Part: STRINGER SPLICE — CORRODED (BS 333) · airframe 31,321 hrs · 22,517 cycles

STRINGER SPLICE 25R, BS 333 HAS CORROSION. MAINTENANCE REPLACED THE STRINGER SPLICE.

Part: STRINGER — CORRODED (BS 364) · airframe 31,321 hrs · 22,517 cycles

STRINGER 26R HAS CORROSION AT BS 364. MAINTENANCE REPLACED THE STRINGER.

Part: STRINGER SPLICE — CORRODED (BS 333) · airframe 31,321 hrs · 22,517 cycles

STRINGER SPLICE 26R HAS CORROSION AT BS 333. REPLACED THE STRINGER SPLICE.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 31,321 hrs · 22,517 cycles

PAX DOOR INTERCOSTAL CORRODED. COMPLIED WITH EA 25-2017-101 AND ECTC 25-2017-101.

Part: STRINGER — CORRODED (BS 333-349) · airframe 31,321 hrs · 22,517 cycles

STRINGER 26L HAS CORROSION BETWEEN BS 333 - 349. MAINTENANCE REPLACED THE STRINGER.

Part: DOUBLER — CORRODED (BS 295-310) · airframe 31,321 hrs · 22,517 cycles

TCAS DOUBLER HAS CORROSION BETWEEN BS 295 - 310. MAINTENANCE REMOVED AND REPLACED THE TCAS DOUBLER.

Part: BUTTSTRAP — CORRODED (BS 333) · airframe 31,321 hrs · 22,517 cycles

BS 333 BUTTSTRAP HAS CORROSION, FORWARD AND AT SIDE STRINGERS 26 - 27R. MAINTENANCE COMPLIED WITH ECTC EA 42-2017-015.

Part: SKIN — CORRODED (BS 969-1000) · airframe 31,321 hrs · 22,517 cycles

CORROSION ON LOWER SKIN AROUND RIVETS FROM BS 969 TO 1000, STR 27. REMOVED CORROSION. MEASURED THICKNESS OF SKIN AND PERFORMED EDDY CURRENT. COMPILED WITH EA 25-2017-103, AND EA 25-2017-102.

Part: SKIN — CORRODED (FUSELAGE) · airframe 31,321 hrs · 22,517 cycles

CORROSION JUST BELOW AFT LAVATORY SERVICING PORT. REMOVED CORROSION, PERFORMED A THICKNESS MEASUREMENT AND EDDY CURRENT. COMPLIED WITH EA 43-2017-13, AND EC/TC EA 43-2017-134.

Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 31,321 hrs · 22,517 cycles

STRINGER 26R INTERCOSTAL BS 349 - 364 CORRODED. MAINTENANCE REPLACED THE INTERCOSTAL.

Part: FLOOR SUPPORT — CORRODED (BS 469-485) · airframe 31,321 hrs · 22,517 cycles

RBL 9 FLOOR SUPPORT CORRODED BETWEEN BS 469 AND 485. COMPLIED WITH STS EA 38-2017-138

Part: SEAT TRACK — CORRODED (BS 349-485) · airframe 31,321 hrs · 22,517 cycles

SEAT TRACK ON RBL 9, BETWEEN BS 349 - 485 IS CORRODED OUT OF LIMITS. REMOVED AND REPLACED THE SEAT TRACK, COMPLIED WITH EC/TC REO 670-53-00-343, AND REO 670-53-00-343

Part: ANGLE — CORRODED (BS 939) · airframe 31,321 hrs · 22,517 cycles

WING TO FUSELAGE AFT SUPPORT STRUCTURE AT BS 939 HAS CORROSION AT LOWER FLANGE. REPLACED THE SUPPORT STRUCTURE ANGLE.

Part: STRAP — CORRODED (BS 909) · airframe 31,321 hrs · 22,517 cycles

CENTER FRAME ON WING TO FUSELAGE AFT SUPPORT STRUCTURE AT BS 909 CORRODED AT THE LOWER FLANGE. REPLACED AFT SUPPORT STRUCTURE STRAP.

Part: FLOOR SUPPORT — CORRODED (NOT REPORTED) · airframe 31,321 hrs · 22,517 cycles

CRAWLWAY FLOOR SUPPORT ANGLE CORRODED. MAINTENANCE REPLACED CRAWLWAY FLOOR SUPPORT ANGLE.

Part: THRESHOLD — CORRODED (SERVICE DOORWAY) · airframe 31,321 hrs · 22,517 cycles

SERVICE DOOR THRESHOLD PLATE CORRODED BEYOND 30 PERCENT ON LOWER SURFACE. REPLACED THE SERVICE DOOR THRESHOLD PLATE.

Part: STRINGER — CORRODED (BS 333-349) · airframe 31,321 hrs · 22,517 cycles

STRINGER 25R HAS CORROSION BETWEEN BS 333 - 349. MAINTENANCE REMOVED AND REPLACED THE STRINGER.

Part: DRAG ANGLE — CRACKED (VERTICAL STAB) · airframe 31,321 hrs · 22,517 cycles

RIGHT VERTICAL STAB FWD DRAG ANGLE AFT END CRACKED. COMPLIED WITH ECTC REO 670-55-31-018 REV A.

Part: ANGLE — CRACKED (VERTICAL STAB) · airframe 31,321 hrs · 22,517 cycles

RIGHT VERTICAL STAB AFT DRAG ANGLE FWD END CRACKED. REPLACED THE DRAG ANGLE.

Part: ATTACH FITTING — CRACKED (VERTICAL STAB) · airframe 31,321 hrs · 22,517 cycles

LEFT VERTICAL STAB ATTACHMENT TO FUSELAGE DOUBLER CRACKED. COMPLIED WITH REO 670-55-31-078, REV A.

Part: SMOKE DETECTOR — FAULTY (AFT LAVATORY) · airframe 30,330 hrs · 21,781 cycles

PILOT REPORTED AN AFT LAV SMOKE WARNING MESSAGE DURING APPROACH. APPEARS TO BE A FALSE INDICATION. MX REMOVED AND REPLACED THE SMOKE DETECTOR AND OPS CHECKED GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: WIRE — DISCONNECTED (EMERGENCY LIGHTS) · airframe 28,800 hrs · 20,608 cycles

FWD ENTRY EMERGENCY EXIT LIGHT INOPERATIVE. FOUND LOOSE CONNECTION, SECURED WIRE CONNECTION IAW AMM 33-51-05. OPS CHECK GOOD, NO DEFECTS NOTED.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 27,292 hrs · 19,367 cycles

LEFT EMERGENCY OVERWING LIGHT INOPERATIVE. REPLACED THE LAMP IAW AMM 33-51-15. OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (FLASHLIGHT) · airframe 26,998 hrs · 19,131 cycles

F/A FLASHLIGHT IS NOT WORKING. REPLACED THE FLASHLIGHT BATTERIES IAW GMM 3-8.7.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 26,763 hrs · 18,943 cycles

GALLEY FWD LOWER EXIT SIGN HAD TWO BULBS BURNED OUT. R & R THE BULBS IAW AMM 33-51-05. OPS CHECKED GOOD.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 26,763 hrs · 18,943 cycles

12CD LOWER SIDEWALL EXIT SIGN HAD ONE LIGHT BULB BURNED OUT. R & R THE BULB IAW AMM 33-51-05. OPS CHECKED GOOD.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 26,281 hrs · 18,536 cycles

12CD LOWER EXIT SIGN HAVE ONE LIGHT BULB BURNED. REPLACED BULB IN EXIT SIGN AT 12CD IAW AMM 33-51-11, OPS CHECKED GOOD.

Part: CABLE — WRONG PART (PAX DOOR) · airframe 26,028 hrs · 18,342 cycles

PAX DOOR WILL NOT OPEN, ICE BREAKER GETTING STUCK. FOUND INCORRECT ICE BREAKER CABLE INSTALLED. INSTALLED CORRECT ICE BREAKR CABLE IAW AMM 52-11-15 & IPC 52-11-15. PAX DOOR OPS CHECKS GOOD. NO FURTHER DEFECTS NOTED AT THIS TIME.

Part: SPRING — FAILED (PAX DOOR) · airframe 26,002 hrs · 18,317 cycles

FWD PAX DOOR W/NOT OPEN, DOORS AND OVERWING EMERGENCY EXITS. REPLACED SPRING ON PRSSURE VENT FLAP IAW AMM 52-11-75.

Part: DOOR — OUT OF ADJUST (MAIN PAX) · airframe 25,995 hrs · 18,310 cycles

PAX DOOR WILL NOT OPEN FROM INSIDE OR OUTSIDE. ADJUSTMENT OF RT UPPER PAX DOOR TENSION BUTTON AND NUTPLATE REPLACEMENT.

Part: DOOR — UNKNOWN (MAIN CABIN) · airframe 25,989 hrs · 18,307 cycles

MAIN CABIN DOOR WILL NOT OPEN FROM INSIDE. OPS CHECK PASSENGER DOOR IAW AMM 52-11-00.

Part: PROXIMITY SENSOR — LOOSE (EMERGENCY EXIT) · airframe 25,408 hrs · 17,862 cycles

RT OVERWING EMERGENCY EXIT DOOR FAILS DOOR WARNING OPS TEST. INSPECTED RT OVERWING EMERGENCY EXIT DOOR IAW AMM 52-21-00-820-801 A01 AND 52-21-00-220-801 A01 FOUND THE PROXIMITY SENSOR FITTING TO BE LOOSE. TIGHTENED RT OVERWING EMERGENCY EXIT DOOR PROXIMITY SENSOR FITTING IAW AMM 20-21-00-910-801 A01 FUNCTIONAL TEST GOOD.

Part: BUSHING — UNKNOWN · airframe 25,408 hrs · 17,862 cycles

CONNECTOR, PN CN622-008-007, FAN COWL FWD K BAR FOR N146PQ, LT ENGINE, RV 161789. LT CONNECTOR APPROVED. R & R BUSHINGS IN LT ENGINE K-BAR IAW REO 670-54-22-002. C/W EC/TC FOR INSTALLATION OF BUSHINGS IN ENGINE K-BAR IAW REO 670-54-22-002. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 25,408 hrs · 17,862 cycles

AFT DRAIN MAST AFT AT MOUNT IN FUSELAGE IS DAMAGED. REPAIRED IAW REO 670-53-61-1108.

Part: STRAP — CORRODED (FUSELAGE) · airframe 25,408 hrs · 17,862 cycles

ATTACH STRAP ON L/E OF BELLY PANEL 193AB CORRODED. REMOVED AND REPLACED THE STRAP IAW SRM 51-42-13, 001-001-A01, SRM 51-42-06-001-001-A01 AND DWG CC690-39052.

Part: ANGLE — CRACKED · airframe 25,408 hrs · 17,862 cycles

BS 280 BULKHEAD ANGLE IS CRACKED. REMOVED AND REPLACED THE ANGLE IAW SRM 51-42-06-001-001-A01 AND SRM 51-40-11-001-001-A01.

Part: ANGLE — CORRODED (BS 310-349) · airframe 25,408 hrs · 17,862 cycles

KICKPLATE ANGLE BETWEEN S 310 - 349 IS CORRODED OUT OF LIMITS. REMOVED AND REPLACED THE KICKPLATE ANGLE IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 25,408 hrs · 17,862 cycles

COCKPIT FLOORBEAM ANGLE CRACKED. REPLACED THE ANGLE IAW SRM 51-42-06-001-001-A01.

Part: STRUCTURE — CORRODED (BS 349) · airframe 25,408 hrs · 17,862 cycles

RBL 9 FLOOR PACKER CORRODED AT FS 349. R & R FLOOR PACKER AT FS349 AND RBL 9 IAW SRM 51-42-06-001-001-A01.

Part: FLOORBEAM — CRACKED (COCKPIT) · airframe 25,408 hrs · 17,862 cycles

RT COCKPIT FLOORBEAM CORRODED. REPAIRED IAW SRM 51-42-06-001-001-A01, DWG CC670-33052.

Part: STRUCTURE — CORRODED (BS 333) · airframe 25,408 hrs · 17,862 cycles

RBL 9 FLOOR PACKER CORRODED AT BS 333. R & R FLOOR PACKER IAW SRM 51-42-06-001-001-A01.

Part: BULKHEAD WEB — CORRODED (BS 280) · airframe 25,408 hrs · 17,862 cycles

BULKHEAD WEB BS 280 FOUND CORRODED. REPAIRED IAW REO 670-53-11-954 01 AND GREO 670-53-11-594, REV.

Part: BULKHEAD WEB — CORRODED (BS 280) · airframe 25,408 hrs · 17,862 cycles

BULKHEAD WEB BS 280 FOUND CORRODED. REPAIRED IAW REO 670-53-11-59401 AND GREO 670-53-11-594 REV.

Part: SEAT TRACK — CORRODED (BS 581-677) · airframe 25,408 hrs · 17,862 cycles

SEAT TRACK AT RBL 9 BETWEEN BS 581 - 677 CORRODED. FOUND BEYOND ALLOWABLE LIMITS IAW SRM 53-31-49-101-001-A01. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A03 AND AMM 53-00-49-400-801-A03.

Part: FLOOR SUPPORT — CORRODED (BS 280-319) · airframe 25,408 hrs · 17,862 cycles

RT FLOOR SUPPORT FROM BS 280 - 319 IS CORRODED. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01 AND FOUND OUT OF LIMITS IAW REO 670-53-00-390. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-42-06-001-001-A01 AND 51-42-13-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 611-830) · airframe 25,408 hrs · 17,862 cycles

SEAT TRACK AT LBL 9 BETWEEN BS 611 - 830 CORRODED. FOUND BEYOUND ALLOWABLE LIMITS IAW SRM 53-31-49-101-001-A01. REMOVED AND REPLACED THE SEAT TRACKIAW AMM 53-00-49-000-801A-063 & 53-00-49-400-801-A03, STEPS 4.B, 3, 9-C.

Part: SEAT TRACK — CORRODED (BS 611-830) · airframe 25,408 hrs · 17,862 cycles

SEAT TRACK AT RBL 9 BETWEEN BS 611 - 830 CORRODED. FOUND BEYOND ALLOWABLE LIMITS IAW SRM 53-31-49-101-001-A01. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801A-063 AND AMM 53-00-49-400-801-A03, STEPS 4.B, 3, 9-C.

Part: FLOOR SUPPORT — CORRODED (BS 310-349) · airframe 25,408 hrs · 17,862 cycles

FLOOR SUPPORT BS 310 - 349 FOUND CORRODED . REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-42-000-001-001-A01, 51-42-21-001-001-A01 AND 51-41-02-001-001-A01.

Part: FLOOR SUPPORT — CORRODED (BS 319-349) · airframe 25,408 hrs · 17,862 cycles

FLOOR SUPPORT BS 319 - 349 FOUND CORRODED. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01 AND FOUND TO BE OUT OF LIMITS IAW SRM 53-21-23-101-002-A01. REPLACED THE FLOOR SUPPORT IAW SRM 51-40-11-001-001-A01.

Part: SKIN — CORRODED (BS 280) · airframe 25,406 hrs · 17,861 cycles

SKIN BS 280 S27 CORRODED . REMOVED CORROSION IAW SRM 51-21-06-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 485-581) · airframe 25,408 hrs · 17,862 cycles

SEAT TRACK AT RBL 9 BETWEEN BS 485 - 581 CORRODED. FOUND BEYOND ALLOWABLE LIMITS IAW SRM 53-31-49-101-001-A01. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A03 AND AMM 53-00-49-400-801-A03.

Part: SEAT TRACK — CORRODED (BS 349) · airframe 25,406 hrs · 17,861 cycles

SEAT TRACK SEGMENT IS CORRDOED BEYOND LIMITS AT BS 349. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A02.

Part: SEAT TRACK — CORRODED (BS 581-677) · airframe 25,408 hrs · 17,862 cycles

SEAT TRACK AT LBL 9 BETWEEN BS 581 - 677 CORRODED. FOUND SKIN BEYOUND ALLOWABLE LIMITS IAW SRM 53-31-49-101-001-A01. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801A-063 AND AMM 53-00-49-400-801-A03, STEPS 4.B, 3,9-C.

Part: SKIN — CORRODED (FUSELAGE) · airframe 25,406 hrs · 17,861 cycles

FUSELAGE SKIN UNDER AFT DRAIN MAST FOUND TO BE CORRODED. BLENDED DAMAGE IAW SRM 51-21-06-001-001. REPAIRED IAW EA 32-2014-208. MAJOR REPAIR.

Part: FRAME — CORRODED (BS 250) · airframe 25,408 hrs · 17,862 cycles

FRAME BS 250 S27 CORRODED. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01.

Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 25,406 hrs · 17,861 cycles

CENTER RT LATCH PIN INTERCOSTAL BETWEEN BS 349 - 364 CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-21-23-101-003-A01. REMOVED AND REPLACED IAW SRM 51-42-21-001-001-A01 51-42-06-001-001-A01 AND DWG SH670-32075. MAJOR REPAIR.

Part: FLOOR PANEL — CRACKED (E/E BAY) · airframe 25,406 hrs · 17,861 cycles

LT SIDE FWD EQUIP BAY FLOOR PANEL CRACKED. REPAIRED IAW REO 670-53-11-509 AND GREO670-53-11-509. REV B. MAJOR REPAIR.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 25,408 hrs · 17,862 cycles

AFT DRAIN MAST AFT RT MOUNT IN FUSELAGE IS DAMAGED. REPAIRED IAW REO 670-53-61-1108

Part: BATTERY — INOPERATIVE (MEGAPHONE) · airframe 24,631 hrs · 17,266 cycles

CABIN MEGAPHONE NOT WORKING. RESEATED AND SECURED LOOSE BATTERIES.

Part: CIRCUIT BOARD — FAILED (EMERGENCY LIGHTS) · airframe 23,654 hrs · 16,539 cycles

EMERGENCY LIGHTS CYCLE ON AND OFF WITH EMERGENCY LIGHTS SWITCH IN THE ARM POSITION R & R PRINTED CIRCUIT BOARD ASSY JB-11, PCB5, IAW AMM 24-06-11, IPC 24-06-11 ITEM 40, OPS CHECK GOOD. PN ON AND OFF E520005-705A, SN ON E0102, SN OFFE0250.

Part: SAFETY VALVE — FAILED (NR 2) · airframe 23,654 hrs · 16,539 cycles

CABIN ALT CAUTION MESSAGE AT FL 340. FOLLOWED QRH. UNABLE TO CONTROL CABIN PRESSURE, DIVERTED EMERGENCY DECLARED. INTEGRATED MDC. SAFETY VALVE 2 POSTED. R & R NR 2 SAFETY VALVE & OPS CHECKED GOOD IAW AMM 21-32-03, REF AIPC 21-32-03, ITEM 5.

Part: UNKNOWN — ODOR (CABIN) · airframe 21,802 hrs · 15,175 cycles

STRONG ODOR LIKE BURNING RUBBER, REPORTED BY F/A AND PAX, ONCE DURING FLIGHT, THEN ON APPROACH AS FLAPS DEPLOYED TO 8 AND 45. ODOR ONLY IN FIRST CLASS CABIN. COULD NOT DUPLICATE BURN LIKE ODOR, RAN LT & RT PACKS WITH APU IAW AMM 21-51-00. NO DEFECTS NOTED. RAN ENGINES IAW AMM 71-00-00 AND ISOLATED, TRYING TO DUPLICATE ALSO, OPS TESTED FLAPS AND SLATS IAW AMM 27-52-00 TO DUPLICATE WRITE UP NO DEFECTS NOTED, COCKPIT AND CABIN ODOR NORMAL. ACFT OK FOR SERVICE AT THIS TIME.

Part: UNKNOWN — ODOR (CABIN) · airframe 21,071 hrs · 14,670 cycles

BURNING RUBBER OR CHEMICAL ODOR REPORTED IN CABIN DURING FLIGHT. COMPLIED WITH SL-21-028, NO DEFECTS NOTED.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 20,609 hrs · 14,335 cycles

SEVERAL EMERGENCY LIGHTS INOPERATIVE. R & R BATTERY PACK IAW AMM 33-51-17-000-801 AND 35-51-17-400-801. PERFORMED OPS TEST OF THE EMERGENGY POWER SUPPLY UNIT IAW AMM 33-51-17-710-801. OPS CHECKED GOOD.

Part: GLOWSTRIP — DAMAGED (CABIN) · airframe 20,609 hrs · 14,335 cycles

FOUND GLOWSTRIP DAMAGED BETWEEN ROWS 15-17. REMOVED AND INSTALLED NEW GLOWSTRIP BETWEEN ROWS 15-17 IAW AMM 33-51-01-000-801 (A04) AND 33-51-01-400-801 (A04) NO DEFECTS NOTED.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 20,609 hrs · 14,335 cycles

LOWER SILL ANGLE CORRODED, GALLEY SERVICE DOOR SURROUND. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-21-23-101-001-A01. REMOVED LOWER SILL ANGLE IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01. INSTALLED NEW SILL ANGLE IAW SRM 51-42-06-001-001-A01 AND DWG SH670-31950. REPAIR CLASSIFIED AS MAJOR REPAIR. FOUND TO BE SATISFACTORY.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 20,609 hrs · 14,335 cycles

CORROSION FOUND ON SILL ANGLE. BLENDED CORROSION AND FOUND ARE OUT OF LIMITS IAW SRM 53-21-23-001-002-A01. LOCATED AND DRILLED AND INSTALLED IAW SRM 51-40-06-001-001-A01 AND 51-42-06-001-001-A01 AND DWG SH670-31950. REPAIR CLASSIFIED AS MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (BS 349-355) · airframe 20,590 hrs · 14,320 cycles

SEAT TRACK AT RBL 9 FS 349 TO 355 CORRODED. R & R SEAT TRACK IAW AMM 53-00-49-000-801 AND AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 844-879) · airframe 20,590 hrs · 14,320 cycles

SEAT TRACK AT RBL 9 FS 844 TO 879 CORRODED. R & R SEAT TRACK IAW AMM 53-00-49-000/400-801.

Part: SILL — CORRODED (BS 310-319.7) · airframe 20,609 hrs · 14,335 cycles

CORROSION ON SILL PLATE, RT SIDE FS 310 TO 319.7. FOUND TO BE OUT OF LIMITS, R & R FOUND TO BE SASTISFACTORY.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 20,590 hrs · 14,320 cycles

FLOORBEAM ANGLE FOR CRAWLWAY FLOOR PANEL 141ALF AT FS 280 CORRODED. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. REMAINING MATERIAL THICKNESS IN 3 AREAS BEYOND LIMITS OF SRM 53-00-00-101-001. INSTALLED SEVICEABLE FLOORBEAM ANGLE IAW SRM 51-42-21-001-001-A01, 51-42-13-001-001-A01, 51-42-00-001-001-A0.

Part: FLOOR SUPPORT — CORRODED (BS 349-364) · airframe 20,590 hrs · 14,321 cycles

CORROSION ON RT FLOOR SUPPORT FS 349 TO 364. REMOVED CORROSION IAW SRM 51-21-06-001-01-A01. REMAINING MATERIAL THICKNESS OUT OF LIMITS IAW SRM 53-00-00-101-001-A01. CUT AWAY DAMAGED FLOOR SUPPORT ONLY AS SHOWN IAW REO 670-53-21-899. FOUND TO BE SATISFACTORY.

Part: SEAT TRACK — CORRODED (BS 785) · airframe 20,590 hrs · 14,320 cycles

RT SIDE WALL SEAT TRACK CORRODED AT FS 785. REMOVED CORRODED SEAT TRACK AND REPLACED WITH NEW ONE IAW AMM 53-00-49-000-801(A03) AND 53-00-49-400-801(A03).

Part: SEAT TRACK — CORRODED (BS 477.4-500) · airframe 20,590 hrs · 14,320 cycles

SEAT TRACK AT LBL 9, 477.4 TO 500 HAS CORROSION. AREA FOUND TO BE OUT LIMITS IAW 53-31-49-101-001-A01. REMOVED SEAT TRACK IAW 53-31-49-000-801-A01. INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-801-A03.

Part: SEAT TRACK — CORRODED (BS 280-477.4) · airframe 20,590 hrs · 14,320 cycles

SEAT TRACK AT LBL 9, FS 280 TO 477.4 HAS CORROSION ENTIRE LENGTH. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801 (CONFIG A03). INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-801-A03.

Part: STRIKER — CORRODED (FUSELAGE) · airframe 20,590 hrs · 14,321 cycles

SEAL STRIKER PLATE ON GALLEY SERVICE DOOR SURRROUND HAS CORROSION ON M INBD SURFACE AT WL71.970 BETWEEN FS319.70 AND FS349. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-21-23-101-001-A01. REMOVED SEAL STRIKER PLATE IAW SRM 51-42-06-001-001-A01. INSTALLED NEW SEAL STRIKER PLATE IAW SRM 51-42-06-001-001-A01 AND DWG SH670-31950. REPAIR CLASSIFIED AS MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 20,590 hrs · 14,320 cycles

RT SIDE FS 280 FLOORBEAM HAS CORROSION DAMAGE. CORRODED BEYOND LIMITS IAW SRM 53-00-00-101-001-A01. REMOVED AND REPLACED FLOORBEAM. COMPLIED WITH REO 670-53-11-047, REV E DATED 08/13/2009. FOUND TO BE SATISFACTORY.

Part: FLOOR SUPPORT — CORRODED (BS 1030) · airframe 20,590 hrs · 14,320 cycles

RT FLOOR SUPPORT IS CORRODED AT NUTPLATE POSITION FS 1030.00. REMOVED SURFACE CORROSION IAW MM 670-35404-003. DAMAGE DIMESIONS 1"X1.5"X.002" DEEP O .063" - 061" REMAINING. NO DAMAGE ALLOWED IAW SRM 53-61-43-101-001. COMPLIED WITH REO 670-53-61-916. FOUND TO BE SATSIFACTORY.

Part: BULKHEAD — CORRODED (BS 280) · airframe 20,590 hrs · 14,320 cycles

RIGHT SIDE SKID FS 280 BULKHEAD LOWER WEB CORRODED. CORRODED BEYOND LIMITS IAW SRM 53-11-10-201-003-A01. NDT NEW BULKHEAD LOWER WEB IAW REO 670-53-11-594. FOUND TO BE SATISFACTORY.

Part: FLOOR SUPPORT — CORRODED (BS 1048) · airframe 20,590 hrs · 14,321 cycles

LEFT FLOOR SUPPORT CORRODED AT NOT PLATE LOCATION JUST AFT OF CARGO DOOR FS 1048. REMOVED CORROSION, .002 MATERIAL. REMOVED WITH .061 REMAINING IAW SRM 51-21-06-001-001-A01 JUST AFT OF CARGO DOOR FS 1048. COMPLIED WITH REO 670-53-61-915. FOUND TO BE SATISFACTORY.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 20,590 hrs · 14,320 cycles

FWD FLOORBEAM ANGLE AT FS 280 HAS CORROSION DAMAGE. REMOVED FWD FLOORBEAM ANGLE. LOCATED AND DRILLED FWD FLOORBEAM ANGLE IAW SRM 51-42-06-001-001. REPLACED FWD FLOORBEAM ANGLE IAW SRM 51-42-06 AND 51-42-21.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 20,590 hrs · 14,320 cycles

LT SIDE FS 280 FLOORBEAM HAS CORROSION DAMAGE. CORROSION IS BEYOND REPAIRABLE LIMITS IAW SRM 53-00-00-101-001-A01. R & R FLOORBEAM. COMPLIED WITH REO 670-53-11-047, REV E DATED 08/13/2009. FOUND TO BE SATISFACTORY.

Part: SILL — CORRODED (CARGO DOORWAY) · airframe 20,590 hrs · 14,321 cycles

AFT CARGO DOOR SILL INBD FACE CORRODED AT 4 LOCATIONS AS MARKED BETWEEN FS 1000.00 TO FS 1045.00. REMOVED CORROSION ON AFT CARGO DOOR SILL AT 4 LOCATIONS WITH .008 BEING THE DEEPEST IAW SRM 51-21-06-001-001-A01. COMPLIED WITH REO 670-53-61-915. FOUND TO BE SATISFACTORY.

Part: FLOOR SUPPORT — CRACKED (E/E BAY) · airframe 20,590 hrs · 14,320 cycles

FWD EQUIPMENT COMPARTMENT FLOOR SUPPORT NEXT TO ADG PUMP BETWEEN FUSELAGE SKIN AND FRAME (FS 193) IS CRACKED. COMPLIED WITH REO 670-53-11-509 ON FWD E & E BAY FLOOR TYPE 2 REPAIR. FOUND TO BE SATISFACTORY. S

Part: SILL — CORRODED (SERVICE DOORWAY) · airframe 20,590 hrs · 14,321 cycles

GALLEY SERVICE DOOR FRAME SILL IS CORRODED FROM THE FWD DOOR FRAME TO THE AFT DOOR FRAME. MOUNTING ANGLE CORROSION FOUND TO BE OUT OF LIMITS. REMOVED OLD MOUNTING ANGLE IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01. INSTALLED NEW MOUNTING ANGLE IAW SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01 AND DWG SH670-31950. REPAIR CLASSIFIED AS MAJOR REPAIR.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 20,590 hrs · 14,320 cycles

PAX DOOR AFT SIDE RISER PANEL DRAG ANGLE CRACKED AT CENTER. REMOVED DRAG ANGLE IAW SRM 51-42-06-001-001-A01. INSTALLED NEW REPAIR PARTS DRAG ANGLE IAW SRM 51-11-04-201-002-A01.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 20,297 hrs · 14,101 cycles

F/O FLASHLIGHT INOPERATIVE. REPAIRED F/O FLASHLIGHT IAW AMM 25-61-02.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 20,297 hrs · 14,101 cycles

F/A FLASHLIGHT INOPERATIVE. R & R THE FWD F/A FLASHLIGHT IAW AMM 33-21-12. OPS CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 20,297 hrs · 14,101 cycles

F/A FLASHLIGHT INOPERATIVE. REPAIRED IAW AMM 25-61-02, OPS CHECKED GOOD.

Part: DOOR — LACK OF LUBE (MAIN PAX) · airframe 19,776 hrs · 13,707 cycles

FORWARD PASSENGER DIFFICULT TO OPEN. REMOVED EXCESS LUBRICATION AND OPS CHECKED PAX DOOR IAW AMM 5-11-01. OPS CHECKED GOOD.

Part: MEGAPHONE — UNSERVICEABLE (CABIN) · airframe 19,716 hrs · 13,660 cycles

MEGAPHONE HAS MISSING NUTPLATE AND WILL NOT STAY TOGETHER. R & R MEGAPHONE IAW AMM 25-61-14. IPC REF 25-61-14, FIG 1C ITEM 5. OPS CHECKED GOOD.

Part: COVER — BROKEN (EMERGENCY LIGHT) · airframe 19,235 hrs · 13,322 cycles

EMERGENCY LIGHT AT PAX DOOR HAS BROKEN COVER. R & R COVER ASSY IAW AMM 33-51-11. OPS CHECKED GOOD.

Part: ACTUATOR — FAILED (RUDDER) · airframe 19,003 hrs · 13,157 cycles

IN CRUISE FLIGHT, AUTOPILOT ENGAGED, RECEIVED UNCOMMANDED RUDDER INPUTS (YD 1 WAS DEFFERRED AT THE TIME) INPUTS WERE LT AND RT OF CENTER AND NEEDED FULL RUDDER DEFLECTION AT TIMES TO COUNTER THE DEFLECTION. DECLARED AN EMERGENCY AND LANDED. R & R YAW DAMPER LINEAR ACTUATOR NR 2 IAW AMM 22-22-01. OPS CHECKED GOOD.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 17,235 hrs · 11,907 cycles

EXIT SIGN MISSING F/A GALLEY AREA. GALLEY AREA EXIT SIGN LENS FOUND AND INSTALLED AMM 33-51-00,

Part: STRUCTURE — CORRODED (BS 349-364) · airframe 16,727 hrs · 11,555 cycles

CORROSION IN BELLY OF FUSELAGE IN AV BAY BETWEEN FS 349 AND 364 BETWEEN STR 25L AND 26L. REPAIRED IAW REO 670-53-21-662.

Part: CROSSBEAM — CORRODED (BS 280) · airframe 16,727 hrs · 11,555 cycles

FS 280 CROSSBEAM CORRODED. INSTALLED CROSSBEAM REF SRM 51-42-13-001-001

Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 16,727 hrs · 11,555 cycles

CORROSION ON INTERCOSTAL ON 26L AT FS 349 TO FS 364 ON LT SIDE OF INTERCOSTAL. REMOVED INTERCOSTAL IAW SRM 51-42-06, INSTALLED NEW INTERCOSTAL IAW SRM 51-42-06-001-001.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 16,727 hrs · 11,555 cycles

FLOOR PANEL 141ALF FORWARD SUPPORT ANGLE AT FS 280 IS CORRODED. REMOVED PANEL 161ALF IAW SRM 51-41-02. OK TO INSTALL, INSTALLED PNL 131ALF IAW SRM 51-41-02. REMOVED CORRODED SUPPORT ANGLE FROM FRAME AT FS 280 LBL 9 TO RBL 9 IAW SRM 51-42-06. LOCATED,DRILLED AND INSTALLED NEW SUPPORT ANGLE IAW SRM 51-420-11, 51-42-06, 51-42-21, AND 51-25-16. THIS IS A MINOR REPAIR. (CLOSED)

Part: DRAG ANGLE — CRACKED (VERTICAL STAB) · airframe 16,727 hrs · 11,555 cycles

LEFT VERTICAL STAB DRAG ANGLE CRACKED AT AFT END. COMPLIED WITH EC/TC REO 670-55-31-018 IAW REO 670-55-31-018.

Part: CROSSBEAM — CORRODED (BS 280) · airframe 16,727 hrs · 11,555 cycles

FS 280 CROSSBEAM CORRODED. BLENDED CORROSION ON FS 280 BEAM FOUND TO BE OUT OF LIMITS SRM 51-12-00-001-001-A01 AND SRM 53-00-00-001-001-A01. R & R FS 280 CROSSBEAM IAW SRM 51-42-06-001-001 AND 51-42-21-001-001 AND 51-42-13-001-001.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 16,727 hrs · 11,555 cycles

FS 280 FORWARD FLOORBEAM ANGLE IS CORRODED OUT OF LIMITS SRM 53-00-00-101-001-A01. REMOVED FS 280 FWD FLOORBEAM ANGLE PER SRM'S 51-42-21-001-001-A01 AND 51-42-22-001-001-A01. INSTALLED FS 280 FWD FLOORBEAM ANGLE IAW SRM'S 51-42-06-001-001-A01 & 51-42-21-001-001-A01. THIS IS A MINOR REPAIR.

Part: DRAG ANGLE — CRACKED (VERTICAL STAB) · airframe 16,727 hrs · 11,555 cycles

LEFT VERTICAL STAB DRAG ANGLE CRACKED AT AFT END. PERFORMED EDDY CURRENT INSP ON LT SIDE FWD VERTICAL STAB DRAG ANGLE IAW NDT INSP PROCEDURES ET-2. VERIFIED DRAG ANGLE IS CRACKED AT AFT ENG. CRACK IS .65IN IN LENGTH. CUT AND REMOVED DAMAGE AT LT VERTICAL STAB DRAG ANGLE AND REMOVED BURRS IAW STEPS 1 AND 2 OF REO 670-55-31-018. PERFORMED EDDY CURRENT INSP, STEP (3) OF REO 670-55-31-018 IAW NDTM PT 1, 51-20-006-250-A01. NO CRACK NOTED AT THIS TIME. FABRICATED REPAIR DOUBLER AND FILLER, CORROSION TREAT AND PRIMER IAW REO670-55-31-018. FABRICATED A REPAIR DOUBLER AND FILLER, CORROSION TREATED AND PRIMED IAW REO 670-55-31-018. INSTALLED REPAIR IAW REO 620-55-31-018.

Part: FLOOR SUPPORT — CORRODED (BS 985-1015) · airframe 16,727 hrs · 11,555 cycles

CORROSION ON FLOOR SUPPORT ON RIGHT SIDE OF AFT CARGO BAY BETWEEN FS 985.00 AND FS 1015. BLENDED CORROSION ON RT FLOOR SUPPORT SILL IAW SRM 51-21-06-001-001-A01. PERFORMED UT THICKNESS INSPECTION OF BLEND AREA IAW NDT INSP PROCDURE UT-3 MIN. MATERIAL REMAINING IS .062". COMPLIED WITH STEP 2 OF REO 670-53-61-704 NO INDICATIONS NOTED AT THIS TIME. COMPLY WITH STEPS 3 & 4 OF REO 670-53-61-704. COMPLIED WITH STEPS 3 & 4 OF REO 670-53-61-704.

Part: SEAT TRACK — CORRODED (BS 394-485) · airframe 16,727 hrs · 11,555 cycles

SEAT TRACK HAS CORROSION BETWEEN FS 394.00 AND - FS 485.00, RBL 9.00. CHECKED THICKNESS FOUND TO BE OUT OF LIMITS IAW REO 670-53-00-013. INSTALL SERVICABLE SEAT TRACK FROM FS350-485, RBL9.0 IAW AMM 53-00-49-400-801-A03. INSTALLED SERVICABLE SEAT TRACK AT RBL 9.0 FROM FS .350-485. IAW AMM 53-00-49-400-801-A03. REO 670-53-00-013 NOT USED SEAT TRACK WAS REPLACED.

Part: SEAT TRACK — CORRODED (BS 581-677) · airframe 16,727 hrs · 11,555 cycles

SEAT TRACK HAS CORROSION BETWEEN FS 581.00 - FS 677.00, LBL 9.00. CHECKED MATERIAL THICKNESS FOUND TO BE OUT OF LIMITS IAW SRM 53-31-49-101-001-A01. INSTALL SERVICABLE SEAT TRACK FROM FS 581-683.5, LBL9.0 IAW AMM 53-00-49-400-801-A03. INSTALLED SERVICABLE SEAT TRACK LBL9.0 FROM FS 581-683.5, IAW AMM 53-00-49-400-801-A03.

Part: SEAT TRACK — CORRODED (BS 677-693) · airframe 16,727 hrs · 11,555 cycles

SEAT TRACK HAS CORROSION BETWEEN FS 677.00 - FS 693.00, RBL 9.00. CHECKED THICKNESS FOUND TO BE OUT OF LIMITS IAW SRM 53-31-49-101-001-A01. INSTALLED SERVICABLE SEAT TRACK IAW AMM 53-00.

Part: SEAT TRACK — CORRODED (BS 677-693) · airframe 16,727 hrs · 11,555 cycles

SEAT TRACK HAS CORROSION BETWEEN FS 677.00-FS 693.00, LBL 9.00. AFTER FURTHER INSPECTION FOUND SEAT TRACK TO BE DAMAGED OUT OF LIMITS IAW SRM 53-41-49-101-001-A01. REMOVED SEAT RAIL AT FS 677.00, LBL 93.00 IAW AMM 53-00-49-000-801. INSTALLED NEW SEAT RAIL IAW AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 485-581) · airframe 16,727 hrs · 11,555 cycles

SEAT TRACK HAS CORROSION BETWEEN FS 485.00 - FS 581.00, RBL 9.00. REMOVED AND REPLACED CORRODED SEAT TRACK IAW AMM 53-00-49-000-801.

Part: SEAT TRACK — CORRODED (BS 581-677) · airframe 16,727 hrs · 11,555 cycles

SEAT TRACK HAS CORROSION BETWEEN FS 581.00 - FS 677.00, RBL 9.00. CHECKED MATERIAL THICKNESS FOUND TO BE OUT OF LIMITS IAW SRM 53-31-49-101-001-A01. INSTALLED SERVICABLE SEAT TRACK IAW AMM 53-00-49-400-801-A03.

Part: FLOOR SUPPORT — CORRODED (BS 280) · airframe 16,727 hrs · 11,555 cycles

FLOOR SUPPORT ANGLE AT FS 280.00 CORRODED. [OPEN]

Part: SKIN — CORRODED (BS 349-364) · airframe 16,727 hrs · 11,555 cycles

CORROSION IN BELLY OF FUSELAGE IN AVIONIC BAY BETWEEN FS 364 AND 349 BETWEEN ST 26 AND 27L. REPAIRED IAW SRM 51-71-12-001-001.

Part: SKIN — CORRODED (BS 310-317) · airframe 16,727 hrs · 11,555 cycles

CORROSION IN BELLY OF FUSELAGE IN AVIONIC BAY BETWEEN FS 310 AND 317 BETWEEN STR 26 AND 27L. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. ALODINE, PRIMED AND PAINTED AREA IAW SRM 51-42-06-001-001 AND SRM 51-21-11-001-001.

Part: SKIN — CORRODED (BS 295-310) · airframe 16,727 hrs · 11,555 cycles

CORROSION IN BELLY OF FUSELAGE IN AVIONIC BAY BETWEEN FS 295 AND 310 S27R. REMOVED CORROSION IAW SRM 51-42-06-001-001.

Part: SKIN — CORRODED (BS 349-364) · airframe 16,727 hrs · 11,555 cycles

CORROSION IN BELLY OF FUSELAGE IN AVIONIC BAY BETWEEN FS 349 AND 364 BETWEEN STR 25 AND 26L. BLENDED OUT DAMAGE IAW SRM 57-12-00 CUT AND REMOVED DAMAGED FRAME SECTION IAW STEP 1 OF REO 670-53-21-662, P1. REPAIRED IAW REO 670-53-21-662.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 16,438 hrs · 11,350 cycles

SERVICE DOOR EXIT SIGN COVER MISSING. FOUND EXIT SIGN COVER, RESECURED EXIT SIGN. OPS CHECK GOOD REF AMM 33-51-05. (CLOSED)

Part: RELAY — INTERMITTENT (EMERGENCY LIGHTS) · airframe 16,184 hrs · 11,177 cycles

EMERGENCY LIGHT ACTIVATING ON AND OFF STATUS MESSAGE. R & R RELAY K135 IN JB-11, IAW AMM 24-06-11, OPS CHECK GOOD.

Part: LIGHT — DISCONNECTED (CABIN) · airframe 14,726 hrs · 10,095 cycles

CABIN EMERGENCY LIGHT IN CEILING FIRST LIGHT DOES NOT ILLUMINATE WHEN TESTED. FOUND EMERGENCY LIGHT TO BE DISCONNECTED. RECONNECTED FWD CEILING EMERGENCY LIGHT IAW AMM 33-51-05. OPS CHECK GOOD. DEFER CLEARED. PLACARD REMOVED.

Part: LIGHT — DISCONNECTED (CABIN) · airframe 14,726 hrs · 10,095 cycles

REF DMIL 531871-1 CEILING EMERGENCY LIGHT INOPERATIVE, FOUND EMERGENCY LIGHT TO BE DISCONNECTED. RECONNECTED FWD CEILING EMERGENCY LIGHT IAW AMM 33-51-05. OPS CHECK GOOD. DEFER CLEARED. PLACARD REMOVED.

Part: TRIM SYSTEM — MALFUNCTIONED (STABILIZER) · airframe 12,271 hrs · 8,269 cycles

RECEIVED STAB CHA1 INOP MSG, 10 MINS LATER RECEIVED TRIM RUNAWAY AURAL WARNING. DISCONNECTED STAB TRIM [EMERGENCY DECLARED]. FLT 5015 CX.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 11,833 hrs · 7,942 cycles

WORK ORDER 50921 ZONE 1000 ITEM 13 280 FLOOR SUPPORT BEAM CORRODED AT RBL 9.0 AND LBL 9.0.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 11,827 hrs · 7,937 cycles

AAR 2000-0014 RBL9 SEAT TRACK AT FS 349.00 HAS POWDER CORROSION. REMOVED CORROSION & FOUND OUT LIMITS. INSTALLED NEW SEAT TRACK IAW SERM 51-41-02

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 11,032 hrs · 7,339 cycles

G2 GALLEY EMERGENCY LIGHT HAS SEVERAL INOP BULBS.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 11,032 hrs · 7,339 cycles

RT OVERWING EMERGENCY EXIT LOWER EMERGENCY LIGHT HAS SEVERAL INOP BULBS.

Part: UNKNOWN — ODOR (CABIN) · airframe 10,551 hrs · 6,977 cycles

BOTH FAS COMPLAINED OF A STRONG FUEL ODOR DURING FLIGHT. IN AFT CABIN AFT OF ROW 14. RAN APU BOTH A/C PACKS AND FUEL PUMP SYSTEMS NO DEFECTS NOTED REF CRJ-700MM 21-51-00 28-23-02.

Part: FUEL CAP — UNSECURE (FUEL TANK) · airframe 8,811 hrs · 5,740 cycles

FUEL CAP LEFT OFF IN FLT, PERFORMED AIR RETURN LANDED AT 72000 LBS. EMERGENCY DECLARED.

Part: PLACARD — TORN (AIRSTAIR DOOR) · airframe 8,680 hrs · 5,644 cycles

EXIT STICKER ON AIRSTAIR DOOR IS TORN.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 7,409 hrs · 4,811 cycles

FS 280 FWD CENTER FLOOR SUPPORT ANGLE CRACKED. COMPLIED WITH INSPECTION OF THE PRESSURIZATION SYSTEM MANUAL MADE MORTOR AND ALTITUDE LIMITATION IAW PART A OF BOMBARDIER ALERT SERVICE BULLETIN A670BA-21-022. NO DEFECTS FOUND.

Part: WEB — CORRODED (FUSELAGE) · airframe 7,409 hrs · 4,811 cycles

LEFT LOWER FS 280 WEB HAS CORROSION. [07-31-07] CORROSION FOUND TO BE OUT OF LIMITS, REPLACED OF LT LOWER FS 280 WEB PER REO 670-53-11-052.

Part: CROSSBEAM — CRACKED (FUSELAGE) · airframe 7,409 hrs · 4,811 cycles

RIGHT FS 280 CROSSBEAM CRACKED ON UPPER FLANGE O/B OF RBL 9.0. [07-31-07] REPAIRED IAW MODSUM IS67053110026.

Part: WEB — CORRODED (FUSELAGE) · airframe 7,409 hrs · 4,811 cycles

RIGHT LOWER FS 280 WEB HAS CORROSION. [07-31-07] CORROSION FOUND TO BE OUT OF LIMITS PER: REO 670-53-11-052, REPAIRED IAW THE SAME EO.

Part: CROSSBEAM — CRACKED (FUSELAGE) · airframe 7,409 hrs · 4,811 cycles

LEFT FS 280 CROSSBEAM CRACKED ON UPPER FLANGE O/B OF LBL 9.0. COMPLIED WITH E.O. 700-53-0058 REV A.

Part: LIGHT — INOPERATIVE (RT OVERWING) · airframe 6,193 hrs · 3,991 cycles

RIGHT OVERWING AFT EMERGENCY LIGHT IS INOP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 4,828 hrs · 3,136 cycles

2 FWD EMER LIGHTS ON OUTSIDE OF A/C.