JASC 5300
Service difficulty reports · 8,204
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 AALA202501136333Unknown · vibrationAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO CLT DUE TO THE FLIGHT CREW REPORTING THAT AT FL 280 SPEED 310 STARTED GETTING SEVERE VIBRATION FROM TAIL SECTION OF AIRCRAFT. FLIGHT ATTENDANTS REPORTED FROM ROW 15 TO REAR OF AIRCRASDR SWAA2025021784503Panel · debondedPANEL 192E INNER SKIN IS DISBONDED. (MARKED)<[01] PANEL 192E; INNER SKIN WITH DISBOND; WAS REPAIRED IAW SRM 51-70-05-2R-2.;[02] VERIFIED CORRECTIVE ACTION #1SDR 4DPA2025010600002Antenna · misinstalledCREW REPORTED- PASSING 10000’ FEET A LOUD HUMMING NOISE AND STRONG VIBRATION FROM THE COCKPIT THROUGH ROW 7 , CAB RATE WAS SHOWING ZERO AS WE WERE CLIMBING OUT AN AIR RETURN WAS MADE TO BCT DUE TO THE ISSUE. CORR ACTION- MX FOUND WET RTV FWD OF STARLINK WIFI ASDR HALA20250106007Lock · brokenETOPS - FOUND BROKEN DOUBLE LOCK ASSSEMBLY IN MCD AT AFT RH SIDE. REMOVED AND REPLAED DOUBLE LOCK ASSEMBLY IAW A330 CMM 25-52-10.SDR IPXA2025021200557Adapter · corrodedMAIN CABIN CLS ADAPTER FR61 Y0 RH HAS CORROSION NOTED. DOT 7628/09 INSTALLED CLS ADAPTER P/N A53275455200 ON FR61 RH Y0 IAW A300-600 SRM 51-40-21. REQUEST OK TO APPLY TOPCOAT. REVIEWEDSDR IPXA2025011089555Angle · crackedFOUND THE ANGLE CRACK AT STA 1578LBL 80 OUTBOARD IN BULK CARGO COMPARTMENT LEFT AREA (REPLACE). INSTALL NEW PARTS I.A.W SRM 51-40-02-0G REV.91 AND BOEING DWG NO.146T5650 SHEET 5 REV: C. I.A.W AMM 25-57-05-404-006 AND AMM 25-58-04-404-015 REV.144 INSTALLED MAINSDR HNAA2025012100040Structure · corroded53-2233 CARGO DOOR ENTRY FWD L-SHAPE CORRODED AT FR65. REPAIRED IAW SRM 53-31-01 AND EO 1-53-25-0008SDR DALA2024122712021Service Panel · erodedSHIP 3145 EROSION SERVICE PANEL 191CB AT LOWER FUSELAGE. CORRECTIVE ACTION: REPAIRED PER ER/A 622869-14. (0730945)SDR CALA2024121803113Structure · corrodedCABIN FWD WET INNER CHORD STA 344 LBL 61 CORROSION. REMOVED AND REPLACED AT CABIN FWD AREA INNER CHORD LB2 61 PER REF SRM 51-40-020G-0 AND DWG 141A8110 REF AAR N/R 9915662.SDR DALA2024122011881Fitting · damagedREF AA WORK CARD STEP 11. FOUND #4 FITTING O/B AFT HOLE HAS FIBERS BLOWN OUT ON THE INSIDE OF THE FITTING. COMPLIED WITH ER/A622841-14 REV ORIGINAL AND VERIFIED THAT IT MATCHES PRI 622841-14 REV ORIGINAL, REV 1, REV 2, REV 3, REV 4 AND REV 5. (LP# 0713633)SDR HALA20241211361Lock · brokenETOPS - MAIN CARGO LOCK BROKEN. REMOVED AND REPLACED DOUBLE LOCK ASSEMBLY IAW ANCRA CMM 25-51-85. OPS CHECK GOOD.SDR DALA2024120911560Fastener · brokenSHIP 3134 BROKEN FASTENER UNDER FLOOR STRUCTURE LOCATED FR 42 AT LEVEL Y1292 IN PASSENGER CABIN. CORRECTIVE ACTION: COMPLIED WITH ER/A 622235-14. (0700223)SDR CALA2024112702965Beam · corrodedAFT CABIN RT SIDE TRIPLE BEAM CORRODED AT FR68 RMVD AND RPLD AFT CABIN RT SIDE TRIPLE BEAM IAW A319 SRM 51-72- 11-911-002.SDR SWIA202412241121Panel · damagedPANEL 323BT HAS ELONGATED HOLES ON UPPER ROW. (C-CHECK RO 12/21/2024) (FILED CLOSED)REPAIRED PANEL 323BT PER REO 670-55-32-354 REV-- DATE: 2024-12-07. SEE CONTINUATION CARD FOR DETAILS.SDR YENA2024111801489Unknown · vibrationFLT#2009, PBI-LAX. 'CLIMBING OUT OF PBI AND INCREASING TO 250 KNOTS THE CAPT/FO NOTICE A VIBRATION ON THE FLOOR/RUDDER PEDALS. INFLIGHT FELT THE VIBRATION TOWARD THE THE FRONT OF THE AIRCRAFT. SWAPPED AP NO DIFFERENCE SLOWED TO MACH .76 WANED BUT STILL PRESENTSDR VNAA2024111911101Drain · overflowELECTRICAL FIRE SMELL OBSERVED IN GALLEY IN FLIGHT. CREW COMMUNICATION WAS ESTABLISHED, AND NO SMELL WAS OBSERVED IN THE FLIGHT DECK OR BY PASSENGERS IN THE CABIN. NOTE: NO FIRE OR SMOKE PRESENT. / TROUBLESHOT SMELL OBSERVED IN GALLEY IN FLIGHT. TAXIED AIRCRAFSDR AALA202411156220Structure · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LAVATORY L4F-1L LOWER BASE EXTRUSION AT STA 1736, FROM LBL 39.5 TO LBL 102.5. REPAIRED IN ACCORDANCE WITH EA 359231.SDR CALA2024111402860Window Frame · crackedACCOMPLISH INSPECTON REQUIREMENTS OF L/H #3 FLIGHT DECK WINDOW FRAME E-F POST, PER PART 2 OF EC/RA 5311-03308 ON OR BEFORE THE AIRCRAFT REACHING 50,000 TOTAL FLIGHT CYCLES. 5311-03308 FOR DEVIATION PERFORMED. ACCOMPLISH INSPECTION PART 2 OF EC/RA 5311-03308 ONSDR CALA2024111202837Floor Support · corrodedFWD CABIN WET AREA INTERCOSTAL SPOT CORROSION FASTNER HOLES AT LBL 11 BETWEEN STA 328 AND 344 REF AAR N/R 9928261 REMOVED AND REPLACED INTERCOSTAL AT FWD CABIN WET AREA LBL 11 BETWEEN STA 328 TO STA 344 AS PER SRM 51-40-02-0G-0 AND DWG 141A5410 WORK ACCOMPLISHSDR DALA2024111110830Unknown · crackedSHIP 3320 A CRACK WAS FOUND AT HOLE LOCATION #1. CORRECTIVE ACTION: COMPLIED WITH ERA 622047-14AD. (0652147)SDR HNAA2024112001107Structure · corroded53-2082 PAX ENTRY, LWR AFT U-SHAPE CORRODED. RAR U-SHAPE IAW SRM 51-40-02SDR SCNA20241202383Intercostal · crackedWORK ORDER 80719, N/R00114: EMP# 9892 LOWER FUSELAGE FWD CARGO COMPARTMENT BETWEEN STA 500A-500B, RBL 24" INTERCOSTAL WITH CRACK. NOTE: IT WAS FOUND DURING THE REMOVAL OF FLOOR CHANNEL WITH NRI 1-34. RESOLUTION: EMP# 10 QC# 25 REPLACED BAFFLE (INTERCOSTAL) IAWSDR SCNA20241202381SIntercostal · crackedSUPPLEMENTAL: CORRECTION: (** NOTE WEBSITE TIMED OUT **) WORK ORDER 80719, NR00116: EMP# 9892 LOWER FUSELAGE FWD CARGO COMPARTMENT BETWEEN STA 500C-500D, RBL 24" INTERCOSTAL WITH CRACK. NOTE: IT WAS FOUND DURING THE REMOVAL OF FLOOR CHANNEL WITH NRI 1-34. RESDR YENA2024111201462String · corrodedDURING HEAVY MAINTENANCE: CORROSION STRINGER 43L AND BTW FR58 TO FR60 AFT CARGO COMPARTMENT (CPCP FINDING); (RESOLVED ON W/O: 1318564 TASKCARD: NR-00036) REF AE WO 2024-275/1. N/R# 2024 - 538624. PERFORMED PERMANENT REPAIR ON STRINGER 43L AND BTW FR58 TO FR60 SDR SWAA2024121054924Angle · corrodedCORROSION ON ANGLE AT BS992 LBL37 AND LBL43 WL208<[01] REMOVED AND REPLACED WEB SUPPORT ANGLE BS992 LBL37 AND LBL43 WL208 I.A.W SRM 51-10-02-0G-0; SRM 51-40-02-0G-0; BOEING DWG 147A5700 REV: ASDR QXEA2024110800264Beam · corrodedRH BEAM HAS CORROSION BETWEEN FR86 AND FR87. REMOVED AND REPLACED RH BEAM IN AFT WET AREA FR 86-89 REF SRM 51-40-08.SDR IXXA2024102301Skin · damagedDURING HFEC OPEN FASTENER HOLE ROTARY SCAN, DEFECT INDICATIONS WERE NOTED AT THE BOTTOM TWO FASTENER HOLES. LOCATED BETWEEN S-19R AND LWR MAIN SILL CHORD, B STA 332-339.SDR SWAA2024112549700Structure · crackedCRACK INNER CHORD LOCATED BS 303.9 AT LEVEL STR 17L AT FWD GALLEY AREA 2024-645515<[01] REPLACED INNER CHORD AND FASTENERS LOCATED ON BS270 TO BS360 WL 208.10 STR 17L AT FWD GALLEY AREA IAW B737-800 SRM 51-40-02. SRM 51-10-02 Ï¿½TEM 9. DWG 141A8110 SHEET 9 REVSDR SWIA2025010601013Drain Valve · mislocatedDURING INCORPORATION OF SB 670BA-53-57 FUSELAGE, CENTER FUSELAGE MODIFICATION OF THE DRAIN VALVES IN THE CENTER FUSELAGE BETWEEN FS280.00 AND FS33.00 REV C PARTS(S) MISLOCATED LH DRAIN HOLE DOUBLER PLATE. (C-CHECK RO 12/21/2024) (FILED CLOSED)COMPLIED WITH REOSDR IPXA2024101487933Panel · corrodedCORROSION FOUND ON PANEL 196CR LOWER ATTACH FLANGE LOCATED AND DRILLED NEW LOWER T CHORD P/N149N7630-38 I.A.W DRAWING 149N7630 S/N TAG 02089780SDR UATA2024101045310Door Frame · crackedLOWER CARGO DOOR CUTOUT FRAME, LH SIDE "C" CHANNEL HAS A CRACK IN THE UPPER FLANGE JUST AFT OF FRAME 19. INSTALLED AN INTERNAL REINFORCING DOUBLER BEHIND THE CRACK.. SEE FORM 337 FOR DETAILS OF THE REPAIR.SDR EE4Y2024100820978Silencer · no discrepancyDURING INSPECTION CUSTOMER REPORTS ONE (1) UNDOCUMENTED EXISTING REPAIR TO THE TAIL CONE SILENCER OUTER SKIN. THE EXISTING REPAIR HAS BEEN REMOVED AND SKIN CUT OUT MEASURES: 30MM IN LENGTH, 30MM IN WIDTH, MINIMUM EDGE DISTANCE OF EXISTING FASTENER HOLE FROM CUSDR EE4Y2024100820977Silencer · no discrepancyDURING THE CHECK AT AEM, A DENT WAS FOUND IN THE SILENCER RH SKIN P/N 170-50118-003 AT 26INCH FRON AFT EDGE. THE DENT IS OUT OF NEAR TO THE INTERNAL STRUCTURE AT P/N 170-50143-401 BAFFLE #5 LEVEL AND DIMENSIONS ARE: L= 2,059", W= 1,848" AND DEPTH= 0,099". AEM SDR IPXA2024103053923Stringer · crackedMAJOR REPAIR, STRINGER CRACK, AFT SIDE OF STA 2180 S-22L. (REPAIR) REPAIR DAMAGE AREA I.A.W. UPS EO-91737-REQ1 REV.1 . JOB COMPLETED.SDR CALA2024100402560Landing · damagedSUPPORT TASK- FUSELAGE, RIGHT SIDE WTB STRUCTURE AT THE BOTTOM OF 193AR HAS SIGNS OF WEAR ON PANEL LANDING.SDR CALA2024100302541Stringer · corrodedSTRINGER 27L BETWEEN STA 320 AND STA 375 CORRODED, PUNCTURED, AND CRACKED. INTERIM REPAIR TO THE FUSELAGE STRINGER 27L CORROSION, PUNCTURE AND CRACK DAMAGE BETWEEN STA 350 - STA 420 WAS ACCOMPLISHED PER ECRA 5330-07352 PART 1 AT GYR. ACCOMPLISH PERMANENT REPAISDR CALA2024100302543Frame · dentedREF. BAM NR''S 002177257 & 002222808 FOR ALL WORK ACCOMPLISHED. FWD CARGO COMP. STA 500K STR. 24L HAS A DENT ON THE HAT SECTION OF THE FRAME. REPAIRED THE DAMAGED FRAME PER SRM 53-30-07-2R-1 REPAIR 1. REF. BAM NR''S 002177257 & 002222808 FOR ALL WORK ACCOMPLISSDR CALA2024092700700Unknown · unknownBIRDSTRIKE AT 5500 FEET NEAR WINDOW R1. ATTACHED BIRD STRIKE PICS.FURTHER T/S IN PROGRESSSDR SWAA2024110442486Drain Mast · crackedPANEL 194FL ACCESS PANEL - LH UPPER AFT FAIRING APU DRAIN MAST CRACKED @ BASE TO PANEL ATTACHMENT MKD DOT<SDR VNAA20241102005Mount · corrodedCORROSION WAS DETECTED IN THE ANGLED MOUNT (IN THE AREA COVERED BY THE PROTECTOR PLATE) BTW FS 319.70 AND FS 349.00. ANGLE MOUNTING BTW FS 319.70 AND FS 349.00 AT SERVICE DOOR SURROUND STRUCTURE WAS EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-21-23-101-002-ASDR DALA2024092809493Fillet · crackedSHIP 3269 DISC: A320 / FUSELAGE / RH FR68 AT STGR22 RADIAL FLANGE FILLET LOWER RADIUS / CRACK. ER/A 616977-14AD REV A REQUIRES SECTION II FOLLOW-ON INSPECTIONS FOR CONTINUED AIRCRAFT AIRWORTHINESS. C/A: ER/A 616977-14AD REV A SECTION II FOLLOW-ON INSPECTIONS ASDR VNAA202409240006Helicoil · damaged8000FH PERM REPAIR - SPEED TAPE APPLIED - REPAIR DAMAGED JACKING PAD HELICOIL INSERT LHS AND/OR RHS PERFORM PERM REPAIR OF DAMAGED JACKING PAD HELICOIL INSERT-RHS IAW REO 670-57-22-004. JACKING FITTING HELICOIL INSERT WAS EVALUATED OUT OF LIMITS PER REO 670-5SDR CALA2024092302460Skin · dentedREF AMES NON ROUTINE 174011-0200-0084.PER CUSTOMER REQUEST. FORWARD OF THEL2 DOOR,FORWARD REPAIR DOUBLER, THE UPPER FORWARD CORNER APPEARS TO BE DENTED. MEASURED DENT (A)=7.5" (Y)DEPTH .160" A/Y=46 DENT FOUND TO BE O REPAIR PERFORM INSP PER PART 2 OF LATEST RSDR IXXA20240916001Web · corrodedCORROSION NOTED AT MLG WHEEL WELL CENTER WEB. L/H SIDE STA. 1134 AND 15 TO 24 INCHES UP FROM TOP SIDE OF KEEL BEAM.SDR EVCA0202490600241Unknown · crackedCRACK IN 145 STATIONSDR NACA2024083000001Structure · corrodedFWD CARGO THE UPPER CHORD FOUND CORROSION AT RBL 43 STA 588. REMOVE AND REPLACE THE DAMAGED UPPR CHORD 143T8236-7. NO FURTHER ENGINEERING ACTION IS REQUIRED.SDR 2A6D20240828006Structure · gougedGOUGE AT THE OUTBOARD FLANGE RIVNUT LOCATION IN THE FORM OF SHEAR OUT. THE GOUGE WAS MEASURED TO BE APPROXIMATELY 0.1” X 0.1285”X 0.060”.SDR 2A6D20240828003Bulkhead Web · chafedDAMAGE TO THE 15° BULKHEAD LH WEB (PN: 350A21-1032.86) IN THE FORM OF SEVERAL CHAFES. THE CHAFES WERE REPORTED TO BE 0.20” X 0.10” AND 0.004” DEEP, AS WELL AS 0.20” X 0.30” AND 0.010” DEEPSDR ICRR202408270001Link · crackedFAILED EDDY CURRENT PER NDT MANUAL PART 6, CRJ 700 71-21-101-250SDR CALA2024082702287Structure · corrodedR2 DOOR CHORD CORRODED FROM STA 947 THRU STA 996 APPROX. (FOR SDR/ ESFR REPORTING ONLY) R2 CHORD REPLACED ON BAM N/R 002147183. (FOR SDR/ESFR REPORTING ONLY)
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