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 HNAA2024071900551Structure · cracked53-2024 LH REAR FUSE II, CRACK SUSPECTED AROUND 9 RIVETS BTW FR77-80 STR3-7L. REPAIRED IAW EO 1-53-24-0362.SDR AALA202406076515Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN CENTER WING BOX FORWARD SPAR UPPER SHEAR FITTING AT BS 540 AND RBL 54.60. REPLACED SHEAR FITTING PER AARD 57-14-00-1 REPAIR 1. THIS ACCOMPLISHES BOEING SB-737-57-1309.SDR ABXA2024060300420Unknown · vibrationAT LEVEL OFF FL290 HEARD A POP UNDER OUR FEET FOLLOWED BY NOTICEABLE VIBRATION.SDR UIEA2024052300413Structure · corrodedCENTER SECTION AFT FACE FOUND CORROSION ( RH O/J PUMP BONDING AREA )(<P>CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND SRM 51-20-01 REV 100 DATE 20 FEB 2024. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024052600447Structure · cracked1EA CRACK WAS FOUND ON LH NOSE WHEEL WELL FORWARD CORNER FASTENER HOLE(<P>STA 240 LH SIDE PANEL CHORD P/N: 65B07942-609 CRACK AREA REPAIRED IAW RI-53-00-16890 REV A. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024052600448Structure · cracked1EA CRACK WAS FOUND ON THE FASTENER HOLE AT RH STA 240 #3 RD LAYER ( SHIM )(<P>STA 240 RH #3 RD LAYER ( SHIM ) FABRICATED AND INSTALLED IAW RI-53-00-16890 REV A. NO FURTHER DEFECTS NOTED. </P>)SDR SWAA2024062789557Not Reported · crackedCRACK ON INNER CHORD LOCATED ON STA 294.5 AND WL 208.1 RBL 53 AT FWD GALLEY AREA 2024-341087<[01] REPLACED INNER CHORD LOCATED BTW STA 268.25 TO STA 360 AND WL 208.1 RBL 53 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02; DWG 141A8310 SHEET 25 REV: AND DWG 141A83SDR IPXA2024061188975Unknown · corrodedL/H STA 1040 LBL 0-18 HAS CORROSION.SDR COEA2024072606917Skin · corrodedWO 254917 NR 200081 HEAVY CHECK COE/MAJOR REPAIR DISCREPANCY: INTERNAL FUSELAGE HAS LEVEL 2 CORROSION AT STRINGER 10AL BETWEEN FRAMES 20-21 UNDER INSULATION STANDOFF. CORRECTIVE ACTION: REPAIRED PER ATR42 SRM 530000-300-803-A01.SDR FDEA202405180684Stiffener · crackedMEC, LT TUNNEL, FWD SIDE OF STA 246 BEAM HAS 1 EACH CRACKED "L" BRACKET (PN: 141T5814- 136) REMOVED AND INSTALLED NEW STIFFENER PN: 141T5814-136. REF SRM 51-40-02-0G AND BOEING DWG 141T5104, ALODINE AND PRIMED AS REQUIRED. REF SRM 51-20-01-0G. (MINOR REPAISDR SWI2024F00589Structure · corrodedAFT BAGGAGE-BAY UNDERFLOOR FS1000-FS1015 STG26L CORROSION, HN00161455 (C-CHECK RO 7/17/2024) ACCOMPLISHED REPAIR OF STG26L FS1000-FS1015 - REF CRJ 700 SRM 53-00-03-201-001-A01 AND DWG NO MM670-35007 REV W. PRESSURIZATION LEAK CHECK OF FASTENERS IN THSDR CALA2024052001513Unknown · vibrationLOUD NOISE AND VIBRATION FROM NOSE AREA PASSING 25000FT LOCKED FOR FERRY FLIGHT UNLOCKED FOR TECH UPDATES. UPDATED MAA CODE FIX USING VENDOR MAA SCREEN UPDATED MAA CODE FIX USING VENDOR MAA SCREEN FOUND FWD ACCESS DOOR LOOSE ON BOTH FWD ENDS. NO PRESSURIZATIONSDR IPXA2024051574929Unknown · vibration**ATB** **SDR FILED OPEN** CLIMBING THROUGH 3500 FT EXPERIENCED HIGH VIBRATION THAT SHOOK THE A/C.WE LEVELED OFF AT 6000 AND REDUCED TO GREEN DOT. VIBRATION WENT AWAY. NO ECAM OR ABNORMAL INDICATIONS. FIBER GLASS DUST CAME OUTSDR IPXA2024062760200Hinge · damagedDAMAGE FOUND IN HOLES ON MIDDLE HINGE. STEEL (14D) ALUMINIUM (12F, 13F, 15F). OPENSDR DALA2024051505231Unknown · crackedSHIP 178 ER/A 617880-14AD ISSUED FOR CRACKS ON THE OUTER CHORD AT STA 1809.5 AND S-12A RH. CORRECTIVE ACTION: ACCOMPLISH ER/A 617880-14AD SECTION II WITHIN 36 MONTHS OR 6,000FC WHICHEVER OCCURS FIRST FOLLOWING THE ACCOMPLISHMENT OF SECTION I AND EVERY 36 MONTHSDR IPXA2024052337817Drain · unknown*** SUPPLEMENTAL SDR *** ADD SDR FOR EO-82173-JIC001 (FUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R) CONDITION CHECK OK.SDR SWAA2024052884708Panel · corrodedPANEL # 192F CORRODED WHERE DME#1 ATTACHES.<[01] REMOVED AND REPLACED PANEL #192F AS PER REFS B737 AMM 53-51-21-000-802 & AMM 53-51-21-400-802.SDR UIEA2024050800360Screw · interferenceFND EXISTING SCREW INTERFERES WITH WIRE AT STA 560 NEAR RBL 65(<P>1. ACCOMPLISH EI T2024A53M-1060 REV 1 2. JOB COMPLETED AND CONDITION CHECK NORMAL</P>)SDR CALA2024051701495Angle · crackedL/H PACK BAY AFT WALL REAR SPAR UPPER ANGLE CRACKED. SUPPORT TASK NSA EMX N/R00196.SDR 2A6D20240508002Crossbeam · corrodedTHE RH X2244 CROSSBEAM (PN: 350A21-0861.20) IS CORRODED IN AN AREA ON THE LOWER OUTBOARD CORNER OF THE CROSSBEAM. THE DAMAGE WAS REPORTED TO BE 0.572” X 0.179” AND 0.028” DEEPSDR JJBA20240603069Support · corrodedCORROSION FOUND ON LH SILL #3. LH SILL #3 BLENDED OUT OF LIMIT. LH SILL #3 REMOVED AND REPLACEDSDR JJBA20240603068Support · corrodedLH SILL #2 FOUND CORRODED. LH SILL #2 BLENDED OUT OF LIMIT. LH SILL #2 REMOVED AND REPLACEDSDR CALA2024050901413Unknown · noiseFAS REPORT EXTREMELY LOUD BANG AT ROTATION FELT LIKE SOMETHING HIT THE FUSELAGE ON L SIDE OCCURRED DURING AIRCRAFT ROTATION WHEN THE NLG WAS SERVICE CHECK BEFORE THE FLIGHT TO ZURICH NO DEFECTS WERE NOTED OFF THE RUNWAY BUT THE MLG WAS STILL ON THE EITHER. GRSDR UIEA2024050800344Reveal · crackedLH 5 DOOR FWD CUTOUT, DOOR RELEASE HANDLE AREA REVEAL PANEL CRACK. STA 2240 WL 250(<P>1) REPAIR DAMAGE AREA IAW W/S 40322 (SRM 53-60-15-2R-7 REV 100). 2) JOB COMPLETED & CONDITION CHECK NORMAL</P>)SDR SWI2024F00591Striker · bentFORWARD EQUIPMENT COMPARTMENT, LEFT DOOR UPPER SEAL STRIKER IS BENT AT BOTH HINGE POINTS. HN00158016 (C-CHECK RO 7/17/2024) REMOVED AND REPLACED FORWARD EQUIPMENT COMPARTMENT, LEFT DOOR UPPER SEAL STRIKER /LANDING (P/N CC670-33265-1) REF CRJ-700 SRM 5SDR SWIA20240505Structure · crackedFORWARD EQUIPMENT COMPARTMENT, RH DOOR AFT LATCH CUTOUT APPEARS CRACKED. HN00157999 (C-CHECK RO 7/17/2024) LOCATED, DILLED AND INSTALLED NEW RH LOWER TRU BAY DOOR LANDING IAW REO 670-53-11-1969 REV -- DATED 2024-06-05 / DWG C670-33040 REV. -G AND CRJ SDR IPXA2024062404353Panel · tornPANEL 132SG HAS TORN FIBERGLASS AND EDGE DAMAGE. REPAIRED FIBERGLASS BREAKS AND EDGE DAMAGE IAW EO NO: A300-5320-42722-F.SDR IPXA2024062404288Panel · tornPANEL 152QF HAS TORN FIBERGLASS AND DELAMINATED. REPAIRED TORN FIBERGLASS AND DELAMINATION OF PANEL 152QF, I.A.W. EO. A300-5320-42722-F.SDR IPXA2024062104353Panel · damagedPANEL 132SG HAS TORN FIBERGLASS AND EDGE DAMAGE. DOT 109/078. REPAIRED FIBERGLASS BREAKS AND EDGE DAMAGE IAW EO NO: A300-5320-42722-F. MAJOR REPAIRSDR IPXA2024062104288Panel · damagedPANEL 152QF HAS TORN FIBERGLASS AND DELAMINATED. DOT 109/075. REPAIRED TORN FIBERGLASS AND DELAMINATION OF PANEL 152QF, I.A.W. EO. A300-5320-42722-F. MAJOR REPAIRSDR IPXA2024062104413Panel · damagedPANEL 132G HAS FIBERGLASS DAMAGE AND EDGE DAMAGE. DOT 109/080. REPAIRED FIBERGLASS TORN AND EDGE DAMAGE IN PANEL 132 QG, IAW (SREO) EO NO: A300-5320-42722-F. MAJOR REPAIRSDR IXXA2024050204Skin · damagedACCOMPLISH PERMANENT REPAIR OF LIGHTNING STRIKE AT STA 387 STR 33LSDR CALA2024051301466Panel · corrodedCABIN STA952 TO 955 RBL84 TO 87 CENTER SECTION UPPER SURFACE FOUND CORROSION. CABIN STA952-955 RBL84-87 CENTER SECTION UPPER SURFACE PANEL AS PER ECRA 5714-01214 REV - PART 1 ITEM 3 , CREATED NO.1 INTERIM REPAIRED AS PER ECRA5714-01214 REV - PART 1 LP 783689SDR QMLA2024050220048Control Panel · crackedDURING 12 MO, 2" CRACK FOUND IN AVIONICS PANEL P# 429-030-602-109 (BH429 IPC 53-59 ITEM 005) CABIN SIDE BELOW LH AFT MOUNT OF ADIU, LOCATION APROX. STATION 323” X -3.0” BL UP ON REMOVAL OF ADIU FOUND ADIU HARDWARE RETAINER UNDER RH FWD LEG OF ADIU, AND CRACKISDR HALA20240429117Spring · brokenETOPS-DURING X2 INSPECTION FOUND MULTIPLE SPRINGS BROKEN AFT CARGO RAISED FOR IDENTIFICATION. REPLACED SPRINGS AS REQUIRED OK FOR SERVICESDR HALA20240429116Spring · brokenETOPS-DURING X2 INSPECTION FOUND MULTIPLE SPRINGS BROKEN FWD CARGO RAISED FOR IDENTIFICATION. REPLACED SPRINGS AS REQUIRED OK FOR SERVICESDR SWIA2024061700424Structure · ground damageTRANSFER FROM EAML 1337245 : PRIOR TO ATTACHING JET BRIDGE TO AIRCRAFT, RAMP CREW DROVE THE BELT LOADER INTO THE AIRCRAFT NEAR BIN 3. ENTIRE AIRCRAFT SHOOK. UPON INSPECTION FRAME APPEARS BENT DIRECTLY UNDER BIN 3. AIRCRAFT SHORED REF ISE-STR-24-023. AIRCRAFT SSDR SWAA2024052877673Access Panel · damagedACCESS PANEL 193B HAS AN ELONGATED HOLE R/H SIDE ALF DOT 068<[01] APPLIED PERMANEMT REPAIR ON DAMAGE AREA AS MARKED ON PANEL #193B AS PER B737 SRM 51-70-04-2R-9 PARAG 4-D-M; MATERIAL USED: PO#2061896; PO#1690463; TOOL USED: HOT BONDER ID170006; DUE DATE 06-07-SDR HNAA2024051600405Shear Tie · crackedE031911 POSSIBLE SHEAR CLIP CRACKED AT F75, BETWEEN STR 07L-06L. REMOVED CRACKED SHEAR CLIP AT FR 75 BTW 07L-06L, FABRICATED, PREPPED AND INSTALLED SERVICEABLE SHEAR CLIP IAW E01-53-24-0270, EMB 145 SRM 51-40-02, SRM 51-30-01 STEP 2.ISDR WX0A2024041832015Not Reported · damaged(MAJOR REPAIR) FOUND 1 CRACK RADIATING FROM RIVET AT RH FUSELAGE, ONE RIVET FORWARD OF FR14, BETWEEN Z+780 & Z+950. CRACK RADIATES AFT 0.118"" FROM RIVET/CUT OUT DAMAGE FABRICATED, ALODINED, PRIMED AND INSTALLED R/H FILLER AND DOUBLER IAW ERO# R5311-0245 REV SDR CALA2024041501061Plate · missingPDA RIGHT SIDE PROTECTIVE PLATE (NOSE WHEEL SPIN BRAKE) WAS FOUND MISSING FROM ACFT ON ARRIVAL WHILE TROUBLESHOOTING LP 7631557 SDR COMPLETED. INSTALLED PROTECTIVE PLATE . REF AMM 32-42-52-960-001-A.SDR SWAA2024051573720Unknown · crackedCRACK ON INNER CHORD LOCATED ON STA 294.5 AND WL 208.1 RBL 53 AT FWD GALLEY AREA 2024-253372<[01] REPLACED NEW INNER CHORD AND FASTENERS<BR>LOCATED BTW STA 268.25 TO STA 360 AND WL 208.1 RBL 53 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02 AND DRAWING #141A8310SDR WX0A2024041832014Not Reported · cracked(MAJOR REPAIR) FOUND 2 CRACKS RADIATING FROM RIVET AT LH FUSELAGE, ONE RIVET FORWARD OF FR14, BETWEEN Z+780 & Z+950. 1 EA. CRACK RADIATES UP 0.250"" FROM RIVET & 1 EA CRACK RADIATES AFT 0.375"" FROM RIVET/CUT OUT DAMAGE INSTALLED FILLER AND DOUBLER IAW ERO R53SDR JJBA20240418044Floor Support · crackedAT CF1 FLOOR STRUCTURE AREA, CORROSION AND (3X) CRACKS FOUND ON LH OMEGA BEAM #1 BTW FR 19-23. OMEGA BEAM REPAIRED WITH 3 DOUBLERS ON INBD VERTICAL FLANGE AT FR 21, 22, AND 23 (CORROSION LEVEL 1)SDR UIEA2024032100169Ladder · crackedM/D - CREW LADDER #7 STEP FWD & AFT AREA FOUND CRACK (FROM BOTTOM)(<P>CRACK STEP FWD AND AFT AREA REPAIRED AS PER RI-25-50-16803 REV A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024032400208Not Reported · cracked2EA CRACK WERE FOUND ON LH BS 2231 S23L FASTENER HOLE(<P>CRACK AREA REPAIRED AS PER SRM 53-60-15-2R-2 REPAIR 2 FIG 201 DETAIL II, THIS REPAIRED IS CAT B. NO FURTHER DEFECTS NOTED</P>)SDR FDEA202404090451Fitting · crackedRH WING - BASIC WING STRUCTURE FR40 STGR32R - STGR33R I/B HOLE FOUND CRACK COMPLIED WITH FEDEX EA 6-5710-T0378762 REPAIRED THE RH WING BASIC WING STRUCTURE RH FR40 STGR32R - STGR33R FWD FITTING LOWER RADIUS CRACKED HOLE A. TITLE: WINGS - BASIC WING STRUCTUSDR SWAA2024051572069Unknown · corrodedCORROSION INNER CHORD LOCATED BTW STA 328 TO STA 344 LBL 58 AND WL 208.1 AT FWD GALLEY AREA 2024-253241<[01] REPLACED NEW INNER CHORD LOCATED BTW STA 328 TO STA 344 L/H SIDE AND WL 208.1 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02 AND DWG 142A0050 SHEET 15 RESDR R61A2024040400162Seal · damagedDURING AGEING AIRCRAFT INSPECTION. DAR FINDING#19 A SPOT CHECK OF THE AFT AVIONICS SMOKE SEAL DISCOVERED TE L/H SMOKE SEAL IS DAMAGED.SEAL REPAIRED IAW AMM 25-84-01-801-A.SDR AALA202404116142Fitting · not reportedAIRCRAFT IN BASE MAINTENANCE: DUE TO THE MAJOR REPAIR BEING ACCOMPLISHED ON THE FLIGHT DECK WINDSHIELD FRAMING THE RIGHT HAND CONTINUITY FITTING BETWEEN FR 1 AND FR 2 AT Y0 MUST BE REPLACED PER THE INSTRUCTIONS ON EA 351275. MAINTENANCE REPLACED THE RIGHT HAND
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