N820SY

Part: TIE — BROKEN (EXTINGUISHER) · airframe 32,208 hrs · 10,548 cycles

FLIGHT DECK FIRE EXTINGUISHER SAFETY TIE BROKE OFF - RESOLUTION: REMOVED AND REPLACED FLIGHT DECK FIRE EXTINGUISHER REF. AMM 25-64-00. OKAY FOR SERVICE.

Part: SLIDE — DISLODGED (ZONE 800) · airframe 32,039 hrs · 10,481 cycles

CATERING OPENED L2 WITH SLID ARMED AND PULLED SLIDE OUT OF HOUSING. DID NOT INFLATE - REMOVED AND REPLACED L2 DOOR SLIDE PER AMM 25-66-1

Part: GIRT BAR — DAMAGED (ZONE 800) · airframe 31,989 hrs · 10,455 cycles

FWD ENTRY GIRT BAR. PLASTIC PIECE IS MISSING A PIN TO KEEP IT IN PLACE AND NOT SLIDE AROUND. FOUND FWD GIRT BAR RELEASE STOP ASSY ROTATED PREVENTING SPRING CLIP FROM SECURING PROPERLY. RE-ORIENTED TO THE CORRECT POSITON. ASSY WORKS AS SHOULD OKAY FOR SERVICE. REF AMM 25-66-01-400-803.

Part: HOLDER — LOOSE (GIRT BAR) · airframe 31,840 hrs · 10,399 cycles

L1 GIRT BAR HOLDER IS LOOSE. ADJUSTED GIRT BAR HOLDER L1 DOOR REF AMM 25-66-01. OK FOR SERVICE,

Part: LIGHT — UNSECURE (ZONE 200) · airframe 31,840 hrs · 10,399 cycles

PHOTOLUMINESCENT LIGHT STRIP BY ROW 12 DEF SIDE RAISED UP DURING CRUISE CREATING TRIPPING HAZARD. CARPET ON FLOOR ALSO RAISED UP. GOES BACK DOWN ON GROUND REMOVED AND REPLACED ROW 12 DEF PHOTOLUMINESCENT STRIP AND ADHESIVE AND REPLACED CARPET RAPE REF AMM 33-51-15. OKAY FOR SERVICE.

Part: LIGHT — UNSECURE (ZONE 200) · airframe 31,840 hrs · 10,399 cycles

PHOTOLUMINESCENT EMERGENCY ESCAPE PATH MARKING SYSTEM ROW 12DEF STICKING UP AND IS A TRIPPING HAZARD PHOTOLUMINESCENT EMERGANY ESCAPE STRIP REPOSITIONED PROPERLY-OK FOR SERVICE REF AMM 33-51-15

Part: LENS — LOOSE (ZONE 800 SLIDE) · airframe 31,206 hrs · 10,192 cycles

FOUND R1 DOOR SLIDE PACK PRESSURE GAUGE LENS LOOSE IN COVER. REMOVED R1 DOOR SLIDE PACK AND COVER ASSY - RESECURED PRESSURE GAUGE WINDOW AS REQUIRED & REINSTALLED ORIGINAL R1 DOOR SLIDE PACK & COVER ASSY REF AMM 25-66-01 STEP E. OK FOR SERVICE.

Part: LIGHT — UNSECURE (ZONE 200) · airframe 31,165 hrs · 10,181 cycles

DEFECT 809026: 12DEF CARPET AND EXIT PATH LIGHTING IS LIFTING - RESOLUTION: REATTACHED CARPET AND EXIT PATH LIGHTING REF. AMM 25-27-15 OKAY FOR SERVICE

Part: PLACARD — WORN (ZONE 200) · airframe 31,162 hrs · 10,180 cycles

WORK ORDER 95838, NR00003: DURING LAYOVER FOUND EMERGENCY PLACARD "PUSH " AND "PULL " AT F/O R2 WINDOW ILLEGIBLE - RESOLUTION: REPLACED 2 EACH PLACARDS REF 20-10-14

Part: LIGHT — PEELING (ZONE 200) · airframe 30,293 hrs · 9,904 cycles

DEFECT 768171: ROW 12 DEF PHOTOLUMINESENT ESCAPE PATH PEELING UP FROM FLOOR. - - RESOLUTION: SECURED PHOTOLUMINESCENT FLOOR PATH LIGHTS AT 12DEF IAW AMM 33-51-15. OK FOR SERVICE.

Part: LIGHT — UNSECURE (ZONE 200) · airframe 29,824 hrs · 9,793 cycles

DEFECT 799108: 12C AND 12D EXIT PATH LIGHT STRIPS PEELING UP. RESOLUTION: RESECURED ROW 12C + D FLOOR PATH LIGHTING REF AMM 33-51-15. OKAY FOR SERVICE.

Part: CABIN PRESSURE — FAULTED · airframe 29,485 hrs · 9,692 cycles

AT CRUISE ALTITUDE, THE CREW CONTACTED MAINTENANCE TO REPORT CABIN ALTITUDE FLUCTUATIONS OF 1000 TO 2000 FEET. THE CREW MADE THE DECISION TO RETURN TO MSP. THE FLIGHT DESCENDED INITIALLY TO FL250 AND THEN AGAIN TO 10,000 FEET AS A PRECUATION. THE CABIN REMAINED PRESSURIZED DURING THE AIR RETURN. THE FLIGHT LANDED WITHOUT INCIDENT AND WAS NOT OVERWEIGHT.

Part: OUTFLOW VALVE — FAULTED (ZONE 100) · airframe 29,485 hrs · 9,692 cycles

CLIMB THROUGH 330 TO 350 CABIN CLIMB WAS FLUCTUATING +/- 2000 FPM CLIMB & DESCENT. STABLE AT 350. UPON CLIMBING TO 390 CABIN WAS +/- 2000 FPM CLIMB. F/AS REPORTED POPING EARS AND WOOSHING NOISE. AT 390 CABIN ALT CONTINUED CLIMB FROM 8 TO 9.5 AT 2000 FPM. INITIATED DESCENT AT 250 CABIN STABLE. +/- 2000 FPM WHEN LANDING ALITIUDE CHANGED TO MSP. - RESOLUTION: PERFORMED FIM 21-31 TASK 823 FROM PARA. E(C)(3). TO PARA. F(6). NO ISSUES FOUND ON #1 ENG HEALTH CHECK. REMOVED AND REPLACED #1 AND #2 PER COMPANY CONVENIENCE. OK FOR SERVICE. IAW FIM 21-31 TASK 823. REMOVED AND REPLACED OUTFLOW VALVE ASSEMBLY. OPS TEST GOOD. REF AMM 21-31-03. REMOVED AND REPLACED INBOARD AND OUTBOARD POSITIVE PRESURE RELIEF VALVES. REF AMM 21-32-01.

Part: SIGHT GLASS — BROKEN (DOOR SLIDE) · airframe 29,474 hrs · 9,687 cycles

BROKEN WINDOW OF ESCAPE SLIDE COVERS (EAS) OF DOOR R2/L2.

Part: COVER — BROKEN (ZONE 200) · airframe 29,474 hrs · 9,687 cycles

BROKEN COVERS (4 EAS) OF EXIT EMERGENCY LIGHT OF DOOR R1, R2, L1, L2.

Part: COVER — DETACHED (L2 DOOR SLIDE) · airframe 29,074 hrs · 9,528 cycles

AT DOOR 2L THE PLASTIC COVER OVER THE SLIDE DOOR COMES OFF. RESECURED 2L DOOR SLIDE GAUGE COVER REF AMM 20-30-11. OKAY FOR SERVICE

Part: COVER — BROKEN (L2 DOOR SLIDE) · airframe 29,025 hrs · 9,511 cycles

L2 SLIDE PROTECTION COVER ON SLIDE GAUGE BROKEN. RESECURED 2L SLIDE GAUGE COVER WINDOW REF AMM 20-30-11 THIS CLEARS MEL.

Part: SLEEVE — BROKEN (GIRT BAR) · airframe 28,340 hrs · 9,295 cycles

W/O 87181 NR00009: L1 GERT BAR RELEASE STOP OUTER SLEEVE PIECE IS BROKEN OFF. - - RESOLUTION: INSPECTED L1 DOOR GRIT BAR IAW AMM 25--66-00. NO DEFECT NOTED.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 26,109 hrs · 8,519 cycles

DEFECT WORK ORDER 80176: NON ROUTINE CARD 00007: R/H AFT EMERGENCY EXIT DOOR FLIGHT ATTENDANT SEAT LOWER COMPARTMENT DOOR LATCHES NOT FUNCTIONING AS DESIGNED. - - - RESOLUTION: REPLACED LATCH ON R2 DOOR FA SEAT OUTBOARD STOWAGE BOX DOOR REF; AMM 25-25-12

Part: NONE — NONE · airframe 25,253 hrs · 8,220 cycles

DEFECT 688502: FORWARD ENTRY DOOR ESCAPE SLIDE ATTACHMENT DO NOT FIT CORRECTLY. HANGS LOW AND POPS OUT OF BRACKETS. RESOLUTION: REMOVED ESCAPE SLIDE FROM L1 DOOR. & READJUSTED SLIDE & REINSTALLED PER AMM 25-66-01

Part: SKIN — DAMAGED · airframe 24,971 hrs · 8,134 cycles

DEFECT JC 802612 NR 00006: SKIN DAMAGE AT LOWER FWD CORNER OF FWD CARGO DOOR CUTOUT BS 436 STRINGER 25R-26R. RESOLUTION: REPAIRED FUSELAGE SKIN AT FWS CARGO CUTOUT BS 436 STR25R-26R PER ATS ER 23-01056 REV 1R AND SCA ENG-53SCA-11098 REV OO.

Part: LIGHT — INOPERATIVE · airframe 24,300 hrs · 7,904 cycles

DEFECT 720268: DOORS L1 AND R2 EXTERIOR EMERGENCY LIGHTS INOP. RESOLUTION: REPLACED LIGHT BULBS AT DOORS L1 AND R2. OPS CHECK GOOD. EXTERIOR LIGHTS REF: B737 AMM 33-51-04-980-801.

Part: NONE — NONE · airframe 24,299 hrs · 7,903 cycles

***CORROSION*** ON 947 FLOORBEAM UPPER FLANGE STA 947, LBL25, WL208. RESOLUTION: REMOVED AND REPLACED 947 FLOOR BEAM UPPER FLANGE STA947 LBL25 WL208 PER B737 SRM 53-70-51-2R-5 REPAIR 5 AND ATS ER 22-02218 REV 1R AND SCA EA 53-0121 REV 00.

Part: NONE — NONE · airframe 24,299 hrs · 7,903 cycles

N/R00071: ***CORROSION*** ON 986 FLOORBEAM UPPER FLANGE STA 986.5, LBL50-RBL50, WL208. RESOLUTION: REPAIRED FLOORBEAM UPPER CAP BS986.5, LBL50-RBL50, WL208 I.A.W. B737 SRM 53-10-51-2R.

Part: NONE — NONE · airframe 23,314 hrs · 7,586 cycles

DEFECT: 3/31/2022 - SMOKE IN FLIGHT DECK UPON POWER UP TO TAXI. RAN SMOKE QRH PROCEDURE. MXC NOTIFIED. RESOLUTION 4/2/2022 - PERFORMED AMM TASK 21-00-01-100-801 REMOVED AND REPLACED PRIMARY AND SECONDARY HEAT EXCHANGERS AND RAN PACKS AND BLEEDS FOR 30 MINUTES WITH NO SMOKE. AIRCRAFT OK FOR SERVICE.

Part: PLATE — CORRODED (BS 500A-500I) · airframe 19,601 hrs · 6,403 cycles

FWD CARGO SIDE PLATE HAS CORROSION IN SEVERAL AREAS STA 500A TO 500I RBL 21. REMOVED AND REPLACED SIDE PLATE ZEE CHANNEL AND SPLICE SIDE PLATE ON FWD CARGO RT, PER B737-800 SRM 51-10-02 PAR 9 & SRM 53-00-53 REPAIR 5.

Part: SEAL — DAMAGED (PANEL) · airframe 19,601 hrs · 6,403 cycles

A-54-003 ENGINE PYLON PANEL 431AT METAL FINGER SEALS ARE WORN BOTH SIDES OF PANEL. REMOVED AND REPLACED METAL FINGER SEALS ON ENGINE PYLON PANEL 431AZ LT SIDE NO DAMAGE NOTED ON THE RT SIDE, REFERENCE BOEING 737 SRM 51-40-02.

Part: SEAL — DAMAGED (PANEL) · airframe 19,601 hrs · 6,403 cycles

PANEL 441AL FINGERSEAL DAMAGED. REMOVED AND REPLACED SEAL 1 EA ON FINGERSEAL PANEL 441AL, IAW B737-800 AIPC 54-52-00-01E AND SRM 51-40-02 STEP 5B, 8B(1) & C AND FIG 15 (1-7).

Part: SEAL — DAMAGED (PANEL) · airframe 19,601 hrs · 6,403 cycles

FINGERSEAL DAMAGED PANEL 431AL. REMOVED AND REPLACED SEAL 1 EA ON FINGERSEAL PANEL 431 AL, IAW B373-800 AIPC 54-52-00-01E AND SRM 51-40-02 STEP 5B, 8B(1) & C, AND FIG 15 (SHEET 1-7).

Part: SEAL — DAMAGED (PANEL) · airframe 19,601 hrs · 6,403 cycles

FINGERSEAL DAMAGED PANEL 431AR. REMOVED AND REPLACED SEAL 1 EA ON FINGERSEAL PANEL 431 AR, IAW B737-800 AIPC 54-52-00-01E AND SRM 51-40-02 STEP 5B, 8B(1) & C AND FIG 15 (SHEET 1-7).

Part: SEAL — DAMAGED (PANEL) · airframe 19,601 hrs · 6,403 cycles

PANEL 441AR FINGERSEAL DAMAGED. REMOVED AND REPLACED SEAL 1 EA ON FINGERSEAL PANEL 441AR, IAW B737-800 AIPC 54-52-00-01E AND SRM 51-40-02 STEP 5B, 8B(1) & C, AND FIG 15 (SHEET 1-7).

Part: RAIL — CORRODED (FWD CARGO BLKHD) · airframe 19,601 hrs · 6,403 cycles

FWD CARGO AFT BULKHEAD LOWER RAIL HAS CORROSION IN SEVERAL AREAS 500 RBL 21 TO LBL 21. REMOVED CORROSION ON FWD CARGO BULKHEAD LOWER RAIL, 100% MATERIAL LOSS. FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED FWD CARGO AFT BULKHEAD LOWER RAIL, IAW B737-800 SRM 51-10-02 AND B737-800 SRM 51-40-02.

Part: SKIN — DENTED (FUSELAGE) · airframe 10,860 hrs · 3,597 cycles

FOUND DENT BELOW THE R1 DOOR 3" ABOVE STR R-22 AND 16.5" AFT OF STA 291.5, APPROX 3" IN HEIGHT, 1.5" IN WIDTH AND 0.082" IN DEPTH. DAMAGE ADJACENT TO FRAME. DENT REQUIRES REPAIR. ACCOMPLISHED A BORESCOPE INSPECTION OF THE BACK SIDE OF THE DENT AND FOUND NO DAMAGE IN THE AREA OF THE DENT OTHER THAN THE PUSHED IN / BACK SIDE OF THE DENT. DENT PLACED ON MTI. ALSO ENTERED IN SCRATCH AND DENT LOG. DENT REPAIRED, COMPLETED 01NOV17.

Part: SKIN — DAMAGED (NR 1 NACELLE) · airframe 10,860 hrs · 3,597 cycles

AFT FAIRING SKIN PANEL OUTBOARD OF THE NR 1 ENGINE DAMAGED. THE PANEL WAS REMOVED AND REPLACED.

Part: PANEL — CRACKED (LT WING LE) · airframe 10,860 hrs · 3,597 cycles

LEFT LEADING EDGE PANEL 521TB CORNER CRACKED. REMOVED AND REPLACED THE LEADING EDGE PANEL. OK FOR SERVICE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 1,655 hrs · 488 cycles

BOTH LT AND RT OVERWING EMERGENCY LIGHTS ARE INOPERATIVE. R & R BOTH LT AND RT BULBS.