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 CALA9800217Longeron · corrodedINSPECTION FOUND LONGERON 29R CORRODED UNDER FLANGE AT STA 1322. THE CORRODED SECTION OF LONGERON WAS REMOVED AND A NEW SECTION WAS SPLICED IN IAW SRM 53-02, FIGURE 2.Feb 12, 1998 · N37882 · Doug DC981SDR DL72L980376Stringer · corrodedSTRINGER 29R WAS FOUND CORRODED NEAR FS 950E+10. THE STRINGER WAS CUT AT FS 950D+10 AND THE AFT SECTION REMOVED. A NEW SECTION OF STRINGER WAS SPLICED IN PER ER/A 363710-14, REV B.Feb 11, 1998 · N503DA · Boeing 727232SDR DHL9880628CStringer · corrodedAT C-CHECK, CUSP EXTRUSION LT AT STA 1260 CORRODED. FOUND LEVEL 2 EXFOLIATED CORROSION. REMOVED DAMAGED AREA FROM FS 1250 TO 1270, FABRICATED EXTRUSION AND INSTALLED PER EO MMC 382N0820 AND SRM 53-2-5.Feb 11, 1998 · N806DH · Doug DC873FSDR 98FDEA00100Stringer · crackedNR 0502 72C235-02, UPPER LOBE BS 720B - 720C, STR 15L CRACKED AT AFT FASTENER FWD OF ICE LIGHT HOUSING. REPAIRED CRACKED STRINGER PER SRM 53-10-3 FIG 5.Feb 11, 1998 · N477FE · Boeing 727227SDR 98FDEA00097Stringer · crackedNR 0029 003 WHILE WORKING 7-5450-7-3301L PT 11 FOUND CRACK IN STRINGER 14L AT BS 1243. REPAIRED STR 14L, BS 1233 TO BS 1253 IAW FED-EX SRM 53-10-3, 53-10-4.Feb 11, 1998 · N222FE · Boeing 727233SDR UPS98225741Stringer · corrodedINSPECTION TYPE:SI, CORROSION ON STR 21 RT, BS 575, WL 178. REMOVED DAMAGED SECTION OF STRINGER AND SPLICED IN REPAIR SECTION IAW SRM 53-10-3.Feb 10, 1998 · N904UP · Boeing 72751CSDR DL72S980363Stringer · corrodedFUSELAGE/STRINGER 29R/FS 950D PLUS 10, FS 1007. SPLICE REPAIR A SECTION OF STRINGER 29R NEAR FS 950D PLUS 10 WAS FOUND BADLY CORRODED. THE STRINGER WAS CUT AT STATION 950D PLUS 10 AND THE AFT END REMOVED. A NEW SECTION WAS SPLICED IN PER ER/A 363641-14, REVFeb 10, 1998 · N805EA · Boeing 727225SDR CKSA98021Longeron · damagedDUE TO WEATHER IN MIAMI AIRPORT SUCH AS HIGH WINDS, TORNADO'S AND FLYING DEBRIS, DAMAGE LOWER FUSELAGE FS 120.0 STRINGER 35R AND 34R. CUT OUT DAMAGED SECTION OF SKIN AND FABRICATED REPAIR DOUBLER, FILLER PLATE AND FINGER DOUBLERS IAW SRM 53-2-1. CUT OUT DAMAFeb 10, 1998 · N811CK · Doug DC863FSDR CALA9800212Longeron · crackedINSPECTION FOUND LONGERON 2L CRACKED AT STA 1418. A NEW SECTION OF LONGERON WAS SPLICED IN IAW SRM 53-02, FIGURE 18.Feb 10, 1998 · N14890 · Doug DC982SDR ABXA9800076Longeron · crackedDURING C-CHECK, FOUND LONGERON 17R CRACKED AT STATIONS 275, 313, 389, AND 408. REPAIRED CRACKED SECTIONS OF LONGERON IAW DC9 SRM 53-02.Feb 10, 1998 · N938AX · Doug DC931SDR AALA980298Stringer · corrodedTUL - CORROSION INSIDE OF STR 28R AT BS 950E +2 INCHES. REMOVED CORROSION PER SRM 51-10-6, REPAIRED STR PER ESO 11697 DATED 2-2-98. TST: 51,688 HOURS. CYCLES: 31,372. (X)Feb 10, 1998 · N887AA · Boeing 727223SDR AALA980295Stringer · crackedTUL - STR 17R CRACKED AT FORWARD END FASTENER HOLE STA 743. STOP DRILLED CRACK. INSTALLED DOUBLER IAW AARD 51-40-00-1. TST: 54,870 HOURS. CYCLES: 33,161. (X)Feb 10, 1998 · N879AA · Boeing 727223SDR AALA980294Stringer · corrodedTUL - STR 28L CORRODED STA 580 - STA 585. REMOVED CORE, INSTALLED STRINGER REPAIR IAW SRM 53-10-3. TST: 54,870.3 HOURS. CYCLES: 33,161. (X)Feb 10, 1998 · N879AA · Boeing 727223SDR 98FDEA00095Long Beam · corrodedNR 0557 041 STA-PAE - CORROSION (C53-224-01(2)) AROUND NUTCLIP HOLES LBL 45 LONGITUDINAL BEAM BS 838-843, WL 208. REMOVED AND REPLACED LBL 45 LONGITUDINAL BEAM WL 208 FROM BS 740 TO BS 848.5 PER BOEING 727 DRAWING 65-34144.Feb 10, 1998 · N144FE · Boeing 72721CSDR UPS98825806Longeron · corrodedINSPECTION TYPE-C, LONGERON 30R FS 35 TO 55 HAS HEAVY CORROSION AND OUT OF LIMITS. REMOVED AND REPLACED LONGERON IAW SRM 51-1-20D.Feb 9, 1998 · N752UP · Doug DC871FSDR SIMA980409Stringer · corrodedSAW - DURING CPCP-4 INSPECTION, MAINTENANCE REPORTED THAT STRINGER 21 LEFT BETWEEN FRAMES 39 AND 40 CORRODED. MAINTENANCE REPAIRED STRINGER 21 LEFT IAW SRM 53-00-00 FIG 428. A/C WAS RETURNED TO SERVICE. (M)Feb 9, 1998 · N423MQ · Aerosp ATR42300SDR DL72K980334Stringer · crackedSEVERAL OF THE FASTENER HOLES ON THE S18A STRINGER AT FS 940 OF BOTH RT AND LT SIDES WERE FOUND TO HAVE CRACKS AND OR CORROSION IN THEM. REPAIRED PER ERA 331316-14.Feb 9, 1998 · N472DA · Boeing 727232SDR AALA980290Stringer · corrodedTUL - CORROSION AT STR 29L AT STA 971. REMOVED CORROSION PER SRM 51-10-6. TREATED AND PRIMED PER 51-10-6. ACCOMPLISHED REPAIR PER ECO 11697 DATED 2-2-98. TST: 46,991. CYCLES: 24,531. (X)Feb 9, 1998 · N701AA · Boeing 727223SDR AALA980287Stringer · corrodedTUL - STR 25L CORRODED AFT OF 720F. INSTALLED STRINGER SPLICE REPAIR PER SRM 53-10-3 PAGES 1-11. TST: 51,688 HOURS. CYCLES: 31,372. 9X)Feb 9, 1998 · N887AA · Boeing 727223SDR AALA980285Stringer · corrodedTUL - CORROSION ON STR 24R AT STA 1166. REMOVED CORRODED STRINGER SECTION AND REPAIRED WITH STRINGER SPLICE AND DOUBLER PER SRM 53-10-3 PAGES 3-4B. TST: 51,688.24 HOURS. CYCLES: 31,370. (X)Feb 9, 1998 · N887AA · Boeing 727223SDR AALA0283Stringer · corrodedTUL - CORROSION INSIDE STR 25R AT FS 1145. INSTALLED STRINGER SPLICE REPAIR (STA 1140 TO STA 1158) PER SRM 53-10-3. TST: 51,688.24 HOURS. CYCLES: 31,372. (X)Feb 9, 1998 · N887AA · Boeing 727223SDR UPS98825807Longeron · crackedINSPECTION TYPE:C LONGERON 24R, CRACK HAS EXTENDED BEYOND PREVIOUS STOP DRILL AFT PAST 980 BULKHEAD AND HAS EXTENDED PAST STOP DRILL AT F/S 968 FWD TO F/S 962. REMOVED EXISTING REPAIR F/S 960-980, REMOVED LOWER FITTING F/S 960 IAW SRM 51-1-20. STOP DRILLED CFeb 7, 1998 · N866UP · Doug DC873FSDR EIAA98046Stringer · corrosionHKG - DURING 'C5/D' CHECK INSPECTION, AFT CARGO BS 1680 STRINGER 40L HAS CORROSION. REPAIRED IAW SRM 53-10-03 FIG 1. (M)Feb 7, 1998 · N471EV · Boeing 747273CSDR DHL9872414CStringer · corrodedAT C-CHECK, CORROSION AT STRINGER 27L, BS 950 TO 970, IN AFT BAG BIN. CUT OUT DAMAGED AREA, INSTALLED NEW STRINGER FROM STA 950 TO 970 PER SRM 53-10-3, 45 LONG. N/R 3673.Feb 7, 1998 · N724DH · Boeing 727228SDR 98ZZZX1247Longeron · crackedDISCOVERED ON REMOVAL OF LEFT TAIL BOOM PANEL DURING ROUTINE MAINTENANCE. LONGERON WAS CRACKED IN THREE PLACES. SUSPECT CAUSE INDICATES LACK OF PROPER DEBURRING AT RIVET HOLES IN SEVERAL PLACES. PREPPED COMPLETELY PRIOR TO INSTALLATION.Feb 6, 1998 · N2071S · Bell 412SDR 98FDEA00102Stringer · crackedNR 0221 BS 720B PLUS 5, STRINGER 15R END CRACKED AT HI-LOK FWD OF WING SCANNING LIGHT. CUT END OF STR HFEC CHECKED CUT EDGE OF STRINGER. FABRICATED U-CHANNEL OF .040 7075-T6 AND FILLERS. INSTALLED REPAIR IAW SRM 53-10-3 FIG 5.Feb 6, 1998 · N264FE · Boeing 727233SDR AALA980264Longeron · corrodedTUL - LONGERON 52 CORRODED AT STA 1139. REPLACED STR 52 FROM 1156 TO 1139, REINSTALLED BELL FRAMES AND SHEAR TIES PER SRM AARD 51-01-00-05. TREATED, PRIMED AND PAINTED PER SRM 51-21-01 VOL 4. TST: 60,422.53 HOURS. CYCLES: 20,166. (X)Feb 5, 1998 · N131AA · Doug DC1010SDR CALA9800190Stringer · corrodedINSPECTION FOUND STRINGER 27R CORRODED IN AFT CARGO COMPARTMENT BETWEEN STA 720 AND 720A. THE CORRODED SECTION OF STRINGER AND SKIN WERE REMOVED. A STRINGER REPAIR, REPAIR SPLICES, AND DOUBLER WERE FABRICATED AND INSTALLED IAW SRM 51-10-3, FIGURE 1, 53-30-3,Feb 4, 1998 · N17402 · Boeing 727243SDR CALA9800184Longeron · crackedINSPECTION FOUND A 2 INCH CRACK IN LONGERON AT STA 1129, STRINGER 36R. THE LONGERON WAS REMOVED AND REPLACED IAW SRM 53-10-00.Feb 4, 1998 · N14062 · Doug DC1030SDR AWXA9800063Stringer · crackedDURING SCHEDULED C-12 INSPECTION, FOUND CRACK IN STRINGER 14L AT BS 360 AND 350. REPAIRED PER SRM 51-70-13, 51-10-02 AND 51-40-02.Feb 4, 1998 · N158AW · Boeing 7373G7SDR UPS98225849Stringer · corrodedINSPECTION TYPE-SI, CORROSION (C53-111-01.00-01) ON STR 23L BS 352 TO 358. CORROSION FOUND OUT OF LIMITS PER SRM 53-10-1. REPLACED STRINGER WITH NEW ITEM PER SRM 51-10-1 AND 51-30-2.Feb 3, 1998 · N904UP · Boeing 72751CSDR UPS98225783Stringer · corrodedINSPECTION TYPE-SI, CORROSION ON STR 26 LT BS 370 TO 380. REMOVED DAMAGED SECTION, INSTALLED NEW STRINGER AND STRINGER SPLICE PER SRM 53-10-3 WITH FASTENER BS 360 TO 380.Feb 3, 1998 · N904UP · Boeing 72751CSDR SWAA980096Stringer · crackedDURING SCHEDULED SERVICE CHECK, FOUND STR TO FRAME CLIP CRACKED B/S 360, STR 4 RT. REPAIRED PER BOEING SRM.Feb 3, 1998 · N54SW · Boeing 7372H4SDR CALA9800179Stringer · corrodedINSPECTION FOUND STRINGER 28R IN FORWARD CARGO COMPARTMENT CORRODED BETWEEN STA 680 AND 700. THE STRINGER SPLICE WAS REMOVED AND A STRINGER SPLICE WAS FABRICATED AND INSTALLED IAW SRM 53-10-3, 51-30-02, 51-10-2, AND MM 51-20-11.Feb 3, 1998 · N17402 · Boeing 727243SDR CALA9800176Longeron · crackedINSPECTION FOUND A 2 INCH CRACK IN LONGERON AT STA 1129, STRINGER 36L. THE LONGERON WAS REMOVED AND REPLACED IAW SRM 53-00-00.Feb 3, 1998 · N14062 · Doug DC1030SDR 98FDEA00083Stringer · crackedNR 0832 035, AFTER ACCESSING SKIN ON NR 0648, FOUND STRINGER 6 LT TO BE CRACKED AROUND A FASTENER HOLE AT BS 460. REMOVED AND REPLACED LT STRINGER NR 6 SECTION, BS 450-490 IAW FED-EX SRM 53-10-3.Feb 3, 1998 · N145FE · Boeing 72727CSDR UPS98225743Stringer · corrodedINSPECTION TYPE:SI, CORROSION (SDN 53-111-01.00-02) ON STR 25 LT BS 492-497 WL 160. CORROSION FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. CUT OUT DAMAGED SECTION AND COMPLETED STANDARD REPAIR IAW SRM 53-10-3.Feb 2, 1998 · N904UP · Boeing 72751CSDR TWAA9802001Longeron · damagedSTL - DURING OP-9 MAINTENANCE CHECK, THE LOWER LONGERON LEG WAS FOUND DAMAGED AT L23 STATION 1366 AT APU AREA. REPAIRED L23 PER ARA 12000. (M)Feb 2, 1998 · N902TW · Doug DC982SDR TWAA9801701Longeron · crackedSTL - DURING OP16 MAINTENANCE CHECK, LONGERON 5L WAS FOUND WITH A .5 INCH CRACK AT STATION 737. REPAIRED PER SRM 53-02 FIG 18. (M)Feb 2, 1998 · N978Z · Doug DC931SDR TSAA9853078Stringers · cutCUT STRINGERS 23 AND 24R TO FACILITATE AFT OUTFLOW VALVE DOUBLER INSTALLATION. REPAIRS STRINGERS PER SRM 53-10-3 USING NEW DOULBER. (M)Feb 2, 1998 · N805AL · Boeing 7372M6CSDR SWAA980099Stringer · crackedDURING SCHEDULED SERVICE CHECK, FOUND NUMEROUS FASTENER HOLES CRACKED STR 14L B/S 990-1016, WITH HFEC ROTATING PROBE INSPECTION. REPAIRED PER ACO 6717-53 PART II AND XEA X2-53-194.Feb 2, 1998 · N54SW · Boeing 7372H4SDR SWAA980097Stringer · crackedDURING SCHEDULED SERVICE CHECK, FOUND STR 10 RT AT BS 540 HAS CRACKED STR SPLICE FITTING PER HFEC. REPAIRED PER BOEING SRM.Feb 2, 1998 · N54SW · Boeing 7372H4SDR 98ZZZX763Longeron · crackedDURING A MAINTENANCE PROCEDURE INVOLVING THE REMOVAL OF HORIZONTAL STABILIZER AND FUSELAGE FABRIC, FOUND A CRACK IN THE UPPER LONGERON AT THE HORIZONTAL STABILIZER FORWARD ATTACH POINT. THIS LOCATION CANNOT BE SEEN DURING NORMAL INSPECTION PROCEDURES. SB 300Feb 2, 1998 · N76PK · Rhnflu EXTRA300SDR 98ZZZX759Longeron · crackedDURING ROUTINE SERVICE WITH HORIZONTAL STABILIZER REMOVED, FOUND A CRACK IN THE UPPER LONGERON AT THE HORIZONTAL STABILZIER FORWARD ATTACH POINT. THIS LOCATION CANNOT BE SEEN DURING NORMAL INSPECTION PROCEDURES WITH HORIZONTAL STABILIZER INSTALLED. NO DEFECTFeb 2, 1998 · N328PW · Rhnflu EXTRA300SDR B4MR98009Stringer · corrodedDURING ACCOMPLISHMENT OF AD 92-12-03, FOUND STR 28L AT FS 950A HAS CORROSION FWD OF BEAM. REMOVED CORROSION IAW B727 SRM 51-10-1. ULTRASONIC THICKNESS CHECK, INTERGRANULAR CORROSION DETECTED REINSPECT U/T THICKNESS CK .116 NO FURTHER CORROSION NOTED. MADE Feb 1, 1998 · N521DB · Boeing 727243SDR B4MR98007Stringer · corrodedDURING ACCOMPLISHMENT OF AD 92-12-03, FOUND STR 28L AT FS 950A HAS CORROSION AFT OF BEAM. U/T THICKNESS CK .124 REMAINING AFTER CORROSION REMOVED. REMOVED CORROSION IAW B727 SRM 51-10-1. INSTALLED REPAIR STRAP WITH FILLER IAW B727 SB 727-53-179. NON-ROUTINFeb 1, 1998 · N521DB · Boeing 727243SDR 98FDEA00071Stringer · corrodedCORROSION (C53-224-01) ON STRINGER, BS 870 TO 950, STR 2 RT. *S/D* REPAIRED STRINGER 2 RT, BS 870 TO 950 PER FED-EX SRM 53-10-3.Jan 31, 1998 · N143FE · Boeing 72721CSDR UPS98825991Longeron · damgedINSPECTION TYPE:D/CK STA 340 L28L LONGERON IS DAMAGED AT Z FITTING. BLENDED OUT DAMAGED IAW UPS DC8 SRM 53 2 0. FABBED REPAIR STRAP IAW REO 04279 AND DC8 SRM 51 1 24. ALODINED AND PRIMED REPAIR AREA AND STRAP IAW DC8 SRM 51 1 8. INSTALLED REPAIR IAW REO 04Jan 30, 1998 · N703UP · Doug DC871FSDR UPS98825733Longeron · corrodedINSPECTION TYPE:D/CK, L33 LEFT STA 190 TO 390 REQUIRED REPLACEMENT. REMOVED LONGERON STA 190-390, DRILLED NEW LONGERON HALVES IAW DC8 SR M 51 1 24. INSTALLED LONGERON WITH HI-LOKS AND RIVET6S IAW DC8 SRM 5 1 1 20D AND 51 1 21.Jan 30, 1998 · N703UP · Doug DC871FSDR QXEA9800146Stringer · chafedFRAME 18075 AT STRINGER 58 IS CHAFED MORE THAN 50 PERCENT. BLENDED CHAFED AREA, FABRICATED AND INSTALLED REPAIR DOUBLER IAW EA 4-53-339.Jan 29, 1998 · N482US · Fokker F28MK4000
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