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 JR2R20241112277Doubler · corrodedAFT WASTE DOOR CUTOUT ON INTERNAL SIDE CORRODED AROUND FLANGE AREA. REPAIRED.SDR SWAA2024121658778Stringer Clip · crackedINTERIOR; STR CLIP 4L IS CRACKED AT BS 727C.<[01] REMOVED AND REPLACED STRINGER CLIP P/N#143A1010-1 AT BS 727C STR 4L PER SRM 51-40-02-0G-0 AND PER DWG#146A1103.;[02] VERIFIED ACTION 1.<BR>JOB COMPLETE.SDR SWAA2024121658785Stringer Clip · crackedINTERIOR; STRINGER CLIP 4L IS CRACKED AT BS 727E.<[01] REMOVED AND EPLACED STRINGER CLIP 4L BS727E PER SRM 51-40-02; DWG#146A1112 REV:-. AND SRM 51-10-02 PARAGRAPH 9;[02] VERIFIED CORRECTIVE ACTION COMPLETE.SDR SWAA2024121658779Stringer Clip · crackedINTERIOR; STRINGER CLIP 5L IS CRACKED AT BS 727C.<[01] REMOVED AND REPLACED STRINGER CLIP P/N#143A1010-1 AT BS 727C STR 5L PER SRM 51-40-02-0G-0 AND PER DWG#146A1103.;[02] VERIFIED ACTION 1.<BR>JOB COMPLETE.SDR SWAA2024121658780Stringer Clip · crackedINTERIOR; STRINGER CLIP 5R IS CRACKED AT BS 727A.<[01] REMOVED AND REPLACED STRINGER CLIP P/N#143A1010-1 AT BS 727A STR 5R PER SRM 51-40-02-0G-0 AND PER DWG#146A1103.;[02] VERIFIED ACTION 1.<BR>JOB COMPLETE.SDR SWAA2024121658781Stringer Clip · crackedINTERIOR; STRINGER CLIP 5R IS CRACKED AT BS 727C.<[01] REMOVED AND REPLACED STRINGER CLIP P/N#143A1010-1 AT BS 727C STR 5R PER SRM 51-40-02-0G-0 AND PER DWG#146A1103.;[02] VERIFIED ACTION 1.<BR>JOB COMPLETE.SDR SWAA2024121658782Stringer Clip · crackedINTERIOR; STRINGER CLIP 6R IS CRACKED AT BS 727C.<[01] REMOVED AND REPLACED STRINGER CLIP P/N#143A1010-1 AT BS 727C STR 6R PER SRM 51-40-02-0G-0 AND PER DWG#146A1103.;[02] VERIFIED ACTION 1.<BR>JOB COMPLETE.SDR SWAA2024121658783Stringer Clip · crackedINTERIOR; STRINGER CLIP 4R IS CRACKED AT BS 727D.<[01] REMOVED AND REPLACED NEW STRINGER CLIP P/N#143A1010-1 AT BS 727D STR 4R PER SRM 51-40-02-0G-0 AND PER DWG#146A1103.;[02] VERIFIED ACTION 1.<BR>JOB COMPLETE.SDR SWAA2024121658795Stringer Clip · crackedINTERIOR; STRINGER CLIP 5R IS CRACKED AT BS 727E.<[01] REMOVED AND REPLACED STRINGER CLIP 5R BS727E PER SRM 51-40-02; DWG#146A1112 REV:-. AND SRM 51-10-02 PARAGRAPH 9;[02] VERIFIED CORRECTIVE ACTION COMPLETE.SDR SWAA2024121658784Stringer Clip · crackedINTERIOR; STRINGER CLIP 6R IS CRACKED AT BS 727E.<[01] REMOVED AND REPLACED STRINGER CLIP 6R BS727E PER SRM 51-40-02; DWG#146A1112 REV:-. AND SRM 51-10-02 PARAGRAPH 9;[02] VERIFIED CORRECTIVE ACTION COMPLETE.SDR SWAA2024121658786Stringer Clip · crackedINTERIOR; STRINGER CLIP 5L IS CRACKED AT BS 727E.<[01] REMOVED AND REPLACED STRINGER CLIP 5L BS727E PER SRM 51-40-02; DWG#146A1112 REV:-.AND SRM 51-10-02 PARAGRAPH 9;[02] VERIFIED CORRECTIVE ACTION COMPLETE.SDR SWAA2024121658787Stringer Clip · crackedINTERIOR; STRINGER CLIP 6L IS CRACKED AT BS 727E.<[01] REMOVED AND REPLACED STRINGER CLIP 6L BS727E PER SRM 51-40-02; DWG#146A1112 REV:-. AND SRM 51-10-02 PARAGRAPH 9;[02] VERIFIED CORRECTIVE ACTION COMPLETE.SDR SWAA2024121658788Stringer Clip · crackedINTERIOR; STRINGER CLIP 4L IS CRACKED AT BS 767.<[01] REMOVED AND REPLACED STRINGER CLIP P/N#143A1010-1 AT BS 767 STR 4L PER SRM 51-40-02-0G-0 AND PER DWG#146A1103.;[02] VERIFIED ACTION 1.<BR>JOB COMPLETE.SDR SWAA2024121658789Stringer Clip · crackedINTERIOR; STRINGER CLIP 5L IS CRACKED AT BS 767.<[01] REMOVED AND REPLACED NEW STRINGER CLIP P/N#143A1010-1 AT BS 767 STR 5L PER SRM 51-40-02-0G-0 AND PER DWG#146A1103.;[02] VERIFIED ACTION 1.<BR>JOB COMPLETE.SDR REXA2024121601591Skin · corrodedFUSELAGE SKIN P/N SH670-31633-7 HAS A SMALL AREA OF CORROSION ON INTERIOR SURFACE BETWEEN FS295.00 AND FS310.00 ADJACENT TO STRINGER 25R, PREEXISTING DAMAGE TO SKIN PANEL COMMON TO STRINGER 25R AT PREVIOUS REPAIR LOCATION, AND MULTIPLE OVERSIZED HOLES COMMON TSDR SWAA2024121358445Doubler · crackedEGPR DOOR CUT OUT LOWER INTERNAL DOUBLER CRACKED<[01] ACCOMPLISHED REPAIR OF EGPR SURROUND DOUBLER IAW B737-800 SRM 53-10-15-2R-4;[02] ACCOMPLISHED REPAIR OF EGPR SURROUND DOUBLER IAW B737-800 SRM 53-10-15-2R-4. RII OVERSIGHT AND CONSIDERATIONS APPLIED.SDR SWAA2024121258700Splice · corrodedCORROSION SPLICE LOCATED BS360 STR28L AND WL148.8 AT EQUIPMENT ELECTRONIC COMP 2024-701509<[01] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 23-JAN-25; TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811019 ; DUE DATE: SDR ASAA2024111153947Skin · corrodedTOILET VENT BETWEEN STR 21L AND 22L HAS SIGNS OF CORROSION. GROUNDED - YES. ACCOMPLISHED CATEGORY B MAJOR REPAIR TO FUSELAGE SKIN PANEL 147A3110-3 AT STA 20L-23L AT AFT LAV VENT CUTOUT IAW EA 800-53EA-27859 REV 00.SDR R61A2024112900560Doubler · dentedDENT - FR19/20, STR26R/27R. PERFORMED PERMANENT REPAIR ON FR19-20 STGR 26R-27R BY CUTTING DAMAGED AREA AND FABRICATING AND INSTALLING EXTERNAL SKIN DOUBLER REFER ETD2024-170-030805 REV A.SDR R61A2024112900559Doubler · dentedDENT - FR18/19, STR26R/27R. PERFORMED PERMANENT REPAIR ON FR18-19 STGR 26R-27R BY CUTTING DAMAGED AREA AND FABRICATING AND INSTALLING EXTERNAL SKIN DOUBLER REFER ETD2024-170-030805 REV A.SDR R61A2024111400536Skin · damagedBIRD STRIKE ON THE FWD NOSE BETWEEN FRAME 1 AND FRAME 2 AT STR 12L TO 17L. REPAIRED IAW ETD2024-170-030342 ALSO REF VP-047067-2024 N/R 1 FOR WORK ACCOMPLISHED.SDR AALA202411124506Skin · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN ELECTRICAL GROUND POWER RECEPTACLE SURROUND SKIN LOCATED AT STA 235.8, S21R. REPAIRED SKIN PER SRM 53-10-15-2R-4 REPAIR 4.SDR DALA2024111110805Access Panel · corrodedCORROSION ON ACCESS PANEL 5971074 -1 BTW STA Y=636 TO STA Y=655 L29L TO L29R AT FWD CARGO COMPARTMENT. SUMMARY OF NRC 00616: CORROSION LEVEL 2. ACCESS PANEL 5971074-1 BTW STA Y=636 TO STA Y=655 L29L TO L29R AT FWD CARGO COMPARTMENT WAS REPLACED PER B717-200 SRSDR DALA2024111110804Doubler · corrodedCORROSION WAS FOUND ON DOUBLER AT E/E COMPARTMENT ON INTERNAL FUSELAGE SKIN PANEL STA Y=215 TO STA Y=221 BTW LONGERON 28R AND 29R. SUMMARY OF NRC 00626: CORROSION LEVEL 2. DOUBLER ON INTERNAL FUSELAGE SKIN PANEL STA Y=215 TO STA Y=221 BTW LONGERON 28R AND 29R SDR ASAA2024110953720Skin · corrodedBUTT JOINT AT STA 1016 BETWEEN STGR 22L-23R HAS SIGNS OF CORROSION SRXR430X. GROUNDED - YES. ACCOMPLISHED CATEGORY B MINOR REPAIR TO FUSELAGE SKINS 147A3400-4, 147A3110-3, 148A3321-13 AND 148A3311-2 AT STA 1016 BETWEEN STGR 21L AND STGR 23R IAW EA 800-53EA-278SDR ASAA2024110953719Skin · corrodedBUTT JOINT AT STA 887 BETWEEN STGR 20R AND 21R HAS SIGNS OF CORROSION SRXR430X. GROUNDED - YES. ACCOMPLISHED CATEGORY A MINOR REPAIR AT FUSELAGE SKIN P/N 146A3251-32 AND 147A3110-4 AT STA 887 BETWEEN STGR 20R AND STGR 23R IAW EA# 800-53EA-27827 REV 00 SRXR430XSDR CALA2024111402859Skin · dentedWATER TRUCK BACKED INTO AIRCRAFT AND CAUSED DAMAGE. DENT TOTAL GOUGE LENGTH IS 2.4 INCHES. BOTH DENTS ARE FOUND TO BE OUT OF LIMITS PER SRM 53-00-01-1A-5 LOWER DENT IS 9.910 FROM REPAIR ACCOMPLISHED ON ECRA 5330-06581 LOCATION OF DAMAGE IS ON LH SIDE OF AIRCSDR DALA2024111110809Skin · chafedSHIP 3145 CHAFING EXTERNAL SKIN ON FR34 STR 43R AT LOWER FUSELAGE. CORRECTIVE ACTION: EVALUATED REWORK AREA LOC. EXTERNAL SKIN ON FR34 STR 43R AT LOWER FUSELAGE AS PER A319 SRM 51-73-00-801 EVALUATED REWORKED AREALOC. EXTERNAL SKIN ON FR34 AND STR 43R AT LOWERSDR DALA2024111110801Skin · crackedCRACKED FUSELAGE SKIN STA Y 1087 LONG 14R LOCATED CLOSE TO THE LAP SKIN JOINT AND PREVIOUS REPAIR DOUBLER. SUMMARY OF NRC 00052: FUSELAGE SKIN STA Y 1087 LONG 14R LOCATED CLOSE TO THE LAP SKIN JOINT AND PREVIOUS REPAIR DOUBLER WAS REPAIRED PER ER/A 621691-14 RSDR VNAA202411090062Skin · ground damageMANLIFT MADE CONTACT WITH FUSELAGE BETWEEN FS 1108 - 1126, STR 19R - STR 20R. REPAIRED FUSELAGE SKIN IAW CRJ-700 SRM 53-00-01-201-010-A01.SDR VNAA202411090048Skin · corrodedUPON REMOVAL OF STRINGER 22R BETWEEN FS 333.00-349.00 CORROSION WAS FOUND ON INTERNAL FUSELAGE SKIN. REPAIRED IAW MHIRJ REO 670-53-21-2448 REV-- DATED 2024-08-16SDR VNAA2024111090002Skin · scratchedTHE EXTERNAL SIDE OF THE FUSELAGE SKIN IS SCRATCHED AROUND THE PERIMETER OF THE AFT GPS ANTENNA LANDING. (BETWEEN FS 565 AND FS 581, STGR 0). REPAIRED IAW MHIRJ REO 670-53-31-927 REV-- DATED 2024-08-22.SDR VNA2024111000021Skin · scratchedTHE EXTERNAL SIDE OF THE FUSELAGE SKIN IS SCRATCHED AROUND THE PERIMETER OF THE AFT GPS ANTENNA LANDING. (BETWEEN FS 565 AND FS 581, STGR 0) REPAIRED IAW MHIRJ REO 670-53-31-927 REV-- DATED 2024-08-22.SDR 2024FA0000826Skin · crackedON THE LOWER FUSELAGE SKIN AT FS 422 & 779 CORROSION WAS FOUND AROUND THE FASTENER HOLES WHERE THE LOWER FUSELAGE TO WING FAIRINGS ATTACH. AFTER REMOVING THE CORROSION AND THE EVALUATION DETERMINED THE SKIN IN THOSE AREAS WAS OUT OF LIMITS. ENGINEERING WAS REQSDR FDEA202411081648Skin Panel · damagedUPPER FUSELAGE SKIN FOUND LIGHTNING STRIKE AT STA412, S19R-0.6" REPAIRED THE UPPER FUSELAGE SKIN LIGHTNING STRIKE AT STA412, S19R-0.6" PER B767 SRM53- 00-01-2R REPAIR 1 AND EA:H-5330-T0381271 P1, TITLE: FUSELAGE - PLATES & SKINS - LIGHTNING STRIKE ON FUSELASDR DALA2024111410953Doubler · cracked-AD- FUSELAGE PLATE SKIN DOUBLERS STA Y=1178 BTW L1-L3 LH CRACKED. ACCOMPLISH ER/A 546495-14AD REV A SECTION III FOR THE INSPECTION OF THE REAR CANTED BULKHEAD REPAIR. THIS IS AD RELATED. INSPECTIONS CANNOT BE PUSHED PAST 04DEC24. ASSOCIATED ER/A 14-546495 ADDSDR EE4Y2024110821267Skin Panel · dentedDURING ALLEGIANT TASK CARD CR_P3-WEEKLY-CHECK/027 FORWARD FUSELAGE LEFT SKIN PANEL SURFACE IS FOUND DENTED AT FR29 BETWEEN STRINGERS 37LH AND 38LH WAS FOUND. THE FUSELAGE SKIN PANEL WAS REPAIRED IAW A320 SRM 53-21-11-300-093 PRINCIPLE 2 FIG 001. THIS IS MAJOR SDR DALA2024110810727Skin · gougedGOUGE ON EXTERNAL SKIN BTW STA 123 AND L-29L TO L-30 AT FUSELAGE. SUMMARY OF NRC 00092: EXTERNAL SKIN BTW STA 123 AND L-29L TO L-30 AT FUSELAGE WAS REPAIRED PER B717-200 SRM 53-03-01-2R PROCEDURE 1, REPAIR 1 PAR 6.A. FIG 202. PERFORM A VISUAL INSPECTION EVERY SDR SWAA2024121257804Support Bracket · crackedCRACK ON SUPPORT BRACKET LOCATED BS 867 BTW STR 2R TO STR 3R AT PASSENGER CABIN 2024-701450<[01] REPLACED SUPPORT BRACKET LOCATED BS 867 BTW STR 2R TO STR 3R AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 146A7901 SHEET 66 REV A.<BR>SDR HNAA2024121101186Doubler · corrodedF006237 INTERIOR SKIN DOUBLER CORRODED AT BTW FR6162 BTW STR20-21L. REPAIRED IAW EO1-53-24-0672SDR SWAA2024120557438Gusset · crackedCRACK ON GUSSET LOCATED BS500I AND STR21R AT FWD CARGO COMPARTMENT 2024-686249<[01] REPLACED GUSSET AND FASTENERS LOCATED BS500I AND STR21R AT FWD CARGO COMPARTMENT I.A.W B737-800 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG: 143A7902; SHEET 256; REV ?B?. SEE INDSDR SWIA202411270007Skin · dentedCOMPLY WITH SCHEDULED MAINTENANCE CODE: RA91126-ETD2024-170-014527 REV :/ DATED 5/24/2024 MXCODEID74779-PR - COMPLY WITH ETD2024-170-014527 REV :/ DATED 5/24/2024 PERMANENT REPAIR FOR TWO DENTS LOCATED BETWEEN FR21 AND FR22 AND BETWEEN STGR14L AND STGR15L (JUSDR DALA2024111110844Skin · damagedDAMAGE FOUND ON FUSELAGE BETWEEN STRINGER 26LH TO STRG28L/H AND FRAME 32 TOFRAME33.REF LOG:6625106. COMPLETED ALL STEPS OF PRI 621793-14 REV O . COMPLETED ALL STEPS OF PRI 621793-14 REV 1 W BLADES 302615 . COMPLETED ALL STEPS OF PRI 621793-14 REV 2. W BLADES 3SDR DALA2024111110838Skin · wornSHIP 1808 RH FWD REPAIR SKIN UNDER H/STAB SEAL AREA FOUND WEAR. CORRECTIVE ACTION: DAMAGED AREA REPAIRED AS PR B767-400 SRM 53-80-01. (0648249)SDR ASAA2024110753696Skin · corrodedBUTT JOINT STA 360 BETWEEN STGR 5R AND 6R HAS SIGNS OF CORROSION SRXR430X. GROUNDED - YES. ACCOMPLISHED CATEGORY A MINOR REPAIR AT STA 360 BUTT SPLICE BETWEEEN STGR 5R AND 6R ON SKIN P/N 143A3131-28 IAW EA# 800-53EA-27821 REV 00SDR ASAA2024110753695Skin · corrodedBUTT JOINT AT STA 1088 BETWEEN STGR 16R-17R HAS SIGNS OF CORROSION SRXR430X. GROUNDED - YES. ACCOMPLISHED CATEGORY A MINOR REPAIR AT STA 1088 BUTT JOINT BETWEEN STGR 16R-17R ON SKIN P/N 148A3321-13 IAW EA# 800-53EA-27820 REV 00SDR DALA2024110810761Skin · dentedSHIP 3160 DENT EXTERNAL SKIN LOC. BTW FR82 TO FR83 AT LEVEL STGR 3 LH ON UPPER FUSELAGE. CORRECTIVE ACTION: COMPLIED WITH ER/A 621495-14. (0648987)SDR DALA2024110810751Skin · dented(LOG 0648823) DURING INSPECTION, A CREASED DENT WAS FOUND ON THE FUSELAGE SKIN P/N 141A3521-12 AT BS 355, 2 INCHES OUTBOARD OF S-28R. REPAIRED DAMAGE PER ERA 621875-14.SDR DALA2024110810746Skin · dented(LOG 0649150) DENT ON FUSELAGE EXTERNAL SKIN LOWER SURFACE LOCATED AT 2" O/B OF STR 28R AND STA 351.2 + 4". C/W ER/A 621875-14 REV ORIGINAL.SDR AALA202411076792Doubler · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN FORWARD FUSELAGE EXTERNAL POWER ACCESS DOOR SURROUND DOUBLER AT STA 235.8, FROM S21R TO S22R. REPAIRED DOUBLER PER SRM 53-10-15-2R PROCEDURE 4.
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