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 IPXA2017051417075Skin · damagedFUSELAGE SKIN DAMAGED AT FRAME 20, STRINGER 28R. REPAIRED IAW EO A300-5330-63906-C.SDR SWAA2017060514082Doubler · crackedL1 DOOR CUTOUT INTERNAL DOUBLER CLOSEOUT CRACKED BELOW LOWER HINGE CUTOUT. R & R DOUBLER IAW SRM AND DWG.SDR R61A201705130364Finger Doubler · corrodedDURING HEAVY CHECK, CORROSION WAS FOUND ON THE FWD CARGO DOOR BEAM FWD FINGER DOUBLER. REMOVED AND REPLACED THE FINGER DOUBLER IAW SRM 51-43-02, AND 51-41-02.SDR QXEA2017051700359Strap · corrodedINTERNAL FUSELAGE LONGITUDINAL SKIN STRAP BETWEEN STRINGERS. 31 AND 32L HAS EVIDENCE OF SURFACE CORROSION 4 INCHES FORWARD OF FRAME BS 176. REMOVED AND BLENDED LIGHT CORROSION ON INTERNAL FUSELAGE LONGITUDINAL SKIN STRAP IAW SRM 53-00-00, REPAIR 20. FOUND TSDR ASOA201705131572Skin · dentedFUSELAGE DAMAGE BETWEEN FS 265 AND FS 280 BETWEEN STR 15R AND 16R. REPAIRED DAMAGED AREA OF FUSELAGE SKIN IAW REO 670-53-11-1277 REV O.SDR DALA2017051403874Doubler · debondedDISBONDED REPAIR DOUBLER BS 294, BETWEEN LONGERONS 17 & 18L. THE DOUBLER WAS REPLACED IAW SRM 53-04-3, FIG 2, & 51-30-2.SDR SWAA2022012498289Scuff Plate · crackedFWD CARGO FWD CORNER THRESHOLD PLATE IS CRACKED. / REPAIRED FWD CARGO FWD CORNER THRESHOLD PLATE PER RO# 7530028-A6R.SDR SWAA2022012498290Scuff Plate · crackedFWD CARGO AFT CORNER THRESHOLD PLATE IS CRACKED. / REPAIRED FWD CARGO AFT CORNER THRESHOLD PLATE PER RO# 7530065-A9R.SDR SWAA2022012405238Scuff Plate · crackedAFT CARGO DOOR CUT-OUT LOWER FWD CORNER SCUFF PLATE CRACKED. / AFT CARGO DOOR CUTOUT LOWER FWD CORNER SCUFF PLATE CRACKED REMOVED CRACKED SCUFF PLATE AND HAD BACK SHOP WELD CRACK ON WO # 35684-1000-0001 REINSTALLED NEWLY WELDED SCUFF PLATE ON JOB # EA 1-A53-20SDR FDEA201705121404Skin · crackedEMPENNAGE RIGHT SIDE AT BUTTJOINT BETWEEN FRAMES 98 AND 99 HAS A THREE INCH CRACK IN SKIN. TRIMMED CRACK AND FABRICATED A REPAIR IAW SRM 57-19-12, AND SRM 53-19-12. MAJOR REPAIR.SDR DALA2017051303963Skin · corrodedFUSELAGE SKIN BULGING WITH FASTENERS PULLING, BS 1219, STRINGER 32L, APPROXIMATLEY 8 INCH AREA, 12 INCHES AFT OF PREVIOUS REPAIR. REPAIRED IAW ERA 558384-14.SDR DALA2017051303873Skin · dentedDENT ON EXTERNAL FUSELAGE SKIN BETWEEN BS 646 - 645, LONGERONS 29L - 29R. THE SKIN WAS REPAIRED IAW ETI-88-17-147, REV 6, AND ER/A 558091-14, REV ORIGINAL.SDR DALA2017051303865Skin · crackedCRACK ON PRODUCTION DOUBLER UPPER SKIN STA Y=1176 CANT BTW LONG 1 TO 3 RT AFT ACCESSORY COMPARTMENT. REPAIR WAS ACCOMPLISHED PER ETI-17-17-052 REV ORIGINAL AND ER/A 558094-14 REV ORIGINAL.SDR DALA2017051203844Skin · crackedFUSELAGE SKIN AT BS 1725, STRINGER 7R FOUND CRACKED. REPAIRED IAW SRM 53-80-01 AND ERA 555753-14.SDR IXXA20170802258Skin · crackedEXTERNAL SKIN CRACKED AROUND FASTENER HEAD AT BS 1725.5 RIGHT SIDE. REPAIRED THE SKIN IAW SRM 53-80-01. REPAIR 6. ACFT GROUNDED.SDR ABXA20170511060Skin · corrodedCORROSION ON RIGHT SKIN COMMON TO TEE FITTING AT BS 955. THE SKIN WAS REPAIRED. AIRPLANE WAS GROUNDED.SDR ABXA20170511058Skin · corrodedCORROSION ON SKIN COMMON TO LEFT FAILSAFE STRAP AT BS 955. THE SKIN WAS REPAIRED. AIRPLANE WAS GROUNDED.SDR RAIA201705110001Skin · crackedSKIN CRACKED ABOVE STRINGER 2L FRAME 75. CUTOUT DAMAGE AND APPLIED FILLER AND DOUBLER .SDR REXA2017051100592Skin · corrodedWHILE REMOVING THE STRINGER SLICED 26R AT BS 333, FOUND CORROSION ON THE FUSELAGE SKIN. REMOVED DAMAGE AND REPAIRED THE SKIN IAW EA CRJ953-05653.
"SDR DALA2017051203838Skin · crackedCRACK IN FUSELAGE NEAR AFT AIR STAIRS DOOR CUTOUT LEFT SIDE MID POINT, BS 1531. REPAIRED IAW SRM 53-0001.SDR DALA2017051203815Skin · crackedCRACKS ON PRODUCTION DOUBLER UPPER SKIN STA Y=1176 CANT BTW LONGS 3L TO 3R AFT ACCESSORY COMPARTMENT. CRACK ON PRODUCTION DOUBLER UPPER SKIN STA Y=1176 CANT BTW LONGS 1 TO 3 LT AFT ACCESSORY WAS REPAIRED PER SRM 53-30-08-2R PROCEDURE 10 REPAIR 10. HFEC INSPECTSDR FDEA201705111396Skin · dentedDURING A WALK AROUND INSPECTION, FOUND A DENT IN THE FUSELAGE, 14 INCHES FWD OF THE ACCESSORY DOOR. INSTALLLED A REPAIR IAW 53-20-00.SDR ASOA201705101591Doubler · corrodedTCAS DOUBLER CORRODED BETWEEN FS 295- FS 310. REMOVED STRINGER, RECEIVED AND LOCATED HOLES IN NEW STRINGER AND INSTALLED PER SRM 51-42-06-001-001-A01.SDR DALA2017051103887Skin · dentedAFT LOWER FUSELAGE SKIN, BS 1701+7, BETWEEN STRINGERS 28 AND 29R, HAS TWO DENTS. REPAIRED THE SKIN IAW ER/A 557227-14, REV 0, AND RE/A 557224-14 REV ORIGINAL.SDR ASOA201705101562Skin Panel · damagedSKIN DAMAGED BETWEEN FS 1015-1031 AND BETWEEN STR 14R-15R. C/W EC/TC EO900-53-30-00001 REV A. C/W WITH EC/TC EO900-53-30-00001SDR ASOA201705101560Skin Panel · damagedSKIN DAMAGED BETWEEN FS 1015-1031 AND BETWEEN STRINGER 14R-15R. COMPLIED WITH EC/TC EO 900-53-30-00001.SDR AALA20170510004Skin · crackedNOSE LANDING GEAR AFT FOLLOW UP DOOR IS CRACKED AT THE RIGHT AFT CUT OUT. REPAIRED IAW SRM 53-05-00-001 AND SGO9530030.SDR DALA2017051103771Skin · corrodedCORROSION ON FUSELAGE SKIN FROM BS 1874 TO 2033.5 BETWEEN STRINGERS 43 AND 44L. REPAIRED IAW ERA 558381-14, REV ORIGINAL.SDR DALA2017051103770Skin · damagedDAMAGE ON FUSELAGE SKIN AT BS 2022 BETWEEN STRINGERS 43 AND 44L. REPAIRED IAW SRM 53-00-01, REPAIR 7.SDR SWAA2022012479171Scuff Plate · crackedAFT CARGO BAY FWD SCUFF PLATE CRACKED / REPAIRED AFT CARGO BAY SCUFF PLATE IAW EA 1 A53-2076 REV 11SDR SWAA2022012466301Scuff Plate · crackedFWD CARGO; FWD CORNER THRESHOLD CRACKED / FWD CORNER THRESHOLD REMOVED AND REPLACED IAW AMM 53-11-02. REFERENCE WIP'S AND TASKS BELOW FOR INDIVIDUAL SIGN-OFFS.SDR SWAA2022012498146Door · crackedEXT ELECTRICAL DOOR AFT LANDING HAS CRACK AT RIVET HOLE FOR LANDING PAD / REMOVED DAMAGE AREA OF EGPR DOUBLER PER SRM 53-10-15-2R-4 REPAIR 4. PERFORMED HFEC OF CUT OUT AREA PER NDT PART 6 51-00-00 PROC 23. NO DEFECTS NOTED. FABRICATED REPAIR PARTS; TREATED ANDSDR DALA2020120804002Skin · damagedEVIDENCE OF REWORK EXTERNAL SKIN LOCATED AT FR 24A+5" LEVEL OF STGR 41L ON LOWER FUSELAGE. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR ON EXTERNAL SKIN LOCATED AT FR 24A+5" AT LEVEL OF STR 41L ON LOWER FUSELAGE, AS PER A320 FAM SRM 53-00-11-300-042.SDR DALA2017051003833Skin · corrodedCORROSION BELOW PRODUCTION DOUBLERS AT MID CARGO COMPARTMENT DOOR. REPAIRED IAW ERA 558092-14, REV O AND ETI 90-17-038 REV O. (LP# 0013408)SDR DALA2017051003832Doubler · crackedAFT ACCESSORY COMPARTMENT CRACKED INNER FUSELAGE PRODUCTION DOUBLER, BS 1520 BETWEEN LONGERON 3R TO 2R. REPAIRED IAW SRM 53-10-03, ETI 90-17-030 AND ERA 558299-14.SDR DALA2017051003829Doubler · crackedAFT ACCESSORY COMPARTMENT CRACKED INNER FUSELAGE PRODUCTION DOUBLER, BS 1520, BETWEEN LONGERONS 3R TO 2R. REPAIRED IAW ETI 90-17-030 AND ERA 558099-14 REV O.SDR SWAA2022012431295Scuff Plate · crackedMID THRESHHOLD FAR AFT CARGO DOOR IS CRACKED AT FWD EDGE MEASURING 3' IN LENGTH. MOD / INSTALLED NEW SERVICEABLE THRESHOLD BULLNOSE PER 53-11-02SDR AALA201705129029Skin · crackedAIRCRAFT BELLY HAS A 1 INCH CRACK BELOW THE AFT CARGO FLOORING OPENING AT BS 1219, STRINGER 39L. REPAIRED IAW SRM 53-00-01-2R-1. AIRCRAFT WAS GROUNDED.SDR FDEA201705081372Skin · dentedDENT ON EXTERIOR UPPER FUSELAGE BS 453, STRINGER 7R. REPAIRED IAW EA F-5330-T0333088 P1, AND SRM 53-00-01-2R, REPAIR 15.SDR DALA2017050903748Skin · nickedNICK ON RIGHT HAND EXTERNAL FUSELAGE SKIN, STA 1542 CANT PROJECTIONS L17R. FOUND TO BE OUT OF LIMITS. REPAIRED IAW SRM 51-31-02 AND 53-31-02.SDR DALA2017050903746Skin · crackedFUSELAGE SKIN CRACK AT NOSE STRUT DOOR AFT HINGE RIGHT HAND SIDE. IN WORK/FIXED.SDR DALA2017050903684Skin · damagedSUNKEN FASTENERS ON REPAIR DOUBLER ON THE SKIN AT BS 200 AND 218, LONGERON 26L. THE REPAIR WAS REPLACED IAW SRM 53-04-3, FIG 10.SDR DALA2017050803627Skin · wornWORN OUT DOUBLER AND HOUSING OF HOLD OPEN HOOK AT FWD PASSENGER ENTRY DOOR. DOUBLER WAS REPLACED IAW SRM 52-05 FIG 20A. HOUSING WAS BLENDED OUT AND MEASURED IAW SRM 52-01 PAR 3 FIG 1 AND (UT) WAS ACCOMPLISHED ON HOUSING IAW NDT SPM 04-00-07 PAR. 5 FIG.3 (SHEETSDR DALA2017050803625Skin · damagedDURING INSPECTION, AN INDICATION OF MATERIAL THINNING 0.051, SKIN. REMAINING WAS FOUND AT BS 580, L29R, JUST FWD OF PREVIOUS REPAIR. FUSELAGE SKIN WAS REPAIRED IAW ER/A 558084-14, REV ORIGINAL.SDR SWAA2017051613718Skin · dentedEXTERNAL FUSELAGE SKIN DENTED AT BS 380, BETWEEN STR 16L TO STR 17L. REPAIRED SKIN PER EA AND ER.SDR ASOA201705061556Doubler · corrodedTCAS ANTENNA INTERNAL DOUBLER BETWEEN FS 295.00 AND 310.00, NEAR STRINGER 27 IS CORRODED. REMOVED AND REPLACED TCAS ANTENNA INTERNAL DOUBLER BETWEEN FS 295.00 AND 310.00 NEAR STRINGER 27 IAW SRM 51-42-06-001-001 A01.SDR DALA2017050703652Skin · crackedHFEC INSPECTION FOUND ONE CRACK ON THE SKIN ALONG THE EDGE OF THE COVER PLATE AT BS 687 BETWEEN STRINGERS 36 AND 37R. REPAIRED IAW SRM 53-00-01.SDR DALA2017050703651Skin · crackedHFEC INSPECION FOUND ONE CRACK ON THE SKIN ALONG THE EDGE OF THE COVER PLATE AT BS 687 BETWEEN STRINGERS 36 AND 37R. DAMAGE CUT OUT IAW SRM 53-00-01. NO CRACK FOUND AND REPAIRED THE SKIN.SDR SWAA2022012117766None · corroded***CORROSION*** ASD MOPSILL BS947-986 RBL65. / REMOVED MOPSILL CORROSION ASD BS 947 TO BS 986 RBL 65. ORIGINAL THICKNESS 0.080'. REMOVED CORROSION AREA 5'X1.5' REMAINING THICKNESS 0.065' FOUND TO BE OUT OF LIMITS IAW SRM 53-70-15-1A-1 STEP 4 FIG 103 DETAIL D. SDR SWAA2022012117767None · corroded***CORROSION*** AED MOPSILL BS947-986 LBL65. / REMOVED CORROSION ON MOPSILL AT AED BS 947 TO BS 986 LBL 65. ORIGINAL THICKNESS 0.080' REMOVED CORROSION AREA 12'X2'. REMAINING THICKNESS 0.060' FOUND TO BE OUT OF LIMITS IAW SRM 53-70-15-1A-1 STEP 4 FIGURE 103 DE
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