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 SWAA2023040512590Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE LOCATED ORSS241 AT LT WING 2023-143018<[01] REPLACED CORRUGATED PLATE LOCATED ON ORSS 241 AT LT WING IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 115A2001 SHEET 30 AND REV A.;[02] CORRECTED STEP 1.<BR>REPLACED CORRUGATED PLATE SDR IPXA2023032592240Bracket · crackedINSPECTION TYPE:CL/H WING CENTER FLAP O/B EDGE HAS BROKEN BRACKETREMOVED AND REPLACED IAW SRM 51-40-21SDR SWAA2023032412557Angle · crackedCRACK ANGLE TRAILING EDGE LOCATED ORSS 287 LOWER SIDE RT WING 2023-165217<[01] REPLACED ANGLE AND FASTENERS LOCATED ORSS 287 LOWER SIDE RT WING IAW B737-700 SRM 51-40-02 AND DWG 115A3700 SHEET 27 REV - ; SEE INDIVIDUAL SING-OFF BELOW.;[02] CORRECTED STEP 1<BR>SDR SWAA2023032412548Angle · crackedCRACK SUPPORT ANGLE LOCATED DEFLECTION CONTROL AT LT WING 2023-165209<[01] REPLACED NEW SUPPORT ANGLE LOCATED DEFLECTION CONTROL AT LT WING I.A.W. B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9. SEE INDIVIDUAL SIGN OF BELOW.;[02] TASK COMPLETED <BR>SEE INDIVIDUSDR SWAA2023030711810Panel · crackedR/H WING TE SHELF PANEL 651FB WEDGE FAIRING CRACKED/DAMAGED.<[01] ADJUSTED R/H WING TE SHELF PANEL 651FB PER AMM 27-51-11.;[02] PERFORMED R/H MAIN LANDING GEAR WHEEL WELL STRUT DOOR ADJUSTMENT PER AMM 32-13-11. NO DEFECTS NOTED.;[03] ADJUSTED R/H WING TE SHELFSDR SWAA2023032011905Intercostal · crackedINTERCOSTAL AT UPPER TRAILING EDGE PANEL INBOARD OF L/H WING DEFLECTION RIB IS CRACKED.<[01] REMOVED INTERCOSTAL AT UPPER TRAILING EDGE PANEL INBOARD OF L/H WING DEFLECTION RIB PER SRM 51-40-02;[02] INSTALLED NEW INTERCOSTAL AT UPPER TRAILING EDGE PANEL I/B OFSDR SWAA2023030610810Angle · crackedLEFT WING TRAILING EDGE TOP FIXED PANEL SUPPORT ANGLE CRACKED AT O/B FASTENER HOLE<[01] REMOVED AND REPLACED SUPPORT ANGLE REF SRM 51-40-02.SDR AALA202303064743Tab · debondedAIRCRAFT WAS GROUNDED: LEFT WING OUTBOARD TRAILING EDGE FLAP TAB LOWER SURFACE PREVIOUS METAL REPAIR DEBONDED. MAINTENANCE REPLACED THE FLAP TAB PER AMM 27-54-62.SDR SWAA2023040410696Flap · debondedLEFT WING O/B AFT FLAP I/B END; UPPER AND LOWER SURFACE IS DISBONDED<[01] REMOVED LEFT WING O/B AFT FLAP IAW AMM 27-51-22-000-801.;[02] UPDATED PARTS INFO;[03] UPDATED PARTS;[04] OK TO INSTALL L/H O/B AFT FLAP;[05] OK TO INSTALL L/H O/B AFT FLAP;[06] RECEIVED SDR SWAA2023032010591Fitting · crackedL/W REAR SPAR FIXED T/E PANEL 551GB FWD WIGGLE FITTING CRACKED AND SHEARED FASTENERS @ ORSS 261 MKD DOT<[01] REMOVED AND REPLACED WIGGLE PLATE AT LH WING REAR SPAR FIXED T/E (PANEL 551GB) REF: SRM 51-40-02-0G-0.;[02] VERIFIED INSTALLATIONSDR SWAA2023032010747Fitting · elongatedL/W REAR SPAR FIXED T/E PANEL 551GB INB FWD SUPPORT LINK UPPER FITTING HOLE ELONGATED @ REAR SPAR MKD DOT<[01] REMOVED AND REPLACED SUPPORT BRACKET AT L/W REAR SPAR FIXED T/E PANEL 551GB REF B-737-700 SRM 51-40-02-0G-0;[02] VERIFIED STEP 1SDR KCSA202302271006Bracket · damagedL/H I/B AFT FLAP NO. 1 SPINDLE FWD BEARING RETAINING BRACKET BOLT HOLES DAMAGEDSDR SWAA2023030110280Flap · delaminatedR/H OTBD AFT FLAP HAS A 6 BY 6 DELAMINATION ON INBD LOWER SIDE<[01] DELAMINATED AREA IS IN ZONE 5 OF R/H OTBD TRAILING EDGE FLAP. DELAMINATION IS 6? X 6? INBD LOWER AREA. INSTALLED SPEED TAPE IAW SRM 57-53-01-1A-5-B00238. REQ TAP TEST AND GVI DAILY WITH INSP OSDR DALA2023022301376None · noneAIRCRAFT 3122, CORROSION IB FLAP ON BEARING BORE TRACK 2 ON LH WING. CORRECTIVE ACTION: REPAIRED ATTACH FITTING ON INBOARD FLAP, AT FLAP TRACK 2 LEVEL. AS PER ER/A 604916-14 REPAIRED ATTACH FITTING ON INBOARD FLAP, AT FLAP TRACK 2 LEVEL, AS PER ER/A 604916-14SDR AALA202302171429Skin · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN LOWER SKIN OF LEFT HAND FLAPERON FROM WS 520.50 TO WS 652.0 LOCATED 11 INCHES FROM LEADING EDGE SPAR AND 14 INCHES FROM INBOARD EDGE. REPAIRED SKIN PER SRM 57-65-01-2R.SDR SWAA2023032302590Angle · crackedCRACK ANGLE TRAILING EDGE LOCATED ON ORSS 272 RT WING 2023-116833<[01] REPLACED ANGLE TRAILING EDGE LOCATED ON ORSS 272 RT WING IAW B737-700 SRM 51-10-02 PARAGRAPH 9 AND B737-700 SRM 51-40-02;[02] TASK COMPLETEDSDR SWAA2023032302591Angle · crackedCRACK ANGLE TRAILING EDGE AREA LOCATED AT LEVEL ORSS261 LT WING 2023-116836<[01] REPLACED ANGLE TRAILING EDGE AREA LOCATED AT LEVEL ORSS261 LT WING IAW B737-700 SRM 51-10-02 PARAGRAPH 9; AND B737-700 SRM 51-40-02 AND DRAWING 115A6200 REV: -;[02] TASK COMPLETEDSDR DALA2023021501185Unknown · unknownCORROSION AT LWR FLAP FITTING ATTACH POINTS ON FWD INBD DRIVE FITTING ASSY RH SIDE. REMOVED HINGE FLAP FITTING NONROUTINE CARDS #09 & 01. REMOVED DAMAGE AT HOLE #12 BORE AND #13 BORE AND SPOT FACE WITHIN LIMITS PER B717 OHM 27-50-5 FIG 602. PERFORMED MPI INSPESDR CALA2023021300423Skin · missingPDA 2 FOUND DAMAGE TO RIGHT WING OUTBOARD TRAILING EDGE FLAP. ALUMINUM SKIN MEASURING APROX 22" X 12" DETACHED FROM LOWER TE FLAP. DAMAGED RH TRAILING EDGE FLAP REPLACED. PARTS USED: 29-5753-9-0010,QTY :1 1072614,QTY :1 ROTABLE PARTS CHANGE WAS INDICATED - SDR DALA2023080906496Unknown · unknownSHIP 3122 CORROSION SPOTS FOUND ON OUTB'D AND INB'D SURFACES OF LUG FITTING AT FLAP TRACK 2 LEVEL OF INB'D FLAP ON LH WING. CORRECTIVE ACTION: REPAIRED PER 604916-14. (2626293)SDR SWAA2023032302285Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE IRSS 232 RT WING 2023-116797<[01] REPLACED CORRUGATED PLATE TRAILING EDGE IRSS 232 RT WING IAW B737-700 SRM 51-10-02; 51-40-02 AND DRAWING 115A2001 REV A;[02] CORRECTED STEP 1. REPLACED PLATE ASSY LOC. TRAILING EDGE IRSS 23SDR SWAA2023032302286Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE IRSS 215 RT WING 2023-116796<[01] REPLACED CORRUGATED PLATE TRAILING EDGE IRSS 215 RT WING IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 115A2001 SHEET 29 REV-. SEE INDIVIDUAL SIGN OFFS BELOW.;[02] COMPLETEDSDR SWAA2023032302287Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE ORSS 261 RT WING 2023-116794<[01] REPLACED CORRUGATED PLATE TRAILING EDGE ORSS 261 RT WING IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9. SEE INDIVIDUAL SIGN OFFS BELOW.;[02] COMPLETE TASK CERTIFIEDSDR SWAA2023032002337Flap · debondedCUSTOMER REQUEST - DEBONDED IB MAIN FLAP WEDGE PANEL LOWER SURFACE AT RT WING 2023-127406<[01] TOOL USED CALIPER P/N 500-197-30 S/N A21147765 DUE DATE 08/NOV/23.;[02] TOOL USED BOND TESTER PN S-3 SN 064 DUE DATE 19-JUL-23;[03] TOOL USED: HOT BONDER P/N:HCS9200SDR SWAA2023030202324Support Bracket · crackedCRACK SUPPORT BRACKET TRAILING EDGE LOCATED FWD FACE SUPPORT BEAM MAIN LANDING GEAR RT WING 2023-109646<[01] TOOL USED CALIPER PN 500-196-30 SN B21141563 CAL DUE DATE 30 NOV 23 AND RADIUS GAUGE PN 2204A3 SN AE-29974 CAL DUE DATE 15 JUL 23.;[02] TOOL USED: TEMPSDR SWAA2023030202325Angle · crackedCRACK ANGLE TRAILING EDGE LOCATED WS278.5 DEFLECTION CONTROL RIB AREA RT WING 2023-109645<[01] REPLACED ANGLE TRAILING EDGE LOCATED WS278.5 DEFLECTION CONTROL RIB AREA RT WING IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02;[02] CORRECTED STEP 1. REPLACED ANSDR SWAA2023032302051Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE ORSS 261 LT WING 2023-116748<[01] REPLACED CORRUGATED PLATE TRAILING EDGE ORSS 261 LT WING AND FASTENER IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02. AND DWG 15A2711 SHEET 6 REV-. SEE INDIVIDUAL SIGN OFF BELOW.;[02] COSDR SWAA2023032302052Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE IRSS 215 LT WING 2023-116749<[01] REPLACED CORRUGATED PLATE AND FASTENERS LOC. TRAILING EDGE IRSS 215 LT WING IAW B737-700 SRM 51-40-02 AND SRM 51-10-02. SEE INDIVIDUAL SIGNOFFS BELLOW.;[02] COMPLETE TASK CERTIFIEDSDR SWAA2023032302053Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE IRSS 232 AT LT WING 2023-116750<[01] REPLACED CORRUGATED PLATE TRAILING EDGE IRSS 232 AT LT WING IAW B737-700 SRM 51-10-02; 51-40-02 AND DRAWING 115A2001 REV A;[02] CORRECTED STEP 1; REPLACED PLATE ASSY TRAILING EDGE IRSS 2SDR SWAA2023032302049Angle · crackedCRACK ANGLE TRAILING EDGE DEFLECTION CONTEO RIB ORSS 272 LT WING 2023-116744<[01] REPLACED ANGLE AND FASTENERS TRAILING EDGE DEFLECTION CONTEO RIB ORSS 272 LT WING IAW B737-700 SRM 51-10-02 PARAGRAPH 9 AND B737-700 SRM 51-40-02;[02] TASK COMPLETEDSDR IPXA2023021591018Fairing · damagedINSPECTION TYPE:1CL/H WING I/B FLAP I/B ATTACH FILLET FAIRING WAS DAMAGED.REPAIRED DAMAGED FILLET FAIRING ON THE L/H WING I/B FLAP I/B SIDE IAW SRM 53-00-00 FIG 204, FIG 203 PG 212-213. (MINOR)SDR SWAA2023030201782Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE LOCATED ON ORSS 261 AT LT WING 2023-109636<[01] REPLACED CORRUGATED PLATE LOC ON TRAILING EDGE LOCATED ON ORSS 261 AT LT WING IAW B737-700 SRM 51-40-02 AND 51-10-02 ITEM 9;[02] CERTIFIED WORK PERFORMED.SDR SWAA2023030201783Support Angle · crackedCRACK TRAILING EDGE SUPPORT ANGLE LOCATED ORSS 271 AT LT WING 2023-109637<[01] REPLACED TRAILING EDGE SUPPORT ANGLE LOCATED ORSS 271 AT LT WING IAW SRM B737-700 51-10-02 ITEM 9; SRM B737-700 51-40-02 AND DWG 115A2930; SHEET 7; REV-. SEE INDIVIDUAL SIGN OFF BELSDR AALA202302238285Bracket · excess playAIRCRAFT IN BASE MAINTENANCE: RIGHT WING TRAILING EDGE INBOARD FLAP INTERCONNECTING STRUT AFT FITTING / BRACKET BEARING HAS EXCESSIVE PLAY AT RIB 13 OF THE INBOARD FLAP. MAINTENANCE REPLACED FITTING / BRACKET PER SRM 51-72-11.SDR SWAA2023021600725Structure · brokenFOUND BROKEN CLIP AT LEFT WING REAR SPAR LOWER SECTION WSTA 220 WHERE PANEL SUPPORT BEAM ATTACHED.<[01] REMOVED BROKEN CLIP AT L/H WING REAR SPAR LOWER SECTION WSTA 220 AS PER B737-700 SRM 51-40-02-0G-0.;[02] RECEIVED NEW CLIP AND LOCATED NEW FASTENER HOLES ASSDR SWAA2023021600293Beam · elongatedFOUND PANEL 551FB BEAM ASSY (P/N: 115A2753-13) WITH ENLONGATED BUSHING HOLE.<[01] REMOVED BEAM ASSY P/N: 115A2753-13 WITH ENLONGATED BUSHING HOLE AT PANEL 551 FB AS PER BOEING 737-700 SRM 51-40-02-0G-0;[02] VERIFIED;[03] RECEIVED NEW BEAM ASSY P/N115A2753-13 WSDR CALA2023021000389Skin · dentedL/H WING INBD MAIN FLAP LOWER SURFACE HAS 3EA DENTS THAT ARE OUT OF LIMITS AND REQUIRES REPAIRS. OTBD OF OTBD MAIN TRACK TRANSCRIBED FROM HAECO GSO N/R 9284791 CHECKED LIMITS OF 3EA DENTS AND FOUND TO BE OUT OF LIMITS IAW B7 ALODINED IAW B757-200 AMM 51-21-04SDR CALA2023021000388Skin · dentedL/H WING INBD MAIN FLAP LOWER SURFACE HAS 1EA DENT THAT IS OUT OF LIMITS AND REQUIRES REPAIR. OTBD MAIN TRACK. TRANSCRIBED FROM HAECO NR 9284826 CHECKED LIMITS OF DENT AND FOUND TO BE OUT OF LIMITS IAW B757-20 PAINTED IAW B757-200 AMM 51-21-10-377-039, 51-21-1SDR FDEA202302071766Flap · damagedDUE BIRD STRIKE INSPECTION FOUND DAMAGE ON LH OUTBOARD FLAP BETWEEN INBOARD FAIRING AND FLAPERON. IT MEASURES 1"X 0,8" AND IT S LOCATED 2" FROM TRAILING EDGE. TERMINATING ACTION ACCOMPLISHED FOR SRM 57-53-01SDR AALA202302107507Panel · crackedAIRCRAFT IN BASE MAINTENANCE: RIGHT WING OUTBOARD TRAILING EDGE FLAP LEADING EDGE PANEL 5 CRACKED. MAINTENANCE REPLACED PANEL PER SRM 51-72-11.SDR CALA2023020800354Skin · punctured(B757-57-3-0417) L/H WING INBD FWD FLAP LOWER SURFACE IS PUNCTURED APPROX 16" INBD FROM THE OUTBD EDGE (MARKED IN RED). TRANSC RIBED FROM HAECO GSO NRC# 9284695 REPAIRED L/H WING I/B FWD FLAP LOWER SURFACE 16" IB FROM THE O/B EDGE IAW B757 SRM: 51-70-10-2R-2SDR SWAA2023030299634Plate · crackedR WING T/E WIGGLE PLATE CRACKED AT ORSS 262<[01] REMOVED AND REPLACED R WING WIGGLE PLATE AT ORSS 262 IAW BOEING DWG 115A2001 AND SRM 51-40-02;[02] VERIFIED CORRECTIVE ACTION 1.SDR SWAA2023031399449Panel · debondedCUSTOMER REQUEST - DEBONDED IB MAIN FLAP WEDGE PANEL LOWER SURFACE AT LT WING 2023-112679<[01] TOOL USED; CALIPER PN: 500-197-30; SN: B20189526; DUE DATE: 20/DEC/23.;[02] TOOL USED: HOTBONDER P/N: HCS9200B-AV S/N: 18196021 DUE DATE: 24-JAN-24; PROSITECTOR 6000SDR SWAA2023031399450Flap · debondedCUSTOMER REQUEST - DEBONDED OB AFT FLAP LOWER SURFACE LOCATED INBOARD SIDE AT LT WING 2023-112680<[01] TOOL USED; CALIPER PN: 500-197-30; SN: B20189526; DUE DATE: 20/DEC/23.;[02] TOOL USED CALIPER PN: 500-464 S/N: B17030933 DUE DATE: 17/OCT/23;[03] TOOL USED: SDR SWAA2023030999425Fitting · crackedL/W REAR SPAR DEFLECTION CONTROL RIB T/E PANEL VERTICAL SEAL FITTING CRACKED @ FASTENER TAIL MKD DOT<[01] ENTER IN ERROR - DUPLICATE ITEM - THIS FAULT WILL BE ACCOMPLISHED ON FAULT #TTG8Q00HKJXV (TO BE REPLACE FITTING);[02] VERIFIED STEP 1SDR SWAA2023021699319Bracket · crackedPANEL 551FB HAS A L SHAPED BRACKET CRACKED AT FWD O/B.<[01] REMOVED BRACKET CRACKED AT FWD O/B ACCESS PANEL 551FB AS PER BOEING 737-700SRM 51-40-02-0G-0;[02] ADDING TO STEP 1.<BR>REMOVED CRACKED BRACKET (P/N: 287A9152-53) AT FWD O/B ACCESS PANEL 551FB AS PER BSDR SWAA2023021698981Angle · elongatedL/W LOWER T/E PANEL 551FB T/E SUPPORT ANGLE FWD O/B HAS ELONGATED HOLE<[01] NEW BEAM ASSY WILL BE INSTALLED ON TASK CARD: TTG8Q00HQ1R4;[02] VERIFIED STEP#1 AS CORRECT .SDR DALA2023020600900Not Reported · not reportedSHIP 6822 ER/A 596489-14AD REV. B; WINGS / TRAILING EDGE DEVICES / LH INBD MAIN FLAP / INBD TRACK / FWD SUPPORT / ELONGATED HOLE. CORRECTIVE ACTION: 596489-14AD. (2613125)SDR DALA2023020600899Not Reported · not reportedSHIP 6822 ER/A 596443-14AD REV. B; WINGS / TRAILING EDGE DEVICES / RH INBD MAIN FLAP / INBD TRACK / FWD SUPPORT / ELONGATED HOLE. CORRECTIVE ACTION: REF ERA 596443-14AD. (2613022)SDR SWAA2023030698056Skin · delaminatedL/W O/B AFT FLAP LOWER SURFACE SKIN DELAMINATED 25' FROM O/B END<[01] IDENTIFIED L/W O/B AFT FLAP IAW SRM 57-53-01-0I-4 FIGURE 2 TABLE 2 ITEM 5 <BR><BR>DAMAGE EXCEEDS ALLOWABLE DAMAGE LIMITS IAW SRM 57-53-01-1A-5 PAR.4 A(3)<BR><BR>DAMAGE TO BE REPAIRED IAW SRM
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