JASC 5313

Service difficulty reports · 36,310

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.

SDR 06FDEA1558Stringer · dentedREWORK REQUIRED ON STRINGER 3R BS 401 HAS OPEN HOLE, BS 367 STRINGER IS DENTED. REPAIRED PER EA 7-5310-96627.Apr 20, 2006 · N485FE · Boeing 727227SDR ASAA0640459Stringer · damagedFOUND STRINGER DAMAGED. REMOVED AND REPLACED STRINGER WITH NEW ITEM PER SRM 53 00 03 REPAIR 1.Apr 19, 2006 · N764AS · Boeing 7374Q8SDR 06FDEA1514Longeron · crackedCTR CARGO COMPT CRACK 8 INCHES ON LONGERON 44 RT FROM STA 1671 TO STA 1681. CUT CAP FRAME AT STA 1681 LONG 44-45, REPLACED LONGERON IAW SRM 51-33-01 PAR 6-10 VOL 2. INSTALLED SPLICE REPAIR IAW SRM 53-30-00 FIG 5-8 VOL 1.Apr 19, 2006 · N68054 · Doug MD1010FSDR QXEA200601544Stringer · corrodedYYC C3 FORWARD FUSELAGE, UNDER FLOOR PANEL 133BZ STATION X-18.25 AND STRINGER 33 IS CORRODED. REPAIRED IAW DHC-8 Q400 SRM TASK 51-21-00-350-801, 51-25-10-370-801 AND SRM TASK 51-25-15-370-801.Apr 18, 2006 · N425QX · Bombdr DHC8402SDR 2006UALA00716Stringer · corrodedAFT CARGO COMPARTMENT STATION 847 STRINGER 22R HAS CORROSION ON STRINGER. CUT OUT DAMAGED STR AND REPLACED WITH NEW SECTION PER SRM 53-00-03.Apr 17, 2006 · N341UA · Boeing 737322SDR 06FDEA1484Longeron · crackedLONGERON 48L FOUND CRACKED AFTER SPLICE REMOVAL FOR REPAIR, FORWARD OF STA 5 -113, CENTER CARGO COMPARTMENT. REMOVED AND REPLACED WITH NEW LONGERON IAW SRM 51-33-01 VOL.II. REPAIR CLASSIFIED AS MAJOR IAW FEDEX GMM 6-2-100.Apr 17, 2006 · N582FE · Doug MD11SDR 06FDEA1483Longeron · crackedLONGERON 52 STA 979 FOUND CRACKED AFTER FASTENERS REMOVED FOR CORROSION CLEAN UP ON CAP ANGLE FORWARD CARGO. COMPLIED WITH FEDEX EA 1-5330-95835.Apr 17, 2006 · N582FE · Doug MD11SDR QXEA200601129Stringer · corrodedPDX - C4 CORROSION ON STRINGER 31 AT FRAME 202.75, FORWARD SIDE AROUND RIVETS. REPAIRED IAW DHC-8-200 SRM 51-20-11, 51-20-41.Apr 16, 2006 · N356PH · Dhav DHC8202SDR KCSA061145Fitting · corrodedFUSELAGE STRINGER END FITTING IS CORRODED AT AFT SIDE OF STA 2360 BULKHEAD, STR 48L.Apr 16, 2006 · N716CK · Boeing 747122SDR SWAA061264Stringer · crackedDURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE STRINGER CRACKED AT BS 500, STR 10R. REPAIRED STRINGER PER SRM.Apr 16, 2006 · N355SW · Boeing 7373H4SDR 2006UALA00694Stringer Clip · crackedSTRINGER CLIPS CRACKED AT BS 907 AT STRINGER 1. REMOVED & REPLACED STR CLIPS AT EACH LOCATION REF SRM 51-40-02.Apr 15, 2006 · N932UA · Boeing 737522SDR DU4R2006388Longeron · corrodedFOUND CORROSION LONGERON 28L BETWEEN FS 1287 TO FS 1320. CUT OUT SECTION OF LONGERON FS 1200 TO 1338. DRILLED UP AND INSTALLED NEW LONGERON IAW MD-80 SRM 51-30-1 AND 51-10-3.Apr 15, 2006 · N926DL · Doug MD88SDR EIA2006100Stringer · gougedFOUND BS 280, STR 34L GOUGED ON BOTTOM AROUND FASTENERS AND FLANGE BENT. REMOVED DAMAGE, FABBED AND INSTALLED REPAIR PER B747 SRM 51-30-02 PAGE 8, 9 AND 32, 51-20-01, 51-30-05 PAGE 5, 6 AND 9 AND 51-10-02 PAGE 7.Apr 14, 2006 · N489EV · Boeing 747230BSDR DU4R2006389Longeron · corrodedFOUND EXFOLIATED CORROSION ON UPPER CORNER CAVITY OF AFT CARGO DOOR ABOVE LONGERON 19R STA Y = 1154. REMOVED AND REPLACED UPPER DOOR BEAM AT FWD CORNER OF AFT CARGO DOOR ABOVE L-19R STA Y = 1154 IAW DOUGLAS DWG 5936072 AND MD-88 SRM 51-30-5.Apr 14, 2006 · N926DL · Doug MD88SDR CA060413007Stringer Splice · corroded(CAN) CORRODED EXTERNAL STRAP ON RT SIDE OF FUSELAGE AT BS 1180 ALONG STRINGER 17. (TC NR 20060413007)Apr 13, 2006 · Boeing 757200SDR ASAA0640454Stringer · damagedFOUND STRINGER DAMAGED. REPAIRED PER SRM 53 00 03 FIG 201 REPAIR 1.Apr 13, 2006 · N764AS · Boeing 7374Q8SDR EIA2006098Stringer · tool damageFOUND BS 300 STRINGER 14L HAS TOOL MARK AND CRACK. REMOVED AND REPLACED STRINGER PER B747 SRM 51-30-02.Apr 12, 2006 · N489EV · Boeing 747230BSDR 06FDEA1404Longeron · corrodedCENTER CARGO RIGHT LONGERON 48R BETWEEN STA 1561 TO 1581 CORRODED. CENTER CARGO RIGHT SIDE STA 1561 TO STA 1581 LONGERON 48R SPLICE CORROSION REMOVED AND FOUND WITHIN LIMIT AS PER SRM 53-00-01 FIGURE 3 VOLUME I. ORIGINAL THICKNESS = 0.200", MATERIAL REMOVEApr 12, 2006 · N582FE · Doug MD11FSDR 06FDEA1430Stringer · corrodedRT A/C BAY STRG 40 BETWEEN FS 44-47 HAS NUMEROUS SPOTS OF CORROSION ON SKIN AROUND RIVETS AND ON TOP OF VERTICAL FLANGE REF N00733. REMOVED CORROSION IAW A310-200 SRM 51-74-10. FOUND 1 AREA OUT OF LIMITS, REPAIRED IAW EA 6-5315-98992.Apr 12, 2006 · N455FE · Airbus A310322SDR 06FDEA1429Stringer · corrodedRT A/C BAY STRG 44 HAS NUMEROUS SPOTS OF CORROSION AROUND RIVETS, SIDE TOP OF VERTICAL FLANGE BETWEEN FS 44-47, REF N00729. REMOVED CORROSION IAW A310-200 SRM 51-74-10 FOUND 2 AREAS OUT OF LIMITS. REPAIRED IAW EA 6-5315-98992.Apr 12, 2006 · N455FE · Airbus A310222SDR 061133Stringer · bentFUSELAGE STRINGER IS BENT AT STA 1930, STR 1R.Apr 12, 2006 · N716CK · Boeing 747122SDR 06FDEA1412Longeron · corrodedCORROSION LONGERON 52 BETWEEN BS 1761 AND BS 1781 IN CENTER CARGO COMPARTMENT. REMOVED AS PER SRM 51-21-01 VOL.II. ORIGINAL MATERIAL THK. 0.125" REMOVED 0.005"X L=20"X W=1" REMAIN 0.120" FOUND WITHIN LIMIT AS PER SRM 53-00-01 FIG.1A VOL.I. CLASSIFIED MINOR Apr 12, 2006 · N526FE · Doug MD11SDR 06FDEA1408Longeron · corrodedCORROSION LONGERON 51R BETWEEN BS 1721 AND BS 1741 IN CENTER CARGO COMPARTMENT. CORROSION REMOVED AS PER SRM 51-21-01 VOL.II. MATERIAL ORIGINAL THK. 0.125" REMAIN 0.121" FOUND WITHIN LIMIT AS PER SRM 53-00-01 FIG.1A VOL.I. CLASSIFIED MINOR REPAIR PER GMM 6-2-Apr 12, 2006 · N526FE · Doug MD11SDR 06FDEA1395Longeron · crackedEMPENNAGE AFT FUSELAGE APPROX STA 2007-2033 BETWEEN LONGERON 45R TO 46R, CAP SUSPECTED CRACKED. EMPENNAGE, AFT FUSELAGE APPROX STA 2007-2033 BETWEEN LONGERON 45R TO 46R END CAP REPAIRED AS PER FEDEX EA NR 1-5310-95817, TITLE: FUSELAGE LONGERON 45R CRACKED BApr 11, 2006 · N582FE · Doug MD11FSDR 06FDEA1394Longeron · crackedEMPENNAGE AFT FUSELAGE APPROX STA 2007-2033 BETWEEN LONGERON 45L TO 46L, CAP SUSPECTED CRACKED. EMPENNAGE AFT FUSELAGE APPROX STA 2007-2033 BETWEEN LONGERON 45L TO 46L END CAP REPAIRED AS PER FEDEX EA NR 1-5310-95818, TITLE: FUSELAGE LONGERON 45L CRACKED BETWApr 11, 2006 · N582FE · Doug MD11FSDR A6WA200640148Stringer · bentFS 605 STRINGER 20L IS BENT. (K) MAINTENANCE REPAIRED BY REMOVING DAMAGE SECTION OF STRINGER FS 600 TO 620, FABRICATED REPLACEMENT STRINGER AND SPLICES, INSTALLED REPAIR PARTS IAW CRJ 200 SRM 53-00-03 PAGE 204. (M)Apr 11, 2006 · N466AW · Cndair CL6002B19SDR 06FDEA1374Longeron Splice · crackedCENTER CARGO - LEFT HAND LONGERON 41 SPLICE AT STA 5-113 TO 1541 CRACKED. CRACKED SPLICE ON CENTER CARGO LEFT HAND LONGERON 41 AT STA 5-113 TO 1541 REMOVED AND REPLACED AS PER SRM 51-33-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Apr 11, 2006 · N582FE · Doug MD11SDR 061132Fitting · corrodedFUSELAGE STRINGER END FITTING IS CORRODED AT STA 1480, STR 47R.Apr 11, 2006 · N716CK · Boeing 747122SDR 06FDEA1393Stringer · corrodedLT A/C BAY STR 49 HAS NUMEROUS SPOTS OF CORROSION ALONG RIVETED AREAS, TOP/SIDE SKIN OF VERTICAL FLANGE BETWEEN FR 39-40/41-42-43-44 AS MARKED. REMOVED RIVETS AND BRACKETS TO ACCESS CORROSION PER A310 SRM 51-40-21, REMOVED CORROSION ON STRINGER 49 LT PER A310Apr 11, 2006 · N455FE · Airbus A310222SDR 06FDEA1391Stringer · corrodedA/C BAY LT STR 41 HAS NUMEROUS SPOTS OF CORROSION ALONG RIVETED AREAS TOP SIDE SKIN OF VERTICAL FLANGE AS MARKED ON BETWEEN FR 44-45-46-47 -2 EA ELEC CLAMP BRACKET BETWEEN FR 46-47. REMOVED AND REINSTALLED FASTENERS TO ACCESS CORROSION REMOVAL PER A310 SRM 5Apr 11, 2006 · N455FE · Airbus A310222SDR 06FDEA1390Stringer · corrodedLEFT A/C BAY L-STR 44 HAS NUMEROUS SPOTS OF CORROSION ALONG RIVETED AREAS, TOP/SIDE SKIN OF VERTICAL FLANGE AS MARKED BETWEEN FR44-45-46-47. REMOVED AND REINSTALLED FASTENERS TO ACCESS CORROSION PER SRM 51-40-21. REMOVED CORROSION PER A310 SRM 51-74-40 MEASUApr 11, 2006 · N455FE · Airbus A310222SDR 06FDEA1389Stringer · corrodedA/C BAY LT STR 42 AND STIFFENERS HAVE NUMEROUS SPOTS OF CORROSION ALONG RIVETED AREAS TOP SIDE SKIN OF VERTICAL FLANGE BETWEEN FR 39-42. REMOVED CORROSION IAW A310-200 SRM 51-74-10 FOUND 1EA AREA OUT OF LIMITS, 2 INCHES AFT OF FR 40/41 STR 42 LT REPAIRED IAW Apr 11, 2006 · N455FE · Airbus A310222SDR 06FDEA1388Stringer · corrodedA/C BAY LT STR 47 HAS NUMEROUS AREAS OF CORROSION ALONG RIVETED SURFACE, TOP SKIN AND VERTICAL FLANGE BETWEEN FR 39-44.5. REMOVED CORROSION IAW A310-200 SRM 51-74-10, FOUND 8EA AREAS OUT OF LIMITS. REPAIRED IAW EA 6-5315-98983.Apr 11, 2006 · N455FE · Airbus A310222SDR 06FDEA1387Stringer · corrodedLT A/C BAY STR 48 HAS NUMEROUS SPOTS OF CORROSION ALONG RIVETED AREAS, TOP SIDE SKIN OF VERTICAL FLANGE BETWEEN FR 42, 43, 44. REMOVED CORROSION ON STR 48 LT IAW A310-200 SRM 51-74-10 FOUND 1EA AREA OUT OF LIMITS 3 INCHES FWD OF FR 42 STR 48 LT. COMPLIED WITApr 11, 2006 · N455FE · Airbus A310222SDR 06FDEA1384Stringer · corrodedA/C BAY LT STR 44 HAS NUMEROUS SPOTS OF CORROSION ALONG RIVETED AREA ON TOP SIDE SKIN OF VERTICAL FLANGE BETWEEN FS 39, 40, 41, 42, 43 AND 44. REMOVED CORROSION IAW A310-200 SRM 51-74-10. FOUND 2 AREAS OUT OF LIMITS IAW A310-200 SRM 53-10-00 FIG 103 TABLE 10Apr 11, 2006 · N455FE · Airbus A310222SDR 06FDEA1382Stringer · corrodedLT A/C BAY STR 50 HAS NUMEROUS SPOTS OF CORROSION ALONG RIVETED FASTENER AREA TOP SIDE SKIN OF VERTICAL FLANGE BETWEEN FR 39, 40, 41, 42, 43 AND 44. REMOVED CORROSION IAW A310-200 SRM 51-74-10. FOUND 4 EACH AREAS OUT OF LIMITS PER A310-200 SRM 53-10-00 FIG 1Apr 11, 2006 · N455FE · Airbus A310222SDR 06FDEA1381Stringer · corrodedLT A/C BAY L-STR 40 HAS NUMEROUS SPOTS OF CORROSION ALONG RIVETED AREAS, TOP SIDE SKIN OF VERTICAL FLANGE BETWEEN FS 40, 41, 42, 43, 44, 45, 46, 47, 48. REMOVED CORROSION IAW A310-200 SRM 51-74-10, FOUND 1 AREA OUT OF LIMITS. REPAIRED 1 AREA 2 INCHES AFT OF Apr 11, 2006 · N455FE · Airbus A310222SDR 06FDEA1380Stringer · corrodedA/C BAY LEFT STR 41 HAS NUMEROUS AREAS OF CORROSION ALONG RIVETED AREA TOP SIDE OF VERTICAL FLANGE BETWEEN FR 39, 40, 41, 42, 43, 44. REMOVED CORROSION AT DISCREPANCY AREAS FOUND 1 EACH AREA OUT OF LIMITS 6 INCHES AFT OF FR 42 ON STR 41 LT REPAIRED IAW EA 6-5Apr 11, 2006 · N455FE · Airbus A310222SDR ASAA0610443Stringer · crackedFOUND CRACKED STRINGER. REPLACED STRINGER WITH FABRICATED REPAIR PART PER SRM 51 30 05 AND ASA EA 5310 02583.Apr 11, 2006 · N742AS · Boeing 737290CSDR ASAA0610426Stringer · crackedFOUND STRINGER CRACKED. REPAIRED CRACKED STRINGER PER SRM 53 10 3 FIG 1.Apr 11, 2006 · N742AS · Boeing 737290CSDR ASAA0610418Stringer · corrodedFOUND STRINGER CORRODED. REPAIRED PER SRM 53-10-03.Apr 11, 2006 · N742AS · Boeing 737290CSDR ASAA0610439Stringer · crackedFOUND STRINGER CRACKED AT GND FASTENER HOLES. REPAIRED PER ERO 5373 AND EA 5310 02599.Apr 11, 2006 · N742AS · Boeing 737290CSDR ASAA0610427Stringer · crackedFOUND STRINGER CRACKED. REPLACED CRACKED STRINGER IAW SRM 53 10 3 ERO 5735 AND EA5360 01056.Apr 11, 2006 · N742AS · Boeing 737290CSDR KCSA061117Stringer · dentedFOUND STRINGER S-28L AT BS 455 DENTED BEYOND LIMITS.Apr 11, 2006 · N715CK · Boeing 747209BSDR CALA0600118Stringer · corrodedINSPECTION FOUND STRINGER 25R CORRODED ON SIDE FLANGE AT STA 986 IN AFT BILGE AREA. THE STRINGER WAS REPAIRED IAW SRM 53-00-03, PAGE 201-207, FIGURE 201, DETAIL VII.Apr 10, 2006 · N14346 · Boeing 7373T0SDR EIA2006103Stringer · crackedFOUND BS 520 STR 29L LWR CARGO AREA HAS CRACKED FLANGE. REMOVED DAMAGE STRINGER STA 520 - 548 STR 29L FABBED AND INSTALLED STRINGER AND SPLICE PER B747 SRM 53-10-03 FIG 1 DETAIL II.Apr 9, 2006 · N489EV · Boeing 747230BSDR 061120Fitting · corrodedFOUND FUSELAGE STRINGER END FITTING HAS BOLT HOLES CORRODED AT STA 2360, STR 48L.Apr 9, 2006 · N716CK · Boeing 747122SDR KCSA061119Fitting · corrodedFOUND FUSELAGE STRINGER END FITTING HAS BOLT HOLES CORRODED AT STA 2360, STR 38R.Apr 9, 2006 · N716CK · Boeing 747122SDR CALA0600107Stringer · corrodedINSPECTION FOUND STRINGER 27R CORRODED JUST AFT OF STA 500D. THE CORRODED SECTION OF STRINGER WAS REMOVED AND REPAIR PARTS WERE INSTALLED IAW SRM 53-30-03.Apr 8, 2006 · N12322 · Boeing 7373T0SDR DU4R2006384Longeron · corrodedFOUND CORROSION ON LT L-27L FS 1287 - 1307 AND FS 1320. REMOVED CORRODED SECTION OF LONGERON 27L FS 1290 TO 1338. FABRICATED AND INSTALLED REPAIR LONGERON 60 INCHES FROM S1242886-7844 IAW MD-80 SRM 53-05D FIG 18 AND 51-10-3.Apr 7, 2006 · N926DL · Doug MD88
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