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 TRAX200701565Bracket · crackedLEFT INBOARD FLAP 2 OMEGA BRACKET CRACKED ON FLAP BEAM RIB 5.SDR ASAA0782131Vane · gougedLEFT WING O/B FLAP I/B VANE GOUGED ON L/E AREA MARKED. REMOVED PREVIOUS REPAIR DOUBLER, PREPARED AREA, FABRICATED REPAIR DOUBLER BONDED AND INSTALLED FASTENERS IAW MD 80 SRM 51-70-2 PG 11 23 PAR 10C PG 32 AND PAR 18B PG 91.SDR ASAA0782129Vane · dentedRIGHT WING I/B FLAP I/B VANE LWR SURFACE HAS GRAVEL DAMAGE (DENTED). PREPARED DAMAGED AREA, FABRICATED FILLER AND REPAIR DOUBLER BONDED AND INSTALLED FASTENERS IAW MD80 SRM 51-70-2 PGS 23, 43, 46, 59, 63 AND 64.SDR USAA920071116Skin · debondedMCN - MAJOR REPAIR - C20 CHECK - LEFT WING OUTBOARD FOREFLAP HAS AREA DEBONDED, WS 206.5 - WS 214.5. REPAIRED LEFT WING OUTBOARD FOREFLAP, WS 206.5 - WS 214.5 IAW B737 SRM 51-70-10-2R4.SDR WRLA2007114Rib · crackedDURING 4C+12A CHECK, FOUND LT OUTBOARD FLAP NR 2 STOP FITTING CRACKED REF EGAT NRC U05061. PERFORMED BOEING SERVICE BULLETIN MD11-57-075, REPLACED DAMAGED RIB REV 00.SDR WRLA2007115Rib · crackedDURING 4C+12A CHECK, FOUND RT OUTBOARD FLAP NR 2 STOP FITTING CRACKED. REF EGAT NRC U05062. PERFORMED BOEING SERVICE BULLETIN MD-11-57-075, REPLACED DAMAGE RIB REV 00.SDR ASAA0782127Vane · delaminatedLEFT INBOARD FLAP OUTBOARD FLAP VANE DELAMINATED ON UPPER SURFACE 53 INCHES FROM OUTBOARD END. PREPARED DAMAGED AREA, FABRICATED FILLER AND DOUBLER REPAIR PARTS, LOADED AND INSTALLED FASTENERS IAW MD 80 SRM 51-70-2 PAT 18B PGS 91 95.SDR SWAA075195Skin · delaminatedDURING SCHEDULED 14Y CHECK, FOUND RT WING OUTBOARD FORE FLAP INBOARD END DELAMINATED. REPAIRED FLAP PER SRM.SDR SWAA075177Skin · delaminatedDURING SCHEDULED HC2 CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD END. REPAIRED FLAP PER SWA EA.SDR SWIA200719164Structure · crackedLEFT OUTBOARD FLAP IS CRACKED ALONG TRAILING EDGE, FOUND AT C-CHECK. REPLACED FLAP ASSEMBLY PER CRJ200 AMM 27-54-05-400-801.SDR UIEA200700458Structure · damagedDAMAGE WAS FOUND TO THE I/B END OF THE LT O/B MID FLAP. THE DAMAGE IS DUE TO CONTACT OF THE MID FLAP WITH THE FIXED STRUCTURE ADJACENT TO THE I/B AILERON. REPAIRED IAW XEO 57-101507-1.SDR SWAA075129Flap · delaminatedDURING SCHEDULED MV2 CHECK, FOUND LEFT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED FLAP PER MM.SDR SWAA075136Flap · delaminatedDURING SCHEDULED BRDG CHECK, FOUND LEFT WING OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD END. REPAIRED FLAP PER SRM.SDR SWAA075145Flap · delaminatedDURING SCHEDULED BRDG CHECK, FOUND LEFT WING INBOARD FOREFLAP DELAMINATED. REMOVED AND REPLACED FLAP PER MM.SDR 07FDEA04637Skin · delaminatedLT OUTBOARD AFT FLAP, T/E INBOARD CORNER IS DELAMINATED REPAIRED LT OUTBOARD AFT FLAP T/E CORNER REF SRM 51-40-20 PARA 6, 7, 19, -21. THIS IS CLASSIFIED AS A MAJOR REPAIR.SDR S9BA200700021Skin · corrodedRT TRAILING FLAP SKIN CORRODED AT ATTACHMENT HINGE FITTING. REMOVED AND REPLACED RT TRAILING FLAP.SDR SWAA075108Wedge · delaminatedDURING SCHEDULED 18Y CHECK, FOUND RIGHT WING INBOARD MID FLAP T/E WEDGE LOWER SURFACE DELAMINATED. REMOVED AND REPLACED WEDGE PER MM.SDR 07FDEA04607Skin Panel · corrodedFOUND CORROSION ON RT TOP SKIN ON WHOLE AREA AROUND FASTENER HOLES. REPAIR PERORMED BY BLENDOUT CORROSION, OVERSIZING THE HOLES AND FLAP PEENING IAW EA 6-5720-112522 AND RAS/BAE/1005287/2007 ISS A.SDR 07FDEA04606Support Fitting · crackedCRACK FOUND DURING HFEC OPEN HOLE INSPECTION ON THE MOST OUTBOARD, LOWER FASTENER HOLE COMMON TO THE ARC4008 AND ARC4009 LEFT OUTBOARD FLAP SUPPORT FITTING. 10-30-07 REMOVED AND REPLACED AS PER MD11 CMM 57-52-04. FLAP ADJUSTMENT TEST CARRIED OUT AS PERSDR 07FDEA04605Support Fitting · crackedCRACK FOUND DURING HFEC OPEN HOLE INSPECTION ON THE MOST OUTBOARD, LOWER FASTENER HOLE COMMON TO THE ARC4008 AND ARC4009 RIGHT WING OUTBOARD FLAP SUPPORT FITTING. 10-30-07 REMOVED AND REPLACED AS PER MD11 CMM 57-52-04. FLAP ADJUSTMENT TEST CARRIED OUT SDR DHL2007801501Structure · brokenLT INBD FLAP UPPER PLATING BROKEN 1" STA XW 106.000. PERFORMED MAJOR REPAIR IAW SRM 57-7-1 FIG 1 PG 2. REMOVED DAMAGED PLATING IAW SRM 57-1-0 PG 1, SRM 51-1-21. FABRICATED NEW PLATING (AL2024T3 0.040") IAW SRM 57-7-1 FIG 1 PG 2 ITEM D. CLEANED, TREATED ANDSDR NWAA073506303Web · crackedDURING "L" CHECK, FOUND CRACK IN LT WING INBOARD TRAILING EDGE FORE FLAP OUTBOARD WEB ASSEMBLY AT WBL 442.0. REPAIRED PER EA 63-210880.SDR AMTA200700503Skin · damagedLT WING AFT FLAP LOWER SURFACE HAS MULTIPLE DENTS AND DINGS. REPAIRED IAW SAA EA 737-5753-09-A1150, INTERM REPAIR REINSPECT EVERY 3500 FLIGHT HOURS OR 24 MONTHS WHICHEVER COMES FIRST IAW ATA ERA 737-57R-6171. (K)SDR AMTA200700502Skin · damagedRT WING IB AFT FLAP LOWER SURFACE HAS MULTIPLE NICKS AND GOUGES IN MLG TIRE PATHWAYS. REPAIRED IAW SAA EA 737-5753-09-A1150 INTERM REPAIR REINSPECT EVERY 3500, FLIGHT CYCLES OR 24 MONTHS WHICHEVER COMES FIRST IAW ATA ERA 737-57R-6170 1405-523. (K)SDR 07FDEA04585Skin · delaminatedRIGHT WING INBOARD FOREFLAP UPPER SURFACE DELAMINATED 72" FROM INBOARD EDGE. REPAIRED SURFACE DELAMINATION REF SRM 51-40-20 PARA'S 7, 14, 15, 19, 20, 22 TAP TEST GOOD. THIS IS CLASSIFIED AS A MAJOR REPAIR. PRIMED AND PAINTED REPAIR AREA REF M/M 51-20-151-7.SDR SWAA075072Skin · delaminatedDURING SCHEDULED 18Y CHECK, FOUND RIGHT WING INBOARD FORE FLAP UPPER SURFACE DELAMINATED. REPAIRED FORE FLAP PER SRM.SDR SWAA075074Skin · delaminatedDURING SCHEDULED 8Y CHECK, FOUND RIGHT WING OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD T/E. REPAIRED FLAP PER SRM.SDR AMTA200700492Panel · dentedIB REMOVABLE PANEL ON LWR SURFACE OF LT WING IB MAINFLAP IS DENTED (3) AREAS. REPAIRED IAW SAA EA 757-5753-09-A1012. (K) PRIMED REPAIR AND BONDING SURFACES AS REQUIRED BY EA. (M)SDR AMTA200700489Wedge · damagedSAA, INSPECTION FOUND NUMEROUS DENTS, CRACKS AND PUNCTURES ON THE RT IB AFT FLAP WEDGE LOWER SKIN PN 133A2700-18. REPAIRED IAW EA`S 737-5753-09A1099 AND 737-5753-09A1098. REPAIR IS INTERIM AND REQUIRES RE-INSPECTION EVERY 3500 FLIGHT CYCLES OR 24 MONTHS WHICSDR AMTA200700488Wedge · puncturedINSPECTION FOUND NUMEROUS DENTS, CRACKS AND PUNCTURES ON THE LT IB AFT FLAP TRAILING EDGE WEDGE LOWER SKIN PN 113A2700-17. ACCOMPLISHED REPAIR IAW SAA EA 737-5753-09-A1098. (M)SDR 07FDEA04578Support Bracket · corrodedRIGHT WING, OUTBOARD FLAP INBOARD HINGE AFT FAIRING SUPPORT OUTBOARD LOWER MOUNTING BORE FOUND CORROSION. 10-24-07 REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-116494. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.SDR 07FDEA04722Skin · delaminatedLT WING, FLAP INBD W/ DBONDS AT THE T/E BETWEEN RIB 2 AND RIB 8 REPLACE TRAILING EDGE IAW FEDEX EA 6-5710-115293.SDR USAA920071093Support Angle · crackedMIA - MAJOR REPAIR - C-2 CHECK - LEFT WING TRAILING EDGE OUTBOARD FLAP INBOARD EDGE AFT SUPPORT ANGLE CRACKED, WS 355. REPLACED LEFT WING TRAILING EDGE OUTBOARD FLAP INBOARD EDGE AFT SUPPORT ANGLE CRACKED, WS 355 IAW B767 SRM 51-40-02.SDR 2007UALA04198Skin · damagedON ARRIVAL FOUND DAMAGE AT LEFT INBOARD T/E FLAP LOWER SKIN BY 2.5 INCH X 1 INCH DENT AND 2.5 U-SHAPE CRACK AND 1.25 INCH IN SIDE DENT. DENT IS 5 INCHES FROM T/E SIDE FASTENER AND 11 INCHES FROM L/E FASTENER. ALSO, 17.5 INCH FROM FLAP L/E AND 20 INCHES FROM SDR SWAA075049Flap · delaminatedDURING SCHEDULED HC2 CHECK, FOUND LEFT WING OUTBOARD FOREFLAP DELAMINATED AT INBOARD END. REMOVED AND REPLACED FLAP PER MM.SDR SWAA075046Skin · delaminatedDURING SCHEDULED 18Y CHECK, FOUND RIGHT WING INBOARD FOREFLAP DELAMINATED AT UPPER SURFACE. REPAIRED FLAP PER SRM.SDR SWAA075050Flap · delaminatedDURING SCHEDULED BRDG CHECK, FOUND LEFT WING OUTBOARD MID FLAP INBOARD L/E DELAMINATED. REPAIRED FLAP PER SRM.SDR 07FDEA04572Skin · dentedLT WING INBOARD FLAP LOWER SURFACE FOUND DENTED. 10-29-07 REPAIR CARRIED OUT AT LT WING INBOARD FLAP LOWER SURFACE AS PER SRM 57-10-00 FIGURE 3 VOLUME I. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.SDR SWAA075033Skin · delaminatedDURING SCHEDULED C1 CHECK, FOUND LEFT WING INBOARD FOREFLAP UPPER SURFACE DELAMINATED. REMOVED AND REPLACED FLAP PER MM.SDR SWAA075032Skin · delaminatedDURING SCHEDULED C1 CHECK, FOUND RIGHT WING INBOARD FOREFLAP UPPER SURFACE DELAMINATED. REMOVED AND REPLACED FLAP PER MM.SDR 07FDEA04559Rib · crackedDURING COMPLIANCE WITH EO NR 6-5750-7-5000 P2, RIB 7 FLANGE WAS FOUND TO BE CRACKED COMPLIANCE WITH EO NR 6-5750-7-5000 P4. REPLACEMENT OF DAMAGED RIB 7.SDR 07FDEA04558Rib · crackedDURING COMPLIANCE WITH EO NR 6-5750-7-5000 P2, RT INBD FLAP RIB 25 WAS FOUND TO BE CRACKED IN UPPER RADIUS REPLACEMENT OF DAMAGED PART.SDR 07FDEA04557Rib · crackedDURING COMPLIANCE WITH EO NR 6-5750-7-5000 P2, RT INBD FLAP RIB 25 WAS FOUND TO BE CRACKED IN UPPER RADIUS REPLACEMENT OF DAMAGED PART.SDR 07FDEA04723Skin · debondedRT WING INBD FLAP T/E W/ VARIOUS DEBONDS TRAILING EDGE WAS REPLACED IAW SRM 51-72-10 AND EA 6-5710-115293.SDR SWAA075022Flap · delaminatedDURING SCHEDULED HC1 CHECK, FOUND LEFT WING OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD END. REMOVED AND REPLACED FLAP PER MM.SDR 07FDEA04537Skin · delaminatedRIGHT WING INBOARD FOREFLAP UPPER SURFACE DELAMINATED 96" FROM INBD EDGE. REPAIR SURFACE DELAMINATION REF SRM 51-40-20 PARA'S 7, 14, 15, 19, 20, 22. TAP TEST GOOD PRIMED AND PAINTED REPAIR AREA, REF MM 51-20-151-7. THIS IS CLASSIFIED AS A MINOR REPAIR.SDR 07FDEA04536Skin · gougedRIGHT WING INBOARD FORE FLAP UPPER SURFACE GOUGE, 93" FROM INBOARD EDGE. REPAIR SURFACE DELAMINATION REF SRM 51-40-20 PARA, S 7, 14, 15, 19, 20, 22 TAP TEST GOOD. PRIMED AND PAINTED AREA REF MM 51-20-151-7. THIS IS CLASSIFIED A MINOR REPAIR.SDR 2007UALA04151Flap · gougedLT INBOARD FORE FLAP INBOARD EDGE HAS GOUGES CREATED BY TOO LONG OF SCREWS INSTALLED IN UPPER FIXED PANEL. FOUND IMPROPER SCREW LENGTH INSTALLED IN PANEL ABOVE DAMAGED FLAP. REMOVED LT INB FORE FLAP AND SENT TO SHOP FOR REPAIR. A/C RECEIVED A ROBBED FLAP FROSDR UIEA200700433Wedge · damagedLT INBD TRAILING EDGE FOREFLAP DAMAGED. THE DAMAGE IS 10 FOOT LONG PIECE MISSING FROM THE T/E WEDGE. THE PIECE MISSING VARIES FROM 0.5" WIDE AT O/B END, AND IS 1.0" WIDE AT I/B END (LAST 4") AND IS 9 FEET I/B FROM I/B EDGE. IT IS BELIEVED THIS DAMAGE HAS BESDR 07FDEA04524Carriage · damagedSPLIT FLAPS OUTBOARD ON DEPARTURE. COMPLIED WITH QRH FLAPS WOULD NOT RETRACT VIA ALTERNATE METHOD. CREW DEBRIEFED OUTBD FLAPS STAYED AT 5 DEG WHILE INBD FLAPS CAME TO 2 DEG AS COMMAMDED. L/E VALVE C/B ON P6 PANEL PULLED BY CREW AS PART OF QRH. REF WRI 27-
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