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 A6WA2018072445946Skin · damagedRIGHT INBOARD FLAP, LOWER SKIN DINGED AND PTTED. REMOVED AND REPLACED RT IB FLAP IB LOWER SKIN IAW SRM 51-42-13.SDR A6WA2018072445945Skin · damagedLEFT INBOARD FLAP LOWER IB SKIN DINGED AND PITTED. REMOVED AND REPLACED LH IB FLAP IB LOWER SKIN IAW SRM 51-42-13.SDR A6WA2018072445943Skin · chafedRIGHT I/B FLAP VANE LEADING EDGE CHAFED AT WS 56.00. REPLACED RIGHT WING I/B FLAP VANE LEADING EDGE IAW SRM 51-42-13.SDR SWIA2018073144920Vane · chafedRT INBD FLAP CENTER OUTBD FLAP VANE CAP IS CHAFED. (C-CHECK) RO: 07/29/2018 REMOVED AND REPLACED RT INBOARD FLAP CENTER VANE CAP IAW SRM.SDR SWIA2018073144919Vane · chafedRT INBD FLAP OUTBD FLAP VANE CAP IS CHAFED. (C-CHECK) RO: 07/29/2018. REMOVED AND REPLACED RT INBOARD FLAP OUTBOARD VANE CAP IAW SRM.SDR SWAA2022021657478Flap · delaminatedLEFT OUTBOARD AFT FLAP HAS DELAM AT THE INBOARD TRAILING EDGE CORNER / REPAIRED LEFT OUTBOARD AFT FLAP INBOARD TRAILING EDGE DELAM IAW B737 SRM 57-53-01-2R-4 AND SRM 51-70-10-2R-0SDR FDEA201807171764Bracket · corrodedLT O/B FLAP O/B FWD (WING SIDE) PIVOT HOLE BORE FOUND WITH CORROSION. IDLER BRACKET ATTACH HOLE BORE REWORKED AS PER SRM 51-21-01-0G. EXISTING HOLE DIA 1.0", FINAL HOLE DIA 1.384", LOCAL BLEND POSITION 9 O'CLOCK POSITION, L=0.25" X W= 0.25", DEPTH=0.065". I/B SDR FDEA201807171763Hinge · corrodedRT O/B FLAP O/B AFT HINGE (FLAP SIDE) PIVOT I/B HOLE BORE FOUND WITH CORROSION. AFT HINGE (FLAP SIDE) PIVOT I/B HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-52-04. EXISTING HOLE DIA 1.148", FINAL HOLE DIA 1.182", MAXIMUM ALLOWABLE HOLE DIA 1.150". OSDR FDEA201807171762Hinge · corrodedRT O/B FLAP I/B AFT HINGE PIVOT I/B HOLE BORE FOUND WITH CORROSION. AFT HINGE PIVOT I/B HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-52-04. EXISTING HOLE DIA 1.149", FINAL HOLE DIA 1.182", MAXIMUM ALLOWABLE HOLE DIA 1.150". REPAIR BUSHING FABRICATEDSDR FDEA201807171761Hinge · corrodedLT O/B FLAP I/B AFT HINGE (FLAP SIDE) I/B PIVOT HOLE BORE FOUND WITH CORROSION. CORRODED PIVOT HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-52-04. EXISTING HOLE DIA 1.124". FINAL HOLE DIA 1.182", MAXIMUM ALLOWABLE HOLE DIA 1.150". OVERSIZED BUSHING SDR IPXA2018071831736Skin · damagedRT WING INBD MID FLAP DAMAGED AT UPPER OTBD FLAP CARRIAGE CUT OUT INCLUDING INNER RIB & UPPER SKIN. REPAIRED PER SRM 51-70-17, REF LP 860767 ITEM 1 FOR ADDITIONAL REPAIR INFO.SDR A6WA2018071845939Skin · chafedRIGHT I/B FLAP VANE LEADING EDGE SKIN CHAFED. REPLACED RIGHT I/B FLAP VANE LEADING EDGE SKIN IAW SRM 51-42-13.SDR FDEA2018071641711Hinge Bracket · corrodedRT INBOARD FLAP OUTBOARD AFT HINGE (FLAP SIDE) INBOARD PIVOT HOLE BORE FOUND WITH CORROSION. CORROSION (HOLE G AND F) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-52-03. EXISTING HOLE DIA 1.255", FINAL HOLE DIA 1.284", MAXIMUM ALLOWABLE HOLE DIA 1.220". OVERSSDR FDEA2018071641710Hinge Bracket · corrodedRT INBOARD FLAP OUTBOARD AFT HINGE (FLAP SIDE) OUTBOARD PIVOT HOLE BORE FOUND WITH CORROSION. CORROSION (HOLE A AND B) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-52-03. EXISTING HOLE DIA 1.290", FINAL HOLE DIA 1.326", MAXIMUM ALLOWABLE HOLE DIA 1.220". OVERSDR FDEA2018071641709Hinge Bracket · corrodedLT INBOARD FLAP OUTBOARD AFT HINGE (FLAP SIDE) PIVOT OUTBOARD HOLE BORE FOUND WITH CORROSION. CORROSION (HOLE A AND B) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-52-03. EXISTING HOLE DIA 1.254", FINAL HOLE DIA 1.2835", MAXIMUM ALLOWABLE HOLE DIA 1.220". OVESDR FDEA2018071641708Hinge Bracket · corrodedLT INBOARD FLAP OUTBOARD AFT HINGE (FLAP SIDE) PIVOT INBOARD HOLE BORE FOUND WITH CORROSION. CORROSION (HOLE G AND F) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-52-03. EXISTING HOLE DIA 1.1885", FINAL HOLE DIA 1.222", MAXIMUM ALLOWABLE HOLE DIA 1.220". OVSDR A6WA2018071845937Skin · damagedRIGHT I/B FLAP LOWER SKIN AREAS OF DENTS AND PITS. REPLACED LOWER SKIN IAW SRM 51-25-16.SDR FDEA2018071641712Skin · damagedRT WING CENTER FLAP APPROX 16" FROM INBD END AND 19" FROM LEADING EDGE, LOWER SURFACE SKIN PREVIOUS REPAIR DEBONDED / CRACKS. REPLACED STRINGER SECTION, REPAIR ANGLE, PACKING PLATE, PACKING STRIPS, AND INSTALLED REPAIR FLAP SKIN DOUBLER IAW SRM 57-50-00-201 FISDR SWAA2018071623520Skin · crackedRT WING INBD AFT FLAP LOWER SKIN CRACKED AT STA 96.5. R&R FLAP PER MM.SDR FDEA201807121688Repair · damagedLT I/B FLAP VANE, I/B END HAS A DAMAGED REPAIR ON TOP SKIN. REPAIRED DAMAGE ON LT I/B FLAP VANE, I/B END TOP SIDE, IAW SRM 51-71-00 VOL 2, PAR 16.SDR KCSA201807121195Flap Track · corrodedNR 8 T/E FLAP TRACK I/B SIDE LOAD BEARING AREA WORN AND CORRODED.SDR KCSA201807121194Flap Track · corrodedNR 7 T/E FLAP TRACK I/B SIDE LOAD BEARING AREA WORN AND CORRODED.SDR KCSA201807121193Flap Track · corrodedNR 6 T/E FLAP TRACK I/B SIDE LOAD BEARING AREA WORN AND CORRODED.SDR KCSA201807121192Flap Track · corrodedNR 3 T/E FLAP TRACK I/B SIDE LOAD BEARING AREA WORN AND CORRODED.SDR KCSA201807121191Flap Track · corrodedNR 2 FLAP TRACK I/B SIDE LOAD BEARING AREA WORN AND CORRODED.SDR KCSA201807121190Flap Track · corrodedNR 1 T/E FLAP TRACK, I/B SIDE LOAD BEARING AREA WORN AND CORRODED.SDR DALA2018071804546Cover · missingRIGHT WING MOST OUTBOARD FLAP TRACK MOVABLE FAIRING RIGHT SIDE COVER MISSING. APPLIED SPEED TAPE AND DEFERRED PER CDL 57-00-07.SDR DALA2018071104448Vane · gougedLT WING LE OF FLAP VANE GOUGED AFT OF CENTER HINGE POINT OB FLAP- REF NRC 189. FLAP VANE REPLACED ON NRC 189.SDR IPXA2018080332357Skin · chafedINSPECTION TYPE:3C, LT I/B FLAP VANE CENTER TRACK CUT OUT ON I/B FLAP SKIN IS CHAFED AT I/B & O/B SIDES. REPAIRED LT I/B FLAP SKIN AT CENTER FLAP VANE TRACK CUT OUT STA XIFH =216.3 IAW EA 011-5753-01-A7382 REV IR AND EO MD11-5750-69441-A. (MINOR)SDR IPXA2018080132245Skin · damagedINSPECTION TYPE:3C, LT I/B FLAP CENTER AFT LOWER SKIN IS DENTED AND CREASED AT STA XIFH183.3 TOXIFH189.3. REPAIRED FLAP LOWER SKIN AT STA XIFH 183.3 TO XIFH 189.3 IAW EA 0115753-01-A7367 REV I/R AND EO MD11-5750-69384-A. (MAJOR)SDR A6WA2018070945927Skin · chafedRT I/B FLAP VANE MID LEADING EDGE CHAFED. REPLACED FLAP VANE MID LEADING EDGE IAW SRM 51-42-13.SDR A6WA2018071345928Skin · chafedLT I/B FLAP VANE I/B LEADING EDGE CHAFED. REPLACED FLAP VANE I/B LE IAW SRM 51-42-13.SDR IPXA2018081132663Fitting · crackedLEFT WING OTBD FLAP, INBD FWD HINGE SIDE LOAD FITTING TENSION STRAP WAS BROKEN IN HALF. REPAIRED THE FLAP INBD HINGE SIDE LOAD FITTING TENSION STRAP IAW EA 011-5753-01-A7384-IR, AND EO MD11-5750-69523-A. MAJOR.SDR FDEA2018080361874Skin · dentedLT INBD MAIN FLAP HAS 2 DENTS ON LOWER SURFACE REPAIRED IAW EA F-5750-T0341340 P1.SDR A6WA201845922Skin · chafedLEFT INBOARD FLAP VANE MID LEADING EDGE CHAFED. REPLACED FLAP VANE LEADING EDGE IAW SRM 51-42-13.SDR R61A201807050799Support · corrodedWHILE AC WAS IN FOR HEAVY CHECK FOUND RT WING IN BOARD MAIN FLAP INMOST FLAP TRACK SUPPORT HAS CORROSION. MX REMOVED CORROSION FLAP TRACK FAIRING SUPPORT PN 170-14654-404. IAW ETD2018-170-076715. AC REMAINS IN IND FOR COMPLETION.SDR AALA2018070969016Skin · damagedLEFT WING TRAILING EDGE OUTBOARD FLAP LOWER SKIN HAS WATER INGRESSION. REPAIRED THE FLAP LOWER SKIN IAW EA 282185A.SDR DALA2018070604414Skin · dentedDURING INSPECTION FOUND DENT OUT OF LIMITS ON LOWER SKIN AT LT INBOARD AFT FLAP LT WING. LOWER SKIN AT LT INBOARD AFT FLAP LT WING (AI) WAS REPAIRED PER SRM 51-70-10-2R-0.SDR IPXA2018071131594Channel · crackedINSPECTION TYPE:1C, LEFT WING FLAP FAIRING 533AT FWD CHANNEL DENTED FOUND CRACK. REMOVED AND REPLACED CHANNEL BY FABRICATING AND INSTALLING IAW DWG A57965531 AND SRM 51-40-21.SDR SWAA2022022146503Skin · delaminatedRIGHT WING OUTBOARD TRAILING EDGE FLAP AFT INBOARD CORNER DELAMINATED MEASURES 9' X 7' / REPAIRED PER EA REPAIR-57EA-05381. TRACKING FOR FINAL REPAIR EC/TC REPAIR-57EA-05384AMT 103595SDR AALA201807059039Skin · corrodedAIRCRAFT WAS IN BASE MAINTENANCE. LEFT HAND WING MAIN INBOARD FLAP UPPER SKIN CORRODED AT INBOARD SIDE. REPLACED LEFT HAND WING INBOARD MAIN FLAP PER AMM 27-51-02.SDR DALA2018070404358Skin · gougedRT WING ON NR 3 FLAP VANE IB SIDE UPPER SURFACE GOUGED. REMOVED DAMAGED SKIN (7" X 7") AND ACCOMPLISHED PERMANENT REPAIR ON NR 3 FLAP VANE LEADING EDGE (16.5" X 12.1" DOUBLER) IAW SRM 57-03D PAR 11 AND FIGURE 11.SDR SWAA2018070223276Flap · delaminatedLT WING INBOARD MAIN FLAP DELAMINATED ALONG AFT EDGE. R&R MAIN FLAP PER AMM.SDR P5CA2018070900115Flap · damagedLT WING NR 10 VC FLAP O/B FOLDING NOSE DAMAGE. FLAP O/B FOLDING NOSE CRACK AREAS REPAIRED IAW RI NO: RI-57-40-12802 REV A.SDR DALA2018070304342Vane · gougedLEFT WING OUTBD END OF FWD FLAP FIXED VANE L/E HAS DAMAGE (GOUGED). INSTALLED SAME O/B FIXED VANE AFTER SHOP VISIT PER AMM TASK 27-50-02.SDR YENA201806260924Skin · damagedDURING CURRENT (6/2018) C-9 HEAVY CHECK AT GSO, WAS REPORTED WITH FRAYING DAMAGE COMMON TO THE LT OUTBOARD FLAP (PN D5757420200400/ SN TB-12720) AT THE UPPER SKIN AROUND A FILLED PRODUCTION INSPECTION HOLE (SE REF /1/ REO FOR DETAILS). CONTACTED AND INSTRUCTSDR FQAR20180602739Bracket · crackedDURING A SCHEDULED INSPECTION THE FORWARD FLAP BACKET WAS FOUND TO BE CRACKED, BRACKET IS LOCATED IN THE TUNNEL AND IS THE FORWARD MOUNTING POINT FOR THE FLAP HANDLE ASSEMBLY. SUSPECT CRACKING IS CAUSED BY CREWS IN ADVERTANTLY STEPPING ON THE FLAP HANDLE WHEN SDR FDEA201806261580Skin · corrodedRIGHT WING OUTBOARD FLAP, OUTBOARD END STATIC WICK BASE IS LOOSE AND CORRODED ACCOMPLISHED EA 6-5750-T0340592 STEPS 1 THRU 8 DATED 06/20/18. TITLE: WINGS - FLIGHT SURFACES - RT O/B FLAP, OUTER TRAILING EDGE UPPER SKIN CORROSION BELOW STATIC DISCHARGER. TRIMOSDR SWIA2018080244950Vane · chafedREPLACE THE RT INBD FLAP CENTER VANE CAP. (C-CHECK) RO: 08/01/2018 REPLACED RT INBD FLAP CENTER VANE CAP WITH NEW PART IAW SRM.SDR FDEA201806251576Skin · gougedLT WING INBD FLAP UPPER SKIN HAS GOUGE (4 PLACES) COMPLIED WITH EA 6-5750-T0340423 DATED JUNE 19, 2018. TITLE: WINGS - FLIGHT SURFACES - LT WING INBD FLAP TOP SKIN REPAIR, BETWEEN RIB 5 AND RIB 7 TRACK RIB 2, BETWEEN STRINGERS 2.1 AND 2.2. MAJOR REPAIR.
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