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 COEA2016071005917Stiffener · corrodedFWD PRESSURE BULKHEAD RT STIFFENER HAS CORROSION. REPLACED THE STIFFENER.Jul 10, 2016 · N917FX · Aerosp ATR42300SDR REXA2016071001281Bulkhead · crackedAPB IS CRACKED AT LBL 27.5 AND APPROXIMATELY WL 130, JUST ABOVE CARGO DOOR TRACK. REPAIRED APB AT LBL 27.5 APPROXIMATELY WL 130 IAW REO 601R-53-61-1541.Jul 10, 2016 · N8918B · Cndair CL6002B19SDR DALA2016071205231Plate · crackedACRID ODOR OF BURNING ELECTRICAL, FOLLOWED BY WEATHER RADAR FAIL ON ND. DURING INSPECTION, FOUND D477 WEATHER RADAR CONNECTOR DAMAGED AT PRESSURE BULKHEAD, DISCONNECTED BOTH SIDES TO INSPECT THE CONNECTOR SUPPORT PLATE. FOUND PLATE CRACKED. INSTALLED TIMEJul 10, 2016 · N693DL · Boeing 757232SDR WVER0710201602Bulkhead Web · corrodedLEFT BS 280 LOWER BULKHEAD WEB IS CORRODED.Jul 10, 2016 · N245LR · Cndair CL6002D24SDR WVER0710201601Bulkhead Web · corrodedRIGHT BS 280.00 LOWER BULKHEAD WEB IS CORRODED.Jul 10, 2016 · N245LR · Cndair CL6002D24SDR REXA2016070801422Bulkhead · not reportedPRESSURE BULKHEAD AT BS 559 BL 23L-23R. REPAIRED BULKHEAD IAW GREO 601R-53-41-260, GREO 601R53-41-609 AND REO 601R53-41-2068.Jul 8, 2016 · N819AY · Cndair CL6002B19SDR DALA2016070905242Bulkhead · damagedLEFT SIDE AFT PRESSURE BULKHEAD LOWER SPLICE AT STRINGERS 26-27L FOUND ONLY TWO FASTENERS ON SPLICE. COMPLIED WITH PRI/ERA 5485614.Jul 8, 2016 · N916DN · Doug MD9030SDR DALA2016070905241Bulkhead · damagedFOUND ONLY TWO FASTENERS ON RIGHT SIDE OF AFT PRESSURE BULKHEAD LOWER SPLICE AT STRINGERS 26 - 27R. COMPLIED WITH PRI/ERA 5485614. (LP# 2573916)Jul 8, 2016 · N916DN · Doug MD9030SDR FDEA201607082316Cap · crackedLEFT STA 595 BULKHEAD TEE CAP VERTICLE LEG AT LONGERON 41L HAS 1.25 IN CRACK EXTENDING THROUGHOUT THE LOWER FASTENER HOLE. INSTALLED NEW T-CAP BETWEEN LONGERON 37L AND 44L IAW EA.Jul 8, 2016 · N381FE · Doug MD1010FSDR FDEA201607082315Cap · crackedLEFT STA 595, BULKHEAD TEE CAP VERTICAL LEG AT LONGERON 43L HAS 2" CRACKS EXTENDING THROUGHOUT BOTH FASTENER HOLES AND INTO THE RADIUS. INSTALLED NEW T-CAP FROM LONGERON 37L TO 44L IAW EA.Jul 8, 2016 · N381FE · Doug MD1010FSDR SIMA20160706004Bulkhead · corrodedRIGHT HAND COCKPIT BULKHEAD AT BS 280 HAS CORROSION ON THE AFT SIDE, FLOOR LEVEL. REPAIRED IAW EO CR-53MR-174Jul 6, 2016 · N519AE · Cndair CL6002C10SDR SIMA20160706005Bulkhead · corrodedLEFT HAND COCKPIT BULKHEAD AT BS 280 HAS CORROSION ON THE AFT SIDE, FLOOR LEVEL BETWEEN LBL 9 AND 18. REPAIRED IAW EO CR-53MR-174Jul 6, 2016 · N519AE · Cndair CL6002C10SDR AALA20160706004Bulkhead · crackedLEFT WHEEL WELL .040" THICK VERTICAL PRESSURE PANEL CRACKED AT BS 663, BETWEEN LBL 24.92 - 31.83. REPAIRED VERTICAL PRESSURE PANEL IAW EA 261626.Jul 6, 2016 · N940AN · Boeing 737823SDR AALA20160706003Bulkhead · crackedBULKHEAD CRACKED AT BS 663.75 APPROXIMATELY RBL 30. REPAIRED THE BULKHEAD IAW EA 261610.Jul 6, 2016 · N940AN · Boeing 737823SDR WVER0706201600004Stiffener · crackedBS 202.75 FWD SIDE OF BULKHEAD LBL 30 STIFFENER HAS A .15 INCH CRACK INDICATION AT THE UPPER EDGE OF FLANGE. FAILED NDT INSPECTION.Jul 6, 2016 · N923FJ · Cndair CL6002D24SDR WVER0706201603Stiffener · crackedBS 202.75 FWD SIDE OF BULKHEAD RBL 30 STIFFENER HAS A CRACK INDICATION .20 INCHES LONG AT THE UPPER EDGE OF FLANGE. FAILED NDT INSPECTION.Jul 6, 2016 · N923FJ · Cndair CL6002D24SDR REXA2016070501346Bulkhead · chafedAFT PRESSURE BULKHEAD FWD FACE CHAFED UNDER NUTPLATE BRACKET AT LBL 9. REPAIRED AFT PRESSURE BULKHEAD IAW REO 601R-53-61-5754.Jul 5, 2016 · N8694A · Cndair CL6002B19SDR SWAA2016071853985Pressure Panel · crackedRIGHT MAIN WHEEL WELL VERTICAL PRESSURE WEB CRACKED AT BS 663, BETWEEN RBL 35 TO RBL 41. REPAIRED WEB IAW SRM.Jul 5, 2016 · N775SW · Boeing 7377H4SDR SWAA2016071353745Bulkhead · crackedAFT PRESSURE BULKHEAD CRACKED AT BS 1016, STRINGER 6L. REPAIRED THE BULKHEAD IAW ACO.Jul 5, 2016 · N570WN · Boeing 7377CTSDR SWAA2016071253701Bulkhead Web · crackedMAIN WHEEL WELL VERTICAL PRESSURE BULKHEAD WEB CRACKED AT BS 663, RBL 35. REPAIRED BULKHEAD WEB IAW SRM.Jul 5, 2016 · N927WN · Boeing 7377H4SDR SWAA2016071853978Bulkhead · crackedLEFT ACFT BAY BULKHEAD UPPER FORWARD SIDE CHORD CRACKED AT BS 663, LBL 8. REPAIRED CHORD IAW EA.Jul 4, 2016 · N772SW · Boeing 7377H4SDR SWAA2016071253722Stiffener · crackedLEFT HORIZONTAL STIFFENER ON FORWARD BULKHEAD CRACKED AT BS 663, LBL 8. R & R STIFFENER IAW SRM.Jul 4, 2016 · N772SW · Boeing 7377H4SDR REXA2016070301276Bulkhead · crackedFS 202.75 BULKHEAD IS CRACKED AT THE PARKING BREAK PASS THROUGH. REPAIRED FS 202.75 BULKHEAD AT THE PARKING BRAKE PASS THROUGH IAW REO 601R-53-11-563, REV C.Jul 3, 2016 · N8918B · Cndair CL6002B19SDR VNAA2016070300004Bulkhead · crackedREAR PRESSURE BULKHEAD WEB AROUND THE LINTEL ATTACHMENT FITTING FAILED NON-DESTRUCTIVE TESTING. MAINTENANCE PERFORMED A MAJOR REPAIR TO PRESSURE BULKHEAD WEB FS621, LINTEL INSTALLATION AND PERFORMED CHECKS IAW THE AMM. THE ACFT CONTINUES HEAVY CHECK MAINTENAJul 3, 2016 · N209PS · Cndair CL6002B19SDR AALA201607299021Pressure Panel · crackedAIRCRAFT IN BASE MAINTENANCE: CENTER WING BOX PRESSURE PLATE CRACKED AT FRAME 43 AND -Y1650. REPLACED PRESSURE PLATE IAW SRM 51-42-11 AND DWG D53370500.Jul 2, 2016 · N710UW · Airbus A319112SDR AALA20160703001Bulkhead Web · crackedWHEEL WELL WEB HAS CRACKS AT BS 633, RBL 35 AND LBL 43. INSTALLED DOUBLER IAW EA 261790.Jul 2, 2016 · N919AN · Boeing 737823SDR SWAA2016080254432Bulkhead · crackedRIGHT BULKHEAD WEB AND INNER CHORD CRACKED AT BS 727, WL 200 LOWER FASTENER HOLE. REPAIRED BULKHEAD WEB IAW EA.Jul 1, 2016 · N774SW · Boeing 7377H4SDR CALA2016070100399Frame · corrodedAFT CARGO COMPT CORROSION AT FRAME LOCATED AT STA 1460 BETWEEN STR 29R TO STR 30. EVALUATED CORROSION ON FRAME LOCATED AT STA 1460 BETWEEN STRINGER 29R AND 30 AND FOUND OUT OF LIMITS IRW B757-300 SRM 53-00-07 RY 101 ALLOW. DAM 1. REPAIRED FRAM EIAW 5310-0688Jul 1, 2016 · N57863 · Boeing 75733NSDR ASOA2016063015161Bulkhead · crackedREAR PRESSURE BULKHEAD FORWARD FACE IS CRACKED ABOVE CARGO DOOR AFT TRACK AREA. REPAIRED IAW REO 601R-53-61-5772.Jun 30, 2016 · N686BR · Cndair CL6002B19SDR SWAA2016071954033Bulkhead Web · crackedMAIN WHEEL WELL VERTICAL PRESSURE WEB CRACKED AT BS 663, BETWEEN RBL 34 TO 41. REPAIRED THE BULKHEAD WEB IAW SRM.Jun 30, 2016 · N486WN · Boeing 7377H4SDR AALA20160701009Bulkhead Web · crackedDAMAGE ON INNER ALUMINUM BULKHEAD, APPROXIMATELY 4" FORWARD OF THE LT SIDE GEAR TRUNNION. DAMAGE RESULTED IN A 2.75" BY 4" LOSS OF MATERIAL TO THE INNER ALUMINUM WEB AND A 0.090" DENT IN THE STEEL WEB. REPAIRED PER SRM 53-05-00-001, FIG 36 AND EA 261750. AIRCRJun 29, 2016 · N969TW · Doug DC983SDR FDEA201606272156Tee Fitting · crackedRIGHT STA 595, BULKHEAD T-CAP FWD LEG JUST BELOW LONGERON 37R HAS A .5" CRACK EXTENDING FROM THE RADIUS TO THE FWD FASTENER HOLE. REPAIRED IAW EA 8-5310T0325916 SPLICED T-CORD AND INSTALLED NEW SECTION.Jun 27, 2016 · N381FE · Doug MD1010FSDR V0XD20160629141Bulkhead · corrodedFS280 RT BULKHEAD AFT WEB IS CORRODED. REPAIRED RT WEB BY CUTTING OUT DAMAGED SECTION. FABRICATED WEB AND BUTT STRAP AND INSTALLED IAW REO 670-53-11-594, DATED 27, APR 2011. WO 80413, WC 2096.Jun 27, 2016 · N159GJ · Cndair CL6002C10SDR AALA201607299037Pressure Deck · crackedAIRCRAFT IN BASE MAINTENANCE: CENTER LOWER FUSELAGE FORWARD CARGO COMPARTMENT PRESSURE DECK MEMBRANE PLATE HAS CRACK INDICATION AT FR 36 + 7" AND -Y1523. REPAIRED MEMBRANE PLATE IAW EA 261647.Jun 25, 2016 · N710UW · Airbus A319112SDR FDEA201606242133Cap · crackedLEFT STA 595 BULKHEAD TEE CAP VERTICAL LEG AT LONGERON 43L HAS A 2.00" CRACK EXTENDING THROUGH BOTH FASTENER HOLES AND INTO THE RADIUS. INSTALLED NEW TEE CAP FROM LONGERON 37L TO 44L PER EA.Jun 24, 2016 · N381FE · Doug MD1010FSDR DALA2016062504938Bulkhead · damagedREQUIRED REINFORCING ANGLES OF LT APB LOWER TEE CHORD CUT LINE REF CARD 5310-01449-01, STEP 9, LT APB LOWER TEE CHORD WAS REPAIRED IAW ETI 88-16-224, REV 1 AND ER/A 547797-14, REV ORIGINAL.Jun 24, 2016 · N900DE · Doug MD88SDR DALA2016062504937Bulkhead · damagedREQUIRED REINFORCING ANGLES OF RT APB LOWER TEE CHORD CUT LINE REF CARD 5310-01449-01, STEP 13. RT APB LOWER TEE CHORD WAS REPAIRED IAW ETI-88-16-224, REV 1 AND ER/A 547797-14, REV ORIGINAL.Jun 24, 2016 · N900DE · Doug MD88SDR CALA2016062700385Firewall · gougedFWD APU FIREWALL AT STA 1885.2 HAS SMALL GOUGE, CENTER LOWER AREA. REMOVED GOUGE, CUTOUT, ON FWD APU FIREWALL AT STA 1885.2 LOWER CENTER AREA, REF SRM 51-10-02, PERFORMED UT THICKNESS INSP. FOUND OUT OF LIMITS, REF SRM 53-80-08. FABRICATED AND AMP; INSTALLEJun 24, 2016 · N57863 · Boeing 75733NSDR FDEA201606232132Cap · crackedLEFT STA 595 BULKHEAD TEE CAP VERTICAL LEG AT LONGERON 41L HAS A 1.25" CRACK EXTENDING THROUGH THE LOWER FASTENER HOLE.Jun 23, 2016 · N381FE · Doug MD1010FSDR DALA2016062404902Splice · cutSPLICE IN APB, STA 1338, TEE CHORD BETWEEN L26L AND L27L WITH NO FASTENERS IN FORMER TAB, SPLICE CUT IS BETWEEN FORMER TAB AND L26L END FITTING. REPAIRED IAW PRI 548159-14, REV "0" AND "1" AND FINAL ER/A 548159-14, REV "A".Jun 23, 2016 · N958DL · Doug MD88SDR WVER201662336801Stiffener · crackedFS 202.75 BULKHEAD LBL 30, STIFFENER IS CRACKED AT TOP APPROXIMATELY 0.25" LONG. REPAIRED IAW SRM 53-11-10-2001-005-A01.Jun 23, 2016 · N368CA · Cndair CL6002C10SDR FDEA201606222117Bulkhead · crackedFOUND 15" LONG CRACK IN THE CAC AFT WALL LT SIDE ABOVE THE NR 2 PNUEMATIC DUCT FEED THROUGH DURING FUSELAGE PRESSURIZATION CHECK. RECEIVED FINAL EA 8-5300-T0326238; FUSELAGE, GENERAL-STA 1159 PRESSURE BULKHEAD REPAIR, LT SIDE, COMPLIED WITH.Jun 22, 2016 · N554FE · Doug MD1010FSDR AALA20160621012Pressure Panel · crackedAIRCRAFT WAS IN BASE MAINTENANCE. CENTER WING REAR SPAR VERTICAL PRESSURE WEB AT FUSELAGE STA 663.75 IS CRACKED BETWEEN LBL 40 AND LBL 45.6 AND BETWEEN RBL 40 AND RBL 45.6. REPAIRED WEB IAW EA 261275 AND EA 261273.Jun 21, 2016 · N937AN · Boeing 737823SDR SWAA2016070553433Bulkhead Web · crackedLEFT BULKHEAD WEB CRACKED AT BS 663.75. REPAIRED THE BULKHEAD WEB IAW EA.Jun 20, 2016 · N477WN · Boeing 7377H4SDR REXA2016061901186Bulkhead · gougedAFT PRESSURE BULKHEAD, FWD LOWER RT SIDE HAS SKIN GOUGED. REPAIRED APB LOWER SKIN AT RBL 36.50 IAW REO 601R-53-61-2155, REO 601R-53-61-1285 REF WIP STEP 10 LEAK CHECK GOOD IAW AMM 21-51-00-790-802, STEP 3A & 3B.Jun 19, 2016 · N8928A · Cndair CL6002B19SDR REXA2016061901185Bulkhead · gougedAFT PRESSURE BULKHEAD, FWD LOWER RT SIDE HAS SKIN GOUGED. REPAIRED APB FWD LOWER SKIN AT RBL 27.50 IAW REO 601R-53-61-2155, REO 601R-53-61-1285 REF WIP ITEM 10 LEAK CHECK GOOD IAW AMM 21-51-00-790-802, STEP 3A & 3B.Jun 19, 2016 · N8928A · Cndair CL6002B19SDR SWAA2016071954026Bulkhead Web · crackedMAIN WHEEL WELL VERTICAL PRESSURE WEB CRACKED AT BS 663, RBL 42. R & R THE BULKHEAD WEB IAW SRM & DWG.Jun 18, 2016 · N476WN · Boeing 7377H4SDR QXEA2016062800414Bulkhead · damagedRADOME BULKHEAD, PN 85310146 REQUIRES REPLACEMENT. REMOVED RADOME BULKHEAD, REF SRM 51-42-05-00-01. INSTALLED NEW BULKHEAD SKIN PN 85310146 AT FS X66.00 IAW SRM 51-42-05, SRM 51-42-45 AND DWG:85310011, REV AN. REMOVED ALL STIFFENERS FWD OF RADOME BULKHEAD RJun 18, 2016 · N423QX · Bombdr DHC8402SDR SWAA2016071853924Pressure Panel · crackedMAIN WHEEL WELL VERTICAL PRESSURE WEB CRACKED AT BS 663, RBL 42, CENTER WING BOX. REPAIRED WEB IAW SRM.Jun 17, 2016 · N477WN · Boeing 7377H4SDR SWAA2016071853923Pressure Panel · crackedMAIN WHEEL WELL VERTICAL PRESSURE WEB CRACKED AT BS 663, RBL 41, CENTER WING BOX. REPAIRED WEB IAW SRM.Jun 17, 2016 · N477WN · Boeing 7377H4
Back to JASC 5312