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 07FDEA00096Structure · corrodedRIGHT WING OUTBOARD FLAP INBOARD HINGE INBOARD AFT HOLE FOUND CORRODED. REPAIRED AS PER FEDEX E.A. 1-5750-107761, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.SDR 07FDEA00095Structure · corrodedRIGHT WING OUTBOARD FLAP INBOARD HINGE INBOARD FORWARD HOLE FOUND CORRODED. REPAIRED AS PER FEDEX EA 1-5750-107761, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.SDR 07FDEA00094Structure · corrodedRIGHT WING OUTBOARD FLAP INBOARD AFT HINGE OUTBOARD AFT BOLT HOLE FOUND CORRODED. REMOVED AND REPLACED AS PER CMM 57-52- 04. FLAP ADJUSTMENT REFER TO FEDEX EO 1-5720-7-5001 PT2, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.SDR 07FDEA00093Structure · corrodedRIGHT WING OUTBOARD FLAP INBOARD AFT HINGE OUTBOARD CENTER BOLT HOLE FOUND CORRODED. REPAIRED AS PER FEDEX E.A. 1-5750-107761, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.SDR SWAA070214Carriage · corrodedDURING SCHEDULED 22Y CHECK, FOUND LT WING INBOARD MID FLAP OUTBOARD CARRIAGE CORRODED. REMOVED AND REPLACED MID FLAP CARRIAGE PER MM.SDR IXXA07SMN031SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION FOUND LEFT HAND OUTBOARD FLAP HAS A NON STANDARD REPAIR FROM STATION XF384.000 TO STATION XF390.000. REMOVED EXISTING SKIN PANEL WITH NON STANDARD REPAIR. FABRICATED NEW SKIN PANEL. BONDED BOTH PARTS. WITH HYSOL. CLEANED, TSDR IXXA07SMN030SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING OUTBOARD FLAP HAS A NON STANDARD REPAIR ON UPPER SURFACE FROM STATION XF216.000 TO STATION XF220.000. REMOVED EXISTING NON STANDARD REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACKS OR CORRSDR ASAA0741381Skin · misrepairedRIGHT I/B FORE FLAP HAS 2 REPAIRS WITHIN ONE INCH OF EACH OTHER. EDGE DISTANCE IS TOO SHORT PER SRM. REMOVED PREVIOUS REPAIRS, PREPPED AREA FABRICATED AND INSTALLED REPAIR PIECES IAW SRM 51-70-10 REPAIR 1.SDR SWAA070136Skin · delaminatedDURING SCHEDULED C1 CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD T/E. REMOVED AND REPLACED AFT FLAP PER MM.SDR 07FDEA00077Support Fitting · crackedLEFT WING O/B FLAP ARC4012 OUTBOARD SUPPORT FITTING FOUND CRACK. LEFT HAND OUTBOARD FLAP ASSEMBLY REMOVED AND REPLACED AS PER AMM 27-50-30-4. ADJUSTMENT AND TEST CARRIED OUT FOUND SATIS AS PER AMM 27-50-00-5.SDR SWAA070126Rib · corrodedDURING SCHEDULED 10Y CHECK, FOUND RIGHT WING INBOARD FORE FLAP INBOARD RIB CORRODED. REMOVED AND REPLACED FORE FLAP RIB PER SRM.SDR SWAA070125Rib · corrodedDURING SCHEDULED 10Y CHECK, FOUND RIGHT WING INBOARD FORE FLAP OUTBOARD RIB CORRODED. REMOVED AND REPLACED FORE FLAP RIB PER SRM.SDR 07FDEA00073Fitting · corrodedLT WING OUTBOARD TRAILING EDGE FLAP FITTING ARC4009 FASTENER HOLES CORROSION BEYOND LIMIT. LT WING OUTBOARD FLAP REMOVED AND REPLACED AS PER AMM 27-50-30. P/N ON: NRC6753-503, S/N ON: 098 REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.SDR TRAX200700069Bracket · brokenLT WING AT RIB 13 UPPER FLAP BEAM OMEGA BRACKET BROKEN AT LOWER SECTION.SDR N921R54815Skin · dentedLT WING XW 68 INBOARD FLAP TRAILING EDGE LOWER SURFACE WITH DENT ( L=3 1/8, A=2 1/2, Y=.0935). CUTOUT DAMAGED AREA AND FABRICATED FILLER, SPLICE AND SKIN IAW DC8 SRM 57-2-5 AND DC8 SRM 57-7-1. TREATED AND PRIMED REPAIR AREA AND PARTS IAW DC8 SRM 51-1-8. INSSDR ASAA0741359Skin · chafedRIGHT OUTBOARD MID FLAP INBOARD SIDE LWR SURFACE OF LEADING EDGE HAS CHAFING DAMAGE. REPAIRED OUTBOARD MID FLAP LEADING EDGE IAW SRM 57-53-01 FIG 201.SDR AWXA200700045Skin · delaminatedPHX - LEFT WING OUTBOARD FLAP LOWER SURFACE DELAMINATED, WS 8268 - WS 9235. REPAIRED LEFT WING OUTBOARD FLAP LOWER SURFACE, WS 8268 - WS 9235 IAW A320 SRM 57-30-00.SDR SWAA070069Carriage · corrodedDURING SCHEDULED 18Y CHECK, FOUND RIGHT WING INBOARD MID FLAP OUTBOARD CARRIAGE CORRODED. REMOVED AND REPLACED FLAP CARRIAGE PER MM.SDR SWAA070068Torque Tube · corrodedDURING SCHEDULED 18Y CHECK, FOUND RIGHT WING INBOARD MID FLAP OUTBOARD TORQUE TUBE CORRODED. REMOVED AND REPLACED TORQUE TUBE PER MM.SDR AWXA200700043Skin · debondedPHX - LEFT WING OUTBOARD TRAILING EDGE FLAP HAS A SMALL AREA DISBOND AT INBOARD LOWER END, WBL 230.68. REPLACED LEFT WING OUTBOARD TRAILING EDGE FLAP IAW AWA TASK CARD R3M27034.SDR DHL2007743500Skin · delaminatedRT WING O/B FOREFLAP HAS DELAMINATION DAMAGE. REMOVED DELAMINATED AREA APPROX 4.8" BY 2". CLEANED AND PREPPED REPAIR AREA TO BOND IAW B727 SRM 51-40-20 PAR 7 FIG 3. FABRICATED LOWER FILLER AND DOUBLER FROM .016" 2024T3 PO NR 9003189, REPAIR CORE FROM HRP-3/SDR SWAA070063Skin · delaminatedDURING SCHEDULED HC2 CHECK, FOUND RIGHT WING OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD LOWER CORNER. REMOVED AND REPLACED AFT FLAP PER MM.SDR AWXA200700044Skin · delaminatedPHX - LEFT WING OUTBOARD FOREFLAP, UPPER SURFACE INBOARD END DELAMINATED, WBL 202.69 - WBL 413.61. REPLACED LEFT WING OUTBOARD FOREFLAP IAW AWA TASK CARD R3M27022.SDR DHL2007747001Skin · gougedRT INBD FORE FLAP O/B LEADING EDGE HAS GOUGE ON REPAIR DOUBLER. REMOVED AND REPLACED DAMAGED REPAIR FROM RT INBD FORE FLAP O/B LEADING EDGE IAW B727 SRM 57-50-4.SDR 07FDEA00035Skin · delaminatedLEFT WING, INBOARD FLAP VANE LOWER OUTBOARD SURFACE FOUND DELAMINATED. REPAIRED AS PER FEDEX E.A. 1-5750-105602, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.SDR 07FDEA00034Skin · delaminatedRIGHT WING, INBOARD FLAP VANE LOWER INBOARD SURFACE FOUND DELAMINATED. REPAIRED AS PER FEDEX E.A. 1-5750-105603, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.SDR 07FDEA00033Skin · delaminatedLEFT WING, INBOARD FLAP VANE LOWER OUTBOARD SURFACE FOUND DELAMINATED. REPAIRED AS PER FEDEX E.A. 1-5750-105602, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.SDR AWXA200700037Skin · delaminatedPHX - LEFT WING INBOARD FORE FLAP UPPER SURFACE DELAMINATED IN SEVERAL PLACES, WBL 73 - WBL 184.275. REPLACED LEFT WING INBOARD FORE FLAP IAW AWA TASK CARD R3M27008.SDR HALA0700052Flap · ground damageRT O/B FLAP LWR T/E WAS DAMAGED BELOW THE NR 12 SPOILER WHILE POSITIONING SCISSOR LIFT. THE CORNER OF THE RAIL CONTACTED THE FLAP. REPAIRED DAMAGE ON THE RIGHT O/B FLAP LWR T/E BELOW THE NR 12 SPOILER IAW SRM 51-70-0G.SDR UPS07449155Panel · delaminatedINSPECTION TYPE:C LEFT WING INBOARD T/E MID FLAP INBOARD FWD PANEL SEVERAL LOCATION FOUND DELAMINATED. FIBERGLASS REPAIRED AS PER BOEING MESSAGE 1-2716766520-2 AND RS R57-55-35719 AND UPS ENGINEERING FILE 747-57-20133.SDR UPS07449154Panel · delaminatedINSPECTION TYPE:C LEFT WING INBOARD T/E MID FLAP LWR AFT INBOARD PANEL SEVERAL LOCATION FOUND DELAMINATED. FIBERGLASS REPAIRED AS PER BOEING MESSAGE 1-2716766520-2 AND RS R57-55-35719 AND UPS ENGINEERING FILE 747-57-20133.SDR QXEA200603362Flap · out of adjustPDX C3 - RIGHT INBOARD FLAP DOES NOT MEET GAP CHECK BETWEEN FLAP AND FLAP SHROUD AT APPROXIMATELY STATION YW48.00. REPAIRED IAW RD 8/4-57-001, DHC-8-400 SRM 51-42-45, 51-42-05.SDR SWAA070036Skin · debondedDURING SCHEDULED 10Y CHECK, FOUND RT WING INBOARD FORE FLAP UPPER SKIN DISBONDED AT OUTBOARD TRAILING EDGE. REPAIRED SKIN SRM.SDR SWAA070033Carriage · corrodedDURING SCHEDULED 10Y CHECK, FOUND LT WING INBOARD MID FLAP OUTBOARD CARRIAGE CORRODED AT TORQUE TUBE ATTACHMENT BORE. REMOVED AND REPLACED OUTBOARD CARRIAGE PER MM.SDR SWAA070032Carriage · corrodedDURING SCHEDULED 10Y CHECK, FOUND LT WING INBOARD MID FLAP INBOARD CARRIAGE CORRODED AT TORQUE TUBE ATTACHMENT BORE. REMOVED AND REPLACED INBOARD CARRIAGE PER MM.SDR SWAA070013Skin · debondedDURING SCHEDULED 10Y CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP LOWER SKIN DISBONDED AT OUTBOARD T/E. REMOVED AND REPLACED AFT FLAP PER MM.SDR NSVA200600241Link · looseL AND R FLAP SAFETY (SWITCH LINKS LOOSE) MOTOR INOP. REMOVED AND REPLACED L AND R SAFETY LINKS IAW BMM 27-50-00 RAN FLAPS, OPS CK GOOD P/N 101-521030-5. REMOVED AND REPLACED FLAP MOTOR IAW B1900 MM CH 27-5003-211, OPS CHECK IAW B 1900, PN ON/OFF 100-524073-1SDR 06FDEA04330Skin · damagedLT WING FOREFLAP IS DAMAGED APPROX 79" FROM IB END. DAMAGE IS ON NOSE LE APPROX 3" LONG (DENT) REMOVED DAMAGE FROM L/E OF FLAP, FABRICATED REPAIR DOUBLER AND INSTALLED IAW SRM 57-50-2, AND SRM 57-50-4 PG 2A & 2B.SDR SROM200600022Carriage · crackedDURING ROUTINE ACCOMPLISHMENT OF ULTRASOUND INSPECTION OF THE SPINDLES ON THE OB FLAPS IAW AD 2003-24-08 FOUND THE RT IB SPINDLE TO SHOW A CRACK INDICATION. LAST ULTRASONIC INSPECTION PERFORMED 46 CYCLES AGO. REPLACED SPINDLE AND CARRIAGE ASSEMBLY WITH NEW PSDR A6WA200640416Strip · unknownWHEN FLAPS 45 DEGREES SELECTED A/C STARTS TO VIBRATE AND ROLL TO LEFT. DUIRNG TAKEOFF FLAPS 20 EXCESSIVE RIGHT AILERON TRIM REQUIRED. PERFORMED BLENDING OF L/E TEFLON STRIP OF FLAPS IAW SL-RJ-27-022 AMM 27-15 AND AMM 27-54-01-370-001 SECTION 8. (M)SDR AWXA200700030Pin · corrodedSAL - CORROSION ON LEFT WING FLAP TRACK NR 2 BEAM SPIGOT PINS, WS 2508 - WS 3059. REPLACED LEFT WING FLAP TRACK NR 2 BEAM SPIGOT PINS, WS 2508 - WS 3059 IAW AWA EO 57-44-03.SDR QXEA200603250Flap Track · corrodedC4 PDX - LEFT WING NR 4 FLAP TRACK INBOARD SIDELOAD ROLLER TRACK SURFACE IS WORN AND CORRODED. REPAIRED IAW RD8-57-988.SDR QXEA200603248Flap Track · chafedC4 PDX - LEFT WING INBOARD FLAP INBOARD LOWER TRACK HAS CHAFE DAMAGE ON UPPER SURFACE AT 7" FROM FORWARD EDGE. REPAIRED IAW RD8-57-985.SDR QXEA200603223Flap Track · damagedC4 PDX - REWORK, LEFT WING NR 4 FLAP TRACK OUTBOARD LOWER TRACK, UPPER SURFACE HAS DIVOTS, TRACK SURFACE WAS TREATED WITH NEW SURFACE COATING PRIOR TO REPAIR OF DIVOTS. COATING REQUIRES REMOVAL TO COMPLETE REPAIR. REPAIRED IAW RD8-57-988.SDR QXEA200603218Flap Track · corrodedC4 PDX - LEFT WING NR 4 FLAP TRACK LOWER SURFACE OF LOWER INBOARD TRACK IS PITTED. REPAIRED IAW RD8-57-988.SDR QXEA200603219Flap Track · corrodedC4 PDX - LEFT WING NR 4 FLAP TRACK OUTBOARD SIDE LOAD ROLLER "TRACK SURFACE" IS WORN AND CORRODED. REPAIRED IAW RD8-57-988.SDR QXEA200603252Flap Track · damagedC4 PDX - LEFT WING NR 5 FLAP TRACK UPPER DEAD WEIGHT ROLLER TRACK SURFACE HAS DIVOTS. REPAIRED IAW RD8-57-989.SDR QXEA200603247Flap Track · chafedC4 PDX - LEFT WING INBOARD FLAP INBOARD UPPER TRACK HAS CHAFE DAMAGE ON LOWER SURFACE AT 8.5" FROM FORWARD EDGE. REPAIRED IAW RD8-57-985.SDR QXEA200603246Flap Track · chafedC4 PDX - LEFT WING INBOARD FLAP INBOARD UPPER TRACK HAS CHAFE DAMAGE ON UPPER SURFACE AT 8.5" FROM FORWARD EDGE. REPAIRED IAW RD8-57-985.SDR 06FDEA04283Hinge Bracket · corrodedLHW I/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT O/B BORE FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER E.A.1-5750-106569. ORIGINAL 1.300" FINAL 1.328" MAX ALLOWABLE 1.220". BUSHING FABRICATED AND INSTALLED AS PER E.A. 1-575
Back to JASC 5753