JASC 5415

Service difficulty reports · 1,305

Reports filed under 5415 · Nacelle/Pylon, Attach Fittings, 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 = '5415'
  ORDER BY difficulty_date DESC"

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SDR DL757070446Fitting · damagedDURING ACCOMPLISHMENT OF EA 06-070332-03AD, SIP MOD, HOLE NR 51 AS IDENTIFIED IN THE EA REQUIRED OVERSIZING BEYOND THE EA MAX. THE EA ALLOWS OVERSIZING TO 1ST OVER, AND THE HOLE REQUIRED OVERSIZING TO 2ND OVER. BOEING PROVIDED AMOC 8100 APPROVAL OF THE OVERSMay 4, 2007 · N627DL · Boeing 757232SDR QXEA200700758Fitting · crackedC4 PDX - LEFT NACELLE OUTBOARD SHOULDER FITTING IS CRACKED LOCATED AT UPPER OUTBOARD SECTION OF NACELLE FORMER XN210.0. REPAIRED IAW RD8/4-54-154 AND SRM 51-42-05.Apr 29, 2007 · N401QX · Bombdr DHC8402SDR 2007UALA01270Lug · corrodedBORE CORRODED AND SCRATCHED - NR 1 PYLON STRUT FITTING BEARING LUG, BOTH SIDES. [SUP 05-16-07] BORE CORRODED AND SCRATCHED - NR 1 PYLON STRUT FITTING BEARING LUG, BOTH SIDES. ACCOMPLISHED BORING THE DSB UNDER WING FITTINGS PER COA 899993040 & SB 747-54A2218Apr 24, 2007 · N178UA · Boeing 747422SDR 2007UALA01269Lug · corrodedBORE CORRODED AND SCRATCHED - NR 1 PYLON UNDER WING FITTING BEARING LUG, BOTH SIDES. [SUP 05-16-07] BORE CORRODED AND SCRATCHED - NR 1 PYLON UNDER WING FITTING BEARING LUG, BOTH SIDES. ACCOMPLISHED BORING THE DSB UNDER WING FITTINGS PER COA 899993040 & SB 74Apr 24, 2007 · N178UA · Boeing 747422SDR 2007UALA01268Lug · corrodedBORE CORRODED AND SCRATCHED - NR 4 PYLON DUAL SIDE BRACE FITTING BEARING LUG, BOTH SIDES. [SUP 05-16-07] BORE CORRODED AND SCRATCHED - NR 4 PYLON DUAL SIDE BRACE FITTING BEARING LUG, BOTH SIDES. ACCOMPLISHED BORING THE DSB UNDER WING FITTINGS PER COA 8999930Apr 24, 2007 · N178UA · Boeing 747422SDR 2007UALA01267Lug · corrodedBORE CORRODED AND SCRATCHED - NR 4 PYLON UNDER WING FITTING BEARING LUG, BOTH SIDES. [SUP 05-16-07] BORE CORRODED AND SCRATCHED - NR 4 PYLON UNDER WING FITTING BEARING LUG, BOTH SIDES. ACCOMPLISHED BORING THE DSB UNDER WING FITTINGS PER COA 899993040 & SB 74Apr 24, 2007 · N178UA · Boeing 747422SDR KCSA071150Brace · gougedNR 1 PYLON DIAGONAL BRACE HAS TWO GOUGES AT FWD ATTACH POINT.Apr 16, 2007 · N709CK · Boeing 747132SDR KCSA071149Brace · chafedNR 4 PYLON DIAGONAL BRACE CHAFED OUT OF LIMITS AT LOWER ATTACH POINT.Apr 16, 2007 · N709CK · Boeing 747132SDR 2007UALA01157Fitting · damagedNR 2 PYLON AFT OTBD MID-SPAR FITTING UPPER TANG HAS DRILL START BESIDE FASTENER HOLE. [06-14-07] MAJOR REPAIR ACCOMPLISHED. REPAIRED DAMAGED AREA. CLEANED DRILL START WITH SPOT FACE. SHOT PEENED, PASSIVATED AND INSTALLED FASTENER.Apr 14, 2007 · N506UA · Boeing 757222SDR 07FDEA01477Attach Fitting · corrodedCORROSION ON PYLON NR 2 BEARING HOLE ON RIB 18 LOWER ATTACH FITTING. REPAIR PERFORMED BY REAM UP HOLE AND CHAMFER ON EACH SIDE IAW SB: A310-54-2021 AND EA 6-5451-103241.Apr 12, 2007 · N810FD · Airbus A310SDR UIEA200700158Attach Angle · crackedNR 2 PYLON CAP SKIN OUTBOARD LOWER ATTACH ANGLE FOUND CRACKED AS MARKED. REPAIRED AS PER SRM 54-11-02 FIG 7.Apr 3, 2007 · N516MC · Boeing 747243BSDR 07FDEA01309Nacelle · crackedNR 1 ENGINE FIXED COWL UPPER SECTION CRACKED AT UPPER FWD CORNER. REPLACED FIXED COWL, NEW COWL INSTALLED ON WC 70T0001-01.Apr 3, 2007 · N463FE · Boeing 727225SDR BUW2007F00002Fitting · looseDURING THE INSPECTION FOR SB 07-71-01 THE FUEL RETURN LINE AT THE FIREWALL BULKHEAD FITTING WAS FOUND LOOSE. (K)Apr 1, 2007 · N199CA · Cessna 182TSDR DL76L070515Fitting · damagedTHE NR 1 PYLON MID SPAR ATTACH FITTING WAS DAMAGED BY AND ELECTRICAL SHORT. THE DAMAGED AREA OF THE FITTING WAS BLENDED AWAY, NO REINFORCEMENT NECESSARY.Mar 31, 2007 · N191DN · Boeing 767332SDR 07FDEA01158Attach Fitting · corrodedFOUND CORROSION IN AFT PYLON ATTACH FITTING HOLE , PYLON NR 2, RIB 18 REPAIR PERFORMED WITH SB A31-52-2021, APPROVED BY EA 6-5450-106340.Mar 28, 2007 · N816FD · Airbus A310304SDR 07FDEA01157Attach Fitting · corrodedCORROSION IN AFT PYLON ATTACH FITTING HOLE , PYLON NR 2, RIB 18 REPAIR PERFORMED WITH SB A31-52-2021, APPROVED BY EA 6-5450-106340.Mar 28, 2007 · N816FD · Airbus A310304SDR EIA2007068Attach Angle · crackedNR 3 PYLON STA 270 BULKHEAD AFT SIDE I/B AND AFT O/B OF FRONT SPAR CHORD ASSY HAS SKIN TO BULKHEAD ATTACH ANGLES CRACKED. REPAIRED NR 3 PYLON STA 270 BULKHEAD AFT SIDE I/B AND O/B SIDE SKIN TO BULKHEAD ATTACH ANGLES PER B747 SRM 54-120-03 FIG 19, 51-20-01 FIGMar 22, 2007 · N479EV · Boeing 747132SDR 07FDEA01052Mount · chafedOLD CHAFING MARK ON PYLON NR 1 FWD PYLON TO ENGINE MOUNT FITTING. REPAIR PERFORMED BY INSTALLATION OF AN PROTECTION ANGLE, APPROVED BY RAS 018876/027/2002 ISSUE "A" AND EA 6-5450-106441.Mar 21, 2007 · N816FD · Airbus A310304SDR DL76L070222Angle · crackedTHE NR 1 PYLON MIDSPAR FITTING CLOSEOUT ANGLE WAS FOUND CRACKED. THE CRACKED ANGLE WAS REPLACED, REF AD 2005-19-23, 01-074944-12AD.Mar 20, 2007 · N172DN · Boeing 767332SDR 07FDEA01028Bolt · shearedNR 1 ENG PYLON FWD LOWER ATTACH FITTING/TOMBSTONE HAS 2 BOLTS PULLED, OUT/SHEARED AT 3:00 O`CLOCK AND 9:00 O`CLOCK POSTION. REMOVED LOWER PLUG PLATE AND 6EA. BOLTS IN REFERANCE TO MM 54-00-01-4. INSPECTED ALL 6EA BOLT HOLES AND FOUND NO CORROSION. INSTALLEMar 20, 2007 · N396FE · Doug MD1010FSDR DL76L070223Angle · crackedTHE NR 2 PYLON MIDSPAR FITTING CLOSEOUT ANGLE WAS FOUND CRACKED. THE CRACKED ANGLE WAS REPLACED, REF AD 2005-19-23.Mar 19, 2007 · N172DN · Boeing 767332SDR DL76L070219Fitting · crackedTHE NR 2 PYLON MIDSPAR FITTING WAS FOUND WITH A CRACK IN ONE FASTENER HOLE. THE FASTENER HOLE WAS OVERSIZED TO REMOVE THE CRACK. REF AD 2005-19-23; 01-074944-12AD.Mar 18, 2007 · N172DN · Boeing 767332SDR 07FDEA00866Attach Fitting · dentedNICK IN PYLON ATTACH FITTTING AND PYLON REINFORCEMENT PLATE. REPAIR WAS PERFORMED IAW EA 6-5720-103365 AND RAS/BAE/1003600/2006 ISSUE "A" (BLEND OUT).Mar 15, 2007 · N813FD · Airbus A310324SDR QXEA200700420Mount · corrodedC4 PDX - FOUND LEFT MAIN LANDING GEAR ACTUATOR UPPER MOUNT POINT ON H MEMBER HAS FRETTING CORROSION ABOVE BOLT HOLE. REPAIRED IAW RD8-54-1178.Mar 14, 2007 · N367PH · Dhav DHC8202SDR QXEA200700422Mount · corrodedC4 PDX - LEFT MAIN LANDING GEAR ACTUATOR LOWER MOUNT ON H MEMBER HAS FRETTING CORROSION AROUND LOWER BOLT HOLES. REPAIRED IAW RD8-54-1178.Mar 14, 2007 · N367PH · Dhav DHC8202SDR DL76L092046Fitting · unknownNACELLES/PYLONS ATTACH FITTING - MIDSPAR FITTING REPAIR IAW EO 01-074944-12 ME03 POS 1, C/W EO 01-074944-12, ME03, POS 1.Mar 13, 2007 · N172DN · Boeing 767332SDR 07FDEA00795Skin · damagedPYLON SUPPORT BRACKET HOLES ON LT/RT WING BOTTOM SKIN DAMAGED. REPAIR PERFORMED IAW EA 6-5720-103398.Mar 13, 2007 · N813FD · Airbus A310324SDR DHL2007781005Attach Angle · crackedFOUND UPPER OTBD NR 3 PYLON ATTACH ANGLE CRACKED AT HOLE "P" AT ENG BL 28, REF B727 SB 54A0010. REMOVED CRACKED ANGLE, FABRICATED NEW ANGLE FROM P/N 4130 ANNEALED, .100" X 20.5" X 3", PO NR 7114153, PER B727 SRM 54-10-2 FIG 3, 51-30-2, AND 51-30-5. HEAT TREAFeb 26, 2007 · N781DH · Boeing 727227SDR F3LA200700028Bearing · corrodedDURING C-2 CHECK, INSPECTION REPORTED RT PYLON PANEL 483BL, BOTH SPHERICAL BEARINGS HAD CORROSION. REPLACED BEARINGS IAW AMM 20-21-11-991-003.Feb 18, 2007 · N929FR · Airbus A319111SDR F3LA200700032Bearing · corrodedDURING C-2 CHECK, INSPECTION REPORTED LT PYLON PANEL 473BL, ONE SPHERICAL BEARING CORRODED. REPLACED SPHERICAL BEARING PER AMM 51-42-11.Feb 16, 2007 · N929FR · Airbus A319111SDR DL76S070094Fitting · scoredDURING THE ACCOMPLISHMENT OF BOEING S/B 767-54-0081 R1 WHILE IN HMV AT ACTS THE OUTBOARD PYLON SIDE LOAD FITTING BORE WAS WITH DEEP SCORE MARKS AND OVERSIZED TO 2.244" WHICH EXCEEDS S/B CLEANUP LIMITS. THIS IS SUBJECT TO AD 2004-16-12. THE DAMAGE WAS CLEANEDFeb 7, 2007 · N126DL · Boeing 767332SDR 07FDEA00204Attach Angle · chafedNR 1 PYLON LT ATTACH ANGLE FOR PANEL 488GL CHAFED. REMOVED, FABRICATED AND INSTALLED NEW DOUBLER IAW AUB7198 REV AN, DC/MD 10 SRM 51-35-01 VOL II. MECH 2891, QC227.Jan 30, 2007 · N368FE · Doug MD1010FSDR 07FDEA00203Attach Angle · chafedNR 1 PYLON ATTACHED ANGLE FOR PANEL 488GL CHAFED. REMOVED, FABRICATED AND INSTALLED NEW DOUBLER IAW DAC DRAWING AUB7108 REV AN, AND DC10/MD 10 SRM 51-35-01 VOL II, MECH 2891, QC227.Jan 30, 2007 · N368FE · Doug MD1010FSDR CA070123008Fairlead · worn(CAN) DURING MAINTENANCE INSPECTION , FOUND AFT FUSELAGE EQUIPMENT BAY HYDRAULIC LINE CLAMPS (FAIRLEAD), WITH CENTER (PRESSURE LINE) HOLES WORN THROUGH RUBBER/SILICON COMPOUND AND ALLOWING TUBING TO CHAFE ON METAL PORTION OF BLOCK. BLOCK PN TA3050024-03 CONSIJan 23, 2007 · Cndair CL6002B19SDR SWIA200717666Beam · crackedRIGHT NACELLE INBOARD BEAM AT HYDRAULIC BAY IS CRACKED, DISCOVERED DURING A-CHECK INSPECTION. REPLACED RIGHT NACELLE INBOARD BEAM AT HYD BAY PER SRM 51-40-02 AND SEE RII 54-900-1000.Jan 13, 2007 · N215SW · Emb EMB120ERSDR SWIA200617649Support · crackedLEFT NACELLE OUTBOARD SUPPORT JUST FORWARD OF HYD BAY FIREWALL IS CRACKED, DISCOVERED DURING C-CHECK INSPECTION. REPAIRED OUTBOARD SUPPORT HALF FRAME FORWARD OF HYD BAY FIREWALL IN LEFT NACELLE PER SRM 54-20-04 FIG 201 AND RII 54-900-1000.Nov 4, 2006 · N218SW · Emb EMB120ERSDR USAA061294Skin · crackedFOUND SKIN CRACKED NR 1 ENG PYLON AT PANEL 5727 O/B SIDE. INSTALLED DOUBLER IAW TY 54-30-07, DEFECT SIZE: 3".Oct 30, 2006 · N406US · Boeing 737401SDR YENA200679Cowl Door · delaminatedON C4 CHECK INSPECTION, ENG NR 1 OUTBOARD FAN COWL DELAMINATION FOUND ON THE OUTER SKIN BEYOND STRUCTURAL LIMITS, 40" LONG X 21" WIDE APPROXIMATELY. REMOVED AND REPLACED NR 1 ENG OUTBOARD FAN COWL AS PER AMM 71-13-16.Oct 20, 2006 · N543JB · Airbus A320232SDR DL76S060869Fitting · damagedTHE NUMBER 2 PYLON UPPER SPAR FITTING WAS FOUND TO HAVE A PREVIOUSLY OVERSIZED HOLE, AT THE AFT OUTER PERIMETER FASTENER. A BOEING APPROVED REPAIR WAS INSTALLED AT THE SUBJECT LOCATION, PER ERA 456536-14.Oct 20, 2006 · N123DN · Boeing 767332SDR DL76S060793Fitting · fatiguedDURING REWORK OF THE FORWARD UPPER SPAR FITTING PER SIP EO, CRACKING INDICATIONS WERE FOUND AT AFT OUTBOARD FASTENER LOCATIONS COMMON TO MIDSTRUT BULKHEAD FITTING ON EACH PYLON. HOLES WERE OVERSIZED AND BUSHED BACK TO DIAMETER.Sep 28, 2006 · N124DE · Boeing 767332SDR IXXA06SMN312SClamp · improperDURING ROUTINE C CHECK INSPECTION, FOUND ON NUMBER 2 PYLON ACCESS DOOR NUMBER 297, GENERATOR FEEDER CABLES ATTACH CLAMP IMPROPER. REMOVED FASTENERS. REMOVED DAMAGED AREA. FABRICATED REPAIR PARTS, (AL 2024 T3 0.016). BONDED BOTH PARTS WITH HYSOL. CLEANED, Sep 21, 2006 · N825BX · Doug DC871FSDR DL757060762Fitting · oversizedNR 2 PYLON UPPER LINK WING FITTING WAS FOUND WITH AN INNER LUG DIA. GREATER THAN ALLOWED. THE HOLE WAS OVERSIZED AND INSPECTED. AN OVERSIZED BUSHING WAS INSTALLED. REF AD 2003-18-05Sep 13, 2006 · N632DL · Boeing 757232SDR QXEA200602513Attach Bracket · crackedC4 YYC - RIGHT NACELLE OUTBOARD ANTI-SKID VALVE ATTACHMENT BRACKET CRACKED. REPAIRED IAW EA 2-54-295 AND SRM 51-40-11.Sep 9, 2006 · N357PH · Dhav DHC8202SDR QXEA200602122Attach Fitting · corrodedPDX C4 - NR 2 LEFT MAIN LANDING GEAR RETRACTION ACTUATOR ATTACHMENT FITTING AND MOUNTING SURFACE ON NACELLE HAVE CORROSION AND PITTING. REPAIRED IAW RD 8-54-1178, PAGE 1.Aug 12, 2006 · N359PH · Dhav DHC8202SDR YEN200678Cowl Door · debondedENG NR 1 LT FAN COWL DOOR INNER AND OUTER SKIN WAS FOUND DISBONDED OUT OF THE SRM ALLOWABLE LIMITS. DAMAGE IS 36 BY 15 INCHES. REMOVED AND REPLACED NR 1 LT FAN COWL AS PER AMM 71-13-16.Aug 11, 2006 · N565JB · Airbus A320232SDR DL76S060603Fitting · crackedTHE NR 2 PYLON OUTBOARD PITCH LOAD FITTING WAS FOUND CRACKED. THE CRACKED HOLE WAS OVERSIZED TO REMOVE THE DAMAGE AND AN OVERSIZED FASTENER WAS INSTALLED REF AD 2004-16-12.Jul 21, 2006 · N122DL · Boeing 767332SDR HALA0600636Attach Angle · crackedNR 1 ENG STRUT ACCESS 447DB CUTOUT O/B SMALL ATTACH ANGLE LOOSE WITH POSSIBLE CRACK IN UPPER RADIUS, APPROX 8 INCHES AFT OF DIAGONAL BRACE AFT END. REMOVED NR 1 ENG STRUT ACCESS 447DB CUTOUT O/B SMALL ATTACH ANGLES. FABRICATED NEW ANGLES, HEAT TREATED, DRILLJul 19, 2006 · N596HA · Boeing 767300SDR AWXA200601443Skin · dentedSAL - DENT ON EXTERNAL SKIN AT LOWER SIDE PANEL RT OF FWD FUSELAGE SECTION ON FS 19 + 1" STRINGER 31 + 1". MAINTENANCE PERFORMED PERMANENT REPAIR ON EXTERNAL SKIN AT LOWER SIDE PANEL RT OF FWD FUSELAGE SECTION ON FRAME 19 + 1" STRINGER 31 + 1" IAW SRM A320 53Jul 19, 2006 · N619AW · Airbus A320232SDR DL76S060586Fitting · damagedDURING ACCOMPLISHMENT OF S/B 767-54-0081, THE SIDE LINK FITTING WAS SPOTFACED IN THE WRONG LOCATION. A FILLER WAS INSTALLED IN THE SPOTFACED AREA.Jul 13, 2006 · N122DL · Boeing 767332SDR HALA0600477Angle · crackedNR 1 ENGINE PYLON O/B SKIRT FAIRING 2ND ANGLE FWD OF AFT ENG MOUNT CRACKED PAST STOP DRILL. REMOVED CRACKED SKIRT FAIRING ANGLE, 2ND FROM FWD OF AFT ENGINE MOUNT ON NR 1 ENGINE PYLON O/B SIDE AND INSTALLED NEW ANGLE PER SRM 51-40-04 AND SRM 51-40-02.Jun 24, 2006 · N594HA · Boeing 767300
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