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 DALA2023063005257Flap · dented(LOG 2835506) I/B MAIN AFT FLAP HAS MULTIPLE DENTS LOWER SIDE. REPLACED LH IB AFT FLAP IAW B737-800 AMM 27-51-12.SDR SWAA2023062671508Wedge · debondedL/H INBOARD MAIN FLAP WEDGE HAS DISBONDED REPAIR DOUBLER.<[01] REPAIRED MAIN FLAP WEDGE PER SRM 51-70-10-2R-2 AND SRM 51-70-2R-0 REF. FROM SRM 57-53-01-2R-7;[02] INSPECTION C/WSDR SWAA2023073183461Angle · crackedCRACK ANGLE TRAILING EDGE LOCATED ORSS307 LT WING 2023-404897<[01] REPLACED ANGLE AND FASTENERS LOCATED TRAILING EDGE LOCATED ORSS307 LT WING IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9 AND DWG 115A3700 SHEET 32 REV -. AND DWG 115A3712 SHEET 5 REV.-. SEESDR SWAA2023073184202Angle · crackedCRACK ANGLE TRAILING EDGE LOCATED ORSS307 LT WING 2023-404897<[01] REPLACED ANGLE AND FASTENERS LOCATED TRAILING EDGE LOCATED ORSS307 LT WING IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9 AND DWG 115A3700 SHEET 32 REV -. AND DWG 115A3712 SHEET 5 REV.-. SEESDR CALA2023062602036Panel · missingPANEL MISSING LT WING OUTBOARD FLAP OTBD END. FOR PANEL MISSING LT WING OTBD FLAP. RAN FLAPS TO VERIFY THEY OPERATE NORMAL, OP CHECKED GOOD. LT WING AUX TRACK FAIRING MISSING, COMPLIED WITH CDL. TOMC APPROVES THE USE OF CDL 57J FOR LT OTBD FLAP AUX. TRACK FASDR DALA2024041504398Vane · delaminatedFOUND TRAILING EDGE FLAP AFT MOVEABLE VANE DELAMINATED AND DISBOND ON LOWER SURFACE. MAINTENANCE REPAIRED THE AREA PER ERA 612964-14 REV ORIGINAL.SDR ASAA2023062244224Flap · dentedLESSOR ITEM 383: DENT DISCOVERED ON RIGHT HAND INBOARD FLAP TOP (UPPER SURFACE) GROUNDED - YES. CLEANED SANDED AND REPAIRED LESSOR ITEM 383, DENT ON RIGHT HAND INBOARD FLAP UPPER SURFACE 49" FROM INBD EDGE , 9" FROM T/E DIA 1" DEPTH .027, CATEGORY A POTTING PESDR SWAA2023072870139Panel · debondedCUSTOMER REQUEST - DEBONDED IB MAIN FLAP WEDGE PANEL LOWER SURFACE AT RT WING 2023-404776<[01] TOOL USED: CALIPER P/N:500-464 S/N:B17030933 DUE DATE: 17-OCT-23.;[02] TOOL USED: ULTRASONIC FLAW DETECTOR; P/N: EPOCH 650; S/N: 190984811 DUE DATE: 24-JAN-24;[03] TSDR FDEA202306211066Flap · dentedLEFT WING, OUTBOARD FLAP LOWER SKIN WITH DENT AT 6" FROM LOWER EDGE AND 21" FROM INBOARD EDGE D= 0.023" L= 2.250" W= 1.220" LEFT WING, OUTBOARD FLAP LOWER SKIN WAS REPAIRED IAW B767 SRM 57-53-01-2R, FIG 201 SHEET 1, 3-6 AND SRM 51-70-06-0G, FIG 9 SHEET SDR SWAA2023062759592Bracket · crackedPANEL 551FB OUTBOARD FORWARD BRACKET IS CRACKED<[01] REMOVED AND INSTALLED FORWARD OUTBOARD BRACKET ON PANEL 551FB PER SRM 51-40-02.;[02] VERIFIED REMOVAL AND REPLACEMENT OF FORWARD OUTBOARD BRACKET ON PANEL 551FB PER SRM 51-40-02.SDR SWAA2023062060905Panel · crackedRT WING UPPER SURFACE PANEL #651ET HAS APPROX 14 INCH CRACK<[01] REMOVED AND REPLACED PANEL PER AMM 57-50-01;[02] C/W INSPECTIONSDR IPXA2023062893534Tee Angle · crackedINSPECTION TYPE:3CR/H WING O/B FLAP O/B HINGE LWR TEE SUPPORT ANGLE IS CRACKED.REPLACED CRACKED TEE AT THE R/H WING O/B FLAP O/B HINGE LWR SUPPORT ANGLE IAW SRM 51-31-01 (MINOR)SDR FDEA202306141035Flap · delaminatedRIGHT WING I/B FWD FLAP I/B END UPPER SKIN DISBONDED. ACCOMPLISHED PERMANENT REPAIR OF DISBONDED UPPER SKIN ON R/W INBD FLAP BONDED PART 113N2324 IAW B757 57-53-01-2R FIG 201 DETAIL 3 AND SRM 51-70-10-2R-0G.SDR IPXA2023063093551Hinge · corrodedINSPECTION TYPE:3CL/H WING A/C SIDE O/B FLAP I/B HINGE #3 LUG BORE HAS CORROSION ATSTA XW=486.403.REPAIRED CORRODED HINGE ASSY. #3 LUG BORE AT THE L/H WING A/C SIDE O/B FLAP I/B HINGE AT STA XW=486.403 IAW VTSAA EA 011-5710-01-A9987 I/R AND UPS EO MD11-5740-87SDR SWAA2023062158464Fairing · elongatedDOT A24-2 #1 FLAP TRACK AFT FAIRING ASSY. AFT SEAL RETAINER HOLE ELONGATED IN COMPOSITE FAIRING SKIN.<[01] EVALUATED AND FOUND AFT SEAL RETAINING O/B HOLE ELONGATED IN SOLID LAMINANTE AS MARKED. FOUND TO BE REPAIRABLE IAW SRM 57-53-70-2R-1 STEP 2(B)(2) AND SRMSDR FDEA202306121025Flap · dentedRH WING, OUTBOARD FLAP, LOWER SURFACE WITH DENT AT 52" FROM OUTER EDGE AND 10.75" FROM LOWER EDGE. RH WING, OUTBOARD FLAP, LOWER SURFACE, DENT WAS REPAIRED IAW B767 SRM 57-53-01-2R FIG. 201 SHEET 6 REPAIR 1 AND SRM 51-70-06-0G PAR. 5.A. FIG. 9 REV. 85 DECSDR SWIA202307030611Flap Track · wornL/H WING FLAP TRACK 1A HAS THICKNESS REDUCTION OF .028". ASSET TC2-7153 DUE 11-17-23. (C-CHECK RO 6/30/2023) REMOVED AND REPLACED LH WING FLAP TRACK 1A. REF AMM 57-54-25. TW TC2-7216 DUE 5-17-24SDR AALA202307255569Bracket · wornAIRCRAFT IN BASE MAINTENANCE: RIGHT WING TRAILING EDGE INBOARD FLAP ATTACH FITTING / BRACKET FOR THE INTERCONNECTING STRUT IS WORN ON THE OUTBOARD SIDE OF THE FLAP BETWEEN RIBS 8 AND 9. REPLACED ATTACH FITTING / BRACKET PER SRM 51-42-11.SDR AALA202307259213Bracket · wornAIRCRAFT IN BASE MAINTENANCE: LEFT WING TRAILING EDGE INBOARD FLAP ATTACH FITTING / BRACKET FOR THE INTERCONNECTING STRUT IS WORN ON THE OUTBOARD SIDE OF THE FLAP BETWEEN RIBS 8 AND 9. REPLACED ATTACH FITTING / BRACKET PER SRM 51-42-11.SDR IPXA2023070893624Hinge · wornINSPECTION TYPE:3CR/H I/B FLAP O/B HINGE LOWER O/B LUG HOLE #6 IS OUT OF LIMITS AT STA XW=-254.REPAIRED HINGE ASSY AT THE R/H I/B FLAP O/B HINGE AT STA XW=-254 IAW VTSAA EA 011-5740-01-A9988 I/R, UPS EO MD11-5750-87385-A DATED 07/07/23 AND FAA FORM 8100-9 SIGNSDR IPXA2023070893623Hinge · wornINSPECTION TYPE:3CR/H I/B FLAP O/B HINGE LOWER I/B LUG HOLE #7 IS OUT OF LIMITS AT STA XW=-254.REPAIRED HINGE ASSY. AT THE R/H I/B FLAP O/B HINGE AT STA XW=-254 IAW VTSAA EA 011-5740-01-A9988 I/R, UPS EO MD11-5750-87385-A DATED 07/07/23 AND FAA FORM 8100-9 SIGSDR IPXA2023062893535Hinge · corrodedINSPECTION TYPE:3CR/H WING A/C SIDE O/B FLAP O/B HINGE #2 LUG BORE HAS CORROSION AT STA XW=-638.305.REPAIRED CORRODED #2 LUG BORE AT THE R/H WING A/C SIDE O/B FLAP O/B HINGE AT STA XW=-638.305 IAW VTSAA EA 011-5710-01-A9985 I/R AND UPS EO MD11-5740-87383-A DATSDR IPXA2023062893536Hinge · corrodedINSPECTION TYPE:3CR/H WING A/C SIDE O/B FLAP O/B HINGE #3 LUG BORE HAS CORROSION AT STA XW=-638.305.REPAIRED CORRODED #3 LUG BORE AT THE R/H WING A/C SIDE O/B FLAP O/B HINGE AT STA XW=-638.305 IAW VTSAA EA 011-5710-01-A9985 I/R AND UPS EO MD11-5740-87383-A DATSDR VNAA202306230019Skin · nickedSEVERAL NICKS ON LOWER SKIN OF RH INBOARD FLAPS FLS 15.00 TO FLS 65.5. NICKS ON LOWER SKIN OF RH INBOARD FLAPS BTW FLS 15.00 TO FLS 65.5 WERE BLENDED OUT PER CRJ900 SRM 51-12-00-001-001-A01, BTW FLS 42 TO FLS 65 WERE EVALUATED WITHIN LIMITS PER CRJ-900 SRM SDR VNAA202306230018Skin · dentedDENT (1EA) ON UPPER SKIN INBOARD FLAPS AT LH WING ZONE 584. DENT (1EA) ON UPPER SKIN INBOARD FLAPS AT LH WING ZONE 584 WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 57-52-01-101-001-A01 AND WAS REPAIRED PER EA 23-C9-57-0692 REV. IR SECTION III. PERMANENT REPAIRSDR VNAA202306230017Skin · nickedSEVERAL NICKS ON LOWER SKIN OF LH INBOARD FLAPS FLS 15.00 TO FLS 65.5 NICKS ON LOWER SKIN OF LH INBOARD FLAPS BTW FLS 15.00 TO FLS 65.5 WERE BLENDED OUT PER CRJ900 SRM 51-12-00-001-001-A01, BTW FLS 42 TO FLS 65 WERE EVALUATED WITHIN LIMITS PER CRJ-900 SRM SDR IPXA2023063093549Hinge · corrodedINSPECTION TYPE:3CL/H WING O/B FLAP I/B FWD HINGE AFTER REMOVAL OF BUSHING FOUND INCOMING #1 LUG BORE OUT OF LIMITS.REPAIRED HINGE ASSY. #1 LUG BORE AT THE L/H WING O/B FLAP I/B FWD HINGE IAW VTSAA EA 011-5710-01-A9987 I/R AND UPS EO MD11-5740-87381-A DATED 06SDR FDEA202306081053Flap · unknownAGING AIRCRAFT ASSESSMENT : EXISTING DOUBLER REPAIR FOUND ON RH I/B FLAP LWR SKIN BTW STGR 2.8~2.9,RIB 10~11 COMPLIED WITH ATTACHMENT B OF EO:E6-5100-7-5000 D7 PT1, TITLE:STRUCTURES-REPAIR CATALOG-A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 SDR FDEA202306081052Flap · unknownAIRCRAFT REPAIR ASSESSMENT : EXISTING DOUBLER REPAIR FOUND ON RH I/B FLAP UPR SKIN BTW STGR 2.1~2.2,RIB 5~9 COMPLIED WITH ATTACHMENT B OF EO:E6-5100-7-5000 D7 PT1, TITLE:STRUCTURES-REPAIR CATALOG-A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CSDR FDEA202306081051Flap · unknownAIRCRAFT REPAIR ASSESSMENT : EXISTING DOUBLER REPAIR FOUND ON RH I/B FLAP LWR SKIN BTW RIB 19~19A,T/E-12" COMPLIED WITH ATTACHMENT B OF EO:E6-5100-7-5000 D7 PT1, TITLE:STRUCTURES-REPAIR CATALOG-A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFRSDR IPXA2023070893618Bracket · corrodedINSPECTION TYPE:3CL/H WING A/C SIDE I/B FLAP O/B HINGE #3 LUG I/B FLAP I/B FACE HAS CORROSION AT STA XW=254.000.REPAIRED CORRODED HINGE BRACKET ASSY. AT THE L/H WING A/C SIDE I/B FLAP O/B HINGE AT STA XW=254.000 IAW VTSAA EA 011-5740-01-B0002 I/R, UPS EO MD11-SDR IPXA2023070893622Hinge · corrodedINSPECTION TYPE:3CL/H WING FLAP SIDE I/B FLAP O/B HINGE #7 LUG BORE HAS CORROSION AT STA XW=-254.REPAIRED CORRODED HINGE ASSY AT THE L/H WING FLAP SIDE I/B FLAP O/B HINGE AT STA XW=-254 IAW VTSAA EA 011-5740-01-B0017 I/R, UPS EO MD11-5750-87572-A DATED 07/07/2SDR IPXA2023070893621Hinge · corrodedINSPECTION TYPE:3CL/H WING FLAP SIDE I/B FLAP O/B HINGE #6 LUG BORE HAS CORROSION AT STA XW=254.REPAIRED CORRODED HINGE ASSY. AT THE L/H WING FLAP SIDE I/B FLAP O/B HINGE AT STA XW=254 IAW VTSAA EA 011-5740-01-B0017 I/R AND EO MD11-5750-87572-A DATED 07/07/23 SDR IPXA2023070893619Bracket · corrodedINSPECTION TYPE:3CL/H WING A/C SIDE I/B FLAP O/B HINGE #3 LUG O/B FACE HAS CORROSION AT STA XW=254.000.REPAIRED CORRODED HINGE BRACKET ASSY. AT THE L/H WING A/C SIDE I/B FLAP O/B HINGE AT STA XW=254.000 IAW VTSAA EA 011-5740-01-B0002 I/R, UPS EO MD11-5740-8756SDR IPXA2023070793611Bracket · corrodedINSPECTION TYPE:3CR/H WING A/C SIDE I/B FLAP O/B HINGE #3 LUG I/B FACE HAS CORROSION AT STA XW=-254.REPAIRED CORRODED HINGE AT THE R/H WING A/C SIDE I/B FLAP O/B HINGE IAW VTSAA EA 011-5740-01-B0006 I/R AND UPS EO MD11-5740-87565-A DATED 07/05/23 AND FAA FORM SDR IPXA2023070693600Bracket · corrodedINSPECTION TYPE:3CL/H WING A/C SIDE O/B FLAP O/B HINGE #3 LUG I/B FACE HAS CORROSION.REPLACED HINGE ASSY. AT THE L/H WING A/C SIDE O/B FLAP O/B HINGE IAW AMM 57-53-01-400-801. (MINOR)SDR IPXA2023070693599Bracket · corrodedINSPECTION TYPE:3CR/H WING A/C SIDE O/B FLAP O/B HINGE #1 LUG BORE HAS CORROSION.REPLACED HINGE ASSY. AT THE R/H WING A/C SIDE O/B FLAP O/B HINGE IAW AMM 57-53-01-400-801. (MINOR)SDR IPXA2023070693598Bracket · corrodedINSPECTION TYPE:3CR/H WING A/C SIDE O/B FLAP I/B HINGE #1 LUG BORE HAS CORROSION.REPLACED HINGE ASSY. AT THE R/H WING A/C SIDE O/B FLAP I/B HINGE IAW AMM 57-53-01-400-801. (MINOR)SDR IPXA2023070193574Lever · wornINSPECTION TYPE:3CL/H WING A/C SIDE I/B FLAP I/B ACTUATOR MOUNT BOTH BUSHING ARE MIGRATED AT STA XIFH=116.850.REPAIRED BOTH LUG BORE AT THE L/H WING A/C SIDE I/B FLAP I/B ACTUATOR MOUNT AT STA XIFH=116.850 IAW VTSAA EA 011-5700-01-A9982 I/R AND UPS EO MD11-574SDR SWAA2023061557099Flap · delaminatedLH OB AFT FLAP HAS DELAMINATION<[01] R&R LH OB AFT FLAP IAW AMM 27-51-22<BR>TORQUE WRENCH SN: 0410007017 CALC DUE DATE: 31 OCT 2023<BR>TORQUE WRENCH SN: DKG02732 CALC DUE DATE: 31 NOV 2023<BR>OPS CHECK GOOD;[02] VERIFIED THE FOLLOWING:<BR>R&R LH OB AFT FLAP IASDR FDEA202306070999Flap · dentedLH OB FLAP LWR SURFACE FROM IB TO OB 110INCH CROSS TE TO LE 6.2INCH FOUND ONE DENT. EVALUATED LH OB FLAP LWR SURFACE FROM IB TO OB 110INCH CROSS TE TO LE 6.2INCH DENT DAMAGE SIZE LXW=3.1"X1.5" OUT OF ALLOWABLE LIMIT AS PER B777 SRM 57-53-01-1A ALLOWABLE DASDR SWIA20230606Unknown · dentedR/H SIDE INBOARD FLAP CENTER LOWER SKIN HAS DENT (MARKED) (C-CHECK RO 7/23/2023) REPAIRED DENT ON R/H I/B FLAP LOWER SKIN REF CRJ 200 SRM 57-52-00, REPAIR #3, FIGURE 202. COMPLIED FULLY W/SKYCARD 51-900-1003-SKY.SDR DALA2023072105917Unknown · unknownSHIP 3116 CORROSION BONDING PLATE FLAP TRACK FAIRING 632CB ON RH WING. CORRECTIVE ACTION: REPAIRED PER ER/A 608480-14. (2803132).SDR DALA2023072105916Unknown · unknownSHIP 3116 CORROSION BONDING PLATE FLAP TRACK FAIRING 2 (531CB) ON LH WING. CORRECTIVE ACTION: REPAIRED PER ER/A 608480-14. (2803113)SDR DALA2023060704638Unknown · unknownAIRCRAFT 3116, CRACK FLAP TRACK FAIRING 633CB BONDING PLATE ON RH WING. CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTIONS ON FLAP TRACK FAIRING 633CB OF RH WING AS PER ER/A 608480-14 REV. ORIGINAL APPROVEDDATE: 30/MAY/23. SECTION I HAS BEEN COMPLIED WITH. (LP 2SDR IPXA2023070693597Bracket · corrodedINSPECTION TYPE:3CL/H WING O/B FLAP I/B HINGE HAS CORROSION AT THE LOWER I/B ATTACH POINT.REPLACED CORRODED HINGE ASSY. AT THE L/H WING O/B FLAP I/B HINGE IAW AMM 57-53-01-400-801. (MINOR)SDR LR7A2023060503292Baffle · crackedDURING SCHEDULED B-2 CHECK UNDER JOB CARD HB2703, FOUND RH OUTBOARD FLAP BAFFLE UPPER SKIN CRACKED AT OWFS0R. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-12. NR# 1000955655.SDR AALA202309066891Support · wornAIRCRAFT IN BASE MAINTENANCE: RIGHT WING INBOARD FLAP TRACK #1 FLAP DRIVE TRUNNION, TORSION SUPPORT ASSEMBLY AT FLAP RIB 1. REPLACED TORSION SUPPORT ASSEMBLY PER CMM 57-52-21.SDR IPXA2023063093553Hinge · corrodedINSPECTION TYPE:3CL/H WING A/C SIDE O/B FLAP O/B HINGE #3 LUG BORE HAS CORROSION AT STA XW=638.305.REPAIRED CORRODED HINGE ASSY. #3 LUGE BORE AT THE L/H WING A/C SIDE O/B FLAP O/B HINGE AT STA XW=638.305 IAW VTSAA EA 011-5740-01-A9986 I/R AND UPS EO MD11-5740-SDR IPXA2023063093552Hinge · corrodedINSPECTION TYPE:3CL/H WING A/C SIDE O/B FLAP I/B HINGE #2 LUG BORE HAS CORROSION AT STA XW=486.403.REPAIRED HINGE ASSY. #2 LUG BORE AT THE L/H WING A/C SIDE O/B FLAP I/B HINGE AT STA XW=486.403 IAW VTSAA EA 011-5710-01-A9987 I/R AND UPS EO MD11-5740-87381-A DA
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