N838AS

Part: LIGHT — FAILED (PAX DOOR) · airframe 33,986 hrs · 31,081 cycles

ASD HANDLE BETA LIGHT FAILED FUNCTIONAL TEST. REMOVED ASD HANDLE BETA LIGHT IAW AMM 33-51-09-000-801. INSTALLED SERVICEABLE BETA LIGHT ON ASD HANDLE IAW AMM 33-51-09.

Part: SKIN — BURNED (BS 235-250) · airframe 33,986 hrs · 31,081 cycles

BURN ON SKIN BETWEEN BS 235 - 250 AND BETWEEN STRINGERS 22L AND 23L. COMPLIED WITH REO 601R-53-00-115.

Part: SKIN — DAMAGED (WING) · airframe 33,986 hrs · 31,081 cycles

FASTENER HOLE IN LOWER WING PLANK IS PREVIOUSLY OVERSIZE TO .339. REPAIRED IAW REO 601R-57-21-2014. MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (BS 409) · airframe 33,986 hrs · 31,081 cycles

LT SIDE WALL SEAT TRACK CORRODED AT FS 409.16-409.112. R & R SEAT TRACK IAW SRM 51-40-11-00, AMM 53-01-11-000-802, AND 53-01-11-400-802.

Part: BULKHEAD — DAMAGED · airframe 33,986 hrs · 31,081 cycles

TOOL DAMAGE AT LBL 9.0 WL 95.5 BEHIND ISOLATOR AFT PRESSURE BULKHEAD FWD FACE. REPAIRED IAW REO 601R-53-31-4206, REV C. MAJOR REPAIR

Part: SEAT TRACK — CORRODED (BS 544-559) · airframe 33,986 hrs · 31,081 cycles

RT SIDE WALL SEAT TRACK CORRODED AT BS 544- 559+80. REMOVED SEAT TRACK IAW AMM 53-01-11-000-802. INSTALLED NEW SEAT TRACK IAW AMM 53-01-11-400-802.

Part: BULKHEAD — DAMAGED · airframe 33,986 hrs · 31,081 cycles

TOOL DAMAGE AT RBL 9.0, WL 94.5 BEHIND ISOLATOR AFT PRESSURE BULKHEAD FWD FACE. REPAIRED IAW REO601R-53-61-4206, REV C. MAJOR REPAIR

Part: SEAT TRACK — CORRODED (BS 499-544) · airframe 33,986 hrs · 31,081 cycles

LEFT SIDE WALL SEAT TRACK CORRODED AT FS 499-544. R & R SEAT TRACK IAW SRM 51-40-11-00, AMM 53-01-11-000-802, AND 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 554-559) · airframe 33,986 hrs · 31,081 cycles

LT SIDE WALL SEAT TRACK CORRODED AT FS 554-559+80. REMOVED THEN INSTALLED SERVICEABLE SEAT TRACK IAW AMM 53-01-11-000-802, 53-01-11-400-802 AND SRM 51-40-11.

Part: SEAT TRACK — CORRODED (BS 409) · airframe 33,986 hrs · 31,081 cycles

RT SIDE WALL SEAT TRACK CORRODED AT FS 409+16-409.00+112. REMOVED THEN INSTALLED NEW SEAT TRACK IAW AMM 53-01-11-000-802, 53-01-11-400-801 AND SRM 51-40-11.

Part: SEAT TRACK — CORRODED (BS 409-449) · airframe 33,986 hrs · 31,081 cycles

LT SIDE WALL SEAT TRACK CORRODED AT FS 409+112-449.85. R & R SEAT TRACK IAW SRM 51-40-11-00, AMM 53-01-11-000-802, AND 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 349-409) · airframe 33,986 hrs · 31,081 cycles

SEAT TRACK CORRODED AT FS 349-409+16. R & R SEAT TRACK IAW SRM 51-40-11-00, AMM 53-01-11-000-802, AND 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 409-449.85) · airframe 33,986 hrs · 31,081 cycles

RT SIDE WALL SEAT TRACK CORRODED AT FS 409-449.85. R & R SEAT TRACK IAW SRM 51-40-11-00, AMM 53-01-11-000-802, AND 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 449-499) · airframe 33,986 hrs · 31,081 cycles

LT SIDE WALL SEAT TRACK CORRODED AT FS 449.85-499. R & R SEAT TRACK IAW AMM 53-01-11-000-802 & 53-01-11-400-802.

Part: INTERCOSTAL — CRACKED (CARGO DOOR) · airframe 33,986 hrs · 31,081 cycles

CARGO DOOR, LOWER AFT CORNER INTERCOSTAL CRACKED. REMOVED CRACKED INTERCOSTAL AND DRILLED SERVICABLE, NEW, INTERCOSTAL TO FIT IAW SRM 51-40-00 AND 51-40-11. INSTALLED INTERCOSTAL IAW SRM 51-42-06 AND 51-42-21.

Part: BRACKET — CRACKED (CARGO DOOR) · airframe 33,986 hrs · 31,081 cycles

CARGO DOOR FWD LOWER SUPPORT BRACKET CRACKED. REMOVED SUPPORT BRACKET IAW SRM 51-42-06. INSTALLED SUPPORT BRACKET IAW SRM 51-42-06 AND DWG 601R35050.

Part: ISOLATOR — BROKEN (BULKHEAD) · airframe 33,986 hrs · 31,080 cycles

BROKEN ISOLATOR FOUND ON AFT PRESSURE BULKHEAD FWD FACE. R & R ISOLATOR IAW SRM 51-42-06-00 AND SRM 51-42-13-00.

Part: STIFFENER — CRACKED (RT WING) · airframe 33,986 hrs · 31,081 cycles

CRACK FOUND ON STIFFENER ON INTERIOR OF RT WING L/E AT ACCESS PANEL CUT-OUT 630CZ. REMOVED DAMAGED EDGING/STIFFENER FROM RT WING LOWER L/E. DRILLED UP NEW PART IAW SRM 51-40-11. INSTALLED NEW EDGING ON RT L/E IAW SRM 51-42-13 AND 51-42-06 AND DWG NO PL601R12044.

Part: SUPPORT ANGLE — CRACKED (BS 621) · airframe 33,986 hrs · 31,081 cycles

CARGO TRACK SUPPORT ANGLE CRACKED AT LBL 27 AT FS 621 BELOW FLOOR AT WL 73.50. REMOVED SUPPORT ANGLE IAW SRM 51-77-00 AND 51-42-21. INSTALLED NEW SUPPORT ANGLE IAW SRM 51-77-00+51-42-21.

Part: STIFFENER — CRACKED (LT WING) · airframe 33,986 hrs · 31,081 cycles

STIFFENER ON THE INTERIOR OF THE LT WING L/E AT PANEL 530DZ IS CRACKED. REMOVED DAMAGED EDGING FROM WING L/E WS 149.58 TO 247.95 IAW SRM 51-42-06 AND 51-42-13. DRILLED NEW PART IAW SRM 51-40-11. INSTALLED NEW EDGING ON LT WING L/E IAW SRM 51-42-13 AND 51-42-06 AND DWG NR PL601R12044.

Part: ANGLE — CRACKED (BS 621) · airframe 33,986 hrs · 31,081 cycles

ANGLE CRACKED BELOW AFT CARGO DOOR PULLEY BRACKET AT FS 621. REMOVED ANGLE IAW SRM 51-42-21 AND INSTALLED NEW ANGLE IAW SRM 51-42-21, 51-42-02 AND DWG 601R35050.

Part: BRACKET — CRACKED (BS 718) · airframe 33,986 hrs · 31,081 cycles

LT BRACKET CRACKED AT FS 718, BELOW STR 11L. REPAIRED IAW REO 601R-53-61-5060.

Part: BRACKET — CRACKED (BS 484) · airframe 33,986 hrs · 31,081 cycles

CRACKED BRACKET INBD SIDE FS 484, LBL 27. R & R BRACKET IAW SRM 51-42-21.

Part: INTERCOSTAL — CRACKED (BS 621) · airframe 33,986 hrs · 31,081 cycles

INTERCOSTAL CRACKED ON AFT SIDE PRESSURE BULKHEAD AT FS 621, STR 14L. R & R INTERCOSTAL IAW SRM 51-42-20-00 DWG NR 601-35012.

Part: INTERCOSTAL — CRACKED (BS 621) · airframe 33,986 hrs · 31,081 cycles

INTERCOSTAL CRACKED ON AFT SIDE PRESSURE BULKHEAD AT FS 621 STR 14R. REMOVED & INSTALLED NEW INTERCOSTAL IAW SRM 51-42-20 DWG 601-35012.

Part: LIGHT — BROKEN (GALLEY) · airframe 33,986 hrs · 31,081 cycles

GALLEY CLOSE OUT PANEL HAS BROKEN EMERGENCY EXIT LIGHT. R & R EMERGENCY LIGHT SIGN ON GALLEY CLOSE OUT PANEL IAW AMM 33-51-13-000-801/33-51-13-400-801. EMERGENCY LIGHTS CHECKED GOOD IAW AMM 33-51-00-710-801.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 33,986 hrs · 31,081 cycles

RT CABIN FLOOR SUPPORT CORRODED FS 409 TO 559. BLENDED CORROSION DAMAGE IAW SRM 51-21-06-00. REPAIRED IAW REO 601R-53-41-666.

Part: SILL — CORRODED (CARGO DOORWAY) · airframe 33,986 hrs · 31,081 cycles

CARGO DOOR SILL CORRODED BS 574 -621. REMOVED CORROSION IAW SRM 51-21-06. FOUND OUT OF LIMITS IAW SRM 53-61-23, TR 53-27, FIG 10Z. MAJOR REPAIR.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 33,986 hrs · 31,081 cycles

LEFT CABIN FLOOR SUPPORT CORRODED FS 409 TO 559. REPAIRED IAW REO 601R-53-41-666. MAJOR REPAIR.

Part: HINGE FITTING — GOUGED (LT WING TE FLAP) · airframe 33,986 hrs · 31,081 cycles

LT INBD FLAP, INBD HINGE, LOWER OUTBD LUG GOUGED ON OTBD SIDE. BLENDED DAMAGE IAW SRM 51-12-00, REMOVED .007" MATERIAL IN DAMAGED AREA OF LT INBD FLAP, INBD HINGE LOWER OTBD LUG ORIGINAL THICKNESS .390". MAJOR REPAI2.

Part: FITTING — CRACKED (DOOR ACTUATOR) · airframe 33,986 hrs · 31,081 cycles

NLG DOOR ACTUATOR FITTING CRACKED AT LOWER SECTION. REMOVED RT DOOR MECHANISM ASSY IAW AMM 32-22-14-000-801 BUILT UP DOOR MECHANISM ASSY IAW ACMM 32-30-20 INSTALLED RT NLG DOOR MECHANISM IAW AMM 32-22-15-400-801. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW ASA SOP 5702.

Part: SKIN — BURNED (BS 235-250) · airframe 33,986 hrs · 31,081 cycles

BURN ON SKIN BETWEEN FS 235 - 250 AND STRINGERS 22L AND 23L. REPAIRED IAW SRM 51-42-13 AND GREO 601R-53-00-115 REV E. MAJOR REPAIR.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 33,361 hrs · 30,419 cycles

EMERGENCY OVERWING EXIT LIGHT ON THE RT SIDE. GLASS BROKEN. REINSTALLED RT EMERGENCY LIGHT COVER ON EXIT. FUSELAGE BACK INTO PLACE IAW AMM 33-51-21. OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,868 hrs · 29,897 cycles

RT MIDDLE EXTERIOR EMERGENCY LIGHT INOPERATIVE.

Part: STRUCTURE — CRACKED (RT WING) · airframe 32,210 hrs · 29,238 cycles

RT WING CRACKED AT WS 148 AT REAR SPAR, CONFIRMED BY EDDY CURRENT. REPAIRED IAW REO 601R-57-21-1794, REV A, REO 601R-57-21-130-01, REO 601R-57-21-130, REV J DATED 03/08/2011, REO 601R-57-21-131, AND IAW REO 601R-57-21-131, REV A DATED 08/29/2011.

Part: SENSOR — FAILED (PAX DOOR) · airframe 30,844 hrs · 27,756 cycles

PAX DOOR OUT HANDLE CAUTION MESSAGE IN FLIGHT. DIVERTED, & EMERGENCY DECLARED. R & R PAX DOOR OUTER HANDLE SENSOR PS2MB IAW AMM 52-70-04, OPS CHECKED GOOD.

Part: WEB — CRACKED (BS 280) · airframe 30,012 hrs · 26,864 cycles

FS 280 WEB HAS A 1.5" LONG CRACK AT LBL 9.0. REO 601R-53-11-2208, REV HAS BEEN ACCOMPLISHED.

Part: FLOOR SUPPORT — CORRODED (BS 439-449) · airframe 30,005 hrs · 26,854 cycles

CORRODED FLOOR SUPPORT BETWEEN FS 439.00 AND FS 449.85 LBL 42.00. COMPLIED WITH EC/TC REO 601R-53-41-666 AND REO 601R-53-41-666, REV B.

Part: SKIN — CORRODED (BS 559) · airframe 30,005 hrs · 26,853 cycles

FUSELAGE BELLY SKIN HAS APPROX 20 RIVETS WITH CORROSION AROUND THEM AT FS 559.1 FS 559+18, STRINGER 25L - 25R. REPAIRED IAW REO 601R-53-00-440.

Part: SKIN — CORRODED (BS 559-574) · airframe 30,005 hrs · 26,853 cycles

FUSELAGE BELLY SKIN HAS HEAVY CORROSION AROUND FASTENERS AT FS 559+80 - 574 S25L - 25R. REPAIRED IAW REO 601R-53-00-440.

Part: SILL — CORRODED (BS 310-349) · airframe 30,005 hrs · 26,853 cycles

PASSENGER DOOR LOWER SILL ANGLE IS CORRODED ON INBD SIDE AROUND FASTENERS AND PROXIMITY SENSOR FS 310 - 349. REPAIRED IAW SRM 51-27-19.

Part: FRAME — CORRODED (BS 605) · airframe 30,005 hrs · 26,853 cycles

FUSELAGE FRAME AT FS 605 IS CORRODED BETWEEN STR 25 LT & RT. REPAIRED IAW ALL SRM`S.

Part: WEB — CRACKED (BS 280) · airframe 30,005 hrs · 26,853 cycles

FS 280 WEB HAS A 1.5 INCH LONG CRACK AT LBL 9.0. REPAIRED IAW REO 601R-53-11-2208.

Part: FRAME — CORRODED (BS 605) · airframe 30,005 hrs · 26,853 cycles

FUSELAGE FRAME AT FS 605 IS CORRODED. BETWEEN S25 LT & RT. REPAIRED IAW ALL SRM`S.

Part: WEB — CRACKED (BS 280) · airframe 30,005 hrs · 26,853 cycles

FS 280, WEB HAS A 1.5 INCH LONG CRACK AT LBL 9. REPAIRED IAW SRM 51-42-13.

Part: SUPPORT ANGLE — CRACKED (LT WING SKIN) · airframe 30,005 hrs · 26,853 cycles

LT WING INBD AFT PANEL SUPPORT ANGLE CRACKED ON AFT TOP SIDE FAR INBD SUPPORT ANGLE. R & R ANGLE IAW SRM 51-42-21. THIS REPAIR IS CLASSIFIED AS A MINOR REPAIR.

Part: FLOORBEAM — CORRODED (BS 349) · airframe 30,005 hrs · 26,853 cycles

FLOORBEAM AT FS 349 IS CORRODED BETWEEN RBL 36 AND RBL 45. REPAIRED IAW REO 601R-53-21-2185.

Part: SILL — CORRODED (BS 521-544) · airframe 30,005 hrs · 26,853 cycles

FOUND CORROSION BETWEEN FS 521.00 AND 544.00 NEAR LBL 42.00 ON SILL ANGLE AND SILL PANEL. REMOVED CORROSION IAW REO 601R-53-41-666, SECTION 1.2A & 2.2A. PERFORMED EDDY CURRENT IAW REO 601R-53-41-666. NO INDICATIONS NOTED. APPLIED PROTECTIVE TREATMENT IAW REO 601R-53-41-666, SECTIONS 1.2 & 2.2 STEPS D-F.

Part: FLOOR PANEL — CORRODED (BS 439-449.85) · airframe 30,005 hrs · 26,853 cycles

FOUND CORROSION BETWEEN FS 439 & 449.85 NEAR LBL 42.00 ON FLOOR PANEL. REMOVED CORROSION IAW REO 601R-53-41-666. REMAINING THICKNESS, 0.045" SECTION 1.2A. PERFORMED EDDY CURRENT IAW REO 601R-53-41-666. NO INDICATIONS NOTED. APPLIED PROTECTIVE TREATMENT IAW REO 601R-53-41-666, STEPS D-F, SECTION 1.2.

Part: SILL — CORRODED (BS 521-544) · airframe 30,005 hrs · 26,853 cycles

FOUND CORROSION BETWEEN FS 521 & FS 544 NEAR LBL 42 ON SILL ANGLE & SILL PANEL. REPAIRED IAW REO 601R-53-41-666.

Part: SILL — CORRODED (BS 461-513) · airframe 30,005 hrs · 26,853 cycles

FOUND CORROSION BETWEEN FS 461 & 513 NEAR LBL 42 ON SILL ANGLE & FLOOR SILL PANEL. REMOVED AND REPLACED IAW REO 601R-53-41-666.

Part: SILL — CORRODED (BS 461-513) · airframe 30,005 hrs · 26,853 cycles

FOUND FURTHER CORROSION BETWEEN FS 461 & 513 NEAR LBL 42.00 ON SILL ANGLE & FLOOR SILL PANEL. REMOVED CORROSION FROM SILL ANGLE IAW REO 601R-53-41-666 SECTION 1.2A & 2.2A. PERFORMED EDDY CURRENT IAW REO 601R-53-41-666B. NO INDICATIONS NOTED. RESTORED PROTECTIVE TREATMENT IAW REO 601R-53-41-666, SECTIONS 1.2 & 2.2 STEPS D-F.

Part: SILL — CORRODED (BS 424) · airframe 30,005 hrs · 26,853 cycles

PRESSURE FLOOR SILL UPPER SURFACE CORRODED BETWEEN RBL 36 AND RBL 42, NEAR FS 424.00 0N FLOOR SILL ANGLE. REPAIRED IAW REO 601R-53-41-1484.

Part: SPAR — CRACKED (RT WING) · airframe 30,005 hrs · 26,853 cycles

UPON REMOVAL OF RT T/E SKIN PANEL, FOUND CAP ANGLE CRACKED. REMOVED DAMAGED RT T/E SKIN PANEL CAP ANGLE IAW SRM 51-42-21. LOCATED AND DRILLED UP NEW SERVICEABLE CAP ANGLE IAW SRM 51-40-11 AND INSTALLED SAME IAW SRM 51-42-21. THIS REPAIR REQUIRES MAJOR/MINOR CLASSIFICATION IAW ASA SOP 5702. THIS REPAIR IS CLASSIFIED AS A MINOR REPAIR IAW ASA SOP 5702. (SDR CLOSED)

Part: FRAME — CORRODED (BS 379) · airframe 30,005 hrs · 26,853 cycles

FRAME 379, BETWEEN STR 22 & 23R UNDER DCU NR 2 HAS CORROSION.

Part: FRAME — CORRODED (BS 605 S25L/R) · airframe 30,005 hrs · 26,853 cycles

FRAME AT FS 605 IS CORRODED BETWEEN S25L & 25R. REMOVED FRAME SECTION IAW SRM 51-42-06 AND SRM 51-42-21. INSTALLED NEW FRAME IAW SRM 51-42-06 AND 51-42-21.

Part: FLOORBEAM — CORRODED (BS 559) · airframe 30,005 hrs · 26,853 cycles

LEFT FS 559 FLOORBEAM BETWEEN LBL 27 & LBL 45 CORRODED. REMOVED CORROSION IAW SRM 51-21-06, MAT REMOVED WAS .005".

Part: BULKHEAD — CRACKED (AFT) · airframe 30,005 hrs · 26,853 cycles

FOUND REAR PRESSURE BULKHEAD WEB HAS INDICATION NOTED AT LBL 27.50, WL 130 APPROX .3" IN LENGTH 90 PERCENT FSH. FAILED NDT INSPECTION. REPAIRED REAR PRESSURE BULKHEAD WEB IAW REO 601R-53-61-1541.

Part: FRAME — CORRODED (BS 319.7) · airframe 30,005 hrs · 26,853 cycles

FRAME 319.70 CORRODED BETWEEN S26 AND 27R. REMOVED CORROSION, REMOVED 0.002" OF MATERIAL IAW SRM 51-21-06, SRM 51-42-06.

Part: SILL — CORRODED (BS 319) · airframe 30,005 hrs · 26,853 cycles

SERVICE DOOR SILL AT FS 319 IS CORRODED. REMOVED AND REPLACED DOOR SILL IAW SRM 51-42-06 AND SRM 51-42-13.

Part: SILL — CORRODED (BS 319-349) · airframe 30,005 hrs · 26,853 cycles

SERVICE DOOR LOWER SILL ANGLE HAS SEVERAL AREAS OF CORROSION BETWEEN FS 319 & FS 349. REMOVED AND REPLACED SILL ANGLE IAW SRM 51-42-21, 51-42-06, & 51-42-12.

Part: FRAME — CORRODED (BS 379 S22-23R) · airframe 30,005 hrs · 26,853 cycles

FRAME 379, BETWEEN S22-23R UNDER DCU NR2 HAS CORROSION. BLEND OUT CORROSION ON FRAME. REMOVED 0.004" MATERIAL FROM 0.050" ORIGINAL THICKNESS OF FRAME MATERIAL AND REMAINING 0.046"" MATERIAL, WITHIN LIMITED ALLOWANCES IAW SRM 51-21-06. INSTALLED FRAME IAW SRM 51-42-21 AND SRM 51-42-06.

Part: SILL — CORRODED (BS 461) · airframe 30,005 hrs · 26,853 cycles

PRESSURE FLOOR SILL UPPER SURFACE CORRODED NEAR RBL 42 NEAR FS 461 ON FLOOR SILL DOUBLER. REMOVED CORROSION AND FOUND TO BE WITHIN REPAIRABLE LIMITS IAW REO 601R-53-41-666. 0.001" MAX MATERIAL REMOVED REMAINING THICKNESS OF 0.079". PERFORMED EDDY CURRENT IAW REO 601R-53-41-666N. NO INDICATIONS NOTED.

Part: BEAM — CORRODED (BS 349) · airframe 30,005 hrs · 26,853 cycles

FLOOR SUPPORT STRUCTURE TRANSVERSE BEAM AT FS 349 IS CORRODED AT LBL 45. REMOVED CORROSION ON BEAM AND FOUND TO BE WITHIN ALLOWABLE LIMTS IAW SRM 51-21-06. MAX MATERIAL REMOVED .005". ALODINED AREA IAW SRM 51-21-11. POINTED PREP IAW SRM 51-25-16.

Part: ISOLATOR — BROKEN (BULKHEAD) · airframe 30,005 hrs · 26,853 cycles

BROKEN ISOLATOR ON REAR PRESSURE BULKHEAD FWD FACE AT RBL 42.9 APPROX 26" ABOVE FLOOR. R & R ISOLATOR IAW SRM 51-42-13. REPAIR IS CLASSIFIED AS A MINOR REPAIR.

Part: STRINGER — CORRODED (BS 310-319.7) · airframe 30,005 hrs · 26,853 cycles

STRINGER 26R, BETWEEN FS 310 AND 319.70 CORRODED.

Part: FRAME — CORRODED (BS 310 S26-27R) · airframe 30,005 hrs · 26,853 cycles

FRAME 310 IS CORRODED BETWEEN STGR 27 AND 26R. REPLACED FRAME SECTOR IAW SRM 51-40-11, 51-42-06, AND 51-42-21.

Part: SILL — CORRODED (BS 445) · airframe 30,005 hrs · 26,853 cycles

PRESSURE FLOOR SILL UPPER SURFACE CORRODED NEAR LBL 42, NEAR FS 445 ON FLOOR SILL DOUBLER. REMOVED CORROSION, FOUND TO BE WITHIN REPAIRABLE LIMITS IAW REO 601R-53-41-666. 0.010 MAX MATERIAL REMOVED. REMAINING MATERIAL THICKNESS OF 0.070". PERFORMED EDDY CURRENT IAW REO 601R-53-41-666B. NO INDICATONS NOTED.

Part: BRACKET — CORRODED (BS 315-344) · airframe 30,005 hrs · 26,853 cycles

BRACKETS & CLEATS AT FS 315 & 344 WL 73.0 LBL 43 ARE CORRODED. INSTALLED BRACKETS TO CLEATS IAW SRM 51-42-06 AND 51-40-13.

Part: BEAM — CORRODED (BS 349) · airframe 30,005 hrs · 26,853 cycles

FLOOR SUPPORT STRUCTURE TRANSVERSE BEAM AT FS 349 IS CORRODED BETWEEN RBL 36 & RBL 45. LOCATED & DRILLED NEW TRANSVERSE BEAM IAW SRM 51-40-06 & SRM 51-40-11. INSTALLED TRANSVERSE BEAM IAW SRM 51-42-06 & 51-42-21.

Part: SILL — CORRODED (BS 424) · airframe 30,005 hrs · 26,853 cycles

PRESSURE FLOOR SILL UPPER SURFACE CORRODED BETWEEN RBL 36 & RBL 42 NEAR FS 424. REMOVED PAINT IAW AMM 51-26-00-150-803. FOUND AREA TO BE OUT OF LIMITS IAW REO 601R-53-41-666. REPAIRED IAW REO 601R-53-41-1484.

Part: SILL — CORRODED (BS 310-349) · airframe 30,005 hrs · 26,853 cycles

PAX DOOR LOWER SILL ANGLE IS CORRODED ON INBD SIDE AROUND FASTENERS AND PROX SENSOR FS 310 - 349. REMOVED SILL IAW SRM 51-42-06, 51-42-13 AND 51-42-21. LOCATED, DRILLED AND ASSEMBLED NEW SILL ANGLE IAW SRM 51-42-06 AND 51-42-13. INSTALLED PAX SILL ANGLE IAW 200 51-42-06 AND 51-42-21 AND 51-42-13.

Part: SILL — CORRODED (BS 424) · airframe 30,005 hrs · 26,853 cycles

PRESSURE FLOOR SILL UPPER SURFACE CORRODED BETWEEN LBL 36 & LBL 42, NEAR FS 424.00 ON FLOOR SILL ANGLE. REMOVED CORROSION, FOUND TO BE WITH A REPAIRABLE LIMITS IAW REO 610R-53-41-666. PERFORMED EDDY CURRENT IAW REO 610R-53-41-666B. NO INDICATIONS NOTED.

Part: SILL — CORRODED (BS 473) · airframe 30,005 hrs · 26,853 cycles

PRESSURE FLOOR SILL UPPER SURFACE CORRODED 2 LOCATIONS NEAR LBL 42, NEAR FS 473 ON FLOOR SILL ANGLES. FOUND TO BE OUT OF REPAIRABLE LIMITS IAW REO 601R-53-41-666, BLEND AREAS MEASURE 0.020" OF DEEPEST LOCATION AFTER CORROSION REMOVAL REMAINING THICKNESS 0.035". CUT OUT DAMAGE IAW REO 601R-53-41-1486. PERFORMED NDT INSPECTION IAW NDTM PT 1 51-20-06. NO INDICATIONS NOTED. FABRICATED REPAIR PARTS IAW REO 601R-53-41-1486 STEPS 4-8 P1. INSTALLED ALL REPAIR IAW REO 601R-53-41-1486, STEPS 9-11 P1.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 30,005 hrs · 26,853 cycles

SEAT TRACK AT RBL 9 CORRODED FROM FS 559+4 TO FS 559+80. REPLACED CORRODED SEAT TRACKS IAW AMM 53-01-11-400-802 STEP 3B.

Part: SEAT TRACK — CORRODED (BS 399.5-409) · airframe 30,005 hrs · 26,853 cycles

CABIN SEAT TRACK AT RBL 9 CORRODED FROM FS 399.5 - 409+126. REMOVED SEAT TRACK IAW AMM 53-01-11-802, STEP 3B. INSTALLED NEW SEAT TRACK IAW AMM 53-01-11-420-001.

Part: SKIN — CORRODED (BS 559) · airframe 30,005 hrs · 26,853 cycles

FUSELAGE BELLY SKIN HAS APPROX 20 RIVETS WITH CORROSION AT FS 559.00+10 - 559.00+18, S25L-25R. REPAIRED IAW REO 601R-53-00-440.

Part: SEAT TRACK — CORRODED (BS 409-559) · airframe 30,005 hrs · 26,853 cycles

SEAT TRACK AT LBL 9 CORRODED FROM FS 409+126 - 559+4. REMOVED SEAT TRACK IAW AMM 53-01-11-000-802. DRILLED & COUNTERSUNK NEW SERVICEABLE SEAT TRACK IAW SRM 51-40-11, STEPS 3A & 6AB. INSTALLED NEW SERVICEABLE SEAT TRACK IAW AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 364-399.5) · airframe 30,005 hrs · 26,853 cycles

CABIN SEAT TRACK AT LBL 9 CORRODED FROM FS 364 TO FS 399.5. REPLACED RT SEAT TRACK IAW AMM TASK 53-01-11-400-802, STEP 3B.

Part: SKIN — CORRODED (BS 559-574) · airframe 30,005 hrs · 26,853 cycles

FUSELAGE BELLY SKIN HAS HEAVY CORROSION AROUND FASTENERS AT FS 559.00+80 - 574, S25L-25R. REPAIRED AND PERFORMED EDDY CURRENT IAW STEP 3 IAW REO 601R-53-00-440. NO INDICATIONS NOTED.

Part: PAINT — BLISTERED (BS 319-349) · airframe 30,005 hrs · 26,853 cycles

FUSELAGE SKIN, NUTPLATES & NUTPLATE FASTENERS UNDER SERVICE DOOR SCUFF PLATE ARE CORRODED FS 319.70-349.00 JUST ABOVE S16AR, JUST BELOW S18R. FOUND NO EVIDENCE OF CORROSION, PAINT WAS BLISTERED IN AREAS IAW SRM 51-21-06 & 21-26-00.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 29,855 hrs · 26,687 cycles

NR7 EXTERIOR EMERGENCY LIGHT INOP. RELAMPED NR7 EXTERIOR EMERGENCY LIGHT IAW AMM 33-51-21. OPS CHECK GOOD. RELAMPED NR 7 EXTERIOR EMERGENCY LIGHT IAW AMM 33-51-21. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (ROW 10) · airframe 28,884 hrs · 25,619 cycles

EMERGENCY CEILING LIGHT AT ROW 10 INOP. R & R EMERGENCY CEILING LIGHT AT ROW 10 IAW AMM 33-51-16. OPS CHECKED GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 28,738 hrs · 25,441 cycles

RIGHT MIDDLE OVERWING EMERGENCY LIGHT INOP. RELAMPED RT MIDDLE OVERWING EMERGENCY LIGHT IAW AMM 33-51-01. OPS CHECK GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 28,518 hrs · 25,185 cycles

THE SECOND CEILING LIGHT IS INOP. REPLACED EMERGENCY LAMP. OPS CHECK GOOD IAW THE AMM CHAP 33-51-16.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,809 hrs · 24,358 cycles

RT 2ND FROM FRONT EXTERNAL EMERGENCY LIGHT INOP. R & R RT 2ND FROM FRONT EXT EMERGENCY LIGHT IAW AMM 33-51-21.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 27,590 hrs · 24,116 cycles

CAPT'S FLASHLIGHT INOP. REPLACED CAPT'S FLASHLIGHT. OPS CHECK GOOD. REF AMM 25-60-00.

Part: CIRCUIT BREAKER — ODOR (HYD PUMP) · airframe 27,565 hrs · 24,086 cycles

IN FLIGHT HEAVY ELECTRICAL OZONE SMELL. ODOR LASTED 5-10 SECONDS DID NOT RETURN NO CIRCUIT BREAKERS WERE POPPED ALL SYSTEMS NORMAL. R & R HYD PUMP NR 2 C/B AND TRU NR 1 C/B IAW AMM 20-23-00. OPS CK GOOD.

Part: MANIFOLD — INTERMITTENT (NLG STEERING) · airframe 27,515 hrs · 24,023 cycles

STEERING INOP CAUTION MSG AFTER GEAR EXTENSION COMPLIED WITH QRH, MSG CLEARED, EXTENDED GEAR AGAIN, MSG REAPPEARED 1 MINUTE LATER. CONTINUED WITH QRH, TURNED OFF NWS AND LT IT OFF, MSG CLEARED (EMERGENCY DECLARED -- TRUCKS STANDING BY AS A PRECAUTION) TS AND INTERPRETED MDC CODES TO FLAG ELECTRO HYD SERVO VALVE, ECU AND HYD MANIFOLD. R & R ELECTRO HYD SERVO VALVE IAW AMM 32-51-15. R & R HYD MANIFOLD IAW AMM 32-51-15. OPS AND LEAK CHECK GOOD. ALSO CYCLED GEAR.

Part: FRAME — CORRODED (BS 349) · airframe 26,398 hrs · 22,754 cycles

FOUND FRAME 349 LOWER SECTION TO BE CORRODED BEYOND ALLOWABLE LIMITS. REMOVED THE CORRODED LOWER SECTION OF FRAME AT FS 349, VISUALLY ENSURED THERE WAS NO UNDERLYING DAMAGE ON SKIN, LOCATED, AND DRILLED A NEW FRAME SECTION AT FS 349 IAW SRM 51-40-11. NEW FRAME SECTION REQUIRES INSTALLATION. INSTALLED NEW FRAME SECTION AT FS 349 IAW SRM 51-42-06 AND 51-42-21. FASTENERS REQUIRE PAINT. PAINTED FASTENERS AND APPLIED CPC IAW SRM 51-25-00 AND 51-21-11. FASTENERS REQUIRE PAINT ON EXTERIOR OF ACFT. PAINTED FASTENERS IAW SRM 51-25-01.

Part: FRAME — CORRODED (BS 333) · airframe 26,398 hrs · 22,754 cycles

FOUND THE FS 333 LOWER FRAME SECTION TO BE CORRODED BEYOND ALLOWABLE LIMITS.

Part: POST — CRACKED (BS 409) · airframe 26,398 hrs · 22,754 cycles

FS 409+128 VERTICAL POST AT RBL 18.0 HAS INDICATIONS NOTED ON BOTH I/B AND O/B C-CHANNELS AT THE UPPER JOGGLE (APPROX WL 65.0). INDICATIONS ARE 50% FSH AND APPROX 0.2" IN LENGTH. FAILS NDT INSPECTION AT THIS TIME. (INDICATIONS ARE IN THE AFT RADIUS OF BOTH C-CHANNELS). MARKED ON A/C. REMOVED FS 409+128 VERTICAL POST AT RBL 18 IAW SRM 51-42-06. INSTALLED NEW SERVICEABLE INBD AND OTBD RBL 18 POSTS AT FS 409+128 IAW REO 601R-53-41-889 AND SRM 51-42-06 AND 51-42-22.

Part: POST — CRACKED (BS 409) · airframe 26,398 hrs · 22,754 cycles

FS 409+128 VERTICAL POST AT LBL 18.0 HAS INDICATIONS NOTED ON BOTH I/B & O/B C-CHANNELS AT THE UPPER JOGGLE (APPROX WL 65.0). INDICATIONS ARE 50% FSH AND APPROX 0.2" IN LENGTH. FAILS NDT INSPECTION AT THIS TIME. (INDICATIONS ARE IN THE AFT RADIUS OF BOTH C-CHANNELS). MARKED ON A/C. REMOVED VERTICAL POST FS 409+128 LBL 18.0 IAW SRM 51-42-06. INSTALLED NEW SERVICEABLE POSTS AT F.S. 409+128 LBL 18 INBD AND OTBD IAW SRM 51-42-06 AND 51-42-22 C/W EC/TC REO 601R-53-41-889.

Part: ANGLE — CRACKED (BS 625) · airframe 26,398 hrs · 22,754 cycles

RIGHT MID FS 625 OBLIQUE ANGLE IS CRACKED.

Part: FLOOR SUPPORT — CORRODED (BS 574-621) · airframe 26,398 hrs · 22,754 cycles

LBL 27.0 FLOOR SUPPORT OTBD SIDE HAS CORROSION AROUND FASTENER HOLES, FS 574.0 TO FS 621.0. REMOVED UPPER FLOOR SUPPORT CAP AT LBL 27.0 FROM FS 559+112 TO FS 621 IAW SRM 51-42-06. INSTALLED SERVICEABLE FLOOR SUPPORT CAP AT LBL 27 FROM 574 TO 621 IAW REO 601R-53-61-3409.

Part: BULKHEAD — CRACKED (BS 559) · airframe 26,398 hrs · 22,754 cycles

FOUND FS 559 BULKHEAD WEB HAS 2 INDICATIONS NOTED: 1) RT WEB I/B OF RBL 18, WL 59.10 INDICATION NOTED APPROX. .5" IN LENGTH, 100% FSH, 2) RT WEB O/B OF RBL 9, WL 54.10 APPROX. .2" IN LENGTH, 50% FSH, AND FOUND FS 559 LT CAP ANGLE HAS INDICATION NOTED APPROX. .2" IN LENGTH, 80% FSH. ALL FAILED NDT. COMPLIED WITH EC/TC REO 601R-53-41-260 IAW REO 601R-53-41-260.

Part: CARGO TRACK — CORRODED (BS 616-621) · airframe 26,398 hrs · 22,754 cycles

CARGO TRACK LBL 9.0 FS 616 TO FS 621 IS CORRODED.

Part: SEAT TRACK — CORRODED (BS 559-567) · airframe 26,398 hrs · 22,754 cycles

CARGO BAY SEAT TRACK RBL 9.0 FS 559.96 TO FS 567 IS CORRODED. REMOVED CARGO BAY SEAT TRACK RBL 9.0 IAW SRM 51-41-00. REPLACED AND INSTALLED SERVICEABLE CARGO BAY SEAT TRACK 9.0 IAW SRM 51-41-02.

Part: SEAT TRACK — CORRODED (BS 559-567)

CARGO BAY SEAT TRACK LBL 9.0 FS 559+96 TO FS 567 IS CORRODED. REMOVED AND REPLACED CARGO BAY SEAT TRACK LBL 9.0 F.S. 559+96 TO F.S. 567 IAW SRM 51-41-02.

Part: STRUCTURE — CORRODED (BS 333-364 S27) · airframe 26,398 hrs · 22,754 cycles

MAIN AVIONICS COMPARTMENT FS 333.00, STR 27 TO FS 364.00, STR 27 HAS AREAS OF CORROSION. CORROSION FROM FRAME STA 333 TO FRAME STA 364 AROUND STR 27 HAS BEEN ADDRESSED WITH INDIVIDUAL NON ROUTINES TO COVER ALL CORROSION. REF 8727611.

Part: SUPPORT ANGLE — CRACKED (BS 461)

RT WING TO FUSELAGE ACCESS FAIRING SUPPORT ANGLE CRACKED AT FS 461.50. REMOVED AND REPLACED RT WING TO FUSE ACCESS FAIRING SUPPORT ANGLE AT FS 461.50 IAW SRM 51-42-06. SELF CONTOURING SEALING PAD ON ANGLE AT 461.50. APPLIED SELF CONTOURING SEALING PAD TO RT WING TO FUSELAGE ACCESS FAIRING SUPPORT ANGLE AT FS 461.50 IAW AMM 51-23-00-390-802.

Part: SUPPORT ANGLE — CRACKED (BS 449) · airframe 26,398 hrs · 22,754 cycles

RT WING TO FUSELAGE ACCESS FAIRING SUPPORT ANGLE CRACKED AT FS 449.85. REMOVED AND REPLACED RT WING TO FUSE ACCESS FAIRING SUPPORT ANGLE AT FS 449.85 IAW SRM 51-42-06. SELF CONTOURING SEALING PAD ON ANGLE AT 449.85. APPLIED SELF CONTOURING SEALING PAD TO RT WING TO FUSELAGE ACCESS FAIRING SUPPORT ANGLE AT FS 449.85 IAW CRJ 200 AMM 51-23-00-390-802.

Part: WARNING MESSAGE — ACTIVATED · airframe 26,253 hrs · 22,601 cycles

CARGO BTL LO ON CLIMBOUT OF ATL. EMERGENCY DECLARED -- AIRCRAFT RETURNED TO AFTER T/O.

Part: HYDRAULIC SYSTEM — MALFUNCTIONED (NR 2) · airframe 25,956 hrs · 22,310 cycles

HYD SYSTEM 2 LOW PRESSURE IN FLIGHT. EMERGENCY DECLARED, EQUIPMENT WAS STANDING BY.

Part: WARNING SYSTEM — ACTIVATED (NLG) · airframe 25,703 hrs · 22,058 cycles

UPON TAKEOFF, RECEIVED A "NOSE DOOR OPEN" MSG. WRH ADVISED RETURN TO AIRPORT. FLT 5399 DEL 67 MINS. NC/08C EMERGENCY DECLARED.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 24,675 hrs · 21,118 cycles

REPAIR ANGLE AT FS 484, RBL 27 CRACKED.

Part: STEP — CRACKED (AIRSTAIR) · airframe 2,361,546 hrs · 20,169 cycles

ASD LOWER STEP CRACKED. REMOVED AND REPLACED ASD LOWER STEP IAW AMM 52-11-00. OPS CHECKED GOOD. REMOVED AND REPLACED ASD LOWER STEP IAW AMM 52-11-00. OPS CHECKED GOOD. (B)

Part: DOOR — OUT OF ADJUST · airframe 2,346,242 hrs · 20,040 cycles

ASD HARD TO CLOSE, ADJUSTED PAX DOOR COUNTERBALANCE SYSTEM IAW MM 52-11-17. OK FOR SERVICE. (B)

Part: DOOR — BINDS (ASD) · airframe 23,240 hrs · 19,852 cycles

VERBALLY REPORTED BY FELLOW MTC CONTROLLER MERRICK REPORTED BY STATION PERSONNEL THAT ASD DIFFICULT TO OPERATE.

Part: DOOR — STUCK (MAIN PAX) · airframe 22,629 hrs · 19,335 cycles

PASSENGER DOOR WILL NOT OPEN OR CLOSE.

Part: FLAP SYSTEM — FAILED (TE FLAPS) · airframe 22,385 hrs · 19,148 cycles

FLAP FAIL DURING APPROACH AT ZERO. TOWER DECLARED EMERGENCY. EMERGENCY EQUIPMENT ON STANDBY. FLT 4877 CX.

Part: PLACARD — MISSING (COCKPIT) · airframe 22,174 hrs · 18,972 cycles

AAR - CREW ESCAPE HATCH PLACARDS MISSING (X 4).

Part: PLACARD — DAMAGED (EMERGENCY EXIT) · airframe 22,174 hrs · 18,972 cycles

EMERGENCY EXIT AND CLOSED PLACARD ON SERVICE DOOR UNLEDGIBLE. REMOVED UNLEDGIBLE ""CLOSED"" PLACARD AND REPLACED WITH SERVICEABLE PN S1874, IAW CRJ 200 AMM 11-20-00. JC13349. EMERGENCY EXIT PLACARD ON SERVICE DOOR WITH SERVICEABLE PLACARD PN S1880 IAW CRJ MM 11-20-00.

Part: TRACK — CRACKED (THRUST REVERSER) · airframe 22,174 hrs · 18,972 cycles

RIGHT THRUST REVERSER LOWER O/B TRACK IS CRACKED. 10-9-07 REMOVED UNSERVICEABLE RT THRUST REVERSER LOWER O/B TRACK IAW CRJ AMM 78-34-11. PICKED UP NUTPLATES ON SERVICEABLE TRACK IAW CRJ SRM 51-42-06. REAMED AFT MOUNT BUSHING ON TRACK IAW CRJ AMM 20-26-00. INSTALLED SERVICEABLE TRACK P/N 228-50809-803 IAW CRJ AMM 78-34-11. PERFORMED OPS CHECK OF RT THRUST REVERSER IAW CRJ AMM 71-00-00. NO DEFECTS NOTED.

Part: ATTACH ANGLE — CRACKED (LT WING) · airframe 22,174 hrs · 18,972 cycles

LT WING L/E 530JL I/B ATTACH ANGLE IS CRACKED IN UPPER AND LOWER RADIUS. REMOVED LT L/E WING ATTACH ANGLE THAT WAS CRACKED, AND LOCATED NEW SERVICEABLE P/N 600-12045-11 AND INSTALLED, IAW CRJ SRM 51-40-11.

Part: PLACARD — DAMAGED (PAX DOOR) · airframe 22,174 hrs · 18,972 cycles

AAR - PAX DOOR PANEL 832BT HAS DAMAGED -EXIT- PLACARD. REMOVED ADN APPLIED NEW SERVICEABLE EXIT PLACARD PN S1574-18 TO PAX DOOR PANEL 832BT IAW CRJ 200 AMM 11-30-00.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 22,174 hrs · 18,972 cycles

AAR - RIGHT HAND 621 OBLIQUE ANGLE CRACKED (INTERCOSTAL). REMOVED CRACKED OBLIQUE ANGLE AND LOCATED AND INSTALLED SERVICEABLE RT OBLIQUE ANGLE (P/N 601-35012-52) IAW CRJ 200 SRM 51-42-21. 1367. 10-1-07.

Part: INTERCOSTAL — CRACKED (BS 484) · airframe 22,174 hrs · 18,972 cycles

INTERCOSTAL CLIP CRACKED AT FS 484, LBL 27 O/B. REMOVED CRACKED INTERCOSTAL CLIP AT FS 484 LBL 27 O/B IAW CRJ 200 SRM 51-42-21. DUPLICATED ANGLE, LOCATED, DEBURRED, ALODINED, PRIMED, AND PAINTED IAW CRJ 200 SRM 53-41-43. INSTALLED SERVICEABLE ANGLE IAW CRJ 200 SRM 51-42-21.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,839 hrs · 18,694 cycles

EMERGENCY LIGHT SWITCH IN COCKPIT HAS SEVERAL INOP BULBS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,839 hrs · 18,694 cycles

SECOND FROM AFT CEILING EMERGENCY LIGHT INOP.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 21,779 hrs · 18,648 cycles

FLAP ASYMMETRY IN FLIGHT LT AT ZERO AND RT AT 8-9. AFTER AIR RETURN RT INDICATION SHOWS 11 DEGREES BUT THE FLAPS PHYSICALLY SHOW AT ZERO. A/C RETURNED TO PIA AFTER T/O. EMERGENCY DECLARED. FLT 4678 DEL 495 MINS.

Part: FLAP — FAILED (WING) · airframe 21,169 hrs · 18,170 cycles

FLAPS FAIL MESSAGE ON APPROACH TO CVG. FLAPS FAILED AT 0'. BRAKE TEMPS MAXED OUT AT 4. EMERGENCY DECLARED. FLT 4863 CX AND ON 04/08/07 FLT 4421 CX.

Part: FLAP — MALFUNCTIONED (WING) · airframe 21,097 hrs · 18,111 cycles

FLAPS AGAIN, FAILED AT 0 DEG PERFORMED 0 DEG FLAP LANDING ON 41,000 CARD. REPEAT WRITE UP. EMERGENCY EQUIPMENT ON STANDBY.

Part: FLAP SYSTEM — FAILED (TE FLAPS) · airframe 21,075 hrs · 18,093 cycles

FLAPS AGAIN FAILED AT ZERO. PERFORMED ZERO FLAP LANDING ON 41,000 LB CARD. REPEAT WRITE-UP. EMERGENCY DECLARED. FLTS 4913, 4818, 4683 CX.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 21,076 hrs · 18,093 cycles

FLAPS FAIL CAUTION WHEN SELECTED FROM 0 TO 8 INDICATION SHOWED ALL FLAPS AT 0. EMERGENCY DECLARED.

Part: FLAP SYSTEM — FAILED (TE FLAPS) · airframe 21,076 hrs · 18,093 cycles

FLAPS FAIL AT 0 ON APP. EMERGENCY DECLARED. FLT 4762 DEL 35 MINS.

Part: UNKNOWN — ODOR (CABIN) · airframe 20,521 hrs · 17,687 cycles

AIRCRAFT PERMEATED WITH A STRONG SMELL, POSSIBLY MOLD OR MILDEW ISSUE. CHECK ACM SOCKS.

Part: A/C PACK — ODOR · airframe 20,385 hrs · 17,585 cycles

AIR COMING FROM PACKS SMELLS LIKE DIRTY SOCKS. FLT 4425 DEL 15 MINS.

Part: FITTING — CRACKED (AIRSTAIR) · airframe 19,954 hrs · 17,268 cycles

ASD - FWD ANCHOR FITTING CRACKED.

Part: STEP — BROKEN (AIRSTAIR) · airframe 19,954 hrs · 17,268 cycles

ASD - BTM STEP BROKEN.

Part: ANCHOR FITTING — CRACKED (FUSELAGE) · airframe 19,954 hrs · 17,268 cycles

ASD FWD ANCHOR FITTING CRACKED. COMPLIED WITH E.O 600-52-0066B AS PER S/B 601R-52-116 BY REPLACING FWD AND AFT ASD COUNTER BALANCE SWIVEL LEVERS AND ANCHOR FITTINGS. OPS CK GOOD.

Part: STEP — CRACKED (PAX DOOR) · airframe 19,548 hrs · 16,938 cycles

TOP STEP CRACKED ON MAIN PAX DOOR

Part: STEP — CRACKED (PAX DOOR)

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

Part: LIGHT — INOPERATIVE (CABIN)

DURING A GROUND INSPECTION IN CAE, THE AFT CEILING EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE AFT CEILING EMERGENCY LIGHTS. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: SILL — CORRODED (FUSELAGE)

DURING A C-CHECK, THE SERVICE DOOR SILL AREA WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINT REMOVED LIGHT CORROSION IN 2 PLACES OF SERVICE DOOR SILL AREA. CLEANED, TREATED, PRIMED AND PAINTED AREAS IAW SRM. (K)

Part: FLOORBEAM — CORRODED (FUSELAGE)

DURING A C-CHECK IN MCN, THE FLOORBEAM ATTACH POINTS, AT FS 621 TO FS 560, LBL 37L, WERE FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE FLOOR ATTACH POINTS, AT FS 621 TO 560, LBL 37L IAW CRJ 200 SRM 51-42-06. (M)

Part: SKIN — CORRODED (BS 605)

DURING A C-CHECK IN MCN, THE FORWARD FS 605, AT STRINGER 26-27, WAS FOUND TO BE CORRODED. AFTER MAINTENANCE BLENDED, ALODINED, AND PRIMED THE FORWARD FS 605, AT STRINGER 26-27, IAW REO 601R-53-61-1565, IT WAS FOUND TO BE WITHIN LIMITS. (M)

Part: SKIN — CORRODED (BS 610)

DURING A C-CHECK IN MCN, THE INTERNAL SKIN AT FS 610, AT STRINGER 22LT, UNDER THE CARGO FLOOR, WAS FOUND TO BE CORRODED. MAINTENANCE REPAIRED THE INTERNAL SKIN AT FS 610, STRINGER 22 LT, UNDER THE CARGO FLOOR IAW BOMBARDIER REO 601R-53-61-1565. (M)

Part: WEB — CORRODED (FUSELAGE)

DURING A C-CHECK IN MCN, THE FLOOR ATTACH WEB , AT FS 559 PLUS 80 TO 621, BL 45 RT, WAS FOUND TO BE CORRODED. AFTER MAINTENANCE BLENDED, ALODINED, AND PRIMED THE FLOOR ATTACH WEB, AT FS 559 PLUS 80 TO 621, BL 45 RT, IAW REO 601R-53-61-1564, IT WAS FOUND TO BW WITHIN LIMITS. (M)

Part: CARGO TRACK — CORRODED (CARGO BAY)

DURING A C-CHECK IN MCN, THE CARGO COMPARTMENT SEAT TRACKS WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE WILL REMOVE AND REPLACE THE CARGO COMPARTMENT SEAT TRACKS. (M)

Part: FLOORBEAM — CORRODED (BS 615)

DURING A C-CHECK IN MCN, THE FLOORBEAM AT FS 615, RBL 9, WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FLOORBEAM AT S 615, RBL 9, IAW CRJ 200 SRM 51-42-06, 51-42-20, AND 51-00. (M)

Part: ATTACH ANGLE — CORRODED (FUSELAGE)

DURING A C-CHECK IN MCN, THE FLOOR ATTACH ANGLE, AT BL 45 LT, FS 559 PLUS 112 TO PLUS 80, WAS FOUND TO BE CORRODED. AFTER MAINTENANCE BLENDED, ALODINED, AND PRIMED THE FLOOR ATTACH ANGLE AT BL 45 LT, FS 559 PLUS 112 TO PLUS 80 IAW REO 601R-53-61-1564, IT WAS FOUND TO BE WITHIN LIMITS. (M)

Part: SKIN — CORRODED (FUSELAGE)

DURING A C-CHECK IN MCN, SKIN CORROSION WAS FOUND AT LBL 36 AND RBL 36, AT FS 409 PLUS 28 THROUGH FS 559. AFTER MAINTENANCE BLENDED, ALODINED, AND PRIMED THE SKIN CORROSION AT LBL 36 AND RBL 36, AT FS 409 PLUS 28 THROUGH FS 559, IAW REO 601R-53-41-370, IT WAS FOUND TO BE WITHIN LIMITS. (M)

Part: WIRE — DAMAGED (CABIN)

DURING A C-CHECK IN MCN, THE EMERGENCY FLOOR LIGHT WIRING AT THE LAVATORY WAS FOUND TO BE DAMAGED. MAINTENANCE IS REMOVING AND REPLACING THE CONNECTORS TO THE EMERGENCY FLOOR LIGHTS AT THE LAVATORY. (M)

Part: CLIP — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE RIGHT OUTBOARD CLIP AT FS 484, RBL 36 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE RIGHT OUTBOARD CLIP AT FS 484, RBL 36 IAW ASA EO 600-53-0098. (M)

Part: CLIP — CRACKED (FUSELAGE)

DURING A C-CHECK, THE LT IB CLIP AT FS 484, LBL 27 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE LT IB CLIP AT FS 484, LBL 27 IAW EO 600-53-0098.

Part: PRESSURE PANEL — CORRODED (FUSELAGE)

DURING A C-CHECK IN MCN, THE PRESSURE FLOOR SKIN AT LBL 36 AND RBL 36, FROM FS 409 PLUS 28 TO FS 559, WAS FOUND TO BE CORRODED BEYOND LIMITS. AFTER MAINTENANCE BLENDED, ALODINED, AND PRIMED THE PRESSURE FLOOR SKIN AT LBL 36 AND RBL 36, FROM FS 409 PLUS 28 TO FS 559, IN ACCORDANCE WITH REO 601R-53-41-370. (M)

Part: BEAM — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE FS 280 BEAM, OUTBOARD OF RBL 9, WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE WILL BE REPAIRING THE FS 280 BEAM, OUTBOARD OF RBL 9, IAW ASA EO`S 600-53-0090 AND 600-53-0091. (M)

Part: SKIN — CRACKED (FS 640)

DURING AN A-CHECK IN BTR, THE RIGHT FS 640, AT STRINGER 9 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE RIGHT FS 640, AT STRINGER 9. OPERATIONAL CHECKS GOOD. (M)

Part: DOUBLER — CRACKED (BS 640)

DURING AN A-CHECK IN BTR, THE RIGHT FS 640 BONDED SKIN DOUBLER, AT STRINGER 8-13, WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE WILL REPAIR THE RIGHT FS 640 BONDED SKIN DOUBLER, AT STRINGER 8-13, IAW ASA EO 600-53-0107. (M)

Part: FRAME — CRACKED (BS 640)

DURING AN A-CHECK IN BTR, THE RIGHT SIDE 640 FRAME DOUBLER WAS FOUND TO POSSIBLY BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE RIGHT SIDE FS 640 FRAME DOUBLER IAW CRJ200 SRM 51-40-00. (M)

Part: LIGHT — INOPERATIVE (CABIN)

FLT 4906 - DURING AN OVERNIGHT MAINTENANCE VISIT TO CAE, THE FLOOR LEVEL EMERGENCY LIGHT BY THE PASSENGER DOOR WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE INOPERATIVE EMERGENCY LIGHT ASSEMBLY. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: RELAY — SHORTED (EMERGENCY LIGHTS)

DURING A GROUND INSPECTION, AN AC ESS BUSS FAULT MESSAGE WAS RECEIVED AND THE EMERGENCY LIGHTS REMAINED ON. MAINTENANCE REMOVED AND REPLACED THE AC ESS TRANSFER RELAY. OPERATIONAL CHECKS GOOD AIRCRAFT OK FOR SERVICE. (K)

Part: LIGHT — INOPERATIVE (CABIN)

DURING HANGAR MAINTENANCE IN MCN, THE EMERGENCY FLOOR LIGHT STRIP WAS FOUND TO BE DAMAGED IN SEVERAL PLACES. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY FLOOR LIGHT STRIP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LIGHT — BROKEN (CABIN)

DURING HANGAR MAINTENANCE IN BTR, THE EMERGENCY FLOOR TRACK LIGHTING AT ROW 5 WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED A BROKEN EMERGENCY FLOOR LIGHT STRIP AT ROW 5. OPERATIONAL CHECK GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: STEP — BROKEN (PAX DOOR)

FLT 4533 - DURING A GROUND INSPECTION IN ATL, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND BROKEN AT THE FOLDING ROD CONNECTION POINT. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: STEP — CRACKED (PAX DOOR)

DURING HANGAR MAINTENANCE IN MCN, THE LOWER STEP ON THE PASSENGER DOOR WAS FOUND CRACKED AT THE STAY ROD ATTACHMENT. MAINTENANCE REMOVED AND REPLACED THE LOWER STEP ON THE PASSENGER DOOR. (M)

Part: STEP — CRACKED (PAX DOOR)

DURING AN A-CHECK IN MCN, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. (M)

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT)

DURING A C-CHECK, THE FORWARD EMERGENCY FLOOR LIGHT TRACK WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR1 EMERGENCY BATTERY PACK AND THE FORWARD EMERGENCY FLOOR LIGHT STRIP. OPERATIONAL CHECKS GOOD.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT)

DURING A C-CHECK, THE FORWARD EMERGENCY FLOOR LIGHT TRACK WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 1 EMERGENCY BATTERY PACK AND THE FORWARD EMERGENCY FLOOR LIGHT STRIP. OPERATIONAL CHECKS GOOD.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 13,754 hrs

DURING C-CHECK INSPECTION, THE LT AND RT SIDE FLOOR SUPPORT ANGLES AT FS 621 WERE FOUND CRACKED. MAINTENANCE REPAIRED THE CRACKED FLOOR SUPPORT ANGLES IAW REO 601R5361117.

Part: STEP — CRACKED (PAX DOOR)

DURING C-CHECK, THE PASSENGER DOOR TOP STEP WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR TOP STEP.

Part: SILL — CORRODED (FUSELAGE)

DURING C-CHECK INSPECTION, THE CARGO COMPARTMENT SILL PLATE BETWEEN FS 562.72 AND FS 589.00 WAS FOUND TO HAVE CORROSION IN SEVERAL AREAS, AND WAS ALSO CRACKED. MAINTENANCE IS REPAIRING THE SILL PLATE IN THE CARGO COMPARTMENT IAW REO 601R5361690 AND EO 600530095.

Part: RIB — CRACKED (WING)

DURING C-CHECK INSPECTION, THE RT MLG BATT RIB WAS FOUND CRACKED. MAINTENANCE REPAIRED THE CRACKED MLG BATT RIB IAW EO 600570039A AND 600570042.

Part: CLIP — CRACKED (FUSELAGE)

DURING C-CHECK INSPECTION, THE CLIPS AT FS 280 WERE FOUND CRACKED ON BOTH IB AND OB SIDES OF RBL AND LBL 9. MAINTENANCE REMOVE AND REPLACED CRACKED CLIPS IAW SRM 5100.

Part: PSEU — MALFUNCTIONED (PAX DOOR)

FLT 4736 - DURING CLIMB-OUT FROM ICT-ATL, THE CREW RECEIVED A PASSENGER DOOR LATCH CAUTION MESSAGE. QRH PROCEDURES WERE COMPLIED WITH. THE FLIGHT ATTENDANT VERIFIED SECURITY OF THE DOOR AND DETERMINED IT WAS CORRECTLY CLOSE. PRESSURIZATION BEING NORMAL, THE AIRCRAFT CONTINUED TO CLIMB. WHEN PASSING THROUGH 15,000 FEET A PASSENGER DOOR WARNING WAS RECEIVED AND IMMEDIATE DESCENT INITIATED. THE AIRCRAFT RETURNED TO ICT AND CREW REQUESTED EMERGENCY EQUIPMENT DUE TO HIGH GROSS WEIGHT AND ICY RUNWAY CONDITIONS. THE AIRCRAFT LANDED SAFELY IN ICT. MAINTENANCE REMOVED AND REPLACED THE PROXIMITY SENSOR ELECTRONIC UNIT (PSEU). OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: FITTING — CRACKED (PAX DOOR)

DURING A HANGAR INSPECTION IN MCN, THE FORWARD PASSENGER DOOR CABLE ANCHOR FITTING WAS FOUND TO BE CRACKED. MAINTENANCE WILL MONITOR CRACK AND REPLACE DOOR CABLE ANCHOR FITTING WITHIN 100 FLIGHT HOURS PER REO 601R-52-11-416. MAINTENANCE REMOVED AND REPLACED THE FORWARD PASSENGER DOOR CABLE ANCHOR FITTING. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DURING A SCHEDULED INSPECTION IN XNA, THE AFT OVERHEAD CABIN EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BURNED OUT EMERGENCY LIGHT BULB. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: PUMP — LEAKING (ENGINE)

FLT 4773 - EN ROUTE TO SAT, HYDRAULIC LOW PRESSURE MESSAGE ILLUMINATED ON EICAS. IAW QRH AND COMPANY PROCEDURES, CREW SAFELY LANDED AT NEAREST AIRPORT, HOU. MAINTENANCE REPLACED THE ENGINE DRIVEN PUMP. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING INSPECTION, NR 2 EMERGENCY LIGHTING SYSTEM BATTERY PACK FOUND INOPERATIVE. MAINTENANCE REPLACED THE NR 2 EMERGENCY LIGHTING SYSTEM BATTERY PACK. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING INSPECTION, NR 1 EMERGENCY LIGHTING SYSTEM BATTERY PACK FOUND INOPERATIVE. MAINTENANCE REPLACED THE NR 1 EMERGENCY LIGHTING SYSTEM BATTERY PACK. OPERATIONAL CHECK WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (X)