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 ASAA0946223Skin · dentedLEFT I/B TRAILING EDGE WEDGE LOWER SKIN HAS TWO DENTS AT 19 INCHES, 19.8 INCHES FROM I/B END 4.5 INCHES, 5 INCHES FROM TRAILING EDGE. REMOVED DAMAGED AREA, FABRICATED, TREATED, PRIMED AND BONDED DOUBLER AND FILLER REPAIR.SDR ASAA0946222Skin · nickedLEFT I/B TRAILING EDGE WEDGE PNL LOWER SKIN NICKED 44.5 INCHES FROM I/B END 5 INCHES FROM TRAILING EDGE. PREPPED DAMAGED AREA, FABRICATED, TREATED, PRIMED AND BONDED DOUBLER AND FILLER REPAIR.SDR CA090909004Skin · chafedFLAP SKIN PN 101-160001-3 CHAFED DUE TO CONTACT WITH RAISEBECK WING LOCKER. PROBABLY DUE TO IMPROPER SHIMMING OF LOCKER ASSY.SDR IPXA09156899Doubler · gougedINSPECTION TYPE:3/C REPAIR SURVEY SEQ 146-W3-01 ON LEFT WING CENTER FLAP UPPER SKIN DOUBLER REPAIR IS GOUGED. FABBED AND INSTALLED REPAIR DOUBLER IAW EO A300-5750-34432-A AND SAA EA 300-5753-01-A1929.SDR IPXA09656862Wedge · misrepairedINSPECTION TYPE:C LT WING O/B TRAILING EDGE FLAP TRAILING EDGE WEDGE LOWER SURFACE I/B AREA THE EXISTING REPAIR PATCH NON-STANDARD REPAIR. COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-07 PAR 5G FIG 14 REV 44. THIS IS CLASSIFIED AS MAJOR REPAIR WITHSDR IPXA09656859Wedge · misrepairedINSPECTION TYPE:C LT WING O/B TRAILING EDGE FLAP T/E WEDGE LOWER SURFACE I/B AREA THE EXISTING REPAIR PATCH NON-STANDARD REPAIR. COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-07 PAR 5G FIG 14 REV 44. THIS REPAIR CLASSIFIED AS MAJOR REPAIR WITH MATERSDR IPXA09656854Wedge · misrepairedINSPECTION TYPE:N/A LT WING O/B TRAILING EDGE FLAP TRAILING EDGE WEDGE LOWER SURFACE I/B AREA THE EXISTING REPAIR PATCH NON-STANDARD REPAIR. COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-07 PAR 5G FIG 14 REV 44. THIS REPAIR IS CLASSIFIED AS MAJOR RESDR SWAA094601Flap · delaminatedDURING SCHEDULED SPV CHECK, FOUND RT WING O/B TRAILING EDGE FLAP DELAMINATED. REPAIRED FLAP PER MM.SDR USAA2009081292095Flap · debondedMCN - C22 - MAJOR REPAIR - DEBONDED LEFT INBOARD FORE FLAP AT WBL 117.63 TO WBL 121.38. REPAIRED LEFT INBOARD FORE FLAP AT WBL 117.63 TO WBL 121.38 IAW B737-300 SRM 51-70-102R3.SDR IPXA09156898Skin · chafedINSPECTION TYPE:3/C LT WING CENTER FLAP UPPER SKIN CHAFED, APP 24 INCHES ABOVE RUB STRIP NR 4 FLAP TRACK. FABBED AND INSTALLED REPAIR DOUBLER IAW EO A300-5750-34429-A AND SAA EA 300-5753-01-A1939.SDR IPXA09656789Fitting · crackedINSPECTION TYPE:C LT WING I/B MAIN FLAP DRIVE ARM UPPER FITTING LWR FLANGE CRACKED, CRACK AT BOTH I/B & O/B FLANGE. LT WING I/B MAIN FLAP DRIVE ARM UPPER FITTING REPAIRED AS PER SRM 57-53-02-2R1 FIG 201 REV 44, THIS REPAIR IS CLASSIFIED AS MAJOR REPAIR WITH MSDR ASAA0946212Skin · dentedLT INBD FOREFLAP HAS NUMEROUS DENTS AT UPPER CHAMBER. BONDED .016 DOUBLER IAW SRM.SDR SWAA094622Flap · delaminatedDURING SCHEDULED MV2 CHECK, FOUND RT WING O/B TRAILING EDGE FLAP DELAMINATED. REMOVED AND REPLACED FLAP PER MM.SDR USAA2009081292094Flap · debondedMCN - C22 - MAJOR REPAIR - DEBONDED RIGHT OUTBOARD AFT FLAP AT WBL 412.88 TO WBL 414.38. REPAIRED RIGHT OUTBOARD AFT FLAP AT WBL 412.88 TO WBL 414.38 IAW B737-300 SRM 51-70-10-2R4.SDR IPXA09156910Skin · corrodedINSPECTION TYPE:3/C LT WING O/B FLAP, O/B STATIC WICK BASE CORRODED BETWEEN BASE AND FLAP SKIN. FABBED AND INSTALLED REPAIR DOUBLER IAW UPS EO A300-5750-34431-A AND A SAA EA 300-5753-01-A1937.SDR UIEA200900039Skin · delaminatedRT WING INBD MID FLAP UPPER SURFACE AT WBL 347.78 AND 22.0 INCHES FROM T/E HAS AN AREA OF 1.0 BY 1.0 INCH OF DELAMINATION. PERMANENT REPAIR ACCOMPLISHED IAW SRM 51-40-09, FIG. 5, SHEETS 3 AND 8. REF: EO 4757A484.SDR SWAA094628Flap · delaminatedDURING SCHEDULED MV2 CHECK, FOUND LT WING O/B TRAILING EDGE FLAP DELAMINATED. REMOVED AND REPLACED FLAP PER MM.SDR SWAA094568Flap · delaminatedDURING SCHEDULED CV CHECK, FOUND LT WING O/B TRAILING EDGE FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.SDR 2009FA0000629Skin · debondedDISBOND ON T/E OF LT INBD MAIN FLAP AT FLAP STA 237.88 TO 224.63.SDR IPXA09156869Structure · misrepairedINSPECTION TYPE:5YR REPAIR SURVEY SEQUENCE 161-W4-01 DOES NOT CORRELATE WITH SRM. REPAIRED IAW UPS EO A300-5750-34408-B AND SAA EA 300-5750-01-A1910.SDR IPXA09M56841Skin · misrepairedINSPECTION TYPE:1C REPAIR SURVEY SEQUENCE 271-W3-03 HAS EXISTING REPAIR AT LT WING I/B FLAP UPPER SKIN BETWEEN STA XIFH 213.050-219.550 DOES NOT CORRELATE TO MD-11 SRM VOL1 57-20-00 FIG 6. REMOVED EXISTING REPAIR, FABRICATED AND INSTALLED REPLACEMENT REPAIR ISDR IPXA09156852Skin · chafedINSPECTION TYPE:5YR RT WING MID TRAILING EDGE FLAP HAS SMALL ROUND CHAFE MARK AT CENTER OF FLAP TOP OF SKIN. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER IN REF TO EO A300-5750-34413-A AND EA 300-5753-01-A1930.SDR ASAA0946245Skin · dentedLEFT O/B FORE FLAP LOWER SKIN HAS DENT 43 INCHES FROM I/B END 5.2 INCHES FROM T/E. PREPPED DAMAGED AREA, FABRICATED, TREATED, PRIMED AND BONDED REPAIR DOUBLER.SDR ASAA0946244Skin · dentedRIGHT I/B FORE FLAP UPPER SURFACE HAS DENT. PREPPED AREA, FABRICATED, TREATED, PRIMED AND BONDED REPAIR DOUBLER.SDR ASAA0946243Skin · dentedRIGHT I/B FORE FLAP LOWER SURFACE DENTED 38 INCHES FROM I/B END 8 INCHES FROM T/E. PREPPED DAMAGED AREA, FABRICATED, TREATED, PRIMED AND BONDED REPAIR DOUBLER AND FILLER.SDR ASAA0946242Skin · dentedRIGHT I/B FORE FLAP LOWER SURFACE DENTED 14 INCHES FROM I/B END 5 INCHES FROM T/E. PREPPED DAMAGED AREA, FABRICATED, TREATED, PRIMED AND BONDED REPAIR DOUBLER AND FILLER.SDR ASAA0946234Skin · dentedRIGHT I/B FORE FLAP LOWER SURFACE DENTED 47 INCHES FROM I/B END AND 3 INCHES, 8 INCHES FROM T/E. PREPPED DAMAGED AREA, FABRICATED, TREATED, PRIMED AND BONDED REPAIR DOUBLER.SDR ASAA0946200Skin · dentedRIGHT T/E INBD AFT FLAP UPPER OTBD SURFACE HAS A DENT. BONDED .016 REPAIR DOUBLER IAW SRM 51 70 10 REPAIR 2.SDR ASAA0946199Skin · dentedRIGHT WING INBD AFT FLAP UPPER SURFACE AT WBL 100.5 DENTED 5 INCHES FWD OF T/E. BONDED .016 REPAIR DOUBLER IAW SRM 51 70 10 REPAIR 2.SDR CA090714005Attach Bracket · worn(CAN) DURING INSP, CRACKING AROUND ACTUATOR ATTACH BRACKET WAS FOUND ON RT OTBD FLAP. FLAP WAS REMOVED FOR REPAIR AND IT WAS INSPECTED FOR OTHER DAMAGE. INBD AFT FLAP ATTACH BRACKET WAS BADLY WORN FROM WASHER/BRG. FLAP ON LT SIDE WAS REMOVED TO INSPECT ITSDR IPXA09156870Strap · damagedINSPECTION TYPE:5YR REPAIR RT OUTBOARD FLAP P/N A57960650007, S/N FH1257 FOR AC 161UP. REPAIRED IAW EO A300-5750-34408-B AND SAA EA 300-5750-01-A1910.SDR IPXA09M56846Wedge · gougedINSPECTION TYPE:1C REPAIR SURVEY SEQ 271-W4-08 RT INBOARD FLAP T/E WEDGE GRINDING MARKS BETWEEN STA XIFH 183.300 AND XIFH 201.300. REMOVED RT INBOARD FLAP T/E WEDGE BETWEEN STA 183.300 AND 201.300. REPAIRED AND INSTALLED T/E WEDGE REF EO MD11-5750-34399-A, ESDR IPXA09M56843Skin · misrepairedINSPECTION TYPE:1C REPAIR SURVEY SEQUENCE 271-W4-09 EXISTING REPAIR AT RT WING I/B FLAP UPPER SKIN BETWEEN STA XIFH 133.900-140.600 DOES NOT CORRELATE TO MD-11 SRM VOL 1 57-10-00 FIG 33. REMOVED EXISTING REPAIR, FABRICATED AND INSTALLED REPLACEMENT REPAIR IAWSDR SWAA094460Flap · delaminatedDURING SCHEDULED 2HC1 CHECK, FOUND LT WING O/B AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.SDR AALA20090714TUL01Skin Panel · dented2 SMALL DENTS ON LEFT HAND INBOARD FLAP LOWER SIDE. REMOVED AND REPLACED LOWER SKIN ON PANEL PER ESO 80095.SDR FDEA200907142617Rib · chafedFOUND CHAFING MARKS ON RT INNER FLAP RIB 12, RIB 27 AND RIB 18-19 TOP AND BOTTOM SKIN. REPAIR PERFORMED BY BLEND OUT AT RIB 12 FRONT SPAR-STR.2.1 AND RIB 27, CUT OUT REPAIR IAW SRM 57-50-00 FIG 205 AT RIB 12-STR.2.1-2.2 TOP SKIN, CUT OUT REPAIR AT RIB 18- 19 SDR IPXA09156868Skin · gougedINSPECTION TYPE:5YR LT WING CENTER FLAP UPPER SKIN GOUGED, OUTBOARD OF NR 3 FLAP TRACK. FABBED AND INSTALLED REPAIR DOUBLER IAW EO A300-5750-34414-A, SAA EA 300-5753-01-A1926.SDR IPXA09156833Skin · gougedINSPECTION TYPE:5YR LT WING CENTER FLAP UPPER SKIN IS GOUGED, NR 4 FLAP TRACK. REMOVED DAMAGE AND FABRICATED AND INSTALLED REPAIR DOUBLER PER A300-600 SRM 57-50-00 PG 220 FIG 205.SDR ASAA0946226Skin · dentedLEFT I/B TRAILING EDGE AFT FLAP LOWER SKIN HAS A DENT AT 9.8 INCHES FROM I/B END 6 INCHES FROM TRAILING EDGE. PREPPED DAMAGED AREA, FABRICATED, TREATED, PRIMED AND BONDED EXTERNAL DOUBLER REPAIR.SDR FDEA200907132601Skin · crackedRT WING EXT SURFACE FOUND CRACK ON UPPER EXT SKIN OTBD FLAP. REPAIRED SKIN IAW SRM 57-10-00 FIG 85 VOL I.SDR FDEA200907132597Hinge Bracket · corrodedLT WING INBD FLAP AFT HINGE FITTING OTBD HINGE INBD PIVOT HOLE FOUND CORROSION. REPAIRED IAW EA 1-5750-132148.SDR FDEA200907132596Hinge Bracket · corrodedRT WING INBD FLAP AFT HINGE FITTING OTBD HINGE OTBD PIVOT HOLE FOUND CORROSION. REPAIRED IAW EA 1-5750-132149.SDR FDEA200907132595Hinge Bracket · corrodedRT WING INBD FLAP AFT HINGE FITTING OTBD HINGE INBD PIVOT HOLE FOUND CORROSION. REPAIR IAW EA 1-5750-132149.SDR FDEA200907132593Hinge Bracket · corrodedLT WING INBD FLAP AFT HINGE FITTING OTBD HINGE OTBD PIVOT HOLE FOUND CORROSION. REPAIRED IAW EA 1-5750-132148.SDR ASAA0946247Skin · damagedLEFT WING I/B FLAP T/E WEDGE HAS PUNCTURE AND DENT. PREPPED DAMAGED AREA, FABRICATED, TREATED, PRIMED AND BONDED REPAIR DOUBLER AND FILLER.SDR UIEA200900043Flap Track · damagedNR 5 FLAP TRACK RT SIDE SCRATCHED BY BROKEN CARRIAGE ROLLER. REPAIRED IAW EO T2009A57B-749 REV 00.SDR FDEA200907112584Skin · dentedLT WING EXT FOUND 2 EA DENTS ON INBD FLAP LOWER EXT. SKIN LWR PNL. 1): 0.75 INCH X 0.50 INCH MAX DEEP 0.070 INCH. 2): 0.50 INCH X 0.50 INCH MAX DEEP 0.060 INCH. REPAIRED AREA IAW SRM 57-00-01 FIG 4 SHT 2 VOL I.SDR FDEA200907112583Skin · dentedLT WING EXT FOUND 1 EA DENT .75 INCH X 1 INCH MAX DEEP .060 INCH ON INBD FLAP LWR EXT. SKIN LWR PANEL. REPAIRED AREA IAW SRM 57-00-01 FIG 4 SHT 2 VOL I.SDR QXEA2009071300528Skin · chafedTOP OF LT INBD FLAP HAS LIGHT CHAFE DAMAGE AT APPROX YW-50. REMOVED PAINT FROM CHAFE AREA AT YW-50 ON LT INBD FLAP IAW SRM 51-26-10-02-01 PARA 1-5D(14) AND 5F. BLENDED CHAFE IAW SRM 57-51-30-02-01 PARA 1-6B(5). HFEC INSP BLENDED AREA FOR CRACKS IAW NDTM PARTSDR QXEA2009071300527Skin · chafedTOP OF LT INBD FLAP HAS LIGHT CHAFE DAMAGE AT APPROX YW-60. REMOVED PAINT FROM CHAFE AREA AT YW-60 ON LT INBD FLAP IAW SRM 51-26-10-02-01 PARA 1-5D(14) AND 5F. BLENDED CHAFE IAW SRM 57-51-30-02-01 PARA 1-6B(5). HFEC INSP BLENDED AREA FOR CRACKS IAW NDTM PART
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