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 2016FA0000025Doubler · crackedFORWARD AND AFT COMM ANTENNA DOUBLERS AND SKIN CRACKED.SDR 2016FA0000024Doubler · crackedSKIN AND DOUBLER CRACKING UNDER AFT COMM ANTENNA. FOUND DOUBLER TOO SMALL AND THIN.SDR DALA2016102510212Skin · gougedFUSELAGE SKIN L-1 PASSENGER DOOR DENT AND GOUGE. REPAIRED PER ERA 532474-14.SDR DALA2016102607662Doubler · corrodedLOWER FUSELAGE ANTENNA INTERNAL DOUBLER IS CORRODED AT FS 212 BETWEEN L229L & LONGERON 30 IN E&E COMPARTMENT. APPLIED TOP COAT ON AREA IAW AMM 51-10-00 701. REMOVED CORROSION FROM INTERNAL DOUBLER STA 212 BETWEEN 629L & L30L IAW SRM 51-10-04. NO LIMITS IN SSDR ASAA2016011915324Skin · crackedFUSELAGE GROUND AIR CONDITION DOOR CUTOUT SKIN ON RT SIDE IS CRACKED. ACFT GROUNDED. REPAIRED FUSELAGE SKIN AT THE GROUND AIR CONDTION DOOR CUTOUT IAW SRM 53-30-01-2R-2, REPAIR 2.SDR UHLA201601190035Skin · gougedSEVERAL GOUGES ON AFT CARGO DOOR LOWER CUTOUT. R & R AFT CARGO DOOR LOWER CUT-OUT BEAM IAW SRM 51-40-02, 51-41-01, AND 51-43-01.SDR SWAA2016012048184Skin · corrodedSKIN CORRODED IN AFT CARGO THRESHOLD SCUFF PLATE DOME NUT HOLES. REPAIRED SKIN EA.SDR FDEA201601190198Skin · dentedSKIN DENTED & CREASED AT BS 465, STRINGER 22R - 23R. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01 FIG 101 DETAIL III. REPAIRED IAW SRM 53-00-01 FIG 201 R16. THIS IS CATEGORY B REPAIR. MAJOR REPAIR.SDR SWAA2016012148259Skin · crackedFUSELAGE SKIN CRACKED AT BS 259.5+12, STRINGER 15L. REPAIRED SKIN IAW EA.SDR FDEA201601180183Skin · corrodedFORWARD CARGO, BILGE AREA , CORRODED AT STATION 824, LONGERON 51R & 52. NR 532 APPLIES TO THIS REPAIR. REPAIRED FWD CARGO BILGE IAW EA 8-5330-T0322604 PART 1.SDR DALA2017020901116Skin · corrodedDURING WALK AROUND FOUND FUSELAGE SKIN CORROSION AT STA 1583 BETWEEN S-25R AND S-25L. REPAIRED PER ERA 543061-14.SDR DALA2016011800415Skin · wornWEAR ON BS 1309, LONGERON 19R OUTER FUSELAGE SKIN. REPAIRED IAW SRM 53-04-2, FIGURE 2, SHEET 3.SDR COEA2016011649801Skin · damagedHEAVY CHECK COE & MAJOR REPAIR. FUSELAGE CROWN HAS TWO CREASES, BETWEEN FRAMES 37 - 38, ABOVE AFT CARGO DOOR RAIN TROUGH. REPAIR IAW SRAS S536R0259 10017 DATED 2 26 16.SDR COEA2016011648801Skin · corrodedDURING HEAVY CHECK, FUSELAGE LT LATERAL UPPER SKIN PANEL HAS TWO CREASES, BETWEEN FRAMES 37 - 38, ABOVE AFT CARGO DOOR RAIN TROUGH. REPAIRED IAW SRAS S536R0259 10017. MAJOR REPAIR.SDR SWAA2016020548741Skin · crackedFUSELAGE SKIN CRACKED AT BS 500A+12, STR 3L. REPAIRED SKIN IAW EA.SDR SWIA201641777Skin · corrodedEXTERNAL FUSELAGE SKIN CORRODED UNDER ADF ANTENNA BETWEEN FS 409+64 AND FS 409+84, STRINGERS 1L AND 1R. C-CHECK, NOT RELEASED YET, WORK IN PROGRESS.SDR DALA2016011700412Skin · crackedRUN CRACK ON EXTERNAL FUSELAGE SKIN BS 100 BETWEEN LONGERONS 27 - 28R. HFEC INSPECTION WAS PERFORMED ON EXTERNAL FUSELAGE SKIN BETWEEN LONGERONS 27RT -28RT, BS 100 AND WAS FOUND A CRACK OF 0.375" LENGTH IAW NDT SPM 06-10-01.001. CRACK WAS STOP DRILLED WITH 0SDR DALA2016011700410Doubler · wornWORN DOUBLER, TITANIUM, ON AFT LAVATORY PANEL BS 1287-1309. DOUBLER WAS FABRICATED IAW SRM 51-30-2, 51-10- 3 AND DWG 5911423, REV CD.SDR DALA2016011700408Skin · damagedLIGHTNING STRIKE ON COUNTERSINK AT FUSELAGE SKIN BS 261 BETWEEN LONGERON 29LT TO 30. FUSELAGE SKIN BS 261 BETWEEN LONGERON 29LT TO 30 IN REF MON, 88 L/L , 0592913; VIS ER/A 498753-II; FSLG SKN ; 996. WAS REPAIRED IAW SRM 53-04-2, FIGURE 2, SHEET 6 AND 33. PERSDR A6WA201643466Skin · damagedAIRCRAFT SKIN AT ADF ANTENNA MOUNTING SURFACE HAS SCRIBE DAMAGE AROUND PERIMETER. REPAIRED ACFT SKIN AT ADF ANTENNA MOUNTING AREA IAW SUPPLEMENT 16-013A.SDR A6WA201643464Skin · corrodedFUSELAGE SKIN UNDER TCAS ANTENNA HAS CORROSION AROUND FASTENER HOLES & SCRIBE MARKS ON MATING SURFACE, INCLUDING UNDER SEALANT AROUND ANTENNA. REMOVED CORROSION & SCRIBE MARKS IAW SRM 51-21-06, 51-12-00 & REPAIRED REWORKED AREA IAW 253-00236 REV A.SDR COEA2016011516801Skin Panel · corrodedHEAVY CHECK COE & MAJOR REPAIR. REAR CTR FUSELAGE, RT LATERAL LOWER SKIN PANEL HAS LEVEL 2 CORROSION UNDER THE SERVICE DOOR SCUFF PLATE. REPAIR IAW SRAS CE 588 16 9955 DATED 2 17 16.SDR SWAA2016021048876Skin Panel · crackedUPPER SKIN PANEL COMMON TO THE SHEAR FITTING, CRACKED IN 2ND HOLE FROM THE REAR, AT BS 547, LBL 32.40. REPAIRED SKIN IAW ER & EA.SDR SWAA2016013048467Skin · crackedSKIN CRACKED AT BS 469, STRINGER 2L. REPAIRED SKIN IAW EA.SDR IPXA2016012998610Skin · damagedINSPECTION TYPE:D1, DURING D1, PLUS C1 CHECK OF DATUM ACFT, BROKEN AND DENT WERE FOUND ON THE SKIN BS 2595, BETWEEN STRINGERS 38 - 42R. REPAIRED IAW SRID 4-3117883658, AND EO B-747-5330-59589-A.SDR SWAA2016012648380Skin · crackedSKIN CRACKED AT BS 273, STRINGER 4L. REPAIRED SKIN IAW SRM.SDR SWAA2016012648379Skin · crackedSKIN CRACKED AT BS 361, STRINGER 6R. REPAIRED SKIN IAW EA.SDR SWAA2016012648378Skin · crackedSKIN CRACKED AT BS 364.5, STRINGER 5L. REPAIRED SKIN IAW EA.SDR SWAA2016012648377Skin · crackedSKIN CRACKED AT BS 469, STRINGER 2L. REPAIRED SKIN IAW EA.SDR QXEA2016012000020Angle · corrodedEDGE ANGLE AT AFT PASSENGER DOOR LT SURROUND STRUCTURE BS 669.3 - 697.6 IS CORRODED. LOCATED AND DRILL NEW THRESHOLD, PN 85339512-101, EDGE ANGLE, REF SRM 51-40-07. CONTINUED TO DRILL EDGE ANGLE, REF SRM 51-40-07. INSTALLED EDGE ANGLE REF SRM 51-42-05, 51SDR AALA20160115007Skin · corrodedAIRCRAFT WAS IN BASE MX. FUSELAGE SKIN CORRODED FWD OF AFT LAVATORY SERVICE PAN ASSEMBLY AT APPROX FS 1681 & STRINGER 26R. REPAIRED SKIN IAW EA 256605.SDR CALA2016011895006Skin · corrodedDURING HORIZONTAL STAB INSPECTION FOUND SKIN TO HAVE INTERGRANULAR CORROSION, FWD OF DOOR 312AR, AT APPROX STRINGER 25 RT, STATION 3366, FRAME 70 APB. ACCOMPLISHED REPAIR IAW ECRA 5330-05303 STEPS 1 A & B.SDR CALA2016011895005Doubler · corrodedLAVATORY SERVICE PANEL, INTERIOR DOUBLER HAS CORROSION. EVALUATED CORROSION, FOUND TO BE OUT OF LIMITS. R & R INTERIOR DOUBLER.SDR AALA20160115012Skin · crackedAIRCRAFT WAS IN BASE MX. FUSELAGE SKIN CRACKED IN 3 LOCATION, BETWEEN L2L - L4L, AT STATION 1437. ACCOMPLISHED REPAIR IAW SRM 53-04-00-001.SDR DALA2016011500361Skin · dentedPROTUBERANCE ON, BETWEEN LONGERON 24RT AND 25RT BS 168 AT OUTER FUSELAGE SKIN. THIS DAMAGE WAS FOUND WITH PREVIOUS REPAIR IAW SRM 53-04-2, FIG 2, SHEET 3.SDR ASOA2016115005Skin · dentedFORWARD FUSELAGE 1, SKIN LT SIDE HAS DAMAGE FROM A BIRD STRIKE. CUTOUT DAMAGED AREA, FABRICATED DOUBLER AND FILLER. REMOVED DAMAGED SECECTION OF RIB 4 AND SPLICED IN NEW SECTION. HFEC EFFECTED AREA AND NO DEFECTS NOTED AT THIS TIME.SDR WVER2016011400003Skin · dentedDENT IN FUSELAGE STRUCTURE AT STRINGER 16R, FS 250 - 265.SDR DALA2016011400307Skin · corrodedSKIN CORROSION BETWEEN FRAMES 56 AND 57, 2 PLACES BETWEEN STR 41L AND 42L AND 1 PLACE BETWEEN STR 42L AND 43L, BLENDED OUT AREAS OF CORROSION IAW SRM 21-73-00 REF PRI, ER/A, 542941-14AD, REV 0, 1, 2, 3.SDR TIPR2016011424814Skin · dentedFUSELAGE SKIN DENTED OVER FRAME AT BS 480 AT STR 27-28, RT. REPAIRED IAW REO-G19404, CAT B REPAIR.SDR DALA2020040202130Repair · unknownPER ER/A 541967-14 REV A ITEM 10, REPAIR REMOVED AND RE-INSTALLED PER SRM 53-00-11, FIG 239 AND IS CONSIDERED PERMANENTSDR SWAA2016030349610Skin · crackedSKIN CRACKED AT BS 540, BETWEEN STRINGER 22R - 23R. REPAIRED SKIN IAW EA.SDR SWAA2016012248280Post · crackedFLIGHT COMPARTMENT RT NR 3 WINDOW FRAME E - F POST, SECOND LOWER FASTENER HOLE CRACKED. REPAIRED POST IAW ACO.SDR SWAA2016012248279Post · crackedFLIGHT COMPARTMENT LT NR 3 WINDOW FRAME E - F POST, SECOND LOWER FASTENER HOLE CRACKED. REPAIRED POST IAW ACO.SDR SWIA201641802Buttstrap · corrodedBUTT STRAP AT BS 333 CORRODED OUT OF LIMITS. R & R BUTT STRAP FROM STRINGERS 25R TO STR 26L, IAW EA.SDR SWAA2016011548024Doubler · crackedGROUND SERVICE EXHAUST DUCT DOUBLER CRACKED AT INBD LOWER FLANGE. R & R DOUBLER IAW SRM.SDR DALA2016011400300Skin · crackedCRACK ON FUSELAGE SKIN BS 1480. THE SKIN WAS REPAIR IAW SRM 53-01.SDR DALA2016011400295Skin · corrodedCORROSION ON INTERNAL FUSELAGE SKIN, BELLY DRAIN AREA, FROM BS 725 TO 731 BETWEEN LONGERON 30 AND LONGERON 29 RT AT MID CARGO COMPARTMENT. CORROSION WAS REMOVED IAW SRM 51-10-3, PAR 26 AREA WAS REPAIRED IAW ETI-88-16-004. REPAIR IAW ER/A 541602-14 REV ORIGINSDR DALA2016011300247Skin · debondedLEFT ALTERNATE STATIC PORT INTERNAL DOUBLER DISBONDED FROM SKIN. REPLACED INTERNAL DOUBLER AND BONDED TO SKIN IAW DWG 5911412. REPLACED INTERNAL DOUBLER AND BONDED TO SKIN IAW DWG 5911412.SDR Y2PA2016011200001Skin · corrodedMAINTENANCE DISCOVERED A MISSING RIVET FROM THE BELLY SKIN AT FS 585. UPON FURTHER INSPECTION, IT WAS DETERMINED THAT THERE WAS INTERNAL AND EXTERNAL CORROSION AND A TEMPORARY REPAIR WAS INSTALLED AND THE AIRCRAFT WAS FERRIED FOR REPAIR. MAINTENANCE INSTALLESDR KCSA201601121002Bear Strap · crackedRIGHT MED NR 5 UPPER AFT CORNER LOWER HOLE HAS A CRACK INDICATION.
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