JASC 5720
Service difficulty reports · 13,638
Reports filed under 5720 · Wing Miscellaneous Structure, 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 = '5720' 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 = '5720' 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 SWAA2022021663457Bracket · crackedRIGHT WING WEB ANGLE ATTACH BRACKET @ DEFLECTION CONTROL RIB CRACKED / [01] REMOVED DAMAGED BRACKET; LOCATED; DRILLED NEW BRACKET PER SRM 51-40-02. OK TO INSTALL;[02] REMOVED AND REPLACED PER SRM 51-40-02SDR SWAA2022022163355Strap · corrodedLEFT WING FWD BOOST PUMB HOUSING CORRODED AT UPPPER BONDING STRAP / [01] OPENED AND COLLARED THE NO. 1 FWD BOOST PUMP CIRCUIT BREAKER PER AMM 28-22-41-000-801 STEP 2H(4(B)) AND GAINED ACCESS TO CORROSION PER AMM 28-22-41-000-801 STEPS 4H(5; 8(UPPER STRAP ONLY)SDR SWAA2022022163359Strap · corrodedRIGHT WING FWD BOOST PUMP HOUSING CORRODED AT UPPER BONDING STRAP / [01] REMOVED UPPER SUPPORT ANGLE AT R/H BOOST PUMP FOR ACCESS TO FRONT SPAR WEB PER SRM57-20-10-1A-3;[24] REPAIRED CORROSION ON RIGHT WING FWD BOOST PUMP HOUSING AT UPPER BONDING STRAP IAW SWASDR SWAA2022013162708Angle · crackedLEFT WING LOWER TRAILING EDGE PANEL 651AB SUPPORT ANGLE CRACKED AT O/B ATTACH POINT ; CORRECTION; PANEL 561AB / [01] REMOVED AND REPLACED LEFT WING LOWER TRAILING EDGE PANEL 561AB SUPPORT ANGLE P/N:115A3758-9 I/A/W B737 SRM 51-40-02-0G-0. <BR>A-TAG#WN9095; [02SDR REXA2022012600121Support Angle · corrodedTIRE BURST SUPPORT ANGLE LH SIDE FOR PROTECTIVE COVERING CORRODED
"REMOVED & REINSTALLED PANEL 541AB IAW CRJ900 AMM 28-11-01-000/400-802
(A02) LEAK TEST GOOD IAW CRJ900 AMM 28-11-01-400-802-A01. REMOVED,
DRILLED, LOCATED, & INSTALLED SERVICABLE TIRE BURSSDR FDEA202201140069None · shearedREFER TO HUB STRIKE DAMAGE TO LH SLAT UPON INSPECTION OF UNDERLYING STRUCTURE AFTER REMOVAL OF BONDED PANEL ASSY 521ZB, DISCOVERED HOLE IN LEFT WING FIXED LEADING EDGE PANEL. HOLE IS APPROX. 2.5 X 2.0". COMPLIED WITH EA H-5720-T0366424 PART 1. "WING-SECONDASDR ABXA2022011324Skin · corrodedDURING AIRCRAFT C-CHECK AT AIRBORNE (TAMPA). AMES NR 0148 - LH WING, LOWER SURFACE, I/B WING AREA, CORROSION IN TWO SPOTS AROUND FASTENERS, AFT OF FUEL PNLS 531AB AND 531BB. DURING AIRCRAFT CURRENT CHECK AT AIRBORNE (TAMPA), MAINTENANCE DISCOVERED CORROSION ONSDR SWAA2022020961104Bracket · crackedRIGHT WING; BULB SEAL SUPPORT ANGLE BRACKET CRACKED; OUTBOARD END @ DEFLECTION CONTROL RIB; FORWARD OF SEAL; (MARKED; PICTURE) ; / [01] REMOVED AND REPLACED SUPPORT ANGLE BRACKET P/N 115A6260-1 PER SRM 51-40-02.; [02] INSPECTED AS REQUIRED.SDR SWAA2022013160902Bracket · elongatedA22-05; RIGHT WING INBD L/E; VIEWING THROUGH 611AT; PNEUMATIC DUCT ATTACH BRACKET WORN & ELONGATED AT ATTACH FASTENERS; MRK'D. ; / [01] REPLACE PNEUMATIC DUCT ATTACH BRACKET AS VIEWED THROUGH 611 AT IN RH WING L/E IAW AMM 36-13-01-400-801 STEP 7.G.(8) AND SRM SDR FDEA202201120057Former · crackedRIGHT WING LEADING EDGE UPPER SURFACE LES 560 HAS A POPPED RIVET HEAD REMOVED AND REPLACED THE CRACKED R/W L/E NOSE FORMER AT LES 560, OSS 565, IAW BAC DWG 114T2162, REV. -. REMOVED AND REINSTALLED THE NOSE FORMER ATTACH ANGLE IAW FEDEX EA H-5720- T0366360-SDR FDEA202201120058Bracket · crackedL/W L/E NOSE FORMER ATTACH BRACKET AT OSS 441.6 IS CRACKED REMOVED AND REPLACED THE R/W L/E NOSE FORMER ATTACH BRACKET AT OSS 441.6 IAW FEDEX EA H-5720- T0366352-P1, DATE: 11JAN2022, TITLE: WINGS - SECONDARY WING STRCT - LH WING, LEADING EDGE, ANGLE, OSS 44SDR FDEA202201120056Former · crackedRIGHT WING LEADING EDGE AT LES480 SLAT TRACK CLOSE OUT CURTAIN OUTBOARD FITTING RIVETS PULLED LOOSE FROM LEADING EDGE REMOVED AND REPLACED THE R/W L/E NOSE FORMER FOR THE LES480 SLAT TRACK CLOSE OUT CURTAIN IAW BAC DWG 114T2161, REV. -. REMOVED AND REINSTASDR SWAA2022021464890Access Panel · brokenBROKEN FUEL TANK STICK ASSY ON ACCESS PANEL 532NB AT LT WING ; 2022-11379 / [01] REPLACED ACCESS PANEL 532NB ASSY AT LT WING IAW B737-700 SRM 51-10-02. INSTALLATION OF THIS ACCESS PANEL WILL BE COMPLETED WITH TASK CARD TTG8Q00A8AFD. SEE INDIVIDUAL SIGNS OFF; [SDR SWAA2022021464891Access Panel · brokenBROKEN FUEL TANK FLOAT ON ACCESS PANEL 532QB AT LT WING ; 2022-11376 / [01] REPLACED ACCESS PANEL 532QB ASSY AT LT WING IAW B737-700 SRM 51-10-02.; [02] TASK COMPLETEDSDR SWAA2022021460578Access Panel · brokenBROKEN ACCESS PANEL 632NB QUANTITY INDICATOR AT RT WING ; 2022-11366 / [01] REPLACED ACCESS PANEL 632NB QUANTITY INDICATOR AT RT WING I.A.W. B737-700 AMM 28-44-11-400-802; AND THE LEAK TEST OF THE ACCESS PANEL 632NB WILL BE COMPLETED WITH TASK TTG8Q0095DSD; [0SDR SWAA2022013160493Angle · crackedLEFT WING TRAILING EDGE PANEL INBOARD OF DEFLECTION CONTROL RIB; LOWER SUPPORT ANGLE CRACKED AT OUTBOARD END. DOT 234/04 ; / [01] REMOVED CRACKED ANGLE IAW SRM 51-40-02-0G-0; [02] NEW ANGLE VERIFIED AS P/N 115A2156-7 A110117 IAW DWG 115A2512 SHT 16 REV-; [03] SDR ASAA2022011039661Skin · corrodedCORROSION NOTED DURING NDI INSPECTION CUSTOMER CARD 572127-01-1A-2R-C007 AT THE UPPER R/W SKIN LOWER SURFACE LOCATED 3" O/B OF RIB 10 COMMON TO THE UPPER REAR SPAR GROUNDED - YES. CORROSION NOTED DURING NDI INSPECTION CUSTOMER CARD 572127-01-1A-2R-C007 AT THE SDR ASAA2022011039660Skin · corrodedCORROSION NOTED DURING NDI INSPECTION CUSTOMER CARD 572127-01-1A-2R-C007 AT THE UPPER R/W SKIN LOWER SURFACE LOCATED 5" O/B OF RIB 14 COMMON TO THE UPPER REAR SPAR GROUNDED - YES. CORROSION NOTED DURING NDI INSPECTION CUSTOMER CARD 572127-01-1A-2R-C007 AT THE SDR ASAA2022011039659Skin · corrodedCORROSION NOTED DURING NDI INSPECTION CUSTOMER CARD 572127-01-1A-2R-C007 AT THE UPPER R/W SKIN LOWER SURFACE LOCATED 5" O/B OF RIB 19 COMMON TO THE UPPER REAR SPAR GROUNDED - YES. CORROSION NOTED DURING NDI INSPECTION CUSTOMER CARD 572127-01-1A-2R-C007 AT THE SDR ASAA2022011039658Skin · corrodedCORROSION RIGHT WING UPPER SKIN AT RIB 19 T/E BETWEEN SPOILERS 4/5 HAS CORROSION AT FASTENERS GROUNDED - YES. CORROSION RIGHT WING UPPER SKIN AT RIB 19 T/E BETWEEN SPOILERS 4/5 HAS CORROSION AT FASTENERS INSP AND REPAIRED PER EA A320-57EA-01458 REV 00 DATED 8/SDR ASAA2022011039657Skin · corrodedCORROSION NOTED DURING NDI INSPECTION CUSTOMER CARD 572127-01-1A-2R-C007 AT THE UPPER R/W SKIN LOWER SURFACE LOCATED 5" O/B OF RIB 11 COMMON TO THE UPPER REAR SPAR GROUNDED - YES. CORROSION NOTED DURING NDI INSPECTION CUSTOMER CARD 572127-01-1A-2R-C007 AT THE SDR ASAA2022011039653Skin · corrodedCORROSION RH WING UPPER SKIN AT RIB 5 T/E JUST FWD OF #1 SPOILER I/B HINGE HAS CORROSION AT FASTENERS GROUNDED - YES. CORROSION RH WING UPPER SKIN AT RIB 5 T/E JUST FWD OF #1 SPOILER I/B HINGE HAS CORROSION AT FASTENERS INSP AND REPAIRED PER EA A320-57EA-01458SDR ASAA2022011039651Skin · corrodedCORROSION RIGHT WING UPPER SKIN AT RIB 8 TO 10" HAS CORROSION AT FASTENERS GROUNDED - YES. CORROSION RIGHT WING UPPER SKIN AT RIB 8 TO 10" HAS CORROSION AT FASTENERS INSPECTED AND REPAIRED PER EA A320-57EA-01458 REV 00 DATED 8/22/2022SDR ASAA2022011039608Skin · corrodedCORROSION ON LEFT WING UPPER TRAILING EDGE SKIN LOWER SURFACE 3 INCHES I/B OF RIB 21 GROUNDED - YES. CORROSION ON LEFT WING UPPER TRAILING EDGE SKIN LOWER SURFACE 3" I/B OF RIB 21 REPAIRED PER EA # A320-57EA-01457 REV 00, DATED 08/11/2022SDR ASAA2022011039607Skin · corrodedL/H WING UPPER SKIN 6" I/B OF RIB 19 LOWER SURFACE HAS AREA OF CORROSION GROUNDED - YES. L/H WING UPPER SKIN 6" I/B OF RIB 19 LOWER SURFACE AREA OF CORROSION REPAIRED PER EA # A320-57EA-01457 REV 00, DATED 08/11/2022SDR ASAA2022011039606Skin · corrodedL/H WING UPPER SKIN 3" I/B OF RIB 18 LOWER SURFACE HAS AREA OF CORROSION GROUNDED - YES. L/H WING UPPER SKIN 3" I/B OF RIB 18 LOWER SURFACE AREA OF CORROSION REPAIRED PER EA # A320-57EA-01457 REV 00, DATED 08/11/2022SDR ASAA2022011039605Skin · corrodedCORROSION ON LEFT WING UPPER TRAILING EDGE SKIN UPPER SURFACE HAS 17 EA CORRODED FASTENERS AT FALSE SPAR RIB 9 GROUNDED - YES. CORROSION ON LEFT WING UPPER TRAILING EDGE SKIN UPPER SURFACE AT 17 EA FASTENERS AT FALSE SPAR RIB 9 REPAIRED PER EA # A320-57EA-0145SDR ASAA2022011039604Skin · corrodedCORROSION ON LEFT WING UPPER TRAILING EDGE SKIN LOWER SURFACE AT FALSE RIB 8 GROUNDED - YES. CORROSION ON L/H WING UPPER TRAILING EDGE SKIN LOWER SURFACE AT FALSE REAR SPAR RIB 8 REPAIRED PER EA # A320-57EA-01457 REV 00, DATED 08/11/2022SDR ASAA2022011039603Skin · corrodedCORROSION ON LEFT WING UPPER TRAILING EDGE SKIN LOWER SURFACE 3" O/B OF RIB 10 GROUNDED - YES. CORROSION ON L/H WING UPPER TRAILING EDGE SKIN LOWER SURFACE 3" O/B OF RIB 10 REPAIRED PER EA # A320-57EA-01457 REV 00, DATED 08/11/2022SDR ASAA2022011039602Skin · corrodedLEFT WING UPPER TRAILING EDGE SKIN LOWER SURFACE AT RIB 16 HAS CORROSION GROUNDED - YES. CORROSION AT LEFT WING UPPER TRAILING EDGE SKIN LOWER SURFACE AT RIB 16 REPAIRED PER EA # A320-57EA-01457, DATED 08/11/2022, REV 00SDR ASAA2022011039590Skin · corrodedL/H WING UPPER SKIN AT RIB 17 T/E JUST FWD OF #4 SPOILER I/B HINGE HAS CORROSION GROUNDED - YES. L/H WING UPPER SKIN AT RIB 17 T/E JUST FWD OF #4 SPOILER I/B HINGE CORROSION AT FASTENERS REPAIRED PER EA # A320-57EA-01457, DATED 08/11/2022, REV 00SDR ASAA2022011039589Skin · corrodedL/H WING UPPER SKIN AT RIB 13 T/E JUST FWD OF #2/3 SPOILERS HAS CORROSION GROUNDED - YES. CORROSION ON L/H WING UPPER SKIN AT RIB 13 T/E FASTENERS JUST FWD OF #2/3 SPOILERS REPAIRED IAW EA # A320-57EA-01457, DATED 08/11/2022 REV 00SDR ASAA2022011039588Skin · corrodedL/H WING UPPER SKIN AT RIB 5 T/E JUST FWD OF #1 SPOILER I/B HINGE HAS CORROSION AT FASTENERS GROUNDED - YES. L/H WING UPPER SKIN AT RIB 5 T/E JUST FWD OF #1 SPOILER I/B HINGE CORROSION AT FASTENERS REPAIRED PER EA # A320-57EA-01457 REV 00, DATED 08/11/2022SDR ASAA2022011039587Skin · corrodedL/H WING UPPER SKIN AT RIB 19 T/E BETWEEN SPOILERS 4/5 HAS CORROSION AT FASTENERS GROUNDED - YES. L/H WING UPPER SKIN AT RIB 19 T/E BETWEEN SPOILERS 4 AND 5 CORROSION AT FASTENERS REPAIRED PER EA # A320-57EA-01457 REV 00, DATED 08/11/2022.SDR ASAA2022011039586Skin · corrodedCORROSION NOTED DURING NDI INSPECTION CUSTOMER CARD 572127-01-1A-2L-C007 AT UPPER LEFT WING SKIN LOWER SURFACE LOCATED 3" O/B OF RIB 15 COMMON TO THE UPPER REAR SPAR. GROUNDED - YES. CORROSION ON L/H WING UPPER SKIN LOWER SURFACE 3" O/B OF RIB 15 COMMON TO THESDR ASAA2022011039585Skin · corrodedCORROSION NOTED DURING NDI INSPECTION CUSTOMER CARD 572127-01-1A-2L-C007 AT UPPER LEFT WING SKIN LOWER SURFACE LOCATED 3" O/B OF RIB 14 COMMON TO THE UPPER REAR SPAR. GROUNDED - YES. CORROSION ON L/H WING UPPER SKIN LOWER SURFACE 3" O/B OF RIB 14 COMMON TO THESDR ASAA2022011039584Skin · corrodedCORROSION NOTED DURING NDI INSPECTION CUSTOMER CARD 572127-01-1A-2L-C007 AT THE UPPER L/H WING SKIN LOWER SURFACE LOCATED 4" O/B OF RIB 11 COMMON TO THE UPPER REAR SPAR. GROUNDED - YES. CORROSION ON L/H WING UPPER SKIN LOWER SURFACE 4" O/B OF RIB 11 COMMON TO SDR ASAA2022011039583Skin · corrodedCORROSION NOTED DURING NDI INSPECTION CUSTOMER CARD 572127-01-1A-2L-C007 AT UPPER L/W SKIN LOWER SURFACE LOCATED 6" I/B OF RIB 7 COMMON TO THE UPPER REAR SPAR. GROUNDED - YES. CORROSION ON L/H WING UPPER SKIN LOWER SURFACE 6" I/B OF RIB 7 COMMON TO THE UPPER RSDR SWAA2022022159720Bracket · crackedCRACK FIXED TRAILING EDGE SUPPORT BRACKET LOCATED ORSS 271 APROX; BETWEEN RIB 7 AND RIB 8 AT LT WING 2022-15932 / [01] REPLACED FIXED TRAILING EDGE SUPPORT BRACKET (WEB) LOCATED ORSS 271 APROX; BETWEEN RIB 7 AND RIB 8 AT LT WING IAW B737-700 51-10-02 Ï¿½TEM 9 SDR FDEA202201100110Landing · crackedRIGHT LOWER WING FUEL ACCESS PANEL AT XORS 685-702 HAS A CRACK INDICATION AT BOLT HOLE 29. REPAIRED R/H LOWER WING FUEL ACCESS PANEL HOLE29 IAW SRM 57-20- 02-2R PG25 - PG31.SDR SWAA2022011260405Angle · crackedCRACK NOTED AT BS 663, LBL 09 BULKHEAD ATTACH ANGLE. REMOVED FASTENERS IN REPAIR AREA IAW SRM 51-40-02-0G-0. CUT AND REMOVED DAMAGED ATTACH ANGLE IAW SRM 57-10-10-2R-5 REPAIR 5. PERFORMED DVI OF REPAIR AREA AND UNDERLYING STRUCTURE. NO DEFECTS. COMPLETED SDR DALA2022011200240None · noneSHIP 687 LIGHTNING STRIKE DAMAGE FOUND ON RT BLENDED WINGLET APPROX 4 INCHES BELOW UPPER T/E TIP. CORRECTIVE ACTION: PERFORMED LIGHT BLENDOUT AT THE TRAILING EDGE WINGLET TIP, ALODINE AND PRIMED ALSO PAINTED THE ARE PER B757 SRM 57-31-01. (2081109)SDR SWAA2022021459619Plate · crackedCRACK INBOARD TRAILING EDGE CORRUGATED PLATE ORSS 270 APROX. AT RT WING ; 2022-11295 / [01] REPLACED CORRUGATED PLATE AND FASTENERS LOCATED INBOARD TRAILING EDGE ORSS 270 APROX. AT RT WING. IAW B737-700 SRM: 51-40-02 AND 51-10-02. Ï¿½TEM 9.; [02] REPLACED CORRSDR SWAA2022022159681Bracket · brokenBROKEN SUPPORT BRACKET LOCATED IRSS140 REAR SPAR UPPER AREA AT RT WING 2022-15834 / [01] REPLACED SUPPORT BRACKET LOCATED IRSS140 REAR SPAR UPPER AREA AT RT WING I.A.W B737-700 DWG 115A2000 REV: A AND SRM 51-10-02 ITEM 9. SEE INDIVIDUAL SIGNOFFS BELOW;[02] CORSDR SWAA2022021459614Structure · crackedCRACK SUPPORT STRUCTURE WING TO BODY FAIRING ANGLE AT LEVEL BS 500D AND STRINGER 19L AT LT WING ; 2022-11274 / [01] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 02-FEB-22; TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 14SDR MASA20220107013None · corrodedTHE RH WING FUEL ACCESS PANEL WAS FOUND TO HAVE CORROSION. PERFORM PERMANENT REPAIR CRJ7/9 SRM 57-12-32, FIG. 57-12-32-991-801, ITEM 2 (REV. 38 DATED 9 JULY 2021) AND SRM 57-12-32-001-A01, ALLOWABLE DAMAGE (REV. 38 DATED 9 JULY 2021 ). DEFECT LOCATION: RH WINGSDR SWAA2022021459037Float · crackedCRACK ACCESS PANEL 532QB ON FLOAT AT LT WING ; 2021-585137 / [01] REPLACED FLOAT ON ACCESS PANEL 532QB AT LT WING IAW ROCKWELL COLLINS CMM 28-40-11. TASK CARD TTG8Q00A5JSX COMPLETED. SEE INDIVIDUAL SIGN OFF BELOW.; [02] REPLACED FLOAT ON ACCESS PANEL 532QB AT SDR SWAA2022021459038Float · crackedCRACK ACCESS PANEL 632QB ON FLOAT AT RT WING ; 2021-585132 / [01] REPLACED FLOAT ON ACCESS PANEL 632QB AT RT WING IAW ROCKWELL COLLINS CMM 28-40-11. TASK CARD TTG8Q00A5LGG COMPLETED. SEE INDIVIDUAL SIGN OFF BELOW.; [02] REPLACED FLOAT ON ACCESS PANEL 632QB AT SDR SWAA2022013159312Plate · crackedR/H WING LOWER TRAILING EDGE WIGGLE PLATE PHENOLIC STRIP CRACKED IN TWO PLACES BETWEEN #7 AND #8 FLAP TRACK FAIRINGS APPROXIMATED ORSS 409 -440 (MARKED) ; / [01] REMOVED AND REPLACED R/H WING LOWER TRAILING EDGE WIGGLE PLATE BETWEEN #7 AND #8 FLAP TRACK FAIRINSDR SWAA2022021458586Plate · crackedCRACK ACCESS PANEL 651EB TRAILING EDGE PLATE AT RT WING (1 EA) ; 2022-11204 / [01] REPLACED PLATE (NUTPLATE STRIP) ON ACCESS PANEL 651EB TRAILING EDGE AT RT WING IAW DRAWING 115A2787 REV:A AND SRM B737-700 51-10-02 Ï¿½TEM 9; SEE INDIVIDUAL SIGNOFFS BELOW.; [02
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