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.

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 CARGSep 11, 2005 · N302AW · Boeing 7373G7SDR 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.Sep 11, 2005 · N874UP · Doug DC873FSDR 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 DWGSep 9, 2005 · N801UP · Doug DC873FSDR UPS05845549Fitting · crackedLEFT FWD LOWER TRAP FITTING IS CRACKED. REMOVED AND REPLACED TRAP FITTING IAW DC-8 SRM 51-3-0 AND 51-2-20D.Sep 9, 2005 · N801UP · Doug DC873FSDR 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 51Sep 9, 2005 · N681CA · Boeing 7272S7SDR 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 Sep 9, 2005 · N9185Z · Helio H295SDR 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 ENSep 6, 2005 · N154AW · Boeing 7373G7SDR 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 03-5311-052Sep 6, 2005 · N154AW · Boeing 7373G7SDR 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 AMSep 6, 2005 · N154AW · Boeing 7373G7SDR 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. INSTSep 6, 2005 · N154AW · Boeing 7373G7SDR 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)Sep 6, 2005 · N424AW · Cndair CL6002B19SDR SWAA052712Stringer Clip · crackedDURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 294, STR 13L. REMOVED AND REPLACED CLIP PER SRM.Sep 6, 2005 · N614SW · Boeing 7373H4SDR 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 LIMSep 4, 2005 · N806DH · Doug DC873FSDR 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 SEALASep 4, 2005 · N806DH · Doug DC873FSDR 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.Sep 4, 2005 · N721CX · Doug DC872SDR 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.Sep 3, 2005 · N801UP · Doug DC873FSDR 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.Sep 3, 2005 · N721CX · Doug DC872SDR 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 BSSep 3, 2005 · N154AW · Boeing 7373G7SDR 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 DISep 2, 2005 · N806DH · Doug DC873FSDR 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.Sep 2, 2005 · N801UP · Doug DC873FSDR 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.Sep 2, 2005 · N801UP · Doug DC873FSDR UPS05845456Fitting · crackedLWR CARGO STA 1140 L35R FWD FITTING CRACKED 2 INCHES LONG. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-20D.Sep 2, 2005 · N801UP · Doug DC873FSDR 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.Sep 2, 2005 · N218FE · Boeing 727200SDR SWAA052663Stringer Clip · crackedDURING SCHEDULED D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 294, STR 13L. REMOVED AND REPLACED CLIP PER SRM.Sep 1, 2005 · N614SW · Boeing 7373H4SDR 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)Aug 31, 2005 · N772AS · Boeing 7374Q8SDR 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.Aug 31, 2005 · N801UP · Doug DC873FSDR 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.Aug 31, 2005 · N801UP · Doug DC873FSDR SWAA052644Stringer Clip · corrodedDURING SCHEDULED D CHECK, FOUND FUSELAGE STRINGER CLIP CORRODED AT BS 807, RBL 7. REMOVED AND REPLACED CLIP PER SRM.Aug 31, 2005 · N614SW · Boeing 7373H4SDR 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.Aug 26, 2005 · N526UP · Boeing 747212BSDR SWAA052596Stringer Clip · crackedDURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 380, STR 8L. REMOVED AND REPLACED CLIP PER SRM.Aug 26, 2005 · N617SW · Boeing 7373H4SDR SWAA052594Stringer Clip · crackedDURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 360, STR 8L. REMOVED AND REPLACED CLIP PER SRM.Aug 26, 2005 · N617SW · Boeing 7373H4SDR 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.Aug 25, 2005 · N672DL · Boeing 757232SDR SWAA052577Stringer Clip · crackedDURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 767, STR 27R. REMOVED AND REPLACED CLIP PER SRM.Aug 25, 2005 · N369SW · Boeing 7373H4SDR SWAA052570Stringer Clip · crackedDURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 663.75, STR 10R. REMOVED AND REPLACED CLIP PER SRM.Aug 25, 2005 · N617SW · Boeing 7373H4SDR 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.Aug 24, 2005 · N413SW · Cndair CL6002B19SDR 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 .Aug 24, 2005 · N360FE · Doug MD1010FSDR USAA051039Angle · crackedLEFT PACK BAY, AFT RIGHT CORNER CRACKED. FABRICATED ATTACH ANGLE SRM 51-10-02 BOEING DWG 66-24798, DEFECT SIZE: 1 INCH.Aug 23, 2005 · N588US · Boeing 737301SDR 2005UALA00853Fitting · crackedCRACK IN FUSELAGE MAIN FRAME FITTING UNDER CABIN FLOOR AT STA 616 RBL 70, INNER CHORD AT BOTTOM 2 RIVETS.Aug 21, 2005 · N913UA · Boeing 737522SDR 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)Aug 20, 2005 · N839AS · Cndair CL6002B19SDR 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 CORRAug 20, 2005 · N839AS · Cndair CL6002B19SDR 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 WITHAug 19, 2005 · N839AS · Cndair CL6002B19SDR 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)Aug 17, 2005 · N444US · Boeing 7374B7SDR 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)Aug 17, 2005 · N110UW · Airbus A320214SDR 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.Aug 17, 2005 · N483FE · Boeing 727227SDR ASAA0570055Fitting · corrodedPAE - DURING C-CHECK, FOUND LEFT WHEEL WELL CUTOUT AFT WEB CORRODED. REPAIRED IAW SRM 51-40-02. (M)Aug 16, 2005 · N614AS · Boeing 737790SDR 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)Aug 16, 2005 · N588US · Boeing 7373B7SDR UPS05845236Fitting · corrodedHEAVY CORROSION ON SPLICE FITTING STA 210 L7R. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.Aug 16, 2005 · N750UP · Doug DC871FSDR 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.Aug 16, 2005 · N483FE · Boeing 727227SDR 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)Aug 15, 2005 · N449US · Boeing 7374B7SDR 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.Aug 15, 2005 · N750UP · Doug DC871F
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