N623NK

Part: BUSHING — CORRODED (ZONE 300) · airframe 41,206 hrs · 18,857 cycles

AFTER BUSHINGS REMOVAL CORROSION WAS FOUND ON INNER BORE HINGE FITTING Ñ4 OB LUG AT RH ELEVATOR (1 EA) RAF 3589622-02 CREATED -REPAIRED BOTH BORES AND REPLACED BUSHING (1 E/A) ON HINGE FITTING #4 OUTBOARD LUG AT RH ELEVATOR IAW SRM 55-26-41-300-005 THIS REPAIR IS CATEGORY B INSPECTION THRESHOLD FROM COMPONENT FIRST FLIGHT 6 YEARS SUBSEQUENT INSPECTION AT INTERVALS OF 6 YEARS NDT INSPECTION TYPE: DETAILED INSPECTION IAW SRI 55-26-41-205-001

Part: BUSHING — CORRODED (ZONE 300) · airframe 41,206 hrs · 18,857 cycles

AFTER BUSHING REMOVAL CORROSION WAS FOUND ON INNER BORE HINGE FITTING #1, 2, AND 3 AT LH ELEVATOR RAF 3589621-02 CREATED SEE APPENDIX 3589621-02-REPAIRED BOTH BORES AND REPLACED BUSHINGS (2 EA) ON HINGE FITTING #1,2 AND 3 AT LH ELEVATOR IAW SRM 55-26-41-300-004 THIS REPAIR IS CATEGORY B INSPECTION THRESHOLD FROM COMPONENTS FIRST FLIGHT 6 YEARS SUBSEQUENT INSPECTION AT INTERVALS OF 6 YEARS NDT INSPECTION TYPE: DETAILED INSPECTION IAW SRI 55-26-41-205-001

Part: BUSHING — CORRODED (ZONE 300) · airframe 41,206 hrs · 18,857 cycles

AFTER BUSHINGS REMOVAL CORROSION WAS FOUND ON INNER BORE HINGE FITTING Ñ6 AT RH ELEVATOR (2EA). RAF 3589622-01 CREATED-REPAIRED BOTH BORES AND REPLACED BUSHINGS (2 E/A) ON HINGE FITTING #6 AT RH ELEVATOR IAW SRM 55-26-41-300-006 THIS REPAIR IS CATEGORY B INSPECTION THRESHOLD FROM COMPONENT FIRST FLIGHT 6 YEARS SUBSEQUENT INSPECTION AT INTERVALS OF 6 YEARS NDT INSPECTION TYPE: DETAILED INSPECTION IAW SRI 55-26-41-205-001

Part: SKIN PANEL — CRACKED (ZONE 100) · airframe 41,206 hrs · 18,857 cycles

CRACK INDICATION FOUND IN FASTENER HOLE (LOWER INBOARD POSITION) LOCATED AT FR 68 DOOR STOP FITTING 1 RH SIDE. RAF 3589624-01 GENERATED -PERFORMED REPAIR ON FASTENER HOLE (LOWER INBOARD POSITION) LOCATED AT FR.68 DOOR STOP FITTING #1 RH SIDE SRM 53-41-12-300-008, 53-41-12-300-010 AND D53480082 REPAIR CATEGORY B INSPECTION THIS REPAIR AT DEFINED INTERVALS, REPAIR EMBODIMENT 24500 FC,FH NOT RELEVANT SUBSEQUENT INSPECTIO AT INTERVALS:10700 FC, FH NOT RELEVANT SRI 53-41-12-205-009

Part: SKIN PANEL — CRACKED (ZONE 100) · airframe 41,206 hrs · 18,857 cycles

CRACK INDICATION FOUND IN FASTENER HOLE ( LOWER INBOARD POSTION) LOCATED AT FR 68 DOOR STOP FITTING 6 LT SIDE. RAF 3589623-02 GENERATED -PERFORMED REPAIR ON FASTENER HOLE (LOWER INBOARD POSITION) LOCATED AT FR.68 DOOR STOP FITTING #6 LH SIDE IAW SRM 53-41-12-300-008, 53-41-12-300-010 AND DRAWING D53480082 REPAIR CATEGORY B INSPECTION THIS REPAIR AT DEFINED INTERVALS REPAIR EMBODIMENT 24500 FC FH NOT RELEVANT, INSPECTION AT INTERVALS 10700FC SRM 53-41-12-205-009

Part: BUSHING — CORRODED (ZONE 300) · airframe 41,206 hrs · 18,857 cycles

AFTER BUSHINGS REMOVAL CORROSION WAS FOUND ON INNER BORE HINGE FITTING Ñ3 AT RH ELEVATOR (2EA) RAF 3589623-01 CREATED-REPAIRED BOTH BORES AND REPLACED BUSHINGS (2 EA) ON HINGE FITTING #3 AT RH ELEVATOR IAW SRM 55-26-41-300-004 THIS REPAIR IS CATEGORY B INSPECTION THRESHOLD FROM COMPONENT FIRST FLIGHT 6 YEARS SUBSEQUENT INSPECTION AT INTERVALS OF 6 YEARS NDT INSPECTION TYPE: DETAILED INSPECTION IAW SRI 55-26-41-205-001

Part: FLASHLIGHT — NO TEST (ZONE 200) · airframe 41,145 hrs · 18,822 cycles

FLIGHT ATTENDANT POSITION L2 FLASHLIGHT INOP-R/R L2 FLASHLIGHT IAW AMM 25-63-00. OPERATIONAL CHECK OK. A/C OK FOR SVC.

Part: MEGAPHONE — INOPERATIVE (ZONE 200) · airframe 39,431 hrs · 17,964 cycles

FWD MEGAPHONE INOP-R+R MEGAPHONE IAW AMM 25-65-01. MOC 77744 NOTIFIED

Part: A/C PACK — ODOR (NR 1) · airframe 37,654 hrs · 17,070 cycles

FUME EVENT ON DECENT (PACK 1)-PERFORMED TSM 05-50-00-810-831-A. IDENTIFIED SOURCE OF ODOR TO BE PACK 1. SEE LP 3445741-2 FOR CORRECTIVE ACTION.

Part: UNKNOWN — ODOR (CABIN) · airframe 37,626 hrs · 17,052 cycles

FA SMELLED STRONG EXSAUST IF THE AFT GALLEY DURING DECENT / LANDING-PERFROMED TSM 05-50-00-810-831-A NO DEFECTS NOTED AT THIS TIME AFT GALLEY SMELLED OF CIGARETTES A/C OK FOR SERVICE MOC 109580

Part: A/C PACK — ODOR (NR 2) · airframe 37,380 hrs · 16,931 cycles

DIRTY SOCK SMELL MID-CABIN AFT GOING THROUGH 5000 ON LANDING FUMES QRH APPLIED PACK 2 OFF, X BLEED SHUT-SMEL PERSISTED -PREFORMED IDENTIFICATION OF CABIN ODOR IAW TSM 05-50-00-810-831-A FOUND PACK 2 TO BE SOURCE OF FUME EVENT. REF LOG PAGE 3446070-2

Part: UNKNOWN — ODOR (CABIN) · airframe 37,377 hrs · 16,930 cycles

FA'S STATED THAT WHEN THE GEAR CAME DOWN AT 2000FT THEY SMELLED A WET SOCK SMELL-PERFORMED FUME EVENT FAULT ISOLATION PROCEDURES IAW TSM 05-50-810-831. PERFORMED ENGINE RUNS OF ENG #1 & ENG #2 IAW AMM 71-00-00."NO FUMES OR SMOKE NOTED." R&R RECIRC FILTERS IAW AMM 21-21-41. OK FOR SVC.

Part: UNKNOWN — ODOR (CABIN) · airframe 36,757 hrs · 16,649 cycles

FUME EVENT DIRTY SOCK SMELL FRONT OF AIRCRAFT SLOWING TO APPROACH SPEED. TURNED PACK 1 OFF SMELL DISAPATED ( PACKS - A320 WITH MOD. 30626/MP K6443 (ENHANCED ECS) OR A321 WITH MOD. 157080/MP K17996 (PACK FLOW SELECTOR) AND WITH MOD. 30626/MP K6443 (ENHANCED ECS) )--

Part: A/C PACK — ODOR (NR 1) · airframe 36,743 hrs · 16,644 cycles

"DIRTY SOCK" SMELL FUME EVENT JUST PRIOR TO LANDING- 8000FT. 210 KTS, LOW THRUST. TURNING PACK 1 OFF IMMEDIATELY CLEARED THE ODOR.-PERFORMED TSM 21-00-00-810-802-A AND TSM 05-50-00-810-831. PERFORMED ENG 1 AND ENG 2 RUNS IAW AMM 71-00-00. NO DIRTY SOCK SMELL NOTED. PERFORMED OPS TEST OF APU IAW AMM 49-00-00. RAN PACK 1 AND PACK 2 ISOLATED. NO SMELL NOTED DURING AND OPERATION. NO FURTHER DEFECTS NOTED. A/C OKAY FOR CONTINUED SERVICE.

Part: A/C PACK — ODOR · airframe 36,253 hrs · 16,430 cycles

SMELL OF CAT URINE IN COCKPIT AND CABIN DID FUME ELIMINATION QRH AND PACK 1+2 FAULT-PERFORMED PACK BURN IAW AMM 21-00-00 PACK 1 GOOD NO SMELL NOTED. PACK 2 FAULTED DURING TEST AND TRANSFERED TO LOG PAGE 3354563-2. A/C OK FOR SERVICE.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 36,093 hrs · 16,356 cycles

FUME /DIRTY SOCKS SMELL DURING DESCENT THROUGH 10-12,000FT.-PERFORMED LEVEL B REMOVAL OF THE CONTAMINATION OF THE ECS (PACK 2) IAW AMM 21-00-00-615-803-A OPS CHK GOOD NO SCENT NOTED A/C OKAY FOR SVC

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 36,020 hrs · 16,330 cycles

FUME EVENT DESCENDING 7,000 SMELL VINEGAR-PER TSM 05-50-00-810-831 RAN BOTH PACKS ON APU BLEED NO SIGN OF CONTAMINATION.RAN BOTH ENG BLEED FOUND NO CONTAMINATION FROM ENG#2 PACKS 2 BUT HAD ODOR FROM ENG#1 PACK1.R/R BOTH RECIRCULATION FILTERS IAW AMM 21-21-41.A/C OK FOR SVC

Part: FLASHLIGHT — INOPERATIVE (FWD GALLEY) · airframe 35,696 hrs · 16,194 cycles

FWD LH FA JUMPSEAT FLASHLIGHT INOP. ( FLASHLIGHT AND HOLDERS (FLIGHT DECK OR CABIN) )-R/R FLASHLIGHT ASSY. IAW AMM 25-6-000. OPS CHECK GOOD. THIS CLEARS DMI#3291772-1. MOC NOTIFIED. PLACARD REMOVED. DMI LOG UPDATED.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 34,228 hrs · 15,539 cycles

AROUNF 5000 FT ON DOWNWIND SMELLY SOCK SMELL FAR ABOUT 2 MINS COCKPIT-OPS TEST IAW 36-11-00 NO SMELLS NOTED AT THIS TIME. ACFT OK FOR CONT SRVC

Part: MEGAPHONE — INOPERATIVE (ZONE 900) · airframe 31,606 hrs · 14,409 cycles

MEGAPHONE INOP-R + R MEGAPHONE IAW AMM 25-63-00. OPS CHECK GOOD

Part: NONE — DAMAGED (RUDDER HINGE) · airframe 31,584 hrs · 14,399 cycles

RUDDER HINGE ARM BEARING #4 HAS ELONGATED HOLE IN EXISTINE REPAIR. RAF-01 2907254-02 GENERATED-ACCOMPLISHED VERTICAL STAB ATTACHMENT FITTINGS HINGE ARM BR4 EXISTING BUSHING REPAIRS AND ENLONGATED HOLES REPAIR IN ACCORDANCE WITH EA # 55-0489-22 REVISION # 0 REPAIR CATEGORY B REPAIR CLASSIFICATION MINOR AND IAW EO 5536-2211

Part: NONE — DAMAGED (RUDDER #3) · airframe 31,584 hrs · 14,399 cycles

RUDDER HINGE FITTING #3 REQUIRE REPLACEMENT DUE TO ELONGATED BUSHINGS IN PREVIOUS REPAIRS. RAF-01 2907255-01-ACCOMLPISHED VERTICLE STAB ATTACH FITTING HINGE ARM BR 3 REPLACEMENT IN ACCORDANCE WITH EA # 55-0488-22, REVISION # O. REPAIR CATEGORY "A", REPAIR CLASSIFICATION "MAJOR " AND IN ACCORDANCE WITH EO # 5536-2210.

Part: PROXIMITY SENSOR — OUT OF ADJUST (AFT CARGO DOOR) · airframe 28,143 hrs · 12,838 cycles

DOOR AFT CARGO INDICATION OPEN IN FLIGHT ( ECAM DOOR PAGE INDICATIONS CARGO DOOR )-PERFORMED ADJUSTMENT OF 32WV PROX SW IAW AMM 52-71-00 OPS CHECK GOOD. THIS CLEARS DMI# 2778592-1 MXC NOTIFIED

Part: BOTTLE — LOW PRESSURE (R2 DOOR) · airframe 26,573 hrs · 12,105 cycles

R2 DOOR BOTTLE LOW. SERVICED R2 DOOR IAW AMM 52-10-00.

Part: A/C PACK — ODOR (AC BAY) · airframe 24,717 hrs · 11,255 cycles

DESCENDING THROUGH 7000' FA'S REPORTED OIL SMELL. PERFORMED SUPP PROC, ISOLATED PACK 1, SMELL DISSIPATED. ( PACKS A320 WITH MOD 31283/MP P7125 (FWC H2-F1 STND) AND WITH MOD. 30626/MP K6443 (ENHANCED ECS) - FAULT CAUTIONS ASSOCIATED WITH OPERATIVE SIDE NOT DISPLAYED )--

Part: UNKNOWN — ODOR (CABIN) · airframe 23,405 hrs · 27,712 cycles

DURING FLIGHT FA REPORTSD STRONG ELECTRICAL ODOR ROW 14-UPON ARRIVAL, NO ODOR PRESENT. DROPPED CEILING PANELS AND SIDEWALL AND PSU PANELS IN SUSPECTED AREA. FLIR INFARED CAMERA USED BY FIRE DEPT, NO HOT SPOTS OR HEAT SOURCE FOUND. INSPECTED AIRCRAFT WITH SNIFFER, NO TRACES FOUND. VISUALLY INSPECTED LIGHTS, BALLASTS,WIRING AND INFLATABLE SEAT BELT CONTROLLERS, NO SMELL OR DAMAGE FOUND. NO C/B'S POPPED. INSPECTED BAG BINS AND WHEEL WELLS, WITH FIREMAN NO HEAT SOURCE OR ODOR FOUND. NO ODOR FROM APU BLEED. RAN BOTH ENGINES, NO ODOR FOUNDOR TRACES FROM SNIFFER IN PACKS. COULD NOT DUPLICATE A/C OK FOR SERVICE I/A/W TSM 24-00-00 AND 05-50-00 AND AMM 71-00-00

Part: HANDSET — MALFUNCTIONED (AFT GALLEY) · airframe 23,192 hrs · 10,543 cycles

AFT GALLEY HAND MICROPHONE STUCK IN THE ON/TALK POSITION -R/R AFT GALLEY MEGAPHONE IN REF SPIRIT DRAWING EMERGENCY EQUIPMENT A320

Part: HINGE FITTING — CORRODED (RUDDER) · airframe 23,015 hrs · 10,461 cycles

RUDDER HINGE ARM FITTING AND HINGE ARM BEARING 3 HAVE ELONGATED HOLES. RAF-01 244097401 OPENED-PERFORMED PERMANENT REPAIR AS PER SPIRIT AIRLINES EO 5536-1902 (N623NK-PERMANENT REPAIR OF ELONGATED HOLES ON VERTICAL STABILIZER

Part: UNKNOWN — ODOR · airframe 16,715 hrs · 7,649 cycles

ODOR EVENT ON FINAL APPROACH. PERF TSM 05-50-00-810-831-A ISOLATED PACKS, APU, ENGINES. COULD NOT DUPLICATE SMELL. A/C OK FOR SERVICE.

Part: MEGAPHONE — INOPERATIVE (GALLEY) · airframe 11,688 hrs · 5,331 cycles

AFT GALLEY MEGAPHONE UNSERVICEABLE. R & R AFT GALLEY MEGAPHONE IAW DRAWING NK320-232-EQ REV 4.

Part: OXYGEN MASK — BROKEN (COCKPIT) · airframe 10,244 hrs · 4,654 cycles

F/O OXYGEN MASK RED INFLATION GRIP BROKEN. R & R F/O'S OXYGEN MASK & OPS CHECKED GOOD IAW 35-12-41. NO FURTHER DEFECTS

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 9,838 hrs · 4,464 cycles

F/O EMERGENCY FLASHLIGHT INOPERATIVE.

Part: STRUCTURE — DAMAGED · airframe 4,093 hrs · 1,895 cycles

CREW REPORTED A LIGHTNING STRIKE AFTER DEPARTURE. DIVERTED, DECLARED EMERGENCY. EXTENSIVE DAMAGE FOUND ON ACFT. L

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 1,905 hrs · 913 cycles

F/O FLASHLIGHT INOPERATIVE. REPLACED FLASHLIGHT IAW AMM 33-10-00. OPS CHECKED NORMAL.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 789 hrs · 371 cycles

R4 F/A SEAT FLASHLIGHT WILL NOT TEST". R & R R4 DOOR F/A SEAT FLASHLIGHT IAW CMM. OPS CHECKED & TESTED GOOD.

Part: FLASHLIGHT — NO TEST (AFT CABIN) · airframe 535 hrs · 241 cycles

AFT F/A FLASHLIGHT INOPERATIVE DURING FUNCTIONAL TEST. R & R FLASHLIGHT IAW AMM. OPS CHECKED GOOD.