N847VA
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
59 reports on file, 2016-02-21 – 2024-04-30.
Part: SKIN — CHAFED (RT WING LE) · airframe 35,266 hrs · 11,749 cycles
CUSTOMER REQUEST:DB #28, RH WING LEADING EDGE SLAT #3 CHAFFING MARKS- REINSPECT TO VALIDATE DAMAGE RECORDED ON NRC 39664 FROM W/O 375225 AND NRC:27505 SO:536489 GROUNDED - YES. CUT OUT DAMAGED AREA, FABRICATED EXTERNAL PLATE AND INSERT IAW A320 SRM 57-44-21-300-001 FIG.2. ALODINED AND PRIMED REPAIR PARTS IAW A320 SRM 51-21-11/001. INSTALLED REPAIR PARTS IAW A320 SRM 57-44-21-300-001 FIG.2. APPLIED TOP COAT IAW A320 SRM 51-23-11. LENGTH OF REPAIR IS 14.5ÿ½L X 2.7ÿ½H LOCATED 15ÿ½ AFT OF LEADING EDGE. THIS IS A CATEGORY A REPAIR. SLAT PN#D5746093000500 SN#5961P
Part: SKIN — DENTED (RT WING TE FLAP) · airframe 35,266 hrs · 11,749 cycles
LESSOR ITEM 767 RH WING TRAILING EDGE IB FLAP LOWER SURFACE I/B CLUSTER OF DENTS REQUIRES REPAIR. GROUNDED - YES. REPAIRED RH WING TRAILING EDGE IB FLAP LOWER SURFACE I/B CLUSTER. FINAL DIMENSIONS OF REPAIR ARE 12.5"W X 11.8"L LOCATED 47.5" FROM INBRD AND STOPS 60" TO OUTBOARD. PREFORMED PERMANENT REPAIR LOCATED IN ZONE 2. LAW A320-200 SRM 57-52-00-300-093 AND SRM 57-52-00-283-105. A/C INFO: S/N: 04948 FH: 35266:10 FC:11748 WV:015 P/N:057570650005300 SERIAL NO: TB14948.
Part: FITTING — CORRODED (FRMS 24A-28) · corrosion level 2 · airframe 35,266 hrs · 11,749 cycles
DURING MX, FOUND LIGHT CORROSION SPOTS ON FWD CARGO THRESHOLD, DOOR SILL PLATE, FROM FR24A TO FR28 GROUNDED - YES. EVALUATED FWD CARGO THRESHOLD DOOR SILL PLATE FROM FR24A-FR28, FOUND TO HAVE 2EA FITTINGS, 1EA PLATE, AND 3EA SEAL PLATES OUT OF LIMITS IAW A320 SRM 53-21-28-283 REMOVED AND REPLACED 2EA FITTING P/N D5323133520215 PO:1081434.1, P/N E5323126820000 PO:1083278 IAW A320 SRM 51-42-11 AND AIRBUS DWG E53231272 ISSUE A. REMOVED AND REPLACED 1EA PLATE AND 3EA SEAL PLATES P/N D5323100320000 PO:1081427.1, P/N D5323079520002 PO:1081432.1 IAW A320 SRM 51-42-11 AND AIRBUS DWG E53231589 ISSUE B RESTORED SURFACE PROTECTION IAW A320 SRM 51-21-11 AND A320 SRM 51-75-12.
Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 35,266 hrs · 11,749 cycles
LH WING TRAILING EDGE, FLAP TRACK #3 AREA, BROKEN FILLER COMPOUND AND EVIDENCE OF WATER INGRESS, ABRASION RESISTANT PAINT BROKEN AND MISSING GROUNDED - YES. EVALUATED LESSOR ITEM 800. LH WING TRAILING EDGE, FLAP TRACK #3 AREA, P/N D5757420200600, NSN(SN) DAMAGE IS 88.4" FROM I/B END ON UPPER SURFACE AND 1" FROM T/E IN ZONE 2. LENGTH OF DAMAGE IS 1.6", WIDTH IS 1" AND .500" DEEP. WITHIN REPAIRABLE LIMITS IAW A320 IPC 57-53-21-014 REV DATE 01NOV23, SRM 57-53-00-283-074 FIG 1 SH. 1 REV DATE 16JAN2023 AND SRM ADL AND REPAIR MOD LIST REV DATE NOV 01/23. REPAIRED IAW ASA A320 SRM 57-53-00-300-120, A320 NTM 51-10-03, A320 NTM PART 6 51-10-08, A320 SRM 51-77-11-911-023, EA CMPT-57EA-02086, A320 SRM 51-21-11, A320 SRM 51-24-00. RESTORED FINISH IAW ASA A320 SRM 51-21-10 AND A320 AMM 51-75-12. PART MARKED PER EA CMPT 57EA 02086 & PMS 01-06-12 A320-214, S/N:04948, FH 35266:10, FC:11749, WV=015 FINAL DOUBLER SIZE 5.8"X3"
Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 35,266 hrs · 11,749 cycles
LESSOR ITEM 799: (77751) RH WING TRAILING EDGE, FLAP TRACK #3 AREA, BROKEN FILLER COMPOUND AND EVIDENCE OF WATER INGRESS, ABRASION RESISTANT PAINT BROKEN AND MISSING GROUNDED - YES. REPAIRED R/H WING TRAILING EDGE FLAP TRACK #3 AREA WITH CAT. A PERMANENT REPAIR IAW A320 SRM 57-53-00-283-013 REV. 147 01NOV2023, 57-53-00-300-121 REV 147 01 NOV 2023, EA# CMPT-57EA-02098. FH:35266:10, FC:11749, WV:015. #1 69"-72" FROM I/B, #2 88.5"-91.5" FROM I/B, DEPTH .004 WIDTH .5 LOCATED IN ZONE 2 FINAL DOUBLER SIZES FOR BOTH DOUBLER 6.3"X3.2"
Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 35,266 hrs · 11,749 cycles
GENERATED FROM CUSTOMER CARD # G1871683 LESSOR 731, DB#10 ; LEFT WING INBOARD FLAP LOWER SKIN, OB CLUSTER OF DENTS REQUIRES REPAIR GROUNDED - YES. REPAIRED LEFT WING INBOARD FLAP LOWER SKIN OUTBOARD CLUSTER OF DENTS LOCATED 84" FROM INBOARD TO OUTBOARD AND STOPS AT 99". SIZE OF REPAIR IS 15" X 12.7 LOCATED IN ZONE 2. S/N TB14948 PART NUMBER D5757065005200 IAW A320 SRM 57-52-001/201 SRM 57-52-00-300-095, ASA EA NUMBER CMPT-57EA-02078-PRELIMINARY. A/C INFO: N847VA S/N:04948 FH:35266:10 FC:11749 WV:015. PERFORMED PERMANENT REPAIR
Part: FRAME ANGLE — CORRODED (FRM 71) · corrosion level 2 · airframe 35,266 hrs · 11,749 cycles
LESSOR ITEM 631: CORROSION ON FUSELAGE FRAME ANGLE AT FR 71 AND ACCESS 312AR GROUNDED - YES. REMOVED AND REPLACED AT FR71 AND ACCESS 312AR ANGLE P/N D53571550-22600, PO# 1080995.3 IAW A320SRM 51-42-11/001 AND AIRBUS DWG # D53571510 ISSUE:K REMOVED CORROSION ORIG .047, MATERIAL LOSS .020 REMAINING .027 FOUND TO BE OUT OF LIMITS REF A320 SRM 53-51-12-01-A
Part: SKIN — DENTED (FRM 9 S36L) · airframe 35,266 hrs · 11,749 cycles
LESSOR ITEM 603; (74480) DENT/NICK ON FUSELAGE SKIN FR 9 AND STRG 36 LH APPROX GROUNDED - YES. STRIPPED AREA TO EVALUATE AS PER A320 SRM 51-75-11/001. DENT LOCATION IS 4.3 INCHES ABOVE STR 36 AND 3.5 INCHES FORWARD OF FRAME 8. DENT MEASURES 1.5 INCHES IN LENGTH AND .0375 IN WIDTH. DENT MEASURES .001 AND FOUND TO BE WITHIN ALLOWABLE NEGLIGABLE DAMAGE AS PER A320 SRM 51-73-11/001. APPLIED PROTECTIVE TREATMENTS AS PER A320 SRM 51-21-11/001, TOPCOATED AS PER A320 SRM 51-75-12-911-001 THIS IS A CAT A REPAIR NO FURTHER ACTION REQUIREDON DEFERRAL.
Part: FLOORBEAM — CORRODED (FRM 34) · corrosion level 2 · airframe 35,266 hrs · 11,749 cycles
FOUND FLOOR SUPPORT CORRODED AT FR34 IN FWD CARGO COMPARTMENT GROUNDED - YES. REMOVED CORROSION ORIG .039 MATERIAL LOSS .039 FOUND TO BE OUT OF LIMITS REF A320 SRM 51-73-00/001 AND 53-21-14-03-11 REMOVED AND REPLACED FLOOR SUPPORT REF AIRBUS DWG D53915503 ISSUE K
Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 35,266 hrs · 11,749 cycles
CABIN FLOOR PANEL 251FF DELAMINATED GROUNDED - YES. REMOVED AND REPLACED NEW FLOOR BOARD PANEL 251FF, P/N: E5367191000000 TO BE INSTALLED ON NON ROUTINE 32103 (HAECO) CUST. CARD NO: G1871103
Part: SKIN — DENTED (RT WING TE FLAP) · airframe 35,266 hrs · 11,749 cycles
DENT/NICK ON RH OUTBOARD FLAP LOWER SKIN TRAILING EDGE OVER INBOARD FLAP TRACK FAIRING GROUNDED - YES. CLEANED AREA AND EVALUATED DENT IAW-A320-SRM-57-53-00-283-092 FIG 1 AND FOUND TO BE WITHIN LIMITS PER L= .375" D= .0025 PERFORMED HFEC IAW-A320-NTM-51-10-08, AND RESTORED EXTERIOR PROTECTIVE TREATMENTS AND EXT FINISHES IAW-A320-SRM-51-21-11/001 BETWEEN FLAP RIB 5A TO 5B 2.0 FWD OF AFT SPAR THIS IS A CAT A REPAIR NO FURTHER ACTION REQUIRED TOOL DATA=T8492H CAL - 26/OCT/24
Part: SKIN — CORRODED (RT WING TE FLAP) · airframe 35,266 hrs · 11,749 cycles
LESSOR ITEM 38; (74009) R/H INNER FLAP UPPER SURFACE I/B SURFACE CORROSION GROUNDED - YES. REMOVED CORROSION ORIG .023 MATERIAL LOSS .004 REMAINING .019 HFEC AND DVI NO DEFECTS NOTED, REMOVED AND REINSTALLED FASTENERS FOUND TO BE WITHIN LIMITS, RESTORED COATINGS REF ASA EA CMPT-57EA-02054 REV 00 THIS IS CAT A REPAIR NO FURTHER ACTION REQUIRED
Part: SKIN — CORRODED (LT WING) · airframe 35,266 hrs · 11,749 cycles
LEFT WING TOP SKIN, EVIDENCE OF CORROSION AROUND THE BONDING POINT GROUNDED - YES. REMOVED CORROSION ORIG .150, MATERIAL LOSS .004, REMAINING .146 FOUND TO BE WITHIN LIMITS, HFEC, BHEC, DVI NO DEFECTS NOTED REMOVAL AND REINSTALL BONDING SPIGOT MEASUREMENTS 1.80L X 1.70W BETWEEN RIB 19 AND 20 5 INCHES AFT OF FWD SPAR REF A320 SRM 57-21-11-300-026 AND SRM 57-21-11-203-014. THIS IS A CAT A REPAIR NO FURTHER ACTION REQUIRED.
Earlier reports · 2016–2023 · 46 reports
2023
Part: SKIN — DENTED (FRM 79) · airframe 35,266 hrs · 11,749 cycles
LESSOR ITEM 100; (73875) 1 OFF DENT L/H REAR FUSELAGE LOWER APPROX FR 79. GROUNDED - YES. EVALUATED DENT 7.2" AFT OF FR 76, 1.8" DOWN OF STGR 26LH. D/A LESS THAN OR EQUAL TO 0.1 DENT IS .018/1 LESS THAN OR EQUAL TO 0.1 FOUND TO BE WITHIN LIMITS IAW ASA A320 SRM 53-51-11-283-004 FIG 3 SHEET 1 DENT IS A CATEGORY B TOOL USED T8492H CAL DUE 26/DEC/24. INSPECTION THRESHOLD FROM TIME OF ADL EMBODIMENT 60,000 FC 120,000 INSPECTION AT INTERVALS AND METHOD TBD REF A320 SRI 53-51-11-205-003
Part: SKIN — DENTED (FRM 74) · airframe 35,266 hrs · 11,749 cycles
R/H REAR FUSELAGE FR 74 2 OFF DENTS REAR OF PANEL 313AR DENTED FROM INSIDE. GROUNDED - YES. EVALUATED DENT 1 5.8" AFT OF FR 73, 2.1" DOWN OF STGR 27 RH. DIA<0.1 DENT IS .033/1.5<0.1 FOUND TO BE WITHIN LIMITS IAW A320 SRM 53-51-11-283-004 AND 53-00-11-283-005. TOOL USED T8492H CAL DUE 26/DEC/24. EVALUATED DENT 2 5.3" FWD OF FR 74, 1.6" DOWN OF STGR 31 RH. DIA<0.1 DENT IS .015/1.1 <0.1 FOUND TO BE WITHIN LIMITS IAW A320SRM 53-51-11-283-004 AND 53-00-11-283-005. TOOL USED T8492H CAL DUE 26/DEC/24 THIS IS A CAT B REPAIR INSPECTION THESHOLD FROM TIME OF ADL 60,000 FC 120,000 FH INSPECTION INTERVAL AND METHOD TBD.
Part: SKIN — GOUGED (FRM 67) · airframe 35,266 hrs · 11,749 cycles
GOUGE ON L-2 DOOR LOWER EDGE FR67 GROUNDED - YES. CLEANED AREA AND REMOVED EDGE DAMAGE L= .075 D=ORG=.098. AFTER DAMAGE REMOVAL D= .090 TOTAL MAT LOSS= .008 MAX ALLABLE LOSS = .031, MAX ALLOWABLE LENGTH= 1.18 AND FOUND TO BE WITHIN LIMITS IAW-A320-SRM-52-10-00-283-001 FIG 2 AND 7. RESTORED PROTECTIVE FINISHES IAW-A320-SRM-51-21-11 AND A320-SRM 51-75-12 TOOL DATE= # 8928U CAL DUE= 27/OCT/24 THIS IS A CAT.B REPAIR, INSPECTION THRESHOLD FROM TIME OF ADL/ REWORK EMBODIMENT FOR THE UNRIVETED AREA 60,000 FC, F/H NOT RELEVANT, INSPECTION INTERVALS AND METHOD TBD.
Part: FLOOR SUPPORT — CORRODED (FRM 30-34) · corrosion level 2 · airframe 35,266 hrs · 11,749 cycles
LESSOR ITEM 407; (75078) CORROSION ON FWD CARGO FR 31 LH AND RH LATERAL FLOOR SUPPORTS GROUNDED - YES. REMOVED CORROSION RH FLOOR SUPPORT ORIG .0394 MATERIAL LOSS .0197 REMAINING .0197 REMOVED CORROSION ON LH FLOOR SUPPORT ORIG .0394 MATERIAL LOSS .0195 REMAINING .0199 BOTH FOUND TO BE OUT OF LIMITS NET A320 SRM 51-73-00/001 REMOVED AND REPLACED BOTH FLOOR SUPPORTS REF AIRBUS DWG D53915500 ISSUE K.
Part: FLOOR SUPPORT — CORRODED (FRM 58) · corrosion level 2 · airframe 35,266 hrs · 11,749 cycles
CORROSION ON AFT CARGO FR 58 AND RH LATERAL FLOOR SUPPORT GROUNDED - YES. REMOVED CORROSION ORIG .0394 MATERIAL LOSS .0394 REMAINING 0.0 FOUND TO BE OUT OF LIMITS REF A320 SRM 53-41-14-08-A REMOVED AND REPLACED CORNER SECTION REF AIRBUS DWG D53470478 AND A320 SRM 51-42-11/001
Part: FLOOR SUPPORT — CORRODED (FRMS 32-33) · corrosion level 2 · airframe 35,266 hrs · 11,749 cycles
LESSOR ITEM 406; (75080) CORROSION ON FWD CARGO LH AND RH LATERAL FLOOR SUPPORT AND FR 32/33 GROUNDED - YES. REMOVED CORROSION RH FLOOR SUPPORT ORIG 0394 MATERIAL LOSS .0145 REMAINING .0249 REMOVED CORROSION ON LH FLOOR SUPPORT ORIG .0394 MATERIAL LOSS .0175 REMAINING .0219 BOTH FOUND TO BE OUT OF LIMITS REF A320 SRM 51-73-00/001 REMOVED AND REPLACED BOTH FLOOR SUPPORTS ON CUSTOMER CARD G1871619.
Part: SKIN — GOUGED (FRMS 52-56) · airframe 35,266 hrs · 11,749 cycles
LESSOR ITEM 613; (74470) SEVERAL DENT/GOUGES MARKS ON FUSELAGE SKIN FR 52/56 AND STRG 39/41 RH GROUNDED - YES. REMOVED DAMAGE ORIG .236 MATERIAL LOSS .008, REMAINING .228 ACCOMPLISHED HFEC AND DUI NO DEFECTS NOTED APPEARANCE OF DENT WAS MULTIPLE LAYERS OF PAINT FOUND TO BE WITHIN LIMITS NET A320 SRM 53-41-11-283-043 FIG 005 SH 003 THIS IS A CAT B REPAIR INSPECTION THRESHOLD FROM AIRCRAFT FIRST FLIGHT 1100 FC FH NOT RELEVANT SUBSEQUEBT INSPECTIONS INTERVAL 1100 FC FH NOT RELEVANT INSPECTION METHOD GVI REF A320 SRI 53-41-11-205-016 AND A320 SRI-INTRO PARA F(2)
Part: SHEAR PLATE — CORRODED (FRMS 69-70) · corrosion level 2 · airframe 35,266 hrs · 11,749 cycles
LESSOR ITEM S67: (74635) PAX CAB CORROSION ON SHEAR PLATES AND UNDER STRUCTURE FR69/70 AND-Y 1292 GROUNDED - YES. EVALUATED SHEAR PLATE AND PLATE SUPPORT AT FR69 TO FR70, -Y1292 TO -Y1732, STR 23, R/HSIDE, FOUND TO BE 100% CORRODED AND OUT OF ALLOWABLE LIMITS PER A320 SRM 51-74-00/001. REMOVED AND REPLACED SHEAR PLATE AND PLATE SUPPORT PER A320 SRM 51-42-11/001 AND AIRBUS DWG D53470100, SHT 6, REV R AND AIRBUS DWG D53471124, SHT 1, REV D. CAT A SHEAR PLATE P/N - D534711240300, PO# 1077688.1 PLATE SUPPORT P/N - D5347112420300, PO# 0
Part: DOOR SILL — CORRODED (CABIN) · corrosion level 2 · airframe 35,266 hrs · 11,749 cycles
LESSOR ITEM 563: (74639) R-2 DOOR CORROSION ON SILL PLATE 3 PLACES GROUNDED - YES. REMOVED CORROSION AT ALL 3 LOCATIONS ORIG .063, MATERIAL LOSS .040 REMAINING .0236 FOUND TO BE OUT OF LIMITS REF A320 SRM 53-41-14-283-002 TRIMMED OUT DAMAGE , FABRICATED, LOCATED, DRILLED, ALODINED, PRIMED, PAINTED, AND INSTALLED REPAIR AT FR68 STR23 RH REF A320 SRM 53-41-14-300-001 THIS IS A CAT A REPAIR NO FURTHER ACTION REQUIRED
Part: SHEAR PLATE — CORRODED (FRMS 69-71) · corrosion level 2 · airframe 35,266 hrs · 11,749 cycles
LESSOR ITEM 567: (74635) PAX CAB CORROSION ON SHEAR PLATES AND UNDER STRUCTURE BOTH SIDES FR 69/70 AND -Y 1292/1292 GROUNDED - YES. EVALUATED SHEAR PLATES AT FR69 TO FR70, -Y1292 AND Y1292, STR 23, L/HSIDE. FOUND TO BE 100% CORRODED AND OUT OF ALLOWABLE LIMITS PER A320 SRM 51-74-00/001. REMOVED AND REPLACED SHEAR PLATE PER A320 SRM 51-42-11/001 AND AIRBUS DWG D53470100,SHT6, REV R AND AIRBUS DWG D53471124,SHT 1, REV D. SHEAR PLATES ON R/HSIDE, WORK COMPLETED ONNR CARD #32570, SO# 536415, CUSTOMER CARD # G1871570. CAT A SHEAR PLATE P/N - D5347112420200, PO# 1077688.2
Part: DOOR SILL — CORRODED (R1) · airframe 35,266 hrs · 11,749 cycles
R/H FWD ENTRY DOOR R1 LOWER CUTOUT AT GIRT BAR PLATE ATTACHMENT EVEDENCE OF CORROSION FOUND. WL HTTPS:// GROUNDED - YES. REMOVED CORROSION. REMAINING MAT. THICKNESS .203 FOUND TO BE WITHIN LIMITS AS PER A320 SRM 53-11-14-283-005 HI FRQ AS PER NTM 51-10-08. APPLIED PROTECTIVE TREATMENTS AS PER A320 SRM 51-21-11. TOP COATED AS PER A320-SRM 51-75-12 MAX ALLOWED MUST BE GREATER THAN .177 REMAINIG FOUND TO BE WITHIN LIMITS REF A320 SRM 53-11-4-283-005 THIS IS A CAT B REPAIR INSPECTION THRESHOLD 60,000FC FH NOT RELEVANT INSPECTION INTERVALS AND METHOD TBD REF A320 SRI 53-11-14-205-001
Part: DOOR SILL — CORRODED (L1) · airframe 35,266 hrs · 11,749 cycles
FWD L/H ENTRY DOOR LOWER CUTOUT CORROSION FOUND ON GIRT BAR PLATE FITTING GROUNDED - YES. REMOVED CORROSION. 4EACH HOLES. REMAINING MAT THICKNESS .153 FOUND TO BE WITHIN LIMITS AS PER A320 SRM 53-11-14-283-005, HFEC PERFORMED AS PER NTM 51-10-08. APPLIED PROTECTIVE TREATMENTS AS PER A320 SRM 51-21-11. TOP COATED AS PER A320 SRM 51-75-12. HOLE 1 REMAINING .153 HOLE 2 REMAINING .192 HOLE REMAINING .153 HOLE #4 REMAINING .159 MAX ALLOWED MUST BE GREATER THAN .1476 FOUND TO BE WITHIN LIMITS REF A320 SRM 53-11-14-283-005 THIS IS A CAT B REPAIR INSPECTION THRESHOLD 60,000 FC FH NOT RELEVANT INSPECTION INTERVAL AND METHOD TBD REF A320 SRI 53-11-14-205-001
Part: SKIN — DENTED (FRMS 76-77) · airframe 35,266 hrs · 11,749 cycles
LESSOR ITEM 568:(74533) DENT ON FUSELAGE SKIN FR 76/77 STRG 21/21/LH GROUNDED - YES. EVALUATED DENT LENGTH=1.6" WIDTH=1.4" DEPTH=.021". 7.2"AFT OF FRAME 76 AND 1.6" BELOW STRINGER 28. D/A= .013125 FOUND TO BE WITHIN LIMITS IAW A320 SRM 53-51-11-283-004. PERFORMED DVI AND HFEC AND FOUND NO DEFECTS. CATEGORY "B" REPAIR. INSPECTION THRESHOLD FROM TIME OF ADL 60,000 FC 120,000 FH SUBSEQUENT INSPECTION AT INTERVALS AND METHOD TBD REF A320 SRI 53-51-11-205-003
Part: SKIN — DAMAGED (FRM 3) · airframe 35,266 hrs · 11,749 cycles
LESSOR ITEM 598: (74485) LIGHTNING STRIKE ON FUSELAGE SKIN AT FR 3 8 INCHES FROM CENTER LINE TO RH SIDE GROUNDED - YES. REMOVED AND REPLACED FASTENER WITH LIGHTNING STRIKE MARK. IAW A320 SRM 53-11-11-300-034. AND SRM 51-42-11 AND AIRBUS DWG D3D53M3540 ISSUE B. PRIMED INSTALLED FASTENER IAW A320 SRM 51-21-11, PAINTED FASTENER IAW A320 SRM 51-75-11. THIS IS A CAT A REPAIR NO FURTHER ACTION REQUIRED
Part: FLOOR PANEL — PUNCTURED (CABIN) · airframe 35,266 hrs · 11,749 cycles
LESSOR ITEM 535: CABIN FLOOR PANEL 251GF SMALL HOLE 1/3 FROM FRONT EDGE. GROUNDED - YES. EVALUATED PANEL 251GF CABIN FLOOR PANEL AS BEYOND REPAIRABLE LIMITS AND REQUIRES REPLACEMENT IAW A320-200 SRM 53-02-00-283-001 TABLE 2 REV.146-FH=35266:10 FC=11749 WV=015, RECEIVED NEW FLOOR BOARD PANEL P/N: E5367193900000 TO BE INSTALLED ON NON-ROUTINE: 32103(HAECO), CUST CARD NO: G1371103
Part: FLOOR PANEL — DENTED (CABIN) · airframe 35,266 hrs · 11,749 cycles
CABIN FLOOR PANEL 251LF 1 OFF DENT GROUNDED - YES. EVALUATED PANEL 251LF CABIN FLOOR PANEL AS BEYOND REPAIRABLE LIMITS AND REQUIRES REPLACEMENT IAW A320-200 SRM 53-02-00-283-001 FIGURE 2 SHEET A REV 146. FH:35266:10, FC 11749, WV 015. RECIEVED NEW FLOOR PANEL 251LF P/N E367190500000, TO BE INSTALLED ON NON-ROUTINE 32103 (HAECO) CUST. CONTROL# G18771103
Part: FLOOR PANEL — DENTED (UNKNOWN) · airframe 35,266 hrs · 11,749 cycles
LESSOR ITEM 541: CABIN FLOOR CENTER PANEL 251AF MANY DENTS. GROUNDED - YES. RECEIVED NEW FLOOR BOARD PANEL 251AF P/N:E5367190500000 TO BE INSTALLED ON NON-ROUTINE OPS 32103 (HAECO) CUST CARD: G1871103
Part: FLOORBOARD — DENTED (CABIN) · airframe 35,266 hrs · 11,749 cycles
LESSOR ITEM 543: CABIN FLOOR CENTER PANEL 241JF MANY DENTS GROUNDED - YES. EVALUATED 241JF CABIN CENTER FLOOR PANEL AS BEYOND REPAIRABLE LIMITS & REQ'S REPLACEMENT IAW A320-200. SRM 53-02-00-283-001 TABLE 2-REV.146. FH - 35266:10, FC-11749, WV-015. RECEIVED NEW FLOOR BOARD PANEL 241JF, P/N: E536719090000 TO BE INSTALLED ON NON ROUTINE 32101(HAECO), CUST. CARD NO., G1871101
Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 35,266 hrs · 11,749 cycles
LESSOR ITEM 553: CABIN FLOOR PANEL 252XF DAMAGED IN 2 OFF PLACES. GROUNDED - YES. EVALUATED PANEL 252XF CABIN FLOOR PANEL AS BEYOND REPAIRABLE LIMITS AND REQUIRES REPLACEMENT IAW A320-200 SRM 53-02-00-283-001 TABLE 2 REV. 146 FH=35266:10 FC=11749 WV=015, RECEIVED NEW FLOOR BOARD 252XF, P/N: E5367175100000, TO BE INSTALLED ON NON-ROUTINE 32103 (HAECO) CUST CARD NO G1871103
Part: FLOOR PANEL — DENTED (UNKNOWN) · airframe 35,266 hrs · 11,749 cycles
LESSOR ITEM 542: CABIN FLOOR PANEL 241KF DENT 1/3 FROM REAR. GROUNDED - YES. REPAIRED LESSOR ITEM 542 CABIN FLOOR PANEL 241KF P/N E5367161600000 AT 3EA DENTED AREAS OF UPPER SKIN IAW A320 SRM 53-02-00-283-001 AND 53-02-00-300-001, FINAL REPAIR SIZE AREA#1 20.5ÿ½ FROM AFT EDGE, 4ÿ½ FROM L/H EDGE .4ÿ½ DIA. AREA#2 37.6ÿ½ FROM AFT EDG 3.6ÿ½ FROM L/H EDGE .5ÿ½ WIDE/1.4ÿ½ LONG. AREA#3 29.25ÿ½ FROM FWD EDGE, 4.25ÿ½ FROM R/H EDGE, .5ÿ½ WIDE/3ÿ½ LONG. ALL REPAIRS ARE CATEGORY A PERMENANT REPAIRS. A/C N874VA, FLIGHT CYCLES 11749, FLIGHT HOURS 35266:10, WV015
Part: FLOOR PANEL — DENTED (UNKNOWN) · airframe 35,266 hrs · 11,749 cycles
LESSOR ITEM 544: CABIN FLOOR PANEL IN FORWARD VESTIBULE CENTER DENTED. GROUNDED - YES. REPAIRED LESSOR ITEM 544: CABIN FLOOR PANEL IN FORWARD VESTIBULE CENTER. PANEL 221DF DENT LOCATED 8.5" FROM AFT EDGE AND 3.5" FROM IWBD EDGE IAW A320-214. SRM 53-02-00-283-001 AND 53-02-00-300-001.P/N:E5367148200000, A/C: N847VA, S/N: 04948 F/H: 35266:10, F/C:11749, W/V: 015. PERMANT CAT A REPAIR
Part: FLOOR PANEL — DENTED (UNKNOWN) · airframe 35,266 hrs · 11,749 cycles
LESSOR ITEM 528: CABIN FLOOR PANEL 232LF 5 OFF DENTS. GROUNDED - YES. EVALUATED AND REPLACED NEW FLOOR BOARD P/N:E536192300000 TO BE INSTALLED ON NON-ROUTINE 32098(HAECO), CUST CARD NO. G1871098
Part: FLOOR PANEL — PUNCTURED (UNKNOWN) · airframe 35,266 hrs · 11,749 cycles
LESSOR ITEM 549: CABIN FLOOR PANEL 232SF SMALL HOLE AT REAR R/H EDGE AND HOLE 1/3 WAY FRONT GROUNDED - YES. EVALUATED 232SF CABIN FLOOR PANEL AS BEYOND REPAIRABLE LIMITS & REQÿ½S REPLACEMENT IAW A320-200-SRM 53-02-00-283-001 TABLE 2 REV.146. FH-35266:10, FC-11749, WV-015, RECEIVED NEW FLOOR BOARD PANEL 232SF INSTALLATION ON NON ROUTINE 32098. G1871098 P.O#1077076.4
Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 35,266 hrs · 11,749 cycles
LESSOR ITEM 537: CABIN FLOOR PANEL L3 DOOR 3 OFF DENTS. PANEL 261LG GROUNDED - YES. EVALUATED AND RECEIVED NEW FLOOR PANEL 261LG, P/N: E5367180500000 TO BE INSTALLED ON NON-ROUTINE 32105 (HAECO) CUST. CARD NO: G1871105
Part: FLOOR PANEL — DENTED (UNKNOWN) · airframe 35,266 hrs · 11,749 cycles
LESSOR ITEM 545: CABIN FLOOR PANEL IN FORWARD VESTIBULE R/H P/N E5367148100000 6+ DENTS. GROUNDED - YES. EVALUATED PANEL P/N E5367148100000 CABIN FLOOR PANEL AS BEYOND REPAIRABLE LIMITS AND REQUIRES REPLACEMENT IAW A320-200 SRM 53-02-00-283-001 TABLE 2 REV. 146. FH: 35266:10 FC: 11749 WV= 015, NEW FLOOR BOARD PANEL RECEIVED P/N: 5367190300000 TO BE INSTALLED ON NON ROUTINE 32096 (HAECO) CUST. CARD NO G1871096 PO:1077106.2
Part: FLOOR PANEL — PUNCTURED (UNKNOWN) · airframe 35,266 hrs · 11,749 cycles
LESSOR ITEM 552: CABIN FLOOR 252NF DAMAGED IN 1 PLACE GROUNDED - YES. REPAIRED PUNCTURE ON CABIN FLOOR PANEL 252NF IAW A320-200 SRM 53-02-00-300-001. THIS IS A CATEGORY A PERMENANT REPAIR. FH-35266:10 FC-11749 WV-015
Part: FLOOR PANEL — DENTED (UNKNOWN) · airframe 35,266 hrs · 11,749 cycles
LESSOR ITEM 504: CABIN FLOOR PANEL 251BF 2 OFF DENTS. GROUNDED - YES. REPAIRED 2EA DENTS ON CABIN FLOOR PANEL 251BFIAW A320-200 SRM 53-02-00-300-001 THIS IS A CATEGORY A PERMENANT REPAIR. FH-35266:10 FC-11749 WV-015
Part: FLOOR PANEL — DENTED (UNKNOWN) · airframe 35,266 hrs · 11,749 cycles
LESSOR ITEM 539: CABIN FLOOR PANEL 252BF 2OFF DENTS GROUNDED - YES. EVALUATED 252BF CABIN FLOOR PANEL AS BEYOND REPAIRABLE LIMITS & REQÿ½S REPLACEMENT IAW A320-200 SRM 53-02-00-283-001 TABLE 2 REV.146. FH-35266:10, FC-11749, WV-015. RECEIVED NEW FLOOR BOARD PANEL 252BF, P/N:E5367192300000 TO BE INSTALLED ON NON-ROUTINE OPS 32103 (HAECO) LOST CARD NO. #G1871103
Part: FLOOR PANEL — DELAMINATED (UNKNOWN) · airframe 35,266 hrs · 11,749 cycles
LESSOR ITEM 533: CABIN FLOOR PANEL 231VF 5 OFF DENTS. GROUNDED - YES. EVALUATED PANEL 231VF CABIN FLOOR PANEL AS BEYOND REPAIRABLE LIMITS AND REQUIRES REPLACEMENT IAW A320-200 SRM 53-02-00-283-001 TABLE 2 REV. 146. FH= 35266:10 FC= 11749 WV= 015, RECEIVED NEW PANEL P/N: E5367190600000, SEE NON-ROUTINE: 32098 FOR INSTALLATION CUSTOMER CARD# G1871098 P.O#1077106.1
Part: FLOOR PANEL — DELAMINATED (UNKNOWN) · airframe 35,266 hrs · 11,749 cycles
LESSOR ITEM 530: CABIN FLOOR PANEL 231 LF 1 OFF DENT GROUNDED - YES. EVALUATED 231 LF CABIN FLOOR PANEL AS BEYOND REPAIRABLE LIMITS & REQÿ½S REPLACEMENT IAW A320-200 SRM 53-02-00-283-001 TABLE2 REV.146. FH-35266:10, FC-11749, WV-015. NEW FLOOR BOARD PANEL RECEIVED P/N:E5367192300000; TO BE INSTALLED ON NON ROUTINE CARD 32098 (HAECO) CUST. CARD NO. G1871098 PO:1077033.3
Part: FLOOR PANEL — DELAMINATED (UNKNOWN) · airframe 35,266 hrs · 11,749 cycles
LESSOR ITEM 546: CABIN FLOOR PANEL 232EF DAMAGED 8" FROM REAR EDGE. GROUNDED - YES. EVALUATED 232EF CABIN FLOOR PANEL AS BEYOND REPAIRABLE LIMITS AND REQUIRES REPLACEMENT IAW A320-200 SRM 53-02-00-283-001 TABLE2 REV.146. FH=35266:10 FC:11749 WV=015 RECEIVED NEW FLOOR BOARD PANEL 232EF, P/N:5367191600100, TO BE INSTALLED ON NON ROUTINE 32098 (HAECO) CUST CARD NO G1871098. PO:1077072.1
Part: FLOOR PANEL — DENTED (UNKNOWN) · airframe 35,266 hrs · 11,749 cycles
LESSOR ITEM 550: CABIN FLOOR PANEL 241CF 2 OFF DENTS ON EDGE. GROUNDED - YES. EVALUATED 241CF CABIN FLOOR PANEL AS BEYOND REPAIRABLE LIMITS & REQÿ½S REPLACEMENT IAW A320-200 SRM 53-02-00-283-001 TABLE 2 REV.146. FH=35266:10 FC=11749 WV=015, NEW FLOOR BOARD RECEIVED P/N:E5367150900000, TO BE INSTALLED ON NON ROUTINE 32098 (HAECO), CUST. CARD NO:G1871098.
Part: FLOOR PANEL — DELAMINATED (UNKNOWN) · airframe 35,266 hrs · 11,749 cycles
LESSOR ITEM 529: CABIN FLOOR PANEL 231KF MANY DENTS GROUNDED - YES. EVALUATED AND RECEIVED NEW FLOOR BOARD PANEL 231KF, P/N: E5367190500000 TO BE INSTALLED ON NON-ROUTINE 32098 (HAECO) CUST. CARD NO:G1871098 PO:1077069.3
Part: FLOOR PANEL — DELAMINATED (UNKNOWN) · airframe 35,266 hrs · 11,749 cycles
LESSOR ITEM 527: CABIN FLOOR PANEL 231QF 3 OFF DENTS. GROUNDED - YES. EVALUATED AND RECEIVED NEW FLOOR BOARD PANEL 231QF, P/N: E536190500000, TO BE INSTALLED ON NON ROUTINE 32098 (HAECO), CUST. CARD NO. G1871098 PO:1077069.2
Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 35,266 hrs · 11,749 cycles
CABIN FLOOR PANEL 251RF TOTALLY DE-LAMINATED. GROUNDED - YES. EVALUATED 251RF CABIN FLOOR PANEL AS BEYOND REPAIRABLE LIMITS AND REQUIRES REPLACEMENT IAW A320-200 SRM 53-02-000-283-001 TABLE 002 FIG 2 FH 35266:10, FC 11749, WV 015. RECEIVED NEW FLOOR PANEL 251RF P/N E367190500000, TO BE INSTALLED ON NON ROUTINE 32103 (HAECO), CUST. CONTROL# G1871103 PO:1077076.2
Part: FLOOR PANEL — PUNCTURED (UNKNOWN) · airframe 35,266 hrs · 11,749 cycles
LESSOR ITEM 551: CABIN FLOOR PANEL 242MF HOLE MID BOARD. GROUNDED - YES. REPAIRED LESSOR ITEM 551 CABIN FLOOR PANEL 242MF P/N E5367151200100 AT 5EA PUNCTURED AREAS OF UPPER SKIN IAW A320 SRM 53-02-00-283-001 AND 53-02-00-300-001, FINAL REPAIR SIZE AREA#1 24" FROM FWD EDGE, 4.7" FROM I/B EDG 025" DIA. AREA#2 52.9" FROM FWD EDGE, 4.25" FROM O/B EDGE, .4" DIA. AREA #3 80.2" FROM FWD EDGE, 9.1" FROM I/B EDGE, .25" DIA. AREA#4 96.8" FROM FWD EDGE, 4.6" FROM I/B .25" DIA. AREA#5 96.6" FROM FWD EDGE, 4" FROM O/B EDGE .3" DIA, ALL REPAIRS ARE CATEGORY A PERMANENT REPAIRS. A/C N847VA, FLIGHT CYCLES 11749, FLIGHT HOURS 35266:10, WV015
Part: FLOOR PANEL — DELAMINATED (UNKNOWN) · airframe 35,266 hrs · 11,749 cycles
LESSOR ITEM 554: CABIN FLOOR PANEL 241MF DE-LAMINATED AT CUT OUT GROUNDED - YES. RECIEVED NEW FLOOR BOARD 241MF, P/N: E5367151200000 TO BE INSTALLED ON NON-ROUTINE OPS 32101 (HAECO) CUST CARD NO. G1871101
Part: FLOOR PANEL — DELAMINATED (UNKNOWN) · airframe 35,266 hrs · 11,749 cycles
LESSOR ITEM 538: CABIN FLOOR PANEL REAR P/N E53675201800 3 OFF DENTS. GROUNDED - YES. EVALUATED AND RECEIVED NEW FLOOR PANEL P/N: E5367191100000, TO BE INSTALLED ON NON-ROUTINE: 32103 (HAECO), CUST. CARD N#G1871103 P.O.#1077209.1
Part: FLOOR PANEL — DENTED (UNKNOWN) · airframe 35,266 hrs · 11,749 cycles
LESSOR ITEM 534: CABIN FLOOR PANEL 241AF 3 OFF DENTS. GROUNDED - YES. VALUATED PANEL 241AF CABIN FLOOR PANEL AS BEYOND REPAIRABLE LIMITS AND REQUIRES REPLACEMENT IAW A320-200 SRM 53-02-00-283-001 TABLE 2 REV.146. FH=35266:10 FC=11749 WV=015, RECEIVED NEW FLOOR BOARD PANEL, P/N:E5367190700000, TO BE INSTALLED ON NON ROUTINE 32098 (HAECO), CUST. CARD NO:G1871098.
Part: FLOOR PANEL — DELAMINATED (UNKNOWN) · airframe 35,266 hrs · 11,749 cycles
LESSOR ITEM 547: CABIN FLOOR PANEL 232MF DAMAGED 6" FROM REAR EDGE. GROUNDED - YES. EVALUATED 232 MF CABIN FLOOR PANEL AS BEYOND REPAIRABLE LIMITS & REQÿ½S REPLACEMENT IAW A320-200 SRM 53-02-00-283-001 TABLE2 REV.146. FH-35266:10, FC-11749, WV-015. NEW FLOOR BOARD PANEL RECEIVED P/N:E5367150100000; TO BE INSTALLED ON NON ROUTINE CARD 32098 (HAECO) CUST. CARD NO. G1871098 PO:1077076.3
Part: FLOOR PANEL — PUNCTURED (UNKNOWN) · airframe 35,266 hrs · 11,749 cycles
LESSOR ITEM 548: CABIN FLOOR PANEL 232UF DAMAGED IN 2 OFF PLACES 1/4 WAY FROM FRONT EDGE. GROUNDED - YES. REPAIRED 2EA PUNCTURES ON CABIN FLOOR PANEL 232UF IAW A320-200 SRM 53-02-00-300-001. THIS IS A CETEGORY A PERMENANT REPAIR. FH-35266:10 FC-11749. WV-015
Part: DOOR SILL — CORRODED (FRM 68) · corrosion level 2 · airframe 35,266 hrs · 11,749 cycles
R2 DOOR AT FRAME 68 DOOR SILL WEB CORRODED AT AFT GIRT BAR FITTING AND WEB. GROUNDED - YES. REMOVED CORROSION ORIG .063 MATERIAL LOSS .040 REMAINING .023 FOUND TO BE OUT OF LIMITS REF A320 SRM 53-41-14-283-002 AREA REPAIRED ON CUSTOMER CARD G1871530 HAECO CARD 32530 ATTACHED THIS IS A CAT A REPAIR NO FURTHER ACTION REQUIRED
2017
Part: FLOORBEAM — CORRODED (FRAME 68)
CORROSION FOUND ON AFT CABIN AREA FLOORBEAM Y765 BTW FR 68. THE EXTENT OF THE DAMAGE IS 2 INCHES LENGTH X 1 INCH WIDTH MATERIAL REMOVED .035 INCHES. THE FLOORBEAM WAS R & R IAW A320 SRM 51-42-11
Part: SHEAR PLATE — CRACKED (FRAMES 69-70)
FOUND CRACK ON AFT CABIN AREA RT LATERAL SHEAR PLATE BTW FR 69 - 70. SHEAR PLATE WAS R & R IAW 320 SRM 51-42-11.
Part: SHEAR PLATE — CRACKED (FRAMES 69-70)
FOUND CRACK ON AFT CABIN AND LT LATERAL SHEAR PLATE BTW FR 69-70. SHEAR PLATE WAS R & R IAW A320 SRM 51-42-11.
2016
Part: FAN — FAILED (CABIN) · airframe 17,547 hrs · 4,756 cycles
REPORTED ELECTRICAL ODOR ON TAXI OUT FOR VX24. ACFT RETURNED TO GATE. MAINTENANCE FOUND RT CABIN FAN FAULTED AND PROCEEDED TO PLACE ON MEL, FOR REPLACEMENT ON NEXT MAINTENANCE OPPORTUNITY. NO FURTHER DEFECTS NOTED.