JASC 5312

Service difficulty reports · 20,047

Reports filed under 5312 · Fuselage Main, Bulkhead, newest first.

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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"

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SDR HALA9700151Blkhd Support · corrosionSBA - FROM C-CHECK NON-ROUTINE NR 18N00080. RIGHT STA 1260 STR 12 CANTED BULKHEAD SUPPORT ANGLE HAS LEVEL 2 CORROSION. FABRICATED AND INSTALLED THE SUPPORT ANGLE PER SRM 51-10-4 AND SRM 51-30-0. ACFT TT: 43,408 HOURS. TOTAL CYCLES: 70,298. (X)Aug 6, 1997 · N669HA · Doug DC951SDR RRXA97215Press Dome Web · crackedDURING A MAINTENANCE VISIT, FOUND PRESSURE DOME WEB CRACKED, AT STA 680 AND LONGERON 31 LEFT. *S/D* FABRICATED AND INSTALLED REPAIR ON PRESSURE WEB IAW DC-8 SRM 53-2-5, FIGURE 14.Aug 5, 1997 · N950R · Doug DC863SDR UPS97424011Bulkhead Chord · misdrilledINSPECTION TYPE-C, PRESS BULKHEAD BS 2360 DURING MOD OF BULKHEAD FOUND AT LOWER SIDE RT OF BL 0. CLOSE FASTENER SPACING (NOT IAW SRM) AT LOWER Y-CHORD AND WEB SIGMENTS. (NOT POSSIBLE TO MODIFY, PARTLY REPL OF CHORD NECESSARY). REPAIRED LOWER Y-CHORD AT RT OF Aug 4, 1997 · N673UP · Boeing 747123SDR TWAA9810107Bulkhead Angle · crackedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND FORWARD CARGO PRESSURE BULKHEAD ANGLE AFT OF STR 24L AT FS 608, HAD CRACK IN RADIUS. REPLACED WITH NEW PART PER SRM 51-01, AND TWA STD PRACTICES. TOTAL TIME: 70,084 HOURS. TOTAL CYCLES: 84,015. (X)Aug 4, 1997 · N977Z · Doug DC931SDR MWEA97710Bulkhead Skin · crackedDURING D-CHK, FOUND CRACK AFT PRESS BULK SKIN. MTC REPAIRED IAW SB53-137 PG 50.Aug 4, 1997 · N216ME · Doug DC932SDR MWEA97708Doubler · misrepairedDURING D-CHK, FOUND PREV REPAIR FS 980 FROM 26L TO 26R IMPROP. MTC REPAIRED IAW 53-03 FIG 2A.Aug 4, 1997 · N216ME · Doug DC932SDR MWEA97706Bulkhead Angle · crackedDURING D-CHK, FOUND CRACK IN ANGLE FIT BLW VENT DOOR JAMB AFT OF AFT PRESS BULK. MTC REPAIRED IAW SRM 53-05 FIG 40 AND 51-10-3.Aug 4, 1997 · N216ME · Doug DC932SDR MWEA97705Bulkhead Tee · nickedDURING D-CHK, FOUND NICKS AND GOUGES AFT OF AFT PRESS BULK TEE FIT. MTC REPAIRED IAW SRM 53-01 FIG 1.Aug 4, 1997 · N216ME · Doug DC932SDR 97ZZZX3809Bulkhead · crackedDURING PHASE 2 INSPECTION OF TAIL AREA, CRACKING AND STOP-DRILLING NOTICED ON STA 257.6 BULKHEAD AT HORIZONTAL SPARE ATTACH POINTS. STOP-DRILLING IS NOT AN APPROVED REPAIR PER BEECH SI 990, REV 2 PART II. A P/N 55-4030-5S REINFORCEMENT KIT NEEDED TO BE INSTAAug 4, 1997 · N788CF · Beech 58SDR AALA971410Bulkhead · corrodedT-ANGLE CORRODED AT SEAT TRACKS AND GALLEY SUPPORT ATTACH AREAS AFT PRESSURE BULKHEAD STATION 2007 AT FLOOR AREA. REMOVED AND REPLACED T-ANGLE IAW AARD 51-10-00-01. (M)Aug 3, 1997 · N1757A · Doug MD11SDR DL73K971606Bulkhead Web · crackedDURING REPETITIVE INSPECTIONS PER SI 3-69482-12, THE STA 178 BULKHEAD WAS FOUND CRACKED AT LBL 5.7, WL 200. A REPAIR HAD PREVIOUSLY BEEN INSTALLED ON THE RIGHT SIDE OF THE PRESSURE BULKHEAD PER B737-200 SRM 53-10-11. UPON REMOVAL OF THIS REPAIR DOUBLER, A NEAug 1, 1997 · N317DL · Boeing 737232SDR 9723849619Bulkhead · corrodedDURING M CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON NOSE LANDING GEAR WHEEL WELL AFT BULKHEAD LOWER T ANGLE FS 110, RBL 18. REPAIRED PER EA 96-112828.Jul 31, 1997 · N619NW · Doug DC932SDR P5CA9701517Bulkhead Fitting · crackedCRACK BS 1241 BULKHEAD AFT HOLE AT PASSENGER DECK FITTING, CRACK .0625 RUNNING DOWNWARD. REAMED HOLE TO 0.875 AS PER SB 53-2283, HOLE CHECKED CRACK FREE.Jul 30, 1997 · N853FT · Boeing 747122SDR 9715009926Bulkhead Angle · crackedDURING L-CHECK, FOUND A CRACK IN LOWER T-ANGLE ON THE NOSE LANDING GEAR WHEEL WELL FS 37 BULKHEAD. REPAIRED PER EA 99-151597.Jul 30, 1997 · N926NW · Doug DC932SDR SWAA970657Bulkhead · crackedDURING SCHEDULED D-CHECK, FOUND A CRACK INDICATION AT BS 178, AT WL 217 TO 217.5 AND AT 201.5 TO 202. REPAIRED BOTH PER TI-353-036 AND BOEING SRM.Jul 29, 1997 · N358SW · Boeing 7373H4SDR ABXA9701306Blkhd Fitting · crackedDURING C-CHECK, FOUND A RADIAL CRACK AND A BEND RADIUS CRACK IN THE LT UPPER CORNER OF THE AFT PRESSURE BULKHEAD DOOR JAMB. REPAIRED AFT PRESSURE BULKHEAD DOOR JAMB LT UPPER CORNER IAW DC-9 SB 53-137 AND ABX REA D953-20562-MR.Jul 28, 1997 · N901AX · Doug DC932SDR ABXA9701305Blkhd Fitting · crackedDURING C-CHECK, FOUND THE AFT PRESSURE BULKHEAD DOOR JAMB FITTING P/N 3917624-517, LT SIDE, CRACKED. REPLACED FITTING IAW DC-9 SRM 51-30-2 AND 51-30-1.Jul 28, 1997 · N901AX · Doug DC932SDR ABXA9701304Blkhd Fitting · crackedDURING C-CHECK, FOUND THE AFT PRESSURE BULKHEAD DOOR JAMB FITTING P/N 3917624-519, LT SIDE, CRACKED. REPLACED FITTING IAW DC-9 SRM 51-30-2 AND 51-30-5.Jul 28, 1997 · N901AX · Doug DC932SDR ABXA9701309Press Bulkhead · corrodedDURING C-CHECK, FOUND THE PRESSURE BULKHEAD AT FS 604 IN FORWARD LOWER CARGO COMPARTMENT BEHIND THE AUX FUEL TANK BULGED AND CORRODED IN 4 PLACES WITH THE RIVET HEADS SHEARED OFF, AT THE TOP OF THE BULKHEAD WING STA'S X 4 LT AND X 24 LT AND AT THE BOTTOM OF THJul 26, 1997 · N901AX · Doug DC932SDR ABXA9701307Blkhd Fitting · crackedDURING C-CHECK, FOUND A BEND RADIUS CRACK IN THE AFT PRESSURE BULKHEAD DOOR JAMB UPPER RT CORNER. *S/D* REPAIRED IAW DC9 S/B 53-137 AND ABX REA D953-20562MR.Jul 26, 1997 · N901AX · Doug DC932SDR TWAA9805802Bulkhead · corrodedMCI - DURING OP 16 MAINTENANCE, FOUND AFT PRESS BULKHEAD CORRODED AT STATION 996, AFT OF LONGERON 29R, FWDSIDE OF BULKHEAD. REMOVED CORROSION PER SRM 51-10-3 AND REPAIRED BULKHEAD PER SRM 53-03 FIG 9 SHT 2, AND SRM 51-60-0 PAGE 15 ITEM E. (M)Jul 25, 1997 · N924L · Doug DC932SDR TWAA9805705Bulkhead · corrodedMCI - DURING OP 16 MAINTENANCE CHECK, IN TAIL COMPARTMENT FOUND THE LOWER AFT SIDE OF PRESS BULKHEAD HAD BULGE AND CORROSION ON A Y-CHORD RBL, 4 INCHES. REMOVED CORROSION PER SRM 51-10-3, REPAIRED BULKHEAD PER SRM 53-03, FIG 9 SHT 2, AND SRM 51-00-0 PAGE 15 IJul 25, 1997 · N924L · Doug DC932SDR CALA9701173Bulkhead · crackedINSPECTION FOUND A .25 AND .375 INCH CRACK AT FASTENER HOLES IN NLG WHEEL WELL RIGHT SIDEWALL BULKHEAD STA 286. THE CRACKS WERE STOP DRILLED, A DOUBLER AND STRAP REPAIR WERE FABRICATED AND INSTALLED IAW BOEING SERVICE BULLETIN 727-53-0145.Jul 25, 1997 · N45793 · Boeing 727232SDR AALA971332Bulkhead Angle · corrodedTUL - FOUND CORROSION ON THE TOP OF THE PRESSURE BULKHEAD T-ANGLE AT STATION 2006 8 INCHES INBOARD OF THE RIGHT FUSELAGE. REMOVED CORROSION FROM T-ANGLE PER SRM 57-00-01 AND INSTALLED REPAIR PER ESO4100D DATED 7-24-97. (M)Jul 25, 1997 · N1760A · Doug MD11SDR CALA9701192Bulkhead T-Cap · corrodedINSPECTION FOUND FORWARD PRESSURE BULKHEAD T-CAP CORRODED JUST AFT OF EXT POWER BOX. THE CORRODED SECTION OF T-CAP WAS REMOVED AND REPLACED IAW ECRA 5310-03544.Jul 23, 1997 · N541NY · Doug DC932SDR MWEA97666Doubler · tornDURING D-CHECK, FOUND THE AFT PRESSURE BULKHEAD DOOR JAMB AFT ATTACHMENT WEB HAS TORN OFF SECTION OF METAL AT STATION Z 520 ON RT TOP AFT CORNER. MTC REPAIRED IAW SVC ORD 0186/SBT.Jul 21, 1997 · N216ME · Doug DC932SDR C2XA97CL066Fire Wall · crackedCLE - DURING A SCHEDULED INSPECTION, THE APU FIRE WALL WAS FOUND CRACKED APPROXIMATELY 8 INCHES ACROSS THE CENTER LINE OF THE WALL. MAINTENANCE ACCOMPLISHED A TEMPORARY REPAIR IAW CONTINENTAL EXPRESS EC5310-01081. AIRCRAFT RELEASED FOR SERVICE. NOTE: PERMAJul 21, 1997 · N14931 · Emb EMB145ERSDR C2XA97CL065Firewall · crackedCLE - DURING A SCHEDULED INSPECTION THE APU FIREWALL WAS FOUND TO BE CRACKED APPROXIMATELY 20 INCHES ACROSS THE CENTER LINE OF THE WALL. MAINTENANCE ACCOMPLISHED A TEMPORARY REPAIR IAW CONT EXPRESS EC5310-01082. AIRCRAFT RELEASED FOR SERVICE. (M)Jul 21, 1997 · N13929 · Emb EMB145ERSDR 97ZZZM877Press Bulkhead · oil cannedDURING C-CHECK, FOUND AFT PRESSURE BULKHEAD STR BS 1016 HAS OIL CANNING AT THE ONE O'OCLOCK PIE SECTION. FABRICATED CHANNEL AND STRAP FROM 2024-0 15.75 INCH BY 3.25 INCH AND 2024 T3 .032 16.5 INCH BY 2 INCH IAW B737 SRM 53-10-4. INSTALLED IAW B737 SRM 53-10-Jul 21, 1997 · Boeing 7372P6SDR CALA9701120Bulkhead Web · crackedINSPECTION FOUND A 17 INCH CRACK ON PRESSURE BULKHEAD WEB AT STA 1521 BETWEEN Z= 74 AND 80. FILLER, DOUBLER, AND A FINGER DOUBLER WERE FABRICATED AND INSTALLED IAW ECRA 5330-02559 AND SRM 53-20-00, FIGURE 6.Jul 20, 1997 · N76073 · Doug DC1030SDR C2XA97IA215Blkhd Stiffener · corrodedIAH - DURING C-CHECK INSPECTION, THE LOWER VERTICAL STIFFENER ON THE AFT PRESSURE BULKHEAD WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED STIFFENER, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Jul 19, 1997 · N34817 · Aerosp ATR42320SDR ABXA9701271Bulkhead Web · crackedDURING C-CHECK, FOUND THE RT SIDE BULKHEAD WEB AT FS 37 CRACKED AT A RIVET. *S/D* REPAIRED WEB IAW DC9 SRM 53-01.Jul 19, 1997 · N908AX · Doug DC931SDR CALA9701155Bulkhead Tee · crackedAFT PRESSURE BULKHEAD T-CAP CRACKED STATION 996 LONG 1 TO 6 LEFT 20 RIGHT SIDE 19. REPLACED DAMAGED T-CAP SECTION PER EC/RA 5310-03531.Jul 17, 1997 · N17533 · Doug DC932SDR AALA971266Bulkhead Angle · corrodedTUL - T-ANGLE CORRODED AT GALLEY SUPPORT NR 4 ATTACH POINT AT AFT PRESSURE BULKHEAD. REMOVED CORRODED SECTION AND INSTALLED 12 INCH LONG DOUBLER ON T-ANGLE AT PRESSURE BULKHEAD PER ESO 41000 DATED 7-3-97. TST: 16,333:37 HOURS. CYCLES, 2,775. (X)Jul 11, 1997 · N1761R · Doug MD11SDR DL72S971444Blkhd Stiffener · crackedA CRACK WAS FOUND IN THE VERTICAL STIFFENER AT RBL 36.83 ON THE FORWARD SIDE OF THE BS 1183 BULKHEAD. THE CRACK IS APPROX .5 INCH LONG AND IS LOCATED AT APPROX WL 249 IN THE INB'D RADIUS OF THE AFT CHORD. THIS AREA IS ADDRESSED IN EO 4-59821-3, WHICH INCORPOJul 10, 1997 · N468DA · Boeing 727232SDR CA970722016Bulkhead · worn(CAN) DURING THE INSPECTION ON REMOVAL OF THE FLOOR INSPECTION COVERS, IT WAS DISCOVERED THAT THE RUDDER AND ELEVATOR CABLES HAD BEEN RIDING ON AND CUTTING THE BULKHEADS BELOW THE FLOOR FROM STA 8.12 TO STA 124.00. CABLES REMOVED AND INSPECTED AND FOUND TO BEJul 10, 1997 · Cessna 172LSDR MWEA97625Bulkhead Angle · crackedDURING C-CHECK, FOUND CRACK ON LOWER SIDE OF APB FORWARD SIDE HORIZONTAL STIFFENER GL JUST INSIDE OF STA 996 FRAME. MTC REPAIRED IAW DAC DRAWING J060110.Jul 9, 1997 · N301ME · Doug DC932SDR MWEA97624Bulkhead Angle · crackedDURING C-CHECK, FOUND CRACK ON APB FORWARD SIDE HORIZONTAL STIFFENER 3L ANGLE JUST INBOARD OF STA 996 FRAME. MTC REPAIRED IAW DAC DRAWING J060110.Jul 9, 1997 · N301ME · Doug DC932SDR CKSA97387Bulkhead Ring · corrodedDURING ACCOMPLISHMENT OF AD 93-20-03 FOUND LEVEL 2 CORROSION: AFT PRESSURE BLKHD STIFFENER RING CORRODED FROM BELOW FLOOR WL200 TO OUTER RING RT SIDE. REPAIRED AFT PRESSURE BLKHD STIFFENER RING BELOW FLOOR WL200 IAW L1011 SRM 53-11-00 FIG 809. NON-ROUTINE 10Jul 9, 1997 · N109CK · Lkheed 1011385115SDR CKSA97370Bulkhead Frame · corrodedDURING ACCOMPLISHMENT OF AD 93-20-03 FOUND LEVEL 2 CORROSION: AFT PRESSURE BULKHEAD, FS 1809 RT SIDE, FRAME CORRODED BETWEEN STRINGERS R-21 AND R-22 AREAS. REPAIRED AFT PRESSURE BULKHEAD, FS 1809 RT SIDE, FRAME BETWEEN STR R-21 AND R-22 IAW L1011 SRM 53-11-0Jul 9, 1997 · N109CK · Lkheed 1011385115SDR CKSA97360Bulkhead · puncturedDURING ROUTINE C CHECK INSPECTION FOUND: PUNCTURE IN FWD FACE OF 940 BULKHEAD, RIGHT BUTTLINE 24 APPROX 36 ABOVE C-1 PIT FLOOR. REPAIRED 940 BULKHEAD OF PUNCTURE IAW LOCKHEED L1011 SRM REF NBR 51-50-07. NON-ROUTINE TASK CARD NUMBER 106843.Jul 9, 1997 · N109CK · Lkheed 1011385115SDR CKSA97359Bulkhead Door · puncturedDURING ROUTINE C CHECK INSPECTION FOUND: PUNCTURE IN FWD FACE OF ACCESS DOOR FROM C-1 PIT TO MESC, STA 940, LOWER OUTBOARD AREA. REPAIRED FWD FACE OF ACCESS DOOR OF 940 BULKHEAD FROM PUNCTURE IAW LOCKHEED L1011 SRM REF NBR 51-50-07. NON-ROUTINE TASK CARD NUJul 9, 1997 · N109CK · Lkheed 1011385115SDR CKSA97358Bulkhead · puncturedDURING ROUTINE C CHECK INSPECTION FOUND: PUNCTURE IN FORWARD FACE OF 940 BULKHEAD RIGHT BUTTLINE 10 AT C-1 PIT FLOOR. REPAIRED 940 BULKHEAD OF PUNCTURE IAW LOCKHEED L1011 SRM REF NBR 51-50-07. NON-ROUTINE TASK CARD NUMBER 106841.Jul 9, 1997 · N109CK · Lkheed 1011385115SDR CKSA97357Bulkhead · puncturedDURING ROUTINE C CHECK INSPECTION FOUND: PUNCTURE IN FWD FACE OF 940 BULKHEAD LEFT BUTTLINE 36 10 ABOVE FLOOR LINE OF C-1 PIT. REPAIRED 940 BULKHEAD OF PUNCTURE IAW LOCKHEED L1011 SRM REF NBR 51-50-07. NON-ROUTINE TASK CARD NUMBER 106840.Jul 9, 1997 · N109CK · Lkheed 1011385115SDR CKSA97356Bulkhead · corrodedDURING ROUTINE C CHECK INSPECTION FOUND LEVEL 2 CORROSION: CORROSION AND PUNCTURE IN FWD FACE OF BULKHEAD 940 LEFT BUTTLINE 60 AT C-1 PIT FLOOR. REPAIRED 940 BULKHEAD OF CORROSION AND PUNCTURE IAW LOCKHEED L1011 SRM REF NBR 51-50-07. NON-ROUTINE TASK CARD NJul 9, 1997 · N109CK · Lkheed 1011385115SDR P5CA9701366Bulkhead · crackedFORWARD CARGO BS 400 LBL 90 BULKHEAD CRACKED NOSE TUNNEL BS 400 RT SIDEWALL AREA BULKHEAD WEB CRACKED AT RBL 90 APPX. REPAIRED CUTOUT PER SB 747-53-2095.Jul 8, 1997 · N854FT · Boeing 747122SDR P5CA9701318Bulkhead Chord · crackedCRACK FOUND APPX 1.25 INCH LONG ALONG RADIUS FORWARD CARGO COMPARTMENT, BS 1000 BULKHEAD LOWER CHORD BETWEEN S-46R TO S-47R, STOP DRILLED AS PER SB 747-53-2316.Jul 8, 1997 · N854FT · Boeing 747122SDR P5CA9701314Buklhead Chord · crackedCRACK FOUND APPX 1.25 INCH LONG ALONG RADIUS, FORWARD CARGO COMPARTMENT BS 1000 BULKHEAD LOWER CHORD BETWEEN S-46L AND S-47L. STOP DRILLED AS PER SB 747-53-2316.Jul 8, 1997 · N854FT · Boeing 747122SDR P5CA9701312Bulkhead Chord · crackedCRACK FOUND APPX 1.25 INCH LONG ALONG RADIUS, FORWARD CARGO COMPARTMENT, BS 1000 BULKHEAD LOWER CHORD BETWEEN S-46L AND S-47L. STOP DRILLED PER SB 747-53-2316.Jul 8, 1997 · N854FT · Boeing 747122SDR 97ZZZX3350Bulkhead · crackedTHE CRACK WAS FOUND IN THE AFT BULKHEAD VERTICAL BEAM LBL 26.83 WL 257.0. THE CRACK IS ATTRIBUTED TO PRESSURIZATION CYCLES. RECOMMENDATION: THE SB 53-0182 RECOMMENDED TO INSTALL THE PREVENTIVE MODIFICATION AT OR BEFORE 60,000 CYCLES. SUBMITTER RECOMMENDED Jul 3, 1997 · N259US · Boeing 727251
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