JASC 5310
Service difficulty reports · 38,528
Reports filed under 5310 · Fuselage Main, Structure, 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 = '5310' 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 = '5310' 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 CALA2025102310444Door Frame · crackedCRACK INDICATION NOTICED ON RT SIDE E-F POST NR 3 FASTENER HOLE. ACCORDING WITH EA 5310-08195 REV. OP 004 STEP B (26). IF CRACK IS OBSERVED AFTER IT WAS REAMED TO THE PRE COLD WORKED DIAMETER. COMPLIED WITH ECRA 5310-08708. REF AAR RFD NONROUTINE 1000048714. SDR CALA2025102310441Pressure Deck · deformedCOCKPIT FLOOR DENTED JUST AFT OF PEDESTAL. ELEVATED FLIGHT DECK FLOOR WEB BETWEEN BS 250-260 LBL20-RBL20, FOUND AREAS WITH SHARP GOUGES, OUT OF LIMITS IAW SRM 53-10-51-1A-1 ALLOWABLE DAMAGE 1 SECT 41. FLOOR STRUCTURE FIG 105 SHT 2 DETAIL D. REMOVED DAMAGED SDR FDEA202510222063Beam · crackedLOWER CENTER CARGO DOOR UPPER DOOR JAMB CENTER BEAM FOUND CRACKED AT BS 1746.925. LOWER CENTER CARGO DOOR UPPER DOOR JAMB CENTER BEAM CRACKED AT STATION 1746.925 REPAIRED AS PER MD-11 SRM 53-50-15-2R FIGURE 201 REPAIR 2. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2SDR JR2R20251022521Seal Rest · corrodedAFT CARGO DOOR CUTOUT, FWD SEAL REST IS CORRODED OUT OF LIMITS. REPAIREDSDR AALA202601144395Structure · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION TO APU INLET LOWER CHORD LOCATED FROM BS 1148 TO BS 1156 AT LBL 25. REPAIRED CHORD PER EA 369247.SDR JJBA20251120106Crossbeam · corrodedCENTER FUSELAGE III, RT CROSSBEAM AT FRAME 35 CORRODED. CFIII, RH CROSSBEAM AT FRAME 35 BLENDED AND FOUND OUT OF LIMIT. CENTER FUSELAGE III, RH CROSSBEAM AT FRAME 35 REMOVED AND REPLACEDSDR REXA2025110600978Door Sill · corrodedAFT CARGO DOOR SILL IS CORRODED. ON FURTHER INVESTIGATION, FOUND AFT BAGGAGE BAY DOOR FLOOR SILL TO BE PREVIOUSLY REPAIRED DUE TO BEING BEYOND LIMITS GIVEN IN SRM 53-61-23-201-001-A01. PREVIOUS REPAIR PARTS AND DISCREPANT FLOOR SUPPORT CORRODED, AFT BAGGAGE BSDR CALA2025102710558Fitting · crackedSHEAR FITTING AT STATION 540 AND RBL 15.04 IS CRACKED. REMOVED AND REPLACED SHEAR FITTING AT STATION 540 AND RBL 15.04 IAW B737-800 SRM 51-40-02 AND BAC DWG 111A2000 REV ORIGINALSDR YENA2025102301052Door Frame · corrodedDURING HEAVY MAINTENANCE: INSIDE CABIN FWD WET AREA CPCP RELATED TASK- LEFT SIDE BEAM Y503.2 CORROSION FRAME 16 STR 23L; REF HAECO WO 440613 NR 44278. REMOVED SURFACE CORROSION ON FWD WET AREA L/T SIDE Y.503.2 AT STR 23L FR 16 MAT LOSS .022 MATERIAL ALLOWABLE SDR CALA2025102310434Pan · corrodedLOWER FUSELAGE POTABLE WATER SERVICE DOOR CUTOUT INSIDE CORROSION IN SEVERAL AREA. REMOVED AND INSTALLED NEW DOUBLER AND PORTABLE WATER SERVICE PAN AT AFT CARGO IAW SRM 51-40-02-0G-0, DWG 147A7221 AND DWG 147A722.SDR 2025F00248Housing · corrodedREPAIR CORROSION IN NLG HOUSING TUNNEL PER TEXTRON FIELD REPAIR FR-680A-0043-15554. REPAIRED CORROSION IN NLG HOUSING TUNNEL BY REPLACING PANELS PN: 7411212-3, 7411212-4, AND OVER-SIZING HOLE IN TOP SKIN 7411212-9 FROM A BJ4 FASTENER TO A BJ5 FASTENER IAW TEXTSDR EE4Y2025102123355Window Frame · damagedDURING ACCOMPLISHMENT OF THE ALLEGIANT TASK A32X-531135-03-1-001, UPPER FUSELAGE LH WINDSHIELD SIDE POST AT FR4 UPPER ATTACHMENT INTERNAL SIDE FWD INBOARD HOLE WITH CRACK INDICATION DUE TO ITS OVALITY.AIRBUS WAS CONTACTED FOR REPAIR INSTRUCTIONS. AIRBUS PROVIDSDR EE4Y2025102123354Door Frame · crackedDURING ACCOMPLISHMENT OF THE ALLEGAINT TASK A32X-53-260-002, UPPER FUSELAGE AFT PASSENGER CREW DOOR FR66 RH AT DOOR STOP FITTING # 1 LOWER INBOARD FASTENER HOLE WITH CRACK INDICATION WAS FOUND. PERFORMED REPAIR LOCATED AT UPPER FUSELAGE AFT PASSENGER CREW DOORSDR EE4Y2025102123353Door Frame · crackedDURING ACCOMPLISHMENT THE ALLEGIANT TASK A32X-53-260-003, UPPER FUSELAGE AFT PASSENGER CREW DOOR FR60 LH AT DOOR STOP FITTING # 1 LOWER INBOARD FASTENER HOLE WITH CRACK INDICATION WAS FOUND.PERFORMED REPAIR AT UPPER FUSELAGE AFT PASSENGER /CREW DOOR FR68 LH ATSDR AALA202510214204Window Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED FLIGHT DECK CENTER WINDSHIELD FRAMING LEFT HAND CONTINUITY FITTING BETWEEN FR 2 AND FR 3 AT Y0 LEFT. REPLACED CONTINUITY FITTING PER EO 5319Y017-002.SDR AALA202510218031Window Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED FLIGHT DECK CENTER WINDSHIELD FRAMING RIGH HAND CONTINUITY FITTING BETWEEN FR 2 AND FR 3 AT Y0 RIGHT. REPLACED CONTINUITY FITTING PER EO 5319Y017-002.SDR IXXA20251020002Stub Beam · crackedFRAME INNER CHORD IS CRACKED IN THE TRANSITION RADIUS STUB BEAM STA 903.5 RIGHT SIDESDR AALA202511051088Door Sill · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT LEFT PASSENGER / CREW DOOR CUTOUT LOWER SILL BETWEEN FR 66 AND FR 68 AT S23L. REPAIRED LOWER SILL PER SRM 53-41-14-300-001 STEP 2.A FIGURE 001 PRINCIPLE 5.SDR AALA202511058831Door Sill · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT AFT PASSENGER / CREW DOOR CUTOUT LOWER SILL EXISTING REPAIR BETWEEBN FR 66 AND FR 68 AT S23R. REPAIRED LOWER SILL PER SRM 53-41-14-300-001. PRINCIPLE 7.SDR AALA202601142879Angle · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON R2 DOOR LOWER CUT OUT INNER CHORD (CREASE ANGLE) LOCATED BETWEEN BS 947 AND BS 986.5, AT RBL 45. REPLACED CREASE ANGLE PER AARD 51-00-05-1.SDR CALA2025102710556Window Frame · crackedLEFT NR 3 WINDOW POST HOLE NR 3 IS CRACKED IN THE 3 AND 9 O'CLOCK POSITION. ACCOMPLISHED REO-G25600 ACCOMPLISHED REPAIR AT FLIGHT DECK LT NR 3 WINDOW POST,REMOVED DAMAGED,FABBED AND INSTALLED -1 DOUBLER -2 TRIPLER,-3 FILLER, AND INTERNAL DOUBLER IAW REO:G256SDR DALA2025102207716Door Frame · crackedSHIP 9520 CRACK OF 0.350IN LENGTH WAS FOUND ON LH OVERWING FRAME STA Y=737 IN REFRENECE TO CARD 5310-01439-01B / JOB 068-0003, STEP 4. LEFT OVERWING FRAME STA Y=737 WAS REPLACED PER B717-200 SRM 51-41-02-0G AND 51-41-05-0G. (1258141)SDR AALA202510202957Door Sill · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT AFT PASSENGER / CREW DOOR CUT OUT LOWER SILL BETWEEN FR 66 AND FR 68 AT S23L. REPLACED SILL PER SRM 51-72-11.SDR SWIA2025102700017Door Frame · dentedDURING REPLACEMENT OF APU INLET DOOR FRAME SUPPORT 5-OFF OVERSIZED HOLES AND DENT DAMAGE WERE FOUND BETWEEN BS 654.5 - 672.2 AT S4L AFFECTING THE STACK UP OF S4L, BS 654.5 FRAME SECTOR, MTG FITTING AND CLIP. COMPLIED WITH REO 601R-53-61-8400 REV-, DATED 2025-1SDR DALA2025102407822Door Sill · corroded1 REPORTED BY LINARES 00705131 MSP 17OCT25 ENTR 00532877 W FWD PAX DOOR - CORROSION NOTED AROUND MULTIPLE HOLES ALONG LOWER SILL AND SILL FLOOR (M)(P) LOG-PAGE UPDATED @ 17OCT25 1800 UTC 02 CORR BY REYNOLDS 00390101 MSP 17OCT25 ATA 5331 RII: N ENTR 00532877 W SDR DALA2025102407811Door Sill · corrodedDURING H-CHECK IN MSP, MAINTENANCE WAS ACCOMPLISHING EO WORKCARD 5331-01297-01C (SB BD500-530010 ISSUE 004). DURING MODIFICATION , THE FWD CARGO DOOR SURROUND STRUCTURE C02313004-005 LOWER SILL , AND C02312110 BOTTOM SKIN WERE FOUND CORRODED AFTER SCUFF PLATE SDR CALA2025102110336Fitting · damagedEA-3271-01017-001 TAIL SKID ASSEMBLY SUPPORT FITTING REPLACEMENT UNDER WORK INSTRUCTIONS STEP 7 (B)(4) PRE-EXISTING HOLE AT .250. COMPLETED ALL STEPS PER UAL ECRA 5380-01430 REV- FOR REPAIR.SDR 2025FA0000723Sump · brokenSTATIC CONDENSATION BULB P/N S-1258-1 FOUND SEPARATED FROM AN 1/8 PIPE BY PIPE 90 DEGREE FITTING. THESE CONDENSATION BULBS ARE OF VERY CHEAP PLASTIC AND ARE FAMOUS FOR LEAKING RIGHT OUT OF THE BOX. THERE SEEMS TO BE NO OTHER PART OF BETTER QUALITY. I HAVE SEENSDR SWIA20251201016Plate · damagedCOMPLY WITH REO 670-53-22-099, SPLICE REPAIR TO MTG PLATE BETWEEN BS 319 - 333, RT. COMPLIED WITH SPLICE REPAIR TO MTG PLATE BETWEEN IAW REO 670-53-22-099 REV-. ALL CHECKED GOOD.SDR JJBA20251024059Door Frame · corrodedCORROSION AT RT SERVICE DOOR ENTRANCE FRM 20-22 RBL 19. REMOVED AND REPLACED RT SERVICE DOOR ENTRANCE FROM 20-22 RBL 19.SDR JJBA20251024057Rib · crackedRH WHEEL WELL RIB CRACKED IN MULTIPLE SPOTS. REMOVED AND REPLACED RH WHEEL WELL RIB.SDR JJBA20251024055Rib · crackedLH WHEEL WELL RIB CRACKED IN MULTIPLE SPOTS. REMOVED AND REPLACED LH WHEEL WELL RIB.SDR HALA2025FA0000720Frame · corrodedAPU FIRE BOTTLE ACCESS COMPARTMENT ACCESS CUTOUT AFT SIDE FR 94A ASSEMBLYY FOUND CORROSIONSDR VNAA20251015048Fitting · corrodedFITTING P/N SH670-33389-1 @ F.S 533 STR 25L IS CORRODED. INSTALLED NEW FITTING P/N SH670-33389-1 IAW CRJ 700 SRM 51-42-21-001-001-A01 & CRJ 700 SRM 51-45-00-001-001-A01 SH670-33389-1SDR VNAA20251015045Window Frame · chafedPILOT AND COPILOT'S WINDOW UPPER SILL IS GOUGED ABOVE THE LH AND RH WINDSHIELD SIDE POST. REPAIRED UPPER SILL IAW MHIRJ REO 670-53-11-2088 REV-.SDR SWIA2025121901015Drain · misrepairedWHILE WORKING SB 601R-57-054 INADVERTENTLY REAMED SATELLITE HOLES FOR WATER DRAINS AT BL 0 ON LT & RT SIDES BETWEEN STRINGERS 14-15. REPAIRED SATELLITE HOLES FOR WATER DRAINS AT BL 0 ON LT AND RT SIDE BETWEEN STRS 14-15 IAW REO 601R-57-21-3982 REV -.SDR CALA2025102710550Stop Fitting · gougedAFT ENTRY DOOR (L2) UPPER STOP FITTING HAS GOUGE. REMOVED AND REPLACED L-2 DOOR UPPER FWD STOP FITTING IAW DWG 147A6125 REV- AND SRM 51-40-02-0G-0.SDR DALA2025102007622Door Sill · no discrepancyERA 622251-14 REV A HAS FOLLOW-ON INSPECTION FOR THE FORWARD CARGO DOOR SILL AREA. ACCOMPLISH SECTION II WITHIN 32,191 FC OR 57,868 FH. THEN EVERY 9,400 FC OR 16,450 FH THEREAFTER. ASSOCIATED ER/A 00-622251 ADDED FOR AC 8145. (LP# 1253822)SDR FDEA202510152005Tee Angle · crackedWHILE ACCOMPLISHING NON DESTRUCTIVE TEST HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION, HOLE A AT TEE CAP (NCA6042-15) FOUND WITH CRACKED. CRACK AT TEE CAP (NCA6042-15) HOLE A REPAIRED AS PER EA # 1-5330-T0385040 PART 1 TITLE: FUSELAGE - PLATES & SKINS SDR SWI2026F00029Retainer · chafedFWD UPPER RETAINING PLATE FOR LT WING STUB FAIRING CHAFING AGAINST FUSELAGE EXTERNAL SKIN. REPAIRED FWD UPPER RETAINING PLATE FOR LH WING STUB FAIRING (APRON SKIN) IAW REO 601R-53-41-3365 REV -. COMPLIED WITH TASK CARD 51-900-1003-SKY.SDR JJBA20251112035Sill Drain · corrodedCORROSION ON MOP SILL FRAMES 42-49 STR 16R. REMOVED CORRODED MOP SILL AND INSTALLATION OF NEW MOP SILL LOCATED AT FR 42-49 STGR 16LSDR CALA2025101710223Door Frame · crackedUPON REMOVAL OF R1 DOOR INNER CHORD FOUND FWD STUB FRAME LOWER CORNER CRACKED BS 296, WL 210. COMPLETED INSTALLATION OF FWD LOWER STUB FRAME IAW SRM 51-40-02-0G-0, AND DWG 141A8370.SDR CALA2025101710222Crease Beam · corrodedFWD WET AREA RT, R1 DOOR CREASE BEAM BS 270-340 HAS CORROSION ON TOP AND SIDE OF ANGLE. REMOVED AND REPLACED CREASE BEAM AT R1 DOOR IAW SRM 51-40-02 AND DWG 141A8310 REV -.SDR VNAA20251014020Landing · corrodedFUSELAGE PANEL SUPPORT STRUCTURE BETWEEN F.S. 629 TO F.S. 613 IS CORRODED. REPLACED LOWER STRAP PN SH670-39054-3 AT FS629 IAW CRJ-700 SRM 51-42-06-001-001-A01, AND 51-40-11-001-001-A01.SDR EE4Y2025101423333Box Beam · crackedDURING ACCOMPLISHMENT OF THE ALLEGIANT TASK A32X-53-240-001, UPPER FUSELAGE PAX CABIN FR43 S-15 RH AT SIDE BOX BEAM AREA,MID AND REAR OPEN FASTENER HOLE LOCATION WITH CRACK INDICATION WAS FOUND.AIRBUS WAS CONTACTED REQUESTING REPAIR INSTRUCTIONS. AIRBUS PROVIDSDR VNAA20251014012Door Frame · crackedUPPER ELECTRIC ACCESS DOOR SURROUND STRUCTURE FS173.00 TO FS193.00 DOOR LANDING RH PN/ CC670-33151-4 FOUND TO BE CRACKED AT AFT LATCH CUT OUT. REMOVED AND REPLACED DOOR LANDING IAW CRJ-700 SRM 51-40-11-001-001-A01, SRM 51-42-06-001-001-A01, AND MHIRJ REO 670SDR EE4Y2025101423332Box Beam · crackedDURING ACCOMPLISHMENT OF THE ALLEGIANT TASK A32X-53-240-001, UPPER FUSELAGE PAX CABIN FR43 S-15LH AT SIDE BOX BEAM AREA, REAR OPEN FASTENER HOLE LOCATION WITH CRACK INDICATION WAS FOUND.AIRBUS WAS CONTACTED REQUESTING REPAIR INSTRUCTIONS. AIRBUS PROVIDED THE RSDR EE4Y2024091720906Box Beam · crackedDURING ACCOMPLISHMENT OF THE ALLEGIANT TASK A32X-53-240-001, UPPER FUSELAGE PAX CABIN FR43 S-15LH AT SIDE BOX BEAM AREA, REAR OPEN FASTENER HOLE LOCATION WITH CRACK INDICATION WAS FOUND.AIRBUS WAS CONTACTED REQUESTING REPAIR INSTRUCTIONS. AIRBUS PROVIDED THE RSDR FDEA202510141981Door Frame · crackedLEFT 3 AFT DOOR JAME LOWER WEB AT STATION 1310 FOUND CRACKED. CANIN-LEFT 3 AFT DOOR JAME LOWER WEB AT STATION 1310 CRACKED REPAIR CARRIED OUT AS PER MD-11 SRM 53-40-15-2R FIGURE 201 REPAIR 3. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR DALA2025101407500Bracket · damagedTOOLING DAMAGE ON BRACKET AT FASTENERS FWD SIDE OF FRAME 26 @ P'6. CORRECTIVE ACTION: REPAIRED PER ERA 628177-14 REV. ORIG. (1251281)
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