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 P5CA9800099Stringer · corrodedLEVEL 1 CORROSION AT FUSELAGE LEFT STRINGER 20 AT BS 1605. BLENDED AND TREATED PER SRM 51-10-01.Jan 21, 1998 · N856FT · Boeing 747132SDR SWAA980047Stringer · damagedDURING SCHEDULED D CHECK, FOUND STRINGER 24R WITH A HOLE AT BS 941. REPLACED DAMAGED SECTIONS PER BOEING SRM.Jan 20, 1998 · N63SW · Boeing 7372H4SDR SWAA980046Stringer · damagedDURING SCHEDULED D CHECK, FOUND STRINGER 24R DAMAGED AT BS 867-878. REPLACED DAMAGED SECTIONS PER BOEING SRM.Jan 20, 1998 · N63SW · Boeing 7372H4SDR SWAA980045Stringer · corrodedDURING SCHEDULED D CHECK, FOUND STRINGER 27L CORRODED AT BS 1004, AND AT S27R AT BS 1009. REPLACED DAMAGED SECTIONS PER BOEING SRM.Jan 20, 1998 · N63SW · Boeing 7372H4SDR AALA980185Stringer · corrodedTUL - STR 28L CORRODED INSIDE HAT SECTION STA 594 TO STA 596. REMOVED CORRODED SECTION OF STRINGER. INSTALLED STRINGER REPAIR PER SRM 53-10-3 PAGE 4B. TST: 54,792 HOURS. CYCLES: 33,779. (X)Jan 20, 1998 · N872AA · Boeing 727223SDR AALA980184Stringer · corrodedTUL - OUTBOARD FLANGE OF STR 29L HAS CORROSION. INSTALLED REPAIR PER ESO 11697 DATED 1-13-98. TST: 54,792. CYCLES: 33,779. (X)Jan 20, 1998 · N872AA · Boeing 727223SDR UPS98825633Longeron · crackedINSPECTION TYPE-C, LONGERON 24R FITTING AT FS 879 HAS CRACK. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D AND 53-2-0.Jan 19, 1998 · N750UP · Doug DC871FSDR UPS98825624Longeron · corrodedINSPECTION TYPE:C LONGERON 24L FITTING HAS HEAVY CORROSION F/S 940. REMOVED AND REPLACED FITTING IAW SRM 53-2-0.Jan 19, 1998 · N750UP · Doug DC871FSDR UPS98825621Longeron · crackedINSPECTION TYPE:C LONGERON 24L FITTING CRACKED AT F/S 960. REMOVED AND REPLACED FITTING IAW SRM 51-3-0 AND 53-2-0.Jan 19, 1998 · N750UP · Doug DC871FSDR UPS98825503Stringer · corrodedINSPECTION TYPE-B CK, CORROSION FOUND AT STR 30R BETWEEN STR 25 TO 35 DOME NUT ATTACH POINTS FOR EXTERNAL AIR COND DOOR GRND HOOK UP. EXPOSED STRINGER AREAS WITH CORROSION. BLENDED 5 AERAS OF CORROSION PERFORMED THICKNESS TEST PER QC THICKNESS TESTER CL304. Jan 19, 1998 · N707UP · Doug DC871FSDR MWEA98068Longeron · crackedLONGERON 4L WAS FOUND CRACKED AT FUSELAGE STATION 160 AND FUSELAGE STATION 200. REMOVED DAMAGED LONGERON, ORDERED NEW PART, INSTALLED NEW LONGERON IAW SRM 51-30-2.Jan 19, 1998 · N215ME · Doug DC932SDR MWEA98066Longeron · damagedTHE LONGERON AT FS 980 17L WAS FOUND WITH ELONGATED HOLES. REMOVED DAMAGED SECTION OF LONGERON, FABRICATED REPAIR SECTION IAW SRM 53-02 FIG 18, INSTALLED REPAIR SECTION IAW 51-30.Jan 19, 1998 · N215ME · Doug DC932SDR MWEA98033Longeron · damagedDURING D-CHECK, THE LONGERON 10 LEFT AT FS 965 HAS A DRILL STRIKE. REMOVED DAMAGED SECTION, FABRICATED REPAIR SECTIONS IAW SRM 53-02 FIG 18, INSTALLED REPAIR SECTIONS IAW SRM 51-30.Jan 19, 1998 · N215ME · Doug DC932SDR MWEA98032Longeron · crackedD-CHECK, LONGERON 2R AT FS 756 FOUND CRACKED. REMOVED DAMAGED SECTION OF LONGERON, FABRICATED REPAIR SEC IAW 53-02, INSTALLED REPAIR SECTIONS IAW SRM 51-30.Jan 19, 1998 · N215ME · Doug DC932SDR MWEA98031Longeron · crackedDURING D-CHECK, LONGERON 3R WAS FOUND CRACKED AT FS 756. REMOVED DAMAGED SECTION, FABRICATED REPAIR SEC IAW 53-02 FIG 18. INSTALLED REPAIR SEC IAW 51-30.Jan 19, 1998 · N215ME · Doug DC932SDR DL72S980147Stringer · corrodedSTRINGER 30 WAS CORRODED NEAR FS 990. THE STRINGER WILL BE CUT AT FS 990 AND A REPLACEMENT SECTION SPLICED IN. REPAIR PER ERA331185-14.Jan 19, 1998 · N403DA · Boeing 727232SDR AALA0175Stringer · corrodedTUL - CORROSION INSIDE STR 28R STA 990. BLENDED OUT CORROSION AND INSTALLED STRAP DOUBLER REPAIR PER ESO 11697 DATED 1-19-98. TST: 56,192 HOURS. CYCLES: 34,665. (X)Jan 19, 1998 · N864AA · Boeing 727223SDR UPS98225576Stringer · corrodedINSPECTION TYPE-D, CORROSION ON STRINGER 21R BS 735. STRINGER REPAIR CARRIED IAW SRM 53-10-3 FIG 1.Jan 18, 1998 · N943UP · Boeing 72722CSDR 9807906612Longeron · crackedDURING M-CHECK, FOUND CRACK ON STR 7L AT FS 1040 AND 1060. REPAIRED PER EA 66-156558.Jan 18, 1998 · N612US · Boeing 747251BSDR USAA980013Stringer · corrodedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 1 INCH AREA OF CORROSION AT STRINGER 21L, STATION 887 STRINGER. CORROSION TASK NR C 53-202-01. INSTALLED STRINGER SPLICE PER REPAIR DOCUMENT SRM 53-00-03. (M)Jan 17, 1998 · N387US · Boeing 7373B7SDR UPS98225619Stringer · crackedINSPECTION TYPE:D ON REMOVAL OF DAMAGE ON OUTER CHORD OF FRAME AT BS 880 RT STRINGER 15R, SUSPECT CRACK FOUND IN LOWER HOLE STRINGER. REPAIR CARRIED IAW SRM 53-10-3Jan 16, 1998 · N943UP · Boeing 72722CSDR ABXA9800024Longeron · crackedDURING C-CHECK, FOUND LONGERON 13R CRACKED AT STA 965. REPAIRED LONGERON IAW DC9 SRM 53-02.Jan 16, 1998 · N932AX · Doug DC933FSDR ABXA9800022Longeron · crackedDURING C-CHECK, FOUND LONGERON 16L CRACKED AT STA 965. REPAIRED LONGERON 16L IAW DC9 SRM 53-02.Jan 16, 1998 · N932AX · Doug DC933FSDR ABXA9800021Longeron · crackedDURING C-CHECK, FOUND LONGERON 4L CRACKED AT STA 160. REPAIRED LONGERON 4L IAW DC9 SRM 53-02.Jan 16, 1998 · N932AX · Doug DC933FSDR AALA980167Stringer · corrodedTUL - SKIN BULDGED AND FASTENER HEADS DISHED STA 480 STR 26R. INSTALLED DOUBLER REPAIR ON STR FORWARD AND AFT OF STA 480. TST: 56,192 HOURS. CYCLES: 34,665. (X)Jan 16, 1998 · N864AA · Boeing 727223SDR AALA980161Stringer · gougedTUL - STA 910 BOTTOM SIDE OF STR 18A LT BADLY GOUGED. INSTALLED STRAP PER ESO 11697 DATED 1-5-98. TST: 56,192 HOURS. CYCLES: 34,665. (X)Jan 16, 1998 · N864AA · Boeing 727223SDR AALA980154Stringer · corrodedTUL - STR 29L, CORROSION FOUND AT STA 1166. INSTALLED STRINGER SPLICE PER SRM 53-10-3, PAGE 4B. TST: 56,192 HOURS. CYCLES: 34,665. (X)Jan 16, 1998 · N864AA · Boeing 727223SDR AALA980153Stringer · corrodedTUL - SKIN BULGED AND FASTENER HEADS DISHED AT STA 1148 AND STR 26L. INSTALLED STRINGER SPLICE AT STR 26L AND STA 1148 PER SRM 53-10-3, PAGES 3-4B. TST: 56,192 HOURS. CYCLES: 34,665. (X)Jan 16, 1998 · N864AA · Boeing 727223SDR AALA980152Stringer · corrodedTUL - CORROSION AT FASTENER OUTBOARD FLANGE STR 28L STA 720F + 15 INCHES. REMOVED CORROSION AND REPAIRED PER ESO 11697 DATED 1-2-98. TST: 56,192 HOURS. CYCLES: 34,665. (X)Jan 16, 1998 · N864AA · Boeing 727223SDR AALA980151Stringer · corrodedTUL - CORROSION IN STR 28R STA 688 - STA 692. INSTALLED NEW SECTION OF STR AT HAT CHANNEL PER SRM 53-10-3 PAGES 1 AND 2, ESO 11647 DATED 1-8-98. TST: 56,192 HOURS. CYCLES: 34,665. (X)Jan 16, 1998 · N864AA · Boeing 727223SDR UPS98225495Stringer · crackedINSPECTION TYPE-SI, DISCOVERED END OF STR 15L TO BE CRACKED AT BS 720+5. AREA OF DAMAGE REMOVED AND STRINGER END REPAIRED PER SRM 53-10-3 AND SRM 51-30-2.Jan 14, 1998 · N214UP · Boeing 7272A1SDR CALA9800049Stringer · crackedINSPECTION FOUND A .5 INCH CRACK IN STRINGER 15L AND 15R AT STA 720B. THE CRACKED AREAS WERE CUT OUT, REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 51-10-2 AND 53-10-3, FIGURE 5.Jan 14, 1998 · N76752 · Boeing 727227SDR CALA9800048Stringer · crackedINSPECTION FOUND A .5 INCH CRACK IN END OF STRINGER 15L AT STA 720C. THE CRACKED AREA WAS CUT OUT, A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-2 AND 53-10-3, FIGURE 5.Jan 14, 1998 · N76752 · Boeing 727227SDR AALA980117Stringer · corrodedTUL - CORROSION ON UPPER OUTBOARD FLANGE STR 29L STA 950F TO STA 1000. REMOVED CORROSION AND INSTALLED REPAIR PER ESO 11697 DATED 1-2-90. TST: 54,792 HOURS. CYCLES: 33,779. (X)Jan 13, 1998 · N872AA · Boeing 727223SDR AALA980116Stringer · corrodedTUL - STA 680 STR 27R HAS CORROSION ON INBOARD AND OUTBOARD SIDES OF STRINGER. REPLACED STRINGER CAP, ALODINED, AND TREATED AFFECTED AREA PER SRM 51-10-2. (X)Jan 13, 1998 · N872AA · Boeing 727223SDR 98FDEA00444Longeron · crackedSTA-VCE: AFT FUSELAGE UPPER TAIL BODY AT STA Y 2092, FOUND 1 CRACK ON LONGERON NR 9 LT SIDE. (REF SRM VOL III, 53-17-01, PAGE 20 FIG 5 AND PAGE 1, FIG 1). REMOVED SHEAR CLIPS AND BRACKETS, CUT OUT SECTION OF CRACK. INSTALLED REPAIR LONGERON WITH SPLICES PEJan 13, 1998 · N365FE · Doug DC1010SDR 98FDEA00443Longeron · crackedN1088 STA-VCE: AFT FUSELAGE UPPER TAIL BODY AT STA Y 2092, FOUND 1 EA CRACK ON LONGERON NR 8, LT SIDE. (REF SRM VOL III, 53-17-01, PAGE 20, FIG 5 AND PAGE 1, FIG 1). REMOVED SHEAR CLIPS AND BRACKETS, CUT OUT SECTION OF CRACK. INSTALLED REPAIR LONGERON WITJan 13, 1998 · N365FE · Doug DC1010SDR 98FDEA00442Longeron · crackedN1087 STA-VCE: AFT FUSELAGE UPPER TAIL BODY AT STA Y 2092, FOUND 1 EA CRACK ON LONGERON NR 5 LT SIDE. (REF SRM VOL III, 53-17-01, PAGE 20, FIG 5 AND PAGE 1, FIG 1). REMOVED SHEAR CLIPS AND BRACKETS, CUT OUT SECTION OF CRACK. INSTALLED REPAIR LONGERON WITHJan 13, 1998 · N365FE · Doug DC1010SDR 98FDEA00441Longeron · crackedSTA-VCE: AFT FUSELAGE UPPER TAIL BODY AT STA Y 2092, FOUND 1 CRACK ON LONGERON NR 4 LT SIDE. (REF SRM VOL III, 53-17-01, PAGE 20, FIG 5 AND PAGE 1, FIG 1). REMOVED SHEAR CLIPS AND BRACKETS, CUT OUT SECTION OF CRACK. INSTALLED REPAIR LONGERON WITH SPLICES PJan 13, 1998 · N365FE · Doug DC1010SDR AALA980089Stringer · crackedTUL - LEFT FUSELAGE STR 24L CRACKED AND FUSELAGE SKIN DENTED FROM STA 475 TO STA 478. INSTALLED STRINGER REPAIR PER SRM 53-10-3. INSTALLED FUSELAGE SKIN DOUBLER PER SRM 53-30-3. TST: 46,539 HOURS. CYCLES: 24,289. (X)Jan 12, 1998 · N703AA · Boeing 727223SDR USAA980006Stringer · wornINT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND 1 INCH BY 1 INCH WORN AREA BS 1040 PLUG 4 S26L STRINGER. INSTALLED DOUBLER, REPAIRED PER SRM 53-00-03. (X)Jan 10, 1998 · N784AU · Boeing 7374B7SDR AALA980090Stringer · corrodedTUL - CORROSION FIRST STRINGER TO RIGHT OF BOTTOM CENTERLINE 58R BETWEEN FRAMES 61 AND 62. REMOVED AND REPLACED STR 58R FROM FRAMES 58 TO 62.5 PER SRM 51-72-10 AND SRM 53-10-14. TST: 26,550.31 HOURS. CYCLES: 10,536. (X)Jan 10, 1998 · N19059 · Airbus A300B4605RSDR USAA980010Stringer · corrodedROA - DURING CX-1 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 4 INCH CORROSION STRINGER 27L, BSL 967. REMOVED CORRODED STRINGER AND INSTALLED STRINGER SPLICE, REPAIRED PER SRM 53-10-3 FIG 1. (M)Jan 9, 1998 · N242US · Boeing 737201SDR AALA980059Stringer · corrodedTUL - CORROSION ON STR 27R STA 1030 - STA 1040 AND SKIN UNDER STRINGER. REMOVED CORROSION, REPAIRED PER SRM 53-30-3, FIG 3. TST: 67,236 HOURS. CYCLES: 44,034. (X)Jan 9, 1998 · N727AA · Boeing 727227SDR 98FDEA00453Longeron · damagedSTA-VCE LONGERON NR 45, BETWEEN STA 1521 AND 1541 PRESENTS A PUNCHING DAMAGE NEAR THE 4TH HOLE IN THE MIDDLE ROW. MAJOR REPAIR PERFORMED IAW EA 8-5315-38441.Jan 9, 1998 · N377FE · Doug DC1010SDR 9800005Longeron · crackedDURING C-CHECK, FOUND LONGERON 16R CRACKED AT STA 1041. REPAIRED LONGERON DC9 SRM 53-02.Jan 9, 1998 · N968AX · Doug DC941SDR 9800004Longeron · crackedDURING C-CHECK, FOUND LONGERON 17L CRACKED AT THE FRAME ATTACH BOLTS STA 1056. REPLACED LONGERON FROM STA 1036 TO 1072 DC9 SRM 53-02.Jan 9, 1998 · N968AX · Doug DC941SDR CALA9800010Longeron · corrodedINSPECTION FOUND LOWER LT DOOR JAMB LONGERON (INSIDE NR 1 A/C PACK COMPARTMENT) AT STA 562-595 CORRODED. A NEW LONGERON SECTION, REPAIR ANGLES, AND STRAPS WERE FABRICATED AND INSTALLED IAW ECRA 5310-03653.Jan 8, 1998 · N68046 · Doug DC1010SDR AALA990046Longeron · corrodedTUL - FOUND CORROSION ON LONGERON 51R BETWEEN STATION 1964 AND 1975. REMOVED CORROSION ON LONGER 51R PER SRM 51-21-01. REPLACED STRINGER 651R END CAP PER AARD 51-01-00-05. TREATED PAINTED AND PRIMED PER SRM 51-21-01 VOL 2. (M)Jan 8, 1998 · N144AA · Doug DC1030SDR UPS98825417Longeron · corrodedINSPECTION TYPE-D, LONGERON 36 AT FS 220 CORRODED BEYOND LIMITS. REMOVED AND REPLACED LONG IAW SRM 51-1-21 AND 51-1-20D.Jan 7, 1998 · N852UP · Doug DC873F
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