N883AS

Part: FRAME — CRACKED (BS 319) · airframe 31,006 hrs · 28,680 cycles

PRIOR TO INSTALLING FASTENERS ON FLANGE OF FRAME 319.00 WHICH WERE REMOVED DUE TO CORROSION. MECHANIC FOUND CRACK AT VERY CORNER FASTENER HOLE. COMPLIED WITH EA 20-2015-363 P1. RECEIVED AND COMPLIED WITH FINAL EA 20-2015-363. RECEIVED AND COMPLIED WITH ECTC EA 20-2015-363.

Part: DOOR SILL — CRACKED (BS 605) · airframe 31,006 hrs · 28,680 cycles

CARGO DOOR CUTOUT LOWER SILL CRACKED AT BS 605. COMPLIED WITH EC/TC REO 601R-53-61-433 AND REO 601R-53-61-433, REV B.

Part: DOOR SILL — CRACKED (BS 589) · airframe 31,006 hrs · 28,680 cycles

CARGO DOOR CUTOUT LOWER SILL CRACKED AT FS 589.00, MARKED. COMPLIED WITH EC/TC REO 601R-53-61-433 AND REO 601R-53-61-433, REV B, DATED 10/9/2009 AS WRITTEN.

Part: SEAT TRACK — CORRODED (BS 405-409) · airframe 31,006 hrs · 28,680 cycles

SEAT TRACK CORRODED AT LBL9, FS 405 TO 409.00+120. BLENDED CORROSION IAW SRM 51-21-06. FOUND TO BE OUT OF LIMITS IAW SRM 53-21-49. REMOVED SEAT RAIL IAW AMM TASK 53-01-11-000-802. COMPLIED WITH ECTC REO 601R-53-00-485. INSTALLED NEW SERVICEABLE SEAT TRACK AT LBL9, FS 405-409+120 IAW AMM 53-01-11-400-802.

Part: FLOORBEAM — CORRODED (BS 349) · airframe 31,006 hrs · 28,680 cycles

UPON REMOVING UPPER COMPOSITE CAP FOR FROM ON JOB 8 OP 9 DISCOVERED ADDITIONAL CORROSION ON AFT LT-ANGLE ON 349 CROSSBEAM, RBL 40. REMOVED UPPER SUPPORT ANGLE FROM 349.00 CROSS BEAM REMOVED, 4 EA SOLID RIVETS AND 6 HILITES THROUGH ATTACHING MOUNT IAW SRM 51-42-06 AND 51-42-21. LOCATED HOLES IN SERVICEABLE SUPPORT ANGLE SRM 51-40-11. INSTALLED SERVICABLE SUPPORT ANGLE ON 349 CROSSBEAM IAW SRM 51-42-06 DWG 601R38783.

Part: SKIN — CORRODED (WING) · airframe 31,006 hrs · 28,680 cycles

WING PLANK ACCESS HOLE FOR FUEL PANEL 540BB LAND SURROUND HAS CORROSION PITTING. COMPLIED WITH ECTC EO 000-57-81.

Part: SKIN — CORRODED (WING) · airframe 31,006 hrs · 28,680 cycles

WING PLANK HOLE FUEL PANEL 640BB LAND SURROUND HAS CORROSION/PITTING. COMPLIED WITH EC/TC EO 600-57-81 C/W IAW REO 601R-57-21-030, REV L. COMPLIED WITH REO 601R-57-21-2392. RECEIVED AND COMPLIED WITH ECTC REO 601R-57-21-2392.

Part: FRAME — CRACKED (BS 333) · airframe 31,006 hrs · 28,680 cycles

FRAME 333, CRACKED AT STR 1 RT. RECEIVED AND COMPLIED WITH 601R-53-21-2680 PI. REMOVED FRAME AND STARTED DRILLING NEW FRAME IAW SRM 51-42-06 & 51-42-21. DRILLED AND INSTALLED FRAME 333 AT SIGN RT IAW SRM 51-41-11 AND 51-42-06, & 51-42-21 AND DWL 601R 32004. RECEIVED AND COMPLIED WITH 601R-53-21-2680 PL AND FINAL. RECEIVED AND COMPLETED ECTC REO 601R-53-21-2680.

Part: ANGLE — CRACKED (BS 280) · airframe 31,006 hrs · 28,680 cycles

ANGLE CRACKED AT FS 280 AND RBL 9. R & R ANGLE WITH SRM 51-42-21-00.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 31,006 hrs · 28,680 cycles

DEFECT DESCRIPTION: SEAT TRACK AT RBL9 BETWEEN FS 559.00+80 & 559.00+96 HAS CORROSION THAT NEED TO BE EVALUATED. SEAT TRACK FOUND TO BE OUT OF LIMITS IAW SRM 53-51-49-01. REMOVED SEAT TRACK AT RBL9 BETWEEN FS 559.00 AND FS 559.00+96 IAW AMM 53-00-49-000-801. COMPLIED WITH EC/TC REO 601R-53-00-485, FABRICATED SEAT RAILS IAW GREO 601R-53-00-485, REV A. INSTALLED FABRICATED SEAT TRACK AT RBL9, FS 559.00+80 AND FS 559.00+96 IAW AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 559-574) · airframe 31,006 hrs · 28,680 cycles

SEAT TRACK AT RBL 9 BETWEEN FS 574.00 & 559.00+112 HAS CORROSION THAT NEED TO BE EVALUATED. SEAT TRACK FOUND TO BE OUT OF LIMITS IAW SRM 53-51-49-01. REMOVED SEAT TRACK AT RBL 9 BETWEEN FS 574.00 AND 559.00+112 IAW AMM 53-00-49-000-801. COMPLIED WITH EC/TC REO 601R-53-00-485 FABRICATED SEAT RAIL IAW GREO 601R-53-00-485, REV A. INSTALLED FABRICATED SEAT TRACK AT RBL9, FS 574.00 AND 559.00+112 IAW AMM 53-00-49-400-801.

Part: FLOOR SUPPORT — CORRODED (BS 409-559) · airframe 31,006 hrs · 28,680 cycles

LEFT PRESSURE FLOOR SILL CORRODED AT SEVERAL LOCATIONS BETWEEN FS 409 & FS 559. COMPLIED WITH EC/TC REO 601R-53-41-666-01, REV A, DATED OCT.23,2013.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 31,006 hrs · 28,680 cycles

SEAT TRACK AT LBL9 BETWEEN FS 559.00+80 & 559.00+96 HAS CORROSION THAT NEED TO BE EVALUATED. SEAT TRACK FOUND TO BE OUT OF LIMITS IAW SRM 53-51-49-01, REMOVED AND REPLACED. REMOVED SEAT RAIL AT LBL9 BETWEEN FS 559+80 AND 559+96 IAW AMM 53-00-48-000-801. COMPLIED WITH EC/TC REO 601R 53-00-485, FABRICATED SEAT RAILS IAW GREO 601R-53-00-485 REV A. INSTALLED NEW FABRICATED SEAT TRACK AT LBL9 BETWEEN FS 559.00+80 AND FS 559.00+96 IAW AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 605-621) · airframe 31,006 hrs · 28,680 cycles

SEAT TRACK AT LBL BETWEEN FS 605.00 & 621.00 HAS CORROSION THAT NEED TO BE EVALUATED. REMOVED SEAT TRACK AT LBL BETWEEN FS 605.00 AND 621.00 IAW AMM 53-00-49-000-801. INSTALLED SEAT TRACK AT LBL BETWEEN FS 605.00 & 612.00 IAW AMM 53-01-11-400-802. COMPLIED WITH EC/TC REO 601R-53-00-485.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 31,006 hrs · 28,680 cycles

SEAT TRACK AT RBL9 BETWEEN FS 559.00 & 559.00+96 HAS CORROSION THAT NEED TO BE EVALUATED. SEAT TRACK FOUND TO BE OUT OF LIMITS IAW SRM 53-51-49-01. R & R SEAT TRACK SECTION AT RBL9, FS 559 AND 559.00+86 IAW AMM 53-01-11-000-802 AND 53-01-11-400-802 AND FABRICATED SEAT RAIL IAW GREO 601R-53-00-485, REV A. RECEIVED, COMPLIED WITH ECTC 601R-53-00-485 FABRICATED SEAT RAIL IAW GROE 601R-53-00-485, REV A.

Part: FLOOR SUPPORT — CORRODED (BS 559) · airframe 31,006 hrs · 28,680 cycles

CORROSION FOUND ON LT FLOOR SILL BETWEEN FS 559.00+32 & 559.00+80, NEED TO BE EVALUATED. COMPLIED WITH EC/TC REO 601R-53-00-526.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 31,006 hrs · 28,680 cycles

SEAT TRACK AT LBL18 BETWEEN FS 559.00+80 & 559.00+96 HAS CORROSION THAT NEED TO BE EVALUATED. SEAT TRACK FOUND TO BE OUT OF LIMITS IAW SRM 53-51-49-01. R & R SEAT TRACK AT LBL 18 BETWEEN 559+80 AND 559+96 IAW AMM 53-01-11-000-802 AND 53-1-11-400-02 AND FABRICATED IAW GREO 601R-53-00-485, REV A. FABRICATED SEAT RAILS IAW GREO 601R-53-00-485, REV A ECTC COMPLIED WITH.

Part: FLOOR SUPPORT — CORRODED (BS 559) · airframe 31,006 hrs · 28,680 cycles

CORROSION FOUND ON RT FLOOR SILL BETWEEN FS 559.00+16 & 559.00+32 NEED TO BE EVALUATED. COMPLIED WITH EC/TC REO 601R-53-00-526-01.

Part: FLOOR SUPPORT — CORRODED (BS 409-559) · airframe 31,006 hrs · 28,680 cycles

RIGHT PRESSURE FLOOR SILL CORRODED AT SEVERAL LOCATIONS BETWEEN FS 409 & FS 559. COMPLIED WITH EC/TC REO 601R-53-41-666-01 AND REO 601R-53-41-666, REV C, DATED 11/6/12 AS WRITTEN.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 31,006 hrs · 28,680 cycles

SEAT TRACK AT LBL9 BETWEEN FS 559.00 & 559.00+96 HAS CORROSION THAT NEED TO BE EVALUATED. SEAT TRACK FOUND TO BE OUT OF LIMITS IAW SRM 53-51-49-01. REMOVED SEAT TRACK AT LBL9 BETWEEN FS 559.00 AND 559.00+96 IAW AMM 53-01-11-000-802. COMPLIED WITH EC/TC REO 601R 53-00-485, FABRICATED SEAT RAILS IAW GREO 601R-53-00-485, REV A. INSTALLED NEW FABRICATED SEAT TRACK AT LBL9 BETWEEN FS 559.00 AND FS 559.00+96 IAW AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 559-574) · airframe 31,006 hrs · 28,680 cycles

SEAT TRACK AT LBL9 BETWEEN FS 574.00 & 559.00+112 HAS CORROSION THAT NEED TO BE EVALUATED. SEAT TRACK FOUND TO BE OUT OF LIMITS IAW SRM 53-51-49-01. REMOVED SEAT RAIL AT LBL9 BETWEEN FS 574.00 AND 559.00+112 IAW AMM 53-00-48-000-801. COMPLIED WITH EC/TC REO 601R 53-00-485 FABRICATED SEAT RAILS IAW GREO 601R-53-00-485, REV A. INSTALLED NEW FABRICATED SEAT TRACK AT LBL9 BETWEEN FS 574.00 AND FS 559.00+112 IAW AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 409) · airframe 31,006 hrs · 28,680 cycles

SEAT TRACK SEGMENT CORRODED ON RBL 9 FROM BS 409 TO 409+128 IN 6 SPOTS. COMPLIED WITH EC/TC REO 601R-53-00-485 FABRICATED SEAT TRACK IAW GREO 601R-53-00-485, REV A. FOUND TO BE OUT OF LIMITS IAW SRM 53-21-49. REMOVED AND REPLACED THE SEAT TRACKIAW AMM 53-01-11-000-802 AND AMM 53-01-11-400-802.

Part: ISOLATOR — BROKEN (AFT BULKHEAD) · airframe 31,006 hrs · 28,680 cycles

AFT PRESSURE BULKHEAD FWD FACE, SEVEN BROKEN INSOLATORS. R & R ISOLATORS IAW SRM 51-42-10.

Part: FLOOR SUPPORT — CORRODED (BS 409) · airframe 31,006 hrs · 28,680 cycles

RBL 9 FLOORBEAM TOP CAP CORRODED BETWEEN FS 409 TO FS 409+96 IN 10 SPOTS MOSTLY AROUND SCREW HOLES. REMOVED SEAT RAIL FORM FS 409-FS 409+112. INSTALLED SEAT RAIL FS 409-40-+112 IAW AMM 53-01-11-40-802. BLENDED & REMOVED CORROSION SRM 51-123-00-00 IN 11 LOCATIONS. COMPLIED WITH SRM 53-00-43, REPAIR NR 2. COMPLIED WITH EC/TC REO 601R 53-00-005.

Part: ATTACH FITTING — CRACKED (BS 484) · airframe 31,006 hrs · 28,680 cycles

BROKEN CLEAT AT FS 484.00 & RBL 28 INTERSECT NEED REPLACEMENT. REMOVED BROKEN CLEAT AT FS 484.00 & RBL 28 INTERSECT IAW SRM 51-42-21. INSTALLED SERVICEABLE CLEAT IAW SRM 51-42-21, DWG 601R31171.

Part: FLOOR SUPPORT — CORRODED (BS 405-409) · airframe 31,006 hrs · 28,680 cycles

LBL9 FLOORBEAM FROM FS 405 TO 409.00+120 IS CORRODED AT FS 410 AND FS 409.00+120. AFTER EVALUATION ITS DISCOVERED THAT DAMAGE IS OUT OF LIMITS WITH SRM AND SPLICE REPAIRS ARE REQUIRED. REPAIRED FLOORBEAM AT LBL9, FWD SPLICE FS 409+26-409+5 AND AFT SPLICE FS 409+116-409+135 IAW SRM 53-00-43. REPAIR NR 2, FIGURE 203.

Part: SEAT TRACK — CORRODED (BS 449-499) · airframe 31,006 hrs · 28,680 cycles

CORROSION ALONG RT SIDE SEAT TRACK BETWEEN BS 449+85 TO 499, COMPLIED WITH EC/TC REO 601R 53-00-055. REMOVED RT SIDE SEAT TRACK IAW AMM 53-01-11-000-802. INSTALLED RT SIDE SEAT TRACK IAW AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 544-559) · airframe 31,006 hrs · 28,680 cycles

CORROSION ON LT SIDE SEAT TRACK BETWEEN FS 544.00 & 559.00+80. COMPLIED WITH EC/TC REO 601R-53-00-055. REMOVED SIDE SEAT TRACK IAW AMM TASK 53-01-11-000-802. INSTALLED A NEW SEAT TRACK IAW AMM 53-01-11-400-802.

Part: FLOOR SUPPORT — CORRODED (BS 319) · airframe 31,006 hrs · 28,680 cycles

RIGHT FLOOR SILL CORRODED AT FS 319.70. R & R ANGLE DOUBLER ON RT FLOOR SILL AT FS 319.70 IAW SRM 31-42-06 AND SRM 51-42-13 AND SRM 51-42-15.

Part: SEAT TRACK — CORRODED (BS 409-461) · airframe 31,006 hrs · 28,680 cycles

CORROSION ON RT SIDE SEAT TRACK FROM BS 409+128 - 461. COMPLIED WITH EC/TC REO 601R-53-00-055. REMOVED RT SIDE SEAT TRACK IAW AMM 53-01-11-000-802. INSTALLED RT SIDE SEAT TRACK IAW AMM 53-01-11-000-802.

Part: SKIN — CRACKED (LT WING) · airframe 31,006 hrs · 28,680 cycles

CRACK FOUND IN WING PLANK ON LT SIDE AT 148.019, AFT SIDE LOWER PLANK, LENGTH .718. COMPLIED WITH EC/TC REO 601R-57-21-130 & GREO 601R-57-21-130, REV DATED 11/27/2013 AS WRITTEN. COMPLIED WITH EC/TC REO 601R-57-21-131 & GREO 601R-57-21-131, REV DATED 11/27/2013 AS WRITTEN.

Part: FITTING — CHAFED (BS 364) · airframe 31,006 hrs · 28,680 cycles

FITTING CHAFED ON FS 364.00 FWD OF THE AVIONIC DOOR, 2EA. REMOVED CHAFE AT FS 364.00 FITTINGS FWD OF THE AVIONICS DOOR, 2EA IAW SRM 51-12-00-00, BLEND LENGTH 1.3" X .5". COMPLIED WITH STS EA 26-2015-203, REV A DATED 12/16/2015. RECEIVED AND COMPLIED WITH ECTC EA 36-2015-203.

Part: SKIN — DENTED (WING ROOT) · airframe 31,005 hrs · 28,679 cycles

DENT ON RT WING L/E NEAR WING ROOT, REF AFDL FOR INTERM REPAIR IAW STS EA 25-2014-051, PERMANENT REPAIR REQUIRED. DENT ON RT WING L/E NEAR WINGROOT REPAIRED. NO DEFECTS NOTED. RECEIVED DISPOSITION AND COMPLIED WITH EA 26-2015-199. REMOVED L/E INNER SKIN PANEL FOR ACCESS TO REPAIR AREA IAW SRM 51-42-06 51-42-13. REINSTALLED INNER SKIN PANEL IAW SRM 51-42-13 AND DWG 601R12016. RECEIVED AND COMPLIED WITH ECTC EA 26-2015-199, REV B.

Part: SUPPORT ANGLE — DAMAGED · airframe 30,838 hrs · 28,503 cycles

EXT POWER RECEPTACLE AFT SUPPORT ANGLE DAMAGED. REMOVED DAMAGE BRACKET. DRILLED UP NEW BRACKET IAW REO 601R-53-11-009. INSTALLED THE SUPPORT ANGLE IAW REO 601R-53-11-009. REPAIR CLASSIFIED AS MAJOR REPAIR IAW GMM 5-3.

Part: PLATE — DAMAGED (DAMAGED) · airframe 30,838 hrs · 28,503 cycles

EXT POWER RECEPTACLE DAMAGE. FABRICATED JOGGLE PLATE IAW REO 601R-53-11-009. INSTALLED IAW REO 601R-53-11-009. MAJOR REPAIR IAW GMM 5-3.

Part: BRACKET — DAMAGED · airframe 30,838 hrs · 28,503 cycles

EXT POWER RECEPTACLE SUPPORT BRACKET DAMAGE. REMOVED DAMAGE BRACKET. DRILLED UP NEW BRACKET IAW REO 601R-53-11-009. INSTALLED THE BRACKET IAW REO 601R-53-11-009. REPAIR CLASSIFIED AS MAJOR IAW GMM 5-3.

Part: GLOWSTRIP — DETERIORATED · airframe 30,147 hrs · 27,780 cycles

PHOTOLUMINESCENT FROM ROW 1CD TO ROW 8CD WATER DAMAGED. R & R PHOTOLUMINESCENT INSERT FROM ROW 1CD TO ROW 8CD IAW STC ST02687AT.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 29,598 hrs · 27,209 cycles

LIGHTED FLOOR-LEVEL EXIT SIGN INOPERATIVE LT SIDE OF GALLEY. R & R WIRE SPLICE CONNECTOR IAW SPM 20-17-31. SYSTEM OPS CHECKED GOOD. NO FURTHER ACTION.

Part: WINDSHIELD — FAILED (COCKPIT) · airframe 28,905 hrs · 26,513 cycles

F/O WINDSHIELD BEGAN ARCING AND SMALL CRACK, RAN QRH PROCEDURE 11-14, WINDSHIELD SHATTERED ONE MINUTE LATER. REMOVED AND REPLACED THE F/O'S WINDSHIELD IAW AMM 56-11-01. OPS AND LEAK CHECKED GOOD. ACFT OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,438 hrs · 26,066 cycles

EMERGENCY LIGHT BELOW F/A JUMPSEAT IS INOPERATIVE AND ITS WIRING HARNESS IS NOT TIED DOWN. R & R THE LIGHT IAW AMM 33-51-10.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 28,400 hrs · 26,031 cycles

RIGHT FORWARD EXTERNAL EMERGENCY LIGHT IS INOPERATIVE. R & R RT FWD EXTERNAL EMERGENCY LIGHT BULB IAW AMM 33-51-21. OPS CHECKED GOOD.

Part: FITTING — DAMAGED (RT MLG DOOR) · airframe 27,297 hrs · 24,927 cycles

RT MLG FWD DOOR SPACER FITTING HAS ELONGATED HOLE ON FUSLAGE SIDE. REPAIRED IAW EC/TC REO 601R-57-21-2059. MAJOR REPAIR.

Part: LIGHT — UNSERVICEABLE (CABIN) · airframe 27,297 hrs · 24,925 cycles

NUMEROUS COMPONENTS OF THE EMERGENCY TRACK LIGHTS FOUND UNSERVICEABLE. INSTALLED SERVICEABLE COVERS IAW ASA 33-51-00 SUPPLEMENT AND SAFETGLO MM 41-10, 33-60-10.

Part: FLOOR SUPPORT — CORRODED (BS 559) · airframe 27,297 hrs · 24,925 cycles

MINOR CORROSION FOUND AROUND FASTENER HOLES ALONG RT FLOOR SUPPORT RBL 17 BETWEEN BS 559 + 48 TO FS 559 + 112. REPAIRED FLOOR SUPPORT IAW GREO 601R-53-00-526 AND EC/TC REO601R-53-00-526. MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (BS 409) · airframe 27,297 hrs · 24,925 cycles

SEAT TRACK AT BS 409 TO 409+112 IS CORRODED IN VARIOUS PLACES AND HAS A GOUGE, R & R SEAT TRACK IAW AMM 53-01-11-000-802 AND 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 394-409) · airframe 27,297 hrs · 24,925 cycles

SEAT TRACK BS 394 TO 409 LBL 9 IS CORRODED IN VARIOUS PLACES, R & R SEAT TRACK IAW AMM 53-01-44-943-003 AND 53-01-420-001.

Part: SEAT TRACK — CORRODED (BS 364-394) · airframe 27,297 hrs · 24,925 cycles

SEAT TRACK BS 364 TO 394, LBL 9 IS CORRODED IN VARIOUS PLACES. R & R SEAT TRACK IAW AMM 53-01-11-946-003 AND 53-01-11-420-001.

Part: SEAT TRACK — CORRODED (BS 364-394) · airframe 27,297 hrs · 24,925 cycles

SEAT TRACK BS 364 TO 394, RBL 9 CORRODED IN VARIOUS AREAS. R & R SEAT TRACK IAW AMM 53-01-11-000-802 AND 53-01-11-400-802.

Part: SKIN — CRACKED (FUSELAGE) · airframe 27,297 hrs · 24,925 cycles

SKIN BELOW ADG PUMP CRACKED. REPAIRED IAW REO 601R-53-11-245. MAJOR REPAIR.

Part: SKIN — GOUGED (FUSELAGE) · airframe 27,297 hrs · 24,925 cycles

PASSENGER DOOR HINGE HALF ON FUSELAGE GOUGED AT LAST ASD HINGE LUG LAND. REPAIRED AREA ON THE PASS DOOR HINGE AFT LAND LUG IAW REO 601R-53-21-814 AND ECTC REO 601R-53-21-814. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW ASA SOP 5702.

Part: FAN — FAILED (DISPLAY) · airframe 27,002 hrs · 24,620 cycles

INFLIGHT DISPLAY COOL MASTER CAUTION MESSAGE. RAN QRH, MESSAGE WOULD NOT EXTINGUISH. ACFT RETURNED, EMERGENCY DECLARED, R & R NR 2 DISPLAY COOL FAN IAW AMM 21-24-19. IPC 21-24-00, FIG 10, ITEM 38 AND R & R COCK DISPLAY COOL AIR FILTER IAW 21-24-15. OPS CK GOOD, NO FURTHER DEFECT NOTED.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 26,268 hrs · 23,845 cycles

FLOOR LEVEL EMERGENCY FLOODLIGHT LENS MISSING ON WARDROBE. INSTALLED LENS IAW AMM 33-51-19.

Part: CONTROL SYSTEM — MALFUNCTIONED (RUDDER) · airframe 25,212 hrs · 22,772 cycles

UNCOMMANDED RUDDER MOVEMENTS, WITH YAW DAMP OFF OR ON. DISCONNECTED AP/ YAW DAMPER, ACFT CONTINUED TO MAKE UNCOMMANDED RUDDER INPUTS. ACFT DIVERTED, EMERGENCY DECLARED. COMPLIED WITH FDR DOWNLOAD IAW AMM 31-31-01. REMOVED & REPLACED NR 1 AND NR 2 YAW DAMPER ACTUATORS IAW AMM 22-22-01, OPS & LEAK CHECKED GOOD. R & R NR 1 AND NR 2 FCC CARDS IAW AMM 22-12-14, OP'S CHECKED GOOD. R & R AILERON & RUDDER TRIM CONTROL PANEL IAW AMM 27-12-10, OP'S CHECKED GOOD. COMPLIED WITH OP'S & LEAK CHECK OF RUDDER PCUS' NR 1, NR 2, AND NR 3 IAW AMM 27-23-01. NO DEFECTS NOTED. ACFT OK FOR SERVICE.

Part: ANCHOR FITTING — CRACKED (PAX DOOR) · airframe 23,886 hrs · 21,334 cycles

FWD PAX DOOR ANCHOR FITTING CRACKED. R & R FWD PAX DOOR ANCHOR FITTING IAW AMM 52-11-17. R & R FWD PAX DOOR ANCHOR FITTING IAW AMM 52-11-17.

Part: BEAM — CORRODED (BS 349-364) · airframe 23,300 hrs · 20,660 cycles

TRANSVERSE BEAM CORRODED AT SERVICE DOOR AND FLOOR EDGE MEMBERFROM FS 349 TO 364. REPAIRED IAW GMM 3-3.

Part: SILL — CORRODED (BS 304-349) · airframe 23,288 hrs · 20,646 cycles

SILL PLATE HAS CORROSION AT SERVICE DOOR AND FLOOR EDGE HAS CORROSION FROM FS 349 TO 304.00. REMOVED CORRODED SILL PLATE IAW SRM 51-42-06, 51-42-13 AND 51-42-21. DRILLED AND LOCATED IAW SRM 51-40-06 AND 51-40-11. COMPLIED WITH REO 601R-53-21-2235. PERFORMED EDDY CURRENT OF SILL PLATE CUTLINES IAW NDTM 51-20-06. NO INDICATIONS NOTED. INSTALLED SILL PLATE.

Part: FRAME — CORRODED (BS 333) · airframe 23,288 hrs · 20,646 cycles

FOUND FS 333 LOWER FRAME IS CORRODED. FS 333 LOWER FRAME REPLACED.

Part: FRAME — CORRODED (BS 349) · airframe 23,288 hrs · 20,646 cycles

ON REMOVAL OF INTERCOSTAL, FOUND FRAME FS 349 CORRODED. MAJOR REPAIR.

Part: POST — CRACKED (BS 409) · airframe 23,288 hrs · 20,646 cycles

FS 409 + 128 POST RBL FAILS NDT WITH INDICATION IN INBD AFT UPPER RADIUS GREATER THAN 50 PERCENT SCREEN HEIGHT. REPAIRED IAW REO 601R-53-41-1521.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 23,288 hrs · 20,646 cycles

PAX DOOR FLOOR SUPPORT ANGLE HAS CORROSION AROUND NUTPLATE AND PROX SWITCH. (OPEN)

Part: BULKHEAD WEB — CRACKED · airframe 23,288 hrs · 20,646 cycles

FOUND REAR PRESSURE BULKHEAD WEB HAS INDICATIONS NOTED AT LBL 18.00, WL106 APPROX .5" IN LENGTH 90 PERCENT FSH FAILED NDT INSPECTIONS. BONDED 2 STANDOFF ON RT WING AFT SPAR WEB BETWEEN WS 0 & WS 62.5 AND 1 LT WING AFT SPAR WEB BETWEEN WS 0 & WS 62.5 IAW SRM 51-22-00.

Part: FRAME — CORRODED (BS 333) · airframe 23,288 hrs · 20,646 cycles

DURING REPAIR, FOUND FS 333 LOWER FRAME IS CORRODED. REMOVED FRAME IAW SRM CH 51-42-06 & 51-42-21 & FOUND CORROSION TO BE OUT OF LIMITS. LOCATED & DRILLED NEW SERVICEABLE FRAME IAW SRM CH 51-40-11. INSTALLED FRAME IAW SRM 51-42-06 AND 51-42-21.

Part: FITTING — CORRODED (PAX DOOR) · airframe 23,288 hrs · 20,646 cycles

PAX DOOR LOWER PORTION 4 EA FITTINGS HAVE CORROSION UNDER CMS 532-02. REMOVED 4 EA CLIPS FROM PAX DOOR LOWER CORNERS IAW SRM 51-42-06. REPLACED 4 EA FITTINGS ON PAX DOOR LOWER PORITION IAW SRM 51-42-06.

Part: FRAME — CORRODED (BS 349) · airframe 23,288 hrs · 20,646 cycles

UPON REMOVAL OF INTERCOSTALS BETWEEN STR 26L & 26R, FS STA 349 TO 364, FOUND FS 349 FRAME CORRODED. REMOVED FRAME SECTION IAW SRM 51-42-06 AND SRM 51-42-21. INSTALLED NEW LOWER FRAME SECTION IAW SRM 51-42-06 AND SRM 51-42-21.

Part: STRUCTURE — CORRODED (PAX DOOR) · airframe 23,288 hrs · 20,646 cycles

PAX DOOR HAS CORROSION UNDER CMS 532-02. REMOVED FWD AND AFT LOWER PAX DOOR CORNERS, LOCATED, DRILLED AND INSTALLED NEW SERVICEABLE 601R319983-3S AND 601R319983-4S CORNERS IAW SRM'S 51-42-06 AND 51-42-21.

Part: FRAME — CORRODED (BS 349) · airframe 23,288 hrs · 20,646 cycles

UPON REMOVAL OF INTERCOSTAL BETWEEN STR 26R AND 26L BETWEEN FS 349 AND 364, FOUND FS 349 CORRODED IN NUMEROUS AREAS BEWN STR 24L AND 24R. REPAIRED IAW SRM.

Part: BULKHEAD WEB — CRACKED · airframe 23,288 hrs · 20,646 cycles

FOUND REAR PRESSURE BULKHEAD WEB HAS A CRACK INDICATION NOTED AT LBL 36.20, WL 80 APPROX .5" IN LENGTH 50 PERCENT FSH FAILED NDT INSPECTION. REPAIRED IAW SRM 51-42-06 AND 51-42-21.

Part: POST — CRACKED (BS 409) · airframe 23,288 hrs · 20,646 cycles

FS 409+128 VERTICAL POST RBL18 FAILS NDT WITH AN INDICATION IN INBD AFT UPPER RADIUS GREATER THAN 50 PERCENT. REMOVED POST IAW SRM 51-42-22. INSTALLED NEW POST IAW SRM 51-42-06 AND REO 601R-53-41-889 & 601R-53-41-1521.

Part: FRAME — CORRODED (BS 349) · airframe 23,288 hrs · 20,646 cycles

UPON REMOVAL OF INTERCOSTALS BETWEEN STR 26R & 26L BETWEEN FS 349 & 364, FOUND FS 349 CORROSION IN NUMEROUS AREAS BETWEEN STR 24L & 24R. REMOVED CORROSION IAW SRM.

Part: INTERCOSTAL — CORRODED (BS 349) · airframe 23,288 hrs · 20,646 cycles

INTERCOSTAL LOCATED IN AVIONICS BAY ENTRANCE BETWEEN FS 349.0 & FS 364.0, STR 26R CORRODED. REPAIRED IAW SRM 51-42-21.

Part: BEAM — CORRODED (BS 280) · airframe 23,288 hrs · 20,646 cycles

FS 280 TRANSVERSE BEAM BETWEEN LBL 18 AND RBL 18 HAS SEVERAL AREAS OF CORROSION. REMOVED MINOR CORROSION ON FS 280 TRANSBEAM AFT J ANGLE IAW SRM 51-21-06. MATERIAL REMOVED .002 WITHIN LIMITS IAW SRM 53-00-00, FIG 102, SHEET 2. FWD J ANGLE BETWEEN LBL AND RBL 9 REQ REPLACEMENT, CORRODED BEYOND LIMITS. REMOVED FWD J ANGLE AND INSTALLED NEW SERVICEABLE FWD J ANGLE PN 600-34017-351S AT FS 280 LBL 9 TO RBL 9 IAW SRM 51-42-06 AND 51-42-21. FWD J ANGLE REQ'S PAINT ON THE TOP SIDE. PAINTED SURFACE OF ANGLE IAW SRM 51-25-16. (SDR CLOSED)

Part: BRACKET — CRACKED (RT WING) · airframe 23,288 hrs · 20,646 cycles

RT WING L/E INBD SECTION 620JL HAS CRACKED BRACKET AT OTBD END WS140.00. LOCATED, DRILLED AND DEBURRED NEW ANGLE IAW SRM 51-40-11. INSTALLED IAW SRM 53-00-47 AND CMM CGFP-02, REPAIR I.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 23,288 hrs · 20,646 cycles

INTERCOSTAL LOCATED IN AVIONICS BAY CORRODED. FOUND INTERCOSTAL TO HAVE LIGHT CORROSION AND TO BE WITHIN LIMITS IAW SRM 53-00-00. REMOVED CORROSION IAW SRM 53-21-23, 53-00-00 AND 51-21-06. ORIGINAL THICKNESS .080, MATERIAL REMOVED MAX .008. FOUND TO BE IN LIMITS IAW SRM 53-00-00, FIG 102, SH 1 AND SH 2.

Part: ANGLE — CRACKED (BS 621-625) · airframe 23,288 hrs · 20,646 cycles

RT FS 621 TO 625 OBLIQUE ANGLE IS CRACKED. R & R ANGLE IAW SRM 51-42-21.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 23,288 hrs · 20,646 cycles

INTERCOSTAL IN AVIONIC BAY CORRODED. REPAIRED IAW SRM 51-42-06, SRM 51-42-21.

Part: BULKHEAD WEB — CRACKED · airframe 23,288 hrs · 20,646 cycles

FOUND REAR PRESSURE BULKHEAD WEB HAS A CRACK INDICATION NOTED AT LBL 18.00, WL106 APPROX .5" IN LENGTH 90 PERCENT FSH FAILED NDT INSPECTION. REPAIRED IAW REO 601R-53-61-1285.

Part: BEAM — CORRODED (BS 349) · airframe 23,288 hrs · 20,646 cycles

FS 349 TRANSVERSE BEAM OTBD END AT PAX DOOR HAS CORROSION. REMOVED CAP ON FS 349 BEAM AT PAX DOOR ENTRANCE TO ACCESS CORROSION REMOVAL IAW SRM 51-42-13. REINSTALLED BEAM CAP IAW SRM 51-42-13, 51-42-15 AND 51-25-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 23,288 hrs · 20,646 cycles

PAX DOOR FLOOR SUPPORT ANGLE HAS CORROSION AROUND THE NUT PLATES. REMOVED ANGLE IAW SRM 51-42-06, 51-42-10 AND 51-42-21. INSTALLED NEW ANGLE IAW SRM 51-42-06, 51-42-11 AND 51-42-21.

Part: BEAM — CORRODED (BS 349) · airframe 23,288 hrs · 20,646 cycles

FS 349, TRANSVERSE BEAM HAS CORROSION AT SERVICE DOOR AND FLOOR EDGE MEMBER HAS CORROSION FROM FS 349 TO 364.00. REMOVED CORRODED ANGLE AND INSTALLED NEW ANGLE PN 38783-13 IAW SRM 51-42-06 AND 51-42-21. REMOVED MINOR CORROSION IAW SRM 51-21-06. MAT REMOVED .003". DAMAGE WITHIN ALLOWABLE LIMITS IAW SRM 53-00-00, FIG 102, SHEET 2.

Part: FLOOR SUPPORT — CORRODED (BS 409) · airframe 23,288 hrs · 20,646 cycles

FLOOR STRUCTURE, RBL 9 FROM FS 409.00+16 TO 409.00+64 HAS SEVERAL AREAS OF CORROSION. REMOVED CORROSION IAW REO 601R-53-00-005 STEP 1, FOUND TO BE WITHIN LIMITS IAW REO 601R-53-00-005, SHEETS 4-7 AND SRM 51-21-06.

Part: FITTING — CRACKED (WINDSHEILD) · airframe 23,288 hrs · 20,646 cycles

CO-PILOTS WINDSHIELD AFT LOWER FITTING ON SIDE POST IS CRACKED IN THE RADIUS. REMOVED CO-PILOTS WINDSHIELD AFT LOWER FITTING ON SIDE POST AND INSTALLED NEW SERVICEABLE FITTING PN 601R-332535-45 IAW SRM 51-42-21. THIS REPAIR REQUIRES MAJOR/MINOR CLASSIFCATION IAW ASA SOP 5702. THIS REPAIR IS CLASSIFIED AS A MINOR REPAIR IAW ASA SOP 5702. (SDR CLOSED)

Part: WINDOW FRAME — CRACKED (COCKPIT) · airframe 23,288 hrs · 20,646 cycles

PILOTS WINDSHIELD AFT LOWER FITTING ON SIDE POST IS CRACKED IS CRACKED IN THE RADIUS. LOCATED AND DRILLED NEW WINDSHIELD FITTING LOWER AFT PILOT SIDE IAW SRM 51-40-11 AND INSTALLED NEW WINDSHIELD FITTING LOWER AFT PILOT SIDE IAW SRM 51-42-21.

Part: ISOLATOR — BROKEN (BS 621 BULKHEAD) · airframe 23,288 hrs · 20,646 cycles

TWO ISOLATORS ARE BROKEN ON FS 621 BULKHEAD. REMOVED BROKEN ISOLATORS IAW SRM 51-42-10, FIG 4. INSTALLED NEW ISOLATORS IAW SRM 51-42-13, FIG 2.

Part: SIGN — DISLODGED (EMERGENCY LIGHTS) · airframe 22,701 hrs · 19,990 cycles

GALLEY EXIT SIGN FELL OFF. R & R GALLEY EXIT LIGHT IAW AMM 33-00-00.

Part: DRAG ANGLE — CORRODED (PAX DOOR) · airframe 22,547 hrs · 19,821 cycles

REF AIRSTAIR DOOR AFT DRAG ANGLE BY MOTOR PULLEY BRACKET CRACKED. REPAIRED AIRSTAIR DOOR DRAG ANGLE IAW EC/TC REO 601R-52-11-513. CLEARED, ADVISED. (CLOSED)

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 22,521 hrs · 19,790 cycles

AFT DRAG ANGLE BY MOTOR PULLEY CRACKED E/C T/C REO 601R-52-11-503. COMPLIED WITH REINSPECTION IAW E/C T/C REO 601R-52-11-503. NO FURTHER CRACK PROPAGATION NOTED. (CLOSED)

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 22,440 hrs · 19,706 cycles

ASD AFT DRAG ANGLE BY MOTOR PULLEY CRACKED REINSPECT. C/W REINSPECT OF PAX DOOR AFT DRAG ANGLE CRACK IAW REO601R-52-11-503. NO FURTHER DAMAGE NOTED. (OPEN)

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 22,402 hrs · 19,665 cycles

AFT DRAG ANGLE BY MOTOR PULLEY CRACKED, REINSP. COMPLIED WITH VISUAL REINSPECT OF AFT DRAG ANGLE. NO FRUTHER DAMAGE NOTED AS OF THIS TIME IAW REO601R-52-11-503. (OPEN)

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 22,351 hrs · 19,607 cycles

AFT DRAG ANGLE CRACK DUE REINSPECT. C/W REINSPECT OF AFT DRAG ANGLE CRACK IAW REO 601R-52-11-503. NO FURTHER DEFECTS NOTED AT THIS TIME. (CLOSED)

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 22,233 hrs · 19,475 cycles

PAX DOOR AFT DRAG ANGLE CRACKED BY MOTOR PULLEY. C/W REINSPECT OF PAX DOOR AFT DRAG ANGLE BY MOTOR PULLEY IAW REO 601R-52-11-503. NO FURTHER DEFECTS NOTED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,233 hrs · 19,475 cycles

RT EMERGENCY LIGHT BY SERVICE DOOR INOP. R & R RT EMERGENCY LIGHT IAW AMM 33-51-21. OPS TEST GOOD. R & R RT EMERGENCY LIGHT IAW AMM 33-51-21. OPS TEST GOOD. (CLOSED)

Part: OIL SYSTEM — LOW (ENGINE) · airframe 22,250 hrs · 19,498 cycles

LT ENGINE OIL PRESSURE WARNING IN FLIGHT. EMERGENCY DECLARED AS A PRECAUTION, SERVICED NR 1 AND NR 2 ENGINES TO FULL, REQUIRES ENGINES RUN. OPEN COWLINGS AND INSPECTED NR 1 ENGINE FOUND NO LEAKS. CLOSED COWLING. SERVICED ENGINES IAW IAW AMM 12-13-79. OPENED AND CLOSED COWLING IAW AMM 71-11-01.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 21,818 hrs · 19,015 cycles

AFT DRAG ANGLE BY MOTOR PULLEY CRACKED, REINSP DUE C/W REINSP OF PAX DOOR AFT DRAG ANGLE IAW REO 601R-52-11-503. (CLOSED)

Part: BPSU — FAILED (TE FLAPS) · airframe 21,792 hrs · 18,984 cycles

FLAPS FAILED ON TAKEOFF AT 8 DEG WHEN ATTEMPTED TO RETRACT. RETURNED TO DEPARTURE AND LANDED. FLAPS 8 DEG AFTER RUNNING QRH WITH LESS THEN 40 FPM DESCENT, ACFT RETURNED TO DEPARTURE AFTER T/O -- EMERGENCY DECLARED. TROUBLESHOT IAW FIM 27-50-00, FLAGGED LEFT BPSU. R & R LT BPSU IAW AMM 27-51-10. OPS CHECK GOOD.

Part: BPSU — FAILED (TE FLAPS)

FLAPS FAIL CAUTION MESSAGE ON APPROACH. FLAPS AT ZERO SELECTING 8 DEGREES. DIVERTED, EMERGENCY DECLARED. COMPLIED WITH AD2009-06-12

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 21,058 hrs · 18,127 cycles

RT EMERGENCY LIGHT INOP FWD OF EMERGENCY DOOR EXIT. R & R RT EMERGENCY LIGHT BULB FWD OF EMERGENCY DOOR EXIT IAW AMM 33-50-01 OPS CK GOOD.

Part: FRAME — CRACKED (BS 718) · airframe 19,579 hrs · 16,430 cycles

FS 718 FRAME DOUBLER HAS POSSIBLE CRACK.

Part: BULKHEAD — CRACKED · airframe 19,579 hrs · 16,430 cycles

PRESSURE BULKHEAD IS CRACKED APPROX ½" L AT 12 O'CLOCK POSITION FOR PARKING BRAKE CABLE BULKHEAD FITTING.

Part: BULKHEAD — CRACKED (BS 621) · airframe 19,579 hrs · 16,430 cycles

50 PERCENT FSH HFEC INDICATION NOTED APPROX 0.25" LONG IN THE FS 621.00 BULKHEAD WEB, EXTENDING FROM THE VB LWR CORNER OF THE LINTEL FITTING. FAILS NDT INSP AT THIS TIME. REPAIR IAW EC/TC REO 601R-53-61-1230 HAS BEEN COMPLETED AND REPAIR C/W THE REQUIREMENTS OF EC/TC AND REO 601R-53-61-1230 REV D.

Part: BULKHEAD — CRACKED (BS 621) · airframe 19,579 hrs · 16,430 cycles

80 PERCENT FSH HFEC INDICATION NOTED APPROX 0.3 IN LENGTH IN FS 621.00 PRESSURE BULKHEAD WEB AT LBL 27.5, WL 131.00 (APPROX) INDICATION IS MARKED ON ACFT. FAILS NDT INSP AT THIS TIME. C/W EC/TC REO 601R-53-61-1541. BEAD SEALED AROUND REPAIR IAW SRM 51-23-00 SECTION B STEPS 1-6. COMPLIED WITH EC/TC REO 601R-53-61-1541.

Part: POST — CRACKED (BS 409) · airframe 19,579 hrs · 16,430 cycles

FS 409+128 VENT POST RBL 18 FAILS NDT INSP WITH AN INDICATION IN THE OTBD AFT RADIUS. MEASURES GREATER THAN 50PERCENT SCREEN HEIGHT. APPROX .2 INCHES LONG. REMOVED FS 409+128 RBL 18 IB & OB POSTS IAW SRM 51-42-06. ALSO REMOVED 3 EACH SCREWS FROM ADEL CLAMPS THAT WERE ATTACHED TO THE POSTS. ATTACHED TO INBD POST AND BOTH NEED INSTALLED. ASSEMBLED INBD AND OTBD POSTS AT FS4-9 AND 128 RBC 18 IAW SRM 51-42-06. INSTALLED INBD AND OTBD POSTS IAW REO 60R-53-41-889 AND INSTALLED 3 EACH ADEL CLAMPS TO POSTS IAW SRM 51-41-02. 15 EACH RIVETS AT TOP OF FS 409+128 RBL 18 POST IAW SRM 51-42-06. COMPLIED WITH EC/TC REO 601R-53-41-889 AND MEET ALL REQUIREMENTS OF REO 601R-53-41-889.

Part: POST — CRACKED (BS 409) · airframe 19,579 hrs · 16,430 cycles

FS 409+128 VERT POST LBL 18 FAILS NDT INSP WITH AN INDICATION IN OTBD AFT RADIUS AND AT INBD AFT RADIUS. BOTH MEASURES GREATER THAN 50 PERCENT SCREEN HEIGHT (APPROX .2 INCHES LONG). REMOVED FS 409+128 LBL 18 INBD AND OTBD POSTS IAW SRM 51-42-06. LOCATED AND DRILLED POST IAW SRM 51-40-11. INSTALLED NEW POST AT FS 409+128 LBL18 INBD AND OTBD IAW SRM 51-42-06 AND REO 601R-53-41-889. COMPLIED WITH EC/TC REO 601R-53-41-889 AND MET ALL THE REQUIREMENTS OF REO 601R-53-41-889.

Part: ANGLE — CORRODED (SERVICE DOORWAY) · airframe 19,579 hrs · 16,430 cycles

SERVICE DOOR THRESHOLD LOWER ANGLE BETWEEN FS 319.7 AND FS 349.00 (BENEATH STOP FITTINGS) HAS CORROSION RUNNING UNDER LOCK FASTENER HEADS AND STOP FITTING SERRATED MOUNT PLATES. DRILLED OFF & REMOVED SERVICE DOOR THRESHOLD LWR ANGLE. CHEMICALLY STRIPPED CORRODED AREA & CORROSION EVALUATED IAW SRM 51-21-06. FOUND DAMAGE TO BE WITHIN ALLOWABLE LIMITS IAW SRM 53-00-00. LPI REQUIRED. PERFORMED LPI ON BLENDED AREAS IAW NDTM 51-20-08. INDICATIONS OF CORROSION/DAMAGE NOTED IN ALL 8 STOP FITTING MOUNT HOLES.

Part: ANGLE — CRACKED (BS 621-625) · airframe 19,579 hrs · 16,430 cycles

LT AFT FUSELAGE 621-625 OBLIQUE ANGLE CRACKED. REMOVED LT AFT FUSELAGE 621-625 OBLIQUE ANGLE. INSTALLED NEW SERVICEABLE OBLIQUE ANGLE (LT AFT FUSELAGE 621-625) IAW CRJ 200 SRM 51-42-21, STEPS 5(A) AND STEP 9 (C, 1,

Part: CARGO TRACK — CORRODED (BS 615) · airframe 19,578 hrs · 16,430 cycles

CARGO BAY LBL 9 SEAT TRACK AT FS 615.5 CORRODED. REMOVED CARGO SEAT TRACK AT FS 615.5 LBL 9 BY REMOVING SCREWS. LOCATED, DRILLED AND CSK SERVICEABLE SEAT TRACK IAW SRM 51-40-11. SEAT TRACK REQUIRES INSTALLATION. REPLACED AND INTALLED SERVICEABLE SEAT TRACK IAW SRM 51-41-02 SECTION 3 STEP 2(A THRU D). SEALED AREA ON SEAT TRACK IAW SRM 51-23-00 SECTION E STEP 1 THRU 6.

Part: ANGLE — CRACKED (BS 621-625) · airframe 19,579 hrs · 16,430 cycles

RT AFT FUSELAGE 621-625 OBLIQUE ANGLE CRACKED. REMOVED RT AFT FUSELAGE 621-625 OBLIQUE ANGLE. INSTALLED NEW SERVICEABLE OBLIQUE ANGLE IAW SRM 51-42-21, STEP 5(A) AND STEP 9 (C, 1 A, B, & 2).

Part: SEAT TRACK — CORRODED (BS 559) · airframe 19,578 hrs · 16,430 cycles

CARGO BAY SEAT TRACK LBL 27 FS 559.0+80 CORRODED. REMOVED CARGO BAY SEAT TRACK LBL 27 AT FS 559+80 IAW AMM SUBTASK 3(B)1-3. LOCATED, DRILLED, AND CSK HOLES IN SERVICEABLE SEAT TRACK IAW SRM 51-40-11. REMOVAL PERFORMED IAW AMM SUBTASK 53-01-11-020-002 (3) B1-3. SEAT TRACK REQUIRES INSTALLATION. REPLACED AND INSTALLED SERVICEABLE SEAT TRACK IAW SRM 51-41-02 SECTION 3 STEP 2 (A THROUGH D). SEALED AREA ON SEAT TRACKS IAW SRM 51-23-00 SECTION E STEPS 1 THROUGH 6.

Part: SEAT TRACK — CORRODED (BS 574) · airframe 19,579 hrs · 16,430 cycles

CARGO BAY SEAT TRACK RBL 9 FS 574 CORRODED. REMOVED CARGO BAY SEAT TRACK AT RBL 9 FS 574 BY REMOVING SCREWS FROM TRACK. LOCATED, DRILLED AND CSK SERVICEABLE SEAT TRACK IAW SRM 51-40-11. SEAT TRACK REQUIRES INSTALLATION. REPLACED AND INSTALLED SERVICEABLE SEAT TRACK IAW SRM 51-41-02 SECTION 3 STEP 2(A THRU D). SEALED AREA ON SEAT TRACK IAW SRM 51-23-00, SECTION E STEPS 1 THRU 6.

Part: SEAT TRACK — CORRODED (BS 574) · airframe 19,578 hrs · 16,430 cycles

CARGO BAY LBL 9 SEAT TRACK CORRODED JUST FWD OF FS 574.00. REMOVED CARGO BAY SEAT TRACK AT LBL 9 FS 574 BY REMOVING SCREWS. LOCATED, DRILLED AND CSK SERVICEABLE SEAT TRACK IAW SRM 51-40-11. SEAT TRACK REQUIRES INSTALLATION. REPLACED AND INSTALLED SERVICEABLE SEAT TRACK IAW SRM 51-41-02 SECTION 3 STEP 2(A THRU D). SEALED AREA ON SEAT TRACK IAW SRM 51-23-00 SECTION E STEP 1 THRU 6.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 19,579 hrs · 16,430 cycles

CARGO BAY SEAT TRACK RBL 9 FS 559+80 CORRODED. REMOVED CARGO BAY SEAT TRACK AT RBL 9 FS 559+80 BY REMOVING SCREWS FROM TRACK. LOCATED, DRILLED AND CSK SERVICEABLE SEAT TRACK IAW SRM 51-40-11. SEAT TRACK REQUIRES INSTALLATION. REPLACED AND INSTALLED SERVICEABLE SEAT TRACK IAW SRM 51-41-02 SECTION 3 STEP 2(A THRU D). SEALED AREA ON SEAT TRACK IAW SRM 51-23-00, SECTION E STEPS 1 THRU 6.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 19,578 hrs · 16,430 cycles

CARGO BAY SEAT TRACK LBL 9 FS 559.00+80 CORRODED. REMOVED CARGO BAY SEAT TRACK AT RBL 9 FS 559.+80 BY REMOVING SCREWS FROM TRACK. LOCATED, DRILLED AND CSK SERVICEABLE SEAT TRACK IAW SRM 51-40-11. SEAT TRACK REQUIRES INSTALLATION. REPLACED AND INSTALLED SERVICEABLE SEAT TRACK IAW SRM 51-41-02 SECTION 3 STEP 2(A THRU D). SEALED AREA ON SEAT TRACK IAW SRM 51-23-00, SECTION E STEPS 1 THRU 6.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 19,579 hrs · 16,430 cycles

CARGO BAY SEAT TRACK RBL 27 FS 559+80 CORRODED. REMOVED CARGO BAY SEAT TRACK AT RBL 27 F.S. 559+80 IAW AMM SUBTASK 53-01-11-020-002 (B)1-3. LOCATED HOLES IN SERVICEABLE SEGMENT AND CSK HOLES IAW SRM 51-40-11. SEAT TRACKS REQUIRE INSTALLATION IAW AMM. REPLACED AND INSTALLED SERVICEABLE SEAT TRACK IAW SRM 51-41-02 SECTION 3 STEP 2 (A-D). SEALED AREA ON SEAT TRACK IAW SRM 51-23-00 SECTION E STEPS 1-6.

Part: CHANNEL — CRACKED (CARGO DOORWAY) · airframe 19,579 hrs · 16,430 cycles

CARGO DOOR SURROUND STRUCTURE CHANNEL IS CRACKED. REMOVED CARGO DOOR SURROUND STRUCTURE CHANNEL. INSTALLED NEW CHANNEL AT CARGO DOOR SURROUND STRUCTURE USING SOLID RIVETS IAW SRM 51-42-06, STEP 2(A) AND STEP 8(A).

Part: FRAME — CRACKED (BS 559) · airframe 19,579 hrs · 16,430 cycles

WHILE PERFORMING FS 559 BULKHEAD WEB AND FRAME INSP AN INDICATION WAS NOTED AT THE LT CAP ANGLE AT BUTT LINE 18 IN RADIUS APPROX .30 IN LENGTH AND 79 PERCENT FULL SCREEN HEIGHT. FAILS NDT. COMPLIED WITH EC/TC REO 601R-53-41-260 IAW REO 601R-53-41-260 REV D.

Part: POST — CRACKED (BULKHEAD) · airframe 19,579 hrs · 16,430 cycles

WHILE PERFORMING FS 559 BULKHEAD WEB AND FRAME CAP ANGLE INSP AN INDICATION WAS NOTED AT THE LT WEB VERTICAL POST BL 18, WL 52 AT CHEM MILL RADIUS APPROX .20 IN LENGTH AND 40 PERCENT F.S.H. FAILS NDT. REPAIRED FS 559 BULKHEAD WEB BETWEEN LBL 9 AND LBL 18 POST IAW REO 601R-53-41-609 DEVIATION. COMPLIED WITH EC/TC REO 601R-53-41-609 AND MET ALL THE REQUIREMENTS OF REO 601R-53-41-609 REV.A.

Part: FLOORBEAM — CORRODED (BS 349) · airframe 19,579 hrs · 16,430 cycles

FLOOR SUPPORT CROSS MEMBER CORRODED AT FS 349 S18 UPPER OTBD END. DRILLED OFF, REMOVED FWD CLIP PN 601R38303-175 AFT CLIP PN 601R31148-18 AND TEE BRACKET PN 601R38334-3 FROM OTBD END OF FS 349 CROSSBEAM AT RBL 42 TO ACCESS CROSSBEAM CORROSION. REMOVED 3EA HI-LITES FROM FS 349 BELOW CROSSBEAM RBL 42 TO ACCESS T-BRACKET FASTENER REMOVAL. ALL WORK IAW SRM 51-42-21, REMOVAL STEP 11 A AND B AND SRM 51-42-06 REMOVAL STEP 11A-B6. REMOVED ALL CORROSION IAW SRM 651-21-06 STEP 1, 2, 3, A,B, 1-5. ALODINED AREA IAW SRM 51-21-11 PART D1 A-F. APPLIED PRIMER AND TOP COAT IAW SRM 51-25-16 STEPS 1-5.

Part: POST — CRACKED (BULKHEAD) · airframe 19,579 hrs · 16,430 cycles

WHILE PERFORMING FS 559 BULKHEAD WEB AND FRAME CAP ANGLE INSP AN INDICATION WAS NOTED AT THE RT VERTICAL POST BL 9, WL 58.70 APPROX 1" OTBD OF POST ON WEB VERTICALLY, INDICATION IS APPROX 10 IN LENGTH AT 23 PERCENT FULL SCREEN HEIGHT. FAILS NDT. C/W EC/TC REO 601R-53-41-260 IAW REO 601R-53-41-260 REV D.

Part: FLOOR SUPPORT — CORRODED (BS 319.7 S18) · airframe 19,579 hrs · 16,430 cycles

FLOOR SUPPORT BRACKET CORRODED AT FS 319.7 S18. REMOVED FLOOR SUPPORT BRACKET FOR REPLACEMENT IAW SRM 51-42-06 PG 18. REMOVED SILL PLATES JUST FWD OF SUPPORT BRACKET AND ATTACH CLIP JUST AFT OF SUPPROT BRACKET IAW SRM 51-42-06. INSTALLED NEW SERVICEABLE FLOOR SUPPORT BRACKET IAW SRM 51-40-11 AND 51-42-21. REINSTALLED SILL PLATES FWD OF SUPPORT BRACKET. ATTACH CLIP AFT OF SUPPORT BRACKET IAW SRM 51-42-06 AND 51-42-13.

Part: PLACARD — DETERIORATED (ESCAPE HATCH) · airframe 19,579 hrs · 16,430 cycles

CREW ESCAPE HATCH PLACARDS ARE DETERIORATED. APPLIED NEW SILKSCREENS TO CREW ESCAPE HATCH IAW MM 11-10-03, TASK 11-10-03-400-801 SECTION 1A, B AND C 2A.

Part: FLOOR SUPPORT — CRACKED (BS 484) · airframe 19,579 hrs · 16,430 cycles

LT FS 484 FLOOR SUPPORT ANGLE CRACKED LBL 27. REMOVED FS 484 FLOOR SUPPORT ANGLE AT LBL 27 IAW SRM 51-42-06. NEW CLIP NEEDS INSTALLED. INSTALLED A NEW CLIP IAW REO 601R-53-41-059 REV.B STEPS 9-12 AND 14. REQUIRES AN ECTC. REPAIR TO THE INTERCOSTALS AT FS 484 BETWEEN BL 27.00 AND BL 36.00 IS COMPLETED IAW REO 601R-53-41-059 AND MEETS WITH ALL THEIR REQUIREMENTS.

Part: FLOORBEAM — CRACKED (BS 484) · airframe 19,579 hrs · 16,430 cycles

RT FS 484 PREVIOUS REPAIR FLOOR SUPPORT ANGLE CRACKED AT RBL 36.

Part: FLOORBEAM — CRACKED (BS 484) · airframe 19,578 hrs · 16,430 cycles

RT FS 484 PREVIOUS REPAIR FLOOR SUPPORT ANGLE AT RBL 27 CRACKED. REMOVED CRACKED CLIP IAW SRM 51-42-21 STEP 11 A AND B. INSTALLED NEW SERVICEABLE CLIP AT RBL 27 IAW SRM 51-42-21 STEP 9 A1 STEP C1 A AND B AND PART 2.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 19,187 hrs · 16,008 cycles

THREE CAUTION MSG GROUND SPOILER, DEPLOY SPOILER FLIGHT SPOILERS SPOILERONS INFLIGHT BEFORE ALL RECEIVED FLIGHT SPOILERS STATUS MSG. AIRCRAFT RETURNED TO ATL AFTER T/O. EMERGENCY DECLARED. FLT 5439, 5619 CX.

Part: DOOR — STUCK (CABIN) · airframe 19,169 hrs · 15,989 cycles

MAIN CABIN DOOR WILL NOT OPEN. FLT 5529 DEL 30 MINS. PASSENGER DOOR POWER ASSIST SYSTEM.

Part: SIGN — BROKEN (CABIN) · airframe 18,264 hrs · 15,148 cycles

EMERGENCY EXIT SIGN BROKEN AT SERVICE DOOR.

Part: WIRE HARNESS — DAMAGED (NLG STEERING) · airframe 17,384 hrs · 14,325 cycles

AFTER TAKEOFF RECEIVED "STEERING INOP" CAUTION MSG. COMPLIED WITH QRH AND LANDED WITH NWS INOP. REMOVED STEERING WIRING HARNESS P/N 17300-233 & INSTALLED STEERING WIRING HARNESS P/N 17300-233 ALL WORK PERFORMED IAW AMM SECTION 32-61-25, OPS CHECK REQUIRED. PERFORMED OPS CHECK GOOD. PERFORMED OPS CHECK IAW SECTION 32-61-00 & FOUND NOSE WHEEL STEERING IN GOOD WORKING CONDITION.

Part: WIRE — DAMAGED (EMERGNECY LIGHTS) · airframe 15,643 hrs · 12,794 cycles

LEFT AFT MOST EXTERNAL EMERGENCY LIGHT INOP. EXTERIOR EMERGENCY LIGHTS - ONE OF TWO REARWARD ON EACH SIDE. FOUND WIRE (BETWEEN LIGHT AND TB107) BROKEN. REPAIRED WIRE IAW CRJ 200 ELECTRICAL/ELECTRONICS STANDARD PRACTICES MANUAL. OPS CK GOOD.

Part: FITTING — CORRODED · airframe 15,389 hrs · 12,560 cycles

HORIZONTAL ANTI-ROTATION FITTING CORRODED.

Part: SKIN — CORRODED (ACCESS PANEL) · airframe 15,378 hrs · 12,548 cycles

FUEL ACCESS CUTOUT 550BB HAS CORROSION ON I/N SIDE. CORROSION AT CUTOUT 65000 REMOVED PER REO 601R-57-21-030-07 ELITE STRUCTURAL SERVICES WO 50237 5000-0064. SUPPLEMENTAL - SDR CLOSED 11/20/07.

Part: SKIN — CORRODED (ACCESS PANEL) · airframe 15,378 hrs · 12,548 cycles

AAR - FUEL ACCESS CUTOUT 640BB HAS CORROSION ON O/B SIDE. CORROSION AT CUTOUT 540BB REMOVED PER REO 601R-57-21-030 ON ELITE STRUCTURAL SERVICER. SUPPLEMENTAL - SDR CLOSED 11/20/07.

Part: ATTACH FITTING — CRACKED (BLOCKER DOOR) · airframe 15,378 hrs · 12,548 cycles

LEFT T/R BLOCKER DOOR NR 7 LINK ATTACH LUG CRACKED.

Part: ATTACH FITTING — CRACKED (THRUST REVERSER) · airframe 15,378 hrs · 12,548 cycles

AAR - LEFT T/R BLOCKER DOOR NR 7 LINK ATTACH LUG CRACKED. DUPLICATE ENTRY (SEE DEFECT 119411-1) SUPPLEMENTAL - SDR CLOSED 11/13/07.

Part: HINGE — CORRODED (LT ELEVATOR) · airframe 15,378 hrs · 12,548 cycles

LT ELEVATOR CENTER HINGE BEARING HAS AXIAL AND RADIAL PLAY AND CORROSION. CORROSION REMOVED.

Part: BULKHEAD — CRACKED (BS 280) · airframe 15,378 hrs · 12,548 cycles

AAR - PILOTS BULKHEAD AT FS 280.0 AND LBL 9.0 IS CRACKED IN LOWER RADIUS. PERFORMED REPAIR TO PILOT'S BULKHEAD AT FS 280.0 AND LBL 9.0, PER: REO 601R-53-11-171, REV D. SUPPLEMENTAL - SDR CLOSED 11/13/07.

Part: ANGLE — CRACKED (BS 484) · airframe 15,378 hrs · 12,548 cycles

AAR - FS 484 I/B OF LBL 36 ANGLE IS CRACKED.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 15,378 hrs · 12,548 cycles

AAR - FS 280 FLOOR SUPPORTS CRACKED O/B OF RBL 9.0. PERFORMED REPAIR TO FS 280.0 BULKHEAD AT RBL 9.0 PER: REO 601R-53-11-171, REV D, IAW EO 600-53-0090. SUPPLEMENTAL - SDR CLOSED 11/13/07.

Part: DOUBLER — CRACKED (PAX DOOR) · airframe 15,378 hrs · 12,548 cycles

DOUBLER INSIDE PAX DOOR AT FS 333 IS CRACKED. REMOVED CRACKED UN-SERVICEABLE DOUBLER FROM INSIDE PAX DOOR AT FS 333. LOCATED NEW SERVICEABLE DOUBLER P/N 601R318094-2 AT PAX DOOR FS 355 IAW CRJ 200 SRM 51-42-06, 51-42-10 AND 51-42-21. 14212

Part: PLACARD — DAMAGED (PAX DOOR) · airframe 15,378 hrs · 12,548 cycles

PANEL 832 BT ON PAX DOOR HAS 1 EACH DAMAGED EXIT PLACARD.

Part: ESCAPE HATCH — STUCK · airframe 15,378 hrs · 12,548 cycles

CREW ESCAPE HATCH FAILS FUNCTIONAL TEST, REQUIRES MORE THAN 120 INCH POUNDS TO OPEN. REMOVED CREW ESCAPE HATCH HANDLE ASSEMBLY. 13254. OK TO INSTALL NEW CREW ESCAPE HATCH HANDLE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,235 hrs · 12,429 cycles

LEFT AFT OVERWING EMERGENCY LIGHT LAMP INOP.

Part: UNKNOWN — UNKNOWN (NLG STEERING) · airframe 14,008 hrs · 11,206 cycles

STEERING INOP MESSAGE FOLLOWED BY GEAR DISAGREE MESSAGE, NOSE GEAR WOULD NOT RETRACT, RETURNED TO ATL. EMERGENCY DECLARED BY TOWER. FLTS 4603, 4639 CX.

Part: PANEL — MISSING (RT NACELLE) · airframe 13,539 hrs · 10,797 cycles

ON POST FLIGHT INSPECTION FOUND THE RIGHT HAND UPPER FIXED COWL MISSING.

Part: DOUBLER — UNKNOWN (BS 640) · airframe 13,519 hrs · 10,776 cycles

LEFT FS 640 DOUBLER SUSPECT CRACKED, REF EO600-53-69 0002.

Part: DOUBLER — UNKNOWN (BS 640) · airframe 13,519 hrs · 10,776 cycles

RIGHT FS 640 DOUBLER SUSPECT CRACKED, REF EO600-53-69 0002. REPAIRED IAW ASA EO 600-53-81 REP

Part: LIGHT — BROKEN (CABIN) · airframe 13,462 hrs · 10,719 cycles

EMERGENCY FLOOR LIGHTING AT ROW 5D BROKEN IN PIECES. FLT 4284 DEL 330 MINS.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 13,408 hrs · 10,669 cycles

ASD EMERGENCY EXIT SIGN HAS BULBS INOP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,248 hrs · 10,540 cycles

MID CEILING EMERGENCY LIGHT INOP.

Part: STRUCTURE — CRACKED (AIRSTAIRS) · airframe 12,476 hrs · 9,906 cycles

SD POSSIBLE CRACK UNDER TOP AFT STEP.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 12,296 hrs · 9,768 cycles

FOS COCKPIT FLASHLIGHT INOP.

Part: STEP — BROKEN (DOOR)

DURING A GROUND INSPECTION, THE PASSENGER DOOR BOTTOM STEP SUPPORT WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR BOTTOM STEP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: LAMP — BURNED OUT (GALLEY)

DURING A GROUND INSPECTION,, THE EMERGENCY EXIT LIGHT AT THE SERVICE DOOR WAS FOUND WITH BULBS BURNED OUT. MAINTENANCE REMOVED AND REPLACED THE LAMPS IN THE EMERGENCY EXIT LIGHT AT THE SERVICE DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: LAMP — BURNED OUT (CABIN)

DURING A GROUND INSPECTION, THE EMERGENCY EXIT SIGN, NEAR THE FORWARD CLOSET, WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE EMERGENCY EXIT SIGN, NEAR THE FWD CLOSET. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: FLASHLIGHT — BURNED OUT (COCKPIT)

DURING A GROUND INSPECTION, THE CAPTAIN`S COCKPIT FLASHLIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE CAPTAIN`S COCKPIT FLASHLIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: CLIP — CRACKED (FUSELAGE)

DURING C-CHECK, THE LT FS 280 CLIP WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LT FS 280 CLIP IAW SRM. (K)

Part: STEP — SEPARATED (PAX DOOR)

DURING A GROUND INSPECTION IN FLO, THE ACTUATOR ROD WAS FOUND TO BE SEPARATED FROM THE BOTTOM STEP ON THE PASSENGER DOOR. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR AND RECONNECTED THE ACTUATOR ROD TO THE BOTTOM STEP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: STEP — CRACKED (PAX DOOR)

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

Part: OIL SYSTEM — LOW (RT ENGINE)

FLT 4151 - DURING CRUISE FROM FPO-ATL, WHILE IN HOLDING PATTERN OVER ATL, CREW OBSERVED THE RT ENG OIL PRESS FLUCTUATING FROM APPROX 37 TO 50 PSI. THE CREW WAS INSTRUCTED TO DIVERT TO BHM AND THEN THEY RECEIVED A 'RT ENGINE OIL PRESSURE' MESSAGE ACCOMP BY A RED TRIPLE CHIME. THE CREW BROUGHT THE RT THRUST LEVER TO IDLE. THE QRH WAS C/W AND AN EMERGENCY WAS DECLARED. THE OIL PRESSURE VARIED FROM 30 TO 40 PSI DURING THE REMAINDER OF THE FLT WITH THE A/C LANDING SAFELY IN BHM. MX SERVICED THE RT ENG WITH THREE AND ONE-HALF QTS OF OIL AND ALSO INSP THE RT ENG OIL SYS CHIP DETECTOR, OIL FILTERS AND PERFORMED ENG RUNS FOR THIRTY MINUTES. NO DEFECTS WERE NOTED. OPS CHECKS GOOD. A/C OK FOR SERVICE. (M)

Part: BPSU — MALFUNCTIONED (T/E FLAP)

DURING CRUISE, AT APPROXIMATELY 25,000 FEET THE CREW RECEIVED A FLAP FAIL MESSAGE WITH THE FLIGHT CONTROL PAGE SHOWING BOTH THE LT AND RT FLAPS AT ZERO DEGREES. THE QRH WAS COMPLIED WITH, AND EMERGENCY DECLARED AND THE AIRCRAFT RETURNED TO DEPARTURE, LANDING SAFELY. MAINTENANCE REMOVED AND REPLACED THE LT BRAKE AND POSITION SENSOR UNIT (BPSU) AND ALSO THE FLAP ELECTRONIC CONTROL UNIT (FECU). OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: CLIP — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE RIGHT SIDE CLIP AT FS 484, RBL 27 AND 36 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE RIGHT SIDE CLIP AT FS 484, RBL 27 AND 36 IAW ASA EO 600-53-0098. (M)

Part: CLIP — CRACKED (FUSELAGE)

DUIRNG A C-CHECK IN MCN, THE CARGO COMPARTMENT LEFT AND RIGHT OUTBOARD CLIPS AT FS 280 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CARGO COMPARTMENT LEFT AND RIGHT OUTBOARD CLIPS AT FS 280 IAW SRM 51-42-21. (M)

Part: SUPPORT BEAM — CRACKED (LT ENGINE)

DURING A C-CHECK IN MCN, THE LEFT LOWER ENGINE SUPPORT BEAM PANEL AT BL 36.20 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE LEFT LOWER ENGINE SUPPORT BEAM PANEL AT BL 36.20 IAW ASA EO 600-53-0070. (M)

Part: PLATE — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE CARGO COMPARMTENT DOOR FLOOR LANDING PLATE AT THE RIVET, FS 589 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE CARGO COMPARTMENT DOOR FLOOR LANDING PLATED AT FS 589 IAW ASA EO 600-53-0117. (M)

Part: MOUNT — CRACKED (PAX DOOR)

DURING A C-CHECK IN MCN, THE AFT ANCHOR MOUNT ON THE PASSENGER DOOR WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE AFT ANCHOR MOUNT ON THE PASSENGER DOOR. (M)

Part: CLIP — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE LT AND RT AFT PRESSURE WALL SIDE CLIPS AT FS 625 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE LT AND RT AFT PRESSURE WALL SIDE CLIPS AT FS 625. (M)

Part: FLOOR SUPPORT — CRACKED (CARGO BAY)

DURING A C-CHECK IN MCN, THE CARGO COMPARTMENT FLOOR SUPPORT ANGLES AT FS 621 ON THE LEFT AND RIGHT SIDES WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE CARGO COMPARTMENT FLOOR SUPPORT ANGLES AT FS 621 ON THE LEFT AND RIGHT SIDES IAW ASA EO 600-53-0105. (M0

Part: FRAME — CRACKED (FUSELAGE)

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

Part: STEP — BROKEN (PAX DOOR)

DURING HANGAR MAINTENANCE IN MCN, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND BROKEN AT THE ATTACH LINK. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. (M)

Part: FITTING — CRACKED (PAX DOOR)

DURING AN A-CHECK IN MCN, THE PASSENGER DOOR FORWARD ANCHOR FITTING WAS FOUND CRACKED. MAINTENANCE REMVOED AND REPLACED THE PASSENGER DOOR FORWARD ANCHOR FITTING. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: CABLE — WORN (PAX DOOR)

DURING A GROUND INSPECTION, THE FLIGHT ATTENDANT REPORTED THAT THREE ATTEMPTS WERE MADE BEFORE THE MAIN PASSENGER DOOR WOULD OPEN. MAINTENANCE REMOVED AND REPLACED THE MAIN PASSENGER DOOR WHEEL CABLE ON THE LT SIDE. OPERATIONAL CHECKS GOOD. AIRCRAFT, OK FOR SERVICE.

Part: WINDOW — CRACKED (COCKPIT)

DURING DESCENT INTO DFW AT APPROXIMATELY 11,000 FEET, THE F/O'S SIDE WINDOW, OUTER PANE CRACKED. THE AIRCRAFT LANDED SAFELY IN DFW. MAINTENANCE REMOVED AND REPLACED THE F/O'S SIDE WINDOW. OPERATIONAL AND LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: BULB — BURNED OUT (EXTERIOR)

DURING GROUND INSPECTION, THE RT EXTERIOR EMERGENCY LIGHT OVER THE WING WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE RIGHT EXTERIOR EMERGENCY LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE.

Part: BEARING — SEIZED (LT MLG)

POST FLIGHT INSP, CREW REPORTED, LT OUTBOARD TIRE ASSEMBLY MISSING. THE LANDING INTO HPN WAS SMOOTH WITH NO VIBRATIONS. THE ASSEMBLY WAS RECOVERED ON ATL AIRPORT PROPERTY. MAINTENANCE R&R THE MLG AXLE ASSEMBLY, LT OUTBOARD BRAKE ASSEMBLY, AND THE LT INBOARD AND OUTBOARD WHEEL ASSEMBLIES. PERFORMED A GEAR SWING AND INSP THE LT MLG PIVOT POINTS. NO DEFECTS NOTED. BASED ON THE TEAR DOWN ANALYSIS, IT WAS CONCLUDED THE POSSIBLE CAUSE WAS DUE TO A SECOND INNER BEARING SEAL BEING TRAPPED BETWEEN THE WHEEL AND THE AXLE SPACER. THE INNER FACE OF THE METAL PORTION HAD IMPRESSIONS AND SURFACE DEFORMATIONS THAT SUGGEST CONTACT BETWEEN THE SEAT AND THE BRAKE ATTACHMENT BOLTS. (M)