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 SWAA2024050974754Angle · crackedWING CENTER SECTION REAR SPAR VAPOR BARRIER ATTACH ANGLE CRACKED AT STA. 663.75 AND RBL.10 APPROX.<[01] ACCOMPLISHED WING CENTER SECTION VAPOR BARRIER UPPER ANGLE REPAIR AT RBL 10 STA 663 REF 57-10-10-2R-5;[02] CORRECTION TO STEP 1: ACCOMPLISHED WING CENTER SESDR SWAA2024041171901Beam · crackedRIGHT WING FIXED LEADING EDGE NOSE BEAM CRACKED AT SLAT STATION 50. RIGHT WING FIXED LEADING EDGE NOSE BEAM CRACKED REWORKED PER E/A 24-157-00924. C/W INSP PER E/A 24-157-00924. C/W RII OF REPAIR REF E/A 24-157-00924SDR FDEA202404070447Frame · crackedWINGS - BASIC WING STRUCTRUE - INSPECTION OF FR40 LOWER OUTBOARD RADIUS, LH SIDE, OUND CRACK AT AREA A STARTED FROM THE HOLE A LWR EDGE COMPILED WITH EO 6-5710-E0333575 D P5. REPAIRED THE CRACKED AREA A ON LH SIDE FR40 FWD FITTING LOWER OUTBOARD RADIUS. THSDR IPXA2024051575400Shroud · gougedLEFT WINGTIP LE HAS A DENT FRONT INBD SIDE. APPLIED TREAT AND PRIMER IAW SRM 51-21-10 PARAGRAPH 2. INSTALLED NEW SHROUD ASSY IAW SRM 51-40-21, PARAGRAPH 13. INSTALLED STRIP IAW IAW SRM 51-40-21 PARAGRAPH 5. APPLIED TOP COAT IN AREA IAW SRM 51-75-10, PARAGRAPHSDR HNA2024050900001Bonding Strap · corrodedCORROSION FOUND ON UPPER AND LOWER ATTACHMENT BRACKETS ON RH WING TIP. FABRICATED AND INSTALLED UPPER AND LOWER BONDING STRAPS ON R/H WINGTIP IAW EMB-145LR SRM 51-40-02SDR FDEA202404020433Former · crackedFOUND FORMER CRACKED AT RH WING STATION 441 0000704471 : FLEEHEARTY, AARON T - 02-APR-2024 21:46 INSTALLED NEW FORMER AND L-ANGLE FROM WING STA 441 REF B767 SRM 51-40-02, B767 SRM 57-41-09-2R AND FDX DWG SR67-57-002SDR DALA2024040804146Wing · damaged.SHIP 3244 DISC: **FLT SAFETY REQUEST*** PER TOPP 60-70-35 DUE TO A/C WINGTIP STRIKE DAMAGE. C/A: DUE TO FLT SAFETY REQUEST PLEASE PERFORM DFDR DOWNLOAD PER AMDS WORK CARD 3131-7001 USING P/N: FDS 400-301. (LP: 0271564)SDR DALA2024040404087Winglet · handler errorSHIP 3245 DISC: AFTER PUSH, TUG DISCONNECTED RH WING WAS STRUCK BY A319 LOWER WINGLET DAMAGED. C/A: PERFORMED INSPECTION OF OUTBOARD ON RT WING FOR DAMAGED FENCE PER A320 AMM 05-51-35-200-001A. ALL DISCREPANCIES WILL BE WORKED ON NON-ROUTINES. (LP: 5838354)SDR SWAA2024042567681Service Panel · corrodedCORROSION FUEL STATION PANEL LOCATED LEADING EDGE AT LEVEL OFSS 385 AT RT WING. REPAIRED FUEL STATION PANEL LOCATED L/E AT LEVEL OFSS 385 AT RT WING. IAW EA #24-157-01008-WIP1; EA #24-157-01008.SDR DALA2024032603803Bolt · strippedSHIP 1708 NUMBER 2 T/E FLAP GEAR ROTARY ACTUATOR REACTION RING MOUNT BOLT AT APPROX 10 O'CLOCK POSITION AS VIEWED FROM I/B SIDE HAS NO THREADS PROTRUDING THROUGH LOCK NUT. CORRECTIVE ACTION: INSTALLED CORRECT NUT PER B767 IPC 27-51-20-02 (0260328)SDR DALA2024032603802Bushing · nickedSHIP 1708 #1 POS ROTARY ACT I/B SUPPORT BUSHING APPEARS TO BE NICKED. CORRECTIVE ACTION: REPLACED BEARING ASSY PER W/C 2751-01046-02B (0260254)SDR CALA2024032800889Intercostal · crackedREF AMES NON ROUTINE: 168798-0600-0021. GENERATING ITEM: 63-5700 -1-2602. RW FIXED LEADING EDGE INTERCOSTAL AT RWS 538 CRACKED AT UPPER CORNER MARKED D-0007. REPLACED RW FIXED LEADING EDGE INTERCOSTAL AT RWS 538, WITH PN 14T2207-6 PER B767 SRM 51-40-02 PARAGRASDR IXXA2024041404Support · crackedRH WING FIXED L.E. FRAME SUPPORT STRUCTURE JUST O/B OF W.S.651 IS CRACKEDSDR SWAA2024040963628Winglet · corrodedCORROSION SPLIT SMITAR LOC TRAILING EDGE UPPER POSITION 2024-160824 CORROSION SPLIT SMITAR LOC TRAILING EDGE UPPER POSITION RT WING. REPLACED SPLIT SMITAR ARROW HEAD TRAILING EDGE RH IAW SRM 51-40-02-0G-0.SDR IXXA20240405001Former · crackedRH WING OUTBD LE HAS A CRACKED BRACKET TO THE NO.8 INBD CURATIN SPRING APPROXIMATELY WS 465. HAECO WO 320005 NON ROUTINE 34217SDR SWAA2024040960424Housing · corrodedCORROSION INTERNAL CAVITY LEADING EDGE REFUEL PANEL CASE AT RT WING. REPLACED FUEL QUANTITY INDICATOR HOUSING RT WING IAW SRM 51-40-02 TEST IS OK.SDR A6WA202403048720Landing · cracked50057 334424 601R-57-21-3821 HRS 24.45 CRACK FOUND ON LOWER WING SKIN LANDING UNDER ACCESS PANEL 601R10213-4. AIRCRAFT REMOVED FROM SERVICE. (RH MLG) REPAIR WAS PERFORMED TO THE RH WING LOWER AFT PLANK BY MHI MRT. REF. MHI RJ REO 601R-57-21-3821 REV. A DASDR YENA2024030500315Skin · corrodedDURING HEAVY MAINTENANCE: LH WING UPPER SKIN T/E AREA SIGNS OF CORROSION BETWEEN RIB 11 AND RIB 12; REF STS WO W003143 NR N0314 PERFORMED REPAIR IAW EA 110-2024-014 REV A, RDAF 80659065/092/2024AAND EC # A24-233-01. PERFORMED BY STS TECH MA0091 AND RII BY STS SDR IPXA2024040157286Fitting · cracked*** SUPPLEMENTAL SDR *** FAULT: CRACK FOUND AT 10 O'CLOCK POSITION FACING AFT AT FR40 LOWER JUNCTION RH SIDE. APPLIED PROTECTION SURFACE ON FASTENERS HEAD IAW SRM 51-23-10. (8 OZ PAINT CUP #02-012-176) AND APPLIED CIC IAW EO: M-5100-2780-L ON STIFFENER AT FR 4SDR SWAA2024031556790Plate · defectiveREFUEL PANEL INDICATORS PLATE DEFECTIVE<[01] REMOVED AND REPLACED P15 REFUEL PANEL PLATE I/A/W BOEING AMM 28-21-00-000-801 & 28-21-00-400-801; OPS CHECKS FOUND NORMAL;[02] VERIFIED P15 REFUEL PANEL PLATE REPLACEMENT.SDR FDEA202402210206Fitting · damagedDURING ACCOMPLISHED W/C EF-5730-E0340076 P11 STEP #3 PAGE 5 OF 13. FOUND #8 HOLE 2ND OVERSIZED. REMOVED & REINSTALLED #1 ENG IB & OB FAN COWLS, #1 PYLON BULLNOSE, IB TORQUE TUBE BTWN SLAT 4 & 5, Y-DUCT, LUBE FITTING, FUEL SUPPLY LINE & UPPER LINK IAW B757SDR KCSA202402211027Fitting · crackedL/H WING SUPPORT BEAM END FITTING IS CRACKED.SDR FDEA202402210205Unknown · misoverhauledWHILE CARRY OUT EO E G-5710-E0366409 D PART7, FOUND FIGURE 57, SHEET 2 OF 5, THE SECTION CUT B-B ARROW NOT MATCH THE VIEW B-B ORIENTATION SHOWN. DISCREPANCY IN EO E G-5710-E0366409 D PART7, FIGURE 57, SHEET 2 OF 5 SECTION CUT B-B ARROW ORIENTATION IS CLARISDR FDEA202402210204Unknown · misoverhauledWHILE CARRY OUT EO E G-5710-E0366409 D PART7, FOUND FIGURE 53, SHEET 2 OF 3, THE SECTION CUT B-B ARROW NOT MATCH THE VIEW B-B ORIENTATION SHOWN AND THE GAP 0.60 MIN IS TOO WIDE TO LOCATE THE REPAIR ANGLE. DISCREPANCY IN EO E G-5710-E0366409 D PART7, FIGURESDR FDEA202402210203Unknown · misoverhauledWHILE CARRY OUT EO E G-5710-E0366409 D PART7, FOUND FIGURE 51, SHEET 2 OF 3, THE SECTION CUT B-B ARROW NOT MATCH THE VIEW B-B ORIENTATION SHOWN AND THE "0.60 - 0.30 TYPICAL GAP" SHOWN SEEMS TOO BIG. DISCREPANCY IN EO E G-5710-E0366409 D PART7, FIGURE 51, SSDR FDEA202402210202Unknown · misoverhauledWHILE CARRY OUT EO E G-5710-E0366409 D PART7, FOUND FIGURE 49, SHEET 2 OF 3, THE SECTION CUT B-B ARROW NOT MATCH THE VIEW B-B ORIENTATION SHOWN. DISCREPANCY IN EO E G-5710-E0366409 D PART7, FIGURE 49, SHEET 2 OF 3 SECTION CUT B-B ARROW ORIENTATION IS CLARISDR FDEA202402210201Unknown · misoverhauledWHILE CARRY OUT EO E G-5710-E0366409 D PART7, FOUND FIGURE 47, SHEET 2 OF 4, THE SECTION CUT D-D ARROW NOT MATCH THE VIEW D-D ORIENTATION SHOWN. DISCREPANCY IN EO E G-5710-E0366409 D PART7, FIGURE 47, SHEET 2 OF 4 SECTION CUT D-D ARROW ORIENTATION IS CLARISDR FDEA202402210199Unknown · misoverhauledWHILE CARRY OUT EO E G-5710-E0366409 D PART8, FOUND FIGURE 120, SHEET 2 OF 5, THE SECTION CUT B-B ARROW NOT MATCH THE VIEW B-B ORIENTATION SHOWN. DISCREPANCY IN EO E G-5710-E0366409 D PART8, FIGURE 120, SHEET 2 OF 5, SECTION CUT B-B ARROW ORIENTATION IS CLSDR FDEA202402210198Unknown · misoverhauledWHILE CARRY OUT EO E G-5710-E0366409 D PART8, FOUND FIGURE 116, SHEET 2 OF 3, THE SECTION CUT B-B ARROW NOT MATCH THE VIEW B-B ORIENTATION SHOWN AND THE 0.60 MIN GAP TOO WIDE TO LOCATE THE REPAIR ANGLE. DISCREPANCY IN EO E G-5710-E0366409 D PART8, FIGURE 1SDR FDEA202402210197Unknown · misoverhauledWHILE CARRY OUT EO E G-5710-E0366409 D PART8, FOUND FIGURE 114, SHEET 2 OF 3, THE SECTION CUT B-B ARROW NOT MATCH THE VIEW B-B ORIENTATION SHOWN AND THE "0.60 - 0.30 TYPICAL GAP" SEEMS TOO BIG. DISCREPANCY IN EO E G-5710-E0366409 D PART8, FIGURE 114, SHEETSDR FDEA202402210196Unknown · misoverhauledWHILE CARRY OUT EO E G-5710-E0366409 D PART8, FOUND FIGURE 112, SHEET 2 OF 3, THE SECTION CUT B-B ARROW NOT MATCH THE VIEW B-B ORIENTATION SHOWN. DISCREPANCY IN EO E G-5710-E0366409 D PART8, FIGURE 112, SHEET 2 OF 3, SECTION CUT B-B ARROW ORIENTATION IS CLSDR FDEA202402210195Unknown · misoverhauledWHILE CARRY OUT EO E G-5710-E0366409 D PART8, FOUND FIGURE 110 SHEET 2 OF 4, THE SECTION CUT D-D ARROW NOT MATCH THE VIEW D-D ORIENTATION SHOWN. DISCREPANCY IN EO E G-5710-E0366409 D PART8, FIGURE 110 SHEET 2 OF 4, SECTION CUT D-D ARROW ORIENTATION IS CLASDR AALA202404153249Fitting · corrodedAIRCRAFT IN BASE MAINTENACE: CORROSION ON RIGHT WING MAIN LANDING GEAR RETRACTION ACTUATOR ATTACHMENT BRACKET / JACK FITTING BETWEEN WS 70 AND WS 141, BETWEEN RIBS 2 AND RIB 3. REPAIRED JACK FITTING PER SRM 57-26-13-300-008.SDR AALA202404150942Fitting · corrodedAIRCRAFT IN BASE MAINTENACE: CORROSION ON LEFT WING MAIN LANDING GEAR RETRACTION ACTUATOR ATTACHMENT BRACKET / JACK FITTING BETWEEN WS 70 AND WS 141, BETWEEN RIBS 2 AND RIB 3. REPAIRED JACK FITTING PER SRM 57-26-13-300-008.SDR UIEA2024021900092Winglet · not reportedLEFT WINGLET SCRAPED.(<P>TRANSFERED TO DMI 203268 IAW CDL 57-28-01 DUE DATE 18JUN24. PLACARD INSTALLED. </P>)SDR FDEA202402190187Fitting · damagedDURING INSP OF R/H WING OUTER-UPPER SKIN FITTINGS AND DIAGONAL BRACE FASTENNERS AND SHIM PER E 5730-E0340076 L P12 STEP:3 HOLE 14 FASTENNER FOUND SECOND OVER SIZE. REPAIR/COMPLIED WITH FEDEX EA# F-5730-T0378078 P1 TITLE: WINGS- PLATES AND SKIN- RH WING - SDR DALA2024022102430Support · damaged(LOG 0207922) FOUND RIGHT WING T/E PANEL AFT RIB SUPPORT DAMAGED. REMOVED RT WING T/E PANEL AFT RIB SUPPORT REF BACDWG'S 115A3700 SHEET 82 AND 115A3712 SHEET 7. LOCATED AND DRILLED AND INSTALLED T/E PANEL AFT RIB SUPPORT PN # (115A3758Y36), 2 EA FITTING PN # (SDR FDEA202402180184Structure · unknownWHILE ACCOMPLISHING EO # EG-5710-E0366409D-PART8, FOUND RIGHT HAND RING CHORD MODIFICATION KIT PART NUMBER 005W0129-4 SHORTAGE REPAIR ANGLE PART NUMBER 691W0017-2. EO # EG-5710-E0366409D PART8 WORK ACCOMPLISHED WITH THE RIGHT HAND RING CHORD REPAIR ANGLESDR DALA2024022002351Shim · migratedSHIP 696 AA AD IN REF AMDS 5720-01100-02B MIGRATED SHIM " 1C " ON INBD DRAG FITING AT RH WING. CORRECTIVE ACTION: SUMMARY OF NRC 00283. INBD DRAG FITTING AT RH WING WAS REPAIRED PER ER/A 598799-14AD REV. A SECTION VI. PERMANENT REPAIR. (0205318)SDR DALA2024022002337Shield · damagedSHIP 3157 R/H WINGTIP GLAZE SHIELD ASSY DAMAGED. CORRECTIVE ACTION: REPAIRED PER ER/A 615976-14. (5452786)SDR HNAA2024030400187Support Bracket · cracked00252 RH WING PANEL SUPPORT BRACKETS ON WING UPPER SURFACE ALONG Y 1085 ARE CRACKED. INSTALLED NEW SERVICEABLE ANGLES P/N 145-67034-002,P/N 145-67291-002 AND P/N 145-67290-004 @ RH OVERWING IAW EMB145LR SRM 51-40-02. SPLICED AND LOCATED AND DRILLED NEW FAIRINSDR ABXA2024021900626Plate · corrodedDURING C-24 MAINTENANCE CHECK AT HAECO AMERICAS, DURING C-24 MAINTENANCE CHECK AT HAECO AMERICAS, AND DURING ACCOMPLISHMENT OF SB 767-53A0 I 00 REV 02, MAINTENANCE DISCOVERED CORROSION ON THE RIGHT-HAND BEARING PLATE PIN I I ITI008-1 AS SHOWN IN FIGURE I. THE SDR AALA202402205188Sleeve · wornAIRCRAFT IN BASE MAINTENANCE: LEFT PYLON AFT ATTACH FITTING UPPER SLEEVE WORN. REPLACED SLEEVE PER AMM 54-51-00.SDR SWAA2024021652190Winglet · delaminatedRT OUTER WINGLET HAS DELAMINATION<[01] UPON FURTHER INSPECTION; FOUND DELAMINATION OUT OF LIMITS PER SRM 57-30-01. LENGTH- 5.5? WIDTH- 5.3?. REFERENCE TABLE 1:M ALLOWABLE DAMAGE FOR FIGURE 101.;[02] UPON FURTHER INSPECTION; FOUND DELAMINATION OUT OF LIMITS PERSDR DALA2024021402128Winglet · damaged(LOG 5598700) LEFT WINGTIP DAMAGED. NUMBER 1 SLAT ALSO DAMAGED. PERFORMED HFEC INSPECTION PER B737 AMM 05-51-36-210-801 ON LT WINGTIP ARM FOR WINGLET STRIKE- NO DEFECT NOTED- REF STEP 2 ERA 615811-14. REMOVED AND REPLACED NO.1 SLAT PER AMDS W/C 2780-452701. INSDR SWAA2024031451608Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE LOCATED AT LEVEL ORSS 214 AT RT WING 2024-121620<[01] REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED AT LEVEL ORSS 214 AT RT WING IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9;[02] CERTIFIED STEP 1 COMPLETEDSDR VNAA202402290008Canister · crackedCRACK IN CANISTER NO.3 , STA. WS148 OF INTERNAL RH MAIN FUEL TANK. CANISTER NO.3 , STA. WS148 OF INTERNAL RH MAIN FUEL TANK WAS REPAIRED PER REO 670-57-42-577.REV.--SDR P7UR202402160001Retainer · brokenDURING OPEN UPS FOR REQUIRED MAINTENANCE INSPECTIONS, PANEL 671BB RETAINER ASSEMBLY SEAL ANGLE WAS FOUND WORN IN NUMEROUS AREAS AND THE INBOARD END FOUND BROKEN DUE TO CONTACT WITH AILERON BALANCE WEIGHT ATTACH FITTING DURING AILERON MOVEMENTS. DURING EVALUATISDR FDEA202402120144Former · crackedRIGHT WING FIXED LEADING EDGE FORMER AT XOS 584 FOUND CRACK ABOUT 2 INCHES. RT WING FIXED LEADING EDGE AT XOS 584 CRACKED FORMER REMOVED AND REPLACED IAW MD-11 SRM 51-31-01-OG. FORMER FABRICATED IAW DRAWING ARB 2931 REVISION H. REPAIR CLASSIFIED AS MAJOR IASDR 2024FA0000274Fillet · crackedWE HAVE FOUND EVIDENCE OF CRACKING ON THE BULKHEAD - WING FILLET, STA. 181
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