N135EV

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 36,708 hrs · 26,860 cycles

THE RT FS 280 FLOORBEAM HAS DEEP CORROSION AND REQUIRES REPLACEMENT. REMOVED BS 280 RT FLOORBEAM IAW SRM 51-42-06-001-001-A01, SRM 51-42-13-001-001-A01, SRM 51-42-21-001-001-A01, INSTALLED A NEW RT BS 280 FLOORBEAM, IAW SRM 51-42-06-001-001-A01, SRM 51-42-13-001-001-A01, SRM 51-42-21-001-001-A01, AND SRM 51-42-22-001-001-A01. LOCATED AND DRILLED NEW RT BS 280 FLOORBEAM IAW SRM 51-40-11-001-001-A01, APPLIED CIC IAW SRM 51-21-11-001-001-A01.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 36,708 hrs · 26,860 cycles

THE LH FS 280 FLOOR BEAM HAS DEEP CORROSION AND REQUIRES REPLACEMENT REMOVED FS280.00 LH CROSSBEAM IAW CRJ-900 SRM 51-42-06-001-001-A01, SRM 51-42-13-001-001-A01, SRM 51-42-21-001-001-A01 INSTALLED NEW LH FS 280 CROSSBEAM PN CC670-34094JP-1S IAW SRM 51-42-06-001-001-A01, SRM 51-42-13-001-001-A01, SRM 51-42-21-001-001-A01 AND SRM 51-42-22-001-001-A01. LOCATED AND DRILLED NEW LH FS 280 CROSSBEAM PN CC670-34094JP-1S IAW CRJ 900 SRM 51-40-11-001-001-A01APPLIED CIC ON FS 280 BEAMS IAW CRJ 900 SRM 51-21-11-001-001-A01.

Part: DIAPHRAGM — CORRODED (ZONE 100) · airframe 36,708 hrs · 26,860 cycles

LAVATORY STRUCTURAL LANDING BELOW FWD LAV SERVICE PORT IS CORRODED. LAVATORY DIAPHRAGM IS OUT OF LIMITS IAW SRM 53-21-23-101-005-A02, DUE TO MORE THAN 30 PERCENT OF THE LENGTH OF A MEMBER IS CORRODED. LOCATED AND DRILLED A NEW SERVICEABLE FWD LAVATORY DIAPHRAGM IAW SRM 51-40-11-001-001-A01. INSTALLED THE NEW SERVICEABLE FWD LAVATORY DIAPHRAGM IAW SRM 51-42-06-001-001-A01, INSTALLED SAME SERVICEABLE ANGLE FROM BS 394, STR 23R PN SH670-32287-3 IAW SRM 51-42-06-001-001-A01. INSTALLED SAME SERVICEABLE IMPACT ANGLE FROM FWD LAVATORY IAW SRM 51-42-06-001-A01. INSTALLED DRAIN VALVE FROM FWD LAVATORY IAW AMM 38-31-20-400-802-A01. INSTALLED THE HEATED GASKET FROM THE TOILET DRAIN ASSY FROM FWD LAV IAW AMM 38-31-15-400-803-A01. INSTALLED THE RINSE-FILL VALVE FROM FWD LAV IAW AMM 38-31-08-400-802-A01. INSTALLED THE UPPER DRAIN FROM FWD LAV IAW AMM 38-31-19-400-802-A01. R & R FOR A NEW SERVICEABLE SEAL PLATE SH670-32319-1, INSTALLED IN COMMON WITH FWD LAV DIAPHRAGM IAW SRM 51-42-06-001-001-A01. PREFORMED LEAK TEST IAW AMM 38-10-00-790-802-A01. NO LEAKS FOUND AT TIME OF TEST.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 36,708 hrs · 26,860 cycles

F.S. 280 FWD J ANGLE IS CORRODED. REMOVED 280 J ANGLE IAW CRJ 900 SRM 51-42-06-001-001-A01, AND 51-42-21-001-001-A01. LOCATED AND DRILLED NEW J-ANGLE AT FS280, P/N: CC670-34095-1S, IAW CRJ-900 SRM 51-40-11-001-001-A01. INSTALLED NEW J-ANGLE AT FS280, P/N: CC670-34095-1S, IAW CRJ-900 SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01.

Part: ANGLE — CORRODED (ZONE 200) · airframe 36,708 hrs · 26,860 cycles

BS 280 FWD J ANGLE IS CORRODED. REMOVED THE J ANGLE IAW SRM 51-42-06-001-001-A01, & 51-42-21-001-001-A01. LOCATED AND DRILLED NEW J-ANGLE AT FS280, P/N: CC670-34095-1S, IAW CRJ-900 SRM 51-40-11-001-001-A01. INSTALLED NEW J-ANGLE AT FS280, P/N: CC670-34095-1S, IAW CRJ-900 SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01.

Part: DOOR — CRACKED (ZONE 800) · airframe 34,458 hrs · 24,999 cycles

LH AFT EE DOOR FWD LUG IS SUSPECTED TO BE CRACKED. REQUIRES EVAL COMPLIED WITH ENDEAVOR AIR EA CRJ952-17932 REV IR 12/10/2024

Part: DOOR — CRACKED (ZONE 800) · airframe 34,458 hrs · 24,999 cycles

R/H AFT EMERGENCY EXIT DOOR AFT LUG CRACKED. COMPLIED WITH ENDEAVOR AIR EA CRJ952-17933 REV IR 12/10/2024.

Part: DOOR — CRACKED (ZONE 800) · airframe 34,458 hrs · 24,999 cycles

LH FWD EE DOOR FWD LUG IS SUSPECTED TO BE CRACKED. REQUIRES EVAL COMPLIED WITH ENDEAVOR AIR EA CRJ952-17934 REV IR 12/10/2024.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 34,458 hrs · 24,999 cycles

CORROSION FOUND ON FLOOR SILL LEFT HAND SIDE AT FS 792 AND FS 801 ON THE OUTBOARD HOLES. COMPLIED WITH MHIRJ REO 690-53-41-506 REV-- DATED 2024-12--09

Part: NONE — NONE (NONE) · airframe 34,458 hrs · 24,999 cycles

WHILE PERFORMING SERVICE BULLETIN 670BA-53-044 REVISION G, DATED JUL05/2022 FOUND FITTINGS AT STR12A LH AND RH SIDES PN CC670-33563-001SB AND CC670-33562-001SB CANNOT BE INSTALLED AS DESCRIBED IN SERVICE BULLETIN DUE TO AIRCRAFT EXISTING FASTENER PITCH COMPLIED WITH MHIRJ REO 690-53-11-1896 REV-- DATED 2024-12--08

Part: TERMINAL BLOCK — BURNED (WINDSHIELD) · airframe 30,660 hrs · 21,656 cycles

AT 3500 MSL COCKPIT CREW NOTED METALLIC BURNING SMELL AND SMOKE FROM LOWER LEFT CORNER OF CAPTAINS WINDSHIELD NEAR VENT/POWER ELEMENT. CLEANED AND RESECURED LOOSE WIRES TO THE TERMINAL BLOCK REF AMM 56-11-01. PERFORMED OPS CHECK OF THE WINDOW TEMP CONTROLLER IAW AMM 30-41-06. LET WINDSHIELD RUN FOR 30 MINS WITH NO ISSUES. OPS CHECK GOOD.

Part: LAMP — INOPERATIVE · airframe 30,052 hrs · 21,155 cycles

R/H AFT EXTERIOR EMERG LIGHT INOP REMOVED AND REPLACED R/H AFT EXTERIOR EMERG LIGHT BULB IAW AMM 33-51-15. OPS CHECK GOOD. P/N: 8GH002473-08

Part: FAIRING — CRACKED · airframe 29,443 hrs · 20,661 cycles

RH ENGINE UPPER COWL HINGE LINE FAIRING 443BT CRACKED PERFORMED REPAIR ON RH ENGINE UPPER COWL HINGE LINE FAIRING PER EA CRJ954-12492 REV D DATED 05/24/2022

Part: HINGE — CORRODED · airframe 29,443 hrs · 20,661 cycles

PAX DOOR STEP 832ET, UPPER HINGE HAS AREAS OF CORROSION CA REMOVED CORRODED UPPER HINGE AND REPLACED WITH NEW HINGE PER CRJ900 SRM 51-42-06-001-001-A01

Part: STRINGER — CORRODED · airframe 29,443 hrs · 20,661 cycles

STGR 21R AT FS 364.00 TO FS 379.00 CORROSION PERFORMED REPAIR ON STGR 21R AT FS 364.00 TO FS 379.00 PER EA CRJ953-13542 REV IR DATED 05/05/2022

Part: STRINGER — CORRODED · airframe 29,443 hrs · 20,661 cycles

STGR 21R AT FS 394.00 TO FS 409.00 CORROSION PERFORMED REPAIR ON STGR 21R AT FS 394.00 TO FS 409.00 PER EA CRJ953-13543 REV IR DATED 05/09/2022

Part: STRINGER — CORRODED · airframe 29,443 hrs · 20,661 cycles

STGR 20R AT FS 437.00 TO FS 453.00 CORROSION PERFORMED REPAIR ON STGR 20R FS 437.00 TO FS 453.00 PER EA CRJ953-13568

Part: STRINGER — CORRODED · airframe 29,443 hrs · 20,661 cycles

STGR 20R AT FS 394.00 TO 409.00 CORROSION PERFORMED REPAIR ON STGR 20R AT FS 394.00 TO 409.00 PER EA CRJ953-13497 REV IR DATED 05/03/2022

Part: STRINGER — CORRODED · airframe 29,443 hrs · 20,661 cycles

STGR 19R AT FS 364.00 TO FS 379.00 HAS SIGNS OF CORROSION ON UPPER SURFACE PERFORMED REPAIR ON STGR 19R AT FS 364.00 TO FS 379.00 PER EA CRJ953-13544 REV IR DATED 05/06/2022

Part: STRINGER — CORRODED · airframe 29,443 hrs · 20,661 cycles

STGR 25R FS280.00 TO FS364.00 CORROSION PERFORMED REPAIR ON STGR 25R FROM FS 280.00 TO FS 364.00 PER EA CRJ953-12932 REV IR DATED 2/16/2022 AND CRJ953-12933 REV IR DATED 2/16/2022

Part: SPLICE — CORRODED · airframe 29,443 hrs · 20,661 cycles

STGR 20R AT FS 477.00 CORRODED. REMOVED CORRODED JOINT SPLICE ON STGR 20R AT FS 477.00 AND REPLACED WITH NEW JOINT SPLICE ER CRJ900 SRM 51-21-06 AND 51-42-21

Part: STRINGER — CORRODED · airframe 29,443 hrs · 20,661 cycles

"STGR 24R FS 280.00 TO FS 349.00 HAS SEVERAL PITS AROUND FASTENER TAILS. " PERFORMED REPAIR ON STGR 24R FROM FS 280.00 TO FS 364.00 PER EA CRJ953-13023 REV IR DATED 3/3/2022 AND EA CRJ953-12015 REV IR DATED 3/2/2022.

Part: WEB — CRACKED · airframe 29,443 hrs · 20,661 cycles

SUSPECTED CRACK ON PAX DOOR AFT WEB SKIN DRAG ANGLE PERFORMED REPAIR ON PAX DOOR AFT WEB SKIN DRAG ANGLE PER CRJ900 SRM 52-11-04-201-002-A01.

Part: SEAL — TORN · airframe 29,443 hrs · 20,661 cycles

CREW ESCAPE HATCH HAS TORN SEAL REMOVED, REPLACED, AND LUBRICATED CREW ESCAPE HATCH IAW CRJ900 AMM 52-22-07, AMM 12-20-52, AMM 52-22-00

Part: STRINGER — CORRODED · airframe 29,443 hrs · 20,661 cycles

REPAIR REQUIRED ON STRINGER 21R FROM FS 333.00 TO FS 349.00 DUE TO CORROSION. PERFORMED REPAIR ON STRINGER 21R FROM FS 333.00 TO FS 349.00 PER EA CRJ953-13183 REV IR DATED: 4/9/2022

Part: STRINGER — CORRODED · airframe 29,443 hrs · 20,661 cycles

STGR 21R FROM FS 310.00 TO FS 333.00 CORRODED PERFORMED REPAIR ON STRINGER 21R FROM FS 310.00 TO FS 333.00 PER EA CRJ953-13182 REV IR DATED: 4/9/2022

Part: BEAM — CRACKED · airframe 29,443 hrs · 20,661 cycles

PAX DOOR AFT GAS SPRING SUPPORT BEAM CRACKED REMOVED CRACKED PAX DOOR GAS SPRING SUPPORT BEAM AND REPLACED WITH NEW BEAM. REF. CRJ900 SRM 51-42-06-001-001-A01

Part: PLATE — WORN · airframe 29,443 hrs · 20,661 cycles

EXCESSIVE WEAR ON PAX DOOR FWD AND AFT GUIDE PLATE BLENDED OUT LIGHT WEAR ON PAX DOOR FWD AND AFT GUIDE PLATES PER CRJ900 SRM 52-11-06-201-001-A01

Part: NONE — WORN · airframe 29,443 hrs · 20,661 cycles

RH ENGINE LOWER CORE COWL RUB STRIP HAS HEAVY WEAR REMOVED WORN RH ENG. LOWER CORE COWL RUB STRIP AND REPLACED WITH NEW RUB STRIP PER EA CRJ954-13184 REV A DATED: 4/5/2022.

Part: CHANNEL — CRACKED · airframe 29,443 hrs · 20,661 cycles

AFT CARGO DOOR AFT TRACK LOWER U-CHANNEL SUPPORT BRACKET CRACKED REMOVED CRACKED U-CHANNEL BRACKET ON AFT CARGO DOOR AFT LOWER TRACK AND REPLACED WITH NEW BRACKET PER CRJ900 SRM 51-42-06-001-001-A01

Part: STRINGER — CORRODED · airframe 29,443 hrs · 20,661 cycles

STRINGER 22R AT FS 333.00 CORRODED REMOVED AND REPLACED DAMAGED STRINGER 22R AT FS 333.00 PER CRJ900 SRM 51-42-21-001-001-A01.

Part: STRINGER — CORRODED · airframe 29,443 hrs · 20,661 cycles

STRINGER 26L BETWEEN FS 280.00 TO FS 364.00 CORRODED PERFORMED REPAIR ON STRINGER 26L BETWEEN FS 280.00 TO FS 364.00 PER EA CRJ953-12941 REV IR DATED 2/17/2022

Part: STRINGER — CORRODED · airframe 29,443 hrs · 20,661 cycles

STRINGER 26R BETWEEN FS 280.00 TO FS 364.00 HAS CORROSION AROUND SEVERAL FASTENER TAILS. PERFORMED REPAIR ON STRINGER 26R BETWEEN FS 280.00 TO FS 364.00 PER ENGINEERING AUTHORIZATION CRJ953-12934 REV IR DATED 2/16/2022.

Part: LIGHT — WORN (CABIN) · airframe 23,042 hrs · 15,538 cycles

SEVERAL EMERGENCY LIGHT STRIPS WERE WORN THROGHOUT THE CABIN. REPLACED IAW AMM 33-51-01-400-801, STEP A.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 23,042 hrs · 15,538 cycles

PAX DOOR EXTERNAL EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE BULB IAW AMM 33-51-15. OPS TESTED GOOD IAW AMM 33-51-15-710-801.

Part: INTERCOSTAL — CRACKED (PASSENGER DOOR) · airframe 23,042 hrs · 15,538 cycles

AFTER REMOVAL OF PAX DOOR INNER SKIN FOUND AFT LOWER INTERCOSTAL DENTED AND CRACKED. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-40-11, 51-42-06, AND 51-42-21.

Part: INTERCOSTAL — CRACKED (PASSENGER DOOR) · airframe 23,042 hrs · 15,538 cycles

AFTER REMOVAL OF PAX DOOR INNER SKIN FOUND AFT UPPER INTERCOSTAL DENTED AND CRACKED. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-40-11, 51-42-06, AND 51-42-21.

Part: FITTING — CRACKED (PASSENGER DOOR) · airframe 23,042 hrs · 15,538 cycles

PASSENGER DOOR MACHINED LINTLE CRACKED AT BS 282. REPAIRED LINTLE IAW REO 670-53-21-493, REV D.

Part: FRAME — CORRODED (BS 333) · airframe 23,042 hrs · 15,538 cycles

FRAME AT BS 333, STRINGER 27 WAS FOUND CORRODED. RPAIRED THE FRAME IAW SRM 53-00-06.

Part: INTERCOSTAL — CRACKED (PASSENGER DOOR) · airframe 23,042 hrs · 15,538 cycles

AFTER REMOVAL OF THE PAX DOOR INNER SKIN, FOUND FWD, UPPER INTERCOSTAL WAS DENTED AND CRACKED. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-42-06, AND 51-42-21.

Part: FLOOR SUPPORT — CORRODED (BS 1015-1031) · airframe 23,042 hrs · 15,538 cycles

AFT CARGO, LBL 27 FLOOR SUPPORT WAS CORRODED, BS 1031 - 1015. REMOVED THE CORRODED SECTION OF THE FLOOR SUPPORT AND INSTALLED A REPAIR IAW REO 670-53-00-029.

Part: HINGE — CRACKED (DOOR STEP) · airframe 23,042 hrs · 15,538 cycles

PAX DOOR TOP STEP 832ET INBD HINGE WAS CRACKED AND CORRODED. REMOVED & REPLACED THE DOOR STEP HINGE IAW AMM 53-11-04.

Part: ATTACH BRACKET — CRACKED (NOSE HYD BAY) · airframe 23,042 hrs · 15,538 cycles

NOSE HYDRAULIC COMPARTMENT, UPPER ACCUMULATOR, FWD ATACHMENT BRACKET CRACKED. REPLACED THE ATTACH BRACKET IAW SRM 51-42-21.

Part: STEP — CRACKED (PASSENGER DOOR) · airframe 23,042 hrs · 15,538 cycles

PAX DOOR MID STEP WAS CRACKED, LT SIDE. REMOVED THE CRACK AND FOUND WITHIN LIMITS IAW SRM 52-11-04.

Part: OXYGEN MASK — LEAKING (COCKPIT) · airframe 22,013 hrs · 14,791 cycles

OBSERVER`S OXYGEN MASK LEAKING. R & R THE OBSERVER`S OXYGEN MASK IAW AMM 35-11-12, OPS CHECKED GOOD.

Part: CONNECTOR — DEFECTIVE (BLEED LOOP) · airframe 21,915 hrs · 14,719 cycles

L BLEED DUCT WARNING CAME ON IN CRUISE FLIGHT, FOLLOWED BY RAPID DECENT TO 10000' FOLLOWED QRH CHECKLIST SUCCESSFULLY. AIRCRAFT LANDED UNEVENTFULLY. REPLACED ELBOW CONNECTIONS LT BLEED LOOP A, MT137P2, MT202P2, AND LOOP B MT203P1 IAW AMM 36-21-01 OPS TEST GOOD P/N ON/OFF 35201-9MT SEE NRWC 630626 FOR DETAILS. EMERGENCY WAS DECLARED BY THE CREW.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 21,788 hrs · 14,622 cycles

EMERGENCY LIGHTS IN GALLEY RT SIDE FWD & AFT HAVE BULBS OUT. REPLACED THE BULBS, OP TESTED GOOD IAW AMM 33-51-00. P

Part: SMOKE DETECTOR — FALSE ACTIVATION (AFT LAVATORY) · airframe 21,686 hrs · 14,555 cycles

WARNING MESSAGE FOR SMOKE AFT LAVATORY. REMOVED AND REPLACED THE AFT LAVATORY SMOKE DETECTOR IAW AMM 26-16-01. OPS CHECKED GOOD.

Part: SMOKE DETECTOR — FALSE ACTIVATION (FWD LAVATORY) · airframe 21,686 hrs · 14,555 cycles

WARNING MESSAGE SMOKE FWD LAVATORY. REMOVED AND REPLACED THE FWD LAVATORY SMOKE DETECTOR IAW AMM 26-16-01. OPS CHECKED GOOD.

Part: HOUSING — CRACKED (E/E DOOR HANDLE) · airframe 21,684 hrs · 14,553 cycles

MAIN AVIONICS BAY DOOR HANDLE HOUSING CRACKED. REMOVED THE DOOR HANDLE HOUSING AND INSTALLED A NEW HOUSING IAW SRM 51-42-21-001-001. OPS CHECKED IAW AMM 52-42-00-710-801. OPS CHECK GOOD.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 21,684 hrs · 14,553 cycles

WHILE PERFORMING DRAG ANGLE REPAIR FOUND STIFFNER COMMON TO THE REPAIR AREA DAMAGED. REMOVED AND REPLACED THE STIFFNER IAW SRM 51-42-06.

Part: SIGN — CRACKED (MAIN CABIN) · airframe 21,300 hrs · 14,263 cycles

FWD SERVICE DOOR EMERGENCY EXIT LIGHT LENS CRACKED AND LIGHT ASSY DAMAGED. "REMOVED DAMAGED LIGHT LENS ASSY FWD SERVICE DOOR EMERGENCY EXIT SIGN IAW CRJ900 AMM 33-51-05-000-801 4B. A13 CONFIG. INSTALLED NEW FWD SERVICE DOOR EMERGENCY EXIT LENS AND LIGHT ASSEMBLY IAW CRJ900 AMM 33-51-05-400-801 A13 ITEM 4B. OPS CHECK IS GOOD.

Part: ELEVATOR — DAMAGED (RIGHT) · airframe 21,259 hrs · 14,231 cycles

RIGHT ELEVATOR TRAILING EDGE DAMAGED. FABRICATED A REPAIR. ALODINE AND PRIMED THE REPAIR DOUBLER, AND FILLER. TOUCHED UP CUTLINES, AND CLEANED REPAIR AREA IAW SRM 55-21-01.

Part: DOOR — BINDING (MAIN PAX) · airframe 18,513 hrs · 12,282 cycles

FA REPORTS DIFFICULTY IN OPENING MAIN PASSENGR DOOR. DOOR LEVER HAD TO BE OPENED 3 TIMES BEFOR DOOR WOULD OPEN. DOOR ALSO RATTLES WHEN OPENED. PREFORMED OPERATIONAL TEST OF PAX DOOR MULTIPLE TIMES AND OPS CHECKED GOOD IAW AMM 52-11-00.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 17,433 hrs · 11,500 cycles

EXIT SIGN UNDER FORWARD F/A JUMPSEAT MISSING COVER. REPLACED LENS FOR FLOOR FLOOD LIGHT ENTRANCE IAW AMM 33-51-11.

Part: MEGAPHONE — INOPERATIVE (AFT CABIN) · airframe 17,250 hrs · 11,361 cycles

AFT F/A MEGAPHONE INOPERATIVE. R & R THE MEGAPHONE IAW AMM 25-61-14. OPS CHECKED GOOD.

Part: MEGAPHONE — UNKNOWN (CABIN) · airframe 15,381 hrs · 10,002 cycles

PASSENGER COMPARTMENT MEGAPHONE REQUIRES REPLACEMENT. WORK COMPLETED IAW N/R-00003. R & R PASSENGER COMPARTMENT MEGAPHONE AND BRACKET IAW AMM 25-61-14 AND AIPC REF 25-61-14, FIG 1K ITEM 5.

Part: ANGLE — CORRODED (SERVICE DOORWAY) · airframe 15,358 hrs · 9,984 cycles

WHILE PERFORMING EVALUATION ON SERVICE DOOR SILL MOUNTING ANGLE, FOUND UPPER MOUNTING ANGLE TO BE CORRODED. REMOVED UPPER MOUNTING ANGLE FROM SERVICE DOOR DUE TO IT BEING OUT OF LIMITS IAW SRM 53-21-23-101-001-A02 AND 51-42-06-001-001-A01. INSTALLED NEW ANGLE MOUNT ON SERVICE DOOR SILL IAW SRM 51-42-06-001-001-A01.

Part: DOOR SILL — CORRODED (SERVICE DOORWAY) · airframe 15,358 hrs · 9,984 cycles

SERVICE DOOR SILL MOUNTING ANGLE HAS CORROSION. EVALUATED DAMAGE AND FOUND AREA TO BE OUT OF LIMITS IAW SRM 53-21-23-101-001-A02. REMOVED 4 EA PROTECTOR WEBS FOR THE FLOOR PLATE AND SILL MOUNTING ANGLE FROM SERVICE DOOR IAW SRM 51-42-06-001-001-A01, AND 51-42-21-001-001-A01. INSTALLED NEW SERVICE DOOR SILL MOUNTING ANGLE IAW SRM 51-42-06-001-001-A01, AND DWG SH 680-31950 LOCATED, DRILLED AND INSTALLED 4 EA SERVICEABLE PROTECTOR WEBS AND 4 EA SERVICEABLE CLIPS AT SERVICE DOOR SILL REF: SRM 51-48-06-001-001-A01 AND DWG SH670-31950.

Part: STRINGER — CORRODED (BS 364 S26R) · airframe 15,358 hrs · 9,984 cycles

WHILE REMOVING CORROSION ON BS 364 INTERCOSTAL S26R FOUND CORROSION ON STRINGER S26R BETWEEN FS 364-FS 349. HEAVY PITTING CORROSION ON STR 26R BETWEN FS 364-FS 349 EXCEEDING LIMITS OF SRM 53-21-03-101-006-A02. STARTED REMOVAL OF STR 26R REF SRM 51-42-06-001-A01. CONTINUED AND COMPLETED REMOVAL OF STR 26R FROM FS 364- FS 333 REF: SRM 51-42-06-001-001-A01, SEE ITEM 6 FOR INSTALLATION OF SERVICEABLE STR. REMOVED INTERCOSTAL AT FS 364-FS 349, STR 26R FOR FOM REMOVED 2 EA CLIPS 1 AT FS 349 AND 1 AT FS 333 STR 26R TO FOM REF SRM 51-42-06-001-001-A01. INSTALLED STRINGE CLIP AT FS 333 STR 26R IAW SRM 51-42-06-001-001-A01. REINSTALLED RIVETS AT FS 349 BETWEEN STRINGER 27 AND 25R IAW SRM 51-42-06-001-001-A01. REMOVED STR 26R SPLICE AT FS 333 SPLICE FOUND CORRODED REF: SRM 51-42-06-001-001-A01. LOCATED AND DRILLED HOLES IN NEW SERVICEABLE STR 26R SPLICE AT FS 333 IAW SRM 51-40-11-001-001-A01. INSTALLED STRINGER SPLICE IAW CRJ900 SRM 51-42-06-001-001-A01. INSTALLED SERVICEABLE STR 26R REF: SRM 51-42-06-001-001-A01. LOCATED AND DRILLED HOLES IN NEW SERVICEABLE STR 26R BETWEEN FS 333 AND 364 IAW SRM 51-40-11-001-001-A01. INSTALLED STRING 26R IAW SRM 51-42-06-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 785-847) · airframe 15,358 hrs · 9,984 cycles

LT SIDE SEAT TRACK CORRODED FROM BS 785.15 - 847+16. FOUND TO BE OUT OF LIMITS SRM 53-41-51-101-001-A02. R & R THE SEAT TRACK IAW AMM 53-00-49-000-801-A11 AND 53-00-49-400-801-A11.

Part: SEAT TRACK — CORRODED (BS 744-761) · airframe 15,358 hrs · 9,984 cycles

RT SIDE SEAT RAIL CORRODED FROM BS 744.15 - 761.85. REMOVED THE SEAT TRACK IAW AMM 53-00-49-000-801, A11. INSTALLED NEW, SERVICEABLE SEAT TRACK IAW AMM 53-00-49-400-801, A11.

Part: SEAT TRACK — CORRODED (BS 720) · airframe 15,358 hrs · 9,984 cycles

RT SIDE SEAT TRACK CORRODED AT FS 720.85. R & R THE SEAT TRACK IAW AMM 53-00-49-000-801 A11 AND 53-00-49-400-801-A011.

Part: SEAT TRACK — CORRODED (BS 785-847) · airframe 15,358 hrs · 9,984 cycles

RT SIDE SEAT TRACK CORRODED FROM BS 785.15 - 847+16. BLENDED CORROSION IAW SRM 51-21-06-001-001-A01. FOUND TO BE OUT OF LIMITS IAW SRM 53-41-51-101-001-A02. REMOVED THE SEAT TRACK IAW AMM 53-00-49-000-801-A11. INSTALLED NEW SERVICEABLE SEAT TRACK IAW AMM 53-00-49-400-801-A11.

Part: FLOORBEAM — CORRODED (BS 349) · airframe 15,358 hrs · 9,984 cycles

BS 349 FLOORBEAM CORRODED AT RBL 8. R & R FLOORBEAM IAW SRM 51-42-06-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 661-677) · airframe 15,358 hrs · 9,984 cycles

SEAT TRACK FROM BS 661.00+62 - 677 AT LBL 27 CORRODED IN SEVERAL PLACES. BLENDED CORROSION AND FOUND OUT OF LIMITS IAW SRM 51-21-06-001-001-A01 AND REO 670-53-00-013. REMOVED SEAT TRACK IAW AMM TASK 53-00-49-000-801-A11. LOCATED AND DRILLED HOLES IN NEW SEAT TRACK EXTRUSTION IAW SRM 51-40-11-001-001-A01. INSTALLED SEAT TRACK IAW AMM 53-00-49-400-801, CONFIG A11.

Part: INTERCOSTAL — CORRODED (BS 364) · airframe 15,358 hrs · 9,984 cycles

FS 364 INTERCOSTAL AT 26R HAS CORROSION. REMOVED CORROSION ON VERTICAL LEG IAW SRM 51-21-06-001-001 AND 51-12-00-001-001-A01 TR 51-0050. SUBMITTED TO ENGINEERING FOR PERMANENT DISPOSITION REF SRM 51-13-01-001-001-A01. COMPLIED WITH FA 32-2015-137.

Part: INTERCOSTAL — CORRODED (BS 634) · airframe 15,358 hrs · 9,984 cycles

FS 364 INTERCOSTAL AT 27L HAS CORROSION. REMOVED CORROSION IAW SRM 51-12-00-001-001-A01 AND 51-21-23-101-003-A01. SUBMITTED FOR PERMANENT DISPOSITION REF: SRM 51-13-01-001-001-A01. COMPLIED WITH EA 32-2015-135.

Part: SEAT TRACK — CORRODED (BS 681-661) · airframe 15,358 hrs · 9,984 cycles

SEAT TRACK FROM BS 581 - 661+62 AT LBL 27 CORRODED IN SEVERAL PLACES. REMOVED CORROSION FROM SEAT TRACK. FOUND TO BE OUT OF LIMITS IAW REO 670-53-00-013. R & R THE SEAT TRACK IAW AMM 53-00-49-000-801-A11 AND 53-00-49-400-801-A11.

Part: SEAT TRACK — CORRODED (BS 661-677) · airframe 15,358 hrs · 9,984 cycles

SEAT TRACK FROM BS 661 + 62 - 677 RBL 27 CORRODED IN SEVERAL PLACES. SEAT TRACK FOUND TO BE OUT OF LIMITS IAW REO 670-53-00-13. REV J. R & R THE CORRODED SEAT TRACK IAW AMM 53-00-49-000-801-A11, AND 53-00-49-400-801-A11.

Part: FRAME — CORRODED (BS 319) · airframe 15,358 hrs · 9,984 cycles

FRAME BS 319, FWD SIDE CORRODED 26L-26R. REMOVED CORROSION ON FRAME IAW SRM 51-21-06-001-001-A01.

Part: FRAME — CORRODED (BS 333) · airframe 15,358 hrs · 9,984 cycles

FRAME BS 333 FWD SIDE CORRODED STR 27. REMOVED CORROSION IAW SRM 53-21-06-001-001-A01 AND 51-12-00-001-001-A01. NO DAMAGED ALLOWED ON FRAME IAW SRM 53-21-06-101-006-A02. COMPLIED WITH ECTC EA 32-2015-144.

Part: SEAT TRACK — CORRODED (BS 364-477) · airframe 15,358 hrs · 9,984 cycles

SEAT TRACK BS 364-477.40, LBL 27 HAS CORROSION DAMAGE. R & R CORRODED SEAT TRACK WITH NEW SERVICABLE SEAT TRACK IAW SRM 51-41-02-001-001-A01.

Part: INTERCOSTAL — CORRODED (BS 364) · airframe 15,358 hrs · 9,984 cycles

FS 364, INTERCOSTAL AT 27R HAS CORROSION. REMOVED CORROSION AT FS 364, 27R IAW SRM 51-12-00-001-001-A01 & 51-21-06-001-001-A01. SUBMITTED TO ENGINEERING FOR PERMANENT DISPOSITION REF SRM 51-13-01-001-001-A01. COMPLIED WITH EA 32-2015-136.

Part: LAP JOINT — CORRODED (BS 280-282) · airframe 15,358 hrs · 9,984 cycles

CIRCUMFERENTIAL JOINT BS 280-282.86 HAS CORROSION STRINGERS 26L-26R. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. COMPLIED WITH EA 32-2015-134.

Part: DOOR SILL — CORRODED (PAX DOORWAY) · airframe 15,358 hrs · 9,984 cycles

PAX DOOR SILL ANGLE CORRODED. REMOVED CORRODED PAX DOOR SILL ANGLE IAW SRM 51-42-02-001-001- AND 51-42-06-001-001. LOCATED DRILLED HOLES IN NEW SERVICEABLE PAX DOOR SILL ANGLE IAW DWG SH670-31825. INSTALLED NEW ANGLE IAW SRM 51-41-02-001-001-A01.

Part: FRAME — CORRODED (BS 295) · airframe 15,358 hrs · 9,984 cycles

FRAME BS 295 CORRODED BOTH SIDES AT STR 27. REMOVED CORROSION FROM FRAME BOTH SIDES IAW SRM 51-21-06-001-001-A01. DAMAGE FOUND TO BE OUT OF LIMITS IAW SRM 53-21-06-101-002-A02. COMPLIED WITH EA 32-2015-147.

Part: DOUBLER — CORRODED (TCAS ANTENNA) · airframe 15,358 hrs · 9,984 cycles

LOWER TCAS ANTENNA DOUBLER CORRODED. R & R LOWER TCAS DOUBLER WITH A NEW SERVICEABLE DOUBLER IN REF TO SRM 51-42-06-001-001-A01. REMOVED STRINGER 27 FORWARD OF TCAS BRACKETS, 3EA HILGHTS FROM STRINGER 27 AFT OF BRACKET AND 1EA STRINGER CLEAT TO FOM IN REF TO SRM 51-42-06-001-001-A01. INSTALLED STRINGER 27 FWD OF TCAS DOUBLER IAW SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01 AND INSTALLED AFT BRACKET OF TGR 27 AND CLEAT IAW SRM 51-42-06-001-001-A01.

Part: FLOOR SUPPORT — CORRODED (COCKPIT) · airframe 15,358 hrs · 9,984 cycles

AFT COCKPIT FLOOR SUPPORT AND ANGLE CORRODED. REMOVED CORROSION ON AFT COCKPIT FLOOR AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00-00-101--001-A01 AND 51-21-06-001-001-A01. R & R AFT COCKPIT FLOOR SUPPORT ANGLE REF DWG CC670-34095 SRM 51-40-11-001-001-A01, 51-23-00-001-001-A01, 51-42-06-001-001-A01, 51-25-06-001-001-A01 AND 51-25-16-001-001-A01.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 15,358 hrs · 9,984 cycles

FLOORBEAM ANGLE ON AFT SIDE BS 280 CORRODED. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. FOUND OUT OF LIMITS. R & R IAW SRM 51-42-06-001-001-A01, 51-42-12-001-001-A01, 51-42-21-001-001-A01, 51-40-11-001-001-A01.

Part: FRAME — CORRODED (BS 310) · airframe 15,358 hrs · 9,984 cycles

FRAME BS 310 CORRODED FWD SIDE STR 27-26R. REMOVED CORROSION FROM FWD SIDE IAW SRM 51-26-06-001-001-A01.

Part: LIGHT — DETERIORATED (CABIN) · airframe 15,358 hrs · 9,984 cycles

EMERGENCY LIGHTS VERY DIRTY AND COVERS CRACKED THROUGH OUT AIRCRAFT. CLEANED ALL LIGHTS AND REPLACED ALL COVERS. FOUND EMERGENCY LIGHTS TO BE FADED AND NON REFLECTIVE. REPLACED TRACK LIGHTS.

Part: ANGLE — CRACKED · airframe 15,381 hrs · 10,002 cycles

PANEL 171CL IS CRACKED AT RIVET HOLE AS MARKED. UPON FURTHER EVALUATION, STIFFENER WAS FOUND TO BE CRACKED AS WELL, COMMON TO SAME RIVET HOLE. REMOVED CRACKED 2-ANGLE STIFFENER. INSTALLED NEW 2 ANGLE IAW SRM 51-42-06-001-001. COMPLIED WITH EA 12-2015-112 REV A. RECEIVED AND COMPLIED WITH ECTC EA 12-2015 112.

Part: UNKNOWN — SMOKE (CABIN) · airframe 15,239 hrs · 9,907 cycles

ON CLIMBOUT, PASSING 28,500 FT, RECEIVED LT BLEED DUCT WARNING MSG, FOLLOWED QRH, RECEIVED CABIN ALT MSG AND HAD SMOKE IN THE CABIN. O2 MASKS WERE DEPLOYED, DECLARED EMERGENCY, LANDED, AFTER LANDING FIRE DEPT BOARDED AND FOUND SMOKE IN CABIN. ENROUTE, ACFT DIVERTED DUE TO MAINTENANCE. COMPLIED WITH OPS CHECK OF BLEED AIR DETECTION SYS IAW AMM 36-21-00. OPS CHECK GOOD.

Part: DUCT — LEAKING (BLEED SYS) · airframe 15,152 hrs · 9,847 cycles

WHILE CLIMBING THRU FL250, RECEIVED LT BLEED DUCT WARNING MSG FOLLOWED BY TOTAL PRESSURIZATION FAILURE, EXECUTED EMERGENCY DESCENT TO 10K, FOLLOWED QRH AND DIVERTED. ENROUTE, ACFT DIVERTED DUE TO MAINTENANCE. WING ANTI-ICE DUCT OPS AND LEAK CHK GIID IAW AMM 30-11-00. CABIN PRESS CONTROL OPS CHK GOOD IAW AMM 21-31-00.

Part: SKIN — CRACKED (PAX DOOR) · airframe 14,462 hrs · 9,390 cycles

PAX DOOR AFT SKIN CRACKED UNDER SIDE STIFFENER, AND FWD SIDE UNDER HAND RAIL CLIP BRACKET.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 13,436 hrs · 8,714 cycles

EMERGENCY LIGHT IN GALLEY IS INOPERATIVE. R & R NR 1 EMERGENCY LIGHT BATTERY CHARGER HOUSING IAW AMM 33-51-17.

Part: CONTROL PANEL — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 12,551 hrs · 8,134 cycles

EMERGENCY LIGHTS CAME ON WHEN ACFT POWERS DOWN. ACFT ON THE GROUND SWITCHES IN OFF POSITION, ALL EMERGENCY LIGHTS ARE ON. R & R PAX SIGNS, EMERGENCY LIGHTS CONTROL PANEL IAW AMM 33-24-07-000-801. PERFORMED OPS TEST IAW AMM 33-51-00-710-802.

Part: GROUND STUD — FOULED (EMERGENCY LIGHT) · airframe 12,551 hrs · 8,134 cycles

EMERGENCY LIGHTS WILL NOT ACTIVATE FROM THE F/A LIGHTING PANEL. R & R COCKPIT EMERGENCY LIGHT SWITCH IAW ESPM 20-45-51. FOUND BAD GROUND AT GS1505. REMOVED, CLEANED AND REINSTALLED GROUND STUD GS1505, WIRE FAH7299N IAW AMM 20-23-00. SYSTEM CHECKS GOOD IAW AMM 33-51-00.

Part: GROUND STUD — FOULED (EMERGENCY LIGHTS) · airframe 12,551 hrs · 8,134 cycles

EMERGENCY LIGHTS WILL NOT ACTIVATE FROM F/A PANEL WHEN COCKPIT SWITCH IS IN OFF & ARM POSITION. FOUND BAD GROUND AT GS1505. REMOVED, CLEANED AND REINSTALLED GROUND STUD GS1505, WIRE FAH7299N, IAW AMM 20-23-00. SYS CHECKS GOOD IAW AMM 33-51-00.

Part: PCB — UNSECURE (EMERGENCY LIGHT) · airframe 12,537 hrs · 8,123 cycles

EMERGENCY LIGHTS WILL NOT TURN ON FROM F/A'S TEST SWITCH WITH FLT DECK EMERGENCY LIGHT SWITCH IN ARM. SECURED PCB-4 IN JB-11. PERFORMED OPS CHECK OF EMERGENCY LIGHTS IAW AMM 33-24-07. OPS CHECK GOOD. PERFORMED OPS CHECKS 3 TIMES. NO DEFECTS NOTED.

Part: CIRCUIT BOARD — UNSECURE (EMERGENCY LIGHTS) · airframe 12,537 hrs · 8,123 cycles

EMERGENCY LIGHT WILL NOT TURN ON FROM F/A'S TEST SWITCH, SECURED PCB-4 IN JB-11. PERFORMED OPS CHECK OF EMERGENCY LIGHTS IAW AMM 33-24-07. OPS CHECK GOOD. PERFORMED OPS CHECKS 3 TIMES. NO DEFECTS NOTED.

Part: WIRE — DISCONNECTED (EMERGENCY LIGHTS) · airframe 11,803 hrs · 7,652 cycles

AFT LEFT EXT EMERGENCY OVER WING LIGHT INOPERATIVE. FOUND WIRE EXTRACTED FROM PIN. REPAIRED WIRE IAW ESPM 20-16-43. OPS CHECKED IAW AMM 33-51-15. OPS CHECKED GOOD.

Part: GLOWSTRIP — MISSING (CABIN) · airframe 11,250 hrs · 7,331 cycles

PHOTO LUMINESCENT FLOOR LIGHTING IN GALLERY IS MISSING. REPLACED PHOTO LUMINESCENT STRIP IAW AMM 33-51-01, NO FURTHER DEFECT NOTED.

Part: CONNECTOR — BROKEN (EMERGENCY LIGHT) · airframe 10,551 hrs · 6,853 cycles

PANEL 172CR EMERGENCY LIGHTING WIRE CONNECTORS ARE BROKEN. REPLACED LIGHT ASSY WITH NEW IAW AMM 33-51-15-400-801.

Part: SEAT TRACK — CORRODED (BS 485-581) · airframe 10,521 hrs · 6,838 cycles

CORROSION DAMAGE ON SEAT TRACK BS 485 - FS 581, RBL 9.0. REMOVED CORRODED SEAT TRACK IAW SRM 51-41-02-001-001-A01. INSTALLED SERVICEABLE SEAT TRACK IAW SRM 51-41-02-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 349-485) · airframe 10,521 hrs · 6,838 cycles

CORROSION DAMAGE ON SEAT TRACK BS 349 - 485 RBL 9.0. R & R SEAT TRACK IAW AMM 53-00-49-000-801 AND 53-00-49-400-801.

Part: SILL — CORRODED (BS 1000-1047) · airframe 10,519 hrs · 6,837 cycles

AFT CARGO DOOR CUT OUT LOWER SILL HAS CORROSION DAMAGE FS 1000 - FS 1047. REPAIRED IAW SRM 51-231-06-001-001-A01 AND GREO 670-53-61-913.

Part: SEAT TRACK — CORRODED (BS 581-661) · airframe 10,521 hrs · 6,838 cycles

CORROSION DAMAGE ON SEAT TRACK BS 581 - 661.0 + 32 RBL 9.0. REMOVED CORRODEDSEAT TRACK IAW SRM 51-41-02-001-001-A01. INSTALLED SERVICEABLE SEAT TRACK IAW SRM 51-41-02.

Part: SEAT TRACK — CORRODED (BS 581-661) · airframe 10,521 hrs · 6,838 cycles

CORROSION DAMAGE ON SEAT TRACK BS 581 - 661.0 + 32 LBL 9.0. REMOVED AND INSTALLED SERVICEABLESEAT TRACK IAW 53-00-49-000-801 AND 53-00-49-400-801.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 10,521 hrs · 6,838 cycles

AFT FLOORBEAM ANGLE AT FS 280 CORRODED. REMOVED AFT FLOORBEAM ANGLE IAW SRM 51-42-06-001-001. LOCATED AND DRILLED NEW FLOORBEAM ANGLE AT IAW SRM 51-40-001-001. INSTALLED NEW FLOORBEAM ANGLE IAW SRM 51-42-06-001-001 AND DWG CC670-33052.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 10,521 hrs · 6,838 cycles

FS 280 FLOORBEAM CORRODED ON TOP FLANGE, LBL 12. REMOVED FLOORBEAM IAW SRM 51-42-06-001-001. LOCATED AND DRILLED NEW FLOORBEAM IAW SRM 51-40-11-001-001. INSTALLED NEW FLOORBEAM IAW SRM 51-42-06-011-001.

Part: SEAT TRACK — CORRODED (BS 669-720) · airframe 10,521 hrs · 6,838 cycles

LT SIDE SEAT TRACK FROM BS 669-720 HAS MULTIPLE AREAS OF CORROSION. REMOVED SEAT TRACK IAW 53-00-49-000-801 (A11). INSTALLED SERVICEABLE SEAT TRACK IAW AMM 53-00-49-400-801-A11.

Part: SEAT TRACK — CORRODED (BS 785-847) · airframe 10,521 hrs · 6,838 cycles

LT SIDE SEAT TRACK BS 785 - 847+16 HAS MULTIPLE AREAS OF CORROSION. REMOVED SEAT TRACK IAW SRM 51-41-02-001-001-A01 AND AMM 53-00-49-000-801. INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-801-AALL.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 10,521 hrs · 6,838 cycles

FLOORBEAM AT FS 280 CORRODED. REMOVED CORROSION IAW SRM 51-21-06-001-001 AND IAW REO 690-3-21-458.

Part: FLOORBEAM — CRACKED (BS 276) · airframe 10,519 hrs · 6,837 cycles

COCKPIT FLOORBEAM CRACKED AT FS 276, LBL 12. REPAIRED IAW REO 690-53-11-500.

Part: SEAT TRACK — CORRODED (BS 744-761) · airframe 10,521 hrs · 6,838 cycles

LT SIDE SEAT TRACK BS 744 - 761 HAS CORROSION. REMOVED PASSENGER SEAT TRACK IAW AMM 53-00-49-000-801. INSTALLED SERVICEABLE SEAT TRACK IAW AMM 53-00-49-400-801.

Part: FLOORBEAM — CRACKED (BS 276) · airframe 10,519 hrs · 6,837 cycles

COCKPIT FLOORBEAM CRACKED AT FS 276, RBL12. REPAIRED IAW REO 690-53-11-500.

Part: POST — CORRODED (COCKPIT DOOR) · airframe 10,519 hrs · 6,837 cycles

LT COCKPIT DOOR POST AT FS 280, LBL 11, WL 73, CORRODED. REPAIRED IAW SRM 51-21-06-001-001 AND REO 690-53-11-504.

Part: BULKHEAD — CORRODED (BS 280) · airframe 10,519 hrs · 6,837 cycles

RT FS 280 LOWER BULKHEAD WEB CORRODED ON INBD CORNER. REPAIRED IAW ECTC REO 670-53-11-594 01 AND GENERIC REO 670-53-11-594, REV-1. MAJOR REPAIR.

Part: FLOOR SUPPORT — CRACKED (BS 276) · airframe 10,521 hrs · 6,838 cycles

COCKPIT FLOOR SUPPORT ANGLE RT SIDE CRACKED AT FS 276. REMOVED CRACKED ANGLE AT RBL 12, WL73 IAW SRM 51-42-06-001-001-A01, LOCATED FSTENER HOLES IN NEW ANGLE IAW SRM 51-40-11-001-001-A01. INSTALLED SERVICABLE ANGLE IAW SRM 51-42-06-001-001 AND 51-42-21-001-001.

Part: FLOOR SUPPORT — CRACKED (BS 276) · airframe 10,521 hrs · 6,838 cycles

COCKPIT FLOOR SUPPORT ANGLE CRACKED AT FS 276. REMOVED CRACKED ANGLE AND INSTALLED SERVICABLE ANGLE IAW SRM 51-42-06-001-001 AND 51-42-21-001-001.

Part: POST — CORRODED (COCKPIT DOOR) · airframe 10,519 hrs · 6,837 cycles

RT COCKPIT DOOR POST AT FS 280, RBL 11, WL 73 CORRODED. REPAIRED IAW SRM 51-21-06-001-001 AND REO 690-53-11-504 NDTM PART 1, 51-20-006.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 10,521 hrs · 6,838 cycles

FS 280 FLOORBEAM CORRODED, TOP FLANGE RBL 12, CORRODED. REMOVED FLOORBEAM IAW SRM 51-42-06-001-001. LOCATED AND DRILLED NEW FLOORBEAM IAW SRM 51-40-11-001-001. INSTALLED NEW FLOORBEAM IAW SRM 51-42-06-011-001.

Part: BULKHEAD — CORRODED (BS 280) · airframe 10,521 hrs · 6,838 cycles

LT FS 280 LOWER BULKHEAD WEB CORRODED ON INBD CORNER. REPAIRED IAW EC/TC REO 670-53-11-594 AND GENERIC REO 670-53-11-594, REV DATED 04/27/2011.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 10,519 hrs · 6,837 cycles

PAX DOOR AFT SIDE DRAG ANGLE CRACKED NEAR PAX DOOR ASSIST PULLEY. REPAIRED IAW AFT DRAG ANGLE REPAIR FOR PAX DOOR STEPS IAW SRM 52-11-04-201-002-A01.

Part: LIGHT — MISSING (GALLEY) · airframe 10,151 hrs · 6,608 cycles

EMERGENCY LIGHT MISSING IN GALLEY AREA. COMPLETED IAW AMM 33-51-01.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 9,702 hrs · 6,331 cycles

PAX DOOR AFT SIDE DRAG ANGLE CRACKED NEAR PAX DOOR ASSIST PULLEY. [OPEN]

Part: COMPUTER — MALFUNCTIONED (STALL WARNING) · airframe 9,032 hrs · 5,894 cycles

RECEIVED "STALL FAIL" CAUTION MESSAGE WHILE LATER WE RECIEVED CONTINIOUS IGNITION, THE WARBLER & STICK SHAKER ACTIVATED. THE LOW SPEED & HIGH SPEED CUES SHOWED ON THE LT AIRSPEED TAPE WHILE INDICATING 280KTS. ACFT RETURNED TO DEPARTURE AFTER T/O. EMERGENCY DECLARED AS A PRECAUTION. R & R STALL COMPUTER. OPS CHECK STALL COMPUTER - GOOD IAW AMM 27-35-01-710-801. SDR CLOSED.

Part: SCREW — LOOSE (MEGAPHONE) · airframe 7,973 hrs · 5,218 cycles

F/A REPORTS THAT SCREWS HAVE COME LOOSE ON MEGAPHONE. R & R MEGAPHONE IAW AMM 25-61-14 AND IPC REF 25-61-14, ITEM 5. CHECKED GOOD.

Part: CONTROL UNIT — INTERMITTENT (SLATS) · airframe 7,525 hrs · 4,939 cycles

SLATS FAILED AT 0. EMERGENCY DECLARED. R & R SLAT FLAP CONTROL UNIT IAW AMM 27-51-05. OPS CHECKED GOOD REF 25-51-05, FIG 1, ITEM -5.

Part: GLOWSTRIP — DAMAGED · airframe 6,759 hrs · 4,519 cycles

SECTION OF PHOTOLUMINESENT LIGHTING DAMAGE, 1 MISSING NEAR FC LAV. R & R SECTION OF PHOTOLUMINESENT LIGHT IAW AMM 33-51-01.

Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 5,946 hrs · 4,001 cycles

MEGAPHONE IS INOPERATIVE. R & R MEGAPHONE IAW AMM 25-16-14.

Part: DOOR — OUT OF ADJUST (MAIN PAX) · airframe 5,346 hrs · 3,587 cycles

FWD PASSENGER DOOR DOES NOT OPEN OR CLOSE NORMALLY. CORRECTLY ROUTED ASD ASSIST CABLE OPS CK GOOD IAW AMM 52-11-08.

Part: SLAT SYSTEM — FAILED · airframe 4,557 hrs · 3,085 cycles

SLAT FAIL CAUTION MSG ON APPROACH INTO ATL COMPLIED W/QRH (EMERGENCY DECLARED). RESET AND OPS CHECKED GOOD IAW FIM 27-81-00 810-801 A01. (CLOSED)

Part: STUD — CONTAMINATED (EMERGENCY LIGHT) · airframe 3,273 hrs · 2,245 cycles

WITH COCKPIT EMERGENCY LIGHT SWITCH IN ARMED POSITION, F/A EMERGENCY LIGHT SWITCH IS INOP. CLEANED GROUND STUD GS 1505 IAW ESPM 20-26-00. PERFORMED CONTINUTIY OF GROUND STUD IAW ESPM 20-12-01. EMERGENCY LIGHTS OPS CHECK GOOD IAW AMM 33-51-00. (CLOSED)

Part: GLOWSTRIP — DAMAGED (CABIN) · airframe 3,171 hrs · 2,174 cycles

FLOOR EMERGENCY GLOW STRIP IN FRONT OF GALLEY CARTS POSSIBLY DAMAGED FROM WATER. ABOUT 2 FT OF LIGHTING NO LONGER GLOWS IN THE DARK. REPOSITIONED & GLUED FLOOR GLOW STRIP BACK INTO PLACE IAW AMM 25-60-01. OPS CKD GOOD.

Part: PUMP — FAILED (HYD SYSTEM) · airframe 1,702 hrs · 1,212 cycles

HYD SYS (2) VOLUME DROPPED TO 5 PERCENT EDP 2 AND PUMP 2B BOTH GAVE CAUTION MESSAGES. PRESSURE STAYED AT 2800 UNTIL FINAL APPROACH. TT FOR EDP PUMP WAS AT 55 MINUTES, TT FOR PUMP 2A WAS AT 20 MINUTES. SYS 2 VOLUME DROPPED TO 0 PERCENT ON FINAL (10 MIN) EMERGENCY DELCARED. (EMERGENCY DECLARED)

Part: SIGN — DAMAGED (EMERGENCY LIGHTS) · airframe 1,481 hrs · 1,064 cycles

EMERG EXIT SIGN ( LIGHT LENS/ COVERS (INCLUDING EMERGENCY LIGHT). REMOVED AND REPLACED EXIT SIGN HARDWARE. OPS CHECK NORMAL. IAW AMM 33-51-05 DMIL AND PLACARD REMOVED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 1,141 hrs · 834 cycles

CABIN EMERGENCY LIGHTS INOPERATIVE FROM F/A STATION [GATE RETURN].

Part: SLAT SYSTEM — FAILED · airframe 1,050 hrs · 765 cycles

SLATS FAIL IN FLIGHT, SLATS CAUTION REMAINS [EMERGENCY DECLARED].