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 EE4Y2017082504162Skin · dentedDURING THE STRUCTURAL INSPECTION, IT WAS FOUND AT LH FWD UPPER FUSELAGE SKIN, FOUND DENTS ABOVE STRINGERS 16L AND 23 - 24.SDR EE4Y2017082504161Skin · dentedDURING THE STRUCTURAL INSPECTION, IT WAS FOUND AT LT FWD UPPER FUSELAGE SKIN, FOUND TWO DENTS LOCATED BETWEEN STRINGERS 18 - 19L, FRAMES 11 - 12.SDR DALA2017082500001Skin · crackedSKIN IS CRACKED AT LAP, BS 1087, LONGERON 14R. REPAIRED IAW ER/A 561280-14, REV ORIG.SDR C77A20170824001Skin · puncturedDURING A SERVICE CHECK WALK AROUND, A PUNCTURE WITH INSULATION MATERIAL EXPOSED WAS FOUND BELOW THE CAPTAIN DV WINDOW. THE PUNCTURE WAS LOCATED BETWEEN FRAMES 10 AND 11 AND JUST BELOW STRINGER 18L. REPAIRED IAW ETD2017-170-072268. MAJOR REPAIR.SDR WVER2017082424301Skin · damagedMULTIPLE DAMAGE ON LOWER FUSELAGE SKIN PANEL LOCATED BETWEEN BS 1031 - 1051, STRINGERS 21R AND 26R. DAMAGE CAUSED BY AIR CONDITIONING EXTERNAL CONNECTION COVER AND LANYARD STRIKING FUSELAGESDR DALA2019030601501Skin · crackedER/A 561324-14 SECT I ISSUED FOR CORROSION BETWEEN L-29R & L-30R. FOLLOW ON ACTION IS REQUIRED. 561324 SECT II DUE WITHIN 24MONTHS OR 6600 CYCLES, WHICHEVER OCCURS FIRST. DTA IS REQUIRED. ASSOCIATED ER/A 00-561324 ADDED FOR AC 9511. CHANGED INSP TASK. ER/A REVSDR DALA201808165101Skin · crackedFOUND A CRACK IN THE FUSELAGE SKIN AT BS 1087, LONGERON 14R. REPAIRED IAW ER/A 95-561280.SDR DALA2017082406354Skin · corrodedCORROSION IN BELLY SKIN BY THE LAV WASTE TANK VENT. COMPLIED WITH PRI 561324-14 REV 0 AND REPAIRED REF ER/A 561324-14 REV ORIG.SDR SWAA2022020183333Skin · damagedSUPPLEMENTAL INFORMATION: TRANSFERRED FROM LOG PAGE 0026722: INSPECTION FOUND DAMAGE TO SKIN AROUND RIVET MEASURING 0.045' DEEP BY 1/16' BY 1/16' WIDE AT STA 727 S-7L / REPAIRED SKIN DAMAGE AT BS 727 STR 7L PER ER 17-03880 REV IR AND EA 1-753-31647 REV IRSDR IPXA2017091521745Cap · crackedINSPECTION TYPE: C3, LEFT UNDERWING BARREL CANTED PANEL CAP FOUND CRACKED AT BS 1236.8, RBL 92. REPAIRED THE PANEL CAP IAW EA 01-5310-01-A6953, REV I/R, AND EO MD11-5310-65691-A. MAJOR.SDR IPXA2017091521742Cap · crackedINSPECTION TYPE: C3, RT UNDERWING BARREL CANTED PANEL CAP AT BS 1236.8 IS CRACKED. REPAIRED THE PANEL CAP IAW EA 011-5310-01-A6952, REV I/R, AND EO MD11-5310-65684-A. MAJOR.SDR IPXA2017091421725Skin · gougedINSPECTION TYPE: 3C, EXTERIOR FUSELAGE SKIN IS GOUGED AT BS 1153, LONGERON 44L. REPAIRED THE SKIN IAW EA 011-5330-01-A6984, REV I/R, AND EO MD11-5330-65670-A. MAJOR.SDR IPXA2017091421724Skin · gougedINSPECTION TYPE: 3C, EXTERIOR FUSELAGE SKIN GOUGED, RT SIDE BS 1153, LONGERON 44R. REPAIRED IAW EA 011-5330-01-A6975, REV IR, AND EO MD11-5330-65671-A. MAJOR.SDR IPXA2017090721440Filler · chafedINSPECTION TYPE: 3C, TAILCONE RT INTERNAL DOUBLER SKIN FILLER CHAFED AT BS 2165, Z=61.5. REMOVED, FABRICATED, AND REPLACED THE TAILCONE DOUBLER SKIN FILLER IAW EO MD11-5330-59647-A.SDR SWAA2017082815947Skin · crackedEXTERNAL GROUND POWER RECEPTACLE DOOR CUTOUT CRACKED AT AFT SIDE BELOW LATCH LANDING. REPAIRED THE SKIN IAW SRM.SDR YENA201708210682Skin · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON EXTERNAL SKIN LOCATION FRAMEA 97 TO 98, STRINGERS 29L TO 29R ON LOWER FUSELAGE SKIN. PERFORMED A REPAIR IAW EA 53-0373-17 PART 1 AND EC E17-701-01.SDR DALA2017082206326Skin · dentedFUSELAGE SKIN HAS MULTIPLE DENTS BETWEEN STA 232 AND L-16L TO L-18L. REPAIRED FUSELAGE SKIN STA 229 TO 262 BETWEEN LONGERON 18LT TO 15LT IAW SRM 53-00-01 REPAIR 6. THIS IS A PERMANENT REPAIR.SDR F3LA2017082900197Splice Plate · corrodedTHE FORWARD CARGO SKIN SPLICE PLATE CORRODED AT FRAME 26, STRINGER 40 - 41R. REMOVED AND REPLACED THE PLATE IAW SRM 53-21-42-11, AND 53-21-11.SDR ASOA201708201869Skin · chafedFUSELAGE SKIN CHAFFED FS 96900-FS 985.00 STR 27. COMPLIED WITH EC TC REO 670-53-00-290 REV D DATED 09-10-2015 AS WRITTEN. PERFORMED UT THICKNESS INSPECTION IAW BSC NDT INSPECTION PROCEDURE 4.3, MIN MATERIAL REMAINING IS .091", ORIGINAL IS .188", REMOVED IS .0SDR ASOA201708201858Skin · corrodedMAIN AVIONICS DOOR SURROUND HAS CORRISION.. REMOVED AND REPLACED IAW MODSUM IS67053210097, EC/TC REO 670-53-21-242, AND REO 670-53-21-242.SDR AALA20170819004Skin · crackedCRACK ON FUSELAGE SKIN BETWEEN BS 37 AND 110, RIGHT NOSE LANDING GEAR ABOVE AFT STRUT DOOR HINGE BEYOND STOP DRILL. REPAIRED IAW SRM 53-05-00-001.SDR SWIA201743848Skin · dentedDENT BELOW THE CARGO DOOR BETWEEN BS 605 AND 621. REPAIRED THE SKIN IAW REO, PRESSURE CHECKED GOOD.SDR COEA2017081804919Skin · corrodedCORROSION AROUND AND ADJACENT TO FASTENERS ON THE RT LOWER SKIN SURFACE BETWEEN FRAMES 25 & 26. REPAIRED IAW ES-3861/17.SDR IPXA2017091221626Skin · gougedINSPECTION TYPE: 3C, FUSELAGE SKIN AT BS 1781 - 1787, LONGERONS 39 - 42R GOUGED. REPAIRED THE SKIN IAW EA 011-5330-01-A6973, REV I/R, AND EO MD11-5330-65632-A.SDR SIMA20170818002Skin · crackedRT AFT FUSELAGE FR 75 BELOW STR 2R SKIN CRACKED AT FASTENER HOLE. REPAIRED CRACKED AREA ON RT AFT FUSELAGE FR 75 BELOW STR 2R SKIN AT FASTENER HOLE IAW SRM 53-31-01 ITEM 11 FIG 219.SDR EE4Y2017082204077Skin · canningDURING THE STRUCTURAL INSPECTION OF THE UPPER REAR FUSELAGE IT WAS FOUND THE FUSELAGE SKIN WITH AN OIL CAN AT BS 1006 3 INCH BELOW STRG 16L. THE AFFECTED SKIN AREA HAS BEEN REPAIRED IAW SRM 53-80-01, REPAIR 6.SDR ABXR2017081800009Skin · corrodedSKIN CRACK AT BS 544 - 566 STRINGERS 37 - 38L. REPAIRED IAW REA4728REA01SDR ABXR201708180001Skin · corrodedFUSELAGE SKIN AT BS 1260 ABOVE STRINGER 31 HAS CORRODED HOLE IN SKIN. REPAIRED IAW REA 47284REA02 REVA ,767 SRM 51-40-02, 51-40-05.SDR 2017F00197Skin · corrodedFUSELAGE SKIN CORRODED.SDR 2017F00196Skin · corrodedFUSELAGE AND TAILCONE SKIN CORRODED REPAIRED IAW ENGINEERING DQ8835M1, REV A.SDR SWAA2017091816397Skin · corrodedFUSELAGE LOWER SKIN CORRODED AT BS 953, LBL 8.5. REPAIRED SKIN IAW ER AND EA.SDR SWIA201743718Doubler · corrodedCORROSION ON TCAS DOUBLER BETWEEN BS 295 - 310, STRINGERS 26R - 26L. REMOVED AND REPLACED THE TCAS ANTENNA DOUBLER IAW SRM. NO LEAKS NOTED.SDR SWIA201743716Skin · corrodedCORROSION ON INNER FUSELAGE SKIN BETWEEN BS 326.70 AND 2 INCHES OUTBD OF STRINGER 25R. CORROSION FOUND TO BE OUT OF LIMITS. CUT AWAY DAMAGE AND APPLIED REPAIR DOUBLER IAW REO.SDR AALA201708249034Finger Doubler · corrodedCORROSION ON FORWARD CARGO FINGER DOUBLER AT STRINGER 26R, BETWEEN FRAMES 24 AND 27. REPLACED THE FINGER DOUBLER IAW SRM 51-40-02.SDR CALA2017081802726Skin · wornWEAR ON EXTERIOR LT FUSELAGE SKIN AT VERTICAL STABILIZER TO FUSELAGE INTERFACE AREA BS 1582 TO 1605.5. INTERIM REPAIR ACCOMPLISHED IAW ECRA 5330-06139, PART 1, STEP 1.SDR CALA2017081802724Skin · damagedWEAR MARK ON EXTERIOR RT FUSELAGE SKIN AT VERTICAL STABILIZER TO FUSELAGE INTERFACE AREA BS 1582 - 1605.5. INTERIM REPAIR ACCOMPLISHED IAW ECRA 5330-06139, PART 1, STEP 1.SDR EPUA20170817001Skin · corrodedDURING SCHEDULED INSPECTION, DEFECTS WERE NOTED AT STRINGER 15R AT BS 355.75 FOUND TO BE DEBONDED FROM THE SKIN WITH CORROSION.SDR V0XD20170817001Skin · damagedRT SKIN DAMAGED AT FRAME STATION 202.00 AT 2 O'CLOCK POSITION. REMOVED AND REPLACED SKIN IAW REO 670-53-11-1311, DATED 2017-08-15, SRM 51-24-36, 51-40-11, 51-42-06 AND CRJ700 NDTM 51-20-006.SDR DALA2018122607416Skin · dented(LOG 3491444) FOUND ON ARRIVAL- SMALL DENT AFT OF L2 DOOR. DENT IS 30" AFT OF L2 DOOR STATION 1020. DAMAGE LOCATED ON EXTERNAL FUSELAJE SKIN AS STATION 1019.5 BETWEEN STRINGERS 14L AND 15L WAS REPAIRED PER B737-800 SRM 53-80-01 REPAIRSDR FDEA201708162286Skin · gougedFOUND GOUGED ON LOWER BELLY NEAR BS 1721, LONGERON 47L. REPAIRED THE SKIN IAW SRM 53-20-00, FIG 6.SDR FDEA201708162285Skin · crackedFOUND CRACK ON FUSELAGE JUST AFT OF CTR CARGO DOOR AROUND BS 1801 AND STRINGER 45L. REPAIRED THE SKIN IAW SRM 53-20-00, FIG 6.SDR AALA201708179017Skin · crackedCRACK INDICATIONS ON THE SKIN PANEL IN FASTENER HOLES AT FRAME 35 AND STRINGER 30R. REPAIRED THE SKIN IAW EA 272131.SDR DALA2017081606256Skin · damagedFUSELAGE SKIN UNDER VERTICAL STAB FWD FAIRING, THREE FASTENER HOLES DAMAGED BS 1118, RBL 4. REPAIRED IAW ER/A 560967-14AD, REV 0. AND ER/A 560967-14AD, REV ORIGINAL.SDR DALA2017081606255Skin · crackedSKIN CRACKED LEFT SIDE OF FUSELAGE JUST BELOW SKATE ANGLE OF VERTICAL LEADING EDGE. COMPLIED WITH ER/A 560998-14AD, REV A.SDR JR2R20170816050Skin · corrodedFUSELAGE SKIN IS CORRODED AT THE AFT LAVATORY SERVICE PANEL DOOR FWD LOWER CORNER. REPAIRED THE SKIN IAW EA 25-2017-085.SDR SWAA2022013085948Scuff Plate · crackedFWD CARGO BAY FWD CORNER THRESHOLD CRACKED. / FWD CARGO BAY FWD CORNER THRESHOLD REPAIRED PER SWA EA 1-A53-2076 REV 11SDR SWAA2022013085954Scuff Plate · corrodedCORROSION ON ASD MOPSILL INBD CHORD BS993 RBL60 WL 208 / REMOVED AND REPLACED ASD MOPSILL I.A.W BOEING DWG 147A8501 AND SRM 51-40-02-0G-0.SDR SWAA2022013019698None · corroded***CORROSION*** ON L/H MOPSILL; BS-302 TO BS-348; WL-207 / REMOVED AND REPLACED L/H FWD MOPSILL PER SRM 51-40-02 & DWG #141A8110SDR CALA2017081802720Skin · scratchedLOWER EMPENAGE SKIN BS 1788 - 1809 STRINGER 30 - 32L, FOUND SCRATCHED. REPAIRED IAW SRM 53 -00-01, REPAIR 6, FIG 201.SDR DALA2017081606291Skin · dentedFUSELAGE SKIN, BS 650 ABOVE STRINGER 26R LAP SPLICE DENTED.
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