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 REXA2018122171288Skin · corrodedWHILE REMOVING CORROSION FOUND CORROSION ON FUSELAGE INNER SKIN FS
280-295 BETWEEN S27-26R
REPAIRED INNER SKIN IAW EA CRJ 953-07909 REV IR
SDR ASOA2018121465343Skin · dentedREF: CO# 7476718 JOB# 7747675 OP# 62: FUSELAGE SKIN REPAIR REQUIRED BELOW CARGO DOOR BETWEEN FS 605.0 TO FS 625.0 AND STR 18L TO 22L. C/A: PERFORMED PERMANENT REPAIR I.A.W. EXPRESSSJET ECTC REO 601R-53-61-6789.SDR CALA2018120702526Access Panel · gougedAFT FUSELAGE TAIL SECTION FR69 RH, FWD OF ACCESS 312AR HAS GOUGE S AT FASTENERS HOLES (Y267) (A3NB-53-4-6229) PER HAECO LCQ REF. NO. 9296354. GENERATED BY V894372. AFT FUSELAGE FR69 RH FABRICATED AND INSTALLED EXTERNAL DOUBLER R EPAIR IAW A320 SRM 53-41-11-300SDR DALA2018120707092Doubler · corroded(AIRCRAFT 6703, L/P 0854699) INITIAL INSPECTION: CORROSION ON DOUBLER OF INTERNAL SKIN AT LAVATORY SERVICE PANEL.E&E. SUMMARY: IN REF NRC 00500 (CORROSION LEVEL 2) DOUBLER OF INTERNAL SKIN AT LAVATORY SERVICE PANEL.E&E WAS REPLACED PER B757-200 DWG 141N8631 RESDR JJBA201812076004Skin · corrodedAIRCRAFT DATA PLATE FORWARD RIGHT RIVET IS LOOSE AND SKIN AREA AT FORWARD SIDE HAS SURFACE CORROSION. CORROSION EXTENDS 100% THROUGH SKIN AND REQUIRES CUT-OUT AND REPAIR. PERFORMED CUT-OUT AND FABRICATED DOUBLER OUT OF ALCLAD 2024T3, 040" AND FILLER OUT OF ALCSDR SWAA2019011427975Skin · corrodedDORSAL FIN ON EXTERNAL SKIN CORRODED BETWEEN BS 1006 TO BS 907, BETWEEN STR 2L TO STR 2R. REPAIRED SKIN IAW ER AND EA.SDR SIMA2018122105015Skin · cracked1/4 INCH DIAGONAL CRACK ( TOP L TO BOTTOM R) FOUND IN FUSELAGE SKIN AT FRAME 75 JUST ABOVE STRINGER 2L. 1" AREA OF PAINT REMOVED AND AREA DYE PEN'D FOR BETTER VISIBILITY AND LOCATION OF CRACK. AREA AROUND FLAW TAPED OFF.-C/A-REPAIRED CRACK IN FUSELAGE SKIN AT SDR ABXA201812065137Skin · crackedCRACK IN THE FUSELAGE SKIN AT BODY STATION 757.3 AND BETWEEN STRINGERS 25R AND 26R. THE SKIN WAS REPAIRED. THE AIRPLANE WAS GROUNDED.SDR ASOA201812067187Doubler · gougedGOUGE AT FRAME 51, STRINGER 19R. REPLACED REPAIR DOUBLER IAW SRM 53-24-02.SDR C77A2018120500002Skin Panel · dentedDURING BASIC CHECK AT EAMS, A CREASED DENT WAS DISCOVERED ON THE FORWARD FUSELAGE LOWER SKIN PANEL, P/N 170-05669-005, LOCATED BETWEEN FR14/FR15 AND STGR20L/STGR21L (REF PHOTOS 1-2 AND ETD2018-170-121906, FIGURE 1). THE DENT MEASURES THE FOLLOWING APPROXIMATE SDR DALA2019013100745Skin · not reportedFUSELAGE SKIN STA 1654.5 AND STR 13AR C/W ERA 565537-14.SDR SWAA2019011728604Skin · dentedFUSELAGE SKIN DENT AT BS 1016+3, STR 13L. REPAIRED SKIN ER & EA.SDR SWAA2019011728590Skin · dentedFUSELAGE SKIN DENT AT BS 1016+10, STR 16L. REPAIRED SKIN PER EA.SDR SWAA2019011728589Skin · dentedFUSELAGE SKIN DENT AT BS 1016+15, STR 15L. REPAIRED SKIN PER ER & EA.SDR SWAA2019011527848Skin · corrodedNOSE LANDING GEAR WHEEL WELL EVIDENCE OF CORRODED AROUND MULTIPLE NUTPLATE HOLES FOR RT CEILING PANEL 114AC. REPAIRED SKIN IAW EA.SDR SWAA2019011527983Skin · damagedSKIN DAMAGED AT BS 453.5, STR 28L. REPAIRED SKIN IAW SRM.SDR SWAA2018122027760Doubler · crackedRT HORSESHOE DOUBLER FOR A/C EXHAUST CRACKED AT BS 663. R&R DOUBLER IAW DWG AND SRM.SDR ASOA2018121935346Skin · dentedREF: CO# 7496618 JOB# 7749665 OP# 30: 2EA DENTS ON FUSELAGE SKIN BETWEEN F.S.235.00 AND F.S.250.00, STRINGER 24L AND STRINGER 25L.C/A: REPAIRED DAMAGE I.A.W. BOMBARDIER REO 601R-53-11-3352 REV.A, DATED 2018/11/29 AND EXPRESSJET EC/TC REO 601R-53-11-3352 REV.ASDR YENA2018120730833Doubler · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON RH TRANSPONDER ANTENNA DOUBLER CORRBET FR19 -FR20; REF NRC FOR ALL WORK ACP. RH TRANSPONDER ANT DOUBLER RPL IAW SRM 51-41-02SDR SIMA201812073008Skin · dentedTRANSFERRED FROM AML 4424546 ITEM 3, FOUND LARGE DENT WITH GAUGE BETWEEN STGR 12R & 14R AND BETWEEN FR 22A & 23. W=4.875IN, L=9.125IN, DEPTH=0.218IN. THIS IS A MAJOR REPAIR-C/A-REPAIRED DENT IAW ERS-EM-53MR-3545SDR FDEA201812033423Skin · crackedFWD A/C PACK EXHAUST DOOR LOWER FWD CORNER FUSELAGE SKIN CRACK. REPAIRED CRACKED SKIN PER SRM 53-50-00 FIG 3A AN EA 8-5330-T0343870 P1.SDR FDEA201812033422Skin · crackedFWD A/C PACK EXHAUST DOOR LOWER AFT CORNER FUSELAGE SKIN CRACK. REPAIRED CRACKED SKIN PER SRM 53-50-00 FIG 3A AND EA 8-5330-T0343870 P2.SDR SIMA201812043001Skin · dentedAIRCRAFT SKIN DENTED OUTWARD NEAR FS333.00 BETWEEN STRINGERS 20-21 LEFT. -C/A-REPAIRED SKIN NEAR FS333 BETWEEN STR 20-21 IAW ERS-CR-53MR-3534.SDR SWIA2018122145384Skin · dentedEXTERIOR LOWER LEFT HAND SKIN - APROX. FS. 682.00 STGR 20R €“ DENTED. (C-CHECK) RO: 12/20/2018 REPAIRED DENT IAW REO.SDR SWIA2018122145383Skin · dentedEXTERIOR LOWER RIGHT HAND SKIN - APROX. FS. 654.00 STGR 20R €“ DENTED. (C-CHECK) RO: 12/20/2018 REPAIRED DENT IAW REO.SDR V0XD20181213004Tripler · gougedAFT LOWER FUSELAGE EXISTING REPAIR AT F.S. 977.00 AND STGR 27 HAS A GOUGE. CORRECTIVE ACTION: REPAIRED FUSELAGE SKIN AT F.S. 977.00 AND STGR 27 IAW BOMBARDIER REO 670-53-61-1505 REV.B(P1) DATED 2018-12-04, 670-53-61-1505 REV. A DATED 2018-12-03, 670-53-61-920SDR CALA2018120702493Skin · corrodedAGING AIRCRAFT INSP (M.FLASH)-CENTER WING TANK UPPER SKIN,UPPER SURFACE AT BS 953 AND LBL 88 HAS LARGE AREA OF EXFOLIATION CORROSION. REF. AAR N/R:9453495 REMOVED CORROSION ON CENTER TANK UPPER SKIN UPPER SURFACE AT B.S 953,LBL88 AND INSTALLED REPAIR,REF.UNITESDR DALA2018120427014Skin · dented(AIRCRAFT 6816, L/P 0848093) ON PREFLIGHT, FOUND TWO DENTS IN AIRCRAFT FUSELAGE JUST FORWARD OF 2L DOOR. CORRECTIVE ACTION: FABRICATED DOUBLER AND PICKED UP FASTENER HOLES ON SKIN TO .189 PER PRI 573400-14, REV. 1. FINISHED DRILLING UP ALL DOUBLER AND COUNTERSSDR SWAA2019011627999Skin · corrodedFUSELAGE SKIN CORRODED BETWEEN BS 440+12 TO BS 440+15 COMMON TO FORWARD CARGO DOOR SCUFF PLATE. REPAIRED SKIN IAW EA & ER.SDR SWAA2019011627998Skin · corrodedFUSELAGE SKIN CORRODED AT BS 480+4 COMMON TO FORWARD CARGO DOOR AFT CORNER CASTING. REPAIRED SKIN PER ER AND EA.SDR SIMA2018121030005Skin · crackedRH EXTERNAL FUSELAGE SKIN CRACKED AROUND 2 RIVETS FR 78-C/A-RH EXTERNAL FUSELAGE SKIN CRACKED AROUND 2 RIVETS FR 78 REPAIRED IAW ERS-EM-53MR-3518SDR REXA201812101209Skin Splice · corrodedINITIAL INSPECTION. CORROSION ON SKIN SPLICE FS 281 BTW STRG 24L-24R AT MAIN AVIONICS COMPARTMENT. (SM)(E/E) (TCI 100-09). COMPLETE: SKIN SPLICE (BUTTSTRAP) ON FS 281 BTW STRG 24L-24R WAS REPAIRED PER EA NO:CRJ953-07946 EA REV. IR.SDR CALA2018120202488Skin · crackedREFERENCE AAR LOG ITEM 9019374, ROTO PROBE INSEPCTION SHOWS CRAC K INDICATION IN MULTIPLE LAYERS @ FR35, STR 30L LOWER AFT HOLE AAR ACCOMPLISHED INTERIM REPAIR, PART 1 STEPS 1-23 OF ECRA 5331- 02304. NEED TO ACCOMPLISH A PERMANENT REPAIR PER PART 3 ON OR BE FOSDR DALA2019102106038None · noneSHIP 6816 PER ERA 573400-14, SECTION II DTE IS REQUIRED ON THE FUSELAGE SKIN BETWEEN BS 560 & 587 AT STRINGER 16L. CORRECTIVE ACTION: C/W ERA 573400-14 REV B , ALL WORK DOCUMENTED ON NRC #154, LOG PAGE CREATED FOR REPETITIVE INSPECTION#1321306 AND LOG PAGE #13SDR SWIA2018122145382Skin · dentedEXTERIOR LOWER RIGHT HAND SKIN - APROX. FS. 672.00 STGR 20 €“ DENTED. (C-CHECK) RO: 12/20/2018 REPAIRED DENTED AREA IAW REO.SDR SWAA2022022564835Skin · corroded***CORROSION*** ON EXTERNAL SKIN UNDER VERTICAL STAB 1013-1093 BETWEEN STR 3L-3R / CORROSION WAS FOUND ON EXTERNAL SKIN STA. 1016-1088; STR. 3L-3R IN AREA OF 78.0'L X 30.0'W X .005'D FOUND IN LIMITS PER SRM 53-00-01-1A-1; FIG. 103; DET. C+D. AREA @ STA. 1030-1SDR FXGA201811281827Skin · crackedCRACKED FUSELAGE SKIN UNDER COMM ANTENNA AT F/STA 348 BETWEEN STRINGER 1L AND 1R. CRACKED FUSELAGE SKIN UNDER NR 2 COMM ANTENNA AT F/STA 348 BETWEEN STRINGER 1L AND 1R. PERFORM SKIN REPAIR PER DC-6 A&B OHM FIGURE 12-22.SDR R61A201901100045Skin · dentedDURING HEAVY CHECK MAINTENANCE FOUND EXTERNAL FUSELAGE SKIN 7 DENTS BETWEEN FR18 AND FR19 AND STR 26R AND 27R. FOUND OUT OF LIMITS IAW SRM 53-10-01. CUTOUT DAMAGE AREA, FABRICATED REPAIR DOUBLER AND FILLER AND INSTALLED IAW ETD2019-170-000690. A/C REMAINS IN CSDR DALA2018112906953Doubler · dentedDENT EXTERNAL SKIN DOUBLER REPAIR ON LOWER FUSELAGE FROM FRAME 25 TO FRAME 26 BETWEEN STRINGER 43L TO 42R. REPLACED IAW SRM 51-42-11 AND DWG P19110-21115, REV C.SDR DALA2018113006937Skin · corroded(AIRCRAFT 672, L/P 0844166) AFT EXTERIOR FUSELAGE SKIN CORRODED, STATION 1720 AT STRINGER 28RT. REF WO.0672_11/20/2018_LTO, TASK CARD B757 VIRTUAL ROUTINE/012, NR00012. REPAIRED ARE PER ERA 573331-14 REV.ORIGINAL. REMOVED EXISTING REPAIRS, BLENDED AREAS PER B7SDR DALA2018112906912Skin · damaged(LOG 0844029) DURING INSPECTION FOUND PREVIOUS BLEND DONT IDENTIFICATED STATION 727I BTW STR 20L TO 19L (FUS). PREVIOUS BLEND OUT WAS REPAIRED PER B737-800 SRM 53-00-01 REPAIR 36.SDR DALA2018112986897Skin · damagedLH FUSELAGE SKIN AT STA 133 TO 172 2 EACH LIGHTING AREA DAMAGED. REPAIRED PER SRM 53-00-01. (LP 0843644)SDR SWAA2022022863101Skin · dentedRIGHT SIDE FUSELAGE SKIN AT STA. 196.5 ; 6' ABOVE LOWER SKIN LAP DENT IN SKIN L= 4.20' W = 3.60' Y= .148' W/Y RATIO = 24 OUT OF LIMITS PER SRM 53-00-01-1A-1 ALSO OIL CANNING IS APPROX.. 4' DIAMETER AND PRESSED IN APPROX. .500' FROM NORMAL. / REPAIRED PER EA 1-SDR SWAA2019011627993Skin · chafedEXTERNAL SKIN CHAFED UNDER DORSAL FIN BETWEEN BS 867 TO BS 887, STR 1R. REPAIRED SKIN IAW EA AND ER.SDR ASOA2018121475340Skin · dentedREF: CO# 7476718 OP# 62 FUSELAGE SKIN HAS 1 EA DENT BETWEEN FS605 AND FS589 FROM STR 24L TO 25L. C/A PERFORMED PERMANENT REPAIR IAW EXPRESSJET ECTC EA 32-2018-239SDR CALA2018120202453Skin · corrodedDURING 2C CHECK CORROSION DAMAGE WAS FOUND FUSELAGE SKIN INTERNAL SURFACE FROM FS 2344 TO FS2358 ON AND BETWEEN S40R & S43R. ECRA 5330-06474 PART 1 INTERIM REPAIR.SDR RAIA2018122960001Skin · crackedR/H WING UPPER I/B SURFACE AT FRAME 48 NUTPLATE SUPPORT ON TOP OF WING IS CRACKED....REMOVED & REPLACED R/H UPPER I/B SURFACE ANGLE SUPPORT AT FRAME 48 ON TOP OF WING.SDR DALA2018120407015Skin · corroded(AIRCRAFT 672, L/P 0841547) CORROSION WAS FOUND AT STA. 1720, STR S-27R. TE CORROSION AT THIS LOCATION EXTENDS UNDER A PREVIOUSLY INSTALLED DOUBLER/TRIPLER REPAIR VIA ER/A 475339 WHICH WAS SUPERCEDED BY ER/A 492565. THE ER/A ASSOCIATED WITH THIS LOG PAGE AUTHOSDR DALA2018112766843Skin · corrodedFOUND DURING DVI LOWER WING SKIN HAS A 1 INCH CRACK AT A FASTENER AT STA. 983 STR. 9. REPAIRED PER ERA 573238-14. (LP 5141052)SDR DALA2018112756841Skin · corrodedCORROSION LEVEL: 2 CORROSION FOUND ON FUSELAGE SKIN ON STA925 AND 2 INCH ABOVE THE FLOOR LEVEL. REPAIRED PER ERA 573021-14. (LP 0839762)
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