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 ARWA9606005Longeron · crackedA 9.5 CRACK STOP HOLE, OLD REPAIR HAS EXTENDED 3 FORWARD ON LONGERON 24R. REMOVED AND REPLACED LONGERON 24R PER DOUGLAS DRAWING 5750198 AND 5615475.SDR 96FDEA01132Stringer · corrodedNR 0032 AND 010. CORROSION (C53-113-10-1) ON STRINGER 26L, BS 680 TO BS 700. REMOVED CORRODED STR 26L, BS 668 - BS 740. INSTALLED REPAIR STR SECTION IAW FEDEX SRM 53-10-3.SDR TSAA9653043Stringer · corrodedDURING HEAVY MAINTENANCE VISIT, FOUND STRINGER 26L EXFOLIATED AT BS 907. REPAIRED PER ECO 2599R1. AIRCRAFT RETURNED TO SERVICE. (M)SDR C2XA96IA148Stringer · corrodedIAH - DURING C-CHECK INSPECTION, STRINGER 16 RIGHT AT FRAME 36 WAS FOUND TO BE CORRODED. MX REMOVED THE DAMAGED PORTION OF THE STRINGER AND INSTALLED A REPAIR DOUBLER PER ATR 42 SRM 53-00-00 AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR DHL9672112CStringer · crackedAT C-CHECK, FOUND STRINGER 18 R AT STA 404 CORRODED AND CRACKED. CUT OUT DAMAGED AREA AND INSTALLED SPLICE 12 LONG PER SRM AND STRINGER 13 LONG.SDR CALA9600953Longeron · crackedINSPECTION FOUND TWO 1 INCH CRACKS IN LONGERON 3L AT STA 160. THE LONGERON WAS REPAIRED IAW SRM 53-02.SDR SWAA960516Stringer · crackedDURING SCHEDULED 1/4 D-CHECK, FOUND STRINGER 14R AT BS 1121 CRACKED. REPAIRED PER BOEING SRM.SDR SWAA960512Stringer · crackedDURING SCHEDULED D-CHECK, FOUND STRINGER CRACKED AT BS 495, S22R. REPLACED WITH NEW SECTION PER BOEING SRM.SDR SWAA960508Stringer · corrodedDURING SCHEDULED D-CHECK, FOUND O/B SIDE OF STRINGER CORRODED AT BS 907, RBL 15, WL 166, S26R. REPAIRED PER BOEING SRM.SDR SWAA960504Stringer · crackedDURING SCHEDULED D-CHECK, FOUND STRINGER CRACKED AT BS 1010, S6R. SPLICED IN NEW SECTION PER BOEING SRM.SDR DHL9672125CStringer · corrodedAT C-CHECK, FOUND CORROSION ON STR 16L STA 837 BELOW EMERGENCY EXIT CUTOUT. REMOVED AND INSTALLED NEW STRINGER FROM BS 830 TO 850 PER SRM 51-10-1.SDR DHL9672111CStringer · crackedAT C-CHECK, FOUND STRINGER 9 RIGHT IS CRACKED AT BS 680. CUT OUT DAMAGED SECTION OF STRINGER AND INSTALLED REPAIR PER SRM 53-10-3, REPAIR 12 INCHES.SDR UPS96420350Stringer · crackedINSPECTION TYPE: C. FOUND CRACK IN STRINGER 31 LT BSTA 1635 TO 1640. STRINGER 31 LT REPLACED BETWEEN STA 1635 - 1650. REPAIR CARRIED OUT IAW SRM 53-10-03, FIG 1.SDR 96ZZZM1221Longeron · crackedSTL - DURING OP-15, FOUND .25 INCH CRACK IN LONGERON 2R, STATION813, UNDER OUTBOARD BOLT. REPAIRED PER SRM 53-02, FIGURE 2 AND TWA STANDARDPRACTICES. AIRCRAFT TOTAL TIME 41,166, AIRCRAFT TOTAL CYCLES36,801.SDR DHL9672101CStringer · crackedAT C-CHECK, FOUND STR 22 LT CRACKED BETWEEN STA 720A AND 720B. FABRICATED AND INSTALLED STRINGER REPAIR 7 INCHES LONG PER SRM 53-10-3.SDR UPS96820518Longeron · crackedINSPECTION TYPE CS2, HEAVY CORROSION AND CRACKED LONGERON 24R FITTING BETWEEN FS 879 TO 902. REPAIRED PER UPS EO.SDR DHL9672121CStringer · crackedAT C-CHECK, FOUND STRINGER 4L CRACKED AT STA 420. CUT OUT DAMAGED AREA, INSTALLED REPAIR PER SRM 53-10-3, 20 LONG.SDR AALA960893Stringer · crackedTUL - FOUND STRINGER END CRACKED STRINGER 15R AT THE LIGHT BOX FORWARD SIDE STATION 720B PLUS 4. REMOVED CRACK STRINGER AND SPLICED NEW STRINGER AS PER SRM 53-10-3 FIG 1. (M)SDR AALA960891Stringer · corrodedFOUND CORROSION IN STRINGER 27R AT STATION 701. REMOVED OUT OF LIMITS STRINGER AND REPAIRED PER SRM 53-10-3. (M)SDR AALA960888Stringer · corrodedTUL - FOUND STRINGER 27 LEFT HAS CORROSION STATION 514 TO STATION 525. CUT OUT CORROSION AND REPLACED STRINGER 27L FROM STATION 513 TO STATION 525, PER SRM 53-10-3 PG 3-4B. (M)SDR AALA960885Stringer · corrodedTUL - FOUND CORROSION ON OUTBOARD SIDE STRINGER 29R TWO INCHES AFT OF 950E. REPLACED AFT SECTION OF STRINGER 29RT STATION 950D PLUS 10 INCHES TO STATION 990 PLUS 10 INCHES PER ESO 11697. (M)SDR UPS96420375Stringer · crackedINSPECTION TYPE: C. BULK CARGO COMP: STA 2140 LT, FRAME STRINGER CUTOUT CRACKED AT STR 45. FRAME STR CUTOUT REPAIRED IAW SRM 53-10-04, FIG 41.SDR UPS96420371Stringer · crackedINSPECTION TYPE: C. AFT CARGO COMP: AT STA 2180, STR 46 RT, STRINGER END CRACKED JUST IN FRONT OF SPLICE. STA 2180, STR 46, REPAIRED IAW SRM 53-10-03.SDR IXXA96110Longeron · corrodedDURING ROUTINE B-CHECK INSPECTION, CORROSION WAS FOUND ON LONGERON 25 LEFT BETWEEN FUSELAGE STATIONS 1550 AND 1570. CORRODED SECTION WAS REMOVED. REPAIR OF THE AREA WAS ACCOMPLISHED BY INSTALLING A NEW SECTION IAW FAA DER APPROVED DRAWING 853-40-96. (M)SDR IXXA96109Longeron · corrodedDURING ROUTINE B-CHECK INSPECTION, LONGERON 24 LEFT WAS FOUND CORRODED BETWEEN FUSELAGE STATIONS 857 AND 867. CORROSION WAS REMOVED, REPAIR DOUBLER FABRICATED AND INSTALLED IAW THE AIRCRAFT STRUCTURAL REPAIR MANUAL 53-2-2. (M)SDR IXXA96108Longeron · crackedDURING ROUTINE B-CHECK INSPECTION, LONGERON 24 RIGHT WAS FOUND TO BE CRACKED. THE LONGERON WAS REPLACED IAW DOUGLAS DRAWING 5751027 AND THE AIRCRAFT STRUCTURAL REPAIR MANUAL. (M)SDR IXXA96107Longeron · corrodedDURING ROUTINE B-CHECK INSPECTION, LONGERON 25 RIGHT WAS FOUND CORRODED BETWEEN FUSELAGE STATIONS 1550 AND 1570. THE DAMAGED SECTION WAS REMOVED AND REPLACED WITH A NEW SECTION. THE LONGERON WAS REPAIRED IAW DRAWING 853-39-96 WHICH WAS FAA DER APPROVED 5/13/SDR UPS96420385Stringer · corrodedINSPECTION TYPE: C. BULK CARGO COMP: DURING ACCOMPLISHMENT OF FRAME REPAIR AT BS 2060, S-29 LT, FOUND CORROSION IN STRINGER AT FRAME/STRINGER-CLIP ATTACHMENT. REMOVED DAMAGED SECTION OF STRINGER FROM BS 2050 TO BS 2070 AND REPAIRED STRINGER IAW SRM 53-20-0SDR UPS96220439Stringer · corrodedINSPECTION TYPE SI, CORROSION ON STRINGER 1 STA 330 TO 400. MECHANICALLY REMOVED CORROSION, REWORK AREA AT STR 1 STA 380 TO 400 DEEMED OUT OF LIMITS IAW SRM 53-10-1. REPAIRED STR 1 IAW 53-10-3.SDR 97ZZZX341Longeron · chafedATW - RT MOST UPPER AIRBRAKE HINGE MOUNTING LONGERON ASSY HAS BEEN CHAFED BY THE AIRBRAKE ACTUATOR TO A DEPTH OF .040 INCH. CORRECTIVE ACTION: REPAIRED CHAFED AREA IAW BAE FAX DJR/RJ063096 AND BAE SRM CHAPTER 51-00-00 STANDARD PRACTICES AND PROCEDURES.SDR 96DHL72197CStringer · crackedAT C-CHECK, STRINGER 26L HAS CORROSION BETWEEN STA 580 AND 600. FABRICATED AND INSTALLED REPAIR PER SRM 53-10-8 STRINGER 14 AND SPLICES 2 EA 11 LONG.SDR CALA9600901Stringer · corrodedINSPECTION FOUND STRINGER 28R FLANGE CORRODED AT F.S. 685. THE CORRODED SECTION OF STRINGER WAS REMOVED. A NEW STRINGER AND SPLICE WERE FABRICATED AND INSTALLED IAW SRM 53-10-3.SDR 96DHL72190CStringer · dentedAT C-CHECK, SMALL DENTS AT FUS STA 300 STR 14, 15, RT. REPAIRED STRINGER AT STA 14 PER SRM 53-10-3, 18.SDR GAIA9617Longeron · corrodedDURING C-CHECK INSPECTION, REVEALED CORROSION ON THE RIGHT LONGERON 18 CUSP MEMBRANE BETWEEN FUSELAGE STATION 256 TO 275. REPAIRED FLOOR IAW KITTY HAWK EA D9-53-032. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR 9612849921Fitting · corrodedDURING M-CHECK, FOUND CORROSION ON THE LONGERON 20L END FITTING AT FS 980 TO 996. REPLACED END FITTING PER SRM 53-11-3, PG 13.SDR 9612819902Longeron · crackedDURING H-CHECK, FOUND A CRACK AND CORROSION ON LONGERON 26R AT FS 351. REPAIRED LONGERON (P/N 5911412-113) PER EA 99-109059.SDR SWAA960477Skin · crackedDURING SCHEDULED BC3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 755, S23L. REPAIRED PER BOEING SRM.SDR CALA9600942Longeron · corrodedINSPECTION FOUND LONGERON 48L CORRODED AT STA 1701 TO 1721. A REPAIR WAS PERFORMED IAW ECRA 5310-03291.SDR CALA9600936Stringer · corrodedINSPECTION FOUND STRINGER 28R CORRODED AT STA 520 T0 540. THE CORRODED STRINGER SECTION WAS REMOVED. A NEW STRINGER AND SPLICE WERE FABRICATED AND INSTALLED IAW SRM 53-10-3 AND 51-30-2.SDR USAA960468Stringer · corrosionROA - DURING 'BX TRANSIT' CHECK VISUAL INSPECTION, FOUND 2 INCH BY 3 INCH CORROSION STRINGER 27L BS 986.5. INSTALLED DOUBLER AND STRINGER, REPAIRED PER SRM 53-10-3. (M)SDR UPS96220425Stringer · corrodedINSPECTION TYPE SI, FOUND STR 22L TO BE CORRODED AT BS 428.5. REMOVED CORROSION, SPLICE SECTION AT BS 440, CUT DAMAGED STRINGER, FOUND STR 22L AT BS 412 TO BE CORRODED BEYOND LIMITS AS WELL. CUT STRINGER AT BS 407, FABRICATED REPAIR PARTS AND INSTALLED NEW SSDR 97ZZZX340Longeron · damagedATW - FORWARD PASSENGER DOOR FUSELAGE UPPER LONGERON AFT OF FUSELAGE FR NR 14 HAS DRILL MARK BOTTOM SURFACE APPROXIMATELY .018 INCH DEEP. PART NEEDS TO BE MADE, CHECKED, ALODINED, NOTED FOR CRACKS. CORRECTIVE ACTION: REC'D FAX JM/RJ0624-96 DAI/1011/55 ALLOWSDR UPS96220418Stringer · corrodedINSPECTION TYPE SI, CORROSION ON RT STRINGER NR 7 STA 405. REMOVED CORROSION, 1 BY .025 BY .025 OF ORIGINAL .032 OUT OF LIMITS, FABRICATED REPAIR PARTS AND INSTALLED ON A/C AFTER TREATING AFFECTED AREA IAW SRM 51-10-6, 53-10-2 AND SRM 53-10-3.SDR CALA9600855Stringer · corrodedINSPECTION FOUND STRINGER CHANNEL CORRODED AT STA 351.2 TO 360, S20L. THE STRINGER CHANNEL WAS REMOVED AND A NEW CHANNEL WAS FABRICATED AND INSTALLED IAW SRM 51-10-2, 51-30-2 AND BOEING DRAWING 69-48934.SDR 96FDEA01034Stringer · corrodedCORROSION (C53-224-01, -1) ON STR NR 4R BS 720 A TO 700. MECHANICALLY REMOVED CORROSION ON STR NR 4R BS 720 A TO 700 FOUND TO BE OUT OF LIMITS PER FEDEX SRM 53-10-1. REPLACED STR 720 PLUS 10 TO BS 720 A PLUS 10 PER FEDEX SRM 53-10-3.SDR CALA9600848Stringer · corrodedINSPECTION FOUND A 3 INCH SECTION OF STRINGER 21R CORRODED AT BS 416. THE CORRODED SECTION OF STRINGER WAS REMOVED AND REPAIR CHANNEL AND ANGLES WERE INSTALLED IAW SRM 53-10-3 FIGURE 1.SDR CALA9600847Stringer · corrodedINSPECTION FOUND CORROSION OVER AN 18 INCH SECTION OF STRINGER 22R BETWEEN BS 390 AND 410. THE CORRODED SECTION OF STRINGER WAS REMOVED. REPAIR CHANNEL AND ANGLES WERE INSTALLED IAW SRM 53-10-3 FIGURE 1.SDR USAA960461Stringer · out of limitsINT - DURING Q-4 CHECK, VISUAL INSPECTION FOUND FASTENER HOLE EDGE DISTANCE OUT OF LIMITS (SHORT EDGE MARGIN) STR 18A, STA 727L, AFT LOWER HOLE. INSTALLED REPAIR ANGLE, REPAIRED PER EA 41124. (X)SDR USAA960457Stringer · corrodedINT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 9 INCH CORRODED AREA AFT CARGO BS 967-987 STRINGER 25L. INSTALLED STRINGER SPLICE AND REPAIRED PER SRM 53-10-3. (M)SDR USAA960456Stringer · corrodedINT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 10 INCH CORRODED AREA STRINGER 27L BS 948. CUT OUT CORRODED SECTION OF STRINGER FABRICATED NEW SECTION AND SPLICED BACK IN, REPAIRED PER SRM 53-10-3. (M)
Back to JASC 5313