JASC 5754

Service difficulty reports · 17,348

Reports filed under 5754 · Leading Edge Devices, newest first.

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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"

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SDR DL72S953642Rib · crackedDURING SHOP INSPECTION, NR 2 L/E SLAT WAS FOUND WITH RIB NR 5 CRACKED. REPAIRED PER MM 57-54-0.Sep 8, 1995 · N406DA · Boeing 727232SDR DL72S953641Rib · crackedDURING SHOP INSPECTION, NR 2 L/E SLAT WAS FOUND WITH SUPPORT RIB NR 2, 20 INCH CRACK. REPAIRED PER MM 57-54-0 FIG 814.Sep 8, 1995 · N406DA · Boeing 727232SDR DL72S953636Angle · crackedNR 6 SLAT, .25 INCH CRACK AT FASTENER HOLE IN ATTACH ANGLE AFT OF RIB, 6 INCHES O/B OF TAI DUCT. REPAIRED PER MM 57-54-0 FIG 805A.Sep 7, 1995 · N499DA · Boeing 727232SDR DL757953617Te Wedge · damagedUPON INSPECTION, HAIL DAMAGE WAS FOUND TO THE T/E WEDGE. NEEDED TO C/W AD 90-23-06. REPAIRED BOTH ITEMS PER SRM 57-43-02 FIG 202, FOR NR 7 L/E SLAT PANEL.Sep 6, 1995 · N658DL · Boeing 757232SDR DL72S954234Rib · crackedDURING A ROUTINE SHOP INSPECTION, NR 8596 WAS WRITTEN FOR A CRACK IN THE 3RD RIB FROM I/B EDGE OF THE NR 2 SLAT. THE CRACK WAS REPAIRED PER M/M 57-54-0 FIG 819.Sep 6, 1995 · N401DA · Boeing 727232SDR DL72S954233Rib · crackedDURING A ROUTING SHOP INSPECTION, NR 8598 WAS WRITTEN FOR A CRACK IN THE 17TH RIB FROM I/B EDGE OF THE NR 2 SLAT. THE CRACK WAS REPAIRED PER M/M 57-54-0 FIG 819.Sep 6, 1995 · N401DA · Boeing 727232SDR DL72S954232Rib · crackedDURING A ROUTINE SHOP INSPECTION, NR CARD 8598 WAS WRITTEN FOR A CRACK IN THE 15TH RIB FROM I/B EDGE OF THE NR 2 SLAT. THE CRACK WAS REPAIRED PER M/M 57-54-0 FIG 805.Sep 6, 1995 · N401DA · Boeing 727232SDR DL72S953669Rib · crackedNR 1 SLAT I/B TRACK I/B RIB CRACKED. DRILLED DOUBLER AND INSTALLED PER M/M 57-54-0 PG 806 AND 807.Sep 6, 1995 · N499DA · Boeing 727232SDR DL72S953643Rib · crackedDURING SHOP INSPECTION, THE 4TH RIB FOR I/B END WAS FOUND CRACKED. THE RIB WAS REPAIRED PER SRM 57-54-00. THE LOWER COVE PANEL ATTACH ANGLE UNDERNEATH THE I/B UPSTOP WAS FOUND TO HAVE A CRACK. THE ANGLE WAS REPAIRED PER SRM 57-54-0 FIG 812, FOR NR 2 L/E SLASep 6, 1995 · N419DA · Boeing 727232SDR DL72S953633Rib · crackedDURING HMV, FOUND NR 1 SLAT WITH CRACKED RIB AT TRACK ATTACH AREA. REPAIRED PER MM 57-40-0 PG 806 AND 807.Sep 6, 1995 · N499DA · Boeing 727232SDR 96ZZZM434Skin · dentedDURING C-CHECK, FOUND MSI 702-0125-1003, DENT AT RW SLAT STATION 193.5. CUT OUT DENTED (DAMAGED) AREA. INSTALLED FLUSH REPAIR PER SRM 57-50-3 FIG 1 (REPAIR II). INSTALLED DOUBLER .080 2024-0 4.5 INCH BY 7.25 INCH FILLER .063 2024-T3 2.75 INCH BY 5 INCH. FASep 6, 1995 · N702DH · Boeing 72730CSDR EISA95378Skin · corrosionDURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND CORROSION AROUND FASTENER HOLES ON NR 3 SLAT SKIN OUTBOARD OF THE OUTBOARD TRACK, (SOME MATERIAL PREVIOUSLY REMOVED). REMOVED CORROSION IAW SRM 51-10-6, FOUND MATERIAL TO BE OUT OF LIMITS BY 20 Sep 5, 1995 · N357NE · Boeing 72782SDR EISA95375Skin · damagedDURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, EXCESSIVE METAL REMOVED FROM NR 4 SLAT SKIN NEXT TO TELESCOPING DUCT PANEL SEAL. FABRICATED REPAIR IAW SRM 57-30-3, ALODINED IAW SRM 51-10-2, SEALED REPAIR IAW SRM 57-30-5. INSTALLED REPAIR IAW SRM 5Sep 5, 1995 · N357NE · Boeing 72782SDR EISA95372Rib · crackedDURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND NR 3 SLAT ACTUATOR RIB CRACKED INBOARD RIB. REMOVED INNER SKIN TO ACCESS AREA. FABRICATED ANGLE FROM 7075-0 X .040 IAW B727 SRM CH 57-50-3. HEAT TREATED TO T-6 IAW BAC 5606 AND RWB SCALE PN NRSep 5, 1995 · N357NE · Boeing 72782SDR EISA95361Skin · corrosionDURING A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, CORROSION AROUND FASTENERS FORWARD OF REPAIR ON NR 3 SLAT SKIN AT ACTUATOR ATTACH POINT WAS FOUND. CORROSION WAS FOUND TO BE OUT OF LIMITS BY APPROXIMATELY 20 PERCENT. FABRICATED REPAIR IAW SRM 57-Sep 5, 1995 · N357NE · Boeing 72782SDR EISA95356Fitting · corrodedUPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, CORROSION WAS FOUND ON THE MOUNT FITTING AT INBOARD END OF NR 2 LEADING FLAP. REMOVED NR 2 KRUGER FLAP. REMOVED AND REPLACED MOUNT FITTING. REPLACED ATTACH ANGLE AND REINSTALLED NR 2 KRUGER FLAP IAWSep 5, 1995 · N357NE · Boeing 72782SDR DL72S953614Angle · crackedFOUND ON A-1 LETTER CHECK, .25 INCH CRACK NR 2 L/E SLAT COVE SKIN ATTACH ANGLE. REPAIRED PER MM 57-54-0.Sep 5, 1995 · N543DA · Boeing 727232SDR DL72S953602Skin · crackedDURING HMV, NR 2 SLAT LOWER SKIN ATTACH ANGLE CRACKED UNDER I/B STOP PAD. REPAIRED PER MM 57-54-0 PG 816.Sep 3, 1995 · N499DA · Boeing 727232SDR DL72W953580Doubler · crackedPREVIOUS DOUBLER REPAIR CRACKED BENEATH NR 7 L/E SLAT I/B DOWN STOP PAD. CRACK WAS FOUND AT F-1 LTR CHECK. REPLACED DOUBLER PER MM 57-54-0.Sep 1, 1995 · N294WA · Boeing 727247SDR UPS204350Bullnose · crackedWHILE IN FOR C-CHECK, MAINTENANCE FOUND NR 5 K-FLAP BULLNOSE CRACKED AT OUTBOARD LUG ATTACH POINT, INBOARD FASTENERS HOLES. REMOVED CRACKED BULLNOSE AND INSTALLED NEW BULLNOSE PER SRM 51-30-2, 51-30-8, M.M. 27-81-00.Aug 31, 1995 · N905UP · Boeing 72751CSDR DL72S953566Rib · crackedDURING SHOP INSPECTION, NR 4 L/E SLAT WAS FOUND WITH NR 6 L/E SUPPORT RIB CRACKED. REPAIRED PER MM 57-54-0 FIG 814.Aug 31, 1995 · N411DA · Boeing 727232SDR DL72S953554Skin · crackedDURING A-1 LETTER CHECK, FOUND COVE SKIN SUPPORT ANGLE CRACKED 1 INCH FROM O/B END ON NR 4 SLAT. REPAIRED PER MM 57-54-0.Aug 30, 1995 · N492DA · Boeing 727232SDR DL72S953553Skin · crackedDURING A-1 LETTER CHECK, FOUND COVE SKIN SUPPORT ANGLE CRACKED .3750 INCH UNDER TAI DUCT ON NR 2 SLAT. REPAIRED PER M/M 57-54-0 AND ID PER PS 900-5-1 NR 4.Aug 30, 1995 · N492DA · Boeing 727232SDR UPS204345Bonding Jumper · corrodedWHILE IN FOR C-CHECK, MAINTENANCE FOUND NR 2 K-FLAP OUTBOARD BONDING JUMPER UPPER ATTACH POINT IS PITTED. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS PER SRM 57-50-1, CUT OUT DAMAGE AND REPAIRED PER SRM 57-50-3.Aug 29, 1995 · N905UP · Boeing 72751CSDR DL72S953531Angle · crackedCRACK, 25 INCHES, NR 2 SLAT INBOARD UPSTOP PAD. FOUND AT C-1 LTR CK. SLAT WAS REPLACED AND ROUTED TO SHOP.Aug 28, 1995 · N419DA · Boeing 727232SDR DL72S953530Rib · crackedNR 6 SLAT HAS .50 INCH CRACK INBOARD OF ACTUATOR ATTACH POINT AT FORWARD RIB. FOUND AT C-1 LTR CK. REPAIRED PER MM 57-54-0.Aug 28, 1995 · N419DA · Boeing 727232SDR EISA95328Flap · corrodedUPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, UPON REMOVAL OF CORROSION IN NR 6 K-FLAP BEHIND INBOARD ADJUSTMENT BRACKET, AREA FOUND TO BE OUT OF LIMITS PER THE SRM 57-50-1. REMOVED AND REPLACED THE NR 6 KRUGER FLAP IAW B727 MM 27-81-1. OPS CHECAug 27, 1995 · N357NE · Boeing 72782SDR DL72S953513Le Rib · crackedDURING SHOP INSPECTION, NR 4 L/E SLAT WAS FOUND WITH CRACKED L/E RIB AT THE ACTUATOR ATTACH FITTING. REPAIRED PER MM 57-54-0 FIG 804.Aug 26, 1995 · N411DA · Boeing 727232SDR EISA95379Rib · corrosionDURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND CORROSION ON RIB ABOVE INBOARD END OF NR 5 LEADING EDGE FLAP (CORROSION UNDER WIRE STAN OFF 3 ON TOP). REMOVED CORROSION IAW SRM 51-10-6. REMOVED T-ANGLE FROM RIB IAW SRM 51-40-3. FABRICATED NAug 25, 1995 · N357NE · Boeing 72782SDR UPS804317Skin · crackedWHILE IN FOR C-CHECK, MAINTENANCE FOUND A CRACK IN THE RIGHT WING OUTBOARD MID-SLOT PANEL. MAINTENANCE REPLACED THE SLOT PANEL PER MM 27-80-02.Aug 24, 1995 · N709UP · Doug DC873FSDR UPS804307Skin · crackedWHILE IN FOR C-CHECK, MAINTENANCE FOUND A CRACK IN THE RIGHT INBOARD WING SLOT OUTBOARD END UPPER SURFACE. MAINTENANCE REMOVED THE ANGLE REPAIR, STOP DRILLED, REPAIRED AND REINSTALLED PER SRM 51-3-0, 57-2-0, AND 51-1-20.Aug 24, 1995 · N806UP · Doug DC873FSDR DL72S953494Ribs · crackedDURING SHOP INSPECTION, NR 7 L/E SLAT WAS FOUND WITH NR 2 L/E RIB CRACKED IN LOWER AFT CORNER. REPAIRED PER MM 57-54-0 FIG 814.Aug 24, 1995 · N495DA · Boeing 727232SDR DL72S953493Le Ribs · crackedDURING SHOP INSPECTION, NR 3 L/E SLAT WAS FOUND WITH SEVERAL CRACKED L/E RIBS. ACCOMPLISHED REPAIRS PER MM 57-54-0.Aug 24, 1995 · N470DA · Boeing 727232SDR DL72S953481Bracket · crackedDURING HMV, FOUND I/B MOUNT BRACKET CRACKED FOR THE NR 5 L/E FLAP ACTUATOR. REPAIRED PER 57-20-21.Aug 23, 1995 · N515DA · Boeing 727232SDR 95FDEA01172Bullnose · corrodedCORROSION ON NR 6 K-FLAP O/B BULLNOSE ACTUATING ROD LOWER ATTACH POINT AT BULLNOSE. REMOVED AND REPLACED NR 6 K-FLAP PER FEDEX MM 27-81-01.Aug 22, 1995 · N156FE · Boeing 72725SDR 95FDEA01170Skin · corrodedCORROSION ON NR 4 K-FLAP O/B UPPER GROUND WIRE ATTACH POINT. REMOVED AND REPLACED NR 4 K-FLAP PER FEDEX MM 27-81-1.Aug 22, 1995 · N156FE · Boeing 72725SDR 95FDEA01169Bonding Jumper · corrodedCORROSION ON NR 5 K-FLAP I/B UPPER BONDING JUMPER ATTACH POINT. REMOVED AND REPLACED NR 5 K-FLAP PER FEDEX MM 27-01-01.Aug 22, 1995 · N156FE · Boeing 72725SDR 95FDEA01168Skin · corrodedCORROSION UNDER DATA PLATE NR 2 K-FLAP. REMOVED AND REPLACED NR 2 K-FLAP PER FEDEX MM 57-53-0.Aug 22, 1995 · N156FE · Boeing 72725SDR DL72S953639Skin · crackedNR 5 SLAT SKIN WORN ON UPPER SURFACE AT FENCE ATTACHMENT. BURNISHED WORN AREA AND DYE PENETRANT INSP SHOWS CRACKS AT 3 FENCE ATTACH HOLES. ROUTED DAMAGE AT ATTACH HOLES, FABRICATED AND DRILLED DOUBLER PER M/M 57-54-0.Aug 21, 1995 · N499DA · Boeing 727232SDR DL72S953668Rib · crackedDURING HMV, FOUND NR 7 SLAT RIB CRACKED AT FASTENER HOLE, I/B OF I/B STOP PAD. FABRICATED REPAIR PER M/M 57-54-0 PG 807 AND INSTALLED REPAIR PER MM 57-54-0 PG 807.Aug 20, 1995 · N499DA · Boeing 727232SDR DL72S953649Web · crackedDURING HMV, FOUND WEB CRACKED NR 5 SLAT. REPAIRED WEB PER MM 57-54-0 FIG 805.Aug 20, 1995 · N499DA · Boeing 727232SDR DL72S953637Skin · wornNR 6 SLAT SKIN WORN AND CHAFED INBD OF INBD TRACK FAIRING AND BELOW SLAT ACTUATOR ON LWR TRAILING EDGE. TRIMMED AWAY DAMAGED PORTION OF TAB AND FABRICATED DOUBLER AND FILLER PER MM 57-54-0 PG 820.Aug 20, 1995 · N499DA · Boeing 727232SDR DL72S953632Angle · crackedUPON HMV, FOUND .25 INCH CRACK AT FASTENER HOLE IN ATTACH ANGLE AFT OF RIB 6 OUTBD OF T.A.I. DUCT. REPAIRED PER M/M 51-54-0, FIG 805A.Aug 20, 1995 · N499DA · Boeing 727232SDR DL72S953610Rib · crackedDURING HMV, FOUND NR 4 SLAT RIB CRACKED .5 INCH, ON O/B SIDE OF O/B TRACK FITTING. REPAIRED RIB PER MM 57-45-0 FIG 814.Aug 20, 1995 · N499DA · Boeing 727232SDR DL72S953591Rib · crackedDURING HMV, NR 8 L/E SLAT WAS FOUND WITH CRACKED INTERNAL SUPPORT RIB. REPAIRED PER MM 57-54-0 PG 814.Aug 20, 1995 · N499DA · Boeing 727232SDR DL72S953638Skin · crackedDURING HMV, FOUND NR 5 SLAT RIVET MISSING IN LWR T/E SKIN O/B OF O/B TRACK. SKIN WORN AT FENCE ATTACHMENT AND WORN THIN AT BOLT HOLE ON LWR T/E SKIN. REF NR CARD 1148, BURNISHED WORN AREA. DIE PENETRANT INSP SHOWS CRACK AT 3 FENCE ATTACH HOLES. FABRICATED Aug 19, 1995 · N499DA · Boeing 727232SDR UPS204229K-Flap · pittedWHILE IN FOR C-CHECK, MAINTENANCE FOUND NR 6 K-FLAP CENTER LUG PITTED ON LOWER I/B HOLE AND UPPER O/B HOLE. MAINTENANCE REMOVED AND REPLACED NR 6 K-FLAP PER MM 27-81-01.Aug 18, 1995 · N939UP · Boeing 72727CSDR UPS204228K-Flap · pittedWHILE IN FOR C-CHECK, MAINTENANCE FOUND NR 5 K-FLAP I/B LUG IS PITTED AROUND BOLTS AND EDGE LUG. MAINTENANCE REMOVED AND REPLACED NR 5 K-FLAP PER MM 27-81-01.Aug 18, 1995 · N939UP · Boeing 72727CSDR UPS204227K-Flap · corrodedWHILE IN FOR C-CHECK, MAINTENANCE FOUND NR 4 K-FLAP O/B LUG PITTED AROUND UPPER AND LOWER BOLTS. MAINTENANCE REMOVED AND REPLACED NR 4 K-FLAP PER MM 27-81-01.Aug 18, 1995 · N939UP · Boeing 72727CSDR UPS204226K-Flap · corrodedWHILE IN FOR C-CHECK, MAINTENANCE FOUND NR 3 K-FLAP I/B LUG UPPER BOLT HAS CORROSION AROUND THE NUT. MAINTENANCE REPLACED THE NR 3 K-FLAP PER MM 27-80-00.Aug 18, 1995 · N939UP · Boeing 72727C
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