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 ABXA9900744Longeron · crackedDURING C-CHECK, FOUND LONGERON 17 LEFT AT STATION 1041 CRACKED. REPLACED LONGERON SECTION IAW DC9 SRM 53-02.Oct 12, 1999 · N957AX · Doug DC941SDR UPS99230884Stringer · corrodedINSPECTION TYPE:SI, WHILE WORKING 997311 FOUND CORROSION ON STR 6 LT BS 1130 TO BS 1150. REPAIRED STR 6 LT AT BS 1130 TO BS 1150 PER SRM 53-10-3, 51-30-2.Oct 11, 1999 · N951UP · Boeing 72725CSDR SCNA99769Stringer · corrodedDURING HEAVY MAINTENANCE CHECK, FORWARD CARGO PIT FS 620, STR 27R HAD CORROSION OUT OF LIMITS ON I/B FLANGE AT PREVIOUS REPAIR. REMOVED CORROSION IAW B727 SRM 511006. FABRICATED STRINGER REPAIR FROM BAC 1498147 IAW B727 SRM 531003. TREATED AND PRIMED IAW B7Oct 10, 1999 · N294SC · Boeing 7272M7SDR UPS99830918Longeron · corrodedINSPECTION TYPE:C1 LONGERON 32R, FWD OF FS 1766 IS CORRODED OUT OF LIMITS UNDER THE SPLICE FITTING. CUT OUT DAMAGED SECTION OF THE LONGERON AND SPLICED IN A NEW SECTION IAW SRM 53-2-2 FIG 10.Oct 9, 1999 · N814UP · Doug DC873FSDR UPS99230924Stringer · corrodedINSPECTION TYPE:C, STRINGER CORRODED AT BS 480 STR 28L. STRINGER SPLICE SECTION REPAIRED IAW SRM 51-20-1 FIG 7.Oct 9, 1999 · N930UP · Boeing 72722CSDR UPS99230938Stringer · corrodedINSPECTION TYPE:SI, WHILE WORKING 997311 FOUND CORROSION ON STR 5 LT BS 1130 - BS 1148. CORROSION FOUND OUT OF LIMIT. CUT OUT DAMAGED AREA BS 1112 - 1165 STR 5 LT, FABRICATED REPAIR PARTS AND INSTALLED PER SRM 53-10-3 FIG 3.Oct 8, 1999 · N951UP · Boeing 72725CSDR TWAA9914103Longeron · crackedDURING CHECK-C, MAINT FOUND LONGERON 6R CRACKED .375 INCH AT STA 756. REPAIRED PER SRM 53-02, FIG 18.Oct 8, 1999 · N976Z · Doug DC931SDR TWAA9913905Longeron · crackedDURING CHECK-C MAINT, FOUND LONGERON 8L WAS CRACKED .375 INCHES AT STA 680. SPLICED NEW SECTION OF LONGERON USING SRM 53-02, FIG 18 FOR SPLICE.Oct 8, 1999 · N976Z · Doug DC931SDR DL733992236Stringer · crackedTHE LEFT STRINGER 18A WAS FOUND CRACKED AT FS 727. THE DAMAGE WAS FOUND AT MV AND REPAIRED PER ERA 333643-14.Oct 8, 1999 · N313WA · Boeing 737347SDR SWAA991674Stringer · corrodedDURING SCHEDULED D CHECK, FOUND STRINGER 27L CORRODED AT BS 937. REPAIRED STRINGER PER SRM.Oct 7, 1999 · Boeing 7372H4SDR DL76S992346Stringer · corrodedSTRINGER 39R WAS FOUND CORRODED BEYOND ALLOWABLE LIMITS AT STA 1540. A REPLACEMENT SECTION OF STRINGER WAS INSTALLED PER SRM 53-00-03-2-202.Oct 6, 1999 · N117DL · Boeing 767332SDR DL76S992343Stringer · corrodedSTRINGER 38L AT STATION 1540 WAS FOUND CORRODED BEYOND ALLOWABLE LIMITS. A REPLACEMENT SECTION OF STRINGER WAS INSTALLED PER SRM 53-00-03-2-202.Oct 6, 1999 · N117DL · Boeing 767332SDR DL76S992342Stringer · corrodedCORROSION WAS FOUND IN STRINGER 39L AT STATION 1540 AND WAS BEYOND ALLOWABLE LIMITS. A REPLACEMENT SECTION OF STRINGER WAS SPLICED IN PER SRM 53-00-03-2-202.Oct 6, 1999 · N117DL · Boeing 767332SDR RRXA003421Longeron · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE LONGERON END FITTINGS AT STA 70 L31R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 53-2-0.Oct 5, 1999 · N605AL · Doug DC873FSDR SWAA991664Stringer · crackedDURING SCHEDULED D CHECK, FOUND STRINGER 14R CRACKED AT BS 807. REPAIRED STRINGER PER SRM.Oct 5, 1999 · Boeing 7372H4SDR DL767992214Stringer · corrodedFUSELAGE STRINGER S-21AR, BS 1010, RBL 97.42, CORROSION REPAIR. STRINGER 21AR WAS FOUND WITH EXTENSIVE CORROSION AT FS 1010 AND RBL 97.42. THE STRINGER FORMS AN END CAP FOR THE MLG HORIZONTAL PRESSURE BULKHEAD. THE CORROSION WAS REMOVED WITH A 5 INCH CUTOOct 5, 1999 · N102DA · Boeing 767232SDR RRXA000259Longeron · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LONGERON 30 RIGHT AT STA 25, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW LONGERON IAW DC-8 SRM 53-2-0.Oct 4, 1999 · N605AL · Doug DC873FSDR 20000522AP007Longeron · corrodedFOUND DURING D-CHECK, UPPER FUSELAGE CABIN, CORROSION AT L30R STATION 25. REMOVED CORROSION, REMOVED LONGERON IAW DC-8 SRM 51-1-8, 53-2-0. FABRICATED LONGERON. TREATED, PRIMED AND INSTALLED IAW DC-8 SRM 53-2-2, 51-1-8, 51-1-21. (M)Oct 4, 1999 · N605AL · Doug DC873FSDR SWAA991661Stringer · corrodedDURING SCHEDULED A2 CHECK, FOUND CORROSION AT STRINGER 27R, BS 1010. REPAIRED STRINGER SECTION PER SRM.Oct 4, 1999 · Boeing 7372H4SDR MWEA99664Longeron · corrodedMODERATE CORROSION AT ATTACHMENT OF LONGERON 23 LEFT AND FUSELAGE FROM 180. MAINTENANCE FABRICATED AND INSTALLED NEW DOUBLER.Oct 4, 1999 · N302ME · Doug DC932SDR ABXA9900740Longeron · crackedDURING C-CHECK, FOUND LONGERON 17 LEFT CRACKED AT STATION 945. REPLACED LONGERON 17 LEFT AT STATION 945 IAW DC9 SRM 51-30-2.Oct 4, 1999 · N924AX · Doug DC931SDR AALA991508Stringer · corrodedTUL - STR 22L CORRODED FROM STA 1166 - STA 1183 AND STRINGER CLIPS AND END FITTING BELOW LAVATORY SERVICE PANEL. DESIGN LEAK. CUT OUT CORRODED PIECES OF STRINGER, REMOVED AND REPLACED STRINGER. INSTALLED SPLICE AND NEW END FITTING AND CLIPS PER SRM 53-10-3,Oct 2, 1999 · N720AA · Boeing 727227SDR UPS99230817Stringer · corrodedINSPECTION TYPE:C CORROSION STR 26R CORRODED BS 720F PLUS 16 740-4. REPAIRED STR 26R SRM 53-10-3, SPLICED IN NEW SECTION FROM BS 720F PLUS 5 TO BS 720F PLUS 16, AFTER BLENDING CORROSION OUT OF LIMITS.Sep 30, 1999 · N212UP · Boeing 727247SDR UPS99230816Stringer · corrodedINSPECTION TYPE:C CORROSION ON KEEL BEAM STRINGER 29L BS 950E PLUS 12 TO 950E PLUS 15 LBL 7 WL 138 (C53-113-01.06-02). REPAIRED PER ER NR 99-6148 AND 727 SRM.Sep 30, 1999 · N212UP · Boeing 727247SDR UIEA99086Stringer · misdrilledDURING ACCOMPLISHMENT OF SB 747-53A2390 FIG 19, DETAIL L, OVERSIZING HOLES AT STRINGER 39 LEFT AND RIGHT SIDES FROM .25 INCH BY .375 INCH WOULD CAUSE UNACCEPATABLE EDGE DISTANCE. PER TELEX TLS-AMS-99-00033H, PERFORMED HFEC OPEN HOLE INSPECTION, OVERSIZED HOLESep 29, 1999 · N526MC · Boeing 7472D7BSDR MWEA99624Longeron · crackedLONGERON 3R AND 4R IS CRACKED AT STATION 756. MAINTENANCE FABRICATED AND INSTALLED REPAIR SPLICE.Sep 29, 1999 · N204ME · Doug DC932SDR USAA991001Stringer · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 4.5 INCH CRACK BS 1138 TO STATION 1143 STRINGER 5R. INSTALLED REPAIR ANGLE PER EA 65627A. (M)Sep 27, 1999 · N342US · Boeing 737301SDR TWAA9914004Stringer · crackedDURING OP 16 MAINT CHECK FOUND CABIN STRINGER 4L CRACKED AT FORMER STA 200. REPLACED STRINGER FROM APPROX STA 230 TO 170. INSTALLED REPAIR SPLICE AT STA 170 PER SRM 53-02, FIG 18.Sep 27, 1999 · N979Z · Doug DC931SDR 99ZZZX3998Stringer · corrodedDURING A C-CHECK, CORROSION WAS NOTED ON STR 26R STA 1183.Sep 27, 1999 · N303FV · Boeing 727230SDR USAA991026Stringer · corrodedTPA - DURING A CX-4 CHECK VISUAL INSPECTION, FOUND A CORRODED AREA LOCATED UNDER STR 27R, STA 930, CORROSION LEVEL 1. REPLACED CORRODED AREA PER SRM 53-10-3 FIG 1. (X)Sep 25, 1999 · N237US · Boeing 737201SDR USAA991028Stringer · corrodedCLT - DURING A RON VISUAL INSPECTION FOUND CORROSION 9 INCHES BY 2 INCHES BY .075 INCH AT BS 500B PLUS 14 INCHES, STR 28R STRINGER (KEEL BEAM). CORROSION LEVEL 2. REMOVED CORROSION, INSTALLED KEEL BEAM REPAIR ANGLES AND SHIMS PER EA 65660. (X)Sep 24, 1999 · N225US · Boeing 737201SDR UPS99830857Longeron · crackedINSPECTION TYPE:C123 LONGERON 35R IS CRACKED AT FS 1050. CUT OUT DAMAGED AREA AND SPLICED LONGERON IAW DH SK718-251.Sep 24, 1999 · N718UP · Doug DC871FSDR MWEA99617Longeron · crackedLONGERON 23 AND 24 WAS CRACKED AT STATION 200 AND LONGERON 25 WAS CRACKED AT STATION 160. MTC FABRICATED AND INSTALLED LONGERONS.Sep 24, 1999 · N302ME · Doug DC932SDR DLL10992155Stringer · crackedTHE LBL 25.5 KEELSON STRINGER WAS FOUND WITH A 1.5 INCH LONG CRACK RUNNING FWD-AFT IN THE HORIZONTAL FLANGE AT FS 1357. THE STRINGER WAS CUT AT FS 1357 AND THE AFT END REMOVED. A NEW AFT SECTION WAS FABRICATED AND SPLICED IN PER ER/A 368337-14, REV A.Sep 24, 1999 · N720DA · Lkheed 10113851SDR CALA9901285Stringer · dentedINSPECTION FOUND STRINGER 5L DENTED AT STA 827 AND BETWEEN STA 842 AND 892. STRINGER REPAIRS WERE INSTALLED IAW SRM 53-00-03, FIGURE 201 AND 203.Sep 23, 1999 · N17356 · Boeing 7373T0SDR AT9900765Longeron · crackedFOUND LONGERONS 3 AND 4 AT BS 148-178 CRACKED. REMOVED CRACKED SECTIONS, TRIMMED TO FIT AND INSTALLED NEW SECTIONS OF LONGERONS 3 AND 4 WITH SPLICES IAW DC9 SRM 53-02 FIGURE 18.Sep 23, 1999 · N812AT · Doug DC932SDR 99FDEA00464Stringer · corrodedSTR 30 IS CORRODED BETWEEN BS 1148 AND 1166 IN AFT CARGO. REMOVED AND REPLACED STR 30 PER SRM 53-10-3.Sep 22, 1999 · N190FE · Boeing 72722SDR AALA991436Stringer · corrodedTUL - CORROSION ON STR 43L BETWEEN FRAMES 68-69. REPLACED STRINGER PER SRM 53-10-14. TST: 32,012.26. CYCLES: 12,872. (X)Sep 21, 1999 · N7055A · Airbus A300B4605RSDR HNAA9900129Stringer · corrodedSTRINGER 31S FROM X467 - X445 HAS CORROSION, MOSTLY AROUND RIVET HOLES. RIVETS CIRCLED IN RED NEED REMOVED FOR FURTHER EVALUATION. REMOVED RIVETS. SEVERAL AREAS OF CORROSION MEASURE FROM .003 - .012 DEEP. SPLICED STRINGER IAW RD8-53-1834.Sep 20, 1999 · N908HA · Dhav DHC8102SDR HNAA9900128Stringer · corrodedSTRINGER 31S FROM X488 - X467 HAS CORROSION AROUND RIVET HOLES. RIVETS CIRCLED IN RED NEED REMOVED AND CORROSION EVALUATED. REMOVED RIVETS. SEVERAL AREAS OF CORROSION MEASURES FROM .003 - .022 DEEP. SPLICED STRINGER 31S IAW RD8-53-1834.Sep 20, 1999 · N908HA · Dhav DHC8102SDR AALA991494Longeron · crackedTUL - FOUND LONGERON 4L CRACKED AT BELLFRAME 160. REPAIRED LONGERON PER SRM 53-02 PAGE 48 FIG 18. (M)Sep 20, 1999 · N246AA · Doug DC982SDR TWAA9912904Longeron · crackedFOUND A .1875 INCH CRACK AT LONGERON 6L STA 718. REPAIRED PER SRM 53-02, FIG 18. CHECK-C 7-14-98 STL.Sep 19, 1999 · N921L · Doug DC932SDR TWAA9912903Longeron · crackedFOUND A .25 INCH CRACK IN LONGERON 6L AT STA 658. REPAIRED PER SRM 53-02, FIG 18. CHECK-C 7-14-98 STL.Sep 19, 1999 · N921L · Doug DC932SDR AALA991416Stringer · corrodedTUL - STR 35R CORRODED AT FRAME 65. REMOVED AND REPLACED CORRODED STRINGER PER SRM 53-10-18. TST: 32,012.26 HOURS. CYCLES: 12,872. (X)Sep 17, 1999 · N7055A · Airbus A300B4605RSDR 2000ZZZX691Longeron · corrodedLONGERON 6R STA 1490 TO STA 1600, HAS AREAS OF EXFOLIATION. REMOVED CORROSION IAW DC-8 SRM 51-1-8. TREATED, PRIMED, AND REPAIRED PER DC-8 SRM 53-2-2 PAGES 59/60 PER EO 99-136 WITH APPROVED 8110-3 DATED 8-11-99. REF: ZANTOP INTERNATIONAL AIRLINES, INC., ZIASep 16, 1999 · N812TC · Doug DC8F55SDR 2000ZZZM210Longeron · corrodedLONGERON 6R STATION 1490 TO 1600 HAS AREAS OF EXFOLIATION. REMOVED CORROSION IAW DC-8 SRM 51-1-8. TREATED, PRIMED AND REPAIR PER DC-8 SRM 53-2-2 PAGE 59/60 PER EO NR 99-136 WITH APPROVED 8110-3 DATED 8/11/99. (M)Sep 16, 1999 · N812TC · Doug DC8F55SDR UPS99830847Longeron · corrodedINSPECTION TYPE:C123 LONGERON 31L BELOW THE FRAME AT FS 1340 IS CORRODED BEYOND LIMITS. CUT OUT THE DAMAGED LONGERON AND SPLICED IN A NEW SECTION OF LONGERON IAW DH SK718-829.Sep 15, 1999 · N718UP · Doug DC871FSDR UPS99830844Longeron · corrosionINSPECTION TYPE:C123 BATH TUB FITTING AND BEAM HAVE HEAVY CORROSION INSIDE WEB AT FS 330 TO 340, LONGERON 36. REMOVED AND REPLACED THE FITTING AND THE BEAM (LONGERON) IAW SRM 51-1-20D AND 53-2-0 FIG 1F.Sep 15, 1999 · N718UP · Doug DC871FSDR UPS99830796Longeron · crackedINSPECTION TYPE:C123, LONGERON 35L FS 215 - 220 WAS CRACKED BEYOND THE STOP DRILL AND CORROSION WAS FORMING INSIDE THE CRACK. CUT OUT THE DAMAGED LONGERON, FS 190 - 230 AND SPLICED IN A NEW SECTION OF LONGERON IAW SRM 53-2-2 FIG 10.Sep 15, 1999 · N718UP · Doug DC871FSDR TWAA9915903Longeron · crackedDURING OP 16 MAINT CHECK, FOUND LONGERON 4L WITH 2 INCH CRACK AT STA 160 AND 200. REPLACED LONGERON PER SPM 6-70-01, PAGE 2.Sep 15, 1999 · N983Z · Doug DC931
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