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.
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 SWAA062468Bulkhead · crackedDURING SCHEDULED 20Y CHECK, FOUND AFT PRESSURE BULKHEAD DOME CAP CRACKED AT BS 1016, STR 4L. REPAIRED DOME CAP PER ER.SDR SWAA062467Bulkhead · crackedDURING SCHEDULED 20Y CHECK, FOUND AFT PRESSURE BULKHEAD DOME CAP CRACKED AT BS 1016, STR 7R. REPAIRED DOME CAP PER SRM.SDR SWAA062466Bulkhead · crackedDURING SCHEDULED 20Y CHECK, FOUND AFT PRESSURE BULKHEAD DOME CAP CRACKED AT BS 1016, FIRST FASTENER AT 7 O'CLOCK POSITION. REPAIRED DOME CAP PER SRM.SDR AWXA200601356Bulkhead · crackedFOUND VERTICAL BEAM WEB CRACKED FROM TOOLING HOLE AT BS 178, WL 230 , RBL 17.1. REPAIRED VERTICAL BEAM WEB AT BS 178, WL 230, RBL 17.1 IAW B 737-300 SRM 53 - 10 - 08 - 2R 12 FIG 201.SDR AWXA200601355Bulkhead · crackedFOUND VERTICAL BEAM WEB CRACKED FROM FASTENER HOLE AT BS 178 WL 185 LBL 17.1. MAINTENANCE REPAIRED VERTICLE BEAM WEB AT BS 178, WL 185. LBL 17.1 IAW B737-300 SRM 53-10-08-2R 12, FIG 201.SDR SWAA062431Bulkhead · crackedDURING SCHEDULED 20Y CHECK, FOUND BULKHEAD CRACKED AT BS 294.5, STR 9L. REMOVED AND REPLACED WEB SECTION PER SRM.SDR UPS06847602Pressure Panel · crackedINSPECTION TYPE:C1-3 LT MLG WHEEL WELL STA 940 LBL 63 PRESSURE DECK SKIN IS CORRODED AND CRACKED. CUT OUT DAMAGED AREA IAW SRM 53-2-0. FABRICATED AND INSTALLED REPAIR DOUBLERS AND FILLERS IAW SAA EA 008-5320-01-A0300, UPS EO DC8-5330- 24740-A, DOUGLAS DWG 564SDR UPS06847579Bulkhead · crackedINSPECTION TYPE:C1-3 LT AFT MAIN CABIN APB STA 1766 LBL 30 APROX 48 INCHES ABOVE FLOOR IS CRACKED. CUT OUT DAMAGED AREA AT FS 1766 LBL 30 IAW SAA EA 008-5305-01- A0305. FABRICATED AND INSTALLED REPAIR PARTS IAW SAA EA 008-5305-01- A0305, UPS EO DC8-5330-2477SDR UPS06847570Bulkhead · crackedINSPECTION TYPE:C1-3 AFT MAIN CABIN RT SIDE OF APB CRACKED AT RBL 30-33 AND FROM RBL 36-40 APPROX 60 INCHES ABOVE FLOOR LINE. CUT OUT CRACKED AREA IAW SRM 53-2-5 FIG 14A. FABRICATED AND INSTALLED -25 AND -27 DOUBLER, -9, -11 AND -19 FILLER IAW SRM 53-2-5 FIGSDR CALA0600250Bulkhead · buckledINSPECTION FOUND THE AFT PRESSURE BULKHEAD OIL CANNED AT 11 O'CLOCK POSITION, ZONE 2, BS 1016. AN INTERIM REPAIR WAS PERFORMED IAW ECRA 5311-01261. A DIP WAS INITIATED TO ACCOMPLISH PT 2A INSPECTION AFTER 49K FLIGHT CYCLES, BUT BEFORE 50K FLIGHT CYCLES, AND SDR WRLA2006024Stiffener · corrodedDURING C3 CK, FOUND CORROSION IN LT MAIN GEAR WELL AFT PRESSURE BULKHEAD, STA 1521, ON THE VERTICAL STIFFENER (LWR AFT AREA). REMOVED CORROSION AND REPLACED STIFFENER.SDR WRLA2006020Bulkhead · corrodedDURING C3 CHECK, FOUND CORROSION IN LT MAIN GEAR WHEEL WELL AFT PRESSURE BULKHEAD, STA 1521, VERTICAL STIFFENER LOWER SUPPORT WEB AND ASSOCIATED ANGLES. REMOVED CORROSION AND REPLACED STIFFENER, WEB, AND ANGLES PER SRM PROCEDURES.SDR AWXA200601377Bulkhead · corrodedMCN - FOUND CORROSION ON THE BS 1016 AFT PRESSURE BULKHEAD FWD FACE-BOTTOM OF THE CENTER (LWR) STIFFENER CHANNEL. CORROSION IS OUT OF LIMITS IAW B737-300 SRM 53-80-08 IAI FIG 101. REPAIRED CENTER (LWR) STIFFENER CHANNEL BS 1016 AFT PRESSURE BULKHEAD IAW B737SDR UPS06447677Pressure Panel · crackedINSPECTION TYPE:C NLG WW RT INTERNAL SIDE STA348 WL173 WHEEL WELL SIDE FOUND CRACKED AS MARKED, CRACK LENGTH 2.215". NOSE W/W BS 350 RT SIDE PANEL BETWEEN WL160 AND WL170 REPAIRED AS PER RS R53-18-35532 CONTINUE INSPECTION ARE REQUIRED AS GIVEN IN SB 747-53A2SDR UPS06447617Pressure Panel · crackedINSPECTION TYPE:C NLG W/W RT INTERNAL SIDE STA352 WL181 W/W SIDE FOUND CRACK CROSS OVER STOP HOLE AS MARKED. CRACK LENGTH 2.37 NOSE W/W BS350 RT SIDE PANEL BETWEEN WL160 AND WL170 REPAIRED AS PER RS R53-18-35532 REFER NRC6739 FOR WORKING DETAIL. CONTINUE ISDR UPS06847422Bulkhead · crackedINSPECTION TYPE:C1 AFT PRESS BULKHEAD CRACKED AT STA 1766 L12L SIDE. CUT OUT DAMAGED AREA IAW SRM 53-2-5 FIG 14A. FABRICATED AND INSTALLED -25, -27 DOUBLERS, -9,-11, AND -19 FILLERS IAW SRM 53-2-5 FIG 14A 51-1-21, AND 51-1-20D THIS REPAIR REQUIRES MPI IAW TRSDR QXEA200601768Pressure Panel · corrodedPDX C4 - FOUND PRESSURE PANEL 121BL HAS ONE SPINNING NUTPLATE AND SEVERAL RUSTY NUTPLATES. REPAIRED IAW DHC-8-200 SRM 51-40-00.SDR QXEA200601767Pressure Panel · corrodedPDX C4 - FORWARD PRESSURE PANEL 122AR HAS SEVERAL RUSTY NUT PLATES. REPAIRED IAW DHC-8-200 SRM 51-40-00.SDR 06FDEA2447Pressure Panel · corrodedFOUND LT WHEEL WELL PRESSURE WEB CORRODED B/S 886, LBL 45 WL 202. BLENDED CORROSION FROM LT WW PRESSURE WEB 1"X1" 100% MAT. THICKNESS OUT OF LIMITS PER 51-30-1. REMOVED WEB AND FABRICATED NEW WEB FROM 2024-T30.032" LOT #664145 AND INSTALLED ALL IAW SRM 51SDR EIA2006113Bulkhead · crackedFOUND AFT CARGO STA 1480 BULKHEAD, RBL 27 STR 32 RT LEVEL FOUND "L" ANGLE STIFFENER CRACK. "L" ANGLE STIFFENER REPLACED IAW B747 SRM 51-30-02 PAGE 2, PG 3. MADE FROM FORMED ANGLE 7075-T6 0.063".SDR DHL2006762513Firewall · damagedNR 2 VERT FIREWALL HAS HOLE WORN THROUGH DOUBLER 6:30 POSITION AT T/E STA 1352. REMOVED EXISTING REPAIR AT NR 2 VERT FIREWALL 6:30 POSITION IAW B727 SRM 51-30-2. FABRICATED NEW REPAIR DOUBLER FROM 7075T6 .050 PO NR 900342 DIM 11 3/4" BY 2 1/2" IAW B727 SRM 5SDR AWXA200601199Bulkhead · crackedVERTICAL BEAM CRACKED W/L 183 B/S 178 RBL 5.7. REPAIRED VERTICAL WEB WL 183, BS 178, RBL 5.7 IAW AWA ER NR 03 - 5300 - 06184 - 551. THIS NON-ROUTINE ALSO REPAIRS A CRACK ON VERTICAL BEAM WEB BS 178, W/L 178 RBL 5.7 ON CARD NR 5926794 ZONE 1A SEQUENCE NR 072 SDR AWXA200601107Bulkhead · crackedFOUND WEB CRACKED 178 BULKHEAD ADJACENT TO FASTENER LBL 9.0 WATERLINE 234. REPAIRED CRACKED WEB AT 178 BULKHEAD LBL 9.0 WATERLINE 234 IAW B737-300 SRM 53-10-08-2R 9 FIG 201.SDR QXEA200602213Pressure Blkhd · chafedPDX: NLG WHEEL WELL FWD SIDE OF FWD PRESSURE BULKHEAD, LT OF CENTER HAS A CHAF MARK 1.0 INCH WIDE AND .25 INCHES LONG. MAINTENANCE REPAIRED IAW RD 8/4-53-1224, NDTM PART 6, 51-00-04, MODSUM PACKAGE IS4Q3200025, Q400 AMM TASK 32-31-00-867-801 AND AMM TASK 32-SDR AWXA200601114Bulkhead · crackedFOUND VERTICAL BEAM WEB CRACKED B/S 178 RBL 17.1 W/L 230. REMOVED AND REPLACED VERTICAL WEB B/S 178, RBL 17.1, WL 218 - 235 IAW B737-300 SRM 51-40- 02-06 FIG 8, 12 SRM 51-40-05-06 FIG 2.SDR AWXA200601112Bulkhead · crackedWEB CRACKED 178 BULKHEAD ADJACENT TO FASTENER RBC 9.0 WC 234. REPAIRED WEB AT BS 178, RBL 9.0, WC 234 IAW B737-300 SRM 53-10-08-2R9 FIG 201.SDR LR7A06084Bulkhead · crackedDURING SCHEDULED B2 CHECK PER JOB CARD HB5301 FOUND RT MWW REAR BULKHEAD CRACKED AT FS 617, RBL 70, WL 188. REPAIRED BULKHEAD IAW SMP583 FIG 53-40-10.SDR LR7A06083Bulkhead · crackedDURING SCHEDULED B2 CHECK PER JOB CARD HB5302 FOUND AFT FUSELAGE UPPER BULKHEAD WEB CRACKED AT FS 946, LBL 50, WL 260. REPAIRED WEB IAW SMP583 FIG 51-140-17.SDR LR7A06080Bulkhead · crackedDURING SCHEDULED B2 CHECK PER JOB CARD HB5302 FOUND RT AFT FUSELAGE BULKHEAD WEB CRACKED AT FS 880, RBL 65, WL 195. FABRICATED AND INSTALLED WEB DOUBLER IAW SMP583 51-60, 51-70 AND FIG 51-140-17.SDR SWAA062239Pressure Panel · crackedDURING SCHEDULED PM CHECK, FOUND NLG W/W CEILING PANELS CRACKED AT RT BS 250 AND LT BS 250. REPAIRED CEILING PANELS PER SWA EA.SDR FAA0607002Firewall · crackedWHILE UNDERGOING AN ANNUAL INSPECTION THE ENGINE FIREWALL WAS FOUND TO BE CRACKED WHERE THE EXHAUST HANGER BRACKETS ATTACH ON THE LT SIDE. ADDITIONAL CRACKING WAS ALSO FOUND ON THE INNER BULKHEAD.SDR FAA0607001Firewall · crackedWHILE UNDERGOING AN ANNUAL INSPECTION THE ENGINE FIREWALL WAS FOUND TO BE CRACKED WHERE THE EXHAUST HANGER BRACKETS ATTACH ON THE LT SIDE. ADDITIONAL CRACKING WAS ALSO FOUND ON THE INNER BULKHEAD.SDR N8142GFirewall · crackedWHILE UNDERGOING AN ANNUAL INSPECTION THE ENGINE FIREWALL WAS FOUND TO BE CRACKED WHERE THE EXHAUST HANGER BRACKETS ATTACH ON THE LT SIDE. ADDITIONAL CRACKING WAS ALSO FOUND ON THE INNER BULKHEAD.SDR LR7A06078Bulkhead · crackedDURING PRE-FLIGHT INSPECTION FOUND BULKHEAD WEB CRACKED AT FS 902, RBL 66 & 68, WL 213, 233 & 261. REPLACED WEB IAW SMP583 51-10 PG 3 AND 51-70.SDR LR7A06077Bulkhead · crackedDURING PRE-FLIGHT INSPECTION FOUND BULKHEAD CAP CRACKED AT FS 902, LBL 66, WL 218. REPAIRED BULKHEAD CAP IAW SMP583 53-50-17.SDR DU4R2006529Fitting · corrodedTWO CORRODED AND ELONGATED HOLES IN TEE CHORD AT AFT PRESSURE BULKHEAD P/N 146N8726U2 AND 146N8722-16 BS 1720 RBL 57. OVERSIZED 2 EA HOLES AND INSTALLED FREEZE PLUGS IN UPPER HOLE AND INSTALLED OVERSIZED BOLT IN LOWER HOLE, INSTALLED NEW TEE FITTING IAW B757 SDR AWXA200601115Bulkhead · crackedFOUND CRACK INDICATION ON BS 178 BULKHEAD, WL 218, LBL 12. REPAIRED CHECK ON BS 178 BULKHEAD, WL 218 LBL 12 IAW B737-300 SRM 53-10-08-2R 9 FIG 201.SDR AWXA200601101Bulkhead · crackedFOUND VERTICLE WEB CRACKED LBL 17.1, BS 178M WC 230. REMOVED AND REPLACED WEB AT LBL 17.1, BS 178, WC 235 - 218 IAW B 737-300 SRM 51-40-02-06 FIG 8 AND 12 AND SRM 51-40-05-06 FIG 2.SDR 2006UALA01211Bulkhead · crackedLT MLG WW BULKHEAD BEADED WEB PANEL IS CRACKED AT BS 665 LBL31 WL 202.SDR TRAX200600400Bulkhead · crackedSTATION 280 BULKHEAD CRACKED AT RBL9 BEFORE FLOOR LEVEL.SDR AWXA200601045Bulkhead · crackedMCN - MAJOR REPAIR - NR 5926721 - DURING C15 CHECK DISCOVERED CRACK, .5 INCHES, AT BS178 BULKHEAD AT WL 218 AND BL 12L. MAINTENANCE REPAIRED CRACK ON BS 1789 BULKHEAD, WL 218 AND BL 12L IAW B737-300 SRM 53-10-08-2R9 FIG 201.SDR AWXA200601044Bulkhead · crackedDURING C15 CHECK DISCOVERED WEB AT BS 178 BULKHEAD CRACKED, .125 INCHES, AT WL 234 AND BL 9.0R. MAINTENANCE CUT OUT DAMAGED PORTION AREA IAW BOEING 737-300 SRM 53-10-08-2R9. MAINTENANCE INSTALLED DOUBLER AND FILLER REPAIR AT BS 178 BULKHEAD, WL 234 AND BL 9.SDR ABXA060242Bulkhead · dentedDENT IN AFT PRESSURE BULKHEAD (NEA53800006-787AX1) WAS OUT OF LIMITS IAW B767 SRM 53-80-08. REPAIRED DENT IN AFT PRESSURE BULKHEAD IAW B767 SRM 53-80-08. WORK ACCOMPLISHED ON JC 2024 T-3. CUT OUT 1 INCH PO 408452415. 24 EA BACR15BB5 FASTENERS.SDR EIA2006116Pressure Panel · corrodedLT BODY GR W/W TOP PRESS DECK, STA 1403.75 LBL 33.99, ONE OFF ANGLE STRAP BESIDE THE FORGING FOUND CORRODED AND CRACKED. FABRICATED SPLICE ANGLE, REMOVED AND REPLACED SPLICE ANGLE P/N 65B13346-1 ON LT BLG W/W TOP PRESS DECK, STA 1403.75 LBL 33.99 PER B747 SRMSDR QXEA200601885Bulkhead · chafedPDX C3 - FORWARD PRESSURE BULKHEAD CHAFED INSIDE NOSE WHEEL WELL, LEFT SIDE BEHIND CABLE GUIDE. REPAIRED IAW RD 8/4-53-1224.SDR AWXA200601070Vertical Beam · crackedDURING C17 CHECK DISCOVERED VERTICAL BEAM WEB CRACKED, .500 INCHES, AT BS 178, WL 175 AND BL 5.7L. MAINTENANCE CUTOUT DAMAGE, FABRICATED REPAIR AND INSTALLED REPAIR ON VERTICAL BEAM WEB AT BS 178, BL 5.7 AND WL 175 IAW B737-300 SRM 53-10-08-2R12 FIG 201 DETAISDR AWXA200601066Vertical Beam · crackedDURING C17 CHECK DISCOVERED VERTICAL CHORD CRACKED, .375 AND .125 INCHES, AT THE INBOARD AND OUTBOARD RADIUS AT BS 178, BL 5.7L AND WL 184. MAINTENANCE CUT OUT AND REMOVED DAMAGED PART OF VERTICAL CHORD AT BS 178, BL 5.7L AND WL 184, I/B AND O/B RADIUS. REPASDR C1HA200678003Pressure Panel · crackedRIGHT WHEEL WELL HAS CRACK AT STA 870 BELOW APU LOAD CONTROL VALUE AT RBL 24. NDT CONFIRMED CRACK THAT ENDS AT FASTENER HOLE. FABRICATED DOUBLERS IAW 727 SRM 53-10-9, FIG 5 AND INSTALLED REPAIRED WEB IAW B727 SRM 3-10-9 FIG 5.SDR SWAA062028Stiffener · crackedDURING SCHEDULED SPV CHECK, FOUND BULKHEAD VERTICAL CHORD CRACKED AT BS 178, LBL 5.7. REPAIRED BULKHEAD CHORD PER SRM.SDR C2XA06SH60Firewall · crackedSHV DURING C-CHECK APU FIREWALL CRACKED AT UPPER RT APU SUPPORT BRACKET. MAINTENANCE REPAIRED APU FIREWALL AT UPPER RT SUPPORT BRACKET IAW EMB 145 SRM 53-32-13 FIG 202 DET B. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.
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