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 LR7A2012100500401Splice · corrodedDURING SCHEDULED C-10, FOUND LEFT OTBD FLAP T/E SPLICE EXFOLIATION CORROSION AT OWS 173. R & R SPLICE IAW SMP 583 51-70.SDR FDEA201210053566Skin · damagedRIGHT WING OTBD MAIN FLAP UPPER PANEL MATING SURFACE FOUND TOOL MARK ON SCREW HOLE AT FLAP STA 586.85. REPAIRED AS PER EA F-5730-162307. REPAIR IS MAJOR.SDR FDEA201210053565Skin · damagedRIGHT WING OTBD MAIN FLAP UPPER PANEL MATING SURFACE FOUND TOOL MARK ON SCREW HOLE AT FLAP STA 586.6. REPAIRED AS PER EA F-5730-162307. REPAIR IS MAJOR.SDR FDEA201210053563Skin · damagedRT WING OTBD MAIN FLAP UPPER PANEL SURFACE FOUND TOOL MARK ON SCREW HOLES AT FLAP STA 341.6. REPAIRED AS PER E.A. F-5730-162307 PART 1. REPAIR IS MAJOR.SDR UALA2012100805672Skin · corrodedRIGHT WING INBOARD AFT FLAP, UPPER SKIN O/B TRAILING EDGE CORRODED IN SEVERAL AREAS. REPAIRED RT WING INBOARD AFT FLAP TRAILING EDGE 2EA AREAS UPPER SKIN BY BONDING FILLER SKIN & DOUBLERS IAW SRM 57-53-01 & 51-70-10. SEALED DOUBLERS IAW SRM 51-20-05 & BAC DSDR FDEA201210053564Skin · damagedRIGHT WING OTBD MAIN FLAP UPPER PANEL MATING SURFACE FOUND TOOL MARK ON HOLE AT FLAP STA 585.85. REPAIRED AS PER EA F-5730-162307 PART 1. REPAIR IS MAJOR.SDR FDEA201210053562Skin · damagedRIGHT WING OTBD MAIN FLAP UPPER PANEL MATING SURFACE FOUND TOOL MARK ON SCREW HOLES AT FLAP STA 338.6. REPAIRED AS PER E.A. F-5730-162307 PART 1. REPAIR IS MAJOR.SDR FDEA201210053561Skin · damagedRT WING OTBD MAIN FLAP UPPER PANEL MATING SURFACE FOUND TOOL MARK ON SCREW HOLE FLAP STA 585.6. REPAIRED AS PER E.A. F-5730-162307 PART 1. REPAIR IS MAJOR.SDR UALA2012100805676Skin · damagedRIGHT WING INBOARD AFT FLAP, LOWER TRAILING EDGE SKIN HAS 5 INCH CREASE. RECEIVED DAMAGE AT RIGHT WING INBOARD AFT FLAP LOWER T/E SKIN 83 INCHES FROM OTBD END IAW SRM 57-53-01 & 51-70 -10 REPAIR BY BONDING SKIN & DOUBLER IAW SRM 57-53-01 & 51-70-10. REPAIR RSDR UALA2012100805675Skin · damagedRIGHT WING INBOARD AFT FLAP, LOWER SKIN INBOARD SIDE DENTED IN SEVERAL AREAS. REMOVED DAMAGE ON DENTS, FABRICATED REPAIR PARTS, BONDED REPAIRS AND CURED, AND APPLIED CONDUCTIVE COATING IAW SRM 57-53-01 & 51-70-10 & 57-70-05, PREP AND PAINTED AREAS IAW GPM 5-0SDR IPXA2M76153Vane · dentedINSPECTION TYPE: 4C, RT INBD FLAP VANE LOWER SURFACE HAS MULTIPLE DENTS. REPAIRED RT INBD FLAP VANE IAW EA-011-5753-01-A4362 REV IR AND EO MD11-5750-49006-B.SDR USAA2012102500009Strut · corroded2S CHECK - CORROSION ON LEFT WING INTERCONNECTING STRUT BETWEEN WS 4067 TO WS 4862 & BETWEEN RIB 8 TO RIB 9. REPLACED LEFT WING INTERCONNECTING STRUT IAW A319 AMM 27-51-44-400-01-A.SDR USAA2012102500008Strut · corroded2S CHECK - CORROSION ON RIGHT WING INTERCONNECTING STRUT BETWEEN WS 4067 TO WS 4862 & BETWEEN RIB 8 TO RIB 9. REPLACED RIGHT WING INTERCONNECTING STRUT IAW A319 AMM 27-51-44-400-01-A.SDR USAA2012100800018Cap · delaminatedQ6 CHECK - DELAMINATION ON RIGHT WING TRAILING EDGE FLAP UPPER END CAP APPROX 2 INCHES FROM TRAILING EDGE. REPLACED RIGHT WING TRAILING EDGE FLAP UPPER END CAP IAW EA 104226.SDR QXEA2012100401149Beam · damagedRT WING NR 4 FLAP TRACK BEAM HAS DAMAGE ON INBD SIDE OF WEB. REMOVED DAMAGE IAW RD 8/4-57-1238. PERFORMED UT THICKNESS OF BLEND IAW NTM 51-00-04-910-801 PT 1. MIN REMAINING THICKNESS 0.141" COMPLETED STEP 6 OF RD 8/4-57-1238. DAMAGE IS IN LIMITS IAW RD 8/4-SDR QXEA2012100401148Flap Track · damagedRT WING NR 3 UPPER FLAP TRACK HAS A SMALL AREA OF WEAR AT AFT END. REMOVED DAMAGED IAW RD 8/4-57-1511. MEASURED FLAP TRACK AND FOUND MIN REMAINING THICKNESS 0.321 TO BE WITHIN LIMITS OF RD 8/4-57-1511. COMPLIED WITH STEP 5 OF RD 8/4-57-1511. VERIFIED AFFECTESDR QXEA2012100401147Flap Track · damagedRT WING NR 3 LOWER FLAP TRACK HAS DAMAGE AT AFT END. REMOVED DAMAGE IAW RD 8/4-53-1511. PERFORMED UT THICKNESS OF BLEND IAW NTM 51-00-04-910-801 PT 1. MIN REMAINING THICKNESS .239". FOUND DAMAGE OUT OF LIMITS IAW RD 8/4-57-1511. MAPPED AND SUBMITTED TO ENSDR QXEA2012100401144Flap Track · damagedLT WING NR 4 FLAP TRACK BEAM WEB AREA HAS DAMAGE ON INBD AND OTBD SIDES. REMOVED DAMAGE IAW RD 8/4-57-1238. PERFORMED UT THICKNESS OF BLENDS IAW NTM 51-00-04-910-801 PT 1. MIN REMAINING THICKNESS .114". DAMAGE OUT OF LIMITS IAW RD 8/4-57-1238. MAPPED DAMASDR SWAA2012100808313Flap · delaminatedRIGHT WING OUTBOARD AFT FLAP DELAMINATED ON TRAILING EDGE. REMOVED AND REPLACED AFT FLAP PER MM.SDR ERAA20120075Flap · delaminatedRIGHT INBOARD FLAP DELAMINATED ON P/N: 85750002-010.SDR ERAA20120074Flap · delaminatedLEFT INBOARD FLAP DELAMINATED ON P/N:85750002-009 AND 85750002-010.SDR IPXA12B75643Structure · damagedLT INBD FLAP T/E DAMAGED. REPAIRED IAW EO B747-5750-48492-A.SDR UALA2012100305601Spherical Bearin · faultyLANDING FLAPS FULL HAD MOD VIBRATION. RETURNED TO FLAPS 3 VIB CEASED. RETURNED FLAP FULL VIB. LEFT FLAP SPHERICAL BEARING. LT WING NR 1 FLAP CARRIAGE CENTER GUIDE ROLLER RETAINING NUTS NEED TO BE INSTALLED PER MM TO COMPLETION. INSTALLED AND TORQUED RETAISDR SWIA201231901Flap · defectiveAT FLAPS 45 PLANE ROLLS UNCOMMANDED. (FLT 6450) REMOVED PAINT RUNS FROM ALL FOUR FLAP TRAILING EDGE UNDERSIDES AND UPPER LEADING EDGE SURFACES IN REFERENCE TO CRJ MM.SDR UALA2012100205589Cotter Pin · missingRIGHT WING INBOARD MIDFLAP INBOARD CARRIAGE SPINDLE AFT ATTACH LINK LOWER CASTLELATED NUT IS MISSING COTTER KEY. FOUND WASHER MS15795-828 NOT INSTALLED AS CALLED OUT PER AMM. TORQUED CASTLE NUT AND INSTALLED COTTER PIN PER AMM. RIGHT WING INBOARD MIDFLAP, ISDR AALA20121001003Skin · damagedHAIL DAMAGE ON LEFT OUTBOARD FLAP UPPER SURFACE. ACCOMPLISHED BONDED REPAIR PER SRM 57-53-01.SDR AALA20121001002Skin · damagedLEFT OUTBOARD FLAP LOWER SURFACE HAD DENT WITH PUNCTURE. ACCOMPLISHED BONDED REPAIR PER SRM 57-53-01.SDR SWAA2012101708590Skin · crackedRIGHT WING FORE FLAP INBOARD LOWER SKIN CRACKED. REPAIRED FORE FLAP IAW SRM.SDR REXA2012111101492Skin · dentedLEFT INBOARD FLAP LOWER SKIN DENTED APPROXIMATELY 4 INCHES OUTBOARD OF INBOARD EDGE. REPAIRED IAW SRM 57-52-00 FIGURE 2.SDR USAA2012102900005Flap · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON RIGHT OUTBOARD FLAP UPPER INTERNAL AREA OUTBOARD SIDE BETWEEN WS 10204 TO WS 10729 AT RIB 15. REPLACED RIGHT OUTBOARD FLAP IAW A319 AMM 27-54-62-400-001-A.SDR SWAA2012101108450Spindle · crackedLEFT WING NR 1 O/B FLAP O/B SPINDLE CARRIAGE CRACKED. REMOVED AND REPLACED SPINDLE IAW AMM AND MT.SDR SWAA2012100108133Spindle · corrodedLEFT WING NR 1 FLAP CARRIAGE SPINDLE CORRODED, FAILED INSPECTION. REMOVED AND REPLACED NR 1 O/B FLAP SPINDLE CARRIAGE ASSY PER M/M.SDR FDEA201209283486Support Angle · damagedLEFT OTBD FLAP INBD HINGE UPPER ANGLE HAS BROKEN SUPPORT. REMOVED BROKEN SUPPORT IAW SRM 51-31-01, VOL 2. FABRICATED NEW SUPPORT IAW SRM 51-31-01, VOL 2 PAGE 63, SRM 51-21-01, VOL 2, PAGE 17, SRM 51-10-00 VOL 2, PAGE 62 AND DWG ARC0744. INSTALLED SUPPORT ASDR UALA2012092905498Flap · dentedMULTIPLE DENTS ON LEFT OUTBOARD TRAILING EDGE FLAP. FOUND 18 DENTS ON FLAP. ALL DENTS ARE LESS THAN .118\ IN DEPTH AND LESS THAN 1.575\ IN WIDTH PER SRM 57-53-00 PAGE 129 OK TO FLY FOR 1000 FC BEFORE REPAIR NECESSARY. TAP TEST ACCOMPLISHED NO DELAMINATION FSDR UALA2012092905497Flap · dentedMULTIPLE DENTS ON LEFT INBOARD TRAILING EDGE FLAP. FOUND 16 DENTS ON FLAP. ALL DENTS ARE LESS THAN .118\ DEEP AND LESS THAN 1.575\ IN WIDTH. PER SRM 57-52-00 PG 137 OK TO FLY FOR 1000 FC BEFORE REPAIR REQUIRED. ACCOMPLISHED TAP TEST NO DELAMINATION FOUND.SDR UALA2012092905496Flap · dentedMULTIPLE DENTS ON RIGHT INBOARD TRAILING EDGE FLAP. FOUND 7 DENTS ON FLAP. ALL DENTS ARE LESS THAN .118\ DEEP AND AND LESS THAN 1.575\ IN WIDTH. PER SRM 57-52-00 PAGE 137 OK TO FLY FOR 1000 FC BEFORE REPAIR NECESSARY. TAP TEST ACCOMPLISHED NO DELAMINATION SDR AALA20121001011Flap · debondedLEFT WING INBOARD AFT FLAP APPROXIMATELY 25 INCHES INBOARD OF CANOE. ACCOMPLISHED BONDED REPAIR PER SRM 51-70-10-2R.SDR AALA20121001010Skin · dentedDENT IN UPPER SKIN OF AFT INBOARD FLAP. ACCOMPLISHED HOT BOND REPAIR PER SRM 51-70-10-2R.SDR ABXA20120927279Attach Fitting · crackedLOUD POPPING NOISE HEARD WHEN LEFT FLAP WAS EXTENDED OR RETRACTED. AT AFT WING SPAR STATION 908 FOUND REAR SPAR DEFLECTION CONTROL TRACK SUPPORT FOR OUTBOARD TRAILING EDGE FLAP BROKEN OFF AT SPAR SIDE LOWER LOBE ATTACH FITTING. REMOVED AND REPLACED OUTBOARDSDR AALA20120927004Skin Panel · damagedRIGHT WING OUTBOARD TRAILING EDGE WEDGE UPPER SKIN PANEL DAMAGED BY HAIL. ACCOMPLISHED BONDED REPAIR PER SRM 51-70-07.SDR AALA20120927002Skin · delaminatedRIGHT WING OUTBOARD FLAP LOWER SKIN SURFACE DELAMINATED. ACCOMPLISHED BONDED REPAIR PER SRM 51-70-07.SDR FDEA201209273473Skin · damagedRT OTBD FLAP UPPER SURFACE SKIN IS SEPARATED FROM STRUCTURE DUE TO PULLED THRU FASTENERS 60" FROM OTBD END. REPAIRED IAW SRM 57-10-00, FIG 7, VOL I. MAJOR REPAIR.SDR FDEA201209263451Skin · damagedRT WING OTBD MAIN FLAP UPPER PANEL NR 3 FROM INBD, FIVE HOLES FOUND ELONGATED. REPAIRED AS PER EA F-5730-162307 PART 1. REPAIR IS MAJOR.SDR FDEA201209263449Skin · damagedRT WING OTBD MAIN FLAP UPPER PANEL NR1 FROM INBD FIVE HOLES FOUND ELONGATED. REPAIRED AS PER EA F-5730-162307 PART 1. REPAIR IS MAJOR.SDR FDEA201209263448Skin · damagedRT WING OTBD MAIN FLAP UPPER PANEL MATING SURFACE FOUND TOOL MARK ON SCREW HOLE. REPAIRED AS PER E.A. F-5730-162307 PART 1.SDR FDEA201209263447Skin · damagedRT WING OTBD MAIN FLAP UPPER PANEL MATING SURFACE FOUND DAMAGED ON SCREW HOLE AT 337.85. REPAIRED AS PER EA F-5730-162307 PART 1. REPAIR IS MAJOR.SDR AALA20121009002Skin Panel · damagedAN INTERIM REPAIR WAS ACCOMPLISHED ON THE UPPER LEFT CORNER FASTENER HOLE OF THE LEFT INBOARD MAIN FLAP UPPER SKIN PANEL. INSTALLED PERMANENT EXTERNAL DOUBLER REPAIR AS PER EA B737-57-026476.SDR A6WA20121008550Vane · chafedRIGHT I/B FLAP VANE LEADING EDGE CHAFED 3 SPOTS. INBOARD LEADING EDGE FOUND TO BE OUT OF LIMITS. BLENDED DAMAGE ON RIGHT I/B FLAP VANE LEADING EDGE FOUND CENTER AND AFT LEADING EDGE TO BE WITHIN LIMITS IAW REO 601R-57-52-004 REV C. REPLACED I/B LEADING EDGESDR DXTA2012F00201Flap Track · corrodedRIGHT "B" FLAP TRACK CORRODED, REPAIREDSDR 2012FA0000648Flap Track · corrodedRIGHT "C" FLAP TRACK CORRODED, R & R IAW BP1159W40119.
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