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 N6W2025F00002Blanking Plate · corrodedCORROSION ON FITTING OF FLOOR SUPPORT STRUCTURE AT FS280 / RBL12 AND LBL12. REMOVED AND REPLACED FLOOR SUPPORT STRUCTURE AT FS280 IAW CRJ 700 SRM 51-42-21.Jun 27, 2025 · N513GJ · Cndair CL6002C11SDR SWI2025F01409Structure · corrodedAFT FUSELAGE, WET AREA FS 942.00 BETWEEN STRG 26L TO 26R HAS CORROSION DAMAGED. COMPLIED WITH REO 690-53-51-486 AND CRJ900 SRM 53-00-06-201-001-A03 FIGURE 53-00-06-991-868 FOR REPAIR OF AFT FUSELAGE WET AREA FS 942.00 BETWEEN STRG 26L TO STRG 26R NO FURTHER Jun 26, 2025 · N806SK · Cndair CL6002D24SDR SWIA2025F01408Structure · corrodedAFT FUSELAGE, WET AREA FS 1000.00 BETWEEN STRG 26L TO 26R HAS CORROSION DAMAGED. COMPLIED WITH REO 690-53-61-1647 AND CRJ900 SRM 53-00-06-201-001-A03 FOR REPAIR OF FRAME 1000.00 BETWEEN STRG 26L AND 26R NO FURTHER ACTION IS REQUIRED,Jun 26, 2025 · N806SK · Cndair CL6002D24SDR SWIA2025F01407Structure · corrodedAFT FUSELAGE, WET AREA FS 927.00 BETWEEN STRG 26L TO 26R HAS CORROSION DAMAGED. COMPLIED WITH REO 690-53-51-486 AND CRJ900 SRM 53-00-06-201-001-A03 FIGURE 53-00-06-991-868 FOR REPAIR OF AFT FUSELAGE WET AREA FS 927.00 BETWEEN STRG 26L TO STRG 26R NO FURTHER Jun 26, 2025 · N806SK · Cndair CL6002D24SDR SWIA2025F01406Structure · corrodedAFT FUSELAGE, WET AREA FS 954.00 BETWEEN STRG 26L TO 26R HAS CORROSION DAMAGED. COMPLIED WITH REO 690-53-51-486 AND CRJ900 SRM 53-00-06-201-001-A03 FIGURE 53-00-06-991-868 FOR REPAIR OF AFT FUSELAGE WET AREA FS 954.00 BETWEEN STRG 26L TO STRG 26R.Jun 26, 2025 · N806SK · Cndair CL6002D24SDR SWIA2025100600026Structure · corrodedAFT FUSELAGE, WET AREA FS 1049.00 BETWEEN STRG 26L TO 26R HAS CORROSION DAMAGED. COMPLIED WITH REO 690-53-61-1647 FOR REPAIR OF FS 1047.00 BETWEEN STRG 26L AND 26R AND CRJ900 SRM 53-00-06-201-001-A03 NO FURTHER ACTION IS REQUIRED.Jun 26, 2025 · N806SK · Cndair CL6002D24SDR SWAA2025072985563Beam · corrodedBS 986 BEAM PREVIOUS REPAIR IS CORRODED ON UPPER SURFACE AND BETWEEN REPAIR PARTS FROM RBL 42 TO RBL 45, WL 207.9 TO WL 208.1. DISCREPANCY AREA TO BE REMOVE AND REPAIRED FROM BS 986, RBL 25-RBL 50, WL208 ON CCN TTG8Q013DS97 DUE TO ADJACENT DAMAGE REPORTED EXCJun 26, 2025 · N296WN · Boeing 7377H4SDR SWAA2025072285898Crease Beam · corrodedCORROSION CREASE BEAM LOCATED STA639 PLUS 2 INCHES AND RBL64 WL208.1 PASSENGER CABIN 2025-403073. REPLACED CREASE BEAM (INNER CHORD SECTION) LOCATED STA 616+13 INCH TO BS 663.75+9 INCH RBL64 WL208.1 PASSENGER CABIN.IAW B737-700 SRM 51-40-02 SRM 51-10-02 ITEM Jun 26, 2025 · N446WN · Boeing 7377H4SDR SIMA20250626005Gusset · corrodedAFT GALLEY FLOOR STRUCTURE, THE RH FLOOR BEAM GUSSET HAS CORROSION AT FR 89-90. SSI 53-23-005. (MAJOR REPAIR) (LEVEL 2 CORROSION). RAR THE AFT GALLEY FLOOR STRUCTURE, RH FLOOR BEAM GUSSET AT FR 89-90 IAW ERJ 175 SRM 51-40-08Jun 26, 2025 · N245NN · Emb ERJ170200LRSDR AALA202507163315Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED CENTER FUSELAGE PRESSURE DECK CORNER FITTING AT FR 36 AND -Y1525.34. REPLACED CORNER FITTING PER SRM 51-42-11.Jun 26, 2025 · N178US · Airbus A321211SDR AALA202507155201Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED CENTER FUSELAGE PRESSURE DECK CORNER FITTING AT FR 36 AND +Y1525.34. REPLACED PRESSURE DECK CORNER FITTING PER SRM 51-42-11.Jun 26, 2025 · N178US · Airbus A321211SDR JJBA20250711017Door Frame · corrodedCARGO DOOR CORRODED AT FWD LOWER CORNER FRAME 65. REMOVED CORROSION CARGO DOOR AT FWD LOWER CORNER FRAME 65. REMOVED CARGO DOOR FWD LOWER CORNER AT FRAME 65 RECEIVED NEW PART. LOCATED, DRILLED AND INSTALLED NEW PARTJun 26, 2025 · N13202 · Emb EMB145XRSDR JJBA20250711016Door Frame · corrodedLOWER CARGO DOOR FRAME CORROSION AROUND NUTPLATE HOLES AT FRAME 66. REMOVED CORROSION LOWER CARGO DOOR FRAME AROUND NUTPLATE HOLES AT FRAME 66 OUT OF LIMITS. REMOVED AND INSTALLED NEW PARTS. LOCATED, DRILLED, AND INSTALLED.Jun 26, 2025 · N13202 · Emb EMB145XRSDR AALA202507021874Tee Angle · crackedAIRCRAFT IN BASE MAINTENANCE: LEFT ECS BAY "T" ANGLE CRACKED AT STA 650 AFT OUTBOARD CORNER OF ECS DOOR 192CL SURROUND STRUCTURE. REMOVED AND REPLACED "T" ANGLE. PER SRM 51-10-02, SRM 51-40-02, AND IPC53-42-00.Jun 26, 2025 · N931NN · Boeing 737823SDR CALA2025070106106Crease Beam · corrodedAFT WET AREA RH DOOR CREASE BEAM HAS MULTIOPLE SPOTS OF CORROSION. REMOVED CORROSION ORG THICKNESS .180 REMOVED .105 REMAINING .075 AND FOUND TO BE OUT OF LIMITS PER EC/RA 5321-01330 REV A AND SRM 53-70-15-1A-1. REMOVED CREASE BEAM PER B737-800 SRM 51-40-02. Jun 26, 2025 · N35204 · Boeing 737824SDR YENA2025062700656Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FASTENER HOLE 3 (LOWER/INBOARD POSITION) LOCATED AT FR68 LH, DOOR STOP FITTING 1. AT PASSENGER CABIN. CRACK DEPTH = 0.088 INCHES, CRACK DIRECTION: 12 OCLOCK; (RESOLVED ON W/O: 1380871 TASKCARD: NR-00010) FUR-Jun 26, 2025 · N508JL · Airbus A320232SDR 2025FA0000429Frame · crackedFS 280 FLOOR BEAM CRACKED , RH SIDE. REPAIRED I/A/W BOMBARDIER REO 601R-53-11-3994 REV. -- 2025-06-04 AND BOMBARDIER REO 601R-53-11-926 REVB 2006-05-10.Jun 26, 2025 · N886AS · Cndair CL6002B19SDR JR2R20250625111Doubler · corrodedAFT DRAIN MAST FUSELAGE DOUBLER CORRODED. REWORKEDJun 26, 2025 · N88327 · Emb ERJ170200LLSDR JR2R20250625443Doubler · corrodedAFT DRAIN MAST FUSELAGE DOUBLER CORRODED. REWORKEDJun 26, 2025 · N88327 · Emb ERJ170200LLSDR MAS2025F00002Seal Rest · corrodedFWD CARGO DOOR OPENING LOWER FWD SEAL STRIKER CORRODEDJun 26, 2025 · N88327 · Emb ERJ170200LLSDR AALA202509035981Window Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON LOWER RADIUS OF THE WINDSHIELD CENTER POST LOWER ATTACHMENT AREA INTERNAL SIDE LH. CRACK L= 0.098 INCH. MAINTENANCE PERFORMED TIME LIMITED REPAIR OF MIRROR FITTING REPAIR LH LOC ON CENTER WINDSHIELD FRAMEJun 25, 2025 · N826AW · Airbus A319132SDR AALA202509023860Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON CONTINUITY FITTING OF THE WINDSHIELD LOWER ATTACHMENT AREA INTERNAL SIDE LH. CRACK L= 0.157 INCH. MAINTENANCE PERFORMED TIME LIMITED REPAIR ( REPLACED CONTINUITY FITTING) WINDSHIELD LOWER ATTACHMENT AREA Jun 25, 2025 · N826AW · Airbus A319132SDR SIMA20250625001Seal Rest · corrodedSSI# 53-21-009 FWD CARGO DOOR CUTOUT FWD CORNER SEAL DEPRESSOR IS GOUGED ON EDGES AND HAS CORROSION AT NUT PLATE HOLE. (MAJOR REPAIR) (LEVEL 2 CORROSION). RAR THE FWD CARGO DOOR CUTOUT FWD CORNER SEAL DEPRESSOR IAW ERJ 175 AMM 20-10-01.Jun 25, 2025 · N245NN · Emb ERJ170200LRSDR DALA2025070104890Threshold · corroded2R DOOR THRESHOLD PANEL FWD AND AFT INBD CORNERS HAVE CORROSION. -M-. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0583:5300-2016/001 00353 REMOVED AND REPLACED AFT SERVICE DOOR THRESHOLD PANEL REF A220 AMP 53-00-47. (LP# 1044440)Jun 25, 2025 · N107DU · Airbus BD5001A10SDR DALA2025063004858Stub Frame · damagedSHIP 6807 DURING HOLE SCANS OF STATION 1000 LEFT SIDE UNDER STUB BEAM 1 FORWARD OUTBOARD HOLE COMMON TO THE SKIN AND STRINGER, DEFECT NOTED, HOLE FOUND TO BE ELONGATED IN STRINGER ONLY. CORRECTIVE ACTION: REPAIRED STATION 1000 FWD HOLE PER ER/A 626574-14 PRI RJun 25, 2025 · N710TW · Boeing 7572Q8SDR DALA2025063004857Stub Frame · damagedSHIP 6807 DURING HOLE SCANS NOTED DEFECT AT STATION 1000 L/H OUTBOARD AFT HOLE UNDER STUB BEAM COMMON TO THE SKIN AND STRINGER. CORRECTIVE ACTION: REPAIRED STATION 1000 AFT HOLE PER ER/A 626574-14 PRI REV 04. (1045508)Jun 25, 2025 · N710TW · Boeing 7572Q8SDR DALA2025063004856Stub Frame · damagedSHIP 6714 DURING HOLE SCANS NOTED DEFECT AT STATION 1000 L/H OUTBOARD AFT HOLE UNDER STUB BEAM COMMON TO THE SKIN AND STRINGER. CORRECTIVE ACTION: REPAIRED STATION 1000 AFT HOLE PER ER/A 626574-14 PRI REV 04. (1045502)Jun 25, 2025 · N6714Q · Boeing 757232SDR CALA2025063006031Insulation · contaminatedSMOKE AGAIN IN MAIN WHEEL WELL. OPERATED FLIGHT CONTROLS, FLAPS, BOTH ENGINE THRUST REVERSERS, AND PARKING BRAKE WHILE BOTH HYDRAULIC EMDPS WERE RUNNING MULTIPLE TIMES, FOUND NO ACTIVE HYDRAULIC LEAK IN THE WHEEL WELLS AT THIS TIME. CORRECTED HYDRAULIC LJun 25, 2025 · N37267 · Boeing 737824SDR DALA2025062604803Crossbeam · crackedSHIP 3135 CRACK INDICATION WAS FOUND AT HOLE #2 AND #16 OF CROSSBEAM JUNCTION AREA OF FR16RH. CORRECTIVE ACTION: COMPLIED WITH ER/A 626548-14AD. (1045556).Jun 25, 2025 · N335NB · Airbus A319114SDR DALA2025062604800Structure · crackedSHIP 3135 CRACK WAS FOUND AROUND A FASTENER HOLE COMMON TO THE BULKHEAD AT FR35 AND STGR 30 LH LEVEL. CORRECTIVE ACTION: COMPLIED WITH ER/A 575262-14AD. (1045830).Jun 25, 2025 · N335NB · Airbus A319114SDR DALA2025062604799Frame · crackedSHIP 3135 FOUND CRACK AT HOLE W1, W3 IN FRAME35 WEB & HOLE #2 IN FRAME FLANGE. CORRECTIVE ACTION: COMPLIED WITH ER/A 575262-14AD. (1045802).Jun 25, 2025 · N335NB · Airbus A319114SDR DALA2025062604798Stiffener · crackedSHIP 3135 CRACK INDICATION ON HORIZONTAL UPPER STIFFENER OF LATERAL WINDOW FRAME 4 LH SIDE. CORRECTIVE ACTION: COMPLIED WITH ER/A 575007-14AD. (1045582).Jun 25, 2025 · N335NB · Airbus A319114SDR DALA2025062504770Door Frame · crackedSHIP 3135, FOUND CRACK AT HOLE ON FASTENER HOLE #6 AT THE DOUBLE JOGGLE AREA OF THE RH FRAME 20 AROUND PASSENGER SERVICE DOOR. COMPLIED WITH ER/A 626357-14AD.Jun 25, 2025 · N335NB · Airbus A319114SDR SWIA2025082500624Door Frame · crackedFOUND CRACK UNDER RIGHT TRU DOOR LANDING. (C-CHECK RO 8/21/2025) INSTALLED REPAIR TO UPPER FLANGE ON SUPPORT INTERCOSTAL AT ELECTRONIC BAY FLOOR ON RIGHT TRU DOOR LANDINGCOMPLIED WITH THE ALL STEPS OF REO 690-53-11-2032 REV. --. DATED 2025-07-04.COMPLIEJun 24, 2025 · N804SK · Cndair CL6002D24SDR SWAA2025072985116Beam · crackedCRACK NOTED ON FSD NR 4 BEAM (141A6536-14) IN RADIUS ADJACENT TO MOST I/B FASTENER; L: 0.4. CRACK ON FSD NR 4 BEAM. REPAIRED ON CUSTOMER RO NO: P007KHVS-1.Jun 24, 2025 · N296WN · Boeing 7377H4SDR SWAA2025072985117Beam · crackedCRACK NOTED ON FSD NR 5 BEAM IN RADIUS ADJACENT TO MOST OTBD FASTENER, L: 0.4. CRACK ON FSD NR 5 BEAM IN RADIUS ADJACENT TO MOST O/B FASTENER; L: 0.4. REPAIRED ON CUSTOMER RO P007KHVS-1 JN 584186.Jun 24, 2025 · N296WN · Boeing 7377H4SDR AALA202507049792Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON FASTENER HOLE OF FR 36 RESSURE DECK MEMBRANE AT -Y1292 -2 INCHES. CRACK DIRECTION 12 OCLOCK LOOKING UP AND AFT. C RACK D= 0.110 INCH. MAINTENANCE REPLACED CORNER FITTING LOC. FR 36 PRESSURE DECK MEMBRANEJun 24, 2025 · N766US · Airbus A319112SDR AALA202507015404Pressure Deck · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON FASTENER HOLE OF FR 36 PRESSURE DECK MEMBRANE AT -Y1292 -9 INCHES. CRACK DIRECTION 1 OCLOCK LOOKING UP AND AFT. CR ACK D= 0.100 INCH. MAINTENANCE PERFORMED TIME LIMIT REPAIR ON FR 36 PRESSURE DECK MEMBRANJun 24, 2025 · N766US · Airbus A319112SDR DALA2025063004834Beam · corroded(LOG 1043697) CORROSION ON BEAM UPPER AND LOWER AREAS STA 947.5 AND 53.0 LBL AT W2. BEAM UPPER AND LOWER AREAS STA 947.5 AND 53.0 LBL AT W2 WAS REPAIRED PER B737-800 SRM 53-70-51-2R POCEDURE 5 REPAIR 5.Jun 24, 2025 · N3771K · Boeing 737832SDR VNAA20250625006Pulley Bracket · chafedHN00246730 DISCREPANCY: FOUND RH SIDE FS280 AILERON PULLEY BRACKET TO BE CHAFED AND REQUIRE REPLACEMENT. CORRECTIVE ACTION: LOCATED AND DRILLED NEW BRACKET P/N CC670-94802-7-01, AND TRANSFERRED BRACKET FROM OLD PULLEY IAW CRJ-700-SRM-51-40-11-001-001-A01 AND 5Jun 24, 2025 · N530EA · Cndair CL6002C10SDR AALA202508090339Fitting · burredAIRCRAFT IN BASE MAINTENANCE: DAMAGE RACK 80VU BURRED MATERIAL ON LOWER LATERAL FITTING LH IN AFT AVIONIC COMPARTMENT MEASURE BURRED MATERIAL IS L=0.027 INCH. MAINTENANCE PERFORMED INTERIM REPAIR, REPLACEMENT LOWER LATERAL FITTING LH LOC. ON AFT LOWER AVIONICJun 23, 2025 · N770UW · Airbus A319112SDR AALA202508091529Fitting · burredAIRCRAFT IN BASE MAINTENANCE: DAMAGE RACK 80VU BURRED MATERIAL ON LOWER LATERAL FITTING RH AND WAS FOUND IN CONTACT WITH STRUCTURE IN AFT AVIONIC COMPARTMENT MEASURE BURRET MATERIAL 0.116 INCH. MAINTENANCE PERFORMED INTERIM REPAIR, REPLACEMENT LOWEJun 23, 2025 · N770UW · Airbus A319112SDR SWIA2025071600623Beam · corrodedREAR FUSELAGE L/H BEAM CORRODED FR 86 TO FR 89. REMOVED AND REPLACED REAR FUSELAGE LH BEAM AT FR86-89, REF EMB SRM 51-40-08. LH BEAM REPLACED WITH OEM PART. THERE IS NO CHANGE TO WIEGHT AND BALANCEJun 23, 2025 · N121SY · Emb ERJ170200LRSDR SCNA20250707246Pressure Deck · crackedCRACK OF 0.625 IN LENGTH ON VERTICAL PRESSURE WEB AT LEFT SIDE OF VERTICAL PRESSURE DECK WEB STA 663 LBL 34 IN REFERENCE TASK CARD ENG-57SCA-11508 STEP 5. A). PRESSURE WEB AT LEFT SIDE OF VERTICAL PRESSURE DECK WEB STA 663 LBL 34 WAS REPAIRED PER B737-800 SRMJun 23, 2025 · N841SY · Boeing 737800*SDR SWIA2025070100623Buttstrap · damagedREPAIR FS 280 LOWER BUTT-STRAP BETWEEN STR25L (C-CHECK RO 06/29/2025)PERFORMED REPAIR FS 280 LOWER BUTT-STRAP BETWEEN STR25L BY COMPLYING WITH REO 690-53-21-1936 REV-- DATED 2025-06-27, COMPLIED WITH 51-900-1002-SKY, LEAK CHECK PASSEDJun 23, 2025 · N800SK · Cndair CL6002D24SDR CALA2025062505867Sill Drain · odorOVERWHELMING PUTRID ODOR PESENT THRU OUT ENTIRE CABIN AND COCKPIT. FOWARD CARGO PIT WAS FULL OF FISH ON ARRIVAL FISH WATER / JUICE WAS COMMING OUT OF FUSELAGE DRAIN HOLES SUGGEST MM 51-00-62-200-801 AND AMM 25-52-00-100-801 FOR CLEAN UP AND SMELL REMOVAL REMOJun 23, 2025 · N62884 · Boeing 737924ERSDR ASAA2025062259613Frame · crackedFUSELAGE BS 727B LEFT IS CRACKED AT THE AC RAIL SUPPORT BRACKET INBD FASTENER HOLE. GROUNDED - YES. REPAIRED BS 727B LEFT IAW TC AD20241807-700-25-1L FIG 5.Jun 22, 2025 · N644AS · Boeing 737790SDR SIMA20250622002Seal Rest · corrodedSSI 53-21-009: FWD CARGO DOOR FUSELAGE CUTOUT LOWER EDGE IS CORRODED AT 2 HOLES. (MAJOR REPAIR) (LEVEL 2 CORROSION). RAR FWD CARGO DOOR FUSELAGE CUTOUT LOWER EDGE (SEAL REST) IAW ERJ 175 SRM 51-40-08.Jun 22, 2025 · N245NN · Emb ERJ170200LRSDR CALA2025072206838Pressure Web · crackedCENTER WING BOX REAR SPAR VERTICAL PRESSURE WEB HAS CRCK INDICATION BETWEEN RBL 31.83 AND RBL 40 (LENGTH 2") RBL 40- RBL 45. 64 (LENGTH 2" ) (REF AAR NR 1000038 596)REPAIRED DAMAGE CRACK AT THE CENTER WING REAR SPAR VERTICAL PRESSURE WEB BETWEEN RBL 31.83 ANJun 22, 2025 · N14228 · Boeing 737824SDR SWAA2025071584305Crease Beam · corrodedCORROSION CREASE BEAM AT LEVEL STA 639 RBL 64 AND WL 208.1 AT PASSENGER CABIN. REPLACED CREASE BEAM (INNER CHORD) AND FASTENERS AT LEVEL BTW STA 613 TO BS 664 RBL 64 AND WL 208.1 AT PASSENGER CABIN IAW SRM 51-40-02; SRM 51-10-02 Ï¿½TEM 9 AND DWG 144A5901 SHEEJun 22, 2025 · N429WN · Boeing 7377H4
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