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 UPS00233742Fitting · crackedINSPECTION TYPE:C, LT WING DOOR (MLG) AFT HINGE FITTING ON NR 4 FLAP TRACK CRACKED. HINGE FITTING REMOVED IAW MM 20-80-01. FITTING REPLACED IAW MM 20-80- 01.SDR CALA0001382Frame · crackedINSPECTION FOUND A 3 INCH CRACK IN LT MLG WHEEL WELL DOOR FRAME AT O/B FORWARD CORNER. THE FRAME WAS REMOVED AND REPLACED IAW SRM 51-30-2, 51-30-1, AND 51-30-8.SDR TWAA0016111Structure · crackedDURING CHECK-C MAINT, THE LT MLG WHEEL WELL DOOR WAS CRACKED AFT EDGE. STOP DRILLED CRACK. INSTALLED DOUBLER REPAIR PER ILLUSTRATION IN SRM 52-05, FIG 28, SHEET 6.SDR CA000925010Door · damaged(CAN) AIRCRAFT DEPARTED, CDL32-12A APPLIED PIOR TO DEPARTURE DUE R/H GEAR TRUNNION DOOR DAMAGE. CDL INDICATED A MINOR AIRCRAFT WEIGHT PENALTY. VMO/MMO SWITCH PLACED IN ALTERNATE POSITION DUE CDL. ON AKEOFF, (APPROX 250 KTS) OVERSPEED AURAL WARNING AND BARBER PSDR EISA20000173Fitting · crackedPERFORMED BHFEC AT FLAP TRACK LANDING GEAR DOOR FED HINGE FITTING ATTACHMENT HOLES LT AND RT SIDE 7 HOLES TOTAL. REAMED HOLES PER BOEING SB 727-32-0340.SDR RRXA002999Door · misrepairedDURING A MAINTENANCE VISIT FOUND A BAD REPAIR TO THE LT MAIN LANDING GEAR DOOR AFT LWR CORNER, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.SDR AU001004Door · separated(AUS) RT MAIN LANDING GEAR STRUT AND TRUNNION DOORS MISSING.INVESTIGATION FOUND OTHER DAMAGE INCLUDING RH BRAKE LINES AND BOGIE TILT ACTUATOR HYDRAULIC LINES. IMPACT DAMAGE OCCURRED TOTHE WING TO BODY FAIRING (PANEL 196KR) AND UNDERWING PANEL 615SB. THE RH HORSDR L1GA200000282Fitting · crackedA 1 INCH CRACK INSIDE LT WHEEL WELL DOOR FWD END AT FITTING. REMOVED AND FABRICATED NEW FITTING.SDR 00FDEA00589Skin · crackedDURING ROUTINE INSP, LEFT MAIN LAND GEAR DOOR INNER SKIN FOUND CRACKED. CUT OUT DAMAGED AREA, FAB DOUBLER AND FILLER, AND INSTALL PER IAW SRM 51-40-2.SDR RRXA001047Door · damagedCLIMBOUT FROM RDU, UPLATCH CHECK FAILED. BOTH RED UNSAFE LIGHTS ON (GEAR AND DOOR UNSAFE) WITH LEFT ALT DOOR. LIGHT ON ALSO. C/W QRH CHECKLIST, PLACED GEAR HANDLE TO UP AND ALL LIGHTS WENT OUT. RECHECKED UPLATCH, UPLATCH THEN CHECKED NORMAL WITH ALL LIGHTSSDR C2XA00IA248Handle · brokenIAH - FLT 2908 - DURING TAXI, THE CREW REPORTED A NOISE COMING FROM LEFT MAIN LANDING GEAR, THE AIRCRAFT RETURNED TO THE GATE, WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AFFECTED AREA AND FOUND THE LEFT FORWARD OUTBOARD MLG DOOR SWINGING FREE. MAINTENANCE RSDR TWAA0013209Door · crackedDURING CHECK-C MAINT IN THE LT WHEEL WELL, THE WHEEL WELL DOOR FWD O/B CORNER WAS CRACKED. STOP DRILLED CRACK WITH 0.250 DRILL BIT. MANUFACTURED DOUBLER FROM 7075-0, 0.063 MATERIAL. HEAT TREATED TO 7075-T6 CONDITION. FABRICATED DOUBLER PER ARA 17041. ATTASDR AU001022Bracket · cracked(AUS) RT NOSE LANDING GEAR DOOR FORWARD HINGE BRACKET CRACKED ACROSS WEB. CRACK LENGTH 23MM (0.905IN).SDR TWAA0013125Hinge · crackedDURING CHECK-C MAINT, ON RT MLG DOOR, THE RT MAIN GEAR DOOR HINGE WAS CRACKED AT FWD END. REMOVED AND REPLACED CRACKED SECTION OF DOOR HINGE PER SPM 6-70-1 AND SRM 51-30-1. INSTALLED HI-LOKS PER SRM 51-60-0 PAGE 36, AND SRM 51-30-5.SDR ABXA000386Pan · crackedLEFT MAIN LANDING GEAR DOOR WAS CRACKED IN UPPER FORWARD DOOR PAN. REPLACED PAN IAW DC9 SRM 53-30-2.SDR ABXA000376Pan · crackedRIGHT MAIN LANDING GEAR DOOR HAD CRACK IN UPPER PAN. REPLACED RIGHT MAIN GEAR DOOR IAW DC9 SRM 51-30-2.SDR RAAA00E9028Skin · crackedDURING SCHEDULED NR 1 MAINT CHECK, FOUND RIGHT NOSE GEAR DOOR INNER SKIN CRACKED AT AFT HINGE MOUNT AREA. CRACK AT FWD EDGE RUNNING VERTICAL. REPAIRED RIGHT NOSE GEAR DOOR IAW LOCKHEED SRM 51-3-7 FIG 1 & 53-2-1 FIG 2 & 51-2-14.SDR C2XA00CL055Hinge · wornCLE - FLT 3121 - THE LEFT MAIN GEAR WOULD NOT RETRACT (RECYCLED TWICE AND GEAR CAME UP) BOTH GREEN LIGHTS EXTINGUISHED AND BOTH RED REMAINED ILLUMINATED. WIND NOISE COULD BE HEARD FROM LEFT MAIN. MAINTENANCE INSPECTED AND REMOVED AND REPLACED FORWARD AND AFTSDR ABXA000391Structure · delaminatedLEFT FLYING DOOR (FORWARD HALF) HAD AREA OF DELAMINATION. REPLACED OUTBOARD LEFT MAIN LANDING GEAR DOOR.SDR CALA0001124Door · crackedINSPECTION FOUND A 3.6 INCH CRACK IN LT MLG DOOR AFT LOWER CORNER REPAIR. THE EXISTING REPAIR WAS REMOVED AND A DOUBLER WAS INSTALLED IAW SRM 51-30-2, 52-05, FIGURE 28, AND 51-10-3.SDR CA000905005Stop · loose(CAN) SHORTLY AFTER TAKEOFF AIRCRAFT REPORTED THE LEFT MAIN GEAR DOOR WOULD NOT CLOSE AFTER GEAR RETRACTION. THE GEAR WAS CYCLED SEVERAL TIMES WITH THE SAME RESULT. THE CREW ELECTED TO RETURN TO WITH THE GEAR DOWN SELECTION NORMAL - 5 GREEN LIGHTS AND BOTH MAISDR 20000829SH005Fitting · brokenLEFT MAIN LANDING GEAR AFT OUTBOARD DOOR, AFT HINGE FITTING WAS FOUND BROKEN DURING C-CHECK INSPECTION. POSSIBLE CAUSE, FATIGUE. (X)SDR UPS00434061Structure · corrodedINSPECTION TYPE:C, R-BODY GEAR INNER DOOR, CORROSION ALONG THE UPPER EDGE, EXTERNALLY. NEW DOOR FITTED IAW MM 32-14-00 REF NRC 44309520/44309103.SDR UPS00434059Skin · crackedINSPECTION TYPE:C, R-BODY GEAR DOOR, SKIN CRACKED AND DAMAGED AT THE UPPER AFT CORNER. NEW DOOR FITTED IAW MM 32-14-05.SDR 20000814SH004Hinge Fitting · brokenRIGHT MAIN LANDING GEAR AFT INBOARD DOOR, AFT HINGE FITTING WAS FOUND BROKEN DURING C-CHECK INSPECTION. POSSIBLE CAUSE: FATIGUE. SUBMITTER RECOMMENDED REPLACING MONITOR AT REGULAR INTERVALS. (X)SDR GAIA00431Hinge · wornDISCREPANCY: DURING A 'C' CHECK INSPECTION, FOUND LEFT GEAR STRUT DOOR, FORWARD HINGE BUSHINGS HAD MIGRATED OUT AND LOOSE. CORRECTIVE ACTION: REPAIRED LEFT GEAR DOOR FORWARD HINGE PER S/B 727-32-0340, AND TIMCO REO S00248.SDR DHL200070924CSkin · gougedLEFT MAIN LANDING GEAR FLYING DOOR HAS GOUGE AT LOWER SKIN ON TOP OF REPAIR. REMOVED OLD REPAIR PER SRM 51-30-2. CLEANED, TREATED AND PRIMED AREA PER SRM 51-10-2. FABRICATED REPAIR DOUBLER PER SRM 51-40-2. HEAT TREATED DOUBLER PER SRM 51-10-3. TREATED ANDSDR C2XA00IA192Door · disconnectedIAH - FLT 3581 - THE CREW REPORTED THAT THE LEFT FORWARD NOSE GEAR DOOR WOULD NOT CLOSE AND A LOUD NOISE COMING FROM THE NOSE LANDING GEAR COMPARTMENT. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE RECONNECTED THE LEFT FORWARD NLG DOOR AND OPERATISDR 20000724SH011Door · failedDURING ATTEMPT OF EXTENSION OF LANDING GEAR, MLG EXTENDED NORMALLY, NLG WOULD NOT EXTEND. REPEATED ATTEMPTS WERE MADE TO EXTEND NOSE GEAR WITH NO SUCCESS. ACFT MADE SUCCESSFUL GEAR UP LANDING IN GRASS. UPON LIFTING ACFT TO EXTEND GEAR, FOUND RT NOSE GEAR DOSDR P2EA00232Structure · corrodedYYC - DURING C-CHECK, FOUND THE LEFT MAIN LANDING GEAR INNER DOOR EDGE FRAME CASTING CORRODED, 16 INCHES LONG, 1 INCH LONG, .20 INCH DEEP. REPLACED THE LEFT MAIN LANDING GEAR INNER DOOR WITH SERVICEABLE GEAR DOOR IAW BMM 32-13-11. (M)SDR CA000621042Bolt · sheared(CAN) AFTER A/C ARRIVED AT GATE (YUL) MAINT FOUND ON WALK AROUND CHECK DAMAGE TO RT LOWER WING PANEL , RT LDG GEAR DRAG STRUT, & RIGHT LDG GEAR STRUT DOOR. HEAD OF BOLT ATTACHING RIGHT STRUT DOOR TO LANDING GEAR STRUT FOUND SHEARED OFF. STRUT DOOR THEN ALLOWEDSDR RRXA001002Structure · crackedLT GEAR DOOR CRACKED IN TWO PLACES (MAIN LANDING). PERFORMED PLATING REPAIR IAW DC-8 SRM CHAP 52-2-0 FIG 2.SDR CALA0000927Structure · crackedINSPECTION FOUND A .5 INCH CRACK IN RT MLG I/B DOOR AFT LOWER CORNER AT REPAIR DOUBLER. REMOVED AND REPLACED DOUBLER IAW SRM 51-30-1.SDR SWAA001142Link · brokenDIVERSION, DURING GEAR RETRACTION HEARD A LOUD NOISE FOLLOWED BY A VIBRATION IN NLG AREA. FOUND LT NLG UPPER DOOR LINK BROKEN. REMOVED AND REPLACED LINK PER MM.SDR ABXA000319Skin · delaminatedDURING C-CHECK, FOUND RIGHT MAIN LANDING GEAR OUTBOARD DOOR DELAMINATED 40 SQ INCHES ON INTERIOR SIDE AND 36 SQ INCHES ON EXTERIOR SIDE. REPLACED DOOR IAW DC9 OHM 32-10-6 AND DC9 MM 32-12-01.SDR 20000628SH002Hinge · failedREAR HINGE CASTING FAILED HALFWAY ALONG ARM OF RADIUS, PN 35/815016/7 WHILE APPROACH TO LAND: POSSIBLE CAUSE IS WEAR IN THE FRONT HINGE PIVOT BRACKET BOLT HOLES WHICH COULD CAUSE VIBRATION. INSPECT BOTH FRONT AND REAR BOLT HOLES FOR WEAR ALIGNMENT BY DISCONNSDR CALA0000907Structure · crackedINSPECTION FOUND A 1 INCH CRACK AT CORNER OF LT MLG DOOR. THE DOOR CORNER WAS REPAIRED IAW SRM 51-31-01.SDR MWEA00650Frame · crackedMKE - RIGHT MLG INBOARD FORWARD FRAME CRACKED. MAINTENANCE FABRICATED AND INSTALLED REPAIR DOUBLER. (M)SDR CALA0000888Skin · crackedINSPECTION FOUND A 2 INCH CRACK IN REPAIR DOUBLER OF RT MLG DOOR AT I/B LOWER FORWARD CORNER. THE DOUBLER WAS REMOVED AND REPLACED IAW SRM 51-30-02.SDR CALA0000871Skin · crackedINSPECTION FOUND THE RT AFT NOSE GEAR DOOR CORRODED ON INNER SKIN SURFACE WITH A 2 INCH CRACK AT LOWER EDGE OF DOOR. THE CORROSION WAS REMOVED IAW SRM 51-10-3 AND MATERIAL LOSS WAS FOUND WITHIN LIMITS IAW SRM 52-06. THE DOOR WAS REMOVED, THE CRACK WAS STOP DSDR RRXA002655Doubler · damagedDURING A MAINTENANCE VISIT FOUND A PATCH REPAIR THAT IS TORN NEAR SEAL ON THE LT MLG DOOR, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 51-1-21, 51-1-21A, SDR CALA0000857Doubler · chafedINSPECTION FOUND LT MLG DOOR AFT LOWER CORNER REPAIR DOUBLER CHAFED. THE REPAIR DOUBLER WAS REMOVED AND A NEW DOUBLER WAS INSTALLED IAW SRM 51-30-02.SDR DL72S001069Structure · damagedUPON GEAR RETRACTION HEARD LOUD NOISE ACCOMPANIED WITH UNSAFE INDICATION. REPAIRED NOSE GEAR DOORS AND LINKAGE.SDR CALA0000763Angle · chafedINSPECTION FOUND LT MLG WHEEL WELL AFT DOOR JAMB T ANGLE CHAFED AT STA 1003. THE T ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-2 AND 51-30-5.SDR MWEA00455Angle · crackedLEFT AFT MLG DOOR JAM T ANGLE CRACKED. REMOVED AND FABRICATED T ANGLE AND INSTALLED.SDR MWEA00453Angle · crackedRIGHT AFT MLG DOOR JAM T ANGLE CRACKED. REMOVED AND FABRICATED T ANGLE AND INSTALLED.SDR DHL200070707CFrame · crackedRT MAIN LANDING GEAR WING DOOR LOWER END FRAME IS CRACKED ON O/B BEND RADIUS AT FWD END. REMOVED CRACKED END FRAME AT RT MLG WING DOOR LWR END AS PER SRM 51-30-2. INSTALLED NEW END FRAME AT RT MLG WING DOOR LOWER END FWD SIDE PER SRM 51-30-2. TREATED AND PRSDR QXEA0001367Angle · chafedPDX- ANGLE IS CHAFED THROUGH WHERE THE RIGHT HAND INBOARD MAIN LANDING GEAR DOOR AFT OUTBOARD EDGE CONTACTS THE FUSELAGE FAIRING. REPAIRED IAW HORIZON AIR EA 4-57-410.SDR ABXA000260Hinge · crackedRIGHT MAIN LANDING GEAR DOOR HINGE CRACKED AT LOBE. REPLACED HINGE IAW DC9 SRM 51-30-1.SDR CALA0000597Structure · crackedRIGHT MAIN LANDING GEAR DOOR UPPER CORNER CRACKED (1). REMOVED AND INSTALLED NEW CORNER PER SRM 52-84-0, 51-10-03, AND 51-30-02.
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