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 R61A2025082500373Seal Rest · corrodedDURING HEAVY CHECK FOUND CORROSION AFT CARGO CUT OUT, AFT UPPER SEAL REST BETWEEN FR 79-80 FOUND CORRODED. REPAIRED IAW ETD 2025-170-926736Aug 9, 2025 · N208QJ · Emb ERJ170200LRSDR R61A2025082500372Seal Rest · corrodedDURING HEAVY CHECK FOUND CORROSION CF I FWD CARGO DOOR CUTOUT, AFT LOWER SEAL REST BETWEEN FR 26-27 STGR 26R FOUND CORRODED. REMOVED AND REPLACED AFT LOWER SEAL REST IAW SRM 51-41-01Aug 9, 2025 · N208QJ · Emb ERJ170200LRSDR R61A2025082500371Seal Rest · crackedDURING HEAVY CHECK FOUND CORROSION CF I FWD CARGO DOOR CUTOUT MIDDLE LOWER SEAL REST BETWEEN. FR25-26, STGR 26R FOUND CORRODED. REMOVED AND REPLACED MIDDLE LOWER SEAL REST IAW SRM 51-41-01Aug 9, 2025 · N208QJ · Emb ERJ170200LRSDR YENA2025081200828Window Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON WINDSHIELD CENTER LOWER POST ON UPPER TENSION BOLT AREA ON LH SIDE CRACK LENGTH = 0.250 INCH APPROX; AEROMAN WO#2025-190/1 WCC# 2025-416536 FOR WORK PERFORMED; PERFORMED PERMANENT REPAIR ON FUSELAGE WINDSHIELAug 9, 2025 · N608JB · Airbus A320232SDR YENA2025081200827Window Frame · crackedDURING HEAVY MAINTENANCE: WINDSHIELD FRAME CENTER POST LOWER NODE AREA CRACKED. POST REPAIR INSPECTIONS OF THE MIRROR FITTINGS (TBD) AEROMAN EA 53-0371-22 REV. 0. AIRBUS RDAF 81098121/004/2022#A. AIRBUS DOSSIER 81098121. AIRBUS TD/81039011/009/2022#A. Aug 9, 2025 · N608JB · Airbus A320232SDR JR2R20250809930Seal Rest · corrodedFWD CARGO DOOR OPENING, LOWER FWD SEAL REST CORRODED. REPLACEDAug 9, 2025 · N88331 · Emb ERJ170200LRSDR SWIA202509250808Strap · corrodedCORROSION FOUND ON INNER SIDE OF JOIN STRAP AT FS333.00 BETWEEN STGR 23R AND 22R. (30632613) (C-CHECK RO 09/24/2025)BLENDED OUT CORROSION AND RESTORED FINISH ON INNER SIDE OF JOINT STRAP/DOUBLER AT FS333.00 BETWEEN STGR 23R AND 22R. FOUND WITHIN LIMITS. REF. Aug 8, 2025 · N461SW · Cndair CL6002B19SDR AALA202508183034Stop Fitting · gougedAIRCRAFT IN BASE MAINTENANCE: L1 DOOR STOP FITTING AT BS 344, S7L GOUGED. REPLACED STOP FITTING PER AMM 52-11-01.Aug 8, 2025 · N934NN · Boeing 737823SDR CALA2025081107566Dome Nut · brokenBROKEN DOME NUTS IN FWD PIT FROM BS 690 TO 730 L/H SIDE AT MAIN CABIN FLOOR LEVEL. ECRA 5330-07581 AND EA757-5330 -13-A4304 ACCOMPLISHED.Aug 8, 2025 · N14120 · Boeing 757224SDR UIEA2025073101074Beam · crackedONE CRACK WAS FOUND ON LT NOSE WHEEL WELL SIDE PANEL BEAM, BS 260-280 WL 180. BEAM REPLACED IAW SRM 51-10-02 & NEW BEAM HOLE'S TRANSFERRED IAW SRM 51-40-05 & NEW BEAM INSTALLED IAW SRM 51-40-02. NO FURTHER DEFECTS NOTED.Aug 8, 2025 · N446MC · Boeing 7474B5FSDR AALA202509028347Floorbeam · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION FLOOR BEAM +Y1292 FR 66 AT AFT GALLEY AREA, MEASURE OF CORROSION ARE: L= 1.613 INCH W= 1.060 INCH D= 0.040 INCH. MAINTENANCE REPLACED FLOOR BEAM Y1292 BETWEEN FR64 TO FR66 AFT GALLEY AREA LH SIDE IAW A320 SRM 51-72-11-91Aug 7, 2025 · N664AW · Airbus A320232SDR AALA202509020656Shear Plate · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK SHEAR PLATE STR 23L BTW FR69 AND FR70 AT AFT GALLEY AREA. CRACK L= 1.465 IN. MAINTENANCE REPLACED SHEAR PLATE LOC. ON STR 23L BTW FR69 AND FR70 AT AFT GALLEY AREA. IAW A320 SRM 51-42-11-801, SRM 51-72-11-911-001 AND DWG D53Aug 7, 2025 · N664AW · Airbus A320232SDR CALA2025081407756Window Frame · no discrepancyON THE L3 WINDOW FRAME E-F POST ACCOMPLISH INSPECTION REQUIREMENTS PER PART 2 OF EC/RA 5311-03376 ON OR BEFORE 50,000 TOTAL CYCLES. L3 WINDOW FRAME E-F POST ACCOMPLISH INSPECTION REQUIREMENTS PER PART 2 OF ECRA 5311-03376 ON OR BEFORE 50,000 TOTAL CYCLES.Aug 7, 2025 · N37253 · Boeing 737824SDR SWAA2025081199183Sill Drain · odorTERRIBLE SMELL COMING FROM AFT GALLEY FLOOR DRAINS<[01] CLEANED AND FLUSHED AFT ENTRY AND AFT SERVICE DOOR SILL DRAINS REF AMM 38-31-00Aug 7, 2025 · N8693A · Boeing 7378H4SDR DALA2025081105965Support Beam · corroded(LOG 1130808) MULTIPLE AREAS OF CORROSION ALONG LENGTH OF AFT CARGO RH FLOORBOARD TO SIDEWALL TRANSITION SUPPORT BEAM. REMOVED TRANISTION BEAN SECTION FROM STA 727I TO STA 767, FABRICATED NEW TRANSITION BEAM AND INSTALLED. REMOVED TRANSITION BEAM AND INSTALLEDAug 7, 2025 · N869DN · Boeing 737932ERSDR VNAA20251016011Seat Track · corrodedCORROSION AND SCRATCHES ON SEAT RAIL LBL9.00, FS581.00 TO FS661+32. DUE TO EXCESSIVE DAMAGE ON SEAT RAIL LBL9.00, FS581.00 TO FS661+32. WERE FOUND OUT OF LIMITS PER CRJ-900 SRM 53-31-49-101-001-A02 THEREFORE WERE REPLACED PER CRJ 900 AMM 53-00-49 (CONFIIG A12Aug 6, 2025 · N641NN · Bombdr CL6002D15SDR SWIA2025090200806Beam · corrodedAFT WET AREA LH BEAM HAS CORROSION AT FR 87. INSTALLED AFT WET AREA LH BEAM BETWEEN FR86 - FR89 IAW SRM 51-40-08.Aug 6, 2025 · N118SY · Emb ERJ170200LRSDR CALA2025081407755Window Frame · crackedEA 5310-08195 REV B CRACK FOUND AT LH SIDE NUMBER 3 WINDOW FRAME POST 4TH HOLE FROM THE BOTTOM. ACCOMPLISHED ON THE LT NR 3 WINDOW POST FRAME E-F IAW ECRA 5310-08666 PART 1. AFTER 49900 TOTAL AIRCRAFT FLIGHT CYCLES (FC), BUT BEFORE 50000FC PERFORM AN INSPAug 6, 2025 · N14235 · Boeing 737824SDR CALA2025081107558Pressure Deck · dentedFLIGHT DECK FLOOR HAS DENTS BETWEEN BS 251.5 AND BS 259.5 AND BETWEEN LBL-12 AND RBL-12. REMOVED DAMAGE, ACCOMPLISHED HFEC AND GVI WITH NO DEFECTS NOTED, ACCOMPLISHED INSURANCE CUT, FABRICATED REPAIR PARTS, RESTORED COATINGS AND INSTALLED AND TOP COAT REF HAEAug 6, 2025 · N62895 · Boeing 737924ERSDR JJBA20250808015Mount · corrodedCORROSION FOUND ON RAT 2 ANTENNAE MOUNT, BETWEEN FRAMES 65 AND 66. REPAIRED CORROSION FOUND UNDER RAT 2 ANTENNA MOUNT ON REAR FUSELAGE LOWER SKIN BETWEEN FR 65 AND 66.Aug 6, 2025 · N12135 · Emb EMB145XRSDR R61A2025080600342Beam · corrodedDURING HEAVY CHECK FOUND AFT CARGO DOOR CUTOUT LOWER BEAM PLATE FR 77-80 STR 27 CORRODED. REPLACED LOWER BEAM IAW AMM 20-10-01-410-801-A00.Aug 6, 2025 · N728YX · Emb ERJ170200LRSDR R61A2025080600339Seal Rest · corrodedDURING HEAVY CHECK FOUND AFT SERVICE DOOR R2 LOWER SEAL REST FR 85-87 CORRODED. REPLACED SEAL REST IAW SRM 51-41-01Aug 6, 2025 · N728YX · Emb ERJ170200LRSDR SWI2025F01443Door Frame · out of limitsFS409 RBL18 VERTICAL POST HAS INDICATIONS IN THE AFT RADIUS OF @WL69 AS FOLLOWS: INBD SIDE: 65% FSH BY .75" LONG, & OUTBD SIDE: 55% BY .3" LONG. FAILED NDT INSPECTION. (C-CHECK RO 10/19/2025)REMOVED AND REPLACED FS 409 RBL 18 POSTS INSTALLED NEW ONES P/N 601Aug 5, 2025 · N933EV · Cndair CL6002B19SDR SWIA2025102000805Door Frame · out of limitsFS409 BL0 VERTICAL POST HAS INDICATIONS IN THE AFT RADIUS OF @WL69 AS FOLLOWS: LH SIDE: 60% FSH BY .4" LONG, & RH SIDE: 70% BY .4" LONG. FAILED NDT INSPECTION. (C-CHECK RO 10/19/2025)REPLACED 409+128 POSTS AT BL0 IAW REO 601R-53-41-889 REV D DATED 2018, COMPAug 5, 2025 · N933EV · Cndair CL6002B19SDR VNAA20251016007Door Sill · corrodedCORROSION ON LOWER SILL OF SURROUND STRUCTURE, AFT BAGGAGE BAY DOOR. LOWER SILL OF SURROUND STRUCTURE, AFT BAGGAGE BAY DOOR WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01, SRM 51-42-13-001-001-A01 AND SRM 51-42-21-001-001-A01.Aug 5, 2025 · N641NN · Bombdr CL6002D15SDR AALA202510140621Structure · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND IN HOLE LOCATED ON FUSELAGE AT FR35 AND STGR 30 LH. (CRACK: 0.125 INCH). MAINTENANCE ACCOMPLISHED TIME LIMITED REPAIR ON HOLE 2 LOC FR 35 AT LEVEL STGR 30LH IAW EA 367091.Aug 5, 2025 · N664AW · Airbus A320232SDR SWAA2025091098730Door Frame · crackedCRACK FRAME AT FWD ENTRY DOOR CUT OUT BS 312 BTW STRINGERS 5L TO STRINGER 6L PASSENGER CABIN. REPAIRED FRAME AT FWD ENTRY DOOR CUT OUT BS 312 BTW STRINGERS 5L TO STRINGER 6L PASSENGER CABIN SEE TTG8Q014FBE3.Aug 5, 2025 · N8617E · Boeing 7378H4SDR VGCA20250805026Beam · corrodedRIGHT OTBD END OF THE SIDELOAD BEAM CORRODED. CENTER FUSELAGE BULKHEAD SIDELOAD BEAM CORRODED AT BS740 FROM LBL30 TO RBL30Aug 5, 2025 · N216WE · Boeing 7272S2FSDR VGCA20250805019Window Frame · corrodedAFT UPPER FUSELAGE WINDOW FRAMES CORROSION FROM BS950A-950C AND S-10R TO S-14RAug 5, 2025 · N216WE · Boeing 7272S2FSDR VGCA20250805018Structure · corrodedCORROSION AT MULTIPLE LOCATIONS AT A-NUT ATTACHMENTS. FORWARD LOWER FUSELAGE LONGITUDINAL STABILIZER LOWER CHORD REPAIRED AT BL0 FROM BS450-660Aug 5, 2025 · N216WE · Boeing 7272S2FSDR AALA202508065312Fastener · looseAIRCRAFT WAS NOT GROUNDED: LAVATORY-A DOOR IS STICKING WHEN OPENING AND CLOSING. TIGHTENED LOOSE FASTENERS ON THRESHOLD DOOR. PER CMM25-48-48. OPERATIONAL CHECK GOOD.Aug 5, 2025 · N932NN · Boeing 737823SDR AALA202510082347Door Frame · no discrepancyAIRCRAFT IN BASE MAINTENANCE: MODIFICATION OF OVERWING EMERGENCY EXIT 843 FRAME, BETWEEN FR 38 AND FR 39, BETWEEN BEAM 2 AND BEAM 3, REQUIRED DUE TO POTENTIAL CRACK PER EO 5210Y228. MODIFICATION OF FRAME ACCOMPLISHED PER EO 5210Y228.Aug 4, 2025 · N664AW · Airbus A320232SDR AALA202510080186Door Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN OVERWING EXIT 843 RIGHT HAND LOAD TRANSMITTING PROFILE BETWEEN FR 38 AND FR 39, BETWEEN BEAM 2 AND BEAM 3. REPLACED SEGMENT PER EO 5210Y228.Aug 4, 2025 · N664AW · Airbus A320232SDR AALA202510080481Door Frame · no discrepancyAIRCRAFT IN BASE MAINTENANCE: MODIFICATION OF OVERWING EMERGENCY EXIT 843 FRAME, BETWEEN FR 38 AND FR 39, BETWEEN BEAM 2 AND BEAM 3, REQUIRED DUE TO POTENTIAL CRACK PER EO 5210Y228. MODIFICATION OF FRAME ACCOMPLISHED PER EO 5210Y228.Aug 4, 2025 · N664AW · Airbus A320232SDR AALA202510087242Door Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN OVERWING EXIT 844 RIGHT HAND LOAD TRANSMITTING PROFILE BETWEEN FR 40 AND FR 41, BETWEEN BEAM 2 AND BEAM 3. REPLACED SEGMENT PER EO 5210Y228.Aug 4, 2025 · N664AW · Airbus A320232SDR AALA202510089637Door Frame · no discrepancyAIRCRAFT IN BASE MAINTENANCE: MODIFICATION OF OVERWING EMERGENCY EXIT 844 FRAME, BETWEEN FR 40 AND FR 41, BETWEEN BEAM 2 AND BEAM 3, REQUIRED DUE TO POTENTIAL CRACK PER EO 5210Y228. MODIFICATION OF FRAME ACCOMPLISHED PER EO 5210Y228.Aug 4, 2025 · N664AW · Airbus A320232SDR AALA202510088979Door Frame · no discrepancyAIRCRAFT IN BASE MAINTENANCE: MODIFICATION OF OVERWING EMERGENCY EXIT 844 FRAME, BETWEEN FR 40 AND FR 41, BETWEEN BEAM 2 AND BEAM 3, REQUIRED DUE TO POTENTIAL CRACK PER EO 5210Y228. MODIFICATION OF FRAME ACCOMPLISHED PER EO 5210Y228.Aug 4, 2025 · N664AW · Airbus A320232SDR AALA202509033975Sill Drain · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON R2 ENTRY LOWER SILL INNER CHORD (CREASE ANGLE) LOCATED FROM BS 967 TO BS 986, AT RBL 47. REPLACED CHORD PER AARD 51-00-05-1.Aug 4, 2025 · N974AN · Boeing 737823SDR AALA202509029143Door Sill · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON L2 DOOR CUTOUT LOWER SILL PLATE BETWEEN FR 66 AND FR 68 AT S22L. REPLACED SILL PLATE PER SRM 51-72-11.Aug 4, 2025 · N151UW · Airbus A321211SDR AALA202509021909Door Sill · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT HAND AFT PASSENGER / CREW DOOR CUTOUT LOWER SILL PLATE AT FR 68 AND S23L. REPLACED SILL PLATE PER SRM 51-72-11.Aug 4, 2025 · N151UW · Airbus A321211SDR AALA202508158154Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT RIGHT PASSENGER / CREW DOOR CUTOUT LOWER SILL CENTER SHAPE FITTING BETWEEN FR 66 AND FR 68 AT S23R. REPLACED CENTER SHAPE FITTING PER SRM 51-44-11.Aug 4, 2025 · N151UW · Airbus A321211SDR DALA2025080505857Vertical Beam · crackedCRACK ON UPPER EDGE OF Y0 VERTICAL BEAM. REPLACED Y0 VERTICAL BEAM AND FASTENERS LOCATED FR1 AS PER SRM 51-42-11, SRM 51-72-11.Aug 4, 2025 · N355NB · Airbus A319114SDR ASAA2025080360125Web · corrodedAFT WET AREA R/H WEB SUPPORT STA 986 TO 1016 RBL 45 HAS CORROSION. GROUNDED - YES. REMOVED CORROISON FOUND TO BE OUT OF LIMITS , REMOVED & REPLACED WEB IAW B737-800 SRM 51-40-02-0G-0 & 51-40-05-0G-0. W 1, O .050, R .088, L 4, D .012.Aug 3, 2025 · N526AS · Boeing 737890SDR CALA2025080807519Seal · debondedCAPT LEFT SIDE WINDOW CONTINUOUS RATTLING NOISE FOUND. L1 WINDOW UPPER HUMP SEAL DISBONDED. APPLIED SPEED TAPE PER TEMPORARY REPAIR REF DMC-B787-A-56-11-00-03A-663A-A.Aug 3, 2025 · N27959 · Boeing 7879SDR DALA2025080405835Fitting · corrodedSHIP 3146 LOWER FUSELAGE FWD CARGO COMPARTMENT DOOR CUTOUT LATCH FITTING WITH CORROSION AT FR27. CORRECTIVE ACTION: REPLACED LATCH FITTING IAW A319 SRM 51-72-11 -911-001. (1122732).Aug 3, 2025 · N346NB · Airbus A319114SDR YENA2025080600804Window Frame · crackedDURING HEAVY MAINTENANCE: FUSELAGE/WINDSHIELD FRAME/CENTER POST LH & RH CONTINUITY FITTING LH/RH CRACK; ACCOMPLISHED REPAR OF THE PREVIOUSLY ACCOMPLISHED TEMP REPAIR (ORIGINAL DEFECT WAS A CRACK) ON LH CENTER POST LWR ATTACHMENT CORNER RADIUS IAW AEM EA 53-003Aug 2, 2025 · N527JL · Airbus A320232SDR YENA2025080600802Window Frame · crackedDURING HEAVY MAINTENANCE: FUSELAGE / WINDSHIELD FRAME / CENTER POST LH & CONTINUITY FITTING LH/RH / CRACK – PERMANENT REPAIR; REFERENCES: /1/ TEMPORARY REPAIR IAW A22-539-01 /2/ AEM EA 53-0036-25 REV 0 (COVER AND PARTS 1 - 4) /3/ AIRBUS RDAF 81073709/033/2025#Aug 2, 2025 · N527JL · Airbus A320232SDR DALA2025111708377Nut Plate · damagedER/A 628114-14; A220-100, RT EMERGENCY EXIT DOOR CUTOUT SURROUND STRUCTURE, FRAME 42. SUBJECT REPAIR REQUIRES FOLLOW-ON ACTION. ACCOMPLISH ER/A 628114-14, SECTION II WITHIN 1,000 FLIGHT HOURS FROM 16,139 TOTAL FLIGHT HOURS. ASSOCIATED ER/A 14-628114. SECTIONAug 1, 2025 · N118DU · Airbus BD5001A10SDR JJBA20251111060Retainer · corrodedDURING INSPECTION FOR OK TO INSTALL, FOUND CORROSION ON R/H DV WINDOW RETAINER RING FRAME. REMOVED CORROSION FROM RH DV WINDOW RETAINER RING FRAME. REPLACED DV WINDOWAug 1, 2025 · N12135 · Emb EMB145XRSDR VNAA202509260009Seal Rest · corrodedCORROSION ON SEAL REST WAS FOUND. SEALS REST WERE CLEANED PER CRJ-700 SRM 51-26-00-001-001-A01 AND FWD CORNER SEAL RETAINER BAGG DR NO CORROSION WAS FOUND ALSO RETAINER SEAL MID SECTION AND RETAINER SEAL AFT CORNER WERE REPLACED PER CRJ- 700 SRM 51-42-06-00Aug 1, 2025 · N526EA · Cndair CL6002C10
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