JASC 5710
Service difficulty reports · 4,458
Reports filed under 5710 · Wing Main, Frame 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 = '5710' 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 = '5710' 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 SWAA2024112757150Vapor Barrier · crackedL/H A/C BAY STA 663 ANGLE TO VAPOR BARRIER CRACKED AT FASTENER HOLE LBL 9<[01] REMOVED FASTENERS COMMON TO REPAIR AT STA 663 VAPOR BARRIER ATTACH ANGLE VERTICAL FLANGE IAW SRM 57-10-10-2R-5.;[02] CUT AND REMOVED DAMAGED PORTION OF L/H A/C BAY STA 663 ANGLE PERSDR SWAA2024112757151Vapor Barrier · crackedR/H A/C BAY STA 663 ANGLE TO VAPOR BARRIER CRACKED AT FASTENER HOLE RBL 10<[01] REMOVED FASTENERS COMMON TO REPAIR AT STA 663 VAPOR BARRIER ATTACH ANGLE VERTICAL FLANGE IAW SRM 57-10-10-2R-5.;[02] CUT AND REMOVED DAMAGED PORTION OF R/H A/C BAY STA 663 ANGLE PESDR SWAA2024121056919Bracket · crackedCRACK BODY STATION 540 LBL 7 BRACKET AT AIR CONDITIONING BAY 2024-685477<[01] REPLACED BRACKET LOCATED STATION 540 LBL 7 AT AIR CONDITIONING BAY IAW B737-700 SRM 51-40-02-0G.;[02] REPLACED BRACKET LOCATED STATION 540 LBL 7 AT AIR CONDITIONING BAY IAW B737-700 SDR SWIA2024122301377Beam · chafedLH INBOARD FLAP FLS24.00 VANE ACTUATOR BEAM CHAFFED (C-CHECK RO 12/20/2024) REPAIRED LH INBOARD FLAP FLS24.00 VANE ACTUATOR BEAM COMPLIED WITH REO 670-57-52-257 REV A DATED 2024-08-20. PERFORMED ELECTRICAL EXTENSION AND RETRACTION OF THE SLATS AND FLAPSSDR SWAA2024120571586Angle · wornWEAR ON ANGLE LOCATED BS540 PLUS 9INCH AND RBL40 AT CENTER WING BOX 2024-680424<[01] ON STEP 5: TOOL USED EDDY CURRENT EQUIPMENT PN: NORTEC500D; SN: N500X11290U021704; DUE DATE: 14 APR 25;[02] REPAIRED ANGLE LOCATED BS540 PLUS 9INCH AND RBL40 AT CENTER WING BOSDR SWAA2024112656227Vapor Barrier · crackedL/H VAPOR BARRIER ANGLE CRACKED AT APPROX LBL 8.<[01] REMOVED DAMAGE; FORMED PARTS; ALODINED; PRIMED AND INSTALLED REPAIR PARTS AT VAPOR BARRIER ATTACH ANGLE L/H. STA LBL 5 TO LBL20 APROX. IAW B737-800 SRM 57-10-10-5-2R. ACCOMP. HFEC CUT EDGES; IAW B737 NDT MASDR SWAA2024112656228Vapor Barrier · crackedR/H VAPOR BARRIER ANGLE CRACKED AT APPROX RBL 8<[01] REMOVED; LOCATED; DRILLED; AND INSTALLED NEW VAPOR BARRIER ATTACH ANGLE; CHANNEL; STIFENER AND FITTING AT WING SECTION REAR SPART R/H FROM STA RBL 5 TO RBL 65 IAW B737-800 SRM 57-10-10-2R-5 ACCOMPLISHED A OPSDR EE4Y2024103121223Plate · corrodedDURING ACCOMPLISHMENT OF THE ALLEGIANT TASK A32X-545156-01-1-001_P1-OP-UP-ENG/001 ,ENGINE# 1 PYLON OUTBOARD CENTER SECTION AT RIB 8 STR 5R BOTTOM REINFORCEMENT PLATE WITHCORROSION WAS FOUND. OEM WAS CONTACTED FOR REPAIR INSTRUCTIONS. AIRBUS PROVIDED REPAIRINSTSDR EE4Y2024103121222Plate · corrodedDURING ACCOMPLISHMENT OF THE ALLEGIANT TASK A32X-545156-01-1-002_P1-OP-UP-ENG/001 ,ENGINE # 2 PYLON OUTBOARD CENTER SECTION AT RIB 8 STR 5R BOTTOM REINFORCEMENT PLATE WITH CORROSION WAS FOUND. OEM WAS CONTACTED FOR REPAIR INSTRUCTIONS. AIRBUS PROVIDED REPAIR ISDR DALA2024103110531Strut · corrodedSHIP 3134 CORROSION ON CONNECTORS 7542VC AND 7540VC OF INTERCONNECTING STRUT ON RH WING. CORRECTIVE ACTION: REPLACED CONNECTORS AS PER AIRBUS AWM 27-51-11, AWM 27-51-12, ESPM 20-44- 11 PAGEBLOCK 0101 CONFIG 01 AND AIRBUS ESPM 20-52-21-760-00002. (0636436)SDR DALA2024102910490Bonding Plate · corrodedSHIP 3133 CORROSION BONDING PLATE FLAP TRACK FAIRING 4 (533CB) ON LH WING. CORRECTIVE ACTION: COMPLIED WITH ER/A 620443-14. (0629887)SDR DALA2024102910488Bonding Plate · corrodedSHIP 3133 CORROSION BONDING PLATE FLAP TRACK FAIRING 3 (532CB) ON LH WING. CORRECTIVE ACTION: COMPLIED WITH ER/A 620443-14. (0629892)SDR DALA2024102910487Bonding Plate · corrodedSHIP 3133 CORROSION ON BONDING PLATE FLAP TRACK FAIRING 631CB RH WING. CORRECTIVE ACTION: COMPLIED WITH ER/A 620443-14. (0629898)SDR SWAA2024121053294Vapor Barrier · crackedCRACKED PREVIOUS REPAIR VAPOR BARRIER BS 663 RBL 25 TO RBL 40 (MARKED)<[01] CRACKED PREVIOUS REPAIR VAPOR BARRIER; BS 663 RBL 25 TO RBL 40; WAS REMOVED AND REPLACED WITH A NEW REPAIR IAW SRM 51-70-04-2R-10.;[02] JOB COMPLETE.SDR DALA2024102810469Plate · corrodedSHIP 3160 CORROSION FOUND ON PYLON REINFORCING PLATE, BOTTOM SKIN AT RIB 8 AND STR 5 ON LH WING. CORRECTIVE ACTION: PERFORMED REPAIR PER ER/A 620429-14. (0627371)SDR SWAA2024111251536Mount · corrodedPANEL 632JB MOUNTING RING HAS EVIDENCE OF CORROSION.<[01] PROCURED SERVICEABLE REPLACEMENT RING FROM STOCK. RING TO BE INSTALLED ON CLOSE TASK# TTG8Q00W3AFA.;[02] VERIFIED NEW RING WILL BE REPLACED ON TASK CARD # TTG8Q00W3AFA.SDR SWAA2024111251535Mount · corrodedPANEL 632FB MOUNTING RING HAS EVIDENCE OF CORROSION.<[01] PROCURED SERVICEABLE REPLACEMENT RING FROM STOCK. RING TO BE INSTALLED ON CLOSE CARD# TTG8Q00W3BVC;[02] PROCURED SERVICEABLE REPLACEMENT RING FROM STOCK. RING TO BE INSTALLED ON CLOSE CARD# TTG8Q00W3AFGSDR SWAA2024102851744Panel · crackedPANEL CRACKED AT FASTENER HOLE. RIGHT WING INBOARD FLAP TRACK LOWER WING SKIN PANEL. PANEL CRACKED AT FASTENER HOLE. APPROX. 0.5 IN. LENGTH TO EDGE OF PANEL. RIGHT WING INBOARD FLAP TRACK LOWER WING SKIN PANEL. ITEM (8) 115A2723 SRM 57-51-01-0I-1.<[01] 04 - RESDR UIEA2024101701048Access Panel · puncturedLH WING, OUTBOARD FLAP T. E. (ACCESS PANEL 566 JT) INTERNAL SURFACE HONEYCOMB WITH PUNCKTURE(<P>PUNCTURE WAS REPAIRED IAW SRM 57-53-01-2R-1 & SRM 51-70-10-2R-4. NO FURTHER DEFECTS NOTED</P>)SDR IPXA2024120337570Panel · crackedCUT OUT UNDER PANEL 513AB IS CRACKED. DOT 101-01 TG-101. INSTALLED DOUBLERS IAW A300-600 SRM 51-40-21 WITH FASTENERS P/N:MS20426AD4-4, BATCH# 0004249215,NUT PLATE P/N: MS21060-3,BATCH:0004177915.SDR DALA2025012400602Erosion Shield · peelingLH WINGLET LEADING EDGE EROSION TAPE PEELED UP AT LOWER EDGE. LH WINGLET LEADING EDGE WHERE EROSION TAPE IS DAMAGED AND FOUND NO UNDERLYING DAMAGE. TRIMMED OFF EXCESS BOOT MATERIAL TO MEET AERODYNAMIC SMOOTHNESS IAW A220 ASRP 57-32-00-00AAA-662A-A. FWD TO MONISDR IPXA2024102428366Hinge Fitting · crackedCRACKED SUPPORT RIB RIGHT WING NO : 10 SPOILER INBOARD SUPPORT RIB (REPLACE). I.A.W AMM 27-61-02-424-023 REV.143 AND AMM 27-61-00-825-072 REV.143 ADJUST THE NO.12 SPOILER PCA AND RESULT WAS SATISFIED. I.A.W AMM 20-10-09-404-007 REV.143 DO A LEAK CHECK TEST FSDR A8ZR202410240001Beam · crackedCRACK FOUND ON R/H WING NOSE BEAM BETWEEN WING STA 668 TO 694 BEHIND ACCESS PANEL 621SB. ACCOMPLISHED REPAIR ON R/H WING NOSE BEAM IAW BOEING MESSAGE NUMBER ESI-NAC-24-0101-07B AND RDR NUMBER ESI-NAC-24-0101-14B FOR THE INSTALLATION OF REPAIR SPLICE AND RE-ENFSDR DALA2024101610133Structure · corrodedSHIP 3134 CORROSION ON INTERNAL AREA LOC. BTW RIB5 AND RIB6 FLAP TRACK 3 ON RH WING. CORRECTIVE ACTION: REMOVED O/B FLAP ON R/H WING ON UNSERVICEABLE CONDITION, THE REMOVAL WAS DOCUMENTED ON AMDS CARD #2750-1020-RT. (0610437)SDR SWAA2024102948206Support · crackedR/H WINGLET; UPPER SURFACE SUPPORT STRUCTURE FOR PNL #627BR IS CRACKED<[01] REMOVED R/H WINGLET I.A.W AMM 57-31-21-000-801 <BR><BR>TORQUE WRENCH: AAR 40186<BR>DUE DATE: 12/26/24<BR><BR>LOAD CELL: AAR 6424<BR>DUE DATE: 04/05/24;[02] TRANSFERED WINGLET REMOVAL TSDR DALA2024101410083Fitting · corrodedSHIP 3143 CORROSION TRAILING EDGE FITTING LOCATED BTW RIB 7 TO RIB 8 ON LH WING. CORRECTIVE ACTION: REPLACED FITTING ON TRAILING EDGE LOCATED BTW RIB 7 TO RIB 8 ON LH WING AND FASTENERS AS PER A319 SRM 51-42-11 AND SRM 51-72-11. (0607442)SDR AALA202410314292Support Frame · excess playAIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY AILERON HINGE SUPPORT FRAME 3 ON RH WING. REPLACED AILERON-HINGE SUPPORT FRAME N0 3 ON RH WING IAW AMM 57-51-31-000-001-A AND AMM 57-51-31-400-001-A.SDR AALA202410315458Support Frame · excess playAIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY AILERON HINGE SUPPORT FRAME 2 ON RH WING. REPLACED AILERON-HINGE SUPPORT FRAME N0 2 ON RH WING IAW AMM 57-51-31-000-001-A AND AMM 57-51-31-400-001-A.SDR AALA202410314097Support Frame · excess playAIRCRAFT WAS IN BASE MAINTENANCE: EXCESSIVE PLAY AILERON HINGE SUPPORT FRAME NO. 1 ON RH WING. REPLACED AILERON-HINGE SUPPORT FRAME N0. 1 ON RH WING IAW AMM 57-51-31-000-001-A AND AMM 57-51-31-400-001-A.SDR HNAA2024111101066Torque Box · damagedF001233 RH WING TQ BOX OB FWD LOCATION HAS OVERSIZED J-BOLT HOLE. REPAIRED IAW EO1-57-24-0639SDR DALA2024101009957Bonding Strap · corrodedSHIP 3143 CORROSION ACCESS PANEL 531CB BONDING STRAP ON LH WING. CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTIONS ON FLAP TRACK FAIRING 531CB AS PER ER/A 620280-14. (0601050)SDR DALA2024101109965Door · broken-AD- BROKEN INBD BUTE DOOR OUTBD EDGE AT RH WING. (AD) SUMMARY OF NRC 00171: INBD BUTE DOOR OUTBD EDGE AT RH WING WAS REPAIRED PER ERA 618696-14TR REV ORIGINAL SECTION I. ASSOCIATED ER/A 14-618696 ADDED FOR AC 9528. (LP #0598854)SDR DALA2024101510102Strut · corrodedSHIP 3160 CORROSION ON INTERCONNECTING STRUT AT LH WING. CORRECTIVE ACTION: REPLACED INTERCONNECTING STRUT AT LH WING AS PER A320 FAM AMM 27-51-44-000-001-A. (0595847)SDR FDEA202410061431Support Fitting · corrodedRH MLG FWD LUG RIB 5 CORROSION IN BORE. REMOVED CORROSION FROM RH MLG FWD LUG RIB 5 PER AIRBUS R57240425 AND EA # 6-5710-T0380814 P1.SDR IXXA2024100606Access Panel · puncturedLEFT GENERATOR P31 PANEL PUNCTUREDSDR SWAA2024101544659Plate · crackedLEFT WING I/B WAFFLE PLATE UNDER PANEL 551EB CRACKED.<[01] REMOVED AND INSTALLED NEW L/H WING I/B WAFFLE PLATE UNDER PANEL 551EB PER SRM 51-40-02.;[02] INSPECTION C/WSDR UIEA2024092400945Sealant · missingRH WING, INSIDE FUEL TANK REAR SPAR, MISSING FILLET SEALANT ON SHUT OFF VALVE (2 E/A'S) BTW RIB 1/6.(<P>RH WING, INSIDE FUEL TANK REAR SPAR, FILLET SEALANT ON SHUT OFF VALVE WAS APPLIED IAW AMM TASK 28-21-02-404-021. NO FURTHER DEFECT NOTED</P>)SDR UIEA2024092500951Fill Port · corrodedRH WING, UPPER SURFACE, BASE OF OVERWING FILL PORT ADAPTER WITH EVIDENCE OF CORROSION(<P>OVERWING FILL PORT ADAPTER. CORROSION LEVE 1 WAS REWORKED, INSPECTED AND ALLOWABLE LIMITS FOUND IAW SRM 57-20-01-1A-1</P>)SDR DALA2024093009550Reinforcement · corrodedSHIP 3148 CORROSION LOWER SURFACE ON PYLON REINFORCING PLATE LOC. AT RIB8 AT LEVEL STR 5 ON LH WING. CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTIONS ON BOTTOM SKIN PYLON REINFORCING PLATE AT RIB 8 AND STR 5, LH SIDE AS PER ER/A 620045-14AD REV. (0579898)SDR FDEA202409271380Support Fitting · corrodedBUSH E HAS DAMAGE TO CHROME FACE. REMOVED AND REPLACED BUSHING D AND E PER AIRBUS R57240425.SDR HNAA2024103001044Torque Box · damagedE056822 RH WING TORQUE BOX 1 LOWER FWD CENTER FASTENER HOLE IS OVERSIZED AND DAMAGED. PREPPED, FABRICATED, AND INSTALLED BUSHINGS AND HILOCK IN RH WING TORQUE BOX 1 LOWER FWD HOLE IAW ETS2024-145-025752 "REV A" AND EO1-57-24-0603SDR SWIA20241203288Beam · damagedLEFT INBOARD FLAP OUTBOARD FLAP VANE ACTUATOR BEAM HAS FLAT SPOTS ON LOWER SURFACE. (MARKED IN RED) (C-CHECK RO 11/30/2024) DAMAGE (FLAT SPOTS), REMOVED BY BLENDING FROM LEFT INBOARD FLAP, INBOARD FLAP VANE ACTUATOR BEAM (OUTER TUBE), UPPER AND LOWER SSDR SWIA202412031288Beam · damagedLEFT INBOARD FLAP OUTBOARD FLAP VANE ACTUATOR BEAM HAS FLAT SPOTS ON LOWER SURFACE. (MARKED IN RED) (C-CHECK RO 11/30/2024) DAMAGE (FLAT SPOTS), REMOVED BY BLENDING FROM LEFT INBOARD FLAP, INBOARD FLAP VANE ACTUATOR BEAM (OUTER TUBE), UPPER AND LOWER SSDR DALA2024092409386Plate · corrodedSHIP 3148 CORROSION FOUND ON IB AND OB AL PLATES (FACES AND BORES) AT TRACK #3 IN THE INNER AND OUTER RIB 5 ECCENTRIC BEARING. CORRECTIVE ACTION: REPAIRED PER ER/A 620418-14. (0564838)SDR FDEA202409191329Fitting · corrodedCORROSION FOUND BETWEEN BUSHES 'D" AND "E" DURING RH RIB 5 INSPECTION COMPLIED WITH FED EX EA 6-571-T0316490 PT2 AND R57240425. MAJOR REPAIR. EA 6-5710- T0316490 WINGS - BASIC WING STRUCTURE - CORROSION REPAIR OF RIB 5 FWD LUG RH. MPN A57240810214.SDR SWAA2024102338078Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE LOCATED AT LEVEL ORSS 295 AT RT WING 2024-572854<[01] REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED AT LEVEL ORSS 295 AT RT WING I.A.W DWG 115A3712 SHEET: 7 REV: A ; DWG 115A3700 SHEET: 41 REV: - AND B737-700 SRM 51-10-02SDR CALA2024091602427Beam · damagedRH SIDE PNEUMATIC PANEL LOOSE. VERIFIED FLAP PEEN ON DISCREPANT AREA REF SRM 57-10-13-2R-3 OK TO TREAT AND PRIME REPAIR PARTS AND REPAIR AREAREF SRM OK TO INSTALL REPAIR PARTS REF SRM 57-10-13-2R-3 VERIFIED INSTALLATION OF REPAIR REF SRM 57-10-13-2R-3 AND GMM SDR CALA2024091602426Beam · wornRH SIDE PNEUMATIC PANEL LOOSE. VERIFIED FLAP PEEN ON DISCREPANT AREA REF SRM 57-10-13-2R-3 OK TO TREAT AND PRIME REPAIR PARTS AND REPAIR AREAREF SRM OK TO INSTALL REPAIR PARTS REF SRM 57-10-13-2R-3 VERIFIED INSTALLATION OF REPAIR REF SRM 57-10-13-2R-3 AND GMM SDR DALA2024091208971Strut · corrodedSHIP 3133 CORROSION INTERCONNECTING STRUT ON L/H WING. CORRECTIVE ACTION: REPLACED INTERCONNECTING STRUT ON LH WING. THE INSTALLATION ACCOMPLISHED PERAMDS CARD 2750-6010-LT AND AMDS CARD2750 -6020-LT. (0551912)SDR SWAA2024102843441Web · corrodedCORROSION WEB INTERNAL CAVITY LEADING EDGE FUEL INDICATORS AT RT WING 2024-572135<[01] TOOL USED ON STEP 3 UT EQUIPMENT P/N: 45MG; S/N: 130064101; CAL DUE DATE: 13-DEC-24;[02] TOOL USED ON STEP 4; 5 AND 6 ET EQUIPMENT: P/N: NORTEC 600D; S/N: 220272512; CAL DUE
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