N306NV

Part: BATTERY PACK — NO TEST (ZONE 200) · airframe 54,320 hrs · 32,618 cycles

(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"

Part: BATTERY PACK — NO TEST (ZONE 200) · airframe 53,618 hrs · 32,259 cycles

(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."

Part: MEGAPHONE — EXPIRED (ZONE 200) · airframe 52,092 hrs · 31,654 cycles

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

Part: EPSU — UNKNOWN (UNKNOWN) · airframe 50,256 hrs · 30,829 cycles

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"

Part: PRESSURE PANEL — CRACKED (ZONE 200) · airframe 47,299 hrs · 29,266 cycles

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.

Part: HINGE ARM — CRACKED (VERTICAL STAB) · airframe 29,799 hrs · 48,357 cycles

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"

Part: EPSU — NONE · airframe 48,037 hrs · 29,646 cycles

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."

Part: EPSU — NONE · airframe 48,037 hrs · 29,646 cycles

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."

Part: PRESSURE DECK — CRACKED (ZONE 100) · airframe 47,298 hrs · 29,266 cycles

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

Part: LENS — MISSING · airframe 47,192 hrs · 29,216 cycles

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"

Part: EPSU — FAILED (CABIN) · airframe 46,396 hrs · 28,769 cycles

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."

Part: CONNECTOR — DIRTY (EMERGENCY LIGHT) · airframe 46,142 hrs · 28,623 cycles

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."

Part: SWIVEL — LEAKING (HYD LINE) · airframe 46,018 hrs · 28,561 cycles

(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."

Part: BATTERY PACK — FAILED (CABIN) · airframe 44,057 hrs · 27,576 cycles

EPSU FAILED EMERGENCY LIGHTING TEST / REPLACED EMERGENCY BATTER PACK "

Part: WARNING MESSAGE — FALSE ACTIVATION (HYD PUMP) · airframe 43,736 hrs · 27,400 cycles

(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"

Part: HOSE — FAILED (HYD SYSTEM) · airframe 43,733 hrs · 27,399 cycles

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

Part: MEGAPHONE — INOPERATIVE (FWD CABIN)

FWD MEGAPHONE INOPERATIVE. R & R THE MEGAPHONE.

Part: PACKING — DAMAGED (HYDRAULIC SYS) · airframe 39,556 hrs · 25,301 cycles

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

Part: OVEN — ODOR (GALLEY) · airframe 32,065 hrs · 21,788 cycles

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.