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 ASAA2019102931143Doubler · crackedEXTERNAL POWER RECEPTACLE DOOR (114AR) LOWER SURROUND STRUCTURE IS CRACKED AND HAS SEPARATION. GROUNDED - YES. REPAIRED EXTERNAL POWER RECEPTICLE DOOR CUT OUT DOUBLER IAW 737-900ER SRM 53-10-15-2R REPAIR 4 FIG 204.SDR DALA2019101735951Access Panel · crackedDURING INSPECTION, FOUND CRACK ON CUT OUT AT EXTERNAL POWER RECEPTACLE ACCESS. CRACK ON CUT OUT AT EXTERNAL POWER RECEPTACLE ACCESS WAS REPAIRED PER B737-800 S.R.M 53-10-15 REPAIR 5.SDR FDEA2019101422615Skin · corrodedAFT ACCESSORY COMPARTMENT HAS EVIDENCE OF CORROSION ON THE RT SIDEWALL. REPAIRED IAW SRM 53-70-01-2R, FIG 201.SDR DALA2023090707337Unknown · unknownSHIP 668 SHIP 668 - ER/A 581643-14AD - FUSELAGE / DOOR SURROUND STRUCTURE / L1 DOOR / FWD UPPER CORNER / CRACK IN BEARSTRAP. CORRECTIVE ACTION: REF ERA 581643-14AD. (1310552)SDR SWAA2019110438487Skin · corrodedMULTIPLE AREAS CORRODED AROUND THE FASTENER HEADS ON FUSELAGE SKIN UNDER DORSAL FIN BETWEEN BS. 887 TO BS. 1007, BETWEEN STR. 2L TO STR. 2R. / REPAIRED SKIN IAW EA AND ER.SDR DALA2019101205867Skin · crackedCRACK ON EXTERNAL FUSELAGE SKIN BTW STA 1025 AND 1035 STRINGERS 13 AND 15 LH SIDE. EXTERNAL FUSELAGE SKIN BTW STA 1025 AND 1035 STRINGERS 13 AND 15 LH SIDEL WAS REPAIRED PER ER/A 582117-14 REV.ORIGINAL (SECTION I PERMANENT REPAIR) AND ETI-17-19-175 REV.2. (LP1SDR FDEA201910112604Skin · dentedEXTERIOR FUSELAGE SKIN DENTED AT STA 408 BETWEEN STRINGER 10L AND 11L REPAIRED PER EA# F-5310-T0349762-P1SDR FDEA201910112592Skin · dentedLOWER AFT CARGO FUSELAGE AT BS 1635 BETWEEN STR27R AND 28R HAS PITTING CORROSION ON INTERNAL SURFACE ACOMPLISHED WORK IAW EA F-5310-T0349844SDR EE4Y201910119891Skin · damagedFUSELAGE SKIN FROM BS500F+10 TO BS540, BETWEEN S-16LH AND S-19LH WING TO BODY FAIRING AREA, EXTERNAL SURFACE WITH EXISTING BLENDOUT.WAS REPAIRED PER AERONAUTICAL ENGINEERS EO9693 IR,DATED 10/04/2019.(REF:JOB:A1H217 ITEM 2-61)SDR SWAA2022041959375Tail Cone · delaminatedLIGHT SWITCH IN EMPENAGE TAIL CONE FOUND LOOSE DUE TO DELAMINATED COMPOSITE JUST BELOW THE FWD LOWER CORNER OF THE ACCESS CUT OUT / REVOMED LIGHT SWITCH FOR ACCESS ; REPAIRED DELAMINATION ON EMPENNAGE TAIL CONE JUST BELOW FWD LOWER CORNER STA 1166 OF ACCESS ; SDR SWAA2019110638646Skin · damagedDAMAGED FUSELAGE SKIN BS 1040+6" TO 1040+13" STR 1" ABOVE 23R TO 2" ABOVE 24R REQUIRES SKIN REPAIR (REFERENCE CUSTOMER CARDS T986010,T986011,T986013, T986014, T986015, T986016, T986018). / REPAIR TO FUSELAGE SKIN AT BS 1040+6" TO BS 1040+13" 1" ABOVE SDR DALA2019101315872Skin · dentedDENT RH SIDE STATIC PORT DURING PREFLIGHT F/O FOUND DENT ON RIGHT SIDE OF NOSE (F/O SIDE) REFER TO (LOG PAGE 4600672). PERFORMED REPAIR ON FUSELAGE SKIN ON RIGHT SIDE OF (F/O SIDE) IAW SRM A319 53-11-11-300-041.SDR HEER20191010343Skin · corrodedFORWARD SHELL ASSEMBLY FOUND TO BE CORRODED - THREE PLACES: BOTH FORWARD CORNERS AND AT AN EXISTING INSERT. FORWARD SHELL ASSEMBLY WILL BE REPAIRED.SDR EVCA2019101000002Skin · crackedSKIN EDGE CRACK FOUND AT APPROX. STA 155, LBL 19 TO 21 AND WL 72. CRACK 2 IN LONG THROUGH 2 RIVETS.SDR DALA2020100903324Skin · damagedDURING PERMANENT REPAIR OF CROWN SKIN DAMAGE PER ER/A 581456-14, DAMAGE REMOVAL REQUIRED THE REMOVAL ON GPS ANTENNAS AND / MOUNTING STRUCTURE REF ERA 581683-14. CORRECTIVE ACTION: REF ERA 581683-14 REV A.SDR HNAA2019111400359Skin · damagedFUSELAGE SKIN HAS A BURN MARK AT FRAME 63 BETWEEN STR20R-21R....FIX: INSTALLED FILLER AND REPAIR DOUBLER IAW SRM 53-31-01,ITEM 4,FIG 204,SHEET 1, AND EO1-53-19-0500. NOTE: A/C IN HVY CHK (ABI)SDR FDEA2019101092543Skin · gougedLOWER FUSELAGE HAD A DENTED AREA AT BS 513, BETWEEN STRINGERS 28L AND 29L. EVALUATED DENTED AREA AND FOUND THE AREA TO HAVE TWO GOUGES IAW IAW SRM 51-10-02-0G, AND BLENDED AREA AND FOUND MINIMUM THICKNESS REMAINING OF SKIN AREA .030. FOUND TO BE OUT OF LIMSDR DALA2019101115844Skin · corrodedSKIN BENEATH STUB BEAM AT RT FUSELAGE, BS 883.5 WAS CORRODED RBL 90. REPAIRED THE SKIN IAW ERA 581549-14, REV 0.SDR CALA20191011730Skin · corrodedREF FCD 5100-02772 LAV VENT PORT HAS CORROSION STA 917L BETWEEN STRINGERS 21L AND 22L FUSELAGE SKIN AT STA 917 BETWEEN STR''S 21L AND 22L HAVE BEEN REPAIRED IAW SRM 53-70-01 REP 3 INSP THRESHOLD @ 50,000 TOT F/C FOLLOWED BY REPEAT INTERVALS AT EACH SUBSEQUENT SDR REXA2019102481482Fastener · corrodedINITIAL INSPECTION: CORROSION ON FASTENERS (2E/A) BTW FS669.40 AND FS677 STGR.25R AT FUSELAGE SKIN.(FUS)
SUMMARY: ON NRC. 00119 FASTENERS (2E/A) BTW FS669.40 AND FS677 STGR. 25R AT FUSELAGE SKIN WERE REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01SDR DALA2019101195862Doubler · corrodedDURING INSPECTION FOUND ANTENNAS M2295 AND M2296 IN REF NRC S/N 00417, CORROSION WAS FOUND ON INTERNAL DOUBLER AT AFT CARGO COMPARTMEN SKIN. DOUBLERS OF NATS AIR PHONE ANTENNAS M2295 AND M2296 WERE REPAIRED PER ETI-37-19-328 REV. 1 AND ER/A: 582030-14.SDR DALA2019101195861Skin · corrodedDURING INSPECTION FOUND ANTENNAS M2295 AND M2296 IN REF NRC S/N 00417, CORROSION WAS FOUND ON SETTLEMENT AREA AT FUSELAGE SKIN. SKIN SETTLEMENT AREA OF NATS AIR PHONE ANTENNAS M2295 AND M2296 WAS REPAIRED PER ETI-37-19-328 REV. 1 AND ER/A: 582030-14.SDR FDEA2019101082499Skin · dentedETERIOR FUSELAGE SKIN IS DENTED AT APPROX BS 1630 ON STR17R. REMOVED EFECTED FASTENERS PREFORMED HFEC TO OPEN HOLES AND EFECTED AREA FOUND NO CRACKS. OVERSIZED OPEN HOLES AND INSTALLED NEW FASTENERS IAW EA F-5330-T0349901.SDR DALA2019100905800Skin · corrodedAFTER FWD LAVATORY SERVICE PANEL WAS REMOVED, CORROSION WAS FOUND ON EXTERNAL FUSELAGE SKIN AND INTERNAL DOUBLER. REPAIRED PER. ER/A 581923-14 REV. ORIGINAL; SECTION I AND ETI-57-19-117 REV.2 AND REPAIR APPROVAL IS LIMITED TO 57,500 TOTAL AIRCRAFT CYCLES ONLSDR GTIA2019100984677Skin · dentedDENT FOUND ON REAR FUSELAGE BTW FR. 70 - 71 AND STR.16L - 17L. DIMENSIONS: L=25MM, W=25MM, D=0.70MM. RAF-01 252899301 OPENED-THE AFFECTED AREA WAS REPAIRED AS PER EO 5351-9041 SEPT 27 2019 ATTACHED TO JOBCARD 0001002927790-0010 THE EMBOIDED REPAIR LIFE TO 6 SDR JR2R2019100812110Skin · crackedFUSELAGE SKIN FWD OF FS 1016 AND ABOVE S-24L HAD CRACK DAMAGESDR IPXA2019101874800Skin · corrodedINSPECTION TYPE:2CCENTER WING BOX UPPER SKIN HAS CORROSION AT F/S 1152, RBL=108 AND STRINGER 15.REPAIRED CORRODED CENTER WING BOX UPPER SKIN AT F/S 1152, RBL=108 AND STRINGER 15 IAW VT-SAA EA 011-5730-01-A7927 REV. IR AND UPS EO MD11-5730-74362-A. (MINOR)SDR FDEA201910072480Skin · scratchedSURFACE SCRATCHES ON THE FUSELAGE SKIN AT BS 900 - 920. FOUND TO BE OUTSIDE PERMITTED LIMITS. REPAIRED IAW EA F-5330-T0349853 P (1).SDR DALA2024061106028Skin · crackedCRACKS WERE FOUND AFFECTING SKIN 5936436-101. AND FINGER DOUBLER 5936436-39 (M/F 0.025 7075-T6 CLAD SHEET) AT STA 1037 & L14L. FAA STAGE III APPROVAL REQUIRES INITIAL AND RECURRING GENERAL VISUAL INSPECTIONS THAT BEGIN AND ARE REPEATED EVERY C-CHECK OR 24 MSDR COEA2019112640810Skin · corrodedWO 205731 NR 200121 HEAVY CHECK COE/MAJOR REPAIR: CENTER FUSELAGE UPPER R/H SKIN INTERIOR SURFACE HAS LEVEL 2 CORROSION BETWEEN FRAMES 28D-29 BETWEEN STRINGERS 10R-11R. CORRECTIVE ACTION: REPAIRED PER SRAS ES_0107986_01...15487 ISSUE A, DATED 11/20/2019.SDR COEA2019112639810Skin · corrodedWO 205731 NR 200108 HEAVY CHECK COE/MAJOR REPAIR: CENTER FUSELAGE UPPER R/H SKIN INTERIOR SURFACE HAS LEVEL 2 CORROSION AFT OF FRAME 23C BELOW STRINGER 8R. CORRECTIVE ACTION: REPAIRED PER SRAS ES_0107986_01...15487 ISSUE A, DATED 11/20/2019.SDR COEA2019112638810Skin · corrodedWO 205731 NR 200101 HEAVY CHECK COE/MAJOR REPAIR: CENTER FUSELAGE UPPER R/H SKIN INTERIOR SURFACE HAS LEVEL 2 CORROSION AFT OF FRAME 23B BELOW STRINGER 8R. CORRECTIVE ACTION: REPAIRED PER SRAS ES_0107986_01...15487 ISSUE A, DATED 11/20/2019.SDR COEA2019112236810Skin · corrodedWO 205731 NR 200130 HEAVY CHECK COE/MAJOR REPAIR: CENTER FUSELAGE UPPER R/H SKIN INTERIOR SURFACE HAS LEVEL 2 CORROSION BETWEEN FRAMES 28-28A STRINGERS 7R-8R. CORRECTIVE ACTION: REPAIRED PER SRAS ES_0107986_01...15487 ISSUE A, DATED 11/20/2019.SDR COEA201911225810Skin · corrodedWO 205731 NR 200127 HEAVY CHECK COE/MAJOR REPAIR: CENTER FUSELAGE UPPER R/H SKIN INTERIOR SURFACE HAS LEVEL 2 CORROSION BETWEEN FRAMES 28A-28B BETWEEN STRINGERS 10R-11R. CORRECTIVE ACTION: REPAIRED PER SRAS ES_0107986_01...15487 ISSUE A, DATED 11/20/2019.SDR COEA201911224810Skin · corrodedWO 205731 NR 200125 HEAVY CHECK COE/MAJOR REPAIR: CENTER FUSELAGE UPPER R/H SKIN INTERIOR SURFACE HAS LEVEL 2 CORROSION BETWEEN FRAMES 28C-28D BETWEEN STRINGERS 8R-10R. CORRECTIVE ACTION: REPAIRED PER SRAS ES_0107986_01...15487 ISSUE A, DATED 11/20/2019.SDR COEA2019112263810Skin · corrodedWO 205731 NR 200122 HEAVY CHECK COE/MAJOR REPAIR: CENTER FUSELAGE UPPER R/H SKIN INTERIOR SURFACE HAS LEVEL 2 CORROSION BETWEEN FRAMES 28D-29 BETWEEN STRINGERS 7R-8R. CORRECTIVE ACTION: REPAIRED PER SRAS ES_0107986_01...15487 ISSUE A, DATED 11/20/2019.SDR COEA201911229810Skin · corrodedWO 205731 NR 200092 HEAVY CHECK COE/MAJOR REPAIR: CENTER FUSELAGE UPPER R/H SKIN INTERIOR SURFACE HAS LEVEL 2 CORROSION BETWEEN FRAMES 23-23A, STRINGERS 6AR-7R. CORRECTIVE ACTION: REPAIRED PER SRAS ES_0107986_01...15487 ISSUE A, DATED 11/20/2019.SDR COEA201911228810Skin · corrodedWO 205731 NR 200091 HEAVY CHECK COE/MAJOR REPAIR: CENTER FUSELAGE UPPER R/H SKIN INTERIOR SURFACE HAS LEVEL 2 CORROSION FORWARD OF FRAME 23A, BETWEEN STRINGERS 8-9R. CORRECTIVE ACTION: REPAIRED PER SRAS ES_0107986_01...15487 ISSUE A, DATED 11/20/2019.SDR COEA201911227810Skin · corrodedWO 205731 NR 200077 HEAVY CHECK COE/MAJOR REPAIR: REAR FUSELAGE UPPER R/H SKIN INTERIOR SURFACE HAS LEVEL 2 CORROSION FORWARD OF FRAME 40, ABOVE STRINGER 6R. CORRECTIVE ACTION: REPAIRED PER SRAS ES_0107970_01...15483 ISSUE A, DATED 11/18/2019.SDR COEA2019112264810Skin · corrodedWO 205731 NR 200117 HEAVY CHECK COE/MAJOR REPAIR: REAR FUSELAGE UPPER R/H SKIN INTERIOR SURFACE HAS LEVEL 2 CORROSION BETWEEN FRAMES 29-30, STRINGERS 3R-4R. CORRECTIVE ACTION: DOUBLER REPAIR PER SRAS ES_0107970_01...15483 ISSUE A, DATED 11/18/2019.SDR COEA2019112261810Skin · corrodedWO 205731 NR 200079 HEAVY CHECK COE/MAJOR REPAIR: REAR FUSELAGE UPPER R/H SKIN INTERIOR SURFACE HAS LEVEL 2 CORROSION BETWEEN FRAMES 39-40, STRINGERS 3R-4R. CORRECTIVE ACTION: REPAIRED PER SRAS ES_0107970_01...15483 ISSUE A, DATED 11/18/2019.SDR COEA2019112260810Skin · corrodedWO 205731 NR 200078 HEAVY CHECK COE/MAJOR REPAIR: REAR FUSELAGE UPPER R/H SKIN INTERIOR SURFACE HAS LEVEL 2 CORROSION BETWEEN FRAMES 39-40, STRINGERS 4R-5R. CORRECTIVE ACTION: REPAIRED PER SRAS ES_0107970_01...15483 ISSUE A, DATED 11/18/2019.SDR COEA2019112269810Skin · corrodedWO 205731 NR 200064 HEAVY CHECK COE/MAJOR REPAIR: REAR FUSELAGE UPPER R/H SKIN INTERIOR SURFACE HAS LEVEL 2 CORROSION BETWEEN FRAMES 40-41, STRINGERS 3R-4R. CORRECTIVE ACTION: DOUBLER REPAIR PER SRAS ES_0107970_01...15483 ISSUE A, DATED 11/18/2019.SDR COEA2019112268810Skin · corrodedWO 205731 NR 200064 HEAVY CHECK COE/MAJOR REPAIR: REAR FUSELAGE UPPER R/H SKIN INTERIOR SURFACE HAS LEVEL 2 CORROSION NEAR FRAMES 40-41, STRINGERS 3R-4R. CORRECTIVE ACTION: BLENDOUT PER SRAS ES_0107970_01...15483 ISSUE A, DATED 11/18/2019.SDR COEA2019112267810Skin · corrodedWO 205731 NR 200061 HEAVY CHECK COE/MAJOR REPAIR: REAR FUSELAGE UPPER R/H SKIN INTERIOR SURFACE HAS LEVEL 2 CORROSION BETWEEN FRAMES 41-42, STRINGERS 5R-6R. CORRECTIVE ACTION: REPAIRED PER SRAS ES_0107970_01...15483, ISSUE A, DATED 11/18/2019.SDR COEA20191119810Skin · corrodedWO 205731 NR 200080 HEAVY CHECK COE/MAJOR REPAIR: FORWARD FUSELAGE R/H UPPER SKIN INTERIOR SURFACE HAS LEVEL 2 CORROSION BETWEEN FRAMES 13-14, STRINGERS 5R-6R. CORRECTIVE ACTION: REPAIRED PER SRAS ES_0107816_01...15468 ISSUE A, DATED 11/15/2019.SDR COEA2019110865810Skin · corrodedWO 205731 NR 200109 REAR FUSELAGE LOWER R/H SKIN INTERIOR SURFACE HAS LEVEL 2 CORROSION BETWEEN FRAMES 32-33 STRINGERS 12R-13R. CORRECTIVE ACTION: REPAIRED PER SRM 530000-300-805-A01.SDR COEA2019110864810Skin · corrodedWO 205731 NR 200085 HEAVY CHECK COE/MAJOR REPAIR: FWD FUSELAGE UPPER R/H INTERIOR SURFACE HAS LEVEL 2 CORROSION FWD OF FRAME 17 BETWEEN STRINGERS 9R-10R. CORRECTIVE ACTION: REPAIRED PER SRM 530000-300-803-A01.SDR IPXA2019103098462Access Door · crackedINSPECTION TYPE:A300ACCESS DOOR 313AL LOWER FOUND CORNER IS CRACKEDREPAIRED IAW A300-600 SRM 51-77-11 AND EA 300-5240-27-A2383.SDR DALA2019100765763Doubler · corrodedCORROSION ON DOUBLER REPAIR EXTERNAL SKIN OF AFT LAVATORY. DOUBLER REPAIR EXTERNAL SKIN OF AFT LAVATORY WAS REPLACED PER ER/A 542102-14 REV. ORIGINAL, SECTION 1.
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