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 MALA070019Skin · damagedTHE RT FLAP TRAILING EDGE, APPROXIMATELY 9.0 INCHES FROM THE INBOARD END, IS DAMAGED. THE DAMAGE HAS BEEN REPAIRED IAW MESABA EO NR S57143. REF: EAMS WORK ORDER 217373 TASK 6501.SDR ASAA0741418Skin · dentedRIGHT I/B AFT FLAP UPPER SKIN DENTED. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED FILLER AND DOUBLER IAW SRM 51-70-10.SDR EIA2007024Fitting · corrodedFOUND NR 6 FLAP TRACK AFT ALIGNMENT FITTING WITH CORROSION ON SURFACE BETWEEN FITTING AND WING SKIN. HOLES WERE OVERSIZED AND SPOT FACED. REPAIR BUSHINGS INSTALLED PER BOEING MESSAGE 1-277661910-9.SDR DHL2007802513Angle · crackedLT OTBD FLAP "T" ANGLE CRACKED 1" STA XF 165.000. REMOVED CRACKED T ANGLE IAW SRM 51-1-21. FABRICATED NEW T-ANGLE (EXTRUSION P/N 1243286) IAW SRM 57-7-0 FIG 3, SRM 51-2-0 FIG 50. CLEANED, TREATED AND PRIMED AREA AND T-ANGLE IAW SRM 51-1-8B. INSTALLED T-ANGSDR DHL2007802512Angle · crackedRT OUTBD FLAP SHOWS "T" ANGLE WITH CRACK 1" AT STA XT 165.000. REMOVED CRACKED T-ANGLE IAW SRM 51-1-21. FABRICATED NEW T-ANGLE (EXTRUSION P/N 1213286) IAW SRM 57-7-0 FIG 3, SRM 51-2-0 FIG 50. CLEANED, TREATED AND PRIMED AREA AND T-ANGLE IAW SRM 51-1-8B. INSDR DHL2007802508Rib · crackedRT INBD FLAP RIB 1" CRACK STA XW 125.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1. REMOVED CRACKED RIB IAW SRM 51-1-21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW RIB IAW SRM 57-7-1 FIG 2 SHEET 4, SRM 51-1-21, SRM 51-SDR AMTA200700032Attach Fitting · chafedLEFT NR 2 FLAP OUTBOARD ATTACH FITTING WITH CHAFING. REPAIRED PER EER 12926 GAMCO WORKORDER 316063. (M)SDR AMTA200700031Attach Fitting · gougedGOUGE ON NR 3 FLAP LEFT INBOARD ATTACH FITTING. REPAIRED PER EER 12910 GAMCO WORKORDER 316063. (M)SDR AMTA200700030Attach Fitting · gougedRIGHT NR 1 FLAP OUTBOARD ATTACH FITTING HAS GOUGES. REPAIRED PER EER 12925 GAMCO WORKORDER 316063. (M)SDR AMTA200700029Attach Fitting · chafedRIGHT WING NR 1 FLAP INBOARD ATTACH FITTING WITH CHAFING MARK. REPAIRED PER EER 12929 GAMCO WORK ORDER 316063. (M)SDR AMTA200700028Attach Fitting · gougedRIGHT WING NR 3 FLAP INBOARD ATTACH FITTING UPPER SURFACE WITH GOUGE. REPAIRED PER EER 12928 GAMCO WORKORDER 316063. (M)SDR AMTA200700027Attach Fitting · gougedRIGHT WING NR 2 FLAP ATTACH FITTING TOP AREA WITH GOUGE. REPAIRED PER EER 12927 GAMCO WORK ORDER 316063. (M)SDR AMTA200700026Skin · chafedRIGHT WING NR 1 FLAP VANE ASSY FOUND DEEP CHAFING ALONG THE UPPER SKIN FROM INBOARD TO OUTBOARD OF VAN. REPAIRED PER EER 12978 GAMCO WORKORDER 316063. (M)SDR UPS07M49580Stop Fitting · crackedINSPECTION TYPE:C RIGHT WING O/B TRAILING EDGE FLAP UP-STOP CRACKED AS MARKED AT O/B FLAP I/B FLAP MOUNT HINGE AREA, LEADING EDGE AREA. ALL REMOVAL OF RIGHT WING O/B FLAP I/B & O/B SUPPORT CUT OUT PER AMM20-50-02 R5 R55 TO GAIN ACCESS TO REMOVE & RE-INSTALL NSDR UPS07M49579Fitting · crackedINSPECTION TYPE: C, LT WING O/B TRAILING EDGE FLAP UP-STOP FITTING CRACKED AS MARKED AT O/B FLAP I/B MOUNTED HINGE AREA, LEADING EDGE AREA. ALL REMOVAL OF LEFT WING O/B FLAP I/B & O/B SUPPORT CUT OUT PER AMM 20-50-02 R55 TO GAIN ACCESS TO REMOVE & RE-INSTALLSDR ASAA0741417Structure · dentedLT IB FORE FLAP HAS SEVERAL DENTS ON THE LOWER SURFACE. PREPPED DENTED AREAS FABRICATED AND INSTALLED A REPAIR DOUBLER IAW SRM 51 70 10.SDR ASAA0741406Flap · delaminatedLEFT OUTBOARD T/E FLAP IS SPLIT (DELAMINATED) AT INBOARD EDGE. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED FILLER AND DOUBLER IAW SRM 51-70-10.SDR AWXA200700108Access Panel · delaminatedSAL - MAJOR REPAIR - BC-4 CHECK - RIGHT WING OUTBOARD FLAP LEADING EDGE ACCESS PANEL DELAMINATED, BETWEEN RIB 5 AND RIB 6. REPAIRED RIGHT WING OUTBOARD FLAP LEADING EDGE ACCESS PANEL BETWEEN RIB 5 AND RIB 6 IAW AWA ER 25-5753-07021-SS1.SDR SWAA070300Skin · delaminatedDURING SCHEDULED 22Y CHECK, FOUND RIGHT WING INBOARD FORE FLAP UPPER SURFACE DELAMINATED AT OUTBOARD END. REPAIRED FORE FLAP PER SRM.SDR SWAA070299Wedge · delaminatedDURING SCHEDULED 22Y CHECK, FOUND RT WING INBOARD MID FLAP WEDGE LOWER SKIN DELAMINATED AT OUTBOARD END. REPAIRED MID FLAP WEDGE PER SRM.SDR SWAA070289Wedge · debondedDURING SCHEDULED C4 CHECK, FOUND RIGHT WING INBOARD MID FLAP T/E WEDGE DISBONDED AT OUTBOARD END. REMOVED AND REPLACED MID FLAP WEDGE PER MM.SDR CA070124003Roller · worn(CAN) PILOT REPORTED INTERFERENCE WITH AILERON CONTROL UPON APPROACH WHEN FLAPS WERE APPROXIMATELY 30 PERCENT. AIRCRAFT LANDED WITHOUT INCIDENT. INVESTIGATION REVEALED RT OB FLAP IB HINGE ATTACH BRACKET, PN 35-165050-31, FAILED AT THE AFT ROLLER ASSY ATTACH SDR SWIA200718018Brace · crackedRT NACELLE FLAP INTERNAL BRACING HAS A CRACK AT A STIFFENER. (DISCOVERED DURING C-CHECK INSPECTION) NEW STIFFENER INSTALLED IAW SRM 120 51-10-02 PG. 3 SEC. 3A.SDR IXXA07SMN034SSkin Panel · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT INBOARD FLAP SKIN PANEL HAS A NON STANDARD REPAIR FROM STATION XW104.000 TO STATION XW108.000. REMOVED SKIN PANEL WITH EXISTING NON STANDARD REPAIR. FABRICATED NEW SKIN PANEL AND INTERNAL BONDED DOUBLERS. BONDEDSDR IXXA07SMN033SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT OUTBOARD FLAP UPPER SKIN HAS A NON STANDARD REPAIR FROM STATION XF326.000 TO STATION XF333.000. REMOVED EXISTING NON STANDARD REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACKS OR CORROSION FOUNDSDR IXXA07SMN032SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND A NON STANDARD REPAIR ON THE LEFT OUTBOARD FLAP FROM STATION XF169.000 TO STATION XF174.000. REMOVED EXISTING SKIN PANEL WITH NON STANDARD REPAIR. FABRICATED NEW SKIN PANEL AND BONDED DOUBLER. BONDED BOTH PARTS WITH SDR IXXA07SMN035SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT INBOARD FLAP UPPER SKIN HAS A NON STANDARD REPAIR FROM STATION XW132.000 TO STATION XW135.000. REMOVED EXISTING SKIN WITH NON STANDARD REPAIR. FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AREA AND NEW SKIN ASDR 2007UALA00142Skin · delaminatedLEFT WING OTBD FORE FLAP INBD END DELAMINATED. MAJOR REPAIR: REPAIRED FLAP PER SRM 95-57-53-04 IN SHOP. REINSTALLED.SDR SWAA070280Wedge · delaminatedDURING SCHEDULED 10Y CHECK, FOUND LT WING INBOARD FORE FLAP T/E WEDGE DELAMINATED AT OUTBOARD L/E. REPAIRED FORE FLAP PER SRM.SDR SWAA070279Wedge · delaminatedDURING SCHEDULED 10Y CHECK, FOUND LT WING INBOARD FORE FLAP T/E WEDGE DELAMINATED AT INBOARD L/E. REPAIRED FORE FLAP PER SRM.SDR DHL2007802515Angle · crackedFOUND LT INBD FLAP T/E ANGLE 1.500" CRACK STA XW 129.000. REMOVED CRACKED REINFORCING ANGLE IAW SRM 51-1-21. FABRICATED NEW REINFORCING ANGLE (AL2024"0" 0.050") IAW SRM 57-7-1 FIG 2 SHEET 1. HEAT TREATED FROM "0" TO AL2024T4 IAW SRM 51-1-1 PG 1-13-17. CLEASDR DHL2007743502Skin · delaminatedRT IB TE FOREFLAP LOWER SKIN PRESENTS DELAMINATION APPROX AT WBL 210.0. CUT OUT DELAMINATED AREA APPROX 13" BY 15.5". FABRICATED FILLER APPROX 13" BY 15.5" AND DOUBLERS 2EA APPROX 3" BY 15.5" FROM 2024T3 .016 PO NR 9003189. CLEANED, PREPPED, BONDED, TREATEDSDR DHL2007788001Skin · debondedLT WING OUTBOARD AFT FLAP SHOW DISBONDED SPOT TEMPORARY REPAIR FROM TE OUTBOARD END. REMOVED DELAMINATED AREA APPROX 9.75" BY 3.8" (UPPER SKIN) AND 3" BY 8.6" (LOWER SKIN), CLEANED AND PREPPED REPAIR AREA TO BOND. FABRICATED UPPER FILLER (9.75" BY 3.9") UPPSDR KPVA20071Torque Tube · brokenFIRST FLAP DRIVE TORQUE TUBE CONNECTED TO FPU ON RIGHT SIDE IS BROKEN. REMOVED AND REPLACED RT FIRST FLAP DRIVE TORQUE TUBE IAW DHC-8 MM, CHAP 27-52-20 PG 201-209.SDR AWXA200700298Wedge · delaminatedMCN - FOUND RIGHT WING INBOARD MIDFLAP TRAILING EDGE WEDGE PANEL LOWER SURFACE DELAMINATED, WS 161.5 - WS 168. REPAIRED RIGHT WING INBOARD MIDFLAP TRAILING EDGE WEDGE PANEL LOWER SUFACE, WS 161.5 - WS 168 IAW B737-300 SRM 51-70-10-2R4.SDR AWXA200700139Wedge · delaminatedMCN - FOUND RIGHT WING INBOARD MID FLAP, LOWER SURFACE TRAILING EDGE WEDGE DELAMINATED, WS 116.8 - WS 124.0. REPAIRED RIGHT WING INBOARD MID FLAP, LOWER SURFACE TRAILING EDGE WEDGE, WS 116.8 - WS 124.0 IAW B737-300 SRM 51-70-10-2R4, REPAIR NR 4, FIGURE 202.SDR SWAA070245Torque Tube · corrodedDURING SCHEDULED 22Y CHECK, FOUND RT WING INBOARD MID FLAP INBOARD TORQUE TUBE CORRODED. REMOVED AND REPLACED TORQUE TUBE PER MM.SDR SWAA070244Torque Tube · corrodedDURING SCHEDULED 22Y CHECK, FOUND RT WING INBOARD MID FLAP OUTBOARD TORQUE TUBE CORRODED. REMOVED AND REPLACED TORQUE TUBE PER MM.SDR SWAA070243Torque Tube · corrodedDURING SCHEDULED 22Y CHECK, FOUND LT WING INBOARD MID FLAP OUTBOARD TORQUE TUBE CORRODED. REMOVED AND REPLACED TORQUE TUBE PER MM.SDR SWAA070242Torque Tube · corrodedDURING SCHEDULED 22Y CHECK, FOUND LT WING INBOARD MID FLAP INBOARD TORQUE TUBE CORRODED. REMOVED AND REPLACED TORQUE TUBE PER MM.SDR UPS07M49399Hinge · corrodedINSPECTION TYPE:C RIGHT WING O/B FLAP, I/B AFT HINGE FOUND PIVOT POINT BUSHINGS 2EA CORRODED. RIGHT AFT O/B FLAP I/B HINGE PIVOT POINT BUSHINGS REMOVED PER BSOPM 20-20 -7 R56. RIGHT AFT O/B FLAP I/B HINGE PIVOT BORE & SPOTFACE CORROSION REMOVED & FOUND EXCEESDR ASAA0741397Skin · dentedTHE LEFT WING TRAILING EDGE I/B FORE FLAP HAS A DING AT WBL 96.5. CUT OUT THE DAMAGED AREA ON THE LWR SKIN, FABRICATED AND INSTALLED A SKIN FILLER AND A REPAIR DOUBLER IAW SRM 51-70-10 PARA 7, 8, 11, 15, 18 AND 20.SDR ASAA0741396Skin · dentedTHE LEFT WING TRAILING EDGE I/B FORE FLAP LWR SURFACE IS DINGED AT WBL 126. REMOVED THE DAMAGED AREA OF LWR SKIN, FABRICATED AND INSTALLED A SKIN FILLER AND A REPAIR DOUBLER IAW SRM 51-70-10 PARA 7, 8, 11, 15, 18 AND 20.SDR ASAA0741395Skin · dentedTHE RIGHT WING TRAILING EDGE I/B FORE FLAP LWR SURFACE HAS MULTIPLE DENTS AND DINGS FROM WBL 101.5 - 121.5. REMOVED THE DAMAGED AREA OF LOWER SKIN, FABRICATED AND INSTALLED A SKIN FILLER AND REPAIR DOUBLER IAW SRM 51-70-10 PARA 7, 8, 11, 15, 18 AND 20.SDR ASAA0741393Skin · dentedTHE LEFT WING TRAILING EDGE I/B FORE FLAP LWR SURFACE HAS AN EXISTING REPAIR WITH MULTIPLE DENTS AND DINGS AT WBL 119. REMOVED THE EXISTING REPAIR DOUBLER AND DAMAGED AREA OF LWR SKIN FABRICATED AND INSTALLED A SKIN FILLER AND A REPAIR DOUBLER IAW SRM 51-70-1SDR 07FDEA00123Skin · delaminatedEXISTING REPAIR FOUND AT LT IN FOREFLAP UPPER SURFACE 91" FROM INBD END FOUND DELAMINATED. REMOVED OLD REPAIR AND REPAIRED AREA REF SRM 51-40-20 PGS 1-62 AND APPLIED EXTERIER PROTECTIVE FINISH REF MM 51-21-151-7 PGS 1-4. CLASSIFIED AS A MAJOR REPAIR.SDR 07FDEA00120Fitting · corrodedLT INB FLAP FOUND FITTING ITEM 665 WITH NR 3EA HOLES WITH CORROSION REF IPC 27-51-10-01 VIEW F. REMOVED SUPPORT IAW SRM 51-31-01 VOL 2 PAG 6-10. REMOVED CORROSION AND CORROSION LOCAL BLEND IAW SRM 51-21-01 VOL 2 PAR 34A AND IAW SRM 57-20-00 VOL 1 FIG 19. RESDR 07FDEA00099Structure · corrodedRIGHT WING OUTBOARD FLAP OUTBOARD HINGE OUTBOARD CENTER HOLE FOUND CORRODED. REPAIRED AS PER FEDEX E.A. 1-5750-107762, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.SDR 07FDEA00098Structure · corrodedRIGHT WING OUTBOARD FLAP OUTBOARD HINGE OUTBOARD AFT HOLE FOUND CORRODED. REPAIRED AS PER FEDEX EA 1-5750-107762, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.SDR 07FDEA00097Structure · corrodedRIGHT WING OUTBOARD FLAP INBOARD HINGE OUTBOARD AFT HOLE FOUND CORRODED. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-107761, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.
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