JASC 5330
Service difficulty reports · 79,347
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 DALA2019102806213Skin · dentedSHIP 6716 FUSELAGE LEFT SKIN ON STATION 630 STRINGER S15.5 DENT. CORRECTIVE ACTION: PERMANENT REPAIR ON FUSELAGE SKIN STA 580 660 & S-14L-S-19L WAS PERFORMED PER ER/A 582486-14AD REV.ORG. (4891918)SDR DALA2019022601231Skin · debondedSHIP 682 DISBOND BETWEEN SKIN AND BEARSTRAP/DOUBLER AND TRIPLER REPAIR AT UPPER FORWARD CORNER OF THE L1 PAX DOOR. CORRECTIVE ACTION: REF ERA 569571-14AD REV ORIG. (0611022)SDR CALA2018070301538Skin · damagedFUSELAGE DAMAGE AT AFT CARGO DOOR CUTOUT, AT STA767-STA794 STR22R - STR26R. ALL REPAIRS ACCOMPLISHED IN ACCORDANCE WITH EC/RA 5300-06394. REPAIRED IN ACCORDANCE WITH EC/RA 5330-06394 TO STEP PART 1E7.SDR SWAA2018062523027Skin · crackedEXTERNAL POWER DOOR CUTOUT AFT LIP CRACKED. REPAIRED CUTOUT PER SRM.SDR DALA2018062204147Skin · corrodedLOWER FUSELAGE AFT OF AFT CARGO DOOR. FOUND CORROSION ON RIVETS AT ANTENNA DELETE PLATE BS 1510 BETWEEN STRINGERS 28 - 29. REMOVED THE ANTENNA BACKING DOUBLER AND DAMAGED SKIN IAW SRM 53-00-01. PERFORMED HFEC OF CUT-OUT IAW NDT PART 6 54-00-01, AND BOLT HOSDR JGVR20180621002Skin · corrodedREMOVED AIRCRAFT DATA TAG AND MECHANICALLY BLENDED CORROSION ON AIRCRAFT SKIN. PERFORMED EDDY CURRENT AND ULTRASONIC INSPECTIONS AND REPORTED RESULTS TO ENGINEERING FOR DISPOSITION. REPAIRED CORROSION BLENDS FOUND UNDERNEATH IAW MEMO BY TREATING AND PRIMING THSDR JGVR20180621001Skin · corrodedREMOVED AIRCRAFT DATA TAG AND MECHANICALLY BLENDED CORROSION ON AIRCRAFT SKIN. PERFORMED EDDY CURRENT AND ULTRASONIC INSPECTIONS AND REPORTED RESULTS TO ENGINEERING FOR DISPOSITION. REPAIRED CORROSION BLENDS FOUND UNDERNEATH IAWMEMO BY TREATING AND PRIMING THESDR IPXA2018062203907Skin · nickedBS 1440 AND BELOW STRINGER 24L TO 25L, AREA ON SKIN WAS NICKED. INSTALLED A DOUBLER REPAIR IAW SRM 53-00-01-2R-3, REPAIR 3.SDR CALA2018062201507Skin · crackedINTERNAL FUSELAGE SKIN AT FRAME 35, STRINGER 30R, HAD A CRACK INDICATION. ACCOMPLISHED A PERMANENT REPAIR IAW PART 3, ECRA 5331-02229.SDR DALA2018062104125Bear Strap · crackedHFEC INSPECTION OF THE L1 DOOR UPPER FORWARD CORNER SHOWS A CRACK IN THE BEAR STRAP LAYER, COMPLIED WITH A REPAIR IAW AMDS 5331-01232-02G, JOB 10 .SDR ASOA201807133039Skin · crackedDURING C CHECK INSPECTION EDDY CURRENT INSPECTION REVEALED A CRACK ON THE LT WINDSHIELD LATERAL POST FROM THE FORWARD UPPER FASTENER HOLE EXTENDING AFT TOWARD THE REAR UPPER HOLE. MAINTENANCE REPAIRED IAW SB145-53-0079.SDR SIMA20180619003Skin · crackedFUSELAGE AFT UPPER SKIN CRACKED JUST AFT OF FRAME 75 AND ABOVE STINGER 2L. INSTALLED REPAIR DOUBLER FILLER, DRAG ANGLE AND SHIM IAW SRM 53-31-01.SDR A6WA2018062245903Skin Panel · crackedLEFT HAND TRU DOOR LANDING SKIN PANEL CRACKED BY LATCH CUT OUT. STOPPED DRILLED CRACK IAW REO601R-53-11-2381 REV-.SDR SIMA2018062518006Skin · dentedFOUND A LARGE DENT BETWEEN STRINGERS 15L & 16L, FRAMES 19 & 20, FOUND TO BE OUT OF LIMITS IAW SRM 53-21-01. REPAIRED THE SKIN IAW ERS-EM-53MR-3325.SDR ABXA201806218071Skin · scratchedSCRATCH FOUND ON THE FUSELAGE SKIN AT BS 413, STRINGER 35L. THE SKIN WAS REPAIRED. THE AIRPLANE WAS GROUNDED.SDR ABXA201806218070Skin · dentedFUSELAGE SKIN NEAR BS 463.5, STRINGER 35L WAS DENTED. THE SKIN WAS REPAIRED. THE AIRPLANE WAS GROUNDED.SDR DALA2018062004112Skin · corrodedWHILE REMOVING THE NO LONGER USED AIR PHONE ANTENNA PER ER/A 12-090911-14MA, LINE MX. REPORTS CORROSION ON THE FUSELAGE SKIN OUTER SURFACE UNDER THE REMOVED ANTENNA. THE DAMAGED AREA IS LOCATED AT APPROX FS 757 MIDWAY BETWEEN STRINGERS 27L AND 27R. MAINTENANCESDR DALA2018061804102Skin · dentedDENT EXTERNAL SKIN LOC BTW FR 12 TO FR 13 AND 10" ABOVE UPPER SIDE STR RT ON LOWER FUSELAGE. PERFORMED PERMANENT REPAIR EXTERNAL SKIN LOC BTW FR 12 TO FR 13 AND 10" ABOVE UPPER SIDE STR RT ON LOWER FUSELAGE AS PER SRM 53-00-11-300-029.SDR FDEA201806181513Doubler · crackedEXISTING REPAIR DOUBLER ON FUSELAGE SKIN ABA 7057-1 AT STA 275 FOUND CRACK. CRACKED EXISTING REPAIR DOUBLER ON FUSELAGE SKIN ABA7075-1 AT STA 275 CARRIED OUT REPAIR AS PER EA 1-5330-T0310125 A PART 3, TITLE: FUSELAGE - PLATES & SKINS. FUSELAGE SKIN TRIMOUT REPSDR ASOA2018062716338Skin · crackedDURING A -C- CHECK, FOUND A CRACK ON THE SKIN AT FRAME 75, STRINGER 2R. MAINTENANCE REPAIRED THE SKIN IAW SRM 53-31-01.SDR SWAA2022021808138Doubler · corrodedFWD CARGO; INTERNAL ANTENNA DOUBLER HAS CORROSION ON UPPER SURFACE AND RH SIDE VERTICAL FLANG AT BL 0; STA 500+10 / FWD CARGO INTERNAL ANTENNA DOUBLER HAS CORROSION ON UPPER SURFACE AND RH SIDE VERT FLANG AT BL 0 STA 500+10 BLENDED CORROSION AND FOUND ORIG 'T'SDR SWAA2022021808139Doubler · corrodedFWD CARGO; INTERNAL ANTENNA DOUBLER HAS CORROSION ON UPPER SURFACE AND LH VERTICAL FLANGE AT BL0; STA 500A+14 / REMOVED AND REPLACED INTERNAL ANTENNA DOUBLER @ STA .500A+14 BLD PER DWG #143A3230; NO LIMITS FOUND IN SRMSDR ABXA201806215069Skin · dentedTHE FUSELAGE SKIN ADJACENT TO BS 632 FRAME, BETWEEN STRINGERS 24L AND 25L WAS DENTED. THE SKIN WAS REPAIRED. THE AIRPLANE WAS GROUNDED.SDR AALA201806185001Skin · corrodedCORROSION ON THE FUSELAGE SKIN INTERNAL SURFACE AROUND THE AFT LAVATORY PAN. REPAIRED THE SKIN IAW SRM 51-70-04, AND EA 281446.SDR C77A2018061850001Skin · gougedGOUGE DAMAGE ON THE FORWARD FUSELAGE AFT PLUG LOWER LEFT SKIN, FRAMES 21 - 22, STRINGERS 14L - 16L. ACCOMPLISHED A PERMANENT REPAIR IAW ETD2018-170-066244C.SDR DALA2018061604035Doubler · crackedINITIAL INSPECTION, CRACKED PRODUCTION DOUBLER ON FWD LAVATORY SERVICE PANEL. PRODUCTION DOUBLER ON FWD LAVATORY SERVICE PANEL WAS REPAIRED PER ER/A 569279-14 REV ORIGINAL SEC I AND ETI-88-18-060 REV 4.SDR DALA2018061504023Doubler · corrodedAWR, INITIAL INSPECTION: CORROSION ON PREVIOUS REPAIR DOUBLERS AND FILLER AT AFT LAVATORY SERVICE PANEL SUMMARY OF NRC 00108, CORROSION LEVEL II, TEMPORARY REPAIR ON AFT LAVATORY SERVICE PANEL WAS ACCOMPLISHED PER ER/A 508310-14 REV A SEC III AND ETI-88-18-061SDR SWAA2022021716082Scuff Plate · crackedAFT CARGO BAY FWD CARGO SCUFF PLATE IS CRACKED / REPAIRED AFT CARGO BAY - FWD SCUFF PLATE IAW EA 1-A53-2076 REV 11SDR SWAA2022021756359Scuff Plate · crackedAFT CARGO AFT CORNER DOOR SCUFF PLATE CRACKED / REMOVED AFT CARGO AFT CORNER DOOR SCUFF PALTE AND INSTALLED NEW CORNER DOOR SCUFF PLATE P.O.#683933 ITEM #7530337 I.A.W. AMM 53-11-02-420-801 80664U 06/19/18 LOCATED AND DRILLED NEW SCUFF PLATE I.A.W. SRM 51-40-0SDR SWAA2018072523789Skin · corrodedFUSELAGE SKIN CORRODED AT BS 400+3, STR 25L. REPAIRED SKIN IAW EA.SDR DALA2018061504021Skin · corrodedLT AFT FUSELAGE LAV SERVICE ACCESS DOOR LOWER CUTOUT IS CORRODED AT APPROX STA 1312. IN WORK REPAIR.SDR FDEA201806141487Skin · corrodedCORROSION ON BUTT JOINT AT B STA 440, BETWEEN STR 24-25 RT PERFORMED SKIN REPAIR AT BUTT JOINT AT BSTA 440, STR 24-25R IAW EA F-5330-T0340309. TITLE: FUSELAGE - PLATES & SKINS - FUSE SKIN CORROSION AT BSTA 440 STR 24-25R.SDR C77A2018061400001Doubler · corrodedDURING A CHECK, INSPECTION DISCOVERED CORROSION ON THE WASTE BOX SKIN DOUBLER, FRAME 88 EDGE OF THE DOUBLER. THE THREE AREAS OF CORROSION WAS BLENDED AND THE DEEPEST POST BLEND-OUT AREA MEASURED APPROXIMATELY 1.23 INCHES X 0.98 INCH WITH A MAXIMUM DEPTH OF SDR SWAA2022021716066Skin · corroded***CORROSION*** (FCB) CORROSION AROUND FASTENER HOLES; FUSELAGE SKIN WHERE SCUFF PLATE ATTACHES B.S. 440-492.4. / REPAIRED FUSELAGE SKIN SCUFF PLATE ATTACH POINTS B.S 440 - 492.4 IAW EA 1-753-32899 REV IR AND ER 18-03111 REV IRSDR SWAA2022021723350Scuff Plate · crackedFSD THRESHOLD CRACKED AT AFT CORNER / REPAIRED FSD THRESHOLD IAW EA 1-A53-2076 REV 11SDR SWAA2022021623331Floor Panel · corroded***CORROSION*** FCB FLOOR PANEL 120BF EDGE HAS SURFACE CORROSION. / REPLACED FCB FLOOR PANEL 120 BF WITH NEW PANEL FABRICATED FROM 2024 T3 # 0.71 LOT # 1347031-3 PER DWG 453A1610 AND APPLIED CHEMICAL CONVERSION COATING AND PRIMER PER SOPM 20-43-03 AND AMM 51-2SDR SWAA2018072523785Skin · corrodedFUSELAGE SKIN CORRODED AT BS 360+2, STR 25L. REPAIRED SKIN IAW EA.SDR SWAA2018072523784Skin · corrodedFUSELAGE SKIN CORRODED AT BS 360+10, STR 23L. REPAIRED SKIN IAW EA.SDR ASOA201807133040Skin · wornDURING C CHECK INSPECTION FOUND INNER SKIN OF THE MAIN DOOR AT COCKPIT PARTION UPPER HOLE WORN. MAINTENANCE REPAIRED IAW SRM 53-21-02.SDR SWAA2018071223444Doubler · corrodedEXHAUST DUCT INTERNAL DOUBLER CORRODED AT BS 360+ 6, BETWEEN STR 28L TO STR 28R. R&R DOUBLER IAW DWG.SDR SWAA2018070223217Doubler · corrodedAUXILIARY POWER UNIT INLET CUTOUT UPPER DOUBLER CORRODED AT BS 1088. R&R DOUBLER PER SRM AND DWG.SDR SWIA2018062244806Skin · dentedFUSELAGE SKIN, AFT OF BS 589, BETWEEN STRINGERS 21 AND 22L. INWARD DENT. REPAIRED THE FUSELAGE SKIN IAW REO.SDR SWAA2018072523782Skin · corrodedFUSELAGE SKIN CORRODED AT BS 360+2, STR 26L. REPAIRED SKIN IAW SRM AND EA.SDR SWAA2018062823149Skin · chafedUPPER EXTERIOR SKIN HAS CHAFED AT BS 851, BL 0. REPAIRED SKIN IAW EA.SDR SIMA20180612005Skin · canningRT CENTRAL FUSELAGE I LOWER SKIN DENTS PERMANENT REPAIR ERS-EM-53DF-2832 PTC. ERS-EM-53DF-2832 WAS NO LONGER REQUIRED DUE TO OIL CANNING. ACCOMPLISHED PERMANENT REPAIR IAW ERS-EM-53MR-3304.SDR DALA2018061303984Doubler · corrodedCORROSION ON INTERNAL SKIN DOUBLER AT STA 1540 BETWEEN STR 30 AND 29RT. REMOVED CORROSION AND CHECKED LIMITS PER SRM 53-00-01. FOUND TO BE IN LIMITS. OK TO TREAT AND PAINT TREATED AND PAINTED PER SRM 53-00-01.SDR V0XD20180613005Skin · gougedAFT LOWER FUSELAGE BETWEEN FS 969.00 AND 977.00 THERE ARE MULTIPLE GOUGES. REMOVED DAMAGE FABRICATED AND INSTALLED REPAIR PARTS IAW REO 670-53-00-547 DATED 2018-06-11, AND F670-53-00-547(P1) DATED 2018-06-05.SDR 2A6R201806124782Skin · dentedDURING INSPECTION, FOUND A DENT ON THE LEFT FUSELAGE SKIN PANEL.SDR AALA201806129002Skin · crackedSKIN FOUND CRACKED AT FRAME 68, STRINGER 29L. REPAIRED THE SKIN IAW SRM 53-41-11-300-018, AND EA 281417.SDR 2A6R201806124781Skin · chafedDURING INSPECTION FOUND THE RIGHT UPPER BACK COWLING CHAFED ALMOST COMPLETELY THRU.
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