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 P5CA9700611Bulkhead Angle · corrodedLEVEL 1 CORROSION, STA 1480 BULKHEAD NR 3 HORI STIFFENER AT ANGLE AT LBL 30. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01, TREATED PER 51-10-02 AND MM 51-24-11.SDR P5CA9700610Bulkhead Angle · corrodedLEVEL 1 CORROSION, STA 1480 BULKHEAD NR 6 STIFFENER AT ANGLE AT LBL 38. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01, TREATED PER 51-10-02 AND MM 51-24-11.SDR P5CA9700609Bulkhead · corrodedLEVEL 1 CORROSION, STA 1480 BULKHEAD NR 6 HORI STIFFENER SURFACE AT RBL 13 TO 55. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01, TREATED PER 51-10-02 AND MM 51-24-11.SDR P5CA9700608Bulkhead · corrodedLEVEL 1 CORROSION, STA 1480 BULKHEAD NR 5 HORI STIFFENER SURFACE AT LBL 55 TO RBL 100. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01, TREATED PER 51-10-02 AND MM 51-24-11.SDR P5CA9700607Bulkhead · corrodedLEVEL 1 CORROSION, STA 1480 BULKHEAD NR 4 HORI STIFFENER SURFACE AT LBL 100 TO RBL 100. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01, TREATED PER 51-10-02 AND MM 51-24-11.SDR P5CA9700606Bulkhead · corrodedLEVEL 1 CORROSION, STA 1480 BULKHEAD NR 3 HORI STIFFENER SURFACE AT LBL 100 TO RBL 105. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01, TREATED PER 51-10-02 AND MM 51-24-11.SDR P5CA9700605Bulkhead · corrodedLEVEL 1 CORROSION, STA 1480 BULKHEAD NR 2 HORI STIFFENER SURFACE AT LBL 100 TO RBL 110. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01, TREATED PER 51-10-02 AND MM 51-24-11.SDR AU970533Bulkhead · cracked(AUS) FORWARD PRESSURE BULKHEAD CRACKED IN THREE PLACES:- 1. REAR SIDE OF FORWARD PRESSURE BULKHEAD WEB AT HORIZONTAL BEAM NO7 LEFT OF BL325L - CRACK LENGTH 76.2MM (3IN) 2. REAR SIDE OF FORWARD PRESSURE BULKHEAD WEB AT HORIZONTAL BEAM NO7 RIGHT OF BL325R - CRASDR AU970510Bulkhead · cracked(AUS) FORWARD PRESSURE BULKHEAD CRACKED IN THREE AREAS:-1. FORWARD PRESSURE BULKHEAD REAR SIDE AT HORIZONTAL BEAM 7 LEFT OF BL325L - CRACK LENGTH 76.2MM (3IN)2. FORWARD PRESSURE BULKHEAD REAR SIDE AT HORIZONTAL BEAM 7 RIGHT OF BL325R - CRACK LENGTH 127MM (5INSDR 97FDEA00289Bulkhead Web · corrosionNR 0475 015, CORROSION (SPEC C53-132-02,1) ON STA 870 BULKHEAD WEB RBL 65 TO LBL 65, WL 178. *S/D* REMOVED DAMAGED BULKHEAD STA 870, WEB RBL 65 TO LBL 65 AND INSTALLED NEW WEB PER FED-EX EA 7-5710-34044.SDR P5CA9700580Bulkhead · corrodedLEVEL 1 CORROSION, STA 1480 BULKHEAD AT STIFFENER NR 5 FOUND AT LBL 55 TO 92. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01, TREATED PER 51-10-02 AND MM 51-24-11.SDR P5CA9700579Bulkhead · corrodedLEVEL 1 CORROSION, STA 1480 BULKHEAD AT STIFFENER NR 6 AT RBL 55 TO 80. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01, TREATED PER 51-10-02 AND MM 51-24-11.SDR AU970553Stiffener · corroded(AUS) REAR PRESSURE BULKHEAD STIFFENER CORRODEDSDR EISA97126Bulkhead Angle · crackedDURING ROUTINE C-CHECK INSPECTION OF AFT PIT, AFT BULKHEAD UPPER RT SIDE, FOUND 7 INCH CRACK ON VERTICAL ANGLE FS 1183. REMOVED CRACKED ANGLE, FABRICATED AND INSTALLED NEW ANGLE IAW SRM 53-10-2. (M)SDR AU970538Bulkhead · cracked(AUS) LOWER AFT DOOR POST BULKHEAD CRACKED - FOUND DURING INSPECTION IAW CESSNA SEB 97-1SDR AU970536Bulkhead · cracked(AUS) LOWER AFT DOOR POST BULKHEAD CRACKED - FOUND DURING INSPECTION IAW CESSNA SEB 97-1SDR AU970535Bulkhead · cracked(AUS) LOWER AFT DOORPOST BULKHEAD CRACKED - FOUND DURING INSPECTION IAW CESSNA SEB 97-1SDR DHL9770235DBulkhead · dentedAT D-CHECK, FWD FACE OF FS 178 BULKHEAD DENTED AT 10 TO 11 O'CLOCK 4 FROM OUTSIDE EDGE. CUT OUT DAMAGED AREA, INSTALLED DOUBLER REPAIR PER SRM 53-10-9, 12 X 8.SDR SWAA970477Bulkhead · crackedDURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD CRACKED AT RBL 4.7, WL 201.5 TO 202.25. REPAIRED PER BOEING SRM AND TRAMCO EWO 97-0210.SDR SWAA970475Bulkhead · crackedDURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD CRACKED ON AFT SIDE, BL 0, WL 190, AT LBL 67, WL 201 TO 202.5, AT LBL 4.7, AND WL 199 TO 199.5. REPAIRED PER BOEING SRM AND TRAMCO EWO 97-0211.SDR IXXA9700100Bulkhead Bracket · crackedDURING ROUTINE C-CHECK INSPECTION, THE TOP AFT PRESSURE BULKHEAD SUPPORT BRACKET WAS FOUND CRACKED. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED BRACKET, FABRICATION AND INSTALLATION OF NEW BRACKET IN ACCORDANCE WITH DOUGLAS AIRCRAFT COMPANY SRM 51-1-21, 51-1-0 ANDSDR IXXA9700098Bulkhead Bracket · crackedDURING ROUTINE C-CHECK INSPECTION, FOUND THE AFT PRESSURE BULKHEAD RIGHT SUPPORT BRACKET CRACKED ABOVE THE THIRD STIFFENER. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED BRACKET, FABRICATION AND INSTALLATION OF NEW BRACKET IN ACCORDANCE WITH DOUGLAS AIRCRAFT COMPANYSDR IXXA9700097Bulkhead Fitting · crackedDURING ROUTINE C-CHECK INSPECTION, FOUND THE AFT PRESSURE BULKHEAD LEFT SUPPORT FITTING CRACKED ABOVE THE THIRD STIFFENER. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED FITTING, FABRICATION AND INSTALLATION OF NEW FITTING IN ACCORDANCE WITH DOUGLAS AIRCRAFT COMPANY SDR AU970544Bulkhead · cracked(AUS) FORWARD PRESSURE BULKHEAD CRACKED AT SIDE CHORD RADIUS LH SIDE AT WL207 - CRACK LENGTH APPROXIMATELY 76.2MM (3IN)SDR 9716486642Bulkhead Web · corrodedDURING M-CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON BULKHEAD WEB FORWARD FACE AT FS 1480, RBL 109. REPAIRED PER EA 66-150186.SDR 9709569966Bulkhead · crackedDURING 'M' CHECK, FOUND CRACK IN NOSE LANDING GEAR WHEEL WELL HORIZONTAL PRESSURE BULKHEAD, RIGHT SIDE TOP OF OUTBOARD VERTICAL FRAME FS 110. REPAIRED PER EA 99-112875.SDR ABXA9700987Bulkhead Web · crackedDURING C-CHECK, FOUND THE LT PYLON BULKHEAD WEB CRACKED AT INBOARD END 5 ABOVE THE FLOOR LINE. REMOVED AND REPLACED THE WEB IAW DC9 SRM 51-30-5 AND 51-30-2.SDR 97ZZZX2523Angle · crackedL-ANGLE CRACKED FORWARD BULKHEAD FS 178. INSTALLED NEW ANGLE IAW 727 SRM 51-30-2.SDR 9709589998Bulkhead · crackedDURING 'L' CHECK, FOUND CRACK IN NOSE LANDING GEAR WHEEL WELL HORIZONTAL PRESSURE BULKHEAD, LEFT SIDE, APPROXIMATELY 28 INCHES FROM CUSP FS 110. REPAIRED PER EA 99-112899.SDR UPS97422893Bulkhead Web · damagedINSPECTION TYPE-C, BS 2360 REAR PRESS BULKHEAD 3 FASTENERS IN VERY BAD CONDITION AT 3 O'CLOCK POSITION APPROX RBL 48 SEGMENT LAP JOINT. REPAIRED AFT PRESS BULKHEAD WEB AT SEGMENT LAP JOINT IAW SRM 51-30-02, DFX 97-116 REV 2, FAA FORM 8110-3, REF UPS-AMS-0153TSDR AU970641Web · cracked(AUS) FORWARD PRESSURE BULKHEAD WEB CONTAINED THREE CRACKS IN AREA BELOW THE RADAR SCANNING MOUNTING BRACKETS - TWO CRACKS LOCATED AT LBL 5.7 - ONE CRACK LOCATED AT RBL 5.7 - CRACK LENGTHS 10MM(0.393IN) - FOUND DURING EDDY CURRENT INSPECTION IAW ER B73-53-10-3SDR UPS97422841Bulkhead · crackedINSPECTION TYPE-C, AFT PRESSURE BULKHEAD FOUND CRACK IN BULKHEAD SECTION JUST BELOW RT RADIAL 130 ABOVE STR 24, 4 FROM SKIN JOINT. REPAIRED AFT PRESS BULKHEAD RT RADIAL 130 ABOVE STR 24, 4 FROM SKIN JOINT ACC UPS EO 747-53-0828 AND KLM DFX 97-111. PERFORMED SDR CA970526006Bulkhead · cracked(CAN) CRACK FOUND AT TAIL ROTOR GEARBOX ATTACHMENT POINT. LEFT REAR BOLT HOLE. AIRCRAFT TT: 9,419 HOURS.SDR DL73E970833Bulkhead Web · crackedTHREE CRACKS WERE DISCOVERED ON THE FWD FACE OF THE FS 178 BULKHEAD WEB. TRIMMED OUT CRACKS; 0.050 2024-T3 DOUBER, FILLER AND SHIMS AS REQUIRED; DTA ANALYSIS AT 60,000 CYCLES.SDR DHL9770115CBulkhead Angle · corrodedDURING C-CHECK, FORWARD PIT BS 480 BULKHEAD L-ANGLE FILLER HAS CORROSION BETWEEN STR 25L TO 26L. CLEANED AREA OF CORROSION PER SRM 51-10-2. INSTALLED NEW FILLER AT BS 480 BETWEEN STR 27RT TO 22RT AS PER SRM 51-40-1. FILLER LENGTH 36, N/R3499.SDR AU970744Strap · cracked(AUS) FUSELAGE BULKHEAD SPLICE STRAP LOCATED AT BS1241 CRACKED ON LHAND RH SIDES AT FORWARD AND AFT HOLESSDR 97ZZZX2119Bulkhead · crackedDURING ROUTINE INSPECTION, CRACKS DETECTED IN UPPER LEFT BULKHEAD FLANGE RADIUS ABOVE RUDDER STOP. SUBJECT IS COVERED BY CESSNA SL 72-3 AND AD 72-07-09. SUSPECT CAUSE IS YEARS OF RUDDER STOP CONTACT. SUBMITTER STATED THIS TYPE OF CRACK MAY BE ELIMINATED BY SDR 97ZZZX2099Bulkhead · misinstalledVERTICAL FIN AFT SPAR TO BULKHEAD CLEARANCE EXCESSIVE. MAXIMUM CLEARANCE .070 INCH PER CESSNA 172 SM. P/N 0512159-3 INSTALLED INCORRECTLY OR MACHINED INCORRECTLY BY FACTORY AT LOWER HOLE MACHINE FACE. MISSING .090 INCH OF MATERIAL. FIXED BY INSTALLING .090SDR DHL9770118CBulkhead Bracket · missingDURING C-CHECK, LOWER AFT CARGO COMPARTMENT VERTICAL BEAM END PREVIOUSLY CUT OFF AND MISSING LOWER ATTACH BRACKET AND WEB ON TOP OF STR 22L BL 46.9, 1183 BULKHEAD. INSTALLED ANGLE AS PER SRM 51-40-4, ATTACHED TO VERTICAL BEAM AS PER SRM 51-30-2, N/R 3543.SDR AU970537Bulkhead · cracked(AUS) LOWER AFT DOOR POST BULKHEAD CRACKED - FOUND DURING INSPECTION IAW CESSNA SEB 97-1SDR 9708629929Bulkhead · crackedDURING L-CHECK, FOUND A CRACK IN THE NOSE LANDING GEAR WHEEL WELL HORIZONTAL PRESSURE BULKHEAD FS 110 AT RIGHT INBOARD FITTING. REPAIRED PER EA 99-112886.SDR 9708619972Bulkhead · crackedDURING M-CHECK, FOUND A CRACK IN NOSE LANDING GEAR WHEEL WELL HORIZONTAL PRESSURE BULKHEAD FS 105, LEFT SIDE, 22 INCHES INBOARD OF FUSELAGE SKIN. REPAIRED PER EA 99-112342.SDR 9708609972Bulkhead · crackedDURING M-CHECK, FOUND A CRACK IN THE NOSE LANDING GEAR WHEEL WELL HORIZONTAL PRESSURE BULKHEAD FS 105 ABOVE RIGHT OUTBOARD VERTICAL BEAM. REPAIRED PER EA 99-112342.SDR 9708599998Bulkhead · crackedDURING L-CHECK, FOUND A CRACK IN THE NOSE LANDING GEAR WHEEL WELL HORIZONTAL PRESSURE BULKHEAD, FS 83, LEFT SIDE. REPAIRED PER EA 99-112902.SDR 9708639929Bulkhead · crackedDURING L-CHECK, FOUND CRACK IN NOSE LANDING GEAR WHEEL WELL HORIZONTAL PRESSURE BULKHEAD AT FS 110 AT RIGHT OUTBOARD FITTING. REPAIRED PER EA 99-112886.SDR DHL9780104CBulkhead · crackedAT C-CHECK, AFT PRESSURE BULKHEAD FWD SIDE AT FS 1760 LEFT AT LONGERON 11 BETWEEN STIFFENER 5772638-53 AND -51, THERE IS A 2.00 CRACK. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER AND INSTALLED PER SRM 53-2-5.SDR 9709549929Bulkhead · corrodedDURING L CHECK, FOUND CORROSION ON THE HORIZONTAL FLANGE AT THE T-CAP FS 110 BETWEEN LONGERONS 26L AND 27L. REPAIRED PER EA 99-112892.SDR CALA9700798Bulkhead · crackedINSPECTION FOUND A 1.75 INCH CRACK IN RT MLG WELL BULKHEAD AT STA 870, BELOW APU LOAD CONTROL VALVE. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW ECRA 5310-01544.SDR 9708739929Bulkhead · crackedDURING L-CHECK, FOUND A CRACK IN THE NOSE LANDING GEAR WHEEL WELL HORIZONTAL PRESSURE BULKHEAD FS 110 AT LEFT OUTBOARD FITTING. REPAIRED PER EA 99-112886.SDR CALA9700653Bulkhead Skin · crackedINSPECTION FOUND A .125 CRACK IN SKIN AT APB T-CAP, LONGERON 2L. A REPAIR WAS INSTALLED IAW EA 5361-01001.
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