N871AS

Part: STRUCTURE — DENTED (FUSELAGE) · airframe 34,737 hrs · 32,777 cycles

DENT AT FS STATION 310 BETWEEN STR 11R AND 10R. (C-CHECK) COMPLIED WITH DENT REPAIR AT FS 310 BETWEEN STR 11R AND 10R IAW REO. PRESSURIZATION CHECK GOOD AT THIS TIME.

Part: STRUCTURE — DENTED (FUSELAGE) · airframe 34,737 hrs · 32,777 cycles

FOUND DENT WITH GOUGE AT FS 409+96 STR 22L. (C-CHECK) REPAIRED DENT WITH GOUGE AT FS 409+96 STRINGER 22L IAW REO.

Part: DOUBLER — DAMAGED (NLG WW) · airframe 34,737 hrs · 32,777 cycles

CIRCULAR WEB REPAIR DOUBLER TO NOSE WHEEL WELL RIGHT HAND SIDE DAMAGED. (C-CHECK) REPAIRED CIRCULAR WEB REPAIR DOUBLER AT NLG WHEEL WELL RT SIDE IAW REO.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 34,737 hrs · 32,777 cycles

FLOORBOARD SUPPORT ANGLE IS CORRODED AT FS 621.00 BETWEEN RBL 9.0 AND RBL 27.0. (C-CHECK) REPAIRED CORROSION ON FS 621 FLOOR SUPPORT ANGLE BETWEEN RBL 9 AND 27 IAW REO.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 34,737 hrs · 32,777 cycles

FLOORBOARD SUPPORT ANGLE IS CORRODED AT FS 621.00 BETWEEN LBL 27.0 AND LBL 45.0. (C-CHECK) REPAIRED FLOORBOARD SUPPORT ANGLE AT FS 621.00 BETWEEN LBL 27.0 AND LBL 45.0 IAW REO.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 34,737 hrs · 32,777 cycles

FLOORBOARD SUPPORT BEAM CAP AT LBL-9 IS CORRODED BETWEEN FS 409.00+128 AND FS 559.00. (C-CHECK) REPAIRED FLOORBOARD SUPPORT CAP AT LBL -9 AT FS 409.00+128 AND FS 559.00 IAW REO.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 34,737 hrs · 32,777 cycles

RT FLOOR SILL IS CORRODED BETWEEN FS 310 AND FS 319.70. (C-CHECK) REMOVED AND REPLACED RT FLOOR SILL BETWEEN FS310 AND FS319.70 IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 34,737 hrs · 32,777 cycles

FS 349 FLOORBEAM CORRODED RT BETWEEN RBL 27 AND RBL 36. (C-CHECK) REPAIRED FS 349 FLOORBEAM RT BETWEEN RBL 27 AND 36 IAW REO.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 34,737 hrs · 32,777 cycles

RT PRESSURE FLOOR SILL IS CORRODED IN 6EA LOCATIONS AROUND FASTENER HOLES BETWEEN FS 424.00 AND FS 484.00. (C-CHECK) REPAIRED RT PRESSURE FLOOR SILL PANEL CORROSION AT SIX LOCATIONS COMMON TO THE NUTPLATE HOLES AT FS-429: FS 435.5: FS441: FS447: FS452: AND FS478 IAW REO.

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 34,737 hrs · 32,777 cycles

INDICATION NOTED AT FS621.00 REAR PRESSURE BULKHEAD FWD FACE AT RBL27.50 WL97.50-WL102.75 APPROX. 5.25" IN LENGTH 50% FULL SCREEN HEIGHT. (C-CHECK) REPAIRED FS 621 BULKHEAD WEB AT RBL 27 IAW REO.

Part: STRUCTURE — DENTED (FUSELAGE) · airframe 34,737 hrs · 32,777 cycles

DENT FOUND BETWEEN FS 250.00 AND 265.00, BETWEEN STRINGERS 24L AND 25L. (C-CHECK) COMPLIED WITH DENT REPAIR FOUND BETWEEN FS 250.00 AND 265.00 BETWEEN STRINGERS 24L AND 25L IAW REO. PRESSURE CHECK GOOD AT THIS TIME.

Part: PLATE — DAMAGED (FUSELAGE) · airframe 31,123 hrs · 28,799 cycles

EXTERNAL POWER RECEPTACLE DOOR TOP LAND DAMAGED, ON FUSELAGE SIDE. CUT AWAY DAMAGED SECTION OF EXTERNAL POWER RECEPTACLE DOOR UPPER LAND, ON FUSELAGE SIDE, CLEANED UP CUTLINES REF EC/TC REO 601R-53-11-009. FABRICATED, DRILLED AND DEBURRED JOGGLED PLATE, PN 601R-53-11-009-1 FROM 2024 T-3 .050" REF REO 601R-53-11-009, REV A. FOUND EXTERNAL POWER RECEPTACLE DOOR NOT PROPERLY LATCHING TO NEW JOGGLED PLATE, TRIMMED .200" FROM LATCH ENDS TO GET DOOR TO PROPERLY LATCH, DAMAGE REPORT WAS SENT TO MFG FOR DISPOSITION. COMPLIED WITH REO 601R-52-45-053. INSTALLED JOGGLE TO EXTERNAL POWER RECEPTACLE DOOR TOP LANDING REF EC/TC REO 601R-53-11-009. RII COMPLIED WITH FOR THIS MAJOR REPAIR IAW GMM 3-3.

Part: SKIN — DENTED (BS 593) · airframe 31,123 hrs · 28,798 cycles

FUSELAGE HAS SEVERAL DENTS AT BS 593 BETWEEN STRINGERS 25-26R AND STRINGERS 24-25R. REO 601R-53-61-5529 HAS BEEN ACCOMPLISHED AND ALL STEPS HAVE BEEN DOCUMENTED AND SIGNED FOR ON A NON-ROUTINE WORK CARD.

Part: SIGN — DAMAGED (CABIN) · airframe 31,123 hrs · 28,798 cycles

SERVICE DOOR EXIT SIGN DAMAGED, NEEDS REPLACED. REMOVED DAMAGED SERVICE DOOR EXIT SIGN IAW AMM 33-51-13-000-801. INSTALLED NEW SERVICE DOOR EXIT SIGN IAW AMM 33-51-13-400-801. OPS TEST OF THE "EXIT" SIGN ABOVE THE SERVICE DOOR IS GOOD IAW AMM TASK 33-51-00-710-801.

Part: INTERCOSTAL — DAMAGED · airframe 31,123 hrs · 28,798 cycles

UPON REMOVAL OF TOP PLATE, PN 601R38669-73, FOUND 2 EA FASTENER HOLES ELONGATED IN TOP PLATE AND IN UNDER LYING INTERCOSTAL, PN 601R38669-39. REMOVED INTERCOSTAL PT 601R38669-39 AT RBL 38.45, FS 280 IAW SRM 51-42-06. INTERCOSTAL REQUIRES REPLACEMENT. FABRICATED NEW INTERCOSTAL, PN 601R-53-21-2647-1 IAW REO 601R-53-21-2647. INSTALLED NEW INTERCOSTAL, PN 601R-53-21-2647-1 AT RBL 38.45 BETWEEN FS 280 & FS 295 IAW SRM CH 51-42-06.

Part: FLOOR SUPPORT — CORRODED (NOT REPORTED) · airframe 31,123 hrs · 28,798 cycles

FLOOR SILL DOUBLER FWD OF SERVICE DOOR HAS CORROSION. REMOVED FLOOR SILL DOUBLER FWD OF SERVICE DOOR IAW SRM 51-42-06. INSTALLED NEW SERVICEABLE FLOOR SILL ANGLE FWD OF SERVICE DOOR IAW SRM 51-42-06 & SRM TR 51-32.

Part: SKIN — CRACKED (RT WING) · airframe 31,123 hrs · 28,798 cycles

RIGHT LOWER WING PLANK HAS MULTIPLE INDICATIONS NOTED AT DRAIN HOLE NEAR BOOST PUMP 50 PERCENT FSH AROUND ENTIRE CIRCUMFERENCE, FAILED NDT INSPECTION. BLENDED AREA AROUND DRAIN HOLE .006" MAX MATERIAL REMOVED. AREA MEASURES 2.1" X 2.3". BLENDED AREA IAW SRM 51-21-06. COMPLIED WITH STS EA 32-2015-325.

Part: SKIN — CRACKED (LT WING) · airframe 31,123 hrs · 28,798 cycles

LT LOWER WING PLANK HAS ONE INDICATION NOTED AT WS 87, DRAIN HOLE FWD SIDE .400" LONG BY 90 PERCENT FSH, FAILED NDT INSP. PERFORMED CUTOUT OF DAMAGE TO LT LOWER WING PLANK AT WS 87 DRAIN HOLE FWD SIDE IAW REO NR 601R-57-21-2346. CHAMFER WING PLANK CUTOUT AS REQUIRED IAW REO 601R-57-21-2346. C/W ROTO PEEN OF REWORKED AREA IAW REO 601R-57-21-2346. FABRICATED 1 EA PLUG -3, USING 7075-T6 MATERIAL PO W31214/1 AS REQUIRED IAW REO 601R-57-21-2346.

Part: FRAME — CORRODED (BS 310) · airframe 31,123 hrs · 28,798 cycles

FRAME FS 310, STR 23 & 22R HAS CORROSION AT ATTACHED ANGLE. DAMAGED SECTION OF FS 310, FRAME BETWEEN STR 22R & 23R WAS REPLACED DURING ACCOMPLISHMENT OF REO 601R-53-21-2644.

Part: SIGN — DAMAGED (EMERGENCY LIGHTS) · airframe 31,123 hrs · 28,798 cycles

SERVICE DOOR EXIT SIGN DAMAGED, NEEDS REPLACED. REMOVED DAMAGED SERVICE DOOR EXIT SIGN IAW AMM 33-51-13-000-801. INSTALLED NEW SERVICE DOOR EXIT SIGN IAW AMM 33-51-13-400-801. OPS TEST OF THE "EXIT" SIGN ABOVE THE SERVICE DOOR IS GOOD IAW AMM TASK 33-51-00-710-801.

Part: BULKHEAD — CRACKED (BS 621) · airframe 31,123 hrs · 28,798 cycles

INDICATIONS NOTED AT 621 REAR PRESSURE BULKHEAD, BL 0.00, WL 110.00 APPROXIMATELY 1.700" IN LENGTH VERTICALLY 50 PERCENT FULL SCREEN HEIGHT FAILING NDT. COMPLIED WITH EC/TC REO 601R-53-61-1285 AND GREO 601R-53-61-1285, REV D, DATED 10/31/2011 AS WRITTEN. REO 601R-53-61-5531, REV HAS BEEN ACCOMPLISHED AND ALL STEPS HAVE BEEN DOCUMENTED AND SIGNED FOR ON A NON-ROUTINE WORK CARD.

Part: SEAT TRACK — CORRODED (BS 574-621) · airframe 31,123 hrs · 28,798 cycles

FLOOR SUPPORT TOP PLATES INBD AND OTBD ON LBL 27 FROM FS 574 TO FS 621 HAS CORROSION ON IT. BLENDED FLOOR SUPPORT TOP PLATE AT RBL 9, FS 589-FS 621 MAX MATERIAL REMOVED .012". FOUND TO BE OUT OF LIMITS IAW REO 601R-53-00-005, DETAIL B. REMOVED CORRODED LBL 27 SEAT RAIL TOP CAP BETWEEN FS 574 TO FS 621 AND 621 AFT FITTING IAW SRM 51-42-21, 51-42-06, 51-42-13. INSTALLED NEW SERVICEABLE BEAM 601R35031-3 IAW REO 601R-53-61-3778. 2 BEAMS, PN 600-35031-309 AND P/N 600-35031-307 & 2 CLIPS, PN 600-35031-315 ON LBL 27 BEAM FROM FS 574 TO FS 621 REQUIRE REPLACEMENT DUE TO PREVIOUS REPAIR ON THE EXISTING BEAM. DRILLED/LOCATED NEW SERVICEABLE 600-35031-309, 600-35031-307, FLOORBEAMS IAW SRM 51-40-06, 51-42-06, 51-42-21.

Part: FRAME — CORRODED (BS 589) · airframe 31,123 hrs · 28,798 cycles

FS 589 FRAME IS CORRODED FROM STR 26R TO 23L. UNDER FURTHER INVESTIGATION FOUND DAMAGED AREA TO BE OUT OF LIMITS IAW SRM 53-00-00, FIG 102, SHEET 2. INSTALLED NEW FRAME SECTOR AT FS 589 IAW SRM 51-42-06, PN 601R36025-61. REMOVED STR 23R FROM FS 589.00 TO 605.00 IAW SRM 51-42-06. INSTALLED STR 23R FROM FS 589.00 TO 605.00 IAW SRM 51-42-06.

Part: SEAT TRACK — CORRODED (BS 589-621) · airframe 31,123 hrs · 28,798 cycles

FLOOR SUPPORT TOP PLATE ON LBL 9 HAS CORROSION FROM FS 589 TO FS 621. BLENDED FLOOR SUPPORT TOP PLATE AT LB 9, FS 559-FS 621. MAX MATERIAL REMOVED .011. FOUND TO BE OUT OF LIMITS IAW REO 601R-53-00-005, DETAIL B. UPON FURTHER INVESTIGATION FOUND OUT OF LIMITS AND REQUIRES ENGINEERED DISPOSITION. INSTALLED NEW LBL 9.0, SEAT RAIL BEAM FROM FS 574-621 IAW BSC REO 601R-53-61-3780, REV A DATED 2011-07-15. REMOVED 3 EA CORRODED SEAT TRACK SEGMENTS FROM LBL 9.0 BETWEEN FS 574-621 IAW SRM 51-41-02. LOCATED AND INSTALLED 3 EA SEAT TRACK FILLER SEGMENTS TO LBL 9.0 BETWEEN FS 574-621 IAW SRM 51-41-02. REMOVED CORRODED LBL 9.0, SEAT RAIL CAP BETWEEN FS 571-621. DRILLED/LOC FASTENERS IN NEW CAP IAW SRM 51-42-06 AND 51-42-21. LOCATED AND DRILLED NEW SERVICEABLE SEAT RAIL BEAM PN 601R35031-3 AT LBL 9.0 FS 574-FS 621 IAW SRM CH 51-40-11.

Part: DOOR SILL — CORRODED (BS 589) · airframe 31,123 hrs · 28,798 cycles

CARGO DOOR SILL IS CORRODED. CLIP AT FS 589 UNDER CARGO DOOR SILL FOUND TO BE CRACKED. REMOVED CLIP IAW SRM 51-42-21. LOCATED NEW FASTENER HOLES ON NEW SERVICEABLE CLIP IAW SRM 51-40-11. INSTALLED NEW SERVICEABLE CLIP IAW SRM 51-42-21. DID NOT FABRICATE FLOOR SILL, INSTALLED NEW CERTIFIED SILL, PN 601R35011-63 IAW FABRICATED PART, REO 601R-53-61-1574.

Part: FLOOR SUPPORT — CORRODED (BS 559) · airframe 31,123 hrs · 28,798 cycles

CARGO FLOOR SUPPORT RIGHT EDGE MEMBER HAS CORROSION FROM FS 559+80 TO FS 559+112. DURING REPAIR OF CABIN FLOOR SILL BETWEEN FS 559+80 TO FS 559+112 RT, FOUND CORROSION TO BE OUT OF LIMITS IAW REO 601R-53-00-526, REV-DATED 22 MAY 13. C/W ECTC REO 601R-53-00-526 01 AND GREO 601R-53-00-526, REV DATED 05/22/13 AS WRITTEN.

Part: FRAME — CORRODED (BS 605) · airframe 31,123 hrs · 28,798 cycles

FS 605.00 FRAME HAS CORROSION FROM STR 26R TO 22L. UNDER FURTHER INVESTIGATION FOUND DAMAGED AREA TO BE OUT OF LIMITS IAW SRM 53-00-00, FIG 102, SHEET 2. INSTALLED NEW SERVICEABLE FS 605.00 FRAME, PN 601R36026-27 IAW SRM 51-42-06/51-40-11/51-42-21. REMOVED LT AND RT POST THAT ATTACH TO FS 605 AND TRANSVERSE BEAM IAW SRM 51-42-21. INSTALLED LT & RT POSTS IAW SRM 51-42-21. LOCATED & DRILLED NEW FRAME, PN 601R36026-27 AT FS 605.00, STR 26R TO 22L IAW SRM 51-40-11.

Part: FLOOR SUPPORT — CORRODED (BS 589-621) · airframe 31,123 hrs · 28,798 cycles

FLOOR SUPPORT TOP PLATE ON RBL 9 HAS CORRSION FROM FS 589 TO FS 621. BLENDED CORROSION FROM FLOOR SUPPORT TOP PLATE AT RBL 9, FS 589 TO FS 621. MAX MATERIAL REMOVED .013. FOUND TO BE OUT OF LIMITS IAW REO 601R-53-00-005 RIG B. UPON FURTHER INVESTIGATION FOUND TO BE OUT OF LIMITS, REQUIRES ENGINEERING DISPOSITION. LOCATED AND DRILLED NEW FLOOR SUPPORT TOP PLATE PT 601R35031-3 IAW SRM 51-40-11 AFTER REMOVAL OF UNSERVICEABLE FLOOR SUPPORT TOP PLATE. INSTALLED FLOORBEAM CAP ON RBL 9 BETWEEN FS 569 AND FS 621 IAW REO 601R-53-61-3780.

Part: INTERCOSTAL — CRACKED (BS 621) · airframe 31,123 hrs · 28,798 cycles

FS 621 BULKHEAD AFT SIDE INTERCOSTAL IS CRACKED AT STR 14L. DRILLED, LOCATED FASTENERS AS REQUIRED ON NEW INTERCOSTAL. WORK PERFORMED IAW SRM 51-42-06, 51-42-21 & 51-77-00. INSTALLED NEW INTERCOSTAL AT STR 14L IAW SRM 51-42-06, 51-42-21 & 51-77-00.

Part: VERTICAL SUPPORT — CRACKED (BS 409) · airframe 31,123 hrs · 28,798 cycles

FOUND FS 409.00+128, VERTICAL POST BL 0.0, RT SIDE HAS INDICATION NOTED APPROX .250" LONG 60 PERCENT FSH AT AFT FLANGE RADIUS. FAILED NDT INSPECTION. REMOVED FS 409+128 VERT POST ASSY IAW SRM 51-42-06, 51-42-21. C/W ECTC REO 601R-53-41-889 AND MET ALL THE REQUIREMENTS OF REO 601R-53-41-889. DRILLED, LOCATED NEW SERVICEABLE FS 409+128 BL 0 VERT POST ASSY IAW SRM 51-42-06, 51-42-22.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 31,123 hrs · 28,798 cycles

LT AND RT FLOOR SEAT TRACKS FROM FS 559-FS 559+80 HAVE SEVERAL AREAS OF CORROSION AROUND SCREW HOLES. REMOVED LT AND RT FLOOR SEAT TRACKS FROM FS 559 TO FS 559+80 IAW AMM 53-01-11-000-802 AND SRM 51-41-02. LOCATED HOLES IN BULK MATERIAL, PN N126-2075, PO W35264 FS 559-FS 559+80, LT AND RT IAW SRM 51-40-11 AND REO 601R-53-00-485. ALODINED, PRIMED AND PAINTED SEAT TRACK IAW REO 601R-53-00-485. COMPLETED REO 601R-53-00-485. FABRICATED SEAT RAILS IAW GREO 601R-53-00-485, REV A.

Part: SEAT TRACK — CORRODED (BS 399-409) · airframe 31,123 hrs · 28,798 cycles

LT FLOOR SEAT RAIL FROM FS 399-409+112 HAS SEVERAL AREAS OF CORROSION, SOME SEVERE INTERGRANULAR. REMOVED LT FLOOR SEAT RAIL FROM FS 399 TO FS 409 IAW AMM 53-01-11-000-802 AND SRM 51-41-02. LOCATED HOLES IN BULK MATERIAL, PN N126-2075, PO W35264, FS 399-FS 409+112 IAW SRM 51-40-11. C/W REO 601R-53-00-485, REV-DATED 09/28/12. C/W REO 601R-53-00-485, REV DATED 09/28/12 ECTC. C/W REO 601R-53-00-485, REV DATED 12/07/14 AND IAW SRM 51-41-02. FABRICATED SEAT RAILS IAW GREO 601R-53-00-485, REV A.

Part: RETAINER — BENT (DOOR SEAL) · airframe 31,123 hrs · 28,798 cycles

LOWER EDGE OF PAX DOOR SKIN AND SEAL RETAINER IS BENT AT AREA ADJACENT TO PROXIMITY SWITCH. REMOVED LOWER CENTER PAX DOOR SEAL RETAINER IAW SRM 51-42-13. LOCATED, DRILLED & INSTALLED PAX DOOR SEAL RETAINER IAW SRM 51-40-11-00, 51-42-13-00 & REO 601R-52-11-915 AND REO 601R-52-11-915. COMPLIED WITH EC/TC REO 601R-52-11-915 IAW REO 601R-52-11-915.

Part: FLOOR SUPPORT — CORRODED (BS 409-559) · airframe 31,123 hrs · 28,798 cycles

RT PRESSURE FLOOR SILL PANEL HAS MULTIPLE LOCATIONS OF CORROSION SURROUNDING NUTPLATES FROM FS 409+128 TO FS 559. FOUND QTY 2 BLEND REPAIRS TO FLOOR SILL LOCATED LESS THAN 5" AWAY FROM EACH OTHER. LIMITATION IAW REO 601R-53-41-666-01 IS MINIMUM OF 5" APART. LOCATION OF 2 BLEND REPAIRS ARE AT FS 518.6, RBL 42.5 & FS 522.2, RBL 42.5. BLENDS .006" DEEP. COMPLIED WITH EC/TC REO 601R-53-41-666 01 AND REO 601R-53-41-666, REV C DATED 11/06/2012 AS WRITTEN. REO 601R-53-41-1936, REV HAS BEEN ACCOMPLISHED.

Part: FRAME — CORRODED (BS 310) · airframe 31,123 hrs · 28,798 cycles

FS 310, FRAME IS CORRODED BETWEEN STRS 23R AND 22R. COMPLIED WITH BSC REO 601R-53-21-2644, REV A, DATED 2015/08/11.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 31,123 hrs · 28,798 cycles

FS 280 CROSSBEAM IS CRACKED IN MULTIPLE LOCATIONS. REMOVED 4 EA CLIPS FROM FS 280 AT LBL 9 INBD AND OTBD AND RBL 9 INBD AND OTBD IAW SRM 51-42-06 AND 51-42-21. INSTALLED NEW CLIPS IAW SRM 51-42-06, 51-42-21 AND REO 601R-53-11-171, REV D, 13 FEB 07. CUT AWAY DAMAGED SECTIONS OF FLOOR ANGLE AT LBL 9 AND RBL 9 OF 280 IAW REO 601R-53-11-171. COMPLIED WITH REO 601R-53-11-171 D.

Part: FLOOR SUPPORT — CORRODED (BS 409-559) · airframe 31,123 hrs · 28,798 cycles

LEFT FLOOR SILL ANGLE HAS CORROSION IN MULTIPLE LOCATIONS BETWEEN FS 409+128 TO FS 559. COMPLIED WITH EC/TC REO 601R-53-41-666 01 AND REO 601R-53-41-666, REV C, DATED 11/06/12 AS WRITTEN.

Part: SEAT TRACK — CORRODED (BS 399-409) · airframe 31,123 hrs · 28,798 cycles

RT FLOOR SEAT TRACK FROM BS 399 - 409+112 HAS SEVERAL AREAS OF CORROSION, SOME SEVERE INTERGRANULAR. REMOVED THE SEAT TRACK IAW AMM 53-01-11-000-802 AND SRM 51-41-02. LOCATED HOLES IN BULK MATERIAL, PN: N126-2075, P/O: W35264, FS 399 TO FS 409+112 RT IAW SRM 51-40-11. COUNTERSUNK, STEPPED-UP AND PART TRIMMED TO SIZE, STEPS 1-8 OF REO 601R-53-00-485. COMPLIED WITH REO:601R-53-00-485, REV-- DATED 09/28/12. FABRICATED SEAT RAILS IAW GREO:601R-53-00-485, REV-DATED 09/28/12.

Part: FRAME — CORRODED (BS 310) · airframe 31,123 hrs · 28,798 cycles

FS 310 FRAME HAS CORROSION BETWEEN 26L AND 25L ON FWD FACE. REMOVED CORROSION FRAME 601R32002-69 AT STS 310 BETWEEN 25L STR & 25R STR IAW SRM 51-42-06 & SRM 51-42-21. FOUND TO BE OUT OF LIMIT. RECEIVED NEW SERVICEABLE FRAME SECTOR 601R32002-69. LOCATED & DRILLED ON TOP OF NEW FRAME SECTOR 601R32002-69 IAW SRM 51-40-11 AT BS 310 BETWEEN STR 23L AND STR 23R. LOCATED & DRILLED BOTTOM FRAME SECTOR, PN 601R32002-69 AT BETWEEN STR 23L & STR 23R, BS 310 IAW SRM 51-40-11. INSTALLED NEW SERVICEABLE FRAME SECTOR AT BS 310 BETWEEN STR 25L & 25R IAW SRM 51-42-06 & 51-42-21.

Part: SEAT TRACK — CORRODED (BS 409-559) · airframe 31,123 hrs · 28,798 cycles

LT FLOOR SEAT RAIL FROM FS 409+112-FS 559+4 HAS SEVERAL AREAS OF CORROSION AROUND SCREWS. REMOVED LT FLOOR SEAT RAIL FROM FS 409+112 TO FS 559+4 IAW AMM 53-01-11-000-802 AND SRM 51-41-02. LOCATED HOLES IN BULK MATERIAL, PN N126-2075, P/O W35264, FS 409+112-FS 559+4 LT IAW SRM 51-40-11. C/W REO 601R-53-00-485, REV DATED 09/28/12. FABRICATED AND INSTALLED SEAT RAILS IAW GREO 601R-53-00-485, REV A.

Part: SEAT TRACK — CORRODED (BS 409-559) · airframe 31,123 hrs · 28,798 cycles

RT FLOOR SEAT RAIL FROM FS 409+112-559+4 HAS SEVERAL AREAS OF CORROSION AROUND SCREW AND AT LEAST 1 AREA OF INTERGRANULAR. REMOVED RT FLOOR SEAT RAIL FROM FS 409-112 TO FS 559+4 IAW AMM 53-01-11-000-802 AND SRM 51-41-02. LOCATED HOLES IN BULK MATERIAL, PN:N126-2075, PO:W35264, FS 409+112 TO FS 559+4 RT IAW SRM 51-40-11 AND REO:601R-53-00-485. ALODINED, PRIMED AND PAINTED SEAT TRACK IAW REO:601R-53-00-485. COMPLETED STEPS 7 & 8 OF REO:601R-53-00-485. FABRICATED SEAT RAILS IAW GREO:601R-53-00-485, REV A.

Part: FLOOR PANEL — CORRODED (BS 349-461) · airframe 31,123 hrs · 28,798 cycles

LEFT FLOOR SILL PANEL HAS CORROSION AROUND NUTPLATES BETWEEN FS 439 TO FS 461. R & R NUTPLATES BETWEEN FS 439.00 TO FS 461 IAW SRM 51-45-00 AND 51-42-06. COMPLIED WITH EC/TC REO:601R-53-41-666 01 AND REO:601R-53-41-666, REV C.

Part: HINGE — CHAFED (PAX DOOR) · airframe 31,123 hrs · 28,798 cycles

PAX DOOR HINGE ON ACFT SIDE IS CHAFED BY ROLL PIN ON LAST LUG AFT. COMPLIED WITH REO 601R-53-21-814, REPAIR TYPE IV DISPOSITION FOR DAMAGE TO THE HINGE LUG LAND. PASSENGER DOOR HINGE PIN WORN TO LIMITS, REQUIRES REPLACEMENT. INSTALLED NEW SERVICEABLE PASSENGER DOOR HINGE PIN PN 600-31445-7 IAW AMM 52-11-00-400-802. PERFORMED PRESSURIZED CHECK OF FITS & CLEARANCES OF PAX DOOR IAW AMM 52-11-00-220-802, CHECKED GOOD.

Part: FRAME — CORRODED (BS 295) · airframe 31,123 hrs · 28,798 cycles

FS 295, FRAME HAS CORROSION BETWEEN 26L AND 25L ON AFT SIDE. REMOVED AVIONICS BAY FLOOR SUPPORT BRACKET AT FS 295, BETWEEN STR 25L & 25R IAW SRM 51-42-06. INSTALLED SERVICEABLE AVIONICS BAY FLOOR SUPPORT BRACKET AT FS 295 IAW SRM 51-42-06. REMOVED FS 295, FRAME REINFORCING ANGLE AND LT, RT SPLICE ANGLES IAW SRM 51-42-06. INSTALLED SERVICEABLE FS 295 FRAME REINFORCING ANGLE & LT, RT SPLICE ANGLES.

Part: FLOOR SUPPORT — CORRODED (BS 409-559) · airframe 31,123 hrs · 28,798 cycles

RT PRESSURE FLOOR SUPPORT ANGLE HAS NUMEROUS LOCATION OF CORROSION, FILIFORM, FROM FS 409+128 TO FS 559. COMPLIED WITH EC/TC REO 601R-53-41-666 01 AND REO 601R-53-41-666, REV C.

Part: ANGLE — CORRODED · airframe 31,123 hrs · 28,798 cycles

SERVICE DOOR LOWER SILL ANGLE IS CORRODED IN SEVERAL AREAS. REMOVED SERVICED DOOR LOWER SILL ANGLE IAW SRM 51-40-11. INSTALLED NEW LOWER SILL ANGLE AT SERVICE DOOR IAW SRM 51-42-13, 51-42-21, PN 601R38303-253. RECEIVED NEW LOWER SILL ANGLE, PN 601R38303-253. LOCATED & DRILLED NEW LOWER SILL ANGLE IAW SRM 51-40-11, PN 601R38303-253. INSTALLED, 8 EA, RIVNUTS ON LOWER SILL ANGLE IAW SRM 51-42-34.

Part: CABLE — CHAFED (RT PYLON) · airframe 31,123 hrs · 28,798 cycles

RIGHT PYLON, GREEN IDG CABLE IS CHAFED, APPROXIMATELY 6"-7" OTBD OFF FEED THRU. REPAIRED GREEN 1DG CABLE IN THE RT PYLON IAW REO 601R-24-21-004. COMPLIED WITH EC/TC REO 601R-24-21-004 AND GREO 601R-24-21-004, REV A DATED 07/14/2011 AS WRITTEN.

Part: CABLE — CHAFED (LT PYLON) · airframe 31,123 hrs · 28,798 cycles

LT PYLON, WHITE AND GREEN IDG CABLES ARE CHAFED OTBD OF FEED THRU. REPAIRED WHITE AND GREEN IDG CABLES IN THE LT PYLON IAW REO 601R-24-21-004. COMPLIED WITH EC/TC REO 601R-24-21-004 AND GREO 601R-24-21-004, REV A DATED 07/14/2011 AS WRITTEN.

Part: STRINGER — CRACKED (BS 379) · airframe 31,123 hrs · 28,798 cycles

STR 3L IS CRACKED AT FWD SIDE OF FS 379 APPROXIMATELY .5" LONG. REMOVED FASTENERS FROM STR 3L, FS 379 IAW SRM 51-42-06. COMPLIED WITH SRM 53-00-03, REV 53-51, STR SPLICE REPAIR. INSTALLED STRINGER SPLICE REPAIR AT 3L FWD SIDE OF FS 379 IAW SRM, REV 53-51, SECTION 5A.

Part: SHROUD — CHAFED (RT AILERON LE) · airframe 31,123 hrs · 28,798 cycles

RT AILERON UPPER OTBD L/E SHROUD IS CHAFED FROM 4" INBD OF OTBD HINGE TO OTBD END. BLENDED RT AILERON L/E DAMAGE IAW REO 601R-57-60-013, REV A DATED 08/05/2013. COMPLIED WITH EC/TC REO 601R-57-60-013 IAW REO 601R-57-60-013, REV A.

Part: ISOLATOR — CRACKED (BS 621 BULKHEAD) · airframe 31,123 hrs · 28,798 cycles

FS 621 BULKHEAD FWD FACE ABOVE FLOOR HAS 8 CRACKED SCREW MOUNT ISOLATORS: 4 AT RBL 45, 1 RBL 36, 1 LBL 9, 1 LBL 18 AND 1 LBL 27. REMOVED UNSERVICEABLE ISOLATORS 8 EA IAW SRM 51-42-06. INSTALLED SERVICEABLE ISOLATORS 8 EA IAW SRM 51-42-10.

Part: SHROUD — CHAFED (LT AILERON LE) · airframe 31,123 hrs · 28,798 cycles

LEFT AILERON UPPER L/E SHROUD IS CHAFED FROM ABOUT 6" INBD OF OTBD HINGE TO THE OTBD END. COMPLIED WITH REO 601R-57-60-013, REV A DATE 2013/08/05.

Part: SKIN — DENTED (RT WING) · airframe 30,817 hrs · 28,480 cycles

RIGHT WING FIXED L/E PANEL DENT DAMAGED BY FUEL TRUCK. REMOVED RT WING FIXED L/E PANEL TO SUBMIT DENT DAMAGE. SUBMITTED DENT TO STS ENGINEERING IAW SRM 51-13-01, DENT MEASURES 3.9"L X 3.6"W X .200" DEEP. RECEIVED EA 20-2015-119, 05/18/2015, COLD WORKED DAMAGED AREA RESTORING IT TO ORIGINAL CONTOUR. BLENDED SCRATCHES TO RESTORE CONTOUR, CLEANED REWORKED AREA INSIDE AND OUT. REINSTALLED RT WING FIXED L/E PANEL IAW AMM 57-41-01-04. ALL WORK ACCOMPLISHED IAW EA 20-2015-119.

Part: WIRE — DISCONNECTED (EMERGENCY LIGHTS) · airframe 30,412 hrs · 28,060 cycles

FOUND 4 WIRES GOING TO 2 EMERGENCY LIGHTS ON WARDROBE DAMAGED. REQUIRES NEW PINS/QUICK DISCONNECTS. INSTALLED CONNECTORS FOR EMERGENCY LIGHT AT WAREDROBE IAW ESPM 20-17-00 AND WM 33-51-60. OPS CHECK GOOD IAW AMM 33-51-00.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHTS) · airframe 29,246 hrs · 26,911 cycles

FWD EMERGENCY FLOOD LIGHT INOPERATIVE. ALLOWED EMENGENCY BATTERY PACK TO CHARGE, COMPLIED WITH OPS TEST OF EMERGENCY LIGHTS IAW 33-51-04 AMM OPS TEST CHECK GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 28,370 hrs · 26,067 cycles

RIGHT NR 1 EXTERIOR EMERGENCY LIGHT INOPERATIVE. R & R LAMP IAW AMM 33-51-21. OPS CHECKED GOOD.

Part: ISOLATOR — BROKEN (BS 621 BULKHEAD) · airframe 27,231 hrs · 24,880 cycles

BROKEN ISOLATORS ON FWD SIDE OF FS 621 BULKHEAD. R & R FOUR ISOLATORS IAW SRM 51-42-13-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 27,231 hrs · 24,880 cycles

SEAT TRACK LBL 9 CORRODED BEYOND LIMITS. REMOVED AND INSTALLED SERVICEABLE SEAT TRACK IAW AMM 53-01-11-000-802, & 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 27,231 hrs · 24,880 cycles

SEAT TRACK RBL 9 CORRODED BEYOND SRM LIMITS. REMOVED AND INSTALLED SERVICEABLE SEAT TRACK IAW AMM 53-01-11-000-802 & 53-01-11-400-802.

Part: TRUNNION — CRACKED (RT MLG) · airframe 27,240 hrs · 24,888 cycles

RT MLG TRUNNION HAS ONE FASTENER HOLES WITH CRACK INDICATION. REPAIRED IAW REO 601R-57-21-1973. MAJOR REPAIR

Part: TRUNNION — CRACKED (LT MLG) · airframe 27,240 hrs · 24,888 cycles

LT MLG TRUNNION HAS 3EA HI-LIGHT HOLES WITH CRACK INDICATIONS. REPAIRED IAW REO 601R-5721-1973. MAJOR REPAIR.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 27,231 hrs · 24,880 cycles

FOUND SUPPORT CRACKED. REMOVED FLOOR SUPPORT. LOCATED AND DRILLED IAW SRM 51-40-06 AND SRM 51-40-11. INSTALLED NEW FLOOR SUPPORT PER REO 601R-53-61-1230. REPAIR CLASSIFIED AS MAJOR.

Part: ISOLATOR — BROKEN (BULKHEAD) · airframe 27,231 hrs · 24,880 cycles

ISOLATOR BROKEN ON REAR PRESSURE BULKHEAD FWD FACE AT LBL 9.5. R & R ISOLATOR ON REAR PRESSURE BULKHEAD IAW SRM 51-42-13.

Part: FLOOR SUPPORT — CORRODED (BS 499-513) · airframe 27,231 hrs · 24,880 cycles

CORROSION DAMAGE ON LT SIDE PRESSURE FLOOR SUPPORT ANGLE FS 499 - 513, LBL 43. REPAIRED IAW REO 601R-53-41-666 REV C. CLASSIFIED A MAJOR REPAIR .

Part: FLOORBEAM — CRACKED (BS 484) · airframe 27,231 hrs · 24,880 cycles

PRESSURE FLOORBEAM INBD FLANGE IS CRACKED AT FS 484 AT RBL 36. REPAIRED IAW SRM 51-42-21 AND 51-42-06.

Part: FLOOR SUPPORT — CORRODED (BS 507) · airframe 27,231 hrs · 24,880 cycles

CORROSION DAMAGE ON LT SIDE PRESSURE FLOOR SUPPORT FS 507, LBL 42. REPAIRED IAW REO 601R-53-41-666, REV C. CLASSIFIED A MAJOR REPAIR.

Part: ANGLE — CRACKED (CARGO DOOR) · airframe 27,231 hrs · 24,880 cycles

CARGO DOOR TRACK CROSS MEMBER AFT LOWER ATTACH ANGLE CRACKED. REMOVED ANGLE IAW SRM 51-40-11. LOCATED AND DRILLED BRACKET. INSTALLED ANGLE IAW SRM 51-40-11 AND DWG 601R35050.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 27,231 hrs · 24,880 cycles

AFT PRESSURE BULKHEAD CRACKED IN TWO PLACES AROUND CARGO DOOR CUTOUT AFT LINTEL FITTING. REPAIRED IAW REO 601R-53-61-1230. REPAIR CLASSIFIED AS A MAJOR.

Part: BULKHEAD — CRACKED (AFT) · airframe 27,240 hrs · 24,888 cycles

AFT PRESSURE BULKHEAD SKIN CRACKED ABOVE CARGO DOOR AFT TRACK APPROX 1" LONG. REPAIRED IAW REO 601R-53-61-1541, REV D, DATED 10/31/2011. REPAIR CLASSIFIED AS MAJOR.

Part: FRAME — CRACKED (BS 333) · airframe 27,231 hrs · 24,880 cycles

FRAME BS 333 AT 12 O`CLOCK POSITION IS CRACKED IN HALF. REMOVED DAMAGED FRAME SECTION IAW SRM 51-42-06 AND 51-42-20. LOCATED AND DRILLED REPLACEMENT FRAME IAW SRM 51-42-06. REPAIR CLASSIFIED AS MAJOR.

Part: FLAP — GOUGED (PAX DOOR) · airframe 27,231 hrs · 24,880 cycles

ASD VENT-FLAP GOUGED & DENTED. REPAIRED IAW REO 601R-52-11-1040. CLASSIFIED A MAJOR REPAIR.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 27,231 hrs · 24,880 cycles

ASD AFT DRAG ANGLE CRACKED. REPAIRED IAW REO 601R-52-11-513. REPAIR CLASSIFIED AS MAJOR.

Part: GLOWSTRIP — MISSING (CABIN) · airframe 26,422 hrs · 24,055 cycles

EMERGENCY EXIT ROW 8AB FWD PHOTOLUMINESCENT PATH CHEVRON MARKER MISSING. INSTALLED NEW CHEVRON MARKER AND COVER IAW EO 600-33-0015.

Part: UNKNOWN — ODOR (GALLEY) · airframe 25,256 hrs · 22,813 cycles

ON DESCENT F/A SMELLED AN ELECTRICAL ODOR IN GALLEY AREA, NO VISABLE SMOKE, ODOR WENT AWAY ONCE THE ACFT IS ON THE GROUND. PERFORMED OP'S CK OF LT AND RT PACK IAW AMM 21-51-00. OP'S CK GOOD. NO FURTHER DEFECT NOTED AT THIS TIME.

Part: LIGHT — INOPERATIVE (RT OVERWING) · airframe 24,150 hrs · 21,623 cycles

RIGHT EXTERIOR OVERWING EMERGENCY LIGHT IS INOP. R & R LIGHT IAW AMM 33-51-21. OPS CHECKED GOOD.

Part: FLOOR SUPPORT — CORRODED (BS 349) · airframe 23,166 hrs · 20,535 cycles

FLOORBOARD SUPPORT IN AVIONICS BAY AT FS349.00 CORRODED ON FWD SIDE. REPAIRED IAW REO 601R-53-21-1299, REV.

Part: BEAM — CORRODED (BS 349) · airframe 23,163 hrs · 20,530 cycles

OP 115 AVIONICS BAY BEAM AT FS 349 BTWN STG 26L AND 26R IS CORRODED ON THE FWD SIDE. COMPLIED WITH EC/TC REO 601R-53-21-1299.

Part: BEAM — CORRODED (BS 333) · airframe 23,163 hrs · 20,530 cycles

AVIONICS BAY FUSELAGE BEAM AT FS 333.00 BETWEEN STR 26L- STR 26R IS CORRODED ON FWD AND AFT SIDE. COMPLIED WITH REO 601R-53-21-1299.

Part: FLOOR SUPPORT — CORRODED (CARGO BAY) · airframe 23,163 hrs · 20,530 cycles

CARGO BAY FLOOR SUPPORT AT LBL27 HAS CORRODED NUT PLATES. PERFORMED LPI, TYPE 1, METHOD C ON FABRICATED REPAIR ANGLE IAW SRM 53-00-43 IAW NDT INSP PROCEDURE PT-1 NO INDICATIONS NOTED AT THIS TIME. FABRICATED PARTS IAW SRM 53-00-43, INSTALLED FABRICATED PARTS IAW SRM 53-00-43 REPAIR NR 1.

Part: FLOORBEAM — CORRODED (BS 559) · airframe 23,163 hrs · 20,530 cycles

FLOORBEAM CORRODED AT APPROX 559+96 ON RBL 9. REMOVED CORROSION IAW SRM 51-21-06. FOUND BLEND AREAS WERE WITHIN LIMITS IAW REO 601R-53-00-0005, FIG 1.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 23,163 hrs · 20,530 cycles

CARGO BAY FLOORBEAM AT LBL 27 HAS CORRODED NUT PLATES. REMOVED CORROSION IAW SRM 51-21-06. MECHANICAL MEASURED BLEND AREAS ON LBL 27 BETWEEN FS 621-559+112. ALL BLENDS WITH IN ALLANCE LIMITS IAW SRM 53-61-43 AND 53-00-00. NOMINAL THICKNESS IS .063. REMAINING MIN 15 .058 OR, .006 REMOVED IAW SRM 53-61-43. ALODINED, PRIMED AND PAINTED BLENDED AREAS IAW SRM 51-21-16. 2 LOCATIONS AT APPROX FS 572 AND 600 ON OTBD SIDE OF LBL 27 IS BLENDED OUT OF LIMITS. REPAIRED IAW SRM 53-00-43. CUT OUT DAMAGE, FABRICATED NEW REPAIR ANGLE IAW SRM 53-00-43. PERFORMED EDDY CURRENT INSP OF CUTLINE IAW SRM 53-00-43 NDTM PART 1, 51-20-06. NO INDICATIONS NOTED AT THIS TIME.

Part: ATTACH FITTING — CRACKED (BS 280) · airframe 23,163 hrs · 20,530 cycles

TWO CLIPS CRACKED AT FS 280.00, RBL 9.0. REMOVED CRACKED CLIPS IAW SRM 51-42-06 AND SRM 51-42-21. INSTALLED NEW CLIPS IAW SRM 51-42-06 AND SRM 51-42-21. THIS IS A MINOR REPAIR.

Part: BEAM — CORRODED (BS 349) · airframe 23,163 hrs · 20,530 cycles

AVIONICS BAY FUSELAGE BEAM AT FS 349.00 BETWEEN S26L-R IS CORRODED ON THE FWD SIDE. REMOVE CORROSION & FASTENERS AS REQUIRED. EVALUATE 349 FRAME. REMOVED CORROSION IAW SRM 51-42-06 AND 51-21-06. PERFORMED UT THICKNESS INSP OF BLEND AREA OF FRAME SECTOR IAW MAC NDT INSP PROCEDURE UT-3 MININMUM MATERIAL REMAINING IS .060". REPAIRED IAW REO 601R-53-21-1299.

Part: BEAM — CORRODED (BS 310) · airframe 23,163 hrs · 20,530 cycles

AVIONICS BAY FUSELAGE BEAM AT FS 310.00 IS CORRODED BETWEEN S26L-S26R ON AFT SIDE AND SMALL AREA ON FRONT SIDE AT S27. REMOVED CORROSION DAMAGE IAW SRM 51-42-06 AND SRM 51-21-06.

Part: FLOOR SUPPORT — CORRODED (BS 349) · airframe 23,163 hrs · 20,530 cycles

FLOORBAORD SUPPORT IN AVIONICS BAY AT FS 349.00 CORRODED ON FWD SIDE. REMOVED CORROSION IAW SRM 51-21-06.

Part: BEAM — CORRODED (BS 333 S26L/R) · airframe 23,163 hrs · 20,530 cycles

AVIONICS BAY FUSELAGE BEAM AT FS 333.00 BETWEEN STR26L-STR26R IS CORRODED ON FWD AND AFT SIDE. REMOVED CORROSION IAW SRM 51-42-06 AND SRM 51-21-06.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 23,163 hrs · 20,530 cycles

SEAT TRACK AT APROX FS 559. + 96 AT RBL CORRODED. CORROSION OUT OF LIMITS. REMOVED CORRODED SEAT TRACK IAW AMM 53-01-11-000-802. FABRICATED NEW SEAT TRACK IAW SRM 51-40-06, 51-40-02. INSTALLED NEW SEAT TRACK IAW AMM 53-01-11-400-802.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 23,163 hrs · 20,530 cycles

SEVERAL EMERGENCY LIGHTS INOPERATIVE. R & R NR 3 BATTERY PACK CHARGER ASSY IAW AMM 33-51-05-000-801 AND 33-51-05-400-801.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 22,475 hrs · 19,753 cycles

F/O'S FLASHLIGHT DOES NOT WORK. REPLACED F/O FLASHLIGHT IAW AMM 25-61-00.

Part: DOOR — JAMMED (CABIN) · airframe 22,234 hrs · 19,462 cycles

FLT 5570 - FLIGHT ATTENDANTS REPORTS MAIN PAX DOOR DIFFICULT TO OPEN. COMPLIED WITH PAX DOOR OPS CHECK POSITION CABLE ON DOOR GROUND STAND SUPPORT WHEEL, OK PER CRJ200 AMM 52-11-00.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 20,726 hrs · 17,706 cycles

BURNING ODOR COMING FROM BEHIND CAPT'S SEAT, LIKE RUBBER. POWERED UP ALL SYS. OPENED PILOT SIDE C/B PANELS. INSPECTED, NO DEFECTS FOUND. UNABLE TO DUPLICATE ODOR.

Part: POST — DAMAGED (FUSELAGE) · airframe 19,666 hrs · 16,587 cycles

FS 409.0+128 VERTICAL POST LBL 18.0 HAS INDICATION NOTED AT O/B SIDE WL 69.0 AFT FLANGE APPROX .2 INCH IN LENGTH 50 PERCENT FSH FAILED NDT INSP. REMOVED VERTICAL POST LBL 18 FS 409 + 128 IAW SRM 51-42-06. FABRICATED NEW VERTICAL POST AT LBL 18.0 FS 409.0 + 128 USING 7075.0 .063 PO 104964/1 AS PER SAMPLE IAW SRM 51-24-16 REF DWG 601R32208. HEAT TREATED, FABRICATED NEW VERTICAL POST FROM 7075-0 .071 TO T62 CONDITION IAW AMS 2770. PAINTED IAW SRM 51-25-16. LOCATED, DRILLED & RIVETED INBOARD & OUTBOARD POSTS IAW SRM 51-42-06. INSTALLED VERTICAL POST AT LBL 18.0 FS 409 + 128 IAW REO 601R-53-41-889 AND SRM 51-42-06 & 51-42-22. C/W AS EC/TC REO 601R-53-41-889 AND MET ALL THE REQUIREMENTS OF REO 601R-53-41-889.

Part: ANGLE — CRACKED (CARGO DOOR) · airframe 19,666 hrs · 16,587 cycles

CARGO DOOR SUPPORT BEAM AFT LOWER ANGLE IS CRACKED APPROX .2 INCH IN LENGTH. REMOVED AND REPLACED AFT LOWER ANGLE FOR CARGO DOOR SUPPORT BEAM. INSTALLED WITH LOCK FASTENERS IAW SRM 51-42-21.

Part: ANCHOR FITTING — CRACKED (PAX DOOR) · airframe 19,666 hrs · 16,587 cycles

PAX DOOR FWD/AFT ANCHOR FITTINGS ARE CRACKED. REMOVED PAX DOOR FWD AND AFT ANCHOR FITTINGS AND INSTALLED NEW SERVICEABLE ONES IAW AMM 52-11-17-400-804 STEPS 1-2. WHILE PERFORMING ADJUSTMENT OF PAX DOOR COUNTER BALANCE SYSTEM, FOUND AFT ANCHOR FITTING TO HAVE EXCESSIVE PLAY. PERFORMED ADJUSTMENT CHECK AND OPS CHECK OF FWD ANCHOR FITTING IAW AMM 52-11-17-820-802. OPS TEST GOOD.

Part: ANGLE — DAMAGED (FUSELAGE) · airframe 19,666 hrs · 16,587 cycles

FOUND FS 559 CAP ANGLE HAS A INDICATION NOTED AT LBL 18.0 APPROX .3 INCH LENGTH 80 PERCENT FSH AND RT FS 559 BULKHEAD WEB HAS A INDICATION NOTED AT WL 58.70 TO O/B OF RBL 9. APPROX .2 INCH IN LENGTH 50 PERCENT FSH BOTH FAILED NDT INSP. COMPLIED WITH EC/TC REO 601R-53-41-260 IN ACCORDANCE WITH REO 601R-53-41-260 REV C.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 19,666 hrs · 16,587 cycles

PAX DOOR LOWER SILL ANGLE SEVERELY CORRODED P/N 601R31527-221 LOCATED DIRECTLY BELOW ATTACH NUT PLATES FOR TOP STEP, MARKED. REMOVED PAX DOOR LOWER SILL ANGLE IAW SRM 51-42-06 AND SRM 51-42-10. ANGLE IS OUT OF LIMITS. ANGLE REQUIRES REPLACEMENT. LOCATED SERVICEABLE PAX DOOR LOWER SILL ANGLE IAW SRM 51-40-11. REQUIRES INSTALLATION. INSTALLED PAX DOOR LOWER SILL ANGLE COMMON TO SILL LOCK FASTENERS IAW SRM 51-42-21.

Part: POST — DAMAGED (FUSELAGE) · airframe 19,666 hrs · 16,587 cycles

FS 409+128 VERTICAL POST RBL 18.0 HAS INDICATION NOTED AT I/B SIDE WL 69.0 AFT FLANGE APPROX .2 INCH IN LENGTH 50 PERCENT FSH FAILED NDT INSP. REMOVED POST FS 409 + 128 RBL 18 IAW SRM 51-42-06. FABRICATED NEW VERTICAL POST AT RBL 18.0 FS 409.0 + 128 USING 7075.0 .063 PO 104964/1 AS PER SAMPLE IAW SRM 51-24-16 REF DWG 601R32208. HEAT TREATED, FABRICATED NEW VERTICAL POST FROM 7075.0 .071 TO T62 CONDITION IAW AMS 2770. PAINTED IAW SRM 51-25-16. LOCATED, DRILLED, AND RIVETED I/B AND O/B POSTS IAW SRM 51-42-06. INSTALLED VERTICAL POST RBL 18.0 FS 409 + 128 IAW REO 601R-53-41-889 AND SRM 51-42-06 AND 51-42-22. COMPLIED WITH ECTC REO 601R-53-41-889 AND MET ALL REQUIREMENTS OF REO 601R-53-41-889.

Part: SILL — CORRODED (FUSELAGE) · airframe 19,666 hrs · 16,587 cycles

LT PRESSURE FLOOR SILL ASSY CORRODED ON SILL PNL AND ON FLOOR ANGLE APPROX .002 INCH DEEP FROM FS 513 TO FS 559 UNDER CABIN FLOOR PNL 261DLF. C/W REO 601R-53-41-666 REV O.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 19,666 hrs · 16,587 cycles

RT PRESSURE FLOOR SILL ASSY ANGLE CORRODED APPROX .003 INCH DEEP AT FS 473.15 UNDER CABIN FLOOR PNL 262DRF. C/W REO 601R-53-41-666 REV O.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 19,666 hrs · 16,587 cycles

RIGHT FS 460 FLOOR SUPPORT FITTING CRACKED .5 INCH LONG UNDER CABIN FLOOR PNL 262CRF O/B SIDE OF RBL 9.0. REMOVED CRACKED FLOOR SUPPORT FITTING AT FS 460 RT SIDE AND REPLACED WITH NEW SERVICEABLE FLOOR SUPPORT FITTING IAW CRJ 200 SRM 51-42-21 AND 51-42-06.

Part: DOOR — BINDING (ASD) · airframe 19,178 hrs · 16,124 cycles

ASD HARD TO CLOSE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 18,438 hrs · 15,428 cycles

LT AFT FUSELAGE EMERGENCY LIGHT INOP ON EXTERIOR FUSELAGE.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 17,926 hrs · 14,969 cycles

FIRST OFFICER`S FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED FIRST OFFICER`S FLASHLIGHT. OPS CHECK GOOD IAW AMM 25-61-04. (S)

Part: PUMP — MALFUNCTIONED (HYDRAULIC SYS) · airframe 1,740,010 hrs · 14,513 cycles

HYD 1 LOW PRESS WARNING FOLLOWED BY HYD EDP 1A WARNING OPERATED ENGINE 1. 11 WITH THE FAILED PUMP. PUMP CAVATED A LOUD NOISE AND VIBRATION AFTER T/O. AIRCRAFT RETURNED TO ATL AFTER T/O. EMERGENCY DECLARED. FLT 4596 DEL 126 MINS REMOVED AND REPLACED NR 1 HYD EDP IAW CRJ200AMM29-11-00. OPS CHECK GOOD, [SDR CLOSED]

Part: INDICATOR — MISSING (CABIN) · airframe 17,217 hrs · 14,363 cycles

PHOTOLUMINESCENT AISLE PATH MARKERS MISSING END INDICATOR DOTS.

Part: SUPPORT BEAM — CRACKED (BS 640) · airframe 16,675 hrs · 13,894 cycles

ENGINE SUPPORT BEAM UPPER WEB CRACKED AT AFT EDGE, FS 640, LBL8.0, WL119.12, MEASURES .80 INCHES LONG. ACCOMPLISHED REPAIR TO ENG SUPPORT BEAM BY COMPLYING WITH REO 601R-53-61-345 IAW ASA EO 600-53-0072B CARD EO 600-53-72-0001.

Part: LIGHT — INOPERATIVE (BS 302) · airframe 16,426 hrs · 13,683 cycles

EXTERIOR EMERGENCY LIGHT FORWARD OF THE PASSENGER DOOR AT FS 302.40L IS INOP.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 15,913 hrs · 13,223 cycles

STRONG SMELL OF FUEL IN COCKPIT AND CABIN IN FLT ON APU OR ENG BLEEDS. SMELL GOT WORSE ON THE GROUND WITH SEVERAL OF PASSENGERS COMPLAINING OF NAUSEA AND HEADACHE.

Part: HINGE FITTING — CRACKED (ESCAPE HATCH) · airframe 15,338 hrs · 12,781 cycles

CREW ESCAPE HATCH AFT RIGHT HINGE ARM CRACKED.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 15,338 hrs · 12,781 cycles

FS 280 FLOOR SUPPORT ANGLE IS CRACKED, JUST O/B OF THE LBL 27.0. UPON REMOVAL OF DAMAGED SECTION OF SUPPORT ANGLE THE 280 WEB WAS FOUND TO HAVE MINOR SURFACE CORROSION. REMOVED MINOR SURFACE CORROSION AT 280 WEB PER: CRJ SRM 53-00-00. APPLIED CORROSION PROTECTION PER: CRJ SRM 51-21-11. APPLIED FR7 PRIMER PER: CRJ SRM 51-25-06. REPAIRED FS 280 SUPPORT ANGLE, IAW REO 601R-53-11-136. 06/28/07 REQUIRES TOPCOAT TO FASTENERS AND CIC. 06/28/07 REPAIRED J-ANGLE ON THE PILOTS BULKHEAD AT FS 280 LT BL 9.0, IAW EO 600-53-0091. SUPPLEMENTAL - SDR CLOSED 07/03/07.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 15,338 hrs · 12,781 cycles

FS 280 FLOORBEAM ATTACHMENT CLIP ON I/B SIDE OF RBL 27.0 IS CRACKED. REMOVED DAMAGED ANGLE & FS 280 RBL 9.0 I/B SIDE DUPLICATED SERVICEABLE ANGLE FROM 2024-T3 .050 PO10404 LOCATED AND DEBURRED IAW CRJ SRM 53-21-43. ALODINED AND PRIMED SERVICEABLE ANGLE IAW CRJ SRM 51-25-06. TOP COATED AND INSTALLED SERVICEABLE ANGLE WITH HST 10AG-5, HILITES AND KFM 586-08 NUTS IAW CRJ SRM 51-42-21. SUPPLEMENTAL - SDR CLOSED 07/03/07.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 15,338 hrs · 12,781 cycles

FS 280 FLOORBEAM ATTACHMENT CLIP O/B OF RBL 27.0 IS CRACKED.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 15,338 hrs · 12,781 cycles

FS 280 FLOOR SUPPORT ANGLE IS CRACKED, JUST O/B OF THE LBL 27.0. FABRICATED NEW O/B CLIP LBL 9, AND LOCATED HOLES, IAW CRJ SRM 51-24-26 AND 51-40-11. 06/28/07 INSTALLED CLIP, IAW CRJ SRM 51-42-06 AND 51-42-21. 06/28/07, AT FS 280 LBL 9. SUPPLEMENTAL - SDR CLOSED 07/03/07.

Part: PLACARD — MISSING (ESCAPE HATCH) · airframe 15,338 hrs · 12,781 cycles

CREW ESCAPE HATCH MISSING PLACARDS.

Part: WEB — CRACKED (PAX DOOR) · airframe 15,338 hrs · 12,781 cycles

PAX DOOR UPPER STEP FWD WEB IS CRACKED IN THE RADIUS OF THE CORNER, UNDER THE HANDRAIL SUPPORT FITTING.

Part: HANDLE — CRACKED (PAX DOOR) · airframe 15,338 hrs · 12,781 cycles

PAX DOOR OUTER HANDLE IS CRACKED. [07-26-07] REPAIRED IAW AMM 52-11-03, MM 52-11-25, MM 52-11-03, SRM 51-25-16, AND AMM 52-11-03

Part: WEB — CRACKED (PAX DOOR) · airframe 15,338 hrs · 12,781 cycles

PAX DOOR UPPER STEP AFT WEB IS CRACKED IN THE RADIUS OF THE CORNER UNDER THE HANDRAIL SUPPORT FITTING.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,541 hrs · 12,186 cycles

EMERGENCY LIGHTING AT FLOOR LEVEL INOP FROM ROW 9 AFT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,730 hrs · 11,595 cycles

FLOOR EMERGENCY LIGHTING FROM ROW 8 BACK IS INOP. FLT 4613 DEL 285 MINS.

Part: STEERING SYS — MALFUNCTIONED (NLG) · airframe 13,308 hrs · 11,266 cycles

STEERING INOP CAUTION MESSAGE ON T/O . LANDED WITH NWS OFF, RESET, TAXIED IN NORMALLY. (EMERGENCY DECLARED)

Part: DOOR — STUCK (PAX) · airframe 13,188 hrs · 11,175 cycles

PAX DOOR WILL NOT OPEN

Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,137 hrs · 11,135 cycles

FOUND LT FUSELAGE EMERG LIGHT FWD OF LEADING EDGE INOP.

Part: DOOR — MALFUNCTIONED (MAIN PAX) · airframe 13,137 hrs · 11,135 cycles

THE PAX DOOR WILL NOT CLOSE AND LOCK, FLTS 4280,4903 CX.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 12,728 hrs · 10,805 cycles

R/H AFT EMER LIGHT INOP

Part: LIGHT — INOPERATIVE (FUSELAGE) · airframe 12,580 hrs · 10,690 cycles

FOUND RT FUSELAGE 1 EXTERIOR EMERGENGY LIGHT INOP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 12,309 hrs · 10,483 cycles

AFT EXT EMERG LIGHT ON RT SIDE INOP.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 12,301 hrs · 10,477 cycles

EMERGENCY LIGHTS ARE ON IN ARMED POSSITION... FLTS 4150 + 4383 CX

Part: LAMP — BURNED OUT (FUSELAGE)

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

Part: STEP — DELAMINATED (FUSELAGE)

DURING A GROUND INSPECTION, THE PASSENGER DOOR BOTTOM STEP WAS FOUND TO BE DELAMINATED. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR BOTTOM STEP IAW AMM. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: STEP — BROKEN (PAX DOOR)

DURING A GROUND INSPECTION IN MCO, THE PASSENGER DOOR BOTTOM STEP WAS FOUND TO BE BROKEN. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR BOTTOM STEP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

FLT 4186 - DURING A GROUND INSPECTION IN CAE, THE RIGHT SIDE OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE RIGHT SIDE OVERWING EMERGENCY LIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LAMP — BURNED OUT (EMERGENCY LIGHT)

FLT 4861 - DURING HANGAR MAINTENANCE IN BTR, THE FORWARD EMERGENCY CEILING LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE FORWARD EMERGENCY CEILING LIGHT. OPERATIONAL CHECKS GOOD. (M)

Part: ENGINE — OVERSERVICED (RIGHT)

DURING CRUISE, AT APPROX 28,000 FEET, RT ENGINE OIL TEMP INDICATED IN YELLOW RANGE AT APPROX 160 DEGREES C, THEN INCREASED INTO RED RANGE INDICATING A HIGH OF 165 DEGREES C WITH RT ENGINE OIL PRESSURE INDICATING 44-50 PSI. CREW COMPLIED WITH THE QRH AND REDUCED THE RT ENGINE TO IDLE. AFTER SEVERAL MINUTES, RT ENGINE OIL TEMP DECREASED TO NORMAL AND WAS LEFT AT IDLE FOR THE REMAINDER OF FLIGHT. EMERGENCY WAS DECLARED AND AC LANDED SAFELY. MAINTENANCE FOUND RT ENGINE OIL OVER SERVICED. DRAINED THE ACCY GEAR BOX, PROPERLY SERVICE THE ENGINE OIL AND COMPLIED WITH HIGH POWER GROUND RUNS. ENGINE OIL TEMPERATURE AND PSI INDICATIONS WERE NORMAL. OPS CHECK GOOD. AC OK FOR SERVICE. (K)

Part: ENGINE — MALFUNCTIONED (RIGHT)

DURING CLIMB OUT, AT APPROXIMATELY 12,000 FEET THE CREW RECEIVED A (RT ENGINE OIL PRESSURE) WARNING WITH THE OIL TEMPERATURE INCREASING TO 153 DEGREES CENTIGRADE AND THE OIL PRESSURE FLUCTUATING BETWEEN 24-36 PSI. QRH WAS COMPLIED WITH AND AN EMERGENCY WAS DECLARED. THE AIRCRAFT DIVERTED AND LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE RT ENGINE. OPERATIONAL AND LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE.

Part: WARNING LIGHT — ILLUMINATED (RT ENGINE)

DURING CRUISE, AT APPROX 30,000 FT, CREW RECEIVED A (R ENG OIL PRESS) WARNING MESSAGE. QRH WAS COMPLIED WITH AND THE POWER LEVER WAS BROUGHT TO IDLE WITH THE OIL PRESSURE STABILIZING AT 25-30 PSI. DURING DESCENT THROUGH 10, 000 FEET THE OIL PRSSURE STABILIZED AT 45 PSI AND REMAINTED THROUGH LANDING. AN EMERGENCY WAS DECLARED, AC DIVERTED, LANDING SAFELY. MAINTENANCE INSPECTD RT ENGINE FOR OIL LEAKAGE, SERVICED IT WITH 1.5 QUARTS OF OIL AND RAN THE ENGINE THROUGH ALL POWER SETTINGS. NO DEFECTS WERE FOUND. OPERATIONAL AND LEAK CHECKS GOOD. AC OK FOR SERVICE. (K)

Part: PRESSURE SWITCH — MALFUNCTIONED (RT ENGINE OIL)

DURING CLIMB OUT, AT APPROXIMATELY 16,000 FEET, THE CREW RECEIVED A (R ENG OIL PRESS) MESSAGE. QRH WAS COMPLIED WITH AND POWER WAS BROUGHT BACK TO IDLE ON THE RT ENGINE. OIL PRESSURE STABILIZED AND THE AC CONTINUED ON. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE RT ENGINE OIL PRESSURE SWITCH AND TRANSDUCER. OPERATIONAL AND LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: STEP — CRACKED (PAX DOOR)

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

Part: FITTING — CRACKED (PAX DOOR)

DURING HANGAR MAINTENANCE IN MCN, THE AFT ANCHOR FITTING ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFT ANCHOR FITTING ON THE PASSENGER DOOR. (M)

Part: MOTOR — INOPERATIVE (ACTUATOR)

FLT 4282 - DURING A GROUND INSPECTION IN ABE, THE PASSENGER DOOR WAS FOUND JAMMED CLOSED TAKING OVER FIFTEEN MINUTES TO OPEN. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR ACTUATOR MOTOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

FLT 4201 - DURING A GROUND INSPECTION IN ATL, THE EMERGENCY LIGHTS REMAINED ON WHEN IN THE ARMED OR OFF POSITIONS. MAINTENANCE REMOVED AND REPLACED ALL FOUR OF THE EMERGENCY LIGHT BATTERY PACKS. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

FLT 4430 - FOLLOWING SHUTDOWN OF THE AIRCRAFT IN ATL, THE CREW RECEIVED AN EMERGENCY LIGHTS ON STATUS MESSAGE WITH THE EMERGENCY LIGHTS N THE ARMED POSITION AND THE FLIGHT ATTENDANTS PANEL IN THE OFF POSITION. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHTS BATTERY PACKS. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: CLIP — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE LEFT AND RIGHT PRESSURE WALL CLIP AT FS 625 AFT EQUIPMENT BAY WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE LEFT AND RIGHT PRESSURE WALL CLIP AT FS 625 AFT EQUIPMENT BAY. (M)

Part: SILL — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE CARGO BAY FLOOR SILL PLATE AT FS 562.72-589 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CARGO BAY FLOOR SILL PLATE AT FS 562.72-589 IAW ASA EO 600-53-0095. (M)

Part: CLIP — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE OUTBOARD CLIP AT FS 280, LBL 9 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE OUTBOARD CLIP AT FS 280, LBL 9 IAW SRM 51-42. (M)

Part: SUPPORT ANGLE — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, LEFT AND RIGHT FLOOR SUPPORT ANGLES AT FS 621 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LEFT AND RIGHT FLOOR SUPPORT ANGLES AT FS 621 IAW ASA EO 600-53-0105. (M)

Part: CLIP — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE LEFT AND RIGHT CLIPS AT FS 484, LBL 27 AND RBL 36 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LEFT AND RIGHT LCIPS AT FS 484, LBL 27 AND RBL 36 IAW ASA EO 600-53-0098. (M)

Part: STEP — CRACKED (PAX DOOR)

DURING A C-CHECK IN MCN, THE PASSENGER DOOR TOP STEP WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR TOP STEP CLIP AT FS 625 AFT EQUIPMENT BAY. (M)

Part: STEP — BROKEN (PAX DOOR)

DURING A GROUND INSPECTION IN DFW, THE PASSENGER DOOR BOTTOM STEP WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR BOTTOM STEP ASSEMBLY. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: PDU — INOPERATIVE (THRUST REVERSER)

FLT 4766 - DURING CLIMB-OUT FROM RDU-DFW, AT APPROXIMATELY 14,000 FEET THE CREW RECEIVED A RIGHT THRUST REVERSER UNLOCKED CAUTION MESSAGE. QRH PROCEDURES WERE COMPLIED WITH, AN EMERGENCY DECLARED AND THE AIRCRAFT RETURNED TO RDU, LANDING SAFELY. MAINTENANCE DEFERRED THE RIGHT THRUST REVERSER ON 12/3/2003 UNDER MEL NR 78-30-01. THE ABOVE DISCREPANCY WAS UNDER CONTINUED DEFERRAL WITH THE REPAIRS PERFORMED ON 12/5/2003 AND THE CORRECTIVE ACTION SHOWN ON MRR NR 03624, IN WHICH MAINTENANCE REMOVED AND REPLACED THE POWER DRIVE UNIT SHOWN BELOW AT THAT TIME. (M)

Part: PDU — INOPERATIVE (THRUST REVERSER)

DURING CRUISE FROM IND-DFW, AT APPROXIMATELY 31,000 FEET THE CREW RECEIVED A RIGHT THRUST REVERSER UNLOCK CAUTION MESSAGE. QRH PROCEDURES WERE COMPLIED WITH, AN EMERGENCY DECLARED AND THE AIRCRAFT DIVERTED INTO LIT, LANDING SAFELY. MX DEFERRED THE RIGHT THRUST REVERSER ON 12/3/2003 UNDER MEL NR 78-30-01, AND CLEARED THE DEFERRAL ON 12/5/2003 BY REMOVING AND REPLACING THE POWER DRIVE UNIT ON THE RIGHT THRUST REVERSER. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LIGHT — MISSING (CABIN)

FLT 4853 - DURING A GROUND INSPECTION IN DFW, THE EMERGENCY FLOOR LIGHT STRIP AT ROWS FOUR AND FIVE WAS FOUND TO BE MISSING. MAINTENANCE REPLACED THE EMERGENCY FLOOR LIGHT STRIP AT ROWS FOUR AND FIVE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: FLAP — MALFUNCTIONED (WING)

FLT 4450 - ON DESCENT INTO VPS, CAPTAIN RECEIVED A FLAP FAIL MESSAGE. AN EMERGENCY WAS DECLARED AND A 0 FLAP LANDING WAS MADE. AIRCRAFT LANDED SAFELY IN VPS. REVIEWED HISTORY AND NO FLAP FAILURE HISTORY WAS FOUND. INTERROGATED FECU. SYSTEM TEST PASSED. RESET C/B'S AND FLAP SYSTEM. NO DEFECTS NOTED THROUGH FIVE COMPLETE FLAP CYCLES. AIRCRAFT OK FOR SERVICE. (M)

Part: FLAP — MALFUNCTIONED (WING)

FLT 4463 - ON APPROACH INTO SHV, THE FLAPS FAILED AT 20 DEGREES. THE CAPTAIN FOLLOWED THE APPROPRIATE QRH PROCEDURES. AN EMERGENCY WAS DECLARED AS A PRECAUTION. AIRCRAFT LANDED SAFELY IN SHV. MAINTENANCE RESET THE FLAP SYSTEM AND FOUND IT TO OPERATE NORMALLY. THE FLAPS WERE RUN THROUGH SEVERAL CYCLES WITH NO DEFECTS NOTED. NO FAULTS WERE LOGGED IN THE MAINTENANCE DIAGNOSTIC COMPUTER OR THE AIR DATA COMPUTER. AIRCRAFT RETURNED TO SERVICE. (M)

Part: ELEMENT — MALFUNCTIONED (LT ENGINE)

FLT 4579 - DURING CLIMB-OUT OF TOL, THE LEFT 14TH DUCT LIGHT ILLUMINATED ALONG WITH AN ASSOCIATED AURAL BLEED AIR DUCT MESSAGE. THESE WARNINGS LASTED 1-2 SECONDS AND THEN WENT AWAY BUT CONTINUED TO INTERMITTENTLY REAPPEAR. AFTER THE PILOT HAD TRIED TO RETARD THE THRUST LEVER IN ORDER TO ELMINATE THE WARNINGS, THE WARNINGS APPEARED AND WOULD NOT STOP. THE CAPTAIN SECURED THE ENGINE AND DECLARED AN EMERGENCY. THE AIRCRAFT DIVERTED TO CVG FOR A SAFE LANDING. MAINTENANCE REMOVED AND REPLACED THE LEFT 14TH DUCT SENSING ELEMENT IN THE LEFT ENGINE PYLON. THE ENGINES WRE RAN FOR 30 MINUTES AND NO FAULTS APPEARED. OPS CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (M)