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 DALA2023060604603Unknown · unknownSHIP 3356 DURING HCK AT SAL AND ACCOMPLISHMENT OF EM 5753-01164, THE RH RIB 6 FITTING FORWARD LUG WAS FOUND CORRODED. CORRECTIVE ACTION: REF ERA 608421-14. (2797205)SDR SWAA2023062054639Angle · crackedCRACK ANGLE TRAILING EDGE LOCATED IRSS140 RT WING 2023-361031<[01] REPLACED ANGLE TRAILING EDGE LOCATED IRSS140 RT WING IAW B737-700 SRM 51-40-02-0G-0 AND SRM 51-10-02-0G-0 ITEM 9;[02] REPLACED ANGLE TRAILING EDGE LOCATED IRSS140 RT WING IAW B737-700 SRM 51-40SDR SWAA2023062054641Angle · crackedCRACK ANGLE TRAILING EDGE LOCATED IRSS140 LT WING 2023-361033<[01] REPLACED ANGLE TRAILING EDGE LOCATED IRSS140 LT WING IAW B737-700 SRM 51-40-02-0G-0 AND SRM 51-10-02-0G-0 ITEM 9;[02] REPLACED ANGLE TRAILING EDGE LOCATED IRSS140 LT WING IAW B737-700 SRM 51-40SDR AALA202307244670Fitting · wornAIRCRAFT IN BASE MAINTENANCE: RIGHT WING INBOARD TRAILING EDGE FLAP INBOARD END FITTING / BRACKET ASSEMBLY WORN AND HAS EXCESSIVE PLAY IN THE BEARING AT FLAP RIB 14. REPLACED FITTING / BRACKET ASSEMBLY ON THE RIGHT WING INBOARD FLAP PER SRM 51-42-11.SDR AALA202307204601Bracket · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING TRAILING EDGE INBOARD FLAP REAR SPAR FITTING / BRACKET AT FLAP RIB 14. REPLACED BRACKET PER SRM 51-42-11.SDR DALA2023060604554Unknown · unknownFLAP HINGE ATTACH FITTING INSIDE WING AT XRS 164.00 BOTTOM LUG HORIZONTAL FASTENER HOLES, 3 EA OUTBOARD SIDE - MARKED. COMPLIED WITH ON ERA 6071561-14 AD STEP 38 AND FIGURE 10. (LP #2790427)SDR DALA2023060604553Unknown · unknown3 EA HOLES MISDRILLED IN SKIN BELOW XRS 140.00 - MARKED. COMPLIED WITH ON ERA 607151-14AD STEP 23. (LP #2790419)SDR DALA2023060604552Unknown · unknownTHREE EA HOLES WITH CRACK INDICATION IN SKIN LAYER, IB EDGE OF LOWER WING SKIN DOUBLER IB OF XRS 164.00. MARKED. COMPLIED WITH ON ERA 607151-14AD STEP 27. (LP #2790416)SDR IPXA2023062831080Structure · puncturedLH I/B AFT FLAP HAS A PUNCTURE APPROX 26.75€? FROM TRAILING EDGE & 63€? FROM I/B EDGE. MARKED WITH TAPE.***SM36/LMX4/HGR*** ACCOMPLISHED STEPS 1-14 OF EO-87186-REQ3 PERMANENT REPAIR. THIS CLEARS DEFERRAL MOC 2500762.SDR FDEA202305270964Flap · dentedLH WING CTR FLAP L/E GOT A DENT AT RIB11-2" PFM CUT OUT REPAIR AND MADE THE REPAIR PARTS TO INSTALLED ON REPAIRED AREA. I.A.W A300-600F SRM 57-50-00-201, PARA.4H, P201-P236, FIG.208. THIS REPAIR IS CAT B REPAIR REFER CHAPTER TO SRI:57-50-00-201,IIR:57-50-0SDR DALA2023053104383Unknown · unknownCOMPLY WITH PRI 609042-14 AD REV O., ENSURE FINAL ERA 609042-14 AD REV O MATCHES PRI 609042-14 AD REV O. COMPLIED WITH PRI 609042-14 AD REV O., FINAL ERA 609042-14 AD REV O MATCHES PRI 609042-14 AD REV O. CORRECT NUT INSTALLATION AND WASHER INSTALLATION ON WORSDR SWAA2023062752378Bracket · crackedLH WING UPPER FIXED T/E SHELF PANEL BULB SEAL BRACKET CRACKED ABOVE AFT ENGINE PYLON FAIRING (AREA MARKED)<[01] REMOVED BULB SEAL BRACKET PER SRM 51-40-02.;[02] INSTALLED NEW L/H WING T/E SHELF PANEL BULB SEAL BRACKET (115A2953-1) ABOVE AFT ENGINE PYLON FAIRINSDR SWAA2023062752375Bracket · crackedLH WING UPPER FIXED T/E SHELF PANEL CORNER BRACKET CRACKED INBD OF DEFLECTION RIB (AREA MARKED BETWEEN #5 AND #6 SPOILER)<[01] REMOVED CRACKED CORNER CLIP PER SRM 51-40-02.;[02] DRILLED AND INSTALLED NEW I/B CORNER CLIP COMMON TO DEFLECTION CONTROL RIB ONLY. LSDR VNAA202306230021Skin · dentedDENTS (2EAS) ON UPPER SKIN INBOARD FLAPS AT RH WING ZONE 684. DENTS (2EAS) ON UPPER SKIN INBOARD FLAPS AT RH WING WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 57-52-01-101-001-A01, WERE REPAIRED PER REO 690-57-52-451 REV -- AND STEPS OF EA 23-C9-57-0692 REV. SDR VNAA202306230010Skin · nickedSEVERAL NICKS ON LOWER/FWD FACE OF RH INBOARD FLAP FROM FLS 15.00 TO FLS 65.50. LOWER/FWD FACE OF RH INBOARD FLAP FROM FLS 15.00 TO FLS 65.50 WAS REPAIRED PER CRJ-900 SRM 57-52-01-201-005-A01SDR FDEA202305250939Flap · damagedLEFT INBOARD FLAP OUTBOARD UPPER SKIN PREVIOUS SKIN REPAIR CHAFFED AND CRACKED. REPAIRED PREVIOUS DAMAGED AREA ON LEFT I/B FLAP O/B UPPER SKIN IAW B757 SRM 51-70-10- 2R. MAJOR REPAIRSDR SWAA2023061952037Flap · delaminatedRIGHT HAND WING OUTBOARD AFT FLAP IS DELAMINATED ON THE INBOARD END.<[01] REMOVED R/H WING 'O/B AFT FLAP' IAW AMM 27-51-22.;[02] INSTALLED SERVICEABLE R/H O/B AFT FLAP REF AMM 27-51-22;[03] RII: INSPECTED WORK ACCOMPLISHED IN C/A# 2. THOMAS TESTEMENT (TECHNICISDR SWAA2023061952038Flap · delaminatedLEFT HAND WING OUTBOARD AFT FLAP IS DELAMINATED ON THE INBOARD END.<[01] REMOVED L/H WING; ' O/B AFT FLAP '; IAW AMM 27-51-22.;[02] ACCOMPLISHED INSTALLATION OF L/H WING; ' O/B AFT FLAP ' IAW AMM 27-51-22-400-801 UP TO AND INCLUDING STEPS 3. A;B;C;D;E; AND F. SDR SWAA2023061952046Flap · delaminatedRIGHT HAND INBOARD MAIN FLAP TRAILING EDGE WEDGE HAS LARGE AREA OF DELAMINATING (MKD)<[01] REMOVED DELAMINATED R/H I/B MAIN FLAP T/E WEDGE PER SRM 51-40-02.;[02] REMOVED PART FROM INVENTORY;[03] OKAY TO CLOSE RIGHT HAND INBOARD MAIN FLAP TRAILING EDGE WEDGE;[0SDR SWAA2023052551172Flap · delaminatedLEFT WING OTBD AFT FLAP HAS A DELAMINATION ON UPPER INBD SURFACE. DELAMINATED MEASURES 6'L X 4'W AND IS LOCATED 1.25' FROM T/E AND 1.5' FROM INBD EDGE<[01] CW EA UP TO STEP 6. ADHESIVE INJECTED AT 0540;[02] REPAIRED LEFT WING OTBD AFT FLAP PER EA 23-157-01651.SDR SWIA2024012630522Vane · chafedLEFT WING INBD FLAP VANE LEADING EDGE OUTBD CHAFFED MARKED (C-CHECK RO 1/24/2024) LEFT WING I/B FLAP VANE, O/B LEADING EDGE CHAFFE MARKS BLENDED AND FOUND TO BE BEYOND LIMITS IAW CRJ 200 SRM 57-52-00 AND REO 601R-57-52-004 REV-D, DATED 2012-12-19. FLAP VANSDR AALA202305264263Flap · delaminatedAIRCRAFT IN BASE MAINTENANCE: LEFT WING OUTBOARD TRAILING EDGE FLAP UPPER SURFACE DELAMINATED 138.75 INCHES FROM THE OUTBOARD EDGE AT LEFT WING RIB 10. REPAIRED FLAP PER EA 344153.SDR FDEA202305220913Flap · damagedLW INBOARD MAIN FLAP, UPPER SKIN HAS DAMAGE ON OB EDGE. REPAIRED LW INBOARD MAIN FLAP, UPPER SURFACE SKIN IAW FED EX EA H-5750-T0374477-P1- WING-FLIGHT SURFACES-LH INBD MAIN FLAP, FRANGIBLE STRUCTURE ASSY UPPER SKIN, NICK.SDR FDEA202305220912Flap · damagedRH WING INBD MAIN FLAP UPPER SURFACE HAS EDGE DAMAGE ON OUTBD END. REPAIRED RH WING INBD MAIN FLAP UPPER SURFACE ON OUTBD END IAW FED EX EA H-5750- T0374487-P1-WING-FLIGHT SURFACES-RH INBD MAIN FLAP, FRANGIBLE STRUCTURE ASSY UPPER SKIN NICK.SDR UIEA2023052300507Unknown · unknownDISBOND - R/H WING OUTBD AFT FLAP TOP PANEL(<P>1) CUT OUT THE DISBOND MATERIALS AND CLEAN. MEASURE THE CUT OUT (L =2" W= 1". 39" FROM INBD EDGE 5.5" FROM AFT EDGE. BOND THE FILLER AND EXTERNAL DOUBLER (L= 4.2", W=4") WITH FILM ADHESIVE CURE AT 250„‰ FOR 90 MISDR FDEA202305190910Flap · chafedRIGHT WING INBOARD FLAP LOWER SURFACE HAS CHAFFING WEAR MARKS ON EACH SIDE OF #6 FLAP FAIRING REPAIRED RIGHT WING INBOARD FLAP LOWER SKIN IAW B767 SRM 57-53-01-2R AND 51-70-03-0G.SDR FDEA202305190909Flap · gougedRIGHT WING INBOARD AFT FLAP HAS EDGE DAMAGE ON TRAILING EDGE UPPER SURFACE. REPAIRED RIGHT WING INBOARD AFT FLAP IAW B767 SRM 57-53-01-2R AND 51-70-10-2R.SDR FDEA202305190908Flap · gougedRIGHT WING INBOARD AFT FLAP HAS EDGE DAMAGE ON TRAILING EDGE UPPER SURFACE. REPAIRED RIGHT WING INBOARD AFT FLAP IAW B767 SRM 57-53-01-2R AND 51-70-10-2R.SDR SWIA202401260518Vane · chafedRIGHT INBOARD FLAP VANE LEADING EDGE HAS CHAFFING IN 3EA AREAS (C-CHECK RO 1/24/2024) RIGHT I/B FLAP VANE LEADING EDGE CHAFFING IN 3 AREAS BLENDED AND EVALUATED IAW REO 601R-57-52-004 REV.-D DATED 2012-12-19 PERMANENT REPAIR. I/B & CENTER LEADING EDGES ARESDR SWAA2023062649669Panel · crackedRT WING T/E PANEL 661BB AFT FASTENER HOLES ARE CRACKING AROUND EDGES<[01] IDENTIFIED PANEL 661BB IAW SRM 57-51-01-0I-1 FIGURE 3; TABLE 2; ITEM (9).<BR><BR>PANEL IS BEYOND ALLOWABLE DAMAGE LIMITS IAW SRM 57-51-01-1A-1 PARA 4 B (5)(A).<BR><BR>DAMAGE TO BE REPAIRSDR SWAA2023062163446Panel · crackedRT WING T/E PANEL 661BB AFT FASTENER HOLES ARE CRACKING AROUND EDGES<DAMAGE TO BE REPAIRED IAW SRM 51-70-04-2R-9 AS DIRECTED BY SRM 57-51-01-2R-1 PARA 4 B (2) TABLE 202.<BR><BR>REMOVED DAMAGE TO (52EA) FASTENER HOLES ALL TO A MEASURE OF .5'DIA; CLEANED; WITH NSDR CALA2023051901576Spar · loose#1 FLAP, O/B ATTACH POINT TO FLAP CARRIAGE IS LOOSE AND HAS THREE SHEARED/MISSING BOLTS/HI-LOCS. 5753-02106 REV. -. GENERATED 2 EA ELB LOG PAGES #''S 4615060 AND PAGE LIMITS PER STEP 19 ARE "ACCOMPLISH INITIAL INSPECTION PER CYCLES". 4615786 FOR DIP ENTRIES SDR EBVR202305180002Flap · debondedON LH OB FLAP 1.6 INCHES FROM INBOARD EDGE NEAR DATA TAG, THERE WAS A SPOT OF DISBONDING 7.6 INCHES SQUARE. AQRD REPAIRED AND REPAINTED THE FLAP IAW AQRD RS-825274 REV B DATED 10/31/22 & AQRD 912781 REV A DATED 04/11/2022. THIS WAS A MAJOR REPAIR.SDR ABXA20230623130Flap · dentedWHILEIN C-CHECK IN HAECO MAINTENANCE DISCOVERED R/W I/B FLAP, AFT FLAP TOP SIDE HAS A DENT. MARKED IN RED. EVALUATED DENT ON R/W I/B FLAP AFT FLAP UPPER SURFACE LOCATED 59.25" FROM O/B EDGE 14.5" FROM THE T/E. DENT MEASURE 3.1" LONG, .7" WIDE, .0075 DEPTH IAW SDR SWAA2023062149667Flap · delaminatedLT WING O/B AFT FLAP HAS AREA OF DELAMINATION ON UPPER SURFACE NEAR I/B AFT CORNER.<[01] IDENTIFIED AFT FLAP IAW SRM 57-53-01-0I-4; FIG 2; TABLE 2; ITEM 2.<BR><BR>DAMAGE IS BEYOND ALLOWABLE DAMAGE LIMITS IAW SRM 57-53-01-1A-4 PARA 4.A (5).<BR><BR>DAMAGE IS REPSDR UIEA2023052200499Flap Track · corrodedFOUND #6 FLAP TRACK INBD SIDE CONTACT WITH SIDE LOAD FITTING SURFACE CORROSION(<P>1) REF EI T2023A57M-923 REV 1 SEQUENCE A, PERFORM #6 FLAP TRACK PERMANENT REPAIR. 2) CONDITION CHECK NORMAL</P>)SDR FDEA202305161060Flap · chafedR/H WING OUTBD FLAP CHAFFED ON UPPER SIDE NEAR SPOILER #10 PERFORMED TRAILING EDGE FLAP NOSE SKIN REPAIR - AREA ADJACENT TO A NOSE RIB, PER SRM 57-53-01-2R, REPAIR 3, FIG. 201 SEE FEDEX E.A F-5750-T0374851 FOR TRACKING. MAJOR REPAIRSDR DALA2023051703932Unknown · unknownSHIP 3278 RH FLAP TRUNNION DAMAGE PRIOR BLENDING EXCEEDS MAX LIMITS OF .236", X=.307", Y=.309", DEPTH=.249" TRUNNION DIAMETER 3.000". CORRECTIVE ACTION: COMPLIED WITH ERA 608693-14AD. (2769967)SDR DALA2023051703931Unknown · unknownSHIP 3278 LH FLAP TRUNNION DAMAGE EXCEEDS MAX DEPTH OF .236 BEFORE BLENDING. X=.258, Y=.330, DEPTH=.249 TRUNNION DIAMETER MEASURES 3.020. CORRECTIVE ACTION: COMPLIED WITH ER/A 608691-14AD. (2769961)SDR FDEA202305160873Flap · delaminatedLH OB FLAP LWR SURFACE FROM OB TO IB 124INCH CROSS TE TO LE 7INCH FOUND DELAMINATION . EVALUATED LH OB FLAP LWR SURFACE FROM OB TO IB 124INCH CROSS TE TO LE 7INCH. DELAMINATION DAMAGE SIZE LXW=2"X1.5" OUT OF ALLOWABLE LIMIT. AS PER B777 SRM 57-53-01- 1ASDR SWAA2023062148570Panel · crackedCRACK INTERNAL AREA FLAP TRACK FAIRING ACCESS PANEL 642BB AT RT WING 2023-330139<[01] TOOL USED CALIPER P/N: 500-193-30 S/N: 0000288 DUE DATE: 27-DEC-23.;[02] TOOL USED. HOT BONDER PN: HCS9200B-AV SN: 18196126; DUE DATE 26-MAR-24;[03] TOOL USED: SCALE PN: SPX6SDR SWAA2023052248534Bracket · crackedRIGTH WING LOWER I/B FIXED TRAILING EDGE BRACKET CRACKED<[01] INSTALLED NEW BRACKET AT RIGTH WING LOWER I/B FIXED TRAILING EDGE PER SRM 51-40-02-0G-0;[02] VERIFIED INSTALLATION NEW BRACKET AT RIGTH WING LOWER I/B FIXED TRAILING EDGE.SDR CALA2023051501519Skin · damagedRIGHT WING IB FLAP BOTTOM SKIN HAS EXPOSED COMPOSITE PER HAECO L CQ NR 9292364/38364 GENERATED BY V921755 ACCOMPLISHED REPAIR PER HAECO REO - L24430 REV IR WITH NO DEVIAT ACCMP BY MECH V955356 INSP BY V916884 IONS NOTE: HAECO REO-L24430 REV IR IS INCLUDED WITHSDR FDEA202305130963Flap · dentedRH WING CTR FLAP L/E LWR SURFACE DENT AT O/B EDGE-11", D NOSE T/E -3.125". PFM CUT OUT REPAIR AND MADE THE REPAIR PARTS TO INSTALLED ON REPAIR AREA I.A.W A300- 600F SRM 57-50-00-201, PARA .4H, P201-P236 ,FIG 208. THIS IS CAT B REPAIR REFER CHAPTER TO SRI: 5SDR IPXA2023052535629Flap · dentedLT I/B MAIN T/E FLAP HAS DENT EO 86959 REQ 2 PREVIOUSLY C/W ON T3F18E001TM9H, PLS SEE NEW FAULT T3F18E001TNY5SDR IPXA2023051535629Unknown · unknown**SDR FILED OPEN**LT I/B MAIN T/E FLAP HAS DENT COMPLIED WITH STEPS 1-5 OF EO 86959-PRELIM1SDR CALA2023051501501Skin · puncturedRIGHT WING, INBRD FLAP CENTER BOX LOWER SKIN AT RIB 5 PUNCTURED. ORIGINAL LP4580291 CLOSED INADVERTENTLY. ACCOMPLISHED REPAIR PER HAECO REO - L24430 REV IR WITH NO DEVIAT IONS NOTE: HAECO REO-L24430 REV IR IS INCLUDED WITHIN ECRA AS FI GURES 1-14 FOR REFERENCESDR DALA2023051503796Unknown · unknownSHIP 3278 DAMAGE TO RH INBD FLAP TRUNNION. CORRECTIVE ACTION: COMPLIED WITH ERA 608693-14AD. (2764370)SDR DALA2023051503795Unknown · unknownSHIP 3278 DAMAGE TO LH INBD FLAP TRUNNION. CORRECTIVE ACTION: COMPLIED WITH ERA 608691-14AD. (2764279)SDR A6WA202305118599Vane · chafedLH WING INBOARD FLAP IB FLAP HAS CHAFFING PN 601R14303-41 LH WING LEADING EDGE SKIN MID IB FLAP PN 601R14303-39 ****AIRCRAFT REMOVED FROM SERVICE********* LH WING INBOARD FLAP IB FLAP HAS CHAFFING PN 601R14303-41 LH WING LEADING EDGE SKIN MID IB FLAP PN 601R14
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