JASC 5350

Service difficulty reports · 6,124

Reports filed under 5350 · Aerodynamic Fairings, 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 = '5350'
  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 DLM88081406Radome · crackedBIRD STRIKE ON NOSE OF RADOME. C/W BIRDSTRIKE INSPECTION PER AMM FOUND RADOME CRACKED. REPLACED RADOME PER AMM.Oct 23, 2008 · N937DL · Doug MD88SDR LR7A08119Skin · crackedDURING SCHEDULED B-3 CHECK, PER HB5301 JOB CARD FOUND LT MLG BOTTOM SKIN FAIRING CRACKED AT FS 597, LBL40, WL129 ATTACHMENT TO BELLY AREA. REPAIRED IAW SMP583 FIG 51-140-12.Oct 15, 2008 · N404LC · Lkheed 382GSDR WRLA2008080Skin · misrepairedDURING BRIDGE CHECK, MX FOUND TAILCONE SKIN RT FWD EDGE IMPROPER TRIM OUT AT STA Y2245. REPAIRED DAMAGED AREA IAW ENGINEERING INSTRUCTION W2008A53-119 REV 00 AND EI W2008A53B-119 REV 01.Oct 6, 2008 · N384WA · Doug MD11FSDR MALA080185Fairing · dentedTWO DENTS NOTED IN THE WING TO FUSELAGE FAIRINGS. REPAIRED IAW EO S51031.Oct 2, 2008 · N428XJ · Saab 340BSDR UPS08853739Support Angle · crackedINSPECTION TYPE:SV RT UPPER WING TO FUSELAGE FILLET FAIRING 292B SUPPORT ANGLE CRACKED. REPAIRED DWG 5769482 SRM 51-1-08.Sep 30, 2008 · N702UP · Doug DC871FSDR AALA200802590Frame · crackedCANTED FRAME CRACKED AT TAIL CONE ALIGNMENT PIN AT 9 O`CLOCK POSITION. INSTALLED DOUBLER IN ACCORDANCE WITH ESO 80559 DATED 30 SEP 2008.Sep 30, 2008 · N581AA · Doug DC982SDR AALA200802589Frame · crackedCANTED FRAME IN AFT ACCESSORY AT TAIL CONE ALIGNMENT PIN BELOW MAINTENANCE LIGHT SWITCH WAS CRACKED. INSTALLED DOUBLER IN ACCORDANCE WITH ESO 80559 DATED 30 SEP 2008.Sep 30, 2008 · N581AA · Doug DC982SDR MAL2008F00037Skin · dentedDURING THE 2Y AND N4K NOTED 4 DENTS IN TAIL CONE BETWEEN STA797 AND 803. 1 ABOVE AND 3 BELOW SL1604. REPAIRED IAW EO#S53620.Sep 26, 2008 · N424XJ · Saab 340BSDR 2008FA0000674Frame · crackedDURING ROUTINE INSP FOUND FWD FRAME PN 6712617-13 CRACKED. THE CRACKED FRAME WAS LOCATED IN THE UPPER LT SIDE UNDER THE RUDDER TO STINGER FAIRING. (K)Sep 24, 2008 · N978QS · Cessna 750SDR 2008FA0000673Frame · crackedDURING ROUTINE INSP, FOUND FWD FRAME PN 6712617-13 CRACKED IN (2) LOCATIONS, ON THE TOP LT AND RT SIDES. ALSO FOUND FRAME AFT OF THIS ONE CRACKED. PN 6712617-14 ON THE TOP RT SIDE. (K)Sep 24, 2008 · N960QS · Cessna 750SDR VNAA0809007Radome · delaminatedCREW REPORTED DURING LANDING A BIRD STRIKE TO THE NOSE OF THE ACFT. MX FOUND DELAMINATION ON THE RADOME. THE RADOME WAS R&R. NO OTHER DEFECTS WERE NOTED AND ACFT WAS RELEASED FOR SERVICE.Sep 15, 2008 · N258PS · Cndair CL6002B19SDR WRLA2008106Fairing · puncturedFLIGHT 8010 09/06/08 KBWI/ETAR - DURING FLIGHT A THUMP WAS HEARD AND FELT 5 HOURS INTO FLIGHT AT FL310, NO ABNORMAL INDICATIONS OR HANDLING FOLLOWED. DURING POST FLIGHT INSPECTION, MAINTENANCE FOUND LT WING LDG EDGE WING/BODY FAIRING PUNCTURED AND CRACKED. RSep 6, 2008 · N14075 · Doug DC1030SDR MK7A0811084266Fairing · crackedFOUND CRACKS RADIATING FROM A SINGLE SCREW BORE DURING ROUTINE INSPECTION. INSTALLED NEWLY REPAIRED AND PAINTED ASSY. FOLLOWING DOUBLER INSTALLATION AT SCREW BORE POSITIONS. THIS PART HAS HAD A HISTORY OF SIMILAR CRACK DEVELOPMENT UNTIL DOUBLERS WERE APPLIED. Sep 1, 2008 · N817MH · Urocop EC130B4SDR 08FDEA03696Angle · crackedTHERE IS A CRACKED ANGLE AT THE RT WING TO BODY FAIRING SUPPORT AT BS 1581 BOTTOM EDGE. HEAT TREATED IAW TPS 1003; REV A. FABRICATED THE REPAIR IAW SRM 53-00-01 FIG 2 VOL I. ALODINED & PRIMED IAW SRM 51-21-01 VOL II. INSTALLED THE REPAIR IAW SRM 51-35Sep 1, 2008 · N550FE · Doug MD1010FSDR 08FDEA03695Tee Fitting · crackedTHERE IS A CRACKED VERTICAL ANGLE AT THE RT OVERWING TO BODY FAIRING SUPPORT AT STA 1441. REMOVED TEE ANGLE IAW SRM 51-31-01 VOL II. IAW DWG ANB 7049 REV E. ANNEALED IAW TPS 1003 REV A. FORMED NEW TEE IAW ANB 7049 REV E. LOCATED & DRILLED IAW SRM 51-31-01Sep 1, 2008 · N550FE · Doug MD1010FSDR 08FDEA03694Bracket · crackedTHERE IS A CRACKED BRACKET AT THE RT OVERWING TO BODY FAIRING SUPPORT AT BS 1421 L32R. REMOVED ANGLE IAW SRM 51-31-01 VOL II. FABRICATED IAW DWG ANB 7051 REV C . HEAT TREATED IAW TPS 1003 REV A. ALODINED & PRIMED IAW SRM 51-21-01 PGS 21 & 24 VOL II. INSTASep 1, 2008 · N550FE · Doug MD1010FSDR 08FDEA03693Angle · crackedTHERE IS A CRACKED VERTICAL ANGLE AT THE RIGHT OVERWING TO BODY FAIRING SUPPORT AT STA 1421. REMOVED ANGLE IAW SRM 51-31-01 VOL II. FABRICATED IAW DWG AUB 7051; REV " C ". HEAT TREATED IAW TPS 1003 REV " A ". LOCATED & DRILLED HOLES IAW SRM 51-31-01 VOLSep 1, 2008 · N550FE · Doug MD1010FSDR 08FDEA03692Bracket · crackedTHERE IS A CRACKED BRACKET AT THE LEFT OVERWING TO BODY FAIRING PANEL SUPPORT AT STA 1341; BELOW LONGERON 31L. REMOVED ANGLE IAW SRM 51-31-01 VOL II. HEAT TREATED IAW TPS 1003; REV " A ". ALODINED & PRIMED IAW SRM 51-21-01 PGS 21 & 24 VOL II. INSTALLED Sep 1, 2008 · N550FE · Doug MD1010FSDR 08FDEA03691Bracket · crackedTHERE IS A CRACKED BRACKET AT STA 1361 BETWEEN LONGERONS 31L & 32L. REMOVED ANGLE IAW SRM 51-31-01 VOL II. HEAT TREATED IAW TPS 1003; REV " A ". ALODINED & PRIMED IAW SRM 51-21-01 PGS 21 & 24 VOL II. INSTALLED IAW SRM 51-31-01; VOL II.Sep 1, 2008 · N550FE · Doug MD1010FSDR 08FDEA03690Bracket · crackedTHERE IS A CRACKED BRACKET AT THE LEFT OVERWING TO BODY FAIRING SUPPORT BETWEEN LONGERON 31L & 32L AT STA 1401. REMOVED ANGLE IAW SRM 51-33-01 VOL II. FABRICATED A NEW ANGLE, HEAT TREAT IAW TPS 1003, REV " A ". ALODINED & PRIMED IAW SRM 51-21-01 PGS 21 & 2Sep 1, 2008 · N550FE · Doug MD1010FSDR 08FDEA03689Bracket · crackedTHERE IS A CRACKED BRACKET AT THE LEFT OVERWING TO BODY FAIRING SUPPORT STRUCTURE AT STA 1421 & LONGERON 32L. REMOVED ANGLE IAW SRM 51-33-01 & SRM 51-31-01 VOL II. HEAT TREATED IAW TPS 1003; REV " A ". ALODINED & PRIMED IAW SRM 51-21-01 PGS 21 & 24 VOL II.Sep 1, 2008 · N550FE · Doug MD1010FSDR 08FDEA03688Angle · brokenTHERE IS A BROKEN VERTICAL ANGLE AT THE LEFT WING TO BODY FAIRING SUPPORT AT STA 1421; ABOVE THE LEFT WING. REMOVED & REPLACED ANGLE ANB 7051-3 IAW SRM 51-31-01; VOL II.Sep 1, 2008 · N550FE · Doug MD1010FSDR LR7A08099Skin · warpedDURING SCHEDULED C-9 CHECK, PER JOB CARD HST5301 FOUND RT WW BOTTOM FAIRING SKIN WARPED AT FS 507, WL130, RBL 50. REPAIRED IAW SMP583 CHAP 51-60, 51-70 AND DWG 338735.Aug 19, 2008 · N401LC · Lkheed 382GSDR VNAA0808008Radome · damagedCREW REPORTED LIGHTNING STRIKE. MAINTENANCE INSPECTED ACFT AND REPAIRED DAMAGE ON RADOME AND LT WINGLET. NO OTHER DEFECTS NOTED. ACFT WAS RELEASED FOR SERVICE. (S)Aug 15, 2008 · N257PS · Cndair CL6002B19SDR 08FDEA03388Fairing · crackedPANEL RACK, WING BODY FAIRING 3517 AFT CORNER EXISTING COMPOSITE REPAIR IS CRACKED. REPAIRED PANEL 3517 REF SRM 51-40-9 STEP 7B(1)-7B(12) AND AMM 51-20-151-7. THIS IS CLASSIFIED AS A MINOR REPAIRAug 12, 2008 · N211FE · Boeing 7272S2FSDR 08FDEA03221Frame · corrodedLOWER FUSELAGE LEFT MID SUPPORT FRAME FOR FAIRING 197LL HAS SURFACE CORROSION. REPAIR CARRIED OUT ON WING-TO-BODY FUSELAGE STRUCTURE LOWER CHORD IAW EA NR F-5320-124303. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100.Aug 3, 2008 · N919FD · Boeing 75723ASDR 2008UALA04029Fairing · looseLOOSE PANEL OR FAIRING ON LEFT MID WING AREA FLOATING APPROX 3 INCHES, REPORTED BY FLT ATTENDANTS AND PASSENGERS AND CONFIRMED BY FIRST OFFICER. NO ABNORMAL FLIGHT CHARACTERISTICS. RTFL. *S/D* REPLACED LEFT OUTBOARD RUB STRIP.Jul 28, 2008 · N487UA · Airbus A320232SDR MWE2008F00023Latch · failedWHILE PERFORMING TAILCONE FUNCTIONAL CHECK, INTERIOR HANDLE FAILED TO PULL FROM THE CLIPS. CLEANED DEBRIS AND MINOR CORROSION FROM INNER SURFACES OF RETENTION CUPS. INTERIOR TAILCONE RELEASE HANDLE FORCE CHECKS NOW. (K)Jul 25, 2008 · N927ME · Boeing 717200SDR 08FDEA02984Fairing · crackedRT BODY FAIRING PANEL NR 3349 CRACKED AT EDGE. REMOVED DAMAGED EDGE PLATE. VERIFIED MATERIAL FOR NEW EDGE PLATE, FABRICATED NEW EDGE PLATE, TREATED AND PRIMED AND INSTALLED. REF DWR 65-58505 AND SRM 51-10- 2 PG1, 51-30-2 PG1. THIS IS CLASSIFIED AS A MINORJul 19, 2008 · N273FE · Boeing 727233SDR 08FDEA02976Attach Angle · chafedTAILCONE ACCESS PANEL, CUT OUT, FWD EDGE LATCHING POSITIONS ARE MISSING MATERIAL IN 2 PLACES. FABRICATED A NEW ATTACH ANGLE IAW DC/MD-10 SRM 53-52-01, VOL III AND DAC DWG NRC 6022. ALODINED AND PRIMED ANGLE IAW DC/MD-10 SRM 51-21/01, VOL II. REMOVED AND IJul 18, 2008 · N372FE · Doug MD1010FSDR AIEA200800263Fairing · damagedDURING ARRIVAL WALKAROUND INSPECTION FOUND LOWER RT AFT OF BODY GEAR FUSELAGE FAIRING DAMAGED. ACCOMPLISHED TIME LIMITED REPAIR AS PER EO 4453A188 DATED 7/8/08 ENTERED NON MEL DMI N08-037 FOR REPEAT INSPECTION OF PANEL AT EVERY A-CHECK. (A)Jul 8, 2008 · N408MC · Boeing 74747UFSDR CA080716007Fairing · damaged(CAN) FIRST AIR HAS OBSERVED SEVERAL OCCURRENCES OF DEGRADATION IN THE SURFACE PROTECTION COATING ON THE ACFT LOWER CENTER SECTION FAIRING PANELS. THE MATERIAL IS APPLIED IN ACCORDANCE WITH ATR SERVICE BULLETIN ATR42-53-0102. INVESTIGATION HAS FOUND THAT THE DJul 7, 2008 · Aerosp ATR42300SDR 08FDEA02127Frame · corrodedCORROSION ON TOP OF WING TO BODY FAIRING FRAME WORK AT TWO FWD ADF ANTENNA LEAD POSITION CLAMP ATTACH AT FS 730F, RBL 10, INBOARD OF RT RAM AIR DUCT REMOVED PANELS REF SRM 51-30-2, REMOVED CORROSION REF SRM 53-10-01. FOUND TO BE OUT OF LIMITS REF SRM 51-20-01Jun 3, 2008 · N220FE · Boeing 727233SDR 08FDEA01979Panel · dentedFILLET PANEL NR 152 LT IS DENTED. REPAIRED DAMAGED AREAS (2 EACH) BY REPLACING THE CORE AND APPLYING WET FIBERGLASS OVERLAYS IAW DC/MD-10 SRM 51-62-01; VOL II AND SRM 51-43-01; VOL II; PARA 16. RESTORED SURFACE FINISH IAW DC/MD-10 SRM 51-21-02; VOL II. REMOMay 23, 2008 · N567FE · Doug MD1010FSDR 08FDEA01672Skin · dentedTHE TAILCONE, RIGHT SIDE EXTERNAL SKIN HAS A DENT. REMOVED THE DAMAGE FROM THE RIGHT SIDE EXTERNAL SKIN OF THE TAILCONE IAW SRM 53-00-01; PGS 46 & 50; VOL I. FABRICATED REPAIR DOUBLER; ALODINED; PRIMED AND TOP COATED IAW SRM 51-21-01; VOL II.Apr 29, 2008 · N567FE · Doug MD1010FSDR 2008UALA02452Light · inoperativeEMERGENCY EXIT LIGHT STRIP ON FLOOR AT THE G6 GALLEY IS INOP. REMOVED AND REPLACED EEL STRIP AT G6 GALLEY FLOOR. OPS CHECKED GOOD.Apr 27, 2008 · N314UA · Boeing 737322SDR 08FDEA01625Floor Panel · delaminatedTAIL CONE, PATIO FLOOR; DOOR; DELAMINATED. FABRICATED NEW PATIO FLOOR DOOR; POTTED EDGES, COMPLETED CURE & SANDED THE EDGE POTTING, INSTALLED INSERTS; APPLIED NON-SKID. PART MARKED PANEL; REMOVED HARDWARE FROM THE OLD PANEL & REINSTALLED THE HARDWARE OApr 25, 2008 · N567FE · Doug MD1010FSDR 08FDEA01624Intercostal · crackedTAIL CONE, PATIO DOOR, LATCHING MECHANISM, LT SIDE, INTERCOSTAL CRACKED. REMOVED CRACKED INTERCOSTAL FROM THE TAIL CONE IAW SRM 51-35-01; VOL II. HEAT TREATED IAW DWG HT 042808-6, TESTED 58-60 ON RWD. FABRICATED NEW INTERCOSTAL IAW DWG AKC 7150. ALODINED Apr 25, 2008 · N567FE · Doug MD1010FSDR 08FDEA01531Panel · delaminatedAIR CONDITION EXTERNAL FAIRING PANEL NR 144 HR IS DELAMINATING ON THE INTERNAL SKIN. REPAIRED PANEL BY REMOVING THE DAMAGE AND APPLYING A WET LAY UP IAW SRM 51-77-12 AND RESTORED THE FINISH IAW SRM 51-75-10.Apr 24, 2008 · N661FE · Airbus A300F4605RSDR 08FDEA01510Panel · damagedA/C FAIRING LEFT PANEL 143 FL IS DAMAGED FROM FRETTING. REMOVED DAMAGE; PREPPED THE AREA FOR REPAIR; APPLIED LAY-UP REPAIR & REFINISHED THE SURFACE IAW A300-600 SRM 51-77-12 & SRM 53-15-73.Apr 23, 2008 · N661FE · Airbus A300F4605RSDR P5CA0801557Fairing · dentedLT WING TO BODY FAIRING PANEL 191KL SKIN DENTED EO NR 4453A160 ISSUED AND REQUIRES RE-INSPECTION EVERY 25 FLIGHT CYCLES.Apr 17, 2008 · N450PA · Boeing 74746NFSDR RYNA200800023Brace · crackedFUSELAGE TO LEFT WING FAIRING SUPPORT BRACES ARE CRACKED AT BS 807 NEAR WING LEADING EDGE AREA. REPLACED CRACKED SUPPORT BRACES PER MD-80 SRM 51-10-2.Apr 11, 2008 · N932RD · Doug DC982SDR AALA200800859Release Cable · frayedTUL - RELEASE HANDLE CABLE ASSEMBLY HAS WORN AND FRAYED CABLE ON LEFT SIDE ABOVE THE MID POINT PULLEY. AREA OF DISCREPANCY WAS .125 INCH BY .125 INCH. REPLACED TAILCONE RELEASE CABLE ASSEMBLY ON LEFT SIDE. OPERATIONS CHECK NORMAL.Apr 8, 2008 · N479AA · Doug DC982SDR SROM2008001Support · gougedLEFT HAND MAIN LANDING GEAR WHEEL WELL FAIRING SUPPORT GOUGED AT AFT OUTBOARD SIDE. REPAIRED LT MLG WHEEL WELL SUPPORT AT AFT OUTBOARD SIDE IN ACCORDANCE WITH FAA DER APPROVED FORM 8110-3, 073-1236-08-476 AND ASI SOLUTIONS DRAWING 5350476-1, REV IR, DATED MARCApr 6, 2008 · N733PA · Boeing 737205SDR UPS08M52614Frame · chafedINSP TYPE-C, FWD TAILCONE ACCESS CUT OUT LT FRAME, FOUND CHAFED MARK ON PREVIOUS REPAIR. FWD TAILCONE UPPER FWD DOOR OPENING MECH ASSY REMOVED FOR ACCESS. CHAFE MARK FOUND OUT OF LIMIT & REMOVED IAW SRM 51-31-01 VII R35. FAB NEW FWD TAILCONE FRAME WITH HEATApr 1, 2008 · N295UP · Doug MD11SDR 08FDEA01212Frame · gougedTAIL CONE RIGHT UPPER PATIO DOOR HINGE FRAME IS GOUGED, MATERIAL ID 2024-T3; PO 600955.2 PER DC/MD-10 SRM 53-52-01; VOL III. ALODINED AND PRIMED PER DC/MD-10 SRM 51-21-01; VOL II. INSTALLED DOUBLER PER DC/MD-10 SRM 53-00-01; VOL I.Mar 31, 2008 · N365FE · Doug MD1010FSDR 08FDEA01050Skin · damagedTAIL CONE UPPER AFT SKIN HAS 3 HOLES (LT AFT EDGE). REPAIRED HOLES PER SRM 53-00-01; VOL I. DOUBLER PER SRM 53-00-01; VOL I AND SRM 53-52-01; VOL III; PO 483358.1. ALODINED AND PRIMED PER SRM 51-21-01; VOL II. INSTALLED PER SRM 53-00-01; VOL I AND SRM 51-Mar 19, 2008 · N365FE · Doug MD1010FSDR UPS08M52409Skin · chafedINSPECTION TYPE:C, RIGHT TAIL CONE DOOR ASSY INTERIOR BELOW BARRIER KEEPER SKIN CHAFED. KEEPER SKIN CHAFE MARK REMOVED & REPROTECTED. MAT'L REMOVED 0.008" ORG THK 0.032", REMN THK 0.024" FOUND OUT OF LIMIT. EXCEEDED LIMIT SKIN TRIMMED OFF. HFEC INSP C/O ONMar 17, 2008 · N295UP · Doug MD11SDR 200800309Skin · scratchedRT UPPER AFT WING TO BODY FAIRING, FROM STA 1480 TO STA 1860 FROM STR 23R TO STR 34R HAS SCRIBE MARKS. APPROX STA 1560 STR 39R .003 DEPTH. BLENDED OUT SCRIBE LINES, MATERIAL LOSS IS .003 WITHIN LIMITS ALODINED AND PRIMED AREA PER B747 SP SRM'S 53-31-00 PG 1-Mar 17, 2008 · N708BA · Boeing 747SPB5SDR 200800308Skin · scratchedRT LOWER FWD WING TO BODY FAIRING, FROM STA 620 TO STA 580 FROM STR 34R TO STR 47R SKIN HAS SCRIBE MARKS. APPROX STA 600 STR 32R .005 DEPTH. BLENDED OUT SCRIBE LINES, MATERIAL LOSS IS .005 WITHIN LIMITS, ALODINED AND PRIMED AREA PER B747 SP SRM'S 63-31-00 PGMar 17, 2008 · N708BA · Boeing 747SPB5
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