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 IPXA2021012664885Skin · corrodedINSPECTION TYPE: C4 CENTER WING BOX UPPER SKIN HAS AN AREA OF CORROSION AT STR15 LBL 85. REPAIRED CORRODED SKIN AT CENTER WING BOX STR 15 LBL 85, IAW VT-SAA EA 011-5730-01-A8823 AND UPS EO MD11-5730-79110-A (MINOR).SDR IPXA2021012364804Skin · corrodedINSPECTION TYPE: 4C CENTER WING UPPER SKIN HAS CORROSION AT STRINGER 15 BETWEEN XCW -79 TO XCW -104. REPAIRED CORRODED CENTER WING UPPER SKIN AT STRINGER 15 BETWEEN XCW -79 TO XCW -104, IAW VT-SAA EA 011-5730-01-A8820 REV IR AND UPS EO MD11-5730-79105-A. (MINSDR HNAA2021011400016Skin · crackedFUSELAGE EXTERNAL SKIN IS CRACKED AROUND 1 FASTENER FR 77 BETWEEN STR 8R-9R. FABRICATED AND INSTALLED 1 BUSHING ON FRAME 77 BETWEEN STRINGERS 8R-9R, IAW EMB 145 SRM 53-32-01RE AND EO1-53-21-0001.SDR SWAA2021011140481Skin · corrodedCORROSION, ON FUSELAGE SKIN EXTERNAL SURFACE AROUND FASTENER HOLES BS 669.75+15-BS 685+13, STR 1-STR 2R.SDR SWAA2021011141039Skin · corrodedCORROSION EXTERNAL SKIN TOILET SERVICE DOOR 145AL AT LOWER FUSELAGE.SDR SWAA2021011141040Strap · corrodedCORROSION EXTERNAL SKIN STRAP BELOW TOILET SERVICE DOOR CUTOUT AT LOWER FUSELAGE.SDR DALA2021010800112Skin · damagedDURING LAYOVER IN ATL, GROUND DAMAGE WAS INCURRED TO THE FUSELAGE SKIN BETWEEN STA 888-927 AND STR 23R-24R. MAINTENANCE REPAIRED DAMAGE, PER ERA 589328-14.SDR DALA2021010800111Skin · damagedDURING LAYOVER IN ATL, GROUND DAMAGE WAS DISCOVERED ON THE FUSELAGE SKIN BETWEEN STA 900-915 AND STR 23R TO 24R. STRINGER STR 24R (P/N 147A3215-21) WAS ALSO DAMAGED. MAINTENANCE REPAIRED DAMAGE, PER ERA 589302-14.SDR DALA2021010700106Skin · damagedDURING LAYOVER IN ATL, GROUND DAMAGE WAS INCURRED TO THE FUSELAGE SKIN BETWEEN STA 888-927 AND STR 23R-24R. MAINTENANCE REPAIRED DAMAGE, PER ERA 589328-14.SDR R61A2021012200087Skin · dentedMAJOR: WHILE AIRCRAFT WAS IN FOR HEAVY CHECK. RE-EVALUATE DAMAGE ON FUSELAGE AT FR 21-22 STRG 13R-14R AND REPAIR AS REQUIRED. COMPLIED WITH ETD2021-170-01428 REV A. A DENTED AREA NEEDED REPAIRED. INSTALLED REPAIR DOUBLER AND FILLER BETWEEN FR 21-22 AND STGSDR R61A2021012000084Finger Doubler · gougedWHILE A/C WAS IN HEAVY CHECK. FWD CARGO HORIZONTAL BEAM (DOOR SILL) FWD FINGER PLATE IS GOUGED. REPLACED FINGER PLATE, IAW SRM 51-40-08, 51-43-02. MAJOR REPAIR. A/C REMAINS OUT OF SERVICE FOR HEAVY CHECK COMPLETION.SDR GRTA20201210002Skin · crackedBELLY SKIN CRACKED AT FS 288.25 JUST OUTBOARD OF STRINGER 15L APPROXIMATELY 1" AND 1.5". AFTER FURTHER INVESTIGATION, FOUND FRAME SHIM CORRODED. REPAIRED IAW BEECHCRAFT 1900 SRM 51-70-06.SDR SWAA2021071639873Fitting · brokenBROKEN DRAIN EXTERNAL SKIN BS1016 FUSELAGE EXTERIOR (1 EA) / REPLACED DRAIN FITTING AT BS 1016 ON EXTERNAL SKIN (1EA) WITH P/N 140W2813-1 IAW B737-700 SRM 51-40-02 AND DWG 148A3320 SHEET 30 REV ASDR SWAA2021021247431Skin · dentedDENT EXTERNAL SKIN BS 992.8 MORE 10 INCH AND AT STR 15R AT UPPER FUSELAGE / REPAIRED EXTERNAL SKIN LOCATED BTW BS 992.8 AND BS 1016 BTW STR 13R AND STR 17R IAW EA # 53-0013-21 REV 0 AND 21-153-00187 REV IR. FOR REQUIREMENT INSPECTION SEE TLD # T080517SDR IPXA2021020265225Skin · crackedINSPECTION TYPE:2CR-3 DOOR FWD. JAMB INNER SKIN IS CRACKED BETWEEN STA. 1256.75 TO 1250.75 AND BETWEEN DOOR STOPS 6 & 7.REPAIRED CRACKED R-3 DOOR FWD JAMB INNER SKIN BETWEEN STA. 1256.75 TO 1250.75 AND BETRWEEN DOOR STOPS 6 & 7 IAW VT-SAA EA 011-5310-01-A8816 SDR IPXA2021012764964Doubler · gougedINSPECTION TYPE: 2C EXTERIOR FUSELAGE SKIN REPAIR DOUBLER IS GOUGED AT STA 1153 AND BETWEEN L43R TO 45R. REPAIRED GOUGED EXTERIOR FUSELAGE SKIN REPAIR DOUBLER AT STA 1153 AND BETWEEN L43R TO 45R, IAW VT-SAA EA 011-5530-01-A8828 REV I/R AND UPS EO MD11-5330-79SDR AALA202101209017Skin · corrodedAIRCRAFT IN BASE MAINTENANCE. CORROSION OF LT AFT LOWER FUSELAGE EXHAUST PORT SKIN AT STA 1968 BETWEEN STR 35L AND STR 36L, MEASURING L=2.5 IN, W=1.5 IN, D=0.05 IN. ACCOMPLISHED PERMANENT REINFORCING DOUBLER REPAIR, IAW SRM 53-70-01-2R-1.SDR A6WA202101067515Skin · crackedFS 235 RIGHT SIDE FUSELAGE EXTERNAL SKIN CRACKED AFT OF NOSE LANDING GEAR CUT-OUT, NEXT TO RIGHT RADIUS. AIRCRAFT REMOVED FROM SERVICE. REPAIRED CRACK ON SKIN AT FS 235 RIGHT SIDE AFT OF NOSE LANDING GEAR CUT OUT, IAW CRJ200 REO 601R-53-11-048.SDR HNAA2021011400025Skin · crackedFUSELAGE EXTERNAL SKIN CRACKED AT RIVET ON FR 78 BETWEEN STGR 7L-8L, JUST BELOW SKIN DOUBLER. CRACK ENDS MARKED, SEE NRTC E831911 TASK NR 1 FOR NDT. CUTOUT DAMAGE AREA ON FR 78, STR 6L-7L. MADE REPAIR BUSHINGS AND INSTALLED BUSHING, IAW EMB 145 SRM 53-32-01SDR HNAA2021011400015Skin · crackedFUSELAGE EXTERNAL SKIN IS CRACKED AROUND 6 FASTENERS ON FR 77 BETWEEN STR 4L-7L. CUTOUT TWO DAMAGED AREAS ON EXTERNAL SKIN ON FRAME 77, IAW EMB 145 SRM 53-32-01. INSTALLED 2 BUSHINGS ON EXTERNAL SKIN ON FRAME 77 BETWEEN STRINGERS 5L-7L, IAW EMB 145 SRM 53-32SDR HNAA2021011400014Skin · crackedFUSELAGE EXTERNAL SKIN IS CRACKED AROUND 6 FASTNERS ON FR 78 BETWEEN STR 4L-7L. PERFORMED 3 CUTOUTS AS REQUIRED TO REMOVE DAMAGE FROM FUSELAGE EXTERNAL SKIN AT FR 78 BETWEEN STGR 5L-7L AND FABRICATED AND INSTALLED DOUBLER AND 3 FILLERS, IAW ETD2020-145-035446SDR N6WA2021010404Doubler · corrodedDOUBLER FOR ANT IS CORRODED AT STR 27 FS 295.00. R & R ATC ANTENNA DOUBLER, IAW CRJ 700 SRM 51-42-06 AND 51-42-21.SDR DALA2021010600064Skin · damagedFUSELAGE SKIN DAMAGE DUE TO TAIL STRIKE AT 1740 TO 1750, S-29L TO S-29R. REPAIRED PER ERA 589117-14.SDR DALA2021010600063Skin · damagedDUE TO TAIL STRIKE FUSELAGE SKIN DAMAGED AT 1787 TO BS 1808 S-29L TO S29R. MAINTENANCE REPAIRED PER ERA 589173-14.SDR DALA2021010600062Skin · corrodedFUSELAGE SKIN DAMAGE AT BS 1716 TO SB 1730, S-29L TO S-29R DUE TO TAIL STRIKE DURING LANDING. MAINTENANCE REPAIRED PER ERA 589169-14.SDR DALA2021010600059Skin Panel · damagedDURING LANDING IN JFK, THE A/C SUSTAINED A TAIL STRIKE RESULTING IN DAMAGE TO THE SKIN PANELS 146N3610-9, 148N3214-8 AND 148N3216-1 BETWEEN BS 1720 AND BS 1862, S-29L TO S-29R. CRACK INDICATION IN HOLE AT STA 1771 STRG 29R AT T-CHORD LAYER. C/W ERA 567982-14SDR DALA2021010500043Skin · corrodedCORROSION WAS FOUND IN SKIN DRAIN CUTOUT BETWEEN FR 69-FR 70, STR 31R-STR 32R, LOWER FUSELAGE. CORRECTIVE ACTION: PERFORMED REPAIR, PER ER/A 589202-14AD REV ORIGINAL.SDR VNAA2021010499916Skin · damagedEXT FUSELAGE SKIN HAS AREAS OF DAMAGE BETWEEN FS 969.00 AND FS 985.00 AND STR 26 LT TO 26 RT.SDR DALA2024081508178Skin · damagedSHIP 5639 ER/A 589169-14 ISSUED FOR TAIL STRIKE DAMAGE AT BS 1720 TO BS 1730, S-29L TO S-29R. CORRECTIVE ACTION: REF ERA 589169-14. (1694524)SDR A6WA202101047508Skin · gougedDAMAGED HOLE FOUND AT FS 621-105'' AND BETWEEN STRG 16L TO STRG 17L. AIRCRAFT REMOVED FROM SERVICE. REMOVED NUT PLATE AT FS 621-105'' AND BETWEEN STRG 16L TO STRG 17L, REF CRJ-200 SRM 51-45-00 REV 38. OPENED ELONGATED HOLE TO A NEW DIAMETER OF 0.284'', REF:SDR CALA2021010400006Skin · crackedOVER WING HATCH RT AFT FOUND CRACK AT OUTER SKIN 1 IN IF RT LOAD TRANSMITTING PROFILE TOP SIDE OF NR 2 HORIZONTAL BEAM. A3NB-52- 4-6031-AD, PER HAECO LCQ N/R 9290343/32343. REMOVED AND REPLACED DAMAGED RT SEGMENT FRAME ON RT AFT OW HATCH, IAW A320 SRM 51-42-SDR CALA2021010400005Skin · crackedRT AFT OVER WING HATCH FOUND CRACK AT THE OUTER SKIN 1 AFT OF THE LT LOAD PROFIL TOP AND BOTTOM OF THE NR 2 HORIZONTAL BEAM-A3N B-52-4-6031-AD RELATED NR 9290337/32337. REMOVED AND REPLACED DAMAGED LT SEGMENT FRAME ON RT AFT OW HATCH, IAW A320 SRM 51-42-11 5SDR SWIA202156929Skin · corroded*CORROSION ON THE STRUCTURE ON THE INNER SKIN AROUND THE AFT DRAINMAST PORTAL. STGR27 -STGR26R FS1031.00 - FS1047.00. (MARKED) (C-CHECK) RO 3/11/2021 INNER CHANNEL COMON TO AFT DRAINMAST PORTAL. STGR27 -STGR26R FS1031.00 - FS1047.00 HAS EXFOLIATED CORROSSDR SWAA2021010639322Skin · damagedFUSELAGE SKIN DAMAGE AT AFT CARGO DOOR CUTOUT FWD EDGE BS 797 BETWEEN STR 23 AND 24, 9' ABOVE LOWER EDGE OF CUTOUT JUST BELOW SKIN LAP. REPAIRED DAMAGE, PER EA 20-153-02509(SA-M 326 A1190384).SDR SWAA2021010639321Skin · dentedAFT CARGO OPENING, LOWER BS 835 SKIN HAD A DENT. REPAIRED DAMAGE PER EA 20-153-02520 (SAM 326 A1190385).SDR CALA2021010400004Skin · corrodedRT EXT FUSELAGE HAS CORROSION AT LAV VENT, REPAIRED RH EXT FUSELAGE AT LAV EXHAUST VENT, IAW A320 SRM 53-41-11-300-004.SDR DALA2024072507470Skin · ground damageSHIP 650 A/C SUSTAINED GROUND DAMAGE CAUSING A DENT TOTHE FUSELAGE SKIN ON STRINGER S-24R AND STA 725. CORRECTIVE ACTION: REF ERA 589238-14. (1692753)SDR DALA2021010200003Skin · dentedWORKING ER/A 589238-14 REV A, PERMANENT REPAIR, FUSELAGE DENT SECT 43 STA 725 STR 24R. CUT OUT DAMAGE TO SKIN, PER B757 SRM 53-00-01 REPAIR 28 STEP 4D (1) FIG 201. CUT OUT DAMAGED STRINGER, PER B757 SRM 53-00-03 REPAIR 1 STEP 1 DETAIL II. C/W HFEC SURFACE ISDR DALA2021011400231Access Panel · missingUPON ARRIVAL, THE NGS SERVICE DOOR PANEL (194BR) WAS DISCOVERED TO BE MISSING. MAINTENANCE INSTALLED ANOTHER SERVICABLE PANEL, IAW B757 AMM 20-51. A/C OK FOR SERVICE.SDR A6WA202101047509Skin · crackedFS 220 RIGHT SIDE EXTERNAL SKIN CRACKED AFT OF NOSE GEAR CUT OUT RADIUS. AIRCRAFT REMOVED FROM SERVICE. REPAIRED FUSELAGE EXTERNAL SKIN FS 220.00 RIGHT SIDE AFT OF NOSE GEAR CUT OUT, IAW MHI RJ AVIATION REO 601R-53-11-3647.SDR SWAA2021010739026Skin · dented(REF DEFECT NO 5125) FUSELAGE SKIN HAS A DENT AT STA 315, 5' BELOW STR 27R AND 8' FWD OF E&E CUTOUT. EVALUATED DENT ON FUSELAGE SKIN AT STA 315; 5' BELOW STR 27R AND 8' BELOW OF E7E CUTOUT. DENT MEASURES (L: 5.7 / W: 3.7/ Y: .083 / W/Y: 44.57) OUT OF LIMITS SDR SWIA202055994Doubler · damagedFORWARD VALVE RETAINER DOUBLER P/N KBA670-31630-9SB AT FS280.00 BETWEEN STGR27 AND STGR26R HAS MISLOCATED VALVE HOLE (C-CHECK) RO 2/5/2021 REPAIRED FUSELAGE SKIN BETWEEN FS280.0 - FS333.0 AND STR 26L - STR 26R. REF REO 670-53-21-1914 REV. -- DATED 2021-01-SDR JJBA20201229034Skin · dentedSUSPECTED DENT FOUND ON CENTER FUSE II, BETWEEN FR 27-28 AND BETWEEN STR 1L-2L. DENT ON CENTER FUSE II, BETWEEN FR 27-28 AND BETWEEN STR 1L-2L REPAIRED.SDR DALA2021010104358Landing · crackedDURING CCK AT QRO, WHILE PERFORMING BASE ZONAL INSPECTIONS PER WC 5330-2517, A CRACK WAS REPORTED AFFECTING THE GROUND POWER ACCESS LAND EGPR DOUBLER, BETWEEN STA 219.80 TO 235.80 & S-21R TO S-24R. MAINTENANCE REPAIRED DAMAGE, PER ERA 589204-14.SDR CALA2020123001412Skin · crackedLT FWD OVER WING HATCH FOUND CRACK AT THE OUTER SKIN 1" AFT OF THE LT LOAD PROFIL TOP AND BOTTOM OF THE NR 2 HORIZONATL BEAM -AD RELATED-A3NB-52-4-6031, PER HAECO LCQ N/R 9290338/32338 GENERATED BY V914670. REMOVED AND REPLACED FWD AND AFT ANGLE SEGMENT AT LTSDR FDEA202012280447Skin · crackedCRACK INDICATION ON FRAME 54 (2 INCH AFT SIDE) AND STGR 44 LT (2 INCH UPPER) OPEN HOLE IN AFT CARGO COMPARTMENT (1 EA) (CRACK DIRECTION 12 O CLOCK) PERFORMED REPAIR LOC. ON FRAME 54 (2 INCH AFT SIDE) AND STGR 44 LT (2 INCHES UPPER) OPEN HOLE IN AFT CARGO COMPASDR SWIA202055255Skin · dentedTRANSFER FROM EAML 550059. DENT BETWEEN FS 640 AND 672.2 HAS LARGE DENT APPROXIMATELY 6.4 X 6.3 INCHES WITH HOLE IN CENTER APPROXIMATELY 2.6 X 1.8 INCHES. LT FUSELAGE STRUCTURE DAMAGE BETWEEN FS 640.00 AND FS 672.20, STR 13L AND 16L WAS REPAIRED BY BOMBARDISDR SWIA202054937Skin · damagedDAMAGE IS LOCATED 6.0 INCHES AFT OF BUTT-JOINT OFF FR 21 AND 6.0 INCHES ABOVE STGR 21R OFF OF STGR 20R. THE DAMAGE IS A HOLE IN THE FUSELAGE MEASERING 2.5 INCHES X 2.25 INCHES. CLASSIFIED AS MAJOR REPAIR. FORM M-337 INITIATED. PERFORMED PERMANENT REPAIR ONSDR SWAA2021010439171Skin · damagedLT STA 475, 1.25 ABOVE S25L. DAMAGE OR BLEND OUT IS L .90 X W .70 AND .013 MATERIAL WAS REMOVED. DUE TO LIGHTNING STRIKE DAMAGE. MOD/REPAIRED PER SRM 53-00-01-2R-4 PERMANENT ACTION REQUIRED. PERMANENT REPAIR WITH SOLID FASTENERS MUST BE INSTALLED NO LATER SDR TX9220201228001Skin · corrodedDURING THE CONVERSION OF 737-800 PASSENGER AIRPLANE TO THE FREIGHTER TO DATUM AIRPLANE N239GE(MSN33717), TERRIBLE CORROSION DAMAGE WERE FOUND AT FUSELAGE SKIN AND STRINGERS OF E/E BAY AREA. SECTION 41 INNER SURFACE AT STA 294-STA 360, S-24L S-28L (P/N: 141A3
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