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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR DALA2025122909460Door Frame · crackedFOUND TWO CRACKS ON THE AFT CARGO DOOR FRAME 61 - FRAME FORK AREA, ONE CRACK ON THE FRAME FORK AREA H-5, ANOTHER CRACK ON THE FRAME FORK AREA H-6. CORRECTIVE ACTION: FR61 FRAME FORK REPLACEMENT AS PER CARD 5230- 01164-08 REV MAY 09 2025 AND CARD 5230-01164-10 SDR REXA2026073101368Door Sill · corrodedSILL WITH CORROSION, LOWER PART OF CARGO COMPARTMENT DOOR FRAME AFT DUE TO EXCESS OF DAMAGE LOWER SILL OF CARGO COMPARTMENT DOOR FRAME AFT, WAS REPLACED PER CRJ-900 SRM 53-61-23-201-001-A01, CRJ-900 SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01 AND SRM 5SDR SWIA2025122775789Window Frame · crackedCO-PILOT WINDSHIELD OUTBOARD POST LOWER OUTBOARD CLIP IS VISIBLY CRACKED. REPLACED CRACKED CO-PILOT WINDSHIELD OUTBOARD POST LOWER OUTBOARD CLIP WITH NEW CLIP. IAW SRM 51-42-21-00 REV. 39 AND DWG 601R33007 REV -U.SDR SWIA2025122775787Window Frame · crackedPILOT WINDSHIELD OUTBOARD POST LOWER OUTBOARD CLIP IS VISIBLY CRACKED. REMOVED AND REPLACED WITH 1 EA OF NEW PILOT WINDSHIELD OUTBOARD POST LOWER OUTBOARD CLIP REF. SRM 51-42-21 AND DWG 601R33007 REV -U.SDR YENA2025123001312Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 66 RT IN OPEN FASTENER HOLE UPPER INBO ARD AT DOOR STOP FITTING 7 POSITION, CRACK DIRECTION IS 6 OCLOCK, CRAC K DEPTH IS 0.105 INCH APPROX, AT AFT GALLEY AREA (1 EA); REF AEROMAN WO 2025 278/1 NR 2025-622954 SDR YENA2025123001311Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 68 RH SIDE IN OPEN FASTENER HOLE LOWER INBO ARD AT DOOR STOP FITTING 1 POSITION, CRACKDIRECTION IS 12 OCLOCK, CRA CK DEPTH IS 0.095 INCH APPROX, AT AFT GALLEY AREA (1 EA); (RESOLVED ON W/O: 1409520 TASKCARD: SDR YENA2025123001304Window Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 2 WINDSHIELD CENTER POST LOWER ATTACHMENT C ONTINUITY FITTING RH SIDE, CRACK LENGTH IS 0.200 INCH APPROX, IN COCKP IT (1 EA); REF AEROMAN WO 2025 278/1 NR 2025-622906 PERFORMED REPAIR IAW AEROMAN EA 53-0068-2SDR YENA2025123001303Window Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 2 WINDSHIELD CENTER POST LOWER ATTACHMENT IN TERNAL AREA, LH SIDE, FROM UPPER TENSION BOLT, CRACK DIRECTION IS 2 OC LOCK, CRACK LENGTH IS 0.105 INCH APPROX, IN COCKPIT (1 EA); RESOLVED ON W/O: 1409520 TASKCARSDR YENA2025123001302Window Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 2 WINDSHIELD CENTER POST LOWER ATTACHMENT IN TERNAL AREA, LOWER INBOARD CORNER, LH SIDE, CRACK LENGTH IS 0.230 INCH APPROX, IN COCKPIT (1 EA); (RESOLVED ON W/O: 1409520 TASKCARD: NR-00050) REF AEROMAN WO 2025SDR YENA2025123001301Window Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 2 WINDSHIELD CENTER POST LOWER ATTACHMENT IN TERNAL AREA, LOWER INBOARD CORNER, RHSIDE, CRACK LENGTH IS 0.080 INCH APPROX, IN COCKPIT (1 EA); REF AEROMAN WO 2025 278/1 NR 2025-622907 PERFORM PERMANENT REPAIRSDR YENA2025123001294Pressure Deck · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION FOUND AT FASTENER HOLE, LOCATED AT PRESSURE DECK MEMBRANE TO CENTER BOX AREA, ON FR 36, Y1292 + 9 INCHES TO OTBD, LT SIDE, CRACK DIRECTION IS 12 OCLOCK LOOKING AFT, CRACK DEPTH IS 0.089 INCH REF AEROMAN NR 2025-62326SDR YENA2025123001293Pressure Deck · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FASTENER HOLE LOCATED AT PRESSURE DECK MEMBRANE TO ENTER BOX AREA, ON FR36 AND -Y1292 PLUS 6 INCHES TO OUTBOARD, RH SIDE, CRACK DIRECTION IS 1 OCLOCK LOOKING AFT, CRACK DEPTH IS 0.115 INCH; REF AEROMAN NR 202SDR YENA2025123001292Pressure Deck · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FASTENER HOLE LOCATED AT PRESSURE DECK MEMBR ANE TO CENTER BOX AREA, ON FR36AND Y1292 PLUS 4 INCHES TO OUTBOA RD, LH SIDE, CRACK DIRECTION IS 12 OCLOCK LOOKING AFT, CRACKK DEPTH IS 0.184 INCH; REF AEROMAN NR SDR YENA2025123001291Pressure Deck · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FASTENER HOLE LOCATED AT PRESSURE DECK MEMBR ANE TO CENTER WING BOX AREA, ON FR36 AND Y1292 PLUS 5 INCHES TO OUTBOA RD, LH SIDE, CRACK DIRECTION IS 12 OCLOCK LOOKING AFT, CRACK DEPTH IS 0.119 INCH; REF AEROMASDR YENA2025123001290Pressure Deck · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FASTENER HOLE LOCATED AT PRESSURE DECK MEMBR ANE TO CENTER WING BOX AREA, ON FR3 AND -Y1292 PLUS 2 INCHES TO OUTBO ARD, RH SIDE, CRACK DIRECTION IS 12 OCLOCK LOOKING AFT, CRACK DEPTH IS 0.109 INCH; REF AEROMASDR YENA2025123001287Door Sill · corrodedDURING HEAVY MAINTENANCE: CORROSION LOWER SILL DOOR LOC AFT POSITION ON BULK CARGO COMPARTMENT ( CPCP FINDING); REF AEROMAN WO 2025 278/1 NR 2025-623038 REMOVED AND REPLACED DOOR SILL BEAM LOCATED BTW FR60 THRU FR62, AT LEVEL STR38R, IN BULK CARGO COMPARTMENT SDR YENA2025123001283Window Frame · crackedDURING HEAVY MAINTENANCE: FUSELAGE / NOSE FWD FUSELAGE / WINDSHIELD FRAME / CENTER POST LOWER NODE AREA & CONTINUITY FITTING RH/LH SIDE / CRACKS - PERMANENT REPAIR; REFERENCES: /1/ AEROMAN EA 53-0068-25 (COVER + PARTS 1-6) /2/ AIRBUS DOSSIER 81677616 /3/ AIRBUSDR YENA2025123001281Pressure Panel · crackedDURING HEAVY MAINTENANCE: FUSELAGE / CENTER FUSELAGE / FR 36 LH & RH SIDES / PRESSURE PANEL / CRACK DAMAGES AT MULTIPLE HOLES – TIME LIMITED REPAIR; REFERENCES: /1/ AEROMAN EA 53-0071-25 REV. 0 (COVER + PARTS 1-11) /2/ AIRBUS RDAF 81680593/005/2025#A /3/ AIRBUSDR YENA2025123001280Pressure Panel · crackedDURING HEAVY MAINTENANCE: FUSELAGE / CENTER FUSELAGE / FR 36 LH & RH SIDES / PRESSURE PANEL / CRACK DAMAGES AT MULTIPLE HOLES – TIME LIMITED REPAIR; REFERENCES: /1/ AEROMAN EA 53-0071-25 REV. 0 (COVER + PARTS 1-11) /2/ AIRBUS RDAF 81680593/005/2025#A /3/ AIRBUSDR YENA2025123001279Structure · crackedDURING HEAVY MAINTENANCE: WINGS / CENTER BOX / FRONT SPAR VERTICAL STRINGERS & HORIZONTAL FLOOR BEAMS / @ LEVEL OF FR36 & Y-254 & Y+765 / CRACKS - PERMANENT REPAIR; REFERENCES: /1/ AEROMAN EA 57-0108-25 REV. 0 (COVER + PARTS 1-3) /2/ AIRBUS RDAF 81679714/004/2SDR DALA2025122909447Crossbeam · crackedFUSELAGE FRAMES CROSSBEAM JUNCTION AREA AT FR20 LH HOLES H18 & H26 CRACK. REPAIRED PER ERA 630734-14AD. (1371189)SDR DALA2025122909445Post · corrodedCORROSION ON AFT RH LATERAL POST LAV A. REPAIRED PER ER/A 630720-14. (1372197)SDR REXA2026073101363Striker · corrodedCORROSION AT LOWER SILL, SEAL STRIKER & MOUNTING ANGLES OF WEB FLOOR PROTECTOR BTW FS 320.00 TO FS 349.00 OF SERVICE DOOR SURROUND STRUCTURE. CORROSION AT LOWER SILL, SEAL STRIKER & MOUNTING ANGLES OF WEB FLOOR PROTECTOR BTW FS 320.00 TO FS 349.00 OF SERVICESDR SWAA2026011555811Plate · crackedCRACKED CORRUGATED PLATE, TRAILING EDGE IRSS 215 RT WING. REPLACED CORRUGATED PLATE, TRAILING EDGE, IRSS 215 RT WING IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, DWG 115A2001, SHEET 30, REV A, AND DWG 115A2713, SHEET 3, REV A.SDR CALA2026010712737Deck Plate · dentedFLIGHT DECK FLOOR HAD DENTS BETWEEN BS 260 & 270, LBL 15 & RBL15. REPAIRED FLIGHT DECK FLOOR IAW REO-G25742 STAGE 2 AND RECEIVED FINAL ECRA 5310-08757 CAT A REPAIR WITH NO FOLLOW UP INSPECTIONS.SDR REXA2026010601062Door Frame · corrodedPAX DOOR, BS 327.763 FRAME SEGMENT CORRODED BETWEEN DD6 AND DD7. PAX DOOR, FRAME SEGMENT CORRODED BETWEEN DD6 AND DD7. REMOVED UNSERVICEABLE PAX DOOR, FRAME SEGMENT BETWEEN DD6 & DD7 IAW SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. FOUND PAX DOOR, FRSDR AALA202512301752Window Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON WINDSHIELD CENTER POST LOWER ATTACHMENT AREA INTERNAL SIDE UPPER RADIUS LH. CRACK L= 0.160 INCH. MAINTENANCE PERFORMED TIME LIMITED REPAIR ON WINDSHIELD CENTER POST LOWER ATTACHMENT AREA INTERNAL SIDE UPPSDR SWAA2026011955494Web · corrodedVERTIFCAL WEB HAS CORROSION AT RBL +20 BS 767 - 787. REMOVED AND REPLACED VERTICAL WEB AT BS 767 TO 787 RBL 20 IAW SRM 51-10-02, PARAGRAPH 9, SRM 51-40-02, AND DWG 146A0081, REV-SDR SWIA2026011900224Crossbeam · corrodedHIDDEN CORROSION DAMAGE FOUND AT 2 SPOTS, ON CROSSBEAM 87, AFTER REMOVAL OF THE LT AND RT AFT WET AREA BEAMS. PERFORMED PERMANENT DOUBLER/FILLER REPAIRS ON CROSSBEAM 87 AT RH AND LH FLOOR BEAM POSITIONS REF ETD2025-170-934768 AND SRM 53-00-10/ REPAIR 03P. SEESDR CALA2025122912484Window Frame · crackedL3 WINDOW FRAME POST HOLE NR 3 CRACKED AT PRECOLD WORKED HOLE. CURRENT HOLE SIZE .297 INCHES. REPAIRED THE L3 WINDOW FRAME IAW REO-G25698 AND ECRA 5310-08756.SDR FDEA202512242288Beam · damagedBS 137, BL 0, WL 168 BEAM P/N 141T2160-2 HAS A .350" CRACK ON AFT FLANGE 10.00" UP FROM LOWER END. REF DWR 141T2160 SHEET 2 REV, 141T2110-190#E. THIS REPAIR WAS ACCOMPLISHED ON CARD FRR-7 SIGNING OFF FEDEX PART PER E.A. H-5310-T0384867 PART 1. THIS IS A MASDR CALA2026090119156Door Frame · cracked(B737-53-3-0735) AT L1 DOOR CUTOUT FWD UPPER AREA STA 312 FUSELAGE FRAME HAS CRACK ON THE END OF FRAME. REMOVED DAMAGE FROM FUSELAGE FRAME AT L1 DOOR CUTOUT FWD UPPER AREA STA 312 IAW B737-800 SRM 53-10-07-2R-1. FABRICATED AND INSTALLED NEW REPAIR ANGLE IAW BSDR SWIA2025122375769Plate · damagedDURING ACCESS FOR DAMAGED NUTPLATES. FOUND DAMAGED FASTENER HOLES ON INNER PLATE OF LOW PRESSURE GROUND CONNECTION BETWEEN BS 559+112 - 574. INSTALLED NEW INNER PLATE OF LOW PRESSURE GROUND CONNECTION BETWEEN BS 559+112 - 574 IAW SRM 51-42-06, SRM 51-42-13,SDR DALA2026020900940Door Sill · corrodedAMOC / MONITOR INSPECTION LOG REF 630257-14AD, FWD FUSELAGE, FWD CARGO DOOR SURROUND STRUCTURE SILL BTWN FR 25 - 28. SUBJECT REPAIR REQUIRES ADDITIONAL ENGINEERING APPROVAL. REPAIR APPROVAL IS LIMITED TO 40,600 TOTAL FLT HRS OR 20,300 TOTAL ACFT FLT CYCLESSDR AALA202601144567Crossbeam · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN PASSENGER CABIN FLOOR STRUCTURE BREAK ASSEMBLY PANEL LOCATED AT BS 540 FROM RBL 0 RO RBL 25. REPLACED BREAK ASSEMBLY PANEL PER SRM 51-40-02.SDR AALA202601149944Crossbeam · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN PASSENGER CABIN FLOOR STRUCTURE BREAK ASSEMBLY PANEL LOCATED AT BS 540 FROM LBL 0 RO LBL 25. REPLACED BREAK ASSEMBLY PANEL PER SRM 51-40-02.SDR CALA2026010412644Beam · gougedFOUND DEEP GOUGE LOWER FUS A/C BAY CUTOUT EDGE O/B FWD OF PNEUMATIC PORT. ACCOMPLISHED REPAIR TO THE LOWER SUPPORT BEAM LOWER CHORD AT STA 540 RBL 40.875 AS REQUIRED PER SRM 57-10-13-2R-3SDR JJBA20251231037Door Frame · damagedAFT TOP CORNER OF BAGGAGE DOOR AIRFRAME SIDE MISSING A SECTION OF MATERIAL WHERE BAGGAGE DOOR MATES COMPLY WITH PERMANENT REPAIR. PERMANENT REPAIR WAS PERFORMED.SDR CALA2025122912482Pressure Deck · dentedFLIGHT DECK FLOOR DENTED AT BS 257, BL 0 TO LBL 12. REPAIRED FLIGHT DECK FLOOR WEB AT BS 257, RBL 6 TO LBL17 IAW 53-10-51-2R-2 ,SRM 51-40-02-0G-0.SDR GTIA2025122639225Crossbeam · crackedCRACK INDICATION ON FR. 20 RH CROSSBEAM SPLICE AREA AT OPEN FASTENER HOLE H26. DIA REACHED TO REMOVE CRACK IS 8.013MM RAF-01 3503668-01 GENERATED-PERFORMED PERMANENT REPAIR BUSHING ON FR 20 RH CROSSBEAM SPLICE AREA, AT OPEN FASTENER HOLE H26 CROSSBEAM LAYER ASDR EE4Y2025122323672Window Frame · crackedDURING ACCOMPLISHMENT OF ALLEGIANT WORK CARD 531135-03-1-001 & NTM TASK CARD 53-11-35-250-801-C01CARDS (SDI) THAT ARE RELATED TO ALI TASK 531135, MPD 531135-03, IT WAS FOUND THE WINDSHIELD SIDE POST, FR 4 LT, UPPER ATTACHMENT, UPPER FRAME HORIZONTAL FLANGE WITSDR SWAA2026012854842Crossbeam · crackedCRACKED CROSSBEAM, BS 540, BL 0 - LBL 24.75. REPLACED CROSSBEAM IAW SRM 51-40-02, AND DWG 143A0060, SHEET 64, REV-.SDR SWAA2026012754672Pressure Deck · crackedCRACK INDICATION ON THE HORIZONTAL PRESSURE DECK WEB, LBL 30, BS 663 IN THE PASSENGER CABIN. CRACK LENGTH 0.200 INCH. PERFORMED A PERMANENT REPAIR ON THE PRESSURE DECK WEB, BTW BS 663.75 & BS 675, LBL 20 & 60 IAW SRM 53-40-51-2R-2, REPAIR 2.SDR CALA2025122412411Window Frame · crackedRIGHT NR 3 WINDOW FRAME FOUND CRACKED ON HOLES 3 & 4. PERFORMED REPAIR ON THE RT NR 3 WINDOW FRAME IAW EO 250450 REV. P1, P2, P3 AND IR, EA 5310-08195 REV. C, AND ECRA 5310-08750.SDR FDEA202512222284Crease Beam · corrodedMAIN CABIN. CREASE BEAM. (RH) STA 1200 CORRODED. CORROSION OUT OF LIMITS AT MAIN CARGO COMPARTMENT CREASE BEAM INBOARD CHORD AT STA 1200 RBL 64 WAS REPAIRED IAW B-757 SRM 53-00-13-2RSDR FDEA202512222283Crease Beam · corrodedMCC FLOOR BTWN STA 440 - 460 (RH CREASE BEAM) RBL 64.5 APROX WAS FOUND ON LOCATION WITH CORROSION. CORROSION OUT OF LIMITS AT MAIN CARGO COMPARTMENT, CREASE BEAM INBOARD CHORD BTW STA 440-460 RBL 64.40 WAS REPAIRED IAW B-757 SRM 53-00-13-2RSDR FDEA202512222282Crease Beam · corrodedMAIN CARGO BAY, FLOOR INBOARD CHORD HAS SURFACE CORROSION AROUND NUTS PLATE BETWEEN BS 860 AND 879 CORROSION OUT OF LIMITS AT MAIN CARGO BAY CREASE BEAM INBOARD CHORD BTW STA 860 - 879 RBL 64 WAS REPAIRED IAW SRM 53-00-13-2R.SDR SWAA2026011954389Pressure Deck · crackedCRACK INDICATION ON HORIZONTAL PRESSURE DECK WEB, RBL 41, BS 663. CRACK LENGTH 0.375 INCH. PERFORMED REPAIR ON HORIZONTAL PRESSURE DECK WEB LOCATED BTW RBL 30 TO RBL 60 BTW BS 663.75 TO BS 675 AT PASSENGER CABIN IAW SRM 53-40-51-2R-2, REPAIR 2.SDR SWAA2026011554557Crossbeam · crackedCRACK BRAKE PANEL FLOOR STRUCTURE BS540 AND BTW LBL24.82 TO BL0 AT PASSENGER CABIN. REPLACED BRAKE PANEL FLOOR STRUCTURE BS540 AND BTW LBL24.82 TO BL0 AT PASSENGER CABIN IAW SRM 51-40-02-0G-0 AND DWG 143A0060 SHEET 36 REV.ASDR SWAA2026011554556Crossbeam · crackedCRACKED BRAKE PANEL FLOOR STRUCTURE BS540 AND BTW RBL24.82 TO BL0 AT PASSENGER CABIN. REPLACED BRAKE PANEL FLOOR STRUCTURE BS540 AND BTW RBL24.82 TO BL0 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02; SRM 51-10-02 STEP 9 AND DWG 143A0060 SHEET 36 REV.A MEASURE
Back to JASC 5310