JASC 5753
Service difficulty reports · 31,513
Reports filed under 5753 · Trailing Edge Flaps, 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 = '5753' 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 = '5753' 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 AALA202407080883Strut · defectiveAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED ON APPROACH INTO LAX DUE TO THE FLIGHT CREW REPORTING A FLIGHT CONTROL FLAPS LOCKED MESSAGE WITH THE FLAPS JAMMED AT POSITION 1. AIRCRAFT LANDED AFELY AT LAX WITHOUT FURTHER INCIDENT. **SUPPLEMENTAL REPORT FOR ASDR DALA2024070306734Fairing · corrodedCORROSION FLAP TRACK FAIRING 632CB BONDING PLATE ON RH WING. REPAIRED PER ER/A 618277-14.SDR SWAA2024070308042Skin · delaminatedR/H O/B FLAP TRAILING EDGE FLAP DELAMINATED I/B CORNER.<[01] 01 - REMOVED AND REPLACED PER [AMM 27-51-22-401-NG (OUTBOARD AFT FLAP - REMOVAL/INSTALLATION - PERMANENT)<BR>OPS CHECK GOOD.SDR DALA2024070206694Track · corrodedSHIP 3132 CORROSION PENDULUM TRACK 3 O/B FLAP RH WING. CORRECTIVE ACTION: REPAIRED PER ER/A # 618088-14 REV. ORIGINAL.SDR SWAA2024072907793Skin · delaminatedLH OUTBD AFT FLAP LOWER INBD CORNER HAS DELAMINATION ON UPPER AND LOWER SURFACES.<[01] OK TO INSTALL L/H OUTBD AFT FLAP.;[02] OK TO INSTALL AFT OUTBD FLAP;[03] INSTALLED NEW SERVICEABLE L/H O/B AFT FLAP PER AMM 27-51-22.;[04] INSTALLED NEW SERVICEABLE L/H O/B SDR FDEA202406300885Rib · crackedLH WING CENTER FLAP RIB UPPER FLANGE FOUND 3EA CRACKS AT RIB11, RIB13 BETWEEN REAR SPAR AND STGR2.7 COMPLIED WITH EA 6-5750-T0379691 P1 REPAIRED THE LH WING CENTER FLAP CRACKED RIB UPR FLANGE AT RIB11, RIB13 BETWEEN STGR2.7 AND REAR SPAR. TITLE: WING - FLSDR FDEA202406300884Rib · crackedLH WING CENTER FLAP RIB UPPER FLANGE FOUND 3EA CRACKS AT RIB17, RIB18, RIB20 BETWEEN REAR SPAR AND STGR2.8 COMPLIED WITH EA 6-5750-T0379691 P1 REPAIRED THE LH WING CENTER FLAP CRACKED RIB UPR FLANGE AT RIB17, RIB18, RIB20 BETWEEN STGR2.8 AND REAR SPAR. TITSDR FDEA202406300883Rib · crackedLH WING CENTER FLAP RIB UPPER FLANGE FOUND 3EA CRACKS AT RIB26, RIB27 BETWEEN REAR SPAR AND STGR2.7 COMPLIED WITH EA 6-5750-T0379691 P1 REPAIRED THE LH WING CENTER FLAP CRACKED RIB UPR FLANGE AT RIB26, RIB27 BETWEEN STGR2.7 AND REAR SPAR. TITLE: WING - FLSDR FDEA202406300882Rib · crackedRH WING CENTER FLAP RIB UPPER FLANGE FOUND 1EA CRACK AT RIB20 BETWEEN REAR SPAR AND STGR2.8 COMPLIED WITH EA: 6-5750-T0379692 P1 REPAIRED THE RH WING CENTER FLAP CRACKED RIB UPR FLANGE AT RIB20 BETWEEN STGR2.8 AND REAR SPAR. TITLE: WING - FLIGHT SURFACES SDR FDEA202406300881Rib · crackedRH WING CENTER FLAP RIB UPPER FLANGE FOUND 1EA CRACK AT RIB12 BETWEEN REAR SPAR AND STGR2.8 COMPLIED WITH EA: 6-5750-T0379692 P1 REPAIRED THE RH WING CENTER FLAP CRACKED RIB UPR FLANGE AT RIB12 BETWEEN STGR2.8 AND REAR SPAR. TITLE: WING - FLIGHT SURFACES SDR FDEA202406300880Rib · crackedRH WING CENTER FLAP RIB UPR FLANGE FOUND 5EA CRACKS AT RIB25, RIB26, RIB27 BETWEEN REAR SPAR AND STGR2.7 COMPLIED WITH EA: 6-5750-T0379692 P1 REPAIRED THE RH WING CENTER FLAP CRACKED RIB UPR FLANGE AT RIB25, RIB26, RIB27 BETWEEN STGR2.7 AND REAR SPAR. TITLSDR SWAA2024080907324Skin · debondedCUSTOMER REQUEST - DEBONDED OB AFT FLAP IB SIDE AT RT WING 2024-414774<[01] STEP 4. TOOL USED ULTRASONIC EQUIPMENT PN: EPOCH 650 ; SN: 190859705; DUE DATE: 23-OCT-24.;[02] TOOL USED; HOTBONDER PN: HCS9200B-AV; SN: 18185733; DUE DATE: 25/JAN/25.;[03] TOOL USED;SDR SWAA2024080907325Skin · debondedCUSTOMER REQUEST - DEBONDED OB AFT FLAP IB SIDE AT LT WING 2024-414775<[01] STEP 5. TOOL USED ULTRASONIC EQUIPMENT PN: EPOCH 650 ; SN: 190859705; DUE DATE: 23-OCT-24.;[02] TOOL USED; HOTBONDER PN: HCS9200B-AV; SN: 18185733; DUE DATE: 25/JAN/25.;[03] TOOL USED;SDR DALA2024070106639Strap · tornSHIP 3161 TORN STRAP LOC INTERNAL AREA FLAP TRACK 4 FAIRING (533CB) AT LH WING. CORRECTIVE ACTION: REPAIRED PER ER/A 618700-14. (0418877)SDR SWAA2024070206464Skin · delaminatedRIGHT WING O/B TRAILING EDGE FLAP TRAILING EDGE SPLIT APPROXIMATELY 4.5' LONG FOUR INCHES FROM THE I/B END. ALSO DELAMINATION ON LOWER SURFACE ONLY MEASURING 13.5' LONG AND 9' WIDE. NO MOISTURE NOTED<[01] REMOVED AND REPLACED RIGHT WING OTBD AFT FLAP PER AMM 2SDR SWAA2024070206462Skin · delaminatedLEFT WING INBOARD TRAILING EDGE FLAP WEDGE PANEL HAS TWO DELAMS ON LOWER SURFACE. LOCATION ONE IS 16 FROM OUTBOARD EDGE AND MEASURES 11 X 4 LOCATION TWO IS 2.5 FROM OUTBOARD EDGE AND MEASURES 10 X 8<[01] C/W EA 24-127-01768 ON LH INBOARD TRAILING EDGE FLAP WEDSDR DALA2024070106640Bonding Plate · corrodedSHIP 3132 CORROSION BONDING PLATE FLAP TRACK FAIRING TIP 633CB ON RH WING. CORRECTIVE ACTION: REPAIRED PER ER/A 618279-14. (0418064)SDR SWAA2024071906504Skin · delaminatedRIGHT WING INBOARD MAIN FLAP TRAILING EDGE WEDGE LOWER SKIN IS DELAMINATED ON TRAILING EDGE.<[01] REMOVED AND REPLACED RIGHT WING INBOARD MAIN FLAP TRAILING EDGE WEDGE PER AMM 20-50-11;[02] VERIFIED REMOVED AND REPLACED RIGHT WING INBOARD MAIN FLAP TRAILING EDSDR SWAA2024070106021Flap Track · excess playL/H WING I/B FLAP O/B AFT FLAP TRACK HAS EXCESSIVE PLAY<[01] 01 - REMOVED AND REPLACED INBD AFT FLAP OUTBD TRACK PER [AMM 27-51-16-401-NG (INBOARD AFT FLAP TRACKS - REMOVAL/INSTALLATION - PERMANENT)]SDR DALA2024070106635Flap Track · corrodedSHIP 3132 CORROSION FOUND IN TRACK 2 BEARING HOUSING AT RIB 9 LEVEL ON INB'D FLAP. CORRECTIVE ACTION: REPAIRED PER ER/A 618466-14. (0416133)SDR SWAA2024080505403Fairing · damagedELONGATED HOLE ACCESS PANEL 642EB FLAP SUPPORT FAIRING 6 EXTERNAL SKIN AT RT WING 2024-401992<[01] TOOL USED CALIPER P/N 500-97-30 S/N A18229508 DUE DATE 14 JAN 25;[02] REPLACED ACCESS PANEL 642EB FLAP SUPPORT FAIRING 6 EXTERNAL SKIN AT RT WING IAW B737-800 AMSDR SWAA2024070305395Skin · delaminatedRIGHT OUTBOARD AFT FLAP HAS DELAMINATION ON INBOARD UPPER SKIN AT LOWER CORNER(MARKED).<[01] REMOVED R/H O/B AFT FLAP PER MM 27-51-22.;[02] OK TO INSTALL R/H OUTBOARD AFTFLAP.;[03] REPLACED R/H OUTBOARD AFT FLAP PER MM 27-51-22.;[04] VERIFIED REPLACED R/H OUTBSDR DALA2024062506458Skin · corrodedSHIP 3140 CORROSION OTBD FLAP LOWER SURFACE AT LEVEL TRACK 4 ON RH WING. CORRECTIVE ACTION: REMOVED AND REPLACED EXTERNAL DOUBLER AND FASTENERS LOC OB FLAP LOWER SURFACE AT LEVEL TRACK 4 ON RH WING AS PER A319 SRM 57-53-21-300-003. (0410811)SDR UIEA2024061800535Fairing · delaminatedLHW O/B MID FLAP L/E FAIRING FOUND DELAMINATION(<P>PERFORMED PERMANENT REPAIR AS PER SRM 51-70-07 PAR 5A. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024061800536Fairing · delaminatedLHW O/B MID FLAP L/E FAIRING FOUND DELAMINATION(<P>PERFORMED PERMANENT REPAIR AS PER SRM 51-70-07 PAR 5A. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024061800538Fairing · delaminatedRHW O/B MID FLAP L/E FAIRING FOUND DELAMINATION(<P><SPAN>PERFORMED PERMANENT REPAIR AS PER SRM 51-70-07 PAR 5A. NO FURTHER DEFECTS NOTED.</SPAN></P>)SDR UIEA2024061900556Skin · chafedLHW O/B AFT FLAP UPPER SURFACE O/B AREA FOUND SEVERAL CHAFING MARKS(<P>PERMANENT METAL TO METAL HOTBOND REPAIR AS PER RI NO. RI-57-51-16950 REV.A. NO FURTHER DEFECTS NOTED</P>)SDR SWAA2024080504866Skin · delaminatedL/W OUB AFT FLAP INB END LOWER SURFACE DELAMINATION AROUND PREVIOUS REPAIR MKD DOT<[01] REMOVE AND REPLACED L/W OUB AFT FLAP AS PER AMM 27-51-22-000-801 AND 27-51-22-400-801.;[02] VERIFIED STEP 1SDR SWAA2024080505006Panel · elongatedL/W REAR SPAR LOWER FIXED T/E PANEL 551GB INB AFT SUPPORT ROD LOWER ATTACHED FITTING ELONGATED HOLE MKD DOT<[01] REMOVED AND REPLACED L/W REAR LSPAR LOWER FIXED T/E PANEL# 551GB AFT SUPPORT ROD PER REF SRM 51-40-02-0G-0;[02] VERIFIED STEP:1SDR VNAA202406230010Cradle · corrodedRH I/B FLAP VANE ACTUATOR SYSTEM CRADLE ASSEMBLY AT WS 24.00 IS CORRODEDSDR IPXA20240701367Skin · dentedDENT -SKIN, LH WING OUTBD AFT FLAP OUTBD LOWER SIDE. (REPAIR) PERFORMED NDT/UT REWORKED AREA AND PLUS 8" AROUND HEATED AREA, I.A.W. 747 NDT MANUAL PART 1 51-01-01 AND 747 NDT MANUAL PART 1 51-04-00 REV.176 , RESULT: NO DEFECT FOUND. OPENSDR LR7A2024062003419Skin · pulledDURING SCHEDULED A1 INSPECTION FOUND MULTIPLE RIVETS PULLED THROUGH THE SKIN ON UPPER FLAP SURFACE AROUND RH OUTBOARD FLAP TRACK CARRIAGE / REPAIRED IAW ERO 5750ERO3697 MEA 382-57-24-126SDR AALA202406240192Strut · out of rigAIRCRAFT WAS GROUNDED: DURING FINAL APPROACH INTO LAS WHILE SELECTING FLAPS 2 THE FLIGHT CREW REPORTED A FLAPS LOCKED ALIGNMENT FAULT ECAM MESSAGE AND ABORTED THE APPROACH. THE FLIGHT CREW ACCOMPLISHED THE ECAM PROCEDURES AND LANDED AT LAS WITHOUT FURTHER INCISDR DALA2024062406340Hinge Fitting · damagedELONGATED HOLE AND DAMAGED BOLT WAS FOUND AT RH FLAP HINGE #3. SUMMARY OF NRC 00776: ELONGATED HOLE AND DAMAGED BOLT AT RH FLAP HINGE #3 WAS REPAIRED PER PRI 617866-14 REV 1 & ER/A PRI 617866-14 REV ORIG. DTE REPAIR APPROVAL IS LIMITED TO 24 MONTHS FROM MAY 18SDR VNAA202407110019Doubler · wornIN REF TO JOBCARD 275000·218_R/H.JIC: WEAR ON FLAP VANE ACTUATOR #3 AREA (INNER SKIN) WEAR ON FLAP VANE ACTUATOR #3 AREA (INNER SKIN) WAS REPAIRED PER REO 670-57-52-352 REV --SDR AALA202406242535Trunnion · wornAIRCRAFT WAS GROUNDED: RIGHT WING INBOARD FLAP DRIVE STRUT TRUNNION WORN BEYOND LIMITS PER TASK CARD 26T60057066. MAINTENANCE REPLACED RIGHT WING INBOARD FLAP TRUNNION PER TASK CARD 26L00027003.SDR SWAA2024062103668Fastener · missingLEFT WING #3 FLAP CANOE FAIRING TAIL CONE HAS MISSING FASTENERS AND SEVERAL FASTENERS PULLED COMPLETELY THROUGH COMPOSITE.<[01] 01 - REMOVED AND REPLACED PER [AMM 27-51-18-400-802-NG (INBOARD FLAP SUPPORT AFT FAIRING INSTALLATION - PERMANENT)]SDR SWAA2024072503183Seal · deterioratedINBOARD FLAP UPPER SKIN RIGHT WING PANEL 653ET SEAL DETERIORATED.<[01] REMOVED AND REPLACED SEAL AT R/W INBOARD FLAP UPPER SKIN RIGHT WING PANEL 653ET PER REF SRM 51-40-02-0G-0;[02] VERIFIED CORRECTIVE ACTION STEP 1SDR SWAA2024071803195Fairing · crackedFLAP TRACK # 8 FAIRING 644BB CRACKED AT INTERNAL SKIN AFT MKD DOT<[01] PREPARED FOR REPAIR ON FLAP TRACK # 8 FAIRING 644BB; AS PER SRM 51-70-04-2R-1;INSTALLED REPAIR ON FLAP TRACK # 8 FAIRING 644BB; AS PER SRM 51-70-04-2R-1- MATERIAL USED PO.2061896 AND PO.173SDR SWAA2024071803193Fairing · delaminatedFLAP TRACK # 2 FWD FAIRING 543AB HAS SOLID DELAMINATION @ EXTERIOR SKIN FASTENERS HOLES MKD DOT<[01] SUMMARY :PERFORMED PULSE-ECHO UT INSP FOR DELAMINATION.<BR>IAW B737 NDT PART 4; 51-00-01 & PART 1; 51-01-02.<BR>TOOL: EPOCH 600; B/C 19498 CAL. DUE: 03-25-2025SDR IPXA2024070906325Stiffener · brokenSTR FOUND STIFFENER BROKEN AT L/H SIDE WING I/B FLAP I/B STOP PAD WING STRUCTURE ATA 57-21. VERIFIED REPAIR IS ACCOMPLISHED EO-90826-REQ1, VT-SAA EA 011-5740-01-B0225, REV. I/R.SDR SWIA202408230617Skin · damagedR/H INBD FLAP HAS GOUGE DAMAGE ON LOWER SKIN AT WS54. FWD OF TRAILING EDGE (C-CHECK RO 8/22/2024) REMOVED AND REPLACED R/H I/B FLAP LOWER SKIN, PERFORMED SKIN REPAIR SPLICE IAW CRJ700 SRM 57-52-01, 51-26-01, 51-42-10, 51-40-11, 51-21-11, 51-25-06, 51-25SDR SWAA2024072402665Panel · pulledR/W T/E PANEL 661BB HAS SEVERAL PULLED FASTENER HOLES ON AFT END (MARKED)<[01] R/W T/E PANEL 661BB PULLED FASTENER HOLES REPAIRED IAW SRM 51-70-04-2R-9;[02] JOB COMPLETE.SDR SWAA2024072402666Panel · pulledR/W T/E PANEL 661CB HAS SEVERAL PULLED FASTENER HOLES ON AFT END (MARKED)<[01] R/W T/E PANEL 661CB PULLED FASTENER HOLES REPAIRED IAW SRM 51-70-04-2R-9;[02] JOB COMPLETE.SDR FDEA202406150981Rib · cracked1. 1EA CRACK (15MM) WAS FOUND AT R/H WING CENTER FLAP RIB25 AFT AREA OF TOP SURFACE RIB FLANGE. 2. 2EA CRACKS (5MM & 20MM) WERE FOUND AT R/H WING CENTER FLAP RIB26 AFT AREA OF TOP SURFACE RIB FLANGE. 3. 1EA CRACK (50MM) WAS FOUND AT R/H WING CENTER FLAP SDR SWAA2024070306116Skin · delaminatedRIGHT WING OUTBOARD AFT. FLAP IS DELAMINATED ON LOWER INBOARD END.<[01] REMOVED R/H O/B AFT FLAP PER AMM 27-51-22.;[02] INSTALLED RIGHT WING OUTBOARD AFT FLAP PER AMM 27-51-22;[03] C/W INSPECTION.;[04] CHANGED MEASUREMENTS TO RII;[05] VERIFIED INFO IN C/A #4SDR DALA2024061906221Strut · excess playSHIP 3161 EXCESSIVE PLAY IB FLAP ON NTERCONNECTING STRUCT ON LH WING. CORRECTIVE ACTION: REPLACED INTERCONNECTING STRUT PER A319 FAM AMM 27-51-44- 000-001-A. (0395522)SDR DALA2024061706135Strut · corrodedSHIP 3138 CORROSION INTERCONNECTING STRUT IB FLAP ON LH WING. CORRECTIVE ACTION: REPLACED INTERCONNECTING STRUT IB FLAP ON LH WING PER A319 FAM AMM 27-51-44-000-001-A. (0394447)SDR DALA2024061706134Strut · corrodedSHIP 3138 CORROSION INTERCONNECTING STRUT IB FLAP ON RH WING. CORRECTIVE ACTION: REPLACED INTERCONNECTING STRUT IB FLAP ON RH WING PER A319 FAM AMM 27-51-44-000-001-A. (0394440)SDR FDEA202406140982Rib · cracked1.1EA CRACK (5MM) WAS FOUND AT L/H WING CENTER FLAP RIB11 AFT AREA OF TOP SURFACE RIB FLANGE. 2.1EA CRACK (5MM) WAS FOUND AT L/H WING CENTER FLAP RIB12 AFT AREA OF TOP SURFACE RIB FLANGE. 3.1EA CRACK (25MM) WAS FOUND AT L/H WING CENTER FLAP RIB19 AFT ARE
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