JASC 5310

Service difficulty reports · 38,528

Reports filed under 5310 · Fuselage Main, Structure, newest first.

Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE jasc_code = '5310'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR JR2R20211006415Beam · corrodedCABIN FLOOR CROSS BEAM AT FR17 CORRODED AT RBL30Oct 6, 2021 · N86334 · Emb ERJ170200LRSDR SWAA2021112426946Crease Beam · corrodedSUPPLEMENTAL INFORMATION: CORROSION ON PASSENGER CABIN CREASE BEAM BS714 LBL68 WL208. ; / [01] UPDATED TABLE; [02] REMOVED 1 EA FASTENER IN CREASEBEAM WEB STA 714; LBL 68; WL 208 FOR ACCESS PER SRM 51-40-02-0G-0.;[22] CREASE BEAM WEB REPLACED. ALL WORK ACCOMPLOct 5, 2021 · N780SW · Boeing 737SDR SWAA2021112426947Crease Beam · corrodedCORROSION ON PASSENGER CABIN CREASE BEAM BS716 LBL60 WL208. CREASEBEAM WEB BS 706 - 716; LBL 65 - 70, WL 208 REPLACED ON CARD TTG8Q006SPMB.Oct 5, 2021 · N780SW · Boeing 7377H4SDR SWAA2021112426945Crease Beam · corrodedCORROSION ON CABIN CREASE BEAM BS 713 LBL 69 WL 208. REMOVED 1 FASTENER IN THE CREASE BEAM WEB IAW SRM 51-40-02-0G-0. REMOVED CORROSION ON UPPER SURFACE OF CREASE BEAM WEB. AREA BLENDED IS 1' BY 1' IAW SRM 51-10-02-0G-0. EDDY CURRENT INSPECTED ON BLENDEDOct 5, 2021 · N780SW · Boeing 7377H4SDR SWAA2021111926943None · corrodedCORROSION ON PASSENGER CABIN CREASE BEAM BS727C+18 RBL69 WL208. ; / [01] UPDATED TABLE; [02] REMOVED 1 EA FASTENER IN PASSENGER CABIN CREASEBEAM WEB STA 727C+18; RBL 69; WL 208 FOR ACCESS PER SRM 51-40-02-0G-0.; [03] REMOVED CORROSION ON UPPER SURFACE ON CREASOct 5, 2021 · N780SW · Boeing 737*SDR SWAA2021111926959None · corrodedCORROSION ON FWD ENTRY DOOR CUTOUT LOWER SURFACE OF UPPER SILL WEB BS 307-312 AND BS 313-316 LBL 36 WL 284. ; / [01] VERIFIED APPLICABILITY OF SRM 53-10-15-0I-1 AND SRM 53-10-15-1A-1; [11] REPAIRED CORROSION ON FWD. ENTRY DOOR CUTOUT UPPER SILL WEB LOWER SURFAOct 5, 2021 · N780SW · Boeing 737*SDR SWAA2021110127076Web · corrodedA-061 DOT 2 CORROSION FWD PIT THRESHOLD WEB UPPER SURFACE STA 460 +10' TO STA 480 + 10' RBL 29 WL 155 ; / [01] UPDATED MEASUREMENTS IN CHART; [02] REMOVED CORROSION IAW 51-10-02 10X MAGNIFYING; [03] VERIFIED MEASUREMENTS AND CORROSION REMOVAL ITEMS 1 AND 2; [0Oct 5, 2021 · N901WN · Boeing 7377H4SDR FDEA202110052468Stringer · crackedCENTER UPPER AUXILIARY TANK STRINGER AT LEFT HAND S-52, XCW 48 FOUND CRACK ABOUT 7.5 INCHES IN LENGTH. CENTER UPPER AUXILIARY TANK AT LEFT HAND S-52, XCW 48 CRACK STRINGER REPAIRED AS PER MD-11 SRM 57-10-03-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOOct 5, 2021 · N597FE · Doug MD11FSDR SIMA20211005002None · noneFOUND DAMAGE TO FORWARD PRESSURE BULKHEAD AND RADOME ATTACHMENT FRAME (PN# 170-05355-401)-C/A-REMOVED AND INSTALLED MACHINED FRAME 1 AND 8 EA VERTICAL RIBS AND 4 EACH HORIZONTAL RIBS AND 4 EACH LATCHES IAW EMB 175 SRM 51-40-08Oct 5, 2021 · N202NN · Emb ERJ170200LRSDR FDEA202110052469Frame · crackedRH 1640 FUSELAGE FRAME WEB AND STR 14 LOWER INBD HOLE HAS CRACK INDICATIONS AT 3 AND 9 O'CLOCK POSITION,, VIEWED LOOKING AFT. COMPLIED WITH FUSELAGE - MAINFRAME - STA 1640 FRAME SPLICE REPAIR TO REPLACE CRACK AT ST-14 RIGHT. EA# F-5310-T0363945. MAJOR REPOct 5, 2021 · N988FD · Boeing 757222SDR AALA202110082027Box Beam · crackedAIRCRAFT IN BASE MAINTENANCE: RIGHT HAND SIDE BOX BEAM AT FR 43 AND -Y1622 CRACKED AT THE FIRST HOLE. REPAIRED BOX BEAM PER EO 5315Y066.Oct 5, 2021 · N775XF · Airbus A319112SDR SWAA2021112426452None · corrodedCORROSION ON B.S. 1016 CHORD BETWEEN STRINGERS 25 LEFT AND 25 RIGHT; W.L. 190. ; / [01] EVALUATED CORROSION ON CHORD SPLICE; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0; [02] VERIFIED CORRECTIVE ACTION IOct 4, 2021 · N780SW · Boeing 7377H4SDR SWAA2021112426444Beam · corrodedCORROSION ON B.S.270 LATERAL BEAM AT L.B.L 9; L.B.L. 6; L.B.L. 4; R.B.L. 3 AND R.B.L. 9; W.L. 207.54. ; / [01] REMOVED FASTENER ON BS270 RBL9-LBL9 WL208 I.A.W SRM 51-40-02-0G-0; [08] DAMAGE ON BS270 LATERAL BEAM FROM LBL9-RBL9 WL207.5 18'X1' AREA FOUND TO BE OOct 4, 2021 · N780SW · Boeing 7377H4SDR FDEA202110042459Fitting · crackedAGING AIRCRAFT - EXISTING REPAIR AT NOSE LANDING GEAR TRUNNION FITTING STATION 595 RIGHT HAND SIDE EXISTING REPAIR AT NOSE LANDING GEAR TRUNNION FITTING STATION 595 RIGHT HAND SIDE EVALUATED AND FOUND REPAIRED IAW EA 1-5310-105635 PART 1 TITLE: FUSELAGE Oct 4, 2021 · N597FE · Doug MD11FSDR CALA2021100601784Bulkhead · cracked(SUPPORT TASK) DURING ROTO PROBE OF FASTENER HOLES AT RH FR35 ST R30, DAMAGE INDICATIONS WERE NOTED IN THE TOP AFT HOLE.() COMPLIED WITH EC/RA 5321-02055 TO REPAIR FR35 STR 30 HOLE #1 RH WITH NO DEVIATIONS. ACCOMPLISHED BY EMP#V933440 AT BFM VT MOBILE AEROSPACOct 4, 2021 · N482UA · Airbus A320232SDR CALA2021100601782Bulkhead · damaged(SUPPORT TASK) DURING ROTO PROBE OF FASTENER HOLES AT LH FR35 ST R30, DAMAGE INDICATIONS WERE NOTED IN THE TOP AFT HOLE.() REPAIR FR35 STGR30 HOLE #1 L/H BY COMPLY WITH EC/RA 5321-02055 W ITH NO DEVIATIONS. ACCOMPLISHED BY EMP#V933440 AT BFM VT AEROSPA CE MOBIOct 4, 2021 · N482UA · Airbus A320232SDR CALA2021100601781Bulkhead · crackedDURING ROTO PROBE OF FASTENER HOLES AT LH FR35 STR30, A CRACK IN DICATION WAS NOTED IN THE BOTTOM AFT HOLE.() REPAIRED LH FR35 STR 30 HOLE #2 BY COMPLYING WITH EC/RA 5321-020 55 WITH NO DEVIATIONS. ACCOMPLISHED BY EMP#V933440 AT BFM VT AER OSPACE MOBILE. NR#00Oct 4, 2021 · N482UA · Airbus A320232SDR CALA2021100601780Bulkhead · none(SUPPORT TASK) DURING ROTO PROBE OF FASTENER HOLES AT RH FR35 ST R30, A DAMAGE INDICATION WAS NOTED AT THE BOTTOM AFT HOLE.() REPAIRED R/H FR35 STR30 HOLE #2 BY C/W EC/RA 5321-02055 WITH NO DEVIATIONS. EMP#V933440 AT BFM VT AEROSPACE MOBILE. NR#0013369Oct 4, 2021 · N482UA · Airbus A320232SDR SWAA2021102725516None · corrodedCORROSION ON SUBTHRESHOLD WEB AT FWD CARGO BAY BS 454 - 476, RBL 28, WL 156. EVALUATED DAMAGE ON SUBTHRESHOLD WEB. ORIGINAL THICKNESS .045' DAMAGE REMOVED; .009' REMAINING THICKNESS .0036 L= 2' X W=1.2' DEPTH .009 DAMAGE EXCEED 10% OF ORIGINAL THICKNESS, FOUNOct 3, 2021 · N232WN · Boeing 7377H4SDR ASAA2021100238392Box Beam · crackedTORSION BOX LOWER SIDE SHELL STR15 R FASTENER HOLE IS CRACKED IN PRESSURE PLATE 2ND HOLE FROM AFT PER SB A320-53-1251 FIG. A-GDAAA VIEW D GROUNDED - YES. REPAIRED IAW ASA EA A320-53EA-01109 REV. 00, DATED 12/10/2021, AIRBUS SB A320-53-1251 REV 4, DATED 05/17/Oct 2, 2021 · N628VA · Airbus A300*SDR ASAA2021100238391Box Beam · crackedTORSION BOX LOWER SIDE SHELL STR15 L FASTENER HOLE IS CRACKED IN PRESSURE PLATE, 5TH HOLE FROM AFT, PER SB A320-53-1251, FIG A-GDAAA VIEW D. GROUNDED - YES. REPAIRED IAW ASA EA A320-53EA-01109 REV. 00, DATED 12/10/2021, AIRBUS SB A320-53-1251 REV 4, DATED 05/1Oct 2, 2021 · N628VA · Airbus A300*SDR AALA202110288911Shear Plate · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK FOUND ON SHEAR PLATE STR 23R LOCATED FR69 TO FR70 AFT GALLEY AREA (LENGTH: 1 INCH). REPLACED SHEAR PLATE STR 23R LOCATED BETWEEN FR69 TO FR70 AT AFT GALLEY AREA.Oct 2, 2021 · N153AN · Airbus A300*SDR AALA202110279298Shear Plate · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK FOUND ON SHEAR PLATE. LOCATED AT FR69 TO FR70, STR 23L. LENGTH 1 INCH. REPLACED SHEAR PLATE AT AFT GALLEY AREA PER SRM 51-72-11-911-001.Oct 2, 2021 · N153AN · Airbus A300*SDR AALA202110216401None · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT LEFT HAND PASSENGER / CREW DOOR CUT OUT LOWER SILL BETWEEN FR 66 AND FR 68 AT S23L. REPAIRED LOWER SILL PER SRM 53-41-14-300-001.Oct 2, 2021 · N153AN · Airbus A321231SDR UIEA2021092402099Support · corrodedFX - BODY FAIRING 294JR LOWER SUPPORT CHORD FOUND CORROSION CRACK. FX - BODY FAIRING 294JR LOWER SUPPORT CHORD P/N : 65B15009-4 CORROSION CRACK AREAS REPAIRED IAW RI-53-00-14965 REV AOct 2, 2021 · N472MC · Boeing 74745ESDR UIEA2021092402100Support · corrodedFX - BODY FAIRING 293JL SUPPORT CHORD FOUND CORROSION CRACK. FX - BODY FAIRING 293JL SUPPORT CHORD P/N : 65B15009-3 CORROSION CRACK AREAS REPAIRED IAW RI-53-00-14965 REV AOct 2, 2021 · N472MC · Boeing 74745ESDR CALA2021100401767Skin · corrodedREMOVED CORROSION IAW SRM 51-74-00 ORIGINAL SKIN THICKNESS .063" L=1.660" W=1.020" D=.060" FOUND OT BE OUT OF LIMITS IAW SRM 53-4 1-11-283 FIG. REPAIRED IAW FINAL EC/RA 5331-02766 REV "-" AND EA 320-5341-13-A2686 REV "-" REMOVED CORROSION IAW SRM 51-74-00 ORIGOct 2, 2021 · N482UA · Airbus A320232SDR SWAA2021112425767Web · corrodedSUPPLEMENTAL INFORMATION: FWD CARGO BAY SUB THRESHOLD CORRODED AROUND FASTENER HOLES BS 440+33; 440+33; RBL 29; WL 156 ; / [01] AFTER FURTHER INVESTIGATION; FOUND CORROSION ON SUB THRESHOLD WEB TO BE AT BS 440+33 AND BS 440+39; [02] EVALUATED CORROSION; FOUND Oct 1, 2021 · N780SW · Boeing 737SDR FDEA202110013027Frame · corrodedAFT CARGO - DURING PERFORMING CORROSION REMOVAL OF LWR CLOSE OUT WEB FITTING ABOVE LATCH SPOOLS, FOUND ZEE FRAME P/N AGA7195-3Z HEAVILY CORRODED, REQUIRES NEW ZEE FRAME TO BE FABRICATED FABRICATED NEW ZEE FRAME AGA7195-3 PER DOUGLAS DRAWING AGA7195, MD11 SOct 1, 2021 · N586FE · Doug MD11FSDR SWAA2021110425654Web · crackedFWD CARGO WEB CRACKED AT FASTENER HOLE BS 500 - BS 500A RBL 22 WL 154 ; / [01] REMOED WEB AT FWD CARGO BS 500 - BS 500A RBL 22 WL 154 IAW SRM 51-40-02-0G-0; [02] WEB FORMING AND HEAT TREATMENT ACCOMPLISHED ON PO#839725/1.; [03] LOCATED AND DRILLED REPLACEMENT Oct 1, 2021 · N557WN · Boeing 737790SDR V0XD20211102001Angle · crackedTWO ANGLES CRACKED FROM SHEAR BOXES TO F.S 280 BEAM LBL 9.0 AND RBL 9.0. CORRECTIVE ACTION: REMOVED AND REPLACED ANGLES LBL 9 (P/N: CC670-34099-1) AND RBL 9 (P/N: CC670-34099-2) ON F.S. 280 BEAM IAW CRJ 900 SRM 51-42-21, 51-40-11, 51-21-11, 51-25-06, 51-25-16 Oct 1, 2021 · N951LR · Cndair CL6002D24SDR ASAA2021100136366Track · corrodedAFT CARGO COMPARTMENT FLOOR SUPPORT, RH TIE-DOWN FITTING HAS CORROSION AT BS727F. DOT:V664. GROUNDED - YES. REMOVED CORROSION FROM AFT CARGO FLOOR SUPPORT TIE DOWN AT BS727F PER B737-800 SRM 53-00-53-1A-2; REMOVED 0.050 MAX DEPTH ALLOWED 0.040;FOUND TO BE OUTOct 1, 2021 · N557AS · Boeing 737890SDR ASAA2021100136273Floorbeam · corrodedRH MAIN CABIN FLOOR SUPPORT BEAM UPPER CHORD HAS CORROSION, BS320, RBL-56 DOT:V657. GROUNDED - YES. BLENDED OUT CORROSION, ORIGINAL THICKNESS 0.125 IAW B737-800 SRM 53-10-51.REMOVED 0.037,REMAINING THICKNESS 0.088.AREA OUT OF LIMITS.REPAIRED AREA IAW B737-800 Oct 1, 2021 · N557AS · Boeing 737890SDR FDEA202110012438Doubler · unknownREQUEST BY CUSTOMER TO CREATE A SDR FOR EA G-5310-T0364043 P1 STEP 3 REPAIR FASTENER INTERFERENCE WITH LH LONGERON NEW DOUBLER (143W2314Y405) TRAILING EDGE DURING REPAIR EMBODIMENT CONDITION (DEVIATION) IN EA G-5710-T0364075 P1. THE DOUBLER TRAILING EDGE WOct 1, 2021 · N892FD · Boeing 777FS2SDR CALA2021100401766Beam · corrodedCORROSION ON AFT CABIN FLOOR BEAM Y512.5 AT FR68. (A3NB-53-3-622 2) CORROSION ON FLOOR BEAM Y512.5 FR68 BLENDED OUT IAW SRM 51-74-00 SFR# 1026596. MAINTENANCE ACCOMPLISHED BY V933868 ON WC 0014619 , BLENDED AREA MEASURES LENGTH 1.5" WIDTH 0.15" ORIGINAL THICKNOct 1, 2021 · N495UA · Airbus A320232SDR CALA2021100401765Beam · corrodedCORROSIN ON AFT CABIN FLOOR BEAM Y-1292 AT FR66. (A3NB-53-3-6222 ) BLENDED OUT CORROSION ON AFT CABIN BEAM Y-1292 AT FR66 IAW SRM 5 ING BFM 1-74-00 FIG 1. FLOOR BEAM FOUND TO BE OUT OF LIMITS IAW SRM 53-0 0-15-283-002 L=4.0" W=2.0" D=.046". REMOVED AND REPLACEOct 1, 2021 · N495UA · Airbus A320232SDR CALA2021100401764Beam · corrodedCORROSION ON AFT CABIN FLOOR BEAM Y-765 BETWEEN FR67 AND FR68 (A 3NB-53-3-6222) BLEND OUT CORROSION ON AFT CABIN FLOOR BEAM Y-765 BETWEEN FR67 A E ACCOMPLISHED BY V933486 ON WC 0014617 AT ST ENGINEERING BFM ND FR68IAW SRM 51-74-00 AND FOUND OUT OF LIMITS IAW SOct 1, 2021 · N495UA · Airbus A320232SDR CALA2021100401763Beam · corrodedCORROSION ON AFT CABIN FLOOR BEAM Y-1162.5 AT FR68. (A3NB-53-3-6 222) BLENDED OUT CORROSION ON AFT CABIN FLOOR BEAM Y-1162.5 IAW SRM 5 ENGINEERING BFM 1-74-00 FIG 1. FLOOR BEAM FOUND TO BE OUT LIMITS IAW SRM 53-00-1 5-283-002 L=0.80" W=0.5" D=0.150". REMOVED AOct 1, 2021 · N495UA · Airbus A320232SDR DU4R2021100100096Door · noneDURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FLORIDA FOUND R/H AFT DOOR FRAME, FRAME 68 DOOR STOP #3, OUTBOARD LOWER HOLE HAS A DAMAGED/OUT OF ROUND INDICATION. S/O 193124 N/R 30093 NR00832597Oct 1, 2021 · N315NV · Airbus A319111SDR DU4R2021100100095Frame · crackedDURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FLORIDA FOUND L/H AFT PASSENGER FRAME, FRAME 66, DOOR STOP #1 HAS A CRACK INDICATION IN THE INBOARD LOWER HOLE OF FRAME AT THE 7 O'CLOCK POSITION.Oct 1, 2021 · N315NV · Airbus A319111SDR ASAA2021093036118Angle · corrodedFWD SIDE OF ACCESS DOOR 312AR CUTOUT FRAME 71 HAS CORROSION ON LOWER SUPPORT ANGLE (CLIP) GROUNDED - YES. DUE TO THE EXTENT OF THE CORROSION (50% MATERIAL LOSS), REMOVED LOWER SUPPORT ANGLE (CLIP) FROM FWD SIDE OF ACCESS DOOR 312AR CUTOUT AT FRAME #71. REPLACESep 30, 2021 · N846VA · Airbus A320214SDR CALA2021100101737Plate · corrodedRIGHT HAND SHEAR PLATE @ FR68-70 HAS CORROSION() REPLACED SHEAR PLATE AND SUPPORT FRAME IAW A320 SRM 51-42-11, SH EAR PLATE P/N# D5347112420300 BATCH# 0003689234, NEW SUPPORT FRA ME P/N# D5347112320300 BATCH# 0002507052 FORM 44-0008 ARTACHED E MP# V934583 WORKSep 30, 2021 · N482UA · Airbus A320232SDR V0XD20211121001Stringer · noneCORRODED IN MAIN AVIONIC COMPARTMENT AT FS 319 TO FS 333 ON STGR 25R. CORRECTIVE ACTION: REPAIRED STGR 25R FROM FS 295 TO FS 333 (P/N: SH670-32429-2) IAW CRJ 900 SRM 53-00-03.Sep 29, 2021 · N951LR · Cndair CL6002D24SDR IPXA2021102175186Shim · noneINSPECTION TYPE:A300CENTER FUSELAGE BASE FRAME FITTING AT FR44 LH SIDE HAS CRACK.REPAIRED PER EO A300-5310-46789-G APPENDIX J INSTALL ONLY.Sep 29, 2021 · N146UP · Airbus A300F4622RSDR IPXA2021102175179Doubler · crackedINSPECTION TYPE:A300CENTER FUSELAGE BASE FRAME FITTING AT FR 46 R/H SIDE HAS CRACK.ACCOMPLISHED REPAIR PER EO# A300-5310-46789-G APPENDIX K. INSTALL ONLYSep 29, 2021 · N146UP · Airbus A300F4622RSDR CALA2021100101732None · abnormalAFT CABIN BELOW R2 DOOR SILL AFT OF FRAME 66 STRINGER HAS EXFOLI ATION CORROSION (A3NB-53-3-6033) GENERATED BY V052030 AT HAECO LCQ PER NR 9294659 (28659). REMOVED AND REPLACED STRINGER 25RT AFT OF FR 66RT IAW A320 SRM 5 1-42-11. PERFORMED BY V913406 AND INSP Sep 29, 2021 · N436UA · Airbus A320232SDR AALA202110114864None · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION OF TRANSITION PANEL NEAR FASTENER HOLES BETWEEN STA 500 AND STA 500A AT RBL 26, MEASURING L=1.0 IN, W=1.0 IN, D=0.031 IN. ACCOMPLISHED PERMANENT REINFORCING PLUG REPAIR IAW EA330774.Sep 28, 2021 · N814NN · Boeing 737823SDR CALA2021092801721Shear Plate · corrodedRIGHT HAND SHEAR PLATE @ FR68-70 HAS CORROSION() REPLACED SHEAR PLATE AND SUPPORT FRAME IAW A320 SRM 51-42-11, SH EAR PLATE P/N# D5347112420300 BATCH# 0003689234, NEW SUPPORT FRA ME P/N# D5347112320300 BATCH# 0002507052 FORM 44-0008 ARTACHED E MP# V934583 WORKSep 28, 2021 · N482UA · Airbus A320232SDR CALA2021092801712Stringer · corrodedA3NB-05-3-6022: BULK CARGO COMPT FR 63-64 STRINGER 42R HAS CORRO SION. DOT 116-65 () 283-002. REPAIRED STRINGER SECTION 42 BETWEEN FR63 TO FR64 IAW INSPECTION THRESHOLD FROM TIME OF ADL/REPAIR EMBODIMENT IS SRM 53-00-13-300-001, FIG 001, SHT 1. DIM CUT OUT LIMSep 28, 2021 · N482UA · Airbus A320232SDR CALA2021092801711Stringer · corrodedA3NB-05-3-6022:BULK CARGO COMPT FR 64-65 STRINGER 44 HAS CORROSI ON DOT 116-66 () SPLICE AND STRINGER IAW SRM 51-42-11 FROM FR 63 TO FR 67, CUT SECTION OUT OF DAN50B08 BATCH #2478344, D5348003020700 AND SPLICE, FACTORY SPLICE AND STRINGER REPAIR SECTION IAW SRSep 28, 2021 · N482UA · Airbus A320232
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