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 DALA2017021801411Skin · puncturedRIGHT WING INBD, FORE FLAP LOWER SURFACE PUNCTURED. REPAIRED IAW SRM 51-70-07.SDR DALA2017021700029Flap Track · corrodedCORROSION ON RIGHT WING FLAP TRACK NR 3. REPLACED THE FLAP TRACK.SDR DALA2017021700028Flap Track · corrodedCORROSION LEFT WING FLAP TRACK NR 3. REPLACED THE FLAP TRACK.SDR DALA2017021700027Flap Track · corrodedCORROSION RIGHT WING FLAP TRACK NR 4. REPLACED THE FLAP TRACK.SDR DALA2017021700026Flap Track · corrodedCORROSION LEFT WING FLAP TRACK NR 3. REPLACED THE FLAP TRACK.SDR SWAA2017022211957Skin · delaminatedLEFT WING OUTBOARD AFT FLAP HAS DELAMINATION 15 INCHES FROM OUTBOARD END. R & R THE AFT FLAP IAW MM.SDR FDEA201702160570Rib · crackedNDT X-RAY INSPECTION FOUND LT CTR FLAP RIB20 CRACK AT AFT SECTION COMPLIED WITH EA:6-5750-T0330963 A PT1 EA TITLE:WINGS-FLIGHT SURFACES-CRACKS AT LT CENTER FLAP RIB 12.19.20.25.26 UPPER FLANGES. THIS IS A MAJOR REPAIR IAW GMM6-2-100.SDR FDEA201702160569Rib · crackedNDT X-RAY INSPECTION FOUND LT CTR FLAP RIB 26 CRACK AT AFT SECTION(2EA). COMPLIED WITH EA:6-5750-T0330963 A PT1 EA TITLE:WINGS-FLIGHT SURFACES-CRACKS AT LT CENTER FLAP RIB12.19.20.25.26 UPPER FLANGES THIS IS A MAJOR REPAIR IAW GMM6-2-100.SDR SWAA2017022211975Skin · delaminatedLEFT WING OUTBOARD FORE FLAP DELAMINATED. R & R THE FORE FLAP IAW AMM.SDR SWAA2017022211938Skin · delaminatedLEFT WING INBOARD AFT CORNER OF OUTBOARD AFT FLAP DELAMINATED. R & R THE AFT FLAP IAW MM.SDR FDEA201702150564Skin · crackedLEFT INBD FLAP UPPER SKIN HAD ONE CRACK AT RIVET ROW XIFH 159. REPAIRED IAW SRM 57-00-01, FIG 4, SHEET 2, VOL.1.SDR FDEA201702150563Skin · crackedLEFT INBD FLAP UPPER SKIN HAS TWO CRACKS AT RIVET ROW XIFH 165. REPAIRED IAW SRM 57-00-01, FIG 4, SHEET 2, VOL. 1.SDR FDEA201702150562Skin · crackedLEFT INBD FLAP UPPER SKIN HAS TWO CRACKS AT RIVET ROW XIFH 225. REPAIRED IAW SRM 57-00-01, FIG 4, SHEET 2, VOL. 1.SDR FDEA201702150561Skin · crackedLEFT INBD FLAP UPPER SKIN HAS THREE CRACKS AT RIVET ROW XIFH 231. REPAIRED IAW SRM 57-00-01, FIG 4, SHEET 2, VOL. 1..SDR IPXA2017030614807Support Angle · crackedINSPECTION TYPE: 2C, RT WING O/B FLAP I/B HINGE AFT FAIRING I/B SIDE SUPPORT ANGLE IS CRACKED.REMOVED, FABRICATED AND REPLACED THE SUPPORT ANGLE IAW DWG ARC2229 AND SRM 51-35-02.SDR IPXA2017030614805Beam · crackedINSPECTION TYPE: 2C, RIGHT WING OTBD FLAP INBD HINGE AFT FAIRING, OTBD SIDE SUPPORT BEAM IS CRACKED. REMOVED, FABRICATED, AND REPLACED FLAP FAIRING SUPPORT BEAM IAW DWG ARC2149-4, AND SRM 51-35-02.SDR SWAA2017030112213Skin · delaminatedLEFT WING INBOARD TRAILING EDGE OUTBOARD AFT FLAP DELAMINATED ON UPPER SKIN. REPAIRED THE FLAP IAW SRM.SDR ABXA20170214011Beam · corrodedNR 8 FLAP SUPPORT 1-2-3 BEAM HAS FOUR HOLES SHOWING DEFECTS. REPAIRED IAW REA CO57-62458-MR. AIRCRAFT WAS GROUNDED.SDR SWAA2017021611913Skin · delaminatedLT WING OUTBOARD AFT FLAP INBOARD CORNER LOWER SURFACE DELAMINATED. R&R AFT FLAP IAW AMM.SDR FDEA201702140557Rub Strip · debondedRIGHT OUTBOARD FLAP VANE, FOUND FROM OUTBOARD SECOND RUB STRIP IS DISBONDED AND DELAMINATED. REPAIRED IAW SRM 51-71-00.SDR FDEA201702140552Rib · crackedNDT X-RAY INSPECTION FOUND LT CTR FLAP RIB25 CRACK AT AFT SECTION. COMPLIED WITH EA 6-5750-T0330963 A PT1 EA TITLE:WINGS-FLIGHT SURFACES-CRACKS AT LT CENTER FLAP RIB12.19.20.25.26 UPPER FLANGES. THIS IS A MAJOR REPAIR IAW GMM6-2-100.SDR FDEA201702140551Rib · crackedNDT X-RAY INSPECTION FOUND LT CTR FLAP RIB12 CRACK AT AFT SECTION. COMPLIED WITH EA 6-5750-T0330963 A PT1 EA TITLE:WINGS-FLIGHT SURFACES-CRACKS AT LT CENTER FLAP RIB 12.19.20.25.26 UPPER FLANGES. THIS IS A MAJOR REPAIR IAW GMM6-2-100.SDR FDEA201702140550Rib · crackedNDT X-RAY INSPECTION FOUND LT CTR FLAP RIB19 CRACK AT AFT SECTION(2EA). COMPLIED WITH EA 6-5750-T0330963 A PT1 EA TITLE: WINGS-FLIGHT SURFACES-CRACKS AT LT CENTER FLAP RIB 12.19.20.25.26 UPPER FLANGES. THIS IS A MAJOR REPAIR IAW GMM6-2-100.SDR DALA2017021501235Vane · delaminatedDELAMINATION ON LOWER SURFACE OF CENTER GUIDE VANE, LT OTBD FLAP. THE GUIDE VANE WAS REMOVED AND REPLACED IAW AMM 27-51-03.SDR FDEA201702120525Hinge Bracket · corrodedLEFT WING INBD FLAP FWD (WING SIDE) OTBD HINGE PIVOT HOLE BORE CORRODED. A REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-44-07 AND PER EA 1-5750-T0328840 D, PART 1, STEP 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201702110516Skin · dentedRIGHT WING OTBD FLAP T/E SKIN HAS TWO DENTS INBD OF NR 6 FLAP TRACK. REPAIRED IAW EA 6-5750-T03331264.SDR SWAA2017022712115Plate · crackedLEFT WING FLAP TRACK FAIRING 542BB PLATE CRACKED. R & R THE PLATE IAW SRM AND DWG.SDR AALA20170210012Fitting · corrodedCORROSION ON LEFT WING OUTBOARD FLAP CENTER AFT HINGE FITTING. REMOVED AND REPLACED FITTING IAW AMM 57-40-01-201 AND ESO 800096.SDR KCSA201702101004Access Panel · corrodedINBD MID FLAP UPPER SURFACE APPROX. 30 INCHES INBD AND 18 INCHES FROM BOTTOM EDGE HAS DAMAGED FASTENERS.SDR DALA2017021001122Vane · puncturedRIGHT WING PUNCTURED ON PREVIUS REPAIR ON INBD FLAP INBD VANE. REPAIRED IAW SRM 57-03D PARAGRAPH 11 FIGURE 11.SDR FDEA201702060435Hinge Fitting · corrodedRIGHT WING OTBD FLAP INBOARD AFT HINGE (FLAP SIDE) INBOARD PIVOT BORE FOUND WITH CORROSION. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-52-04. BUSHING FABRICATED AND INSTALLED IAW EA 1-5750- T0331077, PART 1, STEP 1B. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2SDR DALA2017020701030Flap · damagedRIGHT O/B FLAP TRAILING EDGE DAMAGED I/B SIDE REPAIRED PER SRM 57-53-01.SDR IPXA2017022714478Angle · chafedINSPECTION TYPE: 3C, LEFT WING LOWER T/E OTBD FLAP INBD HINGE FAIRING PANEL LANDING CHAFED. REMOVED, FABRICATED, AND INSTALLED A REPLACEMENT ANGLE IAW DWG ARC0744 AND SRM 51-33-01.SDR REXA2017020300179Skin · dentedLEFT INBD FLAP LOWER SKIN HAS FOUR DENTS ON INBD SIDE. REMOVED AND REPLACED THE FLAP SKIN IAW SRM 57-52-00, 51-40-11, & 51-42-13,SDR REXA2017020200177Structure · bentLEFT INBD FLAP, TRAILING EDGE IS BENT IN TWO PLACES ON INBD AREA. REMOVED & REPLACED THE FLAP TRAILING EDGE IAW SRM 51-42-12.SDR FDEA201702020341Vane · corrodedRIGHT WING OTBD FLAP VANE NR 2 FITTING BUSHING HOLE CORRODED. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 57-50-02-2R FIG 201. A SLOT BUSHING WAS FABRICATED IAW EA 1-5750-T0331241, PART 1, STEP 2 AND INSTALLED IAW AMM 27-50-32-4.SDR FDEA201702020340Hinge Bracket · corrodedRIGHT WING OTBD FLAP AFT HINGE, FLAP SIDE, PIVOT OUTBD HOLE BORE FOUND CORRODED. REMOVED THE CORROSION AND FOUND OUT OF LIMITS IAW CMM 57-52-03. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-132706 D, PART 4, STEP 2 & 3.SDR FDEA201702020339Hinge Bracket · corrodedRIGHT WING OTBD FLAP AFT HINGE, FLAP SIDE, PIVOT INBD HOLE BORE FOUND CORRODED. REMOVED THE CORROSION AND FOUND OUT OF LIMITS IAW CMM 57-52-03. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-132706 D, PART 4, STEP 2 & 3.SDR FDEA201702020318Hinge Bracket · corrodedLEFT WING INBD FLAP OUTBOARD AFT HINGE (FLAP SIDE) PIVOT INBD HOLE BORE FOUND WITH CORROSION. REMOVED THE CORROSION AND FOUND OUT OF LIMITS IAW CMM 57-52-03. OVERSIZED BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-132705 C, PART 4, STEP 2A & 2C. CLASSIFIESDR FDEA201702020317Hinge Bracket · corrodedLEFT WING INBD FLAP OTBD AFT HINGE (FLAP SIDE) PIVOT OUTBD HOLE BORE FOUND WITH CORROSION. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW CMM 57-52-03. OVERSIZE BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-132705 C, PART 4, STEP 2A & 2C. REPAIR CLASSSDR DALA2017020300935Skin · delaminatedLT WING OTBD T/E FLAP AFT FLAP LOWER SKIN FOUND THREE DELAMINATION. ONE DELAMINATION APPROX 1.5X1.5 INCH FROM T/E 2 INCH AND FROM INBD 132 INCH. ONE DELAMINATION APPROX 1X1 INCH FROM T/E 5 INCH AND FROM INBD 73 INCH. THE OTHER DELAMINATION APPROX 1X1 INCH FROMSDR DALA2017020300880Vane · corrodedRIGHT WING CORRODED ON LOWER SURFACE INBD SIDE AT RT OTBD FLAP OTBD VANE. THE VANE WAS REPLACED .SDR SIMA20170201004Skin · damagedDURING POSTFLIGHT WALKAROUND, F/O REPORTS A DENT ON LOWER SKIN OF LEFT INBOARD FLAP IN LINE WITH #2 TIRE. DENT IS ALSO IN LINE AND ON A ROW OF FASTENERS. REF LOG PAGE 4054862 ITEM 3. ALSO REFERENCE ERS-CR-57DF-677 PTC SMALL DENT ON LH INBD FLAP LOWER SURFACE SDR SCNA20170201052Bellcrank · wornRIGHT INBOARD MAIN FLAP, INBOARD AFT FLAP BELLCRANK HAS WEAR AT BOTH CABLE CONNECTIONS ON THE UPPER SIDE. REPAIRED RIGHT INBOARD MAIN FLAP, INBAORD AFT FLAP BELLCRANK BOTH CABLE CONNECTIONS ON THE UPPER SIDE.SDR SCNA20170201048Track · wornLEFT INBOARD FLAP, INBOARD PROGRAMMING TRACK IS WORN. REMOVED DAMAGED L/H I/B FLAP I/B PROGRAMMING TRACK P/N: 654A0004-525. REPLACED.SDR SCNA20170201041Structure · delaminatedRIGHT OUTBOARD AFT FLAP, INBOARD TRAILING EDGE CORNER HAS AN AREA OF DELAMINATION. REPAIRED.SDR SCNA20170201040Bellcrank · wornRIGHT INBOARD MAIN FLAP, INBOARD AFT FLAP CABLE BELLCRANK HAS WEAR AT BOTH CABLE CONNECTIONS ON THE LOWER SIDE. REPAIRED RIGHT INBOARD MAIN FLAP, INBOARD AFT FLAP CABLE BELLCRANK BOTH CONNECTION ON THE LOWER SIDE.SDR DALA2017020300945Skin · delaminatedRIGHT WING INBD T/E FLAP AFT FLAP TOP SKIN FOUND TWO DELAMINATION ONE IS FROM T/E 15 INCH AND FROM INBD 98 INCH APPROX 11X10 INCH THE OTHER IS FROM T/E 4.5 INCH AND FROM INBD 180 INCH APPROX 1X1 INCH. REPAIRED IAW SRM 51-70-07 PARA. 5. A(1) FIG 5 REV 98.SDR DALA2017020300944Skin · delaminatedLEFT WING INBD T/E FLAP AFT FLAP TOP SKIN FOUND TWO AREAS DELAMINATION ONE DELAMINATION APPROX 1.5X1 INCH FROM T/E 5.5 INCH AND FROM INBD 151 INCH THE OTHER APPROX 3.5X2 INCH FROM T/E 2 INCH AND FROM INBD 176 INCH. REPAIRED IAW SRM 51-70-07 PARA. 5. A(1) FIG. SDR DALA2017020300943Skin · delaminatedLEFT WING INBD T/E FLAP AFT FLAP TOP SKIN FOUND TWO AREAS DELAMINATION APPROX 1X1 INCH. ONE IS FROM T/E 1.5 INCH AND FROM INBD 128 INCH THE OTHER IS FROM T/E 5 INCH AND FROM OTBD 111 INCH. REPAIRED THE IAW SRM 51-70-07 PARA. 5. A(1) FIG. 5 REV. 98.
Back to JASC 5753