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 SWAA051087Stringer Clip · crackedDURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 705, STR 7R. REMOVED AND REPLACED CLIP PER SRM.Apr 13, 2005 · N313SW · Boeing 7373H4SDR SWAA051060Stringer Clip · crackedDURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 277, STR 10R & STR 14R. REMOVED AND REPLACED CLIP PER SRM.Apr 12, 2005 · N313SW · Boeing 7373H4SDR SWAA051059Stringer Clip · crackedDURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 578, STR 5R TO STR 8R. REMOVED AND REPLACED CLIP PER SRM.Apr 12, 2005 · N313SW · Boeing 7373H4SDR SWAA051058Stringer Clip · crackedDURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 597, STR 1R TO STR 8R. REMOVED AND REPLACED CLIP PER SRM.Apr 12, 2005 · N313SW · Boeing 7373H4SDR USAA050501Fitting · crackedCLT - FOUND BEAM FITTING CRACKED .75 INCH, STATION 601 LEFT LOWER BEAM FITTING. FABRICATED AND INSTALLED REPAIR ANGLE IAW EA 96446 AND TR 53-62-01. (M)Apr 12, 2005 · N440US · Boeing 7374B7SDR UPS05444335Stringer Clip · crackedINSPECTION TYPE:C COCKPIT - BS 360 S-8L FRAME/STR TIE CLIP CRACKED. ( CRACK LENGTH 0.5" ). COCKPIT BS 360 STR -8L TIE CLIP REPLACED AS PER SRM 51-10-01 P.9.Apr 12, 2005 · N523UP · Boeing 747283BSDR SWAA051071Stringer Clip · crackedDURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 727, BL 0. REMOVED AND REPLACED CLIP PER SRM.Apr 12, 2005 · N697SW · Boeing 7373TOSDR SWAA051057Stringer Clip · crackedDURING SCHEDULED D-CHECK, FOUND 2 EA FUSELAGE STRINGER CLIPS CRACKED AT BS 597, STR 8L & STR 9L. REMOVED AND REPLACED CLIPS PER SRM.Apr 12, 2005 · N313SW · Boeing 7373H4SDR SWAA051056Stringer Clip · crackedDURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 578, STR 8L. REMOVED AND REPLACED CLIP PER SRM.Apr 12, 2005 · N313SW · Boeing 7373H4SDR SWAA051054Stringer Clip · crackedDURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 294, STR 13L. REMOVED AND REPLACED CLIP PER SRM.Apr 12, 2005 · N313SW · Boeing 7373H4SDR ASAA0510057Attach Fitting · out of toleranceBSTA 460 BETWEEN STRINGER 20L AND 21L SKIN TO FRAME ATTACHMENT HAS LOW EDGE MARGIN. REPAIRED IAW SRM. (K)Apr 11, 2005 · N730AS · Boeing 737290CSDR UPS05444428Fitting · corrodedU/D - STA 496 RBL 70 TOILET TANK TIE DOWN FTG CORROSION FOUND. CORROSION BLEND OUT 0.020" BY 1" BY 1". TIE DOWN FTG REPLACED AS PER SRM 51-10-01 PG 9.Apr 11, 2005 · N523UP · Boeing 747283BSDR UPS05444372Stringer Clip · corrodedINSPECTION TYPE: C, BS 1600 LT STR 3L TIE CLIP FOUND CORRODED. CORROSION BLEND OUT 0.021 X 1 X 3 INCH EXCEED SRM LIMITS. TIE CLIP REPLACED AT BS 1600 STR 3L AS PER SRM 51-10-01 PG 9.Apr 11, 2005 · N523UP · Boeing 747200SDR UPS05444359Stringer Clip · corrodedINSPECTION TYPE: C - BS 1500, STR 3R, FRAME TIE CLIP FOUND CORROSION. CORROSION BLEND OUT 0.029 X 0.5 X 0.5 INCH EXCEED SRM 53-10-01 FIG 1 LIMITS, TIE CLIP REPLACED AS PER SRM 51-10-01 PG 9.Apr 11, 2005 · N523UP · Boeing 747200SDR UPS05444358Stringer Clip · corrodedINSPECTION TYPE: C- BS 1460 STR 6R FRAME TIE CLIP FOUND CORROSION. CORROSION BLEND OUT 0.010 X 0.5 X 1 INCH EXCEED SRM 53-10-01 FIG 1 LIMITS. TIE CLIP REPLACED AS PER SRM 51-10-01 PG 9.Apr 11, 2005 · N523UP · Boeing 747200SDR UPS05444357Stringer Clip · corrodedINSPECTION TYPE:C M/D- BS 1416 STR -1R FRAME TIE CLIP FOUND CORROSION. CORROSION BLEND OUT 0.020 X 0.5 X 1 INCH EXCEED SRM 53-10-01 FIG 1 LIMITS. TIE CLIP REPLACED AS PER SRM 50-10-01 PG 9.Apr 11, 2005 · N523UP · Boeing 747200SDR UPS05444344Stringer Clip · crackedINSPECTION TYPE: C, M/D - BS 1640 STR 1R FRAME ATT TIE-CLIP FOUND CRACKED. (CRACK LENGTH .0625"), M/D- BS 1640 STR 1R FRAME ATT TIE-CLIP REPLACED AS PER SRM 51-10-01 PG 9.Apr 11, 2005 · N523UP · Boeing 747283BSDR UPS05444343Stringer Clip · crackedINSPECTION TYPE: C, M/D- BS 1640 LT STR -1L TIE-CLIP FOUND CRACKED. (CRACK LENGTH .125" ), M/D BS1640 STR -1L TIE-CLIP REPLACED AS PER SRM 51-10-01 PG 9.Apr 11, 2005 · N523UP · Boeing 747283BSDR UPS05444412Stringer Clip · crackedBS 1940 STR 19R STRINGER TIE CLIP FOUND CRACKED (CRACK LENGTH 1/4 INCH) . BS1940 STR 19R STR TIE CLIP REPLACED AS PER SRM 51-10-01 PG 9.Apr 10, 2005 · N523UP · Boeing 747283BSDR UPS05444360Stringer Clip · corrodedINSPECTION TYPE: C, STA 2100 STR 5R TIE CLIP CORROSION FOUND. CORROSION BLEND OUT 0.012 X 0.5 X 0.5 INCH EXCEED SRM 53-10-01 FIG 1 LIMITS. TIE CLIP REPLACED AS PER SRM 51-10-01 PG 9.Apr 10, 2005 · N523UP · Boeing 747200SDR UPS05444356Stringer Clip · corrodedINSPECTION TYPE:C M/D - STA 1980 STR 4R TIE CLIP CORROSION FOUND. CORROSION BLEND OUT 0.016 X 2 X 2 INCH EXCEED SRM 53-10-01 FIG 1 LIMIT. TIE CLIP REPLACED AS PER SRM 51-10-01 PG 9.Apr 10, 2005 · N523UP · Boeing 747200SDR UPS05444336Stringer Clip · crackedINSPECTION TYPE:C M/D -BS 1940 STR 18R STRINGER TIE CLIP FOUND CRACKED. (CRACK LENGTH 3/8" ) TIE CLIP REPLACED AS PER SRM 51-10-01 PG 9 AT BS 1940 STR 18R AREA.Apr 10, 2005 · N523UP · Boeing 747283BSDR ASOA05319Clip · crackedDURING C-CHECK, THE RT INBOARD CLIP AT FS 484 BETWEEN RBL 9 TO RBL 27 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINT REMOVED AND REPLACED THE RT IB CLIP AT FS 484 BETWEEN RBL 9 TO RBL 27 IAW SRM. (K)Apr 8, 2005 · N820AS · Cndair CL6002B19SDR SWIA200515702Stringer Clip · crackedSTATION 280 LBL 9.00' INBOARD CLIP CRACKED AT TOP RADIUS; RBL 9.00' INBOARD AND OUTBOARD CLIP CRACKED AT TOP RADIUS, ITEM FOUND AT C-CHECK INSPECTION. INSTALLED NEW CLIPS AT STA 280 RBL 9.0 INBD SIDE AND AT STA 280 RBL 9.0 INBD AND OTBD IAW CRJ200 SRM 51-10-0Apr 6, 2005 · N903SW · Cndair CL6002B19SDR UPS05844410Fitting · crackedALL L31L SPLICE FITTINGS (3 TOTAL) CRACKED BETWEEN STA 440-520. REMOVED AND REPLACED ALL (3 EA.) SPLICE FITTINGS IAW SRM 51-20-00, 53-2-2 AND 51-1-20D.Apr 6, 2005 · N810UP · Doug DC873FSDR SWIA200514895Clip · crackedCRACKED CLIP AT STA 625.00 STR 14R, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED FLOOR SUPPORT ANGLE AS PER IAW CRJ REO 601R-53-61-117 REV B.Apr 6, 2005 · N465SW · Cndair CL6002B19SDR A6WA200540141Clip · crackedFOUND CRACK ON CLIP AT FS 280 RIGHT SIDE APPROX .5 INCH IN LENGTH AT TOP CORNER IN. REMOVED AND REPLACED RT FS 280 CLIP IAW CRJ SPM 51-42-06 FOR SOLID RIVETS AND 51-45-21 FOR HILITES. (M)Apr 6, 2005 · N417AW · Cndair CL6002B19SDR 05FDEA00870Fitting · damagedWING FITTING REQUIRED RESLEEVING DUE TO BLENDED DAMAGE OUT OF LIMITS. SO, THE BODY FITTING ALSO NEED TO BE RESLEEVED. REPAIRED LT 740 WING TERMINAL FITTING PER FED EX EA 7-5710-86260.Apr 6, 2005 · N481FE · Boeing 727227SDR UPS05844411Attach Angle · corrodedHAT CHANNEL ATTACH ANGLE O/B SIDE CORRODED STA 920-940 RBL 58 RT W/W. REPAIRED BY REPLACEMENT OF I/B AND O/B HAT CHANNEL ATTACH ANGLES, WEB AND FINGER DOUBLER, REPAIR SPLICES. REPLACEMENT RETAINER AND REPLACEMENT PRESSURE PANEL ANGLE, IAW 51-1-21, 53-2-0, 51Apr 5, 2005 · N810UP · Doug DC873FSDR UPS05844367Fitting · crackedINSPECTION TYPE:C1 A PIT AT DOOR CUTOUT APPROX STA 335 HAS 1 EA CRACKED BACK UP FITTING. REMOVED AND INSTALLED BACKUP FITTING AND SPLICES IAW SRM 53-02-00-05, AND 51-1-20D.Apr 5, 2005 · N810UP · Doug DC873FSDR ASAA0510066Attach Fitting · corrodedYXX - FRAME ATTACHMENT CORRODED AT BS 520 BETWEEN STRINGER 28L AND 28R. REPLACED SKIN TO FRAME ATTACHMENT IAW B737-200 SRM 51-10-1 PARAGRAPH 9A AND 51-30-2 FIGURE 3. (M)Apr 4, 2005 · N730AS · Boeing 737290CSDR A6WA200540159Clip · crackedFLOORBEAM CLIP AT FS 280, LBL 9, INBOARD IS CRACKED IN RADIUS APPROX 33 INCHES. REMOVED AND REPLACED ANGLE P/N 601R31113-57 IAW SRJ SRM 51-42-06, 51-42-21 AND BRAS EO 601R-53-6212. (M)Apr 4, 2005 · N416AW · Cndair CL6002B19SDR EIA2005091Stringer Clip · crackedM/D STA 2220 STR 22L ATTACHED TIE CLIP CRACKED. TIE CLIP REPLACED PER SRM 51-10-01 AND 51-30-02.Apr 4, 2005 · N485EV · Boeing 747212BSDR UPS05844284Attach Fitting · crackedINSPECTION TYPE: C1, FRAME TO INTERCOSTAL FITTING CRACKED 3 INCH LONG, AT STA 900 L18L. REMOVED, FABBED AND INSTALLED REPLACEMENT FITTING IAW SRM 53-2-0, 51-1- 8, 51-1-20D, AND DWG 4779496.Apr 4, 2005 · N810UP · Doug DC873FSDR A6WA200540133Clip · crackedFLOOR SUPPORT BEAM CLIP AT FS484, LBL 36, IS CRACKED FROM TOP RIVET HOLE TO EDGE APPROX. (0.30 INCH). (K)Apr 4, 2005 · N416AW · Cndair CL6002B19SDR A6WA200540132Clip · crackedFLOOR SUPPORT BEAM CLIP AT FS 280, RBL 9 OB IS CRACKED IN RADIUS APPROX 0.52 INCH. (K)Apr 4, 2005 · N416AW · Cndair CL6002B19SDR A6WA200540131Clip · crackedFLOOR SUPPORT BEAM CLIP AT FS 280, RBL 9 IB IS CRACKED IN RADIUS APPROX ( 0.50 INCH). (K)Apr 4, 2005 · N416AW · Cndair CL6002B19SDR A6WA200540130Clip · crackedFLOOR SUPPORT BEAM CLIP AT FS 280, LBL 9, IB IS CRACKED IN RADIUS APPROX (0.33 INCH). (K)Apr 4, 2005 · N416AW · Cndair CL6002B19SDR A6WA200540128Clip · crackedFLOOR SUPPORT BEAM CLIP AS FS280, LBL 9.0, OB IS CRACKED IN RADIUS APPROX 0.30. REMOVED AND REPLACED ANGLE P/N 601R31113-57 IAW CRJ 200 SRM 51-42-06, 51-42-21 AND BRAS EO 601R-53-6212. (M)Apr 4, 2005 · N416AW · Cndair CL6002B19SDR 05FDEA00834Stringer Clip · corrodedCORROSION C53-113-01 (1) UNDER LEVELING COMPOUND BS 660 STR 28R. FOUND CORROSION TO BE 100 PERCENT MATERIAL LOSS, REPAIRED DOUBLER, SHEAR TIE PER SRM 53-10-4, 53-30-3.Apr 4, 2005 · N272FE · Boeing 727200SDR ASOA05297Clip · crackedDURING A C-CHECK, THE ATTACH CLIP AT FS 625 LT ABOVE THE BOX BEAM WAS FOUND TO BE CRACKED BEYOUND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE ATTACH CLIP AT FS 625 LT. (K)Apr 3, 2005 · N820AS · Cndair CL6002B19SDR ASOA05306Fitting · crackedDURING A (C) CHECK, THE FITTING IN THE RT SIDE PRESSURE FLOOR UNDER 262CRF AT APPROX FS 454.00 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE FITTING IN THE RT SIDE PRESSURE FLOOR UNDER 262CRF AT APPROXIMATELY FS 454.00. (K)Apr 3, 2005 · N820AS · Cndair CL6002B19SDR SWIA200515558Fitting · crackedFS 460 OB FLOOR FITTING RBL 9.0 CRACKED, ITEM FOUND AT C-CHECK INSPECTION. FITTING REPLACED IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-23-00, 51-21-11.Apr 2, 2005 · N917SW · Cndair CL6002B19SDR ASOA05292Stringer Clip · crackedDURING A C-CHECK IN MCN, THE RIGHT INBOARD FS 280 CLIP WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE RIGHT INBOARD FS 280 CLIP. (M)Apr 2, 2005 · N862AS · Cndair CL6002B19SDR UPS05844361Fitting · crackedINSPECTION TYPE: C1, BANANA FITTING CRACKED.25 INCH LONG STA 1220 L33R. REMOVED AND REPLACED BANANA FITTING IAW SRM 51-01-20D AND 51-3-0.Apr 2, 2005 · N810UP · Doug DC873FSDR UPS05844278Fitting · crackedC1 FRAME TO CUSP FITTING CRACKED .25 INCH LONG AT STA 260 L21R. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D AND 51-3-0.Apr 2, 2005 · N810UP · Doug DC873FSDR UPS05844276Fitting · crackedC1 FITTING CRACKED 2 INCHES LONG AT STA 760 L13R. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.Apr 2, 2005 · N810UP · Doug DC873FSDR CALA0500095Support Bracket · crackedINSPECTION FOUND A 1.25 INCH CRACK IN ANTENNA SUPPORT BRACKET AT STA 727D + 5 INCH. THE BRACKET WAS REMOVED AND REPLACED IAW SRM 51-40-02.Apr 2, 2005 · N17326 · Boeing 7373T0SDR EIA2005083Shear Tie · crackedM/D BS 2160 21R SHEAR TIE CRACKED. SHEAR TIE REPLACED PER SRM 51-10-01.Apr 1, 2005 · N485EV · Boeing 747212BSDR EIA2005082Shear Tie · crackedM/D BS 1280 S11L-12L SHEAR TIE CRACKED. CRACK SHEAR TIE REPLACED PER SRM 51-10-01.Apr 1, 2005 · N485EV · Boeing 747212B
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