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 SWAA2012122610834Skin · wornRIGHT WING INBOARD FOREFLAP UPPER SKIN WORN THROUGH NEAR INBOARD END. REMOVED AND REPLACED FLAP.SDR SWAA2012122710869Flap · delaminatedRIGHT WING OUTBOARD AFT FLAP INBOARD AFT CORNER DELAMINATED. REPAIRED IAW SRM.SDR SWAA2013010711160Skin · delaminatedDELAMINATION ON UPPER SKIN THE AFT FLAP O/B LEFT WING. REPAIRED UPPER SKIN THE AFT O/B LEFT WING IAW B737-300 SRM 51-70-10-2R-0.SDR WVER201212149343Skin · dentedFOUND DENT ON LT INBD FLAP LOWER SKIN 2.5" FROM INBD EDGE OF SKIN , 12" FORWARD OF SKIN T/E. DENT MEASURES .056" DEEP. DENT WAS FOUND WHILE PERFORMING TASK CARD 000-57-580-302-A01.SDR DALA12016283210Rib · corrodedDURING INSPECTION, FOUND LT OTBD FLAP, INBD RIB L/E HAS 2 AREAS OF PITTING AFTER RUB STRIP REMOVAL. BLENDED CORROSION IAW SRM 51-74-00, AREA L 1 =1.5" W=1.0 "D =0.028"AREA 55"W=0.070" D=0.030". ACCOMPLISHED ER/A 508976-14 REV ORIGINAL SECTION I PERMANENT REPSDR SWAA2012121410669Spindle · faultyFLAPS 5 AIRCRAFT MADE UNUSUAL RUMBLE NOISE. REMOVED AND REPLACED SPINDLE IAW AMM.SDR SWAA2013021512723Flap · delaminatedON WALK-AROUND FOUND 1" DELAMINATION ON TRAILING EDGE OF OUTBOARD FT FLAP APPROX 12" FROM INBOARD END. REMOVED AND REPLACED LEFT OUTBOARD AFT FLAP. P/N: 65-46435-277 S/N OFF: BN-860 S/N ON: 966 L/H AFTSDR SWAA2012121310589Retainer · crackedLEFT WING AFT INBOARD FLAP OUTBOARD UPPER LEADING EDGE SEAL RETAINER IS CRACKED AT LOWER FASTENER HOLE. REMOVED AND REPLACED SEAL RETAINER PER MM.SDR SWAA2012121710732Plate · crackedLEFT WING NR 3 FLAP FAIRING DOOR SPRING CRACKED IN TWO PLACES ON EDGE. REMOVED AND REPLACED PLATE IAW SRM AND BOEING DRAWING.SDR DALA12016293210Carriage · gougedDURING INSPECTION, FOUND RT WING NR 1 FLAP TRACK, FLAP CARRIAGE FWD LOWER TRACK HAS GOUGE (2 EA). ACCOMPLISHED RT WING NR 1 FLAP TRACK, FLAP CARRIAGE FWD LWR TRACK REPAIR BY BLENDING AREA IAW SRM 51-73-00, OTBD L=1.400"W=.250"D =.003", INBD L=1.400"W=.250"D=SDR REXA2012121201736Skin · dentedLEFT INBOARD FLAP LOWER SKIN DENTED AT FLAP STATION 30.0 MEASURING 2.25 X 2.0 X 0.050" DEEP. REPAIRED IAW SRM 57-52-01 REPAIR 1, NON-FLUSH REPAIR.SDR USAA2012121000019Flap · delaminatedRON VISIT - 19 INCH BY 4 INCH WIDE AREA OF DELAMINATION ON LEADING EDGE OF RIGHT OUTBOARD FLAP AT WS 746. REPLACED RIGHT OUTBOARD FLAP LEADING EDGE PANEL IAW B767 AMM 27-51-20-401 & JOB CARD 12L66027001.SDR REXA2012121001544Flap · dentedLEFT INBOARD FLAP (P/N 601R14002-1, S/N SB/RJ/948) FOUND DENTED AT WS 60. REPAIRED IAW SRM 57-52-00 REPAIR 3.SDR QXEA2012120801624Flap Track · damagedLEFT WING NR 4 FLAP TRACK HAS AREAS OF CHIPPED TUNGSTEN CARBIDE COATING ON INBD VERTICAL WEB. BLENDED IAW RD 8/4-57-1238. MIN REMAINING THICKNESS NOTED .153, CONFIRMED AFFECTED AREA CRACK FREE REF NTM 51-00-04-910-801 PT 1 AND 51-00-06-910-801 PT 1. DAMAGE ISDR FDEA201212084268Skin · looseLEFT WING INBD FLAP UPPER SURFACE AT XIFH= 171 RIVETS FOUND LOOSE. REPAIRED IAW SRM 57-50-01 FIGURE 201 REPAIR 4 REVISION 51 AND EA 1-5750-163534 STEP 5 PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 115.SDR DALA1256390608Fairing · damagedLEFT FLAP INBD POSITION OTBD AFT FLAP TRACK FAIRING. CONFIGURED INCORRECT FOR NEW FLAP INSTALLED. REPLACED ATTACH FITTINGS IAW DWG 113N2383. INSTALLED FAIRING IAW AMM 27-51-30.SDR AALA20121217012Skin · damagedRIGHT WING INBOARD FLAP DENT IN BOTTOM SKIN 15 INCHES FROM INBOARD EDGE OF WEDGE. REMOVED AND REPLACED RIGHT INBOARD FLAP AFT WEDGE LOWER SKIN PER ESO 80095 AND SRM 51-01-00.SDR AALA20121217011Skin · damagedRIGHT WING INBOARD FLAP DENT IN BOTTOM SKIN 18 INCHES FROM INBOARD EDGE OF WEDGE. REMOVED AND REPLACED RIGHT INBOARD FLAP AFT WEDGE LOWER SKIN PER ESO 80095 AND SRM 51-01-00.SDR SWAA2012121010375Nut Plate · looseLOOSE BOLTS ON BALL SCREW FITTING AREA AT FLAP TRACK NR 7 RT WING. REPLACED NUT PLATES AND TIGHTENED BOLTS ON BALL SCREW FITTING AREA AT FLAP TRACK NR 7 RT WING IAW SRM 51-40-02.SDR USAA2012120700007Flap · delaminatedPREFLIGHT - RIGHT INBOARD AFT FLAP DELAMINATED AT TRAILING EDGE FOUR (4) INCHES INBOARD OF OUTBOARD END. REMOVED AND REPLACED AFT FLAP IAW B737-400 AMM 27-51-11-404-008.SDR UHLA2012120500044Torque Tube · corrodedCORROSION ON LEFT WING FLAP TORQUE TUBE F5. R & R LEFT WING FLAP TORQUE TUBE F5.SDR SWAA2012121810767Skin · crackedLEFT WING I/B FORE FLAP SIDE SKIN CRACKED. REPLACED FORE FLAP IAW SRM.SDR USAA2013010900010Strut · corroded2S CHECK - CORROSION ON RIGHT WING AFT FLAP INTERCONNECTING STRUT AT WS 4862, RIB 9. REPLACED RIGHT WING AFT FLAP INTERCONNECTING STRUT AT WS 4862, RIB 9 IAW A320 AMM 27-51-44-400-001-A.SDR USAA2013010900009Strut · corroded2S CHECK - CORROSION ON LEFT WING AFT FLAP INTERCONNECTING STRUT AT WS 4862, RIB 9. REPLACED LEFT WING AFT FLAP INTERCONNECTING STRUT AT WS 4862, RIB 9 IAW A320 AMM 27-51-44-400-001-A.SDR SWAA2012121310575Rib · crackedRIGHT WING RIB CRACKED AT TRAILING EDGE EXHAUST GATE I/B END OF O/B FLAP WBL 184.40. REPLACED RIB IAW SRM AND DWG.SDR SWAA2012120710359Fairing · crackedCRACK ON NR 2 FLAP TRACK FAIRING (AFT, ATTACHED TO CENTER FAIRING). REPAIRED NR 2 FLAP TRACK FAIRING (AFT, ATTACHED TO CENTER FAIRING) IAW SRM 51-70-17-0G-0 PARA 4I REP 9.SDR SWAA2012120710342Spherical Bearin · looseLEFT WING AFT FLAP I/B TRACK SPHERICAL BEARING IS LOOSE. REMOVED AND REPLACED BEARING PER M/M.SDR FDEA201212044245Skin · corrodedLT INBD FLAP, FRONT INBD PANEL HAS CORROSION. REMOVED CORROSION ON LT INBD FLAP INBD PANEL IAW-SRM-51-10-02. CHECK LIMIT ORIG MAT .125 MAT LOSS .030 FOUND OUT OF LIMIT IAW-SRM-57-53-01, FIG 101, DET VIII PG 106, WORK ACCOMPLISHED ON EA F-5750-162474. CAT "ASDR UALA2012120407000Support Fitting · gougedTHE NR 4 FLAP TRACK FWD SUPPORT FITTING HAS GOUGE IN THE OUTBOARD WEB AREA. (DAMAGE IS MARKED IN RED). BLENDED FITTING PER SRM 51-10-02. TREATED AND PRIMED BLENDED AREA. REF SEQ 7362040 FOR HFEC. ACPD CATEGORY 'B' REPAIR PER UA-EVA-80076.SDR USAA2013011000008Flap · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION AT 2 POINTS ON INTERNAL AREA BETWEEN INNER RIB & OUTBOARD RIB 14 ON LEFT WING OUTBOARD FLAP BETWEEN WS 486 TO WS 11664 & BETWEEN RIB 9 TO RIB 22. REPLACED LEFT WING OUTBOARD FLAP IAW A320 AMM 27-54-62.SDR USAA2013011000007Rib · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION AT 6 POINTS ON INTERNAL AREA OF OUTBOARD FACE OF RIB 15 ON LEFT WING OUTBOARD FLAP BETWEEN WS 486 TO WS 11664 & BETWEEN RIB 9 TO RIB 22. REPLACED LEFT WING OUTBOARD FLAP IAW A320 AMM 27-54-62.SDR UALA2012120406990Spar · damagedINTERIM REPAIR TO THE RIGHT INBD MAIN FLAP FRONT SPAR LWR CHORD AT MFS 223. REF ECRA 5750-04506.SDR IPXA2M76346Structure · damagedLEFT WING INBD FLAP DAMAGED. REPAIRED IAW EO MD11-5750-49242-A.SDR UHLA2012113000445Torque Tube · corrodedCORROSION ON LEFT WING FLAP TORQUE TUBE F6 AND BEARING SUPPORT F5/F6. R & R LEFT WING FLAP TORQUE TUBE F6 AND BEARING SUPPORT F5/F6.SDR WX0A071423Skin · chafedRIGHT O/B FLAP I/B VANE LEADING EDGE IS CHAFED AT I/B CORNER, 193A029 MARKED. REMOVED RIGHT WING O/B FLAP I/B FLAP VANE AND REPAIRED AREA, RE-INSTALLED AND C/W CLEARENCE CHECKS.SDR FDEA201211304215Hinge Bracket · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE BRACKET SIDE LOAD FITTING UPPER BORE SURFACE FOUND CORRODED. REWORKED AS PER CMM 20-10-6 REVISION 74. EXISTING THICKNESS: 0.452", MATERIAL REMOVED: 0.004", REAMINING THICKNESS: 0.448" FOUND ACCEPTABLE PER EA 1-5750-162SDR FDEA201211304216Hinge Bracket · corrodedLT WING OTBD FLAP, OTBD FORWARD HINGE BRACKET SIDE LOAD FITTING LOWER BORE SURFACE CORRODED. REWORKED AS PER CMM 20-10-6 REVISION 74. EXISTING THICKNESS: 0.452", MATERIAL REMOVED: 0.004", REAMINING THICKNESS: 0.448" FOUND ACCEPTABLE PER EA 1-5750-162399 PSDR FDEA201211294198Skin · looseRIGHT WING INBD FLAP UPPER SURFACE RIVETS XIFH 261 FOUND LOOSE. REMOVED AND REPAIR ACCOMPLISHED PER SRM 57-50-01, FIGURE 201, REPAIR 4, REVISION 51 AND EA 1-5750-163535. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100, REVISION 115.SDR FDEA201211294205Skin · dentedRT WING, INBD FLAP UPPER SURFACE, OTBD OF WS 313, HAS A DENT. REPAIRED FLAP UPPER SURFACE IAW-SRM-51-70-10, CAT."A" MAJOR REPAIR,SDR AALA20121129030Support Bracket · bentTHE RIGHT INBOARD MAIN FLAP HAS A BENT SUPPORT BRACKET 18 INCHES FROM INBOARD EDGE OF THE FLAP ALONG THE AFT 6 INCHES OF THE FLAP LOWER SKIN. REMOVED AND REPLACED THE SUPPORT BRACKET PER AARD 51-00-05-1.SDR UALA2012113006873Panel · dentedAPPEARS TO BE A DENT ON UNDERSIDE OF NR 2 FLAP ALONG TRAILING EDGE RIGHT WING. MEASURED DENT TO BE 2.25" LONG AND .055" DEEP DENT WAS 11.5" FROM EDGE OF TRAILING EDGE WEDGE PANEL AND 3.5" FROM AFT END OF TRAILING EDGE WEDGE PANEL. CF REF SRM 57-53-00 FIG 117SDR USAA2012123100022Flap · corroded2S CHECK - LEVEL 2 EXFOLIATION CORROSION ON LEFT WING OUTBOARD FLAP AT RIB 14. REPLACED LEFT WING OUTBOARD FLAP IAW A319 AMM 27-54-62-400-001-A.SDR ASAA2012112893458Skin · damagedLT OTBD FORE FLAP INBD L/E HAS A HOLE. REMOVED AND INSTALLED A NEW SKIN IAW AMM 20-50-11-912-002, FIG 202.SDR FDEA201211284189Skin · looseRIGHT WING INBD FLAP UPPER SURFACE AT "XIFH" = 269 FOUND LOOSE RIVETS. REMOVED AND REPAIRED ACCOMPLISHED PER SRM 57-50-01, FIGURE 201, REPAIR 4, REVISION 51 AND EA 1-5750-163535. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100, REVISION 115.SDR SWAA2012121010446Flap · delaminatedDELAMINATION ON LEFT FORE FLAP O/B (OUTBOARD AREA). REPAIRED LEFT FORE FLAP O/B (OUTBOARD AREA) IAW B737-300 SRM 51-40-10-2R-0.SDR SWAA2012120310122Flap · puncturedLEFT I/B FLAP PUNCTURED. REMOVED AND REPLACED FLAP IAW AMM.SDR UALA2012112806827Bolt · faultyAIRCRAFT VIBRATION AND TROUBLESHOOT USING ECRA 2754-01023. ACCOMPLISHED TROUBLESHOOTING OF VIBRATION IAW ECRA 2754-01023 STEPS 1, 2, & 3 ARE COMPLETED AND STEP 5 LEFT INBD FLAP TRACK NR 1 COMPLETED, MEASUREMENT ARE OD #1-.3578, ID#3-.3585, OD#3-.4365, ID#2-.4SDR ASAA2012112793413Rib · chafedHARDWARE LOOSE ON UPPER FIXED T/E PANEL BETWEEN INBD AND OTBD FLAPS. REPAIRED RT WING DEFLECTION CONTROL RIB ASSY IAW EA 700-57, EA 09381.SDR SWAA2012112099998Support Bracket · crackedRIGHT WING I/B FLAP O/B UPPER FIXED PANEL SUPPORT BRACKET IS CRACKED. REMOVED AND REPLACED RT WING I/B FLAP O/B UPPER FIXED PANEL SUPPORT BRACKET PER AMM.SDR AALA20121127012Skin · damagedLEFT WING TRAILING EDGE: DAMAGE TO BOTTOM SIDE OF INBOARD FLAP, OUTBOARD WEDGE, INBOARD END. INSTALLED NEW SKIN REPAIR PER SRM 51-70-06.
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