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 SWAA042043Pressure Panel · crackedDURING SCHEDULED 1/4D CHECK, FOUND BEADED PRESSURE WEB AT BS 664, LBL 31.5, CRACKED. REPAIRED PRESSURE WEB PER SRM.Jul 19, 2004 · N523SW · Boeing 7375H4SDR CA040716001Pressure Blkhd · tornAIRCRAFT WAS PARKED ON THE RAMP. MAINTENANCE PERSONNEL WANT TO TOW THE AIRPLANE. WHEN STARTING TO PULL THE AIRPLANE THE NOSE LANDING GEAR ACTUATOR UPPER ATTACHMENT BRACKET FAILED. AFTER THE INCIDENT THE PRESSURE BULKHEAD FOUND TO BE TORN AT THE B.L 0.0 AT THJul 16, 2004 · Lear 35ASDR LR7A04084Bulkhead · crackedDURING SCHEDULED C-5 INSPECTION DRC 2191 ACCOMPLISHMENT FOUND RBL 61 BULKHEAD WEB CRACKED AT FS 614 - 617, WL260. REPLACED WEB AT FS 577 - 617, WL 252 - 270 IAW SMP583 CHP51-60 AND 51-70 AND LAC MEA 382-53-04-053. DRC 2245.Jul 16, 2004 · N403LC · Lkheed 382GSDR CALA0400574Bulkhead · corrodedINSPECTION FOUND APB WEB CORRODED ON BOTTOM SIDE AT STA 1016, BBL 0. REPAIRED IAW ECRA 5311-01200.Jul 15, 2004 · N76355 · Boeing 7373T0SDR UPS04242850Bulkhead · crackedINSPECTION TYPE: C, CRACK ON FWD PRESSURE BULKHEAD AT WL 198 RBL 02. HFEC CARRIED, CRACK CONFIRMED AND END MARKED. REPAIR CARRIED OUT USING REPAIR KIT 65C36289-1. REPAIR CARRIED OUT IAW DRG 65C36289 & SRM 51-30-02.Jul 8, 2004 · N947UP · Boeing 72725CSDR UPS04242842Bulkhead · crackedINSPECTION TYPE:C, INSPECT CRACK ON BS 1183 BULKHEAD, SUSPECT CRACK IS LOCATED ON AFT SIDE OF BULKHEAD, WL 175 APPROX LBL 20. HFEC INSPECTION CARRIED OUT & CRACKS CONFIRMED AND ENDS MARKED. FASTENERS REMOVED AND CRACKS TRIMMED OUT IAW SRM 51-10-6, REPAIR CARJul 8, 2004 · N947UP · Boeing 72725CSDR 04FDEA02029Pressure Panel · canningFUSELAGE OIL CANNING FOUND ON CENTER LANDING GEAR WHEEL WELL RT VERTICAL WEBS FROM STA 1394.5 TO STA 1470. FUSELAGE, MAXIMUM DEPTH OF THE OIL CANNING ON CENTER LANDING GEAR WHEEL WELL RT VERTICAL WEBS FROM STA 1394.5 TO STA 1470 FOUND WITHIN LIMITS PER SRM Jul 8, 2004 · N606FE · Doug MD11FSDR 04FDEA02028Pressure Panel · canningFUSELAGE OIL CANNING FOUND ON CENTER LANDING GEAR WHEEL WELL LEFT VERTICAL WEBS FROM STA 1394.5 TO STA 1470. FUSELAGE, MAXIMUM DEPTH OF THE OIL CANNING ON CENTER LANDING GEAR WHEEL WELL LEFT VERTICAL WEBS FROM STA 1394.5 TO STA 1470 FOUND WITHIN LIMITS PER SRJul 8, 2004 · N606FE · Doug MD11FSDR SWAA041929Bulkhead · crackedDURING SCHEDULED 1/4D CHECK, FOUND BULKHEAD VERTICAL BEAM WEB AT BS 178, RBL 17, CRACKED. REPAIRED WEB PER SRM.Jul 8, 2004 · N327SW · Boeing 7373H4SDR C1HA200479001Bulkhead · crackedLEFT MAIN GEAR WHEEL WELL AFT PRESSURE BULKHEAD UPPER CHORD IS CRACKED AT O/B CORNER, STA 950 BL 60L.Jul 8, 2004 · N679MG · Boeing 727225SDR SWAA041863Stiffener · corrodedDURING SCHEDULED 1/4D CHECK, FOUND RADIAL STIFFENER AT BS 1016, BL 0, CORRODED. REPAIRED STIFFENER PER SRM.Jul 1, 2004 · N692SW · Boeing 7373T5SDR COMA0460389Bulkhead · crackedFORWARD SIDE FS 621.00 BULKHEAD LEFT AND RIGHT FLOOR ANGLES CRACKED. REPAIRED IAW REO 601R-53-61-004.Jun 22, 2004 · N416CA · Cndair CL6002B19SDR SWAA041744Bulkhead · crackedDURING SCHEDULED PM CHECK, FOUND BULKHEAD AT LEFT BS 727, LEFT MLG W/W FLAP MOTOR ATTACH, CRACKED. REPAIRED BULKHEAD PER EA.Jun 21, 2004 · Boeing 7372H4SDR SWAA041722Bulkhead · crackedDURING SPV, FOUND BULKHEAD WEB AT BS 178, RBL 6 TO RBL 10, CRACKED. REMOVED AND REPLACED WEB SECTION PER SRM.Jun 19, 2004 · N684WN · Boeing 7373T0SDR SWAA041714Stiffener · corrodedDURING SCHEDULED 1/4D CHECK, FOUND BULKHEAD RADIAL STIFFENER AT BS 1016, BL 0, CORRODED. REMOVED STIFFENER PER SRM.Jun 17, 2004 · N685SW · Boeing 7373Q8SDR EIA20041130Pressure Panel · delaminatedMAIN CABIN STA 1380, RBL 75.9, PRESSURE DECK WEB SHOWS EVIDENCE OF DELAMINATION. REMOVED DAMAGE, FABBED AND INSTALLED REPAIR IAW SRM 51-10-07, FIG 251-30-05 PGS 6-9, AND 51-30-02.Jun 16, 2004 · N470EV · Boeing 747273CSDR 0401199882Bulkhead · corrodedDURING H-CHECK FOUND CORROSION ON AFT PRESSURE BULKHEAD WEB AT Z=6.0 NEAR L18R. REPAIRED IAW EA 98-199571.Jun 16, 2004 · N670MC · Doug DC951SDR ABXA040228Stiffener · crackedP-DOME STIFFENER OUTBOARD END CLIP CRACKED IN RADIUS AT LONGERON 12 RIGHT. REMOVED AND REPLACED CLIP IAW DC-9 DWG 9915558.Jun 14, 2004 · N959AX · Doug DC941SDR ABXA040231Stiffener · crackedP-DOME STIFFENER OUTBOARD END CLIP CRACKED AT LONGERON 15 LEFT. REPAIRED STIFFENER IAW DC-9 DWG J060110.Jun 14, 2004 · N959AX · Doug DC941SDR ABXA040230Stiffener · crackedP-DOME STIFFENER OUTBOARD END CLIP CRACKED AT LONGERON 14 LEFT. REPAIRED IAW DC-9 SERVICE BULLETIN 53-166.Jun 14, 2004 · N959AX · Doug DC941SDR ABXA040229Stiffener · crackedP-DOME STIFFENER OUTBOARD END CLIP CRACKED AT LONGERON 12 LEFT, TOP AND BOTTOM. REPAIRED LOWER STIFFENER. REPLACED UPPER CLIP IAW DC-9 DWG J060110.Jun 14, 2004 · N959AX · Doug DC941SDR SWAA041683Stiffener · crackedDURING SPV, FOUND BULKHEAD ANGLE STIFFENER AT BS 663, LBL 10 TO LBL 24, CRACKED. REMOVED AND REPLACED STIFFENER SRM.Jun 14, 2004 · N729SW · Boeing 7377H4SDR SWAA041681Frame · crackedDURING SPV, FOUND BULKHEAD SIDE FRAME AT LT AND RT BS 178, WL 208, CRACKED. REMOVED AND REPLACED FRAME SECTIONS PER ACO.Jun 14, 2004 · N650SW · Boeing 7373H4SDR CALA0400534Angle · corrodedINSPECTION FOUND LOWER ANGLE AT AFT BULKHEAD OF FORWARD CARGO COMPARTMENT CORRODED. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-02.Jun 13, 2004 · N13248 · Boeing 737824SDR IXXA060150SPanel · crackedDURING ROUTINE C CHECK, FOUND NUMBER 1 ENGINE PYLON AFT PYLON ADAPTER PANEL CRACKED APPROXIMATELY 2 1/2 INCHES AT FORWARD ACCESS PANEL. REMOVED FASTENERS AS NEEDED TO REMOVE DAMAGE. FABRICATED DOUBLER, LOCATED, DRILLED, TRIMMED, DEBURRED, TREATED, PRIMED, INJun 10, 2004 · N605AL · Doug DC873FSDR AUS20040501Firewall · cracked(AUS) APU FIREWALL CRACKED AT 7 O'CLOCK POSITION. FOUND DURING INSPECTION IAW AD/BAE146/053.Jun 10, 2004 · Bag BAE146300ASDR DL73S040527Bulkhead · corrodedSTATION 1016 BULKHEAD WEB, STIFFENERS AND CHORDS CORRODED AT BL 0. CHORD SUFFERED DAMAGE AT BL 0 DURING COURSE OF REPAIR. AREA REPAIRED IAW ERA 089856-14AD.Jun 9, 2004 · N244WA · Boeing 737247SDR IXXA060212SSupport · corrodedDURING ROUTINE C CHECK FOUND LEFT WHEEL WELL FORWARD BULKHEAD SUPPORT CORRODED AT STATION 857, +X56 AND -Z25. REPLACED SUPPORT PER ALL APPLICABLE DATA.Jun 8, 2004 · N41CX · Doug DC862FSDR USAA040281Stiffener · corrodedPIT - FOUND BULKHEAD STIFFENER 1 INCH BY 2 INCH AREA, STATION 1016 LBL 0. REMOVED CORROSION AND INSTALLED REPAIR PER BOEING DWG 65C28106. (M)Jun 8, 2004 · N575US · Boeing 737301SDR SWAA041624Pressure Panel · crackedDURING SCHEDULED 1/4D CHECK, FOUND BEADED WEB AT BS 672, LBL 31, CRACKED. REPAIRED WEB PER SRM.Jun 8, 2004 · N641SW · Boeing 7373H4SDR IXXA060317SPanel · bulgedDURING ROUTINE C CHECK FOUND RIGHT HAND HORIZONTAL STABILIZER TRAILING EDGE UPPER PANEL BETWEEN STATION XE149 TO XE77 BULGED. REPAIRED PER ALL APPLICABLE DATA.Jun 5, 2004 · N41CX · Doug DC862FSDR USAA040279Bulkhead · corrodedPIT - FOUND WEB CORRODED .25 INCH AREA, STATION 1016, AFT PRESSURE BULKHEAD WEB AT BL 0 UNDER STIFFENER. REMOVED FASTENERS BURNISHED AREA, TREATED, PRIMED, RE-INSTALLED FASTENERS PER EO 5302V112A. (M)Jun 4, 2004 · N589US · Boeing 737301SDR SWAA041566Bulkhead · corrodedDURING SPV, FOUND BULKHEAD WEB AT BS 1016, BL 0, CORRODED. REPAIRED BULKHEAD WEB PER ER.Jun 3, 2004 · N314SW · Boeing 7373H4SDR 04FDEA01600Pressure Panel · canningRIGHT HAND WHEEL WELL - OIL CANNING FOUND AT STA: Y= 1395-1401, Z= -90 TO -100, DEPTH= 0.0549 INCH Y= 1401-1411, Z= -90 TO -100, DEPTH= 0.0941 INCH Y= 1411-1421, Z= -90 TO -100, DEPTH= 0.0921 INCH Y= 1421-1431, Z= -90 TO -100, DEPTH= 0.0976 INCH Y= 1431-14Jun 3, 2004 · N594FE · Doug MD11SDR SWAA041553Bulkhead · corrodedDURING SCHEDULED D-CHECK, FOUND BULKHEAD WEB AT BS 1016, BBL 0, BS 1016, LBL 2, CORRODED. REMOVED AND REPLACED WEB SECTIONS PER SRM AND BAC DRAWING.Jun 2, 2004 · N384SW · Boeing 7373H4SDR UPS04242582Bulkhead · crackedINSPECTION TYPE: C, SUSPECT CRACK IN NLG WW LOCATED ON PRESSURE WEB B STA 240 RBL 24. AREA REPAIRED IAW SRM 51-40-02.Jun 1, 2004 · N950UP · Boeing 72725CSDR 04FDEA01558Pressure Blkhd · corrodedLEFT MLG W/W AFT BULKHEAD IS CORRODED. REMOVED AND REPLACED AFT BULKHEAD SKIN PANEL IAW SRM 51-31-01 AT MAE.Jun 1, 2004 · N68051 · Doug DC1010SDR UPS04242590Bulkhead · crackedINSPECTION TYPE: C, SUSPECT CRACK IN NLG WHEEL WELL WALL AT LBL 24, BS 285 APPROX. REPAIR CARRIED OUT IAW SRM 51-40-2, 51-40-07 & MM 32-33-51.May 31, 2004 · N950UP · Boeing 72725CSDR CALA0400513Pressure Panel · crackedINSPECTION FOUND A 3 INCH CRACK IN PRESSURE WEB AT STA 727, RBL 17, FORWARD SIDE IN WHEEL WELL. THE CRACKED AREA WAS CUT OUT AND A DOUBLER AND FILLERS WERE INSTALLED IAW ECRA 5330-03352.May 28, 2004 · N23661 · Boeing 737524SDR SWAA041509Bulkhead · crackedDURING SCHEDULED 1/4D CHECK, FOUND BULKHEAD DOME CAP AT BS 1016, BL 0, CRACKED. REPAIRED DOME CAP PER EA.May 27, 2004 · N642WN · Boeing 7373H4SDR EIA2004131Pressure Panel · corrodedMAIN CABIN STA 1460, RBL 120 HAS SURFACE CORROSION AT UPPER MAIN WHEEL WELL PRESS WEB. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PER B747 SRM 53-10-07, FIG 2, PGS 4-10.May 26, 2004 · N470EV · Boeing 747273CSDR N150AW0019Pressure Panel · corrodedCORROSION AT BS 1016 AT LOWER DRAIN HOLE ON FORWARD SIDE OF THE PRESSURE PANEL. REPAIRED PER SRM 53-80-08.May 25, 2004 · N150AW · Boeing 7373G7SDR N150AW0015Bulkhead · crackedVERTICAL STIFFENER ON THE AFT SIDE OF BS 178 BULKHEAD IS CRACKED AT LBBL 5.7 AND WL 184. REPAIRED AREA PER SRM 53-10-8.May 25, 2004 · N150AW · Boeing 7373G7SDR N150AW0014Bulkhead · crackedHFEC REVEALED A CRACK INDICATION AT FASTENER AT RBBL 10.5 AND WL 234 ON THE BS 178 BULKHEAD. REPAIRED AREA PER SRM 53-10-8.May 25, 2004 · N150AW · Boeing 7373G7SDR N150AW0013Bulkhead · crackedHFEC REVEALED CRACK INDICATIONS ON THE I/B SIDE OF VERTICAL STRAP ON THE BS 178 BULKHEAD AT RBBL 5.7 AND WL 201 AND THE I/B SIDE OF THE VERTICAL STRAP AT LBBL 5.7 AND WL 198.5. REPAIRED CRACKED AREAS PER SRM 53-10-8.May 25, 2004 · N150AW · Boeing 7373G7SDR N150AW0008Bulkhead · damagedDRILL MARK ON AFT PRESSURE BULKHEAD AT RBL 37.5 AT THE MOISTURE BARRIER RETAINER. REPAIRED PER SRM 53-80-08.May 25, 2004 · N150AW · Boeing 7373G7SDR EIA2004093Pressure Panel · crackedNOSE WHEEL WELL SIDEWALL, LT SIDE HAS 6 INCH CRACK BETWEEN BS 264.5 AND 270.5, WL 154. REMOVED DAMAGE, FABRICATED FILLERS AND DOUBLERS. INSTALLED PARTS PER B747 RM 53-10-04, FIG 116.May 22, 2004 · N470EV · Boeing 747273CSDR CA040520004Bulkhead · cracked(CAN) MAINTENANCE INSPECTION REVEALED CRACKING IN THE LONGITUDINAL BULKHEADS (BOTH) BEHIND EACH ENGINE. THESE BULKHEADS RUN THE LENGTH OF THE NACELLE, FROM THE FIREWALL TO THE TRAILING EDGE OF THE NACELLE. THE CRACKS ARE PRESENT WHERE THE BULKHEADS NARROW TOMay 20, 2004 · Piper PA31TSDR SWAA041446Pressure Panel · crackedDURING SCHEDULED 1/4D CHECK, FOUND BEADED PRESSURE WEB AT BS 663, RBL 40, CRACKED. REPAIRED BEADED PRESSURE WEB PER SRM.May 20, 2004 · N525SW · Boeing 7375H4SDR ARWA20040508Pressure Panel · corrodedDURING AN A-CHECK INSPECTION THE FOLLOWING WAS FOUND; COCKPIT STATION 12.000 AND STA 8.000 SUBFLOOR WAS FOUND WITH CORROSION, RBL 60. REPAIRED FUSELAGE NOSE FLOOR PRESSURE PANEL BETWEEN -12 TO FS 8 AND L22L IAW ELEVEN INC DRAWING AS11566 SHEET 1 THRU 4, DATEDMay 19, 2004 · N906R · Doug DC863F
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