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 DALA2024110410603Skin · scratchedSHIP 3160 SCRATCH ON EXTERNAL SKIN LOCATED AT FR 20 BTW STR 26L TO STR 27L LOWER FUSELAGE. CORRECTIVE ACTION: COMPLIED WITH ER/A 621130-14. (0641576)SDR DALA2024110410602Skin · dentedSHIP 3160 DENTS ON EXTERNAL SKIN LOCATED BTW FR 69 TO FR 70 TW STR 22 R TO STR 23R LOWER FUSELAGE. CORRECTIVE ACTION: COMPLIED WITH ER/A 620969-14. (0641571)SDR 2024FA0000813Skin · corrodedCORROSION WAS FOUND AT FASTENER HOLES ON THE LOWER FUSELAGE EXTERNAL SKIN FS 422 WHERE THE LOWER FUSELAGE TO WING FAIRING ATTACHED TO THE FUSELAGE. AFTER REMOVAL OF THE CORROSION AND EVALUATION THE AFFECTED AREAS THE REMAINING SKIN THICKNESS WAS FOUND TO BE BSDR JR2R20241102800Skin · damagedFUSELAGE SKIN BELOW FWD SERVICE DOOR OPENING COVERD BY SCUFF PLATE HAS NUMEROUS SCRIBE MARKS. REPAIRSDR IPXA2024110905997Skin · corrodedCORROSION , FUSELAGE SKIN STA 1410 BETWEEN S-38R AND S-39R. ACCOMPLISH REPAIR PER EO-91974-REQ1 AND EGAT EI F2024A53M-2800, REV. 0 AND 1.SDR SIMA20241101002Skin · damagedDENT ON RH FUSELAGE AT THE JUNCTION OF FR03 AND STGR 13R. REF AML 106300064 (MAJOR REPAIR). INSTALLED REPAIR DOUBLER AND FILLER AT JUNCTION OF FR 3 AND STGR 13R IAW ERS-EJ-53MR-5083SDR DALA2024110410601Skin · scratchedSHIP 3160 SCRATCH WAS FOUND ON FUSELAGE SKIN AT FR20 BETWN STRG 26L AND Z-1055. CORRECTIVE ACTION: COMPLIED PER ER/A 621130-14. (0639424)SDR CALA2024121803114Skin · corrodedLAVATORY EXHAUST VENT EXTERIOR SURFACE HAS CORROSION WITH BULGING SKIN. REPAIRD EXTERIOR LAV VENT SKIN CORROSION WITH BULGING PER SRM 53 4453 NR 21473, -70-01-2R-3 REPAIR 3 SECTION 47 STA 917 CATEGORY B REPAIR & SUPP LEMENTAL INSPECTION THRESHOLD 50,000 F.C. ASDR IPXA2024111899922Skin · dentedLOWER FUSELAGE SKIN HAS DENT AT STA 440/456 AND STR 28/29. NO DOT TG-101. FABRICATED 1EA REPAIR DOUBLER AND 1EA FILLER TO ACCOMPLISHED E.A# 757-5330-27-A3725 PRELIMINARY 3 STEPS 15.A, 15.B AND 16. P/N: 2024-T3.063C BTCH: 4324672.SDR SWAA2024112655628Angle · crackedCRACK ANGLE - CLIP LOCATED ON BS 500A STR 26L AT FWD CARGO COMPARTMENT 2024-651173<[01] REPLACED ANGLE - CLIP LOCATED ON BS 500A STR 26L AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND INSTALLATION WILL BE DOCUMENTED ON TTG8Q00WG37W SEE INDIVIDUASDR SWAA2024112555322Skin · corrodedCORROSION ON EXTERNAL LOWER FUSELAGE SKIN COMMON TO ATC ANTENNA STA 351.50-357.50; BLO; WL 149.<[01] REPAIRED LWR SKIN COMMON TO ATC ANTENNA IAW EA 24-153-03031;[02] VERIFIED CORRECTIVE ACTIONSDR REXA2024112001504Skin · chafedIN REF TO: DURING INSPECTION OF THE TASK CARD 700-53-900-303 IT WAS DETECTED WEAR ON EXTERNAL LOWER FUSELAGE SKIN BTW FS 977.00 TO 985.00 AND STGR 26L-26R. WEAR ON EXTERNAL LOWER FUSELAGE SKIN BTW FS 977.00 TO 985.00 AND STGR 26L-26R WAS REPAIRED PER EA CRJ75SDR DALA2024110410626Skin · ground damageAIRCRAFT 3812, AIRCRAFT STRUCK BY GROUND VEHICLE AT FORWARD CARGO DOOR WHILE PARKED AT GATE. CORRECTIVE ACTION: REMOVED FASTNERS AND DAMAGED SKIN SECTION REF B737 53-00-01-2R- 23. PERFORMED HFEC OF CUTOUT AREA PER NDT PART 6 51-00-00. NO DEFECTS NOTED. FABRICASDR AALA202411262163Skin · wornAIRCRAFT IN BASE MAINTENANCE: WEAR MARK ON FUSELAGE SKIN INTERNAL SURFACE AT STA 277 PLUS 6 INCHES, FROM S2L TO S3L. ACCOMPLISHED DOUBLER REPAIR PER SRM 53-00-01-2R PROCEDURE 20.SDR IXXA2024111902Skin · crackedR-1 DOOR CUTOUT AFT LOWER CORNER IS CRACKED AT FASTENER HOLE IN FUSELAGE SKINSDR AALA202411062265Skin · corrodedACFT WAS GROUNDED: LARGE AREA OF SEVERE CORROSION APROX 2" X 1" AT BS 887 S27L. RIVET HEAD MISSING AN D SKIN CRACKED APROX 1" LENGTHWISE OF AC. MX FOUND CORROSION ON FUSELAGE SKIN UNDER SPLICE STRAP AT BS 887, FROM S24L TO S27R. ACCOMPLISHED DOUBLER REPAIR PESDR YENA2024103101419Skin · corrodedDURING HEAVY MAINTENANCE: FCCD SILL UNDER SCUFF PLATE FOUND (X5) PLACES OF CORROSION AROUND ATTACHMENT HOLES; REF TO AVIANOR WO 49144 NR 1023, FCCD SILL UNDERNEATH SCUFF PLATE TEMPORARY REPAIR CARRIED OUT I.A.W AC24-1249-01 AND I.A.W REO 500-53-21-099 REV E, DSDR YENA2024103101418Skin · corrodedDURING HEAVY MAINTENANCE: FCCD SKIN AROUND UNDERNEATH SCUFF PLATE FOUND (X9) PLACES OF CORROSION AROUND ATTACHMENT HOLES OF LOWER SCUFF PLATE; REF TO AVIANOR WO 49144 NR 1025, FCCD SKIN AROUND UNDERNEATH SCUFF PLATE TEMPORARY REPAIR CARRIED OUT I.A.W AC24-1251SDR YENA2024103101417Skin · corrodedDURING HEAVY MAINTENANCE: FCCD STRICKER UNDER SCUFF PLATE FOUND (X2) PLACES OF CORROSION AROUND ATTACHMENT HOLES; REF TO AVIANOR WO A49144 NR 1024, FCCD FWD AND AFT LOWER CORNER STRICKERS CORROSION PERMANENT REPAIR CARRIED OUT IAW AC24-1262-01 AND IAW GREO 500SDR YENA2024103101415Skin · damagedDURING HEAVY MAINTENANCE: FUSELAGE / MID FUSELAGE / REAR BARREL / LOWER SKIN FR 57-58 AND STGR 36L / CORROSION - TIME LIMITED REPAIR; REFERENCES: /1/ AIRBUS CANADA REO 500-53-51-200 /2/ AVIANOR DAMAGE REPORT A49144-1096 /3/ ASRP BD500-A-J53-61-01-04AAB-661A-A SDR DALA2024103110526Skin · crackedCRACK ON SKIN ON CUTOUT OF RH SLIDING WINDOW AT COCKPIT (UPPER AFT CORNER). SUMMARY OF NRC 00355: SKIN ON CUTOUT OF RH SLIDING WINDOW AT COCKPIT (UPPER AFT CORNER) WAS REPAIRED PER B717-200 SRM 56-10-02-2R PROCEDURE 1 REPAIR 1 PAR 5 FIGURE 201. (LP #0636659)SDR DALA2025111708390Skin · dentedRAMP REPORTS DENT. RH FUSELAGE. FUSELAGE SKIN ON STA 680 STGR 24R WAS REPAIRED PER B757-200 SRM 53-00-01-2R REPAIR 29. (6466766)SDR HNAA2024120101137Doubler · dented53-2045 DENT AT FWD OF REPAIR DOUBLER AT BTW FR24-25 AT STR21L.. REPAIRED IAW EO1-53-24-0666SDR DALA2024111410944Skin · deformedSHIP 3236 DISC: SKIN DEFORMATION FOUND BETWEEN FRAME 72-74 AND STRINGER 33L-32L. C/A: ACCOMPLISH ER/A 14-621564 REV B SECTION V: ONE-TIME INSPECTION 2 WITHIN TWENTY-FIVE (25) CALENDAR DAYS AFTER ACCOMPLISHMENT OF SECTION I, ACCOMPLISHED ON 10-OCT-24. ASSOCIATESDR ASAA2024102953728Skin · corrodedFUSELAGE SKIN AROUND WATER SERVICE PANEL CUTOUT HAS SIGNS OF CORROSION. GROUNDED - YES. FUSELAGE SKIN-WATER SERVICE CUTOUT STA 907 TO STA 927 S-25R TO S-27R - CORROSION REPAIR, MAJOR REPAIR WAS ACCOMPLISHED IN ACCORDANCE WITH EA 800-53EA-27818.SDR ASAA2024102953724Skin · corrodedBUTT-JOINT AT STA 887 BETWEEN STGR 23R-23L HAS SIGNS OF CORROSION. GROUNDED - YES. ACCOMPLISHED CATEGORY B MINOR REPAIR TO FUSELAGE SKIN PANEL 146A3231-23 AND 147A3400-4 AT STA 887 BETWEEN STGR 23L-23R IAW EA 800-53EA-27825 REV 00.SDR ASAA2024102953723Skin · corrodedLAP SEAM BETWEEN STA 887-907 STGR 23L HAS SIGNS OF CORROSION. SRXR430X. GROUNDED - YES. ACCOMPLISHED CATEGORY B MINOR REPAIR TO FUSELAGE SKINS 14743400-4 AND 147A3110-3 AT STA 887-907 STGR 23L IAW EA 800-53EA-27824 REV 00. SRXR430X.SDR JR2R20241101394Skin · dentedSKIN DAMAGED UST O/B OF REAR JACK PAD ON RH SIDE OF FUSELAGE DURING DOWN JACK. REPAIREDSDR REXA2024103001170Doubler · chafed"CHAFF MARK F.S. 913-927 STR27 IN DOUBLER REMOVED DAMAGE DOUBLER ON FUSELAGE SKIN AT F.S. 913 - F.S. 927 STGR 27, IAW CRJ 900 SRM 51-42-21-001-001-A01. FABRICATED, LOCATED AND DRILLED NEW SERVICEABLE DOUBLER FROM FUSELAGE SKIN AT F.S. 913 - F.S. 927 STGR 27,SDR IPXA2024103027032Skin · pilot errorSDR FILED OPEN, TAIL STRIKE.SDR SWAA2024112754235Stub Frame · crackedCRACK UPPER STUB FRAME BS 294;5 AND BETWEEN STR 9R TO STR 10R PASS CABIN 2024-672399<[01] REPLACED STUB FRAME AND FASTENERS LOCATED ON BS 294.5 BETWEEN STR-7R TO STR-11R IAW B737-700 SRM 51-40-02-0G-0;SRM 51-10-02-0G-0 AND DWG: 141A8370 SHEET: 9 AND 10 REV: D<SDR CALA2024112701323Skin · corrodedFOUND CORROSION ON EXTERIOR SKIN AROUND LAV PAN OPENING AFTER OUTER LAV PAN REMOVAL.ADDED 3EA PICS. BLENDED OUT CORRODED LOWER SKIN REF SRM 51-10-02. THICKNESS OF SKIN REMOVED IS BEYOND ALLOWABLE LIMITS. ACCOMPLISHED STEPS 1. THROUGH 5. OF AVO 13590. REQUEST ISDR SWAA2024112554366Skin · corrodedCORROSION ON EXTERNAL FUSELAGE SKIN UNDER VERTICAL STAB BS1016 - BS1033 LBL12 TO RBL12 WL308. MARKED<[01] COMPLETED CARD;[02] ACCOMPLISHED PER EA 24-153-03047-;[03] VERIFIED CORRECTIVE ACTIONSDR CALA2024110502795Skin · damagedLIGHTNING STRIKE AT STA 1746 STR 37 REMOVED THE "QUICK ACCESS" PANEL FOR SHEET METAL ACCESS BLENDED AREA SRM 5300-01-2R-8. READY FOR NDT. APPROXIMATELY STA 1700.1900 PERFORMED NDT INSP PER PART 6, 51-00-08. BLENDED AREA HAS CRACK LIGHTLY BLENDED AREA SRM 5300-SDR FDEA202410281596Skin · crackedFREIGHT ULD HIT AIRCRAFT AND CREATED A HOLE ON R/H OF A/C AFT OF AFT CARGO DOOR UPDT 25OCT24 08:28 EWR SRM 53-00-00-0G DAMAGE FOUND AROUND STATION 1608 (SECTION 46) . DAMAGE DIMENSIONS ARE 10 FROM FWD TO AFT AND 9 FROM TOP TO BOTTOM WHILE BEING 2 1/SDR SWIA20241027Skin · gougedTRANSFER FROM EAML 1458910 : IN REFERENCE TO EAML# 1458203, 1458228. DAMAGE DESCRIPTION AFTER INSPECTION.MULTIPLE GOUGES/NICKS (MAXIMUM OF 100-OFF LOCATIONS, REF)AND DENTS (9-OFF LOCATIONS, REF) TO FUSELAGE SKIN (DWG: 601R35005, 0.058€? +/-0.002€? THK PAD UPSDR DALA2024103110542Doubler · corroded(LOG 0632681) FWD CARGO COMPARTMENT INSTALLED DOUBLER BETWEEN STA 500C-500D BETWEEN S-27R TO S-27L HAS EVIDENCE OF CORROSION. REMOVED DAMAGED (CORRODED) DOUBLERS LOCATED BTW STA 500C - 500D BTW STR 27R TO STR 27L. FABRICATED AND INSTALLED NEW DOUBLERS PER B737SDR FDEA202410271583Skin · corrodedRIGHT HAND AFT FUSELAGE EXTERNAL SKIN SURFACE FOUND CORROSION BETWEEN STATION 2150 TO 2163. EMPENNAGE : RIGHT HAND AFT FUSELAGE EXTERNAL SURFACE BETWEEN STATION 2150 TO 2163 CORROSION AREA REPAIR CARRIED OUT AS PER MD-11 SRM 53-70-01-2R REPAIR 3 FIGURE 2SDR SWAA2024112753519Stub Frame · crackedCRACK LOWER STUB FRAME BS 294.5 AT LEVEL STRINGER 17R PASS CABIN 2024-672285<[01] REPLACED LOWER STUB FRAME LOCATED BS 294.5 BETWEEN STR 13R TO STR 17R IAW B737-700 SRM 51-40-02-0G-0; SRM 51-10-02-0G-0 AND DWG 141A8370 SHEET: 9 AND 10 REV: D. SEE INDIVIDUAL SISDR SWAA2024112753521Angle · crackedCRACK ANGLE BS 867 BETWEEN STRINGER 1R TO STRINGER 2R AT PASSENGER CABIN 2024-672296<[01] REPLACED ANGLE BS 867 BETWEEN STRINGER 1R TO STRINGER 2R AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9; B737-700 SRM 51-40-02 AND DRAWING 146A7901 SHEET 58 REV - MESDR DALA2024110110569Skin · damagedSHIP 3353 DAMAGE NOTED RH FUSALAGE APPROX 1FT BELOW & 2FT FWD OF 2R DOOR. CORRECTIVE ACTION: COMPLIED WITH ERA 621925-14 REV O. (4014104)SDR DXTA2024103000969Skin · damagedBIRD STRIKE AT 250 KNOTS ON APPROACH - STRIKE OCCURRED JUST UNDER THE COPILOT-SIDE WINDSCREEN REPLACED RH NOSE SKIN IAW BOMBARDIER SRPSA 000733079.SDR DALA2024102810471Skin · scratchedSHIP 3117 SCRATCH BELOW THE DOOR 1L THRESHOLD. CORRECTIVE ACTION: PERFORMED REPAIR PER A319 SRM 53-11. (4005998)SDR SWIA202506301025Skin · damagedFUSELAGE BELLY SKIN AND STRUCTURE AT AFT NLG BAY BULKHEAD AT FS 235.00 TO FS 250.00 AND BETWEEN STRINGERS 26L TO 26R DAMAGED DUE TO CONTACT WITH NLG ASSY. (FILED CLOSED)COMPLIED WITH REO 601R-53-11-3953 REV -- DATED: 2024-12-13 AND ISE-STR-24-077 SHORING MEMOSDR R61A2024110700528Doubler · corrodedWASTE BOX DOUBLER CORRODED IB OF BOX. REMOVED AND REPLACED WASTE BOX DOUBLER REF SRM 51-40-08.SDR ABXA20241025206Skin · damagedDURING CK C5 AT KALITTA EVIDENCE OF LIGHTNING STRIKE ON UPPER HALF FUSELAGE EXTERIOR RIGHT APPROX STA 300 AND S-2, TD35 REPAIR - FUSELAGE SKIN (SECTION 41 ), FULLELAGE SKIN REPAIR BETWEEN CANTED STA 303 AND CANTED STA 325, BETWEEN STRINGERS STR-2R AND STR-3RSDR ABXA20241025205Skin · damaged"DURING CK C5 AT KALITTA EVIDENCE OF LIGHTNING STRIKE ON UPPER HALF FUSELAGE EXTERIOR LEFT APPROX STA 300 AND S-1, TD34 FUSELAGE SKIN PAMAGE AT STRAP WE ARE SEEKING REPAIR OR RELIEF ON THE UPPER FUSELAGE SKIN JUST FORWARD OF STATION 368, WE HAVE TWO BELNDOUSDR ABXA20241025204Skin · damagedDURING CK C5 AT KALITTA EVIDENCE OF LIGHTNING STRIKE ON UPPER HALF FUSELAGE EXTERIOR LEFT APPROX STA 654+110 AND S-1, TD18 WE NEED A REPAIR FOR DAMAGE TO THE UPPER SKIN AND TEAR STRAP. WE CUTOUT DAMAGE ON A SKIN AND TEARSTRAP AT STATION 654+110 BETWEEN STRINGSDR DALA2024102810454Skin · dentedSHIP 3160 DENTS ON EXTERNAL SKIN LOCATED BTW FR 16 TO FR 17 LEVEL STR 32L LOWER FUSELAGE. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR AS PER A319 SRM 53-11-11-300-041. (0627385)SDR CALA2024102802747Skin · dentedDENT ACROSS STRUCTURE LOCATED AT BS 727F & JUST ABOVE S20R EXTERNAL SKIN PERFORM STEPS E 1-4 AFTER BAG BIN ACCESS NO DAMAGE FOUND TO UNDERLYING STRUCTURE REMVED FASTNERS NEED TO COMPLY WITH REPAIR 4 STEP E (1) (2) (3) EWIS COMPLIED WITH AT STA.727F SEE REF. A
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