JASC 5300

Service difficulty reports · 8,205

Reports filed under 5300 · Fuselage Structure (General), 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 = '5300'
  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 DALA2023061904968Unknown · unknownCORROSION ON DIAPHRAGM STA Y=198 TO Y=200 BTW X=-30 AND X=-50 (RH SIDE) AT PAX CABIN. SUMMARY OF NRC 00254: CORROSION LEVEL 2. DIAPHRAGM STA Y=198 TO Y=218 BTW X=-30 AND X=-56 (RH SIDE) WAS REPLACED PER DWG 9936534 REV BW. (LP #2821288)Jun 17, 2023 · N992AT · Boeing 717200SDR SWAA2023081459839Channel · corrodedCORROSION FOUND AFT CARGO RH 'Z' CHANNEL AT STA 727C + 2 RBL 21 WL 155.5 HAS SPOT OF CORROSION.<[01] REPAIR WAS ACCOMPLISHED IN THE ITEM TTG8Q00LP0BE;[02] TRANSFER OF WORK ; AS PER ENTRY #1 ' TTG8Q00LPOBE ' INSP. VERIFIED AS SUCH. THIS N/R IS NOW CLOSEDJun 16, 2023 · N444WN · Boeing 7377H4SDR R61A2023071200095Floor Support · corrodedCENTER FUSELAGE III PAX CABIN FLOOR STRUCTURES LOCATED AT AFT WET AREA, HAVE CORROSION ON RH BEAM AT FR 86-89 STGR 17R AS MARKED. REMOVED AND REPLACED RH BEAM BETWEEN FR 86-89. REF EMB SRM 51-40-08.Jun 16, 2023 · N429YX · Emb ERJ170200LRSDR JJBA20230628023Unknown · unknownCF1, CRACK FOUND ON LH OMEGA BEAM #2 FLOOR STRUCTURE BTW FR 23-24. BEAM REPAIRED WITH A DOUBLER.Jun 16, 2023 · N14179 · Emb EMB145XRSDR CALA2023061601884Floor Support · corrodedB767-53-3-7023, FWD CGO COMPT- STA 498 RBL 39" LATERAL TORQUE BOX PNL SUPPORT CHORD LWR SURFACE FOUND CORROSION TRANSFER REF HXWO 1883060 AND ORIGINATED BY EMP V930061 FWD CARGO COMPT STA498 RBL30 TO RBL40 LATERAL TORQUE BOX WORK ACCOMPLISHED BY MECHANIC V8975Jun 16, 2023 · N649UA · Boeing 767322SDR CALA2023061601883Intercostal · corrodedB767-53-3-7023, FWD CGO COMPT- STA 478 TO 500 RBL 39" LONGITUDINAL FLR SUPPORT LWR SURFACE FOUND CORROSION AS MARK TRANSFER REF HXWO 1883040 AND ORIGINATED BY EMP V930061 FWD CARGO COMPT STA478 TO 497 RBL39" LONGITUDINAL FLOOR WORK ACCOMPLISHED BY MECHANIC V89Jun 16, 2023 · N649UA · Boeing 767322SDR CALA2023061601882Intercostal · corrodedB767-53-3-7025 - FWD CARGO FLOOR STA502-512 RBL36.88 SUPPORT BEAM FOUND CORROSION TRANSFER REF HXWO 1877224 AND ORIGINATED BY EMP V896810 FWD CARGO FLOOR STA502 TO STA512 RBL36.88 FLOOR SUPPORT BEAM WORK ACCOMPLISHED BY MECHANIC V897549 INSPECTED BY V896375 REJun 16, 2023 · N649UA · Boeing 767322SDR CALA2023061601881Unknown · corrodedB767-53-3-7025 - FWD CARGO FLOOR STA512 RBL30-34 SUPPORT BEAM FOUND CORROSION TRANSFER REF HXWO 1877229 AND ORIGINATED BY EMP V896810 FWD CARGO FLOOR STA512 RBL30-40 SUPPORT BEAM REPLACED AS WORK ACCOMPLISHED BY MECHANIC V897549 INSPECTED BY V896375 PER SRM51-Jun 16, 2023 · N649UA · Boeing 767322SDR CALA2023061601880Unknown · corrodedB767-53-3-7023, FWD CGO COMPT STA 502 RBL 39" LATERAL TORQUE BOX PNL SUPPORT CHORD LWR SURFACE FOUND CORROSION TRANSFER REF HXWO 1883048 AND ORIGINATED BY EMP V930061 FWD CARGO COMPT STA502 RBL30 TO RBL40 LATERAL TORQUE BOX PANEL SUPPORT CHORD REPLACED AS PER Jun 16, 2023 · N649UA · Boeing 767322SDR CALA2023061601879Intercostal · corrodedB767-53-3-7025 FWD CGO COMPT STA 550 TR PDU LH MOUNT NUT SUPPORT BEAM FOUND CORROSION TRANSFER REF HXWO 1858966 AND ORIGINATED BY EMP V896510 FWD CARGO COMPT STA544-566 RBL25 AND RBL33.08 SUPPORT WORK ACCOMPLISHED BY MECHANIC V897549 INSPECTED BY V896375 BEAM Jun 16, 2023 · N649UA · Boeing 767322SDR DALA2023061904965Unknown · unknownCORROSION ON DIAPHRAGM FROM STA Y=190 TO Y=200 BTW X=50 AND X=57 (L1 DOOR) AT PAX CABIN. SUMMARY OF NRC 00274: CORROSION LEVEL 2. DIAPHRAGM FROM STA Y=190 TO Y=200 BTW X=50 AND X=57 WAS REPAIRED PER B717 SRM 51-70-10-2R REPAIR 2. (LP #2819862)Jun 16, 2023 · N992AT · Boeing 717200SDR DALA2023061904961Unknown · unknownCRACK ON LOWER SKIN AT CUSP WEB MEMBRANE STA 634. SUMMARY OF NRC 00149: LOWER SKIN AT CUSP WEB MEMBRANE STA 634 WAS REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4 REPAIR 4 FIG.221. (LP #2819538)Jun 16, 2023 · N924AT · Boeing 717200SDR DALA2023061604928Web · corroded(LOG 2818886) FORWARD CARGO COMPARTMENT DOOR CUT OUT LOWER SILL HAS AREAS OF CORROSION ON UPPER SURFACE BETWEEN BS 440 AND BS 490. INSTALLED NEW WEB AT FWD CARGO COMPT DOOR CUT OUT LOWER SILL BETWEEN BS 440 AND BS 490. REF USED DELTA PSM 900-2 NO. 09, DELTA PSJun 16, 2023 · N937DM · Boeing 7379SDR DALA2023061604905Unknown · unknownCRACK ON ANGLE UPPER BEAM AFTER CORNER AT CABIN PAX L1 DOOR. SUMMARY OF NRC 00128: ANGLE UPPER BEAM AFTER CORNER AT CABIN PAX L1 DOOR WAS REPAIRED PER B717-200 SRM 52-10-02-2R PROCEDURE 7, REPAIR 7. (LP #2819045)Jun 16, 2023 · N992AT · Boeing 717200SDR DALA2023061604904Unknown · unknownCORROSION ON LH CUSP WEB IN STA Y=364 AT PASSENGER CABIN STRUCTURE. SUMMARY OF NRC 00566: CORROSION LEVEL 2. LH CUSP WEB IN STA Y=364 AT PASSENGER CABIN STRUCTURE WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4 FIG 215. (LP #2818952)Jun 16, 2023 · N924AT · Boeing 717200SDR ABXA20230623127Skin · crackedDURING C21 MAINTENANCE CHECK AT HAECO AMERICAS, DENT AND CRACK DAMAGE WAS FOUND ON THE FUSELAGE SKIN P/N 148T3251-4. THE DAMAGE IS LOCATED AT STA 1710.5 BELOW THE S-36L SKIN LAP JOINT WITHIN A SKIN CHEM MILLED POCKET WITH A THICKNESS OF 0.056-INCH. THERE ARE NJun 15, 2023 · N220CY · Boeing 767383SDR CALA2023061601876Unknown · corrodedUPON REMOVAL OF GIRT BAR FITTING BASE PLATE TO APPLY REPAIR TO L 2 DOOR SILL FOUND CORROSION AT FR66 PER NR9298903/44903 GEN BY V 080280 RMVD AND RPLD L2 DOOR SILL IAW SRM 51-72-11-911-001 APPLIED TOPC OAT IAW SRM 51-75-12-911-002 BY MECH V928628 INSP BY V0779Jun 15, 2023 · N825UA · Airbus A319131SDR CALA2023061601875Unknown · corrodedUPON REMOVAL OF GIRT BAR FITTING BASE PLATE TO APPLY REPAIR TO R 2 DOOR SILL FOUND CORROSION AT FR66 PER NR9298904/44904 GEN BY V 080280 REMOVED AND REPLACED R2 DOOR SILL IAW SRM 51-72-11 BY MECH V0397 46 INSP BY N078625Jun 15, 2023 · N825UA · Airbus A319131SDR REXA2022061600360Floorbeam · corrodedTHE LH FS 280 BEAM IS CORRODED IN SEVERAL AREAS ON THE LOWER SURFACE IN THE RADIUS. REMOVED AND REPLACED CROSSBEAM I.A.W. BOMBARDIER CRJ900 SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01, 51-42-22-001-001-A01, 51-40-11-001-001-A01, 51-21-11-001-001-A01 AND 51Jun 15, 2023 · N912XJ · Cndair CL6002D24SDR DALA2023061604908Unknown · unknownSHIP 3123 CORROSION FLOOR BEAM -Y765 LOCATED AT FR 66 AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOOR BEAM PER A319 SRM 51-42-11. (2818120)Jun 15, 2023 · N323NB · Airbus A319114SDR DALA2023061604907Unknown · unknownSHIP 3123 CORROSION ON WEB FRAME 20 -Y1600 APROX AT FWD GALLEY AREA. CORRECTIVE ACTION: REPLACED WEB PER A319 SRM 51-72-11. (2818115)Jun 15, 2023 · N323NB · Airbus A319114SDR DALA2023061604900Unknown · unknownCORROSION ON R1 DOOR SERVICE LOWER DOOR JAMB STA Y=168 TO STA Y=200. IN REFERENCE NRC 0428. PTAS. SUMMARY OF NRC 00531: CORROSION LEVEL 2, R1 DOOR SERVICE LOWER DOOR JAMB STA Y=168 TO STA Y=200 WAS REPAIRED PER PRI 609065-14 REV 2 AND ER/A 609065-14 REV ORIGINJun 15, 2023 · N899AT · Boeing 717200SDR DALA2023061604899Unknown · unknownCRACK ON INSIDE JAMB STA Y=160 ON TOP OF PASSENGER ENTRANCE DOOR L1. SUMMARY OF NRC 00143: CRACKED INSIDE JAMB ON TOP OF PASSENGER ENTRANCE DOOR L1 WAS REPLACED PER B717-200 SRM 51-41-02-0G AND 51-41-01-0G. (LP #2818186)Jun 15, 2023 · N957AT · Boeing 717200SDR R61A2023070800387Beam · corrodedAFT PAX DOOR CUTOUT LOWER BEAM IS CORRODED AS MARKED FR 85- FR 87. REMOVED AND REPLACED AFT PAX DOOR CUTOUT LOWER BEAM. REF EMB SRM 51-40-08Jun 14, 2023 · N232JQ · Emb ERJ170200LRSDR CALA2023061601889Frame · crackedFRAME ATTACH BRACKET FOR OVERHEAD BIN IS CRACKED @ STA. 1120 L/H STRINGER 8. D. OSBORNE V921218 (M). FRAME ATTACH BRACKET FOR OVERHEAD BIN IS CRACKED @ STA. 1120 L/H STRINGER 8. D. OSBORNE V921218 (M). ADD EMP:V921218Jun 14, 2023 · N13113 · Boeing 757224SDR CALA2023061601871Stringer · corrodedB767-53-3-7058 AFT OF BULK CGO BILGE STA 1540 S38L STRINGER FOUND CORROSION TRANSFER REF HXWO 1856266 AND ORIGINATED BY EMP V896810 BULK CARGO COMPT BILGE AREA STA1540 STRINGER 38L INTERIM REPAIRED AS PER ECRA 5361-01114 REV - PART 1 ATTCH FORM 44-0008 ITEM 1 Jun 14, 2023 · N649UA · Boeing 767322SDR CALA2023061601870Skin · corrodedB767-53-3-7058 AFT OF BULK CGO BILGE STA 1540 S39 POS INNER SKIN FOUND CORROSION TRANSFER REF HXWO 1856087 AND ORIGINATED BY EMP V896810 FUSELAGE STA1540-STA1562 BETWEEN STR39L AND STR39R SKIN INTERIM REPAIRED AS PER ECRA5361-01114 REV - PART 1 ATTACH FORM 44-Jun 14, 2023 · N649UA · Boeing 767322SDR CALA2023061601869Stringer · corrodedB767-53-3-7058 AFT OF BULK CGO BILGE STA1540 TO STA1562 S39L STRINGER FOUND CORROSION TRANSFER REF HXWO 1856237 AND ORIGINATED BY EMP V896810 BULK CARGO COMPT BILGE AREA STA1540 TO STA1562 STRINGER 39L INTERIM REPAIRED AS PER ECRA 5361-01114 REV - PART 1 ATTACJun 14, 2023 · N649UA · Boeing 767322SDR CALA2023061601865Skin · unknownHOLE IN LEFT AFT FUSELAGE HIT BY CATERING TRUCK UPDATED WITH PHOTOS REMOVED APU AS PER AMM 49-11-00 FOR MX PURPOSE. ADD EMP:U352816,U393377 TRANSFERED APU REMOVAL TO L/P 4785718. PERFORMED VISUAL INSPECTION PER STEPS 1 THROUGH 5 OF AVO 10857 REV A. MEASUREMENJun 14, 2023 · N79541 · Boeing 737824SDR AALA202306211381Unknown · wornAIRCRAFT IN BASE MAINTENANCE: WEAR DAMAGE ON WING CENTER SECTION, ENVIRONMENTAL CONTROL SYSTEMS ACCESS DOOR LATCH, STRIKER PLATE CHORD LOCATED AT BS 545 AND RBL 40.9. REPAIRED CHORD PER SRM 57-10-13-2R-3.Jun 14, 2023 · N950NN · Boeing 737823SDR JJBA20230620018Unknown · unknownCRACKS SUSPECTED (9X) ON RH SKIN AROUND FASTENERS BTW FR 77-80 BTW STR 3R-9R. SKIN REPAIRED WITH 2 DOUBLERS AND 7 BUSHINGSJun 14, 2023 · N14177 · Emb EMB145XRSDR YENA2023061600657Unknown · unknownDURING HEAVY MAINTENANCE: CRACK INTERNAL STRUCTURE SECTION CONNECTION LOCATED FR 66 LEVEL STRINGER 23L AT AFT GALLEY AREA: REF. AERO NR 2023-252550 - R&R NEW STRUCTURE SECTION CONNECTION LOCATED FR66 LEVEL STRINGER 23L AT AFT GALLEY AREA I.A.W A320 SRM 51-72-1Jun 14, 2023 · N568JB · Airbus A320232SDR YENA2023061600656Unknown · unknownDURING HEAVY MAINTENANCE: CRACK INTERNAL STRUCTURE SECTION CONNECTION LOCATED FR66 LEVEL STRINGER 23R AT AFT GALLEY AREA; REF. AERO NR 2023-252552- R&R INTERNAL STRUCTURE SECTION CONNECTION LOCATED FR66 LEVEL STRINGER 23R AT AFT GALLEY AREA IAW A320 SRM 51-42-Jun 14, 2023 · N568JB · Airbus A320232SDR YENA2023061600655Unknown · unknownDURING HEAVY MAINTENANCE: CRACK: SHEAR PLATE STR23L AT FR69-70 AFT GALLEY; REF AEROMAN NR 2023-252548 W/O:2023 200/1: R & R SHEAR PLATE STR23L AT FR69-70 AFT GALLEY AREA IAW SRM 51-72-11, 51-42-11, AND DWG D53470100.Jun 14, 2023 · N568JB · Airbus A320232SDR YENA2023061600654Unknown · unknownDURING HEAVY MAINTENANCE: CRACK: FASTENER HOLE FR35 FWD FACE AT LEVEL OF THE STR30L. L=0.500"; REF AEROMAN NR 2023-252426 W/O: 2023 200/1: REPAIRED CRACK @ FR35 PRESSURE BULKHEAD WEB AND STR30L IAW EA53-0169-23, RDAF 81219770/004/2023#A, PARTS 1 AND 2, DWG R53Jun 14, 2023 · N568JB · Airbus A320232SDR YENA2023061600653Unknown · unknownDURING HEAVY MAINTENANCE: CRACK: FR16RH DOOR STOP FITTING #7 INBD. UPPER 7 O'CLOCK DIRECTION LOOKING FORWARD; REF AEROMAN NR 2023-252292 W/O:2023 200/1: R & R INTERCOSTAL FITTING ON FR16RH DOOR STOP FITTING #7 IAW SRM 53-11-12-300-010, 51-72-11, 51-42-11, AND Jun 14, 2023 · N568JB · Airbus A320232SDR YENA2023061600652Unknown · unknownDURING HEAVY MAINTENANCE: CRACK: FR16RH DOOR STOP FITTING #7 LOWER INBD FASTENER HOLE 11 O'CLOCK LOOKING FORWARD; REF AEROMAN NR 2023-252293 W/O:2023 200/1: R & R INTERCOSTAL FITTING ON FR16RH DOOR STOP FITTING #7 IAW SRM 53-11-12-300-010, 51-72-11, 51-42-11, Jun 14, 2023 · N568JB · Airbus A320232SDR YENA2023061600651Unknown · unknownDURING HEAVY MAINTENANCE: CRACK: OPEN HOLE #5 LOCATED ON FR16RH. CRACK DIRECTION 6 O'CLOCK; REF AEROMAN NR 2023-252299 W/O:2023 200/1: PERFORMED REPAIR HOLE #5 FR16RH IAW JETBLUE EC A23-436-01, DWG R53-13041, EA 53-0212-23 REV 0, AND AIRBUS RDAF 81229902/003/2Jun 14, 2023 · N568JB · Airbus A320232SDR YENA2023061600650Unknown · unknownDURING HEAVY MAINTENANCE: CRACK: RH CONTINUITY FITTING LOCATED ON WINDSHIELD CENTER LOWER NODE AT FR2. L=0.100"; REF AEROMAN NR 2023-252241 W/O:2023 200/1: ACCOMPLISHED REPAIR ON RH CONTINUITY FITTING WINDSHIELD CENTER LOWER NODE AT FR2 IAW AEROMAN EA 53-0159-Jun 14, 2023 · N568JB · Airbus A320232SDR YENA2023061600649Unknown · unknownDURING HEAVY MAINTENANCE: CRACK: UPPER FASTENER LOCATED ON RH WINDSHIELD FRAME CENTER LOWER NODE INTERNAL SIDE. L+0.100"; REF AEROMAN NR 2023-252242 W/O:2023 200/1: ACCOMPLISHED REPAIR UPPER FASTENERS RH WINDSHIELD CENTER LOWER NODE INTERNAL SIDE IAW AEROMAN EJun 14, 2023 · N568JB · Airbus A320232SDR YENA2023061600648Unknown · unknownDURING HEAVY MAINTENANCE: CRACK: UPPER FASTENER LOCATED ON LH WINDSHIELD FRAME CENTER LOWER NODE INTERNAL SIDE. L=0.100"; REF AEROMAN NR 2023-252243 W/O:2023 200/1: ACCOMPLISHED REPAIR UPPER FASTENERS LH WINDSHIELD FRAME CENTER LOWER NODE INTERNAL SIDE IAW AERJun 14, 2023 · N568JB · Airbus A320232SDR YENA2023061600647Unknown · unknownDURING HEAVY MAINTENANCE: CRACK: LOWER RADIUS RH WINDSHIELD FRAME CENTER LOWER NODE INTERNAL SIDE. L=0.400"; REF AEROMAN NR 2023-252244 W/O:2023 200/1: ACCOMPLISHED REPAIR LOWER RADIUS RH WINDSHIELD FRAME CENTER LOWER NODE INTERNAL SIDE IAW AEROMAN EA 53-0159-Jun 14, 2023 · N568JB · Airbus A320232SDR YENA2023061600646Unknown · unknownDURING HEAVY MAINTENANCE: CORROSION INTERNAL STRUCTURE AREA CENTER TANK LOCATED FR41 TO FR42 LH SIDE IN PASSENGER CABIN (CPCP-RELATED MPD TASK 533135-01); PERFORMED REPAIR AT INTERNAL STRUCTURE AREA CENTER TANK LOCATED FR41 TO FR42 LH SIDE IN PASSENGER CABIN IJun 14, 2023 · N568JB · Airbus A320232SDR YENA2023061600643Unknown · unknownDURING HEAVY MAINTENANCE: CORROSION SHEAR TIE LOC. BTW STRINGER 42R AND 43R AT LEVEL OF FRAME 29 IN FWD CARGO COMPARTMENT (CPCP RELATED MPD TASK 532180-01); REF TO AEROMAN W/O 2023 200/1 NR 2023-252559. REMOVED AND REPLACED SHEAR TIE LOC. BTW STRINGER 42R AND Jun 14, 2023 · N568JB · Airbus A320232SDR YENA2023061600642Unknown · unknownDURING HEAVY MAINTENANCE: CORROSION SHEAR PLATE LOCATED FR69 TO FR70 STR 23RH SIDE AT AFT GALLEY AREA (RELATED MPD TASK 534195-01); REF TO AEROMAN W/O 2023 200/1 NR 2023-252546. REMOVED AND REPLACE SHEAR PLATE LOCATED FR69 TO FR7D STR 23RH SIDE AT AFT GALLEY AJun 14, 2023 · N568JB · Airbus A320232SDR YENA2023061600641Unknown · unknownDURING HEAVY MAINTENANCE: CORROSION SHEAR TIE LOC. BTW STRINGER 41R AND 42R AT LEVEL OF FRAME 27 IN THE FWD CARGO COMPARTMENT (CPCP RELATED MPD TASK 532180-01); REF TO AEROMAN W/O 2023 200/1 NR 2023-252563. REMOVED AND REPLACED SHEAR TIE LOC. BTW STRINGER 41R Jun 14, 2023 · N568JB · Airbus A320232SDR YENA2023061600640Unknown · unknownDURING HEAVY MAINTENANCE: CORROSION SHEAR TIE LOC. BTW STRINGER 42R AND 43R AT LEVEL OF FRAME 28 IN FWD CARGO COMPARTMENT (CPCP RELATED MPD TASK 532180-01); REF TO AEROMAN W/O 2023 200/1 NR 2023-252562. REMOVED AND REPLACED SHEAR TIE LOC. BTW STRINGER 42R AND Jun 14, 2023 · N568JB · Airbus A320232SDR YENA2023061600639Unknown · unknownDURING HEAVY MAINTENANCE: CORROSION SHEAR TIE LOC. BTW STRINGER 40R AND 41R AT LEVEL OF FRAME 31 IN FWD CARGO COMPARTMENT (CPCP RELATED MPD TASK 532180-01); REF TO AEROMAN W/O 2023 200/1 NR 2023 252557. REMOVED AND REPLACED SHEAR TIE LOC. BTW STRINGER 40R AND Jun 14, 2023 · N568JB · Airbus A320232SDR YENA2023061600638Unknown · unknownDURING HEAVY MAINTENANCE: CORROSION SHEAR TIE LOC. BTW STRINGER 41R AND 42R AT LEVEL OF FRAME 30 IN FWD CARGO COMPARTMENT (CPCP RELATEDMPD TASK 532180-01); REF TO AEROMAN W/O 2023 200/1 NR 2023-252556. REMOVED AND REPLACED SHEAR TIE LOC. BTW STRINGER 41R AND 4Jun 14, 2023 · N568JB · Airbus A320232SDR YENA2023061600637Unknown · unknownDURING HEAVY MAINTENANCE: CORROSION SHEAR TIE LOC. BTW STRINGER 41R AND 42R AT LEVEL OF FRAME 31 IN THE FWD CARGO COMPARTMENT (CPCP RELATED MPD TASK 532180-01); REF TO AEROMAN W/O 2023 200/1 NR 2023-252541. REMOVED AND REPLACED SHEAR TIE LOC. BTW STRINGER 41R Jun 14, 2023 · N568JB · Airbus A320232
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