JASC 5344
Service difficulty reports · 2,428
Reports filed under 5344 · Fuselage, Door Hinge, 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 = '5344' 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 = '5344' 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 AALA202212122773Hinge · lack of lubeAIRCRAFT WAS NOT GROUNDED: COCKPIT DOOR HARD TO CLOSE. LUBRICATED COCKPIT DOOR HINGE AND DOOR LATCH OPERATIONS CHECK NORMAL PER AMM 52-51-00.SDR AALA202212128962Hinge · lack of lubeAIRCRAFT WAS GROUNDED: CABIN ENTRY DOOR FWD ENTRY LIGHT ILLUMINATED AFTER LANDING. DOOR DIFFICULT TO OPEN. LUBED DOOR HINGES, OPERATED DOOR SEVERAL TIMES. NO DEFECTS NOTED.SDR SWIA2022122967060Hinge · chafedWHILE INSPECTING REPAIR ON PAX DOOR PIANO HINGE HALF ON DOOR SIDE HAS CHAFES ON THE FOLLOWING LUGS (FROM FWD SIDE TO AFT): 1, 2, 4, 5, 12, 13, 15, 16, 19, 20, 22, 24, 25, 26, AND 27. JOB 9780385 OP 00053, CAMP 25881132 FOUND ALL LUGS ON FUSELAGE SIDE OF HINGE SDR FDEA202212053027Hinge Pin · corrodedHINGE PIN AND LOBES ARE RUSTED ON AFT LWR CARGO DOOR. REMOVED RUST ON HINGE PINS AND LOBES ON AFT CARGO DOOR. REMAINING THICKNESS AT SPOTFACE .490 WITHIN LIMITS IAW 52-30-16-1A, FIG 101, SHEET#2, MAJOR REPAIR.SDR AALA202212061188Hinge · out of adjustAIRCRAFT WAS NOT GROUNDED: LAVATORY DOOR HARD TO OPEN AT AFT RIGHT LAVATORY. ADJUSTED AFT RIGHT LAVATORY DOOR HINGE PER AMM 52-50-00.SDR SWIA2022122967057Cover · chafedAFT CARGO DOOR PIANO HINGE BOLTS CHAFING THROUGH PHENOLIC. REMOVED AND REPLACED WITH NEW COVER SPRING AT AFT CARGO DOOR IAW AMM 20-10-01.SDR DALA2022120207733Bolt · loose2L DOOR HARD TO CLOSE/ARM. FOUND LOWER DOOR HINGE BOLTS LOOSE. RETORQUE BOLTS PER B757 AMM 52-11. OPS CHKS GOOD. (9401788)SDR AALA202212021806Hinge · damagedAIRCRAFT WAS NOT GROUNDED: FLIGHT DECK DOOR DIFFICULT TO OPEN DURING FLIGHT. MAINTENANCE REPLACED DAMAGED UPPER DOOR HINGE HARDWARE PER AMM 52-51-00-820-001.SDR AALA202211296737Hinge · lack of lubeAIRCRAFT WAS NOT GROUNDED: LEFT HAND AFT LAVATORY DOOR STICKS. MAINTENANCE LUBRICATED DOOR HINGE PER AMM 25-50-00 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.SDR AALA202211289277Hinge · stickingAIRCRAFT WAS NOT GROUNDED: LAVATORY D DOOR IS DIFFICULT TO OPEN AND CLOSE AND ALSO DIFFICULT TO LOCK. FOUND LAVATORY "D" DOOR JAMMING ON FLOOR SILL WITH LOOSE DOOR HINGE. RESECURED PER AMM 20-50-00. OPERATIONS CHECKED GOOD.SDR AALA2023012341001Hinge Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION ON LEFT HAND MAIN LANDING GEAR DOOR FORWARD HINGE FITTING AFT LUG WEB RADIUS. MAINTENANCE REPLACED HINGE FITTING PER SRM 51-42-11.SDR SWIA2022122767026Lug · corrodedPAX DOOR HINGE DOOR SIDE LUGS NR 1- 27 TOP OUTER SURFACE HAVE CHAFING, AND LUG 27 ROLL-PIN HOLE IS ELONGATED. REMOVED AND TREATED DAMAGE ON PAX DOOR HINGE LUGS 1 THRU 27 AND REPAIRED HINGE ROLL PIN ELONGATED HOLE. IAW REO 601R-52-11-2945 REV -, & REO 601R 52SDR AALA202211302752Hinge · stickingAIRCRAFT WAS NOT GROUNDED: AFT LEFT LAVATORY DOOR DIFFICULT TO OPEN OR CLOSE AND LOCK. ADJUSTED LEFT AFT LAVATORY DOOR HINGE PER AMM 25-40-14.SDR DALA2022112307519Hinge Fitting · crackedCRACK INDICATION FOUND ON FWD FACE FWD LUG OF LH FWD KEEL BEAM HINGE FITTING. COMPLIED WITH ERA 603400-14AD REV.ORIGINAL.SDR AALA202211141739Hinge · out of adjustAIRCRAFT WAS NOT GROUNDED: LAVATORY D DOOR STICKS OPENING AND CLOSING. MAINTENANCE ADJUSTED DOOR HINGE PER CMM 25-47-21.SDR WX0A202211141780Hinge Fitting · damagedNRC 1000-0072: 33284-002 RH MLG DOOR FWD HINGE FITTING, DAMAGE SUSPECTED AROUND BOLT HEAD/RH MAIN LANDING GEAR FWD HINGE FITTING AROUND BOLT AND UNDERNEATH HEAD, GOUGE REMOVED AND FOUND STRUCTURALLY ACCEPTABLE AS PER AIRBUS DOSSIER # 81134396 AND COMPLY AS PESDR AALA202211098666Hinge · out of adjustAIRCRAFT WAS NOT GROUNDED: LAVATORY D DOOR DIFFICULT TO OPEN OR CLOSE. ADJUSTED LAVATORY D DOOR HINGE PER AMM 25-40-14. OPERATIONAL CHECK GOOD.SDR DXTA2022110473290Hinge · damagedMAIN DOOR: REAR HINGE ON TOP TREAD OF MAIN CABIN ENTRY DOOR IS BROKEN, TREAD STICKS UP APPROX 3/4 OF AN INCH. TRIPPING HAZARD. ACCESSED AIRCRAFT AND NOTED THE TOP STEP OF THE MAIN CABIN ENTRY DOOR TO BE UNEVEN, GAINED ACCESS TO HINGES. PERFORMED GVI OF CABIN SDR DALA2022110407165Hinge · corrodedAIRCRAFT 8127, BOTH HINGES ON LAV WASTE SERVICE DOOR (146 BR) CORRODED. CORRECTIVE ACTION: REPLACED WASTE BOX PAN, INBD HINGE FITTINGS, INBD HINGE ARM FITTINGS, AND REMOVED CORROSION ON WASTE B=DOOR DOUBLER PER ER/A 603257-14. LP 2481191SDR AALA202211300349Hinge Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION ON LEFT HAND MAIN LANDING GEAR DOOR FORWARD HINGE FITTING AFT LUG WEB IN THE CORNER RADIUS ON THE KEEL BEAM. MAINTENANCE REPLACED HINGE FITTING PER EA 339820.SDR AALA202211160349Hinge Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION ON LEFT HAND MAIN LANDING GEAR DOOR FORWARD HINGE FITTING AFT LUG WEB IN THE CORNER RADIUS ON THE KEEL BEAM. MAINTENANCE REPLACED HINGE FITTING PER EA 339820.SDR FDEA202210302698Hinge · wornCABIN-UPPER CARGO DOOR, DOOR HINGE FITTING (FUSELAGE SIDE) PART NUMBER ACA7223-1 FOUND 1ST TO 11TH LOBES FROM FORDWARD FOUND OUT OF LIMIT. LOBE HOLES NUMBER 1 TO NUMBER 11 FROM FORWARD AT CABIN - UPPER CARGO DOOR , DOOR HINGE FITTING REWORKED AND FOUND NUMSDR FDEA202210302697Hinge · wornCABIN- UPPER CARGO DOOR, DOOR HINGE FITTING FOUND 1ST TO 11TH LOBES FROM FORWARD FOUND OUT OF LIMITS. LOBE REWORKED AND FOUND NUMBER 1 TO NUMBER 5 HOLES EXCEED LIMIT. NUMBER 6 TO NUMBER 11 HOLES WITHIN LIMIT AS PER MD- 11 SRM52-30-16-1A FIGURE 101 SHEESDR FDEA202210302696Hinge · wornCABIN-UPPER CARGO DOOR, DOOR HINGE FITTING PART NUMBER ACA7332-1 FOUND 1ST TO 9TH LOBES FROM FORWARD FOUND OUT OF LIMIT. LOBE HOLES NUMBER 1 TO NUMBER 9 FROM FORWARD AT CABIN-UPPER CARGO DOOR. DOOR HINGE FITTING PART NUMBER ACA7332-1 REWORKED AS PER MD-11 SDR SWIA202266977Hinge · damagedPAX DOOR PIANO HINGE (FUSELAGE SIDE) HAS NUMEROUS ELONGATED HINGE PIN HOLES (C-CHECK) REMOVED AND INSTALLED NEW PAX DOOR HINGE HALF IAW SRM 53-21-23 STEPS 4. R-V AND REO 601R-53-21-656 REV A. NO LEAKS NOTED.SDR A6WA202210278364Hinge · damagedPAX DOOR FUSELAGE SIDE HAS MULTIPLE LUGS THAT ARE SCRATCH AND HAS PIN HOLES ****AIRCRAFT REMOVED FROM SERVICE**** REPLACE HINGESDR SWIA202266928Hinge · gougedPAX DOOR HINGE LUGS ON FUSELAGE SIDE ARE GOUGED AT MID HINGE. REMOVED AND REPLACED THE DOOR HINGE IAW SRM 53-21-23.SDR WX0A2022111474313Hinge Fitting · damagedNRC 1000-0071 : 33284-001 LH MLG DOOR FWD HINGE FITTING, DAMAGE SUSPECTED AROUND BOLT HEAD / LH MAIN LANDING GEAR FWD HINGE FITTING AROUND BOLT AND UNDERNEATH HEAD, GOUGE REMOVED AND FOUND STRUCTURALLY ACCEPTABLE AS PER AIRBUS DOSSIER # 81134396 AND COMPLY ASSDR REXA2022111102501Hinge · damagedPAX DOOR HINGE FUSELAGE SIDE HAS OBLONGED HOLES. REMOVED AND REPLACED PAX DOOR HINGE FUSELAGE SIDE IAW CRJ900 SRM 53-21-23-201-010-A01. REMOVED AND REINSTALLED LOWER SEAL STRIKER LOCATED BETWEEN F.S 310 TO F.S 349 LH SILL AREA IAW CRJ-900 SRM 51-42-21-001-001SDR REXA2022102502290Hinge · chafedPASSENGER DOOR HINGE FUSELAGE SIDE, AFT LUG LANDING IS CHAFED REMOVED AND REPLACED PASSENGER DOOR HINGE, FUSELAGE SIDE.SDR SWIA202266698None · brokenBROKEN CLIP ATTACH TO STR 7L BETWEEN FS1144.00 AND FS1162.00, INSIDE AFT EQUIPMENT BAY. (C-CHECK RO 10/29/2022) REMOVED AND REPLACED 1 EACH CLIP P/N: MM670-97107-001 AT STR 7L BETWEEN FS1144.00 AND FS1162.00, INSIDE AFT EQUIPMENT BAY REF. CRJ-900 SRM 51SDR SWIA202266663None · crackedPAX DOOR AFT WEB STIFFNER CRACKED (PN601R317745-7) (C-CHECK RO 10/24/2022) REMOVED AND REPLACED PAX DOOR AFT WEB STIFFENER WITH A NEW SERVICEABLE UNIT (PN601R317745-7) REF CRJ 700 SRM 51-42-06-001-001-A01.SDR NACA20220918367Stop Fitting · damagedLOWER DOOR STOP DAMAGED @ FWD GALLEY DOOR STA 332SDR SWIA202266660None · elongatedAFT WEB DRAG ANGLE HA ELONGATED FASTENER HOLE (C-CHECK RO 10/24/2022) INSTALLED NEW PAX DOOR AFT WEB. DRAG ANGLE REF CRJ 700 SRM 51-42-06-001-001-A01SDR SWIA202266646None · crackedVERTICAL STIFFENER ON FS280.00 LOWER WEB AT RBL26 IS CRACKED. (C-CHECK RO 10/24/2022) INSTALLED NEW STIFFENER P/N CC670-34117-6 AT RBL26 / FS280. REF: CRJ700 SRM 51-42-06-001-001-A01, DWG CC670-34010, REV: J.COMPLIED WITH 51-900-1002-SKYSDR SWIA202266645None · crackedVERTICAL STIFFENER ON FS280.00 LOWER WEB AT LBL26 IS CRACKED. (C-CHECK RO 10/24/2022) REMOVED CRACKED STIFFENER AND INSTALLED NEW STIFFENER P/N CC670-34117-5 AT LBL26 / FS280. REF: CRJ700 SRM 51-42-06-001-001-A01, DWG CC670-34010, REV: J.COMPLIED WITH 5SDR SWIA202266640None · corrodedCORROSION FOUND ON RH FS280.00 LOWER WEB (CC670-34170-8) AT RBL9 POST. (C-CHECK RO 10/24/2022) REMOVED EXISTING LOWER FS280 WEB AND SPLICE AND INSTALLED NEW LOWER WEB AND SPLICE. REF: CRJ700 SRM 53-11-10-201-004-A01 / ,COMPLIED WITH 51-900-1002-SKYSDR SWIA202266639None · corrodedCORROSION FOUND ON LH FS280.00 LOWER WEB (CC670-34170-7) AT LBL9 POST. (C-CHECK RO 10/24/2022) REMOVED EXISTING LOWER FS280 WEB AND SPLICE AND INSTALLED NEW LOWER WEB AND SPLICE. REF: CRJ700 SRM 53-11-10-201-004-A01. COMPLIED WITH TASK CARD 51-900-1SDR K11A2023032700192Unknown · corrodedFUSELAGE FLOOR STRUCTURE - SEAT TRACK BETWEEN STA 344 AND STA 360 LBL 44" HAS EVIDENCE OF CORROSION UNDERNEATH FLANGE ( APPROX 4" IN LENGTH).SDR K11A2023032400189Floorbeam · corrodedFUSELAGE FLOOR STRUCTURE - FLOOR BEAM AT STA 328 OBL OUT TO LBL 60" AND RBL 60" EVIDENCE OF CORROSION ON TOP AND UNDERNEATH ATTACHMENT HOLES.SDR A6WA202209088334Floor Support · damagedFLOOR SUPPORT STRUCTURE BETWEEN FS 409+128 - FS 424 & LBL 9 - RBL 27 HAVE ELONGATED HOLES. ***************REMOVED AIRCRAFT FROM SERVICE********************* OPENED DAMAGED HOLES TO MINIMUM DIAMETER COMPLETELY REMOVING DAMAGE WITHOUT EXCEEDING .350" IAW MHIRJ SDR K11A2022092000164None · corrodedFUSELAGE FLOOR STRUCTURE - FLOOR BEAM @ STA 294 FROM LBL 8" TO RBL 12" (FROM 0L R/H TO L/H) ON TOP AND UNDERNEATH ATTACHMENT HOLES.SDR K11A2022092000163None · corrodedFUSELAGE FLOOR STRUCTURE - FLOOR BEAM @ STA 302 RBL 45" HAS EVIDENCE OF CORROSIONSDR K11A2022091600160None · corrodedFUSELAGE FLOOR STRUCTURE - INTERCOASTAL @ STA 344 LBL 11" HAS EVIDENCE OF CORROSIONSDR K11A2023033000197Seat Track · corrodedFUSELAGE FLOOR STRUCTURE - SEAT TRACK AT STA 500C RBL 26" HAS EVIDENCE OF CORROSION.SDR K11A2023032400187Unknown · corrodedFUSELAGE FLOOR STRUCTURE - SEAT TRACK BETWEEN STA 807 & STA 827 RBL 60" HAS EVIDENCE OF CORROSION.SDR K11A2023032400186Unknown · corrodedFUSELAGE FLOOR STRUCTURE - SEAT TRACK BETWEEN STA 767 & STA 787 RBL 60" HAS EVIDENCE OF CORROSION.SDR K11A2023033100199Seat Track · corrodedFUSELAGE FLOOR STRUCTURE - SEAT TRACK BETWEEN STA 867 AND STA 847 LBL 25" HAS EVIDENCE OF CORROSION.SDR K11A2023032700194Seat Track · corrodedFUSELAGE FLOOR STRUCTURE - SEAT TRACK BETWEEN STA 827 AND STA 847 RBL 44" HAS EVIDENCE OF CORROSION.SDR K11A2023032700193Seat Track · corrodedFUSELAGE FLOOR STRUCTURE - SEAT TRACK BETWEEN STA 847 & STA 867 RBL 27" EVIDENCE OF CORROSION.
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