JASC 5312

Service difficulty reports · 20,047

Reports filed under 5312 · Fuselage Main, Bulkhead, 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 = '5312'
  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 AWXA0001862Web · crackedd: upom removal of strap HFEC Indicates crack .7" WL 212 RBL 6.8 on BS178 Blkhd web fwd facec: repaired IAW B737-300 SrM 53-10-08 Pg 287-298Jun 15, 2001 · N305AW · Boeing 7373G7SDR AWXA0001866Web · crackedd: upom removal of strap HFEC Indicates crack .7" WL 212 RBL 6.8 on BS178 Blkhd web fwd facec: repaired IAW B737-300 SrM 53-10-08 Pg 287-298Jun 15, 2001 · N305AW · Boeing 7373G7SDR AWXA0001861Webd: upom removal of strap HFEC Indicates crack .7" WL 212 RBL 6.8 on BS178 Blkhd web fwd facec: repaired IAW B737-300 SrM 53-10-08 Pg 287-298Jun 15, 2001 · N305AW · Boeing 7373G7SDR AWXA0001859Webd: upom removal of strap HFEC Indicates crack .7" WL 212 RBL 6.8 on BS178 Blkhd web fwd facec: repaired IAW B737-300 SrM 53-10-08 Pg 287-298Jun 15, 2001 · N305AW · Boeing 7373G7SDR UPS01236179Bulkhead · crackedINSPECTION TYPE:C, AFT PRESSURE BULKHEAD BS 1183 CRACK OF FWD FLANGE OF BL 17.8 LEFT VERTICAL BEAM AT WL 273 APPROX. REPAIRED/ MODIFIED PER EO B727-5310-11743-B APP C AND E.Jun 14, 2001 · N945UP · Boeing 72722CSDR RRXA11277Web · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO B-PIT TORQUE BOX WEB AT STA515-520, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-4,Jun 13, 2001 · N606AL · Doug DC873FSDR RRXA11275Web · misdrilledDURING A MAINTENANCE VISIT FOUND DRILL DAMAGE TO FWD ENTRY DOOR INNER SKIN FWD LOWER WEB, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-2Jun 13, 2001 · N606AL · Doug DC873FSDR ZW0A0103703Bulkhead · crackedDURING CHECK-C MAINT IN AFT ACCY COMPT FOUND CRACKED WEB APPROX 2 INCHES ON STA 1485 CANTED BULKHEAD, APPROX 10 O'CLOCK POSITION. STOP DRILLED CRACK. REPAIRED WEB PER SRM 53-01, PAGE 9.Jun 12, 2001 · N929TW · Doug DC982SDR P2EA01093Bulkhead · crackedSJO - DURING C-CHECK, INSPECTION PER S/B 737-53A1173, PRESSURE BULKHEAD, BS 178 VERTICAL CHORD CRACKED AT LBL 57 WL 185, PRESSURE BULKHEAD BS 178 RIGHT LATERAL CHORD CRACKED AT WL 207, PRESSURE BULKHEAD, BS 178 LEFT LATERAL CHORD CRACKED AT WL 207. BS 178 FORJun 11, 2001 · N127NJ · Boeing 7372B7SDR P2EA01094Bulkhead · crackedDURING C-CHECK INSPECTION PER S/B 737-53A1173, PRESSURE BULKHEAD BS 178 WEB CRACKED AT WL 234, RBL 12 INCHES, PRESSURE BULKHEAD BS 178 RT SIDE INTERCOSTAL CRACKED AT WL 195, PRESSURE BULKHEAD BS 178 LEFT SIDE INTERCOSTAL CRACKED AT WL 185. BS 178 FORWARD PRESJun 11, 2001 · N127NJ · Boeing 7372B7SDR 01FDEA00414Pressure Panel · crackedDURING ROUTINE INSP LT SIDE WEB IN NOSE WHEEL WELL WAS FOUND CRACKED AT BS 1260. *S/D* REMOVED, REPLACED AND FAB PER IAW BAC 727 SRM 51-20-1, 51-30-2.Jun 11, 2001 · N107FE · Boeing 72722CSDR GAIA01205STBulkhead · crackedDURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED THAT TWO CRACKS IN BS 178 B/H WEB AT FASTENER LOCATIONS WL 235 RBL 10-12. ACCOMPLISHED BS 178 BULKHEAD WEB REPAIR BS 178 WL 235 RBL 10-12 IAW B727 SRM 53-10-9 FIG 4. (M)Jun 11, 2001 · N252US · Boeing 727251SDR GAIA01207STPressure Panel · crackedDURING A LTC INSPECTION, IT WAS DISCOVERED THAT A CRACK IN THE UPPER SKIN IN THE NOSE WHEEL WELL BS 287-292 BBL 0 WL 200. ACCOMPLISHED NOSE WHEEL WELL UPPER SKIN REPAIR BS 287-292 BBL 0 WL 200 IAW B727 SRM 51-40-2 FIG 1. (M)Jun 11, 2001 · N252US · Boeing 727251SDR 01FDEA00401Beam · crackedDURING ROUTINE INSP BS 1183 BULKHEAD VERTICAL BEAM AT LBL 27 FOUND CRACKED AT WL 263. *S/D* REMOVED AND REPLACED PER VERTICAL BEAM PER IAW FEDEX EO 7-5310-7-2346 PART 2.Jun 11, 2001 · N107FE · Boeing 72722CSDR 01FDEA00407Bulkhead · crackedDURING ROUTINE INSP, HFEC IND TWO CRACKS IN BS 1183 BULKHEAD WEB AT WL 283. *S/D* REMOVED AND REPLACED WEB PER IAW FEDEX EO 7-5310-7-5000 PARTS 2 & 4.Jun 11, 2001 · N107FE · Boeing 72722CSDR 01FDEA00406Bulkhead · crackedDURING ROUTINE INSP, HFEC IND CRACK IN BS 1183 BULKHEAD WEB AT WL 283, RBL 17.8. *S/D* REMOVED AND REPLACED PER IAW FEDEX EO 7-5310-7-5000 PARTS 3 & 5.Jun 11, 2001 · N107FE · Boeing 72722CSDR SWAA011695Bulkhead · crackedDURING SCHEDULED SPECIAL VISIT CHECK, FOUND VERTICAL BEAM CRACKED AT BS 178, RBL 17.1. REPAIRED VERTICAL BEAM PER SRM.Jun 11, 2001 · Boeing 7372H4SDR SWAA011694Bulkhead · crackedDURING SCHEDULED SPECIAL VISIT CHECK, FOUND VERTICAL BEAM CRACKED AT BS 178, LBL 17.1. REPAIRED VERTICAL BEAM PER SRM.Jun 11, 2001 · Boeing 7372H4SDR RRXA11273Support · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO A-PIT CROSS SLIDE DOOR JAMB FLOOR SUPPORT AT STA.340 AND L32L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSJun 10, 2001 · N606AL · Doug DC873FSDR RRXA11264Slide · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO A-PIT FLOOR SUPPORT DOOR JAMB AT STA.280 AND L32R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DJun 10, 2001 · N606AL · Doug DC873FSDR RRXA11262Longeron · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO FITTING AT L17R AND IN #60 HOLE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21 AND DWJun 10, 2001 · N606AL · Doug DC873FSDR RRXA11261Strap · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO A/C BAY SUB-FLOOR AT STA.35-55 AND LBL48, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRMJun 10, 2001 · N606AL · Doug DC873FSDR RRXA11260Longeron · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO FWD ACCY COMPARTMENT LONGERON AT STA.45 AND L34R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SJun 10, 2001 · N606AL · Doug DC873FSDR 2001UALA01303Pressure Panel · corrodedCORROSION FOUND ON THE FORWARD EDGE OF THE AFT PRESSURE DECK AT BODY STATION 1681. INSTALLED DOUBLER REPAIR TO DAMAGED AREA. THIS WAS A MAJOR REPAIR.Jun 10, 2001 · N513UA · Boeing 757222SDR 2001UALA00978Bulkhead · crackedBULKHEAD WEB, LWR LT ANT MOUNT INBD EDGE UPPER AND LOWER FASTENER AREA, CRACKED IN 2 PLACES AT BS 178, WL 198-201, LBL 5-6. INSTALLED REPAIR DOUBLER. MAJOR REPAIR ACCOMPLISHED.Jun 10, 2001 · N366UA · Boeing 737322SDR 2001UALA00977Bulkhead · crackedBULKHEAD WEB CRACKED IN 2 PLACES ADJACENT TO RADAR ANTENNA MOUNT FASTENERS AT BS 178, WL 201, RBL 5 TO RBL 6. REPAIRED WITH DOUBLER AND STRUCTURAL FILLERS. MAJOR REPAIR ACCOMPLISHED.Jun 10, 2001 · N366UA · Boeing 737322SDR ABXA010558Bulkhead · crackedMAIN CABIN AFT PRESSURE BULKHEAD WAS CRACKED APPROXIMATELY 63 INCHES ABOVE THE FLOOR BETWEEN THE LEFT BUTT LINE 28 TO LEFT BUTT LINE 40. REPAIRED AREA IAW DAC DWG SRO 8530007, DC-8 SRM 51-1-8, 51-1-20D, 51-3-0, 51-3-1, AND 53-8-5.Jun 9, 2001 · N818AX · Doug DC863SDR 2001UALA00967Bulkhead · crackedBULKHEAD WEB CRACKED AT BS 178, WL 184, RBL 1. ACCOMPLISHED DOUBLER REPAIR. MAJOR REPAIR ACCOMPLISHED.Jun 9, 2001 · N319UA · Boeing 737322SDR ASAA0110323Bulkhead · crackedPAE - DURING SCHEDULED C-CHECK, FOUND WEB AT BS 178, WATERLINE 234 CRACKED. REPAIRED PER EA. (M)Jun 8, 2001 · N746AS · Boeing 7372X6CSDR ASAA0110324Bulkhead · crackedPAE - DURING SCHEDULED C-CHECK, FOUND WEB AT BS 178, WATERLINE 218 CRACKED. REPAIRED PER EA. (M)Jun 8, 2001 · N746AS · Boeing 7372X6CSDR EISA20010094Rivet · shearedRIVET MIGRATED AT 1183 BULKHEAD AFT LT. SIDE 12" O/B OF DOOR CUT-OUT & 10" BELOW DOOR TOP (EO)FOUND DURING B-2 CHECKCORRECTIVE ACTION:CUT-OFF HEAD OF TRAPPED (MIGRATING) RIVET PER E.O. #01-163. INSTALLED TWO EACH HLT 428-6 HILOCS IAW E.O. #01-163 & SEALED WITHJun 8, 2001 · N6813 · Boeing 727223SDR 2001UALA00963Bulkhead · crackedBULKHEAD WEB 2 CRACKS AT UPPER LT WX RADAR ANTENNA MOUNT AT INBD AND OUTBD EDGES OF STRAP AT BS 178, WL 213, LBL 5-6. ACCOMPLISHED DOUBLER REPAIR. MAJOR REPAIR ACCOMPLISHED.Jun 8, 2001 · N366UA · Boeing 737322SDR AWXA0001837Pressure Panel · crackedleft main wheel well upper pressure web cracked at BS 664 LBL 33. repaired damaged area in web IAW ER 03-5702-01123-KB1.Jun 5, 2001 · N168AW · Boeing 73733ASDR AWXA0001834Bulkhead · crackedHFEC indicates cracks at 4 HI-LOK fasteners in BS 178 BLKHD web WL 234.1 LBL 8-14. cut out damaged area and installed repair doubler and filler IAW SRM 53-10-08 pg 265-269 and 53-10-08 pg 265 item 13.Jun 5, 2001 · N168AW · Boeing 73733ASDR AWXA0001833Bulkhead · crackedHFEC indicates cracks at 4 HI-LOK fasteners in BS 178 BLKHD web WL 234.1 RBL 8-14. cut out damaged area of web and installed repair doubler and filler IAW SRM 53-10-08 pg 265-269.Jun 5, 2001 · N168AW · Boeing 73733ASDR ABXA010561Bulkhead · gougedFORWARD RADOME BULKHEAD, FORWARD SIDE, LOWER 0600 POSITION, GOUGE IN WEB. REPAIRED AREA IAW DC-8 SRM 53-2-0, 51-1-21, 51-1-8, 51-1-20, AND DAC DWG 4644898.Jun 4, 2001 · N818AX · Doug DC863SDR ZW0A0103004Bulkhead · wornDURING CHECK-C MAINT FOUND WORN AREA ON STRINGER 1380, BULKHEAD, UPPER LT SIDE, FWD FACE APPROX 11 O'CLOCK. INSTALLED 0.050 DOUBLER OVER RUB AREA PER SRM 53-01.Jun 4, 2001 · N929TW · Doug DC982SDR AWXA0001816Bulkhead · crackedFWD pressure BLKHD BS 178 cracked web at WL 189 BL 0. repaired IAW SRM 51-40-2 fig 1 and SRM 51-30-2 pgs 2&3.Jun 4, 2001 · N186AW · Boeing 737277SDR AWXA0001805Bulkhead · crackedHFEC INSP FWD SIDE OF BS BLKHD WEB FOUND 2 CRACKS RBL 4.7 WL 196.2-197.1 AND 199.9-201.5. REPAIRED IAW SRM 53-10-8 FIG 211 PG 287-298.Jun 4, 2001 · N156AW · Boeing 7373G7SDR AWXA0001804Bulkhead · crackedULTRASONIC CRACK INDICATIONS BS 178 BLKHD WEB FWD FACE 2 LBL 6.6 WL 209.5-210, 212.1-212.4 .5 INCH AND .3 INCH RESPECTIVELY. REPAIRED CRACKS IAW SRM 53-10-08 PG 287-298.Jun 4, 2001 · N156AW · Boeing 7373G7SDR AWXA0001803Bulkhead · crackedULTRASONIC CRACK INDICATION BS 178 FWD FACE BLKHD WEB RBL 6.6 WL 212-212.7 .7 INCH LENGTH. REPAIRED IAW SRM 53-10-8 PG 287-298.Jun 4, 2001 · N156AW · Boeing 7373G7SDR AWXA0001801Pressure Panel · crackedCRACK IN PRESSURE WEB BS 663 APPROX LBL 34 ON TOP OF WEB. REPAIRED IAW ER 03-5702-01135-JS2.Jun 4, 2001 · N156AW · Boeing 7373G7SDR UPS01436111Pressure Panel · crackedINSPECTION TYPE:C, NOSE W/W TOP PNL WEB FOUND CRACKED AT STA 285 - 290 RBL 10 BWL 190 UPPER SURFACE. NOSE W/W TOP PANEL STA 285 - 290 RBL 10 BWL 190 CRACKED WEB REPAIRED AS PER RS R53-18-34659.Jun 2, 2001 · N674UP · Boeing 747123SDR USAA010598Skin · dentedCLT - FOUND BULKHEAD SKIN DENTED 1 INCH BY .5 INCH BY .005 INCH DEEP, BS 1016 PRESSURE BULKHEAD, LBL 10 INCHES FROM CENTER. INSTALLED DOUBLER PER SRM 53-10-4 FIG 3. (M)Jun 1, 2001 · N284AU · Boeing 7372B7SDR SWAA011615Bulkhead · crackedDURING SCHEDULED SPECIAL VISIT CHECK, FOUND BULKHEAD WEB CRACKED AT BS 178, LBL 6 & WL 200. REPAIRED WEB PER SRM.Jun 1, 2001 · N348SW · Boeing 7373H4SDR SWAA011614Bulkhead · crackedDURING SCHEDULED D-CHECK, FOUND BULKHEAD WEB CRACKED AT BS 178, WL 180 & RBL 20. REPAIRED WEB PER SRM.Jun 1, 2001 · Boeing 7372H4SDR DL733010905Bulkhead · crackedINSPECTION OF THE FS 178 BULKHEAD WEB REVEALED A CRACK IN A TOOLING HOLE AT WL 234 AND LBL 12. A SECOND CRACK WAS FOUND AT A FASTENER HOLE AT WL 233 AND LBL 12. THE HOLES WERE OVERSIZED TO REMOVE THE CRACKS. THE AREA WAS THEN REPAIRED WITH AN EXTERNAL ALUMIJun 1, 2001 · N948WP · Boeing 737301SDR QXEA0100984Bulkhead · canningYYC - REAR PRESSURE BULKHEAD FRONT SIDE AT BUTT LINE 1050L AND HORIZONTAL BEAM XI, SKIN IN OIL CANNED INWARDS. REPAIRED IAW HORIZON AIR EA 4-53-1492.May 31, 2001 · N481US · Fokker F28MK4000SDR UPS01436136Bulkhead · crackedINSPECTION TYPE:C, NOSE W/W BS 400 BHD PRESSURE PAN FOUND 2 CRACKS BY APPROX 1 X .5 INCH LONG AS MARKED. NOSE W/W BS 400 BULKHEAD PRESSURE PAN REPLACED AS PER DWG 624U0005 SHEET 7.May 31, 2001 · N674UP · Boeing 747123SDR 2001UALA00893Bulkhead · gougedAFT PRESSURE BULKHEAD FWD WEB IS GOUGED AT BS 1016, WL 259, RBL 13. ACCOMPLISHED DOUBLER REPAIR. MAJOR REPAIR ACCOMPLISHED.May 31, 2001 · N318UA · Boeing 737322
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