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 SWAA950782Stringer · corrodedDURING SCHEDULED MAINTENANCE, FOUND STRINGER 27L CORRODED AT BS 1006. REPAIRED PER BOEING SRM.SDR CAL960220Stringer · corrodedKUL - INSPECTION FOUND CORROSION ON STRINGER 30R AT STATION 1501. THE STRINGER WAS REPAIRED IAW SRM 53-10-00. (M)SDR 95FDEA01800Stringer · corrodedCORROSION (C53-224-01) ON STR 5R, BS 600-740. REPAIRED OUT OF LIMITS AREA IAW FEDEX EA 7-5310-26724A. C/A ADDITION.SDR 95FDEA01798Stringer · corrodedCORROSION (C53-224-04) ON STR 6R, BS 1133 AND BS 1139. REMOVED DAMAGED AREA AND REPAIRED STR IAW FEDEX EA 7-5310-26724.SDR SCNA95287Stringer · missingDURING HEAVY MAINTENANCE VISIT, A PIECE OF STRINGER 24R WAS FOUND MISSING IN THE NOSE GEAR TUNNEL AREA AT STATION 312 TO 328. APPROXIMATELY 1 INCH BY .3750 INCH OF MATERIAL WAS MISSING. FABRICATED AND INSTALLED STRINGER REPAIR IAW B727 SRM 51-30-1, 51-8-1, 5SDR MWEA95521Longeron · corrodedDURING D-CHECK, FOUND RT LONGERON 20 OUTBOARD MEMBER TO BE CORRODED TO EXCESS IN ONE BOLT HOLE AND ALONG THE RADIUS OF THE ANGLE AT STA 730. REPLACED THE OUTBOARD LONGERON MEMBER IAW SRM 51-30.SDR MWEA95501Longeron · corrodedDURING D-CHECK, FOUND LONGERON 21R HAS LIGHT CORROSION LOCATED BETWEEN STA 237 AND 256. REPLACED THE LONGERON SECTION IAW SRM 51-30.SDR MWEA95500Longeron · corrodedDURING D-CHECK, FOUND LONGERON 21R HAS CORROSION JUST AFT OF STA 218 FRAME. REPLACED LONGERON SECTION IAW SRM 51-30.SDR MWEA95491Longeron · corrodedDURING D-CHECK, FOUND LIGHT CORROSION ON LONGERON 29R IN KEEL AREA UNDER THE AUXILIARY HYD RESERVOIR AND ON KEEL WEB. NEW LONGERON WAS INSTALLED IAW SRM 51-10-3.SDR MWEA95490Longeron · corrodedDURING D-CHECK, FOUND LIGHT CORROSION AND BARE METAL ALONG LONGERON 29L IN KEEL AREA AT STA 658-676. A NEW LONGERON WAS INSTALLED IAW SRM 51-10-3.SDR MWEA95468Longeron · crackedDURING D-CHECK, FOUND LONGERON 24R CRACKED AT STA 455. REPLACED THE LONGERON WITH EXTRUSION P/N 27779225 IAW SRM 51-30.SDR MWEA95467Longeron · damagedDURING D-CHECK, FOUND LONGERON 25R DAMAGED AT STA 313. REPLACED THE LONGERON WITH EXTRUSION P/N 2777922-3 IAW SRM 51-30.SDR MWEA95466Longeron · crackedDURING D-CHECK, FOUND LONGERON 25R CRACKED AT FS 455. REPLACED THE LONGERON WITH EXTRUSION P/N 2777922-5 IAW SRM 51-10-4.SDR MWEA95465Longeron · oversized holesDURING D-CHECK, FOUND NUMEROUS LARGE HOLES IN LONGERON THAT WERE LEFT OVER FROM A PREVIOUS REPAIR AT FS 313-332 ON LONGERON 22R. REPLACED THE LONGERON SECTION IAW SRM 51-30 FROM FS 229 TO 370.SDR MWEA95464Longeron · oversized holesDURING D-CHECK, FOUND NUMEROUS LARGE HOLES IN LONGERON THAT WERE LEFT OVER FROM A PREVIOUS REPAIR AT FS 313-332 ON LONGERON 21R. REPLACED THE LONGERON SECTION IAW SRM 51-30.SDR MWEA95450Longeron · oversize holeDURING D-CHECK, FOUND ONE LONGERON WITH OVERSIZED HOLES IN SEVERAL PLACES AT STA 570, LONGERON 26L. REPLACED THE LONGERON AND SPLICE IAW SRM 53-04, FIG 2, FROM STA 551 TO STA 579.SDR MWEA 95473Longeron · corrodedDURING D-CHECK, FOUND CORROSION IN LONGERON 20 IN RT MLG WHEELWELL WHERE FS FRAME 718 MEETS LONGERON 20. REPLACED LONGERON 20 AS PER THE SRM 51-30.SDR ABXA9600202Longeron · corrodedDURING C-CHECK INSPECTION, FOUND LONGERON 30 CORRODED AT STA 752 TO 756. REPAIRED IAW ABX REA D953-13747-MR.SDR 95FDEA01907Stringer · crackedMAIN CARGO STR 15R CRACKED STA 720B JUST FWD OF ICE LIGHT. INSTALLED REPAIR PER SRM 53-10-3, PG 4D.SDR 95FDEA01906Stringer · crackedUPPER LOBE STA 15L CRACKED STA 720B (AT ICE LIGHT). REPAIRED STR 15L CRACK IAW SRM 53-10-3 AND ATTACHED JOB PROGRESS FORM.SDR 95FDEA01905Stringer · crackedUPPER LOBE STR 15L CRACKED STA 720B (AT ICE LIGHT). STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 53-10-3.SDR 95FDEA01877Stringer · corrosionCORROSION ON STR 27R AT BS 541. REPAIRED STR PER FEDEX SRM 53-10-3.SDR USAA951311Stringer · crackINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK S-16R, BETWEEN STATION 500B AND 520, ON STRINGER. INSTALLED STRINGER REPAIR, REPAIRED PER EO 5393X228. (M)SDR USAA951310Stringer · crackedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK STRINGER 16 L, BETWEEN STATION 500B AND STATION 520, ON STRINGER. INSTALLED STRINGER REPAIR, REPAIRED PER EO 5393X228. (M)SDR USAA951308Stringer · gougedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .5 INCH GOUGE IN STRINGER OUTBOARD 'J' SECTION, STATION 1044 STRINGER 27L. INSTALLED REPAIR DOUBLER UNDER 'J' LEG OF STRINGER, AFTER SMOOTHING GOUGE. REPAIRED PER SRM 53-10-3 FIG 1. (M)SDR USAA951305Stringer · gougedINT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND DEEP GOUGE .25 INCH BY 2 INCHES IN UPPER INBOARD LEG OF S26L, BS 1044. INSTALLED STR REPAIR, LESS THAN 1 POUND ADDED, REPAIRED PER SRM 53-10-3, FIGURE 1. (X)SDR USAA951285Stringer · corrosionINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND CORRODED AREA 12 INCH BY 1 INCH AT S-26 R, BS 974 TO BS 986 ON STRINGER. SPLICED NEW STRINGER SECTION IN, REPAIRED PER SRM 53-10-3. CORROSION TASK NR C53-208-01, CORROSION LEVEL 2. (M)SDR USAA951284Stringer · corrosionINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND CORRODED AREA 5 INCH BY 1 INCH S-25 L BS 968 ON STRINGER. INSTALLED DOUBLER WEIGHT CHANGE LESS THAN 1 LB. REPAIRED PER SRM 53-10-3. CORROSION TASK NR C53-208-01, CORROSION LEVEL 2. (M)SDR USAA951283Stringer · corrodedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND CORRODED AREA 6 INCH BY 1 INCH S-27 L, BS 1004 TO BS 1010 ON STRINGER. SPLICED IN NEW STRINGER SECTION WEIGHT CHANGE LESS THAN 1 LB. REPAIRED PER SRM 53-10-3. CORROSION TASK NR C53-208-01, CORROSION LEVEL 2. (SDR USAA951270Stringer · gougedINT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND 3 INCH BY .25 INCH HOLE GOUGED IN OUTBOARD J-SECTION OF STRINGER, STA 1050, STR 27L. FORMED AND INSTALLED DOUBLER FOR J-LEG OF STRINGER, REPAIRED PER SRM 53-10-3, FIGURE 1. (X)SDR AALA952042Stringer · corrodedTUL - CORROSION ON STRINGER AND FLANGE SUPPORT FOR DUCT. STR 45R AND FR 33-34. REMOVED CORROSION AND INSTALLED STRINGER DOUBLER REPAIR PER A300 SRM 53-10-14, PP 202. TREATED, PRIMED, AND PAINTED. TST, 21,241.75 HOURS. CYCLES, 8,851. (X)SDR 9521539969Longeron · crackedDURING A SPECIAL MAINTENANCE VISIT, FOUND A CRACK IN LONGERON 16R IN THE CENTER FUEL TANK. REPAIRED PER EA 99-87836.SDR 9520873213Longeron · corrosionDURING 1C1 MAINTENANCE VISIT, FOUND CORROSION ON STRINGER 41R BETWEEN FRAMES 33-34. REPAIRED STRINGER PER EA 32-104389.SDR USAA951246Longeron · crackedPIT - DURING Q-5 CHECK INSPECTION, FOUND .50 INCH CRACK IN LONGERON AT STA 313, LONGERON 16L. REMOVED DAMAGED AREA AND INSTALLED SPLICE REPAIR PER SRM 53-02, FIGURE 2. (X)SDR ABXA9600041Longerons · double drilledDURING 826AX MOD-DISCOVERED FRAME AT STATION 160, LONGERON 6-9R, STATION 280, LONGERON 7-10R AND STATION 1320, LONGERON 7-10L IS DOUBLE DRILLED. REPAIRED FUSELAGE FRAMES WITH DOUBLE DRILLED HOLES AT STATION 160, LONGERON 6-9R, STATION 280, LONGERON 7-10R AND SDR ABXA9600040Longeron · corrodedDURING 826AX MOD-DISCOVERED LONGERON 27L, FUSELAGE STATIONS 360-420 HAVE SEVERAL SPOTS OF CORROSION. REPAIRED LONGERON 27L UPPER FLANGE AT FUSELAGE STATION 360 J-420 THAT WAS CORRODED IAW ABX REA D853-12871MR.SDR ABXA9600033Longeron · corrodedDURING 826AX MOD, DISCOVERED FUSELAGE FRAME 1020 CORRODED ON UPPER FLANGE BETWEEN LONGERON 28L AND 29L. REPAIRED CORRODED FUSELAGE STATION 1020 FRAME AT LONGERON 28L, UPPER FRAME IAW ABX REA D853-13068MR.SDR ABXA9600032Longeron · corrodedDURING 826AX MOD, DISCOVERED THE LONGERON 1 AT STATION 1615 CORRODED. REPAIRED CORRODED LONGERON 1 AT STATION 1615 IAW ABX REA D853-13069MR.SDR 95FDEA01904Stringer · crackedCRACK IN INNER FLANGE OF STR 3L, STA 407. STOP DRILLED CRACK TO .25 INCH AND INSTALLED REPAIR PART NR 1 53-10-3, PG 4D, FIG 2 (7075T6.040).SDR 96ZZZX453Stringer · brokenLAX - DURING CHECK C-9C, FOUND AT AFT PRESSURE BULKHEAD, STR 56 SEVERED. REPAIRED BY FITTING/FASTENERS INSTALLATION PER SB 093-53-105. AIRCRAFT TOTAL TIME: 63,490 HOUS; 23,355 CYCLES.SDR 96ZZZX3666Stringer · corrodedWHILE PERFORMING CPCP TASK CARD NR C53-113-01.01, FOUND CORROSION BLEEDING FROM FASTENERS ON STR 26L BETWEEN STA 500 - STA 520 IN ZONE 1-13. OPEN AREA FOUND LEVEL 2 CORROSION ON STRINGER. REPLACED SECTION OF STRINGER FROM STA 480 TO STA 515. THE REMAINDER OSDR 95FDEA01860Stringer · corrodedCORROSION (C53-111-01-2), ON STRINGER 28R FROM BS 690 TO 701 ON O/B SIDE OF U-CHANNEL. THE CORROSION WAS FOUND WHILE WORKING CUSTOMER CARD NRO0235. CORROSION WAS FOUND OUT OF LIMITS PER FEDEX SRM 53-10-1. CUT OUT DAMAGED STR 28R BS 680 TO 720, BACK DRILLED SDR 95FDEA01852Stringer · gougedGOUGE IN STR 7 LT, BS 965 WL 285 LBL 58. REMOVED DAMAGED STR AND REPAIRED PER SRM 53-10-3.SDR DL72S954585Stringer · corrodedDURING INSPECTION, FOUND MISSING AND SHEARED RIVETS AT STRINGER NR 29R AT FS 1176. ALSO, FOUND STRINGER CORRODED. REPAIRED BY REPLACING SECTION OF STRINGER PER SRM 53-10-03 PG 3.SDR ABXA9600223Longeron · crackedDURING C-CHECK INSPECTION, FOUND LONGERON 16L CRACKED AT STA 965. REPAIRED LONGERON IAW DC-9 SRM 51-30-2 AND 51-30-5.SDR 96ZZZX480Longeron · crackedLONGERON LOCATED IN THE FUSELAGE, BOTTOM LEFT, CRACKS AROUND THE NUTPLATES DUE TO STRESS FROM THE STEP. SUBMITTER SUGGESTS PREVENTION MAY BE A DOUBLER SLID UNDER THE CHANNEL RIVETED TO THE SKIN. THIS WILL PREVENT THE FLEX AROUND THE NUTPLATES WHERE CRACKS OCSDR 96ZZZX464Longeron · crackedLONGERON LOCATED IN THE FUSELAGE, BOTTOM LEFT, CRACKS AROUND THE NUTPLATES DUE TO STRESS FROM THE STEP. PREVENTION MAY BE A DOUBLER SLID UNDER THE CHANNEL RIVETED TO THE SKIN. THIS WILL PREVENT THE FLEX AROUND THE NUTPLATES WHERE CRACKS OCCUR.SDR ABXA9600225Longeron · crackedDURING C - CHECK INSPECTION, FOUND LONGERON 17R CRACKED AT STA 980. REPAIRED LONGERON IAW DC-9 SRM 53-03, FIGURE 2.SDR ABXA9600224Longeron · crackedDURING C-CHECK INSPECTION, FOUND LONGERON 17L CRACKED AT STA 980 AND STA 965. REPAIRED IAW DC-9 SRM 51-30-2 AND 51-30-5.SDR SWAA950755Stringer · crackedDURING SCHEDULED D-CHECK, FOUND STRINGER FLANGE CRACKED AT BS 475, S22R. REPAIRED PER BOEING SRM.
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