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"

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SDR ASAA9680028Longeron · corrodedPAE - DURING 30K CHECK, CORROSION WAS FOUND ON LONGERON 29R FROM Y1117 TO Y1136. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW ASA EA 5310-01396. (M)Jan 20, 1996 · N936AS · Doug DC982SDR ASAA9680027Longeron · corrodedPAE - DURING 30K CHECK, CORROSION WAS FOUND ON LONGERON 30 FROM Y1245 TO Y1271, X-0, Z-50. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW DC-9 SRM 51-10-03, 51-30-02, 53-14-03 AND 53-02. (M)Jan 20, 1996 · N936AS · Doug DC982SDR 96FDEA00115Stringer · damagedGOUGE ON STRINGER AT BS 460 STR 3R. REMOVED DAMAGED SECTION STR 3R BS 460, FABRICATED AND INSTALLED REPAIR PARTS PER FEDEX SRM 53-10-3.Jan 20, 1996 · N273FE · Boeing 727233SDR 96FDEA00114Stringer · damagedMECHANICAL DAMAGE IN HAT SECTION OF STRINGER, AT BS 620 STR 4R. REMOVED DAMAGED SECTION STRINGER 4R BS 620, FABRICATED AND INSTALLED REPAIR PARTS PER FEDEX SRM 53-10-3.Jan 20, 1996 · N273FE · Boeing 727233SDR DL72S960231Stringer · corrosionHMV ATL, CORROSION STA 1090 TO 1110. BULGED BETWEEN STRINGER AND SKIN APPROX 6 INCHES FWD OF 1090 TO 4 INCHES AFT OF 1110. REPAIRED DAMAGE PER SRM 53-12-0 FIG 807.Jan 19, 1996 · N517DA · Boeing 727232SDR DL72S960169Stringer · crackedDURING INSPECTION, CORROSION WAS REMOVED BY BLENDING AND SPOT FACING IN SEVERAL LOCATIONS ON THE UPPER SURFACE OF THE O/B AND I/B SKIN FLANGES, STRINGER 29L BETWEEN STA 950 AND STA 970. MINIMUM REMAINING FLANGE THICKNESS WAS .100. ALL CORROSION BLENDS ARE COJan 19, 1996 · N419DA · Boeing 727232SDR AALA960105Longeron · corrodedTUL - FOUND CORROSION STATION 1212 TO STATION 1231 LONGERON 26R AND LONGERON END FITTING. INSTALLED LONGERON SECTION AND SPLICED PER ESO 80559 DATED 1-18-96. (M)Jan 19, 1996 · N258AA · Doug DC982SDR 96FDEA00139Stringer · damagedBS 757 TO 759 STR 7L DAMAGE INSIDE STRINGER ABOVE RIVETS THROUGH SKIN. REPLACED STR PER SRM 53-10-3.Jan 19, 1996 · N492FE · Boeing 727227SDR 96FDEA00138Stringer · damagedUPPER LOBE BS 1072 TO 1090 STR 7R DAMAGE TO STRINGER INSIDE U-CHANNEL ABOVE SKIN RIVETS. INSTALLED REPAIR DOUBLER IAW BOEING SRM 53-10-3.Jan 19, 1996 · N492FE · Boeing 727227SDR 96FDEA00086Stringer · corrosionCORROSION (53-111-01-2), ON STR 28L BS 720 PLUS 4 WL 149. REMOVED, FABRICATED AND REPLACED STR 28L BS 720 PLUS 4 WL 149 IAW FEDEX SRM 53-10-2 AND 53-10-3.Jan 19, 1996 · N273FE · Boeing 727233SDR CAL960168Longeron · corrodedKUL - INSPECTION FOUND CORROSION IN RIGHT FLANGE OF LONGERON 30L AT STATION 1412. REPAIRED IAW ECRA 5310-03219. (M)Jan 18, 1996 · N13067 · Doug DC1030SDR CAL960167Longeron · corrodedKUL - INSPECTION FOUND CORROSION IN THE FLANGE OF LONGERON 37L AT STATION 1406. REPAIRED IAW ECRA 5310-03217. (M)Jan 18, 1996 · N13067 · Doug DC1030SDR AALA960076Stringer · corrodedFOUND CORROSION IN STRINGER 27 LEFT STATION 590 - 600. REMOVED CORROSION, CUT OUT BAD SECTION OF STRINGER AND INSTALLED STRINGER REPAIR PER SRM 53-10-3 PG 3-43. (M)Jan 18, 1996 · N898AA · Boeing 727223SDR 96FDEA00141Stringer · damagedUPPER LOBE BS 885 TO 888 STR 7L, DAMAGE TO STRINGER INSIDE U-CHANNEL. REMOVED FASTENERS, CUT OUT DAMAGED AREA, FABRICATED FILLER, REPAIRED PARTS 1, 2, 3. LOCATED AND DRILLED ALL HOLES, TREATED AND PRIMED ALL PARTS AND INSTALLED PER SRM 53-10-3 PAGES 5 TO 8 Jan 18, 1996 · N492FE · Boeing 727227SDR 96FDEA00140Stringer · damagedUPPER LOBE BS 882 TO 889 STR 7R DAMAGED TO STR INSIDE U-CHANNEL ABOVE SKIN RIVETS. REMOVE DAMAGED STR 7R FROM BS 872 TO 898, FABRICATED PARTS 1, 2, 3 AND 4. DRILLED AND INSTALLED PER SRM 53-10-3 FIG 3.Jan 18, 1996 · N492FE · Boeing 727227SDR 96FDEA00066Stringer · corrodedCORROSION (C53-224-03-1/2) ON STR 22R, BS 396. REMOVED CORROSION AT BS 396, STR 22R. REMOVED IN A 1 INCH BY 2 INCH AREA. ORIGINAL METAL THICKNESS IS .040 INCH. REMOVED .009 INCH, FOUND TO BE OUT OF LIMITS PER FEDEX SRM 53-10-1. FABRICATED AND INSTALLED REJan 18, 1996 · N169FE · Boeing 72722SDR 9601661157Longeron · corrodedDURING L-CHECK, FOUND CORROSION ON THE RBL 7 LONGERON FITTING FROM FS 1509 TO 1521 IN THE CENTER GEAR WHEEL WELL. REPLACED THE FITTING PER SRM 51-00-00 FIG 2.Jan 18, 1996 · N157US · Doug DC1040SDR USAA960097Stringer · corrosionINT - DURING CX-6 CHECK VISUAL INSPECTION, FOUND TWO LOCATIONS 2 INCHES BY 4 INCHES CORRODED AND 2 INCHES BY 8 INCHES CORRODED AT STRINGER 27L, BS 927 TO 967. INSTALLED STRINGER AND DOUBLERS. REPAIRED PER SRM 53-10-3, FIG 1. (M)Jan 17, 1996 · N249US · Boeing 737201SDR USAA960087Stringer · corrosionINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 2 INCH CORRODED AREA AT FLOOR STRINGER, BS 787 TO BS 847 RBL 14 INCHES. REMOVED DAMAGED FLOOR STRINGER, COMPLETED INSTALLATION AND REPAIR OF FLOOR STRINGER. REPAIRED PER SRM 53-00-53 FIG 202 ALSO, SRMJan 17, 1996 · N423US · Boeing 737401SDR USAA960062Stringer · corrosionCLT - INSPECTION VISUALLY FOUND LEVEL 2 CORROSION, 6 INCHES LOCATED ON STRINGER 27L AT FS 967. INSTALLED REPAIR CHANNEL AND ANGLES AS PER BOEING SRM 53-00-03 FIGURE 201, DETAIL VII. (M)Jan 17, 1996 · N371US · Boeing 7373B7SDR DP2R5889Stringer · cracksAD 83-15-08 R1 FOUND STRINGER CRACKED. BS 236 STR 23R, .080 INCH LINEAR INDICATION. BS 500, STR 23R, 2 EACH LINEAR INDICATIONS, EACH .300 INCH LENGTH. (X)Jan 17, 1996 · N1543 · Bac 111203AESDR CAL960166Longeron · corrodedKUL - INSPECTION FOUND CORROSION IN FLANGE OF LONGERON 32L AT STATION 1409. REPAIRED IAW ECRA 5310-03215. (M)Jan 17, 1996 · N13067 · Doug DC1030SDR 96FDEA00107Stringer · crackedUPPER LOBE STR 3L STA 440 CRACKED. INSTALLED REPAIR ON STR 3L STA 440 PER MM 53-10-3 PG 5 WITH FAB PARTS ON SHOP ORDER FE7X, FM7K, FM69.Jan 17, 1996 · N487FE · Boeing 727227SDR UPS805414Longeron · crackedWHILE IN FOR C-CHECK MAINTENANCE REPORTED, 4 CRACKS IN O/B LOWER FLANGE OF LONGERON 35L 340 TO 348. REPLACED LONGERON SECTION FS 190 TO 390 PER SRM 51-1-20D.Jan 16, 1996 · N701UP · Doug DC871FSDR UPS805409Longeron · crackedWHILE IN FOR C-CHECK MAINTENANCE REPORTED, LONGERON 35L CRACKED FS 260. REPLACED LONGERON SECTION PER SRM 51-1-20D.Jan 16, 1996 · N701UP · Doug DC871FSDR AALA960073Longeron · corrodedTUL - FOUND LONGERON 25R IS CORRODED FROM STATION 1212-1231. CUT OUT 19 INCHES OF CORRODED LONGERON. INSTALLED NEW PIECE OF LONGERON AND LONGERON SPLICE PER SRM 53-02 FIG 5. (M)Jan 16, 1996 · N258AA · Doug DC982SDR 9601652298Longeron · corrodedDURING H-CHECK, FOUND CORROSION ON STR 27R AT BS 623. REPAIRED STRINGER (P/N 65-56236), PER EA 22-103428.Jan 16, 1996 · N298US · Boeing 727251SDR ASAA9680016Longeron · corrodedPAE - DURING 30K CHECK, CORROSION WAS FOUND ON LONGERON 30L AT Y769 TO Y788. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW DC-9 SRM 51-30-05. (M)Jan 15, 1996 · N936AS · Doug DC982SDR ASAA9680015Longeron · corrodedPAE - DURING 30K CHECK, CORROSION WAS FOUND ON LONGERON 29L AT Y210 TO Y236. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW DC9-SRM 51-10-03, 51-30-02 AND 53-14-01. (M)Jan 15, 1996 · N936AS · Doug DC982SDR 96FDEA00736Stringer · crackedNR 1247, MAIN DECK STRINGER FOUND CRACKED AT BS 1980 AT STR 13L AS MARKED. STRINGER REPAIRED AS PER FEDEX 727 SRM REV 76 53-10-03 FIG 2.Jan 15, 1996 · N640FE · Boeing 747245FSDR 96FDEA00467Stringer · crackedSTATION (SIN) SNRM (1248). MAIN DECK STRINGER FOUND CRACKED AT BS 1980, AT S12L AS MARKED. C/A STRINGER REPAIRED PER FEDEX SRM REV 76-53-10-03, PAGE 2.Jan 15, 1996 · N640FE · Boeing 747245FSDR 96FDEA00073Stringer · crackedFOUND STRINGER 34L SEVERED FWD OF PREVIOUS SKIN CRACK STATION FS 545. FABRICATED STRINGER 34L PER SAMPLE AND INSTALLED PER SRM 51-00-01.Jan 15, 1996 · N602FE · Doug MD11FSDR 96FDEA00071Stringer · crackedFORWARD END OF STRINGER 35L CRACKED FROM RIVET HOLE TO FWD END LENGTH. APPROXIMATELY .1250 INCH FS 545 CONFIRMED BY HFEC. FABRICATED STRINGER 35L PER SAMPLE AND INSTALLED STRINGER PER SRM 51-00-01.Jan 15, 1996 · N602FE · Doug MD11FSDR 9601632298Longeron · corrosionDURING H-CHECK, FOUND CORROSION ON STR 29L AT BS 1000. REPAIRED STRINGER (P/N 65-56144-3), PER EA 22-103431.Jan 15, 1996 · N298US · Boeing 727251SDR UPS805394Longerons · crackedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED, B/T FITTING CRACKED F.S. 1230, BETWEEN LONGERONS 33R-34R. REPLACED FITTING PER SRM 51-1-20D.Jan 14, 1996 · N701UP · Doug DC871FSDR GTIA96NK048Longeron · corrodedDURING C-CHECK, FOUND CORROSION AT THE FOLLOWING STATIONS; STA 889 AND LONGERON 24LT TO 30LT, STATION 945 LONGERON 26LT TO 30LT, STATION 1030 LONGERON 26LT TO 27LT, STA 1129 LONGERON 29RT TO 30RT, STATION 1098 AND 113 FLOOR SUPPORT. REMOVED CORROSION AND TREAJan 12, 1996 · N12536 · Doug DC932SDR GTIA96NK045Longeron · corrodedDURING C-CHECK, FOUND STATION 617 LONGERON 14 LEFT HAS SURFACE CORROSION FROM SKIN TO SPLICE AREA. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3. (M)Jan 12, 1996 · N12536 · Doug DC932SDR GTIA96NK043Longeron · corrodedDURING C-CHECK, FOUND STATION 639, LONGERON 14R HAS SURFACE CORROSION FROM CLIP TO INTERCOSTAL AREA. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3. (M)Jan 12, 1996 · N12536 · Doug DC932SDR GTIA96NK042Longeron · corrodedDURING C-CHECK, FOUND STATION 627 LONGERON 14RH HAS CORROSION FROM SKIN TO SPLICE AREA. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3. (M)Jan 12, 1996 · N12536 · Doug DC932SDR 96FDEA00040Stringer · corrodedCORROSION (C53-224-01), ON STR FLANGE AT BS 720 STR 4L. REMOVED DAMAGED SECTION OF STR, FABRICATED AND INSTALLED REPAIR PARTS PER FEDEX SRM 53-10-3.Jan 12, 1996 · N488FE · Boeing 727227SDR 9601623214Longeron · corrodedDURING 1C1 CHECK, FOUND CORROSION ON FUSELAGE STRINGERS 41R, 43R AND 44 EACH BETWEEN FRAMES 33 TO 34. REPAIRED STRINGERS PER EA 32-105085, -105086 AND -105087.Jan 12, 1996 · N314US · Airbus A320211SDR MWEA95010Longeron · chafedDURING C-CHECK, FOUND FRAME AT STA 1076 LONGERON 20R IS CHAFED FROM LOOSE STANDOFF BRACKET. INSTALLED DOUBLER REPAIR IAW SRM 53-03 FIG 4.Jan 10, 1996 · N602ME · Doug DC932SDR 9600721154Longeron · corrodedDURING T-CHECK, FOUND CORROSION ON LONGERONS 29R TO 31R BETWEEN FS 1401 TO 1521. REPAIRED LONGERONS PER EA 11-104451.Jan 10, 1996 · N154US · Doug DC1040SDR 9600709302Longeron · corrodedDURING H-CHECK, FOUND CORROSION ON LONGERON 26L AT FS 600 TO 675. REPAIRED LONGERON (P/N 5936051-501) PER EA 93-103423.Jan 9, 1996 · N302RC · Doug DC982SDR UPS805397Longerons · crackedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED, LONGERONS CRACKED 35L, F.S. 260-270. REPLACED LONGERON SECTION F.S. 250-310 PER SRM 51-1-20D.Jan 8, 1996 · N701UP · Doug DC871FSDR 96ZZZX2489Stringer · corrodedDURING ROUTINE INSPECTION OF AIRCRAFT, 5 EACH FASTENER HEADS WERE FOUND PULLING THROUGH THE SKIN ALONG FUSELAGE STR 28R AND BS 1030, BS 1060, AND FUSELAGE SKIN WAS FOUND BULGING DUE TO CORROSION. ONCE THE AREA WAS DISASSEMBLED, DAMAGE WAS FOUND TO EXTEND BACKJan 8, 1996 · N40482 · Boeing 72722SDR 96FDEA00106Stringer · corrodedAFT CX COMP STR 29L IS CORRODED ON O/B SIDE AT BELLFRAME STA 950E, AFT SIDE OF BELLFRAME. BEYOND LIMITS PER SRM 53-10-1, REPAIRED PER FEDEX EA 7-5310-26899.Jan 8, 1996 · N487FE · Boeing 727227SDR 96FDEA00033Stringer · damagedMECH DAMAGE AND FASTENERS MISSING IN STR 7L BS 757 TO 759. ACCOMPLISHED STR REPAIR AT STA 740 TO 770 STR 7L PER FEDEX SRM 53-10-1, 53-10-2 AND 53-10-3.Jan 8, 1996 · N488FE · Boeing 727227SDR 96FDEA00027Stringer · damagedDAMAGED STR AT BS 660 STR 7L. REPAIRED DAMAGED STR 7L BS 660 PER FEDEX SRM 53-10-3, BY REMOVING DAMAGED SECTION AND FABRICATING REPAIR PARTS AND INSTALLING THEM.Jan 8, 1996 · N488FE · Boeing 727227SDR CAL960246Stringer · corrodedINSPECTION FOUND STRINGER AND FAIL-SAFE STRAP SKIN CORRODED AT STA 1010 - STA 1014, LBL 18. THE CORRODED AREAS WERE CUT OUT. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-1 AND SRM 53-30-3. (X)Jan 7, 1996 · N73751 · Boeing 727227
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