JASC 5312
Service difficulty reports · 20,045
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 08FDEA04225Angle · crackedRT MAIN GEAR WHEEL WELL AFT BULKHEAD UPPER OB CORNER BS 950 APPROX RBL 67, PRESSURE DECK ATTACH REPAIR ANGLE CRACKED. REMOVED FLOOR PANEL FOR ACCESS, REMOVED REPAIR ANGLE REF SRM 51-30-2. FABRICATED SPLICE PLATE REF DWG 65-89360. TREATED PRIMED SPLICE PLATE SDR SWAA085390Bulkhead · crackedDURING SCHEDULED 16Y CHECK, FOUND VERTICAL WEB CRACKED AT BS 178, LBL 16. REMOVED AND REPLACED VERTICAL WEB PER SRM.SDR ASOA200801394Bulkhead · crackedDURING EDDY CURRENT INSPECTION ON THE 621 BULKHEAD FWD FACE, AN INDICATION WAS NOTED AT LBL 48.00, WL 106, .500 IN LENGTH.SDR ASOA200801322Bulkhead · crackedWHILE PERFORMING TASK AWL253-41-201, AN INDICATION WAS NOTED AT THE FS 559 BULKHEAD WEB OUTBOARD OF RBL 9, WL 58.7 APPROX .300 INCH IN LENGTH AND INBOARD OF RBL 18, WL 58.7 APPROX 1.0 INCH IN LENGTH. REMOVED DAMAGED SECTION OF THE RT WEB, REPAIRED IAW REO 610SDR ASOA200801321Angle · crackedWHILE PERFORMING TASK AWL253-41-201, AN INDICATION WAS NOTED AT THE 559 BULKHEAD CAP ANGLE RADIUS LBL 9 AND LBL 18 APPROX .500 INCH IN LENGTH. ACCOMPLISHED REPAIR TO (LT SIDE ONLY) 559 BULKHEAD AND CAP ANGLE IAW REO 601R-53-41-260 REV C. REQUIRES PAINT. PAISDR ASOA200801320Bulkhead · crackedAN INDICATION WAS NOTED ON THE 621 BULKHEAD FWD FACE DURING AN EDDY CURRENT INSPECTION AT LBL 9.50, WL 110 .350 IN LENGTH. COMPLIED WITH REO 601R-53-61-1285, STEPS 1 THRU 33 FOR REPAIR TO AFT PRESS BULKHEAD FS 621 LBL 9.0. INCORPORATED REO 601R-53-61-2880 DISDR ASAA0873655Bulkhead · dentedDENT ON AFT FACE OF 1016 BULKHEAD 0.032 INCH IN DEPTH BEYOND LIMIT IAW B737 700 SRM 53 80 08. DENT ON AFT FACE OF 1016 BULKHEAD REPAIRED IAW B737 700 SRM 53 80 08 REPAIR 1 AND EA 5310 02829.SDR ASOA200801319Bulkhead · crackedREAR PRESSURE BULKHEAD WEB THAT SURROUNDS THE LINTEL ATTACHMENT FITTING HAS A INDICATION NOTED APPROX .1 INCH IN LENGTH 100 PERCENT FULL SCREEN HEIGHT FAILED NDT INSPECTION. THIS SDR WILL REMAIN OPEN PENDING MAINTENANCE DETERMINATION OF AN APPROPRIATE CORRECTSDR SWIA200820549Bulkhead · crackedC-CHECK, AFT PRESSURE BULKHEAD FORWARD FITTING CRACKED. REPAIRED PER REO.SDR ASOA20081254Bulkhead · damagedBLENDED 280 RT WEB IAW 51-12-00. PERFORMED UT THICKNESS MEASUREMENT OF FS 280.00 RIGHT BULKHEAD WEB, AFTER BLENDING, IAW REO 670-53-11-052 PER CRJ 700 NDTM 51-20-004. MINIMUM THICKNESS IS .038 INCH. 10/2/08 RESTORED A023 FINISH ON RT FS 280 WEB IAW REO 670-SDR CA081122001Bulkhead · cracked(CAN) DURING WALK-AROUND INSP, FOUND BELTFRAME AT 9G BULKHEAD CRACKED BY LT CARGO CAN CUTOUT. TEMPORARY REPAIR CARRIED OUT. A/C FERRIED. PERMANENT REPAIR CARRIED OUT. ACFT RETURNED TO SERVICE.SDR ABXA200810170253Bulkhead · crackedDURING INSPECTION, LOWER TWO FASTENER HOLES OF RIGHT CHORD SHOWED CRACK INDICATION. CRACK LENGTH = .0625 INCH. REPLACED CHORD IAW EA 53800002-003.SDR ASOA200801229Bulkhead · damagedREPAIRED REAR PRESSURE BULKHEAD WEB THAT SURROUNDS LINTEL ATTACHMENT FITTING IAW BOMBARDIER REO 601R-53-61-1230 REV D. FUSELAGE EXTERIOR REQUIRES PAINT. PAINTED LINTEL EXTERIOR REPAIR IAW CRJ SRM 51-25-01. REPAIR PER EC/TC REO 601R-53-61-1230 HAS BEEN COMPLSDR DLM8K081241Bulkhead · crackedTHE STA 1463 CANTED BULKHEAD STRUCTURE AND THE OVERLYING AFTERBODY SKIN PANEL BETWEEN THE VERTICAL STABILIZER ATTACH ANGLES WERE FOUND DAMAGED BETWEEN L-2L AND L-2R. CUT OUT DAMAGE AND INSTALLED REPAIRS TO THE BULKHEAD STRUCTURE. REMOVED AND REPLACED THE SKISDR DL757081233Bulkhead · corrodedDURING HMV AT SAA, CORROSION WAS FOUND IN THE RADIUS OF THE AFT LOWER CHORD OF THE AFT PRESSURE BULKHEAD AT STA 1862. THE CORROSION WAS REMOVED BY BLENDING TO A DEPTH OF 0.030 INCH. THE AREA WAS TREATED FOR CORROSION PREVENTION AND APPROVED AS IS BY BOEING ESDR SWIA200820502Bulkhead · crackedDURING C-CHECK, FS 280 LEFT BULKHEAD WEB CORRODED. REPAIRED PER REO.SDR SWIA200820501Bulkhead · corrodedDURING C-CHECK, FS 280 RIGHT BULKHEAD WEB CORRODED. REPAIRED PER REO.SDR AALA200802571Bulkhead · crackedRT LOWER SIDE PRESSURE BULKHEAD CRACKED AT STATION 110. CRACK LENGTH IS .5 INCH. INSTALLED DOUBLER WITH FINGERS IN ACCORDANCE ESO 80559 DATED 19 SEP 2008.SDR QXEA2008110401060Bulkhead · corrodedPDX - C4 - CORROSION AT RT LOWER BULKHEAD AT FS 280 RBL 9 TO RBL 18. BLENDED CORROSION, FOUND TO BE OUT OF LIMITS PER REO 670-53-11-052. REMOVED RT LOWER WEB PER REO 670-53-11-05 REPAIR NR 2, DRILLED AND DEBURRED NEW WEB REF REO 670-53-11-05 REPAIR NR 2. INSDR USAA920081798Bulkhead · crackedC-18 CHECK, NR 6132091, CRACKED WEB, BS 178, LBL 15, WL 234. REPAIRED WEB, BS 178, LBL 15, WL 234 IAW B737SRM 53-10-08-2R9, FIG 201. (K)SDR USAA920081812Bulkhead · crackedMCN - MAJOR REPAIR - C18 CHECK, CRACKED BULKHEAD WEB SKIN, BS 178, RBL 5.7, WL 212. REPAIRED BULKHEAD WEB SKIN, BS 178, RBL 5.7, WL 212 IAW B737 SRM 53-10-08-2R10 FIGURE 201.SDR LR7A08116Bulkhead · crackedDURING SCHEDULED B-3 CHECK, PER JOB CARD HB5302 FOUND AFT FUSELAGE INTERIOR BULKHEAD FLANGE CRACKED AT FS 847, WL 185, RBL 70. REPAIRED IAW SMP583 FIG 53-50-10.SDR LR7A08115Bulkhead · crackedDURING SCHEDULED B-3 CHECK, PER JOB CARD HB5302 FOUND AFT FUSELAGE INTERIOR BULKHEAD FLANGE CRACKED AT FS 847, WL 185, LBL 70. REPAIRED IAW SMP583 FIG 53-50-10.SDR DL764081214Bulkhead · corrodedDURING AN INSPECTION DURING HMV AT HAECO CORROSION WAS FOUND ON THE BS 955 BULKHEAD WEB AT LBL 90. THE CORROSION WAS REMOVED WITH A 3 INCH BY 10 INCH CUTOUT AND A DOUBLER INSTALLED PER ER/A 467812-14.SDR USAA920081702Bulkhead · crackedPIT FPBH MAJOR REPAIR JOB CARD NR EIA53032. 2 CRACKS ON VERTICAL WEB AT BS 178, WL184, RBL5.7. REPAIRED VERTICAL WEB AT BS 178, WL184, RBL5.7 IAW B737 SRM 53-10-08 AND US AIRWAYS EA NR 111653.SDR NWAA084499851Stiffener · crackedDURING H CHECK FOUND CRACK IN OTBD END OF UPPER AFT PRESSURE BULKHEAD HORIZONTAL STIFFENER. REPAIRED PER EA 98-213643.SDR TRAX200801188Isolator · crackedJOB 8769211 OPERATION 165 5 ISOLATORS ON FS 621 BULKHEAD IN CARGO BAY ARE CRACKED. RESOLVED ON W/O 100685 TASKCARD NR 00240. C/A REPLACED THE 5 CRACKED ISOLATORS ON FS 621 BULKHEAD IAW CRJ 200 SRM 51-42-13.SDR USAA20081690Bulkhead · crackedPIT FPBH MAJOR REPAIR IOG NR 4352192 HIGH FREQUENCY EDDY CURRENT REVEALED CRACK INDICATION AT 4 FASTENERS BS178, WL234, RBL5.7. REPAIRED CRACK AT FASTENERS BS178, WL234, RBL5.7 IAW B737 SRM 53-10-08 FIG 201 REPAIR 9.SDR SWAA085100Bulkhead · crackedDURING SCHEDULED 18Y CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 178, RBL 5.7, WL 183. REPAIRED WEB PER ER.SDR USAA920081685Bulkhead · crackedCLT FPBH MAJOR REPAIR NR 4352195 & 4353371 PITTING CORROSION ABOVE & BELOW HORIZONTAL STIFFENER ON BULKHEAD WEB AT BS178, WL218. ALSO CRACK AT BS218, LBL10. REPAIRED PITTING CORROSION ABOVE & BELOW HORIZONTAL STIFFENER AND CRACK ON BULKHEAD WEB AT BS178, WL2SDR CALA0800902Bulkhead · damagedAFT PRESSURE BULKHEAD WEB FROM FLOOR LEVEL TO Y-CORD FROM APPROXIMATELY LBL 6 TO APPROXIMATELY LBL 20 HAS OVERHEAT DAMAGE. REMOVED AFT PRESSURE BULKHEAD WEB FROM CENTER RING TO Y-CHORD AND REPLACED BULKHEAD WEB (P/N-65-46568Y524) AND DOUBLER (P/N-65-46568-696SDR ASAA0873546Angle · damagedFWD CARGO PIT AFT BULKHEAD LOWER ANGLE BETWEEN STR 26R AND STR 26L AT BS 500D. AREA BLENDED AND FOUND TO BE BEYOND ALLOWABLE DAMAGE LIMIT. LOWER ANGLE REMOVED AND REPLACED WITH MADE REPAIR PART IAW B737 700 SRM 51 20 05 & 51 40 02.SDR SWIA200820516Bulkhead · crackedDURING C-CHECK, AFT PRESSURE BULKHEAD CRACKED AT FITTING UPPER INBOARD CORNER. REPAIRED PER REO.SDR EIA2008049Pressure Panel · corrodedLT MAIN GEAR W/N FWD WALL LOWER IB EDGE HAS CORROSION, ANGLE HOLDING STEAL HAS 100 PERCENT MATERIAL LOSS. WEB CORRODED AT BS 1253 LBL 16- LBL 46. WEB REPAIRED IAW SUPPLEMENTAL WORKSHEET. CORRODED SEAL RETAINER REPLACED SRM 51-30-42 REF NRC NR 112 AND SUPPLEMESDR SWIA200820490Fitting · crackedDURING C-CHECK, REAR PRESSURE BULKHEAD LINTEL FITTING UPPER AND LOWER INBOARD CORNERS CRACKED. REPAIRED PER REO.SDR SWIA200820489Bulkhead · crackedDURING C-CHECK, FS 621 BULKHEAD WEB CRACKED ABOVE LINTEL FITTING. REPAIRED PER REO.SDR SWIA200820484Fitting · crackedDURING C-CHECK, LOWER INBOARD CORNER OF LINTEL FITTING, REAR PRESSURE BULKHEAD, CRACKED. REPAIRED PER REO.SDR SWAA084996Pressure Panel · crackedDURING SCHEDULED BRDG CHECK, FOUND NLG W/W RT CEILING PANEL CUTOUT WEB CRACKED. REPAIRED WEB PER ACO.SDR SWAA084995Pressure Panel · crackedDURING SCHEDULED BRDG CHECK, FOUND NLG W/W LT CEILING PANEL CUTOUT WEB CRACKED. REPAIRED WEB PER ACO.SDR USAA920081922Pressure Panel · crackedMCN C18 MAJOR REPAIR NR 6131676 MLG WW PRESSURE WEB CRACKED AT BS 663.75. WL204, LBL40. REPAIRED MLG WW PRESSURE WEB AT BS 663.75, WL204, LBL40 IAW US AIRWAYS EA NR 130128.SDR SWAA084981Structure · crackedDURING SCHEDULED SPV CHECK, FOUND VERTICAL CHORD CRACKED AT BS 178, LBL 5.5. REPAIRED CHORD PER SRM.SDR KNN2008F00002Bulkhead · crackedWHILE COMPLYING WITH AD 2000-05-29 PARA (A) DURING THE CURRENT C-CHECK, WE FOUND MULTIPLE CRACKS ON THE FWD PRESSURE BULKHEAD AT STA 178. DAMAGE WAS CUTOUT AND REPAIRED IAW SRM 53-10-10 FIG 1. (K)SDR USAA920081699Structure · crackedCLT Q1 MAJOR REPAIR NR 03-0553-8-0349/001. CRACK ON VERTICAL CHORD OF 178 BULKHEAD AT WL 184, LBL5.7. REPAIRED VERTICAL CHORD OF 178 BULKHEAD AT WL 184, LBL5.7 IAW B737 SRM 53-10-08 REPAIR NR 5.SDR USAA920081688Bulkhead · crackedPIT FPBH MAJOR REPAIR NR 4353372 CRACK IN WEB OF RT VERTICAL BEAM OF 178 BULKHEAD AT RBL17, WL230. REPAIRED WEB OF RT VERTICAL BEAM OF 178 BULKHEAD AT RBL17, WL230 IAW B737 SRM 53-10-08.SDR USAA920081638Bulkhead · crackedPIT FPBH MAJOR REPAIR LOG NR 4353301. 2 CRACKS ON 178 BULKHEAD AT RIVET FASTENERS AT WL234, RBL8, ON FORWARD SIDE. REPAIRED 178 BULKHEAD AT RIVET FASTENERS AT WL 234, RBL8 IAW B737 SRM 53-10-08.SDR CALA0800862Bulkhead · canningPER EA 5310-04639 REV A STEP 3.1, AFT PRESURE BULKHEAD HAS ONE OIL CAN SPOT STATION 1016 BETWEEN STR 0L AND 2L AT WATER LINE STATION 304. FABRICATED AND INSTALLED REPAIR PER ECRA 5311-01420. DIP WRITEN TO ACCOMPLISH A PERMANENT REPAIR WITHIN 12 MONTHS FROM SSDR USAA920081637Bulkhead · crackedPIT FPBH MAJOR REPAIR EO NR 5300V152 & LOG NR 4352189. 5 INCH CRACK AFT OF BULKHEAD BS178 TO 182, WL226-234, RBL17. REPAIRED BULKHEAD BS178 TO 182, WL226-234, RBL17 IAW B737 SRM 53-10-08 REPAIR NR 12.SDR COMA086380Bulkhead · crackedCRACK ON AFT PRESSURE BULKHEAD ABOVE CARGO DOOR TRACK AT LBL 27.50. REPAIRED AFT PRESSURE BULKHEAD AT LBL 27.50 IAW REO 601R-53-61-1541.SDR TRAX200801078Isolator · brokenJOB 8801625 OPERATION 57 AFT PRESSURE BULKHEAD FS 621 HAS A BROKEN ISOLATOR AT LBL9, WL93. RESOLVED ON W/O 98370 TASKCARD: NR 00336. REMOVED BROKEN ISOLATOR AND INSTALLED NEW SERVICEABLE ISOLATOR IAW CRJ 200 SRM 51-42-06.SDR C2XA08SH113Firewall · crackedSHV DURING C-CHECK APU FIREWALL CRACKED AT LT UPPER, RT LOWER APU MOUNTS. MX REPAIRED APU FIREWALL LT UPPER, RT LOWER APU MOUNTS IAW EC5330-01838. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
Back to JASC 5312