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 00FDEA00106Skin · wornLEFT WING LEADING EDGE AFT FLEX TOP SURFACE PANEL 517 WORN AT FWD END. INSTALLED FLEX PNL PER MM 27-80-02-4.Feb 23, 2000 · Doug DC1010FSDR 00FDEA00104Rib · crackedLEFT WING LEADING EDGE DROOP NR 2 RIB IS CRACKED AT TOP AFT END, COUNTING I/B TO O/B. NR 3 RIB N470. REPAIRED CRACKED RIBS PER EA 8-5740-47480.Feb 23, 2000 · Doug DC1010FSDR DL72L000514Rib · crackedAT HMV2 FOUND RIB CRACKED O/B SIDE OF TAI DUCT ON N1 L/E SLAT. FABD DOUBLER PER MM 57-54-0 FIG 814, ALODINED PER PS 900-2-4-1 NR 2, INSTALLED PER MM 57-54-0 FIG 814.Feb 22, 2000 · N506DA · Boeing 727232SDR ASAA0040022Skin · gougedSEA - DURING SCHEDULED C-CHECK, THE LEFT WING OUTBOARD FOREFLAP INBOARD END L/E SKIN WAS FOUND TO BE GOUGED. REPAIRED PER EA 5750-01374. (M)Feb 22, 2000 · N791AS · Boeing 737490SDR UPS00231880Flap Track · crackedINSPECTION TYPE:C&SI, NR 3 SLAT, O/B SLAT TRACK, O/B RIB ATTACH POINT HAS SUSPECT CRACK. REPAIR CARRIED OUT AS PER SRM 51-40-2.Feb 21, 2000 · N908UP · Boeing 72727CSDR TWAA0003105Skin · damagedDURING CHECK-C MAINT, THE LT WING NUMBER 2 FOREFLAP HAD HOLE ON BOTTOM SIDE INBD END. REPLACED FOREFLAP WITH SERVICEABLE UNIT PER MM 27-51, AND M27-27-23.Feb 17, 2000 · N64339 · Boeing 727231SDR SWAA000292Skin · delaminatedDURING WALKAROUND INSPECTION FOUND NR 5 L/E SLAT I/B UPPER WEDGE PANEL DELAMINATED FOR APPROX 12 INCHES. REMOVED AND REPLACED SLAT ASSY PER MM.Feb 17, 2000 · N74SW · Boeing 7372H4SDR RIVA0000007Angle · crackedNR 4 SLAT REAR LOWER ANGLE, WS 191 TO WS 198, CRACKED 7 INCHES ALONG PREVIOUS REPAIR. INSTALLED REPAIR DOCUMENTED IN BOEING SRM 51-40-3, FIG 1. REMOVED ANGLE IAW BSRM 51-30-2. FABRICATED REPAIR ANGLE USING .050 INCH 2024 T-3 ALUMINUM. FABRICATED REPAIR ANGFeb 16, 2000 · N364PA · Boeing 7272J0SDR RIVA0000006Rib · crackedNR 4 SLAT, OTBD RIB WS 198 CRACKED, 1 INCH LONG. INSTALLED REPAIR DOCUMENTED IN BOEING SRM 51-40-3. CUT OUT DAMAGED AREA OF RIB. FABRICATED DOUBLER USING .050 INCH 2024 T-3 ALUMINUM. FABRICATED ANGLE USING .063 INCH 2024 T-3 ALUMINUM. APPLIED PROTECTIVE TFeb 16, 2000 · N364PA · Boeing 7272J0SDR RIVA0000005Skin · gougedRIGHT OTBD T/E FOREFLAP HAD GOUGE IN L/E AT WS 550. INSTALLED REPAIR DOCUMENTED IN BOEING SRM 57-50-4, FIG 1. REMOVED DAMAGED AREA. FABRICATED DOUBLER FROM .050 INCH 2024 T-3 ALUMINUM. APPLIED PROTECTIVE TREATMENT IAW BSRM 51-10-2. INSTALLED DOUBLER. REFeb 16, 2000 · N364PA · Boeing 7272J0SDR RIVA0000004Skin · dentedDENT IN LOWER SKIN OF LT OTBD AILERON AT WBL 540.2 INCHES BEHIND FRONT SPAR. INSTALLED FLUSH PATCH REPAIR DOCUMENTED IN THE BOEING SRM 57-50-5. REMOVED DAMAGED SECTION OF SKIN. FABRICATED DOUBLER AND FILLER FROM .020 INCH 7075 T-6 ALUM. APPLIED PROTECTIVE Feb 16, 2000 · N364PA · Boeing 7272J0SDR RIVA0000003Rib · crackedDAMAGE TO RT WING OTBD AFT FLAP, OTBD CONTROL ROD ATTACH BRACKET AND L/E RIB AT WBL 464. REPAIRED RIB AND BRACKET BY REPLACEMENT. USED REPAIR DOCUMENTED IN BOEING SRM 57-50-4 FOR L/E SECTION REMOVED TO GAIN ACCESS. REMOVED L/E SKIN SECTION, FABRICATED DOUBLFeb 16, 2000 · N364PA · Boeing 7272J0SDR RIVA0000002Rib · crackedNR 5 LEADING EDGE SLAT INBOARD RIB, AT ACUATOR ATTACHMENT WS 234 IS CRACKED. REPAIRED IAW BOEING SRM 57-50-3, FIGURE 9. FABRICATED DOUBLER FROM .050 INCH 2024-T3 ALUMINUM. APPLIED PROTECTIVE TREATMENT TO ALL PARTS AS REQUIRED. INSTALLED DOUBLER. REBALANCEFeb 16, 2000 · N364PA · Boeing 7272J0SDR DL72L000319Stiffener · crackedA .5 INCH CRACK IN I/B ATTACH ANGLE/ SPAR STIFFENER FOR NR 4 SLAT ACT. REPLACED STIFFENER PER 57-20-21.Feb 15, 2000 · N512DA · Boeing 727232SDR DL72S000310Skin · wornINSTALLED REPAIR PER B727 MM 57-54-0, FIG 813. SLAT WORN.Feb 14, 2000 · N8889Z · Boeing 727225SDR RRXA000606Skin · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO THE LEFT WING L/E SKIN AT STA 6.225 X LDI AND XW 408, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. REPAIRED AND INSTALLED IAW DC-8 SRM 51-1-21 AND DAC DWG NRFeb 13, 2000 · N831AL · Doug DC873FSDR UPS00231875Flap Track · crackedINSPECTION TYPE:C&SI, NR 2 SLAT, I/B TRACK ATTACH POINT HAS SUSPECT CRACK. REPAIR CARRIED IAW SRM 51-40-2.Feb 11, 2000 · N908UP · Boeing 72727CSDR TWAA0002502Skin · delaminatedDURING CHECK-C MAINT, THE LEFT WING NUMBER 1 LE SLAT ROUND PATCH TOP OF SLAT AT CENTER, 5 INCH DIAMETER WAS DELAMINATING. INSTALLED HOT BOND REPAIR WITH FILLER SKIN 2 INCHES IN DIAMETER AND OVERLAY METAL DOUBLER TO 5 INCH DIAMETER PER SRM 51-70-10.Feb 7, 2000 · N651TW · Boeing 767205SDR F3LA00013Skin · delaminatedDEN - DURING C-5 CHECK, INSPECTION FOUND TWO DENTS WITH DELAMINATION ON UPPER SURFACE OF LT OUTBOARD FOREFLAP, APPROXIMATE 36 INCHES FROM INBOARD END. MAINTENANCE REPAIRED FOREFLAP PER MM 51-70-10, AND INSTALLED AND PERFORMED OPERATIONAL CHECK PER MM 27-51-37Feb 6, 2000 · Boeing 737317SDR UPS00231898Rib · crackedINSPECTION TYPE:C, NR 3 LEADING EDGE SLAT ACTUATOR ROD END ATTACH BOLT OUTBOARD SUPPORT RIB CRACKED AT AFT LOWER CORNER. INSTALLED REPAIR AT OUTBOARD SUPPORT RIB FOR NR 3 LEADING EDGE SLAT ACTUATOR ROD END, MATERIAL USED 321.032. 5 BY 3 IAW B727 SRM 57-50-3.Feb 6, 2000 · N948UP · Boeing 72725CSDR UPS00231897Angle · crackedINSPECTION TYPE:C, NR 2 LEADING EDGE SLAT INBOARD TRACK ROLLER SUPPORT WEBS INBOARD AND OUTBOARD VERTICAL ATTACH ANGLES CRACKED AT FRONT SPAR LOWER CHORD. REPLACED ANGLES AT NR 2 LEADING EDGE SLAT INBOARD TRACK ROLLER SUPPORT WEB INBOARD AND OUTBOARD MATERIALFeb 6, 2000 · N948UP · Boeing 72725CSDR UPS00231895Angle · crackedINSPECTION TYPE:C, NR 3 LEADING EDGE SLAT OUTBOARD TRACK ROLLER SUPPORT WEBS INBOARD AND OUTBOARD VERTICAL ATTACH ANGLES CRACKED AT FRONT SPAR LOWER CHORD. REPLACED INBOARD AND OUTBOARD VERTICAL ATTACH ANGLES AT NR 3 LEADING EDGE SLAT OUTBOARD TRACK ROLLER SUFeb 6, 2000 · N948UP · Boeing 72725CSDR TWAA0002413Structure · crackedDURING CHECK-C MAINT NUMBER 6 LE SLAT HAD A CRACK AT RIVET UNDER ACTUATOR ATTACH FITTING. FABRICATED A REPAIR PER SRM 57-50-3.Feb 4, 2000 · N64339 · Boeing 727231SDR RRXA001686Skin · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE AROUND THE SCREW HOLES ON THE LT WING CENTER LE UPPER SURFACE AT XFS 325 TO XFS 304, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED DOUBFeb 3, 2000 · N994CF · Doug DC862SDR RRXA000991Structure · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE LT WING SCREW HOLES AT THE CENTER LE UPPER SURFACE AT XFS 422, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED DOUBLER FROM 7075-Feb 3, 2000 · N994CF · Doug DC862SDR TWAA0002001Skin · delaminatedDURING CHECK-C MAINTENANCE, THE NUMBER 1 LE SLAT TOP SIDE, AN EXISTING 6 IN BY 6 IN PATCH WAS LOOSE AND DELAMINATING AT THE INBD TE WEDGE. REMOVED OLD REPAIR. INSTALLED METAL TO METAL 250 DEGREEE HOT BOND REPAIR PER SRM 51-70-10 AND SRM 57-43-02.Feb 3, 2000 · N602TW · Boeing 767231SDR CA000209003Bolt · broken(CAN) NR 4 SLAT BOLT BROKEN THROUGH GREASE PASSAGE DUE TO LACK OF LUBRICATION, BOLT WORN. REPLACED.Feb 1, 2000 · Boeing 7372T5SDR RRXA000993Skin · damagedDURING A MAINTENANCE VISIT, FOUND ELONGATED HOLES IN THE LEFT MID-WING L/E ON LOWER SURFACE AT STA XS 520.168, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED DOUBLER FROM 7075-T6 AND INSTALLEJan 31, 2000 · N994CF · Doug DC862SDR RRXA000333Skin · corrodedDURING A MAINTENANCE VISIT FOUND LEFT WING L/E CORRODED, UPPER SURFACE FROM XFS 40 - XFS 100. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPLACEMENT PARTS IAW DC-8 SRM 51-1-20D AND DCJan 31, 2000 · N792FT · Doug DC873FSDR DL72L000259Rib · crackedNR 5 SLAT NR 12 RIB CRACKED. REPAIRED PER MM 57-54-0.Jan 28, 2000 · N507DA · Boeing 727232SDR DL72K000203Le Flap · separatedAFTER T/O FROM DCA, FLAPS DID NOT RETRACT PAST 2 DEGREE POSITION. A/C DIVERTED TO IAD. MTC IN IAD FOUND LT O/B FOREFLAP BROKEN FREE FROM I/B CARRIAGE. REPLACED FOREFLAP.Jan 27, 2000 · N521DA · Boeing 727232SDR P2EA00055Skin · damagedSJO - DURING Q-CHECK, FOUND NR 5 SLAT LOWER TRAILING EDGE DAMAGED AT STATION 198 AND STATION 196. REPAIRED NR 5 SLAT IAW COOPESA EO COO-3-57-065-00, DATED 2/4/2000. (M)Jan 26, 2000 · N603DJ · Boeing 737222SDR DL72L000196Rib · crackedSLAT RIB WAS CRACK AT THE O/B LWR AFT END. REPAIRED PER MM 57-54-0 FIG 814.Jan 26, 2000 · N507DA · Boeing 727232SDR DL72L000238Skin · crackedANTI-ICE SKIN CRACKED AT 4 LOCATIONS. INSTALLED DOUBLER PER MM 57-54-0.Jan 25, 2000 · N507DA · Boeing 727232SDR DL72L000195Rib · crackedSLAT RIB WAS CRACKED AT LWR AFT END NR 2 RIB. INSTALLED A REPAIR DOUBLER PER MM 57-54-0 FIG 814.Jan 24, 2000 · N507DA · Boeing 727232SDR DL72L000194Skin · crackedSLAT CRACKED. INSTALLED REPAIR DOUBLER PER MM 57-54-0 FIG 814.Jan 24, 2000 · N507DA · Boeing 727232SDR RRXA000861Skin · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE AROUND SCREW HOLES LT WING I/B LEADING EDGE UPPER SURFACE AT STA XFS 13.750, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED DOUBLER FROM 707Jan 19, 2000 · N994CF · Doug DC862SDR 0000295516Web · crackedDURING L CHECK, FOUND CRACK ON NUMBER 10 SLAT AFT CLOSURE WEB AT O/B DRIVE TRACK. REPAIRED PER EA 55-173783.Jan 19, 2000 · N516US · Boeing 757251SDR 2000UALA00027Panel · dentedLT WING MOST I/B SLAT LARGE DENTS ON I/B END AND MID SPAN WING FILLET PANEL ON I/B END. ALSO LEFT STABILIZER HAS DEEP DENT IN LEADING EDGE IN MIDDLE OF STABILIZER. DENT IS AT RIB WITH RIVETS PULLING THROUGH SKIN. *S/D* REPAIR A WATER LEAK AT THE FILL VALVEJan 16, 2000 · N1858U · Doug DC1030SDR RRXA000596Skin · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO RIGHT L/E SKIN UPPER AND LOWER SURFACES FROM L/E TO 7 INCHES AFT AT STA XW 761.695 TO XW 736.000, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. REPAIRED PART Jan 16, 2000 · N831AL · Doug DC873FSDR AU000076Wedge · contaminated(AUS) LEADING EDGE SLAT TRAILING EDGE WEDGES CORRODED INTERNALLY & CONTAMINATED WITH MOISTURE.Jan 14, 2000 · Boeing 767277SDR DHL200071711DBracket · crackedAT D CK, RIGHT WING NR 5 LEADING EDGE SLAT O/B TRACK O/B SIDE BRACKET FOR TRACK CRACKED. REMOVED AND REPLACED O/B BRACKET FOR NR 5 SLAT TRACK AS PER B727 SRM 51-30-2M, REF: N/R 2873.Jan 14, 2000 · N717DH · Boeing 72723SDR UPS00231388Skin · corrodedINSPECTION TYPE:C, WHILE WORKING NRC 051378 (WINGS 75), FOUND CORROSION TO BE OUT OF LIMITS ON NR 3 K-FLAP. REMOVED AND REPLACED NR 3 K-FLAP IAW MM 27-81-01.Jan 13, 2000 · N210UP · Boeing 727247SDR DHL200071784DSupport · crackedAT D CK, RT/W O/B VERTICAL ATTACH FOR NR 6 L/E FLAP ACTUATOR, LWR FLANGE CRACKED, STA 307. REMOVED AND REPLACED O/B VERTICAL ATTACH SUPPORT FOR NR 6 FLAP ACTUATOR PER B727 SRM 57-50-3 FIG 8 AND 51-30-2. REF: N/R 2835.Jan 13, 2000 · N717DH · Boeing 72723SDR DHL2000717100Rib · crackedAT D-CHECK, RIGHT WING L/W SLAT NR 4 RIB, I/B SUPPORT FOR I/B TRACK CRACKED AT LOWER LEFT FLANGE. FOUND TWO MORE CRACKS AT NR 4 RIB RIGHT WING NR 6 SLAT. FABRICATED I/B AND O/B RIBS PER SRM 57-50-2 16 X 6.5.Jan 13, 2000 · N717DH · Boeing 72723SDR USAA991468Skin · crackedCLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND FIVE 1 INCH CRACKS ALONG ACTUATOR LOWER SKIN NR 1 SLAT. INSTALLED FILLER AND DOUBLER PER TR 57-50-01. (M)Jan 12, 2000 · N346US · Boeing 737301SDR UPS00231386Skin · crackedINSPECTION TYPE:C, NR 4 SLAT UPPER SURFACE SKIN IS CRACKED AT O/B GUIDEHOOK UPPER FASTENER. REPAIRED PER SRM 57-50-3 FIG 10.Jan 12, 2000 · N210UP · Boeing 727247SDR AALA2000125Fitting · wornTUL - SUPPORT ATTACH FITTING ON OUTBOARD END OF NR 4 LEADING EDGE SLAT HAS EXCESSIVE PLAY. INSTALLED NEW RIB PER SHOP ESO 80117. (M)Jan 12, 2000 · N474 · Doug DC982SDR UPS00831436Doubler · crackedINSPECTION TYPE:C123, R/W CTR L/E BOTTOM I/B INTERIOR DRAIN HOLE CRACKED. SRM DOUBLER REPAIR, FABRICATED REPAIR PARTS AND INSTALLED IAW DC8 SRM 57-2-0 & 51-1-21.Jan 11, 2000 · N752UP · Doug DC871FSDR UPS00231262Skin · dentedNR 1 SLAT HAS DENTS WHICH ARE OUT OF LIMITS. COMPLIED WITH EO B727-5740-1259.Jan 7, 2000 · N940UP · Boeing 727185C
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