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 SWAA2016011548003Skin · crackedSKIN CRACKED AT BS 430+7, STRINGER 6R. REPAIRED SKIN IAW SRM.SDR AALA20160107007Skin · crackedAIRCRAFT WAS IN BASE MX. FUSELAGE SKIN CRACKED FROM FASTENER HOLE AT STATION 189 & LONGERON 22L. ACCOMPLISHED DOUBLER REPAIR IAW DWG SR09530219 & SRM 51-30-02.SDR DALA2016011000156Skin · damagedLIGHTNING STRIKE ON LWR/FWD CORNER WINDOW BELT NR 58. WINDOW BELT WAS REPAIRED IAW ER/A 541594-14, REV ORIGINAL, UT, WAS ACCOMPLISHED IAW NDT SPM 04-00-07, PAR 5, FIG 3, SH 1 AND 2. DIMENTIONS AS FOLLOW WINDOW STA BETWEEN 769 TO 750 RT WINDOW ZONE 1 ORIG THICSDR CALA2016010894981Skin · dentedDENT ON FUSELAGE AT STRINGER 37 RT & BS 654+44, JUST AFT OF FWD CARGO DOOR. REPAIRED FUSELAGE SKIN IAW SRM 53-00-01 FIG 201 REPAIR 12.SDR CALA2016010894976Skin · 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 CALA2016010800034Skin · dentedRIGHT LOWER FUSELAGE SKIN SHOWS DENT DAMAGE, JUST FWD OF BS 740 RT, BETWEEN STRINGERS 24 & 25 RT. REQUIRED INITIATE DIP FOR REINSPECTION ON CYCLE 37500. DAMAGE AREA 1 1/16 X 1 1/2 WITH A DOUBLER 8 1/4 X 8 3/4. ACCOMPLISHED REPAIR IAW SRM 53-00-01 REPAIR 3 WSDR DALA1621279570Skin · crackedFUSELAGE SKIN BS 1087 AND L-14R. CRACK REPAIR.SDR SIMA20160106004Skin · crackedRIGHT AFT FUSELAGE FRAME 75, BELOW STRINGER 2 SKIN CRACKED AT FASTENER MARKED, SETTINGS 400KHZ 135 V-65.0 H-75.0 FILTER LO 100. CRACKED FUSELAGE SKIN AT FRAME 75, STRINGER 2R AREA WILL BE CUT OUT & REPAIRED WITH FILLER & DOUBLER, SEE NRTC E487295 FOR ACCOMPLISDR UHLA201601060026Access Panel · corrodedWASTE BOX ACCESS PANEL EVIDENCE OF CORROSION. R & R WASTE BOX ACCESS PANEL AND INSTALLED PLACARD IAW AMM 53-03-60 AND AMM 20-10-09.SDR DALA2016011300005Skin · damagedDURING M-CHECK, LIGHTNING STRIKE DAMAGE, FRAME 1, STR 33-34 LT. REPAIRED IAW SRM 53-21-11 AND 53-00-11, FIG 219.SDR IPXA2016012698481Skin · dentedINSPECTION TYPE:2C, AFT RT FUSELAGE SKIN HAS DENT WITH CREASE BS 2122 BETWEEN L7R AND L8R ACCOMPLISHED PERMANENT REPAIR ON AFT FUSELAGE SKIN AT BS 2122 BETWEEN L7R AND L8R IAW 011-5370-01-A6050, REV I/R AND EO MD11-5330-59608-A.SDR DALA2016010600050Skin · damagedLIGHTING STRIKE ON FUSELAGE SKIN WINDOW BELT LT SIDE FWD SIDE BETWEEN BS Y=1041 AND 1060. REPAIRED IAW SRM 53-05, FIG 111, NDT SPM 04-00-07, PAR 5, FIG 3, SHEET 1, 2.SDR DALA2016010600049Skin · damagedLIGHTING STRIKE ON FUSELAGE SKIN WINDOW BELT LOWER CENTER BETWEEN BS Y=560 AND 579 LT. REPAIRED IAW SRM 53-05, FIG 111, SHEET 6-8 NDT SPM 04-00-07, PAR 5, FIG 3, SHEET 1 AND 2. ORIGINAL THICKNESS ON BLEND OUT .090" AND REMAINING THICKNESS .085".SDR FDEA201601050032Skin · wornEMPENNAGE, LT SIDE, THE HORIZONTAL STABILIZER BLADE SEAL PERIMETER HAS WEAR AT BS 1862 - 1875, ABOVE STRINGER 17. CHAFE REMOVED, FOUND OUT OF LIMIT IAW SRM 53-80-01 FIG 101 DETAIL VII REV 116. REPAIR CARRIED OUT IAW SRM 53-80-01-2R FIG 201 DETAIL II REV 117.SDR DALA2019011600297Skin · damagedFUSELAGE SKIN AT STATION 654+86, BETWEEN S-39L AND S-38L HAS DENT AND CREASE. C/W ERA 542633-14. (LP 2293561)SDR IPXA2016011797908Skin · crackedINSPECTION TYPE:C, 113.5" LONG CRACK WAS FOUND ON THE STR 20L AT BS 1550. REPAIR IAW SR 4-3105998863 WITH 8100-9 FORM DATE:14/JAN/2016 AND EO:B767-5310-59525-A.SDR SWAA2016010747778Skin · crackedFUSELAGE SKIN CRACKED AT BS 630+5, STRINGER 1L. REPAIRED SKIN IAW EA.SDR ASOA2016010414303Skin · damagedAFT FUSELAGE SKIN DAMAGE CAUSED BY THE AFT LOWER DOOR LATCH PIN. COMPLIED WITH EC/TC REO 601R-53-21-186. THIS IS CONSIDERED A PERMANENT PEPAIR. THIS IS CONSIDERED A MAJOR REPAIR IAW GMM 5-3.SDR DALA2016010500032Doubler · damagedDEFORMED INTERNAL PRODUCTION DOUBLER BETWEEN BS 180-200, LONGERON 9-11R AT RT SERVICE DOOR SURROUNDING SKIN PANEL. REPAIRED IAW ERA 541592-14, REV O.SDR CALA2016010494960Skin · damagedBS 1740 - 1960, STRINGER 46L-46R, FUSELAGE SKIN FOUND PITTING. PITTING WAS REMOVED IAW ECRA 5330-05477.SDR COEA2016010343801Skin Panel · corrodedHEAVY CHECK COE & MAJOR REPAIR. INTERIOR LEVEL 2 CORROSION AFFECTING FWD FUSELAGE, RT UPPER SKIN PANEL AFT OF FRAME 21, STRINGER 5A - 6. REPAIRED IAW SRAS ES-533 16 9984 DATED 2 25 16.SDR COEA2016010342801Skin Panel · corrodedHEAVY CHECK COE & MAJOR REPAIR. INTERIOR LEVEL 2 CORROSION AFFECTING FWD FUSELAGE, RT UPPER SKIN PANEL FWD OF FRAME 21, BETWEEN STRINGER 8 - 10. REPAIR IAW SRAS ES-533 16 9984 DATED 2 25 16.SDR COEA2016010341801Strap · corrodedHEAVY CHECK COE & MAJOR REPAIR. INTERIOR LEVEL 2 CORROSION AFFECTING FWD FUSELAGE, RT UPPER SKIN PANEL STRAP, BETWEEN FRAMES 15-16, STRINGER 11 - 12. REPAIR IAW SRAS ES 533 16 9984 DATED 2 25 16.SDR COEA2016010340801Skin Panel · corrodedHEAVY CHECK COE & MAJOR REPAIR. INTERIOR LEVEL 2 CORROSION AFFECTING FWD FUSELAGE, RT UPPER SKIN PANEL, BETWEEN FRAMES 16 - 17, STRINGER 8 - 9. REPAIR IAW ES 533 16 9984 DATED 2 25 2016.SDR COEA2016010339801Skin Panel · corrodedHEAVY CHECK COE & MAJOR REPAIR. INTERIOR LEVEL 2 CORROSION AFFECTING FWD FUSELAGE, RT UPPER SKIN PANEL, BETWEEN FRAMES 16-17, STRINGER 4 - 5. REPAIR IAW SRAS ES-533 16 9984 DATED 2 25 16.SDR COEA2016010322801Doubler · corrodedWO 155295 NR 200040 HEAVY CHECK COE & MAJOR REPAIR. INTERIOR LEVEL 2 CORROSION AFFECTING CTR FUSELAGE, FWD CROWN PANEL & DOUBLER, FRAME 23D - 24, STRINGER 3 - 3A RT. REPAIR IAW SRAS ES 367 16 9947 DATED 2 12 16.SDR COEA2016010317801Skin · corrodedHEAVY CHECK COE & MAJOR REPAIR. INTERIOR LEVEL 2 CORROSION AFFECTING CTR FUSELAGE FWD CROWN PANEL & DOUBLER, FRAME 23D - 24, STRINGER 3 - 4 LT. REPAIR IAW SRAS ES 367 16 9947 DATED 2 12 16.SDR COEA2016010311801Skin Panel · corrodedHEAVY CHECK COE & MAJOR REPAIR. INTERIOR LEVEL 2 CORROSION AFFECTING CTR FUSELAGE, LT LOWER SKIN PANEL, BETWEEN FRAMES 23A - 23B, STRINGER 12 - 12A. REPAIR IAW SRAS CE-361 16 9926 DATED 1 29 16.SDR COEA2016010302801Skin Panel · corrodedHEAVY CHECK COE & MAJOR REPAIR. INTERIOR LEVEL 2 CORROSION AFFECTING CTR FUSELAGE RT UPPER SKIN PANEL, BETWEEN FRAMES 23B - 23C, STRINGER 10 - 10A. REPAIR IAW SRAS CE 363 16 9925 DATED 1 29 2016.SDR SWAA2016012648387Skin · crackedSKIN CRACKED AT BS 540, STRINGER 22R. REPAIRED SKIN IAW EA.SDR SWAA2016011548002Skin · crackedSKIN CRACKED AT BS 360, STRINGER 5R. REPAIRED SKIN IAW EA.SDR RAIA201601030002Skin · damagedBIRD STRIKE ON LT SIDE OF ACFT NOSE. LARGE DENT AND SKIN TORN AT FROM 4L AND STGR 15L ON LT FUSELAGE DUE TO BIRD STRIKE. C/W REPAIRS IAW EO-EMB145-53-014-O.SDR COEA2016010237801Skin Panel · corrodedHEAVY CHECK COE & MAJOR REPAIR. INTERIOR LEVEL 2 CORROSION AFFECTING REAR CTR FUSELAGE, LT UPPER PANEL, AFT OF FRAME 33 & FWD OF FRAME 34, STRINGER 8 - 10. REPAIR IAW SRAS ES 532 16 9964 DATED 2 24 16.SDR COEA2016010210801Skin Panel · corrodedHEAVY CHECK COE & MAJOR REPAIR. INTERIOR LEVEL 2 CORROSION AFFECTING REAR FUSELAGE, LT LATERAL UPPER PANEL, FRAMES 40 - 41, STRINGER 8 - 9 LT. SMALL DAMAGE EXTERNAL REPAIR SRM 530000-300-801-A01.SDR COEA2016010209801Skin Panel · corrodedHEAVY CHECK COE & MAJOR REPAIR. INTERIOR LEVEL 2 CORROSION AFFECTING CTR FUSELAGE, LT UPPER SKIN PANEL, BETWEEN FRAMES 24 - 25, STRINGER 4 - 5. REPAIR IAW SRAS CE-339 16 9919 DATED 1 29 16.SDR COEA2016010201801Skin Panel · corrodedHEAVY CHECK COE & MAJOR REPAIR. INTERIOR LEVEL 2 CORROSION AFFECTING REAR FUSELAGE RT LATERAL UPPER SKIN PANEL, FRAMES 40 - 41, STRINGER 5 - 6 RT. EXTERNAL DOUBLER REPAIR, SRM 530000-300-803-A01.SDR ASAA2016010214782Skin · crackedRT FUSELAGE AT GROUND AIR CONDITION DOOR CUTOUT IS CRACKED. ACFT GROUNDED. REPAIRED GROUND AIR COND DOOR CUT OUT IAW SRM 53-30-01-2R-2.SDR SWAA2016011147822Skin · crackedFLIGHT DECK RT NR 3 WINDOW FRAME E-F POST, WINDOW PANE ATTACH FASTENER HOLES, 2ND OPENED FASTENER HOLE FROM BOTTOM CRACKED. REPAIRED WINDOW ASSEMBLY IAW ACO.SDR REXA2016010200019Skin Panel · crackedSKIN BELOW AFT LATCH FOR PANEL 211AL IS CRACKED. R & R PANEL IAW SRM 51-42-06 PAR 6, 51-42 -10 PAR 8 & 51-42-21 PAR 6.
SDR DALA2016010500021Skin · crackedCRACK ON AFT CUT OUT SKIN HOUSING AT C2 DOOR. CRACK ON AFT CUT OUT SKIN HOUSING WAS REMOVED IAW ERA 486446-14MA REV ORIGINAL.SDR SCNA20160102001Skin · damagedGROUND POWER DOOR DAMAGED. REPAIRED GROUND POWER DOOR CUTOUT.SDR DALA2016010300012Skin · crackedFOUND APPROXIMATELY 1.75 CRACK IN SKIN APPROXIMATELY 6 IN AFT FROM ELEVATOR ACCUMULATOR ACCESS DOOR. ELEVATOR ACCUMULATOR ACCESS DOOR CUTOUT SKIN CRACKED FROM UPPER AFT CORNER RADIUS TO CLOSEST FASTENER AFT. C/W PRI 542690-14, REV 0,1,2,3,4 AND FINAL, C/W ERSDR DALA2016010300011Skin · damagedLIGHTNING STRIKE ON EXTERNAL FUSELAGE SKIN BS 955 BETWEEN LONGERONS 1 - 2 RT. SKIN WAS REPAIRED. FASTENER WAS REPLACED IAW SRM 53-04-1 PARR 6C2 CONDITION 2. DAMAGE ON SKIN WAS REPARED IAW SRM 53-04-1 PARR 5C CONDITION 1.SDR DALA2016010400044Skin · damagedLIGHTNING STRIKE , BS 288 AT STR 17R, INSPECTION OF AREA ACCOMPLISHED, NO SIGNS OF CRACKS.SDR DALA2016011400369Skin · damagedLIGHTNING STRIKE AT BS 740, 3" ABOVE STR 26RT AT FASTENER, IAW SRM 757 53-00-01, REPAIR 6, PAGE 201, SEC II, DRILLED OUT FASTENER, INSP WITH 10X, INSTALLED BLIND FASTENER, TREATED AND PAINTED ZONE A, CAT C. REPAIR 300 FLIGHT CYCLES NOT TO EXCEED 24 MONTHS. 2SDR DALA2016011400322Skin · damagedLIGHTNING STRIKE AT BS 660 AT STR 26, RT AT FASTENER. IAW SRM 53-00-01, REPAIR 6, PAGE 201, SEC 2. DRILLED OUT FASTENER, INSPECTED WITH 10X, INSTALLED BLIND FASTENER,TREATED AND PAINTED.SDR DALA2016011400321Skin · damagedLIGHTNING STRIKE AT STA 423 3" ABOVE STR 27 RT AT FASTENER. IAW SRM 53-00-01, REPAIR 6, PAGE 201, SEC 2. DRILLED OUT FASTENER, INSP WITH 10X, INSTALLED BLIND FASTENER, TREATED AND PAINTED.SDR DALA2016011400320Skin · damagedLIGHTING STRIKE AT BS 680, 3" ABOVE STR 26 RT AT FASTENER. IAW SRM 53-00-01, REPAIR 6, PAGE 201, SEC II DRILLED OUT FASTENER, INSPECTED WITH 10X, INSTALLED BLIND FASTENER, TREATED AND PAINTED. ZONE A, CAT C, REPAIR INSPECTION INTERVAL AT 1000 CYCLES. TIME LSDR DALA2016011400319Skin · damagedLIGHTNING STRIKE AT BS 540, 4" ABOVE STR 27, RT AT FASTENER. IAW SRM 53-00-01, REPAIR 6, PAGE 201, SEC II. DRILLED OUT FASTENER, INSPECTED WITH 10X, INSTALLED BLIND FASTENER, TREATED AND PAINTED. ZONE A, CAT C, REPAIR INSPECTION, INTERVAL AT 1000 CYCLES. TSDR DALA2016011400318Skin · damagedLIGHTNING STRIKE AT BS 740, 3" ABOVE STR 26 RT AT FASTENER IAW SRM 53-00-01, DRILLED OUT FASTENER, INSPECTED WITH 10X. INSTALLED BLIND FASTENER, TREATED AND PAINTED ZONE A, CAT C, REPAIR 300 FLIGHT CYCLES NOT TO EXCEED 24 MONTHS. 21-0553-8-7103, SN 00683, REP
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