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 DALA2021122207980None · noneSHIP 3248 TOOLING DAMAGE ON AFT SIDE OF SKIN CLIP, BELOW FRAME 73, BETWEEN 73, BETWEEN STRINGERS 31L AND 30L. CORRECTIVE ACTION: REPLACED CLIP PER A320 SRM 51-72-11. (2060597)SDR DALA2021122207979None · noneSHIP 3248 TOOLING DAMAGE ON AFT SIDE OF SKIN CLIPS BELOW FRAME 74 BTW STR 30L 29L AND STR 30R AND 29R. CORRECTIVE ACTION: REPLACED CLIPS PER A320 SRM 51-72-11. (2060595)SDR DALA2021122207978None · noneSHIP 3248 TOOLING DAMAGE ON AFT SIDE OF SKIN CLIPS (5EA) BELOW FRAME 75 BTW STR 39L AND STR 39R. CORRECTIVE ACTION: REPLACED CLIPS PER A320 SRM 51-72-11. (2060588)SDR DALA2021122207977None · noneSHIP 3248 TOOLING DAMAGE ON AFT SIDE OF SKIN CLIP, AFT OF FRAME 73, BETWEEN STRINGERS 30R AND 31R. CORRECTIVE ACTION: REPLACED CLIP PER A320 SRM 51-72-11. (2060583)SDR DALA2021122207976None · noneSHIP 3248 TOOLING DAMAGE ON SKIN CLIPS/FRAME, FORWARD SIDE OF FRAME 72, BETWEEN STRINGERS 32R AND 34R. CORRECTIVE ACTION: REPLACED CLIP PER A320 SRM 51-72-11. (2060581)SDR MASA20211221641None · noneTHE LOWER FUSELAGE SKIN PANEL WERE REPORTED WITH TOTAL OF FOUR ZONES WITH MULTIPLE NICK DAMAGES. PERFORMED PERMANENT REPAIR IAW CRJ7/9 SRM 53-31-01-991-806, ITEM 1, A AND B (REV. 37 DATED AUG. 15, 2019. DEFECT LOCATION: FS 501.00 -FS 661.00 AND STGR 19L -STGRSDR MASA20211221633None · noneTHE FUSELAGE LOWER SKIN PANEL WAS FOUND WITH MINOR CORROSION DAMAGE. PERFORMED PERMANENT REPAIR IAW SRM 53-51-01-001-003-A02 ITEM 1A, D AND E (REV.38 DATED 9 JUL2021). DEFECT LOCATIONS: FS 913.00 -942.00. STGR 20R-STGR 20LSDR MASA20211221632None · noneTHE FUSELAGE LH SKIN PANEL WAS FOUND WITH MINOR CORROSION DAMAGE. PERFORMED PERMANENT REPAIR IAW SRM 53-51-01-001-002-A02 ITEM 1, C, AND D (REV.38 DATED 9 JUL 2021). DEFECT LOCATION: FS 847+16-FS 913 AND STGR 17L-STGR 20LSDR MASA20211221631None · noneTHE FUSELAGE RH SKIN PANEL WAS FOUND WITH MINOR CORROSION DAMAGE. PERFORMED PERMANENT REPAIR IAW SRM 53-51-01-001-004-A02 ITEM 1, A, AND D (REV.38 DATED 9 JUL 2021) - DEFECT LOCATION: FS 875-FS 920 AND STGR 17R - 19RSDR LR7A2021121903071Skin · gougedDURING SCHEDULED B-2 CHECK UNDER JOB CARD HB5302, FOUND THE LH AFT FUSELAGE SKIN GOUGED AT FS954, LBL60, WL225 NEAR THE SLOPING LONGERON. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-12. NR# 1000652410.SDR DALA2021122007891None · none(LOG 2057885) DURING INSPECTION FOUND LIGHTNING STRIKE ON L/H SIDE OF AFT FUSELAGE INSIDE THE LETTER "D" OF REGISTRATION NUMBER. REPAIRED PER B737 SRM 53-00-01-2R.SDR SWAA2022020754454Bear Strap · crackedTYPICAL CRACK FOUND EMANATING FROM EDGE OF BEAR STRAP TO FASTENER HOLE FWD OF FITTING LATCH AT R1 DOOR BETWEEN STA.291.5 AND STA.294.5 BETWEEN S-8R AND S-9R. APPROXIMATE LENGTH OF CRACK : 2' ; TYPICAL CRACK FOND EMANATING FROM EDGE OF BEAR STRAP TO FASTENER HOSDR MASA20211221623None · noneTHE LOWER FUSELAGE SKIN PANEL HAD A PREVIOUS REPAIR INSTALLED PER REO 690-53-21-989 THAT CONFLICTED WITH THE OPERATOR RECOMMENDED SERVICE BULETIN 670BA-53-057 THAT INVOLVES RELOCATING THE DRAIN HOLES FORWARD AND INSTALLING TWO SMALL DOUBLERS FOR THE NEW DRAIN SDR DALA2021122007903None · noneSHIP 6713 C/W UT DIS-BOND INSPECTION PER AMDS 5331-01232-02G AND MARKED AREA OF DIS-BOND BETWEEN FUSELAGE SKIN AND BEARSTRAP. AREA IS 18 '' HIGH ALONG THE L/E OF L1 DOOR FRAME, 4'' HIGH FROM UPPER DOOR HEADER, 9'' FWD OF FWD DOOR FRAME, AND A TOTAL OF 18" HIGHSDR REXA2022012600115Bonding Plate · corrodedLH PYLON IS MISSING A BONDING PLATE ON THE AFT UPPER SKIN.
"REMOVED FASTENERS, LOCATED & DRILLED PLATE IAW CRJ 900 SRM
51-42-13-001-001-A01, 51-40-11-001-001-A01. INSTALLED & PAINTED IAW
CRJ 900 SRM 51-42-15-001-001-A01 & 51-25-16-001-001-A01, AMM SDR SWAA2022011854140Intercostal · crackedFOUND INTERCOSTAL/BAFFLE CRACKED AT FWD. CARGO COMPT. BETWEEN BS 400 & 420;LBL 21. ; / [01] REMOVED INTERCOSTAL/BAFFLE AT FWD CARGO COMPT. STA 400 AND 420;LBL 21 IAW B737-700 SRM 51-40-02-0G-0; [02] LOCTED AND DRILLED NEW INTERCOSTAL/BAFFLE; AT FWD CARGO COMPTSDR ASAA2021121637018Skin · corrodedRH FUSELAGE SKIN IS CORRODED AT LAV OVERBOARD VENT GROUNDED - YES. ACCOMPLISHED CATEGORY A PERMANENT REPAIR TO RH FUSELAGE SKIN AT LAV OVERBOARD VENT BETWEEN FR 69 - 70 STGR 30RH TO STGR 33RH IAW A320 SRM 53-41-11-300-004. WORK ACCOMPLISHED ON DOCUMENT SA01472SDR DALA2021122007900None · noneSHIP 6713 DTE ERA 596065-14 ESTABLISHING STAGE III DTE RESTRICTION FOR ERA 596065-14. CORRECTIVE ACTION: REF ERA 596065-14. (2053961)SDR DALA2021122007896None · noneSHIP 3317 WHILE ON THE LINE IN SLC, THE A/C SUFFERED AN EXPLOSIVE DEPRESSURIZATION WHILE ACCOMPLISHING A PRESSURIZATION TEST PER A330 AMM 05-53-00-780-803-A. THE A/C WAS BEING PRESSURIZED AND AT APPROX. 2 TO 3 PSI THE FWD CARGO DOOR WAS OPENED CAUSING THE EXPLSDR DALA2021121707849None · noneSHIP 1704 RH WHEEL WELL CANTED PRESSURE DECK FOUND CRACK BETWEEN STA955 AND STA977. CORRECTIVE ACTION: THE REPAIR CARRIED OUT TO PRESSURE DECK WEB OF R/H W/W AT STA955 TO STA977, RBL27 AND RBL32 AS PER B767-300 SRM53-50-51-2R-2. (2054139)SDR DALA2022030101300None · noneSHIP 172 FASTENER DAMAGE LOCATION S16L B @ FS157.0. CORRECTIVE ACTIVETION: PERFORMED BLIND FASTENER TEMP REPAIR B767 SRM 53-00-01-2R (2053273)SDR DALA2022030101299None · noneSHIP 172 FASTENER DAMAGE LOCATION S21L @ FS154.0. CORRECTIVE ACTIVETION: PERFORMED BLIND FASTENER TEMP REPAIR B767 SRM 53-00-01-2R (2053271)SDR DALA2022030101298None · noneSHIP 172 FASTENER DAMAGE LOCATION S15L B @ FS220.50. CORRECTIVE ACTIVETION: PERFORMED BLIND FASTENER TEMP REPAIR B767 SRM 53-00-01-2R (2053265)SDR DALA2022030101297None · noneSHIP 172 FASTENER DAMAGE LOCATION S21L @ FS143.5. CORRECTIVE ACTIVETION: PERFORMED BLIND FASTENER TEMP REPAIR B767 SRM 53-00-01-2R (2053261)SDR DALA2022030101296None · noneSHIP 172 FASTENER DAMAGE LOCATION S16L A @ FS172.50, CORRECTIVE ACTIVETION: PERFORMED BLIND FASTENER TEMP REPAIR B767 SRM 53-00-01-2R (2053257)SDR DALA2022030101295None · noneSHIP 172 FASTENER DAMAGE LOCATION S15L A @ FS172.50. CORRECTIVE ACTIVETION: PERFORMED BLIND FASTENER TEMP REPAIR B767 SRM 53-00-01-2R (2053252)SDR DALA2022030101294None · noneSHIP 172 FASTENER DAMAGE LOCATION S15L B @ FS172.50. CORRECTIVE ACTIVETION: PERFORMED BLIND FASTENER TEMP REPAIR B767 SRM 53-00-01-2R (2053249)SDR DALA2022030101293None · noneSHIP 172 FASTENER DAMAGE LOCATION S15L A @ FS172.50. CORRECTIVE ACTIVETION: PERFORMED BLIND FASTENER TEMP REPAIR B767 SRM 53-00-01-2R (2053244)SDR DALA2022030101292None · noneSHIP 172 FASTENER DAMAGE LOCATION S16L A @ FS164.75, CORRECTIVE ACTIVETION: PERFORMED BLIND FASTENER TEMP REPAIR B767 SRM 53-00-01-2R (2053233)SDR DALA2022030101291None · noneSHIP 172 FASTENER DAMAGE LOCATION S15L B @ FS196.50, CORRECTIVE ACTIVETION: PERFORMED BLIND FASTENER TEMP REPAIR B767 SRM 53-00-01-2R (2053230)SDR DALA2022030101290None · noneSHIP 172 FASTENER DAMAGE LOCATION S15L A @ FS212.50, CORRECTIVE ACTIVETION: PERFORMED BLIND FASTENER TEMP REPAIR B767 SRM 53-00-01-2R (2053222)SDR SWAA2022011853491Door · corrodedFOUND CORROSION & WORN AT L-1 DOOR CUTOUT FWD. FRAME LOWER HINGE BOX UPPER FITTING HOLE. PARTIAL REMOVED HINGE BOX AT L-1 DOOR CUTOUT FWD. FRAME LOWER. IAW SRM 51-40-02. INSTALLED EWIS PROTECTION AT L-1 DOOR CUTOUT FWD. LOWER HINGE BOX AREA DURING MAINT. IAWSDR SWAA2022011353548Angle · corrodedFWD CARGO COMPARTMENT FLOOR STRUCTURE STA 500B TO 500C; RBL 24; WL 156 R/H Z-ANGLE HAS CORROSION. A224-12 ; / [01] REMOVED CORROSION IAW SRM 51-10-02 VERIFIED WITH 10X MAGNIFY ORIGINAL THICKNESS .040 MATERIAL REMOVED .007 REMAINING MATERIAL .033 FOUND TO BE OUSDR SWAA2022011353543Angle · corrodedFWD CARGO COMPARTMENT FLOOR STRUCTURE STA 500B+18; LBL 24; WL 156 L/H Z-ANGLE HAS CORROSION. A224-005 ; / [01] REMOVED CORROSION IAW SRM 51-10-02 VERIFIED WITH 10X MAGNIFY ORIGINAL THICKNESS .040 MATERIAL REMOVED .006 REMAINING MATERIAL034 OUT OF LIMITS IAW SRSDR DALA2021121707861None · noneSHIP 6817 PREVIOUS BLEND OUT WITHOUT IDENTIFICATION ON FUSELAGE SKIN STA 400 STR 21R. CORRECTIVE ACTION: SUMMARY OF NRC 00072; PREVIOUS BLEND OUT WITHOUT IDENTIFICATION ON FUSELAGE SKIN STA 400 STR 21R WAS REPAIRED PER ETI-57-21-576 REV. 2 AND ERA NO. 596073-1SDR DALA2021121607826None · none(LOG 2053455) DURING INSPECTION FOUND EROSION ON VERTICAL FIN LEADING EDGE BTW LE STA 108.238 AND LE STA 100.598. VERTICAL FIN LEADING EDGE BTW LE STATION 108.238 AND LE STA 100.598.WAS REPAIRED PER B737-800 S.R.M. 55-30-01-1A-4 PAR. 4.C.(5). AND ER/A 426980-1SDR DALA2021121607825None · noneSHIP 1604 PERMANENT REPAIR DUE PER ERA 595699-14 REV A. CORRECITVE ACTION: REMOVED TEMPORARY REPAIR FROM LOWER FUSE SKIN STA 1417-1502 STR37R TO STR37L AND APPLIED NEW REPAIR IAW ERA#59579614AD REVA (7636169)SDR DALA2021121607824None · noneSHIP 1604 AMOC MONITOR INSPECTION LOG REF ERA 595796-14AD REV.B PENDING AMOC APPROVAL TO AD 2014-14-04 PRIOR TO 50,000 TOTAL FLIGHT CYCLES. CORRECITVE ACTION: DISCONTINUE REVENUE SERVICE ON OR BEFORE 50,000 TOTAL FLIGHT CYCLES PENDING AMOC APPROVAL TO AD 2014-SDR DALA2021121607823None · noneSHIP 1604 DTA MONITOR INSPECTION LOG REF ERA 595796-14 REV. B PENDING DTE APPROVAL DUE PRIOR TO 15 DEC 2022. CORRECITVE ACTION: DISCONTINUE REVENUE SERVICE ON OR BEFORE 15 DEC 2022 PENDING DTE APPROVAL FROM ENABLING TECHNOLOGIES ASSOCIATED ER/A 13-595796 (2053SDR DALA2021121607816None · noneSHIP 1604 REMOVE TEMPORARY REPAIRS AS REQ, CORRECITVE ACTION: REMOVED TEMPORARY REPAIR FROM LOWER FUSE SKIN STA 1417 TO 1502 STR 37R TO 37L AND APPLIED NEW REPAIR IAW ERA 595796-14AD REV A AND REV B. (2053421)SDR SWAA2022020253255Angle · crackedFWD CARGO INTERCOSTAL ATTACH ANGLE CRACKED FWD BS 500C LBL 25 WL 156. PRIOR TO REMOVAL, FOUND PART TO HAVE NO SRM LIMITS AND SO PART IS REPAIRABLE BY REPLACEMENT PER SRM 51-10-02-OG-0 STEP 9. REMOVED FWD CARGO INTERCOSTAL ANGLE IAW SRM 51-40-02. LOCATED ANSDR SWAA2022020253256Angle · crackedFWD CARGO COMPARTMENT INTERCOSTAL ATTACH ANGLE CRACKED AFT BS 500C LBL 25 WL 156. REMOVED THE INTERCOSTAL ANGLE IAW SRM 51-40-02. PRIOR TO REMOVAL, FOUND PART TO HAVE NO SRM LIMITS AND SO PART IS REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02-OG-0, STEP 9. LOSDR SWAA2022020253257Angle · crackedFWD CARGO COMPARTMENT INTERCOASTAL ATTACH ANGLE CRACKED BS 500B, LBL 25, WL 156. REMOVED THE INTERCOSTAL ANGLE IAW SRM 51-40-02. PRIOR TO REMOVAL, FOUND PART TO HAVE NO SRM LIMITS AND SO PART IS REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02-OG-0, STEP 9. LOCATSDR SWAA2022020253258Angle · crackedFWD CARGO INTERCOASTAL ATTACH ANGLE CRACKED AFT BS 400, LBL 25, WL 156. PRIOR TO REMOVAL, FOUND PART TO HAVE NO SRM LIMITS AND SO PART IS REPAIRABLE BY REPLACEMENT PER SRM 51-10-02-OG-0 STEP 9. REMOVED THE INTERCOSTAL ANGLE CRACKED IAW SRM 51-40-02. LOCATED SDR SWAA2022020253259Angle · crackedFWD CARGO INTERCOASTAL ATTACH ANGLE CRACKED, BS 500B, RBL 25, WL 156. PRIOR TO REMOVAL, FOUND PART TO HAVE NO SRM LIMITS AND SO PART IS REPAIRABLE BY REPLACEMENT PER SRM 51-10-02-OG-0 STEP 9. REMOVED FWD CARGO INTERCOSTAL ANGLE IAW SRM 51-40-02. REMOVED ANDSDR SWAA2022020253260Angle · crackedFWD CARGO INTERCOSTAL ATTACH ANGLE CRACKED AFT BS 500C RBL 25 WL 156. REMOVED THE INTERCOSTAL ANGLE IAW SRM 51-40-02.. FOUND PART TO HAVE NO SRM LIMITS AND SO PART IS REPAIRABLE BY REPLACEMENT PER SRM 51-10-02-OG-0 STEP 9. LOCATED AND DRILLED THE INTERCOSTSDR SWAA2022020253261Angle · crackedFWD CARGO INTERCOASTAL ATTACH ANGLE CRACKED FWD BS 500C RBL 25 WL 156. PRIOR TO REMOVAL, FOUND PART TO HAVE NO SRM LIMITS AND SO PART IS REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02-OG-0 STEP 9. REMOVED FWD CARGO INTERCOSTAL ANGLE IAW SRM 51-40-02. REMOVED ASDR SWAA2022013153478Intercostal · crackedCRACK WEB - INTERCOSTAL LOCATED BETWEEN BS492.4 TO BS500A AT LEVEL FLOOR STRUCTURE RH SIDE FWD CARGO COMPARTMENT ; 2021-567087 / [01] REPLACED WEB - INTERCOSTAL LOCATED BETWEEN BS492.4 TO BS500A AT LEVEL FLOOR STRUCTURE RH SIDE FWD CARGO COMPARTMENT IAW B737-7SDR SWAA2022013153165Angle · crackedCRACK ANGLE - CLIP LOCATED BS400 AND STR26L AT LEVEL FLOOR STRUCTURE FWD CARGO COMPARTMENT ; 2021-567086 / [01] REPLACED ANGLE - CLIP LOCATED BS400 AND STR26L AT LEVEL FLOOR STRUCTURE FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 Ï¿½TEM 9 SRM 51-40-02 AND DWSDR DALA2021121607796None · noneSHIP 3263 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR EXTERNAL SKIN LOCATED AT FR 2 AND 22 INCH BELOW OF LH SIDE STRINGER LOWER FUSELAGE. CORRECTIVE ACTION: REPAIRED PER A320 SRM 53-00-11. (2051508)
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