JASC 5753
Service difficulty reports · 31,515
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 IXXA08SMN111SSkin · delaminatedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING NUMBER 4 VANE FLAP DELAMINATED SKIN BETWEEN STATION XF 225.000 TO STA XF 335.000. REMOVED AND REPLACED RIGHT WING NUMBER 4 VANE FLAP. PERFORMED OPS CHECK GOOD TO FLAP SYSTEM IAW DC8 MM 27-51-14 PAGES 201-20SDR IXXA08SMN112SSkin · delaminatedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING NUMBER 5 VANE FLAP DELAMINATED SKIN BETWEEN STATION XF 345.000 TO STA XF 404.000. REMOVED AND REPLACED RIGHT WING NUMBER 5 VANE FLAP. PERFORMED OPS CHECK GOOD TO FLAP SYSTEM IAW DC8 MM 27-51-14 PAGES 201-20SDR IXXA08SMN113SSkin · delaminatedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING NUMBER 6 VANE FLAP DELAMINATED SKIN BETWEEN STATION XF 415.000 TO STA XF 434.000. REMOVED AND REPLACED RIGHT WING NUMBER 6 VANE FLAP. PERFORMED OPS CHECK GOOD TO FLAP SYSTEM IAW DC8 MM 27-51-14 PAGES 201-20SDR ASAA0842890Skin · dentedLEFT I/B AFT FLAPS FORE FLAP LOWER SURFACE DENTED 4' FROM I/B END ON 4.5" FROM TIE. REMOVED PREVIOUS REPAIR, PREPPED AREA, FABRICATED AND INSTALLED REPAIR DOUBLER IAW B737 400 SRM 51 70 10 REPAIR 2.SDR CA080331007Flap Track · gouged(CAN) UPON INSP OF THE IB FLAP TRACK RAILS, GOUGES ARE EVIDENT ON THE UPPER INNER SURFACE FACE AND ON THE UPPER SIDE FACE THAT ARE OUT OF LIMITS. SEE ALSO SDR 20080318006 FOR DETAILS. RAIL AFT, RAIL, RAIL MAIN 1, RAIL MAIN 2 OUT PN: 170-39320-001, 170-39060SDR IXXA08SMN118SSkin · damagedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT INBOARD FLAP SKIN UPPER PLATING NICKED AT STATION XW 112.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGE PLATING. FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTSDR USAA920080840Skin · crackedPIT- MAJOR REPAIR - C4 CHECK - A 5" CRACK ON RIGHT O/B FLAP BOTTOM SKIN AT O/B EDGE. REPAIRED IAW SRM 57-53-01 FIG 201, REPAIR 4.SDR SWAA081691Flap · delaminatedDURING SCHEDULED HC2 CHECK, FOUND LT WING INBOARD T/E AFT FLAP DELAMINATED AT INBOARD END. REMOVED AND REPLACED FLAP PER MM.SDR SWAA081682Flap · delaminatedDURING SCHEDULED BRDG CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED AT OUTBOARD END. REPAIRED FLAP PER SRM.SDR 08FDEA01164Skin · looseLT WING OUTBD FLAP LWR SURFACE FOUND 100 LOOSE RIVETS ON SKIN. REPAIRED SKIN LOOSE FASTENERS IAW SRM 57-20-00 FIG 11 VOL I.SDR 08FDEA01163Skin · looseLT WING OUTBD FLAP UPPER SURFACE FOUND 120 LOOSE FASTENERS ON SKIN. REPAIRED SKIN LOOSE FASTENERS IAW SRM 57-20-00 FIG 11 VOL I.SDR UPS08M52670Hinge · corrodedINSPECTION TYPE-C, RT WING OB FLAP IB HINGE (FLAP MOUNTED) UPPER MOUNTING POINT FWD OB NR 2 BORE HOLE FOUND CORRODED AS MARKED. CORRODED IN AFFECTED AREA REMOVED. ORG DIA 0.599", FINAL DIA 0.6725". FPI C/O ON REWORK AREA & FOUND NO CORROSION EVDNT. BORE FINASDR UPS08M52631Bushing · corrodedINSPECTION TYPE-C, LT WING IB FLAP OB HINGE PIVOT POINT IB LUG BUSHING FOUND CORRODED. CORROSION REMOVED EXCEED LIMIT CMM 57-52-03 PG 442-444 R60 ORIG DIA 1.188, FINAL 1.257 MAX ALLOWABLE 1.220. FPI C/O DACNDTSPMR13PT8 NO CORR EVIDENT. RW K AREA PORTECTED, PSDR UPS08M52630Bushing · corrodedINSPECTION TYPE-C, LT WING IB FLAP OB HINGE PIVOT POINT OB LUG BUSHING FOUND CORRODED. CORROSION REMOVED EXCEED LIMIT CMM 57-52-03PG442-444R60 ORIG DIA 1.187" FINAL 1.258" MAX ALLOWABLE 1.220". FPI C/O NDT SPM R13PT8 NO CORROSION EVIDENT. AREA PROTECTED & PASDR UPS08M52504Hinge · corrodedINSPECTION TYPE:C RHW O/B FLAP O/B HINGE CENTER CAVITY HOLE FOUND CORRODED AS MARKED. RHW AFT O/B FLAP O/B HINGE FWD MOUNTING CENTER CAVITY HOLE CORROSION. REMOVED ORG DIA EVIDENT FLAP HINGE CENTER CAVITY HOLE OF DIA 1.788 INCH EVAL AND FOUND ACCEPTED PER ESDR UIEA200800095Skin · damagedLT OUTBOARD T/E FORE FLAP SURFACE DAMAGE ON BULLNOSE AREA AT OUT BOARD END. REPAIRED PER SRM 51-70-07 AND ATLAS EO 4457A135.SDR DLM90080466Skin · dentedC/W ER/A 096112-14 REPAIR LEFT WING INBOARD MAIN FLAP LOWER SKIN X1F1=41.5 DENT. REPAIRED LEFT WING INBOARD MAIN FLAP LOWER SKIN, IAW ER/A 096112-14 REV B 01-28-06 AND MD90 SRM 57-03D FIG 807D PERMANENT REPAIR. NO FURTHER ACTION REQUIRED.SDR 2008UALA01710Rib · wornLT INBD FLAP, MIDDLE FOREFLAP TRACK BEARING SUPPORT HOLE WORN IN RIB. MAJOR REPAIR ACCOMPLISHED: REPLACED DAMAGED RIB.SDR ASAA0872799Skin · dentedRT INBOARD MAIN FLAP O/B UPPER PANEL (653ET) HAS NUMEROUS DENTS AT UPPER SURFACE RT INBD MAIN FLAP OUTBD UPPER PNL. REPAIRED IAW B737 700 SRM CH 51 70 10 REPAIR 2.SDR 08FDEA01151Hinge Bracket · corrodedDURING MODIFICATION MD10 ACF RT OUTBOARD FLAP INBOARD HINGE WITH RUST, BUSHING WITH PLAY AND SHIM WITH OXIDE. REPLACED HINGE FLAP P/N ARC0502-501 FOR DWG ARC0504.SDR SWAA081641Skin · delaminatedDURING SCHEDULED 16Y CHECK, FOUND RT WING INBOARD FORE FLAP UPPER SKIN DELAMINATED AT OUTBOARD END. REPAIRED FLAP PER SRM.SDR 08FDEA01137Hinge Bracket · corrodedDURING MD10 ACF MODIFICATION FOUND RT OUTBOARD FLAP, OUTBOARD HINGE WITH RUT AND CORROSION. REPLACED BRACKET ASSY OUT FLAP FOR DWG ARC0503-502SDR 08FDEA01136Hinge Bracket · corrodedDURING MD10 ACF MODIFICATION, FOUND LT OUTBOARD FLAP OUTBOARD HINGE WITH ATTACH POINTS WITH OXIDE. REPLACED BRACKET ASSY P/N ARC0503-501 FOR DWG ARC0505.SDR 08FDEA01135Hinge Bracket · corrodedDURING MD10 ACF MODIFICATION, FOUND LT OUTBOARD INBOARD FLAP HINGE WITH ATTACH POINT (FWD) RUST AND BUSHING WITH PLAY. REPLACED BRACKET ASSY FOR DWG ARC0504.SDR UPS08151997Skin · dentedINSPECTION TYPE:5YR RIGHT I/B FLAP LOWER SKIN I/B OF NR 2 FLAP TRACK DENT. MEASURED DENT AND FOUND OUT OF LIMITS IAW A300 SRM 57-50-00 FIG 101. CUT OUT DAMAGED SKIN, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SAA EA 300-5730-01-A1334.SDR 08FDEA01128Panel · dentedLEFT INBD FLAP, LOWER INBD PANEL (P/N ARC 2991-1) IS DENTED AND DEFORMED. THE ACCESS DOOR WITHIN THE PANEL IS MOST DIFFICULT TO CLOSE. REMOVED & REPLACED DOOR HUNGE IAW SRM 51-31-01 VOL II. FABRICATED DOUBLER REPAIR IAW SRM 57-10-00 FIG 85 VOL I. ALODINESDR ASAA0842865Skin · dentedRT WING TRAILING EDGE RT WING INBOARD AFT FLAP LOW SURFACE HAS A SHARP DENT IN LEADING EDGE CAP AT OUTBOARD ACTUATING ROD. DENT ON LT WING TRAILING EDGE RT WING AFT FLAP LOWER SURFACE WAS REPAIRED IAW B737 400 SRM 57 53 01.SDR SWAA081600Flap · brokenLEFT WING FOREFLAP MECHANISM PROTRUDING UNDER WING. REMOVED AND REPLACED FLAP PER MM.SDR SWAA081557Skin · delaminatedDURING SCHEDULED C4 CHECK, FOUND LT WING INBOARD FORE FLAP DELAMINATED ON UPPER SURFACE. REMOVED AND REPLACED FLAP PER MM.SDR 2008747001Wedge · delaminatedUPON INSPECTION TO THE EXTERIOR OF THE AIRCRAFT, FOUND THE LEFT INBOARD TRAILING EDGE MIDFLAP WEDGE DELAMINATED AT WBL 203.0 4 1/2 BY 2 1/2 AREA OF DELAMINATION. REPAIRED BY FLIGHTSTAR AIRCRAFT SERVICES USING BOEING SRM 51-40-20,51-50--2 AND 51-40-21. THIS ISDR WRLA2008031Flap · debondedDURING C-CHECK INSPECTION FOUND RIGHT WING INBOARD FLAP DISBONDED. REF EGAT NRC U07003. REPAIRED PER ENGINEERING INSTRUCTION NO.W2008A57B-202 REV.00SDR SWAA081522Flap · delaminatedDURING SCHEDULED C4 CHECK, FOUND LT WING INBOARD FOREFLAP DELAMINATED. REMOVED AND REPLACED FLAP PER MM.SDR 08FDEA01063Skin · damagedRT INBD FLAP HAS HAIL DAMAGE; SEVERAL DENTS ON THE LOWER SURFACE. RECORDED & REPAIRED AS REQUIRED. REMOVED & INSTALLED RIGHT WING INBD FLAP T/E WEDGE IN REF TO SRM 51-31-01 VOL II.SDR 08FDEA01062Wedge · delaminatedRT OUTBD FLAP T/E WEDGE IS DELAMINATED. REMOVED T/E SECTION IAW SRM 51-35-01 VOL II. LOCATED, DRILLED & DEBURRED NEW T/E SECTION IAW SRM 57-20-00 FIG 10 VOL I. INSTALLED T/E SECTION IAW SRM 57-20-00 FIG 10 VOL I.SDR 08FDEA01061Skin · damagedRT OUTBD FLAP LOWER SKIN HAS HAIL DAMAGE; SEVERAL DENTS. RECORDED & REPAIRED AS REQUIRED. REMOVED & INSTALLED RT WING OUTBD FLAP INBD HINGE FAIRING TO WEDGE BRACKETS IN REF TO SRM 51-31-01 VOL II. REMOVED & INSTALLED 3 EA T/E WEDGES IN REF TO SRM 51-31-01 VOSDR HNAA0800135Support Beam · damagedDURING INSPECTION AFTER INFLIGHT FIRE, THE OUTBOARD NR 3 FLAP TRACK SUPPORT BEAM WAS FOUND TO HAVE FIRE DAMAGE. MAINTENANCE REPLACED SUPPORT BEAM.SDR DHL2008805511Flap · damagedRT OUTBD FLAP L/E PLATING HOLES ELONGATED (STA XF 325.000 - 243.000). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 03-12-08, ASTAR EVA D857-00049 REV IR DATED 03-12-08, SEMAN DWG NR ED-4719 DATED 02-25-08. PERFORMED NDT INSP OF DAMAGED AREA IAW DC8 NDT SSDR SWIA200819369Structure · crackedRIGHT NACELLE FLAP IS CRACKED. REPLACED RIGHT NACELLE FLAP IAW EMB 120 MM 27-50-03. OPS CHECK GOOD.SDR 08FDEA01043Panel · crackedRT INBD FLAP AFT INBD EDGE IS CRACKED. REMOVED, LOCATED, DRILLED & INSTALLED T/E TIP IAW SRM 51-35-02, VOL II. REMOVED, INSTALLED & CHECKED PER AMM 27-50-01-4.SDR 08FDEA01042Panel · chafedLT WING INBD FLAP FWD L/E PANEL IS CHAFED AT THE OUTBD HINGE AREA. BLENDED CHAFFED AREA & FOUND OUT OF LIMITS IAW SRM 57-00-01 VOL I, ORIGINAL THICKNESS 0.080. REMAINING MATERIAL 0.020. MATERIAL REMOVED 0.060. FABRICATED SKIN & INNER DOUBLER IAW DWG ARC 315SDR 08FDEA01041Skin · dentedLT WING INBD FLAP FWD SURFACE HAS MANY DENTS. REMOVED & INSTALLED 2 FLAP WEDGES IN REF TO SRM 51-31-01 VOL II.SDR 08FDEA01040Panel · delaminatedLT WING OUTBD FLAP PANEL 536 HL; CORNER IS DELAMINATED. REPAIRED BY REMOVING THE DAMAGED SKIN FABRICATING A SKIN, PLUG & DOUBLE. HOT BONDED REPAIR & REFINISHED IAW SRM 51-71-00.SDR SWAA081482Flap · delaminatedRIGHT WING OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD T/E. REMOVED AND REPLACED FLAP PER MM.SDR CALA0800233Support Fitting · corrodedLEFT MLG FWD TRUNNION SUPPORT HAS PITTING CORROSION AT UPPER I/B BUSHING. REPAIRED PER EC/RA 5741-01106.SDR 08FDEA01021Rub Strip · wornLT WING FLAP FWD SIDE L/E RUB STRIP IS WORN IN AREAS. BLENDED AREA AND FOUND TO BE OUT OF LIMITS IN REF TO SRM 57-00-01 VOL I. REMOVED RUB STRIPS IN REF TO SRM 51-35-01 VOL II. DRILLED, DEBURRED, & COUNTERSUNK NEW RUB STRIP IN REF TO SRM 51-31-01 VOL II. SDR 08FDEA01020Panel · dentedRT WING OUTBD FLAP; INBD PANEL NR 636 BR IS DENTED IN SEVERAL PLACES. REPAIRED RT WING OUTBD FLAP INBD PANEL 636 BR BY CHECKING LIMITS ON THE DENTS IAW SRM 51-80-01 VOL II. REMOVED DAMAGED AREAS FOUND TO BE OUT OF LIMITS. PERFORMED DOUBLER REPAIR AT THE OUTESDR 08FDEA01011Skin · dentedLT WING INBD FLAP UPPER SURFACE FOUND 1 EA DENT ON SKIN. REPAIRED SKIN IAW SRM 51-10-00 PAR 2 VOL II.SDR 08FDEA01009Hinge Fitting · corrodedRIGHT WING, INBOARD FLAP AFT HINGE AFT INBOARD FASTENER HOLE FOUND CORROSION. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-116428. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 08FDEA01270Flap Track · wornLT FLAP VANE NR 1 TRACK HAS WORN AREAS MARKED. REPAIRED NR 1 FLAP VANE TRACK IAW AIRBUS CMM 57-52-15.SDR 08FDEA01269Flap Track · wornLT FLAP VANE NR 4 TRACK HAS WORN AREAS MARKED. REPAIRED L/W NR 4 FLAP VANE TRACK IAW AIRBUS CMM 57-52-15.
Back to JASC 5753