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 ASAA2024090452430Skin · corrodedREF DEFECT # 300011333 N/R-00004 LAV WASTE VENT SKIN IS OUT OF LIMITS AND REQUIRES REPAIR. GROUNDED - YES. REPAIRED LAV WASTE VENT SKIN IAW 737-800 SRM 53-70-01-2R-3W= .5" O= .125" R= .096" L= 1" D= .029".SDR DALA2024090908798Skin · damagedSHIP 1805 ERA 620270-14AD ISSUED FOR REPAIR TO RH FORWARD DOOR CUTOUT, AFT LOWER SKIN REPAIR. FOLLOW ON ACTION IS REQUIRED. CORRECTIVE ACTION: ERA 620270-14AD ISSUED FOR REPAIR TO RH FORWARD DOOR CUTOUT, AFT LOWER SKIN REPAIR. FOLLOW ON ACTION IS REQUIRED. (05SDR CALA2024090500565Skin · damagedWORK STAND BLEW INTO FUSELAGE WITH 30 TO 40 KTS WINDS.PREPPED A/C FOR INSP. COMPLETED STEPS 1-5 OF AVO13077. NEXT STEP IS INSP. REF AVO 13077 REV B, C/W STEPS 1-9, REF 787 NTM PT4 51-00-06, GIUDED A-SCAN, FOUND DELAMINATION 2" X 13 " LONG. C/W 787 NTM PT4 51-0SDR IXXA2024090403Skin · corrodedLAP SEAM AT S36R BETWEEN STA. 1197+66 AND 1197+88 CORROSIONSDR LR7A2024090303548Skin · crackedDURING SCHEDULED C-15 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND FUSELAGE SKIN CRACKED FASTENER HOLES FS524-477, LBL79, WL227. / REPAIRED IAW LAC MEA 382-53-24-114. DRC# 0104.SDR LR7A2024090303546Skin · crackedDURING SCHEDULED C-15 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND FUSELAGE SKIN CRACKED AT FS617,LBL61, WL260. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. DRC# 0102.SDR LR7A2024090303545Skin · crackedDURING SCHEDULED C-15 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND FUSELAGE SKIN CRACKED FASTENER HOLES AT FS436-477, RBL72, WL233. / REPAIRED IAW LAC MEA 382-53-24-093. DRC# 0101.SDR LR7A2024090303542Skin · crackedDURING SCHEDULED C-15 CHECK UNDER JOB CARD HC5321, FOUND FUSELAGE SKIN CRACKED AT FS708, RBL85, WL192-196. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-10. DRC# 1069. / PSE# 53-40-08, AD 2012-06-09SDR LR7A2024090303537Skin · corrodedDURING SCHEDULED C-15 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND FUSELAGE INNER DOUBLER SKIN CORRODED AT FS787.0E-813.0E, LBL79, WL150-190. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. DRC# 1032.SDR LR7A2024090303536Skin · corrodedDURING SCHEDULED C-15 CHECK UNDER WHILE PERFORMING OTHER MAINTENANCE, FOUND FUSELAGE SKIN CORRODED AT FS777.0E-817.0E, LBL61, WL143. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. DRC# 1031.SDR LR7A2024090303507Skin · crackedDURING SCHEDULED C-15 CHECK UNDER JOB CARD HC5321, FOUND LH FORWARD FUSELAGE SKIN CRACKED AT FS140, LBL60, WL205-211. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-10. DRC# 0878. / PSE# 53-30-08, AD 2012-06-09SDR CALA2024090402377Skin · dentedPROTRUDING DENT AT STA 710 AT S23 RT LWR FUSELAGE. PERFORMED REPAIR SKIN FUSELAGE AT STA 700 TO 720 BETWEEN S23 R/H TE S24 RH IAW B757-200 SRM 53-00-01-2R-29.SDR SWIA2024111200902Skin · dentedFS1015 - 1031 STRG 4RH 2EA EXTERIOR FUSELAGE SKIN DENTS ON TOP OF A FASTENER (MARKED) (C-CHECK RO 11/11/2024) REPAIRED FS1015 - 1031 STRG 4RH 2EA EXTERIOR FUSELAGE SKIN DENTS ON TOP REF CRJ 900 SRM 53-00-01-201-001-A03, FOR REPAIR TYPE 9- NOTED ON FIGUSDR AALA202411060337Skin · corrodedACFT WAS GROUNDED: LARGE AREA OF SEVERE CORROSION APROX 2" X 1" AT BS 887 S27L. RIVET HEAD MISSING AND SKIN CRACKED APROX 1" LENGTHWISE OF AC. MX FOUND CORROSION ON FUSELAGE SKIN UNDER SPLICE STRAP AT BS 887, FROM S24L TO S27R. ACCOMPLISHED DOUBLER REPAIR PERSDR NACA2024090200002Skin · corrodedFUSELAGE SKIN EXTERIOR SURFACE CORROSION AT STA 1043 TO 1021 AND S-1R. REPAIR CARRIED IAW SRMSDR AALA202409060337Skin · corrodedAIRCRAFT WAS GROUNDED: LARGE AREA OF SEVERE CORROSION APROX 2" X 1" AT BS 887 STR 27L. RIVET HEAD MISSING AN D SKIN CRACKED APROX 1" LENGTHWISE OF AC. MX FOUND CORROSION ON FUSELAGE SKIN UNDER SPLICE STRAP AT BS 887, FROM S24L TO S27R. ACCOMPLISHED DOUBLER RESDR CALA2024090300536Skin · crackedWHILE WORKING EA 5310-04550 REV D SKIN AND BULKHEAD OUTER CHORD INSPECTION, A CRACK WAS FOUND IN THE SKIN AREA AT STA 1725 STR 7R. IT WAS INSPECTED ON L/P 8986284. RII INSPECTED AND OKAY TABLE III IS 37500 FLIGHT CYCLES AFTER AIRCRAFT DELIVERY OR 6000 CYCLES ASDR CALA2024090302363Skin · dentedNEW DENT DAMAGE WAS LOCATED AT STA 221.5 AND 1 5 INCHES BELOW S-20L. DENT MEASURE OUT AT .068" DEEP WITH LENGTH OF 4.00" (REPAIR PER SRM). PERFORMED PERMANENT REPAIR ON FUSELAGE SKIN AT STA 221.5 AND 15 INCHES BELOW S-20L IAW B757-200 SRM 53-00-01-2R-29.SDR AALA202409112650Skin · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT, UNDER DOOR LOWER CUT-OUT SCUFF PLATE, ON FUSELAGE SKIN AT STA 438, RBL 25. REPAIRED SKIN PER SRM 51-10-02.SDR ASAA2024083153329Skin · corrodedSTGR 23L FROM STA 727F TO STA 827 HAS SIGNS OF CORROSION. GROUNDED - YES. ACCOMPLISHED CATEGORY A MINOR REPAIR ON FUSELAGE SKIN LAP SEAL STA 727F TO STA 827 AT STGR 23L AND STGR 24L PER EA #800-53EA-27549 REV 00.SDR ASAA2024083153328Skin · corrodedAT STA 967 BETWEEN SGTR 24R AND STGR 25R HAS SIGNS OF CORROSION ON LOWER FWD CORNER OF THE POWERED OUTFLOW VALVE. GROUNDED - YES. ACCOMPLISHED CATEGORY A MINOR REPAIR ON FUSELAGE SKIN SECTION 46 STA 967 AT STGR 24R AND STGR 25R PER EA # 800-53EA-27568 REV 00.SDR ASAA2024083153327Skin · corrodedFWD OF STA 1088 AND AT STGR 25R FWD END OF APU DOOR HAS SIGNS OF CORROSION. GROUNDED - YES. ACCOMPLISHED CATEGORY A MINOR REPAIR ON FUSELAGE SKIN SECTION 48 STA 1088 AT STGR 25R PER EA # 800-53EA-27557 REV 00.SDR ASAA2024083152625Skin · corrodedBETWEEN STA 905 AND STA 927 BETWEEN STGR 21L AND STGR 22L TOILET VENT HAS SIGNS OF CORROSION GROUNDED - YES. ACCOMPLISHED FUSELAGE SKIN DOUBLER REPAIR BETWEEN STA 907 AND STA 927 STGR 21L-22L IAW EA# 800-53EA-27562 REV 00.SDR CALA2024090200528Skin · dentedFOUND DENT REF LP 8972873, AVO13111A HAS BEEN COMPLETED. INSPECTION HAS EMAILED ENGINEERING OF THEIR FINDING STRINGER INSPECTED NO DAMAGE NOTED. VERIFIED ALL STEPS OF AVO COMPLETE ACCOMPLISHED DETAILED VISUAL INSPECTION OF REPAIR AREA REF AVO13111 STEP 15 ANDSDR SWAA2024100932519Stub Frame · brokenBROKEN STUB FRAME LOWER AREA ON BS 294.5 AT LEVEL STR 17R AT FWD GALLEY AREA 2024-528710<[01] TOOL USED ON STEP 6 AND 7:EDDY CURRENT FLAW DETECTOR P/N:NORTEC 600D; S/N:210138103;DUE DATE:10-JUN-25.;[02] PERFORMED REPAIR ON STUB FRAME LOWER AREA ON BS 294.5 AT SDR SWAA2024100932517Support Angle · brokenBROKEN ANGLE - SUPPORT BTW BS 291.5 TO BS 294.5 AT LEVEL STR 17R AT FWD GALLEY AREA 2024-528709<[01] REMOVED AND DISCARDED ANGLE SUPPORT(CLIP) 141A8312-3 IAW B737-700 SRM 53-10-15-2R-7 REPAIR 7 PARAGRAPH 4.B DUE TO STUB FRAME REPAIR. SEE TTG8Q00VKGYW.<BR>SEE ISDR UIEA2024082800851Bear Strap · crackedFORWARD SERVICE DOOR CUTOUT AFT LOWER CORNER WITH THREE CRACK INDICATIONS AT RIGHT SIDE IN HOLE #5 ON THE SKIN AND BEAR STRAP, REPAIR IA W TASK CARD 6753A937, PART 2, STEP 8, SRM 53-10-01-2R-1.(<P>FORWARD SERVICE DOOR CUTOUT AFT LOWER CORNER WITH THREE CRACK ISDR UIEA2024082800850Skin · crackedFORWARD ENTRY DOOR CUTOUT AFT LOWER CORNER WITH A CRACK INDICATION AT LEFT SIDE IN HOLE #4 ON THE SKIN, TWO CRACK INDICATIONS AT LEFT SIDE IN HOLE #5 ON THE SKIN AND BEAR STRAP, REPAIR IAW TASK CARD 6753A937, PART 1, STEP 8, SRM 53-10-01-2R-1.(<P>FORWARD ENTRYSDR CALA2024090302359Skin · crackedEMP - RH HORI STAB LWR SEAL FAIRING 314CRX COVERED LWR SKIN PNL FND CRK AT STA1788 TRANSFER REF NON - ROUTINE WO.3604808. FUSELAGE STA 1725-1803 RH SKIN PANEL REPAIRED AS PER EC/RA 5380-01400 REV-. ATTACH FORM 44-0008 ITEM 1 TO 18 ACCOMPLISHED.SDR CALA2024090302340Skin · damagedDOUBLER REPAIR ON LOWER FUSELAGE LOCATED BETWEEN STA 500F TO 500G BETWEEN STR 28R AND 27R REQUIRES INSPECTION PER SRM 53-00-01-2R-3 REPAIR 3 TABLE 205. PER SRM 53-00-00-01-2R-3 REPAIR 3, DETAILED VISUAL) TABLE 205. REQUEST DIP FOR INSPECTION REQUIREMENTS FOR SDR DALA2024090308633Doubler · corrodedCORROSION ON DOUBLER PRODUCTION OF MASTER DRAIN BTW STA Y=199 AND Y=218, L28R, AND L29R. ALSO STA Y=163, Y= 183 BTW L29L AND L30 AT E/E COMPARTMENT. SUMMARY OF NRC 00295: CORROSION LEVEL 2. PRODUCTION DOUBLER OF MASTER DRAIN BTW STA Y=199 AND Y=218 L28R AND L2SDR CALA2024083002336Skin · damagedR/H #1 FLIGHT DECK WINDOW POST CUT IN INCORRECT SPOT, ONE FASTENER (1") LOWER THAN SHOWN REF EA 5310-04554 OP 8 FIGURE 6 SHT 4. BLOCK 29 STEP (14).(C) PERFORMED CUT OF R/H #1 WINDOW POST, HFEC''D, FABRICATED REPAIR PIECES, TREATED, PRIMED, INSTALLED AND PAINTESDR DALA2024083008580Skin · dentedSHIP 3320 STRINGER DAMAGE FOUND BELOW SKIN DENT FWD OF L2 DOOR AT FR30, STR 27L. CORRECTIVE ACTION: COMPLIED WITH ER/A 620502-14 PRI REV 0 AND PRI REV 1 AND FINAL ER/A 620502-14 REV ORIGINAL. (0529200)SDR DALA2024083008579Skin · dentedSHIP 3320 DENT FWD OF L2 DOOR AT FR30 STA 27L. CORRECTIVE ACTION: REPAIRED PER SRM A330 53-21-11-300-16 AND ERA 620502-14 REV ORIGINAL (5869499)SDR SWAA2024100732120Access Panel · elongatedELONGATED HOLE ACCESS PANEL 193CL BODY FAIRING AT FUSELAGE EXTERIOR 2024-533598<[01] TOOL USED:CALIPER PN: 500-197-30 SN:A18229508; DUE DATE: 14-JAN-25;[02] TOOL USED HOT BONDER P/N HCS9200B-AV S/N 18196127 <BR>DUE DATE: 25/JAN/25;[03] TOOL USED: SCALE P/N: CRSDR CALA2024083000514Tripler · damagedFUSELAGE CRACK AT AFT LAV VENT ON LEFT SIDE OF AIRCRAFT.REF SRM 53-70-01-2R-3 REPAIR 3, STEP 4 D, REMOVED DAMAGE. MEASURES 2.3 FROM CENTER TO BOTTOM AMD 1.8 WIDE. PREVIOUSE ENTRY SHOULD INCLUDE, REQUIRES HFEC REF STEP E OF SRM,PER 737 NDT PART 6, 51-00-00 PRSDR CALA2024083000512Skin · gougedGOUGES ON THE FUSELAGE SKIN BETWEEN STA1197+231/STA1197+253 AND S-24R/S26RSDR DALA2024083008578Skin · dentedSHIP 3320 DENT FWD OF L2 DOOR AT FR30 STG 27L. CORRECTIVE ACTION: REPAIRED PER A330 SRM 53-21-11-300-16. (0528395)SDR 2024FA0000668Skin · corrodedREPAIRED 54 AREAS OF CORROSION ON THE DROP AISLE FUSELAGE SKIN AND STRINGERS BETWEEN FUSELAGE STATION 175 THRU 355. PERFORMED AN EDDY CURRENT AND ULTRASONIC THICKNESS INSPECTION OF THE BLENDED AREAS. CLEANED, TREATED AND PRIMED AREAS FOUND ACCEPTABLE. FABRICATSDR 2024FA0000666Skin · corrodedMECHANICALLY BLENDED LH FUSELAGE PSE SKIN CORROSION LOCATED AROUND LH FWD CABIN WINDOW WITH 1 AREA OF CORROSION, 2ND CABIN WINDOW WITH 1 AREA OF CORROSION, 3RD CABIN WINDOW WITH 5 AREAS OF CORROSION, 4TH CABIN WINDOW WITH 3 AREAS OF CORROSION AND 5TH WINDOW WISDR VNAA20251005022Skin · damagedPREVIOUS REWORK (3EA) BTW STGR 17R TO 16R AND FS 656, FS 661+17, FS 661+46 AT EXTERNAL FUSELAGE WERE REPLACED PER CRJ-900 SRM 53-00-00-201-003-A03 AND REPAIRED PER CRJ 900 SRM 53-00-01-201-001-A03.SDR VNAA20251005021Skin · damagedPREVIOUS REWORK (3EA) BTW STGR 19R TO 17R AND FS 581, FS 603, FS 635 AT EXTERNAL FUSELAGE. PREVIOUS REWORK (3EA) BTW STGR 19R TO 17R AND FS 581, FS 603, FS 635 AT EXTERNAL FUSELAGE WERE REPLACED PER CRJ-900 SRM 53-00-00-201-003-A03 AND REPAIRED PER CRJ 900 SSDR VNAA20251005020Skin · damagedPREVIOUS REWORK (3EA) BTW STGR 20R TO 18R AND FS 385, FS 427, FS 453 AT EXTERNAL FUSELAGE. PREVIOUS REWORK (2EA) BTW STGR 20R TO 18R AND FS 385 AND FS 427 AT EXTERNAL FUSELAGE WERE REPAIRED PER REO 690-53-21-2018 REV - - AND FASTENER (1 EA) BTW STGR 20R TO SDR VNAA20251005019Skin · damagedPREVIOUS REWORK (2EA) BTW STGR 22L TO 20L AND FS 596, FS 606 AT EXTERNAL FUSELAGE. PREVIOUS REWORK (2EA) BTW STGR 22L TO 20L AND FS 596, FS 606 AT EXTERNAL FUSELAGE WERE EVALUATED PER CRJ900 SRM 53-31-01-101-003-A04 AND REPAIRED PER REO 690-53-31-1071 REV.-.SDR VNAA20251005018Skin · damagedPREVIOUS REWORK (4EA) BTW STGR 18L TO 17L AND FS 517, FS 563. FS 575, FS 638 AT EXTERNAL FUSELAGE. FASTENERS (2 EAS) BTW STGR 18L TO 17L AND FS 563. FS 575 AT EXTERNAL FUSELAGE WERE REPLACED PER CRJ900 SRM 53-00-00-201-003-A03, PREVIOUS REWORK BTW STGR 18L TOSDR VNAA20251005017Skin · damagedREVIUS REWORK (2EA) BTW STGR 19L TO 17L AND FS 477.40 AT FWD FUSELAGE. PREVIUS REWORK (2EA) BTW STGR 19L TO 17L AND FS 477.40 AT FWD FUSELAGE WERE REPAIRED PER REO 690-53-00-636 REV - -SDR VNAA20251005016Skin · damagedPREVIOUS REWORK (2EA) BTW STGR 21L TO 20L AND FS 280 TO FS 326 AT FWD FUSELAGE. REWORK BTW STGR 21L TO 20L AND FS 326 AT FWD FUSELAGE WAS REPAIRED PER REO 690-53-21-2030REV - - AND REWORK BTW STGR 21L TO 20L AND FS 326 AT FWD FUSELAGE WAS REPAIRED WITH NRC SDR VNAA20251005015Skin · damagedPREVIOUS REWORK (1EA) IN STGR 23L AND FS 211 AT FWD FUSELAGE. LIGHTNING STRIKE DAMAGE TO FUSELAGE SKIN BTW FS202.75 - FS280.00 AND BTW STR20L-STR23L WERE REPAIRED PER REO 670-53-11-2059 REV - -SDR VNAA20251004024Skin · damagedPREVIOUS REWORK (3EA) BTW STGR 17R TO 16R AND FS 656, FS 661+17, FS 661+46 AT EXTERNAL FUSELAGE. PREVIOUS REWORK (3EA) BTW STGR 17R TO 16R AND FS 656, FS 661+17, FS 661+46 AT EXTERNAL FUSELAGE WERE REPLACED PER SRM 53-00-00-201-003-A03 AND REPAIRED PER SRM 5SDR VNAA20251004023Skin · damagedDISCREPANCY; PREVIOUS REWORK (3EA) BTW STGR 19R TO 17R AND FS 581, FS 603, FS 635 AT EXTERNAL FUSELAGE . PREVIOUS REWORK (3EA) BTW STGR 19R TO 17R AND FS 581, FS 603, FS 635 AT EXTERNAL FUSELAGE WERE REPLACED PER SRM 53-00-00-201-003-A03 AND REPAIRED PER SRM
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