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 ASOA2015022712303Bulkhead Web · corrodedLT 280 WEB CORRODED FOUND AFTER REMOVAL OF BEAM. COMPLIED WITH ECTC REO 670-53-11-594 AND GREO 670-53-11-594, REV.SDR ASAA2015020910676Bulkhead · crackedPOSSIBLE CRACK, WITH SIGNS OF SMOKING, IN RT WHEEL WELL UPPER RT CORNER APPROXIMATELY THREE INCHES FROM CEILING PANEL ON FWD BULKHEAD MIG 2C, 301725 INITIATED. ACFT GROUNDED. RESOLVED ON W/O: 288879 TC: N/R-00004, REPAIRED 2.25" CRACK IN RT MLG WHEEL WELL ATSDR ASOA2015021312223Isolator · brokenAFT PRESSURE BULKHEAD ISOLATOR ABOVE WL 73.50 ON RBL 9.50 IS BROKEN. REMOVED DEFECTIVE ISOLATOR AND INSTALLED NEW ISOLATOR IAW SRM 51-42-13. REPAIR CLASSIFIED AS MINOR IAW GMM 5-3.SDR ASOA2015021312222Isolator · brokenAFT PRESSURE BULKHEAD ISOLATOR ABOVE WL 73.50 ON LBL 9.50 IS BROKEN. REMOVED DEFECTIVE ISOLATOR AND INSTALLED NEW ISOLATOR IAW SRM 51-42-13. REPAIR CLASSIFIED AS MINOR IAW GMM 5-3.SDR REXA2015021300111Bulkhead · damagedFS 621 BULKHEAD HAS EIGHT SCREW MARKS 13 INCHES ABOVE THE FLOOR BETWEEN LBL 36 & RBL 36 WITH MAX DEPTH OF 0.006 INCHES. REPAIRED IAW REO 601R-53-61-2155.SDR REXA2015021300110Bulkhead · chafedFS 621 BULKHEAD FWD FACE CHAFED 3 INCHES ABOVE RBL 31, REMOVED 0.004 INCHES MATERIAL. REPAIRED IAW REO 601R-53-61-2155.SDR SWAA2015021236557Pressure Deck · crackedCENTER WING SECTION REAR SPAR VERTICAL PRESS DECK UPPER WEB CRACKED AT BS 663.75, LBL 35.00. REPAIRED WEB IAW EA.SDR WVER2015020800004Bulkhead Web · corrodedBS 280 LT LOWER BULKHEAD WEB IS CORRODED.SDR SWAA2015032037656Bulkhead · crackedBULKHEAD WEB CRACKED AT BS 227.8, RBL 14.5. REPAIRED WEB IAW EO & EA.SDR SWAA2015031637472Bulkhead · crackedBULKHEAD WEB CRACKED AT BS 227.8, LBL 14.5. REPAIRED WEB IAW EO & EA.SDR DALA2015020701172Bulkhead · crackedCRACK ABOUT 1 INCH, OCCURED AT AFT INNER SURFACE 8 O'CLOCK LT SIDE BULKHEAD. INNER CHORD CRACKED AREA AT 8 O'CLOCK LT SIDE BULKHEAD 2598 CUT AND REMOVED, REPAIR PARTS INSTALLED IAW SRM.SDR SWAA2015031737516Pressure Panel · crackedCENTER WING REAR SPAR VAPOR WEB CRACKED AT BS 663, LBL 31. REPAIRED WEB IAW SRM.SDR ASAA2015020610769Stiffener · corrodedAFTER REMOVAL OF THE BS 1088, BULKHEAD APU AIR INLET RT STIFFENER FOUND CORRECT ON BULKHEAD WEB. ACFT GROUNDED. BLENDED STA 1088 BULKHEAD AT RBL 22, OUT OF LIMITS, REPAIRED AREA IAW EA 400, 53EA 14565, SRM 53-80-08-2R 8, REPAIR 8, 53 8008 1A 1, W 1.00, O .032SDR J72A2015F00030Bulkhead · corrodedDURING "D" CHECK, VISUAL INSPECTION ON THE LOWER AFT FUSELAGE JOINT TO TAIL CONE AREA REVEALED CORROSION ON AFT FUSELAGE CANTED BULKHEAD AND LOWER SKIN AREA.SDR SWAA2015031737520Pressure Panel · crackedCENTER WING REAR SPAR VAPOR WEB CRACKED AT BS 663, BETWEEN LBL 40 TO LBL 45. REPAIRED WEB IAW SRM.SDR SWAA2015031737519Pressure Panel · crackedCENTER WING REAR SPAR VAPOR WEB CRACKED AT BS 663, BETWEEN LBL 30 TO LBL 40. REPAIRED WEB IAW SRM.SDR SWAA2015031737518Pressure Panel · crackedLEFT CTR WING REAR SPAR VAPOR WEB OTBD CRACKED. INBD & BELOW HYDR MOD. REPAIR WEB IAW SRM.SDR SWAA2015031737517Pressure Panel · crackedRIGHT CTR WING REAR SPAR VAPOR WEB OTBD CRACKED, TBD OF B-YSTEM MAIN FILTER MODULE. / REPAIRED WEB IAW SRM.SDR ASAA2015020510758Bulkhead Web · corrodedAFTER REMOVAL OF THE BS 1088, BULKHEAD APU AIR INLET LT STIFFENER THE BULKHEAD WEB WAS FOUND CORRODED UNDER IT. ACFT GROUNDED. BLENDED STA 1088, BULKHEAD AT RBL 34, OUT OF LIMITS REPAIRED AREA IAW EA 400-53EA 14565, SRM 53-80-08-2R-8, REPAIR 8-53-80-08, 1A, SDR ASOA2015020912185Bulkhead · crackedDURING AN EDDY CURRENT INSPECTION OF THE AFT PRESSURE BULKHEAD, FOUND AT LBL 36.2 ABOVE AND OTBD OF THE LOWEST ISOLATOR JUST ABOVE WL 73.50 CRACKED. FOUND A CRACK AT LBL 27.50 JUST ABOVE THE CARGO DOOR TRACK ABOVE WL 121.93, FOUND IS OUT OF LIMITS.SDR ASOA2015020912183Bulkhead · crackedAFT PRESSURE BULKHEAD CRACK AT LBL 36.2 AND WL 73.5.SDR ASOA2015020912182Bulkhead · crackedAFT PRESURE BULKHEAD CRACKED, LBL 27.50 ABOVE AFT CARGO DOOR TRACK.SDR A6WA201542381Bulkhead · gougedRIGHT AFT 280 BULKHEAD SKIN & RIVETS GOUGED.SDR IPXA2015030286605Bulkhead · crackedINSPECTION TYPE:CD 507179: FUSELAGE BULKHEAD PRESSURE PAN REPAIR AT STA 395. REMOVED E AND E COOLING SUPPLY DUCT IAW 21-20-01. REMOVED P3I PANEL TO FOM IAW AMM 24-51-02-024-001. REMOVED 1 EA BRACKET TO FOM IAW SRM 51-40-02. REMOVED BULKHEAD PRESSURE PAN IASDR SWAA2015032337723Pressure Deck · crackedMAIN WW BEADED PRESS DECK CRACKED AT BS 665, RBL 39. REPAIRED DECK IAW ER & EA.SDR SWIA201540740Bulkhead · crackedFS 621, BULKHEAD HAS 2 CRACKS AT LINTEL FITTING. C-CHECK, RO 2/19/15, REPAIRED FS 621 BULKHEAD LINTEL FITTING REF REO. NO LEAKS NOTED, COMPLIED WITH ST.SDR SWIA201540738Bulkhead Web · crackedFS 621, BULKHEAD WEB AT LBL 27.50 HAS CRACK AT TOP OF CARGO DOOR TRACK. C-CHECK, RO 2/19/15. REPAIRED CRACK AT FS 621, BULKHEAD WEB AT LBL 27.50, AT TOP OF CARGO DOOR TRACK REF REO.SDR DALA2015020400885Stiffener · crackedCRACKED STIFFENER ON UPPER FWD PRESSURE DOME BETWEEN BS 1338 LONGERON 1. THE STIFFENER WAS REPLACED IAW SRM 51-30-2, 51-30-5, 51-10-4 AND 51-10-3 P.21 AND 14.SDR DALA2015020300843Panel · crackedCRACK ON BULKHEAD LINING PANEL, RT LOWER SECTION AT BS 2160.SDR DALA2015022201540Bulkhead Web · crackedTHE FS 1437 BULKHEAD WEB WAS SPLICED FROM L1R-L4R TO REMOVE A CRACK. CRACK ON FRAME WAS REPAIRED IAW ER/A 532506-14, REV ORIGINAL.SDR 9EKA02022015008Firewall · crackedON A SCHEDULED INSPECTION, NR 1 ENG TO MGB FIREWALL FEED THROUGH FOUND CRACKED.SDR V0XD20150202037Bulkhead · corrodedLEFT & RIGHT BULKHEAD WEBS AT FS 280 CORRODED. REPAIRED LT & RT BULKHEAD WEBS IAW REO 670-53-11-594 DATE 2011-04-27.SDR DALA2015020200815Tee Fitting · damagedTOOL DAMAGE ON TEE FITTING BS 1338 AFT PRESSURE BULKHEAD. . FABRICATE REPAIR, TREAT, PAINT, AND INSTALLED IAW SRM 51-30-5, 51-30-2, 51-30-1 AND 51-20-0 AND 53-05, FIG 37.SDR A6WA201542356Angle · crackedOBLIQUE ANGLE AT FS 621, BULKHEAD IS CRACKED AT STRINGER 14R.SDR SWIA201540720Bulkhead · scratchedTHERE HAVE BEEN PREVIOUS REPAIRS TO THE AFT BAGGAGE BAY BULKHEAD, BS 621, LBL 27.50. IT HAS BEEN SCRATCHED IN THE CENTER BY A SCREW. C-CHECK, RO 2/10/15, REMOVED DAMAGE AND INSTALLED A NEW FABRICATED DOUBLER TO THE AFT BAGGAGE BAY BULKHEAD, FS621, LBL 27.50 RSDR SWIA201540719Bulkhead · scratchedTHERE HAVE BEEN PREVIOUS REPAIRS TO THE AFT BAGGAGE BAY BULKHEAD, BS 621, LBL 18.00. IT HAS BEEN SCRATCHED IN THE CENTER BY A SCREW. C-CHECK, RO 2/10/15, REMOVED DAMAGED DOUBLER AND INSTALLED FABRICATED DOUBLER TO THE AFT BAGGAGE BAY BULKHEAD, FS621, LBL18.00SDR SWIA201540718Bulkhead · scratchedTHERE HAVE BEEN PREVIOUS REPAIRS TO THE AFT BAGGAGE BAY BULKHEAD, BS 621, RBL 18.00. IT HAS BEEN SCRATCHED IN THE CENTER BY A SCREW. C-CHECK, RO 2/10/15, REMOVED DAMAGED DOUBLER AND INSTALL FABRICATED DOUBLER TO THE AFT BAGGAGE BAY BULKHEAD, FSD 621,
RBL18SDR SWIA201540716Bulkhead · scratchedTHERE HAVE BEEN PREVIOUS REPAIRS TO THE AFT CARGO BAY BULKHEAD, BS 621, RBL 27.50. IT HAS BEEN SCRATCHED IN THE CENTER BY A SCREW. C-CHECK, RO 2/10/15, REMOVED DAMAGED DOUBLER AND INSTALLED NEW FABRICATED DOUBLER TO THE AFT BAGGAGE BAY BULKHEAD FS621, RBL27.SDR SWAA2015021036515Pressure Panel · crackedLEFT MLG WW VERTICAL PRESS WEB CRACKED AT LBL 42. REPAIRED WEB IAW SRM.SDR CALA2015020200076Bulkhead · crackedLEFT WW VERTICAL PRESS DECK CRACKED STATION 663 BETWEEN LBL 31.83 & LBL 40.00, WL200.6 - 192.0. INSTALLED REPAIR DOUBLER IAW SRM 57-10-10 REPAIR 3, ALTERNATIVE E 2. SEE LOG 9718823 FOR INCORPORATED REPAIR & DIP CONTROL 32110.SDR CALA2015020200075Bulkhead · crackedLEFT WW VERTICAL PRESS DECK CRACKED STATION 663, BETWEEN LBL 40 & 45.64, WL 200.6 & 192.0. INSTALLED REPAIR DOUBLER IAW SRM 57-10-10 REPAIR 3 ALTERNATIVE 2. INSPECTION THRESHOLD OF 56K FLIGHT CYCLES AFTER REPAIR INSTALLATION & 36K FLIGHT CYCLES INTERVAL IAW SDR CALA2015020200074Bulkhead · crackedRIGHT WW VERTICAL PRESS DECK CRACKED STATION 663, BETWEEN RBL 40.00 - RBL 45.60, WL200.6 TO 192.0. INSTALLED REPAIR DOUBLER IAW SRM 57-10-10 REPAIR 3, ALTERNATIVE 2. INSPECTION THRESHOLD OF 56K FLIGHT CYCLES AFTER REPAIR INSTALLATION & 36K FLIGHT CYCLES INTESDR CALA2015020293057Bulkhead · crackedBS2598 BULKHEAD RT INNER CHORD CRACK. REMOVED DAMAGE. FABRICATED AND INSTALLED REPAIR PARTS IAW ECRA 5310-06385.SDR CA150205010Bulkhead · deformed(CAN) EVIDENCE OF A HARD LANDING DISCOVERED IN INSPECTION PROCESS. MINOR DEFORMATION OF THE BULKHEAD AND A MINOR WRINKLE IN THE EXTERNAL SKIN WAS EVIDENT. STRUCTURAL REPAIR WAS MADE AND THE AIRCRAFT RELEASED AS REQUIRED.SDR SWIA201540717Bulkhead · scratchedTHERE HAVE BEEN PREVIOUS REPAIRS TO THE AFT BAGGAGE BAY BULKHEAD, BS 621, RBL 36.20. IT HAS BEEN SCRATCHED IN THE CENTER BY A SCREW. C-CHECK, RO 2/10/15, REMOVED DAMAGED DOUBLER AND INSTALLED FABRICATED DOUBLER TO THE AFT BAGGAGE BAY BULKHEAD, FS621, RBL36.2SDR SWIA201540714Bulkhead · crackedCRACK NOTED ON AFT PRESSURE BULKHEAD, FWD FACE, BENEATH LINER SUPPORT ASSY LOCATED ON RBL 9 APPROXIMATELY WL80 NEAR FLOOR LEVEL. C-CHECK, RO 2/10/15, REMOVED DAMAGED PORTION AND INSTALLED FABRICATED REPAIR PARTS ON AFT PRESSURE BULKHEAD, FWD FACE, BENEATH LINSDR ASOA2015020912187Bulkhead Web · crackedFOUND THE BS 559 BULKHEAD WEB HAS CRACK INDICATION NOTED OTBD OF RBL 9.0 APPROXIMATLEY FOUR INCHES IN LENGTH. REPAIRED IAW REO 601R-53-41-260 AND REO 601R-53-41-260, REV E.SDR SIMA20150128013Firewall · crackedAPU FIRE WALL IS CRACKED AT THE LOWER LT MOUNT AREA, THE UPPER LT MOUNT & THE LOWER RT MOUNT AREA. 3 CRACKS TOTAL APPROX 4.5 INCHES IN LENGTH. COMPLIED WITH PART B & C OF EO EM-53AD--1883 R4.SDR SWAA2015021136522Pressure Deck · crackedMAIN WW PRESS DECK CRACKED BETWEEN BS 664 TO 675, LBL 34.50. REPAIRED DECK IAW SRM.SDR ASOA2015020212137Bulkhead · crackedAFT PRESSURE BULKHEAD CRACKED ALONG RBL 27.50 BETWEEN SECOND AND THIRD STAND OFF, FROM FLOOR WL 73.50.
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