N846AS

Part: DOOR — UNKNOWN (SERVICE) · airframe 36,255 hrs · 32,912 cycles

SERVICE DOOR UNABLE TO BE OPENED FROM THE OUTSIDE. PERFORMED OPS TEST OF THE SERVICE DOOR IAW AMM 52-41-00. OPS CHECK GOOD ACFT OK FOR SERVICE.

Part: LIGHT — DAMAGED (CABIN) · airframe 36,223 hrs · 32,877 cycles

EMERGENCY FLOODLIGHT AT SERVICE DOOR DAMAGED. R & R FLOODLIGHT IAW AMM 33-51-19. SYSTEM OPS CHECKED GOOD. NO FURTHER ACTION.

Part: FAIRING — SCRATCHED (HORIZONTAL STAB) · airframe 33,829 hrs · 30,495 cycles

LT LOWER HORIZONTAL STABILIZER TO B-STABILIZER FAIRING SCRATCHED IN 3 LOCATIONS. REPAIRED IAW ECTC REO 601R-55-32-315 PERM REPAIR.

Part: SEAT TRACK — CORRODED (BS 399-409) · airframe 33,829 hrs · 30,495 cycles

SEAT TRACK SEGEMENT 399.5 - 409+126 LBL 9, CORRODED IN SEVERAL AREAS. R & R THE SEAT TRACK IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (BS 364-399) · airframe 33,829 hrs · 30,495 cycles

RBL 9 SEAT TRACK SEGEMENT BS 364 - 399.5 CORRODED IN SEVERAL AREAS. REMOVED AND REPLACED SEAT TRACK SEGMENT IAW AMM TASK 53-01-11-000-802 AND AMM TASK 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 399-409) · airframe 33,829 hrs · 30,495 cycles

RBL 9 SEAT TRACK SEGEMENT BS 399.5- 409+126 CORRODED IN SEVERAL AREAS. REMOVED AND REPLACED SEAT TRACK SEGMENT IAW AMM TASK 53-01-11-000-802 AND AMM 53-01-11-400-802.

Part: FLOOR SUPPORT — CORRODED (BS 349-364) · airframe 33,829 hrs · 30,495 cycles

FOUND CORROSION ON FLOOR SUPPORT AT BS 349 - 364 JUST AFT OF PAX DOOR REMOVED CORROSION IAW SRM 51-21-06-00. BLENDED AREA IS OUT OF LIMITS IAW REO 601R-53-00-530. REPAIRED IAW EC/TC REO 601R-53-21-2558.

Part: SKIN — DENTED (FUSELAGE) · airframe 33,829 hrs · 30,495 cycles

DENT ON LT SIDE FUSELAGE UNDER CABIN PRESSURE GROUND AIR SUPPLY DOOR. RECEIVED AND COMPLIED WITH EC/TC REO 601R-53-61-5309, PERMANENT REPAIR. RECEIVED AND COMPLIED WITH REO 601R-53-61-5309. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702.

Part: SEAT TRACK — CORRODED (BS 424-559) · airframe 33,829 hrs · 30,495 cycles

LEFT SIDE FLOOR SEAT TRACK HAS CORROSION AT BS 424 - 559. R & R SEAT TRACK IAW AMM 53-01-11-000-802 AND 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 364-399) · airframe 33,829 hrs · 30,495 cycles

LT SEAT TRACK HAS CORROSION AT BS 364 - 399.5. R & R SEAT TRACK IAW AMM 53-01-11-000-802 AND 53-01-11-400-802.

Part: FLOOR SUPPORT — CORRODED (BS 310-320) · airframe 33,829 hrs · 30,495 cycles

LT CABIN FLOOR SUPPORT CORRODED FROM BS 310 - 320. R & R IAW SRM 51-42-13-00 AND DWG 601R38670.

Part: LIGHT — FAILED (CABIN) · airframe 33,829 hrs · 30,495 cycles

LEFT & RIGHT OVERWING EMERGENCY EXIT BETA LIGHT ON HANDLE FAILED FUNCTION TEST. R & R LT & RT OVERWING EMERGENCY EXIT BETA LIGHTS ON HANDLE IAW AMM 33-51-09-000-801.

Part: SKIN — DENTED (FUSELAGE) · airframe 33,829 hrs · 30,495 cycles

DENT ON LT SIDE FUSELAGE UNDER CABIN PRESSURE GROUND AIR SUPPLY DOOR. REPAIRED IAW REO 601R-53-61-5309. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR .

Part: DOOR — BINDING (SERVICE) · airframe 33,457 hrs · 30,128 cycles

SERVICE DOOR WILL NOT STAY OPEN AND IS DIFFICULT TO CLOSE. RECYCLED SERVICE DOOR MECHANISM CLEARED JAMMED DOOR IAW AMM 52-41-03.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 32,768 hrs · 29,445 cycles

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

Part: LIGHT — BROKEN (EXTERIOR) · airframe 32,430 hrs · 29,104 cycles

EMERGENCY LIGHT ON FWD SIDE OF PAX DOOR OPENING, BROKEN. R & R EMERGENCY FLOODLIGHT ON WARDROBE IAW VCMM 25-20-52.

Part: FAIRING — GOUGED (VERTICAL STAB) · airframe 32,114 hrs · 28,761 cycles

FOUND VERTICAL STAB LT LOWER MIDDLE FAIRING HAS A GOUGE. CLASSIFIED AS MAJOR REPAIR IAW GMM 5-3. REPAIRED IAW REO 601R-55-32-315.

Part: DOOR — UNKNOWN (MAIN PAX) · airframe 32,090 hrs · 28,738 cycles

PAX DOOR WOULD NOT OPEN. OPENED DOOR AS REQUIRED.

Part: DOOR — UNKNOWN (MAIN PAX) · airframe 31,899 hrs · 28,538 cycles

MAIN ENTRANCE DOOR WILL NOT CLOSE OR OPEN. TROUBLESHOT MAIN PAX DOOR - CYCLED DOOR - DOOR OPS CHECKED OK IAW AMM 52-11-00.

Part: HANDLE — FOULED (PAX DOOR) · airframe 31,525 hrs · 28,178 cycles

RAMP REPORTS PAX DOOR WILL NOT OPEN FROM THE OUTSIDE. FOUND INNER HANDLE RETENTION MECHANISM JAMMED AND LOCKED WITH DIRT AND DEBRIS. CLEANED AND LUBRICATED RETENTION MECHANISM. PERFORMED OPS CHECKED PAX DOOR IAW AMM 52-11-23.

Part: ACTUATOR — UNSERVICEABLE (SERVICE DOOR) · airframe 31,341 hrs · 27,980 cycles

SERVICE DOOR WILL NOT OPEN. R & R SERVICE DOOR HANDLE ACTUATOR IAW AMM 52-41-03. OPS TEST GOOD.

Part: HANDLE — BINDING (PAX DOOR) · airframe 31,258 hrs · 27,893 cycles

PAX DOOR IS HARD TO OPEN. OPS CHECKED GOOD OF PAX DOOR OUTER HANDLE IAW AMM 52-11-03, NO DEFECTS NOTED.

Part: DOOR — BINDING (PAX) · airframe 31,103 hrs · 27,736 cycles

PASSENGER DOOR WILL NOT OPEN FROM OUTSIDE. DAMAGE TO AIRFRAME BOTH SIDES OF DOOR AT HANDLE LEVEL. PERFORM OPS CK OF PAX DOOR OUTER HANDLE IAW AMM 52-11-03, BLENDED DAMAGE IAW REO 601R-53-21-024, AND 601R-53-21-160 FOUND TO BE WITHIN LIMITS, ALLODINED PRIMED AND PAINTED AREA.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 30,969 hrs · 27,607 cycles

NR 3 EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP IAW AMM 33-51-15, OPS CHECKED GOOD.

Part: LAMP — BURNED OUT (FLASHLIGHT) · airframe 30,281 hrs · 26,903 cycles

F/A REPORTS CABIN FLASHLIGHT INOPERATIVE. RELAMPED F/A FLASHLIGHT IAW AMM 26-61-04. SDR CLOSED.

Part: TEE FITTING — CORRODED (BS 319-349) · airframe 30,256 hrs · 26,877 cycles

FWD AND AFT TEE FITTINGS AT SERVICE DOOR ENTRANCE ARE CORRODED BEYOND LIMITS, LOCATED AT FS 319 AND FS 349 WL 73.5 IAW TASK 000-53-900-509. REMOVED CORRODED T FITTING AT FS 349, WL 73.5 IAW SRM 51-42-21. LOCATED AND DRILLED NEW T-FITTING AT FS 349, WL 73.5 IAW SRM 51-40-11. INSTALLED NEW SERVICEABLE T-FITTING, PN 601R38334-3 IAW SRM 51-42-21. PAINTED AREA AT FWD AND AFT T-FITTING AT SERVICE DOOR IAW SRM 51-25-01.

Part: ANGLE — CORRODED (FUSEDLAGE) · airframe 30,257 hrs · 26,879 cycles

PAX DOOR SILL ANGLE IS CORRODED. REMOVED PAX DOOR SILL ANGLE IAW SRM 51-42-06, 51-42-13 AND 51-42-21. RECEIVED NEW SERVICEABLE PAX DOOR SILL ANGLE PN 601R31527-221. LOCATED AND DRILLED FASTENER HOLES IN SILL ANGLE IAW SRM 51-40-11. INSTALLED NEW SERVICEABLE PAX DOOR SILL ANGLE PN 601R31527-221 IAW SRM 51-42-06, 51-42-13 AND 51-42-21.

Part: CARGO TRACK — CORRODED (BS 559) · airframe 30,257 hrs · 26,879 cycles

CARGO TRACK AT RBL 9 FS 559.00+112 HAS CORROSION AROUND FASTENER HOLES. REMOVED CORRODED CARGO TRACK, INSTALLED NEW CARGO TRACK. WORK PERFORMED IAW AMM 53-01-11-000-802/53-01-11-400-802.

Part: BULKHEAD WEB — CRACKED · airframe 30,257 hrs · 26,879 cycles

FOUND REAR PRESSURE BULKHEAD WEB HAS INDICATION NOTED AT LBL 27.50, WL 130 APPROX .3" IN LENGTH 100 PERCENT FSH. LOCATION TOP OF CARGO DOOR AFT TRACK. FAILED NDT INSPECTION. COMPLIED WITH REO 601R-53-61-1541, REV D,

Part: SILL — CORRODED (FUSELAGE) · airframe 30,257 hrs · 26,879 cycles

CARGO DOOR LOWER SILL HAS 1 EA FASTENER HOLE WITH MINOR CORROSION AROUND RIVET THAT ATTACHES TO NUTPLATE AT FS 589.00+6 AT LBL 45. FOUND CARGO DOOR LOWER SILL CORRODED BEYOND LIMITS IAW SRM 53-00-00. REMOVED DAMAGED SILL IAW SRM 51-42-06, 51-42-10 AND 51-42-21. CUT PART FOR CABLE REINSTALLATION, LOCATED FASTENER HOLES IN SILL. ALL WORK WAS IAW REO 601R-53-61-1574.

Part: FLOOR SUPPORT — CORRODED (BS 295-319) · airframe 30,256 hrs · 26,877 cycles

FWD FLOOR SUPPORT AND GALLEY SUPPORT PLATE LOCATED AT RBL 35 FROM FS 295 TO FS 319 IS CORRODED BEYOND LIMITS IAW TASK 000-53-900-509. REMOVED CORRODED FLOOR SUPPORT & GALLEY SUPPORT PLATE FROM FS 310 TO FS 319, RBL 36 AND REPLACED WITH SERVICEABLE FLOOR SUPPORT & GALLEY SUPPORT PLATE IAW SRM 51-42-06 AND 51-42-21.

Part: FLOOR SUPPORT — CORRODED (BS 559-621) · airframe 30,257 hrs · 26,879 cycles

CARGO BAY FLOOR SUPPORT AT LBL 27 HAS MULTIPLE FASTENER HOLES WITH PITTING CORROSION FROM FS 559.00+112 THROUGH 621.00. FOUND FLOOR SUPPORT BEYOND LIMITS IAW SRM 53-00-00. REMOVED DAMAGED CAP FROM LBL 27 FS 559+112 -621.00 IAW SRM 51-42-06 AND 51-42-21. DRILLED, LOCATED AND INSTALLED NEW FLOOR SUPORT IAW SRM 51-40-11, 51-42-21, 51-42-22 AND REO 601R-53-61-3778. COMPLIED WITH EC/TC REO 601R-53-61-3778 AND REO 601R-53-61-3778, REV A.

Part: ATTACH FITTING — CORRODED (FUSELAGE) · airframe 30,256 hrs · 26,877 cycles

SERVICE DOOR LWR SILL ATTACHMENT CLIP LOCATED AT FS 349 IS CORRODED BEYOND LIMITS IAW TASK 000-53-900-509. REMOVED SERVICE DOOR LOWER SILL ATTACHMENT CLIP IAW SRM 51-42-06 & SRM 51-42-21. LOCATED & DRILLED SERVICE DOOR LOWER SILL ATTACHMENT CLIP IAW SRM 51-40-11. INSTALLED NEW SERVICE DOOR LOWER SILL ATTACHMENT CLIP IAW SRM 51-42-21.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 30,257 hrs · 26,879 cycles

SEAT TRACK AT FS 559.00+85, RBL 9 HAS CORROSION AROUND FASTENER HOLES. REMOVED CORRODED FLOOR TRACK AT FS 559.00+85, RBL 9 IAW AMM TASK 53-01-11-000-802. FABRICATED NEW FLOOR TRACK IAW REO 601R-53-00-478. INSTALLED NEW SEAT TRACK IAW AMM 53-01-11-400-802.

Part: FLOOR SUPPORT — CORRODED (BS 349) · airframe 30,257 hrs · 26,879 cycles

FLOOR SUPPORT CORRODED AT FS 349.00 AFT OF SERVICE DOOR BEYOND LIMITS. REMOVED DAMAGED SECTION OF SERVICE DOOR FLOOR SUPPORT FROM FS 349.00 TO FS 368.5 IAW REO 601R-53-21-326. COMPLIED WITH REO 601R-53-21-326 & 601R-53-21-2341.

Part: FLOORBEAM — CORRODED (BS 349) · airframe 30,256 hrs · 26,877 cycles

FLOORBEAM AT FS 349.0 WL 73.5 CORRODED BEYOND LIMITS FROM RBL 27 TO RBL 36 IAW TASK 000-53-900-509. REPAIRED IAW REO 601R-53-21-2342.

Part: FLOOR SUPPORT — CORRODED (BS 559) · airframe 30,257 hrs · 26,879 cycles

FS 559.00+80 -559.00+96 HAS 4 EA FASTENER HOLES WITH CORROSION AT LBL 45 ON FLOOR SUPPORT. BLEND THE CORROSION IAW SRM 51-21-06. REMOVED .006" MATERIAL THICKNESS, LT .057". COMPLIED WITH REO 601R-53-51-196. FOUND TO BE SATISFACTORY.

Part: FLOOR SUPPORT — CORRODED (BS 319-349) · airframe 30,257 hrs · 26,879 cycles

FLOOR SUPPORT ANGLE AT SERVICE DOOR ENTRANCE CORRODED BEYOND LIMITS BETWEEN FS 319 AND FS 349.0 AT WL 73.5 IAW TASK 000-53-900-509. REMOVED FLOOR SUPPORT ANGLE ASSY AT SERVICE DOOR ENTRANCE BETWEEN FS 319 AND FS 349 IAW SRM 51-42-21, 51-42-06 AND 51-42-13. INSTALLED NEW FLOOR SUPPORT ANGLE ASSY AT SERVICE DOOR ENTRANCE IAW SRM 51-42-06, 51-42-13 AND 51-42-21.

Part: ISOLATOR — CRACKED (BS 621 BULKHEAD) · airframe 30,256 hrs · 26,877 cycles

FS 621.00 REAR PRESSURE BULKHEAD HAS AN ISOLATOR BROKEN. REMOVED ISOLATOR, LOCATED HOLES IN NEW BRACKET AND INSTALLED USING MS20470AD5-5. ALL WORK PERFORMED IAW SRM 51-42-06.

Part: ANGLE — CRACKED (BS 484) · airframe 30,256 hrs · 26,877 cycles

LT FS 484.00 INTERCOSTAL ANGLE AT LBL 27 IS CRACKED .5 INCHES LONG IN UPPER RADIUS. REMOVED CRACKED ANGLE AT LBL 27 & REPLACED W/NEW SERVICEABLE ANGLE PN 601R31171-17 IAW SRM 51-42-21. PAINTED FASTENERS ON REPAIRED AREA IAW SRM 51-25-01, APPLIED WATER DISPLACING CORROSION INHIBITING COMPOUND IAW SRM 51-21-11.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 30,256 hrs · 26,877 cycles

IN PASSENGER COMPARTMENT BELOW FLOOR AT FS 280.00 ON RBL 9.00 AND LBL 9.00, INBD ATTACHMENT ANGLES ARE CRACKED. REMOVED THE CRACKED ATTACHMENT ANGLE AT FS 280.00 ON RBL 9.00 IAW SRM 51-42-21. INSTALLED NEW SERVICEABLE ATTACHMENT ANGLE (PN 601R31113-58) AT FS 280.00 ON RBL 9.00 IAW SRM 51-42-21.

Part: ANGLE — CRACKED (BS 484) · airframe 30,256 hrs · 26,877 cycles

LEFT FS 484.00 INTERCOSTAL ANGLE AT LBL 9 IS CRACKED .5" LONG IN UPPER RADIUS. INSTALLED A NEW ANGLE 601R31171-27 PO W17821 IAW AMM 51-42-21.

Part: ANGLE — CRACKED (BS 484) · airframe 30,256 hrs · 26,877 cycles

RIGHT FS 484.00 INTERCOSTAL ANGLE AT RBL 27 IS CRACKED .5" LONG IN UPPER RADIUS. REMOVED CRACKED ANGLE AT RBL 27 & REPLACED W/NEW SERVICEABLE ANGLE PN 601R31171-9 IAW SRM 51-42-21. TOUCHED UP REPAIR FASTENERS IAW SRM 51-25-01. APPLIED WATER DISPLACING CORROSION INHIBITING COMPOUND IAW SRM 51-21-11. SDR CLOSED.

Part: ATTACH ANGLE — CRACKED (RT WING) · airframe 30,256 hrs · 26,877 cycles

RIGHT UPPER WING UNDER FUSELAGE TO WING ACCESS PANEL 162EL VERTICAL ATTACHMENT ANGLE IS CRACKED FS 469.53. REMOVED DAMAGED RT UPPER WING VERTICAL ATTACHMENT ANGLE & REPLACED W/NEW SERVICEABLE ANGLE PN IAW SRM 51-42-13 & 51-42-06.

Part: INTERCOSTAL — CRACKED (BS 460) · airframe 30,256 hrs · 26,877 cycles

LEFT FS 460.00 INTERCOSTAL IS CRACKED AT LBL 9 SECOND RIVET DOWN .5" LONG. CUT AWAY DAMAGE ON INTERCOSTAL WEB AS SHOWN IN REO 601R-53-41-1600 FIG 2 SHEET 2 TO STEP 1 & 2. FABRICATED DOUBLER & FILLER IAW REO 601R-53-41-1600 IAW SRM 51-21-16 TO STEPS 4 OF REO. REO 601R-53-41-1600 HAS BEEN ACCOMPLISHED.

Part: ATTACH ANGLE — CRACKED (LT WING) · airframe 30,256 hrs · 26,877 cycles

LEFT UPPER WING UNDER FUSELAGE TO WING ACCESS PANEL 161EL VERTICAL ATTACHMENT ANGLE IS CRACKED. LOCATED & DRILLED NEW SERVICEABLE VERTICAL ATTACHMENT BRACKET IAW SRM 51-40-11, INSTALLED NEW SERVICEABLE VERTICAL ATTACHMENT BRACKET UNDER ACCESS PANEL 161EL ON LT UPPER WING IAW SRM 51-42-06.

Part: SKIN — CRACKED (LT WING) · airframe 30,257 hrs · 26,879 cycles

LT WING LOWER PLANK IS CRACKED .235" LONG OTBD OF JACK PAD PLUG AT WS 148.019 T/E. COMPLIED WITH EC/TC REO 601R-57-21-131 AND REO 601R-57-21-131, REV A DATED 08/29/2011 AS WRITTEN. COMPLIED WITH EC/TC REO 601R-57-21-130 AND GENERIC REO 601R-57-21-130 REV.J.

Part: SKIN — CRACKED (RT WING) · airframe 30,257 hrs · 26,879 cycles

EXTERIOR SURFACE OF LOWER RT WING PLANK T/E AT WS 148.019 IS CRACKED APPROX 1.0 LONG. COMPLIED WITH EC/TC REO 601R-57-21-131 AND REO 601R-57-21-131 REV A.

Part: PLATE — CORRODED (SERVICE DOOR) · airframe 30,256 hrs · 26,877 cycles

SERVICE DOOR STEP PLATE HAS MAJOR CORROSION. NEW SERVICE DOOR STEP PLATE DRILLED IAW SRM 51-41-04. INSTALLED PLATE IAW AMM 25-33-01-400-802, STEP 3A(8).

Part: ANGLE — CRACKED (BS 621-625) · airframe 30,256 hrs · 26,877 cycles

AFT EQUIPMENT BAY, LT SIDE 621 -625 OBLIQUE ANGLE CRACKED. REMOVED LT SIDE OBLIQUE ANGLE REPLACED WITH SERVICEABLE OBLIQUE ANGLE IAW SRM 51-42-21. PAINT TOUCH UP ANGLE IN AFT EQUIP BAY LT SIDE IAW SRM 51-25-01. SDR CLOSED.

Part: SIGN — MISSING (EMERGENCY LIGHTS) · airframe 30,246 hrs · 26,864 cycles

LIGHTED EXIT SIGN NEAR SERVICE DOOR MISSING. INSTALLED LIGHTED EXIT SIGN NEAR SERVICE DOOR IAW AMM 33-51-10.

Part: DOOR — LACK OF LUBE (MAIN PAX) · airframe 30,170 hrs · 26,783 cycles

PAX DOOR WOULD NOT OPEN FROM OUTSIDE. LUBRICATED PASSENGER DOOR IAW AMM 12-20-52. OPS CHECKED DOOR IAW AMM 52-11-00. ACFT OK FOR SERVICE.

Part: A/C PACK — MALFUNCTIONED · airframe 30,202 hrs · 26,814 cycles

EXCESSIVE FOG FROM LT A/C PACK VENTS RESTRICTING VISIBILITY. . PERFORMED OPS CHECK OF LT PACK ,OPS CHECKED GOOD, NO DEFCT NOTED IAW AMM 21-51-00,

Part: HANDLE — LACK OF LUBE (PAX DOOR) · airframe 30,068 hrs · 26,665 cycles

UNABLE TO OPEN MAIN PAX DOOR FROM INSIDE OR OUTSIDE. LUBRICATED PAS DOOR HANDLE IAW AMM 12-20-52-640-807. OPS CHECKED GOOD, ACFT OK FOR SERVICE.

Part: ROD — LACK OF LUBE (PAX DOOR) · airframe 29,889 hrs · 26,486 cycles

UNABLE TO OPEN MAIN PASSENGER DOOR FROM OUTSIDE. CLEANED AND LUBED OUTER HANDLE ROD. OPS CHECKED PAX DOOR IAW AMM 52-11-00-710-810. NO FAULTS NOTED AT THIS TIME.

Part: LOCK — LACK OF LUBE (PAX DOOR) · airframe 29,735 hrs · 26,314 cycles

F/A REPORTS PAX DOOR DIFFICULT TO OPEN. LUBRICATED EXT HANDLE LOCK ASSY, OPS CHECKED OF PAX DOOR GOOD IAW AMM 52-11-00.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 29,382 hrs · 25,911 cycles

F/A FLASHLIGHT FOR CABIN INOPERATIVE. REPLACED F/A FLASHLIGHT BATTERIES. OK FOR SERVICE IAW AMM 25-60-00.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 29,317 hrs · 25,844 cycles

FLAPS FAIL CAUTION MESSAGE ON TAKEOFF CLIMB. FLAPS FAILED AT 8 DEGREES. ACFT RETURNED TO DEPARTURE, EMERGENCY DECLARED. RESET FLAP SYS IAW AD 2009-06-12.

Part: PIN — UNSERVICEABLE (DOOR HANDRAIL) · airframe 29,280 hrs · 25,802 cycles

CABIN DOOR OPENS PARTIALLY AND THEN SPRINGS BACK CLOSED. R & R AFT HANDRAIL QUICK RELEASE PIN AND LANYARD IAW AMM 52-11-00 AND SECURED IAW EO 600-52-53. OPS CHECKED GOOD.

Part: DOOR — BINDING (PAX) · airframe 27,709 hrs · 24,042 cycles

PAX DOOR VERRY DIFFICULT TO OPEN. LUBRICATED DOOR PINS IAW AMM 12-20-52. OPS CK GOOD, ACFT OK FOR SERVICE. (CLOSED)

Part: HANDLE — DIRTY (PAX DOOR) · airframe 27,592 hrs · 23,915 cycles

PAX DOOR WILL NOT OPEN FROM THE OUTSIDE AND DIFFICULT TO OPEN FROM THE INSIDE. CLEANED DIRT FROM OUTER HANDLE AND PURGED OUT OUTER HANDLE IAW AMM 52-11-00, OPS CK GOOD AT THIS TIME.

Part: DOOR — DIRTY (MAIN PAX) · airframe 27,421 hrs · 23,714 cycles

MAIN CABIN DOOR DIFFICULT TO OPEN AND CLOSE. CLEANED EXCESS DIRT AND GREASE FROM ASD OUTER HANDLE PLUNGER ASSY AND OPS CHECKED DOOR IAW AMM 52-11-00. OPENS AND CLOSES EASILY FROM INSIDE AND OUTSIDE ACFT OK FOR SERVICE.

Part: ESCAPE HATCH — UNKNOWN (COCKPIT) · airframe 27,170 hrs · 23,409 cycles

CREW ESCAPE HATCH REQUIRES PAINT AND PLACARDS. APPLIED PAINT AND PLACARDS TO THE CREW ESCAPE HATCH IAW SRM 51-25-00, AND 11-20-00.

Part: LIGHT — DAMAGED (CABIN) · airframe 27,155 hrs · 23,392 cycles

FLOOR EMERGENCY LIGHT BY PAX ENTRY WAY BACKING/HSG DAMAGED. R & R FLOOR EMERGENCY BY PAX DOOR ENTRY WAY BASE IAW AMM 33-51-19. OPS CHECK GOOD. R & R FLOOR EMERGENCY BY PAX DOOR ENTRY WAY BASE IAW AMM 33-51-19. OPS CHECK GOOD. (CLOSED)

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 27,128 hrs · 23,356 cycles

EMERGENCY LIGHT COVER ON THE FLOOR OF MAIN PASSENGER DOOR FELL OFF. REPLACED EMERGENCY LIGHT COVER LENS NEAR ASD IAW AMM 33-60-00. (CLOSED)

Part: FUSE — BLOWN (BATTERY CHARGER) · airframe 27,120 hrs · 23,346 cycles

NR 2 LT EXTERIOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED NR 2 EMERGENCY BATTERY CHARGER FUSES PER CRJ 200 CMM 33-21-70. OPS CHECKS GOOD. NO DEFECTS NOTED. PLACARD REMOVED.

Part: FUSE — BLOWN (BATTERY CHARGER) · airframe 27,105 hrs · 23,334 cycles

NR 2 LT EXTERIOR EMERGENCY LIGHT INOP, EXTERIOR EMERGENCY LIGHTS - AIRCRAFT NOT OPERATED AT NIGHT ITEM RESOLVE UNDER MDDR: 516560-2. REMOVED AND REPLACED NR 2 EMERGENCY BATTERY CHARGER FUSES PER CRJ 200 CMM 33-21-70. OPS CHECKS GOOD. NO DEFECTS NOTED. PLACARD REMOVED.

Part: STRINGER — CORRODED (BS 333-349 S26L) · airframe 26,823 hrs · 22,996 cycles

STRINGER 26L BETWEEN FS 349 AND 333 HAS MATERIAL LOSS OF 50 PERCENT FROM CORROSION. TOP COAT REQUIRES TO BE APPLIED TO EXTERIOR SIDE OF REPAIR AT FS 299.306, STR 26L RIVET HEADS. PAINTED IAW SRM 51-25-01.

Part: STRINGER — CORRODED (BS 333-349 S26L) · airframe 26,837 hrs · 23,013 cycles

STRINGER 26L BETWEEN FS 349 AND 333 HAS HAS MATERIAL LOSS OF 50 PERCENT FROM CORROSION. RT SPLICE REQUIRES LOCATE/DRILL AND BOTH LT AND RT SPLICE ANGLES REQUIRE INSTALL. PERFORMED EDDY CURRENT INSP ON THE CUT LINES OF STRINGER 26L AT FS 302.5. NO INDICATIONS FOUND AT THIS TIME REPORT ATTACHED IAW STEP 4A(5) OF CRJ SRM 53-00-03 AND NDTM PART 1, 51-20-06. RT SPLICE REQUIRES LOCATE/DRILL AND BOTH LT AND RT SPLICE ANGELS REQUIRE INSTALL. FABRICATD RT STRINGER SPLICE ANGLE AT FS 299 - FS 306 IAW SRM 53-00-03. 2 SPLICES LT & RT REQUIRES INSTALLATION AT STR 26L AT FS 299 - FS 306. INSTALLED LT & RT STRINGER SPLICES IAW SRM 53-00-03, 53-042-06 & 51-42-21. TOP COAT REQUIRED TO EXTERIOR SIDE OF REPAIR AT FS 299 - 306 STR 26L RIVETS HEAD. NDT ON STR 26L PERFORMED PRIOR TO STEP 3 REQ DOCUMENTATION. STEP 7 (ABOVE) IS NDT OF CUT LINES. (CLOSED)

Part: FRAME — CORRODED (BS 605 S26L/R) · airframe 26,823 hrs · 22,996 cycles

FS 605 FRAME CORRODED FWD & AFT SIDE AT STR 26L - 26R. THIS MWC IS A CONTINUATION OF MWC CO 7327210. REPAIRED IAW SRM 51-42-06 AND 51-42-21.

Part: SUPPORT — CRACKED (CARGO DOOR) · airframe 26,823 hrs · 22,996 cycles

CARGO DOOR STEP PLATE SUPPORT IS CRACKED. REMOVED CARGO DOOR STEP PLATE SUPPORT FROM FLOORBOARD 281LLF BY REMOVING 13 SCREWS. SUPPORT REQUIRES INSTALL. INSTALLED NEW SERVICEABLE CARGO DOOR STEP PLATE SUPPORT FLOORBOARD 281LLF BY PLACING INTO POSITION AND INSTALLING 13 SCREWS IAW AMM 20-21-00-910-801.

Part: FLOORBEAM — CORRODED (BS 559) · airframe 26,823 hrs · 22,996 cycles

JUST FWD OF FS 559+112 RBL 9 OTBD FLOOR SUPPORT ANGLE CORRODED. CONTINUATION OF MWC 8732821, OP 220. INSTALLED NEW SERVICEABLE RBL 9 FLOORBEAM TOP CAP AT FS 559 TO FS 574 IAW REO 601R-53-00-381, REV A AND SRM 51-42-34. INSTALLED SERVICEABLE FLOOR SEAT RAILS AND FILLER STRIPS AT FS 559 TO 574 RBL 9 IAW AMM 53-01-11-400-802. INSTALLED TAPE TO FLOORBEAM IAW REO 601R-53-00-381, REV A HAS BEEN ACCOMPLISHED AND ALL STEPS HAVE BEEN DOCUMENTED AND SIGNED FOR ON A NON-ROUTINE WORK CARD. ALL RII'S HAVE BEEN ACCOMPLISHED IAW ASA GMM 3-3 PROCEDURES PRIOR TO THE ACFT BEING RETURNED TO SERVICE.

Part: BUTTSTRAP — CORRODED (BS 333 S25-27L) · airframe 26,823 hrs · 22,996 cycles

BUTT STRAP AT FS 333, STR 25-27L HAS CORROSION. REMOVED FASTENERS COMMON TO CORRODED AREA. BLENDED DAMAGE FOUND TO BE OUT OF LIMITS IAW SRM 53-00-31, FIG 103. REMOVED REMAINING FASTENERS COMMONG TO CUT SPLICE STEP 23L-STR 23R IAW SRM 51-42-06. DRILLED UP NEW BUTT STRAP IAW SRM 51-42-06. OK TO INSTALL. INSTALLED BUTT STRAP AND RESECURED STR 27 IAW SRM 51-42-06. RESECURE REMAINING STRS 26R, 25L,R, AND 24L,R AND SEAL GAP. INSTALLED REMAINING RIVETS MISSING FROM STR 26R, 25L&R AND 24L&R IAW SRM 51-42-06. PAINTED AND GAP SEALED REPAIRED AREA AT FS 333 STR 25L-STR 27 IAW SRM 51-23-00 AND 51-25-01.

Part: FLOORBEAM — CORRODED (BS 559) · airframe 26,823 hrs · 22,996 cycles

FS 559+80 FLOOR SUPPORT CAP STRIP BETWEEN RBL 27- RBL 36 CORRODED. REMOVED FLOOR SUPPORT CAP STRIP IAW SRM 51-42-06. LOCATED, DRILLED AND INSTALLED A SERVICEABLE CAP STRIP AT FS 559+80 BETWEEN RBL 27 - RBL 36 IAW SRM 51-40-11, 51-42-06 AND 51-42-15.

Part: FLOORBEAM — CORRODED (BS 559) · airframe 26,823 hrs · 22,996 cycles

FS 559+80 FLOOR SUPPORT CAP STRIP BET RBL 9 - RBL 27 CORRODED. REMOVED FLOOR SUPPOR TCAP STRIP IAW SRM 51-42-06. INSTALLED NEW CAP STRIP IAW SRM 51-42-06 & 51-45-00.

Part: PRESSURE PANEL — CRACKED (BS 460) · airframe 26,823 hrs · 22,996 cycles

FOUND FS 460 PRESSURE FLOOR HAS INDICATION NOTED BETWEEN BL 0 AND RBL 9.0 3.0" IN LENGTH 50 PERCENT FSH FAILED NDT INSP. AREA MARKED ON ACFT. C/W STEP 1 OF REO 601R-53-41-1276. C/W STEPS 2, 3, AND 5 OF REO 601R-53-41-1276. C/W STEP 4 OF REO 601R-53-41-1276. C/W STEP 6 OF REO 601R-53-41-1276. INSTALLED 10 JOBOLTS AS REQUIRED THROUGH REPAIR IAW REO 601R-53-41-1276. REO 601R-53-41-1276 REV -- HAS BEEN ACCOMPLISHED AND ALL STEPS HAVE BEEN DOCUMENTED AND SIGNED FOR ON A NON-ROUTINE WORK CARD. ALL RII'S HAVE BEEN ACCOMPLISHED PER ASA GMM 3-3 PROCEDURES PRIOR TO THE A/C BEING RETURNED TO SERVICE.

Part: BULKHEAD WEB — CRACKED (AFT) · airframe 26,823 hrs · 22,996 cycles

FOUND REAR PRESSURE BULKHEAD WEB THAT SURROUNDS THE LINTEL ATTACHMENT FITTING HAS INDICATION NOTED .1" IN LENGTH 50 PERCENT FSH. FAILED NDT INSPECTION. REPAIR IAW EC/TC REO 601R53-61-1230 HAS BEEN COMPLETE AND THE REPAIR C/W THE REQUIREMENTS OF EC/TC AND REO 601R-53-61-1230, REV D./ ASA RII C/W 5300010".

Part: POST — CRACKED (BS 409) · airframe 26,823 hrs · 22,996 cycles

FOUND FS 409+128 BL 0.0 RT SIDE VERTICAL POST HAS INDICATION NOTED APPROX .2" IN LENGTH 50 PERCENT FSH. FAILED NDT INSP (WL 69.0 AFT FLANGE RADIUS). REMOVED POST FS 409+128 BL 0 IAW SRM 51-42-06, 51-42-21. LOCATED AND DRILLED UP NEW FS 409+128 BL 0 VERTICAL POST IAW SRM 51-40-11. INSTALLED VERTICAL POST AT FS 409+128 BL 0 IAW 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 REV A.

Part: POST — CRACKED (BS 409) · airframe 26,823 hrs · 22,996 cycles

FOUND FS 409+128, RBL 18.0, OTBD VERTICAL POST HAS INDICATION NOTED APPROX .2" IN LENGTH 60 PERCENT FSH. FAILED NDT INSP (WL 69.0 AFT FLANGE RADIUS). REMOVED VERTICAL POST ON FS 409+128 RBL 18.0 IAW SRM 51-42-06. LOCATED & DRILLED NEW OTBD VERTICAL POST STR 409+128 RBL 18 IAW SRM 51-40-11. ASSEMBLED INBD & OTBD VERTICAL POST 409+128 RBL 18 IAW SRM 51-42-06. 409+128 RBL 18. INSTALLED VERICAL POST 409+128 RBL 18 ASSY IAW SRM 51-42-06 & COMPLIED WITH EC/TC REO 601R-53-41-889 AND MET ALL REQUIRESMENTS OF REO 601R-53-41-889, REV A.

Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 26,823 hrs · 22,996 cycles

CORROSION ON 2EA INTERCOSTALS AT FS 349-364, BETWEEN STR 27 AND 26R, STR 27R AND 26L. REMOVED MINOR SURFACE CORROSION ON INTERCOSTAL AT 27L AND 26L IAW SRM 53-21-17, 53-00-00 & 51-21-06. INSTALLED 2 EA INTERCOSTALS BETWEEN STR 26L & STR 27 AND BETWEEN STR 26R & 27R IAW SRM 51-42-06. TOPCOATED INTERIOR FASTENERS IAW SRM 51-25-16 AND APPLIED CORROSION INHIBITING COMPOUND IAW SRM 51-21-11. REF CO 7328210 JOB 8732821 OP 173 LINE ITEM NR1 FOR REMOVAL OF INTERCOSTALS. INTERCOASTALS INSTALLED IN LINE 2 OF THIS MWC WAS INSTALLED AS A NEW SERVICEABLE INTERCOSTAL AT STR 27 & 26R AND A REPAIRED SERVICEABLE INTERCOSTAL AT STR 27 & 26L.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 26,823 hrs · 22,996 cycles

2 AFT CEILING EMERGENCY FLOODLIGHTS INOP. REMOVED LENS FROM CEILING EMERGENCY FLOODLIGHTS 3 AND 4 IAW AMM TASK 33-51-16-000-801, STEP 3A. REMOVED LAMPS FROM FLOODLIGHTS BY PUSHING LAMP IN AND TURNING IN COUNTERCLOCKWISE DIRECTION. INSTALLED SERVICEABLE LAMPS IN FLOODLIGHTS BY PUSHING LAMP IN AND TURNING IN CLOCKWISE DIRECTION. INSTALLED LENS IN FLOODLIGHTS IAW AMM TASK 33-51-16-400-801 STEP 3A4. CEILING EMERGENCY FLOODLIGHTS 3 AND 4 REQUIRE OPS CK. OPS TEST IS GOOD IAW AMM TASK 33-51-00-710-801.

Part: SUPPORT BEAM — CRACKED (CARGO DOOR) · airframe 26,823 hrs · 22,996 cycles

CARGO DOOR SUPPORT BEAM AFT LOWER ANGLE IS CRACKED APPROX .3" IN LENGTH. R & R CARGO DOOR SUPPORT BEAM AFT LOWER ANGLE IAW SRM 51-42-21.

Part: SIGN — CRACKED (EMERGENCY LIGHT) · airframe 26,823 hrs · 22,996 cycles

PAX DOOR INNER HANDLE BETA LIGHT EXIT SIGN IS CRACKED. REMOVED DAMAGED BETA LIGHT FROM BAY DOOR INNER HANDLE. INSTALLED A NEW BETA LIGHT IAW AMM 20-21-00-910-801.

Part: STRINGER — CORRODED (BS 333-349 S26L) · airframe 26,823 hrs · 22,996 cycles

STRINGER 26L, BETWEEN FS 349 AND FS 333 HAS MATERIAL LOSS OF 50 PERCENT FROM CORROSION. REMOVED STR 26L FROM FS 280 TO FS 364.0 IAW SRM 51-42-06, 51-42-21. CUT STR 2L AT FS 302.5 FOR SPLICE OF NEW SECTION OF STR FROM FS 302.5 TO FS 364 IAW SRM 53-00-03. REINSTALLED STR 26L FROM FS 280 TO FS 299 IAW SRM 51-42-06 AND 51-42-21. INSTALLED NEW SECTION OF STR 26L FROM FS 306 TO FS 364 IAW SRM 51-42-21 AND 51-42-06. DRILLED AND LOCATED LT STR SPLICE AT FS 299-FS 306 IAW SRM 53-00-03.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 26,823 hrs · 22,996 cycles

CARGO BAY RBL 9, 1 SEAT RAIL CORRODED. REMOVED RBL 9 SEAT RAIL IAW SRM 51-41-02. REQUIRES DRILLING NEW HOLES AND INSTALLATION. RBL 9 SEAT RAIL CORROSION IS OUT OF LIMITS OF THE ALLOWABLE DAMAGE IAW SRM 53-61-49. DRILLED HOLES AND INSTALLED NEW SEAT RAIL IAW SRM 53-61-49.

Part: INTERCOSTAL — CORRODED (BS 364-349) · airframe 26,823 hrs · 22,996 cycles

INTERCOSTALS AT LBL 3 AND RBL 3 BETWEEN FRAME 364 AND FS 349 HAVE CORROSION.

Part: FLOORBEAM — CORRODED (BS 559) · airframe 26,823 hrs · 22,996 cycles

FS 559+112, RBL 9 - RBL 27, FLOORBEAM ANGLE CORRODED. REMOVED CORROSION IAW SRM 51-21-06. FLOOR SUPPORT ANGLE CORROSION IS IN LIMITS. REMOVED 1 PERCENT OF THE MATERIAL THICKNESS IAW SRM 53-00-00. PERFORMED LPI ON FS 559-112 RBL 9 - RBL 27 FLOOR SUPPORT ANGLE IAW NDTM 51-20-08. NO INDICATIONS NOTED AT THIS TIME. TREATED AND PAINTED REPAIRED AREA IAW SRM 51-25-16.

Part: FRAME — CORRODED (BS 333 S26L/R) · airframe 26,823 hrs · 22,996 cycles

FRAME 333 HAS CORROSION WITH 100 PERCENT MATERIAL LOSS BETWEEN STR 26L TO STR 26R AT DEEPEST POINT. REMOVED CORRODED FRAME FROM FS 333 BETWEEN STR 26L TO 26R IAW SRM 51-42-06 AND 51-42-21. LOCATED AND DRILLED NEW SERVICEABLE FRAME AT FS 333 BETWEEN STR 26L TO 26R IAW SRM 51-40-11. INSTALLED SERVICEABLE FRAME AT FS 333 BETWEEN STR 26L TO 26R IAW SRM 51-42-06 & 51-42-21. PAINTED REPAIRED AREA AT FS 333 BETWEEN STR 26L TO 26R IAW SRM 51-25-01.

Part: PLACARD — MISSING (EMERGENCY EXIT) · airframe 26,823 hrs · 22,996 cycles

CREW ESCAPE HATCH PLACARDS "CLOSED, ARROW, AND EMERGENCY EXIT" ARE MISSING. APPLIED MISSING ARROW, CLOSED, AND EMERGENCY EXIT SILKSCREENS TO CREW ESCAPE HATCH IAW AMM TASK 11-10-03-400-801. (CLOSED)

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 26,823 hrs · 22,996 cycles

CARGO BAY, LBL 27, 1 SEAT RAIL & 3 NET TIE DOWNS CORRODED. REMOVED 2 SEAT RAILS AND 2 NET TIE DOWNS IAW SRM 51-41-02. CORROSION ON 3 SEAT RAILS AND 2 NET TIE DOWNS IS OUT OF LIMITS OF THE ALLOWABLE DAMAGE IAW SRM 53-61-49. DRILLED HOLES AND INSTALLED 2 NEW SEAT RAILS AND 2 NET TIE DOWNS IAW SRM 53-61-49. INSTALLED SEAT RAIL PN 601R38779-13 IAW SRM 51-41-00.

Part: POST — CRACKED (BS 409) · airframe 26,823 hrs · 22,996 cycles

FS 409+128 VERTICAL BEAM AT LBL 18.0 IS CRACKED ON OTBD BOTTOM CORNER. REMOVED POST ASSY AT FS 409.+128 LBL 18 IAW SRM 51-42-06. R & R OTBD STIFFENER PN 601R32208-155 IAW SRM 51-42-06. C/W EC/TC REO 601R-53-41-889 AND MET ALL THE REQUIREMENTS OF REO 601R-53-41-889 REV A AND IAW SRM 51-42-06.

Part: FLOORBEAM — CORRODED (BS 589) · airframe 26,823 hrs · 22,996 cycles

FS 589, LBL 9 - LBL 27, FLOORBEAM ANGLE CORRODED. REMOVED FLOOR SUPPORT ANGLE IAW SRM 51-40-11. REQUIRE INSTALLATION. FLOOR SUPPORT ANGLE CORROSION IS OUT OF LIMIT OF THE ALLOWABLE DAMAGE IAW SRM 53-00-00. LOCATED AND DRILLED UP NEW FLOOR CAP STRIP PN 601R35031-165 IAW SRM 51-42-06, 51-42-21. INSTALLED NEW FLOOR CAP STRIP PN 601R35031-165 IAW SRM 51-42-06, 51-42-21. INSTALLED MYLAR TAPE ONTO THE FLOOR SUPPORT ANGLE AT FS 589 LBL 9-LBL 22 IAW SRM 51-27-19.

Part: FRAME — CORRODED (BS 310 S26L/R) · airframe 26,823 hrs · 22,996 cycles

FRAME 310, HAS CORROSION WITH 50 PERCENT MATERIAL LOSS AT DEEPEST POINT BETWEEN STR 26L TO 26R. REMOVED FRAME SECTION 310 IAW SRM 51-42-06 AND SRM 51-42-21. LOCATED AND DRILLED UP NEW FRAME SECTION 310 IAW SRM 51-42-06. INSTALLED NEW FRAME SECTION AT FS 310 IAW SRM 51-42-06 AND SRM 51-42-21. PAINTED REPAIRED AREA AT FS 310 BETWEEN STR 26L TO 26R IAW SRM 51-25-01. OP 508 FOR REMOVAL & INSTALLATION OF INSULATION.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 26,823 hrs · 22,996 cycles

CARGO BAY LBL 9, 3 SEAT RAILS AND 2 NET TIE DOWNS CORRODED. REMOVED 2 SEAT RAILS AND 2 NET TIE DOWNS IAW SRM 51-41-02. CORROSION ON 3 SEAT RAILS AND 2 NET TIE DOWNS IS OUT OF LIMITS OF THE ALLOWABLE DAMAGE IAW SRM 53-61-49. DRILLED HOLES AND INSTALLED 2 NEW SEAT RAILS AND 2 NET TIE DOWNS IAW SRM 53-61-49. INSTALLED SEAT RAIL PN 601R38779-13 IAW SRM 51-41-00.

Part: FRAME — CORRODED (BS 319) · airframe 26,823 hrs · 22,996 cycles

FRAME 319 HAS CORROSION WITH 100 PERCENT MATERIAL LOSS AT DEEPEST POINT BETWEEN STR 26L TO STR 26R. R & R LT FS 449.85 OVERWING ATTACHMENT ANGLE IAW SRM 51-42-06, 51-40-11, 51-42-15 AND AMM 51-23-00-100-801.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 26,823 hrs · 22,996 cycles

CARGO BAY RBL 27, 1 SEAT RAIL CORRODED. REMOVED RBL 27 SEAT RAIL IAW SRM 51-41-02. REQUIRES DRILLING NEW HOLES AND INSTALLATION. RBL 27 SEAT RAIL CORROSION IS OUT OF LIMITS OF THE ALLOWABLE DAMAGE IAW SRM 53-61-49. DRILLED HOLES AND INSTALLED NEW SEAT RAIL IAW SRM 53-61-49.

Part: FLOORBEAM — CORRODED (BS 559) · airframe 26,823 hrs · 22,996 cycles

FS 559+112 FLOORBEAM ANGLE BETWEEN RBL 27 - RBL 36 CORRODED. REMOVED CORROSION IAW SRM 51-21-06. FLOOR SUPPORT ANGLE CORROSION IS IN LIMITS. REMOVED 1 PERCENT OF THE MATL THICKNESS IAW SRM 53-00-00. PERFORMED LPI ON FS 559+112 FLOOR SUPPORT ANGLE BETWEEN RBL 27 - RBL 36 IAW NDTM 51-20-08. NO INDICATION NOTED AT THIS TIME. TREATED AND PAINTED REPAIRED AREA IAW SRM 51-25-16.

Part: FRAME — CORRODED (BS 605 S26L/R) · airframe 26,823 hrs · 22,996 cycles

FS 605, FRAME CORRODED FWD & AFT SIDE AT STR 26L - 26R. FOUND CORROSION OF FS 605 FROM TO BE OUT OF LIMITS IAW SRM 53-00-00. REMOVED OUT OF LIMITS FROM SECTION AT FS 605.00 FROM STR 21L - STR 21R IAW SRM 51-42-06. INSTALLED FRAME IAW SRM 51-42-06 & 51-42-21.

Part: FITTING — CORRODED (BS 621) · airframe 26,823 hrs · 22,996 cycles

FS 621, LBL 27, LENTIL FITTING UPPER CORRODED. REMOVED CORRODED FITTING IAW SRM 51-42-21. LOCATED AND INSTALLED IAW EO 601R35031 AND SRM 51-42-22. COMPLIED WITH EC/TC SNIEO 601R35031 S01 AND SNIEO 601R-35031 S01.

Part: FLOORBEAM — CORRODED (BS 559) · airframe 26,823 hrs · 22,996 cycles

JUST FWD OF FS 559+112, RBL 9, OTBD FLOORBEAM ANGLE CORRODED. CORROSION AT FLOOR SUPPORT ANGLE IS OUT OF LIMIT OF THE ALLOWABLE DAMAGE IAW SRM 53-00-00. REMOVED FLOOR SEAT RAILS AND FILLER STRIPS RBL 9 BETWEEN FS 559.00 AND FS 574.00 TO ACCESS FLOORBEAM TOP CAP SUPPORT REPLACEMENT. ALL WORK IAW AMM TASK 53-01-11-000-802. RBL 9 FLOORBEAM SUPPORT TOP CAP PN 601R31119-9. REMOVED RBL 9 FLOORBEAM FLOOR SUPPORT TOP CAP IAW SRM 51-42-06 AND SRM 51-42-21. DRILLED AND LOCATED NEW SERVICEABLE RBL9 FLOORBEAM TOP CAP AT FS 559 TO FS 574 IAW SRM 51-42-06, 51-42-21 AND REO 601R-53-00-381.

Part: ATTACH ANGLE — CRACKED (BS 449.85) · airframe 26,823 hrs · 22,996 cycles

RT FS 449.85 OVERWING ATTACHMENT ANGLE BEHIND PANEL 162EL IS CRACKED. REMOVED ANGLE COMMON TO RT OVERWING ATTACHMENT PANEL 162EL & FS 449.85 IAW SRM 51-42-06. RECEIVED NEW ANGLE FROM STORES. DRILLED & LOCATED HOLES ON ANGLE IAW SRM 51-40-11. OK TO INSTALL. INSTALLED NEW ANGLE (PN 601R31037-48) IAW SRM 51-42-06 & NUTPLATES COMMON TO ANGLE IAW SRM 51-45-00.

Part: ATTACH ANGLE — CRACKED (BS 449) · airframe 26,823 hrs · 22,996 cycles

LT FS 449.85, OVERWING ATTACHMENT ANGLE BEHIND PANEL 161EL IS CRACKED. R & R LT FS 449.85 OVERWING ATTACHMENT ANGLE IAW SRM 51-42-06, 51-40-11, 51-42-15 AND AMM 51-23-00-100-801.

Part: FRAME — CORRODED (BS 319 S26L/R) · airframe 26,823 hrs · 22,996 cycles

FRAME 349 HAS CORROSION WITH 100 PERCENT MATERIAL LOSS BETWEEN STR 26L TO STR 26R AT DEEPEST POINT. REMOVED FRAME AT FS 349 IAW SRM 51-42-06. LOCATED AND DRILLED UP NEW FRAME IAW SRM 51-42-06 AND 51-42-21. INSTALLED ALL RIVETS COMMON TO FRAME THROUGH SKIN AND SUPPORT STIFFENER IAW SRM 51-42-06. INSTALLED REMAINING MISSING FASTENERS AND INTERCOSTALS AT FS 349 IWA SRM 51-42-06. PAINTED REPAIRED AREA AT FS 349 BETWEEN STR 26L TO 26R IAW SRM 51-25-01.

Part: ANGLE — CRACKED (BS 621-625) · airframe 26,823 hrs · 22,996 cycles

REAR PRESSURE BULKHEAD OBLIQUE ANGLE FS 621 TO 625 STR 15 IS CRACKED. R & R OBLIQUE ANGLE PN 601-35012-52 IAW SRM 51-42-21.

Part: PLACARD — DAMAGED (PAX DOOR) · airframe 26,823 hrs · 22,996 cycles

PASSENGER DOOR STEP PLACARD (EXIT) IS DAMAGED. REMOVED WORN PLACARD IAW MM 11-30-00-000-801 AND APPLIED NEW PLACARD IAW 200 MM 11-30-00-400-801.

Part: FRAME — CORRODED (BS 364 S25L/R) · airframe 26,823 hrs · 22,996 cycles

FS 364.00 JUST FWD OF AVIONICS CUTOUT FRAME HAS CORROSION FROM STR 25L TO STR 25R. REMOVED 7 FITTINGS AND 2 EA GUSSET PLATES IAW SRM 51-42-06, 51-42-21 AND 51-41-02 LOCATED AND DRILLED UP FRAME SECTION IAW SRM 51-42-06. INSTALLED NEW SERVICEABLE FRAME SECTION AND 2 EA GUSSET PLATES IAW SRM 51-42-06 AND 51-42-21. DOOR ADJUSTMENT AND PROX SYS CHECK DUE. C/W FUNC AND OPS CHECK IAW AMM 52-42-00-220-801 AND 52-70-08-710-801, CHECK GOOD.

Part: FAIRING — CRACKED (LT NACELLE) · airframe 26,823 hrs · 22,996 cycles

LT LOWER STANG FAIRING, 434BB, INBD SIDE IS CRACKED. RECEIVED LT LOWER STANG FAIRING 434BB. REF MASTER PANEL BOOK PAGE 30 OF 49 FOR INSTALLATION.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 26,768 hrs · 22,939 cycles

NR3 CEILING EMERGENCY LIGHT INOP. NEW 349 FRAME NEED TO BE DRILLED AND INSTALLED. DRILLED NEW FRAME IAW SRM 22 51-40-11. INTERCOSTALS AT STR 25L & 25R, VERTICAL POST AT FS 349L, DRAIN MAST CHANNEL, SUPPORT BRACKET & GANG CLAMP FS 349 24L AND NEW FRAME NEED TO BE INSTALLED. INSTALLED INTERCOSTALS AT STR 25L & 25R, VERTICAL POST AT FS 349L, DRAIN MAST, CHANNEL, SUPPORT BRACKET, GANG CLAMP FS 349 STR 24L, AND NEW FRAME AT FS 349 SRM 51-42-06, 51-42-21, 51-23-00, 51-21-16, AND 51-21-11. (CLOSED)

Part: PLACARD — PEELING (PAX DOOR) · airframe 26,274 hrs · 22,373 cycles

PAX DOOR EXIT PLACARD PEELING. REMOVED AND REPLACED PAX DOOR EXIT PLACARD IAW AMM 11-30-00. REMOVED AND REPLACED PAX DOOR EXIT PLACARD IAW AMM 11-30-00.

Part: LANDING GEAR — MALFUNCTIONED (NOSE) · airframe 26,169 hrs · 22,241 cycles

RECEIVED NLG DISAGREE MSG, RAN QRH (EMERGENCY DECLARED) INSPECTED NOSE LANDING GEAR PROX SYS HANESS, NLG DOOR SYS AND FWD HYD BAY AREA NO DEFECTS FOUND. CYCLED NOSE LANDING GEAR 25 TIMES- NO FAULTS OBSERVED. NLG AND DOORS OPERATE NORMAL IAW AMM 32-20-00. UNABLE TO DUPLICATE DISCREPANCY. ALL OPS AND LEAK CHECKS GOOD. (SDR CLOSED)

Part: FLASHLIGHT — BROKEN (CABIN) · airframe 25,868 hrs · 21,895 cycles

F/A FLASHLIGHT BROKEN. REPLACED FLASHLIGHT IAW AMM 25-60-00.

Part: WARNING MESSAGE — ILLUMINATED (TE FLAPS) · airframe 25,556 hrs · 21,536 cycles

FLAP FAIL MSG AT 30 DEGREES. (EMERGENCY DECLARED - ENROUTE, ACFT DIVERTED TO DUE TO MX)

Part: ANCHOR FITTING — CRACKED (PAX DOOR) · airframe 25,237 hrs · 21,184 cycles

PAX DOOR, AFT ANCHOR FITTING CRACKED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,145 hrs · 21,089 cycles

FLT 5557. EMERG LIGHT SYSTEM INOP WILL NOT TEST.

Part: STEP — CRACKED (ASD) · airframe 23,948 hrs · 19,902 cycles

ASD BOTTOM STEP CRACKED.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 23,014 hrs · 19,037 cycles

AT FS 718.0 BETWEEN STRINGERS 11R AND 12R PREVIOUSLY REPAIRED ATTACH ANGLE CRACKED IN RADIUS. REMOVED PREVIOUS REPAIRS FROM FS 718.0 BETWEEN STRINGERS 11R AND 12R IAW CRJ 200 SRM 51-42-06 AND 51-42-21. LPI CUTLINE AS PER REO 601R-53-61-193 AND CRJ 200 NDTM 51-20-08. NO INDICATIONS NOTED AT THIS TIME. REPAIRED FS 718.00 BETWEEN STRINGERS 11L AND 12L IAW STEPS 2 THROUGH 6 OF BOMBARDIER REO 601R-53-61-193. STEP 1 OF BOMBARDIER REO 601R-53-61-193 TRIM OUT OF FLANGE WAS PREVIOUSLY COMPLIED WITH. ALL WORK WAS COMPLIED WITH IAW ASA EO 600-53-0067 REV A. SUPPLEMENTAL-SDR CLOSED 11/14/2008.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 23,014 hrs · 19,037 cycles

AT FS 718.0 BETWEEN STRINGERS 11L AND 13L PREVIOUSLY REPAIRED ATTACH ANGLES ARE CRACKED IN RADIUS (2 EA). REMOVED PREVIOUS REPAIRS FROM FS 718.0 BETWEEN STRINGERS 11L AND 12L IAW CRJ 200 SRM 51-42-06 AND 51-42-21. CUTLINE AS PER REO 601R-53-61-193 AND CRJ 200 NDTM 51-20-08. NO INDICATIONS NOTED AT THIS TIME. REPAIRED FS 718.00 BETWEEN STRINGERS 11L AND 12L IAW STEPS 2 THROUGH 6 OF BOMBARDIER REO 601R-53-61-193. STEP 1 OF BOMBARDIER REO 601R-53-61-193 TRIM OUT OF FLANGE WAS PREVIOUSLY COMPLIED WITH. ALL WORK WAS COMPLIED WITH IAW ASA EO 600-53-0067 REV A. SUPPLEMENTAL-SDR CLOSED 11/13/2008.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 23,018 hrs · 19,042 cycles

DURING EDDY CURRENT INSPECTION ON THE 621 BULKHEAD FWD FACE, AN INDICATION WAS NOTED AT LBL 48.00, WL 106, .500 IN LENGTH.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 23,014 hrs · 19,037 cycles

WHILE PERFORMING TASK AWL253-41-201, AN INDICATION WAS NOTED AT THE 559 BULKHEAD CAP ANGLE RADIUS LBL 9 AND LBL 18 APPROX .500 INCH IN LENGTH. ACCOMPLISHED REPAIR TO (LT SIDE ONLY) 559 BULKHEAD AND CAP ANGLE IAW REO 601R-53-41-260 REV C. REQUIRES PAINT. PAINTED LT SIDE OF BULKHEAD AND CAP ANGLE IAW SRM 51-25-16. COMPLIED WITH EC/TC REO 601R-53-41-260 IAW REO 601R-53-41-260 REV C.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 23,014 hrs · 19,037 cycles

AN INDICATION WAS NOTED ON THE 621 BULKHEAD FWD FACE DURING AN EDDY CURRENT INSPECTION AT LBL 9.50, WL 110 .350 IN LENGTH. COMPLIED WITH REO 601R-53-61-1285, STEPS 1 THRU 33 FOR REPAIR TO AFT PRESS BULKHEAD FS 621 LBL 9.0. INCORPORATED REO 601R-53-61-2880 DISPOSITION FOR LOW ED ON FS 621 PRESSURE BULKHEAD AT LBL 9.5. COMPLIED WITH EC/TC REO 601R-53-61-1285 AND PROCESSED M-93 WEIGHT CHANGE FORM AS REQUIRED.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 23,014 hrs · 19,037 cycles

WHILE PERFORMING TASK AWL253-41-201, AN INDICATION WAS NOTED AT THE FS 559 BULKHEAD WEB OUTBOARD OF RBL 9, WL 58.7 APPROX .300 INCH IN LENGTH AND INBOARD OF RBL 18, WL 58.7 APPROX 1.0 INCH IN LENGTH. REMOVED DAMAGED SECTION OF THE RT WEB, REPAIRED IAW REO 610R-53-41-260 REV C STEPS 1-14. NUT PLATES REQUIRE SEALANT. AREA REQUIRES PAINT AND CORROSION INHIBITOR. SEALED NUT PLATES, PAINTED AND APPLIED CORROSION INHIBITOR TO REPAIR AREA IAW REO 610R-53-41-260 REV C. COMPLIED WITH EC/TC REO 601R-53-41-260 IAW REO 601R-53-41-260, REV C.

Part: PROXIMITY SENSOR — OUT OF RIG (NLG) · airframe 22,948 hrs · 18,975 cycles

UPON MAIN GEAR TOUCHDOWN RECEIVED NOSE GEAR YELLOW BOX. INITIATED G.A. AND RECEIVED UNSAFE CAUTION WITH NOSE GEAR RED. 3 GREEN NEXT TIME AROUND. EMERGENCY DECLARED. EMERGENCY VEHICLES ON STANDBY AS PRECAUTION. FOUND NLG DOWNLOCK PROX SENSORS PS1GA AND PS2GA TO BE OUT OF RIG. RIGGED PROX SENSORS PS1GA AND PS2GA IAW CRJ 200 AMM 32-61-05. OPS CHECK GOOD. ACFT OK FOR SERVICE.

Part: SILL — CRACKED (CARGO BAY) · airframe 22,869 hrs · 18,903 cycles

INTERCOASTAL AT FS 589 BETWEEN LBL 36 AND CARGO DOOR SILL CRACKED AT SILL ATTACHMENT. THIS SDR WILL REMAIN OPEN PENDING MX DETERMINATION OF AN APPROPRIATE CORRECTIVE ACTION.

Part: FITTING — CRACKED (FUSELAGE) · airframe 22,856 hrs · 18,891 cycles

CLIP CRACKED AT FS605 AT CARGO DOOR SILL AND INTERCOSTAL ATTACHMENT (RESOLVED ON W/O 96197 TASKCARD N/R 00022) JOB COMPLETE ITEM 1. DRILLED UP NEW CLIP IAW CRJ 200 51-40-11RAP 7025969. ITEM 2.

Part: INTERCOSTAL — CRACKED (BS 605) · airframe 22,856 hrs · 18,891 cycles

INTERCOSTAL AT FS 605 BETWEEN LBL 36 AND CARGO DOOR SILL CRACKED AT SILL ATTACHMENT (RESOLVED ON W/O 96197 TASKCARD: N/R 00021) JOB COMPLETE ITEM 1. REFER TO ATTACHED M-234 FORMS FOR WORK ACCOMPLISHED. ITEM 2.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 22,856 hrs · 18,891 cycles

RT INBD FLOOR. SHORT SEAT TRACK AT 559.96 CORRODED (RESOLVED ON W/O 96197 TASKCARD N/R 00025) JOB COMPLETE ITEM 1. R&R RT INBD SHORT SEAT TRACK FROM FS559.96. PER CRJ200 SRM 51-41-00 KR17389 JOB COMPLETED

Part: SEAT TRACK — CORRODED (BS 559) · airframe 22,856 hrs · 18,891 cycles

RT INBD FLOOR SEAT TRACK CORRODED FROM FS 559+16 TO 559+80 (RESOLVED ON W/O 96197 TASKCARD N/R 00024) R&R RT INBD SEAT TRACK FROM FS559+16 TO 559+80. PER SRM 51-41-00.

Part: LIGHT — BROKEN (CABIN) · airframe 22,565 hrs · 18,629 cycles

ESCAPE PATH LIGHTING FWD OF AFT LAV IS CRACKED AND BROKEN REMOVED AND REPLACED EMERGENCY LIGHTING TRACK IAW AMM 33-51-01. OPS CHECK GOOD. (B)

Part: DRAIN LINE — CLOGGED (WATER SEPARATOR) · airframe 2,225,228 hrs · 18,360 cycles

AFTER T/O WHILE RAISING THE GEAR, THERE WAS A SEVERE RANCID ELECTRICAL SMOKE SMELL WITH A HAZY SMOKE IN THE COCKPIT. AIRCRAFT RETURNED TO ATL AFTER T/O, EMERGENCY DECLARED. UNCLOGGED DRAIN LINES FOR LT WATER SEPERATOR IAW AMM 21-51-13-100-802 AND REPLACED COALESCER IAW AMM 21-51-13-140-801 REPLACED MISSING INSULATION BLANKETS ON WATER SEPERATORS PERFORMED FULL GEAR SWING IAW AMM 32-30-00-710-802 AND ENGINE RUNS IAW AMM 71-00-00-710-808 PER REQUEST OF DIRECTOR OF MTC.

Part: PLACARD — MISSING (CABIN) · airframe 21,700 hrs · 17,904 cycles

EXIT PLACARD MISSING FROM INTERIOR ASD. FLT 4330 DEL 35 MINS.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 21,658 hrs · 17,869 cycles

EMERGENCY INTER. LIGHT AT MID CURE CEILING LIGHT AND OVERWING LIGHT AND BATTERY PACK NR 2 INOP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,658 hrs · 17,869 cycles

EMERGENCY LIGHTS AT A/S/D ENTRANCE, FWD LT AND RT WING AND CEILING AFT SIDE OUT. FLT 4485 CX.

Part: STEP — BROKEN (AIRSTAIR DOOR) · airframe 21,467 hrs · 17,707 cycles

ASD BOTTOM STEP BROKEN.

Part: SIGN — LOOSE (EMERGENCY LIGHTS) · airframe 21,210 hrs · 17,492 cycles

EXIT SIGN ABOVE SERVICE DOOR IS LOOSE AND ABOUT TO COME OFF.

Part: SMOKE DETECTOR — ACTIVATED (LAVATORY) · airframe 21,104 hrs · 17,404 cycles

RECEIVED A SMOKE TOILET MESSAGE IN FLIGHT. EN ROUTE TO GRK A/C DIVERTED TO MGM DUE TO MTC. EMERGENCY DECLARED. EMERGENCY EQUIPMENT ON STANDBY. FLT 4549 DEL 63 MINS.

Part: STEP — BROKEN (DOOR) · airframe 20,161 hrs · 16,656 cycles

BOTTOM STEP ON DOOR BROKEN.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,161 hrs · 16,656 cycles

EMERGENCY FLOOR LIGHTING INOP AT 11CD.

Part: RUDDER — MALFUNCTIONED · airframe 19,738 hrs · 16,315 cycles

RIGHT RUDDER 80 PERCENT UNCOMMANDED. EMERGENCY DECLARED. FLTS 4177, 4913, 4888, 4913 CX.

Part: APU — MALFUNCTIONED · airframe 19,716 hrs · 16,300 cycles

CREW REPORTED AT 10,000 FT DURING APU START UP FUMES DETECTED IN THE CABIN AND COCKPIT APU WAS SHUT DOWN AND SMOKE AND FUMES PROCEDURES WERE FOLLOWED AND THE FLIGHT LANDED SAFELY. EMERGENCY DECLARED. FLTS 4575, 4710 CX. AUXILIARY POWER UNIT APU - INTAKE DOOR DEACTIVATED CLOSED.

Part: TORQUE LINK — DISCONNECTED (NLG STEERING) · airframe 19,688 hrs · 16,276 cycles

ON TAKEOFF NLG W/N RETRACT RECEIVED GEAR DISAGREE, WOW INPUT, WOW OUTPUT GEAR DOOR OPEN. FOLLOWED QRH UPON LANDING HAD NO NOSE WHEEL STEERING. FOUND TORQUE LINK DISCONNECTED. A/C RETURNED TO AVP AFTER T/O. EMERGENCY DECLARED.

Part: FLAP — STUCK (WING) · airframe 19,142 hrs · 15,869 cycles

FLAPS STUCK AT 43 DEG DURING APPROACH (LEFT SIDE 43 RIGHT SIDE 45) NO FLAP FAIL MESSAGE WAS RECEIVED. EMERGENCY DECLARED.

Part: UNKNOWN — ODOR (CABIN) · airframe 18,916 hrs · 15,701 cycles

SMELL OF JET FUEL AFTER APU START IN THE AIR.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,267 hrs · 15,226 cycles

EMERGENCY EXIT SIGN BY LT WING EMERGENCY EXIT DOOR AT ROW 8AB IS INOP.

Part: LAMP — BROKEN (EMERGENCY LIGHT) · airframe 18,235 hrs · 15,199 cycles

EMERGENCY FLOOR LIGHTING STRIP HAS BROKEN LAMP. REMOVED & REPLACED WITH SERVICEABLE LAMP IAW CRJ AMM 33-51-01. JPS1057 OPS CK DEFERRED TO 409 WO 3357 W/C 44. JPS1057 (CLOSED)

Part: ANGLE — CRACKED (BS 484) · airframe 18,235 hrs · 15,199 cycles

FS 484 CRACKED LBL 9 OB. REMOVED CRACKED ANGLE AT FS 484, OB SIDE OF LBL 9.0. FABRICATED SERVICEABLE ANGLE FROM 7075.T6 .050 PO 5505-1 IAW CRJ SRM 53-41-43. ALODINED, PRIMED, AND PAINTED SERVICEABLE ANGLE IAW CRJ SRM 51-25-16. INSTALLED REPAIR ANGLE IAW CRJ SRM 51-42-20. DYNATROL AV-25 APPLIED. (SUPPLEMENTAL-SDR CLOSED 8/17/06)

Part: RIB — CRACKED (RT AILERON) · airframe 18,235 hrs · 15,199 cycles

RIGHT AILERON RIB AND ATTACHING ANGLE AT WS 340.481 CRACKED AND CHAFED.

Part: INTERCOSTAL — CRACKED (PAX DOOR) · airframe 18,235 hrs · 15,199 cycles

PAX DOOR INTERCOSTAL CRACKED AT 338.9, DATUM 1. REMOVED INTERCOSTAL AT FS 338.9 DATUM 1 ON PAX DOOR IAW CRJ SRM 51-42-06. LOCATED AND DRILLED NEW INTERCOSTAL P/N 601R31902-318 IAW CRJ SRM 51-40-11. OK TO INSTALL. INSTALLED INTERCOSTAL IAW CRJ SRM 51-42-06 (2 EA) FASTENERS COMMON TO PAX DOOR AFT GUIDE PLATE REQUIRED INSTALLATION. INSTALLED REMAINING FASTENERS IN PAX DOOR INTERCOSTAL IAW CRJ SRM 51-42-06 AND 51-42-21. (SUPPLEMENTAL-SDR CLOSED 8/17/06)

Part: DOOR FRAME — CRACKED (PAX DOOR) · airframe 18,235 hrs · 15,199 cycles

PAX DOOR FRAME CRACKED AT 338.9. REPAIRED IAW ALL SRMS.

Part: STRUCTURE — CRACKED (PAX DOOR) · airframe 18,235 hrs · 15,199 cycles

PAX DOOR EDGE MEMBER CRACKED.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 18,235 hrs · 15,199 cycles

PAX DOOR AFT DRAG ANGLE CRACKED. CUT OUT CRACKED SECTION OF PAX DOOR AFT DRAG ANGLE IAW REO 601R-52-11-513. NDT REQUIRED FOR CUT LINE. NDT PERFORMED ON W/C 350 FABRICATED REPAIR DETAILS FROM NEW ANGLE, 601R31772-5S, OK TO INSTALL. INSTALLED DETAILS IAW REO 601R-52-11-513 REV A. (SUPPLEMENTAL-SDR CLOSED 8/17/06)

Part: CAUTION MESSAGE — UNKNOWN (NLG STEERING) · airframe 18,140 hrs · 15,119 cycles

STEERING INOP CAUTION MSG WHILE NOSEWHEEL WAS RETRACTING DURING AFTER T/O PHASE FROM KPVD. RETURNED TO ATL WITH NO FURTHER INCIDENTS. RESET C/B'S PER MTC AND RESET STEERING TO ARMED POSITION. NO FURTHER DEFECTS NOTED.

Part: HANDLE — STUCK (PAX DOOR) · airframe 18,088 hrs · 15,082 cycles

PASSENGER DOOR DIFFICULT TO OPEN OFTEN AFTER LANDING. HANDLE STUCK ABOUT HALFWAY THROUGH TRAVEL, FINALLY OPENED WHENEXTRA FORCE APPLIED.

Part: PLACARD — FADED (EMERGENCY EXIT) · airframe 17,738 hrs · 14,786 cycles

LT OVER WING EMERGENCY DOOR EXIT PLACARD FADED.

Part: DOOR — MALFUNCTIONED (CABIN) · airframe 17,694 hrs · 14,752 cycles

PAX DOOR W/N OPEN FROM INSIDE OR OUTSIDE.

Part: LIGHT — CRACKED (CABIN)

DURING A HANGAR INSPECTION IN MCN, THE FORWARD AND AFT FLOOR EMERGENCY STRIP LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD AND AFT FLOOR EMERGENCY STRIP LIGHTS. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: STEP — CRACKED (PAX DOOR)

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

Part: ODOR — DETECTED (CABIN)

DURING TAKEOFF, THE CREW NOTICED A STRONG ODOR COMING FROM THE AIR CONDITIONING PACKS IN THE COCKPIT. UPON CHECKING THE ENVIRONMENTAL CONTROL SYSTEM PAGE THE CREW NOTED THE BLEED LINE WAS APPROX 110 PSI WITH ALL OTHER INDICATIONS IN THE NORMAL RANGE. AS THE FLIGHT CONTINUED, THE BLEED LINE PSI RETURNED TO THE NORMAL RANGE AND THE ODOR DISSIPATED. THE ODOR RETURNED WHEN POWER WAS REDUCED FOR DESCENT. THE AIRCRAFT LANDED SAFELY. MAINTENANCE DEFERRED THE CABIN/COCKPIT TEMPERATURE CONTROL SYSTEM LT PACK AUTO MODE UNDER MEL NR 21-61-01-01-A, CAT C EXPIRING 8/25/2005.

Part: DOOR — LACK OF LUBE (MAIN PAX)

AFTER PARKING THE AIRCRAFT, THE PASSENGER DOOR COULD NOT BE OPENED FROM THE INSIDE. MAINTENANCE CLEANED AND LUBRICATED THE TRACK AND ROLLER ASSEMBLY ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. NO FURTHER DEFECTS NOTED. AIRCRAFT OK FOR SERVICE. (K)

Part: STEP — CRACKED (PAX DOOR)

DURING HANGAR MAINTENANCE IN BTR, THE TOP STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLIED THE TOP STEP ON THE PASSENGER DOOR. (M)

Part: STEP — CRACKED (PAX DOOR)

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

Part: DOOR — MALFUNCTIONED (MAIN PAX)

DURING A GROUND INSPECTION, THE PASSENGER DOOR COULD NOT BE OPENED FROM THE INSIDE. MAINTENANCE INSPECTED THE PASSENGER DOOR AND NO DEFECTS WERE NOTED. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: PIN — BINDING (PAX DOOR)

DURING A GROUND INSPECTION, THE PASSENGER DOOR COULD NOT BE OPENED FROM THE INSIDE OR OUTSIDE. MAINTENANCE INSPECTED THE PASSENGER DOOR LINKAGES AND LUBRICATED THE (LATCH) PINS. MAINTENANCE ALSO PRESSURIZED THE AIRCRAFT AND CYCLED THE DOOR SEVERAL TIMES. OPERATIONAL CHECKS GOOD. AC OK FOR SERVICE. (K)

Part: STEP — CRACKED (PAX DOOR)

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

Part: SILL — CORRODED (FUSELAGE)

DURING A C-CHECK IN MCN, THE FLOOR SILL ASSEMBLY AT FS 409 PLUS 128 TO 559 OUTBOARD OF LBL 36 AND RBL 36 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REPAIRED THE FLOOR SILL ASSEMBLY AT FS 409 PLUS 128 TO 559 RT AND LT IAW ASA EO 600-53-0228. (M)

Part: SUPPORT BEAM — CRACKED (FUSELAGE)

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

Part: CLIP — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE INBOARD CLIPS AT FS 484, LBL 27 AND RBL 27 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE INBOARD CLIPS AT FS 484, LBL 27 AND RBL 27 IAW ASA EO 600-53-0098. (M)

Part: INTERCOSTAL — CRACKED (FUSELAGE)

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

Part: INTERCOSTAL — CRACKED (FUSELAGE)

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

Part: CLIP — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE FS 280 CLIPS INBOARD AND OUTBOARD ON THE LEFT AND RIGHT SIDES WRE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE FS 280 CLIPS INBOARD AND OUTBOARD ON THE LEFT AND RIGHT SIDES. (M)

Part: RIB — CRACKED (WING)

DURING A C-CHECK IN MCN, THE LEFT AND RIGHT BATTERY RIB ASSEMBLIES AT WS 53.60 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LEFT AND RIGHT BATTERY RIB ASSEMBLIES AT WLS 53.60 IAW ASA EO 600-57-039A. (M)

Part: PRIORITY VALVE — MALFUNCTIONED (NLG) · airframe 14,140 hrs

DURING TAKEOFF, UPON GEAR RETRACTION, A LOUD NOISE FROM THE NOSE GEAR WAS NOTICED ACCOMPANIED BY A MOMENTARY (DISAGREE) WARNING AND TRIPLE CHIME. THE NOISE CONTINUED FOLLOWED BY THE NOSE GEAR RETRACTING WITH ALL INDICATIONS SHOWING NORMAL. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO DEPARTURE, LANDING SAFELY. MAINTENANCE REMOVED AND REPLACED THE NOSE LANDING GEAR PRIORITY VALVE. OPERATIONAL AND LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: PROBE — BIRD STRIKE (AIR DATA SENSOR)

DURING FERRY FLT, RECEIVED NR 1 & 2 AIRSPEED, ALTITUDE FAIL MESSAGE. NR 1 HORIZ SITUATION INDICATOR WAS UP TO 45 FT OFF FROM STANDBY COMPASS. CREW ALSO RECEIVED GROUND PROXIMITY WARNING WITH GEAR WARNING HORN, FLAP WARNING ACTIVE. ALTITUDE INDICATIONS SHOWED NOSE LOW LT TURN WHEN ACTUALLY AC LEVEL IN RT TURN. EMERGENCY DECLARED, AC LANDED SAFELY. MAINT FOUND DAMAGED PITOT SYS FROM BIRDSTRIKE HAD NOT BEEN DEACTIVATED PROPERLY FOR FERRY FLT CAUSING STATIC SYSTEM TO BE PRESSURIZED. MAINT REMOVED & REPLACED PITOT/STATIC PROBE. OPS AND LEAK CHECKS GOOD. AC FERRIED, FOR COMPLETION TO REPAIR DAMAGE TO FUSELAGE FROM BIRDSTRIKE.

Part: ROD — OUT OF ADJUST (PAX DOOR)

DURING A GROUND INSPECTION, THE PASSENGER DOOR WOULD NOT OPEN FROM THE INSIDE OR OUTSIDE. MAINTENANCE ADJUSTED THE LOCK MECHANISM ROD ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE.

Part: STEP — CRACKED (PAX DOOR)

DURING AN A-CHECK IN BRT, THE LOWER STEP ON THE PASSENGER DOOR WAS FOUND BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LOWER STEP ON THE PASSENGER DOOR. (M)

Part: PUSHROD — OUT OF ADJUST (PAX DOOR)

DURING A GROUND INSPECTION IN DFW, THE PASSENGER DOOR WOULD NOT OPEN FROM THE INSIDE. MAINTENANCE ADJUSTED THE PUSH ROD FROM THE PIVOT ASSEMBLY TO THE LATCH CAM TORQUE TUBE AND INSPECTED THE RIGGING. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: MECHANISM — LACK OF LUBE (PAX DOOR)

FLT 4243 - UPON ARRIVAL OF THE AIRCRAFT AT THE GATE, THE MAIN PASSENGER DOOR COULD NOT BE OPENED. MAINTENANCE WAS ABLE TO OPEN THE DOOR AND ALL PASSENGERS DEPLANED SAFELY. MAINTENANCE LUBRICATED THE MAN PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: DOOR — LACK OF LUBE (PAX)

FLT 4243 - DURING A GROUND INSPECTION IN DFW, THE PASSENGER DOOR WAS FOUND HARD TO OPEN AND CLOSE. MAINTENANCE LUBRICATED THE PASENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: HANDLE — BINDING (PAX DOOR)

FLT 4730 - DURING A GROUND INSPECTION IN DFW, THE PASSENGER DOOR WAS FOUND TO BE STUCK IN THE CLOSED POSITION AND WOULD NOT OPEN. MAINTENANCE LUBRICATED THE PASSENGER DOOR HANDLE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: HINGE — BINDING (PAX DOOR)

DURING A GROUND INSPECTION IN DFW, THE FLT ATTENDANT REPORTED THAT THE PASSENGER DOOR WAS DIFFICULT TO OPEN AND CLOSE. MAINTENANCE LUBRICATED THE PASSENGER DOOR HINGE POINTS. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LAMP — BURNED OUT (EMERGENCY LIGHT)

DURING HANGAR MAINTENANCE IN BTR, THE PASSENGER DOOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR EMERGENCY LIGHT LAMP. (M)

Part: LAMP — BURNED OUT (EMERGENCY LIGHT)

DURING A GROUND INSPECTION IN DFW, THE RT FORWARD EXTERIOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE RIGHT FORWARD EXTERIOR EMERGENCY LIGHT LAMP. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: CONTROL UNIT — OUT OF RIG (TE FLAPS)

DURING TAKEOFF, THE CREW RECEIVED A FLAPS FAIL MESSAGE WHEN SELECTING THE FLAPS TO ZERO DEGREES. QRH PROCEDURES WERE COMPLIED WITH AN EMERGENCY WAS DECLARED. THE AIRCRAFT RETURNED TO ICT AND LANDED SAFELY. MAINTENANCE INSPECTED THE FLAPS AND RESET THE FLAPS ELECTRONIC CONTROL UNIT USING THE BREAKERS IAW ASA EO 600-27-0004A. (M)

Part: COVER — CRACKED (EXIT LIGHT)

DURING A GROUND INSPECTION IN DFW, THE EMERGENCY EXIT LIGHT COVER AT THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT COVER AT THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: STEP — CRACKED (PAX STAIRS)

FLT 4235 - DURING A GROUND INSPECTION IN ATL, THE PASSENGER DOOR BOTTOM STEP WAS FOUND CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR BOTTOM STEP. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: ANGLE — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE AFT PRESSURE BULKHEAD LOWER LEFT AND RIGHT SIDE FLOOR SUPPORT ANGLE AT FS 621 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE AFT PRESSURE BULKHEAD LOWER LEFT AND RT SIDE FLOOR SUPPORT ANGLE AT FS 621 IAW ASA EO 600-53-0105. (M)

Part: PLATE — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE CARGO DOOR FLOOR LANDING PLATE AT THE FORWARD LOWER DOOR STOP WAS FOUND TO BE CRACKED AND CORRODED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE CARGO DOOR FLOOR LANDING PLATE AT THE FORWARD LOWER DOOR STOP IAW SRM 51-00. (M)

Part: FRAME — CRACKED (FUSELAGE)

DUIRNG A C-CHECK IN MCN, THE LEFT SIDE FRAME FS 718 BETWEEN STRINGERS 10 TO 12 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE LEFT SIDE FRAME FS 718 BETWEEN STRINGERS 10 TO 12 IAW ASA EO 600-53-0067A. (M)

Part: FRAME — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE RIGHT SIDE FRAME FS 718 BETWEEN STRINGERS 10 TO 11 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE RIGHT FRAME FS 718 BETWEEN STRINGERS 10 TO 11 IAW ASA EO 600-53-0066. (M)

Part: LIGHT — BROKEN (FUSELAGE)

DURING A HANGAR INSPECTION IN MCN, THE EXTERIOR EMERGENCY LIGHT AT THE AIRSTAIR DOOR WAS FOUND TO BE BROKEN. MAINTENANCE REMOVED AND REPLACED THE EXTERIOR EMERGENCY LIGHT ASSEMBLY AT THE AIRSTAR DOOR. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: FIREWALL — CRACKED (LT PYLON)

FLT 4250 - THE LEFT PYLON FIREWALL AT FRAME STATION 659.75 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE LEFT PYLON FIREWALL AT FRAME STATION 659.75 IAW ASA EO 600-54-0010 AND REO 801R-54-51-004. (M)

Part: ENGINE — LEAKING (LEFT)

FLT 4250 - DURING CRUISE AT APPROXIMATELY 33,000 FT FROM ATL-PHF, THE CREW RECEIVED AN OIL PRESSURE WARNING MESSAGE ON THE LT ENGINE, ALONG WITH AN OIL PRESSURE DROP TO 15 PSI. THE FAN SPEED VIBRATION GAUGE PRIOR TO THE WARNIGN SHOWED .8 TO .9 AND APPEARED TO SPIKE MOMENTS BEFORE THE THRUST LEVER SHUTOFF. QRH PROCEDURES WERE COMPLIED WITH AND THE CAPTAIN SHUTDOWN THE LEFT ENGINE. AN EMERGENCY WAS DECLARED AND EMERGENCY EQUIPMENT REQUESTED. THE AIRCRAFT DIVERTED TO CLT, LANDING SAFELY. MX FOUND THE LEFT ENGINE OIL TANK EMPTY AND SERVICED IT WITH 6 QUARTS OF OIL. MX SUBSEQUENTLY REMOVED AND REPLACED THE LEFT ENGINE. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LIGHT — INOPERATIVE (FUSELAGE)

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

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING A GROUND INSPECTION IN ATL, THE EMERGENCY FLOOR LIGHTING WAS INOPERATIVE THROUGH OUT THE CABIN. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHTING BATTERY PACK IN THE NR 4 POSITION. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: PROXIMITY SENSOR — MALFUNCTIONED (NLG)

DURING APPROACH INTO ABY, THE NOSE GEAR FAILED TO EXTEND. THE CAPTAIN ABORTED THE INITIAL APPROACH. WHILE IN A HOLDING PATTERN, APPROXIMATELY 5 MINUTES AFTER BEING SELECTED DOWN, THE GEAR EXTENDED ON ITS OWN. EVEN WITH THE GEAR SAFE INDICATIONS, A VIBRATIONS WAS STILL FELT COMING FROM THE NOSE AREA. AN EMERGENCY WAS DECLARED AND AN UNEVENTFUL LANDING WAS MADE IN ABY. MAINTENANCE REMOVED AND REPLACED THE NOSE LANDING GEAR NR 2 DOWNLOCK PROXIMITY SENSOR. THE AIRCRAFT WAS JACKED, AND THE GEAR WAS SWUNG SEVERAL TIMES. SYSTEM OPERATIONAL CHECKS GOOD. NO DEFECTS WERE NOTED. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO BAY)

FLT 4669 - DURING THE INITIAL DESCENT INT GPT, AIRCRAFT HAD A CARGO SMOKE AURAL WARNING AND TRIPLE CHIME. CREW DID EMERGENCY PROCEDURE FOR CARGO SMOKE AND DIVERTED TO MOBILE AIRPORT. EVACUATED AIRCRAFT THROUGH MAIN STAIR DOOR AND FIRE MARSHAL OPENED CARGO DOOR AND REMOVED BAGS AND CARGO FROM AIRCRAFT. THERE WAS NO EVIDENCE OF SMOKE OR FIRE. MAINTENANCE REMOVED AND REPLACED BOTH CARGO FIRE BOTTLES AND SQUIBS. OPERATIONAL TESTS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BPSU — INOPERATIVE (TE FLAPS)

FLT 4503 - AFTER DEPARTING HTL ON FLAP RETRACTION, FLAP FAIL MESSAGE CAME ON EICAS. CREW LEVELED OFF AT 6,000 FEET AND PERFORMED AFTER TAKEOFF CHECK LIST. CREW THEN MAINTAINED 200 KNOTS, PERFORMED FLAP FAIL CHECK LIST AND CALLED MAINTENANCE CONTROL. CREW DECLARED AN EMERGENCY. FLIGHT RETURNED TO ATL AND SAFELY LANDED. MAINTENANCE REMOVED AND REPLACED LT BPSU. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (X)