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 ASOA96029Stringer · corrodedDURING C-CHECK INSPECTION, FOUND SKIN DISTORTED ON BELLY OF AIRCRAFT, RIGHT SIDE OF MARKER BEACON ANTENNA. REMOVED RIVETS, INSPECTED AND FOUND CORROSION BETWEEN STRINGER AND BELLY SKIN. SPLICED IN NEW STRINGER, SEALED AND INSTALLED IAW SRM 53-00-03 FIG 201 ASDR ASOA96028Stringer · corrodedDURING C-CHECK INSPECTION, FOUND SKIN DISTORTED ON BELLY OF AIRCRAFT, RIGHT SIDE OF TRANSPONDER ANTENNA. REMOVED RIVETS, REMOVED STRINGER, CLEANED AREA, SEALED AND INSTALLED SPLICED STRINGER IAW SRM 53-00-03 FIG 201 AND 51-22-00 FIG 5. ALL AREAS WERE TREATEDSDR ASOA96027Stringer · corrodedDURING C-CHECK INSPECTION, FOUND CORROSION AT FRAME 20, STRINGER 20R. REMOVED RIVETS, SPLICED STRINGER, CLEANED CORROSION FROM FRAME 20, STRINGER 20R AND SEALED AND INSTALLED STRINGER IAW SRM 53-00-03 FIG 201 AND 51-22-00 FIG 5. (M)SDR 96FDEA01231Stringer · corrodedDISCREPANCY: NR 00157 (011) CORROSION (C53-113-01 )(1) IN FORWARD CARGO BAY ON STR 27 AROUND BOLTS WL 148, BS 720C. CORRECTIVE ACTION: REPAIRED CRACK ON LEFT INTERNAL RIB, STR 13, AFT SIDE BS 870 TERMINAL FITTING IAW FEDEX EA 7-5310-29173.SDR UPS96220761Stringer · corrodedINSPECTION TYPE-D, STR 21R BS 460 TO 480. REPAIRED PER SRM 53-10-3.SDR UPS96220633Stringer · corrodedINSPECTION TYPE-C, FS 620 STR 26L HAS HEAVY CORROSION. FAB'D AND INSTALLED STRINGER SECTION PER SRM 53-10-3 AND 51-30-2.SDR 97ZZZX323Longeron · crackedATW - RT STRUCTURE AFT OF FRAME 50, THERE IS A DIAPHRAGM BETWEEN THE UPPER AND LOWER SPEED BRAKE LOWER HINGE LONGERONS THAT HAS A CRACK IN THE LIP OF ITS LIGHTNING HOLE, APPROXIMATELY .3750 INCH LONG. CORRECTIVE ACTION: STOP DRILLED CRACK END PER AVRO FAX. SDR 96FDEA01215Stringer · corrodedDISCREPANCY: NR 00250 (013) CORROSION (C53-111-01) ON STR 27L CHANNEL STR 536-546 LT FORWARD BAY. CORRECTIVE ACTION: **S/D** REMOVED CORRODED SECTION OF STR FROM BS 530-550 STR 27L. FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 53-10-3, FIG 1.SDR UPS96220632Stringer · corrodedINSPECTION TYPE-C, HEAVY CORROSION ON STR 26L AT STA 600. FAB'D AND INSTALLED STRINGER SECTION PER SRM 53-10-3 AND 51-30-2.SDR 96FDEA01189Stringer · crackedNR0557 AND 014, WHILE WORKING NR0540, FOUND STR 28R AT BS 1057 TO BE CRACKED AND CORRODED. *S/D* REMOVED DAMAGE STRINGER SECTION AT BS 1057 AND INSTALLED REPAIRED PER SRM 53-10-3.SDR 9614839305Longeron · crackedDURING H-CHECK, FOUND A CRACK ON LONGERON 20L AT FS 994. REPAIRED LONGERON (P/N 5936034-501) PER EA 93-105330.SDR CALA9601076Longeron · crackedINSPECTION FOUND A CRACK IN LONGERON 6L AT STA 639. A NEW LONGERON WAS INSTALLED IAW SRM 53-02.SDR CALA9601075Longeron · crackedINSPECTION FOUND A CRACK IN LONGERON 6L AT STA 699. A NEW LONGERON WAS INSTALLED IAW SRM 53-02.SDR CALA9601074Longeron · crackedINSPECTION FOUND A .1250 INCH CRACK IN LONGERON 5R AT STA 699. THE LONGERON WAS REPAIRED IAW SRM 53-02, FIGURE 2.SDR CALA9601073Longeron · crackedINSPECTION FOUND LONGERON 5L CRACKED AT STA 699. THE LONGERON WAS REPAIRED IAW SRM 53-02.SDR CALA9601072Longeron · crackedINSPECTION FOUND A .25 INCH CRACK IN LONGERON 1L AT STA 699. THE LONGERON WAS REPAIRED IAW SRM 53-02, FIGURE 4.SDR CALA9601071Longeron · crackedINSPECTION FOUND A CRACK IN LONGERON 2L AT STA 756. THE CRACKED SECTION OF LONGERON WAS REMOVED AND A NEW SECTION WAS SPLICED IN IAW SRM 53-02, FIGURE 2.SDR 9615362285Longeron · corrodedDURING H-CEHCK, FOUND CORROSION ON STR 29L AT FS 1000. REPAIRED STRINGER (P/N 65-56441) PER EA 22-105471.SDR UPS96220634Stringer · crackedINSPECTION TYPE-C, BS 1333 STR 16L IS CRACKED AT THE PRESS RELIEF DOOR. REPAIRED IAW SRM 53-10-3 AND 51-30-2.SDR 96ZZZM1200Longeron · crackedSTL - DURING SPECIAL CHECK, FOUND A CRACK IN LONGERON 1L, STATION 756. REPAIRED PER SRM 53-02, FIGURE 4, PAGE 5. (M)SDR SWAA960599Stringer · corrodedDURING SCHEDULED D-CHECK, FOUND STRINGER 25R AT BS 947 CORRODED. REPLACED CORRODED SECTION PER BOEING SRM.SDR 9614812285Longeron · corrodedDURING H-CHECK, FOUND CORROSION ON STR 29L BETWEEN BS 970 TO 990. REPAIRED STRINGER (P/N 65-56441) PER EA 22-102131.SDR AALA960963Stringer · corrodedFOUND CORROSION ON STRINGER 29R. CUT AND SPLICED NEW SECTION OF STRINGER PER SRM 53-10-3 PG 11A-11E. (M)SDR AALA960962Stringer · corrodedTUL - CORROSION ON STR 28L JUST AFT OF STA 480. REPAIRED PER SRM 53-10-3, FIGURE 1, PAGE 4. TST: 42,362 HOURS. CYCLES, 22,280. (X)SDR 96FDEA01171Stringer · corrodedNR0224 AND 017, CORROSION (C53-113-01) AROUND FASTENERS INSIDE CHANNEL OF STR 27L AT BS 720F PLUS 17.SDR 9614476612Longeron · corrodedDURING P-CHECK, FOUND CORROSION ON STR 49L FROM BS 1851 TO 1853. REPAIRED STRINGER PER EA 66-101889.SDR TSAA9653051Stringer · corrodedDURING HEAVY MAINTENANCE VISIT, FOUND EXFOLIATION CORROSION ON STRINGER 27R BS 827. REPAIRED STRINGER PER SRM 53-10-3 AND REPAIRED SKIN PER SRM 53-30-3. AIRCRAFT RETURNED TO SERVICE. (M)SDR 9614776612Longeron · corrodedDURING P-CHECK, FOUND CORROSION ON STR 51R AT BS 2163. REPAIRED STRINGER (P/N 65B04369-176) PER EA 66-101900.SDR 96ZZZM1139Longeron · crackedSTL - DURING AS-2, FOUND .5 INCH CRACK IN LONGERON 5R STATION 832. REPAIRED LONGERON 5R PER SRM 53-02 FIGURE 2.SDR 96FDEA01175Stringer · crackedUPPER LOBE, BL 9, 720C, STR 15L CRACKED. REMOVED DAMAGE AND INSTALLED STR SPLICE PER SRM 53-10-3.SDR USAA960488Stringer · corrosionINT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND 5 INCH BY 3 INCH CORRODED AREA STR 27L BS 967 TO BS 972. INSTALLED STRINGER SPLICE, REPAIRED PER SRM 53-10-3, FIGURE 1. CORROSION TASK NR: C53-208-01. CORROSION LEVEL: 2. (X)SDR USAA960483Stringer · corrodedINT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND 7 INCH BY 3 INCH CORRODED AREA, STR 25L, BS 967 TO BS 974. INSTALLED REPAIR DOUBLER, REPAIRED PER SRM 53-10-3. CORROSION TASK NR: C53-202-01. CORROSION LEVEL: 2. (X)SDR 9614466612Longeron · corrodedDURING P-CHECK, FOUND CORROSION ON STR 47L AT BS 1708 AND 1718. REPAIRED STRINGER PER EA 66-101898.SDR USAA960480Stringer · crackedINT - DURING 'Q-6' CHECK VISUAL INSPECTION, FOUND .75 INCH CRACK, STR 18A SHELF, 1 INCH FORWARD OF STA 727 BULKHEAD AT INBOARD VERTICAL FASTENER. STOP DRILL CRACK AND INSTALLED REPAIR KIT. REPAIRED PER EO 5393G256. (X)SDR 9614456612Longeron · corrodedDURING P-CHECK, FOUND CORROSION ON STR 50L AT BS 2150 AND 2170. REPAIRED STRINGER (P/N 65B04369-87) PER EA 66-101895.SDR UPS96420391Stringer · crackedINSPECTION TYPE: C. BULK CARGO COMP: AT STA 2160, STR 46 LT CRACKED AT STRINGER CLIP. REPAIRED STRINGER IAW SRM 53-10-03, FIG 1.SDR CALA9600869Longeron · crackedINSPECTION FOUND A 7 INCH CRACK IN LONGERON 44R BETWEEN STA 1641 AND 1701. THE LONGERON WAS REPAIRED IAW ECRA 5310-03292.SDR 96FDEA01153Stringer · corrodedNR 0225 AND 013. CORROSION C53-113-01(1) AROUND FASTENERS INSIDE CHANNEL OF STR 27R AT BS 720F + 17. ****S/D***** FOUND TO BE OUT LIMITS. REMOVED CORRODED SECTION OF STR 27B. FABRICATED AND INSTALLED REPAIR PARTS IAW FEDEX SRM 53-10-3.SDR 96FDEA01148Stringer · crackedNR0587 AND 035, WHILE WORKING NRO213 FOUND CRACK AND GOUGE IN STR 4R BS 600 IN U-CHANNEL. *S/D* REMOVED DAMAGE AT BS 600 STR 4R, REPAIRED PER FEDEX SRM 53-10-1 FIG 1.SDR UPS96420377Stringer · elongated holesINSPECTION TYPE: C. FORWARD CARGO COMP: FOUND DURING LOWER CHORD REPLACEMENT AT BS 1000, ELONGATED HOLES IN STR 46 RT. REPAIRED IAW TELEX UPS-AMS-95-0144RE / ATA 5321/20.SDR UPS96820645Longeron · corrodedINSPECTION TYPE: C. LONGERON 34L CORRODED AT FS 1700 IN AFT ACCESSORY COMPT, AT TIE FITTING. REMOVED AND REPLACED CORRODED LONGERON SECTION IAW DC8 SRM 53-3-2, ALODINED AND PRIMED AS REQUIRED IAW DC8 SRM 51-1-8.SDR SWAA960547Stringer · crackedDURING SCHEDULED D-CHECK, FOUND STRINGER CRACKED AT BS 727B, S9R. REPLACED STRINGER SECTION PER BOEING SRM.SDR CALA9600977Stringer · damagedINSPECTION FOUND FUSELAGE SKIN DENTED AND STRINGER DAMAGED AT STA 400, STRINGER 18L. THE DAMAGED AREA OF STRINGER WAS REMOVED IAW SRM 53-10-3. THE SKIN WAS RETURNED TO ORIGINAL CONTOUR IAW SRM 51-70, FIGURE 4. REPAIR PARTS FOR STRINGER WERE FABRICATED AND ISDR UPS96220473Stringer · corrodedINSPECTION TYPE SI, FOUND CORROSION ON STRINGER 22 RT BETWEEN STA 351.2 AND STA 360. CORROSION REMOVAL WAS OUT OF LIMITS PER SRM 53-10-01. REMOVED DAMAGED SECTION OF STRINGER, LOCATED AND DRILLED STRINGER REPAIR PARTS, INSTALLED PER SRM 53-10-03, 51-30-02, 5SDR COMA9610209Stringer · corrodedDURING 2C INSPECTION, FOUND STRINGERS IN LOWER FUSELAGE AREA BELOW LAV TO HAVE SURFACE CORROSION. CLEANED LIGHT CORROSION, TREATED AND PAINTED PER M/M 51-20-04.SDR 96ZZZM1137Longeron · crackedSTL - DURING SPECIAL INSPECTION, FOUND .5 INCH CRACK LONGERON 5R STATION 756, REPAIRED PER SRM 53-02 FIGURE 2.SDR ARWA9606058Longeron · corrodedRIGHT WING CENTER SECTION AT STA 960 THROUGH 980, LONGERON 22R, HAS CORROSION, CRACKS AND SHEARED RIVETS. REPAIRED AREA ACCORDING TO DACO ROD SKETCH NR 96-05-20-003.SDR ARWA9606056Longeron · crackedLONGERON 24L HAS 3.5 INCH CRACK AT STA 960. LONGERON 24L WAS REPAIRED IAW DC-8 SRM 53-2-2, FIG 5. FABRICATED DOUBLERS PER DC-8 SRM 51-1-1. TREATED AND INSTALLED DOUBLERS IAW DC-8 SRM 51-1-8 AND 51-1-20D.SDR ARWA9606026Longeron · corrodedFORWARD DECK, LONGERONS 35R AND 36 AT FS 500 HAVE LEVEL 2 CORROSION UNDER FRAME. REPAIRED AREA PER DC-8 SRM 51-1-21, 53-2-0, 51-1-8 AND 51-1-20D.SDR ARWA9606016Longeron · crackedFORWARD CARGO COMPARTMENT AT LONGERON 30R, FS 180, CRACKED 2 INCHES. CRACKED SECTION REMOVED AND REPLACED WITH EXTRUSION PER DC-8 SRM 51-1-8 AND 51-1-20D.
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