JASC 5330
Service difficulty reports · 79,329
Reports filed under 5330 · Fuselage Main, Plate/Skin, 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 = '5330' 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 = '5330' 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 DALA2024122712028Skin · corrodedSHIP 3145 CORROSION ACCESS DOOR 316AR EXTERNAL SKIN LOWER DRAIN AREA IN APU COMPARTMENT. CORRECTIVE ACTION: PERFORMED REPAIR IN ACCESS DOOR 316AR EXTERNAL SKIN LOWER DRAIN AREA IN APU COMPARTMENT AS PER A319 SRM 52-41-22-300-003SDR JR2R2024122600151Skin · corrodedFWD CARGO DOOR AREA BEHIND PROTECTOR PLATE HAS MULTIPLE SCREW HOLES CORRODED.SDR CALA2025012100159Skin · crackedCREASE ACROSS AFT UNDERS IDE OF FUSELAGE. COMPLETED DAMAGE MAP FOR 8 EA DENTS FR 62-64 BETWEEN STR 41LH-43RH SENT TO ENG FOR SUPPORT LOCKING LOG FOR MX FERRY FOR REPAIR AT GSO PICS ADDED MEASURED GOUGE DEPTH IN DENT #1. MATERIAL LOSS IS 0.017 , PERFORMEDSDR SWAA2025013087166Skin · out of limitsSECTION 46 FUSELAGE SKIN HAS A BLEND AT BS 787+4 AND 5' BELOW STR 24R WITHIN 10 INCHES OF AFT CARGO DOOR CUTOUT<[01] REPAIRED PER EA 24-153-03589;[02] VERIFIED CORRECTIVE ACTION COMPLETED.SDR DALA2024122612004Bear Strap · crackedSHIP 670 DURING SCHEDULED EC INSP, FOUND CRACK IN BEARSTRAP OF UPPER FWD CORNER OF L1 DOOR (MKD) FAILED HFEC. CORRECTIVE ACTION: INSTALLED REPAIR AT THE UPPER FWD CORNER OF L1 DOOR, FUSELAGE SKIN PER AMDS WORK CARD 5331-01232-02G AND ERA 623065-14AD, REV ORIG.SDR CALA2024122601660Skin · damagedMULTIPLE BIRD STRIKE ON TO. ACCOMPLISHED BIRD STRIKE INSPECTION PER AMM 05-51-14 FOUND 1 STRIKE BELOW RADOME NO DAMAGE, ONE STRIKE TO ENG 1 INLET LIP NO DAMAGE AND ONE STIKE TO ENG 1 SPINNER NO DAMAGE AND NO BIRD REMAINS DOWN CORE OK TO CONTINUE ACCOMPLISHESDR ASAA2024122454802Skin Panel · corrodedPOSSIBLE CORROSION ON FASTNER HEADS AT STA967 BETWEEN STR23R AND STR26R. SRXR430X. GROUNDED - YES. ACCOMPLISHED CATEGORY "A" MINOR REPAIR TO FUSELAGE SKIN PANEL PN 147A3400-4 BETWEEN STA 947.50 AND STA 986.50 AND BETWEEN STGR S-23R AND STGR S-26R IAW EA800-53ESDR ASAA2024122454801Skin · corrodedJUST BELOW STR23L LAP JOINT AT STA927 STR25L SRXR430X. GROUNDED - YES. ACCOMPLISHED CATEGORY "A" MINOR REPAIR ON FUSELAGE SKIN PN 147A3400-4 AT STA 927 BTW STGR23L AND STGR25L IAW EA 800-53EA-28015 REV00 SRXR430X.SDR ASAA2024122454800Skin Panel · corrodedPOSSIBLE CORROSION AT STR 10L FROM STA 727A TO STA 727B. SRXR430X. GROUNDED - YES. ACCOMPLISHED CATEGORY "A" MINOR REPAI TO FUELAGE SKIN PANEL 146A3151-93 AT STA 727A TO 727B STGR 10L IAW EA 800-53EA-28017 REV00. SRXR430X.SDR VNAA202412240050Skin · corrodedHN00185013 DISCREPANCY: 1EA RIVET HOLE FOUND TO BE CORRODED ON THE LOWER FUSELAGE SKIN BETWEEN F.S.349.00 -F.S.364.00 AND STGR26L-STGR27. CORRECTIVE ACTION: REPAIRED IAW MHIRJ REO 670-53-21-2458 REV-- DATED 2024-10-09 SH690-31351-3SDR VNAA202412240022Skin Panel · corrodedHN00182365 DISCREPANCY: THE EXTERNAL SIDE OF THE FUSELAGE SKIN IS CORRODED BETWEEN FS 977 AND FS 1015.00 AT STGR 23L TO 21R. CORRECTIVE ACTION: COMPLIED WITH REO 670-53-00-753 REV-- DATED 10-15-24SDR SWIA202502241223Skin · damagedRAMP DAMAGE AT APPROXIMATELY FS 220 TO FS 250 IN BETWEEN STRINGER 13 THRU STRINGER 16 (FILED CLOSED) REMOVED AND REPLACED LH FUSELAGE SKIN BETWEEN FS202-FS280 AND STGR11L-STGR17L IN REF TO CRJ 900 SRM 51-42-06, 51-42-21 AND 51-42-22. PERFORMED SKIN WAVINSDR WX0A2025010332255Skin · damaged(AIRCRAFT GROUNDED) (DISCREPANCY NOTED DURING AIRCRAFT HEAVY MX VISIT) S/M ( I042-4) LOWER FUSELAGE, BTW FR3 I - FR32 AT STGR 37R, LIGHTNING STRIKE FOUND / LOWER FUSELAGE EXTERNAL SKFN BTW FR 31-32 AT STGR 37R FOUND OUT OF LIMITS AS PER SRM 53-21 -11 -283-018 SDR ASAA2024122354724Skin Panel · corrodedPOSSIBLE CORROSION AT STR10L AT STA727C. GROUNDED - YES. ACCOMPLISHED CATEGORY A MINOR REPAIR TO FUSELAGE SKIN PANEL 146A3151-93 AT STA727B-727C STR9R 10L IAW EA 800-53EA-28016 REV00.SDR DALA2024122411971Skin · dentedSHIP 3145 DENT WAS FOUND IN EXTERNAL FUSELAGE SKIN BETWEEN FR64-65 AND AT STR 44. CORRECTIVE ACTION: REPAIRED PER ER/A 623131-14. (0725716)SDR DALA2024122311923Skin · dentedSHIP 3308 LOWER HALF FUSELAGE AT FR66 STRG55R FOUND DENT. CORRECTIVE ACTION: APPLIED DOUBLER REPAIR AS PER A330 SRM 53-41-11. (0724657)SDR CALA2025022600446Skin · corroded(B737-53-3-0717) STA 540 BL-0 IN THE MIX BAY, THE SKIN HAS EXFOL IATION AT THE SKIN AND FRAME. TRANSCRIBED FROM HAECO GSO NR 9289 015. REPAIRED FUSELAGE SKIN AT STA 540 BL-0 PER ECRA 5351-03150 AND HAECO GSO REO - G25352 REV IR. REF DIP LOG PAGES 3956169 AND 3SDR ASAA2024122154795Skin Panel · corrodedPOSSIBLE CORROSION ON FASTENER HEADS AT STA 907 BETWEEN STGR 23R TO STGR 25R SRXR430X. GROUNDED - YES. ACCOMPLISHED CATEGORY A MINOR REPAIR TO FUSELAGE SKIN P/N 147A3400-4 AT STA 907 BETWEEN STGRE 23R AND STGR 25R IAW EA 800-53EA-28010 REV 00 SRXR430X.SDR ASAA2024122154793Skin Panel · corrodedPOSSIBLE CORRSION ON FASTENER HEADS BETWEEN STA 90 T0 STA 947. AT STGR 27R SRXR430X. GROUNDED - YES. ACCOMPLISHED ATEGORY A MINOR REPAIR TO FUSELAGE SKIN P/N 147A34000-4 AT STA 907 TO STA 975 IAW EA 8000-53EA-27988 REV 00 SRXR430X.SDR ASAA2024122154791Skin · corrodedPOSSIBLE CORROSION ON FASTENER HEADS AT 12IN AFT OF STA 905 STGR 27L SRXR4430X. GROUNDED - YES. ACCOMPLISHED CATEGORY A MINOR REPAIR TO FUSELAGE SKIN PANEL P/N 147A3400-4 AT STA 887 TO STA 907 AT STGR 27L IAW EA 800-53EA-27989 REV 00 SRXR430X.SDR GTIA2024122338618Access Panel · crackedACCESS PNL 197KB CRACKED RAF-01 3415092-02 -REPAIRED ACCESS PANEL 197KB ON LOWER FUSELAGE AS PER EC #EA5345-24134 AEROMAN EA #53-9066-24 REV.0 PART 1 AND RDAF 81508571/002/2024 HA PERMANENT REPAIR IS CATEGORY "A"SDR DALA2024122311916Skin · chafedSHIP 3147 CHAFING EXTERNAL SKIN AT FRAME 34 BTW STR 43 LH AND RH AT LOWER FUSELAGE. CORRECTIVE ACTION: AS PER TOPP 50-30-15 THE BLOCKS WAS FILLED OUT CORRECTLY ON ORNRC.EVALUATED REWORKED ON EXTERNAL SKIN LOC.FR34 AND STR43LH LOWER FUSELAGE AND FOUND WITHIN LISDR CALA2024122303150Skin · damagedDOUBLER PREVENTATIVE MODIFICATION TO THE L1 DOOR SURROUND FWD U PPER CORNER WAS INSTALLED PER EA 5330-04213 REV D WITH DEVIATION S NOTED IN EC/RA #: 5330-07407. ACCOMPLISH INSPECTION REQUIREMEN TS PER PART 2 OF EC/RA #: 5330-07407 AT FUSELAGE REINFORCED AREA (SDR SWIA20250311220Skin · damagedOVERSIZED COUNTER-SINK LOCATED ON SKIN PANEL OF FS 202.75 BETWEEN STGR 15L AND STGR 16L REQUIRES REPAIR (FILED CLOSED) COMPLIED WITH ALL STEPS IN REO 601R-53-11-3966 REV-- DATED 2025-01-14. PERFORMED PERMANENT REPAIR TO THE FUSELAGE SKIN AND DOUBLER AT FSDR AALA202502204417Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON SKIN PANEL OUTER SURFACE BETWEEN FR 56 AND FR 57, BETWEEN S42L AND S43L. REPAIRED SKIN PANEL PER EA 361430.SDR SWIA20250110220Skin · damagedOVERSIZED COUNTER-SINK LOCATED ON SKIN PANEL OF FS 202.75 BETWEEN STGR 15L AND STGR 16L REQUIRES REPAIR (FILED OPEN) THIS IS CURRENTLY A WORK IN PROGRESSSDR DALA2024122311964Skin · damagedFUSELAGE DAMAGE AFT OF L1 DOOR. REPAIRED A/C PER ER/A 542469-14 REV A. REF 001-0002:0514-2000 NRC 6 FOR DOCUMENTATION OF WORK PERFORMED. (LP #6956730)SDR DALA2024122311962Skin · ground damageAIRCRAFT SUSTAINED DAMAGE FROM JETWAY CONTACT AT LH FRAME STATION BS 237 BETWEEN STR 18L AND STR 17LH. SUMMARY NRC 001-0002:0514-2001/006 00006: COMPLIED WITH ER/A 542469-14 REV A. ENSURED PRI 542469-14 REV 0 MATCHES FINAL ERA. (LP #0719406)SDR ASAA2024122054719Skin · corrodedPOSSIBLE CORROSION ON EXTERNAL FASTENERS ON WATER SERVICE HOUSING GROUNDED - YES. ACCOMPLISHED CATEGORY A MINOR REPAIR TO FUSELAGE SKIN P/N 147A3400-4 AT WATER SERVICE HOUSING FASTENERS AT WATER SERVICE CUTOUT AT STA 907-927 STGR 2R TO STGR 27R IAW EA 800-53ESDR YENA2024122601631Skin · corrodedDURING HEAVY MAINTENANCE: CORROSION FOUND ON UPPER SKIN OF FWD CARGO DOOR SURROUND STRUCTURE ANROUND SCUFF PLATE HOLES; (RESOLVED ON W/O: 1335461 TASKCARD: NR-00012) REF AVIANOR WO 102-J3 NR 3083 CORROSION REPAIRED ON UPPER SKIN OF FWD CARGO COMPARTMENT DOOR SSDR YENA2024122601630Skin · corrodedDURING HEAVY MAINTENANCE: CORROSION FOUND ON UPPER SKIN OF AFT CARGO COMPARTMENT DOOR SURROUND STRUCTURE AROUND SCUFF PLATE HOLES; (RESOLVED ON W/O: 1335461 TASKCARD: NR-00013) REF AVIANOR WO 102-J3 NR 3021 CORROSION REPAIRED IAW EC AC24-1428-01 AND REO 500-53SDR YENA2024122601629Skin · corrodedDURING HEAVY MAINTENANCE: CORROSION FOUND ON LWR SKIN OF AFT PASSENGER DOOR SURROUND STRUCTURE AROUND SCUFF PLATE HOLES; (RESOLVED ON W/O: 1335461 TASKCARD: NR-00014) REF AVIANOR WO 102-J3 NR 3023 CORROSION REPAIRED IAW EC AC24-1399-01 AND REO 500-53-61-1544 TSDR YENA2024122601627Skin · corrodedDURING HEAVY MAINTENANCE: CORROSION FOUND ON LOWER SKIN OF AFT CARGO COMPARTMENT SURROUND STRUCTURE AROUND SCUFF PLATE HOLES; (RESOLVED ON W/O: 1335461 TASKCARD: NR-00016) REF AVIANOR WO 102-J3 NR 3019 CORROSION REPAIRED IAW EC AC24-1401-01 AND REO 500-53-61-1SDR YENA2024122601626Skin · corrodedDURING HEAVY MAINTENANCE: FUSELAGE SKIN AT WASTE ACCESS DOOR CUTOUT FOUND WITH CORROSION ON FWD EDGE; REF AVIANOR WO 102-J3 NR 3033 CORROSION REPAIRED IAW EC AC24-1450-01 AND REO 500-53-61-1545 TEMP REPAIR. DVI IAW ANDTP BD500-A-J51-00-90-01AAA-018A-A AT INTERSDR YENA2024122601615Skin · corrodedDURING HEAVY MAINTENANCE: LOWER FUSELAGE SKIN FOUND WITH CORROSION AROUND FASTENER AT FR78 AND STRG 35L; REF AVIANOR WO 102J-3 NR 3046 CORROSION REPAIRED IAW EC AC24-1500-01 AND REO 500-53-61-1553.SDR YENA2024122601606Doubler · corrodedDURING HEAVY MAINTENANCE: FUSELAGE WASTE ACCESS SURROUNDING CUTOUT FOUND WITH CORROSION AT AFT EDGE INTERNAL DOUBLER; REF AVIANOR PROJ 102J-3, NR 3032, AC24-1431-01 ASSIGNED TO ACCOMPLISH REPAIR PER AIB REO500-53-61-1557 INTELLIFORM UPDATED.SDR YENA2024122601605Skin · dentedDURING HEAVY MAINTENANCE: FUSELAGE / NOSE FUSELAGE / SKIN PANEL / LOWER LH INTERCOSTAL FR 13-15 / DENT DAMAGE - PERMANENT REPAIR; REF AVIANOR PROJ 102J-3, NR 3065, AC24-929-03 ASSIGNED TO ACCOMPLISH REPAIR PER AIB REO500-53-11-272. INTELL-IFORM UPDATED.SDR YENA2024122601593Skin · dentedDURING HEAVY MAINTENANCE: FUSELAGE / LHS FWD FUSELAGE / SKIN AT FR24-26 BETWEEN STR 23L-24L / DENT DAMAGE - PERMANENT REPAIR; REFERENCES: /1/ DAMAGE REPORT 102L-3 – 3065 /2/ REO 500-53-21-911 /3/ REO 500-53-21-1011. AT THE CURRENT C CHECK FOR N3102J AT YMX, MSDR DALA2024122311946Skin · ground damage(LOG 0718954) WHILE ON THE LINE IN UVF, A BELT LOADER STRUCK THE FUSELAGE BELOW THE AFT CARGO DOOR. AFTER PAINT REMOVAL AND BLENDING, THE FOLLOWING DAMAGES WERE FOUND TO BE OUTSIDE OF SRM ALLOWABLE LIMITS: GOUGE #1: 3.2 FWD/AFT, 2.3 L/R, MAX DEPTH OF 0.037;SDR DALA2024122311945Skin · gouged(LOG 0718950) SKIN GOUGED 3 PLACES BETWEEN STA 794.3 TO STA 807 27L AND 27 RT OUT OF LIMITS PER SRM 53-00-01-1A-1. COMPLIED WITH E/RA 623013-14.SDR DALA2024122311944Skin · gouged(LOG 0718932) SKIN GOUGED AT STA 832 ON STR 27L. COMPLIED WITH E/RA 623102-14.SDR ASAA2024121954700Skin · corrodedPOSSIBLE CORROSION ON FASTENERS BETWEEN STA 927 AND STA 947.5 AT STGR 26R SRXR430X. GROUNDED - YES. ACCOMPLISHED CATEGORY A MINOR REPAIR TO FUSELAGE SKIN PANEL P/N 147A3400-4 BETWEEN STA 927 AND STA 947.5 STGR 26R IAW EA 53EA-27979 REV 00 SRXR430X.SDR ASAA2024121954699Skin · corrodedPOSSIBLE CORROSION ON SKIN AND AROUND FASTENER HEAD AT STA 787 AND STGR 23L SRXR430X. GROUNDED - YES. ACCOMPLISHED CATEGORY A MINOR REPAIR TO FUSELAGE SKIN PANEL 146A3231-49 AT STA 787 STGR 23L IAW EA 800-53EA-27975 REV00SDR ASAA2024121954698Skin · corrodedPOSSIBLE CORROSION ON FASTENER HEADS AT STA 905 TO STA 927 BETWEEN STGR 23L AND STGR 24L SRXR430X. GROUNDED - YES. ACCOMPLISHED CATEGORY A MINOR REPAIR ON FUSELAGE SKIN PANEL P/N 147A3400-4 AT STA 907 BETWEEN STA 23L AND STGR 24L IAW EA 800-53EA-27976 REV 00 SSDR SWAA2025012079259Bracket · crackedCRACK SUPPORT BRACKET LOCATED ON PNEUMATIC DUCT ON BS 540 AND RBL 6 AT AIR CONDITIONING BAY (1 EA). REPLACED SUPPORT BRACKET LOCATED ON PNEUMATIC DUCT ON BS 540 AND RBL 6 AT AIR CONDITIONING BAY IAW SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 212A1101 SHEET 14SDR CALA2025010900065Skin · corrodedFWD CARGO COMPARTMENT, AFT BULKHEAD, AIR CONDITIONING GROUND CHECK VALVE OUTLET FLANGE STRUCTURE, AFT SECTION SHOW EVIDENCE OF EXFOLIATING CORROSION. REF. AAR N/R:9928301 BET. STA 500H-450, STR 26L-26R ON A/C N34222 IAW PART 2 OF LAST BETWEEN STA 500H-540, STSDR DALA2024122011875Skin · ground damage(LOG 0717061) WHILE ON THE LINE IN UVF, A BELT LOADER STRUCK THE FUSELAGE BELOW THE AFT CARGO DOOR. AFTER PAINT REMOVAL AND BLENDING, DAMAGE #4 WAS FOUND TO BE OUTSIDE OF SRM REPAIRABLE LIMITS. THE GOUGE WAS APPROXIMATELY 3.6 LH TO RH AND 0.9 FWD-AFT WITH A DSDR DALA2024122011874Skin · ground damage(LOG 0717044) WHILE ON THE LINE IN UVF, A BELT LOADER STRUCK THE FUSELAGE BELOW THE AFT CARGO DOOR. THE A/C WAS FERRIED TO ATL FOR REPAIR, SEE ER/A 622966-14. AFTER PAINT REMOVAL AND BLENDING, THE FOLLOWING DAMAGES WERE FOUND TO BE OUTSIDE OF SRM ALLOWABLE LIMSDR BJNA202412190001Skin · damagedFOUND DENT/GOUGE 10.75IN AFT R1 DOOR AND 9.5 IN BELOW R1 DOOR FLOOR LINE AT WIDTH 0.5725IN AND LENGTH 0.279IN, DEPTH 0.044IN BETWEEN 2 RIVETS. BS 342.2. FOUND GOUGE ON RIVETE LINE 9.5IN BELOW FLOOR LINE R1 DOOR AND 11 IN AFT OF R1 DOOR LINE AT 0.8925IN AND 0SDR DALA2024121811801Skin · crackedCRACKS ON EXTERNAL SKIN STA Y 1153, BTW LONGERON 3L/4L AND BTW LONGERON 2R/3R AT AFT FUSELAGE. SUMMARY OF NRC 00050: EXTERNAL SKIN STA Y 1153, BTW LONGERON 3L/4L AND BTW LONGERON 2R/3R AT AFT FUSELAGE WAS REPAIRED PER ER/A 621926-14 REV ORIG SECTION I PERMANEN
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