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 SWAA071489Vertical Beam · crackedDURING SCHEDULED 10Y CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 184, RBL 17.1. REPAIRED WEB PER SRM.SDR SWAA071490Vertical Beam · crackedDURING SCHEDULED 10Y CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 184, LBL 17.1. REPAIRED WEB PER SRM.SDR TRAX200700427Bulkhead · crackedAFT PRESSURE BULKHEAD FS 621 IS CRACKED AT LINTEL ATTACHMENT FITTING.SDR 07FDEA00967Pressure Panel · damagedFASTENER CAN'T BE INSTALLED AT AFT NOSE LANDING GEAR PANEL, C17-18, P52-53 RT. REPAIR WAS PERFORMED BY FASTENER SUBSTITUTION IAW EA 6-5312-103408 REV A.SDR ABXA070102Bulkhead · crackedAFT PRESSURE BULKHEAD LOWER DOOR CORNER HAD A CRACK IN SKIN. THE REPAIR INSTALLED DID NOT MATCH ANY CONFIGURATION OF DWG J060088 IN NUMBER, PLACEMENT AND MATERIAL OF DOUBLERS. REMOVED PREVIOUS REPAIR. NO CRACKS FOUND. REPAIRED LOWER DOOR CORNER IAW SERVICESDR N865R623002Bulkhead · crackedAFT FLAT PRESSURE BULKHEAD WEB STA 1766 L11L CRACK CPCP 5730 0551.SDR ABXA070075Bulkhead · corrodedAFT LOWER CARGO, AFT BULKHEAD WEB EXFOLIATED AT LEFT BUTT LINE 18 INCHES AT TOP. REPAIRED DAMAGE IAW DC9 SRM 53-01.SDR ABXA070074Bulkhead · corrodedAFT LOWER CARGO, AFT BULKHEAD WEB AND ANGLE EXFOLIATED AT RIGHT BUTT LINE 4 INCHES AT BOTTOM SIDE. REPAIRED DAMAGED IAW ABX ENGINEERING TO DUPLICATE PRODUCTION SPLICE IAW DACO DWG 9915561 AND DC9 SRM 51-30-0.SDR COMA0760257Post · crackedDURING INSPECTION FOUND BULKHEAD VERTICAL POST, LOWER END CRACKED, FS 559, RBL 18. REMOVED DAMAGE AND INSTALLED DOUBLER PER BOMBARDIER REO 601R-53-41-067.SDR WRLA2007047Frame · corrodedDURING C-04 CHECK, CORROSION FOUND AT BULKHEAD TEE CHORD STA Y=2007, Z=20, X=-20. REPAIR PER MD-11 SRM 51-33-01 & 51-35-01 REV.38SDR 07FDEA00837Bulkhead · crackedDURING ACF MODIFICATION, FOUND TO AFT PRESSURE BULKHEAD AT STA 595 LONG 9 LT WITH CRACK 1". REPLACED LONGERON CLIP FOR SRM 51-31-01 VOL II.SDR 07FDEA00833Bulkhead · corrodedFOUND FWD CARGO STA 720D LWR BULKHEAD BEAM HAS CORROSION AT LBL25. REMOVED AND REPLACED ANGLE IAW SRM 51-30-2.SDR ABXA070093Bulkhead · crackedAFT PRESSURE BULKHEAD LEFT UPPER DOOR CORNER HAD 2 CRACKS THAT NEEDED TO BE STOP DRILLED. REMOVED OUTSIDE DOUBLER, STOP DRILLED CRACKS IAW SRO J060088. REINSTALLED DOUBLER IAW SRO J060088 AND DC9 SRM 51-30-5. CRACK LENGTHS WERE 7/8", 3/4" AND 1".SDR N865F624003Bulkhead · crackedAFT FLAT PRESSURE BULKHEAD WEB STA 1766 L-11R-12R CRACK CPCP 5730 0551.SDR 07FDEA00746Panel · unknownOLD CORROSION REPAIR ON FRONT PANEL OF NOSE LANDING GEAR BAY. REPAIR VERIFICATION, PERFORMED IAW RAS/AS/073/02 ISSUE: A, EA FOR TRACKING: 6-5312-103346.SDR EIA2007053Pressure Panel · crackedNOSE WHEEL WELL WEB CRACKED BETWEEN STA 265-280 LT SIDE AT WL 160. REMOVED DAMAGE, NDT'D AREA, FABRICATED AND INSTALLED REPAIR PER B747 SRM 53-10-04 FIGURE 116 PAGES 708-711.SDR AWXA200700438Gusset · crackedMCN - BS 540 BULKHEAD VERTICAL STIFFENER ATTACH ANGLE CRACKED, LBL 45, WL 208. REPLACED BS 540 BULKHEAD VERTICAL STIFFENER ATTACH ANGLE, LBL 45, WL 208 IAW B737-300 SRM 51-40-02.SDR AWXA200700375Bulkhead · crackedMCN - FOUND CRACKED VERTICAL WEB, BS 178, RBL 5.7, WL 180. REPAIRED VERTICAL WEB, BS 178, RBL 5.7, WL 180 IAW B737-300 SRM 53-10-08 FIGURE 201.SDR AWXA200700374Vertical Beam · crackedMCN - FOUND CRACKED VERTICAL WEB, BS 178, LBL 17.1, WL 230. REPAIRED VERTICAL WEB, BS 178, LBL 17.1, WL 230 IAW B737-300 SRM 53-10-08 FIGURE 201.SDR AWXA200700371Vertical Beam · crackedMCN - FOUND CRACKED VERTICLE BEAM WEB, BS 178, RBL 17.1, WL 240. REPAIRED VERTICLE BEAM WEB, BS 178, RBL 17.1, WL 240 IAW B737-300 SRM 53-10-08 FIGURE 201.SDR TRAX200700336Bulkhead · corrodedRIGHT LOWER FS BULKHEAD WEB HAS CORROSION. REPLACED WEB.SDR SWAA071273Pressure Panel · crackedDURING SCHEDULED 18Y CHECK, FOUND NLG WHEEL WELL WEB CRACKED AT BS 251, RBL 7.75. REPAIRED WEB PER ACO.SDR 07FDEA00699Bulkhead · corrodedOLD CORROSION REPAIR IN FUSELAGE CENTER SECTION AT C39 AND CORROSION AT PRESSURE BULKHEAD. REPAIR WAS VERIFIED AND PERFORMED IAW RAS: 047609/013/2006 ISSUE:A.SDR UPS07849598Pressure Panel · crackedINSPECTION TYPE:C3 CRACK IN NLG WHEEL WELL CEILING (PRESSURE WEB) STA -13 LBL 2. REPAIRED PRESSURE WEB IN NLG WHEEL WELL CEILING AT STA -13 LBL 2 IAW SAA EA008-5330-01-A0745, UPS EO DC8-5330-26455-A, AND FAA FORM 8100-9.SDR ABXA070112Pressure Panel · corrodedWHEEL WELL PRESSURE PANEL WAS BULGED AND CRACKED AT APPROXIMATELY FS 708, BUTT LINE 0. REPAIRED WHEEL WELL PRESSURE PANEL APPROXIMATELY FS 708 IAW DC9 REA D953-55487.SDR DXTA200702001Seal · wornLOUD GRINDING NOISE DURING GEAR DOWN CYCLE. DURING CYCLE, 20 SECOND WARNING LIGHT STARTED FLASHING. 3 GREEN/ NO RED WAS INDICATED APPROXIMATELY 10 SECONDS AFTER 20 SECOND WARNING FLASHER. INSPECTED MLG, MLG DOORS NOSE CONE. NO DEFECTS NOTED. PERFORMED MLG SWINSDR SWIA200718133Bulkhead · crackedFS 280 BULKHEAD LBL9 HAS CRACKED CLIP ON OUTBOARD SIDE, DISCOVERED ON C-CHECK INSPECTION. REPLACED CLIP AT STATION 280 LBL9 P/N 601R31113-57 IAW CRJ200 SRM 51-42-20 PGS 23-24.SDR SWIA200718132Bulkhead · crackedSTATION 280 BULKHEAD RBL9 HAS INBOARD AND OUTBOARD CRACKED CLIPS, DISCOVERED ON C-CHECK INSPECTION. REMOVED AND REPLACED INBOARD AND OUTBOARD CLIP PER CRJ200 REO 601-53-11-177 AND STANDARD REPAIR 601R 53-0057A.SDR SWIA200718131Bulkhead · crackedSTATION 280 BULKHEAD RBL 12.0 LOWER FLANGE IS CRACKED, DISCOVERED AT C-CHECK INSPECTION. INSTALLED REPAIR ANGLE -4 CLIPS AND -6 FILLER AT STATION 280 BULKHEAD RBL 12 PER CRJ200 REO 601R53-11-171.SDR A6WA200740098Bulkhead · crackedVISUAL INDICATION OF CRACK IN FWD PRESSURE BULKHEAD FS202.75, WL69.0, LBL23.71 (JUST BELOW PARKING BRAKE CABLE). MEASURES APPROX 1.0 INCH LONG. MAINTENANCE CUT-OUT DAMAGED AREA AND INSTALLED REPAIR DOUBLER IAW REO 601R-53-11-563. (K)SDR UIEA200700124Bulkhead · corrodedBS 1250, L WLG W/W CANTED PRESSURE BULKHEAD, NR 2 PACK COOLING DUCT CUTOUT FOUND CORROSION. REPAIRED ACCOMPLISHED AS PER BOEING SR ID NR 1-289645346-1 THRU -5 AND FAA FORM 8100-9.SDR SWAA071162Bulkhead · crackedDURING SCHEDULED 20Y CHECK, FOUND AFT PRESSURE BULKHEAD WEB CRACKED AT BS 1016, STR 6L. REPAIRED BULKHEAD WEB PER ER.SDR SWAA071163Bulkhead · crackedDURING SCHEDULED 20Y CHECK, FOUND AFT PRESSURE BULKHEAD WEB CRACKED AT BS 1016, STR 6R. REPAIRED BULKHEAD WEB PER ER.SDR SWAA071164Bulkhead · crackedDURING SCHEDULED 20Y CHECK, FOUND AFT PRESSURE BULKHEAD WEB CRACKED AT BS 1016, STR 13L. REPAIRED BULKHEAD WEB PER ER.SDR KCSA071095Bulkhead · dentedAFT PRESSURE BULKHEAD HAS SEVERAL SMALL DENTS RBL 55, WL 220, STA 2400.SDR KCSA071094Bulkhead · dentedAFT PRESSURE BULKHEAD HAS SEVERAL SMALL DENTS RBL 30, WL 200, STA 2390.SDR 07FDEA00612Bulkhead · crackedCLG WW FOUND 1 CRACK 1.25" LONG ON HORIZONTAL BULKHEAD BETWEEN STA 1481 AND 1491 X= 30 RT. TRIMMED OUT DAMAGED PORTION OF WEB AND INSTALLED FILLER AND REPAIR DOUBLER IAW SRM 53-00-01 FIG 4 SHT 2 VOL 1. REPLACED INTERCOSTAL IAW SRM 51-35-01 VOL 1 PAR 1-5. FASDR SWAA071145Pressure Panel · crackedDURING SCHEDULED 18Y CHECK, FOUND BEADED PRESSURE WEB CRACKED AT BS 665, RBL 38. REPAIRED WEB PER SRM.SDR 07FDEA00600Pressure Panel · corrodedMAIN CABIN BTWN STA 535 AND 555 X= 90 BTWN HORIZ PRESS PANEL AND FINGER DOUBLER FOUND CORROSION. REMOVED FINGER DOUBLER AND CORROSION IAW SRM 51-35-01 PAGE 1-13 VOL 2 AND SRM 51-21-01 PAR 34. PERF INSP IAW NDTSPM04 FOUND NOM THK.050", MIN .036" IS OUT OF LIMSDR 07FDEA00589Bulkhead · crackedRT AIR CONDITIONING COMPT CRACK 1" LONG ON INTERNAL VERTICAL BULKHEAD AT STA 495 Z= -58. REMOVED PORTION OF BROKEN WEB, AND REPAIRED IAW SRM 53-40-00 VOL 1 FIG 34. FABRICATED PARTS IAW DETAIL PARTS TRAVELER I035881/N00881 AND IAW SRM 53-40-00 VOL 1.SDR DL757070560Bulkhead · gougedTHE AFT FUSELAGE PRESSURE BULKHEAD WAS DAMAGED DURING A TAIL STRIKE. THE BULKHEAD CHORDS WERE CUT OUT AND A NEW SECTION WAS FABRICATED AND SPLICED IN. REF ER/A'S 460538-14 AND 460643-14 FOR SAME DAMAGE.SDR SWIA200718116Bulkhead · crackedCRACKED CLIP ON AFT SIDE OF STA 280 BULKHEAD, DISCOVERED AT C-CHECK INSPECTION. REPLACED CLIP P/N 601R51570-31 IAW CRJ200 SRM 51-40-11.SDR CALA0700089Bulkhead · corrodedFWD APB LOWER CENTER SECTION WEB CORRODED. REPAIRED IAW ECRA 5311-01298.SDR SWAA071057Bulkhead · crackedDURING SCHEDULED SPV CHECK, FOUND BULKHEAD WEB CRACKED AT BS 178, LBL 12, WL 218. REPAIRED WEB PER SRM.SDR SWAA071056Bulkhead · crackedDURING SCHEDULED SPV CHECK, FOUND BULKHEAD WEB CRACKED AT BS 178, LBL 5.7, WL 207. REPAIRED WEB PER SRM.SDR SWAA071028Bulkhead · crackedDURING SCHEDULED 20Y CHECK, FOUND AFT PRESSURE BULKHEAD WEB CRACKED AT BS 1016, STR 3R. REPAIRED BULKHEAD PER SRM.SDR UPS07449412Pressure Panel · corrodedINSPECTION TYPE:C LEFT BODY LANDING GEAR W/W PRESSURE DECK ATT WEB FOUND SURFACE CORROSION AT STA 1403 LBL 125. CORROSION BLEND OUT 0.034 X 1 X 1 INCH EXCEED SRM 53-10-01 FIG 1 LIMITS. LEFT BODY LANDING GEAR W/W PRESSURE DECK ATT WEB REPAIRED AT STA 1403 LBLSDR LR7A07030Bulkhead · crackedDURING SCHEDULED C-7 CHECK PER JOB CARD HC5313, FOUND RT OUTBOARD BULKHEAD CAP CRACKED AT FS 1012, RBL67, WL270. REPAIRED BULKHEAD IAW MEA 382-53-07-011.SDR LR7A07022Cap · crackedDURING SCHEDULED C-7 CHECK PER JOB CARD HC5315, FOUND RT AFT FUSELAGE BULKHEAD INNER CAP CRACKED AT FS 770, RBL67, WL162. REPAIRED CAP IAW SMP583 53-50-14.SDR LR7A07021Bulkhead · crackedDURING SCHEDULED C-7 CHECK PER JOB CARD HC5324, FOUND RT MWW REAR BULKHEAD WEB CRACKED AT FS 617, RBL 73, WL 185. REPLACED WEB IAW SMP583 51-60.
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