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 2000UALA00735Bulkhead · crackedCRACK FOUND ON THE BODY STATION 178 BULKHEAD WEB. SUPPLEMENTAL DATA UPDATE CRACKS REPAIRED PER BOEING SRM 53-10-08.SDR 2000UALA00733Bulkhead · crackedCRACK FOUND ON THE BODY STATION 178 BULKHEAD WEB. SUPPLEMENTAL DATA UPDATE CRACKS REPAIRED PER BOEING SRM 53-10-08.SDR AU000167Bulkhead · cracked(AUS) REAR PRESSURE BULKHEAD TOP WEB CRACKED IN SEVERAL PLACES.SDR AU000157Bulkhead · cracked(AUS) REAR PRESSURE BULKHEAD LOCATED AT BS 346.75 CRACKED IN TWO PLACES.SDR TWAA0003903Bulkhead · crackedDURING CHECK-C MAINT, FOUND CRACK AT TOP OF SUPPORT DOUBLER ON FWD FACE OF REAR BULKHEAD, STA 1338 BELOW LONGERON 1. REMOVED AND REPLACED EXISTING SUPPORT DOUBLER WITH NEW TWA PN 63-9879. PART SECURED TO BULKHEAD WITH MS20470AD-S RIVETS PER SRM 51-30-2, AND SDR 20000710SH011Bulkhead · misdrilledTHE VERTICAL PYLON FORWARD BULKHEAD AT STA 458 HAD DOUBLE DRILLED HOLES AT THE FASTENER AREA. THE BULKHEAD IS BETWEEN THE UPPER AND LOWER DECKS. THERE WAS A CRACK FOUND AT THE LEFT CORNER OF THE BULKHEAD WEB. (X)SDR WRLA20007Bulkhead · damagedON FEB 21, UPON ARRIVAL AT ATLANTA FOR A SCHEDULED MAINTENANCE CHECK (A-7) DAMAGE WAS DISCOVERED DURING AN INSPECTION OF THE LOWER FORWARD CARGO COMPARTMENT. THE DAMAGE WAS TO THE AFT BULKHEAD STANCHION AT STATION 1119, AND TO THE OTHER ATTACHMENTS OF THE COMSDR QXEA0000730Bulkhead · damagedPDX- FOUR SMALL SCUFFED AREAS ON FORWARD SIDE OF REAR PRESSURE BULKHEAD. REPAIRED IAW FOKKER SRM 51-10-04.SDR RRXA003793Frame · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO FRAME AT STA. 680 AND L31R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW E.O.#00-016 WITH APPROVED 811SDR 2000UALA00765Bulkhead · crackedCRACK FOUND ON THE BODY STATION 178 BULKHEAD WEB. SUPPLEMENTAL DATA UPDATE CRACKS REPAIRED PER BOEING SRM 53-10-08.SDR 2000UALA00734Bulkhead · crackedCRACK FOUND ON THE BODY STATION 178 BULKHEAD WEB. SUPPLEMENTAL DATA UPDATE CRACKS REPAIRED PER BOEING SRM 53-10-08.SDR CA000307008Bulkhead · cracked(CAN) INSPECTION REQUIRED BY CF98-38 FOUND CRACKS IN THE BULKHEAD/CHANNEL ASSY. P/N''S C2FS533 AND C2FS4045A WERE REPLACED.SDR USAA000260Bulkhead · crackedBULKHEAD HAS A .25 INCH CRACK AT BS 663, LBL 25. SPLICED IN DOUBLER PER EA 66610 AND SB 737-53-1184. (M)SDR SWAA000319Bulkhead · crackedDURING SCHEDULED D-CHECK, FOUND NLG WHEEL WELL BULKHEAD CRACKED, BS 246-248, RBL 16. REPAIRED BULKHEAD PER SRM.SDR SWAA000316Bulkhead · crackedDURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD 10 CRACKS, LBL 5 TO RBL 7. REPAIRED BULKHEAD PER SRM.SDR QXEA0000546Rib · corrodedPDX - RIGHT WING RIB 2230 LOWER STRUT BOX CHANNEL HAS BUBBLED POINT, SUSPECT CORROSION ABOVE 7TH STRINGER AFT OF 72A APERATURE. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH 4A1 AND SRM 53-01-01, PAGE 8, ITEM 4C.SDR KPVA200005Bulkhead · dentedREAR PRESSURE BULKHEAD AT STATION X653, STRINGER 11 TO 12 DENTED. REPAIRED REAR PRESSURE BULKHEAD AT STATION X653, STRINGER 11 AND 12 IAW DHC-8-RD8-53-4788. THIS REPAIR WILL REQUIRE REPEAT INSPECTION IAW A LATER ISSURE OF THE REPAIR DRAWING. INTERVAL TO BE SDR 20000329SH016Bulkhead · corrodedDURING A C-CHECK, CORROSION WAS NOTED ON FORWARD BULKHEAD ON LOWER RIB STA 178 RBL 295 TO RBL 18.0. (X)SDR SWAA000276Bulkhead · crackedDURING SCHEDULED 1/4D CHECK, FOUND THRU ULTRASONIC INSPECTION, BS 178 BULHEAD CRACKED, RBL 7, RBL 1 AND LBL 1. REPAIRED BULKHEAD PER SRM.SDR RRXA003795Frame · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO FWD LWR CARGO COMPT BILGE AT STA. 80 AND ABOVE 31L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SDR TWAA0002605Bulkhead · crackedDURING CHECK-C MAINT, FOUND A 2 INCH CRACK IN PRESSURE WEB, RT MLG WHEEL WELL AT STA 940, RBL 55. CONFIRMED CRACK WITH HIGH FREQ EDDY CURRENT. INSTALLED REPAIR DOUBLER PER BOEING PRINT 65-89360, AND AD 92-19-11.SDR 2000ZZZX301Bulkhead · crackedELONGATED FASTENER HOLES, GOUGE AND CRACK DAMAGE ASSOCIATED WITH THE AFT PRESSURE BULKHEAD TEE CHORD SPLICE AT L6L TO L8L. REQUIRED AFT PRESSURE BULKHEAD TEE CHORD AT STA 996 BETWEEN L6L TO L8L PER EIA ECRA 941-53-077-2 REV A.SDR DL72S000273Bulkhead · crackedFS 870 WEB CRACKED RT MLG W/W AT APU LOAD CONTROL VALVE. CUT OUT 1.5 INCH AT 6:00 POS. INSTALLED TIME LIMITED REPAIR PER SRM 53-10-9D FIG 806D.SDR QXEA0000601Bulkhead · crackedPDX - FORWARD PRESSURE BULKHEAD AT CL BEAM 6 IS CRACKED IN RADIUS OF UPPER AND LOWER ANGLES. REPAIRED IAW HORIZON AIR EA 4-53-1007.SDR TWAA0002409Bulkhead · gougedDURING OP 16 MAINT CHECK FOUND GOUGE IN FWD SIDE OF AFT PRESSURE BULK HEAD SKIN BELOW LONGERON 2L. REMOVED FASTENER AND BLENDED GOUGE PER SRM 53-01 FIG 1 AND REINSTALLED FASTENER.SDR USAA000151Bulkhead · crackedCLT - FOUND BULKHEAD WEB CRACKED 1.5 INCHES, STATION 178 RBL 5 BETWEEN WL 197.5 AND 199. INSTALLED DOUBLER PER TR 53-10-07. (M)SDR USAA000150Bulkhead · crackedCLT - FOUND BULKHEAD WEB CRACKED 1 INCH, STATION 178 RBL 5 BETWEEN WL 202 AND 203. INSTALLED DOUBLER PER TR 53-10-07. (M)SDR USAA000145Bulkhead · crackedCLT - FOUND BULKHEAD WEB CRACKED .5 INCH, STATION RBL .5, WL 188. INSTALLED BULKHEAD WEB PER SRM 53-10-08. (M)SDR 20000503SH046Bulkhead · dentedREPAIRS TO FORWARD, LEFT COCKPIT PRESSURE WEB PANEL FROM BS 69 TO BS 83.5 BY REMOVAL OF DAMAGED AREA AND INSTALLATION OF FILLER, DOUBLERS, AND TRIPLER. (EIA ECRA 940-53-042-2).SDR 20000503SH033Bulkhead · crackedREPAIR OF GOUGES IN AFT PRESSURE BULKHEAD AT BS 1017 (CAUSED BY CONTROL CABLES CHAFING STRUCTURE). (EIA ECRA 940-53-027-2). (X)SDR SWAA000224Frame · crackedDURING SCHEDULED 1/2D CHECK, HFEC INSP INDICATED BS 178 BULKHEAD LT SIDE CHORD CRACKED, LBL 26. REMOVED AND REPLACED CHORD SECTION PER SRM.SDR RRXA001697Pressure Panel · distortedDURING A MAINTENANCE VISIT, FOUND DISTORTED SKIN IN THE RT WHEEL WELL AT FWD AND AFT SIDE OF RT MLG OPENING, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED ANGLE FROM 2024-T3 AND INSTALLSDR QXEA0000602Bulkhead · leakingPDX - FORWARD PRESSURE BULKHEAD HAS EVIDENCE OF PRESSURIZATION LEAK ON FORWARD SIDE BETWEEN BEAMS 6 AND 7 AT BL 700R. REPAIRED IAW FOKKER SRM 51-31-01.SDR RRXA003786Fitting · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO CABIN ATTACH FITTING AT STA 1140 AND L21R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 51-1-20SDR 2000UALA00749Bulkhead · crackedCRACK FOUND ON THE BODY STATION 178 BULKHEAD WEB. SUPPLEMENTAL DATA UPDATE CRACKS REPAIRED PER BOEING SRM 53-10-08.SDR EIA2000066Bulkhead · crackedFOUND AFT CARGO COMPT BS 1480 LEFT BULKHEAD WEB CRACKED AT APU BLEED DUCT CUTOUT 1 O-CLOCK POSITION. BS 1480 LEFT BULKHEAD WEB REPAIRED AT APU BLEED DUCT CUTOUT AREA PER BOEING DWG 144U2602 AND SB 747-53-2309. (M)SDR AT0000073Bulkhead · corrodedFOUND CANTED BULKHEAD AT BS 1143, LEFT HAND UNDER THE END OF LEFT HAND PYLON SKIN WAS CORRODED. REMOVED CORROSION, REPLACED SKIN AND DOUBLERS IAW DC9 SRM 53-01 FIGURE 4, 51-30-2, AND 51-30-3.SDR QXEA0000406Bulkhead · dentedPDX - SMALL SHARP DENT IN NOSE LANDING GEAR BAY LEFT-HAND SIDE WALL, BELOW FORWARD ACM MOUNT. REPAIRED IAW FOKKER SRM 53-02-01, PAGE 3.SDR SWAA000184Bulkhead · crackedDURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD CRACKED, WL 234, RBL12. REPAIRED BULKHEAD PER SRM.SDR P2EA00047Bulkhead · crackedSJO - DURING Q-CHECK, FOUND BULKHEAD WEB CRACKED AT BS 227.8 WL 182 AND BL 0. REPAIRED WEB AT BS 227.8 BETWEEN WL 188 AND WL 159 IAW SB 737-53-1054, REV 2, SECTION III, FIG 8 DATED 02/29/96. (M)SDR USAA000090Bulkhead · crackedCLT - Q-1 - STA 727, LBL 23, WL 202, BULKHEAD HAS A .50 INCH CRACK. INSTALLED REPAIR DOUBLER PER TR 53-10-03. (X)SDR USAA000089Bulkhead · crackedCLT - Q-1 - STA 727, RBL 23, WL 202. BULKHEAD HAS A .50 INCH CRACK. INSTALLED REPAIR DOUBLER PER TR 53-10-03. (X)SDR USAA000087Bulkhead · crackedCLT - Q-2 - STA 178, LBL 1.5, WL 204.5, BULKHEAD WEB HAS A .5 INCH CRACK. INSTALLED DOUBLER PER TR 53-10-11. (X)SDR QXEA0000454Bulkhead · dentedPDX - DENTED AREA APPROXIMATELY 3 INCHES LONG BY 2 INCHES HIGH AND .060 DEEP IN AFT SIDE OF REAR WALL OF RIGHT-HAND MAIN LANDING GEAR STRUT BAY, JUST INBOARD OF STRUT PIVOT PIN. REPAIRED IAW HORIZON AIR EA 4-57-351.SDR 00FDEA00035Bulkhead · damagedWHILE WORKING 71C101-02, FOUND STRUCTURAL DAMAGE AT BS 227.8, LBL 12, WL 163 ON PRESSURE BULKHEAD. *S/D* REMOVED AND REPLACED PER SRM 51-40-2 FIG 1.SDR RRXA003794Frame · crackedDURING A MAINTENANCE VISIT FOUND CRACKED DAMAGE TO FWD CARGO COMPT. FWD BULKHEAD LT SIDE AT STA. 80 AND X=60 AND Z=25, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-2SDR SWAA000153Bulkhead · crackedDURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD CRACKED, LBL 6 - LBL 7. REPAIRED BULKHEAD PER SRM.SDR SWAA000144Bulkhead · crackedDURING SCHEDULED 1/2D CHECK, FOUND BS 178 BULKHEAD CRACKED, RBL 5. REPAIRED BULKHEAD PER SRM.SDR SWAA000143Bulkhead · crackedDURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD CRACKED, RBL 6 AND RBL 7. REPAIRED BULKHEAD PER SRM.SDR CALA0000056Bulkhead · crackedINSPECTION FOUND A CRACK IN BULKHEAD AT STA 1309 BETWEEN LONGERONS 15R AND 16R. THE CRACK WAS STOP DRILLED IAW SRM 53-14-03, FIGURE3 AND A REPAIR WAS INSTALLED IAW SRM 51-10-04, 51-10-03, AND 51-30-05.
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