N880AS

Part: SENSOR — OUT OF ADJUST (LT MLG) · airframe 34,641 hrs · 32,129 cycles

GEAR DISAGREE, DECLARED EMERGENCY. PROXIMITY SENSOR WAS OUT OF ADJUSTMENT ON THE LT MAIN LANDING UPLOCK. OPS CHECKED GOOD.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 33,090 hrs · 30,535 cycles

EMERGENCY LIGHTS INOPERATIVE. CHARGED THE BATTERY PACKS AND OPS CHECKED EMERGENCY LIGHTS IAW AMM 33-51-05. OPS CHECKED GOOD.

Part: PSEU — FAILED (MLG) · airframe 32,511 hrs · 30,009 cycles

AT 31,000', ENROUTE, RECEIVED AMBER CAUTION PRIX SYSTEM CHANNEL MESSAGE, FOLLWED QRH MANNUALLY EXTENDED GEAR LANDED. ENROUTE, ACFT DIVERTED DUE TO MAINTENANCE EMERGENCY ACTIONS. R & R PSEU IAW AMM 32-61-01, IPC REF32-61-00, ITEM 5, OPS TEST GOOD, IAW THE NATURE OF THE WRITE UP, GEAR SWING REQUIRED.

Part: BUSHING — DETERIORATED (RT MLG TRUNNION) · airframe 32,489 hrs · 29,991 cycles

RT MLG TRUNNION AFT BUSHING AUX BORE HOLE DIAMETER IS OUT OF LIMITS. REMOVED RT MLG AFT TRUNNION LUG TO TO FIRST OVERSIZE IAW ECTC REO 601R-57-21-003. INSTALLED 1ST OVERSIZE BUSHING IN RT MLG AFT TRUNNION IAW ECTC REC 601R-57-21-003 AND GREO 601R-57-21-003, EV B.

Part: BUSHING — DETERIORATED (LT MLG TRUNNION) · airframe 32,489 hrs · 29,991 cycles

LT MLG TRUNNION AFT BUSHING BORE AUXILIARY HOLE DIAMETER IS OUT OF LIMITS. REAMED LT MLG AFT TRUNNION LUG TO FIRST OVERSIZE IAW ECTC REO 601R-57-21-003. INSTALLED 1ST OVRSIZE BUSHING INLT MLG AFT TRUNNION IAW ECTC REO 601R-57-21-003.

Part: BUSHING — DETERIORATED (RT MLG TRUNNION) · airframe 32,489 hrs · 29,991 cycles

RT MLG TRUNNION FWD BUSHING BORE, AFT SPAR, HOLE DIAMETER IS OUT OF LIMITS. REMOVED AND REAMED THE TRUNNION, MLG TRUNNION FWD BUSHING BORE, AFT SPAR, TO 1ST OVERSIZE IAW ECTC REO 601R-57-21-003. INSTALLED 1ST OVERSIZE BUSHING IN THE RT MLG TRUNNION FWD BUSHING BORE, AFT SPAR, IAW ECTC REO 601R-57-21-003 AND REO 601R-57-21-003, REV B.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 32,489 hrs · 29,991 cycles

SEAT TRACK SEGMENT CORRODED AND OUT OF LIMITS ON RBL9 AND BETWEEN FS 559 TO FS 559+86. REMOVED SEAT TRACK SEGEMENTS AT RBL9 BETWEEN FS559-FS559+86 IAW AMM 53-01-11-000-802. INSTALLED SEAT TRACK SEGMENT AT RBL9 BETWEEN FS 559-559+86 IN REF TO AMM 53-01-11-400-802. COMPLIED WITH ECTC REO 601R-53-00-485 FABCRATED SEAT RAIL IAW GREO 601R-53-00-485 REV A.

Part: INTERCOSTAL — CRACKED (BS 621-625) · airframe 32,489 hrs · 29,991 cycles

ANGLE CRACKED BETWEEN FS 621 AND FS 625.30 AT STR 15R. REMOVED DISCREPANT INTERCOSTAL AND INSTALLED SERVICABLE INTERCOSTAL AT FS 621-FS625.3, RBL45.6, IAW SRM 51-40-11, 51-42-21, 51-21-16.

Part: INTERCOSTAL — CRACKED (BS 621-625) · airframe 32,489 hrs · 29,991 cycles

ANGLE CRACKED BETWEEN BS 621 AND 625.30 AT STR 15L. REMOVED DISCREPANT INTERCOSTAL AND INSTALLED SERVICABLE INTERCOSTAL AT FS 621-FS 625.3, LBL45.6, IAW SRM 51-40-11, 51-42-21, 51-21-16.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 32,489 hrs · 29,991 cycles

ANGLE CLIP CRACKED AT FS 280 AND LBL 9; OTBD SIDE. RECEIVED AND COMPLIED WITH REO 601R-53-11-2904. COMPLIED WITH EC/TC REO 601R-53-11-2904 AND ALL STEPS HAVE BEEN DOCUMENTED AND SIGNED FOR ON A NON ROUTINE WORK CARD.

Part: SEAT TRACK — CORRODED (BS 400-409) · airframe 32,489 hrs · 29,991 cycles

RBL9, FLOOR SEAT RAIL SEGMENT BETWEEN FS 400 TO FS 409+128 IS CORRODED OUT OF LIMITS. EVALUATED RBL9, FLOOR SEAT RAIL FS 400-FS 409+128 FOUND TO BE OUT OF LIMITS IAW SRM 53-21-49. REMOVE SEAT RAIL. REMOVED RBL9, SEAT RAIL FS 400-FS 409+128 IAW AMM 53-01-11-000-802. FABRICATED SEAT RAILS IAW GREO 601R-53-00-485, REV A. INSTALLED SEAT RAIL FROM FS 400 TO FS 409+128 AT RBL9 IAW AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 400-409) · airframe 32,489 hrs · 29,991 cycles

LBL 9 SEAT TRACK SEGMENT BETWEEN FS 400 TO FS 409+128 CORRODED OUT OF LIMITS. REMOVED SEAT TRACK IAW AMM 53-01-11-000-802. INSTALLED SEAT TRACK IAW AMM 53-01-11-400-802. FABRICATED SEAT TRACK IAW GREO 601R-53-00-485, REV A.

Part: SEAT TRACK — CORRODED (BS 364-400) · airframe 32,489 hrs · 29,991 cycles

RBL9 FLOOR SEAT RAIL SEGMENT BETWEEN FS 364 TO FS 400 HAS CORROSION IN A FEW SPOTS. EVALUATED RBL9 FLOORS AT RAIL FS 364-400 FOUND TO BE OUT OF LIMITS IAW SRM 53-21-49. REMOVED RBL9 FLOOR SEAT RAIL FS 364-FS 400 IAW AMM 53-01-11-000-802. INSTALLED NEW FABRICATED SEAT RAIL RBL9 FS 364-FS 400 IAW AMM 53-01-11-400-802.

Part: FLOOR SUPPORT — CORRODED (BS 349-367) · airframe 32,489 hrs · 29,991 cycles

CORROSION ON FLOORSILL AT LBL 47 AND BETWEEN FS 349 TO FS 367. BLENDED CORROSION ON FLOOR SILL AT LBL47 BT FS 349 AND FS 367 IAW SRM 51-21-06 AND FOUND TO BE OUT OF LIMITS IAW EC/TC REO 601R-53-00-530. PERFORMED UT THICKNESS INSP IAW BSC NDTM SEC 4.3 MIN REMAINING THK IS .060" ORIG IS .063, REMOVED IS .003", BLENDED AREAS ARE WITHIN ALLOWABLE LIMITS IAW REO 601R-53-00-530. COMPLIED WITH REO 601R-53-21-2722. REPAIRED FLOOR SILL BETWEEN FS 280 TO FS 409+128 IAW REO 601R-53-00-530 REV A. COMPLIED WITH EC/TC REO 601R-53-21-2722.

Part: SEAT TRACK — CORRODED (BS 364-400) · airframe 32,489 hrs · 29,991 cycles

LBL9 FLOOR SEAT RAIL SEGMENT BETWEEN FS 364 TO FS 400 HAS CORROSION AROUND SEVERAL SCREW HEADS, MARKED. EVALUATED LBL9 FLOOR SEAT RAIL FS 364-400 FOUND TO BE OUT OF LIMITS IAW SRM 53-21-49. REMOVED LBL9 FLOOR SEAT RAIL FS 364-FS 400 IAW AMM 53-01-000-802. COMPLIED WITH EC/TC REO 601R-53-00-485. INSTALLED NEW FABRICATED SEAT RAIL AT LBL9 FS 364-FS 400 IAW AMM 53-01-11-400-802.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 32,489 hrs · 29,991 cycles

ANGLE CLIP CRACKED AT FS 280 AND RBL9, INBD SIDE. RECEIVED REO 601R-53-11-2904 AND COMPLIED WITH ALL STEPS OF REO 601R-53-11-2904. COMPLIED WITH EC/TC REO 601R-53-11-2904 AND ALL STEPS HAVE BEEN DOCUMENTED AND SIGNED FOR ON A NON ROUTINE WORK CARD.

Part: DOOR — LACK OF LUBE (EMERGENCY EXIT) · airframe 32,489 hrs · 29,991 cycles

RIGHT EMERGENCY DOOR FAILED PULL TEST 70 LBS. LUBRICATED RT EMERGENCY EXIT DOOR IAW AMM 12-20-52-640-802. PERFORMED PULL TEST OF RT EMERGENCY EXIT DOOR IAW AMM 52-21-00-720-801, STEPS 4.A, 1, 3. PULL TEST GOOD.

Part: SKIN — CRACKED (BS 192) · airframe 32,489 hrs · 29,991 cycles

LT FWD FUSELAGE SKIN CRACKED BELOW AFT TRU DOOR LATCH AT APPROXIMATELY FS 192.00. REMOVED CRACKED DOOR LAND AT FS 192.00 BELOW TRU DOOR LT IAW SRM 51-42-06 AND 51-42-13-00. LOCATED AND DRILLED NEW SERVICEABLE LT DOOR LAND BELOW AFT TRU DOOR AT APPROXIMATELY FS 192.00 IAW SRM 51-40-06-00, 1-40-11-00 AND DWG 600-33052. INSTALLED NEW SERVICEABLE DOOR LAND LT SIDE AT APPROXIMATELY FS 192.00 BELOW TRU DOOR IAW DWG 600-33052 & SRM 51-42-06, 51-42-13-00. RECEIVED AND COMPLIED WITH REO 601R-53-11-29-05 AND EC/TC.

Part: LIGHT — DAMAGED · airframe 31,477 hrs · 29,086 cycles

FLOOR-LEVEL EMERGENCY FLOOD LIGHT AT MAIN ENTRANCE DOOR DAMAGED. R & R FLOOD LIGHT IAW AMM 33-51-19. SYSTEM OPS CHECKED GOOD. NO FURTHER ACTION.

Part: WIRE — MISINSTALLED (EMERGENCY LIGHT) · airframe 30,862 hrs · 28,551 cycles

REF DMIL A595210 FWD CABIN EMERGENCY CEILING LIGHT INOPERATIVE. TROUBLESHOT FWD EMERGENCY CEILING FLOODLIGHT. FOUND WIRES ON FWD EMERGENCY CEILING FLOODLIGHT INCORECTLY INSTALLED. INSTALLED FWD EMERGENCY CEILING FLOODLIGHT IAW AMM 33-51-16 AND WM 33-51-00. OPS CHECK GOOD DMIL CLEARED PLACARD REMOVED.

Part: WIRE — MISINSTALLED (EMERGENCY LIGHTS) · airframe 30,845 hrs · 28,538 cycles

FWD CABIN EMERGENCY CEILING LIGHT IS INOPERATIVE. TROUBLE SHOT FWD EMERGENCY CEILING FLOODLIGHT. FOUND WIRES ON FWD EMERGENCY CEILING FLOODLIGHT INCORRECTLY INSTALLED. INSTALLED FWD EMERGENCY CEILING FLOODLIGHT IAW AMM 33-51-16 AND WM 33-51-00. OPS CHECK GOOD DMIL CLEARED PLACARD REMOVED.

Part: TRUNNION — DAMAGED (HORIZONTAL STAB) · airframe 30,009 hrs · 27,767 cycles

RIGHT TOP AFT HOLE ON HORIZONTAL STABILIZER TRUNNION AND ACFT HORIZONTAL STABILIZER OVERSIZED TO .4125, MAX IS .380. REMOVED MOUNTING HARDWARE FROM HORIZONTAL STA IAW AMM 27-42-01-000-801. BOTTOM PINS AND TRUNNIONS TEMP INSTALLED. INSTALLED MOUNTING HARDWARE, BOTTOM TRUNNIONS FROM H8TA IAW AMM 27-42-01-400-801. C/W BSC REO 601R-55-11-512. REO 601R-55-11-512, REV HAS BEEN ACCOMPLISHED AND ALL STEPS HAVE BEEN DOCUMENTED AND SIGNED FOR ON A NRI WORK CARD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 29,224 hrs · 26,965 cycles

RIGHT FORWARD EXTERIOR EMERGENCY LIGHT INOPERATIVE. R & R THE LAMP IAW AMM 33-51-21. OPS CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 28,355 hrs · 26,122 cycles

F/A FLASHLIGHT INOPERATIVE. R & R FLASHLIGHT IAW AMM 25-61-04. OPS CHECKED GOOD. ACFT OK FOR SERVICE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 28,014 hrs · 25,795 cycles

GALLEY FLOOR EMERGENCY LIGHT EXIT SIGN HAS FIVE BAD BULBS. REMOVED BULBS FROM THE GALLEY EMERGENCY LIGHT FLOOR EXIT SIGN AND REPLACED WITH SERVICEABLE BULBS IAW 33-51-10-400-801.

Part: ANGLE — CORRODED (BS 364) · airframe 28,014 hrs · 25,795 cycles

TWO ANGLES AT FS 364 LBL AND RBL 18 ARE CORRODED. REMOVED DAMAGED ANGLES IAW SRM 51-42-06. FABRICATED AND INSTALLED NEW ANGLES IAW SNIEO 601R31049-S02.

Part: SKIN — BUCKLED (PAX DOOR) · airframe 28,014 hrs · 25,795 cycles

PAX DOOR FWD AND AFT SKIN ARE BUCKLED, COMPLIED WITH REO:601R-52-11-2227.

Part: SKIN — CRACKED (WING) · airframe 28,014 hrs · 25,795 cycles

LEFT FUEL ACCESS HOLE 550HB HAS MULTIPLE INDICATIONS ON INBD, FWD & AFT SIDE 50 PERCENT FSH, FAILED NDT. C/W ECTC EO 600-57-81 C/W IAW REO 601R-57-21-030, REV L.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 28,014 hrs · 25,795 cycles

DURING VISUAL INSPECTION FOR LIGHTNING STRIKE DAMAGE, FOUND BURNED RIVETS. FOUND TO BE SATISFACTORY.

Part: SKIN — CRACKED (RT WING) · airframe 28,014 hrs · 25,795 cycles

RT BOOST PUMP CUTOUT HAS MULTIPLE INDICATIONS ALL AROUND THE VERTICAL & HORIZONTAL LANDING 50 PERCENT FSH FAILED NDT. BLENDED RT WING LOWER SKIN PLANK AT BOOST PUMP LANDING IAW STS EA 26-2014-050.

Part: BEAM — CORRODED (BS 349) · airframe 28,014 hrs · 25,795 cycles

BS 349.00 TRANSVERSE BEAM IS CORRODED OTBD OF RBL 27.00. REO 601R-53-21-2534 REV--HAS BEEN ACCOMPLISHED AND ALL STEPS HAVE BEEN DOCUMENTED AND SIGNED FOR ON A NRI WORK CARD. RII'S HAVE BEEN ACCOMPLISHED IAW GMM 3-3 PROCEDURES PRIOR TO THE ACFT BEING RETURNED TO SERVICE.

Part: BEARING — WORN (RUDDER) · airframe 28,014 hrs · 25,795 cycles

RUDDER UPPER AND LOWER CENTER HINGE BEARINGS HAVE EXCESSIVE PLAY. COMPLIED WITH EC/TC RIL 0602, REPAIR TYPE II: REPLACEMENT OF THE SWAGED BEARING IAW RIL 602, REV E.

Part: STRIKER — DENTED (PAX DOOR SEAL) · airframe 28,014 hrs · 25,795 cycles

PASSENGER DOOR CUT-OUT SEAL STRIKER, UPPER, AT FS 310 IS DAMAGED. C/W BSC REO 601R-53-22-176 REV IAW SRM 51-42-06 AND 51-40-11.

Part: BRACKET — CORRODED (BS 364) · airframe 28,014 hrs · 25,795 cycles

FOUND MAIN AVIONICS DOOR LATCH PIN RECEIVER SUPPORT BRACKET FS 364.00 FRAME SECTOR AT BL 0 TO BE CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00 T/R 53-27, FIG 102, SHEET 2. CORROSION IS ON OVERLAPPING ELEMENTS THRU RADIUS. LOCATED, DRILLED UP & INSTALLED NEW BRACKET IAW SRM 51-40-11.

Part: INTERCOSTAL — CRACKED (BS 625) · airframe 28,014 hrs · 25,795 cycles

FS 625 CRACKED INTERCOSTAL AT STRINGERS 13 & 14L. REMOVED INTERCOSTAL IAW SRM 51-42-21 AND 51-42-06. LOCATED & DRILLED INTERCOSTAL IAW SRM 51-40-11 AND DWG 601-35012. LOCATED NEW FASTENER HOLES TO NEW SERVICEABLE INTERCOSTAL IAW REO 601R-53-61-5265. MAJOR REPAIR. COMPLIED WITH EC/TC REO 601R-53-61-5265 & GREO 601R-53-61-5265 REV-.

Part: DOOR FRAME — CORRODED (SERVICE DOOR) · airframe 28,014 hrs · 25,795 cycles

SERVICE DOOR SURROUND FWD FITTING AND FLOOR EDGE MEMBER ARE CORRODED AT BS 319. DAMAGE TO FLOOR EDGE MEMBER FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00, TR 53-27 AND REQUIRES REPLACEMENT FROM FS 310-319. REMOVED AND LOCATED NEW PART, PN 601R31148-79 IAW SRM 51-40-11 AND DWG 601R31148. REMOVED FWD FLOOR SILL TO FWD FITTING ATTACHMENT CUP IAW SRM 51-42-06. INSTALLED CLIP IAW SRM 51-42-06. REMOVED JOINT BRACKET, CORROSION OUT OF LIMITS IAW SRM 53-00-00, TR 53-27. REQUIRES REPLACEMENT. REMOVED IAW SRM 51-42-21. LOCATED AND DRILLED UP NEW JOINT BRACKET, PN 601R38335-1 IAW DWG 601R38335 AND SRM 51-40-11. UPON FURTHER INVESTIGATION FOUND CORROSION ON GALLEY SUPPORT ANGLE TO BE OUT OF LIMITS IAW SRM 53-00-00, TR 53-27 AND REQUIRES REPLACEMENT. LOCATED AND DRILLED UP NEW ANGLE PN 601R38669-49 IAW DWG 601R38669 AND SRM 51-40-11. INSTALLED JOINT BRACKET, EDGE MEMBER AND GALLEY SUPPORT ANGLE IAW SRM 51-12-06, 51-42-21.

Part: INTERCOSTAL — CORRODED (BS 364) · airframe 28,014 hrs · 25,795 cycles

BS 364 INTERCOSTAL BETWEEN 26L & 26R CORRODED. R & R INTERCOSTAL IAW SRM 51-42-06 AND 51-42-21.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 28,014 hrs · 25,795 cycles

SERVICE DOOR SILL IS CORRODED. REMOVED SERVICE DOOR SILL ANGLE IAW SRM 51-42-21. LOCATED AND DRILLED UP NEW SERVICE DOOR SILL ANGLE, PN 601R38303-253 IAW SRM 51-40-11 AND DWG 601R38303. INSTALLED SILL ANGLE IAW SRM 51-42-06 AND SRM 51-42-11.

Part: FITTING — CRACKED (BS 460) · airframe 28,014 hrs · 25,795 cycles

BS 460, FITTING ON OTBD SIDE OF RBL 9 IS CRACKED .5". REMOVED THE SUPPORT FITTING IAW SRM 51-42-21 AND 51-42-06. LOCATED, DRILLED AND INSTALLED NEW SERVICEABLE SUPPORT FITTING IAW SRM 51-40-11, 51-42-06 AND 51-42-21. MAJOR REPAIR.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 27,970 hrs · 25,758 cycles

CARGO TRACK CORRODED LBL 9. R & R CARGO TRACK IAW AMM 20-21-00-910-801 AND SRM 51-40-11.

Part: FRAME — CORRODED (BS 364) · airframe 28,014 hrs · 25,795 cycles

FRAME AT BS 364 S23L - 23R IS CORRODED. R & R FRAME SUPPORT ANGLE FROM AFT SIDE OFFS 364.0 IAW SRM 51-42-06. R & R INTERCOSTALS AT LBL/RBL 18.0 BETWEEN FS 349.0-FS 364.0 IAW SRM 51-42-06. R & R FRAME SECTOR AND SPLICE ANGLE FROM FS 364.0 BETWEEN STRINGERS 24L AND 24R IAW SRM 51-42-06.

Part: ISOLATOR — BROKEN (BS 621 BULKHEAD) · airframe 28,014 hrs · 25,795 cycles

BS 621 BULKHEAD FWD FACE HAS A BROKEN ISOLATOR. R & R BROKEN ISOLATOR IAW SRM 51-42-06.

Part: STRINGER CLIP — CORRODED (BS 280) · airframe 28,014 hrs · 25,795 cycles

FS 280, STRINGER CLIP 3L CRACKED. REMOVED FS 280 STRINGER CLIP IAW SRM 51-42-06 AND SRM 51-42-21. LOCATED, DRILLED AND INSTALLED NEW STRINGER CLIP IAW SRM 51-42-06 AND SRM 51-42-21.

Part: ANGLE — CRACKED (BS 484) · airframe 28,014 hrs · 25,795 cycles

RT 484, ANGLE AT RBL 27 IS CRACKED .250L. REMOVED CRACKED ANGLE AND LOCATED, DRILLED & INSTALLED NEW ANGLE IAW SRM 51-40-11, 51-42-06 AND 51-42-21.

Part: BEARING — WORN (LT ELEVATOR) · airframe 27,985 hrs · 25,771 cycles

LEFT ELEVATOR FAILS BEARING BACKLASH FOR HYD SYS FOUND TO BE OUT OF LIMITS REPLACED BEARING IAW EC/TC RIL 0183 AND RIL 0183, REV B.

Part: BEARING — WORN (RT ELEVATOR) · airframe 27,985 hrs · 25,771 cycles

RIGHT ELEVATOR FAILS BEARING BACKLASH FOR HYD SYS FOUND TO BE OUT OF LIMITS. REPLACED BEARINGS IAW AMM 20-26-00-910-807.

Part: DOOR SILL — CORRODED (CARGO BAY) · airframe 28,014 hrs · 25,795 cycles

CARGO BAY DOOR SILL HAS CORROSION AROUND NUTPLATE HOLES. REMOVED CORROSION IAW REO 601R-53-00-526. FOUND TO BE WITHIN LIMITS WITH MAX MATERIAL REMOVED .004, MAX ALLOWABLE .010. COMPLIED WITH EC/TC REO 601R-53-00-526 AND GREO 601R-53-00-526, REV.

Part: SKIN — CORRODED (EMERGENCY DOOR) · airframe 27,985 hrs · 25,771 cycles

RIGHT OVERWING EMERGENCY EXIT DOOR INNER SKIN CORRODED INSIDE BOTTOM OF DOOR. REMOVED 2 CORRODED ANGLES IAW SRM 51-42-06. INSTALLED 2 NEW ANGLES, PN 601R31123-108 AND 107 IAW DWG 601R31123, REV H AND SRM 51-42-06.

Part: SKIN — CHAFED (LT AILERON) · airframe 27,984 hrs · 25,770 cycles

LEFT AILERON UPPER L/E IS CHAFED AT MULTIPLE LOCATIONS. REMOVED DAMAGED UPPER L/E SKIN FROM LT AILERON IAW SRM 51-42-06, REV 32. FITTED, DRILLED, AND INSTALLED NEW UPPER L/E SKIN IAW SRM 51-40-11, 51-42-06, 51-42-13.

Part: SKIN — CRACKED (LT WING) · airframe 27,985 hrs · 25,771 cycles

LT LOWER WING PLANK CRACKED APP 1" AT 148.019. COMPLIED WITH ECTC REO 601R-57-21-130 AND GREO 601R-57-21-130, REV K.

Part: BULKHEAD — CHAFED · airframe 27,984 hrs · 25,770 cycles

FOUND REAR PRESSURE BULKHEAD WEB HAS THREE CHAFED AREAS APPROX .200 INCH LONG BY .200 INCH WIDE .003 INCH DEEP AT RBL 18.00, RBL 27.50 AND RBL 36.20 WL 105. COMPLIED WITH ECTC REO 601R-53-61-2155.

Part: BRACKET — CRACKED (BS 449) · airframe 27,984 hrs · 25,770 cycles

LEFT WING TO FUSELAGE FAIRING BRACKET AT BS 449.85 IS CRACKED. R & R THE FAIRING BRACKET WITH NEW IAW SRM 51-40-11, 51-42-06 AND 51-45-00.

Part: BULKHEAD — CRACKED · airframe 27,984 hrs · 25,770 cycles

FOUND REAR PRESSURE BULKHEAD WEB HAS CRACK INDICATIONS NOTED AT LBL 27.50, WL 130, APPROXIMATELY .2 INCHES IN LENGTH, 90 PERCENT FSH FAILED NDT INSPECTION. COMPLIED WITH EC/TC REO: 601R-53-61-1541.

Part: BRACKET — CRACKED (BS 449-461) · airframe 27,984 hrs · 25,770 cycles

RT WING TO FUSELAGE FAIRING BRACKET AT BS 449.85 - 461 ARE CRACKED. R & R RT WING TO FUSELAGE FAIRING BRACKET IAW SRM 51-42-06, REV 32.

Part: ARM — GOUGED (FLAP HINGE) · airframe 27,984 hrs · 25,770 cycles

FOUND GOUGE ON RT OTBD FLAP CENTER HINGE ARM WS 220.00 BOTTOM INBD MOUNTING LUG. BLENDED GOUGE IAW EA:26-2014-048, REV. ORIGINAL. PERFORMED SHOT PEENING ON THE REQUIRED SURFACE RT OTBD FLAP CENTER HINGE LUG IAW EA 26-2014-048, STEP 3.

Part: DETECTOR — FAILED · airframe 27,173 hrs · 24,902 cycles

DISPLAY COOL MESSAGE IN FLIGHT. COMPLIED WITH QRH. MESSAGE WOULD NOT EXTINGUISH. ACFT RETURNED TO DEPARTURE. INSPECTED DUCT WORK TO FANS. NO DEFECTS NOTED. R & R DIPSLAY COOLING FILTER IAW AMM 21-24-15. NO DEFECTS NOTED. R & R LOW FLOW DETECTOR IAW AMM 21-24-07. OPS CHECKED GOOD. ACFT OK FOR SERVICE.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 26,593 hrs · 24,378 cycles

EMERGENCY LIGHT FWD OF THE PAX DOOR INOP. REPLACED LAMP IAW AMM 33-51-21. OPS CHECKED GOOD.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 24,241 hrs · 22,042 cycles

WARDROBE AND GALLEY EMERGENCY LIGHTS ARE INOPERATIVE. TROUBLESHOT EMERGENCY LIGHTS IAW WDM 33-51-00. FOUND FOUR QUICK DISCONNECT CONNECTORS DISCONNECTED. SWAPED AT LT FWD FLOOR LEVEL EXIST FLOODLIGHT (DS9LY) AND FWD EXIT SIGN (DS10LY). CONNECTED IS9LY AND DS10LY IAW WDM 33-51-00. OPS TEST OF THE WARDROBE AND GALLEY LIGHTS ARE GOOD IAW AMM TASK 33-51-00-710-801.

Part: ATTACH FITTING — CORRODED (BS 320.1-338) · airframe 24,241 hrs · 22,042 cycles

PAX DOOR UPPER HINGE SECTION AT FS 320.10 & FS 338.00 BOTH FWD 7 AFT CLEAT CORRODED BEYOND LIMITS. REMOVED CORRODED CLEAT. FITTED, DRILLED & INSTALLED NEW CLEAT IAW SRM 51-42-06 & 51-42-13.

Part: ATTACH ANGLE — CRACKED (BS 635.3) · airframe 24,241 hrs · 22,042 cycles

ATTACH ANGLE ON FWD OF ENGINE SUPPORT BEAM AT FS 635.30 BL, RBL 27.50 HAS A .3" CRACK IN LOWER CORNER. FAILED VISUAL NDT INSPECTION. REMOVED CRACKED ATTACH ANGEL FWD OF ENGINE SUPPORT BEAM IAW SRM 51-42-06 AND 51-42-21. REPLACED CRACKED ATTACH ANGLE IAW SRM 51-42-06 AND 51-42-21.

Part: ATTACH ANGLE — CRACKED (BS 635.3) · airframe 24,241 hrs · 22,042 cycles

CLIP, ON FWD OF ENGINE SUPPORT BEAM AT FS 635.30 BL, RBL 18.00 HAS A .5" CRACK IN LOWER CORNER. FAILED VISUAL NDT INSPECTION. REMOVED CRACKED CLIP AT FS 635.30 BL, RBL 18.00 IAW SRM 51-42-21. REPLACED CRACKED WITH NEW CLIP IAW SRM 51-42-21.

Part: ATTACH BRACKET — CRACKED (BS 621) · airframe 24,241 hrs · 22,042 cycles

CARGO BAY, AFT BRACKET AT FS 621 CRACKED WHERE BRACKET ATTACHES TO CROSSMEMBER CARGO DOOR. R & R CARGO BAY AFT BRACKET IAW SRM 51-42-21-00.

Part: ANGLE — CORRODED (BS 280) · airframe 24,241 hrs · 22,042 cycles

FS 280.00 BETWEEN LBL 9.00 TO RBL 9.00, FWD AND AFT J ANGLES ARE CORRODED. REMOVED ANGLE IAW SRM 51-42-06, 51-42-21. LOCATED NEW ANGLE IAW SRM 51-40-11. INSTALLED NEW ANGLE IAW SRM 51-42-06 AND 51-42-21.

Part: SEAT TRACK — CORRODED (BS 409) · airframe 24,241 hrs · 22,042 cycles

IN PASSENGER COMPARTMENT, RT SIDE SEAT TRACK AFT OF FS 409+128 IS CORRODED SEVERAL LOCATIONS. COMPLIED WITH EC/TC REO 601R-53-00-055 AND REO 601R-53-00-055, REV A.

Part: SEAT TRACK — CORRODED (BS 409-559) · airframe 24,241 hrs · 22,042 cycles

IN PASSENGER COMPARTMENT SEAT TRACK, FS 409+112 TO 559, LBL 9.00 IS CORRODED. SEAT TRACK FOUND TO BE OUT OF LIMITS IAW SRM 51-21-49. DRILLED AND COUNTERSUNK NEW SERVICEABLE SEAT TRACK IAW SRM 51-40-11. REMOVED CORRODED SEAT TRACK IAW AMM 53-01-11-000-802. INSTALLED NEW SERVICEABLE SEAT TRACK IAW AMM 53-01-11-400-802.

Part: FLOOR SUPPORT — CORRODED (BS 559) · airframe 24,241 hrs · 22,042 cycles

PASSENGER COMPARTMENT AT FS 559.00, LBL 36.00 FLOOR SUPPORT FINGER WEB IS CORRODED.

Part: SEAT TRACK — CORRODED (BS 409) · airframe 24,241 hrs · 22,042 cycles

IN PASSENGER COMPARTMENT RT SIDE SEAT TRACK AFT OF FS 409+128 IS CORRODED AT SEVERAL LOCATIONS. COMPLIED WITH EC/TC REO 601R-53-00-55 AND REO 601R-53-00-055, REV A.

Part: FLOOR SUPPORT — CORRODED (BS 424-559) · airframe 24,241 hrs · 22,042 cycles

IN PASSENGER COMPARTMENT FLOOR SUPPORT BETWEEN FS 424.00 TO FS 559.00 RBL 42.00, AROUND FLOORBOARD ATTACHMENT HOLES, FLOOR SUPPORT CORRODED. COMPLIED WITH ECTC REO 601R-53-41-666 AND REO 601R-53-41-666, REV B.

Part: SEAT TRACK — CORRODED (BS 364-399) · airframe 24,241 hrs · 22,042 cycles

IN PASSENGER COMPARTMENT LBL 9.00 BETWEEN FS 364 TO FS 399, SEAT TRACK CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 51-21-49. REMOVED CORRODED SEAT TRACK & INSTALLED NEW SERVICEABLE SEAT TRACK IAW AMM 53-01-11-000-802 & 53-01-11-400-802.

Part: FLOOR SUPPORT — CRACKED (BS 280) · airframe 24,241 hrs · 22,042 cycles

IN PASSENGER COMPARTMENT, FLOOR STRUCTURE AT FS 280.00 RBL 9.00 OTBD ATTACHMENT ANGLE IS CRACKED. REPAIRED IAW REO 601R-53-11-926, REV B.

Part: SEAT TRACK — CORRODED (BS 396-409) · airframe 24,241 hrs · 22,042 cycles

IN PASSENGER COMPARTMENT, LBL 9.00 FS 396 TO 409+120, SEAT TRACK IS CORRODED. SEAT TRACK FOUND TO BE OUT OF LIMITS IAW SRM 51-21-49. REMOVED CORRODED SEAT TRACK IAW AMM 53-01-11-000-802. LOCATED AND DRILLED NEW SEAT TRACK IAW SRM 51-40-11. INSTALLED IAW AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 409) · airframe 24,241 hrs · 22,042 cycles

IN PASSENGER COMPARTMENT, RBL 9 BETWEEN FS 396 TO 409+120, SEAT TRACK IS CORRODED AT BS 409. SEAT TRACK FOUND TO BE OUT OF LIMITS IAW SRM 51-21-49. REMOVED CORRODED SEAT TRACK IAW AMM 53-01-11-000-802 & LOCATED & DRILLED NEW SERVICEABLE TRACK IAW SRM 51-40-11. INSTALLED SEAT TRACK IAW AMM 53-01-11-400-802.

Part: ANGLE — CRACKED (BS 484) · airframe 24,241 hrs · 22,042 cycles

PASSENGER COMPARTMENT FLOOR STRUCTURE AT FS 484.00, LBL 27.00, ATTACHMENT ANGLE IS CRACKED. REMOVED ANGLE IAW SRM 51-42-21. REPLACED CRACKED ANGLE AT FS 494.00, LBL 27.00 IAW SRM 51-42-21 AND SRM 51-42-06 PN 601R31171-17. T

Part: SEAT TRACK — CORRODED (BS 399) · airframe 24,241 hrs · 22,042 cycles

PASSENGER COMPARTMENT LT SIDE WALL SEAT TRACK AT FS 399.00 IS CORRODED. REPAIRED LT SIDEWALL SEAT TRACK IAW REO 601R-53-00-55. ECTC REQUIRED.

Part: SEAT TRACK — CORRODED (BS 409) · airframe 24,241 hrs · 22,042 cycles

IN PASSENGER COMPARTMENT RT SIDEWALL SEAT TRACK AT FS 409+8 CORRODED. COMPLIED WITH EC/TC REO 601R-53-00-055 AND REO 601R-53-00-055. RII FOUND TO BE SATISFACTORY.

Part: WEB — CORRODED (BS 559) · airframe 24,241 hrs · 22,042 cycles

IN PASSENGER COMPARTMENT AT FS 559.00, RBL 42.900 FLOOR SUPPORT FINGER WEB IS CORRODED.

Part: SEAT TRACK — CORRODED (BS 364-399) · airframe 24,241 hrs · 22,042 cycles

IN PASSENGER COMPARTMENT, RBL 9.900 BETWEEN FS 364 TO 399, SEAT TRACK IS CORRODED. SEAT TRACK FOUND TO BE OUT OF LIMITS IAW SRM 51-21-49. REMOVED SEAT TRACK AND INSTALLED NEW SERVICEABLE SEAT TRACK IAW AMM 53-01-11-000-802 & 53-01-11-400-802.

Part: FRAME — CRACKED (BS 718) · airframe 24,241 hrs · 22,042 cycles

FS 718 FRAME, CRACKED JUST BELOW STRINGER 11 RT. REMOVED DAMAGE IAW REO 601R-53-61-193. PERFORMED LPI CUT LINE IAW NDTM 51-10-08. NO INDICATIONS NOTED.

Part: SEAT TRACK — CORRODED (BS 409-559) · airframe 24,241 hrs · 22,042 cycles

PASSENGER COMPARTMENT SEAT TRACK AT FS 409+112 TO 559, RBL 9.00 IS CORRODED. SEAT TRACK FOUND TO BE OUT OF LIMITS IAW SRM 51-21-49. DRILLED AND COUNTERSUNK NEW SERVICEABLE SEAT TRACK IAW SRM 51-40-11. REMOVED SEAT TRACK IAW AMM 53-01-11-000-802. INSTALLED NEW SERVICEABLE SEAT TRACK IAW AMM 53-01-11-400-802.

Part: ANGLE — CRACKED (BS 625) · airframe 24,241 hrs · 22,042 cycles

FS 625 OBLIQUE LT CRACKED. REMOVED CRACKED OBLIQUE ANGLE COMMON TO LT SIDE FS 625 AND REPLACED IT WITH NEW PART IAW SRM 51-42-21.

Part: CHARGER — UNSERVICEABLE (EMERGENCY LIGHTS) · airframe 24,175 hrs · 21,968 cycles

ALL EMERGENCY LIGHTS ON NR 2 BATTERY INOPERATIVE. R & R NR 2 BATTERY AND BATTERY CHARGER IAW AMM 33-51-04 AND AMM 33-51-05, OPS CHECKED GOOD.

Part: POTENTIOMETER — OUT OF ADJUST (TE FLAPS) · airframe 24,037 hrs · 21,810 cycles

ON ARRIVAL, SELECTED FLAPS TO 8, FLAPS DID NOT MOVE. ACFT RETURNED TO DEPARTURE, EMERGENCY DECLARED. PERFORMED POTENTIOMETER ADJUSTMENT OF THE FECU IAW AMM 27-51-10-830-008. OPS CHECKED GOOD. NO FURTHER DEFECTS NOTED AND R & R RT FLAP BPSU IAW 27-51-10. OPS AND RIG CHECKED GOOD. NO FURTHER DEFECTS NOTED.

Part: FLAP SYSTEM — FAILED (TE FLAPS) · airframe 23,869 hrs · 21,609 cycles

FLAPS FAIL CAUTION MESSAGE- FLAPS FAILED AT 0 DEGREES. EMERGENCY DECLARED, COMPLIED WITH AD 2009-06-12. NO FURTHER DEFECT NOTED.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 23,762 hrs · 21,488 cycles

NR 8 EXTERIOR EMERGENCY LIGHT INOPERATIVE. RELAMPED NR 8 EXTERIOR EMERGENCY LIGHT IAW AMM 33-51-21. OPS CHECKED GOOD.

Part: LATCH — MALFUNCTIONED (PAX DOOR) · airframe 22,993 hrs · 20,617 cycles

DESCENDING THROUGH FL180, WE HAD A PASSENGER DOOR WARNING MESSAGE. RAN QRH WE UNPRESSURIZED THE ACFT. DOOR HANDEL POPPED UP, WE DID NOT ATTEMPT TO RESTOW. GREEN INDICATORS WENT RED (EMERGENCY DECLARED AS A PRECAUTION) REPAIRED INNER DOOR LATCH MECHANISM. OPS CHECKS GOOD IAW AMM 52-11-25. (SDR CLOSED)

Part: LIGHT — BROKEN (CABIN) · airframe 22,737 hrs · 20,350 cycles

MAIN ENTRANCE EMERGENCY LIGHT ASSY BROKEN. R & R MAIN ENTRANCE EMERGENCY LIGHT ASSY IAW AMM 33-51-01.

Part: WARNING SYSTEM — FALSE ACTIVATION (ENGINE OIL PRESS) · airframe 21,981 hrs · 19,513 cycles

LT ENG OIL PRESSURE MESSAGE JUST PRIOR TO LANDING WITH SMOKE REPORTED TRAILING FROM THE ACFT BY THE TOWER. (EMERGENCY DECLARED AND FIRE TRUCKS ROLLED AS A PRECAUTION) PERFORMED OPS CHECK AT LOW POWER AND HIGH POWER ENGINE RUN, OPS CHECK GOOD IAW AMM 71-00-00, ACFT OK FOR SERVICE. SERVICED ENGINE OIL AFTER ENGINE RUN IAW AMM 12-13-79.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 21,888 hrs · 19,414 cycles

FUSELAGE EXTERNAL EMERGENCY LIGHT IN FRONT OF LEFT EMERGENCY EXIT INOP. RELAMPED LEFT NR 3 EXTERNAL EMERGENCY LIGHT IAW AMM 33-51-21, OP'S CHECK GOOD. RELAMPED LEFT NR 3 EXTERNAL EMERGENCY LIGHT IAW AMM 33-51-21, OP'S CHECK GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 20,475 hrs · 17,791 cycles

NR 1 EMERGENCY LIGHT FWD OF PAX DOOR INOP. RELAMPED NR 1 EXTERIOR EMERGENCY LIGHT IAW AMM 33-51-21, OPS CHECK GOOD. RELAMPED NR 1 EXTERIOR EMERGENCY LIGHT IAW AMM 33-51-21, OPS CHECK GOOD. (CLOSED)

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 19,646 hrs · 16,858 cycles

JOB 8760611 OPERATION 412 / PNL 232DZ EXIT SIGN HSG AND LENS COVER CRACKED. R & R EXIT SIGN HSG AND LENS COVER ON PNL 232DZ IAW MM 33-51-13-000-801 AND 33-51-13-400-801. OPS CHECK DUE. OPS CHECK OF THE EMERGENCY LIGHTS GOOD IAW AMM 33-51-00-710-801.

Part: INTERCOSTAL — CORRODED (BS 333-349 S25R) · airframe 19,626 hrs · 16,833 cycles

INTERCOSTAL BETWEEN FS 333.0 AND 349.0 AT STR 25R CORRODED. REMOVED AND REPLACED INTERCOSTAL AT STR 25R IAW SRM 51-42-06 STEPS 9,10 & 11.

Part: FLOORBEAM — CRACKED (BS 605) · airframe 19,626 hrs · 16,833 cycles

WHILE REPLACING THE CARGO FLOOR FILLPLATE ON THE LT SIDE FS 564-621, FOUND THE FS 605 FLOORBEAM TO BE CRACKED, DENTED, GOUGED AND THE HOLE IS ELONGATED AT LBL42. THE DAMAGE IS ALL AROUND ONE HOLE. REPAIR TO TRAVERSE BEAM COMPLETED IAW REO 601R-53-61-3542 AND MEETS WITH ALL ITS REQUIREMENTS.

Part: FLOORBEAM — CRACKED (BS 484) · airframe 19,626 hrs · 16,833 cycles

FS 484.00 RBL 27 OTBD FLOOR SUPPORT ANGLE CRACKED PREVIOUS REPAIRED ANGLE. REPAIR TO THE INTERCOSTAL 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: FRAME — CORRODED (BS 349 S26L/R) · airframe 19,626 hrs · 16,833 cycles

CORROSION ON FS 349.00 FRAME TO ATTACHMENT FLANGE BETWEEN STR 26L - STR 26R. (3 PLACES). REMOVED FRAME IAW SRM 51-42-06 STEPS A, B1 THROUGH 6 AND SRM 51-42-21 STEPS 11A1 AND B1. LOCATED AND DRILLED NEW FRAME SECTOR IAW AMM 51-42-06. INSTALLED NEW FRAME SECTOR P/N 601R3200569 IAW SRM 51-42-06 STEP 1,2,5,8, 9 & 10 AND SRM 51-42-21 STEP 1 THRU 6, 9 AND 10 IAW SRM 51-42-06 STEPS 1,4,5,7,8-10.

Part: FILLER — CRACKED (BS 589-615) · airframe 19,626 hrs · 16,833 cycles

AFT FILLER STRIP LBL 27.0, FS 589.0 TO FS 615.00 CRACKED IN NUMEROUS PLACES. SEAT TRACK FILLER STRIP. R & R FILLER STRIP AT LBL 27.0 FS 589.0 TO 615.0 IAW SRM 51-41-00.

Part: CARGO TRACK — CORRODED (BS 559) · airframe 19,626 hrs · 16,833 cycles

CARGO SEAT TRACK SEGMENT LBL 9.0 F.S. 559+84 TO F.S. 559+96 IS CORRODED. REMOVED CORRODED CARGO SEAT TRACK SEGMENT AT LBL 9.0 FS 559+84 TO F.S. 559+96. REPLACED WITH NEW PART IAW SRM 51-40-11 AND AMM 53-01-11-000-802 AND 53-01-11-400-802.

Part: CARGO TRACK — CORRODED (BS 614-618) · airframe 19,626 hrs · 16,833 cycles

CARGO SEAT TRACK LBL 9.0 F.S. 614.0 TO 618.0 (APPROX) IS CORRODED. REMOVED CORRODED CARGO SEAT TRACK SEGMENT AT LBL 9.0 F.S. 614.0 TO FS 618.0. REPLACED WITH NEW PART IAW SRM 51-40-11 AND AMM 53-01-11-000-802 AND 53-01-11-400-802.

Part: FLOOR SUPPORT — CORRODED (BS 589-621) · airframe 19,626 hrs · 16,833 cycles

CARGO FLOORBEAM CAP LBL 27.0 F.S. 589.0 TO F.S. 621.0 CORRODED AROUND NUTPLATE HOLES. REMOVED PLASTIC GAP STRIP. REMOVED BOLTS FROM ELEVATOR PULLEY ASSY MOUNT. REMOVED FLOORBEAM CAP IAW SRM 51-42-06, STEP 11 AND SRM 51-42-21, STEP 11. LOCATED, DRILLED & INSTALLED CARGO FLOORBEAM CAP IAW REO 601R-53-61-3534. REINSTALLED ELEVATOR CABLE PULLEY BRACKET ASSY IAW SRM 51-41-00. GAP STRIP INSTALLED IAW SRM 51-41-00. C/W EC/TC REO 601R-53-61-3534, REV --DATED 2/14/10. OPS TEST OF ELEV CONTROL SYS GOOD IAW MM 27-31-00-718-801.

Part: FRAME — CORRODED (BS 319.7) · airframe 19,626 hrs · 16,833 cycles

FUSELAGE FRAME HAS CORROSION AT FS 319.7 STR 27. REMOVED 9 EA RIVETS FOR ACCESS TO CORROSION AND BLENDED (APPROX .001-.002) FROM FRAME AT FS 319.7 STR 27 TO REMOVE CORROSION IAW SRM 51-42-06 & 51-21-06 STEP 3E. INSTALLED RIVETS 9 EA AND TREATED, PRIMED, AND PAINTED BLENDED AREA AT FS 319.7, STR 27 IAW SRM 51-42-06, 51-21-11, 51-25-06, AND 51-25-16. PAINTED RIVET HEADS, IAW SRM 51-25-01. PEFORMED PRESSURE LEAK CHECK OF FUSELAGE AT FS 319.7 STR 27 IAW AMM TASK 21-32-00-863-801. NO LEAKS NOTED.

Part: CARGO TRACK — CORRODED (BS 559) · airframe 19,626 hrs · 16,833 cycles

CARGO SEAT TRACK SEGMENT RBL 27.0 FS 559+80 TO 559+96 IS CORRODED. REMOVED CORRODED SEAT TRACK SEGMENT AT RBL 27, FS 559+80 IAW SRM 51-41-02. DRILLED NEW SEAT TRACK IAW SRM 51-40-11. INSTALLED NEW SEAT TRACK IAW SRM 51-41-02 AND AMM TASK 20-21-00-910-801.

Part: ANCHOR FITTING — CORRODED (FUSELAGE) · airframe 19,626 hrs · 16,833 cycles

CARGO BAY ANCHOR FITTINGS AT LBL 27.0, AND AT LBL 9.0 ARE CORRODED. R & R 5EA ANCHOR FITTINGS IN THE CARGO BAY WITH NEW PARTS IAW AMM 20-21-00-910-801.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 19,626 hrs · 16,833 cycles

CARGO SEAT TRACK SEGMENTS LBL 27.0 FS 559+80 TO FS 559+96 IS CORRODED. REMOVED CORRODED CARGO SEAT TRACK SEGMENT AT LBL 27.0 FS 559+80 TO FS 559+96. REPLACED WITH NEW PART IAW SRM 51-40-11 AND AMM 53-01-11-000-802 AND 53-01-11-400-802.

Part: FRAME — CORRODED (BS 333) · airframe 19,626 hrs · 16,833 cycles

FUSELAGE FRAME HAS CORROSION FS 333.0 STR 26L TO STR 27. REMOVED FUSELAGE FRAME AT FS 333.00 STR 23L-23R IAW SRM 51-42-06 & 51-42-21. NEW FRAME SECTOR REQUIRES LOCATED, DRILLED, AND INSTALLED. NEW FRAME SECTOR IS LOCATED AND DRILLED IAW 51-42-06 STEP 7 A & B AND 51-42-21 STEP 5 A, B, & C. NEW FRAME SECTOR REQUIRES INSTALL. NEW FRAME SECTOR AT FS 333.0 STR 23L-23R INSTALLED IAW SRM 51-42-06 AND 51-42-21. REQUIRES PAINT. PAINTED REPAIRED AREA IAW SRM 51-25-01.

Part: CARGO TRACK — CORRODED (BS 559-567) · airframe 19,626 hrs · 16,833 cycles

CARGO SEAT TRACK SEGMENT LBL 9.0, F.S. 559+95 TO F.S. 567 IS CORRODED. REMOVED CORRODED CARGO SEAT TRACK AT LBL 9, FS 559+95 IAW SRM 51-41-02. DRILLED NEW SEAT TRACK IAW SRM 51-40-11. INSTALLED NEW SEAT TRACK IAW SRM 51-41-02 AND AMM TASK 20-21-00-910-801.

Part: FLOORBEAM — CRACKED (BS 460) · airframe 19,626 hrs · 16,833 cycles

FS 460, LBL 9.0 OTBD SIDE OF FLOORBEAM FITTINGS IS CRACKED, APPROX 1.25" IN LENGTH. REMOVED FITTING IAW SRM 51-42-21. DISCONNECTED THE LARGE WIRE BUNDLE CLAMPS TO FACILITATE ACCESS PANEL REMOVAL IAW SRM 51-41-02. REMOVED ADEL CLAMPS FWD AND AFT FITTING TO FACILITATE FITTING REMOVAL. REMOVED FLOOR PANEL NUTPLATE FWD OF FITTING IAW SRM 51-42-10 FOR FITTING REMOVAL. LOCATED & DRILLED NEW FITTING IAW SRM 51-40-11 & INSTALLED FITTING IAW SRM 51-42-21. INSTALLED ACCESS PLATES/PANELS & WIRE BUNDLE CLAMPS & ADEL CLAMPS IAW SRM 51-41-02 & INSTALLED 1 NUTPLATE IAW SRM 51-42-06.

Part: CARGO TRACK — CORRODED (BS 559) · airframe 19,626 hrs · 16,833 cycles

CARGO SEAT TRACK SEGMENT RBL 9.0 FS 559+84 TO 559+96 IS CORRODED. REMOVED CORRODED CARGO SEAT TRACK SEGMENT AT RBL 9.0 FS 559+84 TO FS 559+96. REPLACED WITH NEW PART IAW SRM 51-40-11 AND AMM 53-01-11-000-802 AND 53-01-11-400-802.

Part: CARGO TRACK — CORRODED (BS 559-567) · airframe 19,626 hrs · 16,833 cycles

CARGO SEAT TRACK SEGMENT RBL 9.0 F.S. 559+95 TO F.S. 567.0 IS CORRODED. REMOVED CARGO SEAT TRACK IAW SRM 51-41-02. LOCATED & DRILLED NEW SEAT TRACK IAW SRM 51-40-11. INSTALLED NEW SEAT TRACK IAW AMM 20-21-00-910-801.

Part: POST — CRACKED (BS 409) · airframe 19,626 hrs · 16,833 cycles

FS 409.0+128.0 VERTICAL POST AT LBL 18.00 CHANNEL HAS A 50 PERCENT FSH HFEC INDICATION NOTED APPROX 0.1" LONG IN AFT RADIUS AT THE UPPER JOGGLE. AREA MARKED ON ACFT. FAILS NDT INSP AT THIS TIME. REMOVED VERTICAL POST ASSY IAW SRM 51-42-06, PAR 11. REPLACE OTBD POST HALF AND REINSTALL POST ASSY. LOCATED & DRILLED NEW OTBD CHANNEL IAW SRM 51-40-11 & SHOT THE HALVES OF POST ASSY TOGETHER IAW SRM 51-42-06. INSTALLED VERTICAL POST ASSY IAW SRM 51-42-06, STEP 9 AND REO 601R-53-41-889. COMPLIED WITH EC/TC REO 601R-53-41-779 AND MET ALL THE REQUIREMENTS OF REO 601R-53-41-889. PAINTED REPAIRED AREA IAW SRM 51-25-16. APPLIED CORROSION INHIBITOR TO REPAIRED AREA IAW SRM 51-21-11.

Part: POST — CRACKED (BS 409) · airframe 19,626 hrs · 16,833 cycles

FS 409.0+128 VERTICAL POST AT RBL 18.00 INBD AND OTBD C-CHANNELS HAVE 50 PERCENT FSH INDICATIONS APPROX .01" LONG NOTED IN AFT RADIUS AT UPPER JOGGLES. AREAS MARKED ON ACFT. FAILS NDT INSP AT THIS TIME. REMOVED POST IAW SRM 51-42-06 11 A & B. REMOVED SIX CLAMPS FOR POST REMOVAL IAW SRM 51-41-02. REINSTALL POST. MET ALL THE REQUIREMENTS OF REO 601R-53-41-889. REINSTALLED SERVICEABLE CLAMPS THAT WERE REMOVED FOR ACCESS, IAW SRM 51-41-02. C/W EC/TC REO 601R-53-41-889 AND MET ALL THE REQUIREMENTS OF REO 601R-53-41-889.

Part: BULKHEAD — CRACKED (BS 559) · airframe 19,626 hrs · 16,833 cycles

FS 559.00 PRESSURE BULKHEAD WEB (RHS) HAS 3 INDICATIONS NOTED AS LISTED: 60 PERCENT FSH, 0.5" LONG IN WEB AT RBL 18.0 WL 59.10. 60 PERCENT FSH, 0.2" LONG IN WEB 1" OTBD OF RBL 9.0 WL 58.70. 50 PERCENT FSH, 0.2" LONG IN WEB AT RBL 9.0 WL 54.10. AREAS MARKED ON A/C. FAILS NDT INSPECTION AT THIS TIME. COMPLIED WITH EC/TC REO 601R-53-41-260 IAW REO 601R-53-41-260, REV D.

Part: BULKHEAD — CRACKED (BS 621) · airframe 19,626 hrs · 16,833 cycles

FS 621.00 PRESSURE BULKHEAD HAS A 70 PERCENT FSH HFEC INDICATION NOTED APPROX 0.1" LONG IN THE WEB AT THE UPPER INBD CORNER OF THE LINTEL ATTACH FITTING. FAILS NDT INSP AT THIS TIME. REPAIR IAW EC/TC REO 601R-53-61-1230 HAS BEEN COMPLETED AND THE REPAIR C/W THE REQUIREMENTS OF EC/TC AND REO 601R-53-61-1230 REV D.

Part: BULKHEAD — CRACKED (BS 559) · airframe 19,626 hrs · 16,833 cycles

FS 559.00 PRESSURE BULKHEAD WEB AND CAP ANGLE (LT) HAS 2 INDICATIONS NOTED AS LISTED: 60 PERCENT FSH, 0.2" LONG IN WEB APPROX 1.0" OTBD OF LBL 9.0 @ WL 51.70. 2) 50 PERCENT FSH, 0.2" LONG IN CAP ANGLE RADIUS BELOW LBL 9.0 POST. AREAS MARKED ON ACFT. FAILS NDT INSP AT THIS TIME. C/W EC/TC REO 601R-53-41-609 AND MET ALL REQUIREMENTS OF REO 601R-53-41-609 REV A.

Part: BEARING — LACK OF LUBE (PAX DOOR HANDLE) · airframe 19,626 hrs · 16,833 cycles

PAX DOOR INNER HANDLE FAILS FUNCTIONAL TEST AT 25 LBS FORCE (16 MAX). CLEANED & LUBRICATED THE FUSELAGE LATCH PIN BEARINGS AND REPEATED THE PAX DOOR FUNCTIONAL CHECK ON THE INNER HANDLE IAW AMM TASK 52-11-00-720-802, WITH NO DEFECTS NOTED.

Part: ANGLE — CRACKED (BS 621-625) · airframe 19,626 hrs · 16,833 cycles

RT FS 621 TO 625 OBLIQUE IS CRACKED IN AFT EQUIPMENT BAY. INSTALLED NEW OBLIQUE ANGLE IAW SRM 51-42-21.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 19,626 hrs · 16,833 cycles

PASSENGER DOOR AFT SIDE DRAG ANGLE IS CRACKED. REPAIRED PAX DOOR AFT DRAG ANGLE IAW EC/TC REO 601R-52-11-513.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,405 hrs · 16,571 cycles

NR 2 CABIN CEILING EMERGENCY LIGHT INOP.

Part: BRACKET — UNKNOWN (NLG) · airframe 18,840 hrs · 15,982 cycles

NOSE GEAR DISAGREE ON RETRACTION AFTER TAKEOFF. AIRCRAFT RETURNED TO ATL AFTER T/O. NOSE GEAR DISAGREE ON RETRACTION AFTER TAKEOFF. FLT 4954 DEL 102 MINS N/C=18R. REMOVED AND REPLACED OLEO CENTERED/ EXTENDED SUPPORT BRACKET ON NOSE LANDING GEAR SENSOR. OPS CHECK GOOD. IAW CRJ 200 32-61-05. RII SATISFACTORILY C/W SP 607

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,742 hrs · 15,879 cycles

OVERHEAD EMERGENCY LIGHT FORWARD OF EMERGENCY EXIT ROW INOP. FLT 5455 DEL 25 MINS.

Part: UNKNOWN — UNKNOWN (PAX DOOR) · airframe 18,185 hrs · 15,338 cycles

DURING CLIMB-OUT AT 15000 FT, HEARD WHISTLING NOISE FROM CABIN DOOR AT 17500 FT HEARD POPPING NOISE CABIN THEN CLIMBED AT 4600 FT/MIN. DESCENDED TO 8000 FT RAN QRH. EMERGENCY DECLARED, EN ROUTE TO ATL, A/C DIVERTED TO MKE DUE TO MTC.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,967 hrs · 15,126 cycles

LT OVERWING EMERGENCY LIGHT INOP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,737 hrs · 14,900 cycles

EMERGENCY LIGHT FDW LIGHT ASSY BOTH SIDE AND 1ST LIGHTS OVERWING BOTH SIDE INOP.

Part: UNKNOWN — ODOR (CABIN) · airframe 17,520 hrs · 14,683 cycles

DURING TAKEOFF ROLL SMELLED ODOR SIMILAR TO DIRTY SOCKS AT 800 FT AGL RECEIVED SMOKE TOILET CAUTION MESSAGE. APPROXIMATELY 2 MINUTES LATER RECEIVED RIGHT PACK OVERTEMP CAUTION MESSAGE. OVERTEMP CAUTION MESSAGE EXTINGUISHED AFTER 30 SECONDS. SMOKE TOILET EXTINGUISHED 2 MINUTES LATER. PACK MANUAL. EMERGENCY DECLARED. A/C RETURNED TO VPS AFTER T/O. FLT 5522 DEL 164 MINS. CABIN/COCKPIT TEMPERATURE CONTROL SYSTEMS - AUTOMATIC MODES BOTH AUTO CONTROLS.

Part: DOOR — BINDING (PAX DOOR) · airframe 17,008 hrs · 14,241 cycles

PAX DOOR DIFFICULT TO CLOSE.

Part: DOOR — MALFUNCTIONED (PAX DOOR) · airframe 16,464 hrs · 13,753 cycles

PAX DOOR HARD TO OPEN. OPERATED DOOR FROM OUTSIDE AND INSIDE. NO DEFECTS NOTED. ACFT OK FOR CONTINUED SERVICE. (S)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,419 hrs · 12,832 cycles

CEILING EMERGENCY LIGHT 2ND FROM AFT INOP.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 15,419 hrs · 12,832 cycles

LEFT EXTERNAL EMERGENCY LIGHT IN FRONT OF EMERGENCY EXIT INOP.

Part: BEAM — CRACKED (CARGO DOOR) · airframe 15,178 hrs · 12,616 cycles

AAR - CARGO DOOR LINTEL BEAM LWR AFT ATTACHMENT CLIP CRACKED.

Part: SILL — CORRODED (FUSELAGE) · airframe 15,178 hrs · 12,616 cycles

AAR - CORROSION ON FLOOR SUPPORT SILL, JUST FWD OF SERVICE DOOR AT FS 349.00. CLEANED CORROSION ON FLOOR SUPPORT SILL, JUST FWD OF SERVICE DOOR AT FS 310.00 IAW CRJ-200 SRM 51-21-06. FOUND SURFACE CORROSION ONLY, NO MATERIAL LOSS. OK TO ALODINE, PRIME, AND PAINT. ALODINED, PRIMED, AND PAINTED FLOOR SUPPORT SILL, JUST FWD OF SERVICE DOOR AT FS 310.00 IAW CRJ-200 SRM 51-21-06. SUPPLEMENTAL SDR CLOSED 1/10/08.

Part: HYDRAULIC LINE — CHAFED (LT WING) · airframe 15,178 hrs · 12,616 cycles

LT WING T/E-HYD LINE CHAFING ON WIRE BUNDLE AT WING STA 50 "FLAGGED". E/C PERFORMED IAW NTM CRACK CONFIRMED IN X AXIS, END OF CRACK MARKED. NO CRACK FOUND IN Y AXIS.

Part: BONDING STRAP — FRAYED (LT SPOILERON) · airframe 15,178 hrs · 12,616 cycles

LEFT SPOILERON O/B BONDING STRAP FRAYED. E/C PERFORMED IAW NTM CRACK CONFIRMED IN X AXIS, END OF CRACK MARKED, NO CRACK FOUND IN Y AXIS. PRC APPLY IAW REF. DO/TS-43/08-9701. COMPLIED WITH EC/TC DO/TS-43/08.

Part: RIB — CRACKED (WING) · airframe 15,178 hrs · 12,616 cycles

AAR - RIGHT BATT RIB CRACKED. REMOVED CONNECTOR J410 AND J412 ON RIGHT BATT RIB. REMOVED FASTENERS THRU DOUBLER ON O/B SIDE AND REMOVED NUT PLATES ON ANGLE OF RIGHT BATT RIB. REMOVED DOUBLER ON O/B SIDE AND INSIDE SUPPORT ANGLE ON I/B SIDE OF RIGHT BATT RIB. LOCATED AND DRILLED ANGLE DOUBLER (-10) AND FILLER (-12) WITH CUTOUT OF DAMAGE AS IAW BOMBARDIER REO 601R-57-51-046. INSTALL ANGLE DBLR FILLER AND INBOARD SUPPORT ANGLES. INSTALLED ANGLE DOUBLER FILLER I/B SUPPORT ANGLES IAW BOMBARDIER REO 601R-57-51-09. REINSTALLED CONNECTOR J410 AND J412. OPS CHECK GOOD RII 5001196 IAW CRJ 200 AMM 32-01-00. ALL WORK ACCOMPLISHED PER ASA EC/TC 601R-57-51-046. SUPPLEMENTAL SDR CLOSED 1/15/08.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 14,967 hrs · 12,439 cycles

CAPT'S FLASHLIGHT INOP.

Part: PLACARD — DAMAGED (AIRSTAIR DOOR) · airframe 14,883 hrs · 12,370 cycles

GLOW IN THE DARK "EXIT" STICKER ON AIR STAIR DOOR STEP IS MISSING FIRST THREE LETTERS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,868 hrs · 12,359 cycles

FOUND CABIN EMERGENCY FLOOR LIGHTS INOP AT ROWS 6CD THRU 8CD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,761 hrs · 12,272 cycles

FLOOR LEVEL EMERGENCY LIGHT STRIP ROW 6 THRU 8 INOP. FLT 4418 DEL 33 MINS.

Part: SIGN — INOPERATIVE (EMERGENCY EXIT) · airframe 14,761 hrs · 12,272 cycles

LOWER EMERGENCY EXIT SIGN ROW 8D INOP.

Part: DRAG ANGLE — CRACKED (DOOR) · airframe 14,617 hrs · 12,153 cycles

ASD AFT DRAG ANGLE IS CRACKED (MTC).

Part: LIGHT — BURNED OUT (CABIN) · airframe 14,593 hrs · 12,131 cycles

TWO SECTIONS IN THE PASSENGER CABIN OF THE EMERGENCY LIGHT IS BURNED OUT.

Part: DOOR — BINDING (SERVICE DOOR) · airframe 14,584 hrs · 12,126 cycles

SERVICE DOOR IS VERY HARD TO OPEN AND CLOSE, F/A IS UNABLE TO OPEN SERVICE DOOR.

Part: DOOR — BINDING (SERVICE DOOR) · airframe 14,454 hrs · 12,015 cycles

GROUND PERSONNEL REPORTS THE SERVICE DOOR IS DIFFICULT TO OPEN.

Part: SKIN — CRACKED (FUSELAGE) · airframe 14,349 hrs · 11,924 cycles

LEFT BONDED SKIN CRACKED AT FS 640.00 REO 601R-53-61-506 REV C TO BE CARRIED OUT.

Part: DOOR — BINDS (PAX DOOR) · airframe 14,349 hrs · 11,924 cycles

PAX DOOR HARD TO CLOSE.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 14,344 hrs · 11,918 cycles

LEFT BONDED SKIN DOUBLER CRACKED AT FS 640.00. REO 601R-53-61-506 REV-C CARRIED OUT.

Part: DOOR — STUCK (AIRSTAIR) · airframe 14,165 hrs · 11,788 cycles

ASD HARD TO CLOSE.

Part: BRACKET — CRACKED (AIRSTAIR DOOR) · airframe 14,049 hrs · 11,699 cycles

ASD FWD ANCHOR BRACKET CRACKED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,839 hrs · 11,543 cycles

LEFT WING EMERGENCY LIGHT INOP.

Part: LANDING GEAR — UNKNOWN (MAINS) · airframe 13,435 hrs · 11,234 cycles

AFTER TAKEOFF PLACED GEAR HANDLE UP, FOLLOWED BY GEAR DISAGREE AND NOSE GEAR DOOR OPENED EICAS WARNING MSG'S. C/W QRH PROCEDURES LANDED AND GROUND PERSONNEL INSERTED GEAR PINS INTO GEAR. EMERGENCY DECLARED. A/C RETURNED TO ERI AFTER T/O. FLT 4825 CX.

Part: FLAP — FAILED (WING) · airframe 13,214 hrs · 11,064 cycles

FLAP FAIL AT 0 DEGREE ON APPROACH. EMERGENCY DECLARED.

Part: FLAP — MALFUNCTIONED (WING) · airframe 13,082 hrs · 10,953 cycles

FLAPS FAIL ON APPROACH. EMERGENCY DECLARED.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 13,044 hrs · 10,926 cycles

FLAP FAIL MSG AT ZERO DEGREES, WHEN SELECTED ON APPROACH. EMERGENCY DECLARED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 12,357 hrs · 10,399 cycles

EMERGENCY LIGHT OUT ON TOP OF STAIRS. FLT 4609 DEL 160 MINS.

Part: ANGLE — CORRODED (BS 280) · airframe 12,270 hrs · 10,332 cycles

FOUND FS 280 FWD WEB ANGLE CORRODED. REMOVED AND REPLACED FWD WEB ANGLE WITH SERVICEABLE ANGLE PN 600-34017-351 IAW CRJ SRM 51-42-06.(CLOSED 10/31/06)

Part: INTERCOSTAL — CRACKED (BS 484) · airframe 12,270 hrs · 10,332 cycles

FOUND RT FS 484 INTERCOSTAL I/B ANGLE CRACKED AT RBL 27.

Part: INTERCOSTAL — CRACKED (BS 484) · airframe 12,270 hrs · 10,332 cycles

FOUND LT FS 484 INTERCOASTAL I/B ANGLE CRACKED AT LBL 27.

Part: INTERCOSTAL — CRACKED (BS 484) · airframe 12,270 hrs · 10,332 cycles

FOUND LT FS 484 INTERCOSTAL O/B ANGLE CRACKED AT LBL 36.

Part: INTERCOSTAL — CRACKED (BS 484) · airframe 12,270 hrs · 10,332 cycles

FOUND RT FS 484 INTERCOSTAL O/B ANGLE CRACKED AT RBL 36.

Part: ANGLE — CRACKED (BS 625) · airframe 12,270 hrs · 10,332 cycles

FOUND RT FS 625 OBLIGUE CRACKED. REMOVED CRACKED OBLIQUE ANGLE FROM R/H FS 625. IAW SRM 51-42-21. MDA 1064 10-15-06. DUPLICATED SERVICEABLE OBLIQUE ANGLE FROM 7075 T6 .050 PO 8639-1 IAW CRJ SRM 53-61-17. ALODINED PRIMED AND TOPCOATED SERVICEABLE ANGLE IAW CRJ SRM 51-25-16. INSTALLED SERVICEABLE ANGLE IAW CRJ SRM 51-42-21. (CLOSED 10/31/06)

Part: ANGLE — CRACKED (BS 625) · airframe 12,270 hrs · 10,332 cycles

FOUND LT FS 625 OBLIQUE CRACKED.

Part: ATTACH FITTING — CRACKED (FUSLEAGE) · airframe 12,270 hrs · 10,332 cycles

RANRC NR 319U, 280.00 CLIPS AT RBL 9 AND LBL9 OB CRACKED. REMOVED RT AND LT OB CLIPS. DUPLICATED OB CLIP USING 2024-T3 .050 PO8398-1. MATERIAL ID FROM SRM 53-21-43. OK TO PRIME AND PAINT. PRIMED AND PAINTED IAW SRM 51-25-06. OK TO INSTALL. INSTALLED OB CLIP IAW SRM 51-42-21. DUPLICATED RT OB CLIP USING 2024-T3 .050 PO8398-1. OK TO PRIME AND PAINT. PRIMED AND PAINTED IAW SRM 51-25-16.. OK TO INSTALL. INSTALLED CLIP IAW SRM 51-42-21. (CLOSED 10/31/06)

Part: WEB — CRACKED (BS 280) · airframe 12,270 hrs · 10,332 cycles

RANRC 351. 280.00 WEB CRACKED AT LBL13 NEAR UPPER FLANGE. ALL WORK DONE IAW ASA EO 600-53-91 L/W TH302. (CLOSED 10/31/06)

Part: STRUCTURE — CRACKED (BS 280) · airframe 12,270 hrs · 10,332 cycles

RANRC 350. 280.00 SEB CRACKED AT RBL13 NEAR LWR FLANGE. REMOVED EXISTING FASTENERS REQUIRED FOR REPAIR. MADE CUT OUT IN LOWER WEB AS REQUIRED. FABRICATED -8 FILLER. LOCATED ADDITIONAL HOLES FOR REPAIR. FABRICATED -4 DOUBLER USING S6144-33. LOCATED ALL FASTENER HOLES AS REQUIRED IN -4 REPAIR DOUBLER. OK TO INSTALL DOUBLER AND FILLER. INSTALLED -4 DOUBLER AND -8 FILLER. ALL WORK ACCOMPLISHED IAW EO 600-53-90. NDT REQUIREMENTS COMPLETE ON W/C 411. NO DEFECTS NOTED. RII 5000532 (CLOSED 10/31/06)

Part: FLOOR PANEL — CRACKED (CABIN) · airframe 12,270 hrs · 10,332 cycles

RANRC NR 188// LT FLOOR EDGE POSSIBLY CRACKED AT FS605 AND FS589 FROM FAST. TO EDGE OF PART (MARKED).

Part: FLOOR SUPPORT — CORRODED (BS 559-621) · airframe 12,270 hrs · 10,332 cycles

LT FLOOR EDGE FROM FS 559 TO FS 621 HAS SURFACE CORROSION AND RUSTED ATTACH FAST. AROUND NUT PLATES NUMEROUS LOCATION (MARKED).

Part: FLOOR SUPPORT — CORRODED (BS 574-621) · airframe 12,270 hrs · 10,332 cycles

RANRC NR 203// RT SIDE FLOOR EDGE MEMBER FROM FS621-FS574 SURFACE CORROSION AND RUSTED FAST. AROUND NUTPLATES (MARKED).

Part: ANGLE — CORRODED (BS 621 BULKHEAD) · airframe 12,270 hrs · 10,332 cycles

RANRC NR 202// FLOOR LEVEL ANGLE; 621 BULKHEAD LBL27-LBL37; BARE METAL AND SURFACE CORROSION.

Part: FITTING — CRACKED (FUSELAGE) · airframe 12,270 hrs · 10,332 cycles

UPPER RADIUS CLIPS LEFT AND RIGHT OF THE CENTER OF FS 280 STRUCTURE ARE CRACKED. REMOVED RT I/B RADIUS CLIP. DUPLICATE LT CLIP. MATERIAL ID FROM CRJ SRM 53-21-43. OK TO PRIME AND PAINT. PRIMED AND PAINTED IAW CRJ SRM 51-25-06. OK TO INSTALL. INSTALLED LT CLIP IAW CRJ SRM 51-42-21. DUPLICATED RT CLIP. OK TO PRIME AND PAINT. PRIME AND PAINT CLIP IAW CRJ SRM 51-25-16. OK TO INSTALL. INSTALL CLIP IAW CRJ 51-42-21. (CLOSED 10/31/06)

Part: COVER — CRACKED (CABIN) · airframe 11,928 hrs · 10,068 cycles

CABIN FLOOR EMERGENCY LIGHT TRACK UPPER PROTECTIVE STRIP COVER CRACKED AND DAMAGED AT ROW 1 & 2.

Part: LIGHT — INOPERATIVE (LT WING) · airframe 11,593 hrs · 9,805 cycles

FOUND LT WING EMER LIGHT INOP.

Part: LIGHT — BROKEN (CABIN) · airframe 11,532 hrs · 9,759 cycles

EMERGENCY EXIT LIGHT AT PASS DOOR HOUSING IS BROKEN.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 11,247 hrs · 9,529 cycles

RT O/W EMERG EXIT FWD EXTERIOR LIGHT INOP.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT)

DURING A HANGAR INSPECTION IN BTR, THE NR 2 EXTERIOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE NR 2 EXTERIOR EMERGENCY LIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LAMP — BURNED OUT (EMERGENCY LIGHT)

DURING HANGAR MAINTENANCE, THE RT FWD EXTERIOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE RT FWD EXTERIOR EMERGENCY LIGHT. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: LAMP — BURNED OUT (EMERGENCY LIGHT)

FLT 4786 - DURING A GROUND INSPECTION IN ATL, A FORWARD OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN A FORWARD OVERWING EMERGENCY LIGHT. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: SUPPORT BEAM — CRACKED (FUSELAGE)

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

Part: SUPPORT BEAM — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE CENTER ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL 0 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE CENTER ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL 0 IAW ASA EO 600-53-0072B. (M)

Part: CLIP — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE LEFT INBOARD FS 280 CLIP WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LEFT INBOARD FS 280 CLIP IAW SRM 51-42-06. (M)

Part: SUPPORT ANGLE — CRACKED (FUSELAGE)

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

Part: LENS — CRACKED (CABIN)

DURING A -CHECK IN MCN, THE EMERGENCY EXIT LIGHT BASE AND LENS BY THE SERVICE DOOR WERE FOUND TO BE CRACKED. MAINTENANCE IS REMOVING AND REPLACING THE EMERGENCY EXIT LIGHT ASSEMBY BY THE SERVICE DOOR. (M)

Part: CLIP — CRACKED (FUSELAGE)

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

Part: DOOR — STICKING (MAIN PAX)

DURING A GROUND INSPECTION IN DFW, THE FLIGHT ATTENDANT REPORTED THE PASSENGER DOOR STICKS DURING OPENING. MAINTENANCE INSPECTED THE PASSENGER DOOR AND OPERATIONAL CHECKS WERE GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: BEAM — CRACKED (ENG SUPPORT)

DURING AN A-CHECK, THE LT FORWARD IB CORNER OF THE ENGINE SUPPORT BEAM AT BL 36.20 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LT FORWARD IB CORNER OF THE ENGINE SUPPORT BEAM AT BL 36.20 IAW ASA EO 600-53-0070. (M)

Part: STEP — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE PASSENGER DOOR BOTTOM STEP PUSH PULL ROD BRACKET WAS FOUND LOOSE AND THE BOTTOM STEP CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR BOTTOM STEP AND ADJUSTED THE BOTTOM STEP PUSH-PULL ROD BRACKET. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: BRACKET — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE SPIDER DUCT BRACKET IN THE AFT EQUIPMENT BAY WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE SPIDER DUCT BRACKET IN THE AFT EQUIPMENT BAY IAW AMM 21-52-00. (M)

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

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

Part: APU — FAILED

FLT 4400 - DURING DESCENT INTO HSV FROM DFW AT APPROX 10,500 FEET AND 260 KIAS, AN EXTREMELY POWERFUL ODOR OF JET FUEL OCCURRED IN THE COCKPIT AND CABIN AFTER THE AUXILIARY POWER UNIT WAS STARTED. THE CREW SHUT THE AUXILIARY POWER UNIT DOWN LEAVING THE BLEEDS ON THE ENGINE. THE AIRCRAFT LANDED SAFELY IN HSV. MAINTENANCE DEFERRED THE AUXILIARY POWER UNIT IAW MEL NR 49-10-01, PENDING THE APPROPRIATE REPAIRS. MAINTENANCE CLEARED THIS DEFERRAL BY REMOVING AND REPLACING THE AUXILIARY POWER UNIT. OPERATIONAL AND LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: ODOR — DETECTED (CABIN)

DURING DESCENT, A STRONG FUEL ODOR OCCURRED IN THE COCKPIT AND CABIN WHEN THE BLEEDS WERE SWITCHED FROM THE ENGINE TO THE AUXILIARY POWER UNIT. THE AIRCRAFT LANDED SAFELY. MAINTENANCE INSPECTED THE AUXILIARY POWER UNIT FOR LEAKS AND RAN BOTH ENGINES WHILE TRANSFERRING THE RT ENGINE BLEEDS TO THE AUXILIARY POWER UNIT SEVERAL TIMES. THE FUEL ODOR DID NOT REOCCUR. OPERATIONAL CHECKS GOOD. AIRCRAFT, OK FOR SERVICE.

Part: COALESCER BAG — ODOR (ACM)

DURING DESCENT INTO MOB, AFTER STARTING THE AUXILLARY POWER UNIT AND SWITCHING THE BLEEDS, A FUEL ODOR OCCURRED IN THE COCKPIT AND CABIN. THE FUEL ODOR DISSIPATED AFTER SHUTTING THE AUXILIARY POWER UNIT DOWN. THE AIRCRAFT SAFELY IN MOB. MAINTENANCE REMOVED AND REPLACED BOTH COALESCER BAGS ON THE AIR CYCLE MACHINE. ALSO, BOTH ENGINES WERE RAN WITH THE ENGINE BLEEDS CYCLED ON AND OFF, AND THE AUXILIARY POWER UNIT WAS SHUT DOWN AND RE-STARTED WITH THE ENGINES RUNNING. NO FUEL ODOR WAS NOTED. OPERATIONAL AND LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE.

Part: BULB — BURNED OUT (FUSELAGE)

FLT 4713 - DURING GROUND INSPECTION IN DFW, THE LEFT FORWARD MOST EXTERNAL EMEREGNCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BURNED OUT EXTERNAL EMERGENCY LIGHT BULB. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: BULB — BURNED OUT (CABIN)

DURING GROUND INSPECTION, THE LEFT FORWARD MOST EXTERNAL EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BURNED OUT EXTERNAL EMERGENCY LIGHT BULB. OPERATIONAL CHECK GOOD. AIRCRAFT OK FOR SERVICE. (M)