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 IPXA2018052129816Skin · dentedFUSELAGE SKIN DENTED JUST AFT OF BS 540, STRINGER 19L. REPAIRED THE SKIN IAW EO B757-5330-60844-B, PARAGRAPH 6.C.SDR SWAA2022021436514Skin · damagedFOUND DAMAGE TO SKIN BS 747+1.5 AND 1.75' ABOVE STR 22R / REPAIRED DAMAGED SKIN AT STA. 747+1.5 AND 1.75' ABOVE STR. 22R IAW ATS ER 18-02801 REV. IR AND SOUTHWEST EA REPAIR 53EA-05228 REV. 1SDR YENA201805190963Doubler · crackedDURING C3 CHECK AT LHT (BQN) ON 05/2018, CRACK INDICATION WAS FOUND ON 6 FASTENER HOLES ON THE LIVETV ANTENNA DOUBLER WHILE ACCOMPLISHING LFEC INSPECTION OF THE PEDESTAL DOUBLER (PN: K21105-001). SEE REF /1/ EO FOR MORE DETAILS. LHT REACHED OUT TO THALES FOR RSDR SWIA2018052944733Skin · corrodedLOWER EXTERNAL FUSELAGE SKIN HAS CORROSION AT MATING SURFACE FOR WING TO BODY PANEL, BS 409+96, BL 0. BLENDED CORROSION IAW SRM.SDR YENA2018052280211Skin · deformedDURING HEAVY MAINTENANCE, REAR FUSELAGE JACKING POINT AREA AT FRAMES 73 - 74, STRINGERS 30L - 30R SKIN & ANGLES DEFORMED. REPAIRED.SDR RU3A201805218017Skin · crackedCRACK IN THE LOWER FUSELAGE SKIN. PERFORMED MAJOR REPAIR EO 18-28-31.SDR QU2R20180518001Skin · damagedAIRCRAFT SKIN DAMAGED, FRAME 33 LOWER SECTION. THE DAMAGE IN TWO AREAS BEYOND LIMITS. FABRICATED AND INSTALLED A REPAIR DOUBLER.SDR SWIA2018061444776Skin · dentedFOUND A DENT JUST FWD OF BS 549 JUST BELOW STRINGER 16L. DRESSED DENT BACK TO CONTOUR IAW REO. NO LEAKS NOTED.SDR R61A201805170606Skin · dentedWHILE OUT OF SERVICE IN HEAVY CHECK, MAINTENANCE FOUND DENT ON EXT FUSELAGE SKIN AT FR96 BETWEEN STR3R AND STR4R. MEASURED DENT ON EXT FUSELAGE AT FR 96 BETWEEN STR 3R & 4R, FOUND DENT TO MEASURE WIDTH 1.8" LENGTH 2.2" AND DEPTH 0.050" AND WITHIN LIMITS. PERFOSDR ASAA201805214687Skin · corrodedFUSELAGE SKIN, BS 917, STRINGER 19L, AROUND THE AFT LAVATORY VENT WAS FOUND CORRODED. ACFT GROUNDED. REMOVED THE CORROSION, AND FOUND THE SKIN TO BE ACCEPTABLE FOR CONTINUED SERVICE IAW EA 800-53EA-20323.SDR AALA20180517006Skin · crackedAIRCRAFT IN BASE MAINTENANCE. CRACKED FUSELAGE SKIN AT CANT STATION 1437, LONGERON 2 RIGHT TO LONGERON 4 RIGHT. REPAIRED FUSELAGE SKIN PER SRM 53-04-00-001 FIGURE 27 AND EA 280672.SDR DALA2018051803428Strap · corrodedCORROSION STRAP UNDER LONGERON 26L BTW STA Y=946 TO Y=1002 AT AFT CARGO COMPARTMENT. NEW REPAIR PART WAS INSTALLED PER SRM 51-41-02-0G.SDR DALA2018051803427Skin · crackedCRACK ON EXTERNAL FUSELAGE SKIN STA Y=1037 BTW LONG 13R-14R. PERMANENT REPAIR WAS ACCOMPLISHED PER ETI-17-18-078 R5 AND ER/A 568647-14 REV ORIGINAL.SDR DALA2018051803423Doubler · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE INTERNAL DOUBLER OF THE AFT LAVATORY SERVICE PANEL. THE DOUBLER WAS REPAIRED IAW ERA 568604-14, REV ORIGINAL, AND ETI-88-18-049, REV 1.SDR SWIA2018061444774Skin · dentedDENT FOUND ON BOTTOM FUSELAGE SKIN APPROXIMATELY 30 INCHES AFT OF AEB DOOR. INSTALLED A DOUBLER IAW REO.SDR ASAA2018061164983Bulkhead Web · crackedPRESSURE BULKHEAD WEB AT BS 663 WAS CRACKED IN THE MACHINED POCKET BETWEEN RBL 37 AND RBL 45. ACFT GROUNDED. REPAIRED THE BULKHEAD WEB IAW SRM 57-10-10-2R-3.SDR R61A201806090681Skin · dentedMAJOR REPAIR, FUSELAGE EXTERNAL SURFACE HAS A DENT BETWEEN FR 29 AND FR 30 STR L3 AND L4 5" X .5". REMOVED DENT BY CUTOUT ON FUSELAGE EXTERNAL SURFACE AT FR 29 AND FR 30 STR L3 AND L4 AND PERFORMED PERMANENT DOUBLER REPAIR, REF SRM 53-21-01 R10, 51-75-17. SEESDR COEA2018004628819Skin · dentedDENT ON THE SKIN, BELOW STRINGER 17R AND BETWEEN FRAMES 19 - 20. REPAIRED THE SKIN IAW SRAS ES-2584/18.SDR ASOA201805167081Skin · crackedDURING A C CHECK, FOUND THE LT FUSELAGE SKIN CRACKED AT FRAME 75, STRINGER 1L TO 2L, VERIFIED BY SOP 5711, NDT. REPAIRED IAW SRM 53-31-01.SDR ASOA201805167080Skin · crackedDURING A C CHECK INSPECTION, FOUND THE RT FUSELAGE SKIN AT FRAME 75, STRINGER 1R CRACKED. VERIFIED WITH NDT.SOP 5711. REPAIRED THE SKIN IAW SRM 53-31-01.SDR ABXR2018051670147Skin · crackedRIGHT FUSELAGE EXTERNAL SKIN IS CRACKED AT BS 1725.5, STRINGER 7R.SDR ASOA2018053155141Skin · dentedDENT ON THE SKIN BETWEEN BS 477.4 - 485, STRINGERS 14L - 15L. REPAIRED THE SKIN IAW SRM 53-00-01-201-004-A01, AND EC/TC FUR-53-00-00961.SDR R61A201805150620Skin · dentedWHILE AC WAS IN FOR HEAVY CHECK, REF FINAL REPAIR OF DMI R320057/1 DENT PER ETD2017-170-018619 REV A. PER CUSTOMER TASK CARD R320065/1 (RE-INSPECT) MX PERFORMED PERMANENT REPAIR AT FUSELAGE SKIN 6" FWD OF FR 23 AND 3" BELOW ST 14L, IAW ETD2017-170-018619 REV ASDR R61A201805150613Skin · dentedWHILE AC WAS IN FOR HEAVY CHECK, ACCOMPLISH ETD2017-170-018619 REWORK OF DENT LOCATED AFT OF L1 DOOR BETWEEN FR 20 AND FR 23 STR 14L PER LOG PAGE R320057/1. MX ACCOMPLISHED PERMANENT REPAIR OF DENT IN SKIN LT SIDE AFT OF L1 DOOR IAW SRM 51-10-05 ITEM 10 AND ETSDR IPXA2018052529992Skin · corrodedCORROSION FOUND ON THE FUSELAGE SKIN AT BS 1410 , BETWEEN STRINGERS 38R - 39R. REPAIRED IAW SRID 4-4086081329, AND EO B767-5330-68618-A.SDR IPXA2018052530008Skin · dentedFUSELAGE SKIN DENTED BETWEEN BS 1681 - 1701, LONGERONS 34R - 35R. ACCOMPLISHED A PERMANENT REPAIR IAW EA 011-5330-01-A7280, REV IR, AND EO MD11-5330-68624-A.SDR DALA2018051603404Splice Strap · corrodedAFT CARGO BAY STA 1400 BETWEEN STR 29R-27L, SKIN SPLICE STRAP IS CORRODED. REMOVED AND REPLACED SPLICE STRAP IAW SRM 51-40-02 AND DWG 146N3300 REV H.SDR ASOA2018051855131Skin · damagedDENT, AND SCRATCH ON THE FUSELAGE SKIN BETWEEN BS 477.4 - 485, STRINGER 14L - 15L. REPAIRED THE SKIN IAW SRM 53-00-01-201-004-A01.SDR DALA2018051603371Doubler · corrodedCORROSION ON SEVERAL POINTS ON EXTERNAL SKIN AT FUSELAGE EXTERNAL DOUBLER FROM STA Y=851 TO STA Y=870 BTW LONG 27L AND 27R. CORROSION LEVEL 2, DOUBLERS WERE REPLACED PER SRM 53-20-70-2R REPAIR 1.SDR VNAA2018051599901Skin · crackedFORWARD FUSELAGE SKIN IS CRACKED AT THE LT TRU DOOR AFT LATCH LOCATION. REMOVED AND REPLACED DOOR LANDING IAW SRM 51-42-06 AND 51-42-13.SDR CALA2018051501293Skin · crackedFOUND ONE CRACK ON THE SKIN AT BS 2195.75, BETWEEN STRINGERS 6R AND 7R. AREA TRIMMED OUT IAW DWG 624W0013, SHEET 1, REV B, AN HFEC INSPECTION WAS CARRIED OUT IAW NTM, PART 6, 51-00-01, PROC 2. NO CRACK FOUND. REPAIRED IAW EA 5300-01986, OP 10.SDR CALA2018051501292Skin · crackedFOUND ONE CRACK IN THE SKIN BS 2221.65 BETWEEN STRINGERS 9L AND 10L. AREA TRIMMED OUT IAW DWG 624W0013, SHEET 2, REV B, AN HF EC INSPECTION WAS CARRIED OUT IAW NTM, PART 6, 51-00-01, PROC 2, NO CRACK WAS FOUND. REPAIRED IAW EA 5300-01986, OP 08, L/P 9.SDR DALA2022030401410None · noneSHIP 1817 FUSELAGE SKIN CRACKED AT STA 1661 STR 13R INSP PER AMDS 5330- 01229-01B END OF CRACK MARKED, CORRECIVE ACTION: C/W HFEC INSPECTION OF CUTOUT EDGES AND EXISTING HOLES, INSTALLED REPAIR PER B767 SRM 53-80, REQUIRES REPETATIVE DETAILED VISUAL AND LFEC ISDR DALA2018101005977Skin · corrodedFUSELAGE SKIN, STA 750, L-30 CORROSION REPAIR, PERMANENT REPAIR. C/W ERA 455233-14 REV C, MON CLOSED.SDR DALA2018051503399Skin · dentedLT SIDE OF AFT FUSELAGE HAS PROTRUDING DENT APPROXIMATELY STA 1629 BETWEEN STRINGERS 24L AND 25L. REMOVED DENT AND REPAIRED IAW SRM 53-00-01 REPAIR 3. ADDITIONAL INSPECTIONS REQUIRED.SDR DALA2018051503397Skin · corrodedDURING INSPECTION, FOUND A BULGE IN THE SKIN & CORROSION AT THE AFT PRESSURE BULKHEAD JOINT, 7 OCLOCK POSITION. MAINTENANCE REPAIRED DAMAGE IAW ERA 568535-14, REV ORIG.SDR SWAA2022021612039None · crackedSUPPLEMENTAL INFORMATION: L1 DOOR THRESHOLD REVEAL PANEL CRACKED / REMOVED REVEAL. LOCATED & DRILLED NEW REVEAL IAW SRM 51-40-05 & DWG 141A8221; APPLIED PAINT IAW AMM 51-21-73; INSTALLED NEW REVEAL IAW DWG 141A8220 & SRM 51-40-02 57171U 22MAY18SDR DALA2018051403293Skin · crackedCRACK FOUND ON THE EXTERNAL SKIN BS 1022 BETWEEN LONGERONS 13L - 14L. REPAIRED IAW ER/A 568451-14, REV ORIGINAL, AND ETI-17-18-083, REV 3.SDR DALA2018051403261Skin · corrodedMAINTENANCE NOTED AN AREA OF CORROSION COMMON TO SECTION 47, FUSELAGE SKIN, AT THE FORWARD EDGE OF THE BS 1016 BUTT-SPLICE AND BETWEEN STRINGERS 21L AND 22L. REPAIRED IAW ERA 568535-14.SDR ASOA2018051825130Doubler · chafedPREVIOUS REPAIR DOUBLER BETWEEN BS 977 AND 985, STRINGER 27 EXTERIOR BELLY SKIN IS CHAFED 1.5''X.125''X.006''D. REPAIRED THE DOUBLER IAW ECTC REO 670-53-00-545, REV 0.SDR DALA2018051303365Skin · crackedAFT RT EXTERIOR FUSELAGE SKIN IS CRACKED AT STA 1642 AT STRINGER 14R ( VERIFIED WITH HFEC SURFACE SCAN). SRM REPAIR PER DWG 148T3131, SRM 53-00-01 REPAIR 1 STEP 5 THRU 10 AND INSTALLED REPAIR PARTS IAW SRM 53-00-01 REPAIR 1 STEP 12 THRU 16.SDR SWAA2022021687870Scuff Plate · crackedAFT CARGO PIT CENTER SCUFF PLATE CRACKED / AFT CARGO PIT CENTER SCUFF PLATE REPAIRED I/A/W SWA EA# 1-A53-2076 REV 11SDR SWAA2022021687871Scuff Plate · crackedAFT CARGO PIT FWD CORNER SCUFF PLATE CRACKED / AFT CARGO PIT FWD COVER SCUFF PLATE REPAIRED I/A/W SWA EA # 1-A53-2076 REV 11SDR 2018FA0000288Skin · corrodedALL EXTERIOR EDGE NUTPLATE FOR FORWARD BODY TO WING FAIRINGS, 191BB AND 192BB ARE CORRODED.SDR 7C7A201805150435Skin · dentedTHE BOTTOM FUSELAGE SKIN BETWEEN BS 240.5 - 270.5, STRINGERS 30S - 32S WAS DENTED. REMOVED THE DAMAGE AND REPAIRED IAW RD 8-53-15717 AND ECO 008.53-18.45.SDR SIMA2018052510008Skin · crackedFUSELAGE SKIN UPPER SPLICE PLATE BETWEEN FRAMES 80 AND 81 WAS CRACKED. PERFORMED A PERMANENT REPAIR IAW SRM 51-40-02SDR SIMA2018052510010Skin · crackedRIGHT UPPER FUSELAGE SKIN WAS CRACKED AFT OF FRAME 75 AND ABOVE STRINGER 2R, THE CRACK WAS APPROXIMATELY 1 INCH LONG . PERFORMED A PERMANENT REPAIR IAW SRM 53-31-01, FIG 219SDR 7C7A2018052200441Skin · damagedDAMAGE TO THE RH FUSELAGE SKIN PANEL. REPAIRED IAW RD 8-53-15756, AND ECO 008.53-18.48.SDR 7C7A2018051400410Skin · dentedRIGHT FUSELAGE SKIN PANEL BETWEEN BS 270.5 - 291.4, STRINGERS 17R - 18R DENTED. REPAIRED IAW RD 8-53-15713, AND ECO 008.53-18.33.SDR 7C7A2018051400412Skin · dentedDAMAGED RIGHT FUSELAGE SKIN PANEL BETWEEN BS 234.50 - 240.50, STRINGERS 14R - 15R. REPAIRED IAW RD 8-53-15715, AND ECO 008.53-18.29.
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