JASC 5280
Service difficulty reports · 3,557
Reports filed under 5280 · Landing Gear Doors, 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 = '5280' 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 = '5280' 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 V2JA201209300001Door · out of adjustRAISED LANDING GEAR AFTER TAKEOFF. OBSERVED NORMAL GEAR RETRACTION WITH EXCEPTION OF RT MAIN GEAR IN TRANSIT LIGHT REMAINING ILLUMINATED. CONDUCTED NORMAL CLIMB OUT PROCEDURES COMPLYING WITH DEPARTURE. COMPLETED AFTER TAKEOFF CHECKS NORMALLY. ONCE ABOVE TERRSDR 2012FA0000680Support Bracket · crackedDURING BASE MAINTENANCE, FOUND CRACKED SUPPORT BRACKET, RT MLG DOOR.SDR P5CA2012092300036Door · crackedRIGHT WING LANDING GEAR - SHOCK STRUT INBOARD DOOR FAIRING - LEADING EDGE&NBSP HAS CRACK MEASURING & NBSP;1.437 IN. DAMAGE FOUND TO BE BEYOND THE LIMITS OF SRM 52-80-02, FIGURE 101 ALLOWABLE DAMAGE 4 PER SRM 51-70-02, FIGURE 101 ALLOWABLE DAMAGE GENERAL. PERSDR UALA2012092105360Skin · damagedFOUND SKIN DAMAGE ON LEFT MAIN LANDING GEAR DOOR. DAMAGE MEASURES L=.5IN X W=.375IN X D=.048IN. PER SRM 52-81-14 FIGS 103-105-107. DAMAGE WITHIN ALLOWABLE LIMITS. PERFORMED TEMPORARY REPAIR PER SRM 51-77 -12 PARAGRAPH 2A. REPAIRED LEFT MAIN LANDING DOOR SKSDR UIEA2012091300419Skin · delaminatedRT REAR NOSE DOOR SHOWS SIGNS OF DELAMINATION. REPAIRED IAW EO 6752A007 PART 1.SDR A6WA20120920030Skin · chafedCHAFE ON INNER SKIN OF RIGHT MLG DOOR. REMOVED AND REPLACED INNER SKIN ON RIGHT MLG DOOR IAW CRJ 200 SRM 51-24-16, 51-42-13, 51-40-11, 51-42-22.SDR ABXA20120907272Door · missingUPON MX POST FLIGHT WALK AROUND FOUND RIGHT MAIN GEAR SHOCK STRUT DOOR MISSING AND DAMAGE TO RIGHT TRUNNION DOOR. REMOVED AND REPLACED MLG TRUNNION DOOR ASSY W AMM 32-12-11-4, REMOVED AND REPLACED RIGHT MLG SHOCK STRUT DOOR ASSY IAW 32-12-06 AND 32-12-05 JACKSDR A6WA20120920029Skin · chafedLEFT MLG DOOR LEADING EDGE HAS CHAFING. CHAFING ON LEADING EDGE INNER SKIN FOUND TO BE .022 OUT OF LIMITS, ORIGINAL SKIN IS .051. REPAIR DONE IAW REO 601R-52-82-102.SDR A6WA20120920024Skin · gougedLEFT MAIN LANDING GEAR DOOR IS GOUGED IN 3EA SPOTS ON INSIDE SKIN JUST AFT OF THE DATA PLATE. REMOVED AND REPLACED INNER SKIN & INSTALLED IAW CRJ 200 SRM 51-24-16 & 51-42-10.SDR USAA2012091700016Hinge Fitting · damagedC11 CHECK - NOSE LANDING GEAR LEFT AFT DOOR AFT HINGE FITTING HAS ELONGATED HOLE. REMOVED AND REPLACED FITTING IAW A319 SRM 51-72-11.SDR USAA2012091700015Hinge Fitting · damagedC11 CHECK - NOSE LANDING GEAR RIGHT AFT DOOR AFT HINGE FITTING HAS ELONGATED HOLE. REMOVED AND REPLACED HINGE FITTING IAW A319 SRM 51-72-11.SDR USAA2012082900011Hinge · wornFLT/CHK 2049 - AIRFRAME VIBRATION - SEE FORM- FL 220-260 310-320 KIAS STOPS WHEN RUDDER TRIM IS NOT .2R OR .3R. NO ENGINE OR FLIGHT CONTROL INDICATIONS. INSPECTED NLG DOORS AND ACCOMPLISHED TR320- 5280-10-0005A SECTION (I) REMOVED AND REPLACED BOTH FWD HINGESDR V2JA078L110182612Door · missingDURING DESCENT AT APPROX FL100, HEARD ABNORMAL NOISE FROM FRONT OF ACFT. AFTER LANDING, NOTICED LT FWD MLG GEAR DOOR MISSING.SDR A6WA201240815Door · chafedRIGHT MLG DOOR CHAFED ON LOWER L/E. REPLACED FILLER ON LOWER L/E ON RIGHT MLG DOOR IAW REO 601R-52-82-034.SDR NSVA20120823556Door · damagedLEFT INBOARD MLG REPAIRED IAW TD340-57-12-09 CONTROL=277-44.SDR WX0A071272Frame · crackedRIGHT MLG O/B FRAME CRACKED AT FWD CORNER. FABRICATED REPAIR DOUBLER, AND INSTALLED REPAIR DOUBLER IAW MD-80 SRM 52-05 FIG 59.SDR VNAA2012080500002Door · damagedCREW REPORTED LIGHTNING STRIKE TO AIRCRAFT. MAINTENANCE PERFORMED LIGHTNING STRIKE INSPECTION AND DETERMINED DAMAGE TO RIGHT NOSE LANDING GEAR DOOR AND RIGHT APU DOOR TO BE WITHIN AIRCRAFT SRM LIMITS. AIRCRAFT RELEASED FOR SERVICE.SDR SWAA2013022112980Door · delaminatedRIGHT MAIN LANDING GEAR OUTER DOOR DELAMINATED AT OUTBOARD EDGE. DOOR REMOVED AND REPLACED PER MM.SDR UALA2012080704251Door · out of adjustSTRONG VIBRATION IN CLIMB FROM FL200 TO FL290, 79 MACH. PER VIBRATION REPORTING CHECKLIST FROM IMB CREW, VIBRATION WAS FELT IN COCKPIT AND FWD CABIN. ACCOMPLISHED VIBRATION SURVEY REF TSM 05-50-00, FOUND NLG DOOR AFT RIGHT OUT OF LIMITS, ADJUSTMENT REF SEQ NSDR UIEA2012080100338Fairing · damagedDAMAGE TO THE LEFT WING GEAR STRUT DOOR FAIRING TRAILING EDGE. SINCE DAMAGE EXCEEDS THE SRM 52-80-02, FIG 101, ALLOWABLE DAMAGE LIMITS, ALLOWABLE DAMAGE GENERAL DISPOSITION WAS MADE TO PERFORM A TIME LIMITED REPAIR IAW PART 1 OF EO 4452A155 AND FAA 8110-3. DSDR A6WA201240803Door · chafedLT MLG DOOR L/E CHAFED. LT MLG DOOR L/E PREVIOUS. R & R IAW REO 601R-52-82-016.SDR USAA2012081400006Attach Fitting · corroded2S CHECK - CORROSION ON RIGHT MAIN LANDING GEAR DOOR FORWARD ATTACHMENT FITTING AT FR42, S41R. REPAIRED RIGHT MAIN LANDING GEAR DOOR FORWARD ATTACHMENT FITTING AT FR42, S41R IAW EA 502153.SDR 2012F00130Arm · bentDURING WALK AROUND, MX FOUND THE LEFT CENTER MLG DOOR AFT HINGE ARM SLID OFF IT'S BEARING AT THE HINGE ARM TO AIRCRAFT ATTACH POINT.SDR UALA2012070203526Door · damagedRIGHT MAIN LANDING GEAR WING DOOR (DOOR ON LANDING GEAR) LOWER AFT EDGE IS HITTING DOOR SEAL AND SEAL RETAINER ON WING TO BODY FAIRING. DOOR LOWER AFT EDGE HAS SLIGHT DAMAGE. SEAL AND SEAL RETAINER ON WING TO BODY FAIRING HAVE BEEN SHEARED OFF AND ARE MISSINSDR UVVR2012062700022Door · damagedTHE RT MLG OTBD FAIRING DOOR WAS DAMAGED DURING A VISUAL INSPECTION AFTER THE PILOTS COMPLAINED ABOUT A VIBRATION DURING LANDING.SDR DXTA2012062505016Hinge · crackedDURING LANDING CHECKLIST, PUT LANDING GEAR DOWN WITH 3 POSITIVE GREEN LIGHT INDICATIONS WITH BOTH RED LIGHT IN THE GEAR HANDLE STAYED ILLUMINATED. EXECUTED CHECKLIST WITH NO POSITIVE RESULTS. BOTH RED LIGHT ON THE GEAR HANDLE STAYED ILLUMINATED AT ALL TIME.SDR A6WA201240693Structure · chafedLEFT AND RIGHT MLG DOORS L/E CHAFED. CUTTING AWAY DAMAGED INNER SKIN ON LT MLG DOOR. BLENDED AND SMOOTHED MINOR CHAFING IAW REO 601R-52-82-034 & 601R-52-82-102SDR EE4Y2012102300314Fitting · crackedLOWER FUSELAGE LT INBD MLG DOOR INBD FWD SECTION FITTING WITH A CRACK. REPAIRED LT MLG DOOR INBD FWD FITTING IAW EO COO-9-52-189-12,DTD JULY 03, 2012.SDR EE4Y2012102300313Door · crackedLOWER FUSELAGE RT INBD MLG INBD FWD SECTION FITTING WITH A CRACK. REPAIRED RT MLG DOOR INBD FWD FITTING IAW EO COO-9-52-190-12, DTD JULY 03, 2012.SDR UIEA2012061300264Door · bentLEFT MLG TRUNNION DOOR BENT T/E AFT CORNER. ACCOMPLISHED EO 6752A005, REF ITEM PART 1.SDR USAA2012062000007Hinge · excess play2S CHECK - EXCESSIVE PLAY ON LEFT MAIN LANDING GEAR DOOR HINGE ASSEMBLY BETWEEN FR34 TO FR44. REPLACED LEFT MAIN LANDING GEAR DOOR HINGE ASSEMBLY BETWEEN FR34 TO FR44 IAW A319 CMM 52-81-18.SDR CA120601003Bearing · migrated(CAN) ENROUTE TO DESTINATION, THE F/A NOTICED THAT 1 OF THE RT MLG DOOR WAS NOT FULLY CLOSED. UPON ARRIVAL, THE CAPTAIN REPORTED THAT THE CENTER DOOR AFT SECTION WAS DETACHED FROM THE NACELLE. A MAINTENANCE TEAM TRAVELLED ON A AOG TRIP AND FOUND THE CENTER DSDR CA120531006Fitting · cracked(CAN) DURING DEPARTURE, LINE CREW NOTIFIED THE CREW THAT THE LT GEAR DOOR WAS FLAPPING. THE FITTING WAS REPLACED AND ACFT RETURNED TO SERVICE.SDR 2012FA0000344Door · departedAFTER LANDING, IT WAS FOUND THAT THE RT MLG OTBD FAIRING DOOR HAD DEPARTED DURING FLIGHT. THE HINGE (WHICH IS PART OF THE DOOR ASSY) HAD TORN ALONG THE RIVET LINE, AND THE PUSHROD ATTACHMENT FITTING WAS ALSO TORN. NO DAMAGE TO ANY OTHER ACFT COMPONENTS OR STSDR KY7A12052501Hinge · crackedNLG FAILED TO EXTEND DURING NORMAL OPERATIONS DURING TRAINING FLIGHT. FLIGHT CREW PERFORMED EMERGENCY LANDING GEAR EXTENSION PROCEDURES; NOSE GEAR EXTENDED AND LOCKED. FLIGHT CREW PERFORMED NORMAL LANDING WITH NO FURTHER DIFFICULTY. MX PERSONNEL INSPECTED ASDR A6WA201240642Structure · chafedRT MLG DOOR L/E CHAFED. REMOVED UNSERVICEABLE FILLER AND REPLACED WITH SERVICEABLE FILLER IAW REO 601R-52-82-034.SDR A6WA201240640Structure · chafedLT MLG DOOR CHAFED L/E CORNER BY DOOR BRUSH. REMOVED UNSERVICEABLE EXISTING FILLER AND REPLACED WITH SERVICEABLE FILLER IAW REO 61R-52-82-034, REV NC.SDR GNMA201205230001Web · crackedNLG SUPPORT WEB HAS CRACKS BOTH LT AND RT.SDR UIEA2012052100246Door · damagedDURING WALKAROUND INSPECTION, MX FOUND THE LT WING LANDING GEAR SHOCK STRUT OTBD DOOR T/E DELAMINATED, WITH AREA OF MISSING MATERIAL 2.5" X 23.0" ON AFT EDGE AND AREA OF DELAMINATION ON INSIDE SKIN 3.5" X 13.0" (REF FIG 1). DAMAGE FOUND TO BE BEYOND THE SRM 5SDR A6WA201240762Door · chafedLT MLG DOOR IS CHAFED ON THE INSIDE T/E. REPAIRED LT MLG DOOR CHAFE ON THE INSIDE T/E IAW REO 601R-52-82-351, REV A.SDR A6WA201240560Skin · chafedLEFT MLG DOOR INNER SKIN AND FASTENER CHAFED. BLENDED CHAFE AREA WITHIN LIMITS ORG .040, REMOVED .002, REMAINING .038 IAW SRM 52-82-00, FIG 101. BLENDED AREA NR 5 FOUND TO BE OUT OF LIMITS. REPAIRED IAW REO 601R-52-82-337, R & R CHAFE FASTENER.SDR UIEA2012050400181Fairing · damagedDURING WALKAROUND INSP, MX FOUND THE LT WING LANDING GEAR STRUT DOOR FAIRING - T/E, MEASURING 3.0 IN. X 1.0 IN. (REF FIG 1). DAMAGE FOUND TO BE BEYOND THE SRM 52-80-02, FIG 101 ALLOWABLE DAMAGE 4 LIMITS IAW SRM 51-70-02, FIG 101 ALLOWABLE DAMAGE GENERAL. (DISSDR UIEA2012050400182Fairing · crackedDURING WALKAROUND INSPECTION, MX FOUND THE LT WING LANDING GEAR STRUT DOOR FAIRING - T/E, MEASURING 4.0 IN. (DELAMINATION/DISBOND) X 3.25 IN. (CRACK) REF FIG 1. DAMAGE FOUND TO BE BEYOND THE SRM 52-80-02, FIG 101. ALLOWABLE DAMAGE 4 LIMITS IAW SRM 51-70-02, SDR UALA2012050402648Hinge Fitting · wornLEFT MLG DOOR AFT ATTACH FITTING BOLT HOLES WORN. OVERSIZED HOLES, HOLE FINAL SIZE IS .437,EM WITHIN LIMITS PER AVO 1283. REWORKED LT MLG DOOR AFT HINGE FITTING COUNTERSUNK HOLES REF AVO 1283 AND ECRA 5340- 01464 AND INSTALLED FITTING WITH OVERSIZED HARDWARESDR UALA2012050102579Bolt · looseNOSE GEAR HAS BAD VIBRATION WHEN LIFTED OFF THE GROUND DURING TAKEOFF FELT UNBALANCED. CREW REPORTS VIOLENT SHAKING THRU OUT CABIN AFTER TAKE OFF. FOUND BOLT ON NLG GEAR DOOR ASSY WORN. REPLACED BOLT.SDR A6WA201240543Door · chafedLT MLG DOOR L/E AND T/E CHAFED. BLENDED CHAFE ON LT MLG DOOR T/E FOUND TO BE WITHIN LIMITS ORIGINAL .050. REMOVED .012 REMAINING .038 IAW SRM 51-12-00 AND 52-82-00 USING THICKNESS GAUGE ALODINED, PRIMED AND TOP COATED IAW SRM 51-21-11, 51-25-06, 51-25-16. BSDR AW6A201240538Lug · wornRT MLG DOOR PUSH LUG, WORN BEYOND LIMITS IN REO 601R-52-82-143 INSTALLED SERVICEABLE REPLACEMENT LUG IAW SRM 51-41-011, 51-42-21.SDR A6WA201240539Lug · chafedLT MLG DOOR BELLCRANK PUSH ROD LUG ON DOOR IS CHAFED. REMOVED PUSH ROD, BLENDED CHAFE ON LT MLG DOOR BELL CRANK PUSH ROD LUG FOUND TO BE WITHIN LIMITS, NDT, ALODIZED PRIMED AND TOP COATED, REINSTALLED PUSH ROD IAW AMM 33-42-01, REO 601R-52-82-143, SRMS 51-21-SDR UALA2012042002362Door · delaminatedLEFT MLG STRUT ATTACHED LOWER DOOR, FWD OUTBOARD LOWER EDGE IS DELAMINATED 10 INCHES LONG VERTICAL AND 2 INCHES LONG HORIZONTAL ALONG LOWER EDGE, SKIN IS SPLIT ALONG EDGE. ACCOMPLISHED TAP TEST OF DELAMINATION, CLEANED AREA APPLIED TAPE IAW ECRA 5280-01485. SDR 7AHR201204092588Rib · corrodedCORROSION ON AFT RIB OF LT MLG INNER DOOR. FOUND RIB ON INNER DOOR FOR LT MLG CORROSION BEYOND LIMITS. R & R RIB IAW SRM.
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