N834AS

Part: SKIN — CRACKED (LT WING) · airframe 36,665 hrs · 31,954 cycles

SMALL CRACK IN LT LOWER WING PLANK STA 148. REPAIRED IAW REO 601R-57-51-660 AND REO 601R-57-21-130.

Part: BULKHEAD — CRACKED (BS 280) · airframe 36,665 hrs · 31,954 cycles

BULKHEAD AT FS 280, LBL 28, WL 85.50 HAS STANDOFF, BROKEN OFF WITH RIVET PULLED THROUGH AND HAS A CRACK EXTENDING 1" FROM HOLE. REMOVED DAMAGE IAW REO 601R-53-11-2566. FABRICATED AND INSTALLED REPAIR PARTS IAW REO 601R-53-11-2566.

Part: ANGLE — CRACKED (BS 605) · airframe 36,650 hrs · 31,938 cycles

ANGLE LBL 45 AT BS 605 ANGLE CRACKED AT FRAME. REMOVED CRACKED ANGLE AND REPLACED WITH NEW. LOCATED AND DRILLED FRAME ANGLE SECTION IAW SRM 51-42-21. LOCATED AND DRILLED ANGLE IAW SRM 51-40-06 AND SRM 51-40-11.

Part: SKIN — CRACKED (RT WING) · airframe 36,665 hrs · 31,954 cycles

RIGHT LOWER WING PLANK BOOST PUMP LANDING FOR PANEL 610CB HAS MULTIPLE INDICATIONS NOTED ON HORZ AND VERT SURFACES GREATER THAN 50 PERCENT FSH AROUND ENTIRE CIRCUMFERENCE. FAILED NDT INSPECTION. COMPLIED WITH REO 601R-57-21-2003.

Part: BULKHEAD WEB — CRACKED · airframe 36,665 hrs · 31,954 cycles

FOUND REAR PRESSURE BULKHEAD WEB HAS INDICATIONS NOTED AT LBL 36.20 APPROX WL 79 TO WL 81 2" IN LENGTH 100 PERCENT FSH. FAILED NDT INSPECTION. REPAIRED IAW REO 601R-53-61-5030.

Part: SKIN — DENTED (FUSELAGE) · airframe 36,650 hrs · 31,938 cycles

FUSELAGE SKIN AT FWD LOWER CORNER OF PAX DOOR SURROUND IS DENTED APPROX 1 L X .50 W X .30 D. CUT AWAY DAMAGED SKIN AT PAX DOOR CUTOUT OF FWD LWR CORNER IAW SRM 53-21-31, REPAIR NR 1, STEP 5, A1. COMPLIED WITH EC/TC SRM 53-21-31-01. FABRICATED DOUBLER AND FILLER IAW SRM 53-21-31. MAJOR REPAIR.

Part: BULKHEAD WEB — CORRODED · airframe 36,665 hrs · 31,954 cycles

FOUND REAR PRESSURE BULKHEAD WEB HAS INDICATIONS NOTED AT BL 0.0 APPROX WL 89 TO WL 113 24" IN LENGTH 100 PERCENT FSH. FAILED NDT INSPECTION. REPAIRED IAW SRM CH 51-42-06 AND REO 601R-53-61-5034, REV 2013-09-27.

Part: HINGE — CHAFED (PAX DOOR) · airframe 36,672 hrs · 31,962 cycles

PASSENGER DOOR HINGE ON FUSELAGE SIDE HAS (1 EA) LUG CHAFED APPROXIMATELY .003" DEEP ON LUG NR 13 COUNTING FROM FRONT TO BACK AND HINGE IS CHAFED APPROXIMATELY .045" DEEP AFT OF LUG NR 27 FROM CONTACT WITH HINGE PIN SPRING PIN. COMPLIED WITH REO 601R-53-21-814 REV, TYPE I AND TYPE IV.

Part: ANGLE — CRACKED (BS 625) · airframe 36,648 hrs · 31,936 cycles

IN AFT EQUIPMENT COMPARTMENT AT FS 625.00, BL 45.00, STRINGER 14L AND AT WL 97.5 THE LT INTERCOSTAL, OBLIQUE, ANGLE IS CRACKED APPROX 1.1 LONG. REMOVED DAMAGED CLIP FROM FS 625, STR 14L AND INSTALLED NEW CLIP, PN 601-35012-1 IAW SRM 51-42-21.

Part: FLOOR SUPPORT — CORRODED (BS 280-319.7) · airframe 36,648 hrs · 31,936 cycles

IN PASSENGER COMPARTMENT BETWEEN FS 280 TO 319.7 ON RBL 36.00 FLOOR SUPPORT AT SEVERAL LOCATIONS IS CORRODED. REPAIRED IAW REO 601R-53-00-530.

Part: FLOORBEAM — CORRODED (BS 409) · airframe 36,665 hrs · 31,954 cycles

IN PASSENGER COMPARTMENT BETWEEN FS 409.00 RBL 9.00 THE FLOORBEAM ATTACHMENT HOLES FOR THE FLOORBOARD ARE CORRODED. REMOVED FLOORBEAM CAP IAW SRM'S 51-42-06 AND 51-42-34 AND 51-42-21. LOCATED, TRIMMED, DRILLED REPLACEMENT FLOORBEAM SECTION IAW SRM 51-40-11, 51-24-36. INSTALLED REPLACEMENT SECTION OF FLOORBEAM IAW REO 601R-53-31-801.

Part: SEAT TRACK — CORRODED (BS 364-398) · airframe 36,648 hrs · 31,936 cycles

IN PASSENGER COMPARTMENT BETWEEN FS 364 - 398 ON RBL 9.00 THE SEAT TRACK IS CORRODED AT SEVERAL LOCATIONS. REMOVED SEAT TRACK FS 364.00 TO FS 398.00, RBL 9 IAW AMM 53-01-11-000-812. INSTALLED NEW SERVICEABLE PASSENGER SEAT TRACK FROM FS 364.00 -FS 398.00, RBL 9.00 IAW AMM 53-01-11-400-802. FABRICATED SEAT RAILS IAW GREO 601R-53-00-485.

Part: ISOLATOR — CRACKED (BULKHEAD) · airframe 36,648 hrs · 31,936 cycles

CARGO AFT BULKHEAD HAS ONE BROKEN ISOLATOR UNDER PANEL 281GLW. R & R BROKEN ISOLATOR WITH A SERVICEABLE ISOLATOR IAW SRM 51-42-13 AND SRM 51-42-10.

Part: ISOLATOR — CRACKED (BULKHEAD) · airframe 36,648 hrs · 31,936 cycles

CARGO AFT BULKHEAD HAS ONE BROKEN ISOLATOR UNDER PNL 281FLW. R & R BROKEN ISOLATOR WITH SERVICEABLE ISOLATOR IAW SRM 51-42-10 AND SRM 51-42-13.

Part: FLOOR SUPPORT — CORRODED (BS 449.85) · airframe 36,648 hrs · 31,936 cycles

IN PASSENGER COMPARTMENT AT FS 449.85 ON LBL 36.00 THE FLOOR SUPPORT IS CORRODED. COMPLIED WITH EC/TC REO 601R-53-41-666 AND REO 601R-53-41-666, REV C.

Part: SEAT TRACK — CORRODED (BS 348-409) · airframe 36,665 hrs · 31,954 cycles

IN PASSENGER COMPARTMENT BETWEEN FS 348.00 TO 409.00+116 ON RBL 9.00 THE SEAT TRACK IS CORRODED AT SEVERAL LOCATIONS. REMOVED CORRODED SEAT TRACK FROM RBL 9.00 BETWEEN FS 398.00-FS 409.00+116 IAW SRM 51-41-02. INSTALLED FABBED SEAT TRACK AT RBL 9.0 BETWEEN FS 298.00 TO FS 409.00+116 IAW AMM TASK 53-01-11-400-802. FABRICATED SEAT RAILS IAW GREO 601R-53-00-485.

Part: BULKHEAD WEB — GOUGED (AFT FUSELAGE) · airframe 36,672 hrs · 31,962 cycles

REAR PRESSURE BULKHEAD FWD FACE ABOVE FLOOR HAS SEVERAL GOUGES RANGING FROM .003 TO .010 DEEP. BLENDED GOUGES IAW STEP NR 1 OF REO 601R-53-61-2155.

Part: SEAT TRACK — CORRODED (BS 364-398) · airframe 36,648 hrs · 31,936 cycles

IN PASSENGER COMPARTMENT BETWEEN FS 364 TO 398 ON LBL 9.00 THE SEAT TRACK IS CORRODED AT SEVERAL LOCATIONS. REMOVED SEAT TRACK. LOCATED & DRILLED SERVICEABLE SEAT TRACK, PN N126-2075, PO W/12366 IAW SRM 51-40-11 & SRM 51-40-06. SEAT TRACK INSTALLED AS REQUIRED ON LT SIDE BETWEEN FS 364.00 & FS 398.00 IAW AMM 53-01-11-400-802. FABRICATED SEAT RAILS IAW GREO 601R-53-00-485.

Part: ATTACH ANGLE — CRACKED (BS 280) · airframe 36,665 hrs · 31,954 cycles

IN PASSENGER COMPARTMENT AT FS 280.00 ON RBL 9.00 THE ATTACHMENT ANGLE IS CRACKED (RT). REMOVED DAMAGED CLIP FROM FS 280 ON RBL 9 OTBD PREVIOUSLY INSTALLED IAW REO 601R-53-11-640. FABRICATED CLIP, PN 601R-53-11-640-2, REF REO 601R-53-11-640 FOR MAT SPEC. LOCATED, DRILLED AND INSTALLED CLIP IAW SRM 51-40-11 AND 51-41-21. CLIP FABBED FROM S6144-13, POS13751.

Part: ANGLE — CORRODED · airframe 36,665 hrs · 31,954 cycles

IN PASSENGER COMPARTMENT AT FS 280.00 BETWEEN LBL 9.00 TO RBL 9.00 THE TRANSVERSE BEAM TOP ANGLE IS CORRODED. REMOVED CORRODED ANGLE IAW SRM 51-42-06. LOCATED AND INSTALLED NEW FS 280 FILLER BETWEEN LBL 9 AND RBL 9 IAW REO 601R-53-11-136. COMPLIED WITH EC/TC EO 600-53-91 AND REO 601R-53-11-136, REV A.

Part: SEAT TRACK — CORRODED (BS 409-559) · airframe 36,648 hrs · 31,936 cycles

IN PASSENGER COMPARTMENT BETWEEN FS 409.00+116 TO FS 559.00+5 ON RBL 9.00 THE SEAT TRACK IS CORRODED AT SEVERAL LOCATIONS. REMOVED SEAT TRACK 3X RING HARDWARE. INSTALLED NEW SERVICEABLE SEAT TRACK, PN N126-2075 IAW AMM 53-01-11-900-802. DRILLED NEW SEAT TRACK IAW REO 601R-53-00-485. FABRICATED SEAT RAILS IAW GREO 601R-53-00-485.

Part: POST — CRACKED (BS 409) · airframe 36,650 hrs · 31,938 cycles

FOUND FS 409+128, VERTICAL POST RBL 18.0 INBD AND OTBD SIDES HAVE CRACK INDICATIONS NOTED APPROX .2 INCHES IN LENGTH 50 PERCENT AND 100 PERCENT FSH. FAILED NDT INSPECTION AT AFT FLANGE RADIUS. REMOVED VERTICAL POST IAW SRM 51-42-06. INSTALLED NEW POST IAW SRM 51-42-00 AND REO 601R-53-41-889.

Part: POST — CRACKED (BS 409) · airframe 36,650 hrs · 31,938 cycles

FOUND FS 409+128 VERTICAL POST LBL 18.0 INBD AND OTBD SIDES HAVE CRACK INDICATIONS NOTED APPROX .2 INCHES IN LENGTH 60 PERCENT FSH AT AFT FLANGE RADIUS. FAILED NDT INSPECTION. REMOVED VERTICAL POST IAW SRM 51-42-06. INSTALLED NEW VERTICAL POST IAW SRM 51-42-06 & REO 601R-53-41-889.

Part: ANGLE — CRACKED (BS 484) · airframe 36,648 hrs · 31,936 cycles

IN PASSENGER COMPARTMENT AT FS 484.00 RBL 27.00 THE INTERCOSTAL REPAIR ANGLE IS CRACKED. R & R INTERCOSTAL ANGLE, PN 601R31171-9 FS 484.00, RBL 27.00 IAW SRM 51-42-06 & 51-42-21.

Part: FLOOR SUPPORT — CORRODED (BS 319) · airframe 36,648 hrs · 31,936 cycles

IN PASSENGER COMPARTMENT AT FS 319.00 ON RBL 36 THE SERVICE DOOR CUTOUT FLOORBOARD ATTACHMENT ANGLE IS CORRODED. RT FLOOR SILL SUPPORT BETWEN FS 310 AND FS 319 CORRODED BEYOND LIMITS. REPLACEMENT REQUIRED. INSTALLED NEW FWD RT SUPPORT ANGLE, PN 601R31148-79 AT RBL 36.00, FS 310-319.0 IAW SRM 51-42-06.

Part: FLOORBEAM — CORRODED (BS 349) · airframe 36,650 hrs · 31,938 cycles

IN PASSENGER CABIN FS 349 BETWEEN LBL 27 TO 36, FLOORBEAM TOP CAP IS CORRODED. REMOVED ANGLE IAW SRM 51-42-06. INSTALLED NEW ANGLE IAW SRM 51-42-06, 51-42-21 AND AMM 51-23-00-390-802.

Part: SKIN — CORRODED (RT WING) · airframe 36,665 hrs · 31,954 cycles

RT WING PLANK ACCESS HOLE 640AB LIP HAS SEVERAL AREAS OF PITTING/CORROSION. REPAIRED IAW REO 601R-57-21-030.

Part: FLOOR SUPPORT — CORRODED (CARGO BAY) · airframe 36,665 hrs · 31,954 cycles

IN CARGO BAY BETWEEN FS 574.00 TO 621.00 ON LBL 36.00 THE CARGO DOOR CUTOUT FLOOR SUPPORT AROUND FLOORBOARD ATTACHMENT HOLES IS CORRODED. REMOVED CORRODED CARGO COMPARTMENT FLOOR SUPPORT IAW SRM 51-42-06 AND 51-42-21. INSTALLED NEW CARGO COMPARTMENT FLOOR SUPPORT IAW SRM 51-42-06 AND SRM 51-42-21 AND REO 601R-53-61-1574.

Part: FLOOR SUPPORT — CORRODED (BS 574-621) · airframe 36,648 hrs · 31,936 cycles

IN CARGO BAY BETWEEN BS 574 - 621 LBL 27 FLOOR SUPPORT AROUND ATTACHMENT HOLES CORRODED. REMOVED FLOOR SUPPORT IAW SRM 51-42-06 AND SRM 51-42-21. LOCATED AND DRILLED NEW SERVICEABLE FLOOR SUPPORT IAW SRM 51-40-11. INSTALLED FLOOR SUPPORT IAW REO 601R-53-61-3778.

Part: FLOOR SUPPORT — CORRODED (BS 559) · airframe 36,648 hrs · 31,936 cycles

PAX CABIN BS 449.85 RBL 36 FLOOR SUPPORT IS CORRODED. COMPLIED WITH ECTC REO 601R-53-41-666 AND REO 601R-53-41-666, REV C.

Part: FLOORBEAM — CORRODED (BS 605) · airframe 36,665 hrs · 31,954 cycles

IN CARGO COMPARTMENT AT FS 605.00 ON RBL 9.00 THE FLOORBEAM AROUND FLOORBOARD ATTACHMENT HOLES IS CORRODED. REMOVED FLOORBEAM UPPER CAP AT RBL 9 BETWEEN 569 & FS 621 IAW SRM 51-42-06 AND SRM 51-42-21. LOCATED, DRILLED NEW SERVICEABLE CARGO COMPARTMENT FLOORBEAM CAP, PN 601R35031-3 IAW SRM 51-40-11 AND REO 601R-53-61-3780. COMPLIED WITH EC/TC REO 601R-53-6-3780 AND REO 601R-53-61-3780, REV A DATED 7/15/2011.

Part: SKIN — CORRODED (RT WING) · airframe 36,665 hrs · 31,954 cycles

RT WING PLANK ACCESS HOLE 640BB LIP HAS SEVERAL AREAS OF PITTING/CORROSION. REPAIRED IAW REO 601R-57-21-030 AND REO 601R-57-21-2004.

Part: FLOOR SUPPORT — CORRODED (BS 559) · airframe 36,648 hrs · 31,936 cycles

PAX CABIN FS 559+57 LBL 36 FLOOR SUPPORT IS CORRODED. COMPLIED WITH EC/TC REO 601R-53-00-526 AND GREO 601R-53-00-526 REV.

Part: FLOOR SUPPORT — CORRODED (BS 559) · airframe 36,648 hrs · 31,936 cycles

PAX CABIN BS 559+32 LBL 36.00 THE FLOOR SUPPORT CORRODED. COMPLIED WITH EC/TC REO 601R-53-00-526 AND GREO 601R-53-00-526 REV.

Part: FLOORBEAM — CORRODED (BS 598) · airframe 36,648 hrs · 31,936 cycles

IN CARGO BAY BS 598 LBL 9 FLOORBEAM CORRODED. REPAIRED IAW REO 601R-53-61-5029 AND REO 601R-53-00-005.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 35,690 hrs · 31,064 cycles

CAPTAIN`S FLASHLIGHT NOT WORKING. REPLACED BATTERIES IAW AMM 52-61-00.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 34,140 hrs · 29,689 cycles

EMERGENCY LIGHT AFT OF GALLEY INOPERATIVE. R & R BATTERY PACK IAW AMM 33-51-04. OPS CHECKED GOOD.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 33,667 hrs · 29,247 cycles

FOUND CRACK ON SERVICE DOOR FRAME. ON FWD DOOR SEAL STRIKER. REMOVED AND INSTALLED NEW SEAL STRIKER, IAW SRM 51-42-06, 51-23-00.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHTS) · airframe 32,026 hrs · 27,751 cycles

EMERGENCY LIGHTS INOPERATIVE WITH SWITCH ON. CHARGED BATTERY PACK.

Part: FLOOR SUPPORT — CORRODED (BS 409-559) · airframe 31,911 hrs · 27,644 cycles

PRESSURE FLOOR SKIN ANGLES HAVE CORROSION BETWEEN FS 409.00 +128 AND FS 559.00 RT SIDE. RECEIVED AND COMPLIED WITH EC/TC REO 601R-53-41-666 AND REO 601R-53-41-66.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 31,905 hrs · 27,639 cycles

EMERGENCY LIGHT OVERWING THE LAST ONE AFT OF EMERGENCY EXIT ON LT AND RT INOPERATIVE. REPLACE BATTERY PACK NR4 IAW AMM 33-51-04-000-801. REPLACED NR 4 BATTERY PACK IAW AMM 33-51-04-400-801, OPS TEST GOOD. CEILING PANEL BETWEEN FS559+48R AND FS 559, OR REMOVED IAW AMM 25-26-07-000-801. INSTALLED CEILING PANEL REF AMM 25-26-07-400-801 OK TO CLOSE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 31,905 hrs · 27,639 cycles

FLOOR LEVEL EMERGENCY LIGHT AT SERVICE DOOR INOPERATIVE. REPLACE EMERGENCY LIGHT ASSY AT SVC DOOR, FLOOR LEVER REF AMM 33-51-10-000-801 (ASSY BROKEN) REPLACED EMERGENCY LIGHT FLOOR ASSY IAW AMM 33-51-10-400-801 FAILS OPS TEST. REPLACED EMERGENCY LIGHTS BATTERY PACK NR 1 IAW AMM 33-51-04-400-801. OPS CHECKS GOOD.

Part: PLACARD — WRONG PART (EMERGENCY EXIT) · airframe 31,895 hrs · 27,629 cycles

LEFT EMERGENCY EXIT HAS WRONG PLACARD INSTALLED. REMOVED INCORRECT PLACARD IAW AMM 11-30-00-000-801 AND INSTALLED CORRECT PLACARD, IAW AMM 11-30-00-400-801,

Part: FLOORBEAM — CORRODED (BS 349) · airframe 31,895 hrs · 27,629 cycles

FLOORBEAM HAS CORROSION AT FS 349.00. REPAIRED IAW REO 601R-53-21-1361.

Part: FRAME — CRACKED (BS 280) · airframe 31,895 hrs · 27,629 cycles

BS 280 FRAME APPEARS TO BE CRACKED AFT LOWER SIDE NEAR LBL9.00. COMPLIED WITH ECTC REO 601R-53-11-171.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 31,895 hrs · 27,629 cycles

POSSIBLE CRACK FOUND AT FASTNER LOCATION ON PAX DOOR UNDER AFT DRAG ANGLE. REPAIRED IAW REO 601R-52-11-1991.

Part: SUPPORT — CORRODED (WINGSHIELD) · airframe 31,895 hrs · 27,629 cycles

RT SIDE WINDSCREEN SUPPORT STRUCTURE AT FS 349 CORRODED. REMOVED AND REPLACED WINDSCREEN SUPPORT ANGLE & FITTING IAW SRM 51-42-06 & SRM 51-42-21.

Part: BRACKET — CRACKED (WINDSHIELD) · airframe 31,895 hrs · 27,629 cycles

PILOTS WINDSHIELD SIDE POST LOWER BRACKET CRACKED. R & R BRACKET IAW SRM 51-47-21.

Part: FLOORBEAM — CORRODED (BS 349) · airframe 31,895 hrs · 27,629 cycles

FLOORBEAM HAS CORROSION AT FS 349.00 NEAR AFT END OF SERVICE DOOR CUTOUT. REMOVED CORROSION AND FOUND TO BE BEYOND ACCEPTABLE LIMITS IAW SRM 51-21-06 AND 53-00-00. CORROISON DAMAGE IS THROUGH ENTIRE THICKNESS OF FLOORBEAM. REPAIRED IAW REO 601R-53-21-1361. PERFORMED NDT OF CUT OUT AREAS IAW NDTM 51-20-06. NO INDICATIONS NOTED. HEAT TREATED REPAIR IAW REO 601R-53-21-1361, SRM 51-24-06, AND SRM 51-24-16.

Part: FRAME — CRACKED (BS 280) · airframe 31,895 hrs · 27,629 cycles

BS 280 FRAME APPEARS TO BE CRACKED AFT LOWER SIDE NEAR LBL 9.00. PERFORMED ET INSPECTION IAW MAC NDT INSPECTION PROCEDURE ET-2. VERIFIED FRAME CRACKED. REPAIRED IAW REO 601R-53-11-171. PERFORMED NDT IAW NDTM 51-20-06. NO INDICATIONS NOTED.

Part: SEAT TRACK — CORRODED (BS 364) · airframe 31,895 hrs · 27,629 cycles

SEAT TRACK CORRODED AT RBL 9 AND FS 364.00. CLEANED CORROSION IAW SRM 51-21-11. CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-21-49. REMOVED SEAT TRACK IAW AMM 53-01-11-000-802. LOCATED, DRILLED AND INSTALLED NEW SEAT TRACK IAW SRM 5140-11 AND AMM 52-01-11-400-802. MINOR REPAIR.

Part: SEAT TRACK — CORRODED (BS 559-574) · airframe 31,895 hrs · 27,629 cycles

CARGO COMPARTMENT NET ATTACHMENT SEAT RAIL FROM FS 559.00 + 112 TO FS 574.00 AT LBL 9.00 HAS SURFACE CORROSION. REMOVE SEAT TRACK AND FABRICATED NEW SEAT TRACK IAW SRM CH 51-40-11. OK TO INSTALL. INSTALLED NEW TRACKS IAW AMM 53-01-11-000-802, IAW AMM 53-01-11-000-802 AND SRM 51-41-02. MINOR REPAIR.

Part: ANGLE — CORRODED (BS 409-559) · airframe 31,895 hrs · 27,629 cycles

PRESSURE FLOOR SKIN ANGLES HAVE CORROSION BETWEEN FS 409.00 + 128 AND FS 559.00 LT SIDE. REMOVED CORROSION FROM PRESSURE FLOOR SKIN ANGLES IAW GRO 601R-53-41-666 AND SRM 51-21-06. PERFORMED UT INSPECTIONS OF BLEND AREAS IAW MAC NDT INSP PROCEDURE UT-3 MIN MATERIAL REMAINING FLOOR ANGLES IS .074" ORIGINAL THICKNESSIS .080" REMOVED IS .006" WITHIN ALLOWABLE LIMITS OF REO 601R-53-41-666. RESTORED FINISH TO REWORKED AREAS OF PRESSURE FLOOR SKIN ANGLES IAW GREO 601R-59-41 AND SRM 51-21-16.

Part: ISOLATOR — BROKEN (BULKHEAD) · airframe 31,895 hrs · 27,629 cycles

ISOLATOR AT 18LBL 21.5 " FROM FLOOR IS BROKEN ON CABIN SIDE OF PRESSURE BULKHEAD. R & R ISOLATOR IAW SRM CH 51-42-13. R & R ISOLATOR IAW SRM 51-42-13. THIS IS A MINOR REPAIR.

Part: STRUCTURE — CORRODED (PAX DOOR) · airframe 31,895 hrs · 27,629 cycles

AFT CORNER ON PAX DOOR BY HINGE FOUND BADLY CORRODED. REMOVED AFT CORNER ON PAX DOOR BY HINGE IAW SRM 51-42-21 AND 51-42-06. DRILLED UP AND INSTALLED AFT CORNER IAW SRM 51-42-21 AND 51-42-06.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 31,895 hrs · 27,629 cycles

CARGO COMPARTMENT NET ATTACHMENT SEAT TRACK FROM APPROX FS 559.00+80 TO FS 559.00+96 AT LBL 27.00 HAS SURFACE CORROSION. REMOVED DEFECTIVE SEAT TRACK IAW AMM 53-01-11-000-802. DRILLED AND INSTALLED NEW TRACKS IAW AMM 53-01-11-000-802 IAW AMM 53-01-11-000-802 AND SRM 51-41-02. MINOR REPAIR.

Part: STRUCTURE — CORRODED (PAX DOOR) · airframe 31,895 hrs · 27,629 cycles

FWD CORNER ON PAX DOOR BY HINGE FOUND CORRODED AND PITTED. REMOVED FWD CORNER ON PAX DOOR BY HINGE IAW SRM 51-42-21 AND 51-42-06. DRILLED AND INSTALLED FWD CORNER ON PAX DOOR BY HINGE IAW SRM 51-42-21 AND 51-42-06.

Part: ANGLE — CORRODED (BS 409-559) · airframe 31,895 hrs · 27,629 cycles

PRESSURE FLOOR SKIN ANGLES HAVE CORROSION BETWEEN FS 409.00 +128 AND FS 559.00. RT SIDE. REMOVED CORROSION FROM PRESSURE FLOOR ANGLES IAW GREO 601R-53-41-666 & SRM 51-21-06. PERFORMED UT THICKNESS INSPECTION OF BLEND AREAS IAW MAC NDT INSP PROCEDURE UT-3 MIN MATERIAL REMAINING IS .055", BLEND IS WITHIN ALLOWABLE LIMITS IAW REO 601R-53-41-666 TABLE 2. RESTORED SURFACE FINISH TO REWORKED AREAS IAW STEP 2-2, GREO 606R-53-41 AND SRM 51-21-16.

Part: ATTACH FITTING — CORRODED (FUSELAGE) · airframe 31,895 hrs · 27,629 cycles

FWD ATTACH FITTING CORRODED BY ASD HINGE. REMOVED FWD ATTACH FITTING IAW SRM 51-42-06. FABRICATED IAW SRM 52-10-14 AND 51-40-11 AND INSTALLED IAW SRM 51-42-06.

Part: STRUCTURE — CRACKED (PAX DOOR) · airframe 31,895 hrs · 27,629 cycles

POSSIBLE CRACK FOUND AT FASTENER LOCATION ON PAX DOOR UNDER AFT DRAG ANGLE. PERFORMED EDDY CURRENT INSPECTION OF PAX DOOR INNER SKIN IAW MAC NDT INSP PROCEDURE ET-2. CRACK INDICATION CONFIRMED ON SKIN. CUTOUT DAMAGED AREA IAW REO 601R-52-11-1991 P1. PERFORMED NDT IAW NDTM PART 1, 51-20-06. NO INDICATIONS NOTED. FABRICATED REPAIR IAW REO 601R-52-11-1991 P1.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 31,895 hrs · 27,629 cycles

CARGO COMPARTMENT NET ATTACHMENT SEAT TRACK FROM APPROX FS 559.00+80 TO FS 559.00+96 AT RBL 9.00 HAS SURFACE CORROSION. REMOVED DEFECTIVE SEAT TRACK IAW AMM 53-01-11-000-802. DRILLED AND INSTALLED NEW TRACKS IAW AMM 53-01-11-000-802 IAW AMM 53-01-11-000-802 AND SRM 51-41-02. MINOR REPAIR.

Part: ATTACH FITTING — CORRODED (FUSELAGE) · airframe 31,895 hrs · 27,629 cycles

AFT FITTINGS CORRODED BY ASD HINGE . REMOVED IAW SRM 51-42-06. FABRICATED IAW SRM 52-10-14 AND 51-40-11. INSTALLED IAW SRM 51-42-06.

Part: SKIN — CRACKED (PAX DOOR) · airframe 31,895 hrs · 27,629 cycles

PAX DOOR SKIN CRACKED AT ONE FASTERNER LOCATION NEAR WEATHER STRIP. CUTOUT DAMAGED AREA IAW P1 REO 601R-52-11-1992 STEPS 1 AND 2. NDT AREA COMPLIED WITH STEP 3 OF REP 601R-52-11-1992 IAW NDTM PART , 51-20-06. NO INDICATIONS NOTED. REPAIRED IAW REO 601R-52-11-1992.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 31,895 hrs · 27,629 cycles

CARGO COMPARTMENT NET ATTACHMENT SEAT TRACK FROM APPROX. FS 559.00 + 80 TO FS 559.00 + 96 AT RBL 27.00 HAS SURFACE CORROSION. REMOVED DEFECTIVE SEAT TRACK, DRILLED & INSTALLED NEW TRACKS IAW AMM 53-01-11-000-802 IAW AMM 53-01-11-000-802 AND SRM 51-41-02. MINOR REPAIR.

Part: SEAT TRACK — CORRODED (BS 559-574) · airframe 31,895 hrs · 27,629 cycles

CARGO COMPARTMENT NET ATTACHMENT SEAT RAIL FROM FS 559.00+112 TO FS 574.00 AT RBL 9.00 HAS SURFACE CORROSION. REMOVE SEAT TRACK AND FABRICATED NEW SEAT TRACK IAW SRM 51-40-11. INSTALLED NEW TRACKS IAW AMM 53-01-11-000-802 AND SRM 51-41-02. MINOR REPAIR. (CLOSED)

Part: ATTACH FITTING — CORRODED (PAX DOOR) · airframe 31,895 hrs · 27,629 cycles

CENTER ATTACH FITTING CORRODED ON PAX DOOR BY ASD HINGE. REMOVED CENTER ATTACH FITTING IAW SRM 51-42-06. FABRICATED IAW SRM 52-10-14 AND 51-40-11 AND INSTALLED IAW SRM 51-42-06.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 31,895 hrs · 27,629 cycles

CARGO COMPARTMENT NET ATTACHMENT SEAT TRACK FROM APPOX. FS 559.00 + 80 TO FS 559.00 + 96 AT LBL 9.00 HAS SURFACE CORROSION. REMOVED DEFECTIVE SEAT TRACK IAW AMM 53-01-11-000-802. DRILLED AND INSTALLED NEW TRACKS IAW AMM 53-01-11-000-802 IAW AMM 53-01-11-000-802 AND SRM 51-41-02. MINOR REPAIR.

Part: CONNECTOR — UNSECURE (ANTI ICE SYSTEM) · airframe 31,885 hrs · 27,620 cycles

WING A/ICE SENSOR CAUTION MESSAGE FOLLOWED BY WING OVERHEAT WARNING. FOLLOWED QRH, MESSAGE PERSISTED THROUGHOUT FLIGHT. EMERGENCY DECLARED AND EQUIPMENT ROLLED AS A PRECAUTION. RESECURED ANTI-ICE TEMP CONTROL UNIT CONNECTOR PLUG IAW AMM 30-12-19. PERFORMED OPS CHECK IAW AMM 30-12-00. OPS CHECK GOOD AT THIS TIME.

Part: STRUT — FAILED (NLG) · airframe 31,241 hrs · 27,050 cycles

CREW REPORTED NLG DISAGREE MSG IN FLT, AFTER TAKEOFF. ENROUTE TO IAD ACFT DIVERTED DUE TO MX -- EMERGENCY DELARED AS A PRECUATION. REMOVED AND REPLACED NLG STRUT ASSY IAW AMM 32-21-01. OPS CHECK GOOD. LEAK CHECK GOOD. (CLOSED)

Part: PROXIMITY SENSOR — OUT OF ADJUST (NLG) · airframe 30,482 hrs · 26,400 cycles

GEAR DISAGREE AND NOSE DOOR OPEN MESSAGES UPON GEAR RETRACTION, PERFORMED QRH PROCEDURE AND RECEIVED 3 GEAR DOWN AND LOCKED INDICATIONS. (ACFT RETURNED TO DEPARTURE) SENSOR TO TARGET ADJUSTMENT OF NLG. CENTERED EXTENDED PROX SENSOR REF AMM 32-61-01.

Part: BRACKET — DAMAGED (NLG PROX SWITCH) · airframe 30,149 hrs · 26,090 cycles

GEAR DISAGREE MESSAGE AFTER TAKEOFF, MAIN GEAR UP, NOSE GEAR DOWN. RAN QRH, ALL GEAR DOWN AND LOCKED. (ACFT RETURNED TO DEPARTURE AFTER T/O -- EMERGENCY DECLARED AS A PRECAUTION) FLT 7103 CX, R & R BRACKET FOR NLG CENTERING PROX-SWITCH, RIGGED SWITCH & SERVICED STRUT AS REQUIRED. WORK DONE IAW AMM 12-12-32 & 32-61-25, GEAR SWINGS DONE AS REQUIRED. (CLOSED)

Part: PROXIMITY SENSOR — BENT (NLG) · airframe 29,971 hrs · 25,932 cycles

NOSE GEAR DISAGREE (ACFT RETURNED TO DEPARTURE AFTER T/O -- EMERGENCY DECLARED - EMERGENCY VEHICLES STANDING BY AS A PRECAUTION) FOUND PROX SENSOR AND TARGET BENT ON NLG, (CREW INFORMED US THAT RAMP HAD PROBLEMS GETTING STRAP RELEASED AFTER PUSH-BACK) ADJUSTED SENSOR AND TARGET AND SWUNG NOSE GEAR SEVERAL TIMES WITH NO FURTHER DEFECTS NOTED. (CLOSED)

Part: EXHAUST DUCT — FIRE (APU) · airframe 30,064 hrs · 26,012 cycles

FLT 7128 - FIRE IN APU EXHAUST VISUALLY INSPECTED APU COMPARTMENT AND CONTAINMENT NO DISCREPANCIES NOTED. OPERATED APU AS PER MAINTENANCE MANUAL CRJ 200 AMM 49-10-00 . OPS CHECK GOOD.

Part: OIL SYSTEM — LOW (LT ENGINE) · airframe 29,476 hrs · 25,499 cycles

LT ENGINE OIL PRESSURE SHOULD 47-55 PSI ON TAKEOFF ROLL, ON CLIMB OUT THRU 9000 FT OIL PRESSURE DROPPED BELOW 30 PSI, IN CONJUNCTION WITH "LOW OIL PRESSURE" TRIPLE CHIME. FOLLOWED QRH. AT IDLE, OIL PRESSURE STABILIZED AT 39 PSI .LT IT AT IDLE. (ACFT RETURNED TO DEPARTURE AFTER T/O -- EMERGENCY DECLARED) SERVICED LT ENGINE,TOOK 5 QUARTS. PERFORMED INSP OF LUBRICATION SYS IAW FIM PROCEDURES GE CF-34 3A1 AND 3B1 SPECIAL INSP 15. NO DESCREPANCIES FOUND. PERFORMED OIL CONSUMPTION RUNS ON NR1 ENGINE , NR1 ENGINE WITHIN LIMITS IAW AMM 72-00-00. (CLOSED)

Part: LAMP — INOPERATIVE (MLG INDICATOR) · airframe 29,172 hrs · 25,227 cycles

ON TAKEOFF FROM IAD WE RECEIVED A GEAR DISAGREE MESSAGE. THE NOSE GEAR FAILED TO RETRACT. EMERGENCY DECLARED -- ACFT RETURNED AFTER T/O. RELAMPED LT AFT EXT EMERGENCY LIGHT IAW AMM 33-51-15, OPS CHECK GOOD. RELAMPED LT AFT EXT EMERGENCY LIGHT IAW AMM 33-51-15, OPS CHECK GOOD. (CLOSED)

Part: SENSOR — OUT OF POSITION (NLG) · airframe 28,978 hrs · 25,048 cycles

NOSE GEAR DISAGREE WARNING MSG WITH NOSE DOOR. OPEN WARNING WARNING MSG AFTER GEAR RETRACTED. (EMERGENCY DECLARED - ACFT RETURNED TO IAD AFTER T/O) UPON INSP, FOUND NLG PROX SENSOR S23 OUT OF LIMITS. REPOSITIONED S23 IAW AMM 32-61-00 AND SWUNG NLG IAW 32-33-00. OPS CK GOOD, NO DEFECTS NOTED. (CLOSED)

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 28,563 hrs · 24,664 cycles

EMERGENCEY LIGHT AT LT OVER WING ER EXIT INOP. R & R NR 3 INVERTOR IAW AMM 33-51-07. OPS CK GOOD. ITEM: 1 / R & R NR 3 INVERTOR IAW AMM 33-51-07. OPS CK GOOD.

Part: VALVE — FAILED (A/C PACK) · airframe 28,372 hrs · 24,503 cycles

BURNING ODOR IN MAIN CABIN. (AIR CONDITIONING PACK - LT SIDE)

Part: BYPASS VALVE — FAILED (CABIN AIR) · airframe 28,371 hrs · 24,503 cycles

REMOVED DEFECTIVE LT DUAL BYPASS VALVE AND INSTALLED REPAIRED UNIT. LEAK AND OPS CHECK GOOD AT THIS TIME WORK DONE IAW AMM 21-61-31 PACK NOW OPERATES IN MANUAL MODE ONLY DEFER CLEARED PLACARD REMOVED REF AFDL 527321-1 FOR OPERATION. (CLOSED)

Part: ANCHOR FITTING — CRACKED (PAX DOOR) · airframe 28,051 hrs · 24,241 cycles

PAX DOOR AFT ANCHOR FITTING CRACKED. R & R AFT ANCHOR FITTING ON PASSENGER DOOR IAW AMM 52-11-17. OPS CHECK GOOD. PERFORMED RII SATISFACTORY IAW SP 607 ON INSTALLATION OF AFT PASSENGER DOOR ANCHOR. R & R AFT ANCHOR FITTING ON PASSENGER DOOR IAW AMM 52-11-17. OPS CHECK GOOD. PERFORMED RII SATISFACTORYON INSTALLATION OF AFT PASSENGER DOOR ANCHOR IAW SP 607.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 28,046 hrs · 24,239 cycles

REPAIRED BROKEN WIRES AND OPS CHECK TESTED GOOD IAW ESPM 20-11-00 AND AMM 33-51-00. REPAIRED BROKEN WIRES AND OPS CHECK TESTED GOOD IAW ESPM 20-11-00 AND AMM 33-51-00. (CLOSED)

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 28,046 hrs · 24,239 cycles

PAX DOOR EMERGENCY EXIT SIGN (ON WARDROBE) INOP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,732 hrs · 23,902 cycles

LT EXTERNAL EMERGENCY LIGHT JUST FWD OF EMERGENCY EXIT DOOR INOP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,732 hrs · 23,902 cycles

RT EXTERNAL EMERGENCY LIGHT JUST FWD OF EMERGENCY DOOR INOP.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 27,727 hrs · 23,899 cycles

EMERGENCY LIGHTS AT LT AND RT OVERWING EXITS (STA 416.5) CABIN CEILING NR 3 AND CURVED EMERGENCY EXIT SIGN MID CABIN FACING AFT ARE ALL INOPERATIVE.

Part: FRAME — CRACKED (BS 605) · airframe 27,726 hrs · 23,898 cycles

CRACKED FRAME AT FS 605.00 S9L. PERFORMED E/T INSP ON FS605.00 STR 9 CUT OUT IAW REO 601R-53-61-3408 AND NDT MANUAL 51-20-06 NO DEFECTS NOTED NDT REPORT ATTACHED. COMPLIED WITH FABRICATION OF REPAIR PARTS -1, -2, -3, SHIM & -4 SHIM FROM 7075-T6 & 2024-T3 P/O 91695 & P/O 106125 PER REO 601R-53-61-3408 REV. DRILLED & LOCATED ALL REPAIR PARTS -1,-2,-3 SHIM & -4 SHIM. CUT DAMAGED FRAME PER REO 610R-53-51-3402. DAMAGE REMOVED. INSTALLED REPAIR PARTS ON THE FRAME AT FS 605.00 PER SRM 51-42-06 AND SRM 51-42-21. APPLIED PROTECTIVE FINISH PER SRM 51-51-16. COMPLIED WITH REO 601R-53-61-3408. RII COMPLIED WITH SP607 ALL WORK FOUND TO BE SATISFACTORY.

Part: PLACARD — MISSING (ESCAPE HATCH) · airframe 27,726 hrs · 23,898 cycles

"EMER" PLACARD MISSING ON OUTER ESCAPE HATCH SKIN. INSTALLED SILKSCREEN PRINT TO EMERGENCY ESCAPE HATCH "EMERGENCY EXIT" PER AMM 20-60-11-400-601 1-5.

Part: FRAME — CORRODED (BS 559 S26-27L) · airframe 27,726 hrs · 23,898 cycles

ON 559+96 FRAME BETWEEN S26-27L HAS CORROSION LOWER FRAME. REMOVED FRAME PER SRM 51-42-06. INSTALLED NEW FRAME STRINGERS PER SRM 51-42-06.

Part: DOOR FRAME — CRACKED (BS 319-323) · airframe 27,726 hrs · 23,898 cycles

PAX DOOR FWD FRAMES CRACKED AT UPPER RADIUS AT FS319 AND 323. INSTALLED REPLACEMENT FRAME AT FS323.3 IAW SRM 51-42-13 & 51-42-06.

Part: PRESSURE BLKHD — CRACKED (BS 702) · airframe 27,726 hrs · 23,898 cycles

CRACK IN 702 PRESSURE BULKHEAD LT SIDE LWR WHERE PACKING BREAK CABLE GOES THROUGH. REMOVED -113 BRACKET, WEB STIFFENER AND CHANNEL DOUBLER FROM FS202 BULKHEAD WEB AND CUT OUT DAMAGE AT FS202.75 AT BL23.71 PRESSURE BULKHEAD PER REO 601R-53-11-563. FABRICATED DOUBLER AND SHIMS. LOCATED DOUBLER AND SHIMS. AND INSTALLED IAW REO 601R-53-11-563.

Part: BULKHEAD — CRACKED (BS 559) · airframe 27,726 hrs · 23,898 cycles

CRACK NOTED AT FS559.0 AT RBL18.00, WL59.10 (MARKED IN RED). REMOVED AND DISCARDED POSTS, CUTOUT DAMAGED SECTION OF BULKHEAD WEB, PERFORMED OK TO INSTALL ALL FABRICATED PARTS AND INSTALLED POST STRAP IAW REO 601R-53-41-260.

Part: INTERCOSTAL — CORRODED (BS 621) · airframe 27,726 hrs · 23,898 cycles

AT FS 621.0 BULKHEAD INTERCOSTAL RT SIDE HAS ONE SHEARED RIVET AND CORROSION AT NUTPLATE HOLE.

Part: SKIN — CORRODED (BS 559) · airframe 27,726 hrs · 23,898 cycles

CORROSION ALONG BOTTOM OF BELLY SKIN EXTERNAL SIDE FS 559 AND 93 TO 559 AND 112 AND AT FS 559 AND 45. REMOVED LIGHT SURFACE CORROSION. FOUND TO BE WITHIN LIMITS IAW SRM 53-00-31.

Part: SIGN — BROKEN (CABIN) · airframe 26,921 hrs · 23,091 cycles

PAX DOOR EMERGENCY SIGN BROKE. FLT 5204 DEL 50 MINS.

Part: COVER — MISSING (EMERGENCY LIGHTS) · airframe 26,699 hrs · 22,871 cycles

FLT 5123, EMERGENCY LIGHTS IN CABIN MISSING PLASTIC STRIP AND PHOTO ILLUMINESCENT STRIP IS BROKEN ROWS 9 AND 10. REPLACED EMERGENCY LIGHT FLOOR LENS COVER OPS CHECKS GOOD DONE IAW AMM 33-51-01, THIS CLEARS DEFECT, REMOVED PLACARD.

Part: FEEDER CABLE — DAMAGED (EMERGENCY LIGHTS) · airframe 26,372 hrs · 22,564 cycles

FLT 5590. ELECTROLUMINESCENT FLOOR LEVEL LIGHTING STRIPS FROM ROW 6 TO ROW 7 ARE INOP INTERMITTENTLY. REPLACED FLOOR LIGHTING CABLE ASSY AT 6 AND 7 IAW 33-51-01. DML CLEARED PLACARD REMOVED.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 26,210 hrs · 22,416 cycles

IN REFERENCE TO TASK CARD AWL 53-61-153 02 W/O 107923. DURING EDDY CURRENT INSPECTION OF AFT PRESSURE BULKHEAD, FOUND THAT BULKHEAD IS CRACKED AT LINTEL ATTACH POINT.

Part: STRUCTURE — CRACKED (ASD) · airframe 26,199 hrs · 22,405 cycles

ASD BOTTOM STEP COMPOSITE ATTACHED TO BRACKET CRACKED.

Part: DOOR — BINDING (PAX DOOR) · airframe 25,780 hrs · 22,029 cycles

MAIN PAX DOOR HARD TO PULL CLOSE LAST 2 FEET.

Part: FRAME — CORRODED (BS 333 S25L) · airframe 25,001 hrs · 21,325 cycles

CORROSION ON FRAME AND SKIN AT FS 333 STR 25 LT. FABRICATED AND DRILLED -1 DOUBLER. INSTALLED -1 DOUBLED, AND -2 FRAME INSERT REF CRJ200 SRM 51-42-06. SEALED REPAIR AREA, REFINISHED REPAIR AREA, AND BLENDED AREA ON STRAP AO23. REINSTALLED HYD CLAMPS, ABOVE WORK DONE REF REO 601R-53-21-904. JOB COMPLETE. CC7021316. BLENDED STRAP AND REMOVED CORROSION. BLENDED AREA MEASURES 1"X1.2" WITH .002" MATERIAL REMOVED. REPORTED BLEND DIMENSIONS TO ENGINEERING. REF CRJ200 SRM 51-21-16 PSP7019749 25JUN08. (S)

Part: HANDLE — DIRTY (PAX DOOR) · airframe 2,494,405 hrs · 21,279 cycles

MAIN CABIN DOOR WILL NOT CLOSE THE OUTER HANDLE WILL NOT STOW. FLT 4328 DEL 19 MINS. OPS CHECKED MAIN DOOR, OPS NORMAL AFTER CLEANING OPS PER AMM 52-70-01.

Part: DOOR — BINDS (PAX DOOR) · airframe 24,141 hrs · 20,606 cycles

PASSENGER DOOR DIFFICULT TO CLOSE AND LATCH.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 23,931 hrs · 20,437 cycles

F/A FLASHLIGHT INOP.

Part: STRAP — CRACKED (FUSELAGE) · airframe 23,211 hrs · 19,817 cycles

AAR - RIGHT FS 640 STR 8-13 SKIN BUTT JOINT STRAP IS CRACKED. COMPLIED WITH EC/TC REO 601R-53-61-506,

Part: ANCHOR FITTING — CRACKED (PAX DOOR) · airframe 23,211 hrs · 19,817 cycles

PAX DOOR FORWARD COUNTER BALANCE ANCHOR FITTING IS CRACKED. 10-18-07 REMOVED FORWARD COUNTER BALANCE ANCHOR FITTING IAW CRJ 200 AMM 52-11-17. OK TO INSTALL NEW SERVICEABLE FORWARD COUNTER BALANCE ON COTTER FITTING INSTALLED NEW SERVICEABLE FORWARD COUNTER BALANCE ANCHOR FITTING IAW CRJ 200 AMM 52-11-17. SN 1047, ANCHOR FITTING UPPER ADJUSTMENT BOLT REQUIRES INSTALLATION ORDERED AGAINST WC 8000-0003. INSTALLED ANCHOR FITTING BOLTS IAW CRJ 200 AMM 52-11-17, REQUIRES ADJUSTMENT. CHECKED ADJUSTMENT AND RIG IAW CRJ 200 AMM 52-11-17. RIG AND ADJUSTMENT CHECK GOOD AT THIS TIME.

Part: FITTING — CRACKED (FUSELAGE) · airframe 23,211 hrs · 19,817 cycles

AAR - INBOARD CLIP CRACKED AT FS 280 LBL 9. REFERENCE ROUTINE 50186/2000/0022 FOR CORRECTIVE ACTION 14211 9-11-07. SUPPLEMENTAL - SDR CLOSED 09/14/07.

Part: FITTING — CRACKED (FUSELAGE) · airframe 23,211 hrs · 19,817 cycles

AAR - O/B CLIP CRACKED AT FS 280 LBL 9. REFERENCE ROUTINE 50186/2000/0022 FOR CORRECTIVE ACTION 14211 9-11-07. SUPPLEMENTAL - SDR CLOSED 09/14/07.

Part: PLACARD — WORN (EXTERIOR) · airframe 23,211 hrs · 19,817 cycles

AAR - EXTERIOR PLACARD ON ESCAPE HATCH -EMERGENCY EXIT PUSH- IS WORN.

Part: STEP — CRACKED (PAX DOOR) · airframe 23,211 hrs · 19,817 cycles

PAX DOOR STAIR 832CT IS CRACKED. REPAIRED IAW CRJ 200 SRM 51-40-11, 51-42-06, 51-42-21,

Part: FITTING — CRACKED (FUSELAGE) · airframe 23,211 hrs · 19,817 cycles

AAR - RIGHT O/B INTERCOSTAL FS 484 I/B CLIP CRACKED. REMOVED DAMAGED ANGLE CLIP FROM RIGHT O/B INTERCOSTAL FS 484 I/B SIDE IAW CRJ 200 SRM 51-42-06. FABRICATED AND DRILLED ANGLE CLIP FROM 2024 T-3 .063" PO 950261 IAW CRJ 200 SRM 51-40-11. PERFORMED LPI ON FABRICATED ANGLE FOR INTERCOSTAL REPAIR IAW REO 601R-53-41-059. NO DEFECTS NOTED. REQUIRES OK FOR ALODINE PRIME AND PAINT. ALODINED AND PRIMED IAW CRJ 200 SRM 51-25-06. OK TO INSTALL. INSTALLED SERVICEABLE I/B CLIP ON RIGHT O/B INTERCOSTAL FS 484 IAW REO 601R-53-41-059. OK TO TOPCOAT. TOPCOATED IAW CRJ 200 SRM 51-25-16. SUPPLEMENTAL - SDR CLOSED 09/12/07.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 23,211 hrs · 19,817 cycles

AAR - RIGHT O/B INTERCOSTAL AT FS 484 CRACKED. CUT AWAY DAMAGED (CRACKED) ATTACHMENT FLANGE AT FS 484.00 O/B SIDE RIGHT INTERCOSTAL IAW REO 601R-53-41-059. (FABRICATED) ANGLE CLIP FROM 2024 T-3 .063" (PO 950261). COMPLIED WITH LPI OF CUT LINE AND FABRICATED ANGLE IAW REO 601R-53-41-059. NO DEFECTS NOTED ANGLE CLIP REQUIRES DRILLED AND CONFORMED. LOCATED HOLES AND CONFORMED ANGLE IAW REO 601R-53-41-059 OK TO ALODINE AND PRIME. ALODINED AND PRIMED IAW CRJ 200 SRM 51-25-06. OK TO INSTALL. INSTALLED SERVICEABLE INTERCOSTAL AT RIGHT O/B FS 484 IAW REO 601R-53-41-059. OK TO TOP COAT. TOP COATED IAW CRJ 200 SRM 51-25-16. SUPPLEMENTAL - SDR CLOSED 09/12/07.

Part: FITTING — CRACKED (FUSELAGE) · airframe 23,211 hrs · 19,817 cycles

AAR - LEFT I/B INTERCOSTAL AT FS 484 I/B CLIP CRACKED. REMOVED CRACKED LEFT I/B INTERCOSTAL CLIP AT FS 484 PER CRJ 200 SRM 51-42-06. LPI OF LEFT FS 484 I/B FABRICATED REPLACEMENT ANGLE IAW NDTM 51-20-08. NO DEFECTS NOTED. INSTALLED REPLACEMENT ANGLE IAW CRJ 200 SRM 51-42-06. REFERENCE ATTACHED DOCUMENT FOR DETAILS. SUPPLEMENTAL - SDR CLOSED 09/12/07.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 23,211 hrs · 19,817 cycles

AAR - FLOOR SUPPORT ANGLE AFT OF FS 280 O/B OF RBL 9 IS CRACKED. REFERENCE ROUTINE 50186/2000/0022 FOR CORRECTIVE ACTION. 14211 9-11-07. SUPPLEMENTAL - SDR CLOSED 09/14/07.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 23,211 hrs · 19,817 cycles

AAR - FLOOR SUPPORT ANGLE AFT OF FS 280, O/B OF LBL 9 IS CRACKED. REFERENCE ROUTINE 50186/2000/0022 FOR CORRECTIVE ACTION 14211 9-11-07. SUPPLEMENTAL - SDR CLOSED 09/14/07.

Part: FITTING — CRACKED (FUSELAGE) · airframe 23,211 hrs · 19,817 cycles

AAR - LEFT O/B INTERCOSTAL AT FS 484 I/B AND O/B CLIPS CRACKED. CUT OUT DAMAGED ATTACHMENT FLANGE ON LEFT O/B INTERCOSTAL FS 484 PER REO 601R-53-41-059 NOTE 1. REMOVED CRACKED INTERCOSTAL CLIP PER REO 601R-53-41-059. COMPLIED WITH LPI OF LEFT FS 486 O/B INTERCOSTAL CUTLINE AND FABRICATED REPLACEMENT ANGLES 2 EACH FOR I/B AND O/B LOCATIONS IAW REO 601R-53-41-059. NO DEFECTS NOTED. COMPLIED WITH REO 601R-53-41-059. SUPPLEMENTAL - SDR CLOSED 09/12/07.

Part: PLACARD — DAMAGED (PAX DOOR) · airframe 23,211 hrs · 19,817 cycles

AAR - "OPEN" AND "EXIT" PLACARDS ON PAX DOOR ARE DAMAGED. REMOVED UNSERVICEABLE "OPEN" AND "EXIT" PLACARDS FROM PAX DOOR AND INSTALLED SERVICEABLE P/N'S S1574-18 (EXIT) AND P/N S1574-14 (OPEN), IAW CRJ 200 AMM 11-30-00. SUPPLEMENTAL - SDR CLOSED 09/12/07.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 23,210 hrs · 19,814 cycles

NOSE GEAR DISAGREE WARNING MESSAGE AND STEERING INOP CAUTION MESSAGE WHEN RETRACTING GEAR. A/C RETURNED TO ATL AFTER T/O. EMERGENCY DECLARED.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 23,210 hrs · 19,814 cycles

ON T/O RETRACTED GEAR AND RECEIVED -STEERING INOP- EICAS CAUTION FOLLOWED BY GEAR DISAGREE MANUALLY LOWERED GEAR. REAR DISAGREE MESSAGE OUT. A/C RETURNED TO ATL AFTER T/O. EMERGENCY DECLARED. FLTS 4729, 4700 CX.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 23,210 hrs · 19,812 cycles

NLG GEAR DISAGREE MSG AFTER GEAR HANDLE SELECTED UP. A/C RETURNED TO AVL AFTER T/O. EMERGENCY DECLARED. (LANDING GEAR RETRACTION SYSTEM)

Part: LIGHT — UNSECURE (CABIN) · airframe 23,105 hrs · 19,717 cycles

EMERGENCY LIGHT NEXT TO SERVICE DOOR NEEDS TO BE RESECURED.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 22,682 hrs · 19,388 cycles

F/O`S FLASHLIGHT WILL NOT TURN ON.

Part: DOOR — STIFF (AIRSTAIR) · airframe 22,474 hrs · 19,221 cycles

ASD HARD TO CLOSE. FLT 4574 DEL 25 MINS.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 22,085 hrs · 18,892 cycles

FLIGHT ATTENDANT`S FLASHLIGHT INOP.

Part: STEP — CRACKED (AIRSTAIR DOOR) · airframe 21,992 hrs · 18,818 cycles

ASD BOTTOM STEP IS CRACKED.

Part: BRACKET — CRACKED (PRESS BULKHEAD) · airframe 21,206 hrs · 18,229 cycles

CARGO DOOR SUPPORT BEAM PRESSURE BULKHEAD BRACKET CRACKED.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 21,090 hrs · 18,145 cycles

FLAPS FAIL MSG WHEN TRYING TO SELECT FLAPS 30, FLAPS INDICATED 20. FOLLOWED QRH, LANDED IN CVG WITH NO FURTHER INCIDENTS. EMERGENCY DECLARED; CREW REQUESTED EMERGENCY EQUIPMENT BE ON STBY AS A PRECAUTION. FLT 4791 DEL 100 MINS.

Part: DOOR — STIFF (SERVICE) · airframe 20,814 hrs · 17,951 cycles

SERVICE DOOR IS VERY DIFFICULT TO OPEN.

Part: RIB — CRACKED (LT WING)

DURING A C-CHECK IN MCN, THE LEFT MAIN WHEEL WELL BATTERY RIB ASSEMBLY AT WS 53.60 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE LEFT MAIN WHEEL WELL BATT RIB ASSY IAW ASA EO 600-57-039A. (M)

Part: RIB — CRACKED (RT WING)

DURING A C-CHECK IN MCN, THE RIGHT WHEEL WELL BATT RIB ASSY AT WS 53.60 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE RIGHT WHEEL WELL BATT RIB ASSY AT WS 53.60 IAW ASA EO 600-57-039A. (M)

Part: SILL — CORRODED (BS 541)

DURING A C-CHECK IN MCN, THE LEFT SIDE PRESSURE FLOOR SILL STRUCTURE AT FS 541 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS SUBMITTING A DAMAGE REPORT TO BOMBARDIER FOR ISSUANCE OF AN REO TO DETERMINE THE APPROPRIATE CORRECTIVE ACTION. (M)

Part: PRESSURE PANEL — CORRODED (CABIN FLOOR)

DURING A C-CHECK IN MCN, THE RIGHT SIDE PRESSURE FLOOR SILL STRUCTURE AT FS 461 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS SUBMITTING A DAMAGE

Part: SILL — CORRODED (BS 499-513)

DURING A C-CHECK IN MCN, THE RIVETS ON THE LEFT SIDE PRESSURE FLOOR SILL STRUCTURE AT FS 499 TO FS 513 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS SUBMITTING A DAMAGE REPORT TO BOMBARDIER OR ISSUANCE OF AN REO TO DETERMINE THE APPROPRIATE CORRECTIVE ACTION. (M)

Part: SILL — CORRODED (BS 529)

DURING A C-CHECK IN MCN, THE LEFT SIDE PRESSURE FLOOR SILL STRUCTURE AT FS 529 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS SUBMITTING A DAMAGE REPORT TO BOMBARDIER FOR ISSUANCE OF AN REO TO DETERMINE THE APPROPRIATE CORRECTIVE ACTION. (M)

Part: FRAME — CRACKED (BS 280)

DURING A C-CHECK IN MCN, THE FS 280 FRAME, RBL 9 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE FS 280 FRAME, RBL 9 IAW ASA EO 600-53-0318. (M)

Part: PRESSURE PANEL — CORRODED (CABIN FLOOR)

DURING A C-CHECK IN MCN, THE LEFT SIDE PRESSURE FLOOR SKIN PLANK AT FS 461 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS SUBMITTING A DAMAGE REPORT TO BOMBARDIER FOR ISSUANCE OF AN REO TO DETERMINE THE APPROPRIATE CORRECTIVE ACTION. (M)

Part: SILL — CORRODED (BS 544)

DURING A C-CHECK IN MCN, THE LT AND RT SIDE PRESSURE FLOOR SILL STRUCTURES AT FS 544 WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS SUBMITTING A DAMAGE REPORT TO BOMBARDIER FOR ISSUANCE OF AN REO TO DETERMINE THE APPROPRIATE CORRECTIVE ACTION. (M)

Part: PRESSURE PANEL — CORRODED (CABIN FLOOR)

DURING A C-CHECK IN MCN, THE RIGHT SIDE PRESSURE FLOOR SKIN AT FS 499 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS SUBMITTING A DAMAGE REPORT TO BOMBARDIER FOR ISSUANCE OF AN REO TO DETERMINE THE APPROPRIATE CORRECTIVE ACTION. AFTER MAINTENANCE BLENDED THE RIGHT SIDE PRESSURE FLOOR SKIN AT FS 499, IAW ASA EO 600-53-0319, IT WAS FOUND TO BE WITHIN ACCEPATABLE LIMITS. (M)

Part: SILL — CORRODED (BS 484)

DURING A C-CHECK IN MCN, THE RIGHT SIDE PRESSURE FLOOR SILL AT FS 484 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS SUBMITTING A DAMAGE REPORT TO BOMBARDIER FOR ISSUANCE OF AN REO TO DETERMINE THE APPROPRIATE CORRECTIVE ACTION. MAINTENANCE REPAIRED THE RT SIDE PRESSURE FLOOR SILL AT FS 484 IN ACCORDANCE WITH ASA EO 600-53-0319 CLOSED (M)

Part: DOUBLER — CRACKED (BS 718)

DURING A C-CHECK IN MCN, THE DOUBLER AT FS 718, STRINGER 11 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE DOUBLER AT FS 718, STRINGER 11 IAW ASA EO 600-53-0067A. (M)

Part: FRAME — CRACKED (BS 718)

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

Part: FRAME — CRACKED (BS 718)

DURING A C-CHECK IN MCN, THE FUSELAGE FRAMES FS 718, STRINGER 10 LEFT AND THE FORWARD SIDE OF FS 718, STRINGER 10 AND 11 RIGHT WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE FUSELAGE FRAMES FS 718, STRINGER 10 LEFT AND 11 RT IAW ASA EO600-53-0067A. (M)

Part: STEP — SEPARATED (PASSENGER DOOR)

DURING A GROUND INSPECTION, THE PASSENGER DOOR BOTTOM STEP WAS FOUND TO HAVE A BROKEN ATTACH BRACKET. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR BOTTOM STEP. AIRCRAFT OK FOR SERVICE. (K)

Part: STEP — BROKEN (PAX DOOR)

FLT 4642 - DURING A GROUND INSPECTION IN ATL, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: CONNECTOR — LOOSE (ENGINE)

DURING CLIMB-OUT, JUST PRIOR TO LEVELING OFF AT 23,000 FT, GOT A TRIPLE CHIME MASTER WARNING FOR RT ENG LOW OIL PRESS WHICH IMMEDIATELY VANISHED BUT REPEATED A FEW MIN LATER. OIL PRESS STARTED TO FLUCTUATE BETWEEN 25 & 39 PSI, RT ENG LOW OIL PRESS MESSAGE INTERMITTENT YET FREQUENT. ENG SECURED. EMERGENCY DECLARED & DIVERT. SINGLE ENG LANDING PERFORMED WITHOUT INCIDENT. MX R & R RT ENG. UPON REMOVAL MX FOUND LOWER ENG COWL OIL SOAKED. SERVICED ENG WITH 5 QTS OF OIL. MX ALSO FOUND CONNECTOR ON OIL PRESS TRANSMITTER LOOSE. ENG RAN ON DELTA'S TEST CELL WITH NO LEAKS OR OIL CONSUMPTION. UPON ENG TEAR DOWN MX FOUND SEVERAL AGB CARBON SEALS LEAKING & REPLACED. OPS CHECKS GOOD. ENG RETURNED TO SERVICE. (M)

Part: INTERCOSTAL — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE INTERCOSTAL AT FS 484, LBL 27 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE INTERCOSTAL AT FS 484, LBL 27 IAW ASA EO 600-53-0098. (M)

Part: FLOOR SUPPORT — CRACKED (FUSELAGE)

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

Part: INTERCOSTAL — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE CARGO FLOOR THRESHOLD SILL AT THE AFT INTERCOSTAL WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CARGO FLOOR THRESHOLD SILL AT THE AFT INTERCOSTAL IAW ASA EO 600-53-0117. (M)

Part: CLIP — CRACKED (FUSELAGE)

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

Part: SILL — CRACKED (FUSELAGE)

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

Part: DOOR — MALFUNCTIONED (MAIN PAX)

FLT 4409 - DURING A GROUND INSPECTION IN DFW, THE FILGHT ATTENDANT REPORTED THE PASSENGER DOOR WAS HARD TO CLOSE. MAINTENANCE PERFORMED OPERATIONAL TEST ON THE PASSENGER DOOR WITHOUT ANY DEFECTS NOTED. AIRCRAFT OK FOR SERVICE. (M)

Part: DOOR — MALFUNCTIONED (MAIN PAX)

DURING A GROUND INSPECTION IN DFW, THE FLIGHT ATTENDANT COULD NOT GET THE PASSENGER DOOR TO CLOSE. MAINTENANCE OPERATED THE PASSENGER DOOR SEVERAL TIMES AND WAS UNABLE TO DUPLICATE THE DISCREPANCY. AIRCRAFT OK FOR SERVICE. (M)

Part: FITTING — BINDING (EMERGENCY DOOR)

FLT 4643 - DURING A TRAINING EXERCISE IN ATL, THE LEFT OVERWING EMERGENCY EXIT DOOR AT ROW 8 A/B COULD NOT BE OPENED. MAINTENANCE ADJUSTED THE BEYONET LATCH FITTINGS ON THE LEFT OVERWING EMERGENCY EXIT DOOR AT ROW 8 A/B. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: MECHANISM — LACK OF LUBE (PAX DOOR)

DURING A GROUND INSPECTION IN ATL, THE PASSENGER DOOR WAS DIFFICULT TO OPEN FROM THE OUTSIDE. MAINTENANCE LUBRICATED THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: HINGE — CRACKED (PAX DOOR)

DURING A GROUND INSPECTION IN DFW, THE PASSENGER DOOR TOP STEP HINGE WAS FOUND TO BE CRACKED AND CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR TOP STEP HINGE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: STEP — CRACKED (FUSELAGE)

DURING GROUND INSPECTION IN ATL, THE FLIGHT ATTENDANT REPORTED THE HYDRAULIC ASSIST ON THE MAIN CABIN DOOR CABLE WAS INOPERATIVE. UPON INSPECTION MAINTENANCE FOUND THE BOTTOM STEP ON THE PASSENGER DOOR BROKEN. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: STEP — BROKEN (PAX DOOR)

FLT 4244 - DURING A GROUND INSPECTION IN ATL, THE BOTTOM STEP ON THE MAIN PASSENGER DOOR WAS FOUND TO BE BROKEN. MAINTENANCE REMOVED AND REPLACD THE BOTTOM STEP ON THE MAIN PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LAMP — BURNED OUT (CABIN)

FLT 4134 - DURING A GROUND INSPECTION IN SHV, THE LEFT FORWARD EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LEFT FORWARD EMERGENCY EXIT LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: FITTING — LEAKING (ENGINE)

FLT 4383 - DURING CLIMB-OUT FROM MGM-DFW, AT APPROXIMATELY 22,000 FEET THE CREW RECEIVED A RIGHT ENGINE OIL PRESSURE MASTER WARNING MESSAGE WITH THE OIL PRESSURE DROPPING RAPIDLY TO ZERO PSI. QRH PROCEDURES WERE COMPLIED WITH AND THE CREW SHUT DOWN THE RIGHT ENGINE. THE AIRCRAFT DIVERTED TO MLU AND EMERGENCY VEHICLES WERE REQUESTED AS A PRECAUTION. THE AIRCRAFT LANDED SAFELY IN MLU. MAINTENANCE FOUND THE RIGHT ENGINE MAIN OIL TANK EMPTY, REMOVED AND REPLACED THE SCAVENGE PUMP LINE AND REDUCER FITTINGS. OPERATIONAL AND LEAK AND CHECKS GOOD. AIRCRAFT OK FOR SERVICE. THE AIRCRAFT WAS FERRIED TO MCN AND THE RIGHT ENGINE WAS REMOVED AND REPLACED FOR TEARDOWN INSPECTION OF THE MAIN LINE BEARING AS A PRECAUTION

Part: STEP — BROKEN (PAX DOOR)

FLT 4312 - DURING A GROUND INSPECTION IN DFW, THE ATTACH POINT ON THE LOWER RETRACTABLE PASSENGER DOOR STEP BRACKET WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE LOWER STEP ASSEMBLY ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: FRAME — CRACKED (FUSELAGE)

WHILE COMPLYING WITH ASA EO NR 600-53-0069, FOUND RIGHT ANGLE IN FRAME CRACKED BETWEEN STRINGER 9/10 AND AT RADIUS BETWEEN STRINGERS 13/14. REPAIRED CRACKED FRAMES IAW SRM 51-00 AND REO NR 601R-53-61-576. (M)

Part: FRAME — CRACKED (FUSELAGE)

DURING C-CHECK INSPECTION IN MCN, LEFT AND RIGHT FRAME STATION 718 WAS FOUND TO BE CRACKED BETWEEN STRINGERS 10 AND 12. MAINTENANCE REPAIRED THE CRACKED FRAME IAW ASA E0600-53-0067A. (M)

Part: SUPPORT — CRACKED (FUSELAGE)

WHILE COMPLYING WITH ASA EO600-53-0043A, INSPECTION OF THE ENGINE SUPPORT BEAM, CRACKS WERE FOUND AT THE LEFT AND RIGHT ACCESS PANEL LOWER WEB AND THE UPPER WEB AT THE CENTER AFT SIDE. MAINTENANCE WILL REPAIR THE CRACKED ENGINE SUPPORT BEAM IAW ASA EO 600-53-0070. (M)

Part: LIGHT — INOPERATIVE (EXTERIOR)

DURING A HANGAR INSPECTION IN MCN, THE FORWARD MOST EXTERNAL EMERGENCY LIGHT ON THE LEFT SIDE OF THE FUSELAGE WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BURNED OUT EMERGENCY LIGHT BULB. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: CHARGER — FAILED (CABIN)

DURING GROUND INSPECTION IN ATL, THE LAST FEW SECTIONS OF FLOOR EMERGENCY LIGHTING WERE DISCOVERED INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHTING BATTERY PACK CHARGER. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING GROUND INSPECTION IN ATL, THE LAST FEW SECTIONS OF FLOOR EMERGENCY LIGHTING WERE DISCOVERED INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHTING BATTERY PACK IN THE NR 4 POSITION. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: BATTERY PACK — WEAK (CABIN)

DURING TESTING OF EMERGENCY LIGHTS, THE EMERGENCY LIGHTS AT ROWS 10-12 WERE FOUND INOPERATIVE. MAINTENANCE CHARGED THE EMERGENCY LIGHTING BATTERY PACKS. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE.

Part: HYDRAULIC LINE — CHAFED (HYDRAULIC SYS)

FLT 4751 - DURING FLIGHT FROM ROA TO ATL, PILOT REPORTED ALL FLUID IN THE LEFT HYDRAULIC SYSTEM LOST. AN EMERGENCY WAS DECLARED. AIRCRAFT RETURNED AND LANDED SAFELY IN ROA. MAINTENANCE INSPECTED AIRCRAFT AND FOUND THE HYDRAULIC RESERVOIR SUMP SUCTION LINE CHAFED. MAINTENANCE REPAIRED CHAFED LINE AS WELL AS REMOVED AND REPLACED THE LEFT HYDRAULIC ENGINE DRIVEN PUMP. LEAK AND OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: HYDRAULIC LINE — CHAFED (HYD SYSTEM)

FLT 4572 - CLIMBING THROUGH FL250 INFLIGHT FROM ATL TO CRP, CREW RECEIVED A HYDRAULIC NR 1 LOW PRESSURE MESSAGE. HYDRAULIC QUANTITY IN SYSTEM NR 1 INDICATED ZERO PERCENT. CREW DECLARED AN EMERGENCY AND DIVERTED TO BHM. AIRCRAFT LANDED SAFELY. MAINTENANCE FOUND CHAFFED STEEL BRAIDED HYDRAULIC LINE IN APU BAY. MAINTENANCE REMOVED AND REPLACED LINE AND NR 1 ENGINE HYDRAULIC PUMP. OPS AND LEAK CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY — DISCHARGED (CABIN)

DURING INSPECTION, FOUND NR 2 AND NR 4 EMERGENCY BATTERY PACKS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED NR 2 AND NR 4 EMERGENCY BATTERY PACKS. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (X)