JASC 5340
Service difficulty reports · 22,411
Reports filed under 5340 · Fuselage Main, Attach Fittings, 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 = '5340' 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 = '5340' 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 AWXA200501159Stringer Clip · crackedMCN - DURING C15 CHECK, DISCOVERED STRINGER TIE CRACKED AT BS 727A, STR 25L IN THE AFT CARGO COMPARTMENT. MAINTENANCE REMOVED CRACKED STRINGER TIE IAW BOEING 737-300 SRM 51-40-02-0G. RECEIVED NEW STRINGER TIE AND INSTALLED AT BS 727A, STR 25L IN THE AFT CARGSDR UPS05845517Fitting · corrodedINSPECTION TYPE:C3 DEEP CORROSION PIT OR DRILL START IN BATHTUB FITTING TA STA 315 BETWEEN L33R AND L34R. REMOVED AND REPLACED BATHTUB FITTING IAW SRM 51-1-20D, 51-3-0 AND 51- 1-21.SDR UPS05845550Tee Fitting · corrodedC3 TEE CHORD CRACKED STA 860 RBL 40 UPPER AFT END OF CENTER TANK LOOKING FROM INSIDE MAIN CABIN. AFTER FURTHER EVALUATION CRACK FOUND TO BE CAUSED BY INTERGRANULAR CORROSION, CUT OUT DAMAGE, FABRICATED, AND INSTALLED REPAIR IAW DC-8 SRM 53-2-5 FIG 12 AND DWGSDR UPS05845549Fitting · crackedLEFT FWD LOWER TRAP FITTING IS CRACKED. REMOVED AND REPLACED TRAP FITTING IAW DC-8 SRM 51-3-0 AND 51-2-20D.SDR CIHA200581003Clip · crackedSUPPORT CLIP ON STR 16R CRACKED AT BS 850. REMOVED DAMAGED SPLICE ON STR 16R AT BS 850 IAW 727 SRM 51-30-2. FABBED NEW SPLICE FROM BAC 1498-137 PO 4496178 DIM 6 INCHES IN LENGTH IAW 727 SRM 53-10-2 FIG 9. SPLICE TREATED, PRIMED, AND INSTALLED IAW 727 SRM 51SDR 20050908Tube · crackedCARRY-THRU VERTICAL TUBE CRACKED ON CARRY-THRU ASSEMBLY. THIS CARRY-THRU IS MODIFIED BY STC SA1590CE. TIME IN SERVICE IS UNKNOWN. ALSO NOTED IS THAT THE VERTICAL TUBE WALL THICKNESS WAS .065 INCH RATHER THAN .120 INCH. THE HEAVIER WALL THICKNESS OF .120 IS SDR AWXA200501147Attach Angle · crackedMCN - DURING C18 CHECK, DISCOVERED ATTACH ANGLE CRACKED .05 INCHES IN LENGTH AT BS 360, FROM STRINGER 14L TO STRINGER 15L. MAINTENANCE REMOVED ATTACH ANGLE IAW BOEING 737-300 SRM 51-40-02-0G FIG 8. FORMED REPLACEMENT ATTACH ANGLE IAW AMERICA WEST AIRLINES ENSDR AWXA200501143Stringer Clip · crackedMCN - DURING C18 CHECK DISCOVERED .5 INCH LONG CRACK LOCATED AT STRINGER 16L, BS 348. REMOVED CRACKED CLIP IAW BOEING 737-300 SRM 51-40-02-06 FIG 8. FORMED AND INSTALLED CLIP AT BS 348, STRINGER 16L IAW AMERICA WEST AIRLINES ENGINEERING REQUEST NR 03-5311-052SDR AWXA200501142Clip · crackedMCN - DURING C18 CHECK DISCOVERED CLIP CRACKED, .5 INCHES, AT BS 351.20 AND STR 16L. MAINTENANCE REMOVED CRACKED CLIP AT BS 351.20 AND STR 16L IAW BOEING 737-300 SRM 51-40-02-06 FIG 8. FABRICATED AND INSTALLED REPLACEMENT CLIP AT BS 351.20 AND STR 16L IAW AMSDR AWXA200501139Clip · crackedMCN - DISCOVERED DURING C18 CHECK CLIP CRACKED, .05 INCHES IN LENGTH, AT BS 360, STR 8L ON LOWER SIDE. REMOVED CRACKED CLIP IAW BOEING 737-300 SRM 51-40-02-06 FIG 8. FABRICATED NEW CLIP IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NR 03-5311-05271-ES1. INSTSDR A6WA200540298Angle · crackedLT FS621.0 FLOOR SUPPORT ANGLE HAS A 1 INCH CRACK. MAINTENANCE CUT OUT AND REMOVED DAMAGED ANGLE AT FS 621 LT FITTED AND DRILLED NEW ANGLES AND STRAP AND INSTALLED IAW REO. (K)SDR SWAA052712Stringer Clip · crackedDURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 294, STR 13L. REMOVED AND REPLACED CLIP PER SRM.SDR DHL2005806532Fitting · corrodedITEM REF NR 041339: AFT CARGO COMPT. SPLICE FITTING CORRODED (STA 1260.000-1280.000, L-36) MAJOR REPAIR, PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG. 1. REMOVED CORROSION FROM SPLICE FITTING (STA 1260.000-1280.000 L-36) IAW SRM 51-1-8 PG. 17-18. FOUND OUT OF LIMSDR DHL2005806534Fitting · crackedITEM REF NR 040974: FWD CARGO COMPARTMENT, FLOORBEAM FITTING CRACKED 0.250 IN, STA 280.000 BL 0 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0. REMOVED CRACKED FITTING IAW SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. APPLIED PRC SEALASDR IXXA05RNG056SFitting · crackedDURING INSPECTION CHECK, FOUND A CRACKED FITTING LONGERON 24 STA 857.125 BATH TUB RT. REPAIR WILL BE MADE IAW EWO ATI 53-015 AND SRM 53-2-2 FIGURE 5, TEMPORARY REVISION 53-123.SDR UPS05845505Fitting · crackedINSPECTION TYPE:C3 C PIT STA 1180 LONG 35R BATH TUB FITTING IS CRACKED. REMOVED AND REPLACED BATH TUB FITTING IAW DC-8 SRM 53-2-0 FIG 2D.SDR IXXA05RNG055SFitting · crackedDURING INSPECTION CHECK, FOUND A CRACKED FITTING, LONGERON 24 STA 902 LT. REPAIR WILL BE MADE IAW EWO ATI 53-014 AND SRM 53-2-2 FIG 5 TEMPORARY REVISION 53-123.SDR AWXA200501061Clip · crackedMCN - MAJOR REPAIR - DURING C18 CHECK DISCOVERED ATTACH CLIP CRACKED AT BS 696, BL 01L. MAINTENANCE REMOVED CRACKED CLIP IAW BOEING 737-300 SRM 51-40-02-0G. FABRICATED REPLACEMENT CLIP IAW BOEING 737-300 DWG 65C25482. INSTALLED FABRICATED REPAIR PARTS AT BSSDR DHL2005806523Fitting · crackedFWD CARGO COMPT ZEE FITTING CRACKED 0.500 IN STA 300.000 L-27L. REMOVED CRACKED ZEE FITTING IAW SRM 53-1-0 PG. 1, SRM 51-1-20D. FABRICATED 2EA REPAIR ANGLES IAW SRM 53-2-0 FIG 2D SHEET 1,2, SRM 51-1-4 PG. 1 (FORMING). CUT NEW ZEE FITTING IN HALF USING TRIM DISDR UPS05845547Fitting · crackedC3 C PIT DOOR JAMB FITTING CRACKED I/B OF NR 2 TEE BOLT FITTING AT FWD SIDE. REMOVED AND REPLACED FITTING IAW DC-8 SRM 53-2-0 FIG 2D AND 51-1-20D.SDR UPS05845504Fitting · crackedINSPECTION TYPE:C3 L26L END FITTING APPEARS CRACKED AT STA 1688. REMOVED AND REPLACED LONGERON END FITTING IAW DC-8 SRM 51-1-20D.SDR UPS05845456Fitting · crackedLWR CARGO STA 1140 L35R FWD FITTING CRACKED 2 INCHES LONG. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-20D.SDR 05FDEA02740Fitting · damagedONE HOLE BS 640 BUCKTAIL BEHIND INTERNAL FITTING BETWEEN STR 3L-4L. REPAIRED HOLE, BS 640 BETWEEN STR 3L & 4L PER FED-EX EA. 7-5330-9226A.SDR SWAA052663Stringer Clip · crackedDURING SCHEDULED D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 294, STR 13L. REMOVED AND REPLACED CLIP PER SRM.SDR ASAA0540437Stringer Clip · corrodedOKC - FOUND STRINGER TIE CLIP BS 807 STRINGER RT IS CORRODED. REMOVED CLIP, FABRICATED AND INSTALLED NEW CLIP IAW B737-400 SRM 51-30-1, AND 51-40-2. (M)SDR UPS05845502Fitting · crackedINSPECTION TYPE: C3, LONG END FITTING CRACKED AT STA 1760 L17R. REMOVED AND REPLACED LONGERON END FITTING IAW DC-8 SRM 51-1-21.SDR UPS05845500Fitting · corrodedINSPECTION TYPE:C3 MAIN CABIN BELT FRAME END FITTING CORRDED AT STA 1040 L21R. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D AND 51-3-0.SDR SWAA052644Stringer Clip · corrodedDURING SCHEDULED D CHECK, FOUND FUSELAGE STRINGER CLIP CORRODED AT BS 807, RBL 7. REMOVED AND REPLACED CLIP PER SRM.SDR UPS05445322Stringer Clip · crackedBULK CARGO BS 2060 STR 28L FOUND 1EA TIE CLIP CRACKED, CRACK LENGTH 3/8". TIE CLIP REPLACED AS PER SRM 51-10-01 PG 9.SDR SWAA052596Stringer Clip · crackedDURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 380, STR 8L. REMOVED AND REPLACED CLIP PER SRM.SDR SWAA052594Stringer Clip · crackedDURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 360, STR 8L. REMOVED AND REPLACED CLIP PER SRM.SDR DU4R20050188Stringer Clip · corrodedCORROSION ON S-25L TIE CLIP AT FRAME 1460 IN AFT CARGO. REMOVED, FABRICATED AND INSTALLED REPAIR CLIP 3.50 X 3.20 INCH FROM BAC1518-472 EXTRUSION IAW B757 SRM 51-40-02, 51-20-01 AND DWG 140N2005.SDR SWAA052577Stringer Clip · crackedDURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 767, STR 27R. REMOVED AND REPLACED CLIP PER SRM.SDR SWAA052570Stringer Clip · crackedDURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 663.75, STR 10R. REMOVED AND REPLACED CLIP PER SRM.SDR SWIA200516195Attach Fitting · crackedAFT EQUIPMENT COMPARTMENT; INTERCOSTAL TO SKIN ATTACH CLIP IS CRACKED; FS 635.0; STR 12R, ITEM FOUND AT C-CHECK INSPECTION. REPLACED CLIP IAW CRJ SRM 51-40-11, 51-23-00, 51-42-06, 51-25-16, 51-42-21.SDR 05FDEA02634Angle · corrodedCORROSION FOUND ON LEFT REAR SPAR CAP ANGLE APB 7080-1. REPAIRED IN ACCORDANCE WITH FEDEX EA 8-5340-84036 LT SLANT PANEL TEE ANGLE CORROSION REPAIR .SDR USAA051039Angle · crackedLEFT PACK BAY, AFT RIGHT CORNER CRACKED. FABRICATED ATTACH ANGLE SRM 51-10-02 BOEING DWG 66-24798, DEFECT SIZE: 1 INCH.SDR 2005UALA00853Fitting · crackedCRACK IN FUSELAGE MAIN FRAME FITTING UNDER CABIN FLOOR AT STA 616 RBL 70, INNER CHORD AT BOTTOM 2 RIVETS.SDR ASOA05681Fitting · crackedDURING A C-CHECK, THE FITTING UNDER THE FLOOR AT FS 461, RBL 9 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE FITTING UNDER THE FLOOR AT FS 461, RBL 9. (K)SDR ASOA05699Nut Plate · corrodedDURING A C-CHECK IN MCN, THE NUT PLATE AT FS 530, RBL 44 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS SUBMITTING A DAMAGE REPORT TO BOMBARDIER FOR ISSUANCE OF AN REO TO DETERMINE THE APPROPRIATE CORRECTIVE ACTION. S/D - MAINTENANCE REMOVED THE CORRSDR ASOA05679SWeb · corrodedDURING A C-CHECK, THE LT FLOOR ATTACH WEB AT FS 559.80 TO FS 574 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED THE CORROSION ON THE LT FLOOR ATTACH WEB AT FS 559.80 TO FS 574 BY COMPLYING WITHSDR USAA051025Stringer Clip · crackedBFM - Q2 - STRINGER CLIP, .250 INCH CRACK, STA 277; STR 9 L STR CLIP. INSTALLED REPAIR STRINGER CLIP STA 907 IAW SRM. (K)SDR USAA051013Clip · corrodedPIT - S2 - CLIP, 2 INCH X 1 INCH CORROSION; LEVEL 1; TASK JA-220-53500, FRAME C-20 AND AFT CORNER OF FWD SERVICE DOORWAY. REPAIRED WITH MANUFACTURED PART IAW SRM. (K)SDR 05FDEA02499Stringer Clip · damagedFUSELAGE, UPPER LOBE, STA 680 STR 2L, STRINGER CLIP DAMAGED. REPLACED STRINGER CLIP AT BS 680, STR 2L PER SRM 51-30-2.SDR ASAA0570055Fitting · corrodedPAE - DURING C-CHECK, FOUND LEFT WHEEL WELL CUTOUT AFT WEB CORRODED. REPAIRED IAW SRM 51-40-02. (M)SDR USAA051008Angle · corrodedCLT - Q6 - ANGLE, KEEL BEAM HAS FRETTING WEAR ON IT 17 IN X 1 INCH, CORRODED, STA 727-710, LBL 8. REMOVED SURF CORROSION, BLENDED AND TREATED IAW SRM, DWG. (K)SDR UPS05845236Fitting · corrodedHEAVY CORROSION ON SPLICE FITTING STA 210 L7R. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.SDR 05FDEA02470Stringer Clip · brokenFUSELAGE UPPER LOBE, STA 660, STRINGER CLIP 8L BROKEN. REMOVED AND REPLACED STRINGER CLIP AT STR 8L BS 660 IAW SRM 51-30-2.SDR USAA051004Bracket · crackedCLT - Q1 - BRACKET, 1 INCH, CRACK, STA 360, STR 7L BRACKET. REMOVED DAMAGED BRAKET, FRABRICATED NEW BRACKET AND INSTALLED, ISW SRM AND DWG. (K)SDR UPS05845285Fitting · crackedFS -8 AT L33L BULKHEAD HAS CRACKED END FITTING A/C COMPT. REMOVED AND REPLACED END FITTING AT FS -8 L33L IAW SRM 51-3-0,51-3-2 PG 1 AND 51-1-21.
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