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 DALA2022072905237Flap · delaminatedSHIP 661 DELAMINATED FLAP INBOARD TRAILING EDGE BEHIND FLAP TRACK # 6 AT RH WING. CORRECTIVE ACTION: SUMMARY ON REF NRC 00407 FLAP INBOARD TRAILING EDGE BEHIND FLAP TRACK # 6 AT RH WING WAS REPAIRED PER B757-200 S.R.M. (2338907)SDR SWAA2022090635278Angle · crackedCRACK TRAILING EDGE SUPPER ANGLE LOCATED WS275 AT RT WING 2022-410103 / [01] TRAILING EDGE SUPPER ANGLE LOCATED WS275 AT RT WING IAW SRM 737-700 51-40-02 AND DWG 115A6299 REV -. SEE INDIVIDUAL SIGN OF BELLOW.;[02] TASK CARD COMPLETED <BR>SEE INDIVIDUAL SIGN OFSDR SWAA2022090635283Support Bracket · crackedCRACK SUPPORT BRACKET TRAILING EDGE LOCATED WS253 RT WING 2022410108 / [01] REPLACED SUPPORT BRACKET TRAILING EDGE LOCATED WS253 RT WING IAW B737-700 SRM 51-40-05 AND DRAWING# 115A2930 REV. - REPLACED BRACKET DUE TO NOT FOUND ALLOWABLE DAMAGE ON B737-700 SRM 5SDR SWAA2022090635282None · crackedCRACK REAR SPAR CORRUGATED PLATE LOCATE BETWEEN WS204 TO WS228 AT RT WING 2022-410120 / [01] REPLACED REAR SPAR CORRUGATED PLATE LOCATE BETWEEN WS204 TO WS228 AT RT WING I.A.W. B737-700 SRM 51-40-02 AND DRAWING # 115A2001 REV ?A?;[02] TASK COMPLETEDSDR SWAA2022082333626Web · crackedRT WING T/E SEAL WEB TO DEFLECTION CONTROL RIB IS CRACKED / [01] FOUND NO APPLICABLE SRM REPAIR FOR CRACKED RT WING T/E SEAL WEB TO DEFLECTION CONTROL RIB ANGLE; THEREFORE REPAIRED BY REPLACEMENT PER SRM 51-10-02-0G-0 PARAGRAPH 9. REMOVED AND REPLACED CRACKED SDR 2022FA0000398Skin · gougedR/H INBOARD FLAP HAS A GOUGE ON THE UPPER SURFACE APPROXIMATELY 14" FROM OUTBOARD EDGE AND 1" FROM TRAILING EDGE, MEASURING .5" IN LENGTH AND .03 IN WIDTH, FROM A TOOL FALLING ON THE FLAP.SDR SWAA2022090633771Bracket · crackedCRACK ON BRACKET LOCATED IRSS140 AT RT WING 2022-410000 / [01] REPLACED BRACKET LOCATED IRSS140 AT RT WING IAW B737-700 SRM 51-40-02 AND 51-10-02.<BR>TOOL USED CALIPER DIGITAL P/N:50P-197-30 S/N:A21147765 DUE DATE:15-OCT22;[02] TASK CARD COMPLETEDSDR SWAA2022090633780Bracket · crackedCRACK ON SUPPORT BRACKET LOCATED ORSS 297 AT LT WING 2022-410008 / [01] REMOVED AND REPLACED SUPPORT BRACKET LOCATED ORSS 297 AT LT WING AND FASTENERS IAW B737-700 SRM 51-10-02 AND DRAWING 115A3700 SHEET 31 REV -;[02] TASK CARD COMPLETEDSDR SWAA2022081933747Fitting · crackedR/W RAR SPAR T/E DEFLECTION CONTROL RIB PANEL VERTICAL BULB SEAL FITTING CRACKED @ FASTENER TAIL INB. MKD DOT / [01] REMOVEDND REPLACED BULB SEAL FITTING AT R/W REAR SPART T/E DEFLECTION CONTROL RIB PANEL VERTICAL. REF. SRM. 51-40-02-0G-0-A00279.;[02] CORRECTISDR SWAA2022081935746Fitting · damagedR/W REAR SPAR FIXED T/E LOWER STIFFENER FITTING LOWER SURFACE DRILLED HOLE @ ORSS 261 MKD DOT / [01] MEASURED DAMAGED HOLE AT RT WING REAR SPAR FIXED T/E LOWER STIFFNER ATREA ORSS 261 AS PER B737-7 SRM 57-20-90-1A-2;DEPTH = .044' WITDTH = .210';CALIPER B/C 159SDR SWAA2022081933746Fitting · crackedR/W REAR SPAR LOWER T/E WIGGLE FITTING CRACKED ;SHEARED FASTENERS O/B FLAP TRACK NO-6 / [01] REMOVED AND REPLACED WIGGLE PLATE AT L\H WING T/E O/B OF FLAP TRACK #6 AS PER B737-7 SRM 51-40-02-0G-0;[02] VERIFIED STEP 1SDR SWAA2022081933748Support Angle · crackedL/W REAR SPAR T/E LOWER SUPPORT ANGLE CRACKED @ INB END BELOW SPOILER NO-5 MKD DOT / [01] REMOVED SUPPORT ANGLE AT LW REAR SPAR T/E FOR CRACK SRM 51-40-02-0G-0;[02] RECEIVED NEW ANGLE PP#115A3758-9 LOCATED NEW ANGLE AND DRILLED NEW HOLES SRM 51-40-05-0G-0;[03]SDR SWAA2022081933751Plate · crackedL/W REAR SPAR FIXED T/E LOWER WIGGLE FITTING SHEARED FASTENERS POSSIBLE CRACKED O/B OF FLAP TRACK NO-3 MKD DOT / [01] REMOVED AND REPLACED WIGGLE PLATE AT L/W REAR SPAR O/B OF OF FLAP TRACK #3 AS PER B737-7 SRM 51-40-02-0G-0;[02] VERIFIED STEP 1SDR FDEA202207251794Flap · delaminatedLH WING OB FLAP LWR SURFACE FOUND DELAMINATION AT OTEF STA424 LH WING OB FLAP LWR SURFACE AT OTEF STA424 REPAIRED AS PER B777F SRM 57-53-01-2R REPAIR 2 AND SRM 51-70-04-2R REPAIR1 REV 41.0. B777F SRM 57-53-01-2R REPAIR 2 AND SRM 51-70-04-2R REPAIR1 REV 41SDR SWAA2022080233379Flap · delaminatedRIGHT WING OUTBOARD LOWER FLAP I/B EDGE HAS DELAMINATION / [01] REMOVE SEAL INB EDGE FOR ACCESS TO REPAIR IRW SRM-51-40-02;[02] PERFORMED VISUAL INSPECTION AND TAP TEST INSPECTION AT RIGHT WING O/B FLAP LOWER AND UPPER SKIN I/B EDGE DELAMINATION FOUND. REF B73SDR SWAA2022072733306Flap · delaminatedRH OB AFT FLAP PREVIOUS REPAIR DELAM- REQUIRES R/R / [01] REMOVED AND REPLACED THE RH OB AFT FLAP PER AMM 27-51-21.;[02] C/W RIISDR SWAA2022080232795Flap · debondedLH O/B AFT FLAP LOWER SKIN AT I/B CORNER HAS AN AREA OF DISBOND. / [01] BOND TEST IAW B737 NDT PART 4; 51-00-05. DISBONDED AREA MARKED IN BLACK. TOOL#40082; DUE 11OCT22;[02] EVALUATED AND FOUND DISBOND AS MARKED. FOUND TO BE REPAIRABLE IAW SRM 57-53-01-2R-4 STSDR SWAA2022072733124Flap · peelingMETAL PEELING UP ON RIGHT OUTBOARD AFT FLAP. / [01] INSPECTED AREA OF DAMAGE ON RH O/B AFT FLAP INBOARD END. DAMAGE MEASURED 8? BY 12?. C/W EA 22-157-02190. REINSPECT EACH CYCLE; PERMANENT REPAIR REQUIRED WITHIN 5 CYCLES.SDR SWAA2022090732782None · debondedCUSTOMER REQUEST - DEBONDED EXISTING REPAIR INBOARD CORNER ON OB AFT FLAP AT RT WING. 2022-409841 / [01] TOOL USED CALIPER P/N: 500-197-30 S/N: 15120589 DUE DATE: 28-NOV-22.;[02] TOOL USED: ULTRASONIC FLAW DETECTOR P/N:EPOCH 600 S/N: 120357005 DUE DATE: 07-JANSDR SWAA2022090632777Angle · crackedCRACK OUTBOARD TRAILING EDGE LOC ORSS 272 AT LT WING 2022-409831 / [01] REPLACED ANGLE LOC. OUTBOARD TRAILING EDGE ORSS 272 AT LT WING A.W SRM B737-700 51-40-02 AND DRAWING #115A2930 REV. - DUE TO NOT FOUND ALLOWABLE DAMAGE B737-700 SRM 57-51-02. TOOK MEASURESSDR SWAA2022090632776Angle · crackedCRACK OUTBOARD TRAILING EDGE ANGLE LOC ORSS 282 AT LT WING 2022-409826 / [01] REPLACED ANGLE LOC. OUTBOARD TRAILING EDGE ANGLE; ORSS 282 AT LT WING IAW B737-700 SRM-51-10-02 ITEM 9 AND DWG-115A6200 REV:- SEE INDIVIDUAL SIGN-OFF BELOW;[02] REPLACED ANGLE LOC. OSDR SWAA2022082331357Web · crackedCRACK ON R/H SEAL WEB TO DEFLECTION CONTROL RIB O/B BRACKET ATTACH ANGLE.(MARKED) / [01] FOUND NO APPLICABLE SRM REPAIR FOR CRACKED RT WING T/E SEAL WEB TO DEFLECTION CONTROL RIB ATTACH ANGLE; THEREFORE REPAIRED BY REPLACEMENT PER SRM 51-10-02-0G-0 PARAGRAPH 9SDR SWAA2022082331361Support Angle · crackedLEFT WING UPPER T/E PANEL SEAL SUPPORT ANGLE IS CRACKED AT RSS 270 / [01] FOUND NO APPLICABLE SRM REPAIR FOR CRACKED LT WING T/E UPPER PANEL SEAL SUPPORT ANGLE AT RSS 270; THEREFORE REPAIRED BY REPLACEMENT PER SRM 51-10-02-0G-0 PARAGRAPH 9. REMOVED AND REPLACESDR DALA2022072205078None · none(LOG 2328601) DURING INSPECTION FOUND WEAR AT AFT BRACKET OF FAIRING FLAP SUPPORT #6 RH WING. AFT BRACKET OF FAIRING FLAP SUPPORT #6 RH WING WAS REPAIRED PER ER/A 600872-14 REV. ORIGINAL & PRI 600872-14 REV. 0.SDR CALA2022072001839None · missingPDA 3 RIGHT WING MAIN INBD T/EDGE FLAP COMPLETELY MISSING SEAL AT OUTBD END LOWER POSITION -- SEE PHOTO PHOTO ADDED INSTALLED NEW SEAL AT OUTBD END LOWER POSITION OF INBOARD MAIN FLAP ON RIGHT WING. REF IPC 27-51-11-01.SDR IXXA20220804001Flap · crackedDENT ON LH IND FLAP 59.5 FROM INBD EDGE AND 44.5 FORM TRAILING EDGE. VT-SAA NR B000038SDR KCSA202207191092Skin · corrodedR/H WING I/B AFT FLAP HAS CORROSION ON BOTTOM SIDE OF FLAP SKIN APPROX. 78 INCHES FROM O/B EDGESDR SWAA2022081929973Bracket · crackedCRACK TRAILING EDGE SUPPORT BRACKET LOCATED ORSS273 AT RT WING 2022-365711 / [01] REPLACED SUPPORT BRACKET LOCATED TRAILING EDGE ORSS 273 AT RT WING IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 PART NUMBER USED: 115A2982-10 P.O: 2022 148172;[02] REPLACED SDR SWAA2022081929974Bracket · crackedCRACK TRAILING EDGE BRACKET LOCATED IRSS140 AT RT WING 2022-365714 / [01] REPLACED TRAILING EDGE BRACKET LOCATED IRSS140 AT RT WING I.A.W B737-700 SRM 51-40-02 AND B737-700 SRM 51-10-02 ITEM:9;[02] REPLACED TRAILING EDGE BRACKET LOCATED IRSS140 AT RT WING I.A.SDR CALA2022071801784Flap · gougedB757-06-3-0319: LEFT WING OUTBOARD MAIN FLAP, OUTBOARD LEADING EDGE GOUGED. TRANSCRIBED FROM HAECO GSO NRC# 9280692 REPAIRED LEFT WING O/B MAIN FLAP O/B L/E SKIN PER B757-200 SRM 5 7-53-01-2R-3. THE INSTALLED BLIND RIVETS REQUIRE INSPECTION EVER Y 2500 FLIGHSDR KCSA202207151091Skin · corrodedL/H I/B MIDFLAP HAS AREA OF CORROSION ON UPPER SKIN AFT PANEL SURFACE ABOVE FLAP REAR SPARSDR DALA2022071504891None · noneSHIP 3229 CORROSION CARRIAGE IB FLAP FLAP TRACK 1 BEARING OF PENDULUM ASSY ON RH WING. CORRECTIVE ACTION: REPLACED CARRIAGE IB FLAP FLAP TRACK 1 BEARING PER A320 CMM 27-54-43. (2320267)SDR DALA202208305325Vane · unknownPD: SUMMARY: DENT/DISBOND (SDR) OTHER WARN ITEMS AND DELAMINATED RUBSTRIP. / CA: REPAIRED UNIT. THE WORK SPECIFIED IN BLOCK(S) 11/12 ACCOMPLISHED WITH REFERENCE TO OEM CMM 27-50-1, REV. 61 WITH APPLICABLE DELTA SUPPLEMENTAL INFORMATION AND CSVE, REV. 30.SDR IPXA2022072584513Beam · crackedINSPECTION TYPE:3CL/H O/B FLAP I/B HIMGE AFT FAIRING SUPPORT BEAM IS CRACKED.REMOVED, FABRICATED AND REPLACED BEAM IAW DWG. ARC2149 AND SRM 51-33-01 AND 51-31-01. (MINOR)SDR LR7A2022071303190Skin · crackedDURING SCHEDULED B-2 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND LH INBOARD FLAP LOWER SKIN IS CRACKED AT CWS208L 24" AFT OF LEADING EDGE. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-12. NR# 1000786042SDR LR7A2022071303189Skin · crackedDURING SCHEDULED B-2 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND RH OUTBOARD FLAP CRACKED AT OWFS17R UPPER SKIN 17" FORWARD OF TRAILING EDGE. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-12. NR# 1000786023SDR CALA2022071301715Flap · gougedB757-06-3-0322 LEFT WING, INBOARD MAIN FLAP, LEADING EDGE GOUGED . TRANSCRIBED FROM HAECO GSO NR 9280709SDR SWAA2022071427581Flap · delaminatedDURING WAC FOUND DAMAGE ON INBOARD OF R/H OUTBOARD TRAILING EDGE FLAPS LOWER SKIN DELAMINATION AREA = L: 22.000' W: 10.000' FROM THE LOWER I/B CORNER.MISSING MATERIAL = L: 3.500' W: 2.000' FROM THE LOWER I/B CORNER. SEE ATTACHED IMAGES. / [01] MEASUREMENTS ADDSDR SWAA2022071427473Doubler · delaminatedLH OB AFT FLAP PREVIOUS REPAIR DELAMINATED / [01] REMOVED PREVIOUS REPAIR; PREPPED AREA AND INSTALLED NEW CORE AND REPAIR DOUBLER IAW SRM 51-70-10.SDR SWAA2022071126631Flap · delaminatedLEFT WING OUTBOARD AFT FLAP HAS SEVERAL SPOTS OF DELAMINATION ON THE UNDER AND UPPER SIDE OF THE INBOARD 15 INCHES. (MARKED) / [01] REPAIRED AFT FLAP PER SRM 51-70-05.SDR DALA2022070804761None · noneSHIP 3217 CORROSION INTERCONNECTING STRUT OB FLAP ON LH WING. CORRECTIVE ACTION: CLEAN AND REINSTALLED INTERCONNECTING STRUT ON FLAP ON LH WING. OK FOR SERVICE. (2310711)SDR SWAA2022072926239Flap · delaminatedR/H WING OUTBOARD AFT FLAP DELAMINATED AT INBOARD LOWER SURFACE / [01] RII: OK TO INSTALL OUTBOARD AFT FLAP.;[02] ADDED PARTS INFO;[03] REMOVED & REPLACED AFT FLAP PER AMM 27-51-22.;[04] C/W INSPECTION.SDR AALA202207251080Web · crackedAIRCRAFT IN BASE MAINTENANCE: LEFT WING FLAP FAIRING 577EB INNER AFT WEB CRACKED AT INBOARD AFT END. RG-66. REMOVED AND REPLACED BRACE FROM LEFT WING FLAP FAIRING 577EB INNER AFT AT INBOARD AFT END PER B777-200 SRM 51-40-02-0G.SDR DALA2022070704740None · noneSHIP 664, CORROSION ON LH AFT UNIVERSAL JOINT ASSY OF INBOARD BALLSCREW FROM INBOARD TRAILING EDGE FLAP LH WING WAS FOUND DURING INSPECTION OF COMPONENTS ON CARD. CORRECTIVE ACTION: SUMMARY OF NRC #00596: LH AFT UNIVERSAL JOINT ASSY OF INBOARD BALLSCREW FROM ISDR SWAA2022072224840Angle · crackedCRACK ANGLE TRAILING EDGE LOCATED FALSE SPAR ORSS 280 AT RT WING 2022-384734 / [01] REPLACED ANGLE AND FASTENER ON TRAILING EDGE LOCATED FALSE SPAR ORSS 280 AT RT WING IAW B737-700 SRM 51-40-02 AND DRAWING 115A6200 REV A: SEE INDIVIDUAL STEP SINGOFFS BELOW;[02SDR SWAA2022072224839Web · crackedCRACK WEB TRAILING EDGE LOCATED ON FALSE SPAR ORSS 261 AND ORSS 280 AT RT WING 2022-384733 / [01] REPLACED WEB AND FASTENERS LOC TRAILING EDGE LOCATED ON FALSE SPAR ORSS 261 AND ORSS 280 AT RT WING IAW B737-700 SRM 51-40-02.;[02] CORRECTED STEP 1. REPLACED WEBSDR SWAA2022072224838Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 261 AT LT WING 2022-384731 / [01] REPLACED CORRUGATED PLATE AND FASTENER LOCATED ON TRAILING EDGE ORSS 261 AT LT WING IAW B737-700 SRN 51-40-02 AND DRAWING 114A2714 REV A:;[02] REPLACED CORRUGATED PLATE AND FASSDR UIEA2022062300647Flap · dentedRHW T/E I/B MID FLAP L/E FOUND DENT(PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR.5A)SDR UIEA2022062300648Flap · delaminatedRHW T/E I/B AFT FLAP T/E LOWER SURFACE FOUND DELAMINATION(PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR.5A)SDR 2022FA0000324None · noneTHIS REPORT IS FILED ON BEHALF OF JET AVIATION AG BASEL, APPROVAL NUMBER NO. QV1Y440K.
ON JUNE 28TH 2022, THE AIRCRAFT FALCON 2000 EASY S/N 034 REGISTRATION N234FJ WAS INDUCTED AT JET AVIATION AG BASEL UNDER PROJECT NO. B24FJ001.
FOLLOWING PERFORMANCE OF THE
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