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.
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
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 ERAA20120091Skin Panel · crackedLEFT FINGERNAIL SHROUD SKIN CRACKED ON INBOADD AND OUTBOARD SIDE.SDR ERAA20120090Skin Panel · crackedRIGHT FINGERNAIL UPPER OUTBOARD SKIN CRACKED AT RIVET HOLE.SDR SWAA2012120710360Tail Cone · delaminatedNR 3 FLAP TRACK FAIRING DELAMINATED ON I/B SIDE (MARKED). MOD REMOVED AND REPLACED NR 1 ENGINE AFT TAIL CONE ON THE PYLON PER MM. POS: LT P/N: 65C26300-77A S/N OFF: 211607A S/N ON: WN511 CLOSING LOG PAGE: 8348308SDR EIAA20121022071Skin · crackedNR 3 STRUT CAP SKIN 2 EA FASTENER HOLES CRACKED. NR 3 STRUT CAP SKIN CRACKED FASTENER HOLES REPAIRED PER ENG DOC TEC-EVR-12-0010-10B.SDR EIAA20121022068Skin · crackedNR 1 STRUT CAP SKIN 1 EA FASTENER HOLE CRACKED. NR 1 STRUT CAP SKIN FASTENER HOLE CRACK REPAIRED PER ENGINEERING DOC. TEC- EVR-12-0009-08B.SDR ERAA20120081Skin · chafedLEFT NACELLE TOP SECTION SKIN UNDER FINGERNAIL HAS CHAFED AREA. REPAIRED IAW RD8-54194.SDR QXEA2012102001341Skin · corrodedCORROSION FOUND ON UPPER AFT NACELLE SKIN PANELS INBD AND OTBD. REMOVED CORROSION FROM UPPER AFT NACELLE INBD AND OTBD SKIN PANELS IAW SRM 51-21-00-00-02, REV 11. MIN REMAINING THICKNESS NOTED .024 REF NTM 51-00-04-910-801 PT 1 REV 7. INSPECTED BLENDS WITH HFSDR UALA2012101705946Panel · delaminatedFOUND AFT FAIRING PANEL P/N 149W5231-1 WITH TWO INCH DELAM DURING WALK AROUND INSPECTION. ROUTED TO SHOP FOR REPAIR. REMOVED AND INSTALLED AFT FAIRING PANEL P/N 149W5231-1.SDR USAA2012120600008Skin · crackedQ3 CHECK - NR 2 PYLON OUTBOARD SKIN CRACKED AT PANEL 5823R CUTOUT. REPAIRED SKIN IAW EA 131977.SDR FDEA201210153617Skin · gougedNR 3 PYLON, STATION YWN= 264 HYD CASE DRAIN PAN ADJACENT AREA LT SIDE. EXTERIOR SURFACE FOUND GOUGED. REPAIRED IAW EA 1-5450-163511. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 115.SDR UALA2012101505847Tripler · wornNR 1 PYLON LT SIDE WORN ON TITANIUM TRIPLER AT ACCESS DOOR 433CL CUTOUT. REPAIRED IAW ECRA 5431-01063.SDR USAA2012110500007Skin Panel · worn2C CHECK - 1 INCH DIAMETER HOLE WORN INTO NR 1 PYLON SKIN PANEL AT NACELLE STA 361.9, NACELLE WL 130.0. REPAIRED NR 1 PYLON SKIN PANEL AT NACELLE STA 361.9, NACELLE WL 130.0 IAW B767 SRM 51-70-10 REPAIR 4, FIG 201.SDR ERAA20120069Strap · crackedLEFT NACELLE UPPER ACCESS PANEL LANDING STRAP HAS CRACK AT RIVET FORWARD RIGHT CORNER.SDR CA121017006Skin · unknown(CAN) MAINTENANCE WHEN TROUBLESHOOTING A RECURRING PROBLEM WITH THE RUDDER BOOST, FOUND WATER LEAKING INTO THE PYLON THROUGH A VENT HOLE THAT IS THERE TO PREVENT OVERHEATING OF THE PYLON.SDR FXGA201209271273Skin · crackedNR 1 NACELLE SKIN CRACK AT FUEL DUMP OPENING EO 1273.SDR SWAA2012111509430Fairing · crackedCRACK ON AFT STRUT FAIRING LOWER POSITION OUTBOARD SIDE ENGINE 2. REPAIRED AFT STRUT FAIRING LOWER POSITION AT OUTBOARD SIDE ENGINE 2 IAW EA 1-354-150 0 REV 0 AND EO AEM-HC54-053/12 ROSDR A6WA20120920013Separator · damagedLEFT ENGINE PYLON PANEL 412DB INNER SKIN SEPARATOR HAS WEAR DAMAGE. REMOVED DAMAGED SEPARATORS LOCATED AND DRILLED NEW SERVICEABLE SEPARATORS & RUB STRIP: P/N: 601R37138-27, 601R37138-25 & 601R37138-21) INSTALLED SEPARATORS AND RUB STRIPS TO PANEL 412DB IAW CSDR A6WA20120920011Panel · damagedPANEL 412BT PYLON PANEL LEADING EDGE INNER SIDE HAS GROOVES. PANEL 412BT LEFT PYLON FOUND TO BE OUT OF LIMITS, LOCATED, DRILLED & INSTALLED NEW SERVICEABLE PANEL. P/N 601-37003-159SDR UALA2012091005075Fastener · looseREF EQ 4498 NR 1 ENGINE FOUND FASTENERS LOOSE AT THE FOLLOWING LOCATIONS NR 2, 3, 5, 6, 7, 8, 11, 12, 13, 15, 17 AND 18. REPLACED FASTENERS AT NR 2, 5, 6 AND NR 7 LOCATIONS. REF ECR CONT OF AMIS ITEM 2192017. REPLACED REMAINING FASTENERS REF ECRA 5454-01062SDR CA120907004Fitting · cracked(CAN) NR 1 NACELLE HORSE COLLAR ASSY WAS REMOVED FROM THE ACFT FOR REPAIR OF A CRACKED ANGLE, COMMON FIND. DURING REMOVAL OF THE OUTER COVER/SHROUD MAINTENANCE DISCOVERED 2 CRACKS IN FITTING, PN 85410273-103. FITTING TO BE REPLACED BEFORE RETURN TO SERVICE. SDR ASAA2012091192870Panel · looseWHILE ACCOMP TC 78472000 ENG INLET & FAN DETAIL INSPECTION. FOUND NR 1 ENG INBD LOUVER PANELS LOOSE 200 & 600 POSITIONS AFT LOOKING FWD. ACFT GROUNDED. NR 1 ENG TIGHTENED LOUVER PANELS AT 200 & 600 POSITIONS REF AMM 72-23-07. OK FOR CONT SERVICE.SDR USAA2012082900005Panel · delaminatedFLT/CHK 0641 - FOUND PANEL 423FTL DELAMINATED. REMOVED AND REPLACED PANEL 423FTL.SDR F3LA2012083100781Skin · dentedNR 1 ENGINE NOSE COWL INNER BARREL AT 9:30 POSITION HAS A DENT. REPAIRED IAW SRM 54-10-00, REPAIR 23, PARAGRAPH 2.A,B,C(1-3}, D, E(1 -2), F{1 -2), G AND H( 1-4).SDR F3LA2012083100780Skin · dentedNR 1 ENGINE NOSE COWL INNER BARREL AT 9:00 POSITION HAS A DENT, REPAIRED IAW SRM 54-10-00, REPAIR 23, PARAGRAPH 2.A,B,C(1 -3), D, E(1 -2), F( 1-2), G AND H( 1-4).SDR UALA2012082904849Panel · damagedLT ENGINE UPPER PYLON PANEL NOT FLUSH. REPAIRED PANEL IAW ECRA 5430-01932 & SRM 54-53-70.SDR USAA2012082800011Panel · deformedRON - RIGHT PYLON, OUTBOARD SIDE PANEL 482AR IS DEFORMED. REPLACED RIGHT PYLON, OUTBOARD SIDE PANEL 482AR IAW A319 AMM 54-53-11.SDR KCSA201208221176Skin · damagedNR 4 PYLON RIGHT SKIN BOTTOM SIDE DAMAGED UNDER SPRING HINGE AT NAC STA 236, W/L 150.SDR EIAA20120813060Skin · crackedSKIN CRACKED AT NR 1 PYLON FWD STRUT ACCESS PANEL NR 452AL. CRACK FOUND TO BE OUT OF LIMITS LAW SRM 54-30-01. REMOVED DAMAGE LAW SRM 51-10-01. PERFORMED HFEC OF NR 1 PYLON TRIM OUT AT FWD ACCESS PANEL CUT OUT LAW NOT MANUAL PTS/51-00-00, NO DEFECTS NOTED. SDR USAA2012092500015Doubler · crackedQ6 CHECK - CRACK IN BONDED DOUBLER FOR OPENING OF ACCESS PANEL 5823R ON NR 2 PYLON AT NAC STA 236.75, WL 127.13. REPAIRED NR 2 PYLON AT NAC STA 236.75, WL 127.13 AT OPENING OF ACCESS PANEL NR 5823R IAW B737 SRM 54-50-01-2R-2 FIG 201.SDR USAA2012091800005Doubler · crackedQ6 CHECK - CRACK ON NR 1 PYLON BONDED DOUBLER AT OPENING TO ACCESS PANEL 5723L AT NAC STA 236.75, WL 127.13. REPAIRED NR 1 PYLON BONDED DOUBLER AT OPENING TO ACCESS PANEL 5723L IAW B737 SRM 54-50-01-2R-2 FIG 201.SDR FDEA201208082936Panel · wornNR 2 PYLON CUT-OUT FOR PANEL 457CL EDGE IN CONTACT WITH LATCHES ARE WORN OUT. REPAIRED NR 2 PYLON LT ACCESS DOOR LANDING OF 457CL IAW EA 8-5450-162534, REPAIR CLASSIFED AS MAJOR.SDR UALA2012080804299Panel · damagedRIGHT ENGINE INBOARD AFT PYLON PANEL HAD HINGE PINS REMOVED SO WHEN IT WAS OPEN PANEL FELL TO FLOOR DAMAGING CORNERS OF PANEL. APPLIED REPAIR PLIES TO OUTER SIDE. WHEN CURE IS COMPLETE, WILL NEED FILLER PLIES AND LAY UP ON INNER SIDE, REF SRM 54-50-70 REPAIRSDR UALA2012081304423Skin · crackedCRACK ON 4 ENGINE PYLON BY SCREW HEAD, CRACK IS 2.5 INCHES LONG. TEMP REPAIR MADE PER MM 54-50 -99 PG 801.SDR UIEA2012091000398Access Panel · crackedCRACK AROUND THE FASTENER HOLES ON ACCESS PANEL 472FL OF NR 3 PYLON LT SIDE. REPAIR IAW EI T2012A54B-1996, REV. 00.SDR UIEA2012091000399Access Panel · crackedCRACK ON THE ACCESS PANEL 472GL OF NR 3 PYLON LT SIDE. REPAIR IAW EI NR T2012A54B-1997, REV 00.SDR UIEA2012091000400Access Panel · crackedCRACK ON ACCESS PANEL NR 482ER OF NR 4 PYLON RT SIDE. REPAIR IAW EI NR T2012A54B-1973, REV 00.SDR UIEA2012091000401Access Panel · crackedCRACK ON THE ACCESS PANEL 452ER OF NR 1 PYLON RT SIDE. REPAIR IAW EI NR T2012A54B-1970, REV 00.SDR A6WA201240804Skin · gougedLT LOWER CORE COWL INNER SKIN GOUGED 3 SPOTS, 10 GOUGED LOCATIONS ON LT LOWER CORE COWL INNER SKIN 4 FOUND TO BE WITHIN ALLOWABLE DAMAGE LIMITS AND TO 6 AREAS. REPAIRED IAW REO 601R-71-12-4122.SDR A6WA201240740Skin · dentedLT LOWER CORE COWL INNER SKIN DENTED IN MULTIPLE SPOTS. 10 DENTS LOCATIONS ON LT LOWER CORE COWL. INNER SKIN WITH FOUR REQUIRED AND 6 FOUND TO BE WITHIN ALLOWABLE DAMAGE REO.SDR IPXA12674810Skin · crackedINSPECTION TYPE: 9C, NR 2 PYLON LT STRUT SKIN CRACKED APPROX 1.5" LONG AT ACCESS PANEL NR 442AL CUTOUT. REPAIRED IAW HX RS R-54-51-37402 REV A & EO B767-5430-48154-A JUST AT ACCESS PANEL NR 442AL CUTOUT AFT UPR CORNER AREA, SKIN & DOUBLER ORIG MATL ARE CLAD 2SDR USAA2012080600005Panel · cracked2S CHECK - CRACK ON NR 2 PYLON RIGHT LATERAL PANEL LOWER AFT HOLE ELONGATED & CRACKED AT PYLON STA 4594, RIB 5. REPAIRED NR 2 PYLON RIGHT LATERAL PANEL IAW A320 SRM 54-57-11 FIG 201 & 51-42-11.SDR A6WA201240747Skin · gougedPANEL 445AB HAS NUMEROUS SMALL DENTS AND GOUGES ON INNER SKIN. REPAIR IAW REO 601R-71-12-4124.SDR UALA2012071803885Skin · damagedNR 4 ENGINE INBD CORE COWL AFT RUBSTRIP FASTENER PULLED THROUGH AT 10 O'CLOCK POSITION. REPLACED FASTENER REF:GPM 1-0-8-61.SDR KCSA201207171122Access Panel · crackedNR 2 PYLON O/B AFT MOST ACCESS PANEL HAS CRACK.SDR KCSA201207111119Skin · misrepairedIMPROPER I/B SKIN REPAIR AT NAC STA 206, AFT UPPER CUTOUT OF PYLON ACCESS.SDR KCSA201207111118Skin · misrepairedIMPROPER I/B SKIN REPAIR AT NAC STA 198, FWD LOWER CUTOUT OF PYLON ACCESS.SDR A6WA201240788Panel · chafedPYLON PANEL 422DB HAS 2EA CHAFED SEPARATION. R & R IAW SRM 51-42-06 & 51-40-11.SDR ASAA2012070792505Panel · looseNR 2 ENG FAN BLADE INSPECTION FOUND THREE LOOSE SCREWS IN NOSE COWL LOWER OTBD VENT PANEL AT 6 O`CLOCK POS (ALF) (M), POSSIBLE DAMAGE TO SCREW HOLES IN PANEL. ACFT GROUNDED. REMOVED LOOSE LOCK FASTENERS AND REPLACED WITH LOCK BOLTS IAW EA 800-71EA-09724. SDR FDEA201206192277Skin · corrodedNR 1 PYLON RT SIDE AT ACCESS DOOR 433GR CUT-OUT IS CORRODED. REMOVED SKIN & CORROSION. FOUND TO BE OUT OF LIMITS IAW SRM 54-50-01 FIG 101 DETAIL III . ORIG MAT .188 REMAINING MAT .122. RECEIVED NEW SKIN. LOCATED AND DRILLED IAW SRM 51-40-02 . INSTALLED NESDR FDEA201206192279Skin · corrodedNR 2 PYLON LT SIDE SKIN INTERNAL SURFACE BET, PP STA 144 AND 174 HAS CORROSION. REMOVED CORROSION IAW SRM 51-40-02, FOUND OUT LIMITS IAW SRM 54-50-01, PG 101 DETAIL III. ORIGINAL THICKNESS .090" REMAINING THICKNESS .060". REPAIRED NR 2 PYLON LT SID
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