JASC 5300
Service difficulty reports · 8,205
Reports filed under 5300 · Fuselage Structure (General), 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 = '5300' 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.
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 = '5300' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR TSAA20230606078Unknown · unknownCA 1464/230 CORROSION AT RH REAR FUSELAGE SKIN AT STA 1016, S-4R~S-9R. ALL CORROSION REMOVED AT RH REAR FUSELAGE SKIN AT STA 1016, S-4R ~ S-9R. REMOVED 0.003" MATERIAL & REMAINING 0.059" IS WITHIN ALLOWABLE LIMIT. AREA CLEAN & PROTECTIVE I.A.W. B737-300 SRMSDR TSAA20230606077Unknown · unknownCA 1464/229 CORROSION AT RH REAR FUSELAGE SKIN AT STA 1088, S-3R~S-5R. ALL CORROSION REMOVED AT RH REAR FUSELAGE SKIN AT STA 1088, S-3R ~ S-5R. REMOVED 0.003" MATERIAL & REMAINING 0.060" WITHIN ALLOWABLE LIMIT. AREA CLEAN & PROTECTIVE I.AW. B737-300 SRM 51-SDR TSAA20230606068Unknown · unknownCA 1464/186 CORROSION AT FUSELAGE CROWN DOUBLER BETWEEN STA 500 AND STA 540, S-1R AND S-2R, 14 AREA (L:3.1",W:2.2")(L:1.4",W:1.4")(L:0.9",W:0.5")(L:0.5",W:0.4") (L:1.9",W:0.7")(L:2.3",W:1.4")(L:1.7",W:1")(L:1.3",W:0.6")(L:1.1",W:0.6")(L:0.4",W:0.3)(L:0.8",W:0.SDR TSAA20230606067Unknown · unknownCA 1464/185 CORROSION AT FUSELAGE CROWN SKIN STA727, BETWEEN S-3L AND S-3R, 5 AREA (L:0.7",W:0.5")(L:1.5",W:0.6")(L:5.7"W:0.8)(L:1",W:0.5")(L:0.8",W:0.7"). ALL CORROSION REMOVED AT FUSELAGE CROWN SKIN AT STA 727, BETWEEN S-3L AND S-3R (L:0.7", W:0.5") (L:1.5"SDR TSAA20230606066Unknown · unknownCA 1464/184 CORROSION AT FUSELAGE SKIN STA 947.5, BETWEEN S-2R AND S-3R (L:5.6",W:1.4"). ALL CORROSION REMOVED AT FUSELAGE SKIN AT STA 947.5, BETWEEN S-2R AND S-3R (L:5.6", W:1.4"). REMOVED MATERIAL 0.003" AND REMAINING 0.037" IS WITHIN ALLOWABLE LIMIT. ARESDR TSAA20230606053Unknown · unknownCA 1464/129 SURFACE CORROSION ON FUSELAGE EXTERIOR SKIN BS500B/S24R+2". ALL CORROSION REMOVED AT FUSELAGE EXTERIOR SKIN BS5008, S-24R+2". REMOVED 0.001" AND REMAINING 0.070" IS WITHIN ALLOWABLE LIMIT. AREA CLEAN AND PROTECTIVE IAW B737-300 SRM 51-10-2, 51-2SDR TSAA20230606052Unknown · unknownCA 1464/123 CORROSION AT APU INLET DOOR AT STA 1064, S-15R. CORROSION AT APU INLET DOOR AT STA 1064, S-15R, REPAIRED IAW AIR ASIA EL-737-230506. (ASAP INC. EO 5323-075)SDR TSAA20230606051Unknown · unknownCA 1464/122 CORROSION AT RH SIDE FUSELAGE AT STA 1071, S-20R. ALL CORROSION REMOVED AT RH FUSELAGE AT STA 1071, S-20R.. REMOVED 0.002" MATERIAL AND REMAINING 0.073" IS WITHIN ALLOWABLE LIMIT. AREA CLEAN AND PROTECTIVE IAW B737-300 SRM 51-10-2, 51-20-01 AND SDR TSAA20230606050Unknown · unknownCA 1464/121 CORROSION AT REPAIRED DOUBLER SKIN AT STA 1076, S-17AR. ALL CORROSION REMOVED AT REPAIRED DOUBLER SKIN AT STA 1076.5, S-17AR. REMOVED 0.003" MATERIAL AND REMAINING 0.053" IS WITHIN ALLOWABLE LIMIT. AREA CLEAN AND PROTECTIVE IAW 8737-300 SRM 51-1SDR TSAA20230606049Unknown · unknownCA 1464/119 CORROSION AT RH SIDE FUSELAGE AT STA 1115-1128, S-20R. ALL CORROSION REMOVED AT RH FUSELAGE AT STA 1115-1128, S-20R.
REMOVED 0.004" MATERIAL AND REMAINING 0.067" IS WITHIN ALLOWABLE LIMIT. AREA CLEAN AND PROTECTIVE IAW B737-300 SRM 51-10-2, 51SDR TSAA20230606048Unknown · unknownCA 1464/118 CORROSION AT RH SIDE FUSELAGE AT STA 1156, S-20R. CORROSION ON FUSELAGE SECTION 48 STRAP 65-45688-172 AT STA 1156, REPAIR IAW AIR ASIA EL-737-230507. (V1 AEROSPACE, LLC REPAIR INSTRUCTION R23-01859-001 R01)SDR TSAA20230606047Unknown · unknownCA 1464/117 LIGHT CORROSION AT RIVET AREA OF STRINGER AT STA 1040~1060, S-24L. ALL CORROSION REMOVED AT RIVET AREA OF STRINGER AT STA 1040~1060 S-24L. REMOVED 0.005" AND REMAINING 0.040" IS WITHIN ALLOWABLE LIMIT. AREA CLEAN AND PROTECTIVE IAW B737-300 SRM SDR TSAA20230606046Unknown · unknownCA 1464/116 LIGHT CORROSION AT ACCESS AND BLOWOUT DOOR CUTOUT AREA AT STA 1058, S-20L. ALL CORROSION REMOVED AT ACCESS AND BLOWOUT DOOR CUTOUT AREA AT STA 1058, S-20L. REMOVED 0.002" MATERIAL AND REMAINING 0.054" IS WITHIN ALLOWABLE LIMIT. AREA CLEAN AND PRSDR TSAA20230606045Unknown · unknownCA 1464/115 LIGHT CORROSION AT ACCESS AND BLOWOUT DOOR CUTOUT AREA AT STA 1064, S-23L. ALL CORROSION REMOVED AT ACCESS AND BLOWOUT DOOR CUTOUT AREA AT STA 1064,S-23L. REMOVED 0.002" MATERIAL AND REMAINING 0.054" IS WITHIN ALLOWABLE LIMIT. AREA CLEAN AND PROSDR TSAA20230606044Unknown · unknownCA 1464/114 DENT (1.0" X 0.5" IN AREA, MAX DEPTH=0.015") AT LH SIDE FUSELAGE EXTERNAL SKIN AT STA 1072, IN ABOVE S-22L 0.5" DENT (1.0" X 0.5" IN AREA, MAX DEPTH=0.015") AT LH FUSELAGE EXTERNAL SKIN AT STA 1072. ABOVE TO S-22L 0.5". CHECK WITHIN ALLOWABLE LIMSDR AALA202306079117Unknown · wornAIRCRAFT IN BASE MAINTENANCE: WING CENTER SECTION LOWER SUPPORT BEAM LOWER CHORD WORN AT THE ESC DOOR (192DR OUTBOARD FORWARD LATCH AREA AT BS 545 AND RBL 40.875 AT WL 155. REPAIRED SUPPORT BEAM LOWER CHORD PER SRM 57-10-13-2R REPAIR 3.SDR CALA2023060701774Unknown · unknownREPAIR TO L/H CREASE BEAM SHEAR WEB BS 847-867. ACCOMPLISHED) PLACED ON DIP TO " PERFORM INSPECTION OF THE LH ECRA 5311-03006 ON OR BEFORE THE AIRCRAFT REACHING 50,000 TOTAL CREASE BEAM WEB FROM BS 847-867 IN ACCORDANCE WITH PART 2 OF CYCLES". PREFORMED INTERISDR TSAA20230606033Unknown · unknownCA 1464/101 CORROSION AT FUSELAGE SKIN BETWEEN STA 685 AND STA 706, S-11R AND S-12R (L:3.5", W:1"). ALL CORROSION REMOVED AT FUSELAGE SKIN BETWEEN STA 685 AND STA 706, S-11R AND S-12R (L:3.5", W:1"). REMOVED 0.004" AND REMAINING 0.114" IS WITHIN ALLOWABLE LISDR TSAA20230606018Unknown · unknownCA 1464/50 CORROSION AT FUSELAGE SKIN STA 907, BETWEEN S-15L AND S-16L (L:10", W:0.5"). ALL CORROSION REMOVED AT FUSELAGE SKIN STA 907, BETWEEN S-15L & S-16L (L:10", W:0.5"). REMOVED 0.004" MATERIAL AND REMAINING 0.061" IS WITHIN ALLOWABLE LIMIT. AREA CLEANSDR TSAA20230606017Unknown · unknownCA 1464/49 CORROSION AT FUSELAGE SKIN STA 947.5, BETWEEN S-13L AND S-16L, 2 AREA (L:11", W:0.7")(L:5", W:1"). REMOVED MATERIAL AND REMAINING IS WITHIN ALLOWABLE LIMIT. AREA CLEAN AND PROTECTIVE IAW B737-300 SRM 51-10-2, 51-20-01 AND 53-00-01 ALLOWABLE DAMAGESDR TSAA20230606014Unknown · unknownCA 1464/22 FILIFORM CORROSION WERE FOUND ON FUSELAGE EXTERNAL SKIN AFT CARGO CUTOUT FWD EDGE AS MARK. ALL CORROSION REMOVED AT FUSELAGE EXTERNAL SKIN AFT CARGO CUTOUT FWD EDGE. REMOVED 0.001" MATERIAL AND REMAINING 0.035" IS WITHIN ALLOWABLE LIMIT. AREA CLESDR TSAA20230606013Unknown · unknownCA 1464/21 FILIFORM CORROSION WERE FOUND ON FUSELAGE EXTERNAL SKIN LH SIDE STRINGER 27 STATION 987, 900 TO 903. ALL CORROSION REMOVED AT FUSELAGE EXTERNAL SKIN S-27L STA 987, STA 900 TO STA 903. REMOVED MATERIAL AND REMAINING IS WITHIN ALLOWABLE LIMIT. AREASDR TSAA20230606012Unknown · unknownCA 1464/20 FILIFORM CORROSION WERE FOUND ON FUSELAGE EXTERNAL SKIN LH SIDE STRINGER 26 STATION 900 TO 905. ALL CORROSION REMOVED AT FUSELAGE EXTERNAL SKIN S-26L, STA 900 TO 905. REMOVED 0.002" MATERIAL AND REMAINING 0.061" IS WITHIN ALLOWABLE LIMIT. AREA CLSDR TSAA20230606011Unknown · unknownCA 1464/19 FILIFORM CORROSION WERE FOUND ON FUSELAGE EXTERNAL SKIN RH SIDE STRINGER 27 STATION 938 TO 951, 903 TO 907.
ALL CORROSION REMOVED AT FUSELAGE EXTERNAL SKIN AT S-27R STA 938 TO STA 951, STA 903 TO STA 907. REMOVED MATERIAL AND REMAINING IS WITHINSDR TSAA20230606010Unknown · unknownCA 1464/18 FILIFORM CORROSION WERE FOUND ON FUSELAGE EXTERNAL SKIN RH SIDE STRINGER 26 STATION 922, 926 TO 928, 938 TO 942, 954 TO 957, 982 TO 990. ALL CORROSION REMOVED AT FUSELAGE EXTERNAL SKIN AT S-26R STA 922, STA 926 TO STA 928, STA 938 TO STA 942, STA 9SDR TSAA20230606009Unknown · unknownCA 1464/17 FILIFORM CORROSION WERE FOUND ON FUSELAGE EXTERNAL SKIN LH SIDE STA 986 BETWEEN STRINGER 18 AND 19. ALL CORROSION REMOVED AT FUSELAGE EXTERNAL SKIN AT STA 986 BETWEEN S-18L AND S-19L. REMOVED MATERIAL 0.002" AND REMAINING 0.069" IS WITHIN ALLOWABLSDR TSAA20230606008Unknown · unknownCA 1464/16 FILIFORM CORROSION WERE FOUND ON FUSELAGE EXTERNAL SKIN LH SIDE STRINGER 25 STATION 827 TO 847, 881 TO 901. ALL CORROSION REMOVED AT FUSELAGE EXTERNAL SKIN AT S-25L STA 827 TO STA 847, STA 881 TO STA 901. REMOVED MATERIAL AND REMAINING IS WITHIN ASDR TSAA20230606007Unknown · unknownCA 1464/14 FILIFORM CORROSION WERE FOUND ON FUSELAGE EXTERNAL SKIN LH SIDE STRINGER 20 STATION 727D TO 727D+3, 747 TO 787, 825 TO 827, 868 TO 897 AND 986 TO 990. ALL CORROSION REMOVED AT FUSELAGE EXTERNAL SKIN AT S-20L STA 727D TO STA 727+3, STA 747 TO STA 78SDR TSAA20230606005Unknown · unknownCA 1464/10 FILIFORM CORROSION WERE FOUND ON FUSELAGE EXTERNAL SKIN RH SIDE STRINGER 17 STATION 747 TO 767, STRINGER 24 STATION 847 TO 854. ALL CORROSION REMOVED AT FUSELAGE EXTERNAL SKIN AT S-17R STA 747 TO STA 767, S-24R STA 847 TO STA 854. REMOVED MATERIALSDR TSAA20230606004Unknown · unknownCA 1464/8 FILIFORM CORROSION WERE FOUND ON FUSELAGE EXTERNAL SKIN RH SIDE STRINGER 25 STATION 868 TO 907, 947 TO 957, 990 TO 1006. ALL CORROSION REMOVED AT FUSELAGE EXTERNAL SKIN AT S-25R STA 868 TO STA 907, STA 947 TO STA 957, STA 990 TO 1006. REMOVED MATERSDR TSAA20230606003Unknown · unknownCA 1464/7 FILIFORM CORROSION WERE FOUND ON FUSELAGE EXTERNAL SKIN RH SIDE STRINGER 20 STATION 767 TO 787, 867 TO 897, 927 TO 929. ALL CORROSION REMOVED AT FUSELAGE EXTERNAL SKIN AT S-20R STA 767 TO STA 787, STA 867 TO STA 897, STA 927 TO STA 929. REMOVED MATSDR TSAA20230606002Unknown · unknownCA 1464/6 FILIFORM CORROSION WERE FOUND ON FUSELAGE EXTERNAL SKIN STATION 1016 BETWEEN LH SIDE STRINGER 17 TO 20 AND RH SIDE STRINGER 17-25. ALL CORROSION REMOVED AT FUSELAGE EXTERNAL SKIN AT STA 1016 BETWEEN S-17L TO S-20L AND S-17R TO S-25R. REMOVED 0.002" SDR TSAA20230606001Unknown · unknownCA 1464/5 FILIFORM CORROSION WERE FOUND ON FUSELAGE EXTERNAL SKIN STATION 907 BETWEEN LH SIDE STRINGER 17 AND RH SIDE STRINGER 17. ALL CORROSION REMOVED AT FUSELAGE EXTERNAL SKIN AT STA 907 BETWEEN LH SIDE S-17 AND RH SIDE S-17. REMOVED 0.001" MATERIAL AND RESDR AALA202307250836Fork · wornAIRCRAFT IN BASE MAINTENANCE: AFT AVIONICS COMPARTMENT RACK 80VU LOWER LEFT LATERAL FORK END WORN AT FR 24 AND S32L. REPLACED FORK END PER EA 345511.SDR AALA202307250620Fork · wornAIRCRAFT IN BASE MAINTENANCE: AFT AVIONICS COMPARTMENT RACK 80VU LOWER RIGHT LATERAL FORK END WORN AT FR 24 AND S32R. REPLACED FORK END PER EA 345511.SDR HNAA2023062600229Unknown · unknown00245 COMPLY WITH PERMANENT REPAIR AT LOCATION FR67 & STR21L WITHIN 1200 FLIGHTCYCLES OR THE NEXT HEAVY CHECK WHICHEVER COMES FIRST AS OF OCTOBER 12, 2022 PER SECTION 5 OF ETD 2022-145-031648 REV A AND SRM1142 53-31-01-RE FINAL ACTION. COMPLIED WITH PERMANENSDR SWIA20230613025Unknown · damagedDAMAGE FOUND ON PAX DOOR HINGE LUGS #1, 2, 12, 26 (DOOR SIDE) (C-CHECK RO 6/9/2023) PAX DOOR PINO HINGE LUG DOOR SIDE REPAIRED ORIGINAL MATERIAL IS 0.119" IAW DWG 601R318073 REV. E. LUG #1, 2, 12, 26 MATERIAL THICKNESS REMOVED IS 0.009" TOOL # TUC9237 ESDR CALA2023060701773Unknown · corrodedAFT WET AREA, POSSIBLE CORROSION ON FLOOR BEAM STA 986.5 RBL 44 (REF: AAR NR 99968634)SDR CALA2023060701772Unknown · corrodedAFT WET AREA, POSSIBLE CORROSION ON FLOOR BEAM STA 986.5 LBL 40 (REF: AAR NR 99968651) REPAIRED FLOOR BEAM AT STA. 986.5 LBL 40 AT AFT WET AREA IAW B737-700 SRM 51-10-02-0G, SRM 51-10-02-0G-0, SRM 53-70-51-1A-1, SRM 51-40-02, 51-20-01; SRM, SRM 51-40-05, B737-SDR CALA2023060701771Unknown · corrodedAFT WET AREA, POSSIBLE CORROSION ON FLOOR BEAM STA 947.5 RBL 51 (REF: AAR NR 99968640) REPAIRED FLOOR BEAM STA 947.5 RBL51 IAW B737 SRM 51-10-02, 53-70 -51-1A-1, 51-40-02, SOPM 20-20-02, BOEING SOPM 20-10-03, SRM 51- 20-01, 51-21-72-370-804 & B737 SRM 53-70-51SDR IPXA2023072129156Unknown · puncturedMAIN DECK POSITION 4 CENTER HAS A ONE INCH PUNCTURE IN FLOOR***SM12/LMX2*** INSTALLED NEW PANEL AND REINSTALLED LOCKS AND ROLLERS IAW AMM 53-01-01.SDR IPXA2023062693515Longeron · corrodedINSPECTION TYPE:3C*MAJOR REPAIR* CAC COMP. BILGE AREA LONGERON 46L HAS CORROSION AT STA Y=6-75.REPAIRED CORRODED LONGERON 46L SECTION AT THE CAC COMP. BILGE AREA AT STA Y=6-75 IAW SRM 53-00-05 FIG 201 REPAIR 1. (MAJOR)SDR DALA2023060604578Channel · corroded(LOG 2799798) CORROSION CHANNEL SIDEPLATE LOCATED BTW STA 492.4 TO STA 500A AND STR 26R AT FWD CARGO COMPARTMENT. REPLACED CHANNEL SIDEPLATE LOCATED BTW STA 492.4 TO STA 500A AND STR 26R AT FWD CARGO COMPARTMENT AS PER B737-90ER SRM 51-40-02AND SRM 51-10-02 ITSDR DALA2023060504480Unknown · unknownSHIP 3116 CRACK WASTE TANK PANEL 172AR AT LOWER FUSELAGE. CORRECTIVE ACTION: COMPLIED WITH ER/A 608339-14 REV. ORIGINAL. (2800365)SDR DALA2023060504467Unknown · unknownSHIP 3123 ELONGATED HOLES (4 E/A) ON SECTION CROSSBEAM LOC. AT FR67 AT LEVEL Y1292 AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED CROSSBEAM PER A319 SRM 51-42-11. (2799795)SDR HNAA2023062600228Unknown · unknown00238 LH AFT SIDE OF AIRCRAFT, JUST FWD OF THE APU WAS HIT BY A MANLIFT, PUTTING A HOLE IN THE AIRCRAFT SKIN, REPAIR REQUIRED. REPAIRED LH SIDE OF AIRCRAFT
IAW EMBRAER ETD2023-145-014130SDR AALA202306093519Doubler · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED INTERNAL STRUCTURE DOUBLER REPAIR AT FR 35 BETWEEN S 29R AND S30R. REPAIRED DOUBLER PER EA 268395CSDR TAMF20230607034Unknown · unknownDURING AIRCRAFT UNLOADING PROCEDURE THE AFT CARGO DOOR CUT OUT FRAME WAS HIT WITH A LOADER EQUIPMENT, (FRAME 59A BETWEEN STRINGERS 36RH & 40RH), (FRAME 65 BETWEEN STRINGERS 35RH & 38RH). IN ACCORDANCE WITH THE JOB INSTRUCTION CARD NUMBER JIC 332-53-01367 STRUCSDR DALA2023060604566Unknown · unknownMAIN CABIN BS 986.5 FLOOR BEAM UPPER SURFACE HAS AREAS OF CORROSION BETWEEN RBL 15 AND RBL 48. FABRICATED REPAIR PARTS REPAIR (1) STRAP FROM 7575T6 0.100" CLAD. INSTALLED REPAIR IAW B737 SRM 53-70-51-2R.SDR UIEA2023052500522Unknown · unknownPAX CABIN FWD ENTRY AREA WL 208.1 AT LBL 60, BETWEEN BS 332.1 AND BS 294.5 SIDE BEAM WITH CRACK.(<P>PERFORMED PERMANENT REPAIR ON LOWER MAIN SILL INNER CHORD FWD ENTRY AREA AT BWL 208.1, LBL 60 AT BS 303.9 DUE TO CRACK I/A/W COOPESA E.O #COO-EO-2023-17712-R00
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