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 ASAA2013011493731Skin · dentedLT WING INBD MIDFLAP T/E WEDGE IS DENTED ON LOWER SURFACE AT THE CENTER OF THE WEDGE. ACFT GROUNDED. REPAIRED LT WING INBD MIDFLAP T/E WEDGE ON LOWER SURFACE AT THE CENTER OF WEDGE IAW SRM 51-70-10, REPAIR 4.SDR SWAA2013011611456Spindle · corrodedLEFT WING NR 7 FLAP SPINDLE HAS EVIDENCE OF BASE METAL CORROSION AT THE LOWER SURFACE OF THE SPINDLE PORTION OF THE ROOT. REMOVED AND REPLACED RIGHT OTBOARD MIDFLAP INBOARD (NR 7) CARRIAGE PER MT #327-51-08.SDR IPXA3576962Skin · dentedINSPECTION TYPE: S4C8, DENT ON LOWER SKIN OF LT INBD MAIN FLAP AT MF STA 130.0. DENT 1.25" X .75" X .035 DEEP WITH A SMALL PUNCTURE DRILLED .0625 DIAM HOLE TO CLEAN UP PUNCTURE, FABRICATED REPAIR PARTS IAW 51-70-10-2R-REP NR 2.SDR SWAA2013020412265Flap · delaminatedDELAMINATED O/B AFT FLAP AT LEVEL FLAP TRACK FAIRING NR 1 LEFT WING. REMOVED AND REPLACED AFT FLAP ON CARD.SDR SWAA2013013112173Flap · delaminatedDELAMINATION WAS FOUND ON OUTBOARD AND LOWER CORNER OF OUTBOARD AFT FLAP LEFT WING. REPAIRED OUTBOARD AND LOWER CORNER OF OUTBOARD AFT FLAP LEFT WING IAW B737-300 SRM 51-70-10-2R-0SDR IPXA13576679Skin · dentedLEFT WING INBD MAIN FLAP T/E SKIN DENTED. REPAIRED IAW EO B757-5750-49091-B.SDR CA130116021Fairing · damaged(CAN) DURING WALK AROUND, IT WAS DISCOVERED THAT THE LT OTBD FLAP JACKSCREW FAIRING WAS DAMAGED, WITH A PIECE MISSING. MAINTENANCE PERSONNEL CYCLED THE FLAPS AND DISPATCHED THE ACFT UNDER CDL TO A MAINTENANCE FACILITY WHERE THE FAIRING WAS REPLACED.SDR SWAA2013020412263Flap · delaminatedDELAMINATION ON INBOARD EDGE OF OUTBOARD AFT FLAP RIGHT WING. REMOVED AND REPLACED O/B AFT FLAP RIGHT IAW AMM 27-51-39 STEPS ARE DOCUMENTED ON 357-335-02-02R AND MT 327-51-06 STEP 6ESDR SWAA2013013012146Skin · canningRIGHT WING TRAILING EDGE I/B FLAP UPPER SURFACE SKIN OIL CANNING. REMOVED AND REPLACED WEDGE IAW SRM.SDR REXA2013011500066Vane · chafedLEFT INBOARD FLAP VANE INBOARD LEADING EDGE CHAFED. REMOVED AND REPLACED IAW SRM 57-52-00.SDR REXA2013011500065Vane · chafedLEFT INBOARD FLAP VANE CENTER LEADING EDGE CHAFED. REMOVED AND REPLACED IAW SRM 57-52-00.SDR REXA2013011500064Vane · chafedRIGHT INBOARD FLAP VANE CENTER LEADING EDGE CHAFED. REMOVED AND REPLACED IAW SRM 57-52-00.SDR REXA2013011500063Vane · chafedRIGHT INBOARD FLAP VANE INBOARD LEADING EDGE CHAFED. REMOVED AND REPLACED IAW SRM 57-52-00.SDR USAA2013011400011Skin · debondedC1 CHECK - 5 FOOT AREA OF DISBONDING ON UPPER SURFACE OF RIGHT OUTBOARD FLAP TRAILING EDGE WEDGE BETWEEN 7 TO 12 FEET FROM INBOARD EDGE. REPLACED RIGHT OUTBOARD FLAP TRAILING EDGE WEDGE IAW A320 SRM 51-42-11 & AIRBUS DRAWING D57574280.SDR USAA2013011400010Flap · delaminatedC6 CHECK - DELAMINATION ON UPPER SURFACE OF RIGHT OUTBOARD FOREFLAP ASSEMBLY AT CENTER SECTION OF TRAILING EDGE WEDGE. REPLACED RIGHT OUTBOARD FOREFLAP ASSEMBLY IAW B737 AMM 27-51-37.SDR SWAA2013011411403Flap · delaminatedLEFT OTBD AFT FLAP IS SEPARATED ON T/E OTBD CORNER. REPAIRED LEFT OTBD T/E OTBD CORNER IAW SRM 51-70-10- 2R-0.SDR SWAA2013011411399Spindle · corrodedNR 2 SPINDAL HAS INDICATIONS COATING FLAKING. REMOVED AND REPLACED NR 2 SPINDAL AS PER MT 327-51-08 AND MT 327-51-06 SEE CARDS FOR INDIVIDUAL SIGN OFF.SDR SWAA2013011411398Spindle · corrodedRIGHT WING NR 8 CARRIAGE SPINDLE HAS EVIDENCE OF CORROSION. REMOVED AND REPLACED NR 8 SPINDLE AS PER MT 327-51-07 AND MT 327-51-06 SEE CARDS FOR INDIVIDUAL SIGN OFF.SDR AALA20130109013Skin · dentedHAIL DENT IN TOP SKIN OF INBOARD MAIN FLAP 27 INCHES FROM OUTBOARD END. ACCOMPLISHED BONDED REPAIR PER SRM 51-70-10.SDR REXA2013010900130Plate · chafedINBOARD GUIDE PLATE ON INBOARD AFT HINGE FAIRING ON RIGHT OUTBOARD FLAP HAS CHAFE DAMAGE. REMOVED AND REPLACED INBOARD GUIDE PLATE ON INBOARD AFT HINGE FAIRING WITH NEW UNIT IAW CRJ 200 SRM 51-42-06-00.SDR IPXA3176791Skin · gougedINSPECTION TYPE: 10YR, RT WING OTBD FLAP INBD END BULLNOSE HAS A GOUGE. ACCOMPLISHED REPAIR IAW SRM 57-50-00, PARA 4H, FIG 208.SDR AALA20130108003Skin Panel · damagedLEFT WING INBOARD MAIN FLAP, UPPER SKIN PANEL 113N2401 IS MISDRILLED IN 2 LOCATIONS, MF STATIONS 145.5 AND 209. INSTALLED FREEZE PLUGS PER REO-G15813 REVISION A. INSTALLED FASTENERS THROUGH FREEZE PLUGS AND COMPLETED REPAIR PER EA B757-57-027773.SDR SWAA2013011011344Skin · delaminatedDELAMINATION UPPER AND LOWER SKIN ON I/B AFT FLAP LEFT SIDE. REMOVED AND REPLACED AFT FLAP LEFT SIDE I/B IAW AMM 27-51-11.SDR USAA2013010700012Strut · wornC9 CHECK - LEFT WING FLAP INTERCONNECT STRUT WORN AT Z581. REPLACED LEFT WING FLAP INTERCONNECT STRUT AT Z581 IAW A319 AMM 27-51-44-000-001-A.SDR IPXA13673310Wedge · dentedLT INBD AFT FLAP T/E WEDGE DENTED.SDR IPXA3576784Skin · dentedINSPECTION TYPE:C, LT INBD MAIN FLAP DENT 48" INBD OF OTBD EDGE 22" FWD OF T/E UPPER SUR FACE REF I477607, REPAIRED IAW SRM 51-70-10 REPAIR 3 AND 4 FIG 201. MAJOR REPAIR.SDR SWAA2013011711511Fairing · crackedRIGHT WING FLAP - NR 3 HINGE LWR FAIRING - LWR END CRACKED. SANDED CLEANED PREPARED & PAINTED RIGHT WING FLAP NR 3 HINGE LWR FAIRING AS REQUIRED IAW B717 AMM 51-10-00.SDR SWAA2013011011326Skin · puncturedRIGHT WING I/B FORE FLAP UNDER SURFACE PUNCTURED. REPAIRED FORE FLAP IAW SRM.SDR SWAA2013010911278Flap · delaminatedRIGHT WING O/B AFT FLAP I/B END DELAMINATED. REMOVED, REPLACED, ADJUSTED AND OP'S TEST GOOD ON RIGHT O/B AFT FLAP IAW MM 27-51-39-404-002. (POS:RT; P/N OFF:65-46435-334; S/N OFF:2268; P/N ON: 65-46435-370; S/N ON:2424)SDR SWAA2013010311063Flap · delaminatedRIGHT OUTBOARD AFT FLAP DELAMINATED. REMOVED AND REPLACED RIGHT O/B AFT FLAP PER M/M.SDR SWAA2013010311062Skin · delaminatedLEFT OTBD AFT FLAP DELAMINATED IN SEVERAL AREAS UPPER AND LOWER SURFACES. REMOVED AND REPLACED LEFT O/B AFT FLAP IAW AMM.SDR QXEA2012123101739Flap Track · damagedRT WING NR 4 FLAP TRACK INBD WEB HAS 2 AREAS SHOWING WEAR. BLENDED DAMAGE IAW RD 8/4-57-1238. HFEC SHOWS CRACK FREE. REMAINING MATERIAL WITHIN LIMITS. VERIFIED RIG OF THE FLAPS IAW AMM 27-54-06-400-801.SDR IPXA12576574Skin · dentedLEFT WING OTBD T/E AFT FLAP DENTED. REPAIRED IAW EO B757-5750-49452-A.SDR IPXA12576573Skin · dentedLT WING OTBD T/E AFT FLAP DENTED. REPAIRED IAW EO B757-5750-49452-A.SDR SWAA2013011611475Skin · crackedNR 3 FLAP TRACK FAIRING INNER SKIN CRACKED. REPAIRED SKIN PER EA.SDR IPXA13M76683Vane · chafedINSPECTION TYPE: 3C, CHAFE DAMAGE ON RT INBD FLAP VANE UPPER SURFACE T/E NEAR XIFH138. REPAIRED IAW SRM 57-50-80, REPAIR 2, WET LAY-UP. MAJOR REPAIRSDR USAA2013011500004Flap · damagedC4 CHECK - FIBER DAMAGE ON RIGHT OUTBOARD FLAP LOWER TRAILING EDGE BETWEEN DTEF265.88 TO DTEF267.88. REPAIRED RIGHT OUTBOARD FLAP LOWER TRAILING EDGE BETWEEN DTEF265.88 TO DTEF267.88 IAW B767 SRM 51-70-06-0G, REPAIR A, FIG. 9.SDR QXEA2012122901738Flap Track · wornRIGHT WING NR 3 LOWER FLAP TRACK AFT SURFACE IS WORN. REMOVED TRACK IAW RD 8/4-52-1511. BLENDED AREA. HFEC CRACK FREE. REPAIR WITHIN LIMITS. INSTALLED, VERIFY RIGGING OF FLAPS, REINSTALLED REMOVED PANELS.SDR SWIA201232508Skin · chafedLEFT INBOARD FLAP VANE LEADING EDGE CENTER PANEL CHAFE OUT-OF-LIMITS. (C-CHECK) REPLACED LEFT INBD FLAP VANE MID LEADING EDGE SKIN PANEL IAW SRM.SDR USAA2013013100001Flap · corrodedQ6 CHECK - CORROSION ON LEFT INBOARD FORE FLAP BETWEEN WBL 191 TO WBL 71.24. REPLACED LEFT INBOARD FORE FLAP IAW B737 AMM 27-51-07-004-001 & 27-51-07-404-010.SDR SWIA201232504Skin · chafedRIGHT INBOARD FLAP VANE LEADING EDGE CENTER CHAFE OUT-OF-LIMITS. (C-CHECK) REPLACED RIGHT INBD FLAP VANE LEADING EDGE CENTER SKIN IAW SRM.SDR WX0A071455Skin · chafedRIGHT WING I/B FLAP O/B VANE HAS 2 EA CHAFES ON UPPER SKIN AT I/B END. CUT OUT DAMAGED AREA. FABRICATED REPAIR FILLER AND DOUBLER AND INSTALLED REPAIR PARTS.SDR FDEA201212244367Skin · delaminatedRIGHT WING INBD LOWER FLAP T/E MID SECTION FOUND DELAMINATED. REMOVED DELAMINATED DOUBLER & DAMAGED HONEYCOMB CORE IAW SRM 57-52-12/201. MADE NEW SKIN DOUBLER IAW SRM 57-52-12/201. MADE HONEYCOMB CORE PLUG SRM 57-52-12/201. INSTALLED HONEYCOMB CORE PLUG ANSDR FDEA201212244368Skin · delaminatedLEFT WING OTBD FLAP T/E LOWER SURFACE FOUND DELAMINATED, FROM INBD TO OTBD 2000 MM, DIM:16" X 7". REMOVED DELAMINATED LOWER SKIN IAW SRM 57-53-12/201. MADE NEW SKIN DOUBLER IAW SRM 57-53-12/201. FILLED THE HONEYCOMB CORE WITH COMPOUND IAW SRM 57-53-12/201. SDR UIEA2012122400562Skin · damagedDURING POST FLIGHT WALK-AROUND INSPECTION, PUNCTURE DAMAGE APPROX 4.5" BY 2.5" WAS FOUND ON THE LOWER SURFACE OF THE L/E OF THE RIGHT WING INBD AFT FLAP. PERFORMED A TIME LIMITED REPAIR.SDR SWAA2012122610866Skin · delaminatedLEFT WING O/B TRAILING EDGE FLAP IS DELAMINATED ON LOWER SURFACE. REMOVED AND REPLACED OUTBOARD AFT FLAP AS PER AMM.SDR SWAA2013010711207Stiffener · crackedSTIFFENER CRACKED AT I/N SIDE OF FLAP TRACK FAIRING NR 6 TRAILING EDGE AREA RIGHT WING. REMOVED AND REPLACED TIFFENER IAW SRM AND DWG.SDR AALA20130104004Flap · delaminatedRIGHT OUTBOARD AFT FLAP DELAMINATED INBOARD CORNER. TRIMMED OUT DELAMINATION AND FILLED EXPOSED CORE WITH BMS 5-45 SEALANT (PR-1776M B2) PER SRM 57-53-01-1A 4.SDR SWAA2012122710893Fitting · corrodedRIGHT WING NR 8 FLAP TRACK REAR SPAR FITTING HAS CORROSION AT O/B HOLE. REMOVED, LOCATED, AND INSTALLED NEW REPLACEMENT IAW SRM 57-20-90, OHM 20-50-03.SDR SWAA2012122110815Support Angle · crackedRIGHT WING INBOARD MID FLAP FIXED WING PANEL HAS A CRACK AFT RIGHT CORNER. MARKED IN RED. REMOVE AND REPLACE SUPPORT ANGLE PER SRM 51-40-02.
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