N907EV

Part: SENSOR — OUT OF ADJUST (MLG) · airframe 35,427 hrs · 32,704 cycles

GEAR DISAGREE AND NOSE GEAR DOOR WARNING MESSAGES. ADJUSTED THE SENSOR IAW AMM 32-61-00. NO OTHER DEFECTS NOTED. ACFT OK FOR SERVICE.

Part: BRACKET — FAILED (NLG SENSOR) · airframe 34,694 hrs · 32,008 cycles

GEAR DISAGREE MESSAGE. RETURN TO FIELD. INSTALLED NLG CENTERING SENSOR BRACKET IAW AMM ANC FMM. RETRACTION & EXTENSION CYCLE OF MLG GOOD. OPS CHECKED GOOD.

Part: SWITCH — FAILED (YOKE TRIM) · airframe 33,949 hrs · 31,260 cycles

MACH AND STAB TRIM CAUTION MESSAGES DURING CLIMB OUT, WOULD NOT REENGAGE, AUTOPILOT PITCH WOULD NOT ENGAGE. DECLARED EMERGENCY. REPLACED CA YOKE TRIM DISCONNECT SWITCH IAW AMM. OPS CHECKED GOOD. MACH & STAB TRIM & AUTO PILOT PITCH TRIM OPERATE NORMALLY.

Part: SKIN — CHAFED (RT WING) · airframe 33,831 hrs · 31,124 cycles

LOWER RT WING PLANK IS CHAFED AT RBL 45 AND T/E 1.000" X 4.000" X APPROXIMATELY .040" DEEP. REPAIRED THE WING PLANK IAW REO.

Part: STRUCTURE — CRACKED (RT WING) · airframe 33,831 hrs · 31,124 cycles

INDICATION NOTED AT RT WING BL5 WATER DRAIN FWD SCREW HOLE. REPAIRED IAW REO.

Part: SKIN — DENTED (VERTICAL STAB) · airframe 33,831 hrs · 31,124 cycles

LEFT VERTICAL STAB HAS ONE DENT 10 INCHES FROM T/E AND JUST ABOVE THE NR 2 RIB. REPAIRED VERTICAL STAB IAW REO.

Part: ANGLE — CORRODED (PAX DOOR) · airframe 33,831 hrs · 31,124 cycles

PAX DOOR LOWER MOUNTING ANGLE CORRODED IN MULTIPLE LOCATIONS. REMOVED AND REPLACED THE ANGLE IAW SRM.

Part: FLOOR SUPPORT — CORRODED (BS 310) · airframe 33,831 hrs · 31,124 cycles

LEFT FLOOR SUPPORT CORRODED AT BS 310, LBL 36. REMOVED CORROSION IAW SRM.

Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 33,831 hrs · 31,124 cycles

REAR PRESSURE BULKHEAD WEB HAS MULTIPLE INDICATIONS NOTED 1) LBL9.5 WL 134 APPROX 3 INCHES LONG 60%FSH 2) RBL9.5 WL 134 APPROX 2 INCHES LONG 50%FSH 3) RBL18 WL 134 4 INCHES LONG 90%FSH 4) RBL27.50 WL 134 APPROX 1 INCH 50% FSH 5) RBL27.50 WL111 APPROX 5 INCHES LONG 60%FSH & 6) RBL18 WL 102 APPROX 3 INCHES 50%FSH ALL 6 FAILED NDT INSPECTION. REPAIRED THE BS 621 REAR PRESSURE BULKHEAD IAW REO.

Part: SKIN — DENTED (BS 656) · airframe 33,831 hrs · 31,124 cycles

EXTERNAL FUSELAGE SKIN DENTED, BS 656 BETWEEN STRINGERS 26 AND 27R. REPAIRED THE SKIN IAW REO.

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 33,831 hrs · 31,124 cycles

RT INBOARD FLAP HAS A DENT ON THE LOWER SKIN INBOARD SIDE. REPAIRED THE FLAP SKIN IAW REO.

Part: SKIN — GOUGED (BS 589-602) · airframe 33,831 hrs · 31,124 cycles

THE SKIN HAD SEVERAL SMALL NICKS AND GOUGES FROM BS 589 TO 605 BETWEEN STRINGER 21R & 23R. REPAIRED THE SKIN IAW SRM.

Part: PANEL — DAMAGED (NOT REPORTED) · airframe 33,831 hrs · 31,124 cycles

TWO OVERSIZED HOLES IN PANEL 131AL. REPAIRED TWO OVERSIZED HOLES IN PANEL 131AL AT 10 O'CLOCK AND 9 O'CLOCK POSITIONS IAW REO.

Part: FLOOR SUPPORT — CORRODED (BS 559) · airframe 33,022 hrs · 30,356 cycles

DURING C CHECK, FOUND LBL 46 FLOOR SUPPORT CORRODED BETWEEN BS 559+16 - 559+48. REPAIRED IAW EC/TC REO 601R-53-00-526.

Part: FLOOR SUPPORT — CORRODED (BS 409) · airframe 33,022 hrs · 30,356 cycles

DURING C CHECK, FOUND RT FLOOR SUPPORT CORRODED BETWEEN BS 409+32 - 409+96. REPAIRED IAW EC/TC REO 601R53-00-530.

Part: FLOOR SUPPORT — CORRODED (BS 559) · airframe 33,022 hrs · 30,356 cycles

DURING C CHECK, FOUND RBL 46 FLOOR SUPPORT CORRODED AT BS 559+80. REPAIRED IAW EC/TC REO 601R-53-00-526.

Part: FLOOR SUPPORT — CORRODED (BS 582-621) · airframe 33,022 hrs · 30,356 cycles

DURING C CHECK, FOUND RBL 46 FLOOR SUPPORT CORRODED BETWEEN BS 582-621. REPAIRED IAW EC/TC REO 601R-53-00-526.

Part: STIFFENER — CRACKED (PAX DOOR) · airframe 33,022 hrs · 30,356 cycles

DURING C CHECK, FOUND PAX DOOR ASSIST MOTOR AFT SIDE PANEL STIFFENER CRACKED AT LOWER SECTION. C/W EC/TC REO 601R-52-11-1376 REV A.

Part: SKIN — DAMAGED (ZONE 100) · airframe 33,022 hrs · 30,356 cycles

DURING C CHECK, FOUND FASTENER HOLE DAMAGED ON FUSELAGE SKIN DURING INSTALLATION OF PANEL 132AL. REPAIRED THE SKIN IAW REO 601R-53-11-162 & EC/TC REO 601R-53-11-162. MAJOR REPAIR.

Part: WIRE — MISINSTALLED (EMERGENCY LIGHT) · airframe 32,646 hrs · 29,991 cycles

NUMBERS 1, 2, AND 7 EXTERNAL EMERGENCY LIGHTS INOPERTIVE. ACFT NOT OPERATED AT NIGHT. FOUND WIRES TO FORWARD NR 1 SERVICE DOOR EMERGENCY LIGHT INCORRECTLY INSTALLED. R & R NR 1 LT AND RT EMERGENCY LIGHT SOCKETS AND REPLACED FUSE TO NR 1 BATTERY PACK. R & R NR 4 BATTERY PACK. PERFORMED OPS CHECK OF EMERGENCY LIGHTS. EMERGENCY LIGHTS OP CHECK GOOD IAW AMM'S 33-51-00, 33-51-05 AND 33-51-21 CMM REF 33-21-70. THIS CLEARS THIS MEL. PLACARD REMOVED.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 32,588 hrs · 29,935 cycles

NR 2 CABIN EMERGENCY CEILING FLOOD LIGHT INOPERATIVE. REPLACED THE LAMP IAW AMM 3-51-16. OPS CHECKED GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 32,588 hrs · 29,935 cycles

NR 2 EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMP IAW AMM 33-51-21. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 32,284 hrs · 29,670 cycles

RIGHT NR 3 EXTERIOR EMERGENCY LIGHT INOPERATIVE. R & R RT NR 3 EXTERIOR EMERGENCY LIGHT BULB IAW AMM 33-51-21. OPS CHECK GOOD.

Part: SIGN — DAMAGED (CABIN) · airframe 31,087 hrs · 28,605 cycles

LIGHTED FLOOR-LEVEL EXIT SIGN AT SERVICE DOOR DAMAGED. R & R SIGN IAW AMM 33-51-10. SYSTEM OPS CHECKED GOOD. NO FURTHER ACTION.

Part: INVERTER — FAILED (EMERGENCY LIGHTS) · airframe 30,807 hrs · 28,354 cycles

LIGHTED FLOOR-LEVEL EXIT SIGN AT RT OVERWING EMERGENCY EXIT INOPERATIVE. R & R AFFECTED INVERTER IAW 33-51-07. SYSTEM OPS CHECKED GOOD. NO FURTHER ACTION.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 28,764 hrs · 26,495 cycles

RT OVERWING EMERGENCY EXIT SIGN INOPERATIVE. OPS CHECKED EMERGENCY LIGHT IAW AMM 33-51-00. OPS CHECKED GOOD.

Part: FRAME — CORRODED (BS 364) · airframe 28,578 hrs · 26,320 cycles

BS 364, FRAME IS CORRODED BETWEEN STR 26L AND 26R. REPAIRED.

Part: STIFFENER — CRACKED (BS 409) · airframe 28,560 hrs · 26,303 cycles

FS 409+128, BL 0 VERT POST RT SIDE HAS AN INDICATION NOTED IN THE AFT FLANGE RADIUS AT WL 69, APPROX .250" LONG BY 50 PERCNET FSH. FAILED NDT. R & R RT VERT POST AT BL 0 PN 601R32208-132 IAW CRJ 200 51-42-22, 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. ATTACHED CERTIFICATION FOR ANGLE PN 601R32208-132.

Part: POST — CRACKED (BS 409) · airframe 28,578 hrs · 26,320 cycles

FS 409+128, RBL 18 INBD VERT POST HAS AN INDICATION NOTED IN THE AFT FLANGE RADIUS AT WL 69 APPROX .5" LONG X 50 PERCENT FSH. FAILED NDT INSP. REMOVED LT AND RT VERTICAL POSTS AT FS 409+128, RBL 18 IAW SRM 51-42-06 AND 51-42-22. C/W ECTC REO: 601R-53-41-889 AND MET ALL REQUIREMENTS OF REO:601R-53-41-889, REV A. LOCATED, DRILLED AND BENCH ASSEMBLED NEW FS 409+128, RB18 POST HALVES IAW SRM 51-40-11 AND 51-42-06.

Part: PIN — CORRODED (LATCH) · airframe 28,578 hrs · 26,320 cycles

LT AND RT LATCH IN INTERCOSTALS ARE CORRODED BETWEEN FS 349 AND FS 364. REMOVED LT AND RT LATCH PIN INTERCOSTALS IAW SRM 51-42-06 AND 51-42-21. INSTALLED LT LATCH PIN INTERCOSTAL 601R31049-9 AND RT LATCH PIN INTERCOSTAL 601R31049-10 IAW SRM 51-42-06, 51-42-21. LOCATED AND DRILLED NEW LT AND RT INTERCOSTALS IAW SRM 51-40-11.

Part: ISOLATOR — CRACKED (BULKHEAD) · airframe 28,560 hrs · 26,303 cycles

REAR PRESSURE BULKHEAD FWD FACE OF WEB HAS A MISSING ISOLATOR AND A BENT AND CRACKED ISOLATOR AT RBL 27.50 AND WL 75.00. R & R ISOLATOR BRACKET AND INSTALLED NEW ISOLATOR IAW SRM 51-42-06.

Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 28,560 hrs · 26,303 cycles

FOUND REAR PRESSURE BULKHEAD WEB HAS INDICATIONS NOTED AT BL 0.0, WL 108-112, 3.5" L, 70 PERCNET FSH. FAILED NDT INSPECTION. COMPLIED WITH EC/TC REO 601R-53-61-1285 AND GREO 601R-53-61-1285, REV D.

Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 28,560 hrs · 26,303 cycles

FOUND REAR PRESSURE BULKHEAD WEB HAS INDICATIONS NOTED AT BL 0.0, WL 131-134, 2.5" L, 50 PERCENT FSH. FAILED NDT INSPECTION. COMPLIED WITH EC/TC REO 601R-53-61-1285 AND REO 601R-53-61-1285, REV D.

Part: FLOOR SUPPORT — CORRODED (BS 409-559) · airframe 28,555 hrs · 26,298 cycles

CORROSION ON RT UPPER SURFACE OF PRESSURE FLOOR SUPPORT AT VARIOUS LOCATIONS FROM FS 409.00+128 TO FS 559.00. COMPLIED WITH EC/TC REO 601R-53-41-666 & REO 601R-53-41-666, REV C.

Part: FRAME — CORRODED (BS 333) · airframe 28,555 hrs · 26,298 cycles

CORROSION ON FRAME AT FS 333.00 BETWEEN LBL STGR 24 AND RBL STGR 24. REMOVED POSTS AT FS 333 RBL 20 AND LBL 20 IAW SRM 51-42-06 & 51-42-21. UPON FURTHER INVESTIGATION, FOUND TO BE BETWEEN STR 24 & 23L AND STR 24 & 23R, INSTALLED SAME SERVICEABLE VERTICAL POSTS IAW SRM 51-42-06 AND 51-42-21. REMOVED FLOOR SUPPORT BRACKET AT FS 333, BL 0 IAW SRM 51-42-06. INSTALLED FLOOR SUPPORT BRACKET AT FS 333, BL 0 IAW SRM 51-42-06. REMOVED FRAME AT FS 333 BETWEEN STRINGER 24L & 24R IAW SRM 51-42-06, 51-42-21. LOCATED AND DRILLED NEW FRAME AT FS 333 BETWEEN STRINGER 24L & 24R, PN 601R32004-55 IAW SRM 51-40-06, 51-40-11. INSTALLED NEW FRAME AT FS 333 BETWEEN STRINGERS 24L AND 24R IAW SRM 51-42-06 AND 51-42-21. COMPLETED IAW SNIEO 601R32004 S02 REV O. COMPLIED WITH REO 601R-53-21-2576 REV, 2 NOV 14.

Part: CARGO TRACK — CORRODED (BS 559) · airframe 28,555 hrs · 26,298 cycles

CARGO TRACK AT RBL 27 BS 559+79 - 559+95 HAS CORROSION. R & R THE CARGO TRACK SEGMENT IAW SRM 51-41-02-00, 51-41-04-00.

Part: FLOOR SUPPORT — CORRODED (BS 574-621) · airframe 28,555 hrs · 26,298 cycles

LT CARGO FLOOR SUPPORT FROM BS 574 - 621 HAS CORROSION AT FLOORBOARD SCREW HOLES. REPAIRED IAW REO 601R-53-00-526 AND GREO 601R-53-00-526 REV.

Part: CARGO TRACK — CORRODED (BS 612-617) · airframe 28,555 hrs · 26,298 cycles

CARGO TRACK AT LBL 9, BS 612-617 HAS CORROSION AT ATTACHMENT HOLES. R & R THE CARGO TRACK SEGMENT IAW SRM 51-42-02-00, 51-41-04-00.

Part: BRACKET — CRACKED (WINDOW FRAME) · airframe 28,555 hrs · 26,298 cycles

PILOTS SIDE WINDOWS AFT BRACKET IS CRACKED APPROX .250"L AT BOTTOM OF POST. REMOVED AFT, PILOT SIDE WINDSCREEN FITTING IAW SRM 51-42-21. INSTALLED NEW FITTING IAW SRM 51-42-21. LOCATED AND DRILLED NEW BRACKET IAW SRM 51-40-11. COMPLIED WITH SNIEO 601R33007S04. INSTALLED LT SIDE LOWER FITTING SIDE POST, PN:601R33235-3 IAW SNIEO 601R33007S04.

Part: FLOOR SUPPORT — CORRODED (BS 349) · airframe 28,555 hrs · 26,298 cycles

CORROSION ON LT FLOOR SUPPORT AT BS 349 JUST AFT OF PAX DOOR. REPAIRED IAW REO 601R-53-00-530.

Part: CARGO TRACK — CORRODED (BS 559) · airframe 28,555 hrs · 26,298 cycles

CARGO TRACK AT LBL 9 BS 559+87- 559-96 HAS CORROSION AT ATTACHMENT HOLES. R & R THE CARGO TRACK SEGMENT IAW SRM 51-41-02-00, 51-41-04-00.

Part: FLOORBEAM — CORRODED (BS 559) · airframe 28,555 hrs · 26,298 cycles

RBL 9 - 27 FLOORBEAM TEE AT BS 559+112 HAS CORROSION. REPAIRED IAW REO 601R-53-090-005.

Part: FLOORBEAM — CORRODED (BS 559) · airframe 28,555 hrs · 26,298 cycles

RBL 9 - 27 FLOORBEAM CAP BS 559+96 CORRODED . REPAIRED IAW REO 601R-53-00-005.

Part: FLOOR SUPPORT — CORRODED (BS 559-621) · airframe 28,555 hrs · 26,298 cycles

RT CARGO FLOOR SILL FROM FS 559.00+112 TO FS 621.00 HAS FILIFORM CORROSION AT FLOORBOARD SCREW HOLES. REMOVED NUTPLATES FROM RT CARGO FLOOR SILL FROM FS 559.00+112 TO FS 621.00 IAW SRM 51-54-10. INSTALLED 13 NEW SERVICEABLE NUTPLATES, PN MS21059L3 IAW SRM 51-42-15 ON RT SIDE CARGO FLOOR SILL FROM FS 559.00+112 TO FS 621.00. COMPLIED WITH EC/TC REO 601R-53-00-526 AND GREO 601R-53-00-526 REV.

Part: CARGO TRACK — CORRODED (BS 559-568) · airframe 28,555 hrs · 26,298 cycles

CARGO TRACK AT LBL 9 BS 559+110 - 568 HAS CORROSION. R & R THE CARGO TRACK SEGMENT IAW SRM 51-41-02-00, 51-41-04-00.

Part: FLOOR SUPPORT — CORRODED (BS 409-559) · airframe 28,576 hrs · 26,319 cycles

CORROSION ON LT UPPER SURFACE OF PRESSURE FLOOR SUPPORT BS 409+128 - 559.00. BLENDED CORROSION IAW REO 601R-53-41-666 2.2 DISP A AND B. PERFORMED EDDY CURRENT REWORKED AREAS IAW REO 601R-53-41-666, REV C 1.2, STEP C. NO INDICATIONS NOTED AT THIS TIME.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 28,555 hrs · 26,298 cycles

CARGO TRACK AT RBL 9, BS 559+87-559+96 CORRODED. R & R THE CARGO TRACK SEGMENT IAW SRM 51-41-02-00, 51-41-04-00.

Part: CARGO TRACK — CORRODED (BS 559) · airframe 28,555 hrs · 26,298 cycles

CARGO TRACK AT LBL 27, BS 559 HAS CORROSION AT ATTACHMENT HOLES. R & R THE CARGO TRACK SEGMENT IAW SRM 51-41-02-00, 51-41-04-00.

Part: CARGO TRACK — CORRODED (BS 559-568) · airframe 28,555 hrs · 26,298 cycles

CARGO TRACK AT RBL 9 BS 559+110 - 568 CORRODED. R & R THE CARGO TRACK SEGMENT IAW SRM 51-41-02-00, 51-41-04-00.

Part: STRINGER — CRACKED (BS 280) · airframe 28,555 hrs · 26,298 cycles

STRINGER 3L IS CRACKED JUST AFT OF FS 280 APPROXIMATELY 1"L. REMOVED CRACKED ANGLES AT STR 3L FS 280. LOCATED, DRILLED & INSTALLED NEW PARTS IAW SRM 51-40-11 & 51-42-06, PN 600-31057-19, PO W29151, PN 600-31057-20, PO W28468. INSTALLED NEW DRILLED STR 3L ANGLES AT FS 280 IAW EO 601R31057 SNIEO S02. INSTALLED NEW ANGLES 600-31057-19 & 600-31057-20 IAW SNIEO 601R31057 S02.

Part: FRAME — CORRODED (BS 349) · airframe 28,555 hrs · 26,298 cycles

CORROSION ON FRAME AT FS 349.00 BETWEEN LBL STR 24 AND RBL STGR 24. REMOVED CORRODED FRAME SECTOR AT FS 349.00 BETWEEN STR 23L-23R IAW SRM 51-42-06 AND 51-42-21. LOCATED AND DRILLED NEW SERVICEABLE FS 349.00 FRAME SECTOR IAW SRM 51-40-11. INSTALLED IAW SNIEO 601R32005 S02 FRAME AT FS 349 BETWEEN STRINGERS 23L-23R. INSTALLED FRAME, PN 601R32005-69 IAW SNIEO 601R32005 S02.

Part: SKIN — CORRODED (BS 559) · airframe 28,555 hrs · 26,298 cycles

AFT FUSELAGE LOWER SKIN PANELS HAVE SURFACE CORROSION IN NUMEROUS AREAS ON EXTERIOR SIDE OF PANELS FROM FS 559.00 TO FS 559.00+112, STR 26L TO STR 26R. AREAS ARE MARKED. REMOVED 123 EA FASTENERS TO ACCESS LOWER SKIN PANEL CORROSION FROM FS 559 TO FS 559+112 IAW SRM 51-42-06 & 51-42-21. INSTALLED NEW FASTENERS IN AFFECTED AREAS IAW SRM 51-42-06 & 51-42-21 & COMPLIED WITH EA 32-2014-153.

Part: ENGINE — FLAMED OUT (NR 1) · airframe 28,048 hrs · 25,841 cycles

DURING CRUISE AT FL300, NR 1 ENGINE FLAMED OUT. ATTEMPTED TWO RELIGHT ATTEMPTS WITHOUT SUCCESS. LANDED WITHOUT FURTHER INCIDENT. FLAME OUT EMERGENCY DECLARED. ENGINE CHANGED. ACFT OK FOR SERVICE.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 27,221 hrs · 25,012 cycles

LEFT NR 3 EXTERNAL EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP IAW AMM 33-51-21. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (LT OVERWING) · airframe 26,539 hrs · 24,311 cycles

LEFT OVERWING AFT EMERGENCY LIGHT OUT. R & R 7 EXTERIOR EMERGENCY LIGHT IAW AMM 33-51-21. OPS CHECKED GOOD.

Part: LIGHT — BROKEN (CABIN) · airframe 26,433 hrs · 24,203 cycles

LOWER EMERGENCY LIGHT ASSY AT ENTRYWAY BROKEN. R & R LIGHT ASSY IAW AMM 33-51-10, OPS CHECKED GOOD. ACFT OK FOR SERVICE.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 25,842 hrs · 23,662 cycles

LT OVERWING FWD EMEGENCY LIGHT INOPERATIVE. R & R EMERGENCY LIGHT BULB IAW AMM 33-51-21. OPS CHECKED GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 24,465 hrs · 22,296 cycles

NR 1 EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP. OPS CHECKED GOOD IAW AMM 33-51-00.

Part: ANGLE — CORRODED (PAX DOOR) · airframe 24,334 hrs · 22,159 cycles

PAX DOOR LOWER CORNER SECTION CORRODED BEYOND ALLOWABLE LIMITS. REMOVED DAMAGED CORNER IAW SRM 51-42-06, 51-42-10. INSTALLED PAX DOOR FWD CORNER IAW SRM 51-42-06 7, SRM 51-42-10.

Part: FRAME — CORRODED (BS 605) · airframe 24,334 hrs · 22,159 cycles

FS 605.00 FRAME SECTOR HAS CORRODED FRAME FLANGE FWD AND AFT SIDE BETWEEN STRINGERS 27L AND 26L. CORROSION IS OUT OF LIMITS IAW SRM 53-61-15- AND 53-00-00 T/R 53-27, FIG 102, SHEET 2. REPAIRED IAW REO 601R-53-61-4737.

Part: FRAME — CRACKED (BS 718) · airframe 24,333 hrs · 22,158 cycles

LEFT FS 718.0 DOUBLER CRACKED BETWEEN STR 10L & 12L & RT FS 718.0 FRAME FLANGE CRACKED BETWEEN STR 10R & 12R.

Part: FLOOR SUPPORT — CORRODED (BS 559) · airframe 24,328 hrs · 22,151 cycles

FLOOR STRUCTURE HAS CORROSION AROUND FASTENER HOLE JUST FWD OF FS 559+80 AT LBL 45.0. REMOVED CORROSION FROM FASTENER HOLE TO OBTAIN TOTAL DEPTH AT LBL 45.0 JUST FWD OF 559+80 IAW SRM 51-21-00. C/W REO 601R-53-51-208 AND REO 601R-53-51-201.

Part: FLOOR SUPPORT — CORRODED (BS 349) · airframe 24,328 hrs · 22,151 cycles

RIGHT SIDE FLOOR SUPPORT CORRODED AT FS 349 JUST AFT OF SERVICE DOOR. REPAIRED IAW REO 601R-53-21-2378.

Part: FLOOR SUPPORT — CORRODED (BS 621) · airframe 24,333 hrs · 22,158 cycles

FLOOR SUPPORT STRUCTURE CORRODED JUST FWD OF FS 621 AT LBL 9.0. REMOVED BEAM CAP FS 574 TO FS 621 AT LBL 9.00 IAW SRM 51-42-06 & 51-42-21. LOCATED & DRILLED NEW SEAT RAIL BEAM PN 601R35031-3 IAW SRM 51-40-11. INSTALLED FASTENERS ON FLOORBEAM WEBS IAW REO 601R-53-61-3780, PART B. C/W ECTC REO 601R-53-61-3780 AND REO 601R-53-61-378, REV A DATED 7/15/11.

Part: SEAT TRACK — CORRODED (BS 399-409) · airframe 24,328 hrs · 22,151 cycles

LBL 9 SEAT TRACK HAS AREAS OF CORROSION FROM FS 399 TO 409+128. R & R SEAT TRACK IAW SRM 51-40-11 AND 51-41-04 AND AMM 53-01-11-400-802.

Part: FLOORBEAM — CORRODED (BS 409) · airframe 24,328 hrs · 22,151 cycles

FLOORBEAM CAP AT FS 409+32 TO 409+64 RBL 9 CORRODED. REMOVED FLOORBEAM CAP IAW SRM 51-42-06. INSTALLED FLOORBEAM CAP IAW REO 601R-53-31-773. REPAIRED IAW REO 601R-53-31-772, REO 601R-53-31-773 REO 601R-53-00-501.

Part: ANGLE — CORRODED (SERVICE DOORWAY) · airframe 24,333 hrs · 22,158 cycles

SERVICE DOOR SILL ANGLE CORRODED. LOCATED & DRILLED NEW SERVICE DOOR ANGLE IAW SRM 51-40-11. INSTALLED NEW SERIVCEABLE DOOR SILL ANGLE IAW SRM 51-42-21 AND 51-42-13.

Part: SEAT TRACK — CORRODED (BS 399-409) · airframe 24,328 hrs · 22,151 cycles

RBL 9 SEAT TRACK CORRODED FROM FS 399 TO 409+128. R & R SEAT TRACK IAW SRM 51-40-11 AND 51-41-04 AND AMM 53-01-11-400-802.

Part: ANGLE — CRACKED (BS 280) · airframe 24,322 hrs · 22,144 cycles

FS 280, FWD J ANGLE CORRODED BETWEEN LBL 9 AND RBL 9. REMOVED FS 280 FWD J ANGLE BETWEEN LBL 9 & RBL 9 IAW SRM 51-42-06. LOCATED & DRILLED NEW SERVICEABLE FWD J ANGLE, IAW SRM 51-40-11. INSTALLED NEW SERVICEABLE FWD "J" ANGLE IAW SRM 51-42-06.

Part: SILL — CORRODED (CARGO DOORWAY) · airframe 24,333 hrs · 22,158 cycles

CARGO DOOR SILL HAS AREAS OF CORROSION AROUND FASTENER HOLES. REMOVED CARGO DOOR SILL IAW SRM 51-42-06 AND 51-42-21. NEW CARGO DOOR SILL INSTALLED IAW SRM 51-42-06, 51-42-21 AND REO 601R-53-61-1574, REV A.

Part: FLOOR SUPPORT — CORRODED (BS 574-621) · airframe 24,333 hrs · 22,158 cycles

FLOOR SUPPORT CORRODED AT LBL 27.0 FROM FS 621.00 TO FS 574.00. REMOVED CORRODED FLOOR SUPPORT. LOCATED & DRILLED NEW PART IAW SRM 51-40-11 AND REO 601R-53-61-3778. INSTALLED NEW SERVICEABLE FLOOR SUPPORT IAW SRM 51-42-21. COMPLIED WITH REO 601R-53-61-3778 AND GREO 601R-53-61-3778, REV A.

Part: FLOOR SUPPORT — CORRODED (BS 319) · airframe 24,322 hrs · 22,144 cycles

FLOOR SUPPORT AT FS 319.70 JUST FWD OF SERVICE DOOR CORRODED. REMOVED FITTING FOR REPLACEMENT IAW SRM 51-42-21, INSTALLED NEW SERVICEABLE FLOOR SUPPORT IAW REO 601R-53-21-2382 & SRM 51-42-21.

Part: FLOOR SUPPORT — CORRODED (BS 559) · airframe 24,333 hrs · 22,158 cycles

FLOOR SUPPORT CORRODED AT LBL 45.0 BETWEEN FS 559+80 TO 559+112. REPAIRED IAW REO 601R-53-51-209.

Part: SEAT TRACK — CORRODED (BS 364-399) · airframe 24,328 hrs · 22,151 cycles

SEAT TRACK FS 364 TO FS 399 ARE CORRODED. REMOVED DAMAGED SEAT TRACK IAW AMM 53-01-11-000-802 & INSTALLED NEW SERVICEABLE SEAT TRACK IAW AMM 53-01-11-400-802.

Part: FLOOR SUPPORT — CORRODED (BS 559) · airframe 24,333 hrs · 22,158 cycles

FLOOR SUPPORT BETWEEN FS 559.00+80 AND 559.00+112 AT RBL 45 CORROSION AROUND FASTENER HOLES. REMOVED CORROSION IAW SRM 51-21-00. REPAIRED IAW REO 601R-53-51-211.

Part: SEAT TRACK — CORRODED (BS 409-559) · airframe 24,333 hrs · 22,158 cycles

SEAT RAIL FROM 409+128 TO FS 559 AT RBL 9.0 CORRODED. REMOVED SEAT RAIL BETWEEN FS 409+128 TO FS 559.0 AT RBL 9.0 IAW SRM 51-41-02. FABRICATED AND INSTALLED SEAT RAILS IAW GREO 601R-53-00-485.

Part: FLOOR SUPPORT — CORRODED (BS 559) · airframe 24,333 hrs · 22,158 cycles

FLOOR SUPPORT CORRODED AT LBL 45.0 AND FWD OF 559+16 TO 559+32. REPAIRED IAW REO 601R-53-51-207.

Part: FLOOR SUPPORT — CORRODED (BS 559) · airframe 24,328 hrs · 22,151 cycles

FLOOR STRUCTURE CORROSION FOUND AROUND FASTENER HOLES AT RBL 45.0 BETWEEN FS 559+16 AND 559+32. REMOVED CORROSION AROUND FASTENER HOLES TO OBTAIN TOTAL DEPTH IAW SRM 51-21-00 3 TOTAL HOLES. ENGINEERING REQUIRED. REO 601R-53-51-210.

Part: FLOOR SUPPORT — CORRODED (BS 319) · airframe 24,322 hrs · 22,144 cycles

FLOOR SUPPORT AT FS 319 JUST FWD OF SERVICE DOOR CORRODED. REMOVED FWD FLOOR SUPPORT IAW SRM 51-42-06. DRILLED & POSITIONED NEW SERVICEABLE FLOOR SUPPORT IAW SRM 51-40-11.

Part: FLOORBEAM — CORRODED (BS 349) · airframe 24,328 hrs · 22,151 cycles

FLOORBEAM AT FS 349.00 CORRODED JUST AFT OF SERVICE DOOR. REPAIRED IAW SRM 51-42-13.

Part: SEAT TRACK — CORRODED (BS 409-559) · airframe 24,333 hrs · 22,158 cycles

SEAT TRACK FROM 409+128 TO FS 559.0 AT LBL 9.0 CORRODED. REMOVED SEAT TRACK FROM FS 409+128 FS 559.0 AT LBL 9.0 IAW SRM 51-41-02. FABRICATED AND INSTALLED SEAT TRACK IAW GREO 601R-53-00-425.

Part: ANGLE — CRACKED (BS 280) · airframe 24,321 hrs · 22,142 cycles

FS 280 UPPER J ANGLE CRACKED OTBD OF RBL 9 APPROX 2 INCHES. REPAIRED IAW REO 601R-53-11-2420.

Part: SUPPORT ANGLE — CRACKED (BS 484) · airframe 24,322 hrs · 22,144 cycles

FS 484.00 SUPPORT ANGLE CRACKED AT LBL 27.0 AND LBL 36.0. FOUND SUPPORT ANGLE LBLB 36 TO BE SERVICEABLE (NOT CRACKED). ANGLE AT FS 484 AND LBL 27 REQUIRES REPAIR. REMOVED AND INSTALLED NEW SERVICEABLE ANGLE, IAW SRM 51-42-06. FABRICATED ANGLE IAW NDTM 51-20-06. REPAIRED IAW REO 601R-53-41-059.

Part: SUPPORT ANGLE — CRACKED (BS 484) · airframe 24,322 hrs · 22,144 cycles

FS 484.00 AT RBL 27.0 SUPPORT ANGLE CRACKED. REMOVED CRACKED ANGLE IAW SRM 51-42-06 & 51-42-21. REPLACED SUPPORT ANGLE IAW SRM 51-42-06 & 51-42-21.

Part: ANGLE — CRACKED (BS 625) · airframe 24,321 hrs · 22,142 cycles

OBLIQUE ANGLE CRACKED. REMOVED LT OBLIQUE ANGLE AT FS 625 IAW SRM 51-42-21. FABRICATED & INSTALLED NEW OBLIQUE ANGLE IAW REO 61R-53-61-4729.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 24,321 hrs · 22,142 cycles

PAX DOOR AFT DRAG ANGLE CRACKED NEAR DOOR ASSIST PULLEY. R & R DRAG ANGLE IAW SRM 51-42-06.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 23,874 hrs · 21,683 cycles

NR 6 EXTERIOR EMERGENCY LIGHT IS OUT. LAMPED NR 6 EXTERIOR EMERGENCY LIGHT IAW AMM 33-51-19. OPS CHECKED GOOD.

Part: BULKHEAD — CRACKED (BS 202) · airframe 23,576 hrs · 21,397 cycles

CRACK IN BS 202 BULKHEAD. COMPLIED WITH EDDY CURRENT INSPECTION IAW, NDTM 51-20-06 AND CONFIRMED CRACK. CUT OUT DAMAGE IAW GREO 601R-53-11-563, REV B. REPAIR TYPE 4. COMPLIED WITH EDDY CURRENT INSPECTION IAW NDTM 51-20-06. NO DEFECTS NOTED. FABRICATED REPAIR DOUBLER, SHIMS IAW GREO 601R-53-11-563, REV B. REPAIR TYPE 4 AND SRM 51-00-00. INSTALLED REPAIR IAW GREO 601R-53-11-563, REV B. REPAIR TYPE 4.

Part: ATTACH FITTING — CRACKED (BS 484) · airframe 23,192 hrs · 20,975 cycles

DURING DETAILED INSPECTION OF THE PRESSURE FLOOR SKIN IAW NDT MANUAL, PART 9, 53-41-149. FOUND LT SIDE ATTACHMENT FLANGE AT FS 484 CRACKED ALSO CONFIRMED WITH EDDY CURRENT IAW NDTM 51-20-06. / PART 1. R & R LT ANGLE FLANGE IAW REO 601R-53-41-059, REV B. RESTORED FININSH IAW SRM 51-21-16.

Part: ATTACH FITTING — CRACKED (BS 484) · airframe 23,192 hrs · 20,975 cycles

DURING DETAILED INSPECTION OF THE PRESSURE FLOOR SKIN IAW NDT MANUAL, PART 9, 53-41-149. FOUND RT SIDE ATTACHMENT FLANGE AT FS 484 CRACKED ALSO CONFIRMED WITH EDDY CURRENT IAW NDTM 51-20-06. R & R RT ANGLE FLANGE IAW REO 601R-53-41-059, REV B. RESTORED FININSH IAW SRM 51-21-16. (SDR CLOSED)

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 22,964 hrs · 20,706 cycles

RIGHT EXTERIOR EMERGENCY LIGHT NR 4 IS OUT. RELAMPED THE RT EXTERIOR EMERGENCY LIGHT NR 4 AS REQUIRED AND OPS CHECKED GOOD IAW AMM 33-51-00.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 22,674 hrs · 20,375 cycles

EMERGENCY EXIT SIGN MISSING RED LENS. INSTALLED RED LENS IAW AMM 33-51-14.

Part: CIRCUIT BREAKER — TRIPPED (EMERGENCY LIGHT) · airframe 21,936 hrs · 19,535 cycles

IN THE "ARM" POSITION EMERGENCY LIGHTS COME ON. TROUBLESHOT SYS AND FOUND CBPU C2 OUT. RESET C/B SYS OPS CHECKED OK IAW AMM 35-51-00.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 21,248 hrs · 18,743 cycles

F/A FLASHLIGHT INOP. R & R F/A'S FLASHLIGHT.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 20,482 hrs · 17,859 cycles

AFT CABIN EMERGENCY CEILING LIGHT IS INOP. R & R EMERGENCY CEILING LIGHT BULB IAW AMM 33-51-16. OP'S CHECKED GOOD. (CLOSED)

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 20,234 hrs · 17,564 cycles

EXTERIOR EMERGENCY LIGHT AT NR7 POSITION INOP. RELAMPED EXTERIOR EMERGENCY LIGHT AT NR7 POSITION IAW AMM 33-51-21. RELAMPED EXTERIOR EMERGENCY LIGHT AT NR7 POSITION IAW AMM 33-51-21.(CLOSED)

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 19,957 hrs · 17,241 cycles

AFT INTERIOR CEILING EMERGENCY FLOOD LIGHT INOP. RELAMPED AFT INTERIOR CEILING EMERGENCY FLOOD LIGHT IAW AMM 33-51-14. OPS CHECK GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 19,488 hrs · 16,700 cycles

AFT CABIN AND RT NR 2 OUTSIDE EMERG LIGHTS DO NOT OPERATE. REMOVED THE AFT CABIN EMERGENCY LIGHT LENS. R & R THE BULB AND REINSTALLED THE LENS. REMOVED THE 4 SCREWS OF THE RT NR 2 OUTSIDE EMERGENCY LIGHT. R & R THE BULB AND INSTALLLED THE 4 SCREWS OF THE RT NR 2 OUTSIDE EMERGENCY LIGHT IAW AMM 20-21-00-910-801. OPS TEST OF THE EMERGENCY LIGHTS ARE GOOD IAW AMM 33-51-00-710-801.

Part: SUPPORT BRACKET — CRACKED (BS 409) · airframe 19,477 hrs · 16,683 cycles

SUPPORT BRACKET BETWEEN F.S. 409.00+48 F.S. 409.00+64 AND BETWEEN LBL 9 AND RBL 9 IS CRACKED. REMOVED THE CRACKED SUPPORT BRACKET. LOCATED A NEW SUPPORT BRACKET AND INSTALLED THE NEW SUPPORT BRACKET IAW THE SRM 51-40-11, 51-41-02 AND 51-42-06.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 19,477 hrs · 16,683 cycles

FLOOR SUPPORT STRUCTURE IS CRACKED FS 280 AT RBL 9.0, WEB AND CLIP. REMOVED I/B AND O/B RBL 9.0 FS 280 CLIPS IAW SRM 51-42-06 AND 51-42-21. REPLACED I/B CLIP RBL 9.0 WITH NEW SERVICEABLE CLIP IAW SRM 51-42-06 AND 51-42-21. PERFORMED NDT PER NDTM 51-20-06. NO INDICATIONS NOTED. COMPLIED WITH EC/TC 601R-53-11-171 AND MET ALL THE REQUIREMENTS OF REO 601R-53-11-171. REPLACED O/B CLIP IAW REPAIR REO 601R-53-11-171.

Part: PLACARD — TORN (PAX DOOR) · airframe 19,477 hrs · 16,683 cycles

PAX DOOR EXIT PLACARD TORN. REMOVED TORN "EXIT" PLACARD IAW AMM TASK 11-30-00-000-801 & INSTALLED NEW PLACARD S1574-18 TO PAX DOOR STEP IAW AMM TASK 11-30-00-400-801.

Part: PLACARD — FADED (ESCAPE HATCH) · airframe 19,477 hrs · 16,683 cycles

CREW ESCAPE HATCH OPEN, CLOSED AND EMERGENCY EXIT EXTERIOR PLACARDS ARE FADED. APPLIED OPEN, CLOSED, EMERGENCY EXIT SILKSCREENS ON CREW ESCAPE HATCH IAW MM 11-10-03-400-801.

Part: BULKHEAD — CRACKED (BS 202) · airframe 19,477 hrs · 16,683 cycles

PARKING BRAKE CABLE HOLE AT BS 202.75 BULKHEAD APPREARS TO BE CRACKED. PERFORMED EDDY CURRENT INSPECTION OF BULKHEAD AROUND BRAKE CABLE HOLE IAW NDTM 51-20-06. NO INDICATIONS NOTED AT THIS TIME.

Part: STRINGER — CRACKED (BS 718 S10L) · airframe 19,477 hrs · 16,683 cycles

FOUND VISUAL EVIDENCE OF CRACK RADIATING FROM RIVET AT FS 718.00 UPPER SIDE OF STRINGER 10 LT CORNER OF STR 10 LT AND FS 718 (MARKED WITH YELLOW TAPE). PERFORMED EDDY CURRENT INSP ON NOTED AREA IAW NDTM 51-20-06. NO INDICATIONS NOTED (REMOVED YELLOW TAPE).

Part: POST — CRACKED (BS 409) · airframe 19,477 hrs · 16,683 cycles

JOB 8764825 /OPERATION 99. FOUND FS 409.0+128 VERTICAL POST BL 0.0 LT SIDE HAS INDICATION NOTED APPROX .3" IN LENGTH 80 PERCENT FSH AT WL 69.0 AFT FLANGE RADIUS. FAILED NDT INSPECTION. REMOVED VERTICAL POST COMMON TO FS 409+128 BL0 IAW 51-42-06. DRILLED UP POSTS 601R32208-229 AND 601R32208-230 IAW SRM 51-42-06. DEBURRED AND ASSEMBLED POSTS C601R32008-229 AND 290 IAW SRM 51-42-06. INSTALLED VERTICAL POST AT F.S. 409+128 BL 0 IAW REO 601R-53-41-889 AND SRM 51-42-06. APPLIED ANTI-CORROSION COMPOUND TO THE BL 0 POST AT FS 409-128 IAW THE AMM 51-25-56-390-802. C/W EC/TC REO 601R-53-41-889 & MET ALL THE REQUIREMENTS OF REO 601R-53-41-889, REV A.

Part: BULKHEAD — CRACKED (BS 559) · airframe 19,477 hrs · 16,683 cycles

FOUND FS 559 BULKHEAD WEB RT SIDE HAS INDICATION NOTED APPROX .2" IN LENGTH 60 PERCENT FSH OTBD OF RBL 9.0, WL 58.70. FAILED NDT INSPECTION. C/W ECTC REO 601R-53-41-260 IAW REO 601R-53-41-260 REV D.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 19,477 hrs · 16,683 cycles

FOUND REAR PRESSURE BULKHEAD WEB HAS INDICATION NOTED APPROX .3" IN LENGTH 50 PERCENT FSH AT LBL 27.50, WL 130 LOCATED TOP OF AFT CARGO DOOR TRACK. FAILED NDT INSPECTION. COMPLIED WITH EC/TC REO 601R-53-61-1541 AND MET ALL THE REQUIREMENTS OF REO 601R-53-61-1541, REV B.

Part: POST — CRACKED (BS 409) · airframe 19,477 hrs · 16,683 cycles

FOUND FS 409.0+128 VERTICAL POST LBL 18.0 OTBD SIDE HAS INDICATION NOTED APPROX .3" IN LENGTH 80 PERCENT FSH AT WL 69.0 AFT FLANGE RADIUS. FAILED NDT INSP. REMOVED POST AT FS 409.0+128 LBL 18.00 IAW SRM 51-42-06. LOCATED AND DRILLED NEW OTBD POST TO INBD POST AND INSTALLED RIVET IAW SRM 51-42-06 FOR LBL 18 F.S. 409+128. INSTALLED THE LBL 18 409+128 POST AND C/W EC/TC REO 601R-53-41-889 AND MET ALL OF THE REQUIREMENTS OF REO 601R-53-41-889 REV A.

Part: POST — CRACKED (BS 409) · airframe 19,477 hrs · 16,683 cycles

FOUND FS 409.0+128 VERTICAL POST RBL 18.0 OTBD SIDE HAS INDICATION NOTED APPROX .3" IN LENGTH 60 PERCENT FSH AT WL 69.0 AFT FLANGE RADIUS. FAILED NDT INSP. REMOVED ADEL CLAMPS TO ACCESS POST IAW THE SRM 51-41-02. REMOVED THE POST IAW THE SRM 51-42-06. INSTALLED VERTICAL POST IAW SRM 51-42-06, 51-42-22, AND REO 601R-53-41-889. INSTALLED ADEL CLAMPS IAW AMM 20-21-910-84. C/W EC/TC REO 601R-53-41-889 AND MET ALL THE REQUIREMENTS OF REO 601R-53-41-889 REV A.

Part: SUPPORT BEAM — CRACKED (CARGO DOORWAY) · airframe 19,477 hrs · 16,683 cycles

FOUND CARGO DOOR SUPPORT BEAM AFT LOWER ANGLE HAS A CRACK IN RADIUS APPROX .5" IN LENGTH. REMOVED ANGLE IAW SRM 51-42-21. REINSTALL ANGLE AFTER REAR PRESSURE BULKHEAD REPAIR HAS BEEN COMPLETED4. INSTALLED NEW ANGLE ON CARGO DOOR SUPPORT BEAM AFT LOWER IAW SRM 51-42-21.

Part: SELECTOR VALVE — INOPERATIVE (MLG) · airframe 19,459 hrs · 16,662 cycles

GEAR DISAGREE NOSE GEAR UNSAFE, C/W QRH, MANUAL EXTENSION SUCCESSFUL (EMERGENCY DECLARED -- EQUIPMENT REQUESTED TO BE STANDING BY). R & R NLG SELECTOR VLV IAW CRJ 200 32-33-10 LEAK CK OF HYD SYS AND FUNCTIONAL TEST OF THE EXTENTION AND RETRACTION SYS, GOOD, NO DEFECT NOTED AT THIS TIME (CLOSED)

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 19,084 hrs · 16,232 cycles

RT WING AFT EXTERIOR EMERGENCY LIGHT INOP. R & R BULB IAW AMM 33-51-21. OP CKS GOOD. R & R BULB IAW AMM 33-51-21 OP CKS GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,408 hrs · 15,500 cycles

EMERGENCY EXIT LIGHT INOP ON RT SIDE OF FUSELAGE.

Part: LIGHT — INOPERATIVE · airframe 16,392 hrs · 13,603 cycles

RT OVERWING FWD EMERGENCY LIGHT IS INOP.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 15,297 hrs · 12,665 cycles

BOTH L/R AFT EXTERIOR EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED NR 4 BATTERY PACK IAW AMM 33-51-04-400-801 OPS CK GOOD. (B)

Part: FITTING — CRACKED (FUSELAGE) · airframe 15,274 hrs · 12,643 cycles

JOB 8764811 OPERATION 252 FS 280 CLIP AT LBL 9.0 OUTBRD IS CRACKED. REMOVED CRACKED FS 280.0 CLIP AT OUTBOARD LBL 9 AND INSTALLED NEW SERVICEABLE CLIP IAW CRJ 200 SRM 51-42-13 AND 51-42-21. [SDR CLOSED](B)

Part: FLOOR SUPPORT — CRACKED (BS 484)

LT SIDE FS 484 FLOOR SUPPORT INTERCOSTAL HAS A CRACKED FLANGE ON THE I/B SIDE OF LBL 36 AND A CRACK ATTACH ANGLE ON THE O/B SIDE OF LBL 27. DISCONNECTED MOUNT BOLTS ON CABLE GUIDE IAW 51-41-04. REPAIRED LT FS 484 LBL 36 I/B SIDE AND O/B SIDE OF LBL 27 IAW B/A REO 601R-53-41-059 APPLICABLE STEPS. INSTALLED SAME SERVICEABLE MOUNT BOLTS ON CABLE GUIDE IAW SRM 51-41-04. PRESSURE CHECKS DUE. PERFORMED LEAK CHECK OF THE LT SIDE FS 484 FLOOR SUPPORT INTERCOSTAL LBL 36 AND O/B LBL 27 IAW AMM 21-32-00-863-801. NO LEAKS NOTED AT THIS TIME. REPAIRED LT SIDE FS 484 FLOOR SUPPORT INTERCOSTAL IAW REO 601R-53-41-059.

Part: FLOORBEAM — CRACKED (BS 484) · airframe 15,274 hrs · 12,643 cycles

RT SIDE FS 464 FLOOR SUPPORT INTERCOSTAL HAS A CRACKED FLANGE ON THE I/B SIDE OF RBL 36 AND A CRACKED ATTACH ANGLE ON THE O/B SIDE OF RBL 27. DISCONNECTED MOUNT BOLTS ON CABLE GUIDE IAW 51-41-04. REPAIRED RT SIDE FS 484 INTERCOSTAL I/B OF RBL 36 AND O/B SIDE OF RBL 27 IAW REO 601R-53-41-059. INSTALLED SAME SERVICEABLE MOUNT BOLTS ON CABLE GUIDE IAW SRM 51-41-04. PERFORMED LEAK CHECK OF THE RT SIDE FS 484 FLOOR SUPPORT INTERCOSTAL RBL 36 AND O/B RBL 27 IAW AMM 21-32-00-863-801. NO LEAKS NOTED AT THIS TIME. REPAIRED RT SIDE F.S. 484 FLOOR SUPPORT INTERCOSTAL IAW REO 601R-53-41-059 AND REO 601R-53-41-059.

Part: FLOORBEAM — CRACKED (BS 621) · airframe 15,274 hrs · 12,643 cycles

FS 621 RT SIDE FLOORBEAM ANGLE IS CRACKED AT RBL 40. REPAIRED PREVIOUS REPAIR AT FS 621 RT. LOCATED AND DRILLED NEW ANGLE AND REPAIR ANGLE IAW SRM 51-40-11. INSTALLED ANGLES IAW REO 601R-53-61-117 REV C. LEAK CHECK DUE. PERFORMED LEAK CHECK OF THE RT 621 FLOORBEAM ANGLE IAW AMM 21-32-00-863-801. LEAK CHECK GOOD AT THIS TIME. REPAIRED RT FS 621 FLOOR SUPPORT ANGLE IAW REO 601R-53-61-117 REV C AND REO 601R-53-61-117.

Part: PLACARD — UNSERVICEABLE (PAX DOOR) · airframe 1,527,420 hrs · 12,643 cycles

OPERATION 145 EXIT PLACARD ON PAX DOOR STEP 832BT IS UNSERVICEABLE. REMOVED AND INSTALLED NEW SERVICEABLE EXIT PLACARD ON PAX DOOR STEP 832BT IAW AMM 11-30-00-400-801.

Part: HANDLE — CRACKED (PAX DOOR) · airframe 1,524,720 hrs · 12,643 cycles

PAX DOOR EXTERNAL HANDLE IS CRACKED. SB 601R-51-119 REV A, DOORS, PASSENGER DOOR, REPLACEMENT OF THE OUTER HANDLE INCORPORATED. PAINTED PAX DOOR HANDLE IAW 51-25-01.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 1,524,720 hrs · 12,643 cycles

FS 280 CLIP ON I/B SIDE OF RBL 9 IS CRACKED. REMOVED DAMAGED/CRACKED CLIP. INSTALLED NEW CLIP P/N 601R31113-58 IAW SRM 51-42-21.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 1,524,720 hrs · 12,643 cycles

FS 280 FLOOR SUPPORT STRUCTURE IS CRACKED O/B OF LBL 9 AT MLG MANUAL RELEASE PULLEY BRACKET. CUT AWAY CRACKED SECTION OF FLOOR ANGLE IAW REO 601R-53-11-138. COMPLIED WITH REO 601R-53-11-138. PERFORMED LPI OF FS 280 ANGLE LBL 9 REPAIR IAW NDTM 51-20-08. NO INDICATIONS NOTED AT THIS TIME. INSTALLED REPAIR ANGLE AT FS 280 LBL 9 IAW REO 601R-53-11-138. APPLIED PAINT TO REPAIR IAW SRM 51-25-01. FABRICATED REPAIR ANGLE THAT WAS INSTALLED ON STEP 3 USING 7075-0 .050 PO 83061/1. HEAT TREATED PART TO 7075-T62 AS REQUIRED IAW REO 601R-53-11-138 STEPS 3-5 AND AMS2771 FOR HEAT TREAT.

Part: HINGE — CRACKED (ESCAPE HATCH) · airframe 15,274 hrs · 12,643 cycles

CREW ESCAPE HATCH RT HINGE ARM IS CRACKED. REPLACED CREW ESCAPE HATCH RT HINGE ARM IAW CRJ 200 AMM 52-22-00-820-804, STEPS 3 B1, E. REQUIRES INSTALL, FIT AND CLEARANCE CHECK. FIT AND CLEARANCE CHECK OF CREW ESCAPE HATCH IAW CRJ 200 AMM 52-22-00-220-802. CREW ESCAPE HATCH REQUIRES INSTALLATION.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 14,667 hrs · 12,132 cycles

TWO EXTERIOR EMERGENCY LIGHTS INOP ON RIGHT SIDE OF A/C.

Part: PIN — CORRODED (LT MLG) · airframe 14,438 hrs · 11,948 cycles

LT GEAR SIDE STAY PIN CORRODED.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 14,438 hrs · 11,948 cycles

REAR PRESSURE BULKHEAD CRACK UNDER LINEAR FITTING OF CARGO DOOR SURROUNDING STRUCTURE, REO 601R-53-61-1230 TO BE C/OUT.

Part: ANCHOR FITTING — CRACKED (AIRSTAIR DOOR) · airframe 14,350 hrs · 11,871 cycles

ASD FWD ANCHOR FITTING CRACKED. FLT 4673 DEL 206 MINS.

Part: FLAP — MALFUNCTIONED (WING) · airframe 14,197 hrs · 11,746 cycles

FLAPS FAIL CAUTION MESSAGE DURING CRUISE. THE FLAPS WERE AT 0 DEGREES. THERE WERE NO CHANGES ON THE ON THE FLAP SELECTOR. A NO FLAP APPROACH AND LANDING WERE DONE. REPEAT WRITE-UP. TOWER DECLARED EMERGENCY. EMERGENCY EQUIPMENT ON STANDBY.

Part: DETECTION SYS — FAULTED (TE FLAPS) · airframe 14,157 hrs · 11,709 cycles

FLAP FAIL CAUTION MSG AN DESCENT WITH FLAPS SET TO ZERO. FOUND SKEW DETECTION UNIT AT FAULT. EMERGENCY EQUIPMENT ROLLED AS A PRECAUTION. FLT 9970 DEL 370 MINS. NC FLTS 4583, 4652 CX. SKEW DETECTION SYSTEM.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 13,682 hrs · 11,342 cycles

CAPT'S FLASHLIGHT INOP (DIM).

Part: POWER LEVER — STUCK (COCKPIT) · airframe 13,433 hrs · 11,131 cycles

ON DEPARTURE THE LEFT THRUST LEVER WAS STUCK AT TAKEOFF POWER AND WOULD NOT COME BACK. THE N1 WAS SET AT T/O POWER FOR ABOUT 25 MINUTES. AFTER APPROX 20 MINUTES, GOT IT TO COME BACK TO CRUISE POWER. EMERGENCY DECLARED. FLT 4534 DEL 20 MINS.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 13,221 hrs · 10,954 cycles

FLAPS FAIL ZERO POSITON IN FLT 30000 FT, EMERGENCY DECLARED, FLT 4338 DEL 37 MINS. [07-06-07] INSPECTED FLAPS, INTERROGATED FECU & RESET SYSTEM. RESET OK, C/W EO 600-27-0054 A/C OK FOR SERVICE. MOVED TO MCO #044318, PRIORITY 1 REQUIRE C/W OF EO 600-27-0054 WITHIN 72 HRS. C/W EO600-27-0054-01

Part: BEAM — CRACKED (FUSELAGE) · airframe 12,024 hrs · 10,050 cycles

BOX BEAM CRACKED AT UPPER CENTER LOCATION. PERFORMED EDDY CURRENT INSPECTION OF UPPER BOX BEAM JUST FWD OF FIRE LOOP STAND OFF CLIP PER MTC REQUEST IAW CRJ 200 NDTM PART 1. 51-20-06. BOX BEAM IS CRACKED AT UPPER CENTER LOCATION. REMOVED UPPER FIRE BOTTLE BRACKET FOM PER CRJ 200 SRM 51-42-06. INSTALLED ALL REPAIR FASTNERS, INSTALLED FIRE BOTTLE BRACKET IAW REO #601R-53-61-345 AND REO #601R53-61-530 JOB COMPLETE MS 7022223. CLOSED 12/29/06

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT) · airframe 11,768 hrs · 9,851 cycles

FWD EMERGENCY LIGHT LUMINESCENT INVERTER INOP.

Part: HANDLE — CRACKED (E/E BAY DOOR) · airframe 11,716 hrs · 9,808 cycles

AVIONIC DOOR HANDLE IS CRACKED AROUND BOSS. REMOVED AND REPLACED AVIONICS DOOR HANDLE IAW CRJ200 AMM 52-42-00 AND SRM 51-42-06 (CLOSED 11/06/06)

Part: HANDLE — CORRODED (ESCAPE HATCH) · airframe 11,716 hrs · 9,808 cycles

CREW OVHD ESCAPE HATCH OUTER HANDLE SHAFT IS VERY CORRODED. REMOVED AND REPLACED HANDLE ASSY ON OVHD CREW HATCH IAW CRJ 200 SRM 51 42 06 RIG AND OPS CHECK C/W SATISFACTORY (CLOSED 11/03/06)

Part: ATTACH FITTING — CRACKED (BS 280) · airframe 11,716 hrs · 9,808 cycles

LEFT I/B FUSELAGE STA 280 CLIP CRACKED.

Part: LIGHT — DAMAGED (CABIN) · airframe 11,716 hrs · 9,808 cycles

EMERGENCY LIGHT ON F/A STATION IS DAMAGED. REMOVED AND REPLACED EMERGENCY LIGHT ON F/A STATION IAW CRJ200 33-50-00.WPW15097. (CLOSED 11/01/06)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 10,928 hrs · 9,198 cycles

FWD FLOOR EMERGENCY LT TRACK LIGHT INOP.

Part: STEP — CRACKED · airframe 10,404 hrs · 8,797 cycles

FOUND CRACK UNDER TOP STEP ON ASD AFT SIDE.

Part: CARBON SEAL — DETERIORATED (RT ENGINE)

DURING CLIMB OUT, AT APPROX 28,000 FT THE CREW NOTED THE RT ENGINE OIL PRESSURE DROPPED BELOW 25 PSI. THE QRH WAS COMPLIED WITH AND THE CREW BROUGHT THE RT ENGINE BACK TO IDLE. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED, WHERE A SINGLE LANDING WAS PERFORMED SAFELY. MAINTENANCE REMOVED AND REPLACED THE CARBON SEALS IN THE RT ENGINE ACCESSORY GEARBOX IAW AMM. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: LAMP — BURNED OUT (FUSELAGE)

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

Part: HANDLE — CRACKED (PAX DOOR)

DURING A HANGAR INSPECTION IN MCN, THE PASSENGER DOOR OUTER HANDLE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR OUTER HANDLE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: WARNING LIGHT — ILLUMINATED (THRUST REVERSER)

DURING CRUISE FROM GRR-ATL, THE CREW RECEIVED A RIGHT ENGINE THRUST REVERSER DEPLOY LIGHT. THE QRH WAS COMPLIED WITH AND THE CREW DECLARED AN EMERGENCY. THE AIRCRAFT DIVERTED INTO FWA WHERE IT LANDED SAFELY. MAINTENANCE DEFERRED THE RIGHT THRUST REVERSER IAW MEL NR 78-30-01, CAT C, EXPIRING 12-6-05. (M)

Part: RELAY — MALFUNCTIONED (EMERGENCY LIGHTS)

DURING A GROUND INSPECTION IN RDU, THE EMERGENCY LIGHTS REMAINED ON WITH AN ESS AC BUSS CAUTION MESSAGE. MAINTENANCE REMOVED AND REPLACED THE K1XD RELAY. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

DURING AN OVERNIGHT INSPECTION IN VPS, THE OVERHEAD EMERGENCY LIGHT AT ROW 4 WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE OVERHEAD EMERGENCY LIGHT AT ROW 4. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: TIRE — FAILED (MLG)

FLT 4456 - DURING CLIMB-OUT FROM ATL-ICT, THE TOWER ADVISED THE CREW THAT TIRE DEBRIS WERE FOUND ON THE RUNWAY FOLLOWING THEIR TAKEOFF. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO ATL AND LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED BOTH RIGHT MAIN LANDING GEAR (MLG) WHEEL ASSEMBLIES AND THE RIGHT INBOARD MAIN FLAP ASSEMBLY. MAINTENANCE ALSO BOROSCOPED THE RIGHT ENGINE FOR POSSIBLE FOD. NO SIGNS OF ANY FOD WAS NOTED. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: FLOOR SUPPORT — CRACKED (FUSELAGE)

DURING A C-CHECK IN HOT, THE FLOOR SUPPORT ANGLE AT FS 621 RIGHT WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE FLOOR SUPPORT ANGLE AT FS 621 RIGHT IAW ASA EO 600-53-0105. (M)

Part: SUPPORT BEAM — CRACKED (ENGINE) · airframe 7,711 hrs

DURING A C-CHECK, THE ENGINE SUPPORT BEAM LOWER BEW AT BL 36.20 LT AND RT WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE ENGINE SUPPORT BEAM LOWER WEB AT BL 36.20 LT AND RT IAW EO. (K)

Part: SUPPORT BEAM — CRACKED (ENGINE)

DURING HANGAR MAINTENANCE, THE ENGINE SUPPORT BEAM LOWER WEB, BL 36.20 RT AND LT SIDE WAS FOND TO BE CRACKED BEYOND LIMITS. (S) MAINTENANCE PERFORMED THE PERMANENT REPAIR TO THE ENGINE SUPPORT BEAM LOWER WEB, BL 36.20 RT AND LT SIDE IAW EO. (K)

Part: SUPPORT BEAM — CRACKED (ENGINE)

DURING HANGAR MAINTENANCE IN BTR, THE ENGINE SUPPORT BEAM LOWER WEB, BL 36.20 RT AND LT SIDE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS PERFORMING A TEMPORARY REPAIR TO THE ENGINE SUPPORT BEAM LOWER WEB, BL 36.20 RT AND LT SIDE IAW BOMBARDIER RO NR 601R-53-61-361. (M)

Part: LAMP — BURNED OUT (EMERGENCY LIGHT)

FLT 4242 - DURING A GROUND INSPECTION IN BTR, THE FORWARD EMERGENCY CEILING LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD EMERGENCY CEILING LIGHT LAMP. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: PANEL — CRACKED (PAX DOOR)

DURING A C-CHECK IN MCN, THE PASSENGER DOOR LOWER PANEL ON THE TOP STEP DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE TOP STEP LOWER PANEL ASSEMBLY ALONG WITH THE LOWER HINGE. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: STEP — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE TOP AND BOTTOM PASSENGER DOOR STEPS WERE FOUND CRACKED. MAINTENANCE IS REMOVING AND REPLACING THE TOP AND BOTTOM PASSENGER DOOR STEPS. (M)

Part: FLOOR SUPPORT — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE CARGO AFT WALL FLOOR SUPPORT ANGLE AT FS 621 ON THE LEFT SIDE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CARGO AFT WALL FLOOR SUPPORT ANGLE AT FS 621 ON THE LEFT SIDE IAW ASA EO 600-53-0105. (M)

Part: INTERCOSTAL — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE INTERCOSTAL AT FS 621-625, NEAR STRINGER 14L WAS FOUND CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE INTERCOSTAL AT FS 621-625, NEAR STRINGER 14L IAW SRM 51-40. (M)

Part: CONTROL UNIT — INOPERATIVE (STAB TRIM)

FLT 4295 - DURING CLIMB-OUT FROM DFW-JAX, THE STABILIZER AND MACH TRIMS DISENGAGED AT APPROXIMATELY 400 FEET. QRH PROCEDURES WERE COMPLIED WITH AND AN EMERGENCY WAS DECLARED. THE AIRCRAFT RETURNED TO DFW AND LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE HORIZONTAL STABILIZER TRIM CONTROL UNIT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: BULB — BURNED OUT (EMERGENCY LIGHT)

FLT 4414 - DURING A GROUND INSPECTION IN MGM, THE RIGHT WING FORWARD EMERGENCY LIGHT WAS FOND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE RIGHT WING FORWARD EMERGENCY LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: SMOKE — DETECTED (CABIN)

FLT 4017 - DURING CLIMB-OUT FROM MCN-ATL, THE CREW RECEIVED A LAVATORY SMOKE MESSAGE AND THE CABIN FILLED WITH SMOKE. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO MCN, LANDING SAFELY. MAINTENANCE PERFORMED GROUND RUNS AT POWER WITH THE ENGINE BLEEDS ON AND NO SMOKE REOCCURRED. MAINTENANCE SUSPECTED RESIDUAL GLYCOL FROM A PRIOR COMPRESSOR WASH CAUSED THE SMOKE DURING CLIMB-OUT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)