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.

SDR UHLA201504210359Rib · crackedDURING INSPECTION, THE RT WING ZONE 651, RIB 22 WAS FOUND TO BE CRACKED AT YA 9031.0. THE AREA WAS REPAIRED IAW ETD 2015-145-041608.Apr 21, 2015 · N274SK · Emb EMB145LRSDR ASAA2015042111471Pressure Panel · crackedRT WHEEL WELL RT UPPER PRESSURE PANEL CRACKED. ACFT GROUNDED. REPAIRED RIGHT WHEEL WELL PRESSURE PANEL IAW B737-800 SRM 57-10-10-2R-3 ALTERNATIVE 2,INSTALLED AND REMOVED TEMPORARY EWIS PROTECTION COVES IAW B737-800 AMM 20-630-07,RESTORED FINILSH IA WB737-800Apr 21, 2015 · N579AS · Boeing 737890SDR ASOA2015051412835Angle · crackedBS 280 WEB ANGLE CRACKED AT LBL 26. REMOVED CRACKED ANGLE IAW SRM 51-42-06-001-001-A01. INSTALLED SERVICEABLE ANGLE IAW SRM 51-42-06-001-001-A01 AND DWG CC670-34010.Apr 20, 2015 · N751EV · Cndair CL6002C10SDR ASOA2015051412834Angle · crackedBS 280 WEB ANGLE CRACKED AT RBL 26. R & R ANGLE IAW SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01.Apr 20, 2015 · N751EV · Cndair CL6002C10SDR SWIA201541156Bulkhead · unknownACCOMPLISHED REO TO RT SIDE BS 559, PRESSURE BULKHEAD, ACCOMPLISHED REO TO THE RT SIDE BS 559, PRESSURE BULKHEAD. COMPLIED WITH ST 51-900-1003, ATTACHED BTAC FROM M-210B FOR WORK PERFORMED.Apr 20, 2015 · N929EV · Cndair CL6002B19SDR SWIA201541155Bulkhead · unknownACCOMPLISH REO TO LT SIDE FS 559 PRESSURE BULKHEAD, ACCOMPLISHED REO TO LT SIDE BS 559, PRESSURE BULKHEAD. COMPLIED WITH ST 51-900-1003, ATTACHED BTAC M-210B FOR WORK PERFORMED.Apr 20, 2015 · N929EV · Cndair CL6002B19SDR ASOA2015051312816Bulkhead Web · corrodedBS 280, BULKHEAD WEB LT SIDE CORRODED. COMPLIED WITH EC/TC REO 670-53-11-594 AND GREO 670-53-11-594, REV DATED 04/27/2011. Apr 19, 2015 · N751EV · Cndair CL6002C10SDR ASOA2015051312815Bulkhead Web · corrodedF/S 280 BULKHEAD WEB RT SIDE CORRODED. COMPLIED WITH EC/TC REO 670-53-11-594 01 AND GREO 670-53-11-594, REV DATED 04/27/2011.Apr 19, 2015 · N751EV · Cndair CL6002C10SDR DALA2016112309147Doubler · corrodedCORROSION ON DOUBLER BS 1338 BETWEEN LONGERONS 28L - 28R AT AFT PRESSURE BULKHEAD AREA. THE DOUBLER WAS REPLACED IAW SRM 51-10-4 , 51- 30-2 , 51-30-5 , 51-10-3 PARAGRAPH 14 AND 21.Apr 16, 2015 · N967DL · Doug MD88SDR FDEA201504161244Doubler · damagedAPU FWD BULKHEAD RT SIDE HAS A DAMAGED AND GOUGED PREVIOUS REPAIR. REMOVED DAMAGE DOUBLER IAW SRM 51-40-02, FABRICATED NEW DOUBLER IAW SRM 53-80-08-2R, INSTALLED NEW DOUBLER AFT APU FWD BULKHEAD RH SIDE IAW SRM 51-40-02 AND 53-80-08-2R.Apr 16, 2015 · N938FD · Boeing 75723ASDR SWAA2015052640043Support · crackedBULKHEAD SUPPORT CRACKED AT BS 727+3, RBL 3. R & R SUPPORT IAW SRM.Apr 15, 2015 · N7819A · Boeing 7377Q8SDR SIMA20150415009Firewall · crackedAPU FIREWALL HAS TWO EACH CRACKS AT THE P274 MAIN ELECTRICAL CONNECTOR, INBD LOWER SCREW ATTACHMENT POINT. CRACKS ARE APPROX 3/8 INCH LONG EACH. REPAIRED AREA IAW SRM CH 53-32-13.Apr 15, 2015 · N605KS · Emb EMB145LRSDR SWAA2015042438953Bulkhead · crackedLEFT BULKHEAD CHORD CRACKED AT BS 540, STRINGER 22L, SECOND FASTENER DOWN ON AFT SIDE. REPAIRED CHORD IAW EA.Apr 15, 2015 · N436WN · Boeing 7377H4SDR ASAA2015041511372Bulkhead · crackedCRACK IN THE VAPOR BARRIER RT W/W FWD BULKHEAD, METAL AREA BEHIND "B" RES. ACFT GROUNDED. CUT OUT DAMAGE, FABRICATED AND INSTALLED CAT "B" REPAIR IAW SRM 57-10-10-2R-3, REPAIR 3, DET 2. INSPECTION THRESHOLD IS 56,000 FLIGHT CYCLES AFTER REPAIR INSTALLED. RApr 15, 2015 · N568AS · Boeing 737890SDR AALA201505269002Pressure Panel · cracked3S CHECK, PRESS PLATE FASTENER HOLE CRACKED IN THE FWD CARGO COMPARTMENT DECK MEMBRANE AT FRAME 36 LT & STRINGER 33 LT. REPAIRED IAW EA 250509.Apr 14, 2015 · N647AW · Airbus A320232SDR AALA201505269001Pressure Panel · cracked3S CHECK, PRESS PLATE FASTENER HOLE CRACKED IN THE FWD CARGO COMPARTMENT DECK MEMBRANE AT FRAME 36, STRINGER 33 RT. REPAIRED IAW EA 250509.Apr 14, 2015 · N647AW · Airbus A320232SDR AALA201505219006Pressure Panel · cracked3S CHECK CRACKED PRESS PLATE IN THE MAIN GEAR WW FWD OF FRAME 43 & -Y1650. REPLACED PRESS PLATE IAW SRM 51-42-11 & 51-72-11.Apr 14, 2015 · N647AW · Airbus A320232SDR AALA201505219005Pressure Panel · cracked3S CHECK CRACKED PRESS PLATE IN MAIN GEAR WW FWD OF FRAME 43 & +Y1650. REPLACED PRESS PLATE IN MAIN GEAR WW IAW SRM 51-42-11 & 51-72-11.Apr 14, 2015 · N647AW · Airbus A320232SDR ASOA2015050812782Bulkhead Web · corrodedRIGHT 280 WEB CORRODED. COMPLIED WITH ECTC REO 670-53-11-59401 AND GREO 670-53-11-594, REV--.Apr 14, 2015 · N176PQ · Cndair CL6002D24SDR ASOA2015050812781Bulkhead Web · corrodedLEFT 280 WEB CORRODED. COMPLIED WITH ECTC REO 670-53-11-59401 AND GREO 670-53-11-594, REV-- .Apr 14, 2015 · N176PQ · Cndair CL6002D24SDR SWAA2015042738959Bulkhead · crackedLEFT MAIN WW BULKHEAD WEB CRACKED AT BS 663, LBL 44. R & R WEB IAW SRM.Apr 14, 2015 · N214WN · Boeing 7377H4SDR WVER2015042693403Bulkhead Web · corrodedFOUND THE LT LOWER FS 280 WEB TO HAVE MINOR CORROSION.Apr 13, 2015 · N934FJ · Cndair CL6002D24SDR V0XD20150406092Bulkhead · corrodedLEFT FS 280.00 BULKHEAD WEB CORRODED. REMOVED LT FS 280.00 BULKHEAD WEB, FABRICATED & INSTALLED NEW FS 280.00 BULKHEAD WEB IAW 670-53-11-594 DATED 27 APRIL 2011.Apr 11, 2015 · N642CA · Cndair CL6002C10SDR SWIA201541122Bulkhead Web · crackedCRACK NOTED BS 621 BULKHEAD WEB, FWD FACE, BENEATH LWR LINER SUPPORT ASSY AT LBL18 APPROXIMATE WL75. CUTOUT CRACK AND INSTALLED DOUBLER/REPAIR AT FS 621 BULKHEAD WEB AT LBL 18, WL 75 REF, FINAL, REO. ALL STEPS COMPLIED WITH, LEAK CHECK GOOD.Apr 9, 2015 · N593ML · Cndair CL6002B19SDR SWAA2015041738633Pressure Panel · crackedMAIN WW VERTICAL PRESS WEB CRACKED AT BS 663, BETWEEN RBL 32 - 3. REPAIRED WEB IAW SRM.Apr 9, 2015 · N729SW · Boeing 7377H4SDR Y2PA2015041600020Doubler · crackedDURING C CHECK, DISCOVERED AFT PRESS BULKHEAD UPPER DOOR JAMB DOUBLER CRACKED. REPAIRED AFT PRESS BULKHEAD UPPER DOOR JAMB DOUBLER IAW SB 53-166 PAGE 30 PARAGRAPH 11 & DWG J060110. R & R LT DOOR JAMB CHANNEL IAW SB 53-166 PAGE 30 PARAGRAPH 11 & DWG J060110 FApr 9, 2015 · N196US · Doug DC915FSDR Y2PA2015041600019Pressure Deck · corrodedDURING C CHECK, DISCOVERED LT WW UPPER PRESS DECK FLOOR OTBD CORNER AFT SUPPORT & FRAME STATION 618 HAS SIGNS OF HEAVY EXFOLIATION. REPAIRED LT WHEEL UPPER PRESS DECK FLOOR AT FRAME 618 BY INSTALLING A NEW DOUBLER & FASTENERS IAW SRM 53-30-00.Apr 9, 2015 · N196US · Doug DC915FSDR Y2PA2015041600015Support Channel · crackedDURING C CHECK, DISCOVERED AFT PRESS BULKHEAD PAX ENTRY DOOR BOTTOM SUPPORT BEAM CRACKED. INSTALLED AFT BULKHEAD PAX ENTRY DOOR LOWER SUPPORT CHANNEL IAW SRM REFERENCES 51-20-0 PAGE 8-11 PARAGRAPH 5-8 SRM 51-30-7 PAGE 7, 12 - 14 PARAGRAPH 6 & 8 & SRM 51-30-5 Apr 9, 2015 · N196US · Doug DC915FSDR SWIA201541010Bulkhead · crackedFWD PRESSURE BULKHEAD CRACKED WHERE PARKING BRAKE CABLE PASSES THROUGH. THIS HAS BEEN DETERMINED TO BE A MAJOR REPAIR. A5 INSP, INSTALLED DOUBLER ON FWD PRESSURE BULKHEAD WHERE PARKING BRAKE CABLE PASSES THROUGH FS 202.75, BL 23.71 IAW REO.Apr 8, 2015 · N699BR · Cndair CL6002B19SDR SIMA20150407007Firewall · crackedAPU FIREWALL CRACKED ON THE AFT RT SIDE. COMPLETED REPAIR OF APU FIREWALL IAW ETN-EM-53-244 & EO-EM-53AD-1883.Apr 7, 2015 · N607AE · Emb EMB145LRSDR SWAA2015041038340Bulkhead · crackedLEFT WW FWD BULKHEAD VERTICAL PRESS WEB CRACKED AT BS 663.75, LBL 33.83. REPAIRED WEB IAW EA.Apr 7, 2015 · N220WN · Boeing 7377H4SDR AALA201504089007Flange · brokenFUEL CONFIG LIGHT ON FINAL, CTR TANK SHOWED 1.2, THEN DOWN TO .06 , THEN ON GATE READING 0.8. UPON INSPECTION FOUND CRACKED BULKHEAD PLUMBING FLANGE ON RT WING CTR TANK WALL. R & R BULKHEAD PLUMBING FLANGE IAW AMM 20-11-00, 28-22-07 & 28-11-00. ACCOMPLISHEDApr 7, 2015 · N902AW · Boeing 7572S7SDR DALA2015040902715Frame · crackedCRACKED FORMER ON AFT PRESSURE BULKHEAD FS Y=1338 PROJECTION LONGERON 7R. FORMER WAS REPLACED IAW SRM 51-30-1, 51-30-2 AND 51-30-5. LP 1896855.Apr 6, 2015 · N967DL · Doug MD88SDR ASAA2015040411576Frame · crackedRIGHT LOWER BULKHEAD CHORD AT STA 540 HAS 1 EA FASTENER HOLE CRACK, BS 540-BS 540, STR 22R-STR 23R. ACFT GROUNDED. REPAIRED IAW EA 900-57EA-14971 AND REO-G18873, REV A.Apr 4, 2015 · N323AS · Boeing 737990SDR DALA2015040602609Bulkhead · crackedCRACKED BULKHEAD BS 1437 AND 10 HRS POSITION. BULKHEAD WAS REPAIRED IAW ERA 519146-14MA, REV A.Apr 4, 2015 · N967DL · Doug MD88SDR SWAA2015042438923Pressure Panel · crackedVERTICAL PRESS WEB CRACKED AT BS 663, BETWEEN LBL 24.92 - 31.83. REPAIRED WEB IAW FAS EA.Mar 31, 2015 · N727SW · Boeing 7377H4SDR SWAA2015040938295Doubler · crackedMAIN WW VERTICAL PRESS WEB DOUBLER CRACKED AT BS 663, BETWEEN LBL 34 - 41. REPAIRED DOUBLER IAW SRM.Mar 31, 2015 · N406WN · Boeing 7377H4SDR K11A2015033025001Pressure Deck · corrodedLEFT WHEEL WELL PRESSURE DECK CORROSION AT STA 930.Mar 30, 2015 · N725CK · Boeing 727224SDR ASOA2015042712658Bulkhead Web · crackedFOUND REAR PRESSURE BULKHEAD WEB THAT SURROUNDS THE LINTEL ATTACHMENT FITTING HAS INDICATION NOTED APPROX .500 IN LENGTH 90 PERCENT FSH FAILED NDT INSPECTION. COMPLIED WITH EC/TC REO:601R-53-61-1230 AND GREO:601R-53-61-1230, REV F, DATED 10/31/2011 AS WRITTENMar 28, 2015 · N922EV · Cndair CL6002B19SDR ASOA2015042712657Bulkhead Web · crackedFS 280 WEB IS CRACKED OTBD OF RBL 9 IN RADIUS OF LOWER FLANGE. C/W ECTC REO 601R-53-11-171 AND MET ALL THE REQUIREMENTS OF REO 601R-53-11-171.Mar 28, 2015 · N922EV · Cndair CL6002B19SDR USAA2015040100010Angle · corrodedC1 CHECK, CORROSION ON FWD CARGO COMPARTMENT AFT BULKHEAD LOWER ANGLE AT BS 845 BETWEEN LBL 19 & RBL 19. REPLACED ANGLE IAW SRM 51-40-02.Mar 28, 2015 · N937UW · Boeing 7572B7SDR ASOA2015042412646Isolator · crackedFS 621 BULKHEAD, PANEL MOUNT ISOLATORS, 4, ARE CRACKED AT: LBL 27 BOTTOM, RBL 27 BOTTOM AND RBL 43 1ST AND 3RD FROM BOTTOM. IN ADDITION FOUND 6 MORE ISOLATORS CRACKED. R & R 10 ISOLATORS IAW SRM 51-42-10.Mar 27, 2015 · N922EV · Cndair CL6002B19SDR SWIA201541001Bulkhead · crackedBS 202 BULKHEAD AT PARKING BRAKE CABLE PASS THRU CRACKED. REPAIRED FWD PRESSURE BULKHEAD IAW REO.Mar 27, 2015 · N953SW · Cndair CL6002B19SDR SIMA20150325012Firewall · crackedAPU FIRE WALL CRACKED BY RT LOWER MOUNT. REPAIRED CRACK IN APU FIREWALL BY RT LOWER MOUNT IAW SRM 53-32-13 & ETN-EM-53-244.Mar 25, 2015 · N676AE · Emb EMB145LRSDR SWAA2015040638160Pressure Panel · crackedLEFT WW VERTICAL PRESS WEB LOWER CHORD CRACKED AT BS 663, LBL 34. REPAIRED CHORD IAW EA.Mar 25, 2015 · N208WN · Boeing 7377H4SDR SWAA2015040638140Bulkhead · crackedLEFT WW FWD BULKHEAD OTBD OF PACK EXHAUST CRACKED. REPAIRED BULKHEAD IAW EA.Mar 25, 2015 · N208WN · Boeing 7377H4SDR SWAA2015051839778Bulkhead · crackedAFT PRESS BULKHEAD WEB CRACKED AT BS 1016, STRINGER 23L. REPAIRED WEB IAW EA.Mar 24, 2015 · N356SW · Boeing 7373H4SDR ASOA2015033012497Bulkhead Web · crackedWHILE PERFORMING EC/TC AWL 53-61-153-02, ECI OF THE AFT PRESSURE BULKHEAD, FOUND CRACK INDICATION ON THE BULKHEAD WEB AT LBL 36.20 AT ZEE MEMBER HEEL LINE ADJACENT TO THE FASTENERS ON THE OTBD SIDE. THIS INDICATION EXCEEDS LIMITATIONS IAW NDTM PART 6, 53-61-1Mar 24, 2015 · N857AS · Cndair CL6002B19SDR ASOA2015033012496Bulkhead Web · crackedWHILE PERFORMING EC/TC AWL 53-61-153-02, ECI OF THE AFT PRESSURE BULKHEAD, FOUND 3 SEPARATE LOCATIONS ON THE BULKHEAD WEB WITH CRACK INDICATIONS AT LBL 18.00 AT ZEE MEMBER HEEL LINE ADJACENT TO THE FASTENERS ON THE OTBD SIDE. THESE INDICATIONS EXCEED LIMITATIMar 24, 2015 · N857AS · Cndair CL6002B19SDR SIMA20150323010Firewall · crackedAPU FIREWALL HAS ABOUT A 1" CRACK AT THE LOWER RIVET ON RT STIFFENER. APU FIREWALL HAS ABOUT 3/4" CRACK AT THE LOWER RIVET ON THE LT STIFFENER. REPLACED APU FIREWALL IAW EO-EM-53AD-1883 PART D.Mar 23, 2015 · N610AE · Emb EMB145LR
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