JASC 5300
Service difficulty reports · 8,206
Reports filed under 5300 · Fuselage Structure (General), 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 = '5300' 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 = '5300' 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 UIEA2022092101010None · noneFWD CGO COMPT STA 600-660 RBL 38-56 BALL MAT PANEL FOUND DAMAGED(<P>BALL MAT SKIN REPAIRED AS PER SRM 53-00-53-2R-2 REPAIR 2 FIG 201</P>)SDR UIEA2022092801051Skin · corrodedAFT CARGO COMPT STA 1700 - STA 1720 S45R - S46R INTERNAL SKIN FOUND CORROSION(<P>CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND 51-20-01 WITHIN SRM 53-00-01 ALLOWABLE DAMAGE 2 FIG 101 LIMITS </P>)SDR UIEA2022101601143None · noneEO: 4453B919-2: STA 2598 BULKHEAD LH FRAME SUPPORT LOWER CORNER WL 271, LBL 38 FASTENER HOLE CRACK / CAT B REPAIR.(<P>EO: 4453B919-2: STA 2598 BULKHEAD LH FRAME SUPPORT LOWER CORNER WL 271, LBL 38 FANRENER HOLE CRACK / CAT B EXISTING REPAIR AREA REINSTALLED IASDR UIEA2022101901151None · noneM/D CGO - BS 1220 INTERCOSTAL WEB CRACK AT RBL 117 REPAIR. PLEASE CONFIRM THE REPAIR SCHEME REFER TO EO 4453A267 AND SRM 51-70-13 FIG201 REPAIR(<P>INTERCOSTAL WEB REPAIRED AS PER RI NO. RI-53-00-15935 REV.A</P>)SDR JJBA20221107008None · none3 CRACKS SUSPECTED ON LH OMEGA BEAM #1 AT FR 21, 22, 23. BEAM REPAIRED WITH 3 DOUBLERS. 3 REPAIR DOUBLERS ON LH CENTER FUSE 1 OMEGA BEAM, ON INBD FLANGE AT FR 21, 22 AND 23SDR JJBA20221107006None · noneCF2 LH OMEGA BEAM #2, 2 SUSPECTED CRACKS AT FR 26, 28. CRACKS ON LH OMEGA BEAM #2 REPAIRED. 2 REPAIR DOUBLERS ON LH CENTER FUSE 2 OMEGA BEAM O INBD FLANGE AT FR 26 & 28SDR JJBA20221107001None · noneCF3 CORROSION FOUND ON LH SILL #4. AFTER INVESTIGATION, FITTING DAMAGED UNDERNEATH SILL. FITTING REPAIRED WITH 2 BUSHINGSSDR JJBA20221107007None · noneCF3 LH OMEGA BEAM FOUND CORRODED AND 2 CRACKS SUSPECTED AT FR51 AND FR 52. AFTER NDT INSPECTION (2X) CRACKS CONFIRMED ON LH OMEGA BEAM #2. CUT OUT AT 2X CRACK LOCATION AT FR 51 AND FR 52 PERFORMED. CF3 LH OMEGA BEAM CRACKS REPAIRED.SDR JJBA20221107004None · noneCENTER FUSE 4, FRAME 59 CRACKED BTW STR 15L-16L. CENTER FUSE 4, ON FRAME 59 BTW STR 15L-16L, RIVETS REMOVED FOR INVESTIGATION. FR 59 BTW 14L-15L SPLICE REMOVED. MADE REPAIR PART LOCALLY FABRICATED. CENTER FUSE 4, FRAME 59 BTW 15L-16L, CRACK REPAIREDSDR JJBA20221107003None · noneCORROSION FOUND ON RAD ALT #2 ANTENNA BASE DOUBLER BTW FR68-69 AND BTW STR 21L-21R IN RF1 AREA. AT RAD ALT #2, AFTER INVESTIGATION INNER AND EXTERNAL DOUBLER CORROSION FOUND OUT OF LIMIT AND SKIN CRACKED AROUND FASTENERS. DOUBLER AND FILLER FOR #2 ANTENNA FABRSDR UIEA2022102101168None · noneCORROSION ON ACCESS PANEL SUPPORT FOR KEEL BEAM BETWEEN STA 889 TO STA 915.5(<P>ACCESS PANEL SUPPORT P/N 145T8629-2 WAS REPLACED PER PRODUCTION DRAWING AND SRM 51-10-02</P>)SDR CALA2022102402938None · crackedLH FR68 STR22 INNER CAP AND WEB FLANGE CRACKED AD 20-22-15-05 PE R NR9298099 / 22099 GEN BY V061632 RPR AT LH FR68 STR22 RPR AREA PER PART 3 OF THE LATEST REV OF 5341-01349 PART 1.2. ECRA 5341-01349 ON OR BEFORE 39,741 TOTAL ACFT FC IAW ECRA ACMP INTERIM REPAISDR YENA2022110201085None · noneFLT#562, SJU-BOS. 'ENCOUNTERED MOMENTARY SEVERE TURBULENCE (5 - 6 SECONDS) DURING CLIMB OUT. DARK (NIGHT), NO RADAR RETURNS; DOWNLOADED HMU FLIGHT DATA PER AMM BD500-A-J46-11-01-01AAA-752A-A. ALL PARAMETERS ARE WITHIN LIMITS PER TECH SUPPORT. AIRCRAFT IS OK FOSDR CALA2022102402927None · crackedCRACK PLATE LOC. BTW FR68TO FR69 L/H SIDE AT AFT GALLEY AREA SEE AEROMAN NON ROUTINE 2022-359949 REPLACED NEW PLATE LOC. BTW FR 68 TO FR69 L/H SIDE AT AFT GALLY AREA IAW A320 SRM 51-42-11-001 AND A320 SRM 51-72-11-911- 001, DWG D53480019SDR CALA2022102402924Skin · noneLIGHTNING STRIKE ON FWD UPPER FESELAGE SKIN BTW FR41-42 STGR 3-4LH A3NB-05-3-6040 SEQ#19 ZONE:200. LTPR NR0050011802080010 P WAS PERFORMED. REWORK IS BEYOND ADL PER SRM 53-31-11-283-001 R 001 FIGURE 001 REV 142. DIP WITH INSPECTION THRESHOLD FROM TIME INSPECTISDR CALA2022102402917None · crackedCRACK INDICATION FOUND AT FASTENER HOLE LOCATED AT FRAME 35 AND STR 30 RH SIDE AT FWD CARGO COMPARTMENT. CRACK DIRECTION IS 3 AND 9 OCLOCK APROX LOOKING AFT. CRACK DEPTH IS 0.055 INCHES APROX. REPAIR BEFORE FURTHER FLIGHT. SEE AEROMAN NON ROUTINE 2022-394074 BSDR CALA2022102402916Door Sill · corrodedL2 DOOR SILL PLATE IS CORRODED. PER HAECO LCQ NON-ROUTINE 929444 1/44441 GENERATED BY V892442 SPEC: A3NB-53-3-6357. REPAIRED (2) DOOR SILL PLATE AT FR68 IAW A319 SRM 53-41-14-300-0 01 FIGURE 001 REPAIRED TOPCOAT IAW SRM 51-75-12-911-002 PERFORME D V928628 INSPSDR CALA2022102402918Skin · crackedCRACK INDICATION ON FRAME 35 RH SIDE IN OPEN FASTENER HOLE LOWER AND MORE AFT AT LEVEL OF STGR30, CRACK DIRECTION IS 2 OCLOCK IN FWD CARGO COMPARTMENT (1 EA) SEE AEROMAN NON ROUTINE 2022-359824 SKIN, AND FR35 LAYARS ONLY) AND F5 AT FR35 AND F5 AT FR35 AND RESDR JJBA20221107002None · noneCRACK SUSPECTED (6X) ON RH SKIN AROUND FASTENERS BTW FR 77-80 BTW STR 3L-9L. SKIN REPAIRED WITH 8 BUSHINGS REPAIRSDR CALA2022102402909None · crackedREV B (AD 2022-02-11) L/H FR20 DOOR STOP FITTING #7 UPPER INBD H OLE (H1) FOUND CRACKED AFTER HFEC ROTO INSPECTION. CRACK APPEARS IN INTERCOASTAL LAYER AT APPROXIMATELY 4 O''CLOCK "REPAIR BEFORE NEXT FLIGHT" REMOVED AND REPLACED CRACKED INTERCOASTAL AT FR20 LHSDR CALA2022102402908None · crackedLH FR68 STR22 INNER CAP AND WEB FLANGE CRACKED AD 20-22-15-05 PE R NR9298099 / 22099 GEN BY V061632 RPR AT LH FR68 STR22 RPR AREA PER PART 3 OF THE LATEST REV OF 5341-01349 PART 1.2. ECRA 5341-01349 ON OR BEFORE 39,741 TOTAL ACFT FC IAW ECRA ACMP INTERIM REPAISDR 2A6D202210200001Doubler · crackedREAR DOUBLER P/N: L533M1321262 FOUND CRACKED DURING INSPECTIONSDR UIEA2022100501091Support Bracket · corroded***CORROSION*** FWD CARGO LH SIDEWALL LINER SUPPORT BRACKET HAS CORROSION, STA500A, BETWEEN S23L & S24L (REMOVED AND REPLACED BRACKET PER SRM 51-40-02 AND BOEING DRAWING 417A2150)SDR UIEA2022100501092Support Bracket · corroded***CORROSION*** FWD CARGO LH SIDEWALL LINER SUPPORT BRACKET HAS CORROSION, STA500H, BETWEEN S23L & S24L (REMOVED AND REPLACED BRACKET PER SRM 51-40-02 AND BOEING DRAWING 417A2150)SDR UIEA2022100501093Support Bracket · corroded***CORROSION*** FWD CARGO LH SIDEWALL LINER SUPPORT BRACKET HAS CORROSION, STA500G, BETWEEN S23L & S24L (REMOVED AND REPLACED BRACKET PER SRM 51-40-02 AND BOEING DRAWING 417A2150)SDR UIEA2022100701099Threshold Web · corroded***CORROSION*** AFT CARGO COMP CARGO DOOR CUTOUT WEB HAS CORROSION STA787+9 - 827+5, RBL26, WL156. (REMOVED DAMAGED THRESHOLD WEB. INSTALLED REPLACEMENT THRESHOLD WEB PN# 146A8123-25 PER DWG# 146A8340 AND SRM 51-40-02-0G-0)SDR UIEA2022101701147Frame · out of limitsFOUND DOUBLE DRILLED FRAME HOLE STA 500B RBL21 WL156 (REPAIRED BS 500B, RBL 21 WL 153 DAMAGE PER; ATS ER 22-02343 REV IR)SDR UIEA2022101701149Channel · corroded***CORROSION***FWD CARGO COMP. CORROSION ON LH ZEE CHANNEL, STA. 460+10 - 500G+7, LBL 23, WL 157(<P>REMOVED AND REPLACED Z CHANNEL STA. 400 - 500I, LBL 23, WL 157 PER DWG# 143A7505 AND SRM 51-40-02-0G-0</P>)SDR DALA2022102106807Structure · crackedSHIP 3253 WHILE PERFORMING HFEC PER AMDS 5316-01052-05A, CRACK DETECTED IN PREVIOUS WORK AREA. CORRECTIVE ACTION: COMPLIED WITH ERA 603007A REV. O SECTION 1. (8952014)SDR 2022FA0000637Canopy · brokenI WAS FLYING AT APPROXIMATELY 5,000' AGL WHEN THE CANOPY DEPARTED THE AIRPLANE. WHEN I REALIZED WHAT HAPPENED, THE AIRPLANE WAS PITCHED DOWN AT ABOUT A 60 DEGREE ANGLE. I WAS ABLE TO RAISE THE NOSE TO A LEVEL FLIGHT POSITION AND CONTINUE TO A GRASS STRIP ABOUTSDR YENA2022102101032None · noneFLT#1567, HPN-PBI. ALL FA'S SAID THEY SMELLED AN AMONIA-TYPE SMELL DURING DECENT. DURING DEBRIEFING. 2 AFT FA'S SAID SMELLED THE SAME SMELL INITIAL CLIMB SERVICE BUT DID NOT NOTIFY THE FLIGHT CREW AT THE TIME. SYMPTOMS WERE WATERY EYES & BLURRY VISION; ACCOMPSDR YENA2022102101036None · noneFLT#454, MCO-EWR. 'DURING LUBRICATION OF THS CONTROL CHAIN, QC NOTICED CORROSION ON THE PERIMETER OF THE THS ACCESS DOOR; REMOVED AND REPLACED DOOR ASSY THS ACCESS REF AMM 52-41-04. NOTE INSTALL ONLY DUE TO DOOR REMOVED UNSERIALIZED IN TRAX.'SDR YENA2022101701028None · noneFLT#891, BOS-TPA. 'INFLIGHT REPORTED STRONG SMELL OF BURNING CRAYONS ROW 5-9, ODOR PERSISTED THROUGHOUT FLIGHT. NO ATTEMPT AT ODOR ISOLATION WAS MADE; COMPLIED WITH INFO NOTICE 2017-T015J, SECTION B2. DECONTAMINATION LEVEL 2, TYPE 10 WAS ACCOMPLISHED PER TSM 5SDR YENA2022101701027None · noneFLT#1454, SJU-FLL. 'DIRTY SOCKS/CHEMICAL SMALL REPORTED BY ALL INFLIGHT CREW DURING CRUISE AROUND ROW 25 AFT CABIN; COMPLIED WITH INFORMATION NOTICE 2017-T015 SECTION A. ISOLATED FAULT TO TYPE 10 (A) 1, C PER TSM 05-50-00-810-085-B/TSM 0550-00-810-085-D. AIRCRSDR A6WA202210158344None · corrodedFLOOR BEAM CAP RBL 9 FROM FS559+96 TO FS 559+16 HAS AREA OF CORROSION ****AIRCRAFT REMOVED FROM SERVICE **** FLOOR BEAM REPLACEDSDR YENA2022101701025None · noneFLT#2467, BOS0CLT. (AIRCRAFT PERFORMED AN AIR TURN ABCK TO BOS) 'ENG VIB ON RIGHT ENGINE AT FL 340 AND X. 79 MACH ASSOCIATED CAUTION MSG. COMPLIED WITH. MSG EXTINGUISHED WITH THROTTLE REDUCTION; REFERENCE AMP 72-00-00-16AAA-0B5A-A. ITEM IS ON CURRENT DEFERRALSDR A6WA202210148341None · corrodedFLOOR BEAM CAP LBL27 NEAR FS559+112 HAS AREA OF CORROSION ***AIRCRAFT REMOVED FROM SERVICE **** REPAIRED FLOOR BEAM CAP LBL 27 NEAR FS 559+112 REF CRJ 200 SRM 53-00-43SDR DALA2022122308306Structure · not reportedERA 602625-14AD ISSUED FOR REPAIR TO INNER CHORD AT BS 1197, LBL 7. AMOC TO AD 2021-10-19 REQUIRED WITHIN 34,208 ADDITIONAL CYCLES. ASSOCIATED ER/A 00-602625.SDR YENA2022101401022None · noneFLT#1869, JFK-PUJ. 'DIRTY SOCK SMELL STARTED DURING DESCENT AND STAYED UNTIL ENGINE SHUTDOWN. PACK 1 WAS TURNED OFF AND THAT HELPED ALLEVIATE THE SMELL SLIGHTLY FLIGHT ATTENDANTS REPORTED A STRONG SMELL IN THE CABIN; COMPLIED WITH INFORMATION NOTICE 2017-T015 SDR GTIA2022101336717None · noneSMELL OF MUST DIRTY SOCKS AT 6000 DETECTED ON FLIGHT DECK ONLY-PERFORMED TSM 05-50-00-810-831-A FOUND APU TO BE CAUSE .APU FOUND TO HAVE OIL IN / AT INLET . APU TO BE DEFERED ON LP 3098006-1 PACK BURN OUT ACCOMPLISHED ON ENG RUN WITH HUFFER CART NO ODOR DETECTSDR FXGA202210102224None · noneDENT ON FUESELAGE SKIN AT F/STA 393, STR 15L. TO REPAIR DENT DAMAGE ON THE FUSELAGE SKIN AT F/STA 393, STR 15L. PERFORM FUSELAGE SKIN REPAIR PER STS EA 81-2022-122. RE-INSPECTION INSTRUCTIONS TO BE PROVIDED WITH DTA NO LATER THAN 12 MONTHS FROM REPAIR COMPLETISDR SWIA202266674None · crackedCOCKPIT FLOOR, LH CONSOLE AFT SUPPORT ANGLE IS CRACKED AT FRAME 12. (C-CHECK RO 10/25/2022) / REMOVED, REPLACED, AND RESTORED SURFACE PROTECTION TO COCKPIT FLOOR, LH CONSOLE AFT SUPPORT ANGLE AT FRAME 12. REF SRM 51-40-08, 51-23-06.SDR SWIA202266673None · crackedCOCKPIT FLOOR, AFT END OF THE CONNECTOR FWD FUSELAGE I SUPPORT BETWEEN FRAMES 11 AND 12 HAS A CRACKED ANGLE. (C-CHECK RO 10/25/2022) / REMOVED, REPLACED, AND RESTORED SURFACE PROTECTION TO COCKPIT FLOOR, AFT END OF THE CONNECTOR FWD FUSELAGE I SUPPORT SDR SWIA202266606None · damagedBIRD STRIKE DAMAGE BELOW LEFT SIDE WINDSHIELD WIPER. (FILED CLOSED) COMPLIED WITH PERMANENT REPAIR TO FUSELAGE SKIN AT FRAME 4 BETWEEN STRINGERS 02L AND 4L REF ETD 2022-170-031092 REV:/. COMPLIED WITH STRUCTURAL MAJOR REPAIR RII CARD 51-00-00-002-SKY-U. SESDR GTIA2022101036715None · noneODOR IN COCKPIT AND MID CABIN DURING CRUISE,MELTING WAX OR WIRE SMELL, SEEMES TO DISAPATE WITH PACK 2 OFF, AIR STORT IN SKRG CART HAD VERY HEAVY BLACK EXHAUST SMELL RETURNED BRIEFLY WHEN FLYING THROUGH A CLOUD DURING ARRIVAL. -PERFORMED IDENTIFICATION OF THE CSDR FDEA202210072506Doubler · misrepairedDURING PERFORMING EO G-5710-E0365655 B P8 STEP8.C.(5), FOUND 01EA ZLJ-8(BACB30NY8K*) COUNTERSUNK FASTENER AT STA998 STGR35 RHS TOO CLOSE TO EDGE OF MACHINED STEP OF DOUBLER P/N : 143W2314Y406, AND WILL RESULT IN KNIFE EDGE WITH MACHINED STEP ON AFT EDGE SDR FDEA2022101172505Doubler · misrepairedDURING PERFORMING EO G-5710-E0365655 B P7 STEP8.C.(5), FOUND 01EA ZLJ-8 COUNTERSUNK FASTENER AT STA 998 S35L TOO CLOSE TO EDGE OF MACHINED STEP OF DOUBLER P/N 143W2314Y405, AND WILL RESULT IN KNIFE EDGE WITH MACHINED STEP ON AFT EDGE OF COUNTERSUNK HOLE.SDR DALA2022101006538None · noneSHIP 3416 SEVERE TURBULANCE FL 320 FOR APPROXIMATELY 3 MINUTES. CORRECTIVE ACTION: ACCOMPLISHED ERA 602870-14 AND PERFORMED INSPECTION AFTER FLT IN EXCESSIVE TURBULANCE, NO DEFECTS & FAULTS FOUND THEN OPS CHECKED OK PER A330 AMM 05-51. (9550677)SDR 2022FA0000582None · noneAIRPLANE HAD A PITCH TRIM RUNAWAY OCCUR AT 4000 FEET WHICH CAUSED THE AIRPLANE TO DIVE NOSE DOWN. DISCONNECTED THE AUTOPILOT AND REALIZED THAT THE TRIM RAN OUT VERY QUICKLY. TOOK THE TRIM OUT TO RECOVER THE AIRCRAFT FROM THE DIVE. DURING TROUBLESHOOTING FOUND SDR R61A2022110400688Seat Track · corrodedL/H SEAT TRACK FOUND CORRODED AT FR 74. R&R IAW SRM 53-00-10 FIG 206.
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