JASC 5753
Service difficulty reports · 31,521
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 04FDEA00446Hinge · corrodedLEFT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), INBOARD PIVOT HOLE SPOT FACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-74320 - WINGS - LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED.SDR 04FDEA00445Hinge · corrodedLT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT HOLE INBOARD BORE CORRODED. COMPLIED WITH FEDEX EA 1-5750-74320 - WINGS - LT AND RT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED.SDR 04FDEA00444Hinge · corrodedLEFT WING - OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT HOLE OUTBOARD BORE CORRODED. COMPLIED WITH FEDEX EA 1-5750-74320 - WINGS - LT AND RT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED.SDR 04FDEA00443Hinge · corrodedLEFT WING - OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT INBOARD BORE CORRODED. COMPLIED WITH FEDEX EA 1-5750-74320 - WINGS - LT AND RT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED.SDR 04FDEA00442Hinge · corrodedLEFT WING - OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT OUTBOARD BORE CORRODED. COMPLIED WITH FEDEX EA 1-5750-74320 - WINGS - LT AND RT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED.SDR 04FDEA00441Hinge · corrodedRT WING - OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), OUTBOARD PIVOT HOLE SPOT FACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-74320 - WINGS - LT AND RT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED.SDR 04FDEA00440Hinge · corrodedLT WING - OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT OUTBOARD HOLE SPOT FACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-74320 - WINGS - LT AND RT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED.SDR 04FDEA00439Hinge · corrodedLEFT WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT INBOARD HOLE SPOT FACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-74319 - WINGS - LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED.SDR 04FDEA00438Hinge · corrodedLT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT OUTBOARD HOLE SPOT FACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-74319. LT AND RT OUTBOARD FLAP INBOARD HINGE BRACKET BORE CORRODED.SDR 04FDEA00437Hinge · corrodedLEFT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT INBOARD BORE CORRODED. COMPLIED WITH FEDEX EA 1-5750-74319 - LT AND RT OUTBOARD FLAP INBOARD HINGE BRACKET BORE CORRODED.SDR 04FDEA00436Hinge · corrodedLT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT OUTBOARD BORE CORRODED. COMPLIED WITH FEDEX EA 1-5750-74319 - LT AND RT OUTBOARD FLAP INBOARD HINGE BRACKET BORE CORRODED.SDR 04FDEA00435Hinge · corrodedLT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), PIVOT HOLE INBOARD BORE CORRODED. COMPLIED WITH FEDEX EA 1-5750-74319 - LT AND RT OUTBOARD FLAP INBOARD HINGE BRACKET BORE CORRODED.SDR SWAA040510Flap · delaminatedDURING SCHEDULED C1 CHECK, FOUND LT WING INBOARD AFT FLAP DELAMINATED ON T/E. REMOVED AND REPLACED LT WING INBOARD FLAP PER MM.SDR 04FDEA00428Fitting · crackedRIGHT WING : OUTBOARD TRAILING EDGE FLAP STOP FITTING FOUND CRACK. RT WING OUTBOARD TRAILING EDGE FLAP STOP FITTING REMOVED AND REPLACED AS PER SRM 51-31-01 VOL IISDR 04FDEA00429Fitting · crackedLEFT WING OUTBOARD TRAILING EDGE FLAP STOP FITTING FOUND CRACK. LT WING - OUTBOARD TRAILING EDGE FLAP STOP FITTING REMOVED AND REPLACED AS PER SRM 51-33-01 VOL II.SDR 2004F00163Skin · delaminatedAT C-CHECK, FOUND LEFT WING INBOARD MID FLAP LOWER SURFACE TRAILING EDGE WITH DELAMINATION. FABRICATED FILLER AND DOUBLER. CUT NEW CORE. BONDED, CURED, SANDED, CLEANED, TREATED, PRIMED AND SEALED. (M)SDR CALA0400131Attach Angle · crackedINSPECTION FOUND A 1.2 INCH CRACK IN NR 2 FLAP TRACK FAIRING ATTACH ANGLE. AN ANGLE REPAIR WAS INSTALLED IAW SRM 51-70-13.SDR IXXA0400024SSkin · wornDURING A ROUTINE C-CHECK INSPECTION RIGHT INBOARD FLAP UPPER PANEL DOUBLER HAS WEAR OUT OF LIMITS STA XW.104.000-110.000 MAJOR REPAIR. MAINTENANCE PERFORMED MAJOR REPAIR IN ACCORDANCE WITH DC8 STRUCTURAL REPAIR MANUAL 51-1-21A PG 1-4. FABRICATED NEW PLATING SDR 04FDEA00410Flap Track · wornLEFT I/B FLAP VANE CENTER TRACK WORN. APPLIED A LIGHT COAT OF MIL-G-81322 (MOBILE 28) GREASE TO THE LOWER SURFACE OF CENTRE VANE SUPPORT TRACK OF THE I/B FLAP LT AS PER FEDEX EA 1-5750-74226 PT1. WINGS - TE FLAPS - I/B TE FLAP VANE - CENTRE VANE SUPPORT TSDR SWAA040481Bearing · wornDURING THRU FLIGHT CHECK, FOUND LINEAR MOVEMENT WHEN PUSHING UP ON LT INBOARD CARRIAGE ON OUTBOARD LT FLAP. REMOVED AND REPLACED LT NR 2 MID FLAP CARRIAGE SPHERICAL BEARING PER MM.SDR IXXA0400023SSkin · wornDURING A ROUTINE C-CHECK FOUND RIGHT OUTBOARD FLAP UPPER PANEL DOUBLER HAS WEAR OUT OF LIMITS, STATION 159.00 - 213.00. MAINTENANCE REMOVED SKIN SEGMENT WITH DOUBLER ON IT. IN ACCORDANCE STRUCTURAL REPAIR MANUAL CHAPTER 57-1-0 AND 57-7-1 FIG 4 AREA WAS CLEANSDR OWF2004F00001Bracket · crackedBRACKET CRACKED FROM CORRODED FOUND DURING C CHECK INSPECTION. UNIT REPLACED WITH NEW PART.SDR SWAA040464Flap · brokenAIRCRAFT ROLLS LEFT WITH FLAPS AT 30 OR 40 DEGREES, REQUIRES A LOT OF AILERON TO HOLD LEVEL. REMOVED AND REPLACED LEFT OUTBOARD MID FLAP ASSEMBLY PER MM.SDR 2004FA0000262Hinge · crackedCONDUCTED ANNUAL INSPECTION ON AIRCRAFT. FOUND BOTH LEFT AND RIGHT WING FLAP CONTROL ROD ATTACH POINTS TO CONTROL SURFACES TO BE CRACKED. SPECULATE DAMAGE MAY HAVE BEEN INDUCED BY WIND ACTION AND LACK OF USE OF CONTROL SURFACE LOCK.SDR UPS04241973Flap Track · crackedINSPECTION TYPE: C, NR 7 FLAP TRACK FAIRING I/B TRACK CRACKED. REPLACED TRACK IAW DRW 65-21796 & SRM 51-30-02.SDR SWAA040459Skin · delaminatedDURING SCHEDULED C1 CHECK, FOUND RT WING INBOARD T/E FOREFLAP UPPER SURFACE DELAMINATED. REMOVED AND REPLACED INBOARD FOREFLAP PER MM.SDR 04FDEA00403Horn · corrodedRIGHT WING OUTBOARD FLAP VANE NR 1 FLAP VANE ATTACH HORN HAS PITTED AFT HOLE.SDR 04FDEA00404Skin · corrodedRIGHT WING OUTBOARD FLAP VANE NR 2 FLAP VANE ATTACH HORN HAS 2 CORRODED/PITTED HOLES. REPAIRED PER EA 8-5750-68462.SDR 04FDEA00405Skin · corrodedRIGHT WING OUTBOARD FLAP VANE, NR 3 FLAP VANE ATTACH HORN HAS TWO CORRODED/PITTED HOLES. REPLACED PER M/M 27-50-03-2 AND TORQUED PER M/M 20-50-20.SDR 04FDEA00406Skin · corrodedRT WING OUTBOARD FLAP, NR 4 FLAP VANE ATTACH HORN HAS 2 CORRODED AREAS AROUND HOLES. REPLACED NR 4 FLAP VANE ATTACH HORN PER M/M 27/50/03/2 AND TORQUED BOLTS PER M/M 20/50/20.SDR 04FDEA00408Skin · corrodedRIGHT WING OUTBOARD, D-FLAP, NR 5 FLAP VANE ATTACH HORN HAS TWO CORRODED / PITTED HOLES. REPLACED NR 5 FLAP VANE HORN PER M/M 27/50/03/2 AND TORQUED PER 20/50/02.SDR 04FDEA00401Bracket · crackedLEFT WING O/B FLAP I/B HINGE FAIRING (FLAP SIDE) AFT SUPPORT FOUND CRACKED. LT WING O/B FLAP I/B HINGE FAIRING (FLAP SIDE) AFT CRACKED SUPPORT REMOVED & FABRICATED AS PER DRWG ARC4230 (REF EARN 46) & INSTALLED AS PER AMM 20-50-02.SDR 04FDEA00400Bracket · brokenRIGHT WING I/B FLAP O/B HINGE FAIRING LOWEST O/B FAIRING SUPPORT BRACKET BROKEN. RH WING I/B FLAP O/B HINGE FAIRING LOWEST O/B FAIRING BROKEN SUPPORT BRACKET REMOVED & REPLACED AS PER SRM 51-33-01 VOL2.SDR AWXA200400220Skin · delaminatedMCN - MAJOR REPAIR - DURING C-04 CHECK THE LT INBOARD FLAP WAS FOUND DELAMINATED AT REPAIR ON LOWER SURFACE, OUTBOARD OF NR 2 FLAP FAIRING. MAINTENANCE REMOVED EXISTING REPAIR DOUBLER ON LOWER SURFACE, OUTBOARD OF NR 2 FLAP FAIRING; FABRICATED A NEW REPAIR DOSDR QXEA200400141Bracket · crackedPDX - SECONDARY FLAP DRIVE TORQUE SENSOR BRACKET IS CRACKED AT TOP LEFT HAND END OF BRACKET WHERE RIVETED TO REAR SPAR. REPAIRED IAW HORIZON AIE EA 2-27-252.SDR CALA0400100Skin · delaminatedINSPECTION FOUND THE NR 1 T/E FOREFLAP DELAMINATED BELOW NR 2 SPOILER PANEL, LT WING. THE FOREFLAP WAS REMOVED AND REPLACED IAW MM 27-51-37.SDR 04FDEA00394Support · gougedCOMPLY WITH EA 8-5750-73880 WINGS - INBOARD FLAP ACTUATOR SUPPORT ASSY BARREL NUT HOLE GOUGED. REPAIR P/N ARC0329-1. COMPLIED WITH EA 8-5750-73880.SDR AUS20040073Arm · corroded(AUS) FLAP SUPPORT ARM TO FLAP SUPPORT ARM RIB RIVETS MISSING DUE TO CORROSION.SDR UIEA200400013Panel · delaminatedDURING D-CHECK AT SIN, FOUND TOP PANEL P/N 65B08540-202 DELAMINATED. AREA AFFECTED EXCEED SRM REPAIR LIMITS. THE DAMAGED SKIN WAS REMOVED AND DISCARDED. A METAL TO METAL HOT BOND REPAIR WAS ACCOMPLISHED PER 747 SRM 51-40-06 SECTION 3 REQUIREMENTS. DETAIL VSDR UIEA200400012Spar · corrodedDURING DC-CHECK AT SIN, FOUND CORROSION ON THE LOWER SECTION OF THE UPPER T-CHORD OF SPAR NR 1 AND NR 2 OF RIGHT INOARD MID FLAP. FOUND ON ROUTINE CARD 12FM40010. CORROSION LEVEL 1. LOCALLY BLEND OUT CORROSION DAMAGE FROM THE EFFECTED CHORD FLANGE LOWER SURSDR DL73S040144Flap Track · corrodedTHE REAR ENGINE MOUNT ATTACH HOLES, LOCATED AT THE NR 2 AND NR 3 T/E FLAPS, OUTBOARD TRACKS WERE NOTED WITH CORROSION IN THE BORES. CORROSION WAS REMOVED AND TRACKS WERE REWORKED PER ERA 386130-14.SDR 04FDEA00380Fairing · crackedLEFT WING O/B FLAP I/B HINGE FAIRING FOUND O/B BRACKET CRACKED. LT WING O/B FLAP I/B HINGE FAIRING FWD OUTER CRACKED BRACKET REMOVED, FABRICATED, AS PER DRWG ARC7717 & COMPLIED AS PER EA 1-5750-74228. TE FLAP O/B TE FLAP AFT HINGE BRACKET AERODYNAMIC FAIRSDR ASAA0410054Access Panel · debondedOKC - DURING SCHEDULED C-CHECK, FOUND THE LEFT WING FLAP ACCESS PANEL AT WS 87.75-125.5 DISBONDED. REPAIRED PER EA. (M)SDR SWAA040424Spindle · brokenIN THE LANDING PHASE OF FLIGHT, WHEN FLAPS 30 WERE SELECTED, A LOUD POPPING/SNAPPING SOUND WAS HEARD, AND THE AIRCRAFT COMMENCED AN UNCOMMANDED ROLL TO THE RIGHT. NO ABNORMAL FLAP/LED INDICATIONS OBSERVED. 45 DEGREE YOKE DEFLECTION REQ'D TO LAND. FOUND OUTBSDR 04FDEA00359Track · chafedLEFT I/B FLAP CTR VANE TRACK CUTOUT HAS CHAFE MARK ON I/B & O/B FITTING AND SKIN. LT I/B FLAP CTR VANE TRACK CUTOUT HAS CHAFE MARK ON I/B & O/B - CHAFE MARK AT I/B & O/B SKIN EDGE TRIMMED 0.080 AS PER SRM 51-21-01 VOL 2 WITHIN LIMIT AS PER SRM 57-00-01 FISDR 04FDEA00360Support Bracket · corrodedLEFT O/B FLAP I/B HINGE O/B PIVOT HOLE CORRODED. LT O/B FLAP I/B HINGE O/B PIVOT HOLE CORROSION REMOVED & REPAIRED AS PER FEDEX EA 1-5750-75244 TITLE - WINGS - TE & TE DEVICES - LT O/B FLAP I/B SUPPORT BRACKET CORROSION REMOVAL & REPAIR.SDR 04FDEA00361Support Bracket · corrodedLEFT O/B FLAP I/B HINGE I/B PIVOT HOLE AND LUG CORRODED. LT O/B FLAP I/B HINGE I/B PIVOT HOLE & LUG CORRODED. LT O/B FLAP I/B HINGE I/B PIVOT HOLE & LUG CORROSION REMOVED & REPAIRED AS PER FEDEX EA 1-5750-75244 TITLE - WINGS - TE & TE DEVICES - LH O/B FLAP ISDR 04FDEA00362Support Bracket · corrodedLEFT O/B FLAP O/B HINGE O/B PIVOT HOLE CORRODED. LT O/B FLAP O/B HINGE O/B PIVOT HOLE CORROSION REMOVED & REPAIRED AS PER FEDEX EA 1-5750-75245 TITLE - WINGS - TE & TE DEVICES - LT O/B FLAP O/B SUPPORT BRACKET CORROSION REMOVAL & REPAIR.SDR 04FDEA00350Hinge · corrodedRIGHT O/B FLAP I/B HINGE (FLAP SIDE) I/B PIVOT HOLE AND LUG CORRODED. RT O/B FLAP I/B HINGE (FLAP SIDE) I/B PIVOT HOLE & LUG SURFACE CORROSION REMOVED & REPAIRED AS PER FEDEX EA 1-5750-74310. WINGS - RT O/B FLAP I/B AFT HINGE BRACKET BORE CORRODED.SDR 04FDEA00351Hinge · corrodedRIGHT O/B FLAP I/B HINGE (FLAP SIDE) O/B PIVOT HOLE CORRODED. RT O/B FLAP I/B HINGE (FLAP SIDE) O/B PIVOT HOLE CORROSION REMOVED & REPAIRED AS PER FEDEX EA 1-5750-74310. RT O/B FLAP I/B AFT HINGE BRACKET BORE CORRODED.
Back to JASC 5753