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 DL73K001222Bulkhead · crackedA TYPICAL CRACK WAS FOUND IN THE FS 178 BULKHEAD WEB AT WL 233.5, RBL 7 DURING INSPECTIONS MANDATED PER AD 2000-05-29. THE CRACK WAS REPAIRED PER B737-200 SRM 53-10-11, FIG. 1 AND DOCUMENTED PER ER/A 377622-14AD.SDR LR7A00117Bulkhead · crackedDURING SCHEDULED A-CHECK PER JOB CARD HA1200, FOUND LEFT FS 990 BULKHEAD T FITTING AND WEB CRACKED, LBL 62. REPLACED WEB AND FITTING PER SRM SMP 583-53-50 D & C2.SDR 2000UALA00756Bulkhead · crackedCRACK FOUND ON THE BODY STATION 178 BULKHEAD WEB. SUPPLEMENTAL DATA UPDATE CRACKS REPAIRED PER BOEING SRM 53-10-08.SDR SWAA001146Bulkhead · crackedDURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD CRACKED IN 4 PLACES, LBL 6 TO RBL 6. REPAIRED BULKHEAD PER SRM.SDR RRXA002750Bulkhead · damagedDURING A MAINTENANCE VISIT FOUND NUMEROUS PATCHES TO THE FWD LWR CARGO COMPT MID BULKHEAD, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW EO NR 00-107 WITH APPROVED 8110-3 DATEDSDR CA000719020Bulkhead · cracked(CAN) WHILE PERFORMING UNSCHEDULED MAINTENANCE, A BULGE WAS OBSERVED ON FUSELAGE SKIN AROUND THE FORWARD WING SPAR PICKUP FITTING. FURTHER INSPECTION REVEALED BOTH LT AND RT FROST SPAR ATTACHMENT BULKHEADS P/NS 41658-0 AND -1 WERE CRACKED AND ALSO LT AND LT FSDR SWAA001138Bulkhead · crackedDURING SCHEDULED D CHECK, FOUND BS 178 BULKHEAD CRACKED AT LBL 17.5. REPAIRED BULKHEAD PER SRM.SDR SWAA001136Bulkhead · crackedDURING SCHEDULED SERVICE CHECK, FOUND BS 178 BULKHEAD AND CHORD CRACKED AT LBL 5. REPAIRED BULKHEAD AND CHORD PER SRM.SDR RRXA002738Pressure Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE CENTER WING AFT LT TOP PANEL AT STA 848.00 AND LBL 60 TO 58 INCHES, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAISDR 20000619SH013Bulkhead · crackedDURING C-CHECK, FOUND CRACK IN DOUBLER ON THE AFT PRESSURE BULKHEAD BS 996. CAUSE UNKNOWN. (X)SDR DL72E001189Bulkhead · puncturedTHE FS 178 BULKHEAD WEB WAS PUNCTURED DUE TO GROUND CONTACT WITH THE WING-TIP OF ANOTHER AIRCRAFT. THE WEB DAMAGED WAS CLEANED UP WITH A 13 X 9 CUTOUT. THE CUTOUT WAS REPAIRED WITH AN ALUMINUM DOUBLER INSTALLED PER ER/A 377552-14, REV A.SDR DLM90001163Bulkhead · crackedTHE FS 1520 CANTED BULKHEAD WEB WAS FOUND WITH A 4.5 INCH CRACK ALONG THE WEB SPLICE JOGGLE LINE AT STRINGER 8L. THE WEB WAS CUT TO REMOVE THE DAMAGED SECTION. A NEW SECTION OF WEB WAS SPLICED IN WITH AN ALUMINUM DOUBLER AND TRIPLER PER ER/A 377529-14, REVSDR USAA000849Pressure Panel · crackedCLT - FOUND SKIN CRACKED .5 INCH, W/W STATION 664, LBL 31 PRESSURE DECK SKIN. REPAIRED PER TR 53-60-04 FIG 1. (M)SDR 20000626SH020Bulkhead · crackedINSTALLED KIT, PN 55-4030-5S, SI 0090 REV II. INSPECTED FOR POSSIBLE CRACKS. FOUND CRACKS ON BOTH LT AND RT SIDES OF BULKHEAD. CRACK .75 INCH LT SIDE. CRACK .3750 INCH RT SIDE, SAME LOCATION. (X)SDR UPS00232917Bulkhead · corrodedINSPECTION TYPE:C, WHILE WORKING CUSTOMER NR 134500 FUSELAGE 88 DISCOVERED MAIN WHEEL WELL RT FWD BULKHEAD CORRODED BS 870 RBL 45 - 54. REMOVED CORROSION 5.5 X 8 AREA RBL 45 TO 54 PER SRM 51-10-6. FABRICATED FILLER AND REPAIR PLATE AND SHIMS AND INSTALLED ALSDR ASAA0080372Bulkhead · corrodedPHX: DURING 15K CHECK CORROSION WAS FOUND ON DOUBLER AND TIE STRAP ON LOWER FORWARD FACE OF AFT PRESSURE BULKHEAD, FS 1338, LBL 3 TO RBL 3.REMOVED DAMAGED MATERIAL AND INSTALLED NEW DOUBLER AND STRAP IAW DC9 SRM 53-14-03.SDR UPS00233141Bulkhead · crackedINSPECTION TYPE:C+SI SUSPECT CRACK ON BS 178 BULKHEAD LT STR 17L. HFEC INSPECTION CARRIED OUT IAW B727-NDT MANUAL, PT6,51-00-00,FIG4. CRACK CONFIRMED ON BS 178 BULKHEAD LT ANGLE, AT STR 17L. CRACK CUT OUT IAW SRM 51-40-3 FIG1 .HFEC INSP C/O IAW B727 SDR USAA000815Bulkhead · crackedCLT - FOUND TWO CRACKS IN BULKHEAD .25 INCH AND .75 INCH, WL 201, LBL 5. FABRICATED AND INSTALLED REPAIR PART PER TR 53-10-08 FIG 209. (M)SDR DL72W001154Bulkhead · crackedA 1 INCH CRACK FOUND ON THE WEB OF THE STA 178 BULKHEAD AT RBL 3 AND WL 197. DAMAGE FOUND ADJACENT TO EXISTING REPAIR. EXISTING REPAIR REMOVED AND NEW REPAIR INSTALLED FOR CUTOUT MEASURING 7.5 UP/DWN BY 12.5 IB/OB. ER/A 334537-14 REV A.SDR 20001103SH002Fitting · corrodedLEFT WING - BODY BULKHEAD FITTING STA 870 WITH PITTING CORROSION AT AFT FACE SURFACE AND INSIDE OF BORE. (X)SDR GAIA00560Bulkhead · crackedDURING HEAVY C-CHECK AT TIMCO/OSC, FOUND CRACK ON BULKHEAD WEB AT RBL 8 WL 177. REPAIRED WEB IAW S/B 727-53-0175 R3. THIS AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR GAIA00351Pressure Panel · crackedDURING HEAVY C-CHECK AT TIMCO/OSC, FOUND CRACK ON LEFT SIDE OF NOSE WHEEL WELL SIDE WALL STATION 268. REPAIRED SIDE WALL IAW SB 727-53-0065. THIS AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR GAIA00356Bulkhead · chafedDURING HEAVY C-CHECK AT TIMCO/OSC, FOUND BS 1183 BULKHEAD AFT SIDE HAS CHAFFED AREA WL 188 RBL 12. REPAIRED BULKHEAD IAW SB 727-53-0175 R3. THIS AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR UPS00832963Bulkhead · crackedINSPECTION TYPE:C2, AFT PRESSURE BULKHEAD LT SIDE CRACKED LBL 32 APPROX L11L. REPAIRED AREA IAW DAC DWG SR08530007. ALODINED AND PRIMED IAW DC8 SRM 51-1-8.SDR QXEA0001705Bulkhead · corrodedPDX- CORROSION ON AND AROUND RIVETS ON REAR PRESSURE BULKHEAD AT BL 1050R TO BL 425R AT BEAM XII. REPAIRED IAW HORIZON AIR EA 4-53-1210, FOKKER SRM 51-10-4, AND SRM 53-01-01, PAGE 6B.SDR QXEA0001702Bulkhead · corrodedPDX- CORROSION ON AND AROUND RIVETS ON REAR PRESSURE BULKHEAD BETWEEN BL 425R TO BL 425L AT BEAM IX. REPAIRED IAW FOKKER SRM 51-31-01 AND HORIZON AIR EA 4-53-1208.SDR QXEA0001701Bulkhead · corrodedPDX- CORROSION ON AND AROUND RIVETS ON REAR PRESS BULKHEAD BETWEEN BL 425R TO BL 425L AT BEAM VIII. REPAIRED IAW FOKKER SRM 51-31-01 AND HORIZON AIR EA 4-53-1208.SDR QXEA0001700Bulkhead · corrodedPDX- CORROSION ON AND AROUND RIVETS ON REAR PRESSURE BULKHEAD BETWEEN BL 425R TO BL 425L AT BEAM VII. REPAIRED IAW FOKKER SRM 51-31-01 AND HORIZON AIR EA 4-53-1208.SDR QXEA0001699Bulkhead · corrodedPDX- CORROSION ON AND AROUND RIVETS ON REAR PRESSURE BULKHEAD BETWEEN BL 425R TO BL 425L AT BEAM VI. REPAIRED IAW FOKKER SRM 51-31-01 AND HORIZON AIR EA 4-53-1208.SDR QXEA0001493Bulkhead · corrodedPDX- CORROSION ON AND AROUND RIVETS ON REAR PRESSURE BULKHEAD BETWEEN BL425R TO BL425L AT BEAM V. REPAIRED IAW HORIZON AIR EA 4-53-1210 AND 51-10-04.SDR QXEA0001492Bulkhead · corrodedPDX- CORROSION ON AND AROUND RIVETS ON REAR PRESSURE BULKHEAD BETWEEN BL 425R TO BL 405L AT BEAM IV. REPAIRED IAW HORIZON AIR EA 4-53-1210, AND 51-10-04.SDR QXEA0001513Bulkhead · corrodedPDX- CORROSION ON REAR PRESSURE BULKHEAD AT BEAM VI BL1050R TO 425R. REPAIRED IAW HORIZON AIR EA 4-53-1208 AND FOKKER SRM 51-10-4.SDR QXEA0001670Pressure Panel · crackedPDX- CRACK AT NOSE LANDING GEAR BAY AT STATION 2475. REPAIRED IAW HORIZON AIR EA 4-53-1209, FOKKER SRM 53-02-18, PAGE 13, FIGURE 5, AND SRM 51-30-02.SDR SWAA001047Bulkhead · crackedDURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD CRACKED, LBL 5 AND RBL 5.7. REPAIRED BULKHEAD PER XEA''S X2-53-278, X2-53-279 AND SRM.SDR 2000UALA00729Bulkhead · crackedCRACK FOUND ON THE BODY STATION 178 BULKHEAD WEB. SUPPLEMENTAL DATA UPDATE CRACKS REPAIRED PER BOEING SRM 53-10-08.SDR DLL14001101Bulkhead · crackedTHE FS 1363 BULKHEAD WEB WAS FOUND WITH A .4 TYPICAL CRACK EMANATING FROM A FASTENER HOLE AT THE LBL 42.5 WEB JOINT AT WL 126. THE CRACKED AREA WAS TRIMMED OUT OF THE WEB AND REPAIRED WITH AN ALUMINUM DOUBLER PER L1011 SRM 53-11-00 FIG 851, LAC S/B 93-53-268SDR QXEA0001481Bulkhead · crackedPDX- FORWARD PRESSURE BULKHEAD CRACKED AT AFT SIDE ALONG BEAM VII BETWEEN CENTERLINE AND 6 LEFT OF CENTERLINE, JUST ABOVE LOWER RIVET ROW. REPAIRED IAW FOKKER SRM 53-02-18 FIGURE 14.SDR QXEA0001480Bulkhead · crackedPDX- FORWARD PRESSURE BULKHEAD CRACKED AT AFT SIDE ALONG BEAM VII, BETWEEN 7-14 OUTBOARD OF BL 325R, BETWEEN 2 HORIZONTAL RIVET ROWS. REPAIRED IAW FOKKER SRM 53-02-18 FIGURE 14 AND 51-31-01.SDR SWAA001023Pressure Panel · crackedDURING SCHEDULED 1/2D CHECK, FOUND PRESS WEB CRACKED, BS 663, RBL 39, AND BS 665, RBL 34. REPAIRED WEB PER TI-353-032.SDR USAA000842Bulkhead · crackedPIT - FOUND BULKHEAD WEB CRACKED 3 INCHES, STATION 965 BULKHEAD (LEFT) 8 INCHES FROM FLOOR. REPLACED SECTION OF WEB PER EA 55292. (M)SDR LR7A00134Bulkhead · crackedDURING SCHEDULED C2 INSPECTION, FOUND FS 93 BULKHEAD WEB CRACKED AT TWO LOCATIONS RBL 25. REPAIRED PER SRM SMP 583-51-140-12. NR 39361.SDR LR7A00133Frame · crackedDURING SCHEDULED C2 INSPECTION, FOUND FS 93 BULKHEAD LOWER FRAME CRACKED FROM RBL 20 LOWER FITTING ATTACH BOLT HOLE. REPAIRED PER LAC MEA 382-53-00-064. NR 39358.SDR QXEA0001766Bulkhead · corrodedPDX- CORROSION ON AND AROUND RIVETS ON REAR PRESSURE BULKHEAD BETWEEN BL 1050R TO BL 425R AT BEAM 5. REPAIRED IAW FOKKER SRM 51-31-01 AND SRM 51-10-04.SDR QXEA0001765Bulkhead · corrodedPDX- CORROSION ON AND AROUND RIVETS ON REAR PRESSURE BULKHEAD BETWEEN BL 1050L TO BL 425L AT BEAM 8. REPAIRED IAW FOKKER SRM 51-31-01 AND SRM 53-01-01, PARAGRAPH 4B AND SRM 53-02-04, FIGURE 7.SDR QXEA0001703Bulkhead · corrodedPDX- CORROSION ON AND AROUND RIVETS ON REAR PRESSURE BULKHEAD BETWEEN BL 1050R TO BL 425R AT BEAM X. REPAIRED IAW FOKKER SRM 51-31-01, SRM 51-10-4, AND SRM 53-01-01, PAGE 6.SDR SWAA001018Pressure Panel · crackedDURING SCHEDULED SERVICE CHECK, FOUND LT W/W PRESSURE WEB CRACKED, BS 663, LBL 33. REPAIRED WEB PER TI-353-046.SDR SWAA001025Pressure Panel · crackedDURING SCHEDULED SPECIAL VISIT, FOUND LT MLG W/W PRESS WEB CRACKED JUST O/B OF AILERON QUADRANT. REPAIRED WEB PER MM.SDR SWAA001005Bulkhead · crackedDURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD CRACKED, RBL 11-12, WL 207. REPAIRED BULKHEAD PER SRM.SDR COMA0060476Structure · damagedTHE INBOARD LEFT HAND AND RIGHT HAND VERTICAL POSTS ON THE PRESSURE BULKHEAD AT FS 409 AND 128 REQUIRES REMOVAL TO ALLOW FOR THE REMOVAL OF 2 RIVETS GOING THROUGH THE FUSELAGE. THE RIVETS REQUIRE REMOVAL TO ACCOMPLISH CANADAIR S/B 601R-53-050. PERFORMED A MASDR QXEA0001768Bulkhead · corrodedPDX- CORROSION ON AND AROUND RIVETS ON REAR PRESSURE BULKHEAD BETWEEN BL425R TO BL 425L AT BEAM 10. REPAIRED IAW FOKKER SRM 51-10-01, PAGE 9, PARAGRAPH 4B AND SRM 53-01-01, PAGE 6, PARAGRAPH 4 B2.
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