N851AS

Part: SEAT TRACK — CORRODED (BS 409-559) · airframe 36,060 hrs · 32,686 cycles

FLOOR SEAT RAIL BETWEEN FS 409.00+128 AND FS559.00 AT RBL 9 IS CORRODED. EVALUATED AND FOUND DAMAGE TO BE OUT OF LIMITS REF SRM 53-41-49. R & R SEAT RAIL BETWEEN FS 409.00+128 AND FS 559.00 AT RBL 9 REF COMPLIED WITH GREO 601R-53-00-485, REV A, AMM 53-01-11-000-802, 53-01-11-400-802. RECEIVED EC/TC FABRICATED SEAT RAILS IAW GREO 601R-53-00-485, REV A.

Part: SEAT TRACK — CORRODED (BS 409-559) · airframe 36,060 hrs · 32,686 cycles

SEAT RAIL BETWEEN FS 409.00+128 AND FS 559.00 AT LBL9 IS CORRODED. REMOVED SEAT RAIL BETWEEN FS 409 + 128 & FS 559.00, LBL 9 IAW AMM 53-01-11-000-802. INSTALLED SEAT RAIL BETWEEN FS 409+128-FS 559.00 IAW AMM 53-01-11-400 802. FINISHED COUNTERSINKING & INSTALLED SEAT RAIL IAW AMM 53-01-11-400-802, SRM 51-40-11. COMPLIED WITH REO 601R-53-00-485 ECTC. FABRICATED SEAT RAILS IAW GREO 601R-53-00-485, REV A, REO 601R-53-00-485.

Part: SKIN — CRACKED (RT WING) · airframe 36,060 hrs · 32,686 cycles

DURING FASTENER HOLE INSPECTION OF RT LOWER WING PLANK 1EA HOLE HAS CRACK INDICATION. RECEIVED & COMPLIED WITH ADR JLEB-15-3626196, REF SRM 51-40-11. RECEIVED & COMPLIED WITH FINAL REO 601R-57-21-2394. RECEIVED & COMPLIED WITH ECTC REO 601R57-21-2394.

Part: PLATE — CORRODED (BS 589-605) · airframe 36,060 hrs · 32,686 cycles

CORROSION FOUND TIE DOWN BLOCK AT BS 589 - 605 AND LBL9. R & R ANCHOR PLATE IAW SRM 51-41-02.

Part: FLOOR SUPPORT — CORRODED (BS 589-605) · airframe 36,060 hrs · 32,686 cycles

CORROSION FOUND ON FLOORBEAM, OTBD SIDE, FS 589.00-605.00 AND LBL9. REMOVED DAMAGE AND FOUND NOT WITHIN LIMITS IAW SRM 53-00-00. REMOVED FLOOR SUPPORT BEAM CAP IAW SRM 51-42-21, 51-42-06. STARTED INSTALLATION OF LT SIDE OF NEW SERVICABLE FLOOR SUPPORT BEAM CAP IAW SRM 51-42-21. INSTALLED REMAINING FASTENERS EXCEPT FASTENERS THRU FLOOR RAIL FITTING AT FS 621 IAW REO 601R 53-61-3780, REV A. INSTALLED FLOOR RAIL FITTING AT FS 621 REF AMM 20-21-00, SRM 51-42-22, REO 601R 53-61-3780, REV A. COMPLIED WITH ECTC REO 601R-53-61-3780 AND REO 601R-53-61-3780, REV A DATE 7/15/2011 AS WRITTEN. REO 601R-53-61-37890 IS CLASSIFIED AS A MAJOR ALTERATION.

Part: PLATE — CORRODED (BS 559) · airframe 36,060 hrs · 32,686 cycles

CORROSION FOUND ON TIE DOWN LOCK AT FS559+96-559-.00+112 AND F, LBL27. R & R ANCHOR PLATE AT 559.00+96-559.00+112 AND LBL27 IAW SRM 51-41-02. UPON REPLACMENT OF ANCHOR PLATE AT 559.00+96-559.00+112, LBL27 FOUND ANCHOR PLATE FWD OF THAT TO BE CORRODED ALSO. REPLACED ANCHOR PLATE IAW SRM 51-41-02 AT FS 559.00+96-559.00+112 AND LBL27.

Part: SEAT TRACK — CORRODED (BS 559-574) · airframe 36,060 hrs · 32,686 cycles

CORROSION FOUND FOUND ON SEAT TRACK AT FS559.00+112-574.00, LBL9. REMOVED CORROSION IAW SRM 51-21-06-00. SEAT TRACK OUT OF LIMITS IAW SRM 53-61-49. REMOVED SEAT TRACK IAW SRM 51-41-00. INSTALLED NEW SEAT TRACK IAW AMM 53-01-11-400-802. COMPLIED WITH EC/TC REO 601R-53-00-485. FABRICATED SEAT RAILS IAW GREO 601R-53-00-485, REV A.

Part: STRUCTURE — CORRODED (BS 559) · airframe 36,060 hrs · 32,686 cycles

CORROSION FOUND RBL4.0 SILL AT 559+80-559.00+96. BLENDED CORROSION IAW SRM 51-21-06. COMPLIED WITH EC/TC REO 601R-53-00-526 01 AND GREO 601R-53-00-526, REC, DATED 05-22-2013 AS WRITTEN.

Part: DOOR SILL — CRACKED (BS 589-605) · airframe 36,060 hrs · 32,686 cycles

CRACKS FOUND ON CARGO DOOR SILL AT FS589.00 AND 605.00 AND LBL 4.0. COMPLIED WITH EC/TC REO 601R-53-61-433 AND REO 601R-53-61-433, REV B, DATED 10/9/2009 AS WRITTEN.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 36,060 hrs · 32,686 cycles

CORROSION FOUND ON SEAT TRACK BETWEEN 559.00+80 TO 559.00+98 AND RBL 9. REMOVED SEAT TRACK FROM FS 559.+87 TO 559+96 RBL9 IAW AMM 53-01-11-000-802. INSTALLED NEW SEAT TRACK BETWEEN FS 559.+80 AND FS 559.00+96 AT RBL9 REF: AMM 53-01-11-400-802. REMOVED SEAT TRACK FROM FS 559+87 TO 559.00+96 RBL9 IAW AMM 53-01-11-000-802. INSTALLED SERVICEABLE SEAT TRACK FS FS 559+87 TO 559.00+96, RBL9 IAW AMM 53-01-11-400-802. COMPLIED WITH EC/TC REP 601R-53-00-485. FABRICATED SEAT RAILS IAW GREO 601R-53-00-485, REV A.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 36,060 hrs · 32,686 cycles

CORROSION FOUND ON SEAT TRACK AT 559.00+ 559.00+96 AND RBL 27. EVLAUATED AND FOUND DAMAGE TO BE OUT OF LIMITS IAW SRM 53-51-49. R & R SEAT RAIL BETWEEN FS 559.00+80 AND 559.00+96, RBL 27, REF: AMM 53-01-11-000-802 AND 53-01-11-400-802. FABRICATED SEAT RAILS IAW GREO 601R-53-00-485, REV A, FS559.00+80-FS559.00+96, RBL27.

Part: PLATE — CORRODED (BS 574-589) · airframe 36,060 hrs · 32,686 cycles

CORROSION FOUND TIE DOWN BLOCK AT BS 574 - 589 AND LBL9. R & R ANCHOR PLATE IAW SRM 51-41-02.

Part: FRAME — CORRODED (BS 559) · airframe 36,060 hrs · 32,686 cycles

CORROSION FOUND AROUND SCREW HOLES AT FS 559.00+69 AND 559.00+80 RBL9 ON OTBD SIDE. REMOVED DAMAGE AND FOUND NOT WITHIN LIMITS IAW SRM 53-00-00 AT FS 559+69 AND 559+80 RBL9. REPAIRED FLOORBEAM AT FS 559.00+69 TO 559.00+80 RBL9 IAW SRM 53-00-43 FLOOR SUPPORT STRUCTURE REPAIR NR 1 PROCEDURE 59 REAPPLIED CK. REMOVED FOR REPAIR AND DWG 601R311119.

Part: SKIN — CRACKED (RT WING) · airframe 36,060 hrs · 32,686 cycles

RT WING PLANK CRACKED AT WS 148.019. REMOVED RT INBD LOWER T/E INBD OF "PIE PANEL" IAW SRM 51-42-21, 51-42-06. INSTALLED INBD LOWER T/E INBD OF "PIE PANEL", REF SRM 51-42-06 AND SRM 51-42-21 AND DWG 601R10225. COMPLIED WITH ECTC REO 601R-57-21-130 01 AND REO 601R-57-21-130, REV K DATED 11/27/2013 AS WRITTEN. COMPLIED WITH ECTC REO 601R-57-21-131 AND REO 601R-57-21-131 IAW B DATED 11/28/2013 AS WRITTEN. INSTALLED -10 REPAIR STRAP AS REQUIRED, REF SRM 51-42-21 AND REO 601R-57-21-130-01.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 36,014 hrs · 32,635 cycles

RIGHT EXTERIOR EMERGENCY LIGHT NR 2 INOPERATIVE. RELAMPED RT EXTERIOR EMERGENCY LIGHT NR 2 IAW AMM 33-51-21. OPS CHECK GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 34,827 hrs · 31,378 cycles

AFT CENTER CEILING EMERGENCY LIGHTS INOPERATIVE. REPLACED NR 2 EMERGENCY LIGHT BATTERY IAW AMM 33-51-24-400-801. OPS CHECK GOOD IAW AMM 33-51-00-710-801. VERIFIED NR 2 EMERGENCY LIGHT BATTERY IS EFFECTIVE FOR INSTALLATION ON THIS ACFT IAW AMM SUPPLEMENT 33-51-04I17.

Part: BULKHEAD — CRACKED (BS 621) · airframe 34,827 hrs · 31,378 cycles

2 INDICATIONS NOTED AT 621 REAR PRESSURE BULKHEAD FWD FACE AT BL 0.0, WL 110 APPROXIMATELY 1.350" IN LENGTH VERTICALLY AND 90 PERCENT FULL SCREEN HEIGHT INDICATION AND WL 108 APPROXIMATELY .250 IN LENGTH VERTICALLY AT 20 PERCENT FULL SCREEN HEIGHT. FAILING NDT. CUT OUT DAMAGED PORTION OF WEB IAW NOTE 1 OF REO 601R-53-61-1285. CUT UPPER STRAP ON FS 621.00 IAW SHEET 12, VIEW C OF REO 601R-53-61-1285. MANUFACTURED ALL REPAIR PARTS TO FIT SURROUNDING STRUCTURE IAW REO:601R-53-61-1285, REF NOTE 5, NOTES 3 THRU 9 COMPLIED WITH, NOTE 2 NOT APPLICABLE.

Part: STIFFENER — CRACKED (CARGO DOOR) · airframe 34,827 hrs · 31,378 cycles

CARGO DOOR AFT VERTICAL MEMBER, PN:601R35027-31, CRACKED APPROXIMATELY 5" LONG INSIDE OF DOOR FS 605. REMOVED AFT VERTICAL MEMBER IAW SRM 51-42-06. INSTALLED NEW AFT VERTICAL MEMBER IAW SRM 51-42-06. LOCATED AND DRILLED NEW AFT VERTICAL MEMBER IAW SRM 51-40-11. COMPLIED WITH IAW AMM 52-31-00-400-801. OPS CHECKED GOOD AND CLEARANCE CHECKED GOOD.

Part: SKIN — BURNED (BS 265) · airframe 33,943 hrs · 30,484 cycles

ONE BURNED FASTENER ON BS 265 STRINGER 16L. FOUND DAMAGE CONTAINED TO FASTENER HEAD ONLY. REMOVED FASTENER IAW SRM 51-42-06. COMPLED WITH EC/TC REO 601R-53-00-115. WET INSTALLED TEMP FASTENER, CR3222 4-3 IAW REO 601R-53-00-115, REV E. RESTORED SURFACE FINISH IAW SRM 51-25-01. CREATED MCO A190649 IAW SOP 5719. THIS IS CONSIDERED A MAJOR REPAIR IAW GMM 5-3.

Part: SKIN — DAMAGED (BS 235) · airframe 33,943 hrs · 30,484 cycles

ONE BURN LOCATED 1 INCH AFT OF BS 235 AND ON STRINGER 16L. FOUND DAMAGE CONTAINED TO FASTENER HEAD ONLY. REMOVED FASTENER IAW SRM 51-42-06. COMPLED WITH EC/TC REO 601R-53-00-115 WET INSTALLED TEMP FASTENER, CR3222 5-4 IAW REO 601R-53-00-115, REV E. RESTORED SURFACE FINISH IAW SRM 51-25-01. CREATED MCO A190649 IAW SOP 5719. THIS IS CONSIDERED A MAJOR REPAIR IAW GMM 5-3.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 33,782 hrs · 30,328 cycles

F/A FLASHLIGHT INOPERATIVE. R & R FLASHLIGHT IAW AMM 25-61-04. OPS CHECKED GOOD.

Part: SKIN — DAMAGED (BS 654-672) · airframe 33,738 hrs · 30,286 cycles

DENT AND HOLE IN FUSELAGE SKIN BETWEEN BS 654-672 AND STRINGERS 26 - 27R. FOUND DAMAGE TO BE IN A NON-REPAIRABLE LOCATION IAW SRM 53-00-31. SUBMITTED DAMAGE REPORT TO STS IAW SRM TR 51-27. RECEIVED EA 12-2014-219, P1, 09/11/2014. CUT AWAY DAMAGED SECTION, PUNCTURE TO .5625" CIRCLE REPORTED CUT-OUT DIMENSION TO STS FOR FINAL REPAIR, DRESSED BACK DENTS , AND ENSURED NO UNDERLYING STRUCTURE DAMAGE. TOUCHED UP CUT LINES. ALL WORK ACCOMPLISHED IN IAW EA 12-2014-219, P1. THIS IS CONSIDERED A MAJOR REPAIR IAW GMM 5-3. RECEIVED EA 12-2014-219, 09/12/2014. FABRICATED REPAIR DOUBLER, 2024-T3 .050" BATCH 1852686, LAYED OUT NEW FASTENER PATTERN , DRILLED AND FINAL SIZED ALL NEW HOLES IN SKIN , AND DOUBLER. DEBURRED AND REMOVED ALL SHARP EDGES, ALODINED, AND PRIMED DOUBLER. ALL WORK ACCOMPLISHED IAW EA 12-2014-219. OK TO PROCEED WITH INSTALLATION OF REPAIR DOUBLER. APPLIED SEALANT TO BOTH FAYING SURFACES, DOUBLER + SKIN, WET INSTALLED ALL FASTENERS, NAS1097AD5 RIVETS, REMOVED ALL EXCESS SEALANT, RESTORED SURFACE FINISH AND CORROSION PROTECTION, ALL WORK ACCOMPLISHED IAW EA 12-2014-219. THIS JOB IS CONSIDERED A PERMANENT REPAIR.

Part: CABLE — LOOSE (PAX DOOR) · airframe 32,295 hrs · 28,873 cycles

MAIN PAX DOOR IS JAMMED, WILL ONLY OPEN ABOUT 1 FOOT. FOUND CABLE OFF OF PULLEY INSTALLED PAX DOOR ASSIST CABLE IAW AMM 52-11-08, OPS CHECK GOOD.

Part: BULB — BURNED OUT (EMERGENCY LIGHTS) · airframe 31,509 hrs · 28,093 cycles

EMERGENCY LIGHT AT SERVICE DOOR INOPERATIVE. R & R BULB IAW AMM 33-51-21, OPS CHECKED GOOD.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 31,387 hrs · 27,959 cycles

WIRE BROKEN AT CONNECTOR FOR EMERGENCY LIGHT ON SERVICE DOOR SURROUND PANEL 232BZ. REPAIRED WIRE IAW ECSPM 20-17-00. OPS CHECKED GOOD IAW AMM 31-51-00-710-801.

Part: STRUCTURE — MISREPAIRED (FUSELAGE) · airframe 31,387 hrs · 27,959 cycles

WHILE WORKING SB 601R-25-187, FOUND REPAIR AT LBL 27 TO HAVE BEEN DONE INCORRECTLY. REPAIRED IAW SRM 51-42-21 AND REO 601R-53-61-4939.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 31,387 hrs · 27,959 cycles

VERTICAL ANGLE AT LBL 27.50 ON FWD SIDE OF THE ENG BEAM IS CRACKED AT THE BOTTOM OF THE ANGLE APPROX 1"L. REMOVED CRACKED ANGLE AT LBL 27.50 IAW SRM 51-42-06 AND SRM 51-42-21. LOCATED AND DRILLED SERVICEABLE ANGLE AT LBL 27.50 IAW SRM 51-40-11. INSTALLED NEW SERVICEABLE ANGLE IAW SRM 51-42-06, 51-42-21.

Part: SKIN — CRACKED (RT WING) · airframe 31,386 hrs · 27,958 cycles

RT FUEL ACCESS HOLE 650BB FAILS NDT WITH AN INDICATION ON FWD SIDE OF HOLE GREATER THAN 50 PERCENT SCREEN HEIGHT. REPAIRED IAW REO 601R-57-21-030, REV J.

Part: SKIN — CRACKED (LT WING) · airframe 31,387 hrs · 27,959 cycles

LT FUEL ACCESS HOLE 540EB FAILS NDT WITH AN INDICATION ON INBD SIDE OF HOLE GREATER THAN 50 PERCENT SCREEN HEIGHT. REPAIRED IAW REO 601R-57-21-030, REV J.

Part: SKIN — CRACKED (RT WING) · airframe 31,386 hrs · 27,958 cycles

RT FUEL ACCESS HOLE 650CB FAILS NDT WITH INDICATIONS GREATER THAN 50 PERCENT SCREEN HEIGHT ON FWD SIDE OF HOLE. REPAIRED IAW REO 601R-57-21-030, REV J.

Part: SKIN — CRACKED (RT WING) · airframe 31,386 hrs · 27,958 cycles

RT FUEL ACCESS HOLE 650AB FAILS NDT WITH AN INDICATION ON FWD INBD SIDE OF HOLE GREATER THAN 50 PERCENT SCREEN HEIGHT. REPAIRED IAW REO 601R-57-21-030, REV J.

Part: SKIN — CRACKED (RT WING) · airframe 31,386 hrs · 27,958 cycles

RT FUEL ACCESS HOLE 640DB FAILS NDT WITH AN INDICATION ON INBD SIDE OF HOLE GREATER THAN 50 PERCENT SCREEN HEIGHT. REPAIRED IAW REO 601R-57-21-030, REV J.

Part: SKIN — CRACKED (RT WING) · airframe 31,386 hrs · 27,958 cycles

RT FUEL ACCESS HOLE 650DB FAILS NDT WITH INDICATIONS ON FWD SIDE OF HOLE GREATER THAN 50 PERCENT SCREEN HEIGHT. REPAIRED IAW REO 601R-57-21-030, REV J.

Part: SILL — CORRODED (FUSELAGE) · airframe 31,386 hrs · 27,958 cycles

SERVICE DOOR LOWER SILL IS CORRODED. REPAIRED IAW SRM 51-42-21, 51-40-11, 51-42-21, 51-42-10, 52-142-00.

Part: FRAME — CORRODED (BS 319.7) · airframe 31,386 hrs · 27,958 cycles

FUSELAGE FRAME BS 319.7 CORRODED ON FWD AND AFT SIDES BETWEEN S26L AND 26R. REMOVED CORRODED FRAME SECTOR IAW SRM 51-42-06, 51-42-21. DRILL & LOCATED 319.70 FRAME SECTOR IAW SRM 51-42-06, 51-42-21. INSTALLED NEW SERVICEABLE FRAME IAW SRM 51-42-06 AND 51-42-21.

Part: INTERCOSTAL — CRACKED (BS 621-625) · airframe 31,386 hrs · 27,958 cycles

INTERCOSTAL CRACKED FROM FS 621-625 AT S13L. REMOVED INTERCOSTAL IAW SRM 51-42-06 AND 51-42-21. LOCATED AND DRILLED NEW INTERCOSTAL IAW SRM 521-40-06 AND 51-40-11. INSTALLED INTERCOSTAL IAW SRM 51-42-06 AND SRM 51-42-21.

Part: BRACKET — CRACKED (WINDSHIELD) · airframe 31,365 hrs · 27,933 cycles

CO-PILOTS WINDSHIELD RT SIDE POST LWR AFT SUPPORT BRACKET IS CRACKED. REMOVED, DRILLED, LOCATED AND INSTALLED NEW SUPPORT BRACKET, PN 601R33235-4S IAW SRM 51-40-11 AND 51-42-21.

Part: SKIN — CORRODED (LT WING) · airframe 31,386 hrs · 27,958 cycles

LEFT WING LOWER WING PLANK ACCESS HOLE AT WS 54.897, HOLE NR 1 AT PANEL LOCATION 540BB HAS PITTING CORROSION AT FORWARD AND AFT ENDS IN THE CRITICAL REGIONS. DEEPEST AREA IS APPROXIMATE .003" DEEP. REPAIRED IAW REO 601R-57-21-030.

Part: SEAT TRACK — CORRODED (BS 364-409) · airframe 31,386 hrs · 27,958 cycles

PASSENGER COMPARTMENT SEAT TRACK AT RBL 9 CORRODED FROM FS 364 THRU 409+128. R & R SEAT TRACK IAW SRM 51-41-00/51-40-11.

Part: STRINGER — CRACKED (PAX DOOR) · airframe 31,386 hrs · 27,958 cycles

PAX DOOR STRINGER 3L IS CRACKED AT FS 280. R & R ONE STRINGER IAW 51-42-21-00 AND 51-42-06-00.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 31,365 hrs · 27,933 cycles

FWD FLOORBEAM ANGLE CRACKED AT FS 280, RBL 9.0. REMOVED CRACKED ANGLE IAW SRM 51-42-06 AND 51-42-21. LOCATED, DRILLED AND INSTALLED NEW ANGLE IAW SRM 51-42-06 AND 51-42-21.

Part: FRAME — CORRODED (BS 310) · airframe 31,386 hrs · 27,958 cycles

FUSELAGE FRAME BS 310 CORRODED ON THE FWD AND AFT SIDES BETWEEN S26L AND 26R. REMOVED CORRODED FRAME IAW SRM 51-42-06, 51-42-21. LOCATED, DRILLED AND INSTALLED NEW FRAME SEGMENT.

Part: INTERCOSTAL — CORRODED (BS 349) · airframe 31,386 hrs · 27,958 cycles

PASSENGER COMPARTMENT INTERCOSTAL AT FS 349 RBL 36.45 CORRODED. REPAIRED IAW REO 601R-53-21-2439.

Part: ANGLE — CRACKED (BS 621-626) · airframe 31,386 hrs · 27,958 cycles

OBLIQUE ANGLE CRACKED AT FS 621-626 AT S14L. REMOVED OBLIQUE ANGLE IAW SRM 51-42-21. DRILLED AND INSTALLED NEW ANGLE IAW SRM 51-40-11 & 51-42-21.

Part: MOUNT — CORRODED (GALLEY) · airframe 31,386 hrs · 27,958 cycles

GALLEY FWD INBD AND AFT INBD FLOOR STRUCTURE MOUNT PLATES AT FS 295 AND 315 RBL 5 CORRODED AND FWD OTBD MOUNT PLATE AT FS 285 RBL 36 CORRODED. REPAIRED IAW EO 601R38669 AND 51-42-06 & 51-42-10.

Part: ANGLE — CORRODED (BS 310-364) · airframe 31,386 hrs · 27,958 cycles

PASSENGER COMPARTMENT FLOOR SILL CORRODED AT RBL 45 FROM BS 310 - 364 TO INCLUDE SERVICE DOOR SILL ANGLE. REPAIRED IAW SRM 51-40-11, 51-42-06.

Part: SEAT TRACK — CORRODED (BS 364-409) · airframe 31,386 hrs · 27,958 cycles

PASSENGER COMPARTMENT SEAT TRACK AT LBL 9 CORRODED FROM FS 364 THRU 409+128. REMOVED SEAT TRACK IAW AMM 53-01-11-946-003. INSTALLED SEAT TRACK IAW AMM 53-01-11-400-802, SRM 51-40-11.

Part: FRAME — CORRODED (BS 333) · airframe 31,386 hrs · 27,958 cycles

FUSELAGE FRAME BS 333 CORRODED ON FWD AND AFT SIDES BETWEEN STR 26L AND STR 26R. INSTALLED NEW FRAME SEGMENT IAW SRM 51-42-06 AND 51-42-21.

Part: LIGHT — CRACKED (SERVICE DOOR) · airframe 31,365 hrs · 27,933 cycles

SERVICE DOOR INNER HANDLE BETA LIGHT CRACKED AT LOWER FASTENER HOLE. REMOVED BETA LIGHT FROM SERVICE DOOR INNER HANDLE BY REMOVING 2 MOUNTING SCREWS AND INSTALLED NEW SERVICEABLE LIGHT, PN 601R38774-3 BY INSTALLING 2 SCREWS IAW AMM 23-51-09-400-802.

Part: SILL — CORRODED (PAX DOORWAY) · airframe 31,365 hrs · 27,933 cycles

PASSENGER DOOR LOWER SILL IS CORRODED. REMOVED DOOR SILL IAW SRM 51-42-06 AND 51-42-21. LOCATED, DRILLED NEW SILL IAW SRM 51-40-11 AND INSTALLED IAW SRM 51-42-06 AND 51-42-21.

Part: FLOORBEAM — CRACKED (BS 484) · airframe 31,365 hrs · 27,933 cycles

FS 484.00 INBD AND OTBD FLOORBEAM ANGLE AT LBL 27.0 AND LBL 35.0 ARE CRACKED. REMOVED INBD AND OTBD SUPPORT ANGLEIAW SRM 51-42-21. INSTALLED NEW SERVICEABLE SUPPORT ANGLE IAW REO 601R-53-41-059.

Part: LIGHT — BROKEN (CABIN) · airframe 31,365 hrs · 27,933 cycles

EMERGENCY LIGHT ON THE GALLEY OTBD TRIM PANEL IS BROKEN. R & R LIGHT IAW AMM 33-51-10-400-801. OPS CHECKED GOOD IAW AMM 33-51-00-710-801.

Part: ATTACH ANGLE — CRACKED (BS 621-625) · airframe 31,365 hrs · 27,933 cycles

FS 621-625 INTERCOSTAL ATTACH ANGLE LOWER AT BL 45, STR 15R, WL 87.5 CRACKED. REMOVED CRACKED ATTACH ANGLE IAW SRM 51-42-21. LOCATED AND DRILLED NEW ATTACH ANGLE IAW SRM 51-40-11 AND 51-40-06 AND INSTALLED IAW SRM 51-42-21.

Part: POST — CRACKED (BS 409) · airframe 31,365 hrs · 27,933 cycles

FOUND FS 409+128, RBL 18, OTBD VERTICAL POST HAS AN INDICATION NOTED IN THE AFT FLANGE RADIUS AT WL 69 APPROXIMATELY .250" X 50 PERCENT FSH. FAILED NDT INSPECTION. REPAIRED IAW SRM 51-42-06, SRM 51-42-22, SRM 51-40-11 & 51-42-06.

Part: POST — CRACKED (BS 409) · airframe 31,365 hrs · 27,933 cycles

FOUND FS 409+128 BL 0 LT & RT VERT POSTS HAVE INDICATIONS NOTED IN THE AFT FLANGE. RADIUS, BOTH APPROX .250" X 50 PERCENT FSH. FAILED NDT INSPECTION. REMOVED DAMAGED POST ASSY AT FS 409+128 BL 0 IAW SRM 51-42-06 & SRM CH 51-42-21. LOCATED & DRILLED NEW SERVICEABLE POST HALVES, REINFORCEMENT ANGLES, & SUBASSEMBLED ALL PARTS IAW SRM 51-40-11 & 51-42-06. INSTALLED NEW POST ASSY IAW SRM 51-42-06 & REO 601R-53-41-889.

Part: POST — CRACKED (BS 409) · airframe 31,365 hrs · 27,933 cycles

FOUND FS 409+128 LBL 18 INBD VERT POST HAS AN INDICATION NOTED IN THE AFT FLANGE RADIUS AT WL 69 APPROX .250" X 60 PERCENT FSH. FAILED NDT INSPECTION. REMOVED FS 409+128 LBL 18 POST IAW SRM 51-42-06. SEPARATED CRACKED INBD POST FROM SERVICEABLE OTBD POST. LOCATED & DRILLED NEW SERVICEABLE INBD POST, PN 601R32208-31S & RIVETED POST TOGETHER IAW SRM 51-42-06 & 51-40-11. INSTALLED FS 409+128 LBL 18 POST ASSY IAW SRM 51-42-22 AND REO 601R-53-41-889.

Part: FLOORBEAM — CRACKED (BS 484) · airframe 31,365 hrs · 27,933 cycles

FS 484.00 I/B FLOORBEAM SUPPORT ANGLE AT RBL 27.0 IS CRACKED. REMOVED INBD ANGLE AT FS 484.00, RBL 27.00 IAW 51-42-21-00. LOCATED AND INSTALLED NEW SERVICEABLE SUPPORT ANGLE AT FS 484.00 AND RBL 27.0 IAW SRM 51-40-11 AND SRM 51-42-21.

Part: BULKHEAD — CRACKED (AFT) · airframe 31,221 hrs · 27,775 cycles

UPON PERFORMING AWL 53-61-163 02 ET INSPECTION OF THE AFT PRESSURE BULKHEAD, RECEIVED CRACK INDICATION THAT ARE OUT OF LIMITS AT LBL 27.50 JUST ABOVE THE CARGO DOOR TRACK. REPAIRED IAW REO 601R-53-61-1541, REV D.

Part: BULKHEAD — CRACKED (AFT) · airframe 31,221 hrs · 27,775 cycles

ON PERFORMING AWL 53-61-163 02 ET INSPECTION OF THE AFT PRESSURE BULKHEAD, RECEIVED CRACK INDICATIONS THAT ARE OUT OF LIMITS AT RBL 27.50 ABOVE THE SECOND LINER CLIP FROM FLOOR. REPAIRED IAW REO 601R-53-61-1285 (REV D).

Part: STRUCTURE — CRACKED (LT WING) · airframe 31,221 hrs · 27,775 cycles

FOUND LT WING TO BE CRACKED AT W/S 149, LOWER SURFACE, JUST OTBD OF JACK PAD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 28,385 hrs · 24,763 cycles

SERVICE DOOR EMERGENCY LIGHT INOPERATIVE. R & R BATTERY PACK OPS CHECKED GOOD IAW AMM 33-51-04

Part: LAMP — BURNED (EMERGENCY LIGHT) · airframe 28,256 hrs · 24,619 cycles

LT FUSELAGE EXTERNAL EMERGENCY LIGHT 2ND FROM FRONT INOPERATIVE. RELAMPED LT FUSELAGE EXTERNAL EMERGENCY LIGHT 2ND FROM FRONT AS REQUIRED. OPS CHECKED GOOD IAW AMM 33-51-00.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 27,437 hrs · 23,733 cycles

RT NR 4 EMERGENCY LIGHT INOP. RELAMPED RT NR 4 EXTERNAL EMERGENCY LIGHT IAW AMM 33-51-21. RELAMPED RT NR 4 EXTERNAL EMERGENCY LIGHT IAW AMM 33-51-21.

Part: DOOR — BINDING (MAIN PAX) · airframe 27,336 hrs · 23,617 cycles

PAX DOOR WILL NOT OPEN FROM INSIDE. OPS CHECKED PAX DOOR GOOD IAW AMM 52-11-01. OK FOR SERVICE.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 27,261 hrs · 23,523 cycles

CORROSION THROUGHOUT INSIDE OF PAX DOOR WHERE LEVELING COMPOUND WAS REMOVED. REMOVED UNSERVICEABLE DRAINAGE RAMP ANGLE AND INSTALLED SERVICEABLE DRAINAGE RAMP ANGLE IAW SRM 51042006 AMD SRM 51-42-21. THIS IS A MAJOR REPAIR. RII FOUND TO BE SATISIFACTORY.

Part: STIFFENER — CHAFED (FUSELAGE) · airframe 27,261 hrs · 23,523 cycles

VERTICAL STIFFNER AT BL 0.00 IS CHAFED FROM 10TH STAGE ISUL. VALVE. BLENDED CHAFED AREA ON VERTICAL STIFFNER AT BL0.00 IAW SRM 51-21-00. FOUND TO BE WITHIN LIMITS IAW REO 601R-53-61-1523. THIS IS A MAJOR REPAIR. REO 601R-53-61-1523. LEAK TEST REQUIRED REF TASK 36-11-00-79-801 PERFORMED LEAK CHECK GOOD IAW 36-11-00-790-801 NO DEFECTS NOTED. COMPLIED WITH EC/TC REO 601R-53-61-1523. RII FOUND TO BE SATISFACTORY.

Part: SEAT TRACK — GOUGED (BS 559) · airframe 27,257 hrs · 23,515 cycles

RIGHT SIDE SEAT RAIL GOUGED 6 IN FWD OF STA 559. COMPLIED WITH EC/TC REO 601R-53-00-055 AND REO 601R-53-00-055, REV NC 4/5/200 THIS IS A MAJOR REPAIR. RII FOUND TO BE SATISFACTORY 5001437.

Part: INTERCOSTAL — CRACKED (PAX DOOR) · airframe 27,257 hrs · 23,515 cycles

PAX DOOR UNDER INNER SKIN FWD SIDE UPPER CORNER HAS A CRACKED INTERCOSTAL. ACCESS THROUGH PNL 832GL. REMOVED UNSERVICEABLE INTERCOSTAL UNDER PAX DOOR INNER SKIN FWD SIDE UPPER CORNER AND REPLACED WITH NEW SERVICEABLE INTERCOSTAL IAW SRM 51-42-03 AND 51-42-21 THIS IS A MAJOR REPAIR, RII FOUND TO BE SATISIFACTORY. (CLOSED)

Part: DOOR FRAME — CRACKED (FUSLAGE) · airframe 27,257 hrs · 23,515 cycles

PAX DOOR FRAME CRACKED IN RADIUS APPROX 6" FROM AFT CAM ROLLER. REPAIRED IAW REO 601R-52-11-402.

Part: ANGLE — CRACKED (BS 484) · airframe 27,257 hrs · 23,515 cycles

CRACKED ANGLE FS 484 LBL-28. REPAIRED IAW REO 601R-53-41-059 AND REO 601R-53-41-1412.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 27,257 hrs · 23,515 cycles

CRACK IN FWD DRAG ANGLE ON PAX DOOR BY ASSIST PULLEY. REPAIRED CRACK IN FWD DRAG ANGLE ON PAX DOOR IAW REO 601R-52-11-513.

Part: SILL — CORRODED (BS 499) · airframe 27,261 hrs · 23,523 cycles

CORROSION ON LT FLOOR SILL APPROX FS 499. COMPLIED WITH REPAIR TO LT FLOOR SILL AT APPROX FS 499 IAW REO 601R-53-41-1401. MAJOR REPAIR. COMPLIED WITH ECTC REO601R-53-41-1401 AND ALL STEPS ARE COMPLETED. RII FOUND TO BE SATISFACTORY.

Part: HINGE FITTING — DAMAGED (PAX DOOR) · airframe 27,261 hrs · 23,523 cycles

PAX DOOR HINGE HALF FUSELAGE HAS SEVEN DAMAGED LUGS. BLENDED (7) DAMAGED LUGS ON PAX DOOR HINGE HALF FUSELAGE SIDE IAW REO 601R-53-21-1279. COMPLETED WITH ECTC REO 601R-53-21-1279 AND REO 601R-53-21-1279 AND ALL STEPS COMPLETED THIS IS A MAJOR REPAIR. RII FOUND TO BE SATISFACTORY.

Part: SKIN — DAMAGED (PAX DOOR) · airframe 27,257 hrs · 23,515 cycles

SCRATCHES & GOUGES ON PAX DOOR INNER SKIN WHERE ASSIST MOTOR CABLE PULLEY BRACKET ATTACHES. BLENDED SCRATCHES AND GOUGES ON PAX DOOR INNER SKIN IAW SRM 51-12-00. ORIGINAL MATERIAL .040, MATERIAL REMOVED.002, REMAINING MAT. THICKNESS .037 FOUND TO BE WITHIN LIMITS IAW SRM 52-00-31. THIS IS A MAJOR REPAIR RII FOUND TO BE SATISFACTORY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,293 hrs · 22,406 cycles

NR2 CEILING EMERGENCY LIGHT INOP. R & R NR 2 CEILING LIGHT IAW IAW AMM 33-51-01. OPS CK GOOD. R & R NR2 CEILING LIGHT IAW AMM 33-51-01. OPS CK GOOD. (CLOSED)

Part: PLACARD — PEELING (PAX DOORWAY) · airframe 26,034 hrs · 22,095 cycles

PAX DOOR EXIT PLACARD PEELING. R & R PAX DOOR EXIT PLACARD IAW AMM 11-30-02. OK FOR SVC. R & R PAX DOOR EXIT PLACARD IAW AMM 11-30-02. OK FOR SVC.

Part: DOOR — BINDING (MAIN PAX) · airframe 25,316 hrs · 21,248 cycles

PAX DOOR HARD TO OPEN. OPS CKD ASD SEVERAL CYCLES AND CLOSES AND OPENS NORMALLY IAW AMM 52-10-00. NO DEFECTS NOTED. (CLOSED)

Part: ACTUATOR — FAILED (APU INTAKE DOOR) · airframe 25,059 hrs · 20,959 cycles

APU INHIB WHITE DASHES ON APU START IN AIR. FOLLOWED BY TEMPORARY APU OVERTEMP WARNING. ALSO NOTED STRONG OIL ODOR FROM APU BLEED AIR. ON POST FLIGHT FOUND SMOKE COMING FROM RAM AIR INLET. ( APU AIR INTAKE DOOR LINEAR ACTUATOR - INTAKE DOOR IS DEACTIVATED. R & R APU DOOR ACTUATOR IAW AMM 49-14-16. OP'S CHECK GOOD, DEFER CLEARED, PLACARD REMOVED.

Part: CABLE — MISROUTED (PAX DOOR) · airframe 25,105 hrs · 21,011 cycles

PAX DOOR HARD TO OPEN. FOUND CABLE FOR DOOR ASSIST CAUGHT ON BRACKET. REROUTED CABLE. DOOR OPERATION GOOD IAW AMM 52-11-00. ACFT OK FOR SERVICE.

Part: FIRE WARNING — ILLUMINATED (APU BAY) · airframe 24,698 hrs · 20,547 cycles

APU FIRE BOTTLE BLOWN (EMERGENCY DECLARED) FLT 5469, DEL 84 MINS.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 24,574 hrs · 20,409 cycles

CAPTAINS FLASHLIGHT INOP.

Part: WIRE — LOOSE (RT FIRE LOOP) · airframe 24,532 hrs · 20,364 cycles

RT FIRE FAIL CAUTION MSG LOOP B FAILED TEST. REINSTALLED LOOSE WIRE ON BOTTOM OF ENGINE ON PYLON, OPS CHECK GOOD IAW AMM 26-11-05 DMIL CLEARED PLACARD REMOVED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,457 hrs · 20,287 cycles

AFT MOST CEILING EMERGENCY LIGHT INOP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,417 hrs · 19,236 cycles

FLOODLIGHTS DS4LA, DS5LA, AND DS6LA HAVE SEVERAL (2 EACH) BULBS INOP.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 23,417 hrs · 19,236 cycles

FOUND ANGLE AT FS 621 LBL 36 ABOVE FLOOR LANDING PLATE CORRODED. REMOVED ANGLE AT FS 621, LBL 36 ABOVE FLOOR LANDING PLATE IAW CRJ 200 SRM 51-42-06.

Part: BULKHEAD — CRACKED (BS 559) · airframe 23,417 hrs · 19,236 cycles

FS 559 BULKHEAD IS CRACKED AT LBL 18.00 INBD LOWER EDGE OF VERTICAL POST ADJACENT TO BOLT HOLE .4 INCHES LENGTH AND RUNS VERTICAL. REPAIRED BULKHEAD I/B LOWER EDGE ADJACENT TO BOLT HOLE IAW REO 601R-53-41-926.

Part: SUPPORT BEAM — CRACKED (CARGO DOOR) · airframe 23,417 hrs · 19,236 cycles

CARGO DOOR SUPPORT BEAM LOWER ANGLE IS CRACKED APPROX .3 INCHES IN LENGTH. REMOVED AND REPLACED CARGO DOOR SUPPORT BEAM LOWER ANGLE IAW SRM 51-42-21.

Part: POST — DAMAGED (FUSELAGE) · airframe 23,417 hrs · 19,236 cycles

FS 409.0+128 VERTICAL POST LBL 18 O/B SIDE AT WL 69.0 HAS A INDICATION NOTED APPROX .2 INCH IN LENGTH 60 PERCENT FSH FAILED NDT INSP. THIS SDR WILL REMAIN OPEN PENDING MTC DETERMINATION OF AN APPROPRIATE CORR ACTION.

Part: SUPPORT ANGLE — CRACKED (FLOORBEAM) · airframe 23,417 hrs · 19,236 cycles

FLOORBEAM SUPPORT ANGLE AT O/B SIDE OF RBL 9 AT FS 280 IS CRACKED. REMOVED FLOORBEAM ANGLE IAW SRM 51-42-21. FABRICATED ANGLE & INSTALLED IAW SRM 51-42-21.

Part: POST — DAMAGED (FUSELAGE) · airframe 23,416 hrs · 19,236 cycles

FS 409.0+128 VERTICAL POST LBL 18 O/B SIDE AT WL 69.0 HAS A INDICATION NOTED APPROX .2" IN LENGTH 60% FSH FAILED NDT INSP. REMOVED VERT SUPPORT POST AT FS 409+128, LBL 18.0 IAW CRJ 200 SRM CH 51-42-06. LOCATED AND INSTALLED VERT SUPPORT POST AT FS 409+128 LBL 18.0 IAW CRJ 200 SRM 51-42-22 & 51-42-06.

Part: FLOOR PANEL — CORRODED (BS 409-559) · airframe 23,417 hrs · 19,236 cycles

FOUND CORROSION OF RT SIDE PRESSURE FLOOR SKIN FROM FS 409.0+128 TO FS 559.0 UNDER FLOOR PNL 262DRF. CORROSION LOCATED IN SEVERAL AREAS. COMPLIED WITH REO 601R-53-41-666.

Part: FLOOR PANEL — CORRODED (BS 409-559) · airframe 23,417 hrs · 19,236 cycles

FOUND CORROSION ON PRESSURE FLOOR SKIN FROM FS 409.0+128 TO FS 559.00 ON LT SIDE OF ACFT UNDER FLOOR PNL 261DLF. CORROSION LOCATED IN SEVERAL AREAS.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 23,417 hrs · 19,236 cycles

ANGLE ON O/B SIDE OF LBL 18 AT FS 484.00 IS CRACKED. REMOVED AND REPLACED ANGLE IAW SRM 51-42-21.

Part: POST — DAMAGED (FUSELAGE) · airframe 23,416 hrs · 19,236 cycles

FS 409.0+128 VERTICAL POST RBL 18.0 INBD AND OTBD SIDES AT WL 69.0 HAS INDICATIONS NOTED APPROX .2 INCH IN LENGTH 60 PERCENT FSH BOTH FAILED NDT INSP. REMOVED VERT SUPPORT POST AT FS 409+128, RBL 18.0 IAW SRM 51-42-06. NEW INBD AND OTBD POST HALVES REQUIRE FABRICATION AND INSTALLATION. FABRICATED RBL 18 AND O/B REPLACEMENT POSTS IAW SRM 51-24-21, REF. DWG 601R32208. TREATED, PRIMED AND TOPCOATED IAW SRM 51-21-11, 51-25-06, 51-25-16. INSTALLED POSTS IAW SRM 51-42-06 AND REO 601R-53-41-889. C/W EC/TC REO 601R-53-41-889 AND MET ALL THE REQUIREMENTS OF REO 601R-53-41-889 ASA RII C/W 5300011

Part: FLOORBEAM — CORRODED (BS 621) · airframe 23,417 hrs · 19,236 cycles

LT SIDE FS 621 FLOOR SUPPORT ANGLE HAS CORROSION AROUND SCREW HOLES UNDER PNLS 281LLF AND 281JLF.

Part: FLOORBEAM — CRACKED (BS 484) · airframe 23,417 hrs · 19,236 cycles

RT SIDE FS 484 ANGLE BETWEEN RBL 9 AND RBL 18 IS CRACKED AT INBD AND OTBD SIDE. REPAIRED ANGLE AT FS 484 IAW REO 601R-53-41-059 & ECTC 601R-53-41-059.

Part: POST — DAMAGED (FUSELAGE) · airframe 23,417 hrs · 19,236 cycles

FS 409.0+128 VERTICAL POST RBL 18.0 I/B AND O/B SIDES AT WL 69.0 HAS INDICATIONS NOTED APPROX .2 INCH IN LENGTH 60 PERCENT FSH BOTH FAILED NDT INSP. THIS SDR WILL REMAIN OPEN PENDING MTC DETERMINATION OF AN APPROPRIATE CORR ACTION.

Part: BULKHEAD — CRACKED (BS 559) · airframe 23,417 hrs · 19,236 cycles

FS 559.0 PRESSURE BULKHEAD WEB HAS (3) INDICATIONS NOTED WITH EDDY CURRENT INSPECTION. INDICATION AS LISTED: (1) RBL 18.0 WL 59.10 HAS 75 PERCENT FSH APPROX 0.5 INCH LONG (2) RBL 9.0 WL 54.10 HAS 80 PERCENT FSH APPROX 0.7 INCH LONGERON (3) LBL 18.0 WL 52.10 HAS 50 PERCENT FSH APPROX 0.3 INCH LONG. FAILS NDT INSPECTION AT THIS TIME. REPAIRED IAW REO 601R-53-41-260 STEPS 1-14.

Part: STRUCTURE — DAMAGED (CARGO BAY) · airframe 23,417 hrs · 19,236 cycles

LT SIDE CARGO FLOOR EDGE MEMBER FS 74.00 TO FS 613 HAS CORROSION AT NUT PLATES AND IS CRACKED AT FS 589.00, FS 605 FROM RIVET HOLES TO EDGE. INSTALLED NEW CARGO FLOOR EDGE MEMBER IAW REO 601R-53-61-1574, SRM 51-42-06, AND SRM 51-42-21.

Part: STRUCTURE — CRACKED (PAX DOOR) · airframe 23,417 hrs · 19,236 cycles

PASSENGER DOOR FWD AND AFT ANCHOR FITTINGS ARE CRACKED. INSTALLED FWD AND AFT COUNTERBALANCE ANCHOR FITTINGS IAW AMM 52-11-17-400-804.

Part: FLOORBEAM — CORRODED (BS 559-621) · airframe 23,417 hrs · 19,236 cycles

CARGO FLOORBEAM CAP LBL27 FS 559+112 TO FS 621 HAS CORROSION AT NUTPLATES. BLENDED DAMAGE AT FLOOR BEAM CAP, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00 FIG 101. REMOVED SEAT TRACK. IAW SRM 51-42-06, 51-42-21. CUT AND REMOVED FLOORBEAM CAP IAW SRM 53-00-43 FIG 203. PERFORMED EDDY CURRENT INSP REWORKED EDGES PER NDTM 51-20-06. NO INDICATIONS NOTED. REMOVED AND REPLACED FLOORBEAM CAP IAW REO 601R-53-61-3131.

Part: FLOOR SKIN — DAMAGED (CABIN) · airframe 23,417 hrs · 19,236 cycles

FS 460.00 FLOOR HAS (2) INTERMITTENT LPI INDICATIONS APPROX 1.5 INCH FWD OF THE INTERCOSTALS. SIZES AND LOCATIONS ARE AS LISTED 1 4 INCH INDICATION FROM LBL 1.0 TO LBL 5.0. 2 6.5 INCH INDICATION FROM RBL 1 TO RBL 7.5. FAILS NDT INSP AT THIS TIME. REPAIRED CRACKS AT FS 460 FLOOR SKIN LBL 1.0" TO LBL 5.0" AND RBL 1.0" TO RBL 7.5" IAW REO 601R-53-41-884. COMPLIED WITH EC/TC REO 601R-53-41-884A BY PERFORMING TEMPORARY REPAIRS TO THE PRESSURE FLOOR WEB AT FS 460.00 PER REO 601R-53-41-884 REV. B. ALL REQUIREMENTS OF THE REO WERE MET.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,127 hrs · 16,374 cycles

EMERGENCY LIGHT INOP RIGHT SIDE OF FUSELAGE MIDDLE LAMP ABOVE WING.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,958 hrs · 16,225 cycles

LEFT AFT EXTERIOR EMERGENCY LIGHT INOP.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 19,677 hrs · 16,020 cycles

CAPTAIN'S FLASHLIGHT IS INOP.

Part: PRESSURE PANEL — CORRODED (BS 526) · airframe 19,292 hrs · 15,725 cycles

RT PRESSURE FLOOR HAS CORROSION AT FS 526 FLOOR TO SIDEWALL ATTACH. MARKED BLENDED OUT LIGHT SURFACE CORROSION IAW CRJ 200 SRM 51-21-06. DB 20877. COMPLIED WITH EC/TC REO 601R-53-41-523.

Part: FRAME — CORRODED (BS 364) · airframe 19,292 hrs · 15,725 cycles

FRAME AT FS 364 AT STGR 27 CORRODED. WORK COMPLETED IN ACCORDANCE WITH CRJ 200 SRM 51-42-06, CRJ 200 SRM 51-21-06, CRJ 200 NDTM 51-20-04, CRJ 200 SRM 51-42-06, CRJ 200 SRM 51-00-00 & IAW CRJ 200 SRM 51-21-11.

Part: FRAME — CORRODED (BS 349) · airframe 19,292 hrs · 15,725 cycles

FRAME AT FS349 AT STGR 27 CORRODED. REMOVED FRAME AT BS 349, BLENDED CORROSION FROM UNDERSIDE OF FRAME FOUND TO BE OUT OF LIMITS PER SRM, REMOVED INTERCOSTAL AT RT BS 349 AFT TO DOOR FRAME AND REMOVED LT VERT. FRAME AT ELEC. JUCTION BOX. INSTALLED NEW FRAME PER SRM 51-40-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 19,292 hrs · 15,725 cycles

ASD SILL FLOOR SUPPORT ANGLE CORRORED IN SEVERAL PLACES (MARKED).

Part: BEAM — CORRODED (BS 349) · airframe 19,292 hrs · 15,725 cycles

TRANSVERSE BEAM CORRODED AT FS 349 AND RBL 45.

Part: FRAME — CORRODED (BS 333 S27) · airframe 19,292 hrs · 15,725 cycles

FRAME AT FS 333 AT STGR 27 CORRODED. WORK COMPLETED IN ACCORDANCE WITH CRJ 200 SRM 51-21-06, CRJ 200 NDTM 51-20-04. CRJ 200 SRM CRJ 200 51-00-00 APPLIED CIC IAW CRJ 200 SRM 51-21-11.

Part: PRESSURE PANEL — CORRODED (BS 460) · airframe 19,292 hrs · 15,725 cycles

PRESSURE FLOOR SKIN CORRODED AT FS 460 BETWEEN LBL 27.00 AND LBL 36.00 (MARKED).

Part: DOOR — CORRODED (EMERGENCY EXIT) · airframe 19,292 hrs · 15,725 cycles

LEFT EMERGENCY EXIT HAS CORROSION, BOTTOM INTERNAL AROUND NUT PLATES FOR ALIGNMENT FITTINGS.

Part: SEAT TRACK — CORRODED (BS 409) · airframe 19,292 hrs · 15,725 cycles

LEFT SIDE PASSENGER SEAT SIDE RAILS CORRODED AND GOUGED AS MARKED AFT OF FS 409+128. BLENDED SIDE WALL SEAT RAIL P/N 601R38312-21 AT FS 409+130 TO DIMENSIONS OF 1" X 3" X .017 DEEP AND AT FS 409+147 TO DIMENSIONS OF 1" X 1" X .007 DEEP. BLENDED SIDEWALL SEAT RAIL P/N 601R38312-115 AT FS 460 TO DIMENSIONS OF 1" X 1" X .004 AND AT FS 494 TO DIMENSIONS OF 1" X 1" X .013. BLENDED SIDEWALL SEAT RAIL P/N 601R38312-25 AT FS 547 TO DIMENSIONS OF 1" X 3" X .007 DEEP AND AT FS 559+39 TO DIMENSIONS OF 1" X 2" X .006 DEEP AS PER CRJ 200 SRM 51-12-00. RECEIVED DAMAGE LIMITS FROM BOMBARDIER, LIMITS OF CRJ200 SRM 53-21-49 FIG 101. ALL SIDE SEAT RAIL BLEND OUTS LEFT SIDE AFT OF 409+128 ARE WITHIN LIMITS OF CRJ200 SRM 53-2

Part: SEAT TRACK — CORRODED (BS 409) · airframe 19,292 hrs · 15,725 cycles

LT SIDE PASSENGER SEAT SIDE RAILS CORRODED AND GOUGED AS MARKED FWD OF FS 409+128. BLENDED SIDEWALL SEAT RAIL PN 601R38312-31 AT FS 385 TO DEMINSIONS OF 1"X1"X.007 DEEP. BLENDED SIDEWALL SEAT RAIL PN 601R38312-29 AT STA 409+22 TO DEMINSIONS OF 1"X1"X .007 DEEP, AT FS 409+51 TO DEMINSIONS OF 1"X3"X.006 AND AT 409+64 TO DEMINSIONS OF 1"X6"X.034" AS PER CRJ 200 SRM 51-12-00. ALL SIDE SEAT RAIL BLEND OUTS LT SIDE FWD OF 409+128 ARE WITHIN LIMITS OF CRJ200 SRM 53-21-49 FIG 101 EXCEPT TO BLEND OUT TO SEAT RAIL PN 601R38312-29 AT FS 409+64. REPAIRED LT. SIDE SEAT RAIL AT 409+64 IAW BOMBARDIER REO 601R-53-00-055 .

Part: SEAT TRACK — CORRODED (BS 409) · airframe 19,292 hrs · 15,725 cycles

RIGHT SIDE PASSENGER SEAT SIDE RAILS CORRODED AND GOUGED AS MARKED FWD OF FS 409+128. BLENDED SIDE WALL SEAT TRACK P/N 601R38312-29 AT FS 409+86 TO DIMENSION OF 1" X 1" X .004 DEEP AS PER CRJ200 SRM 51-12-00. RECEIVED DAMAGE LIMITS FROM BOMBARDIER, LIMITS OF CRJ200 SRM 53-21-49 FIG 101. ALL SIDE SEAT RAIL BLEND OUTS RIGHT SIDE FWD OF 409+128 ARE WITHIN LIMITS OF CRJ200 SRM 53-21-49 FIG 101. C/W A044 FINISH ON BLENDED AREAS ON RIGHT SIDE SEAT RAILS IAW CRJ200 SRM 51-21-16. SUPPLEMENTAL - SDR CLOSED 05/25/07.

Part: SHAFT — CORRODED (DOOR HANDLE) · airframe 19,292 hrs · 15,725 cycles

CREW ESCAPE HATCH OUTER HANDLE SHAFT SHOWS SIGNS OF CORROSION.

Part: SEAT TRACK — CORRODED (BS 409) · airframe 19,292 hrs · 15,725 cycles

RIGHT SIDE PASSENGER SEAT SIDE RAILS CORRODED AND GOUGED AS MARKED AFT OF FS 409+128. BLENDED SIDEWALL SEAT RAIL P/N 601R38312-115 AT STA 449.85 TO DIMENSIONS OF 1" X 1" X .007 DEEP AND AT STA 495.98 TO DIMENSIONS OF 1" X 1" X .008 DEEP. BLENDED SIDEWALL SEAT RAIL P/N 601R38312-25 AT STA 559 + 10 TO DIMENSIONS OF 1" X 12" X .008 AND AT STA 559+36 TO DIMENSIONS OF 1" X 1" X .004 DEEP AS PER CRJ 200 SRM 51-12-00. RECEIVED DAMAGE LIMITS FROM BOMBARDIER, LIMITS OF CRJ200 SRM 53-21-49 FIG 101. ALL SIDE SEAT RAIL BLEND OUTS RIGHT SIDE AFT OF 409+128 ARE WITHIN LIMITS OF CRJ200 SRM 53-21-49 FIG 101. C/W A044 FINISH ON BLENDED AREAS ON RIGHT SIDE SEAT RAILS IAW CRJ200 SRM 51-21-16. SUPPLEMENTAL - SDR CLOSED 05/25

Part: ANGLE — CRACKED (RT WING) · airframe 18,300 hrs · 15,032 cycles

RANRC 82. RT WING MID LE, IB ATTACHMENT ANGLE IS CRACKED. REMOVED AND REPLACED RT WING AND LE IB ATTACHMENT ANGLE WITH SERVICEABLE ANGLE PN 600-12045-12 IAW CRJ AMM 20-21-00 MC892SDR.

Part: MOTOR — ODOR (LAVATORY) · airframe 17,996 hrs · 14,815 cycles

LAV MOTOR HAS A ELECTRICAL SMOKE ODOR.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 17,546 hrs · 14,483 cycles

EMERGENCY EXIT LIGHT AT SERVICE DOOR HAS BULB INOP.

Part: ENGINE — BIRD INGESTION (LEFT) · airframe 17,307 hrs · 14,298 cycles

BELIEVE TO HAVE IMPACTED SOMETHING IN FLIGHT SHORTLY AFTER TAKEOFF. IMPACT SOUNDED LIKE IT CAME FROM LEFT SIDE OF A/C. EMERGENCY EQUIPMENT ROLLED AS A PRECAUTION. A/C RETURNED TO ATL AFTER T/O INSPECTED A/C FOUND BIRD REMENENTS UNDER LT. WING , CLEANED AND PERFORMED ENGINE RUN . NO DEFECTS NOTED. (CLOSED)

Part: COVER — OUT OF POSITION (CABIN) · airframe 16,946 hrs · 14,004 cycles

MAIN ENTRY DOOR LOWER EMERGENCY EXIT LIGHT COVER FELL OFF.

Part: COVER — BROKEN (CABIN)

DURING A GROUND INSPECTION, THE FORWARD RT SIDE EMERGENCY EXIT LIGHT COVER WAS FOUND TO BE BROKEN. MAINT REMOVED AND REPLACED THE FORWARD RT SIDE EMERGENCY EXIT LIGHT COVER. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: ENGINE — MALFUNCTIONED (RIGHT)

FLT 4534 - DURING CRUISE FROM ATL-SBN, THE CREW RECEIVED A LOW OIL PRESSURE WARNING ON THE RIGHT ENGINE. THE QRH WAS COMPLIED WITH AND THE RIGHT ENGINE WAS REDUCED TO IDLE FOR THE REMAINDER OF THE FLIGHT. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED TO CVG. THE AIRCRAFT LANDED SAFELY IN CVG. MAINTENANCE REMOVED AND REPLACED THE RIGHT ENGINE. THE MRR WILL REMAIN OPEN PENDING AN ENGINE TEAR DOWN REPORT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: FRAME — CRACKED (FUSELAGE)

DURING A C-CHECK, THE FS 280 FRAME AT RBL 9 LOWER ANGLE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE FS 280 FRAME AT RBL 9 LOWER ANGLE IAW EO. (K)

Part: FLOORBEAM — CORRODED (FUSELAGE)

DURING A C-CHECK, THE FORWARD AND AFT FLOOR SUPPORT ANGLES AT FS 280 BETWEEN LBL 9 AND RBL 9 WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE FORWARD AND AFT FLOOR SUPPORT ANGLES AT FS 280 BETWEEN LBL 9 AND RBL 9 IAW EO. (K)

Part: BULKHEAD — CORRODED (FUSELAGE)

DURING A C-CHECK, THE PILOTS BULKHEAD WEB AT FS 280 BETWEEN LBL 9 AND RBL 9 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE PILOTS BULKHEAD WEB AT FS 280 BETWEEN LBL 9 AND RBL 9 IAW EO. (K)

Part: SEAT TRACK — CORRODED (FUSELAGE)

DURING A C-CHECK, THE SEAT RAIL FLOOR AT FS 379, LBL 9 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE SEAT RAIL FLOOR AT FS 379, LBL 9. (K)

Part: PRESSURE PANEL — CORRODED (FUSELAGE)

DURING A C-CHECK, THE PRESSURE FLOOR AT LBL 36, RBL 36 FROM FS 409+128 TO FS 559 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE PRESSURE FLOOR AT LBL 36, RBL 36 FROM FS 409+128 TO FS 559 IAW EO. (K)

Part: SILL — CRACKED (FUSELAGE)

DURING C-CHECK, THE CARGO COMPARTMENT FLOOR SILL PLATE WAS FOUND TO BE CRACKED AND CORRODED AROUND THE SCREW HOLES BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE CARGO COMPARTMENT FLOOR SILL PLATE. (K)

Part: CLIP — CRACKED (BULKHEAD)

DURING A C-CHECK, THE CLIP AT FS 625 LT AFT PRESSURE BULKHEAD WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CLIP AT FS 625 LT AFT PRESSURE BULKHEAD IAW SRM. (K)

Part: CLIP — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE AVIONICS BAY FS 280 CLIP AT LBL 9 AFT OUTBOARD SIDE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE AVONICS BAY FS 280 CLIP AT LBL 9 AFT OUTBOARD SIDE IAW CRJ 200 SRM 51-42-21. (M)

Part: FRAME — CRACKED (FUSELAGE)

DURING HANGAR MAINTENANCE, THE LT FRAME STA 640 WAS FOUND TO BE CRACKED AFT OF LBL 10 BEYOND LIMITS. THE AIRCRAFT WAS INSPECTED AND FOUND TO BE SAFE FOR A FERRY FLIGHT FOR PERFORMANCE OF THE APPROPRIATE CORRECTIVE ACTION. THE AIRCRAFT LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE LT 640 FRAME AND DOUBLER IAW SRM. (K)

Part: STEP — BROKEN (PAX DOOR)

FLT 4748 - DURING A GROUND INSPECTION IN DFW, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND BROKEN. THE PASSENGER DOOR ALSO CLOSED BY ITSELF UPON POWER UP. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR, AND ALSO REPOSITIONED THE SWITCH GUARD. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: OIL SYSTEM — LOW (RT ENGINE)

DURING CLIMB-OUT FROM DFW-MEM, PASSING THROUGH 21,000 FT THE CREW RECEIVED AN ENGINE OIL PRESSURE WARNING MESSAGE FOR APPROXIMATELY TWO SECONDS ON THE RT ENGINE AND THEN IT EXTINGUISHED. THE OIL PRESSURE WAS MONITORED WHICH FLUCTUATED RAPIDLY BETWEEN 25 TO 45 PSI. THE CREW COMPLIED WITH THE QRH, PULLING THE POWER TO IDLE AND THE OIL PRESSURE STABILIZED AT 42 PSI. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO DFW, LANDING SAFELY. MAINTENANCE SERVICED THE RT ENGINE OIL TO THE PROPER LEVEL. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LIGHT — CRACKED (GALLEY)

DURNIG A C-CHECK IN MCN, THE EMERGENCY EXIT LIGHT IN THE GALLEY BY THE SERVICE DOOR AND THE EMERGENCY EXIT FLOOR FLOODLIGHT AT THE PASSENGER DOOR WERE FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT ASSEMBLY IN THE GALLEY BY THE SERVICE DOOR AND THE EMERGENCY EXIT FLOOR FLOODLIGHT ASSEMBLY AT THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: RIB — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE LEFT AND RIGHT WHEEL WELL BATT RIB ASSEMBLIES AT WS 53.60 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LEFT AND RIGHT WHEEL WELL BATT RIB ASSEMBLIES AT WS 53.60 IAW ASA EO 600-57-0042. (M)

Part: INTERCOSTAL — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE INTERCOSTALS AT FS 484, BL 27.00-36.00 ON THE LEFT AND RIGHT SIDES WRE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE INTERCOSTALS AT FS 484, BL 27-36 ON THE LEFT AND RIGHT SIDES IAW ASA EO 600-53-0111. (M)

Part: FRAME — CRACKED (FUSELAGE)

DURING A C-CHECK, THE FS 640 FORWARD ON THE RT SIDE BETWEEN STRINGERS 13R AND 14R WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE FS 640 FORWARD ON THE RT SIDE BETWEEN STRINGERS 13R AND 14R IAW ASA EO 600-53-0088. (M)

Part: ANGLE — CRACKED (FUSELAGE)

DURING A C-CHECK, THE CARGO AFT WALL FLOOR SUPPORT ANGLES AT FS 621 ON THE LT AND RT SIDES WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CARGO AFT WALL FLOOR SUPPORT ANGLES AT FS 621 ON THE LT AND RT SIDES IAW ASA EO 600-53-0105. (M)

Part: FITTING — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE FORWARD CABLE ANCHOR MOUNT FITTING ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE IS REMOVING AND REPLACING THE FORWARD CABLE ANCHOR MOUNT FITTING ON THE PASSENGER DOOR. (M)

Part: SUPPORT BEAM — CRACKED (ENGINE)

DURING A C-CHECK, THE CENTER ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL 0 WAS FOUND CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CENTER ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL 0 IAW ASA EO 600-53-0072. (M)

Part: STEP — CRACKED (FUSELAGE)

DURING HANGAR MAINTENANCE IN MCN, THE PASSENGER DOOR BOTTOM STEP WAS FOUND CRACKED AT THE ATTACH ROD. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR BOTTOM STEP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: CARBON SEAL — LEAKING (ENGINE)

DURING CLIMB-OUT FROM DFW-SAT, AT APPROX 19,000 FT THE CREW RECEIVED A RIGHT ENGINE OIL PRESSURE WARNING. QRH PROCEDURES WERE COMPLIED WITH AND THE CREW REDUCED THE RIGHT ENGINE TO IDLE. THE OIL PRESSURE CONTINUED TO FLUCTUATE BETWEEN 40 TO 45 PSI AND SHORTLY AFTERWARDS FLUCTUATED INTO THE RED RANTE. THE CREW FOLLOWED QRH PROCEDURES AND SHUT DOWN THE RT ENGINE. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED SAFELY IN SAT. MAINTENANCE REMOVED AND REPLACED THE INTEGRATED DRIVE GENERATOR CARBON SEAL ASSY ON THE RIGHT ENGINE, THEN PERFORMED AN OIL CONSUMPTION CHECK. NO DEFECTS WERE NOTED. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: SNAP RING — MISSING (RT ENGINE)

FLT 9331 - DURNG APPROACH INTO ATL FROM MCN, THE CREW RECEIVED A RIGHT ENGINE OIL PRESSURE WARNING MESSAGE. THE OIL PRESSURE WAS AT 25 PSI AND CONTINUED TO DECREASE. THE CREW COMPLIED WITH QRH PROCEDURES AND SHUTDOWN THE RIGHT ENGINE. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED SAFELY IN ATL. MAINTENANCE INSTALLED A MISSING RIGHT ENGINE CRANK PAD SNAP RING, AND REMOVED AND REPLACED THE RIGHT ENGINE OIL TRANSDUCER (P/N 601509199). OPS AND LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LAMP — BURNED OUT (EMERGENCY LIGHT)

DURING HANGAR MAINTENANCE IN BTR, THE EXTERIOR RIGHT AFT EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EXTERIOR RIGHT AFT EMEGENCY LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: BULB — BURNED OUT (CABIN)

DURING A GROUND INSPECTION AT MGM, THE NR 3 OVERHEAD EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 3 OVERHEAD EMERGENCY LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: WINDSHIELD — CRACKED (COCKPIT)

FLT 4459 - DURING FLIGHT FROM CAE TO DFW, F/O''S FORWARD WINDSHIELD CRACKED AT 35,000 FEET. AN EMERGENCY WAS DECLARED. AIRCRAFT DIVERTED TO JAN AND LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED FORWARD RIGHT WINDSHIELD. LEAK AND OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: LIGHT — INOPERATIVE (CABIN)

CREW REPORTED RIGHT EMERGENCY EXIT LIGHT ON IN FLIGHT. MAINTENANCE RESET EMERGENCY EXIT LIGHT. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RELEASED FOR FURTHER SERVICE. (M)