JASC 5414

Service difficulty reports · 4,361

Reports filed under 5414 · Nacelle/Pylon, Plate/Skin, 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 = '5414'
  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 FDEA201206192278Skin · corrodedNR 1 PYLON RT SIDE SKIN INNER SURFACE, STA 153 - 172, HAS CORROSION. FOUND TO BE OUT OF LIMITS IAW SRM 54-50-01, FIG 101, DETAIL III. LOCATED AND DRILLED. INSTALLED NEW RT AFT SKIN AND ALL ATTACHING PARTS IAW SRM 51-40-02 AND DWG 311N5002. MAJOR REPAIR.Jun 19, 2012 · N958FD · Boeing 757236SDR ABXR2012061800053Skin · damagedNR 2 ENGINE IDG ACCESS DOOR ON OTBD CORE COWL HAS PLAY AT HINGE POINT. REPAIRED IAW EO 6771A001, REV B DATED 6/16/12, AND SOPM 20-50-03. APPROVAL ON 8110-3 DATED 6/16/12 BY DERT-710167-SW.Jun 18, 2012 · N709AX · Boeing 767231SDR DALA12001946301Panel · separatedDURING WALKAROUND INSPECTION, FOUND PYLON PANEL FROM NUMBER 3 ENG INBEDED INTO NUMBER 4 ENG LEFT FAN COWL. MAINTENANCE REPAIRED DAMAGE PER ERA 504512.Jun 14, 2012 · N661US · Boeing 747451SDR KCSA201206131109Skin · crackedNR 4 PYLON STA 211.9 INBOARD EDGE WEB SKIN CRACKED FROM RIVET HOLE APPROX 3/4 INCH.Jun 13, 2012 · N795CK · Boeing 747251BSDR NOCA06912Skin · crackedSKIN CRACKED ON LEFT NACELLE STRUT CUTOUT FOR PANEL 432AL, UPPER AFT FASTENER. REPAIRED CRACK PER ATS ER 12-02257 DATED 7-11-12 & NAA EO 767-54-042.Jun 12, 2012 · N767NA · Boeing 767324SDR REXA2012060700924Skin · damagedLT UPPER ENGINE COWL PYLON HINGE PANEL BROKEN. REMOVED AND REPLACED LT UPPER ENGINE COWL PYLON HINGE PANEL SKIN IAW SRM 51-42-06 AND 51-42-13.Jun 7, 2012 · N912XJ · Cndair CL6002B19SDR USAA2012053100011Skin · crackedC2 CHECK - CRACK ON PYLON SKIN RIGHT CROWN BETWEEN NAC STA 206 TO STA 215. REPAIRED PYLON SKIN RIGHT CROWN BETWEEN NAC STA 206 TO STA 215 IAW TYPICAL REPAIR 737-5430-10-0054.May 25, 2012 · N445US · Boeing 7374B7SDR KCSA201205231097Skin · crackedNR 4 PYLON I/B SKIN PREVIOUS REPAIR CRACKED PAST STOP DRILL AT NAC STA 197.May 23, 2012 · N795CK · Boeing 747251BSDR KCSA201205231091Skin · damagedNR 3 PYLON LT SIDE SKIN AND FIRE SEAL GOUGED AFT OF NAC STA 221.9.May 23, 2012 · N795CK · Boeing 747251BSDR AALA20120520015Skin · crackedLEFT PYLON UPPER TORQUE BOX SKIN CRACKED WHERE INTEGRATED DRIVE GENERATOR FEEDER CABLES PASS THRU. INSTALLED DOUBLER REPAIR PER AARD 54-52-01-1.May 20, 2012 · N320AA · Boeing 767223SDR A6WA201240611Skin · damagedCORE COWL 435AB INNER SKIN DAMAGED IN 5 PLACES. REPLACED DAMAGE IAW REO 601R-71-12-4114 AND CMM 71-12-01.May 19, 2012 · N437AW · Cndair CL6002B19SDR KCSA201205191080Skin · crackedNR 1 PYLON OUTBOARD SKIN IS CRACKED AT NAC STA 197.May 19, 2012 · N791CK · Boeing 747251FSDR FDEA201205161822Skin · gougedNR 2 PYLON SAIL FAIRING LOWER SKIN AFT SURF HAS CHAFE MARKS AND 2EA GOUGES. DAMAGE FOUND OUT OF LIMITS IAW SRM 54-50-70 FIG 105, FIG 101, DETAIL IV. REPAIRED IAW EA F-5450-159925.May 16, 2012 · N962FD · Boeing 7572G5SDR FDEA201205151813Skin · corrodedLEFT PYLON RT SIDE BETWEEN PP STA 176 TO PP STA 144 INTERNAL SKIN WITH CORROSION.May 15, 2012 · N962FD · Boeing 7572G5SDR A6WA201240535Panel · crackedRT ENGINE PYLON PANEL 422AB HAS CRACKED SEAL RETAINER. REMOVED UNSERVICEABLE RT ENG PYLON PANEL 422AB SEAL RETAINER AND INSTALLED SERVICEABLE SEAT RETAINER IAW SRM 51-42-06.May 11, 2012 · N406AW · Cndair CL6002B19SDR A6WA201240548Panel · crackedPANEL 412AT CRACKED. REMOVED UNSERVICEABLE RETAINER & SEAL. REPLACED WITH SERVICEABLE RETAINER AND SEAL IAW SRM 51-40-11, 51-42-06, AMM 54-63-01.May 10, 2012 · N403AW · Cndair CL6002B19SDR UALA2012051002676Skin · wornDURING C CHECK FOUND OTBD PYLON CUTOUT FOR PNL 433CL, 4 LATCHES HAVE WORN INTO PYLON SKIN. REPAIRED PER EVA UA-EVA 80249. HFEC INSPECTED PER NDT 51-00-01 PT 6, NO CRACKS NOTED.May 9, 2012 · N788UA · Boeing 777222SDR FDEA201205091773Skin · crackedNR 1 ENGINE AFT PYLON LOWER HORIZONTAL SKIN BETWEEN RIB 18 & 19 HAS 2 EA 1" CRACKS EXTENDING FROM HYD DRAIN PASS THRU FITTING. REMOVED AND REINSTALLED HYD PASS THRU FITTINGS & LINES TO FOM IAW AMM 29-00-00-04. R & R CRACKED WEB SUPPORT IAW SRM 51-40-21. REMay 9, 2012 · N656FE · Airbus A300F4605RSDR UALA2012051002677Tripler · damagedPYLONS SKINS TITANIUM TRIPLERS HAVE WEAR DAMAGE, REPAIRED IAW ECRA 5431-01056.May 8, 2012 · N788UA · Boeing 777222SDR FDEA201205041733Skin · crackedNR 1 ENGINE PYLON LT SIDE LOWER SKIN PANEL CRACKED POSITION NEAR AFT ENGINE MOUNT. REPAIRED IAW SRM 51-40-21 AND SRM 54-56-10 C2. THE REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.May 4, 2012 · N806FD · Airbus A310324SDR FDEA201205041732Skin · crackedNR 1 ENGINE PYLON RT SIDE LOWER SKIN PANEL CRACKED POSITION NEAR AFT ENGINE MOUNT. REPAIRED IAW SRM 51-40-21 AND SRM 54-56-10 C2. THE REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.May 4, 2012 · N806FD · Airbus A310324SDR FDEA201205031726Skin · chafedLEFT PYLON AFT OTBD LWR CORNER CHAFED, COMPLIED WITH EA F-5450-160554. CAT "A" MAJOR REPAIR.May 3, 2012 · N989FD · Boeing 757231SDR UALA2012050102578Skin · wornNR 1 PYLON LOWER SKIN WORN, AS DEEP AS .020 ALONG ENTIRE WIDTH OF PYLON. LOCATED 12 INCHES AFT OF AFT ENGINE MOUNT. BLENDED AREA. AREA LOCATED 5.125 AFT OF RIB 5. INSTALLED DOUBLER RPR PER EC-RA 5451-01084.May 1, 2012 · N454UA · Airbus A320232SDR C77A20120502021Access Panel · erodedACCESS PANEL 419KL HAS ONE SCREW HOLE THAT SCREW PULLED THRU. REAM THE HOLE MAINTAINING ED IAW ETD, BOND COUNTERSUNK WASHER NAS1169 TO THE ACCESS PANEL ON WO 485382-412 IAW ETD 2012-170-006100 AND EO EA E175-54-095 REV. IR WO 557505.May 1, 2012 · N625CZ · Emb ERJ170200LRSDR DALA1234230690Panel · damagedNR 1 NACELLE PANEL 431AT DAMAGED. ACCOMPLISHED PERMANENT REPAIR PER SRM 54-31-01 PG 103 FIG 101.Apr 30, 2012 · N690DL · Boeing 757232SDR CA120502007Skin · punctured(CAN) DURING A SCHEDULED NR 1 ENGINE CHANGE, THE UPPER CORE COWL WAS FOUND WITH A1" PUNCTURE IN IT. INVESTIGATION REVEALED THAT THE CORE COWL WAS IN CONTACT WITH THE TOP OF THE OIL TANK LEVEL SENSOR ON THE REMOVED ENGINE. A NEW CORE COWL WAS INSTALLED ON THE Apr 29, 2012 · Cndair CL6002B19SDR FDEA201204271657Skin · crackedNR 2 NACELLE SKIN UPPER EDGE AT AFT HINGE IS CRACKED. CUT OUT DAMAGED AREA AND INSTALLED FILLER AND REPAIR DOUBLER IAW EA F-7111-159923. MAJOR REPAIR.Apr 27, 2012 · N989FD · Boeing 757231SDR V0XR2012042700006Skin · dentedDENT ON LT SIDE OF OF RT NACELLE AT XN=72.0 AND ZN=1.0. DENT ON COWL ASSY IS LOCATED 6.25" FROM TOP EDGE OF DOOR AND 8.25" FROM FORWARD EDGE. DENT IS MEASURED AT 0.015 DEEP AND 0.700 DIAMETER AND FOUND TO BE IN LIMITS WITH SRM 54-00-16 AND REPAIR DWG 8-71-885Apr 27, 2012 · N842EX · Dhav DHC8106SDR C77A20120426019Skin · damagedRT PYLON PANEL 429YR HAS A WORN ELONGATED ATTACHMENT HOLE. REAMED THE HOLE ROUND, AND BONDED A NAS1169C10 DIMPLE WASHER IAW ETD 2012-170-005581 AND EA E175-54-094.Apr 22, 2012 · N624CZ · Emb ERJ170200LRSDR UALA2012042302437Panel · erodedNR 3 ENG PYLON UPPER FWD PANEL HAS EROSION ON INBRD LEADING EDGE OF PANEL. REPAIRED & PRIMED, PAINTED.Apr 21, 2012 · N122UA · Boeing 747422SDR FDEA201204191487Skin · misrepairedNR 2 PYLON EXTERIOR APPROX STA Y = 2334 FOUND MISREPAIRED. REPAIRED IAW EO E1-5100-7-5001B PT1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.Apr 19, 2012 · N577FE · Doug MD11FSDR UALA2012042002354Panel · missingNR 1 ENG PYLON MISSING ROUND PANEL ON THE INBD SIDE (436AR). REPLACED MISSING PANEL WITH NEW PANEL.Apr 18, 2012 · N653UA · Boeing 767322SDR A6WA201240471Skin · chafedLEFT UPPER CORE COWL HAS A CHAFED AREA, FWD LOWER CORNER CHAFE MARK IS APPROX 10" LONG. REPAIRED LT CORE COWL IAW REO 601R-71-12-4106.Apr 17, 2012 · N443AW · Cndair CL6002B19SDR UIEA2012051400230Skin · crackedCRACKED NR 1 PYLON RT 452ER PANEL CUT OUT SKIN EDGE CRACK AT NAC STA 228. REPAIRED DAMAGE AREA IAW SRM 54-50-01, REPAIR 2, REV 20.Apr 16, 2012 · N747BC · Boeing 7474J6SDR UIEA2012050700192Skin · crackedCRACKED NR 1 PYLON, RT 452ER PANEL CUT OUT SKIN EDGE CRACKED AT NAC STA 228. REPAIR DAMAGE AREA IAW SRM 54-50-01, REPAIR 2, REV 20.Apr 16, 2012 · N747BC · Boeing 7474J6SDR USAA2012041900007Skin · crackedC1 CHECK - CRACK IN RIGHT PYLON SKIN AT PANEL 5828R OPENING AT INBOARD AFT CORNER. REPAIRED RIGHT PYLON SKIN AT PANEL 5828R OPENING IAW TYPICAL REPAIR 737-5430-10-0054.Apr 16, 2012 · N442US · Boeing 7374B7SDR USAA2012042600018Skin · crackedC6 CHECK - CRACK IN NR 2 PYLON SKIN DOUBLER AT INBOARD SIDE OF ACCESS PANEL 5728L CUTOUT AT NAC STA 206.5-215.1. REPAIRED SKIN DOUBLER AT INBOARD SIDE OF ACCESS PANEL 5728L CUTOUT AT NAC STA 206.5-215.1 ON NR 2 PYLON IAW TYPICAL REPAIR T/R 737-5430-10-0054.Apr 11, 2012 · N444US · Boeing 7374B7SDR USAA2012042600017Skin · crackedC6 CHECK - CRACK IN NR 2 PYLON SKIN DOUBLER AT INBOARD SIDE OF ACCESS PANEL 5828R CUTOUT AT NAC STA 206.5-215.1. REPAIRED SKIN DOUBLER AT INBOARD SIDE OF ACCESS PANEL 5828R, CUTOUT AT NAC STA 206.5-215.1 ON NR 2 PYLON IAW TYPICAL REPAIR T/R 737-5430-10-0054.Apr 11, 2012 · N444US · Boeing 7374B7SDR ZKFR2012040900001Skin · delaminatedDURING ENGINE CHANGE, CORE COWL SEGMENT FOUND DELAMINATED. MFG HAS A REPAIR FOR THIS PROBLEM BUT UNFORTUNATELY THE EXTENT OF DAMAGE TO THIS CORE COWL IS BEYOND ALL LIMITS OF REPAIR. THE REPAIR IS USUALLY FOR A SMALL AMOUNT OF LIFTING AT THE CORNERS OF THE BOApr 9, 2012 · N261PA · Braero HAWKER1000SDR FDEA201204091313Skin · crackedNR 1 NACELLE STRUT PYLON STRUCTURE INBD ACCESS HOLE CUT-OUT INNER EDGES FOR PANEL NR 433LR FOUND WITH 1" CRACK AT PPSTA 185.0. AREA TRIMMED AND REPAIR CARRIED OUT IAW EA F-5450-158034, PART 1. REPAIR IS CLASSIFIED AS MAJOR.Apr 9, 2012 · N959FD · Boeing 757236SDR UALA2012040602136Skin · dentedNR 2 ENG NOSE COWL HAS OUT OF LIMIT DENT AT 12 O'CLOCK POSITION. REPLACED NOSE COWL ASSY.Apr 6, 2012 · N576UA · Boeing 757222SDR USAA2012051400025Skin · crackedQ1 CHECK - 2 CRACKS ON RIGHT NACELLE SKIN BETWEEN NAC STA244.5 TO NAC STA250.4, BETWEEN NAC STA126.0 TO NAC STA126.4. REPAIRED RIGHT NACELLE SKIN BETWEEN NAC STA244.5 TO NAC STA250.4, BETWEEN NAC STA126.0 TO NAC STA126.4 IAW EA 130873.Apr 6, 2012 · N427US · Boeing 7374B7SDR FDEA201204061276Skin · crackedNR 1 ENGINE PYLON, AFT LOWER FAIRING, LOWER SKIN CRACKED 2 INCHES INCHES LONG, AROUND HYD RESERVOIR PRESSURIZATION LINE HOLE CUT OUT BETWEEN PYLON RIB 19 - 20. REMOVED CRACKED WEB ASSY AND INSTALLED NEW WEB ASSY ON NR 1 ENGINE LOWER AFT PYLON AREA BETWEEN RIB Apr 6, 2012 · N670FE · Airbus A300F4605RSDR UALA2012040602134Skin · wornNR 1 PYLON LOWER SKIN WORN AS DEEP AS .020 ALONG ENTIRE WIDTH OF PYLON. LOCATED 12" AFT OF AFT ENG MOUNT. BLENDED AREA. AREA LOCATED 5.125 AFT OF RIB 5. OKAY TO CF PER SRM. NEEDS TO BE RE-EVALUATED AND REPAIRED AT NEXT "C" CHECK OR 4500 FLIGHT CYCLES OR 20Apr 5, 2012 · N454UA · Airbus A320232SDR UALA2012040502099Skin · wornNR 2 PYLON CUT OUT FOR ACCESS DOOR 443CL INBD SIDE SKIN TRIPLER P/N 311W3453-5 WORN AT PLATE LATCH CONTACT AREAS. REPAIRED ON DOCK WU Q1849X REQUIRES REPETITIVE INSP FOR WEAR EVERY 30 DAYS AND MUST BE PERMANENTLY PAIRED BY 9-22- 2010 PER UA EVA 73615. REPAIRApr 3, 2012 · N782UA · Boeing 777222SDR EIAA20120403034Skin · damagedNR 2 PYLON RT FRAMES STA 259 AND 234, RT SKIN BELOW LOUVER CUTOUT ARE HEAT DAMAGED. REMOVED DAMAGE, FABBED REPAIR PARTS AND INSTALLED PER ECRA 489-54-025-2.Apr 3, 2012 · N489EV · Boeing 747230BSDR EIAA20120403033Skin · damagedNR 4 PYLON RT BETWEEN FRAMES STA 248 AND 259, RT INTERNAL SKIN AT STIFFENER 2 TO 4 AND FRAMES HEAT DAMAGED. REMOVED DAMAGE, FABBED REPAIR PARTS AND INSTALLED PER ECRA 489-54-025-2.Apr 3, 2012 · N489EV · Boeing 747230BSDR EIAA20120403032Skin · damagedNR 2 PYLON RT BETWEEN FRAMES STA 259 AND 270, RT SKIN BETWEEN STIFFENERS 2 AND 3 HEAT DAMAGED. REMOVED DAMAGE, FABBED REPAIR PARTS AND INSTALLED PER ECRA 489-54-025-2.Apr 3, 2012 · N489EV · Boeing 747230BSDR EIAA20120403031Skin · damagedNR 1 PYLON RT BETWEEN FRAMES STA 234 AND 270, RT INTERNAL SKIN BETWEEN STIFFENERS 2 AND 4 HEAT DAMAGED. REMOVED DAMAGE, FABBED REPAIR PARTS AND INSTALLED PER ECRA 489-54-025-2.Apr 3, 2012 · N489EV · Boeing 747230BSDR EIAA20120403030Skin · damagedNR 3 PYLON RT BETWEEN FRAMES STA 234 AND 248, RT INTERNAL SKIN AT STIFFENER 3 AND STIFFENER HEAT DAMAGED. REMOVED DAMAGE, FABBED REPAIR PARTS AND INSTALLED PER ECRA 489-54-025-2.Apr 3, 2012 · N489EV · Boeing 747230B
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