JASC 5400
Service difficulty reports · 1,907
Reports filed under 5400 · Nacelle/Pylon Structure, 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 = '5400' 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 = '5400' 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 SWIA20230815004Unknown · dentedREMOVED LH LOWER FAN COWL DOOR TO FACILITATE PERMANENT REPAIR FOR DENT ON LT ENG COWL DOOR ASSY (FILED CLOSED)INSTALLED NEW LH FAN COWL DOOR SEE CP 27023226-1 FOR MX PERFORMED AND PARTS INFOSDR CALA2023081402505Access Door · missingDURING ETOPS PDSC, FOUND #2 ENGINE RT SIDE STRUT ACCESS DOOR 446BR MISSING. LOCATION PIC ADDED. CDL 54D REQUESTED. DEFERRED IAW CDL 54D. MISSING INSTALLED NEW #2 ENGINE RT SIDE STRUT ACCESS DOOR PANEL 446BR PER AMM 20-11-00 AND AIPC 54-53-01-17 ITEM 647.SDR P5CA2023080300063Unknown · unknownLIGHTING STRIKE ON UPPER FUSELAGE OUTER SKIN AT STA.396.75 AND 5" BELOW STGR 3RH(<P>LIGHTNING STRIKE WAS REPAIRED ON UPPER FUSELAGE OUTER SKIN AT STA 396 AND 5" BELOW STR 2 RH </P>)SDR P5CA2023080900071Unknown · unknownCRACK ON PYLON #1 FWD UPPER SPAR WEB BETWEEN NAC STA 221.25 - 237.5, POWER FEEDER CABLE CUTOUT(<P>REPAIR WAS ACCOMPLISHED BY MXA EO TRE6754178 (SR ID 4-5858404778) <SPAN>AND BOEING SB 767-54-0090</SPAN></P>)SDR CALA2023080702432Panel · damagedPDA 2 REF LOG PAGE 5354332, AND ECRA 5450-02357, THE AIRCRAFT ARRIVED WITH PANEL 110 MISSING. MISSING PANEL PLACED ON DIP FOR 25 FLT HOURS. MISSING FLEX SEAL PANEL 110 HAS BEEN PLACED ON DIP. REMOVED AND REPLACED CRACKED METAL SEAL PANEL. NO FURTHER DEFECTS NSDR IXXA2023080103Acoustic Panel · delaminated#2 PYLON O/B STRUT FAIRING SKIN ( ARROWHEAD PANEL ) DELAMINATEDSDR SWAA2023073183566Fairing · cracked#2 ENGINE PYLON AFT STRUT SUPPORT FAIRING ASSY. CRACKED.<[01] REMOVED CRACKED AFT STRUT SUPPORT FAIRING ASSY. PER SRM 51-40-02.;[02] LOCATED AND DRILLED NEW AFT. STRUT SUPPORT FAIRING ASSY. PER SRM 51-40-05.;[03] REMOVED AND REPLACED PYLON AFT. STRUT FAIRING BSDR CALA2023080202414Fastener · missingPDA 3 LEFT ENG O/B PYLON PANEL HAS 2 EACH FASTENERS MISSING. SEE PHOTO. ADDED PHOTO. ADDED PHOTO. REINSTALLED 2 EACH SCREWS AS REQUIRED.SDR IPXA2023072893758Fairing · crackedINSPECTION TYPE:CPANEL 413BL HAS A CRACK IN CORNER UNDER THE SEAL.REPAIRED CRACK IAW SRM 54-52-51.SDR FDEA202307271315Unknown · unknownLEFT HAND PYLON - FOUND EXISTING REPAIR AT LOWER SPAR BETWEEN RIB 9 AND RIB 10 REQUIRES EVALUATION FOR CONFORMITY TO APPROVED DATA. THE EXISTING REPAIR ON LT PYLON LOWER SPAR BETWEEN RIB 9 & RIB 10 WAS EVALUATED & FOUND IN CONFORMITY WITH DWG: 41R54600029 SDR FDEA202307271308Intercostal · crackedEMPENNAGE - FROM #2 ENGINE INTAKE DUCT ACCESS PANEL FOUND RIGHT HAND INTERCOSTAL AFT EDGE CRACKS 1.8" BETWEEN STATION 2161 REAR CENTER SPAR TO REAR SPAR AREA. EMPENNAGE RIGHT HAND INTERCOSTAL AFT EDGE CRACKED 1.8" BETWEEN STATION 2161 REAR CENTER SPAR TO RSDR SWI2023F00376Unknown · crackedR/H UPPER TRANSCOWL A-BRACKET CRACKED (C-CHECK RO 9/13/2023) REMOVED DAMAGED STAND-OFF ANGLE (A-BRACKET) & INSTALLED NEW STAND-OFF ANGLE P/N CN624-2082-201 ON R/H UPPER TRANSCOWL, REF. REO 670-54-21-971, REV. A, 2017-05-11. COMPLIED WITH SKY CARD 51-900SDR SWI2023F00375Unknown · chafedR/H UPPER TRANSCOWL COAMING CHAFED THROUGH DISHING AND SKIN (C-CHECK RO 9/13/2023) REPAIRED R/H UPPER TRANSCOWL REF MHIRJ REO 670-54-21-1207 REV A 2015-08-27, AND REO670-54-21-1567 REV -- 2023-07-31.COMPLIED WITH SKYCARD 51-900-1002SDR SWIA20230726Unknown · crackedLEFT OVERWING APRON HAS SIGNS OF FRETTING. (C-CHECK RO 10/29/2023) REMOVED FRETTING AT LEFT OVERWING APRON REF CRJ200 SRM 51-12-00. AREA WAS BLENDED AND NDT PER REO 601R-53-41-341 REV C DATE 2009-JUN-10 PERMANENT REPAIR (REF ITEM 1A AND 2A), FROM FS 516.8SDR CALA2023072602338Screw · missingPDA 3 UPPER PYLON PANEL ON #1 ENG O/B HAS 1 EACH MISSING SCREW. REPLACED 1 EACH SCREW ON #1 ENG O/B PYLON.SDR IPXA2023072893757Angle · crackedINSPECTION TYPE:4C#3 PYLON UPPER WIRE HARNESS SUPPORT HAS A CRACKED ANGLE AT THE AFT SIDE ABOVE PRECOOLER.REMOVED, FABRICATED AND REPLACED ANGLE AT THE #3 PYLON AT THE AFT SIDE ABOVE PRECOOLER IAW SRM 54-05-41 AND DWG AUB7564. (MINOR)SDR ABXA20230814167Attach Fitting · damagedDURING C1 MAINTENANCE CHECK AT HAECO AMERICAS, MAINTENANCE REPORTED NO. 1 PYLON UPPER SURFACE ATTACH HOOKS ((313T1105-5 AND 313T1105-6) HAS WORN DAMAGES. THE -5 FITTING HAS 2 DAMAGES OF 0.032% AT LOWER AND APPROX. 0.025% AT THE UPPER. THE -6 FITTING HAS 0.061 SDR AALA202307284582Spigot · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT HAND PYLON LOWER SPIGOT FITTING BORE BETWEEN PYLON STATIONS 6793 AND 7063, BETWEEN PYLON RIBS 4 AND 5. REPLACED LOWER SPIGOT FITTING PER SRM 54-51-12.SDR AALA202307288369Spigot · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT HAND PYLON LOWER SPIGOT FITTING BORE BETWEEN PYLON STATIONS 6793 AND 7063, BETWEEN PYLON RIBS 4 AND 5. REPLACED LOWER SPIGOT FITTING PER SRM 54-51-12.SDR DALA2023072005883Unknown · unknownSHIP 3166 DAMAGE TO WING TO BODY FAIRING RT. SIDE PANEL 192EB. AT BOTTOM OF FASTENER EDGE. CORRECTIVE ACTION: PERFORMED REPETITIVE INSPECTION OF SPEED TAPE PER SRM 51-77-12-911-001. (8675608)SDR FDEA202307141216Shear Tie · cracked1EA ATTACH CLIP IS CRACKED AT #2 PYLON AFT BULKHEAD ON INBD SIDE AT APPROX NAC STA 295, JUST BELOW INBD MID-SPAR FITTING REMOVED AND REPLACED #2 PYLON, INBOARD SHEAR TIE AT NAC STA 297 IAW BAC DWG 313T2310, SHEET 95, REVISION -SDR FDEA202307121203Bracket · cracked#1 PYLON/NACELLE, I/B SIDE, ACCESSED BY PANEL 437BR, HYD. RESERVOIR BAY FWD BULKHEAD UPPER CORNER ATTACH BRACKET CRACKED REMOVED AND REPLACED ATTACH BRACKET LOCATED ON #1 PYLON/NACELLE, I/B SIDE, ACCESSED BY PANEL 437BR, HYD. RESERVOIR BAY FWD BULKHEAD UPPSDR CALA2023072102305Fastener · missingPDA 3 #2 ENGINE AFT PYLON OUTSIDE STRUT FAIRING PAN ASSEMBLY MISSING ONE FASTENER. ONE MISSING FASTENER. SEE DETAIL III AND IV. CONFIRMED ONE MISSING FASTER. NO PART AVAILABLE GIGJL. AS PER SRM 51-10-05-2R-1 PARAGRAPH 4, ALL CONDITIONS ARE PERMITTED FOR DIP 5SDR FDEA202307101195Fitting · cracked#1 PYLON AFT FAIRING, INBD SIDE FRAME, NAC STA 380, MID ATTACH CLIP, IS CRACKED. REMOVED AND REPLACED ATTACH CLIP (BRACKET) LOCATED ON #1 PYLON AFT FAIRING, INBD SIDE FRAME, NAC STA 380, PER BOEING DWG 313T2303, REV -SDR FDEA202307101194Fitting · cracked#2 PYLON AFT FAIRING, OTBD SIDE, FRAME ATTACH CLIP, AT APPROX. NAC STA 380, IS CRACKED REMOVED AND REPLACED ATTACH CLIP LOCATED ON #2 PYLON AFT FAIRING, OTBD SIDE, FRAME ATTACH CLIP, AT APPROX. NAC STA 380, PER BOEING DWG 313T2303, REV -SDR IXXA2022071004Cowling · damaged#2 ENGINE I/B CORE COWL HAS A HOLE IN THE UPPER AFT EXTERIOR NAC 220-225SDR DALA2023071005550Unknown · unknownSHIP 3118 CORROSION SPIGOT FITTING RECEPTACLE ON BORE ON LH PYLON. CORRECTIVE ACTION: REPLACED SPIGOT LOWER FITTING ON LH PYLON AS PER A319 SRM 54-51- 12-300-001. (2855459)SDR IPXA2023072433614Doubler · corrodedFAULT- #1 ENGINE PYLON OUTBD SKIN, INNER SURFACE FWD OF VENT PANEL OPENING HAS EXFOLATION CORROSION. DOT 8-001. CERTIFIED ALL ACTION STEPS ON THIS NON-ROUTINE CARD WERE ACCOMPLISHED AND COMPLETED. INSPECTION COMPLETESDR IPXA2023072433661Pylon · damagedFAULT- #2 ENGINE PYLON OUTBD SKIN, INNER SURFACE HAS EXFOLATION CORROSION. DOT 8-005 AND IN RED. REVIEWEDSDR HYIA20230707001Fitting · crackedWHILE PERFORMING LIGHTED BORESCOPE INSPECTION PROCEDURE AS OUTLINED IN TEXTRON MEL-54-02R3 TO SATISFY AD2017-10-09, A CRACK WAS VISUALLY IDENTIFIED ON THE INBOARD VERTICAL LEG OF THE LEFT HAND OUTBOARD NACELLE FITTING. THIS CRACK MEASURES APPROXIMATELY .138 INSDR IPXA2023072586340Pylon · damagedFAULT: #2 ENG I/B FWD PYLON SKIN WITH CORROSION AT OUTSIDE SKIN. DOT 07308-001 VERIFIED JOB COMPLETE AND ACCOMPLISHED IAW UPS EO-87576-REQ1 AND VT MAE 757-5450-27-A3280 REV-SDR NACA2023070700009Unknown · unknownNO.2 PYLON O/B AFT FAIRING ACCESS PANEL FWD HINGE ATTACHMENT FITTINGS FOUND CORROSION. REMOVED AND REPLACED THE ATTACHMENT FITTING AT #2 PYLON O/B AFT FAIRING ACCESS PNL FWD HINGE IAW SRM 51-40-02 REVISION NO.122 APR 15/2023.SDR SWAA2023083075852Fastener · loose#2 ENGINE AFT FAIRING LOWER HEAT SHEILDS HAVE LOOSE FASTENERS ON O/B SIDE<[01] REMOVED AND REPLACED WORN & LOOSE FASTENERS IN #2 ENGINE AFT FAIRING LOWER HEAT SHIELD ACCESS PANELS O/B SIDE PER AMM 54-52-08-010-801; AMM 54-52-08-010-802 AND AMM 20-60-11-201; 1 SDR IXXA2023070802Doubler · damagedPREVIOUSLY INSTALLED DOUBLER ON THE INNER SKIN OF THE #1 ENGINE O/B FAN COWL WAS FAOUND TO HAVE RUBBING DAMAGE. REMOVED AND REPLACED DOUBLERSDR IPXA2023061793461Skin · gougedINSPECTION TYPE:C#2 ENGINE OB EXHAUST CONE AREA HAS A GOUGEREPAIRED AREA IAW PW SRM 54-40-00SDR DALA2023061604931Unknown · unknownSHIP 195 #1 ENG LT SIDE NACELLE STRUT ACCESS DOOR MISSING. CORRECTIVE ACTION: DEFERRED / PLACARDED PER B767-300 CDL 54-53-02, DISPATCH APPROVED, NO M PROC (4789525)SDR CALA2023061601891Panel · missingPILOT REPORTS PNL MISSING FROM #2 ENGINE. ADDED PHOTO REMOVED AND REPLACED #2 ENGINE LEFT HAND COWLING IDG ACCESS DOOR ASSY PER IPC 71-11-02 DOOR OPS CHKS NORMAL MANUAL REFER TASK 71-11-04/401 AND 71-11-04-820-802-FOOSDR UIEA2023060900623Unknown · unknownDENT ON ENG #1 PRIMARY EXHAUST OUTER SKIN AT NAC STA 341.67 BETWEEN 4/5 O'CLOCK(<P>DENT WAS EVALUATED AND FOUND WITHIN ALLOWABLE LIMITS IAW B767-300 SRM 54-42-30-1A-1 A.D. 1 FIG 101 SHEET 3 NOTE N DETAIL VIII REV 122 15 APR 23. DENT WAS ADDED ON DENT LOG DAMAGSDR GTIA2023060937249Spar · damagedPYLON #2 LOWER SPAR CNA ANTI-CHAFFING PLATE REPAIR. RAF01 2998992-1 CREATED.-VERIFIED NR # 5001240577-0050 AND TC # 1004012741-0010. REPAIR HAS BEEN ACCOMPLISHED AS PER SPIRIT EA 5451-2316 WITH REINSPECTION REQUIREMENT AT 49,000FC/61,200FH FROM ADL/REPAIR EMBOSDR GTIA2023060937250Spar · damagedPYLON #1 LOWER SPAR CNA ANTICHAFTING PLATE REPAIR. RAF01 2998991-2 CREATED.-VERIFIED NR #5001240778-0030 AND TC #1004012742-0010. REPAIR HAS BEEN ACCOMPLISHED AS PER SPIRIT EA 5451-2315 WITH REINSPECTION REQUIREMENT AT 49,000FC/61,200FH FROM ADL/REPAIR EMBODIMSDR GTIA2023060937251Structure · gougedDURING HMV FOUND PYLON #1 BTW RIB 8-9 I/B WITH A GOUGE RAF # 2998990-01 OPEN.-VERIFIED NR #5001240972-0010 AND TC #1004009463-0010. REPAIR HAS BEEN DONE AS PER SPIRIT EA 5452-2314 REV. 00.SDR HNAA2023062800239Unknown · unknownE980072 RH PYLON FWD YOKE UPPER FLANGE AFT FASTENER HOLE HAS RELEVANT INDICATION DURING HFEC ROTOSCOPE INSPECTION. PERFORMED BUSHING REPAIR TO RH PYLON FWD YOKE UPPER FLANGE AFT FASTENER HOLE IAW SB145-54-0008 AND EO1-53-23-0160.SDR HNAA2023062800238Unknown · unknownE980070 LH PYLON FWD YOKE UPPER FLANGE AFT FASTENER HOLE ELONGATED. PERFORMED BUSHING REPAIR TO LH PYLON FWD YOKE UPPER FLANGE AFT FASTENER HOLE IAW SB145-54-0008 AND EO1-53-23-0159.SDR HNAA2023062600212Unknown · unknownE980070 LH PYLON FWD YOKE UPPER FLANGE AFT FASTENER HOLE ELONGATED. PERFORMED BUSHING REPAIR TO LH PYLON FWD YOKE UPPER FLANGE AFT FASTENER HOLE IAW SB145-54-0008 AND EO1-53-23-0159.SDR HNAA2023062600208Unknown · unknownE980072 RH PYLON FWD YOKE UPPER FLANGE AFT FASTENER HOLE HAS RELEVANT INDICATION DURING HFEC ROTOSCOPE INSPECTION. PERFORMED BUSHING REPAIR TO RH PYLON FWD YOKE UPPER FLANGE AFT FASTENER HOLE IAW SB145-54-0008 AND EO1-53-23-0160.SDR IXXA2023060607Unknown · unknown#1 PYLON, I/B SIDE, SUPPORT ANGLE CRACKED IN HYD BAY DOOR FWD HINGE CUTOUT.SDR SWAA2023060855662Fairing · cracked#2 ENGINE PYLON TIP FARING IS CRACKED<[01] C/W EA 23-154-01804SDR IXXA2023062800001Angle · cracked#2 PYLON FWD TORQUE BOX, I/B AFT UPPER CLOSE OUT ANGLE CRACKED, VIEWED THROUGH ACCESS 446ARSDR DALA2023060604555Unknown · unknownCORROSION ON CHORD ANGLE AT AFT PRESSURE BULKHEAD LOWER AREA (FWD FACE) STA Y=1053 BTW LONG 28LH-28RH AT AFT CARGO COMPARTMENT (C2). SUMMARY OF NRC 00208: CORROSION LEVEL 2. ANGLE AT AFT PRESSURE BULKHEAD LOWER AREA (FWD FACE) STA Y=1053 BTW LONG 28LH-28RH WERSDR CALA2023060201745Nose Cowl · damagedBIRD STRIKE ON #2 ENG NOSE COWL 9:00 ALF AND RT KRUEGER FLAP. 2ND BIRD STRIKE ON LT KRUEGER FLAP AND FIXED LANDING LIGHT. LT LOWER FUSELAGE NOSE LANDING GEAR. RT RAM AIR INTAKE. #2 ENG INNER NOSE COWL. RT MLG, PARTIALLY CLEANED. LOWER RT WING I/B OF #2 ENG. AC
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