JASC 5754
Service difficulty reports · 17,344
Reports filed under 5754 · Leading Edge Devices, 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 = '5754' 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 = '5754' 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 AWXA200400513Skin · crackedMCN - MAJOR REPAIR - DURING C-17 CHECK FOUND A .25 INCH CRACK IN NR 5 SLAT LOWER SKIN AT FASTENER HOLES BELOW INBOARD AUXILIARY TRACK. MAINTENANCE REMOVED DAMAGE IN NR 5 SLAT LOWER SKIN; FABRICATED A FILLER AND SPLICE PLATE; INSTALLED REPAIR PARTS IAW B737-30SDR SWAA041194Skin · crackedDURING SCHEDULED C1 CHECK, FOUND LT WING NR 2 L/E SLAT SKIN AT INBOARD EDGE CRACKED. REPAIRED SLAT SKIN PER EA.SDR ASAA0410213Skin · crackedDURING C-CHECK, FOUND RT OUTBOARD SLAT CRACKED AND DELAMINATED AT UPPER TRAILING EDGE. REMOVED DAMAGE AND INSTALLED DOUBLER IAW EA 5740-01391. (M)SDR C1HA200485004Wedge · gougedNR 6 SLAT CRACK AT FASTNER HOLE/2 GOUGES IN WEDGE EXTRUSIONSDR 2004UALA00414Wedge · delaminatedT/E WEDGE DELAMINATED AT OTBD TRACK AREA LOWER SURFACE. MAJOR REPAIR ACCOMPLISHED. T/E WEDGE SKIN REPLACED & REPAIRED.SDR DHL2004803541Skin · corrodedRT WING INBOARD SLOT L/E UPPER SKIN CORRODED AT XILD 42.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DWG V43-R03, ED EDV43-3. REMOVED FASTENERS IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 21, SRM 51-3-0 PG 1. TRIMMED OUT DAMAGED AREA IAW DWG V43-R03, ED EDV43-3SDR DHL2004803538Vane · elongatedLT WING IB. VANE SLOR HOLES ELONGATED STA XS 247.000. PERFORMED MAJOR REPAIR IAW ED EDV43-9, DWG V43-R09. REMOVED FASTENERS IAW SRM 51-1-21 PG.1, SRM 51-3-0 PG.1, SRM 51-1-20D PG.21. TRIMMED OUT DAMAGED SECTION IAW ED ECV43-9, DWG V43-R09. PERFORMED NDT INSP.SDR AWXA200400454Panel · crackedMCN - MAJOR REPAIR - DURING C-17 CHECK A 1 INCH CRACK WAS FOUND IN NR 5 SLAT OUTBOARD COVE PANEL SKIN AT STAB STA 255.7. MAINTENANCE REMOVED CRACKED NR 5 SLAT OUTBOARD COVE PANEL AT SS 255.7; FABRICATED A NEW REPLACEMENT PANEL PER DWG 65C26602; INSTALLED REPASDR SWAA041109Skin · crackedDURING SCHEDULED C1 CHECK, FOUND LT WING, NR 2 L/E SLAT LOWER SKIN AT AFT ROW OF RIVETS, CRACKED. REPAIRED NR 2 L/E SLAT SKIN PER SRM.SDR ABXA040157Clip · crackedWING LEADING EDGE SPLICE ANGLE AND DOUBLER CRACKED JUST OUTBOARD OF NR 6 SLAT TRACK. REPLACED ANGLE / DOUBLER IAW DC-9 SRM 51-30-2 AND 51-30-5.SDR 04FDEA00960Skin · dentedLT WING DENT MARK FOUND ON OUTBOARD NOSE SURFACE AREA OF SLAT NR 6. DENTED AREA AT LH WING OUTBOARD NOSE SURFACE OF SLAT NR 6 TRIMMED AS PER SRM 57-00-01, FIG.7, VOL. I. REPAIR PARTS FABRICATED & INSTALLED AS PER SRM 57-00-01, FIG.7, VOL.I & SRM 51-35-01,SDR UPS04242357Web · crackedINSPECTION TYPE: C, 5 FLAP ACTUATOR TRUNNION SUPPORT BOX I/B WEB CRACKED. K FLAP ACTUATOR REMOVED, TRUNNION SUPPORT BOX I/B WEB REMOVED. WEB FABRICATED IAW DWG 65-16263. NEW K FLAP ACTUATOR TRUNNION SUPPORT BOX I/B WEB FITTED IAW SRM 51-30-02SDR AWXA200400476Skin · delaminatedDURING C-17 CHECK FOUND THE UPPER NO. 5 SLAT WEDGE DELAMINATED AT SS 147.5. MAINTENANCE REMOVED PREVIOUSLY INSTALLED REPAIR DOUBLERS ON NO. 5 SLAT WEDGE AT SS 147.5; FABRICATED NEW REPLACEMENT DOUBLERS; BONDED REPAIR PARTS TO SLAT IAW B737-300 SRM 51-70-10, FISDR GTIA040401Rib · damagedFTW - FOUND RIGHT WING NR 5 SLAT OUTBOARD EDGE SEAL IS TORN. OUTBOARD RIB NR 5 SLAT REMOVED. FOUND RIB TO BE DAMAGED BEYOND REPAIR. NEW RIB SEAL AND RETAINER INSTALLED. (M)SDR UPS04242223Rib · crackedINSPECTION TYPE:C NR 3 L/E SLAT, CRACK AT ACTUATOR ATTACH RIB (O/B RIB). REPAIR CARRIED OUT IAW SRM 51-30-02, 51-30-03, 57-50-03 & MM 28-81-11 & 27-00-00.SDR UPS04242220Rib · crackedINSPECTION TYPE:C NR 2 L/E SLAT CLOSURE RIB AT INBOARD END OF SLAT CRACKED. REPAIR CARRIED OUT IAW SRM 51-30-02, 51-20-1 & MM 20-10-05.SDR UPS04242177Skin · crackedINSPECTION TYPE:C NR 4 K-FLAP HAS CRACK ON INNER ANTI-ICE SKIN AROUND RIVET HOLE I/B OF O/B ACTUATION LINKAGE FOR BULLNOSE. REPAIR CARRIED OUT IAW SRM 51-30-2, 57-50-3.SDR AWXA200400372Skin · crackedDURING C-15 CHECK 6 EACH .3125 INCH CRACKS WERE FOUND IN NR 2 SLAT LOWER SKIN EMANATING FROM FASTENER HOLES BELOW THE INBOARD AUXILIARY TRACK AT FS 134.0 LEFT. MAINTENANCE REMOVED DOUBLER OUTBOARD OF DAMAGED AREA; CUT OUT CRACKED AREA OF NR 2 SLAT LOWER SKIN;SDR 2004UALA00354Support · brokenTIE DUCT FLANGE & SUPPORT BRACKET BROKEN. REMOVED AND REPAIRED BROKEN TAI DUCT FLANGE AND BROKEN SUPPORT, REINSTALLED.SDR SWAA040968Skin · delaminatedDURING SCHEDULED SERVICE CHECK, FOUND LT WING NR 2 LEADING EDGE SLAT DELAMINATED. REMOVED AND REPLACED LT WING NR 2 LEADING EDGE SLAT PER MM.SDR 04FDEA00820Slat Track · crackedRT WING LEADING EDGE SLAT TRACK 16, I/B SUPPORT RIB FOUND CRACK. RT WING LEADING EDGE SLAT TRACK 16, I/B SUPPORT RIB REMOVED AND REPLACED AS PER SRM 51-31-01 VOL II.SDR 04FDEA00819Slat Track · crackedLEFT WING LEADING EDGE SLAT TRACK 16, I/B SUPPORT RIB FOUND CRACK. LT WING LEADING EDGE SLAT TRACK 16, I/B SUPPORT RIB REMOVED AND REPLACED AS PER SRM 51-31-01 VOL II.SDR MWEA040035Doubler · corrodedLEFT WING LEADING EDGE HAS CORROSION 12 FT OUTBOARD OF NR 1 SLAT INBOARD IDLER ARM. FABRICATED AND INSTALLED REPAIR DOUBLER.SDR ASAA0410156Skin · dentedOKC - DURING MAINTENANCE CHECK, FOUND NR 2 SLAT UPPER TRAILING EDGE SKIN DENTED AT TRACK AREA WING STATION 505. REPAIR IAW SRM. (M)SDR CALA0400243Skin · dentedINSPECTION FOUND LT WING NR 6 SLAT SKIN DENTED. REPAIRED IAW SRM 57-43-01, REPAIR 2.SDR GTIA040432Fitting · crackedRT NR 5 SLAT OB SEAL TORN. (EDGE SEAL) FURTHER INVESTIGATION FOUND END FITTING CRACKED. REMOVED RT NR 5 SLAT OB END FITTING. INSTALLED END FITTING.SDR SWAA040743Skin · delaminatedDURING SCHEDULED 1/2D CHECK, FOUND NR 2 AND NR 5 L/E SLAT TRAILING EDGES DELAMINATED. REPAIRED SLATS PER SRM.SDR GTIA040475Bracket · damagedTEMPORARY BLEND OUT REPAIR TO SLAT BRACKET (PN 9937501-2) RT WING STA 199. REMOVED TEMPORARY DOUBLER. FABRICATED -3 FILLER AND -5 DOUBLER IAW EA 2780-0405. INSTALLED -3 FILLER AND -5 DOUBLER.SDR AWXA200400299Skin · crackedPHX - MAJOR REPAIR - DURING 8-DAY CHECK SEVERAL CRACKS WERE FOUND PROGRESSING FROM RIVET HOLES ON LOWER LT EDGE OF NR 2 SLAT, SLAT STA 200. MAINTENANCE CUTOUT DAMAGE ON LOWER LT EDGE OF NR 2 SLAT, AT SLAT STA 200; FABRICATED A FILLER AND DOUBLER; INSTALLED RESDR SWAA040729Skin · crackedDURING SCHEDULED 1/4D CHECK, FOUND NR 3 L/E SLAT LOWER SKIN SURFACE CRACKED 30 INCHES FROM INBD END. REPAIRED SLAT SKIN PER SRM.SDR AWXA200400255Skin · crackedLCQ - MAJOR REPAIR - DURING C-12 CHECK A 1.5 INCH CRACK WAS FOUND BETWEEN TWO RIVET HOLES ON LOWER EDGE OF NR 3 SLAT WS 321.5. MAINTENANCE CUT OUT DAMAGE ON LOWER EDGE OF NR 3 SLAT AT WS 321.5; FABRICATED A FILLER & DOUBLER; INSTALLED REPAIR PARTS IAW B737-30SDR AWXA200400316Wedge · debondedMCN - MAJOR REPAIR - DURING C-15 CHECK THE NR 5 SLAT WEDGE WAS FOUND DISBONDED ON UPPER SURFACE ABOVE ACTUATOR. MAINTENANCE REMOVED EXISTING REPAIR ON UPPER SURFACE OF NR 5 SLAT WEDGE ABOVE ACTUATOR; FABRICATED A DOUBLER & REPAIR CORE; INSTALLED REPAIR PARTS SDR AWXA200400315Wedge · debondedMCN - MAJOR REPAIR - DURING C-15 CHECK THE NR 5 SLAT WEDGE WAS FOUND DISBONDED ON LOWER SURFACE ABOVE ACTUATOR. MAINTENANCE CUT OUT DAMAGED AREA OF NR 5 SLAT WEDGE; FABRICATED A DOUBLER & FILLERS; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-70-10 FIG 23 PG 85JSDR AWXA200400314Wedge · debondedMCN - MAJOR REPAIR - DURING C-15 CHECK THE NR 6 SLAT WEDGE WAS FOUND DISBONDED ON UPPER SURFACE AT INBOARD END AND BETWEEN OUTBOARD MAIN & AUXILIARY TRACKS. SLAT BEYOND ECONOMICAL REPAIR, REMOVED AND REPLACED NR 6 SLAT.SDR AWXA200400313Wedge · debondedMCN - MAJOR REPAIR - DURING C-15 CHECK THE NR 3 SLAT WEDGE WAS FOUND DISBONDED ON THE UPPER SURFACE AT INBOARD CORNER. MAINTENANCE CUT OUT DISBONDED AREA OF SKIN ON UPPER SURFACE OF NR 3 SLAT WEDGE; FABRICATED A FILLER & DOUBLER; INSTALLED REPAIR PARTS IAW B7SDR AWXA200400283Skin · crackedMCN - MAJOR REPAIR - DURING C-15 CHECK 2 CRACKS WERE FOUND ON NR 6 SLAT LOWER SKIN BELOW ACTUATOR WBL 440.98 RT. MAINTENANCE CUT OUT DAMAGE ON NR 6 SLAT LOWER SKIN WBL 440.98 RT; FABRICATED A FILLER AND SPLICE PLATE; INSTALLED REPAIR PARTS IAW B737-300 SRM 57SDR AWXA200400244Skin · crackedMCN - MAJOR REPAIR - DURING C-15 CHECK 2 CRACKS WERE FOUND ON NR 3 SLAT LOWER SKIN BELOW ACTUATOR AT WBL 234.4. MAINTENANCE CUTOUT DAMAGE ON NR 3 SLAT LOWER SKIN WBL 234.4; FABRICATED A FILLER AND DOUBLER PER DWG 65C26603; INSTALLED REPAIR PARTS IAW 57-43-01 SDR AWXA200400241Skin · crackedLCQ - MAJOR REPAIR - DURING C-12 CHECK A 2 INCH CRACK WAS FOUND AT RIVET HOLE ALONG LOWER AFT EDGE OF NR 6 SLAT, SPAR STA 597. MAINTENANCE CUT OUT DAMAGE ON NR 6 SLAT AT SPAR STA 597; FABRICATED A FILLER & REPAIR DOUBLER; INSTALLED REPAIR PARTS IAW B737-300 SSDR UPS04M42511Slat Track · crackedINSPECTION TYPE: C, LT WING SLAT TRACK NR 16, 11B WEB SUSPECTED CRACK. HFEC INSPECT FOUND CRACK APPROX .375 INCH LENGTH. REMOVAL CUTOUT FOR ACCESS AS PER 27-80-32 R45. CRACK I/B WEB RIB AT LT WING SLAT TRACK NR 16 REMOVED AS PER SRM 51-33-01 & 51-35-01 V2RSDR UPS04M42510Slat Track · crackedINSPECTION TYPE: C, RT WING SLAT TRACK NR 16, I/B WEB SUSPECTED CRACK. HFEC INSPECT CUTOUT FOUND TEAR AT LHW SLAT TRACK NR 16 I/B WEB. REMOVAL ACCESS AS PER AMM 27-80-32 R45. CRACKED I/B WEB AT RHW SLAT NR 16 REMOVED PER SRM 51-33-01 & 51-35-01 V2R34. PICKSDR CALA0400201Skin · gougedINSPECTION FOUND RT UPPER WING L/E SKIN GOUGED BETWEEN NR 5 AND NR 6 SLAT, AT WS 250. REPAIRED IAW SRM 51-70-17.SDR 04FDEA00542Slat Track · crackedLT WING SLAT TRACK 16 I/B SUPPORT RIB FOUND CRACKED. LT WING SLAT TRACK NR 16 I/B SUPPORT RIB REMOVED AND REPLACED AS PER SRM 51-31-01 VOL. II.SDR ASAA0480142Slat Track · gougedOKC - DURING HV6 CHECK, FOUND NR 2 SLAT LEFT NR 8 TRACK HORN IS GOUGED ALONG LOWER EDGE. REMOVED DAMAGED SECTION AND PERFORMED HFEC REPAIR PER EA 5740-01380. (M)SDR ASAA0480141Skin · corrodedOKC - DURING HV6- CHECK - FOUND NR 1 SLAT FORWARD INBOARD PIN MATING SURFACE AND CASTING HOLE IS CORRODED. REAMED HOLE AND INSTALLED BUSHING EPR EA 5740-01382. (M)SDR DHL2004750026Rod End · crackedDURING C-CHECK, NR 7 SLAT AT ACT ROD END HAS INBOARD ATTACH FRAME CRACKED IN LOWER FWD RADIUS. REMOVED CRACKED RIB, LOCATED, DRILLED AND INSTALLED NEW RIB P/N 65-17310-3, PO 413646 IAW B727 SRM 51-30-2 FIG 1 & 2. ACCOMPLISHED L/E FLAPS OP'S CHECK FOUND OK IASDR 2004UALA00214Wedge · separatedSEPARATION OF TRAILING EDGE WEDGE. REPLACED T/E WEDGE. REPAIRED LOWER SEAL PANELS.SDR DHL2004750019Rod End · crackedDURING -C- CHECK, NR 2 SLAT AT ACT ROD END ATTACH HAS INBOARD ATTACH FRAME CRACKED IN FWD LOWER RADIUS. REMOVED AND REPLACED AT NR 2 SLAT AT ACT ROD END ATTACH HAS INBOARD ATTACH FRAME BY FWD LOWER 2 EA RIB SUPPORT PO 413627 P/N 65-17310-4 AND PIL 413644 P/NSDR DHL2004750018Frame · crackedDURING -C- CHECK, NR 3 SLAT AT ACT ROD END HAS OUTBOARD ATTACH FRAME IS CRACKED IN AFT RADIUS. REMOVED AND REPLACED NR 3 SLAT AT ACT ROD AND OUTBOARD ATTACH FRAME AFT 2 EA RIB SUPPORT PO 4136-27 P/N 65-17294-13 AND PO 413643 P/N 65-17294-14 IAW B727 SRM 51-30SDR DHL2004750017Rib · crackedDURING -C- CHECK, DISCREPANCY AS FOLLOWS; NR 7 SLAT INTERIOR RIB O/B OF ACTUATOR ATTACH POINT CRACK INDICATION WS 640 NDT CONFIRMED. REMOVED CRACKED RIBS LOCATED, DRILLED AND INSTALLED NEW RIB P/N 65-17310-4, PO 410362 IAW B727 SRM 51-30-2, FIG 1 & 2.SDR SWAA040549Wedge · delaminatedDURING SCHEDULED C4 CHECK, FOUND RT WING NR 4 L/E SLAT WEDGE IS DELAMINATED AT T/E. REMOVED AND REPLACED NR 4 SLAT PER MM.
Back to JASC 5754