N273NV

Part: MEGAPHONE — NO TEST (ZONE 200) · airframe 40,656 hrs · 27,021 cycles

(AIRCRAFT NOT GROUNDED) F.A.'S REPORT 1 MEGAPHONE DOES NOT TEST PROPERLY. / PERFORMED OPERATIONAL CHECK OF FWD FA MEGAPHONE PER AMM 25-65-51-710-002-A. OPS CHECK GOOD."

Part: EPSU — NO TEST (ZONE 200) · airframe 40,539 hrs · 26,962 cycles

(AIRCRAFT NOT GROUNDED) FAILED EPSU SYSTEM TEST. REMOVED AND REPLACED EPSU REF WO531467"

Part: BATTERY PACK — NO TEST (ZONE 200) · airframe 39,583 hrs · 26,494 cycles

(AIRCRAFT NOT GROUNDED) CABIN EMERGENCY LIGHTINGCHECK BATTERY CAPACITY FAILURE / REMOVED AND REPLACED EPSU BATTERY 10WL, 11WL, 12WL, 13WL IAW AMM 33-51-38-000-002-A/33-51-38-400-002-A. OPS CHECK GOOD"

Part: FRAME — CRACKED (ZONE 200) · airframe 38,011 hrs · 25,809 cycles

DURING INSPECTION AS PER ALLEGIANT WORK CARD 53-260-003 IN THE FR68LHS DOOR STOP FITTING 1 LOWER INBOARD HOLE CRACK WAS FOUND. THIS DAMAGE WAS REPAIRED IN ACCORDANCE A320 SRM 53-41-12-300-011 AND 53-41-12-300-011 PARAG 2A FIG 008. THIS REPAIR IS MAJOR CAT B. THIS REPAIR WAS DOCUMENTED UNDER COOPESA JOBA1P213 ITEM 2-75

Part: DOOR SILL — CORRODED (ZONE 200) · airframe 38,011 hrs · 25,809 cycles

DURING INSPECTION AS PER ALLEGIANT WORK CARD 534143-01-3-001 , UPPER FUSELAGE FROM FR67/FR68 STGR23LH AFT ENTRY DOOR SILL WIHT DAMAGED ANCHOR NUT ,CORROSION AND BARE METAL AROUND FASTENER HEAD. THE UPPER FUSELAGE AT FR68-26MM AT LEVEL STGR 23LH L2 AFT ENTRY DOOR SILL IAW A320 SRM 53-41-14-300-001 PRINCIPLE 5. REMOVED AND INSTALLED ANCHOR NUT IAW A320 PMS 01-05-46 PARAG 3.5.2 AND 3.3.2 MAJOR CATEGORY CAT A. THIS REPAIR WAS DOCUMENTED UNDER COOPESA A1P213 ITEM 2-88.

Part: SKIN — DELAMINATED (ZONE 300) · airframe 38,011 hrs · 25,809 cycles

DURING INSPECTION AS PER ALLEGIANT WORK CARD 554003-01-1-001 AND REMOVAL OF RUDDER TO COMPLY WITH NON ROUTINE ITEM 3-52 WAS FOUND RH UPPER AND LOWER HOIST POINTS LOOSE AND DAMAGED. PERFORMED PERMANENT REPAIR CAT A AT RUDDER SHELL SKIN PANEL RH AROUND UPPER # 3 HOIST POINT IAW A320 SRM 55-41-13-300-029 PARAG 2A AND AROUND LOWER FWD # 2 HOIST POINT IAW A320 SRM 55-41-13-300-030 PARAG 2A

Part: LUG — CRACKED (ZONE 300) · airframe 38,011 hrs · 25,809 cycles

DURING INSPECTION AS PER ALLEGIANT WORK CARD 552600-01-001, EMPENAGE LH ELEVATOR I/B AND O/B ACTUATOR FITTING O/B LOCKING LUG WITH CRACK WAS FOUND. PERFORMED REPAIR AT LH ELEVATOR I/B AND O/B ACTUATOR FITITNG LOCKING LUG IAW A320 SRM 55-26-47-300-001 PARAG 2A FIG 001 SHEET 1. THIS REPAIR IS CAT A. THE REPAIR WAS DOCUMENTED UNDER COOPESA JOB A1P213 ITEM 3-47.

Part: SKIN — DELAMINATED (ZONE 300) · airframe 38,011 hrs · 25,809 cycles

DURING INSPECTION AS PER ALLEGIANT WORK CARD 554003-01-1-001, EMPENNAGE RUDDER RH SIDE PANEL WITH DELAMINATION AROUND TRAILING EDGE FASTENER # 12.PERFORMED PERMANENT REPAIR CAT A AT RUDDER SHELL SKIN PANEL RH T/E FASTENER 12 (ZONE W) IAW A320 SRM 55-41-13-283-016 ADL PARAG 2.A(2) TABLE 4, FIG 002 AND A320 SRM 55-41-13-300-025 PARAG 2A. THE REPAIR WAS DOCUMENTED UNDER COOPESA JOB A1P213 ITEM 3-52

Part: DOOR FRAME — CRACKED (ZONE 200) · airframe 38,011 hrs · 25,809 cycles

DURING INSPECTION AS PER ALLEGIANT WORK CARD 53-260-003 IN THE FR68RHS DOOR STOP FITTING 1 LOWER INBOARD HOLE CRACK WAS FOUND. THIS DAMAGE WAS REPAIRED IN ACCORDANCE A320 SRM 53-41-12-300-008/010. THIS REPAIR IS MAJOR CAT B. THIS REPAIR WAS DOCUMENTED UNDER COOPESA JOBA1P213 ITEM 2-76

Part: CONTROL HANDLE — OUT OF LIMITS (RT DOOR SLIDE) · airframe 38,011 hrs · 25,809 cycles

(AIRCRAFT NOT GROUNDED) REF: NRI 2-4 - PASSENGER CABIN, AFT RH DOOR, MECHANISM OF THE EMERGENCY ESCAPE SLIDE, LOAD OF THE EMERGENCY CONTROL HANDLE IS OUT OF LIMITS. / PERFORMED AFT RH DOOR FUNCTIONAL TEST OF THE RELEASE MECHANISM OF THE EMERGENCY ESCAPE SLIDE IAW A320 AMM TASK 52-10-00-720-005-A. COOPESA A1P213 2-4. NOTE: FOR LUBRICATION SEE ITEM 7-94.

Part: CONTROL HANDLE — OUT OF LIMITS (ZONE 800) · airframe 38,011 hrs · 25,809 cycles

(AIRCRAFT NOT GROUNDED) REF: NRI 2-3 - PASSENGER CABIN, AFT LH DOOR, MECHANISM OF THE EMERGENCY ESCAPE SLIDE, LOAD OF THE EMERGENCY CONTROL HANDLE OUT OF LIMITS. / PERFORMED AFT LH DOOR FUNCTIONAL TEST OF THE RELEASE MECHANISM OF THE EMERGENCY ESCAPE SLIDE IAW A320 AMM TASK 52-10-00-720-005-A. COOPESA A1P213 2-3. NOTE: FOR LUBRICATION SEE ITEM 7-92.

Part: EPSU — NO TEST (EMERGENCY LIGHTS) · airframe 37,413 hrs · 25,505 cycles

ALL EPSU BATTERIES REQUIRE REPLACEMENT. FAILED BATTERY CAP TEST. / REMOVED AND REPLACED ALL 4 CABIN EPSU BATTERIES (10WL, 11WL, 12WL, AND 13WL) IAW AMM 33-51-38-000-002-A AND 33-51-38-400-002-A. OPS CHECK GOOD."

Part: EPSU — FAULTED (EMERGENCY LIGHTS) · airframe 36,806 hrs · 25,270 cycles

EPSU 12WL BAT FAULT / R+R EPSU 12WL BATTERY IAW AMM 33-51-38-400-002-A. OPS CHECK GOOD"

Part: SKIN PANEL — DENTED (ZONE 600) · airframe 31,761 hrs · 23,198 cycles

DURING THE ALLEGIANT WORK ORDER 00440067-17 WAS FOUND RH WING LE SLAT #2 WITH DENT ON UPPER SIDE OF RT #2 LE SLAT 6-8 OUTBOARD OF PYLON STS EA 80-2021-097 REV IR. CORRECTIVE ACTION: REPAIRED SLAT SKIN LE AREA FROM INBD TRACK+75.5MM TO INBD TRACK+104.5MM PER A320 SRM TASK 57-40-00-300-033 FIGURE 001 SHEET 1, 7 THRU 11 REV. 138 DATED 08-01-2021. SEE COOPESA JOB: A1K285, ITEM 18-11 FOR DETAILS.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 34,512 hrs · 24,334 cycles

L1 AND R1 EMERGENCY LIGHTS AND SIGNS ARE INOP WHILE ON BATTERY POWER / REMOVED AND REPLACED FWD BATTERY OPS CHECK GOOD REF TSM 33-51-00-810-812-A"

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 34,491 hrs · 24,326 cycles

EPSU TEST SHOWS FAULT AT 11WL / REMOVED & REPLACED EPSU BATTERY AT 11WL AND OPS CHECK GOOD IAW AMM 33-51-38-400-002-A"

Part: BATTERY — INOPERATIVE · airframe 34,182 hrs · 24,195 cycles

OPERATIONAL TEST OF EPSU BAT CAP TEST AND FOUND AFT LEFT BATTERY OF THE EPSU REQUIRED A REMOVAL AND REPLACE. / REMOVED AND REPLACED AFT LEFT BATTERY OF THE EMERGENCY POWER SUPPLY UNIT. IAW AMM 33-51-38-000-002-A AND AMM 33-51-38-400-002-A"

Part: BATTERY — INOPERATIVE · airframe 33,980 hrs · 24,100 cycles

WHILE PERFORMING EMERGENCY LIGHT CHECK DURING WEEKLY EPSU (12WL) EMER R FAILED / REMOVED AND REPLACED 12WL BATTERY WITH INSPECTED BATTERY IAW AMM 33-51-38-000-002-A, 33-51-38-400-002-A. OPS CHECK GOOD. NO OTHER DEFECTS NOTED AT THIS TIME. BITE TEST GOOD."

Part: NONE — NONE

NRC 2000-0018: 031-2 EXTERNAL FUSELAGE SKIN AREA OF FRAME 2 AND 14IN ABOVE Z-339 LH SIDE, PREVIOUS DENT OUT OF LIMIT CATEGORY C, PERMENENT REPAIR NEED TO DO AT THIS VISIT. REFERENCE TASK CARD # 4002010-0000-0002 AND # 4002010-0000-0004 DAMAGE ID # 76./031-2 EXTERNAL FUSE SKIN AREA OF FRAME 2 AND 14 INCHES ABOVE Z-339 LH SIDE, REPAIRED AS PER SRM 53-11-11-300-041. SEE AWS FOR ADDITIONAL WORK DETAILS. REPAIR CATEGORY ""B"" RE-INSPECTION AS PER SRI 53-11-11-205-037. INSPECTION THRESHOLD: 60000 FC OR 120000 FH (WHICHEVER OCCUR FIRST) CURRENT FC: 24039 CURRENT FH: 33838.0"

Part: NONE — NONE · airframe 33,838 hrs · 24,039 cycles

NRC 2000-0016: 031-1 EXTERNAL FUSELAGE SKIN AREA OF FRAME 9 AND 11.9IN ABOVE LH SLIDING WINDOW CUTOUT, PREVIOUS DENT OUT OF LIMIT CATEGORY C, PERMENENT REPAIR NEED TO DO AT THIS VISIT. REFERENCE TASK CARD # 4002010-0000-0001 DAMAGE ID # 77. / ON EXTERNAL FUSELAGE SKIN, AT FR9 AREA, AND 11.9'' ABOVE L/H SLIDING WINDOW CUTOUT, PERMANENT REPAIR PERFORMED AS PER SRM 53-11-11-300-075 REV. 141. SEE AWS FOR NDT REPORTING AND WORK PERFORMED DETAILS. REPAIR CATEGORY B. REINSPECTION TO BE PERFORMED AS PER SRI 53-11-11-205-055. CURRENT FC: 24039 FH: 33838.00. INSPECTION THRESHOLD OF 48 000 FC OR 96000FH FROM TIME OF ADL/REPAIR EMBODIMENT. DEFECT ITEM #77."

Part: NONE — NONE · airframe 33,838 hrs · 24,039 cycles

NRC: 9000-0008 RH AFT DOOR COUOUT EMERGENCY SIGN LENS BROKEN / RH AFT DOOR CUTOUT EMERGENCY SIGN LENS REPLACED IAW AMM 33-51-13-400-001-A"

Part: MEGAPHONE — NONE · airframe 33,090 hrs · 23,749 cycles

FORWARD MEGAPHONE INOP / R/R FWD MEGAPHONE PER LOPA A2250011L03"

Part: NONE — NONE · airframe 32,632 hrs · 23,564 cycles

L1 FLIGHT ATTENDANT FLASHLIGHT NOT WORKING. / REMOVED AND REPLACED BATTERY ASSY FOR L1 DOOR FA BATTERY IAW AMM 25-60-10. OPS-CHECK GOOD."

Part: EPSU — FAILED (12WL) · airframe 31,939 hrs · 23,276 cycles

BATTERY AT FIN 12WL FAIL EPSU BATTERY CAP TEST / REMOVED AND REPLACED BATTERY IAW AMM 33-51-38. OPS CHECKS GOOD"

Part: PLATE — CORRODED (ZONE 500) · corrosion level 2 · airframe 31,761 hrs · 23,198 cycles

LH WING FIXED TRAILING EDGE REAR FALSE SPAR OVERHANG WITH CORROSION BETWEEN WING RIB 7 AND 8. NOTE: THE TOP SKIN PANEL 2 WAS REPAIRED AS PER AIRBUS DOSSIER NO: 80981761 GUIDELÑINES AS STATED IN COOPESA ENGINEERING ORDER NO: COO-EO-2021-14151 INSTRUCTIONS (FOR ADDITIONAL DETAILS SEE COOPESA JOB: A1K285 NON ROUTINE ITEM: 5-1 DOCUMENTS).

Part: EPSU — NO TEST (EMERGENCY LIGHTS) · airframe 30,151 hrs · 22,532 cycles

EMERGENCY LIGHT BATTERY 10WL FAILED. / R&R'D EPSU BATTERY REF AMM 33-51-38 PB 401 OPS CHECK GOOD.

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHTS) · airframe 29,513 hrs · 22,260 cycles

WORK CARD 335100-03-1-001 CABIN EMERGENCY LIGHTING TEST FAILED. EPSU BATTERY 11WL AND 13WL REQUIRE REPLACMENT. R & R EPSU BATTERY 11WL AND 13WL, PER AMM 33-51-38-000-002-A AND 33-51-39-400-002-A. OPERATIONS CHECK GOOD.

Part: BATTERY PACK — WARNING MESSAGE (EMERGENCY LIGHTS) · airframe 29,096 hrs · 22,098 cycles

BAT/EPSU 10WL FWD L MSG DISPLAYED / REPLACED EPSU 10WL FWD L BATT IAW AMM 33-51-38-000-002-A/33-51-38-400-002-A OPS CHECK GOOD IAW AMM 33-51-00-710-001-A"

Part: STRINGER SPLICE — CORRODED (FRAMES 28-29) · corrosion level 2 · airframe 23,742 hrs · 19,835 cycles

DURING SCHEDULED MAINTENANCE, FOUND FORWARD CARGO STRINGER 44R SPLICE WAS CORRODED AT FRAME 28.

Part: SKIN — DENTED (FRAMES 1 & 2) · airframe 23,742 hrs · 19,835 cycles

DURING SCHEDULED MAINTENANCE, THE FUSELAGE SKIN RT, AFT OF BULKHEAD, FRAMES 1 & 2 APPROX. STR. 33 WAS DENTED. S/O 193052 N/R 38031