N306NV

AIRBUS A319-112 None injury Part 121 — ALLEGIANT AIR, LLC

ATA 2120

(AIRCRAFT NOT GROUNDED) DIRTYS SOCK SMELL REPORTED BY ALL FA'S (T/O VERY STRONG LINGERING TOP OF DESCENT STRONG, LINGERING ON LANDING & TAXI IN / PERFORMED TASK CARD A32X-21-000-001. NO SMELLS NOTED. A/C OK FOR SERVICE.

ATA 2120

(AIRCRAFT NOT GROUNDED) DIRTY SOCK ODOR OBSERVED THROUGHOUT CABIN DURING DESENT AND APPROACH BEGINNING AT 18,000 FEET. AIR SMS REPORT SUBMITTED. / PERFORMED RE INSPECTION OF WORK PERFORMED FROM TASK CARD A32X-21-000-001 IAW ALLEGIANT PROCEDURES. NO DISCREPANCIES FOUND. M313 MDDR # 231848 GENERATED TO PERFORM LEVEL 2 TASK CARD THE NEXT 5 CALENDAR DAYS."

ATA 2120

(AIRCRAFT NOT GROUNDED) DIRTY SOCK ODOR REPORTED BY ALL FA'S AND SEVERAL PAX. SMELL DETECTED IN FWD, MID, AND AFT CABIN. DURATION 5 MINUTES ALTITUDE 3500 MSL DURING APPROCH. APU OFF. / T/S PER TSM 05-50-00-810-831-A AND PERFORMED TC A32X-21-00-001 SMELL REPRODUCED WITH APU BUT NOT WITH ENGINES.C/W LEVEL 2 ODOR EVENT TASK CARD 21-000-002. COMPLIED WITH PHASE 3 OIL TYPE SMELL WORK CARD NO 21-000-003 COMPLETED.

ATA 2120

AIRCRAFT NOT GROUNDED, WET SOCK SMELL OCCURED DURING DESCENT STARTING AT APPROX 7000 FT. STARTED DISSIPATING AT 2000 FT. WAS GONE AFTER TOUCHDOWN. PILOTS AND ENTIRE CABIN SMELLED ODOR. BOTH PACKS ON, APU OFF. ACCOMPLISHED TASK CARD 21-000-001. NO ODOR DETECTED. PREFORMED TC 21-000-002 THIS ACTION CLEARS M313 MDDR #229248 (W/O: 547466, TASKCARD: NR-00002). C/W POST LEVEL 3 TASK CARD A32X-05-000-011. NO DEFECTS FOUND AT THIS TIME.

ATA 3350

(AIRCRAFT NOT GROUNDED) DUE TO WEEKLY CHECK , PERFORMED BITE TEST ON EPSU BATTERY. BATTERY AT FIN 13WL FOUND NOT SERVICABLE. REMOVED AND REPLACED EPSU BATTERY AT FIN 13WL IAW AMM 33-51-38-000-002-A AND 33-51-38-400-002-A"

ATA 3350

(AIRCRAFT NOT GROUNDED) FAILED CAPACITY TEST. C/W TC A32X-335100-03-1-001. REMOVED AND REPLACED ALL FOUR EPSU BATTERIES DUE TO CAPACITY FAILURE IAW AMM 33-51-38-000-002-A AND 33-51-38-400-002-A. OP'S CHECKS SATISFACTORY. WO# 521556, WEEKLY CHECK AND CABIN EMERGENCY LIGHTING BATTERY TEST ACCOMPLISHED. AWR ACCOMPLISHED IAW GMM CHAPTER 2 SECTION 6."

ATA 2560

(AIRCRAFT NOT GROUNDED) FWD FA MEGAPHONE FOUND EXPIRED / REMOVED AND REPLACED EXPIRED MEGAPHONE AND RESECURED PER LOPA A1250001LO3_REV L"

ATA 3350

AFT LH BATTERY FAILED EPSU BATTERY CAPACITY CHECK / REMOVED EPSU BATTERY AFT LH (13WL) REF. AMM 33-51-38-000-002-A AND INSTALLED SERVICEABLE BATTERY REF. AMM 33-51-38-400-002-A. OPERATIONAL CHECK OKAY"

ATA 5321

DURING THE ALLEGIANT ENGINEERING ORDER NUMBER E53331-0006 REV. 03 INSPECTION AND E53331-0007 REV. REV. 03 DATED 08/07/2019 AS RELATED TO A.D. 2018-06-04, WE FOUND FASTENER CRACK ON PRESSURE PANEL TO FLEX AT FR 36 LH SIDE. CORRECTIVE ACTION: REPAIRED FR35-FR36 LH SIDE PRESSURE PANEL ATTACHMENT HOLES PER RDAF: 81029141/004/2022 #B DATED 02/28/2022 SEE COOPESA WORK ORDER: A1M078, ITEM: 9-3 FOR DETAILS.

ATA 5530

DURING A DROP-IN AT STS MOD CENTER IN MELBOURNE, FL (MLB), THE VERTICAL STABILIZER WAS REPORTED WITH RUDDER VIBRATION DURING FLIGHT. MAINTENANCE PERFORMED ALLEGIANT EO NO. E554-0010 TO INSTALL NEW VERTICAL TAIL PLANE (VTP) HINGE ARM FITTINGS EQUIPPED WITH BEARINGS AT BR1 THROUGH BR5 AND BR7, WITH THE INTENT OF REDUCING AIRCRAFT VIBRATION FINDINGS (PER SB55-1062). HOWEVER, HINGE ARMS BR2 AND BR3 WERE FOUND WITH ELONGATED HOLES AND CRACKS WITHIN HOLES (1,2, 4 THROUGH 9) IN BR2. MAINTENANCE REMOVED THE DAMAGE WITH THE FOLLOWING RESULTS: BR2 HOLE 3 WITH NOMINAL (0.250"), HOLES 1, 2, 4 THROUGH 8 ARE FIRST OVERSIZE (0.267"), HOLE 9 WITH A FINAL DIAMETER OF 0.312". BR3 HOLES 1 THROUGH 6, 8 AND 9 ARE FIRST OVERSIZE (0.265") AND HOLE 7 WITH A DIAMETER OF 0.312"

ATA 3300

EMERGENCY POWER SUPPLY UNIT 11WL FAILED CAPACITY TEST. / REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT BATTERY 11WL IAW AMM 33-51-38 PB 401 CONF 00."

ATA 3300

EMERGENCY POWER SUPPLY UNIT 13WL FAILED CAPACITY TEST. / EMERGENCY POWER SUPPLY UNIT 13WL REMOVED AND REPLACED IAW AMM'S 33-51-38-000-001-A AND 33-51-38-400-001-A. REFER NR00963807 FOR OPERATIONAL CHECK."

ATA 5330

DURING MAINTENANCE ACCOMPLISHMENT WERE FOUND TWO ATTACHING FASTENER HOLES WITH CRACKS LOCATED AT LH PRESSURE DECK MEMBRANE ONLY AT FR36 STR30-31LH, THE DAMAGES WERE FOUND OUT OF ALLOWABLE DAMAGE LIMITS AS PER SB A320-1263 AND SB A320-1264, DUE TO THIS FACT DETAILS WERE SENT TO AIRBUS ASKING FOR REPAIR INSTRUCTIONS AND FINAL APPROVAL. AFTER AIRBUS EVALUATION, REPAIR INSTRUCTIONS WERE PROVIDED UNDER DOSSIER 81029141. THE REPAIR WAS UNDLE UNDER COO JOB A1M078 ITEM 1-6

ATA 3350

LENS MISSING ON LIGHT NEAR EXIT SIGN ON R2 DOOR / R&R CABIN EMERGENCY LIGHT ASSEMBLY MOUNTED IN R2 DOOR IAW AMM 33-51-11 PB 401. OPS TEST GOOD. A/C OK FOR SERVICE"

ATA 3350

TC 335100-03-1-001 FAILED CAP CHECK. / REMOVE AND REPLACED EMERGENCY LIGHT BATTERY @ POSITIONS 10WL, 11WL, 12WL, & 13WL REF AMM 33-51-38 PB401. OPS CHECKS GOOD."

ATA 3350

CABIN EMERGENCY LIGHT FAULT (11 WL) / CLEANED CONNECTOR AT (11WL) MESSAGE CLEARED FROM CIDS1; TEST NORMAL REF TC 05-000-002 AND AMM 33-51-00. ALSO REF ESPM 20-55-40."

ATA 2910

(EMERGENCY DECLARED) HYD G ENG 1 LO PR IN FLIGHT / REMOVED AND REPLACED FLEX LINE & SWIVEL. LEAK CHECKS NORMAL IAW AMM 32-12-00-991-01500-00-A. PERFORMED A FUNCTIONAL TEST OF THE NORMAL EXTENSION AND RETRACTION OF THE LANDING GEAR, OPERATIONS NOMINAL, NO FAULTS OR DEFECTS NOTED W/ REF TO AIRBUS AMM 32-31-00-720-002-A."

ATA 3350

EPSU FAILED EMERGENCY LIGHTING TEST / REPLACED EMERGENCY BATTER PACK "

ATA 2913

(EMERGENCY DECLARED) HYD GREEN ENG 1 PUMP LO PR., HYD G RV1. LO / PERFORMED CHECK FOR CAVITATION, FOUND NO HYDRAULIC DPI'S EXTENDED OR PHYSICAL DAMAGE TO PUMP, AND NO SIGN'S OF LEAKS"

ATA 2910

(RMERGENCY DECLARED) G SYS LO PR / REPLACED FLEX HOSE OLD ELBOW FITTING"

ATA 2560

FWD MEGAPHONE INOPERATIVE. R & R THE MEGAPHONE.

ATA 2913

EMERGENCY DECLARED, HYD "Y" RSVR LOW LVL ECAM APPEARED. R&R DAMAGED FILTER PACKING.

ATA 2530

FLIGHT ATTENDANT REPORTS GALLEY OVEN CREATED A BURNING ELEC SMELL. ONCE OVEN TURNED OFF, SMELL WENT AWAY. DEFERRED OVEN IAW NEF 25-03A-01, CAT D, EXP 11/5. NEF LOG UPDATED.