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 LR7A2019062841579Skin · crackedDURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND FORWARD FUSELAGE RH SKIN WITH REDUNDANT HOLE AT FS235, WL206, RBL85. / REPAIRED IAW LOCKHEED SMP583 SRM, FIG. 51-140-10. NR# 2902.SDR LR7A2019062841562Skin · warpedDURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5321, FOUND LH AFT FUSELAGE EXTERIOR SKIN WARPED AT FS869, WL180 TO WL230, A DENT AT FS902 WL178, AND REPAIR DOUBLER AT WL182. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 2SDR LR7A2019062841560Skin · warpedDURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5321, FOUND LH AFT FUSELAGE EXTERIOR SKIN WARPED AT FS737 TO FS770, WL170 TO WL230, AND LBL85. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70.SDR LR7A2019062841558Skin · damagedDURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5321, FOUND RH AFT FUSELAGE RIVET MISSING WITH MULTIPLE REPAIR DOUBLERS AT FS889 TO FS902, WL180 TO WL230, AND RBL85. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583 SRM, CH. 51-60 & 51-70.SDR LR7A2019062841557Skin · warpedDURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5321, FOUND RH FUSELAGE SKIN WARPED AT FS337 TO FS377, WL140 TO WL250, AND RBL85. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70.SDR LR7A2019062841556Skin · wrinkledDURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5321, FOUND BOTTOM LH MAIN WHEEL WELL FAIRING WRINKLED, AND CRACKED WITH MULTIPLE REPAIR AT FS491 TO FS617, WL135, AND LBL45 TO LBL85. / REPAIRED IAW LAC MEA 382-53-06-097.SDR LR7A2019062401555Skin · warpedDURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5321, FOUND BELLY SKIN WARPED AT FS537 TO FS577, LBL60 TO RBL60, AND WL126. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70.SDR LR7A2019062841552Skin · warpedDURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5321, FOUND LH FUSELAGE EXTERIOR SKIN AT FS777.0E TO FS 817.0E, WL140 TO WL 236, AND LBL85 WARPED. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70.SDR LR7A2019062841551Skin · warpedDURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5321, FOUND LH FUSELAGE EXTERIOR SKIN FS657 TO FS697, WL140 TO WL250, AND LBL85 WARPED WITH TEMPORARY REPAIR. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70.SDR LR7A2019062841550Skin · warpedDURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5321, FOUND RH FUSELAGE EXTERIOR SKIN AT FS657 TO FS697, WL140 TO WL240, AND RBL85 WARPED WITH TEMPORARY REPAIR AT WL200. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70.SDR LR7A2019062841549Skin · warpedDURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5321, FOUND RH FUSELAGE EXTERIOR SKIN WARPED AT FS777.0E TO FS817.0E, AND WL140 TO WL236, RBL85. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70.SDR LR7A2019062841540Skin · crackedDURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5321, FOUND THE LH FWD FUSELAGE EXTERIOR SKIN CRACKED AT FS160, WL236, LBL65. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 2097. / PSE# 53-30-08, AD 2012-06-09SDR LR7A2019062841536Skin · corrodedDURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5321, FOUND THE FUSELAGE LOWER SKIN CORRODED AND WITH LOOSE RIVETS; FS180-196, LBL61-RBL61. REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70.SDR AALA2019062859001Skin · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION FORWARD CARGO COMPARTMENT INTERNAL SURFACE SKIN BETWEEN FR 35 AND FR 35.2 AT S41R. REPAIRED SKIN PER EA 504103A.SDR DALA2019062503831Skin · damagedFUSELAGE SKIN DAMAGE AT BS 180. REPAIRED THE SKIN IAW SRM 53-04-3.SDR DALA2019062503828Skin · corrodedCORROSION ON LOWER SKIN OF STA Y=851 AND STRINGER 30. CORROSION ON LOWER SKIN OF STA Y=851 AND STRINGER 30 WAS REPAIRED PER B-717-200 SRM 53-20-70-2R-1 FIG .201.SDR IPXA2019062443637Skin · dentedFUSELAGE SKIN DENT REPAIR AT BS 620, STRINGERS 27L TO 28L REPAIRED IAW EO B767-5330-69067-B.SDR IPXA2019062443682Skin · dentedSKIN DENTED AND GOUGED AT FRAMES 79 - 80, STRINGERS 55-56R. ACCOMPLISHED DOUBLER REPAIR PER EO A300-5330-72931B.SDR SWAA2022051144868Skin · buckledREF LP 1138480 - FGUESLAGE SKIN REPAIR FROM BS 727H - 727J AND BETWEEN STR23L-25L. REPAIR-53EA-07003 ( MX NOTE ) / REF NR X979661; R/R LEFTHAND SKIN PANEL 146A3201-32 ATAG # ZP0119 IAW SRM 51-40-05-0G-1; SRM 51-40-02-06-0 AND DRWG 146A3200 REV ASDR ASOA201906257060Skin · crackedR/H UPPER FUSELAGE SKIN CRACKED AT FRAME 75. REPAIRED AREA BY CUTTING OUT DAMAGE, FABRICATED AND INSTALLED FILLER, DOUBLER, SHIM AND REPAIR ANGLE, SEALED, ALODINED, PRIMED AND PAINTED. AIRCRAFT STILL IN C CHECK.SDR DALA2019062533817Skin · corrodedCORROSION ON UPPER SKIN STA Y=717 X=-19 AND Z-10 AT WING BOX. NRC 00483: CORROSION LEVEL 2, CORROSION WAS REPAIRED PER ER/A 579114-14 REV. ORIGINAL: SECTION I.SDR DALA2019062533816Skin · corrodedCORROSION ON UPPER SKIN STA Y=708 X=-24 AND Z-10 AT WING BOX. NRC 00482: CORROSION LEVEL 2, CORROSION WAS REPAIRED PER ER/A 579114-14 REV. ORIGINAL: SECTION I.SDR DALA2019062533812Skin · corrodedCORROSION ON UPPER SKIN FROM STA Y=715 TO Y=737 BTW X=44 TO X=60 AND Z=-10 AT WING BOX. NRC 00481: CORROSION LEVEL 2, CORROSION WAS REPAIRED PER ER/A 579113-14 REV. ORIGINAL: SECTION I. ASSOCIATED ER/A 14-579113.SDR DALA2019062433791Skin · damagedCRACK AT FUSELAGE SKIN STA 1022 BETWEEN LONG. 13/14R. FUSELAGE SKIN STA 1022 BETWEEN LONG. 13/14RH (FUS) WAS REPAIRED PER ERA/A 579005-14 REV. ORIGINAL, SECTION I PERMANENT REPAIR AND ETI-17-19-077 REV. 3.SDR SWAA2022031040651Skin · dentedDENT OUT OF LIMITS AT STA 769 BETWEEN STRNGERS 14 AND 15 L/H / REPAIRED DENT DAMAGED ON FUSELAGE SKIN AT STA: 769; BETWEEN S-14L AND 15L PER REF: SOUTHWEST E.A. NO. 1-753-35199 REV. IR; BOEING SR:4-4532083192.SDR CA190625026Doubler · corroded(CAN) CORROSION DAMAGE NOTED ON WASTE ACCESS DOUBLER OPERATOR REPORTED CORROSION DAMAGE ON REAR BARREL BOTTOM SKIN, WASTE ACCESS DOUBLER PIN C01342310-103 REF. CORROSION WAS BLENDED AND MINIMUM REMAINING DIMENSIONS ARE SHOWN IN FIGURE 1. AS REPORTED BY SAMCOSDR CA190621011Skin · corroded(CAN) THE CUSTOMER REPORTED MULTIPLE LOCATIONS OF BLENDED CORROSION (MIN. REMAINING THK OF 0.055`) ON FUSELAGE LH & RH SKIN PANELS (P/N 601R38321) AND LOWER FUSELAGE SKIN (P/N 601R38323) BETWEEN FS409.00+64 & FS409.00+128 AND BETWEEN STR 17L & STR 17R. (TC# 20SDR GTIA2019062413431Skin · crackedCRACK FOUND AT APU AIR INTAKE HOUSING LH AND RH. DAMAGE LENGTH #1, 1.0 IN. #2, 1.0 IN. DAMAGE WIDTH #1, 1.0 INCHES, #2, 1.5 INCHES. CAT A. -REVIEWED LTPRNRI 5000896730-0010 AND HAS BEEN ACCOMPLISHED.PERMANENT REPAIR HAS BEEN ACCOMPLISHED ON APU AIR INTAKE HOUSSDR IPXA2019071144318Skin · dentedINSPECTION TYPE:4C LT SIDE SKIN DENT AND GOUGED AT STA 330 REQUIRES PERMANENT REPAIR. REPAIRED DENTED & GOUGED LT FUSELAGE SKIN AT STA. 330 ABOVE Z=-2.900 IAW EA 011-5330-01-A7835 REV. IR AND EO MD11-5330-73199-A. (MAJOR)SDR HKGA201906260034Skin · gougedSKIN GOUGED BETWEEN FRAMES 39-40, STRINGERS 18-19L. FABRICATED A DOUBLER AND FILLER SHIM AND APPLIED ALODINE AND EPOXY PRIMER TO DOUBLER AND SHIM PARTS IAW SRM 50-00-01 REV 58. APPLIED EDGE SEAL AND TOP COAT IAW SRM 51-22-00.SDR V0XR20190625AV1Skin · chafedLIGHT CHAFE INTO FUSELAGE SKIN JUST AFT OF FS 913 AT STRINGER 27 REPAIRED IAW REO 60-53-51-195SDR HKGA201906250007Skin · dentedREWORKED DENT IAW SRM 51-7400 REV 58. CONFIRMED AFFECTED AREA CRACK FREE IAW NDIM 51-00-03 REV 3. TREATED, PRIMED, AND APPLIED TOPCOAT IAW CPM 51-21-04 REV 10.SDR DALA2019062103700Finger Doubler · corrodedCORROSION ON FINGER DOUBLER FROM STA Y=943 TO 960 AND Y=1005 TO Y=1044 BELOW LH LONGERON AT AFT CARGO COMPARTMENT WAS FOUND OUT OF LIMITS. NRC 00691: CORROSION LEVEL 2, SECTION OF FINGER DOUBLERS STA Y=943 TO Y=960 AND Y=1005 TO Y=1044 BELOW LH LONGERON AT AFTSDR EE4Y2019062009071Skin · crackedFWD GALLEY DOOR UPPER HINGE AREA FOUND OPEN HOLES WITH CRACK INDICATION. THE DAMAGED AREA WAS REPAIRED PER INSTRUCTIONS PROVIDED BY DER DRAWING 19-010-1200 AND APPROVED UNDER FAA FOR 8110-3 PROVIDED BY DER.SDR FDEA201906191529Skin · dentedDENT ON FUSELAGE SKIN AT B/S 522, 1" BELOW STR 26L DENT MEASURED AND EVALUATED AND FOUND OUT OF LIMITS IAW SRM 53-00-01-1A, REV 127 FIG 101 DET III, CARRIED OUT REPAIR IAW EA #F-5330-T 347883 P1 .TITLE:FUSELAGE - PLATES & SKINS -DENT AT BSTA522,1" BELOW STR26SDR DALA201906213697Doubler · corrodedCORROSION ON DOUBLER STA 1053 OVER PROJECTION STG 30 ON LOWER BULHEAD AREA AT AFT CARGO COMPARTMENT. THE DOUBLER WAS REPLACED PER B717-200 SRM 51-41-05-0G AND SRM 53-20-08-0I- 2 FIG. 1.SDR RAIA2019062090001Skin · crackedAFT FUSELAGE EXTERIOR SKIN AT FRAME 78 & STR 5R HAVE SUSPECTED CRACK EXTENDING FROM RIVET- PERFORMED HFEL INSPECTION OF SUSPECTED CRACK. CRACK CONFIRMED AND APPROXIMATE LENGTH MARKED ON SKIN. CUT OUT DAMAGE ON AFT FUSELAGE SKIN AT FR 78. PERFORMED HFESDR DALA2019062003691Skin · cracked(LOG 1131376) DURING INSPECTION FOUND CRACKED SKIN CUT OUT EXTERNAL POWER AREA AT LOWER FUSELAGE. REPAIRED CUT-OUT EXTERNAL POWER AREA AT LOWER FUSELAGE AS PER B737-800 SRM 53-10-15 FIG 204 REPAIR 4.SDR DALA2023052504150Unknown · unknownTHIS ER/A 527176-14 INCORPORATES FAA FORM 8110-3. ACCOMPLISH SECTION II INSPECTION INSTRUCTIONS. THE SUBJECT ER/A IS NOW AT REV A. AT OR PRIOR TO 35,500 TOTAL AIRCRAFT FLIGHT CYCLES, AND REPETITIVELY THEREAFTER EVERY 4,000 FLIGHT CYCLES, ACCOMPLISH SECTION II SDR SWAA2022031047575Skin · corroded***CORROSION*** ON FUSELAGE SKIN; UNDER DORSAL FIN; AT B.S. 947-1007; LBL15; RBL15 / REMOVED DAMAGE ON FUSELAGE SKIN UNDER DORSAL FIN BS 947-1007 LBL 15 - RBL 15 AND REPAIRED PER ATS ER #19-03811 REV IR AND SWA EA #1-753-35198 REV IRSDR SWAA2022031040601Skin · dentedDENT AT FUSELEGE SKIN STA 1025.125 STR 15R AND 16R 5.1' WITH 3.3' DEPTH .158 W/Y=20.88 FOUND OUT OF LIMITS REF. 737-700 S.R.M 53-00-01-1A-1. / REPAIR DENT DAMAGED ON FUSELAGE SKIN AT STA: 1025.125; BETWEEN STRINGERS 15R AND 16R PER REF. SOUTHWEST E.A. NO: 1-75SDR CALA2019062210988Skin · corrodedCORROSION ON STRUCTURE BETWEEN FR12-FR13, STR41L-39L AFTER REMOVAL OF SURFACE CORRISION ON SKIN THE REMAINING THICKNESS FOUND TO BE NOMINAL .079" IAW A320 SRM 53-11-11-283-001, REMOVED FABRICATED AND REPLACED STR 39L BETWEEN FR12-13 AND THE FWD GUSSET AT FR13 SDR ASOA2019061964030Skin · corrodedDURING MX INSPECTION, CORROSION WAS DISCOVERED ON THE AFT EXTERNAL FUSELAGE SKIN COMING FROM UNDER THE AIRCRAFT DATA PLATE. MX CUT OUT THE DAMAGED AREA AND PERFORMED A FILLER/DOUBLER REPAIR, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICESDR R61A201906160616Access Panel · corrodedWHILE IN HEAVY CHECK - CORROSION WASTE SERVICE PANEL. REMOVED AND REPLACED WASTE SERVICE PANEL REF EMB 175 AMM 53-03-62SDR CA190618004Buttstrap · corroded(CAN) CIRCUMFERENTIAL JOINT BUTTSTRAP IS CORRODED BETWEEN STRINGERS 27CL AND 25R. (TC# 20190618004)SDR DALA2022020400739None · noneSHIP 5809 HIS ER/A 564381-14 INCORPORATES FAA FORM 8110-3. ACCOMPLISH SECTION II INSPECTION INSTRUCTIONS. THE SUBJECT ER/A IS NOW AT REV. C. CORRECTIVE ACTION: REF ERA 564381-14AD REV C. (1122743)SDR SWAA2022031032902Scuff Plate · corroded***CORROSION*** ON FORWARD SERVICE DOOR SCUFF PLATE SUPPORT AT B.S. 300-328; R.B.L. 61. W.L. 208.1. / REMOVED AND INSTALLED NEW F.WD. SERVICE DOOR SCUFF PLATE SUPPORT AT B.S. 300-328; R.B.L.61. W.L.208! ITEM #7530250 IAW SRM 53-10-15-01-2 SRM 53-10-15-1A-2; SRSDR CA190617022Skin · corroded(CAN) MULTIPLE CORROSION SPOTS ON FUSELAGE SKIN PANEL BETWEEN FS953-FS977 AND STR 20R-27. (TC# 20190617022)SDR ASAA2019061439686Skin · corrodedCORROSION FOUND AT LAP SPLICE JUST BELOW LAV WASTE VENT APPROX STA 909.5. GROUNDED - YES. REMOVED FASTENERS TO FACILITATE CORROSION REMOVAL. REMOVED AND BLENDED CORROSION AT LAP JOINT FROM STA 905.5 TO STA 915.5. LOWEST THICKNESS REMAINING IS .058". ACCOMP HFESDR IPXA201906143237Skin · dentedINSPECTION TYPE:SEG3REF DI D607396 LH FUSELAGE NOSE SECTION STA 215 WK 210 SKIN GOUGE.REPAIRED PER RCD 115825 UPS EO B757-5330-72671-A & VT MAE EA 757-5310-27-A2348 REV.
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