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.

SDR 97ZZZX3349Bulkhead · beam crackedTHE CRACK WAS FOUND IN THE AFT BULKHEAD VERTICAL BEAM LBL 36.83 (LT/RT). THE SUSPECT CAUSE WAS THE RESULT OF FATIGUE THAT WAS CAUSED BY PRESSURIZED FLIGHTS. SUBMITTER RECOMMENDATION: THERE SHOULD BE A LIMITED TIME TO INSTALL THE PREVENTIVE MODIFICATION PER Jul 3, 1997 · N259US · Boeing 727251SDR 97ZZZX3348Bulkhead · beam crackedTHE CRACK WAS FOUND IN THE AFT BULKHEAD VERTICAL BEAM LBL 36.83 (LT/RT). THE SUSPECT CAUSE WAS THE RESULT OF FATIGUE THAT WAS CAUSED BY PRESSURIZED FLIGHTS. SUBMITTER RECOMMENDATION: THERE SHOULD BE A LIMITED TIME TO INSTALL THE PREVENTIVE MODIFICATION PER Jul 3, 1997 · N259US · Boeing 727251SDR ABXA9701180Bulkhead · corrodedDURING C-CHECK, FOUND LEFT MLG WHEEL WELL UPPER PRESSURE BULKHEAD LOWER SURFACE CORRODED BEYOND LIMITS. REPAIRED IAW ABX REA D95320038MR.Jun 30, 1997 · N931AX · Doug DC933FSDR QXEA9700363Bulkhead Beam · crackedPDX - CRACK IN LEFT SIDE OF BEAM NR V IN RADIUS BETWEEN LAST 3 RIVETS ON FORWARD SIDE OF FRONT PRESSURE BULKHEAD. REPAIRED LEFT HAND HORIZIONTAL BEAM NR V AS PER E.A. 4-53-183.Jun 29, 1997 · N493US · Fokker F28MK4000SDR SWAA970595Bulkhead · dentedDURING SCHEDULED C4 CHECK, FOUND PRESSURE BULKHEAD BS 178 DENTED FLOOR LEVEL. REPAIRED PER BOEING SRM.Jun 28, 1997 · N313SW · Boeing 7373H4SDR SWAA970588Bulkhead · dentedDURING SCHEDULED D-CHECK, FOUND PRESSURE BULKHEAD BS 178 DENTED AT RBL 33, WL 166. REPAIRED PER BOEING SRM.Jun 26, 1997 · N684WN · Boeing 7373T0SDR CALA9701144Bulkhead Frame · corrodedCORROSION ON FRAME 1016 SURFACE STG 29L AND 29R AT BOTTOM OF AFT PRESSURE BULKHEAD. REMOVED DAMAGED AREA. INSTALLED PART IN ACCORDANCE WITH SRM 51-10-1 AND DRWG DHCSK 248-024.Jun 26, 1997 · N10248 · Boeing 737219SDR P5CA9701237Bulkhead Chord · corrodedLEVEL 1 CORROSION FWD CARGO STA 1000 LOWER LOBE BULKHEAD LOWER CHORD S43R TO S44R. REMOVED CORROSION PER BOEING SRM 51-10-01 AND TREATED PER 51-10-02.Jun 25, 1997 · N854FT · Boeing 747122SDR P5CA9701236Bulkhead Chord · corrodedLEVEL 1 CORROSION FWD CARGO STA 1000 BULKHEAD LOWER CHORD S43L TO S44L. REMOVED CORROSION PER BOEING SRM 51-10-01 AND TREATED PER 51-10-02.Jun 25, 1997 · N854FT · Boeing 747122SDR P5CA9701235Bulkhead Chord · corrodedLEVEL 1 CORROSION FWD CARGO STA 1000 BULKHEAD LOWER CHORD S45L TO S46L. REMOVED CORROSION PER BOEING SRM 51-10-01 AND TREATED PER 51-10-02.Jun 25, 1997 · N854FT · Boeing 747122SDR P5CA9701234Bulkhead Chord · corrodedLEVEL 1 CORROSION FWD CARGO STA 1000 BULKHEAD LOWER CHORD S46L TO S47L. REMOVED CORROSION PER BOEING SRM 51-10-01 AND TREATED PER 51-10-02.Jun 25, 1997 · N854FT · Boeing 747122SDR P5CA9701233Bulkhead Chord · corrodedLEVEL 1 CORROSION FWD CARGO STA 1000 BULKHEAD LOWER CHORD S47L TO S47R. REMOVED CORROSION PER BOEING SRM 51-10-01 AND TREATED PER 51-10-02.Jun 25, 1997 · N854FT · Boeing 747122SDR P5CA9701232Bulkhead Chord · corrodedLEVEL 1 CORROSION FWD CARGO STA 1000 BULKHEAD LOWER CHORD S46R TO S47R. REMOVED CORROSION PER BOEING SRM 51-10-01 AND TREATED PER 51-10-02.Jun 25, 1997 · N854FT · Boeing 747122SDR P5CA9701231Bulkhead Chord · corrodedLEVEL 1 CORROSION FWD CARGO STA 1000 BULKHEAD LOWER CHORD S45R TO S46R. REMOVED CORROSION PER BOEING SRM 51-10-01 AND TREATED PER 51-10-02.Jun 25, 1997 · N854FT · Boeing 747122SDR P5CA9701230Bulkhead Chord · corrodedLEVEL 1 CORROSION FWD CARGO BS 1000 BULKHEAD LOWER CHORD S44R TO S45R. REMOVED CORROSION PER BOEING SRM 51-10-01 AND TREATED PER 51-10-02.Jun 25, 1997 · N854FT · Boeing 747122SDR AU970954Bulkhead · cracked(AUS) FORWARD PRESSURE BULKHEAD WEB FORWARD FACE CRACKED IN THE FOLLOWING AREAS:- 1. THREE CRACKS LOCATED AT RBL 5.7 UNDER RADAR SCANNING SUPPORT BRACKETS - CRACK LENGTHS 15MM (0.59IN), 20MM (0.787IN) AND 24MM (0.944IN) 2. ONE CRACK LOCATED AT LBL 5.7 UNDER Jun 25, 1997 · Boeing 73733ASDR ABXA9701171Bulkhead Radial · crackedDURING C-CHECK, FOUND AFT PRESSURE BULKHEAD RADIAL STIFFENER AT THE 5 O'CLOCK POSITION CRACKED. REPLACED RADIAL IAW DC-9 SRM 51-30-2.Jun 25, 1997 · N931AX · Doug DC933FSDR MWEA97586Bulkhead · gougedDURING C-CHECK, STA 989.407 7 O'CLOCK POSITION TAIL COMPART BULKHEAD GOUGED. MAINT REPAIRED IAW SRM 53-01 FIG 2 SHT 4.Jun 24, 1997 · N800ME · Doug DC914SDR 9713069987Bulkhead Web · corrodedDURING M-CHECK, FOUND CORROSION ON AFT PRESSURE BULKHEAD SUPPORT WEB FS 966. REPAIRED PER EA 99-112992.Jun 24, 1997 · N987US · Doug DC932SDR VJ970264Bulkhead Tee · corrodedDURING A SCHEDULED MAINTENANCE INSPECTION, CORROSION WAS FOUND ON AFT SIDE OF FRAME AND ON PRESSURE BULKHEAD AT STA 996 AND STR 27L IN AFT BAGGAGE AREA. CLEANED CORROSION, REMOVED AND REPLACED TEE CHORD AND REPAIRED PRESSURE BULKHEAD IAW WITH SRM 53-05, FIG Jun 20, 1997 · N916VV · Doug DC932SDR DLL10971227Bulkhead Cap · crackA CRACK WAS FOUND AT FS 449 JUST INBOARD OF LBL 72.5. THE CRACK WAS LOCATED ON THE VERTICAL LEG OF THE 449 BULKHEAD CAP AND EXTENDED DOWN TO THE UPPER FASTENER HOLE. THE CRACK WAS ROUTED OUT AND REPAIRED WITH AN ANGLE. THIS REPAIR WAS APPROVED BY FAA/DER FOJun 20, 1997 · N727DA · Lkheed 10113851SDR CALA9701268Bulkhead · crackedINSPECTION FOUND A 2.5 INCH CRACK IN RT OUTBOARD END OF LOWER BULKHEAD T-CHORD AT STA 1156. THE CRACKED SECTION OF CHORD WAS CUT OUT, A NEW CHORD AND SPLICES WERE FABRICATED AND INSTALLED IAW DAC DRAWING SR10530073 AND SRM 51-21-0.Jun 20, 1997 · N68043 · Doug DC1010SDR ZZDA5311997Bulkhead · cannedDURING C-CHECK, FOUND AFT PRESSURE BULKHEAD AT BS 1016 HAS OIL CANNING AT THE 2 O'CLOCK RADIUS PIE SECTION. FABRICATED CHANNEL AND STRAP FROM 2024-0 .040 INCH, 16.8750 INCHES BY 3.25 INCHES, 2 INCHES BY 15.25 INCHES IAW B 737 SRM 53-10-4. INSTALLED IAW B 737Jun 19, 1997 · Boeing 7372P6SDR AALA971111Bulkhead Beam · crackedTUL - RIGHT AFT PRESSURE BULKHEAD CENTER SUPPORT BEAM CRACKED AT THE FASTENER HOLES 28 INCHES ABOVE THE FLOOR. STOP DRILLED THE CRACKS AND INSTALLED DOUBLER KIT PER SB 727-53-0192, IT NR 65C34406-13. TST: 55,431 HOURS. CYCLES, 34,330. (X)Jun 19, 1997 · N868AA · Boeing 727223SDR 97ZZZM876Press Blkhd · oil cannedDURING C-CHECK, FOUND AFT PRESSURE BULKHEAD AT BS 1018 HAS OIL CANNING AT THE 2 O'CLOCK RADIUS PIE SECTION. FABRICATED CHANNEL ANS STRAP FROM 2024-0 .040 16.875 INCH BY 3.75 INCH 2 INCH BY 15.25 INCH IAW B737 SRM 53-10-4. INSTALLED IAW B737 SRM 53-10-4 AND MJun 19, 1997 · Boeing 7372P6SDR ABXA9701390Bulkhead Jamb · crackedWHILE COMPLYING WITH VISUAL INSPECTION OF THE AFT PRESSURE BULKHEAD IAW AD 85-01-02 PER SB 53-137, FOUND THE BULKHEAD DOOR JAMB CRACKED JUST BELOW THE UPPER LEFT CORNER OF DOOR CUTOUT. REPLACED CRACKED DOUBLER IAW DC-9 SRM CHAPTER 51-30-5.Jun 18, 1997 · N962AX · Doug DC941SDR QXEA9700377Bulkhead Web · crackedPDX - REAR PRESSURE BULKHEAD BELOW CABIN FLOOR IN CARGO BAY, HAS A CRACK IN THE BULKHEAD WEB UNDER LOWER FLOOR OF HORIZIONTAL BEAM III 6 OUTBOARD OF BL 425R. LENGTH OF CRACK APPROX 1.75 . REPAIRED CRACK ON REAR PRESSURE BULKHEAD ON BEAM III PER FOKKER SRM 53Jun 17, 1997 · N493US · Fokker F28MK4000SDR QXEA9700375Bulkhead Beam · crackedPDX - REAR PRESSURE BULKHEAD BEAM II RIGHT END IS CRACKED IN RADIUS OF UPPER ATTACH FLANGE. REPAIRED HORIZONTAL BEAM II PER FOKKER SRM 53-02-18 FIGURE 13 SECTION B-B.Jun 17, 1997 · N493US · Fokker F28MK4000SDR MWEA97531Bulkhead Ftg · corrodedDURING D-CHECK, FOUND MODERATE CORROSION ON LONGERON END FITTING 23 LT STA 996. MTC REMOVED AND REPLACED END FITTING IAW SRM 51-30-2 AND 51-30-5.Jun 17, 1997 · N216ME · Doug DC932SDR MWEA97530Bulkhead Ftg · corrosionDURING D-CHECK, FOUND CORROSION ON AFT SIDE OF AFT PRESURE BULKHEAD LONGERON 24R AND 24L FITTINGS AT FS 996. MTC REMOVED AND REPLACED FITTING IAW SRM 51-30-2 AND 51-30-5.Jun 17, 1997 · N216ME · Doug DC932SDR MWEA97529Bulkhead Ftg · corrosionDURING D-CHECK, FOUND CORROSION ON AFT SIDE OF AFT PRESSURE BULKHEAD LONG 23L AT STATION 996 LONG END FITTING. MTC REMOVED AND REPLACED END FITTING IAW SRM 51-30-2 AND 51-30-5.Jun 17, 1997 · N216ME · Doug DC932SDR ABXA9701381Bulkhead Clip · crackedWHILE COMPLYING WITH 'D' INSPECTION, FOUND THE AFT PRESSURE BULKHEAD FORWARD LATERAL STIFFENER END CLIP CRACKED AT LONGERON 9 LEFT. REMOVED AND REPLACED CLIP IAW DC-9 SRM CHAPTERS 51-30-1 AND 51-30-5.Jun 17, 1997 · N962AX · Doug DC941SDR ABXA9701379Bulkhead Clip · crackedWHILE COMPLYING WITH 'D' INSPECTION, FOUND THE AFT PRESSURE BULKHEAD LATERAL STIFFENER END CLIP CRACKED AT LONGERON 9 RIGHT. REMOVED AND REPLACED END CLIP IAW DC-9 SRM CHAPTERS 51-30-1.Jun 16, 1997 · N962AX · Doug DC941SDR ABXA9701378Bulkhead Clip · crackedWHILE COMPLYING WITH 'D' INSPECTION, FOUND THE AFT PRESSURE BULKHEAD LATERAL STIFFENER CRACKED AT LONGERON 7R. REMOVED AND REPLACED END CLIP IAW DC-9 SRM CHAPTERS 51-30-1 AND 51-30-5.Jun 16, 1997 · N962AX · Doug DC941SDR SWAA970553Bulkhead Skin · crackedDURING SCHEDULED SERVICE CHECK, FOUND BULKHEAD BS 178 SKIN CRACKED AT WL 220, BL 13. REPAIRED PER BOEING SRM.Jun 15, 1997 · N52SW · Boeing 7372H4SDR 9711659936Bulkhead · crackedDURING LINE CHECK, FOUND CRACK IN NOSE LANDING GEAR WHEEL WELL HORIZONTAL PRESSURE BULKHEAD AT FS 105. REPAIRED PER EA 99-122993.Jun 15, 1997 · N1799U · Doug DC931SDR QXEA9700362Bulkhead Beam · crackedPDX - AFT SIDE OF FORWARD PRESSURE BULKHEAD IS CRACKED AT HORIZONTAL BEAM VIII BL325L. STOP DRILLED CRACK, DRILLED UP REPAIR AND INSTALLED AD RIVETS IN NEW HOLES AND INSTALLED NEW DOUBLER PER SRM 53-02-18.Jun 14, 1997 · N493US · Fokker F28MK4000SDR 9712189156Blkhd Stiffener · crackedDURING L-CHECK, FOUND CRACK IN AFT PRESSURE BULKHEAD RADIAL STIFFENER 14R. REPAIRED PER EA 91-112956.Jun 13, 1997 · N8915E · Doug DC914SDR TWAA9804701Press Web · crackedMCI - DURING OP16 MAINTENANCE CHECK, FOUND 4 HOLES AND DENTS IN FWD BLKHD OF NOSE WHEEL WELL, 12 TO 14 INCHES RBL AND APPROX 27 TO 30 INCHES UP FROM FUSELAGE SKIN. STOP DRILLED CRACKS, NDT OK. INSTALLED DOUBLER SKIN PER TYPICAL WEB REPAIR SRM 51-70-13. (M)Jun 12, 1997 · N607TW · Boeing 767231SDR ABXA9701377Bulkhead Skin · crackedWHILE COMPLYING WITH 'D' INSPECTION, FOUND THE AFT PRESSURE BULKHEAD DOOR JAMB CRACKED ON RIGHT SIDE. REPAIRED DOOR JAMB IAW DC-9 SRM CHAPTER 53-05.Jun 12, 1997 · N962AX · Doug DC941SDR AALA971078Bulkhead 'T' · corrodedTUL - FOUND LIGHT CORROSION AT L48 AND PRESS BULKHEAD 'T' CAP. REMOVED LIGHT CORROSION FROM T-CAP AND CUT OUT DAMAGED SKIN PER SRM 51-21-01 PAGE 29. TREATED, PRIMED, PAINTED AND PRESS BULKHEAD 'T' CAP, RESEALED WITH PROSEAL C-24 SEALER, FUSELAGE SKIN REPAIREJun 12, 1997 · N128AA · Doug DC1010SDR SWAA970533Bulkhead · crackedDURING SCHEDULED C-CHECK, FOUND A 7 INCH CRACK AT BS 178 BULKHEAD. REPAIRED PER BOEING SRM.Jun 11, 1997 · N52SW · Boeing 7372H4SDR AU970754Bulkhead · cracked(AUS) PRESSURE BULKHEAD WEB AT BS 178 CRACKED IN FIVE PLACES ADJACENT TO WEATHER RADAR SUPPORT BRACKET ATTACHMENTSJun 11, 1997 · Boeing 737376SDR AU970717Chord · cracked(AUS) FORWARD PRESSURE BULKHEAD LH SIDE CHORD CRACKED IN RADIUS AT WL 207 - CRACK LENGTH 40MM (1.574IN) AND WL 195 - CRACK LENGTH 51.5MM (2.027IN) - FOUND DURING INSPECTION IAW ER B73-53-10-39Jun 10, 1997 · Boeing 737377SDR AU970646Bulkhead · cracked(AUS) FUSELAGE BULKHEAD LH AND RH LOWER AFT DOOR POSTS PNO 0512187-1 LH AND PNO 0512187-2 RH CRACKED IN AREA INDICATED BY SERVICE BULLETINJun 10, 1997 · Cessna 172PSDR ABXA9701370Bulkhead Clip · crackedWHILE COMPLYING WITH 'D' INSPECTION, FOUND THE AFT PRESSURE BULKHEAD FORWARD LATERAL STIFFENER END CLIP CRACKED AT LONGERON 12 RIGHT. REPLACED END CLIP IAW DC-9 SRM CHAPTERS 51-30-1 AND 51-30-5.Jun 10, 1997 · N962AX · Doug DC941SDR ABXA9701369Bulkhead Clip · crackedWHILE COMPLYING WITH 'D' INSPECTION, FOUND THE AFT PRESSURE BULKHEAD FORWARD LATERAL STIFFENER END CLIP CRACKED AT LONGERON 14 RIGHT. REMOVED AND REPLACED END CLIP IAW DC-9 SRM CHAPTERS 51-30-1 AND 51-30-5.Jun 10, 1997 · N962AX · Doug DC941SDR ABXA9701368Bulkhead Clip · crackedWHILE COMPLYING WITH 'D' INSPECTION, FOUND THE AFT PRESSURE BULKHEAD FORWARD LATERAL STIFFENER END CLIP CRACKED AT LONGERON 14 LEFT. REMOVED AND REPLACED END CLIP IAW DC-9 SRM CHAPTERS 51-30-1 AND 51-30-5.Jun 10, 1997 · N962AX · Doug DC941SDR ABXA9701367Bulkhead Clip · crackedWHILE COMPLYING WITH 'D' INSPECTION, FOUND THE AFT PRESSURE BULKHEAD FORWARD LATERAL STIFFENER END CLIP CRACKED AT LONGERON 15 LEFT. REMOVED AND REPLACED END CLIP IAW DC-9 SRM CHAPTERS 51-30-1 AND 51-30-5.Jun 10, 1997 · N962AX · Doug DC941SDR SWAA970546Bulkhead Web · crackedDURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD WEB CRACKED AT LBL 4.7. REPAIRED PER BOEING SRM.Jun 9, 1997 · N528SW · Boeing 7375H4
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