N821AS

Part: SENSOR — OUT OF ADJUST · airframe 39,862 hrs · 38,090 cycles

NOSE DOOR OPEN, GEAR DISAGREE WARNING MESSAGE, AFTER GEAR IS SELECTED UP, PERFORMED QRH, MESSAGES CLEARED, RETURNED TO FIELD. ADJUSTED WOW SENSOR. SWUNG GEAR MULTIPLE TIMES. NO DEFECTS NOTED.

Part: LINE — FAILED (FUEL CONTROL) · airframe 38,113 hrs · 36,003 cycles

DURING CLIMBOUT, NR 2 ENGINE ROLLED BACK TO IDLE. RETURNED TO FIELD. R & R RT ENGINE P3 LINE TO FUEL CONTROL TUBE ASSEMBLY WITH A SERVICEABLE UNIT IAW AMM. OPS CHECKED GOOD.

Part: TUBE — BROKEN (PAX DOOR) · airframe 37,996 hrs · 35,864 cycles

PAX DOOR WIRE HARNESS UNDER TOP STEP HAS BROKEN TUBING, REPAIRED THE TUBING IAW GREO.

Part: HINGE — GOUGED (PAX DOOR) · airframe 37,996 hrs · 35,864 cycles

PASSENGER DOOR HINGE HALF LUG NR 27 FROM FORWARD SIDE HAS GOUGES. REPAIRED THE HINGE LUG IAW REO.

Part: ANGLE — CRACKED (BS 280) · airframe 37,996 hrs · 35,864 cycles

LBL 9, BS 280 INBD ANGLE IS CRACKED AT UPPER RADIUS. INSTALLED FABRICATED INBD ANGLE IAW REO.

Part: HINGE — GOUGED (PAX DOOR) · airframe 37,996 hrs · 35,864 cycles

PASSENGER DOOR FUSELAGE SIDE HINGE HALF 6TH AND 8TH LUG FROM FORWARD SIDE HAVE GOUGES. BLENDED GOUGE ON PAX DOOR HINGE LUGS NR 6 AND NR 8 IAW REO.

Part: STRUCTURE — CRACKED (AFT CARGO BAY) · airframe 37,996 hrs · 35,864 cycles

AFT CARGO BAY AT BS 605 HAS A CRACK AT CARGO DOOR. PERFORMED CUT OUT OF DAMAGED AREA ON FLOOR LANDING PLATE AT FS 605.0, REF REO. PERFORMED ET INSP ON REWORKED AREA AND UNDERLAYING STRUCTURE IAW REO. NO DEFECTS NOTED, BTAC NDT-9, TOUCHED UP REWORKED AREA REF REO. PLUGGED REDUNDANT HOLE WITH MS20470AD5 RIVET, REF REO.

Part: BULKHEAD — CRACKED (BS 202) · airframe 37,996 hrs · 35,864 cycles

BS 202 BULKHEAD IS CRACKED AT THE PARKING BRAKE CABLE PASSTHROUGH HOLE. REPAIRED THE BULKHEAD IAW REO.

Part: FLOOR SKIN — CRACKED (TRU BAY) · airframe 37,996 hrs · 35,864 cycles

TRU BAY FLOOR SKIN IS CRACKED AT BS 193. REPAIRED TRU BAY FLOOR SKIN IAW REO.

Part: ANGLE — CRACKED (BS 280) · airframe 37,996 hrs · 35,864 cycles

BS 280, RBL 9.0 INBD AND OTBD ANGELS ARE CRACKED AT UPPER RADIUS. R & R THE ANGLES IAW REO.

Part: ATTACH ANGLE — CRACKED (BS 202) · airframe 37,996 hrs · 35,864 cycles

CRACKED ATTACH ANGLE STRINGER TO BS 202 BULKHEAD IN AFT LOWER AREA OF NOSE HYDRAULIC COMPARTMENT. R & R ATTACH ANGLE IAW SRM AND EA.

Part: LEVER — WORN (PAX DOOR) · airframe 37,996 hrs · 35,864 cycles

PASSENGER DOOR FORWARD PULL IN LEVER LOBE WORN. REPAIRED IAW REO.

Part: PANEL — CRACKED (COCKPIT) · airframe 37,996 hrs · 35,864 cycles

COCKPIT PANEL 221ALC CRACKED & BROKEN IN MULTIPLE PLACES. REPAIRED DAMAGED AREAS ON PANEL IAW EA.

Part: ATTACH FITTING — CHAFED (LT MLG) · airframe 37,996 hrs · 35,864 cycles

LEFT MLG STRUT TO BELLCRANK ATTACHMENT POINT CHAFED. REMOVED AND INSTALLED SCREW ATTACHING BELLCRANK TO THE ROD IAW SRM 51-41-02. BLENDED CHAFE DAMAGE ON LT MLG STRUT-TO-BELL CRANK ATTACHMENT POINT REF REO. EVALUATION, ORIGINAL MATERIAL THICKNESS .140" TOOL TUC4790 DUE 31-MAR-2015. REMAINING MATERIAL THICKNESS .132" TOOL TUC4790 DUE 31-MAR-2015. MATERIAL REMOVED .008". ALLOWABLE MATERIAL LOSS .014". BLEND FOUND TO BE WITHIN LIMITS. RESTORED FINISH TO BLENDED AREA REF SRM.

Part: ATTACH FITTING — CHAFED (MLG) · airframe 37,996 hrs · 35,864 cycles

RIGHT MLG STRUT TO BELLCRANK ATTACHMENT POINT CHAFED. REMOVED AND INSTALLED BOLT ATTACHING RT MLG BELLCRANK TO THE ROD IAW SRM. BLENDED CHAFE DAMAGE ON RT MLG BELLCRANK IAW REO. BLEND FOUND TO BE WITHIN LIMITS IAW REO. RESTORED FINISH TO BLENDED AREA IAW SRM.

Part: STRUCTURE — CORRODED (UNKNOWN) · airframe 37,996 hrs · 35,864 cycles

CORROSION AROUND NUTPLATE HOLE UNDER PANEL 141BL. C-CHECK, REPAIRED IAW REO.

Part: PANEL — CHAFED (RT WING) · airframe 37,996 hrs · 35,864 cycles

RIGHT WING BUTTE PANEL 694PB HAS CHAFE DAMAGE ON UPPER SURFACE. REPAIRED PANEL IAW EA.

Part: FITTING — CHAFED (THRUST REVERSER) · airframe 37,996 hrs · 35,864 cycles

RIGHT ENGINE THRUST REVERSER HAS BOTTOM INBD MAIN TRACK AFT END FITTING CHAFED, UPPER SIDE. REPAIRED THE THRUST REVERSER INBD LOWER MAIN TRACK AND ANCHOR FITTING IAW GREO.

Part: SKIN — DENTED (SPOILER) · airframe 37,996 hrs · 35,864 cycles

RIGHT WING INBD GROUND SPOILER HAS MULTIPLE SMALL DENTS ON LOWER SURFACE. DENTS ARE WITHIN ALLOWABLE LIMITS, NO FURTHER ACTION REQUIRED, REF REO.

Part: PANEL — FAILED (VISOR) · airframe 37,996 hrs · 35,864 cycles

RIGHT UPPER VISOR PANEL 326AR FAILED GAP CHECK. REPAIR VISOR PANEL 326AR IAW REO.

Part: PANEL — FAILED (VISOR) · airframe 37,996 hrs · 35,864 cycles

LEFT UPPER VISOR PANEL 326AL, FAILED GAP CHECK. REPAIR VISOR PANEL IAW REO.

Part: SKIN — CHAFED (CARGO DOOR) · airframe 37,996 hrs · 35,864 cycles

CARGO BAY DOOR EXTERIOR SKIN HAS SIX CHAFES AROUND THE RIM OF THE DOOR HANDLE. R & R THE DOOR HANDLE ASSY IAW SRM. PERFORMED OPS CHECK OF THE CARGO DOOR WARNING SYSTEM IAW AMM AND REO.

Part: VANE — CRACKED (APU EXHAUST) · airframe 37,996 hrs · 35,864 cycles

BOTTOM VANE OF APU EXHAUST OUTLET IS CRACKED. REPAIED IAW REO.

Part: STRUCTURE — ERODED (LT ENGINE) · airframe 37,996 hrs · 35,864 cycles

FOUND EROSION ON THE LT ENGINE NOSE COWL, 6 O'CLOCK POSITION, TO BE WITHIN LIMITS. REPAIRED IAW CMM AND REO.

Part: FIRE BOTTLE — DISCHARGED (CARGO BAY) · airframe 37,288 hrs · 35,059 cycles

IN FLIGHT GOT CARGO BOTTLE LOW MESSAGE. RETURNED TO DEPARTURE. R & R LT CARGO BOTTLE.

Part: LINE — BLOWN (UNKNOWN) · airframe 37,256 hrs · 35,023 cycles

RETURNED TO FIELD WITH A BLOWN FIRE BOTTLE. REINSTALLED A DISCONNECTED LINE BLOWING HOT AIR ON THE FIRE BOTTLE.

Part: FIRE BOTTLE — FAILED (CARGO BAY) · airframe 37,246 hrs · 35,013 cycles

CARGO BOTTLE LOW MESSAGE. REPLACED THE SMALL CARGO FIRE BOTTLE.

Part: O-RING — LEAKING (APU FUEL) · airframe 36,968 hrs · 34,722 cycles

WITH PACKS ON, APU STRONG FUEL ODOR THROUGHOUT FLIGHT DECK AND CABIN. WITH PACKS ON ENGINES ODOR DIMINISHES. REPLACED O-RING ON FUEL CONTROL ELBOW TO FUEL SOLENOID, LEAK AND OPS CHECKED GOOD IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,443 hrs · 34,160 cycles

LOWER EXIT LIGHTS ON MAIN CABIN DOOR & GALLEY SERVICE DOOR ARE BURNED OUT. FLT 2938 RELAMPED.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 36,134 hrs · 33,819 cycles

EMERGENCY LIGHTS DO NOT ILLUMINATE. FLT 2971 CHARGED EMERGENCY LIGHTS BATTERY PACKS.

Part: WIRE — OUT OF POSITION (CABIN) · airframe 34,890 hrs · 32,540 cycles

EMERGENCY EXIT LIGHT NEAR MAIN CABIN DOOR DOES NOT ILLUMINATE. REPOSITIONED WIRES BEHIND EMERGENCY LIGHT.

Part: PROXIMITY SWITCH — FAILED (PAX DOOR) · airframe 34,842 hrs · 32,488 cycles

RECEIVED PASSENGER DOOR OUTER HANDLE CAUTION MESSAGE. REPLACED PROXIMITY SWITCH. OPS CHECKED GOOD.

Part: UNKNOWN — FUMES (CABIN) · airframe 34,652 hrs · 32,308 cycles

SMELLING FUMES IN CABIN. (FLT 2980) INSPECTED APU ENCLOSURE. BOTH AC PACKS HAVE NORMAL INDICATION WITH NO SIGNS OF OVERHEATING. NO SMOKE SMELLS NOTED.

Part: FAN — MALFUNCTIONED (GALLEY) · airframe 34,573 hrs · 32,227 cycles

ELECTRICAL SMOKE SMELL COMING FROM GALLEY A/C VENT. NO SMOKE AND NO PAX ON BOARD. (FLT 2962) REPLACED GALLEY EXHAUST FAN. OPS CHECK GOOD AT THIS TIME. P/N ON: AE0405A01 P/N OFF: AE0405A02 S/N ON: 1145 S/N OFF: L0865

Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,306 hrs · 31,951 cycles

OVERHEAD EMERGENCY EXIT ROW LIGHT BURNED OUT. (FLT 2850) RELAMPED EMERGENCY LIGHT.

Part: BRAKE — SEIZED (LT MLG) · airframe 34,258 hrs · 31,901 cycles

LEFT MAIN BRAKE SEIZED. (FLT 2988) REPLACED NR 1 MLG WHEEL ASSEMBLY, RE-INSTALLED QUICK DISCONNECT. P/N 501071-1 S/N ON FEB01-3686 S/N OFF APR97-1354 P/N 5010520-1 S/N ON APR99-1669 S/N OFF NOV02-3692

Part: ACCESS PANEL — CORRODED (LT WING) · airframe 34,169 hrs · 31,811 cycles

LEFT WING ACCESS PANEL 540EB HOLE HAS SIGNS OF CORROSION IN SEVERAL AREAS. (C-CHECK) LOWER WING PLANK CUTOUT COMMON TO PANEL 540EB REWORKED IAW REO.

Part: ACCESS PANEL — CORRODED (RT WING) · airframe 34,169 hrs · 31,811 cycles

RIGHT WING ACCESS PANEL 650BB HOLE HAS SIGNS OF CORROSION IN SEVERAL AREAS. (C-CHECK) LOWER WING PLANK CUTOUT COMMON TO PANEL 650BB REPAIRED IAW REO.

Part: ACCESS PANEL — CORRODED (LT WING) · airframe 34,169 hrs · 31,811 cycles

LEFT WING ACCESS PANEL 550HB HOLE HAS SIGNS OF CORROSION IN SEVERAL AREAS. (C-CHECK) LOWER WING PLANK CUTOUT COMMON TO PANEL 550HB REPAIRED IAW REO.

Part: ACCESS PANEL — CORRODED (RT WING) · airframe 34,169 hrs · 31,811 cycles

RIGHT WING ACCESS PANEL 640BB HOLE HAS SIGNS OF CORROSION IN SEVERAL AREAS. (C-CHECK) LOWER WING PLANK COMMON TO PANEL 640BB REPAIRED IAW REO.

Part: ACCESS PANEL — CORRODED (RT WING) · airframe 34,169 hrs · 31,811 cycles

RIGHT WING ACCESS PANEL 640FB HOLE HAS SIGNS OF CORROSION IN SEVERAL AREAS. (C-CHECK) RIGHT LOWER WING PLANK CUTOUT COMMON TO PANEL 640FB REWORKED IAW REO.

Part: ACCESS PANEL — CORRODED (RT WING) · airframe 34,169 hrs · 31,811 cycles

RIGHT WING ACCESS PANEL 650HB HOLE HAS SIGNS OF CORROSION IN SEVERAL AREAS. (C-CHECK) CORROSION AT LOWER WING PLANK COMMON TO PANEL 650HB REPAIRED IAW REO.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 34,169 hrs · 31,811 cycles

FLOOR SUPPORT AT FS 621 LBL 9 UNDER FLOORBOARD 281JLF HAS FRETTING CORROSION. (C-CHECK) INSTALLED NEW FLOOR SUPPORT AT LBL 9 FS 574-621 IAW REO.

Part: ACCESS PANEL — CORRODED (LT WING) · airframe 34,169 hrs · 31,811 cycles

LEFT WING ACCESS PANEL 550AB HOLE HAS SIGNS OF CORROSION IN SEVERAL AREAS. (C-CHECK) LEFT LOWER WING PLANK COMMON TO ACCESS PANEL 550AB REWORKED IAW REO.

Part: ACCESS PANEL — CRACKED (LT WING) · airframe 34,169 hrs · 31,811 cycles

LEFT WING ACCESS PANEL 510AB HOLE HAS SIGNS OF CORROSION IN SEVERAL AREAS. (C-CHECK) LOWER WING PLANK CUTOUT COMMON TO PANEL 510AB REWORKED IAW REO.

Part: ACCESS PANEL — CORRODED (RT WING) · airframe 34,169 hrs · 31,811 cycles

RIGHT WING ACCESS PANEL 640AB HOLE HAS SIGNS OF CORROSION IN SEVERAL AREAS. (C-CHECK) RIGHT LOWER WING PLANK ACCESS PANEL CUTOUT COMMON TO PANEL 640AB REWORKED IAW REO.

Part: ACCESS PANEL — CORRODED (RT WING) · airframe 34,169 hrs · 31,811 cycles

RIGHT WING ACCESS PANEL 640DB HOLE HAS SIGNS OF CORROSION IN SEVERAL AREAS. (C-CHECK) RIGHT LOWER WING PLANK CUTOUT COMMON TO PANEL 640DB REWORKED IAW REO.

Part: ACCESS PANEL — CORRODED (LT WING) · airframe 34,169 hrs · 31,811 cycles

LEFT WING ACCESS PANEL 540BB HOLE HAS SIGNS OF CORROSION IN SEVERAL AREAS. (C-CHECK) MARKED AREAS OF LOWER WING PLANK COMMON TO PANEL 540BB REWORKED IAW REO.

Part: POST — CRACKED (FUSELAGE) · airframe 34,169 hrs · 31,811 cycles

CRACK NOTED & MARKED ON FS 409.0+128 VERT POST AT RBL 18.00 WL 69.00 OUTBOARD AFT RADIUS. (C-CHECK) REMOVED AND REPLACED FS 409+128 VERT POST RBL18 IAW REO.

Part: POST — CRACKED (FUSELAGE) · airframe 34,169 hrs · 31,811 cycles

CRACK NOTED & MARKED ON FS 409.0+128 VERT POST AT LBL 18.00 WL 69.00 OUTBOARD AFT RADIUS. (C-CHECK) REMOVED AND REPLACED FS 409.0+128 VERT POST AT LBL 18.00 WL 69.00 OUTBOARD POST IAW REO.

Part: POST — CRACKED (FUSELAGE) · airframe 34,169 hrs · 31,811 cycles

CRACK NOTED & MARKED ON FS 409.0+128 VERT POST AT RBL 18.00 WL 69.00 INBOARD AFT RADIUS. (C-CHECK) REMOVED AND INSTALLED NEW RBL 18 I/B VERTICAL POST AT FS 409+128 IAW REO.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 34,169 hrs · 31,811 cycles

CRACK NOTED & MARKED ON FS 409.0+128 VERT POST RIGHT CLIP AT BL 0.00 WL 69.00 OUTBOARD AFT RADIUS. (C-CHECK) REPLACED FS 409+128 POST BL 0.00 RIGHT VERTICAL POST USING AND STIFFENER ANGLE IAW REO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 34,169 hrs · 31,811 cycles

CRACK NOTED AND MARKED ON FS 621 BULKHEAD WEB, FWD FACE, ABOVE UPPER CARGO DOOR TRACK FITTING. (C-CHECK) REPAIRED FS 621 BULKHEAD WEB, FWD FACE, ABOVE UPPER CARGO DOOR TRACK FITTING IAW REO.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,058 hrs · 31,689 cycles

EMERGENCY LIGHTS AT MAIN CABIN DOOR AND GALLEY DOOR BURNED OUT. (FLT 2974) RELAMPED EMERGENCY LIGHTS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,779 hrs · 31,403 cycles

GALLEY EMERGENCY EXIT LAMP IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: PROXIMITY SWITCH — OUT OF POSITION (CABIN DOOR) · airframe 33,490 hrs · 31,105 cycles

MAIN CABIN DOOR HANDLE TRIGGER IS DIFFICULT TO OPEN FROM OUTSIDE. (FLT 2932) FOUND PASSENGER DOOR OUTER HANDLE PROXIMITY SWITCH TO BE OBSTRUCTING THE HANDLE. ADJUSTED SWITCH IAW AMM.

Part: LIGHT — BROKEN (CABIN) · airframe 32,808 hrs · 30,399 cycles

EMERGENCY EXIT LIGHT ON THE SIDE OF GALLEY NEAR THE GALLEY DOOR IS BROKEN. (FLT 2920) REPLACED EXIT LIGHT ON SIDE OF GALLEY.

Part: DOOR — DIRTY (MAIN CABIN) · airframe 32,554 hrs · 30,133 cycles

FLT 2979, THE MAIN CABIN DOOR IS DIFFICULT TO OPEN AND CLOSE. CLEANED AND LUBRICATED MAIN CABIN DOOR HANDLE END LOCKING MECHANISM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,508 hrs · 30,089 cycles

OVERHEAD EMERGENCY LIGHT IS OUT IN GALLEY. (FLT 2981) RELAMPED EMERGENCY LIGHT.

Part: CIRCUIT BREAKER — TRIPPED (EMERGENCY LIGHT) · airframe 31,054 hrs · 28,519 cycles

EMERGENCY LIGHTS IN CABIN COME ON WHEN SWITCH IS IN THE ARMED POSITION. RESET CIRCUIT BREAKER NO FAULTS AT THIS TIME. REF AMM 33-51-00.

Part: HANDLE — LACK OF LUBE (MAIN DOOR) · airframe 30,970 hrs · 28,425 cycles

MAIN DOOR REQUIRES EXCESSIVE FORCE TO OPERATE TEE HANDLE, REPEAT WRITE UP. LUBRICATED PAX DOOR INNER HANDLE IAW AMM 52-11-00, NO DEFECT NOTED. (CLOSED)

Part: SEAT TRACK — CORRODED (CABIN) · airframe 30,571 hrs · 27,977 cycles

RIGHT NR 2 SEAT TRACK IS CORRODED. REMOVED AND REPLACED RT NR 2 SEAT TRACK IAW AMM 53-01-11 RII FOUND TO BE SATISFACTORY.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 30,571 hrs · 27,977 cycles

FS 280 CENTER FLOORBEAM UPPER SURFACE IS CORRODED. REMOVED CORROSION. ALODINED, PRIMED AND TOP COATED IAW SRM 51-21-06, 51-21-11, 51-25-06, 51-25-16.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 30,571 hrs · 27,977 cycles

LEFT SEAT TRACK OVER LBL 27 IN CARGO AREA CORRODED. R & R SEAT TRACK IAW AMM 53-01-11.

Part: PRESSURE PANEL — DAMAGED · airframe 30,571 hrs · 27,977 cycles

PRESSURE PANEL 132AL FUSELAGE CUTOUT HAS ON DAMAGED AND ELONGATED FASTENER HOLE. COMPLIED WITH EC/TC REO 601R-53-11-162 REPAIR TO PRESSURE PANEL 132 AL FUSELAGE CUTOUT FASTENER HOLE IAW REO 601R-53-11-162 REV. B THIS IS A MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 30,571 hrs · 27,977 cycles

LEFT NR 4 SEAT TRACK CORRODED. R & R SEAT TRACK IAW AMM 53-01-11.

Part: ATTACH FITTING — CRACKED (BS 280) · airframe 30,571 hrs · 27,977 cycles

LBL 9 FS 280 O/B CLIP IS CRACKED. R & R IAW SRM 51-40-11 AND 51-42-21.

Part: BULKHEAD — SCRATCHED (BS 621) · airframe 30,576 hrs · 27,983 cycles

BS 621 BULKHEAD FWD FACE HAS 12 EA SCREW MARKS (CIRCLED). COMPLIED WITH EC/TC REO 601R-53-61-2155 AND MET ALL THE REQUIREMENTS OF REO 601R-53-61-2155. THIS IS A MAJOR REPAIR. RII FOUND TO BE SATISFACTORY.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 30,576 hrs · 27,983 cycles

FLOORBEAM BETWEEN 281LLF AND 281JLF HAS SURFACE CORROSION. REMOVED DAMAGED FLOORBEAM BETWEEN 281LLF & 281JLF AND REPLACED WITH NEW SERVICEABLE BEAM. DUPLICATED FROM N126-1577 EXTRUSION IAW SRM 51-42-06. RII FOUND TO BE SATISIFACTORY. 5001437 HEATER OPS CK GOOD IAW AMM 21-55-04-710-801.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 30,571 hrs · 27,977 cycles

RIGHT SEAT TRACK NR 3 HAS CORROSION. R & R SEAT TRACK IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 30,571 hrs · 27,977 cycles

RIGHT NR 6 SEAT TRACK IS CORRODED. R & R SEAT TRACK IAW AMM 53-01-11.

Part: ATTACH FITTING — CRACKED (BS 280) · airframe 30,571 hrs · 27,977 cycles

RBL 9 FS 280 I/B CLIP IS CRACKED. R & R IAW SRM 51-40-11 AND 51-42-21.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 30,571 hrs · 27,977 cycles

RIGHT NR 1 SEAT TRACK IS CORRODED. R & R SEAT TRACK IAW AMM 53-01-11.

Part: SKIN — CORRODED (FUSELAGE) · airframe 30,571 hrs · 27,977 cycles

NUMEROUS AREAS OF CORROSION ON AIRCRAFT SKIN BELOW SERVICE DOOR BEHIND SCUFF PLATE. NUMEROUS ANCHOR NUTS HAVE CORRODED RIVETS. REMOVED MINOR CORROSION . NO MATERIAL LOSS NOTED IAW SRM 51-21-06.

Part: ISOLATOR — CRACKED (BS 621 BULKHEAD) · airframe 30,571 hrs · 27,977 cycles

ISOLATOR CRACKED ON 621 BULKHEAD. REMOVED UNSERVICABLE ISOLATOR AND INSTALLED SERVICABLE ISOLATOR IAW SRM 51-42-13.

Part: FLOORBEAM — CORRODED (BS 589) · airframe 30,571 hrs · 27,977 cycles

FLOORBEAM AT FS 589.00 TO BL 27.0 CORRODED. REMOVED CORROSION IAW SRM 51-21-06.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 30,571 hrs · 27,977 cycles

RIGHT NR 4 SEAT TRACK CORRODED. R & R SEAT TRACK IAW AMM 53-01-11.

Part: ATTACH FITTING — CORRODED (PAX DOOR) · airframe 30,571 hrs · 27,977 cycles

PAX DOOR AFT CLEAT IS CORRODED. REMOVED UNSERVICEABLE PAX DOOR CLEAT AND BRACKET P/N 601R31527-217 AND INSTALLED SERVICEABLE CLEAT AND BRACKET IAW SRM 51-42-06 THIS IS A MAJOR REPAIR RII FOUND TO BE SATISFACTORY.

Part: ISOLATOR — BROKEN (BS 621 BULKHEAD) · airframe 30,571 hrs · 27,977 cycles

BS 621 BULKHEAD HAS BROKEN ISOLATOR. REMOVED UNSERVICABLE ISOLATOR AND INSTALLED SERVICABLE ISOLATOR IAW SRM 51-42-13.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 30,571 hrs · 27,977 cycles

LEFT NR 1 SEAT TRACK IS CORRODED. R & R SEAT TRACK IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 30,571 hrs · 27,977 cycles

LEFT NR 5 SEAT TRACK CORRODED. R & R SEAT TRACK IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 30,571 hrs · 27,977 cycles

RIGHT NR 5 SEAT TRACK IS CORRODED. R & R SEAT TRACK IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (LAVATORY) · airframe 30,571 hrs · 27,977 cycles

BOTH SEAT TRACKS IN LAVATORY AREA HAVE CORROSION.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 30,571 hrs · 27,977 cycles

FLOOR SUPPORT UNDER FLOORBOARD 231CLF ARE CORRODED IN AREA AROUND PAX DOOR HANDRAIL RECESSES. BLENDED MINOR CORROSION, MATERIAL LOSS .002 REMAINING MATERIAL AND IS WITHIN SERVICEABLE LIMITS IAW SRM 53-00-00.

Part: SEAT TRACK — CORRODED · airframe 30,571 hrs · 27,977 cycles

LEFT NR 3 SEAT TRACK HAS CORRODED HARDWARE AND IS GOUGED. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (BS 499) · airframe 30,571 hrs · 27,977 cycles

RIGHT SEAT TRACK AROUND FS 499 HAS CORROSION. REPLACED SEAT TRACK FROM FS 409+128 TO 559+20.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 30,571 hrs · 27,977 cycles

LEFT NR 6 FLOOR SEAT TRACK CORRODED. R & R SEAT TRACK IAW AMM 53-01-11.

Part: PRESSURE PANEL — DAMAGED · airframe 30,571 hrs · 27,977 cycles

PRESSURE PANEL 131AL FUSELAGE CUTOUT HAS SEVEN ELONGATED FASTNER HOLES. COMPLIED WITH EC/TC REO 601R-53-11-162. REPAIRS TO PRESSURE PANEL 131 AL FUSELAGE CUTOUT FASTENER HOLES IAW REO601R-53-11-162 ERV B THIS IS A MAJOR REPAIR

Part: BULKHEAD — SCRATCHED (BS 621) · airframe 30,571 hrs · 27,977 cycles

BS 621 BULKHEAD HAS SCRATCH IN FWD FACE. BLENDED SCRATCHED AREA ON BS 621 FWD BULKHEAD LBL27 REMOVED .003 OF MATERIAL. REMAINING MATERIAL IS STILL WITHIN SERVICEABLE LIMITS IAW REO 53-61-2155. BLENDED IAW CRJ 200 SRM 51-12-00. THIS IS A MAJOR REPAIR. COMPLIED WITH ECTC REO 601R-53-61-2155, AND MET ALL THE REQUIREMENTS OF REO 601R-53-61-2155.

Part: ATTACH BRACKET — CRACKED (LT WING) · airframe 30,571 hrs · 27,977 cycles

HINGE ARM ASSEMBLY AT WS.220.0 LT, CRACKED FWD O/B ATTACH BRACKET. REMOVED UNSERVICEABLE BRACKET AND REPLACED WITH NEW SERVICEABLE BRACKET IAW SRM 51-42-06.

Part: ATTACH FITTING — CORRODED (BS 280) · airframe 30,571 hrs · 27,977 cycles

RBL 9 FS 280 O/B ATTACH FITTING IS CRACKED. R & R IAW SRM 51-40-11 AND 51-42-21.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 30,571 hrs · 27,977 cycles

CORROSION ON FLOOR SUPPORT JUST FORWARD OF SERVICE DOOR. REMOVED AND REPLACED FLOOR SUPPORT ANGLE JUST FWD OF SERVICE SRM 51-42-06.

Part: SEAT TRACK — CORRODED (BS 486) · airframe 30,571 hrs · 27,977 cycles

LEFT SEAT TRACK APPROXIMATELY FS 486 HAS CORROSION. REPLACED SEAT TRACK.

Part: BRACKET — DAMAGED (BS 621 BULKHEAD) · airframe 30,571 hrs · 27,977 cycles

BS 621 BULKHEAD HAS 1 EA DAMAGED BRACKET AND BROKEN ISOLATORS. REMOVED UNSERVCIABLE ISOLATORS AND INSTALLED SERVICABLE ISOLATORS IAW SRM 51-42-13.

Part: ATTACH FITTING — CRACKED (BS 484) · airframe 30,571 hrs · 27,977 cycles

RIGHT I/B BS 484 CLIP RBL 36 APPEARS TO BE CRACKED. R & R IAW REO 601R-53-41-059, REV B.

Part: HANDLE — GOUGED (CARGO DOOR) · airframe 30,571 hrs · 27,977 cycles

CARGO DOOR HANDLE CUT OUT IS GOUGED IN TWO PLACES. BLENDED GOUGE ON CARGO DOOR HANDLE CUTOUT MATERIAL REMOVED .090 WITH MAX AMOUNT ALLOWABLE OF .100 REMAINING MATERIAL IS WITH IN SERVICEABLE LIMITS IAW REO 601R-52-31-086 COMPLIED WITH REO 601R-52-31-086 THIS IS A MAJOR REPAIR RII FOUND TO BE SATISFACTORY.

Part: RIB — CRACKED (LT WING) · airframe 30,571 hrs · 27,977 cycles

RIB CRACKED IN LT MLG WW. REPAIRED IAW REO 601R-57-51-046.

Part: BEAM — CRACKED (NACELLE) · airframe 30,571 hrs · 27,977 cycles

LT UPPER OTBD ANGLE ON ENGINE BEAM CRACKED ON AFT END. REMOVED ANGLE AND REPLACED WITH NEW ANGLE IAW SRM 51-42-21.

Part: ANTI-ICE SYSTEM — WARNING MESSAGE · airframe 30,485 hrs · 27,875 cycles

RECEIVED ANTI ICE DUCT WARNING MSG CLIMBING THROUGH FL 250 C/W QRH AND MSG EXTINGUISHED. ENROUTE, ACFT DIVERTED DUE TO MX -- EMERGENCY DECLARED. PERFORMED OPS TEST OF THE BLEED LEAK DETECTION SYS IAW AMM 36-21-00. OPS TEST GOOD. (CLOSED)

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 30,356 hrs · 27,737 cycles

CAPT'S FLASHLIGHT INOP. REPLACED CAPT'S FLASH LIGHT IAW AMM 25-61-00. (CLOSED)

Part: FITTING — CORRODED (EMERGENCY EXIT) · airframe 29,952 hrs · 27,264 cycles

LT OVERWING EMERGENCY EXIT HAS CORROSION ON LOWER LATCH FITTING REF TO OLD MCO 528892-2. REPAIRED IAW REO 601R-53-21-057 REV C.

Part: FITTING — CORRODED (EMERGENCY EXIT) · airframe 29,952 hrs · 27,264 cycles

LT OVERWING EXIT CORROSION AT LOWER LATCH FITTING. THIS ITEM IS INCORPORATED UNDER NEW EC/TC REO 601R-52-21-057 THIS CLEARS MCO 528892-2 REF TO AFDL 528987-3 FOR NEW MCO.

Part: FITTING — CORRODED (EMERGENCY EXIT) · airframe 29,952 hrs · 27,264 cycles

RT OVERWING EMERGENCY EXIT HAS CORROSION AT LWR LATCH FITTING. FOUND CORROSION ON LT WING EMERGENCY EXIT DOOR PN 601R30000-957, SN SB/RU/391. NOT THE RT EMERGENCY EXIT DOOR AS PREVIOUSLY REPORTED. FOUND LT AND RT OVERWING EMERGENCY EXITS WERE SWAPPED. SWAPPED LT AND RT EMERGENCY EXITS TO CORRECT POSITION IAW AMM 52-21-00. (CLOSED)

Part: BULB — BURNED OUT (EMERGENCY LIGHTS) · airframe 29,712 hrs · 26,995 cycles

RT FWD EMERGENCY LIGHT INOP. R & R RT FWD EMERGENCY LIGHT BULB.

Part: PACKING — LEAKING (HYD SYSTEM) · airframe 29,571 hrs · 26,840 cycles

CAUTION MSG HYD 3 LOW PRESS THROUGH 10000 FEET. RAN QRH LANDED WITH 3 GREEN, APPLIED BRAKE PRESSURE UPON LANDING AND PRESSURE AND QUANTITY REDUCED TO 0 (EMERGENCY DECLARED) FOUND CUT PACKING ON PLUG TO HYD SYSTEM NR 3 PRESSURE MANIFOLD ASSY. R & R PACKING IAW 29-12-05 SERVICED HYD SYSTEM NR3 TO 60 PERCENT IAW 12-20-00 LEAK AND OPS CK GOOD NO DEFECTS NOTED AT THIS TIME.

Part: ANGLE — CRACKED (BS 559) · airframe 29,256 hrs · 26,461 cycles

CRACK IN CAP ANGLE RADIUS AT LBL 18.0, FS 559. CONTINUATION FROM OP 35. SEALED PRIMED AND PAINTED REPAIR AREA ALL WORK DONE IAW SRM 51-23-00 AND SRM 51-25-00. APPLIED CIC, COMPLIED WITH EC/TC REO 601R-53-41-260 IAW REO 601R-53-41-260.

Part: WEB — CRACKED (BS 559) · airframe 29,256 hrs · 26,461 cycles

CRACK IN BULKHEAD WEB OTBD OF RBL 9.0 AT FS 559.00 AREA MARKED. APPLIED CIC TOO REPAIR AREA, NO LEAK CHECK REQUIRED IAW REO 601R-53-41-260 OR REO 601R-53-41-609. COMPLIED WITH EC/TC REO 601R-53-41-260 IAW REO 601R-53-41-260 REV D. COMPLIED WITH EC/TC REO 601R-53-41-609 02, AND MET ALL THE REQUIREMENTS OF REO 601R-53-41-609 REV B FOR DEVIATION E.

Part: BULKHEAD — CRACKED (BS 559) · airframe 29,256 hrs · 26,461 cycles

CRACK IN BULKHEAD WEB OUTBOARD OF RBL 9.0 AT FS 559.00 AREA IS MARKED. REMOVED LOWER RT CAP ANGLE RBL9 AND RBL18 AND BONDED DOUBLER AND DISCARDED FABRICATED NEW REPAIR PARTS AND DOUBLER IAW REO 601R-53-41-260 & REO 601R-53-41-609. INSTALLED 11 FABRICATED REPAIR ITEMS EXCEPT FASTENERS IN TOP OF RBR9, OTBD RBL9, INBD AND RBL 18 POST AND STRINGER CLIPS AND FASTNERS IN STRAP 601R32023-183. INSTALLED FASTENERS IN TOP OF RBL 9 & RBL 18 INSTALLED STRINGER CLIPS AND INSTALLED 601R32026-183 AND STEP 9 IAW REO 601R-53-41-260. LEAK CHECK DUE. DCASTO 161721 5/11/10 APPLIED SEALANT PRIMER AND PAINT ALL WORK DONE IAW SRM 51-13-00 AND SRM 51-25-00.

Part: ANGLE — CRACKED (BS 559) · airframe 29,256 hrs · 26,461 cycles

CRACK IN CAP ANGLE RADIUS AT LBL 18.0, FS 559.00. CUT CAP ANGLE LOWER IAW REO 601R-53-41-260, REMOVED DAMAGE SECTION. PILOTED ADDED FASTENERS TO 559 BULKHEAD REPAIR AREA ALL WORK DONE IAW SRM 51-40-11. REQUEST NDT AT CUT LINE IAW REO 601R-53-41-260. REF REO PL601R-53-41-260 PAGE 3 ATTACHED TO NRC FOR NDT, REMOVED LBL 9 & 18 POST AND STRINGER CLIPS, FABRICATED ALL REPAIR PARTS FOR LT SIDE REPAIR IAW REO PL 601R-53-41-260. INSTALLED ALL FABRICATED REPAIR PARTS ON LT SIDE 559 REPAIR IAW REO 601R-53-41-260.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,582 hrs · 25,678 cycles

EMERGENCY LIGHTS INOP FLT 5323. CREW ARRIVED AT ACFT WITH SWITCH IN ON POSTION.

Part: UNKNOWN — ODOR (CABIN) · airframe 28,468 hrs · 25,551 cycles

FOR PERIOD OF APPROX 1MIN IN DESCENT, NOTED A ODOR SIMILAR TO THAT OF LIGHTING OF A MATCH. F/A CONFIRMED IT WAS NOT FROM PAX. ALL COCKPIT INDICATION NORMAL. NO RELAY CLICKING , CB POPPING, ODOR DISSIPATED AFTER 1 MIN.

Part: LIGHT — FALSE ACTIVATION · airframe 27,378 hrs · 24,408 cycles

EMERGENCY LIGHTS ILLUMINATED IN FLT APX BELOW 10,000 FT.

Part: UNKNOWN — MALFUNCTIONED (CABIN) · airframe 27,430 hrs · 24,456 cycles

AIRPLANE PRESSURIZED NORMALLY UNTIL FL230 WHEN WE NOTICED THE CABIN CLIMBING 2300 FT/MIN DELTA P WAS APPROX 5.5 PRIOR TO THE EVENT. INITIATED AN IMMEDIATE DESCENT TO 10000 FEET. CABIN ALT NEVER EXCEEDED 4300 FEET (ACFT RETURNED TO DEPARTURE AFTER T/O) FLT 5624 DEL 120 MINS.

Part: STRUCTURE — CRACKED (LT MLG WW) · airframe 27,252 hrs · 24,286 cycles

POSSIBLE CRACK IN LT WHEEL WELL AT AILERON QUADRANT OUTBOARD ATTACH POINT (MARKED).

Part: VERTICAL BEAM — CRACKED (FUSELAGE) · airframe 27,252 hrs · 24,286 cycles

PRESSURE FLOOR AFT BULKHEAD FS 559.00 HAS CRACKED VERTICAL BEAM AT LBL 9.0 OUTBOARD SIDE FWD LOWER RADIUS. REPAIRED IAW EC/TC REO 601R-53-41-057.

Part: VERTICAL BEAM — CRACKED (FUSELAGE) · airframe 27,252 hrs · 24,286 cycles

PRESSURE FLOOR FWD BULKHEAD FS 409.00+128 HAS CRACKED VERTICAL BEAM AT LBL 18.0 OUTBOARD SIDE LOWER AFT RADIUS. REPAIRED CRACK ON VERTICAL BEAM ON BULKHEAD IAW REO 601R-53-41-056. COMPLIED WITH EC/TC REO 601R-53-41-056 STEPS 4 & 5.

Part: VERTICAL BEAM — CRACKED (FUSELAGE) · airframe 27,252 hrs · 24,286 cycles

PRESSURE FLOOR FWD BULKHEAD FS 409.00+128 HAS CRACKED VERTICAL BEAM AT RBL 9.0 INBOARD SIDE FWD LOWER RADIUS. REPAIRED DAMAGED AREA PER REO 601R-53-41-910 REFER TO EC/TC REO 601R-53-41-910.

Part: VERTICAL BEAM — CRACKED (FUSELAGE) · airframe 27,252 hrs · 24,286 cycles

PRESSURE FLOOR FWD BULKHEAD FS 409.00+128 HAS CRACKED VERTICAL BEAM AT RBL 18.0 OUTBOARD SIDE AFT LOWER RADIUS. REPAIRED BULKHEAD VERTICAL BEAM IAW REO 601R-53-41-056.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 27,252 hrs · 24,286 cycles

TWO INTERCOSTALS CRACKED FORWARD AND AFT OF LEFT WING TO FUSELAGE MIDDLE ATTACH FITTING. REMOVED FORWARD AND AFT MIDDLE ATTACH INTERCOSTAL FITTINGS IAW SRM 51-42-06. INSTALLED ANGLE PER SRM 51-42-21 AND 51-42-06.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 27,252 hrs · 24,286 cycles

SEAT TRACK AT FS 559+80.00 TO 559+96.00 RBL 27.00 CORRODED.

Part: STRUCTURE — CRACKED (WING) · airframe 27,252 hrs · 24,286 cycles

SUSPECT CRACK AT WS 127.25 WHILE C/W TASK CARD 000-57-540-604.

Part: PRESSURE PANEL — CORRODED (FUSELAGE) · airframe 27,252 hrs · 24,286 cycles

PRESSURE FLOOR SKIN HAS SEVERAL AREAS OF CORROSION BETWEEN FS 409+128 TO FS 559.00 BETWEEN LBL35 TO 45L. BLENDED AND REPAIRED IAW REO 601R-53-41-906

Part: SUPPORT — CRACKED (CARGO BAY) · airframe 27,252 hrs · 24,286 cycles

AFT CARGO DOOR SUPPORT STRUCTURE TO 621 BULKHEAD CLIP APPEARS CRACKED.

Part: PRESSURE PANEL — CORRODED (FUSELAGE) · airframe 27,252 hrs · 24,286 cycles

PRESSURE FLOOR SKIN HAS SEVERAL AREAS OF CORROSION BETWEEN FS 409+128 TO FS 559.00 BETWEEN RBL 35 TO 45R. BLENDED CORROSION IAW SRM 51-21-06.

Part: FINGER DOUBLER — CORRODED (FUSELAGE) · airframe 27,252 hrs · 24,286 cycles

LEFT FINGER DOUBLERS ON PRESSURE FLOOR FS 409+128 -559 CORRODED. BLENDED CORROSION IAW SRM 51-21-06.

Part: FINGER DOUBLER — CORRODED (FUSELAGE) · airframe 27,252 hrs · 24,286 cycles

RIGHT FINGER DOUBLERS ON PRESSURE FLOOR FS 409+128 -559 CORRODED. BLENDED CORROSION IAW SRM 51-21-06. PERFORMED UT THICKNESS INSPECTION IAW NDTM 51-20-04.

Part: INTERCOSTAL — CRACKED (ASD) · airframe 27,252 hrs · 24,286 cycles

ASD TOP FWD INTERCOSTAL -9 CRACKED.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 27,252 hrs · 24,286 cycles

FLOOR SUPPORT HAS CORROSION IN CARGO BAY UNDER PANEL 282JRF ALONG THE WALL. COMPLIED WITH EC/TC REO 601R-53-61-3105 IAW REO 601R-53-61-3105. BLENDED CORROSION IN CARGO BAY UNDER PANEL 282JRF ALONG THE WALL. ( BLENDED 3 SPOTS AND ABOUT .002 OF MATERIAL FROM EACH SPOT) PER SRM 51-21-06.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 27,252 hrs · 24,286 cycles

SEAT TRACK HAS CORROSION UNDER FWD CARGO / LAV WALL. BLENDED CORROSION ON SEAT TRACK UNDER FWD CARGO / LAV WALL AND FOUND TO BE WITHIN LIMITS IAW SRM 53-21-49.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 27,252 hrs · 24,286 cycles

RT SIDE FS 718.00 (BETWEEN STR 10 AND 11R) FRAME INTERNAL DOUBLER IS CRACKED IN THE LOWER RADIUS. REMOVED CRACKED INTERNAL DOUBLER OUT AIRCRAFT IAW SRM 51-42-21. FABRICATED AND DRILLED NEW AFT INTERNAL DOUBLER FROM 600-36030-32 PER REO 601-53-61-243 SG 7020421. INSTALLED REPAIR DOUBLERS PER REO 601R-53-61-243 SG 7020421.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 27,252 hrs · 24,286 cycles

AFT EQUIPMENT COMPARTMENT LT AND RT ANGLES AT INTERCOSTAL BETWEEN FS 621.00 AND 625 STR 14 LT AND RT ARE CRACKED.

Part: STEP — BROKEN (DOOR) · airframe 26,714 hrs · 23,822 cycles

ASD TOP STEP BROKEN.

Part: DOOR — BINDING (PAX DOOR) · airframe 26,600 hrs · 23,709 cycles

PAX DOOR DIFFICULT TO CLOSE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 25,902 hrs · 23,084 cycles

AFT INTERIOR EMERG. LIGHT INOP. RELAMPED EMERGENCY AFT INTERIOR LIGHT IAW AMM 33-51-16. OPS CK GOOD.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 25,520 hrs · 22,738 cycles

APU OVERTEMP WARNING MSG ON INFLIGHT 300 KTS AT FL 250, EMERGENCY DECLARED. FLT 4292 DEL 55 MINS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,413 hrs · 20,932 cycles

THE 2ND FROM AFT CEILING EMERGENCY LIGHT INOP.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 22,869 hrs · 20,516 cycles

CRACK AT INTERCOSTAL FUSELAGE STA 559 CARGO BAY ENTRY DOOR UNDER PANEL 281LLF (MARKED).

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 22,869 hrs · 20,516 cycles

LEFT FS 484 INTERCOSTAL CRACKED ON I/B SIDE. REMOVED DAMAGED CLIP FROM L/H FS 484 INTERCOSTAL I/B SIDE. FABRICATED SERVICEABLE CLIP USING 2024-T3, .063", PO# 8743-1. ALODINED, PRIMED, AND PAINTED IAW CRJ SRM 51-25-16. INSTALLED CLIP IAW REO-601R-53-41-059.

Part: PLACARD — UNKNOWN (PAX DOOR) · airframe 22,870 hrs · 20,516 cycles

PAX DOOR STEP 832AT -EXIT- PLACARD REQUIRES REPLACEMENT.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 22,869 hrs · 20,516 cycles

RIGHT FS 484 INTERCOSTAL CRACKED ON I/B SIDE.

Part: LIGHT — UNKNOWN (CABIN) · airframe 22,870 hrs · 20,516 cycles

PASSENGER DOOR EMERGENCY ILLUMINATION STRIPS REQUIRES REPLACEMENT (8EA) MARKED. [SUP 05-02-07] REMOVED AND REPLACED 1 PASSENGER DOOR EMERGENCY ILLUMINATION STRIP ON STEP 832CT AFT SIDE WITH NEW SERVICEABLE EMERGENCY ILLUMINATION STRIP IAW CRJ CMM 11-30-00, REMOVED AND REPLACED 7 PASSENGER DOOR EMERGENCY ILLUMINATION STRIPS ON STEPS 832BT, 832CT, AND CENTER TWO STEPS IAW CRJ AMM 11-30-00,

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 22,869 hrs · 20,516 cycles

LEFT FS 484 INTERCOSTAL CRACKED ON O/B SIDE.

Part: LIGHT — INOPERATIVE (RT OVERWING) · airframe 22,751 hrs · 20,429 cycles

RIGHT OVERWING EMERGENCY LIGHT INOP.

Part: WINDOW — CRACKED (COCKPIT) · airframe 22,063 hrs · 19,871 cycles

F/O`S SIDE WINDOW CRACKED, DECLARED AN EMERGENCY.

Part: SIGN — INOPERATIVE (CABIN) · airframe 21,167 hrs · 19,121 cycles

FWD PAX EMERGENCY EXIT SIGN INOP.

Part: ODOR — DETECTED (GALLEY)

THE FLIGHT ATTENDANT REPORTED A POSSIBLE BURNING ODOR ASSOCIATED WITH THE NR 1 GALLEY HEATER. (M)

Part: DOOR — STIFF (MAIN PAX)

DURING A GROUND INSPECTION, FA REPORTED THE PASSENGER DOOR DIFFICULT TO CLOSE FROM INSIDE. MAINTENANCE OPENED AND CLOSED THE PASSENGER DOOR SEVERAL TIMES WITH NO DEFECTS NOTED. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: O-RING — LEAKING (APU FUEL)

FLT 4358 - DURING CRUISE FROM DHN-ATL, THE CREW NOTICED A BURNING OIL TYPE ODOR COMING THROUGH THE AIR CONDITIONING SYSTEM INTERMITTENTLY, OCCURRING ON BOTH THE ENIGNE AND AUXILLARY POWER UNIT BLEEDS. THE AIRCRAFT LANDED SAFELY IN ATL. MAINTENANCE FOUND A EXCESSIVE FUEL LEAK ON THE AUXILLARY POWER UNIT AND REMOVED AND REPLACED AN O-RING ON THE FUEL SOLENOID. MAINTENANCE ALSO REMOVED AND REPLACED A COALESCER BAG FOR PREVENTATIVE MAINTENANCE AND CLEANED ALL AREAS AROUND THE APU. MAINTENANCE RAN THE PACKS WITH THE APU AND ENGINE FOR ONE HOUR. NO SMELLS WERE NOTED. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: COALESCER BAG — ODOR (RT AND LT)

FLT - 4393 - DURING CRUISE, DESCENT AND LANDING FROM MGM-CVG, THE CREW NOTICED AN OILY TYPE SMELL IN THE COCKPIT AND CABIN. THE AIRCRAFT LANDED SAFELY IN CVG. MAINTENANCE REMOVED AND REPLACED THE LEFT AND RIGHT COALESCER BAGS IAW CRJ AMM 21-00. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: ANGLE — CORRODED (BULKHEAD)

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

Part: CLIP — CRACKED (FUSELAGE)

DURING A C-CHECK, THE FS 625 LT/RT CLIPS IN THE AFT EQUIPMENT BAY WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE FS 625 LT/RT CLIPS IN THE AFT EQUIPMENT BAY. (K)

Part: SUPPORT BEAM — CRACKED (ENGINE)

DURING A C-CHECK, THE ENGINE SUPPORT BEAM AT BOTH RIVET HOLES UNDER THE FIRE LOOP WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL0 IAW EO. (K)

Part: FRAME — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE FS 280 FRAME AT APPROXIMATELY LBL 11 AND RBL 11 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE FS 280 FRAME AT APPROXIMATELY LBL 11 AND RBL 11 IAW ASA EO 600-53-0123. (M)

Part: SEAT TRACK — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE SEAT TRACK AT FS 559 PLUS 78 TO PLUS 88, RBL 9 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE SEAT TRACK AT FS 559 PLUS 78 TO PLUS 88, RBL 9. (M)

Part: CLIP — CRACKED (FUSELAGE)

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

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

DURING C-CHECK, THE FLOOR ATTACH ANGLE AT FS 621 TO FS 559+112, LBL27 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS REPAIRING HE FLOOR ATTACH ANGLE AT FS 621 TO FS 559+112, LBL 27 IAW REO. (K)

Part: COVER — CRACKED (EMERGENCY EXIT)

DURING C-CHECK, THE EMERGENCY EXIT LIGHT COVER ABOVE THE SERVICE DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT COVER ABOVE THE SERVICE DOOR. (K)

Part: HANDLE — CRACKED (E/E BAY DOOR)

DURING A C-CHECK, THE MAIN AVIONICS BAY DOOR HANDLE WAS FOUND CRACKED AT THE BASE. MAINTENANCE IS REMOVING AND REPLACING THE MAIN AVIONICS BAY DOOR HANDLE. (K)

Part: STEP — CRACKED (PAX DOOR)

DURING C-CHECK, THE PASSENGER DOOR TOP STEP WAS FOUND CRACKED. MAINTENANCE REPAIRED THE PASSENGER DOOR TOP STEP IAW CMM. (K)

Part: SKIN — CRACKED (FUSELAGE)

DURING A C-CHECK, THE NOSE LANDING GEAR WHEEL WELL AFT CUT OUT ON THE LT SIDE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTNANCE IS REPAIRING THE NOSE LANDING GEAR WHEEL WELL FUSELAGE SKIN RADIUS LT AT FS 235 IAW EO. (K)

Part: SKIN PANEL — CRACKED (LT WING)

DURING A C-CHECK, THE LOWER WING PLANK AT WS 148.019 LT/RT WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LOWER WING PLANK AT WS 148.019 LT/RT IAW EO. (K)

Part: SWITCH — MALFUNCTIONED (TRIM DISCONNECT)

DURING CLIMB OUT, BETWEEN 3,000 TO 4,000 FT, CREW RECEIVED A STAB TRIM AND MACH TRIM DISCONNECT CAUTION MESSAGE. CREW LEVELED AC OFF TO 4,000 FT, SLOWED TO 200 KNOTS TO COMPLY WITH QRH, WHICH DID NOT RESOLVE PROBLEM. THE AC RETURNED TO DEPARTURE. UPON APPROACH, WHEN ADVANCING THE FLAPS TO 8 DEGREES AND THEN TO 20 DEGREES, FORWARD PRESSURE WAS REQUIRED AT WHICH TIME THE CREW REQUESTED EMERGENCY VEHICLES BE PLACED ON STANDBY AS A PRECAUTION. AC LANDED SAFELY. MAINT REMOVED AND REPLACED F/O TRIM DISCONNECT SWITCH; AND ALSO PERFORMED FULL HORIZ STAB TRIM CONTROL UNIT OPS CHECK. OPS CHECK GOOD. AC OK FOR SERVICE. (K)

Part: FRAME — CRACKED (FUSELAGE)

DURING AN A-CHECK, THE LT FS 640 DOUBLER, LT FS 640 FRAME AND THE SKIN BUTT JOINT STRAP ON THE LT SIDE AT FS 640, STRINGER 8-13 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE LT FS640 DOUBLER AND LT FS640 FRAME IAW SRM 53-00 AND REPAIRING THE SKIN BUTT JOINT STRAP ON THE LT SIDE AT FS640, STRINGER 8-13 IAW REO 601R-53-61-506.

Part: STEP — CRACKED (PAX DOOR)

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

Part: STEP — BROKEN (PAX DOOR)

DURING A GROUND INSPECTION IN DFW, THE BOTTOM STEP BRACKET 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: STEP — BROKEN (PAX DOOR)

FLT 4123 - DURING A GROUND INSPECTION IN DFW, THE BOTTOM STEP ON THE PASSENGER FOOR WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: HANDLE — BINDING (PAX DOOR)

FLT 4954 - DURING A GROUND INSPECTION IN DFW, THE PASSENGER DOOR WAS HARD TO CLOSE AND THE HANDLE WOULD NOT STAY IN THE CLOSED POSITION. MAINTENANCE LUBRICATED THE OUTSIDE AND INSIDE PASSENGER DOOR HANDLES. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: STEP — BROKEN (PAX DOOR)

FLT 4858 - DURING A GROUND INSPECTION, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: STEP — CRACKED (AIRSTAIR)

DURING A C-CHECK IN MCN, THE PASSENGER DOOR BOTTOM STEP WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: SKIN — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE FUSELAGE SKIN RADIUS ON THE RIGHT SIDE AT FS 235 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE FUSELAGE SKIN RADIUS ON THE RIGHT SIDE AT FS 235 IAW ASA EO 600-53-0122. (M)

Part: FRAME — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE FORWARD SIDE OF FS 640 FRAME AT THE ENGINE SUPPORT BEAM AS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED FS 640 FRAME AT THE ENGINE SUPPORT BEAM. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

DURING A C-CHECK IN MC, THE LEFT AND RIGHT 9.00 AND 27.00 FLOORBEAMS BETWEEN FS 280.00 AND FS 409.00 PLUS 5.00 IAW ASA EO 600-53-0052A. (M)

Part: ANGLE — CRACKED (TAIL)

DURING A C-CHECK IN MCN, THE VERTICAL STABILIZER RIGHT VISOR PANEL ANGLE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE VERTICAL STABILIZER RIGHT VISOR PANEL ANGLE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: ANGLE — CRACKED (FUSELAGE)

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

Part: ANGLE — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE CARGO COMPARTMENT FLOOR SUPPORT ANGLE AT FS 621 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CARGO COMPARTMENT FLOOR SUPPORT ANGLE AT FS 621 IAW ASA EO 600-53-0105. (M)

Part: SKIN — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE FUSELAGE SKIN AT THE AUXILIARY POWER UNIT INLET, FS 654.50 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE FUSELAGE SKIN AT THE AUXILIARY POWR UNIT INLET, FS 654.50 IAW ASA EO 600-53-0121. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

DURING A C-CHECK IN MCN, THE FORWARD LONG SEAT TRACKS AT LBL 9 AND RBL 9 WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FORWARD LONG SEAT TRACKS AT LBL 9 AND RBL 9 IAW WITH SRM 51-00. (M)

Part: MECHANISM — OUT OF ADJUST (AFT PAX DOOR)

DURING HANGAR MAINTENANCE IN MCN, THE AFT PASSENGER DOOR WAS FOUND TO BE HARD TO OPEN AND CLOSE. MAINTENANCE ADJUSTED THE AFT PASSENGER DOOR COUNTER BALANCE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LAMP — BURNED OUT (EXTERIOR)

FLT 4693 - DUIRNG A GROUND INSPECTION IN ATL, THE MIDDLE EXTERIOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE MIDDLE EXTERIOR EMERGENCY LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: SWITCH — FAILED (FUEL SYSTEM)

FLT 4513 - DURING CLIMB-OUT FROM ATL, A LOW FUEL PRESSURE CAUTION MESSAGE ON THE RIGHT ENGINE WAS RECEIVED. THE CAPTAIN SHUT DOWN THE ENGINE AND DECLARED AN EMERGENCY. THE AIRCRAFT RETURNED TO ATL AND LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE FUEL BOOST PUMP SWITCH. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: FRAME — CRACKED (FUSELAGE)

DURING HANGER MAINTENANCE, A CRACK WAS DISCOVERED IN FRAME STATION 718 BETWEEN STRINGERS 10 AND 12 ON THE LEFT AND RIGHT SIDES. MAINTENANCE REPAIRED THE CRACKED FRAME IAW EO/REO.

Part: BEAM — CRACKED (ENG SUPPT BEAM)

DURING (C) CHECK INSPECTION, WHILE COMPLYING WITH EO, VISUAL INSPECTION OF THE ENGINE SUPPORT BEAMS, BOTH SIDES WERE FOUND TO HAVE A CRACK. MAINTENANCE COMPLIED WITH EO TO SERVICE AS THE PERMANENT REPAIR FOR THE ENGINE SUPPORT BEAM CRACK.

Part: O-RING — BROKEN

UPON CLIMB-OUT FROM ATL, PASSING THROUGH 17,000 FT, CAPTAIN RECEIVED RIGHT ENGINE OIL PRESSURE WARNING. OIL PRESSURE WAS READING 23 PSI AND THE TEMPERATURE WAS 98 DEGREES. CAPTAIN SECURED THE ENGINE IN FLIGHT BY FOLLOWING EMERGENCY AND ABNORMAL CHECKLISTS. AIRCRAFT RETURNED AND LANDED SAFELY IN ATL. MX INSPECTED RIGHT ENGINE AND FOUND UPPER UNION ON B SUMP SCAVENGE PUMP UPPER RIGHT INSTALLED WITH A BROKEN SEAL. MAINTENANCE REMOVED AND REPLACED UNION O-RING AND REINSTALLED UNION. THE RIGHT ENGINE WAS GROUND RAN AT HIGH POWER SETTINGS FOR 30 MINUTES. NO LEAKS OR DEFECTS WERE NOTED. AIRCRAFT RETURNED TO SERVICE. (M)

Part: WINDOW — CRACKED (COCKPIT)

FLT 4503 - DURING FLIGHT FROM ATL TO XNA, CAPTAINS SIDE WINDOW SHATTERED. AIRCRAFT RETURNED TO ATL AND LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED CAPTAINS SIDE WINDOW. OPERATIONAL AND LEAK CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: FECU — INOPERATIVE (TE FLAPS)

CREW GOT FLAP FAIL MESSAGE WHEN SELECTING FLAPS FROM EIGHT TO ZERO DEGREES. CREW DECLARED AN EMERGENCY AND LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE FECU. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (X)

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO BAY)

ALT/ROA - FLT 7273 - ON CLIMB-OUT THROUGH 9,000 FEET, CARGO SMOKE LIGHT CAME ON ONCE FOR ABOUT 2 SECONDS. CREW CONTACTED MTC CNTL AND WERE INSTRUCTED TO RETURN TO ATL. RECEIVED OTHER MOMENTARY WARNINGS DURING 10 MILE FINAL APPROACH. LANDING MADE SAFELY IN ATL WITHOUT FURTHER INCIDENT AND AIRCRAFT WAS TAXIED TO THE GATE. ATL MAINTENANCE REMOVED AND REPLACED BOTH CARGO COMPARTMENT SMOKE DETECTORS. OPERATIONAL TESTS WERE GOOD AND THE AIRCRAFT WAS RELEASED FOR FURTHER SERVICE. (X)