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 97ZZZX1266Longeron · corrodedDURING MPV MAINTENANCE CHECK, FOUND CENTER W/W TUNNEL LONGERON 48L LOWER FLANGE BADLY CORRODED, STA 1506. SUSPECT CAUSE WAS MOISTURE. PROPER APPLICATION OF CORROSION PREVENTIVE COULD PREVENT RECURRENCE.SDR USAA960786Stringer · corrosionROA - DURING CX-1 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 5 INCH CORROSION STRINGER 27L BS 957 TO 962. REMOVED CORROSION AND INSTALLED STRINGER SPLICE. REPAIRED PER SRM 53-10-3 FIG 1. (M)SDR CALA9700385Longeron · corrodedINSPECTION FOUND LONGERON 4L CORRODED BETWEEN BS 1119 TO 1139. THE CORRODED SPLICE WAS REMOVED AND A NEW ONE WAS FABRICATED AND INSTALLED IAW SRM 53-10-00 FIGURE 3, 53-13-01 FIGURE 33 AND 51-21-01.SDR CALA9601788Stringer · corrodedINSPECTION FOUND FUSELAGE STRINGER 24L CORRODED FROM FS 970 TO 1000. THE CORRODED SECTION OF STRINGER WAS REMOVED IAW SRM 51-10-6. STRINGER REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 53-10-3, 51-10-2 AND 51-30-2.SDR SWAA961361Stringer · crackedDURING SCHEDULED D-CHECK, FOUND STRINGER CRACKED AT BS 498, S23R. REPLACED DAMAGED SECTION PER BOEING SRM.SDR HAL960129Longeron · corrodedDURING C-CHECK, FOUND CORROSION ON THE LONGERON OUTBOARD OF THE LOWER LEG OF 51L AT STATION 1330 TO 1340. REPAIRED LONGERON PER SRM 53-10-00. TREATED AND PRIMED PER SRM 51-21-01. (M)SDR GTIA9700129Longeron · corrodedMHV - SURFACE CORROSION WITH EXFOLIATION ON LONGERON DIRECTLY BENEATH OUTFLOW VALVE IN AFT PIT, RIB ANGLE IN FRONT OF OUTFLOW VALVE HAS SURFACE CORROSION DOWN AND TO RT OF VALVE. REMOVED CORRODED STRAP, FABRICATED NEW PART ALODINED, PRIMED, AND INSTALLED IAW SDR COMA9610379Stringer · corrodedINSPECTION REVEALED THE FUSELAGE FWD SECTION OF STRINGER 18L CORRODED. THE STRINGER WAS REPAIRED PER AERODESIGN REPORT NR 1990-A, REV IR, DATED 11-6-96.SDR COMA9610347Stringer · corrodedDURING 2C INSPECTION, FOUND FUSELAGE STRINGER 18L CORRODED AT FWD END, FS 4088.0. REPAIRED STRINGER PER AERODESIGN REPORT NR 1990-2, REV IR DATED 9-15-96.SDR AALA961780Stringer · crackedTUL - FOUND STATION 720B STRINGER 15L CRACKED AT END. REMOVED STRINGER, MADE FILLER, REPLACED AND REPAIRED WITH U-CHANNEL AND SPLICE REPAIR PER SRM 51-10-3. (M)SDR AALA961779Stringer · gougedTUL - FOUND STRINGER 28L DEEP GOUGES AND DENTED STATION 450-480. INSTALLED STRINGER SPLICE ON STRINGER 28L, STATION 450-480 PER SRM 51-10-1 PAGE 4. (M)SDR USAA960784Stringer · corrosionROA - DURING CX-4 CHECK, VISUAL INSPECTION FOUND 2 INCH BY 12 INCH CORROSION, STR 27L, BS 967. REMOVED CORROSION AND INSTALLED DOUBLER AND SPLICED, REPAIRED PER SRM 53-10-3, FIG 1. (X)SDR MZZA96181Stringer · corrodedTNN - DURING 1/4 D-CHECK INSPECTION ON A/C AT AIR ASIA, SEVERE CORROSION WAS FOUND ON FORWARD CARGO COMPARTMENT STRINGER 28R BETWEEN BS 700 AND BS 720. THE CORRODED STRINGER FROM BS 684 TO BS 725 WAS TRIMMED OUT AND REPLACED WITH NEW HAT SECTION STRINGER PER SDR GTIA9700125Stringer · corrodedMHV - NUMEROUS PATCHES OF SURFACE CORROSION ALONG TOP OF RIGHT STRINGER FORWARD OF AFT CARGO DOOR TO FORWARD BULKHEAD OF AFT PIT. SECTION CLOSEST TO CARGO DOR IS DELAMINATING. REMOVED BOTH ENDS, FABRICATED AND INSTALLED (2) SPLICES AND (2) ENDS IAW SRM 53-02SDR 9626239952Longeron · crackedDURING PERIODIC CHECK, FOUND LONGERON 30 'T' CHORD CRACKED IN RADIUS AT FS 609, RIGHT KEEL AREA. REPAIRED PER EA 99-120157.SDR USAA960782Stringers · crackedPIT - DURING FC-1 CHECK, FOUND .5 INCH CRACK AND 1.625 INCH CRACK IN FRAME 22293 AT STRINGER NR 54 AND AT STRINGER NR 56. STOP DRILLED AND INSTALLED REPAIR ANGLES PER EA 34103. (M)SDR MZZA96172Stringer · corrodedTNN - DURING 1/4 D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, INTERGRANNULAR CORROSION WAS FOUND ON AFT CARGO COMPARTMENT AT STRINGER 27R OUTBOARD CHORD BETWEEN BS 950E AND 950E PLUS 5. THE CORRODED STRINGER 27R OUTBOARD CHORD WAS CLEAN UP AND REPAIRED PER EC/SDR ABXA9700166Longeron · crackedWHILE COMPLYING WITH A C INSPECTION, FOUND LONGERON 4 LEFT CRACKED AT FS 446. REPAIRED LONGERON 4 LEFT IAW ABX REA D953-17397-MR.SDR 97ZZZM297Longeron · corrodedDURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND FORWARD CARGO PIT CORRODED AND BLOWN OUT SPLICE, AT BULKHEAD STATION 218 TO STATION 237 LONGERON 29R. REMOVED CORROSION AND SPLICE FOUND TO BE OUT OF LIMITS, IAW DC-9 SRM 53-01 FIG 1. REMOVED LSDR 97ZZZM296Longeron · corrodedDURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND THE FORWARD PIT LONGERON 29R HAS CORROSION UNDER LONGERON, AT SPLICE BETWEEN STATION 218 BULKHEAD AND STATION 237. REMOVED SPLICE IAW DC-9 SRM 51-30-2, CORROSION ON SPLICE FOUND TO BE OUT OF LIMISDR 97ZZZM280Longeron · corrodedDURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND E/E BAY LONGERON 29L AND 29R CORRODED BEYOND LIMITS FUSELAGE STATION 120, AND L30. CORRODED LONGERONS 29L, 29R AND 30 REMOVED 3 NEW LONGERONS FABRICATED IAW DC-9 SRM 53-11-1. LONGERONS TREATED ASDR 97ZZZM278Longeron · crackedDURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND FORWARD CARGO COMP LONGERON 29R END FITTING CAP CRACKED AT STATION 580 APPROXIMATELY 2 INCHES LONG. REMOVED FASTENERS, REMOVED CRACKED END CAP FITTING, DRILLED NEW FITTING, TREATED AND INSTALLED SDR 97ZZZM142Longeron · corrosionDURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND CORROSION IN THE SKIN AT STATION 580 LONGERON 30, LEVEL 2. (M)SDR 97ZZZM140Longeron · corrodedDURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND E/E BAY LONGERON 29L AND 29R CORRODED BEYOND LIMITS FS 120 AND L30.SDR 97ZZZM139Longeron · corrodedDURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND FORWARD CARGO PIT CORRODED AND BLOWN OUT SPLICE AT BULKHEAD STATION 218 TO STATION 237 LONGERON 29R. (M)SDR 97ZZZM138Longeron · crackedDURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND FORWARD CARGO COMP LONGERON 29R END FITTING CAP CRACKED AT STATION 580 APPROX 2 INCHES LONG. (M)SDR 97ZZZM137Longeron · corrodedDURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND THE FORWARD PIT LONGERON 29R HAS CORROSION UNDER LONGERON AT SPLICE BETWEEN STATION 218 BULKHEAD AND STATION 237. (M)SDR HAL960121Stringer · corrodedDURING C-CHECK, FOUND CORROSIONI ON STRINGER 52 FROM STATION 814 TO 820 IN THE FORWARD CARGO COMPARTMENT. REMOVED CORRODED STRINGER AND REPLACED WITH ATTACHED SPLICES PER AARD 51-01-00. (M)SDR USAA960770Stringer · corrodedINT - DURING Q-4 CHECK, VISUAL INSPECTION FOUND 4 INCH BY 2 INCH CORRODED STRINGER AT S28L BS 525. INSTALLED DOUBLER, REPAIRED PER EA 41784. CORROSION TASK NR: C53-208-01. CORROSION LEVEL: 2. (X)SDR 97ZZZX1768Longeron · crackedDURING A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND .75 INCH CRACK AT FASTENER HOLE LONGERON 12L STA 645. REMOVED CRACKED AREA, FABRICATED 2 EACH STACKED ANGLE REPAIRS IA-4150-2 2024-T3 .040 INCH 5 INCHES BY 2 INCHES IAW DC9 SRM 53-01 FIG 2. SDR 97ZZZM144Longeron · crackedDURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND THE FORWARD PIT FRAME AT FS 389 AND LONGERON 30 FRAME CRACKED AT BOTTOM, CRACK LENGTH 3, 1 INCH. (M)SDR 97ZZZM143Longeron · crackedDURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND THE FORWARD PIT FRAME AT FS 408 AND LONGERON 30 FRAME WAS CRACKED AT THE BOTTOM, THREE 1 INCH CRACKS. (M)SDR SWAA961296Stringer · crackedDURING SCHEDULED D-CHECK, FOUND STRINGER 16R AT BS 520 CRACKED. REPLACED STRINGER PER BOEING SRM.SDR USAA960762Stringer · corrodedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .5 INCH BY 3 INCH CORRODED AREA BS 500 D PLUS 2 INCHES STRINGER 28R. REMOVED CORRODED AREA INSTALLED REPAIR PARTS COMPLETED REPAIR, REPAIRED PER SRM 53-30-12 FIG 202. (M)SDR MZZA96151Stringer · corrodedTNN - DURING 1/4 D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, SEVERE CORROSION WAS FOUND ON FORWARD CARGO COMPARTMENT STRINGER 26L BETWEEN BS 706 AND BS 710. THE CORRODED STRINGER FROM BS 704 TO BS 712 WAS TRIMMED OUT AND REPAIRED PER B727 SRM 53-10-3 FIGURE 1SDR HAL960117Longeron · corrodedDURNG C-CHECK, FOUND CORROSION ON LONGERON 51R BETWEEN STATION 1964 AND STATION 1975. INSTALLED LONGERON SPLICE REF SRM 53-10-00. ALL PARTS ALODINED, PRIMED AND SEALED PER SRM 51-21-01. (M)SDR RAIA961168Stringer · corrosionSTL - FOUND CORROSION ON STRINGER 21L FROM 40 TO 41. MAINTENANCE TREATED MINOR CORROSION. (M)SDR RAIA961167Stringers · corrosionSTL - MAINTENANCE FOUND CORROSION ON STRINGERS 21R AND 21L BETWEEN FRAMES 23 AND 25. MAINTENANCE TREATED MINOR CORROSION. (M)SDR RAIA961166Stringers · corrosionSTL - FOUND CORROSION ON STRINGER 21L AND 21R BETWEEN FRAME 16 AND 18. MAINTENANCE TREATED MINOR CORROSION PER ATR SRM 51-21-42. (M)SDR GTIA9700123Longeron · corrodedMHV - LONGERON IN 3RD LEFT SIDE BAY FOR AFT BULKHEAD OF AFT PIT IS CORRODED HAS ABOUT 8 INCHES SECTION OF EXFOLIATION. FABRICATED, TREATED, FINISHED, AND INSTALLED A NEW STIFFENER PER THE FOLLOWING SRM'S 51-10-0, 51-10-3, AND 51-30-4. (M)SDR GAIA9636Longeron · crackedDURING C-CHECK INSPECTION, REVEALED TWO CRACKS ON LONGERON 30 BY THE PRODUCTION SPLICE AT FUSELAGE STATION 360. REPAIRED LONGERON IAW KITTY HAWK EA D9-35-040. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR CALA9601895Longeron · crackedINSPECTION FOUND A 1 INCH CRACK IN LONGERON 16L AT STA 965. THE LONGERON WAS REPLACED IAW SRM 53-02.SDR CALA9601894Longeron · crackedINSPECTION FOUND A .75 INCH CRACK IN LONGERON 12L, 12R, AND 13R AT STA 965. SPLICE REPAIRS WERE INSTALLED IAW SRM 53-02, FIGURE 2A.SDR CALA9601778Longeron · crackedINSPECTION FOUND A 1 INCH CRACK IN LONGERON 17L AT STA 965. A LONGERON REPAIR WAS INSTALLED IAW SRM 53-02, FIGURE 2A.SDR 97ZZZM294Longeron · crackedDURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND A 2 INCH CRACK IN THE FORWARD PIT AT FS 389 LONGERON 30. REMOVED CORROSION MATERIAL LOSS .001 TO .002 WITHIN LIMITS TREATED AND PRIMED IAW DC-9 SRM 51-10-3, 51-30-3. (M)SDR 97ZZZM281Longeron · corrosionDURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND CORROSION IN THE E/E COMP AT L30 FROM STATION 160 TO 218. LONGERON 30 CORRODED BEYOND LIMITS IAW DC-9 SRM 53-01. LONGERON REMOVED BETWEEN STATION 160 AND STATION 229. NEW LONGERON FABRICATED IASDR 97ZZZM135Longeron · crackedDURNING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND A CRACK IN THE FORWARD PIT FRAME AT FS 408 AND LONGERON 30. (M)SDR 9627493202Longeron · corrodedDURING C-CHECK, THE FLOOR STRINGER AT FRAME 68, Y 1270 LEFT SIDE WAS FOUND WITH AREAS OF CORROSION. REPAIRED PER EA 32-106173.SDR RAIA961137Stringer · corrosionSTL - FOUND CORROSION ON STRINGER 17L FROM FRAME 34-39. MAINTENANCE TREATED CORROSION PER ATR SRM 51-21-42. (M)SDR RAIA961136Stringer · corrosionSTL - FOUND CORROSION ON STRINGER 20L AT FRAME 32. MAINTENANCE TREATED CORROSION PER ATR SRM 51-21-42. (M)
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