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 USAA060050Stringer Clip · crackedFOUND TIE CLIP CRACKED, BS 312 S-27L. FABRICATED AND INSTALLED NEW TIE CLIP IAW SRM 51-40-03 AND 02 AND BOEING DRW 69-37411, DEFECT SIZE: .25".Jan 17, 2006 · N784AU · Boeing 7374B7SDR IXXA06SMN037SFitting · corrodedDURING ROUTINE C CHECK INSPECTION, MAIN CARGO MPT FITTING FRAME, BEAM CORRODED STA 1308.000 L21L. REMOVED CORROSION IAW DC-8 SRM 51-1-8 PAGES 17-18. FOUND OUT OF LIMITS IAW DC-8 SRM 53-2-0 PAGE 2P. REMOVED CORRODED FITTING IAW DC-8 SRM 51-1-20D. CLEANED, TJan 16, 2006 · N606AL · Doug DC873FSDR ABXA060056Fitting · crackedFITTING AT LONGERON 24, FS 879, CRACKED. REPAIRED FITTING IAW REA D853-53104.Jan 16, 2006 · N812AX · Doug DC863FSDR CA060116007Bracket · brokenUPON APPROACH TO LAND ON LAKE, FLAPS 10 SELECTED. A/C IMMEDIATELY BEGAN TO ROLL TO LT, RETURNED FLAPS TO ZERO, A/C RETURNED TO LVL FLT. TRIED TO DEPLOY FLAPS AGAIN (SLOWLY) AND OBSERVED RT FLAP DEPLOYED NORMALLY, LT FLAP DID NOT MOVE, A/C THEN RETURNED TO WJan 15, 2006 · Cessna A185FSDR PIDA06007Attach Angle · crackedUPPER O/B ATTACH ANGLE FOR THE LEFT RAM AIR DUCT IS CRACKED. REPLACED ATTACH ANGLE PER SRM 51-10-02 AND 51-40-00.Jan 15, 2006 · N380WL · Boeing 7373G7SDR ABXA060043Fitting · corrodedBATHTUB FITTING HAD CORROSION AT LONGERON 34, ATTACH POINT BS 879. CORROSION FOUND OUT OF LIMITS OF DC8 SRM 53-2-0. REMOVED FITTING IAW DC8 SRM 51-1-20D. INSTALLED NEW FITTING IAW DC8 SRM 53-2-0, 51-1-20D, 51-3-1, AND 51-1-8.Jan 14, 2006 · N825AX · Doug DC863SDR ASAA0640038Stringer Clip · crackedPAE - FOUND STRINGER CLIP CRACKED AT BS 500B, STRINGER 11 RT. REMOVED AND REPLACED STRINGER CLIP AT BS 500B, STRINGER 11 RT IAW B737-400 SRM 51-40-02. (M)Jan 13, 2006 · N780AS · Boeing 7374Q8SDR ASAA0640037Stringer Clip · crackedPAE - FOUND STRINGER CLIP CRACKED AT BS 500D, STRINGER 11 RT. REMOVED AND REPLACED STRINGER CLIP AT BS 500D, STRINGER 11 RT IAW B737-400 SRM 51-40-02. (M)Jan 13, 2006 · N780AS · Boeing 7374Q8SDR ASAA0640036Stringer Clip · crackedPAE - FOUND STRINGER CLIP CRACKED AT BS 500A, STRINGER 11 RT. REMOVED AND REPLACED STRINGER CLIP AT BS 500A, STRINGER 11 RT IAW B737-400 SRM 51-40-02. (M)Jan 13, 2006 · N780AS · Boeing 7374Q8SDR UPS06846119Fitting · corrodedINSPECTION TYPE:C1 HEAVY CORROSION ON FITTING IN OB UPPER AFT CORNER OF LT W/W STA 974 LBL66. REMOVED, FABRICATED AND INSTALLED FITTING IAW 51-1-20D, DWG 2647420,Jan 13, 2006 · N702UP · Doug DC871FSDR AWXA200600171Fitting · corrodedSAL - MAJOR REPAIR - DURING C07 CHECK DISCOVERED CORROSION ON CORNER FITTING LOWER SILL, FRAME 20 AT BL Y1975L. NO ALLOWABLE LIMITS WERE FOUND IN THE AIRBUS SRM. MAINTENANCE REMOVED AND INSTALLED A NEW FITTING AT FRAME 20 AND Y1975L IAW AIRBUS 320 SRM 51-72-Jan 13, 2006 · N602AW · Airbus A320232SDR AWXA200600168Fitting · corrodedSAL- MAJOR REPAIR - DURING C-07 CHECK CORROSION WAS FOUND ON RIVET AND CORNER SILL PLATE. CORNER SILL FRAME 20R REPLACED IAW A320 SRM 51-72-11 PAGE 1-2.Jan 13, 2006 · N602AW · Airbus A320232SDR UPS06846033Fitting · crackedINSPECTION TYPE:C1 MAIN CABIN LONGERON END FITTING HAS A 4" CRACK, STA 680 L8R. REMOVED END FITTING IAW SRM 51-1-20D, FABRICATED AND INSTALLED LONGERON END FITTING AT STA 680 L8R IAW SRM 51-01-20D.Jan 13, 2006 · N702UP · Doug DC871FSDR ABXA060044Fitting · corrodedBATHTUB FITTING HAD CORROSION AT LONGERON 24, ATTACH POINT BS 940. CORROSION FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-20. INSTALLED NEW FITTING IAW DC8 SRM 53-2-0, 51-1-20D, 51-3-0, AND 51-1-8.Jan 13, 2006 · N825AX · Doug DC863SDR ABXA060038Fitting · crackedLEFT WHEEL WELL (KEEL AREA) LONGERON ATTACH END FITTING AT STA 750, LEFT BUTT LINE 8 (BELOW HYD RESERVOIR) HAD A 6 - 8 INCH CRACK ON VERTICAL LEG. REMOVED AND REPLACED ATTACH END FITTING IAW DC9 SRM 51-30-1 AND 51-30-5.Jan 13, 2006 · N947AX · Doug DC931SDR 06FDEA0183Stringer Clip · corrodedINTERIOR FUSELAGE, STR CLIPS HAS CORROSION BETWEEN BS 700 TO BS 720, STR 2L. REMOVED AND REPLACED THREE STR CLIPS AT STR 2L BS 700, BS 703 AND BS 713 IAW SRM 51-30-2.Jan 13, 2006 · N488FE · Boeing 727200SDR A6WA200640038Clip · crackedFS 280 FLOORBEAM CLIP OB SIDE LBL 9 IS CRACKED NEAR RADIUS APPROX .50 INCH. MAINTENANCE INSTALLED NEW CLIP OB SIDE LBL 9 IAW SRM. (K)Jan 12, 2006 · N428AW · Cndair CL6002B19SDR A6WA200640041Clip · crackedFS 280 FLOORBEAM CLIP OB SIDE RBL 9 IS CRACKED REAR RADIUS APPROX .50 INCH. MAINTENANCE REMOVED AND REPLACED BRACKET PN 601R31113-58 IAW SRM. (K)Jan 12, 2006 · N428AW · Cndair CL6002B19SDR A6WA200640040Clip · crackedFS 280 FLOOR BEAM CLIP IB SIDE RBL 9 IS CRACKED NEAR RADIUS APPROX .50 INCHES. MAINTENANCE REMOVED AND REPLACED ANGLE PN 601R3111358 IAW SRM. (K)Jan 12, 2006 · N428AW · Cndair CL6002B19SDR A6WA200640039Clip · crackedFS 280 FLOORBEAM CLIP IB SIDE LBL 9 IS CRACKED NEAR RADIUS APPROX .50 INCH. MAINTENANCE INSTALLED NEW CLIP AT IB SIDE LBL9 IAW SRM. (K)Jan 12, 2006 · N428AW · Cndair CL6002B19SDR AWXA200600316Attach Angle · corrodedMCN - DURING C24 CHECK DISCOVERED CORROSION ON WEB ATTACH ANGLE AT BS 847, WL 157 AND BL 20R. MAINTENANCE REMOVED AND INSTALLED NEW WEB ATTACH ANGLE AT BS 847, WL 157 AND BL 20R IAW BOEING 737-300 SRM 51-40-02-0G FIGURES 8, 12, AND 13.Jan 12, 2006 · N328AW · Boeing 7373B7SDR AWXA200600170Fitting · corrodedSAL - MAJOR REPAIR - DURING C07 CHECK DISCOVERED LEVEL 2 CORROSION ON LOWER SILL BRACKET FROM FORWARD PASSENGER LT DOOR. NO ALLOWABLE DAMAGE LIMITS WERE FOUND IN THE AIRBUS SRM. MAINTENANCE REMOVED AND INSTALLED A NEW FITTING ON THE FORWARD LT PASSENGER DOORJan 12, 2006 · N602AW · Airbus A320232SDR CA060111002Bracket · splitON LANDING IN YYZ,FORWARD ATTENDANTS SEAT BELT CAME FREE OF THE ATTACH BRACKET. UPON INVESTIGATION IT WAS FOUND THAT A WASHER WAS MISSING FROM THE RETAINING BOLT. THIS MISSING WASHER WAS LEFT OFF THE BOLT AT INSTALLATION BY A PREVIOUS OPERATOR.Jan 11, 2006 · Boeing 737522SDR ASAA0640020Fitting · corrodedFWD LAV AFT WALL IB TIE DOWN FITTING CORRODED. REMOVED AND REPLACED FWD LAV AFT WALL IB TIE DOWN FITTING IAW SRM. (K)Jan 10, 2006 · N780AS · Boeing 7374Q8SDR AWXA200600376Clip · crackedMCN - DURING C24 CHECK DISCOVERED INTERCOSTAL SUPPORT CLIP CRACKED. 500 INCHES IN LENGTH, AT BS 693.75, WL 207 AND BL. 25L. MAINTENANCE REMOVED, FABRICATED AND INSTALLED REPLACEMENT INTERCOSTAL SUPPORT CLIP AT BS 693.75, WL 207 AND BL .25L IAW AMERICA WEST AIJan 10, 2006 · N328AW · Boeing 7373B7SDR AWXA200600332Stringer Clip · crackedMCN - DURING C24 CHECK DISCOVERED STRINGER CLIP CRACKED, .125 INCHES IN LENGTH, AT BS 847 AND STR 4L. MAINTENANCE REMOVED AND INSTALLED NEW STRINGER CLIP AT BS 847 AND STR 4L IAW BOEING 737-300 SRM 51-40-02-0G FIGURES 8 AND 12.Jan 10, 2006 · N328AW · Boeing 7373B7SDR AWXA200600330Stringer Clip · crackedMCN - DURING C24 CHECK DISCOVERED TWO INTERCOSTAL SUPPORT CLIPS CRACKED, .4 INCHES, AT BS 693.75 AND BL .25R. MAINTENANCE REMOVED, FABRICATED AND INSTALLED REPLACEMENT INTERCOSTAL SUPPORT CLIPS AT BS 693.75 AND BL .25R IAW AMERICA WEST AIRLINES ENGINEERING REJan 10, 2006 · N328AW · Boeing 7373B7SDR USAA060005Attach Angle · crackedFOUND ANGLE CRACKED BS 877; S-11L. REMOVED CRACKED ANGLE. FABRICATED AND INSTALLED NEW ANGLE IAW BOEING DRW 69-45156; SRM 51-10-02, DEFECT SIZE: APPROX 1/4" CRACK.Jan 10, 2006 · N784AU · Boeing 7374B7SDR USAA060015Stringer Clip · crackedFOUND TIE CLIP CRACKED S-4R, BS 727E. INSTALLED NEW CLIP CC NR 1133482. INSTALLED IAW SRM 51-10-02, DEFECT SIZE: SHEETMETAL NR 5958 S-4R TIE CLIP CRACKED BS 727E.Jan 10, 2006 · N784AU · Boeing 7374B7SDR USAA065Attach Angle · crackedBS 877; S-11L CRACKED. REMOVED CRACKED ANGLE. FABRICATED & INSTALLED NEW ANGLE IAW BOEING DRW 69-45156; SRM 51-10-02, DEFECT SIZE: APPROX .25 INCH CRACK.Jan 10, 2006 · N784AU · Boeing 7374B7SDR USAA0615Stringer Clip · crackedS-4R, BS 727E CRACKED. INSTALLED NEW CLIP CC 1133482, INSTALLED IAW SRM 51-10-02, DEFECT SIZE: SHEETMETAL 5958 S-4R TIE CLIP CRACKED BS 727E.Jan 10, 2006 · N784AU · Boeing 7374B7SDR 06FDEA0139Stringer Clip · corrodedINTERIOR FUSELAGE, STR CLIP 3L HAS CORROSION BS 720A. *S/D* REMOVED AND REPLACED STR CLIP 3L BS 720 IAW SRM 51-30-2.Jan 10, 2006 · N488FE · Boeing 727200SDR 06FDEA0137Stringer Clip · crackedINTERIOR FUSELAGE, STR CLIP 4L IS CRACKED, BS 680. *S/D* REMOVED AND REPLACED CRACKED STR CLIP 4L AT BS 680 IAW SRM 51-30-2.Jan 10, 2006 · N488FE · Boeing 727200SDR 06FDEA0133Stringer Clip · corrodedINTERIOR FUSELAGE, STR CLIP 3R HAS CORROSION BS 720A. *S/D* REMOVED AND REPLACED STR CLIP 3R BS 720A IAW SRM 51-30-2.Jan 10, 2006 · N488FE · Boeing 727200SDR 06FDEA0132Stringer Clip · corrodedINTERIOR FUSELAGE, STR CLIP 5R HAS CORROSION BS 720A. *S/D* REMOVED AND REPLACED STR CLIP 5R BS 720A IAW SRM 51-30-2.Jan 10, 2006 · N488FE · Boeing 727200SDR USAA055Attach Angle · crackedBS 877; S-11L CRACKED. REMOVED CRACKED ANGLE. FABRICATED & INSTALLED NEW ANGLE IAW BOEING DRW 69-45156; SRM 51-10-02, DEFECT SIZE: APPROX .5 INCH CRACK.Jan 10, 2006 · N784AU · Boeing 7374B7SDR USAA0515Tie Clip · crackedSTR 4R, BS 727E CRACKED. INSTALLED NEW CLIP CC 1133482, INSTALLED IAW SRM 51-10-02, DEFECT SIZE: SHEETMETAL 5958 S-4R TIE CLIP CRACKED BS 727E.Jan 10, 2006 · N784AU · Boeing 7374B7SDR AWXA200600334Attach Angle · corrodedDURING C24 CHECK DISCOVERED CORROSION ON THE R1 LOWER SILL, INBOARD ATTACH ANGLE FROM BS 304 TO BS 324, BL 62R AND WL 209. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-10-15-1A1. MAINTENANCE REMOVED AND INSTALLED NEW ATTACH ANGLE AT THE Jan 9, 2006 · N328AW · Boeing 7373B7SDR AWXA200600333Stringer Clip · crackedMCN - DURING C24 CHECK DISCOVERED STRINGER CLIP CRACKED, .125 INCHES IN LENGTH, AT BS 616 AND STR 4R. MAINTENANCE REMOVED AND INSTALLED NEW STRINGER CLIP AT BS 616 AND STR 4R IAW BOEING 737-300 SRM 51-40-02-0G FIGURES 8 AND 12.Jan 9, 2006 · N328AW · Boeing 7373B7SDR AWXA200600331Stringer Clip · crackedMCN - DURING C24 CHECK DISCOVERED TWO STRINGER CLIPS CRACKED, .125 INCHES IN LENGTH EACH, AT BS 639 STR 2L AND STR 4L. MAINTENANCE REMOVED AND INSTALLED NEW STRINGER CLIP AT BS 639 2L AND 4L IAW BOEING 737-300 SRM 51-40-02-0G FIGURES 8 AND 12.Jan 9, 2006 · N328AW · Boeing 7373B7SDR AWXA200600329Stringer Clip · crackedMCN - DURING C24 CHECK DISCOVERED STRINGER CLIP CRACKED, .25 INCHES, AT BS 663 AND STR 10L. MAINTENANCE REMOVED, FABRICATED AND INSTALLED REPLACEMENT STRINGER TIE CLIP AT BS 663 AND STR 10L IAW BOEING 737-300 SRM 51-40-02-0G FIGURES 8, 12 AND BAC DWG 69-41437Jan 9, 2006 · N328AW · Boeing 7373B7SDR UPS06846018Fitting · corrodedINSPECTION TYPE:C1 MAIN CARGO DOOR JAMB PLATE FITTING HAS HEAVY INTERGRANULAR CORROSION. REMOVED CORRODED FITTING IAW SRM 51-1-21 LOCATED AND DRILLED NEW FITTING AND INSTALLED AT MAIN CARGO DOOR JAMB IAW SRM 51-3-2, 51-1-21, AND SRM 51-3-0.Jan 8, 2006 · N852UP · Doug DC873FSDR UPS06845977Attach Angle · crackedINSPECTION TYPE:C1 MAIN CARGO DOOR JAMB PLATE,THRESHOLD ATTACHED ANGLE CRACKED 1/4" AT FWD LATCH SPOOL. REMOVED, FABRICATED AND INSTALLED REPLACEMENT ATTACH ANGLE IAW SRM 51-3-0 AND DWG NR 5772786. TVL # 7268745.Jan 8, 2006 · N852UP · Doug DC873FSDR AWXA200600317Attach Angle · crackedMCN - DURING C24 CHECK DISCOVERED CRACK, 1.1 INCHES LONG, ON THE R1 DOOR LOWER FORWARD TORQUE BOX FLOOR WEB ATTACH ANGLE AT BS 298, WL 208 AND BL 53R. MAINTENANCE REMOVED, FABRICATED AND INSTALLED REPLACEMENT WEB ATTACH ANGLE AT BS 298, WL 208 AND BL 53R IAWJan 7, 2006 · N328AW · Boeing 7373B7SDR ASOA06076Nut Plate · corrodedDURING A C-CHECK, CORROSION WAS FOUND AROUND THE NUT PLATE AT FS 536, LBL42. MAINTENANCE REPAIRED AROUND THE NUT PLATE AT FS 536, LBL 42, IAW REO. (K)Jan 7, 2006 · N844AS · Cndair CL6002B19SDR USAA061Clip · corrodedSTA 1670-1680 CORRODED. REMOVED & REPLACED WITH NEW FLOOR SUPPORT (CLIP) PER SRM 53-00-51, 51-10-02, 51-40-05, 51-20-01, DEFECT SIZE: 5.40"L X 2.40"W X .069"D.Jan 7, 2006 · N629AU · Boeing 7572B7SDR USAA051Clip · corrodedSTA 1670-1680 CORROSION. REMOVED AND REPLACED WITH NEW FLOOR SUPPORT (CLIP) IAW SRM 53-00-51, 51-10-02, 51-40-05, 51-20-01, DEFECT SIZE: 5.40 INCH L X 2.40 INCH W X .069 INCH D.Jan 7, 2006 · N629AU · Boeing 7572B7SDR SWIA200616539Attach Fitting · crackedAFT EQUIPMENT COMP, INTERCOSTAL CLIPS ARE CRACKED, LT & RT, FS 621.00 - FS 625.00, STR 14L & STR 14R. ITEM FOUND AT C-CHECK INSPECTION. CLIPS REPLACED IAW CRJ REO 601R-53-61-100 REV NC AND REO 601R-53-61-422 REV NC.Jan 6, 2006 · N906SW · Cndair CL6002B19SDR SWIA200616537Attach Fitting · crackedFUSELAGE, FLOORBEAM TO TRANSVERSE ATTACH CLIPS ARE CRACKED, I/B & O/B LOCATIONS, FS 280.0, RBL 9.0. ITEM FOUND AT C-CHECK INSPECTION. INBOARD CLIP REPLACED IAW SRM 51-40-11, 51-23-00, 51-42-06, 51-42-21, 51-21-11 AND 51-25-16. OUTBOARD CLIP REPLACED IAW CRJJan 6, 2006 · N906SW · Cndair CL6002B19SDR ASOA06023SDoubler · corrodedDURING A C-CHECK, CORROSION WAS FOUND ON THE DOUBLER AT FS 467-473, LBL 43-37. MAINTENANCE REPAIRED THE DOUBLER AT FS 467-473, LBL 43-37, IAW REO. (K)Jan 6, 2006 · N844AS · Cndair CL6002B19
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