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 SWAA2023030897320Fitting · crackedRT WING TRAIL EDGE RIB WBL 201.90 HAS AFT UPPER FITTING CRACKED THRU. 8-24<[01] REMOVED AND REPLACED AFT UPPER FITTING AT RT WING TRAIL EDGE RIB WBL 201.90 PER REF SRM-51-40-02-0G-0.;[02] FINAL INSPECTION; T/E RIB REPLACED.SDR DALA2023020100805None · noneSHIP 3122 - CORROSION FLAP TRACK BOLT AND NUT ON CARRIAGE 2, 3 AND 4 ON LH WING. CORRECTIVE ACTION: REPLACED FLAP TRACK BOLT AND NUT ON CARRIAGE 2, 3 AND 4 ON LH WING AS PER A320 FAM AMM 27-54-46. (2608775)SDR DALA2023020100804None · noneSHIP 3122 - CORROSION OB FLAP EXCENTRICAL BEARING ON TRACK 4 ON RH WING. CORRECTIVE ACTION: ACCOMPLISHED ON AMDS CARD 2750-6020-RT. (2608761)SDR UIEA2023013140080Skin · delaminatedRH O/B FORE FLAP I/B L/E FOUND DELAMINATION (28" TO I/B EDGE)(<P>PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR.5A</P>)SDR UIEA2023013140081Skin · chafedRH O/B FORE FLAP I/B L/EÂ FOUND 2EA CHAFING (42" TO I/B EDGE)(<P>PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR.5A</P>)SDR UIEA2023013150083Skin · delaminatedRH O/B FORE FLAP L/E FOUND DELAM (BETWEEN NO.2 AND NO.3 FORE FLAP LEVER)(<P>PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR.5C</P>)SDR UIEA2023013100085Skin · chafedRH O/B AFT FLAP UPPER O/B PNL FOUND CHAFING.(<P>PERFORMED METAL HOTBOND REPAIR AS PER SRM 51-70-10 REPAIR 4</P>)SDR UIEA2023013140075Skin · delaminatedRHW I/B MID FLAP LOWER SURFACE FOUND DELAMINATION (O/B OF #5 FLAP TRACK)(<P>PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR.5A</P>)SDR UIEA2023013140076Skin · delaminatedRHW I/B MID FLAP L/E MOST I/B AREA FOUND DELAMINATION(<P>PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR.5A</P>)SDR UIEA2023013140078Skin · delaminatedLHW O/B FORE FLAP I/B L/E FOUND 1EA DELAMINATION (39" TO I/B EDGE)(<P>PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR.5A</P>)SDR VNAA2023012719991Hinge Fitting · damagedLEFT WING IB FWD FLAP HINGE FITTING, HOLES THROUGH WINGPLANK AT W.S. 54.55 ARE REAMED TO .410" AND STILL HAVE DAMAGE IN WING PLANK STRUCTURE INSIDE HOLES.SDR DALA2023103108940Unknown · unknownSHIP 3255 ER/A 605558-14AD ISSUED FOR REPLACEMENT OF THE LH INBD FLAP TRUNNION. CORRECTIVE ACTION: COMPLIED WITH ERA. (2601735)SDR SWAA2023030895855Angle · elongatedL/W REAR SPAR FIXED T/E LOWER PANEL 551GB I/B ATTACHED ANGLE FWD FASTENER HOLE ELONGATED AND BUSING ; BOLT ; NUT MISSING MKD DOT<[01] REMOVED DAMAGE ANGLE AT LT WING T/E LOWER PANEL 551GB I/B SIDE PER REF B737 SRM 51-40-02-0G-0;[02] LOCATED AND DRILLED NEW ANGSDR SWAA2023030895856Beam · elongatedL/W REAR SPAR FIXED T/E DEFLECTION CONTROL RIB PANEL O/B SUPPORT ATTACHMENT POINT LOCATION ' A' ELONGATED HOLES ;EXCESSIVE PLAY MKD DOTS<[01] REMOVED HARDWARE AT L/W REAR SPAR FIXED T/E DEFLECTION CONTROL RIB PANEL O/B SUPPORT ATTACHMENT POING LOCATION 'A'AS PSDR SWAA2023020995550Bracket · crackedLEFT WING TRAILING EDGE PANEL SUPPORT ATTACH BRACKET CRACKED AT RSS. 211.(51-001)<[01] REMOVED AND REPLACED PANEL SUPPORT ATTACH BRACKET AT LEFT WING TRAILING EDGE AT STA RSS 211 PER BOEING 737-700 SRM 51-40-02-0G-0;[02] VERIFIED REPLACEMENTSDR SWAA2023012795336Skin · delaminatedRIGHT OUTBOARD AFT FLAP DELAMINATED AT BOTTOM INBOARD CORNER.<[01] ACCOMPLISHED WITH EA 23-157-00293. (TTG8Q00HG3ZA)SDR LR7A2023012603263Skin · dentedDURING SCHEDULED B-2 CHECK UNDER JOB CARD HB2703, FOUND LH OW FLAP TRAILING EDGE LOWER SKIN DENTED AT OWFS151-157L. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-12. NR# 1000882583. / PSE# 57-50-16, AD 2012-06-09SDR DALA2023020300856Not Entered · not enteredSHIP 6709 LIGHTNING DAMAGE TO LT WING INBD AFT FLAP. CORRECTIVE ACTION: REMOVED LT WING INBD AFT FLAP REF B757 AMM 27-51. DAMAGE REPAIRED ON NRC 001 IAW R.I. 605564-14. REINSTALLED AFT FLAP IAW B757 AMM 27-51. (9882320)SDR DALA2023012600656Bearing · out of limitsSHIP 3309 PER AMDS CARD 2754-2011 FOUND # 3 FLAP TRACK AFT LINK UPPER AND LOWER BEARINGS OUT OF LIMITS. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. INSTALLED LINK ASSEMBLY.SDR DALA2023012400559Skin · delaminatedDURING INSPECTION FOUND RT WING OTBD FLAP INBOARD T/E DAMAGED & DELAMINATED. REMOVED OTBD FLAP T/E IN REF TO B737 AMM 27-51. INSTALLED SERVICEABLE RH OTBD AFT T/E FLAP AND ADJUSTED IAW AMM 27-51.SDR DALA2023012300494Trunnion · damagedSHIP 3267 LH I/B FLAP TRUNNION DAMAGED BEYOND ALLOWABLE LIMITS. CORRRECTIVE ACTION: R/R FITTING PER A320 CMM 57-52-21. OK FOR SERVICE. (9880801)SDR SWAA2023030694129Panel · pulledR/W T/E PANEL 661BB HAS SEVERAL PULLED FASTENER HOLES (MARKED)<[01] IDENTIFIED PANEL 661BB IAW SRM 57-51-01-0I-1 FIGURE 3 TABLE 3 ITEM 9.<BR>FOUND DAMAGE TO BE OUT OF ALLOWABLE LIMITS IAW SRM 57-51-01-1A-1 PARA 4.B(5).<BR>DAMAGE TO BE REPAIRED IAW SRM 51-70-04SDR SWAA2023030694122Fairing · pulled#8 FLAP TRACK FAIRING 644BB FASTENERS FOR AFT SEAL RETAINER HAVE PULLED FASTENERS (MARKED)<[01] PART/MATERIAL IDENTIFIED PER SRM 57-53-70-0I-1 FIGURE. 4 TABLE 3 ITEM 3.<BR>PULLED FASTENER HOLES EXCEED THE ALLOWABLE LIMITS AS GIVEN IN SRM 57-53-70-1A-1. PARA 4 SDR SWAA2023020994110Fitting · crackedLEFT WING REAR SPAR T/E DEFLECTION CONTRL RIB PANEL VERTICAL BULB SEAL FITTING CRACKED I/B SIDE MKD DOT<[01] REMOVED AND REPLACED VERTICAL BULB SEAL FITTING AT LEFT WING REAR SPAR T/E DEFLECTOR CONTROL RIB PANEL PER BOEING 737-700 SRM 51-40-02-PG-0;[02] VERIFISDR AALA202301263512Bushing · migratedAIRCRAFT IN BASE MAINTENANCE: RIGHT WING FLAPERON SUPPORT STRUCTIRE OUT BOARD MAIN HINGE, HAT BUSHING MIGRATED AT RIGHT COVE LIP DOOR REAR SPAR. MAINTENANCE REPLACED FITTING ON MAIN HINGE AT RIGHT COVE LIP DOOR REAR SPAR PER B777-200 SRM51-40-02-0G.SDR IPXA2023013090441Angle · brokenINSPECTION TYPE:1CLH WING CENTER FLAP OB SIDE ANGLE PLATE BROKENREMOVED AND REPLACED IAW SRM 51-40-21SDR IPXA2023013090440Angle · brokenINSPECTION TYPE:1C, RT WING CENTER FLAP OB SIDE ANGLE PLATE BROKEN. REMOVED AND REPLACED IAW SRM 51-40-21SDR DALA2023012400563Flap Track · crackedFOUND OUT LH WING IB AFT FLAP IB TRACK ATTACHED FITTING CRACKED AT IB FWD FLAP AFT WEB. LH WING I/B AFT FLAP I/B TRACK ATTACHED FITTING CRACK WITH 6.3" AT I/B FWD FLAP AFT WEB, REMOVED AND FABRICATED, INSTALLED AS PER PRI: 605334-14.SDR DALA2023012400562Skin · wornFOUND OUT LT WING IB AFT FLAP EXTERNAL UPPER SURFACE WORN AT 2 INCHES TO IB EDGE AND 6 INCHES TO FWD EDGE. REPAIRED THE LT WING IB AFT FLAP EXTERNAL UPPER SURFACEIAW PRI 605336-14.SDR DALA2023012400561Web · crackedFOUND LT WING IB FLAP AFT WEB UPPER CHORD CRACKED AT AFT WEB IB UPPER CORNER. LT WING I/B FLAP AFT WEB UPPER CHORD CRACK WITH 1.4" AT AFT WEB I/B UPPER CORNER, CUT OUT AND REPAIRED IAW PRI: 605332.SDR DALA2023022301375None · noneAIRCRAFT 3122, CORROSION OUTBOARD FLAP ON BEARING BORE TRACK 3 ON RH WING. CORRECTIVE ACTION: REPLACED O/B FLAP RH WING. (LP 2591594)SDR SWAA2023012493456Fairing · cracked#7 FLAP CANOE AFT TAIL CONE CRACKED<[01] OK TO CONTINUE PER CDL 57-10-3 SP1B #7 FLAP CANOE TAILCONE REMOVED;[02] INSTALLED #7 FLAP CANOE AFT TAIL CONE REF AMM 27-51-28. CDL PLACARD REMOVED. REF LOGPAGE 2332206 FOR REMOVAL.SDR DALA2023012300503Skin · wornSHIP 1820 FOUND OUT LH WING IN AFT FLAP EXTERNAL UPPER SURFAE WORN AT 2 INCHES TO IB EDGE AND 6 INCHES TO FWD EDGE. CORRECTIVE ACTION: THE REPAIRED ON LH WING IB AFT FLAP EXTERNAL UPPER SURFACE AT 2 INCHES TO IB EDGE AND 6 INCHES TO FWD EDGE AS PER PRI 605336-SDR SWAA2023021393151Wedge · delaminatedL/W I/B MAIN FLAP T/E OUTBD LOWER SURFACE DELAMINATED<[01] REMOVED L/W OUTBOARD FLAP INBOARD UPPER AND LOWER SEALS AS PER AMM 27-51-11;[02] REMOVED L/W INBOARD FLAP OUTBOARD UPPER SEAL AS PER AMM 27-51-11;[03] VERIFIED STEP 1 AND 2;[04] REMOVED L/W INBOARD T/ESDR DALA2023013000740Flap Track · corrodedSHIP 3122 - CORROSION OUTBOARD FLAP ON BEARING BORE TRACK 3 ON LH WING. CORRECTIVE ACTION: REMOVED OUTBOARD FLAP LH.SDR DALA2023013000739Strut · corrodedSHIP 3151 - CORROSION INBD FLAP INTERCONNECTING STRUT INTERNAL STRUCTURE ON LT WING. CORRECTIVE ACTION: REMOVED INTERCONNECTING STRUT ON LT WING.SDR DALA2023013000738Strut · corrodedCORROSION INBD FLAP INTERCONNECTING STRUT INTERNAL STRUCTURE ON RT WING. CORRECTIVE ACTION: REMOVED INTERCONNECTING STRUT ON RH WING. (2590364)SDR DALA2023012000450Trunnion · damagedLEFT FLAP TRUNNION DAMAGED. R & R THE FLAP TRUNNION IAW CMM 57-52-21.SDR IXXA2023011901Flap Track · corrodedIB FLAP TRACKS CORRODED..SDR AALA202303010895Doubler · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING OUTBOARD TRAILING EDGE FLAP LOWER SURFACE EXTERNAL DOUBLER AT FLAP TRACK #4, AT WS 8268 AND RIB 15. MAINTENANCE REPLACED DOUBLER PER SRM 57-53-21-300-003.SDR AALA202304129548Doubler · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING OUTBOARD TRAILING EDGE FLAP LOWER SURFACE EXTERNAL DOUBLER AT FLAP TRACK 4. REPLACED DOUBLER PER SRM 57-53-21-300-003 AND SRM 51-42-11.SDR IPXA2023011769955Skin · dentedMAJOR REPAIR, LEFT WING INBOARD FLAP LOWER SURFACE SKIN DENTED AT TRAILING EDGE REPAIRED IAW E.O. A300-5750-84804-B.SDR KCSA202301121002Link Assy · crackedL/H I/B FLAP I/B LINK ASSEMBLY CRACKEDSDR SWAA2023021390019Wedge · looseLEFT MAIN FLAP O/B T/E AREA COMPOSITE LOWER EDGE SECTION LOOSE DOT 48 EVALAUTED AREA O/B T/E LOWER SKIN SECTION DELAMINATED<[01] PERFORMED VISUAL INPECTION AND TAP TEST AT L\W MAIN FLAP O\B T\E WEDGE ON LOWER SURFACE FOUND DELAMINATION SIZE 30'X9.5' PER B737 NSDR SWAA2023012490005Skin · crackedCRACK FOUND AT EXTERNAL LOWER SURFACE OF RH I/B AFT FLAP 19.5' FROM I/B EDGE AND 3.375' FROM T/E. CRACK CONFIRMED IAW NDTM PART 6; 51-00-00 PROCEDURE 23. CRACK LENGTH : 0.393'. CUT OUT DAMAGED AERA AT R\H I\B AFT FLAP ON LOWER SURFACE SIZE 1.5'X0.5' NO CORESDR 6CBA2023011623016Skin · dentedDURING A PRELIMINARY INSPECTION PRIOR TO A SCHEDULED INSPECTION, THE AIRCRAFT WAS FOUND TO HAVE HAIL DAMAGE TO THE LEFT AND RIGHT WINGS, AILERONS, FLAPS, HORIZONTAL STABILIZERS, AND ELEVATORS. AILERONS AND ELEVATORS WERE DENTED BEYOND SRM LIMITS IAW SRM 12-B-SDR SWAA2023020887738Panel · pulledL/W PANEL 561BB HAS PULLED FASTENER HOLES (MARKED)<APPLIED SLURRY MIXTURE OF CHOPPED FIBERS AND LAMINATING RESIN BMS8-301 CL1 LOT#JH2EAA8895 TO FASTENER HOLES; AND SET TO CURE USING HOT BONDER ID: NCX000523 DUE:06/2023 IAW SRM 51-70-04-2R-9 PAR.4 D-F;[05] CURESDR SWAA2023020887740Panel · pulledPANEL 561AB HAS SEVERAL PULLED FASTENER HOLE ON AFT END (MARKED)<APPLIED SLURRY MIXTURE OF CHOPPED FIBERS AND LAMINATING RESIN BMS8-301 CL1 LOT#JH2EAA8895 TO FASTENER HOLES; AND SET TO CURE USING HOT BONDER ID: ATS2802 DUE:10/2023 IAW SRM 51-70-04-2R-9 PAR.4 DSDR SWAA2023020887730Panel · pulledPANEL 551CB HAS SEVERAL PULLED FASTENER HOLE ON AFT END (MARKED) PANEL FOUND TO BE 561CB NOT 551CB< APPLIED SLURRY MIXTURE OF CHOPPED FIBERS AND LAMINATING RESIN BMS8-301 CL1 LOT#JH2EAA8895 TO FASTENER HOLES; AND SET TO CURE USING HOT BONDER ID: ATS2802 DUE:10SDR SWAA2023020187508Bracket · crackedLEFT WING LOWER I/B T/E FIXED PANEL #551FB HAS 1 EACH BRACKET AT INNER AFT SEAL RETAINER ATTCH. CRACKED (MKD)<[01] REMOVED AND REPLACED BRACKET (1EACH) AT INNER AFT SEAL RETAINER;LEFT WING LOWER I/B.T/E. PANEL#551FB;PER B 737-700 SRM 51-40-02-0G-0.;[02] VERIFI
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