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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR SWAA042043Pressure Panel · crackedDURING SCHEDULED 1/4D CHECK, FOUND BEADED PRESSURE WEB AT BS 664, LBL 31.5, CRACKED. REPAIRED PRESSURE WEB PER SRM.SDR 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 THSDR 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.SDR CALA0400574Bulkhead · corrodedINSPECTION FOUND APB WEB CORRODED ON BOTTOM SIDE AT STA 1016, BBL 0. REPAIRED IAW ECRA 5311-01200.SDR 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.SDR 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 CARSDR 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 SDR 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 SRSDR SWAA041929Bulkhead · crackedDURING SCHEDULED 1/4D CHECK, FOUND BULKHEAD VERTICAL BEAM WEB AT BS 178, RBL 17, CRACKED. REPAIRED WEB PER SRM.SDR C1HA200479001Bulkhead · crackedLEFT MAIN GEAR WHEEL WELL AFT PRESSURE BULKHEAD UPPER CHORD IS CRACKED AT O/B CORNER, STA 950 BL 60L.SDR SWAA041863Stiffener · corrodedDURING SCHEDULED 1/4D CHECK, FOUND RADIAL STIFFENER AT BS 1016, BL 0, CORRODED. REPAIRED STIFFENER PER SRM.SDR COMA0460389Bulkhead · crackedFORWARD SIDE FS 621.00 BULKHEAD LEFT AND RIGHT FLOOR ANGLES CRACKED. REPAIRED IAW REO 601R-53-61-004.SDR SWAA041744Bulkhead · crackedDURING SCHEDULED PM CHECK, FOUND BULKHEAD AT LEFT BS 727, LEFT MLG W/W FLAP MOTOR ATTACH, CRACKED. REPAIRED BULKHEAD PER EA.SDR SWAA041722Bulkhead · crackedDURING SPV, FOUND BULKHEAD WEB AT BS 178, RBL 6 TO RBL 10, CRACKED. REMOVED AND REPLACED WEB SECTION PER SRM.SDR SWAA041714Stiffener · corrodedDURING SCHEDULED 1/4D CHECK, FOUND BULKHEAD RADIAL STIFFENER AT BS 1016, BL 0, CORRODED. REMOVED STIFFENER PER SRM.SDR 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.SDR 0401199882Bulkhead · corrodedDURING H-CHECK FOUND CORROSION ON AFT PRESSURE BULKHEAD WEB AT Z=6.0 NEAR L18R. REPAIRED IAW EA 98-199571.SDR ABXA040228Stiffener · crackedP-DOME STIFFENER OUTBOARD END CLIP CRACKED IN RADIUS AT LONGERON 12 RIGHT. REMOVED AND REPLACED CLIP IAW DC-9 DWG 9915558.SDR ABXA040231Stiffener · crackedP-DOME STIFFENER OUTBOARD END CLIP CRACKED AT LONGERON 15 LEFT. REPAIRED STIFFENER IAW DC-9 DWG J060110.SDR ABXA040230Stiffener · crackedP-DOME STIFFENER OUTBOARD END CLIP CRACKED AT LONGERON 14 LEFT. REPAIRED IAW DC-9 SERVICE BULLETIN 53-166.SDR 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.SDR SWAA041683Stiffener · crackedDURING SPV, FOUND BULKHEAD ANGLE STIFFENER AT BS 663, LBL 10 TO LBL 24, CRACKED. REMOVED AND REPLACED STIFFENER SRM.SDR SWAA041681Frame · crackedDURING SPV, FOUND BULKHEAD SIDE FRAME AT LT AND RT BS 178, WL 208, CRACKED. REMOVED AND REPLACED FRAME SECTIONS PER ACO.SDR CALA0400534Angle · corrodedINSPECTION FOUND LOWER ANGLE AT AFT BULKHEAD OF FORWARD CARGO COMPARTMENT CORRODED. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-02.SDR 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, INSDR AUS20040501Firewall · cracked(AUS) APU FIREWALL CRACKED AT 7 O'CLOCK POSITION. FOUND DURING INSPECTION IAW AD/BAE146/053.SDR 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.SDR 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.SDR 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)SDR SWAA041624Pressure Panel · crackedDURING SCHEDULED 1/4D CHECK, FOUND BEADED WEB AT BS 672, LBL 31, CRACKED. REPAIRED WEB PER SRM.SDR 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.SDR 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)SDR SWAA041566Bulkhead · corrodedDURING SPV, FOUND BULKHEAD WEB AT BS 1016, BL 0, CORRODED. REPAIRED BULKHEAD WEB PER ER.SDR 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= 1431-14SDR 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.SDR 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.SDR 04FDEA01558Pressure Blkhd · corrodedLEFT MLG W/W AFT BULKHEAD IS CORRODED. REMOVED AND REPLACED AFT BULKHEAD SKIN PANEL IAW SRM 51-31-01 AT MAE.SDR 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.SDR 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.SDR SWAA041509Bulkhead · crackedDURING SCHEDULED 1/4D CHECK, FOUND BULKHEAD DOME CAP AT BS 1016, BL 0, CRACKED. REPAIRED DOME CAP PER EA.SDR 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.SDR N150AW0019Pressure Panel · corrodedCORROSION AT BS 1016 AT LOWER DRAIN HOLE ON FORWARD SIDE OF THE PRESSURE PANEL. REPAIRED PER SRM 53-80-08.SDR 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.SDR 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.SDR 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.SDR N150AW0008Bulkhead · damagedDRILL MARK ON AFT PRESSURE BULKHEAD AT RBL 37.5 AT THE MOISTURE BARRIER RETAINER. REPAIRED PER SRM 53-80-08.SDR 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.SDR 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 TOSDR SWAA041446Pressure Panel · crackedDURING SCHEDULED 1/4D CHECK, FOUND BEADED PRESSURE WEB AT BS 663, RBL 40, CRACKED. REPAIRED BEADED PRESSURE WEB PER SRM.SDR 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, DATED
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