N857AS

Part: SKIN — DENTED (BS 250) · 34,970 cycles

FUSELAGE SKIN HAS A DENT JUST FWD OF BS 250 BETWEEN STRINGERS 23 AND 24L. REPAIRED IAW REO.

Part: SKIN — DAMAGED (NLG DOOR) · 34,970 cycles

AFT NLG DOOR HAS A LARGE CREASE RUNNING ACROSS ENTIRE LENGTH OF OUTER SKIN. REPAIRED THE NLG DOOR IAW SRM.

Part: BULKHEAD — CRACKED (BS 621) · 34,970 cycles

REAR PRESSURE BULKHEAD WEB CRACKED. REPAIRED IAW REO.

Part: FLOOR SUPPORT — CORRODED (BS 439-499) · 34,970 cycles

RIGHT FLOOR SUPPORT CORRODED, RBL 9, BS 439 TO 499. REPAIRED IAW REO.

Part: FLOOR SUPPORT — CORRODED · 34,970 cycles

FLOOR SUPPORT IS CORRODED, LBL 9, BS 461 TO 473.15. REPAIRED THE FLOOR SUPPORT IAW REO.

Part: FRAME — CORRODED (BS 349) · 34,970 cycles

BS 349 FRAME FWD SIDE IS CORRODED BETWEEN STRINGERS 26 AND 27L. BLENDED IAW SRM.

Part: SKIN — DENTED (BS 654-672) · 34,970 cycles

FUSELAGE SKIN DENTED BETWEEN BS 654.5 AND 672.2, STRINGERS 20L AND 21L. REPAIRED IAW REO.

Part: SKIN — DENTED (BS 605-621) · 34,970 cycles

FUSELAGE SKIN HAS TWO DENTS BETWEEN BS 605 AND 621, STRINGERS 19L AND 20L. REPAIRED THE SKIN IAW REO.

Part: SKIN — DENTED (BS 682-700) · 34,970 cycles

FUSELAGE SKIN HAD ONE PROTRUDING DENT BETWEEN BS 682 AND 700, STRINGER 23L AND 22L. REPAIRED IAW REO.

Part: SKIN — DENTED (RT WING TE FLAP) · 34,970 cycles

RIGHT FLAP LOWER SKIN DENTED. REPAIRED IAW REO.

Part: FLAP — DAMAGED (LEFT WING) · 34,970 cycles

DAMAGE ON THE LT OTBD FLAP AT. REPAIR IAW REO.

Part: SKIN — CHAFED (BS 349) · 34,970 cycles

FUSELAGE SKIN, PREVIOUS REPAIR AT BS 349 IS CHAFED AT STRINGER 16L. REPAIRED THE SKIN IAW REO.

Part: SKIN — DENTED (RT WING TE FLAP) · 34,970 cycles

RIGHT FLAP LOWER SKIN DENTED. REPAIRED IAW SRM.

Part: FLOOR SUPPORT — CORRODED (BS 409) · 34,970 cycles

FLOOR SUPPORT CORRODED. REMOVED AND REPLACED THE FLOOR SUPPORT, BS 409+5 TO 409+118 IAW REO.

Part: SKIN — CHAFED (BS 310) · 34,970 cycles

FUSELAGE SKIN AT BS 310 IS CHAFED AT STRINGER 16L. REPAIRED IAW REO.

Part: SKIN — BURNED (BS 333-349) · airframe 35,480 hrs · 32,634 cycles

ONE BURN BETWEEN BS 333 AND 349 BETWEEN STRINGERS 25 - 26L. DRILLED THROUGH SKIN BAY TO REMOVE LIGHTNING BURN IAW EC/TC REO 601R-53-00-115 REV H. FABRICATED INTERNAL REPAIR WASHER. CONTROLLED COUNTERSINK AND INSTALLED NAS1097AD5 SOLID RIVET AND RESTORED FINISH IAW EC/TC REO 601R-53-00-115 REV H SECTION 1/B (B3).

Part: SKIN — BURNED (E/E DOOR) · airframe 35,480 hrs · 32,634 cycles

MULTIPLE BURN MARKS ON AFT EQUIPMENT BAY DOOR AT FWD EDGE LT SIDE. FOUND TO BE OUT OF LIMITS IAW EC/TC REO 601R-53-00-115 REV H. COMPLIED WITH DISPOSITION EA 25-2016-199 , SECTION 1 PERMANENT REPAIR , ITEMS 5-9.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 34,825 hrs · 31,933 cycles

FLOOD LIGHT ON AFT SIDE OF WARDROBE INOPERATIVE, VARIOUS EMERGENCY EXIT LIGHTS ARE INOPERATIVE, AND VARIOUS CEILING PANELS ARE INOPERATIVE. REPAIRED BROKEN WIRE SPLICE CONNECTORS 3 EA ON WARDROBE FLOOD LIGHT EXIT LIGHTS AND CEILING EXIT LIGHTS IAW ESPM 20-17-31 ALL OPS TESTS GOOD.

Part: BRACKET — CRACKED (BS 484) · airframe 34,825 hrs · 31,933 cycles

CRACKED FOUND ON BOTH INBD, OTBD BRACKET ON CABLE INTRCOSTAL AT FS 484.00 AND BETWEEN LBL 27 AND 36. R & R ANGLE ON INBD CABLE INTERCOSTAL IAW SRM 51-40-11 AND 51-42-20. RECEIVED AND COMPLIED WITH REO 601R-53-41-2011 AND ECTC REO 601R-53-41-2011. COMPLIED WITH REO 601R-53-41-059, REV B, DATE SEP16,2009 NOTE 13 IAW NDTM PART 1, 51-20-06. FABRCIATED 1 ANGLE HAS CRACK INDICATTION SIGNAL EXCEEDS 50 PERCENT FS4 FROM REFERENCE NOTY SIGNAL. COMPLIED WITH REO 601R-53-41-0596 REV B, DATED SEP.16,2009, NOTE 13 IAW NDTM PART 1, 51-20-06 ON FABRICATED -1 ANGLE NO INIDCATIONS NOTED AT THIS TIME.

Part: BRACKET — CRACKED (BS 484) · airframe 34,825 hrs · 31,933 cycles

CRACK FOUND ON OTBD BRACKET ON CABLE INTERCOSTAL AT FS 484.00 + LBL27. R & R THE BRACKET IAW SRM 51-40-11 AND 51-42-20.

Part: FLOOR SUPPORT — CORRODED (BS 409) · airframe 34,825 hrs · 31,933 cycles

CORROSION AROUND NUTPLATE HOLE ON RBL 9 BS 409+48 AND +64. REPAIRED FLOOR SUPPORT IAW SRM 53-00-43.

Part: FITTING — CRACKED (WINDSHIELD) · airframe 34,825 hrs · 31,933 cycles

LT AND RT WINDSHIELD CENTER POST LOWER FITTINGS CRACKED. R & R LT AND RT WINDSHIELD CENTER POST LOWER FITTINGS IAW SRM TASK 51-40-11 AND 51-42-21.

Part: FRAME — CRACKED (BS 333) · airframe 34,825 hrs · 31,933 cycles

CRACK ON FRAME AT FS 333 BETWEEN STR 0 - STR 1R. R & R FRAME AT BS 333 BETWEEN STRINGER 5R IAW SRM 51-42-06 AND DWG 601R 32004-5.

Part: FLOORBEAM — CORRODED (BS 621) · airframe 34,825 hrs · 31,933 cycles

CORROSION FOUND ON FS 621 FLOORBEAM BETWEEN RBL 40-27. REMOVED CORROSION DAMAGE IAW SRM 51-21-06 ON PREVIOUS REPAIR FOUND DAMAGE TO BE OUT OF LIMITS IAW SRM 53-00-00.

Part: SEAT TRACK — CORRODED (BS 409-559) · airframe 34,825 hrs · 31,933 cycles

SEAT TRACK RBL 9 BS 409+128 - 559+16 FOUND CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11-000-802, AND, 53-01-11-400-802, AND GREO 601R-53-00-485, REV A.

Part: SEAT TRACK — CORRODED (BS 364-409) · airframe 34,825 hrs · 31,933 cycles

LEFT SEAT TRACK AT BS 364-409, LBL 9, HAS CORROSION. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-1-11-00, AMM 53-01-11-400-802, AND REO 601R-53-00-485.

Part: FLOORBEAM — CORRODED (NOT REPORTED) · airframe 34,825 hrs · 31,933 cycles

CORROSION FOUND ON FLOORBEAM AROUND SCREW HOLE. BLENDED AND REMOVED CORROISON IAW SRM 51-21-06-00. BLENDED AREA IS OUT OF ALLOWABLE LIMITS IAW REO 601R-5-53-00-005.

Part: SEAT TRACK — CORRODED (BS 364-409) · airframe 34,825 hrs · 31,933 cycles

RIGHT SIDE SEAT TRACK AT BS 364 - 409+16 HAS CORROSION. FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11-04, AMM 53-01-11-400-802, AND REO 601R-53-00-055 REV B.

Part: SEAT TRACK — CORRODED (BS 409) · airframe 34,825 hrs · 31,933 cycles

LEFT SIDE SEAT TRACK AT BS 409+112, AND +128 HAS CORROSION. FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11-000-802, AMM 53-01-11-400-802, AND REO 601R-53-00-055, REV B.

Part: SEAT TRACK — CORRODED (BS 364-409) · airframe 34,825 hrs · 31,933 cycles

LT SIDE SEAT TRACK BS 364 - 409+16 HAS CORROSION. FOUND TO BE OUT OF LIMITS, REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11-000-802, AMM 53-01-11-400-802, REO 601R-53-00-055 AND REO 601R-53-00-055. REV B.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 34,825 hrs · 31,933 cycles

SEAT TRACK CORRODED AT BS 559 - 559+80 LBL 9. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11-000-802, AMM 53-01-11-400-802, AND REO 601R-53-00-485.

Part: FLOOR SUPPORT — CORRODED (BS 409) · airframe 34,825 hrs · 31,933 cycles

CORROSION AROUND NUTPLATE HOLES ON FLOOR SUPPORT RBL9, F/S 409.80+32-409.00+48. REMOVED THE CORROSION IAW SRM 51-21-06 AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00. REPAIRED THE FLOOR SUPPORT IAW SRM 53-00-43.

Part: SEAT TRACK — CORRODED (BS 364-409) · airframe 34,825 hrs · 31,933 cycles

RT SEAT TRACK AT BS 364 - 409 HAS CORROSION RBL 9. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11-000-802 AND AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 409-559) · airframe 34,825 hrs · 31,933 cycles

SEAT TRACK LBL 9 F/S 409+128 - 559+16 HAS CORROSION. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11-000-802, AMM 53-01-11-400-802, AND REO 601R-53-00-485.

Part: CARGO TRACK — CORRODED (BS 559) · airframe 34,825 hrs · 31,933 cycles

CARGO TRACK CORRODED AT BS 559+96-87. REMOVED AND REPLACED THE CARGO TRACK IAW AMM 53-01-11-000-802, AMM 53-00-49-400-801, AND REO 601R-53-00-485.

Part: CARGO TRACK — CORRODED (BS 559) · airframe 34,825 hrs · 31,933 cycles

CARGO TRACK CORRODED AT BS 559+69 LBL 27. REMOVED AND REPLACED THE CARGO TRACK IAW AMM 53-00-49-000-802, AMM 53-00-49-400-802, AND REO 601R-53-00-485.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 34,825 hrs · 31,933 cycles

SEAT TRACK CORRODED AT BS 559 -559+80, RBL 9. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11-000-802, AMM 53-01-11-400-802, AND REO 601R-53-00-485.

Part: SEAT TRACK — CORRODED (BS 409) · airframe 34,825 hrs · 31,933 cycles

RT SIDE SEAT TRACK AT BS 409+16, AND +112 HAS CORROSION. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-14-11-000-802, AMM 53-00-49-400-801, AND REO 601R-53-00-485.

Part: SEAT TRACK — CORRODED (BS 409) · airframe 34,825 hrs · 31,933 cycles

LEFT SIDE SEAT TRACK AT BS 409+16, AND +112 HAS CORROSION. FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11-000-802, AMM 53-01-11-400-802, REO 601R-53-00-055 AND REO 601R-53-00-055, REV B.

Part: CARGO TRACK — CORRODED (BS 559) · airframe 34,825 hrs · 31,933 cycles

CARGO TRACK CORRODED AT BS 559 - 559+96, LBL 9. REMOVED AND REPLACED THE CARGO TRACK IAW AMM 53-00-49-000-801, AMM 53-00-49-400-801, AND REO 601R-53-00-485.

Part: SEAT TRACK — CORRODED (BS 409) · airframe 34,825 hrs · 31,933 cycles

RT SIDE SEAT TRACK AT BS 409+112 AND +128 HAS CORROSION. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11-400-802.

Part: SKIN — DAMAGED (NOT REPORTED) · airframe 34,473 hrs · 31,540 cycles

AFT FUSELAGE SKIN DAMAGE CAUSED BY THE AFT LOWER DOOR LATCH PIN. COMPLIED WITH EC/TC REO 601R-53-21-186. THIS IS CONSIDERED A PERMANENT PEPAIR. THIS IS CONSIDERED A MAJOR REPAIR IAW GMM 5-3.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 33,612 hrs · 30,659 cycles

RT EXTERNAL EMERGENCY LIGHT, IS INOPERATIVE. R & R EMERGENCY LIGHT BULB IAW AMM 33-51-21. OP'S CHECKED GOOD.

Part: RIVET — MISINSTALLED · airframe 32,960 hrs · 29,978 cycles

UPON INSPECTION OF INSTALLED RIVETS ON PRESSURE BULKHEAD REPAIR AT LBL18. FOUND MULTIPLE BUCKTAILS OUT OF LIMITS IAW SRM 51-42-06, FIG 8 AND 9. REPAIR IS BEING CONDUCTED IAW REO 601R-53-61-1285. REPLACED, DISCREPEANT RIVETS IAW SRM 51-42-06, AND REO 601R-53-61-1285, REV D. THIS IS CONSIDERED A MAJOR REPAIR IAW GMM 5-3, RII COMPLIED WITH IAW GMM 3-3.

Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 32,960 hrs · 29,978 cycles

WHILE PERFORMING EC/TC AWL 53-61-153-02, ECI OF THE AFT PRESSURE BULKHEAD, FOUND 3 SEPARATE LOCATIONS ON THE BULKHEAD WEB WITH CRACK INDICATIONS AT LBL 18.00 AT ZEE MEMBER HEEL LINE ADJACENT TO THE FASTENERS ON THE OTBD SIDE. THESE INDICATIONS EXCEED LIMITATIONS IAW NDTM PART 6, 53-61-153. CRACKS ARE ORIENTATED VERTICAL AND LOCATIONS AND LENGTH ARE MARKED ON THE BULKHEAD WEB.

Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 32,960 hrs · 29,978 cycles

WHILE PERFORMING EC/TC AWL 53-61-153-02, ECI OF THE AFT PRESSURE BULKHEAD, FOUND CRACK INDICATION ON THE BULKHEAD WEB AT LBL 36.20 AT ZEE MEMBER HEEL LINE ADJACENT TO THE FASTENERS ON THE OTBD SIDE. THIS INDICATION EXCEEDS LIMITATIONS IAW NDTM PART 6, 53-61-153. CRACK IS ORIENTATED VERTICAL AND LOCATION AND LENGTH IS MARKED ON THE BULKHEAD WEB.

Part: COVER — BROKEN (EMERGENCY LIGHT) · airframe 32,936 hrs · 29,952 cycles

EMERGENCY EXIT LIGHT COVER ON MAIN PASSENGER DOOR SIDEWALL IS BROKEN. REPLACED FLOOR EMERGENCY FLOOD LIGHT BASE, REF AMM 33-51-19.

Part: SHEAR PIN — BROKEN (ELEVATOR PCU) · airframe 32,890 hrs · 29,902 cycles

ON TAKEOFF, IT TOOK A NOTICABLE AMOUNT OF BACK PRESSURE TO LIFT ACFT OFF RUNWAY. TRIM WAS SET TO 7.0. FLT CONTINUED WITH AUTOPILOT WITH NOTHING NOTICEABLE UNTIL LANDING. WHEN DISCONNECTING A/P AT 500', TRIM 7.2 IN THE FLARE AT 100', ELEVATOR CONTROL WAS LOST. WAS UNABLE TO FLY ACFT TO RUNWAY. R & R ELEVATOR PCU SHEAR PINS IAW SB 601R-55-008. OPS CHECK GOOD, NO FURTHER DEFECTS NOTED AT THIS TIME. ACFT RETURNED TO SERVICE.

Part: SUPPORT BEAM — CRACKED (CARGO DOORWAY) · airframe 32,129 hrs · 29,117 cycles

CARGO DOOR SUPPORT BEAM MEMBER ANGLE CRACKED ON AFT SIDE ATTACHMENT TO FS 621 BULKHEAD. REMOVED CRACKED ANGLE AND INSTALLED NEW IAW SRM 51-42-21.

Part: ISOLATOR — CRACKED (BS 621 BULKHEAD) · airframe 32,129 hrs · 29,117 cycles

FS 621, BULKHEAD ISOLATOR BROKEN. R & R ISOLATOR WITH NEW IAW SRM 51-42-06.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT) · airframe 31,148 hrs · 28,167 cycles

SERVICE DOOR INTERIOR EMERGENCY FLOOD LIGHT INOPERATIVE. RECONNECTED EMERGENCY LIGHT CONNECTOR IAW AMM 33-51-19, OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 31,043 hrs · 28,058 cycles

FORWARD MOST INTERIOR AND EXTERIOR EMERGENCY LIGHTS WILL NOT STAY ILLUMINATED. R & R NR 1 EMERGENCY BATTERY PACK IAW AMM 33-51-04. OPS CHECKED GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 30,910 hrs · 27,929 cycles

EXTERIOR SERVICE DOOR EXIT LIGHT IS INOPERATIVE. R & R LAMP IAW AMM 33-51-21-000-801/400-80. OPS CHECKED GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 30,910 hrs · 27,929 cycles

PAX DOOR EXIT EMERGENCY LIGHT INOPERATIVE. R & R LAMP IAW AMM 33-51-21-000-801/400-80. OPS CHECKED GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 30,910 hrs · 27,929 cycles

FIRST CENTER AISLE EMERGENCY LIGHT IS INOPERATIVE. R & R LAMPS IAW AMM 33-51-16-000-801 AND 33-51-16-400-801. OP CHECKED GOOD.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT) · airframe 30,910 hrs · 27,929 cycles

LEFT OVERWING EXIT SURROUND EMERGENCY LIGHTS INOPERATIVE. CONNECTED P26LY & J27LY TO J26LY & P27LY AND P34LY & J35LY TO J34LY & P35LY. OPS CHECKED EMERGENCY LIGHTS IAW AMM 35-51-00-710-801. OPS CHECKED GOOD.

Part: WEB — CORRODED (BS 574-589) · airframe 30,910 hrs · 27,929 cycles

FOUND WEB CORRODED BS 574 - 589 LBL 27. REMOVED WEB IAW SRM 51-42-06. LOCATED AND DRILLED NEW WEB IAW SRM 51-40-11. INSTALLED WEB IAW SRM 51-42-06.

Part: ANGLE — CORRODED (BS 280 BULKHEAD) · airframe 30,910 hrs · 27,929 cycles

AT FS 280.00 BULKHEAD TOP OF AFT REPAIR ANGLE IS CORRODED BETWEEN LBL9 AND RBL, PLUS BOTH INBD AND OTBD CLIPS ON LBL9 AT 280 ARE CRACKED, AND INBD AND OTBD CLIPS ON RBL9 AT 280 ARE CRACKED, REPLACE PARTS IAW REO 601R-53-11-9261. REMOVED 4 EA CRACKED CLIPS (SHIMS) AT LBL AND RBL 9 IAW SRM 51-42-06. REMOVED THE AFT REPAIR ANGLE AND RT SPLICE IAW SRM 51-42-06 LOCATED AND DRILLED AMD CUTOUT SECTION OF THE AFT REPAIR ANGLE IAW REO 601R-53-11-926. INSTALLED AFT REPAIR ANGLE IAW SRM 51-42-06 AND REO 601R-53-11-926.

Part: FLOOR SUPPORT — CORRODED (BS 559-621) · airframe 30,910 hrs · 27,929 cycles

FLOOR SUPPORT BS 559+112 - 621 LBL 27 CORRODED. COMPLIED WITH EC/TC REO 601R-53-61-3778 AND GREO 601R-53-61-3778, REV A. MAJOR REPAIR.

Part: FLOOR SUPPORT — CORRODED (BS 280 BULKHEAD) · airframe 30,910 hrs · 27,929 cycles

AT FS 280.00 BULKHEAD FWD FLOOR SUPPORT ANGLE IS BADLY CORRODED. REPLACED FWD FLOOR ANGLE AT FS 280.00 BULKHEAD IAW SRM 51-42-06. REMOVED FWD FLOOR SUPPORT ANGLE AT F/S 280.00 IAW SRM 51-42-06-00 AND 51-42-00. LOCATED AND DRILLED NEW FLOOR ANGLE, FWD, IAW CRJ200 51-40-11. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702.

Part: FLOORBEAM — CORRODED (BS 484) · airframe 30,910 hrs · 27,929 cycles

PRESSURE FLOORBEAM AT LBL 45 AND FS 484 HAS CORROSION. COMPLIED WITH EC/TC REO 601R-53-41-666 01 AND REO 601R-53-41-666, REV C. MAJOR REPAIR.

Part: FLOOR SUPPORT — CORRODED (BS 589) · airframe 30,910 hrs · 27,929 cycles

FLOOR SUPPORT BS 589 CORRODED. REMOVED IAW SRM 51-42-06-00 AND 51-42-21-00. LOCATED & DRILLED NEW SERVICEABLE FLOOR SUPPORT IAW SRM 51-40-11-00 AND INSTALLED IAW SRM 51-42-06-00 AND 51-42-21-00.

Part: FLOORBEAM — CORRODED · airframe 30,910 hrs · 27,929 cycles

FLOOR PANEL 281JLF HAS ONE FLOORBEAM CAP CORRODED. REMOVED FASTENERS IAW SRM 51-42-06-00 ALSO 51-42-21-00. LOCATED AND STARTED DRILLING NEW SERVICEABLE FLOORBEAM CAP IAW SRM 51-40-11-00 AND IAW SRM 51-40-11-00. MAJOR REPAIR.

Part: FLOOR SUPPORT — CORRODED (BS 513) · airframe 30,910 hrs · 27,929 cycles

PRESSURE FLOOR SUPPORT AT LBL 45 AND BS 513. HAS CORROSION. COMPLIED WITH EC/TC REO 601R-53-41-666 01 AND REO 601R-53-41-666, REV C. MAJOR REPAIR.

Part: FLOOR SUPPORT — CORRODED (BS 449) · airframe 30,910 hrs · 27,929 cycles

PRESSURE FLOOR SUPPORT AT LBL45 AND BS 449. HAS CORROSION. COMPLIED WITH EC/TC REO 601R-53-41-666 01 AND REO 601R-53-41-666, REV C. MAJOR REPAIR.

Part: WINDOW FRAME — CRACKED (COCKPIT) · airframe 30,910 hrs · 27,929 cycles

FLIGHT DECK RT WINDSHELD SIDE POST. SUPPORT CRACKED. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702. REMOVED RT WINDSHIELD SIDE POST SUPPORT ANGLE IAW SRM 51-42-06. INSTALLED SERVICABLE RT SIDE POST LOWER SUPPORT ANGLE AND RESTORED FINISH IAW EO 601R34032, SNIEO S01 AND DWG 601R34032, DWG 01R33010. RECEIVED EO, DWG NR 601R34032 PRELIMINARY 5XXP1 TO FABRICATE RT WINDSHIELD SIDE POST SUPPORT 5NIEO S01. FABRICATED SUPPORT ANGLE AND HEAT TREATED TO T62, TEMPER IAW EO DWG NR 601R34032 PRELIMINARY 5XXP1, SNIEO S01.

Part: CARGO TRACK — CORRODED (AFT CARGO BAY) · airframe 30,910 hrs · 27,929 cycles

CARGO TRACK CORRODED IN AFT CARGO BAY LBL 9 BS 621. R & R CARGO TRACK IAW AMM 53-01-11-000-802 AND 53-01-11-400-802.

Part: STRUCTURE — CHAFED (CARGO DOOR) · airframe 30,910 hrs · 27,929 cycles

CARGO DOOR HAS CHAFE DAMAGE AT TOP CENTER. COMPLIED WITH REO 601R-52-31-198 AND EC/TC REO 601R-52-31-198. MAJOR REPAIR.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 30,562 hrs · 27,560 cycles

RT SIDE EMERGENCY LIGHT LENS COVER LOOSE. R & R RT SIDE FWD EMERGENCY EXTERNAL LIGHT LENS IAW AMM 33-51-21. OPS CHECKED GOOD, NO DEFECTS NOTED.

Part: PIN — MISSING (PAX DOOR) · airframe 29,846 hrs · 26,851 cycles

DOOR HANDLE OF FWD PAX DOOR WILL NOT OPEN. UPON FURTHER INSPECTION FOUND PRESSURE RELIEF VALVE FOR PAX DOOR HAD PINS MISSING ON ROTATING SHAFT. REPLACED MISSING PINS IAW AMM CH 52-11-15. OPS CHECKED DOOR IAW AMM CH 52-11-15-710-801. OPS CHECK GOOD, NO DEFECTS NOTED. ACFT OK FOR SERVICE.

Part: APU — ODOR · airframe 29,401 hrs · 26,361 cycles

FUEL ODOR IN FLT. OPS CHECK PACK IAW AMM 21-00-00. OPS CHECKED GOOD CLEAN OLD FUEL OF APU CLOSER 49-10-00.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 28,820 hrs · 25,761 cycles

EMERGENCY LIGHTS INOPERATIVE IN ON POSITION ON OVERHEAD PANEL AND F/A PANEL. R & R TWO BATTERY PACKS IAW AMM 33-51-04, IPC REF 33-51-04, ITEM 77 AND 137.

Part: DOOR — BINDING (MAIN PAX) · airframe 27,704 hrs · 24,611 cycles

F/A UNABLE TO OPEN PAX DOOR. RAMPER, AFTER WORKING WITH HANDLE GOT DOOR OPEN. PERFORMED OPS CHECK OF PAX DOOR IAW AMM 52-11-00. OPS CHECKED GOOD. ACFT OK FOR SERVICE.

Part: SENSING ELEMENT — OUT OF POSITION (MLG WW) · airframe 27,551 hrs · 24,457 cycles

LEFT ANTI ICE DUCT WARNING ON CLIMBOUT, QRH COMPLIED WITH. MESSAGE PERSISTED FOR ADDITIONAL 5+ MINUTES BEFORE SELF EXTINGUISHING ON SHORT FINAL. RETURNED TO DEPARTURE, EMERGENCY DECLARED. FOUND SENSING ELEMENT TOUCHING DUCTING IN LT MLG WW AREA. REPOSITION SENSING ELEMENT. PERFORM DUCT MON TEST, AND RAN BOTH ENGINES WITH 14TH STAGE BLEED AIR. OPS CHECK GOOD IAW AMM 36-21-00. (SDR CLOSED)

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT) · airframe 27,191 hrs · 24,050 cycles

EXTERIOR EMERGENCY LIGHT, AFT OF SERVICE DOOR INOPERATIVE. FOUND CONNECTOR TO BE LOOSE, TIGHTENED CONNECTOR TP162032. AW AMM 25-26-01-400-801 OPS TESTED GOOD. (SDR CLOSED)

Part: HANDLE — CRACKED (CARGO DOOR) · airframe 27,191 hrs · 24,050 cycles

CARGO DOOR SKIN CRACKED AT HANDLE CUTOUT. PERFORMED EDDY CURRENT INSPECTION OF CARGO DOOR HANDLE HOUSING IAW MAC NDT PROCEDURE ET-2 EA. END OF HANDLE HSG IS VERIFIED CRACKED. R & R CARGO DOOR HANDLE HOUSING IAW SRM 51-42-21-00. INSTALLED OUTER HANDLE ASSY IN NEW CARGO DOOR HANDLE HOUSING IAW CMM 52-31-03. PERFORMED PRESSURE CHECK IAW AMM 21-32-00-863-801, NO LEAKS NOTED.

Part: WIRE — DISCONNECTED (EMERGENCY LIGHT) · airframe 27,185 hrs · 24,042 cycles

RIGHT EMERGENCY LIGHT AT SERVICE DOOR INOPERATIVE. REMOVED EMERGENCY EXIT PANEL IAW AMM 25-31-01-000-802. CONNECTED EXIT LIGHT AND REINSTALLED PANEL IAW AMM 25-31-01-400-802. OPS TEST OF EMERGENCY LIGHTS WAS PERFORMED IAW AMM 33-51-00-710-804. OPS TESTED GOOD.

Part: DOUBLER — CORRODED (EMERGENCY EXIT) · airframe 27,185 hrs · 24,042 cycles

LEFT SIDE EMERGENCY EXIT INTERNAL DOUBLER CORRODED, LOCATED BEHIND HOOK FITTING MS162053. REPAIR CLASSIFIED AS MINOR.

Part: FRAME — CORRODED (BS 349) · airframe 27,185 hrs · 24,042 cycles

FRAME FS 349.00 CORRODED BETWEEN STR 26L AND 26R. REPAIRED IAW REO 601R-53-21-2276.

Part: FRAME — CORRODED (BS 319.7) · airframe 27,170 hrs · 24,024 cycles

FRAME 319.70 CORRODED BETWEEN STR 26L AND 36R. REPAIRED IAW REO 601R-53-21-2276.

Part: SILL — CORRODED (FUSLEAGE) · airframe 27,170 hrs · 24,024 cycles

DOOR SILL PLATE CORRODED.

Part: FRAME — CORRODED (BS 364) · airframe 27,170 hrs · 24,024 cycles

FRAME BS 364 HAS CORROSION BETWEEN STR 26L & 26R. REPAIRED IAW REO 601R-53-21-2276.

Part: CABLE — CORRODED (DOWNLOCK) · airframe 27,170 hrs · 24,024 cycles

LEFT EMERGENCY EXIT INTERNAL DOUBLER CORRODED. REMOVED RIVETS TO ROLL SKIN BACK IAW SRM 51-42-011-00. PERFORMED UT THICKNESS INSP IAW MAC NDT PROCEDURE UT-3 MIN MATERAIL REMAINING IS .039", ORIGINAL IS .040", MATERIAL REMOVED IS .001". CORROSION ON INTERIOR OF OUTER DOOR FRAME FLANGE (LOWER AFT) -61 SPLICE ANGLE FLANGE AND SEAL RETAINER. REMOVED CORROSION IAW SRM 51-21-06 FROM FRAME FLANGE .8" X.3" X .005" - .045" REMAINING FROM ANGLE FLANGE .5" X 1.3" X .003" - .047" REMAINING, FROM SEAL RETAINER .8" X 3" X .003" - .037" REMAINING MATERIAL. ALL BLENDS REQUIRE SUBMISSION TO RT ALL ARE BEYOND LIMITS OF SRM 52-00-00. DAMAGE IS ADJACENT TO FASTENER HOLES. RII FOUND TO BE SATISFACTORY. (SDR CLOSED)

Part: FLOORBEAM — CORRODED (BS 349) · airframe 27,170 hrs · 24,024 cycles

FLOORBEAM AT BS 349 CORRODED. REPAIRED IAW REO 601R-53-21-2273.

Part: FRAME — CORRODED (BS 333) · airframe 27,170 hrs · 24,024 cycles

FRAME BS 333.00 CORRODED BETWEEN STR 26L AND 26R. REPAIRED IAW REO 601R-53-21-2276.

Part: INTERCOSTAL — CORRODED (E/E BAY DOOR) · airframe 27,170 hrs · 24,024 cycles

LEFT & RT INBD FWD INTERCOSTALS FOR AVIONIC BAY DOOR FS 349 -364 CORRODED. REPAIRED IAW 601R-53-21-2276.

Part: SILL — CORRODED (BS 349) · airframe 27,170 hrs · 24,024 cycles

PAX DOOR SILL AFT CORNER AND FS 349.00 AND FLOOR SILL CORRODED. REPAIRED IAW REO 601R-53-21-2275.

Part: FLOORBEAM — CORRODED (BS 349) · airframe 27,170 hrs · 24,022 cycles

CABIN AREA, FLOORBEAM AT FS 349 CORRODED. REPAIRED IAW REO 601R-53-21-2273.

Part: SILL — CORRODED (FUSELAGE) · airframe 27,170 hrs · 24,022 cycles

DOOR SILL STRAP AND LOWER PAX DOOR CUT OUT CORRODED. BLENDED CORROSION ON DOOR SILL STRAP LOWER EDGE OF CUTOUT IAW SRM 51-21-06. PERFORMED UT THICKNESS INSPECTION OF BLEND AREA IAW MAC NDT PROCEDURE UT-3, MIN MATERIAL REMAINING IS .089" ORIGINAL IS .100" MATERIAL REMOVED IS .011". DAMAGE EXCEEDS ALLOWABLE DAMAGE LIMITS OF SRM 53-21-23. REPAIRED IAW REO 601R-53-21-2272. COMPLIED WITH NDTM PART 1, IAW 51-20-06. NO INDICATIONS NOTED.

Part: DOUBLER — CORRODED (EMERGENCY EXIT) · airframe 27,170 hrs · 24,022 cycles

LT EMERGENCY EXIT DOOR INTERNAL DOUBLER CORRODED. BLENDED CORROSION, PERFORMED NDT, NO CRACKS NOTED.

Part: SILL — CORRODED (PAX DOORWAY) · airframe 27,170 hrs · 24,022 cycles

PAX DOOR SILL PLATE CORRODED. INSTALLED NEW SILL PLATE IAW SRM 51-42-06 AND 51-42-21.

Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 27,170 hrs · 24,022 cycles

INTERCOSTAL FOR AVIONICS BAY DOOR FS 349-364 CORRODED. REMOVED CORROSION INBD INTERCOSTAL IAW SRM 51-21-06.

Part: FLOOR SUPPORT — CORRODED (BS 319) · airframe 27,170 hrs · 24,022 cycles

CORROSION ON FWD FLOOR SUPPORT BRACKET AT RBL 40, FS 319. BRACKET CORRODED BEYOND ALLOWABLE DAMAGE LIMIT. REPLACED BRACKET.

Part: TIE DOWN — CORRODED (BS 574-589) · airframe 27,170 hrs · 24,022 cycles

CARGO TIE DOWN POINT BETWEEN FS 574.00 AND 589.00 AT LBL 9 CORRODED. CORRODED TIE DOWN IS OUT OF LIMITS IAW SRM 53-61-49. R & R CARGO TIE DOWN REF SRM 51-42-02.

Part: CARGO TRACK — CORRODED (BS 559) · airframe 27,170 hrs · 24,022 cycles

CARGO TRACK AT BL 27.0, FRAME 559+112 IS CORRODED. CORROSION IS OUT OF LIMITS IAW SRM 53-61-49. R & R CARGO TIE DOWN PLATE REF SRM 51-42-02.

Part: CARGO TRACK — CORRODED (BS 559) · airframe 27,170 hrs · 24,022 cycles

CARGO TRACK AT FS 559.00+80 TO 559.96 AND RBL 9 CORRODED. CARGO TRACK IS OUT OF LIMITS IAW 53-51-49. R & R CARGO TRACK IAW SRM 53-61-49.

Part: CARGO TRACK — CORRODED (BS 559) · airframe 27,170 hrs · 24,022 cycles

CARGO TRACK AT FS 559.00+80 TO 559.00+96 AND RBL 27 CORRODED. CORROSION IS OUT OF LIMITS IAW RM 53-51-49. R & R CARGO TRACK IAW SRM 53-61-49.

Part: STRUCTURE — CRACKED (BULKHEAD) · airframe 27,170 hrs · 24,022 cycles

AFT EQUIPMENT BAY AFT PRESSURE BULKHEAD HAS TWO CLIPS CRACKED AT 625.00 AND VERTICAL STIFFENER RBL 36.20. R & R 2EA CLIPS IAW SRM 51-42-06-00 AND 51-42-21-00.

Part: CARGO TRACK — CORRODED (BS 559) · airframe 27,170 hrs · 24,022 cycles

CARGO TRACK AT BL 27.0 BETWEEN FRAMES 559+80 AND 559+96 IS CORRODED. CORROSION TO CARGO TRACK IS OUT OF LIMITS IAW RM 53-51-49. R & R CARGO TRACK IAW SRM 53-61-49.

Part: CARGO TRACK — CORRODED (BS 559-574) · airframe 27,170 hrs · 24,022 cycles

CARGO TRACK AT FS 559.00+112 TO 574.00 AND LBL 9 CORRODED. CORROSION IS OUT OF LIMITS IAW SRM 53-41-49. REMOVED AND REPLACED CARGO TRACK IAW SRM 51-41-02 REF SRM 53-51-49.

Part: FLOORBEAM — CORRODED (BS 349) · airframe 27,170 hrs · 24,022 cycles

CABIN AREA FLOORBEAM AT 349.00 CORRODED. REMOVED CORROSION IAW SRM 51-21-06, 53-21-15, & 53-00-00.

Part: FLOOR SUPPORT — CORRODED (BS 319) · airframe 27,170 hrs · 24,022 cycles

CABIN AREA FLOOR SUPORT CORRODED AT FS 319.00 AND FWD CORNER OF SERVICE DOOR SILL. REMOVED CORROSION IAW SRM 51-21-06. FOUND WITHIN ALLOWABLE DAMAGE LIMITS IAW SRM 53-21-43 AND 53-00-00. REPAIR IS CLASSIFIED AS MINOR.

Part: CARGO TRACK — CORRODED (BS 559-574) · airframe 27,170 hrs · 24,022 cycles

CARGO TRACK AT F S559.00+112 TO 574.00 AND RBL 9 CORRODED. CORROSION OUT OF LIMITS. R & R CARGO TRACK IAW SRM 53-61-49

Part: ANCHOR FITTING — CRACKED (PAX DOOR) · airframe 27,170 hrs · 24,022 cycles

PAX DOOR FWD ANCHOR FITTING CRACKED. REMOVED ANCHOR FITTING IAW AMM 52-11-17-000-803 AND 52-11-17-000-805. INSTALLED NEW ANCHOR FITTING IAW AMM 52-11-17-400-803 AND 51-11-17-400-805.

Part: CARGO TRACK — CORRODED (BS 559) · airframe 27,170 hrs · 24,022 cycles

CARGO TRACK AT FS 559.00+80 TO 559.00+96 AND RBL 9 CORRODED. CORROSION IS OUT OF LIMITS RM 53-51-49. R & R CARGO TRACK IAW SRM 53-61-49

Part: DOUBLER — CORRODED (EMERGENCY EXIT) · airframe 27,170 hrs · 24,022 cycles

LEFT SIDE EMERGENCY EXIT INTERNAL DOUBLER CORRODED. LOCATED BEHIND HOOK FITTING. REMOVED CORROSION IAW SRM 51-21-06.

Part: TIE DOWN — CORRODED (BS 589-605) · airframe 27,170 hrs · 24,022 cycles

CARGO TIE DOWN POINT BETWEEN FS 589.00 AND 605.00 AT LBL 9 CORRODED. CARGO TIE DOWN OUT OF LIMITS IAW SRM 53-61-49. R & R CARGO TIE DOWN REF SRM 51-42-02.

Part: FRAME — CORRODED (BS 333) · airframe 27,170 hrs · 24,022 cycles

FRAME BS 333.00 CORRODED BETWEEN STR 26L AND 26R. REMOVED CORROSION IAW SRM 51-21-06, 51-41-02, 51-42-06. PERFORMED UT THICKNESS INSPECTION OF BLENDED AREA IAW MAC NDT PROCEDURE UT-3. MINIMUM MATERIAL REMAINING .047", ORIGINAL 050", MATERIAL REMOVED .003".

Part: FRAME — CORRODED (BS 319.7) · airframe 27,170 hrs · 24,022 cycles

FRAME BS 319.70 CORRODED BETWEEN STR 26L AND 26R. REMOVED CORROSION IAW SRM 51-21-06 AND 51-42-06. PERFORMED UT THICKNESS INSPECTION OF BLEND AREA IAW MAC NDT PROCEDURE UT-3. MINIMUM MATERIAL REMAINING .047", ORIGINAL .050", MATERIAL REMOVED .003". REPAIRED IAW REO 601R-53-21-2276.

Part: SEAT TRACK — CORRODED (BS 364-394) · airframe 27,170 hrs · 24,022 cycles

SEAT TRACK CORRODED AT FS 364-394 AND LBL 9. CORROSION FOUND OUT OF LIMITS IAW SRM 53-21-49. REMOVED SEAT TRACK IAW AMM 53-01-11-000-802, DRILLED & COUNTERSINK NEW SEAT TRACK IAW SRM 51-40-11, APPLIED A023 FINISH CODE IAW SRM 51-25-16, INSTALLED NEW SEAT TRACK IAW AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 409) · airframe 27,170 hrs · 24,022 cycles

SEAT TRACK CORRODED AT FS 409.00 TO 409.00+128 AND RBL 9. CORROSION OUT OF LIMITS IAW SRM 53-31-49. REMOVED CORRODED SEAT TRACK IAW AMM 53-01-11-000-802. DRILLED AND COUNTER SINK NEW PART SRM 51-40-11. INSTALLED NEW SEAT TRACK IAW AMM 53-01-11-400-802.

Part: SUPPORT BRACKET — CRACKED (ACM) · airframe 27,170 hrs · 24,022 cycles

SUPPORT BRACKET UNDER RT ACM CRACKED. REMOVED AND DRILLED NEW SERVICEABLE SUPPPORT BRACKET IAW SRM 51-42-06. INSTALLED SERVICABLE SUPPORT BRACKET IAW SRM 51-42-06.

Part: PRESSURE PANEL — CORRODED (CABIN FLOOR) · airframe 27,170 hrs · 24,022 cycles

CABIN AREA PRESSURE FLOOR CORRODED AT FS 559.00 BETWEEN RBL 36 AND STR 18. COMPLIED WITH EC/TC REO 601R-53-41-666 AND REO 601R-53-41-666. RII FOUND TO BE SATISFACTORY. (SDR CLOSED)

Part: SEAT TRACK — CORRODED (BS 409) · airframe 27,170 hrs · 24,022 cycles

SEAT TRACK CORRODED AT FS 409.00 TO 409.00+128 AND LBL 9. CORROSION FOUND OUT OF LIMITS IAW SRM 53-31-49. REMOVED SEAT TRACK IAW AMM 53-01-11-000-802. DRILLED AND COUNERSUNK HOLES IAW SRM 51-40-11. INSTALLED NEW SERVICABLE FLOOR SEAT TRACK.

Part: FLOOR PANEL — CORRODED (BS 529) · airframe 27,170 hrs · 24,022 cycles

CABIN AREA PRESSURE FLOOR CORRODED AT FS 529.00 AND BETWEEN LBL 36 TO STR 18 2EA PLACES. BLENDED CORROSION IAW SRM 51-21-06. PERFROMED UT THICKNESS INSPECTION OF BLENDED AREAS IAW MAC NDT PROCEDURE UT-3. MINIMUM MATERIAL REMAINING .072", ORIGINAL IS .080", MATERIAL REMOVED IS .008" MIN MATERIAL REMAINING ON CHEM MIL .053" ORIGNAL .055", MATERIAL REMOVED IS .002" MIN MATERIAL REMAINING .067", ORIGINAL .080" MATERIAL REMOVED .013" BLENDED AREAS WITHIN LIMITS IAW REO 601R-53-41-666, TABLE 14, TABLE 2.

Part: FLOOR PANEL — CORRODED (BS 529) · airframe 27,170 hrs · 24,022 cycles

CABIN AREA PRESSURE FLOOR CORRODED AT FS 529 BETWEEN RBL 36 AND STR 18 2 EA PLACES. PERFORM EC/TC 601R-53-41-666. COMPLIED WITH EC/TC REO 601R-53-41-666 AND REO 601R-53-41-666, REV B.

Part: SEAT TRACK — CORRODED (BS 409-559) · airframe 27,170 hrs · 24,022 cycles

SEAT TRACK CORRODED AT FS 409.00 TO 559.00 AT RBL 9. CORROSION FOUND OUT OF LIMITS IAW SRM 53-41-49. REMOVED SEAT TRACK IAW AMM 53-01-11-000-802. DRILLED AND COUNTERSUNK NEW PARTIAW SRM 51-40-11. INSTALLED NEW SEAT TRACK IAW AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 364-394) · airframe 27,170 hrs · 24,022 cycles

SEAT TRACK CORRODED AT FS 364-394 RBL 9. CORROISON FOUND OUT OF LIMITS IAW SRM 53-21-49. REMOVED SEAT TRACK IAW AMM 53-01-11-000-802, DRILLED AND COUNTERSUNK NEW SEAT TRACK IAW SRM 51-40-11, APPLIED A023 FINISH CODE IAW SRM 51-25-16, INSTALLED NEW SEAT TRACK IAW AMM 53-01-11-400-802.

Part: FRAME — CORRODED (BS 364) · airframe 27,170 hrs · 24,022 cycles

FRAME BS 364.00 CORRODED BETWEEN STR 26L AND 26R. REMOVED CORROSION IAW SRM 51-21-06. PERFORMED UT THICKNESS INSPECTION OF BLENDED AREA IAW MAC NDT PROCEDURES. MINIMUM MATERIAL REMAINING .0794. REMAINING MATERIAL WITHIN ALLOWABLE LIMITS SRM 53-21-23 & 53-00-00.

Part: FLOOR PANEL — CORRODED (BS 513) · airframe 27,170 hrs · 24,022 cycles

CABIN AREA PRESSURE FLOOR CORRODED AT FS 513 AND BETWEEN RBL 36 AND STR 18. COMPLIED WITH EC/TC REO 601R-53-41-666 AND REO 601R-53-41-666, REV B.

Part: FRAME — CORRODED (BS 349) · airframe 27,170 hrs · 24,022 cycles

FRAME FS 349.00 CORRODED BETWEEN STR 26L AND 26R. REMOVED CORROSION IAW SRM 51-21-06 + 51-42-06. PERFORMED UT THICKNESS INSPECTION OF BLEND AREA IAW MAC NDT PROCEDURES UT-3. MINIMUM MATERIAL REMAINING .062", ORIGINAL O63", MATERIAL REMOVED .001". FOUND MORE CORROSION AT FRAME FS 349.00 BETWEEN STR 27R & 26R. REMOVED CORROSION IAW SRM 51-42-06 & 51-21-06. PERFORMED UT THICKNESS INSPECTION OF BLEND AREA IAW MAC NDT INSPECTION PROCEDURE UT-3. MINIMUM MATERIAL REMAINING .062", ORIGINAL .063", MATERIAL REMOVED IS .001".

Part: SILL — CORRODED (FUSELAGE) · airframe 27,170 hrs · 24,022 cycles

PAX DOOR SILL PLATE CORRODED AND FLOOR SUPPORT. DAMAGE EXCEEDS ALLOWABLE DAMAGE LIMITS IAW SRM 53-21-26 & 53-00-00, FIG 102. REMOVED SILL IAW SRM 51-42-06-00/ 51-42-21-00. INSTALLED SILL IAW DWG 601R31527.

Part: CHANNEL — CRACKED (BS 409) · airframe 26,890 hrs · 23,707 cycles

CRACK INDICATION NOTED AT FS 409+128 RBL 18 WL 69.0 OTBD CHANNEL AFT RADIUS APPROX .10 IN LENGTH 70 PERCENT FULL SCREEN HEIGHT FAILED NDT. LOCATED NEW CHANNEL IAW SRM 51-40-11 AND 51-42-06. INSTALLED CHANNEL IAW REO 601R-53-41-889, STEP 1.

Part: CHANNEL — CRACKED (BS 409) · airframe 26,890 hrs · 23,707 cycles

CRACK INDICATION NOTED AT FS 409+128, LBL 18, WL 69.0 OTBD CHANNEL AFT RADIUS APPROX .10 IN LENGTH 53 PERCENT FULL SCREEN HEIGHT FAILED NDT. INSTALLED NEW CHANNEL IAW SRM 51-42-06 AND SRM 51-42-22 AND REO 601R-53-41-889.

Part: CHANNEL — CRACKED (BS 409) · airframe 26,890 hrs · 23,707 cycles

CRACK INDICATION NOTED AT FS 409+128, BL 0.00 CHANNEL AT WL 69.00. REPLACED CHANNEL IAW REO 601R-53-41-889.

Part: FITTING — CRACKED (BS 621 BULKHEAD) · airframe 26,890 hrs · 23,707 cycles

CRACK INDICATION NOTED AT FS 621 REAR PRESSURE BULKHEAD FWD FACE AT INBD EDGE OF THE LINTEL MACHINED FITTING, APPROX .10" LENGTH AND 85 PERCENT FULL SCREEN HEIGHT. FAILED NDT. REPAIRED FITTING IAW REO 601R-53-61-1230 & REO 601R-53-61-4353.

Part: DOOR — BINDING (MAIN PAX) · airframe 26,274 hrs · 22,997 cycles

MAIN PAX DOOR DIFFICULT TO OPEN. COMPLIED WITH VISUAL INSPECTION OF PAX DOOR IAW AMM 52-11-00. OPS CHECKED GOOD.

Part: HANDLE — OUT OF ADJUST (PAX DOOR) · airframe 25,737 hrs · 22,384 cycles

F/A COULD NOT OPEN PASSENGER DOOR, THE HANDLE WOULD NOT RAISE. HAD TO HAVE GROUD PERSONNEL OPEN THE DOOR FROM THE OUTSIDE. OPS CHECK AND ADJUSTED INNER PAX DOOR HANDLE IAW AMM 52-11-21. OPS CHECK GOOD.

Part: O-RING — LEAKING (PRESSURE SWITCH) · airframe 25,429 hrs · 22,044 cycles

NR 2 ENG OIL PSI FLUCTUATING 15 PSI AT CRUISE AND IDLE POWER. AS LOW AS 32 TO 47 PSI (EMERGENCY DECLARED) FOUND NR 2 ENG OIL PRESS SWITCH O-RING LEAKING STEADY STREAM. R & R SAID O-RING IAW AMM 79-31-03. PERFORMED LEAK AND OIL CONSUMPTION TESTS IAW AMM 71-00-00. NO LEAKS OR OIL CONSUMPTION NOTED.

Part: LATCH — OUT OF ADJUST (PAX DOOR) · airframe 25,413 hrs · 22,030 cycles

PAX BOARDING DOOR LATCHING MECHANISM IS DIFFICULT TO SECURE, CLOSED AND TO OPEN. DOOR HANDLE OR LATCHING MECHANISM APPEARS TO BE OUT OF ADJUSTMENT. LUBED DOOR HANDLE AND MECHANISM. OPS CHECK GOOD.

Part: LIGHT — DAMAGED (CABIN) · airframe 25,349 hrs · 21,961 cycles

EMERGENCY EXIT LIGHT, ON WARDROBE AT ENTRY WAY IS DAMAGED. R & R EMERGENCY EXIT LIGHT ASSY ON WARDROBE AT ENTRY WAY IAW AMM 33-51-19. R & R EMERGENCY EXIT LIGHT ASSY ON WARDROBE AT ENTRY WAY IAW AMM 33-51-19.

Part: PLACARD — DETERIORATED (CABIN) · airframe 24,852 hrs · 21,378 cycles

ASD "TO OPEN", "EXIT", AND MULTIPLE "VERTICAL STRIPES" ARE DETERIORATED. R & R ASD "TO OPEN", "EXIT", AND SIX "VERTICAL STRIPES" IAW AMM 11-30-00. R & R ASD "TO OPEN", "EXIT", AND SIX "VERTICAL STRIPES" IAW AMM 11-30-00. (CLOSED)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,839 hrs · 21,364 cycles

THE THIRD EMERGENCY LIGHT ON THE RT SIDE OF ACFT IS INOP. REPLACED THE THIRD EMERGENCY LIGHT ON THE ACFT RT SIDE. OPS CHECK GOOD. DONE IAW THE AMM CHAP 33-51-21. (CLOSED)

Part: LEVER — FAILED (TE FLAPS) · airframe 24,546 hrs · 21,016 cycles

FLAPS FAIL MESSAGE, FLAPS FAIL AT 20 DEG. (EMERGENCY DECLARED) COMPLIED WITH TROUBLESHOOTING OF FLAPS IAW FIM 27-50-00. NO FURTHER ACTION REQUIRED WITH ORIGINAL FAULT AS "FLAP LEVER FAULT", CODE 19 C1 AND 19 C2, FLAP LEVER TEST PASS & FLAP OPERATING NORMALLY ON GROUND. COMPLIED WITH AD 2009-06-12, REFER TO WO NR177976. (CLOSED)

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 24,512 hrs · 20,969 cycles

RT FWD EXTERNAL EMERGENCY LIGHT IS INOP. RELAMPED RT FWD EXTERNAL EMERGENCY LIGHT IAW AMM 33-51-21.OPS CHECK GOOD. RELAMPED RT FWD EXTERNAL EMERGENCY LIGHT IAW AMM 33-51-21. OPS CHECK GOOD.

Part: DOOR — BINDING (MAIN PAX) · airframe 24,277 hrs · 20,679 cycles

PAX DOOR HARD TO OPEN. OPENED AND CLOSED PAX DOOR 5 TIMES, OPS CKD GOOD IAW AMM 52-11-01. (CLOSED)

Part: INDICATOR — FALSE INDICATION (FIRE DETECTION) · airframe 24,200 hrs · 20,591 cycles

CARGO BOTTLE LOW CAUTION MESSAGE IN FLT COMPLIED WITH QRH (ENROUTE, ACFT DIVERTED DUE TO MX - EMERGENCY EQUIPMENT DID RESPOND) INSPECTED BOTH CARGO FIRE BOTTLE PRESSURE GAUGES IAW AMM CH 26-25-01 AND PERFORMED OPS TEST IAW AMM CH 26-25-00. NO DEFECTS FOUND. ACFT OK FOR SERVICE.

Part: DOOR — BINDING (EMERGENCY EXIT) · airframe 24,163 hrs · 20,544 cycles

PAX DOOR HARD TO OPEN. REMOVED AND REPLACED RT EMERGENCY FLOOR LEVEL EXIT PANEL IAW CRJ 200 AMM 33-51-10 OPS CHECK GOOD NO DEFECTS AT THIS TIME. [SDR CLOSED]

Part: DOOR — BINDING (MAIN PAX) · airframe 24,163 hrs · 20,544 cycles

MAIN CABIN DOOR DIFFICULT TO OPEN. OPS CHECKED PAX DOOR IAW AMM 52-11-00. COULD NOT DUPLICATE, OPS CHECKED GOOD IAW AMM. OK FOR SERVICE.

Part: DOOR — BINDING (MAIN PAX) · airframe 24,082 hrs · 20,448 cycles

PAX DOOR WILL NOT OPEN. PREFORMED OPS TEST OF PAX DOOR IAW IAW AMM 52-11-00-710-801, NO DEFECTS FOUND, OK FOR SERVICE. (CLOSED)

Part: DOOR — BINDING (MAIN PAX) · airframe 23,710 hrs · 20,016 cycles

F/A REPORTS MAIN PAX DOOR DIFFICULT TO OPEN-THE LEVER WAS DIFFICULT. INSP PAX DOOR FOUND NO DEFECTS. LUBED DOOR HANDLE, OPS CK OK IAW AMM 52-11-00. (CLOSED)

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 23,405 hrs · 19,663 cycles

CAPT'S FLASHLIGHT INOP. REPLACED CAPT FLASHLIGHT. IAW AMM 25-60-00, OPS TEST OK. DEFER CLEARED PLACARD REMOVED.

Part: WINDSHIELD WIPER — MALFUNCTIONED · airframe 23,365 hrs · 19,618 cycles

WINDSHIELD WIPERS WOULD NOT TURN OFF. (A/C RETURNED TO DEPARTURE AFTER T/O. TOWER DECLARED EMERGENCY AND HAD TRUCKS STANDING BY) REMOVED AND REPLACED CAPT. AND FO'S WIPER CONTROL PANEL IAW AMM 30-42-11OPS CK GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 23,222 hrs · 19,450 cycles

NR 8 EXT EMERGENCY LIGHT IS INOP. RELAMPED NR 8 EXT EMERGENCY LIGHT IAW AMM 33-51-21, OP'S CHECK GOOD, RELAMPED NR 8 EXT EMERGENCY LIGHT IAW AMM 33-51-21, OP'S CHECK GOOD.

Part: INTERCOSTAL — CRACKED (BS 484) · airframe 23,144 hrs · 19,364 cycles

SUSPECTED CRACK ON L CLIP CONNECTING INTERCOSTAL TO ACFT SUPPORT BEAM FS484 RT SIDE RBL.

Part: ATTACH FITTING — CRACKED (INTERCOSTAL) · airframe 23,144 hrs · 19,364 cycles

PERFORMED E/T INSP ON INBD AND OTBD CLIPS OF INTERCOSTAL AT FS484 IAW NDTM 51-20-06 OIN EACH PART RADIATING FROM TOP FASTENER HOLE. C/W REO 601R-53-41-059 REV B DATED 09/16/09. C/W ECTC TASK CARD REO 601R-53-41-059 B 23 NOV 09. LEAK CHECK GOOD IAW AMM 21-51-00-790-801. RII C/W IAW SP 607 ALL WORK PERFORMED SATISFACTORY IAW NDTM 51-20-06 REO 601R-53-41-059 21-51-00-790-801.

Part: ISOLATOR — BROKEN (BS 621 BULKHEAD) · airframe 23,145 hrs · 19,366 cycles

DRILLED AND REMOVED BROKEN ISOLATORS IAW SRM 51-42-06. CC21 01/04/10. REPLACED ISOLATORS WITH NEW ISOLATORS 5 EA ON 621.00 PRESSURE BULKHEAD IAW SRM 51-42-10. CC21 01/04/10. (12) PRIME AND ALODINE PARTS IAW SRM 51-25-06.

Part: ISOLATOR — BROKEN (BS 621 BULKHEAD) · airframe 23,146 hrs · 19,366 cycles

FIVE BROKEN INSOLATORS ON 621.00 PRESSURE BULHEAD.

Part: FLOOR SUPPORT — CORRODED (BS 574-621) · airframe 23,143 hrs · 19,362 cycles

CORROSION ON LBL 27.00 FLOOR SUPPORT AROUND NUTPLATE HOLES FROM FS 574-621.

Part: ATTACH ANGLE — CRACKED (BS 484) · airframe 23,143 hrs · 19,362 cycles

SUSPECTED CRACK ON L CLIP CONNECTING INTERCOSTAL TO ACFT SUPPORT BEAM FS484 RT SIDE RBL. PERFORMED E/T INSP ON INBD AND OTBD CLIPS OF INTERCOSTAL AT FS484 IAW NDTM 51-20-06 OIN EACH PART RADIATING FROM TOP FASTENER HOLE SEE ATTACHED NDT REPORT. REO 601R-53-41-059 REV B DATED 09/16/09. C/W ECTC TASK CARD REO 601R-53-41-059 B 23 NOV 09. LEAK CHECK GOOD IAW AMM 21-51-00-790-801. RII C/W IAW SP 607 ALL WORK PERFORMED SATISFACTORY IAW NDTM 51-20-06 REO 601R-53-41-059 21-51-00-790-801.

Part: BULKHEAD — CRACKED (BS 621) · airframe 23,143 hrs · 19,362 cycles

CRACK NOTED AT MARKED ON FS 621 BULKHEAD, FWD FACE, ABOVE CARGO DOOR TRACK FITTING.

Part: BULKHEAD — CRACKED (BS 559) · airframe 23,143 hrs · 19,362 cycles

FS 559.0 PRESSURE BULKHEAD CRACKED AT WL 59.1 INBD OF RBL 18, WL 54.1 OTBD OF RBL 9 AND CAP ANGLE RADIUS LBL 18.

Part: GLOWSTRIP — DAMAGED (CABIN) · airframe 23,143 hrs · 19,362 cycles

ALL CABIN PHOTOLUMINESCENT STRIPS DAMAGED BEYOND LIMITS.

Part: FAIRING — CRACKED (NACELLE) · airframe 23,143 hrs · 19,362 cycles

RT UPPER STANG FAIRING IS CRACKED PNL 444BT.

Part: POST — CRACKED (FUSELAGE) · airframe 23,143 hrs · 19,362 cycles

JOB 2741115 OPERATION 76 /FS409.0+128 VERT POST AT RBL18.0 HAS A CRACK LOCATED ON THE AFT SIDE OF THE FWD INBD FLANGE, CRACK IS MARKED.

Part: GLOWSTRIP — DAMAGED (CABIN) · airframe 23,143 hrs · 19,362 cycles

PHOSPHORESCENT STRIP FOR EMERGENCY EXIT RIPPED ( STRIP FALLS OUT) - BY SEATS 8 CD, 9 CD.

Part: ROD — BENT (SERVICE DOOR) · airframe 22,388 hrs · 18,563 cycles

SERVICE DOOR LOWER STABILIZER ROD BENT. RELATED TO DEFECT NR 465475-1 & 207966-1.

Part: ROD — BROKEN (DOOR STAB) · airframe 22,388 hrs · 18,563 cycles

RT SIDE SERVICE DOOR INTERNAL STABILIZER ROD BROKEN [RELATED TO DEFECT NR 465475-3 AND 209618-1.

Part: LANDING GEAR — MALFUNCTIONED (LT MLG) · airframe 22,267 hrs · 18,430 cycles

ACFT REMOVED FROM SERVICE TO COMPLY WITH WO NR 120960, LT MAIN GEAR DID NOT EXTEND DURING LANDING CAUSING DAMAGE TO ACFT. PER NTSB AND FAA INVESTIGATION REF TO W/O 120960 FOR ALL MAINTENANCE PERFORMED TO RETURN A/C TO SERVICE.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 22,267 hrs · 18,430 cycles

LEFT MAIN GEAR DISAGREE ON APPROACH. EMERGENCY DECLARED. COMPLIED WITH ISE-STR-09-016.

Part: UNKNOWN — MALFUNCTIONED (LANDING GEAR) · airframe 22,267 hrs · 18,430 cycles

LEFT MAIN LANDING GEAR INDICATED 'UP' WITH GEAR LEVER DOWN UNTIL 3RD RECYCLE. EMERGENCY DECLARED. LANDING GEAR RETRACTION SYSTEM.

Part: LIGHT — BROKEN (CABIN) · airframe 21,831 hrs · 18,011 cycles

FLT 5226, ONE OF CABIN EMERGENCY STRIP IS BROKEN. REPLACED BROKEN BROKEN CABIN EMERGENCY STRIP IAW AMM 33-51-01.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,643 hrs · 16,905 cycles

LT OVER WING EMERGENCY LIGHT INOP. RELAMPED LT OVER WING EMERGENCY LIGHT IAW CRJ200AMM 33-51-21. OP CHECKS GOOD.

Part: DOOR — MALFUNCTIONED (PAX DOOR) · airframe 20,442 hrs · 16,721 cycles

CANNOT CLOSE PAX DOOR. FLT 4451 DEL 551 MINS NC. CHECKED PAX DOOR PUSHRODS, OUTER AND INNER LOCKS. OPS CHECKED PAX DOOR OVER 20 TIMES, INSIDE AND OUTSIDE. PAX DOOR WORKS SMOOTHLY EVERY TIME IAW CRJ 100 AMM 52-11-00. NO DEFECTS NOTED AT THIS TIME. ACFT OK FOR SERVICE. (S)

Part: DOOR — STIFF (MAIN PAX) · airframe 20,241 hrs · 16,557 cycles

MAIN CABIN DOOR DIFFICULT TO CLOSE (OUTER HANDLE). PERFORMED OPERATIONAL TEST OF PASSENGER DOOR IAW CRJ 200 MM 52 11 00 WITH NO DEFECTS NOTED AT THIS TIME. (S)

Part: ROLL PIN — DAMAGED (SERVICE DOOR) · airframe 20,024 hrs · 16,359 cycles

SERVICE DOOR DIFFICULT TO CLOSE REMOVED AND REPLACED ROLL PIN ON SERVICE DOOR RELEASE HANDLE OPS CHECK GOOD IAW AMM 52-41-02. (B)

Part: DOOR — BINDING · airframe 19,861 hrs · 16,217 cycles

FORWARD DOOR HARD TO CLOSE. FLT 4852 DEL 29 MINS.

Part: DOOR — MALFUNCTIONED (PAX DOOR) · airframe 19,861 hrs · 16,217 cycles

PAX DOOR WILL NOT CLOSE. FLT 4209 DEL 39 MINS.

Part: DOOR — MALFUNCTIONED (PAX DOOR) · airframe 19,861 hrs · 16,217 cycles

CABIN DOOR DIFFICULT TO CLOSE.

Part: BRACKET — CORRODED (RT SPOILERON) · airframe 19,812 hrs · 16,173 cycles

AAR - CORROSION ON LOWER MOUNT BOLT SAFETY BRACKET MOUNT BOLT FOR RT SPOILERON I/B PCU (I/B BRACKET).

Part: ATTACH ANGLE — BROKEN (PAX DOOR) · airframe 19,812 hrs · 16,173 cycles

AAR - PAX DOOR TOP STEP ATTACH ANGLE IS BROKEN.

Part: HANDLE — LACK OF LUBE (EMERGENCY EXIT) · airframe 19,812 hrs · 16,173 cycles

AAR - LEFT OVERWING EMERGENCY EXIT FAIL PULL TEST ON EXIT HANDLE. LUBRICATED DOOR & RETESTED, NO DEFECTS NOTED AT THIS TIME IAW CRJ 200 MM 12-20-52 & 52-21-00. SUPPLEMENTAL SDR CLOSED 3/27/08.

Part: HANDLE — LACK OF LUBE (EMERGENCY EXIT) · airframe 19,812 hrs · 16,173 cycles

RIGHT OVERWING EMERGENCY EXIT FAIL THE PULL TEST ON EXIT HANDLE. LUBRICATED & RETESTED, NO DEFECTS NOTED AT THIS TIME IAW MM 112-20-52 & 52-21-00.

Part: DRAG ANGLE — CRACKED (WING) · airframe 19,812 hrs · 16,173 cycles

RT DRAG ANGLE I/B OF RIGHT BATTERY RIB IS CRACKED. REMOVED FASTENERS FROM R/H DRAG ANGLE & REMOVED ANGLE AFT OF DRAG ANGLE 15021. REMOVED DRAG ANGLE, LOCATED FASTENER LOCATION ON SERVICEABLE DRAG ANGLE. OK TO INSTALL. INSTALLED NEW SERVICEABLE DRAG ANGLE IAW SRM 51-42-21.

Part: NUT — CORRODED (RT SPOILERON) · airframe 19,812 hrs · 16,173 cycles

CORROSION ON RT WING SPOILERON HINGE POINT NUTS. REMOVED AND REPLACED O/B HINGE POINT NUT ON RT WING SPOILERON WITH NEW SERVICEABLE NUT IAW AMM 27-64-01.

Part: NUT — CORRODED (RT SPOILER) · airframe 19,812 hrs · 16,173 cycles

AAR - CORROSION ON RT WING FLIGHT SPOILER HINGE POINT NUTS.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 19,812 hrs · 16,173 cycles

INTERCOSTAL CLIP CRACKED AT FS 484 LBL 28. REPAIRED, IAW REO 601R-53-41-059.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 19,812 hrs · 16,173 cycles

INTERCOSTAL CLIP CRACKED AT FS 484 LBL 36. REMOVED CRACKED LIGHTED FLOOR LEVEL EXIT SIGN P/N BR9279-106 IAW AMM 33-51-10. INSTALLED SERVICEABLE LIGHTED FLOOR-LEVEL EXIT SIGN P/N BR9279-106 IAW AMM 33-51-10. OPS CHECK REQUIRED. PERFORMED OPS CHECK IAW AMM 33-51-00. NO DEFECTS NOTED AT THIS TIME.

Part: PLACARD — MISSING (EMERGENCY EXIT) · airframe 19,812 hrs · 16,173 cycles

AAR - EMERGENCY ESCAPE HATCH PLACARDS CREW INSTRUCTION, OPEN, ARROW AND CLOSE ARE DAMAGED OR MISSING.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 19,812 hrs · 16,173 cycles

AAR - INTERCOSTAL CLIP CRACKED AT FS 484 LBL 36.

Part: PLACARD — DAMAGED (EMERGENCY EXIT) · airframe 19,812 hrs · 16,173 cycles

AAR - LEFT OVERWING EMERGENCY EXIT PUSH PLACARD DAMAGED.

Part: DOOR — STUCK (SERVICE) · airframe 18,977 hrs · 15,474 cycles

UNABLE TO CLOSE SERVICE DOOR.

Part: COFFEEMAKER — ODOR (GALLEY) · airframe 18,733 hrs · 15,288 cycles

CLIMBING THRU F260 TO F300 HAD A STRONG SMOKE LIKE ODOR. SMELLED LIKE BURNING RUBBER OR PLASTIC. F/A REPORTED, BEFORE DEPARTURE COFFEE WAS SPILLED IN THE COFFEEMAKER.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,631 hrs · 15,211 cycles

EMERGENCY LIGHTS 6 THROUGH 9 WILL NOT ILLUMINATE.

Part: ANCHOR FITTING — CRACKED (AIRSTAIR DOOR) · airframe 18,527 hrs · 15,128 cycles

ASD AFT ANCHOR FITTING CRACKED.

Part: BRACKET — CRACKED (CARGO DOOR) · airframe 18,242 hrs · 14,923 cycles

CARGO DOOR AFT RAIL SUPPORT BEAM BRACKET CRACKED.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 17,966 hrs · 14,706 cycles

FUEL SMELL IN COCKPIT & IN FLIGHT.

Part: FLAP SYSTEM — FAILED (TE FLAPS) · airframe 17,220 hrs · 14,119 cycles

RECEIVED FLAPS FAIL ON APPROACH WHEN SELECTING FLAPS FROM 0 TO 8. EMERGENCY DECLARED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,570 hrs · 12,852 cycles

CEILING EMERGENGY LIGHT, 1EA. INOP.

Part: SKIN — CRACKED (AIR STAIR DOOR) · airframe 15,526 hrs · 12,821 cycles

EVIDENCE OF POSSIBLE SKIN CRACK UNDER TOP ASD STEP FWD SECTION.

Part: WARNING LIGHT — ILLUMINATED (COCKPIT) · airframe 15,319 hrs · 12,648 cycles

REFER TO AFDL 288324 ITEM 2, MACH TRIM, STAB TRIM, AUTO PILOT PITCH TRIM FAIL CAUTION MESSAGE ILLUMINATED IN FLIGHT WOULD NOT RESET UNTIL 3RD ATTEMPT, FLT 4375 CX. REFER TO MAINT ENTRY #288324-3 FOR CORRECTIVE ACTION. AN EMERGENCY WAS DECLARED.

Part: WARNING LIGHT — ILLUMINATED (FUEL QTY) · airframe 15,284 hrs · 12,621 cycles

AFTER 1 HR IN FLIGHT, AUTO XFLOW INHIBIT STATUS MSG CAME ON. ALSO, LOST RIGHT FUEL QUANTITY, INDICATION AND TOTAL FUEL QUANTITY (AN EMERGENCY WAS DECLARED).

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 15,125 hrs · 12,494 cycles

SERVICE DOOR EXTERNAL EMERGENCY LIGHT INOP

Part: PRESSURE BLKHD — CRACKED (FUSELAGE)

DURING A C-CHECK, THE PRESSURE BULKHEAD FORWARD FACE, AT FS 409+128, BOTTOM OB RADIUS OF THE VERTICAL BEAM AT RBL 18, WAS FOUND TO BE CRACKED. MAINTENANCE REPAIRED THE PRESSURE BULKHEAD FORWARD FACE, AT FS 409+128, BOTTOM OB RADIUS OF THE VERTICAL BEAM AT RBL 18 IAW REO. (K)

Part: STRINGER — CRACKED (FUSELAGE)

DURING C-CHECK, STR 14R, JUST AFT OF FS 280, WAS FOUND TO BE CRACKED. THIS MRR WILL REMAIN OPEN PENDING MAINTENANCES DETERMINATION OF AN APPROPRIATE C/A. (K)

Part: SILL — CORRODED (FUSELAGE)

DURING A C-CHECK, THE FLOOR SILL, AROUND THE NUT PLATE HOLE AT FS 529.00 AND 36 LBL, WAS FOUND TO BE CORRODED. MRR WILL REMAIN PENDING MAINTENANCE DETERMINATION OF AN APPROPRIATE C/A. (K)

Part: SILL — CORRODED (FUSELAGE)

DURING A C-CHECK, FS 605.00, JUST BELOW THE WATER TANK ON THE FLOOR SILL, AROUND THE NUT PLATE HOLE, WAS FOUND TO BE CORRODED. THIS MRR WILL REMAIN OPEN PENDING MAINTENANCE DETERMINATION OF AN APPROPRIATE C/A. (K)

Part: STRUCTURE — CRACKED (FUSELAGE)

DURING C-CHECK, STATION 202, NEAR THE PARKING BRAKE CABLE, WAS FOUND TO BE CRACKED. THIS MRR WILL REMAIN OPEN PENDING MAINTENANCES DETERMINATION OF AN APPROPRIATE C/A. (K)

Part: INTERCOSTAL — CRACKED (FUSELAGE)

DURING A C-CHECK, A SUSPECTED CRACK WAS FOUND AT FS 280, JUST OB OF LBL 9, ON THE INTERCOSTAL NEXT TO THE LANDING GEAR MANUAL RELEASE PULLEY BRACKET. THIS MRR WILL REMAIN OPEN PENDING MAINTENANCE DETERMINATIOM OF AN APPROPRIATE C/A. (K)

Part: WEB — CRACKED (FUSELAGE)

DURING C-CHECK, THE CENTER BOX BEAM UPPER WEB, UNDER THE FIRE LOOP BRACKET AT FS 640, WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINENANCE REPAIRED THE CENTER BOX BEAM UPPER WEB, UNDER THE FIRE LOOP BRACKET AT FS 640, IAW EO. (K)

Part: INTERCOSTAL — CORRODED (FUSELAGE)

DURING C-CHECK, THE INTERCOSTAL AT FS 280, BETWEEN LBL 9 AND RBL 9, WAS FOUND TO BE CORRODED. THIS MRR WILL REMAIN OPEN PENDING MAINTENANCE DETERMINATION OF AN APPROPRIATE C/A. (K)

Part: CLIP — CRACKED (FUSELAGE)

DURING A C-CHECK, THE FS 280 LT SIDE OB CLIP WAS FOUND TO BE CRACKED. THIS MRR WILL REMAIN OPEN PENDING MAINTENANCES DETERMINATION OF AN APPROPRIATE C/A. (K)

Part: PLACARD — WORN (FUSELAGE)

DURING C-CHECK, THE PASSENGER DOOR EXIT PLACARD WAS FOUND TO BE WORN. THIS MRR WILL REMAIN OPEN PENDING MAINTENANCE DETERMINATION OF AN APPROPRIATE C/A. (K)

Part: FRAME — CRACKED (BS 718 S10-11L)

DURING A C-CHECK, THE LT SIDE FRAME AT FS 718, BETWEEN STR 10 AND 11L, WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE LT SIDE FS 718, BETWEEN STR 10 AND STR 11, IAW EO. (K)

Part: WEB — CRACKED (FUSELAGE)

DURING A C-CHECK, THE LT AND RT SIDE LOWER BOX BEAM WEB, AT THE FWD IB ACCESS PANEL NUT PLATE, WAS FOUND TO BE CRACKED. THIS MRR WILL REMAIN OPEN PENDING MAINTENANCE DETERMINATION OF AN APPROPRIATE C/A. (K)

Part: FRAME — CRACKED (FUSELAGE)

DURING A C-CHECK, THE RT SIDE FRAME AT FS 718, BETWEEN STR 10 AND 11R, WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE RT SIDE FS 718, BETWEEN 10 AND 11R, IAW EO. (K)

Part: SUPPORT ANGLE — CRACKED (FUSELAGE)

DURING C-CHECK, THE FS 280 AFT FLOOR SUPPORT ANGLE, AT THE EMERGENCY EXIT PULLEY BRACKET, OB OF LBL9, WAS FOUND TO BE CRACKED. THIS MRR WILL REMAIN OPEN PENDING MAINTENANCE DETERMINATION OF AN APPROPRIATE C/A. (K)

Part: CLIP — CRACKED (FUSELAGE)

DURING A C-CHECK, THE STATION 625 CLIP, AT STR 14L, WAS FOUND TO BE CRACKED. THIS MRR WILL REMAIN OPEN PENDING MAINTENANCE DETERMINATION OF AN APPROPRIATE C/A. (K)

Part: LENS — CRACKED (CABIN)

DURING C-CHECK, THE EXIT LIGHT LENS COVER, FORWARD OF THE SERVICE DOOR, WAS FOUND T BE CRACKED. MAITENANCE REMOVED AND REPLACED THE EXIT LIGHT LENS COVER, FORWARD OF THE SERVICE DOOR. (K)

Part: LIGHT — INOPERATIVE (CABIN)

DURING A GROUND INSPECTION IN CAE, THE SECOND OVERHEAD EMERGENCY CEILING LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE SECOND OVERHEAD EMERGENCY CEILING LIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: HINGE — BROKEN (PAX DOOR)

DURING A C-CHECK IN MCN, THE TOP STEP HINGE ON THE PASSENGER DOOR WAS FOUND BROKEN. MAINTENANCE IS REMOVING AND REPLACING THE OTP STEP HINGE ON THE PASSENGER DOOR. (M)

Part: CLIP — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE INBOARD CLIP AT FS 484, LBL 27 AND OUTBOARD CLIP T FS 484, LBL 36 WERE FOUND TO BE CRAKCED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE INBOARD CLIP AT FS 484, LBL 27 AND REPAIRING THE OUTBOARD CLIP AT FS 484, LBL 36 IAW ASA EO 600-53-0098. (M)

Part: BRACKET — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE RAM AIR SPIDER DUCT BRACKET IN THE AFT EQUIPMENT BAY WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE RAM AIR SPIDER DUCT BRACKET IN THE AFT EQUIPMENT BAY IAW AMM 21-52. (M)

Part: RIB — CRACKED (WING)

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

Part: PLATE — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE CARGO DOOR SILL FLOOR LANDING PLATE AT FS 605 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTNENANCE IS REPAIRING THE CARGO DOOR SILL FLOOR LANDING PLAT AT FS 605 IAW ASA EO 600-53-0117. (M)

Part: FLOOR SUPPORT — CRACKED (FUSELAGE)

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

Part: CLIP — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE CLIPS AT FS 280, LBL 9 INBOARD AND AT RBL 9 INBOARD AND OUTBOARD WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CLIPS AT FS 280, LBL 9 INBOARD AND AT RBL 9 INBOARD AND OUTBOARD IAW SRM 51-00. (M)

Part: HANDLE — CRACKED (E/E DOOR)

DURING A C-CHECK IN MCN, THE MAIN AVIONICS BAY DOOR HANDLE AS FOUND CRACKED AT THE BASE BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE MAIN AVIONICS BAY DOOR HANDLE. (M)

Part: STEP — BROKEN (PAX DOOR)

FLT 4667 - DURING A GROUND INSPECTION IN ATL, THE PASSENGER DOOR BOTTOM STEP WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR BOTTOM STEP. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: COVER — MISSING (EXIT SIGN)

DURING HANGAR MAINTENANCE IN BTR, THE AFT CEILING EMERGENCY EXIT SIGN COVER WAS FOUND MISSING. MAINTENANCE REPLACED THE AFT CEILING EMERGENCY EXIT SIGN COVER. (M)

Part: FIXTURE — BROKEN (EMERGENCY LIGHT)

DURNG AN A-CHECK IN BTR, THE PASSENGER DOOR EMERGENCY EXIT LIGHT FIXTURE NEAR THE FLIGHT ATTENDANTS STATION WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR EMERGENCY EXIT LIGHT ASSEMBLY NEAR THE FLIGHT ATTENDANTS STATION. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: MECHANISM — DAMAGED (PAX DOOR)

FLT 4332 - DUIRNG A GROUND INSPECTION IN DFW, THE PASSENGER DOOR WAS VERY HARD TO OPEN FROM THE OUTSIDE. MAINTENANCE REMOVED AND REPLACED THE PULL-IN MECHANISM ASSEMBLY. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DURING A GROUND INSPECTION IN MGM, THE CEILING EMERGENCY EXIT LIGHT AT ROW 10 WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED A LAMP IN THE CEILING EMEGENCY EXIT LIGHT AT ROW 10. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: WINDOW — CRACKED (COCKPIT)

FLT 4403 - DURING CRUISE FROM GRR-ATL, AT APPROXIMATELY 24,000 FEET, THE CREW NOTICED A SMALL CRACK IN THE PILOT'S LEFT SIDE WINDOW. THE CRACK PROGRESSED SLOWLY AND THEN SUDDENLY POPPED ACROSS THE WINDOW. THE AIRCRAFT REDUCED SPEED AND LANDED SAFELY IN ATL. MAINTENANCE REMOVED AND REPLACED THE PILOT'S LEFT SIDE WINDOW. OPERATIONAL AND PRESSURE CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: WINDSHIELD — FAILED (COCKPIT)

DURING CRUISE FLIGHT FROM ATL-ORH, AT FL330, THE CAPTAINS WINDSHIELD SHATTERED. AN EMERGENCY WAS DECLARED AND AN EMERGENCY DESCENT WAS PERFORMED AT A SLOWER AIRSPEED OF APPROXIMATELY 250 KIAS TO 10,000 FEET. AIRCRAFT DIVERTED TO JFK AND MADE AN UNEVENTFUL LANDING. (M)

Part: SEAL — WORN (COMPRESSOR)

DURING THE INITIAL APPROACH, THE CAPTAIN RECEIVED A (SMOKE TOILET) INDICATION. THE FLIGHT ATTENDANT VERIFIED SMOKE IN THE CABIN. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED SAFELY. THE SMOKE HAD DISSIPATED AT TIME OF LANDING. THE TEAR DOWN REPORT OF THE APU FROM HONEYWELL STATES THAT THE COMPRESSOR SEAL WAS FOUND WORN CAUSING AN OILY ROTATING GROUP TO INFECT THE BLEED AIR WITH AN OIL SMELL. THIS COULD ALSO CAUSE SMOKE TO CIRCULATE THROUGHOUT THE CABIN.

Part: SENSOR — FAILED (A/C BAY)

FLT 4531 - ON FINAL APPROACH INTO ATL, SHORTLY AFTER APU START UP, THE 'SMOKE TOILET' MESSAGE ILLUMINATED. THE CAPTAIN IMMEDIATELY SHUT DOWN THE APU AND TRANSFERRED THE BLEEDS BACK TO THE ENGINE. THE MESSAGE EXTINGUISHED. THE FLIGHT ATTENDANT REPORTED A SLIGHT BUILD UP OF SMOKY HAZE IN THE CABIN THAT QUICKLY DISSIPATED ON LANDING. AIRCRAFT LANDED SAFELY IN ATL. MAINTENANCE REMOVED AND REPLACED THE LEFT COALESCER SOCK AND DUCT TEMPERATURE SENSOR. OPERATIONAL CHECKS NORMAL. AIRCRAFT RETURNED TO SERVICE. (M)

Part: COALESCER BAG — CONTAMINATED (CABIN)

ON FINAL APPROACH INTO ATL, SHORTLY AFTER APU START UP, THE 'SMOKE TOILET' MESSAGE ILLUMINATED. THE CAPTAIN IMMEDIATELY SHUT DOWN THE APU AND TRANSFERRED THE BLEEDS BACK TO THE ENGINE. THE MESSAGE EXTINGUISHED. THE FLIGHT ATTENDANT REPORTED A SLIGHT BUILD UP OF SMOKY HAZE IN THE CABIN THE QUICKLY DISSIPATED ON LANDING. AIRCRAFT LANDED SAFELY IN ATL. MAINTENANCE REMOVED AND REPLACED THE LEFT COALESCER SOCK AND DUCT TEMPERATURE SENSOR. OPERATIONAL CHECKS NORMAL. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BRACKET — BENT (NLG)

FLT 4404 - AFTER TAKEOFF FROM ATL, THE NOSE LANDING GEAR WOULD NOT RETRACT AND STAYED DOWN AND LOCKED AFTER THE GEAR WAS SELECTED UP. AN EMERGENCY WAS DECLARED. AIRCRAFT RETURNED TO ATL AND MADE AN OVERWEIGHT LANDING. MAINTENANCE PERFORMED AN OVERWEIGHT LANDING INSPECTION IAW THE CRJ MX MANUAL AND NO DEFECTS WERE NOTED. MAINTENANCE REMOVED AND REPLACED THE NOSE GEAR PROXIMITY SWITCH BRACKET, WHICH WAS FOUND TO BE BENT. MAINTENANCE ADJUSTED THE PROXIMITY SWITCH AND SWUNG THE GEAR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (M)