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 TWAA9812108Stringer · bentDUE TO A DAMAGE INCIDENT STR 37L WAS BENT AND TWISTED AND RIVETS POPPED. CENTER STRAP TWISTED BETWEEN STA 429 AND 456. REPAIRED PER 767 SRM 53-00-03, DETAIL III, AND ARA 11576.Jul 19, 1998 · N605TW · Boeing 767231SDR TWAA9812107Stringer · crackedDUE TO A DAMAGE INCIDENT STR 35L WAS CRACKED AT STA 456. REPAIRED PER 767 SRM 53-00-03, DETAIL III.Jul 19, 1998 · N605TW · Boeing 767231SDR TWAA9812106Stringer · crackedDUE TO A DAMAGE INCIDENT STR 36L WAS CRACKED AT STA 456. REPAIRED PER 767 SRM 53-00-03 DETAIL III.Jul 19, 1998 · N605TW · Boeing 767231SDR RRXA99203Longeron · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO LONGERON 28 RIGHT BETWEEN STA 1460 TO STA 1480, DAMAGED BEYOND LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW LONGERON SECTION IAW DC-8 53-2-2. (CORRJul 18, 1998 · N995CF · Doug DC862SDR AALA981413Stringer · corrodedTUL - FOUND STRINGER CLIP CORRODED. ALODINED, PRIMED AND PAINTED AREA PER SRM 51-75-10-2. INSTALLED NEW STRINGER END PER SRM 51-72-10-10 W/SPLICE PER SRM 53-10-14-2. (M)Jul 18, 1998 · N40064 · Airbus A300B4605RSDR TWAA9812208Stringer · corrodedDURING CHECK-C, FOUND FUSELAGE STRINGERS CORRODED AT FS 660 TO 680, S27L TO S27R. REMOVED 3 T ANGLE STIFFENERS, REMOVED CORROSION BY ABRASIVE SANDING AND RE-INSTALLED PER SRM 51-10-6, PG 5.Jul 17, 1998 · N54335 · Boeing 727231SDR HEEA0015194Channel · mismanufacturedCHANNEL NOT FORMED CORRECTLY.Jul 17, 1998 · Bell 206L1SDR CALA9801263Stringer · corrodedINSPECTION FOUND STRINGER/FRAME CORRODED AROUND FASTENERS AT KEEL BOX INTERIOR, STA 598, STRINGER 29R. THE KEEL BOX WEB WAS REMOVED. TWO REPAIR ANGLES WERE FABRICATED IAW SRM 53-01, FIGURE 2 AND 51-10-2A. THE ANGLES AND KEEL BOX PANEL WERE INSTALLED IAW SRM Jul 17, 1998 · N18544 · Doug DC932SDR AALA981407Stringer · corrodedTUL - FOUND STRINGER 48R CORRODED JUST FORWARD OF FRAME 66. REMOVED CORRODED PORTION OF STRINGER 48R AND REPAIRED AREA IAW 53-10-14-2. (M)Jul 17, 1998 · N40064 · Airbus A300B4605RSDR AALA981400Stringer · corrodedTUL - STR 27R CORRODED BETWEEN BS 620 - BS 626. REMOVED CORROSION PER 51-10-6 AND INSTALLED U-CHANNEL DOUBLER IN STR 27R FROM BS 620 - BS 626 PER ESO 11697 DATED 6-30-98. TST: 52,996 HOURS. CYCLES: 32,076. (X)Jul 17, 1998 · N882AA · Boeing 727223SDR 98FDEA00462Stringer · corrodedCORROSION (C53-224-02) ON STRINGER 9 LT, BS 380 TO 460. *S/D* REPAIRED STR 9 LT, BS 380 TO 480 PER FED-EX SRM 53-10-3.Jul 17, 1998 · N144FE · Boeing 72721CSDR 98FDEA00461Stringer · corrodedCORROSION (C53-224-02) ON STRINGER 1 BL 0 BS 560 TO 580, BS 520 TO 540. *S/D* REMOVED CORROSION FROM STR 1, FOUND IT TO BE OUT OF LIMITS. REPAIRED STR 1, BS 520 TO 540 IAW FED-EX SRM 53-10-3.Jul 17, 1998 · N144FE · Boeing 72721CSDR AALA981397Stringer · corrodedTUL - STRINGER 55L BETWEEN FRAMES 64 AND 65 HAS DEEP CORROSION. INSTALLED STRINGER REPAIR PER SRM 53-10-14. (M)Jul 16, 1998 · N40064 · Airbus A300B4605RSDR AALA981396Stringer · corrodedTUL - STRINGE R55L BETWEEN FRAMES 63 AND 64 HAS DEEP CORROSION. INSTALLED STRINGER REPAIR FROM FRAME 63 TO FRAME 65 PER SRM 53-10-14. (M)Jul 16, 1998 · N40064 · Airbus A300B4605RSDR AALA981394Stringer · corrodedTUL - FOUND STRINGER 51L BETWEEN FRAMES 65 AND 66 HAS DEEP CORROSION. REPAIRED STRINGER PER SRM 53-10-14-2. TREATED AND PAINTED PER SRM 51-21-01 AND INSTALLED NEW FASTENERS. (M)Jul 16, 1998 · N40064 · Airbus A300B4605RSDR TWAA9811909Longeron · corrodedDURING OP 16 MAINTENANCE CHECK, FOUND LONGERON 24L WITH INNER GRANULAR CORROSION ON ATTACH FITTING AT FWD SIDE OF FS 996. REMOVED CORROSION PER SRM 51-10-03, STEP 35, PAGE 21. ALODINED AND PRIMED PER TWA STD PROCEDURES. INSTALLED NEW ATTACH FITTING PER SRM Jul 15, 1998 · N995Z · Doug DC932SDR P2EA98138Stringer · crackedSJO - C-CHECK ITEM - FUSELAGE STRINGER 10L CRACKED AT BS 529.5. DEFECT SIZE L - 0.095 INCH. REPAIRED STRINGER 10L BETWEEN BS 278 AND BS 302 PER SRM 53-10-3 FIG 3 SHEET 4. SEE COOPESA W.O. L1-0616-2-204, VAM 100 NR 555. (X)Jul 14, 1998 · N204AU · Boeing 737247SDR DHL9872127DStringer · corrodedAT D-CHECK, SPOT OF CORROSION FROM STA 950D TO 950E AT STR 18L. REMOVED DAMAGED AREA, INSTALLED REPAIR PER SRM 53-10-3, 9 X 2.5. N/R 3249.Jul 14, 1998 · N721DH · Boeing 727228SDR DHL9872126DStringer · corrodedAT D-CHECK, SPOT OF CORROSION AT STRINGER 18L BETWEEN BS 950E AND 950F. CUT OUT DAMAGED SECTION OF STRINGER, INSTALLED REPAIR PER SRM 53-10-3 FROM 950E THROUGH 950F. N/R 3242.Jul 14, 1998 · N721DH · Boeing 727228SDR AALA981382Stringer · corrodedTUL - STRINGER 53R CORRODED BETWEEN FRAME 63 AND FRAME 64. REMOVED CORRODED SECTION OF STRINGER 53R AND SPLICE IN NEW SECTION IAW SRM 53-10-14-2. (M)Jul 14, 1998 · N40064 · Airbus A300B4605RSDR AALA981381Stringer · corrodedTUL - STRINGER 54L BETWEEN FRAMES 69 AND 70 HAS DEEP CORROSION. CUT OUT CORRODED AREA AND REPAIRED AS PER SRM 53-10-14-2. TREATED, PRIMED AND PAINTED AS PER SRM 51-21-10. (M)Jul 14, 1998 · N40064 · Airbus A300B4605RSDR 98ZZZX3077Stringer · corrodedDURING ANNUAL INSPECTION, FOUND CORROSION IN THE LEFT LOWER COWL SIDE RAIL FORWARD END. THE STRINGER HAD EXFOLIATION ON THE TOP OF THE STRINGER. REPLACED WITH NEW PART.Jul 14, 1998 · N104WD · Cessna P210NSDR UPS98227167Stringer · corrodedINSPECTION TYPE-SI, CORROSION (C53-221-01.00-01) ON STR 1 AT STA 291. REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1. REMOVED DAMAGED AREA OF STRINGER AND FABRICATED REPAIR PARTS IAW SRM 53-10-3 SRM 53-10-4.Jul 13, 1998 · N906UP · Boeing 72730CSDR TWAA9812010Longeron · crackedDURING OP 15 MAINT CHECK, FOUND LONGERON 17R CRACKED AT STA 965. REPLACED CRACKED LONGERON PER SRM 53-02, PG 48 TO 53. INSTALLED RIVETS COMMON TO SKIN AND LONGERON PER SRM 51-30, PG 1 AND 6. USED MS 20615-M-4 AND AN960B4 WASHERS.Jul 13, 1998 · N980Z · Doug DC931SDR TWAA9811903Longeron · crackedDURING OP 16 MAINTENANCE CHECK, FOUND LONGERON 29R CRACKED JUST FORWARD ON STATION 587 FRAME. REMOVED AND REPLACED LONGERON END PER DWG INST 592176 PER SRM 51-01 PAG 1 ITEM C. INSTALLED WITH NEW FASTENERS PER DOUGLAS INST DWG 592176 AND SRM 51-60-0. (M)Jul 13, 1998 · N995Z · Doug DC932SDR TWAA9811505Longeron · crackedDUIRNG OP 16 MAINTENANCE CHECK, FOUND LONGERON 17R AT STA 980 WITH .50 INCH CRACK AT ATTACH HOLE TO FORMER. REPLACED SECTION OF LONGERON FROM STA 956 TO STA 996. INSTALLED LONGERON REPAIR SPLICE PER SRM 53-02, FIGURE 18. CFT TT: 77,783 HOURS. ACFT TC: 84,Jul 13, 1998 · N998R · Doug DC932SDR SWAA981366Stringer · corrodedDURING SCHEDULED C4 CHECK, FOUND CORRODED AFT LOWER LOBE 5-27L, ON STRINGER FROM BS 967-1006. REPAIRED PER BOEING MM.Jul 13, 1998 · Boeing 7372H4SDR SWAA981359Stringer · gougedDURING SCHEDULED D CHECK, FOUND STRINGER GOUGED AT BS 295 STR 11 LT. REPAIRED PER BOEING SRM.Jul 13, 1998 · N336SW · Boeing 7373H4SDR CALA9801296Stringer · crackedINSPECTION FOUND A 1.5 INCH CRACK IN STRINGER 15L AT STA 720B. THE CRACKED AREA WAS CUT OUT IAW SRM 53-10-32. REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 53-10-3, 51-10-6, AND 53-10-3.Jul 12, 1998 · N17773 · Boeing 727227SDR CALA9801241Longeron · crackedINSPECTION FOUND LONGERON 16R CRACKED AT UPPER FLANGE AND LONGERON 16L CRACKED OUT OF UPPER AND LOWER ATTACH CLIP FASTENERS, STA 965. THE CRACKED AREAS OF LONGERONS WERE REMOVED IAW SRM 51-30-2. LONGERONS AND SPLICES WERE FABRICATED AND INSTALLED IAW SRM 53-Jul 11, 1998 · N18544 · Doug DC932SDR CALA9801240Longeron · crackedINSPECTION FOUND THREE CRACKS IN LONGERON 17R AT FRAME ATTACH HOLES FROM STA 945 TO 980. THE CRACKS WERE .5 TO 1 INCH LONG. THE CRACKED AREAS OF LONGERON WERE REMOVED IAW SRM 53-02, FIGURE 18. LONGERON REPAIRS WERE FABRICATED AND INSTALLED IAW SRM 53-02, FIJul 11, 1998 · N18544 · Doug DC932SDR TWAA9811905Longeron · crackedDURING OP 16 MAINTENANCE CHECK, FOUND LONGERON 30 CRACKED JUST FORWARD OF STA 578 FRAME. INSTALLED NEW LONGERON END PER INSTL DWG 592176 PER SRM 51-01, PG 1 ITEM C. INSTALLED WITH NEW FASTENERS PER SRM 51-60-0 AND INSTL DWG 592176. ACFT TT: 77,210 HOURS. AJul 10, 1998 · N995Z · Doug DC932SDR TWAA9811904Longeron · crackedDURING OP 16 MAINTENANCE CHECK, FOUND LONGERON 29L CRACKED JUST FORWARD OF STA 578 FRAME. REMOVED AND REPLACED LONGERON END PER INSTL DWG 592176 PER SRM 51-01, ITEM C. INSTALLED NEW STRINGER PER INSTL DWG 592176 AND SRM 51-60-0. ACFT TT: 77,210 HOURS. ACFJul 10, 1998 · N995Z · Doug DC932SDR MWEA98776Longeron · dentedFOUND DENT ON LONGERON 10L AT STATION 807. MAINTENANCE REPLACED LONGERON SECTION.Jul 10, 1998 · N601ME · Doug MD88SDR MWEA98774Longeron · dentedFOUND LONGERON 9L DENTED AT STATION 809. MAINTENANCE REPLACED LONGERON SECTION.Jul 10, 1998 · N601ME · Doug MD88SDR C2XA98IA251Stringer · corrodedIAH - DURING C-CHECK INSPECTION, FOUND STR 20 RIGHT BETWEEN FRAMES NR 15 AND NR 16 CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE STRINGER IAW ATR-42 SRM 51-25-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. TT: 17,852.4 HOURS. TC: 20,Jul 10, 1998 · N11835 · Aerosp ATR42320SDR RRXA99202Longeron · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO LONGERON 35 LEFT AT STA 980, DAMAGED BEYOND LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW LONGERON SECTION IAW DC-8 53-2-0 FIGURE 1F. (CORROSION DAMAJul 9, 1998 · N995CF · Doug DC862SDR SWAA981326Stringer · crackedDURING SCHEDULED D-CHECK, FOUND CRACKED STRINGER CLIP AT BS 380, STR 21L, WL 174. REPAIRED PER BOEING SRM.Jul 8, 1998 · N336SW · Boeing 7373H4SDR RRXA99225Longeron · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO LONGERON 24 RIGHT AT STA 880, DAMAGED BEYOND LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW LONGERON SECTION IAW DC-8 53-2-2 FIGURE 10. (CORROSION DAJul 8, 1998 · N995CF · Doug DC862SDR TWAA9811008Longeron · crackedMCI - DURING OP 15 MAINTENANCE CHECK, FOUND LEFT FLANGE OF LONGERON 4L CRACKED AT ATTACHMENT TO FORMER AT FS 200. REPLACED LONGERON PER SRM 53-02, PG 48 TO PG 53. REPLACED FASTENERS COMMON TO SKIN USING NAS 1097 AD-6. ACFT TT: 69,860 HOURS. ACFT TC: 81,1Jul 7, 1998 · N980Z · Doug DC931SDR TWAA9811007Longeron · crackedMCI - DURING OP 15 MAINTENANCE CHECK, FOUND LONGERON 4L WITH CRACKED FLANGES AT STA 160. REPLACED LONGERON PER SRM 53-02, PG 48 TO PG 53. REPLACED FASTENERS COMMON TO SKIN USING NAS 1097-6. ACFT TT: 69,860 HOURS. ACFT TC: 81,151. (X)Jul 7, 1998 · N980Z · Doug DC931SDR TWAA9811006Longeron · crackedMCI - DURING OP 15 MAINTENANCE CHECK, FOUND LONGERON 4L CRACKED AT FS 200. REPLACED LONGERON PER SRM 53-02, PG 48 TO PG 53. REPLACED FASTENERS COMMON TO SKIN AND LONGERON WITH NAS 1097-6. ACFT TT: 69,860 HOURS. ACFT TC: 81,151. (X)Jul 7, 1998 · N980Z · Doug DC931SDR SWAA981290Stringer · crackedDURING SCHEDULED D-CHECK, FOUND CRACKED STRINGER AT BS 297 WL 256 LBL 54. REPAIRED PER BOEING SRM.Jul 7, 1998 · N336SW · Boeing 7373H4SDR ABXA9800611Longeron · crackedWHILE COMPLYING WITH C-CHECK, FOUND LONGERON 17 RIGHT CRACKED AT FUSELAGE STATION 786. REPLACED LONGERON 17 RIGHT SECTION AT STATION 786 IAW DC9 SRM.Jul 7, 1998 · N927AX · Doug DC915SDR SWAA981272Stringer · crackedDURING SCHEDULED D-CHECK, FOUND CRACKED STRINGER 4R AT BS 907 STRINGER SERVICE AND 4L AT BS 907 STRINGER SPLICE. REMOVED AND REPLACED PER BOEING SRM.Jul 6, 1998 · N336SW · Boeing 7373H4SDR UPS98227136Stringer · corrodedINSPECTION TYPE:SI CORROSION (C53-111-01.00-01) ON STR 21R BS 312. REPLACED STRINGER CHANNEL FROM BS 292 TO 315 IAW SRM 51-10-7, 53-10-1 AND 53-10-3.Jul 3, 1998 · N906UP · Boeing 72730CSDR UPS98227131Stringer · corrodedINSPECTION TYPE:SI CORROSION (C53-111-01.00-02) ON STR 22R BS 480-500. REPLACED 22R STR CHANNEL BS 480 TO 500 PER 727 SRM 53-10-3.Jul 3, 1998 · N906UP · Boeing 72730CSDR RRXA99204Longeron · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO LONGERON 26 LEFT BETWEEN STA 1440 TO STA 1480, DAMAGED BEYOND LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW LONGERON SECTION IAW DC-8 53-2-2. (CORROJul 3, 1998 · N995CF · Doug DC862SDR AALA981324Stringer · corrodedTUL - FOUND CORROSION ON STRINGER 27R OUTBOARD LEG (VERTICAL) AT STATION 620. INSTALLED STRINGER REPAIR PER SRM 53-10-3 PGS 4C-4E. REMOVED CORROSION PER SRM 51-10-6, TREATED AND PRIMED AREA. (M)Jul 3, 1998 · N719AA · Boeing 727227SDR AALA981311Stringer · crackedTUL - STRINGER CRACKED 15L STA 720B FORWARD OF ICE LIGHT HOUSING AT END OF STRINGER. REPAIRED STR 15L FORWARD OF ICE LIGHT STA 720B PER SRM 53-10-3. TST: 70,062 HOURS. CYCLES: 49,889. (X)Jul 3, 1998 · N719AA · Boeing 727227
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