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 IPXA2017070719043Skin · corrodedINSPECTION TYPE: 3C, UPPER SKIN HAS CORROSION AT STRINGER 15. REPAIRED THE SKIN IAW EA 011-5730-01-A6876, REV I/R, AND EO MD11-5730-64823-A.SDR SIMA20170321004Skin · crackedRT UPPER FUSELAGE SKIN CRACKED JUST AFT OF FRAME 75 AND ABOVE STRINGER 2R, CRACK IS APPROX 1/4" LONG. REPAIRED CRACK ON RT SIDE OF FUSELAGE AFT OF FR75 ABOVE STR 2R IAW SRM 53-31-01 ITEM 11.SDR SIMA20170321003Skin · crackedLT UPPER FUSELAGE SKIN CRACKED IN 2 PLACES, CRACK 1 IS JUST AFT OF FRAME 75 AND ABOVE STRINGER 2L, CRACK IS APPROX 1/2" LONG, CRACK 2 IS AT THE FIRST FASTENER BELOW STRINGER 2L ON FRAME 75, ALL CRACK ENDS ARE MARKED. REPAIRED LT FUSELAGE CRACK JUST AFT FR 75 ASDR DALA2017032202343Skin · dentedDENT ON EXTERNAL SKIN AT BS1600 AND BTW STR 29L AND STR 30 ON LOWER FUSELAGE. PERFORMED PERMANENT REPAIR AT BS 1600 AND BTW STR30 ON LOWER FUSELAGE AS PER SRM 53-00-01 REPAIR 3 FIG 201.SDR UIEA2017032200381Skin · corrodedSKIN CORROED AT BS 1350, LBL 9. ACCOMPLISHED EI T2017A53M-445, REV 2.SDR UIEA2017032200382Skin · corrodedCORRODED SKIN AT BS 1350, RBL 9. ACCOMPLISHED EI T2017A53M-445, REV 2.SDR DALA2017032202284Skin · crackedBS 1087 ABOVE LONGERON 14L FUSELAGE SKIN CRACKED. HFEC VERIFIED IAW NDT SPM 06-10-01.001 ETHF PROCEDURE 1. REPAIRED IAW ERA 555590-14 REV 0.SDR IXXA20170412221Skin · corrodedAFT LOWER CARGO FUSELAGE SKIN CORRODED AT BS 1197 - 1219, STRINGER 33 - 35R. TWO AREAS BLENDED OUT OF LIMITS. CUT OUT DAMAGED AREAS, FABRICATED AND INSTALLED DOUBLER, TRIPLER, AND TWO FILLERS IAW SRM 53-00-01, FIGURE 201, REPAIR 14.SDR DALA2017032102272Skin · crackedCRACK ON FUSELAGE SKIN AT FRAME 1494 BETWEEN STRINGERS 3 & 4 LEFT SIDE OF VERTICAL STABILIZER. COMPLIED WITH ERA 556786-14 REV O.SDR DALA2017032102271Skin · crackedCRACK ON FUSELAGE SKIN AT FRAME 1494 BETWEEN STRINGERS 3 & 4 ON RIGHT SIDE OF VERTICAL STABILIZER. COMPLIED WITH ERA 556787-14 REV O.SDR ASOA201703201351Strap · corrodedCIRCUMFERENTIAL STRAP INTERNAL SKIN CORRODED BTW STGRS 25R-26L FS 280.00. COMPLIED WITH EA 32-2017-066 AND EC/TC EA 32-2017-066. REPAIR OF STRAP FS 280.00 BTW STR 25R-26L.SDR ASOA201703203044Skin · crackedCRACK FOUND ON SKIN FRAME 75, STRINGER 2L. REPAIRED IAW SRM 53-31-01, FIG 219, SHT 1.SDR F3LA2017041300098Skin · dentedEXTERIOR FUSELAGE SKIN DENTED AT FRAME 23 + 15" STRINGER 24L. CUT OUT DAMAGE AREA, FABRICATED AND INSTALLED A DOUBLER REPAIR IAW SRM 53-11-11, AND 53-00-00-11-300-042.SDR F3LA2017041300097Skin · dentedFUSELAGE DENTED BETWEEN STRINGERS 16 AND 17L, FRAMES 78 AND 79. DENT FOUND TO BE OUT OF LIMITS IAW SRM 53-11-283-009, FIGURE 1 DIAGRAM 1, REPAIRED IAW SRM 53-51-11-300-002.SDR SIMA20170319003Skin · crackedLT REAR FUSELAGE SKIN CRACK JUST AFT OF FRAME 75, ABOVE STRINGER 2L. PERFORMED PERMANENT REPAIR OF LT REAR FUSELAGE SKIN JUST AFT OF FRAME 75 ABOVE STRINGER 2L IAW SRM 53-31-01.SDR DALA2017031902199Skin · crackedSKIN PANEL CRACKED BS 1041, 1022, 984, 946, AND BS 886. DAMAGED AREAS WERE REPAIRED IAW SRM 53-05 FIG. 122.SDR 7C7A2017031800298Skin Panel · dentedREPAIR FOR DENT, SCRATCH DAMAGE TO EXTERIOR LOWER FUSELAGE SKIN. REPAIRED IAW RD8-53-15090, RD8-53-15104, RD8-53-15115 AND ECO008.53-17.11SDR AALA20170320010Skin · corrodedAIRCRAFT WAS GROUNDED. DURING WALK AROUND, FOUND SMALL AREA OF DEFORMATION/BULGE MEASURING 1.5 INCH AT FUSELAGE STATION 440 BETWEEN STRINGERS 33L AND 34L. REPAIRED IAW SRM 53-00-01-2R-1 AND SRM 53-30-03-2R-1.SDR DALA2017032002220Skin · dentedFOUND GOUGE AND DENT BETWEEN WINDOWS 15 AND 16 RT SIDE ON CROWN BETWEEN S-1R AND S-2R. REF NRC 001 AND ERA 556793-14 REV ORIG FOR REPAIR INSTRUCTIONS.SDR DALA2017031802182Skin · dentedDENT SKIN BTW FR 80 AND FR 81 STR 1R TO STR 2R AT RUDDER AREA ON UPPER FUSELAGE.SDR DALA2017031802181Skin · dentedDENT SKIN AT FR 79 BTW STR 4L AND STR 5L APPROX ON UPPER FUSELAGE, PERMANENT REPAIR ON THIS AREA AS PER SRM 53-51-11 FIG 20102 PAG 8.SDR CALA2017031700615Skin · crackedCRACK DETECTED IN SKIN AROUND FASTENER BS 540 BETWEEN STRINGERS 22 AND 23L. REPAIRED IAW EA 5310-05878, REV.D.SDR GTIA2017031701826Skin · dentedFOUND A DENTED SKIN PANEL FRAMES 23 - 24, STRINGERS 24-25L. REPAIRED IAW EO 5311-1716.SDR IPXA2017040715907Skin · corrodedINSPECTION TYPE: 3C, AFT FUSELAGE RIGHT SIDE EXTERIOR SKIN AND EXISTING REPAIR DOUBLER CORRODED BS 2107 - 2164, LONGERON 33 - 35R. REPAIRED IAW EA 011-5330-01-A6733, REV IR, AND EO MD11-5330-63842-A. (MAJOR)SDR IPXA2017032915662Skin · corrodedINSPECTION TYPE: 3C, UPPER SKIN HAS CORROSION AT BS 1219, STRINGER 15L. REPAIRED THE SKIN IAW EA 011-5730-01-A6727, REV IR, AND EO MD11-5730-63743-A.SDR IPXA2017032915646Skin · corrodedINSPECTION TYPE: 3C, MAIN CARGO UPPER SKIN HAS CORROSION AT BS 1227 RBL 80.25. REPAIRED IAW EA 011-5730-01-A6725, REV IR, AND EO MD11-5730-63734-A.SDR DALA2017032202341Doubler · damagedWHILE REPAIRING STA 627STR 16L STRINGER CRACK, NOTED EXISTING ERA 476695-14 REPAIR DOUBLER HAD PREVIOUSLY BEEN INSTALLED. DISCOVERED ELONGATED HOLES IN REPAIR. ERA MAJOR SKIN/STRINGER REPAIR REQUIRED. REPAIRED ELONGATED HOLES ON EXISTING REPAIR STA 627 STR 16LSDR 7C7A2017031600297Skin · dentedDENTS ON SKIN BETWEEN BS 167 - 182, ABOVE AND BELOW STRINGER 24L. REPAIRED IAW RD8-53-15109 AND ECO008.53-17.13SDR ASOA201703141363Doubler · corrodedTCAS ANTENNA DOUBLER HAS CORROSION. REMOVED AND REPLACED THE DOUBLER IAW SRM 57-42-06-001-001-A01.SDR DALA2017031502089Doubler · corrodedLOWER FUSELAGE ANTENNA DOUBLER CORRODED BETWEEN BS 1440 - 1460 BL 0. REMOVED CORROSION. FABRICATED AND INSTALLED A NEW DOUBLER AND TRIPLER IAW ER/A 555817-14 ORGINAL.SDR IXXA20170412232Bear Strap · corrodedTHE BEAR STRAP WAS CORRODED BS 1263-1274, BETWEEN STRINGERS 34 - 35R. THE BEAR STRAP WAS FOUND OUT OF LIMITS IAW SRM 51-10-02. FABRICATED AND INSTALLED A DOUBLER AND TRIPLE IAW SRM 53-00-01, AND ED 47224REA44.SDR SWAA2017032812774Doubler · crackedDOUBLER CRACKED AT BS 520, AFT OF RAM AIR DOOR GROUND STUD BRACKET. REPAIRED THE DOUBLER IAW EA AND ER.SDR SIMA20170313006Skin · damagedA DENT AND GOUGE ON CENTER FUSELAGE SKIN. ACCOMPLISHED ERS-EJ-53MR-2559. MAJOR REPAIR.SDR AALA20170313002Skin · corrodedAIRCRAFT WAS NOT GROUNDED. AFT LAVATORY VENT EXIT HOLE HAS CORROSION AT FASTENERS THAT ARE MOUNTED TO THE INTERNAL VENT TUBING. REPAIRED IAW EA 268253 AND SRM 51-40-02.SDR 7C7A2017031300295Skin · damagedDENT AND SCRATCH DAMAGE TO RT FUSELAGE SKIN, AFT AND BELOW ICE SHIELD. REPAIRED IAW RD 8-53-15089 AND ECO008.53-17-11.SDR ASOA201703133020Skin · corrodedREAR FUSELAGE BETWEEN FRAMES 65 - 68 AND STRINGERS 21R-21R CORRODED UNDER BOTH AFT RADIO ALTIMETER ANTENNAS. AFT RADIO ANTENNA BASES WERE REPLACED IAW SRM 51-40-02. SKIN UNDER RADIO ANTENNA BASE WAS REPAIRED IAW ETD2017-145-018880.SDR CALA2017031100577Skin · dentedDENT LOCATED AT STA 1058 RIGHT SIDE OF FUSELAGE JUST BELOW THE APU INLET WAS FOUND TO BE OUT OF LIMITS AS PER SRM 53-00-01 FIG 103 DETAIL (G) EXTERNAL REPAIR INSTALLED IN ACCORDANCE WITH SRM 53-00-01 REPAIR 3.SDR ASOA201703113019Skin · dentedBELLY SKIN, BETWEEN FRAMES 17 - 19, STRINGERS 21L - 21R HAD MULTIPLE DENTS. REPAIRED IAW ETD2017-145-019784 REV A. HFEC INSPECTION PERFORMED WITH NO DAMAGE FOUND.SDR 7C7A2017031100292Doubler · corrodedCORROSION DAMAGE TO AFT CARGO DOOR SKIN DOUBLER. REPAIRED IAW RD8-53-15082 AND ECO008.53-17.06.SDR CALA2017031000556Skin · dentedFUSELAGE SKIN HAS A DENT AFT OF L-1 DOOR AT STA 383 BETWEEN STR- 7L AND STR-8L. ACCOMPLISHED REPAIR REF EC/RA 5330-05986.SDR 7C7A2017031000289Skin Panel · dentedDENT DAMAGE TO LT FUSELAGE SKIN. REPAIRED IAW RD8-53-15088 AND ECO 008.53-17.10.SDR 7C7A2017031000258Skin Panel · dentedDENT DAMAGE TO THE LT SIDE FUSELAGE SKIN REPAIRED IAW RD 8-53-15085 AND ECO008.53-17.09.SDR DALA2017031001930Skin · damagedBS 1727 - 1737, STRINGER 44 - 45L, SKIN AREA FOUND WITH EXISTING BLEND OUT AREA. FOUND OUT OF LIMITS IAW SRM 53-00-01, FIG 102 ALLOWABLE DAMAGE 1. DAMAGE TRIMMED OUT AND REPAIRED IAW ERA 552724-14, REV ORIGINALSDR VGCA20170309003Butt Joint · corrodedCORROSION ON BUTTSTRAP, STR 29R, BS 1010, RT SIDE, AFT CARGO BAY.SDR DALA2017031002051Doubler · corrodedLOWER FUSELAGE ANTENNA ADAPTER PLATE UNDER ANTENNA AT BS 440 - 456 BETWEEN STRINGERS 29 AND 30R CORRODED. REPAIRED IAW ERA 555819-14.SDR IPXA2017031014953Skin · dentedRIGHT FUSELAGE SKIN DENTED AND GOUGED AT BS 520. REPAIRED THE SKIN IAW EO B747-5330-63430B.SDR DALA2017031001924Skin · crackedSKIN HAS 3/16 INCH LONG CRACK FROM RIVET HOLE AT BS 1087, APPROXIMATELY ONE INCH ABOVE LONGERON 14L. REPAIRED IAW PRI 556129-14, REVISION 0, AND COMPLIED WITH ER/A 556129-14, REVISION ORIGINAL.SDR DALA2017031001923Skin · crackedSKIN HAS A .50 INCH LONG WYE SHAPED CRACK AT BS 1087, APPROXIMATELY ONE INCH ABOVE LONGERON 14R. REPAIRED IAW PRI 556130-14, REVISION 0, AND COMPLIED WITH ER/A 556130-14, REVISION ORIGINAL.SDR DALA2017031001922Skin · crackedSKIN HAS A ONE INCH LONG CRACK AT BS 1076, APPROXIMATEY ONE INCH ABOVE LONGERON 14R. REPAIRED IAW PRI 556130-14, REVISION 0, AND COMPLIED WITH ER/A 556130-14, REVISION ORIGINAL.SDR JR2R20170309484Doubler · corrodedFWD LAVATORY SERVICE PANEL CUTOUT CORRODED AT LOWER EDGE. REPAIRED THE DOUBLER IAW EA 30-2017-042.
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