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"

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 USAA020309Stringer · corrodedPIT - FOUND STRINGER CORRODED ON ENDS OF STRINGER STATION 323.7 AND BL 0 TO S28R. (M)Jul 30, 2002 · N393US · Boeing 7373B7SDR USAA020299Stringer · crackedPIT - FOUND STRINGER CRACKED .125 INCH, AT RIVET STATION 927 AT STRINGER 8R AND 9R. REMOVED CRACK AND INSTALLED OVERSIZED FASTENER PER 51-40-05. (M)Jul 30, 2002 · N393US · Boeing 7373B7SDR USAA020300Stringer · crackedPIT - FOUND STRINGER CRACKED .25 INCH, STATION 907, STRINGER 8L-9L AT RIVET. REMOVED CRACKED AND INSTALLED A REPAIR ANGLE PER TYPICAL REPAIR 53-10-14A. (M)Jul 30, 2002 · N393US · Boeing 7373B7SDR UPS02839138Longeron · crackedINSPECTION TYPE:C1 R2 DOOR UPPER AFT DOOR JAMB LONGERON 11 CRACKED APPROX 2 INCHES, FOUND BY X-RAY INSPECTION. REMOVED AND REPLACED LONGERON IAW DC8 SRM 51-1-21 AND 51-1-20D.Jul 30, 2002 · N715UP · Doug DC871FSDR UPS02839126Longeron · crackedINSPECTION TYPE:C1 R2 DOOR UPPER AFT DOOR JAMB LONGERON 11 CRACKED APPROX 2 INCHES, FOUND BY X-RAY INSPECTION. REMOVED AND REPLACED LONGERON IAW DC8 SRM 51-1-21 AND 51-1-20D.Jul 30, 2002 · N715UP · Doug DC871FSDR UPS02839125Longeron · crackedINSPECTION TYPE:C1 R2 DOOR UPPER AFT DOOR JAMB, LONGERON 11 CRACKED APPROX 2 INCHES, FOUND BY X-RAY INSPECTION. REMOVED AND REPLACED LONGERON IAW DC8 SRM 51-1-21 AND 51-1-20D.Jul 30, 2002 · N715UP · Doug DC871FSDR AWXA200200763Attach Angle · crackedMCN - MAJOR REPAIR - DURING C-18 CHECK A 1 1/2" CRACK WAS FOUND ON WEB UPPER CHORD (ATTACH ANGLE) AT FASTENER HOLES BS 500B TO BS 520, BL 0, WL 208.1. MAINTENANCE REMOVED WEB UPPER CHORD BS 500B TO BS 520, FABRICATED A REPAIR ANGLE AND INSTALLED REPAIR IAW DWGJul 30, 2002 · N183AW · Boeing 737277SDR 2002UALA01250Stringer · dentedFUSELAGE STRINGER 16L DENTED STATION 610-615. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. INSTALLED STRINGER SPLICE REPAIR.Jul 30, 2002 · N542UA · Boeing 757222SDR MWEA020468Fastener · crackedSKIN CRACK INDICATION NOTED STATION 180 JUST RIGHT OF LONGERON ONE. -- REMOVED AND INSTALLED FASTENERS INTO FORMERS.Jul 30, 2002 · N800ME · Doug DC914SDR MWEA020469Finger Doubler · crackedSKIN CRACKED INDICATION NOTED STATION 525 JUST RIGHT OF LONGERON ONE (MARKED). -- FABRICATED AND INSTALLED SKIN PLUG AND FINGER DOUBLER.Jul 30, 2002 · N800ME · Doug DC914SDR SIMA200221204Stringer · gougedABI - FOUND STRINGER 19L GOUGED. BLENDED GOUGE. FABRICATED TWO DOUBLER, FOUR SHIMS. REPAIR DONE IAW EMB145 SRM 145/1142, CHAPTER 53, REV 18, 53-24-02, EMB GST 2298/02A, AND STANDARD SRM PRACTICES. (M)Jul 27, 2002 · N623AE · Emb EMB145LRSDR UPS02838977Longeron · crackedINSPECTION TYPE:C2 LONG 24L IS CRACKED AT STA 978. STOP DRILLED CRACK, NDT VERIFIED CRACK TERMINATES AT STOP DRILL, FABRICATED AND INSTALLED DOUBLER IAW SRM 53-2-2 FIG 5.Jul 26, 2002 · N772UP · Doug DC871FSDR GTIA020912Longeron · crackedFTW - FOUND E/E BAY LONGERON 24L AT STATION 200 HAS EXFOLIATION/CRACK WHERE CAP IS FASTENED TO LONGERON. REMOVED DAMAGED SECTION OF LONGERON. LOCATED AND DRILLED NEW LONGERON AND LONGERON SPLICE. INSTALLED LONGERON AND SPLICES. (M)Jul 24, 2002 · N819NK · Doug DC981SDR SIMA200221202Stringer · gougedABI - FOUND STRINGER 19R GOUGED. BLENDED GOUGE. FABRICATED A DOUBLER ANGLE, TWO SHIMS. REPAIR DONE IAW EMB-145 SRM 145/1142, CHAPTER 53 REV 18, 53-24-02, AND STANDARD SRM PRACTICES. (M)Jul 24, 2002 · N623AE · Emb EMB145LRSDR SWAA021653Splice · crackedDURING SCHEDULED 1/2D CHECK, FOUND STRINGER SPLICE'S CRACKED (2 EA) AT BS 908, STR 4R AND STR 4L. REPAIRED SPLICE'S PER SRM.Jul 24, 2002 · N330SW · Boeing 7373H4SDR ASAA0280233Longeron · corrodedOAK - DURING C-CHECK, FOUND LONGERON 30, IN MID CARGO AREA, CORRODED BEYOND LIMITS FROM STATION 636 TO 655. REPLACED LONGERON 30 FROM STATION 579-788 PER SRM 51-30-5, PAGE 3, FIG 2. (M)Jul 23, 2002 · N951AS · Doug DC982SDR F3LA200200206Tie Clip · crackedDURING C-7 CHECK, INSPECTION FOUNG A BROKEN TIE CLIP TO STRINGER AT STA 639 STR 4L. mAINTENANCE INSTALLED NEW STRINGER TIE CLIP AT STA 639 STR 4L IN ACCORDANCE WITH SRM 51-10-02 AND 51-40-03.Jul 23, 2002 · Boeing 737317SDR F3LA200200205Tie Clip · crackedDURING C-7 CHECK, INSPECTION NOTED CRASKS IN TIE CLIP TO STRINGER AT TOP RIVET AT STA 663 STR 10 LH. MAINTENANCE REPAIRED THE CONDITION BY INSTALLING A NEW CLIP AT STA 663 STR 10 L IN ACCORDANCE WITH SRM 51-10-02.Jul 23, 2002 · Boeing 737317SDR ZW0A0208003Longeron · damagedDURING CHECK-C LONGERON 28R DAMAGED AT FUSELAGE STATION 110 TO FUSELAGE STATION 129. REPAIRED LONGERON 28A FUSELAGE STATION 110 TO FUSELAGE STATION 129 PER SRM 53-02 FIG 18. NO CRACKS FOUND PART 6-51-00-03.Jul 23, 2002 · N9619V · Doug DC983SDR 02FDEA00507Stringer · corrodedCORROSION SKIN BULGE AT BS 1075, STRINGER R28. REMOVED AND REPLACED STRINGER PER SRM 53-10-1, 53-10-3.Jul 22, 2002 · N203FE · Boeing 727200SDR F3LA200200200Stringer · crackedDURING C-7 CHECK, INSPECTION REPORTED A CRACK IN TIE CLIP TO STRINGER AT STA 616, STR 4R. MAINTENANCE REMOVED AND REPLACED CRACKED STRINGER WITH NEW PART IN ACCORDANCE WITH SRM 51-10-02.Jul 22, 2002 · Boeing 737317SDR ABXA030229Longeron · corrodedREMOVE AND REPLACE LONGERON 32 LEFT INBOARD CHANNEL STA. 190 - 385. REMOVED CORRODED SECTION, FABRICATED LONGERON AND SPLICES. INSTALLED IAW DC-8 SRM 51-1-20D, 53-2-2, AND 51-1-8.Jul 20, 2002 · N816AX · Doug DC863FSDR ABXA030228Longeron · corrodedLONGERON 32 LEFT OB CHANNEL AT STA. 370 WAS CORRODED. REMOVED CORRODED SECTION OF LONGERON, FABRICATED LONGERON AND SPLICES. INSTALLED IAW SRM 51-1-20D, 51-1-24, AND 53-2-2.Jul 20, 2002 · N816AX · Doug DC863FSDR ABXA030230Longeron · corrodedLONGERON 35 RIGHT INBOARD CHANNEL WAS CORRODED AT STA 340. CUT AND REMOVED DAMAGED SECTION, FABRICATED NEW SECTION AND REPAIR SPLICES. INSTALLED IAW DC-8 SRM 53-2-2 AND 51-1-20D.Jul 20, 2002 · N816AX · Doug DC863FSDR IXXA0200100SSkin · corrodedDURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED ON THE FUSELAGE SKIN STATION 1000 LONGEORN 19L. REPAIR ACCOMPLISHED, REMOVAL OF DAMAGE, FABRICATION AND INSTALLAION OF REPAIR DOUBLER IN ACCORDANCE WITH THE DOUGLAS STRUCTURAL REPAIR MANUAL AND ENGINEEJul 20, 2002 · N41CX · Doug DC862FSDR CALA0200422Longeron · corrodedINSPECTION FOUND LONGERON 20L CORRODED AT FS 1174. REPAIRED IAW ECRA 5310-04264.Jul 20, 2002 · N83873 · Doug DC982SDR ASAA0280228Longeron · corrodedOAK - DURING C-CHECK, FOUND CORROSION AROUND AND UNDER RIVETS ALONG LONGERON 22R AT FUSELAGE STATION 160-180. CUT OUT DAMAGED SKIN FROM STATION 150 TO 177 BETWEEN L21R AND L23R. SPLICED IN NEW L22R SECTION FROM STATION 110-229 PER SRM 53-02 FIG 18. INSTALLEJul 19, 2002 · N951AS · Doug DC982SDR GTIA020872Longeron · crackedFTW - FOUND LONGERON 25L AT STATION 160 IN E/E COMPARTMENT IS CRACKED. REMOVED DAMAGED SECTION OF LONGERON. LOCATED AND DRILLED LONGERON SPLICE. INSTALLED LONGERON AND SPLICES. (M)Jul 19, 2002 · N819NK · Doug DC981SDR ABXA020167Longeron · crackedLONGERON 17 CRACKED AT FS 256. REPLACED SECTION OF LONGERON 17 RIGHT, STATION 230 - 268 IAW DC-9 SRM 53-02.Jul 18, 2002 · N974AX · Doug DC941SDR 2002FA0000849Stringer · crackedDURNING ANNUAL INSPECTION FOUND RIVETS SHEARED AND MISSING FROM HOLES ON RIGHT REAR WING SPAR ATTACH FITTING ASSY. THIS ASSEMBLY IS ATTACHED TO CENTER SECTION. CARRY THRU UNDER BAGGAGE COMPARTMENT FLOOR. ALSO ON THIS AC THE STRINGER WAS CRACKED AND BUCKLED. Jul 18, 2002 · N6174P · Piper PA24250SDR CALA0200418Longeron · corrodedINSPECTION FOUND LONGERON 26L CORRODED ON O/B SURFACE AT FS 1200. THE LONGERON WAS REMOVED AND REPLACED IAW ECRA 5310-04268.Jul 18, 2002 · N83873 · Doug DC982SDR CALA0200414Longeron · corrodedINSPECTION FOUND LONGERON 19L CORRODED AT FS 1174. THE CORRODED SECTION OF LONGERON WAS REMOVED AND REPLACED IAW EA 9-5312-2-A0961.Jul 18, 2002 · N83873 · Doug DC982SDR GTIA020938Stringer · corrodedFTW - FOUND STRINGER 30 CORRODED FS 617 TO 610, FS 617-636, 636-655, 674-655. FOUND TO BE OUT OF LIMITS. REMOVED LONGERON REPAIR STATION. FABRICATED LONGERON SPLICES AND REPAIR STATION. INSTALLED LONGERON 30 AND SPLICES REPAIR. (M)Jul 16, 2002 · N819NK · Doug DC981SDR GTIA020937Splice · corrodedFTW - FOUND STRINGER 30 SPLICE FITTING CORRODED FS 579-595. DUPLICATED LONGERON SPLICE. SPLICES FS 579-FS 595 TO BE INSTALLED ON WC B00038 118 N 00108. (M)Jul 16, 2002 · N819NK · Doug DC981SDR SIMA200220003Stringer · chafedABI - FOUND STRINGER 19R CHAFED. BLENDED CHAFED, FABRICATED AND INSTALLED A DOUBLER ANGLE, IAW EMB 145 SRM 145/1142, CHAPTER 53, REV 18 53-24-02, AEA ETN-51-020. (M)Jul 16, 2002 · N625AE · Emb EMB145LRSDR SIMA200220002Stringer · chafedFOUND STRINGER 19L CHAFED. BLENDED CHAFE, FABRICATED AND INSTALLED TWO DOUBLER ANGLES IAW EMB GST-2182/02, AEA ETN-51--020. (M)Jul 16, 2002 · N625AE · Emb EMB145LRSDR ASOA02412Stringer · corrodedDURING C-CHECK INSPECTION IN BNA, STRINGER 17 LEFT WAS FOUND TO BE CORRODED OUT OF LIMITS BETWEEN FRAMES 20 AND 22. MAINTENANCE REMOVED AND REPLACED THE CORRODED STRINGER IAW SRM 51-40-02. (M)Jul 15, 2002 · N639AS · Emb EMB120ERSDR ASOA02411Stringer · corrodedDURING C-CHECK INSPECTION IN BNA, CORROSION WAS FOUND OUT OF LIMITS ON STRINGER 18 LEFT BETWEEN FRAMES 13A AND 15A. MAINTENANCE REMOVED AND REPLACED THE CORRODED STRINGER SECTION IAW SRM'S 51-25-00 AND 51-40-02. (M)Jul 15, 2002 · N639AS · Emb EMB120ERSDR ASOA02410Stringer · corrodedDURING C-CHECK INSPECTION IN BNA, STRINGER 21 LEFT WAS FOUND TO BE CORRODED OUT OF LIMITS BETWEEN FRAMES 12 AND 13. MAINTENANCE REMOVED AND REPLACED THE CORRODED SECTION OF STRINGER IAW SRM'S 53-00-00 AND 51-21-02. (M)Jul 15, 2002 · N639AS · Emb EMB120ERSDR CALA0200399Longeron · corrodedINSPECTION FOUND LONGERON 21L CORRODED ON OUTBOARD SURFACE AT FS 1117. THE CORRODED SECTION OF LONGERON WAS REMOVED AND REPLACED IAW ECRA 5310-04264.Jul 15, 2002 · N83873 · Doug DC982SDR CALA0200397Stringer · corrodedINSPECTION FOUND STRINGER 26R CORRODED AT STA 1006-1016. THE CORRODED SECTION OF STRINGER WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW SRM 51-10-02.Jul 14, 2002 · N17344 · Boeing 7373T0SDR C7WA200200018Stringer · corrodedDURING C-CHECK INSPECTION, FOUND LEVEL 2 CORROSION ON FS STRINGER 26L BETWEEN BS 480 AND BS 720D. REPAIRED FUSELAGE STRINGER 26L FROM BS 480 TO BS 680 IAW SRM 53-10-3 FIG 1. (M)Jul 13, 2002 · N511PE · Boeing 727232SDR C7WA200200017Stringer · corrodedDURING C-CHECK INSPECTION, FOUND LEVEL 2 CORROSION ON STRINGER 25R BETWEEN BS 720F AND BS 740. REPAIRED FUSELAGE STRINGER 25R FROM BS 720D PLUS 5.00 TO BS 740 IAW SRM 53-10-3 FIG 3. (M)Jul 13, 2002 · N511PE · Boeing 727232SDR C7WA200200016Stringer · corrodedDURING C-CHECK INSPECTION, FOUND LEVEL 2 CORROSION ON STRINGER 22R BETWEEN BS 720 AND BS 740. REPAIRED FUSELAGE STRINGER 22R BETWEEN BS 720E PLUS 1.50 TO BS 740 IAW SRM 53-10-3 FIG 1. (M)Jul 13, 2002 · N511PE · Boeing 727232SDR C7WA200200015Stringer · corrodedDURING C-CHECK INSPECTION AT COOPESA-SJO, FOUND LEVEL 2 CORROSION ON STRINGER 21R BETWEEN BS 720F AND BS 740. REPAIRED FUSELAGE STRINGER 21R BETWEEN BS 720E PLUS 4.00 TO BS 740 IAW SRM 53-10-3 FIG 1. (M)Jul 13, 2002 · N511PE · Boeing 727232SDR C7WA200200014Stringer · corrodedDURING C-CHECK INSPECTION, FOUND LEVEL 2 CORROSION ON FUSELAGE STRINGER 25L BETWEEN BS 720F AND BS 740. REPAIRED FUSELAGE STRINGER 25L BETWEEN BS 720E PLUS 5.00 AND BS 740 IAW SRM 53-10-3 FIG 3. (M)Jul 13, 2002 · N511PE · Boeing 727232SDR C7WA200200013Stringer · corrodedDURING C-CHECK INSPECTION, FOUND LEVEL 2 CORROSION ON STRINGER 22L BETWEEN BS 720F AND BS 740. REPAIRED FUSELAGE STRINGER 22L FROM BS 720E PLUS 4.00 TO BS 740 IAW SRM 53-10-3 FIG 1. (M)Jul 13, 2002 · N511PE · Boeing 727232SDR C7WA200200012Stringer · corrodedDURING C-CHECK INSPECTION, FOUND LEVEL 2 CORROSION STRINGER 21L BETWEEN BS 720 AND 740. REPAIRED FUSELAGE STRINGER 21L FROM BS 720E PLUS 3 TO BS 740 IAW SRM 53-10-3 FIG 1. (M)Jul 13, 2002 · N511PE · Boeing 727232SDR C7WA200200011Stringer · corrodedDURING C-CHECK INSPECTION, FOUND LEVEL 2 CORROSION ON STRINGER 29R FROM BS 480 TO BS 540. REPLACED STRINGER 29R SECTION BETWEEN BS 480 AND BS 545 IAW SRM 51-30-2. (M)Jul 13, 2002 · N511PE · Boeing 727232SDR C7WA200200007Stringer · corrodedDURING C-CHECK INSPECTION, FOUND EXT FUSELAGE BETWEEN BS 440 AND BS 450 AT STRINGER 23R SKIN BULGED. REPAIRED STRINGER 23R FROM BS 440 TO BS 473 DUE TO LEVEL 2 CORROSION IAW SRM 53-10-3 FIG 1. FUSELAGE SKIN FOUND SATISFACTORY. (M)Jul 13, 2002 · N511PE · Boeing 727232
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