JASC 5101

Service difficulty reports · 482

Reports filed under 5101 · Aircraft Structures, 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 = '5101'
  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.

SDR 05FDEA04093Repair · unknownSMIS 424 51-00 0007102 27SEP05 MC1 CLOSE R MOD TYPE Y MOD NO. 9-AGING-INSP REV NO. PS PT1 AGING AIRPLANE SAFETY RULE (AASR) 14CFR 121.368, 121 .370A COMPLY WITH AGING 9-AGING-INSP REV NO. POS PT1 ENT BY: 067708 INFO 30NOV05 21:26 MC1 R DIDec 3, 2005 · N424FE · Airbus A310SDR 05FDEA04092Repair · nonePREVIOUS REPAIR INSTALLED AT FUSELAGE LT SIDE AT STA 1923, FR35, STR 22LT. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. REPAIR CONFORMS TO AN EXISTING FEDEX EDec 3, 2005 · N424FE · Airbus A310SDR 05FDEA04090Repair · not an sdrPREVIOUS REPAIR INSTALLED AT FUSELAGE LOWER EDGE OF R1 DOOR AT STA 1250 TO STA 1262, FS 15B. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. REPAIR EVALUATED ANDDec 3, 2005 · N424FE · Airbus A310203SDR 05FDEA04089Repair · nonePREVIOUS REPAIR INSTALLED AT FUSELAGE LOWER EDGE OF R1 DOOR AT STA 1202 TO STA 1214, FR14B. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. REPAIR EVALUATED AND Dec 3, 2005 · N424FE · Airbus A310203SDR 05FDEA04088Repair · nonePREVIOUS REPAIR INSTALLED AT FUSELAGE RIGHT SIDE, BELOW R1 DOOR AT STA 1187 TO STA 1212, FS 14A TO FS 15. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. REPAIR Dec 3, 2005 · N424FE · Airbus A310SDR PCSA12020501Unknown · noisyAFTER DEPARTURE FLT 8412 CLIMBED TO CRUISE FL320, REPORTED ACFT EXPERIENCED A LOUD BANG & SUBSEQUENT SIGNIFICANT VIBRATION, RETURNED, VIBRATION FELT BY CREW SEVERAL TIMES PRIOR TO LANDING. MX PREFORMED A VISUAL INSP OF THE NR 1, 2, & 3, ENG INTAKES & EXHAUST IDec 2, 2005 · N604AJ · Boeing 727225SDR QXEA200501733Unknown · unknownRDD FLIGHT NR 2310, BOTH CONDITION LEVERS INADVERTANTLY BROUGHT BELOW MINIMUM RESULTING IN NR 1 AND NR 2 PEC CAUTION LIGHTS AND PROP RPM 1060-1070. MAINTENANCE C/W Q400 FIM TASK 61-20-05-810-822. RESET SET FAULT CODES. C/W AUTO FEATHER TEST. NO DEFECTS NOTNov 30, 2005 · N412QX · Bombdr DHC8402SDR 05FDEA03784Blanket · burnedCAC LT SIDE BLANKET BURNED JUST UNDER NR 1 PNEUMATIC DUCT.Nov 12, 2005 · N319 · Doug DC1030SDR CA051109005Lead · unknown(CAN) AIRCRAFT TTSN 5412.7 HOURS. AD CF-2005-10 C/W SEPT 12/05. NO FAULT FOUND.Oct 31, 2005 · Namer HARVARD4SDR CA051104017Skin Panel · damaged(CAN) DURING DESCENT, AIRCRAFT HIT GOOSE. AIRCRAFT LANDED NORMALLY. DAMAGE FOUND ON IB RT LE (DENT .7500 INCH DEEP 4.5 INCH WIDE AND 8.5 INCH LONG). MFG AUTHORIZED FERRY FLIGHT WITH THIS DAMAGE TO MAINTENANCE BASE. MAINTENANCE REMOVED LEADING EDGE FOR INSPEOct 20, 2005 · Cndair CL6002B19SDR CA051104016Radome · bird strike(CAN) DURING DESCENT, IMPACT WITH GOOSE. AIRCRAFT LANDED NORMALLY. MAINTENANCE FOUND RADOME BADLY DAMAGED AND ALSO DAMAGE TO BULKHEAD AT STATION X-7.0. RADOME ASSEMBLY REPLACED AND FACTORY REPAIR DRAWING CARRIED OUT TO REPAIR UPPER RT CORNER OF RADOME BULKHEAOct 20, 2005 · Dhav DHC8311SDR IXXA05SMN225SRivet · improperDURING C CHECK INSPECT, AFT LWR FUSELAGE BELLY, STA FS 1254.000 L-35.5R, UPGRADE REPAIR DOUBLER TO INCORPORATE A MIN OF 3 ROWS OF RIVETS. PERFORMED MAJOR REPAIR IAW DC8 SRM 53-2-1 FIG 7, EO SEMAN NR 20051198 DATED 09-20-05. REMOVED EXISTING REPAIR DOUBLER IAOct 13, 2005 · N829BX · Doug DC871FSDR WRLA2005144Unknown · unknownUPON GEAR DOWN HAD A VIOLENT SHUDDER LIKE ACFT HIT SOMETHING & LOUD NOISE, THEN COULD NOT GET RT MLG DOWN ON PRIMARY OR SECONDARY SYS. LOST NR 1 TRANSPONDER, INTERMITTENT LOSS OF OTHER SYS: AUTO FLT, CAC, ETC. MLG HELD AT LANDING BUT STILL HAVE RED MLG LIGHOct 11, 2005 · N274 · Doug MD11FSDR KBM2005F00254Case · tornUNITS ARE TORN AND WORN. REMOVED AND REPLACED CASE. (M)Aug 10, 2005 · N751H · Snias AS350B2SDR CA050722005Radio · inoperative(CAN) RETURNED TO BASE WITH NO WORKING RADIOS. IT WAS RETURNING FROM WERE IT HAD BEEN RAINING HEAVILY WHILE THEY WERE ON THE GROUND. IT WAS FOUND THAT SOME MOISTURE HAD MADE ITS WAY FROM AN UNKNOWN LOCATION ABOVE THE RADIOS AND WORKED ITS WAY DOWN DURING FLIGHJul 19, 2005 · Stbros SC7SERIES3SDR 2005FA0000582Cable · damagedCABLE DISCONNECTED FROM CABLE PULL HANDLE. PROBABLY BAD CRIMP. SAME PROBLEM ENCOUNTERED ON OTHER AIRCRAFT OF THIS TYPE AND PA-46-310P AS WELL.Apr 14, 2005 · Piper PA46350PSDR DHL2005367510Seat Track · corrodedDURING "C" CHECK, CABIN SEAT TRACK AT FS 18 THRU FS 21A AT BL 28R HAS CORROSION. INSTALLED NEW SECTION OF SEAT TRACK AT MAIN CABIN FROM FS 18 TO FS 21A BL 28R IAW A-300 SRM 53-10-10 MAT. USED TMS 60-22457 PO NR 2113624. TREATED AND PAINTED NEW SEAT TRACK IAWApr 3, 2005 · N367DH · Airbus A300B4203SDR DHL2005782571Fitting · corrodedSTRINGER 19 RT ATTACH FITTING CORRODED AT BS 1183. REMOVED & REPLACED FITTING AT STR 19 BS 1183 IAW B727 SRM 51-30-2.Mar 29, 2005 · N782DH · Boeing 727227SDR WLDA2004106Structure · vibrationDAY/BRU ABORTED TAKEOFF AT 70 KTS DUE TO VIBRATION. INSPECTED ALL WHEELS AND BRAKES, FLAPS AND SPOILERS, NOSE GEAR AND NR 1 & 3 INLETS, NO DEFECTS NOTED. REVERIFIED ALL TIRE PRESSURE, ALL CHECKED NORMAL.Nov 27, 2004 · N304 · Doug DC1030FSDR SWIA200414129Unknown · unknownJUST AFTER TAKEOFF WITH FLAPS 20 AND TRIMS CENTERED THE AIRCRAFT ROLLS TO THE RIGHT. THIS HAPPENS IMMEDIATELY AFTER WEIGHT OFF WHEELS AND BECOMES LESS PRONOUNCED AFTER FLAP RETRACTION AND/OR INCREASE IN SPEED. SANDED ABRASION RESISTANT TEFLON FILM TO SPECIFINov 23, 2004 · N463SW · Cndair CL6002B19SDR IXXA060009SRepair · scheduled maintDURING ROUTINE C-CHECK REMOVE EXISTING FUSELAGE SKIN REPAIR LOCATED AT STATION 220 LONGERON 35 RIGHT DUE TO DTA REQUIREMENTS. REMOVED NECESSARY FASTENERS, AND EXISTING DOUBLER, REMOVED DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, REMOVED, TERATED, PRIMNov 10, 2004 · N825BX · Doug DC871FSDR ABXA040376Structure · vibrationIN DESCENT, LEVELED OFF AT 300 KIAS, INCURRED VIBRATION, SLOWED TO 290 KIAS, VIBRATION WENT AWAY THEN CAME BACK AGAIN WHEN ACCELERATING THROUGH 295 KIAS. INSPECTED FOR GENERAL CONDITION & SECURITY OF THE FOLLOWING ITEMS: NOSE GEAR AREA, FUSELAGE, FLAPS, SLATSNov 7, 2004 · N971AX · Doug DC941SDR MASA200400619Unknown · bird strikeREJECTED TAKEOFF DUE TO BIRD STRIKE. MAINTENANCE C/W INSPECTION AND FOUND NO DAMAGE.Nov 1, 2004 · N914FJ · Cndair CL6002D24SDR IXXA0060010SRepair · scheduled maintDURING ROUTINE C CHECK REMOVE EXISTING EXTERNAL SKIN REPAIR AT STATION 172 LONGERON 35 RIGHT DUE TO DTA REQUIREMENTS. REMOVED FASTENERS AS NEEDED AND EXISTING DOUBLER. FABRICATED NEW REPAIR PARTS, LOCATED, DRILLED, REMOVED, TREATED, PRIMED, INSTALLED NEW REPOct 11, 2004 · N825BX · Doug DC871FSDR 2004000012Floor Panel · overheatedEXCESSIVE HEAT COMING FROM FLOOR AND WALL FORWARD AND AFT OF L-2 DOOR. TROUBLESHOOTING AS OF 10/5/04.Oct 4, 2004 · N17085 · Doug DC1030SDR ASAA0480497Sealant · missingOKC - C-CHECK-LOG PG 5784367, SEALANT MISSING LT IDLER HINGE. NO ROTATION NOTED, APPLIED SEALANT TO BOTH ENDS OF BOLT IAW EA 5750-01098.Sep 24, 2004 · N973AS · Doug DC983SDR MALA040438Structure · vibrationA/C HAS A LATERAL VIBRATION SIMILAR TO LIGHT TURBULENCE, SEEMS TO BE MORE PRONOUNCED AT SPEEDS ABOVE 210. AIRCRAFT IS SHOWING SIMILAR VIBRATION AT ALL ALTITUDES. MAINTENANCE INSPECTED AIRCRAFT RUDDER DAMPNER, ALL PANELS SWING GEAR RAN ENGINE, TESTED FLT CONTJun 8, 2004 · N402XJ · Saab 340BSDR ARWA20040503Seal Depressor · damagedON CLIMB PRESSURIZATION LEAK HAPPENED AT FL 280. UNABLE TO MAINTAIN CABIN PRESSURE 10,000 FT. REMOVED AND REPLACED LOWER SEAL DEPRESSOR IAW AERONAUTICAL ENGINEERS DRAWING AE2412 & DC8 SRM 51-3-0 PAGE 1, 2 & 3. PERFORMED CABIN PRESSURIZATION OPS CHECK IAW NAMay 11, 2004 · N345JW · Doug DC863SDR AT0700031Structure · ground damageCATERING TRUCK STRUCK AIRCRAFT ON RIGHT SIDE NEAR R-1 DOOR. INSTALLED REPAIR CLASS 3 PAGE 219-226 LONGERON 19R-20R STA 210-200 AS PER B717 SRM 53-00-01 AND RES 04-0289 WO 24177 AND N/R 3052 AVBORNE.Mar 27, 2004 · N980AT · Boeing 717200SDR 2004F00210Structure · vibrationDURING CLIMB, IT WAS EXPERIENCED A STRONG VIBRATION IN ALL PHASES OF FLIGHT ABOVE 300 KNOTS. THE AIRCRAFT WAS DEVIATED FROM ITS NORMAL FLIGHT SCHEDULE TO SAL STATION FOR MAINTENANCE. THE AIRCRAFT REMAINS ON GROUND AT SAL STATION FOR MAINTENANCE. (M)Dec 21, 2003 · N981LR · Airbus A320233SDR 03FDEA01096Structure · noisyPASSING 10K MSL, EXTREMELY LOUD SQUEAL APPEARED IN COCKPIT. PRESSURIZATION NORMAL. CLIMBED TO 14K AND SQUEAL REMAINED ON. NOISE WENT OUT PASSING 10K MSL IN DESCENT. SHUT OFF ALL RADIOS & COULD NOT ISOLATE PROBLEM. PRESSURIZED A/C TO 8.5 PSI NO SQUEAL OR HJul 13, 2003 · N283FE · Boeing 727200SDR DHL2003367505Angle · corrodedItem Ref. N/R: 0029420:Fwd. pit sub floor area R/H side Sta. 2029 BL55R upper floor support angle upper surface corrosion. Corrective action:Removed fastners IAW A300 SRM 51-30-30,removed corrosion floor support angle IAW A300 SRM 51-40-11. Material thickness Feb 26, 2003 · N367DH · Airbus A300B4203SDR QXEA200501777Clamp · looseSEA FLIGHT NR 2334: ON TAXI, FA HEARD LOUD GROWL SOUND AROUND ROW 12 AND BACK. ON PARKING, TURNED OFF PTU AND SOUND WENT AWAY. MAINTENANCE FOUND PARK BRAKE ACCUMULATOR (MOUNTED UNDER PTU) CLAMPS LOOSE. TIGHTENED CLAMPS. RAN PTU, NOTICEABLE NOISE DROP IN PTDec 11, 2002 · N401QX · Bombdr DHC8402SDR C2XA02TY100Floor Support · corrodedTYS During a scheduled inspection the left hand sidewall floor support at station 5292.0 was found to be corroded in several areas. Maintenance removed and replaced the flooor support IAW EMB-145 SRM 51-40-02, the repair was satisfactory. The aircraft willJun 12, 2002 · N15973 · Emb EMB145SDR DHL2002802561FittingMAIN CARGO COMPT BATH TUB FITTING WITH 3 IN CRACK IN IT STA 857.000 L-71.REMOVED CRACKED FITTING PER SRM 51-1 20D PG 21, AND SRM 51-1-23 FIG 4B. CLEANED TREATED AND PRIMED AREA PER SRM 51-1-8B. INSTALLED NEW FITTING PER SRM 51-1-20D PG 9 AND SRM 51-1-23 FIG 48May 23, 2002 · N802DH · Doug DC873SDR CA020507016Hinge · mismanufactured(CAN) HINGE HALF - MISMANUFACTURED. PLEASE NOTE RMA RECEIVED TWO C6WFM1218-27 CLEATS FROM DIFFERENT SUPPLIERS, 1 MAY 4/01 FOR RMA INVENTROY AND 1 APRIL 23/02 FOR A WORK ORDER. BOTH CLEATS ARE MISMANUFACTURED. THE CLEAT FROM C6WFM1218-27 APRIL 23/02 IS LOT 000May 2, 2002 · Dhav DHC6SDR AUS20020110Structure · corroded(AUS) EXFOLIATION CORROSION FOUND AT NO3 CARGO DOOR UPPER FORWARD SIDEAT STN 1090, STRINGER 20R. FOUND DURING CPCP INSPECTION.Jan 5, 2002 · Boeing 727277SDR C2XA02IA004Floor Support · corrodedIAH- DURING "C" CHECK IT WAS NOTED THAT THE FLOOR BEAM CROSS STRUCTURE ABOVE FUSELAGE FRAME 23 WAS CORRODED AT THE INBOARD FORWARD CORNER. IAH- MAINTENANCE REMOVED THE DAMAGED AREA,AND, INSTALLED A DOUBLER WITH A FILLER,AND, THE AIRCRAFT WAS APPROVED FOR REDec 28, 2001 · N13964 · Emb EMB145SDR IXXA0100080SClip · corrodedDURING ROUTINE C-CHECK INSPECTION CORROSION WAS DETECTED IN THE AFT CABIN FLOORBEAM AT STATION 1584. REMOVED DAMAGED FLOORBEAM AND INSTALLED NEW FLOOR SUPPORT AND CLIP NUTS IN ACCORDANCE WITH DOUGLAS STRUCTURAL MAINTENANCE MANUAL.Nov 18, 2001 · N21CX · Doug DC862SDR DHL2001801568Fitting · crackedWING CNTR SECTION (MAIN CARGO COMT)FITTING CRACKED 1 IN AT STA 798.000,XCW 23L/H.REMOVED CRACKED FITTING PER SRM 51-120D PG 21.CLEANED TREATED AND PRIMED AREA PER SRM 51-1-8B.INSTALLED NEW FITTING PER SRM 51-1-20D PG 9.Oct 11, 2001 · N801DH · Doug DC873FSDR 01FDEA00741Structure · vibrationAFTER T/O PASSING 235 KTS & CLIMBING THROUGH APPROX 4000 FT ACFT BEGAN TO VIB WITH LOUD NOISE COMING FROM BELOW & AFT OF PILOT SEATS. PACKS TURNED OFF, NO HELP. THROTTLES BACK TO IDLE, NO HELP. FLAPS DOWN TO 22 GEAR DOWN 210 KTS, NO HELP. GEAR UP 180 KTS, Aug 18, 2001 · N397FE · Doug DC1010SDR ARWA0010804Stringer · crackedDURING SCHEDULED MAINTENANCE:FOUND 2 INCH CRACK AT STATION 940 STRINGER 23R.CORRECTIVE ACTION:REPAIRED I.A.W. E.O. DRAWING # AS11300 DATED 08/09/01Aug 13, 2001 · N29UA · Doug DC861FSDR 01FDEA00574Skin · crackedN 351 #2 ENGINE INLET AFT SIDE HAS CRACK. R&R PER IAW EA & SRM REQ.Jul 18, 2001 · N377FE · Doug DC1010SDR ARWA0010709Floor PanelDURING SCHEDULE MAINTENANCE. N/R 488. DISCREPANCY: FWD ENTRY AREA, FLOOR PANEL SUPPORT STRUCTURE IS CORRODED FROM STA 260 TO STA 280 AT LBL30. CORRECTIVE ACTION: REMOVED AND REPLACED FLOOR PANEL STA260 TO 280 AT LBL 30 IAW SRM 51-40-01.Jun 29, 2001 · N307GB · Lkheed 1011385115SDR ARWA0010714BracketDURING SCHEDULE MAINTENANCE. N/R 633. DISCREPANCY: EVIDENCE OF CORROSION, RIGHT WING TO FUSELAGE BRACKET AT WHEEL WELL. CORRECTIVE ACTION: REMOVED CORROSION, FILLED AREA WITH DEVCON, FABRICATED -11 DOUBLER AND INSTALLED WITH HILOCKS. PRIMED + PAINTED AS REQUIRJun 29, 2001 · N307GB · Lkheed 1011385115SDR ARWA0010707FittingDURING SCHEDULE MAINTENANCE. N/R 493. DISCREPANCY: C2 CARGO DOOR CUT-OUT, CENTER UPPER DOOR SILL PIVOT CLEVIS ATTACH FITTING IS CRACKED. CORRECTIVE ACTION: REMOVED FASTENERS C2 CARGO DOOR CENTER UPPER DOOR SILL PIVOT FITTING, CLEAN SURFACE CORROSION IAW SRM 51Jun 29, 2001 · N307GB · Lkheed 1011385115SDR ARWA0010706SpliceDURING SCHEDULE MAINTENANCE. N/R 235. DISCREPANCY: SPLICE CRACKED AT FS 1203 BELOW WL200. CORRECTIVE ACTION: REMOVED CRACKED SPLICE & REPLACED WITH NEW ONE IAW SRM 51-40-01.Jun 29, 2001 · N307GB · Lkheed 1011385115SDR ARWA0010705SpliceDURING SCHEDULE MAINTENANCE. N/R 234. DISCREPANCY: FS 1183 BELOW WL 200 CRACK ON SPLICE. CORRECTIVE ACTION: INSTALLED SPLICE AT FS 1183 RH IAW SRM 51-40-01.Jun 29, 2001 · N307GB · Lkheed 1011385115SDR SIMA200117404Structure · vibrationMIA - FLT 5369 - VERY STRONG VIBRATION NOTICED AFTER GEAR RETRACTION, MAX SPEED 160KIAS. RETURNED TO MIA. PERFORMED NOSE LANDING GEAR FORWARD DOOR PRELOAD CHECK AND GEAR EXTENSION AND RETRACTION IAW AMM. FOUND DOORS FLUSH AND IN CONTACT WITH STOPS. OPS CHEJun 23, 2001 · N971NA · Aerosp ATR42300SDR IXXA0100048SPan · crackedDURING ROUTINE C CHECK INSPECTION, THE "A" PIT BASKET DOOR AFT CENTER SECTION DOOR PAN WAS FOUND CRACKED. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED PAN, FABRICATION AN INSTALLATION A NEW SIDE PAN IN ACCORDANCE WITH DOUGLAS STRUCTURAL REPAIR MANUAL, DACO DRAWING 5Mar 7, 2001 · N820BX · Doug DC871F
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