JASC 5350
Service difficulty reports · 6,124
Reports filed under 5350 · Aerodynamic Fairings, 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 = '5350' 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 = '5350' 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 AWXA200301180Support Angle · crackedLCQ - MAJOR REPAIR - DURING C-09 CHECK A .75 INCH CRACK WAS FOUND ON SUPPORT BRACKET UNDER RT WING TO BODY FAIRING AT BS 1300, STR 21 RT. MAINTENANCE CUT OUT DAMAGE ON SUPPORT BRACKET UNDER RT WING TO BODY FAIRING AT BS 1300, STR 21 RT; PERFORMED HFEC INSPECTSDR AWXA200301179Support Angle · crackedLCQ - MAJOR REPAIR - DURING C-09 CHECK A 1.25 INCH CRACK WAS FOUND ON SUPPORT BRACKET UNDER RT WING TO BODY FAIRING AT BS 1300, STR 25 RT. MAINTENANCE CUT OUT DAMAGE ON SUPPORT BRACKET UNDER RT WING TO BODY FAIRING AT BS 1300, STR 25 RT; PERFORMED HFEC INSPECSDR DHL2003805594Skin · delaminatedLEFT WING-FUSELAGE NR 708 UPPER FAIRING INTERNAL SKIN DELAMINATED, STA 1040.000 - STA 1080.000. REMOVED AND REPLACED LEFT WING TO FUSELAGE UPPER FAIRING NR 708 (STA 1040.000 - 1080.000) IAW SRM 51-3-0 PG 1.SDR 03FDEA01335Hinge · gougedDOORS - SERVICE - TAIL CONE - PATIO DOOR HINGE REPAIR P/N AKC7011-1. COMPLY WITH EA 8-5240-72249 REV NR POS ENT BY: 402783. FACT 18AUG03 23:02 BFM R COMPLIED WITH EA 8-5240-72249 DOORS - SERVICE- TAIL CONE- PATIO DOOR HINGE REPAIR P/N AKC 7011-1 AT SDR AWXA200300925Plate · crackedDURING C-04 CHECK A .3750 INCH CRACK WAS FOUND IN RADIUS OF FUSELAGE FAIRING CLOSING PLATE AT FR 34, Y1600, Z1610. MAINTENANCE REMOVED CRACKED CLOSING PLATE AT FR 34, Y1600, Z1610; FABRICATED A NEW REPLACEMENT CLOSING PLATE; INSTALLED REPAIR PART IAW A320 SRMSDR 03FDEA01160Clip · crackedNR 359 LT FUSELAGE UPPER WING TO BODY SUPPORT RIB ATTACH ANGLES 2EA CRACKED AT STA 1361. CLOSING ACTION ON 07/20/03 REMOVED AND REPLACED BODY SUPPORT ATTACH ANGLES IAW SRM 53-31-01.SDR 2003F00547Radome · lightning strikeTHE AIRCRAFT WAS STUCK BY LIGHTNING DURING FLIGHT. THE FLIGHT CREW NOTICED THE RADAR SCREEN WENT BLANK THEN CAME BACK UP AND FUNCTIONED NORMALLY. THE RADOME HAD BEEN BURNED AND THE LEFT ELEVATOR TRIM TAB HAD A HOLE IN THE TRAILING EDGE. THE LIGHTNING STRIKESDR DHL2003804006Radome · dentedRADOME HAS A 12 INCH CREASE LOWER LEFT SIDE. REMOVED AND REPLACED RADOME ASSY IAW DC-8 M/M 53-50-1. OPS CHECKS GOOD.SDR 03FDEA01086Rib · crackedTAILCONE , LT SIDE- INTERNAL RIB IS CRACKED, FWD END AT NR 2 RIB: 24 INCHES BELOW MAINT PLATFORM. ACCOMPLISHED AT MAE UNDER W/O NO.13414. FABRICATED REPAIR AND INSTALLED REPAIR IAW/SRM 53-00-01 FIG 10 REPAIR PARTS FABRICATED ON MAE TRAVELLER NO. T2/347SDR AWXA200300807Panel · delaminatedDURING C-03 CHECK THE LOWER CENTER BELLY FAIRING (191BB) WAS FOUND DELAMINATED ALONG THE FORWARD LOWER EDGE AT THE RT AFT OUTBOARD CORNER, FR 34. MAINTENANCE REMOVED AND REPLACED THE LOWER CENTER BELLY FAIRING (191BB) IAW A320 AMM SUBTASK 53-35-13-020-052-AO SDR HI12003F00000Channel · damagedDAMAGE TO FUSELAGE DUE TO CHAFE FROM LOWER WING STRUT FAIRING. DAMAGE FOUND ON AIRCRAFT. RECOMMEND P/M OF RUBBER CHANNEL IN THE IPC BE ADDED TO PAGE 57-10-04.SDR DHL2003604767Skin · corrodedTAIL CONE EXTERNAL SKIN SHOWS INTERIM REPAIR AND SEVERAL CORROSION SPOTS BETWEEN STA.1916.000 AND STA.1951.000. PERFORMED MAJOR REPAIR IAW EODHL-030565, ED-3394. REMOVED FASTENERS AND INTERIM REPAIRS. REMOVED CORROSION. FOUND OUT OF LIMITS. TRIMMED OUT THE SDR DHL2003604597Tie · crackedFUSELAGE TAIL CONE INTERIOR - LT TIE 1.000 CRACKED AT STA. 1951.000. STOP DRILLED CRACK AND FABRICATED DOUBLER (2024-T3 AL0.040) IAW SRM 53-2-0 PG.1-2. CLEANED, TREATED AND PRIMED AREA AND DOUBLER IAW SRM 51-1-8B. INSTALLED NEW DOUBLER IAW SRM 51-1-21 PG.1, SRSDR DHL2003604588Frame · crackedTAIL CONE SECTION - FRAME CRACKED 1.000 STA. 1937.000 LH SIDE. STOP DRILLED CRACK AND FABRICATED DOUBLER (2024-T3 AL0.040) IAW SRM 53-2-0 FIG.2. CLEANED, TREATED AND PRIMED AREA AND DOUBLER IAW SRM 51-1-8B. INSTALLED NEW DOUBLER IAW SRM 51-1-21 PG.1, SRM 51-SDR DHL2003604589Frame · crackedTAIL CONE SECTION FRAME CRACKED 1.000 STA 1923.000 RT SIDE. STOP DRILLED CRACK AND FABRICATED DOUBLER IAW SRM 53-2-0 FIG 2. CLEANED, TREATED AND PRIMED AREA AND DOUBLER IAW SRM 51-1-8B. INSTALLED DOUBLER IAW SRM 51-1-21 PG 1, SRM 51-3-0 PG 1.SDR DHL2003604590Tie · crackedFUSELAGE TAIL CONE INTERIOR RT TIE 1.000 CRACKED AT STA 1923.000. STOP DRILLED CRACK AND FABRICATED DOUBLER IAW SRM 53-2-0 FIG 1B. CLEANED, TREATED AND PRIMED AREA AND DOUBLER IAW SRM 51-1-8B. INSTALLED DOUBLER IAW SRM 51-1-21 PG 1, SRM 51-3-0 PG 1.SDR 2003UALA00478Skin · puncturedFUSELAGE TAILCONE SKIN AT STA 1848, LBL 24 PUNCTURED. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED REPAIR DOUBLER.SDR AUS20030575Radome · bird strike(AUS) BIRDSTRIKE ON SURVEILLANCE RADOME.SDR MWEA030231Doubler · crackedSKIN DOUBLER AROUND LEFT RADOME CUTOUT IS CRACKED. -- REMOVED AND INSTALLED DOUBLER.SDR 2003F00476Fairing · delaminatedAT C-CHECK, FOUND BELLY FAIRING 197CB DELAMINATED. REPAIRED FAIRING IAW SRM S3-45-12 PAGE 220, FIGURE 205. (M)SDR 2003F00482Fairing · delaminatedAT C-CHECK, FOUND BELLY FAIRING 197EB DELAMINATED. REPAIRED FAIRING IAW SRM S3-4S-12, PAGE 220 FIGURE 205. (M)SDR 2003F00480Fairing · delaminatedAT C-CHECK, FOUND RIGHT BELLY FAIRING 197GB, DELAMINATED. REPAIRED BELLY FAIRING 197GB IAW SRM S3-4S-12, PAGE 220 FIG 205. (M)SDR 2003F00474Fairing · delaminatedAT C-CHECK, FOUND BELLY FAIRING 192AB DELAMINATED. REPAIRED FAIRING IAW SRM 51-77-12 PAR 3B, FIGURE 3. (M)SDR 2003F00488Access Panel · delaminatedAT C-CHECK, FOUND RIGHT BELLY FAIRING ACCESS PANEL, 198GB, DELAMINATED STATION 2456. REPAIRED PANEL IAW SRM 51-77-12, PAR 3B, FIGURE 3. (M)SDR DLM88030469Radome · damagedON ARRIVAL DFW FOUND RADOME DAMAGED. LOWER LEFT CENTER. APPROX 6 INCHES IN DIAMETER, SPONGY FEELING. REPLACED RADOMESDR MWEA030211Skin · damagedSKIN DAMAGE ON FUSELAGE AT RADOME LEFT HINGE. FABRICATED AND INSTALLED DOUBLER AND FILLER.SDR 2003F00477Skin · dentedAT C-CHECK, FOUND DENT ON REAR CONE SKIN FS 82, STATION 38035. REPAIRED DENT IAW SRM 53-51-11 FIGURE 203 PAGE 217-218. (M)SDR QXEA0300572Latch · damagedPDX- DAMAGED RIVET AT STATION 169.00 ON BOTTOM, ONE INCH LEFT OF LOWER RADOME LATCH .5 INCH AFT OF FRAME FRONT. REPAIRED IAW CRJ-700 SRM 51-25-16 AND 51-42-13.SDR MWEA030209Pin · crackedRADOME RIGHT UPPER GUIDE PIN LOWER CRACKED. INSTALLED DOUBLER.SDR MEX2003172Lock · brokenTHE RADOME RIGHT LOCK WAS BROKEN BY F.O.D. THE RADOME LOCK WAS REPLACED IAW MM 53-51-02, TEST CORRECT.SDR DHL2003801068Panel · delaminatedLT WING TO FUSELAGE UPPER FILLET NR 706 INTERNAL SKIN DELAMINATED (STA 912.000-980.000). REMOVED AND REPLACED LT WING TO FUSELAGE UPPER FILLET NR 706 (STA 912.000-980.000) IAW SRM 51-1-21 PG 1.SDR DHL2003604502Panel · delaminatedRT WING UPPER SURFACE - NR 708 FILLET OUTER SKIN DELAMINATED STA 980.000 - 1040.000. REMOVED AND REPLACED NR 708 FILLET ON RT WING UPPER SURFACE, STA 980.000 - STA 1040.000 IAW SRM 51-3-0 PG 1.SDR CA030502001Radome · bird strike(CAN) CREW REPORTED ' BIRD STRIKE LT SIDE OF NOSE CONE ON DEPARTURE CLIMBING THROUGH 1500' INDICATED, IE 1000 FT AGL. ALL ENGINE INDICATIONS, FLT CONTROLS ETC NORMAL.RADAR ANT LIGHT CONTINUOUSLY FLASHING, IE RADAR ANTENNA WILL NEED TO BE READJUSTED. MAINTENASDR AWXA200300546Angle · crackedMCN - MAJOR REPAIR - DURING C-04 CHECK A .5 INCH CRACK WAS FOUND ON ATTACH ANGLE AT FR 34 ON FAIRING SUPPORT STRUCTURE AT AFT UPPER EDGE OF PANEL 192AB. MAINTENANCE REMOVED DAMAGED ATTACH ANGLE AT FR-34; FABRICATED A NEW REPLACEMENT ATTACH ANGLE; INSTALLED RESDR LR7A03042Longeron · crackedDURING SCHEDULED B2 INSPECTION PER JOB CARD HB3200 FOUND LT MLG WW POD WL 200 LONGERON CRACKED AT FS 477, LBL 80. REPLACED LONGERON IAW SRM SMP 583 51-70. NR 0015, 02/REP/61 AND 02/REP/62.SDR UPS03240686Rib · corrodedINSPECTION TYPE: C&SI, FUSELAGE FAIRING NR 3430, FWD FORMED SECTION SUPPORT RIB HAS EVIDENCE OF HEAVY CORROSION UNDER ANCHOR NUT PLATES, JUST FWD OF GRND MOVER DOOR CUT OUT DOOR REMOVED IAW SRM 51-30-02. FRAME REMOVED IAW SRM 51-30-02. CORR OSION REMOVESDR 03FDEA00594Frame · crackedFORWARD TAIL CONE MOST AFT MAIN FRAME LT SIDE FOUND WITH CRACK. FWD TAIL CONE MOST AFT MAIN FRAME LH SIDE CRACK REPAIRED AS PER DWG. AKC7539 AND SRM 53-00-01, VOL.II.SDR UPS03240675Frame · corrodedINSPECTION TYPE: C&SI, FUSELAGE FAIRING NR 3431, AFT FORMED SECTION HAS HEAVY CORROSION UNDER FLOATING ANCHOR NUTS REMOVED FASTENERS ON FRAME IAW SRM 51-30-02. CORRODED SECTION OF FRAME FOUND TO BE OUTSIDE LIMITS IAW SRM 51-10-01 FIG 1 & CORRODED SECT ION OF SDR 03FDEA00532Radome · damagedRADOME FAILED MOISTURE CHECK. REMOVED AND REPLACED RADOME IAW FED EX M/M 53-15-000-04.SDR DHL2003801034Frame · crackedTAIL CONE LT FRAME WITH 0.500 INCH CRACK IN STA 1961.000. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. STOP DRILLED CRACK AT STA 1961.000 IAW SRM 53-1-0 FIG 1B. FABRICATED DOUBLER (2024-T3 AL0.040) IAW SRM 53-2-0 FIG 1B. CLEANED, TREATED AND PRIMED IAW SRM 51-1SDR UPS03240642Radome · damagedINSPECTION TYPE: C&SI, RADOME FAILED MOISTURE CHECK. RADOME REPLACED IAW MM 53-15-00. RESISTANCE CHECK CARRIED OUT ON RADOME IAW MM 53-15-00. CHECK FOUND TO BE SATISFACTORYSDR QXEA0300495Fairing · chafedPDX - WING TO FUSELAGE FAIRING, PANEL 262HT FUSELAGE ATTACH FLANGE HAS SEVERAL CHAFE AREAS. REPAIRED IAW RD 8/4-53-451.SDR QXEA0300493Fairing · chafedPDX - WING TO FUSELAGE FAIRING, PANEL 262AT FUSELAGE ATTACH FLANGE HAS SEVERAL CHAFE AREAS. REPAIRED IAW RD 8/4-53-451.SDR QXEA0300492Fairing · chafedPDX - WING TO FUSELAGE FAIRING, PANEL 261FT FUSELAGE ATTACH FLANGE HAS SEVERAL CHAFE AREAS. REPAIRED IAW RD 8/4-53-451.SDR QXEA0300491Fairing · chafedPDX - WING TO FUSELAGE FAIRINGS, PANEL 261CT FUSELAGE ATTACH FLANGE HAS SEVERAL CHAFE AREAS. REPAIRED IAW RD 8/4-53-451.SDR QXEA0300490Fairing · chafedPDX - WING TO FUSELAGE FAIRINGS, PANEL 261LT FUSELAGE ATTACH FLANGE. HAS SEVERAL CHAFE AREAS. REPAIRED IAW RD 8/4-53-451.SDR UPS03240684Frame · corrodedINSPECTION TYPE: C&SI, BODY FAIRING NR 3430, HAS CORRODED FRAME AFT OF GND. COOLING FAN DOOR CUT OUT. FRAME REMOVED IAW SRM 51-30-02. CORROSION REMOVED IAW SRM 51-10-06 OUT OF LIMITS IAW SRM 51-10-01. NEW FRAME FABRICATED IAW SRM 51-20- 1 FIG 7. NEW FRASDR 03FDEA00400Intercostal · crackedN 132 TAILCONE LT MAINT PLATFORM WEB IS CRACKED BETWEEN 2EA ACTUATOR ROD/STIFFNERS/ SUPPORT ANGLES PARALLER TO MAINT PLATFORM AT NON-SKID AREA. CLOSING ACTION ON 04/07/03. REMOVED CRACKED DOUBLER AND INTERCOSTAL IAW SRM 51-35-01. FABRICATED REPAIR DOUBSDR AWXA200300425Panel · crackedMCN - MAJOR REPAIR - DURING C-04 CHECK A 1 INCH CRACK WAS FOUND ON WING TO BODY FAIRING CLOSING PLATE AT FR 34, LBL 64. MAINTENANCE REMOVED DAMAGED CLOSING PLATE AT FR 34, LBL 64; FABRICATED A NEW REPLACEMENT CLOSING PLATE; INSTALLED REPAIR PART IAW A320 SRM SDR AWXA200300406Attach Angle · crackedMCN - MAJOR REPAIR - DURING C-04 CHECK A 1 INCH CRACK WAS FOUND ON LT FORWARD BELLY FAIRING VERTICAL ATTACH ANGLE BS 1483.4, 13 INCHES FROM OUTBOARD GROUND AIR CONDITIONING ATTACH POINT. MAINTENANCE REMOVED CRACKED LT FORWARD BELLY FAIRING VERTICAL ATTACH ANG
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