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 A6WA201240622Bulkhead · dentedAFT RT BS 280 BUKLHEAD HAS TWO DENTS NEAR INBD EDGE FROM CONTACT FROM GALLEY STORAGE COMPARTMENT DOOR CUT AWAY DAMAGE ON AFT RT SIDE OF BS 280 BULKHEAD AND INSTALLED REPAIR DOUBLER AND FILLER IAW REO 601R-53-11-1727, REV E.May 7, 2012 · N442AW · Cndair CL6002B19SDR REXA2012051600667Bulkhead · damagedFS 755 BULKHEAD AFT FACE LOWER LT WEB AND ATTACHMENT FLANGE HAS 10 AREAS OF BUCKING BAR IMPACT DAMAGE. REPAIRED IAW SRM 53-00-00.May 7, 2012 · N8932C · Cndair CL6002B19SDR REXA2012050700440Bulkhead · crackedAFT PRESSURE BULKHEAD WEB (FS 621) CRACKED AT LBL 27.5, WL 130. REPAIRED IAW BOMBARDIER REO 601R-53-61-1541.May 7, 2012 · N8923C · Cndair CL6002B19SDR MASA2012050734760Stiffener · crackedAFT SIDE FS 202.75 BULKHEAD BL 0.00 VERTICAL STIFFENER IS CRACKED. OPEN HVY-CK. REPAIRED AFT VERTICAL STIFFENER AT FS 202.75 BULKHEAD IAW BOMBARDIER REO 690-53-11-379.May 6, 2012 · N919FJ · Cndair CL6002D24SDR SWIA201230739Bulkhead · cracked(C-CHECK) FS 621.0 BULKHEAD WEB IS CRACKED AT LBL 36.20 6 INCHES ABOVE FLOOR. REPAIRED FS 621.0 BULKHEAD WEB AT LBL 36.20.May 5, 2012 · N629BR · Cndair CL6002B19SDR DALA1229051404Failsafe · corrodedLT STA 955 REAR SPAR BULKHEAD FAIL SAFE STRAP FASTENER HOLE CORRODED. REPAIRED AS PER ERA 501535-14AD, REV ORG.May 5, 2012 · N144DA · Boeing 767332SDR DALA1229041404Tee Fitting · corrodedRIGHT BS 955 REAR SPAR BULKHEAD FITTING FOUND CORRODED AT TEE FITTING. REPLACED TEE FITTING AS PER ERA 501536-14AD, REV ORG.May 5, 2012 · N144DA · Boeing 767332SDR DALA1229031404Tee Fitting · crackedLEFT BS 955 REAR SPAR BULKHEAD FITTING CRACKED AT TEE FITTING. TEE FITTING REPLACED AS PER ERA 501535-14AD, ORG.May 5, 2012 · N144DA · Boeing 767332SDR DALA1229021404Failsafe · crackedRIGHT BS 955 REAR SPAR BULKHEAD FAILSAFE STRAP CRACKED, AREA TRIMMED OUT AND REPAIRED AS PER ERA 501536-14AD REV. ORGMay 5, 2012 · N144DA · Boeing 767332SDR SWIA201230612Bulkhead · cracked(C-CHECK) FS 202 BULKHEAD HAS CRACK AT PARKING BRAKE THROUGH-HOLE. REPAIRED CRACK AT FS 202 BULKHEAD.May 4, 2012 · N928SW · Cndair CL6002B19SDR R61A201205030283Support Angle · crackedWHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND THE LEFT WHEEL WELL FORWARD BULKHEAD UPPER SUPPORT CRACKED. MAINTENANCE REMOVED AND REPLACED THE LEFT FORWARD BULKHEAD UPPER SUPPORT BRACKET IAW EMB 175 SRM 51-40-02, 51-42-01, AND 51-43-01. THE AIRCRAFT ISMay 3, 2012 · N134HQ · Emb ERJ170200LRSDR REXA2012050400432Bulkhead · gougedPRESSURE BULKHEAD WEB AT FS 621 GOUGED IN 4 PLACES AT LBL 7 FORWARD SIDE 0.006 INCH DEEP. REPAIRED BY BOMBARDIER REO 601R-53-61-2155.May 3, 2012 · N8948B · Cndair CL6002B19SDR SWAA2012053104497Attach Angle · crackedRIGHT MLG WHEEL WELL AFT BULKHEAD LWR INBOARD ATTACH ANGLE CRACKED. REMOVED AND REPLACED ANGLE IAW SRM & BAC DWG.May 2, 2012 · N610WN · Boeing 7373H4SDR SWAA2012051804142Bulkhead · crackedBULKHEAD CRACKED AT BS 663, RBL 28. REPAIRED BULKHEAD IAW ATS ER AND EA / RBL 35.May 2, 2012 · N773SA · Boeing 7377H4SDR SWAA2012051804141Bulkhead · crackedBULKHEAD CRACKED AT BS 663, RBL 35. REPAIRED BULKHEAD IAW ATS ER AND EA.May 2, 2012 · N773SA · Boeing 7377H4SDR SWAA2012051804140Bulkhead · crackedBULKHEAD CRACKED AT BS 663, LBL42. REPAIRED BULKHEAD IAW ATS ER AND EA.May 2, 2012 · N773SA · Boeing 7377H4SDR DALA1228369263Bulkhead · crackedFOUND CRACK FWD FACE Y1520.22 ZRS - 16.00 RBL 20 REAR SPAR BULKHEAD. REMOVED LOUVER, REMOVED STIFFENERS AND WEB. FABRICATED NEW WEB, INSTALLED NEW WEB AND PREEXISTING STIFFENERS AND LOUVER BOX PER SRM 51-30-05, 51-30-02 AND 53-10-04 VOL II.May 2, 2012 · N963DN · Doug MD9030SDR DALA1228076305Frame · crackedDURING INSPECTION, FOUND CRACK AT BS 1000 BULKHEAD FRAME AT S38R. REPAIRE IAW WORK CARD.May 1, 2012 · N665US · Boeing 747451SDR USAA2012050700007Bulkhead · crackedFPBH VISIT - CRACK IN VERTICAL WEB AT BS 178 BETWEEN WL 226 & WL 232, RBL 17. REPAIRED VERTICAL WEB AT BS 178 BETWEEN WL 226 & WL 232, RBL 17 IAW B737 SRM 53-10-08-2R-12.May 1, 2012 · N457UW · Boeing 7374B7SDR REXA2012050200430Bulkhead · gougedPRESSURE BULKHEAD WEB AT FS 621 GOUGED IN 4 PLACES AT LBL 7 FORWARD SIDE. REPAIRED IAW BOMBARDIER REO 601R-53-61-2155.May 1, 2012 · N8948B · Cndair CL6002B19SDR SWAA2012060404568Bulkhead · crackedBULKHEAD CRACKED AT BS 663.75, RBL 35. REPAIRED BULKHEAD IAW EA.Apr 30, 2012 · N7730A · Boeing 7377BDSDR DALA1229749234Bulkhead · damagedDURING HMV AT MIA, THE AFT FUSELAGE WAS DAMAGED DURING A JACKING INCIDENT. AREAS REPAIRED PER ERA 502764-14 REV O AT AFT PRESSURE BULKHEAD STA 1395 APB AND SKIN L-22L.Apr 27, 2012 · N934DN · Doug MD9030SDR EPUA2012050101Bulkhead · crackedAFT CANTED BULKHEAD AT BS 474.4 CRACKED AT ELEVATOR PUSH PULL TUBE OPENING. DURING REMOVAL AFT VERTICAL SPAR WEB (2631021-12) WAS FOUND TO HAVE EXCESSIVE FRETTING, VERTICAL SPAR WEB ALSO REPLACED.Apr 27, 2012 · N411GV · Cessna 208BSDR GLBA2012042701Bulkhead · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND TWO CRACKS IN THE FWD PRESSURE BULKHEAD ALONG THE OTBD ROW OF FASTENERS NEXT TO THE RT NOSE GEAR WEB AT FS 84.00, .375" IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 12-1Apr 27, 2012 · N184UX · Beech 1900DSDR CA120504003Bulkhead · corroded(CAN) FOUND BULKHEAD AT FRAME 39, CORRODED AND PERFORATED BETWEEN STRINGERS 54-55L AND BELOW WATERLINE Z-2557.Apr 25, 2012 · Airbus A310304SDR LR7A2012042500376Bulkhead · crackedDURING SCHEDULED B-3 CHECK, FOUND FUSELAGE BULKHEAD WEB CRACKED AT FS 880, WL 254, LBL 60. REPAIRED IAW SMP583 FIG 51-140-17.Apr 25, 2012 · N405LC · Lkheed 382GSDR GLBA2012042602Bulkhead · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK ON THE FWD PRESSURE BULKHEAD ALONG ROW OR FASTENERS NEXT TO THE LT NOSE GEAR WEB, FS 84.00, 7.25" IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 12-1900-53-029. MAApr 25, 2012 · N184UX · Beech 1900DSDR AALA20120424014Firewall · wornAUXILIARY POWER UNIT COMPARTMENT FIREWALL AFT FACE CHAFED FROM RIGHT DOOR HOLD OPEN HOOD BODY STATION 1787, RIGHT BUTTLINE 10. INSTALLED DOUBLER PER SRM 53-80-08-2R.Apr 24, 2012 · N663AM · Boeing 757223SDR FDEA201204241548Bulkhead · crackedCENTER LANDING GEAR WHEEL WELL FWD BULKHEAD FOUND CRACK ON RT TEE FITTING UPPER AREA. R & R IAW SRM 51-31-01, REV 49. REPAIR CLASSIFIED AS MAJOR GMM 6-2-100, REV 114.Apr 24, 2012 · N606FE · Doug MD11FSDR 2012FA0000306Bulkhead · crackedAFT BULKHEAD INSPECTED IAW AD 72-07-09. FOUND A CRACK IN LOWER INBD CORNER OF RT CUTOUT. REPLACED BULKHEAD.Apr 23, 2012 · N6824R · Cessna T210GSDR ASOA201201330Stiffener · crackedFS 409+128 BULKHEAD LBL 18 POST FAILS NDT WITH A CRACK INDICATION GREATER THAN 50 PERCENT SCREEN HEIGHT APPROX .100 LONG IN OTBD AFT RADIUS. REMOVED POST IAW SRM 51-42-06. LOCATED AND DRILLED POST IAW SRM 51-40-11-00. INSTALLED NEW POST IAW REO 601R-53-41Apr 23, 2012 · N447CA · Cndair CL6002B19SDR WX0A071176Bulkhead · crackedFLIGHT COMPARTMENT LOWER VERTICAL BULKHEAD WED IS CRACKED AT RBL 8-63 AND LBL 3-3 AS FS 120. CUT OUT DAMAGED AREAS, FABRICATED REPAIR DOUBLERS, FILLERS AND INSTALLED IAW BOEING DWG #9911590 AND MD80 SRM 51-70-4.Apr 23, 2012 · N412NV · Doug MD88SDR SWIA201230686Bulkhead · crackedFS 621 BULKHEAD WEB IS CRACKED AT LBL 27.50 AT TOP OF CARGO TRACK. (C-CHECK) REPAIR FS 621 BULKHEAD WEB AT LBL 27.50 AT TOP OF CARGO TRACK.Apr 22, 2012 · N441SW · Cndair CL6002B19SDR SWIA201230454Bulkhead · crackedCRACK ON THE LEFT SIDE FS 559.0 PRESSURE BULKHEAD. (C-CHECK) REPAIR CRACK ON THE LEFT SIDE FS 559.0 PRESSURE BULKHEAD.Apr 21, 2012 · N464SW · Cndair CL6002B19SDR SWIA201230453Bulkhead · crackedCRACK ON THE RIGHT SIDE FS 559.0 PRESSURE BULKHEAD. (C-CHECK) REPAIR CRACK AT RIGHT SIDE FS 559.0 PRESSURE BULKHEAD.Apr 21, 2012 · N464SW · Cndair CL6002B19SDR CA120509009Bulkhead · dented(CAN) ACFT WAS OPEN FOR INSPECTION. NOTICED THAT BULKHEAD WAS DENTED. ALSO FOUND OUT THAT DEALER HAS NOTED THAT THIS IS A COMMON PROBLEM IN MANY OF THE NEWER MODEL. THIS DAMAGE IS NOT NEGLIGABLE IAW SRM. SUGGEST THAT MFR IS CONTACTED TO MODIFY THE SRM TO ALLOApr 20, 2012 · Cessna T182TSDR SWAA2012052104161Bulkhead · crackedVERTICAL BEAM WEB CRACKED AT BS 178, LBL 17. REPAIRED WEB IAW EA AND EO.Apr 20, 2012 · N640SW · Boeing 7373H4SDR DALA1225816301Bulkhead · corrodedDURING INSPECTION, MAINTENANCE FOUND CORROSION AT FORWARD CARGO BS 1000 BULKHEAD LOWER CHORD AREA LEFT SIDE BETWEEN STRINGERS S-46 AND S-47. DEFERRED.Apr 20, 2012 · N661US · Boeing 747451SDR 2012FA0000216Bulkhead · crackedCRACKS FOUND IN FLANGE OF BOTH THE LT AND RT FUSELAGE BULKHEAD AT STATION 17. CRACKS RADIATING FROM THE UPPER BOLT HOLE WHERE THE FUELING STEP ATTACHES. BOLT HOLE IS TOO CLOSE TO BEND RADIUS OF BULKHEAD, CAUSING DISTRESS WHEN BOLT IS TIGHTENED.Apr 20, 2012 · N821CP · Cessna 182TSDR 2012FA0000215Bulkhead · crackedCRACKS FOUND IN FLANGE OF BOTH THE LEFT AND RIGHT FUSELAGE BULKHEADS AT STATION 17. CRACKS RADIATING FROM UPPER BOLT HOLE WHERE FUELING STEP ATTACHES. BOLT HOLE IS TOO CLOSE TO BEND RADIUS OF BULKHEAD, CAUSING DISTRESS WHEN BOLT IS TIGHTENED. SECOND INSTANCApr 20, 2012 · N883CP · Cessna 182TSDR SWAA2012052104160Bulkhead · crackedVERTICAL BEAM WEB CRACKED AT BS 178, RBL 5.7. REPAIRED WEB IAW EA AND EO.Apr 19, 2012 · N640SW · Boeing 7373H4SDR A6WA201240490Bulkhead · dentedRT AFT SIDE OF 280 BULKHEAD DENTED FROM GALLEY DOOR COMPLIED WITH REO 601R-53-11-1727, REV F.Apr 19, 2012 · N446AW · Cndair CL6002B19SDR SWAA2012051403987Bulkhead · crackedVERTICAL BEAM WEB CRACKED AT BS 178, LBL 5.7. REPAIRED WEB IAW SRM.Apr 19, 2012 · N640SW · Boeing 7373H4SDR QXEA2012041900333Bulkhead Web · corrodedFWD PAX DRAFT BULKHEAD SUPPORT WEB AT STA X32.400 HAS AREAS OF CORROSION. REMOVED BULKHEAD SUPPORT WEB IAW SRM 51-42-45-02-01. FOUND TO BE OUT OF LIMITS IAW SRM 51-21-00-00-02. INSTALLED NEW WEB SUPPORT IAW SRM 51-42-45-02-01.Apr 19, 2012 · N417QX · Bombdr DHC8402SDR V0XR20120422J0023Bulkhead Web · corrodedFS 280 LT BULKHEAD WEB CORRODED BEYOUND SERVICEABLE LIMITS. R & R FS 280 LT BULHEAD WEB LAW SRM 51-42-06, 51-42-13, 51-42-21, 51-23-00, REO670-53-11-052.Apr 19, 2012 · N368CA · Cndair CL6002C10SDR SWIA201230570Bulkhead · crackedCRACK ON FS 621 AFT PRESSURE BULKHEAD FORWARD FACE AT WL 133.1 LBL 27.50. (C-CHECK) REPAIRED FS 621 AFT PRESSURE BULKHEAD FORWARD FACE AT WL 133.1 LBL 27.50.Apr 18, 2012 · N709BR · Cndair CL6002B19SDR DALA1228881501Tee Fitting · corrodedLEFT BS 955 REAR SPAR BULKHEAD TEE FITTING CORRODED. FITTING REPLACED REF ERA 501532-14AD REV ORIG.Apr 17, 2012 · N1501P · Boeing 7673P6SDR DALA1228861501Tee Fitting · corrodedRT BS 955 REAR SPAR BULKHEAD TEE FTG FASTENER HOLES CORRODED. FITTING REPLACED REF ERA 501533-14AD REV ORIG.Apr 17, 2012 · N1501P · Boeing 7673P6SDR SWAA2012042703504Bulkhead · crackedMAIN CABIN PRESSURE VERTICAL WEB BULKHEAD CRACKED AT BS 663, RBL 28. REPAIRED WEB IAW EA.Apr 17, 2012 · N420WN · Boeing 7377H4SDR DALA1223721501Tee Fitting · corrodedFS 955 RT REAR SPAR BLKHD "T" FITTING AT FAILSAFE HAS CORROSION, WORKING FROM A PRI.Apr 17, 2012 · N1501P · Boeing 7673P6
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