N840AY

Part: BULKHEAD WEB — DAMAGED (BS 621) · airframe 25,056 hrs · 25,169 cycles

FWD FACE BS 621 BULK HEAD HAS 18 SCREW SHANK MARKS ON SKIN & RIVET HEADS. REPAIRED FWD FACE OF F.S 621 BULKHEAD (18EA) ARCAB IAW MHI REO 601R-53-61-7570.

Part: SKIN — DENTED (BS 700 S17-18R) · airframe 25,056 hrs · 25,169 cycles

FOUND DENT ON RIGHT AFT FUSELAGE JUST AFT OF FS 700.0 BETWEEN STRINGERS 18R AND 17R. REPAIRED DENT ON RH SIDE OF FUSELAGE JUST AFT OF F.S 700.0 BETWEEN R 18R AND 17R IAW CRJ 200 SRM 53-00-31.

Part: BRACKET — CRACKED (LT NACELLE) · airframe 25,056 hrs · 25,169 cycles

LH PYLON HAS A CRACKED BRACKET "REPAIRED LH PYLON INTERVAL (BRACKET) IAW ENDEAVOR AIR E.A. NO. CRT 258-11191 "

Part: FRAME — CORRODED (BS 333) · airframe 25,056 hrs · 25,169 cycles

F.S 333 FRAME HAS CORROSION ON FWD SIDE AT STGR 26L. FLOOR BOARD SUPPORT FOUND TO BE OUT OF LIMITS. " REMOVED CORROSION IAW CRJ 200 SRM 51-21-06 FOUND TO BE WITHIN LIMITS IAW CRJ 200 SRM 53-00-00 REAPPLIED TOPCOAT PER SRM 51-21-11 51-25-06 AND 51-25-16. REMOVED AND REPLACED FRAME IAW CRJ 200 SRM 51-42-04 "

Part: RETAINING CLIP — CRACKED (BS 280) · airframe 25,056 hrs · 25,169 cycles

F.S 280 RBL 9 OB CLIP IS CRACKED "REMOVED AND REPLACED F.S 280 RBL 9 OB CLIP IAW CRJ 200 SRM 51-24-16 AND 51-42-21 "

Part: RETAINER — CRACKED (BS 484) · airframe 25,056 hrs · 25,169 cycles

FS 484 RBL 22 OB CLIP IS CRACKED REMOVED AND REPLACED CLIP IAW CRJ 200 SRM 51-42-21

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 23,978 hrs · 23,907 cycles

DURING WALK-AROUND FOUND EXTERIOR EMERGENCY LIGHT 3 INOP (FS 406+120.50L) RELAMPED EXTERIOR EMERGENCY LIGHT 3 IAW AMM 33-51-21, OPERATIONAL TEST GOOD, NO DEFECTS NOTED AT THIS TIME. P/N 1317

Part: STRIKER — BENT (PAX DOOR SEAL) · airframe 23,255 hrs · 23,155 cycles

PASSENGER DOOR SEAL STRIKER AT FS 310.00 STGR 8L PREVIOUS REPAIR IS DAMAGED. INCLUDES 8804031/235. REMOVED PREVIOUS REPAIR, FOUND ELONGATED HOLES. REPLACED FWD SEAL STRIKER AT FS 310.00 STGR 8L IAW CRJ 200 SRM 51-42-06 & 51-42-21. OPS/LEAK CHECK GOOD.

Part: FLOOR SUPPORT — CORRODED (BS 559-621) · airframe 23,255 hrs · 23,155 cycles

RH FLOOR SILL CORRODED AROUND FLOORBOARD FASTENER HOLES BTWN FS 559+80 AND FS 621. INCLUDES 8804031/221. BLENDED FLOOR SILL RH AT FS 574-621 AND FOUND TO BE WITHIN LIMITS AND REPLACED RH FLOOR SILL AT 559+80 - 559+112 IAW BSC REO 601R-53-00-526 AND SRM 51-42-06.

Part: STIFFENER — CRACKED (BS 409) · airframe 23,255 hrs · 23,155 cycles

VERTICAL BEAM ON FRAME 409.00+128 AT RBL 18.0 SHOWS EVIDENCE OF A CRACK IN BOTTOM RADIUS OB SIDE OF BEAM. R/R 409+128 POST AT RBL 18.0 IAW BSC REO 601R-53-41-889 REV B.

Part: SEAT TRACK — CORRODED (BS 364-409) · airframe 23,255 hrs · 23,155 cycles

LH SIDE SEAT RAIL CORRODED BETWEEN FS 364 AND FS 409.00+18.02. REMOVED & REPLACED LH SIDE SEAT RAIL BETWEEN FS 364 AND FS 409.00+18.02 WITH A NEW SERVICEABLE SEAT RAIL PN 601R38312-31 IAW CRJ 200 AMM 53-01-11-000-802 AND 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 364-409) · airframe 23,255 hrs · 23,155 cycles

RH SIDE SEAT RAIL CORRODED BETWEEN FS 364 AND FS 409.00+18.02. R/R SIDE SEAT RAIL RH BETWEEN FS 364 AND FS 409+1.02 IAW CRJ 200 AMM 53-01-11-400-802. NO DEFECTS NOTED. PN 601R38312-31. WVAC EMP 722 STAMP

Part: SEAT TRACK — CORRODED (BS 535-559) · airframe 23,255 hrs · 23,155 cycles

RH SIDE SEAT RAIL CORRODED BETWEEN FS 535.02 & FS 559.00+79. REMOVED AND REPLACED SEAT TRACK IAW CRJ 200 AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 444-495) · airframe 23,255 hrs · 23,155 cycles

LH SIDE SEAT RAIL CORRODED BETWEEN FS 444.02 AND FS 495.98. REMOVED AND REPLACED L/H SIDE SEAT RAIL BETWEEN FS 444.02 AND FS 495.98 WITH A NEW SERVICEABLE RAIL P/N 601R38312-115S IAW CRJ200 AMM 53-01-11-000-802 AND 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 495-535) · airframe 23,255 hrs · 23,155 cycles

LH SIDE SEAT RAIL CORRODED BETWEEN FS 495.98 AND FS 535.02. REPALCED SEAT TRACK IAW GREO 601R-53-00-055.

Part: SEAT TRACK — CORRODED (BS 409-444) · airframe 23,255 hrs · 23,155 cycles

LH SIDE SEAT RAIL CORRODED BETWEEN FS 409.00+111.02 AND FS 444.02 REMOVED AND REPLACED L/H SIDE SEAT RAIL BETWEEN FS 409.00+111.02 AND FS 444.02 WITH A NEW SERVICEABLE SEAT RAIL IAW CRJ200 AMM 53-01-11-000-802 AND 53-01-11-400-802 P/N 601R38312-119S.

Part: CHANNEL — CRACKED (VERTICAL STAB) · airframe 23,255 hrs · 23,155 cycles

VERTICAL STAB LEADING EDGE PANEL 324AT INNER WEB DAMAGE AT BOTTOM OF LEADING EDGE AND SEVERAL RIVETS PULLED THROUGH. REMOVED AND REPLACED CHANNEL ON L/E OF VERTICAL STAB IAW CRJ200 SRM 51-42-06. WVAC EMP STAMP 771

Part: SEAT TRACK — CORRODED (BS 535-559) · airframe 23,255 hrs · 23,155 cycles

LH SIDE SEAT RAIL CORRODED BETWEEN FS 535.02 AND FS 559.00+79. REMOVED AND REPLACED LH SIDE SEAT RAIL BETWEEN FS 535.02 AND FS 559.00+79 IAW BOMBARDIER REO 601R-53-00-55. WVAC EMP STAMP 769

Part: SEAT TRACK — CORRODED (BS 409) · airframe 23,255 hrs · 23,155 cycles

LH SIDE SEAT RAIL CORRODED BETWEEN FS 409.00+18.02 AND FS 409.00+111.02. REMOVED AND REPLACED L/H SIDE SEAT RAIL BETWEEN FS 409.00+18.02 AND FS 409.00+111.02 IAW BOMBARDIER REO #601R-53-00-055, STEPS 1 THRU 3 REPAIR ""B"" COMPLETE SEGMENT REPLACEMENT REV C DATED 2017-03-21 P/N: N126-2075.

Part: BRACKET — CRACKED (BS 528) · airframe 23,255 hrs · 23,155 cycles

HYD SYS #3 PRESSURE TRANSDUCER BRACKET CRACKED IN RH MLG WHEEL WELL CEILING FS 528, RBL 18-27. REMOVED DAMAGED HYD STS #3 PRESSURE TRANSDUCER BRACKET AND REPLACED WITH NEW ITEM PN601R752662-157 IAW CRJ 200 SRM 51-42-06.

Part: SEAT TRACK — CORRODED (BS 409) · airframe 23,255 hrs · 23,155 cycles

LH SIDE SEAT RAIL CORRODED BETWEEN FS 535.02 AND FS 559.00+79. REMOVED AND REPLACED LH SIDE SEAT RAIL BETWEEN FS 535.02 AND FS 559.00+79 IAW BOMBARDIER REO 601R-53-00-55.

Part: SEAT TRACK — CORRODED (BS 409) · airframe 23,255 hrs · 23,155 cycles

LH SIDE SEAT RAIL CORRODED BETWEEN FS 409.00+111.02 AND FS 444.02. REMOVED AND REPLACED L/H SIDE SEAT RAIL BETWEEN FS 409.00+111.02 AND FS 444.02 WITH A NEW SERVICEABLE SEAT RAIL IAW CRJ200 AMM 53-01-11-000-802 AND 53-01-11-400-802 P/N 601R38312-119S.

Part: SEAT TRACK — CORRODED (BS 409) · airframe 23,255 hrs · 23,155 cycles

RH SIDE SEAT RAIL CORRODED BETWEEN FS 409.00+18.02 AND FS 409.00+111.02. REMOVED AND REPLACED R/H SEAT RAIL BETWEEN FS 409.00+18.02 AND FS 409.00+111.02 IAW BOMBARDIER REO NO. 601R-53-00-055 REV C DATED 2017-03-21 STEPS 1 TO 3 (REPAIR ""B"" COMPLETE SEGMENT REPLACEMENT).

Part: FITTING — CRACKED (BS 235) · airframe 23,255 hrs · 23,155 cycles

LH WINDSHIELD SIDE POST LOWER OB FITTING IS CRACKED. REMOVED & REPLACED CRACKED LH WINDSHIELD SIDE POST LOWER FITTING WITH A NEW SERVICEABLE SIDE POST LOWER FITTING IAW CRJ 200 SRM 51-42-21. PN 601R33235-4S.

Part: FITTING — CRACKED (BS 235) · airframe 23,255 hrs · 23,155 cycles

RH WINDSHIELD SIDE POST OB FITTING IS CRACKED. REMOVED & REPLACED CRACKED RH WINDSHIELD SIDE POST LOWER FITTING WITH A NEW SERVICEABLE SID EPOST LOWER FITTING PN 601R33235-3S IAW SRM 51-42-21.

Part: OXYGEN MASK — FAILED (FIRST OFFICER'S) · airframe 21,356 hrs · 21,156 cycles

FIRST OFFICER`S OXYGEN MASK HEAD BAND WONT INFLATE AND FAILED A FFOD TEST. REMOVED AND REPLACED THE OXYGEN STOWAGE BOX AND MASK IAW AMM 35-11-15, OPS CHECKED GOOD, NO DEFECTS NOTED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,171 hrs · 20,976 cycles

SECOND EMERGENCY LIGHT ON THE CEILING BY ROW 5 IS OUT. RELAMPED SECOND EMERGENCY LIGHT LAW AMM 33-51-16. OPS CHECK GOOD NO DEFECTS NOTED AT THIS TIME.

Part: UNKNOWN — SMOKE (COCKPIT) · airframe 20,701 hrs · 20,489 cycles

AFTER LANDING, ON TURNING ONTO TAXIWAY, COCKPIT FILLED WITH SMOKE. SMOKE AND BURNING ODOR REPORTED IN CABIN. THERE WAS NO HEAVY BRAKING ON LANDING. FIRE DEPARTMENT INSPECTED THE AIRCRAFT. NO EVIDENCE OF SMOKE OR FIRE. TAXIED TO THE GATE. INSPECTED THE ACFT, OPERATED APU AND PACKS AT 80*C, CHECKED GOOD, NO FUMES NOTED. OPERATED ENGINES AND PACKS. NO FUMES NOTED. NO DEFECTS NOTED. ACFT OK FOR SERVICE.

Part: OXYGEN MASK — NO TEST (FIRST OFFICER'S) · airframe 20,669 hrs · 20,448 cycles

FIRST OFFICER`S OXYGEN MASK TEST BUTTON FAILED. R & R THE OXYGEN BOX IAW AMM 35-11-15. OPS CHECKED GOOD. SERVICED CREW OXYGEN TO 1780 PSI IAW AMM 12-16-35.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 20,039 hrs · 19,768 cycles

LEFT FORWARD EMERGENCY LIGHT BURNED OUT. REPLACED THE LAMPS IAW AMM 33-51-21.OPS CHECKED GOOD.

Part: GEAR — DEFECTIVE (NOSE) · airframe 20,025 hrs · 19,753 cycles

GEAR DISAGREE ON DEPARTURE. NOSE GEAR STAYED DOWN. PERFORMED QRH. LANDED WITHOUT INCIDENT. PERFORMED QRH. MESSAGE CLEARED, LANDED WITHOUT DISCREPANCY.

Part: DUCT — LOOSE · airframe 19,841 hrs · 19,554 cycles

JUST AFTER ROTATION, APU FIRE WARNING ACTIVATED. RAN QRH, INDICATION PERSISTED FOR A FEW MINUTES AFTER BOTTLE DISCHARGE. APU FIRE FAIL & APU FIRE INDICATIONS PERSISTED INTERMITTENTLY THROUGHOUT FLIGHT. FOUND LOOSE DUCT TO UPPER ATTACHMENT OF APU LCV. REATTACHED LOOSE DUCT PROPERLY INTO CLAMP IAW THE IAW AMM 49-51-01. OPS CHECKED GOOD.

Part: OXYGEN MASK — LEAKING (FLIGHT DECK) · airframe 19,352 hrs · 19,015 cycles

FIRST OFFICER`S OXYGEN MASK IS LEAKING. REMOVED AND REPLACED THE OXYGEN MASK IAW AMM 35-11-12-500-801. OPS AND LEAK CHECKED GOOD.

Part: UNKNOWN — ODOR (CABIN & COCKPIT) · airframe 18,962 hrs · 18,616 cycles

STARTED APU ON APPROACH CHECK AT 10,000' GOT VERY FOUL SMELL IN CABIN + COCKPIT, BUT ALL INDICATIONS WERE NORMAL. SHUTDOWN APU AND SMELL WENT AWAY LANDED W/ NO ISSUES. INSPECTED APU ENCLOSURE FOR LEAKS AND NO LEAKS NOTED AND PERFORMED ADJ/ TEST OF APU IAW AMM 49-10-00. ALL CHECKS GOOD. A/C OK FOR SVC.

Part: BULKHEAD WEB — SCRATCHED (BS 621) · airframe 18,747 hrs · 18,401 cycles

CARGO AFT BULKHEAD FWD FACE SCRATCHED, RT 12 INCHES ABOVE FLOOR, 8 INCHES INBD OF FUSELAGE. REMOVED DAMAGE IAW SRM 51-12-00. FOUND TO BE WITHIN LIMITS IAW REO #601R-53-61-5924.

Part: DOOR SILL — CORRODED (BS 310-349) · airframe 18,747 hrs · 18,401 cycles

PAX DOOR OPENING LOWER FRAME, LOWER ANGLE HAS CORROSION SPOTS ON THE INBD AND OTBD SIDE BETWEEN BS 310 AND 349. REMOVED AND REPLACED THE LOWER SILL ANGLE IAW SRM 51-42-21 AND 51-42-06.

Part: BULKHEAD WEB — CHAFED (BS 621) · airframe 18,747 hrs · 18,401 cycles

CARGO AFT BULKHEAD CHAFED IN SEVERAL PLACES BS 621. REMOVED DAMAGE IAW SRM 51-12-00.

Part: BULKHEAD — CRACKED (BS 202) · airframe 18,747 hrs · 18,401 cycles

BS 202 BULKHEAD HAS CRACKS AT BRAKE CABLE PASS THRU HOLE. REPAIR THE BULKHEAD IAW REO 601R-53-11-563.

Part: STIFFENER — CRACKED (BS 621-625) · airframe 18,747 hrs · 18,401 cycles

AFT ACCESSORY BAY, LT SIDE VERTICAL STIFFENERS, OTBD ANGLE IS CRACKED ADJACENT TO STRINGER 15L. REMOVED AND REPLACED THE STIFFENER IAW SRM 51-42-21.

Part: INTERCOSTAL — CRACKED (BS 621-625) · airframe 18,747 hrs · 18,401 cycles

BS 621 - 625 INTERCOSTAL ANGLE AT STRINGER 14L FOUND CRACKED. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-42-06, 51-42-21, AND 51-42-22.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 18,747 hrs · 18,401 cycles

LEFT INBD FLAP LOWER SKIN HAS FOUR DENTS ON INBD SIDE. REMOVED AND REPLACED THE FLAP SKIN IAW SRM 57-52-00, 51-40-11, & 51-42-13,

Part: STRUCTURE — BENT (LT WING TE FLAP) · airframe 18,747 hrs · 18,401 cycles

LEFT INBD FLAP, TRAILING EDGE IS BENT IN TWO PLACES ON INBD AREA. REMOVED & REPLACED THE FLAP TRAILING EDGE IAW SRM 51-42-12.

Part: RIB — DAMAGED (LT WING TE FLAP) · airframe 18,747 hrs · 18,401 cycles

UPON REMOVAL OF LT LOWER INBD SKIN FOUND TWO DAMAGED RIBS. REMOVED & REPLACED THE RIBS IAW SRM 51-42-06.

Part: SEAT TRACK — CORRODED (BS 409-458) · airframe 18,747 hrs · 18,401 cycles

IN PASSENGER CABIN RIGHT SIDEWALL SEAT TRACK NR 4 IS CORRODED AND GOUGED. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (PAX CABIN) · airframe 18,747 hrs · 18,401 cycles

IN PASSENGER CABIN RIGHT SIDEWALL SEAT TRACK NR 5 IS CORRODED AND GOUGED. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11.

Part: DEFIBRILLATOR — DISCHARGED (CABIN) · airframe 18,677 hrs · 18,336 cycles

AED NOT CHARGED IAW FA. INSTALLED SERVICEABLE AED. OK FOR SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 18,219 hrs · 17,868 cycles

DURING WAKE UP CHECK, FOUND EMERGENCY LIGHT NR 6 OUT. REPLACED THE LAMPS IAW AMM 33-51-21, OPS TESTED GOOD.

Part: CLAMP — LOOSE (BLEED AIR) · airframe 17,915 hrs · 17,570 cycles

AFTER TAKE OFF, WITH BLEEDS ON THE ENGINE. 10TH DUCT WARNING MESSAGE. QRH COMPLETED. NORMAL LANDING AFTER DIVERSION. LEAKS FOUND COMING FROM ACM CLAMPS FOUND BOLTS ON ACM FRONT HOUSING LOOSE & THE CLAMPS FOR ACM NR 1 DUCTING LOOSE AS WELL. ALL BOLTS & CLAMPS TIGHTENED. ACM COMPRESSOR HOUSING BOLTS TIGHTENED ALL CHECKS GOOD IAW 21-50-00

Part: LIFE VEST — TORN (CABIN) · airframe 17,512 hrs · 17,149 cycles

ONE EACH INFANT LIFE VEST & FLIGHT ATTENDANT LIFE VEST TORN. R & R ONE EACH INFANT & FLIGHT ATTENDANT LIFE VEST IAW AMM 25-61-03 & IAW PA 25-096A.

Part: LIFE VEST — UNSERVICEABLE (CABIN) · airframe 16,376 hrs · 16,032 cycles

ONE INFANT LIFE VEST BAG TORN. R & R ONE INFANT LIFE VEST IAW PA-25-096A.

Part: CABLE — BROKEN (CABIN DOOR) · airframe 16,150 hrs · 15,811 cycles

FLIGHT ATTENDANT REPORTS MAIN CABIN DOOR DIFFICULT TO OPEN & CLOSE. HANDLE HARD TO PUSH DOWN TO CLOSE & HARD TO LIFT WHEN OPENING. FOUND ICE BREAK CABLE ASSEMBLY BROKEN & JAMMING DOOR MECHANISM. R & R ICE BREAK CABLE ASSEMBLY IAW AMM 52-11-15. OPERATIONS CHECKED GOOD. HANDLE MOVES SMOOTH AS NORMAL. ACFT OK FOR SERVICE.

Part: WIRE HARNESS — DEFECTIVE (NLG) · airframe 16,116 hrs · 15,780 cycles

NOSE GEAR DIDN`T RETRACT AFTER TAKEOFF, HAD GEAR DISAGREE WARNING ABOUT 6 SECONDS AFTER GEAR SELECTED UP. REPLACED NLG WOW NR 2 HARNESS IAW AMM 32-61-25. REINSTALLED NLG COLLAR IAW PA 32-066C. OFF SHIMS RECORDED .061 & .065, ON SHIMS RECORDED .0415 & .0415. R & R NLG BRACKET ASSEMBLY IAW CMM 32-20-04. GEAR DISAGREE TROUBLESHOOTING REQUIREMENTS, SERVICED NLG STRUT IAW AMM 12-12-32-610-803. REF NON-ROUTINE WC N72992.

Part: OXYGEN MASK — LEAKING (COCKPIT) · airframe 15,866 hrs · 15,515 cycles

CAPT O2 MASK HARNESS LEAKS DURING TEST. R & R CAPTAINS SIDE O2 MASK IAW AMM 35-11-12. OPERATIONS CHECKED GOOD. OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,755 hrs · 15,401 cycles

EMERGENCY LIGHT INTERIOR WHITE BULB INOPERATIVE. RELAMPED AS REQUIRED. PN INSTALLED & REMOVED OL3071BPE GPL. OPERATIONS CHECKED GOOD.

Part: PBE — DAMAGED (GALLEY) · airframe 15,681 hrs · 15,324 cycles

GALLEY PBE DAMAGED. R & R GALLEY PBE IAW AMM 35-30-00.

Part: BULKHEAD — CHAFED (FUSELAGE) · airframe 15,636 hrs · 15,278 cycles

FORWARD FACE OF FS 621 BULKHEAD, CHAFED AT 11 PLACES BETWEEN WL87.5 & WL103.5, LBL 27.5 & RBL 36.2, WITH MAX DEPTH OF 0.007 INCHES DEEP. REPAIRED IAW REO 601R-53-61-5446.

Part: SKIN — DENTED (FUSELAGE) · airframe 15,636 hrs · 15,278 cycles

MAINTENANCE FOUND THE FUSELAGE SKIN TO BE DENTED AT APPROX FS 293 ON STRINGER 17L. THE DENT MEASURES 1.1” X 0.7” X 0.005” DEEP. REPAIRED IAW EA CRJ253-03272 & ASSOCIATED 8110-3.

Part: SMOKE DETECTOR — DEFECTIVE (CARGO BAY) · airframe 15,612 hrs · 15,254 cycles

FORWARD CARGO SMOKE DETECTOR IS SHOWING A RED LIGHT. R & R FWD CARGO SMOKE DETECTOR. OPERATIONS CHECKED GOOD IAW AMM 26-15-01.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 15,507 hrs · 15,136 cycles

CABIN EMERGENCY LIGHT INOPERATIVE. COMPLETED ON ACFT CHARGE FOR OVER 6 HRS IAW RADIANT CMM 25-60-03. OPS TEST IAW CAMM 33-51-00. OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 14,494 hrs · 14,139 cycles

LEFT FWD OVERWING EMERGENCY LIGHT & PAX DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. R & R LT FWD OVERWING EMERGENCY & PAX DOOR EXTERIOR EMERGENCY LAMPS IAW AMM 33-51-21. OPERATIONS CHECKED GOOD.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 14,267 hrs · 13,904 cycles

FLIGHT ATTENDANT FLASHLIGHT INOPERATIVE. R & R FLASHLIGHT BATTERY IAW AMM 25-61-02.

Part: LENS — MISSING (EXIT SIGN) · airframe 14,188 hrs · 13,836 cycles

CENTER AISLE FLIGHT ATTENDANT CALL EMERGENCY EXIT SIGN WHITE LENS CAP MISSING. DEFERRED EMERGENCY EXIT SIGN WHITE LENS COVER IAW NEF C6 FOR 120 DAYS.

Part: SHAFT — LACK OF LUBE (TE FLAP) · airframe 13,599 hrs · 13,274 cycles

FLAP FAIL AT 20 DEGREES. PERFORMED TROUBLESHOOTING IAW FIM REV 45 IAW AD 2009-06-12 PARAGRAPH H 6 I IAW AMOC DATED JULY 22, 2013 & PA AD27-052N. PERFORMED FLEX SHAFT LUBE IAW CHECKLIST & AMM 27-53-10, OPERATIONS CHECKED GOOD.

Part: LIGHT — LOOSE (CABIN) · airframe 13,582 hrs · 13,256 cycles

A SECTION OF THE EMERGENCY FLOOR STRIP LIGHTING FROM AROUND SEAT 2C WAS FOUND UNPLUGGED & LOOSE ON THE FLOOR. SECURED FLOOR TRACK LIGHTING NEAR 1 & 2 CD IAW AMM 33-50-00.

Part: WARNING MESSAGE — ILLUMINATED (CABIN PRESSURE) · airframe 12,862 hrs · 12,509 cycles

CABIN ALTITUDE CAUTION MESSAGE FOLLOWED BY CABIN ALTITUDE WARNING.

Part: WARNING LIGHT — ILLUMINATED (CABIN PRESSURE) · airframe 12,852 hrs · 12,497 cycles

CABIN ALTITUDE WARNING MESSAGE, UNCONTROLABLE IN BOTH MODES.

Part: SKIN — DENTED (RT AILERON) · airframe 12,839 hrs · 12,487 cycles

DENT ON RT AILERON NEAR INBD EDGE AT WS288. REPAIRED IAW REO 601R-57-61-477.

Part: BULKHEAD — DAMAGED (BS 621) · airframe 12,839 hrs · 12,487 cycles

FS 621 PRESSURE BULKHEAD HAS A LINE OF SCREW MARKS APPROX WL86 WITH MAXIMUM MATERIAL LOSS OF 0.009". REPAIRED IAW REO 601R-53-61-4960.

Part: BULKHEAD — DAMAGED (BS 621) · airframe 12,839 hrs · 12,487 cycles

FS 621 PRESSURE BULKHEAD HAS A LINE OF SCREW MARKS APPROX WL75.5 WITH MAXIMUM MATERIAL LOSS OF 0.005". REPAIRED IAW REO 601R-53-61-2155.

Part: FLOORBEAM — CRACKED (BS 484) · airframe 12,839 hrs · 12,487 cycles

SUPPORT ANGLE ON RT SIDE AT FS 484 ARE CRACKED AT RBL 27 AND RBL 36. REPAIRED IAW REO 601R-53-41-059.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 12,839 hrs · 12,487 cycles

FLOORBEAM UPPER AND LOWER CAPS ARE CRACKED AT FS 280, LBL 9 AND RBL 10. REPAIRED IAW REOS 601R-53-11-136/601R-53-11-171.

Part: FLOOR SUPPORT — CRACKED (BS 280) · airframe 12,839 hrs · 12,487 cycles

FWD SIDE OF FS 280 BULKHEAD LBL 9 THE FLOOR SUPPORT ANGLE IS CRACKED. REPAIRED IAW REO 601R-53-11-138.

Part: BULKHEAD — CRACKED (BS 280) · airframe 12,839 hrs · 12,487 cycles

FS 280 BULKHEAD, RBL 9 INBD AND OTBD CLIPS AND THE LBL 9 INBD AND OTBD CLIPS ARE CRACKED. REPAIRED IAW REO 601R-53-11-171.

Part: ENGINE — MALFUNCTIONED (RIGHT) · airframe 11,989 hrs · 11,650 cycles

ON FLIGHT 4134 (IAH - MEM) WHILE CLIMBING THROUGH 5,000FT HEARD A POP AND LOST THRUST (BOTH AT THE SAME TIME). NO INDICATIONS OF SPOOL, ITT WAS WITHIN LIMITS, ENGINE FAILURE. CREW SUSPECTED FLAMEOUT AND ATTEMPTED TO RESTART PER QRH. ENGINE DID NOT RELIGHT. EMERGENCY WAS DECLARED, AN AIR RETURN WAS PERFORMED AND THE AIRCRAFT LANDED SAFELY. REMOVED AND REPLACED RIGHT ENGINE IAW AMM 71-00-00 AND CHECKLIST. OPS LEAK CHECK GOOD. FUNCTIONAL CHECK GOOD.

Part: LENS — MISSING (CABIN) · airframe 11,913 hrs · 11,570 cycles

MID CEILING LIGHT INDICATOR ON CABIN EMERGENCY LIGHT MISSING 1 WHITE LENS COVER AND 1 AMBER LENS COVER. REPLACED AMBER AND WHITE LENS ON AFT SIDE OF MID CABIN EMERGENCY LIGHT. PART NUMBER 6201203 AND 6201201. OPS CHECK OF LIGHT'S GOOD.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 11,806 hrs · 11,463 cycles

FLASHLIGHTS INOP. REPLACED BATTERY. OPS CHECK GOOD.

Part: LIGHT — BROKEN (CABIN) · airframe 10,980 hrs · 10,594 cycles

EXIT LIGHT ON FORWARD SIDE OF PASSENGER DOORWAY IS BROKEN ABOUT KNEE HEIGHT. REPLACED EXIT LIGHT ASSY P/N BR9179-013 REF 33-51-10. OPS CHECK GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 9,092 hrs · 8,327 cycles

RT FWD EXT EMERGENCY COVE LIGHT OUT. RELAMPED LIGHT OPS CHECKS GOOD. LENSE COVER IS MISSING (1) SCREW. DEFERRED RT FWD EMERGENCY LIGHT IAW MEL 33-51-2A ENTERED INTO MM02 MXC NOTIFIED 4632. INSTALLED MISSING SCREW AS REQUIRED. REMOVED FROM MM02 MXC 0948 NOTIFIED.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 8,490 hrs · 7,650 cycles

DURING ROUTINE CHECK NOTED EMERGENCY LIGHT INOPERATIVE. RELAMPED EMERGENCY LIGHT IAW REF 33-51-21 PN ON/OFF 1317.