N872AS

Part: ISOLATOR — CRACKED (BS 621 BULKHEAD) · airframe 29,980 hrs · 27,507 cycles

FS 621, BULKHEAD, ISOLATOR CRACKED. R & R ISOLATION MOUNTS IAW SRM 51-42-06.

Part: SKIN — DAMAGED (BS 509-605) · airframe 28,400 hrs · 25,933 cycles

DAMAGE ON FUSELAGE SKIN BETWEEN FS 509-605, S25-26R. EC/TC REO 601R-53-61-4388, REV A HAS BEEN ACCOMPLISHED.

Part: ATTACH BRACKET — CRACKED (FUSELAGE) · airframe 28,400 hrs · 25,933 cycles

CARGO TRACK UPPER CROSSBEAM AFT LOWER ATTACH BRACKET CRACKED. R & R ATTACH BRACKET IAW SRM 51-42-21 AND 51-40-11.

Part: BULKHEAD — CRACKED · airframe 28,399 hrs · 25,931 cycles

REAR PRESSURE BULKHEAD WEB FORWARD FACE IS CRACKED ABOVE CARGO DOOR. COMPLIED WITH ECTC REO 601R-53-61-1541. CLASSIFIED AS A MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (BS 364-409) · airframe 28,399 hrs · 25,931 cycles

FIRST SEGMENT OF SEAT TRACK AT RBL 9.0 FROM BS 364-409 HAS CORROSION AT MULTIPLE LOCATIONS. COMPLIED WITH ECTC REO 601R-53-00-482 FABRICATED SEAT RAILS IAW GREO 601R-53-00-485. REMOVED SEAT TRACK AT RBL 9.0 FROM FS364-409 IAW AMM 53-01-11, TASK 53-01-11-000-802. INSTALLED NEW SERVIEABLE FLOOR SEAT RAIL AT RBL 9, FS364 TO FS409 IAW AMM 53-01-11-400-802.

Part: INTERCOSTAL — CRACKED (PAX DOOR) · airframe 28,399 hrs · 25,931 cycles

INTERCOSTAL CRACKED INSIDE PAX DOOR ACCESS PANEL 832BR, UPPER FLANGE. REMOVED INTERCOSTAL IAW SRM 51-40-11 AND 51-42-06. INSTALLED INTERCOSTAL IAW SRM 51-40-11 & 51-42-06.

Part: SEAT TRACK — CORRODED (BS 364-409) · airframe 28,399 hrs · 25,931 cycles

FIRST SEGMENT OF SEAT TRACK LBL 9, BS 364-409 CORRODED. FABRICATED SEAT TRACK IAW GREO 601R-53-00-485. REMOVED SEAT TRACK BS 364 - 399 IAW SRM 51-41-02-00 AND AMM 53-01-11-000-802. INSTALLED NEW SEAT TRACK IAW AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 409) · airframe 28,399 hrs · 25,931 cycles

SECOND SEGMENT OF SEAT TRACK AT LBL 9.0 BS 409 - 409+112 CORRODED. REMOVED SEGEMENT OF SEAT TRACK IAW AMM 53-01-11-000-802. INSTALLED NEW SEGMENT OF SEAT TRACK IAW AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (409) · airframe 28,399 hrs · 25,931 cycles

SECOND SEGMENT OF SEAT TRACK AT RBL 9.0 FROM BS 409-409+112 HAS CORROSION AT MULTIPLE LOCATIONS. COMPLIED WITH ECTC REO 601R-53-00-485. REMOVED SEAT TRACK IAW AMM 53-01-11-000-802, AT RBL9 FROM 409-409+112. INSTALLED SEAT TRACK IAW ECTC REO 601R-53-00-485. COMPLIED WITH ECTC REO 601R-53-0-485 FABRICATED SEAT RAILS IAW GREO 601R-53-00-485.

Part: BULKHEAD — GOUGED (BS 621) · airframe 28,406 hrs · 25,938 cycles

THE AFT PRESSURE BULKHEAD FWD FACE AT BS 621 GOUGED. REPAIRED IAW EC/TC REO 601R-53-61-5152. REPAIR CLASSIFIED AS MAJOR.

Part: ATTACH BRACKET — CRACKED (BS 589) · airframe 28,406 hrs · 25,938 cycles

CRACKED ATTACH BRACKET BENEATH CARGO DOOR CUTOUT LOWER SILL AT FS 589 FRAME. REMOVED AND REPLACED ATTACH BRACKET IAW SRM 51-42-06-00.

Part: FRAME — CORRODED (FUSELAGE) · airframe 28,399 hrs · 25,931 cycles

FRAME BETWEEN STRINGERS 26-27L, MINOR CORROSION FOUND AROUND FASTENERS. REMOVED LIGHT CORROSION IAW SRM AND TR 53-27, FOUND OUT OF LIMITS IAW SRM TR 53-27. COMPLIED WITH EA 25-2014-004.

Part: INTERCOSTAL — CRACKED (BS 630) · airframe 28,399 hrs · 25,931 cycles

DURING INSPECTION OF THE REAR PRESSURE BULKHEAD WEB AFT SIDE, FOUND INTERCOSTAL AT BS 630, STRINGER 14R TO BE CRACKED. R & R INTERCOSTAL IAW SRM 51-42-11.

Part: BRACKET — BROKEN (RT WING) · airframe 28,399 hrs · 25,931 cycles

RT WING STUB FAIRING FWD MOUNT BRACKET BROKEN ON T/E. R & R MOUNT BRACKET IAW SRM 51-42-20-00.

Part: SKIN — CRACKED (LT WING) · airframe 28,406 hrs · 25,938 cycles

LEFT WING LOWER WING PLANK T/E CRACKED AT WS 148.019. COMPLIED WITH EC/TC REO 601R-57-21-131 AND 601R-57-21-131, REV A. COMPLIED WITH EC/TC REO 601R-57-21-130, REV K. REPAIR CLASSIFIED A MAJOR.

Part: DOOR — DAMAGED (CARGO) · airframe 28,399 hrs · 25,931 cycles

CARGO DOOR HAS A GROOVE WORN INTO IT, TOP/CENTER AREA. COMPLIED WITH GREO 601R-52-31-198. MAJOR REPAIR. COMPLIED WITH REO 601R-52-31-198 REV A DATED JAN 30,2013.

Part: HANDLE — LACK OF LUBE (PAX DOOR) · airframe 28,399 hrs · 25,931 cycles

DURING FUNCTIONAL CHECK OF THE PAX DOOR, FOUND INNER HANDLE FORCE TO UNLATCH OUT OF LIMITS. CLEANED AND LUBRICATED PAX DOOR IAW AMM 12-20-52-640-810. PERFORMED FUNCTIONAL TEST OF PAX DOOR IAW AMM 52-11-00-720-802, FOUND WITHIN LIMITS. TESTED GOOD.

Part: STRUCTURE — CRACKED (RT WING) · airframe 28,406 hrs · 25,938 cycles

RIGHT WING CRACKED AT WS 149. REPAIRED IAW EC/TC REO 601R-57-21-130 01 AND REO 601R-57-21-130, REV R. REPAIR CLASSIFIED AS MAJOR.

Part: SKIN — CRACKED (RT WING) · airframe 27,885 hrs · 25,397 cycles

RT WING CRACKED AT WS 149. REPAIRED IAW GREO 601R-57-21-138, REV A AND NDTM 51-20-08. REPAIR CLASSIFED AS MAJOR IAW GMM 5-3.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 27,885 hrs · 25,397 cycles

PAX DOOR DRAG ANGLE CRACKED. ORIGINATING FROM RIVET HOLE AND CRACK IN RADIUS , MID-POINT OF ANGLE. REPAIRED IAW REO 601R-52-11-2184, REV A.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 27,187 hrs · 24,685 cycles

EMERGENCY FLOOD LIGHT AT PAX DOOR LENS COMING OFF DUE TO BASE BEING BROKEN. R & LENS ASSY IAW AMM 33-23-02.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 25,579 hrs · 23,072 cycles

F/A FLASHLIGHT INOPERATIVE. REPAIRED F/A FLASHLIGHT IAW AMM 25-61-02. OPS CHECKED GOOD, OK FOR SERVICE.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT) · airframe 24,728 hrs · 22,164 cycles

EMERGENCY LIGHT BATTERY INOPERATIVE. EMREGENCY LIGHT SWITCH WAS LEFT IN ARM POSITION, CHARGED EMERGENCY LIGHT BATTERY IAW AMM 33-51-00. OPS CHECKED GOOD.

Part: BEAM — CORRODED · airframe 24,026 hrs · 21,393 cycles

TRANSVERSE BEAM HAS CORROSION BEYOND ALLOWABLE LIMITS AT OTBD END RBL 42, WL 73, MEASURES APPROX 2" LONG X 1" WIDE AND .012 DEEP WITH MATERIAL LOSS AT FWD OTBD CORNER OF UPPER LIP. REO 601R-53-21-2231, REV A HAS BEEN ACCOMPLISHED AND ALL STEPS HAVE BEEN DOCUMENTED AND SIGNED FOR ON A NON-ROUTINE WORK CARD.

Part: FLOOR SUPPORT — CORRODED (BS 574-621) · airframe 24,026 hrs · 21,393 cycles

THE INBD AND OTBD FLANGES OF FLOOR SUPPORT AT LBL 27 ARE CORRODED AROUND THE NUTPLATE HOLES FS 574 TO 621. REMOVED FLOOR SUPPORT IAW SRM 51-42-06, 51-42-21, 51-42-10. INSTALLED, APPLIED PAINT, AND CORROSION INHIBITOR IAW SRM 51-25-16 & 51-21-11.

Part: FLOOR SUPPORT — CORRODED (BS 574-621) · airframe 24,026 hrs · 21,393 cycles

THE INBD AND OTBD FLANGES OF FLOOR SUPPORT LBL 27 ARE CORRODED AROUND THE NUTPLATE HOLES FS 574 TO 621.

Part: SEAT TRACK — CORRODED (BS 439-499) · airframe 24,026 hrs · 21,393 cycles

RT SIDE SEAT TRACK FROM FS 439.00 TO FS 499.00 HAS AREAS OF CORROSION AROUND SCREW REO 601R-53-00-055 AND REO 601R-53-00-055, REV NL. REO 610R-53-00-055 DOES NOT ALLOW FOR FABRICATION OF WHOLE SEAT TRACK PN 601R38312-115, ITEM 3 OF MWC 8754211/106. RECEIVED NEW SEAT TRACK SECTION . R & R SEAT TRACK ON RT SIDE BS 444 - 495 IAW REO 601R-53-00-055, REV NC.

Part: BRACKET — CRACKED (BS 621 BULKHEAD) · airframe 24,026 hrs · 21,393 cycles

FS 621 BULKHEAD HAS BENT ISOLATOR BRACKETS. REMOVED ISOLATOR MOUNT BRACKETS & ISOLATORS. INSTALLED NEW ISOLATORS IAW SRM 51-42-06.

Part: FITTING — CRACKED (WINDSHIELD) · airframe 24,026 hrs · 21,393 cycles

LT/RT WINDSHIELD CENTER POST LOWER FITTINGS ARE CRACKED. DRILLED & LOCATED NEW LT & RT WINDSHIELD CENTER POST LOWER FITTINGS IAW SRM 51-40-06 & 51-40-11.

Part: POST — DAMAGED (BS 409) · airframe 24,026 hrs · 21,393 cycles

FS 409+128 VERT POST LBL 18 FAILS NDT WITH AN INDICATION IN OTBD AFT UPPER RADIUS GREATER THAN 50 PERCENT SCREEN HEIGHT. REMOVED POST ASSY IAW SRM 51-42-06. LOCATED AND DRILLED NEW POST IAW SRM 51-40-06. INSTALLED NEW SERVICABLE POST IAW SRM 51-42-06 AND REO 601R-53-41-889.

Part: SUPPORT ANGLE — CORRODED (BS 319-349) · airframe 24,026 hrs · 21,393 cycles

SERVICE DOOR CUTOUT LOWER SUPPORT ANGLE CORRODED AT SEVERAL LOCATIONS BETWEEN FS 319 AND FS 349. SERVICE DOOR CUTOUT LOWER SUPPORT ANGLE PN 601R38303-105 IS CORRODED AT SEVERAL LOCATIONS BETWEEN FS 319 AND FS 349. (CLOSED)

Part: POST — DAMAGED (BS 409) · airframe 24,026 hrs · 21,393 cycles

FS 409+128 VERT POST RBL 18 FAILS NDT WITH AN INDICATION IN OTBD AFT UPPER RADIUS GREATER THAN 50 PERCENT SCREEN HEIGHT. REMOVED POST ASSY IAW SRM 51-42-06. INSTALLED NEW SERVICEABLE POST IAW SRM 51-42-06 & REO 601R-53-41-889.

Part: BEAM — CORRODED (BS 349) · airframe 24,026 hrs · 21,393 cycles

FS 349, TRANSVERSE BEAM HAS CORROSION BEYOND ALLOWABLE LIMITS AT OTBD END RBL 42, WL 73, MEASURES APPROX 2" LONG X 1" WIDE X .012" DEEP WITH MATERIAL LOSS AT FWD OTBD CORNER OF UPPER LIP. REPAIRED IAW SRM 51-42-06, 51-42-21, 51-40-11 AND REO 601R-53-21-2231.

Part: POST — DAMAGED · airframe 24,026 hrs · 21,393 cycles

FS 409+128 VERTICAL POST BL 0 FAILS NDT WITH AN INDICATION IN RT AFT UPPER RADIUS GREATER THAN 50 PERCENT SCREEN HEIGHT. REMOVED POST IAW SRM 51-42-06. REPAIRED IAW REO 601R-53-41-889 AND SRM 51-42-06.

Part: FLOOR SUPPORT — CRACKED (BS 621) · airframe 24,026 hrs · 21,393 cycles

LEFT FS 621 FLOOR SUPPORT ANGLE IS CRACKED. REPAIRED THE DAMAGED IAW REO 601R-53-61-117

Part: ATTACH FITTING — CORRODED (FUSELAGE) · airframe 24,026 hrs · 21,393 cycles

FOUR FRAME ATTACH FITTINGS ON PAX DOOR LWR SECTION UNDER CMS 532-02 ARE CORRODED. REMOVED ATTACH FITTINGS IAW SRM 51-42-06. FOUND BEYOND LIMITS. INSTALLED FITTINGS IAW SRM 51-42-06.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 24,026 hrs · 21,393 cycles

FS 280 FLOORBEAM ANGLE CRACKED AT LBL 10 FROM MLG ALT EXT PULLEY BRACKET UPPER OTBD BOLT. REMOVED ANGLE IAW SRM 51-42-06 AND 51-42-20. INSTALLED ANGLE IAW REO 601R-53-11-926.

Part: BRACKET — CRACKED (WINDSHIELD) · airframe 24,026 hrs · 21,393 cycles

PILOT WINDSHIELD SIDE POST LOWER AFT SUPPORT BRACKET CRACKED. RECONNECTED LT WINDSHIELD HEATER POWER TERMINAL BLOCK WIRES IAW AMM 56-11-01-400-801. DISLODGED PILOT'S SIDE INSTRUMENT PANEL FOR ACCESS IAW SRM 51-44-00 AND 51-44-06. INSTALLED INSTRUMENT PANEL IAW SRM 51-44-10 & 51-44-06. REMOVED AFT LOWER WINDSHIELD POST BRACKET FOR REPLACEMENT IAW SRM 51-42-21. INSTALLED NEW WINDSHIELD POST BRACKET IAW SRM 51-42-21. THIS REPAIR REQUIRES MAJOR/MINOR CLASSIFICATION IAW ASA SOP 5702. THIS REPAIR IS CLASSIFIED AS A MINOR REPAIR IAW ASA SOP 5702. AFT LOWER WINDSHIELD POST BRACKET REQUIRES PRIMER AND DINITROL. APPLIED PRIMER TO WINDSHIELD POST BRACKET IAW SRM 51-25-06 AND DYNATROL IAW SRM 51-21-11. OPS TET OF THE WINDSHIELD TEMP CONTROLLERS REQUIRED. REF AMM 30-41-01-710-801. OPS TEST GOOD IAW AMM 30-41-01-710-801. (SDR CLOSED)

Part: SEAT TRACK — CORRODED (BS 439-499) · airframe 24,026 hrs · 21,393 cycles

RT SIDE SEAT TRACK FS 439 TO 499 CORRODED. REMOVED SEAT TRACK SEGMENT IAW AMM 53-1-11-000-802. DRILLED, COUNTERSUNK NEW SEAT TRACK IAW REO 601R-53-00-055. INSTALLED SEAT TRACK IAW REO 601R-53-00-055.

Part: ATTACH FITTING — CRACKED (BS 484) · airframe 24,026 hrs · 21,393 cycles

FS 484 INTERCOSTAL INBD CLIP CRACKED ON OTBD SIDE OF LBL 27 PRESSURE FLOORBEAM. R & R INBD CLIP IAW SRM 51-42-06 & 51-42-21. THIS REPAIR REQUIRES MAJOR/MINOR CLASSIFICATION IAW ASA SOP 5702. THIS REPAIR IS CLASSIFIED AS A MINOR REPAIR IAW ASA SOP 5702. (SDR CLOSED)

Part: ANGLE — CRACKED (BS 621-625) · airframe 24,026 hrs · 21,393 cycles

LEFT UPPER FS 621 TO FS 625 OBLIQUE ANGLE IS CRACKED. R & R ANGLE IAW SRM 51-42-21 AND 51-25-16.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 24,026 hrs · 21,393 cycles

FS 280, LBL 9 OTBD FLOORBEAM CLIP IS CRACKED IN UPPER PANELS. REPAIRED.

Part: FLOORBEAM — CRACKED (BS 460) · airframe 24,026 hrs · 21,393 cycles

FS 460 SUPPORT ON OTBD SIDE OF RBL 9 PRESSURE FLOORBEAM IS CRACKED. REMOVED CRACKED SUPPORT FITTING IAW SRM 51-42-06, 51-42-21 & 51-40-11. INSTALLED NEW SUPPORT IAW SRM 51-42-06 & 51-42-21.

Part: ATTACH FITTING — CRACKED · airframe 24,026 hrs · 21,393 cycles

FS 484 INTERCOSTAL INBD AND OTBD CLIPS ARE CRACKED BETWEEN RBL 27 AND RBL 36 PRESSURE FLOORBEAMS. R & R IAW SRM 51-42-06 AND SRM 51-42-21.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 22,761 hrs · 19,995 cycles

FLOOR LEVEL EMERGENCY FLOOD LIGHT MISSING COVER. REMOVED AND REPLACED FLOOR LEVEL EMERGENCY FLOOD LIGHT ASSY IAW AMM 33-51-19, OP CK'S GOOD NO DEFECTS NOTED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,069 hrs · 19,187 cycles

LT EXT EMERGENCY LIGHT (NR 7) WILL NOT ILLUMINATE WHEN COMMANDED. RESOLVED ON W/O: 179683 TASKCARD: N/R-00007. REMOVED AND REPLACED LT EXT EMERGENCY LIGHT (NR 7) LAMP IAW CRJ 200 AMM 33-51-21. OPS CHECK GOOD. REMOVED AND REPLACED LT EXT EMERGENCY LIGHT (NR 7) LAMP IAW CRJ 200 AMM 33-51-21. OPS CHECK GOOD.

Part: WIRE — DAMAGED (EMERGENCY LIGHTS) · airframe 21,911 hrs · 19,011 cycles

RT EMERGENCY EXIT SIGN AT ROW 8CD INOP. REPAIRED DEFECTIVE SPLICE ON RT EMERGENCY EXIT SIGN FIXTURE AT ROW 8CD IAW ESPM 20-17-10, OPS CHECK GOOD. REPAIRED DEFECTIVE SPLICE ON RT EMERGENCY EXIT SIGN FIXTURE AT ROW 8CD IAW ESPM 20-17-10, OPS CHECK GOOD. (CLOSED)

Part: FIRE BOTTLE — LOW (CARGO BAY) · airframe 20,907 hrs · 17,877 cycles

CARGO BOTTLE LOW ILLUMINATED. REMAINED ON 10 TO 15 MIN. AND THEN EXTINGUISHED. (EMERGENCY DECLARED) (CARGO COMPARTMENT FIRE EXTINGUISHING SYSTEM) R & R LRD CARGO FIRE BOTTLE IAW AMM 26-25-01. OPS CHK GOOD. (CLOSED)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 20,589 hrs · 17,521 cycles

FOUND SECTION OF EMERGENCY LIGHTS INOP. REMOVED AND REPLACED NO. 3 EMERGENCY LIGHT BATTERY PACK IAW AMM 33-51-04 OPS CHK GOOD.

Part: LIGHT — BROKEN (CABIN) · airframe 19,787 hrs · 16,648 cycles

EMERGENCY AREA FLOOD LIGHT ON BOTTOM OF FA STATION IS BROKEN. REMOVED AND REPLACED F/A STATION FLOOD LIGHT IAW MM 33-51-19-000-81 NO DEFECTS NOTED.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 19,787 hrs · 16,648 cycles

CORROSION DAMAGE ON MAIN AVIONICS DOOR CUTOUT SUPPORT FRAME FS 349.00 TO FS 364.00 BETWEEN STR 26 LT AND STR 27 (MARKED). REMOVED CORROSION ALODINED & PRIMED RESHOT RIVETS TOP COAT & CIC PER CRJ 200 SRM 51-21-06, 51-42-06 & 51-25-02. REMOVED RIVETS CAUSE OF CORROSION DAMAGE AT MAIN AVIONICS DOOR CUT OUT SUPPORT FRAME FS 349.00 TO FS 364.00 BETWEEN STR 26LT AND STR 27 IAW CRJ 200 51-21-06 AND 51-42-06. ALL CORROSION DAMAGE ON FRAME FS 349.00 TO 364.00 BETWEEN STR 26LT AND STR 27 NOT REMOVED IAW CRJ 200 SRM 51-21-06. REMOVED REST OF CORROSION, ALODINED PRIMED, SHOT IN RIVETS & PAINT TOP COAT & CIC PER CRJ 200 SRM 51-21-06, 51-42-06, AND 51-25-02.

Part: FRAME — CORRODED (BS 364)

CORROSION DAMAGE ON FS 364.00 FRAME FROM STR 26 LT TO STR 25 RT. REMOVED RIVETS & T FITTING CLEANED UP MINOR CORROSION ALODINED & PRIMED SHOT IN RIVETS & INSTALLED T FITTING PER SRM 51-21-06, 51-42-06, AND 51-25-02. REMOVED RIVETS ON FS 364.00 FRAME CAUSE OF CORROSION DAMAGE IAW SRM 51-21-06 AND 51-42-06. ALL CORROSION DAMAGE ON FS 364.00 FRAME FROM STR 26 LT TO STR 25 RT NOT REMOVED IAW SRM 51-21-06. CLEANED UP CORROSION ALODINED & PRIMED RESHOT RIVETS INSTLALLED T FITTING TOP COAT & CIC PER SRM 51-21-06/ 51-42-06/ 51-25-02.

Part: FRAME — CRACKED (FUSELAGE) · airframe 19,787 hrs · 16,648 cycles

IN REFERENCE TO TASK CARD AWL2 53-41-201, FRAME CAP ANGLE IS CRACKED AT LBL 18.0 ON OUTBOARD SIDE AT FS 559.00. REPAIRED IAW REO 601R-53-41-1044.

Part: CARGO TRACK — CORRODED (BS 559-570)

CORROSION DAMAGE ON FLOOR TRACK IN CARGO COMPT FS 559.0+112 TO 570.0 AT LBL 9.0 (MARKED). REMOVED AND REPLACED CORRODED TRACK PER AMM 53-01-11.

Part: CARGO TRACK — CORRODED (BS 559) · airframe 19,787 hrs · 16,648 cycles

CORROSION DAMAGE ON FLOOR TRACK IN CARGO COMPT FS 559.0+86 TO 559.0+96 AT RBL 9.0 (MARKED). REMOVED AND REPLACED CORRODED TRACK PER AMM 53-01-11.

Part: CARGO TRACK — CORRODED (BS 559-570) · airframe 19,787 hrs · 16,648 cycles

CORROSION DAMAGE ON FLOOR TRACK IN CARGO COMPT FS 559.0+112 TO 570.0 AT RBL 9.0 (MARKED). REMOVED AND REPLACED CORRODED TRACK PER AMM 53-01-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 19,787 hrs · 16,648 cycles

CORROSION AROUND NUT PLATE ON RT FLOOR LANDING FS 559.0+112 AT APPROX RBL-40. REMOVED CORROSION EDDY CURRENT CHECKED AREA, REPLACED RIVETS IN NUT PLATE ALODINE AND PRIMED AREA PER REO 601R-53-51-094.

Part: ANGLE — CRACKED (BS 625) · airframe 19,787 hrs · 16,648 cycles

RIGHT 625 AFT BULKHEAD ANGLE CRACKED AT STRINGER 14. REMOVED AND REPLACED THE RIGHT BULKHEAD ANGLE AT FS 625, STR 14 IAW SRM 51-42-21.

Part: CARGO TRACK — CORRODED (BS 559) · airframe 19,787 hrs · 16,648 cycles

CORROSION DAMAGE ON FLOOR TRACK IN CARGO COMPT FS 559.0+80 TO 559.0+96 AT RBL 27.0 (MARKED). REMOVED AND REPLACED CORRODED TRACK PER AMM 53-01-11.

Part: ANGLE — CRACKED (BS 625) · airframe 19,787 hrs · 16,648 cycles

LEFT 625 AFT BULKHEAD ANGLE CRACKED AT STRINGER 14. REMOVED AND REPLACED THE LEFT BULKHEAD ANGLE, FS 625 IAW SRM 51-42-21.

Part: CARGO TRACK — CORRODED (BS 615) · airframe 19,787 hrs · 16,648 cycles

CORROSION DAMAGE ON FLOOR TRACK IN CARGO COMPT FS 615.00 AT LBL 9.0 (MARKED). REMOVED AND REPLACED CORRODED TRACK PER AMM 53-01-11.

Part: FRAME — CORRODED (BS 333) · airframe 19,787 hrs · 16,648 cycles

CORROSION AT FS 333.0 AND BL 0.0. FRAME REMOVED AND REPLACED PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 19,787 hrs · 16,648 cycles

AFT PRESSURE BULKHEAD SKIN IS CRACKED AT LINTEL ATTACH POINT ABOVE LINTEL. REPAIR PER EC/TC REO 601R-53-61-1230 HAS BEEN COMPLETE AND THE REPAIR COMPLIES WITH THE REQUIREMENTS OF EC/TC AND REO 601R-53-61-1230 REV. D.

Part: RIB — CRACKED (BATTERY) · airframe 19,787 hrs · 16,648 cycles

RIGHT BATT RIB IS CRACKED. COMPLIED WITH REO 601R-57-51-046.

Part: DRAG ANGLE — CRACKED (ASD) · airframe 19,787 hrs · 16,648 cycles

ASD AFT SIDEWALL LOWER DRAG ANGLE CRACKED.

Part: LIGHT — BROKEN (CABIN) · airframe 19,787 hrs · 16,648 cycles

EMERGENCY LIGHT BROKEN AT SERVICE DOOR. REMOVED AND REPLACED EMERGENCY LIGHT ASSY IAW MM 33-51.

Part: OIL SYSTEM — MALFUNCTIONED (LEFT) · airframe 19,644 hrs · 16,484 cycles

FROM CLIMB AROUND 7500 FT LEFT OIL PRESSURE WENT TO RED INDICATION THEN BACK TO NORMAL LEFT DIPPING AND SPIKING TO NORMAL RANGE LOWS AROUND 30 PSI WITH CONSISTENT JUMPS TO 45-60 CONSTANTLY DIPPING AND SPIKING WITH ONE READING 25 PSI. RETURNED TO ATL. AIRCRAFT RETURNED TO ATL AFTER T/O, EMERGENCY DECLARED & EMERGENCY VEHICLES ROLLED AS A PRECAUTION. FLT 5461 DEL 187 MINS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,496 hrs · 16,327 cycles

CABIN EXIT SIGN FWD SECTION HAS BULBS BURNED OUT.

Part: STEP — CRACKED (ASD) · airframe 18,115 hrs · 15,057 cycles

ASD LOWER STEP CRACKED.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 16,052 hrs · 13,281 cycles

NR 1 EMERGENCY LIGHTING BATTERY PACK IS INOP.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 15,989 hrs · 13,225 cycles

FO'S FLASHLIGHT INOP.

Part: DOOR — MALFUNCTIONED (SERVICE DOOOR) · airframe 15,322 hrs · 12,691 cycles

SERVICE DOOR WILL NOT CLOSE.

Part: INTERCOSTAL — CRACKED (BS 484) · airframe 15,218 hrs · 12,609 cycles

RIGHT FS 484 INTERCOSTAL ANGLE CRACKED AT RBL 36.0. REMOVED CRACKED ANGLE AT RBL 36.0 FS RIGHT 484. DUPLICATED ANGLE FROM 2024-T3, .063 IAW REO 601R-53-41-059. ALODINED, PRIMED, AND PAINTED ANGLE AND INSTALLED ANGLE IAW REO 601R-53-41-059. PERFORMED PRESSURIZATION LEAK CHECK IAW CRJ AMM 21-31-00. NO DEFECTS NOTED. SUPPLEMENTAL - SDR CLOSED 07/17/07.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 15,218 hrs · 12,609 cycles

COCKPIT FLOORBOARD SUPPORT ANGLE AT FS 280 HAS CORROSION. UPON FURTHER INVESTIGATION OF COCKPIT FLOORBOARD SUPPORT ANGLE AT FS 280 HAS MINOR SURFACE CORROSION. REMOVED MINOR CORROSION FROM ANGLE, IAW CRJ SRM 51-21-06. ALODINED, PRIMED AND TOPCOATED, IAW CRJ SRM 51-21-16. REMOVED COCKPIT FLOORBOARD SUPPORT ANGLE AT FS 280, TO PERFORM THE ABOVE CORRECTIVE ACTION. 07/05/07 INSTALLED COCKPIT FLOORBOARD SUPPORT, IAW CRJ SRM 51-42-06. 07/12/07 MINOR SURFACE CORROSION WITHIN SERVICEBLE LIMITS, IAW CRJ SRM 53-11-43. 07/12/07 SUPPLEMENTAL - SDR CLOSED 07/16/07.

Part: WEB — CORRODED (BS280) · airframe 15,218 hrs · 12,609 cycles

FS 280 WEB HAS CORROSION NEAR BL 0.0. REPAIRED DAMAGE TO 280 WEB, IAW ASA REO 601R-53-11-926. INSTALLED ALL FASTENERS, EXCEPT 8 JO-BOLTS IN -1 AND -2 WEB SPLICES. 07/12/07 INSTALLED REMAINING 8 JO-BOLTS, 4 AT LBL 9.00 FS 280.00 AND 4 AT RBL 9.00 FS 280.00. INSTALLATION OF JO-BOLTS, IAW CRJ 200 SERIES SRM 51-23-00 AND 51-42-22. SUPPLEMENTAL - SDR CLOSED 07/17/07.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 15,218 hrs · 12,609 cycles

FS 280 FLOORBEAM ANGLE AT LBL 9.0 I/B CRACKED. REMOVED DAMAGED FLOORBEAM ANGLE, DUPLICATED PART FROM 2024-T3 .050, PO 950029 AND INSTALLED NEW SERVICEABLE ANGLE, IAW CRJ SRM 51-24-16 AND 51-42-21. 07/12/07 DUPLICATED PART, IAW AND IN CONJUNCTION WITH REO 601R-53-11-926 B. SUPPLEMENTAL - SDR CLOSED 07/16/07.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 15,218 hrs · 12,609 cycles

FS 280 FLOORBEAM ANGLE AT RBL 9.0 I/B CRACKED. REMOVED DAMAGED FLOORBEAM ANGLE, DUPLICATED PART FROM 2024-T3 .050, PO 950029 AND INSTALLED NEW SERVICEABLE ANGLE, IAW CRJ SRM 51-24-16 AND 51-42-21. 07/12/07 DUPLICATED PART, IAW AND IN CONJUNCTION WITH REO 601R-53-11-926 B. SUPPLEMENTAL - SDR CLOSED 07/16/07.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 15,218 hrs · 12,609 cycles

FS 280 FLOORBEAM ANGLE AT RBL 9.0 O/B CRACKED. REMOVED DAMAGED FLOORBEAM ANGLE, DUPLICATED PART FROM 2024-T3 .050, PO 950029 AND INSTALLED NEW SERVICEABLE ANGLE, IAW CRJ SRM 51-24-16 AND 51-42-21. 07-12-07. DUPLICATED PART, IAW AND IN CONJUNCTION WITH REO 601R-53-11-926-B. SUPPLEMENTAL - SDR CLOSED 07/16/07.

Part: DOOR — STIFF (MAIN PAX) · airframe 14,743 hrs · 12,239 cycles

CREW REPORTS PAX DOOR HARD TO OPEN.

Part: CAUTION MESSAGE — ILLUMINATED · airframe 13,534 hrs · 11,375 cycles

R FIRE FAIL" CAUTION MESSAGE APPEARS INTERMITTENTLY DURING DESCENT, FLT 4559 CX AND ON 11/4/06 FLT 4692 CX.

Part: FIRE WARNING — ILLUMINATED · airframe 13,471 hrs · 11,326 cycles

INTERMITTENT RIGHT FIRE FAIL MSG IN FLT.

Part: FIRE WARNING — FALSE ACTIVATION (RT NACELLE) · airframe 13,479 hrs · 11,332 cycles

INTERMITTENT RT FIRE FAIL MSG IN FLT.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 13,054 hrs · 11,025 cycles

LEFT LOWER EXIT LIGHT COVER MISSING NEAR PAX DOOR.

Part: APU — SMOKE · airframe 12,859 hrs · 10,870 cycles

DURING APU START , SMOKE CAME OUT OF APU, SHUT APU DOWN AND BLEW FIRE BOTTLE

Part: WARNING SYSTEM — ACTIVATED (HYDRAULIC SYS) · airframe 12,824 hrs · 10,846 cycles

AT FL 250, NR 2 HYD LOW PRESS MSG FOLLOWED QRH. TURNED OFF NR 2 ELEC PUMP NR 2 QTY 5 PERCENT. PRESS DROPPED TO 800-1200 PSI. RAN LIKE THAT FOR 22 MINUTES. NR 2 HYD TEMP WENT TO ABOUT 50 C. EN ROUTE TO ILM, A/C DIVERTED TO CAE DUE TO MTC. DECLARED AN EMERGENCY, FLT 4425 CX.

Part: LIGHT — INOPERATIVE (FUSELAGE) · airframe 12,292 hrs · 10,423 cycles

LT OVERWING WXIT FWD EXT EMERGENCY LIGHT INOP.

Part: FCU — MALFUNCTIONED (TE FLAPS)

DURING CRUISE, THE CREW RECEIVED A FLAPS FAIL INDICATION. AFTER COMPLYING WIT THE QRH THE FLIGHT CONTINUED. AN EMERGENCY WAS DECLARED. THE AIRCRAFT LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE ELECTRONIC FLAP CONTROL UNIT (FECU). OPS CHECK OF THE FLAP SYSTEM IAW 27-51-05 WAS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: SILL — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE CARGO BAY FLOOR SILL AT FS 562.72-589 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CARGO BAY FLOOR SILL AT FS 582.72-589 IAW ASA EO 600-53-0095. (M)

Part: FLOOR SUPPORT — CRACKED (FUSELAGE)

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

Part: INTERCOSTAL — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE LEFT AND RIGHT INTERCOSTALS AT FS 484, BL 27 TO 36 ON THE OUTBOARD SIDE WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE LEFT AND RIGHT INTERCOSTALS AT FS 484, BL 27 TO 36 ON THE OUTBOARD SIDE IAW ASA EO 600-53-0098. (M)

Part: ANGLE — CRACKED (FUSELAGE)

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

Part: CLIP — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE INBOARD AND OUTBOARD CLIPS AT FS 280, LBL 9 AND RBL 9 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE INBOARD AND OUTBOARD CLIPS AT FS 280, LBL 9 AND RBL 9. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DURING HANGER MAINTENANCE, THE FORWARD EMERGENCY CEILING LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD EMERGENCY CEILING LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK THE SERVICE.

Part: DOUBLER — CRACKED (FUSELAGE)

DURING AN A-CHECK IN BTR, THE DOUBLER AT FS 640, STRINGER L10 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE DOUBELR AT FS 640, STRINGER L10 IAW SRM 51-00. (M)

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

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

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

FLT 4382 - DURING A GROUND INSPECTION IN MGM, THE EMERGENCY CEILING LIGHT AT ROW TEN WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY CEILING LIGHT LAMP AT ROW TEN. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: CONNECTOR — DISCONNECTED (CABIN)

DURING A GROUND INSPECTION IN ATL, THE EMERGENCY FLOOR LIGHTS BETWEEN ROWS ONE TO FIVE WERE FOUND TO BE INOPERATIVE. MAINTENANCE RECONNECTED THE EMERGENCY FLOOR LIGHTS BETWEEN ROWS ONE TO FIVE. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: BULB — BURNED OUT (EMERGENCY LIGHT)

FLT 4611 - DURING A GROUND INSPECTION IN DFW, THE NR 5 EXTERIOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 5 EXTERIOR EMERGENCY LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: ACM — FAILED (ACM BAY)

ON TAXI OUT OF GSP THE CABIN FILLED WITH SMOKE. THE AIRCRAFT WS EVACUATED ON THE TAXIWAY THROUGH THE PASSENGER DOOR AND THE OVERWING EMERGENCY EXITS. THE CAPTAIN DID NOT RECEIVE ANY FAULT WARNINGS OR MESSAGES. MAINTENANCE REMOVED AND REPLACED THE RIGHT ACM. THE FAILED ACM HAD NO ROTATION OF THE COMPRESSOR OR TURBINE. THIS ALLOWED HOT BLEED AIR TO ENGER THE CABIN. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: BULB — BURNED OUT (FUSELAGE)

DURING GROUND INSPECTION IN ATL, THE LEFT OVERWING EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BURNED OVERWING EMERGENCY LIGHT BULB. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)