N932XJ

Part: BATTERY — INOPERATIVE · airframe 29,914 hrs · 20,228 cycles

FWD LH +RH E-LIGHT INOP R+R PS35 BATTERY ASSY IAW 33-51-17-400-801 P/N ON/OFF 2013-1ASMI S/N OFF 1355 S/N ON 14558

Part: LIGHT — MISSING · airframe 28,944 hrs · 19,476 cycles

FLOOR PROXIMITY LIGHTS MISSING BOTH SIDES AT EXITS AND AFT INSTALLED PROX LTS P/N'S PL1100LH07 & PL1600LH07 IAW AMM 33-51-01

Part: STRINGER — CORRODED (BS 280-265 S27R) · airframe 28,719 hrs · 19,289 cycles

FOUND STR 27R CORRODED AT FS250-FS265. 2.0" X 1.0" X .021" DEEP. REPAIRED PER EA# CRJ953-12410

Part: CASCADE — GOUGED · airframe 28,719 hrs · 19,289 cycles

FOUND RH ENGINE LOWER CASCADE GOUGED .022" DEEP. AFTER EVALUATION, ORGINAL PART FOUND TO BE OUT OF LIMITS. REPLACED WITH NEW PART IAW CRJ900 SRM 78-34-01

Part: SEAT TRACK — CORRODED · airframe 28,719 hrs · 19,289 cycles

R/H SIDE SEAT RAIL TRACK APPROX 3 FT AFT OF AFT E DOOR HAS A CLIP WITH A BROKEN SCREW IN IT AND CORROSION AROUND THE SCREW. REMOVED AND REPLACED R/H SIDE SEAT RAIL IAW CRJ900 SRM 51-41-02

Part: PANEL — DAMAGED · airframe 28,719 hrs · 19,289 cycles

R/H I/B FLAP VANE L/E PANEL 684 FT HAS A ELONGATED HOLE PANEL 684FT OUT OF LIMITS DUE TO DAMAGE NEAR FASTENER HOLE IAW CRJ900 57-52-01-001-A01. LOCATED AND DRILED NEW PANEL IAW CRJ900 SRM 51-40-11 RESTORED FINISH IAW CRJ900 SRM 51-21-11, 51-25-06 AND 51-25-16.

Part: BULKHEAD — DAMAGED · airframe 28,719 hrs · 19,289 cycles

AFT FACE OF PRESSURE BULKHEAD FS 1098, 20, AT LT LOWER O/B AIR DUCT FLANGE AT 5:00 POSITION HAS A BOLT WORKING LOOSE AND CUTTING INTO THE FLANGE AND MAYBE HE BULKHEAD. REPAIRED IAW EA CRJ953-12316 REMOVED AND REPLACED LOWER O/B L/H BLEED AIR DUCT IAW CRJ900 AMM 30-11-02

Part: PANEL — CHAFED · airframe 28,719 hrs · 19,289 cycles

L/H WING ACCESS PANEL #584ET HAS CHAFING. CHAFING ON ACCESS PANEL 584ET WAS FOUND TO BE OUT OF LIMITS IAW CRJ900 SRM 57-52-01 LOCATED AND DRILLED ACCESS PANEL 584ET IAW CRJ900 SRM 51-40-11. RESTORED PAINT FINISH IAW CRJ 900 SRM 51-21-11, 51-25-06 AND 51-25-16.

Part: CHANNEL — CORRODED · airframe 28,719 hrs · 19,289 cycles

FS 295-FS310 BTW STGR 26L TO ATGR 26R CHANNEL TCAS LOWER CORROSION. REMOVED AND REPLACED LWR TCAS ANTENNA CHANNEL IAW CRJ900 SRM 51-42-06, REMOVED AND REPLACED LWR TCAS ANTENNA IAW CRJ900 AMM 34-43-07

Part: DIAPHRAGM — CORRODED (LAV SERVCE DOOR) · airframe 28,719 hrs · 19,289 cycles

FOUND DIAPHRAGM FOR FWD LAV SERVICE DOOR CORRODED. CORROSION IS 4.0" X 1.0" X .050" DEEP. REMOVED AND REPLACED 2 (EA) ANGLES AND 1 (EA) LOWER DIAPHRAM IAW CRJ900 SRM 51-42-06 "

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 28,434 hrs · 19,026 cycles

EXIT LIGHT OUT AT ROW 5 FOUND DURING FA PREFLIGHT. R & R THE BATTERY ASSY PS36 IAW AMM 33-51-17. ALL CHECKED GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 28,389 hrs · 18,985 cycles

EXTERIOR EMERGENCY LIGHT RH FWD IS INOPERATIVE. REMOVED AND REPLACED LIGHT BULB IAW AMM 33-51-15

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 28,372 hrs · 18,972 cycles

FWD SERVICE DOOR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED THE LAMPS IAW AMM 33-51-15, OPS FAILED. R & R THE PS35 BATTERY ASSY AND BATTERY CHARGER ASSY IAW AMM 33-51-17, OPS TESTED GOOD.

Part: SIGN — MISSING (MAIN CABIN) · airframe 24,774 hrs · 16,186 cycles

ROW 13 REARWARDS FACING 'EMERGENCY EXIT' SIGN MISSING. ROW 13 REARWARDS FACING EMERGENCY EXIT SIGN INSTALLED IAW CRJ900 AMM 3 3-51-07. NO FURTHER ACTION REQUIRED.

Part: OVEN — ODOR (GALLEY) · airframe 23,797 hrs · 15,470 cycles

OVEN EMITTED A BURNING ODOR. R & R THE GALLEY OVEN IAW AMM 25-32-01, OPS CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (GALLEY) · airframe 23,738 hrs · 15,422 cycles

EMERGENCY FLASHLIGHT IN THE GALLEY WAS NOT CHARGING. REPLACED THE FLASHLIGHT IAW AMM 25-61-02, OPS CHECKED GOOD.

Part: SEAL — BROKEN (FWD FLASHLIGHT) · airframe 23,664 hrs · 15,373 cycles

FWD F/A FLASHLIGHT NEXT TO JUMPSEAT HAS A BROKEN SEAL & DOES NOT WORK. REPLACED THE FWD FLASHLIGHT SEAL IAW AMM 25-60-00.

Part: LIGHT — INOPERATIVE (LT WING) · airframe 23,316 hrs · 15,128 cycles

FWD OVERWING EMERGENCY LIGHT OUT DEFERRED LT OVERWING EMERGENCY LIGHT (FWD) IAW MEL 33-51-2C. RELAMPED LT FWD OVERWING EMER LIGHT IAW AMM 33-51-15, OPS CHECK GOOD.

Part: SMOKE WARNING — FALSE ACTIVATION (FWD LAVATORY) · airframe 22,841 hrs · 14,805 cycles

FORWARD LAVATORY SMOKE MASTER WARNING ILLUMINATED IN FLIGHT FOR FIVE SECONDS, AND THEN DISSAPEARED. NO SMOKE WAS DETECTED. REMOVED & REPLACED FWD LAVATORY SMOKE DETECTOR IAW AMM 26-16-01. OPS CHECKED GOOD. ACFT OK FOR SERVICE.

Part: HEATER — ODOR (GALLEY) · airframe 22,652 hrs · 14,668 cycles

VERY STRONG ODOR OF BURNING ELECTRICAL WIRES NOTED AT THE FORWARD FLIGHT ATTENDANT STATION NEAR PHONE & PA. ODOR ALSO NOTED IN COCKPIT. COMPLIED WITH FIM 21-22-00, FOUND ODOR TO BE FROM DUCT BEHIND PANEL 231AL. ODOR GOES AWAY WITH PACKS AND RECIRCULATION FAN OFF. REMOVED AND REPLACED THE GALLEY HEATER IAW AMM 21-23-64, OPS CHECKED GOOD.

Part: FEEDER CABLE — BROKEN (EMERGENCY LIGHTS) · airframe 22,300 hrs · 14,452 cycles

OVERWING FWD EMERGENCY LIGHT HAS A BROKEN POWER LEAD. REMOVED AND REPLACED THE LIGHT ASSEMBLY IAW AMM 33-51-15-400-801. SYSTEM OPS CHECKED GOOD IAW AMM 33-51-00-710-802.

Part: HOUSING — CRACKED (E/E BAY DOOR) · airframe 22,300 hrs · 14,452 cycles

MAIN AVIONICS COMPARTMENT DOOR HANDLE HOUSING IS CRACKED AT THE BASE OF THE HANDLE. REMOVED AND REPLACED MAIN AVIONICS COMPARTMENT DOOR HANDLE HOUSING IAW SRM 51-42-21. PERFORMED OPS TEST IAW AMM 52-42-00-710-801 STEP 4 A, OPS CHECKED GOOD.

Part: LONGERON — CRACKED (BS 280) · airframe 22,300 hrs · 14,452 cycles

LONGERON 3L, BS 280 IS CRACKED. REPAIRED THE LONGERON IAW REO 670-53-21-493, AND EOR53568 REV ONE.

Part: WEB — CRACKED (PASSENGER DOOR) · airframe 22,300 hrs · 14,452 cycles

PAX DOOR AFT WEB IS CRACKED AT BOTTOM STEP RISER. REPAIRED PAX DOOR WEB IAW SRM 52-11-04.

Part: SEAT TRACK — CORRODED (BS 693-977) · airframe 2,230 hrs · 14,452 cycles

MAIN CABIN SEAT TRACK IS CORRODED AND GOUGED, RBL 15, BS 693 - 977. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49, SRM 51-40-11, SRM 51-21-11, AND REO 670-53-00-343, REV M.

Part: SEAT TRACK — CORRODED (BS 693-977) · airframe 22,300 hrs · 14,452 cycles

MAIN CABIN SEAT TRACK IS CORRODED AND GOUGED, LBL 15, BS 693 - 977. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49, AND REO 670-53-00-343, REV M.

Part: SEAT TRACK — DAMAGED (CABIN) · airframe 22,300 hrs · 14,452 cycles

RIGHT SIDE SEAT TRACK 9 HAS A MISSING FASTENER. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49, AND REO 670-53-00-343.

Part: STRINGER — CORRODED (BS 305-339) · airframe 22,300 hrs · 14,452 cycles

AFTER REMOVING WET INSULATION FOUND A STRINGER 27 CORRODED AT BS 310. REMOVED AND REPLACED THE STRINGER BETWEEN BS 305 TO 339 IAW SRM 51-42-06, AND 51-42-21.

Part: SEAT TRACK — GOUGED (CABIN) · airframe 22,300 hrs · 14,452 cycles

RIGHT SEAT TRACK 3 GOUGED. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49, AND REO 670-53-00-343, REV M.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHTS) · airframe 21,797 hrs · 14,079 cycles

DURING PREFLIGHT INSPECTION THE EMERGENCY LIGHTS WERE NOT COMING ON AND THE EMERGENCY SWITCH ON THE FA'S PANEL WAS FOUND IN THE ON POSITION. SUSPECT THE BATTERIES ARE DEAD. PERFORMED AN OPS TEST OF THE EMERGENCY POWER UNIT IAW AMM 33-51-7. OPS CHECK PASSED. NO FURTHER DEFECTS NOTED AT THIS TIME.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 21,387 hrs · 13,780 cycles

FWD ENTRANCE EMERGENCY LIGHT BULBS BURNED OUT. REPLACED THE BULBS IAW AMM 33-51-05, OPS CHECKED GOOD.

Part: GLOWSTRIP — MISSING (CABIN) · airframe 20,298 hrs · 13,044 cycles

ON CENTER CARPET R+R NOTED. RT AFT EMERGENCY EXIT FWD GLOW STRIP MISSING. REPLACED FWD GLOW STRIP AS REQUIRED IAW AMM 33-52-01.

Part: FLASHLIGHT — INOPERATIVE (FWD CABIN) · airframe 20,249 hrs · 13,013 cycles

FWD FA FLASHLIGHT DOES NOT SHOW THAT IT IS CHARGING. REMOVED & REPLACED FLASHLIGHT IAW AMM 25-61-02.

Part: LIGHT — MISSING (CABIN) · airframe 19,988 hrs · 12,837 cycles

EMERGENCY LIGHT MISSING AT ROW 13CD FORWARD. REPLACED THE LIGHT STRIP IAW AMM 31-51-11. ACFT OK FOR SERVICE.

Part: STRAP — BROKEN (FLASHLIGHT) · airframe 19,794 hrs · 12,708 cycles

FWD FA REPORTS SEAL ON FWD FLASHLIGHT IS BROKEN. R & R THE FLASHLIGHT STRAP IAW AMM 25-61-02. ACFT GOOD FOR SERVICE AT THIS TIME.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 19,647 hrs · 12,599 cycles

CUSTOMER WALK AROUND; FLIGHT DECK FLASHLIGHTS, 2, RED LIGHT IS NOT ON. REMOVED AND REINSTALLED NEW SERVICEABLE BATTERIES ON LT & RT COCKPIT, FLIGHT DECK FLASHLIGHTS IAW AMM 25-61-02-000-801-A10 & 25-61-02-400-801 A10 AND CMM 25-60-11.

Part: LIGHT — INOPERATIVE (LT WING) · airframe 19,647 hrs · 12,599 cycles

2 FORWARD OVERWING EMERGENCY LIGHTS ON LT WING AND 2 AFT OVERWING EMERGENCY LIGHTS ON THE WING INOPERATIVE. CONTINUATION CARD 81519411, OP 255. REMOVED PANEL 251NLW AND REINSTALLED PANEL AFTER CONNECTING P377 CONNECTOR IAW ESPM 20-26-00 AND AMM 25-26-01-400-801-A17. REMOVED AND REINSTALLED PASSENGER SEAT 8AB IAW AMM 25-21-01-400-801-A31. OPS CHECK GOOD.

Part: BEARING — CRACKED (RT WING) · airframe 19,647 hrs · 12,599 cycles

RIGHT WING AFT LINK AT WS 797, LOWER BEARING HAS A CRACK AND LINK IS MAKING CONTACT WITH ATTACHMENT FITTING. COMPLIED WITH EO R57200 , R57189 AND R57190 FOR INSPECTION AND REPLACEMENT.

Part: RETAINER — DAMAGED (PAX DOOR) · airframe 19,647 hrs · 12,599 cycles

DURING ENTRY OF CABIN IT WAS NOTICED THAT THE PAX DOOR SEAL RETAINER WAS DAMAGED BY PROXIMITY SENSOR CONDUIT CLAMP GETTING CAUGHT IN WAY DURING DOOR CLOSE. REMOVED AND REPLACED THE SEAL RETAINER IAW SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01 AND REO:670-52-11-022 REV C.

Part: PANEL — DAMAGED (PAX DOOR) · airframe 19,647 hrs · 12,599 cycles

ON INSTALLATION, FOUND HINGE ON UPPER STAIR PANEL ASSEMBLY BROKEN. LOCATED AND DRILLED HINGE ON UPPER STAIR PANEL ASSEMBLY IAW SRM 51-40-11-001-001-A01. ATTACHED HINGE ASSEMBLY TO THE UPPER STAIR PANEL IAW AMM 51-11-04-400-801-A01 STEPS A.2.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 19,647 hrs · 12,599 cycles

LEFT AND RT JACK FITTING SUPPORT INTERCOSTALS BETWEEN FS 280 TO FS 265 ARE CORRODED. CONTINUATION CARD 81519411 OP 233. REPLACED LT/RT JACK FITTING SUPPORT INTERCOSTALS BETWEEN FS 280 AND FS 265 IAW EA CRJ953-04677.

Part: DOOR SILL — CORRODED (BS 1000-1047) · airframe 19,647 hrs · 12,599 cycles

AFT CARGO DOOR SILL IS CORRODED FROM BS 1000 TO 1047. REPLACED THE AFT CARGO DOOR SILL IAW SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-42-21-001-001-A01, 51-41-02-001-001-A01, & 51-42-13-001-001-A01.

Part: FRAME — CORRODED (FUSELAGE) · airframe 19,647 hrs · 12,599 cycles

FRAME IS CORRODED AT FS 310 BETWEEN STR 26L TO STR 25R. CONTINUATION CARD 81519411, OP 228. REPAIRED FS 310 FRAME BETWEEN STR 26L TO STR 25R IAW REO 670-53-21-799.

Part: FRAME — CORRODED (FUSELAGE) · airframe 19,647 hrs · 12,599 cycles

FRAME IS CORRODED AT FS 265 BETWEEN STR 26R TO 26L. UPON INVESTIGATION, FOUND NO CORROSION TO FS 265 FRAME, CORROSION LIMITED TO STIFFENING ANGLE. R & R STIFFENING ANGLE IAW SRM 51-40-11-001-001-A01 & 51-42-06-001-001-A01.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 19,647 hrs · 12,599 cycles

SERVICE DOOR LOWER SILL ANGLE CORRODED BETWEEN FS 310 AND FS 349. CONTINUATION CARD 81519411, OPS 190 & 195. REPAIRED SERVICE DOOR LOWER SILL ANGLE BETWEEN FS 310 AND FS 349 BY REMOVING AND REINSTALLING SCUFF PLATE IAW AMM 53-21-23-000-801-A01 AND AMM 53-21-23-400-801-A01. REMOVED AND REINSTALLED NEW SERVICEABLE LOWER MOUNT ANGLE IAW SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. REMOVED AND REINSTALLED NEW SERVICEABLE OTBD STRIKER ANGLE IAW SRM 51-42-06-001-001-A01 AND SRM 51-40-11-001-001-A01. REMOVED CORRODED WEBS 4 EA PN: SH670-32040-3 & 4, 4 EA ANGLES SH670-31982-1 IAW SRM 51-42-06-001-001-A01 & SRM 51-40-11-001-001-A01. REMOVED AND REINSTALLED SAME SERVICEABLE SERVICE DOOR FITTINGS IAW SRM 51-41-02-001-001-A01. PAINT AND DINITROL IAW SRM 51-21-16-001-001-A01 AND 51-21-11-001-001-A01.

Part: INTERCOSTAL — CORRODED (BS 349) · airframe 19,647 hrs · 12,599 cycles

INTERCOSTAL AT STRINGER 20R, BS 349 CORRODED. REPLACED THE INTERCOSTAL IAW SRM 51-40-11-001-001-A01, AND 51-42-06-001-001-A01.

Part: FRAME — CORRODED (FUSELAGE) · airframe 19,647 hrs · 12,599 cycles

FRAME IS CORRODED AT FS 349 BETWEEN STR 26R TO 26L. CONTINUATION CARD 81519411, OP 191. REMOVED CORRODED FRAME AT FS 349 STR 26R TO 26L IAW SRM 51-42-06-001-001-A01, 51-40-11-001-001-A01 AND 51-42-21-001-001-A01.

Part: FRAME — CORRODED (FUSELAGE) · airframe 19,647 hrs · 12,599 cycles

FRAME IS CORRODED AT FS 319 BETWEEN STR 27 TO 26L. REPAIRED FRAME FS 319 BETWEEN STR 27 TO 26L IAW SRM 51-42-06-001-001-A01 AND REO 670-53-21-799.

Part: WEB — CRACKED · airframe 19,647 hrs · 12,599 cycles

CRACK ON FLOOR WEB CORNER FWD OF BS 202 BULKHEAD AT BOTTOM OF LT CAP ANGLE. REPAIRED THE WEB IAW REO 670-53-11-509 REV D.

Part: CHANNEL — CRACKED · airframe 19,647 hrs · 12,599 cycles

CHANNEL CRACKED TEN INCHES FROM THE AFT END. REPLACED THE CHANNEL AND JOINT STRAP IAW SRM 51-24-36-001-001-A01, 51-21-16-001-001-A01, AND 51-42-10-001-001-A01.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 19,647 hrs · 12,599 cycles

CONTINUATION OF JOB 81519411/190, CO 15194116. SERVICE DOOR LOWER SILL ANGLE CORRODED BETWEEN FS 310 AND FS 349. REPAIRED SERVICE DOOR LOWER SILL ANGLE BETWEEN FS 310 AND FS 349 BY REMOVING AND REINSTALLING SCUFF PLATE IAW AMM 53-21-23-000-801-A01 AND AMM 53-21-23-400-801-A01. REMOVED AND REINSTALLED NEW SERVICEABLE LOWER MOUNT ANGLE IAW SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. REMOVED AND REINSTALLED NEW SERVICEABLE OTBD STRIKER ANGLE IAW SRM 51-42-06-001-001-A01 AND SRM 51-40-11-001-001-A01. REMOVED CORRODED WEBS 4 EA PN:SH670-32040 3 & 4, 4 EA ANGLES SH670-31982-1 IAW SRM 51-42-06-001-001-A01 AND SRM 51-40-11-001-001-A01. REMOVED AND REINSTALLED SAME SERVICEABLE SERVICE DOOR FITTINGS IAW SRM 51-41-02-001-001-A01. PAINT AND DINITROL IAW SRM 51-21-16-001-001-A01 AND 51-21-11-001-001-A01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 19,647 hrs · 12,599 cycles

FLOOR SUPPORT ANGLE FOR 141ALF AT FS 280 IS CORRODED. REPLACED FLOOR SUPPORT ANGLE FOR 141ALF AT FS 280 IAW SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-42-15-001-001-A01, 51-45-00-001-001-A01 AND 51-42-21-001-001-A01.

Part: FRAME — CORRODED (FUSELAGE) · airframe 19,647 hrs · 12,599 cycles

CONTINUATION FROM JOB 81519411, OP 7, FRAME IS CORRODED AT FS 349 BETWEEN STR 26R TO STR 26L. REPAIRED CRACK ON FLOOR WEB CORNER RT FORWARD OF FS 202 BULKHEAD IAW REO 670-53-11-509, REV D DATED 2016/06/29.

Part: WEB — CRACKED · airframe 19,647 hrs · 12,599 cycles

CRACK ON FLOOR WEB CORNER FWD OF BS 202 BULKHEAD AT BOTTOM OF RT CAP ANGLE. REPAIRED THE WEB IAW REO 670-53-11-509 REV D.

Part: DOOR SILL — CORRODED (BS 310-349) · airframe 19,647 hrs · 12,599 cycles

PAX DOOR FLOOR SILL HAS CORROSION AT SEVERAL PLACES BETWEEN BS 310 - 349. REPLACED THE DOOR SILL ANGLE IAW SRM 51-41-02-001-001-A01, 51-40-11-001-001-A01, 51-42-21-001-001-A01, 51-42-06-001-001-A01, AND 20-21-00-910-801-A01.

Part: SEAT TRACK — CORRODED (BS 669-977) · airframe 19,647 hrs · 12,599 cycles

RIGHT SIDE SEAT TRACK CORRODED FROM BS 669.4 - 977. REMOVED, FABRICATED, REPLACED THE SEAT TRACK IAW REO 670-53-00-343 REV M AND AMM 53-00-49-000/400-801-A07.

Part: DRAG ANGLE — CRACKED (VERTICAL STAB) · airframe 19,647 hrs · 12,599 cycles

AFT DRAG ANGLE ON RT SIDE OF VERTICAL STAB IS CRACKED APPROXIMATELY .5 INCH. REMOVED AND REPLACED AFT DRAG ANGLE IAW SRM 51-40-11-001-001-A01, 51-42-13-001-001-A01, 51-42-21-001-001-A01, AND 51-42-22-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 379-669) · airframe 19,647 hrs · 12,599 cycles

RIGHT SEAT TRACK CORRODED BS 379 - 669.4. REMOVED, FABRICATED, AND REPLACED THE SEAT TRACK IAW GREO:670-53-00-343 AND AMM 53-00-49-000/-400-801-A01.

Part: BULKHEAD WEB — CORRODED (BS 280) · airframe 19,647 hrs · 12,599 cycles

BS 280 LEFT LOWER BULKHEAD WEB CORRODED AT INBD SIDE UNDER CORROSION CAP APPROX LBL 12. REPLACED THE BULKHEAD WEB IAW REO 670-53-11-594 AND SRM 53-11-10-201-003-A01.

Part: SEAT TRACK — CORRODED (BS 669-977) · airframe 19,647 hrs · 12,599 cycles

LEFT SIDE SEAT TRACK CORRODED FROM BS 669.4 - 977. REPLACED THE SEAT TRACK IAW REO 670-53-00-343 AND AMM 53-00-49-000/-400-801-A07.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 19,647 hrs · 12,599 cycles

INTERCOSTALS, 2 EA AT STR 27 HAVE CORROSION BETWEEN FS 349 TO FS 364. R & R, 2 EACH INTERCOSTALS, PN SH670-32075-3 & SH670-32075-4 AT STR 27, FS 349 - FS 364.00 IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01, 51-40-11-001-001-A01, 51-21-11-001-001-A01 & 51-25-00-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 581-661) · airframe 19,647 hrs · 12,599 cycles

NR 3 SEAT TRACK FROM BS 581 - 661+32 RBL 9 IS CORRODED AND HAS DAMAGE. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-400-801-A07, SRM 51-40-06-001-001-A01 AND REO 670-53-00-343 REV M.

Part: SEAT TRACK — CORRODED (BS 677-830) · airframe 19,647 hrs · 12,599 cycles

NR 5 SEAT TRACK FROM BS 677 - 830+40 RBL 9 IS CORRODED AND HAS DAMAGE. INSTALLED A NEW SEAT TRACK IAW AMM 53-00-49-400-801 CONFIG A07.

Part: SEAT TRACK — CORRODED (BS 661-677) · airframe 19,647 hrs · 12,599 cycles

NR 4 FLOOR SEAT TRACK FROM BS 661+32 - 677 IS CORRODED AND HAS DAMAGE AT LBL 9. INSTALLED A NEW SEAT TRACK IAW REO 670-53-00-343 REV M & AMM 53-00-49-400-801-A07.

Part: SEAT TRACK — CORRODED (BS 661-677) · airframe 19,647 hrs · 12,599 cycles

NR 4 SEAT TRACK FROM BS 661+32 - 677 RBL 9 IS CORRODED AND HAS DAMAGED. LOCATED AND DRILLED A NEW SEAT TRACK IAW REO 670-53-00-343 REV M AND INSTALLED IAW AMM 53-00-49-400-801 (A07).

Part: SEAT TRACK — CORRODED (BS 847-977) · airframe 19,647 hrs · 12,599 cycles

NR 7 FLOOR SEAT TRACK FROM BS 847+48 - 977 HAS MINOR CORROSION AND DAMAGE RBL 9. REMOVED & REPLACED SEAT TRACK IAW AMM 53-00-49-400-801 (A07) & REO 670-53-00-343 REV M.

Part: SEAT TRACK — CORRODED (BS 364) · airframe 19,647 hrs · 12,599 cycles

NR 1 SEAT TRACK AT LBL 9 BS 364 HAS MINOR CORROSION. FABRICATED & INSTALLED A NEW SEAT TRACK IAW REO 670-53-00-343 REV M & AMM 53-00-49-400-801-A07.

Part: SEAT TRACK — CORRODED (BS 847-977) · airframe 19,647 hrs · 12,599 cycles

NR 7 SEAT TRACK FROM BS 847+48 - 977 HAS CORROSION AND DAMAGE LBL 9. REMOVED, FABRICATED AND INSTALLED A NEW SEAT TRACK IAW REO 670-53-00-343 AND AMM 53-00-49-000/400-801-A07.

Part: SEAT TRACK — CORRODED (BS 349-485) · airframe 19,647 hrs · 12,599 cycles

NR 1 SEAT TRACK FROM BS 349 TO 485 RBL 9 HAS MULTIPLE LOCATIONS OF CORROSION AND DAMAGE. FABRICATED A NEW SEAT TRACK IAW REO 670-53-00-343 REV M, AND INSTALLED IAW AMM 53-00-49-980-801-A01.

Part: SEAT TRACK — CORRODED (BS 847) · airframe 19,647 hrs · 12,599 cycles

SEAT TRACK RBL 9 HAD CORROSION BETWEEN FS 847 - 847+48. FABRICATED AND INSTALLED A NEW SEAT TRACK IAW REO 670-53-00-343 AND AMM 53-00-49-400-801-A07.

Part: ATTACH ANGLE — CORRODED · airframe 19,647 hrs · 12,599 cycles

ATTACH ANGLE AT STRINGER 26L HAS CORROSION. LOCATED, DRILLED, INSTALLED, PAINTED AND CHECKED THE NEW ATTACH ANGLE SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-21-11-001-001-A01, 51-25-00-001-001-A01 AND 51-42-21-001-001-A01. "

Part: SEAT TRACK — CORRODED (BS 485-581) · airframe 19,647 hrs · 12,599 cycles

NR 2 SEAT TRACK, LBL 27 BS 485 - 581 HAS CORROSION AND DAMAGE. REMOVED, FABRICATED & INSTALLED A NEW SEAT TRACK SEGMENT IAW GREO 670-53-00-343 & AMM 53-00-49-000/400-801-A07.

Part: SEAT TRACK — CORRODED (BS 677-830) · airframe 19,647 hrs · 12,599 cycles

NR 5 SEAT TRACK FROM BS 677 - 830+40 IS CORRODED AND HAS DAMAGE LBL 9. REMOVED, FABRICATED & REPLACED THE SEAT TRACK SEGMENT IAW GREO 670-53-00-343 & AMM 53-00-49-000/400-801-A07.

Part: SEAT TRACK — CORRODED (BS 581-661) · airframe 19,647 hrs · 12,599 cycles

NR 3 SEAT TRACK FROM BS 581 - 661+32 HAD CORROSION AND DAMAGE FROM SEATS LBL 9. REMOVED, FABRICATED AND INSTALLED A SERVICEABLE SEAT TRACK IAW REO 670-53-00-343, AND AMM 53-00-49-000 & AMM 53-00-49-400-801-A07.

Part: CROSSBEAM — DAMAGED (BS 280) · airframe 19,647 hrs · 12,599 cycles

BS 280 CROSSBEAM HAS TWO SHEARED RIVETS AT RBL 12 AND CORROSION. REMOVED & REPLACED THE CROSSBEAM IAW SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01, & 51-42-21-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 379-669) · airframe 19,647 hrs · 12,599 cycles

LEFT SEAT TRACK CORRODED BS 379 - 669.4. REMOVED AND REPLACED THE SEAT TRACK IAW REO 670-53-00-343 REV M, SRM 51-40-11-001-001-A01 AND AMM 53-00-49-400-801-A01.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 19,647 hrs · 12,599 cycles

INTERCOSTAL AT STR 26R IS CORRODED BETWEEN FS 349 TO FS 364. R & R INTERCOSTAL AT STR 26R IAW SRM 51-42-06-001-001-A01, 51-40-11-001-001-A01, 51-42-21-001-001-A01.

Part: CROSSBEAM — CORRODED (FUSELAGE) · airframe 19,647 hrs · 12,599 cycles

FS 280M CROSSBEAM HAS 4 SHEARED RIVETS AT LBL 12 CORROSION CAP WITH EVIDENCE OF CORROSION AROUND HOLES AND UNDER CAP. CONTINUATION CARD 81519411 OP 175, REMOVED AND REINSTALLED DRIP TRAY LT IAW SRM 51-42-13-001-001-A01. R & R CROSSBEAM, TRANSVERSE IAW SRM'S 51-40-11-001-001-A01, 51-42-06-001-001-A01 AND 51-42-13-001-001-A01. REMOVED AND REINSTALLED CENTER CORROSION CAP LBL 12 TO RBL 12 IAW SRM 51-42-06-001-001-A01. LEFT CORROSION CAP TO BE INSTALLED JOB 81519411, OP 174.

Part: DOUBLER — CORRODED (DOOR FRAME) · airframe 19,647 hrs · 12,599 cycles

SERVICE DOOR FRAME DOUBLERS AT BS 319 AND 349 APPROXIMATELY WL 73 ARE CORRODED IN THE CORNERS. REMOVED AND REPLACED SERVICE DOOR FRAME DOUBLERS IAW SRM 51-42-21-001-001-A01 AND 51-77-00-001-001-A011.

Part: FLOORBEAM — DAMAGED (BS 280) · airframe 19,647 hrs · 12,599 cycles

CORROSION CAP AT BS 280 HAS 18EA ELONGATED HOLES. INSTALLED SERVICEABLE CORROSION CAP IAW SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01 AND 51-77-00-001-001-A01.

Part: GUARD — DAMAGED (LT MLG WW) · airframe 19,647 hrs · 12,599 cycles

LEFT MLG WHEEL WELL INNER SPLASH GUARD PANEL SCREW PULLED THRU INNER GUARD. REMOVED AND REPLACED THE LT MLG WHEEL WELL INNER SPLASH GUARD IAW SRM 51-40-11-001-001-A01, 51-42-21-001-001-A01, 51-42-06-001-001-A01, 51-41-02-001-001-A01, AND 51-45-00-001-001-A01.

Part: CROSSBEAM — CORRODED (BS 280) · airframe 19,647 hrs · 12,599 cycles

BS 280 CROSSBEAM HAS FOUR SHEARED RIVETS AT LBL 12 AND CORROSION. REMOVED AND REPLACED THE CROSSBEAM IAW SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND 51-42-13-001-001-A01.

Part: ANGLE — CORRODED (BS 280 FLOORBEAM) · airframe 19,647 hrs · 12,599 cycles

BS 280 CROSSBEAM FWD J ANGLE CORRODED. REPLACED THE CROSSBEAM FWD J-ANGLE IAW SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND 51-42-13-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 485-581) · airframe 19,647 hrs · 12,599 cycles

NR 2 SEAT TRACK FROM BS 485 - 581 RBL 9 IS CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-40-06-001-001-A01, 51-40-11-001-001-A01, REO:670-53-00-343 AND AMM 53-00-49-400-801.

Part: STRINGER — CORRODED (BS 295-310) · airframe 19,647 hrs · 12,599 cycles

STRINGER 24R IS CORRODED AROUND SEVERAL RIVETS BETWEEN BS 310 - 295. REPLACED THE STRINGER IAW SRM 51-42-06-001-001-A01, AND 51-42-21-001-001-A01.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 19,647 hrs · 12,599 cycles

STRINGER 25R IS CORRODED BETWEEN FS 310 TO FS 292. REPLACED STR 25R BETWEEN FS 310 TO FS 292, STR PN:SH670-31212-2 IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01 AND 51-42-13-001-001-A01.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 19,647 hrs · 12,599 cycles

STR 26R IS CORRODED BETWEEN FS 310 TO FS 295. REPLACED STR 26R BETWEEN FS 310 TO FS 295 IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01 AND 51-42-13-001-001-A01.

Part: LIGHT — UNSECURE (CABIN) · airframe 19,141 hrs · 12,242 cycles

ILLUMINATION STRIP ON FLOOR OF EXIT ROW 12A NOT ADHERING TO FLOOR. SECURED LIGHT STRIP IAW AMM 33-51-01. SECURITY CHECKED GOOD.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 18,408 hrs · 11,756 cycles

AFT FLIGHT ATTENDANT FLASHLIGHT RED LIGHT NOT BLINKING. R & R AFT FLIGHT ATTENDANT EMER FLASHLIGHT BATTERY IAW AMM 25-61-02. ALL CHECKED GOOD.

Part: WINDOW — CRACKED (COCKPIT) · airframe 16,948 hrs · 10,749 cycles

AT FL 230 WINDSHIELD HEAT LOW CLEAR SKIES FIRST OFFICERS SIDE WINDOW OUT PANEL SHATTERED. R & R IAW CRJ 900 TASK 56-12-01-00-801. FOR OPERATIONAL TEST OF WINDSHIELD TEMP CONTROLLER 3209517-2 LEAK TEST REQUIRED.

Part: CONNECTOR — DIRTY (CABIN) · airframe 15,314 hrs · 9,615 cycles

EMERGENCY CABIN INDICATION LIGHT BURNED OUT. DEFER EMER CALL SWITCH LIGHT IAW CRJ900. MEL 23-40-1C PLACARD INSTALLED ENTERED IN MM02 MXC NOTIFIED 96211. INSPECTION REVEALED DEBRIS COLLECTED ON CONNECTOR P327 INDUCING GAP ON CONNECTOR & PREVENTING FULL CONTACT BETWEEN PINS. REMOVED DEBRIS & REINSTALLED CONNECTOR IAW AMM 25-24-13. OPERATIONS CHECKED CRADLE IAW AMM 23-31-10, OPERATIONS CHECKED GOOD. DRY CLEAR MMO2 UPDATED, MXC NOTIFIED & PLACARD REMOVED. ACFT OK FOR SERVICE.

Part: LIGHT — MISSING (CABIN) · airframe 15,227 hrs · 9,558 cycles

EMERGENCY STRIP MISSING ROW 12. INSTALLED NEW FLOOR TRACK LIGHTING STRIP IAW AMM 33-51-01. OK FOR SERVICE.

Part: LIGHT — MISSING (CABIN) · airframe 14,936 hrs · 9,368 cycles

EMER LIGHTING STRIP ON FLOOR BY SEAT 12AB IS MISSING. INSTALLED NEW EMER FLOOR TRACK LIGHTS IAW AMM 33-51-01. PN ON PL88-910LH00, PN ON PL88-930LH05 & PN ON PL88-900LH00.

Part: SKIN — DENTED (TE FLAP) · airframe 14,765 hrs · 9,262 cycles

FOUND A DENT IN THE LT INBD FLAP LOWER SKIN. REPAIRED IAW EA CRJ957-02766.

Part: SKIN — DENTED (TE FLAP) · airframe 14,785 hrs · 9,267 cycles

LEFT WING INBD FLAP LOWER SKIN HAS DENT AT FLS63.50. DENT MEASUREMENTS ON LT WING INBD FLAP LOWER SKIN FLS63.50 WAS 2.40 INCHES L X 1.79 INCHES W X .100 INCHES D. DAMAGE RESPECT SUBMITTED IAW CRH 900 SRM 57-52-01-101-001-A01. REQUIRED DENT ON LT WING INBD LOWER SKIN AT FLS63.50 IAW ECRA J957-02766 REV IR. THIS IS A MAJOR REPAIR. DTA REQUIRED WITHIN 12 MONTHS FROM 7/23/14 ON LHIB FLAP CC670-14002-7, SN 15179 LOWER SKIN DENT AT FLS 63.50, 3.7 INCHES FROM TE REPAIRED IAW ECRAJ957-02766.

Part: RACK — DAMAGED (CARGO BAY) · airframe 14,785 hrs · 9,267 cycles

WI FI UNIT IN AFT BAG BAY HAS DAMAGE TO OTBD SIDE FWD & AFT UPPER CORNERS. REPAIRED WI FI RACK DAMAGE IAW EA CRJ946-02767.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 14,785 hrs · 9,267 cycles

PASSENGER DOOR HAS A CRACK IN THE DRAG ANGLES AT PREVIOUS REPAIR. REMOVED REPAIR ANGLE IAW SRM 51-42-10-001-001-A01. INSTALLED NEW REPAIR ANGLE ON PAX DOOR AFT DRAG ANGLE IAW SRM 52-11-04-201-002-A01.

Part: ACCESS PANEL — CHAFED (TE FLAP VANE) · airframe 14,785 hrs · 9,267 cycles

TASK CARD 900-27-580-101 LT INBD FLAP VANE ACCESS PANEL 584ET CHAFFED ACROSS RIVET HEAD. LOCATED & INSTALLED TWO EACH NUTPLATES IAW SRM 51-42-06-001-001-A01. PRIMED NEW PANEL IAW SRM 51-25-06-001-001-A01. TOP COATED PANEL IAW SRM 51-25-16-001-001-A01.

Part: LIGHT — UNKNOWN (CABIN) · airframe 13,748 hrs · 8,578 cycles

GALLEY FLOOR TRACKS REQUIRE REPLACEMENT. REPLACED GALLEY LT & RT FLOOR TRACK EMERGENCY LIGHT STRIPS IAW CRJ900 MM 33-51-01.

Part: CONTROL VALVE — MALFUNCTIONED (AC BAY) · airframe 13,352 hrs · 8,340 cycles

DURING PUSHBACK WE RECEIVED A LT PACK AUTO FAIL CAUTION ASSOCIATED WITH AN ODOR. WE SHUT OFF LT PACK & ODOR WENT AWAY & CAUTION WENT AWAY IN ABOUT 5 MINUTES. IAW MEL 21-51-1 B. ENTERED IN MM2 MC ADVICES PLACARD INSTALLED. R & R TEMP CONTROL VLV IAW AMM 21-51-20, OPERATIONS NO GOOD. ITEM REMAINS DEFERRED, NEEDS ACM.

Part: LENS — MISSING (EXIT SIGN) · airframe 13,307 hrs · 8,308 cycles

CENTER OVERHEAD AISLE EXIT SIGN FWD SIDE MISSING BLUE & RED LENS CAPS. LENS CAPS DEFERRED IAW NEF N33-50-1. TRANSFERRED TO MMO2 CTRL 2348532-1, NOTIFIED MOC 53212 CAT E 90 DAYS.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 13,300 hrs · 8,300 cycles

EMERGENCY FLASHLIGHT IN GALLEY BY SERVICE DOOR INOPERATIVE. R & R FLASHLIGHT IAW AMM 25-61-02.

Part: LIGHT — UNSECURE (CABIN) · airframe 13,029 hrs · 8,123 cycles

FLOOR TRACK LIGHTING NEAR 13C IS DETACHED. SECURED EMERGENCY FLOOR TRACK STRIP AT 13C IAW AMM 33-51-01.

Part: LIGHT — MISSING (CABIN) · airframe 13,018 hrs · 8,116 cycles

EMERGENCY LIGHT MISSING. REPLACED MISSING EMERGENCY LIGHT IAW 33-51-01. OPS CHECKED GOOD.

Part: COOLING FAN — FAILED (E&E BAY) · airframe 11,721 hrs · 7,316 cycles

DURING CRUISE STARTED SMELLING ELECTRIC BURN SMELL AFTER ABOUT 20 MINS WE HEARD THE AVIONICS FAN GRINDING AND COMING TO A STOP FOLLOWED BY THE AVIONICS COOL FAN CAUTION MESSAGE BEING DISPLAYED. FOLLOWED THE NON-NORMAL CHECKLIST, MESSAGE WENT AWAY. IT APPEARED AGAIN ON THE GROUND IN SLC. PERFORMED MAINT AS REQUIRED & DEFERRED NR 1 DISPLAY COOLING FAN IAW MEL 21-24-2C. ENTERED INTO MM02. MXC 1390 NOTIFIED. PULLED AND COLLARED C/B U2-- REMOVED AND REPLACED NR 1 DISPLAY SUPPLY FAN B12 P/N AE0804A04, S/N OFF 01185, S/N ON 01048 IAW AMM 21-24-12. CLEARED FROM MM02, MXC NOTIFIED 0782.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 11,527 hrs · 7,192 cycles

280 CIRCUMFERENTIAL JOINT CORRODED BETWEEN STR 26L AND 26R. A251-048. REPAIRED 280 CIRCUMFERENTIAL JOINT BETWEEN STR 26L AND STR 26R IAW CRJ900 REO# 690-53-21-443 AND EO#R53317.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 11,527 hrs · 7,192 cycles

RBL 12 CRACKED JUST FWD OF 280 BEAM. REPAIRED RBL 12 BEAM IAW EO#R53314.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 11,527 hrs · 7,192 cycles

LOWER VHF ANTENNA DOUBLER CORRODED BETWEEN FS 295 AND FS 310. REMOVED CORROSION LWR VHF ANTENNA BETWEEN FS 295 & FS 310. FOUND WITHIN LIMITS IAW CRJ900 SRM 51-21-06. EO#R53277.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 11,527 hrs · 7,192 cycles

LBL 12 CRACKED JUST FWD OF 280 BEAM. REPAIRED LBL 12 BEAM IAW EO#R53314.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 11,527 hrs · 7,192 cycles

FWD EQUIPMENT BAY FLOOR IS CRACKED IN CORNER CUTOUT AT FS 193.00 RIGHT SIDE. REPAIRED FWD EQUIPMENT BAY FLOOR CORNER CUTOUT AT FS 193.00 RIGHT SIDE IAW EO #R53316.

Part: CROSSBEAM — CORRODED (FUSELAGE) · airframe 11,527 hrs · 7,192 cycles

LEFT 280 CROSSBEAM CORRODED A251-053. REMOVED AND REPLACED LEFT FS 280 BEAM IAW EO R53315&R53127 & R53117.

Part: CROSSBEAM — CORRODED (FUSELAGE) · airframe 11,527 hrs · 7,192 cycles

RIGHT 280 CROSSBEAM CORRODED A251-053. REMOVED AND REPLACED RIGHT FS 280 BEAM IAW EO#R53158&R53127 & R53117. P/N CC670-34094-25.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 11,527 hrs · 7,192 cycles

280 CROSSBEAM SPLICE IS CORRODED. A251-051. REMOVED AND REPLACED 280 CROSSBEAM SPLICE IAW CRJ900 SRM 51-42-06. P/N CC670-34095-35.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 11,509 hrs · 7,182 cycles

ALL THREE CEILING PANEL EMERGENCY LIGHTS AFT OF OVERWING EXIT DOORS AND BOTH RT AND LT AFT OF WING EMERGENCY EXTERIOR LIGHTS FAIL TO STAY ON. REMOVED AND REPLACED EMERGENCY BATTERY PACK 4 IAW CRJ900 AMM 33-51-17. OPS TEST S/W OF EMERGENCY LIGHTS IAW CRJ900 AMM 33-51-00. OPS CHECK GOOD.

Part: LIGHT — LOOSE (CABIN) · airframe 11,223 hrs · 6,999 cycles

THERE IS A LOOSE FLUORESCENT STRIP AROUND EMERGENCY EXIT ROWS 12CD. RE-INSTALLED FLUORESCENT TRACK STRIP FOR SEAT 12CD IAW CRJ900 AMM 33-51-01. OPS CHECK GOOD.

Part: FLASHLIGHT — MISSING (COCKPIT) · airframe 11,165 hrs · 6,967 cycles

MISSING YELLOW FLASHLIGHT FROM FLT DECK. COCKPIT YELLOW FLASHLIGHT DEFERRED PER MEL 25-61-4A. ENTERED INTO MM02 MXOC NOTIFIED. PLACARD INSTALLED. REPLACED BATTERY POWERED FLASHLIGHT, FLIGHT DECK AS REQUIRED. PLACARD REMOVED, REMOVED FROM MM02, MXC NOTIFIED 52994.

Part: LIGHT — DAMAGED (CABIN) · airframe 9,869 hrs · 6,158 cycles

INSPECTION OF THE EMERGENCY FLOOR TRACK LIGHTING IN THE FORWARD GALLEY AREA FOUND DAMAGED. REMOVED AND REPLACED BOTH SIDES, IN FRONT OF GALLEY CARTS IAW MM 33-51-01.

Part: LIGHT — LOOSE (CABIN) · airframe 9,869 hrs · 6,158 cycles

CREW REPORTED FLOOR TRACK LIGHT STRIP IN GALLEY LOOSE. REPLACED DAMAGED SECTION OF FLOOR TRACK LIGHT PER AMM 33-51-01.

Part: SKIN — DENTED (FUSELAGE) · airframe 7,564 hrs · 4,726 cycles

LT AFT FUSELAGE DENTED 6 FT AFT OF CARGO DOOR AND 36 INCHES BELOW LT ENGINE NACELLE. DENT IS APPROX .7500 TO 1 INCH IN DEPTH AND 8 INCHES IN DIAMETER. RIVETS ARE POPPED AND OTHERS STRESSED. REPAIRED FUSELAGE SKIN AND STRINGER AT FS 1108-1098, STRINGER 14L - 15L IAW REO 690-53-61-190.

Part: SKIN — GOUGED (BS 1047) · airframe 7,564 hrs · 4,726 cycles

1 INCH LONG VERTICAL GOUGE ON EXTERNAL SKIN AT FS 1047.00 AND BETWEEN S21 AND 23L. COMPLIED WITH REO 690-53-61-192-C AND EO R53137.

Part: SIGN — BROKEN (EMERGENCY LIGHT) · airframe 7,038 hrs · 4,398 cycles

EMERGENCY EXIT SIGN ABOVE SERVICE DOOR BROKE LOOSE. INSTALLED NEW EXIT SIGN ASSY ABOVE SERVICE DOOR, PN BF5-0382-901.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 6,821 hrs · 4,276 cycles

NOTED GENERAL VICINITY, LT GALLEY ARE EMERGENCY FLOOR PATH LIGHTING DEGRADED. R & R LT GALLEY EMERGENCY FLOOR PATH LIGHTING. REF AM 3-51, OPS CHECKS GOOD.

Part: GLOWSTRIP — DETACHED (CABIN) · airframe 6,608 hrs · 4,156 cycles

EMERGENCY FLOOR GLOW IN THE DARK STRIP HAS BECOME DETACHED IN FRONT OF GALLEY CART. RESECURED EMERGENCY FLOOR GLOW STRIP.

Part: DOOR FRAME — GOUGED (FUSELAGE) · airframe 6,509 hrs · 4,099 cycles

DOOR FRAME UPPER AFT GOUGED. REPAIRED AFT UPPER DOOR SEALS USING REO 670-53-22-001 TYPE 1 AS REF.