N949FR

Part: FITTING — CRACKED (FRAME 16) · airframe 46,323 hrs · 22,213 cycles

DISCREPANCY: REFERENCE PEMCO N/R: 2650N340 RH FR16 UPPER DOUBLE JOGGLE AREA FWD LOWER HOLE (C) SHOWS CRACK INDICATION IN THE MIDDLE LAYER AT 9 OCLOCK POS. VIEWED FROM THE EXTERIOR CORRECTIVE ACTION: REPAIRED R/H FR16 UPPER DOUBLE JOGGLE FASTENER HOLE "C" PER AIRBUS REPAIR DRAWING R531-13041 ISSUE E AND EA: A9-53R-35035, HOLES #C AND #D REQ ROTOTEST REINSPECTION WITH A THRESHOLD OF 6800FC AND INTERVALS OF 4742 FC.

Part: FITTING — WORN (RT MLG DOOR) · airframe 46,323 hrs · 22,213 cycles

DISCREPANCY: REFERENCE PEMCO N/R: 2650N344 RH MLG DOOR AFT KEEL BEAM HINGE FITTING FWD LUG WORN TOTAL CYCLES 122,213 CORRECTIVE ACTION: REPAIRED R/H MLG DOOR AFT KEEL BEAM, HINGE FITTING LUG PER AIRBUS REPAIR R533 70508 ISSUE B, AREA REQ RE-INSPECTION WITH A THRESHOLD OF 8500FC AND INTERVALS OF 8500FC PER RDAS REF 80700416/006/2019

Part: HINGE FITTING — WORN (ZONE 100) · airframe 46,323 hrs · 22,213 cycles

DISCREPANCY: REFERENCE PEMCO N/R: 2650N343 LH MLG DOOR AFT KEEL BEAM HINGE FITTING FWD LUG WORN CORRECTIVE ACTION: REPAIRED L/H MLG DOOR AFT KEEL BEAM, HINGE FITTING LUG PER AIRBUS REPAIR R533 70508 ISSUE B, AREA REQ RE-INSPECTION WITH A THRESHOLD OF 8500FC AND INTERVALS OF 8500FC PER RDAS REF 80700416/006/2019

Part: FITTING — CRACKED (FRAME 16) · airframe 46,323 hrs · 22,213 cycles

DISCREPANCY: REFERENCE PEMCO N/R: 2650N341 RH FR16 UPPER DOUBLE JOGGLE AREA AFT LOWER HOLE (BL SHOWS CRACK INDICATION IN THE INBD LAYER AT 9 OCLOCK POS. VIEWED FROM THE EXTERIOR CORRECTIVE ACTION: REPAIRED R/H FR16 DOUBLE JOGGLE UPPER CORNER HOLE "B" IAW AIRBUS REPAIR DRAWING R531-13041 AND EA: A9-53R-35035

Part: STRUCTURE — CRACKED (EMERGENCY EXIT) · airframe 46,323 hrs · 22,213 cycles

DISCREPANCY: REFERENCE PEMCO N/R# 2650N261 R/H EMERG EXIT DOOR, FWD, INNER SEGMENT (SEGMENT #1 FWD) HAS CRACK INDICATIONS. CORRECTIVE ACTION: FAVRICATED & INSTALLED CRACK REPAIR ANGLE ON R/H EMERG. EXIT DOOR, FWD, INNER SEGMENT I.A.W. A319 FRONTIER EA# A9-52R-35025

Part: STRUCTURE — CRACKED (EMERGENCY EXIT) · airframe 46,323 hrs · 22,213 cycles

DISCREPANCY: REFERENCE PEMCO N/R# 2650N260 L/H EMERG EXIT DOOR, FWD, INNER SEGMENT (SEGMENT #1 FWD) HAS CRACK INDICATIONS. CORRECTIVE ACTION: FAVRICATED & INSTALLED CRACK REPAIR ANGLE ON L/H EM ERG. EXIT DOOR, FWD, INNER SEGMENT I.A.W. A319 FRONTIER EA# A9-52R-35025

Part: UNKNOWN — ODOR (CABIN) · airframe 42,186 hrs · 20,187 cycles

NOTICED A FOUL ODOR COMING FROM AFT GALLEY AND LAST ROWS.THE ODOR WENT AWAY AND CAME BACK. PERFORMED TROUBLESHOOTING IAW TSM 05-50-00-810-831-A. RAN PACKS NR 1 AND 2 COULD NOT DUPLICATE THE ODOR ON THE GROUND. PERFORMED BORESCOPE ON THE NR 1 ENGINE HPC STAGE 1 AND 2 AND BOOSTER. NO OIL WETTING PRESENT. PERFORMED MINIMUM IDLE LEAK CHECK WITH PACKS ON, NO LEAKS NOTED. TSM 71-00-00-810-802A THRU STEP 4A(4).

Part: DOOR — MISALIGNED (RT MLG) · airframe 41,993 hrs · 20,095 cycles

MOVED LANDING GEAR LEVER TO UP POSITION AFTER TAKEOFF. GEAR DID NOT RETRACT. LANDING GEAR NOT UPLOCKED FAULT. PERFORMED QRH PROCEDURE. FAULT CLEARED. BOTH LGCIUS AGREE LANDING GEAR IS UP AND LOCKED. LG SYSTEM DISAGREE ECAM ON TAXI IN AT DEN. PERFORMED EXTENSION AND RETRACTION OF GEAR DOORS IAW AMM 32-31-00-720-002-A. OPS CHECK GOOD. REMOVED AND REINSTALLED ORIGINAL RT MLG DOOR, SEE NR. PERFORMED EXTENSION RETRACTION TEST. OPS CHECK GOOD. IAW AMM 32-31-00-720-002-A AND AMM 32-12-11 PB401.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,950 hrs · 19,109 cycles

CABIN FLOORBEAM Y+1292 HAS CORROSION AT FR16-20. FLOORBEAM REMOVED AT FR16-20 FOUND TO BE OUT OF LIMITS IAW SRM 53-11-14-283-004 AND LOCATE AND DRILL IT IAW SRM 51-72-11 AND INSTALLED IAW SRM 51-72-11-911-00.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,950 hrs · 19,109 cycles

CABIN FLOORBEAM Y-1292 HAS CORROSION AT FR 20. REMOVED AND REPLACED FLOORBEAM Y-1292 AT FR 20 IAW SRM 51-42-11, 51-72-11-911-001 AND 53-11-14-283-004.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,950 hrs · 19,109 cycles

CABIN FLOOR BEAM Y+254 HAS CORROSION AT FR20. REMOVED AND REPLACED FLOOR BEAM Y+254 FR12 TO FR23 P/N D5311281820401 IAW SRM 51-42-11, 51-72-11-911-001 AND 53-11-14-283-004.

Part: DOOR SILL — CORRODED (FRAME 66) · corrosion level 2 · airframe 39,950 hrs · 19,109 cycles

DISCREPANCY: L2 DOOR SILL CORRODED AT FR66. CORRECTIVE ACTION: REFERENCE PEMCO NR 177N259. REMOVED AND REPLACED L2 DOOR SILL IAW A319 SRM 51-72-11, 51-42-11 AND 51-44-11./END/

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,950 hrs · 19,109 cycles

FLOORBEAM +512 CORRODED AT FR66-67. REMOVED AND REPLACED FLOORBEAM +512 LT SIDE IAW SRM 51-44-11, 51-72-11-911-001 AND 53-00-14-283-002.

Part: DOOR SILL — CORRODED (FRAME 68) · corrosion level 2 · airframe 39,950 hrs · 19,109 cycles

DISCREPANCY: R2 DOOR SILL CORRODED AT FR68. CORRECTIVE ACTION: REFERENCE PEMCO NR 1777N258. REMOVED AND REPLACED R2 DOOR SILL IAW A319 SRM 51-72-11, 53-41-14, 51-42-11, 51-44-11 AND 20-21-11-911-001-A./END/

Part: THRESHOLD — CORRODED · corrosion level 2 · airframe 39,950 hrs · 19,109 cycles

FORWARD CARGO BAY DOOR CUT OUT LOWER SILL UPPER SIDE HAS CORROSION AROUND FASTENERS AND FASTENER HOLES, SEVERAL AREAS. REMOVED AND INSTALLED A NEW WEB IAW SRM 51-72-11-911-001, 51-74-00, 51-73-11, 51-42-11, AND 51-44-11.

Part: BATTERY — DISCHARGED (CABIN) · airframe 38,189 hrs · 18,207 cycles

EPSU BATTERY 12WL RIGHT FAULT. FAILS TEST. REMOVED AND REPLACED BATTERY ASSEMBLY 12WL RIGHT. REFERENCE AMM 33-51-38-000-002A AND AMM 22-51-38-400-002A. EPSU UNIT P/N 3214-62-10 S/N 007451. OPERATIONAL CHECK GOOD.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 38,189 hrs · 18,207 cycles

DURING EMERGENCY LIGHT TEST L1 EPSU INOPERATIVE. REMOVED AND REPLACED EPSU 10WL FWD. OPERATIONAL CHECK OK. REFERENCE AMM 33-51-38 PAGE BLOCK 401.

Part: FITTING — OUT OF ADJUST (R2 DOOR) · airframe 33,991 hrs · 16,276 cycles

DEFECT 1047578, DURING CRUISE THE R2 DOOR PRESS LIGHT WARNING INDICATION CAME ON & SLIDE INDICATION WENT OUT ON ECAM DOOR PAGE. ADJUSTED THE R2 DOOR GIRT BAR FITTINGS & PERFORMED LOAD ADJUSTMENT OF THE CONTROL HANDLE & OPERATIONAL CHECKED GOOD IAW AMM 52-13-00-820-001-A & 52-13-00-820-002-A01.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,982 hrs · 16,271 cycles

DURING C6 C CHECK NON ROUTINE INSPECTION NOTED THE R2 DOOR SILL HAS AREAS OF CORROSION BETWEEN FRAME 67 & 68. REPAIRED R2 DOOR SILL PLATE BETWEEN FRAME 67 & 68 IAW SRM 53-41-14.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,982 hrs · 16,271 cycles

DURING C6 C CHECK NON ROUTINE INSPECTION NOTED CORROSION ON FLOORBEAM Y512 ON FRAME 66 ON HARD POINT. R & R FLOORBEAM Y512 ON FRAME 66 IAW SRM AT FRAME 64 & 67 IAW 51-21-11.

Part: SHEAR PLATE — CRACKED (FUSELAGE) · airframe 33,982 hrs · 16,271 cycles

DURING C6 C CHECK NON ROUTINE INSPECTION NOTED LT LATERAL SHEAR PLATE, BETWEEN FRAME 69 & 70 CRACKED. R & R NEW SHEAR PLATE & SHEAR PLATE SUPPORT ON LT SIDE IAW SRM 51-42-11.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,982 hrs · 16,271 cycles

DURING C6 C CHECK NON ROUTINE INSPECTION NOTED RT LATERAL SHEAR PLATE BETWEEN FRAME 69 & 70 CORRODED. R & R RT LATERAL SHEAR PLATE IAW SRM 51-42-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,982 hrs · 16,271 cycles

DURING C6 C CHECK NON ROUTINE INSPECTION NOTED AREAS OF CORROSION FOUND ON Y1292, BETWEEN FRAME 66 & 68. R & R NEW Y1292 IAW SRM 52-42-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,982 hrs · 16,271 cycles

DURING C6 C CHECK NON ROUTINE INSPECTION, NOTED CORROSION AT FLOORBEAM Y765M, AT FRAME 66 & 68. R & R FLOORBEAM BETWEEN FRAME 66 & 77 IAW SRM 51-42-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,982 hrs · 16,271 cycles

DURING C6 CHECK NON ROUTINE NR 779N175 INSPECTION NOTED SEVERAL AREAS OF CORROSION FOUND ON Y765 FLOORBEAM, BETWEEN FRAME 66 & 68. R & R FLOORBEAM IAW SRM 51-42-11.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,960 hrs · 12,208 cycles

SEAT 4C EMERGENCY PATH LIGHT INOPERATIVE. R & R SEAT 4C EMERGENCY PATH LIGHT IAW AMM 33-51-19 PB401, OPERATIONS CHECKED GOOD.

Part: SILL — CORRODED (ZONE 100) · corrosion level 2 · airframe 21,583 hrs · 9,886 cycles

C-CHECK: R2 DOOR SILL BEAM CORRODED AROUND FASTENER HOLE AT FRAME 66. REPAIRED DOOR SILL BEAM WITH CUTOUT, FILLER AND SPLICE IAW SRM 53-41-14 PB201, PARA 5.A, FIG 201.

Part: LIGHT — BURNED OUT (R2 DOOR SLIDE) · airframe 21,583 hrs · 9,886 cycles

C-CHECK: R2 DOOR "SLIDE ARMED" LIGHT DOES NOT ILLUMINATED DURING TEST. REMOVED SLIDE ARMED INDICATOR LIGHT ASSY IAW AMM 52-76-000-002-A. INSTALLED SERVICEABLE SLIDE ARMED LIGHT ASSY IAW AMM 52-73-21-400-002A. OPS CHECK GOOD IAW AMM 52-73-00-710-001-A.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 21,583 hrs · 9,886 cycles

C-CHECK: MAIN CABIN LT SEATS, ROW 13 HAS BURNED OUT LAMP FOR EMERGENCY EXIT LIGHT. R & R LAMP IAW AMM 33-51-19-420-052D. OPS CHECKED GOOD LAW AMM 33-51-00-71 0-00L-A.

Part: FRAME — CORRODED (ZONE 200) · corrosion level 2 · airframe 21,583 hrs · 9,886 cycles

C-CHECK: FRAME 68-1292, RM 51-42-11, PARA 5 AND SRN 53-00-14 PB 101B.

Part: SILL — CORRODED (ZONE 200) · corrosion level 2 · airframe 21,583 hrs · 9,886 cycles

C-CHECK: LT SIDE DOOR SILL BEAM CORROSION AROUND FASTENER HOLE. REPAIRED IAW REF SRM 53-41-14 PB 201, NOTE 1.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 21,583 hrs · 9,886 cycles

C-CHECK: BS 1292 FLOORBEAM CORROSION. R & R FLOORBEAM IAW SRM 51-42-11 PAR 5 AND SRM 53-00-14, PB 101, B. (2), FIGURE 102.

Part: SHEAR PLATE — CORRODED (ZONE 200) · corrosion level 2 · airframe 21,583 hrs · 9,886 cycles

C-CHECK; FRAME 69 RT SIDE SHEAR PLATE CORROSION. R & R SHEAR PLATE IAW EO A0-53EO-31434.

Part: SHEAR PLATE — CORRODED (ZONE 200) · corrosion level 2 · airframe 21,583 hrs · 9,886 cycles

C-CHECK: FRAME 69 LT SIDE SHEAR PLATE CORROSION. R & R SHEAR PLATE EO A0-53EO-31434.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 21,583 hrs · 9,886 cycles

C-CHECK: FLOORBEAM CORRODED IN TWO AREAS. R & R FLOORBEAM IAW SRM 51-42-11, PARA 5 AND SRM 53-00-14, PB 101 B.

Part: FLOORBOARD — DAMAGED (ZONE 200) · airframe 21,384 hrs · 10,746 cycles

C-CHECK: COCKPIT FLOORBOARD, 211GF SURFACE IS DAMAGED. FOUND DAMAGE TO FLOORBOARD, 211GF BEYOND REPAIRABLE LIMITS. REPLACED FLOORBOARD IAW SRM 53-12-00 IAW DIAGRAM 101.

Part: SPAR — DENTED (RT WING) · airframe 16,978 hrs · 7,638 cycles

C-CHECK: NON ROUTINE NR30121; RT WING L/E STA 7792/RIB 14 IS DENTED WITH INTERNAL DAMAGE AT CLOSEOUT WEB. REPAIRED RIGHT WING L/E DAMANGE STATION 7792/RIB 14 REPAIRED IAW EA A9-57R-32036 INSTRUTIONS 1-4 AS WRITTEN. HFEC INSPECTED, NO CRACKS WERE FOUND.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 16,978 hrs · 7,639 cycles

C-CHECK: NON ROUTINE 30064; FLOORBEAM ON FRAMES 66-68 HAS CORROSION AT FASTENER HOLES, BLENDED CORROSION, MEASURED OUT OF LIMITS. ORIGINAL THICKNESS .100", REMAINING .078". SRM 53-41-14 4A(1)AND 53-00-14 4B, FIG 102. LOCATED AND DRILLED NEW BEAM. IAW SRM 51-42-11 PARA 5A, B. APPLIED CORROSION PREVENTIVE COMPOUND. IAW SRM 51-23-13 PARA 2, 1-2.

Part: FLOORBEAM — CORRODED (CABIN) · corrosion level 2 · airframe 16,978 hrs · 7,638 cycles

C-CHECK: NON ROUTINE NR 30063; FLOORBEAM ON FRAMES 66- 68 HAS CORROSION AT FASTENER HOLES, BLENDED CORROSION, MEASURED OUT OF LIMITS. ORIGINAL THICKNESS .100", REMAINING .080". SRM 53-41-14 4A(1)AND 53-00-14 4B, FIG 102. LOCATED AND DRILLED NEW BEAM. IAW SRM 51-42-11 PARA 5A, B. APPLIED CORROSION PREVENTIVE COMPOUND. IAW SRM 51-23-13 PARA 2, 1-2.

Part: OIL SYSTEM — LEAKING (APU) · airframe 14,074 hrs · 6,312 cycles

REF LOG PAGE 522934. ITEM 1. FOUL ODOR EMITS FROM PACKS WITH BOTH APU AND ENGINE BLEEDS. FOUND APU OIL LEAKING INTO BLEED AIR. APU RENDERED INOPERATIVE. APU PLACED ON MEL.

Part: CONTROL PANEL — DEACTIVATED (EMERGENCY LIGHTS) · airframe 12,364 hrs · 5,550 cycles

REFERENCE LOG PAGE 489469. DURING FLIGHT THE CREW NOTED THE AFT F/A PANEL HAD NO POWER AND COULD NOT MANUALLY TURN ON EMERGENCY LIGHTING FROM AFT PANEL. MX RESET THE CIDS SYS IAW AMM 23-73-00-740-005.

Part: GROMMET — UNSECURE (GUSTLOCK) · airframe 11,044 hrs · 4,928 cycles

DURING C2 C-CHECK, INSP NOTED THE GUSTLOCK ON THE R1 DOOR DOES NOT ENGAGE WITH THE DOOR IN THE FULL OPEN POSITION. MX FOUND THE NYLON GROMMET ON GUSTLOCK RELEASE ROD TO BE UNSEATED CAUSING GUSTLOCK TO STICK IN THE UNLOCKED POSITION. MX RESEATED THE GROMMET AND PERFORMED OPS CHECK IAW AMM 52-11-12-820-051 AND 52-10-00-220-055.

Part: EPSU — INOPERATIVE (EMERGENCY LIGHTS) · airframe 5,553 hrs · 2,440 cycles

DURING C1 C CHECK, INSPECTION REPORTED THE OPERATIONAL TEST OF THE EMERGENCY LIGHTS FAILED WITH A FAULT MESSAGE OF "EPSU (13WL) AFT L/DEU B." MAINTENANCE REMOVED AND REPLACED THE EPSU IN ACCORDANCE WITH THE REQUIREMENTS OF AMM 33-51-38-000-001 AND AMM 33-51-38-400-001. UPON COMPLETION OF THE INSTALLATION, THE EPSU OPERATIONALLY CHECKED GOOD.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 5,553 hrs · 2,440 cycles

DURING C1 C CHECK, INSPECTION REPORTED AFT CARGO PIT FLOOR PANEL 151VG WAS DAMAGED BEYOND REPARABLE LIMITS. MAINTENANCE REMOVED THE FLOOR PANEL IN ACCORDANCE WITH THE REQUIREMENTS OF AMM 53-42-14-000-001 AND REPLACED IT WITH A NEW FLOOR PANEL IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 51-42-11, PARAGRAPH 5. FOLLOWING THE REPLACEMENT OF THE FLOOR PANEL IT WAS INSPECTED AND FOUND ACCEPTABLE.

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 5,553 hrs · 2,440 cycles

DURING C1 C CHECK, INSPECTION REPORTED AFT CARGO PIT FLOOR PANEL 151ZG WAS DAMAGED BEYOND REPAIRABLE LIMITS. MAINTENANCE REMOVED AND REPLACED THE FLOOR PANEL IN ACCORDANCE WITH THE REQUIREMENTS OF AMM 53-42-14-400-001. FOLLOWING THE REPLACEMENT OF THE FLOOR PANEL, IT WAS INSPECTED AND FOUND ACCEPTABLE. CORRECTED C CHECK FROM C5 TO C1 ON 02/27/08/END/.