JASC 5754

Service difficulty reports · 17,348

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.

SDR DL72S960463Rib · crackedDURING INSPECTION, NR 6 L/E SLAT WAS FOUND WITH NR 1 L/E SUPPORT RIB CRACKED. REPAIRED PER MM 57-54-0.Jan 29, 1996 · N419DA · Boeing 727232SDR UPS805343Fitting · crackedMAINTENANCE REPORTED, FLAP FITTING CRACKED ON O/B FLAP I/B FITTING. REMOVED AND REPLACED FITTING.Jan 28, 1996 · N705UP · Doug DC871FSDR DL72S960219Skin · crackedNR 4 KRUEGER FLAP HAS TWO 1 INCH CRACKS AT O/B CUTOUT FOR LWR LIP ATTACH FITTING. REPAIRED PER SRM 57-50-3.Jan 28, 1996 · N517DA · Boeing 727232SDR DL72S960218Skin · crackedLOWER L/E SKIN CRACKED AND WORN AT FENCE ATTACH HOLE. SKIN WAS REPAIRED PER M/M 57-54-0. FOUND DURING SHOP INSPECTION OF NR 5 LE SLAT.Jan 28, 1996 · N408DA · Boeing 727232SDR DL72S960217Skin · crackedOUTER SKIN CRACKED AT FENCE ATTACH HOLE AND GROOVED AT REMAINING ATTACH HOLES. SKIN WAS REPAIRED PER M/M 57-54-0. FOUND DURING SHOP INSPECTION OF NR 5 L/E SLAT.Jan 28, 1996 · N408DA · Boeing 727232SDR DL72S960216Rib · crackedRIB WAS FOUND TO BE CRACKED ON INSPECTION. RIB WAS REPAIRED PER M/M 57-54-00. FOUND DURING SHOP INSPECTION OF NR 5 L/E SLAT.Jan 28, 1996 · N408DA · Boeing 727232SDR DL76L960192Slat · damagedTHE NR 7 SLAT TRAILING EDGE WEDGE LOWER SKIN WAS FOUND WITH A HOLE. THE HOLE IS .5 INCH IN DIAMETER AND IS LOCATED 42 INCHES INBOARD FROM THE OUTBOARD EDGE AND 4 INCHES FOWARD OF THE AFT EDGE. THE TRAILING EDGE WEDGE IS MANUFACTURED WITH 0.016 5052-H38 FACE Jan 25, 1996 · N172DN · Boeing 767332SDR DL72S960198Angle · crackedFOUND DURING A-1 LETTER CHECK, .5 INCH CRACK NR 2 L/E SLAT COVE SKIN ATTACH ANGLE, ADJACENT TO O/B TRACK. REPAIRED PER M/M 57-54-0.Jan 25, 1996 · N489DA · Boeing 727232SDR P5CA9600042Flap · crackedFOUND CRACK ON LOWER EDGE OF LEADING EDGE FLAPS 6 AND 7. REPAIRED IAW SRM 51-40-09.Jan 24, 1996 · N855FT · Boeing 747124SDR P5CA9600041Panel · crackedFOUND CRACK ON LEADING EDGE FIBERGLASS PANEL ON LEADING EDGE FLAPS 6, 7, 10, 11. REPAIRED IAW SRM 51-40-09.Jan 24, 1996 · N855FT · Boeing 747124SDR P5CA9600040Skin · crackedFOUND TOP EDGE CRACKED ON LEADING EDGE FLAPS 19, 23 AND 25 RT WING. REPAIRED IAW SRM 51-40-09.Jan 24, 1996 · N855FT · Boeing 747124SDR DL72S960174Spar · crackedDURING SHOP INSPECTION FOR WING SLAT PANEL, FOUND LEADING EDGE SPAR HAD A TEMPORARY REPAIR. REPAIRED SPAR PER MM 7-54-0 FIG 802 A.Jan 24, 1996 · N536DA · Boeing 727232SDR UPS205331Slat · crackedWHILE IN FOR C-CHECK MAINTENANCE REPORTED, NR 5 SLAT AFT LOWER CHORD O/B END CRACKED. REMOVED AND REPLACED NR 5 SLAT IAW MM 27-81-11.Jan 23, 1996 · N934UP · Boeing 72721CSDR UPS205330Bonding Jumper · corrosionWHILE IN FOR C-CHECK MAINTENANCE REPORTED, NR 6 FLAP O/B LOWER BONDING JUMPER HAS CORROSION AROUND ATTACH BOLT UPPER END LOWER SURFACE. REMOVED AND REPLACED NR 6 K-FLAP IAW MM 27-81-01 AND 27-81-00.Jan 23, 1996 · N934UP · Boeing 72721CSDR UPS205329Angle · crackedWHILE IN FOR C-CHECK MAINTENANCE REPORTED, NR 7 SLAT I/B TRACK I/B RIB SUPPORT ANGLE CRACKED. REPAIRED IAW 57-50-03, 51-30-2, OHM 57-51-41, MM 27-81-11 AND SRM 51-20-1.Jan 23, 1996 · N934UP · Boeing 72721CSDR DL72S960177Angle · crackedFOUND DURING E-2 LETTER CHECK, NR 7 L/E SLAT COVE SKIN ATTACH ANGLE CRACKED .375 INCH BELOW TAI DUCT. REPAIRED PER M/M 57-54-0 FIG 805.Jan 23, 1996 · N405DA · Boeing 727232SDR DL72S960176Angle · crackedFOUND DURING E-2 LETTER CHECK, NR 2 L/E SLAT COVE SKIN ATTACH ANGLE CRACKED BELOW TAI DUCT. REPAIRED PER M/M 57-54-0 FIG 805.Jan 23, 1996 · N405DA · Boeing 727232SDR DL72L960208Ribs · crackedDURING INSPECTION, NR 6 L/E SLAT WAS FOUND WITH RIBS NR 12, 13, 14 AND 15 CRACKED. ACCOMPLISHED REPAIRS PER MM 57-54-0.Jan 19, 1996 · N504DA · Boeing 727232SDR 96FDEA00101K-Flap · corrodedNR 5 K-FLAP O/B LUB O/B SIDE UPPER MOUNT BOLT HAS CORROSION UNDER NUT. CORROSION WAS FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED NR 5 K-FLAP AND FUNCTIONAL CHECK IAW FEDEX MM 27-81-1.Jan 19, 1996 · N488FE · Boeing 727227SDR P5CA9600004Le Flap · bentFOUND LEADING EDGE FLAP NR 10 OUTBOARD CORNER FOLDED AND BENT. REPAIRED IAW SRM 57-50-03 AND INSTALLED PER SRM 51-30-02.Jan 18, 1996 · N855FT · Boeing 747124SDR DL757960136Te Wedge · delaminatedDURING INSPECTION, FOUND THE TRAILING EDGE WEDGE ON THE NR 4 SLAT DELAMINATED IN THE UPPER SKIN. THERE IS A PREVIOUS REPAIR DOUBLER THAT MEASURES 2 INCHES FORE/AFT AND 10 INCHES WIDE, INSTALLED IN THE DAMAGED REGION. REPAIRED TRAILING EDGE WEDGE IN ACCORDANCJan 18, 1996 · N646DL · Boeing 757232SDR DL757960124Te Wedge · delaminatedDURING INSPECTION, NR 8 L/E SLAT TRAILING EDGE WEDGE WAS FOUND DELAMINATED. REPLACED WEDGE PER SRM 57-43-07.Jan 18, 1996 · N634DL · Boeing 757232SDR DL72L960210Angle · crackedLOWER FWD ANGLE CRACKED AT NR 13 RIB. REPAIRED PER MM 57-54-0 PG 807A. ALSO, WIND EROSION FWD OUTER SKIN. REPAIRED L/E WIND EROSION PER SRM 57-50-3 FIG 8 FOR L/E SLAT NR 6.Jan 18, 1996 · N504DA · Boeing 727232SDR CAL960264Rib · chafedINSPECTION FOUND A .3125 INCH CHAFED HOLE IN WEB AT INNER SKIN FLANGE OF RT WING L/E SLAT NR 7 OUTBOARD RIB. THE AREA WAS DRESSED OUT. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 57-50-3, FIGURE 9. (X)Jan 18, 1996 · N17402 · Boeing 727243SDR DL72W960119Angle · crackedFOUND ON A1 LETTER CHECK, TWO .5 INCH CRACKS AT NR 2 L/E SLAT COVE SKIN ANGLE, BELOW TIA DUCT. REPAIRED PER MM 57-50-0.Jan 17, 1996 · N292WA · Boeing 727247SDR DL72S960104Angle · crackedFOUND DURING E-2 LETTER CHECK, .375 INCH CRACK NR 4 L/E SLAT COVE SKIN LWR ATTACH ANGLE AT O/B END. REPAIRED PER M/M 57-54-0 PAR 5A.Jan 16, 1996 · N408DA · Boeing 727232SDR DL757960090Te Wedge · delaminatedT/E WEDGE WAS FOUND TO BE DELAMINATED DURING SHOP INSPECTION FOR NR 5 L/E SLAT. THE NOTED T/E WEDGE WAS REPLACED PER SRM 57-43-02.Jan 15, 1996 · N607DL · Boeing 757232SDR DL72W960092Angle · crackedDURING C-1 LETTER CHECK, FOUND .5 INCH CRACK AT NR 2 L/E SLAT COVE SKIN ATTACH ANGLE BELOW I/B UPSTOP PAD. REPAIRED PER M/M 57-54-0.Jan 15, 1996 · N2811W · Boeing 727247SDR DL72E960086Rib · crackedSLAT NR 6, RIB NR 10 AND 12 CRACKED. REPAIRED PER M/M 57-54-0 FIG 814.Jan 14, 1996 · N2829W · Boeing 727247SDR DL72L961087Rib · crackedREPAIRED CRACKED RIB AS PER SRM 57-54-0 FIG 814.Jan 10, 1996 · N504DA · Boeing 727232SDR DL72S960475Rib · crackedUPON ROUTINE INSPECTION, A CRACK WAS FOUND ON 2ND RIB FROM I/B END. REPAIRED AS PER SRM 57-50-3 FIG 9, FOR NR L/E SLAT.Jan 9, 1996 · N419DA · Boeing 727232SDR 96FDEA00035Lug · corrodedNR 5 K-FLAP O/B LUG O/B SIDE UPPER MOUNT BOLT HAS CORROSION UNDER NUT. CORROSION WAS FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED NR 5 K-FLAP AND FUNCTIONAL CHECKED IAW FEDEX MM 27-81-1.Jan 8, 1996 · N488FE · Boeing 727227SDR DL72K960295Skin · crackedUPON ROUTINE INSPECTION, THE TAI DUCT SKIN CUTOUT WAS CRACKED. REPAIRED AS PER MM 57-54-0, FOR NR 1 L/E SLAT.Jan 7, 1996 · N481DA · Boeing 727232SDR DL72K960244Slat · crackedUPON INSPECTION FOR NR 1 LEADING EDGE SLAT, GROUND DAMAGE WAS FOUND. REPAIRED PER SRM 57-50-3.Jan 7, 1996 · N481DA · Boeing 727232SDR CAL960148Attachment · crackedSTATION 31J - INSPECTION FOUND A 1 INCH CRACK AT OUTBOARD BULL NOSE AFT LINKAGE ATTACHMENT OF RIGHT WING NR 4 KRUEGER FLAP. THE CRACK WAS STOP DRILLED. DOUBLERS AND ANGLES WERE FABRICATED AND INSTALLED IAW SRM 57-30-3, 51-10-2, AND 51-30-8. (M)Jan 6, 1996 · N73751 · Boeing 727227SDR DL72S960172Angle · crackedCRACK FOUND IN LWR AFT ATTACH ANGLE. REPAIRED PER M/M 57-54-00 FOR NR 4 L/E SLAT.Jan 5, 1996 · N495DA · Boeing 727232SDR DL72S960171Skin · crackedDURING INSP, THE FOLLOWING DAMAGE WAS FOUND REQUIRING MRR'S N/R 0058 CRACKS FOUND IN NR 9 AND NR 18 RIB. REPAIRED PER M/M 57-54-0 FIG 805. N/R 0059 CRACKS FOUND IN REPAIR DOUBLERS ON NR 11 AND 12 RIBS. REPAIRED PER M/M 57-54-00. N/R 0062 CRACK FOUND IN UPPJan 5, 1996 · N495DA · Boeing 727232SDR DL72S954793Skin · crackedFOUND DURING A-1 LETTER CHECK, NR 8 SLAT LWR COVE SKIN ATTACH ANGLE CRACKED AT I/B STOP PAD. REPAIRED PER M/M 57-54-0 PAR 12.Dec 28, 1995 · N497DA · Boeing 727232SDR DL72S954792Skin · crackedFOUND DURING A-1 LETTER CHECK, NR 7 SLAT LWR COVE SKIN ATTACH ANGLE CRACKED O/B END. REPAIRED PER M/M 57-54-0 PAR 5A.Dec 28, 1995 · N497DA · Boeing 727232SDR DL72W954736Angle · crackedNR 2 SLAT COVE SKIN ATTACH ANGLE AT TAI DUCT. PREVIOUS REPAIR DOUBLER CRACKED .25 INCH. FOUND DURING F-1 LTR CK TPAMM. REPAIRED PER 57-54-0.Dec 19, 1995 · N297WA · Boeing 727247SDR DL72W962734Skin · crackedAFT LOWER SKIN CRACKED I/B END. REPAIRED PER M/M 57-54-0.Dec 18, 1995 · N2807W · Boeing 727247SDR DL72S954727Angle · crackedFOUND DURING E-2 LETTER CHECK, NR 2 L/E SLAT COVE SKIN ATTACH ANGLE CRACKED UNDER TAI DUCT. REPAIRED PER M/M 57-54-0.Dec 18, 1995 · N521DA · Boeing 727232SDR CKSA95149Panel · corrosionKOSC - DURING C-CHECK INSPECTION, FOUND OUTBOARD SLOT INBOARD PANEL CORRODED AT LEADING EDGE. INSTALLED NEW OUTBOARD SLOT INBOARD PANEL IAW DC-8 SRM 57-2-0, 51-3-0 AND MM 27-41-2. (M)Dec 17, 1995 · N801CK · Doug DC855SDR CKSA95148Panel · corrosionKOSC - DURING C-CHECK INSPECTION, FOUND OUTBOARD SLOT OUTBOARD PANEL 1 SPOT CORROSION, 1 SCREW MISSING. INSTALLED NEW PANEL IAW DC-8 SRM 51-3-0 AND MM 27-41-2. (M)Dec 17, 1995 · N801CK · Doug DC855SDR EISA95527Rib · crackedFOUND NR 8 SLAT OUTBOARD TRACK, OUTBOARD RIB SKIN BULGED AND CRACKED. FABRICATED REPAIR PER SRM 57-50-03. INSTALLED REPAIR PER SRM 51-30-02. (M)Dec 14, 1995 · N110NE · Boeing 72781SDR EISA95516Skin · crackedFOUND LEFT WING NR 1 SLAT UPPER TRAILING EDGE SKIN CRACKED ABOVE OUTBOARD HOOK. FABRICATED AND INSTALLED DOUBLER PER SRM. (M)Dec 13, 1995 · N110NE · Boeing 72781SDR DL72S954731Rib · crackedFOUND ON CV2 CHECK TRANSFERRRED FROM N/R 33 ITEM NR 2, .4375 INCH CRACK AT NR 6 SLAT NOSE RIB INBD SIDE OF ACTUATOR. REPAIRED PER M/M 57-54-0 AND ID PER PS 900-5-1 NR 4.Dec 12, 1995 · N531DA · Boeing 727232SDR DL72S954706Angle · crackedFOUND ON CV2 CHECK, TWO CRACKS IN NR 7 SLAT COVE PANEL ATTACH ANGLE BELOW TAI DUCT. REPAIR: REPAIRED PER M/M 57-54-0, PAR 5A.Dec 12, 1995 · N531DA · Boeing 727232SDR DL72S954705Angle · crackedFOUND ON CV2 CHECK 1.) 1.25 INCH CRACK AT NR 7 SLAT COVE PANEL ATTACH ANGLE JUST INBOARD OF INBOARD TRACK. 2.) SCREWS/BOLTS LOOSE AT NR 7 SLAT INBOARD TRACK FAIRING. REPAIR: 1.) REPAIRED PER M/M 57-54-0 PAR 2. 2.) REPAIRED AS SECURED FASTENERS.Dec 12, 1995 · N531DA · Boeing 727232SDR DL72S954740Rib · crackedFOUND ON CV2 CHECK, .75 INCH CRACK PAST PREVIOUS STOP DRILL I/B NOSE RIB AT ACTUATOR ROD END ATTACH NR 4 SLAT. REPAIRED RIB PER M/M 57-54-0 PAR 4, NR 4 SLAT.Dec 11, 1995 · N531DA · Boeing 727232
Back to JASC 5754