JASC 5310

Service difficulty reports · 38,519

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 AALA202602276737Door Sill · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT HAND AFT ENTRY WAY LOWER SILL INNER CHORD (CREASE ANGLE) AT STA 979, LBL 53. REPLACED INNER CHORD PER AARD 51-00-05-1.Feb 9, 2026 · N983AN · Boeing 737823SDR AALA202602234945Fitting · gougedAIRCRAFT IN BASE MAINTENANCE: AFT ENTRY DOOR FUSELAGE CUTOUT STRUCTURE AFT SIDE FRAME-MOUNTED CENTERING TRACK FITTING HAS A GOUGE AT THE LOWER SIDE. REMOVED AND REPLACED AFT ENTRY DOOR FUSELAGE CUTOUT STRUCTURE AFT SIDE FRAME MOUNTED CENTERING TRACK FITTING THFeb 9, 2026 · N989AN · Boeing 737823SDR 2026FA0000109Stiffener · crackedFUSELAGE AFT LWR SKIN, STIFFENER CRACKED. REPLACED WITH FACTORY NEW STIFFENER.Feb 9, 2026 · N472TA · Piper PA28181SDR DALA2026021000958Bracket · damagedFRAME 40.1, LH SIDE, STRINGER 7, TOOLING DAMAGE ON BRACKET. REPAIRED PER ERA 631888-14, REV'S 0. (1443595)Feb 9, 2026 · N861NW · Airbus A330223SDR REXA2026080301403Drain Pan · crackedCRACK AND BEND LEFT AND RIGHT DRAIN PAN AT AFT EQUIPMENT COMPARTMENT. LEFT AND RIGHT DRAIN PAN AT AFT EQUIPMENT COMPARTMENT WERE REPAIRED PER CRJ/700 SRM 51-71-59-001-001-A01 AND CRJ/700 SRM 51-25-16-001-001-A01Feb 8, 2026 · N398CA · Cndair CL6002C10SDR REXA2026080301402Drain Pan · crackedCRACK AND BEND LEFT AND RIGHT DRAIN PAN AT AFT EQUIPMENT COMPARTMENT. LEFT AND RIGHT DRAIN PAN AT AFT EQUIPMENT COMPARTMENT WERE REPAIRED PER CRJ/700 SRM 51-71-59-001-001-A01 AND CRJ/700 SRM 51-25-16-001-001-A01Feb 8, 2026 · N398CA · Cndair CL6002C10SDR AALA202603091575Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON CORNER FITTING LOCATED AT FR68 AT LEVEL STR 23RH AFT GALL EY AREA MEASURES OF CORROSION ARE: L=4.394IN, W= 1.039IN; D= 0.009IN. MAINTENANCE REPLACED CORNER FITTING AND FASTENERS LOCATED BTW FR68 AT LEVEL STR 23RH AFTFeb 8, 2026 · N9006 · Airbus A319115SDR ABXA20260208063Failsafe · not reportedDURIING C6 CHECK, ON WO 15843154, REPAIRED RH FAILSAFE TRIM-OUT AND RE-ASSEMBLY, STA. 955 IAW ABX-EA-5350-0014-0013. (RH FAILSAFE) AND AMES DOC. 47207ORD04. C6 CHECK COMPLETED AND AIRCRAFT RETURNED TO SERVICE.Feb 8, 2026 · N1229A · Boeing 767306SDR ABXA20260208062Failsafe · not reportedDURIING C6 CHECK, ON WO 15843154, REPAIRED THE LT FAILSAFE TRIM-OUT AND RE-ASSEMBLY, BS 955 IAW EA-5350-0013-0013. LT FAILSAFE AND AMES DOC. 47207ORD03. C6 CHECK COMPLETED AND AIRCRAFT RETURNED TO SERVICE.Feb 8, 2026 · N1229A · Boeing 767306SDR YENA2026021100191Skin · dentedDURING HEAVY MAINTENANCE: DENT EXTERNAL SKIN DOOR 812 AT LOWER FUSELAGE; (RESOLVED ON W/O: 1425349 TASKCARD: NR-00009) REF AEROMAN WO # 2025=414/1 NR # 2025-717302 EVALUATED DENT ON EXTERNAL SKIN DOOR 812 AT LOWER FUSELAGE AND FOUND WITHIN LIMITS I.A.W A320 SRFeb 8, 2026 · N613JB · Airbus A320232SDR YENA2026021100185Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 68 LH SIDE IN OPEN FASTENER HOLE LOWER INBOA RD AT DOOR STOP FITTING 1 POSITION, CRACK DIRECTION IS 6 OCLOCK, CRACK DEPTH IS 0.105 INCH, AT AFT GALLEY AREA (1 EA); (RESOLVED ON W/O: 1425349 TASKCARD: NR-00038Feb 8, 2026 · N613JB · Airbus A320232SDR YENA2026021100184Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 68 RH SIDE IN OPEN FASTENER HOLE LOWER INBOA RD AT DOOR STOP FITTING 5 POSITION, CRACK DIRECTION IS 7 OCLOCK, CRACK DEPTH IS 0.090 INCH, AT AFT GALLEY AREA (1 EA); (RESOLVED ON W/O: 1425349 TASKCARD: NR-00039Feb 8, 2026 · N613JB · Airbus A320232SDR YENA2026021100182Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 66 RH SIDE IN OPEN FASTENER HOLE UPPER INBO ARD AT DOOR STOP FITTING 3 POSITION, CRACK DIRECTIONS ARE 1 AND 6 OCLOCK, CRACK DEPTH IS 0.095 INCH, AT AFT GALLEY AREA (2 EA); (RESOLVED ON W/O: 1425349 TASKCARD: Feb 8, 2026 · N613JB · Airbus A320232SDR YENA2026021100181Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 66 RH SIDE IN OPEN FASTENER HOLE UPPER INBO ARD AT DOOR STOP FITTING 3 POSITION, CRACK DIRECTIONS ARE 1 AND 6 OCLOCK, CRACK DEPTH IS 0.095 INCH, AREA 2 FOR PURPOSE OF TRACKING; (RESOLVED ON W/O: 1425349 TASKCFeb 8, 2026 · N613JB · Airbus A320232SDR YENA2026021100180Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 66 RH SIDE IN OPEN FASTENER HOLE UPPER INBO ARD AT DOOR STOP FITTING 3 POSITION, CRACK DIRECTIONS ARE 1 AND 6 OCLOCK, CRACK DEPTH IS 0.095 INCH, AREA 3 FOR PURPOSE OF TRACKING; (RESOLVED ON W/O: 1425349 TASKCFeb 8, 2026 · N613JB · Airbus A320232SDR YENA2026021100177Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 68 RH SIDE IN OPEN FASTENER HOLE LOWER INBOA RD AT DOOR STOP FITTING 1 POSITION, CRACK DIRECTIONS ARE 12 AND 6 OCLOCK, CRACK DEPTH IS 0.115 INCH, AT AFT GALLEY AREA (2 EA); REF AEROMAN N/R 2025-717397, ACCOMPFeb 8, 2026 · N613JB · Airbus A320232SDR YENA2026021100176Window Frame · crackedDURING HEAVY MAINTENANCE: CRACK FOUND ON UPPER RADIUS OF WINDSHIELD CENTER POST LOWER ATTACHMENT AREA RH SIDE. CRACK L= 0.109 INCH. CRACK DIRECTION 11 O CLOCK; REF AEROMAN N/R 2025-717306, ACCOMPLISHED THE PERMANENT REPAIR OF THE CRACKS ON THE WINDSHIELD FRAMIFeb 8, 2026 · N613JB · Airbus A320232SDR YENA2026021100175Window Frame · crackedDURING HEAVY MAINTENANCE: CORROSION UPPER SURFACE TRAILING EDGE LOWER AREA OF SKINAT LEVEL RIB 15 ON RH WING; REF AE WO # 2025-414/1 NR # 2025-716959 ACCOMPLISHED PERMANENT REPAIR ON RH WING/TOP SKIN PANEL 2 / TEOH LWR SURFACE / RIB 15 I.A.W EA 57-0135-25(COVEFeb 8, 2026 · N613JB · Airbus A320232SDR YENA2026021100170Door Frame · crackedDURING HEAVY MAINTENANCE: FUSELAGE/ REAR FUSELAGE/ FR68 RH DOOR STOP FITTING #1/ CRACK/ PERMANENT REPAIR; REFERENCES: /1/ AEROMAN EA 53-0101-25 (COVER, PART 1+2) /2/ AIRBUS DOSSIER 81714674 /3/ AIRBUS RDAF 81714674/003/2025#A /4/ A320 SRM 53-41-12-300-011. DESFeb 8, 2026 · N613JB · Airbus A320232SDR YENA2026021100168Window Frame · crackedDURING HEAVY MAINTENANCE, WINDSHIELD FRAME CENTER POST, LOWER NODE AREA CRACKED. REFERENCE: EA 53-0097-25, SB A320-53-1331, RDAF 81709993/003/2025 A, MESSAGE 81709993/010, REPAIR INSTRUCTION R53113430, ISSUE G, REPAIR INSTRUCTION R53112919 ISSUE K, REPFeb 8, 2026 · N613JB · Airbus A320232SDR DALA2026020900910Door Frame · puncturedPUNCTURED BULKHEAD DOOR JAM AT LOWER SECTION AT Y= 1053, X= 7 APPROX AFT ACCESSORY BAY. REPAIRED IAW SRM 51-70-10. (1442140)Feb 8, 2026 · N949AT · Boeing 717200SDR AALA202604289710Door Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK EMERGENCY EXIT DOOR 833 ON LOAD TRANSMITTING PROFIL R/H SIDE IN PASSENGER CABIN. LENGTH OF CRACK IS= 0.562 INCH. MAINTENANCE REPLACED LOAD TRANSMITTING PROFILE R/H SIDE (SEGMENT FWD) AND BEAM 1 AND ACCOMPLISHED MODIFY ON EMFeb 7, 2026 · N653AW · Airbus A320232SDR AALA202604288846Door Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK EMERGENCY EXIT DOOR 844 ON VERTICAL FRAME INTERNAL AREA IN PASENGER CABIN. MAINTENANCE REPLACED LOAD TRANSMITTING (FWD AND AFT SEGMENT) AND UPPER BEAM 1, AND ACCOMPLISHED MODIFY OVERWING EMERGENCY EXIT DOOR 844, IAW EO# 5210Feb 7, 2026 · N653AW · Airbus A320232SDR SWAA2026022468868Stub Frame · crackedCRACK FOUND R1 DOOR STUB FRAME, .1 INCH ABOVE SEAL DEPRESSOR, BS 291.5 +10, L: .3 INCHES. REMOVED AND REPLACED THE R1 DOOR STUB FRAME IAW SRM 51-40-02.Feb 7, 2026 · N948WN · Boeing 7377H4SDR CALA2026021013654Door Sill · corrodedR1 DOOR LOWER SILL UPPER SKIN ATTACH ANGLE BTWN BS 324 - 365 CORRODED. REMOVED AND REPLACED THE ANGLE ON TRAVELER#T26/1849387 AND HEAT TREATED TO T42 IAW SRM 51-40-02-0G-0, & DWG 141N8422-41.Feb 7, 2026 · N57869 · Boeing 75733NSDR CALA2026021013653Door Sill · corrodedFWD CARGO DOOR CUTOUT STRUCTURE LOWER SILL PLATE AT S26R CORRODED. REMOVED AND INSTALLED A NEW FWD CARGO DOOR CUTOUT LOWER PLATE IAW SRM 51-40-02, & DWG 143A8120.Feb 7, 2026 · N35236 · Boeing 737824SDR SWAA2026031668561Crossbeam · crackedCRACK ON BRAKE PANEL LOCATED BS 540 BTW BL 0 TO LBL 24.75 WL 208.1 AT PASSENGER CABIN. REPLACED BRAKE PANEL LOCATED BS 540 BTW BL 0 TO LBL 24.75 WL 208.1 AT PASSENGER CABIN IAW B737-800 SRM- 51-40-02 AND DRAWING 143A0060 SHEET 64 REV - .Feb 6, 2026 · N8629A · Boeing 7378H4SDR SWAA2026031668560Crossbeam · crackedCRACK ON BRAKE PANEL LOCATED BS 540 BTW BL 0 TO RBL 24.75 WL 208.1 AT PASSENGER CABIN. REPLACED BRAKE PANEL LOCATED BS 540 BTW BL 0 TO RBL 24.75 WL 208.1 AT PASSENGER CABIN IAW SRM- 51-40-02 AND DRAWING 143A0060 SHEET 64 REV -.Feb 6, 2026 · N8629A · Boeing 7378H4SDR AALA202602265218Door Sill · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON R2 ENTRY LOWER SILL INNER CHORD (CREASE ANGLE) BETWEEN BS 947 AND BS 992 AT RBL 54. REPLACED INNER CHORD PER AARD 51-00-05-1.Feb 6, 2026 · N910AN · Boeing 737823SDR DALA2026020900939Doubler · corrodedCORROSION FOUND ON WASTE BOX INTERNAL DOUBLER. C/W ER/A 608712-14, REV A, SECTION IV. (LP# 1439003)Feb 6, 2026 · N134DU · Airbus BD5001A10SDR AALA202602062537Keel Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON KEEL BEAM LATTICE FITTING AT STA 880 FROM LBL 12 TO RBL 12. REPLACED LATTICE FITTING PER DWG 45024110-509.Feb 6, 2026 · N828AA · Boeing 7879SDR REXA2026080301384Landing · cracked"CRACK ON AFT RH DOOR LANDING AT FS 188.00 (LATCH CUT OUT OF ACCESS DOOR 212AR) RH DOOR LANDING AT FS 188.00 (LATCH CUT OUT OF ACCESS DOOR 212AR) WAS MANUFACTURED PER EA NO: CRJ953-21561 REV IR, DWG CC670-33151-6 REV ""D"", AND REPLACED PER CRJ 900 SRM 51-42-0Feb 5, 2026 · N918XJ · Cndair CL6002D24SDR VNAA20260511010Door Frame · corrodedCOCKPIT DOOR POST IS CORRODED AT RBL 11 W.L.72.5. REPAIRED RBL 11 COCKPIT DOOR POST IAW BOMBARDIER GREO 670-53-11-745 REV -A DATED 2016-10-28.Feb 5, 2026 · N512AE · Cndair CL6002C10SDR AALA202604287088Window Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND LOCATED ON UPPER TENSION BOLT, WINDSHIELD CENTER POST LH SIDE. CRACK DIRECTION: 1 OCLOCK (VIEW ON LH SIDE), CRACK LEN GHT= 0.200 INCH APPROX, AD-2020-17-03. MAINTENANCE ACCOMPLISHED TIME LIMITED REPAIR INSTFeb 5, 2026 · N653AW · Airbus A320232SDR AALA202604284966Window Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND LOCATED ON UPPER TENSION BOLT, WINDSHIELD CENTER POST LH SIDE. CRACK DIRECTION: 1 OCLOCK (VIEW ON LH SIDE), CRACK LEN GHT= 0.200 INCH APPROX, AD-2020-17-03. MAINTENANCE ACCOMPLISHED TIME LIMITED REPAIR INSFeb 5, 2026 · N653AW · Airbus A320232SDR SWAA2026030968011Door Frame · crackedCRACKED DOOR FRAME, BS 312, STR 5L - STR 6L. PERFORMED A REPAIR ON THE DOOR FRAME IAW EA NM-22-153-01244, REV B.Feb 5, 2026 · N8628A · Boeing 7378H4SDR SWAA2026022468046Pressure Deck · crackedCRACK FOUND ON MID PASSENGER CABIN HORIZONTAL PRESSURE DECK AT RBL 43, BS 663 +1, LENGTH: .27'. PERFORMED REPAIR AT HORIZONTAL PRESSURE DECK BETWEEN BS 663 - 675, RBL 30 - RBL 65 IAW SRM 53-40-51-2R-2, REP 2. 02] REJECTION OF CORRECTIVE ACTION 1: EXTERIOR Feb 5, 2026 · N948WN · Boeing 7377H4SDR JJBA20260217041Block · corrodedUPON REMOVAL OF RT WHEEL WELL AFT RIB FOUND RADIUS BLOCK CORRODED. REPLACED 1 EACH REPLACEMENT RADIUS FILLER ONTO 1 EACH RIB.Feb 5, 2026 · N14168 · Emb EMB145XRSDR UIEA2026020500034Spar Web · corrodedDAMAGE ON CENTER WING REAR SPAR WEB RH SIDE NEAR JETTISON PUMP AT STA 1240 RBL 93. ACCOMPLISHED EI T2026A57M-110 REV 1. JOB COMPLETED AND CONDITION CHECK GOOD.Feb 5, 2026 · N481MC · Boeing 747443SDR UIEA2026020500035Door Frame · crackedPERFORM SB 4453A356 PART 1-3, FOUND CRACK HOLE AT DOOR NR 2 LH FWD EDGE FRAME, BS 800 S16L AREA. PERFORM EI T2026A53M-162 REV 0. ACCOMPLISH EI T2026A53M-162 REV 1. NO FURTHER DEFECTS NOTED.Feb 5, 2026 · N481MC · Boeing 747443SDR FDEA202602050135Frame · unknownEXISTING REPAIR ON FUSELAGE FRAME AT FR28 BETWEEN STGR8LH AND STGR12LH REQUIRES EVALUATION FOR CONFORMITY. EVALUATED AND NO RECORD FOUND. REMOVED THE EXISTING REPAIR AND RE-REPAIRED THE FRAME PER EA 6-5310-T0386358. TITLE: FUSELAGE - MAINFRAME - EXISTINFeb 5, 2026 · N658FE · Airbus A300F4605RSDR VNAA20260326002Channel · corrodedCORROSION ON TWO NUT CHANNELS OF LT & RT P-SEALS OF BODY FARING PANELS AT MLG WW. THE NUT CHANNELS WERE REMOVED IAW SRM 51-21-06-001-001-A01, EVALUATED, AND FOUND OUT OF LIMITS IAW SRM 53-00-00-101-001-A01. REPLACED IAW SRM 51-41-02-001-001-A01.Feb 4, 2026 · N642NN · Bombdr CL6002D15SDR SWAA2026030367560Crossbeam · crackedCRACKED CROSSBEAM, BS 540, LBL 1. REPLACED CROSSBEAM IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 143A0060, SHEET 46, REV -. MEASUREMENT OF CRACK: L= 0.885 INCH.Feb 4, 2026 · N7731A · Boeing 73776NSDR SWAA2026030367561Crossbeam · crackedCRACKED CROSSBEAM, BS 540, RBL 1. REPLACED CROSSBEAM IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 143A0060, SHEET 46, REV -. MEASUREMENT OF CRACK:: L= 0.889 INCH.Feb 4, 2026 · N7731A · Boeing 73776NSDR SIMA2026022404002Seal Rest · corrodedSSI 53-21-009: FWD CARGO DOOR LOWER FUSELAGE CUTOUT/ SEAL DEPRESSOR HAS CORROSION AT THE LOWER NUT PLATE HOLES. (MAJOR REPAIR) (LEVEL 2 CORROSION). REMOVED AND REPLACED FWD CARGO DOOR LOWER FUSELAGE CUTOUT SEAL DEPRESSOR IAW ERJ 170 SRM 51-40-08 AND AMM 20-10-Feb 4, 2026 · N770JM · Emb ERJ170100LRSDR IPXA2026021241625Deck Plate · corrodedMAIN CABIN FLOOR STRUCTURE, DECK PLATE STA 1700-1720 BL0 -RBL 50 HAS 15EA AREAS WITH CORROSION. REMOVED CORROSION IN 15 AREAS. MAIN CABIN FLOOR STRUCTURE, DECK PLATE BS 1700-1720, BL0 -RBL 50.IAW SRM 51-10-02 TABLE 101. RESTORED SURFACE PROTECTION IAW.SRM 5Feb 4, 2026 · N460UP · Boeing 75724APFSDR AALA202602096039Crossbeam · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN PASSENGER CABIN FLOOR SUPPORT BREAK ASSEMBLY PANEL AT BS 540, RBL 2. REPLACED BREAK ASSEMBLY PANEL PER AARD 51-00-05-1.Feb 4, 2026 · N950NN · Boeing 737823SDR IXXA20260204001Support Angle · crackedMCD AFT SEAL SUPPORT ANGLE CRACKED.Feb 4, 2026 · N389AZ · Boeing 767319SDR 2026FA0000081Window Frame · corrodedRIGHT WINDOW FRAME BETWEEN BS 544 AND 566, CORRODED.Feb 4, 2026 · N342CM · Boeing 76735DSDR 2026FA0000080Window Frame · corrodedRIGHT WINDOW FRAME BETWEEN BS 522 AND 544, CORRODED.Feb 4, 2026 · N342CM · Boeing 76735D
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