JASC 5313
Service difficulty reports · 36,313
Reports filed under 5313 · Fuselage Main, Longeron/Stringer, 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 = '5313' 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 = '5313' 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 9902639975Intercostal · crackedDURING PERIODIC CHECK, FOUND INTERCOSTAL 9911557-3 AT FS 154, LONGERON 14R CRACKED. REPAIRED PER EA 99-164421.SDR USAA990616Stringer · corrodedTPA - DURING CX-4 CHECK, FOUND CORROSION ON STRINGER .5 INCH BY 3 INCH AT STATION 1006 STRINGER 27L. REMOVED AND REPLACED STRINGER THAT WAS CORRODED, CLEANED AND TREATED SAME PER SRM 53-10-3 AND EA 64746. (M)SDR UPS99830026Longeron · crackedINSPECTION TYPE:C2 LONGERON 33R IS CRACKED BETWEEN FS 600 AND 620. CUT OUT DAMAGED SECTION AND REPAIRED IAW DH SK750-128X.SDR ABXA9900585Fitting · crackedFITTING CRACKED AT STATION 1180 AND LONGERONS 34 LEFT TO 35 LEFT. REPAIRED IAW DC8 SRM 51-1-20D AND 53-2-0.SDR AALA990910Longeron · corrodedTUL - FOUND CORROSION ON LONGERON 58 FORWARD OF FRAME 57.1. REPAIRED PER 53-10-14-2. (M)SDR HNAA9900087Stringer · corrodedSTRINGER 25S HAS CORROSION AND PITTING AT X504, REMOVAL OF THE RIVET REQUIRED. REMOVED RIVET AT LOCATION, EVALUATED AND BLENDED CORROSION FOUND AREA OUT OF LIMITS APPROX .013. BLENDED AND REMOVED ALL CORROSION, INSTALLED NESTED ANGLE AS SAME TYPE AS STRINGERSDR 99ZZZX2923Stringer · corrodedDURING A C-CHECK, CORROSION WAS NOTED ON STR 29R, BS 1090.SDR SWAA991043Stringer · crackedDURING SCHEDULED SPECIAL VISIT CHECK, FOUND STRINGER 19R 2 EACH CRACKS, BS 276, AND BS 310. REPAIRED STRINGER PER SRM.SDR SWAA991042Stringer · crackedDURING SCHEDULED SPECIAL VISIT CHECK, FOUND STRINGER 4L CRACKED, BS 907. REPAIRED STRINGER PER SRM.SDR ABXA9900472Longeron · crackedDURING C-CHECK, FOUND LONGERON 16 RIGHT CRACKED AT AFT SIDE OF RIGHT FORWARD PYLON BULKHEAD, STATION 1041. REPAIRED LONGERON IAW DC9 SRM 53-02.SDR TWAA9909003Stringer · crackedDURING CHECK-C MAINT FOUND AT STA 412 AND STRINGER 34R THE STRINGER WAS CRACKED DUE TO CORROSION IN TWO PLACES. REMOVED 29 IN DAMAGED SECTION AND INSTALLED NEW SECTION WITH SPLICE REPAIR PER SRM 53-00-03.SDR TWAA9909002Stringer · corrodedDURING CHECK-C MAINT FOUND CORROSION AT APPROXIMATELY STA 412, STRINGER 36R. REMOVED 26 INCH LONG DAMAGED SECTION OF STRINGER 36R AND INSTALLED NEW SECTION PER SRM 53-00-03.SDR SWAA991032Stringer · crackedDURING SCHEDULED D CHECK, FOUND STRINGER 10R CRACKED AT BS 767, BS 787, BS 807, BS 827, AND BS 847. REPAIRED STRINGER PER SRM.SDR SWAA991029Stringer · corrodedDURING SCHEDULED SERVICE CHECK, FOUND CORROSION ON STRINGER 27R, BS 967. REPAIRED STRINGER PER SRM.SDR RRXA991395Longeron · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, LONGERON 31 LEFT AT STA 1220. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED PLATE DOUBLER IAW DC8 SRM 51-1-21 AND IAW FAA APPROVED TENNESDR MZZA99126Stringer · corrodedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 4 INCH BY 32 INCH AREA CORROSION WAS FOUND ON STRINGER 26R BETWEEN BS 448 AND BS 480. THE CORRODED PART OF STRINGER WAS TRIMMED AND REPAIRED PER B727 CHAPTER 53-10-03 FIG 1. (M)SDR HNAA9900075Stringer · corrodedSTRINGER 31S HAS PITS AT TWO RIVETS, LOCATED AT APPROX X520 & X517. RIVETS NEED REMOVED FOR FURTHER EVALUATION. REMOVED FIVE RIVETS AT STRINGER 31S APPROX X520 & X517. FOUND AREA EXCESSIVELY PITTED. REMOVED AND REPLACED SECTION OF STRINGER AND TENSION FITSDR HNAA9900071Stringer · corrodedSTRINGER 31S HAS PITTS AT TWO RIVETS, LOCATED AT APROX X520 AND X512. RIVETS NEED REMOVED FOR FURTHER EVALUATION. REMOVED FIVE RIVETS AT STRINGER 31S APROX X520 AND X517. FOUND AREA EXCESSIVELY PITTED. TWO AREAS OUT OF LIMITS APROX .015 AND ONE AREA IN RADSDR GTIA9901042Longeron · crackedMHV - FOUND STATION 237-277 STRINGER 16L AND STATION 237-323 STRINGER 17L LONGERONS CRACKED AT FRAME ATTACH POINTS. REMOVED AND REPLACED STRINGER 16L FROM STATION 237-277 STRINGER 17L FROM 237-323 IAW DC940 SRM 53-02 FIG 18. (M)SDR TWAA9909601Longeron · crackedDURING OP 16 MAINT CHECK, FOUND A CRACK IN LONGERON 5R, APPROXIMATELY .75 INCH LONG THROUGH RIVET STA 679. REPAIRED PER DRAWING SR09530128.SDR HNAA9900080Stringer · corrodedCORROSION IN BELLY AT STRINGER 30P AT STATION 500 (WILL NEED SPLICE). REMOVED AND REPLACED STRINGER SPLICE.SDR CALA9900673Longeron · crackedINSPECTION FOUND A 4 INCH CRACK IN LONGERON 29L SPLICE AT STA 1204. A SPLICE REPAIR WAS INSTALLED IAW SRM 51-30-5.SDR AU990916Stringer · corroded(AUS) STRINGER 58 DIMPLED LAP JOINT LOCATED IN THE RIGHT REAR FUSELAGE SKIN BETWEEN FS 16495 AND FS 17845 CORRODED.SDR UPS99229845Stringer · corrodedINSPECTION TYPE:SI, CORROSIN AND TOOLING DAMAGE ON STRINGER 7 LT BS 720B AND 1270+18. REMOVED CORROSION DAMAGE, FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. PERFORMED STRINGER REPAIR PER SRM 53-10-3.SDR SWAA991015Stringer · corrodedDURING SCHEDULED D CHECK, FOUND CORROSION AT STRINGER 27L, BS 374-378. REPAIRED STRINGER PER SRM.SDR MWEA99340Longeron · corrodedLONGERON 24L AT STATION 1375 IS EXFOLIATED. MTC FABRICATED AND INSTALLED NEW LONGERON.SDR SWAA991006Stringer · corrodedDURING SCHEDULED D-CHECK, FOUND CORROSION ON STRINGER 24R , BS 433-436. REPAIRED STRINGER PER SRM.SDR QXEA9901294Stringer · misinstalledPDX - STRINGER 50, A SECTION FROM FRAME 4900 TO SPLICE BETWEEN FRAMES 5805 AND 6305 IS INCORRECT THICKNESS FOR THIS LOCATION. REPLACED STRINGER IAW HORIZON AIR EA 4-53-824.SDR USAA990549Stringer · crackedCLT - DURING Q-1 CHECK, FOUND 2 INCH CRACK IN STRINGER 4L AT STATION 907 ABOVE TIE CLIP AT STRINGER 4L. INSTALLED SPLICE ANGLE PER EA 64679 AND SRM 51-10-02. (M)SDR GTIA9901035Longeron · crackedMHV - FOUND STATION 1041, STATION 1051 LONGERON NR 17 CRACKED BOTH MARKED IN RED. REMOVED AND REPLACED LONGERON NR 17 STATION 1041 AND 1051 AND SHOVEL CUPS PER SRM 51-10-1 AND 51-30-2 LONGERON INSTALLED USING EXISTING SPLICES. (M)SDR COMA9960257Stringer · crackedDOUBLER AFT OF FS 718 HAS APPROX 4 INCH CRACK IN RADIUS AT STRINGER 11. REPAIRED PER WVAC EO NR 601R-53-0058.SDR C2XA99IA304Stringer · corrodedIAH - DURING C-CHECK INSPECTION, STRINGER 17 RIGHT WAS FOUND TO BE CORRODED BETWEEN FRAMES 27 AND 30. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF STRINGER IAW ATR42-320 SRM 51-25-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA99IA303Stringer · corrodedIAH - DURING C-CHECK INSPECTION, STRINGER 19 RIGHT WAS FOUND TO BE CORRODED BETWEEN FRAMES 27 AND 29. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF STRINGER IAW ATR42-320 SRM 51-25-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA99IA302Stringer · corrodedIAH - DURING C-CHECK INSPECTION, STRINGER 18 RIGHT WAS FOUND TO BE CORRODED BETWEEN FRAMES 27 AND 30. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF STRINGER IAW ATR42-320 SRM 51-25-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR RRXA991559Longeron · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO LONGERON 34 RIGHT, AT STA 1260. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW LONGERON SECTION IAW DAC DRAWING 5754184. (CORROSISDR RRXA991557Longeron · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO LONGERON 34 LEFT, BETWEEN STA 1240 AND STA 1260. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW LONGERON SECTION IAW DAC DRAWING 3SDR RRXA991547Longeron · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO LONGERON 35 RIGHT AT STA 1280. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW LONGERON SECTION IAW DAC DRAWING 3646937. (CORROSIONSDR RRXA991534Longeron · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, LONGERON 34 RIGHT AT STA 580. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW LONGERON SECTION IAW DC8 SRM 53-1-20 FIGURE 1. (CORROSISDR RRXA991529Longeron · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION TO LONGERON 32 RIGHT, BETWEEN STA 460 TO STA 600. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. REPAIRED LONGERON 32 RIGHT BY CLAD PLATING AND INSTALLED IAW DC8 SRM 51-1-21SDR MWEA99344Longeron · crackedLONGERON 3L IS CRACKED AT STATION 160. MTC FABRICATED AND INSTALLED LONGERON AND SPLICE.SDR CALA9900655Stringer · crackedINSPECTION FOUND A CRACK IN STRINGER 22L AT STA 1610-1640. A STRINGER SPLICE REPAIR WAS PERFORMED IAW SRM 53-00-03 AND ECRA 5331-01055.SDR ABXA9900403Longeron · crackedDURING C-CHECK, FOUND LONGERON 26 LEFT CRACKED AT STATION 945. REPLACED LONGERON SECTION IAW DC9 SRM 51-30-2.SDR 99ZZZX2453Stringer · corrodedDURING A C-CHECK, CORROSION WAS NOTED ON STR 28R AND STR 28L AT STA 360.SDR 99ZZZX3121Bulkhead · crackedPILOT REPORTED RUDDER AND TRIM STIFFNESS. EXAMINATION FOUND BULKHEADS IN LOWER FORWARD FUSELAGE SECTION, PN 2413001-3, 2413001-4, 2413001-5, 2413001-6, CRACKED. THESE CRACKS ARE BELOW CENTER RUDDER TORQUE TUBE BEARINGS AFT ATTACH POINTS. SUBMITTER STATED THSDR 99ZZZX3120Bulkhead · crackedPILOT REPORTED RUDDER AND TRIM STIFFNESS. EXAMINATION FOUND BULKHEADS IN LOWER FORWARD FUSELAGE SECTION, PN 2413001-3, 2413001-4, 2413001-5, 2413001-6, CRACKED. THESE CRACKS ARE BELOW CENTER RUDDER TORQUE TUBE BEARINGS AFT ATTACH POINTS. SUBMITTER STATED THSDR 99ZZZX3119Bulkhead · crackedPILOT REPORTED RUDDER AND TRIM STIFFNESS. EXAMINATION FOUND BULKHEADS IN LOWER FORWARD FUSELAGE SECTION, PN 2413001-3, 2413001-4, 2413001-5, 2413001-6, CRACKED. THESE CRACKS ARE BELOW CENTER RUDDER TORQUE TUBE BEARINGS AFT ATTACH POINTS. SUBMITTER STATED THSDR 99ZZZX3118Bulkhead · crackedPILOT REPORTED RUDDER AND TRIM STIFFNESS. EXAMINATION FOUND BULKHEADS IN LOWER FORWARD FUSELAGE SECTION, PN 2413001-3, 2413001-4, 2413001-5, 2413001-6, CRACKED. THESE CRACKS ARE BELOW CENTER RUDDER TORQUE TUBE BEARINGS AFT ATTACH POINTS. SUBMITTER STATED THSDR QXEA9901265Stringer · crackedPDX - THERE IS A CRACKED STRINGER AT TOP STRUCTURE IN RIGHT-HAND MAIN LANDING GEAR STRUT BAY, DIRECTLY ABOVE THE GEAR STRUT AFT LUG. REPAIRED IAW FOKKER SRM 51-31-1 AND SRM 51-30-02.SDR USAA99089Longeron · crackedPIT - DURING Q-4 CHECK, FOUND .5 INCH CRACK IN LONGERON 5 LT AT STATION 680. CUT OUT DAMAGED SECTION AND INSTALLED LONGERON REPAIR SECTION AND SPLICES PER SRM 53-02 FIG 18. (M)SDR USAA990503Longeron · crackedPIT - DURING Q-4 CHECK, FOUND 1 INCH CRACK IN LONGERON AT STATION 965 AT LONGERON 17L. SPLICED IN LONGERON PER SRM 53-22. (M)
Back to JASC 5313